20030813000082003081300008NE 2003 8 13 HEEA088652 220030801A74219550175400 IGNITER AEROSPAS355 AS355* EU TMECA ARRIELARRIEL2B NE ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03970AE 3235 IGNITER WORN TO LIMITS. TO BE SENT TO VENDOR. 1G72 3U3 U H11EU E00054EN 20030813000282003081300028SW 2003 8 13 HEEA088582 120030804A6230 BEARING BELL 412 412 1182202SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L A2454 33006 BEARINGS WORN. SHOP REPAIR. 1G72 4U H4SW 20030813000492003081300049NM 2003 8 13 2003UALA00463 120030530A3350 LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29566UA 26670 LEFT AFT OFF-WING EMERGENCY SLIDE LIGHT, AFT OF AFT OVERWING HATCH IS INOPERATIVE. RELAMPED LIGHT. 2L72 4F4 FRTA2NM E17NE 20030813000582003081300058NM 2003 8 13 UPS03440830 120030521A5740 FITTING BOEING747 747200 1384847NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, RT WING REAR SPAR BS 1241 KICK FTG HOLE-D FOUND CRACK AT KICK FTG APPROX 0.030 INCH RUNNING I/B. HOLE-D REPAIRED AS PER RS R57-12-35029 AND EO B747-5710-18862-A. 2L74 4F RTA20WE 20030813000632003081300063NM 2003 8 13 UPS03440835 120030518A5320 FLOOR SUPPORT BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 BULK CARGO STA 1920-1940 LBL 15 FLOOR SUPPORT STRUCTURE UPPER AND LOWER SURFACE CORRODED. BULK CARGO STA 1920-1940 LBL L5 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20. CORROSION BLEND OUT (0.020 INCH X 1.25 INCH X 6 INCH). 2L74 4F RTA20WE 20030813000692003081300069SO 2003 8 13 SWIA200312081 120030606A315080055711 WARNING SYSTEM EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07235SW 120310 FIRE BELL WENT OFF WITHOUT ANY MAP LIGHTS INDICATION WHILE APU WAS RUNNING ON THE GROUND AFTER 5 MIN. REPLACED AURAL WARNING UNIT WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N OFF 0411. 2L72 4T RTA31SO 20030813000812003081300081NM 2003 8 13 2003UALA00467 120030401A5754114W426012 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 9 LE SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29780UA 26944 T/E WEDGE DELAMINATED, SLAT NR 9. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED & REINSTALLED T/E WEDGE. SLAT OVERHAULED. 2L72 4F4 FRTT0001SE E46NE 20030813000902003081300090NE 2003 8 13 2003UALA00490 220030611A7320 FMU AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE FAILED A UALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP29437UA 655 NR 1 ENGINE EXPERIENCED A FLAMEOUT. REPLACED FMU. REMOVED FMU DISASSEMBLED AT OEM, REVEALING A BUILD ERROR IN THE SPILL VALVE SLEEVE. 2L72 4F4 FRTA28NM E40NE 20030813000942003081300094NM 2003 8 13 UPS03240848 120030613A2612 FIRE DETECTOR BOEING727 72725C 138400HNM MLG WW MALFUNCTIONED A IPXAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO01951UP 19850 AIR TURNBACK FOR WHEEL WELL FIRE INDICATION IN FLIGHT ALL CHECKLIST COMPLIED WITH DEF M261369. INSPECTED TIRES, BRAKES, WHEEL ASSEMBLIES & ALL 3 WHEEL WELLS FOR FOR INDICATION OF FIRE. NO EVIDENCE OF FIRE OR OVERHEAT WAS FOUND REPLACED OVERHEAT DETECTION UNIT OPS CKS OK. THIS CLEARS M261369. 2L73 4F A3WE 20030813001332003081300133NM 2003 8 13 0301346641 120030724A2530 COFFEEMAKER BOEING747 747212B 1384886NM CENTER GALLEY BURNED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01641NW 21941 DURING FLIGHT, A BURNING ODOR EMITTED IN THE AREA OF DOOR 4R. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE CENTER GALLEY FORWARD COFFEEMAKER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030813001432003081300143NM 2003 8 13 SWAA031756 120030805A53116546546 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8L AND STR 9L, BS'S 827, 867, 887 AND 907. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030813001452003081300145NM 2003 8 13 SWAA031758 120030805A5315BAC1509 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, WL 208 AND LBL 53. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20030813001602003081300160NM 2003 8 13 SWAA031670 120030726A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT BS 344 AT STR 25R, BS 475 AT STR 17R, BS 747 AT STR 20L AND BS 830 AT STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000012003081400001NM 2003 8 14 SWAA031712 120030730A3350BR2013 LIGHT BOEING737 7373H4 1384600NM FWD CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW NR 3. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20030814000082003081400008NM 2003 8 14 SWAA031720 120030801A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030813000462003081300046NM 2003 8 13 2003UALA00460 120030529A3350 LAMP BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29648UA 25285 EXTERIOR EMERGENCY LIGHT INOPERATIVE AFT OF LEFT WING. RELAMPED LIGHT. 2L72 4F4 FRTA1NM E24NE 20030813000502003081300050NM 2003 8 13 2003UALA00464 120030604A5313 STRINGER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 AFT CARGO STRINGER 34R AT STATION 1337 HAS HEAVY CORROSION ON SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION AND DOUBLER REPAIR. 2L72 4F4 FRTA1NM E3NE 20030813000572003081300057NM 2003 8 13 UPS03440829 120030519A5341 FITTING BOEING747 747200 1384847NM CRACKED CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, LT BS 1241 WING REAR SPAR LOWER SPLICE PLATE ONE EACH BOLT HOLE -K- LOCATION FOUND CRACK AND CORROSION AT 3 O'CLOCK POSITION 0.040 INCH DEPTH APPROX AND 5 O'CLOCK POSITION 0.040 INCH APPROX RESPECTIVELY. REPAIRED AS PER R57-12-35029 AND EO B747-5710-18862-A. 2L74 4F RTA20WE 20030813000622003081300062NM 2003 8 13 UPS03440834 120030518A5320 FLOOR SUPPORT BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 BULK CARGO STA 1920-1940 LBL 30 FLOOR SUPPORT STRUCTURE UPPER AND LOWER SURFACE FOUND CORRODED. BULK CARGO STA 1920-1970 LBL 30 INCH FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20. CORROSION BLEND OUT (0.025 INCH X .875 INCH X 6 INCH). 2L74 4F RTA20WE 20030813000642003081300064NM 2003 8 13 UPS03440836 120030518A5320 FLOOR SUPPORT BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, BULK CARGO STA 1920-1980 LBL 8 FLOOR SUPPORT STRUCTURE UPPER AND LOWER SURFACE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01& 51-10-02 & FLOOR SUPPORT REPAIRED AT BS 1920 TO 1950 LBL 8 AS PER SRM 53-10-07 FIG 20. CORROSION BLEND OUT (0.020 INCH X 1 INCH X 8 FT). 2L74 4F RTA20WE 20030813000672003081300067NM 2003 8 13 UPS03440839 120030518A5320 FLOOR SUPPORT BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, BULK CARGO STA 1920-1980 RBL 15 FLOOR SUPPORT UPPER AND LOWER SURFACE CORROSION FOUND. BULK CARGO STA 1920-1950 RBL 15 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 & CORROSION REMOVED & REPROTECTED AT BS 1950-1980 AREA AS PER SRM 51-10-01 & 51-10-02 CORROSION BLEND OUT (0.020 INCH X 1.5 INCH X 7 INCH). 2L74 4F RTA20WE 20030813000962003081300096SO 2003 8 13 SWIA200312100 120030611A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN WILL NOT TEST A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07299SW 120329 EMERGENCY LIGHTS DO NOT TEST PROPERLY. CENTER SECTION LIGHTS GO INOP AFTER COUPLE SECONDS. INSTALLED NEW K201 RELAY AND OPS CHECK GOOD. 2L72 4T RTA31SO 20030813001072003081300107WP 2003 8 13 GTIA030563 120030625A5320 WEB DOUG DC9 DC982 3022082WP SUBFLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN SUBFLOOR CORRODED AT FS 207 24 INCHES RBL, VISIBLE FROM E/E COMPARTMENT. REMOVED WEB STATION 200 TO 218. FABRICATED NEW SUBFLOOR. INSTALLED NEW SUBFLOOR WEB. (M) 2L72 4F A6WE 20030813001202003081300120WP 2003 8 13 AALA20030780 120030701A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 14D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001262003081300126NM 2003 8 13 USAA030116 120030708A574365C3649223 SUPPORT FITTING BOEING737 737301 1384611NM MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND MLG BEAM AFT SUPPORT FITTING HAS APPROX .5 INCH CRACK, UPPER OUTBOARD HOLD ON MLG BEAM AFT SUPPORT FITTING, RSS 224.14. OVERSIZED HOLE AND INSTALLED STRAP ACROSS UPPER REAR SPAR CHORD PER EA 76210. (M) 2L72 4F RTA16WE 20030813001272003081300127WP 2003 8 13 AALA20030669 120030618A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21227AA 49177 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON WALL ACROSS FROM FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS ASSEMBLY ON WALL ACROSS FROM FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001312003081300131WP 2003 8 13 AALA20030699 120030628A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217547A 53029 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY EXIT FLOOR LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001342003081300134 2003 8 13 SWAA031747 420030805A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030813001542003081300154NM 2003 8 13 SWAA031664 120030724A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030813001842003081300184NM 2003 8 13 SWAA031694 120030728A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26L AND 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030814000282003081400028NM 2003 8 14 SWAA031699 120030730A53206551698 SPLICE BOEING737 7373H4 1384600NM STRINGER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030814000562003081400056WP 2003 8 14 UPS03841035 120030705A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C2 FUSELAGE SKIN CRACKED AT VERT FIN AND CENTER SPAR CANT BULKHEAD AT TACH POINT FS 1770 LONG 8L. TRIMMED OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOULBER AND SKIN FILLER IAW DC8 SRM 53-2-1 FIG 7. PERFORMED HFEC IAW DC8 NDT SPM 06-10-01.001. NO CRACKS NOTED. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2L74 4F RT4A25 20030814000642003081400064EA 2003 8 14 SWIA200312222 120030731A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07594SW8275 4784 7285 STAB CHANNEL 1 HSTCU DISENGAGED DURING FLIGHT, UNABLE TO RE-ENGAGE. MACH TRIM FAILURE INFLIGHT DESCENDING FROM 11000 MSL AND SLOWING FROM 280 KIAS, ABLE TO RE-ENGAGE VIA QRH. REMOVED & REPLACED HSTA IAW MM 27-42-01. REMOVED & REPLACED MCU IAW 27-42-05. OPS CHECKS GOOD IAW 27-41-00. P/N OFF/ON 7062-3, S/N OFF 606, S/N ON 734. 2L72 4F RTA21EA 20030814000732003081400073 2003 8 14 CALA0300373 420030710A31604073610916 DISPLAY BOEING737 737724 13844BYNM COCKPIT INOPERATIVE A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW27167038128 28764 THE CAPTAIN'S OUTBOARD PRIMARY FLIGHT DISPLAY FAILED INFLIGHT. A STRONG BURNING ODOR WAS PRESENT IN THE COCKPIT. THE CENTER DISPLAY UNIT AND INBOARD DISPLAY UNIT FLICKERED ON APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. 2L72 4F RTA16WE 20030814000742003081400074NM 2003 8 14 CALA0300374 120030709A5320 ANGLE BOEING737 737524 1384721NM R-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711641 28902 INSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED AT AFT AREA OF DOOR CUTOUT. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030814000752003081400075NM 2003 8 14 CALA0300375 120030619A5511 SPAR BOEING737 7373T0 1384582NM HORIZONTAL STAB DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 AN EXISTING REPAIR ON THE RT HORIZONTAL STABILIZER FRONT SPAR NEEDED TO BE REPLACED. THE EXISTING REPAIR WAS LOCATED AT STAB STA 245 ON THE FORWARD FLANGES OF THE UPPER AND LOWER CHORDS. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5510-01682. 2L72 4F RTA16WE 20030814000842003081400084SO 2003 8 14 SWIA200312173 120030708A323012038594501 MODULE EMB 120 EMB120ER 3260203SO MLG MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07235SW 120310 AFTER TAKEOFF LANDING GEAR HANDLE WAS SELECTED UP BUT GEAR REMAINED DOWN WITH ALL A&B GREEN AND RED LIGHTS ILLUMINATED. GEAR HANDLE WAS SELECTED DOWN, RED LIGHTS WENT OUT. RETURNED FOR LANDING. REPLACED LANDING GEAR CONTROL HANDLE. OPS CHECK GOOD. S/N OFF 120-228. 2L72 4T RTA31SO 20030814001232003081400123WP 2003 8 14 UPS03841038 120030708A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, CABIN SEAT TRACK AT STA 218/BL49L SCALLOPS ARE WORN. BLENDED SCALLOPS IAW DC8 SRM 53-2-3. ORIG WIDTH .600, .420 REMAINING OUT OF LIMITS IAW DC8 SRM 53-2-3. CUT OUT IAW DC8 SRM 53-2-3. ALODINED AND PRIMED CUTOUT IAW DC8 SRM 51-1-8. INSTALLED NUT CHANNEL P/N MS21064L4-8 ON TO CHANNEL P/N DC8-53B-007-006 IAW DC8 SRM 53-2-3 FIG 6D. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3-0 & 53-2-3 FIG 6D. 2L74 4F RT4A25 20030814001292003081400129NM 2003 8 14 2003UALA00577 120030718A5321 FLOOR PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29380UA 24655 MAIN CABIN FLOOR PANEL AT APB CRACKED BS 1016+12 RBL 2. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED PANEL. 2L72 4F4 FRTA16WE E2GL 20030814001532003081400153NM 2003 8 14 AALA20030450 120030411A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21184AN 29594 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM 9D-12D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT SECTION FOR 9D-12D AND CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030814001612003081400161NM 2003 8 14 AALA20030415 120030405A3350 RECEPTACLE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21658AA 24616 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT 9D LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT SEAT LIGHT RECEPTACLE AT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000422003081500042EU 2003 8 15 HEEA088619 120030717A243231908001 BATTERY BOLKMS117 BK117A1 5626010EU MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03230H 7136 MASTER BATTERY WILL NOT HOLD A CHARGE. REPAIRED. 1G72 3U H13EU 20030815000432003081500043SW 2003 8 15 HEEA088620 120030726A243239563001 BATTERY BELL 214 214ST 1182106SW MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 MASTER BATTERY DEAD. 2G72 4U H10SW 20030815000462003081500046SW 2003 8 15 HEEA088493 120030711A7921212061534001 TUBE BELL 412 412 1182202SW OIL COOLER CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 OIL COOLER TUBE CHAFED. SCRAPPED. 1G72 4U H4SW 20030815000482003081500048SW 2003 8 15 HEEA088556 120030805A6730212076005101 SERVO BELL 412 412 1182202SW CYCLIC LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033893P 33012 CYCLIC SERVO LEAKING FROM PILOT VALVE. SHOP REPAIR. 1G72 4U H4SW 20030813000032003081300003EU 2003 8 13 HEEA088648 120030724A7714645500051 TRANSMITTER AEROSPAS355 AS355* EU ENG TACH FLUCTUATES E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03975AE 2777 ENGINE NG RPM INDICATION NEEDLE HIGH AND FLUCTUATES 2-3 PERCENT AT FULL POWER SETTING. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030813000042003081300004SW 2003 8 13 HEEA088591 120030713A632194501031 BRAKE ASSY BELL 412 412 1182202SW MAIN ROTOR WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 ROTOR BRAKE ASSY WEAK. SHOP REPAIR. 1G72 4U H4SW 20030813000102003081300010EU 2003 8 13 HEEA088654 120030725A2432RG390E BATTERY BOLKMS105 BO105S 5626006EU MASTER OVERHEATED E HEEAO OTHER M OVER TEMP NRNOT REPORTED 1 SW03135AE63 S838 BATTERY STARTS SLOW AND GETS HOT. SHOP REPAIR. 1G72 3U H3EU 20030813000432003081300043NM 2003 8 13 2003UALA00457 120030530A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 MAIN CABIN, FLOORBEAM IS CORRODED AT BS 852, LBL 60. MAJOR REPAIR ACCOMPLISHED. REPLACED DAMAGED SECTION OF CABIN FLOORBEAM AND INSTALLED SPLICE REPAIRS. 2L72 4F4 FRTA1NM E24NE 20030813001012003081300101EA 2003 8 13 SWIA200312105 120030604A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 PAX DOOR CABLE MOUNT ON DOOR FRAME HAS CORROSION. DISCOVERED DURING AVIONICS MODIFICATION. REMOVED CORRODED CABLE MOUNT AND INSTALLED NEW IAW CRJ SRM 51-40-11, 51-42-20. P/N OFF: 444-2439-1. 2L72 4F RTA21EA 20030813001062003081300106WP 2003 8 13 AALA20030702 120030629A3350 TERMINAL DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21286AA 49298 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT SEAT 20DEF INOPERATIVE. REPLACED CEILING EMERGENCY EXIT LIGHT TERMINAL AT SEAT 20 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001382003081300138 2003 8 13 SWAA031751 420030806A2565D31354 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030813001402003081300140NM 2003 8 13 SWAA031753 120030805A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD CEILING EMERGENCY EXIT LIGHT LENS MISSING AT ROW NR 2. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030813001732003081300173 2003 8 13 SWAA031683 420030729A2565D31354 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030813001962003081300196 2003 8 13 SWAA031644 420030724A2565 INDICATOR BOEING737 7373H4 1384600NM FWD ENTRY DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030814000182003081400018NM 2003 8 14 SWAA031730 120030803A53306545776 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000242003081400024NM 2003 8 14 SWAA031736 120030803A2913623337 PUMP BOEING737 7375H4 138449DNM NR 1 ENGINE HYD FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29505SW 24182 AIR TURNBACK, ON GEAR RETRACT 'A' SYSTEM HYD PUMP LIGHTS AND MASTER CAUTION LIGHTS ILLUMINATED, 'A' SYSTEM HYD PRESS DROPPED TO 1000 PSI. REMOVED AND REPLACED ENGINE DRIVEN HYD PUMP 'A' AND CASE DRAIN FILTER PER MM. 2L72 4F RTA16WE 20030814000272003081400027NM 2003 8 14 SWAA031698 120030730A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 947 AT STR 23R, BS 967 AT STR 21L AND BS 787 AT STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000402003081400040NM 2003 8 14 SWAA031766 120030807A335020121 LIGHT BOEING737 7372H4 138448CNM FWD CABIN WILL NOT TEST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED PM CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY LIGHT BASE WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BASE PER MM. 2L72 4F A16WE 20030814000412003081400041NM 2003 8 14 SWAA031767 120030806A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20030814000422003081400042NM 2003 8 14 SWAA031771 120030807A57536546435278 SKIN BOEING737 7373H4 1384600NM RT OUTBD FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED C4 CHECK, FOUND RT OUTBD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBD T/E FLAP PER MM. 2L72 4F RTA16WE 20030814000882003081400088SO 2003 8 14 SWIA200312168 120030707A5411 FRAME EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07188SW 120039 LT ENGINE FRAME 1 CRACKED. DISCOVERED DURING C-CHECK. REMOVED & REPLACED FRAME 1 PER SB 120-54-0036 WITH NEW P/N 120-0351-003. 2L72 4T RTA31SO 20030814000952003081400095NM 2003 8 14 2003UALA00568 120030716A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29663UA 27160 MAIN CABIN AT STA 1197+80 LBL 89 SEAT TRACK HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPLACEMENT TRACK AND SPLICES. 2L72 4F4 FRTA1NM E24NE 20030814001142003081400114NM 2003 8 14 CALA0300417 120030727A5330 SKIN BOEING737 737524 1384721NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND FUSELAGE SKIN GOUGED JUST LEFT OF RUDDER SEAL AT STA 1116. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-80-01. 2L72 4F RTA16WE 20030814001162003081400116WP 2003 8 14 UPS03840951 120030704A33505708458503 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS BATTERY PACK IS DEAD. REPLACED BATTERY PACK, OPS OK. 2L74 4F RT4A25 20030814001212003081400121NM 2003 8 14 CALA0300428 120030731A5730 SKIN BOEING737 737524 1384721NM LT WING LE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND A GOUGE IN LT WING FIXED L/E UPPER SKIN PANEL AT O/B END OF NR 2 SLAT. THE SKIN WAS REPAIRED IAW SRM 51-70-16 AND ECRA 5721-01048. 2L72 4F RTA16WE 20030814001252003081400125WP 2003 8 14 UPS03841043 120030708A5330 PANEL DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, PNL 192E, SURFACE CORROSION AT BOLT HOLES, INNER SURFACE (MARKED). REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2 -0 FIG 1F. NEW PNL FABRICATED ON OP 50007 IAW DAC DWG 5750365. 2L74 4F RT4A25 20030814001262003081400126NM 2003 8 14 2003UALA00574 120030721A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29930UA 26655 PRESSURIZED FUSELAGE DAMAGED 5 INCHES FORE AND AFT AND 4 INCHES INBOARD TO OUTBOARD. DAMAGE IS JUST FWD OF STA 219 ON RIGHT SIDE OF FWD E&E DOOR [FWD OF NOSE GEAR DOORS]. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030814001302003081400130NM 2003 8 14 2003UALA00578 120030718A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29380UA 24655 DENT FOUND ABOUT 3 FT FROM DOOR 2L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030814001482003081400148NM 2003 8 14 AALA20030600 120030526A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21195AN 32389 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3EF INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030814001502003081400150NM 2003 8 14 AALA20030390 120030401A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21682AA 25339 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030814001592003081400159NM 2003 8 14 AALA20030588 120030519A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21664AA 25298 MIA - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT LIGHT ON AFT OVERWING EXIT INOPERATIVE. REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT ON AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000052003081500005NM 2003 8 15 AALA20030405 120030403A3350 MODULE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21185AN 32379 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS FOR FIRST CLASS AND TWO IN COACH INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000062003081500006NM 2003 8 15 AALA20030385 120030329A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21672AA 25337 DFW - DURING OVERNIGHT MAINTENANCE, EMREGENCY EXIT SEAT MOUNTED LIGHT AT 11D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000382003081500038 2003 8 15 HEEA088522 420030802A3454066400702 RECEIVER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 VOR RECEIVER INOPERATIVE. IN SHOP REPAIR. 1G72 4U H4SW 20030815000562003081500056SW 2003 8 15 HEEA088501 120030711A243239563001 BATTERY BELL 412 412 1182202SW MASTER WILL NOT TEST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 MASTER BATTERY WON'T TEST PROPERLY. 1G72 4U H4SW 20030815000602003081500060SW 2003 8 15 HEEA088506 120030711A6710412076620101 UNIVERSAL BELL 412 412 1182202SW COLLECTIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 COLLECTIVE UNIVERSAL WORN. REPAIRED. 1G72 4U H4SW 20030813001142003081300114WP 2003 8 13 GTIA030562 120030622A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT AT STATION 160 LBL 4 TO RBL 4 IS CORRODED. FABRICATED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030813001492003081300149NM 2003 8 13 SWAA031762 120030803A27504221T1003 MOTOR BOEING737 7377H4 1384404NM RT MLG W/W FAULTY A SWAAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SW29760SW 27874 FLAPS STAYED AT 0 WHEN SELECTED. ALTERNATE FLAPS WERE USED TO GET FLAPS TO 10, ALTERNATE T/E FLAP DRIVE CIRCUIT BREAKER TRIPPED. RESET CB, ATTEMPED MORE FLAPS AND CB CONTINUED TO TRIP. REMOVED AND REPLACED ALTERNATE FLAP DRIVE MOTOR PER MM. OPS CK'D FLAPS WITH HYDRAULICS AND WITH ALTERNATE FLAP DR MOTOR PER MM. 2L72 4F RTA16WE 20030813001642003081300164 2003 8 13 SWAA031674 420030727A25656557463 BRACKET BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE, BOTH FWD AND AFT GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED FWD AND AFT BRACKETS PER MM. 2L72 4F RTA16WE 20030813001822003081300182 2003 8 13 SWAA031692 420030729A256561621469 SLIDE BOEING737 7375H4 138449DNM SERVICE DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030813002012003081300201NM 2003 8 13 SWAA031649 120030724A5755654645170A SKIN BOEING737 7373G7 1384595NM RT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C3 CHECK, FOUND NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED NR 3 FLIGHT SPOILER PER MM. 2L72 4F RTA16WE 20030813002092003081300209NM 2003 8 13 SWAA031706 120030731A3350101073 LENS BOEING737 7377H4 1384404NM FWD ENTRY DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29416WN 32453 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030814000262003081400026NM 2003 8 14 SWAA031697 120030729A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 400, STRINGER 4R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030814000472003081400047NM 2003 8 14 UPS03241072 120030709A53306518420111 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C SKIN CRACK FOUND AT FWD CORNER CUTOUT OF FWD ENTRY DOOR S-7L. NOTE: WHEN NDT WAS CARRIED OUT IN REPAIR AREA, IT WAS FOUND THAT THERE WAS CORROSION BETWEEN THE SKIN AND BONDED DOUBLER IN THE AREA SURROUNDING THE FWD ENTRY DOOR SKIN PANEL P/N 65-18420-111. REPLACED IAW SHANNON MRO EO 2003-041-003. REFERENCE UPS EO B727-5330-19084. 2L73 4F A3WE 20030814000632003081400063EA 2003 8 14 SWIA200312221 120030727A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07437SW 7564 EMERGENCY AISLE LIGHT INOP OVER ROW 5. REMOVED AND REPLACED EMERGENCY CEILING LIGHT BULB OVER ROW 5 AS REQUIRED. OPS CHECK GOOD IAW MM 33-00-00. 2L72 4F RTA21EA 20030815000092003081500009WP 2003 8 15 GTIA030567 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 180 7 INCHES TO 44 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030815000142003081500014SW 2003 8 15 HEEA088571 120030806A7160209062214101 ACTUATOR BELL 412 412 1182202SW PARTICLE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 PARTICLE ACTUATOR MOTOR DOES NOT EXTEND OR RETRACT. 1G72 4U H4SW 20030815000152003081500015SW 2003 8 15 HEEA088610 120030727A3110209070263003 INDICATOR BELL 412 412 1182202SW DUAL VOLT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 DC NEEDLE INOP/SIGHT GLASS COMES OFF. 1G72 4U H4SW 20030815000332003081500033 2003 8 15 HEEA088519 420030715A3452066106200 TRANSPONDER BELL 206 206L1 1182107SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406EH 45183 TRANSPONDER SENDING SIGNAL INTERMITTENTLY. IN SHOP REPAIR. 1G71 3U H2SW 20030815000372003081500037SW 2003 8 15 HEEA088509 120030728A291070072J000B204 HOSE BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03142PH 33150 HYDRAULIC HOSE LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20030815000442003081500044SW 2003 8 15 HEEA088491 120030711A6420 BEARING BELL 412 412 1182202SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH NHFS10830 33150 TAIL ROTOR LINK HAS BEARINGS WORN. SCRAPPED. 1G72 4U H4SW 20030815000622003081500062SW 2003 8 15 HEEA088459 120030714A6240206076373001 TACH GENERATOR BELL 206 206L4 1182110SW ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F 52038 SPLINED SHAFT OF TACH GEN REMAINED IN TRANS OIL PUMP. 1G71 3U NCH2SW 20030813001322003081300132NM 2003 8 13 0301356638 120030724A2530 COFFEEMAKER BOEING747 747251B 1384892NM GALLEY SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01638US 23549 DURING FLIGHT, SMOKE EMITTED FROM THE NR 2 COFFEEMAKER. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE COFFEEMAKER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030813001582003081300158NM 2003 8 13 SWAA031668 120030724A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 520 AT STR 10L, BS 727D AT STR 22L AND BS 767 AT STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030813001982003081300198NM 2003 8 13 SWAA031646 120030723A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030814001082003081400108SO 2003 8 14 RAIA00306164 120030615A49104501968B APU EMB 145 EMB145 3260210SO APU BAY FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03803HK 145077 APU FAILED. MAINTENANCE DEFERRED APU PER MEL; SUBSEQUENTLY CLEARING THE DEFERRAL BY REMOVING AND REPLACING THE APU. 2L72 4F RTT00011AT 20030814001122003081400112 2003 8 14 801DM0010 420030722A2230948E414G2 COMPUTER BOEING757 757200 1384950NM THRUST MANAGE FAILED A PIDAO OTHER O OTHER CRCRUISE 1 SO05801DM 26240 AIRCRAFT FAILS TO MAINTAIN SPEED DURING CRUISE, TURN AUTO THROTTLE OFF, SPEED STABILIZES. REMOVED AND REPLACED THRUST MANAGEMANT COMPUTER IAW MM22-31-01. OPS CHECKS NORMAL. 2L72 4F RTA2NM 20030814001172003081400117NM 2003 8 14 UPS03M40939 120030602A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 INSPECTION TYPE: C, FOUND CORROSION ON SEAT TRACK AT RBL 27.5 BETWEEN STA 675 TO 755. CORROSION ON SEAT TRACK AT RBL 27.5 BETWEEN STA 675-755 BLENDED OUT AS PER SRM 51-21-01V2R33-ORI:0.090 & REMOVED 0.050 FOUND EXCEEDED LIMIT AS PER SRM 53-70-00V1R33. NEW SEAT TRACK AT 27.5 BETWEEN 675-755 INSTALLED AT EXISTING SPLICE AS PER SRM51-31-01V2R33. 2L73 4F RTA22WE 20030814001442003081400144WP 2003 8 14 GTIA030568 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200 44 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030814001552003081400155NM 2003 8 14 AALA20030319 120030317A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21604AA 27055 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SLIDE LIGHT AT R4 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT SLIDE LIGHT LAMP SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000222003081500022SW 2003 8 15 HEEA088529 120030805A6330 BEARING BELL 206 206L3 1182108SW GEARBOX MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH LK2204 51303 GEARBOX MOUNT HAS WORN BEARINGS. IN SHOP REPAIR. 1G71 3U H2SW 20030815000572003081500057SW 2003 8 15 HEEA088502 120030715A243239563001 BATTERY BELL 214 214ST 1182106SW MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M 28102 MASTER BATTERY WILL NOT HOLD A CHARGE. SENT TO UNITED BATTERIES FOR INSPECTION AND REPAIR. 2G72 4U H10SW 20030815000662003081500066SW 2003 8 15 HEEA088469 120030709A321230905 VALVE BELL 412 412 1182202SW EMERGENCY FLOAT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 EMERGENCY FLOAT VALVE SHEAR HEAD BLOWN. REPAIRED. 1G72 4U H4SW 20030815000722003081500072 2003 8 15 HEEA088478 420030708A2350A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 NR 1 VHF LIGHT STATIC. FOUND S1 SELECTOR SWITCH NOISY. CLEANED S1 SWITCH. REPAIRED. ALSO REPLACED 5 EACH MONITOR SWITCHES, REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030815000732003081500073SW 2003 8 15 HEEA088511 120030717A7921209062501005 OIL COOLER BELL 412 412 1182202SW ENGINE MISMANUFACTURED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03800Y 33134 OIL COOLER WOULD NOT FIT PROPERLY; COULD NOT INSTALL COWLING. 1G72 4U H4SW 20030815001022003081500102EU 2003 8 15 BAQA087117 120030804A2917704A37721034 PRESSURE SWITCH AEROSPAS365 AS365N2 8680815EU HYD SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 HYD SYSTEM PRESSURE SWITCH INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030815000472003081500047SW 2003 8 15 HEEA088555 120030728A3340212075139001 LANDING LIGHT BELL 412 412 1182202SW EXTERIOR INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 LANDING LIGHT INTERMITTENTLY WILL NOT TURN OFF. SHOP REPAIR. 1G72 4U H4SW 20030815000612003081500061SW 2003 8 15 HEEA088507 120030711A6710412310400101 ROD BEARING BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D4843 33076 WORN. SCRAPPED. 1G72 4U H4SW 20030815000692003081500069SW 2003 8 15 HEEA088472 120030714A6320406340100101 PUMP BELL 206 206L4 1182110SW TRANSMISSIO OIL DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F 52038 TACH GEN SPLINED SHAFT STUCK IN OIL PUMP. 1G71 3U NCH2SW 20030815000892003081500089SW 2003 8 15 HEEA088429 120030729A76032543391 SHAFT CLARK 1000 1000CLARK 2230102SW THROTTLE MISMARKED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 THROTTLE SHAFT RECEIVED AS PART NUMBER 2543391. THE PART IS REALLY PART NUMBER 2543661. THE THROTTLE LEVER WAS MODIFIED AND THE THROTTLE LEVER AND THROTTLE SHAFT WERE REPLATED. UNABLE TO USE THIS PART. SENT TO CADORATH AEROSPACE FOR WARRANTY REPAIR. 1Q71 3R 2A6 20030815001012003081500101EU 2003 8 15 BAQA088344 120030701A6220704A33640088 ADAPTER AEROSPAS365 AS365N2 8680815EU FREQUENCY BULGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME770 6417 FREQUENCY ADAPTER BULGING. REPLACED WITH SERVICEABLE UNITS. 1G72 3U RTH10EU 20030818000182003081800018 2003 8 18 HEEA088374 420030611A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X6223 760050 AFCS ACTUATOR KICKING. REPAIRED. 1G72 3U H1NE 20030818000412003081800041SW 2003 8 18 HEEA088498 120030714A63103034508WFC FILTER ELEMENT BELL 412 412 1182202SW GEARBOX BYPASSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 GEARBOX FILTER ELEMENT FOUND BYPASS INDICATOR TRIPPED. REPAIRED. 1G72 4U H4SW 20030818000502003081800050EU 2003 8 18 XG3R088675 120030812A33406485000 LIGHT UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE ANTI COLLISION BROKEN B XG3RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 500 3560 23004 ANTI-COLLSION LIGHT INOPERATIVE. REPLACE ANTI-COLLISION LIGHT ASSEMBLY. 1G72 3U3 U H9EU E00054EN 20030818000542003081800054SW 2003 8 18 HEEA088512 120030708A79218543909 OIL COOLER BELL 206 206L3 1182108SW ENGINE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW036603X 51412 OIL COOLER LEAKING FROM THE CORE. 1G71 3U H2SW 20030818000572003081800057SW 2003 8 18 HEEA088525 120030713A6700 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA RE2893 51542 BEARINGS WORN. IN SHOP REPAIR. 1G71 3U H2SW 20030818000622003081800062SW 2003 8 18 HEEA088548 120030728A7722206375007103 INDICATOR BELL 206 206L3 1182108SW TOT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 TOT INDICATOR STICKS AT AMBIENT DURING START INTERMITTENT. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030818000712003081800071SW 2003 8 18 HEEA088587 120030711A6220412310400101 ROD BEARING BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D1124 33076 MAIN ROTOR ROD BEARING WORN. SHOP REPAIR. 1G72 4U H4SW 20030818000822003081800082 2003 8 18 HEEA088634 420030804A2312064102300 TRANSCEIVER BOLKMS105 BO105S 5626006EU VHF MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033071K S859 PILOT REPORTED STATIC IN ALL PHASES FROM RADIO. IN SHOP REPAIR. 1G72 3U H3EU 20030818000862003081800086 2003 8 18 BAQA088190 420030723A3422066040211411 SYMBOL GENERATOR BOLKMS117 BK117A1 5626010EU RADAR SYSTEM MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME36 7243 PART ONLY LASTED 36.2 HOURS. RACK FAN WILL NOT TURN ON. FAN OPERATIONAL. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030818000892003081800089EU 2003 8 18 HEEA088644 120030725A2510 CABLE AEROSPAS355 AS355* EU INERTIA REEL BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 INERTIA REEL CABLE ASSY BROKEN. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030813001852003081300185NM 2003 8 13 SWAA031695 120030729A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 807 + 1, STR 25R. REPAIRED STR PER SRM. 2L72 4F RTA16WE 20030813002032003081300203NM 2003 8 13 SWAA031651 120030723A53106546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, WL 148 AND LBL 3. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030813002062003081300206NM 2003 8 13 SWAA031654 120030724A53306531914 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 178, WL 234, LBL 7.7 AND WL 195, RBL 0.5. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000292003081400029NM 2003 8 14 SWAA031700 120030730A335020131A BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030814000362003081400036 2003 8 14 SWAA031740 420030805A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030814000452003081400045CE 2003 8 14 DXTA200300078 120030805A3240662700066 LINE CESSNA560 560XL 2076702CE HYDRAULIC SYS LEAKING E DXTAK NONE K FLUID LOSS ININSP/MAINT 1 GL07610QS 5605210 DURING POST FLIGHT INSPECTION FOUND HYDRAULIC FLUID LEAKING OUT OF RIGHT WHEEL WELL. INSPECTED RIGHT WHEEL WELL AND FOUND FLUID LEAKING OUT FROM SPEED BRAKE RETRACT LINE. FURTHER INSPECTION FOUND SPEED BRAKE EXTEND LINE, FLAP EXTEND AND RETRACT LINES CHAFED BEYOND LIMITS AND THE EMERGENCY PNEUMATIC BRAKE LINE WAS 50 PERCENT CHAFED THROUGH AT THE RHS AND 75 PERCENT CHAFED THROUGH AT THE LHS BY THE NYLON LINE CLAMPS. PERFORMED VISUAL INSPECTION TO THE LEFT WHEEL WELL AND FOUND SAME RESULTS. REPLACED ALL HYDRAULIC & PNEUMATIC LINES IAW CESSNA 560XL MM CHAPTER 27-51-00, 27-61-00, AND 32-42-09 OPS AND LEAK CHECKED GOOD. 2L72 4F RTA22CE 20030814000522003081400052NM 2003 8 14 2003UALA00591 120030726A5320 FLOOR SUPPORT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29380UA 24655 CABIN FLOOR SUPPORT VERTICAL BEAM CRACKED BELOW FLOOR LEVEL BS 639 RBL 46. MAJOR REPAIR ACCOMPLISHED: SPLICED IN NEW 80 INCH IN SECTION OF UPPER T-CAP. 2L72 4F4 FRTA16WE E2GL 20030814000872003081400087SO 2003 8 14 SWIA200312167 120030707A5310 WINDOW POST EMB 120 EMB120ER 3260203SO COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07188SW 120039 RIGHT WINDSHIELD POST CRACKED. DISCOVERED DURING C-CHECK. COMPLIED WITH SB120-53-0072. 2L72 4T RTA31SO 20030814000982003081400098 2003 8 14 RAIA00306156 420030605A34607003938907 CONTROL PANEL JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03558HK12230 41071 5632-FSM- SMOKE IN FLIGHT DECK. MAINTENANCE REMOVED AND REPLACED FLIGHT DIRECTOR CONTROL PANEL. 2L72 4T RTA41NM 20030814001202003081400120NM 2003 8 14 UPS03M40946 120030603A5347S49291477075T6 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 INSPECTION TYPE: C, CABIN - FOUND CORROSION ON SEAT TRACK AT RBL 8.5 BETWEEN STA 790 TO 859. CORROSION ON SEAT TRACK RBL 8.5 BETWEEN STA 790 TO STA 859 BLENDED OUT AS PER SRM 51-21-00 V2R33 ORI THK:0.090 INCH & REMOVED 0.050 INCH FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 V1R3. SEAT TRACK RBL 8.5 STA 780 TRIMMED & SMOOTHED AS PER SRM 53-70-00 V1R33. NEW SEAT TRACK REWORKED FROM STA 780-869, RBL 8.5 AS PER SRM 53-70-00V1R33. 2L73 4F RTA22WE 20030814001352003081400135EU 2003 8 14 RAIA00306167 120030619A7930 ENGINE AEROSPATR72 ATR72202 8680940EU OIL PRESSURE OUT OF ADJUST A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03721TE 217 LEFT ENGINE OIL PRESSURE INDICATES LOW. MAINTENANCE ADJUSTED NR 1 OIL PRESSURE. 2H72 4T RTA53EU 20030814001582003081400158NM 2003 8 14 2003F00514 120030717A21205416744 ACTUATOR BOEING737 737800* NM LT RAM AIR DOOR INOPERATIVE A MYWAO OTHER J WARNING INDICATION CLCLIMB 1 SO19732MA 30618 LEFT PACK LIGHT ILLUMINATED IN FLIGHT. PREVIOUS DMI NR 3104 ON LEFT RAM AIR DOOR FULL OPEN LIGHT REMAINS ON AFTER FLAPS ARE RETRACTED. RETURNED TO MIAMI. REMOVED AND REPLACED LEFT RAM AIR ACTUATOR IAW AMM 21-51-21. OPS CHECKED GOOD. TROUBLE SHOT LEFT PACK LIGHT IAW FIM 21-52 TASK 834. OPERATIONAL CHECKED GOOD. RETURNED TO AIRCRAFT TO SERVICE. (M) 2L72 4F RTA16WE 20030815000192003081500019EU 2003 8 15 HEEA088659 120030807A641011731743 BLADE BOLKMS117 BK117A1 5626010EU TAIL ROTOR PEELING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TAIL ROTOR BLADE PAINT PEELING. 1G72 3U H13EU 20030815000532003081500053SW 2003 8 15 HEEA088497 120030715A77223030083 COMPENSATOR BELL 412 412 1182202SW ENGINE TRIM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 TRIM COMPENSATOR CAUSED ITT INDICATIONS TO FLUCTUATE AND THEN DROPPED TO ZERO WITH ENGINE RUNNING. 1G72 4U H4SW 20030815000652003081500065SW 2003 8 15 HEEA088468 120030430A243230135002 BATTERY BELL 206 206B3 1181506SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 MASTER BATTERY WEAK. REPAIRED. 1G71 3U H2SW 20030815001032003081500103GL 2003 8 15 HEEA088363 220030718A72610292005250 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW031546G 760076 ENGINE LEAKS OIL. 1G72 3U3 U H1NE E1GL 20030815001042003081500104NE 2003 8 15 HEEA088404 120030802A62207610608000050 DAMPENER SKRSKYS76 S76A 8143006NE MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 MAIN ROTOR DAMPENER LEAKING. SHOP REPAIR. 1G72 3U H1NE 20030818000012003081800001NE 2003 8 18 HEEA088364 220030712A73230292858180 METERING VALVE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE ENGINE GOV OUT OF ADJUST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE444 3234 RED GOVERNOR LIGHT ON GROUND RUN UP. FAULT CODE 129. FAIL2 CODE 4002. 1G71 3U3 U H9EU E00054EN 20030818000112003081800011 2003 8 18 HEEA088413 420030722A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 NR 1 YAW FULL DEFLECTION. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030818000172003081800017 2003 8 18 HEEA088373 420030611A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X 760050 AFCS ACTUATOR STICKING. REPAIRED. 1G72 3U H1NE 20030818000342003081800034SW 2003 8 18 HEEA088477 120030726A2810412361641101 FUEL CELL BELL 412 412 1182202SW LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 FUEL CELL LEAKING. 1G72 4U H4SW 20030818000352003081800035SW 2003 8 18 HEEA088481 120030720A5300205001914103 HORN BELL 412 412 1182202SW TAILBOOM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 MECHANICAL DAMAGE INSIDE OF HORN BEYOND LIMITS. SCRAPPED. 1G72 4U H4SW 20030818000382003081800038SW 2003 8 18 HEEA088487 120030724A3212206050247109 FLAP BELL 206 206L3 1182108SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 EMERGENCY FLOAT FLAP ASSY WORN AND TORN. SCRAPPED. 1G71 3U H2SW 20030818000392003081800039SW 2003 8 18 HEEA088488 120030728A3241206324460 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MLG SKID TUBE HAS CORROSION 10 INCHES AFT OF FWD X-TUBE. SCRAPPED. 1G71 3U H2SW 20030818000472003081800047 2003 8 18 BAQA088666 420030813A3454066302440 INDICATOR BOLKMS117 BK117B1 5626012EU COCKPIT STUCK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G1596 7179 GLIDE SLOPE FLAG STICKS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030818000532003081800053SW 2003 8 18 HEEA088508 120030715A2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL LEVEL SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 FUEL IND SHOWED ZERO WITH FUEL IN TANK. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030818000592003081800059SW 2003 8 18 HEEA088533 120030717A3210206050221009 SUPPORT BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 MLG SUPPORT WORN AND CORRODED. IN SHOP REPAIR. 1G71 3U H2SW 20030818000612003081800061SW 2003 8 18 HEEA088535 120030803A3246206053184102 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 SKID TUBE CORRODED AND WORN FLAT SPOTS ON THE BOTTOM OF THE SKID. IN SHOP REPAIR. 1G71 3U H2SW 20030818000652003081800065 2003 8 18 HEEA088564 420030801A34222594484 TRANSMITTER BELL 412 412 1182202SW FLUX VALVE PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 COPILOT RMI PRECESSES. SHOP REPAIR. 1G72 4U H4SW 20030818000662003081800066SW 2003 8 18 HEEA088570 120030806A2931209070262111 INDICATOR BELL 412 412 1182202SW HYD PRESSURE INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 INDICATOR STICKS INTERMITTENTLY. 1G72 4U H4SW 20030818000692003081800069SW 2003 8 18 HEEA088585 120030711A6220412310400101 ROD BEARING BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MAIN ROTOR ROD BEARING WORN. SHOP REPAIR. 1G72 4U H4SW 20030818000772003081800077SW 2003 8 18 HEEA088613 120030701A6720 BEARING BELL 412 412 1182202SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 WORN BEARINGS. REPLACED BEARING DSP4, DSRP4 AND DW5 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030818000852003081800085EU 2003 8 18 HEEA088637 120030721A2435150SG122Q STARTER GEN AEROSPAS355 AS355* EU ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 STARTER GENERATOR WILL NOT PICK UP LOAD OR CRANK ENGINE. TO BE SENT TO VENDOR FOR CREDIT. 1G72 3U H11EU 20030818000922003081800092 2003 8 18 BAQA088337 420030805A3421109290 GYRO BOLKMS117 BK117B1 5626012EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 GYRO UNIT CAUSES API AND RATE GYRO CAUTION LIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030819000052003081900005 2003 8 19 BAQA088144 420030719A34163A433220F281CL ALTIMETER UROCOPEC135 EC135P1 8680990EU COCKPIT INACCURATE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TS849 0167 ALTIMETER UNIT IS OFF AND HAS EXCESSIVE FRICTION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030819000112003081900011WP 2003 8 19 AALA20030775 120030716A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219619V 53566 DURING OVERNIGHT MAINTENANCE, FORWARD TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030815000552003081500055SW 2003 8 15 HEEA088482 120030720A6230206010360005 LINK ASSY BELL 206 206L3 1182108SW M/R PITCH CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 FOUND CORROSION ON LOWER END OF P/C LINK NEAR JAM NUT. SCRAPPED. 1G71 3U H2SW 20030815000582003081500058SW 2003 8 15 HEEA088474 120030710A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K9864 33020 CHORDWISE CRACK AT STATION 125 INCHES ON BOTH THE UPPER AND LOWER SIDE. THE CRACK IS 5 INCH LONG. 1G72 4U H4SW 20030818000062003081800006 2003 8 18 HEEA088391 420030716A3455066104701 TRANSCEIVER SKRSKYS76 S76A 8143006NE ADF MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 AUDIO FADES OUT. SENSE COAX CONNECTOR IS LOOSE. IN SHOP REPAIR. 1G72 3U H1NE 20030818000102003081800010 2003 8 18 HEEA088412 420030710A22157690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH7632 760505 AFCS ACTUATOR PRODUCING HARD OVER LT. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20030818000252003081800025 2003 8 18 HEEA088462 420030717A3416212070238007 INDICATOR BELL 412 412 1182202SW ALTIMETER INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 ALTIMETER INDICATOR READS 100 FT OFF. REPAIRED. 1G72 4U H4SW 20030818000362003081800036SW 2003 8 18 HEEA088485 120030717A6220 BEARING BELL 206 206L3 1182108SW LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X LK10290 51412 MAIN ROTOR LINK ASSY HAS WORN BEARINGS. 1G71 3U H2SW 20030818000402003081800040SW 2003 8 18 HEEA088492 120030711A2820212061532001 TUBE BELL 412 412 1182202SW FUEL SYSTEM CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 FUEL SYSTEM TUBE CHAFED. REPAIRED. 1G72 4U H4SW 20030819000342003081900034WP 2003 8 19 AALA20030651 120030610A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21569AA 49351 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT AIRSTAIR FORWARD CEILING PANEL INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ELECTRICAL QUICK DISCONNECT FOR AFT AIRSTAIR FORWARD CEILING PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030819000352003081900035NM 2003 8 19 AALA20030704 120030630A3350 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21362AA 24043 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 12B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030819000432003081900043NM 2003 8 19 AALA20030056 120030107A5315 FLOORBEAM BOEING767 767223 1385123NM 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21332AA 22331 FOUND FLOORBEAM UPPER FLANGE AT STATION 347 RBL 45.5 HAD CORROSION BLENDED BEYOND SRM LIMITS. REQ ENGINEERING APPROVAL TO REPAIR PER ATTACHED DRAWING. FLOORBEAM REPAIRED AT STATION 347 PER MRB 767-2428. (M) 2L72 4F RTA1NM 20030819000512003081900051SO 2003 8 19 RAIA00306169 120030619A2760 PROXIMITY SENSOR EMB 145 EMB145 3260210SO SPOILERS DIRTY A RAIAO OTHER J WARNING INDICATION LDLANDING 1 CE03807HK 145119 DURING LANDING RECEIVED SPOILER FAIL MESSAGE. MAINTENANCE INSPECTED AND CLEANED LEFT CENTER PROXIMITY SWITCH. 2L72 4F RTT00011AT 20030819000542003081900054NE 2003 8 19 RAIA00306172 220030624A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RIGHT MALFUNCTIONED A RAIAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CE03561HK 41077 75109 RT ENGINE WILL NOT MAKE POWER. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. 2L72 4T4 TRTA41NM E18NE 20030819000552003081900055EU 2003 8 19 RAIA00306173 120030624A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03558HK 41071 LEFT SIDE EMERGENCY FLOOR LIGHTS INOP. RE-SECURED CONNECTOR AT SEAT 9A. 2L72 4T RTA41NM 20030819000602003081900060NM 2003 8 19 C1HA200385006 120030811A3350 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 LT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PACK IAW 727 MM 33-50-22, ALL OPS NORMAL. 2L73 4F A3WE 20030819000622003081900062SO 2003 8 19 SWIA200312120 120030522A5412 FIREWALL EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 RIGHT NACELLE FIREWALL HAS SMALL CRACK. FOUND DURING C-CHECK INSPECTION. APPLIED DOUBLER IAW 120 SRM 51-10-02. 2L72 4T RTA31SO 20030819000722003081900072NM 2003 8 19 2003UALA00443 120030521A7333 INDICATOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 ENGINE MALFUNCTIONED A UALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP29929UA 26652 724329 AIRCRAFT ABORTED TAKEOFF, AIRCRAFT SWERVED DURING THE TAKEOFF ROLL. CAUSE IS STILL TO BE DETERMINED. CREW ABORTED TAKEOFF DUE TO NR 1 ENGINE GAUGE INDICATING FUEL FLOW ROLLBACK TO ZERO. NO FLAMEOUT REPORTED AND ALL OTHER ENGINE INDICATIONS WERE NORMAL. THE FUEL FLOW TRANSMITTER, MAIN ENGINE CONTROL, MAIN FUEL PUMP, AND POWER MANAGEMENT CONTROL WERE REMOVED AS PRECAUTIONARY AND WILL BE HELD FOR ENGINEERING REVIEW. IN ADDITION, THE PRIMARY EIS PANEL WAS REPLACED, WIRING CHECKED FOR DAMAGE AND D830 CONNECTOR CLEANED & CHECKED WITH NO DEFECTS FOUND. 2L72 4F4 FRTA16WE E2GL 20030819000752003081900075NM 2003 8 19 CALA0300390 120030715A5347 SEAT TRACK BOEING777 777224 1385225NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778009 29479 INSPECTION FOUND SEAT TRACK CROWN CORRODED AT BS 1513, LBL 85. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTT00001SE 20030819000992003081900099NM 2003 8 19 C1HA200396014 120030804A335037067001 BATTERY BOEING727 727200 138407ENM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA AFT AIRSTAIRS OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD BATTERY, OPS CHECK NORMAL. 2L73 4F RTA3WE 20030819001072003081900107NM 2003 8 19 UPS03440923 120030701A2910 HYDRAULIC SYSTEM BOEING747 747121 1384871NM NR 2 FAILED A IPXAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01682UP 20349 ATB - NR 2 HYD SYSTEM FAILURE. REMOVED & REPLACED NR 2 EDP AS REQUIRED DUE TO OVERHEAT IAW MM 29-11-05. OPS & LEAK CHECK REQUIRED. RAN NR 2 ENG FOR LEAK CHECK OF NR 2 HYD (EDP) PUMP GROUND CK'S NORMAL. OK FOR SERVICE. HYD PRESSURE CHECK NORMAL. 2L74 4F A20WE 20030819001162003081900116NM 2003 8 19 2003UALA00499 120030615A5540 WEB BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RUDDER DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 VERTICAL STAB REAR SPAR ABOVE RUDDER, UPPER WEB DAMAGED BY STATIC DISCHARGE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW WEB. 2L72 4F4 FRTA1NM E24NE 20030819001262003081900126NM 2003 8 19 0301155511 120030619A335020131A POWER SUPPLY BOEING757 757251 1384970NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01511US 23199 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE SEATS 1-32. REPLACED POWER SUPPLY AT DOOR 2R M732, P/N 2013-1A. 2L72 4F RTA2NM 20030819001312003081900131EA 2003 8 19 032226322 120030810A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING MAINTENANCE INSPECTION THE RT FWD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030819001342003081900134NM 2003 8 19 CALA0300356 120030702A3260 SENSOR BOEING737 737524 1384721NM MLG OUT OF ADJUST A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713624 27528 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM HOU. THE AIRCRAFT WAS RETURNED TO HOU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED AND TESTED THE MLG SAFETY SENSORS IAW MM 32-09-01. AN OPERATIONAL CHECK OF THE GEAR WAS PERFORMED IAW MM 32-32-04 AND 32-33-00 AND THE GEAR RETRACTED NORMALLY. 2L72 4F RTA16WE 20030819001442003081900144EA 2003 8 19 SWIA200312150 120030625A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 280 FLOORBEAM I/B AND O/B ATTACH ANGLES RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. 2L72 4F4 FRTA21EA E15NE 20030818000902003081800090EU 2003 8 18 HEEA088649 120030720A770070BMB01020 CONTROL UNIT AEROSPAS355 AS355* EU ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE 3234 RED GOVERNOR LIGHT COMES ON WITH FAIL 2 0000 AFTER AIRCRAFT WAS STARTED. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H11EU 20030818000912003081800091 2003 8 18 HEEA088656 420030723A34143839949002 INDICATOR AEROSPAS355 AS355* EU AIRSPEED STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 AIRSPEED INDICATOR HAS A STICKING NEEDLE AND 20 KTS OFF. 1G72 3U H11EU 20030818000952003081800095NE 2003 8 18 HEEA088434 120030717A243229490001 BATTERY SKRSKYS76 S76A 8143006NE MASTER OVERHEATED E HEEAO OTHER M OVER TEMP NRNOT REPORTED 1 SW031545K 760047 BATTERY HOT LIGHT CAME ON IN FLIGHT. REPAIRED. 1G72 3U H1NE 20030819000152003081900015NM 2003 8 19 USAA030099 120030627A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48149 23319 FOUND SKIN CRAKED .75 INCHES LONG, SKIN BS 360 S27L, S27R, LOWER CENTERLINE. INSTALLED DOUBLER FROM BS 360-380 ON BOTTOM C/L OF SKIN PER TYPICAL REPAIR 53-30-07. (M) 2L72 4F RTA16WE 20030815000702003081500070SW 2003 8 15 HEEA088476 120030726A2810412361640101 FUEL CELL BELL 412 412 1182202SW LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 FUEL CELL LEAKING. 1G72 4U H4SW 20030815000872003081500087 2003 8 15 HEEA088420 420030728A3442MI5852013 INDICATOR SKRSKYS76 S76A 8143006NE WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 WEATHER RADAR RANGE SHIFTS BACK AND FORTH. SHOP REPAIR. 1G72 3U H1NE 20030818000022003081800002 2003 8 18 HEEA088372 420030710A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03776P 8624 760275 AFCS ACTUATOR INOPERATIVE. 1G72 3U H1NE 20030818000332003081800033SW 2003 8 18 HEEA088473 120030708A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 MAIN ROTOR BLADE CRACKED ON BOTTOM AND OUTBOARD TAB UNBONDED. REPAIRED. 1G72 4U H4SW 20030818000422003081800042SW 2003 8 18 HEEA088503 120030617A6230 BEARING BELL 412 412 1182202SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P1040 A2969 33012 WORN BEARINGS. REPLACED 2 EACH BEARINGS 412-010-424-103 DUE TO WORN; RACE 412-010-418-101 DUE TO PITTING; RACE 412-010-418-105 DUE TO PITTING; BEARING 412-010-427-101 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030818000792003081800079SW 2003 8 18 HEEA088615 120030719A6730212076005111 SERVO BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R13546 36007 GOUGED PISTON. FOUND PISTON AND GLANDS SCORED. REPAIRED. 1G72 4U H4SW 20030819000012003081900001EU 2003 8 19 BAQA088681 120030807A6210117151311 BLADE BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR DAMAGED W BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG4460 7506 MAIN ROTOR BLADE HAS MINOR LEAD LAG PLAY. BLADE LASTED ONLY 421.6 HOURS SINCE LAST REPAIR. PART IS ALSO DUE LOOP INSPECTION. 1G72 3U3 UNCH13EU E19EU 20030819000102003081900010EA 2003 8 19 A6WA200340106 120030624A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 INTERMITTENT A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31416AW 7603 INTERMITTENT IDG 2 CAS MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF MESSAGE CLEARED. BRAKE TEMP REMAIN IN NORMAL RANGE. COMPLIED WITH 'CM' ACTION. PLACARDED AND PLACED ON MEL. SERVICED NR 2 IDG AND RECONNECTED, CHECKS OK. REMOED FROM MEL. (M) 2L72 4F RTA21EA 20030819000222003081900022NM 2003 8 19 USAA030107 120030630A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19532AU45356 23379 FOUND SKIN CRACKED 1 INCH, STATION 727E, STRINGER 23L. INSTALLED REPAIR DOUBLER PER TR 53-60-03. (M) 2L72 4F RTA16WE 20030819000232003081900023NM 2003 8 19 AMTA200300779 120030614A2497 WIRE HARNESS BOEING757 75723N 1384973NM CABIN BURNED A AMTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11518AT 27974 FLT NR 598 - STRONG OIL ODOR IN CABIN NEAR CENTER OF AIRCRAFT. FOUND BURNED WIRE BUNDLE AT TEMP SENSOR D02584. SPLICED WIRES PER WSPM TEMP CONTROL. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030819000372003081900037WP 2003 8 19 AALA20030662 120030614A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2133502 49739 DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 14D INOPERATIVE. REPLACED SEAT MOUNTED EMEGENCY EXIT LIGHT ASSEMBLY AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030819002062003081900206NM 2003 8 19 SWAA031770 120030806A53306545726 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 915 AT STR 23L, BS 915 AT STR 24L AND BS 975 AT STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030819002072003081900207NM 2003 8 19 CALA0300424 120030720A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714342 23580 INSPECTION FOUND FLOORBEAM CORRODED UNDER LAV-A AT STA 294.5, LBL 24.67. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-51 AND ECRA 5311-01159. 2L72 4F RTA16WE 20030815000512003081500051 2003 8 15 HEEA088495 420030710A2210222331617103 ISOLATION MOUNT BELL 230 230 1182149SW AUTOFLIGHT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RC 23037 SEPERATION BETWEEN ELASTOMER AND CENTER PORTION OF MOUNT. 1G72 3U NCH9SW 20030818000032003081800003NE 2003 8 18 HEEA088380 120030724A32977655200110107 WIRE HARNESS SKRSKYS76 S76A 8143006NE MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 UNSAFE LIGHT ON COCKPIT WILL NOT EXTINGUISH. SCRAPPED WIRE HARNESS. 1G72 3U H1NE 20030818000072003081800007 2003 8 18 HEEA088392 420030715A3416066030640001 ENCODER SKRSKYS76 S76A 8143006NE ALTIMETER INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 ALTMETER ENCODER INACCURATE, READING OFF. IN SHOP REPAIR. 1G72 3U H1NE 20030818000202003081800020 2003 8 18 HEEA088443 420030726A3457 DISPLAY SKRSKYS76 S76A 8143006NE GPS CONTROL UNITBROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 282 760035 DISPLAY IS BROKEN. 1G72 3U H1NE 20030818000452003081800045 2003 8 18 BAQA088335 420030808A3120B1894522281A CLOCK UROCOPEC135 EC135T1 5620026EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH2328 0131 CLOCK INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030818000642003081800064SW 2003 8 18 HEEA088558 120030805A2910212076015001 CHECK VALVE BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033893P 33012 HYD CHECK VALVE LEAKING. SHOP REPAIR. 1G72 4U H4SW 20030818000672003081800067SW 2003 8 18 HEEA088577 120030729A6220 BEARING BELL 412 412 1182202SW PENDULUM ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P A1369 33012 MAIN ROTOR PENDULUM ASSY HAS ROUGHNESS IN BEARINGS. SHOP REPAIR. 1G72 4U H4SW 20030818000932003081800093EU 2003 8 18 HEEA088432 120030719A71970292697570 WIRE HARNESS AEROSPAS355 AS355* EU GOVERNOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE 3234 RED GOVERNOR LIGHT ON GROUND RUN UP. FAULT CODE 129 FAIL CODE 4002. 1G72 3U H11EU 20030819000082003081900008EU 2003 8 19 BAQA085963 120030717A6710L673M40A1001 ACTUATOR UROCOPEC135 EC135T1 5620026EU FENESTRON LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME2173 0144 FENESTRON ACTUATOR LEAKING. BOLT SPINNING IN ARM. BEARINGS WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030819000202003081900020WP 2003 8 19 AALA20030655 120030611A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21234AA 49181 DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT 14D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030819000562003081900056 2003 8 19 RAIA00306174 420030625A3421HG2010AC02 INDICATOR EMB 145 EMB145LR 3260212SO NR 2 AHRS OVERHEATED A RAIAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK6167 145044 EICAS MESSAGE NR 2 AHRS OVERHEAT. MAINTENANCE REMOVED AND REPLACED THE NR 2 AHRS. 2L72 4T RTT00011AT 20030819000782003081900078NM 2003 8 19 CALA0300393 120030716A5330 SKIN BOEING757 757224 1384958NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717122 27564 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 450, S22L TO S23L, 2.5 FEET ABOVE E&E DOOR. THE DENT WAS 10 X 2 INCHES WITH A DEPTH OF 0.070 INCH. THE SKIN WAS REPAIRED IAW SRM 53-00-01 AND ECRA 5330-03267. 2L72 4F RTA2NM 20030819000892003081900089SO 2003 8 19 SWIA200312109 120030614A2121AE1711AA0 FAN EMB 120 EMB120ER 3260203SO RT PACK MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07288SW7412 7412 120316 SMOKE IN CABIN AND ASSOCIATED RIGHT PACK FAIL. REPLACED RIGHT PACK GROUND COOLING FAN. OPS CHECKED NORMAL. 2L72 4T RTA31SO 20030819001192003081900119NM 2003 8 19 2003UALA00502 120030614A29134205401 PUMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT ENG HYD FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29543UA 25698 LOST LEFT HYD SYSTEM PRESSURE AND FLUID. LT ENGINE DRIVEN PUMP FAILED RESULTING IN A LOSS OF HYDRAULIC FLUID AND SYSTEM PRESSURE. LEFT ENGINE DRIVEN PUMP WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED. 2L72 4F4 FRTA2NM E17NE 20030819001222003081900122NM 2003 8 19 2003UALA00504 120030616A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE POWER DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29364UA 24533 SHEET METAL AT EXT POWER DOOR LOWER LATCH STOP CRACKED BETWEEN RIVET HOLES. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED INTERNAL DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030819001482003081900148NM 2003 8 19 0301226719 120030610A5320 WEB BOEING747 747251F 1384898NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01619US 21321 DURING H-CHECK FOUND CORROSION ON WEB OF AFT CARGO DOOR SEAL DEPRESSOR AT BS 1830 WL 108. REPAIRED PER EA 67-165070. 2L74 4F A20WE 20030819001842003081900184NM 2003 8 19 SWAA031784 120030809A32216545819 ATTACH FITTING BOEING737 7375H4 138449DNM NLG CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED RON, FOUND NLG ACTUATOR ATTACH FITTING GUSSETT CRACKED AT RADIUS. REMOVED AND REPLACED NLG ACTUATOR ATTACH FITTING PER BOEING DRAWING. 2L72 4F RTA16WE 20030819001982003081900198WP 2003 8 19 UPS03840853 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RT WING L/E UPPER RIB IS CRACKED AT XFS 304. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030819002152003081900215NM 2003 8 19 2003UALA00604 120030731A5347 SEAT TRACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29380UA 24655 CRACK IN SEAT TRACK SUPPORT BEAM SUPPORT STRUCTURE AT BS 639 RIGHT BL 46. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SUPPORT TRACK. 2L72 4F4 FRTA16WE E2GL 20030819002182003081900218CE 2003 8 19 DXTA200300044 120030609A3241MS24166D2 RELAY CESSNA560 560XL 2076702CE ANTI SKID INOPERATIVE E DXTAO OTHER K FLUID LOSS LDLANDING 1 GL07630QS 5605130 LOST BRAKES ON LANDING ROLLOUT. USED EMERGENCY BRAKES TO STOP ACFT. POWER BRAKES AND ANTI SKID ANNUNCIATORS DID COME ON WHEN ACFT LOST BRAKES. POST FLIGHT REVEALED A PUDDLE OF FLUID ON THE GROUND AND ON THE NOSE GEAR, UNDER THE NOSE OF THE ACFT. TROUBLESHOT TO SKID CONTROL RELAY. REPLACED WITH NEW PER CESSNA 560XL M/M CHAPTER 32-42-08. SYSTEM OPERATIONAL CHECKED GOOD. 2L72 4F RTA22CE 20030819002272003081900227WP 2003 8 19 UPS03840981 120030714A3350 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: ASV, EMERGENCY LIGHTS WILL NOT TEST. FOUND EMERGENCY LIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01, OP CHECK GOOD. 2L74 4F RT4A25 20030820000012003082000001WP 2003 8 20 UPS03841118 120030815A2910 FITTING DOUG DC8 DC871F 302199DWP HYD SYSTEM LEAKING A IPXAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO01772UP 46072 CREW REPORTED LOSING HYD SYSTEMS. DECLARED EMERGENCY. A/C LANDED W/O INCIDENT. HYD QTY DROPPED TO STANDPIPE LEVEL FOLLOWED BY RUDDER & AILERON CONTROL MANUAL LIGHTS COMING ON, (FL 390 & 150 NM FROM DESTINATION). REMOVED AND REPLACED RESERVOIR AIR PRESS REGULATOR ASPIRATOR & TEE-FITTING IAW MM 29 10 03 2, OPS CHECKED NORMAL. 2L74 4F RT4A25 20030820000032003082000003WP 2003 8 20 UPS03841120 120030815A3350 BATTERY DOUG DC8 DC871F 302199DWP EMERGENCY LIGHTINTERMITTENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS CAME ON EMERGENCY EXIT & EMERGENCY EXIT CONTROL C/B`S PULLED AND RESET EMERGENCY EXIT LIGHTS STILL ON. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY & RELAY UNIT PER MM 33 50 01 2, OPS CHECK NORMAL. 2L74 4F RT4A25 20030820000052003082000005NM 2003 8 20 03FDEA01304 120030814A2130 INDICATOR BOEING727 727200 138407ENM PRESS CONTROL FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25469FE 21581 ON CLIMBOUT OF TUS, CABIN CONTINUED TO CLIMB TO 2000 27QRH PROCEDURES WERE PERFORMED AND CABIN PRESSURE DID NOT RESPOND. 2L73 4F RTA3WE 20030820000082003082000008NM 2003 8 20 03FDEA01301 120030814A3620UNK CLAMP BOEING727 727200 138407ENM ZONE 400 LOOSE A FDEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 SO25218FE 21101 DURING CLIMBOUT PASSING APPROX FL270 22 ENG 1 STRUT OVERHEAT 22 LIGHT ILLUMINATED. PERFORMED THE APPROPIATE RED TAB PROCEDURE AND LIGHT EXTINGUISHED. AFTER CLOSING N1 BLEED. SUSPECT AIR BLEED LEAK ITS ON THE FUSELAGE SIDE OF THE BLEED AIR VALVE PER RED TABS. PERFORMED HI-POWER NUMBER 1 ENGINE RUN-UP WITH CREW. FOUND AT NUMBER 1 BLEED AIR VALVE EXIT 2C CLAMP LOOSE. ADJUSTED CLAMP PROPERLY CHECK NO AIR LEAKS 22 ENG 1 STRUT OVERHEAT 22 LIGHT NOT ILLUMINATED DURING THE HI-POWER ENGINE RUN-UP. 2L73 4F RTA3WE 20030820000092003082000009NM 2003 8 20 03FDEA01130 120030723A3260189915 UPLOCK SENSOR BOEING727 727200 138407ENM ZONE 700 FAILED A FDEAK NONE J WARNING INDICATION CLCLIMB 1 SO25220FE 20934 AFTER TAKEOFF LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. COMPLIED WITH QRH AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LEFT MAIN GEAR UP AND LOCKED PROX SENSOR (M827) IAW 727 WDM 32-60-01 SENSOR NEEDS TO BE REINSTALLED AND OP'S CHECKED. REPLACED LEFT MAIN GEAR UPLOCK SENSOR IAW 727 MM 32-61-081-4. OPS CHECK GOOD. OK FOR SERVICE. 2L73 4F RTA3WE 20030820000102003082000010NM 2003 8 20 03FDEA01185 120030731A5312 SKIN BOEING727 727200 138407ENM NLG WW GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 NOSE WHEEL WELL SKIN GOUGED AROUND PANEL OPENING 3223 (4 PLACES) 247 - 250. BLENDED GOUGE IN WW SKIN AT BS 237. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. DAMAGE WILL BE REPAIRED ON N00468. 2L73 4F RTA3WE 20030820000172003082000017NM 2003 8 20 03FDEA00852 120030603A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 LOWER WEB OF DELTA KEEL BEAM HAS CORROSION ON UPPER SURFACE AROUND SUPPORT STRUCTURE AND LOWER SURFACE AROUND FASTENER HEADS, BS 740-870. REMOVED AND REPLACED LOWER WEB OF DELTA KEEL BEAM BS 740 TO BS 870 RBL 5 TO LBL 5 PER SRM 51-20-1. 2L73 4F RTA3WE 20030820000222003082000022NM 2003 8 20 03FDEA01007 120030625A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT WING INBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BORE FOUND CORROSION. RT WING INBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BORE CORROSION REPAIR CARRIED OUT IN ACCORDANCE WITH FEDEX EA 1-5750-69360 - WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBOARD FLAP HINGE BRACKET ASSEMBLY - REPAIR. 2L73 4F RTA22WE 20030820000302003082000030NM 2003 8 20 03FDEA00857 120030504A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 HFEC INDICATION FOUND IN INBOARD & OUTBOARD PIVOT HOLE BORE SURFACE ON OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) RT WING. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-66421 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE AFT SUPPORT BORE CORRODED. 2L73 4F RTA22WE 20030820000312003082000031EU 2003 8 20 03FDEA01124 120030722A5347A5327828622300 SEAT TRACK AIRBUS300 A300B4605R 3930308EU ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25659FE 757 DURING OFFLOAD, HUB ADVISED BROKEN YZ LATCH LOCK IN POS 11RT. CLOSE INSP NOTED SEAT TRACK DAMAGED. REPLACED LATCH IAW A300-600 AMM 25-58-00 AND SEAT TRACK ADAPTER REPLACED IAW EA 6-5310-71945 PT 2. 2L72 4F RTA35EU 20030820000342003082000034NM 2003 8 20 03FDEA01069 120030625A5730APB74411 SKIN DOUG MD11 MD11 3023602NM WING BOX CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 MAIN DECK - BETWEEN BS 1160-1170, RIGHT XCW 80-100, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK. 2L73 4F RTA22WE 20030820000352003082000035NM 2003 8 20 03FDEA01068 120030625A5730APB74411 SKIN DOUG MD11 MD11 3023602NM CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 MAIN DECK - BETWEEN BS 1215-1235, RIGHT XCW 50-115, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK. 2L73 4F RTA22WE 20030820000442003082000044NM 2003 8 20 03FDEA01137 120030723A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT O/B FLAP (FLAP SIDE) - I/B HINGE I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACE CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE- I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS - TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030820000532003082000053NM 2003 8 20 03FDEA00882 120030616A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 CORROSION (C53-113-01) FWD CARGO STA 660, RBL 6 IN STR 28R. REMOVED CORROSION AND REPAIRED STR 28 RT AT BS 660 PER SRM 53-10-1, 53-10-3, FIG 1. 2L73 4F RTA3WE 20030820000792003082000079EU 2003 8 20 03FDEA00915 120030619A5315 FLOORBEAM AIRBUS300 A300F4605R 3930327EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE 742 FWD CARGO CROSS BEAM AT FRAME (30) IS CRACKED APPROX 1.5 INCH LONG, 18 INCHES RIGHT OF CENTER. REPAIRED IAW SRM 53-10-15 FIGURE 208 SHEET 2. 2L72 4F RTA35EU 20030820000832003082000083NM 2003 8 20 03FDEA00870 120030522A5753ARC70551 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LT WING - OUTBOARD TRAILING EDGE FLAP VANE ASSY FOUND NR 3 VANE TRACK SUPPORT'S FWD MOST MOUNT HOLE WITH CORROSION IN BORE SURFACE (NUMBERED FROM INBOARD). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-71714 - WINGS - LEFT OUTBOARD FLAP VANE - NR 3 VANE TO TRACK SUPPORT CORRODED. 2L73 4F RTA22WE 20030820000932003082000093CE 2003 8 20 DXTA200300047 120030614A3297 WIRE HARNESS CESSNA500 560CESSNA 2076750CE ANTI SKID SYS DEFECTIVE E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07330QS 5600329 ON LANDING, BRAKE PRESSURE AVAILABLE BUT SLOW TO APPLY. DURING TAXI IN, ABOUT 10 MPH, BRAKES RELEASE AND ENGAGE INTERMITTENTLY. TROUBLESHOT AND FOUND RT ANTI-SKID WIRING HARNESS DEFECTIVE. REMOVED & REPLACED HARNESS IAW 560 M/M CH 32-42-07, OPS CHECKED GOOD. 2L72 4F RTA22CE 20030820000942003082000094NM 2003 8 20 UPS03640985 120030721A5420 SUPPORT BRACKET BOEING767 767300 1385204NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01322UP 27748 PER A/C STATUS DURING REPAIR OF CDL 262636 FOUND VERTICAL SUPPORT BRACKET CRACKED AT UPPER ANGLE. REPAIRED IAW SRM 54-52-70. 2L72 4F RTA1NM 20030815000792003081500079SW 2003 8 15 HEEA088526 120030711A6700 BEARING BELL 206 206L4 1182110SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 BEARINGS WORN. IN SHOP REPAIR. 1G71 3U NCH2SW 20030815000922003081500092NE 2003 8 15 HEEA088379 120030708A62407645001076103 INDICATOR SKRSKYS76 S76A 8143006NE TRIPLE TACH INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 TRIPLE TACH ROTOR NEEDLE OPERATION INTERMITTENT. 1G72 3U H1NE 20030815000992003081500099NE 2003 8 15 HEEA088399 120030802A62207610600701101 BOLT SKRSKYS76 S76A 8143006NE MAIN ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 MAIN ROTOR HEAD BOLT WORN. SHOP REPAIR. 1G72 3U H1NE 20030818000232003081800023SW 2003 8 18 HEEA088456 120030718A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW MAIN ROTOR WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 MAIN ROTOR ACTUATOR WEAK. 1G71 3U H2SW 20030818000272003081800027SW 2003 8 18 HEEA088464 120030714A8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 STARTER WOULD NOT ENGAGE. 2G72 4U H10SW 20030818000722003081800072 2003 8 18 HEEA088588 420030714A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 ADI INDICATOR INOPERATIVE. WILL NOT CAGE. IN SHOP REPAIR. 1G71 3U H2SW 20030818000732003081800073SW 2003 8 18 HEEA088594 120030726A3212D24922117 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MLG EMERGENCY FLOAT LEAKING. SHOP REPAIR. 1G72 4U H4SW 20030819000302003081900030NM 2003 8 19 USAA030103 120030601A5347 SEAT TRACK BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US40013 23990 FOUND SEAT TRACK CORRODED .5 INCH BY 1 INCH OF CORROSION, RIGHT INBOARD SEAT TRACK STATION 907. CORROSION LEVEL 1. REMOVED CORROSION, BLEND OUT, PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20040310000062004031000006EA 2004 3 10 A6WA200340108 120030715A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A A6WAK NONE F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL31416AW3710 7603 STAB TRIM CHANNEL 1 DISCONNECT WHEN YOKE TRIM SWITCH ENGAGED FROM EITHER SIDE. FERRIED TO DEN. REMOVED AND REPLACED HORIZ STAB P/N 8396-2 S/N 827, AND MCU P/N 7062-3 P/N 849, IAW AMM 27-42-01. OPS CHECK GOOD. REPORT CONFIRMED FAULT REMOVED REPLACED CH1 RVDT. REMOVED AND REPLACED DEFECTIVE RESISTOR, IC, DIODE AND INDUCTOR. (M) 2L72 4F RTA21EA 20030819000382003081900038WP 2003 8 19 AALA20030639 120030607A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21973TW 53623 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 7DEF INOPERATIVE. REATTACHED EMERGENCY EXIT LIGHT WIRES AT SEAT 7DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030819000942003081900094WP 2003 8 19 UPS03841045 120030718A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C2 CABIN FLOOR TRACK -G- WORN SCALLOP AT FS 505.0. CUT OUT SEAT TRACK IAW DC8 SRM 53-2-3 & 51-3-0. INSTALLED SEAT TRACK AND SPLICES IAW DC8 SRM 53-2-3. 2L74 4F RT4A25 20030819000982003081900098EA 2003 8 19 03220643 120030808A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27643BR 7363 DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030819001152003081900115NM 2003 8 19 2003UALA00498 120030612A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29196UA 28715 EEL LIGHTS INOPERATIVE AT THE FOLLOWING LOCATIONS SEAT 39HJK, 42(OVHD), 16 (OVHD), EXT EEL RT SIDE 4TH ASSY AFT BULB. 2L74 4F4 FRTA20WE E24NE 20030819001292003081900129WP 2003 8 19 UPS03840911 120030612A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3, EXTERIOR FUSELAGE SKIN STA 670 ON CENTERLINE OF BELLY, SKIN AT ANTENNA MOUNT FOUND TO BE CORRODED. BLENDED CORROSION. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED DOUBLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1 AND 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS AND FINGER DOUBLERS IAW DC8 SRM 51-1-20D & 51-1-20B. 2L74 4F RT4A25 20030819001922003081900192 2003 8 19 SWAA031781 420030808A2565D31354 SLIDE BOEING737 7377H4 1384404NM FWD SVC DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030819002282003081900228NM 2003 8 19 C1HA200381028 120030813A2710 MOUNT BOEING727 7272S7 138407ZNM AILERON TAB CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 LT INBOARD AILERON TAB MOUNT, CENTER AND OUTBOARD FITTINGS CRACKED. 2L73 4F A3WE 20030819002352003081900235NM 2003 8 19 234TR0010 120030725A5330 SKIN BOEING737 737228 13844AGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 FUSELAGE SKIN CRACKED AFT OF COOLING AIR EXHAUST VENT. REPAIRED PER BOEING SB 737-53-1117. 2L72 4F RTA16WE 20030819002372003081900237NE 2003 8 19 2003UALA00522 220030628A72309512M28G09 VANE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COMPRESSOR UNSERVICEABLE A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29386UA 24661 724453 AIRCRAFT RETURNED TO FIELD AFTER ENGINE HAD A COMPRESSOR STALL JUST AFTER TAKEOFF. DISASSEMBLY OF THE ENGINE SHOWED TEARS AND MISSING MATERIAL ON COMPRESSOR BLADES AND VANES STAGES 6 THROUGH 9 DUE TO A STAGE 8 VANE SECTOR HONEYCOMB FAILURE. FAILURE OF THE HONEYCOMB IS A RESULT OF SEAL SLOT CRACKING WHICH EVENTUALLY ALLOWS THE HONEYCOMB TO SEPARATE FROM THE VANE SECTOR. THE HONEYCOMB IS INSTALLED WITH A TIGHT SNUG FIT TO THE SEAL SLOTS. BECAUSE OF THE THIN SLOT WALLS AND SNUG HONEYCOMB FIT A CAUTION WAS ADDED IN THE JOB INSTRUCTION CARD (JIC) WHEN INSTALLING VANES SECTOR SEALS TO ENSURE STRESS RISERS ARE NOT INTRODUCED TO THE SEALS SLOTS DURING HONEYCOMB INSTALLATION. 2L72 4F4 FRTA16WE E2GL 20030820000022003082000002WP 2003 8 20 UPS03841119 120030815A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AS PER MM 33 50 01 2. 2L74 4F RT4A25 20030820000682003082000068NM 2003 8 20 03FDEA01111 120030718A5414 SKIN BOEING727 727200 138407ENM NR 2 NACELLE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 NR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350. FOUND AREA ON 1350 RING CHORD TO HAVE 100 PERCENT MATERIAL LOSS AND CRACKED OUT OF LIMITS. REMOVED 1350 RING CHORD. DRILLED UP AND INSTALLED NEW 1350 CHORD IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20030820000842003082000084NM 2003 8 20 03FDEA00833 120030526A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD AFT FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR ROD-END HOLES, LT AND RT BUSHINGS LOOSE, WORN (FLAP SIDE). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69347 - WINGS - LT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030820001062003082000106WP 2003 8 20 UPS03841030 120030704A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE BENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, AFT PIT AT STA 1255 L29R LONGERON SPLICE BENT. REMOVED LONGERON SECTION. LOCATED & DRILLED NEW LONGERON SECTION AND SPLICES IAW DC8 SRM 51-1-24. INSTALLED LONGERON AND SPLICED IAW SR M DC8 51-1-20D. 2L74 4F RT4A25 20030820001082003082000108NM 2003 8 20 UPS03440971 120030618A542065B904124748 WEB BOEING747 747123 1384873NM NR 2 NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: C, NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD, CRACK REVEALED AT I/B SIDE AFT FRAME WEB LOWER EDGE AS MARKED. NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD FRAME WEB REPAIRED AS PER RS R54-53-35039 AND ENGINEERING FILE NUMBER 747-54-20037. 2L74 4F A20WE 20030820001262003082000126WP 2003 8 20 UPS03841110 120030726A5311561214853 FRAME DOUG DC8 DC873F 302199FWP AFT CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C2, MAIN CABIN CANTED FRAME IS CORRODED BEYOND LIMITS AT STA 1746 AT LONG 26L. REMOVED CANTED FRAME BETWEEN LONG 26L TO 36, FABRICATED AND INSTALLED FRAME AND SPLICES IAW DWG 5612148 AND SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20030820001462003082000146CE 2003 8 20 DXTA200300048 120030614A3260 UPLOCK SWITCH CESSNA750 750 2076810CE MLG OUT OF RIG E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07912QS 7500012 GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION FOR SEVERAL MINUTES. RIGGED LANDING GEAR UPLOCK SWITCHES IAW THE CESSNA CITATION 750 M/M CH 32-30-05. FUNCTIONAL TEST OF LANDING GEAR SYSTEM REVEALED NO DEFECT PER CESSNA MM CH 32-00-01. 2L72 4J RTT00007WI 20030820001532003082000153EA 2003 8 20 COMA0370025 120030809A2750 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA TE FLAPS ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01369CA 10079 FLIGHT 5668 ABORTED T/O FOR FLAP CONFIG WARNING. T/O WAS SUCCESSFUL ON SECOND ATTEMPT. 2L72 4F RTA21EA 20030820001632003082000163EA 2003 8 20 COMA0360362 120030808A3000 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01915CA 7013 FLIGHT 5316 ANTI ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE. NO FAULTS FOUND DURING ANTI ICE OPERATION. 2L72 4F RTA21EA 20030820001652003082000165NM 2003 8 20 CALA0300378 120030711A2121731376A COOLING FAN BOEING757 757224 1384958NM E&E COMPT INOPERATIVE A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW273413121859 28971 AN ELECTRICAL BURNING ODOR WAS OBSERVED IN THE CABIN AND COCKPIT WHILE EN ROUTE FROM EWR TO SFO. THE ODOR WAS ACCOMPANIED BY AN EQUIP COOLING FAN OVERHEAT LIGHT ILLUMINATING. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 EQUIP COOLING FAN AT FAULT. THE COOLING FAN WAS REMOVED AND REPLACED IAW MM 21-58-06 AND OPERATIONAL CHECKS WERE GOOD. THE E&E COMPARTMENT WAS CHECKED FOR BURNED WIRING AND NONE WAS FOUND. 2L72 4F RTA2NM 20030820001672003082000167NM 2003 8 20 UPS03241066 120030714A5330 SKIN BOEING727 72725C 138400HNM DOOR CUTOUT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, EVIDENCE OF CRACK AROUND FASTENER AT MID GALLEY DOOR CUTOUT BS 640, S-8L. REPAIR CARRIED OUT IAW SMRO EO 2003-041-004. REFERENCE UPS EO B727- 5330-19065. 2L73 4F A3WE 20030820001762003082000176 2003 8 20 SWAA031743 420030803A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030820001782003082000178NM 2003 8 20 SWAA031744 120030805A53116546546 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, BETWEEN STR 22R AND STR 23R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030820001822003082000182EA 2003 8 20 COMA0360350 120030806A3260864002 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA LT MLG MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01912CA 7011 FLIGHT 5791 GEAR DISAGREE WARNING, LT MLG INDICATED INTRANSIT. REPLACED THE LT MLG UPLOCK PROXIMITY SENSOR. 2L72 4F RTA21EA 20030820001962003082000196NM 2003 8 20 03FDEA01263 120030721A5543 TAB BOEING727 727100 1384036NM ZONE 300 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25103FE 19199 LOWER RUDDER TAB 2FH SIDE UPPER END IS DELAMINATED AT AFT END. 2L73 4F RTA3WE 20030820002102003082000210EU 2003 8 20 ASOA03334 120030724A5320S5397071635601 BRACKET AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE LEFT UPPER AND LOWER ATTACHMENT BRACKETS FOR THE BANANA SEAL PANEL WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT UPPER AND LOWER ATTACHMENT BRACKETS FOR THE BANANA SEAL PANEL IAW SRM 53-91-42. (M) 2H72 4T RTA53EU 20030819000642003081900064SO 2003 8 19 SWIA200312122 120030522A5415 BRACKET EMB 120 EMB120ER 3260203SO HYDRAULIC PACK CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 LEFT LOWER OUTBOARD HYDRAULIC PACK BRACKET CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED LEFT LOWER OUTBOARD HYDRAULIC PACK BRACKET WITH NEW ONE. 2L72 4T RTA31SO 20030819001122003081900112WP 2003 8 19 UPS03840918 120030618A534047507181 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, KEELBEAM TO FRAME FITTING IS CRACKED AT STA 702 LT SIDE OF KEELBEAM. REMOVED AND REPLACED FITTING IAW DWG 4750718 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20030819001182003081900118EU 2003 8 19 2003UALA00501 120030615A5230 LATCH AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR CONTAMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29420UA 489 FWD CARGO DOOR WARNING LIGHT CAME ON. DOOR HANDLE LATCH FOUND CONTAMINATED WITH DEBRIS OF AN UNKNOWN NATURE PREVENTING FULL SEATING. LATCH WAS CLEANED OF DEBRIS AND LUBRICATED. 2L72 4F4 FRTA28NM E40NE 20030328000032003032800003NM 2003 3 28 CA030212006 120030206A3230DSC252B40124 HOSE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 2 HYD SYS LEAKING W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA 3867538675 (CAN) AFTER DEPARTURE DURING GEAR UP SELECTION, LOSS OF NR 2 HYDRAULIC QUANTITY AND FAILURE OF GEAR TO RETRACT . AIRCRAFT RETURNED FOR NORMAL LANDING . MAINTENANCE INSPECTION FOUND NLG DOWNLOCK ACTUATOR FLEX LINE CRACKED/LEAKING . TEMPORARTY FLEX LINE INSTALLED AND HYDRAULIC SYSTEM RE-FILLED. LINE DSC252B4-0124 DOM 9-95 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030328000202003032800020EU 2003 3 28 CA030218005 120030216A3260ABS012110 PROXIMITY SENSOR AIRBUS320 A320212 3930322EU CFMINTCFM56 CFM565A3 NE NLG FAILED W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) AFTER TAKE-OFF AND GEAR RETRACTION, 'NLG DOOR OPEN' MESSAGE APPEARED ON ECAM. GEAR CYCLED, BUT MESSAGE REPEATED. AIRCRAFT RETURNED FROM FLIGHT. POST FLIGHT REPORT INDICATED NOSE GEAR DOOR PROX. SENSORS 30GA AND 31 GA FAILED. BOTH SENSORS REPLACED, AND SYSTEM CHECKED SERVICEABLE. AIRCRAFT RELEASED TO SERVICE. 2L72 4F4 FRTA28NM E29NE 20030328000212003032800021SW 2003 3 28 CA030218006 120030205A321121949 TUBE BBAVIA7 7GCBC 1220601SW LYC O360 O360C2E 41514EA MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRCRAFT HAS OVER 2,700 HOURS OF TOWING GLIDERS OFF A GRASS STRIP. DEFECT WAS FOUND DURING RECOVERING OF FUSELAGE. VERTICAL CRACK ON BOTH SIDES OF LT REAR GEAR 'U' BOLT BUSHING IN 'U' BOLT ATTACH TUBE. 1H71 3O3 ONCA759 E286 20030328000302003032800030EU 2003 3 28 49201 120030325A7120 MOUNT AMD FALC20FALCON200 2730150EU GARRTTATF3 ATF3* 29002WP ENGINE CRACKED E ERYAK NONE O OTHER ININSP/MAINT 1 CE07412AB5261 492 P20138 DURING THE PERFORMANCE OF A 600 ENGINE INSPECTION, FOUND CRACKS AROUND ENGINE MOUNTING PADS IN THE MID-FRAME. A LOANER ENGINE IS BEING INSTALLED, WHERE THE AFFECTED ENGINE IS BEING SENT TO GARRETT FOR EVALUATION. 2L72 4F4 FRTA7EU E7WE 20030328000322003032800032EU 2003 3 28 ASOA03088 120030304A5412S5421230500100 FIREWALL AEROSPATR72 ATR72 EU PWA PW120 PW127 NE LT NACELLE CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO11630AS 336 DURING HANGER MAINTENANCE IN MCN, THE LEFT NACELLE UPPER FIREWALL WAS FOUND TO BE CRACKED WITH MATERIAL FALLING OUT. MAINTENANCE REPAIRED THE CRACKED NACELLE FIREWALL BY INSTALLING A DOUBLER IAW SRM. 2H72 4T4 TRT E20NE 20030328000382003032800038SO 2003 3 28 C2XA03TY023 120030210A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE RAMP ANGLE AT THE FWD CENTER OMEGA BEAM WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000402003032800040SO 2003 3 28 C2XA03TY025 120030210A531314521725001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND CHAFING ON STRINGERS 19L-19R AT FRAME 53. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED BOTH AREAS IAW EMB 135/145 SRM 53-24-02. ALODINED AND PRIMED IAW EMB 135/145 CPM51-21-04;05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000412003032800041SO 2003 3 28 C2XA03TY026 120030210A322014524475003 BRACE EMB 145 EMB145LR 3260212SO NLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION MAINT FOUND CORROSION ON THE LT AND RT NLG BRACE CAPS. MAINTENANCE REMOVED AND REPLACED BOTH CAPS IAW EMB 135/145 AMM 32-20-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000542003032800054NM 2003 3 28 C8GA20030007 120030305A27512061121 INDICATOR BOEING727 7272A1 138407FNM TE FLAP DEFECTIVE A C8GAA UNSCHED LANDING O OTHER CLCLIMB 1 SO15286SC10 21601 FLT 723 FROM ROC TO TOL. AFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATOR INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGREE POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO ROC AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE OUTBOARD FLAP POSITION INDICATOR WAS REPLACED. OPERATIONAL CHECKS WERE ACCOMPLISHED IAW MM 27-52-21 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030328000602003032800060NM 2003 3 28 CALA0300098 120030216A5320 PAN BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND LAV FLOOR PAN FASTENER CORRODED AT STA 1016, RBL 13. A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-20-02. 2L72 4F RTA16WE 20030328000622003032800062 2003 3 28 CALA0300106 420030308A2565100503115 LIGHT DOUG DC9 DC982 3022082WP TAILCONE SLIDE INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW091781242094 49250 THE TAILCONE SLIDE LIGHT FAILED BATTERY TEST. THE SLIDE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 25-62-01. 2L72 4F A6WE 20030328000662003032800066NM 2003 3 28 CALA0300118 120030314A5542 SKIN BOEING737 7373T0 1384582NM RUDDER DEBONDED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916310 23361 INSPECTION FOUND LT RUDDER T/E SKIN DISBONDING IN THIRD LAYER OF EXISTING REPAIR 28 INCHES FROM LOWER END. A REPAIR WAS INSTALLED IAW ECRA 5540-01163. 2L72 4F RTA16WE 20030328000672003032800067NM 2003 3 28 CALA0300133 120030320A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A 1 INCH CRACK IN RT PRESSURE DECK AT STA 664. REPAIRED IAW SRM 53-60-51. 2L72 4F RTA16WE 20030328000702003032800070NM 2003 3 28 CALA0300142 120030325A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND AFT CARGO COMPARTMENT LOWER LOBE INTERIOR FRAME CORRODED AT BS 847 BETWEEN S28L AND S28R. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGURE 208. 2L72 4F RTA16WE 20030328000712003032800071NM 2003 3 28 CALA0300143 120030325A5512 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED IN TWO LOCATIONS: STABILIZER STATION 107.5 AND 289.1. THE AREAS WERE REPAIRED IAW SRM 55-10-1, FIGURE 203, SHEETS 1 & 2. 2L72 4F RTA16WE 20030328000722003032800072NM 2003 3 28 CALA0300144 120030326A5230 SKIN BOEING737 737524 1384721NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916618 27331 INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030328000922003032800092EA 2003 3 28 COMA0370009 120030322A291067075296001 LINE CNDAIRCL600 CL6002C10 1390015EA NR 2 HYD SYS LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01354CA930 10064 FLIGHT 5741 - NR 2 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPAIRED CHAFED HYDRAULIC TUBING IN AFT EQUIP BAY. 2L72 4F RTA21EA 20030328000992003032800099EU 2003 3 28 CX7A194J31 120030222A26121734362450 SENSOR SAAB SF340 340B 7860101EU RT TAILPIPE CONTAMINATED A CX7AEC ENGINE SHUTDOWN ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03306CE 340B203 RT ENGINE TAIL PIPE HOT WARNING CAME ON SHORTLY AFTER T/O REMAINED ON AFTER ENGINE SHUTDOWN 2L72 4T RTA52EU 20030328001052003032800105EU 2003 3 28 DHL2003362002 120030113A2612 CONNECTOR AIRBUS300 A300B4203 3930306EU NR 2 ENGINE FAILED A DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01362DH 84 ENGINE NR 2 LOOP A-LIGHT ILLUMINATED ON PREFLIGHT. RERACKED DETECTOR CONNECTOR PLUG ON CONTROL UNIT IAW A300 M/M 26-12-11. CLEANED LOOP-B AND LOOP A-FAN CASE CONNECTORS IAW A300 M/M 26-12-12. OPS CHECKED GOOD. 2L72 4F RTA35EU 20030331000182003033100018EA 2003 3 31 A6WA200340024 120030106A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 HYDRAULIC BRACKET AT FS 656 LT SIDE AT STRINGER 9 HAS AN ELONGATED THRU HOLE AT HYDRAULIC PRESSURE LINE REMOVED, REPAIRED, AND INSTALLED BRACKET. NDT PERFORMED, NO INDICATIONS NOTED. 2L72 4F RTA21EA 20030331000292003033100029WP 2003 3 31 AALA20030036 120030108A3260833703 DOWNLOCK SENSOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW21241AA 49254 ORD - FLT 357 - EN ROUTE LGA-ORD, UNSAFE NOSE GEAR INDICATION DURING APPROACH TO ORD. GEAR WAS DOWN 3 GREEN LIGHTS ALL MECHANICAL VISUAL INDICATION AGREE, ON SHORT FINAL. RECEIVED AUDIO LANDING GEAR ALONG WITH A RED LIGHT IN THE NOSE GEAR. THIS HAPPENED 304 TIMES WITH A QUICK FLASH OF THE RED LIGHT. DID A GO-AROUND AND CYCLED THE GEAR, ALL INDICATIONS WERE NORMAL AND THE NOSE GEAR FLASHED RED ONE TIME. LANDED ORD WITHOUT INCIDENT. SENSOR BAD, REPLACED NOSE GEAR DOWNLOCK SENSOR. SWUNG GEAR 4 TIMES. NO FAULTS NOTED. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000322003033100032WP 2003 3 31 AALA20030039 120030108A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 DURING OVERNIGHT MAINTENANCE, FORWARD LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000332003033100033WP 2003 3 31 AALA20030040 120030109A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW217521A 49898 DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN SEATS 8F AND 12F INTERMITTENT. CLEANED AND SECURED EMERGENCY EXIT LIGHT GROUND WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000342003033100034WP 2003 3 31 AALA20030042 120030109A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21487AA 49680 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000472003033100047WP 2003 3 31 AALA20030209 120030219A3350 BALLAST DOUG DC9 DC982 3022082WP CABIN BURNED OUT A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21249AA 49269 EN ROUTE MIA-CLT, IMMEDIATELY AFTER TAKEOFF, NR 1 FLIGHT ATTENDANT CALLED AND SAID THE CABIN WAS FILLING UP WITH SMOKE. CREW CHECKED BOTH LAVATORIES AND THOUGHT SMOKE WS COMING FROM UPPER SIDEWALL VENTS. SHUT OFF BOTH PACKS AND RECIRCULATION FAN. SMOKE SEEMED TO DISSIPATE. RETURNED AND LANDED MAI IMMEDIATELY. NR 1 FLIGHT ATTENDANT COULD NOT SEE PAST ROW 14 FROM AT FORWARD ENTRY DOOR. PASSENGERS SAID IT SMELLED LIKE ELECTRICAL. SMOKE SEEMED TO BE COMING FROM AROUND ROW 29B. REPLACED LIGHT BALLAST. GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000492003033100049WP 2003 3 31 AALA20030212 120030218A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21403A 49314 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000502003033100050WP 2003 3 31 AALA20030222 120030223A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT LIGHTS AT TAIL CONE AREA INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000522003033100052WP 2003 3 31 AALA20030230 120030221A2163 SENSOR DOUG DC9 DC982 3022082WP ACM BAY LEAKING A AALAG O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW21418AA 49329 AT CRUISE AT 33,000 FT, CREW SELECTED TAIL DE-ICE CABIN PRESSURE WOULD START TO DESCEND AT ABOUT 300 FT PER MINUTE. CREW RAN CHECKLIST AND WERE ABLE TO CORRECT PROBLEM. CABIN STARTED TO CLIMB AT ABOVE 1,000 FT PER MINUTE. AGAIN CREW WENT THROUGH CHECKLIST AND WERE ABLE TO STOP CLIMB BY TIME CABIN WAS PASSING 8,000 FT. CREW DECLARED AN EMERGENCY AND DEPLOYED OXYGEN MASKS. AIRCRAFT DESCENDED TO 9,000 FT AND CREW WAS ABLE TO CONTROL CABIN AND CLIMBED BACK UP TO 15,000 FT. LANDED TPA WITHOUT INCIDENT. REPLACED LT AIR CONDITIONING SUPPLY HIGH TEMP SENSOR AND GASKET. ACCOMPLISHED AIRFOIL ANTI-ICE TEST. ACCOMPLISHED CABIN DECAY TEST AND FOUND TO BE WITHING LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)2L72 4F A6WE 20030331000662003033100066EA 2003 3 31 ASOA03090 120030307A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ACM ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11880AS 200108160 7606 DURING DESCENT INTO MOB, AFTER STARTING THE AUXILLARY POWER UNIT AND SWITCHING THE BLEEDS, A FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN. THE FUEL ODOR DISSIPATED AFTER SHUTTING THE AUXILIARY POWER UNIT DOWN. THE AIRCRAFT SAFELY IN MOB. MAINTENANCE REMOVED AND REPLACED BOTH COALESCER BAGS ON THE AIR CYCLE MACHINE. ALSO, BOTH ENGINES WERE RAN WITH THE ENGINE BLEEDS CYCLED ON AND OFF, AND THE AUXILIARY POWER UNIT WAS SHUT DOWN AND RE-STARTED WITH THE ENGINES RUNNING. NO FUEL ODOR WAS NOTED. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030331000772003033100077NM 2003 3 31 AWXA200300320 120030317A5312651630086 FRAME BOEING737 7373S3 1384711NM 178 BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON LT SIDE FRAME OF 178 BULKHEAD, WL 195. MAINTENANCE REMOVED DAMAGED SIDE FRAME, 178 BULKHEAD, WL 195; FABRICATED A NEW REPLACEMENT SIDE FRAME PER DWG 65-16300; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3 & 6. 2L72 4F RTA16WE 20030331000792003033100079NM 2003 3 31 AWXA200300322 120030315A5320651630534 ANGLE BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK CORROSION WAS FOUND ON ANGLE AT FIRST OFFICERS SIDE STATION 219, BELOW THE RT NR 2 SLIDING WINDOW. MAINTENANCE REMOVED CORRODED ANGLE AT FIRST OFFICERS SIDE STATION 219, BELOW THE RT NR 2 SLIDING WINDOW; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-16305; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030331000882003033100088SO 2003 3 31 C2XA03SH065 120030329A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 SHV-DURING C-CHECK, REPAIR DOUBLER ON T-REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331001102003033100110EU 2003 3 31 DHL2003364001 120030124A3240 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG DISCHARGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01364DH 141 RT BRAKE PEDAL SOFT. BRAKES GRAB SUDDENLY. CHECKED AND FOUND RIGHT SIDE LOW PRESSURE BRAKE SYSTEM NEEDED REPLENISHED. REPLENISHED RIGHT SIDE PER M/M 12-12-32. CHECKED NORMAL. 2L72 4F RTA35EU 20030331001112003033100111EU 2003 3 31 DHL2003364003 120030202A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 2 ENGINE CHAFED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01364DH 141 ENGINE NR 2 LOOP-A LIGHT ILLUMINATED. ENGINE OR APU LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURES COMPLETED. DEFERRED PER MEL 26-12-01-1, DMI 11849 ASSIGNED. REF DMI 11849 - ENGINE NR 2 LOOP-A LIGHT ILLUMINATED. ENGINE OR APU LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURES COMPLETED. TROUBLESHOT FOUND WIRE BUNDLE RUBBING AGAINST A-LOOP IN HOT SECTION. REPAIRED AND SECURED WIRE BUNDLE. INSPECTED A-LOOP. NO DEFECTS NOTED RAN ENGINE AT CRUISE T/O POWER AND SYSTEM OPS CHECKED GOOD PER M/M 26-12-00. DMI CLEARED. 2L72 4F RTA35EU 20030331001242003033100124NM 2003 3 31 DHL2003740504 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FUSELAGE FRAME AT STA 600 IS DENTED AND CRACKED BETWEEN STR 16R-17R. CUT OUT DAMAGED FRAME AND FABRICATED REPAIR FROM 7075-T6 .063. CLEANED, TREATED AND PRIMED AND INSTALLED REPAIR PER SRM 51-40-1. 2L73 4F RTA3WE 20030331001382003033100138NM 2003 3 31 DHL2003740519 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH IN FWD CARGO FRAME HAS A DENT INTO THE RADIUS AT BS 680 STR 24 LT. REMOVED FASTENERS AT FRAME BS 680 STR 24L PER SRM 57-30-2. CUT OUT DAMAGED FRAME AREA PER SRM 57-40-3 FIG 1. FABRICATED FRAME REPAIR FROM 7075-T6 0.063 (12.5 X 6 INCH) PER SRM 51-40-3 FIG 1. TREATED AND PRIMED PER SRM 57-10-2, INSTALLED REPAIR PER SRM 57-40-3 FIG 1. 2L73 4F RTA3WE 20030401000052003040100005EU 2003 4 1 03089312 120030330A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27312UE 41025 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FWD EMERGENCY BATTERY PACK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030401000132003040100013NM 2003 4 1 372PA0018 120030325A3350362624 LIGHT BOEING737 737306 13844BGNM CABIN BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 AFT SECTION OF CABIN FLOOR EMERGENCY STRIP LIGHTING OUT. FOUND DIRTY SOCKETS AT INVERTER STRIP, CLEANED SAME. REMOVED AND REPLACED AFT SECTION OF FLOOR LIGHTS PER MM 33-51-21. OPS CHECK GOOD PER MM 33-51-02. 2L72 4F RTA16NE 20030328000122003032800012SO 2003 3 28 CA030214006 120030214A57200062061002 SKIN PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA WINGS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE DOUBLERS ON THE BOTTOM OF THE WING WALK SKINS JUST OUTBOARD OF THE INBOARD STAMPED STIFFENERS WERE SEVERELY CRACKED. THE AFT SKIN CRACK WAS 42CM IN LENGTH. THE FORWARD SKIN HAD 3 CRACKS 5CM IN LENGTH. THIS AREA IS NOT NORMALLY ACCESSIBLE BUT THIS AIRCRAFT HAD AN EXTRA INSPECTION HOLE INSTALLED FROM A PREVIOUS SB. THIS AREA SHOULD BE INSPECTED WITH A BORESCOPE ESPECIALLY ON HIGHER TIME AIRCRAFT. 1L71 3O3 O 2A13 E274 20030401000292003040100029EA 2003 4 1 ASOA03049 120030208A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11874AS 7551 DURNG A GROUND INSPECTION IN DFW, THE FORWARD PASSENGER DOOR EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD PASSENGER DOOR EXTERNAL EMERGENCY LIGHT LAMP. (M) 2L72 4F RTA21EA 20030401000522003040100052NM 2003 4 1 CA030220009 120030217A2910BACH8B04NN0202T HOSE BOEING737 737* NM PWA JT8 JT8D17 52049NE HYD SYSTEM RUPTURED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER SELECTING LANDING GEAR UP ON CLIMB, WARNING RED/GREEN NOSE GEAR LIGHTS ILLUMINATED. CONTACTED MCC AND WERE ADVISED TO LOWER GEAR AND CONTINUE TO MAINT BASE. FUEL REMAINING WAS NOT SUFFICIENT AND ELECTED TO RETURN. NOTICED SYSTEM "A" HYDRAULICS QUANTITY HAD DEPLETED TO ZERO. ATC ADVISED AND CFR WAS CALLED. A/C LANDED IAW 'LOSS OF SYSTEM 'A' FLUIDS NON NORMAL CHECKLIST WITH NO INCIDENTS TO REPORT. MAINTENANCE INSPECTION REVEALED NOSE GEAR LOCK ACTUATOR - LOCK PORT HOSE FOR GEAR UP FOUND RUPTURED HOSE. REPLACED HOSE AND HYDRAULICS SERVICED. SYSTEM GROUND CHECKED, SERVICEABLE WITH NO LEAKS . AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2L72 4F4 FRTA16WE E2EA 20030401000742003040100074NM 2003 4 1 DHL2003741500 120030331A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C CHECK, FUSELAGE SKIN OIL CANNING AFT BS 1050 BELOW STR 23 LT, REMOVED FASTENER AT FUSELAGE SKIN OIL CANNING AFT BS 1050 BELOW STR 23 LT IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM. APPROX. 2 X 1 INCH IAW B-727 SRM 53-30-2. 2L73 4F RTA3WE 20030401001132003040100113WP 2003 4 1 DHL2003804504 120030110A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING CTR L/E FORMER PART WITH 2 INCH CRACK AT STA XFS 521.250. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED DOUBLER ANGLE (2024.T3 AL 0.063) PER SRM PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20030401001542003040100154WP 2003 4 1 DHL2003804664 120030309A53305654693404 PANEL DOUG DC8 DC873F 302199FWP CENTERWING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LOWER FUSELAGE 723 RT CENTERWING LOWER PANEL INNER SKIN DELAMINATED CORR: R/R RH LOWER PANEL 723 IAW SRM51-3-0 PG. 1 2L74 4F RT4A25 20030401001632003040100163WP 2003 4 1 DHL2003804772 120030304A55435644220501 TAB DOUG DC8 DC873F 302199FWP RUDDER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 REMOVAL /INSTALLATION OF RUDDER TAB REQUIRED DUE TO DELAMINATION IN BOTH SIDES OF SKIN. R & R RUDDER TAB IAW MM 27-21-2 PG. 201-204 ADJUSTED RUDDER TAB IAW MM 27-21-2 PG. 204-207 REFER TO N/R 0607 FOR OPS CK 2L74 4F RT4A25 20030401001672003040100167WP 2003 4 1 DHL2003804776 120030211A53307075T6 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FWD. SERVICE DOOR- AFT LOWER JAMB CORNER CRACKED 1.562 STA. 190.000. PERFORMED MAJOR REPAIR IAW SRO8530021 , REMOVED FASTNERS IAW SRM 51-1-20D PG. 21 CUT - OUT DAMAGED AREA IAW DWG SR8530021. FABRICATED FILLER AND DOUBLER (7075T6 .063 &TRIPLER (7075T6.080) IAW DRAWING SR08530021. CLEANED TREATED AND PRIMED FILLER ,DOUBLER & TRIPLER IAW SRM 51-1-8B. INSTALLED FILLER , DOUBLER AND TRIPLER WITH NEW FASTNERS IAW DWG SR08530021 , SRM 51-1-20D PG. 9 , SRM51-1-15 PG. 1. 2L74 4F RT4A25 20030401001722003040100172WP 2003 4 1 DHL2003804782 120030215A5754 ANGLE DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING CENTER L/E FORMER AND ANGLE DOUBLER UPPER PART CRACKED.500 INCH. AT XFS 420.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21 PG. 1 , SRM 51-1-20D PG. 21 STOP DRILLED FORMER CRACK IAW SRM 57-2-0 PG. 9-10 FERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG. 1-17 , SRM 51-1-4 PG. 1-3 AND DPS1-05.3. CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ABNGLES DOUBLER IAW SRM57-2-0 PG. 9-10 AND SRM 51=1=21 PG 1 SRM 51=1=20D PG. 9 2L74 4F RT4A25 20030401001842003040100184CE 2003 4 1 DIN2003F00000 120030210A242030B10719A GENERATOR LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP NR 1 ENGINE FAILED B DINRO OTHER O OTHER NRNOT REPORTED 1 EA13127GT 625 067 SHAFT SHEARED ON GENERATOR WITH RELATIVITY LOW TIME SINCE OVERHAUL. SHAFT SHEARED .5000 INCH FROM DRIVE SPLINE, SLIGHT CORROSION CAN BE SEEN AT FAILURE POINT. PERHAPS A MORE THOROUGH NDI DURING THE LAST OVERHAUL COULD HAVE FOUND THIS DEFECT. THE GENERATOR WAS SENT OUT FOR REPAIRS, THE SHAFT WAS REPLACED, NO OTHER DEFECTS WERE NOTED AND IT IS BACK IN SERVICE. NORMAL SCHEDULED MAINTENANCE ON THESE GENERATORS IS, 1050 HOURS TSO A BEARING CHANGE IS REQUIRED, AND AT 2000 HOURS TSO, OVERHAUL IS REQUIRED. (W) 2L72 4F4 F A10CE E6WE 20030402000052003040200005SO 2003 4 2 2003F00178 120030401A3297 WIRE PIPER PA32 PA32R300 7103213SO MLG BROKEN A UDPAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP23 32R7680084 SELECTED GEAR UP AND IT OPERATED NORMALLY. ABOUT 1/2 WAY THROUGH FLIGHT, THE PILOT NOTICED THE LANDING GEAR CIRCUIT BREAKER HAD TRIPPED. IT WOULD NOT RESET. RESET THE BREAKER AND THE GEAR OPERATED NORMALLY. A BROKEN WIRE WAS DISCOVERED IN THE LEFT WHEEL WELL THAT OPERATED THE SQUAT SWITCH AND IT HAD ELECTRICALLY SHORTED. THE WIRE WAS REPAIRED AND THE GEAR OPERATED NORMALLY ON JACKS. FAR 43.9 WAS COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1L71 3O A3SO 20030625001342003062500134NM 2003 6 25 03FDEA00367 120030401A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CONVEX DENT IN SKIN AT BS 1020, JUST ABOVE STR 26L CONVEX DENT IN SKIN AT BS 1020 JUST ABOVE STRINGER 26L, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 2A, DETAIL II. REMOVED DENT 1 INCH DIAMETER X .063. FABRICATED REPAIR AND INSTALLED IAW SRM 53-30-3 FIG. 24 USING .063 2024-T3 2L73 4F RTA3WE 20030402000282003040200028NM 2003 4 2 2003UALA00235 120030301A2780755299B ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLAT WORN A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29571UA3530035300 26681 SLAT DISAGREE INDICATION CAME ON AFTER TAKE-OFF. INHIBITED SLAT MOVEMENT DUE TO FAULTED NR 11 LEADING EDGE SLAT ACTUATOR. REMOVED AND REPLACED THE SUBJECT LEADING EDGE SLAT ACTUATOR WITH NEW SERVICEABLE ACTUATOR 2L72 4F4 FRTA2NM E17NE 20030402000442003040200044NM 2003 4 2 2003UALA00321 120030325A5313 STRINGER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29789UA 26935 STRINGER AT STA 500 TO 520 LEFT SIDE OF FUSELAGE DAMAGED. MAJOR REPAIR ACCOMPLISHED WITH STRINGER SPLICE 2L72 4F4 FRTT0001SE E46NE 20030402000542003040200054NM 2003 4 2 2003UALA00331 120030326A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 847, STR 8L FRAME WEB IS CRACKED AT FASTENER HOLE MAJOR REPAIR ACCOMPLISHED. CRACK REMOVED, REPAIR DOUBLER INSTALLED 2L72 4F4 FRTA16WE E2GL 20030402000662003040200066NM 2003 4 2 2003UALA00343 120030303A5754114W42102 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 14 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 14 SLAT, WITH BULB SEAL FOAM CORE SECTION IS MISSING. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030819001572003081900157NM 2003 8 19 2003UALA00514 120030619A3350362624 LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29936UA 26667 AFT FLOOR EMERGENCY EXIT LIGHTING (EEL) INOPERATIVE AT THE GATE. REPLACED EEL LAMP STRIP. GROUND TEST EMERENCY LIGHT SYSTEM, CHECKS NORMAL. 2L72 4F4 FRTA16WE E2GL 20030819001592003081900159NM 2003 8 19 2003UALA00595 120030728A2752 FLAP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE WINGS FAILED A UALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP29949UA 26692 WING FLAPS WOULD NOT GO TO POSITION 40 WHEN SELECTED. MADE FLAPS 30 LANDING. INSPECTION REVEALED THAT THE NR 3 AND 6 FLAP JACKSCREWS HAD SURFACE CORROSION. THE JACKSCREWS AND BALLNUTS WERE REPLACED. THE NR 3 AND 6 JACKSCREWS AND BALLNUTS WERE REPLACED. THE AIRCRAFT WAS TESTED AND NO FAULTS WERE FOUND. UPON FURTHER INSPECTION IN THE SHOP IT WAS NOTED THAT THE CORROSION ON THE JACKSCREWS HAD COME FROM THE BALLNUTS. INTERNAL INSPECTION OF THE BALLNUTS REVEALED SEVERE PITTING AND CORROSION DUE TO FAILURE OF THE INTERNAL CHROME PLATING. 2L72 4F4 FRTA16WE E2GL 20030819001962003081900196EA 2003 8 19 SWIA200312207 120030723A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07923SW4427 4427 7681 STAB TRIM CH 1 WILL NOT ENGAGE. INSTALLED SERVICEABLE STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01 AND 27-42-05. MCU P/N OFF/ON 7062-3, S/N OFF 230, S/N ON 468. OPS CHECK GOOD. 2L72 4F RTA21EA 20030819002092003081900209NM 2003 8 19 UPS03241006 120030711A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, LIGHTNING STRIKE DAMAGE AT BS 590 S25R. FASTENER REMOVED AND AREA CLEANED IAW SRM 51-30-02. HFEC INSP CARRIED OUT ON DAMAGED AREA IAW B727 NDTM PT 6 FIG 4. RESULT CRACK FOUND AS MARKED ON A/C & ENDS OF CRACK MARKED. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 13. 2L73 4F A3WE 20030819002232003081900223EA 2003 8 19 SWIA200312139 120030620A3397 GROUND WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSLOOSE A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07455SW 7760 EMERGENCY LIGHTS COME ON WITH SWITCH IN OFF POSITION AND AC POWER ON THE AIRCRAFT. FOUND GROUND STUD N1011 LOOSE. TIGHTENED GROUND STUD N1011, SYSTEM OPS CHECK GOOD. 2L72 4F RTA21EA 20030819002392003081900239NM 2003 8 19 2003UALA00525 120030629A2613 WARNING LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE WING-BODY OVERHTFALSE INDICATIONA UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29928UA 26651 AIRCRAFT DIVERTED EN ROUTE DUE TO A WING-BODY OVERHEAT INDICATION. AIRCRAFT EXPERIENCED LEFT WING-BODY OVERHEAT WARNING INDICATION IN CRUISE FLIGHT WITH APU SUPPLYING AIR. WING-BODY OVERHEAT INDICATION LIGHT EXTINGUISHED PER THE IRREGULAR PROCEDURE. AIRCRAFT DIVERTED TO ABQ AND LANDED WITHOUT INCIDENT. ACCOMPLISHED INSPECTION OF THE AIRCRAFT. LEFT WING-BODY OVERHEAT INDICATION SYSTEM CHECKED NORMAL PER THE TROUBLESHOOTING PROCEDURES. MAINTENANCE ALSO PERFORMED INSPECTION OF LEFT AIR-CONDITIONING BAY, WING LEADING EDGE AREA, AND AFT CARGO COMPARTMENT FOR SIGNS OF PNEUMATIC LEAKS. NO LEAKS WERE FOUND AND AIRCRACT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20030820000272003082000027NM 2003 8 20 03FDEA00793 120030505A5753ARC050312 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING, OUTBOARD FLAP, OUTBOARD FWD HINGE WITH ACTUATOR HOLES CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69243 WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030820000692003082000069NM 2003 8 20 03FDEA01112 120030718A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 CORROSION ON FRAME SHEAR TIE AND FUSE SKIN AT BS 720C LBL 12, WL 150. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM, 51-30-2, 51-10-1, 53-10-1, 51-10-2, 51-10-3. 2L73 4F RTA3WE 20030820000742003082000074NM 2003 8 20 03FDEA00861 120030606A5310 ANGLE BOEING727 727200 138407ENM CARGO DOOR BEAM CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25487FE 21490 WHILE WORKING CARD 00357 (DOOR 6030) DISCOVERED A CORROSION ON LOWER BEAM ANGLE WEB 45 INCHES AFT OF FWD EDGE 1.5 INCHES UP FROM BOTTOM EDGE ON NR 1 CARGO DOOR. REMOVED CORROSION ON LOWER BEAM ANGLE WEB 45 INCHES AFT OF FWD EDGE, FOUND TO BE OUT OF LIMITS. LOCATED HOLES ON NEW ANGLE AND INSTALLED PART IAW SRM 51-30-2. 2L73 4F RTA3WE 20030820001122003082000112NM 2003 8 20 UPS03240994 120030710A7830 SUPPORT BRACKET BOEING727 72725C 138400HNM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, ENG NR 3 THRUST REVERSER OUTER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-01. 2L73 4F A3WE 20030820001322003082000132NM 2003 8 20 CALA0300432 120030731A5753 ANGLE BOEING737 7373T0 1384582NM NR 3FLAP TRACK CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND A .25 INCH CRACK IN I/B ATTACH ANGLE AT HYD ACCESS PANEL ON REAR SPAR O/B OF NR 3 FLAP TRACK FAIRING. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 57-53-71. 2L72 4F RTA16WE 20030820001442003082000144WP 2003 8 20 UPS03840975 120030711A5610 HINGE PIN DOUG DC8 DC871F 302199DWP COCKPIT WINDOW OUT OF ADJUST A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: PFLT, F/O'S COCKPIT WINDOW WILL NOT OPEN PROPERLY. *SUPPLEMENTAL MRR* T/S TO AFT WINDOW HINGE PIN OUT OF PLACE. REINSTALLED AFT HINGE PIN. PERFORMED ADJ, TEST ALL CKS GOOD. 2L74 4F RT4A25 20030820001572003082000157NM 2003 8 20 2003UALA00487 120030602A21616259410 CONTROLLER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT PACK TEMP MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29651UA 25389 RIGHT PAC TEMP EICAS MESSAGE ILLUMINATED. THE PACK TEMP CONTROLLER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. SHOP FOUND NO FAULTS WITH THE CONTROLLER. 2L72 4F4 FRTA1NM E24NE 20030820001802003082000180NM 2003 8 20 SWAA031746 120030805A531169353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 363, BETWEEN STR 14R AND STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030820001992003082000199NM 2003 8 20 03FDEA00970 120030617A5753ARC0502506 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING- O/B FLAP I/B HINGE O/B LOWER STUD (NUT SIDE) FOUND SURFACE CORROSION. RIGHT WING- O/B FLAP I/B HINGE AFT SURFACE OF O/B LOWER STUD (NUT SIDE) AREA REPAIRED AS PER FEDEX EA 1-5750-69386, TITLE: WINGS- TRAILING EDGE FLAPS- OUTBOARD TRAILING EDGE FLAPS- INBOARD FLAP SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030820002172003082000217EA 2003 8 20 ASOA03333 120030721A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11900EV 7608 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTS BETWEEN SEATS 10-C/D AND 11-C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LAMP STRIP BETWEEN SEATS 10-C/D AND 11-C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030820002282003082000228SO 2003 8 20 ASOA03308 120030714A3397M2275941249 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11639AS 120283 FLT 4824 - DURING A GROUND INSPECTION IN DFW, THE GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED LOOSE WIRING TO THE EMERGENCY LGIHTS UNDER THE GALLEY FLOOR. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030820002292003082000229EA 2003 8 20 ASOA03343 120030725A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11828AS 7213 DURING A C-CHECK IN MCN, THE SEAT TRACKS ON THE LEFT AND RIGHT SIDES AT FS 349 AND LBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SEAT TRACKS ON THE LEFT AND RIGHT SIDES AT FS 349 AND LBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030820002342003082000234EA 2003 8 20 ASOA03319 120030712A5210601R3190169 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING A GROUND INSPECTION IN DFW, THE MAIN PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE MAIN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030821000032003082100003NM 2003 8 21 USAABB03117 120030724A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU 22192 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030821000042003082100004EA 2003 8 21 ASOA03324 120030719A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11828AS 7213 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGH SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20030821000062003082100006EA 2003 8 21 ASOA03322 120030719A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING HANGAR MAINTENANCE IN BTR, THE EXTERIOR RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR RIGHT AFT EMEGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030821000072003082100007EU 2003 8 21 ASOA03329 120030710A5320 ANGLE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURING A C-CHECK IN BNA, THE RIGHT Z-ANGLE BETWEEN FS 39 AND FS 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT Z-ANGLE BETWEEN FS 39 AND FS 41 IAW SRM 51-25-01 AND 51-25-02. (M) 2H72 4T RTA53EU 20030821000122003082100012NM 2003 8 21 USAASB03116 120030719A5240 PROGRAMMING ARM BOEING737 7373B7 1384580NM SERVICE DOOR OUT OF ADJUST A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19515AU 23701 AFTER TAKEOFF FROM PHL, CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL PRESSURIZATION MODES. OUTFLOW VALVE WAS SHOWING CLOSED. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE PROGRAMMING ARM ADJUSTMENT ON THE AFT RIGHT SERVICE DOOR LOOSE AND OUT OF ADJUSTMENT. ADJUSTED DOOR AND TIGHTENED LOCK. OPERATIONAL CHECK GOOD. DOOR WARNING SYSTEM OPERATIONALLY CHECKS GOOD PER MM 52-41-21. ACCOMPLISHED SATISFACTORY PRESSURIZATION CONFIDENCE CHECK PER JOB CARD. (M) 2L72 4F RTA16WE 20030821000152003082100015NM 2003 8 21 USAASB03115 120030719A3610 CLAMP BOEING737 7373B7 1384580NM PNEUMATIC DUCT LOOSE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19373US 22952 ON CLIMB-OUT FROM PIT, AT FL170, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED WHEN THROTTLE WAS RETARDED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE TIGHTENED A LOOSE PNEUMATIC DUCT CLAMP ON NR 1 ENGINE. LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030821000202003082100020NM 2003 8 21 USAASB03119 120030721A27501817389 TRANSMITTER BOEING737 7373B7 1384580NM TE FLAPS FAILED A USAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA19529AU 24411 ALB - FLT 970 - ON APPROACH INTO ALB, THE TRAILING EDGE FLAPS SPLIT AT 15 UNITS. AT 25 UNITS, THE FLAPS WOULD NOT MOVE. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP POSITION TRANSMITTER PER MM TASK 27-58-12-004-001. OPS CHECK GOOD. ALSO, REMOVED AND REPLACED ALTERNATE FLAP DRIVE MOTOR P/N 793T100-7, PER MM TASK 27-51-59-404-007 FOR NOT DRIVING FLAPS UP. OPERAITONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030821000422003082100042GL 2003 8 21 03FDEA01123 220030721A7200 ENGINE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 3 MALFUNCTIONED A FDEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO25361FE68751 48260 451352 NR 3 ENG HUNG DURING HIGH ALTITUDE SHUT DOWN. RELIGHT AND FAILED TO RECOVER DURING DESCENT RESULTING IN NR 3 ENG SHUT DOWN. 2L73 4F4 F A22WE E23EA 20030821000442003082100044NM 2003 8 21 03FDEA01021 120030625A5753ARC050311 FITTING DOUG MD11 MD11 3023602NM TE FLAP HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING - OUTBOARD T/E FLAP, FWD OUTBOARD HINGE FITTING FOUND HYDRAULIC ACTUATOR ASSEMBLY MOUNT HOLE INBOARD SIDE WITH CORROSION (WING SIDE FITTING). REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69356 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030821000732003082100073NM 2003 8 21 03FDEA00865 120030608A3620 CONTROLLER DOUG MD11 MD11 3023602NM MANIFOLD FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25580FE 48471 AIR MANFOLD NR 2 FAIL ALERT- COMPLIED WITH QRC PROCEDURES RETURNED TO KEWR- NORMAL LDG 4L. FOUND AIR LEAK AT CLAMP ON AFT END OF PRECOOLER ASSY. REPLACED CLAMP AT NR 2 PYLON PRECOOLER AFT END PER MM 36-13-01-2 LEAK CHECK GOOD WITH AIR FROM AIR START. REPLACED MANIFOLD FAILURE DETECTION CONTROLLER AS PER 36-23-01-4 - OPS AND RTS NORMAL. RAN NR 2 ENG PER JRH AT POWER, NO FAULTS, PERFORMED DECAY CHECK PER JRH 7-10, PASSED. MANIFOLD PRESSURE DROPPED FROM 40 PSI TO 30 PSI IN 25 SEC WITH A TEMP OF 105C. CHECKED MFC AFTER RUN, NO CURRENT FAULTS, NO FAULTS IN REVIEW AND PASSED RTS. 2L73 4F RTA22WE 20030821000742003082100074WP 2003 8 21 03FDEA00864 120030610A2751 WARNING SYSTEM DOUG DC10 DC1030 3023501WP COCKPIT MALFUNCTIONED A FDEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO25316FE 48314 ON APP AT GEARDOWN 4 GREEN AND FLAPS 35 LVL 2 ALERT SLAT DISAG DURING GO-AROUND AT FLAPS 22 ALERT WENT OUT. CLEANED UP CONFIG AND RECYCLED GEAR AND FLAPS ON DOWNWIND. GEAR FLAPS AND SLATS ALL WORKED NORMAL. FLAPS 50 NORMAL LANDING. PERFORMED FCC RTS WITH NO FAULTS. ALSO, CHECKED FOR CURRENT /FAULT REVIEW IN ALL AIU'S PER FIM. A/C OK FOR SVC. 2L73 4F A22WE 20030821000872003082100087NM 2003 8 21 03FDEA00807 120030523A5753ARC198414 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP - HINGE AFT FITTING FOUND INBOARD ACTUATOR BORE WITH MINOR CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69346 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030821000922003082100092NM 2003 8 21 03FDEA00689 120030507A5510ALC8100 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 HORIZONTAL STAB CENTER BOX LT 31L BORE EXISTING BUSHING REMOVED FOUND BORE SIDEWALL AND BEARING SURFACE WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR. 2L73 4F RTA22WE 20030819002262003081900226WP 2003 8 19 UPS03840980 120030618A531447507182N FITTING DOUG DC8 DC873F 302199FWP LOWER FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, EXTERIOR FUSELAGE KEELBEAM TO FRAME ATTACH FITTING IS CRACKED AT STA 702 RT SIDE OF KEELBEAM INSIDE STRESS PANEL AT LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 4750718 AND SRM 51-1-20D. 2L74 4F RT4A25 20030819002332003081900233NM 2003 8 19 CALA0300371 120030708A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717309 23360 INSPECTION FOUND A 3 INCH CRACK IN PRESSURE DECK AT STA 665, RBL 35, JUST O/B OF J-BOX IN RT WHEEL WELL CEILING. THE PRESSURE DECK WAS REPAIRED IAW SRM 53-60-51, PAGE 213-221. 2L72 4F RTA16WE 20030819002402003081900240NM 2003 8 19 2003UALA00526 120030630A2120 DUCT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN PRESSURE COLLAPSED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29654UA 25392 UNABLE TO MAINTAIN CABIN PRESSURIZATION. FORWARD EQUIPMENT COOLING FORWARD EXHAUST VALVE DUCT WAS FOUND SMASHED AND THE FORWARD EQUIPMENT COOLING OVERBOARD EXHAUST VALVE HINGE WAS CRACKED. THE DUCT AND VALVE WERE REPLACED. A FOREIGN OBJECT PENETRATED THE DUCT AND DAMAGED THE VALVE. THE SHOP FINDING OF THE REMOVED VALVE INDICATED THAT THE ACTUATOR OPERATED NORMALLY BUT THE HINGE WAS CRACKED. THAT COULD CAUSE MISALIGNMENT OF THE ACTUATOR DOOR. 2L72 4F4 FRTA1NM E24NE 20030819000462003081900046NM 2003 8 19 AALA20030547 120030501A5310 BEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21370AA 25197 THE 9-10 BEAM BOTH LEFT AND RIGHT HAD CORROSION REMOVED IN THE 2ND HOLE FROM OUTBOARD END, LEFT HOLE AT 463 AND RIGHT HOLE AT .532. FABRICATE A1-N1-BR BUSHING WITH .001 INTERFERENCE FIT WET WITH BMS 6-95 SEALANT. FINAL REAM ID TO ORIGINAL DUB SPEC. INSTALLED REPAIR WASHER PER AARD 51-20-01-1. (M) 2L72 4F RTA1NM 20030819000662003081900066EA 2003 8 19 SWIA200312124 120030616A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 484 LT INTERCOSTAL O/B FLANGE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F4 FRTA21EA E15NE 20030819000872003081900087EA 2003 8 19 SWIA200312175 120030712A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07445SW24 24 7651 FLAP FAIL CAUTION MESSAGE APPEARED 20 MIN AFTER DEPARTURE. REMOVED AND REPLACED LT BPSU. RIGGED LEFT AND RIGHT BPSU IAW MM 27-51-10. FOUND FECU POTENTIOMETER OUTSIDE LIMIT. ADJUSTED FECU POTENTIOMETERS. REMOVED AND REPLACED FLAP CONTROL LEVER PER CRJ MM 27-51-00. OPS CHECK OF FLAP CONTROL LEVER GOOD. FLAP OPS CHECK GOOD. P/N: 7-45500-1 S/N OFF: 0470. 2L72 4F4 FRTA21EA E15NE 20030819000882003081900088NE 2003 8 19 SWIA200312176 320030711A6111RFC11M16A BLADE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07579SW 120347 RT ENGINE NR 3 PROP BLADE HAS APPROX .375 INCH CRACK ON TRAILING EDGE. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED R-3 PROP BLADE IAW MM 61-13-04. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20030819000922003081900092EA 2003 8 19 COMA0360356 120030809A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01487CA 7729 FLIGHT 5480 LT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20030819001022003081900102NM 2003 8 19 C1HA200381025 120030810A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 FLOOR T-ANGLE CORRODED BS 305 RBL 40. 2L73 4F A3WE 20030819001062003081900106NM 2003 8 19 UPS03240922 120030607A5330 SKIN BOEING727 727185C 138406NNM NR 3 RT WINDOW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, CRACKS IN SKIN FROM FASTENER HOLES AROUND NR 3 RT WINDOW CUTOUT FWD OF BS 259.5 AT S10R AREA. FASTENERS REMOVED AND DAMAGED AREA TRIMMED OUT IAW SRM 53-30-3 FIGUR E 29. REPAIR PARTS FABRICATED IAW SRM 53-30-3 FIG 29. REPAIR PARTS PARTIALLY INSTALLED IAW SRM 53-30-3. REMAINING FASTENERS INSTALLED IAW SRM 53-30-03 FIG 29. 2L73 4F A3WE 20030819001082003081900108NM 2003 8 19 UPS03540933 120030701A2910316N310049 LINE BOEING757 75724APF 1384969NM LT ENG HYD SYS FAILED A IPXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01428UP 25459 ON CLIMBOUT FROM CIA LT HYD SYS FAILED. DIVERTED TO CGN. EMERGENCY DECLARED. LANDED W/O INCIDENT. A/C TOWED TO RAMP. REMOVED AND REPLACED TUBE ASSY HYD PRESSURE ON LT ENG STRUT. REMOVED AND REPLACED TUBE ASSY CLAMPS IAW MM 20-10-11-4 & IAW IPC 29-11-61-01. 2L72 4F RTA2NM 20030819001102003081900110WP 2003 8 19 UPS03840916 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, RT WING L/E LOWER RIB IS CRACKED AT XFS 741. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030819001142003081900114NM 2003 8 19 2003UALA00593 120030728A2931 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT ILLUMINATED A UALAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION LDLANDING 1 WP29505UA 24626 LEFT HYDRAULIC SYSTEM PRESSURE AND REVERSER EICAS ILLUMINATED. LEFT HYDRAULIC PRESSURE LINE FROM LEFT ELECTRIC HYDRAULIC PUMP FAILED. REPLACED LINE. 2L72 4F4 FRTA2NM E17NE 20030819001172003081900117NM 2003 8 19 2003UALA00500 120030615A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 AFT CARGO PIT AT BS 1197 BETWEEN RBL 40-45, FRAME T-CAP IS CORRODED UNDER AND AROUND NUT PLATE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW INNER CHORD. 2L72 4F4 FRTA1NM E24NE 20030819001202003081900120NM 2003 8 19 2003UALA00503 120030613A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 TWO SKIN DENTS ON LT SIDE JUST ABOVE E&E COMPARTMENT DOOR. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20030819001402003081900140EU 2003 8 19 03219309 120030807A3350 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27309UE 41022 DURING MAINTENANCE INSPECTION THE FWD EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED THE WIRING IN THE FORWARD EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030819001472003081900147EU 2003 8 19 03222332 120030810A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27332UE 41100 DURING MAINTENANCE INSPECTION THE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030819001492003081900149NM 2003 8 19 2003UALA00506 120030615A278110612229 SWITCH BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CONTACTS INTERMITTENT A UALAO OTHER O OTHER APAPPROACH 1 WP29955UA 26703 AIRCRAFT LANDED UNDER AMBER ALERT DUE TO LEADING EDGE FLAP DISAGREE INDICATION. TROUBLESHOOTING IDENTIFIED A FAILED NR 4 FLAT EXTEND SWITCH. THE SWITCH WAS REPLACED AND THE SYSTEM WAS TESTED TO ENSURE PROPER OPERATION. 2L72 4F4 FRTA16WE E2GL 20030820000892003082000089EU 2003 8 20 03FDEA00867 120030610A3260 RELAY AIRBUS300 A300F4605R 3930327EU NLG FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25651FE 728 AFTER GEAR RETRACTION GOT ECAM WARNING- GEAR FAILED TO RETRACT, GEAR INDICATOR PANEL SHOWED NO LIGHTS. MOMENTS LATER GOT BOTH YAW DAMPERS BOTH PITCH TRIM AND ATS FAILURE. UNABLE TO RESET. RETURNED FOR LANDING. ALSO BOTH FD FAILED. UPDT 10JUN03 15:27 FLL R REMOVED AND REPLACED NLG SHOCK ABS RELAY 94GB DUE TO PROX FAULTING SHOCK ABS NOSE FAIL (SN CODE) & MTP FAULTING NOSE RELAY FAIL. OPS CHECKED NORMAL PER A300 M/M 32-31-7 1-4. FACT 10JUN03 16:27 FLL R PERF AFS LAND TEST TO CHECK YAW DAMP, ATS, PITCH TRIM & F/D'S. OPS CHECKS GOOD PER A-300 TSM 22-00-00. 2L72 4F RTA35EU 20030820001312003082000131NM 2003 8 20 CALA0300431 120030731A5320 MOUNT BOEING737 7373T0 1384582NM LT AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND LT AFT LAV WALL MOUNT CORRODED AT DOOR HINGE MOUNT WALL. THE CORRODED EDGE WAS TRIMMED OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-70-12. 2L72 4F RTA16WE 20030820001912003082000191NM 2003 8 20 730PA0004 120030702A3350 BULB BOEING737 7373L9 1384470NM EMERGENCY LIGHT BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05730PA 27294 EMERGENCY LIGHT INOP LEFT SIDE OF FUSELAGE. REPLACED BULB, OPS CHECKS GOOD. 2L72 4F RTA16WE 20030820001982003082000198NM 2003 8 20 03FDEA00971 120030625A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 BS 740 FLOORBEAM IS CHAFED IN AREAS FROM LBL-45 RBL 45 WL 208. REPAIRED FLOORBEAM IAW EA 7-5310-54878. 2L73 4F RTA3WE 20030821000462003082100046NM 2003 8 21 03FDEA01023 120030627A5754ARC2512503 FITTING DOUG MD11 MD11 3023602NM TE FLAP HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING (FLAP SIDE) - INBOARD T/E FLAP, OUTBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE OUTBOARD SIDE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69357 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030821000762003082100076NM 2003 8 21 03FDEA00862 120030606A5230 ANGLE BOEING727 727200 138407ENM CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25487FE 21490 CORROSION (C53-111-02) ON FWD CARGO DOOR LOWER BEAM ANGLE 27 INCHES AFT OF FWD EDGE 1.5 INCH UP FROM BOTTOM EDGE. REMOVED CORROSION ON FWD CARGO DOOR LOWER BEAM ANGLE AND T-ANGLE AT FWD EDGE AT 27 INCHES. FOUND TO BE OUT OF LIMITS. LOCATED HOLES ON NEW T-ANGLE AND LOWER BEAM AND INSTALLED PART IAW SRM 51-30-2. 2L73 4F RTA3WE 20030821001022003082100102EU 2003 8 21 09FDEA00895 120030616A5420 BRACKET AIRBUS300 A300B4605R 3930308EU NR 2 PYLON BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 NR 2 PYLON PANEL 425 AL TETHER ANCHOR BROKEN. REMOVED AND REPLACED ANCHOR IAW SRM 51-40-21. 2L72 4F RTA35EU 20030821001092003082100109NM 2003 8 21 03FDEA01181 120030731A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 NOSE WHEEL WELL SKIN GOUGED AROUND PANEL OPENING 3124 BS 249 LT. 2L73 4F RTA3WE 20030821001332003082100133EU 2003 8 21 03FDEA00890 120030616A5720 CLIP AIRBUS300 A300B4605R 3930308EU LT WING BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 LEFT WING PANEL 572CB END CLIP IS BROKEN. REMOVED AND REPLACED CLIPS IAW SRM 51-40-21 ON N00596. 2L72 4F RTA35EU 20030821001882003082100188NM 2003 8 21 03FDEA00814 120030525A5753NRC6753504 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - INBOARD TRAILING EDGE FLAP, OUTBOARD AFT FLAP -HINGE FITTING FOUND LT AND RT PIVOT BEARING BORE HOLES WITH CORROSION (FLAP SIDE). REPAIR CARRIED-OUT AS PER CMM 57-52-03 AND FEDEX EA 1-5750-69351 - WINGS - RT INBOARD FLAP OUTBOARD HINGE CORROSION - REPAIR. 2L73 4F RTA22WE 20030821002362003082100236NM 2003 8 21 QXEA200300919 120030720A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- LEFT HAND WING NR 4 FLAP TRACK HAS PITTING CORROSION ON BOTH SIDES OF TRACK. REPAIRED IAW HORIZON AIR EA 2-57-225. 2H72 4T RTA13NM 20030821002372003082100237 2003 8 21 RAAIA00306176 420030629A31607011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU NR 1 FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03551HK7467 41040 5570-STL- DURING TAXI NR 1 SYMBOL GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 SYMBOL GENERATOR. 2L72 4T RTA41NM 20030821002472003082100247WP 2003 8 21 03FDEA01334 120030818A5753 SUPPORT ANGLE DOUG DC10 DC1010 3022110WP T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 LEFT WING I/B FLAP FAIRING PANEL SUPPORT STRUCTURE ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE ON N00420 WO 23696. 2L73 4F A22WE 20030820001702003082000170NM 2003 8 20 UPS03241067 120030714A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C EVIDENCE OF CORROSION AT LAP JOINT BS 820 TO BS 870, S-4R REPAIR CARRIED OUT IAW UPS EO B727-5330-0509. 2L73 4F A3WE 20030820001712003082000171NM 2003 8 20 CALA0300381 120030712A5230 BEAM BOEING737 737524 1384721NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711641 28902 INSPECTION FOUND A 1 INCH CRACK IN C-1 DOOR T-BEAM. A REPAIR WAS INSTALLED IAW SRM 51-70-12. 2L72 4F RTA16WE 20030820001752003082000175 2003 8 20 RAIA00307181 420030701A34207003360948 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AHRS INOPERATIVE A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03556HK133232584 41073 NR 1 AHRS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. 2L72 4T RTA41NM 20030820002192003082000219EU 2003 8 20 ASOA03335 120030724A5260 SKIN AEROSPATR72 ATR72212 8680945EU AIRSTAIR DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE AIRSTAIR DOOR WEB SKIN FORWARD SIDE WAS FOUND TO BE CRACKED AT THE CENTER STEP. MAINTENANCE INSPECTED AND FOUND AIRCRAFT OK FOR FURTHER SERVICE. THE PERMANENT REPAIR WILL BE COMPLIED WITH ON THE NEXT A-CHECK. (M) 2H72 4T RTA53EU 20030820002212003082000221EA 2003 8 20 ASOA03341 120030727A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT INOPERATIVE A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11874AS 7551 DURING TAKEOFF FROM ATL-TRI, THE FLIGHT ATTENDANT NOTICED SMOKE FILLING THE CABIN THROUGH THE VENTS ALONG WITH THE CREW RECEIVING A SMOKE TOILET MESSAGE. THE CREW IMMEDIATELY TURNED OFF BOTH PACKS AND INITIATED THE SMOKE TOILET CHECKLIST AND SMOKE REMOVAL PROCEDURES. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030820002382003082000238EA 2003 8 20 ASOA03318 120030712A5210600319469 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 FLT 4332 - DUIRNG A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS VERY HARD TO OPEN FROM THE OUTSIDE. MAINTENANCE REMOVED AND REPLACED THE PULL-IN MECHANISM ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030821000862003082100086NM 2003 8 21 03FDEA00792 120030427A5753ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RIGHT WING FOUND OUTBOARD FLAP, INBOARD HINGE WING SIDE WITH ACTUATOR HOLE LOCATION INBOARD MOST WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69242 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT & RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030821001302003082100130EU 2003 8 21 03FDEA00892 120030616A5320A9249635720000 BRACKET AIRBUS300 A300B4605R 3930308EU CARGO BAY BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 FWD CARGO ANT CABLE ATTACH BRACKET IS BROKEN AT FR 22 LBL 24 STR 45L. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21 401. 2L72 4F RTA35EU 20030821002582003082100258WP 2003 8 21 GTIA030583 120030701A5321 ANGLE DOUG DC9 DC982 3022082WP FLOORBOARD BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND RIGHT COCKPIT FLOORBOARD ATTACHED SYNTHETIC ANGLE BROKEN, HEAVY FOOD/DIRTY DEPOSITS. REMOVED SYNETHETIC ANGLE. FORMED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2L72 4F A6WE 20030821002602003082100260WP 2003 8 21 GTIA030589 120030701A5321 ANGLE DOUG DC9 DC982 3022082WP FLOORBOARD CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND COCKPIT FLOORBOARD FS 120-160 LEFT ATTACHED SYN ANGLE CRACKED, CORRODED AND DIRTY. REMOVED CRACKED ANGLE. FORMED NEW ANGLE. FABRICATED NEW FLOORBOARD. INSTALLED NEW ANGLE. (M) 2L72 4F A6WE 20030821002722003082100272WP 2003 8 21 GTIA030590 120030702A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN FS 1338 FLOORBEAM UPPER SIDE CORRODED/BARE METAL LBL 57-RBL 57. CUT APPROX 2 INCHES BY 1 INCH SECTION OUT OF TOP FLANGE. FABRICATED REPAIR ANGLE-FILLER. INSTALLED REPAIR ANGLE AND FILLERS. (M) 2L72 4F A6WE 20030821002742003082100274NM 2003 8 21 USAASB03122 120030726A324139353 VALVE BOEING737 737301 1384611NM ANTI-SKID SYS FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19558AU 23512 PIT - FLT 1723 - AFTER TAKEOFF FROM PIT, UPON GEAR RETRACTION, THE ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. SINCE THE AIRCRAFT WOULD BE OVERWEIGHT FOR LANDING IN PVD, AND DUE TO SHORT RUNWAYS, DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD ANTI-SKID VALVE. LEAK CHECK GOOD. PERFORMED ANTI-SKID ADJUSTMENT TEST PER MM 32-42-00. CHECKS GOOD. (M) 2L72 4F RTA16WE 20030821002802003082100280NM 2003 8 21 USAABB03127 120030730A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 CLT - THE FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 WAS ILLUMINATED AT ALL TIMES. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030821002822003082100282NM 2003 8 21 USAABB03121 120030725A2421727792K IDG BOEING757 7572B7 1384964NM LT ENGINE MALFUNCTIONED A USAAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19624AU 27245 CLT - FLT 615 - ON CLIMB-OUT FROM CLT, AT ABOUT 9,000 FEET, THE CREW RECEIVED AN EICAS MESSAGE THAT THE LEFT ENGINE GENERATOR DROPPED OFF LINE. THE LEFT GENERATOR OFF LIGHT WAS ALSO ILLUMINATED. THE APU WAS ALREADY ON MEL SO THE FLIGHT RETURNED TO THE FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. CREW REPORTED THAT THE LEFT GENERATOR CONDITION RETURNED TO NORMAL AFTER GENERATOR SWITCH RESET. MAINTENANCE REMOVED AND REPLACED THE LEFT IDG. LEAK CHECK AND OPERATIONAL CHECK GOOD PER MM 24-11-00. CLEARED THE MEL ON THE APU BY REPLACING THE APU BATTERY, P/N 18550. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20030822000132003082200013WP 2003 8 22 03FDEA01348 120030820A3222 STRUT DOUG DC10 DC1010 3022110WP NLG DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2568057 48264 AFTER T/O LAX, RAISED GEAR & GOT NOSE GEAR UNSAFE UP BOTH POSITIONS. PER RED TABS LOWERED GEAR HANDLE & GOT 3 GREEN. ATTEMPTED TO RAISE GEAR HANDLE & WERE UNABLE. RAN RED TABS FOR GEAR HANDLE, WOULD NOT RAISE. RETURNED TO KLAX. JACKED AIRCRAFT REF DC-10-10 AMM 07-11-00-2. PERFORMED EXTENSION RETRACTION TEST IAW DC-10-10 AMM 32-30-00-5. OBSERVED NLG STRUT EXTENDING SLOW. STRUT NEEDS SERVICE. OBSERVED BLACK FLUID WHILE DRAINING STRUT. SUGGEST STRUT SEAL INSPECTION/CHANGE. C/W DC10 W/C 32T2401 NOSE GEAR STRUT REPACK. OP'D CK NOSE RETRACTION & EXTENSION PER MM 32-30-00-5. 2L73 4F A22WE 20030822000162003082200016NM 2003 8 22 03FDEA01344 120030802A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 FUSELAGE SKIN DENT (2 PLACES) RIGHT SIDE BETWEEN STA Y 475.0 TO 495.0 LONGERONS 45R TO 46R (A = APPROX 1.5 INCH D; B = APPROX 0.50 INCH D). FUSELAGE SKIN DENT ( 2 PLACES ) RT SIDE BETWEEN STA Y = 475.0 TO 495.0 LONGERONS 45 RT TO 46 RT ( A = APPROX. 1.5 INCH D; B = APPROX. 0.50 INCH D ) REPAIRED CARRID OUT AS PER SRM 53-20-00 VOL.1. 2L73 4F RTA22WE 20030822000502003082200050NM 2003 8 22 2003UALA00563 120030716A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 CABIN AT BS 852, RBL 56, TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE, ANGLE AND FILLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20030822001092003082200109EU 2003 8 22 RAIA00307188 120030708A28209409019 FLOW VALVE JETAIRJETSTMJETSTM4101 1500501EU FUEL SYSTEM MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03555HK16595 41072 5452-STL- RT FUEL PRESSURE FELL TO ZERO. MAINTENANCE REMOVED AND REPLACED MOTIVE FLOW VALVE ACTUATOR. 2L72 4T RTA41NM 20030328000452003032800045SO 2003 3 28 C2XA03TY031 120030226A5530145207350003 HOUSING EMB 145 EMB145LR 3260212SO VERTCAL STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716981 145208 DURING A SCHEDULED 2C INSPECTION THE LT AND RT VERT STAB SPHERICAL BEARING HOUSING HAD LITE CORROSION. MAINTENANCE REWORKED BOTH VERTICAL BEARING HOUSINGS IAW EC 5510-01052 AND EMB 145 AMM 51-50-01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328001012003032800101EU 2003 3 28 CX7A194J33 120030302A61208210172 GOVERNOR SAAB SF340 340B 7860101EU HAMSTD14RF 14RF19 NE OVERSPEED DEFECTIVE A CX7ACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL03301CE 340B191 IMMEDIATELY AFTER T/O NOTICED AN UNUSUAL YAW, NOTED LEFT PROP RPM WAS ERRATIC. IT WOULD NOT EXCEED 1340 RPM. T/M LOCKOUT HAD NO AFFECT PER CHECKLIST. ALL OTHER ENGINE INDICATIONS NORMAL. 2L72 4T RTA52EU 6 CP11NE 20030331000192003033100019EA 2003 3 31 A6WA200340025 120030106A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 FS FRAME 718 IS CRACKED .25 INCHES AT TOP RIVET HOLE AT STRINGER 11 LT SIDE, INCORPORATED MFG REO 601R-53-61-193 REV A. 2L72 4F RTA21EA 20030331000202003033100020EA 2003 3 31 A6WA200340026 120030105A5320 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 RT BOOST PUMP ACCESS HOLE HAS FAILED FASTENER HOLE AT 1:00 O`CLOCK POSITION PERFORMED REPAIRS NR 1 AND NR 2 OF REO 601R-57-21-169 BY OPENING UP HOLE. FABRICATING BUSHING AND INSTALLING BUSHING. 2L72 4F RTA21EA 20030331000712003033100071EU 2003 3 31 ASOA03095 120030216A5320S5367800821600 ANGLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, THE RIGHT Z-ANGLE BETWEEN FRAMES 39R TO 41R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT Z-ANGLE BETWEEN FRAMES 39R TO 41R IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030331000722003033100072EU 2003 3 31 ASOA03096 120030216A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, THE SEAT TRACK BETWEEN FRAMES 31R TO 36R, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAMES 31R TO 36R, IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030331000732003033100073EU 2003 3 31 ASOA03097 120030216A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, THE SEAT TRACKS BETWEEN FRAMES 36R TO 39R AND 39L TO 41L WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FRAMES 36R TO 39R AND 39L TO 41L IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030331000932003033100093SO 2003 3 31 C2XA03SH078 120030330A532014524199401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE LT OUTBOARD FLOOR SUPPORT AT FRAME 18 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331001032003033100103EA 2003 3 31 COMA0360165 120030326A5610NP1393221 WINDOW CNDAIRCL600 CL6002B19 1900309EA LEFT FAILED A COMAO OTHER O OTHER CRCRUISE 1 SO01971CA15030 7145 FLT 5016 PILOTS SIDE WINDOW SHATTERED. REPLACED WINDOW. 2L72 4F RTA21EA 20030331001152003033100115EU 2003 3 31 DHL2003368001 120030114A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU LAVATORY MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01506TA 207 LAV SMOKE DETECTOR SOUNDED HAD TO BE DISCONNECTED. OPS CHECKED SMOKE DETECTOR IAW M/M 26-17-00. OPS CHECKED GOOD. 2L72 4F RTA35EU 20030401000342003040100034EA 2003 4 1 ASOA03054 120030210A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11846AS 7328 DURING A GROUND INSPECTION IN DFW, THE RIGHT SIDE AFT EMERGENCY LIGHT OVERWING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE AFT EMERGENCY LIGHT LAMP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000362003040100036NM 2003 4 1 AWXA200300323 120030328A3397BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 2 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030401000412003040100041GL 2003 4 1 C2XA03CL079 220030325A724023074735 COMBUSTION LINER EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 ENGINE WRONG PART A C2XAK NONE O OTHER ININSP/MAINT 1 SW27111091066 145657 CAE312285 3/25/03 EXPRESS JET AIRLINES WAS NOTIFIED BY ROLLS ROYCE THAT AIRCRAFT 11109, NR 2 ENGINE HAD THE WRONG P/N COMBUSTION LINER INSTALLED AT THE FACTORY. THE AIRCRAFT WAS FERRIED TO CLEVELAND FOR A ENGINE CHANGE. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030401001182003040100118WP 2003 4 1 DHL2003804510 120030117A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER LOWER PART CRACKED AT 1/2 IN STA XFS 460.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001522003040100152WP 2003 4 1 DHL2003804662 120030210A57305769933183 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING OUTBOARD FLAP VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO67.000. PERFORMED MAJOR REPAIR IAW EO DHL 030109 , ED-3222 REMOVED FASTNERS IAW SRM 51-1-21 PG. 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075T6AL .071) A FILLER ( 7075T6AL .063) AND INTERNAL DOUBLER (075T6AL .050) IAW EO DHL030109 , ED-3222. CLEANED TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B , APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1 . INSTALLED FILLERS & DOUBLERS AT LT WING OUTBD VANE SLOT UPPER SKIN WITH NEW FASTNERS IAW EO DHL 030109, ED-3222 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030401001812003040100181WP 2003 4 1 DHL2003873003 120030227A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT STUCK A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01873SJ 46091 F/O'S SLIDING WINDOW WILL NOT OPEN. FOUND WINDOW JAMMED. UNSTUCK WINDOW. OPS CHECKED GOOD PER M/M 56-10-3. 2L74 4F RT4A25 20030402000322003040200032NM 2003 4 2 2003UALA00290 120030317A335058781 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN CONTAMINATED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29350UA 24301 EMERGENCY ELECTRICAL LIGHTING FIXTURE INOPERATIVE FROM ROW 15 TO THE BACK OF AIRCRAFT. FOUND RIBBON CABLE FOR THE EEL LIGHTS SOAKED WITH WATER. REMOVED CABLE AND CHECKED INDIVIDUAL LIGHTS. REPLACED POWER STRIP CABLE, OPS NORMAL. 2L72 4F4 FRTA16WE E2GL 20030402000362003040200036NM 2003 4 2 2003UALA00311 120030322A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 CABIN LT SIDE STA 616 FRAME CRACKED BELOW CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND FILLER. 2L72 4F4 FRTA16WE E2GL 20030402000372003040200037NM 2003 4 2 2003UALA00312 120030323A5313 STRINGER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29954UA 26739 FUSELAGE STR S21-R DAMAGED BETWEEN BS 887 AND BS 907. MAJOR REPAIR ACCOMPLISHED. PERFORMED ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030402000402003040200040NM 2003 4 2 2003UALA00317 120030324A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 827, STR 9R FRAME WEB IS CRACKED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER WAS INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030403000722003040300072SO 2003 4 3 C2XA03CL081 120030331A2730 CONTROL CABLE EMB 135 EMB135ER 3260203SO ELEVATOR LOOSE A C2XAO OTHER O OTHER APAPPROACH 1 SW2725504 145186 CLE FLT 2828 THE CREW REPORTED ELEVATOR LOST EFFECTIVENESS ON FINAL AT 130-125 KIAS. ELEVATOR FEELS SLOPPY ON GROUND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX ADJUSTED CABLE TENSIONS AND REMOVED AND REPLACED CAPTAINS ELEVATOR CABLE TENSIONER/REGULATOR OPERATIONAL CHECKS AND TEST FLIGHT WAS GOOD. 2L72 4F RTT00011AT 20030403000782003040300078NM 2003 4 3 CALA0300151 120030328A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND STRINGER 25R CORRODED AT BS 364 AND S24R WAS CORRODED AT BS 360. REPAIRED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20030403000942003040300094EA 2003 4 3 COMA0360175 120030330A2750860D10018ABCD COMPUTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01868CA3118 7427 FLIGHT 5928 FLAPS FAIL CAUTION DURING LANDING. REPLACED THE FECU. 2L72 4F RTA21EA 20030403001242003040300124NM 2003 4 3 DL733030151 120030213A2612 FIRE LOOP BOEING737 737347 1384647NM APU UNSERVICEABLE A DALAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO27304WA37986 23345 35523C DURING PUSHBACK APU FIRE WARNING CAME ON APU SHUTDOWN AND INDICATION EXTINGUISHED APPROXIMATELY 2 MINUTES LATER. FIRE INDICATION RETURNED AND REMAINED ON. CREW FIRED APU EXTINGUISHER BOTTLE AND FIRE LIGHT DID NOT GO OUT. INSPECTED APU AND COMPARTMENT AREA NO EVIDENCE OF FIRE NO EVIDENCE OF FIRE DETECTED BY GROUND OR FIRE RESPONSE PERSONNEL. DEFERRED APU FIRE DETECTION AND EXTINGUISHING SYSTEM TO MEL, APU INOPERATIVE. TESTED FIRE LOOP SYSTEM, UNABLE TO DUPLICATE PROBLEM. 2L72 4F RTA16WE 20030403001262003040300126NM 2003 4 3 DL733030266 120030322A7830 PROXIMITY SENSOR BOEING737 7373B7 1384580NM NR 2 ENGINE T/R MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27951WP 22951 NR 2 T/R LIGHT ILLUMINATED CLIMBING THROUGH 12,000 FT. RETURN TO SLC QRH PROCEDURES COMPLIED WITH. REVERSER LIGHT ON OVERHEAD PANEL. ATB. CLEANED SIX PROXIMITY SENSORS FOR THE LEFT AND RIGHT T/R HALVES. CLEANED CANNON PLUGS FOR RIGHT AND LEFT SYNC LOCKS. REPLACE ENG ASSESSORY UNIT PER MM 78-34-06-4. NR 2 T/R SYSTEM CHECKS GOOD. NO REVERSER FAULT LIGHT NOTED. 2L72 4F RTA16WE 20030404000032003040400003NM 2003 4 4 373PA0008 120030402A335086210066 BATTERY PACK BOEING737 7373Y0 1384671NM EMERGNENCY LIGHTDISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 EMERGENCY EXIT FLOOR PATH LIGHT SEAT 6 AND SEAT 11 DIM. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-51. 2L72 4F RTA16WE 20030404000082003040400008WP 2003 4 4 ABXA030125 120030317A5320991555047 INTERCOSTAL DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 CORROSION AROUND INTERCOSTAL NUTPLATES UPPER AND LOWER SURFACE, BETWEEN LONGERON 28 LEFT AND LONGERON 27 LEFT, F.S. 979 - 996. REPLACED INTERCOSTAL IAW DOUGLAS DRAWING 9915550 AND DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20030404000092003040400009WP 2003 4 4 ABXA030126 120030324A53103924028501N FITTING DOUG DC9 DC932F 3022067WP KEEL AREA CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 LONGERON END CRACKED, LEFT CANTED KEEL AREA, JUST AFT OF FORWARD "P" DOME, LONGERON 29 LEFT. REPLACED LONGERON 29 LEFT END CAP IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030404000112003040400011NM 2003 4 4 AWXA200300333 120030402A2560P4010021 BATTERY BOEING737 737277 1384570NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28179AW 22646 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE FORWARD LT EMERGENCY FLASHLIGHT HAD NO BLINKING LIGHT. MAINTENANCE REMOVED AND REPLACED THE FORWARD LT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030404000162003040400016NM 2003 4 4 CALA0300163 120030401A5241 SKIN BOEING737 7373T0 1384582NM GALLEY DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND R-2 DOOR EXTERNAL SKIN DENTED AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030404000172003040400017NM 2003 4 4 CALA0300164 120030401A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND TOP SURFACE OF TOP CAP OF LATERAL FLOORBEAM AT STA 1016 CORRODED AT LT SIDE AREA UNDER LAV TANK. REPAIRED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030404000262003040400026WP 2003 4 4 DHL2003873007 120030401A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT LACK OF LUBE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ 46091 F/O'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED F/O'S SLIDING WINDOW AND LUBRICATED ACTUATING ASSEMBLY AS REQUIRED. OPS CHECKED GOOD IAW M/M 56-10-3. 2L74 4F RT4A25 20030404000342003040400034EU 2003 4 4 03FDEA00379 120030403A7830 FILLET AIRBUS310 A310 EU NR 2 ENG T/R TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 2 ENG I/B THRUST REVERSER CORE UPPER AFT FILLET PANEL TORN. R/R FILLET PANEL PER IAW SRM 51-40- 2. 2L72 4F RTA35EU 20030404000452003040400045NM 2003 4 4 DL757030094 120030124A5310143N85121 DOOR FRAME BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 THE OUTBOARD STRUCTURE OF THE LOWER SILL BEAM OF THE C1 DOOR OPENING WAS FOUND CORRODED. TO REMOVE THE CORROSION, THE OUTER STRUCTURE AND WEB OF THE FS 620 FRAME WERE CUT BETWEEN STRINGERS 25R & 26R AND THE LOWER SECTIONS REMOVED. THE SILL STRUCTURE WAS REPLACED AND THE FRAME AND WEB SECTIONS SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 384357-14, REV A. 2L72 4F RTA2NM 20030404000462003040400046NE 2003 4 4 DL757030100 220030128A7261PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 MALFUNCTIONED A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO27698DL44277 29911 716511 RT ENGINE FAILURE ON CLIMBOUT, APPROX 18,000FT. EICAS STATUS PAGE RT ENGINE SEC SEL-RT ENGINE LOW N1-RT ENGINE OIL PRESS-RT ENGINE FUEL ON SOL. EPCS PAGE OIL PRESS RED NO OTHER FAULTS RECORDED. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20030404000512003040400051NM 2003 4 4 DL757030184 120030223A3350 BATTERY BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27608DA 22815 EMERGENCY LIGHTS AFT OF SEAT 38 INOP. REMOVED AND REPLACED LIGHT PACK AND BATTERY ASSEMBLY. 2L72 4F RTA2NM 20030404000522003040400052NM 2003 4 4 DL757030188 120030221A5315146N51116 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27652DL 24392 THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH MULTIPLE AREAS OF CORROSION. THE UPPER CAP FLANGE WAS TRIMMED OFF FROM END TO END (LBL 61 - RBL 61). A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED ON THE FLOORBEAM. THE REPAIR WAS ACCOMPLISHED PER ER/A 384525-14, REV A. 2L72 4F RTA2NM 20030404000702003040400070NM 2003 4 4 DL757030289 120030324A5511185N700178 STRUCTURE BOEING757 757232 1384965NM HORIZONTAL STAB DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27612DL 22819 THE LOWER STRUCTURE OF THE RT HORIZONTAL STABILIZER AUXILIARY SPAR WAS FOUND DENTED AT SPAR STA 330. THE STRUCTURE WAS CUT AND THE DAMAGED SECTION REMOVED. A NEW SECTION OF STRUCTURE WAS INSTALLED WITH 2 STEEL REPAIR ANGLES AND A STRAP PER ER/A 384563-14, REV A. 2L72 4F RTA2NM 20030404000762003040400076NM 2003 4 4 DL764030158 120030214A2780 BOLT BOEING767 767432ER 1385134NM NR 9 SLAT BROKEN A DALAO OTHER D INFLIGHT SEPARATION LDLANDING 1 SO27828MH 29699 L/E SLAT ASYMMETRY ILLUMINATED ON FINAL. FOUND NR 9 SLAT OUTBOARD TARGET AND ROLLER MISSING. REPLACED SAME. SLAT BOLT BROKE. 2L72 4F RTA1NM 20030404000812003040400081NM 2003 4 4 DL767030165 120030219A3350 LIGHT BOEING767 767232 1385132NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27108DL 22220 EXTERIOR EMERGENCY LIGHT LT SIDE STA 1240 INOPERATIVE. RELAMPED,NO HELP. SUSPECT POWER SUPPLY. REPLACED FUSES IN POWER SUPPLY, LIGHT CHECK GOOD. 2L72 4F RTA1NM 20030404001172003040400117NM 2003 4 4 ASAA0340004 120030109A3397 WIRE BOEING737 7374Q8 138447QNM ROW 19 BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01782AS 25113 SEA - DURING LINE CHECK, FOUND THE EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 19. REPAIRED BROKEN WIRE. TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA16WE 20030404001242003040400124NM 2003 4 4 DL767030249 120030317A2150 A/C PACK BOEING767 767232 1385132NM A/C BAY MALFUNCTIONED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27108DL 22220 AFTER TAKEOFF, STRONG ELECTRICAL SMELL IN COCKPIT AND FLT ATT REPORTED ELECTRICAL SMELL AND SMOKE IN CABIN. INSPECTED RT PACK BAY, NORMAL RAN PACK USING APU AIR, TURBINE INLET TEMP ROSE HIGH. NO OVENS IN USE DURING TAKEOFF. RAN GASPER AND RECIRC FANS, OPS NORMAL. FWD RT PACK TO MCO AND PLAC PER MEL 21-51-01A. 2L72 4F RTA1NM 20030404001252003040400125NM 2003 4 4 GAIA03010OP 120030220A33501000677 LIGHT BOEING727 727223 1384074NM COCKPIT INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW076831 20184 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030404001302003040400130NM 2003 4 4 DL767030283 120030327A5754114T411221 WEDGE BOEING767 767232 1385132NM L/E SLAT DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27103DA 22215 RIGHT WING SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14. 2L72 4F RTA1NM 20030404001412003040400141 2003 4 4 SWAA030461 420030302A2565D31354 SLIDE BOEING737 7375H4 138449DNM AFT ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING WALK AROUND INSP, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030404001552003040400155 2003 4 4 SWAA030537 420030309A25656574550 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM. 2L72 4F A16WE 20030404001612003040400161 2003 4 4 SWAA030551 420030311A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030404001652003040400165NM 2003 4 4 SWAA030555 120030310A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 663, STR'S 10R & 10L, BS 560, STR 7R & BS 706, STR 11R. REMOVED AND REPLACED STR CLIPS PER SRM. 2L72 4F RTA16WE 20030404001812003040400181NM 2003 4 4 SWAA030587 120030314A3350BR2013 CONNECTOR BOEING737 7377H4 1384404NM CABIN NOT SEATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29712SW 27846 EEPLS LIGHTS AT TWO SECTIONS ILLUMINATED WHEN SWITCH IN AUTO POSITION. RESEATED CONNECTORS AT FWD BATTERY PACKS PER MM. 2L72 4F RTA16WE 20030404001822003040400182NM 2003 4 4 SWAA030589 120030315A57536571909117 CARRIAGE BOEING737 7372H4 138448CNM T/E FLAP FRACTURED A SWAAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 SW29096SW 23055 WHEN ANY FLAP POSITION IS SELECTED, T/O OR LANDING, AIRCRAFT ROLLS SIGNIFICANTLY TO LEFT. FOUND NR 2 FLAP SPINDLE FRACTURED. REMOVED AND REPLACED NR 2 FLAP CARRIAGE PER MM. 2L72 4F A16WE 20030407000242003040700024WP 2003 4 7 ASAA0380091 120030117A53473957317501 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY TIEDOWN BRACKET IS CORRODED. REPLACED BRACKET PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20030407000502003040700050NM 2003 4 7 KPVA20034 120030127A33506104789 BATTERY PACK DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13805WP 353 RIGHT FORWARD EMERGENCY EGRESS LIGHT, RIGHT FORWARD EMERGENCY DOOR EXIT LIGHT AND FORWARD 2ND CEILING EMERGENCY LIGHT INOPERATIVE DURING OP CHECK OF EMERGENCY LIGHT CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK 3351PS2 IAW DHC-8 MM CHAPTER 33-51-00 PAGE 201. OPS CHECK GOOD. (M) 2H72 4T RTA13NM 20030407000722003040700072SO 2003 4 7 SIMA200301501 120030113A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO GALLEY CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21636AE 145160 ABI - DURING A IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT A 16.5 BY 21 SECTION OF THE DIGITAL. FABRICATED A REPLACEMENT STRAP. FABRICATED TWO REPAIR DOUBLERS, AND SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) CHAPTER 53-21-10. (M) 2L72 4T RTT00011AT 20030407000752003040700075EU 2003 4 7 SIMA200305016 120030219A7712C821453 TAB SAAB SF340 340B 7860101EU LT ENG PCU BROKEN A SIMAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21902AE 340B269 DFW - FLT 3635 - DURING CLIMB-OUT OF DFW, AFTER GEAR WAS SELECTED UP LEFT ENGINE TORQUE INDICATION WENT TO ZERO. ENGINE SHUTDOWN AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LOCKING TAB ON THE LEFT ENGINE PCU CABLE WAS BROKEN. THE CABLE WAS REMOVED AND REPLACED IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030328000342003032800034SO 2003 3 28 C2XA03CL077 120030326A2530500064001 COFFEEMAKER EMB 135 EMB135ER 3260203SO GALLEY SHORTED A C2XAO OTHER O OTHER CRCRUISE 1 SW2714505 145192 CLE FLIGHT 2022 THE CREW REPORTED A INTERMITTENT SMELL OF ELECTRICAL SMOKE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEEMAKER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030331000942003033100094SO 2003 3 31 C2XA03TY043 120030328A3260852701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO MLG OUT OF ADJUST A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2713968 145138 DURING CLIMB RECEIVED A ICAS MESSAGE OF LDG AIR/GND FAIL AT ROTATION. LANDING GEAR WOULDN'T RETRACT. AIR RETURN AND MAINT FOUND PROX SWITCHES OUT OF ADJUSTMENT. DID A RE-ADJUSTMENT OF THE SWITCHES AND DID THE GEAR SWINGS AS REQUIRED. A/C WAS PUT BACK INTO SERVICE. ALL WORK WAS IAW EMB 135/145 AMM32-34-00 GEAR SWINGS AND 32-62-00 ADJUSTMENT OF SWITCHES. 2L72 4F RTT00011AT 20030331001262003033100126NM 2003 3 31 DHL2003740506 120030203A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT AFT PIT FLOORBEAM AT RBL 15 IS CRACKED AT NUT PLATE STA 950E. REMOVED FASTENERS PER SRM 57-30-2. CUT OUT DAMAGED AREA 2 PLACES PER SRM 51-40-3 FIG 3. FABRICATED DOUBLER ANGLES (2024 T3) .050 PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-30-2. INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2. 2L73 4F RTA3WE 20030331001282003033100128NM 2003 3 31 DHL2003740509 120030201A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 SMALL SKIN CREASE LT SIDE OF FUSLAGE BS 620 STR 25L. MADE CUT OUT IN DAMAGED SKIN PER SRM 53-30-3 FIG 2. FABRICATED REPAIR DOUBLER 2024-T3 .063. FABRICATED FILLER 2024-T3 .050 PER SRM 53-30-3 FIG 2. TREATED AND PRIMED REPAIR PARTS PER SRM 51-10-2. INSTALLED REPAIR PER SRM 51-30-2. 2L73 4F RTA3WE 20030331001332003033100133NM 2003 3 31 DHL2003740514 120030202A5340 CHANNEL BOEING727 7272Q9 138448MNM FUSELAGE CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH CABIN BS 1166 STR 10.3 LT ATTACHING GILLINER SUPPORT SHOWS CHAFE MARK. CUT OUT DAMAGED AREA (2.5 X 1 INCH) AND FABRICATED DOUBLER (7075-T6 .090) PER SRM 53-10-2 AND 51-40-3. TREATED AND PRIMED PARTS PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51-30-2. 2L73 4F RTA3WE 20030331001492003033100149NM 2003 3 31 DHL2003742003 120030118A2612 FIRE LOOP BOEING727 727225 1384077NM NR 3 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01742DH 21290 ENGINE NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED TO DMI LOG PER DHL MEL 26-9 CAT-C DDD 01-28-2003 DMI 11670. PLACARD INSTALLED. RE; DMI 11670 - NR 3 ENGINE FIRE GROUND FAULT LIGHT ILLUMINATES INTERMITTENTLY. FOUND 3 FIRE LOOP TOUCHING COWLING. REPOSITIONED PER 26-11-01. CHECKED GOOD. CLEARS DMI NR 11670. PLACARD REMOVED. 2L73 4F A3WE 20030401000622003040100062NM 2003 4 1 CA030225003 120030223A3520 OXYGEN MASK BOEING737 7372T5 1384474NM PWA JT8 JT8D17 52049NE CABIN MISINSTALLED W B EMER. DESCENT W INADEQUATE Q C CRCRUISE 1 CA (CAN) A/C EXPERIENCED RAPID DEPRESSURIZATION. CLIMBED TO 15,000 FT IN APPROX 5-10 SECONDS. O2 SYS DEPLOYED AUTOMATIC. STANDBY MODE DID NOT OPERATE NORMALLY BUT CABIN PRESSURE WAS RECAPTURED. DURING EMER DESCENT WITH MANUAL MODE MAINT REPLACED CABIN PRESSURE CONTROLLER AND VERIFIED A/C INTEGRITY AND PRESS SYS FUNCTION DURING A GROUND RUN. PSG INDICATED EXPERIENCED NO OR LOW FLOW FROM O2 SYSTEM DURING DESCENT. MAINT FOUND SEVERAL O2 MASK HOSES IMPROPERLY ROUTED AND KINKED. MASKS AND HOSES REPLACED AS REQUIRED, O2 BOTTLE REPLACED AND A/C RELEASED FOR SERVICE. A/C OPERATED NORMALLY FOR SEVERAL FLIGHTS. RESTRICTED A/C TO 25,000 FEET BY APPLICATION OF O2 SYSTEM INOP MEL. 2L72 4F4 FRTA16WE E2EA 20030401000682003040100068NE 2003 4 1 CA030228006 220030226A7297 WIRE AIRBUS330 A330243 3930330EU RROYCERB211 RB211TRENT77 NE ENGINE DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION OF ENGINE IT WAS NOTICED THAT THE FOLLOWING WIRES WERE DAMAGED. DAMAGE WIRES WAS CAUSED BY CHAFING. 1 WIRE BETWEEN CONNECTOR 3009VC2A AND 3012VC2A2-WIRE BETWEEN CONNECTOR 3009VC2A AND 3012VC2A. WIRES WERE REPLACED IAW MAINTENANCE MANUAL AND RE-CLAMPED. 2L72 4F4 FRTA46NM E39NE 20030401000842003040100084NE 2003 4 1 2003F00168 220030401A72300319257000 DIFFUSER UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE ENGINE CRACKED A O OTHER O OTHER NRNOT REPORTED 1 SW09120TL1709 1141 34152 COMPRESSOR STALLS DEVELOP AS DIFFUSER VANES DETERIORATE. BORESCOPE INSPECTION REVEALS 7 OUT OF 10 ENGINES IN FLEET HAVE 1 OR MORE DIFFUSER VANES CRACKED OR PARTIALLY MISSING. THIS ENGINE REMOVED DUE TO COMPRESSOR SURGE/ STALL EVENTS AND DIFFUSER VANE CRACKS BEYOND MANUFACTURER'S SERVICEABILITY CRITERIA. 1G72 3U3 UNCR0001RD E34NE 20030401001042003040100104NM 2003 4 1 DHL2003782002 120030320A2612 FIRE DETECTOR BOEING727 727227 1384078NM ENGINE WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01769AT 21998 ENGINE FIRE TEST IN ENGINE AND WHEEL WELL POSITION DOSE NOT ILLUMINATE NR 1 FIRE HANDLE NOR SOUND BELL. TEST SWITCH HELD FOR 60 SECONDS. DEFERRED PER DHL MEL REF 26-5 CONTROL 12325 CAT-C EXPIRES 3-30-03. PLACARD INSTALLED. 2L73 4F A3WE 20030403000692003040300069EU 2003 4 3 AWXA200300331 120030331A3243 BRAKE AIRBUS320 A320231 3930325EU MLG MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28627AW 66 ON TAKEOFF ROLL AT PHX EN ROUTE FOR ONT FLIGHT CREW THOUGHT THEY MAY HAVE EXPERIENCED A POSSIBLE BRAKE LOCKUP. AS A PRECAUTION, DECLARED AN EMERGENCY AT ONT. 2L72 4F RTA28NM 20030403000742003040300074SO 2003 4 3 C2XA03CL083 120030402A326023092900401 UPLOCK EMB 145 EMB145ER 3260211SO RIGHT MLG STICKING A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW2714938 145029 CLE FLIGHT# 2225 THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE WITH A RED RIGHT MAIN INDICATION ON GEAR RETRACTION.THE GEAR WAS RECYCLED AND EXTENDED PROPERLY THEN RETRACTED WITH A DISAGREE MESSAGE AGAIN.THE CREW REPORTED BOTH MAIN GEAR WERE FELT TO BUMP UP AND LOCK.THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN GEAR UP LOCK BOX ASSEMBLY.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030403000752003040300075SO 2003 4 3 C2XA03TY044 120030402A532014522459003 ANGLE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717524 145399 DURING A SCHEDULED 1-C INSPECTION THE RAMP ANGLE IN THE CENTER GALLEY AREA WAS FOUND CORRODED. MAINT. R & R THE RAMP ANGLE IAW 51-40-02.ALL WAS C/W AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030404000102003040400010NE 2003 4 4 ARWA20030401 220030403A7261 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 2 LACK OF LUBE A ARWAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO198969U 46070 671379 AFTER T/O FROM UTP, DURING CLIMB, FE OBSERVER NR 2 OIL QUANITY INDICATOR READING 2 GALLONS & DECREASING. SWAPPED INDICATORS, NO CHANGE. FOLLOWED ABNORMAL PROCEDURES FOR FUEL DUMPING, LANDED (UTP) LESS THAN MLWG. SERVICED NR 2 ENGINE OIL WITH 9 QTS. OF OIL. INSPECTED ENGINE FOR EVIDENCE OF OIL LEAK, NONE NOTED. PERFORMED ENGINE RUN UP IAW MM 71-00, LEAK CK ENGINE, SHUT-DOWN, INSPECTED WITH NO DEFICIENCIES NOTES AND NO ADDITIONAL OIL SERVICED. AIRCRAFT RETURNED TO SERVICE & PLACED ON OIL WATCH. 2L74 4F4 F 4A25 1E8 20030404000252003040400025NM 2003 4 4 DHL2003782004 120030402A2611 SMOKE DETECTOR BOEING727 727227 1384078NM CARGO BAY INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01769AT 21998 NR 1 SMOKE DETECTOR FOR MAIN CARGO DECK IS INOPERATIVE. PERFORMED OPS CHECK OF CARGO SMOKE DETECTION SYSTEM IAW 26-16-01. OPS CHECKED NORMAL. 2L73 4F A3WE 20030408000742003040800074EU 2003 4 8 03FDEA00381 120030403A2710A5724266100100 BRUSH HOLDER AIRBUS310 A310 EU RT WING AILERON DETACHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 N 517 RT WING ALL SPEED AILERON LWR BRUSH ASSY HAS BECOME DETACHED FROM STRUCTURE. REMOVED AND REPLACED BRUSH ASSY. IAW/SRM 51-40-21 PG.7 UNDER W/O NO. 13350 FEDEX 04/04/2003. 2L72 4F RTA35EU 20030407000782003040700078EU 2003 4 7 SIMA200306201 120030224A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHTSINOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21903AE 340B282 TYR - FLT 3670 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 6, 7 AND 8 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT 22LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030407000812003040700081SO 2003 4 7 SIMA200306401 120030204A532014522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION. PASSENGER DOOR ENTRY FLOOR SUPPORTS HAVE CORROSION. REMOVED SUPPORTS AND INSTALLED SERVICEABLE SUPPORTS IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030407000892003040700089SO 2003 4 7 SIMA200306409 120030215A534713500439007 SEAT TRACK EMB 135 EMB135LR 3260305SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION, LEFT FORWARD LOWER SEAT TRACK CORRODED BETWEEN FRAME 18-23. REMOVED AND INSTALLED SERVICEABLE LEFT FORWARD SEAT TRACK IAW EMB 135 AMM 53-01-06. (M) 2L72 4F RTT00011AT 20030407000982003040700098NM 2003 4 7 TSAA0353005 120030120A53136545805 STRINGER BOEING737 7372M6C 1384708NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 TWO RIVETS SHOW CRACK INDICATIONS USING LFEC AT BS 227.8 STRINGER 27R. REMOVED ADJACENT FASTENERS AND STRINGER. USING HFEC CONFIRMED NO CRACK INDICATION USING ROTARY PROBE IAW BOEING TELEX ALO-HNL-03-0031H. (M) 2L72 4F RTA16WE 20030407001072003040700107NM 2003 4 7 UIEA200300011 120030225A542065B89058502 STIFFENER BOEING747 747243B 1384830NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15540MC87875 22508 DURING CURRENT C-CHECK AT SIAEC, FOUND NR 3 PYLON NR 3 LONGITUDINAL STIFFENER VERTICAL FLANGE, BELOW PRECOOLER EXHAUST VENT, CRACKED THREE PLACES AT NAC 245, 247 AND 257. PYLON PREVIOUSLY MODIFIED PER SB 747-54-2163 AND 747-54-2091 WHICH CONSISTS OF AN UPPER ANGLE INSTALLE DON THE STIFFENER FROM NAC 234 TO 272 ALONG WITH AN EXTERNAL SKIN DOUBLER. ADDITIONAL REPAIR CONSISTS OF A LOWER ANGLE INSTALLED FROM NAC 234 TO 252. CRACK AT NAC 257 MAY BE LEFT AS IS. HFEC INSPECTED ALL OPEN HOLES COMMON TO BOTH ANGLES AND HOLES IN THE REMAINING REPAIR. NO ADDITIONAL CRACKING FOUND ON STIFFENER OR ALUMINUM SKIN. REPAIR ANGLE INSTALLED PER STANDARD SRM PRACTICES IAW SB'S MENTIONED ABOVE. (M) 2L74 4F A20WE 20030408000032003040800003EA 2003 4 8 2003F00210 120030129A2611473052 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0777286 7286 FLT 6199 - DFW-PHX, AIRCRAFT HAD A MOMENTARY CARGO SMOKE INDICATION. MAINTENANCE PERFORMED A VISUAL INSPECTION. NO DEFECTS NOTED. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030815000672003081500067NE 2003 8 15 HEEA088470 220030718A7532312320301 BLEED VALVE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 BLEED VALVE CAUSES ENGINE TEMP TO VARY 80 DEGREES AT FLAT PITCH AFTER A POWER CHANGE THEN RETURNED TO ORIGINAL POWER SETTING. SENT TO AVIALL FOR EXCHANGE. 1G72 4U4 U H4SW E22EA 20030813001122003081300112WP 2003 8 13 GTIA030557 120030720A7120K22199SA31 MOUNT DOUG DC9 DC983 3022083WP ENGINE SHIFTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 DTW - FOUND FORWARD LOWER VIBE ISOLATION MOUNT SHIFTED. REPLACED FORWARD LOWER VIBE ISOLATION MOUNT. REPLACED FORWARD LOWER VIBE ISOLATION MOUNT. (M) 2L72 4F RTA6WE 20030813001812003081300181NM 2003 8 13 SWAA031691 120030728A53106546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 767, WL 148 AND RBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030813001862003081300186 2003 8 13 SWAA031554 420030715A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030813001872003081300187 2003 8 13 SWAA031555 420030714A2565 INDICATOR BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030813001902003081300190NM 2003 8 13 SWAA031558 120030715A335010126211 LIGHT BOEING737 7373H4 1384600NM EXIT SIGN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR VERTICAL EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030813001952003081300195NM 2003 8 13 SWAA031643 120030724A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030814000322003081400032NM 2003 8 14 SWAA031703 120030730A57536573732 SKIN BOEING737 7373H4 1384600NM OUTBD FORE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED SPECIAL VISIT, FOUND LT OUTBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT OUTBD T/E FORE FLAP PER MM. 2L72 4F RTA16WE 20030814000572003081400057NM 2003 8 14 UPS03241063 120030717A5532 PANEL BOEING727 72725C 138400HNM VERTICAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, VERTICAL FIN LEADING EDGE LOWER PANEL 9501, MATING STRAP HAS A CRACK IN THE OUTER SKIN. CRACK STOP DRILLED IAW SRM 51-10-01, REPAIR DOUBLER FABRICATED IAW SRM 51-20-01, FIG 7. REPAIR DOUBLER INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20030814000612003081400061SO 2003 8 14 SWIA200312114 120030618A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07190SW 120050 WHITE EMERGENCY TRACK LIGHTING A-BEAM GALLEY INOP, SINGLE LIGHT. INSPECTED AND FOUND BROKEN WIRE. REPAIRED BROKEN WIRE ON WHITE EMERGENCY LIGHT TRACK A-BEAM GALLEY IAW EMB120 WM 20-21-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030814000812003081400081EA 2003 8 14 SWIA200312086 120030528A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 FS 484 LT INTERCOSTAL O/B FLG CRACKED. DISCOVERED DURING C-CHECK. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-41-059 REV A. NDT-HFEC CARRIED OUT IAW REO 601R-53-41-059. NO CRACKS NOTED. 2L72 4F4 FRTA21EA E15NE 20030814001332003081400133NM 2003 8 14 0301196716 120030630A5330 SKIN BOEING747 747251F 1384898NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING L-CHECK FOUND CORROSION ON SKIN AT AFT CARGO DOOR CUTOUT LOWER CORNER BS 1920 S42R. REPAIRED PER EA 67-165074. 2L74 4F A20WE 20030814001362003081400136WP 2003 8 14 GTIA030573 120030701A5321 FLOORBOARD DOUG DC9 DC982 3022082WP CABIN DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND CABIN FLOOR BOARD FORWARD R1 DOOR CORRODED INSERTS, BOARD DELAMINATED, EDGE FILL INCOMPLETE. FABRICATED NEW PANEL. (M) 2L72 4F A6WE 20030814001392003081400139NM 2003 8 14 AALA20030396 120030401A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21626AA 24584 DFW - DURING OVERNIGHT OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 6E INOPERATIVE. SECURED EMERGENCY EXIT LIGHT WIRE HARNESS AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000592003081500059SW 2003 8 15 HEEA088504 120030623A6230 BEARING BELL 412 412 1182202SW LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0333008 36004 MAIN ROTOR LINK ASSY HAS WORN BEARINGS. REPLACED 4 EACH BEARINGS 412-310-400-107 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030819001512003081900151NM 2003 8 19 2003UALA00508 120030617A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29789UA 26935 UPPER FUSELAGE SKIN DENTED AT STA 654 STRINGER 6R TO 7R. 2L72 4F4 FRTT0001SE E46NE 20030819001562003081900156NM 2003 8 19 2003UALA00513 120030619A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29584UA 26706 EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE AT DOOR 4L. 2L72 4F4 FRTA2NM E17NE 20030819001652003081900165NM 2003 8 19 VNAA0308006 120030810A2910ZCV1571 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE HYD SYSTEM FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07431JS20827 3028 DURING FLIGHT, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR PRESSURE LOW CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE HYDRUALIC CHECK VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030819001672003081900167 2003 8 19 VNAA0308004 420030807A31407013348937 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NR 2 FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07471PS4373 1501 3007 IN FLIGHT, THE PROXY SYSTEM AND THEN THE NR 2 DATA ACQUISITION UNIT FAILED. FLIGHT 4069 THEN RETURNED TO PIT. MAINTENANCE THEN INSPECTED AND REPLACED THE NR 2 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030819001732003081900173WP 2003 8 19 UPS03840855 120030616A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LT WING CENTER L/E UPPER RIBS ARE CRACKED AT XFS 366.5 AND XFS 379. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030819001762003081900176NM 2003 8 19 SWAA031739 120030805A3350301500 LENS BOEING737 7372H4 138448CNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F A16WE 20030819001802003081900180NE 2003 8 19 VNAA0308007 220030811A7320 ECU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07431JS 3028 DURING TAKEOFF, THE LEFT HAND ENGINE CONTROL UNIT FAILED AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE THEN PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE THE INCIDENT. AFTER GOOD OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00, THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030819001812003081900181EA 2003 8 19 COMA0360359 120030811A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01999CA13087 7230 FLIGHT 5607 GEAR DISAGREE WARNING. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20030819001832003081900183EA 2003 8 19 COMA0360361 120030811A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01920CA 7022 FLIGHT 5739 GEAR DISAGREE WARNING. REPLACED THE RT MLG UPLOCK PROXIMITY SENSOR. 2L72 4F RTA21EA 20030819001852003081900185NM 2003 8 19 SWAA031785 120030809A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED (5 EA) IN CABIN. REMOVED AND REPLCED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030819001862003081900186NM 2003 8 19 UPS03640982 120030717A5245149T721063 DOOR BOEING767 76734AF 1385212NM A/C BAY SEPARATED A IPXAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 SO01304UP 27242 LOUD THUMP HEARD AT 27,000 FT ALT. UPON ARRIVAL FOUND LT AIR CON BAY DOOR MISSING WITH SURROUNDING DAMAGE, LEFT ECS BAY DOOR (193NL) MISSING & DAMAGED THE AIRCRAFT UPON ITS DEPARTURE. FOLLOWING ITEMS ARE OPENED AGAINST THE DOOR & DAMAGE. ACCOMPLISHED EO B767-5100-18952. 2L72 4F RTA1NM 20030819001882003081900188NM 2003 8 19 SWAA031783 120030810A53116935365 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 296, WL 208.5 AND RBL 55. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030819001902003081900190EA 2003 8 19 SWIA200312204 120030719A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07412SW 7101 OVERHEAD EMERGENCY LIGHT NEXT TO LAV IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. P/N: 1317. 2L72 4F RTA21EA 20030819001992003081900199WP 2003 8 19 UPS03840854 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RT WING OUTBOARD LE LOWER RIB IS CRACKED AT XFS 816. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030815000862003081500086 2003 8 15 HEEA088419 420030716A2215A7701878 STOP SKRSKYS76 S76A 8143006NE AFCS ACTUATOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035435V 98050411 760158 AFCS ACTUATOR STOP SHAFT WILL NOT CENTER. INSPECTED BY ACCESSORY SHOP AND FOUND THAT STOP SHAFT WOULD NOT CENTER BACK ON TEST. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030815000962003081500096NE 2003 8 15 HEEA088388 120030712A77140177555240 TACHOMETER SKRSKYS76 S76A 8143006NE ENG OVERSPEED INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 OVERSPEED LIGHT INTERMITTENTLY COMES ON FOR NO REASON. TO BE SENT TO VENDOR. 1G72 3U H1NE 20030818000552003081800055SW 2003 8 18 HEEA088516 120030423A6720PHI41294 BEARING BELL 412 412 1182202SW TAIL ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 TAIL ROTOR HEAD HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030818000762003081800076 2003 8 18 HEEA088612 420030731A34221113025 INDICATOR BELL 412 412 1182202SW HSI ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 COMPASS CARD READS ERRATIC. 1G72 4U H4SW 20030818000882003081800088EU 2003 8 18 BAQA088352 120030807A2150510286C GEARBOX UROCOPEC135 EC135T1 5620026EU 90 DEGREE SEIZED B BAQAK NONE O OTHER NRNOT REPORTED 1 EA03554ME363 0154 90 DEGREE GEARBOX SEIZED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030819000092003081900009EU 2003 8 19 KBMA088152 120030702A6520350A33215001 BEARING AEROSPAS355 AS355* EU T/R SPIDER WORN B KBMAK NONE O OTHER ININSP/MAINT 1 WP19345SH 3345 TAIL ROTOR SPIDER END BALL BEARING WAS WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030819000282003081900028NM 2003 8 19 AALA20030693 120030616A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21369AA 25196 FOUND CORROSION ON BEAM RBL 33 STATION 780-840 OUT OF SRM LIMITS. REMOVED CORROSION FROM AREA, DYE PENETRANT OF AREA FOR CRACKS. ROTO PEENED BLENDED AREA. APPLIED ALODINE AND 2 COATS OF PRIMER, FILLED BLENDED AREA WITH BMS 5-95 SEALANT. (M) 2L72 4F RTA1NM 20030819000392003081900039NM 2003 8 19 AALA20030695 120030623A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21792AN 30253 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS COAT CLOSET EMERGENCY EXIT LIGHT BROKEN. REPLACD FIRST CLASS COAT CLOSET EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030819000492003081900049EA 2003 8 19 A6WA200340107 120030713A2931 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA HYD PRESSURE ILLUMINATED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31444ZW 7788 AFTER TAKEOFF, RECEIVED EDP HYD. (M) 2L72 4F RTA21EA 20030819000762003081900076NM 2003 8 19 CALA0300391 120030715A5347 SEAT TRACK BOEING777 777224 1385225NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778009 29479 INSPECTION FOUND SEAT TRACK CROWN CORRODED AT BS 1497-1530, RBL 74. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 3, FIGURE 202. 2L72 4F RTT00001SE 20030819000932003081900093EA 2003 8 19 COMA0360357 120030807A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01518CA 7816 FLIGHT 5439 FLAPS FAILED AT 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030819001132003081900113WP 2003 8 19 0301279615 120030708A213110256861 CONTROLLER DOUG DC9 DC932 3022066WP CABIN PRESSURE MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CRCRUISE 1 GL01615NW 47129 AT FL330, THE CABIN ALTITUDE BEGAN CLIMBING AS PRESSURIZATION BECAME UNCONTROLLABLE. A RAPID DESCENT WAS NOT NECESSARY BECAUSE THE CABIN HAD REACHED 14,500 FT AND ALL OF THE PASSENGER OXYGEN MASKS DEPLOYED. COMPLIED WITH COM PROCEDURES AND FLT CONTINUED TO DESTINATION AT 10,000 FT. THE LANDING WAS UNEVENTFUL AT ATL. MAINTENANCE REPLACED THE PRESSURE CONTROLLER, ALL USED OXYGEN GENERATORS, AND REPACKED THE MASKS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030819002082003081900208NM 2003 8 19 UPS03241005 120030711A5310 DOUBLER BOEING727 72725C 138400HNM BEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, CORROSION ON DELTA BEAM LT WEB DOUBLER AT BS 740. REMOVED CORRODED DOUBLER IAW SRM 51-30-02. REMOVED CORROSION FOUND ON DELTA BEAM WEB & FOUND TO BE WITHIN LIMITS IAW SRM 51-10-01 & 53-1 0-2. FABRICATED REPAIR PARTS IAW SRM 53-10-2. CARRIED OUT REPAIR IAW SRM 51-20-1 FIG 7. 2L73 4F A3WE 20030819002102003081900210NM 2003 8 19 UPS03241007 120030715A5313 STRINGER BOEING727 72725C 138400HNM B HYD SYS BAY DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, HOLE IN FLANGE OF STRINGER B-HYD SYS COMPARTMENT O/B OF HYD RESERVOIR. REPAIRED STRINGER IAW SRM 53-10-3 FIG 2, DAMAGED REMOVED IAW SRM 51-10-06. CUT LINE TO BE NDT'D HFEC INSP CARRIED OUT AROUND CUT LINE ON THE ABOVE AREA IAW B727 NDTM PT 6 51-00 -00 FIG 4 RESULT - NDF. 2L73 4F A3WE 20030819002132003081900213CE 2003 8 19 DXTA200300068 120030715A2910 HYDRAULIC SYSTEM CESSNA750 750 2076810CE LT ENGINE LEAKING A DXTAO OTHER K FLUID LOSS CRCRUISE 1 GL07935QS 7500135 IN CRUISE AT FL 410 HYDRAULIC VOLUME LOW CAS MESSAGE ILLUMINATED ON THE A-HYD SYSTEM, VOLUME SHOWED 16 PERCENT. INITIATED EMERGENCY CHECKLIST AND UNLOADED THE A-HYD PUMP, USED THE EMERGENCY BLOWDOWN SYSTEM TO LOWER THE GEAR. GOOD BRAKES AND STEERING AFTER LANDING, ON POST FLIGHT FOUND FLUID DRIPPING FROM LT ENG DRAIN MAST. TROUBLESHOT AND FOUND LT ENG DRIVEN HYDRAULIC PUMP FAILED. REMOVED AND REPLACED HYDRAULIC PUMP, DRAINED HYDRAULIC SYSTEM "A" & CLEAN SYSTEM "A" FILTERS, SERVICED HYDRAULIC SYSTEM AND BLED SYSTEM AGAIN. INSTALLED NEW FILTERS AND OPS CHECKED GOOD IAW CE 750 MM CHAPTER 29-10-08. 2L72 4J RTT00007WI 20030819002192003081900219NM 2003 8 19 2003UALA00588 120030723A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29199UA 28717 FLOORBEAM UPPER FLANGE IS BENT AT BL 0 AND BS 1800. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER CHORD. 2L74 4F4 FRTA20WE E24NE 20030819002242003081900224EA 2003 8 19 SWIA200312140 120030527A5220 ESCAPE HATCH CNDAIRCL600 CL6002B19 1900309EA FUSELAGE OUT OF ADJUST A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 CREW ESCAPE HATCH STEP PROFILE AND EDGE GAPS TO FUSELAGE SKIN ARE OUT OF LIMITS. ADJUSTMENT OF THE CREW ESCAPE HATCH CARRIED OUT IAW CRJ MM 52-22-00. NO FAULTS FOUND ON FUNCTIONAL TEST OF CREW ESCAPE HATCH. 2L72 4F RTA21EA 20030815000682003081500068SW 2003 8 15 HEEA088471 120030715A2841393008047 INDICATOR BELL 412 412 1182202SW FUEL SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 FUEL INDICATOR INTERMITTENT FLUCTUATION. 1G72 4U H4SW 20030815000752003081500075 2003 8 15 HEEA088453 420030710A34211113034 INDICATOR BELL 412 412 1182202SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 ATTITUDE INDICATOR GLIDE SLOPE FLAG WILL NOT PULL. 1G72 4U H4SW 20030815000762003081500076 2003 8 15 HEEA088454 420030710A34211113034 INDICATOR BELL 412 412 1182202SW ATTITUDE PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 ATTITUDE INDICATOR PRECESSING. 1G72 4U H4SW 20030815000842003081500084SW 2003 8 15 HEEA088466 120030714A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P14444 33012 STARTER GENERATOR WILL NOT ENGAGE. 1G72 4U H4SW 20030818000132003081800013NE 2003 8 18 HEEA088422 120030711A7600NYLC504482 MOTOR SKRSKYS76 S76A 8143006NE BEEP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 STICKS ON LOW SIDE GOING UP. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030818000312003081800031NE 2003 8 18 HEEA088383 120030712A2400A1077B RELAY SKRSKYS76 S76A 8143006NE DC SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 GENERTOR LIGHT WILL NOT GO OUT, DC POWER IS SUPPLIED TO SYSTEM. SENT TO PRECISION HELIPARTS FOR WARRANTY REPAIR. 1G72 3U H1NE 20030818000582003081800058SW 2003 8 18 HEEA088532 120030722A6320206040184001 PUMP BELL 206 206B3 1181506SW OIL SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032275Y 3626 MAIN ROTOR GEARBOX OIL PUMP LEAKING. IN SHOP REPAIR. 1G71 3U H2SW 20030818000602003081800060SW 2003 8 18 HEEA088534 120030803A3246206053184101 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 SKID TUBE CORRODED AND WORN FLAT SPOTS ON THE BOTTOM OF THE SKID. IN SHOP REPAIR. 1G71 3U H2SW 20030818000682003081800068SW 2003 8 18 HEEA088581 120030728A6230 BEARING BELL 412 412 1182202SW LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH A2213 33150 MAIN ROTOR LINK ASSY BEARINGS WORN. SHOP REPAIR. 1G72 4U H4SW 20030818000872003081800087EU 2003 8 18 BAQA088351 120030724A2821430129501 FUEL FILTER BOLKMS117 BK117A1 5626010EU FUEL SYSTEM WILL NOT TEST B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03587MC2380 7086 FUEL FILTER BYPASS TEST FAILED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030819000172003081900017WP 2003 8 19 AALA20030653 120030611A3350 CIRCUIT BOARD DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21584AA 53247 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT ROWS 13-17 INOPERATIVE. REPOSITIONED EMERGENCY EXIT LIGHT BATTERY CIRCUIT BOARD AT TERMINAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030819000192003081900019NM 2003 8 19 AALA20030656 120030611A3350 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219630A 53561 SEA - DURING OVERNIGHT MAINTENANCE, FORWARD LEFT TAIL COMPARTMENT EMERGENCY EXIT LIGHTING SIGN INOPERATIVE. REPLACED FORWARD LEFT TAIL COMPARTMENT EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030815000452003081500045SW 2003 8 15 HEEA088489 120030422A6710212001034101 FORCE GRADIENT BELL 412 412 1182202SW FLT CONTROLS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 FORCE GRADIENT STICKING AND BEARING WORN. REPAIRED. 1G72 4U H4SW 20030815000902003081500090 2003 8 15 HEEA088430 420030703A2312064102302 TRANSCEIVER SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER NRNOT REPORTED 1 SW03762P 760060 EMITS LOUD POPPING SOUND AND TRANSMITS AND RECEIVE GARBLED. REPLACED BAD I305 IC CHIP. REPAIRED PROBLEM. REMOVED CORROSION FROM CHASSIS. ADJUSTED C/N SQUELCH AND REALIGNED TRANSMITTER. BENCH CHECK GOOD. 1G72 3U H1NE 20030815000932003081500093 2003 8 15 HEEA088440 420030709A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH6941 760224 AFCS ACTUATOR WORN AND CORRODED. REPLACED CLUTCH WASHER A768336-1 DUE TO WORN; ROD END BEARING MS21151-8C DUE TO ROUGH; POTENTIOMETER (2 EA) A768343-3 DUE TO NULL IN CENTER. REPAIRED. 1G72 3U H1NE 20030815000942003081500094 2003 8 15 HEEA088441 420030726A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 AFCS ACTUATOR WILL NOT WORK. INSPECTED BY ACCESSORY SHOP AND FOUND UNIT TO BE INOPERATIVE. SENT TO HELICOPTER SUPPORT, INC. FOR WARRANTY REPAIR. 1G72 3U H1NE 20030818000442003081800044EU 2003 8 18 BAQA088661 120030807A3710907BDC2224 PUMP BOLKMSBK117 BK117C1 5626025EU VACUUM SYS INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY218 7544 VACUUM PUMP INOPERATIVE. PART HAS 218 HOURS ON IT SINCE NEW. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030818000482003081800048NE 2003 8 18 CCHA088667 220030809A73200319928460 HMU UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ENGINE DEFECTIVE B CCHAO OTHER S AFFECT SYSTEMS CRCRUISE 1 SO19911CK1445 0138 30172 ENGINE DEGRADE LIGHT IN FLIGHT RETURNING TO BASE. MEMORY FAULT CODES 117 & 118. (RESOLVER & FEDEC FAIL) FAULT CODES CLEARED UPON NEXT START, HOWEVER TOT DURING START REACHED 895 FOR ONE SECOND. REPLACED HMU WITH S/N 198B. 1G72 3U3 U H88EU E34NE 20030818000832003081800083 2003 8 18 HEEA088635 420030804A2312071121540 CONTROL UNIT BOLKMS105 BO105S 5626006EU COMMS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033071K S859 CHANGED WITH KTR908 TRANSCEIVER DUE TO PILOT REPORTED STATIC IN COMM 2 SYSTEM. IN SHOP REPAIR. 1G72 3U H3EU 20030818000842003081800084EU 2003 8 18 HEEA088636 120030804A63201054190206 OUTER DEFLECTION BOLKMS105 BO105S 5626006EU M/R GEARBOX SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR GEARBOX OUTER DEFLECTION SPLIT IN THE BEND RADIUS. TO BE SENT TO VENDOR FOR CREDIT. 1G72 3U H3EU 20030818000972003081800097EU 2003 8 18 BAQA088103 120030715A28411179405403 INDICATOR BOLKMS117 BK117B1 5626012EU FUEL QTY FLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03912TG2041 7174 MAIN TANK NEEDLE FLUCTUATING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030819000252003081900025NM 2003 8 19 AMTA200300929 120030714A26125816 FIRE DETECTOR BOEING757 75733N 1384931NM APU BAY INOPERATIVE A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11554TZ 32588 EICAS STATUS MSG, APU FIRE LP1 DISPLAYED. REMOVED AND REPLACED APU NR 1 FIRE LOOP DETECTOR IAW 757 MM 26-15-02-4, OPS CHECK OK. (M) 2L72 4F RTA2NM 20030819000312003081900031NM 2003 8 19 AALA20030503 120030427A2420GEN3005 IDG BOEING757 757223 1384957NM RT ENGINE FAILED A AALAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SW21608AA 27446 RIGHT GENERATOR DRIVE LIGHT ILLUMINATED IN CRUISE FOLLOWED BY RIGHT GENERATOR CONTROLLER LIGHT FOLLOWED PCDR PRESSED RIGHT GEN DRIVE DISCONNECT SWITCH. APU STARTED OK, NORMAL OPS SUBSEQUENTLY. REMOVED AND REPLACED RIGHT IDG NR 2 ENGINE, SERVICED IDG. RAN ENGINE, OPS CHECK NORMAL ON ALL PARAMETERS. NO LEAKS NOTED PER AMM. (M) 2L72 4F RTA2NM 20030819000412003081900041EA 2003 8 19 A6WA200340105 120030624A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31417AW 7610 IDG CAUTION APPEARED ON TAKEOFF ROLL. COMPLIED WITH 'CM' ACTION PLACARDED AND PLACED ON MEL. RESET NR 2 IDG DISCONNECT MECHANISM. SERVICED IDG AS REQUIRED, OPS CHECK GOOD. REMOVED FROM MEL. (M) 2L72 4F RTA21EA 20030819000732003081900073NM 2003 8 19 2003UALA00452 120030529A3260849704 PSEU BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29641UA78 25091 WITH GEAR UP AND GEAR HANDLE OFF, THREE GREEN LIGHTS AND TAIL SKID LIGHT ILLUMINATED. LANDING GEAR MONITOR AND WARNING ELEX STATUS MESSAGES ILLUMINATED. REPLACED PSEU AND ELEX WARNING POWER SUPPLY MODULE. 2L72 4F4 FRTA1NM E24NE 20030819001012003081900101NM 2003 8 19 C1HA200381024 120030808A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 SEAT TRACK CRACKED AT BS 960 LBL 45. 2L73 4F A3WE 20030819001362003081900136NM 2003 8 19 CALA0300358 120030703A521060B100076 ROD END BOEING757 757224 1384958NM L-4 DOOR SHEARED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717122 27564 THE L-4 DOOR LOWER LATCHING SHAFT AFT OUTPUT ROD EYE END WAS FOUND SHEARED AT CONNECTION TO GIRT BAR. THE OUTPUT ROD WAS REPLACED IAW MM 52-11-20 AND GIRT BAR RIG HOLES CHECKED WITH RIGGING HOLES ON LOWER GATE IAW MM 52-11-01. 2L72 4F RTA2NM 20030819001462003081900146EA 2003 8 19 SWIA200312152 120030626A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 284 RT INTERCOSTAL O/B FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F4 FRTA21EA E15NE 20030819001542003081900154NM 2003 8 19 2003UALA00511 120030617A339758783 WIRE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29949UA 26692 EMERGENCY ELECTRICAL LIGHTING (EEL) INOPERATIVE BETWEEN ROWS 14 AND 19. REPLACED FEEDER CABLE. 2L72 4F4 FRTA16WE E2GL 20030819001612003081900161NE 2003 8 19 2003UALA00600 220030730A7230 BLADE BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29528UA 25018 RIGHT ENGINE COMPRESSOR STALL, EGT OVERTEMP. OIL PRESSURE DROPPED TO ZERO. ENGINE TEARDOWN VERIFIED THAT THE HPT T1 BLADE FAILED. PRATT & WHITNEY HAS BEEN INVESTIGATING THIS FAILURE FOR ROOT CAUSE AND DETERMINED THAT THE SYMPTOMS AND PART CONDITION ARE UNIQUE IN THIS EVENT. THE HPT T1 BLADE FAILED FROM A STRESS CORROSION CRACK ABOVE THE PLATFORM. AS AN ADDED NOTE, THIS TURBINE BLADE DID NOT HAVE PWA 545 PROTECTIVE COATING IN THE DAMPER POCKET. 2L72 4F4 FRTA2NM E17NE 20030819002252003081900225EA 2003 8 19 SWIA200312141 120030619A2760270003 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07403SW8616 8616 7028 ON TAXI OUT RECEIVED A SPOILERON (RIGHT) MESSAGE, WAS UNABLE TO CLEAR. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW 27-60-00. OPS CHECK GOOD. NO LEAKS NOTED. 2L72 4F RTA21EA 20030819002302003081900230 2003 8 19 DXTA200300051 420030621A3400 DISPLAY CESSNA560 560XL 2076702CE COCKPIT LIGHTNING STRIKEE DXTAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL07629QS 5605306 AIRCRAFT STRUCK BY LIGHTNING, AVIONICS SCREENS LOOK LIKE TIE DYE SHIRTS. SEEMS TO HAVE ENTERED THROUGH THE NOSE (CO-PILOT SIDE DIVERTER SCREW) EXITED OUT A BURNED HOLE OVER CO-PILOT SIDE SECOND PAX WINDOW. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20030819002382003081900238NM 2003 8 19 2003UALA00523 120030628A2780 MODULE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LE FLAPS LOOSE A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29378UA 24653 AIRCRAFT ABORTED TAKEOFF WHEN FORWARD PANEL L/E FLAP INTRANSIT LIGHT AND OVERHEAD PANEL L/E FLAP INTRANSIT LIGHT ILLUMINATED. TROUBLESHOOTING REVEALED THAT PIN NR 14 ON CONNECTOR D728B OF THE M229 FLAP/SLAT POSITION INDICATION MODULE WAS PUSHED BACK AND NOT LOCKED IN THE CONNECTOR, RESULTING IN AN OPEN CIRCUIT. THE PIN WAS REINSTALLED IN THE CONNECTOR AND VERIFIED TO LOCK IN PLACE. TAKEOFF WARNING TEST WAS ACCOMPLISHED AND SYSTEM OPERATED PROPERLY. 2L72 4F4 FRTA16WE E2GL 20030820000232003082000023NM 2003 8 20 03FDEA01006 120030624A5753ARC2512503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT WING, INBOARD TRAILING EDGE FLAP, OUTBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE INBOARD SIDE CORRODED (FLAP SIDE). REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5750-69357 WINGS - TRAILING EDGE & TRALING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030820000422003082000042NM 2003 8 20 03FDEA01139 120030723A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT I/B FLAP (FLAP SIDE) - O/B HINGE O/B PIVOT HOLE AND LUG INNER AND OUTER SURFACE CORRODED. RT I/B FLAP (FLAP SIDE)- O/B HINGE, O/B PIVOT HOLE AND LUG INNER AND OUTER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69257 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RH INBD FLAP HINGE BRACKET ASSY REPAIR. 2L73 4F RTA22WE 20030820000452003082000045NM 2003 8 20 03FDEA01136 120030723A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT O/B FLAP (FLAP SIDE) - I/B HINGE O/B ACTUATOR ATTACHMENT HOLE CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE O/B ACTUATOR ATTACHMENT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS - TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030820000522003082000052NM 2003 8 20 03FDEA00922 120030618A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE FOUND CORROSION. RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE REPAIRED AS PER FEDEX EA1-5750-69375, RIGHT HAND OUTBOARD FLAP - INBOARD SUPPORT BRACKET - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030820000582003082000058NM 2003 8 20 03FDEA01261 120030812A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 CORROSION 28 C53-224-01 281 29 29 AT FASTENER HOLE 2C ON FLOORBEAM 2C LOWER SIDE OF FLANGE 2C STA 680 2C RBL 41 WL 208. REMOVED CORROSION BS 680, RBL 41 AND RBL 37 OUT OF LIMITS. REPAIRED FLOORBEAM IAW SRM 53-10-1 AND EA 7-5310-54933. 2L73 4F RTA3WE 20030820000592003082000059WP 2003 8 20 03FDEA00855 120030604A5410 BOLT DOUG DC10 DC1030 3023501WP NR 1 PYLON LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 REF EO 8-5410-7-3321 ITEM A 1 AND 2 GAIN ACCESS TO NR 1 PYLON AFT BULKHEAD REAR BOLTS, 5 OF THEM FOUND LOOSE. EO 8-5410-7-3321 BOLTS WERE INSPECTED AND HOLES CHECKED BY NDT DEPT. BOLTS RETORQUED AND AREA PREP FOR CLOSING. 2L73 4F A22WE 20030820000722003082000072NM 2003 8 20 03FDEA01116 120030719A2612 FIRE WARNING BOEING727 727200 138407ENM COCKPIT FALSE ACTIVATIONA FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25266FE 21672 SHORTLY AFTER TAKEOFF WHILE CLIMBING THROUGH 3000 FEET THE FIRE WARNING LIGHT ON THE CENTER FWD PANEL ILLUMINATED, ACCOMPANIED BY THE FIRE WARNING BELL. THE WARNING LASTED FOR APPROXIMATELY 2-3 SECONDS WITH NO OTHER INDICATIONS AND DISCONTINUED SPONTANEOUSLY WITH NO CREW ACTION REQUIRED. TESTED FIRE WARNING SYSTEM SEVERAL TIMES, OPS CHECK NORMAL AT THIS TIME REF B727-200 MM CHAP 26-11-001. 2L73 4F RTA3WE 20030820000772003082000077NM 2003 8 20 03FDEA01121 120030721A5330 STRUCTURE BOEING727 727200 138407ENM PYLON-BODY WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25494FE 21532 NR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350. 2L73 4F RTA3WE 20030820000852003082000085 2003 8 20 03FDEA00869 420030613A34426225132101 TRANSFORMER BOEING727 727200 138407ENM WEATHER RADAR FAILED A FDEAA UNSCHED LANDING O OTHER CRCRUISE 1 SO25236FE 21330 ON THE 20-40 MILE RANGE THE FAIL MESSAGE APPEARS WITH NO RETURNS. AT THE 80 MILE RANGE IT WOULD WORK INTERMITTENLY. REMOVED AND REPLACED WX RADAR R/T IAW 727 M/M 34-41-041-4. OK FOR SERVICE. 2L73 4F RTA3WE 20030815001002003081500100EU 2003 8 15 BAQA088269 120030801A6320L633M2010101A004MOUNT UROCOPEC135 EC135P1 8680990EU MAIN ROTOR LEAKING B BAQAK NONE O OTHER NRNOT REPORTED 1 EA03601FH504 0069 MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030818000082003081800008NE 2003 8 18 HEEA088400 120030805A62207610608000050 DAMPENER SKRSKYS76 S76A 8143006NE MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03763P 760166 MAIN ROTOR DAMPENER LEAKING. SHOP REPAIR. 1G72 3U H1NE 20030818000142003081800014NE 2003 8 18 HEEA088423 120030724A2150PHIS761017801 A/C PACK SKRSKYS76 S76A 8143006NE ODOR E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 LOAD SHED BOX HAS BURNED ODOR WHEN COVER REMOVED - AIR CONDITIONER INOPERATIVE. SHOP REPAIR. 1G72 3U H1NE 20030818000432003081800043SW 2003 8 18 AGQA088682 120030605A2435212075199001 CONTACTOR BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NR 1 ENGINE BROKEN W AGQAK NONE O OTHER ININSP/MAINT 1 EA138530F 30920 INTERMITTENT, SLOW STARTS, CONTACTOR. 1G71 4U4 U H4SW E22EA 20030819000022003081900002EU 2003 8 19 BAQA088110 120030709A2841L316M30C1004 DISPLAY UROCOPEC135 EC135P1 8680990EU FUEL QTY ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME43 0009 FUEL QUANTITY ERRATIC. 135-SB31-006-2.C REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030819000322003081900032NM 2003 8 19 AMTA200300930 120030714A2613 WARNING LIGHT BOEING757 75733N 1384931NM LT ENGINE ILLUMINATED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11557TZ 32591 LT ENGINE OVERHEAT EICAS MSG ILLUMINATED. ALL ATA PROCEDURES COMPLETED. LIGHT EXTINGUISHED. FLIGHT COMPLETED NORMALLY. PERFORMED BITE CHECK PER FIM 26-12-00 FIG 103. VISUALLY INSPECTED NR 1 ENGINE PYLON AREA, NO DEFECTS FOUND. RAN ENGINES 15 MINUTES, NO OVERHEAT DETECTED. (M) 2L72 4F RTA2NM 20030819000652003081900065EA 2003 8 19 SWIA200312123 120030616A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 280 FLOORBEAM O/B ATTACH ANGLE RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601R31113-58. 2L72 4F4 FRTA21EA E15NE 20030819000962003081900096WP 2003 8 19 UPS03841047 120030717A5413 STRINGER DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, STRINGER S-61 HAS VERTICAL CRACK 1 ALT. REMOVEDD DAMAGED STRINGER SECTION. REPLACED CORRODED AFT END FITTING P/N 3640143-503, FABBED 2 EA SPLICE RPR ANGLES IAW DC8 SRM 57-2-2. LOC ATED AND DRILLED STRINGER SECTION, 2 EA SPLICE RPR ANGLES, & FITTING; ALODINED & PRIMED; INSTALLED ALL IAW DC8 SRM 51-1-8, 57-2-2, 51-1-24, 51-1-20D, 51-1-23, AND 51-3-0. 2L74 4F RT4A25 20030819001252003081900125NM 2003 8 19 0301146312 120030619A335020131A POWER SUPPLY BOEING757 757251 1384970NM EMERGENCY LIGHT FAILED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01511US 23199 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE SEATS 1-32. REPLACED POWER SUPPLY AT DOOR 2R M732, P/N 2013-1A. 2L72 4F RTA2NM 20030819001282003081900128NM 2003 8 19 UPS03540912 120030628A2750 FSEU BOEING757 75724APF 1384969NM TE FLAPS INOPERATIVE A IPXAO OTHER J WARNING INDICATION DEDESCENT 1 SO01459UP 25480 T/E FLAP DISAGREE WHEN POSITIONING FLAPS FROM 20 TO 30 SETTING ACCOMPLISHED T/E FLAP DISAGREE CHECKLIST NORMAL 20 FLAP LANDING ACCOMPLISHED. PERFORMED FIM 27 BLOCK 108 FOUND NR 1 FSEU SHOW NO MOVEMENT. NR 2 & 3 FSEU'S SHOW EXTERNAL FAULTS. REMOVED AND REPLACED NR 1 FSEU PER 27 51 01. OPS CHECKS NORMAL AT THIS TIME. 2L72 4F RTA2NM 20030819002022003081900202 2003 8 19 SWAA031779 420030809A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29436WN 32456 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030819002212003081900221NM 2003 8 19 751PA0020 120030718A3350 INDICATOR BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAO OTHER L NO TEST NRNOT REPORTED 1 SO05751PA 23928 EMERGENCY LIGHT INDICATOR INOP AND LENS BROKEN AT SEAT ROW 20ABC. RELAMPED AND REPLACED BROKEN LENS CAP. CHECKS OK PER MM 25-60. 2L72 4F RTA2NM 20030820000162003082000016NM 2003 8 20 03FDEA00952 120030623A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 CRACKED FRAME SHEAR TIE STA 540 ABOVE STR 18L. REPAIRED SHEAR TIE BS 540 ABOVE STR 18L IAW SRM 51-40-3. 2L73 4F RTA3WE 20030820000202003082000020NM 2003 8 20 03FDEA00849 120030603A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-113-01(17) SHEAR TIE BS 560 BETWEEN STR 26-27L. CORROSION ON SHEAR TIE IN A .75 X .75 INCH AREA FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-1, 51-30-2, 51-10-2. 2L73 4F RTA3WE 20030820000292003082000029NM 2003 8 20 03FDEA00860 120030606A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25487FE 21490 CORROSION (C53-113-01), ON FRAME BS 950D STR 29R. CUT OUT AND REMOVED DAMAGED AREA OF FRAME. FABRICATED AND INSTALLED REPAIR BS 950D, STR 29R IAW SRM 53-10-4, FIG 15. 2L73 4F RTA3WE 20030820000362003082000036NM 2003 8 20 03FDEA01067 120030625A5730APB74411 SKIN PANEL DOUG MD11 MD11 3023602NM CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 MAIN DECK - BETWEEN BS 1215-1235, RIGHT XCW 0-50, CENTER WING UPPER PANEL STRUCTURE FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK. 2L73 4F RTA22WE 20030820000992003082000099NM 2003 8 20 VNAA0308003 120030805A21505729C000002 A/C PACK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RIGHT FAILED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07440JS110875043 3058 THE CREW REPORTED THAT WITH BLEED AIR SELECTED, THERE WAS SMOKE AND NOISE COMING FROM THE RIGHT HAND PACK. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND FOUND THE AIR COOL MACHINE BLADES WERE DAMAGED. MAINTENANCE THEN REPLACED THE RIGHT HAND PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030820001302003082000130NM 2003 8 20 CALA0300430 120030731A5753 BRACKET BOEING737 737524 1384721NM NR 8 FLAP TRACK CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND A .75 INCH CRACK IN RT WING NR 8 FLAP TRACK FORWARD FAIRING ATTACH BRACKET. REPAIRED IAW ECRA 5740-02040. 2L72 4F RTA16WE 20030819001622003081900162NM 2003 8 19 2003UALA00601 120030722A5754114N300358 WEDGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29518UA 24871 T/E WEDGE DELAMINATED AND SECTION HAD INFLIGHT SEPARATION. MAJOR REPAIR ACCOMPLISHED. REPLACED T/E WEDGE. 2L72 4F4 FRTA2NM E17NE 20030819001662003081900166 2003 8 19 VNAA0308005 420030808A34427008470822 INDICATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE WX RADAR FAILED A VNAAO OTHER O OTHER CLCLIMB 1 GL07459PS149395384 3070 DURING FLIGHT, THE WEATHER RADAR FAILED INTERMITTENTLY AND THE CREW RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE WEATHER RADAR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030819001792003081900179EA 2003 8 19 COMA0360355 120030809A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYS FAILED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01457CA9584 7612 FLIGHT 5476, NR 2 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED THE NR 2 EDP. 2L72 4F RTA21EA 20030815000632003081500063SW 2003 8 15 HEEA088460 120030710A2435209060221001 STARTER GEN BELL 412 412 1182202SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K2841 33020 STARTER GENERATOR INOPERATIVE. 1G72 4U H4SW 20030818000162003081800016 2003 8 18 HEEA088365 420030706A34221113025 INDICATOR SKRSKYS76 S76A 8143006NE HSI STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 COMPASS CARD STICKS. 1G72 3U H1NE 20030818000222003081800022SW 2003 8 18 HEEA088450 120030804A2820214066226103 CHECK VALVE BELL 412 412 1182202SW FUEL SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0333008 36004 FUEL SYSTEM CHECK VALVE FAILURE. 1G72 4U H4SW 20030818000292003081800029 2003 8 18 HEEA088381 420030724A22107690001812102 BRAKE SKRSKYS76 S76A 8143006NE AUTOFLIGHT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 FORE AND AFT CYCLIC STIFF AND RATCHETY. 1G72 3U H1NE 20030819000792003081900079 2003 8 19 RAIA00306175 420030626A2215 CONTROL CABLE AEROSPATR42 ATR42300 8680920EU A/P ROLL SERVO FRAYED A RAIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CE03426TE 228 CREW REPORTED AILERONS AS STICKY. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT ROLL SERVO CABLES. 2H72 4T RTA53EU 20030819000812003081900081WP 2003 8 19 UPS03841044 120030708A53476015176 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, CENTER FLOOR TRACK BL 0 STA 1190 IS EXCESSIVELY WORN. BLENDED FLOOR TRACK (ORIG .420, REM .550) OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGED FLOOR TRACK, LOCATED, DRILLED & DEBURRED NEW SEAT TRACK 60-15176 IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK IAW DC8 SRM 53-2-3/51-3-0. 2L74 4F RT4A25 20030819001412003081900141EA 2003 8 19 SWIA200312147 120030627A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07590SW 7077 FLIGHT TO SLC FLAPS FAIL CAUTION. FLAPS UP, CONTINUED TO SLC. REPLACED LEFT BRAKE POSITION SENSOR UNIT. OPS CHECK GOOD IAW 27-51-10. P/N OFF/ON 855D100-9, S/N OFF 593A. 2L72 4F RTA21EA 20030819001682003081900168 2003 8 19 VNAA0307010 420030731A34427008470822 CONTROL UNIT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE WEATHER RADAR FAILED A VNAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07432JS1546095 3045 WHILE EN ROUTE FROM PHL TO GSP CREW REPORTED RADAR INOPERATIVE. CREW DIVERTED TO PIT WHERE MAINTENANCE REPLACED THE RADAR UNIT. AIRCRAFT DEPARTED WITH NO OTHER MAINTENANCE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030819001722003081900172EA 2003 8 19 SWIA200312128 120030616A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117 REV A. P/N: 601R-53-61-117-4. 2L72 4F4 FRTA21EA E15NE 20030819002422003081900242NM 2003 8 19 2003UALA00530 120030701A2421420990 WIRE HARNESS BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE LT IDG DAMAGED A UALAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION NRNOT REPORTED 1 WP29205UA 28714 GENERATOR FAILED PRIOR TO ETOPS ENVIRONMENT. A PRIOR ON FINAL APPROACH TO SFO ON 6/30/2003. LEFT IDG WAS REPLACED AND OPERATIONAL CHECKED NORMAL. THE SIMILAR PROBLEM OCCURRED IN FLIGHT FROM SFO-KIX ON 7/1/2003 WITH THE AIRCRAFT RETURNING TO SFO. PERFORMED WIRING CHECK OF ROLS FROM GCU PER FIM24-11, TASK 807. RESERVICED AND RECONNECTED THE IDG. RAN ENGINE PER JRH AND OPERATIONAL CHECKED OF THE GENERATOR WAS NORMAL. PERFORMED VERIFICATION FLIGHT EN ROUTE TO DEN. PROBLEM REOCCURRED ON DESCENT TO DEN. THE WIRE W0623-2959B-20 WAS FOUND SHORTED. THE HARNESS WAS REPLACED AT SFO. RAN ENGINE & OPERATIONAL CHECKED IDG. SHOP CONFIRMED WIRE FAILED SHORTED TO GROUND OR SHIELD. 2L72 4F4 FRTT0001SE E46NE 20030820000112003082000011EU 2003 8 20 03FDEA00947 120030621A5414 SKIN AIRBUS300 A300F4605R 3930327EU TRANSLATING COWLDELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE12987 R677014 742 NR 1 ENGINE RT TRANSLATING COWL IS DELAMINATED, FWD UPPER CORNER AT THE 2 O'CLOCK POSITION OF THE INNER BARREL 2 X 4 INCHES. REPAIRED BY T/R REPLACEMENT PER EA 6-7830-66985 WORK DOCUMENTED ON M-1805, S00029. 2L72 4F RTA35EU 20030820000182003082000018NM 2003 8 20 03FDEA00851 120030603A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-113-01,2) ON SHEAR TIE BS 950B, LBL 8-10, WL 140. REMOVED CORROSION ON SHEAR TIE BS 950B LBL 8-10 WL 140 AREA .65 X 5.00 X .013 INCH DEEP FROM ORIGINAL .071 FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED SHEAR TIE PER SRM 53-10-4. 2L73 4F RTA3WE 20030820000482003082000048WP 2003 8 20 03FDEA01133 120030724A2780ARH0500505 DRIVE LINK DOUG DC10 DC1030 3023501WP SLATS & FLAPS DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25317FE 46835 I/B SLAT DRIVE MECHANISM FWD BEARING AFT RETAINER GREASE SEAL IS BLOWN OUT OF POSITION. REMOVED AND REPLACED SLAT DRIVE MECHANISM PER AMM 27-83-01-2. 2L73 4F A22WE 20030820000512003082000051NM 2003 8 20 03FDEA00923 120030618A5753ARC0503503 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING O/B FLAP O/B HINGE I/B LOWER BORE FOUND CORROSION. LT WING O/B FLAP O/B HINGE I/B LOWER BORE REPAIRED AS PER FEDEX EA 1-5750- 69373 OUTBOARD TRAILING EDGE FLAP - SUPPORT BRACKETS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030820000552003082000055WP 2003 8 20 03FDEA01148 120030725A5347 SPLICE DOUG DC10 DC1010 3022110WP SEAT TRACK DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 NR S- 23 COMPLY WITH EA 8-5310-70987. FUSELAGE - MAINFRAME, MINOR DEVIATION TO SEAT TRACK SPLICE. CLOSING ACTION ON 07-23-03 COMPLIED WITH EA 8-5310-70987. 2L73 4F A22WE 20030820000572003082000057NM 2003 8 20 03FDEA00848 120030426A5753ARC70531 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LEFT OUTBOARD FLAP VANE, INBOARD NR 1 VANE TRACK FITTING FWD MOUNT HOLE CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69349 - WINGS - OUTBAORD FLAP VANE INBOARD SUPPORT CORROSION - REPAIR. 2L73 4F RTA22WE 20030820000632003082000063NM 2003 8 20 03FDEA01063 120030708A5753ARC41252 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 RIGHT OUTBOARD FLAP, FOUND 01 EACH CRACK ON NOSE RIB SUPPORT ISLAND, APPROX. 0.25 INCH IN LENGTH. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71833 WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR. 2L73 4F RTA22WE 20030820000702003082000070NM 2003 8 20 03FDEA01114 120030718A3620 WARNING LIGHT DOUG MD11 MD11 3023602NM COCKPIT FALSE ACTIVATIONA FDEABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25580FE 48471 DURING CLIMB SHOWED LEVEL ONE AIR SYS 2 OFF, ALERT FOLLOWED SHORT LAG BY LEVEL THREE MANF 2 FAIL ALERT. RAN CHECKLIST AND RETURNED TO NRT WITH ENGINE 2 AT IDLE THRUST. WITH ENGINE AT IDLE, ALERT WAS REMOVED. FACT 18JUL03 10:04 NRT R, REPLACED MANIFOLD FAILURE SENSING ELEMENT (35625-4-255) AT ZONE 14A PER AMM36-23-7. SOMETIMES MFC ABORT DURING ACCESS, REMOVED AND REPLACED MFC AND R-T-S TEST PASSED PER AMM36-23-01. CHECKED ALL ELEMENT A&B, FOUND NO SHORT TO GROUND. PERFORMED ENG RUN PER MD11JRH WITH NR 135532. DECAY C'K PASSED 27 SEC. FOUND NO DEFECT. 2L73 4F RTA22WE 20030820000902003082000090NM 2003 8 20 03FDEA00866 120030612A5260 WARNING LIGHT BOEING727 727200 138407ENM DOORS ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25484FE 21466 AMBER AFT STAIR LIGHT ILLUMINATED AFTER TAKEOFF, EXTINGUISHED AFTER LANDING. RAN RED TAB CHECKLIST AND TALKED TO GOCC LANDING OK. MEL 12JUN03 09:42 MEM U ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22JUN03 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT - INOP. 2L73 4F RTA3WE 20030820000922003082000092NM 2003 8 20 751PA0019 120030716A3397 WIRE BOEING757 757200 1384950NM EMERGENCY LIGHT BROKEN A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05751PA 23928 SEVERAL EMERGENCY PATH LIGHTS INOP AFT OF L2 DOOR. REPAIRED BROKEN WIRE AT ROW 15C. OPS CHECK OK PER MM 33-50. 2L72 4F RTA2NM 20030820000972003082000097NM 2003 8 20 0301196717 120030630A5330 SKIN BOEING747 747251F 1384898NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING L-CHECK FOUND CORROSION ON SKIN AT AFT CARGO DOOR CUTOUT LOWER CORNER BS 1920 S42R. REPAIRED PER EA 67-165074. 2L74 4F A20WE 20030815000812003081500081SW 2003 8 15 HEEA088578 120030728A6230 BEARING BELL 412 412 1182202SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH A1591 33150 MAIN ROTOR LINK HAS BEARINGS WORN. SHOP REPAIR. 1G72 4U H4SW 20030819000422003081900042NM 2003 8 19 USAA030108 120030621A5210 PAN BOEING737 737301 1384611NM DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 FOUND DOOR PAN CRACKED .5 INCH LONG, MED DOOR PAN CRACKED AFT SIDE. DOUBLER INSTALLED PER 52-10-02/51-70-11. (M) 2L72 4F RTA16WE 20030819000692003081900069EA 2003 8 19 SWIA200312127 120030616A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV A. P/N: 601R-53-6117-3. 2L72 4F4 FRTA21EA E15NE 20030819000802003081900080EA 2003 8 19 SWIA200312212 120030722A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM07455SW1116 1116 7760 STAB TRIM INDICATOR SHOWING ERRATIC INDICATIONS. REMOVED AND REPLACED HSTA IAW MM 27-40-00. 2L72 4F RTA21EA 20030819001272003081900127NM 2003 8 19 UPS03240913 120030626A5330 SKIN BOEING727 72722C 138400FNM BELOW WINDSHIELDCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: ASV, SKIN PANEL BELOW L1 AND R1 CENTER WINDOW POST HAS .375 INCH CRACK FROM EDGE TO RIVET. CONFIRMED BY DYE PENETRANT INSP. REPLACED SKIN PANEL AS PER SRM ADDENDUM EO B727-5330-5128A. 2L73 4F A3WE 20030819001432003081900143EA 2003 8 19 SWIA200312149 120030625A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 193 ELECTRICAL BAY RT FLOOR CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED FLOOR IAW CRJ REO 601R-53-11-245, REV NC. 2L72 4F4 FRTA21EA E15NE 20030820001732003082000173NM 2003 8 20 CALA0300383 120030711A5330 SKIN BOEING777 777224 1385225NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778009 29479 INSPECTION FOUND FUSELAGE SKIN DENTED 3 INCHES FORWARD OF STA 676, FORWARD OF L-2 DOOR BETWEEN STRINGERS 27L AND 28L. REPAIRED IAW SRM 53-00-01, REPAIR 7. 2L72 4F RTT00001SE 20030820001742003082000174NM 2003 8 20 CALA0300384 120030711A5230 SKIN BOEING737 737524 1384721NM AFT CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711641 28902 INSPECTION FOUND THE AFT CARGO DOOR EXTERNAL SKIN DENTED 21 INCHES FROM FORWARD DOOR EDGE AND 40 INCHES FROM TOP EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2L72 4F RTA16WE 20030820002042003082000204EU 2003 8 20 ASOA03328 120030710A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURING A C-CHECK IN BNA, THE LEFT OUTBOARD SEAT TRACK BETWEEN FS 29-36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD SEAT TRACK BETWEEN FS 29/36 IAW SRM 51-25-04 AND 51-25-02. (M) 2H72 4T RTA53EU 20030820002072003082000207EU 2003 8 20 ASOA03326 120030710A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FS 39/41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FS 39/41 IAW SRM 51-40-02 AND 51-25-04. (M) 2H72 4T RTA53EU 20030819000272003081900027NM 2003 8 19 AALA20030694 120030616A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21369AA 25196 FOUND FLOORBEAM AT STATION 764 HAD CORROSION REMOVED ON UPPER SURFACE, AT RBL 33 REPAI AS FOLLOWS, FABRICATE REPAIR STRAP OUT OF 301.5 HARD STAINLESS STEEL .050 INCH THICK. ALODINE BARE OF ALUMINUM SURFACES FINISH BLEND AND REPAIR PARTS WITH 2 COATS OF BMS10-11 PRIMER, FILL BLENDS WITH BMS5-92, INSTALL REPAIR STRAP WITH BMS 5-95. AT RBL 43, RBL 8 AND RBL 44 REPAIR AS FOLLOWS, ALODINE AND PRIME ALL BARE ALUMINUM SURFACES FINISH BLENDED AREA WITH 2 COATS OF BMS 10-11 PRIMER FILL BLENDS WITH BMS-5-95. (M) 2L72 4F RTA1NM 20030819000522003081900052EU 2003 8 19 RAIA00306170 120030622A3297 WIRE HARNESS AEROSPATR72 ATR72202 8680940EU MLG CHAFED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03723TE 283 LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPAIRED WIRE HARNESS TO RT WOW SWITCH. 2H72 4T RTA53EU 20030819000822003081900082NM 2003 8 19 2003UALA00548 120030708A3350 BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 EXIT FLOOR LIGHTING INOP FROM ROWS 23-30. REPLACED BATTERY PACK. 2L72 4F4 FRTA2NM E17NE 20030819001032003081900103NM 2003 8 19 UPS03240919 120030611A2710 BUSS TIE BOEING727 727185C 138406NNM RT I/B AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C&SI, RT I/B AILERON BUS QUADRANT CORRODED IN CABLE GROOVE. RIGHT I/B AILERON BUS QUADRANT REPLACED AS REQUIRED UP TO STEP D6 INCLUSIVE IAW MM 27-10-56. 2L73 4F A3WE 20030819001522003081900152NM 2003 8 19 2003UALA00509 120030617A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29789UA 26935 SKIN DENTED AT STATION 287, STRINGER 18 - 19 RT. 2L72 4F4 FRTT0001SE E46NE 20030819001642003081900164NM 2003 8 19 2003UALA00603 120030731A2130 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29808UA 804 FLIGHT DIVERTED DUE TO PRESSURIZATION FAILURE. REPLACED CPC1 AND SKIN AIR OUTLET VALVE. 2L72 4F4 FRTA28NM E40NE 20030819001712003081900171NM 2003 8 19 SWAA031764 120030807A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT UPPER EMERGENCY FLASHLIGHT PER MM. 2L72 4F RTA16WE 20030819001892003081900189CE 2003 8 19 DXTA200300043 120030608A3260 SQUAT SWITCH CESSNA750 750 2076810CE MLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07902QS 7500002 AFTER TAKEOFF LANDING GEAR FAILED TO RETRACK, GEAR HANDLE WOULD NOT MOVE. ACCOMPLISHED AIR TURNBACK TO SAN AND LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING SQUAT SWITCH DUE TO INTERNAL FAILURE. OPERATIONAL CHECKED GOOD, WORK DONE IAW 750 MM CHAPTER 32-60-00. 2L72 4J RTT00007WI 20030819001932003081900193 2003 8 19 234TR0002 420030715A34306223255005 RECEIVER BOEING737 737228 13844AGNM VOR SYSTEM UNRELIABLE A PIDAO OTHER O OTHER APAPPROACH 1 SO05234TR 23004 BOTH VOR RECEIVERS ARE ERRATIC AND UNRELIABLE. REMOVED AND REPLACED BOTH RECEIVERS. OPS CHECKS GOOD PER MM 34-31-41. 2L72 4F RTA16WE 20030819002052003081900205NM 2003 8 19 SWAA031776 120030808A335065C34691 LIGHT BOEING737 7373H4 1384600NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW NR 14 ABC. SECURED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030820000252003082000025NM 2003 8 20 03FDEA01004 120030625A5753ARC70541 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT WING OUTBOARD FLAP VANE 2ND VANE MOUNT FITTING FROM INBOARD FOUND MOUNT HOLE AND BUSHING WITH CORROSION. REPAIR CARRIED OUT AT RT WING OUTBOARD FLAP VANE 2ND VANE MOUNT FITTING FROM INBOARD MOUNT HOLE AS PER EA 1-5750-71731 : WINGS - RIGHT AND LEFT OUTBOARD FLAP VANE - NR 2 VANE TO TRACK SUPPORT CORRODED. 2L73 4F RTA22WE 20030820000432003082000043NM 2003 8 20 03FDEA01138 120030723A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT O/B FLAP (FLAP SIDE) - I/B HINGE O/B PIVOT HOLE CORRODED. SNRM N0463 - LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE O/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030820000752003082000075NM 2003 8 20 03FDEA01119 120030719A361089812621 REGULATOR BOEING727 727200 138407ENM MALFUNCTIONED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25207FE1182511825 22929 SMOKE OR FUMES IN COCKPIT CLIMBING THRU FL 180 NO INDICATION ON S/O PANEL EXCEPT VERY HIGH DUCT PRESSURE L AND R ABOVE 65 PSI. BLEED SWAPPED TO 2 AND 3 LOWERED PRESSURE TO NORMAL RANGE (BETWEEN 30 40 PSI). REMOVED AND REPLACED HIGH PRESSURE SHUT OFF VALVE USING MM-36-12-042, LEAK CHECK NORMAL. ENTERED COCKPIT TO DEBRIEF CREW, NOTICE NO SMOKE OR ODOR AT THAT TIME. RAN ALL THREE ENGINES, AND WAS UNABLE TO DUPICATE WRITEUP. PER T/S TREE FLOW CHART SUGGEST FOR PRECAUTIONARY MEASURES TO CHANGE HIGH PRESSURE REGULATOR AND HIGH PRESSURE MODULATING SHUT OFF VALVE. REMOVED AND REPLACED LT HIGH PRESSURE REGULATOR REF MM CHP 36-12-051. PERFORMED HIGH PRESSURE BLEED CONTROL SYSTEM TEST, OPS NORMAL REF B727JRH. 2L73 4F RTA3WE 20030820001002003082000100NM 2003 8 20 513NA0001 120030724A5610141T480013 WINDOW BOEING757 7572T7 1384914NM COCKPIT CRACKED A PIDAO OTHER O OTHER CRCRUISE 1 SO05513NA 23895 LEFT FWD WINDOW CRACKED. REPLACED NR 1 FWD WINDOW PER MM 56-11-01 AND REPLACED WINDOW HEAT CONTROLLER PER MM 30-41-01. OPS CHECKS GOOD. 2L72 4F RTA2NM 20030820001552003082000155 2003 8 20 0301291223 420030713A2330 SWITCH DOUG DC10 DC1030 3023501WP SEATS 24FG & 25HMALFUNCTIONED A NWAAK NONE O OTHER CRCRUISE 1 GL01223NW 46580 ZONE 'C' FLIGHT ATTENDANT CALL LIGHTS INTERMITTENTLY RING FROM VARIOUS ROWS AND SEATS. FORTY MINUTES PRIOR TO LANDING, FLIGHT ATTENDANT NOTED A BURNING RUBBER ODOR FROM MID GALLEY AREA. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. REPLACED SEB AT SEATS 24 FG AND 25 HJ. 2L73 4F A22WE 20030820001582003082000158NM 2003 8 20 2003UALA00569 120030716A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29663UA 27160 MAIN CABIN BETWEEN STA 774 AND 785 AND LBL 55, SEAT TRACK HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION WITH SPLICE DOUBLERS. 2L72 4F4 FRTA1NM E24NE 20030820001612003082000161NM 2003 8 20 2003UALA00573 120030717A2131 CONTROLLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29325UA 23957 AIRCRAFT DIVERTED EN ROUTE WHEN FLIGHT CREW COULD NOT CONTROL CABIN PRESSURIZATION. AUTOMATIC FLOW CONTROL VALVE FAILED. REPLACED AUTO FLOW CONTROL VALVE. 2L72 4F4 FRTA16WE E2GL 20030820002122003082000212EA 2003 8 20 ASOA03314 120030716A7120 FRAME CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING AN A-CHECK IN BTR, THE RIGHT ENGINE FRAME 640 BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ENGINE FRAME 640 BETWEEN STRINGERS 9 AND 12 IAW ASA EO 600-53-0075. (M) 2L72 4F RTA21EA 20030328000072003032800007EA 2003 3 28 CA030213003 220030210A7230 CASE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA COMPRESSOR PUNCTURED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) PIN SIZE HOLE LOCATED ON NR 2 PT6T-3 POWER SECTION GAS GENERATOR CASE AT APPROXIMATELY 7 O'CLOCK POSITION 3 3/4 INCHES AFT OF FIRST CIRCUMFIRENTIAL SEAM WELD (BY P3 AIR BOSS SUPPLYING AIR TO TORQUEMETER CLUTCH SEAL) WHILE PERFORMING VISUAL INSPECTION OF GAS GENENERTOR CASE. SILIGHT AIR LOSS FROM HOLE BUT NOT AFFECTING POWER ASSURANCE FIGURES (APPROXIMATELY +1.7 TO 1.9 PERCENT N1). POWER SECTION CHANGED. 1G71 4U4 U H4SW E22EA 20030328000112003032800011 2003 3 28 CA030214005 420030207A2340301 SWITCH BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA PUSH/TALK FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) PUSH TO TALK SWITCH REPLACED AFTER FAILURE. NEW PUSH TO TALK SWITCH FAILED WITH 4.7 HOURS USED. SWITCH COMPLETELY BROKEN TO PIECES. ONLY CREW ACTION WAS TO USE HAND MICROPHONE AND HAVE CAPTAIN SIDE DO THE MAJORITY OF COMMUNICATION. 2L72 4T4 TRTA24CE E4EA 20030328000162003032800016WP 2003 3 28 CA030214010 120030205A8097 WIRE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524* NE NR 1 PYLON CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING NR 1 ENGINE START, THE ENGINE START VALVE SWITCH LIGHT DID NOT ILLUMINATE. INSPECTION FOUND WIRES DAMAGED DUE TO CHAFING. THE FOLLOWING WIRES WERE FOUND MELTED, BURNED AND SOLDERED. THE LOCATION OF WIRES WERE ON THE ENGINE NR 1 PYLON, UNDER PANEL 452 AT, TOWARD THE FWD OF PANEL UNDER THE LT HINGE OUTBOARD COVER UNDER AND FWD OF THE PHENOLIC ROLLER GUIDE, CAUSED THE CHAFING. WIRE WAS FOR THE START VALVE INDICATION AND WIRE WAS FOR THE DISCHARGE BOTTLE INDICATION. THIS PREVENTED THE INDICATION IN THE FLIGHT COMPARTMENT. THE WIRES WERE REPAIRED IAW WD STANDARD PRACTICE MANUAL 20-15-04. 2L73 4F4 F A23WE E12EU 20030328000172003032800017SW 2003 3 28 CA030217001 120030214A5510206020121010 FITTING BELL BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL HORIZONTAL STAB CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) CRACKS FROM RIVIT HOLE IN 0.125 INCH STAMPED ATTACHMENT FLANGE COMPLETELY ACROSS FLANGE SEPARATING IT INTO TWO PIECES. (NOTE) THERE IS NO DANGER OF STABILIZER SEPARATION FROM THE AIRCRAFT AS THE FLANGE ISSTILL RIVITED TO THE INBOARD RIB IN 5 OTHER PLACES, THE STABILIZER IS CLAMPED TO THE SPAR IN 4 PLAC ES AND THERE IS A STOP ASSEMBLY TO PREVENT SEPARATION AS WELL. THIS PROBLEM HAS BEEN WITH US A LONG TIME BUT WHAT BRINGS THIS ONE TO LIGHT IS WE HAVE FOUND SIX (6) CRACKS ON 5 AIRCRAFT IN TWO MONTHS. RECOMMEND CREWS BE MORE VIGILENT ON INSPECTIONS SO TO DETECT CRACKS BEFORE THEY HAVE A CHANCE TO GROW. 1G71 3U3 U H2SW E4CE 20030328000242003032800024NM 2003 3 28 0300626632 120030324A2197DM553 CONNECTOR BOEING747 747251B 1384892NM GASPER FAN BROKEN A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL01632US 23112 DURING APPROACH A STRONG ELECTRICAL FUME EMITTED BETWEEN THE NR 2 AND NR 3 CABIN COMPARTMENT. PULLED THE NR 2 AND NR 3 GALLEY CIRCUIT BREAKERS AND THE FLIGHT LANDED WITHOUT INCIDENT. REPAIRED BROKEN GASPER FAN WIRE PINS NR 4 AND NR 5 ON ELECTRICAL PLUG DM553. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030328000292003032800029EU 2003 3 28 2003F00157 120030326A290012TW13 SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COLLECTIVE INTERMITTENT E S4WAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 WP074027Q3202 2904 9456 DURING CRUISE FLIGHT THE PILOT FELT THE CONTROLS GET "HARD" LIKE A HYDRAULIC SYSTEM FAILURE, BUT AIRCRAFT STILL FLYABLE. PILOT OPTED TO DO PRECAUTIONARY LANDING IN AN OFF-AIRPORT AREA WITH NO INCIDENT REGARDING PERSONNEL OR AIRCRAFT. AFTER INSPECTING SYSTEM FOUND HYDRAULIC CUTOFF SWITCH ON PILOT'S COLLECTIVE TO BE INTERMITTENT AND PUTTING SYSTEM INTO BYPASS AND LOCKING THE CONTROL SERVOS. AFTER REPLACING THE SWITCH THE AIRCRAFT OPERATED NORMALLY. 1G71 3U3 U H9EU E19EU 20030328000312003032800031 2003 3 28 811AV032403 420030324A34257011702933 CONTROL PANEL AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE COCKPIT SMOKE C O OTHER O OTHER NRNOT REPORTED 1 EA25811AV 64 74 DURING CLIMB, CREW SMELLED A BURNING ODOR AND SMOKE IN THE VICINITY OF FLIGHT GUIDANCE CONTROL PANEL. CREW TURNED OFF BACK LIGHTING TO PANEL, SMOKE AND ODOR DISIPATED. FLIGHT CONTINUED TO DESTINATION UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL PART NUMBER 7011702933. OPERATIONAL CHECKED GOOD. (P) 2L73 4F4 FRTA46EU E1NM 20030328000432003032800043SO 2003 3 28 C2XA03TY028 120030210A534714530641011 SEAT TRACK EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION, MULTIBLE SEAT TRACKS HAD CORROSION. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IN THE CABIN IAW EMB 145MM-53-01-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000592003032800059NM 2003 3 28 CALA0300095 120030303A5311 FRAME BOEING737 737924 13848A1NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0937409 30126 THE GROUND POWER CABLE CONNECTOR SHORTED TO THE FUSELAGE STRUCTURE AT THE RECEPTACLE CUTOUT. THE FRAME WEB AT STA 235.8, WL 180 WAS FOUND TO HAVE HEAT DAMAGE. THE AREA WAS REPAIRED IAW ECRA 5311-01146. 2L74 4F RTA16WE 20030328000632003032800063WP 2003 3 28 CALA0300107 120030308A5350 CABLE DOUG DC9 DC982 3022082WP TAILCONE OUT OF RIG A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 THE TAILCONE FAILED TO DROP WITHIN SPECIFICATIONS AT ALL THREE POSITIONS DURING FUNCTIONAL TEST. THE PULL EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW 53-53-00. 2L72 4F A6WE 20030328000642003032800064NM 2003 3 28 CALA0300110 120030310A335020121 CHARGER BOEING737 737524 1384721NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914605 27318 INSPECTION FOUND FIRST CLASS CABIN SEATS WITH EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE DURING "A" CHECK. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-02. 2L72 4F RTA16WE 20030328000652003032800065NM 2003 3 28 CALA0300112 120030312A3397 WIRE BOEING757 757224 1384958NM ROW 16 LEFT BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0933103 27293 INSPECTION FOUND EMERGENCY PATH LIGHTS FROM ROW 8-26 INOPERATIVE. MAINTENANCE FOUND WIRING BROKEN AT ROW 16 LEFT AND FUSES BLOWN AT BATTERY PACK ROW 9 RT. THE DAMAGED WIRING WAS REPAIRED IAW WDM 33-51-15 AND 33-51-14. REPLACED BLOWN FUSES ON M736 AND M10919. ALLWIRING REPAIRED IAW STANDARD PRACTICES CHAPTER 20. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00. 2L72 4F RTA2NM 20030328000682003032800068WP 2003 3 28 CALA0300134 120030321A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914840 49580 INSPECTION FOUND A 1/2 INCH CRACK IN CANTED FRAME CAP AT STA 1446, L3R. REMOVED AND REPLACED CAP IAW SRM 51-30-2. 2L72 4F A6WE 20030625001292003062500129EU 2003 6 25 03FDEA00356 120030328A5410 PANEL AIRBUS310 A310 EU NR 2 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 2 ENG I/B TRANSLATING COWL UPPER T- TRACK SLIDER CRACKED OFF. INSTALLED NEW UPPER SLIDER WITH NEW TRANSLATING SLEEVE W/C NOO193 2L72 4F RTA35EU 20030625001252003062500125EU 2003 6 25 03FDEA00357 120030321A5510 SPAR CAP AIRBUS310 A310 EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 LT HORIZONTAL UPPER AFT SPAR CAP CORRODED APPROX. 4FT. FROM FUSELAGE. UNDER MAE W/O NO. 13350. REPAIRED AFT SPAR CAP IAW SRM 55-13-11 AND SRM 51-41-01. 2L72 4F RTA35EU 20030331000172003033100017EA 2003 3 31 A6WA200340023 120030106A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 OBLIQUE ANGLE AT FS 625 LT SIDE IS CRACKED ONE INCH IN RADIUS. REMOVED AND REPLACED CRACKED OBLIQUE ANGLE AT FS 625 LT SIDE WITH NEW. 2L72 4F RTA21EA 20030331000302003033100030WP 2003 3 31 AALA20030037 120030108A3260 DOWNLOCK SENSOR DOUG DC9 DC982 3022082WP MLG DEFECTIVE A AALAO OTHER N FALSE WARNING APAPPROACH 1 SW21465A 49595 ORD - FLT 854 - EN ROUTE FLL-ORD, ON APPROACH ORD, AFTER PUTTING LANDING GEAR HANDLE DOWN. RGHT GEAR WARNING LIGHT ILLUMINATED. USED MANUAL GEAR EXTENSION TO EXTEND LANDING GEAR. GEAR SHOWED DOWN AND LOCKED. LANDED ORD WITHOUT INCIDENT. REPLACED D1-27 SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000512003033100051WP 2003 3 31 AALA20030229 120030222A2612 WARNING SYSTEM DOUG DC9 DC983 3022083WP E&E BAY DEFECTIVE A AALAO OTHER N FALSE WARNING CLCLIMB 1 SW21571AA 49353 EN ROUTE ACA-ORD, DURING CLIMB, RECEIVED INTERMITTENT APU AURAL WARNING, NO LIGHTS. WARNING STOPPED BUT AFTER LEVEL OFF AT 29,000 FT WARNING STARTED AGAIN. RECEIVED RT ENGINE FIRE WARNING (AGAIN NO LIGHTS). LANDED MEX WITHOUT INCIDENT. INSPECTED AND CHECKED ENGINE AND APU FIRE DETECTION SYSTEM, NO FAULTS NOTED. REPLACED CENTRAL AURAL WARNING UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000532003033100053WP 2003 3 31 AALA20030244 120030225A3397 CONNECTOR DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21567AM 53293 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4D INOPERATIVE. INSERTED EMERGENCY EXIT LIGHT PIN IN CONNECTOR ON PLUG TO SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000552003033100055WP 2003 3 31 AALA20030249 120030227A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21474 49649 DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. REATTACHED EMERGENCY EXIT LIGHT BATTERY FOR TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000562003033100056NE 2003 3 31 ABXA030120 220030318A7200 ENGINE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 4 DEFECTIVE A ABXAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL23818AX2148 46075 671350 ON CLIMBOUT, THE NR 4 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 4 OIL PRESSURE NOTED TO BE 32 PSI. WHEN POWER REDUCED, OIL PRESSURE WAS 20 PSI. SHUT DOWN THE NR 4 ENGINE AT 1036Z. WINDMILLING OIL PRESSURE 8-10 PSI IN CLIMB AND CRUISE. AIRCRAFT FERRIED TO ILN WHERE MAINTENANCE REPLACED THE NR 4 ENGINE IAW JOB CARD 8090507 AND DC-8 MM. TRIMMED ENGINE IAW DC8-8A AND 8B. 2L74 4F4 F 4A25 1E8 20030331000582003033100058CE 2003 3 31 AMWA18 120030305A5346 PLATE BEECH 1900 1900D 1154162CE LT ENG TRUSS DAMAGED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07237YV UE237 WHILE PERFORMING AN "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THAT THE LEFT PRESSURE PLATES HAVE RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE PER THE STANDARD REPAIR MANUAL 57-95-02. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030331000652003033100065NE 2003 3 31 ASOA03089 220030306A7261 O-RING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE FAILED A ASOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11532AS 458 DURING CLIMB OUT, THE LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE QRH, SHUT THE LT ENGINE DOWN AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE OIL FILTER O-RING ON THE LT ENGINE AND ADDED THREE QUARTS OF OIL. ALSO, THE REDUCTION GEAR BOX AND MAIN OIL TANK CHIP DETECTORS WERE PULLED FOR POSSIBLE FOREIGN OBJECT DAMAGE. NO DAMAGE WAS FOUND. THE ENGINE RUN AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20030819001782003081900178CE 2003 8 19 DXTA200300065 120030708A2800 VENT LINE CESSNA750 750 2076810CE FUEL SYSTEM OUT OF POSITION E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07997QS 7500208 WING TANK "FULL R AMBER CAS" MESSAGE ILLUMINATED IN CRUISE FLIGHT 10 MINS AFTER LEVELING AT FL 290. FUEL GAUGES SHOWED 2460LB BOTH SIDES. VISUAL INSPECTION IN AIR SHOWED FUEL VENTING OUT OF RIGHT WING. INSPECTED INBOARD AND OUTBOARD TRANSFER FLOAT VALVES, NO DEFECT NOTED. INSPECTED INBOARD VENT TUBE AND FOUND THE GAP BETWEEN UPPER EDGE AND UPPER WING SKIN OUT OF TOLERANCE, REPOSITIONED RIGHT INBOARD VENT TUBE, OP'S CHECK GOOD IAW CESSNA 750 MM CH 28-10-04. 2L72 4J RTT00007WI 20030820000072003082000007NM 2003 8 20 03FDEA01302 120030814A21215007024620 FAN BOEING727 727200 138407ENM ZONE 100 SHORTED A FDEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25207FE 22929 GASPER FAN C/B POPPED IN FLT IMMEDIATELY FOLLOWING MILD SMOKEY ODOR IN COCKPIT. DID NOT RESET C/B ODOR WENT AWAY. REMOVED AND REPLACED GASPER FAN PER 727-200 M 2FM 21-23-011-4 2C, OPS CHECK OK. 2L73 4F RTA3WE 20030820000152003082000015NM 2003 8 20 03FDEA00951 120030621A5753 STRUCTURE DOUG MD11 MD11 3023602NM LT WING TE FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LT WING, I/B FLAP CTR (FLAP VANE TRACK) CUTOUT FOUND CHAFED. LT WING, I/B FLAP CTR (FLAP VANE TRACK) CUTOUT, DAMAGED RIB REMOVED AS PER SRM 51-31-01 VOL II, ON SKIN EDGES CHAFE MARKS SMOOTHED OUT AND FOUND WITHIN LIMIT AS PER SRM 57-00-01 VOL I FIG 1A, NEW RIB FABRICATED AS PER DRAWING ARC 2951, RIB INSTALLED AS SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20030820000382003082000038NM 2003 8 20 03FDEA01065 120030625A5730APB74411 SKIN PANEL DOUG MD11 MD11 3023602NM CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 MAIN DECK - BETWEEN BS 1215-1235, LEFT XCW 0-50, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING/UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK. 2L73 4F RTA22WE 20030820000472003082000047NM 2003 8 20 03FDEA01134 120030723A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT I/B FLAP (FLAP SIDE) - O/B HINGE O/B PIVOT HOLE AND O/B PIVOT LUG INNER AND OUTER SURFACES CORRODED. LT I/B FLAP (FLAP SIDE)- O/B HINGE O/B PIVOT HOLE AND O/B PIVOT LUG INNER AND OUTER SURFACES REPAIRED AS PER FEDEX EA 1-5750-69256 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT INBD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030820000672003082000067WP 2003 8 20 03FDEA01110 120030718A5753ARC1984 FITTING DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 COMPLY WITH EA 8-5750-70979. WINGS - RT OUTBOARD FLAP - INBOARD HINGE LUG CORROSION REPAIR (P/N ARC19840 ENT BY: 60601C RPT BY: 60601C PLND: MECH:02 SPAN:0 D 02:00 PARTS: ENT BY:402783 17JUL03 14:38:47 S=S FACT 18JUL03 11:47 BFM U COMPLIED WITH EA 8-5750-70979 WINGS - RT OUTBOARD FLAP-INB'D HINGE LUG CORROSION REPAIR (P/N ARC 1984) ENT BY: 39017C RPT BY: 39017C CLOSED ON 07/18/2003 ON FEDEX NR S00012 ACCOMPLISHED AT MAE UNDER W/O NR 13414. 2L73 4F A22WE 20030820000822003082000082NM 2003 8 20 03FDEA01265 120030718A5330 SKIN BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25103FE 19199 AFT CARGO COMPT DOOR LOWER BEAM 22 FOR INTERIOR SKIN IS CRACKED BEYOND STOP DRILL AT FWD END. 2L73 4F RTA3WE 20030820000882003082000088NM 2003 8 20 03FDEA00832 120030526A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RT WING - OUTBOARD TRAILING EDGE FLAP, AFT INBOARD FLAP-HINGE ASSEMBLY FOUND PIVOT BEARING, INBOARD MOUNT HOLE WITH BUSHING LOOSE (FLAP SIDE). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69346 - WINGS - RT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030820001092003082000109NM 2003 8 20 UPS03440972 120030618A541165B904124950 FRAME BOEING747 747123 1384873NM NR 2 NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: C, NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD, CRACK REVEALED AT O/B SIDE FWD FRAME WEB LOWER O/B EDGE AS MARKED. NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD FRAME WEB REPAIRED AS PER RS R54-53-35039 AND UPS ENGINEERING FILE NR 747-54-20037. 2L74 4F A20WE 20030820001102003082000110NM 2003 8 20 UPS03440973 120030622A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: C-FX, STA 500, S38L SUPPORT FRAME FOUND CRACK AS MARKED. FX STA 500 STR 38L SUPPORT FRAME REPAIRED AS PER RS R53-12-35040 AND EO B747-5310-18971-A. 2L74 4F A20WE 20030820001182003082000118EA 2003 8 20 COMA0360368 120030810A531160036030 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01781CA10235 7312 FRAME ANGLE AT FS 718 CRACKED. COMPLIED WITH EA 10-5320-00236 AND S/B 601R-53-055 PART B. 2L72 4F RTA21EA 20030820001192003082000119NM 2003 8 20 CALA0300409 120030724A555369379951 BUSHING BOEING737 737524 1384721NM VERTICAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT O/B FORWARD AND AFT AND RT O/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE PER DRAWING 65-46872. 2L72 4F RTA16WE 20030820001232003082000123NM 2003 8 20 QXEA200300932 120030729A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 LACK OF LUBE A QXEAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 NM09411QX 4055 ON FLIGHT 2369 AFT STAIRS WILL NOT FULLY DEPLOY. CLEANED AND LUBED STAIR TRACKS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030820001272003082000127WP 2003 8 20 UPS03841092 120030723A53103755822515N FITTING DOUG DC8 DC873F 302199FWP FWD. LOWER CARGOCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C2, CRACKED BATH TUB FITTING STATION 320 BETWEEN LONG 28L AND 29L. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20030820001342003082000134 2003 8 20 243TR0005 420030719A3421258733511 GYRO BOEING737 737228 13844AGNM COCKPIT INACCURATE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 NR 1 VERTICAL GYRO SHOWS 3.5-4 DEGREES PITCH UP. REPLACED VERTICAL GYRO PER MM 34-21-21. 2L72 4F RTA16WE 20030820001352003082000135NM 2003 8 20 QXEA200300931 120030730A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 MALFUNCTIONED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09402QX 4032 AFT STAIRS WILL NOT EXTEND. REPOSITIONED GUIDE ARM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030820001372003082000137WP 2003 8 20 0301159607 120030515A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 BETWEEN RBL 16 AND RBL 19. REPAIRED PER EA 96-190981. 2L72 4F A6WE 20030820001502003082000150NM 2003 8 20 QXEA200300922 120030718A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- LEFT HAND INBOARD NR 4 SEAT TRACK OUTBOARD TRACK FLANGE IS CORRODED AT STATIONS X182.00-252.70. REPAIRED IAW DHC-8 SRM 51-40-11, 51-20-31 AND RD 8-53-4473. 2H72 4T RTA13NM 20030820001512003082000151NM 2003 8 20 QXEA200300920 120030719A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- RIGHT HAND OUTBOARD NR 10 SEAT TRACK HAS CORROSION IN CENTER. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20030820001542003082000154NE 2003 8 20 234TR0004 220030719A73217436025 FUEL CONTROL BOEING737 737228 13844AGNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE MALFUNCTIONED A PIDAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 SO05234TR 23004 709092 NR 1 ENGINE ROLLED BACK ON SHORT FINAL APPROACH. REPLACED IGNITION EXCITER BOX PER MM 74-11-11 AND REPLACED FUEL CONTROL UNIT PER MM 73-09-255. OPS CHECKS OK. 2L72 4F4 FRTA16WE E2EA 20030820001642003082000164NM 2003 8 20 373PA0018 120030805A3350873100112 LIGHT BOEING737 7373Y0 1384671NM CABIN WILL NOT TEST A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 FLOOR LEVEL EMERGENCY LIGHT, SECOND FROM LAST WILL NOT TEST PROPERLY. REPLACED FLOOR LEVEL EMERGENCY LIGHT ASSEMBLY IN AFT CABIN. OPS CHECKS NORMAL PER MM 33-50. 2L72 4F RTA16WE 20030820001662003082000166NM 2003 8 20 UPS03241065 120030714A5753 SKIN BOEING727 72725C 138400HNM TE FLAPS DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, LEFT O/B AFT FLAP - DISBOND AT UPPER SURFACE 5 TO 20 INCHES FROM O/B END. REPAIR CARRIED OUT IAW SRM 51-40-20. 2L73 4F A3WE 20030820001812003082000181 2003 8 20 SWAA031763 420030805A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030820001872003082000187EA 2003 8 20 COMA0360349 120030806A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SO01786CA 7333 FLIGHT 5793 LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030820001882003082000188NM 2003 8 20 UPS03441057 120030723A5330 SKIN BOEING747 747123 1384873NM LH STR 19 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, FX SKIN STR 19L STA 2280 - 2285 FOUND .25 INCH COUNTERSINK FASTENERS AT TOP ROW. FX SKIN AT STA 2280 - 2285 STR 19L AREA SKIN REPAIRED PER SRM 53-30-03 FIGURE 17. SKIN TRIMMED OFF PER SRM 53-30-03 FIG 17. 2L74 4F A20WE 20030820001922003082000192SO 2003 8 20 RAIA00307190 120030712A3350 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCONNECTED A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03801HK 145053 EMERGENCY LIGHT AT SERVICE DOOR INOP. RECONNECTED SERVICE DOOR EXIT LIGHT. 2L72 4F RTT00011AT 20030820001972003082000197NM 2003 8 20 03FDEA01262 120030730A5330 SKIN BOEING727 727100 1384036NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25103FE 19199 CRACK INDICATED AT BS 441 BETWEEN STR 1L AND 2L. 2L73 4F RTA3WE 20030820002002003082000200NM 2003 8 20 03FDEA00969 120030625A2613 WARNING LIGHT BOEING727 727100 1384036NM FIRE PROTECTION ILLUMINATED A FDEAK NONE J WARNING INDICATION CRCRUISE 1 SO25188FE 19081 WITH LEFT A/C PACK OPERATING THE LOWER AFT BODY OVERHEAT LIGHT ILLUM AFTER AT LEAST 30 MINS OF PACK OPS. AFTER TURNING OFF LT PACK, THE LIGHT EXTINGUISHED WITHIN 2 MINS. TURNED RT PACK ON, THE LIGHT CAME BACK ON AFTER 5 MINS. CHECKED AFT AIRSTAIR AREA FOR LEAKS, NONE FOUND. NO LEAKS IN WHEEL WELL AREAS. NO LEAKS IN KEEL BEAM AREA. RAN PACKS FOR 1.5 HRS WITH ENGINES RUNNING. NO LEAKS OR PROBLEMS FOUND. NO LEAKS OR OTHER PROBLEMS FOUND IN AFT BELLY AREAS. FIRE LOOPS IN KEEL BEAM AND AFT AIRSTAIRS CHECK OK. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20030820002022003082000202EU 2003 8 20 ASOA03330 120030710A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURING A C-CHECK IN BNA, THE FLOORBEAM AT FS 36 TO FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOORBEAM AT FS 36 AND FS 39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20030820002052003082000205EU 2003 8 20 ASOA03327 120030710A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURING A C-CHECK IN BNA, THE RIGHT OUTBOARD SEAT TRACK BETWEEN FS 29 AND FS 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK BETWEEN FS 29 AND FS 36 IAW SRM 51-25-04.. (M) 2H72 4T RTA53EU 20030820002152003082000215 2003 8 20 2003F00516 420030723A3421 INDICATOR LEAR 55 55LEAR 5170702CE ADI MALFUNCTIONED A FUBAA UNSCHED LANDING O OTHER CLCLIMB 1 NE0383WM 043 TAKING OFF FROM ISP CO-PILOTS ADI STARTED TO ROLL. SWAPPED NR 1 AND NR 2 ADI'S. AIRCRAFT FLEW 5 FLIGHTS WITH NO PROBLEM. (M) 2L72 4F A10CE 20030820002162003082000216 2003 8 20 GTIA030581 420030724A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 SLIDE PACK L1 DOOR OFF SLIDE PACK L2 DISCONNECTED. REMOVED AND RESECURED L1 AND L2 DOOR SLIDE PACKS. NO DEFECTS NOTED. (M) 2L72 4F A6WE 20030819001042003081900104NM 2003 8 19 UPS03240920 120030609A5751 HINGE BOEING727 727185C 138406NNM O/B AIL IDLER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE CRACKED & BROKEN. REPLACED LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE IAW MM 27-10-04 & ON REMOVAL OF HINGE, PIN FOUND TO BE DAMAGED, PIN REPLACED IAW MM 27-10-04. 2L73 4F A3WE 20030819001302003081900130NM 2003 8 19 SWAA031774 120030807A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030819001822003081900182EA 2003 8 19 COMA0360360 120030811A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01709CA 7238 FLIGHT 5229 LT THRUST REVERSER UNLOCKED MESSAGE DURING FLIGHT. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030819002172003081900217NM 2003 8 19 0301306306 120030714A2530 OVEN BOEING747 747451 1384940NM G1B GALLEY BURNED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01666US 23821 DURING FLIGHT, A STRONG BURNING FUME EMITTED FROM THE G1B GALLEY RIGHT OVEN. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030820000122003082000012EU 2003 8 20 03FDEA00948 120030621A5320A53986750214 INTERCOSTAL AIRBUS300 A300B4605R 3930308EU ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE 742 THE INTERCOSTAL IS CRACKED AND DEFORMED BETWEEN FRAME 85 AND 86 AT STR 33R IN THIS COMPARTMENT. REPAIRED BY REPLACING CRACKED INTERCOSTAL FLANGE IAW A300-600 SRM 51-40-20 WORK DOCUMENTED ON M-1805 N00242. 2L72 4F RTA35EU 20030820001032003082000103NM 2003 8 20 UPS03241050 120030714A5753 SKIN BOEING727 72725C 138400HNM I/B MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, LEFT I/B MIDFLAP LWR SURFACE 2 CRACKS AT FWD I/B & O/B CORNERS OF SKIN CUTOUT FOR I/B AFT FLAP ACTUATING ROD. CRACK STOP DRILLED TO .250 INCH IAW SRM 51-10-1. REPAIR CARRIED OUT IAW MRO EO 2003-041-002. UPS FILE NR 727-27-20007. 2L73 4F A3WE 20030820001112003082000111EA 2003 8 20 COMA0360370 120030810A531160036030 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01781CA10235 7312 FRAME ANGLE AT FS 718 CRACKED. COMPLIED WITH EA 10-5320-00236 AND S/B 601R-53-055 PART C. 2L72 4F RTA21EA 20030820001152003082000115WP 2003 8 20 UPS03840988 120030719A5753 WEB DOUG DC8 DC873F 302199FWP RH INBD FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 RIGHT INBOARD FLAP, INBOARD CLOSEOUT WEB CRACKED. REMOVED EXISTING DOUBLER & ACCESS PANEL. REMOVED EXISTING SUPPORT ANGLE AND HAT CHANNEL FOR ACCESS. DRILLED OFF I/B WEB ASSY FOR REPLACEMENT. CLEANED AND PRIMED MATING SURFACES OF RIB & DOUBLER AS PER DC8 SRM 51-1-8 DP 70236. 1ST INNER DOUBLER TO NEW WEB IAW SRM 51-1-20. 2L74 4F RT4A25 20030820001402003082000140NM 2003 8 20 CALA0300406 120030724A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 312-328, LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030820001622003082000162NM 2003 8 20 2003UALA00571 120030718A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29332UA 24193 LOWER SKIN CRACKED AT AFT END OF EQUIPMENT COOLING AIR EXHAUST DUCT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030820002222003082000222NM 2003 8 20 USAASB03096 120030630A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 MAINTENANCE REPORTED THE MID-CABIN BULL NOSE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FAULTY BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030820002252003082000225NM 2003 8 20 USAASB03097 120030702A3397 WIRE BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 PHL - PILOT REPORTED THE EMERGENCY LIGHT AT SEAT 5C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT 5C. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030820002352003082000235NM 2003 8 20 USAASB03094 120030628A3397 WIRE BOEING737 7374B7 1384702NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US 24556 MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030820002412003082000241EU 2003 8 20 ASOA03340 120030727A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11536AS 465 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030821000092003082100009NM 2003 8 21 USAASB03120 120030723A361032895624 CONTROL VALVE BOEING737 737301 1384611NM NR 1 ENGINE FAILED A USAAO OTHER J WARNING INDICATION DEDESCENT 1 EA19586US30562 23931 ON SLOW DESCENT TO PHL, FROM FL370 TO FL350, THE NR 1 ENGINE BLEED TRIPPED FOLLOWED BY A PACK TRIP. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED TO PHL UNPRESSURIZED. BLEED RESET AFTER COOLING PERIOD PER QUICK REF HANDBOOK PROCEDURES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PRECOOLER CONTROL VALVE ASSEMBLY PER MM. ALSO, REMOVED AND REPLACED THE NR 1 ENGINE PRECOOLER CONTROL VALVE SENSOR, P/N 129666-2, AS PRECAUTIONARY. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030821000182003082100018 2003 8 21 USAABA03020 420030624A25655A32652 ASPIRATOR AIRBUS330 A330323 3930335EU ESCAPE SLIDE CRUSHED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19 CLT - SHOP FOUND THE SLIDE ASPIRATOR CRUSHED DURING INSPECTION. MAINTENANCE REPLACED THE ASPIRATOR. DAMAGE TO THE ASPIRATOR IS ATTRIBUTED TO ORIGINAL PACKING AT THE FACTORY. (M) 2L72 4F RTA46NM 20030821000342003082100034NM 2003 8 21 03FDEA01172 120030726A5320A5A7114519 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 CTR CARGO LEFT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING FOUND CRACK. LEFT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20030821000382003082100038NM 2003 8 21 03FDEA01011 120030624A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR OUTBOARD LUG FOUND PITTING CORROSION. RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR OUTBOARD LUG REPAIRED AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000412003082100041NM 2003 8 21 03FDEA01016 120030627A5754ARC050214 HINGE DOUG MD11 MD11 3023602NM LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE FOUND CORROSION. RIGHT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5750-69354 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030821000512003082100051NM 2003 8 21 03FDEA01058 120030702A5712ARB2850506 RIB DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 RIGHT WING, LEADING EDGE RIB CRACK INBOARD OF NR 16 SLAT TRACK. RIGHT WING, LEADING EDGE RIB INBOARD OF NR 16 SLAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20030821000532003082100053NM 2003 8 21 03FDEA01051 120030702A5753 BUSHING DOUG MD11 MD11 3023602NM LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT WING OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG BUSHING FOUND LOOSE. LEFT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT LUG LOOSE BUSHING REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000692003082100069NM 2003 8 21 03FDEA00918 120030617A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT BORE FOUND CORROSION. RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT BORE REPAIRED AS PER FEDEX EA 1-5750-69372, TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000712003082100071NM 2003 8 21 03FDEA00938 120030620A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 CRACKED FRAME SHEAR TIE STA 580 ABOVE STR 18L. REPAIRED SHEAR TIE CLIP AT BS 580 ABOVE 18L PER SRM 51-40-3. 2L73 4F RTA3WE 20030821000822003082100082NM 2003 8 21 03FDEA00931 120030620A5510ALC8100 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT HORIZONTAL STAB UPPER CENTER PLANK 16L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. LEFT HORIZONTAL STAB UPPER CENTER PLANK 16L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030328000152003032800015EU 2003 3 28 CA030214009 120030210A1430NAS1351N412 BOLT AIRBUS310 A310300 3930305EU GE CF6 CF680C2A5 NE BRAKE ACCUM LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING THE A-01 CHECK, RT MAIN LANDING GEAR, EMERGENCY BRAKE MANIFOLD WAS SUSPECTED TO BE LEAKING. INSPECTION FOUND THE ALTERNATE BRAKE RETURN ACCUMULATOR LOOSE ON THE MANIFOLD, DUE TO THE FACT THAT THE BOLTS INSTALLED TO SECURE THE ACCUMULATOR WERE NOT WIRE LOCKED. T 2L72 4F4 FRTA35EU E13NE 20030328000262003032800026NM 2003 3 28 03084428 120030325A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27428FJ 3193 DURING MAINTENANCE INSPECTION, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030328000422003032800042SO 2003 3 28 C2XA03TY027 120030210A531014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE CARGO DOOR SILL WAS FOUND CORROCDED. MAINTENANCE REMOVED DOOR, REMOVED THE COVER SILL, LOCATED, DRILL NEW DOOR SILL, INSTALLED DOOR PROTECTIVE STRIPS AND INSTALLED DOOR. PRESSURE CHECK WAS GOOD IAW 135/145 SRM 53-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000752003032800075NE 2003 3 28 CH1A200382005 220030324A7230 COMPRESSOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A C1HAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 GL15682CA 22019 ON APPROACH TO LAS AT 500FT, NR 2 ENGINE COMPRESSOR STALLED. DID NOT USE NR 2 REVERSER. FLT ATTND REPORTED COMP STALL ON ROLL OUT 2L73 4F4 F A3WE E2EA 20030328000802003032800080 2003 3 28 CNMA200300001 420030117A25655WD230100201 SLIDE DOUG DC10 DC1030 3023501WP CABIN DISLODGED A CNMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0759083 20760 47926 WHILE AT GATE FLIGHT ATTENDANT OPENED R-1 DOOR WITHOUT DISARMING DOOR. SLIDE CAME OUT OF ITS CONTAINER AND LANDED ON TOP OF CATERING TRUCK AWAITING TO DELIVER. APPARENTLY SLIDE DID NOT FALL FAR ENOUGH TO ACTIVATE DEPLOYMENT MECHANISM. SLIDE WAS REMOVED AND REPLACED, SLIDE BEING SENT IN TO CHECK AND OVERHAUL. (P) 2L73 4F A22WE 20030331000672003033100067EA 2003 3 31 ASOA03091 120030308A2750 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WING CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO11874AS SBRJ614 7551 DURING HANGAR MAINTENANCE, THE LT FLAP VANE SPOILER, MIDDLE SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FLAP VANE SPOILER, MIDDLE SEAL PLATE IAW SRM. 2L72 4F4 FRTA21EA E15NE 20030331000742003033100074EU 2003 3 31 AWXA200300317 120030313A5315D53472075000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK CORROSION WAS FOUND AT 6 EACH NUT PLATES ON LOWER SURFACE OF FLOORBEAM BETWEEN FR 66+10 AND FR 68, LBL 57, Y1732. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED AREA OF FLOORBEAM BETWEEN FR 66+10 AND FR 68, LBL 57, Y1732; FABRICATED 2 EACH FILLERS AND A REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, PG. 202-213, FIG. 201. 2L72 4F RTA28NM 20030331000752003033100075EU 2003 3 31 AWXA200300318 120030326A5210FE1740011 DAMPER AIRBUS320 A320231 3930325EU PAX DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW42143 082 DURING C-03 CHECK THE L-2 DOOR DAMPER ASSEMBLY WAS FOUND LEAKING. MAINTENANCE REMOVED AND REPLACED THE L-2 DAMPER ASSEMBLY IAW AMM TASK 52-13-14-400-001, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAILURE OF DAMPER CYLINDER ASSEMBLY S/N 280 FINDING LEAKAGE THE FRONT AND REAR CUPS DUE TO WORN SEALS. DETERIORATED SEALS WERE ALSO FOUND ON THE PERCUSSION AND BOTTLE ASSEMBLY. REPLACED ALL WORN PARTS AND COMPLIED WITH S/B'S FE174-52-2 & 3R1, P/N CHANGED TO FE174-004. 2L72 4F RTA28NM 20030331000802003033100080NM 2003 3 31 BJNA030220 120030228A5730 SKIN BOEING737 737282 13844ATNM LT WING CORRODED A BJNAO OTHER O OTHER NRNOT REPORTED 1 WP11789TM46481 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE LT WING OUTBOARD BOOST PUMP CUTOUT AREA. BLENDED OUT THE CORROSION, HOWEVER THE REMAINING MATERIAL THICKNESS WAS BELOW MINIMUM REQUIRED, AND THE CUT OUT OF MATERIAL WAS BEYOND SRM LIMITS. FABRICATED AND INSTALLED REPAIR FILLERS IAW SRM. 2L72 4F RTA16WE 20030331000972003033100097NM 2003 3 31 CALA0300146 120030327A5512 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED IN FOUR PLACES FROM STA 231-272. THE SKIN WAS REPAIRED IAW SRM 55-10-01, FIGURE 203. 2L72 4F RTA16WE 20030331000992003033100099NM 2003 3 31 CALA0300148 120030327A3260 CABLE BOEING737 737524 1384721NM RT MLG OUT OF RIG A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0918622 27526 THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM EWR. APPROPRIATE CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN GEAR AIR/GROUND SENSE TELEFLEX CABLE OUT OF ADJUSTMENT DURING MAIN GEAR SAFETY SENSOR CHECK. THE TELEFLEX CABLE WAS ADJUSTED IAW MM 32-09-01 AND 27-62-51. GROUND SPOILERS CHECKED GOOD. ALL CONNECTIONS WERE LUBRICATED. SYSTEM OPERATIONS CHECKS WERE GOOD. GEAR RETRACTION WAS GOOD IAW MM 32-32-00. 2L72 4F RTA16WE 20030331001052003033100105EU 2003 3 31 DHL2003362007 120030211A2611 CONTROL PANEL AIRBUS300 A300B4203 3930306EU SMOKE DETECT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01362DH 84 ON S/O'S PANEL, AND CARGO SMOKE DETECTION PANEL, THE AFT FAULT MAGNETIC INDICATOR IS AMBER. DUCT WON'T TEST. DEFERRED IAW MEL 26-11-01-2. PLACARD INSTALLED. CONTROL 11968. REF DMI 11968 ON S/O PANEL, THE ELEC CARGO SMOKE DETECTION PANEL. THE AFT DUCT FAULT M1 IS AMBER, IT WON'T TEST. RE-RACKED THE ELECTRIC AND CARGO SMOKE DETECTOR AMPLIFIER. SYSTEM OPS CHECKED GOOD IAW A300 26-14-04. THIS CLEARS DMI 11968. PLACARD REMOVED. 2L72 4F RTA35EU 20030331001062003033100106EU 2003 3 31 DHL2003362008 120030321A2497 BUSS AIRBUS300 A300B4203 3930306EU WARNING PANEL DAMAGED A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01362DH 84 ON APPROACH INTO LICZ, WE HAD A ELECTRIC LIGHT ILLUMINATED ON THE MASTER WARNING PANEL AND SINGLE STROKE CHIME ASSOCIATED WITH A/C BUSS NR 1 OFF ILLUMINATED ON S/O PANEL COMPLETED ABNORMAL PROCEDURES. FOUND NR 1 A/C BUSS WARNING CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. SELECTED NR 1 A/C BUSS. BUSS POWERED TO 115VAC 400 HZ. PERFORMED CHECK OF NR 1 A/C BUSS DISTRIBUTION IAW A-300 M/M 24-50-00. NO DEFECTS NOTED. 2L72 4F RTA35EU 20030331001392003033100139NM 2003 3 31 DHL2003740525 120030221A5310 DOOR FRAME BOEING727 7272Q9 138448MNM CARGO BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT, C-2 DOOR LOWER CUTOUT LOWER FRAME IS CORRODED AND CRACKED IN 3 AREAS. REMOVED THRESHOLD MOUNT FITTINGS FROM C-DOOR FOR ACCESS IAW SRM 51-30-2. REMOVED 2 EA PREVIOUS REPAIRS SPLICE PLATES FROM LWR TEE CHORD IAW SRM 51-30-2. REMOVED FWD AFT, MIDDLE SEAL RETAINERS AND MOUNTS FOR ACCESS IAW SRM 51-30-2. REMOVED LWR T-CHORD FOR REPLACEMENT IAW SRM 51-30-2. FABBED NEW LWR T-CHORD USING 60-9794 PO 301733 DIM 4 INCH X 57.5 INCH IAW SRM 53-10-2 FIG 5 & 51-20-1. ALODINED AND PRIMED T-CHORD IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2. REINSTALLED C-2 DOOR THRESHOLD MOUNTS AND RETAINERS IAW SRM 57-30-2. 2L73 4F RTA3WE 20030331001402003033100140NM 2003 3 31 DHL2003740526 120030221A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT, C-2 DOOR LOWER CUTOUT UPPER DOOR FRAME IS CORRODED AROUND NUT PLATES ON INBOARD FLANGE LOWER SURFACE BETWEEN STA 950E-990 STR 27R. REMOVED NUT PLATES FROM UPPER DOOR FRAME I/B SIDE FOR CORROSION REMOVAL IAW SRM 51-10-2. REMOVED CORROSION FROM UPPER DOOR FRAME IAW SRM 51-10-6 WITH A MATERIAL LOSS OF OVER 50 PERCENT AND IS OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED NEW UPPER DOOR FRAME DIMENSIONS 94 INCHES X 2 INCHES USING 60-20317 PO 3017135 IAW SRM 53-10-2 FIG 5. ALODINED AND PRIMED NEW PIECE IAW SRM 51-10-2 AND INSTALLED UPPER DOOR FRAME IAW SRM 51-30-2. INSTALLED NUT PLATES ON UPPER DOOR FRAME IAW SRM 51-30-2. 2L73 4F RTA3WE 20030401000112003040100011 2003 4 1 250TR0008 420030323A2230L6901 TRANSMITTER BOEING737 7372K5 138448XNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER O OTHER CRCRUISE 1 SO05250TR 22597 AUTO THROTTLE KEEPS DISCONNECTING DURING FLIGHT. REPLACED LT. ENGINE THRUST LEVER POSITION TRANSMITTER PER MM 22-31-81. OPS CHECKED OK. 2L72 4F RTA16WE 20030328000102003032800010EA 2003 3 28 CA030214004 220030205A7414 POINTS PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA MAGNETO LOOSE W O OTHER R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 CA BO19607FR (CAN) LT ENGINE WILL NOT START. REMOVED LEFT MAGNETO AND DISASSEMBLED, FOUND RETARD POINTS NOT OPENING, FOLLOWER PLASTIC AND FELT RIVETS LOOSE AND NOT OPENING POINTS PROPERLY. 1L72 3O3 O A20SO E14EA 20030401000212003040100021WP 2003 4 1 AALA20030227 120030227A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21454AA 49559 DURING OVERNIGHT MAINTENANCE, OVERHEAD CEILING EMERGENCY EXIT LIGHT FORWARD OF AFT EXIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000242003040100024EA 2003 4 1 ASOA03044 120030206A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11914EV 7752 DURING APPROACH INTO ATL FROM DAL, APPROXIMATELY 5,000 FT AND 250 KIAS, THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW SELECTED AN 8 DEGREE FLAP SETTING WITH NO NOTABLE FLAP CHANGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RE-RIGGED BOTH BRAKE POSITION SENSOR UNITS, RESET AND RAN THE FLAPS THROUGH FIFTEEN CYCLES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000512003040100051NM 2003 4 1 CA030220007 120030212A56107560001 WINDOW BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE COCKPIT CRACKED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA 60204 (CAN) DURING CLIMB, CAPTAINS NR 2 WINDOW CRACKED DUE ELECTRICAL ARCING. AIRCRAFT RETURNED TO BASE. NR 2 WINDOW REPLACED AND CHECKED SERVICEABLE. TIME 60204.19 CYC.58513. 2L72 4F4 F A16WE E2EA 20030328000912003032800091EA 2003 3 28 COMA0360164 120030321A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA E&E BAY DOOR OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01960CA 7117 FLIGHT 9492 AVIONICS DOOR CAUTION MESSAGE AT 8000 FT. ADJUSTED THE AVIONICS DOOR PROXIMITY SENSOR. 2L72 4F RTA21EA 20030328000972003032800097EU 2003 3 28 CX7A194J29 120030203A26131734362450 SENSOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03302CE 340B193 TAILPIPE HOT CWP ON LEFT ENGINE DURING T/O ROLL. ABORTED T/O. 2L72 4T RTA52EU 20030331000102003033100010EU 2003 3 31 03FDEA00355 120030328A7830 PANEL AIRBUS310 A310 EU THRUST REVERSER PEELING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 1 ENGINE OUTBOARD THRUST REVERSER TRANSLATING PANEL UPPER SLIDER TEFLON PEELING UP, AND SLIDER DAMAGED. 2L72 4F RTA35EU 20030331000152003033100015EA 2003 3 31 2003F00167 120030213A270060093000103 CONTROL UNIT CNDAIRCL600 CL6002B16 1900305EA RT WING INTERMITTENT A O2GAO OTHER F FLT CONT AFFECTED LDLANDING 1 NE03601VH 5043 FLAPS STOPPED AT 2 DEGREES POSITION WHEN FLAPS SELECTED TO 20 DEGREES. RESET CONVETERS AT FLAP CONTROL UNIT. FLAPS OPERATED NORMALLY FOR REMAINDER OF FLIGHT. CHANGED FLAP BDU. AIRCRAFT RETURNED TO SERVICE WITH NO PROBLEMS. (M) 2L72 4F RTA21EA 20030331000212003033100021EA 2003 3 31 A6WA200340027 120030106A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 OBLIQUE ANGLE AT FS 625 RT SIDE IS CRACKED 1 INCH IN RADIUS REMOVED AND REPLACED CRACKED OBLIQUE ANGLE AT FS 625 RIGHT SIDE. 2L72 4F RTA21EA 20030331000362003033100036WP 2003 3 31 AALA20030060 120030114A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21476AA 49651 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS OVER WALKWAY IN TAIL COMPARTMENT INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT BATTERY FOR TAILCONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000372003033100037WP 2003 3 31 AALA20030061 120030114A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21205AA 49155 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERWING SIGN AT ROW 21 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000412003033100041WP 2003 3 31 AALA20030184 120030208A21205953625521 DUCT DOUG DC9 DC982 3022082WP TAIL CRACKED A AALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW21203AA 49145 EN ROUTE MIA-IAH, ON CLIMB-OUT, PASSING 14,000 FT, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. LEVELED AIRCRAFT AT 16,000 FT AND ACCOMPLISHED PROCEDURE. WITH HIGH PRESSURE BLEED OFF, THE LIGHT EXTINGUISHED. RETURNED MIA WITHOUT INCIDENT. AFTER LANDING, IT WAS NOTED THAT THE GROUND INSTRUMENT COOLING FAN WAS NOT IN OPERATION. REPLACED WATER SEPARATOR DUCT. PERFORMED LEAK CHECK, NO LEAKS NOTED. PERFORMED OPERATIONS CHECK OF TAIL COMPARTMENT OVERHEAT SYSTEM. NO FAULTS NOTED. ALSO, ACCOMPLISHED GROUND CHECK OF INSTRUMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000462003033100046WP 2003 3 31 AALA20030200 120030216A3350 CONTACTOR DOUG DC9 DC982 3022082WP CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21476AA 49651 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT L2 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000692003033100069EA 2003 3 31 ASOA03093 120030308A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11880AS 7606 DURING DESCENT, A STRONG FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN WHEN THE BLEEDS WERE SWITCHED FROM THE ENGINE TO THE AUXILIARY POWER UNIT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE AUXILIARY POWER UNIT FOR LEAKS AND RAN BOTH ENGINES WHILE TRANSFERRING THE RT ENGINE BLEEDS TO THE AUXILIARY POWER UNIT SEVERAL TIMES. THE FUEL ODOR DID NOT REOCCUR. OPERATIONAL CHECKS GOOD. AIRCRAFT, OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030331000782003033100078NM 2003 3 31 AWXA200300321 120030324A53206545834551 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD END OF INTERCOSTAL BETWEEN FLOORBEAMS AT BS 328 AND BS 344, LBL 46. MAINTENANCE REMOVED DAMAGED INTERCOSTAL BETWEEN FLOORBEAMS AT BS 328 AND BS 344, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030331001072003033100107EU 2003 3 31 DHL2003362500 120030207A5311 FRAME AIRBUS300 A300B4203 3930306EU FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 DENT (CREASE) IN FRAME 24 BETWEEN STRINGER 8 AND 9. REMOVED WALL PANEL FOR ACCESS. CUT OUT DAMAGED AREA FROM FRAME. FABRICATED DOUBLER. INSTALLED DOUBLER 0.50, CLEANED AREA. REINSTALLED WALL PANEL. ALL WORK DONE PER A 300 SRM 53-10-10 PG 269-270. 2L72 4F RTA35EU 20030331001132003033100113EU 2003 3 31 DHL2003367001 120030201A2710 STRUCTURE AIRBUS300 A300B4203 3930306EU AILERON VIBRATION A DHLAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO01367DH 265 CONTINUOUS MODERATE AIRFRAME VIBRATION WHEN ABOVE FLIGHT LEVEL 200 AND 250 KIAS. EMERGENCY DECLARED. RETURNED TO LAX. SUSPECT ALL-SPEED AILERONS. PERFORMED ADJUSTMENTS ON BOTH ALL-SPEED AILERONS IAW 27-10-00. GROUND OPS CHECKED GOOD AT THIS TIME. RT FUEL JETTISON VALVE FAILED TO OPEN ON PRIMARY SYSTEM. VALVE OPENED USING SECONDARY SYSTEM. CHECKED PER M/M 28-31-00. NO DEFECTS NOTED. OK FOR SERVICE. OVERWEIGHT LANDING AT 298,000 LBS. PERFORMED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-11. NO DEFECTS NOTED. 2L72 4F RTA35EU 20030331001222003033100122NM 2003 3 31 DHL2003740502 120030213A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FWD CARGO FRAME HAS 3 DENTS AT BS 700 STR 38 L. REMOVED FASTENERS FOR ACCESS PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 57-40-3. FABRICATED REPAIR 7075-T6 .063 PER SRM 53-10-3 FIG 3. ALODINED AND PRIMED PER SRM 51-10-2, INSTALLED REPAIR PER SRM 57-40-3 FIG 1. 2L73 4F RTA3WE 20030331001412003033100141NM 2003 3 31 DHL2003740527 120030226A5521 SPAR BOEING727 7272Q9 138448MNM RT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 RT ELEVATOR TAB HAS 3 O/B HINGES LOOSE AT ELEVATOR REAR SPAR ATTACH POINT, CHECK FOR SPAR CRACKS PER S/B 55-0089. REMOVED DAMAGED SPAR AND INSTALLED NEW SPAR (P/N 65C30825-24) PO 301742 IAW S/B 727-55-0089 FIG 6 AND SUPPORT FITTINGS. 2L73 4F RTA3WE 20030401000022003040100002NM 2003 4 1 03087403 120030328A3350362624 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27403FJ 3149 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030401000092003040100009EA 2003 4 1 03090668 120030331A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27668BR 7544 DURING MAINTENANCE INSPECTION, THE OVERHEAD CABIN EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030328000182003032800018CE 2003 3 28 CA030218001 120030203A5711101110367 SPAR CAP BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE WING CORRODED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) CORROSION ON UPPER RIGHT AND LEFT FORWARD WING SPAR CAPS BETWEEN WS 223 & 236 AND WS 122 & 132. CORROSION IS BEYOND LIMITS, WINGS TO BE REMOVED AND SPARS TO BE REPLACED AS DIRECTED BY BEECHCRAFT ENGINEERING. 1L72 4T4 T A24CE E4EA 20030401000192003040100019WP 2003 4 1 AALA20030220 120030223A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21567AM 53293 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS IN FORWARD GALLEY AND FLIGHT DECK INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONNECTIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030401000302003040100030EA 2003 4 1 ASOA03050 120030209A3350OL3071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11857AS 7411 DURING A GROUND INSPECTION IN MGM, THE CEILING EMERGENCY EXIT LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A LAMP IN THE CEILING EMEGENCY EXIT LIGHT AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000702003040100070NM 2003 4 1 CA030228013 120030219A2740651948220 GEARBOX BOEING727 727225 1384077NM PWA JT8 JT8D7B 52053NE STAB TRIM FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING COLD WEATHER, PRE-DEPARTURE CHECK BY MAINTENANCE PERSONNEL, THE STABILIZER TRIM SYSTEM WAS OPERATED. DURING OPERATION A VIBRATION AND NOISE WAS NOTICED. UPON INVESTIGATION IT WAS FOUND THAT THE BRAKE ASSEMBLIES IN THE STABILIZER TRIM GEARBOX WERE NOT FUNCTIONING CORRECTLY, CAUSING THE VIBRATION AND NOISE. THE STABILIZER TRIM GEARBOX AND JACKSCREW ASSEMBLY WAS REPLACED WHICH RECTIFIED THE DEFECT. INVESTIGATION OF PRIOR FLIGHTS DID NOT SHOW ANY PREVIOUS PROBLEMS. 2L73 4F4 F A3WE E2EA 20030401000762003040100076NM 2003 4 1 DHL2003741502 120030323A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DISCREPANCY AS FOLLOWS DURING C CHECK, B.S. 1030 CIRCUM. IS CRACK LT SIDE 3" ABOVE FLOOR. REMOVED FASTENER AT BS 1030 CIRCUM LT SIDE 3 INCH ABOVE FLOOR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030401000902003040100090NM 2003 4 1 DHL2003747001 120030125A2612 FIRE LOOP BOEING727 727224 1384076NM NR 1 OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01747DH 22253 ON P6-3 CIRCUIT BREAKER PANEL NR 1 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED NR 1 GROUND FAULT DETECTION SYSTEM TO DMI 11753 IAW MEL 26-9. PLACARD INSTALLED. RE; DMI 11753 - NR 1 GROUND FAULT ILLUMINATED. REPOSITIONED FIRE LOOP THAT WAS TOUCHING COWL, CHECKED GOOD PER 26-11-0. CLEARS DMI 11753. PLACARD REMOVED. 2L73 4F A3WE 20030401001122003040100112WP 2003 4 1 DHL2003804503 120030116A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING CTR L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 416.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCEMENT ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001242003040100124WP 2003 4 1 DHL2003804516 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN AT XFS 610.000 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001282003040100128WP 2003 4 1 DHL2003804520 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART HAS A 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001462003040100146WP 2003 4 1 DHL2003804556 120030215A57305769589505 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING L/E UPPER SKIN CORRODED BETWEEN STA. XFS291.5000 AND XFS 304.000 CORR: PERFORMED MAJOR REPAIR IAW EO DHL 030108 , ED-3214. REMOVED FASTNERS IAW SRM51-1-21 PG. 1 REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM57-2-0 PG 16 TRIMMED OUT DAMAGED SKIN SEGEMENT IAW EO DHL 030108 , ED-3214. FABRICATED A REPAIR DOUBLER (7075T6AL.071) AND THREE FILLERS (7075T6AL.063) IAW EO DHL030108 , ED-3214. CLEANED , TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B APPLIED PRC TO ALL FAYING SURFACES IAW SRM 51-1-15 PG. 1 INSTALLED DOUBLERS AND FILLERS AT LH L/E UPPER SKIN WITH NEW FASTNERS IAW EO DHL 030108, ED-3214, SRM51-1-21 PG. 1 2L74 4F RT4A25 20030401001472003040100147WP 2003 4 1 DHL2003804557 120030210A57105769933183 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING OUTBD VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO58.000 PERFORMED MAJOR REPAIR IAW EO DHL 030109 ED-3222 . REMOVED FASTNERS IAW SRM 51-1-21 PG 1 TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075T6AL.063) AND INTERNAL DOUBLER (7075T6AL.050) IAW EO DHL030109 , ED-3222 . CLEANED TREATED , & PRIMED INNER SURFACE IAW SRM51-1-8B APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG. 1 INSTALLED FILLERS AND DOUBLERSAT LH WING OUTBD VANE SLOT UPPER SKIN WITH NEW FASTNERS IAW EO DHL 0-30109 , ED-3222, SRM51-1-21 PG. 1 2L74 4F RT4A25 20030401001562003040100156WP 2003 4 1 DHL2003804666 120030202A53403750257U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 AFT CARGO COMPT. SPLICE FITTING CRACKED 3.000 INCH BETWEEN STA. 1040.000-1060.000 , L31R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1 AND FAX BOEING -SEU-LIM - 03-00003H DATE 20TH 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED , TREATED AND PRIMED AREA IAW SRM51-1-8B. INSTALLED NEW FITTING ON AFT CARGO COMPT. BTWN STA. 1040.000 AND STA. 1060.000 , L31R IAW SRM51-1-20D PG. 9 2L74 4F RT4A25 20030401001732003040100173WP 2003 4 1 DHL2003804873 120030216A57305611002502 SKIN DOUG DC8 DC873F 302199FWP RT WING TE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING T/E UPPER PANEL SKIN DELAMINATED ( STA XW 5.000-47.000) R & R RT WING UPPER T/E PANEL (STA. XW5.000-47.000) IAW SRM 51-3-0 PG. 1 2L74 4F RT4A25 20030401000612003040100061EU 2003 4 1 CA030225002 120030220A5520SD3316213XB BRACKET STBROSSD3 SD360 8100606EU PWA PT6 PT6A65AR 52043NE HARTZLHCB5M HCB5MP3 GL ELEVATOR TRIM CRACKED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 31865 (CAN) BRACKET WAS INSPECTED AS PART OF A FLEET CAMPAIGN INITIATED IN-HOUSE. BRACKET WAS FOUND TO HAVE A .7500 INCH CRACK AND A .2500 INCH CRACK FROM THE OUTSIDE EDGES MOVING INWARD. THE TRIM TAB WAS REMOVED AND REPLACED WITH A SERVICEABLE TRIM TAB. THE REMOVED BRACKET AND THE MASS BALANCE WEIGHT HAVE BEEN SENT TO MFG FOR ANALYSIS. 2H72 4T4 T A41EU E4EA 6 CP44GL 20030401000722003040100072NE 2003 4 1 CA030304002 220030227A7200 ENGINE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE NR2 STALLED W E ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 CA (CAN) NR 2 ENGINE STALL IN LEVEL FLT. ECAM MSG NR 2 ENGINE STALL THEN NR 2 ENGINE SHUT DOWN. ECAM ACTIONS CARRIED OUT. CHANGED NR 2 ENGINE IAW AMM. 2L72 4F4 FRTA28NM E29NE 20030401000812003040100081NM 2003 4 1 DHL2003745003 120030123A3260 SWITCH BOEING727 727224 1384076NM MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION UPON MOVING GEAR HANDLE FROM UP TO OFF POSITION. S/O RT GEAR DOOR LIGHT ILLUMINATED, AND FRONT PANEL DOOR LIGHT ILLUMINATED. BROUGHT LEVER BACK TO UP AND ALL DOOR LIGHTS EXTINGUISHED. TROUBLESHOT SYSTEM, FOUND DEBRIS AT RT MLG WARNING SWITCH. CLEANED AND RESECURED. PERFORMED OPERATIONAL SYSTEM TEST, NO DEFECTS NOTED REF M/M 32-62-11. 2L73 4F A3WE 20030401000822003040100082NM 2003 4 1 DHL2003745005 120030205A261210607723 WARNING SYSTEM BOEING727 727224 1384076NM FIRE WARNING MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01745DH 20665 FIRE WARNING BELL IS MAKING STRANGE NOISE AND NO BELL. REPLACED AURAL WARNING BOX. OPS CHECKED GOOD IAW B727 M/M 31-26-0. 2L73 4F A3WE 20030401001112003040100111WP 2003 4 1 DHL2003804502 120030120A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 422.750. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001302003040100130WP 2003 4 1 DHL2003804522 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 641.250. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001412003040100141WP 2003 4 1 DHL2003804549 120030206A57205769859U164 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT ZEE PAN WING ZEE PAN FITTING CRACKED 2.00STA. XW 223.000 CORR: REMOVED FITTING ZEE PAN(CRACKED CONDITION)IAW SRM51-3-0 PG. 1 CLEANED , TREATED, & PRIMED AREA IAW SRM51-1-8B , INSTALLED NEW FITTING ZEE PAN ON RH WING L/E , STA. XW 233.000 IAW SRM51-3-0 PG. 1 2L74 4F RT4A25 20030401001482003040100148WP 2003 4 1 DHL2003804558 120030202A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING L/E UPPER SKIN CORRODED BETWEEN STA 422.750 AND XFS 427.000 PERFORMED MAJOR REPAIR IAW SRM57-2-1 PAGE 2 FIG. 38 REMOVED CORROSION ON L/E UPPER SKIN IAW SRM51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. CUT OUT CORRODED AREA IAW SRM 57-2-1 PG. 2, FIG.38 CLEANED , TREATED, AND PRIMED FILLER & DOUBLER INNER PART IAW SRM 51-1-8B. INSTALLED FILLER & DOUBLER ON LT WING STA. XFS 422.750-XFS 427.000 AND APPLIED PRC SEALANT IAW SRM 57-2-1 PG. 2 FIG 38, SRM51-1-21 PG. 1 SRM51-1-15 PG 1, FOR REMOVAL AND RE-INSTALLATION OF CENTER L/E SEE N/R0318. 2L74 4F RT4A25 20030401001492003040100149WP 2003 4 1 DHL2003804559 120030307A552257025792 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 REMOVAL / INSTALLATION OF THE RT ELEVATOR GEAR TAB DUE TO DELAMINATION ON UPPER SKIN. R & R RT ELEVATOR GEAR TAB IAW MM 27-30-3 PG. 201-206 REFER TO N/R 0607 FOR OPS CHECK. 2L74 4F RT4A25 20030401001532003040100153WP 2003 4 1 DHL2003804663 120030207A533056544401 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING NR 718 CENTERWING LOWER PANEL EXTERNAL SKIN DELAMINATED STA 730.000-STA 779.000 R & R NR 718 CENTERWING LOWER PANEL ON LT WING , STA 730.000-STA. 779.000 IAW SRM 51-3-0 2L74 4F RT4A25 20030401001592003040100159WP 2003 4 1 DHL2003804669 120030208A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT ELEVATOR UPPER SKIN SURFACE DENTED ( STA. 44.907 - 50.000) PERFORMED MAJOR REPAIR IAW EO DHL 030102, ED-3219 . REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 REMOVED DAMAGED SKIN SEGMENT IAW EO DHL 030102 , ED-3219. CLEANED TREATED AND PRIMED NEW SKIN INTERIOR IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG. 1 INSTALLED NEW SKIN SEGMENT ONRT ELEVATOR TOP SURFACE WITH NEW FASTNERS IAW EO DHL 030102 , ED-3219 AND SRM 51-1-21 PG. 1 SEE N/R 2052 FOR RT. ELEVATOR REMOVAL AND INSTALLATION. SEE N/R 2645 FOR WEIGHT AND BALANCE 2L74 4F RT4A25 20030401001822003040100182WP 2003 4 1 DHL2003873004 120030307A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP CARGO BAY MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01873SJ 46091 NR 6 POSITION SMOKE DETECTOR SELECT DOES NOT ILLUMINATE DURING TEST. MAY BE INOPERATIVE PER MEL 26-6-2 DMI NR 12210 PLACARD INSTALLED. REF. DMI NR 12210 NR 6 POSITION ON SMOKE DETECTOR SELECT DOES NOT ILLUMINATE DURING TEST. PERFORMED OPERATIONAL TEST OF NR 6 CARGO SMOKE DETECTOR PER DC-8 M/M 26-10-00. OPS CHECKED GOOD. THIS CLEARS DMI #12210. 2L74 4F RT4A25 20030408000692003040800069NM 2003 4 8 03FDEA00359 120030304A5740ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, O/B FLAP, I/B HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLES 2 EACH CORRODED. WINGS - RIGHT O/B FLAP, I/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORROSION REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1-5740- 68589. 2L73 4F RTA22WE 20030403000262003040300026NM 2003 4 3 03FDEA00360 120030401A5330 SKIN BOEING727 727200 138407ENM DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 N00175 EXTERIOR SKIN IS DENTED AT STA. 702F STR-4R. DENT AT 702F+15 STR 4R WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1, PG 2A, DETAIL II. CUT OUT DAMAGED SKIN 1 INCH DIAMETER AND REPAIRED IAW SRM 53-30-3. 2L73 4F RTA3WE 20030402000262003040200026EU 2003 4 2 1140311144 120030114A2910109072924119 TRANSDUCER AGUSTAA109 A109E 0260119EU NR 2 HYD SYS INOPERATIVE A NXTAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW19144CF12 11144 DURING PATIENT FLIGHT, NR 2 MAIN HYDRAULICS PRESSURE QUICKLY FELL INTO THE CAUTION RANGE. IN ANTICIPATION OF TOTAL LOSS NR 2 SYSTEM. I SLOWED BELOW VIE, EXTENDED GEAR ( 3 GREEN) CONTINUING TO SLOW TO 90 KNOTS. DECLARED AN EMERGENCY, MADE AN UNEVENTFUL PRECAUTIONARY LANDING. SLOW TO VIE, EXTEND LANDING GEAR, LANDED AT NEAREST AIRPORT. 1G72 3U RTH7EU 20030402000462003040200046NM 2003 4 2 2003UALA00323 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT AT STA 1340 BETWEEN STR 25L AND 26L, TOP OF FRAME IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20030402000582003040200058NM 2003 4 2 2003UALA00335 120030327A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 SEAT TRACK CORRODED, BS 800-808, LBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIRED SEAT TRACK WITH SPLICE SECTION AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030402000722003040200072NM 2003 4 2 A6WA200330005 120030304A3260DOLN1076B CONNECTOR DORNERDO32 DO328100 2996000NM GROUND MATRIX INTERMITTENT A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31331MX 3074 PROXY SYSTEM FAIL MESSAGE IN FLT. FOUND INTERMITTENT CONNECTION AT GROUND MATRIX 80VPNV. CLEANED AND RERACKED GROUND MATRIX. OPS CHECK GOOD AT THIS TIME. (IPC REF: 24-50-01-1-370) 2H72 4T RTA45NM 20030403000252003040300025NM 2003 4 3 03013 120030331A5210 STRUCTURE BOEING747 747132 1384882NM PAX DOOR TORN A KCSAK NONE O OTHER ININSP/MAINT 1 GL23709CK 20247 ON THRU FLIGHT INSPECTION, FOUND L-2 DOOR FORWARD LOWER EDGE BELOW BOTTOM HINGE TO LOWER "R" STRAP PULLED LOOSE AND TORN. APPROX. SIZE 10 INCH ON FRONT; BOTTOM BROKE LOOSE APPROX. 6 INCH AFT; SHEET METAL IS TORN UPWARD APPROX. 6 INCHES. 2L74 4F A20WE 20030403000322003040300032EU 2003 4 3 148891 120030402A3220 LANDING GEAR SAAB SF340 SF340A 7850100EU NLG VIBRATION A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL17149SZ 340A149 FLIGHT 4507 CRW-PIT. A/C EXPERIENCED SEVERE NOSEWHEEL SHIMMY AT ABOUT 40-45 KNOTS DURING INITIAL TAKE-OFF ROLL. CREW ABORTED TAKE-OFF AND RETURNED TO GATE. CREW DID NOT EXPERIENCE ANY SHIMMY DURING NORMAL TAXIING. A/C TAKEN OUT OF SERVICE 4-2-03 AT1519. 2L72 4T RTA52EU 20030403000642003040300064SO 2003 4 3 ASOA03056 120030211A541012039731001 FRAME EMB 120 EMB120ER 3260203SO NACELLE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11266AS 120188 DURING A HANGAR CHECK IT TXK, THE LOWER AFT SECTION NACELLE HALF-FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER AFT SECTION NACELLE HALF-FRAME IAW SRM 54-20-04. (M) 2L72 4T RTA31SO 20030403000662003040300066NM 2003 4 3 AWXA200300328 120030330A2730285T0015116 COMPUTER BOEING757 757225 1384959NM STAB TRIM MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28913AW 22207 ON CLIMB OUT, RECEIVED EICAS MESSAGE "ELEV ASYM", NO ADVERSE CONTROL FEEL, TURNED BACK FOR REPAIR. MAINT R & R LT STAB TRIM AILERON LOCKOUT COMPUTER, OPERATIONAL TEST GOOD. PERFORMED TEST FLT TO VERIFY SYS INTEGRITY; PRIOR TO FIRST TAKEOFF PULLED RT ADC CIRCUIT BREAKER TO DEFAULT TO LT STAB TRIM AILERON COMPUTER, A/C FLEW WITHOUT EVENT. RESET RT ADC CIRCUIT BREAKER AND PULLED LT BREAKER TO ISOLATE RT STAB TRIM AILERON COMPUTER. ON CLIMB AT APPROX 230 KTS RECEIVED EICAS MESSAGE "ELEV ASYM", CLEARED PRIOR TO LANDING. INSPECTED BOTH STAB TRIM AILERON COMPUTERS, NO FAULTS NOTED. VERIFIED ELEVATOR ASYM ACT MOVES FROM HIGH SPEED & RETURNS TO NORMAL. R & R RT STAB TRIM AILERON L/O COMPUTER, OPS TEST GOOD. 2L72 4F RTA2NM 20030328000042003032800004NM 2003 3 28 CA030212008 120030212A323282970018011 CYLINDER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG DOOR UPLOCK CORRODED W O OTHER O OTHER NRNOT REPORTED 1 CA LI0021 (CAN) DURING SCHEDULED AIRCRAFT INSPECTION MLG DOOR UPLOCK ACTUATOR FOUND LEAKING. COMPONENT REMOVED AND SENT TO SHOP, SHOP INSPECTION FOUND SEVERE CORROSION IN THE UPLOCK PISTON ROD BORE AND PISTON RETAINING NUT . PART DETERMINED BEYOND ECONOMICAL REPAIR. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030328000092003032800009NE 2003 3 28 CA030214003 220030207A8520LW13923 BUSHING PIPER PA60 PA60602P 7106015NM LYC O540 IO540AA1A 41532NE CONNECTING ROD CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING INSPECTION OF AN ENGINE IN FOR CRANKCASE REPAIR AND AD 2002-20-51, 4 OUT OF 6 CONNECTING ROD BUSHINGS WERE FOUND CRACKED OR BROKEN. SOME BUSHINGS HAD ROTATED IN THE CONNECTING ROD, PROBABLY AFTER CRACKING.NO HISTORY OF OVERBOOST, OVERSPEED, OR DETONATION REPORTED. 1M72 3O3 ORTA17WE 1EA 20030820002362003082000236NM 2003 8 20 USAASB03092 120030627A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19523AU 23858 MAINTENANCE REPORTED THE EMERGENCY LIGHTS FROM SEAT ROWS 17 THROUGH 22 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030821000052003082100005EA 2003 8 21 ASOA03323 120030719A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11828AS 7213 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030821000172003082100017 2003 8 21 USAABA03010 420030430A25654A38571 REGULATOR AIRBUS330 A330323 3930335EU ESCAPE SLIDE MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19 4552 DURING SLIDE TESTING IN THE SHOP, THE SLIDE DID NOT INFLATE WHEN THE REGULATOR WAS ACTIVATED. AFTER APPLYING A SHARP RAP TO THE REGULATOR, THE SLIDE INFLATED NORMALLY. MAINTENANCE IN THE SHOP FOUND THE REGULATOR BORE SCORED WHICH WAS MOST LIKELY CAUSED BY CHATTERING OF THE SPRING WASHERS. (M) 2L72 4F RTA46NM 20030821000212003082100021 2003 8 21 USAABA03011 420030430A25654A38571 REGULATOR AIRBUS330 A330323 3930335EU ESCAPE SLIDE MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19 CLT - DURING SLIDE TESTING IN THE SHOP, THE SLIDE DID NOT INFLATE WHEN THE REGULATOR WAS ACTIVATED. AFTER APPLYING A SHARP RAP TO THE REGULATOR, THE SLIDE INFLATED NORMALLY. MAINTENANCE IN THE SHOP FOUND THE REGULATOR BORE SCORED WHICH WAS MOST LIKELY CAUSED BY CHATTERING OF THE SPRING WASHERS. (M) 2L72 4F RTA46NM 20030821000242003082100024NM 2003 8 21 03FDEA00965 120030624A5511ALC8100 SPAR CAP DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STAB RIGHT UPPER AFT SPAR CAP BARREL NUT BORE NR 36R FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. RIGHT HORIZONTAL STAB UPPER AFT SPAR CAP BARREL NUT BORE NR 36R REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030821000272003082100027NM 2003 8 21 03FDEA00962 120030622A5510ALC8100 BARREL NUT DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STAB LEFT UPPER CENTER PLANK BARREL NUT BORE NR 21L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LEFT HORIZONTAL STAB UPPER CENTER PLANK BARREL NUT NR 21L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030402000122003040200012EU 2003 4 2 030903292 120030331A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSBURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27329UE 41097 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FWD EXIT SIGN WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030402000142003040200014EA 2003 4 2 03091620 120030401A33500L6839BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY SIGN BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27620BR 7179 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE PERSONNEL REPLACED LAMP IN THE EMERGENCY EXIT SIGN OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030402000202003040200020EU 2003 4 2 0300643221 120030330A2910 O-RING AIRBUS320 A320211 3930320EU PTU MANIFOLD LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01321US 262 RECEIVED YELLOW SYSTEM HYDRAULIC RESERVOIR LOW LEVEL WARNING. ECAM INDICATED ZERO QUANTITY IN YELLOW SYSTEM RESERVOIR. DEACTIVATED YELLOW HYDRAULIC SYSTEM PER COM AND LANDED UNEVENTFULLY. REPLACED O-RING AT THE PTU MANIFOLD AND LEAK CHECKED OK. SERVICED YELLOW HYDRAULIC SYSTEM. RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA28NM 20030403000302003040300030NM 2003 4 3 03FDEA00369 120030401A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 MECHANICAL DAMAGE TO FRAME BS 420 BETWEEN STR 6 RT AND 7 RT. INSTALLED REPAIR CHANNEL ON FRAME PER SRM 53-10-4. 2L73 4F RTA3WE 20030402000492003040200049NM 2003 4 2 2003UALA00326 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT STA 1360 ABOVE STR 26L, TOP OF FRAME FLANGE IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR 2L72 4F4 FRTA2NM E17NE 20030402000562003040200056NM 2003 4 2 2003UALA00333 120030327A5755 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SPOILER INOPERATIVE A UALALA ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION LDLANDING 1 WP29180UA 25224 A/C RECEIVED NO RIGHT SPOILER INPUT/RESPONSE ON APPROACH INTO LAX 2L74 4F4 FRTA20WE E24NE 20030402000632003040200063NM 2003 4 2 2003UALA00340 120030305A5754114W424011 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 6 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED 2L72 4F4 FRTT0001SE E46NE 20030403000352003040300035 2003 4 3 249TR0016 420030331A2220 WARNING LIGHT BOEING737 7372K5 138448XNM MACH TRIM ILLUMINATED A PIDAO OTHER N FALSE WARNING CRCRUISE 1 SO05249TR 22598 MACH TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. UNABLE TO DUPLICATE. PERFORMED BITE TEST VIA PDCS CDU, NO FAULTS NOTED. 2L72 4F RTA16WE 20030403000462003040300046NM 2003 4 3 AMTA200300305 120030304A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 EPL RED LIGHT 1 EACH AT ROW 29 INOPERATIVE. FOUND DISCONNECTED EPL WIRE AND 32D, CIRCUIT TO RED LIGHT AT 29 VERIFIED OPERATIVE. (M) 2L72 4F RTA2NM 20030403000702003040300070NM 2003 4 3 AWXA200300332 120030326A53206517684642 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON FORWARD OUTBOARD CORNER OF INTERCOSTAL, JUST FORWARD OF L-1 DOOR AT BS 294 TO BS 303, STR 7 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT BS 294 TO BS 303, STR 7 L/H; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12 2L72 4F RTA16WE 20030328000232003032800023EU 2003 3 28 2003FA0000327 120030320A4930160353500 LINE BRAERODH125 BAE125800A 1500285EU APU FUEL LEAKING C O OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL0774NP 1286 NA0440 AFTER APU SHUTDOWN PILOT OBSERVED SMOKE COMING FROM TAILCONE JUST PROIR TO ATTEMPTING REFUEL. REFUEL PROCESS ABORTED AND REARBAY ACCESS DOOR OPENED TO INVESTIGATE. CREW MEMBER OBSERVED DENSE WHITE SMOKE COMING FROM REAR BAY. FURTHER INVESTIGATION REVEALED A SPLIT IN THE FUEL MANIFOLD FOR THE APU. SBT62T49108 ADDRESSES THIS PROBLEM, HOWEVER IT IS ONLY AN OPTIONAL BULLETTIN. 2L72 4F RTA3EU 20030328000252003032800025EU 2003 3 28 03084302 120030325A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27302UE 41013 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030328000462003032800046SO 2003 3 28 C2XA03TY034 120030313A531014521699003 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716911 145446 DURING A SCHEDULED 1-C INSPECTION THE OMEGA BEAM AT FRAME 20 WAS CORRODED. MAINTENANCE CUT OUT DAMAGED AREA, FAB, ALODINE, PRIME, PAINTED AND INSTALLED REPAIRED DOUBLER, FILLER AND SHIMS IAW EMB 135/145 SRM 53-21-10, 51-40-02;CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030331000382003033100038WP 2003 3 31 AALA20030086 120030121A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2176200 53290 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTS IN AFT GALLEY AREA INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR AFT GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030821000902003082100090NM 2003 8 21 03FDEA00805 120030523A5753ARC198414 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP HINGE AFT FITTING FOUND OUTBOARD PIVOT BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69346 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030408000072003040800007WP 2003 4 8 ASAA0380081 120030113A5320S170631741 ANGLE DOUG DC9 DC983 3022083WP BULKHEAD CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY AFT BULKHEAD PANEL MOUNTING STRAP ATTACH ANGLE CORRODED. REPLACED ANGLE PER SRM 51-10-2 AND 51-30-5. (M) 2L72 4F RTA6WE 20030408000202003040800020WP 2003 4 8 ASAA0380109 120030125A5320991157912 BRACKET DOUG DC9 DC982 3022082WP FUSELAGE FRAME CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OAK - FOUND DURING C-CHECK, FORWARD SERVICE DOOR FORWARD UPPER CORNER FRAME SUPPORT BRACKET CRACKED. FABRICATED AND REPLACED BRACKET PER SRM 51-30-5, 51-10-3, AND DAC DWG 9911579. (M) 2L72 4F A6WE 20030408000242003040800024EA 2003 4 8 SIMA200300818 120030104A2782M766385A ACTUATOR CNDAIRCL600 CL6002C10 1390015EA SLAT FAILED A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21501BG 10017 DFW - FLT 3902 - CREW REPORTED A SLATS FAULT CAUTION ON EICAS. MAINTENANCE REMOVED AND REPLACED THE LEFT (S/N 0164) AND RIGHT OUTBOARD SLAT ACTUATORS IAW CRJ MM. AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. CHECK FLIGHT WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030408000252003040800025EA 2003 4 8 SIMA200301201 120030109A2820CC6706210401 TUBE CNDAIRCL600 CL6002C10 1390015EA CENTER TANK CRACKED A SIMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21505AE 10053 BOI - FLT 3902 - DURING CLIMB, CREW REPORTED A FUEL IMBALANCE CAUTION MESSAGE. USED PUMPS AND GRAVITY TO MOVE FUEL FROM CENTER WING TANK. AIRCRAFT CONTINUED TO DFW. IN BOI, CENTER TANK HAD 200 LBS AND WINGS HAD 5,500 LBS. MAINTENANCE FOUND A FUEL TUBE ASSEMBLY CRACKED IN THE LEFT CENTER WING TANK. TUBE WAS REMOVED AND REPLACED IAW CRJ MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030408000262003040800026SO 2003 4 8 SIMA200302003 120030116A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21647AE 145222 SWF - FLT 4133 - CREW REPORTED SEVERAL EMERGENCY LIGHTS IN THE AFT CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTEYR IN THE NR 4 POWER SUPPLY UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030408000462003040800046NM 2003 4 8 USAABB03024 120030223A3350 BATTERY BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19621AU 27200 PIT - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 9 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030408000492003040800049NE 2003 4 8 USAASA03013 220030209A7200 ENGINE AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FAILED A EA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA19708UW 0972 THE FLT WAS APPROXIMATELY 65 MILES FROM SJU, CLIMBING THROUGH FL200, WHEN A LOUD BANG WAS HEARD THROUGHOUT THE AIRCRAFT, FOLLOWED BY VIBRATION AND A LOSS OF N2 INDICATION. THE ENGINE WAS SHUTDOWN BY THE CREW WHILE THE ENGINE PARAMETERS BEGAN TO DECAY. FLIGHT RETURNED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT ENGINE. OPERATIONALLY CHECKS OK. (M) 2L72 4F4 FRTA28NM E37NE 20030328000362003032800036SO 2003 3 28 C2XA03TY021 120030210A531014522460013 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE CENTER OMEGA BEAM WAS CORRODED. MAINTENANCE CUT OUT THE DAMAGED AREA AND FAB NEW FILLER REPAIR. INSTALLED NEW PIECE IAW EMB 135/145 SRM 53-21-10; 51-40-02. ALODINED, PRIMED IAW EMB 135/145 CPM 51-21-04;05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030331000852003033100085SO 2003 3 31 C2XA03SH062 120030329A531014526437001 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE RT BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331001022003033100102NM 2003 3 31 CH1A200394006 120030327A7100 ENGINE BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 2 STALLED A C1HAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL15294AS 22146 COMPRESSOR STALL ENGINE NR 2 AT BEGINNING OF TAKEOFF ROLL EPR APPROX 1.3 2L73 4F4 F A3WE E2EA 20030401000332003040100033EU 2003 4 1 ASOA03053 120030210A33507012210 LIGHT AEROSPATR72 ATR72 EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11641AS 387 DURING A GROUND INSPECTION IN MGM, THE CEILING EMERGENCY LIGHT AT ROW 14 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT LAMP AT ROW 14. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030401000532003040100053EA 2003 4 1 CA030221001 120030207A5610NP1393211 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE COCKPIT CRACKED W A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 CA 15995 (CAN) DURING CLIMBOUT CAPTAINS WINDSHIELD CRACKED. DECLARED AN EMERGENCY AND RETURNED TO BASE. REMOVED AND REPLACED WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20030401000572003040100057CE 2003 4 1 CA030224001 120030213A1430 FASTENER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE TORQUE TUBE LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON INSPECTION OF THE ELEVATOR SYSTEM AND TAIL AREA, THE LT ELEVATOR TORQUE TUBE FASTENERS WERE FOUND LOOSE. OUT OF THE 8 FASTENERS, 7 WERE LOOSE AND 1 HAD SHEARED OFF. NO OVERSIZE FASTENERS ARE APPROVED ON (SERIAL NUMBER UE-258) AIRCRAFT AND AFTER. THE TORQUE TUBE WAS REPLACED AND THE APPROPRIATE INSPECTIONS AND RIGGING CARRIED OUT. SUGGEST PARTICULAR CARE TAKEN WHEN INPSECTING THIS ITEM. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030401001212003040100121WP 2003 4 1 DHL2003804513 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART WITH A 1 IN CRACK AT STA XFS 785.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001222003040100122CE 2003 4 1 DHL2003804514 120030114A5754 FRAME BEECH 200 200BEECH 1152920CE LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804 BB724 LT WING INBD L/E FORMER CRACKED 1 IN AT STA XFS 597.500 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 1L72 4T A24CE 20030625001362003062500136NM 2003 6 25 03FDEA00364 120030401A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION ON BS 344 FLOORBEAM LBL 55 - RBL 15 WL 208. REMOVED CORROSION ON UPPER CHORD OF FLOORBEAM BS 344 LBL 55 - RBL 15, WL 208 MAX REMOVAL 1 X 1 X 0.030 INCH ORIGINAL THICKNESS 0.090 OUT OF LIMITS IAW SRM 51-10-6 &7 SRM 53-10-1. ACCOMPLISHED REPAIR ON UPPER CHORD OF FLOORBEAM AT BS 344 BL 0 - LBL 65 (SKIN) IAW SRM 53-10-8 FIG 9. 2L73 4F RTA3WE 20030402000242003040200024NM 2003 4 2 03FDEA00370 120030401A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION ON UPR FLANGE OF FLOORBEAM BS 910 RBL 55 WL 208 LWR SURFACE AT NUT PLATE HOLE. 2L73 4F RTA3WE 20030402000502003040200050NM 2003 4 2 2003UALA00327 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT STA 1400 BETWEEN STR 25L AND 26L, FRAME UPPER FLANGE DENTED IN TWO AREAS MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR 2L72 4F4 FRTA2NM E17NE 20030403000452003040300045NM 2003 4 3 AMTA200300293 120030225A335020131A BATTERY PACK BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 FORWARD RIGHT SIDE EGRESS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-07-02. OPS CHECKED GOOD. (M) 2L72 4F RTA2NM 20030403001232003040300123NM 2003 4 3 DL733030147 120030212A534265495587 FITTING BOEING737 737347 1384647NM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308WA 23441 CORROSION WAS FOUND IN THE BORES OF BOTH THE LT AND RT PRIMARY FORWARD CLEVIS LUGS. THE LHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.440 INCH TO REMOVE THE CORROSION. THE RHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.408 INCH. NO OTHER MACHINING WAS DONE. THE DAMAGE WAS FOUND AT HMV. 2L72 4F RTA16WE 20030404000382003040400038 2003 4 4 DL73K030295 420030327A3410 LINE BOEING737 737247 138448DNM NR 1 ADC DAMAGED A DALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO27243WA 23517 CAPT'S A/S INDICATOR FAILED ABOVE 110K ON TAKEOFF. ON T/O IT WENT TO 45K, AFTER AIRBORNE TO 360K, LATER DECREASED TO 45K PRIOR TO LANDING. REPLACED PITOT FLEX LINE ON FRONT OF NR 1 ADC, PERFORMED LEAK CK PER MM AND FOUND NO LEAKS. ALL INST TEST OK PER MM. 2L72 4F A16WE 20030404000392003040400039NM 2003 4 4 DL73K030310 120030329A531065458076 DOOR FRAME BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27382DL 23609 THE UPPER STUB SECTION OF THE R1 DOOR OPENING FWD FRAME WAS FOUND WITH A 1.1 INCH CRACK IN THE BEND RADIUS EMANATING FROM THE FRAME CUTOUT FOR THE UPPER DOOR STOP FITTING. THE CRACK WAS REMOVED WITH A TRIM OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER ER/A 384769-14, REV A. 2L72 4F A16WE 20030407000142003040700014WP 2003 4 7 ASAA0380069 120030112A5310991980549 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, SHEAR TIE CORRODED AT FS 1250. REPLACED SHEAR TIE PER SRM 51-10-2, 51-10-3, AND 53-14-3. (M) 2L72 4F RTA6WE 20030407000732003040700073SO 2003 4 7 SIMA200302001 120030115A2121011768500 FAN EMB 135 EMB135LR 3260305SO CARGO BAY BURNED OUT A SIMAFD ACTIVATE FIRE EXT. RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW21727AE 145326 BOS - FLT 4510 - DURING TAXI OUT, CREW REPORTED THE BAGGAGE SMOKE MASTER WARNING LIGHT ILLUMINATED. CREW DISCHARGED THE BAGGAGE FIRE BOTTLE AND RETURNED TO GATE. MAINTENANCE OPENED THE CARGO DOOR AND NOTICED A STRONG ELECTRICAL ODOR. THE CARGO COMPARTMENT FAN WAS REMOVED AND REPLACED IAW EMB MM. OPEATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE AFTER FIRE BOTTLE WAS REPLACED. (M) 2L72 4F RTT00011AT 20030407000762003040700076SO 2003 4 7 SIMA200305402 120030221A2611 SMOKE DETECTOR EMB 135 EMB135LR 3260305SO CARGO BAY MALFUNCTIONED A F ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SW21727AE 145326 DURING TAXI OUT, CREW RECEIVED BAGGAGE WARNING. CREW VERIFIED NO ACTUAL FIRE PRESENT AND FOLLOWED CHECKLIST AND EXTINGUISHED FIRE BOTTLES. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS AND CARGO SMOKE DETECT TEST SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. FIRE BOTTLES WERE ALSO REPLACED PRIOR TO FLIGHT. (M) 2L72 4F RTT00011AT 20030625001332003062500133NE 2003 6 25 03093403 220030403A720030B310001 ENGINE DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT MALFUNCTIONED A VTZAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA27403FJ5217 3149 DURING CRUISE LT ITT EXCEEDED IN FLIGHT. ENGINE WAS NOT SHUTDOWN. WHEN RETURNING TO CVG, GOT A FLAPS OVERSPEED BY 1 KNOT. WHEN SELECTED FLAPS TO ZERO HE GOT A FLAT CONTROL FAIL. AIRCRAFT LANDED AND EXCEEDED MAX OVER WEIGHT LANDING LIMIT. CREW SHUTDOWN THE ENGINE AFTER LANDING. TAXIED AIRCRAFT TO THE GATE AND DEPLANED AT GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT ENGINE ASSY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030408000752003040800075NM 2003 4 8 03FDEA00383 120030404A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 N00557 CORROSION ON FRAME 950E WL148 LBL18. REMOVED CORROSION ON FRAME BS 950E WL 148 LBL 18 IAW SRM 51-10-1. REMOVED .75 W X 3 L X .012 D. ORIGINAL THICKNESS IS .071. OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 15. 2L73 4F RTA3WE 20030408000842003040800084WP 2003 4 8 03FDEA00393 120030405A2550 ROLLER TRAY DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE CARGO AREA CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25317FE 46835 NR 771 CENTER PIT, STA 1741 AT RBL 45, CARGO ROLLER TRAYS CRACKED BETWEEN OMNI ROLLERS. CLOSING ACTION ON 04/05/03. REMOVED AND REPLACED DAMAGED ROLLER TRACK WITH 60-11325/29 BATCH NR 0000306010. IAW SRM 53-42-01 FIG 13. SRM 51-21-01. 2L73 4F4 F A22WE E23EA 20030401000862003040100086NM 2003 4 1 0300635526 120030305A5414 DOUBLER BOEING757 757251 1384970NM PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01526US 23620 DURING "L" CHECK FOUND CRACK IN RIGHT HAND STRUT SKIN AND INNER DOUBLER OF NR 2 PYLON. REPAIRED PER EA 55-194405. 2L72 4F RTA2NM 20030401000882003040100088NM 2003 4 1 DHL2003746002 120030207A2611 WARNING LIGHT BOEING727 727224 1384076NM NR 1 ILLUMINATED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01746DH 22252 RTO AT 169,300 POUNDS, ZERO AIRSPEED, -2C, 720 PA IN CVG. BRAKE ENERGY NORMAL, AFTER DEICING WHILE IN POSITION ON RUN-WAY WITH 80 PERCENT N1, THE NR 1 SMOKE DETECTOR WARNING LIGHT ILLUMINATED MOMENTARILY PRIOR TO TAKEOFF. REJECTED TAKE-OFF. THE LIGHT EXTINGUISHED WHEN THRUST REDUCED. COMPLETED RTO FLOW CHART REFERRED TO GOM 8.8-2. THE NR 1 SMOKE DETECTOR WARNING LIGHT ILLUMINATED MOMENTARILY. RAN THE MAIN CARGO SMOKE EMERGENCY CHECKLIST AS A PRECAUTION. AIRCRAFT RETURNED TO NORMAL CONFIGURATION. RAN THE MECHANICAL DISCREPANCY FLOW CHART TO COMPLETION. 2L73 4F A3WE 20030401000962003040100096NM 2003 4 1 DHL2003753001 120030305A2510 SEAT BELT BOEING727 727223 1384074NM COCKPIT MALFUNCTIONED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01753DH 22468 UNABLE TO ADJUST CAPTAIN'S SEAT BELT PROPERLY. CAPTAIN'S SEAT BELT OPS CHECKED NORMAL AS REQUIRED. INSPECTED ASSEMBLY PER BMM 25-10-0. 2L73 4F A3WE 20030401000972003040100097NM 2003 4 1 DHL2003754001 120030109A3220 SNUBBER BOEING727 727223 1384074NM NLG LOOSE A DHLAO OTHER JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 SO01754DH 22008 STARTING A CLIMB AT FL250 AND 340 KIAS IN LITE MOD TURBULENCE, NOSE GEAR DOOR LIGHT ILLUMINATED ON FORWARD AND S/O PANEL WITH ASSOCIATED SLIPSTREAM NOISE. AIRCRAFT SLOWED TO 270 KIAS LIGHTS OUT BUT NOISE AND VIBRATION REMAINED AFTER 5 MIN. NOISE/VIBRATION GONE AND AIRCRAFT RETURNED TO NORMAL SPEED. INSPECTED NOSE GEAR DOOR AND LINKAGE. TIGHTENED NOSE WHEEL SNUBBER. ALL PANELS CHECKED GOOD FOR SECURITY. NOSE GEAR DOOR OPERATES NORMAL AND INDICATIONS IAW M/M 32-22-00. 2L73 4F A3WE 20030401001152003040100115WP 2003 4 1 DHL2003804506 120030116A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING CENTER L/E FORMER CRACKED 1 INCH AT STA XFS 483.750 (UPPER). REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030402000132003040200013NM 2003 4 2 03091402 120030401A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27402FJ 3147 DURING PREFLIGHT INSPECTION, MAINTENANCE PERSONNEL RESET EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICEE CREW REPORTED THAT THE CENTER EMERGENCY LIGHT WAS INOPERATIVE. 2H72 4T RTA55NM 20030625001352003062500135NM 2003 6 25 03FDEA00365 120030401A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION ON BS 680 FLOORBEAM, LBL 5 TO LBL 43, WL 208. REMOVED CORROSION, BS 680 FLOORBEAM UPPER CHORD AT NUTPLATE LOCATIONS LBL 5 TO LBL 43. ORIGINAL THICKNESS OF .130 MAX DEPTH OF REMOVAL LBL 27-29 FOUND TO BE .032. OUT OF LIMITS PER B727 SRM 53-10-1. REMOVED STIFFENER AT LBL 25. REMOVED DAMAGED UPPER CHORD FROM LBL 27 TO 29.5. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED PARTS AND FASTENERS WET WITH SEALANT. REINSTALLED STIFFENER AT LBL 25. ALL WORK ACCOMPLISHED IAW B727 SRM 53-10-8 FIG 3 & 51-10-2. 2L73 4F RTA3WE 20030402000482003040200048NM 2003 4 2 2003UALA00325 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT STA 1440 BETWEEN STR 25L AND 26L UPPER FRAME FLANGE DENTED IN TWO AREAS MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20030402000512003040200051NM 2003 4 2 2003UALA00328 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT STA 1480 JUST ABOVE AND BELOW STR 25L FRAME TO FLANGE DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR 2L72 4F4 FRTA2NM E17NE 20030402000602003040200060NM 2003 4 2 2003UALA00337 120030306A5754114W42101 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 1 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 1 SLAT MAJOR REPAIR ACCOMPLISHED. DELAMINATED SKIN REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030403000332003040300033WP 2003 4 3 15HA0358001 120030216A324095409762 BRAKE CVAC 340 340CVAC 242270AWP NR 1 INOPERATIVE A I5HAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL23584E 24 A/C TRANSITIONED FROM THE RUNWAY TO THE TAXIWAY, CREW WAS INFORMED THAT THE LT LANDING GEAR APPEARED TO BE ON FIRE. TAXIED A/C TO A SAFE AREA. FIRE TRUCK WAS DISPATCHED, BUT NO FIRE WAS OBSERVED. MAINT CREW FOUND THE PRESSURE LINE TO NR 1 BRAKE, VERY LOOSE AND AREA COVERED WITH HYDRAULIC FLUID. AFTER INSP, MAINT FOUND NO EVIDENCE OF FIRE DAMAGE. LINE WAS TIGHTENED AND TESTED UNDER PRESSURE AND HYDR SYS RESERVICED. A/C WAS RETURNED TO SERVICE. NR ONE BRAKE WAS REPLACED NEXT DAY THEN DISMANTLED AND INSPECTED TO FIND CAUSE OF FIRE. NOTHING ABNORMAL WAS DISCOVERED. BRAKE WAS REASSEMBLED WITH NEW SEALS AND PUCKS AND RETURNED TO STORES. 2L72 4R 6A6 20030403000412003040300041NM 2003 4 3 AMTA200300256 120030222A3397 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 ROW 37-39 EGRESS FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED TERMINAL TO LAMP ASSEMBLY IAW AMM 33-51-11-3, OP CHECK OK. (M) 2L72 4F RTA2NM 20030403001052003040300105NM 2003 4 3 DL72S030211 120030305A7120 MOUNT BOEING727 727232 1384082NM NR 1 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27523DA 21583 INSPECTION OF THE NR 1 ENGINE FWD MOUNT SUPPORT FITTING ATTACH HOLES PER AD 97-05-08 REVEALED A CRACK INDICATION IN THE HOLE G-LOCATION. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK INDICATION AND AN INSURANCE CUT APPLIED. AN OVERSIZE FASTENER WAS THEN INSTALLED. THE WORK WAS ACCOMPLISHED PER FED-EX S/B 727-5410A01 AND ER/A 384663- 14AD. 2L73 4F A3WE 20030403001112003040300111NM 2003 4 3 DL72S030304 120030331A7830 PROXIMITY SENSOR BOEING727 727225A 1384077NM PWA JT8 JT8D17A 52049NE NR 3 ENGINE T/R OUT OF ADJUST A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO278882Z76535 21579 687354 ON T/O AT APPROX 80 KTS NR 3 REVERSER LIGHT CAME ON. T/O ABORTED. ADJUSTED PROX SWITCH. 2L73 4F4 FRTA3WE E2EA 20030404000272003040400027NM 2003 4 4 DL738030264 120030320A5511185A120111 STRUCTURE BOEING737 737832 13844CFNM ELE STA 30.972 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO273748Y 30489 WHILE ACCOMPLISHING THE REQUIRED ELEVATOR MODS PER AD 2003-03-22, A CLEVIS FITTING ATTACH HOLE WAS COUNTERSUNK ON THE WRONG SURFACE OF THE MATING STRUCTURE. THE HOLE WAS OVERSIZED TO REMOVE THE MAJORITY OF THE COUNTERSINK AND AN OVERSIZE FASTENER INSTALLED WITH A CORRECT COUNTERSINK. THE WORK WAS ACCOMPLISHED PER ER/A 384741-14AD. 2L72 4F RTA16WE 20030404000632003040400063NM 2003 4 4 DL757030257 120030317A2760276002121 ACTUATOR BOEING757 757232 1384965NM NR 12 SPOILER UNSERVICEABLE A DALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO27632DL 23613 UNCOMMANDED ROLL TO THE RIGHT. SPOILER MESSAGE DISPLAYED. REPLACED NR 12 SPOILER PCA. ADJUSTED AND TEST PER AMM. 2L72 4F RTA2NM 20030404001272003040400127NM 2003 4 4 DL767030281 120030327A5754114T411222 WEDGE BOEING767 767232 1385132NM L/E SLAT DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27101DA 22213 SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14. 2L72 4F RTA1NM 20030404001782003040400178 2003 4 4 SWAA030582 420030315A2565D31354 SLIDE BOEING737 7375H4 138449DNM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN CLOSING DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030408001142003040800114NM 2003 4 8 2003UALA00360 120030402A5310 ANGLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 FWD CABIN ANGLE AT STATION 291 STRINGER 10R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ANGLE. 2L72 4F4 FRTA16WE E2GL 20030408001352003040800135NM 2003 4 8 AWXA200300341 120030321A53306545841123 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A .0625 INCH CRACK WAS FOUND ON R-1 DOOR EXTERNAL SKIN AT LOWER AFT CORNER OF LOWER HINGE CUTOUT. MAINTENANCE CUTOUT CRACKED AREA OF R-1 DOOR EXTERNAL SKIN AT LOWER AFT CORNER OF LOWER HINGE CUTOUT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA E.O. 52-00-02. 2L72 4F4 FRTA16WE E2GL 20030408001362003040800136NM 2003 4 8 AWXA200300342 120030403A5320655384420 FLOOR SUPPORT BOEING737 7373G7 138447JNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.8750 INCH CRACK WAS FOUND ON FLOOR BOARD SUPPORT(C) CHANNEL IN AFT CARGO COMPARTMENT BS 727D, RBL 13. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR BOARD TRACK IN AFT CARGO COMPARTMENT BS 727D, RBL 13; FABRICATED A NEW SECTION OF FLOOR BOARD TRACK, A REPAIR PLATE, AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG. 202, PG. 204-205. 2L72 4F4 FRTA16WE E2GL 20030409000082003040900008NM 2003 4 9 AWXA200300351 120030312A57546546431285 SKIN BOEING737 7373S3 1384711NM LT FOREFLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW149253313 23734 DURING C-16 CHECK SEVERAL AREAS OF THE LT OUTBOARD FOREFLAP UPPER SURFACE WERE FOUND DELAMINATED AT THE INBOARD END. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD FOREFLAP IAW BMM 27-51-37, PG. 401-407. 2L72 4F RTA16WE 20030407000262003040700026WP 2003 4 7 ASAA0380093 120030117A532099363680102 ANGLE DOUG DC9 DC983 3022083WP RT MLG WW CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, VERTICAL ANGLE IN RIGHT WHEEL WELL IS CRACKED AT FORWARD INBOARD LOWER CORNER. REPLACED ANGLE PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20030407000272003040700027WP 2003 4 7 ASAA0380094 120030121A5311SR09530057025 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT LOWER FLANGE FRAME CORRODED AT FS 1231. REPLACED DAMAGED SECTION OF FRAME PER SRM 53-03. (M) 2L72 4F RTA6WE 20030407000482003040700048WP 2003 4 7 GTIA030037 120030203A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSBROKEN A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23802NK 53168 FLL - TAILCONE EMERGENCY LIGHTS DO NOT WORK. REPAIRED BROKEN WIRES, OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20030407000822003040700082SO 2003 4 7 SIMA200306402 120030204A532014521725013 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 ABI - A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL HAS CORROSION ON PREVIOUS REPAIR. REMOVED CORRODED SERVICE DOOR SILL AND INSTALLED SERVICEABLE DOOR SILL IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030408000192003040800019WP 2003 4 8 ASAA0380107 120030125A5320991157911 BRACKET DOUG DC9 DC982 3022082WP FUSELAGE FRAME CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OAK - FOUND DURING C-CHECK, FORWARD SERVICE DOOR AFT UPPER CORNER FRAME SUPPORT BRACKET CORRODED. FABRICATED AND REPLACED BRACKET PER SRM 51-30-5, 51-10-3, AND DAC DWG 9911579. (M) 2L72 4F A6WE 20030408000232003040800023EA 2003 4 8 SIMA200300601 120030103A3600 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA NR 1 BLEED DIRTY A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21504AE 10044 DFW - FLT 3873 - SHORTLY AFTER TAKEOFF CREW REPORTED A NR 1 BLEED LEAK WARNING. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS RETURNED TO DFW AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. A LEAK CHECK ON THE BLEED DUCTS FOUND NO DEFECTS. THE LOOP CONNECTION WERE CLEANED AND AN OPERATIONAL CHECK WAS COMPLIED WITH AND NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030408000392003040800039EU 2003 4 8 SIMA200305005 120030215A5414ALCLAD2024Y3 SKIN SAAB SF340 340B 7860101EU LEFT NACELLE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21371AE 340B371 ABI - DURING A MBV INSPECTION, THE LEFT NACELLE INBOARD FILLET AREA WAS FOUND TO BE CHAFED. BLENDED CHAFE. PERFORMED AN EDDY CURRENT INSPECTION OF BLENDED AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM (72LKS 3079, REV 41) 54-10-10 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20030408000792003040800079WP 2003 4 8 03FDEA00387 120030405A5320 PLATE DOUG MD10 MD1010F WP GE CF6 CF66D 30020GL FUSELAGE TORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25393FE 46627 NR 279 FORWARD PIT, BETWEEN FS 920-960 RIGHT CEILING PANEL 2 EA ATTACHED PRESSURE RELIEF DOOR SCREEN PLATES ARE TORN, BENT, ABRADED AND ALSO LAMP CUT-OUT SCRAP PLATE. CLOSING ACTION. 04/05/03. ON BLENDED DAMAGE AREA ON PANELS IAW SRM 53-02-01. NEG MATERIAL LOSS. VENT NR 2 ROUTED TO FAB SHOP. RECEIVED NEW PART FROM FAB ON T/R TZ/3227442. DRILLED MOUNTING HOLES IAW SRM 51-31-01. TREATED IAW SRM 51-31-01. RETURNED TO PARTS RACK. 2L73 4F4 FRTA22WE E23EA 20030410000242003041000024NM 2003 4 10 SWAA030601 120030317A5551181A0161 PIN BOEING737 7377H4 1384404NM LT&RT HORIZ STABCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED 5Y CHECK, FOUND BOTH LT & RT HORIZ STAB AFT LUG UPPER ATTACH PINS CORRODED. REMOVED AND REPLACED ATTACH PINS PER MM. 2L72 4F RTA16WE 20030410000322003041000032WP 2003 4 10 GTIA030086 120030209A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 160-200 RBL 44 HAS CORROSION. REMOVED FLOOR SUPPORT AT STATION 160-200 RBL 44. FABRICATED REPLACEMENT FLOOR SUPPORT. REPLACEMENT FLOOR SUPPORT FS 160-200 RBL 44 TO BE INSTALLED AS W/O B00059 05-N-81. (M) 2L72 4F A6WE 20030410000382003041000038NM 2003 4 10 SWAA030614 120030318A53126516300 BULKHEAD BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 180, WL 180 & LBL 5.25. REPAIRED BULKHEAD WEB PER SWA EA. 2L72 4F A16WE 20030410000432003041000043WP 2003 4 10 GTIA030089 120030206A5310 SHEAR TIE DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND SHEAR TIE ASSEMBLY HAS CORROSION AN GOUGE. FOUND SHEAR TIE TO BE OUT OF LIMITS. FORMED SHEAR TIE. (M) 2L72 4F A6WE 20030410000512003041000051WP 2003 4 10 GTIA030092 120030212A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND CABIN PRESSURE FLOORBOARD RIGHT STATION 265-313 4 EACH RIVETS PULLED THROUGH SKIN AND CRACKED. REMOVED CRACKED SKIN. FABRICATED NEW FLOORBOARD SKIN. INSTALLED NEW SKIN. (M) 2L72 4F A6WE 20030410000522003041000052NM 2003 4 10 SWAA030637 120030320A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20030410000622003041000062NM 2003 4 10 SWAA030643 120030319A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410000862003041000086NM 2003 4 10 SWAA030658 120030323A5310589357 WINDOW POST BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C1 CHECK, FOUND CAPT'S UPPER WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20030410000872003041000087NM 2003 4 10 SWAA030659 120030322A3350100031 LIGHT BOEING737 7373H4 1384600NM CABIN DEFECTIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT ON BULKHEAD ILLEGIBLE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030410000892003041000089NM 2003 4 10 SWAA030661 120030322A5311963820 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 209. REMOVED AND REPLACED RT CHORD PER SRM. 2L72 4F RTA16WE 20030410000992003041000099NM 2003 4 10 SWAA030671 120030321A53126516300 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (7 EA) AT BS 178, BETWEEN LBL 6 & RBL 12. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030410001042003041000104NM 2003 4 10 SWAA030676 120030325A57546573714 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT AFT FASTENERS 17 INCHES FROM OTBD END. REPAIRED SLAT PER SWA EA. 2L72 4F RTA16WE 20030410001052003041000105NM 2003 4 10 SWAA030677 120030324A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, ABOVE STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001272003041000127SO 2003 4 10 SIMA200304804 120030214A5610163500111 WINDSHIELD EMB 145 EMB145 3260210SO COCKPIT FAILED A SIMAA UNSCHED LANDING O OTHER DEDESCENT 1 SW21612AE 145079 ORD - FLT 4212 - DURING FLIGHT, THE CAPTAINS WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030410001312003041000131SO 2003 4 10 SIMA200304809 120030201A531514522463001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 ABI - DURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGE AREA TO COMPLETELY REMOVE THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REPAIR AREA. FABRICATED A U-SHAPED DOUBLER. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-21-10 FIG 207 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030410001442003041000144NM 2003 4 10 SWAA030698 120030326A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT LOWEST FASTENER ON STR 5R. REPAIRED BULKHEAD PER SRM. 2L72 4F RTA16WE 20030410001462003041000146NM 2003 4 10 SWAA030700 120030328A33506104789 BATTERY BOEING737 7372T4 1384492NM CARGO BAY DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHTS INOP AT OVERWING EXIT AND FWD OF AFT CARGO DOOR. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030410001532003041000153NM 2003 4 10 SWAA030707 120030330A531196380 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED 1/4D CHECK, FOUND BOTH LEFT AND RIGHT SIDE CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED BOTH LT/RT SIDE CHORDS PER SWA ACO AND SRM. 2L72 4F RTA16WE 20030404000582003040400058 2003 4 4 DL757030215 420030304A2210 VIDEO DISPLAY BOEING757 757232 1384965NM COCKPIT BURNED A DALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27647DL 24218 F/A REPORTED SMELL IN CABIN AND ORANGE GLOW COMING FROM VIDEO CONTROLLER UNIT. FOUND VIDEO ON LIGHT ARCED AND SHORTED. REPLACED VIDEO ON LIGHT. 2L72 4F RTA2NM 20030404000642003040400064NM 2003 4 4 DL757030263 120030318A5742112N700323 FITTING BOEING757 757232 1384965NM LT WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27612DL 22819 WHILE ACCOMPLISHING THE ENGINE PYLON AND WING MODIFICATIONS REQUIRED BY AD 2000-20-09, 2 ATTACH HOLES FOR THE INBOARD SIDE LOAD FITTING WERE DAMAGED. THE HOLES WERE OVERSIZED TO CLEAN AND ROUND CONDITION AND INSPECTED FOR CRACKS. OVERSIZE BOLTS WERE INSTALLED IN THE HOLES PER ER/A 384569-14AD. 2L72 4F RTA2NM 20030404000722003040400072NM 2003 4 4 DL757030291 120030324A5330143N33203 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27612DL 22819 THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 620 BETWEEN STRINGERS 16L & 17L NEAR AN EXISTING SKIN CUTOUT REPAIR. THE EXISTING REPAIR WAS REMOVED AND UNDERLYING SKIN AND CUTOUT INSPECTED. THE DENT WAS REMOVED WITH A CUTOUT, BOTH AREAS WERE REPAIRED WITH A SINGLE ALUMINUM REPAIR. DOUBLER INSTALLED PER ER/A 384552-14, REV A. 2L72 4F RTA2NM 20030404001292003040400129NM 2003 4 4 DL767030282 120030327A5754114T411221 WEDGE BOEING767 767232 1385132NM L/E SLAT DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27102DA 22214 LEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14. 2L72 4F RTA1NM 20030404001392003040400139NM 2003 4 4 SWAA030449 120030302A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030404001682003040400168NM 2003 4 4 SWAA030564 120030311A3350612825 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED RON, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT INOP AT RT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030404001692003040400169NM 2003 4 4 SWAA030565 120030313A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29342SW 24133 EEPLS SECTION LOOSE. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030404001722003040400172NM 2003 4 4 SWAA030568 120030311A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030404001852003040400185 2003 4 4 SWAA030596 420030314A2565D31354 SLIDE BOEING737 737301 1384611NM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030410001572003041000157NM 2003 4 10 SWAA030711 120030329A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29732SW 27864 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (5 EA) IN AFT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030410001652003041000165EU 2003 4 10 SIMA200304811 120030211A53302024T3 SKIN SAAB SF340 340B 7860101EU FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21371AE 340B371 ABI - DURING AN MBV INSPECTION, THE RIGHT INLET COMPARTMENT INBOARD SIDE CHANNEL WAS FOUND CHAFED BEYOND SRM LIMITS. BLENDED THE CHAFED AREA, NOT EXCEEDING THE PRESENT DEPTH. PERFORMED AN EDDY CURRENT INSPECTION OF BLENDED AREA, NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER AND SHIM. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS005026 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20030410001692003041000169NE 2003 4 10 BTA2003F00001 220030212A7200 ENGINE RKWELLNA265 NA26580 7630108CE GE CF700 CF7002D2 30010NE RIGHT FLAMED OUT E BTAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 GL23382LS 38051 304368B AIRCRAFT IN FLIGHT AT HIGH ALTITUDE (FL410) AIRCRAFT GOT SLOW (APPROXIMATELY 165 KNOTS). RIGHT ENGINE FLAMED OUT. ADVISE ATC THAT WE HAD ENGINE PROBLEM AND REQUEST TO GO DOWN TO FL270 TO RESTART ENGINE. DESCENDED TO FL270 AND RESTARTED ENGINE. NO OTHER ABNORMALITIES OCCURRED DURING BALANCE OF FLIGHT. AFTER AIRCRAFT RETURNED. ENGINE WAS INSPECTED IN INLET, EXHAUST AND ACCESSORY SECTIONS, NO FAULTS FOUND. ENGINE WAS GROUND PERFORMANCE RAN WITH NO FAULTS FOUND. OK FOR RETURN TO SERVICE. NOTE: AN ALTITUDE ACCELERATION TEST WAS PERFORMED ON THIS AIRCRAFT ON 02/27/2003 AND THE RIGHT ENGINE FLAMED OUT AT FL370. AIRCRAFT WAS RESTRICTED TO FL350. 2L72 4F4 F A2WE E7EA 20030410001702003041000170SO 2003 4 10 EEJ2003F00000 120030311A8120LW12277885 WASTEGATE VALVE PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA TURBOCHARGER DAMAGED E EEJAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 NM0727354 1605 317752180 RL292468A ON 3/10/03 PILOT REPORTED RIGHT ENGINE LOST POWER AT ALTITUDE, MANIFOLD PRESSURE DROPS TO 23 INCHES, WASTEGATE VALVE FOUND TO BE DEFORMED AND CRACKED. REPLACED WASTEGATE AND AIRCRAFT CHECKED, OK. 1L72 3O3 O A20SO E14EA 20030410001712003041000171NE 2003 4 10 EGR2003F00001 120030213A6240 CONNECTOR SKRSKYS76 S76C 8143008NE GEARBOX INDICATOCONTAMINATED E EGRAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA17761AF 760524 AT CRUISE FLIGHT (6000 FT) IFR MAIN GEAR BOX PRESSURE LIGHT ON. WATER ON CONNECTOR PLUGS. RETURNED TO AIRPORT, MAINTENANCE CALLED, CLEANED CONNECTOR PLUGS. RETURNED TO SERVICE. 1G72 3U NCH1NE 20030410001732003041000173NE 2003 4 10 EGR2003F00003 120030214A2120 ODOR SKRSKYS76 S76A 8143006NE CABIN DETECTED E EGRAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA17764LF 760264 CREW SMELLED ODOR SIMULAR TO ELECTRICAL BURNING IN CABIN, WHILE CABIN HEATING WAS OPERATING AT LEVEL OFF CRUISE. FLIGHT CANCELLED WITH LANDING MADE AT NEAREST SUITABLE LANDING AREA. CABIN HEATING SYSTEM SWITCHED OFF WHILE AIRCRAFT WAS LANDED TO NEAREST SAFE LANDING AREA, ODOR BEGAN TO DISIPATE DURING MANUVER TO LAND. NORMAL SHUTDOWN, UNEVENTFUL LANDING. COULD NOT DUPLICATE DISCREPANCY. 1G72 3U H1NE 20030821000942003082100094NM 2003 8 21 03FDEA00690 120030507A5510ALC8100 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 HORIZONTAL STAB CENTER BOX RT 31R BORE EXISTING BUSHING REMOVED FOUND SIDEWALL AND BEARING SURFACE WITH CORROSION. REAM BORE TO 1.181 INCH MAX CORROSION STILL PRESENT ON SIDEWALL SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR. 2L73 4F RTA22WE 20030820000322003082000032NM 2003 8 20 03FDEA01125 120030722A3260 ACCESSORY UNIT BOEING727 727200 138407ENM MLG MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25483FE 21465 AFTER TAKEOFF LANDING GEAR LEVER RAISED TO UP POSTION. LANDING GEAR WARNING HORN STAYS ON STEADY WITH RED UNSAFE LIGHTS IN NOSE, LT AND RT LANDING GEAR ANNUNCIATOR. COMPLIED WITH QRH. AFTER 5 MIN IN FLT LIGHTS EXTINGUISHED AND HORN STOPPED. RE-RACKED LANDING GEAR ACCESSORY BOX. MOISTURE FOUND, DRIED OUT. C/W SYS CHECK AND CHECKED GOOD. NOTIFIED MOCC. ALL IAW GMM 32-09-122-5. 2L73 4F RTA3WE 20030820000392003082000039NM 2003 8 20 03FDEA01014 120030626A5753ARC050214 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE INBOARD FOUND CORROSION. SNRM N0613: RT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE INBOARD CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5750-69354 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030820001362003082000136NM 2003 8 20 0301145511 120030619A335020131A POWER SUPPLY BOEING757 757251 1384970NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01511US 23199 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE SEATS 1-32. REPLACED POWER SUPPLY AT DOOR 2R, M732, P/N 2013-1A. 2L72 4F RTA2NM 20030820001412003082000141NM 2003 8 20 CALA0300407 120030724A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT AT STA 328-344, LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 65C33973. 2L72 4F RTA16WE 20030820001862003082000186NM 2003 8 20 2003UALA00561 120030715A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 FUSELAGE SKIN HAS TWO CRACKS COMING FROM E&E COOLING AIR EXHAUST AFT EDGE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030821000312003082100031EU 2003 8 21 03FDEA00911 120030619A5310DRWNOA53772636 DOOR FRAME AIRBUS300 A300B4605R 3930308EU CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 MAINFRAME- FUSELAGE FRAME DENT REPAIR AT FR20A. FACT 19JUN03 11:40 BFM R WORK COMPLIED WITH EA 6-5310-70932 A/C ARRIVED AT MAE WITH AN INCOMING TRACKING ACTION (REF FEDEX EA 6-5310-50593). THE AFFECTED MEMBER IS SHOWN AS ITEM 10 OF AIRBUS A300-600 SRM REF 53-13-13 FIG 203. CLOSING ACTION ON 06/19/2003. 2L72 4F RTA35EU 20030821000332003082100033NM 2003 8 21 03FDEA01061 120030706A5347S4929148S SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 FORWARD CABIN - L1 DOOR ENTRANCE TRACK FOUND CORRODED AT STA 420 - 457. CORROSION BLENDED CARRIED OUT FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1. 2L73 4F RTA22WE 20030821000352003082100035NM 2003 8 21 03FDEA01297 120030807A5753 FITTING DOUG MD11 MD11 3023602NM TE FLAP HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING 2FB FLAP 2FB HINGE FITTING 28 WING SIDE 29 LOWER PIVOT ATTACHMENT BORE HOLE FOUND CORROSION. LT WING O/B FLAP O/B HINGE FITTING ( WING SIDE ) LOWER PIVOT ATTACHMENT HOLE BORE REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030821000992003082100099NM 2003 8 21 03FDEA00818 120030527A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 EXT SKIN IS CRACKED AND BULGED OUTWARD AT BS 700, STR 27 LT. REPAIRED DAMAGED SECTION OF SKIN BS 688 TO BS 714 STR 26 LT PER SRM 53-30-3 FIG 5 AND FED EX EA 7-5330-70412. REMOVED AND REPLACED SHEAR TIE PER SRM 51-20-1, 51-10-2. 2L73 4F RTA3WE 20030821001142003082100114NM 2003 8 21 03FDEA00879 120030616A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 CORROSION (C53-224-06) TOP OF FLOORBEAM BS 328, LBL 40, WL 208. 2L73 4F RTA3WE 20030821001252003082100125NM 2003 8 21 03FDEA00899 120030617A261177401 SMOKE DETECTOR BOEING727 727200 138407ENM CARGO BAY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25212FE 22934 ON T/O CPR PASSING 3000 AGL NR 4 UPPER DECK SMOKE DETECTOR LIGHT ILLUMINATED, MASTER FIRE LIGHT ON GLARESHIELD ILLUMINATED. FIRE WARNING BELL SOUNDED, DOWN LOADED CARGO. CHECKED CARGO FOR DEFECTS, FOUND NO DEFECTS. PRECAUTIONARY CHANGED NR 4 SMOKE DETECTOR P/N 77 40-1, S/N 211 INSTALLED IN NR 4 POSTION IAW 727 MM 26-16-011-4. 2L73 4F RTA3WE 20030821001482003082100148NM 2003 8 21 03FDEA01081 120030709A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 EXTERIOR SKIN HAS DENT AT BS 203 RBL 14 STR 26R. SKIN DENT BS 203, RBL 14, STR 26R OUT OF LIMITS PER SRM 53-30-1. REPAIRED SKIN PER SRM 53-30-3. 2L73 4F RTA3WE 20030821001552003082100155WP 2003 8 21 03FDEA01234 120030810A5753 BUSHING DOUG DC10 DC1030 3023501WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 LEFT INBOARD FLAP - FLAP MOUNTED HINGE BUSHINGS CORRODED. REMOVED AND REPLACED 4EA BUSHINGS IAW CMM 57-52-01 N 2FR. 2L73 4F A22WE 20030821001872003082100187NM 2003 8 21 03FDEA01038 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 AFT CARGO BAY BS 950F FRAME IS DENTED IN 3 PLACES BETWEEN STR 26L AND 25L. REPAIRED FRAME AT BS 950F BETWEEN STRS 25L & 26L PER SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20030821002202003082100220EU 2003 8 21 RAIA00307182 120030703A33506047051 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03561HK 41077 5480-STL- FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY AND POWER SUPPLY. 2L72 4T RTA41NM 20030821002242003082100224EU 2003 8 21 RAIA00307186 120030708A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03565HK 41082 MX-STL- AFT EMERGENCY FLOOR PATH LIGHT INOP. RESECURED CONNECTOR TO PATH LIGHT STRIP. 2L72 4T RTA41NM 20030821002412003082100241EA 2003 8 21 COMA0360352 120030805A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01963CA3128 7127 FLIGHT 5667 FLAPS FAIL MESSAGE. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20030821002442003082100244NM 2003 8 21 UPS03241010 120030711A7830 FAIRING BOEING727 72725C 138400HNM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C ENG NR 3 THRUST REV O/B FAIRING IS CRACKED NEAR FWD SUPPORT BRACKET UPPER EXISTING DOUBLER AT CRACK LOCATION REMOVED IAW SRM 51-30-02. CRACKS TOP DRILLED IAW SRM 78-30-01 0.025 HOLE. HFEC INSP CARRIED ON STOP DRILL IAW B727 NDTM PT 6 51-00-00 FIG 4 RESULT - CRACK CONTAINED. EXISTING DOUBLER RE-INSTALLED IAW SRM 51-30-2. 2L73 4F A3WE 20030821002482003082100248EU 2003 8 21 03FDEA01333 120030818A5315A532753410000 FLOORBEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25684FE 802 MAIN DECK FLOORBEAM AT FRAME 58, 24 INCHES RIGHT OF CENTER, IS CRACKED 3 INCHES DOWN FROM TOP APPROX 1 INCH LONG. REPAIRED IAW FEDEX EA 6-5310-72527. 2L72 4F RTA35EU 20030821002542003082100254WP 2003 8 21 GTIA030595 120030624A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - DENT AT FS 408 BETWEEN LONGERON 29R. REMOVED DAMAGED SKIN BETWEEN L29R TO L29L AND BETWEEN FS 406 TO 409. FABRICATED NEW SKIN FILLER. FABRICATED NEW FINGER DOUBLER. FABRICATED NEW DOUBLER. MATERIAL ID FOR REPAIR STRAP. INSTALLED STRAP FINGER DOUBLER, REPAIR DOUBLER, AND FILLER. (M) 2L72 4F A6WE 20030820001792003082000179NM 2003 8 20 SWAA031745 120030805A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 363, BETWEEN STR 13R AND STR 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030820002012003082000201NM 2003 8 20 03FDEA00967 120030621A5753ARC70561 FITTING DOUG MD11 MD11 3023602NM O/B FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING- O/B FLAP VANE NR 4 FITTING FWD HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-69380 - WINGS - TRAILING EDGE FLAPS - LEFT HAND OUTBOARD FLAP - VANE SUPPORTS - CORROSION REPAIR AND REFURBISHMENT. 2L73 4F RTA22WE 20030821000252003082100025NM 2003 8 21 03FDEA00964 120030624A5510ALC8100 BARREL NUT DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STAB LEFT UPPER FWD PLANK BARREL NUT BORE NR 1L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. HORIZONTAL STAB LEFT UPPER FWD PLANK BARREL NUT BORE NR 1L REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030821000362003082100036WP 2003 8 21 03FDEA01106 120030717A5753 HINGE DOUG DC10 DC1010 3022110WP TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 COMPLY WITH EA 8-5740-70982 LEFT I/B FLAP-HINGE ASSY ATTACHING LUG REWORK. CLOSING ACTION ON 07/17/03, ON N/R S00017. COMPLIED WITH EA NR 8-5740-70982, LEFT I/B FLAP-HINGE ASSY ATTACHING LUG REWORK. 2L73 4F A22WE 20030821000372003082100037WP 2003 8 21 03FDEA00693 120030507A5270 WARNING LIGHT DOUG DC10 DC1010 3022110WP A/C DOOR ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25367FE 46605 IN CRUISE AT FL330 30 MIN AFTER TAKEOFF THE AIR COND DOORS CAUTION LIGHT ILLUMINATED. CABIN PRESS WAS ON SCHED IN STBY MODE. RED TABS RAN, DIVERT TO KMEM. DUPLICATED INTERMITTENT LIGHT AT PACK NR 3 COMPARTMENT DOOR. FOUND PLUG P1-1616 CORRODED. REPLACED PLUG P1-1616 AND SWITCHED S1-255 AND S1-257 REF DC-10 WDM 52-71-02, SWMP AND MM 52-70-07-2. PLUG P1-1617 AND P1-1618, AND SWITCH S1-256 PREVIOUSLY CHANGED. ALL 3 AIR CONDITIONING COMPARTMENT DOOR WARNING SWITCHES CHECK NORMAL REF DC-10 MM 52-70-07-2. 2L73 4F A22WE 20030821000782003082100078NM 2003 8 21 03FDEA00935 120030620A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT HORIZONTAL STAB UPPER AFT PLANK 30L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS. 2L73 4F RTA22WE 20030821001172003082100117EU 2003 8 21 03FDEA00876 120030612A3297 WIRE HARNESS AIRBUS300 A300B4605R 3930308EU NLG FAULTY A FDEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25651FE 728 AFTER TO/ECAM LAND GEAR RETR FAULT BOTH PITCH TRIM LEVERS FAULTED-TRIPPED OFF & WOULD NOT RESET ATS LEVER TRIPPED OFF-WOULD NOT RESET-HAD NO ELECTRIC TRIM ON GEAR EXTENSION, RED INTRANSIT LIGHT ON NOSE GEAR DID NOT ILLUMINATE, GEAR EXTENDED. REMOVED AND REPLACED THE FOLLOWING LOOMS NLG UPPER RIGHT HAND ELECTRICAL HARNESS AND NLG UPPER LEFT HAND ELECTRICAL HARNESS, NLG STRUT ELECTRICAL HARNESS. PERFORMED FULL JACKING AS PER MM CHAPTER 7-11-00-0. ALSO PERFORMED NORMAL EXTENSION AND RETRACTION TEST OF GEARS AS PER MM CHAPTER 32-31-00-5. CYCLED LANDING GEAR 5 TIMES IN THE NR 1 IND POS AND 5 TIMES IN THE NR 2 IND POS. ALL CYCLES NORMAL AND INDICATIONS NORMAL. 2L72 4F RTA35EU 20030821001602003082100160NM 2003 8 21 03FDEA01163 120030723A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT O/B FLAP (FLAP SIDE) I/B HINGE I/B PIVOT HOLE AND I/B PIVOT LUG INNER AND OUTER SURFACES FOUND CORRODED. RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACES REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821002572003082100257WP 2003 8 21 GTIA030597 120030716A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTIA - FOUND CABIN FLOORBOARD AT FS 1271-1338 CTR CORRODED AND BROKEN INSERTS AND BROKEN CORNER/EDGES. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030821002652003082100265WP 2003 8 21 GTIA030592 120030709A5755 FITTING DOUG DC9 DC982 3022082WP SPOILER CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND LEFT OUTBOARD SPOILER TORSION BAR INBOARD FITTING HAS CORROSION. REMOVED FITTING. LOCATED AND DRILLED NEW ORDERED TORSION BAR FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20030821002752003082100275NM 2003 8 21 USAABB03125 120030728A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19619AU 27198 TPA - FOUND THE FLOOR PROXIMITY EMERGENCY EXIT LIGHT AT SEAT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030821002832003082100283NM 2003 8 21 AT0300019 120030705A33506011779 BATTERY PACK BOEING717 717200 1383700NM CABIN DISCHARGED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15953AT 55015 OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-125 OPS CHECK GOOD. 2L72 4F TRA6WE 20030821002842003082100284NM 2003 8 21 AT0300023 120030809A33508039251 BATTERY PACK BOEING717 717200 1383700NM CABIN DISCHARGED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15977AT 55036 EMERGENCY LIGHTS OUT IN FORWARD CABIN, AT L-1 DOOR AND R1 DOOR. REMOVED AND REPLACED 35-118 BATTERY PACK OPS CHECK GOOD. 2L72 4F TRA6WE 20030822000242003082200024NM 2003 8 22 03FDEA01247 120030803A5712ARB2850502 RIB DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING 2316 SLAT TRACK INBOARD RIB FOUND CRACK 2C LENGTH OF CRACK APPROX 0.5 22. RT WING NR 16 SLAT TRACK INBOARD RIB REMOVED AND NEW RIB INSTALLED AS PER SRM 51-35-01 VOL. II AND SRM 51-33-00 VOL. II. 2L73 4F RTA22WE 20030822000342003082200034NM 2003 8 22 03FDEA01047 120030705A2742418575 TRIM MOTOR DOUG MD11 MD11 3023602NM HORIZ STAB CONTAMINATED A FDEAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO25587FE2280022800 48489 UPON APPLICATION OF POWER UP FOR TAKEOFF THE STABILIZER MOVED FROM 7.3 TO 5.4. AFTER REJECTED TAKEOFF WHILE ON TAXIWAY STABILIZER, RESET TO 7.3. UPON SUBSEQUENCY TAXI THE STAB MOVED BY ITSELF TO 9.2 AND THEN BACK TO ABOUT 5. T/S AND FOUND NR 2 TRIM MOTOR C/P RECEPTICAL FULL OF WATER AND C/P P1-1924, ALSO FULL OF WATER, DUE PREVIOULSLY BADLY ASSEMBLED. REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR, POSITION NR 2, IN REFERENCE TO REMOVED AND REPLACED CANNON PLUG P1-1924 ON NR 2 TRIM MOTOR PER MD11 WDM 22-22-01. 2L73 4F RTA22WE 20030822000352003082200035NM 2003 8 22 03FDEA01082 120030710A26121014A FIRE DETECTOR BOEING727 727200 138407ENM APU FAILED A FDEAF ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SO25477FE 21394 TEN MIN AFTER TAKEOFF THE RED LIGHT IN THE APU FIRE SHUTOFF HANDLE ILLUMINATED. THERE WAS NO RINGING OF THE FIRE BELL IN ACCORDANCE WITH QRH. THE APU FIRE HANDLE WAS PULLED AND APU BOTTLE DISCHARGE BUTTON PUSHED. THE RED LIGHT IN THE APU FIRE HANDLE REMAINED ILLUMINATED. EGT WAS 100C WHEN THE LIGHT CAME ON AND SLOWLY DECREASED DURING THE FLIGHT. *S/D* REPLACED APU FIRE & OVERHEAT DETECTION POWER UNIT MM. 2L73 4F RTA3WE 20030822000442003082200044NM 2003 8 22 2003UALA00520 120030625A3297BR20AXH5V3 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NLG PULLED A UALAK NONE N FALSE WARNING CLCLIMB 1 WP29328UA 24148 UPON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT (RED) CAME ON. FOUND WIRE 328-201-24R PULLED OUT OF SPLICE SP374. REPLACED SPLICE SP374, SP376 AND LATCHING RELAY R374. 2L72 4F4 FRTA16WE E2GL 20030822000582003082200058NM 2003 8 22 03FDEA01188 120030725A5744ARC0502505 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORRODED. LEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DRAWING ARC0502 SHT 4. 2L73 4F RTA22WE 20030822000652003082200065NM 2003 8 22 UPS03441101 120030723A531365B07658182 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RT TUNNEL STA 320 - STA 340 STRINGER 42 FOUND CRACKED. STRINGER REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20030822000702003082200070NM 2003 8 22 2003UALA00516 120030617A5754114N300333 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29546UA 25367 NR 5 SLAT T/E WEDGE LOWER SKIN DELAMINATED. REPLACED 100 PERCENT OF UPPER & LOWER SKIN OF THE T/E WEDGE. 2L72 4F4 FRTA2NM E17NE 20030822000862003082200086NE 2003 8 22 CALA0300386 220030713A7200 ENGINE BOEING757 757224 1384958NM RROYCERB211 RB211535E4 54555NE NR 2 SHUTDOWN A CALAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 SW2758101 27291 31320 THE NR 2 ENGINE AUTO SHUTDOWN WITH OIL LOSS AND OIL PRESSURE DROP WHILE EN ROUTE FROM LIM TO EWR. THE AIRCRAFT DIVERTED TO MBJ WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. INVESTIGATION CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE SHUTDOWN WAS DUE TO FAILURE OF RADIAL DRIVE BEARING. 2L72 4F4 FRTA2NM E12EU 20030822000872003082200087NM 2003 8 22 CALA0300387 120030714A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND A .5 INCH CRACK IN RT MAIN FRAME ANGLE AT STA 616 FLOOR LINE. A STIFFENING ANGLE REPAIR WAS INSTALLED IAW ECRA 5311-01157. 2L72 4F RTA16WE 20030822000922003082200092SO 2003 8 22 RAIA00306179 120030629A335078241 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03803HK 145077 MX-PIT- EMERGENCY LIGHT INOP AT LT EMERGENCY EXIT. REMOVED AND REPLACED EMERGENCY LIGHT AT EXIT. 2L72 4F RTT00011AT 20030331000442003033100044WP 2003 3 31 AALA20030192 120030212A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21456AA 49561 DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN AFT ACCESSORY COMPARTMENT INOPERATIVE. RESEATED EMEGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000902003033100090SO 2003 3 31 C2XA03SH075 120030329A532014524131009 SUPPORT BRACKET EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE PASSENGER DOOR THRESHOLD SUPPORTS WHERE FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT BRACKETS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000912003033100091SO 2003 3 31 C2XA03SH076 120030330A531013500322001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE LT SILL BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000922003033100092SO 2003 3 31 C2XA03SH077 120030330A531014522460015 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE LT BUTT STRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331001042003033100104EA 2003 3 31 COMA0360166 120030326A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01937CA 7044 FLIGHT 5214, 1ST SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. SECURED WIRING CONNECTOR ON FLOOR STRIP LIGHTING. 2L72 4F RTA21EA 20030401000492003040100049EA 2003 4 1 CA030219003 120030218A2932ACA3581D71 CHECK VALVE CNDAIRCL600 CL600* EA LYC ALF502ALF502L2C NE HYD SYSTEM INADEQUATE W K NONE N FALSE WARNING ININSP/MAINT 1 CA (CAN) NR 2 HYDRAULIC MANIFOLD EDP (ENGINE DRIVEN PUMP) CHECK VALVE BACKS OUT, O-RING AND BACKUP RING SHEAR ALLOWING PRESSURE INTO THE EDP PRESSURE SWITCH WHEN THE ELECTRIC PUMP IS ON AND ENGINE IS SHUT DOWN. RECURRING DEFECT DUE TO IMPROPER LOCKING DEVICE ON THE CHECK VALVE. MFG FIELD SERVICE REP. NOTIFIED. NO ACTION TAKEN BY MANUFATURER. 2L72 4F4 FRTA21EA E6NE 20030401001272003040100127WP 2003 4 1 DHL2003804519 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 653.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001432003040100143WP 2003 4 1 DHL2003804552 120030212A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING T/E UPPER SKIN SURFACE WITH 1/2 INCH CRACK IN IT. (XRS285.000-305.000) CUT OUT DAMAGED AREA IAW SRM57-2-0 FIG. 2 FABRICATED FILLER (2024T3,032) & DOUBLER (2024T3.050) IAW SRM57-2-0 FIG. 2. CLEANED , TREATED AND PRIMED FILLER & DOUBLER INNER SURFACE IAW SRM51-1-8B INSTALLED FILLER AND DOUBLER IAW SRM 57-2-0 FIG2 , SRM51-1-21 PG. 1 2L74 4F RT4A25 20030401001502003040100150WP 2003 4 1 DHL2003804660 120030228A57303889713 PANEL DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING LOWER SKIN SURFACE HAS 1.5 INCH CRACK AT STA XRS 455.000, BETWEEN S-63L AND S-64-L PERFORMED MAJOR REPAIR IAW EO DHL 030115, ED-3216 , REMOVED FASTNERS IAW IAW SRM 512-1-20D PG. 21 TRIMMED OUTDAMAGED SKIN SEGMENT IAW EO DHL 030115 , ED-3216. FABRICATED REPAIR DOUBLER (7075T6AL 0.100) & TRIPLER (7075T6AL 0.125) & FILLER (7075 T6 AL 0.211) & SHIM (7075T6AL 0.025)IAW EO DHL 030115 , ED-3126. CLEANED TREATED AND PRIMED INNER SURFACE OF REPAIR DOUBLER , TRIPLER , FILLER, SHIM , SHIM. IAW SRM 51-1-8B APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG. 1 INSTALLED DOUBLER , TRIPLER , FILLER , SHIM WITH NEW FASTNERS IAW EO DHL 030115, ED-3216, SRM51-1-20D PG. 9 FOR LEAK CHECK SEE N/R 2591 2L74 4F RT4A25 20030402000212003040200021EU 2003 4 2 0300653226 120030331A2121 FAN AIRBUS320 A320211 3930320EU E/E BAY BURNED OUT A NWAAA UNSCHED LANDING EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01326US 282 DURING CRUISE EXPERIENCED RUMBLING/VIBRATION SEEMING TO COME FROM AVIONICS COMPARTMENT. ALSO EXPERIENCED ELECTRICAL BURING ODOR (NO SMOKE). DIVERTED TO BHM AND LANDED UNEVENTFULLY. VERIFIED AVIONICS BLOWER FAN FAULTY AND APPLIED MEL PROVISIONS. RAN PACK AND VERIFIED ABSENCE OF ODOR AND SMOKE. RETURNED A/C TO SERVICE. 2L72 4F RTA28NM 20030402000272003040200027NM 2003 4 2 2003UALA00212 120030226A282260721011 PUMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUEL BOOST DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29199UA7154 28717 A/C RECEIVED RT-STAB FUEL PUMP EICAS INDICATION. RT HST TRANSFER PUMP FAILED TO OPERATE. THIS A/C WAS OPERATING UNDER THE CERTIFICATE LIMITATIONS OF AD 2002-24-52 AMOC LETTER 140S-02-384 DATED 12/6/02. THIS LIMITATION DID NOT ALLOW THE CREW TO SELECT THE LT TX PUMP ON WHEN THE RT PUMP FAILED. A FLIGHT MANUAL BULLETIN WAS ADOPTED TO ALLOW THE CREW TO SELECT THE LT PUMP ON IF THE RH PUMP FAILS. THE PUMP SENSE PORT THREADS WERE STRIPPED. IT IS UNLIKELY THAT THIS CAUSED THE EICAS MESSAGE WITHOUT CREATING A LARGE FUEL LEAK. IT PASSED THE BENCH CHECKS AND STATOR X-RAY INSPECTION. 2L74 4F4 FRTA20WE E24NE 20030402000332003040200033NM 2003 4 2 2003UALA00308 120030322A7830 RELAY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE ISOLATION VALVE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29669UA 30025 A/C RECEIVED REVERSER ISOLATION VALVE INDICATION BEFORE ETOPS ENTRY POINT. THE REV ISLN VLV LIGHT IS INHIBITED IN FLIGHT. THE ONLY SINGLE FAILURE THAT WOULD CAUSE THIS MESSAGE IN FLIGHT IS FAILURE OF K10359 OR K206 RELAYS, REF WDM 78-36-21 PG 4 SH 1. THESE RELAYS WERE REPLACED ALONG WITH THE PRESSURE SWITCHES AND ANOTHER RELAY. A CONTRIBUTING FACTOR FOR THIS TURNBACK WAS THE A/C FLIGHT MANUAL 7-26 FOR IRREGULARS GIVES A CAUTION THAT ADDITIONAL SYSTEM FAILURE MAY CAUSE INFLIGHT DEPLOYMENT. THIS IS NO LONGER TRUE WITH THE CHANGES MADE DURING SYNC LOCK INST. THIS CAUTION IS GOING TO BE CHANGED TO REFLECT CHANGES POST SYNC LOCK INSTALLATION. 2L72 4F4 FRTA1NM E24NE 20030402000522003040200052NM 2003 4 2 2003UALA00329 120030326A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 867, STR 9R FUSELAGE FRAME WEB CRACKED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT, DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030402000652003040200065NM 2003 4 2 2003UALA00342 120030301A5754114W423012 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 12 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 T/E WEDGE DELAMINATED - NR 12 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030402000682003040200068NM 2003 4 2 2003UALA00345 120030314A5754114W416021 WEDGE BOEING777 777222 1385219NM NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29206UA 30212 T/E WEDGE DELAMINATED - NR 6 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. 2L72 4F RTT0001SE 20030408000732003040800073NM 2003 4 8 03FDEA00372 120030402A3220 BUSHING BOEING727 727200 138407ENM ZONE 700 MISSING A FDEAO OTHER J WARNING INDICATION CRCRUISE 1 SO25484FE 21466 TEST FLIGHT. UPON RAISING LANDING GEAR, NOSE GEAR RED LIGHT AND RED DOOR LIGHT STAYED ON. AIR CREW COULD HEAR SOMETHING STILL IN AIRSTREAM. LOG BOOK ENTRY REQ. UPON FURTHER INVESTIGATION, FOUND BUSHING FROM LOCK & POSITION SWITCH CONTROL ARM TO BE MISSING. INSTALLED BUSHING IN CONTROL ARM. PERFORMED OPERATIONAL TEST ON NLG IAW FED-EX M/M 32-61-071-5. FUNCTIONAL CHECKED GOOD. 2L73 4F RTA3WE 20030403000712003040300071SO 2003 4 3 C2XA03BT046 120030320A7500 O-RING EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A C2XAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW2714940 145033 CREW REPORTED, "BLEED NR 2 LEAK IN FLIGHT" CREW PREFORMED PRECAUTIONARY ENGINE SHUTDOWN. MAINTENANCE FOUND LEAKING FAN AIR VALVE THERMOSTAT O-RINGS, REMOVED AND REPLACED FAN AIR VALVE THERMOSTAT O-RINGS. OPS.CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030403000882003040300088 2003 4 3 COMA0360168 420030325A2210 CLUTCH CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT OUT OF TOLERANCEA COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01915CA7490 7013 FLIGHT 5847 A/P TRIM CAUTION MESSAGE - AILERONS FELT NOTICABLE STIFF. COULD NOT DUPLICATE DISCREPANCY, FOUND THE AUTO PILOT SERVO SLIP-CLUTCH OUT OF TOLERANCE, ADJUSTED SLIP CLUTCH TO PROPER VALVE. 2L72 4F RTA21EA 20030403000912003040300091EA 2003 4 3 COMA0360172 120030330A2621385000183 BOTTLE CNDAIRCL600 CL6002B19 1900309EA FIRE EXTING DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA11696 7241 FLIGHT 5198 CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLES. 2L72 4F RTA21EA 20030403001002003040300100NM 2003 4 3 DL72S030143 120030211A5522 SKIN BOEING727 727232 1384082NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27410DA 21222 UPPER SKIN OF LT ELEVATOR WAS FOUND WITH OVERSIZED COUNTER SINKS IN ATTACHMENT HOLES COMMON TO THE REAR SPAR. REPAIR PER ER/A 417786-14AD. 2L73 4F A3WE 20030403001042003040300104 2003 4 3 DL72S030208 420030303A3421344003685 INDICATOR BOEING727 727225A 1384077NM COCKPIT MALFUNCTIONED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27805EA 22436 CAPTS ATTITUDE INDICATOR INTERMITTENT. ROLLS TO 45/90 DEGS WITH AFF FAIL FLAG AND A COMPARITOR ROLL LIGHT. REPLACED CAPTS ADI AND VG PER M/M. SYS CHECKS NORMAL. 2L73 4F RTA3WE 20030403001092003040300109NM 2003 4 3 DL72S030279 120030326A5753 FAIRING BOEING727 727225A 1384077NM RT WING LOOSE A DALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO278882Z 21579 AT FL300 SPEED .78/285KTS THE AIRCRAFT HAD MODERATE TO SEVERE VIBRATION IN AIRCRAFT AND CONTROLS. FOUND INBOARD RT FLAP ELEPHANT EAR AND CANOE LOOSE. REPAIRED SAME. 2L73 4F RTA3WE 20030403001162003040300116NM 2003 4 3 DL733030081 120030123A2530255001852 COFFEEMAKER BOEING737 737347 1384647NM 2L AFT GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27306WA 23347 FLT ATTENDANT VERBAL REPORT, LT AFT GALLEY COFFEEMAKER HAS ELECTRIC ODOR. REPLACED COFFEEMAKER, OPS CHECK NORMAL. NO ODOR. 2L72 4F RTA16WE 20030403001172003040300117NM 2003 4 3 DL733030088 120030124A33500201820001 LIGHT BOEING737 7373B7 1384580NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27952WP 23378 EMERGENCY LIGHT ASSY IS BROKEN BY THE R-1 DOOR. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS NORMAL. 2L72 4F RTA16WE 20030403001272003040300127NM 2003 4 3 DL733030275 120030324A33500201991008 LIGHT BOEING737 7373B7 1384580NM 24 DEF DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27951WP 22951 FOUND CABIN EMERGENCY EXIT LIGHT INOP AT SEAT 24DEF. REPLACED WIRE CONNECTORS AT LIGHT ASSY. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20030404000292003040400029NM 2003 4 4 DL73K030117 120030130A5330654576988 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27379DL 23606 THE FUSELAGE SKIN AT FS 480 WAS GOUGED AND CRACKED BY GROUND EQUIPMENT JUST BELOW THE STRINGER 26R SKIN LAP JOINT. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384498-14. 2L72 4F A16WE 20030404000432003040400043NM 2003 4 4 DL73S030191 120030224A7120 SUPPORT FITTING BOEING737 737232 1384475NM ENGINE MOUNT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 FWD ENGINE MOUNT SUPPORT FITTING ASSY WAS FOUND WITH O/S MOUNT HOLES. REPAIR PER ER/A 422119-14AD. 2L72 4F RTA16WE 20030404000442003040400044NM 2003 4 4 DL757030067 120030116A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27618DL 22908 FLT ATTENDANTS REPORTED AN ODOR SIMILAR TO HOT PLASTIC IN THE REAR OF THE AFT CABIN THAT THE APPARENT CAUSE OF HEADACHES FOR SEVERAL PASSENGERS AND FLT ATTENDANTS. AIRCRAFT WAS IN CRUISE. ANTI ICE WAS NOT IN USE. ODOR DID NOT INCREASE WHEN USING ANTI ICE IN DESCENT. OPERATED AIR CONDITION SYSTEM FOR 30 MINS. COULD NOT DUPLICATE ANY SMELL OR ODOR. 2L72 4F RTA2NM 20030404000472003040400047NM 2003 4 4 DL757030101 120030128A2560 PLACARD BOEING757 757232 1384965NM CABIN WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27693DL 29725 THE 3 RT RAFT SURVIVAL KIT HAS DIRECTIONS PLACARDS THAT IS HARD TO READ. REMOVED AND REPLACED 3 RIGHT SURVIVAL KIT. 2L72 4F RTA2NM 20030404000482003040400048NM 2003 4 4 DL757030115 120030128A5330143N347111 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27685DA 27588 THE FUSELAGE SKIN WAS GOUGED BY TOOLING AT FS 500, JUST BELOW THE STRINGER 26R SKIN LAP JOINT. THE GOUGE WAS REMOVED FROM THE SKIN WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384441-14, REV A. 2L72 4F RTA2NM 20030404000672003040400067NM 2003 4 4 DL757030276 120030322A5330141N32312 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27614DL 22821 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 405 NEAR STRINGER 22L. THE DENT WAS REMOVED WITH A 4 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS INSTALLED PER ER/A 384744-14. 2L72 4F RTA2NM 20030404000772003040400077NM 2003 4 4 DL764030159 120030215A2400 GCU BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 2 ENGINE INOPERATIVE A DALAD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 SO27838MH6741 29711 706239 ON LT ENG SHUT DOWN LOST ALL ELECTRICAL POWER ON A/C WITH RT ENGINE STILL RUNNING. REPLACED RT GCU. A/C FAULT OCCURRED ON PUSHBACK. 2L72 4F4 FRTA1NM E23EA 20030404001162003040400116NM 2003 4 4 ASAA0310007 120030111A335007912 LIGHT BOEING737 737290C 138448VNM ROW 17 INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - FOUND EMERGENCY EXIT LIGHTS AT ROW 17 INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 17, THEN LIGHT TESTED NORMAL. (M) 2L72 4F A16WE 20030404001182003040400118WP 2003 4 4 ASAA0380078 120030115A33500105606 LIGHT DOUG DC9 DC983 3022083WP FWD CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01950AS 53023 SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING AT ROW 2 WAS FOUND 'PULLED INOP'. REPAIRED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030404001322003040400132NM 2003 4 4 DL767030285 120030327A5754114T411320 WEDGE BOEING767 767232 1385132NM L/E SLAT DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27105DA 22217 RIGHT WING SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14. 2L72 4F RTA1NM 20030404001382003040400138NE 2003 4 4 SWAA030421 220030221A7250 TURBINE BOEING737 7372H4 138448CNM PWA JT8 JT8D9 52048NE NR 1 ENGINE FAILED A SWAAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW29089SW 22904 687795 AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB EXPERIENCED NR 1 ENG HIGH EGT IND, REDUCED PWR TO NR 1 ENG. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 F A16WE E2EA 20030404001462003040400146NM 2003 4 4 SWAA030496 120030305A335065C27095 BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN RT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030404001482003040400148NM 2003 4 4 SWAA030503 120030305A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED RON, FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20030404001562003040400156NM 2003 4 4 SWAA030539 120030308A32116546113 TRUNNION PIN BOEING737 7373K2 13844BANM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED A1 CHECK, SWA SI 11251-32, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030404001622003040400162NM 2003 4 4 SWAA030552 120030311A3350BR2013 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP FROM ROW NR 16 TO AFT GALLEY. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20030404001672003040400167NM 2003 4 4 SWAA030559 120030311A53126516300 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 207 & RBL 15. REPAIRED WEB PER SRM. 2L72 4F A16WE 20030404001742003040400174NM 2003 4 4 SWAA030572 120030313A575565C2525A51A SPOILER BOEING737 7373T5 1384608NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED C2 CHECK, FOUND NR 0 GROUND SPOILER DELAMINATED AT ACTUATOR ATTACH POINT. REMOVED AND REPLACED NR 0 GROUND SPOILER PER MM. 2L72 4F RTA16WE 20030404001752003040400175NM 2003 4 4 SWAA030574 120030313A52306547952524 DOOR FRAME BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED (3 EA) AT PULLEY SUPPORT BRACKET MOUNT. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20030404001762003040400176 2003 4 4 SWAA030578 420030313A2565D31354 SLIDE BOEING737 7372H4 138448CNM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F A16WE 20030404001842003040400184NM 2003 4 4 SWAA030595 120030317A335020131A BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED PM CHECK, FOUND EEPLS INOP IN AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030407000092003040700009WP 2003 4 7 ASAA0380062 120030109A532059360331 MOUNT DOUG DC9 DC983 3022083WP ANTENNA CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, ANTENNA MOUNTING CORRODED AND PITTED AT FS 1127. BLENDED CORROSION. ALTHOUGH BEYOND LIMITS, WAS ACCEPTED PER EA 5330-01612 AND BAC TLX AOC-OKC-02-00166H. (M) 2L72 4F RTA6WE 20030407000182003040700018WP 2003 4 7 ASAA0380073 120030112A5311SR09530057625 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, FRAME CORRODED IN AFT CARGO BAY. REPLACED FRAME SEGMENT PER SRM 51-30-2 AND 51-30-5. (M) 2L72 4F RTA6WE 20030407000382003040700038WP 2003 4 7 GTIA030023 120030124A3260 SENSOR DOUG DC9 DC981 3022081WP LT MLG DOOR MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23805NK 48058 SJU - FLT 770 - APPROXIMATELY 25 MINUTES AFTER TAKEOFF, GEAR DOOR OPEN LIGHT ILLUMINATED AND REMAINED ON FOR 10 MINUTES, THEN WENT OUT. REMOVED AND REPLACED LEFT LANDING GEAR DOOR SENSOR. OPS CHECK GOOD. (M) 2L72 4F A6WE 20030407000412003040700041WP 2003 4 7 GTIA030027 120030113A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND FLOOR PANEL STATION 332-370 IS DELAMINATED. FABRICATED REPLACEMENT PANEL. (M) 2L72 4F RTA6WE 20030328000332003032800033 2003 3 28 BSAA030231 420030205A344506650012704 INDICATOR SWRNGNSA227 SA227AC 8780603SW TCAS FAILED G BSAAO OTHER O OTHER DEDESCENT 1 SW15430MA AC710B NR 1 VSI FAILED DURING DESCENT. CREW LANDED WITH NO FURTHER INCIDENT AFTER DECLARING EMERGENCY. REPLACED VSI/TCAS INDICATOR, SYSTEM TEST GOOD. 2L72 4T RTA8SW 20030328000492003032800049SO 2003 3 28 C2XA03TY040 120030326A531014522460015 GUSSET EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 DURING A SCHEDULED INSPECTION THE OMEGA BEAM GUSSET WAS FOUND TO HAVE SEVERAL AREA OF CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM GUSSET AT FRAME 20 IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030328000942003032800094SO 2003 3 28 CX2A03RI001 120030113A3231 RELAY EMB 145 EMB145LR 3260212SO MLG FAILED A C2XAO OTHER P NO WARNING INDICATION DEDESCENT 1 SW2713988 145265 BDL-FLT 2150 CREW REPORTED DURING DESCENT AT 250 KTS, SOUNDED AS THOUGH NOSE GEAR DOORS OPENED, NO OTHER INDICATIONS. MAINTENANCE REMOVED AND REPLACED RELAY K0642 LANDING GEAR CONTROL RELAY, PERFORMED SATISFACTORY OPERATIONAL TESTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331001292003033100129NM 2003 3 31 DHL2003740510 120030204A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH FUSELAGE FRAME AT STA 1090 BETWEEN STR 16R AND 17R HAS DENT AND ELONGATED HOLE. CUT OUT DAMAGED AREA PER SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER (7075-T6-.090) PER SRM 51-10-2. TREATED, PRIMED AND PAINTED AREA PER SRM 51-10-2. INSTALLED REPAIR PER SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20030331001312003033100131NM 2003 3 31 DHL2003740512 120030202A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CABIN BS 1166 FRAME CRACKED AND BENT 3 INCHES ABOVE FLOOR STRINGER 17 L. CUT OUT DAMAGED AREA 2 X 1.5 INCH, FABRICATED DOUBLER (7075-T6 .090) PER SRM 51-40-3 FIG 1. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51-30-2. 2L73 4F RTA3WE 20030401000102003040100010EA 2003 4 1 03090671 120030331A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27671BR 7572 DURING MAINTENANCE INSPECTION, THE RT NR 1 EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030401000392003040100039NE 2003 4 1 AWXA200300326 220030329A7230AC67926 BLEED VALVE BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE ZONE 420 FAILED A AWXAC ABORTED TAKEOFF AJ FLAME/FIRE WARNING INDICATION TOTAKEOFF 1 WP28905AW519709942 23567 30560 ON TAKEOFF FROM PHX EN ROUTE FOR LAX AS THROTTLES ADVANCED HEARD A LOUD BANG, REJECTED TAKEOFF DUE TO POSSIBLE NR 2 ENGINE COMPRESSOR STALL. PAX ALSO REPORTED SEEING FLAMES COMING OUT REAR OF ENGINE. MAINT PERFORMED ENGINE SURGE PROCEDURES AND BORESCOPED THE NR 2 ENGINE. NO DEFECTS WERE NOTED. PERFORMED COMPRESSOR AIRFLOW CONTROL TEST NR 3 PER T/C F5M72603. NR 2 ENGINE HIGH PRESSURE (HP) BLEED VALVE FAILED TO OPEN AND CLOSE PER SCHEDULE TABLE 1, COND. A & C. REMOVED AND REPLACED HP2 BLEED VALVE IAW BMM 75-32-04. HP2 BLEED SOLENOID SHOWED EVIDENCE OF CONTAMINATION SO IT WAS ALSO REMOVED AND REPLACED IAW BMM 75-32-05. BLEW OUT LINES AND RE-ACCOMPLISHED TEST NR , SYS OPERATES NORMALLY. PART 2L72 4F4 FRTA2NM A12EU 20030401000432003040100043SO 2003 4 1 C2XA03SH079 120030331A531014522460015 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 SHV-DURING C-CHECK THE AFT FLOORBEAM BUTT STRAP WAS FOUND TO HAVE A GOUGE AT FRAME 18 CENTER LINE. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030401000852003040100085NE 2003 4 1 2003F00169 220030401A72300319257000 DIFFUSER UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE ENGINE CRACKED A O OTHER O OTHER NRNOT REPORTED 1 SW09120TL1709 1141 34152 COMPRESSOR STALLS DEVELOP AS DIFFUSER VANES DETERIORATE. BORESCOPE INSPECTION REVEALS 7 OUT OF 10 ENGINES IN FLEET HAVE 1 OR MORE DIFFUSER VANES CRACKED OR PARTIALLY MISSING. THIS ENGINE REMOVED DUE TO COMPRESSOR SURGE/ STALL EVENTS AND DIFFUSER VANE CRACKS BEYOND MANUFACTURER'S SERVICEABILITY CRITERIA. 1G72 3U3 UNCR0001RD E34NE 20030401001402003040100140WP 2003 4 1 DHL2003804548 120030208A575457696003 STRUCTURE DOUG DC8 DC873F 302199FWP LT WING LE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT OUTER WING LEADING EDGE SHOWS ELONGATED HOLES, STA XW 485.000 PERFORMED MAJOR REPAIR IAW E.O. DHL030107, ED-3207. REMOVED SKIN SEGMENT IAW EO DHL 030107, ED-3207. FABRICATED DOUBLER (7075T6AL0.063 IAW EO DHL 030107 , ED - 3207. CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACESIAW SRM51-1-15 PG. 1 INSTALEED DOUBLER IN LH OUTER WING L/E WITH NEW FASTNERS IAW EODHL030107, ED-3207 & SRM51-1-21 PG 1. 2L74 4F RT4A25 20030401001452003040100145WP 2003 4 1 DHL2003804555 120030209A57545769589504 STRUCTURE DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING CTR L/E UPPER PART CORRODED, STA. XW 257.000-XFS329.000 PERFORMED MAJOR REPAIR IAW EO DHL 030106 , ED-3212. REMOVED FASTNERS IAW 51-1-21 PG1 REMOVED CORROSION ON RT WING CTR L/E UPPERPART SRM51-18 PAGE 17-18. FOUND OUT OF LIMITS IAW SRM57-2-0 PAGE PG. 16 FABRICATED A REPAIR DOUBLER (7075T6AL.071) AND FILLER (7075T6AL.063) IAW EO DHL030106, ED-3212. CLEANED, TREATED, AND PRIMED INNER SURFACE IAW SRM51-1-8B , APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG1 , INSTALLED FILLER + DOUBLER AT RT. WING CTR. L/E UPPERPART (STA. XW257.000 - XFS329.000) USING NEW FASTNER IAW EO DHL030106 , ED-3212 & SRM51-1-21 PG.1 2L74 4F RT4A25 20030401001692003040100169WP 2003 4 1 DHL2003804779 120030217A573056110171 PANEL DOUG DC8 DC873F 302199FWP LT WING TE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING T/E LOWER PANEL EXTERNAL SKIN DELAMINATED 5.000 INCH AT STA. XW106.000. R & R LT WING T/E LOWER PANEL IAW SRM 51-3-0 2L74 4F RT4A25 20030401001702003040100170WP 2003 4 1 DHL2003804780 120030214A573056110012 PANEL DOUG DC8 DC873F 302199FWP RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA. XW5.000-32.000. R & R RT WING T/E UPPER PANEL IAW SRM 51-3-0 PG. 1. 2L74 4F RT4A25 20030403000282003040300028NM 2003 4 3 03FDEA00362 120030401A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION ON FLOORBEAM, STA 620, RBL 11, WL 208 (FASTENER HOLE). REMOVED CORROSION ON FLOORBEAM BS 620 RBL 11 WL 208 IN AN AREA OF 1 X 1 X .019 FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE FABRICATED REPAIR PARTS DRILLED, ALODINED, PRIMED AND INSTALLED REPAIR ALL WORK ACCOMPLISHED IAW SRM 51-30-2, 53- 10-1 FIG 4, 53-10-8 FIG 8 AND MM 51-20-151-7. 2L73 4F RTA3WE 20030402000572003040200057NM 2003 4 2 2003UALA00334 120030327A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 FUSELAGE STA 807 BETWEEN STR 27R AND 27L - SKIN IS CREASED. STA 817, STR 26L - SKIN IS DENTED. STA 807 BETWEEN STR 27R AND 25R - SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED. THREE DAMAGED AREAS CUT OUT, ONE LARGE DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030402000742003040200074NM 2003 4 2 AMTA200300238 120030218A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11524AT 30233 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 5 SLAT POWER SUPPLY IAW MM 33-51-07-2. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030403000802003040300080NM 2003 4 3 CALA0300153 120030328A5532 SKIN BOEING737 7373T0 1384582NM VERTICAL STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE SKIN DENTED AT L/E STA 132.92 + 6 AND AT 226.54 + 1.3. THE DENTED AREAS WERE REPAIRED IAW SRM 55-30-01, FIGURE 203. 2L72 4F RTA16WE 20030403000832003040300083NM 2003 4 3 CALA0300156 120030331A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 312 AND 320, R-1 DOOR THRESHOLD. REPAIRED WITH REPLACEMENT PART IAW SRM 51-40-02. 2L72 4F RTA16WE 20030403000852003040300085NM 2003 4 3 CALA0300158 120030401A3397 WIRE BOEING757 757224 1384958NM R4 EXIT SIGN CHAFED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914118 27560 THE R-4 DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE DURING TEST WHILE IN "C" CHECK. MAINTENANCE FOUND EMERGENCY EXIT SIGN WIRING HAD CHAFING DAMAGE AND A BLOWN FUSE AT EMERGENCY LIGHTS POWER SUPPLY M736. THE WIRING WAS REPAIRED IAW BOEING STANDARD WIRING PRACTICES MANUAL 20-61-11. THE FUSE WAS REPLACED AND TESTING WAS SATISFACTORY IAW MM 33-51-07. 2L72 4F RTA2NM 20030403000892003040300089EA 2003 4 3 COMA0360170 120030329A325016650101 TILLER CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO01932CA15767 7038 FLIGHT 5427 NOSE WHEEL STEERING FAILED DURING T/O. REPLACED THE STEERING TILLER. 2L72 4F RTA21EA 20030408000122003040800012WP 2003 4 8 ASAA0380086 120030114A5347S292235714400 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY TIEDOWN TRACK IS CORRODED AROUND FASTENER HOLES. REPLACED TRACK PER SRM 51-10-4 AND 51-30-1. (M) 2L72 4F RTA6WE 20030408000152003040800015WP 2003 4 8 ASAA0380102 120030123A53475936663501 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OAK - FOUND DURING C-CHECK, TIEDOWN TRACK FLOR MOUNT HOLES ARE CORRODED IN AFT CARGO BAY. REPLACED TIEDOWN TRACK PER SRM 51-30-2 AND 51-10-4. (M) 2L72 4F RTA6WE 20030408000272003040800027SO 2003 4 8 SIMA200302005 120030118A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21731BE 145356 EWR - FLT 4503 - DURING PREFLIGHT, CREW REPORTED ALL THE EMERGENCY LIGHTS TO BE INOPERATIVE. AIRCRAFT WAS INSPECTED AND FERRIED TO BOS FOR REPAIR. MAINTENANCE COLD NOT DUPLICATE DISCREPANCY AFTER AIRCRAFT LANDED IN BOS. SUSPECT BATTERIES CHARGED DURING FLIGHT. NO PARTS WERE CHANGED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030408000352003040800035SO 2003 4 8 SIMA200304101 120030205A335020131A BATTERY EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21830AE 145615 CVG - CREW REPORTED WHEN POWER WAS REMOVED FROM AIRCRAFT THE EMERGENCY LIGHTS STAYED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY IAW EMB AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030408000412003040800041EA 2003 4 8 SIMA200330602 120030104A2781 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA FLAP/SLATS FALSE INDICATIONA SIMAO OTHER N FALSE WARNING DEDESCENT 1 SW21501BG 10017 BOI - FLT 3901 - DUIRNG DESCENT, CREW REPORTED A SLAT FAULT MESSAGE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. VISUAL INSPECTION OF SLATS/FLAPS AND AN OPERATIONAL CHECK WAS COMPLIED WITH. NO DEFECTS WERE REPORTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030408000482003040800048NM 2003 4 8 USAABB03026 120030226A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19602AU 22196 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030408000502003040800050NE 2003 4 8 USAASA03019 220030223A7200 ENGINE AIRBUSA319 A319112 3930323EU CFMINTCFM56 CFM565B5 NE NR 2 MALFUNCTIONED A EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19703UW 0904 779418 SJU - FLT 8910 - EN ROUTE SJU-CLT, ON CLIMB-OUT OF SJU, CREW RECEIVED ECAM MESSAGE 'ENG 2 FUEL CTL FAULT' AND 'ENG 2 N2 OVER LIMIT'. THE CREW SHUT DOWN THE NR 2 ENGIEN AND RETUREND TO SJU. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 18 MINUTES. MAINTENANCE REPLACED THE NR 2 ENGINE. OPERATIONALLY CHECKS OK. (M) 2L72 4F4 FRTA28NM E37NE 20030328000782003032800078NM 2003 3 28 CH1A200393007 120030323A7931 INDICATOR BOEING727 727212 138407GNM NR 3 ENGINE MALFUNCTIONED A C1HAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL15293AS 21348 AFTER TAKE OFF NR 3 ENGINE OIL QUANITY GAUGE DROPPED FROM 3 1/2 DOWN TO 0. PRESSURE REMAINED 45 PSI 2L73 4F A3WE 20030821000472003082100047NM 2003 8 21 03FDEA01024 120030627A5744ARC050311 FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING (WING SIDE) - OUTBOARD T/E FLAP, OUTBOARD HINGE FITTING FOUND HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORRODED. LEFT WING (WING SIDE) - OUTBOARD T/E FLAP, OUTBOARD HINGE FITTING HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORROSION REPAIR IAW FEDEX EA 1-5750- 69356 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030821000482003082100048NM 2003 8 21 03FDEA01025 120030627A5753ARC198413 FITTING DOUG MD11 MD11 3023602NM TE FLAP HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING (FLAP SIDE) - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE OUTBOARD SIDE CORRODED. LEFT WING (FLAP SIDE) - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING PIVOT BEARING MOUNT HOLE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1- 5750-69352 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000492003082100049NM 2003 8 21 03FDEA01060 120030704A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO FLOOR SEAT TRACK CRACKED AT STA 695, LBL 27.5. REPAIR CARRIED-OUT AT MAIN DECK CARGO FLOOR SEAT TRACK BETWEEN STA 680 AND STA 745 IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20030821000582003082100058NM 2003 8 21 03FDEA01196 120030801A2612894120 FIRE LOOP BOEING727 727200 138407ENM NR 1 ENGINE FALSE INDICATIONA FDEAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 SO25281FE 22348 ENGINE FIRE LIGHT (DASHBOARD AND FIRE HANDLE) NUMBER 1 ENGINE ILLUMINATED MOMENTARILY INFLIGHT ON APPROACH (APPROX 11,000FT AND 300K), ACCOMPANIED BY FIRE BELL. LIGHT AND BELL WENT OUT, FIRE TEST CHECK OK, ALL ENGINE INDICATIONS NORMAL. APPROXIMATELY 3 MINUTES LATER, NR 1 FIRE LIGHT AND BELL CAME ON AGAIN AND WENT OFF BY ITSELF IN ONE SECOND, FIRE TESTED OK AGAIN, ALL INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION ELEMENT PER AMM 26-11-012-01. TESTED FIRE DETECTION SYSTEM PER AMM 26-11-001-0, NO FAULTS NOTED. SYSTEM OPS CKS NORMAL. 2L73 4F RTA3WE 20030821000592003082100059WP 2003 8 21 03FDEA01197 120030801A5311 SPLICE DOUG DC10 DC1030 3023501WP FRAME CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 LEFT MLG WHEEL, AFT END, OUTBOARD WALL, FRAME REPAIR IS CRACKED. CLOSING ACTION ON 07/19/03. FOUND CRACK IN FRAME REPAIR. REMOVED IAW SRM 53-33-01 FAB NEW SPLICE IAW GMM 7-0-1-001 SECTION 3C FROM 7070-T6 .125C. INSTALLED NEW SPLICE IAW SRM 31-33-01. 2L73 4F A22WE 20030821000642003082100064NM 2003 8 21 03FDEA00927 120030617A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT BORE FOUND CORROSION. RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT BORE REPAIRED AS PER FEDEX EA 1-5750-69372 TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000722003082100072NM 2003 8 21 03FDEA00937 120030620A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25487FE 21490 CORROSION AFT CARGO BAY STA 950D STR 29 LT SHEAR TIE HAS CORROSION. REPAIRED SHEAR TIE AT BS 950D STR 29 LT IAW FED EX EA 7-5310-54855. 2L73 4F RTA3WE 20030821000752003082100075NM 2003 8 21 03FDEA01054 120030702A5753ARC199114 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT LUG LOOSE BUSHING. REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030819002112003081900211NM 2003 8 19 UPS03241008 120030717A5754 SKIN BOEING727 72725C 138400HNM NR 4 KRUEGER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, SMALL CRACK 1 INCH IN LENGHT ON TAI SKIN OF NR 4 KREUGER FLAP, JUST I/B OF ACTUATOR ROD END ATTACH POINT ON FLAP. RECTIFICATION CARRIED OUT IAW UPS EO B727-5750-3082. 2L73 4F A3WE 20030819002142003081900214 2003 8 19 SWAA031769 420030806A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030820000212003082000021NM 2003 8 20 03FDEA00901 120030616A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 SNRM N0516 - MAIN DECK CABIN: STA Y635, X0 FOUND SEAT TRACK CRACKED. SNRM N0516 - DAMAGED SEAT TRACK AT STA Y635; X0 SPLICED AND REPAIRED BETWEEN STA Y625 AND STA Y665 PER SRM 53-70-00 VOL I. 2L73 4F RTA22WE 20030820000492003082000049EU 2003 8 20 03FDEA00889 120030616A5710 CLIP AIRBUS300 A300B4605R 3930308EU LT WING PANEL BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 LT WING PANEL 572LB END CLIP IS BROKEN. REMOVED AND REPLACED CLIP IAW SRM 51-40-21 ON N00595 AT MAE. 2L72 4F RTA35EU 20030820000662003082000066NM 2003 8 20 03FDEA01109 120030718A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 CORROSION ON SHEAR TIE AFT SIDE BS 1130, BETWEEN STR 29 AND 28 LT. REMOVED CORROSION ON SHEAR TIE AFT SIDE 2.20 X 1.80 X .007 INCH MAX, IAW SRM 51-10-6. ORIGINAL MATERIAL .050, OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR SHEAR TIE OF 7075 T6 .050 LOT 504450 PER SRM 51-10-3, SRM 51-20-1, SRM 51-30-5, ALODINED PER SRM 51-10-2 PAR 3G, PRIMED, PAINTED AND INSTALLED IAW FED-EX MM 51-20-151-7 SEC 5-8 AND SRM 51-30-2 SEC 4. 2L73 4F RTA3WE 20030820001382003082000138NM 2003 8 20 CALA0300404 120030724A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND FLOOR SUPPORTS AT STA 344-360 BL 0 AND LBL 10 CRACKED. THE CRACKS WERE .5 INCH AND 4 INCH. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND DRAWING 65C33970-53. 2L72 4F RTA16WE 20030820002272003082000227EA 2003 8 20 ASOA03309 120030715A26114462534 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11701EV 10020 DURING TAKEOFF FROM MGM-ATL, THE CREW RECEIVED AN AFT LAVATORY SMOKE MESSAGE. NO SMOKE OCCURRED IN THE AIRCRAFT. THE AIRCRAFT RETURNED TO MGM AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE AFT LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030820002312003082000231NM 2003 8 20 USAASB03095 120030628A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US 23935 MAINTENANCE REPORTED THE AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERAITONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030820002332003082000233EA 2003 8 20 ASOA03320 120030715A5210601R31903319 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE ADJUSTED THE LATCH MECHANISM DOOR LINKAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030820002422003082000242EA 2003 8 20 ASOA03316 120030717A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030821001082003082100108NM 2003 8 21 03FDEA01182 120030731A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 RT KEEL BEAM UPPER FLANGE INSIDE APU CUTOUT STA 873 RBL 6 CRACKED. REPAIRED CRACKED RT KEEL BEAM UPPER FLANGE AT BS 873 PER EA 7-5310-54931. 2L73 4F RTA3WE 20030821001152003082100115NM 2003 8 21 03FDEA00877 120030616A5330 SKIN BOEING727 727200 138407ENM FUSELAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25487FE 21490 EXTERIOR SKIN, LIGHTNING STRIKE BS 355, .5 INCH BELOW STRINGER 21 LT. 2L73 4F RTA3WE 20030821001272003082100127EU 2003 8 21 03FDEA00896 120030616A7830491B1313032006 ANGLE AIRBUS300 A300B4605R 3930308EU THRUST REVERSER CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 NR 1 ENG OUTBOARD T/R LWR FWD CLOSE OUT PANEL AFT ANGLE CHAFED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-21 PG 7. 2L72 4F RTA35EU 20030821001412003082100141NM 2003 8 21 03FDEA00886 120030616A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 CORROSION (C53-113-01, 2) BULGING SKIN ON STR 28L, BS 1055. 2L73 4F RTA3WE 20030821001442003082100144NM 2003 8 21 03FDEA00884 120030616A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 CORROSION ON INTERIOR SIDE OF SKIN AT BS 664, RBL 4 TO LBL 4. 2L73 4F RTA3WE 20030821001492003082100149WP 2003 8 21 03FDEA01236 120030810A5753ARC0154 HINGE BRACKET DOUG DC10 DC1030 3023501WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 FLAP HINGE BRACKET LOWER O5 CB BOLT HOLE BORE PITTED ENT BY 3A 484466 RPT BY 3A 484466. FACT 04AUG03 05 3A45 BFM COMPLIED WITH EA 8-5740-70995 WINGS - LT INBOARD FLAP 2C HINGE ASSY ATTACH LUG REWORK 40 MAE NT BY 3A 39014C RPT BY3A 39014C. 2L73 4F A22WE 20030821001692003082100169NM 2003 8 21 03FDEA01031 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 FRAME DENTED BS 500 STR 22R. FRAME AT BS 500, STR 22R DENT OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F RTA3WE 20030821001712003082100171NM 2003 8 21 03FDEA01033 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 FRAME DENTED BS 540 STR 24L. CUT OUT DENTED SECTION OF FRAME STR 24L BS 540 2.2 X 1 X .050 INCH. FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-3. 2L73 4F RTA3WE 20030821001722003082100172NM 2003 8 21 03FDEA01034 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 FRAME DENTED BS 560 STR 22L TO 24L. REMOVED DAMAGED AREA OF DENTED FRAME BS 560, STR 22L TO 24L. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PART. ALL IAW SRM 53-10-1 FIG 1, 51-40-3 FIG 1, 51-20-04 PGS 3 AND 4, FED EX MM 51-20-000-7. 2L73 4F RTA3WE 20030821001742003082100174NM 2003 8 21 03FDEA01036 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 AFT CARGO BAY BS 990 FRAME IS DENTED AT STR 26L. REPAIRED FRAME AT BS 990, STR 26L PER SRM 51-40-3, FIG 1. 2L73 4F RTA3WE 20030821001752003082100175NM 2003 8 21 03FDEA01128 120030721A5753ARB0029507N HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD SIDE LINK FOUND CRACKED. CRACKED O/B SIDE LINK FITTING OF LEFT WING O/B FLAP I/B HINGE FITTING REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20030821001812003082100181WP 2003 8 21 03FDEA01272 120030812A1430716584 BOLT DOUG DC10 DC1010 3022110WP NR 1 PYLON LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO2510060 46970 NR 1 PYLON, TOP PYLON COVER PLATE (AFT OF FWD PYLON MT TO AFT PYLON TO WING MT), BOLTS ARE LOOSE. 2L73 4F A22WE 20030821002272003082100227WP 2003 8 21 0301179929 120030623A27805919526508 DUCT DOUG DC9 DC931 3022065WP LT & RT WINGS LACK OF LUBE A NWAAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL018923E 45838 DURING SLAT EXTENSION ROLL, SLAT DISAGREEMENT ANNUNCIATOR STAYED ON. COMPLIED WITH COM PROCEDURE AND SLATS RETRACTED NORMALLY. AN UNEVENTFUL LANDING WAS MADE AT MKE. MAINTENANCE INSPECTED THE SLAT SYSTEM BUT FOUND NO DEFECTS AND COULD NOT DUPLICATE THE PROBLEM AFTER 15 SLAT EXTENSIONS. THE T-DUCT WAS LUBRICATED AND SYSTEM WAS DEFERRED FOR 5 CYCLES. BOTH LEFT AND RIGHT T-DUCTS WERE REPLACED BY 27JUN03. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030820001212003082000121NM 2003 8 20 QXEA200300930 120030729A6120 CONNECTOR DHAV DHC8 DHC8202 2809007NM ZONE 400 LOOSE A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09359PH 514 ON FLIGHT 2141 ABORTED TAKEOFF DUE TO AUTOFEATHER FAILED TO ARM ON TAKEOFF. POWER LEVERS WERE BROUGHT UP EVEN, ALTHOUGH NR 1 TORQUE LAGGED BY 15 TO 20 PERCENT. THEN BOTH TORQUE'S WERE ABLE TO REACH 80 PERCENT BEFORE THE AUTOFEATHER FAILED TO ARM. REINSTALLED LOOSE NR 1 HBOV SERVO CONNECTOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030820001222003082000122NM 2003 8 20 QXEA200300929 120030729A21203045593 VALVE DHAV DHC8 DHC8202 2809007NM ZONE 100 MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09359PH 514 PDX- ON FLIGHT 2128 BLEED AIR TO FLIGHT DECK SMELLS OF VAPORIZED OIL. REMOVED AND REPLACED P2.5/P3 SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030820001292003082000129NM 2003 8 20 CALA0300429 120030731A5730 PANEL BOEING737 7373T0 1384582NM LT WING DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND LT WING O/B TRAILING EDGE PANEL DELAMINATED. A NEW PANEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030820001942003082000194NM 2003 8 20 03229430 120030817A3350221262183 CONTROL PANEL DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27430FJ 3209 DURING PREFLIGHT INSPECTION THE CREW DISCOVERED THE EMERGENCY LIGHTS WOULD NOT TURN ON. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FLIGHT ATTENDANT LIGHTING PANEL. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030820002142003082000214EA 2003 8 20 ASOA03311 120030715A531560034017739 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DUIRNG HANGAR MAINTENANCE AT CKB, THE FLOORBEAM ON THE PILOTS BULKHEAD AT FS 280, LBL AND RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRD THE FLOORBEAM ON THE PILOTS BULKHEAD AT FS 280, LBL AND RBL 9 IAW ASA EO 600-53-0090. (M) 2L72 4F RTA21EA 20030820002392003082000239EA 2003 8 20 ASOA03317 120030718A5210601R31903319 LATCH CNDAIRCL600 CL6002B19 1900309EA CABIN LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO UNLOCK. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE AND LINKAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030820002402003082000240EA 2003 8 20 ASOA03312 120030715A5320601R35031239 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621, WL 73, RBL AND LBL 40 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621, WL 73, RBL AND LBL 50 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20030821000232003082100023NM 2003 8 21 03FDEA00966 120030621A5753ARC70531 VANE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING- O/B FLAP VANE MOST I/B FITTING FWD HOLE FOUND CORROSION. LEFT WING- O/B FLAP VANE MOST I/B FITTING FWD HOLE REWORK AS PER DWG ARC 7053. BUSHING FABRICATED AS PER FEDEX EA 1-5750-69380, WINGS- TRAILING EDGE FLAPS- LEFT HAND OUTBOARD FLAP- VANE SUPPORTS- CORROSION REPAIR AND REFURBISHMENT. 2L73 4F RTA22WE 20030821000602003082100060NM 2003 8 21 03FDEA01201 120030801A5754 BUSHING BOEING727 727200 138407ENM NR 2 L/E FLAP WORN A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25268FE 21674 AFTER RETRACTING FLAPS TO 2 THE RED L/E ANNUNCIATOR LIGHT REMAINED ILLUMINATED. POSITION TEST SHOWED NR 2 L/E FLAP INTRANSIT. RED TABS COMPLETED AND LIGHT WENT OUT, AFTER 1 MIN RED L/E FLAPS LIGHT ILLUMINATED AGAIN (WITH FLAPS IN THE UP POSITION). RED TABS REINITIATED AND A/C RETURNED TO MEM. TROUBLESHOT THE 2 WIRES AND ASSOCIATED COMPONENTS BETWEEN C/P AT FLAP 2 POS SW, S203, AND LEADING EDGE FLAP POS TEST MODULE, M119, W/MULTIMETER. ALL RINGS NORMAL AND NOT SHORTED TO GND. REF FX727 WDM 27-81-01 AND 27-81-02. REMOVED AND REPLACED WORN BUSHING ON THE NR 2 L/E FLAP SWITCH LINKAGE PER AMM 27-82-001-4. OPS CHECK NORMAL, NO ADJUSTMENT NECESSARY. 2L73 4F RTA3WE 20030821000632003082100063NM 2003 8 21 03FDEA00928 120030619A5511 SPAR CAP DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STAB LT UPPER SPAR CAP 36L BARREL NUT BORE CORROSION FOUND BEYOND EO 1-5510-7-5000 B PT1 LIMITATION. HORIZONTAL STAB LT UPPER SPAR CAP 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030821001062003082100106NM 2003 8 21 03FDEA01183 120030731A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 DENT IN FUSELAGE SKIN BS 1336 ABOVE STR 17R. DENT IN FUSELAGE SKIN BS 1336 ABOVE STR 17R WAS FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. CUT OUT DAMAGE AS PER SRM 53-30-3. FABRICATED REPAIR DOUBLER. ALODINED & PRIMED PER SRM 53-30-3 AND INSTALLED PER SRM 53-30-3. 2L73 4F RTA3WE 20030821001852003082100185NM 2003 8 21 03FDEA01037 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 AFT CARGO BAY BS 970 FRAME IS DENTED AT STR 26L AND 25L AND 23L. REPAIRED FRAME AT BS 970, STR 25L - 26L AND STR 23L PER SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20030821002022003082100202NM 2003 8 21 03FDEA01039 120030617A1430ARC2715509 STUD DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING - O/B FLAP I/B HINGE UPPER I/B STUD FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-69379 - WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAPS - INBOARD FLAP SUPPORT, UPPER INBOARD STUD BOLT - REPAIR AND INTERIM USE. 2L73 4F RTA22WE 20030821002642003082100264WP 2003 8 21 GTIA030594 120030721A5321 CHANNEL DOUG DC9 DC982 3022082WP FLOOBOARD DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN FLOORBOARD AT FS 1250-1309 LEFT OUTBOARD BOTH 'HAT' CHANNELS DISBONDED. RE-BONDED 2 EACH HAT CHANNELS ON FLOORBOARD. (M) 2L72 4F A6WE 20030821002712003082100271WP 2003 8 21 GTIA030585 120030630A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - AFT PIT CORROSION AT FS 1271 LONGERON 26R. FOUND .25 INCH CRACK ON STRAP. FABRICATED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030821002732003082100273NM 2003 8 21 USAASB03109 120030714A335020131A BATTERY PACK BOEING737 7373B7 1384580NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19523AU 23858 PHL - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT GALLEY CEILING. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030821002772003082100277NM 2003 8 21 USAASB03110 120030716A335020131A POWER SUPPLY BOEING737 7373B7 1384580NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19517AU 23703 CLT - FOUND AFT SECTION OF AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) 2L72 4F RTA16WE 20030821002812003082100281WP 2003 8 21 GTIA030587 120030630A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND RIGHT AFT LAVATORY FLOOR STATION 1338 STRINGER 18 CORRODED. REMOVED 9 HI-LOCKS AND 1 GUSSET. FABRICATED NEW GUSSET. FOUND FRAME AT FS 1338 AND 18R TO BE CORRODED BEYOND LIMITS. FABRICATED NEW FRAME REPAIR SECTION, AND FABRICATED SPLICE SECTION. CUT OFF DAMAGED SECTION OF FRAME. INSTALLED NEW FRAME SECTION AND REPAIR SPLICE. INSTALLED GUSSET. (M) 2L72 4F A6WE 20030821002852003082100285WP 2003 8 21 AT0300020 120030709A3397 WIRE DOUG DC9 DC932 3022066WP CABIN DAMAGED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15833AT 47489 ONE SET OF EMERGENCY LIGHTS NEAR AFT WALKING IS INOPERATIVE. REPAIRED WIRE TO CONNECTOR OPS CHECK GOOD IAW DC-9 MM 20-50. 2L72 4F A6WE 20030821002872003082100287NM 2003 8 21 AT0300022 120030803A33508039491 POWER SUPPLY BOEING717 717200 1383700NM CABIN DISCHARGED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15974AT 55034 CHECKED OPERATIONAL OF THE AIRCRAFT EMERGENCY LIGHTING SYSTEM, PER SERVICE CHECK. EMERGENCY EXIT SIGNS ABOVE EXIT DOORS AT ROW 22 FED AND 22 CA DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY FOR EMERGENCY EXIT SIGNS ABOVE EXIT DOORS 22 FED AND 22 CA. PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEMS. OPERATIONAL TEST GOOD, IAW BOEING 717 AMM 33-51. NO DEFECTS NOTED AT THIS TIME. 2L72 4F TRA6WE 20030821002922003082100292EU 2003 8 21 03213330 120030731A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27330UE 41098 DURING MAINTENANCE INSPECTION, FWD EMERGENCY TRACK LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL RESECURED THE CONNECTOR, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTA41NM 20030822000152003082200015NM 2003 8 22 03FDEA01345 120030810A5753 RIB DOUG MD11 MD11 3023602NM T/E FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LEFT WING I/B TRAILING EDGE FLAP VANE TRACK NR 1 & 3 STRUCTURE RIB SURFACE FOUND CHAFED MARKS. CHAFED MARK ON LT WING I/B T/E FLAP VANE TRACK NR 1 & 3 STRUCTURE RIB SURFACE AREA SMOOTHEN OUT AND FOUND WITH IN LIMIT AS PER SRM 57-00-01 FIG. 1A VOL. 1. 2L73 4F RTA22WE 20030822000482003082200048CE 2003 8 22 DXTA200300053 120030626A326065430087 POSITION SWITCH CESSNA500 560CESSNA 2076750CE LT MLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07334QS 5600434 LEFT MAIN LANDING GEAR WOULD NOT COME UP DURING GEAR RETRACTION. TROUBLESHOT SYSTEM FOUND TO BE INTERMITTENT LEFT MAIN GEAR UPLOCK SWITCH. REMOVED AND REPLACED SWITCH WITH NEW, OPERATIONAL CHECK GOOD, ALL WORK DONE IAW CITATION 560 MM CHAPTER 32-61-00. 2L72 4F RTA22CE 20030328000852003032800085EA 2003 3 28 COMA0360067 120030131A5530600210615 BUSHING CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01989CA12093 7215 THE LT VERTICAL STABILIZER LUG BUSHING WAS MIGRATED .025 INCH AT THE HORIZONTAL STABILIZER PIVOT POINT. REMOVED THE MIGRATED BUSHING. PERFORMED NDT/LP1 TO ENSURE NO DAMAGE TO LUG BORE. MACHINED AND INSTALLED A 1ST OVERSIZED BUSHING I/A/W REO 601R-55-31-044. 2L72 4F RTA21EA 20030328001022003032800102CE 2003 3 28 DBC2003F00001 120030225A3260H1113071 UPLOCK SWITCH CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP LT MLG FAILED E DBCAO OTHER N FALSE WARNING CLCLIMB 1 GL1316SU 6500025 AFTER DEPARTING PBI PILOT SELECTED LANDING GEAR UP. LANDING GEAR RETRACTED AND HANDLE IN-TRANSIT LIGHT EXTINGUISHED. A COUPLE OF SECONDS LATER, LANDING GEAR HANDLE IN TRANSIT LIGHT ILLUMINATED FOLLOWED BY IN TRANSIT LIGHT EXTINGUISHING AND LEFT MAIN DOWN AND LOCKED LIGHT ILLUMINATING. PILOTS SELECTED GEAR DOWN AND RETURNED TO PBI. LANDING GEAR WAS UNEVENTFUL. AIRCRAFT WAS PLACED ON JACKS AND A RETRACTION TEST WAS PERFORMED. IT WAS DETERMINED THE UPLOCK SWITCH HAD FAILED WHICH PREVENTED SOLENOID VALVE FROM OPENING AND APPLYING HYDRAULIC PRESSURE TO UPLOCK ACTUATOR. UPLOCK SWITCH REPLACED. OPERATIONS CHECKED GOOD. 2L72 4F4 F A9NM E6WE 20030331001352003033100135NM 2003 3 31 DHL2003740516 120030204A5311 FRAME BOEING737 7372Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH UPPER MAIN DECK CARGO DOOR FUSELAGE FRAME 480 CRACKED FWD SIDE WHERE ATTACHED TO FUSELAGE SKIN. CUT OUT DAMAGED FLANGE AND FABBED REPAIR FROM 7075-T6 AND FILLER FROM 7075-T6 .050 PER SRM 53-10-4 FIG 11. PARTS TREATED AND DRILLED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-4 AND 51-30-2. 2L72 4F A16WE 20030401000182003040100018WP 2003 4 1 AALA20030219 120030220A3350P4010049 BATTERY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21438AA 49456 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 12-17 AISLE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030401000372003040100037NM 2003 4 1 AWXA200300324 120030328A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 8 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28151AW 23219 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030401000452003040100045SO 2003 4 1 C2XA03SH081 120030331A533014527605003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK SKIN WAS FOUND GOUGED UNDER GPU ACCESS PANEL BETWEEN FRAMES 6 AND 8. MAINTENACE REMOVED DAMAGE AND REPAIRED SKIN IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030401000942003040100094NM 2003 4 1 DHL2003751004 120030131A2612 FIRE DETECTOR BOEING727 727264 138408MNM NR 1 ENGINE INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 NR 1 ENGINE FIRE DETECTION A-SYSTEM INOP. NR 1 ENGINE FIRE DETECTION A-SYSTEM MAYBE INOP AND DEFERRED PER MEL 26-6. ASSIGNED DMI 11822 PLACARD INSTALLED. REF DMI 11822 NR 1 ENGINE FIRE DETECTION A-SYSTEM INOP. REF DMI 11822 NR 1 ENGINE FIRE DETECTION A-SYSTEM TESTED IAW M/M 26-11-0. OPS CHECKED NORMAL. NO DEFECTS NOTED. THIS ACTION CLEARS DMI 11822. PLACARDS REMOVED. 2L73 4F A3WE 20030401001032003040100103NM 2003 4 1 DHL2003782001 120030318A2611 CONNECTOR BOEING727 727227 1384078NM SMOKE DETECTOR DIRTY A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01769AT 21998 MAIN CARGO SMOKE DETECTION SYSTEM NR 2 LIGHT FLASHES WHEN TEST SWITCH PRESSED. CLEANED AND RESEATED CONNECTOR PLUG. OPS CHECKED GOOD IAW M/M 26-17-01. 2L73 4F A3WE 20030401001612003040100161WP 2003 4 1 DHL2003804770 120030122A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 MAIN CARGO TRACK WORN IN VARIOUS LOCATIONS . CUT OUT DAMAGED TRACKS IAW SRM 53-2-3 PG 17 , CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW PLUGS AND CHANNEL OR INSTALLED NEW TRACK SECTION IAW SRM 53-2-3 PG. 49-50 2L74 4F RT4A25 20030328000792003032800079NE 2003 3 28 CH1A200395008 220030324A7200 ENGINE BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 2 MALFUNCTIONED A C1HAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 GL15295AS 22147 688229 TAKE OFF ROLL, ENGINES WERE SPOOLED TO 1.4 EPR BRAKES WERE RELEASED AND EPR POWER WAS ABOUT 1.8 WHEN A DIFINITE LOUD VIBRATION WAS HEARD AND FELT. NR 2 N2, N1, AND EPR JUMPED ABRUPTLY AND AUTO PACK TRIP OCCURED. TAKE OFF ABORTED AND RETURNED TO GATE SPEED = 90KTS ALL INDICATIONS ARE NORMAL AT IDLE 2L73 4F4 F A3WE E2EA 20030331000392003033100039WP 2003 3 31 AALA20030088 120030121A3397 WIRE DOUG DC9 DC983 3022083WP CABIN DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21565AA 49347 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDEWALL LIGHTS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT SIDEWALL LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000842003033100084SO 2003 3 31 C2XA03SH061 120030329A531014522226003 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331001452003033100145NM 2003 3 31 DHL2003741001 120030214A2910 MOTOR BOEING727 7272Q9 138448MNM HYD SYSTEM FAILED A DHLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01741DH 21931 A-SYSTEM HYDRAULIC FAILURE. COMPLETED ABNORMAL PROCEDURE. END NR 2 FLUID SHUTOFF FOR 20 MIN. LT WHEEL WELL FLAP HYDRAULIC MOTOR REMOVED AND REPLACED IAW B727 M/M 27-51-62. A-SYSTEM CASE DRAINS AND MOD FILTERS CHECKED FOR CONTAMINATION, NONE NOTED. RESERVICED A-SYSTEM WITH 5.5 GALLONS OF SKYDROL. OPS CHECKED SYSTEM WITH ENGINE DRIVEN PUMPS. 2L73 4F RTA3WE 20030401000032003040100003EU 2003 4 1 03088316 120030329A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27316UE 41055 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS AT SEAT ROW 6 WERE INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030401000312003040100031SO 2003 4 1 ASOA03051 120030209A3350D36604001 BATTERY EMB 120 EMB120RT 3260202SO FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11257AS 120126 DURING A HANGAR CHECK IN MCN, THE FORWARD SEGMENT OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030401000652003040100065WP 2003 4 1 CA030226002 120030226A32429531478 DISK CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13D 03004GL BRAKE DAMAGED W O OTHER J WARNING INDICATION LDLANDING 1 CA (CAN) ON LANDING, THE NR 4 BRAKE DISK FRACTURED AND DAMAGED BOTH NR 3 AND NR 4 WHEELS AND TIRES. THE AIRCRAFT TAXIED TO PARKING WITHOUT INCIDENT. THE FRACTURED DISK WENT UNNOTICED UNTIL PIECES WERE FOUND ON THE RUNWAY AND TAXIWAY A SHORT TIME LATER. MAINTENANCE REPLACED THE NR 4 BRAKE, NR 3 AND NR 4 MAIN WHEELS, AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4R4 T 6A6 E282 20030401000672003040100067WP 2003 4 1 CA030228005 120030222A2121M2801A6A FAN LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE GALLEY SEIZED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) TROUBLE SHOOTING WAS CARRIED OUT BY MAINTENANCE ON ALL CABIN INTERIOR ELECTRICAL SYSTEMS. UNABLE TO DUPLICATE. ALL CABIN SYSTEMS CHECKED SERVICEABLE AS IAW MAINTENANCE MANUAL. DURING ROUTINE INSPECTION,FOUND MID GALLEY EXHAUST FAN INOPERATIVE (SEIZED). FAN REPLACED AND SYSTEM CHECKEDSERVICEABLE. 2L73 4F4 F A23WE E12EU 20030401000712003040100071NE 2003 4 1 CA030303001 220030319A7230 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FAILED W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE, CREW NOTICED OIL PRESSURE DROPPING, PRIOR TO LOWER LIMIT, ENGINE WAS SECURED/SHUTDOWN. FLIGHT CONTINUED TO DESTINATION 20 MINUTES OUT AND LANDING COMPLETED WITHOUT INCIDENT. ENGINE STRIP INDICATES ANOTHER (BLACK OIL/CARBON IN OIL) ENGINE AS ROOT CAUSE FOR LARGE AMOUNTS OF CARBON CONTAMINATING BEARINGS AND PASSAGES. NUMBER TWO BEARING RUNNING DRY AND NUMBER 3 BEARING RUNNING DRY AND FAILED. (ENGINE IS PRE SB14325.) ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E26NE 20030401000732003040100073EU 2003 4 1 DHL2003364006 120030329A3260BED00101C PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU MLG FAILED A DHLAO OTHER O OTHER CLCLIMB 1 SO01364DH 141 AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT RAISE ABOVE NEUTRAL POSITION, WITH SYSTEM NR 1 SELECTED. EMER PUSH BUTTON WAS PRESSED AND GEAR HANDLE WAS MOVED TO THE UP POSITION. GEAR RETRACTED. REPLACED PROXIMITY DETECTOR UNIT IAW M/M 32-61-12; OPS CHECKED GOOD. 2L72 4F RTA35EU 20030408000702003040800070NM 2003 4 8 03FDEA00366 120030401A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 FRAME DENTED BS 990 STR 26L. FRAME DENTED AT BS 990 STR 26L WAS OUT OF LIMITS. COMPLIED WITH FED EX EA 7-5310-69458. 2L73 4F RTA3WE 20030402000612003040200061NM 2003 4 2 2003UALA00338 120030305A5754114W422011 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 2 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 2 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED 2L72 4F4 FRTT0001SE E46NE 20030402000692003040200069NM 2003 4 2 2003UALA00346 120030315A5754114W411010 WEDGE BOEING777 777222 1385219NM NR 14 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29206UA 30212 T/E WEDGE DELAMINATED - NR 14 SLAT BULB SEAL CORE SECTION MISSING. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED, INSTALLED MISSING CORE IN SEAL. 2L72 4F RTT0001SE 20030403000812003040300081NM 2003 4 3 CALA0300154 120030328A5512 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED AT STA 176.50. REPAIRED IAW ECRA 5515-01008. 2L72 4F RTA16WE 20030403000822003040300082NM 2003 4 3 CALA0300155 120030331A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE TORN A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND FORWARD CARGO DOOR SKIN CUTOUT TORN AT BS 440, S24R. THE SKIN WAS REPAIRED IAW ECRA 5330-03222. 2L72 4F RTA16WE 20030401001652003040100165WP 2003 4 1 DHL2003804774 120030227A575556551672 SKIN DOUG DC8 DC873F 302199FWP NR 3 SPOILER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 R & R OF RT SPOILER NR 3 DUE TO DELAMINATION ON UPPER SURFACE. R & R NR 3 RT SPOILER IAW M/M 27-61-1 PG. 201-207 REF: N/R 0607 FOR OPS CHECK 2L74 4F RT4A25 20030402000302003040200030NM 2003 4 2 2003UALA00237 120030305A261267410413294 MODULE BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT SHORTED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29556UA 26650 A/C RECEIVED WHEEL WELL FIRE INDICATION. WHEEL WELL FIRE INDICATION FOUND TO BE CAUSED BY P-3 WHEEL WELL FIRE ANNUNCIATOR L445. ANNUNCIATOR MODULE REPLACED AND OPERATED NORMAL. REMOVED PART TO BE EVALUATED BY VENDOR. 2L72 4F4 FRTA2NM E17NE 20030403000762003040300076SO 2003 4 3 C2XA03TY045 120030402A531014521699003 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717524 145399 DURING A SCHEDULED 1-C INSPECTION THE OMEGA BEAM WAS FOUND CORRODED. MAINT CUT OUT CORRODED AREA, FAB. ANGLE, FILLER, SHIMS AND INSTALLED IAW 135/145/SRM-53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030403000792003040300079NM 2003 4 3 CALA0300152 120030328A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND STRINGER 24R PUNCTURED AT BS 363. REPAIRED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20030403001032003040300103NM 2003 4 3 DL72S030194 120030225A33501000679REVAC LIGHT BOEING727 727225A 1384077NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO278890Z 21859 L-1 EXIT SIGN INOPERATIVE IN EMERGENCY MODE. REPLACED LIGHT ASSY. 2L73 4F RTA3WE 20030403001122003040300112NM 2003 4 3 DL72W030105 120030128A3350 LIGHT BOEING727 727247 138408FNM CABIN INOPERATIVE A DALAO OTHER L NO TEST NRNOT REPORTED 1 SO27297WA 22534 LT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED RACK M964 AND BATTERY, RELAMPED SIGNS, EXERCISED NO SMOKING SWITCH AND NOW CHECKS NORMAL. 2L73 4F A3WE 20030403001142003040300114NE 2003 4 3 DL72W030196 220030225A7261 O-RING BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE LEAKING A DALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27297WA48183 22534 700301 NR 1 ENG OIL LOSS. REPLACED FUEL PUMP SHAFT O-RING. 2L73 4F4 F A3WE E2EA 20030403001182003040300118NM 2003 4 3 DL733030089 120030124A3350 LIGHT BOEING737 7373B7 1384580NM SEAT 17 DEF BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27952WP 23378 EMERGENCY LIGHT ASSY DAMAGE AT SEAT ROW 17 DEF (IN THE SEAT WHITE LIGHT). REPLACED EMERGENCY LIGHT ASSY, CHECKS NORMAL. 2L72 4F RTA16WE 20030403001212003040300121NM 2003 4 3 DL733030144 120030211A2612 CONTROL MODULE BOEING737 737347 1384647NM APU FIRE DETECT FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27304WA 23345 35523C AT 8000 FT APU FIRE LIGHT AND BELL SOUNDED, C/W PROC LIGHT STILL ON. AIR TURNBACK TO OAK. REPLACED FIRE DETECTOR CONTROL MODULE. 2L72 4F RTA16WE 20030404000052003040400005WP 2003 4 4 ABXA030122 120030313A53103926783507 SUPPORT DOUG DC9 DC932F 3022067WP CARGO DOORWAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 THE AFT LOWER CARGO DOOR JAMB, FORWARD LATCH PIN MOUNT WAS CRACKED. REPLACED THE FORWARD LATCH PIN SUPPORT IAW DC-9 SRM. 2L72 4F A6WE 20030404000062003040400006WP 2003 4 4 ABXA030123 120030313A5330591143267 SKIN DOUG DC9 DC932F 3022067WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 FUSELAGE SKIN WAS CRACKED AT STA. 1096, BETWEEN LONGERON 2 LEFT AND LONGERON 3 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030404000072003040400007WP 2003 4 4 ABXA030124 120030317A53209922042506AX SUPPORT DOUG DC9 DC932F 3022067WP AFT CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 FS 851 RIGHT VERTICAL FLOOR SUPPORT FITTING CRACKED. INSTALLED NEW STRUT SUPPORT IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20030404000132003040400013SO 2003 4 4 C2XA03TY046 120030403A213122250NO30201 CONTROLLER EMB 135 EMB135LR 3260305SO CABIN ERRATIC A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2717524 145399 PILOTED WAS IN A CLIMB OUT OF TYS WHEN THE PRESSURIZATION ICIAS MESSAGE WENT INOPERATIVE. THE CREW RETURN TO TYS AND MAINT. R & R THE PRESSURE CONTROLLER, OPS CHECK WAS GOOD IAW EMB 145 MM 21-31-00. AIRCRAFT WAS REL. AND NO FURTHER PROBLEMS OCCURED. 2L72 4F RTT00011AT 20030404000322003040400032WP 2003 4 4 03FDEA00376 120030402A2620 CONTROLLER DOUG MD10 MD1010F WP FIRE EXTING INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25392FE 46626 IN CRUISE (FL330) RECIEVED CARGO FIRE INDICATION WITH MASTER WARNING AND AFT 1 FLASHING DISCHARGE LIGHT. COMPLIED W/ APPROPRIATE PROCEDURES. DIVERT TO STL. ONLY FIRED BOTTLE NR 1. REPLACED LOWER CARGO COMP FIRE EXT CONTAINER NR 1, DISCHARGE HEADS AND DISCHARGE CARTRIDGES. R & R MISC. SYS. CONTROLLER PRECAUTIONARY PER MD10 MM 31-42-01. R&R CARGO FIRE CONTROL PANEL PER MD10 AMM 26-14-10-4 PANEL OPS CK OK, PER MD10 AMM 26-14-01 PG501. PERFORMED FIRE EXTINGUISHER CIRCUITS TEST PER M/M 26-22-01. PERFORMED OPS CHECK ON MSC PER M/M 31-42-01. CARGO FIRE TEST OPS CHECKS GOOD PER M/M 26-14-01. OK FOR SERVICE. 2L73 4F RTA22WE 20030404000422003040400042NM 2003 4 4 DL73S030113 120030129A5312 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CANNING A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 INSPECTION OF THE AFT P-DOME REVEALED A 10 X 8 X .25 INCH OIL CAN IN THE LOWER WEB AREA OF NEAR BL 0. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOULBER PER BAC S/B 737-53A1075 AND ER/A 384318-14AD. 2L72 4F RTA16WE 20030403001022003040300102NM 2003 4 3 DL72S030185 120030224A3350 LIGHT BOEING727 727232 1384082NM COCKPIT MALFUNCTIONED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27523DA 21583 COCKPIT EMERGENCY LIGHT FAILS TO COME ON DURING EMERGENCY POWER CHECK. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK GOOD. 2L73 4F A3WE 20030408000322003040800032SO 2003 4 8 SIMA200302902 120030128A3397 WIRE EMB 145 EMB145LR 3260212SO CABIN DAMAGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21623AE 145109 HOU - FLT 3786 - DURING CREW PREFLIGHT, THE FLOOR PROXIMITY EMERGENCY LGIHTS FROM ROW 7 TO 10 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A WIRE ON THE FLOOR LIGHT STRIP. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030408000592003040800059WP 2003 4 8 0300729606 120030317A2150 CLAMP DOUG DC9 DC932 3022066WP CABIN PRESSURE BROKEN A NWAAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL01606NW 47225 CLIMBING THROUGH FL 210 CREW FELT A THUMP IN THE FORWARD CABIN AND SUBSEQUENTLY LOST CONTROL OF CABIN PRESSURE. OUTFLOW VALVE INDICATED FULL CLOSED BUT THE CABIN CONTINUED TO CLIMB THROUGH 10,500 FEET. FLIGHT CONTINUED TO DESTINATION AT THIS LOWER ALTITUDE AND LANDED WITHOUT INCIDENT AT MEM. MAINTENANCE FOUND A BROKEN CLAMP AND REPLACED IT. AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20030408000602003040800060WP 2003 4 8 0300739954 120030325A21312075301AB CONTROLLER DOUG DC9 DC931 3022065WP CABIN PRESSURE INOPERATIVE A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01921RW 47164 WHILE CRUISING AT FL 150 THE CABIN PRESSURE STARTED TO FLUCTUATE FROM FULL RATE OF CLIMB TO FULL RATE OF DESCENT. CREW STARTED AN EMERGENCY DESCENT AS CABIN PRESSURE STARTED TO CLIMB UNCONTROLLABLY. AIRCRAFT REACHED 1000 FEET EXPEDITIOUSLY AND THE MAXIMUM CABIN ALTITUDE EVER REACHED WAS 8000 FEET. COMPLETED COM AND LANDED WITHOUT FURTHER INCIDENT AT LSE. MAINTENANCE REPLACED THE PRESSURE CONTROLLER AND OUTFLOW VALVE AS PRECAUTIONAREY MEASURE. SUSPECT A/C TO BE INTERMITTENT BETWEEN AIR MODE AND GRND MODE. NO BITE ACCOMPLISHED. 2L72 4F A6WE 20030408000622003040800062EU 2003 4 8 03093312 120030403A3350 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSFAILED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27312UE 41025 DURING MAINTENANCE/INSPECTION ROWS 3 TO 6 EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED CENTER CABIN EMERGENCY BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA41NM 20030401000162003040100016WP 2003 4 1 AALA20030003 120030103A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 DURING OVERNIGHT MAINTENANCE, AFT STAIR SIDEWALL MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR SIDEWALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000792003040100079NM 2003 4 1 DHL2003743005 120030319A2613 SENSOR BOEING727 727225 1384077NM OVERHEAT SHORTED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01743DH 22438 IN CRUISE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER RETARDING NR 1 THRUST LEVER. RAN NR 1 ENGINE AND INSPECTED PNEUMATIC DUCTS IN AFT AIRSTAIR WITH PACKS RUNNING, NO LEAKS NOTED. FOUND SENSOR TOUCHING STRUCTURE. REPOSITIONED, NO FAULTS NOTED. SYSTEM OPS CHECKED IAW M/M 26-14-1. 2L73 4F A3WE 20030401001142003040100114WP 2003 4 1 DHL2003804505 120030112A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER UPPER PART CRACKED 1 INCH AT XFS 483.750. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024.T3AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030401001332003040100133WP 2003 4 1 DHL2003804525 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 628.758. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001342003040100134WP 2003 4 1 DHL2003804545 120030207A27223651629U FITTING DOUG DC8 DC873F 302199FWP RUDDER ACT CORRODED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 CORROSION ON FITTING ATTACHING ACTUATOR TO RUDDER AT STA. ZR61.156. PERFORMED MAJOR REPAIR IAW SRM55-1-0 PG. 1 , REMOVED FITTING IAW SRM 51-1-21 PG. 1 SRM 51-1-20D. PG. 21 REMOVED CORROSION IAW SRM 51-1-8 PGS. 17-18 FOUND OUT OF LIMITS IAW SRM 55-2-0 PAGE 12 , CLEANED , TREATED AND PRIMEDAREA IAW SRM 51-18B. INSTALLED NEW FITTING IAW SRM51-1-21 PG 1 , SRM 51-1-20D PG. 9FOR REBALANCE SEE N/R 2657 2L74 4F RT4A25 20030401001352003040100135WP 2003 4 1 DHL2003804547 120030208A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 STA 1580 LONG 21 RT HAS A DAMAGED FRAME WITH .750 CRACK DUE TO PALLET LOADING DAMAGE ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 PG. 20U-2V SHEET 2. REMOVED FASTNERS IAW SRM 51-1-21 PG.1 , SRM51-1-20D PG 21 , CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 PG 2U/2V SHEET 2 , FABRICATED FRAME SEGMENT &SPLICE (7075 "O" .071/.080) IAW SRM53-2-0 PG. 2U/2V FIG. 2 SHEET 2 HEAT TREATED IAW SRM 51-1-1 PG1,17 , SRM 51-1-4 PGS 1-3 , DPS1-05.3 , CLEANED , TREATED AND PRIMED FRAME & SPLICE IAW SRM51-1-8B , INSTALLED FRAME SEGMENT & SPLICE WITH NEW FASTNERS IAW SRM 53-2-0 PG. 2U/2V FIG. 2 SHEET 2 , SRM51-1-21 PG. 1 , SRM51-120D PG. 9 2L74 4F RT4A25 20030402000252003040200025CE 2003 4 2 049330 120030331A3230 MOTOR BEECH 1900 1900D 1154162CE MLG FAILED A AMWAO OTHER J WARNING INDICATION APAPPROACH 1 CE07165YV UE165 ON APPROACH TO KANSAS CITY, THE LANDING GEAR FAILED TO EXTEND. AFTER PERFORMING THE MANUL EXTENSION CHECK LIST THE GEAR WAS FOUND TO BE DOWN AND LOCKED. THE GEAR WAS PUMPED DOWN ALL THREE GREEN CAME ON. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR MOTOR. WAITING ON VERIFICATION ON PART SERIAL NUMBER AND THERE WILL BE MORE INFORMATION TO COME. 2L72 4T RTA24CE 20030402000392003040200039NM 2003 4 2 2003UALA00315 120030321A2751 INDICATOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE TE FLAPS MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29910UA 25254 AIRCRAFT RETURNED TO FIELD UNDER AMBER ALERT DUE TO SPLIT FLAP INDICATION. REPLACED FLAP POSITION INDICATOR. INSTALLATION AND TESTS NORMAL. REMOVED INDICATOR SENT TO SHOP FOR REVIEW. 2L72 4F4 FRTA16WE E2GL 20030403000422003040300042NM 2003 4 3 AMTA200300258 120030222A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11523AT 30232 EMEGENCY ESCAPE PATH LIGHTS INOPERATIVE AT 2 FED, 3 BULBS. RECONNECTED WIRES TO LIGHT BULB FIXTURES, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030403000952003040300095EA 2003 4 3 COMA0360176 120030330A2611 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA LAT SMOKE FALSE ACTIVATIONA COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01420CA 7451 FLIGHT 5856 SMOKE TOILET CAUTION MESSAGE, F/A VERIFIED SMOKE IN CABIN. COULD NOT DUPLICATE. NO DISCREPANCY FOUND IN ANY SYSTEM. REPLACED THE ACM COOLESCER SOCKS FOR PRECAUTION. 2L72 4F RTA21EA 20030403001152003040300115NM 2003 4 3 DL733030066 120030116A555365468726 FITTING BOEING737 737347 1384647NM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307WA 23440 CORROSION WAS FOUND ON THE AFT FACE OF THE RT REAR SPAR PRIMARY FITTING LUG. THE AFT SIDE OF THE LUG WAS SPOT FACED .005 INCH TO REMOVE THE CORROSION. A REPAIR BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2L72 4F RTA16WE 20030404000552003040400055NM 2003 4 4 DL757030202 120030227A2560 FLASHLIGHT BOEING757 757232 1384965NM CABIN WILL NOT TEST A DALAK NONE L NO TEST ININSP/MAINT 1 SO27661DN 24972 AFT LT EMERGENCY FLASHLIGHT FAILED TEST. REPLACED FLASHLIGHT AND BATTERY. 2L72 4F RTA2NM 20030404000562003040400056NM 2003 4 4 DL757030204 120030228A3350 FLASHLIGHT BOEING757 757232 1384965NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27601DL 22808 ONE LEFT DOOR EMERGENCY FLASHLIGHT NOT WORKING. REPLACED FLASHLIGHT ASSY. 2L72 4F RTA2NM 20030404000732003040400073NM 2003 4 4 DL757030292 120030324A5330146N37506 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27612DL 22819 THE FUSELAGE SKIN WAS FOUND GOUGED AND DENTED NEAR THE R4 DOOR CUTOUT BETWEEN FS 1686 & 1691 AND BETWEEN STRINGERS 15R & 17R. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384536-14, REV A. 2L72 4F RTA2NM 20030404000742003040400074NM 2003 4 4 DL764030077 120030122A5753114T41455 BOLT BOEING767 767432ER 1385134NM TE FLAPS SHEARED A DALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO27826MH 29697 L/E SLAT ASYM MSG DISPLAYED AFTER FLAPS EXTENDED TO 30 ON APPROACH. FOUND NR 1 LEFT SLAT OUTBOARD TARGET MISSING FOR SENSOR 276. REPLACED TARGET WITH NEW BOLT AND BEARING. RAN FLAPS/SLATS SEVERAL TIMES WITH NO EICAS MESSAGES OR FAULTS ON PROX BOX. 2L72 4F RTA1NM 20030404001152003040400115NM 2003 4 4 ASAA0310001 120030105A33508821004 BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - DURING RECON INSPECTION, FOUND INSTALLED PALLET ARRIVED WITH DISCHARGED BATTERY. REMOVED AND REPLACED BATTERY PACK, THEN LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 20030404001432003040400143 2003 4 4 SWAA030471 420030303A25651061323 SLIDE BOEING737 7373G7 1384595NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030404001792003040400179NM 2003 4 4 SWAA030585 120030314A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (28 EA) BETWEEN FWD & AFT GALLEY'S. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20030408001092003040800109CE 2003 4 8 2003F00217 120030221A335099131 BATTERY PACK CESSNA750 750 2076810CE AFT CABIN FAILED A UG8AO OTHER O OTHER NRNOT REPORTED 1 GL235114 7500017 EXIT LIGHT OVER EMERGENCY EXIT INOPERATIVE ON BATTERY. REPLACED AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL TEST IN GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030408001152003040800115NM 2003 4 8 2003UALA00361 120030403A5313 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE STRINGER CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 FWD ENTRY DOOR CUTOUT STRINGER END FITTING CRACKED BS360 STRINGER 15L. MAJOR REPAIR ACCOMPLISHED. REPLACED END FITTING. 2L72 4F4 FRTA16WE E2GL 20030408001162003040800116NM 2003 4 8 2003UALA00362 120030403A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 R5 DOOR EXTERNAL SKIN UPPER PLATE AT LOWER HINGE HAS DAMAGE 2L74 4F4 FRTA20WE E24NE 20030408001242003040800124WP 2003 4 8 AMTA200300215 120030211A3350 POWER SUPPLY LKHEED1011 10113853 5265020WP CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11164AT 1238 FOND EGRESS LIGHTS FORWARD RIGHT SIDE INOPERATIVE. REPLACED FORWARD RIGHT SIDE EGRESS POWER SUPPLY PER MM 33-51-36. OPS CHECK NORMAL. (M) 2L73 4F A23WE 20030408001402003040800140NM 2003 4 8 AWXA200300346 120030312A575465C26603100 STRUCTURE BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE NR 4 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 YVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE, INBOARD CORNER OF THE NR 4 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED NR 4 SLAT, REPAIRED DAMAGE IAW SRM 51-70-10, FIG. 32, PG. 88I, RE-INSTALLED SLAT AND RIGGED SYSTEM IAW BMM 27-81-21, PG. 414-419. 2L72 4F4 FRTA16WE E2GL 20030409000012003040900001EU 2003 4 9 03097322 120030407A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27322UE 41058 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT PORTIONS OF THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030404000232003040400023NM 2003 4 4 DHL2003743007 120030403A2697 CONNECTOR BOEING727 727225 1384077NM NR 3 ENGINE LOOSE A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01743DH 22438 NR 3 GROUND FAULT DETECTOR LIGHT ILLUMINATED IN FLIGHT. FOUND FORWARD ELECTRICAL CONNECTOR LOOSE ON NR 3 ENGINE FIRE SENSING ELEMENT, RE-SECURED CONNECTOR. SYSTEM OPS CHECKED GOOD IAW BMM 26-11-00. 2L73 4F A3WE 20030404000312003040400031NE 2003 4 4 DL73K030177 220030222A752065581232 DUCT BOEING737 737247 138448DNM PWA JT8 JT8D15 52051NE NR 2 ENGINE RUPTURED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27243WA 23517 709162 SHORTLY AFTER LIFT OFF, NR 2 ENGINE OVERHEAT LIGHT CAME ON ACCOMPANIED BY A BLEED TRIP LIGHT. OVERHEAT LIGHT EXTINGUISHED WHEN THRUST LEVERS RETARDED TO IDLE. FOUND SENSE LINE LEAKING AT PRBC AND COWL ANTI-ICE DUCT BLOWN. REPLACED SENSE LINE, COWL DUCT, AND 490 DEGREE OVERHEAT SWITCH. RAN ENGINES TO T/O POWER, OPN AND INDICATION NORMAL. 2L72 4F4 F A16WE E2EA 20030404000402003040400040NM 2003 4 4 DL73K030312 120030327A5753 WEDGE BOEING737 737232 1384475NM RT WING DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 RT INBOARD AFT FLAP T/E WEDGE DELAMINATED. REPAIRED PER ER/A 422903-14. 2L72 4F RTA16WE 20030407000052003040700005NM 2003 4 7 ASAA0310005 120030109A3350873203041 CONTROL MODULE BOEING737 7372X6C 1384552NM MID CABIN INOPERATIVE A ASAAO OTHER O OTHER DEDESCENT 1 NM01747AS 23124 FOUND EMERGENCY TRACK LIGHTING ILLUMINATED ON DESCENT AND THEN EXTINGUISHED PRIOR TO LANDING. REMOVED AND REPLACED CENTER CONTROL MODULE, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20030407000352003040700035WP 2003 4 7 GTIA021397 120030121A5511 RIB DOUG DC9 DC982 3022082WP HORIZONTAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND LT INBOARD HORIZONTAL STABILIZER INBOARD RIB FLANGE WAS A 3 INCH CRACK. REMOVED DAMAGED AREA AT RIB FLANGE. FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR. (M) 2L72 4F A6WE 20030407000802003040700080SO 2003 4 7 SIMA200306203 120030222A2120 ODOR EMB 135 EMB135LR 3260305SO COCKPIT/CABIN DETECTED A SIMABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21711PH 145235 PVD - FLT 4796 - DURING CRUISE FLIGHT, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT AND CABIN. CREW DECLARED AN EMERGENCY AND DIVERTED TO PVD. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS INSPECTED AND AN OPERATIONAL CHECK WITH ENGINES RUNNING WAS COMPLIED WITH. NO DEFECTS WERE NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030407000842003040700084SO 2003 4 7 SIMA200306404 120030128A532014525480003 PLATE EMB 135 EMB135LR 3260305SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 ABI - THIS IS A LEVEL, TWO FINDING FOUND DURNG AN IMBV INSPECTION, LOWER CARGO DOOR CUTOUT SILL PLATE CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW LOWER SILL PLATE IAW EMB 135 SRM 51-40-02, 51-20-03, ETN EB-53-021R1. (M) 2L72 4F RTT00011AT 20030407000922003040700092SO 2003 4 7 SIMA200306412 120030215A532014522460013 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 THIS IS A LEVEL TWO FINDING, FOUND DURING A IMBV INSPECTION GALLEY CENTER BEAM GUSSETT CORRODED. INSTALLED NEW GALLEY CENTER BEAM GUSSETT IAW EMB 135 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04, 51-40-06. (M) 2L72 4F RTT00011AT 20030408000542003040800054NM 2003 4 8 0300676312 120030402A2530 CONTROLLER BOEING747 747451 1384940NM GALLEY OVEN INOPERATIVE A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01672US 30267 DURING FLIGHT SMOKE EMITTED FROM THE NR1 OVEN IN THE UPPER DECK. PULLED GALLEY CIRCUIT BREAKER, AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN CONTROLLER, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030408001292003040800129NM 2003 4 8 AWXA200300335 120030313A53126516300 BULKHEAD BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MAJOR REPAIR - DURING C-16 CHECK 5 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT WL 218 LBL 12, WL 212 LBL 5.7, WL 198 LBL 5.0, WL 198 LBL 62, AND WL 201 LBL 6.2. MAINTENANCE PERFORMED NDT INSPECTION ON BS 178 BULKHEAD WEB AT WL 218 LBL 12, WL 212 LBL 5.7, WL 198 LBL 5.0, WL 198 LBL 62, AND WL 201 LBL 6.2; CONFIRMED WL 198 LBL 62, AND WL 201 LBL 6.2 WERE NOT CRACKED; MARKED END POINTS AND STOP DRILLED WEB AT WL 218 LBL 12, WL 212 LBL 5.7, AND WL 198 LBL 5.0; PERFORMED NDT INSPECTION TO VERIFY CRACKS CONTAINED; FABRICATED REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 210, PG. 285, AND SRM 51-40-02, PG. 6. 2L72 4F RTA16WE 20030410000292003041000029NE 2003 4 10 SWAA030608 220030317A7261 FILTER BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE LT ENGINE DIRTY A SWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW29718SW 27852 IN-FLIGHT SHUTDOWN, DECLARED EMERGENCY. DURING CRUISE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE SUPPLY OIL FILTER & SCAVENGE OIL FILTER PER MM. C/W ENGINE RUN, NO DEFECTS FOUND. 2L72 4F4 FRTA16WE E00055EN 20030410000562003041000056WP 2003 4 10 GTIA030094 120030212A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND PAX CABIN FLOOR WEB CRACKED AT LONGERON 18L STATION 325. CUT OUT DAMAGED WEB. FABRICATED FLOOR WEB AND DOUBLER. INSTALLED WEB AND DOUBLER. (M) 2L72 4F A6WE 20030410000582003041000058WP 2003 4 10 GTIA030095 120030210A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND MAIN CABIN FS 1174 RIGHT OUTBOARD FLOOR PANEL CRACKED. REMOVED DAMAGED FLOOR PANEL. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. REINSTALLED FLOOR PANEL. (M) 2L72 4F A6WE 20030410000592003041000059NM 2003 4 10 SWAA030641 120030320A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 400, WL 148 AND LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030410000772003041000077WP 2003 4 10 GTIA030104 120030224A3340 SWITCH DOUG DC9 DC932 3022066WP LANDING LIGHT CONTAMINATED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23133NK 48111 DTW - FLT 1141 - FOUND SMOKE IN COCKPIT WHILE SITTING AT THE GATE. FOUND ARCING ON LANDING LIGHT SWITCH DUE TO DIRT CONTAMINATION CLEANED SWITCH CONTACTS COULD NOT DUPLICATE ORIGINAL PROBLEM. NO OTHER DEFECTS NOTED AT THIS TIME LIGHTING. OPS CHECK GOOD. (M) 2L72 4F A6WE 20030410000782003041000078NM 2003 4 10 SWAA030652 120030322A33506104791 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED SPECIAL VISIT, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY, RELAMPED EXIT LIGHT PER MM. 2L72 4F A16WE 20030410000792003041000079 2003 4 10 SWAA030653 420030321A25656556685 BRACKET BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE RETAINING BRACKET OUT OF ADJUST. ADJUSTED BRACKET PER MM. 2L72 4F RTA16WE 20030404000492003040400049NM 2003 4 4 DL757030167 120030220A2120 ODOR BOEING757 757232 1384965NM A/C DUCTING DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27678DL 25983 ODOR IN COCKPIT COMING FROM OVERHEAD AIR CONDITIONING DUCT. FOUND TO BE RIGHT RECIRCULATION FAN THE CAUSE. DEACTIVATED FAN AND FWD TO MCO/PLAC PER MEL 21-25-01A. 2L72 4F RTA2NM 20030404000542003040400054NM 2003 4 4 DL757030190 120030221A5310143N85121 DOOR FRAME BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27652DL 24392 THE OUTER CAP OF THE LOWER SILL BEAM OF THE C1 DOOR OPENING WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE THE OUTER STRUCTURE, THE OUTER STRUCTURE AND WEB OF THE FS 620 FRAME WERE CUT AND THE LOWER SECTIONS REMOVED. A NEW SILL STRUCTURE WAS THEN INSTALLED AND THE LOWER SECTIONS OF FRAME CHORD AND WEB SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS PER ER/A 384501-14, REV A. 2L72 4F RTA2NM 20030404000592003040400059NM 2003 4 4 DL757030223 120030307A2913291702437 PUMP BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE CRACKED A DALAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27618DL 22908 716514 LOST RT HYD SYSTEM QUANTITY WHILE HOLDING SHORT OF RUNWAY FOR TAKEOFF. FOUND RT ENGINE DRIVEN HYD PUMP HOUSING CRACKED. REPLACED RT ENGINE DRIVEN HYD PUMP, CASE DRAIN FILTER AND PRESURE FILTER. ALL LEAKED CHECKED GOOD. SERVICED HYD SYSTEM TO FULL. 2L72 4F4 FRTA2NM E17NE 20030404000602003040400060NM 2003 4 4 DL757030237 120030312A3040 DEICE SYSTEM BOEING757 757232 1384965NM COCKPIT WINDOW BURNED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO276714Q 30485 ELEC FUMES IN FLT DECK AND LEFT ENG GEN DROPPED OFF LINE. NO ASSOC STATUS MSGS. DIVERTED TO GSO. LEFT ENG GEN CONFIRMED FAILED. PLACED ON MCO PER MEL. FOUND EVIDENCE OF FUMES WHILE STANDBY POWER CHECK WAS PERFORMED. REPLACED MAIN BATTERY, CHARGER AND INVERTER AS PRECAUTIONARY. DURING CONTINUED T/S, FOUND BURNED TERMINALS ON 3L WINDOW HEAT TERMINAL. THE 3L WINDOW HEAT DEACTIVATED PER MEL. IT IS SUSPECTED THAT THE 3L WINDOW WAS SOURCE OF SMELL THE ENTIRE TIME. 2L72 4F RTA2NM 20030404000622003040400062NM 2003 4 4 DL757030253 120030318A2121731376 FAN BOEING757 757232 1384965NM E/E BAY SEIZED A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27634DL 23615 RETURNED TO IAD AFTER ELECTRICAL FUMES IN COCKPIT AND THROUGHOUT CABIN ON APPROACH, GOT EQUIPMENT COOLING OVERHEAT LIGHT WITH EFI SYMBOLS DEGRADING. FOUND NR 1 FORWARD EQUIPMENT COOLING FAN C/B POPPED AND FOUND NR 1 FAN SEIZED. REPLACED FAN EQUIPMENT COOLING, OP CHECKS NORMAL. 2L72 4F RTA2NM 20030404000652003040400065NM 2003 4 4 DL757030269 120030323A335061020 BATTERY BOEING757 757232 1384965NM FLASHLIGHT DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27655DL 24395 FLASHLIGHT AT 4R NOT FLASHING. REPLACED BATTERY AND BULB. 2L72 4F RTA2NM 20030404000682003040400068NM 2003 4 4 DL757030277 120030325A2910 B-NUT BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENG HYD SYSLOOSE A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27608DA 22815 716563 RIGHT ENG HYD PUMP EICAS MSG AND RT ENG HYD PRESS LIGHT ILLUM ON TAKEOFF. RIGHT ENG HYD PUMP SWITCH TURNED OFF. FOUND PYLON SUPPLY LINE B-NUT LOOSE, SECURED SAME. MOTORED ENG. GOOD PRESSURE, NO LEAKS. 2L72 4F4 FRTA2NM E17NE 20030404000712003040400071NM 2003 4 4 DL757030290 120030324A5315146N51114 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27612DL 22819 THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL DAMAGE. A NEW SECTION OF CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED PER ER/A 384541-14, REV A. 2L72 4F RTA2NM 20030404000792003040400079NM 2003 4 4 DL767030103 120030122A5754114T411419 WEDGE BOEING767 767232 1385132NM LT WING SLAT TE DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27115DA 22227 LEFT WING OUTBOARD SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418205-14. 2L72 4F RTA1NM 20030404000802003040400080NM 2003 4 4 DL767030104 120030122A5754114T411420 WEDGE BOEING767 767232 1385132NM RT WING SLAT TE DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27115DA 22227 RIGHT WING OUTBOARD SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418206-14. 2L72 4F RTA1NM 20030404001192003040400119WP 2003 4 4 ASAA0380088 120030117A33501001191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS230436568 49387 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR NOT CHARGING. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2L72 4F A6WE 20030404001352003040400135NM 2003 4 4 SWAA030411 120030221A335020131A BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030404001372003040400137NM 2003 4 4 SWAA030417 120030223A5755654645262A CASTING BOEING737 7373A4 1384585NM SPOILER CRACKED A SWAAK NONE E VIBRATION/BUFFET UKUNKNOWN 1 SW29673AA 23251 FLT ATTENDANT REPORTS LOUD HUM AND VIBRATION LT SIDE OF CABIN FROM ROWS NR 6 THROUGH ROW NR 17. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM. 2L72 4F RTA16WE 20030404001402003040400140NM 2003 4 4 SWAA030457 120030228A32116546113 TRUNNION PIN BOEING737 7375H4 138449DNM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED RON, SWA SI 11251-32, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030404001442003040400144NM 2003 4 4 SWAA030472 120030303A3350610478 BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030404001492003040400149NM 2003 4 4 SWAA030505 120030305A27816554401 SENSOR BOEING737 7373Q8 1384670NM L/E FLAP FAILED A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29689SW 23387 AIR TURNBACK, AFTER FLAP RETRACTION, NR 4 L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 4 L/E FLAP RETRACT SENSOR PER MM. OPS CK GOOD. 2L72 4F RTA16WE 20030404001602003040400160NM 2003 4 4 SWAA030550 120030311A2910AS118G0194CTR HYDRAULIC LINE BOEING737 7377H4 1384404NM HYD SYSTEM CRACKED A SWAAK NONE K FLUID LOSS CRCRUISE 1 SW29712SW 27846 DECLARED EMERGENCY, DURING FLIGHT A-SYSTEM HYDRAULIC QUANTITY IND WENT TO ZERO. FOUND LINE ON HYD MUFFLER CRACKED. REMOVED AND REPLACED HYD LINE, NR 1 ENG HYD PUMP, CASE DRAIN FILTER & A-SYSTEM MAIN FILTER PER MM. 2L72 4F RTA16WE 20030404001772003040400177NM 2003 4 4 SWAA030580 120030313A3350BR2013 COVER BOEING737 7375H4 138449DNM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 4 & WIRES EXPOSED AT ROW NR 9. REMOVED AND REPLACED COVER AND SECURED WIRES PER MM. 2L72 4F RTA16WE 20030407000082003040700008WP 2003 4 7 ASAA0380037 120030106A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP FWD CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01934AS 49235 DURING APPROACH, NOTED THAT 1ST CLASS CABIN EMERGENCY TRACK LIGHTING WAS FLASHING. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20030407000132003040700013WP 2003 4 7 ASAA0380068 120030112A5310991980549 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, SHEAR TIE IS CORRODED AT FS 1287. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01, 53-03, AND 51-10-3. (M) 2L72 4F RTA6WE 20030407000212003040700021WP 2003 4 7 ASAA0380076 120030113A5310MS20001FY67200 HINGE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, MID CARGO BAY BARRIER DOOR HINGE IS CRACKED. REPLACED HINGE PER SRM 51-10-3, 51-10-4, AND 51-30-1. (M) 2L72 4F RTA6WE 20030407000252003040700025WP 2003 4 7 ASAA0380092 120030117A5347S292235714400 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY FLOOR TRACK CORRODED AT FASTENER HOLES. REPLACED FLOOR TRACK PER SRM 53-05 AND 51-10-3. (M) 2L72 4F RTA6WE 20030407000402003040700040WP 2003 4 7 GTIA030025 120030103A5753 FLAP TRACK DOUG DC9 DC982 3022082WP RT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND RIGHT WING INBOARD FLAP OUTBOARD TRACK, HINGE FITTING STUD HOLE HAS A CRACK. REMOVED REPAIR DOUBLERS. LOCATED AND DRILLED -44 AND -46, REPAIR DOUBLERS. INSTALLED 44 AND 46 DOUBLERS. (M) 2L72 4F A6WE 20030407000772003040700077SO 2003 4 7 SIMA200305414 120030215A532013500469401 STRUCTURE EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, CROSSMEMBER AT FRAME 22 CORRODED. REMOVED AND INSTALLED SERVICEABLE CROSSMEMBER IA FRAME 22 IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030331001082003033100108EU 2003 3 31 DHL2003363001 120030326A3242C200601004 BRAKE ASSY AIRBUS300 A300B4203 3930306EU NR 2 FROZEN A DHLAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01363DH 85 EXCESSIVE THRUST USED TO MOVE A/C AND VIBRATION FELT. FOUND NR 2 BRAKE DAMAGED AND FROZE WITH WHEEL ASSY. REMOVED AND REPLACED NR 2 BRAKE UNIT AND MAIN WHEEL ASSY. IAW M/M 32-41-00 AND 32-42-27. BLEED AND LEAK TEST OK. OPS CHECKED GOOD. 2L72 4F RTA35EU 20030331001252003033100125NM 2003 3 31 DHL2003740505 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 IN FWD CARGO FRAME HAS 2 DENTS INTO THE RADIUS AT BS 660 STR 24 R. REMOVED FASTENERS FOR ACCSES PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 52-10-3. FABRICATED FRAME REPAIR 7076-T6 .063 PER SRM 53-10-3 PG 3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-3 AND 51-10-2. 2L73 4F RTA3WE 20030331001302003033100130NM 2003 3 31 DHL2003740511 120030202A5340 CHANNEL BOEING727 7272Q9 138448MNM FUSELAGE CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CABIN BS 1166 AND 1148 STR 7.5 LT EACH HAVE GILLINER ATTACHING SUPPORT CHAFE MARKS INTO FRAME. CUT OUT DAMAGED AREA AT STA 1166 3 X 1 INCH, AND 1148 3 X 1 INCH PER SRM 51-40-3. FABRICATED DOUBLERS (7075-T6 .100) PER SRM 53-10-2 FIG 5. TREATED PARTS AND AREA, PRIMED PER SRM 51-10-2. INSTALLED 2 EA DOUBLERS PER SRM 51-10-2. 2L73 4F RTA3WE 20030331001322003033100132NM 2003 3 31 DHL2003740513 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH FUSELAGE FRAME AT STA 660 IS DENTED BETWEEN STR 16 R - 17 R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PART (7075-T6 .063) PER SRM 51-40-3. CLEANED, TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 51-40-1. 2L73 4F RTA3WE 20030331001482003033100148NM 2003 3 31 DHL2003742002 120030116A2612 CLAMP BOEING727 727225 1384077NM NR 3 FIRE LOOP LOOSE A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01742DH 21290 NR 3 FIRE DETECTOR GROUND LIGHT ILLUMINATED. DEFERRED NR 3 ENGINE FIRE DETECTOR GROUND LIGHT IAW MEL 26-9-1. CONTROL 11652. REF DMI 11652, NR 3 FIRE DETECTOR GROUND LIGHT ILLUMINATED. CLEANED CONNECTOR AT ENGINE AREA AND RE-SECURED LOOSE HOLDING CLAMP. PERFORMED OPS CHECK AND FOUND SYSTEM NORMAL. NO FAULTS IAW M/M 26-11-00. THIS CLEARS DMI NR 11652. PLACARD REMOVED. 2L73 4F A3WE 20030401000382003040100038NM 2003 4 1 AWXA200300325 120030329A3350BR9660106 LIGHT BOEING737 73733A 1384673NM R-2 DOOR BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT WAS DAMAGED AT R-2 DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT AT R-2 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030401001372003040100137NM 2003 4 1 DHL2003745008 120030331A2612 BULB BOEING727 727224 1384076NM NR 1 FIRE IND BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01745DH 20665 NR 1 ENGINE FIRE INDICATOR LIGHT INOPERATIVE. RE-LAMPED NR 1 ENGINE FIRE INDICATOR LIGHT PER DHL B-727 M/M 26-11-03. OPS. CHECKED SATISFACTORY. 2L73 4F A3WE 20030401001832003040100183WP 2003 4 1 DHL2003873006 120030318A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT STUCK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ 46091 F/O'S SLIDING WINDOW IS DIFFICULT TO OPEN. REMOVED DEBRIS FROM F/O'S SLIDING WINDOW LATCH MECHANISM. OPS NORMAL IAW DC8 M/M 56-00-0. 2L74 4F RT4A25 20030402000712003040200071NM 2003 4 2 A6WA200330003 120030214A2421 ALTERNATOR DORNERDO32 DO328100 2996000NM ENGINE MALFUNCTIONED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31341PH 3065 RIGHT AC VOLT FAIL CAS AND 2ND PHASE DROPS TO 79 VOLTS, REMOVED AND REPLACED ALTERNATOR. (M) 2H72 4T RTA45NM 20030403000342003040300034 2003 4 3 249TR0015 420030330A2220 WARNING LIGHT BOEING737 7372K5 138448XNM MACH TRIM ILLUMINATED A PIDAO OTHER N FALSE WARNING CRCRUISE 1 SO05249TR 22598 MACH TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT, THEN WENT AWAY. COMPLETED MACH TRIM TEST PER MM 22-21-0. OPS CHK OK. 2L72 4F RTA16WE 20030403000382003040300038NM 2003 4 3 AMTA200300253 120030222A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 R1 EXTERIOR EMERGENCY DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK REF 3350/589, PER AMM 33-51-07, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030403000402003040300040NM 2003 4 3 AMTA200300255 120030222A335020121 BATTERY PACK BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 FOUND SEAT ROW 4-10 EGRESS FLOOR TRACK LIGHTS INOPERATIVE. REMOVED AND REPLACED L2 DOOR BATTERY PACK CHARGER REF ATA DISC NR 3350/586, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030404000182003040400018NM 2003 4 4 CALA0300165 120030401A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND A 0.4 INCH CRACK IN SKIN AT UPPER FORWARD CORNER OF PILOT'S WINDOW CD POST AT BS 205, WL 238. REPAIRED IAW SRM 53-10-01, FIGURE 210. 2L72 4F RTA16WE 20030407000882003040700088SO 2003 4 7 SIMA200306408 120030215A532014522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704MR 145174 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING IMBV INSPECTION, PASSENGER DOOR AFT FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED NEW PAX DOOR AFT FLOOR SUPPORT IAW EMB 135 51-20-01, 51-20-03, 51-40-02, 51-40-04. (M) 2L72 4F RTT00011AT 20030407000932003040700093SO 2003 4 7 SIMA200306413 120030215A532014522459003 STRUCTURE EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, GALLEY CENTER BEAM RAMP CORRODED. REMOVED AND INSTALLED SERVICEABLE GALLEY CENTER BEAM IAW EMB 135 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04. (M) 2L72 4F RTT00011AT 20030407001092003040700109EU 2003 4 7 USAA030016 120030207A5320 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19729US9575 1170 CLT - FOUND FLOOR SUPPORT I-BEAM CRACKED .750 INCH, FRAME 12 BL 0. MILLED SECTION OF EXTRUSION, FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 53-11-14. (M) 2L72 4F RTA28NM 20030408000092003040800009WP 2003 4 8 ASAA0380083 120030113A5321S00096 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, FORWARD CARGO BAY NR 4 FLOORBOARD PUNCTURED AND CORRODED. REPLACED FLOOR PANEL PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20030408000342003040800034SO 2003 4 8 SIMA200302904 120030128A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21647AE 145222 ORD - FLT 4240 - CREW REPORTED THE AFT HALF OF THE CABIN EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030408000522003040800052SO 2003 4 8 030011849 120030303A54111159P20502511 FRAME GULSTMG1159 G1159A 3970109SO LT PYLON CRACKED B Y3PRK NONE O OTHER ININSP/MAINT 1 SO35477SJ 477 LEFT HAND PYLON FRAME (WEB) AT FS 556 HAS 2 HORIZONTAL CRACKS RUNNING BETWEEN 2 HYDRAULIC LINE CONNECTIONS. SHEAR WEB PART NUMBER 1159P20502-511. CRACKS ARE WHERE THE FOLLOWING HYDRAULICS LINES ARE ATTACHED TO WEB WITH BULKHEAD FITTINGS: AE700755-1 (FLEX LINE), 1159P20518-103S20, 1159P20518-123-P-12, 1159P20518-7P12. 2L72 4F A12EA 20030331000432003033100043WP 2003 3 31 AALA20030191 120030211A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21276AA 49273 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE CROSSBAR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGH WIRE TO TAIL CONE CROSSBAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000482003033100048WP 2003 3 31 AALA20030210 120030219A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21560AA 53090 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7DEF INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEAT 7DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331001422003033100142NM 2003 3 31 DHL2003740528 120030221A5320 WEB BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 C-1 DOOR LOWER CUTOUT WEB HAS CORROSION. CORROSION ON WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED WEB FROM C1 DOOR LWR CUTOUT FOR REPLACEMENT IAW SRM 51-30-2, FABRICATED NEW WEB DIMENSIONS 60 INCHES X 4 INCHES USING 2024T3 .071 PO 9912182 IAW SRM 53-10-2 FIG 3. ALODINED & PRIMED NEW WEB IAW SRM 51-10-2. INSTALLED NEW WEB IAW SRM 51-30-2. 2L73 4F RTA3WE 20030331001432003033100143NM 2003 3 31 DHL2003740529 120030228A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 SKIN GOUGED AT STR 19R BS 1130-1148. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 4.2 INCHES X 1 INCH AND FABBED DOUBLER FROM 2024T3 .071 PO 9912182 DIM 11.3 INCHES X 10.5 INCHES IAW SRM 53-30-2 FIG 2 & 53-30-3 FIG 1. DOUBLER TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED IAW SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20030410000932003041000093NM 2003 4 10 SWAA030665 120030323A5310589357 WINDOW POST BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND CAPT'S UPPER WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20030410000962003041000096NM 2003 4 10 SWAA030668 120030323A3350311500 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 14 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20030410001062003041000106NM 2003 4 10 SWAA030678 120030324A53306545765 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 530, ABOVE STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030410001162003041000116SO 2003 4 10 SIMA200300803 120030104A5313 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21654AE 145437 ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-24-02, AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030410001232003041000123SO 2003 4 10 SIMA200303603 120030121A29103604481003 ACTUATOR EMB 145 EMB145LR 3260212SO RI WING LEAKING A SIMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21650AE 145417 ORD - FLT 4333 - DURING CLIMB, CREW REPORTED HYDRAULIC 1 QTY MESSAGE ON EICAS. QUANTITY DROPPED TO BOTTOM OF GAUGE AND A E1 HYDRAULIC PUMP FAIL MESSAGE SHOWED ON EICAS. CREW DECLARED AN EMERGENCY. AFTER GEAR WAS SELECTED DOWN PUMP FAIL MESSAGE WENT AWAY. AIRCRAFT WAS LANDED AND TAXIED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE FOUND AND REPLACED A SPOILER ACTUATOR FOR THE RIGHT SPOILER IAW EMB MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030410001332003041000133NM 2003 4 10 SWAA030682 120030325A291065445461473 HYDRAULIC LINE BOEING737 7372T4 1384492NM HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SW29721WN 22697 AIR TURNBACK, DURING TAKEOFF, A-SYSTEM HYDRAULICS FAILED, LOW QUANTITY AND PRESSURE INDICATED. FOUND HYD LINE ON LT MLG ACTUATOR FAILED. REMOVED AND REPLACED HYD LINE ON LT MLG ACTUATOR PER MM. SERVICED AND BLEED HYD SYSTEM, NO FURTHER LEAKS NOTED PER MM. 2L72 4F A16WE 20030410001472003041000147NM 2003 4 10 SWAA030701 120030328A335090083 BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP IN AFT CABIN. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030410001502003041000150 2003 4 10 SWAA030704 420030327A2565D31354 SLIDE BOEING737 7375H4 138449DNM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030410001512003041000151NM 2003 4 10 SWAA030705 120030327A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND BOTH LT/RT FUSELAGE FRAMES CRACKED AT BS 188, STR 17L AND 17R. REMOVED AND REPLACED FRAMES PER SRM. 2L72 4F RTA16WE 20030404001502003040400150 2003 4 4 SWAA030506 420030306A256522D22900 SLIDE BOEING737 7372H4 138448CNM R1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F A16WE 20030404001592003040400159NM 2003 4 4 SWAA030548 120030308A335010126211 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR VERTICAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030410001672003041000167SO 2003 4 10 SIMA200305004 120030212A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-20-01, 51-40-02, 51-20-03, EMB 145 CPM 51-21-04 THROUGH 51-21-06 AND AEAI ETN NR EB53-021R1. (M) 2L72 4F RTT00011AT 20030410001682003041000168SO 2003 4 10 SIMA200305008 120030217A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CETNER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB 135 SRM, SRM 145/1142 REV 20. (M) 2L72 4F RTT00011AT 20030410001812003041000181 2003 4 10 ET32003F00000 420030201A256418D172332 ASPIRATOR AIRCRUISERS BOEING747 747* NM INSIDE LIFE RAFTINOPERATIVE B ET34O OTHER O OTHER NRNOT REPORTED 1 WP07 8862379 RECEIVED SUBJECT LIFE RAFT IN AN (AS REMOVED) CONDITION FOR REGULARLY SCHEDULED MAINTENANCE. DURING PRELIMINARY INSPECTION, FOUND BOTH LIFE RAFT JET PUMP ASSEMBLY INLETS COMPLETELY BLOCKED OFF WITH ORANGE DUCT TAPE. SUCH BLOCKAGE WOULD PREVENT THE RAFT FROM INFLATING TO ITS DESIGN SHAPE AND PRESSURE. THIS RAFT IS BELIEVED TO HAVE BEEN LAST OVERHAULED OR SERVICED IN WA IN JUNE 2001. THIS LIFE RAFT IS OPERATED IS OPERATED BY POLAR AIR CARGO AND WAS REMOVED FROM A/C 853 FOR OVERHAUL DUE TO TIME. 2L74 4F RTA20WE 20030410001902003041000190NM 2003 4 10 GAIA03011OP 120030226A324142527D CONTROL BOX BOEING727 727223 1384074NM ANTI-SKID SYS INOPERATIVE A GAIAO OTHER O OTHER LDLANDING 1 SW076808 19483 ON LANDING, ALL FOUR TIRES WERE BLOWN. REMOVED AND REPLACED ANTI-SKID CONTROL BOX AND ALL 4 MAIN WHEEL ASSEMBLIES. INSPECTED AIR FRAME AND ENGINES FOR DAMAGE. NO DAMAGE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20030410001992003041000199WP 2003 4 10 GTIA030150 120030312A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DETERIORATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO STA 256 (7X56) LBL 15 INCHES FLOOR PANEL SOFT/MUSHEY DETERIORATED CORR INSERTS. FABRICATED NEW FLOOR BOARD. 2L72 4F4 FRTA6WE E2EA 20030410002042003041000204NM 2003 4 10 DL76G030233 120030310A3397 WIRE BOEING767 767332 1382001NM CABIN CHAFED A DALAK NONE L NO TEST ININSP/MAINT 1 SO271603 29695 EMERGENCY TRACK LIGHTING ON SEATS 10FG 11 FG 20 FG INOP. ALSO LARGE WHITE TRACK LIGHT LOCATED ON RT BULKHEAD AFT MID GALLEY AND LARGE WHITE TRACK LIGHT LOCATED RT SIDE MID LAV INOP. FOUND FWD EMERGENCY LIGHT ASSY ON SEAT 6FG SHORTED. REPLACED LIGHT ASSY, OPS CHECKS GOOD. 2L72 4F RTA1NM 20030410002092003041000209 2003 4 10 DL76G030258 420030320A34130665000011001 INDICATOR BOEING767 767332 1382001NM COCKPIT MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271607B 30388 APPROXIMATELY 6 HOURS AND 50 MINS INTO FLIGHT RIGHT VSI CB POPPED AND RIGHT GEN TRIPPED OFF SIMULTANEOUSLY. A SLIGHT ELECTRICAL SMELL WAS NOTED IN THE FLIGHT STATION. THIS DISSIPATED RAPIDLY. GEN WAS RESET SUCCESSFULLY AS PER THE QRH PROCEDURE. RIGHT VSI CB NOT RESET. VERIFIED ELECTRICAL ODOR FROM RT VSI. REPLACED VSI, RESET CB AND OPS CHECK NORMAL. PERFORMED BITE CHECK OF BPCU RT GEN FAULTS DP TRIP IDG RISE TEMP GEN/FDR MAIN BUS/OVERLAP ZONE. PER FIM24-20-00 CHECK FDRS FOR SHORTS, ALL OK. IDG SERVICED PER PDC. REPLACED RT GCU, RUN UP CHECK NORMAL. 2L72 4F RTA1NM 20030410002162003041000216NM 2003 4 10 DL76G030305 120030331A2597 WIRE BOEING767 7673P6 1385105NM CARGO BAY CHAFED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27155DL 25269 DURING L/O SERVICE, OPERATIONAL CHECK OF FWD CARGO COMPARTMENT NOTICED SPARKS AT STATION 500 UNDER FLOOR MATT AND THE FOLLOWING C/BS POPPED AT P35 PNL C166, C168 AND C169. MAINTENANCE IN PROGRESS REPAIRING WIRING. DAMAGE TO WIRING CAUSED BY A SPARE CARGO LOCK FALLEN INTO THE BOTTOM OF THE CARGO COMPARTMENT AND CHAFING ON WIRING. 2L72 4F RTA1NM 20030410002272003041000227NE 2003 4 10 BAQA085203 220030320A7323430121204 GOVERNOR BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101600A 41560NE ENGINE SPLIT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03952CJ119 7052 20 PERCENT TORQUE SPLITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030410002452003041000245NM 2003 4 10 F3LA200300027 120030124A2550 PANEL BOEING737 7373M8 1384615NM CARGO BAY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED TRANSITION PANEL IN AFT CARGO COMPARTMENT, FWD OF DOOR AT STA 767 TO 787, CORRODED AROUND FASTENER HOLES. FABRICATED AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM 51-40-02. 2L72 4F RTA16WE 20030414000092003041400009NM 2003 4 14 SWAA030723 120030331A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 663 AT STR 10R & BS 908 AT 4L. REMOVED AND REPLACED STR TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030414000122003041400012NM 2003 4 14 SWAA030734 120030402A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (3 EA) BS 360 AT STR 5L, BS 616 AT STR 4L AND BS 639 AT STR 4L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030414000172003041400017NM 2003 4 14 SWAA030745 120030402A53126546568 BULKHEAD BOEING737 7373G7 1384595NM AFT FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED BETWEEN 12 & 2 O'CLOCK POSITIONS. REPAIRED BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20030414000212003041400021NM 2003 4 14 SWAA030724 120030331A3350BR2013 COVER BOEING737 7373H4 1384600NM FWD CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED RON, FOUND EEPLS COVER MISSING IN FWD CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY SECTION PER MM. 2L72 4F RTA16WE 20030414000242003041400024NM 2003 4 14 SWAA030727 120030330A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030414000302003041400030NM 2003 4 14 SWAA030721 120030331A551065C25727 SKIN BOEING737 7375H4 138449DNM LT HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 DURING SCHEDULED C2 CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT FWD EDGE OF AFT SPAR. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030414000452003041400045 2003 4 14 CA030312020 420030311A342133211T GYRO BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4N HCE4N3 NE COCKPIT INTERMITTENT W A UNSCHED LANDING O OTHER CLCLIMB 1 CA (CAN) AIRCREW AT GATE REPORTED DIFFICULTY IN HAVING CAPTAINS ATTITUDE INDICATOR COMING ON LINE. A/C WAS TAXIED TO HANGAR WHERE MAINT REPLACED NR 1 VERTICAL GYRO. SYSTEM WAS TESTED AND A/C RETURNED TO GATE. AT APPROX 10,000 FT CAPTAINS ATTITUDE INDICATOR FLAGGED AND INFORMATION WAS TRANSFERRED FROM COPILOTS SIDE. CREW CONTACTED CENTRE AND REQUESTED RETURN TO AIRPORT. UNEVENTFULL LANDING WAS COMPLETED AND A/C WAS ONCE AGAIN BROUGHT TO HANGAR. AFTER INSPECTION THE NR 2 GYRO TAKEN TO AVIONICS SHOP AND TESTED AND THEN REPLACED.FOUND THAT THE NR 1 AND 2 GYRO CONNECTORS HAD BEEN PREVIOUSLY REVERSED. THE NR 1 GYRO WAS POWERING THE NR 2 SIDE AND AS SUCH WRONG GYRO WAS INITIALLY REPLACED. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030414000632003041400063SW 2003 4 14 ALGA085890 120030401A6220406310405101 UNIVERSAL BELL 407 407 1182206SW ROTOR HEAD ROUGH E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03527AL312 53211 BEARING ROUGH AND RATCHETY, REMOVED IAW 407 M/M. REMOVED AND REPLACED WITH NEW ASSY. BY FIEL MAINT. 1G71 3U O H2SW 20030414000722003041400072EU 2003 4 14 HE66085917 120030407A6330L633M2010101 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 FS01135CR763 0164 MAIN ROTOR GEARBOX MOUNT COMPLETELY FAILED. REPLACED. 1G72 3U H88EU 20030331001442003033100144NM 2003 3 31 DHL2003740530 120030228A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 SKIN CREASED BELOW STR 23R AT BS 1060. CUT OUT DAMAGED AREA DIM 6 INCHES X 3 INCHES AT BS 1060 STR 23R AND FABRICATED ONE DOUBLER DIMENSIONS 9.25 INCHES X 15.5 INCHES USING .071 2024T3 PO 9912182 IAW SRM 53-30-3 FIG 1. ALODINED AND PRIMED IAW SRM 57-10-2, INSTALLED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20030331001462003033100146NM 2003 3 31 DHL2003741002 120030301A2897 CONNECTOR BOEING727 7272Q9 138448MNM BOOST PUMP CONTAMINATED A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01741DH 21931 IN CRUISE, FL290 BOTH AFT BOOST PUMP LOW PSI LIGHTS ILLUMINATED IN THE FUEL TANK NR 2 AT THE SAME TIME BOTH CIRCUIT BREAKERS POPPED. PERFORMED ABNORMAL PROCEDURES. INSPECTED FUEL PUMPS AND PLUG CONNECTIONS, CLEANED AND RESET PLUGS, RESET BREAKERS, OPERATED PUMPS FOR 1 HOUR. OPS CHECKED GOOD PER M/M 28-31-00 & 20-11-0. 2L73 4F RTA3WE 20030401000062003040100006EA 2003 4 1 03089633 120030330A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27633BR 7274 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE AFT EMERGENCY FLOOR TRACK LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030401000262003040100026SO 2003 4 1 ASOA03046 120030206A33501317 LIGHT EMB 120 EMB120ER 3260203SO FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11503AS 120275 DURING A GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030401000542003040100054EA 2003 4 1 CA030221002 120030218A5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) FLT 5030 FROM SLC TO HLN, CAPTAINS WINDSHIELD SHATTERED AT FL 260. REPLACED WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20030401000752003040100075NM 2003 4 1 DHL2003741501 120030323A5330 SKIN BOEING727 727* NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21930 DISCREPANCY DURING C CHECK, FUSELAGE UPPER LOBE INTERIOR BS 680 AND CARGO DOOR LWR. SILL BEAM FRAME CRACKED FWD. AND AFT. ALSO MISSING FASTENERS (8 EACH). REMOVED FASTENERS IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED AREA AND FABRICATED ANGLE IAW B-727 SRM. 2L73 4F RTA3WE 20030401000832003040100083NM 2003 4 1 DHL2003745007 120030327A3260 SWITCH BOEING727 727224 1384076NM MLG DIRTY A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 AFTER TAKEOFF WHEN GEAR HANDLE SELECTED TO OFF, POSITION "R GEAR DOOR" LIGHT ON S/O PANEL ILLUMINATED AND RED GEAR DOOR LIGHT ON FORWARD PANEL ILLUMINATED - PERFORMED ABNORMAL PROCEDURES PER AOM, LIGHTS EXTINGUISHED. RT MLG DOOR WARNING SWITCH INSPECTED AND CLEANED. SYSTEM TESTED IAW M/M 32-62-11, WITH NO DEFECTS. 2L73 4F A3WE 20030401000872003040100087NM 2003 4 1 03090405 120030331A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27405FJ 3155 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030401001202003040100120WP 2003 4 1 DHL2003804512 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART WITH 1 IN CRACK AT STA XFS 760.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030402000382003040200038NM 2003 4 2 2003UALA00313 120030323A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29954UA 26739 FUSELAGE FRAME LOCATED AT BS 907 DAMAGED BETWEEN STRINGERS S21-RT AND S22-RT. MAJOR REPAIR ACCOMPLISHED. DOUBLER APPLIED. 2L72 4F4 FRTA16WE E2GL 20030402000732003040200073NM 2003 4 2 AMTA200300183 120030205A492038002981 APU BOEING757 75733N 1384931NM APU BAY INOPERATIVE A AMTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL11557TZ2691 32591 APU HAD AUTO SHUT DOWN FAULT LIGHT ILLUMINATED AND EICAS MSG APU FAULT DISPLAYED. NEXT START ATTEMPT NORMAL, THEN FAILED AGAIN WITH AUTO SHUTDOWN. COMPLIED WITH M 57-49-02 SHEET. REMOVED AND REPLACED APU. (M) 2L72 4F RTA2NM 20030403001282003040300128NM 2003 4 3 DL733030303 120030331A5753 STRUCTURE BOEING737 737347 1384647NM RT WING TE FLAP DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO273301 23181 INBOARD FORE FLAP DELAMINATED. REPAIRED PER ER/A 422922-14. 2L72 4F RTA16WE 20030407000862003040700086SO 2003 4 7 SIMA200306406 120030226A531014525381003 BEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 ABI - DUIRNG AN IMBV INSPECTION, THE CABIN CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 25. REMOVED CORROSION BY CREATING A 5.2 INCH BY 2.75 INCH BY.5 INCH CUTOUT. FABRICATED A Z-SHAPED DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM (SRM 145/1145 REV 20) 53-22-10 FIG 201 SHEET 1 AND INFORMATION CONTAINED IN AMERICAN EAGLE AIRLINES ETN EB 53-032R1 PARA 6 FOR ALTERNATE FASTENERS. (M) 2L72 4F RTT00011AT 20030407000972003040700097NM 2003 4 7 TSAA0353004 120030130A53136546524 STRINGER BOEING737 7372M6C 1384708NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 EXTERIOR 1 INCH FUSELAGE CRACK AT BS 375 AT STRINGER 15L. TRIMMED OUT DAMAGE. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIMMED AREA BY .040 INCH INSURANCE CUT. HFEC ROTARY AND SURFACE PROBLE INSPECTED FASTENER HOLES ALONG STRINGER 15R UNDER THE REPAIR COMMON TO LAP MODIFICATION. REPAIR COMPLETED IAW ECO 33360 AND BOEING SB 737-53A1177. (M) 2L72 4F RTA16WE 20030408000012003040800001EA 2003 4 8 2003F00208 120030219A3260852701 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0797325 7325 FLT 6901 - PHX - AFTER TAKEOFF, THE PILOT RAISED THE GEAR HANDLE AND RECEIVED A GEAR DISAGREE MESSAGE. PILOT PUT HANDLE IN THE DOWN POSITION AND RECEIVED A GEAR DOWN MESSAGE. RETURNED TO THE FIELD AND LANDED SAFELY. MAINTENANCE DISCOVERD A BENT PROXIMITY SENSOR BRACKET ON THE NOSE GEAR. MAINTENANCE REPLACED THE PROX SENSOR BRACKET. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030408000062003040800006WP 2003 4 8 ASAA0380080 120030113A5250592600335 HINGE DOUG DC9 DC983 3022083WP BARRIER DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY BARRIER DOOR HINGE IS CRACKED. REPLACED HINGE PER SRM 51-30-1. (M) 2L72 4F RTA6WE 20030408000082003040800008WP 2003 4 8 ASAA0380082 120030113A53105936442U3 TORQUE BOX DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, TORQUE BOX WEB UPPER SURFACE CORRODED AT FS 1212. REPLACED WEB SECTION PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20030408000302003040800030SO 2003 4 8 SIMA200302704 120030127A335066903 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A SIMAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SW21802AE 145471 BGR - FLT 4620 - MAINTENANCE FOUND THE LEFT FORWARD FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A LIGHT STRIP IN THE FORWARD CABIN IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030408000472003040800047NM 2003 4 8 USAABB03025 120030222A33508731002511REV15 LIGHT BOEING757 757225 1384959NM R1 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19606AU 22202 EWR - FOUND R1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030408000552003040800055NM 2003 4 8 0300686302 120030403A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 10JK-DOOR 2R. RECONNECTED WIRES AND OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030408000582003040800058CE 2003 4 8 0300719927 120030401A2910 LINE CESSNA177 177RG 2073709CE HYD PUMP RUPTURED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL0145835 177RG0756 INBOUND TO RIC THE LEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AND PRESSURE WENT TO ZERO. CREW CONTINUED TO DESTINATION AND PERFORMED MANUAL GEAR EXTENSION ON APPROACH. ALL COM PROCEDURES COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. MAINTENANCE INSTALLED GEAR PINS AFTER LANDING AND THE AIRCRAFT WAS TOWED TO THE GATE. A TEMPORARY HYDRAULIC LINE WAS FOUND TO HAVE RUPTURED IN THE LEFT WING TRAILING EDGE AREA AND WAS REPLACED. NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND FILTERS WERE ALSO REPLACED. AIRCRAFT HAS RETURNED TO SERVICE. 1H71 3O A20CE 20030408000612003040800061EU 2003 4 8 03092308 120030402A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27308UE 41023 DURING MAINTENANCE/INSPECTION FWD EMERGENCY LT STRIP SECTION LOOSE. MAINTENANCE PERSONNEL REINSTALLED LIGHT RETAINING STRIP. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20030408000632003040800063NM 2003 4 8 03093411 120030403A3350 LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE CABIN OUT OF ADJUST A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27411FJ 411FJ DURING MAINTENANCE INSPECTION CREW NOTED EMERGENCY LIGHTS OUT. MAINTENANCE PERSONNEL ADJUSTED FLOOR EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030408000642003040800064EA 2003 4 8 03093623 120030403A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27623BR 7192 DURING MAINTENANCE INSPECTION LT FWD EMERGENCY EXTERIOR LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED BULB TO LT FWD WING EMERGENCY EXTERIOR LIGHT. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURN TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030408000652003040800065EA 2003 4 8 03093644 120030403A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27644BR 7379 DURING MAINTENANCE INSPECTION EMERGENCY LIGHT BY AIRSTAIR 2 BULBS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED LIGHT BULBS. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030408000672003040800067EU 2003 4 8 03095305 120030405A33501317 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27305UE 41019 DURING MAINTENANCE INSPECTION, THE L/H EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20030408000852003040800085WP 2003 4 8 03FDEA00394 120030405A5350 SEAL DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE TAIL CONE CRACKED A FDEAK NONE O OTHER LDLANDING 1 SO25317FE 46835 NR 655 TAILCONE FWD UPPER LT METAL SEAL CRACKED ANS CHAFED. CLOSING ACTION ON 04/05/03. REMOVED LT FWD UPPER METAL SEALS 2EA. FROM TAILCONE IAW SRM 51-31-01, RECEIVED REPLACMENT SEALS ON ATTACHED TRAVELER NR T2/324508. INSTALLED REPLACEMENT SEALS IAW SRM 51-31-01. 2L73 4F4 F A22WE E23EA 20030401000152003040100015WP 2003 4 1 AALA20030002 120030103A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY WALL MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000322003040100032EA 2003 4 1 ASOA03052 120030209A2700SB140981 SEAL CNDAIRCL600 CL6002B19 1900309EA WING LEAKING A ASOAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11884AS 7513 DURING CLIMB-OUT FROM XNA-ATL, WHILE RETRACTING THE FLAPS, THE CREW RECEIVED AN AMBER CAUTION FLAPS FAIL MESSAGE. AN EMERGENCY WAS DECLARED. THE FLAPS FAILED AT ZERO DEGREES AND A ZERO FLAPS LANDING WAS ACCOMPLISHED IN ATL WITHOUT INCIDENT. MAINTENANCE RE-RIGGED THE ENTIRE FLAP SYSTEM, REMOVED MOISTURE FROM THE BRAKE POSITION SENSOR UNIT FLEX SHAFTS AND REPLACED THE TEFLON SEALS ON THE FLEX SHAFTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000562003040100056NM 2003 4 1 CA030221010 120030219A4920 COOLING FAN BOEING737 737217 1384464NM PWA JT8 JT8D17A 52049NE APU UNSECURE W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN) JUST BEFORE PUSH BACK, CABIN RAPIDLY FILLED WITH SMOKE (NON ELECTRICAL IN NATURE). A/C WAS DEPLANED VIA THE LOADING BRIDGE AND SHUT DOWN TO BATTERY. MAINT FOUND THE APU OIL TANK EMPTY AND INLET PLENUM CONTAMINATED WITH OIL. FOUND APU COOLING FAN HAD DEPARTED ITS SHAFT BUT WAS CONTAINED IN HOUSING. COOLING FAN SUPPLIES COOLING AIR TO APU OIL COOLER AND APU GENERATOR ASSY. APU ASSY WAS REPLACED AND A/C EFFECTED BLEED DUCTING PURGED/CLEANED. COOLING FAN SHAFT THREADS WERE NOT DAMAGED. RETAINING NUT BACKED OFF AND THE FAN MIGRATED OFF THE SHAFT. IT IS UNCLEAR AT THIS POINT HOW THE APU OIL WAS ABLE TO CONTAMINATE THE BLEED SYSTEM. FURTHER INFORMATION WILL FOLLOW AFTER THE APU TEARDOWN REPORT IS RECEIVED2L72 4F4 F A16WE E2EA 20030401000992003040100099NM 2003 4 1 DHL2003755001 120030123A3260 PROXIMITY SENSOR BOEING727 727225 1384077NM MLG DIRTY A DHLAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO01755DH 21857 LT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR SELECTED DOWN (PRIMARY). SECONDARY MAIN GEAR LIGHTS DID ILLUMINATE. CREW PERFORMED THE ABNORMAL PROCEDURE AND MADE NORMAL LANDING. ON FINAL APPROACH LIGHT ILLUMINATED. CLEANED PROXIMITY SENSOR PER M/M 32-61-01, AND OPS CHECKED GOOD. 2L73 4F A3WE 20030401001082003040100108WP 2003 4 1 DHL2003803005 120030330A2611 SMOKE DETECTOR DOUG DC8 DC873 302199CWP NR 4 WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01803DH 46123 NR 4 SMOKE DETECTOR WILL NOT TEST. DEFERRED PER MEL 26-6-1. CAT. "C". THIS IS DMI 12416. NR 4 SMOKE DETECTOR WILL NOT TEST REF. DMI 12416. REMOVED AND REPLACED NR 4 SMOKE DETECTOR BULBS PER M/M 26-10-5. SYSTEM OPS CHECKED GOOD. THIS CLEARED DMI 12416. 2L74 4F RT4A25 20030401001172003040100117WP 2003 4 1 DHL2003804509 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART CRACKED 1 IN AT STA XFS. 722.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001642003040100164WP 2003 4 1 DHL2003804773 120030228A575556551681 SKIN DOUG DC8 DC873F 302199FWP NR 4 SPOILER WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING, REMOVAL AND RE-INSTALLATION OF NR 4 SPOILER PANEL, EXTERNAL SKIN WORN 4.00 INCH. R & R NR 4 SPOILER PANEL ON L/H WING IAW 27-61-1 PG. 201-207 FOR OPS CK SEE N/R 0607 2L74 4F RT4A25 20030403001102003040300110NM 2003 4 3 DL72S030300 120030329A323065235996 CONTROL VALVE BOEING727 727232 1384082NM WHEEL WELL LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27533DA 22046 SHORTLY AFTER T/O SYS-A HYD LOW PRESS LIGHT ILLUM. FOUND LANDING GEAR CONTROL VALVE LEAKING AT FITTING. REPLACED FITTING AND O-RING. 2L73 4F A3WE 20030404000142003040400014NM 2003 4 4 CALA0300161 120030401A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716301 23352 INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R CORRODED AT BS 1010. REPAIRED IAW SRM 51-40-02 AND B737-300 AMM 20-50-11. 2L72 4F RTA16WE 20030404000192003040400019NM 2003 4 4 CH1A200394007 120030224A2910BACH8B04NN0157 HOSE BOEING727 727290 138408WNM HYD SYSTEM LEAKING A C1HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL15294AS 22146 NOTICED HYDRAULIC "A" SYSTEM PRESSURE AND FLUID LOSS SHORTLY AFTER FLAP RETRACTION DURING DEPARTURE FROM MBJ 2L73 4F A3WE 20030404000532003040400053NM 2003 4 4 DL757030189 120030221A5330146N31111 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27652DL 24392 ACCOMPLISHMENT OF AN ANTENNA CUTOUT DOUBLER MODIFICATION RESULTED IN DAMAGE TO THE CUTOUT. THE ANTENNA CUTOUT IS LOCATED AT FS 1350 BETWEEN STRINGERS 1 & 2R. THE CUTOUT WAS ENLARGED TO REMOVE THE DAMAGE. TWO EXTERNAL DOUBLERS WERE INSTALLED TO REPAIR THE LARGER CUTOUT PER ER/A 384512 -14, REV A. 2L72 4F RTA2NM 20030404001452003040400145NM 2003 4 4 SWAA030493 120030303A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29782SA 29808 DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT ROW 23. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20030404001802003040400180NM 2003 4 4 SWAA030586 120030314A52406529994 GUIDE ARM BOEING737 737301 1384611NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 FWD SERVICE DOOR ONLY OPENED PARTIALLY. ADJUSTED UPPER GUIDE ARM PER MM. 2L72 4F RTA16WE 20030408000902003040800090NE 2003 4 8 049363 220030401A7200PT6A67DPS ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT FAILED A AMWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE07138YV9114 9114 UE138 WHEN CLEARED FOR TAKEOFF ON FLIGHT 9492, THE CREW ADDED POWER FOR TAKEOFF THEY HEARD AN ODD SOUND FROM THE LEFT ENGINE. IT SOUNDED LIKE A MUFFLED SHOTGUN BLAST. THE CREW ABORTED TAKEOFF AND TAXIED BACK TO THE GATE WITH NO FURTHER INCIDENT. THE ITT AND PROP RPM VARIED UP AND DOWN ON THE TAXI IN. ON SHUTDOWN THE LEFT ENGINE MADE A LOUD VACUUM CLEANER SOUND. MAINTENANCE REMOVED AND REPLACED THE ENGINE. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T4 TRTA24CE E26NE 20030408001022003040800102EA 2003 4 8 2003F00212 120030210A2760 SPOILER CNDAIRCL604 CL604 1900301EA WINGS INOPERATIVE A DHLAO OTHER J WARNING INDICATION LDLANDING 1 GL23599DA 5498 GROUND SPOILERS DID NOT DEPLOY AT KPTK. NONE, EXTENSIVE TROUBLESHOOTING IN WORK. (M) 2L72 4F RTA21EA 20030408001252003040800125WP 2003 4 8 AMTA200300221 120030213A3350 PIN LKHEED1011 10113853 5265020WP CONNECTOR LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11162AT 1220 FOUND EGRESS LIGHTS INOPERATIVE FROM SEAT ROW 6 HJK TO 11 HJK. RECONNECTED PIN TO SOCKET AT ROW 10, SYSTEM OPS CHECK OK. (M) 2L73 4F A23WE 20030408001342003040800134NM 2003 4 8 AWXA200300340 120030323A5420311A1680173 ANGLE BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON ANGLE OF LT PYLON, OUTBOARD OF NR 1 ENGINE AFT MOUNT. MAINTENANCE REMOVED CRACKED ANGLE ON LT PYLON, OUTBOARD OF NR 1 ENGINE AFT MOUNT; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 311A1680; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3 & 4. 2L72 4F4 FRTA16WE E2GL 20030408001372003040800137NM 2003 4 8 AWXA200300343 120030403A5320BAC1509100146 FLOOR SUPPORT BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE CABIN CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2.3125 INCH CRACK WAS FOUND ON FLOOR SUPPORT CHANNEL IN AFT CARGO COMPARTMENT BS 727D, LBL 3. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT CHANNEL IN AFT CARGO COMPARTMENT BS 727D, LBL 3; FABRICATED A 2 EACH REPAIR ANGLES AND A CHANNEL FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG. 201, PG. 201-202. 2L72 4F4 FRTA16WE E2GL 20030408001382003040800138NM 2003 4 8 AWXA200300344 120030320A33971721602 CONNECTOR BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - EEL - DURING C-17 CHECK NUMEROUS SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT CONNECTORS AND WIRES WERE FOUND DAMAGED BETWEEN BS 344 AND BS 947. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS BETWEEN BS 344 AND BS 947 IAW SWPM 20-42-01, PG. 1-6, SWPM 20-30-12, PG. 276-277. OPERATIONAL CHECK WAS GOOD. PART NAME; CONNECTOR, MFG; BRUCE INDUSTRIES, P/N; 172168-1, COND. DAMAGED. 2L72 4F4 FRTA16WE E2GL 20030409000072003040900007NM 2003 4 9 AWXA200300350 120030313A575465C2660399 SKIN BOEING737 7373S3 1384711NM NR 3 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK THE NR 3 LEADING EDGE SLAT UPPER SURFACE WAS FOUND DELAMINATED AT THE INBOARD CORNER. MAINTENANCE REMOVED THE NR 3 LEADING EDGE SLAT; PERFORMED COMPOSITE REPAIR OF THE INBOARD CORNER PER B737-300 SRM 51-70-10, FIG. 32, REPAIR 23; INSTALLED SLAT AND RIGGED SYSTEM IAW BMM 27-81-21, PG. 401-419. 2L72 4F RTA16WE 20030407000112003040700011 2003 4 7 ASAA0380066 420030113A25653961896501 LANYARD DOUG DC9 DC983 3022083WP DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 SEA - DUIRNG PREFLIGHT CHECK, FOUND FORWARD SERVICE R-1 DOOR SLIDE LANYARD BETWEEN HAD BECOME DISCONNECTED. REATTACHED LANYARD. (M) 2L72 4F RTA6WE 20030407000162003040700016WP 2003 4 7 ASAA0380071 120030112A53215936603501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, FLOOR PANEL CORRODED IN AFT CARGO BAY. REPLACED PANEL PER SRM 51-10-2 AND 51-10-3. (M) 2L72 4F RTA6WE 20030407000192003040700019WP 2003 4 7 ASAA0380074 120030112A5230592600335 HINGE DOUG DC9 DC983 3022083WP CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY BARRIER DOOR HINGE CRACKED. REPLACED HINGE PER SRM 51-30-1. (M) 2L72 4F RTA6WE 20030407000452003040700045WP 2003 4 7 GTIA030033 120030113A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND AFT FUSELAGE STATION 1463 RIGHT SIDE INBOARD FACE CANTED WEB CRACKED. REMOVED CRACKED WEBS. FABRICATED WEBS DOUBLE SKIN FROM .050, 7075-T6. INSTALLED FABRICATED DOUBLE WEBS AND 5 STIFFENERS AT STATION 1463 RIGHT SIDE BETWEEN LONGERON 7-13. (M) 2L72 4F RTA6WE 20030407000532003040700053NM 2003 4 7 MEX2003018 120030130A2400 WARNING LIGHT DOUG MD88 MD88 3023688NM RT GENERATOR ILLUMINATED A ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23162PL 49765 FLT 600 - MEX-ATL - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT GENERATOR FAILURE. IN PLATFORM, ENGINES WERE SHUTDOWN. RIGHT GENERATOR WAS INSPECTED NO DAMAGE WAS FOUND. ENGINES WERE STARTED IAW MM 24-20-01, ALL CORRECT. (M) 2L72 4F RTA6WE 20030407001082003040700108NM 2003 4 7 UIEA200300012 120030225A542065B89058502 STIFFENER BOEING747 747243B 1384830NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15540MC 22508 DURING CURRENT C-CHECK AT SIAEC, FOUND NR 4 PYLON NR 3 LONGITUDINAL STIFFENER VERTICAL FLANGE, BELOW PRECOOLER EXHAUST VENT, CRACKED THREE PLACES AT NAC 245, 247 AND 257. PYLON PREVIOUSLY MODIFIED PER SB 747-54-2163 AND 747-54-2091 WHICH CONSISTS OF AN UPPER ANGLE INSTALLED ON THE STIFFENER FROM NAC 234 TO 272 ALONG WITH AN EXTERNAL SKIN DOUBLER. ADDITIONAL REPAIR CONSISTS OF A LOWER ANGLE INSTALLED FROM NAC 234-252. CRACK AT NAC 257 MAY BE LEFT AS IS. HFEC INSPECTED ALL OPEN HOLES COMMON TO BOTH ANGLES AND HOLES IN THE REMAINING REPAIR. NO ADDITIONAL CRACKING FOUND ON STIFFENER OF ALUMINUM SKIN. REPAIR ANGLE INSTALLED PER STANDARD SRM PRACTICES IAW S/B'S MENTIONED ABOVE. (M) 2L74 4F A20WE 20030408000372003040800037EA 2003 4 8 SIMA200304302 120030209A30106643640019 VALVE CNDAIRCL600 CL6002C10 1390015EA LT WING INOPERATIVE A SIMAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SW21504AE 10044 HOU - FLT 3812 - CREW REPORTED A LEFT BLEED DUCT WARNING AFTER TAKEOFF. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS RETURNED TO HOU. THE BLEED SELECTED MESSAGE WENT OUT. MAINTENANCE REMOVED AND REPLACED THE LEFT WING ANTI-ICE VALVE IAW CRJ MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030408000382003040800038NE 2003 4 8 SIMA200304805 220030212A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT MALFUNCTIONED A SIMAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW21341SB 340B341 GEE785559 SBA - FLT 3280 - CREW REPORTED SHUTTING DOWN THE RIGHT ENGINE DUE TO EXTREME UNCONTROLABLE SURGING WITH ACCOMPANYING ITT SPIKE AND TORQUE FLUCTUATIONS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW SAAB MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20030408000452003040800045NM 2003 4 8 USAABB03023 120030218A3350 BATTERY BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19630AU 27808 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 6, 9, 13, 23, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030408000562003040800056 2003 4 8 0300691236 420030402A2565 RESERVOIR DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE ESCAPE SLIDE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01236NW 46934 DURING SLIDE SHOP TEST FOUND RESERVOIR COMPLETELY DEFLATED. FIRING LANYARD WAS INTACT. CAUSE OF CYLINDER DEFLATION COULD NOT BE DUPLICATED. INSTALLED OVERHAULED CYLINDER AND RETURNED SLIDE TO SERVICE. 2L73 4F4 F A22WE E23EA 20030408001302003040800130EU 2003 4 8 AWXA200300336 120030405A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 9 LT BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28651AW 866 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030408001322003040800132EU 2003 4 8 AWXA200300338 120030331A5321D5367005100400 FLOOR PANEL AIRBUS320 A320231 3930325EU CABIN CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A DAMAGED SCREW INSERT, AND 1 1/2 INCH CRACK WERE FOUND ON AFT LAVATORY FLOOR PANEL (261 PF). MAINTENANCE PERFORMED COMPOSITE REPAIR OF CRACK, AND REPLACED DAMAGED SCREW INSERT ON AFT LAVATORY FLOOR PANEL (261 PF) IAW A320 SRM 53-02-00. 2L72 4F RTA28NM 20030410000332003041000033NM 2003 4 10 SWAA030609 120030317A324426066712 TIRE BOEING737 7373H4 1384600NM RT MLG SEPARATED A SWAAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SW29630WN 27705 AIR TURNBACK, UNSAFE RT MLG LIGHT AFTER T/O, LOWERED GEAR GOT THREE GREEN LIGHTS. FOUND NR 4 MAIN TIRE RECAP CAME OFF DURING T/O ROLL AND DAMAGED THE INNER/CENTER RT MLG DOOR, NOT ALLOWING GEAR DOOR TO FULLY RETRACT. REMOVED INNER/CENTER DOOR AS PER CDL. REMOVED AND REPLACED NR 4 MLG TIRE & WHEEL ASSY PER MM. 2L72 4F RTA16WE 20030410000392003041000039NM 2003 4 10 SWAA030617 120030317A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STR TIE CLIP PER SRM. 2L72 4F RTA16WE 20030410000402003041000040NM 2003 4 10 SWAA030623 120030318A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29790SW 30604 EEPLS INOP IN FWD CABIN. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20030410000452003041000045NM 2003 4 10 SWAA030633 120030318A53306545800219 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT LOWER AFT CORNER OF AIRSTAIR CUTOUT, BS 350 BELOW STR 20L. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030410000462003041000046WP 2003 4 10 GTIA030090 120030205A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT FORWARD CABIN STATION 150-200 LBL 6 IS CORRODED. FABRICATED REPLACEMENT FLOOR SUPPORT. (M) 2L72 4F A6WE 20030410000552003041000055 2003 4 10 SWAA030639 420030320A256522D22901151 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED WHEN OPENING THE DOOR. MX FERRY TO MCO, REMOVED AND REPLACED SLIDE PER MM. 2L72 4F A16WE 20030410000652003041000065NM 2003 4 10 SWAA030645 120030320A335010126211 LIGHT BOEING737 7373T5 1384608NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C3 CHECK, FOUND SEVERAL LOWER EMERGENCY EXIT LIGHTS AT BOTH CABIN SVC DOORS AND FWD ENTRY DOOR LAMPS INOP. RELAMPED EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20030410000662003041000066WP 2003 4 10 GTIA030099 120030203A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND AFT PIT CORROSION AT FRAME SECTION STATION 1155, 1165, 1193 AND 1174, RIGHT SIDE. MATERIAL LOSS OUT OF LIMITS FS 1165 T-CLIP AND FS 1193 T-CLIP. LOCATED AND DRILLED TWO NEW CLIPS. INSTALLED TWO NEW CLIPS. (M) 2L72 4F A6WE 20030410000692003041000069WP 2003 4 10 GTIA030101 120030212A5310 STRUCTURE DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND IN PAX CABIN CORROSION AT FS 258 LONGERON 18R. FABRICATED REPAIR FILLER AND REPAIR DOUBLER. REPAIR PARTS INSTALLED. (M) 2L72 4F A6WE 20030410000752003041000075WP 2003 4 10 GTIA030103 120030222A2612 FIRE LOOP DOUG DC9 DC982 3022082WP RT ENGINE MALFUNCTIONED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DTW - FOUND RIGHT ENGINE LOOP A LIGHT ON WOULD NOT GO OUT IN FLIGHT. RIGHT ENGINE LOOP REMOVED AND REPLACED LOOP AS REQUIRED, OPS CHECK GOOD. (M) 2L72 4F A6WE 20030410000822003041000082NM 2003 4 10 SWAA030655 120030321A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29420WN 29825 DURING SCHEDULED C3 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED AT ROW 1. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20030410000912003041000091NM 2003 4 10 SWAA030663 120030322A575465C26602264A SLAT BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2L72 4F RTA16WE 20030410000942003041000094NM 2003 4 10 SWAA030666 120030323A33506104781 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED SPECIAL VISIT, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030410001262003041000126EU 2003 4 10 SIMA200304803 120030214A3350 WIRE SAAB SF340 340B 7860101EU EMERGENCY LIGHT LOOSE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21381AE 340B381 SGF - FLT 3589 - FLIGHT ATTENDANT REPORTED TO CREW THAT A FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT ROW 6A WAS LOOSE AND INOPERATIVE. MAINTENANCE CONNECTED LEAD TO STRIP AND REATTACHED STRIP TO FLOOR IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE CHANGED. (M) 2L72 4T RTA52EU 20030410001432003041000143NM 2003 4 10 SWAA030697 120030326A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 937 AT STR 23R AND BS 975 AT STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001492003041000149NM 2003 4 10 SWAA030703 120030327A14306557463 FASTENER BOEING737 7373Y0 1384671NM GIRT BAR FITTNG WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. REMOVED AND REPLACED FASTENER PER SRM. 2L72 4F RTA16WE 20030404001232003040400123NM 2003 4 4 GAIA03009OP 120030218A2612 WIRE BOEING727 727222 1384073NM NR 2 ENGINE SHORTED A GAIAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SW07180AX 20041 FLT 206 - DFW-IAH - ON APROACH TO IAH, THE FIRE WARNING BELL SOUNDED, AFTER SILENCING THE BELL THE FLIGHT CREW OBSERVED THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS SHUTDOWN AND THE ENGINE FIRE EXTINGUISHER BOTTLES WERE DISCHARGED. INSPECTION REVEALED THAT THE GROUND DETECTION WIRING SHORTED OUT ON AN AIR DUCT AND NO FIRE DAMAGE. THE WIRING WAS REPAIRED THE WIRE BUNDLE WAS REPOSITIONED AND THE ENGINE FIRE EXTINGUISHER BOTTLES WERE REPLACED. THE FIRE DETECTION AND ENGINE OPS CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030404001362003040400136NM 2003 4 4 SWAA030415 120030222A53126545409 PRESSURE PANEL BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 30. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20030404001522003040400152 2003 4 4 SWAA030533 420030310A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030404001532003040400153NM 2003 4 4 SWAA030534 120030308A575465C2660297 SLAT BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT OTBD END. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20030404001712003040400171 2003 4 4 SWAA030567 420030313A2565D31354 SLIDE BOEING737 7375H4 138449DNM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030410001642003041000164 2003 4 10 SWAA030718 420030330A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030410001722003041000172NE 2003 4 10 EGR2003F00002 220030211A7297 WIRE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE NR 2 ENGINE CHAFED E EGRAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA17760AF 760523 NR 2 ENGINE DECU FAULT, T 1 FAILURE IN FLIGHT, ENROUTE. FOUND CHAFED WIRE. REPLACED HARNESS. 1G72 3U3 UNCH1NE E19EU 20030410001752003041000175SO 2003 4 10 EKI2003F00000 120030306A2822IC69 PUMP PIPER PA31 PA31P 7103120SO LYC O541 TIGO541* 41539EA FUEL BOOST FAILED A EKIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP07647SC 31P7300129 AFTER INSTALLATION, DURING FUNCTION GROUND CHECK, BOOST PUMP CIRCUIT BREAKER TRIPPED AFTER APPROXIMATELY 1 MINUTE OF OPERATION. REMOVED PUMP AND INSPECTED FOR BLOCKAGE, FOUND NONE. INSTALLED AND ATTEMPTED GROUND CHECK AGAIN. PUMP MOTOR WOULD SLOW DOWN AFTER 1 MINUTE AND TRIP CIRCUIT BREAKER. REMOVED PUMP FOR WARRANTY. PUMP OVERHAULED BY FLEET SUPPORT SERVICES. (NE5D064N) 1L72 3O3 O A8EA E19EA 20030410001872003041000187SO 2003 4 10 FPI2003F00007 220030324A7414 BEARING CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO MAGNETO LOOSE E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO152013S 193 F02JA110R 21060981 295225R BEARING IN DISTRIBUTOR BLOCK BECAME LOOSE, DISTRIBUTOR GEAR JUMPED TIME, MAGNETO FAILED. (FACTORY REMAN ENGINE AND ACCESSORIES) 1H71 3O3 O 3A21 E5CE 20030410001942003041000194SW 2003 4 10 GCH2003F00000 120030218A7603 THROTTLE BELL 206 206L1 1182107SW ALLSN 250C 250C* GL ENGINES OUT OF ADJUST E GCHAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP195745Y 45531 PART 91 FLIGHT OPERATIONS, AIRCRAFT WAS OVERTORQUED TO 123.4 PERCENT DURING TAKEOFF. MECHANIC INVESTIGATED, FOUND THROTTLE FRICTION HIGH ON MAXIMUM FUEL SETTING AND DID NOT ALLOW FOR POSITIVE CONTACT OF FUEL CONTROL STOPS. 1G71 3U3 U H2SW E4CE 20030410002002003041000200WP 2003 4 10 GTIA030151 120030221A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DETERIORATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO STA 256 (CENTER) FLOOR PANEL SOFT/DAMAGED, DETERIORATED CORE INSERTS. FABRICATED NEW FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20030410002012003041000201NM 2003 4 10 DL76G030231 120030310A2750S256T00611 CONTROL MODULE BOEING767 767332 1382001NM T/E FLAP MALFUNCTIONED A DALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO271611B 30595 TRAILING EDGE FLAP DISAGREE JUST AS FLAPS APPROACHED ONE DEGREE ON FLAP RETRACTION. REPLACED FSEU PER M/M 480771. ADJUSTED FLAP TRANSMITTER 4 AND 5. REMOVED AND REPLACED T/E FLAP PDU CONTROL VALVE MODULE. PERFORMED T/E FLAP PDU TEST AND FLAP/SLAT SHUTOFF VALVE MODULE TEST PER MM, TESTS CHECK OUT GOOD. 2L72 4F RTA1NM 20030410002082003041000208WP 2003 4 10 GTIA030157 120030312A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 196 LBL 44 TO 54 FLOOR SUPPORT CORRODED/ELONGATED HOLES. FABRICATED, LOCATED, AND DRILLED NEW FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030410002122003041000212WP 2003 4 10 GTIA030159 120030207A5313 LONGERON DOUG DC9 DC981 3022081WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 MID CARGO STR 30 CORRODED FS712 TO 598. REMOVED LONGERON 30 FROM STA 590 TO 741. REMOVED LONGERON 30 STA 741 TO 759. FABRICATED NEW LONGERON SECTION FROM FUSELAGE STA 590 TO 662. FABRICATED FORWARD LONGERON SPLICE. FABRICATED NEW LONGERON SECTION FROM FUSELAGE STA 662 TO 759. LOCATED AND DRILLED LONGERON 30 SPLICE REPAIR STA 653-673. INSTALLED SPLICE REPAIR (L NR30 STA 653-673). INSTALLED LONGERON 30 FROM STA 590-759. 2L72 4F4 F A6WE E2EA 20030410002132003041000213NM 2003 4 10 DL76G030273 120030323A2530828450407 OVEN BOEING767 7673P6 1385105NM GALLEY DIRTY A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271501P 24983 F/A REPORTED MINOR SMOKE IN FWD GALLEY. PULLED C/BS. SUSPECT FOOD AS CAUSE AFTER EXAMINATION. FOUND FWD GALLEY OVEN HAS LARGE AMOUNTS OF CHOCOLATE AND CARAMEL. CLEANED OVEN. NO FURTHER SIGNS OF SMOKE DURING OPS CHECK. 2L72 4F RTA1NM 20030410002572003041000257NM 2003 4 10 F3LA200300041 120030128A532065479573 SILL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO DOOR SILL CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15. INSTALLED REPAIR PARTS PER SRM 53-60-15 AND 51-40-02. 2L72 4F RTA16WE 20030410001762003041000176NM 2003 4 10 DHL2003741506 120030322A5320 STRUCTURE BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, LEFT MLG W/W FWD STA 870 O/B STRUCTURE CRACKED OUT FASTENER. REMOVED WEB AT LEFT MLG WHEEL WELL BS 870 FWD O/B STRUCTURE IAW B-727 SRM 51-30-2. PART MADE IAW B-727 SRM 51-20-1 AND 53-10-2 FIG 5. INSTALLED WEB AT LEFT MLG WHEEL WELL BS 870 O/B STRUCTURE IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030410001882003041000188CE 2003 4 10 FTU2003F00005 120030303A322235825148 ROD BEECH 36 A36 1151604CE SHIMMEY DAMPENERLEAKING B FTURO OTHER O OTHER NRNOT REPORTED 1 NE05951LH E2300 DURING AN ANNUAL INSPECTION, REMOVED SHIMMY DAMPENER TO REPLACE O-RINGS DUE TO LEAKAGE. AFTER DISASSEMBLING, INSPECTION REVEALED THAT THE PIN WHICH SECURES PISTON TO ROD WAS FOUND SHEARED. AFTER FURTHER DISASSEMBLY, IN WAS ALSO DISCOVERED THE ROD WAS BENT. PROBABLE CAUSE FOR DAMAGE COULD HAVE BEEN AT ONE TIME THE NOSE TURNING LIMITS WERE EXCEEDED WHILE BEING MOVED WITH A TUG. ALL OTHER PARTS WERE INSPECTED AD FOUND TO BE AIRWORTHY. DAMPENER WAS REASSEMBLED WITH A NEW ROD, PISTON, AND PIN. ALL O-RINGS REPLACED AND SERVICED DAMPENER IAW MM. ON OTHER DAMAGE WAS FOUND ON THE NOSE GEAR OR WHEEL WELL AREA. 1L71 3O 3A15 20030410001982003041000198NM 2003 4 10 DL76G030201 120030227A2121732591B COOLING FAN BOEING767 7673P6 1385105NM CARGO BAY MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271501P 24983 FWD EQUIP COOLING FAN STATUS MSG HAD AN ODOR IN AIR CONDITIONING AT THE SAME TIME. WENT TO STBY ON EQUIP COOLING AND ODOR DIMINISHED. REPLACED FAN. 2L72 4F RTA1NM 20030410002062003041000206NM 2003 4 10 DL76G030248 120030316A3350 CONNECTOR BOEING767 767332 1382001NM CABIN DISCONNECTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO271610D 30594 SEAT ROWS 1-7 LT SIDE EMERGENCY LIGHTS HAVE SEVERAL LIGHTS INOP. FWD TO MCO AND PLACARD PER MEL 33-51-03, CONNECTORS DISCONNECTED AT 6AB, 1AB, 2AB. 2L72 4F RTA1NM 20030410002142003041000214WP 2003 4 10 GTIA030160 120030313A5350 CONTROL CABLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE TAILCONE OUT OF RIG A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23816NK 49140 TAILCONE WILL NOT RELEASE WHILE ACCOMPLISHING STEP D OF WORKCARD N53038. RE-RIGGED TAILCONE PULL CABLE AT THE PULL CABLE HOUSING, OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20030410002152003041000215WP 2003 4 10 GTIA030161 120030316A3350 LIGHT DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE CABIN INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23820NK 49126 FORWARD EMERGENCY LIGHT INOPERTIVE. REMOVED AND REPLACED LIGHT ASSEMBLY, CHECKS GOOD. 2L72 4F4 F A6WE E2EA 20030410002172003041000217NM 2003 4 10 DL76G030306 120030331A2611PU90499 SMOKE DETECTOR BOEING767 767324 1385203NM LAVATORY WILL NOT TEST A DALAK NONE L NO TEST ININSP/MAINT 1 SO27394DL 27394 ON L/O FOUND LT AFT LAV SMOKE DETECTOR WILL NOT TEST. REPLACED DETECTOR, CHECKS OK. 2L72 4F RTA1NM 20030410002302003041000230 2003 4 10 ALGA085818 420030325A8300E6898785 GEAR SKRSKYS76 S76A 8143006NE GEARBOX DEFECTIVE H ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03705AL952 CAG90048 760267 TO COMPLIED WITH MANDATORY SERVICE BULLETIN T-075. PARTS WITH EFFECTIVE S/N'S MAY EXPERIENCE A PROBLEM THAT COULD RESULT IN A N2 DECOUPLE EVENT. REMOVED AND REPLACED. SENT PART TO MFG. 1G72 3U H1NE 20030410002412003041000241NM 2003 4 10 DL76L030120 120030131A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM CABIN WILL NOT TEST A DALAK NONE L NO TEST ININSP/MAINT 1 SO27172DN 24775 DURING ETOPS LAYOVER CHECK FOUND EMERGENCY LIGHTS IN LEFT AISLE FROM SEAT 6B TO 20B AND 24B INOP. T/S EMERGENCY LIGHTING. FOUND EMERGENCY LIGHT POWER SUPPLY AT SEAT 6B (M735) WOULD NOT TEST. REPLACED M735 POWER SUPPLY AT SEAT 6B SIDEWALL PANEL. OPERATED EMERGENCY LIGHTING. ALL NOW CHECKS GOOD. 2L72 4F RTA1NM 20030410002532003041000253NM 2003 4 10 F3LA200300037 120030127A5320 SILL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED R-1 DOOR MOP SILL CORRODED FROM STA 277 TO STA 360. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-51 AND SRM 53-10-15, FIG 101. REPLACED MOP SILL PER SRM 51-10-02 AND SRM 51-40-08. 2L72 4F RTA16WE 20030411000022003041100002 2003 4 11 SWAA030720 420030330A25656567380 LENS BOEING737 7377H4 1384404NM SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE VIEWING WINDOW LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030411000082003041100008 2003 4 11 SWAA030747 420030405A256563550101 SLIDE BOEING737 7377H4 1384404NM FWD ENTRY DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29753SW 29848 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030411000112003041100011NM 2003 4 11 SWAA030750 120030402A5312963820 FRAME BOEING737 7373H4 1384600NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED 1/4D CHECK, FOUND LT BULKHEAD CHORD CRACKED AT BS 178, WL 207. REMOVED AND REPLACED LT BULKHEAD CHORD PER SRM. 2L72 4F RTA16WE 20030411000142003041100014NM 2003 4 11 SWAA030753 120030406A3350300432 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29714CB 27848 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030411000162003041100016NM 2003 4 11 SWAA030755 120030404A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030414000732003041400073EU 2003 4 14 HE66085918 120030407A6720L673M20A1005 ACTUATOR UROCOPEC135 EC135T1 5620026EU MAIN ROTOR DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 FS01135CR763 0164 MAIN ROTOR ACTUATOR EXCESSIVE LEAKING AROUND PISTONS REPLACED 1G72 3U H88EU 20030407000902003040700090SO 2003 4 7 SIMA200306410 120030215A532014521725615 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING A IMBV INSPECTION, AFT SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT GALLEY SERVICE SILL IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030407000912003040700091SO 2003 4 7 SIMA200306411 120030215A532014522178005 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, CENTER SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER SERVICE DOOR SILL IAW EMB 135 SRM 51-40-02, 51-20-03, 51-40-06, AND ETN EB-53-009. (M) 2L72 4F RTT00011AT 20030407001002003040700100NM 2003 4 7 TSAA0353016 120030204A53306546558 SKIN BOEING737 7372M6C 1384708NM FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21805AL 21809 TRIMMED OUT DAMAGE SKIN AT BS 918 ABOVE STRINGER 25R. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIM BY .04 INCH INSURANCE CUT. NDT INSPECTED THE OUTER ROW OF FASTENER HOLES COMMON TO REMOVED EXISTING LAP REPAIR USING ROTARY AND SURFACE PROBLE INSPECTIONS. FABRICATED A .032 INCH DOUBLER, .050 INCH TRIPLER AND TWO .071 INCH FILLERS FROM 2024-T3 CLAD SHEET. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BVMS 10-79 TYPE III PRIMER. INSTALLED REPAIR PARTS WITH FASTENERS IDENTIFIED. APPLIED A FILLET SEAL OF BMS 5-95 SEALANT AROUND THE EDGES. APPLIED CORROSION INHIBITING COMPOUND TO THE INTERNAL AND EXTERNAL SURFACES OF THE REPAIR AREA. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW SRM 53-30-2L72 4F RTA16WE 20030407001102003040700110NM 2003 4 7 USAA030017 120030211A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US49657 23319 CLT - FOUND UNSCHEDULED MAINTENANCE, SKIN CRACKED 2 INCHES, STATION 764 ABOVE STRINGER 21R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M) 2L72 4F RTA16WE 20030408000682003040800068EA 2003 4 8 03095664 120030405A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27664BR 7528 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST FOUR SETS OF GREEN EMERGENCY FLOOR TRACK LIGHTS ILLUMINATED WHEN THE EMERGENCY LIGHTS SWITCH WAS PLACED IN THE (ARMED) POSITION. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030410001972003041000197WP 2003 4 10 GTI030149 120030221A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE CABIN DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN FLOOR PANEL HAS SOFT/MUSHEY DAMAGED DETERIORATED CORR. INSTERS LBR 8 INCH TO 44 INCH STA 200 TO 180 (20X36). FABRICATED NEW PANEL. 2L72 4F4 FRTA6WE E2EA 20030414000072003041400007NM 2003 4 14 SWAA030764 120030405A14306557463 FASTENER BOEING737 7377H4 1384404NM GIRT BAR FITTINGLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29425LV 29829 DURING SCHEDULED C 2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING FASTENER LOOSE. SECURED FASTENER PER SRM. 2L72 4F RTA16WE 20030414000082003041400008 2003 4 14 SWAA030765 420030405A2565D31354 GIRT BAR BOEING737 7377H4 1384404NM FWD SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29425LV 29829 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030414000822003041400082NM 2003 4 14 AUS20030282 120030212A5311691487115 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME LOWER LEG SHEAR TIES LOCATED AT BS 600 BETWEEN STRINGER 27 RT AND STRINGER 28 RT CONTAINED LEVEL 2 CORROSION.FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030414000862003041400086EA 2003 4 14 CA030306003 120030228A5342C2TP57 SPAR DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE FUSELAGE CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) INSPECTION CARRIED OUT AS PER SB 2/47 REV 'D' AD CF-91-42.TAILPLANE SPAR FOUND CRACKED LT AND RT SIDE TOP UNDER PICK-UP BRACKETS C2TP159 AND C2TP160. MODS 2/436, 2/466 AND 2/758 HAD ALREADY BEEN INCORPORATED.AIRCRAFT TTSN 19969.4 HOURS. 1H71 3R3 R A806 5E1 20030414000892003041400089SW 2003 4 14 CA030225004 120030217A6210 STRAP BELL 47 47G2 1181008SW LYC O435 VO435A1E 41516EA M/R BLADE CRACKED W O OTHER J WARNING INDICATION NRNOT REPORTED 1 CA (CAN) DURING MORNING PRE-FLIGHT INSPECTION, BLACK SMOKING POWDER FOUND AFT OF THE DRAG BRACE STRAP. SMALL CRACK IN PAINT FOUND. PAINT STRIPPED, SCRAPPED AWAY AND THE STRAP HAD A CRACK APPROXIMATELY 1/2 INCHLONG FROM A SCREW HOLE TO THE TRAILING EDGE OF STRAP. BLADE RETURNED TO OVERHAUL FACILITY FOR REPAI R. 1G71 3O3 O H1 E279 20030414000912003041400091CE 2003 4 14 CA030225006 120030212A7921636900 OIL COOLER CESSNA402 402B 207590PCE CONT O520 TSIO520VB 17040SO ENGINE CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) OIL COOLER UPPER WELD CRACKED ACROSS. 1L72 3O3 O A7CE E8CE 20030414000942003041400094CE 2003 4 14 CA030227004 120030225A275014601007 CONTROL CABLE CESSNA336 336 2075602CE CONT O360 IO360D 17025SO TE FLAPS FAILED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) OPERATOR EXPERIENCED A ASYMMETRIC FLAP CONDITION DURING LANDING CAUSED BY THE FAILURE OF A FLAP CABLE. THE INBOARD RIGHT HAND FLAP CABLE FAILED AT A POINT WHERE THE CABLE STARTS TO BEND AROUND THE INBOARD RIGHT HAND FLAP BELLCRANK. THIS AREA OF THE CABLE CAN ONLY BE INSPECTED WITH THE REMOVAL OF THECABLE AND/OR BELLCRANK 1H72 3O3 O A2CE E1CE 20030414001092003041400109CE 2003 4 14 CA030304005 120030222A3233 ACTUATOR BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA NOSE LANDING GEAFAILED W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN) THE PILOT REPORTED THAT FOLLOWING THE RETRACTION OF THE LANDING GEAR THE GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. THE LANDING GEAR WAS EXTENDED AND A GEAR SAFE INDICATION WAS OBSERVED. INSPECTION OF THE AIRCRAFT LANDING GEAR SYSTEM REVEALED THAT THE NOSE LANDING GEAR ACTUATOR WOULD OCCATIONALLY SKIP INTERNALLY CAUSING THE LANDING GEAR SYSTEM TO GO OUT OF RIGG. THE NOSE LANDING GEAR ACTUATOR HAS SINCE BEEN REPLACE AND NO FURTHER OCCURENCES HAVE BEEN REPORTED. 1L72 3T4 T A14CE E4EA 20030414000012003041400001NM 2003 4 14 SWAA030758 120030406A53126517582 WEB BOEING737 7373G7 1384595NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/2 D CHECK, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 179, WL 229 AT LBL 17.1 & WL 227 AT RBL 17.1. REMOVED AND REPLACED BOTH LT & RT WEBS PER SRM. 2L72 4F RTA16WE 20030414000042003041400004 2003 4 14 SWAA030761 420030403A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030414000112003041400011NM 2003 4 14 SWAA030730 120030401A3350BR2013 LIGHT BOEING737 7372H4 138448CNM AFT CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29104SW 23110 DURING SCHEDULED C2 CHECK, FOUND EEPLS SECTION INOP IN AFT CABIN. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20030414000132003041400013NM 2003 4 14 SWAA030738 120030402A32106546113 PIN BOEING737 7373Q8 1384670NM LT/RT MLG TRNIONCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, SWA SI 11251-32, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030414000162003041400016NM 2003 4 14 SWAA030744 120030403A5311BAC1517 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED 1/4 D CHECK, FOUND FUSELAGE FRAME SHEAR TIES CORRODED, WL 148, BETWEEN RBL 20 AND LBL 20, BS 787 AND BS 767. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20030414000252003041400025NM 2003 4 14 SWAA030728 120030402A33501000679 LIGHT BOEING737 7372H4 138448CNM FWD DOOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F A16WE 20030414000492003041400049NM 2003 4 14 CA030312024 120030310A323069141001 BUNGEE CYLINDER BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE NLG FROZEN W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER DEPARTURE WHEN GEAR SELECTED UP, NOSE GEAR IND SHOWED DOWN AND LOCKED. AIRCRAFT RETURNED TO YHM. MAINT REPLACED NLG POSITION AND LOCK SWITCHES (NOSE). AIRCRAFT DEPARTED AND RETURNED AGAIN. CREW REPORTED GEAR REMAINED EXTENDED. MAINT FOUND NLG LOCK ACTUATOR BUNGEE FROZEN, REPLACED AND A/C RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20030414000542003041400054EU 2003 4 14 BAQA085939 120030409A249745023501 CONTROL BOX UROCOPEC135 EC135P1 8680990EU ELECTRICAL FAILED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01137MH54 0179 NR 2 AMP OVERLIMIT. INTERMITTENTLY SPIKES BEYOND SERVICEABLE LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030414000602003041400060SW 2003 4 14 HEEA085856 120030328A6510407340339101 BEARING BELL 407 407 1182206SW T/R SHAFT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 TAIL ROTOR SHAFT HAS WORN BEARINGS. REPLACED WITH SERVICEABLE BEARINGS. REPAIRED. 1G71 3U O H2SW 20030414000682003041400068NM 2003 4 14 AUS20030238 120030227A57146545439 WEB BOEING737 737377 NM CENTER WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING CENTRE SECTION SUPPORT BEAM WEB CONTAINED LEVEL 2 CORROSION IN AREA BETWEEN THE HEAT EXCHANGER CUTOUTS. AREA OF CORROSION 6.3MM (0.250IN) IN DIAMETER BY 0.508MM (0.020IN) DEEP.FOUND DURING INSPECTION IAW J3-CA53-0129. 2L72 4F RTA16WE 20030407000152003040700015WP 2003 4 7 ASAA0380070 120030112A5347S00062 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, TIE DOWN TRACK CORRODED IN AFT CARGO BAY. REPLACED TRACK PER SRM 51-10-2, 51-10-4, 51-30-1, AND 51-30-5. (M) 2L72 4F RTA6WE 20030407000172003040700017WP 2003 4 7 ASAA0380072 120030112A5310593607127 GUSSET DOUG DC9 DC983 3022083WP CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, GUSSET CORRODED IN AFT CARGO BAY. REPLACED GUSSET PER SRM 51-10-2 AND 51-10-4. (M) 2L72 4F RTA6WE 20030407000832003040700083SO 2003 4 7 SIMA200306403 120030128A532014522460013 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, CENTER BEAM GUSSET IN GALLEY AREA HAS CORROSION. REMOVED CORRODED CENTER BEAM GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030408000422003040800042NM 2003 4 8 USAA030018 120030221A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US49657 22959 CLT - FOUND UNSCHEDULED MAINTENANCE, FOUND SKIN CRACKED 1.65 INCH, STATION 943 ABOVE S24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20030408000762003040800076 2003 4 8 03FDEA00384 420030403A3443 FMC AIRBUS310 A310 EU INS/IRS NAV INOPERATIVE A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25456FE 318 AFTER ROTATION, GOT IRU AND GPS DO NOT AGREE ON ECAM POSITION UPDATE ACCOMPLISHED O/HEAD. ECAM WARNING STILL PRESENT AFTER UPDATE. ECAM WARNING CLEARED AND POSITIONS CAME INTO AGREEMENT O/HEAD SUBIC VOR DURING RETURN TO SFS. AFTER LANDING, IRU NR 1 DISPLAYED DRIFT 99.9, NR 2 DISPLAYED 99.9 DRIFTS AND NR 3 NO DISPLAY. REMOVED AND REPLACED FMC 1 AND 2 IAW MM 34-60-00 AND UPDATED WITH VERSION FX4-0303-001, OPS CHK SATIS. REMOVED AND REPLACED IRU NR 3 IAW MM 34-25-34 AND BAT NR 3 IAW MM 24-31-11, OPS CHK SATIS. REMOVED AND REPLACED FCC NR 1 DUE, FAULTED ON GROUND SCAN IAW MM 22-18-34, AFS/LAND TEST IAW MM 22-40-00. 2L72 4F RTA35EU 20030410000852003041000085NM 2003 4 10 SWAA030657 120030323A3350311500 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 12 DEF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030410000952003041000095NM 2003 4 10 SWAA030667 120030322A2560P2070001 BATTERY BOEING737 7372H4 138448CNM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030410002292003041000229 2003 4 10 ALGA085813 420030324A8300E6893672 PINION GEAR SKRSKYS76 S76A 8143006NE GEARBOX SPALLED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01705AL952 CAG90048 760267 ON INSPECTION FOUND SPALLING ON GEAR TEETH. REMOVED AND REPLACED. 1G72 3U H1NE 20030410002362003041000236EU 2003 4 10 BAQA084707 120030224A2842L284M30C1003 SENSOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE FUEL CELL INTERMITTENT D BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME 0144 FUEL SENSOR GIVING INTERMITTENT READINGS. ONLY HAVE ONE CORE SO FAR. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H88EU E34NE 20030414000442003041400044EU 2003 4 14 CA030312019 120030218A2913S40 SHAFT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HYD PULLEY WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) SPLINES ON HYDRAULIC PULLEY SHAFT, S40, WORN WELL BEYOND LIMITS. 1G71 3U3 UNCH9EU E19EU 20030414000622003041400062SW 2003 4 14 HEEA085858 120030328A6510407340339101 BEARING BELL 407 407 1182206SW T/R SHAFT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 TAIL ROTOR SHAFT HAS WORN BEARING. REPLACED WITH SERVICEABLE BEARING. 1G71 3U O H2SW 20030414001182003041400118CE 2003 4 14 048329 120030301A5510114620000657 STRUCTURE BEECH 1900 1900D 1154162CE HORIZONTAL STAB BIRD STRIKE A AMWAA UNSCHED LANDING O OTHER CRCRUISE 1 CE07133YV UE133 ON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERITCAL AND HORIZONTAL STABILIZERS. FURTHER POSTFLIGHT INSPECTION, THE RT ENGINE NACELLE WAS FOUND TO HAVE THE ICE LIGHT PANEL MISSING. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPAIRED THE HORIZONTAL AND VERTICAL STABILIZER. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030414001282003041400128SO 2003 4 14 CA030311002 120030224A2421 BEARING ROTAX GULSTMG159 G159 3952202SO RROYCEDART DART5298X 54507EU ALTERNATOR DISINTEGRATED W O OTHER O OTHER NRNOT REPORTED 1 CA 1100 (CAN) R/H ALTERNATOR WOULD NOT STAY ON LINE. SENT FOR PREMATURE OVERHAUL (1000.0 HR TBO). FOUND REAR BEARING DISINTEGRATED TO THE POINT OF ROTOR RUB. THE OVERHAUL COMPANY IS HOLDING BEARING FOR POSSIBLE T.C. INSPECTION. 2L72 4T4 T 1A17 E297 20030415000162003041500016WP 2003 4 15 CA030305009 120030225A324650078902 WHEEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE MLG CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) MAIN WHEEL REPORTED TO LEAK ON THE ACFT.- DURING WHEEL REPAIR, A '3 INCHES' CRACK WAS FOUND ON THE INNER TUBE WELL. 2L72 4F4 FRTA6WE E9NE 20030415000202003041500020WP 2003 4 15 CA030317002 120030316A5230 VALVE LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE CABIN PRESSURE OPEN W O OTHER W INADEQUATE Q C CRCRUISE 1 CA (CAN) LOSS OF CABIN PRESSURE AT FL 310. CABIN RATE OF CLIMB 1500 FPM. RAPID DEPRESSURIZATION DRILL WAS CARRY OUT. WITH CROSS BLEED CLOSED CABIN CAME BACK TO NORMAL. SAFETY VALVE OPEN LIGHT REMAINED ON UNTIL LANDING. 2L73 4F4 F A23WE E12EU 20030408000802003040800080WP 2003 4 8 03FDEA00388 120030405A5420 SEAL DOUG MD10 MD1010F WP GE CF6 CF66D 30020GL ZONE 400 BENT A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25393FE 46627 NR 662 NR 3 PYLON PANEL 488CR RAIN SEALS (2) EA BENT AND TORN. CLOSING ACTION ON 04/05/03. REMOVED 2EA RAIN SEALS ON NR 3 PYLON PANEL 488CR, IAW SRM 51-31-01. FAB NEW RAIN SEALS ON TRAVELER NR T2/324415. DRILLED DEBURED IAW SRM 51-31-01. INSTALLED RAIN SEALS USING MONEL RIVETS IAW SRM 51-31-01. RETURNED TO PARTS RACK. 2L73 4F4 FRTA22WE E23EA 20030408000932003040800093EU 2003 4 8 2003UALA00251 120030309A213390231570381 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29486UA 1620 RETURN TO FIELD DUE TO LOSS OF CABIN PRESSURE. REPLACED OUTFLOW VALVE. 2L72 4F4 FRTA28NM E40NE 20030408001112003040800111NM 2003 4 8 2003UALA00356 120030329A5512 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE HORIZONTAL STAB CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 LT EMPENNAGE SKIN IS CHAFED AT HORIZ STAB LOWER T/E MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN W/DOUBLER AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030408001132003040800113NM 2003 4 8 2003UALA00359 120030401A2710 AILERON BOEING747 747422 1384935NM PWA 4056 PW4056 NE WING MALFUNCTIONED A UALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 WP29175UA 24382 FLT EXPERIENCED AILERON PROBLEMS PRIOR TO LANDING. AUTOPILOT WARNING RECEIVED. DISCONNECTED AUTO PILOT. AIRPLANE COULD NOT TURN LEFT (RIGHT TURNS OK). 2L74 4F4 FRTA20WE E24NE 20030410000302003041000030WP 2003 4 10 GTIA030084 120030131A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND CREASE AT FS 294 TO 313 AT LONGERON 25R REQUIRES REPAIR. CUT OUT DAMAGED AREA FS 294-313. FABRICATED 5 DOUBLERS 4 EACH, 7 STRAPS 4 EACH, 9 FINGER DOUBLER, 11 SKIN SECTION. INSTALLED ALL REPAIR PARTS. (M) 2L72 4F A6WE 20030410000352003041000035 2003 4 10 SWAA030610 420030317A2565D31354 SLIDE BOEING737 7377H4 1384404NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29430WN 33659 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030410000712003041000071 2003 4 10 SWAA030648 420030320A2565D31394475 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE AT MOUNT. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030410000812003041000081NM 2003 4 10 SWAA030654 120030321A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.6, JUST ABOVE STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001302003041000130SO 2003 4 10 SIMA200304808 120030207A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 ABI - DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED EXISTING SHIM AND DOUBLERS. REMOVED SECTION OF THE FORWARD DIGITAL. FABRICATED TWO DOUBLERS AND SHIMS. PREPARED NEW SECTION STRAP. REPAIR DONE IAW EMB 145 SRM (EMB SRM 145/1142 REV 20) CHAPTERS 53-21-10 FIG 203. (M) 2L72 4T RTT00011AT 20030410001522003041000152NM 2003 4 10 SWAA030706 120030327A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 862 AND BS 881. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030410001622003041000162NM 2003 4 10 SWAA030716 120030328A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001632003041000163NM 2003 4 10 SWAA030717 120030328A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) ABOVE STR 10R, AT BS 445, BS 470, BS 500, BS 500A AND BS 500B. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001662003041000166SO 2003 4 10 SIMA200305003 120030219A2910 HYDRAULIC SYSTEM EMB 135 EMB135LR 3260305SO NR 1 FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21739AE 145402 JFK - FLT 4775 - CREW REPORTED A HYDRAULIC SYSTEM 1 FAIL AFTER TAKEOFF. AIR TRAFFIC CONTROL DECLARED A PRECAUTIONARY EMERGENCY. CREW LANDED WITH NO FURTHER INCIDENTS REPORTED. (M) 2L72 4F RTT00011AT 20030410002182003041000218NM 2003 4 10 DL76G030307 120030331A3350767 LIGHT BOEING767 767332 1382001NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO271602 29694 ON L/O, FOUND EMERGENCY EXIT LIGHT INOP. RELAMPED, CHECKS OK. 2L72 4F RTA1NM 20030414001132003041400113EA 2003 4 14 CA030305004 120030228A3246L713049 BEARING DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE WHEEL FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON TAKEOFF LT INBOARD MAIN WHEEL ASSY DEPARTED AIRCRAFT. RAMP AGENT AT DESTINATION ADVISED CREW OF MISSING WHEEL AFTER DEPLANING OF PASSENGERS. SUSPECT THAT INNER AND OR OUTER WHEEL BEARINGS FAILED. INBD WHEEL BEARING P/N L713049.OUTBD WHEEL BEARING P/N L812148. LT MLG SHOCK STRUT, NR 1 & 2 WHEEL AND BRAKE ASSEMBLIES REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030415000782003041500078NM 2003 4 15 CA030328004 120030326A573065454877 PANEL BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE WING MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CAPTAIN DISCOVERED THAT LT LOWER WING FUEL BOOST PUMP PANEL MISSING. SUSPECT PANEL DEPARTED IN FLIGHT. AIRCRAFT OPERATED I.A.W. CDL 57-30-4. 2L72 4F4 F A16WE E2EA 20030415000802003041500080EU 2003 4 15 CA030328006 120030327A25607A1508107 SLIDE AIRBUS330 A330322 3930325EU PWA 4168 PW4168 NE CABIN MALFUNCTIONED W O OTHER L NO TEST NRNOT REPORTED 1 CA (CAN) DURING DEPLOYMENT OF SLIDE RAFT L1 AND L4, AUTOMATIC INFLATION DID NOT OCCUR. DOOR AND SLIDE BOTTLE PRESSURES WERE IN THE GREEN RANGE. DEPLOYMENT NORMAL UP TO POINT OF SPEED LACING NOT RELEASING. MANUAL INFLATION HANDLE PULLED AND REMAINING DEPLOYMENT WAS NORMAL. SLIDE RAFTS TO BE SENT FOR INVESTIGATION. 2L72 4F4 FRTA46NM E36NE 20030408000912003040800091CE 2003 4 8 049569 120030407A3260 WIRE BEECH 1900 1900D 1154162CE MLG BROKEN A AMWAO OTHER N FALSE WARNING APAPPROACH 1 CE07242YV UE242 WHILE ON APPROACH ON FLIGHT 5478 FROM PHILADELPHIA PENNSYLVANIA TO ITHACA NEW YORK, THE LANDING GEAR FAILED TO EXTEND ON NORMAL EXTENSION. AFTER THE CREW PERFORMED AND EMERGENCY EXTENSION ALL THREE GREEN GEAR INDICATIONS WERE GOOD. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT.MAINTENANCE TROUBLESHOT AND LOCATED A BROKEN WIRE BEHIND THE PILOTS LEFT KICK PANEL. MAINTENANCE REPAIRED THE WIRE. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030408000922003040800092NE 2003 4 8 131541 220030407A7261 SUMP SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE INOPERATIVE A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL17104CQ 340A104 367375 DURING TAKE OFF ROLL OF FLIGHT 4493 PIT-CLE LT ENGINE OIL PRESSURE LIGHT ILLUMINATED. RETURNED TO GATE WHERE MAINTANCE DEPARTMENT SERVICED LT ENGINE WITH TWO AND 3/4 QUARTS OF OIL. THIS CLEARED OIL PRESSURE LIGHT DISCREPANCY. AIRCRAFT KEPT DOWN IN PIT WHERE MAINTENANCE IS IN THE PROGRESS OF INSTALLING A LT C-SUMP KIT AND FURTHER TROUBLESHOOTING. 2L72 4T4 TRTA52EU E8NE6 20030408001102003040800110NM 2003 4 8 2003UALA00355 120030329A5512 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE HORIZONTAL STAB CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 RT EMPENNAGE SKIN IS CHAFED AT HORIZ STAB LOWER T/E, MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN W/DOUBLER AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030410000222003041000022WP 2003 4 10 GTIA030082 120030209A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOORBOARD STATION 130-160 DETERIORATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030410000502003041000050NM 2003 4 10 SWAA030636 120030320A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 480, WL 148, RBL 4 TO LBL 4. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030410000702003041000070NM 2003 4 10 SWAA030647 120030320A4950BACC10JJ400E CLAMP BOEING737 7377H4 1384404NM APU LOOSE A SWAAK NONE O OTHER DEDESCENT 1 SW29777QC 30592 CABIN WOULD ONLY DESCEND WITH BOTH A/C PACKS IN HIGH POSITION. FOUND CLAMP LOOSE OF APU DUCT AT BS 1016 PRESS BULKHEAD. SECURED CLAMP, NO LEAKS NOTED PER MM. 2L72 4F RTA16WE 20030410001032003041000103NM 2003 4 10 SWAA030675 120030324A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030410001362003041000136 2003 4 10 SWAA030690 420030326A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030410001552003041000155NM 2003 4 10 SWAA030709 120030329A3350321500 LENS BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C2 CHECK, FOUND CEILING EMERGENCY EXIT LIGHT LENS CRACKED IN AFT CABIN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030410001592003041000159NM 2003 4 10 SWAA030713 120030328A14306557463 FASTENER BOEING737 7377H4 1384404NM GIRT BAR FITTINGWORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. INSTALLED FASTENER PER SRM. 2L72 4F RTA16WE 20030410001602003041000160NM 2003 4 10 SWAA030714 120030328A57536546435 SKIN BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED 1/4D CHECK, FOUND LT OTBD T/E AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED LEFT OTBD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20030410002252003041000225NM 2003 4 10 DL76K030251 120030318A2560MV10S MEGAPHONE BOEING767 767332 1382001NM CABIN DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27175DZ 29696 1ST CLASS MEGAPHONE INOP. ONE C-CELL BATTERY FAILED/SHORTED OUT, DAMAGING THE ELECTRICAL CONTACTS INSIDE THE MEGAPHONE. 2L72 4F RTA1NM 20030410002372003041000237NM 2003 4 10 DL76L030064 120030115A2530828450405 OVEN BOEING767 767332 1382001NM GALLEY FAULTY A DALAA UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 SO271200K 28457 INBOUND OVEN ON FIRST OFFICERS SIDE IN AFT GALLEY WAS ON FIRE AND FLAMES WAS SHOOTING OUT FROM GRILL ABOVE THE OVEN. FLT ATTENDANTS TURNED OFF OVEN AND FLAMES STOPPED. CIRCUIT BREAKERS WERE PULLED LATER. FOUND NR 4 OVEN POWER WIRES BURNED. REMOVED AND REPLACED NR 4 OVEN. CANNON PLUG OK, NO DAMAGE FOUND. CHECKED NEW OVEN, CHECKS OK. BURNED WIRES PART OF THE OVEN UNIT. 2L72 4F RTA1NM 20030414000272003041400027NM 2003 4 14 SWAA030733 120030402A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 727B PLUS 19, STR 10R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030414000292003041400029NM 2003 4 14 SWAA030737 120030402A53106547978 BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED FROM BS 747 TO BS 889. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030414001152003041400115SW 2003 4 14 CA030305006 120030201A6210222015600111 BLADE BELL 230 230 1182149SW MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE BLADE WAS SENT IN FOR A HARD LANDING INSPECTION (NOT A BLADE STRIKE). UPON INSPECTION THE ROTOR BLADE WAS FOUND CRACKED ON THE UPPER SURFACE STATION 224.0 NEAR THE TIP INERTIA WEIGHT. THE CRACK ORIGINATED AT A FASTENER HOLE AND PROGRESSED THROUGH THE BOTH UPPER SURFACE SPAR DOUBLERS AS WELL AS THE SPAR. THE UPPER SURFACE SPAR DOUBLER P/N 222-015-614-101, INTERNAL SPAR DOUBLER P/N 222-015-614-105 WERE CRACKED THROUGH THE ENTIRE CHORD OF THE PART. THE MAIN BLADE SPAR P/N 222-015-251 WAS FOUND CRACKED FROM THE SAME FASTENER HOLE. 1G72 3U NCH9SW 20030414001292003041400129EA 2003 4 14 CA030311004 120030303A78103031988 EXHAUST STACK DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A135 52043NE ENGINE CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) ON HEAVY MAINTENANCE INSPECTION FOUND BOTH EXHAUST DUCT FLANGES ON LARGE EXIT DUCT CRACKED. THIS IS THE THIRD TIME WE HAVE CHANGED AN EXIT DUCT ON A TURBINE CONVERSION INSTALLATION. 1H71 3R4 T A815 E4EA 20030415000082003041500008EU 2003 4 15 CA030220010 120030213A623047896WVC47820X BEARING UROCOP SNIAS 350 AS350BA 8680817EU MAST MAKING METAL W O OTHER J WARNING INDICATION LDLANDING 1 CA M847 (CAN) PILOT REPORTED A SOLID MGB CHIP LIGHT. UPON INSPECTION OF THE MAST CHIP PLUG, TRANSMISSION FILTER AND MGB CHIP PLUG, IT WAS NOTED THAT ALL HAD METAL LOCATED ON EACH. MAST ASSEMBLY CONICAL STRAINER INSPECTED AND SIGNIFICANT AMOUNTS OF METAL WERE FOUND. MAST ASSEMBLY WAS REPLACED. 1G71 3U NCH9EU 20030414001122003041400112EU 2003 4 14 CA030305003 120030228A6321SLW40442M50BP NUT AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20F 03013GL COMBINING G/B LOOSE W K NONE O OTHER ININSP/MAINT 1 CA 24242 (CAN) FLT CREW REPORTED THAT THE ROTOR BRAKE HAD NO EFFECT WHEN APPLIED. THE ROTOR BRAKE PACK WAS BEING INSPECTED AND TO HAVE SHIMS ADJUSTED WHEN THE OUT PUT FLANGE LOCK NUT WAS FOUND ON THE DECK BELOW THE FLANGE. THE OUTPUT FLANGE WAS REMOVED AND INSPECTED WITH NO DAMAGE FOUND. THE MFG. SERVICE REP WAS CONTACTED AND HE ALSO INSPECTED THE PARTS. A NEW LOCK NUT AND WASHER WERE ORDERED AND WILL BE INSTALLED WITH THE PROPER INSTALLATION TOOL WHEN THEY ARRIVE. NOTE: THIS ASSEMBLY HAS NOT BEEN REMOVED OR REINSTALLED SINCE AQUIRING THIS AIRCRAFT A YEAR AGO. 1G72 3U3 U H11EU E4CE 20030414001192003041400119CE 2003 4 14 AMWA16 120030301A5530114640000637 STRUCTURE BEECH 1900 1900D 1154162CE VERTICAL STAB DAMAGED A AMWAA UNSCHED LANDING O OTHER CRCRUISE 1 CE07133YV UE133 ON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERTICAL AND HORIZONTAL STABILIZERS. FURTHER POSTFLIGHT INSPECTION, THE RIGHT ENGINE NACELLE WAS FOUND TO HAVE THE ICE LIGHT PANEL MISSING. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPAIRED THE HORIZONTAL AND VERTICAL STABILIZERS. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030414001242003041400124NM 2003 4 14 CA030307001 120030306A291082950010211 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) HYDRAULIC LEAK FROM RT ARMPIT AREA. FOUND RT BRAKE PRESSURE HYDRAULIC LINE HAS A 1/4 INCH CRACK AT BEND NEAR FUSELAGE CONNECTION POINT. IPC REF 29-00-00 FIG 60. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030414001262003041400126WP 2003 4 14 CA030307003 120030306A3260 DOWNLOCK SWITCH CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13D 03004GL NLG MALFUNCTIONED W O OTHER N FALSE WARNING DEDESCENT 1 CA (CAN) ON APPROACH, CREW FAILED TO GET A GREEN INDICATION FOR THE NOSE GEAR.AFTER INITIATING EMERGENCY PROCEDURES, THE INDICATION APPEARED. THE A/C WAS FERRIED TO A MAINTENANCE BASE, WHERE THE NLG DOWNLOCK SWITCH BRACKET WAS FOUND LOOSE AND SLIGHTLY BENT. THE A/C WAS REPAIRED AND RETURNED TO SERVICE. 2L72 4R4 T 6A6 E282 20030415000232003041500023EU 2003 4 15 CA030317006 120030131A2550704A31813010 CABLE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE CARGO HOOK BROKEN W O OTHER D INFLIGHT SEPARATION CRCRUISE 1 CA (CAN) CARGO HOOK SWING SUSPENSION SYSTEM: WHILE SLING THE LOAD WAS RELEASED DUE TO THE DAMAGE OF THE MANUAL HOOK RELEASE CABLE. IN THE INVESTIGATION IT WAS FOUND THAT WITH THE ONBOARD CARGO HOOK ASSEMBLY HOOK RELEASE CABLE CONTACTS THE SUSPENSION FRAME IN THE REAR QUADRANTS CAUSING DAMAGE AND FAILURE OF THE RESPECTIVE RELEASE CABLE. UNCOMMANDED RELEASE OF THE MANUAL RELEASE IS DUE TO THE CABLE COVERBEING BROKEN WHICH THEN PERMITS ANY FORWARD MOVEMENT OF THE CARGO HOOK CAUSING A PULL ON THE INNERCABLE THEREBY ACTIVATING THE MANUAL RELEASE. 1G71 3U3 U H9EU E19EU 20030415000262003041500026NE 2003 4 15 CA030317017 220030205A7200 ENGINE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) ENGINE CHIP LIGHT ILLUMINATED DURING FLIGHT. PILOT LANDED, REMOVED AND CLEANED THE CHIP PLUG, RETAINING THE METAL, THEN RETURNED THE AIRCRAFT TO BASE FOR THE ENGINEERS INSPECTION. INSPECTED ALL CHIP PLUGS,SCREENS AND FILTER IAW TURBOMECA ARRIEL 1 MAINTENANCE MANUAL. CARRIED OUT 30 MINUTE GROUND RUN AND 30 MINUTE TEST FLIGHT. NO FURTHER CONTAMINATION FOUND. AIRCRAFT HAS ACCUMULATED MORE THAN 14 HRS SINCETHE INCIDENT WITH NO FURTHER CONTAMINATION. ALL PARTICLES RECOVERED AND RETAINED ON THE BASE. ENGINE HAD BEEN REMOVED FROM THE AIRCRAFT ABOUT 65 HRS BEFORE THE CHIP LIGHT TO REPLACE A TIME EXPIRED MO-4 . CHIP DETECTORS ARE BEING MONITORED DAILY ALF. 1G71 3U3 UNCH9EU E19EU 20030415000292003041500029EA 2003 4 15 CA030318004 120030311A5711C6WM102727 SPAR DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A34 52043EA RT WING CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA 1239812398 (CAN) 6 CRACKS BETWEEN RIVETS ON VERTICAL FLANGES. BETWEEN WING STA. 35.15 AND 60.0 CRACKS VISUALLY DISCOVERED - CONFIRMED NDT. 1H72 3T4 TRTA9EA E4EA 20030415000362003041500036SO 2003 4 15 CA030318014 120030306A32221485500102 ACTUATOR EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA NLG STEERING FAILED W O OTHER R PARTIAL RPM/PWR LOSS LDLANDING 1 CA (CAN) SHIMMY WHEN TAXIING & NECESSARY TO CENTRE THE NOSE GEAR MANUALLY IN ORDER TO GET THE GEARS TO RETRACT ON TAKEOFF. AFTER INVESTIGATION IN COLLABORATION WITH THE O/H FACILITY (THE GEAR WAS FRESHLY O/H), WE FOUND THAT IN THE NOSE STEERING RACK ACTUATOR, BOTH SLEEVES P/N 14564 HAD BEEN REINSTALLED WITH DAMAGED LOCKING FEATURE AND THUS RENDERING PROPER ADJUSTMENT OF THE CENTERING MECHANISM IMPOSSIBLE. AT ALL TIME THE PRESENCE OF A 10 DEGREE PLAY WAS THE CAUSE OF THE IMPOSSIBILITY TO ADJUST. THE PROBLEM HAS BEEN FIXED BY REPLACING THE STEERING RACK ACTUATOR BY A NEWLY O/H UNIT. 1L72 4T4 T A21SO E4EA 20030415000372003041500037NM 2003 4 15 CA030318018 120030315A2761 ACTUATOR BOEING737 737217 1384464NM PWA JT8 JT8D17 52049NE NR 2 SPOILER LEAKING W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE THE AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC FLUID. THE AIRCRAFT WAS DIVERTED TO WHERE EMERGENCY VEHICLES MET THE AIRCRAFT ON LANDING.THE LOSS OF FLUID WAS ATTRIBUTED TO THE NR 2 FLIGHT SPOILER ACTUATOR. THE ACTUATOR IS BEING TESTED AND ASSESSED IN THE SHOP. FURTHER INFO WILL FOLLOW WHEN REPORT IS RECEIVED. 2L72 4F4 F A16WE E2EA 20030415000442003041500044GL 2003 4 15 CA030321006 220030320A7260AN150832 STUD RROYCE BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL GEARBOX HOUSING LOOSE W O OTHER O OTHER NRNOT REPORTED 1 CA HL26408 (CAN) A STUD BACKED OUT OF THE ENGINE GEARBOX AND SUBSEQUENTLY MADE CONTACT WITH A ROTATING BOLT THAT SECURES THE TRANSMISSION DRIVE SHAFT WITH THE ENGINE STUB SHAFT. NO DAMAGE RESULTED IN THIS OCCURENCE, HOWEVER THE POTENTIAL HAZARD OF A ROTATING PART CONTACTING A STATIONARY PART WARRANTS INVESTIGATION. 1G72 3U3 U H3EU E4CE 20030408000022003040800002EA 2003 4 8 2003F00209 120030112A2611473052 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW0777286 7286 ASH - FLT 6277 - MCI-PHX - CARGO SMOKE INTERMITTED DURING FLIGHT. MAINTENANCE IS TROUBLESHOOTING AIRCRAFT AT THIS TIME, IN THE HANGAR. MAINTENANCE TROUBLESHOT, MAINTENANCE COULD NOT DUPLICATE. (M) 2L72 4F RTA21EA 20030408000042003040800004EA 2003 4 8 2003F00211 120030201A2750601R93103910 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SW0787353 7353 FLT 6138 - SAN-PHX - AIRCRAFT DECLARED AN EMERGENCY DUE OT A FLAPS FAIL AT 0 DEGREES DURING CRUISE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CURRENTLY TROUBLESHOOTING PROBLEM. MAINTENANCE COMPLIED WITH PARTS 'A' AND 'B' DURING COMPLIANCE WITH PART 'B'. MAINTENANCE ADJUSTED POTS AND BPSU'S. (M) 2L72 4F RTA21EA 20030408000772003040800077WP 2003 4 8 03FDEA00385 120030403A2611 SMOKE DETECTOR DOUG MD10 MD1010F WP GE CF6 CF650* 30018NE CARGO BAY DAMAGED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25392FE 46626 PASSING 5,000 FT IN CLIMB GOT LEVEL 3 CARGO FIRE LWR ALERT. DISCHARGED AGENT IAW CHECKLIST AND RETURNED TO LAND AT KMEM. WHEN LEVEL 3 ALERT CAME ON AGAIN, DISCHARGED OTHER BOTTLE. CARGO FIRE LWR ALERT CAME ON AGAIN 2 MORE TIMES, DURING TAXI IN. CHECKED WIRING, REPAIRED GND ON AFT DET. REMOVED AND REPLACED ALL FOUR SMOKE DETECTORS IAW MM 26-14-01-4 SAFETIED ALL CONNCTOR PLUGS. PERFORMED ALL RETURN TO SERVICE CHECKS , PERFORMED THEM SEVERAL TIMES. OK FOR SERVICE. 2L73 4F4 FRTA22WE E23EA 20030408000882003040800088NM 2003 4 8 03FDEA00397 120030407A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25281FE 22348 COMPLY WITH E.A. NR 7-5330-68760 FUSELAGE SKIN- PRE-EXISTING ELONGATED HOLE AT STA. FACT 07APR03 11:48 BFM R COMPLIED WITH E.A. NR 7-5330-68760 FUSELAGE - SKIN PRE-EXISTING ELONGATED HOLE AT STA.508 UNDER MCD HINGE. 2L73 4F RTA3WE 20030415000212003041500021WP 2003 4 15 CA030317003 120030316A24971103080100 ELECTRICAL BOX LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE CABIN BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) FLIGHT CREW REPORTED BURNING ODOR IN CABIN BETWEEN ROW 22 AND 28.MAINTENANCE FOUND THE SEAT ELECTRONIC BOX (SEB) AT FAULT. UNIT WAS REPLACED AND SYSTEM TESTED RERVICEABLE. 2L73 4F4 F A23WE E12EU 20030415000352003041500035WP 2003 4 15 CA030318013 120030307A324650078902 WHEEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) MAIN WHEEL REPORTED TO LEAK ON THE ACFT.- DURING WHEEL REPAIR, A '4 INCH' CRACK WAS FOUND ON THE INNER TUBEWELL. 2L72 4F4 FRTA6WE E9NE 20030415000422003041500042WP 2003 4 15 CA030320005 120030201A5230 LONGERON CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13 03004GL CARGO DOOR CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 26750 (CAN) A SMALL CRACK INBOARD AND ADJACENT TO THE FORWARD SERVICE DOOR HOOK, YOKE. CRACK IS APPROXIMATELY 1.5 INCHES LONG & DIFFICULT TO SEE WITHOUT A 10 POWER MAGNIFYING GLASS. THE CRACK OCCURRED ON THE OUTBOARD APEX OF A TROUGH CREATED AT THE INBOARD SIDE OF THE YOLK MOUNT FLANGE AND APPEARS TO BE IN AN AREA OF STRETCHED METAL. THE TROUGH, IT APPEARS, WAS CREATED BY EITHER BANGING THE DOOR HOOK AGAINST THE YOLK OR IMPACT DAMAGE FROM SOME OTHER SOURCE IN THE SAME INBOARD DIRECTION. THE LONGERON WAS DENTED DOWNWARD AT THIS POINT REFERRED TO ABOVE. 2L72 4R4 T 6A6 E282 20030415000772003041500077NM 2003 4 15 CA030328003 120030327A2750655032214 TRANSMISSION BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE TE FLAPS SEIZED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) CAPTAIN COULD NOT RETRACT FLAPS AFTER TOUCHDOWN . ASYMMETRIC FLAP CONDITION WOULD NOT ALLOW FLAPS TOMOVE FROM 25 UNITS TO UP POSITION ON GROUND. AFTER APPROXIMATELY 30 SECONDS A LOUD BANG WAS HEARD FROM NR 2 FLAP TRANSMISSION. FLAP THEN MOVED FROM 25 UNITS TO FULL UP POSITION. GRINDING NOISE NOTICED DURING FLAP UP MOVEMENT.NEW FLAP TRANSMISSION ORDERED. 2L72 4F4 F A16WE E2EA 20030414000792003041400079NM 2003 4 14 AUS20030279 120030212A5310 STRAP BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INTERNAL SKIN REINFORCING STRAP LOCATED ON THE AFT SIDE OF FUSELAGE FRAME AT STA 1090 BETWEEN STRINGERS 26RT AND 27RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01. 2L73 4F4 FRTA3WE E2EA 20030415000702003041500070EU 2003 4 15 CA030327006 220030318A72615342 ENGINE BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU LEFT MAKING METAL W O OTHER O OTHER NRNOT REPORTED 1 CA 32262 (CAN) DURING A GROUND RUN, FOLLOWING A PROP REMOVAL AND REINSTALLATION DUE TO AN OIL LEAK, THE MAINTENANCE CREW OBSERVED AN UNUSUALLY HIGH OIL TEMP ON THE LT ENGINE. ENGINE OIL TEMP ALSO CONTINUED TO INCREASE AT AN UNUSUAL RATE DURING THE GROUND RUN. UPON FURTHER INVESTIGATION A SUBSTANTIAL AMOUNT OF METAL WAS FOUND IN ENGINE OIL SCAVENGE FILTER SCREEN. THE ENGINE WAS REPLACED AND THE AIRCRAFTRETURNED TO SERVICE. 2L72 3T4 T A24EU A196 20030415000742003041500074WP 2003 4 15 CA030327010 120030325A324650078902 WHEEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE MLG CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) MAIN WHEEL REPORTED TO LEAK ON THE ACFT.- DURING WHEEL REPAIR, A 4 INCHES CRACK WAS FOUND ON THE INNER TUBE WELL. 2L72 4F4 FRTA6WE E9NE 20030416000162003041600016EA 2003 4 16 SWIA200311674 120030104A274270623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07909SW3316 3316 7558 STAB TRIM CHANNEL 1 INOP MESSAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW RII 27-415. OPS CHECK GOOD AT THIS TIME. HSTA PN OFF: 8396-3 SN OFF: 728. 2L72 4F RTA21EA 20030416000212003041600021 2003 4 16 SWIA200311680 420030105A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AHRS MALFUNCTIONED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM07452SW7543 7543 7716 IN FLIGHT THE FIRST OFFICER'S AHAR INDICATES +3 DEGREES NOSE UP ON THE ADI. TRANSFERRED BOTH DISPLAYS TO AHAR NR 1 AND RETURNED TO DFW. REMOVED NR 2 AHRS COMPUTER AND REPLACED WITH A SERVICEABLE ONE IAW CL600 MM 34-21-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030416000352003041600035NM 2003 4 16 UPS03440363 120030308A5313BAC14981327075 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, FWD CARGO BAY, STA 720 - 740 STRINGER 47 RT FOUND CORROSION CRACK. CORROSION BLEND OUT 0.030 INCH X 1 INCH X 1 INCH EXCEED SRM LIMIT. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F RTA20WE 20030416000662003041600066NM 2003 4 16 UPS03440395 120030304A5312 BULKHEAD BOEING747 747200 1384847NM LT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, LT WING MLGWW - BS 1241 LBL 1 TO LBL 8 PRESSURE BULKHEAD WEB FOUND CORROSION AT BRACKET ATT SURFACE. CORROSION BLEND OUT (0.068 X 2 X 8 INCH) NOT WITHIN SRM 57-10-01 LIMITS, FOR REPAIR REER HX RS NR R53-43-34986 & UPS EA 747-53-20125. 2L74 4F RTA20WE 20030416000682003041600068EU 2003 4 16 MALA030228 120030405A2430 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FIRE A MALAF ACTIVATE FIRE EXT. A FLAME/FIRE NRNOT REPORTED 1 GL15361PX 340B249 DURING START OF FLIGHT 3113, RAMP REPORTED TO CREW RT ENGINE HAD A FIRE. BOTH DC GENERATORS WOULD NOT COME ON-LINE. GROUND PERSONNEL NOTED SMOKE FROM UNDER RT ENGINE COWL. NO INDICATION IN THE FLIGHT DECK. PILOT BLEW BOTH LT AND RT FIRE BOTTLES. AIRPORT FIRE DEPARTMENT THEN OPENED AND DISCONNECTED BOTH BATTERIES. BOTH ENGINE COWLS OPENED AND FIRE DEPARTMENT NOTED RT ENGINE HAD SOME WIRING BURNED. ARRANGED TO HAVE DTW MX GO TO YOW FOR FURTHER TROUBLESHOOTING. MAINTENANCE REPLACED LT & RT STARTER/GEN, REPLACED RT PDU, REPLACED RT ENGINE 533 HARNESS, REPLACED TERMINAL ENDS AT STARTER/GEN, PERFORMED ENGINE RUNS, ALL CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20030416000882003041600088NM 2003 4 16 SWAA030777 120030402A2750657327121 DRIVE GEAR BOEING737 7373H4 1384600NM LT MLG WW WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING APPROACH T/E FLAPS INDICATED SPLIT, WOULD NOT DEPLOY OR RETRACT. REMOVED AND REPLACED SHAFT DRIVE ASSY FOR LT WING T/E FLAPS PER MM. 2L72 4F RTA16WE 20030416001462003041600146SO 2003 4 16 C2XA03SH098 120030408A531014521699003 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK, THE LT BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 19-23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030416001562003041600156NE 2003 4 16 DLM90030294 220030327A7200V2528D5 ENGINE DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 2 SHUTDOWN A DALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO27904DA212979781 53384 020025 NUMBER 2 ENGINE SHUT DOWN ON DESCENT INTO DFW. FOUND NUMEROUS VSV AND ACC FAULTS. REPLACED ENGINE. 2L72 4F4 FRTA6WE E40NE 20030411000132003041100013NM 2003 4 11 SWAA030752 120030406A5752654645522C STRUCTURE BOEING737 7373H4 1384600NM RH AILERON TAB DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED 1/4D CHECK, FOUND RT AILERON TAB DELAMINATED. REMOVED AND REPLACED RT AILERON TAB PER MM. 2L72 4F RTA16WE 20030414000022003041400002NM 2003 4 14 SWAA030759 120030403A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR, LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030414000142003041400014NM 2003 4 14 SWAA030739 120030402A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29779SW 27884 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 4 HINGE WORN. REMOVED AND REPLACED HARDWARE AND BUSHING ON NR 4 HINGE PER MM. 2L72 4F RTA16WE 20030414000232003041400023NM 2003 4 14 SWAA030726 120030327A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 616, WL 201 AT LBL 65 & RBL 65. REPAIRED FRAME PER SWA T1 & BFG ER. 2L72 4F RTA16WE 20030414000372003041400037 2003 4 14 MEX2003055 420030302A2565 GIRT BAR BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE PAX DOOR STUCK W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23802AM 26270 AIRCRAFT RETURNED TO PLATFORM DUE TO LEFT AFT SLIDE DOOR NR 4 WAS NOT ARMED, ARMED AND DISARMED SYSTEM, AFT SLIDE DOOR 4 WAS CHECKED AND IT WAS STUCK. AIRCRAFT WAS SENT TO THE HANGAR. EMERGENCY MECHANISM WAS ADJUSTED IAW MM, TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20030414000382003041400038EA 2003 4 14 CA030312011 120030303A32331700810J ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG DAMAGED W O OTHER N FALSE WARNING APAPPROACH 1 CA 22822 (CAN) GEAR WAS EXTENDED ON APPROACH, GEAR DISAGREE MESSAGE POSTED, RT GEAR UNSAFE RED LIGHT ILLUMINATED. CREW CYCLED GEAR AND PROBLEM OCCURRED AGAIN BUT WITH LT GEAR UNSAFE RED LIGHT ILLUMINATED INSTEAD OF RT GEAR WAS AGAIN RETRACTED AND AN ALTERNATE EXTENSION PERFORMED. ONCE AGAIN LT GEAR UNSAFE RED LIGHT ILLUMINATED. CREW FLEW PAST TOWER TO ENABLE A VISUAL INSPECTION OF GEAR TO BE CARRIED OUT - TOWER CONFIRMED THAT GEAR APPEARED TO BE DOWN AND LOCKED. AN UNEVENTFUL LANDING WAS PERFORMED. LT GEAR UNSAFE RED LIGHT ILLUMINATED AND RT GEAR UNSAFE RED LIGHT FLASHED BEFORE GREEN DOWNLOCKED LIGHT ILLUMINATED. BOTH MLG ACTUATORS WERE REPLACED AND FUNCTIONAL CHECKS PERFORMED. A/C WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030414000472003041400047CE 2003 4 14 CA030312022 120030308A5210 SEAL CESSNA500 550 2076604CE PWA 530 PW530A NE PAX DOOR CONTAMINATED W BA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE AT FL 410, CREW NOTED INCREASED NOISE LEVEL AND CABIN ALT RISING. LOUD BANG FOLLOWED WITH DECOMPRESSION OF CABIN. SECONDARY DOOR SEAL HELD AGAINST TOTAL DECOMPRESSION. EMER DESCENT AND UNSCHEDULED LANDING FOLLOWED. ON GROUND IT WAS FOUND THAT CONSIDERABLE WATER WAS PRESENT IN DOOR SEAL AREA, BOTTOM PORTION. A/C WAS IN HOT AND HUMID ENVIRONMENT, WHICH CAUSED VISABLE SIGNS OF CONDENSATION BOTH INSIDE AND EXTERNALLY. A/C THEN MADE STOP WERE HEAVY RAINS WERE ENCOUNTERED. ONCE IN CRUISE HEADING NORTH, OAT WAS APPROX -50 DEGREES, APPEARS TO HAVE FROZEN ACCUMULATED WATER, WHICH CAUSED A PARTIAL OPENING OF PRIMARY SEAL. DOOR SEAL AND FEED LINE WAS DRIED OUT. A/C RETURNED TO SERVICE. 1L72 4F4 F A22CE E00053EN 20030414000512003041400051NM 2003 4 14 S03J27006 120030209A2720 CONTROL CABLE BOEING747 747400 NM GE CF6 CF680C2B2 30025NE RUDDER OUT OF RIG W SAJFO OTHER O OTHER TXTAXI/GRND HDL 1 WP03 30761 RUDDER DOES NOT FULL DEFLECT TO RT . RUDDER & RUDDER TRIM SYSTEM RIG CHECK FOUND CONTROL CABLE TENSION WAS OUT OF LIMIT. PERFORM RUDDER AND RUDDER TRIM CONTROL SYS ADJ IAW 27-21-00. PERFORM RUDDER TRIM SYS TEST NML. EON 744-27-632292-0017 R1 IS ISSUED TO PERFORM ONE TIME INSPECTION OF RUDDER CABLE TENSION FOR 744F FLEET.5. ALL THE INSPECTION RESULTS WILL BE PROVIDED TO BOEING FOR FURTHER INVESTIGAT. 2L74 4F4 FRTA20WE E13NE 20030414000532003041400053NE 2003 4 14 MEX2003073 220030314A7200 BLADE DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE LT ENGINE DAMAGED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW231075T 49724 DURING TRANSIT CHECK, FOD ON LT ENGINE WAS DETECTED. DURING INSPECTION, DETECTED A BLADE WITH DAMAGE. FAN BLADE FROM ENGINE NR 1 WAS BLENDED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030414000612003041400061SW 2003 4 14 HEEA085857 120030328A6510407340339101 BEARING BELL 407 407 1182206SW T/R SHAFT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 MAKING BLACK GREASE. REPLACED WITH SERVICEABLE BEARING. 1G71 3U O H2SW 20030407000282003040700028NM 2003 4 7 ASAA0380105 120030127A525001T023T507507 DOOR DOUG MD80 MD83 3023681NM COCKPIT OUT OF RIG A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT DOOR COULD NOT BE OPENED. RE-RIGGED DOOR TO INCREASE CLEARANCES, WAS BINDING AT LOWER LEFT CORNER. DOOR THEN OPERATED PROPERLY. (M) 2L72 4F RT 20030407000422003040700042WP 2003 4 7 GTIA030029 120030116A5321 FLOORBOARD DOUG DC9 DC983 3022083WP LAVATORY DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND FLOORBOARD UNDER FORWRAD LAVATORY IS DELAMINATED AROND LAVATORY CONNECTION HOLES, AND FASTENERS ARE CORRODED. REMOVED FLOORBOARD UNDER FORWARD LAVATORY STATION 218-275. REPAIRED FLOORBOARD UNDER FORWARD LAVATORY. INSTALLED FLOORBOARD. (M) 2L72 4F RTA6WE 20030408000102003040800010WP 2003 4 8 ASAA0380084 120030114A5320AE12DC1D0808 CLIP DOUG DC9 DC983 3022083WP FS 1155 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY BRACKET ANGLE CLIP CRACKED. REPLACED CLIP PER SRM 51-30-1. (M) 2L72 4F RTA6WE 20030408000662003040800066EU 2003 4 8 03094311 120030404A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33112UHR WP EMERGENCY LIGHT DISCONNECTED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27311UE 41029 DURING TAXI/GROUND HANDLING EMERGENCY TRACK LIGHTING INOPERATIVE ROW 2-4. MAINTENANCE PERSONNEL RESECURED CONNECTOR AT TRACK LIGHT. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA41NM E4WE 20030410000282003041000028NM 2003 4 10 SWAA030607 120030313A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 328, WL 208 & LBL 28 AND BS 344, WL 208 & LBL 8. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20030416001882003041600188EU 2003 4 16 AWXA200300358 120030409A5610 WINDOW AIRBUS320 A320231 3930325EU COCKPIT FAILED A AWXAO OTHER O OTHER CRCRUISE 1 WP28631AW 077 EN ROUTE FROM PHX TO SNA AT CRUISE THE FIRST OFFICER`S WINDSHIELD INNER PANE SHATTERED SENDING GLASS ALL OVER FLIGHT DECK. EMERGENCY DECLARED, LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER`S WINDSHIELD ASSEMBLY IAW AMM. AS A PRECAUTION ALSO REPLACED RT WINDOW HEAT COMPUTER IAW AMM, OPERATIONAL TEST WAS GOOD IAW AMM. VENDOR BENCH TEST OF WINDOW HEAT COMPUTER S/N 4160031800218 WAS NO FAULT FOUND. CLEARED MEMORY, INSPECTED UNIT PER CMM 30-42-36, AND RETURNED TO SERVICE. VENDOR INVESTIGATION OF WINDSHIELD FAILURE DETERMINED INNER PANE FAILED DUE TO IMPACT DAMAGE ON AFT EDGE 11" UP FROM BOTTOM AFT CORNER. DAMAGE TO THE EDGE PROPAGATED DUE TO THERMAL AND MECHANICAL STRES 2L72 4F RTA28NM 20030416001892003041600189SO 2003 4 16 C2XA03SH088 120030407A531514521713005 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030416001952003041600195NM 2003 4 16 AALA20030290 120030306A5320 PLATE BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21624AA 24582 TUL - FOUND DECK PLATE AFT END CORROSION 12 INCHES RIGHT OF CENTER. BLENDED CORROSION AND INSTALLED DOUBLER PER SRM 53-60-51. (M) 2L72 4F RTA2NM 20030415000492003041500049EA 2003 4 15 CA030321012 120030318A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) SIDE WINDOW SHATTERED OUTER PANE IN FLIGHT TSN 3205HRS 2L72 4F4 FRTA21EA E15NE 20030415000632003041500063EA 2003 4 15 CA030326005 120030323A7921 OIL COOLER DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE NR 1 ENGINE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN) NR 1 ENGINE OIL COOLER FOUND LEAKING. OIL COOLER REPLACED. SERIAL NR UNKNOWN AS DATA PLATE MISSING FROM UNIT. TRYING TO TRACE INFORMATION 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030415000672003041500067NM 2003 4 15 CA030327003 120030312A2710BACB10A824 BEARING BOEING737 7372T7 1384482NM PWA JT8 JT8D17 52049NE AILERON FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB IN MANUAL FLIGHT , BEOND 5 DEG. LT WHEEL DEFLECTION AILERONS FELT VERY HEAVY 9 AS IF IN MANUAL REVERSION ) AT THIS POINT IN TIME RUDDER TRIM 0 UNITS AND ADI BALL CENTERED. AILERON TRIM 1/2 UNIT LT IN STABLE CRUISE. AILERON TOWER SHAFT UPPER BEARING REPLACED AND SYSTEM CHECKED SERVICEABLE. 2L72 4F4 FRTA16WE E2EA 20030416000452003041600045NM 2003 4 16 QXEA0300411 120030327A5270 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DIRTY A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09409QX 4051 HLN-ON FLIGHT NUMBER 2323, AT FL250 ENCOUNTERED MODERATE TURBULENCE FROM MOUNTAIN WAVE ACTIVITY. FUSELAGE DOOR WARNING LIGHT ILLUMINATED AND SYSTEMS PAGE SHOWED A RED AFT PASSENGER SERVICE DOOR ON CAPTAINS SIDE. COMPLIED WITH EMERGENCY CHECKLIST. CLEANED ICE/WATER/DEBRIS FROM PROXIMITY SENSOR. OPEN AND CLOSED DOOR 3-4 TIMES. SYSTEM OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030416000672003041600067NM 2003 4 16 QXEA0300407 120030327A5270 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DIRTY A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09409QX 4051 HLN ON FLIGHT 2323- AT FLIGHT LEVEL 250, ENCOUNTERED MODERATE TURBULANCE FROM MOUNTIAN WAVE ACTIVITY. FUSELAGE DOORS WARNING LIGHT ILLUMINATED AND SYSTEMS PAGE SHOWED A RED AFT PASSENGER SERVICE DOOR ON CAPTIAN'S SIDE. COMPLETED EMERGENCY CHECKLIST AND FLIGHT ATTENDANT REPORTED DOOR WAS CLOSED AND HANDLE WAS IN CLOSED POSITION. NO ABNORMAL SOUNDS, LIGHT WENT OUT AFTER LANDING. CLEANED ICE/WATER/DEBRIS FROM PROXIMITY SENSOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030416001512003041600151EA 2003 4 16 QXEA0300431 120030402A5754 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA RT LE SLAT CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX-RT SLATS CHAFING AGAINST UPPER WING SURFACE AT WS.178.00 AT INBOARD DISCONNECT SENSOR AREA. REPAIRED IAW CRJ700 SRM 51-25-26, SRM 51-00-02 AND SRM 51-25-16. 2L72 4F RTA21EA 20030416001682003041600168SO 2003 4 16 C2XA03SH087 120030407A532014522461011 DOUBLER EMB 145 EMB145ER 3260211SO BEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV-DURING C CHECK THE RIGHT HAND OMEGA BEAM DOUBLER AT FRAME 22 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030416001972003041600197NM 2003 4 16 AALA20030292 120030306A5320 PLATE BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21624AA 24582 TUL - FOUND DECKPLATE HAS CORROSION AFT END, 6.5 INCHES RIGHT OF CENTER. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-60-51. (M) 2L72 4F RTA2NM 20030416001982003041600198NM 2003 4 16 AALA20030293 120030306A5320 INTERCOSTAL BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21624AA 24582 TUL - FOUND STATION 1660-1680 CENTER INTERCOSTAL CORRODED. REMOVED INTERCOSTAL INSTALLED NEW INTERCOSTAL. (M) 2L72 4F RTA2NM 20030416002082003041600208 2003 4 16 SWAA030773 420030403A2565 CABLE BOEING737 7375H4 138449DNM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030416002172003041600217NM 2003 4 16 AALA20030202 120030215A3350P4010049 BATTERY BOEING757 757223 1384957NM CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21627AA 24585 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD BAG BIN EMERGENCY EXIT LIGHTS AT 20D, 22C, AND 24D INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002202003041600220NM 2003 4 16 AALA20030207 120030219A3397 WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21184AN 29594 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK WIRING BROKEN AFT OF COACH DIVIDER. REPLACED DAMAGE SECTION OF EMERGENCY EXIT LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002252003041600225NM 2003 4 16 AALA20030242 120030224A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21187AA 32381 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002372003041600237NM 2003 4 16 CALA0300174 120030405A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND FLOOR SUPPORT CORRODED ON UPPER SURFACE AT STA 328-344, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E2GL 20030416002472003041600247NM 2003 4 16 CALA0300187 120030408A5542 SKIN BOEING757 757224 1384958NM RUDDER CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0921108 27298 THE LT RUDDER SKIN SUSTAINED IMPACT DAMAGE BY A WORKSTAND. THE SKIN WAS DENTED, DELAMINATED, AND HAD A 1.875 INCH CRACK AT RUDDER STA 110. THE SKIN WAS REPAIRED IAW ECRA 5540-01164. 2L72 4F RTA2NM 20030416002502003041600250SO 2003 4 16 C2XA03SH094 120030408A531014521725001 SILL EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV DURING C CHECK THE LEFT SILL AFT OF THE PASSENGER DOOR WAS FOUND HAVE CORROSION BETWEEN FRAMES 19-20. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030416002562003041600256NM 2003 4 16 QXEA0300440 120030405A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PSC- EMERGENCY FLOOR STRIP LIGHTING HAS TWO MISSING RED LIGHTS ON SECOND STRIP FOR FORWARD EMERGENCY EXIT. REMOVED AND REPLACED FLOOR STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030416002662003041600266NM 2003 4 16 CALA0300186 120030409A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, LBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030416002672003041600267EA 2003 4 16 COMA0360183 120030322A3250 SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG STEERING MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01940CA 7048 FLIGHT 5930 CREW REPORTED AT BEGINNING OF TAKEOFF ROLL RECEIVED A STEERING INOP CAUTION MESSAGE. TAKEOFF WAS ABORTED AT LESS THAN 50 KTS. AFTER CLEARING THE RUNWAY, CREW RESET THE STEERING ARM SWITCH, WHICH CLEARED THE MESSAGE. A SUBSEQUENT TAKEOFF WAS PERRFORMED NORMALLY. 2L72 4F RTA21EA 20030416002782003041600278NE 2003 4 16 AALA20030276 220030302A7510 DUCT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT ENGINE DAMAGED A AALAK NONE J WARNING INDICATION CLCLIMB 1 SW21278AA 49294 MIA - FLT 2081 - EN ROUTE FLL-DFW, ON CLIMB-OUT, LEFT THROTTLE BECAME DIFFICULT TO MOVE. SHORTLY THEREAFTER THERE WAS AN ENGINE FIRE WARNING ON LEFT ENGINE. NO INDICATION OF FIRE. ACCOMPLISHED CHECKLIST, FIRE WARNING DISAPPEARED WITH THROTTLE REDUCTION. LANDED MIA WITHOUT INCIDENT. REPLACED LEFT ENGINE UPPER RIGHT ANTI-ICE DUCT. REPLACED FORWARD CUTOFF CABLE AND LEFT ENGINE THROTTLE CABLE. ACCOMPLISHED CABLE RIG CHECK AND ENGINE RUN UP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030416000202003041600020 2003 4 16 SWIA200311678 420030105A3414320AS1 INDICATOR EMB 120 EMB120ER 3260203SO AIR SPEED MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07562SW6547 6547 120336 ABORTED TAKEOFF AT 50-60 KNOTS DUE TO TRIPLE CHIME, RED MASTER WARNING LIGHT AND HIGH SPEED AURAL ANNUNCIATION. REPLACED BOTH LT AND RT AIRSPEED INDICATORS. GROUND TESTED OPS CHECK GOOD. LEFT S/N OFF AJ102. 2L72 4T RTA31SO 20030416000372003041600037EU 2003 4 16 MALA030234 120030409A3350PN330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY EXIT INOPERATIVE A MALAK NONE L NO TEST NRNOT REPORTED 1 GL15449XJ 340B449 EMERGENCY EXIT LOCATOR 28LN WOULD NOT TURN ON. FOUND NO POWER TO LIGHT. MAINTENANCE REPLACED POWER SUPPLY 20LN P/N 3301-51, SN/OFF 2196, SN/ON 1366 IAW SAAB AMM 33-50-10-4. OPS CHECK GOOD. 2L72 4T RTA52EU 20030416001102003041600110NM 2003 4 16 SWAA030787 120030407A53106935365 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030416001152003041600115NE 2003 4 16 DLM88030252 220030318A7250JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 DAMAGED A DALAEC ENGINE SHUTDOWN ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 SO27913DE35769 49956 718208 ON T/O HEARD LOUD BANG AND NR 2 ENG EPR AT 1.5. WITH CLIMB POWER SELECTED RT ENG STAYED AT IDLE 3-5 MINS. THEN OIL QTY WENT TO 0 AND RT ENGINE WAS SHUT DOWN. A/C RETURNED TO ATL. FOUND RT ENG TURBINE DAMAGED. NO DAMAGE FOUND IN FAN OR COMPRESSOR AREA. ENG HAS 1726.7 HRS. REPLACED ENGINE. 2L72 4F4 FRTA6WE E9NE 20030416001162003041600116NM 2003 4 16 DL76L030254 120030318A335020131A BATTERY PACK BOEING767 767332 1382001NM CABIN UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27198DN 28455 EMERGENCY EXIT SIGN AT 1L AND 1R INOP. REPLACED M1208 BATTERY PACK, CHECKS OK. 2L72 4F RTA1NM 20030416001392003041600139NM 2003 4 16 SWAA030789 120030408A53106517582 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727D AND BS 727C, LT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030416001552003041600155NM 2003 4 16 DLM88030293 120030327A7700JT8D219 BLADE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE DAMAGED A DALAA UNSCHED LANDING CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27938DL35541 49811 725368 AFTER TAKEOFF, GSO LEFT ENGINE INGESTED LARGE BIRD. MANY BLADES BENT AND AT LEAST ONE MIDSPAN SHROUD BROKEN OFF. REPLACING ENGINE. 2L72 4F4 FRTA6WE E9NE 20030410000412003041000041NE 2003 4 10 SWAA030630 220030318A7200CFM56 ENGINE BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE NR 1 FLAMED OUT A SWAABA EMER. DESCENT UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SW29718SW 27852 874272 IN-FLT SHUTDOWN, DIVERSION, DECLARED EMERGENCY. EN ROUTE TO MCI, NR 1 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030410000602003041000060 2003 4 10 SWAA030642 420030320A256565C19901 CABLE BOEING737 7373T5 1384608NM SERVICE DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030410000632003041000063NM 2003 4 10 SWAA030644 120030319A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED JUST AFT OF BS 727E, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001242003041000124SO 2003 4 10 SIMA200304801 120030212A2611 WARNING SYSTEM EMB 135 EMB135LR 3260305SO CARGO BAY FALSE ACTIVATIONA SIMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW21727AE 145326 BOS - FLT 4579 - CREW REPORTED A BAGGAGE SMOKE WARNING WHILE ON TAXIWAY. FIRE BOTTLE WAS FIRED THEN A VISUAL CHECK THROUGH THE PEEPHOLE SHOWED NO FIRE. THE INDICATION WENT OUT AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK WAS COMPLIED WITH IAW EMB MM WITH NO DEFECTS NOTED. THE FIRE BOTTLE WAS REPLACED AND THE AIRCRAFT WS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030410001422003041000142NM 2003 4 10 SWAA030696 120030327A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 750 AT STR 19R, BS 755 AT STR 21R AND BS 763 AT STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001932003041000193NM 2003 4 10 GAIA03012OP 120030304A323421ER3 CONTROL HANDLE BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE COCKPIT STICKING A GAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW076831 20184 DURING TAKE OFF, ALL THREE GEAR UNSAFE LIGHTS (RED) AND TAIL SKID LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE DOORS LIGHTS OF FE PANEL WERE NOT ILLUMINATED. AIRCRAFT PERFORMED AN AIR TURN BACK AND LANDED WITHOUT FURTHER INCIDENT AT JAX. FOUND CONTROL HANDLE POSITION SWITCH, STICKING. CLEANED CONTROL HANDLE POSITION SWITCH. PERFORMED GEAR RETRACTION AND EXTENSION. SYSTEM OPERATIONALLY CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20030410001952003041000195NM 2003 4 10 DL76G030126 120030204A2740 CONTROL MODULE BOEING767 767332 1382001NM HORIZ STAB MALFUNCTIONED A DALAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO271609 30574 REJECTED TAKEOFF DUE UNSCHEDULED STAB TRIM. REPLACED THE LEFT AND RT STAB POS TRANSMITTER. MEGGED WIRING FROM RT STAB POS TRANSMITTER TO RT FSPM, ALL CHECK OK. REPLACED LEFT STCM. REPLACED RT SAM MODULE PER AMM. INSTALLATION TESTS OK. INCLUDING AUTOPILOT INTERFACE AND OUTBOARD AILERON LOCKOUT TESTS. 2L72 4F RTA1NM 20030411000032003041100003NM 2003 4 11 SWAA030722 120030330A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 180 & LBL 16. REMOVED AND REPLACED BULKHEAD WEB PER SWA ACO & SRM. 2L72 4F RTA16WE 20030411000122003041100012NM 2003 4 11 SWAA030751 120030406A57546546430190 SKIN BOEING737 7373H4 1384600NM R WING FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED 1/4D CHECK, FOUND RT INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20030414000102003041400010NM 2003 4 14 SWAA030742 120030403A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BETWEEN STRINGERS 15L AND 16L, AND BS 500D, STRINGER 13R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030414000192003041400019 2003 4 14 SWAA030731 420030401A256565C19901 CABLE BOEING737 7372H4 138448CNM AFT ECAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 DURING SCHEDULED C 2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030414000352003041400035WP 2003 4 14 MEX2003054 120030302A2932ST107Q TRANSMITTER DOUG DC9 DC982 3022082WP HYD PRESSURE FAILED W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23491SH 49150 DURING CREW CABIN REVISION, CAPTAIN REPORTED LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH 3000 PRESSURE INDICATION. LT TRANSMITTER HYDRAULIC PRESSURE WAS REPLACED AND IT WAS PERFORMED OPERATIONAL TEST WITH ZERO PRESSURE INDICATION, IAW MM, TESTS CORRECT. 2L72 4F A6WE 20030414000522003041400052NE 2003 4 14 MEX2003075 220030316A7200JT8D219 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE NR 2 FAILED W ASMFA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW23803ML 49726 AIRCRAFT RETURNED TO PLATFORM DUE TO NR 2 ENGINE TAKE OFF THRUST DID NOT ACCELERATE. THE MOISTURE TRAP WAS DRAINED AND TEST WAS CORRECT IAW MM. 2L72 4F4 FRTA6WE E2EA 20030414000702003041400070EU 2003 4 14 AUS20030241 120030228A5320D5347576500200 SILL AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE CARGO DOOR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BULK CARGO DOOR SILL CONTAINED LEVEL 2 CORROSION. AREA OF CORROSION 52.8MM (2IN) BY 25.4MM (1IN) AND 1.27MM (0.050IN) DEEP. FOUND DURING INSPECTION IAW MRBR 53.41.07. 2L72 4F4 FRTA28NM E29NE 20030414000762003041400076 2003 4 14 AUS20030248 420030227A25624535004 ELT BOEING737 73776N 13844CHNM CABIN DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELT CONTINUOUS TRANSMISSION EVEN WHEN SWITCHED OFF. CAUSED BY WATER CONTAMINATION IN THE CONNECTOR. 2L72 4F RTA16WE 20030416001722003041600172NM 2003 4 16 DLM88030318 120030315A5610 CAM FOLLOWER DOUG MD88 MD88 3023688NM COCKPIT OUT OF ADJUST A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27909DL 49540 FIRST OFFICER'S WINDOW WILL NOT OPEN. RESET CAM FOLLOWER AND ADJUSTED, OPS GOOD. 2L72 4F RTA6WE 20030416001942003041600194NM 2003 4 16 AALA20030288 120030305A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21792AN 30253 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BULB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030416002092003041600209NM 2003 4 16 SWAA030774 120030403A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT BS 360, BETWEEN STR 7R AND STR 8R AND AT BS 400, BETWEEN STR 8L AND STR 9L. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030416002162003041600216NM 2003 4 16 AALA20030193 120030112A3397 WIRE BOEING757 757223 1384957NM COCKPIT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21614AA 24490 DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED COCKPIT OVERHEAD EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002362003041600236NM 2003 4 16 CALA0300173 120030405A5320 CREASE BEAM BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A .2500 INCH CRACK IN WEB AT STA 386 INBOARD OF CREASE BEAM. THE CREASE BEAM WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-70-13. 2L72 4F4 FRTA16WE E2GL 20030416002682003041600268NM 2003 4 16 UPS03240422 120030323A5330 SKIN BOEING727 727173C 1384059NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C EVIDENCE OF CORROSION AT CIRCUMFERENTIAL JOINT 480 BETWEEN STRINGER 10R AND 14R. REPAIRED IAW UPS REPAIR FILE 727-53-20106. 2L73 4F A3WE 20030416003602003041600360NM 2003 4 16 UPS03240048 120030106A5330 SKIN BOEING727 72721C 138400MNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE: C, POPPED RIVET HEAD AT BS 1180 STR 7L DUE TO CORROSION. ALSO FURTHER SIGNS OF CORROSION ON STR 7L BETWEEN 1180 & 1150. LFEC INSP PERFORMED AT 1180 STR 7L, 10-15 PERCENT MATERIAL LOSS EVIDENT. CORRODED SKIN REMOVED APPROX 10 INCHES X 5 INCHES STA 1183-1178. LIGHT SURFACE CORROSION REMOVED FROM EXPOSED BONDED SKIN DOUBLER IAW SRM 51-10-02. REPAIRED CARRIED OUT IAW SRM 53-30-03 FIG 3A, CATAGORY-B REPAIR. 2L73 4F A3WE 20030416003682003041600368NM 2003 4 16 UPS03240112 120030107A5755 STRUCTURE BOEING727 72722C 138400FNM NR 1 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, NDT CARRIED OUT ON SPOILERS, SPOILER NR 1 FOUND TO HAVE CORE DAMAGE AND WATER INGRESSION. SPOILER REPAIRED IAW MM 27-61-01 & SRM 51-40-5. 2L73 4F A3WE 20030416003802003041600380NM 2003 4 16 UPS03240119 120030109A2721 SKIN BOEING727 72722C 138400FNM RUDDER TAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, LOWER RUDDER TAB HAS AN AREA OF DELAM AT LWR AFT CORNER RT SIDE. SKIN CRACK AND LARGE DENT ON LT SIDE 12TH FROM BOTTOM ON T/E AREA LOWER RUDDER TAB REPLACED IAW MM 27-20-11. 2L73 4F A3WE 20030416003952003041600395SO 2003 4 16 SWIA200311713 120030112A3397 WIRE EMB 120 EMB120ER 3260203SO NAV LIGHT CHAFED A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07569SW 120344 NAV LIGHT CIRCUIT BREAKER POPPED. RETURNED TO GEG. FOUND CHAFED WIRES IN RIGHT SIDE LEADING EDGE. REPAIRED WIRES AS REQUIRED AS PER EMB MM 33-00-00. LIGHT OPS CHECK GOOD. 2L72 4T RTA31SO 20030416004032003041600403WP 2003 4 16 UPS03840013 120030113A33506012235 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A IPXAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO01803UP 46073 EMERGENCY LIGHTS INOP ON PREFLIGHT. C/BS OUT AND SWITCH IN OFF POSITION AFTER WEEKEND. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK OK. 2L74 4F RT4A25 20030416004042003041600404NM 2003 4 16 UPS03240118 120030113A5755 HINGE BOEING727 72722C 138400FNM NR 11 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, SMALL CRACK ON RT WING UPPER T/E AT SPOILER NR 11 OUTER HINGE CUTOUT. REPAIR CARRIED OUT IAW SRM 57-30-4. 2L73 4F A3WE 20030416004072003041600407EA 2003 4 16 SWIA200311706 120030114A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07589SW 7072 REAR-MOST OVERHEAD EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPS CHECK GOOD. 2L72 4F RTA21EA 20030416004092003041600409EA 2003 4 16 SWIA200311703 120030114A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG STRUT OUT OF ADJUST A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07927SW 7693 ON GEAR RETRACTION GEAR DISAGREE WARNING ACCOMPANIED BY NOSE DOOR OPEN AND NOSE GEAR DOWN INDICATION. RETURNED TO SFO. ADJUSTED NLG STRUT EXTENSION PROX SENSOR. OPS CHECK GOOD. 2L72 4F RTA21EA 20030417000012003041700001SO 2003 4 17 SWIA200311701 120030116A323012043270501 RELAY EMB 120 EMB120ER 3260203SO MLG MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07271YV7 7 120271 GEAR WOULD NOT RETRACT, ONLY THE RED INTRANSIT LIGHTS CAME ON, GEAR STAYED DOWN AND LOCKED. THE HANDLE WOULD MOVE OK BUT THE GEAR DID NOTHING. RETURNED TO PDX. REMOVED AND REPLACED RELAY BOX, CONDUCTED GEAR SWINGS 15 TIMES. ALL CHECKS GOOD IAW EMB 120 MM 32-32-00. 2L72 4T RTA31SO 20030417000162003041700016EA 2003 4 17 SWIA200311723 120030121A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07594SW 7285 FUEL AND EXHAUST ODOR THROUGH THE PACKS AFTER APU START AND BLEED SWAP. RAN AIR CONDITIONER SYSTEM IAW CRJ MM 21-51-00. INSPECTED APU COMPARTMENT, NO LEAKS FOUND. SYSTEM OPERATED NORMALLY WITH NO ODOR OF FUEL OR EXHAUST IN COCKPIT AND CABIN AREA. 2L72 4F RTA21EA 20030417000172003041700017EA 2003 4 17 SWIA200311724 120030118A1430 FASTENER CNDAIRCL600 CL6002B19 1900309EA LT ELEVATOR SHEARED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07594SW 7285 DURING ELEVATOR FIRST FLIGHT OF THE DAY CHECKS FOUND THAT SYSTEM NR 3 WOULD NOT OPERATE THE LT ELEVATOR. SYSTEM NR 1 AND 2 OPERATE NORMALLY. FOUND LEFT ELEVATOR NR 3 PCU HI-LOC SHEARED AT ATTACH POINT ON AFT LINKAGE. REMOVED HI-LOC AND REPLACED IT WITH A SERVICEABLE ONE IAW SRM 51-42-20. OPS CHECK GOOD. 2L72 4F RTA21EA 20030417000212003041700021NM 2003 4 17 UPS03240053 120030114A5312 PANEL BOEING727 72721C 138400MNM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL STA 245 LT SIDE PANEL. REPAIR CARRIED OUT IAW SRM 51-40-2. 2L73 4F A3WE 20030417000222003041700022NM 2003 4 17 UPS03540069 120030122A3260 BULB BOEING757 75724APF 1384969NM MLG INDICATOR BURNED OUT A IPXAL ABORTED APPROACH P NO WARNING INDICATION LDLANDING 1 SO01414UP 23854 DECLARED EMERGENCY, LEFT MAIN GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE WITH THE GEAR HANDLE DOWN. NO GEAR DISAGREE OR DOOR LIGHTS WERE DISPLAYED. RELAMPED LEFT GEAR ANNUNCIATOR PER MM 33-16-02, OPS CHECK NORMAL. PERFORMED PSEU BITE PRECAUTIONARY, NO DEFECTS NOTED. SYSTEM TEST NORMAL PER MM 32-61-00-5. 2L72 4F RTA2NM 20030417000262003041700026WP 2003 4 17 UPS03840072 120030117A53205613430505 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C-2, FORWARD PIT STA 140, BL45R AT CUSP, SUPPORT FITTING CORRODED. FABRICATED NEW PART IAW DAC DWG 5613430. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED AND DRILLED IAW DAC DWG 5613430 AND DC8 SRM 51-1- 20. INSTALLED FITTING IAW DC8 SRM 51-1-20D. REINSTALLED MAIN CABIN SIDEWALL PANEL AT STA 100-150 R AND FWD PIT PANEL AB40 IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030417000362003041700036NE 2003 4 17 MALA030131 220030127A7200 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 OVERHEATED A MALAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL15501XJ E2208 DURING CLIMBOUT ON FLIGHT 3564 OF MEM-JAN, NR 3 ENGINE VIBRATION LIGHT ILLUMINATED. EGT ROSE RAPIDLY N1 DROPPED, SHUTDOWN ENGINE APPROXIMATELY 649 DEGREES EGT. PAX REPORTED SPARKS AT TIME OF VIBE, DISCHARGED NR 3 ENGINE NR 1 BOTTLE. MAINTENANCE DETERMINED NR 3 ENGINE WAS OVERHEATED. INSTALLED NR 3 ENGINE FERRY KIT IAW JOB CARD ON NR 3 ENGINE. A/C HAS BEEN INSPECTED AND IS SAFE FOR FERRY FLIGHT FROM MEM TO MSP. MAINTENANCE IN MSP, REMOVED AND REPLACED NR 3 ENGINE ASSEMBLY IAW JOB CARD 7100-502 PN 2-003-040-15, SN/ON P07889, SN/OFF P07703. REF WORK PACKAGE FOR DETAILS. 2H74 4F4 FRTA49EU E6NE 20030417000522003041700052NM 2003 4 17 UPS03440091 120030125A3350 LIGHT BOEING747 747123 1384873NM MAIN DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 INSPECTION TYPE: PFLT, INOPERATIVE MAIN DECK EMERGENCY LIGHT AFT RIGHT OF CREW LADDER. OPERATIONAL CHECK NORMAL, COULD NOT DUPLICATE. 2L74 4F A20WE 20030417000572003041700057EU 2003 4 17 MALA030134 120030128A3297 WIRE SAAB SF340 340B 7860101EU MLG BROKEN A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15425XJ 340B425 ON APPROACH SELECTED GEAR DOWN AND GOT AN ANTI-SKID CAUTION. ALSO FLIGHT IDLE STOP HAD TO BE PULLED. MAINTENANCE REPLACED WHEEL SPEED TRANSDUCER. NO FIX OHMED 6GA P4/J4 TO ANTI SKID BOX FOUND BREAK AT WIRE. REPAIRED BREAK IAW SF340 MM 32-43-00. 2L72 4T RTA52EU 20030417000582003041700058NM 2003 4 17 PCAA0301026 120030126A2910 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM LEAKING A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA13826EX 389 PIT-FLIGHT 3716 CREW REPORTED HYDRAULIC FLUID LOSS OF NR 1 SYSTEM WHILE IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE INBOARD ROLL SPOILER HYDRAULIC LINE LEAKING BETWEEN THE FUSELAGE AND NR 1 NACELLE. TWO FLEXIBLE LINES WERE INSTALLED AS AN INTERIM REPAIR. AIRCRAFT GROUND RAN AND LEAK CHECK WAS GOOD. HYDRAULIC SYSTEM WAS REPLENISHED AND BLED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417000612003041700061EU 2003 4 17 YENA200302 120030130A3350NSA93412101 MODULE AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15520JB 1446 DURING WEEKLY CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED DIODE MODULE 1158VD, OPS CHECK OF EMERGENCY LIGHTING OK PER AMM 33-51-00-710. 2L72 4F RTA28NM 20030416001122003041600112NM 2003 4 16 SWAA030788 120030408A53106517582 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 380, BS 460 AND BS 488 AND BETWEEN BS 727D AND BS 727E, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030416002582003041600258SO 2003 4 16 LR7A03039 120030407A5311 FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 571 5025 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB5302 FOUND RT FS 880 FRAME WEB CRACKED 1.0 INCH, EMANATING FROM LIGHTENING HOLE AT RBL 66, WL 200. REPAIRED IAW SRM SMP 583 51-140-17. NR 2001. 2H74 4T A1SO 20030416002932003041600293WP 2003 4 16 AALA20030302 120030309A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21295AA 49307 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT DOOR SERVICE LIGHT INOPERATIVE. REPLACED AFT SERVICE DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030416003152003041600315NM 2003 4 16 AALA20030307 120030225A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21366AA 25193 AFW - FLOORBEAM AT STATION 347 HAS CORROSION ON UPPER SURFACE REMOVED. MATERIAL REMAINING IS BEYOND SRM LIMITS, REQUEST ENGINEER APPROVAL TO REPAIR PER SKETCH. REMOVED EXISTING REPAIR STRAPS TO INCORPORATE SINGLE STRAP. REMOVED CORROSION PER REF B AND VERIFIED COMPLETELY REMOVED. FABRICATED REPAIR STRAP AND ENSURED 3 ROWS OF FASTENERS. ALODINED AND PRIMED. FILLED BLEND. INSTALLED REPAIR STRAP WITH SEALANT. (M) 2L72 4F RTA1NM 20030416003632003041600363CE 2003 4 16 DXTA200300003 120030106A2130NZ042 CIRCUIT BOARD CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE CABIN PRESSURE FAILED E DXTAK NONE J WARNING INDICATION DEDESCENT 1 GL07807QS 5600617 DURING DESCENT FROM 35,000, THE EMERGENCY PRESSURIZATION CAME ON AT ABOUT 18,000 AT 10 DEG AND STAYED ON FOR 3-4 SECONDS. 2L72 4F4 FRTA22CE E00053EN 20030416003782003041600378EU 2003 4 16 MALA030115 120030108A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C-CHECK INSPECTION IN CVG, FROM DMR NR 8, AFT OF FRAME 34, 7.00 INCHES UP FROM SKIN SPLICE DENT. REQUIRES PERMANENT REPAIR WITHIN 50 CYCLES PER SRM 53-00-00. PERMANENT REPAIR COMPLETED IAW SRM 53-00-12 AND EO A53050. 2H74 4F RTA49EU 20030416003832003041600383NE 2003 4 16 SWIA200311686 220030109A7261 WARNING LIGHT EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT ENGINE ILLUMINATED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07297SW 120327 115073 AT 90 KTS ON TAKEOFF ROLL RECEIVED AN OIL PRESSURE AURAL WARNING. UNABLE TO DETERMINE WHICH ENGINE IT WAS. TAKEOFF WAS ABORTED. OIL PRESSURE WAS IN THE NORMAL RANGE IN BOTH ENGINES. DETERMINED RIGHT ENGINE TO BE THE CAUSE OF OIL LOW PRESSURE WARNING. REPLACED RIGHT ENGINE DUE TO PREVIOUS HISTORY IAW MM 71-00-00. OPS CHECK GOOD. LEAK CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030417000292003041700029NE 2003 4 17 MALA030120 220030122A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FOD A MALAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL15425XJ 340B425 DURING FLIGHT 2741, LT ENGINE FAILED INFLIGHT. LT ENGINE OVERSPEED. A/C DIVERTED TO FOD. MAINTENANCE REMOVED AND REPLACED LT ENGINE P/N CT7-9B SN/ON GE-E785719, SN/OFF GE-E785665 IAW JC 7100-301, REF WORK PACKAGE DATED 1/23/03 FOR DETAILS. 2L72 4T4 TRTA52EU E8NE 20030417000712003041700071SO 2003 4 17 SWIA200311744 120030126A213122201T011400 CONTROLLER EMB 120 EMB120ER 3260203SO CABIN PRESSURE MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07217SW7430 7430 120286 EN ROUTE AT 11500 FT, RECEIVED A 'CABIN ALT' LIGHT ON THE MAP WITH MASTER WARNING AND TRIPLE CHIME. QRH PROCEDURE FOLLOWED, UNABLE TO CONTROL CABIN PRESSURE IN MANUAL MODE. RETURNED TO SBA. REPLACED PRESSURE CONTROLLER. PRESSURIZED AIRCRAFT, OPS CHECK GOOD. 2L72 4T RTA31SO 20030417000832003041700083NM 2003 4 17 UPS03440132 120030202A3350 LIGHT BOEING747 747212B 1384886NM MAIN DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01526UP 21937 EMERGENCY LIGHT MAIN DECK CEILING AFT OF STAIRS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ON MAIN DECK, OPS OK. 2L74 4F A20WE 20030417000842003041700084 2003 4 17 UPS03840131 420030202A256551561007 SLIDE DOUG DC8 DC871F 302199DWP PAX DOOR DEPLOYED A IPXAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: B, WHILE ADJUSTING SIGHT GAUGE ON L1, EVAC-SLIDE INADVERTENTLY DEPLOYED SLIDE. ALL PROCEDURES WHILE ADJUSTING WERE DONE IAW MM 25-60-04. SLIDE WAS PUNCTURED ON CREW ENTRY STAIRS WHILE INFLATING. REMOVED EVAC-SLIDE FROM ACFT. 2L74 4F RT4A25 20030417000932003041700093 2003 4 17 SWIA200311749 420030130A34183995100208 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07432SW674 674 7548 ON CLIMBOUT OF SLC AT ABOUT 700 FT AGL RECEIVED A STALL FAIL AMBER MESSAGE. PERFORMED QRH ITEMS AND RETURNED TO SLC FOR NORMAL LANDING. REMOVED AND REPLACED STALL PROTECTION UNIT. OPS CHECK GOOD IAW 27-35-01. 2L72 4F RTA21EA 20030417001102003041700110EU 2003 4 17 MALA030141 120030118A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 DURING C-CHECK IN CVG, NR 1 SEAT TRACK SHOWS CORROSION BETWEEN FRAME 18 AND 20A. MAINTENANCE REPAIRED DAMAGE IAW EO A53026. A/C RELEASE DATE 1/30/03. 2H74 4F RTA49EU 20030417001152003041700115NM 2003 4 17 QXEA0300231 120030204A3080 CIRCUIT BREAKER BOMBDRDHC8 DHC8401 1390041NM PROP DEICE TRIPPED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09403QX 4037 SEA-ON FLIGHT NUMBER 2349, PROP DEICE CAUTION LIGHT AS PER CHECKLIST TURNED OFF THEN ON, CAUTION LIGHT WENT AWAY BUT RIGHT HAND PROP DEICE INOPERATIVE. NO GREEN LIGHT, NO ELECTRIC LOAD. NO RIGHT HAND PROP HEATER BOOT BURN THRU'S. FUNCTIONAL CHECK OF PROP DEICE SYSTEM FAIL. NR 2 PROP PULLED/RESET NR 2 PROP DEICE CIRCUIT BREAKER. PROP DEICE SYSTEM FUNCTIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417001262003041700126NM 2003 4 17 QXEA0300242 120030207A3260301450201 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 BROKEN A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09409QX2843 4051 PDX - FLIGHT 353 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE RIGHT MAIN GEAR SHOWED UNSAFE AND THE LIGHT IN HANDLE STAYED ON WHEN THE GEAR WAS RETRACTED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT GEAR DOOR CLOSED PROXIMITY SENSOR AND ADJUSTED THE LEFT DOOR CLOSED PROXIMITY SENSOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417001302003041700130NM 2003 4 17 UPS03440144 120030208A3350S135610A BATTERY PACK BOEING747 747123 1384873NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01676UP 20101 MAIN DECK AT STA 390 AND DOOR SILL FOR L1 EMERGENCY LIGHT DIMMED. REMOVED AND REPLACED EMERGENCY BATTERY, OPS CHECK OK. 2L74 4F A20WE 20030417001492003041700149 2003 4 17 SWIA200311760 420030206A3425 INDICATOR EMB 120 EMB120ER 3260203SO HSI FAILED A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07188SW 120039 CAPTAIN'S HSI FAILURE AFTER TAKEOFF, WENT VERY DIM, THEN BLACK. A MINUTE OR SO LATER IT CAME SLOWLY ON THEN IT WENT SLOWLY BLACK AGAIN. NO FLAGS. REPLACED RELAYS K0395 AND K0397. NR 1 EHSI OPS CHECK GOOD IAW MM 34-22-00. AUX GEN 1 AND 2 OPS CHECK GOOD IAW MM 24-31-00. RELAYS REPLACED IAW MM 24-52-04. P/N OFF: M83536/33-003L. 2L72 4T RTA31SO 20030417001502003041700150 2003 4 17 SWIA200311761 420030204A22166225734002 CONTROL SERVO EMB 120 EMB120ER 3260203SO TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07294SW7031 7031 120321 DURING PREFLIGHT TRIM WHEEL STIFF AND HARD TO MOVE, FELT SLIGHT BINDING WHEN MOVING THROUGH ZERO MARK. ALSO, WHEEL SNAPS BACK 1/2 UNIT AFTER RELEASE (IN MANUAL OR ELECTRIC) WHEN SET. REPLACED ELECTRIC TRIM CONTROL SERVO. TRIM WHEEL HAS FULL MOVEMENT WITHOUT BINDING OR BACK PRESSURE. OPS CHECK GOOD. 2L72 4T RTA31SO 20030417001522003041700152EA 2003 4 17 SWIA200311764 120030201A2752853D10018 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07413SW2615 2615 7102 FLAPS FAIL MESSAGE. FLAPS WOULD NOT MOVE FROM 5 DEGREES POSITION. REMOVED AND REPLACED RIGHT OUTBOARD FLAP INBOARD ACTUATOR IAW CRJ MM 27-53-05. RIGGED FLAPS AND OPS CHECK GOOD. 2L72 4F RTA21EA 20030417001572003041700157EU 2003 4 17 MALA030147 120030209A26207239360501 RESISTOR SAAB SF340 340B 7860101EU DETECTION SYS FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15360PX 340B220 DURING COMPLETION OF TASK CARD 262102, ON LT SIDE AFT CARTRIGES HAS NO POWER TO IT. MAINTENANCE FOUND RESISTOR BOX AT FAULT P/N 7239360-501. MAINTENANCE REMOVED AND REPLACED RESISTOR BOX IAW SAAB AMM 26-21-15. 2L72 4T RTA52EU 20030414000782003041400078NM 2003 4 14 AUS20030268 120030208A5753 FLAP TRACK BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE TE FLAPS CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT OUTBOARD FLAP OUTBOARD TRACK FORWARD ATTACHMENT FITTINGCONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTION IAW CPCP C57-581-06. 2L73 4F4 FRTA3WE E2EA 20030414000812003041400081NM 2003 4 14 AUS20030281 120030212A5311 INTERCOSTAL BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INTERCOSTAL LOCATED IN FORWARD CARGO AREA BETWEEN FRAME BS 580 AND FRAME BS 600 AT STRINGER 28 RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030414000932003041400093CE 2003 4 14 CA030227003 120030226A3233508202085 ACTUATOR BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA MLG DAMAGED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING A SPECIAL INSPECTION, PART OF A FLEET INSPECTION OF ALL LANDING GEAR ACTUATORS . THE LANDING GEAR WAS TESTED DURING THE TEST THE NOSE GEAR ACTUATOR WAS SQUEAKING DURING THE EXTENSION CYCLE. THEACTUATOR WAS REMOVED FROM THE AIRCRAFT. WITH FURTHER INSPECTION WE FOUND THAT THE ACTUATOR MAKES AGRINDING SOUND WHEN TURN BY HAND AND THE NUT MOVES SMOOTHLY FOR 3/4 OF A TURN, THEN TAKES A SMALL STEP BACK BEFORE CONTINUING TO MOVE SMOOTHLY. THIS ACTUATOR ONLY HAD 811 CYCLES SINCE OVERHAUL WITH ANORMAL TBO OF 7500 CYCLES.THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1L72 3T4 T A14CE E4EA 20030408000112003040800011WP 2003 4 8 ASAA0380085 120030114A52505936715503 SKIN DOUG DC9 DC983 3022083WP BARRIER DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, FORWARD CARGO BAY BARRIER DOOR SKIN CRACKED. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20030408000162003040800016WP 2003 4 8 ASAA0380103 120030123A53205936844 PANEL DOUG DC9 DC982 3022082WP MLG WW CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OAK - FOUND DURING C-CHECK, MLG WHEELWELL CUTOUT OUTBOARD AFT PANEL IS CHAFED BEYOND LIMITS. INSTALLED 7075-T6 DOUBLER PER SRM 57-01. (M) 2L72 4F A6WE 20030408000212003040800021WP 2003 4 8 ASAA0380110 120030125A5230591014155 RETAINER DOUG DC9 DC982 3022082WP DOOR SEAL CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OAK - DURING C-CHECK, AFT CARGO DOOR FORWARD SEAL RETAINER AT CAM IS CRACKED. FABRICATED AND REPLACED RETAINER PER SRM 51-30-5, 51-10-2, AND 51-10-3. (M) 2L72 4F A6WE 20030408000312003040800031EA 2003 4 8 SIMA200302901 120030128A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21501BG 10017 DFW - FLIGHT 3863 - DURING CREW PREFLIGHT, THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED TWO EMERGENCY LIGHT BATTERY PACKS (S/N'S 73658/79838) IAW CRJ MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030408000442003040800044NM 2003 4 8 USAABB03021 120030213A3350 BATTERY BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19612AU 27124 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 ILLUMINATED. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030408000992003040800099NM 2003 4 8 2003UALA00352 120030403A2121 FAN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN FAILED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29658UA 27113 CREW REPORTED ELECTRICAL SMELL/SMOKE IN AIRCRAFT. THE RT RECIRCULATION FAN FAILED. THE FAN WAS REPLACED. THE SHAFT BEARINGS FAILED. 2L72 4F4 FRTA1NM E24NE 20030408001182003040800118NM 2003 4 8 373PA0010 120030326A335086210144 BATTERY BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 L1,L2,L3,& L4 DOORS FLOOR EXIT LIGHTS (SIGNS) INOPERATIVE. REMOVED AND REPLACED L1,L2,L3, & L4 DOOR EMERGENCY EXIT IDENTIFIER LIGHT BATTERIES. OPS CHECKED OK. 2L72 4F4 FRTA16WE E2GL 20030408001192003040800119NM 2003 4 8 373PA0011 120030406A335086210066 BATTERY PACK BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 EMERGENCY EXIT LIGHTS NOT WORKING ROWS 1,16,26. REMOVED AND REPLACED BATTERY PACKS IAW MM 33-51-51. OPS CHECK GOOD IAW MAINTENANCE ALERT NR 7. 2L72 4F4 FRTA16WE E2GL 20030625001312003062500131NM 2003 6 25 03FDEA00398 120030304A5753ARC050311 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING O/B FLAP O/B HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLES 2EA CORRODED.O/B HINGE. LEFT O/B FLAP- O/B HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORROSION HOLES REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1- 5740-68587. 2L73 4F RTA22WE 20030409000062003040900006NM 2003 4 9 AWXA200300349 120030312A575465C26602218 SKIN BOEING737 7373S3 1384711NM NR 5 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK THE NR 5 LEADING EDGE SLAT UPPER SURFACE WAS FOUND DELAMINATED AT THE CENTER, INBOARD & OUTBOARD CORNERS. MAINTENANCE REMOVED THE NR 5 LEADING EDGE SLAT; PERFORMED COMPOSITE REPAIR OF THE CENTER, INBOARD & OUTBOARD CORNERS PER B737-300 SRM 51-70-10, FIG. 32, REPAIR 23; INSTALLED SLAT AND RIGGED SYSTEM IAW BMM 27-81-21, PG. 414-419. 2L72 4F RTA16WE 20030410000612003041000061WP 2003 4 10 GTIA030097 120030204A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FORWARD CABIN WEB STATION 220-240 CORRODED. FABRICATED NEW WEB. (M) 2L72 4F A6WE 20030410001282003041000128SO 2003 4 10 SIMA200304806 120030211A532014521725615 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS AROUND THE NUTPLATES. CUT OUT CORRODED AREAS THAT WREE BELOW .040 INCH, OTHER CORRODED AREAS WERE BLENDED. FABRICATED A FORWARD UPPER NUTPLTAE DOUBLER AND LOWER NUT PLATE AND DOUBLER FOR MID AND AFT NUTPLATE. REPAIR DONE IAW EMB IC2003-145/0496 DATED FEB 7, 2003 AND EMB SRM (SRM EMB-145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-40-04, 51-40-06 AND 53-21-02. (M) 2L72 4F RTT00011AT 20030410001292003041000129SO 2003 4 10 SIMA200304807 120030127A532014525480003 SILL EMB 145 EMB145LR 3260212SO CARGO DOORWAY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 ABI - DURING AN IMBV INSPECTION, THE CARGO OPENING LOWER CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CARGO LOWER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-20-01, 51-20-03, 51-40-02, 51-40-04, 51-20-06, AND THE EMB 145 CORROSION PREVENTION MANUAL CHAPTER 51-21-04 ANF 51-21-05. (M) 2L72 4T RTT00011AT 20030410001802003041000180CE 2003 4 10 ESE2003F00000 120030226A304057033 BLOWER CESSNA500 550 2076604CE DEFOGGER FAILED E ESEAIG CABIN DEPRESSURIZATION O2 MASK DEPLOYED BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO11117TA2599 5500464 DECENDING, AFTER A 3 HOUR FLIGHT, THE CREW SMELLED FUMES WHILE PASSING THROUGH 8,000 FEET. FUMES WERE ALSO EXHAUST TYPE FUMES. THE CREW TURNED TEMPERATURE CONTROL TO FULL COLD. THE SMELL DISAPPEARED. LEVEL AT 4,000 FEET ON DOWNWIND LEG , THE CREW SELECTED INCREASED HEAT ON TEMP CONTROLLER. THE FUMES RETURNED AFTER A VERY SHORT PERIOD OF TIME AND THE COCKPIT STARTED FILLING WITH SMOKE. THE CREW DONNED O2 MASKS, DROPED PAX O2 MASKS AND DUMPED PRESSURIZATION. AFTER TURNING TEMPERATURE CONTROL TO FULL COLD, THE COCKPIT REMAINED CLEAR OF ANY FRESH SMOKE. 1L72 4F A22CE 20030410002072003041000207WP 2003 4 10 GTIA030155 120030223A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 48087 INTERCOASTAL STA 1346 RBL 18 HAS CORROSION UPPER AND LOWER SURFACE, IN RIGHT AFT LAV AREA. FABRICATED REPAIR DOUBLER 1 EA AND FILLER 1 EA. INSTALLED REPAIR. 2L72 4F4 F A6WE E2EA 20030410002192003041000219WP 2003 4 10 GTIA030162 120030310A5320 SCREW DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE LT FWD WINDOW MISSING A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23812NK 48021 LEFT FORWARD OVERWING EMERGENCY EXIT WINDOW IS STUCK CLOSED. FORWARD SCREW ON EXIT COVER MISSING THUS JAMMING DOOR CLOSED. INSTALLED SCREW ON COVER, DOOR NOW FUNCTIONS PROPERLY. 2L72 4F4 F A6WE E2EA 20030410002202003041000220 2003 4 10 GTIA030163 420030317A2565D29982113 SLIDE DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE CABIN DISLODGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 48087 RIGHT 1 SLIDE PACK CAME OFF WHEN DOOR WAS OPENED AND LOCKED BACK DIFFICULT TO LOCK BACK. INSTALLED NEW SLIDE PACK RT 1 DOOR. NO OTHER DEFECTS NOTED. DOOR OPEN LATCH OPS CHECK GOOD. 2L72 4F4 F A6WE E2EA 20030411000012003041100001EU 2003 4 11 BAQA084691 120030224A6220 BEARING BOLKMS117 BK117A1 5626010EU PITCH LINK INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME272 20002006 7243 PITCH LINK HAS BEARINGS WORN. EXCESSIVE PLAY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030414000662003041400066 2003 4 14 BAQA085820 420030325A34163A433220F281CL INDICATOR UROCOPEC135 EC135T1 5620026EU ALTIMETER OUT OF TOLERANCEE BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01136MH1636 0161 ALTIMETER FAILED CALIBRATION AND FRICTION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030415000282003041500028WP 2003 4 15 CA030318003 220030304A7261 SHAFT CESSNA441 441 2076020CE GARRTTTPE331TPE33110 01514WP HARTZLHCE4N HCE4N3 NE SCAVENGE PUMP SEIZED W O OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) SCAVENGE PUMP MALFUNCTIONED DUE TO SEIZER OF THE ROTOR DRIVE SHAFT IN THE BUSHING OF THE HOUSING. HONEYWELL SERVICE BULLETIN TPE331-72-2074 REV.1 ADDRESSES THIS PROBLEM BY PUMP REPLACEMENT WITH P/N 3108282-1 AND RECOMMENDS COMPLIANCE AT ENGINE OVERHAUL OR IF THE PUMP REQUIRES REPLACEMENT. THIS SERVICE BULLETIN WAS COMPLETED AT THIS SHOP VISIT AND SHOULD PROVIDE A SUSTANTIAL IMPROVEMENT TO RELIABILITY. 1L72 3T4 TRTA28CE E4WE 5 CP10NE 20030415000682003041500068EU 2003 4 15 CA030327004 120030321A63204638302023 BEARING BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL M/R GEARGOX SPALLED W O OTHER J WARNING INDICATION LDLANDING 1 CA 1120 (CAN) RT INPUT SPLIT INNER RACE BALL BEARING PEELING/SPALLING.VOLUME OF METAL CONTAMINATION CAUSED COLLATERAL DAMAGE TO ALL OTHER INTERNAL BEARINGS AND COMPONENTS. 1G72 3U3 U H3EU E4CE 20030415000712003041500071NM 2003 4 15 CA030327007 120030327A278140174 SWITCH BOEING727 72725C 138400HNM PWA JT8 JT8D7B 52053NE LE FLAPS FAILED W JA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) AFTER TAKE OFF FROM FLAPS SELECTED FROM 5 DEGREES TO 2 DEGRESS, AMBER LEADING EDGE LIGHT ILLUMINATED ON FWD PANEL. MAIN LEADING EDGE PANEL INDICATED NR 5 LE FLAP OUT. FUEL WAS DUMPED AND AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE FOUND THE LEADING EDGE DEVICE TO BE OPERATING NORMAL WITH FALSE INDICATION ONLY. LEADING EDGE DEVICE INDICATION SWITCH WAS REPLACED. SYSTEM CHECKED SERVICABLE. 2L73 4F4 F A3WE E2EA 20030415000762003041500076 2003 4 15 CA030328002 420030326A34608220867008 DISPLAY CNDAIRCL604 CL604 1900301EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) ON AIRCRAFT POWER UP CDU NR 3 SHOWED A BLACK SCREEN. THE MAINTENANCE DIAGNOSTIC COMPUTOR (MDC) LINE REPLACEABLE UNIT (LRU) STATUS INDICATED CODE: CDU 3 FAILED - NO CDU-2OUT. MDC LRU DIAGNOSTICS INDICATED CODE: CDU 3 354 - FAILED. NEW CDU INSTALLED AND SYSTEM FUNCTION CHECKED NORMALLY. 2L72 4F4 FRTA21EA E15NE 20030410000212003041000021WP 2003 4 10 GTIA030080 120030219A7120 ISOLATION MOUNT DOUG DC9 DC982 3022082WP ENGINE OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DTW - FORWARD LOWER ISOLATOR MOUNTS ALIGNMENT MARKS SHIFTED. REMOVED AND REPLACED LOWER VIBRATION ISOLATOR MOUNT. (M) 2L72 4F A6WE 20030410000262003041000026NM 2003 4 10 SWAA030603 120030316A5315BACB30FM6A FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772.5, LBL 3, LBL 17.24, RBL 3 & RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030410000442003041000044NM 2003 4 10 SWAA030632 120030319A33506104781 BATTERY BOEING737 7372T4 1384492NM CARGO BAY DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030410000532003041000053NM 2003 4 10 SWAA030638 120030319A5311963820 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, WL 208. REMOVED AND REPLACED LT CHORD PER SRM. 2L72 4F RTA16WE 20030408000972003040800097 2003 4 8 2003UALA00348 420030328A2210 DAMPER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 YAW LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29422UA 503 LANDED UNDER AMBER ALERT DUE TO A GREEN HYDRAULIC SYSTEM INDICATION AND LOSS OF QUANTITY. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20030408000982003040800098NM 2003 4 8 2003UALA00350 120030329A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 AFT PIT STA 1241, RBL 7, FRAME T-CAP IS CORRODED MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH SPLICE SECTION. 2L72 4F4 FRTA1NM E24NE 20030408001032003040800103EA 2003 4 8 03097658 120030407A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27658BR 7500 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CENTER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030408001172003040800117NM 2003 4 8 373PA0009 120030305A335086210066 BATTERY BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHTINOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 EMERGENCY LIGHT INOPERATIVE AT SEAT 21D. REPLACED BATTERY. 2L72 4F4 FRTA16WE E2GL 20030408001212003040800121NM 2003 4 8 377PA0013 120030403A335058782 LIGHT BOEING737 7373L9 1384470NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05377PA 23718 EMERGENCY FLOOR LIGHTING INOPERATIVE, ROW 20 AFT. REPLACED ROW 17-29 LIGHT STRIP IAW MM 25-60-01. OPS CHECK OK. 2L72 4F4 FRTA16WE E2GL 20030410000422003041000042 2003 4 10 SWAA030631 420030319A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030410000472003041000047NM 2003 4 10 SWAA030634 120030320A52306547952 SKIN BOEING737 7372T4 1384492NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT SIDE OF HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030410001842003041000184NM 2003 4 10 DHL2003741512 120030327A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, BS 440 FRAME DENTED LT ABOVE FLOOR LEVEL. REMOVED FASTENERS BS 440 FRAME LT ABOVE FLOOR LEVEL IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-10-4 FIG 2. INSTALL DOUBLER REPAIR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030410002032003041000203WP 2003 4 10 GTIA030153 120030312A5340 BRACKET DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 MAIN CABIN UNDER FLOOR STA 864 LT FLOORBEAM TO FUSELAGE ATTACH BRACKET CRACKED. REMOVED CRACKED BRACKET. LOCATED AND DRILLED NEW BRACKET. INSTALLED BRACKET. 2L72 4F4 FRTA6WE E2EA 20030410002352003041000235EU 2003 4 10 BAQA085825 120030327A5330L633M2010103A003MOUNT UROCOPEC135 EC135T1 5620026EU TRANSMISSION LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03511ME 0143 AIRCRAFT VIBRATION AND MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030410002432003041000243NM 2003 4 10 DL76L030153 120030213A3260 PSEU BOEING767 767332 1382001NM E/E BAY MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27174DN 24802 AFTER TAKEOFF AND GEAR RETRACTION AND PLACING THE GEAR HANDLE TO THE OFF POSITION, GOT SEVERAL MESSAGES. DID NOT PLACE HANDLE TO THE UP POSITION. RETURNED TO JFK DUE TO MSG OF TAIL SKID. MTC IN PROGRESS. PERFORMED T/S FOR LANDING GEAR HANDLE INTLK PER FIM 32-30-00. ALL FIM STEPS CHECK OK. REPLACED PROX SWITCH ELEX UNIT PER MM. PERFORMED VERIFICATION TEST FLT. LANDING GEAR RET AND AIR GROUND SENSOR INFLT CHECK OK. 2L72 4F RTA1NM 20030411000092003041100009NM 2003 4 11 SWAA030748 120030405A53306545767 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 1010 AT STR 4L & BETWEEN BS 354 TO BS 360 AT STR 4L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030414000422003041400042GL 2003 4 14 CA030312016 220030212A72506829641 BEARING ALLSN HUGHES500N 500N 3027374SW ALLSN 250C 250C20R2 GL NR 5 MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 15913 (CAN) DURING A FLIGHT THE ENGINE CHIP LIGHT ILLUMINATED, THE PILOT LANDED AND THE LOWER CHIP PLUG WAS INSPECTED AND HAD SHINY PARTICLES ON IT. THE AIRCRAFT WAS GROUND RUN FOR 15 MINUTES AND SENT BACK FLYING. THE NEXT DAY HE FLEW FOR 1 HOUR AND HAD ANOTHER CHIP LIGHT. THE UPPER AND LOWER CHIP PLUGS WERE INSPECTED AND HAD METAL PARTICLES ON BOTH. THE AIRCRAFT WAS GROUNDED. THE ENGINE WAS REMOVED AND REPLACED BY A SERVICEABLE ENGINE. THE ENGINE WAS INSPECTED FOR DAMAGE. TURBINE BEARING NO 5 HAD THE OUTERRACE AND BALLS PITTED. NO 5 BEARING REPLACED. TURBINE IS SCHEDULED TO BE REINSTALLED ON MARCH 16,2003 1G71 3U3 UNCH3WE E4CE 20030415000122003041500012SW 2003 4 15 CA030220002 120030128A6320205040246003 BEARING RACE BELL BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE M/R GEARBOX SPALLED W O OTHER O OTHER NRNOT REPORTED 1 CA ADW50227 (CAN) A WEEK PREVIOUS, THE BELL 212 HAD A CHIP LIGHT ON THE M/R TRANSMISSION. THE CHIP PLUGS WERE PULLED AND THE ENGINEER FOUND FINE FUZZ AND SLIVERS, INSIGNIFICANT TO WARRANT FURTHER INVESTIGATION BUT TO MONITOR. NEXT WEEK THE PILOT REPORTED THAT THE CHIP LIGHT WAS FLICKERING. THE HELICOPTER LANDED BACK AT THE HANGAR AND THE ENGINEERS INVESTIGATED THE CHIP LIGHT AND FOUND MORE ACCUMULATION THAN BEFORE.THE FILTER WAS PULLED AND THEY FOUND SIGNIFICANT AMOUNT OF FERROUS METAL. THE M/R TRANSMISSION WASPULLED AND SENT TO THE OVERHAUL SHOP. ON DISASSEMBLY AND INSPECTION THEY FOUND THAT THE INPUT TRI PLEXBEARINGS HAD SPALLED. 1G71 4U4 U H4SW E22EA 20030415000842003041500084EA 2003 4 15 CA030330001 120030327A2897MS141543 CIRCUIT BREAKER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ELECTRICAL SHORTED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) IN CRUISE, THE FLIGHT CREW REPORTED A CROSSFLOW PUMP CAUTION MESSAGE ALONG WITH AUTO CROSSFLOW INHIBIT STATUS MESSAGE. SHORTLY AFTER, THE FUEL IMBALANCE CAUTION MESSAGE APPEARED. A 500 KG IMBALANCE DEVELOPED. THE TANKS READOUT WAS LT 2300, CTR 0, RT 1800.THE FLT CREW DECIDED TO DIVERT THE FLIGHT AND LANDED WITHOUT ANY INCIDENT. MAINTENANCE CONFIRMED THE CROSSFLOW PUMP WAS INOPERATIVE DUE TO A DEFECTIVE CIRCUIT BREAKER. 2L72 4F4 FRTA21EA EOOO63EN 20030410001082003041000108 2003 4 10 SWAA030680 420030325A2565D31354 SLIDE BOEING737 7372H4 138448CNM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F A16WE 20030410001342003041000134SO 2003 4 10 SIMA200304810 120030211A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21639AE 145182 ABI - DURING A IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-20-01, 51-40-02, 51-40-04, 51-40-06 AND EMB 145 CPM 51-21-04 AND 51-21-05. (M) 2L72 4T RTT00011AT 20030410001352003041000135 2003 4 10 SWAA030689 420030327A256522D22901151 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F A16WE 20030410001782003041000178NM 2003 4 10 DHL2003741510 120030326A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, BS 800 AND 824 LT BL 45 SEAT TRACK EARS ARE WORN WITH GOUGES. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW B-727 SRM 51-30-2 AT BS 760 TO 848 LT BL 45. 2L73 4F RTA3WE 20030411000182003041100018NM 2003 4 11 SWAA030757 120030405A27316545166 ROD END BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C1 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB ROD ENDS ON OUTBOARD ROD PER MM. 2L72 4F RTA16WE 20030414000322003041400032NM 2003 4 14 MEX2003079 120030318A28222006286F PUMP BOEING767 767300 1385204NM FUEL SYSTEM DAMAGED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23XAAPB 27618 DURING FUEL PUMP INSTALLATION TEST, THE HOUSING, IMPELLER, SHAFT AND ROTOR ASSEMBLY, STATOR CORE, BEARING THRUST AND WASHER THRUST WERE DISPLACED APPROXIMATELY .1250 INCH, PROMOTING DAMAGES INTO THE AIRCRAFT FUEL TANK VOLUTE AND BRAKING ONE OF THE THREE COMPONENT FLANGES. ADDITIONALLY THE HANDLE PUMP AND PLUNGER SPRING ARE INOPERATIVE. 2L72 4F RTA1NM 20030414000502003041400050EA 2003 4 14 CA030313001 120030227A5610NP13932110 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT FAILED W D RETURN TO BLOCK D INFLIGHT SEPARATION TXTAXI/GRND HDL 1 CA (CAN) RT WINDSHIELD SHATTERED ON TAXI OUT AT CINCINNATI. REMOVED P/N NP139321-10, S/N 02074H1855 (781.7 HOURS AND 576 CYCLES)INSTALLED S/N 99014H6982(SEE ALSO: US NR 2003030500013) 2L72 4F4 FRTA21EA EOOO63EN 20030414000672003041400067NM 2003 4 14 AUS20030237 120030228A57146959273 STIFFENER BOEING737 737377 NM CENTER WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING CENTER SECTION SUPPORT BEAM STIFFENER CONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTION IAW J3-CA53-0129. 2L72 4F RTA16WE 20030414000882003041400088EU 2003 4 14 CA030312004 120030306A3250200143255 TOGGLE BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU NLG STEERING BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE AIRCRAFT WAS TOWED OUT OF THE HANGER, TOWING PROCEDURES BEING FOLLOWED PROPERLY. THE NOSE WHEEL LOWER STEERING TOGGLE LOCATED ON THE TOP OF THE NOSE UNDER CARRIAGE WAS FOUND WITH THE BOLT ATTACH EAR BROKEN OFF. IT IS SUSPECTED TO HAVE BEEN CRACKED PREVIOUSLY, AS THERE IS NO EXCESS PRESSURE APPLIED TO THESE TOGGLES WHILE TOWING. THE TOGGLE ASSEMBLIES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 3T4 T A24EU A196 20030415000172003041500017NE 2003 4 15 CA030313007 220030311A7250 ENGINE BOEING737 737281 138448PNM PWA JT8 JT8D17 52049NE NR 1 FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA 34101 (CAN) FLIGHT 41, NR 1 ENG FAILURE ON CLIMBOUT SHORTLY AFTER TAKEOFF THROUGH 3200 FT ASL, CREW HEARD A BANG FROM NR 1 ENG AFTER CLIMB THRUST WAS SET & FLAPS HAD RETRACTED. CREW IDENTIFIED PROBLEM AS NR 1 ENG NOT PRODUCING THRUST & THE 'EGT' WAS PEGGED HIGH OFF GAUGE. NR 1 ENG WAS SHUTDOWN & MAX CONTINUOUS THRUST SET ON NR 2. FIRE BOTTLES NOT DISCHARGED. NO INDICATION OF FIRE OR HIGH TEMPERATURES AFTER ENGINE WAS SHUTDOWN. CREW DECLARED AN EMERGENCY & RETURNED TO YLW. A/C LANDED WITHOUT INCIDENT. INSPECTION REVEALED NR 1 ENG TURBINE BLADES MELTED DOWN TO APPROX 3 INCH STUBS. MAINTENANCE REPLACED NR 1 ENG. ENG GROUND RUNS & SYS CHECK COMPLETED. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS. 2L72 4F4 F A16WE E2EA 20030414000842003041400084WP 2003 4 14 CA030304001 120030303A3230 LANDING GEAR LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE MAINS MALFUNCTIONED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) AFTER GEAR SELECTED DOWN , THE INTRANSIT LIGHT WAS ON, ALL OTHER GEARS AND DOORS LIGHT WERE OFF. GEARS DID NOT EXTEND. ALTERNATE GEAR EXTENSION PROCEDURE PERFORMED AND GEARS EXTENDED NORMALY. TROUBLE SHOOTING UNDERWAY. 2L73 4F4 F A23WE E12EU 20030416000312003041600031WP 2003 4 16 GTIA030137 120030308A7120K22199SA31 ISOLATION MOUNT DOUG DC9 DC981 3022081WP PWA JT8 JT8D NE NR 1 ENGINE SLIPPED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23810NK 48015 NR 1 ENG. LOWER/ FORWARD ENGINE ISOLATOR SLIPPED AT.2500 INCH. CHANGED. REMOVED AND REPLACED NR 1 ENGINE LOWER/ FORWARD. (PRECAUTIONARY) ENG ISOLATOR. 2L72 4F4 F A6WE E2EA 20030416000642003041600064WP 2003 4 16 MWEA030175 120030414A2730 SWITCH DOUG DC9 DC915 3022036WP ELE ANNUNCIATOR OUT OF ADJUST A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31300ME 45718 ELEVATOR POWER ON ANNUNCIATOR DOES NOT ILLUMINATE ON ELEVATOR POWER CHECK. INSPECTED SWITCH AND PERFORMED ADJUSTMENT TEST. NO DEFECTS NOTED, TEST GOOD. 2L72 4F A6WE 20030416000802003041600080SO 2003 4 16 C2XA03SH106 120030413A531014525422001 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 DURING C-CHECK, THE LT HAND SILL BETWEEN FRAMES 60 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030416001022003041600102NM 2003 4 16 QXEA0300449 120030410A2620 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DIRTY A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09413QX 4060 BOI- ON FLIGHT 2367 RECEIVED A INTERMITTENT APU BOTTLE LOW LIGHT WITH CHECK FIRE DETECTION MASTER WARNING. CLEANED CONNECTOR TO FIRE BOTTLE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030415000852003041500085EA 2003 4 15 CA030331002 220030331A8550CH48110 OIL FILTER PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA ENGINE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) NEW FILTER INSTALLED ON ABOVE AIRCRAFT HAD SEVERE OIL LEAK. LEAK BELIEVED TO BE COMING FROM ROLLED SEAM AT BASE OF FILTER. FILTER REMOVED AND NEW FILTER INSTALLED AND TESTED. 1L71 3O3 O 2A13 E274 20030409000242003040900024NM 2003 4 9 MEX2003045 120030226A2497 WIRE DOUG MD80 MD83 3023681NM GCU, BCU BROKEN W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23E1BTX 49660 AIRCRAFT RETURNED TO PLATFORM DURING PUSH BACK, CAPTAIN REPORTED THAT APU WAS ELECTRICITY OUT OF SERVICE DURING RT ENGINE STARTING. CROSS FEED TEST WAS ACCOMPLISHED WITH NEGATIVE RESULTS. AIRPLANE WAS SENT TO A REMOTE POSITION FOR ITS ATTENTION. THERE, REPLACED GCU AND BCU CONTINUING SAME CONDITION WIRING WAS CHECKED, DETECTING FREAK B1-686 DAMAGED, IT WAS REPLACED IAW MM, TESTS CORRECT. 2L72 4F RT 20030410000202003041000020WP 2003 4 10 GTIA030079 120030219A7120K22199SA31 ISOLATION MOUNT DOUG DC9 DC982 3022082WP ENGINE OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DTW - FOUND FORWARD UPPER ISOLATOR MOUNT ALIGNMENT MARKS SHIFTED. REMOVED AND REPLACED FORWARD UPPER VIBRATION ISOLATOR MOUNT. (M) 2L72 4F A6WE 20030410000342003041000034WP 2003 4 10 GTIA030087 120030210A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FS 200 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FLOOR SUPPORT STATION 200 RBL 9-44 HAS CORROSION. FABRICATED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030410001382003041000138NM 2003 4 10 SWAA030692 120030327A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 908, STR 4R AND STR 10R. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030410001452003041000145NM 2003 4 10 SWAA030699 120030327A2121215201 GASPER FAN BOEING737 7372H4 138448CNM A/C BAY FAULTY A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29090SW 22905 BAD ODOR IN CABIN AND COCKPIT. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F A16WE 20030410001542003041000154NM 2003 4 10 SWAA030708 120030329A57536546430 SKIN BOEING737 7373H4 1384600NM T/E FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C2 CHECK, FOUND LT INBD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LEFT INBD FOREFLAP PER MM. 2L72 4F RTA16WE 20030410001612003041000161NM 2003 4 10 SWAA030715 120030328A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 727E, STR 10R AND STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410001852003041000185SO 2003 4 10 FK62003F00000 120030311A274162701160 CONTROL CABLE PIPER PA44 PA44180 7104402SO TRIM BROKEN B FK6RO OTHER O OTHER NRNOT REPORTED 1 NM09287215352 447995296 AIRCRAFT WAS TRIMMED FOR NOSE HIGH ATTITUDE FOR SLOW FLIGHT TRAINING. PILOT ATTEMPTED TO TRIM NOSE DOWN, WHEN HE NOTICED LOOSE CABLE ACCUMULATING AROUND TRIM WHEEL AND NO REDUCTION OF FORWARD PRESSURE ON CONTROL WHEEL. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION SHOWED FORWARD TRIM CABLE HAD BROKEN IN THE AREA OF THE ELECTRIC TRIM SERVO CAPSTAN. REASON FOR FAILURE IS UNKNOWN, POSSIBLY AGE RELATED. AIRCRAFT IS 24 YEARS OLD. 1L72 3O A19S0 20030410001962003041000196SO 2003 4 10 GM03013 120030320A311017275095 SWITCH GULSTMGV GULFSTREAMGV3980116SO EMERGENCY BATTERDEFECTIVE E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL235101 2639 1197 550 COCKPIT SYSTEMS DID NOT OPERATE ON EMERGENCY BATTERY. EMERGENCY BATTERY SWITCH, COCKPIT OVERHEAD, FOUND DEFECTIVE. REPLACED EMERGENCY BATTERY SWITCH AND FUNCTIONALLY CHECKED EMERGENCY BATTERY SYSTEM IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA12EA 20030410002112003041000211NE 2003 4 10 DL76G030265 220030321A7321 EEC BOEING767 7673P6 1385105NM GE CF6 CF680C2B6 30025NE NR 2 ENGINE MALFUNCTIONED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO271501P39099 695373 24983 695373 R ENG EEC EICAS MESSAGE ON T/O ROLL. FWD TO MCO AND PLACARD PER MEL 73-21-01A. PIMU MONITOR SHOWS NO FAULTS. T/S PER FIM. RAN ENG, NO FAULTS. OK FOR SERVICE. MCO/PLAC REMOVED. 2L72 4F4 FRTA1NM E13NE 20030414000152003041400015NM 2003 4 14 SWAA030743 120030403A143065C16820 RIVET BOEING737 7373H4 1384600NM GIRT BAR FITTINGLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR HOOK ATTACH RIVET SHEARED. INSTALLED RIVET PER SRM. 2L72 4F RTA16WE 20030414000412003041400041CE 2003 4 14 CA030312014 120030311A5751991300009 SKIN 991300001 BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA AILERON CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA 22426 IJ370 (CAN) .5 INCH CRACK FROM TRIM TAB OPENING OUTBOARD CORNER TO FIRST RIVET. 1L72 3T4 T A14CE E4EA 20030414000582003041400058SW 2003 4 14 HEEA085854 120030327A6420407012101107 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR MISINSTALLED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 BEARINGS INSTALLED OPPOSITE OF WHAT THEY ARE SUPPOSED TO BE. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 3U O H2SW 20030415000252003041500025SW 2003 4 15 CA030317016 120030314A6420204010765001 NUT BELL 204 204B 1181404SW LYC T53 T5311B 41549NE TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON VISUAL INSPECTION NUT WAS FOUND TO BE CRACKED AT WORM GEAR THREAD. THESE PARTS HAVE A 1000 HR NDT INSPECTION. THIS COMPANY INCLUDE A 300 HR VISUAL THIS WAS FOUND DURING THE VISUAL. 1G71 4U4 U H1SW E1EA 20030415000522003041500052SO 2003 4 15 CA030324004 120030317A3221 MOUNT PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO NLG CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) LOWER PORTION OF MOUNT ASSEMBLY TUBULAR STRUCTURE CRACKED, MOUNT MUST BE REMOVED TO FURTHER EVALUATEI.E. STRIP AND NDT INSPECTION BEFORE REPAIR STATUS CAN BE DETERMINED. 1L72 3O3 O A7SO E9CE 20030415000662003041500066EU 2003 4 15 CA030327002 120030324A271031073110 SERVO AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE AILERON FAILED W O OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 CA (CAN) ON CLIMB AT 15,000 SIGNIFICANT CYCLIC VIBRATION FELT AT 315 KTS.PROBLEM REDUCED AT SLOWER SPEED AND WORSE WHEN TURNING. RT AILERON SERVO ACTUATOR REPLACED AS PER AMM. 2L72 4F4 FRTA28NM E29NE 20030415000692003041500069NM 2003 4 15 CA030327005 120030320A2751182993 INDICATOR BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE TE FLAPS MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) DURING CLIMB, FLAPS WERE SELECTED TO THE 2 DEGREE POSITION. THE INBOARD FLAPS STAYED AT 5 DEGREE. AIRCRAFT RETURNED TO YYC AND LANDED WITHOUT INCIDENT. FLAP SYSTEM INSPECTED, LUBRICATED ANDCYCLED WITH SYSTEM OPERATING NORMALLY I.A.W. MM 27-51-0. FLAP INDICATORS WERE SWAPPED FOR TROUBLESHOOTING. NO FURTHER PROBLEM DURING SUBSEQUENT FLIGHT. 2L73 4F4 F A3WE E2EA 20030415000972003041500097SW 2003 4 15 CA030401005 120030327A6320206040532005 CASE BELL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL GEARBOX BROKEN W K NONE O OTHER ININSP/MAINT 1 CA BMC51561 (CAN) GEARBOX RECEIVED FOR 1500 HOUR INSPECTION. TOP CASE REMOVED AND 10 TEETH FROM INVOLUTE SPLINES WERE BROKEN WHICH IS NOT IN ITSELF AN UNUSUAL OCCURRENCE. WHEN A NEW REPLACEMENT WAS OBTAINED FROM BELL THE LOCKWIRE HOLES FOR THE FILLER CAP AND CHIP PLUG HAD NOT BEEN DRILLED. A SECOND CASE WAS ACQUIRED FROM BELL AND IT WAS CORRECTLY DRILLED. 1G71 3U3 U H2SW E1GL 20030415001582003041500158WP 2003 4 15 UPS03839998 120030103A3510 REGULATOR DOUG DC8 DC873F 302199FWP OXYGEN SYS BYPASSING A IPXAO OTHER O OTHER CRCRUISE 1 SO01806UP 46006 2ND OBSERVER O2 REGULATOR BY-PASSING AIR IN FLIGHT, LOST O2 EMERGENCY SYSTEM. FOUND FIRST OBSERVERS SUPPLY LINE TO REGULATOR LEAKING AT FITTING, DAMAGED. THIS FITTING WAS DAMAGED AT TEE FITTING BEHIND 2ND OBSERVERS REGULATOR. REMOVED AND REPLACED SUPPLY HOSE, OPS CHECK GOOD. LEAK CHECK GOOD. 2L74 4F RT4A25 20030416000232003041600023 2003 4 16 SWIA200311682 420030105A22106229968001 DAMPENER CNDAIRCL600 CL6002B19 1900309EA NR 2 YAW MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07412SW8519 8519 7101 ON PUSHBACK YD NR 2 STATUS MESSAGE CAME ON. RESET YAW DAMPER NR 2, MESSAGE REOCCURRED. REPLACED NR 2 YAW DAMPER IAW 22-22-01. OPS CHECK OK. 2L72 4F RTA21EA 20030416001142003041600114NM 2003 4 16 DLM11030250 120030316A25304110001137 COFFEEMAKER DOUG MD11 MD11 3023602NM AFT GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27810DE 48565 ELECTRICAL ODOR BY 4L AND R DOOR NO SMOKE OR OTHER ABNORMAL INDICATIONS. FOUND ODOR SMOKE FROM COFFEEMAKERS. REPLACED SAME. 2L73 4F RTA22WE 20030416001172003041600117NM 2003 4 16 DLM88030255 120030319A3350RPS1 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHTSINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27955DL 49886 FOUND ON LAYOVER, AFT CABIN EMERGENCY AISLE LIGHTS AND SIGNS INCLUDING TAIL COMPARTMENT INOP. REPLACED POWER SUPPLY AND BATTERY R5-212. CHECKS GOOD. 2L72 4F RTA6WE 20030416001182003041600118 2003 4 16 DLM88030259 420030320A22104034241971 PROBE DOUG MD88 MD88 3023688NM TAT FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27947DL 49878 IN FLT CREW REPORTED AUTOPILOT PROBLEM, HAD BOTH DFGCS NOT RESPONDING TO ANY FLT GUIDANCE PANEL IMPUTS AND MSG OF FAIL 26 ON FMAS. THEN REPORTED A LITTLE BURNING ODOR AND DECIDED TO DIVERT TO BHM. REPLACED TOTAL AIR TEMP PROBE. PERFORMED DUCT BURNOUT FOR ODOR. 2L72 4F RTA6WE 20030416001382003041600138WP 2003 4 16 AALA20030007 120030106A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SIDEWALL EMERGENCY LIGHTS IN AFT STAIRWELL INOPERATIVE. RESET FORWARD SIDEWALL EMERGENCY LIGHTS IN AFT STAIRWELL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030416001412003041600141 2003 4 16 SWAA030768 420030404A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 FWD SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030416001492003041600149NM 2003 4 16 AALA20030044 120030111A2910 B-NUT BOEING757 757223 1384957NM HYD SYSTEM LOOSE A AALAK NONE K FLUID LOSS CRCRUISE 1 SW21688AA 25730 MIA - FLT 633 - EN ROUTE SJU-DFW, LEFT HYDRAULIC SYSTEM FLUID LOSS. CAPTAIN DECLARED EMERGENCY AND LANDED AT MIA WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND B-NUT LOOSE ON HYDRAULIC RETURN LINE IN DOGHOUSE AREA FOR NR 1 ENGINE. ACCOMPLISHED RETORQUE OF B-NUT AND SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416001582003041600158NE 2003 4 16 DLM88030297 220030328A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 MALFUNCTIONED A DALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO27927DA35310 49714 718179 ON FINAL AT TIME OF AUTO THROTTLE DISCONNECT JUST PRIOR TO LANDING, A/C VEERED TO LEFT. EXECUTED GO-AROUND, NOTICED SMELL IN COCKPIT. INSPECTED ENGINES AND RAN, UNABLE TO DUPLICATE. 2L72 4F4 FRTA6WE E9NE 20030416001592003041600159NM 2003 4 16 DL777030299 120030328A2530 COFFEEMAKER BOEING777 777232 1385232NM GALLEY SPARKS A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27865DA 29737 COFFEEMAKER AT 205 SPARKING TURNED OFF PWR PULLED C/B. REPLACED COFFEEMAKER. 2L72 4F RTT00001SE 20030416001732003041600173NM 2003 4 16 AALA20030217 120030212A2422 INVERTER BOEING767 767323 1385205NM E/E BAY OVERHEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21366AA 25193 AFW - AT SOME TIME DURING IN SERVICE, APPARENT OVERHEAT OF STATIC INVERTER CAUSE SMOKE AND HEAT DISCOLORATION TO C3-1 RACK AND WIRING. REF E-58 NR 3687296, REMOVED, INSPECTED, REINSTALLED AND 0A5 CK E3-1 RACK. NO APPARENT DAMAGE FOUND JUST DISCOLORATION. (M) 2L72 4F RTA1NM 20030416001842003041600184NE 2003 4 16 UPS03540407 220030403A7230 COMPRESSOR BOEING757 75724APF 1384969NM PWA 2037 PW2040 NE LT ENGINE STALLED A IPXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01418UP 23905 LOUD BANG AND HARD YAW TO LT ON TO AT 700 FT AGL. RETURNED TO DFW. BOROSCOPED N2 HIGH COMPRESSOR, NO DEFECTS NOTED. C/W CHECK 4 SVA INSP, NO DEFECTS NOTED. C/W ENG CK 6 14TH STG BLEED SYS. A/C OKAY FOR SERVICE. 2L72 4F4 FRTA2NM E17NE 20030416001912003041600191NM 2003 4 16 AALA20030264 120030302A3610 CLAMP BOEING757 757223 1384957NM BLEED AIR LOOSE A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21660AM 25294 CCS - FLT 2140 - EN ROUTE CCS-MIA, RIGHT ENGINE FIRE WARNING/OVERHEAT LIGHT ILLUMINATED. RETARDED THROTTLE LIGHT EXTINGUISHED AFTER A FEW MINUTES. ADVANCED THROTTLE AGAIN OVERHEAT LIGHT ILLUMINATED. SHUTDOWN RIGHT ENGINE AS A PRECAUTION, NO OVER TEMPERATURE INDICATIONS THEN NOTED. RETURNED AND LANDED CCS WITHOUT INCIDENT. REPLACED PRECOOLER CLAMP AND THE SENSE LINE BETWEEN THE PRESSURE SHUTOFF VALVE AND THE PRECOOLER ON RIGHT ENGINE. RAN ENGINE AND ALL CHECKS WERE NORMAL. LEAK CHECKED OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030415000732003041500073GL 2003 4 15 CA030327009 120030327A3212C2UF1781A CASE DHAV DHC1 DHC1B2 2801736GL FLOAT BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON INSPECTION, WEIGHT REMOVED FROM NOSE GEAR, GEAR SEPARATED FROM FLOAT 1L71 3O EXPA1L71 20030416000522003041600052EU 2003 4 16 MALA030229 120030405A3230D49410001 CONTROL UNIT SAAB SF340 340B 7860101EU MLG FAILED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15414XJ 340B414 DURING FLIGHT 2723, LT MAIN GEAR LIGHT WOULD NOT ILLUMINATE WHEN GEAR WAS DOWN AND LOCKED. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL UNIT P/N D494-10-001, SN/ON 651/10-97, SN/OFF 046/2-84 IAW AMM 32-31-05-2. FOUND LT GEAR LIGHT RECXP, DAMAGED INSIDE. PERFORMED GEAR SWING, OPS CHECK GOOD. 2L72 4T RTA52EU 20030416000712003041600071WP 2003 4 16 ABXA030130 120030403A304013391 CONTROLLER DOUG DC8 DC861 3021952WP WINDSHIELD TEMP DEFECTIVE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23849AX3876 45891 WINDSHIELD HEAT, SPARKS CAME FROM FORWARD RIGHT WINDSHIELD. SPARKS WERE COMING FROM LOWER RIGHT. CIRCUIT BREAKERS WERE PULLED. REPLACED RIGHT WINDSHIELD TEMP. CONTROL DUE TO WINDOW REPLACEMENT IAW DC-8 AMM 30-41-0-1-2-0001. OPS CHECKED GOOD. REPLACED RIGHT WINDSHIELD HEAT TRANSFORMER IAW DC-8 AMM 30-41-02-2-0001. 2L74 4F 4A25 20030416000902003041600090NM 2003 4 16 SWAA030778 120030407A27506563851 MOTOR BOEING737 7373H4 1384600NM FLAP DRIVE FAILED A SWAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW29301SW 22941 AFTER PUSHBACK T/E FLAPS WOULD NOT FULLY EXTEND, CABIN CREW REPORTED NOISE RT OVERWING. REMOVED AND REPLACED FLAP DRIVE MOTOR AND FLAP DRIVE UNIT PER MM. 2L72 4F RTA16WE 20030416002012003041600201NM 2003 4 16 DHL2003781001 120030411A5270 SWITCH BOEING727 727227 1384078NM CARGO DOOR OUT OF ADJUST A DHLAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO01768AT 21996 MAIN CARGO DOOR WARNING LIGHT ON S/O PANEL AND MAIN CARGO DOOR NOT CLOSED AND DOOR WARNING LIGHT ON MAIN CARGO DOOR CONTROL BOX ALL ILLUMINATED WHEN CABIN PRESSURE EXCEEDS 8 PSI. PERFORMED EMERGENCY CHECK LIST, REDUCED CABIN PRESSURE AND ALL LIGHTS EXTINGUISHED WHEN CABIN PRESSURE WENT BELOW 6 PSI. THERE WAS NOT A CHANGE IN CABIN PRESSURE RELATED TO THE WARNING LIGHTS. ADJUSTED MAIN CARGO DOOR CLOSED SWITCH PER BOEING AND AEI MAINTENANCE MANUAL 5-35 PAGE 135 PART 2A THRU D. ALL CARGO DOOR LIGHTS OUT AND NO RED WARNING ON S/O PANEL AT 8.75 PSI PRESSURIZATION. A/C IS SAFE FOR FLIGHT. 2L73 4F A3WE 20030416002072003041600207 2003 4 16 SWAA030772 420030404A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030416002192003041600219NM 2003 4 16 AALA20030205 120030214A3350 STRIP BOEING757 757223 1384957NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT PATH FROM 3EF-7EF INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002272003041600227WP 2003 4 16 AALA20030254 120030227A2121 FAN DOUG DC9 DC982 3022082WP CARGO BAY MALFUNCTIONED A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21228AA 49178 STL - FLT 2216 - EN ROUTE TUL-STL, SHORTLY AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMOKE AND FUMES IN THE CABIN. PILOTS TURNED OFF RECIRCULATION FAN AND RIGHT PACK AND SMOKE DISSIPATED. LANDED IN STL WITHOUT FURTHER INCIDENT. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING PER WORK CARD 21-9-6-01. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030416002342003041600234NM 2003 4 16 CALA0300171 120030405A5320 ANGLE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND SUPPORT ANGLE FOR FORWARD LAV AFT WALL CORRODED AT STA 307. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E2GL 20030416002402003041600240NM 2003 4 16 CALA0300177 120030406A5315 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 20 TO RBL 4. REPAIRED IAW SRM 53-10-51. 2L72 4F4 FRTA16WE E2GL 20030416002412003041600241NM 2003 4 16 CALA0300178 120030406A5347 SEAT TRACK BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND SEAT TRACK CORRODED AT STA 277-294.5, RBL 40. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E2GL 20030416002482003041600248SO 2003 4 16 C2XA03SH089 120030407A531014526437001 BUTT STRAP EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV DURING C CHECK THE RT BUTT STRAP IN LAV WAS FOUND TO HAVE CORROSION AT AFT SECTION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030416002512003041600251NM 2003 4 16 CALA0300188 120030411A5310 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND SHEAR TIE CORRODED AT AFT SIDE OF FRAME STA 500D O/B OF S28R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030416002522003041600252WP 2003 4 16 UPS03840424 120030410A2697 WIRE HARNESS DOUG DC8 DC873F 302199FWP FIRE WARNING CHAFED A IPXAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO01814UP 46090 NUMEROUS INTERMITTENT FIRE WARNING ON NR 4 ENGINE INFLIGHT. PERFORMED ENG FIRE SEVERE DAMAGE CHECKLIST AND SECURED ENGINE. RECEIVED BOTH LIGHT AND FIRE BELL. INSPECTED FIRE WARNING HARNESS AND FOUND RT CORE CHAFED. REPAIRED WIRE PER EOM-2000-16032-A, GROUND RAN ENG AND OPS CHECK GOOD. FIRE WARNING CHECKS GOOD PER MM 26-10-00. 2L74 4F RT4A25 20030416002552003041600255NM 2003 4 16 DHL2003741520 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, FUSELAGE SKIN HAS 2 DENTS FWD BS 520 ABOVE STR 26R AND 1 DENT BELOW STR 26R. CUT OUT 2 EACH DAMAGED AREAS (2 X 1 INCH) AND (1.5 X 1.5 INCH). FABRICATED DOUBLER 2024-T3, .071, PO 9912441 (21" X 13.25 INCH) AND STRUCTURAL FILLER, 2024-T3, .063, PO 9912380, (23 X 10.5 INCH) IAW B-727 SRM 53-30-2 AND 53-30-3 FIG 24. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR WASHERS AS REQUIRED IAW B-727 SRM 53-30-3, FIG 24. INSTALLED STRUCTURAL FILLER AND DOUBLER IAW B-727 SRM 51-30-2. NOTE 1 EACH DENT WITHIN LIMITS A=1 INCH, Y=.015, A/Y=66. 2L73 4F RTA3WE 20030416002622003041600262NM 2003 4 16 QXEA0300437 120030405A5420 WEB BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 NR 2 NACELLE LOWER ASSEMBLY DEBRIS DOOR SURROUND STRUCTURE VERTICAL WEB FORWARD OF DOOR IS CRACKED, UPPER LEFT SIDE. REPAIRED IAW RD8/4-71-016. 2H72 4T RTA13NM 20030416002722003041600272NM 2003 4 16 UPS03640419 120030406A3350 LIGHT BOEING767 76734AF 1385212NM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01319UP 27758 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED AND TESTED PER MM 33-51-16-2, CHECKED OK. 2L72 4F RTA1NM 20030416002822003041600282NM 2003 4 16 AALA20030295 120030308A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21793AN 30255 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030416002862003041600286WP 2003 4 16 AALA20030298 120030307A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21295AA 49307 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY AT FIRST CLASS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030416002942003041600294EU 2003 4 16 AALA20030303 120030306A3397 WIRE AIRBUS300 A300B4605R 3930308EU CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2119059 469 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT RIGHT AFT LAVATORY SIDEWALL FLOOD LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030416003372003041600337WP 2003 4 16 UPS03840031 120030103A5510SE085500094 FITTING DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE: C2, RT HORIZONTAL STAB L/E LOWER T-ANGLE IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG SE08550009, AND SRM 51-1-20D. 2L74 4F RT4A25 20030416000742003041600074EA 2003 4 16 SWIA200311862 120030330A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILERON MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07418SW3287 3287 7446 AT LIFTOFF RECEIVED A WHITE STATUS SPOILERON FAULT MESSAGE ON BOTH RIGHT AND LEFT SIDES. REPLACED BAD SPOILERON PCU IAW MM CH 27-62-01. LEAK CHECK GOOD. OPS CHECK GOOD. 2L72 4F RTA21EA 20030416001372003041600137NM 2003 4 16 QXEA0300418 120030331A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH16679361 477 PDX-FORWARD LEFT HAND EGRESS LIGHT INOPERABLE. REMOVED AND REPLACED NR 1 POWER SUPPLY BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030416001532003041600153NM 2003 4 16 AALA20030198 120030214A3397 WIRE BOEING767 767223 1385123NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21330AA 22330 SFO - DURING OVERNIGHT MAINTENANCE, LEFT SIDE AFT ROWS 31-37 SEATS EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHTS WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416001902003041600190NM 2003 4 16 AALA20030263 120030228A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21796AN 30796 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LOWER LEFT EMERGENCY EXIT LIGHT IN G3 GALLEY COAT CLOSET INOPERATIVE. REPLACED FORWARD LOWER LEFT EMERGENCY EXIT LIGHT ASSEMBLY IN G3 GALLEY COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030416002122003041600212WP 2003 4 16 AALA20030046 120030107A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21593AA 53256 TUL - FOUND LONGERON 2L IS CRACKED AFT OF STATION 1418 FRAME, CRACK APPROX .125 INCH LONG. REMOVED DAMAGED SECTION OF LONGERON, OBTAINED AND INSTALLED EXTRUSION PER AARD 53-30-00-2. (M) 2L72 4F RTA6WE 20030416002182003041600218NM 2003 4 16 AALA20030203 120030215A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21650AA 24608 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 16 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002832003041600283WP 2003 4 16 AALA20030296 120030309A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21474 49649 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY IN TAIL CONE INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030416003402003041600340WP 2003 4 16 UPS03840063 120030103A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C2 RADIOGRAPHIC (X-RAY) INSPECTION DETECTED A CRACK ON THE R-1 DOOR LOWER AFT CORNER APPROX .700 INCHES IN LENGTH, STA190 APPROX AT LONG 20R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 14. 2L74 4F RT4A25 20030416003452003041600345WP 2003 4 16 UPS03840004 120030103A53131415997 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C2, AT STA 1540 STR 24L CRACK INSIDE OF HAT SECTION OF STRINGER AFT PIT. REMOVED DAMAGED SECTION OF LONG IAW DC8 SRM 53-2-2,TR 53-153. FAB NEW SECTION OF LONG FROM EXT S141597 IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, DRILLED 2 SPLICES TO FIT IAW DC8 SRM 53-2-2 FIG 10 TR 53-153. INSTALLED LONGERON SECTION AND 2 SPLICES IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030416003502003041600350SO 2003 4 16 SWIA200311704 120030103A5280 HINGE EMB 120 EMB120ER 3260203SO RT MLG DOOR BROKEN A SWIAA UNSCHED LANDING EFJVIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07294SW 120321 AFTER TAKEOFF THE RT MLG WOULD NOT RETRACT. COMPLIED WITH QRH PROCEDURE. CYCLED GEAR TWICE. RETURNED TO SAN. REMOVED AND REPLACED BROKEN HINGE ON RT MLG OUTBOARD FORWARD DOOR IAW EMB 120 MM 52-81-00. ADJUSTED SEQUENCE VALVE PLUNGER AND SWUNG GEAR. OPS CHECK GOOD. 2L72 4T RTA31SO 20030416003572003041600357NM 2003 4 16 UPS03440014 120030106A5210 BEAM BOEING747 747259B 1384804NM PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE: C, NR 2L DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED AS PER SRM 52-10-02 FIG 10. 2L74 4F RTA20WE 20030416003692003041600369WP 2003 4 16 UPS03840079 120030107A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C-2, SEAT TRACK FOUND CORRODED AT STA 1580 TRACK -H- UNDER SIDE. REMOVED DAMAGED SEAT TRACK, REPLACED PER DC8 SRM 53-2-3 AND 51-3-0. 2L74 4F RT4A25 20030416003822003041600382NE 2003 4 16 SWIA200311705 220030109A7200 ENGINE EMB 120 EMB120RT 3260202SO PWA 118 PW118 NE LEFT MALFUNCTIONED A SWIAEA ENGINE SHUTDOWN UNSCHED LANDING EFRVIBRATION/BUFFET FLT CONT AFFECTED PARTIAL RPM/PWR LOSS CLCLIMB 1 NM07593SW 120191 115435 ON CLIMBOUT HEARD AND FELT A LOUD THUMP AND SLIGHT LOSS OF POWER ON THE LEFT ENGINE. ABOUT 30 SECONDS LATER RECEIVED AN 'OIL' MAP AND AURAL WARNING. OIL PRESSURE WAS '0'. PERFORMED PRECAUTIONARY SHUTDOWN AND RETURNED TO SEA. REMOVED AND REPLACED THE LEFT ENGINE AS PER MM 71-00-00. 2L72 4T4 TRTA31SO E20NE 20030416004052003041600405EA 2003 4 16 SWIA200311699 120030113A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN SHORTED A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07905SW 7437 FORWARD ORANGE EMERGENCY LIGHT STRIP, FLOOR LEVEL FORWARD PASSENGER DOOR EMERGENCY EXIT SIGN, AND MID-LEVEL SERVICE DOOR EMERGENCY EXIT SIGN DO NOT ILLUMINATE. REPLACED TRACK LIGHT FLOOR STRIP NR 1. OPS TEST EMERGENCY LIGHTS GOOD. ORANGE STRIP FLOOR LEVEL PASS AND SERVICE DOOR LIGHTS CHECK GOOD. P/N: 36491-1. 2L72 4F RTA21EA 20030417000062003041700006EU 2003 4 17 MALA030116 120030121A3230 CONNECTOR SAAB SF340 340B 7860101EU MLG LOOSE A MALAK NONE P NO WARNING INDICATION NRNOT REPORTED 1 GL15453XJ 340B453 DURING FLIGHT 3172, LT MLG HAD NO INDICATION OF POSITIVE DOWN AND LOCKED. CREW RAN QRH CONFERRED WITH MAINTENANCE CONTROL, LANDED NORMALLY IN DTW. MAINTENANCE FOUND 5GA CONNECTOR LOOSE. CLEANED AND REINSTALLED CONNECTOR. PERFORMED GEAR SWINGS. ALL CHECKS GOOD. 2L72 4T RTA52EU 20030417000082003041700008NM 2003 4 17 UPS03540038 120030118A575414N141719 SLAT TRACK BOEING757 75724APF 1384969NM NR 6 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01413UP 23853 INSPECTION TYPE: 2C, NR 6 SLAT I/B AUX TRACK ON WING SIDE DAMAGED BY NR 2 ENGINE GENERATOR CABLES. GENERATOR CABLES DAMAGED AND TAI DUCT BUNRT THROUGH. REMOVED AND REPLACED SLAT TRACK PER M/M. SPLICED WIRES PER SRM, REPLACED TAI DUCT PER M/M. 2L72 4F RTA2NM 20030417000092003041700009WP 2003 4 17 UPS03840037 120030115A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE: C2, STA 1400 INTERCOSTAL IS CORRODED BEYOND LIMITS AT RBL 49. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 23. 2L74 4F RT4A25 20030417000192003041700019EA 2003 4 17 SWIA200311726 120030118A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07439SW3269 3269 7578 'STAB CHANNEL 1 INOP' STATUS MESSAGE, WILL NOT ENGAGE ON GROUND. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT IAW 27-41-01. OPS CHECK GOOD AND SELF-TEST GOOD AT THIS TIME. 2L72 4F RTA21EA 20030417000242003041700024NM 2003 4 17 PCAA0301022 120030124A2910 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM BROKEN A PCAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA13979HA 373 ALB-DCA FLIGHT 3922 CREW REPORTED HYDRAULIC CONTENTS ON NR 1 SYSTEM BELOW 1.5 QUARTS AND DROPPING. FLIGHT DIVERTED TO MDT FOR REPAIRS. MAINTENANCE FOUND A BROKEN LINE AT THE LANDING GEAR SELECTOR VALVE. LINE WAS REPLACED. FUNCTION AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417000332003041700033EU 2003 4 17 MALA030126 120030126A5420LH7271110613 DOOR SAAB SF340 340B 7860101EU NR 2 NACELLE LOOSE A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15402XJ 340B402 DURING FLIGHT NR 2789, NR 2 ENGINE O/B NACELLE DOOR NOT SECURED, CAME LOOSE INFIGHT. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED COWL DOOR FRAME ASSEMBLY P/N LH7271110-613 RH7271110-614, SECURED CHECK GOOD. 2L72 4T RTA52EU 20030416000702003041600070NM 2003 4 16 QXEA0300406 120030327A3350XD4N RELAY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT MALFUNCTIONED A QXEAO OTHER O OTHER CLCLIMB 1 NM09353PH 496 BOI-ON FLIGHT NUMBER 2209, EMERGENCY LIGHTS FLICKERED ON & OFF DURING CLIMB. REMOVED AND REPLACED CONTROL RELAY. LIGHT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030416001332003041600133NM 2003 4 16 AALA20030004 120030101A21301305027 CONTROL PANEL BOEING757 757223 1384957NM COCKPIT DEFECTIVE A AALABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21615AM 24491 KIN - FLT 924 - EN ROUTE MDE-MIA, UNCOMMANDED CLIMB OF CABIN BY BOTH AUTO CONTROLLERS. CABIN ALTITUDE ALERT SOUNDED AND EMERGENCY DESCENT INITIATED AND OXYGEN MASKS DEPLOYED. LANDED AT KIN WITHOUT FURTHER INCIDENT. FOUND OVERHEAD CABIN PRESSURE SELECTOR PANEL INOPERATIVE. REPLACED PANEL AND NR 1 CABIN PRESSURE CONTROLLER. PERFORMED PRESSURIZATION CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416001992003041600199NM 2003 4 16 AALA20030294 120030306A5320 INTERCOSTAL BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21624AA 24582 TUL - FOUND STATION 1640-1660 CENTER INTERCOSTAL CORRODED. REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL. (M) 2L72 4F RTA2NM 20030416001092003041600109NM 2003 4 16 SWAA030786 120030408A53106517582 BEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/2 D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 181, WL 230 AND RBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM. 2L72 4F RTA16WE 20030416001542003041600154NE 2003 4 16 DL777030286 220030325A7200 SPACER BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 1 ENGINE MISSING A DALAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO27861DA10552 29952 051175 NR 1 ENGINE VIBRATION. FOUND A SPACER MISSING BETWEEN 2 FAN BLADES, DAMAGED TO ACOUSTIC LINER, BOTH FAN AND THRUST REVERSER LINERS. REPLACED PARTS AND REPAIRED DAMAGE. 2L72 4F4 FRTT00001SEE00050EN 20030416001672003041600167SO 2003 4 16 C2XA03SH086 120030407A532014522461011 DOUBLER EMB 145 EMB145ER 3260211SO BEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV-DURING C CHECK THE RT OMEGA BEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030416001742003041600174NM 2003 4 16 AALA20030226 120030222A3350P4010051112 MODULE BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21330AA 22330 SFO - DURING OVERNIGHT MAINTENANCE, LEFT SIDE ROWS 31-37 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416001782003041600178SO 2003 4 16 C2XA03SH097 120030408A53101452246013 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK, CENTER BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030416001792003041600179EA 2003 4 16 COMA0360177 120030401A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO01982CA1232 7168 FLIGHT 5840 TAKEOFF CON FIG SPOILERS, GROUND AND FLIGHT. REPLACED THE NR 1 SECU. 2L72 4F RTA21EA 20030416001812003041600181EA 2003 4 16 COMA0360180 120030402A499038760016 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE APU FAILED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01466CA 7627 FLIGHT 5779 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU LOW OIL PRESSURE SWITCH. 2L72 4F4 FRTA21EA E15NE 20030416001922003041600192NM 2003 4 16 AALA20030274 120030304A33500201720001 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21760AN 31477 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21C INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030416000502003041600050EU 2003 4 16 MALA030236 120030412A3260 CONNECTOR SAAB SF340 340B 7860101EU MLG INDICATOR DISCONNECTED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15457XJ 340B457 DURING APPROACH ON FLIGHT NR 3098, LT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. MAINTENANCE INSPECTED LEFT MAIN LANDING GEAR FOUND CONNECTOR 5GA-P1 DISCONNECTED. MAINTENANCE RECONNECTED AND CLEANED CANNON PLUG, ALL CHECKS GOOD. PERFORMED LANDING GEAR SWING. ALL IAW SF340 MM CHAP 12. 2L72 4T RTA52EU 20030416001192003041600119NE 2003 4 16 DLM11030260 220030320A7200PW44603 ENGINE DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE NR 1 FLAMED OUT A DALAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO27806DE29305 48477 733751 AT 133 KNOTS THE NR 1 ENGINE SURGED WITH FLAME-OUT, THE FRONT AND BACK. INSPECTION IN THE FRONT AND BACK, LOOKS OK. DUE TO AD 2002-21-10, THIS IS A GROUP 3 TAKEOFF SURGE AND THE ENGINE WILL BE CHANGED. 2L73 4F4 FRTA22WE E24NE 20030416001362003041600136NM 2003 4 16 DL78K030278 120030325A3320 BALLAST BOEING737 737832 13844CFNM AFT GALLEY OVERHEATED A DALAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SO27398DA 30774 ELEC ODOR IN REAR OF AIRCRAFT WITH OVERHEAD LIGHTS FLICKERING. REPLACED AFT GALLEY ENTRANCE LIGHT BALLAST. 2L72 4F RTA16WE 20030416001622003041600162NM 2003 4 16 AALA20030204 120030215A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 NM01789AN 30252 DFW - DURING OVERNIGHT, FORWARD GALLEY SIDEWALL EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030416001832003041600183NM 2003 4 16 AALA20030248 120030226A3397 WIRE BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21358AA 24039 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 20AB-23AB WILL NOT TEST. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 21AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416002112003041600211NM 2003 4 16 SWAA030775 120030403A53206557463 FITTING BOEING737 7377H4 1384404NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING FASTENER LOOSE. SECURED FASTENER PER SRM. 2L72 4F RTA16WE 20030416002152003041600215WP 2003 4 16 AALA20030058 120030109A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170401 49312 TUL - FOUND .25 INCH CRACK AROUND RIVET HEAD, FS 1380. EXTERNAL DOUBLER INSTALLED PER SRM 51-01. (M) 2L72 4F A6WE 20030416002242003041600224WP 2003 4 16 AALA20030237 120030221A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21228AA 49178 TUL - FOUND TWO .25 INCH CRACKS EXTENDING FROM FASTENER HOLE IN FUSELAGE SKIN RIGHT SIDE STATION 1380 BETWEEN LONGERONS 13R AND 14R. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-01-00 FIG 2 SHEET 3. (M) 2L72 4F A6WE 20030416002312003041600231NE 2003 4 16 CX7A194J34 220030320A7532 BLEED VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE LEAKING A CX7AE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL03305CE 340B202 LT BLEED AIR LEAK WHILE IN FLIGHT. SHUT DOWN LEFT ENGINE (IAW CHECKLIST) 2L72 4T4 TRTA52EU E8NE 20030416002392003041600239NM 2003 4 16 CALA0300176 120030406A5315 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917317 23368 INSPECTION FOUND FLOORBEAM CORRODED THROUGH FASTENERS AND SHIM AT STA 986.5, RBL 48. THE CORRODED SECTION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03851. 2L72 4F4 FRTA16WE E2GL 20030416002462003041600246SO 2003 4 16 C2XA03SH093 120030408A531014530628001 BEAM EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION ON THE LOWER FLANGE BETWEEN FRAMES 24-25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED OMEGA BEAM IAW 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030416002492003041600249SO 2003 4 16 C2XAO3SH092 120030408A531014530627001 BEAM EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV DURING C CHECK THE LEFT HAND OMEGA BEAM LOWER FLANGE WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 24-25. MAINTENANCE REMOVED DAMAGED AND REPAIRED AFFECTED SECTION IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030416002532003041600253SO 2003 4 16 C2XA03SH091 120030407A532014522178005 CHANNEL EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV DURING C-CHECK, SERVICE DOOR CENTER THRESHOLD FOUND TO HAVE CORROSION AROUND NUT PLATES. MAINTENANCE REMOVED DAMAGE AND PERFORMED DOUBLER REPAIR TO AFFECTED STRUCTURE IAW EMB SRM 145 53-21-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030416002572003041600257SO 2003 4 16 C2XA03CL088 120030409A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714542 145547 DURING ROUTINE MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 POSITION EMERGENCY BATTERY AND CHARGER. OPERATIONAL CHECKS GOOD. BATTERY P/N 2013-1A, S/N 80601. 2L72 4T RTT00011AT 20030416002642003041600264NM 2003 4 16 CALA0300183 120030408A5310 BEAM BOEING777 777224 1385225NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0978008 29478 INSPECTION FOUND FORWARD CARGO DOOR UPPER EDGE BEAM WEB DENTED. REPAIRED IAW ECRA 5230-01721. 2L72 4F RTT00001SE 20030416002702003041600270GL 2003 4 16 UPS03640415 220030408A73201820CM33P06 EEC BOEING767 76734AF 1385212NM GE CF6 CF6* 30020GL RT ENGINE FAILED A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO01303UP 27241 704298 INSPECTION TYPE: ETOP, ON DESCENT IN HEAVY RAIN, RT ENGINE ROLLBACK, (POSSIBLE FLAME-OUT). ADVANCED THROTTLE AND ENGINE RESPONDED AFTER 10 SECONDS VISUALLY CHECKED INLET AND EXHAUST AREA NO DEFECT NOTED, PERFORMED FUEL SUMP DRAIN CHECK, NO WATER AND DEBRIS FOUND. REMOVED AND REPLACED EEC IAW MM 73-21-15, PERFORMED TEST NR 4, NR 11 AND NR 12 SATISFIED, OK FOR SERVICE. 2L72 4F4 FRTA1NM E23EA 20030416002712003041600271NM 2003 4 16 DHL2003741523 120030326A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, LOWER FWD CARGO COMP AIR CONDITIONING AREA FRAME BS 720F CORRODED BETWEEN STR 26 R/27R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA OF FRAME BS 720 F DIMENSION 6 X .5 INCH AND FABRICATED REPAIR PIECE DIMENSIONS 7.75 X 3.5 INCH USING 7075 T-6 .063 PO 9911861 IAW B-727 SRM 53-10-4 FIG 11. ALODINED AND PRIMED REPAIR PART IAW B-727 SRM 51-10-2. INSTALLED REPAIR IAW B-727 SRM 51-30-2 AND 53-10-4 FIG 11. 2L73 4F RTA3WE 20030416002982003041600298NM 2003 4 16 AALA20030304 120030310A3350 SOCKET BOEING767 767323 1385205NM EXTERIOR CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21342AN 33081 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT ADF ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED RIGHT ADF ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416003002003041600300NM 2003 4 16 AALA20030305 120030310A3350 SOCKET BOEING767 767323 1385205NM EXTERIOR CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21342AN 33081 DFW - DURING OVERNIGHT MAINTENANCE, LEFT SLIDE GROUND EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED LEFT SLIDE GROUND EXTERNAL EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416003262003041600326NM 2003 4 16 AALA20030309 120030311A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21376AN 25445 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT MID GALLEY EMERGENCY DIRECTIONAL FLOODLIGHT NEXT TO FLIGHT ATTENDANT INOPERATIVE. REPLACED RIGHT MID GALLEY EMERGENCY DIRECTIONAL FLOOD LIGHT NEXT TO FLIGHT ATTENDANT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416003282003041600328NM 2003 4 16 AALA20030310 120030312A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35C INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 35C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416000252003041600025NM 2003 4 16 UPS03240006 120030109A3350 BATTERY BOEING727 72727C 138400JNM EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01909UP 19115 INSPECTION TYPE: PFLT. EMERGENCY EXIT LIGHT ASSEMBLIES AT CABIN ENTRY AND CREW ENTRY DOOR BATTERIES DEAD. RECHARGED BATTERIES, OPS CHECKS OKAY. 2L73 4F A3WE 20030416000772003041600077NM 2003 4 16 QXEA0300413 120030328A5420 CHANNEL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 RIGHT HAND LOWER COWL LEFT VERTICAL CHANNEL CRACKED AT LOWER RIVET, AFT OF BYPASS DOOR. REPAIRED IAW RD 8/4-71-016 AND DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20030416001232003041600123NM 2003 4 16 DLM88030262 120030321A53205910130387 ANGLE DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27978DL 53259 DURING ACCOMPLISHMENT OF EA09-075135-03AD, MEO1 OPN 0101 GRAPHIC 1, SHEET 3 STEP 1, THE P-DOME LOWER T-ANGLE WAS DAMAGED. THERE IS NO DAMAGE ALLOWED IN THIS AREA {REF SRM 53-05D FIG 115}. THE ONLY FIX IS TO SPLICE A IN A NEW SECTION {REF SRM 53-03D FIG 37}. THERE IS A CONCERN THAT SINCE THIS EA HAS BEEN ACCOMPLISHED ON ALL A/C, THERE ARE OTHER A/C IN SERVICE, POSSIBLY FOR LONG PERIODS OF TIME, WITH THIS SAME CONDITION. 2L72 4F RTA6WE 20030416001502003041600150WP 2003 4 16 AALA20030064 120030115A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21569AA 49351 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED TAIL CONE EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030416001632003041600163NM 2003 4 16 DLM88030301 120030329A335041B004AD073 BATTERY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27934DL 49721 ON LAYOVER, FOUND F/C OVERHEAD AISLE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER M/M, CHECKS NORMAL. 2L72 4F RTA6WE 20030416001772003041600177NM 2003 4 16 QXEA0300412 120030331A2120 SMOKE DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09345PH 476 BOI- ON FLIGHT 2206 THERE WAS AN UNKNOWN SOURCE OF SMOKE AND FUMES IN CABIN. GROUND RAN AIRCRAFT NR 1 AND NR 2 ENGINES AND BLEEDS, NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030416002382003041600238NM 2003 4 16 CALA0300175 120030406A5755 ANGLE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE NR 5 SPOILER CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 1 INCH CRACK IN SUPPORT ANGLE ON RT WING TRAILING EDGE PANEL JUST OUTBOARD OF NR 5 SPOILER PANEL. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 57-53-71. 2L72 4F4 FRTA16WE E2GL 20030416002902003041600290EU 2003 4 16 AALA20030300 120030307A3350 CONNECTOR FOKKERF28 F28MK0100 4990807EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211406A 11359 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS ROW 11-13 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT BATTERY CONNECTOR AT SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030416003712003041600371SO 2003 4 16 SWIA200311687 120030107A2750 CONNECTOR EMB 120 EMB120ER 3260203SO FLAP ACTUATOR CONTAMINATED A SWIAO OTHER NF FALSE WARNING FLT CONT AFFECTED LDLANDING 1 NM07187SW 120037 CONTROL FAULT ON INBOARD FLAPS DURING FLAP RETRACTION. CLEANED CONNECTOR ON FLAP INBOARD ACTUATORS ON BOTH SIDES. RAN SEVERAL TIMES. NO FAULTS AT THIS TIME. 2L72 4T RTA31SO 20030416003762003041600376SO 2003 4 16 SWIA200311697 120030108A27523082001007 ACTUATOR EMB 120 EMB120RT 3260202SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07269UE3000 2017 120194 FLAP LIGHT ON MAP PANEL ASSOCIATED WITH ADVANCED SWS AND CONTROL FAULT ON OVERHEAD. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50-00. CYCLED FLAPS SEVERAL TIMES. ALL CHECKS GOOD. 2L72 4T RTA31SO 20030416003792003041600379WP 2003 4 16 UPS03840026 120030109A57103704841501 FITTING DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE: C2, RT WING STRINGER END FITTING IS CRACKED I/B OF XRS 74 AT STRINGER 51. REMOVED AND REPLACED FITTING IAW DWG 3704841, AND SRM 51-1-20D. 2L74 4F RT4A25 20030416003902003041600390SO 2003 4 16 SWIA200311710 120030111A243523080013 STARTER GEN EMB 120 EMB120ER 3260203SO APU SHORTED A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 NM07295SW5329 2442 120322 SMELLED SOMETHING BURNING. APU GEN DROPPED OFF LINE. APU SHUT ITSELF DOWN. REPLACED APU CURRENT SENSOR RELAY (FOUND MELTED). FOUND WIRES AT APU STARTER GENERATOR TERMINAL BOARD MELTED. REPLACED APU STARTER GEN WITH SERVICEABLE STARTER GENERATOR. REMOVED DAMAGED TERMINALS AND TRIMMED OFF DAMAGED WIRE ENDS. SWEDGED ON NEW TERMINALS AS REQUIRED. PERFORMED OPS CHECK OF APU STARTER/GEN. OPS CHECK GOOD. 2L72 4T RTA31SO 20030417000042003041700004EA 2003 4 17 SWIA200311707 120030116A7830864808 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07442SW2674 2674 7609 'LEFT REVERSER UNSAFE' MESSAGE AFTER TURNING TR SWITCH OFF. REMOVED AND REPLACED PSEU IAW CRJ MM 32-61-01. CHECKS GOOD ON GROUND. FLIGHT CHECK GOOD. 2L72 4F RTA21EA 20030417000072003041700007NM 2003 4 17 UPS03240021 120030116A2420BA10604501 RELAY BOEING727 72725C 138400HNM E/E BAY INOPERATIVE A IPXAK NONE H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SO01937UP 19302 DURING LANDING ROLLOUT & T/R APPLICATION A PWR LOSS TO THE FLT & ENGINE INSTRUMENTS WAS NOTED. THE COCKPIT WENT MOMENTARILY DARK. APPLIED T/R DURING TAXI IN AND NOTED KW NR 1 JUMPED TO 35 WHILE THE KWNR 2 DROPPED TO ZERO. REMOVED AND REPLACED R58S POWER RELAY AND REPLACED R112 ESSENTIAL POWER RELAY. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. 2L73 4F A3WE 20030417000112003041700011SO 2003 4 17 SWIA200311711 120030115A3350 DIODE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSFAILED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07295SW 120322 TWO RED FLOOR PROXIMITY EMERGENCY LIGHTS OUT AT MAIN CABIN DOOR EXIT. SOLDERED IN NEW DIODE AT ROW 6. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20030417000272003041700027WP 2003 4 17 UPS03840074 120030114A53105751110503 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C-2, FWD CARGO PIT FUSELAGE FRAME LOWER FLANGE CORRODED STA 500 L34L-L35R. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-4-1. FABRICATED -5 & -7 REPAIR PARTS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FABRICATED SHIMS .080 7075-T6 (PO 395941.1) IAW DC8 SRM 53-2-0. ALODINED AND PRIMED SHIMS IAW DC8 SRM 51-1-8. INSTALLED SHIMS, -5 &-7 REPAIR PARTS IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030417000402003041700040SO 2003 4 17 SWIA200311734 120030125A3210 LANDING GEAR EMB 120 EMB120ER 3260203SO MAIN MALFUNCTIONED A SWIAA UNSCHED LANDING EFJVIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07251YV 120251 RIGHT MAIN LANDING GEAR DID NOT RETRACT FOR APPROXIMATELY TWO MINUTES AFTER TAKEOFF. LANDING GEAR CHECKS OK. COULD NOT DUPLICATE PROBLEM. 2L72 4T RTA31SO 20030417000422003041700042EA 2003 4 17 SWIA200311736 120030125A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07412SW 7101 UPON CLIMBING THROUGH 4000 FT THE PASSENGER DOOR LATCH CAUTION MESSAGE ILLUMINATED, FOLLOWED BY A PASSENGER DOOR WARNING MESSAGE. FOLLOWED QRH. RETURNED TO GTF. INSPECTED DOOR AND CHECKED CABIN PRESSURE. DOOR AND PRESSURE CHECKS OK PER MM 21-31-00. 2L72 4F RTA21EA 20030417000442003041700044SO 2003 4 17 SWIA200311738 120030119A27523430001001 ACTUATOR EMB 120 EMB120ER 3260203SO RT TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07270YV 120270 UNCOMMANDED, THE RIGHT INBOARD FLAP WENT DOWN PARTIALLY WHILE AIRCRAFT WAS PARKED. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR AS PER MM 27-50-00. NO LEAKS. OPS CHECK GOOD. 2L72 4T RTA31SO 20030416000142003041600014EU 2003 4 16 XNOA01099 120030107A3230 LANDING GEAR AIRBUS300 A300B4203 3930306EU MAIN MALFUNCTIONED A XN0AO OTHER J WARNING INDICATION APAPPROACH 1 GL23473AS 203 DURING FINAL APPROACH TO DAY MLG WOULD NOT EXTEND. MANUAL EXTENSION PROCEDURE WAS USED. REMOVED & REPLACED ELECTRO VALVE IAW A300 MM 32-31-12. PERFORMED INSPECTION CHECK IAW 32-31-12. NO DEFECTS NOTED. PERFORMED GEAR SWING IAW A300 MM 32-30-00 TO SYS 1 & 2. NO DEFECTS NOTED. 2L72 4F RTA35EU 20030416001032003041600103NM 2003 4 16 SWAA030782 120030407A3350604222 BATTERY BOEING737 7372T4 1384492NM AFT CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHTS INOP IN AFT CABIN. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030416002032003041600203 2003 4 16 ABXA030128 420030401A221075130 SERVO VALVE DOUG DC8 DC863F 302198FWP AUTOPILOT MALFUNCTIONED A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23828AX 45999 UNCOMMANDED YAW IN FLIGHT. AUTOPILOT ON. REPLACED RUDDER POWER PACK TRANSFER VALVE IAW DC-8 MM 27-21-6. 2L74 4F 4A25 20030416002262003041600226NM 2003 4 16 AALA20030246 120030225A3350 CONNECTOR BOEING757 757223 1384957NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21184AN 29594 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM 3ES TO 5ES INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHTING SECTION BETWEEN SEATS 3EF TO 5EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002592003041600259NM 2003 4 16 QXEA0300435 120030404A5415 ATTACH FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 NR 2 NACELLE MID FRAME ASSEMBLY INBOARD LOWER COWL ATTACH LUG HAS ROUGH WEAR IN HOLE. REPAIRED IAW HORIZON AIR EA 6-71-86 AND RD8/4-54-124. 2H72 4T RTA13NM 20030416003542003041600354NM 2003 4 16 UPS03240064 120030104A5511 FRAME BOEING727 72721C 138400MNM HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE: C, SUSPECT CRACK ON LT HORIZONTAL STAB UPPER FRAME JUST I/B OF ELEVATOR RIB STA 173.21. REPAIR CARRIED OUT IAW SMRO EO 2003-001-004 UPS ENGINEERING FILE 727-55-20029. 2L73 4F A3WE 20030416003562003041600356EU 2003 4 16 RAIA00301007 120030105A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSDISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03555HK 41072 MX- STL SECTION OF EMERGENCY PATH LIGHTS INOP. RE-SECURED CONNECTOR TO CENTER SECTION OF EMERGENCY PATH LIGHTS, OPS CHECK OK. 2L72 4T RTA41NM 20030417000512003041700051NM 2003 4 17 UPS03440090 120030125A3350 LIGHT BOEING747 747123 1384873NM MAIN DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 INSPECTION TYPE: PFLT, INOPERATIVE MAIN DECK EMERGENCY LIGHT AFT LEFT OF CREW LADDER. OPS CHECK NORMAL. COULD NOT DUPLICATE. 2L74 4F A20WE 20030417000682003041700068NM 2003 4 17 UPS03240121 120030121A5510 BEAM BOEING727 72722C 138400FNM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, RT HORIZ STAB UPPER T/E BEAM BETWEEN RIB AT STR 66.50 & STR 99.76 IS CORRODED UNDER RUBSTRIP. BEAM REPLACED IAW DRAWINGS 65-20657, 65-20658, 65-20659, 65-20660-65 22402 & 65-22987 2L73 4F A3WE 20030417000722003041700072EA 2003 4 17 SWIA200311746 120030124A27604916405 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07441SW515 424 7602 FLIGHT SPOILERS AND SPOILERONS CAUTION MESSAGE AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE DISPLAYED IN FLIGHT. REMOVED AND REPLACED WITH A SERVICEABLE NR 2 SECU IAW MM 27-61-05. 2L72 4F RTA21EA 20030417000852003041700085EA 2003 4 17 QXEA0300211 120030128A2810D98C09602 SENSOR CNDAIRCL600 CL6002C10 1390015EA ZONE 100 LEAKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09600QX2798 10005 BIL-ON FLIGHT NUMBER 2483, FLUID LEAKING AT AIRCRAFT TAIL NEAR APU. REMOVED AND REPLACED PRIMARY EJECTOR SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030417000882003041700088EA 2003 4 17 QXEA0300214 120030131A261247388904 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09601QX1618 10009 SEA-ON FLIGHT NUMBER 2485, R FIRE FAILURE MASTER WARNING. REMOVED AND REPLACED FIRE DETECTION EXTENSION CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030417001012003041700101NM 2003 4 17 QXEA0300228 120030118A1430 RIVET BOMBDRDHC8 DHC8401 1390041NM ISOLATION MOUNT MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX- FOUR RIVETS MISSING FROM FRAME X-97.5 AND INSTRUMENT PANEL ISOLATION MOUNT C-CHANNEL ON THE RIGHT HAND SIDE OF Y 26.0. REPAIRED IAW DHC-8 Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030417001172003041700117NM 2003 4 17 QXEA0300233 120030131A5411 FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX-LOWER COWL NR 2 MID FRAME IS CRACKED. REPAIRED IAW RD8/4-71-016. 2H72 4T RTA13NM 20030417001212003041700121EU 2003 4 17 RAIA00301023 120030124A3260 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU NLG FALSE INDICATIONA RAIAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 CE03574HK 41093 CMI - NOSE LANDING GEAR DOWN AND LOCK INDICATION INOP. EMERGENCY LANDING. MAINTENANCE PERFORMED FUNCTIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM, NO DEFECTS NOTED. 2L72 4T RTA41NM 20030417001222003041700122SO 2003 4 17 RAIA00301025 120030126A2741 WARNING LIGHT EMB 145 EMB145LR 3260212SO PITCH TRIM FALSE INDICATIONA RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03818HK 145059 5689-STL- PITCH TRIM FAIL WARNING. MAINTENANCE RESET AIRCRAFT POWER, PITCH TRIM OPS CHECK OK. 2L72 4T RTT00011AT 20030417001232003041700123SO 2003 4 17 RAIA00301027 120030127A2913M832481113 O-RING EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL HYD PUMP BROKEN A RAIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 CE03809HK 145187 311258 ELM - RIGHT ENGINE LOW OIL PRESSURE, SHUT DOWN ENGINE IN FLIGHT, EMERGENCY LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP SHAFT O-RING, LEAK CHECK OK. 2L72 4F4 FRTT00011ATTE6CH 20030417001242003041700124SO 2003 4 17 RAIA00301029 120030130A2910 HYDRAULIC SYSTEM EMB 145 EMB145 3260210SO LOW A RAIAO OTHER O OTHER LDLANDING 1 CE03805HK 145096 THUMPING NOISE FROM NOSE WHEEL WELL AREA AFTER LANDING GEAR EXTENDED. MAINTENANCE BLED AND SERVICED THE HYDRAULIC SYSTEM. 2L72 4F RTT00011AT 20030417001352003041700135WP 2003 4 17 UPS03840150 120030130A53205613064178 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE:C1 CLIP IS CRACKED AT STA 80 ABOVE LONG 30L. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5613064 AND SRM 51-1-20D. 2L74 4F RT4A25 20030417001442003041700144NM 2003 4 17 PCAA0302039 120030207A3350 BULB DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT LOOSE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13842EX 341 DURING ROUTINE MAINTENANCE VISIT 3RD RED FLOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. CONNECTOR PIN WAS RESOLDERED, AND BULB REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417001602003041700160EU 2003 4 17 MALA030150 120030131A3020 DUCT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A1 30030NE INTAKE HEAT DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15112XJ DURING FLIGHT NR 3236, LT INTAKE HEAT LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED LT UPPER DUCT REFERENCE 409 CARD 170105 FOR DETAILS. 2L72 4T4 TRTA52EU E8NE 20030417001612003041700161EU 2003 4 17 MALA030145 120030207A261289905202 CONTROL BOX SAAB SF340 SF340A 7850100EU RT FIRE DETECT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL1599XJ 340A099 EN ROUTE TO LNK ON FLIGHT ON FLIGHT NR 2944, RT ENGINE FIRE INDICATION. DIVERTED FLIGHT TO SUX. FOLLOWED MEMORY ITEMS THEN FOLLOWED QRH, DECLARED EMERGENCY, LANDED IN SUX. MAINTENANCE FOUND RT FIRE DETECTION CONTROL BOX P/N 89905202 TO BE BAD. REPLACED BOX IAW AMM-26-11-10 SN/ON 0608, SN/0FF 0655. REPLACED LT AND RT FIRE BOTTLES DUE TO BEING BLOWN, 2L72 4T RTA52EU 20030417001672003041700167NE 2003 4 17 QXEA0300246 220030210A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX1981 10041 GEE965303 NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR BLADES MISSING FROM HP TURBINE. REPLACED ENGINE. AIRCRAFT OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030417001702003041700170NM 2003 4 17 UPS03240158 120030128A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C NDT HAVE MATERIAL LOSS INDICATION OF 15-20 PERCENT ON FUSELAGE SKIN FWD OF BUTT JOINT 360, STR 25R TO 27R. FASTENERS REMOVED FROM ABOVE AREA IAW SRM 51-30-2. TO FACILITATE CORROSION CLEAN UP EXISTING DOUBLER ABOVE STR 25R DE-RIVETED BETWEEN BS 328 AND BS 360 IAW SRM 51-30-2. NEW DOUBLER FABRICATED IAW BOEING DRG 65-18420. NEW DOUBLER FASTENED IAW SRM 51-30-2 AND BOEING DRG 65-18420. 2L73 4F A3WE 20030417001792003041700179EA 2003 4 17 SWIA200311770 120030207A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07597SW1157 1157 7293 ROW 8 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED TB105, BATTERY PACK AND BATTERY CHARGER NR 2 IAW MM 33-51-05 AND WIRING MANUAL STANDARD PRACTICES. OPS CHECK NORMAL. 2L72 4F RTA21EA 20030417001812003041700181SO 2003 4 17 SWIA200311772 120030209A32331959500007 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT MLG MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07224SW 120294 DURING GEAR RETRACTION ON TAKEOFF, THE LEFT MAIN GEAR RED A AND B LIGHTS REMAINED ILLUMINATED AND A NOTICEABLE DRAG CAME FROM THE LEFT SIDE. RETURNED TO DEN. REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR IAW MM 32-11-00. S/N OFF 237. 2L72 4T4 TRTA31SO E20NE 20030417001832003041700183EA 2003 4 17 SWIA200311774 120030115A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 FS 621 FLOOR SUPPORT ANGLE LBL 41 FOUND CRACKED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV-A. ANGLE P/N: 601R53-61-117-1. REPAIR ANGLE P/N: 601R53-61-117-3. 2L72 4F RTA21EA 20030416003312003041600331EA 2003 4 16 SWIA200311728 120030102A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW 7518 FS 280 RBL 9.0 FLOORBEAM I/B ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-21. P/N: 601R3113-58. 2L72 4F RTA21EA 20030416003752003041600375EA 2003 4 16 SWIA200311754 120030108A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07430SW 7523 FS 280 LBL AND RBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REMOVED AND INSTALLED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21 AND 51-23-00. P/N: 601R3113-57. 2L72 4F RTA21EA 20030416003932003041600393EA 2003 4 16 SWIA200311696 120030111A271010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07426SW50 50 7468 LT AILERON FLUTTER DAMPER STATUS MESSAGE AND ICON ON FLIGHT CONTROL PAGE BETWEEN 160-200 KIAS, INTERMITTANTLY. REMOVED AND REPLACED LT AILERON FLUTTER DAMPER IAW MM 27-15-05. OPS CHECKS GOOD ON GROUND. FAILED FLIGHT TEST. 2L72 4F RTA21EA 20030416003972003041600397NM 2003 4 16 P5CA0300720 120030112A541565B913141 FITTING BOEING747 7472U3B 1384846NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 FIVE CRACKS TOTAL FOUND NR 2 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1 INCH & (1) .875 INCH RADIALLY/ O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX .75 INCH & (2) 1 INCH EA RADIALLY. CRACKED BATHTUB FITTING REPLACED AS PER S/B 747-54-2113-R2. 2L74 4F RTA20WE 20030417000462003041700046EA 2003 4 17 SWIA200311740 120030118A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07587SW 7062 AFTER TAKEOFF SELECTED GEAR UP, APPROXIMATELY 10 SECONDS LATER RECEIVED A GEAR DISAGREE WARNING WITH THE MAIN GEAR INDICATING UP AND THE NOSE WHEEL HAVING YELLOW CROSS HATCHING. RAN QRH, RETURNED FOR NORMAL LANDING. SERVICED NLG STRUT WITH MIL H5606 AND NITROGEN IAW 12-12-32. ADJUSTED PROXIMITY SWITCH. AIRCRAFT JACKED AND LANDING GEAR SWUNG SEVERAL TIMES. OPS CHECK GOOD. 2L72 4F RTA21EA 20030417000742003041700074 2003 4 17 SWIA200311748 420030127A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07597SW 7293 STALL FAIL INDICATION OCCURS AT GEAR RETRACTION, INDICATION GOES AWAY AT TOUCHDOWN. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-35-01. OPS CHECKS GOOD. S/N OFF 441. 2L72 4F RTA21EA 20030417000752003041700075WP 2003 4 17 IXXA300010O 120030131A2823 SHUTOFF VALVE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUEL LOOSE A IXXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW11825BX83459409 45978 693278 UPON TAKEOFF ROLL FROM CLT WITH INTENTION TO FLY TO TOL. CREW NOTED NR 4 ENGINE WAS NOT PRODUCING SELECTED POWER. CREW REJECTED TAKEOFF WHEN GROUND SPEED REACHED 80 KNOTS. CREW RETURNED TO BLOCKS. UPON INSPECTION, MAINTENANCE DISCOVERED NR 4 ENG FUEL SHUT OFF LEVER IMPROPERLY SECURED. MAINTENANCE RESECURED FUEL SHUT OFF LEVER. OPERATIONALLY CHECKED ENGINE AND FOUND OPERATION NORMAL. ALL WORK WAS COMPLETED PER THE APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20030417001082003041700108NM 2003 4 17 PCAA0302036 120030206A2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003NM MLG MALFUNCTIONED A PCAAO OTHER O OTHER LDLANDING 1 EA13827EX 390 LGA-FLIGHT 3615 CREW REPORTED THAT WHEN SELECTING GEAR DOWN THE NR 2 HYDRAULIC PRESSURE DROPS TO ZERO. MAINTENANCE BLED NR 2 LANDING GEAR SEQUENCE VALVE, NOSE GEAR ACTUATOR, AND NR 2 HYDRAULIC SYSTEM IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 12-10-29. ENGINE RAN AND OPERATED SYSTEM. LEAK CHECK WAS GOOD, AND ALL SYSTEMS OPERATED NORMALLY. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417001512003041700151SO 2003 4 17 SWIA200311762 120030202A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07293SW6574 6574 120320 ROW 9 OVERHEAD BIN, FLOOR AND DOOR EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTING BATTERY PER 32-00-00. OPS CHECK GOOD NR 3 POSITION. 2L72 4T RTA31SO 20030417001552003041700155 2003 4 17 SWIA200311767 420030204A3418 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA STALL WARNING ACTIVATED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07589SW 7072 STALL FAIL MESSAGE AND MACH TRIM MESSAGE. PERFORMED PITOT MOISTURE PURGE AND TESTED IAW MM 34-11-00. MACH TRIM ENGAGES. OPS CHECKS GOOD. PERFORMED STALL WARNING OPS CHECK IAW MM 27-35-01. STALL WARNING OPS CHECKS GOOD. 2L72 4F RTA21EA 20030417001562003041700156EU 2003 4 17 MALA030146 120030208A7430 RELAY SAAB SF340 340B 7860101EU IGNITION MALFUNCTIONED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15434XJ 340B434 DURING FLIGHT 2782, LT AUTO IGNITION LIGHT REMAINED ILLUMINATED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED LT AUTO IGNITION RELAY 1JA, AND 31PC, ALL CHECKS GOOD. 2L72 4T RTA52EU 20030417001622003041700162EU 2003 4 17 MALA030151 120030206A36105701C000003 SENSOR BAC 146 AVRO146RJ85A1500097EU CUSTOMER AIR MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15522XJ E2347 ON TAKEOFF OF FLIGHT 3649, INTAKE LO PRESS ILLUMINATED COULD NOT RESET IN CLIMB AFTER POWER REDUCTION LIGHT WENT OUT, ON AGAIN WITH POWER INCREASE. ON DESCENT WITH WING AND TAIL ICE ENGINE NR 1 AIR FAULT AND AIR LO TEMP ILLUMINATED WITH N2 LESS THAN 88. AIR RETURN TO MEM. MAINTENANCE REPLACED NR 1 ENGINE TEMP SENSOR IAW AVRO AMM 36-11-21. OPS CHECK GOOD. NO ENGINE AIR FAULT OR LOW TEMP INDICATION P/N 5701C000-003 SN/ON 617948-12, SN/OFF 534537-5 COULD NOT DUPLICATE INTAKE NR 1 LOW PRESS PROBLEM AT ANY POWER SETTING. 2H74 4F RTA49EU 20030417001762003041700176EA 2003 4 17 QXEA0300249 120030211A2611 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 FALSE ACTIVATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09602QX 10010 LAX-FLIGHT544- AIRCRAFT RETURNED TO FIELD WHEN SHORTLY AFTER TAKEOFF, THE CREW RECEIVED 4 CHIMES AND A RED SMOKE AFT LAV MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED AN OPERATIONAL TEST OF THE AFT LAV SMOKE DETECTOR. OPERATIONAL CHECK WAS GOOD AND NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030417001872003041700187NM 2003 4 17 F3LA200300046 120030129A2560 PAD BOEING737 7373M8 1384615NM GIRT BAR LOCK CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON SLIDE GIRT BAR LOCK PAD AT STA 344, LBL 59. FABRICATED AND INSTALLED REPLACEMENT PAD PER SRM 51-40-02. 2L72 4F RTA16WE 20030417001912003041700191NM 2003 4 17 P5CA0300753 120030129A5330 SKIN BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND UPPER LOBE DECK ON BETWEEN STR 8 TO STR 10A RT. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH SEGMENT, SPLICE AND STRAP PER SRM 53-10-04 FIG 10. 2L74 4F A20WE 20030422000122003042200012EA 2003 4 22 ASOA03084 120030226A3350BF50390901 COVER CNDAIRCL600 CL6002B19 1900309EA EXIT SIGN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11861AS 7445 FLT 4479 - DURING A GROUND INSPECTION AT CHS, A LIGHTED EXIT SIGN COVER WAS FOUND TO BE MISSING. MAINTENANCE INSTALLED A LIGHTED EXIT SIGN COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000172003042200017 2003 4 22 MEX2003061 420030307A34204688000307 DISPLAY DOUG DC9 DC987 3022087WP AHRU FAILED A ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW231075T 49724 FLT 169 - CUL-MEX - AIRTURN BACK, DURING CLIMB IN THE FMA, AP TRIM THE NO AUTO LAND MESSAGE WAS SHOWN. THERE WAS A DIFFERENCE BETWEEN RMI'S OF 170 DEGREES. THE FD DISAPPEAR WITHOUT OBEY AUTO THROT AT SELECTED VELOCITIES. TESTS WERE PERFORMED IN STP AND SYSTEM WAS OK. DURING OVERNIGHT SERVICE THE AHRU NR 2 WAS REPLACED IAW MM 34-21-10, TEST PERFORMED IAW MM 22-01-05, ALL CORRECT. (M) 2L72 4F RTA6WE 20030422000382003042200038EA 2003 4 22 ASOA03071 120030220A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 FLT 4551 - DURING A GROUND INSPECTION IN ATL, THE OVERHEAD EMERGENCY CEILING LIGHTS AT ROWS 2 AND 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY CEILING LIGHT LAMP AT ROW 2 AND RESET THE LAMP AT ROW 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000402003042200040EA 2003 4 22 ASOA03074 120030222A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A HANGAR CHECK IN MCN, FRAME STATION 718 BETWEEN STRINGERS 10 TO 12 ON THE LEFT AND RIGHT SIDES, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING FRAME STATION 718 BETWEEN STRINGERS 10 TO 12 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-0067A. (M) 2L72 4F RTA21EA 20030422000552003042200055EU 2003 4 22 BMAC030008 120030227A26121218413 WARNING SYSTEM BAG JETSTMJETSTM3101 1500215EU RT POSITION INTERMITTENT A B16AO OTHER O OTHER TXTAXI/GRND HDL 1 NE05539PA 741 FLT 3531 - PSM - PILOT REPORTED RIGHT FIRE WARNING BELL WEAK. MAINTENANCE FOUND BELL TO BE INTERMITTENT. REPLACED RIGHT FIRE WARNING BELL IAW J-31 AMM 26-10-13. OPS CHECKED GOOD. (M) 2L72 4T RTA21EU 20030422000972003042200097SO 2003 4 22 SIMA200307007 120030306A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 26 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT 6.25 INCH SECTION OF THE DAMGAED BEAM. FABRICATED AN EXTERNAL ANGLE, SHIMS AND FILLER. REPAIR DONE IAW EMB SRM (SRM 145/1142 REV 20) CHAPTERS 53-22-10 FIG 201. (M) 2L72 4F RTT00011AT 20030422001072003042200107 2003 4 22 USAASB03037 420030311A3441HG1050AD05 IRU BOEING737 7374B7 1384702NM E/E BAY FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19433US 24555 EWR - FLT 1132 - AFTER TAKEOFF, CREW OBSERVED THAT THE AIRCRSAFT HAD LOST GYRO AND COMPASS CAPABILITY. AN ATTITUDE FLAG ON THE CAPTAINS SIDE AND FIRST OFFICERS GYRO WAS PRESENT. FLIGHT RETURNED TO FIELD AT EWR AND LANED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REALIGNED THE IRU'S. ALL FLAGS AND SYSTEM CHECK NORMAL. (M) 2L72 4F RTA16WE 20030422001122003042200112SO 2003 4 22 SIMA200307107 120030219A532014521725615 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, SERVICE DOOR FORWARD SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE FORWARD SILL IAW EMB 135 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M) 2L72 4F RTT00011AT 20030422001182003042200118NM 2003 4 22 USAABB03037 120030308A3260MS25237387 BULB BOEING767 7672B7 1385107NM MLG INDICATOR BURNED OUT A USAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 EA19655US 25257 CLT - FLT 95 - ON FINAL APPROACH, WITH GEAR SELECTED DOWN, THE LEFT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE. CREW PERFORMED A TOWER FLY-BY TO VERIFY THAT THE GEAR WAS DOWN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RELAMPED THE GEAR INDICATOR. (M) 2L72 4F RTA1NM 20030422001492003042200149NM 2003 4 22 EIA2003029 120030228A5312 BULKHEAD BOEING747 747132 1384882NM PWA JT9 JT9D3 52050NE FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 CANTED BULKHEAD AT B.S. 1241 RT, CORROSION AT BL0-RBL 5. C/A: REMOVED CORRODED SECTION, REPAIRED ER ECRA 481-53-177-2 AND SRM 53-10-01. INSTALLED DOUBLER PER 747 SRM 51-30-02, PGS 5-9, 38, 57-58. INSTALLED NEW WEB STA 1241-1265 BL4 TO RBL45, IAW SRM 51-30-02 2L74 4F4 F A20WE E20EA 20030423000662003042300066EU 2003 4 23 BAQA085881 120030401A63401179405303 INDICATOR BOLKMS117 BK117A1 5626010EU TRIPLE TACH STICKS H BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME79 7243 TRIPLE TACH INDICATOR, STICKS AT 30 PERCENT UNTIL YOU TAP GLASS AND WILL CLIMB 30 PERCENT IN FLIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030423001082003042300108EU 2003 4 23 ILPA048F 120030124A5312S258FN3231 PRESSURE PANEL BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE7313R 01518WP FUSELAGE CRACKED E ILPAK NONE O OTHER ININSP/MAINT 1 CE03120JC6951 NA0247 DURING ROUTINE INSPECTION OF THE RIVETS AT THE FORWARD PRESSURE BULKHEAD, TWO SEPERATE CRACKS WERE NOTED IN THE LT DISHPAN JUST FORWARD OF THE PILOTS RUDDER PEDALS. THE CRACKS WERE BETWEEN FASTENERS. THE PN S25-8FN323-1 WAS REMOVED & REPLACED IN ACCORDANCE WITH THE AIRCRAFT STRUCTURAL REPAIR MANUAL (SRM) AND CHAPTER 51-20-41. FAA FORM 337 COMPLETED 1/24/03. NO FURTHER DEFECTS TO LIKE COMPONENTS WAS NOTED. 2L72 4F4 F A3EU E6WE 20030424000382003042400038NM 2003 4 24 QXEA0300340 120030308A5320 DOUBLER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - VHF NR 3 ANTENNA MOUNT DOUBLER HAS CORROSION AROUND MOUNT BOLT HOLES. REPAIRED IAW HORIZON AIR EA 6-53-208. 2H72 4T RTA13NM 20030424000662003042400066NM 2003 4 24 IU62003F00001 120030204A2913624022 ADAPTER BOEING737 737* NM HYD PUMP ERODED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 EROSION AROUND STROKING PISTON PORT, FLUID FLOW. STEEL SLEEVE PORT OR ALTERNATE SEAL. (BS1, NR 174248) 2L72 4F RTA16WE 20030424000772003042400077NE 2003 4 24 HXSD0000434 220030211A73200292928540 HMU SNIAS 350 AS350B3 8680954EU TMECA ARRIUSARRIUS2B1 NE ENGINE LEAKING B HXSDO OTHER K FLUID LOSS NRNOT REPORTED 1 AL05403AE 3281 REMOVED HMU / SN 504B DUE TO UNIT LEAKING OUT OF LIMITS. UNIT IS LEAKING BETWEEN HIGH VOLUME PUMP AND HMU BODY. WILL INSTALL SAME UNIT WHEN COMPLETE. RETURNING UNIT TO MFG. FOR REPAIR. 1G71 3U3 U H9EU E34NE 20030417001662003041700166NE 2003 4 17 QXEA0300247 220030210A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX1981 10041 GEE965300 NR 2 ENGINE FAILED SCHEDULED BORESCOPE. FOUND ONE BLADE MISSING FROM HP TURBINE. REPLACED ENGINE. AIRCRAFT OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER(GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030417001772003041700177NM 2003 4 17 MWEA030058 120030208A4930 FUEL CONTROL DOUG MD88 MD88 3023688NM APU FAILED A MWEAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL31601ME 49762 APU FALLS OFF LINE IN FLIGHT. REPLACED APU FUEL CONTROL. 2L72 4F RTA6WE 20030417001862003041700186NM 2003 4 17 F3LA200300044 120030128A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED HAT SECTION BETWEEN STA 328 AND STA 344, RBL 12, CORRODED. FABRICATED AND INSTALLED REPLACEMENT PART PER SRM 51-40-02 AND BAC DRAWING 65C34429. 2L72 4F RTA16WE 20030417001942003041700194NM 2003 4 17 P5CA0300759 120030203A5315 FLOORBEAM BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LEVEL 1 CORROSION FOUND ON FLOORBEAM STA 1800 LBL/RBL-5/WL 208. ACCOMPLISHED WORK PER SRM 51-40-03 FIG 3. 2L74 4F A20WE 20030422000302003042200030NM 2003 4 22 AMTA200300330 120030309A7603 CONTROL BOX BOEING757 75723N 1384973NM THROTTLE OUT OF POSITION A AMTAK NONE O OTHER ININSP/MAINT 1 GL11520AT 27976 UPON TAXIING TO GATE AT ENGINE START LEFT ENGINE GOES INSTANTLY TO TAKEOFF POWER. REPOSITIONED THROTTLE LOWER CONTROL BOX WITH FFG. (M) 2L72 4F RTA2NM 20030422000492003042200049EA 2003 4 22 ASOA03107 120030313A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING A C-CHECK INSPECTION IN MCN, THE LEFT AND RIGHT FRAMES FS 718 BETWEEN STRINGERS 10 TO 12 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING LEFT AND RIGHT FRAMES FS 718 BETWEEN STRINGERS 10 TO 12 IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20030422000762003042200076SO 2003 4 22 SIMA200305012 120030125A532014522461011 DOUBLER EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 DURING IMBV INSPECTION, A LEVEL 2 FINDING WAS FOUND. CORROSION ON DIAMOND DOUBLER ON RIGHT HAT BEAM AT FRAME 22. INSTALLED SERVICEABLE DIAMOND DOUBLER IAW EMB 145 SRM 51-20-01, 51-20-03 AND 51-40-02, 51-40-04, 51-40-06. (M) 2L72 4T RTT00011AT 20030422000892003042200089SO 2003 4 22 SIMA200307101 120030217A532014522459003 SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, GALLEY CENTER RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB 135 SRM 51-20-03 AND 51-40-02. (M) 2L72 4F RTT00011AT 20030422001062003042200106NM 2003 4 22 USAASB03029 120030222A335020131A BATTERY PACK BOEING737 7373B7 1384580NM AFT CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19524AU 23859 IND - MAINTENANCE REPORTED THE CABIN EMERGENCY LIGHT AT THE AFT RIGHT SERVICE DOOR WAS DIM. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030422001302003042200130SO 2003 4 22 SWIA200311820 120030301A27503472001001 FCU EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07271YV3035 1144 120271 ON TAXI OUT, UPON SELECTING FLAPS 15 RECEIVED A CONTROL FAULT. INSTALLED SERVICEABLE FLAP SELECTOR AND FLAP CONTROL UNIT. GROUND OPS CHECK GOOD. P/N: 120-64207-615, S/N OFF: 148978-304, S/N ON: 120237. 2L72 4T RTA31SO 20030422001482003042200148WP 2003 4 22 EIA2003050 120030305A5330 SKIN DOUG DC9 DC933F 302207AWP PWA JT8 JT8D9 52048NE FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09944F 47194 SKIN DENT AND LONGERONS BENT STA NR 275 TO 294 LONGERONS 20 AND 21 RIGHT. CUTOUT DAMAGED SKIN AREA AT BS 275 BETWEEN LONGERONS 20-22 REPAIRED IAW SRM 53-04 PG 42-44, 60BV, 60BU, 60RT, AND 60CK. CUTOUT DAMAGE LONGERON AREA 20R AT BS267-285 AND LONGERON 21 AT B/S 281-285 AND REPAIRED IAW SRM 53-02 PG 48-53 AND ECRA 944-53-162-2. REPETIVE INSPECTIONS TRANSFERED TO EIA COI 004 2L72 4F4 F A6WE E2EA 20030423000672003042300067NE 2003 4 23 BAQA085865 220030331A7310430167601 MANIFOLD BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101750C1 41560NE FUEL SYSTEM CRACKED E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03911WJ567 7050 CRACKED AND LEAKING FUEL AT 10 DEGREE CLOCK NOZZLE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030423001542003042300154NM 2003 4 23 UPS03240280 120030219A5315 FLOORBEAM BOEING727 727108C 1384039NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 344 RBL 24.75 TO 24.75 LBL. CORROSION REMOVED IAW SRM 51-10-6 DEPTH OF BLEND-OUTS MEASURED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01 IN SEVERAL AREAS. FLOORBEAM TOP CHORD REPLACED IAW BOEING DRAWING 65-16316 WITH REF TO SRM 53-10-2 & 51-30-2. 2L73 4F A3WE 20030423001842003042300184NM 2003 4 23 VNAA0303015 120030312A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL07434JS16496252 3051 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 4 TO 6 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030423002032003042300203EU 2003 4 23 QKP2003F00000 120030204A3213SP4YA3 PIN JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MLG STRUT DAMAGED B QKPRO OTHER O OTHER NRNOT REPORTED 1 SO05570HK5445 41089 PIN, (PN SP4YA3), FAILED. VALVE (PN AIR135568) UNSCREWED AND DAMAGED INTERNALS OF MAIN LANDING GEAR SHOCK STRUT (PN AIR83090-2). ACCESS HOLE FOR PIN IS TOO LARGE. 2L72 4T3 TRTA41NM E2WE 20030423002072003042300207NM 2003 4 23 UPS03240307 120030218A5753 ATTACH FITTING BOEING727 727108C 1384039NM NR 2 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, ON INSPECTION OF NR 2 FLAP TRACK CORROSION FOUND ON FWD MOUNT LUG FACES A, B, C & D AND IN FWD LUG BOREHOLES A & B. REPAIR CARRIED OUT IAW SRMO EO'S 2003-008-001 & SMRO 2003-008-014. UPS ENGINEERING FILE NR 727-57-20096. 2L73 4F A3WE 20030424000592003042400059EA 2003 4 24 JBXA03001 120030319A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A JBXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING DEDESCENT 1 SO05592ML 7410 FLT 5135 DCA - BNA. AT START OF DESCENT HAD 14TH STAGE DUCT FAIL MSG ON EICAS. PERFORMED EMER 6-4 CHECKLIST, SHUTDOWN NR 1 ENG AND DIVERTED TO TYS. INSPECTED L 14TH STAGE BLEED AIR DUCT SYSTEM. NO LOOSE CONNECTIONS OR EVIDENCE OF ANY LEAKS NOTED IAW MM 36-12-04. PERFORMED TEST OF BLEED AIR SYSTEM IAW MM 36-21-00. SYSTEM TESTED GOOD. GROUND RAN ENGINES WITH CREW, NO ABNORMAL INDICATIONS NOTED. 2L72 4F RTA21EA 20030424000712003042400071EU 2003 4 24 VJ32003F00023 120030303A2910120A5748 LINE GROB 120 G120A 1660208EU LYC O540 AEIO540D4D5 EA HYD SYSTEM WORN B VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP07864AF592 85004 HYDRAULIC LINE WAS FOUND TO HAVE A HOLE WORN IN IT, DURING REGULAR INSPECTION EVENT. THE CAUSE OF THE WEAR AND HOLE WAS FOUND TO BE A BOLT ON THE LANDING GEAR WEARING ON IT DURING EACH EXTENSION/ RETRACTION CYCLE. THIS LINE SUPPLIED HYDRAULIC PRESSURE TO THE UPLOCK ASSEMBLY FOR THE LANDING GEAR. LINE WAS REPLACED AND PROPER CLEARANCE WAS PROVIDED FOR THE NEW LINE. SUGGEST RELOCATING LINE OR REPOSITIONING UPLOCK ASSEMBLY. 1L71 3O3 ORTA49CE 1E4 20030424000742003042400074NM 2003 4 24 UPS03440335 120030308A5310 DOOR FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C L4, DOOR FWD LOWER CORNER CRACK FOUND AT VERTICAL RADIUS AS MARKED. LWR CORNER REPAIRED AS PER SRM 52-10-02 FIG 10. 2L74 4F RTA20WE 20030424000882003042400088 2003 4 24 GLBA2003034 420030315A34216224565001 GYRO BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAO OTHER O OTHER CRCRUISE 1 NM03240GL2332 UE240 NR 2 EADI ROLL ANNUNCIATE. REMOVED AND REPLACED VERT GYRO, OPS CHECK GOOD. 2L72 4T RTA24CE 20030424001142003042400114NM 2003 4 24 F3LA200300111 120030228A5320 SUPPORT ANGLE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED LATERAL SUPPORT ANGLE CRACKED IN FWD ENTRY AREA, STA. 312, LBL 59, WL 215. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-20-02, 51-20-01, 51-30-01, FIG. 3, AND 51-10-2, PARA. 7. 2L72 4F RTA16WE 20030424001222003042400122NM 2003 4 24 UPS03440345 120030304A5320 FLOOR SUPPORT BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C U/D - FLOOR SUPPORT FOUND HEAVY CORROSION. FLOOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. (DEPTH 0.060 INCH, WIDTH 1 INCH, LENGTH 2 INCH). 2L74 4F RTA20WE 20030424001302003042400130WP 2003 4 24 UPS03840353 120030309A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, FUSELAGE SKIN EXTERNAL MATING SURFACE FOR MARKER BEACON ANTENNA HAS CORROSION STA 660-680 LONG 35L TO 36. REMOVED CORROSION, NDT VERIFIED CORROSION. REMOVED IN AREA, FABRICATED AND INSTALLED DOUBLER IAW SAA SK 880-356. 2L74 4F RT4A25 20030424001342003042400134WP 2003 4 24 UPS03840357 120030325A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK PER UPS MM 33-50-00. 2L74 4F RT4A25 20030424001422003042400142NM 2003 4 24 QXEA0300371 120030313A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 TOP WING TO FUSELAGE AFT APERTURE FOR PANEL 261CT IS CHAFED. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030424001472003042400147EA 2003 4 24 QXEA0300349 120030227A5710 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 CKB - RIGHT HAND WING CRACK FOUND ON STRUCTURE UNDER INBOARD FLIGHT SPOILER. REPAIRED IAW RD 670-57-51-00-4 AND HORIZON AIR EA R-53-77. 2L72 4F RTA21EA 20030424001582003042400158SO 2003 4 24 LR7A03013 120030313A572034862714L STIFFENER LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5711 FOUND LT WING FLAP WELL BULKHEAD WEB BRACE/ STIFFENER CRACKED AT OWS 241. REPLACED STIFFENER IAW SRM SMP 583 51-60 AND 51-70. NR 2033. 2H74 4T A1SO 20030422001542003042200154EU 2003 4 22 MALA030192 120030310A2497 WIRE SAAB SF340 340B 7860101EU STARTER GEN BROKEN A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15434XJ 340B434 DURING FLIGHT 3161, RT MAIN DC GEN FAILED INFLIGHT. CREW ATTEMPTED RESET PER QRH AND 2ND TIME PR MXC BUT GEN WOULD NOT COME BACK ONLINE. AIR RETURN TO DTW. MAINTENANCE UPON INSPECTION FOUND BROKEN WIRE AT RT START/GEN, REPAIRED WIRE AND ALL CHECKS GOOD. 2L72 4T RTA52EU 20030423000022003042300002NM 2003 4 23 S03425013 120030312A2530267100 CHILLER BOEING747 747400 NM PWA 4056 PW4056 NE GALLEY 8 SMOKE W SAJFO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP03 24312 B-18275 IN FLT GALLEY UNIT 8 UPPER CELLING FOUND AIR LEAK AND SMOKE. CK ALL GALLEY 8 EQUIPMENTS FOUND AIR LEAK AND SMOKE CAME FROM CHILLER.CHILLER RPLD AND ALL GALLEY 8 EQUIPMENTS FUNCTION CHECKED NORMAL. 2L74 4F4 FRTA20WE E24NE 20030423000132003042300013NM 2003 4 23 EVAS092009 120030331A5330 SKIN BOEING747 74745E 1384947NM FUSELAGE DENTED W QOCFK NONE L NO TEST ININSP/MAINT 1 WP0316405 27142 DURING D02 CHECK FOUND A DENT IN THE LOWER EXTERIOR SURFACE OF FUSELAGE SKIN OF STA 528 STRINGER S-45L.DENT DIMENSION WAS 3"X1"X0.114".REFORM THE DENT IN SKIN WITH STANDARD PRACTICE.FABRICATE A REIN FORCED INNER DOUBLER FROM TI-6A1-4V 8.75"X5.25"X0.04".INSTALL REPAIR DOUBLER WITH BMS 5-95. 2L74 4F RTA20WE 20030423001132003042300113NM 2003 4 23 F3LA200300087 120030220A5320 SILL BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, FIG. 1, SHEET 4, DETAIL I. REPLACED SILL PER SRM 51-10-2 AND SRM 51-30-02. 2L72 4U RTA16WE 20030423001182003042300118CE 2003 4 23 GLBA2003025 120030227A3610 TUBE BEECH 1900 1900D 1154162CE RT BLEED AIR DISCONNECTED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03204GL UE204 RIGHT BLEED AIR FAIL. RECONNECTED EVA TUBING ON LT INBOARD WING, OPS CHECK GOOD. 2L72 4T RTA24CE 20030423001352003042300135EA 2003 4 23 QXEA0300338 120030312A2611 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA LAV SMOKE ACTIVATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09601QX 10009 BOI - FLIGHT 2528 - AIRCREW RETURNED TO FIELD WHEN AFTER TAKEOFF THE AFT LAVATORY SMOKE DETECTOR SOUNDED. AIRCRAFT CURRENTLY DOWN FOR TROUBLESHOOTING AND MAINTENANCE. 2L72 4F RTA21EA 20030423001632003042300163CE 2003 4 23 GLBA2003033 120030315A24371143800311 METER BEECH 1900 1900D 1154162CE DC SYSTEM INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03226GL60 UE226 RT DC LOAD METER INOP. REMOVED AND REPLACED RT DC LOAD METER. 2L72 4T RTA24CE 20030423001642003042300164CE 2003 4 23 GLBA2003032 120030313A5270 SWITCH BEECH 1900 1900D 1154162CE CARGO DOOR OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03195GL UE195 CARGO DOOR ANNUN ILLUMINATED. ADJUSTED DOOR JAMB SWITCH, OPS CHECK GOOD. 2L72 4T RTA24CE 20030423001782003042300178NM 2003 4 23 VNAA0303018 120030315A2611 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE SMOKE DETECTOR FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07462PS 3084 THE CREW REPORTED A LAV SMOKE CAS MESSAGE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE LAV DETECTOR CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030424000152003042400015NM 2003 4 24 QXEA0300382 120030307A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM ZONE 800 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX- AFT BAGGAGE FLUSH HANDLE LATCH ASSEMBLY IS WORN. REPAIRED IAW DHC-8 Q400 TASK 52-31-01-300-802. 2H72 4T RTA13NM 20030424000402003042400040NM 2003 4 24 QXEA0300342 120030308A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CHAFING ON PANEL ATTACH FLANGE OF PANEL 261FT, AFT FLANGE, BETWEEN CAMLOCK HOLES 1-6. REPAIRED IAW RD 8/4-57-144. 2H72 4T RTA13NM 20030424000532003042400053NM 2003 4 24 QXEA0300328 120030304A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - LEFT HAND AFT FUSELAGE SKIN NICKED AFT OF BAGGAGE DOOR, AFT OF X798 AT STRINGER 17. REPAIRED IAW DHC-8 400 SRM 51-25-02. 2H72 4T RTA13NM 20030424000802003042400080WP 2003 4 24 ZW0A0303303 120030322A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BURNED OUT A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139677W 53627 THE EMERGENCY CEILING LIGHT WAS INOPERATIVE AT ROW 26. REPLACED THE LAMP P/N 7732. CHECK-C 10-05-2002. 2L72 4F RTA6WE 20030424000892003042400089NM 2003 4 24 F3LA200300107 120030228A5320 STRAP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED STABILIZER STRAP CRACKED IN MAIN CABIN AT STA. 312, RBL 45, WL 200. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-51, FIG. 204, SRM 51-30-1, FIG. 3, SRM 51-10-2, PARA. 7, AND SRM 51-20-1. 2L72 4F RTA16WE 20030424001452003042400145NM 2003 4 24 QXEA0300373 120030313A5320 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - TOP WING TO FUSELAGE AFT APERTURE FOR PANEL 261FT IS CHAFED. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030424001712003042400171SO 2003 4 24 LR7A03026 120030313A5320 ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5324 FOUND RT MLG WHEEL WELL CHINE ANGLE CRACKED AT FS 617, RBL 61, WL 180. REPAIRED IAW SRM SMP 583 53-40-27. NR 2167. 2H74 4T A1SO 20030424001882003042400188WP 2003 4 24 MWEA030147 120030328A5524993780433 ACCESS PANEL DOUG DC9 DC981 3022081WP RT ELEVATOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RIGHT ELEVATOR UPPER ACCESS PANEL 3632 DOUBLER DAMAGED AT INBOARD SCREW HOLE. FABRICATED AND INSTALLED DOUBLER AND FILLER AND BALANCED ELEVATOR. 2L72 4F A6WE 20030424001982003042400198EA 2003 4 24 SWIA200311849 120030322A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07595SW 7292 DURING APPROACH INTO SLC RECEIVED A FLAPS FAIL MESSAGE WITH FLAPS AT 20 DEGREES. RAN QRH PROCEDURE AND LANDED WITHOUT INCIDENT. FOUND LEFT BPSU TO BE JUMPY (TURNED SEVERAL TIMES WITH NO CHANGE IN POSITION). REMOVED AND REPLACED LEFT BPSU IAW 27-51-10 AND CHECKED LEFT AND RIGHT FLAP RIGGING IAW MM 27-54-00. P/N: 855D100-9, S/N OFF: 1530B, S/N ON: 1294B. 2L72 4F RTA21EA 20030424001992003042400199 2003 4 24 SWIA200311850 420030322A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07234SW6760 6760 120308 AUTOPILOT AND CAPTAIN'S FLIGHT DIRECTOR PITCHES UP AND DOWN 300 FT PRIOR TO LEVEL OFF. REPLACED AUTOPILOT COMPUTER APC-65B WITH SERVICEABLE UNIT. TESTED AND OPS CHECK GOOD. 2L72 4T RTA31SO 20030424002042003042400204WP 2003 4 24 UPS03840364 120030325A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, INSIDE 60 PANEL STA 1766 AFT SIDE SHEAR TIE ABOVE LONG 9R IS CRACKED. CUT OFF CRACKED SHEAR TIE, FABRICATED SHEAR TIE AND INSTALLED IAW SRM 53-2-0 FIG 2A. 2L74 4F RT4A25 20030424002112003042400211WP 2003 4 24 UPS03840372 120030307A5313 STRINGER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, STRINGER NR 59 HAS CRACK ABOUT 3 INCHES LONG XRS 408.000 505B 4 ALT. REMOVED AND REPLACED STRINGER END FITTING IAW DC8 SRM 51-1-20D AND 51- 3-0 & 51-1-23. LOCATED AND DRILLED AND DEBURRED FITTING (P/N 5644973- 502). 2L74 4F RT4A25 20030425000132003042500013EU 2003 4 25 MALA030208 120030325A3222 BEARING SAAB SF340 340B 7860101EU NLG WHEEL FAILED A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15448XJ 340B448 DURING TAXI ON FLIGHT 3178, EXPERIENCED BEARING FAILURE ON NOSE WHEELS. NOSE TIRES FLAT ON LANDING. MAINTENANCE REMOVED AND REPLACED AXLES, AXLE ADAPTER, BOTH TORQUE LINKS AND BOTH NOSE TIRES SEE CONTINUATION CARDS 062267, 018454, 018447 AND 018503 AND TASK CARDS 3240-303 FOR DETAILS. 2L72 4T RTA52EU 20030425000262003042500026 2003 4 25 SWIA200311855 420030324A2210 CIRCUIT CARD CNDAIRCL600 CL6002B19 1900309EA AUTOFLIGHT FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07905SW 7437 ON DESCENT TO FINAL APPROACH RECEIVED AN AP PITCH TRIM CAUTION MESSAGE. RAN QRH, HEAVY NOSE DOWN WHEN DISCONNECTED. REENGAGED, AP MESSAGE WENT AWAY AFTER RE-TRIMMING. MESSAGE CAME BACK ON SHORT FINAL. REINITIALIZED FCC CARD NR 1 AND FCC CARD NR 2. OPS CHECKED NORMAL. PERFORMED OPERATIONAL CHECK OF AUTOPILOT TRIM SYSTEM. CHECKED NORMAL. 2L72 4F RTA21EA 20030425000302003042500030EU 2003 4 25 RAIAOO3O3O76 120030315A3260OL8562BPEGPL BULB JETAIRJETSTMJETSTM4101 1500501EU MLG INDICATOR BURNED OUT A RAIAO OTHER P NO WARNING INDICATION LDLANDING 1 CE03553HK 41066 NOSE LANDING GEAR DOWN INDICATION DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED, EMERGENCY LANDING. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOWN INDICATOR LIGHT BULB, OPS CK OK. 2L72 4T RTA41NM 20030425000342003042500034NE 2003 4 25 RAIA00303080 220030319A726131041793 TUBE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE ENG OIL PRESSURECRACKED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03554HK 41067 76105 SFM- RIGHT ENGINE OIL PRESSURE DROPPED WITH WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED CRACKED TURBINE OIL PRESSURE TUBE, LEAK AND OPS CK OK. 2L72 4T4 TRTA41NM E18NE 20030425000462003042500046NM 2003 4 25 UPS03440394 120030304A5312 BULKHEAD BOEING747 747200 1384847NM RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, RT WING MLG WW - BS 1241 WING CENTER SECTION REAR SPAR PRESSURE BULKHEAD WEB SURFACE FOUND CORROSION AT RBL 1 TO RBL 6 BRACKET ATT SURFACE. CORROSION BLEND OUT (0.070 X 2 X 8 INCH) NOT WITHIN SRM 57-10-01 LIMITS FOR REPAIR REFFER RS NR R53-43-34986 & UPS EA 747-53-20125. 2L74 4F RTA20WE 20030425000502003042500050WP 2003 4 25 UPS03840392 120030304A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, LOWER RT SECTION FLOORBEAM CORRODED AT STA 879 BL60R WL 10. REMOVED AND FAB NEW SECTION OF FLOORBEAM IAW TIMCO REO G09098. ALODINED AND PRIMED BEAM IAW DC8 SRM 51-1-8. FAB 4 EA CLIPS IAW DAC DWG 5645332. ALODINED AND PRIMED CLIPS IAW DC8 SRM 51-1-8. INSTALLED CLIPS IAW DC8 SRM 51- 1-20D. FAB 4 SPLICE ANGLES IAW TIMCO REO G09098. ALODINED, PRIMED AND INSTALLED ANGLES IAW DC8 SRM 51-1-8 & TIMCO REO G09098. 2L74 4F RT4A25 20030425000622003042500062 2003 4 25 SWIA200311859 420030323A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07924SW1143 1143 7681 STALL FAIL CAUTION AFTER TAKEOFF. WENT AWAY THEN CAME BACK SEVERAL TIMES. REMOVED AND REPLACED STALL COMPUTER. PERFORMED PITOT/STATIC SYSTEM PURGE AND STALL WARNING SYSTEM FUNCTIONAL TEST PER MM 27-35-00. ALL TESTS GOOD. 2L72 4F RTA21EA 20030425000632003042500063EA 2003 4 25 SWIA200311860 120030325A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 1 SPOILER MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07433SW5242 4483 7550 SPOILERONS FAULT STATUS MESSAGE UNABLE TO CLEAR. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW CRJ MM 27-60-01. OPS AND LEAK CHECK GOOD. UPDATE 3/27/03: SPOILERONS FAULT MESSAGE DISPLAYED NON ED-2. REMOVED AND REPLACED NR 1 SECU. OPS CHECK GOOD IAW CRJ MM 27-60-00. 2L72 4F RTA21EA 20030425000672003042500067CE 2003 4 25 WVE2003F00005 120030301A3260426EN98 SQUAT SWITCH LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE MLG DEFECTIVE B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09233FX 154 WHEN DEPARTING, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED AND UPON INSPECTION, MAINTENANCE FOUND LT AND RT MLG STRUTS TO BE SERVICED UNEVEN, AND ROLLER ON RT MLG SQUAT SWITCH WORN. AIRCRAFT WAS JACKED STRUTS WERE SERVICED AND RT MLG SQUAT SWITCH REMOVED AND REPLACED. GEAR RETRACTED SATISFACTORY. DEFECTIVE SQUAT SWITCH. MANUFACTURE EVALUATION. 2L72 4F4 FRTA10CE E35NE 20030425000722003042500072EU 2003 4 25 MALA030213 120030328A302044730501 CONTROL MODULE SAAB SF340 340B 7860101EU DE ICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15454XJ 340B454 INFLIGHT ON FLIGHT 3192, LT INTAKE HEAT CYCLED ON AND OFF. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED DE-ICE CONTROL MODULE P/N 44730-501, SN/OFF L238375, SN/ON A00181. 2L72 4T RTA52EU 20030425000742003042500074EU 2003 4 25 MALA030218 120030401A335010126201 LIGHT BAC 146 AVRO146RJ85A1500097EU CABIN INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15507XJ E2316 ON FLIGHT NR 3461, LOWER FACE PLACE OVER EXIT SIGN IN MAIN CABIN DOOR MISSING. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSEMBLY P/N 10-1262-01. ALL CHECKS GOOD. 2H74 4F RTA49EU 20030423001402003042300140EU 2003 4 23 WTX2003F00000 120030212A2497SN239 PLUG AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP STARTER GEN MELTED E WTXAO OTHER O OTHER NRNOT REPORTED 1 NM0789EC 7390 109 PILOT REPORTED NR 1 ENGINE WOULD NOT START DUE TO LACK OF STARTER ROTATION. TRACED PROBLEM TO MELTED STARTER/GENERATOR PYLON FEED THROUGH PLUG. OUTBOARD TERMINAL END OF PLUG AND TERMINAL END OF CABLE HAD MELTED. IAW SNL AND MM. (PTRS SW15200305957) 3456. 2L72 4F4 F A33EU E6WE 20030424000902003042400090NM 2003 4 24 F3LA200300108 120030228A5320 SUPPORT ANGLE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED FLOOR SUPPORT ANGLE CRACKED FROM STA. 380 TO STA. 400, BL O, WL 208. FABRICATED AND REPLACED ANGLE PER SRM 51-10-02, 53-30-01, 53-30-51, FIG. 1, AND 51-20-01. 2L72 4F RTA16WE 20030424000992003042400099EA 2003 4 24 SWIA200311840 120030320A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07915SW 7615 FLAP FAIL MESSAGE - PERFORMED NO FLAP LANDING. COMPLIED WITH OPS CHECK OF FLAP SYSTEM. CHECKED FECU, NO FAULTS FOUND. OPERATED FLAPS, ALL OPS CHECKS GOOD IAW CRJ MM 27-51-00. 2L72 4F RTA21EA 20030424001062003042400106WP 2003 4 24 MWEA030145 120030326A5347593056671 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 NR 1 SEAT TRACK CORRODED INBOARD OF AFT SERVICE DOOR BY NUT PLATES. LOCATED, DRILLED AND INSTALLED TRACK SECTION. 2L72 4F A6WE 20030424001102003042400110WP 2003 4 24 IXXA0300027O 120030319A2752 FITTING DOUG DC8 DC871F 302199DWP TE FLAP DAMAGED A IXXAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 SW11830BX744941254 45973 ON APPROACH TO BFI CREW RECEIVED A FLAP SPLIT INDICATION ALONG WITH A AIRCRAFT ROLL TO THE LT. CREW RAISED FLAPS AND DIVERTED TO PDX. MAINTENANCE INSPECTION AND REPAIR IS IN PROGRESS. ADDITIONAL INFORMATION WILL BE PROVIDED AS IT BECOMES AVAILABLE. MAINTENANCE FOUND A BROKEN EYE LOBE AND NUT BOLT TO ACTUATOR FLAP LINK MISSING. THE FLAP LINK RT AT STATION 98 WAS BROKEN. MAINTENANCE REPLACED FLAP LINK AND REMOVED AND REPLACED ACUATOR AT STATION 98 IN ACCORDANCE WITH DOUGLAS AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030424001162003042400116SW 2003 4 24 YT2R727265 120030207A7931222060096103 SWITCH BELL 230 230 1182149SW OIL PRESSURE LEAKING B YT2RO OTHER K FLUID LOSS NRNOT REPORTED 1 WP01230SL 23009 ENGINE OIL PRESSURE SWITCH LEAKING. 1G72 3U NCH9SW 20030424001172003042400117SW 2003 4 24 YT2R727264 120030207A73327G1056 SWITCH BELL 230 230 1182149SW OIL PRESSURE INOPERATIVE B YT2RO OTHER O OTHER NRNOT REPORTED 1 WP01230SL 23009 PRESSURE SWITCH SLOWED TO SHUTOFF CAUTION LIGHT. 1G72 3U NCH9SW 20030424001202003042400120NM 2003 4 24 UPS03440343 120030307A5310 FAILSAFE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, RIGHT BS 2231 2 EA FASTENER HOLE CRACK REVEALED ON STRAP BELOW STR 25R REFER FIGURE ATTACHED. M/D - RIGHT BS 2231 STR 25 REVEAL PANEL STRAP REPAIRED AS PER SRM 53-10-04 FIG 115. 2L74 4F RTA20WE 20030424001262003042400126WP 2003 4 24 UPS03840349 120030305A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C2, 1 EA FASTENER PULLED THRU STRAP ON INTERCOSTAL AT STA 1135 LT SIDE AT LONG 35L. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 23. 2L74 4F RT4A25 20030424001432003042400143NM 2003 4 24 QXEA0300368 120030314A5720 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 LEFT HAND WING FORM BRACKET CRACKED (NACELLE TO WING UPPER SHROUD SUPPORT). REPAIRED IAW HORIZON AIR EA 6-54-214. 2H72 4T RTA13NM 20030424001532003042400153 2003 4 24 U30A200300010 420030323A3460B398BAM0208 COMPUTER AIRBUS320 A320212 3930322EU ZONE 127/128 FAULTY A U30AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA17265AV 427 AFTER FLT 306 BWI-CUN, IN CUN AT GATE, THE NR 1 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) FAILED. DEFERRED PER MEL 22-83-01. IN BWI ON 3/25/03, RESET NR 1 FMGC IAW AMM AFS OPER TEST 22-96-00-710-001 AND SYSTEM OPS CHECKED OK. ON 3/25/03, NR 1 FMGC FAILED AGAIN. SWAPPED NR 1 & 2 FMGC'S AND OPS CHECKED BOTH FMGC NR 1 & 2 OK. C/W RVSM RETURN TO SERVICE REQUIREMENTS. ON 3/26/2003, FMGC NR 2 FAILED. REMOVED AND REPLACED NR 2 FMGC IAW 22-83-34-400-001 AND OPS CK'D OK. C/W RVSM RETURN TO SERVICE REQUIREMENTS. 2L72 4F RTA28NM 20030424001602003042400160SO 2003 4 24 LR7A03015 120030313A5310 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB HC5324 FOUND RT MLG WHEEL WELL BOW BEAM CRACKED AT FS 557, RBL 61, WL 200. REPAIRED IAW SRM SMP 583 53-40-14. NR 2076. 2H74 4T A1SO 20030424001612003042400161SO 2003 4 24 LR7A03016 120030313A5320 ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WL 140 CHINE ANGLE CRACKED AT FS 520, LBL 61. REPAIR IAW SRM SMP 583 53-40-27. NR 2079. 2H74 4T A1SO 20030424001742003042400174SO 2003 4 24 LR7A03029 120030313A5320 SUPPORT FITTING LKHEED382 382G 526414USO FUSELAGE BROKEN A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND RT AFT SLOPING LONGERON FS 1041 SUPPORT FITTING CRACKED AT RBL 61, WL 190. FITTING REPLACED IAW SRM SMP 583 51-10 PG 4. NR 2227. 2H74 4T A1SO 20030424001772003042400177SO 2003 4 24 LR7A03032 120030313A5522 STRAP LKHEED382 382G 526414USO ELEVATOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST2708 FOUND RT ELEVATOR LOWER SKIN INNER STRAP CRACKED AT HSS 68 & 75. REPAIRED IAW LAC MEA 382-55-03-013. NR 2246. 2H74 4T A1SO 20030424001782003042400178SO 2003 4 24 LR7A03033 120030313A5312 PRESSURE PANEL LKHEED382 382G 526414USO LT MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL WEB CRACKED AT FS 585 LBL 61, WL 180. REPAIRED IAW LAC MEA 382-53-03-014. NR 2263. 2H74 4T A1SO 20030424001832003042400183WP 2003 4 24 ZW0A0303401 120030322A3350408822101 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13953U 49267 THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 12 TO 17, AND FROM ROW 23 AFT INCLUDING IN TAIL COMPARTMENT. REPLACED BATTERIES FOR ROW 12 TO 17, AND RESEATED BATTERIES FOR ROW 23 AFT. CHECK-C 2-18-03 STL. 2L72 4F A6WE 20030423001422003042300142SO 2003 4 23 JIK2003F00000 120030220A55007105603 SPRING PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA EMPENAGE BROKEN E JIKAO OTHER O OTHER NRNOT REPORTED 1 WP013525G677 317952123 ELEVATOR BUNGEE SPRING WAS FOUND BROKEN ON PRE-FLIGHT. TOTAL TIME ON THE SPRING 677 HOURS. THIS SPRING IS REQUIRED TO BE REPLACED EVER 1000 HOURS, TIS, IAW AD. THIS IS FIRST FAILURE OF THE (PN 7105603) SPRING. 1L72 3O3 O A20SO E14EA 20030423001772003042300177NM 2003 4 23 F3LA200300104 120030228A5320 STRAP BOEING737 7373Q8 1384670NM FUSELAGE DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 26293 DURING EXIT CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT STRAP WITH MISSING MATERIAL AT STA. 847, BETWEEN STR. 24-R AND STR. 25-R. FABRICATED AND INSTALLED REPAIR PER SRM 51-70-13, FIG. 1, 51-20-2, 51-30-1, FIG. 3, AND 51-10-2, PAGE 7. 2L72 4F RTA16WE 20030424000212003042400021WP 2003 4 24 UPS03840314 120030303A53403750257U1 FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C2 LONG 31L SPLICE FITTING IS CRACKED AT STA 600-640. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2L74 4F RT4A25 20030424000652003042400065 2003 4 24 MALA030205 420030320A34206227713004 COMPUTER SAAB SF340 340B 7860101EU COCKPIT FAILED A MALAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL15363PX 340B260 DURING FLIGHT 2737, LT DPU C/B POPPED. LEFT SIDE DPU 1 (G-18) CIRCUIT BREAKER OUT, (POPPED) RESET ONCE, AND POPPED AGAIN. RT SIDE HEADING (F/O) DID NOT MATCH MAG COMPASS. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED NR 1 DPU P/N 622-7713-004, SN/ON 6924, SN/OFF 1347. ALL CHECKS GOOD IAW SF340 MM. 2L72 4T RTA52EU 20030424000852003042400085CE 2003 4 24 GLBA2003037 120030324A561010138402518 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03249GL255 UE249 F/O`S WINDSHIELD SHATTERED. REMOVED AND REPLACED WINDSHIELD. 2L72 4T RTA24CE 20030424000862003042400086SO 2003 4 24 VZG2003F00000 120030312A32311159SCH23111 CONTROL VALVE GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU NLGWW INOPERATIVE B VZGRO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW05444GA8987 301 NOSE LANDING GEAR WOULD NOT EXTEND WITH THE LANDING GEAR HANDLE PLACED IN THE DOWN POSITION. TROUBLESHOT LANDING GEAR AND FOUND THE NOSE GEAR DOOR CONTROL VALVE INOPERATIVE NOT ALLOWING THE GEAR DOOR TO OPEN. NOSE GEAR DOORS WOULD OPEN WHEN GROUND HANDLE WAS OPERATED TO OPEN DOORS. (ON JACKS) THE NOSE GEAR WOULD EXTEND. THE DETERMINED CAUSE OF FAILURE OF THE NOSE DOOR CONTROL VALVE IS UNDETERMINED, HOWEVER THE VALVE WILL BE SHIPPED TO MFG AS A CORE FOR POSSIBLE OVERHAUL. 2L72 4F4 F A12EA E2EU 20030424002032003042400203WP 2003 4 24 UPS03840360 120030302A5512565174759 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, LT UPPER HORIZONTAL STAB SKIN IS CRACKED AND CORRODED AREAS MARKED BETWEEN XE 77 TO XE 99.879. REMOVED, FABRICATED AND REPLACED SKIN PANEL ASSY BETWEEN XE 75.672 TO XE149 IAW DWG 5651747, 8110-3 APPROVED SAA SK 880-658, UPS ENGINEERING FILE NUMBER DC8-55-20012 AND SRM 51-1-21. 2L74 4F RT4A25 20030425000412003042500041EU 2003 4 25 RAIA00303087 120030313A733031055016 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03565HK9419 41082 STL- RIGHT ENGINE IEC FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED PT2 SENSOR, OPS CHECK OK. 2L72 4T4 TRTA41NM E18NE 20030425000822003042500082NM 2003 4 25 QXEA0300389 120030320A2720NAS77A813P BUSHING BOMBDRDHC8 DHC8401 1390041NM ZONE 300 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - FORE RUDDER LOWER MAIN HINGE POINT MISSING BUSHING. REPAIRED IAW HORIZON AIR EA 6-55-26. 2H72 4T RTA13NM 20030425000852003042500085NM 2003 4 25 QXEA0300392 120030319A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - FORWARD BAGGAGE DOOR SURROUND SKIN NICKED/GOUGED, 2 INCHES BELOW THRESHOLD. REPAIRED IAW HORIZON AIR EA 6-53-223. 2H72 4T RTA13NM 20030425000972003042500097NM 2003 4 25 KPVA200311 120030227A256010005511 LIGHT DHAV DHC8 DHC8103 1386005NM COCKPIT INOPERATIVE A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13805WP 353 COCKPIT PORTABLE EMERGENCY LIGHT DIM. REMOVED AND REPLACED PORT EMERGENCY EXIT LIGHT ASSEMBLY AND SECURED IN HOLDING ASSEMBLY AND LATCHED. OPS CHECKED GOOD IAW MM. 2H72 4T RTA13NM 20030425001072003042500107NM 2003 4 25 DLM88030214 120030305A3233 ACTUATOR DOUG MD88 MD88 3023688NM NLG FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27905DE EFS17733 53410 AFTER GEAR RETRACTION, NOTICED LOUD VIBRATION. CYCLED LANDING GEAR, VIBRATION CONTINUED, WORSE AT HIGHER AIRSPEED. FOUND RIGHT NOSE GEAR DOOR OPEN. INSPECTED AREA, NO DAMAGE FOUND. REPLACED RIGHT NOSE GEAR DOOR ACTUATOR PER M/M. CHECKS OK. 2L72 4F RTA6WE 20030428000102003042800010WP 2003 4 28 ZW0A0303601 120030327A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13966TW 53616 THE FIRST FOUR EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. RESEATED THE ELECTRICAL CONNECTOR AT ROW 3 AND 4. CHECK-C 6-7-02 STL. 2L72 4F RTA6WE 20030428000112003042800011NM 2003 4 28 ZW0A0303603 120030327A3350 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT LOOSE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139630A 53561 THE FLOOR EGRESS LIGHTS WERE INOPERATIVE FROM ROW 27 TO 30. RESEATED THE ELECTRICAL CONNECTOR AT ROW 30. CHECK-C 3-1-02 STL. 2L72 4F RT 20030428000262003042800026WP 2003 4 28 GTIA030172 120030310A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FLOORBOARD DAMAGED STA 1079-1146 LT. DRILL AND LOCATE. 2L72 4F4 FRTA6WE E2EA 20030424001852003042400185WP 2003 4 24 ZW0A0303402 120030325A3350 BULB DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BURNED OUT A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13920TV 49369 THE EGRESS LIGHT WAS INOPERATIVE AT CABIN ROW 8. RESEATED THE LAMP. CHECK-C 6-16-02 STL. 2L72 4F A6WE 20030422001512003042200151NM 2003 4 22 EIA2003033 120030228A5311UNK FRAME BOEING747 747132 1384882NM PWA JT9 JT9D3 52050NE BULKHEAD CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 LEFT WING GEAR WW AT RT BS 1241, FWD OF BULKHEAD FTG CHORD IS EXFOLIATED IA. REPAIR IAW EO 57-747-1544-99 REV A, PATS 1, 2, AND 4, AND ECRA 481-57-189-2. 2L74 4F4 F A20WE E20EA 20030422001532003042200153EU 2003 4 22 MALA030189 120030309A3230 HOOK SAAB SF340 340B 7860101EU MLG UPLOCK CONTAMINATED A MALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 GL15364PX 340B262 AFTER TAKEOFF ON FLIGHT 2789, GEAR WOULD NOT LOCK IN UP POSITION. HYDRAULIC PUMP CONTINUED TO RUN, NO HYDRAULIC LEAK OBSERVED. REYECLED GEAR TWICE, GEAR FINALLY CAME UP. ALL SPEEDS WERE COMPLETED WITH GEAR EXTENSION AND RETRACTION. AIR RETURN TO MSP. MAINTENANCE DUPLICATED PROBLEM DURING INITIAL GEAR SWINGS. FOUND LT UPLOCK NOT BEING DEPRESSED BY HOOK ENGAGEMENT. SUSPECT MOISTURE IN THE HOOK/ROLLER ASSEMBLY. LUBED UPLOCK, ROLLERS AND ALL PIVOT POINTS. COMPLETED 15 GEAR CYCLES AND PROBLEM DID NOT RETURN IAW SAAB MM 32-30-00. 2L72 4T RTA52EU 20030423000172003042300017NM 2003 4 23 AUS20030297 120030212A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 27L CONTAINED LEVEL 2 CORROSION AT LOCATION BS 1128.FOUND DURING INSPECTION IAW CPCP C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423000592003042300059 2003 4 23 BAQA085891 420030401A2210117884141 COMPUTER BOLKMS117 BK117B1 5626012EU CSAS INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE 7219 YAW CSAS WILL NOT COME ON LINE. 1G72 3U H13EU 20030423000932003042300093EU 2003 4 23 BAQA085901 120030403A2435 BRUSHES AEROSPSA365 SA365N 8680669EU STARTER GEN WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911UF1067 11301225 6338 STARTER GEN HAS BRUSHES AND COMMUTATOR WORN. HARD CARD ENCLOSED (2). REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030423001032003042300103NE 2003 4 23 GLBA2003010 220030120A72611593732 HOSE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE OIL COOLER DAMAGED A GLBAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM03108UX 120108 LEFT ENGINE PRESS FLUCTUATING BELOW 40 PSI. INSTALLED OIL COOLER HOSE, OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030424000322003042400032WP 2003 4 24 ZW0A0303210 120030313A5280 CHANNEL DOUG DC9 DC983 3022083WP MLG DOOR CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13110HM 49787 DURING CHECK-C,. MAINT THE LT MAIN LANDING GEAR FORWARD INBOARD DOOR FRAME CHANNEL WAS CRACKED. REPLACED THE FWD INBOARD MLG DOOR FRAME CHANNEL PER SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F RTA6WE 20030424001252003042400125WP 2003 4 24 UPS03840347 120030305A53105753113501N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, LONGERON 24L HAS A FITTING CORRODED BEYOND LIMITS AT STA 920. REMOVED AND REPLACED FITTING, FABRICATED AND INSTALLED SPLICES, DOUBLERS AND FILLERS IAW SRM 53-2-0 FIG 8 AND DWG 5753113. 2L74 4F RT4A25 20030424001592003042400159SO 2003 4 24 LR7A03014 120030313A5512 SKIN LKHEED382 382G 526414USO HORIZONTAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5511 FOUND LT HORIZONTAL STAB UPPER TRAILING EDGE SKIN CRACKED AT HSS 180 & 210. REPAIRED IAW SRM SMP 583 55-20-06. NR 2038. 2H74 4T A1SO 20030424001892003042400189WP 2003 4 24 MWEA030148 120030328A53219936637 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOOR PANEL AT STATION 1290 BETWEEN LEFT SEAT TRACKS IS CORRODED. REMOVED AND REPLACED FLOORBOARD. 2L72 4F A6WE 20030424001932003042400193EA 2003 4 24 SWIA200311844 120030323A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07435SW 7555 ON APPROACH RECEIVED A NOSE GEAR DISAGREEMENT ON THE EDI. RAN QRH, CLEARED DISAGREEMENT. SWUNG NOSE GEAR IAW MM CHAPTER 32. INSPECTED PROXIMITY SWITCHES. OPS CHECK GOOD. 2L72 4F RTA21EA 20030424001942003042400194EA 2003 4 24 SWIA200311845 120030324A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07431SW 7536 FORWARD OVERHEAD EMERGENCY EXIT SIGN AT ROW 8 DOES NOT ILLUMINATE AND RIGHT OVERWING FORWARD EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED TB105-3 (P/N 600-59211-1). PERFORMED OPS CHECK OF EMERGENCY LIGHTS. OPS CHECK GOOD. 2L72 4F RTA21EA 20030424002052003042400205WP 2003 4 24 UPS03840365 120030301A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, A/C ACCESSORY BETWEEN STA 55 TO 70 BETWEEN LONG 24R TO 25R FRAME 55 IS CRACKED AT SUPPORT ROD. REMOVED FRAME SECTION AT FS 56 L21L-L26L. FAB NEW FRAME SECTION AND SPLINE IAW DC8 SRM 53-2-0. ALODINED AND PRIMED FRAME & SPLICE IAW DC8 SR M 51-1-8. INSTALLED FRAME AND SPLINE IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20030424002092003042400209WP 2003 4 24 UPS03840369 120030310A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C2, FS 1746 L15R-13R CRACKED FUSE SKIN AT VERT FIN CENTER SPAR CANT BLKHD. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR IAW DC8 SRM 53-2-0, ALODINED & PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED REPAIR IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030428000342003042800034WP 2003 4 28 GTIA030179 120030304A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 (SAS B00068 18N00730) FORWARD CABIN STA 160 LBL 9 TO LBL 52 FLOOR SUPPORT CORR. DRILLED AND LOCATED SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030428000432003042800043EA 2003 4 28 SWIA200311863 120030327A2750 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07924SW 7681 FLAPS FAILED DURING APPROACH FOR LANDING AT DEN. LANDED WITHOUT INCIDENT. INSPECTED FLAPS FOR KINKS. NO DEFECTS NOTED. CYCLED POWER. RESET COMPUTER. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030428000532003042800053NM 2003 4 28 OZIA200341004 120030402A5243 HINGE DORNERDO32 DO328300 NM PWA 306 PW306B NE HYD BAY DOOR BROKEN A OZIAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 CE05410Z 7742 3125 PASSING THROUGH 21,000 FT, THE CREW FELT A VIBRATION. SHORTLY AFTERWARDS, THE FLIGHT ATTENDANT REPORTED TO THE CAPTAIN THAT A DOOR WAS OPEN ON THE SIDE OF THE AIRCRAFT. THE CAPTAIN MADE THE DECISION TO RETURN TO TULSA TO DETERMINE THE DAMAGE DONE. 2H72 4T4 FRTA55NM E35NE 20030428000652003042800065EA 2003 4 28 QXEA0300420 120030401A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX-FORWARD CAGE COMPARTMENT CHIMNEY IN FRONT OF DOOR IS TORN. INSTALLED NEW CENTER CHIMNEY IN FORWARD BAGGAGE PIT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030428000692003042800069NM 2003 4 28 QXEA0300423 120030401A5755 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - SHEET METAL DAMAGE AT OPENING FOR INBOARD SPOILER TOGGLE LINK ASSEMBLY. REPAIRED IAW HORIZON AIR EA 6-57-130. 2H72 4T RTA13NM 20030428000752003042800075SO 2003 4 28 C2XA03SH083 120030407A531014530633001 BUTT STRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV-DURING C CHECK LEFT HAND BUTT STRAP BETWEEN FRAMES 23 AND 29 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030428000792003042800079NM 2003 4 28 DHL2003741516 120030322A5311 FRAME BOEING727 7272Q9 138448MNM PWA JT9 JT9D* NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE C-1 DOOR CUT-OUT FWD. FRAME WEB BS 560 CORROSION THRU FASTENERS HOLES OF NR 6 DOOR STOP ALSO AT WEB. C/A: REMOVED PREVIOUS REPAIR C-1 DOOR FWD. FRAME WEB BS 560 FOR CORROSION REMOVAL IAW B-727 SRM 51-30-2. 2) REMOVED LIGHT SURFACE CORROSION FROM WEB WITH A MATERIAL LOSS .002 AND IS WITHIN LIMITS I.A.W. B-727 SRM 53-10-1 FIG. 1. 3) FABRICATED NEW REPAIR DOUBLER DIMENSIONS 10 IN X 4.5 IN USING 7075 T-6 .063 P.O. NR 9911861 IAW B-727 SRM 51-40-2. 4) PREVIOUS DOUBLER CORROSION CLEAN UP OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG. 1. 5) ALODINED AND PRIMED AREA AND DOUBLER IAW B-727 SRM 51-10-2. 6) INSTALLED NEW REPAIR PIECE IAW B-727 SRM 51-40-2 AND 51-30-2. 2L73 4F4 FRTA3WE E20EA 20030428000872003042800087WP 2003 4 28 MWEA030161 120030407A5754993749816 FILLER DOUG DC9 DC981 3022081WP RT WING LE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RIGHT WING LEADING EDGE INTERNAL, CRACK IN MILLED AREA OF INTERNAL LEADING EDGE AT WING STATION XFS112. FABRICATED AND INSTALLED FILLER, INSTALLED FASTENERS. 2L72 4F A6WE 20030428000882003042800088 2003 4 28 MALA030222 420030401A34164309892909 ALTIMETER BAC 146 AVRO146RJ85A1500097EU COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL15521XJ E2346 DURING FLIGHT 3463, F/O'S ALTIMETER FAILED. AIR RETURN TO MEM. MAINTENANCE REPLACED F/O'S ALTIMETER P/N 4309892-909, SN/OFF 98114537, SN/ON 98074455. OPS CHECK GOOD. 2H74 4F RTA49EU 20030428000922003042800092NM 2003 4 28 DHL2003741519 120030325A5315 FLOORBEAM BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING (C) CHECK, FUSELAGE INTERIOR FLOORBEAMS BS 640 AND BS 660 SPLICE PLATE TO MCD LWR. BEAMS ARE CRACKED 2 EACH NDT CONFIRMED.CA: 1) REMOVED FWD. PIT LT UPPER SIDEWALL GILLINER SUPPORTS FROM BS 580 TO 680. REMOVED LWR JAMB WEB ANGLE LWR EDGE FOR WEB REMOVAL AND ANGLES FWD AND AFT OF FLOORBEAMS TO LWR JAMB WEB BS 640-660. REMOVED LWR JAMB WEB FOR ACCESS AND REMOVED CRACKED SPLICE PLATES FROM BS 640 AND 660. FABRICATED TWO EACH SPLICE PLATES USING 7075-T6 125 PO NR 2706118 DIM. 16 INCHES X 6.5 AND AEI STC SA 179850. 5 ALODINED AND PRIMED NEW PIECES INST. NEW PLATES AT BS 640 AND AEI STC SA 179850. 6) REINSTALLED LWR. JAMB WEB, FLOORBEAM ANGLES, LWR. JAMB, EDGE ANGLE AND FILLER SUPPORTS. 2L73 4F4 FRTA3WE E2EA 20030428000992003042800099NM 2003 4 28 VNAA0303028 120030321A2710 AILERON DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BINDING A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07429JS 3043 THE CREW REPORTED THE AILERONS BIND AT THE NEUTRAL POSITION. MAINTENANCE INSPECTED AILERONS AND CABLES NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S YOKE COVER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-31-01. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH DORINER MAINTENANCE MANUAL 27-11-00 AND AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030428001052003042800105NM 2003 4 28 UPS03240412 120030329A5320 BRACKET BOEING727 727173C 1384059NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, INTERCOSTAL MOUNT BRACKET BS 1060 CRACKED. FABRICATED NEW BRACKET IAW SRM 51-20-1, REPROTECTED BRACKET IAW SRM 51-10-2, MOUNT BRACKET INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20030428001062003042800106NM 2003 4 28 UPS03440414 120030406A3350 BULB BOEING747 747212B 1384886NM EMERGENCY LIGHT BURNED OUT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: A 3, EMERGENCY LIGHTS ON UPPER DECK HAS 1 BULB INOP. RELAMPED 3 LIGHTS AS REQUIRED, OPS CHECKED NORMAL. 2L74 4F A20WE 20030424000562003042400056NM 2003 4 24 QXEA0300331 120030302A5420 SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - NR 1 NACELLE SUPPORT DIAPHRAGM ON OUTBOARD SIDE OF NACELLE, ADJACENT TO WING TRAILING EDGE IS CRACKED AT OUTBOARD FLANGE. REPAIRED IAW DHC-8 RM 51-40-15. 2H72 4T RTA13NM 20030424000682003042400068NM 2003 4 24 IU62003F00003 120030221A552069704631 STOP BOEING737 737* NM ELEVATOR CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 154 STOP IS CRACKING AT RIVET (950). OCCURRED DURING NORMAL OPERATIONS. THE STOP IS MADE OF SOFT ALUMINUM AND WEAKENED BY HOLES FOR RIVETS. (EA2 NR 174550) 2L72 4F RTA16WE 20030424001122003042400112NM 2003 4 24 PCAA0303059 120030323A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DAMAGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13829EX 146 MAINTENANCE DISCOVERED FIRST FOUR EMERGENCY AISLE FLOOR PATH LIGHTS TO BE INOPERATIVE. AN INTERIM REPAIR WAS PERFORMED TO LIGHTING SYSTEM. SECOND AND FOURTH LIGHTS WERE STILL INOPERATIVE. MEL 33-13 WAS ISSUED, AND AIRCRAFT RETURNED TO SERVICE. AT NEXT MAINTENANCE VISIT WIRING UNDER FLOOR WAS REPAIRED AND ALL EMERGENCY LIGHT BATTERIES WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424001652003042400165SO 2003 4 24 LR7A03020 120030313A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND LT BULKHEAD FS 880, LBL 61 LOWER WEB AND INBOARD CAP CRACKED AT WL 200. REPAIRED IAW SRM SMP 583 53-50-17. NR 2154. 2H74 4T A1SO 20030424001662003042400166SO 2003 4 24 LR7A03021 120030313A5312 RIB LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND FS 1023 UPPER BULKHEAD RIB CRACKED BEYOND PREVIOUS REPAIR AT LBL 20, WL 283. REPLACED RIB IAW SRM SMP 583 51-70 & 51-60. NR 2156. 2H74 4T A1SO 20030424001792003042400179SO 2003 4 24 LR7A03034 120030313A5310 STRAP LKHEED382 382G 526414USO FUSELAGE BROKEN A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND LT FUSELAGE SKIN INNER STRAP BROKEN AT FS 787E, LBL 70, WL 250. REPAIRED IAW LAC MEA 382-53-03-012. NR 2264. 2H74 4T A1SO 20030424002132003042400213WP 2003 4 24 UPS03840374 120030301A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, L2 UPPER AFT DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT SKIN EDGE. CRACK LENGTH .1875 INCH LONG FOUND WITH EDDY CURRENT. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FAB FILLER DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0, TR 53-158. ALODINED AND PRIMED REPAIR PARTS IAW DC8 SRM 5 1-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 TR 53-158. 2L74 4F RT4A25 20030425000052003042500005WP 2003 4 25 UPS03840384 120030313A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, EMPENNAGE L17L END FITTING AND LONGERON CRACKED FROM FS 1768-1778. REMOVED OLD L17 LT & END FITTING TO FOM. LOCATED DRILLED DEBURRED NEW L17 LT, END FITTING AND INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030425000522003042500052NM 2003 4 25 UPS03M40400 120030205A5730 SKIN DOUG MD11 MD11F 3023600NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP INSPECTION TYPE: C, RT WING EXTERNAL SURFACE AT STA XORS 683-700 AFT STRINGER 1 FOUND CORRODED AT 3 PLACES AS MARKED. AT STA XORS 685 MATERIAL REMOVED 0.023 INCH ORIGINAL THK:0.200 INCH FOUND OUT OF LIMIT AS PER SRM 57-10-00 VOL 1 FIG 32 REV 32. 10X MAGNIFIED VISUAL INSPECTION ON BLEND OUT AREA CUT OUT AS PER EN1001-03. REWORKED AND PROTECTED AS PER SRM 51-21-01 VOL 2 REV 32. 2L73 4F RTA22WE 20030425001032003042500103WP 2003 4 25 MWEA030153 120030330A2730 PUSHROD DOUG DC9 DC982 3022082WP COCKPIT DEFECTIVE A MWEAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL31809ME 48071 UNCOMMANDED PITCH CHANGE, AUTO-PILOT OFF, FELT LIKE CONTROL SURFACE WERE MOVING WITHOUT CREW INPUT. REPLACED LEFT HAND FORWARD SPRING CARTRIDGE PUSH ROD. 2L72 4F A6WE 20030428000392003042800039WP 2003 4 28 GTIA030165 120030223A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA160 TO 122 (CENTER) FLOOR PANEL HAS SOFT/MUSHEY, DAMAGED SEVERAL INSERTS CORRODED. FABRICATED FORWARD CABIN FLOOR PANEL. 2L72 4F4 FRTA6WE E2EA 20030428000642003042800064EA 2003 4 28 COMA0360179 120030402A2150 DUCT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ACM LOOSE A COMAB EMER. DESCENT O OTHER CRCRUISE 1 SO01969CA 7141 FLIGHT 5090 A (POP) SOUND WAS HEARD AND AIRCRAFT LOST PRESSURIZATION. REINSTALLED LOOSE ACM DUCT ON LEFT WATER SEPERATOR. 2L72 4F4 FRTA21EA E15NE 20030428000972003042800097NM 2003 4 28 VNAA0303031 120030329A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL07470PS3001 3006 DURING PREFLIGHT CREW NOTICED EMERGENCY LIGHTS AT ROWS 3, 4 & 5 TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO PIT AND MAINTENANCE REPLACED THE EMERGENCY BATTERY AT 5 LK IN ACCORDANCE WITH MAINTENANCE MANUAL 33-50-00. AIRCRAFT WAS THEN RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030428001102003042800110EU 2003 4 28 U30A200300012 120030404A27504917011 COMPUTER AIRBUS320 A320214 3930316EU ZONE 120 FAULTY A U30AK NONE O OTHER ININSP/MAINT 1 EA17261AV 1615 DURING MAINTENANCE AFTER FLT 247 IN EWR, THE NR 1 SLAT FLAP SYSTEM FAULTED. REMOVED AND REPLACED THE NR 1 SLAT FLAP CONTROL COMPUTER (SFCC) IAW 27-51-34-000-001, TESTED OK IAW 27-54-00-710-002. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030428001112003042800111NM 2003 4 28 PCAA0304064 120030404A291082970009325 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM SEVERED A PCAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA13979HA 373 LGA-FLIGHT 3960 CREW REPORTED LOSS OF NR 1 HYDRAULIC FLUID IN FLIGHT. ISOLATION LIGHT ILLUMINATED. HYDRAULIC CONTENTS AT .5 QUARTS. NR 1 HYDRAULIC PUMP CAUTION LIGHT ALSO ILLUMINATED, BUT PRESSURE REMAINED NORMAL. EMERGENCY WAS DECLARED. FLIGHT LANDED WITH OUT ANY LOSS OF BRAKES NOR ANY PROBLEMS WITH LANDING GEAR. MAINTENANCE FOUND A HYDRAULIC LINE TO NR 1 INLET PRESSURE MANIFOLD SEVERED. RIGID HYDRAULIC LINE WAS REPLACED WITH A FLEXIBLE LINE IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 20-50-52. HYDRAULIC SYSTEM BLED. NO LEAKS WERE NOTED, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030428001142003042800114WP 2003 4 28 EIA2003052 120030307A5330 SKIN DOUG DC9 DC933F 302207AWP PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09944F 47194 LONGERON, 4 LEFT STA. 484 CRACK IN SKIN GOING RIVET TO RIVET 1.5 INCHES. REPAIRED CRACK AT LONGERON 4L SA 484 IN FUSELAGE SKIN IAW SRM 53-04, PG 218M, 218Z, 218AA, AB. ORIGINAL SKIN 2014 T6 .050 SUBSTITUTED 2024-T3 .050 IAW SRM 51-60-0 PG 5. 2L72 4F4 F A6WE E2EA 20030428001202003042800120NM 2003 4 28 CALA0300168 120030403A5753 STIFFENER BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE NR 3 FLAP TRACK CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 1 INCH CRACK IN NR 3 FLAP TRACK FAIRING STIFFENER. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E2GL 20030428001242003042800124NM 2003 4 28 DHL2003741521 120030323A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, BS 480 RT CIRCUMFERENTIAL DENTED 4 INCHES ABOVE FLOOR. REMOVED FASTENERS AT BS 480 RT CIRCUMFERENTIAL DENTED 4 INCHES ABOVE FLOOR IAW B-727 SRM 51-30-2. CUT OUT DAMAGED IAW B-727 SRM 53-10-4 FIG 2. FABRICATED DOUBLER REPAIR MATERIAL USED 7075 T-6 .071 PO 991208 SIZE 6 X 5.875 X 1 INCH IAW B-727 SRM 53-10-4 FIG 2. TREATED AND PRIMED IAW B-727 SRM 57-10-2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 57-30-2. 2L73 4F RTA3WE 20030428001272003042800127WP 2003 4 28 ZW0A0303904 120030402A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13925TW 49357 THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 603, LONGERON 26R TO 27R. SPLICED IN A NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3 OF ARA. CHECK-C 8-15-02 STL. 2L72 4F A6WE 20030428001312003042800131WP 2003 4 28 ZW0A0303906 120030402A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13925TW 49357 THE FUSELAGE SKIN WAS DAMAGED AT STA 601 TO 604, ABOVE LONGERON 26R, 3.25 INCHES BY 2.625 INCH AND 0.070 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 1. CHECK-C 8-15-02 STL. 2L72 4F A6WE 20030428001362003042800136NM 2003 4 28 QXEA0300433 120030404A3260301450201 SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09412QX2650 4059 PDX - FLIGHT 2340 - FLIGHT DIVERTED WHILE EN ROUTE TO SEA WHEN RECEIVED A WEIGHT ON WHEELS CAUTION LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 1 WOW SENSOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030428001442003042800144EA 2003 4 28 COMA0360184 120030406A3010355483255 SENSOR CNDAIRCL600 CL6002B19 1900309EA LT ANTI ICE SYS MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01477CA 7670 FLIGHT 5800 LT ANTI ICE DUCT WARNING. REPLACED THE LT WHEEL WELL LEAK SENSING ELEMENT. 2L72 4F RTA21EA 20030428001452003042800145CE 2003 4 28 DDXTA20030007 120030210A2497M227591689 WIRE CESSNA500 560CESSNA 2076750CE MAIN POWER CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07330QS7331 5600329 DURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY ADJACENT TO A SHROUDED FUEL CROSSFEED LINE, AND CABIN OUTFLOW VALVES. SHOULD A FIRE START, IT IS POSSIBLE THAT IT COULD GO UNNOTICED UNTIL THE CROSSFEED SHROUD AND LINE IS BREACHED. 2L72 4F RTA22CE 20030428001662003042800166WP 2003 4 28 03FDEA00416 120030409A5420 FLANGE DOUG DC10 DC1030 3023501WP NR 3 PYLON GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 3 PYLON FAIRING 487AR MOUNTING FLANG BOTH SIDES GOUGED. REMOVED AT MOUNTING FLANGES IAW SRM 51-31-01, FOUND BOTH FLANGES TO BE OUT OF LIMITS IAW SRM 51-00-00. FAB 2 NEW FLANGES USING MAT 301-1/4 HARD .05056 IAW SRM 54-31-02, INSTALLED FLANGES IAW SRM 51-35-01. 2L73 4F A22WE 20030428001782003042800178EA 2003 4 28 COMA0360186 120030407A3020355483255 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT ANTI ICE DUCTFALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01451CA 7562 FLIGHT 5335 ANTI ICE DUCT WARNING MESSAGE. REPLACED THE LT WHEEL WELL DUCT LEAK SENSING ELEMENT. 2L72 4F RTA21EA 20030428001932003042800193SO 2003 4 28 C2XA03IA036 120030408A3230355022002NOD2 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG DEFECTIVE A C2XAO OTHER J WARNING INDICATION LDLANDING 1 SW2713553 145585 IAH- FLIGHT 2833, DURING LANDING THE CREW NOTED THAT THE LANDING GEAR LEVER DISAGREE MESSAGE ILLUMINATED. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB-145 MM 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030428001942003042800194SO 2003 4 28 C2XA03IA034 120030404A2611 SMOKE DETECTOR EMB 145 EMB145 3260210SO CARGO BAY MALFUNCTIONED A C2XAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2714974 145161 BAN- FLIGHT 2631, THE CREW NOTED THE BAGGAGE SMOKE INDICATIONS ILLUMINATED. THE CREW DISCHARGED BOTH FIRE BOTTLES IN THE BAGGAGE COMPARTMENT, RETURNED TO BNA AND LANDED WITHOUT INCIDENT. BNA- MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE BAGGAGE COMPARTMENT, NO INDICATIONS OF FIRE OR RESIDUAL SMOKE. PERFORMED BAGGAGE COMPARTMENT FIRE DETECTION TEST, OPS CHECK GOOD. MAINTENANCE REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT FIRE BOTTLES, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030428001982003042800198WP 2003 4 28 0300799615 120030314A5320 BRACKET DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01615NW 47129 DURING H-CHECK, FOUND CRACK IN FUSELAGE HORIZONTAL LEG BRACKET AT BS 69 RT SIDE. REPAIRED PER EA 96-190942. 2L72 4F A6WE 20030428002002003042800200NM 2003 4 28 0300786739 120030404A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01639US 23887 DURING H-CHECK, FOUND CRACKS IN FRAME AT BS 440 S11L AND S12L. REPAIRED PER EA 67-165053. 2L74 4F A20WE 20030428002012003042800201WP 2003 4 28 0300809612 120030313A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING L-CHECK, FOUND CRACKS ON FUSELAGE NOSE SKIN AT BS 69.5 AND BS 76.5. REPAIRED PER EA 96-190940. 2L72 4F A6WE 20030428002032003042800203WP 2003 4 28 03FDEA00404 120030408A5310 SILL DOUG DC10 DC1030 3023501WP CARGO DOORWAY GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 CENTER CARGO DOOR JAMBS AFT STRUCTURE 2 EA UPPER CHAFE PLATES ARE GOUGED. CLOSING ACTION ON 04/07/03. REMOVED 2 EA SCUFF PLATES IAW SRM 51-31-01. REMOVED GOUGES FROM AFT SCUFF PLATE. NEG MATERIAL LOSS IAW SRM 53-00-01. ROUTED LWR SCUFF PLATE FAB SHOP. RECEIVED NEW SCUFF PLATE FROM FAB SHOP. TREATED AND PRIMED 2 EA SCUFF PLATES IAW SRM 51-21-01. INSTALLED 2 EA SCUFF PLATES IAW SRM 51-31-01. 2L73 4F A22WE 20030429000262003042900026NM 2003 4 29 P5CA03000808 120030129A5310 STRUCTURE BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 UPPER LOBE DECK CRACK ON F/S RIGHT BETWEEN STR 8 TO STR 10A. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH SEGMENT, SPLICE AND STRAP PER SRM 53-10-04 FIG -10. 2L74 4F A20WE 20030429000352003042900035NM 2003 4 29 03FDEA00414 120030409A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION (C53-111-01, 3) ON FRAME BS 950E LBL 7 WL 148. REPAIRED FRAME IAW SRM 53-10-4 FIG 15 AND EA 7-5310-69652. 2L73 4F RTA3WE 20030425000202003042500020EA 2003 4 25 QXEA0300405 120030325A4920WE38007703 APU CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MALFUNCTIONED A QXEAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 NM09601QX3483 3483 10009 BOI ON FLIGHT 2544- SMOKE AFT LAVATORY MESSAGE ILLUMINATED FOR LESS THAN ONE MINUTE AND WENT OFF. CHECKED WITH FLIGHT ATTENDENT, AURAL WARNING, NO SMOKE WAS DETECTED. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030425000272003042500027EA 2003 4 25 SWIA200311856 120030321A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM BROKEN A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07913SW 7597 AFTER LANDING UNABLE TO RE-CENTER RUDDER TRIM, TRIMS ONLY TO THE LEFT, RIGHT TRIM INOP. REPAIRED BROKEN WIRES ON SWITCH. OPS CHECK GOOD. 2L72 4F RTA21EA 20030425000572003042500057SW 2003 4 25 TU32003F00002 120030318A6220 BEARING BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL MAIN ROTOR DEBONDED B TU3RO OTHER O OTHER NRNOT REPORTED 1 WP07303PS271 23016 ELASTOMERIC DEBONDED FROM BEARING HOUSING. 1G72 3U3 UNCH9SW E1GL 20030428000202003042800020WP 2003 4 28 MWEA030157 120030402A575459374241 RIB DOUG DC9 DC981 3022081WP SLAT TRACK CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 LEFT NR 0 SLAT TRACK ATTACH RIB STATION XIS40.014 HAS CORROSION IN THE HOLES FOR THE AFT ECCENTRIC'S. REMOVED CORROSION, INSTALLED BUSHING ON LEFT NR 0 SLAT DRIVE TRACK ATTACH RIB. 2L72 4F A6WE 20030428000242003042800024WP 2003 4 28 GTIA030170 120030324A5320 SUPPORT FITTING DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 MAIN CABIN STA 1022 LT SIDE (T) FITTING SUPPORT FRAME CORRODED AND SHIM 1 EA. FABRICATED SHIM. LOCATED AND DRILLED HOLES ON (T) FITTING SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030428001182003042800118NM 2003 4 28 CALA0300166 120030403A5315 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1016, LBL 30. REPAIRED FLOORBEAM IAW SRM 53-00-51. 2L72 4F4 FRTA16WE E2GL 20030428001252003042800125WP 2003 4 28 ZW0A0303902 120030402A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13925TW 49357 THE FUSELAGE SKIN WAS DAMAGED AT STA 576 TO 579, ABOVE LONGERON 26R, 3.75 INCHES BY 3.75 INCHES AND 0.056 IN DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 2. CHECK-C 8-15-02 STL. 2L72 4F A6WE 20030428001342003042800134EA 2003 4 28 QXEA0300432 120030405A2810D98C07606 PRESSURE SWITCH CNDAIRCL600 CL6002C10 1390015EA ZONE 100 LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX924 924 10049 BOI - MAINTENANCE DISCOVERED A FUEL LEAK ON THE CENTER BELLY SECTION OF THE AIRCRAFT. THE NR 1 ENGINE INLET FUEL PRESSURE SWITCH WAS REMOVED AND REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030429000472003042900047EA 2003 4 29 03099647 120030409A339764643 CABLE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27647BR 7399 DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTS FROM SEAT ROW 2 TO 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A CABLE AND ONE LAMP STRIP FOR THE EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030429000552003042900055NM 2003 4 29 DHL2003780005 120030410A33501000679 LIGHT BOEING727 727223 1384074NM COCKPIT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01780DH 22006 FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE OR CHARGE. REPLACED FLIGHT DECK EMERGENCY EXIT LIGHT PER M/M 33-50-00. OPS CHECKED GOOD. 2L73 4F A3WE 20030429000592003042900059NM 2003 4 29 EIA2003056 120030408A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE WORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 LEFT FUSELAGE SKIN STA 2280 TO 2416 WORN AT INTERFACE AREA OF VERTICAL STABILIZER SEAL. REPAIRED AREA PER ECRA 471-53-218-2. 2L74 4F A20WE 20030429000682003042900068 2003 4 29 MWEA030165 420030410A34254055900906 SYMBOL GENERATOR DOUG DC9 DC982 3022082WP COCKPIT DEFECTIVE A MWEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 GL31809ME 48071 DURING CLIMBOUT FIRST OFFICERS NAVIGATION DISPLAY AND PRIMARY FLIGHT DISPLAY FAILED AND CAPTAIN'S NAVIGATION DISPLAY SHOWS BLUE LINES, FOLLOWED BY SYMBOL GENERATOR NR 2 CIRCUIT BREAKER POPPPED. REMOVED AND REPLACED FIRST OFFICERS NR 2 GENERATOR COMPUTER AND CAPTAIN'S NAVIGATION DISPLAY. 2L72 4F A6WE 20030429000762003042900076NM 2003 4 29 P5CA0300818 120030410A5714 SKIN BOEING747 747249F 1384849NM CENTER WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEVEL 1 CORROSION - WING CENTER SECTION UPPER SKIN REAR SPAR LBL 98.58. REPAIRED PER SRM 51-10-01. 2L74 4F A20WE 20030429000832003042900083NM 2003 4 29 AWXA200300359 120030410A3610 SHUTOFF VALVE BOEING737 7373S3 1384711NM NR 1 BLEED SYS INOPERATIVE A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28312AW 24060 MCI - ABORTED TAKEOFF - FLT 702 - PREPARING FOR TAKEOFF AT MCI EN ROUTE FOR PHX LT BLEED PRESSURE INDICATED ZERO, TAXIED OFF RUNWAY AND RETURNED TO GATE. MAINTENANCE ISSUED MEL 36-5, COND 2, NR 1 ENG BLEED AIR SHUTOFF VALVE INOP. WHEN AIRCRAFT RETURNED TO PHX MAINTENANCE LUBRICATED THE VALVE AND PERFORMED AN ENGINE RUN OPERATIONAL CHECK OUT, BLEED OPERATION AND PRESSURE WAS NORMAL. 2L72 4F RTA16WE 20030429000852003042900085NM 2003 4 29 AWXA200300361 120030325A575365C26320 SKIN BOEING737 7373S3 1384711NM TE FLAP CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 LCQ - MAJOR REPAIR - DURING C-18 CHECK A LEADING EDGE REPAIR AT THE INBOARD END OF THE LT OUTBOARD MID FLAP WAS FOUND CHAFED. MAINTENANCE REMOVED EXISTING REPAIR AT THE INBOARD END OF THE LT OUTBOARD MID FLAP; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-53-01, PG 219-222. 2L72 4F RTA16WE 20030425000082003042500008WP 2003 4 25 UPS03840389 120030303A5753 FITTING DOUG DC8 DC873F 302199FWP RT WING TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, RT WING AT STA XF409.6 INBOARD FLAP SUPPORT FITTING CRACKED. REMOVED BOILER PLATE, SLIDER PANEL, INBOARD TRACK, SPRING PANEL, CLOSURE PANEL AND INBOARD BASE FITTING TO FOM. DRILLED AND LOCATED BASE FITTING IAW DAC DWG 5751175. INSTALLED BASE FITTING, CLOSURE PANEL, SPRING PANEL, INBOARD TRACK, SLIDER PANEL AND BOILER PLATE IAW DC8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20030425000192003042500019EA 2003 4 25 QXEA0300408 120030326A2820 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA FUEL CROSSFLOW MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09613QX 10045 PDX- ON FLIGHT 2438, AT 39,000 FT, SAT -65 DEGREES CELCIUS, LEFT AUTO CROSSFLOW ON FUEL PUMPS STARTED CYCLING EVERY FEW SECONDS AND FUEL WAS NOT TRANSFERING FROM RIGHT TO LEFT TANK UNTIL DESCENDED TO LOWER AND WARMER ALTITUDE. TESTED FUEL TRANSFER SYSTEM WITH NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030425000282003042500028EA 2003 4 25 SWIA200311857 120030326A3230750006000 VALVE CNDAIRCL600 CL6002B19 1900309EA SELECTOR MALFUNCTIONED A SWIAA UNSCHED LANDING FEJFLT CONT AFFECTED VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM07426SW6510 6510 7468 NOSE GEAR WILL NOT RETRACT INTO UP AND STOWED POSITION WHEN GEAR LEVER SELECTED UP. RETURNED TO COS. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW MM 32-33-10. SWUNG NOSE GEAR 15-20 TIMES. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20030425000292003042500029EU 2003 4 25 RAIA00303075 120030314A2730AIR135670 SQUAT SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03567HK 41085 BOTH STALL WARNINGS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR WEIGHT ON WHEEL SWITCH, OPS CHECK OK. 2L72 4T RTA41NM 20030425000332003042500033EU 2003 4 25 RAIA00303079 120030319A243551539019E GCU JETAIRJETSTMJETSTM4101 1500501EU STARTER GEN FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03556HK1604150 41073 STL- LEFT HAND STARTER GENERATOR FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED LT HAND GENERATOR CONTROL UNIT, OPS CK OK. 2L72 4T RTA41NM 20030425000352003042500035SO 2003 4 25 RAIA00303081 120030321A325013BF7184 POTENTIOMETER EMB 145 EMB145LR 3260212SO NLG STEERING INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03821HK9308 145068 STL- NOSE WHEEL STEERING JERKED TO THE LEFT DURING TAXI. MAINTENANCE REMOVED AND REPLACED RUDDER PEDAL POTENTIOMETER, OPS CHECK OK. 2L72 4T RTT00011AT 20030425000392003042500039SO 2003 4 25 RAIA00303085 120030327A272015793101 PRESSURE SWITCH EMB 145 EMB145 3260210SO RUDDER INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03803HK8610 145077 PIT- RUDDER HARD OVER FAULT AND SPOILER FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED NUMBER 2 RUDDER PRESSURE SWITCH. LEAK AND OPS CHECK OK. PERFORMED OPS CHECK ON SPOILER SYSTEM, OPS CHECK OK. COULD NOT DUPLICATE. 2L72 4F RTT00011AT 20030425000442003042500044EA 2003 4 25 QXEA0300409 120030328A26129847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX-CENTER FIRE DETECTION CHIMNEY IN THE FORWARD CARGO BAY IS DAMAGED. REMOVED AND REPLACED CHIMNEY IAW CRJ700 MM TASK 26-17-03-400-801-A01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030425000552003042500055SW 2003 4 25 TU32003F00000 120030318A6420 BEARING BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL T/R PITCH LINK WORN B TU3RO OTHER O OTHER NRNOT REPORTED 1 WP07303PS277 23016 BEARINGS WORN BEYOND LIMITS WITH SHORT AMOUNT OF FLIGHT TIME ON COMPONENT. 1G72 3U3 UNCH9SW E1GL 20030425000702003042500070NM 2003 4 25 MYW2003F00000 120030102A33501102837 LIGHT BOEING727 727225 1384077NM AFT AIRSTAIRS INOPERATIVE A MYWAO OTHER O OTHER NRNOT REPORTED 1 SO19804MA 5814 22435 DURING PRE-FLIGHT TRANSIT CHECK FLIGHT TRANSIT AFT AIRSTAIRS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT AIRSTRAIRS OVERHEAD EMERGENCY LIGHT ASSY IAW MM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030425000752003042500075EU 2003 4 25 MALA030215 120030331A3297 WIRE SAAB SF340 340B 7860101EU CONNECTOR BROKEN A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING CONTINUITY CHECK OF SEPARATION BOLT DUAL BRIDGE CIRCUITRY FOUND BROKEN WIRE INSIDE RT CANNON PLUG P/N 851-06RC8-4SNB FOR RT SEPARATION BOLT. IAW SAAB WM-20-30-15 OPS CHECK GOOD. 2L72 4T RTA52EU 20030423001312003042300131 2003 4 23 MALA030195 420030312A3414 INDICATOR SAAB SF340 340B 7860101EU AIRSPEED MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15436XJ 340B436 DURING FLIGHT 3148, F/O'S AIRSPEED INDICATOR BEGAN INDICATING OVER 250 KNOTS, AND KEPT CLIMBING IN 16,000 FT. CAPTS AND STBY INDICATED 210 KNOTS. AIR RETURN TO MSP. MAINTENANCE DRAINED AND PURGED NR 2 PITOT SYSTEM WITH NITROGEN. CLEANED DEBRIS FROM NR 2 PITOT TUBE, DRAIN NR 2 PITOT/STATIC SYSTEM. OPS AND LEAK CHECKS GOOD. IAW SF340 MM CHAP 34, ALSO INSPECTED STBY AND NR 1 PITOT DRAINS FOR MOISTURE. NO DEFECTS NOTED. 2L72 4T RTA52EU 20030423001462003042300146WP 2003 4 23 ZW0A0303006 120030306A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 AT STA 169, THE FRAME FOOT WAS DAMAGED AT LONGERON 19R TO 20R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030423001852003042300185NM 2003 4 23 VNAA0303013 120030312A3240AC69965 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BRAKE FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL07439JS148957820 3057 THE CREW REPORTED A EMERGENCY PARK BRAKE ACCUMULATOR PRESSURE LOW CAS MESSAGE. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE ACCUMULATOR VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030424000222003042400022WP 2003 4 24 UPS03840315 120030228A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, SHEAR TIE IS CRACKED AT STA 640 BETWEEN LONG 26L AND 27L. REMOVED SHEAR TIE SPLICE, FABRICATED AND INSTALLED SPLICE IAW SRM 53-2-0 FIG 2B. 2L74 4F RT4A25 20030424000932003042400093NM 2003 4 24 QXEA0300384 120030319A323048303103 SEQUENCE VALVE BOMBDRDHC8 DHC8401 1390041NM ZONE 700 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09412QX2538 2538 4059 PDX ON FLIGHT 2340- UNSAFE LEFT GEAR LIGHT AFTER TAKEOFF. THE LIGHTS ON WERE AMBER, RED, AND GREEN HANDLE. FLIGHT ATTENDANTS REPORTED THE LEFT GEAR REMAINED DOWN. PERFORMED EMERGENCY PROCEDURE, RECYCLED GEAR TO ACHIEVE 3 UP SAFE. LATER EXTENSION NORMAL. AIRCRAFT DIVERTED TO PDX AND LANDED SAFELY. REMOVED AND REPLACED LEFT MAIN LANDING GEAR MECHANICAL SEQUENCE VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424001382003042400138NM 2003 4 24 F3LA200300113 120030310A5310 DOOR FRAME BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR FRAME ON FUSELAGE CORRODED ON AFT SEALING SURFACE BETWEEN BOTTOM TO SECOND FROM BOTTOM STOP PAD FITTINGS. BLENDED AREA AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PER SRM 53-30-03, FIG. 46 AND EA 53-737-199. TREATED, PRIMED AND INSTALLED REPAIR PER SRM 51-10-02 AND 53-30-03, FIG. 46. 2L72 4U RTA16WE 20030424001492003042400149EA 2003 4 24 QXEA0300351 120030219A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 CKB - RIGHT HAND WING FLAP GUIDE VANES HAVE SOME LOOSE RIVETS. REPAIRED IAW CRJ 700 SRM 51-42-13. 2L72 4F RTA21EA 20030424001502003042400150EA 2003 4 24 QXEA0300347 120030213A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - AT STRINGER 0 OF FS 333 LEFT HAND AND RIGHT HAND SIDES TOP EXISTING HOLE FALLS OUT INTO RADIUS OF ANGLE P/N SH670-31810-985 AND SH670-31810-987. REPAIRED IAW HORIZON AIR EA R-53-75A. 2L72 4F RTA21EA 20030424001632003042400163SO 2003 4 24 LR7A03018 120030313A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND LT FUSELAGE SKIN WARPED AND EXCEEDING DENT LIMITS AT FS 807E - 817E, LBL 67, WL 200. REPLACED SKIN FS 777E TO 817E, WL 200 - 240 IAW SRM SMP 583 51-60, 51-70 & 53-40-01. NR 2106. 2H74 4T A1SO 20030424001722003042400172SO 2003 4 24 LR7A03027 120030313A5714 STIFFENER LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST5710 FOUND LT FRONT BEAM WEB T-SPLICE STIFFENER CRACKED 1.0 INCH AT CWS 175, FS 517, WL 270. T-SPLICE STIFFENER REPLACED IAW SRM SMP 583 57-40-04. NR 2179. 2H74 4T A1SO 20030424002022003042400202WP 2003 4 24 UPS03840359 120030302A5512565174757 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C2 LT UPPER HORIZONTAL STAB MOST I/B SKIN SURFACE IS CORRODED AT STA XE 29.812. REMOVED, FABRICATED AND REPLACED SKIN PANEL ASSY BETWEEN XE 29.812 AND XE75.62 IAW DWG 5651747,8110-3 APPROVED SAA SK 880-658, UPS ENGINEERING FILE NUMBER DC8-55-20012 AND SRM 51-1-21. 2L74 4F RT4A25 20030425000162003042500016NM 2003 4 25 HALA0300080 120030214A31504083700902 COMPUTER BOEING717 717200 1383700NM COCKPIT INTERMITTENT A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13487HA 55132 DURING MODERATE RAIN AN INTERUPTION OF POWER TO CAPTAINS FMS ON APPROACH TO RUNWAY 2, OGG. CONDITION RESTORED ITSELF AFTER 30 SECONDS WITHOUT PILOT ACTION. REMOVED AND REPLACED FCC1. RTS PASSED NO FAULTS NOTED WORK DONE IAW MM. OK FOR SERVICE. 2L72 4F TRA6WE 20030425000482003042500048NM 2003 4 25 UPS03440397 120030329A3097 WIRE BOEING747 747123 1384873NM WINDOW DEICE ARCED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01675UP 20390 ELECTRICAL FUMES IN COCKPIT. FOUND R-1 WINDOW WIRE HOT. WIRE AND POST SO HOT YOU COULD NOT TOUCH THEM. FOUND D404 TERMINAL ARCING AND IT HAD DAMAGED TERMINAL SO IT COULD NOT BE REPAIRED. REMOVED AND REPLACED WINDOW. LT WINDOW HEAT CONTROLLER REMOVED AND REPLACED PER MM 30/41/01. REMOVED AND REPLACED R-1 WINDOW IAW MM 56-11-1. OK FOR SERVICE, 2L74 4F A20WE 20030425000592003042500059SW 2003 4 25 TU32003F00005 120030318A6330222010548105 LINER BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL GEARBOX MOUNT WORN B TU3RO OTHER O OTHER NRNOT REPORTED 1 WP07303PS2469 23016 ATTACHING END AT FLEXTURE WORN AND NEEDS BUFFER PAD REPLACED. 1G72 3U3 UNCH9SW E1GL 20030425000952003042500095NM 2003 4 25 QXEA0300402 120030322A5210 SKIN BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - PASSENGER DOOR SHELL HAS TWO DENTS NEXT TO EACH OTHER 2 INCHES UP FROM STRINGER 73. REPAIRED IAW RD 8/4-52-100 AND HORIZON AIR EA 6-52-256. 2H72 4T RTA13NM 20030425000982003042500098CE 2003 4 25 OIZ2003F00002 120030204A53501016200301 ANGLE BEECH 1900 1900C 1154161CE FAIRING CRACKED A OIZAO OTHER O OTHER NRNOT REPORTED 1 WP19381CR UB69 DURING THE ACCOMPLISHMENT OF THE A.D., A SMALL CRACK WAS FOUND IN THE LEFT VERTICAL TO HORIZONTAL STABILIZER FAIRING ANGLE. THE CRACK WAS LOCATED IN THE APPROXIMATE CENTER OF THE ANGLE AND ALONG THE UPPER SECTION (HORIZONTAL STABILIZER SIDE) OF THE BEND RADIUS. THE CRACK WAS APPROXIMATELY ONE INCH LONG AND WAS INITIALLY NOTED AS A FINE BLACK LINE. THE AREA WAS CLEANED AND DYE PENETRANT INSPECTION WAS PERFORMED TO CONFIRM THE CRACK. THE ANGLE WAS REPLACED WITH A NEW PART. THE ANGLE WAS REPLACED USING A NEW PART. REPLACEMENT PN 101-620030-1U. 2L72 4T RTA24CE 20030425001002003042500100NM 2003 4 25 P5CA0300783 120030315A5730112N61011 ACCESS PANEL BOEING747 74746NF 13848BTNM RT WING BROKEN A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23453PA 30811 GROUND DAMAGE TO RT WING TIP BETWEEN WS 155-25 & WBL 1243-75. TAIL JACK WAS DRAGGED UNDER WING TIP CAUSING DAMAGE TO HEADING EDGE, TRAILING EDGE A FUEL TANK EDGE A FUEL TANK ACCESS PANEL & UNDERSIDE OF WING. PERFORMED DYE PENETRANT CK, FOUND NO CRACKS MATERIAL TO BE WITHIN LIMITS AS PER B747 SRM 57-20-01. SPEED TAPED AREAS OF LEADING EDGE & TRAILING EDGE THAT WHERE DAMAGED AS PER POLAR GMM 3-17-01. PERMANENT REPAIR TO BE PERFORMED AT JFK. THE TAIL STAND WAS REMOVED FROM THE A/C & WHEN THE STAND WAS MOVING, IT WAS DRAGGED UNDER THE WING. CONTINUED OPEN ITEM 453-055 WAS CREATED TO ALLOW A/C OPS WITH DAMAGE, UNTIL A/C ARRIVED AT JFK - WHERE PERMANENT REAIRS WERE COMPLETED PER B747-400 SRM 57-51-01. 2L74 4F RTA20WE 20030425001122003042500112NE 2003 4 25 DLM88030224 220030308A7230 COMPRESSOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE STALLED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27962DL36921 49981 718057 RT ENG WITH NORMAL PWR T/O AT ROTATION HAD A COMPRESSOR STALL. THE ENG ROLLED BACK AND EGT 500 DEGS RISING. REPLACED ENGINE. 2L72 4F4 FRTA6WE E9NE 20030428000022003042800002NM 2003 4 28 DLM88030244 120030315A24302634006106 CHARGER DOUG MD88 MD88 3023688NM E/E BAY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27904DL 49535 CREW FOUND SMOKE COMING FROM TWO FUSELAGE HOLES FWD OF CTR E/E COMPARTMENT DURING PREFLIGHT INSPECTION. MTC AND FOUND BOTH SHIPS BATTERIES OVERHEATING AND VENTING THRU OVERBOARD VENT TUBES. REPLACED BOTH SHIPS BATTERIES, BATTERY CHARGER AND R2-50 RELAY. BATTERIES AND CHARGER CHECK NORMAL. 2L72 4F RTA6WE 20030428000032003042800003NM 2003 4 28 DLM90030245 120030315A4940 RELAY DOUG MD90 MD9030 3023690NM APU FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27915DN12130 P1018 53395 P1018 CREW REPORTS THAT AFTER BLOCK IN THE RAMP REPORTED HEAVY SMOKE/ELECTRIC ODOR EMINATING FROM THE APU. REPLACED STARTER AND START RELAY FOR SLOW SPOOL. 2L72 4F RTA6WE 20030428000062003042800006NM 2003 4 28 UPS03240405 120030402A800032146845 LIGHT BOEING727 727180C 138406GNM START VALVE IND INOPERATIVE A IPXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO01920UP 19873 AT CRUISE NR 1 START VALVE LIGHT FLICKERED THEN CAME ON FOR A FEW SECONDS. ENG BLEED WAS CLOSED AND ENGINE SHUTDOWN IN ACCORDANCE WITH AOM PROCEDURES. REMOVED AND REPLACED NR 1 ENGINE START VALVE IAW TAY ENGINE MM 80-11-01. OPS CHECK NORMAL. 2L73 4F A3WE 20030428000072003042800007NM 2003 4 28 UPS03440403 120030307A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD CORNER HINGE FITTING ATTACH FASTENER HOLES ONE EACH HOLE FOUND CRACK AT SKIN 5 O'CLOCK POSITION .125 INCH LENGTH THRU THICKNESS REFER ATTACHED DRAWING FOR DETAILS. AFT CARGO DOOR CUTOUT FWD CORNER SKIN REPAIRED AS PER HX RS R-53-61-34990 & UPS EA B747-53-20128. 2L74 4F RTA20WE 20030428000082003042800008NM 2003 4 28 UPS03540401 120030331A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01439UP 25470 F/O SMOKE GOGGLES CRACKED. REMOVED AND REPLACED SMOKE GOGGLES. 2L72 4F RTA2NM 20030428000182003042800018CE 2003 4 28 GLBA2003040 120030330A275212952101 ACTUATOR BEECH 1900 1900D 1154162CE TE FLAP FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03100UX10842 UE100 LEFT I/B FLAP FAILED TO RETRACT COMPLETELY. REMOVED AND REPLACED FLAP ACTUATOR , OPS CHECK GOOD. 2L72 4T RTA24CE 20030428000482003042800048NM 2003 4 28 OZIA200341002 120030117A5310001535B6018200 DOOR FRAME DORNERDO32 DO328300 NM PWA 306 PW306B NE FUSELAGE CORRODED A OZIAK NONE O OTHER ININSP/MAINT 1 CE05410Z 7126 3125 BAGGAGE COMPARTMENT DOOR SILL CORRODED. 2H72 4T4 FRTA55NM E35NE 20030428000622003042800062SO 2003 4 28 C2XA03CL084 120030402A3260355022002MOD2 ECU EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL MLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2712934 145019 CLE FLIGHT NR 2268) THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER LIFTOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND THE NOSE GEAR WOW PROXIMITY SWITCH HARNESS. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20030428000662003042800066NM 2003 4 28 QXEA0300422 120030402A2930 SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 200 SMOKE A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09405QX 4047 PDX - BEHIND PANEL 264DR TEE CONNECTED TO HYDRAULIC PRESSURE SENSOR IS SMOKING. REPAIRED IAW HORIZON AIR EA 6-53-226 AND DHC-8 SRM 51-42-05. 2H72 4T RTA13NM 20030428000672003042800067NM 2003 4 28 QXEA0300425 120030401A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 SCRATCH ON FUSELAGE BELLY SKIN APT OF STATION X32.40 BETWEEN STRINGERS 31 AND 31. REPAIRED IAW RD 8/4-53-489. 2H72 4T RTA13NM 20030428000712003042800071EA 2003 4 28 QXEA0300428 120030403A5310 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX-NUMEROUS NICKS AND SCRATCHES AROUND EXTERNAL AIR PANEL. REPAIRED IAW CRJ700 NDT MANUAL 51-20-06. 2L72 4F RTA21EA 20030428000762003042800076SO 2003 4 28 C2XA03SH084 120030407A531514521700007 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV-DURING C CHECK LEFT HAND OMEGA BEAM BETWEEN FRAMES 14 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030428000852003042800085NM 2003 4 28 PCAA0304063 120030403A33506038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAO OTHER L NO TEST NRNOT REPORTED 1 EA13805EX31523 228 AVP-FLIGHT 3559 CREW REPORTED EMERGENCY EXIT LIGHT ON TOP RIGHT SIDE OF FLOOR LEVEL EXIT INOPERATIVE. MAINTENANCE SWAPPED POWER PACKS FOR TROUBLESHOOTING. DID NOT FIX. CANNON PLUG AT EMERGENCY LIGHT INSPECTED. EMERGENCY LIGHT POWER SUPPLY IN COAT CLOSET NR 1 POSITION AND POWER SUPPLY IN CENTER CABIN NR 3 POSITION REPLACED. OPERATIONAL CHECK WAS GOOD AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030428000862003042800086WP 2003 4 28 MWEA030160 120030407A575499375324 SKIN DOUG DC9 DC981 3022081WP RT WING LE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RIGHT WING LEADING EDGE INTERNAL CRACK, LOWER AND FORWARD SURFACE. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLERS. 2L72 4F A6WE 20030428000982003042800098NM 2003 4 28 VNAA0303030 120030325A27501048A000004 ACTUATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT TE FLAPS FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07431JS19817 3028 DURING CRUISE FLIGHT THE FLIGHT CREW REPORTED THAT THE PUSHER FAIL AND FLAP CONTROL FAIL MESSAGES APPEARED ON EICAS. THE FLIGHT CREW DIVERTED TO CAK. MAINTENANCE INSPECTED AND REPLACED THE RT FLAP ACUTATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-51-01. FUNCTIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030428001032003042800103EU 2003 4 28 MALA030226 120030403A2120 ODOR SAAB SF340 340B 7860101EU CABIN DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15448XJ 340B448 BURNING ODOR IN CABIN, ON FLIGHT 3175. BURNING ODOR IN CABIN STRONGER BY HEATERS. DEFERRED CABIN AUXILIARY GROUND HEATING SYSTEM IAW MEL 21-40-1. MX PROCEDURES COMPLIED WITH PULLED AND COLLARED FLIGHT DECK C/B'S, ENTERED INTO DMR MXC NOTIFIED. MAINTENANCE CLEANED FWD HEATER. 2L72 4T RTA52EU 20030424000582003042400058NM 2003 4 24 QXEA030000333 120030227A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - LEFT HAND WING, INBOARD FLAP, UPPER SURFACE HAS CHAFE ON UPPER SURFACE. REPAIRED IAW DHC-8 SRM 57-51-30. 2H72 4T RTA13NM 20030424000722003042400072EU 2003 4 24 VJ32003F00024 120030303A7120J961225 SHOCK MOUNT GROB 120 G120A 1660208EU LYC O540 AEIO540D4D5 EA ENGINE CRACKED B VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP07865AF491 85005 DURING THE REQUIRD 100 HOUR INSPECTION, MOUNT FOUND TO BE CRACKED FROM EXHAUST HEAT. PART WAS REPLACED WITH NEW AND CRACKED MOUNT RETURNED. SUGGEST ALTERNATE MOUNT AND/OR APPLICATION OF HEAT SHIELD TO PROTECT MOUNT. 1L71 3O3 ORTA49CE 1E4 20030424001032003042400103 2003 4 24 GLBA2003039 420030325A3420 CONNECTOR BEECH 1900 1900D 1154162CE NR 1 NAV IND LOOSE A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03253GL UE253 NR 1 NAV FAILED. TIGHTENED CONNECTION ON SPLITTER, OPS CHECK GOOD. 2L72 4T RTA24CE 20030424002162003042400216WP 2003 4 24 UPS03840377 120030327A3350 SWITCH DOUG DC8 DC871F 302199DWP COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 EMERGENCY EXIT LIGHT SWITCH ANNUNCIATOR LIGHT INOP. RELAMPED EMERGENCY EXIT ANNUNCIATOR, OPS CHECK OK. 2L74 4F RT4A25 20030425000512003042500051NM 2003 4 25 UPS03M40399 120030205A5730 SKIN DOUG MD11 MD11F 3023600NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP INSPECTION TYPE: C, RT WING TOP EXTERNAL SURFACE AT XORS 740-745 AFT OF STRUCTURE 1 FOUND CORRODED AT 2 PLACES AS MARKED. REMOVED MATERIAL 0.023 INCH ORIGINAL THK:0.200 INCH FOUND OUT OF LIMIT AT XOR S 740-745 AS PER SRM 57-10-00 FIG 32 VOL 1 REV 32. REWORKED & PROTECTED AS PER SRM 51-21-01 VOL 2 REV 32. 2L73 4F RTA22WE 20030425000542003042500054 2003 4 25 MWEA030151 420030329A34254055900906 SYMBOL GENERATOR DOUG DC9 DC981 3022081WP COCKPIT DEFECTIVE A MWEAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 GL31805ME 48031 FIRST OFFICER'S PRIMARY FLIGHT DISPLAY WENT BLANK. REMOVED AND REPLACED SYMBOL GENERATOR. 2L72 4F A6WE 20030425000932003042500093NM 2003 4 25 QXEA0300400 120030319A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND FUSELAGE NOSE PANEL 122AR POSSIBLE STRUCTURE DAMAGE BY MIS DRILLING OF PANEL SCREW. REPAIRED IAW HORIZON AIR EA 6-53-221. 2H72 4T RTA13NM 20030425001062003042500106NM 2003 4 25 DL76L030213 120030305A2121732592C FAN BOEING767 767332 1382001NM FWD CARGO FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27190DN 28447 DURING CRUISE CREW SMELLED SMOKE ACCOMPANIED WITH AN FWD EQUIP EXHAUST FAN EICAS MESSAGE. CREW ELECTED TO DIVERT TO CMH AS A PRECAUTION. CVG MTC IN CMH CONFIRMED THAT THE EXHAUST FAN WAS BAD AND RUBBING ON SHROUD. DISCONNECTED CANNON PLUG FROM FAN AND FORWARDED TO MCO PER MEL 21-58-04B. 2L72 4F RTA1NM 20030428000362003042800036WP 2003 4 28 ZW0A0303701 120030402A33501315 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BURNED OUT A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139407R 49400 THE AFT STAIRWAY OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 3-17-2003. 2L72 4F RTA6WE 20030428001122003042800112SO 2003 4 28 CHQA000248 120030406A3610 THERMOSTAT EMB 145 EMB145LR 3260212SO BLEED SYSTEM OUT OF ADJUST A CHQAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL11286 145443 BLEED 1 OVER TEMP WARNING DURING CLIMBOUT OF IND. WE HAD JUST EXITED ICING CONDITIONS. FOLLOWED QRH AND WARNING WENT AWAY. TURNED BLEED BACK ON AND WARNING CAME BACK ON. DECLARED INFLIGHT EMERGENCY AND MADE UNEVENTFUL LANDING AT IND. PERFORMED ADJUSTMENT AND TEST OF FAN AIR THERMOSTAT PER AMM 36-11-06. NO DEFECTS NOTED DURING GROUND RUN. 2L72 4T RTT00011AT 20030428001522003042800152SO 2003 4 28 C2XA03CL087 120030408A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27155557793 56 145594 DURING ROUTINE MAINTENANCE SEVERAL EMERGENCY FLOOR AISLE LIGHT STRIPS WERE FOUND INOPERATIVE. ALSO FOUND LEFT AND RIGHT OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY BATTERY OPERATIONAL CHECK WAS GOOD. 2L72 4T RTT00011AT 20030428001532003042800153NM 2003 4 28 DHL2003743008 120030409A2612 FIRE DETECTOR BOEING727 727225 1384077NM NR 3 ENGINE CHAFED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01743DH 22438 NR 3 DETECTOR CIRCUIT GROUND LIGHT COMES ON INTERMITTENTLY. FOUND SENSING ELEMENT TO BE RUBBING ON COWLING, ADJUSTMENT SEEMS TO HAVE CORRECTED PROBLEM, OPS CHECKED GOOD PER BMM 26-11-12. 2L73 4F A3WE 20030428001582003042800158WP 2003 4 28 UPS03840387 120030328A5730 SKIN DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 LOWER WING SKIN CRACK OUTBOARD NR 1 ENGINE PYLON STA XW 508. FERRIED TO SAA FOR REPAIR. *S/D* CUT OUT CRACKED AREA ON SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED WING SKIN FILLER, REPAIR FILLER AND DOUBLER IAW 8110-3 APPROVED SAA SK 772-799, AS A INTERIM REPAIR FOR 18 MONTHS. 2L74 4F RT4A25 20030428001722003042800172WP 2003 4 28 03FDEA00401 120030408A5248 STRIP DOUG DC10 DC1030 3023501WP TAILCONE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 TAIL CONE AFT END OF RT PATIO DOOR, METAL CLOSEOUT STRIP IS WORN THRU (MARKED) 6 INCH LENGTH. CLOSING ACTION ON 04/07/03. REPLACED CLOSEOUT STRIP IAW SRM 51-31-01. NEW CLOSEOUT, FAB PER MAE TRAVLER T2/324996. 2L73 4F A22WE 20030428001752003042800175WP 2003 4 28 03FDEA00406 120030408A5420 BRACKET DOUG DC10 DC1030 3023501WP NR 3 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 3 PYLON FLUID LINE SUPPORT BRACKET CRACKED JUST OUTBOARD OF THROTTLE CABLE QUARDANT. CLOSING ACTION ON 04/08/03. REMOVED SUPPORT BRACKET IAW SRM 51-31-01. FAB NEW SUPPORT BRACKET ON TRAVELER T2/325535. LOCATED AND DRILLED NEW PART IAW SRM 51-31-01. INSTALLED SUPPORT BRACKET IAW SRM 51-31-01. 2L73 4F A22WE 20030429000902003042900090WP 2003 4 29 03FDEA00431 120030411A5420 BRACKET DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 2 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 2 ENGINE FAN CASE ANTI-ICE HOT DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT HAS CRACK. CLOSING ACTION ON 04/10/03. REMOVED AND REPLACED NR 2 ENGINE FAN CASE ANTI-ICE HOT AIR DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT IAW M/M 70-00-00-2. 2L73 4F4 F A22WE E23EA 20030429000962003042900096NM 2003 4 29 CH1A200395011 120030410A5754 RIB BOEING727 727290 138408WNM LE SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 L/E SLAT NR 5 OUTBD SIDE OF ACTUATOR ATTACH POINT TO SLAT, CRACK IN RIB FWD END. 2L73 4F A3WE 20030429001012003042900101WP 2003 4 29 ZW0A0304202 120030409A3350408822101 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139405T 53141 THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 4, 5, 14, 18, 20, AND 28. REPLACED THE BATTERIES IN THE AFFECTED BATTERY PACKS. CHECK-C 10-19-2002 STL. 2L72 4F RTA6WE 20030429001032003042900103SO 2003 4 29 C2XA03SH100 120030413A532014522459003 ANGLE EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK, THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030429001082003042900108SO 2003 4 29 C2XA03SH105 120030413A531014522460015 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV - DURING C-CHECK, THE DIGITAL BUTT STRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030429001102003042900110EU 2003 4 29 RAIA00304098 120030402A612031056294 BETA SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03561HK 41077 STL- RIGHT ENGINE BETA LIGHT ILLUMINATED WHEN TAKEOFF POWER APPLIED. MAINTENANCE REMOVED AND REPLACED BETA SWITCH, OPS CK OK. 2L72 4T RTA41NM 20030429001162003042900116SO 2003 4 29 RAIA00304108 120030408A3230 PIN EMB 145 EMB145 3260210SO PROP SWITCH DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03803HK 145077 PIT- LANDING GEAR WILL NOT RETRACT. MAINTENANCE FOUND PUSHED PIN ON RIGHT AFT PROP SWITCH. CORRECTED AND OPS CK GOOD. 2L72 4F RTT00011AT 20030429001172003042900117SO 2003 4 29 RAIA00304109 120030408A3260 SQUAT SWITCH EMB 145 EMB145 3260210SO MLG OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03803HK 145077 PIT- LANDING GEAR WILL NOT RETRACT. MAINTENANCE ADJUSTED NLG WOW SWITCHES, OPS CK GOOD. 2L72 4F RTT00011AT 20030429001222003042900122GL 2003 4 29 RAIA00304107 220030408A7532SU2226 O-RING EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL BLEED VALVE DETERIORATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03822HK 145069 STL- BLEED NR 1 LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING AT NR 1 ENGINE BLEED AIR VALVE, OPS AND LEAK CHECK OK. 2L72 4T4 FRTT00011ATTE6CH 20030429001452003042900145NM 2003 4 29 CA030220006 120030203A5311 FRAME BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 55240 (CAN) DURING C CHECK,4 CRACKED AROUND FASTENER HOLES WERE FOUND AT STA 727 STR 14R.CRACKS REPAIRED IAW SRM 53-30-3 FIG.42. TIME 55240.59 CYC.52226 2L72 4F4 F A16WE E2EA 20030429001462003042900146EA 2003 4 29 CA030221003 120030112A5610NP13932110 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING C F.O.D. CLCLIMB 1 CA (CAN) CLIMBING OUT OF DENVER AT ABOUT 9600 MSL, WINDSHIELD SHATTERED. SMALL SMUDGE MARK BUT NO FEATHERS. VMC ABOUT 220 KTS.PERFORMED CHECKLIST LEVELED OFF AT 12,000.DECIDED TO RETURN TO DENVER.BURNE D OFF ROUGHLY 2000 LBS OF FUEL TO LAND BELOW 47,000 LBS.INNER PANE WAS INTACT.NORMAL LANDING. DID NOT DECLARE AN EMERGENCY OR ASK FOR EQUIPMENT. REMOVED AND REPLACED CAPTAIN'S FWD WINDSHIELD PER AMM. 2L72 4F4 FRTA21EA E15NE 20030425000832003042500083NM 2003 4 25 QXEA0300390 120030322A5320 MOUNT BOMBDRDHC8 DHC8401 1390041NM ANTENNA CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - NR 3 COMM ANTENNA MOUNT CORRODED. REPAIRED IAW DHC-8 400 SRM 51-21-10, PAGE 201 AND RD 8/4-53-471. 2H72 4T RTA13NM 20030428000042003042800004SO 2003 4 28 O662003F00000 120030326A215039546021 SHUTOFF VALVE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6108 NE A/C PACK FAILED B O66RA UNSCHED LANDING O OTHER CLCLIMB 1 WP01226AL7146 1057 TWO AIR CONDITIONING SHUTOFF VALVES ARE INSTALLED. DURING CLIMBOUT, THE AIRCRAFT WAS PRESSURIZING BUT NOT AT A RATE SUFFICIENT TO ACHIEVE CRUISING ALTITUDE. THE FLIGHT RETURNED TO BASE AND TROUBLESHOOTING REVEALED THE RIGHT AIR CONDITIONING SHUTOFF VALVE HAD FAILED CLOSED. REPLACING THE VALVE RETURNED PRESSURIZATION SYSTEM OPERATION TO NORMAL. AFTER RESEARCHING FLEET DATA WITH THE A/C MFG, IT TURNS OUT THIS VALVE IS NOT A HIGH FAILURE ITEM. ALSO, THE CREW HAS PROCEDURES IN PLACE TO OPERATE THE AIRCRAFT WITH ONE VALVE NOT FUNCTIONING. 2L72 4F4 FRTA12EA E25NE 20030428000152003042800015WP 2003 4 28 GTIA030221 120030316A3350 LIGHT DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE CABIN INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 EMERGENCY OVERHEAD LIGHTS INOPERATIVE IN PAX CABIN AISLE NR 3,7,10,12,14,18,22,25,29. TROUBLESHOT AND REPAIRED EMERGENCY OVERHEAD LIGHTS. 2L72 4F4 FRTA6WE E2EA 20030428001012003042800101NM 2003 4 28 VNAA0303026 120030320A3000851003 EJECTOR VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RH FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07429JS185543582 3043 EN ROUTE, THE CREW RECEIVED AN AIR FOIL DE-ICE FAIL IN ALL MODES AND DIVERTED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE 17HH EJECTOR CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030428001812003042800181NM 2003 4 28 AWXA200300353 120030408A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE AT SEAT ROWS 4 AND 5 LT, A BROKEN WIRE WAS DISCOVERED UNDER SEAT ROW 5 LT. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030428002042003042800204EU 2003 4 28 03FDEA00375 120030402A5754 RIB AIRBUS310 A310 EU RT SLAT NR 2 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25443FE 283 COMPLY WITH EA 6-5740-68775 WINGS-RT SLAT NR 2-LEADING EDGE DAMAGE REPAIR BETWEEN RIB 2 AND RIB 3 UNDER W/O NR 13350 FEDEX N/R NR S00005. *S/D* COMPLIED WITH EA 6-5740-68775 WINGS-RT SLAT NR 2 LEADING EDGE DAMAGE REPAIR BETWEEN RIB 2 AND RIB 3. 2L72 4F RTA35EU 20030428002052003042800205EU 2003 4 28 MALA030232 120030408A21507063250 SEAL BAC 146 AVRO146RJ85A1500097EU NR 2 A/C PACK DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15535XJ E2371 DURING FLIGHT, NR 2 PACK VALVE INDICATES OPEN WHEN SELECTED CLOSED. VALVE CURRENTLY ON MEL. ALSO RECIRC CAN BE SELECTED TO RECIRC WITH ONLY 1 PACK RUNNING. A LOUD POPPING SOUND FROM REAR OF A/C. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED PERI-SEALS ON NR 2 PACK VALVE (P/N 706-3-250). OPS CHECK AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20030429000332003042900033NM 2003 4 29 03FDEA00408 120030408A2121 FAN BOEING727 727200 138407ENM AIR CONDITIONINGINOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25234FE 21328 SHORTLY AFTER LVL OFF AT FLT LEVEL 280 THE NO EQUIP COOLING LIGHT ILLUM. QRH DIRECTED TO CHK / RESET EQUIP COOLING C/B. PULLED AND RESET THE C/B AND LIGHT REMAINED ON. QRH THEN DIRECTED TO SHUT OFF RADIO ALT, VHF, & DME - COMPLIED WITH CHK LIST AND LIGHT REMAINED ON. QRH DIRECTED LAND AT NEAREST SUITABLE AIRPORT - LANDED AT MCI 0201Z. FOUND BLOWER DISCHARGE DUCT MUFFLER/LINER SHIFTED AND BLOCKING HOLE FOR FLOW LIMIT NOZZLE. ALSO FOUND FLEX HOSE FOR FLOW LIMIT NOZZLE COLLAPSED. REMOVED AND REPLACED BLOWER FAN DUE TO FOD DAMAGE REF 727-200 AMM 21-58-011-4. REMOVED AND REPLACED BLOWER DISCHARGE DUCT & FLOW LIMITING NOZZLE FLEX HOSE REF 727-200 AMM 21-58-061-4. OPS CKS OK. 2L73 4F RTA3WE 20030429000452003042900045 2003 4 29 DXTA200300010 420030316A3425 SWITCH RAYTHNDH125 HAWKER800XP 7150012CE GLARESHIELD FAILED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07862QS 258362 WHEN COCKPIT LIGHTS MASTER SWITCH TURNED ON AT FL 330 SMOKE OBSERVED COMING FROM CENTER GLARESHIELD AREA. TURNED OFF SWITCH, SMOKE STOPPED BUT WAS STILL DETECTABLE 15 MIN LATER. 2L72 4F RTA3EU 20030429000662003042900066NM 2003 4 29 AT0300012 120030405A33506011779 POWER SUPPLY BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15954AT 55016 DURING SERVICE CHECK FOUND EMERGENCY EXTERIOR LIGHTS INTERMITTENT OPERATION (OVERWING LIGHTING). REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY, IAW B717 33-51-06, OPS NORMAL. 2L72 4F TRA6WE 20030429001192003042900119NE 2003 4 29 RAIA00304103 220030404A732131059008 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LT ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CE03572HK147502781 41091 76091 RIC- LEFT ENGINE LOW TORQUE. MAINTENANCE REMOVED AND REPLACED THE NR 1 FUEL CONTROL, OPS AND LEAK CK OK. 2L72 4T4 TRTA41NM E18NE 20030429001752003042900175EA 2003 4 29 CA030323001 120030323A2820 FLAPPER VALVE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN1 52008NE FUEL SYSTEM BROKEN W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) BOTH CHECK VALVES WERE REMOVED FROM AIRCRAFT AND DISASSEMBLED.THE CHECK VALVE THAT WAS LOCATED AT THE HAND WOBBLE PUMP IN THE AIRCRAFT WAS FOUND TO HAVE A BROKEN SPRING ON THE INTERNAL FLAPPER VALVE. WHEN EXTERIOR WAS CLEANED, CRACKS WERE FOUND IN THE MAIN HOUSING BODY. THESE WERE MOST LIKELY CAUSED FROM OVER TORQUING OF THE HOSE FITTINGS WHEN PREVIOUSLY ASSEMBLED. THE REAR CHECK VALVE, LOCATED AT THE FUSELAGE FUEL FILTER, WAS FOUND TO ALSO HAVE CRACKS IN THE HOUSING BODY. THE INTERNAL RUBBER SEALS IN BOTH CHECK VALVES WERE FOUND TO BE IN GOOD CONDITION. CORROSION WAS NOTED ON THE INTERNAL THREADS OF THE FORWARD CHECK VALVE. 1H71 3R3 R A806 5E1 20030429001902003042900190EU 2003 4 29 CA030409010 120030408A6720704A34412047 HOSE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) UPON INITIAL INSTALLATION OF HYDRAULIC HOSE (TAIL ROTOR CONTROL SERVO) THE FLARE FITTING SPLIT ALONG LENGTH OF FLARE NUT/FERRULE (ONE PIECE). HOSE RETURNED TO MFG FOR WARRANTY REPLACEMENT. 1G71 3U3 U H9EU E19EU 20030429001962003042900196EU 2003 4 29 CA030410001 120030120A2720 ROD AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE RUDDER DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) RUDDER POSITION FEED BACK ROD ASSEMBLY DAMAGED FROM SKYDROL ROD IS MADE FROM A KEVLAR MATERIAL THAT IF A PRE-EXISTING CONDITION ALLOWS SKYDROL TO CONTAMINATE THE STRUCTURE OF THE ROD IT WILL DETERIORATE. 2L72 4F4 FRTA28NM E29NE 20030429002022003042900202NM 2003 4 29 CALA0300190 120030412A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND INTERCOSTAL CORRODED ON LOWER SURFACE AT NUT PLATES, STA 500C-500D, S26L. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 53-30-53 AND 51-40-02. 2L72 4F RTA16WE 20030429002032003042900203NM 2003 4 29 CALA0300191 120030412A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND INTERCOSTAL CORRODED ON LOWER SURFACE AT NUT PLATES, BS 500C-500B, S26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030429002052003042900205NM 2003 4 29 CALA0300193 120030413A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917317 23368 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 27. THE UPPER T-CAP ON FLOORBEAM WAS REPLACED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030429002082003042900208NM 2003 4 29 VNAA0304005 120030409A3260 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG FAILED A VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL07459PS 3070 ON APPROACH, THE CREW RECEIVED A PROXI SYSTEM FAIL INDICATION AND PERFORMED A GO-AROUND. ON THE SECOND APPROACH, THE LANDING WAS NORMAL AND FLIGHT 4009 LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE THEN INSPECTED THE PROXI SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00, BUT COULD NOT DUPLICATE ANY DEFECTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030429002092003042900209NM 2003 4 29 VNAA0304003 120030409A5270 PSEU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR MALFUNCTIONED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07472PS 3008 EN ROUTE, THE CREW RECEIVED A RED WARNING PANEL DOOR LIGHT AT 24,000 FT. THE CREW DESCENDED AND THE LIGHT EXTINGUISHED AT 21,000 FT. UPON ARRIVAL, THE PSEU WAS RERACKED AND OPERATIONAL CHECKS WERE PERFORMED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030429002122003042900212NM 2003 4 29 VNAA0304001 120030404A2823 ACTUATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FUEL SHUTOFF FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07433JS 3047 EN ROUTE, THE CREW RECEIVED A RIGHT HAND FUEL SHUTOFF VALVE ACTUATOR CLOSED CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND FUEL SHUT OFF VALVE ACTUATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030429002152003042900215NM 2003 4 29 DHL2003746006 120030411A561058935578 WINDSHIELD BOEING727 727224 1384076NM COCKPIT CRACKED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01746DH 22252 R2 WINDOW ARCING. COMPLETED ABNORMAL PROCEDURES. OUTER PANE CRACKED. REMOVED AND REPLACED R2 WINDOW IAW M/M 56-12-11. ADJUSTED ANTI-ICING SYSTEM PER M/M 30-41-02. OPS CHECKED GOOD. REMOVED AND REPLACED NR 2 WINDOW HEAT CONTROLLER IAW M/M 30-40-00. 2L73 4F A3WE 20030429002172003042900217EU 2003 4 29 03FDEA00437 120030411A7714 INDICATOR AIRBUS310 A310 EU ENGINE N1 INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25403FE 230 ON TAKEOFF ROLL AS TOGA WAS SELECTED ON AUTO THROTTLE SYSTEM (FOR FLEX POWER) NR 2 N1 ANALOG POINTER HUNG AT 40 PERCENT, ALSO NR 2 ENGINE SLOW TO ACCELERATE WITHIN 3-5 SECONDS. REJECTED TAKEOFF AT 95 KNOTS. FACT 11APR03 06:34 LAX, REMOVED AND REPLACED NR 2 N1 INDICATOR PER M/M 77-11-12-4, CHECKS OK ACCELERATION OK PER JRH 6-17 R/I 11APR03 06:35 LAX, SCHEDULED REMOVAL/INSTALLATION OFF MFG 63601-450-2 POS 2RH SRL 156 TAG 811648 ON MFG 63601-450-2 SRL 119, TAG 512880. 2L72 4F RTA35EU 20030429002252003042900225NM 2003 4 29 SWAA030809 120030409A26121000127 CONTROL UNIT BOEING737 7373Q8 1384670NM FIRE WARNING FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW29663SW 23256 AIR TURNBACK, DURING TAKEOFF BOTH FWD AND AFT CARGO FIRE INDICATION LIGHTS ILLUMINATED. REMOVED AND REPLACED FIRE WARNING CENTRAL CONTROL UNIT PER MM. 2L72 4F RTA16WE 20030430000052003043000005NM 2003 4 30 QXEA0300493 120030411A5350 FAIRING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - WING TO FUSELAGE FAIRING, PANEL 262AT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030430000192003043000019EU 2003 4 30 AWXA200300450 120030404A5320D5374797000 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK TWO EACH 3/8" CRACKS WERE FOUND AT SCREW HOLES ON FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT FR 28-29, RBL 29. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND SPLICE REPAIR; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5325-00280-JL1. 2L72 4F RTA28NM 20030430000222003043000022EU 2003 4 30 AWXA200300447 120030329A5330D53470410200 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON SKIN AT FR 63 BETWEEN STR 43 AND STR 44 LT. MAINTENANCE CUTOUT DAMAGED SKIN AT FR 63 BETWEEN STR 43 AND STR 44 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-51-11, FIG. 203, PG. 221-224, AND SRM 51-42-11, FIG. 2-7, PG. 7-20. 2L72 4F RTA28NM 20030430000302003043000030NE 2003 4 30 AWXA200300437 220030427A7200 ENGINE AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 FAILED A AWXAGEA O2 MASK DEPLOYED ENGINE SHUTDOWN UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 WP28828AW 1552 V11027 EN ROUTE FROM PHX TO DCA AT FL 370 A LOUD BANG WAS HEARD COMING FROM NR 1 ENGINE, IMMEDIATELY FOLLOWED BY A CLOGGED OIL MESSAGE, ALL OTHER PARAMETERS NORMAL. CREW CONTACTED MOC AND WERE TOLD TO MONITOR ENGINE. APPROXIMATELY 15 MINUTES LATER TWO MORE BANGS WERE HEARD COMING FROM LT ENGINE, THIS TIME FOLLOWED BY AVIONICS AND CARGO SMOKE INDICATIONS. COCKPIT AND CABIN FILLED WITH DENSE SMOKE, MASKS DEPLOYED, CREW AND CABIN WENT ON OXYGEN. DECLARED EMERGENCY AND PREPARED TO DIVERT TO STL, RECEIVED NT 1 ENGINE LOW OIL PRESSURE INDICATION AND SHUTDOWN ENGINE. AT FL 150 SMOKE BEGAN TO DISSIPATE, AND AT FL 100 CREW WAS ABLE TO COME OFF OXYGEN, LANDED AT STL WITHOUT FURTHER EVENT. MAINTENANCE R & R NR 1 ENGINE. 2L72 4F4 FRTA28NM E40NE 20030430000422003043000042NM 2003 4 30 MWEA030187 120030425A2923861555 PUMP BOEING717 717200 1383700NM AUX HYD SYS FAILED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31902ME 55166 INBOARD SPOILER FAIL ALERT, NO SPOILER DEPLOYMENT WITH HYDRAULIC PRESSURE NORMAL. PULLED AND RESET SPOILER ELECTRONIC CONTROL UNIT (SECU) CIRCUIT BRAEKER INBOARD AND OUTBOARD CHANNELS P-35 AND R-35 AND PERFORMED RETURN TO SERVICE. 2L72 4F TRA6WE 20030430000722003043000072NM 2003 4 30 USAASB03042 120030319A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19341US 23510 IND - MAINTENANCE REPORTED THE EMEGENCY LIGHT BATTERY PACK, FOR THE LEFT OVERWING EXIT LIGHT, HAS LOW VOLTAGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030430000852003043000085SO 2003 4 30 SIMA200308406 120030320A531514522453001 FLOORBEAM EMB 135 EMB135LR 3260305SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 ABI - DURING A IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED SECTION OF THE LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM (SRM EMB 145/1142 REV 20) CHAPTERS 53-21-10, FIG 201. (M) 2L72 4F RTT00011AT 20030430000902003043000090SO 2003 4 30 SIMA200309009 120030308A532014524131007 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION PASSENGER DOOR AFT FLOOR SUPPORT BRACKET CORRODED. REMOVED AND INSTALLED NEW SUPPORT IAW EMB135 SRM 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20030428001082003042800108WP 2003 4 28 UPS03840408 120030403A2611898988C CONNECTOR DOUG DC8 DC873F 302199FWP FIRE LOOP LOOSE A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01814UP 46090 NR 4 ENGINE FIRE WARNING SOUNDED INTERMITTENTLY (QUICK ON AND OFF) 3 TIMES. DID NOT SHUT ENGINE DOWN DUE TO WEATHER AND SHORT FINAL TESTED AND TESTED CIRCUITS TESTED GOOD, ENGINE ANTI-ICE ON WITH MODERATE PRECIPITATION. ACCOMPLISHED T/S PER M/M 26-10-00 PAR A, NO DEFECTS NOTED. VISUALLY INSPECTED ALL ENG FIRE LOOPS, FOUND CONNECTOR P1-7008 LOOSE. CLEANED A RESECURED CONNECTOR, REPLACED NR 4 FIRE CONTROL UNIT PRECAUTIONARY SYS, OPS NORMAL REF 26-10-05. 2L74 4F RT4A25 20030428001462003042800146WP 2003 4 28 MWEA030163 120030401A77142CM9ABH7 TACH GENERATOR DOUG DC9 DC932 3022066WP NR 1 ENGINE DEFECTIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31205ME 47601 AFTER ENGINE START NR 1 ENGINE N1 WENT TO ZERO. REMOVED AND REPLACED LEFT ENGINE N1 TACH GENERATOR. 2L72 4F A6WE 20030429000072003042900007NM 2003 4 29 P5CA0300803 120030127A5521 PANEL BOEING747 747283B 1384867NM ELEVATOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 ELE LEFT NR 334 ML HONEYCOMB PANEL INBOARD SURFACE HAS DELAMINATION. REPAIRED BY BONDING FIBERGLASS PLIES USING VACCUM BAG PER SRM 51-40-09. 2L74 4F A20WE 20030417001902003041700190NM 2003 4 17 P5CA0300752 120030129A5330 SKIN BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND ON UPPER LOBE DECK F/S 520 RT BETWEEN STR 7 TO STR 10A. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH SEGMENT, SPLICED & STRAPPED. 2L74 4F A20WE 20030421001972003042100197NM 2003 4 21 AMTA200300368 120030314A2612710127 FIRE LOOP BOEING757 75733N 1384931NM LEFT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11558TZ 32592 LEFT ENGINE FIRE LOOP 2 STATUS LIGHT ON. REMOVED AND REPLACED NR 3 FIRE DETECTOR LOOP NR 2 PER AMM 26-11-01-4. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030421001992003042100199NM 2003 4 21 USAABB03036 120030307A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030422000982003042200098NM 2003 4 22 USAA030022 120030312A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 CLT - FOUND FRAME WEB CRACKED .5 INCH CRACK, BS 1440 AFT CARGO DOOR CUTOUT INBOARD UPPER BOLT HOLE. INSTALLED WEB SPLICE REPAIR PER EA 87120. (M) 2L72 4F RTA2NM 20030422001092003042200109SO 2003 4 22 SIMA200305006 120030213A5330AL2024T3 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21639AE 145182 ABI - DURING A IMBV INSPECTION STRINGER 19L WAS FOUND CHAFED BETWEEN FRAMES 52 AND 53. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 20, 53-24-02. (M) 2L72 4T RTT00011AT 20030422001312003042200131EA 2003 4 22 SWIA200311821 120030228A4960 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU CONTROL ILLUMINATED A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07413SW 7102 DURING DESCENT, APU WAS STARTED. AFTER APU SPOOL-UP DOOR-INHIBIT MESSAGE CAME ON. APU FIRE WAS DETECTED AND APU SHUT DOWN AUTOMATICALLY. APU BOTTLE LIGHT DID NOT ILLUMINATE AND WAS NOT DISCHARGED BY CREW. RESET APU ECU FAIL CODE. OPS CHECKED APU DOOR. OPS CHECKED APU, OPS CHECKS GOOD. 2L72 4F RTA21EA 20030423000822003042300082EU 2003 4 23 BAQA085931 120030408A6220365A3118100451 STARFLEX AEROSPSA365 SA365N 8680669EU MAIN ROTOR DEBONDED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911UF93 6338 BUSHING DEBONDED COMPLETELY (RED ARM). REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030423001042003042300104CE 2003 4 23 GLBA2003015 120030204A3260 UPLOCK SWITCH BEECH 1900 1900D 1154162CE RT MLG OUT OF ADJUST A GLBAO OTHER N FALSE WARNING CRCRUISE 1 NM03100UX UE100 LANDING GEAR IN-TRANSIT LIGHTS FLICKER WITH GEAR UP, ADJUSTED RT MLG UPLOCK SWITCH OPS CHECKED GOOD 2L72 4T RTA24CE 20030423001092003042300109 2003 4 23 GLBA2003017 420030215A3418 VANE BEECH 1900 1900D 1154162CE STALL WARNING STUCK A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03220GL UE220 STALL WARNING SOUNDED ON ROTATION, RELEASED STUCK VANE TEST FLIGHT OK 2L72 4T RTA24CE 20030423001142003042300114CE 2003 4 23 VFGR435L 120030110A14301016100195 RIVET BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA TORQUE TUBE LOOSE B VFGRK NONE O OTHER ININSP/MAINT 1 SO1715031 98 UC103 FOUND LOOSE RIVETS ON FLANGE ADAPTER ATTACHED TO L/H ELEVATOR TORQUE TUBE ASSEMBLY P/N 101-610019-5. 2L72 4T4 TRTA24CE E4EA 20030423001552003042300155NM 2003 4 23 UPS03240281 120030219A5311 FRAME BOEING727 727108C 1384039NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, SUB FRAME AT BS 920 RT HAS SMALL CRACK AT STR 15. SUB FRAME AT BS 920 RT REPAIRED IAW SRM 51-40-03. 2L73 4F A3WE 20030424000022003042400002WP 2003 4 24 MWEA030134 120030309A3243222704 CONTROL VALVE DOUG DC9 DC914 3022034WP LT MLG BRAKE INOPERATIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31500ME 45711 LEFT BRAKE DOES NOT WORK WITH RIGHT HYDRAULIC SYSTEM SELECTED. REMOVED AND REPLACED RIGHT WHEEL WELL BRAKE CONTROL VALVE. 2L72 4F A6WE 20030424000182003042400018NE 2003 4 24 UPS03540311 220030319A7200 ENGINE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE NR 1 FLAMED OUT A IPXAE ENGINE SHUTDOWN X ENGINE FLAMEOUT APAPPROACH 1 SO01465UP 28269 INSPECTION TYPE:N/A NR 1 ENG FLAME OUT UNCOMMANDED IN FLIGHT (ON APPROACH) SHUT DOWN. REPLACED DEGICATED GENERATOR; A & B DEGICATED GENERATOR CONTROL UNITS; BLEED VALVE CONTROL UNIT; & PTU. RAN ENGINES PER 70-00-00/501, OPS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20030424000392003042400039NM 2003 4 24 QXEA0300341 120030308A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CHAFING ON PANEL ATTACH FLANGE OF PANEL 261CT, AFT EDGE AT FIRST FIVE CAMLOC HOLES. REPAIRED IAW HORIZON AIR EA 6-57-122. 2H72 4T RTA13NM 20030424000462003042400046NM 2003 4 24 QXEA0300321 120030228A3213 STRUT BOMBDRDHC8 DHC8401 1390041NM ZONE 700 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - RIGHT HAND MAIN LANDING GEAR STRUT CHAFED AT THREE LOCATION ON AFT SIDE NEAR NITROGEN SERVICE POINT. REPAIRED IAW CMM 32-11-03, PAGE 602, 2A. 2H72 4T RTA13NM 20030429000482003042900048EA 2003 4 29 03099674 120030409A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27674BR 7601 DURING MAINTENANCE INSPECTION, THE LT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030429001152003042900115EU 2003 4 29 RAIA00304105 120030407A3260 PROXIMITY SWITCH AEROSPATR72 ATR72202 8680940EU MLG DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03723TE 283 LANDING GEAR WILL NOT RETRACT. MAINTENANCE CLEANED PROX SWITCHES, OPS CHECK GOOD. 2H72 4T RTA53EU 20030429002262003042900226NM 2003 4 29 SWAA030780 120030408A3213656174010 STRUT BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG UPPER STRUT CORRODED. REMOVED AND REPLACED LEFT MLG OUTER CYLINDER PER MM. 2L72 4F RTA16WE 20030430000352003043000035EA 2003 4 30 COMA0360218 120030427A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01805CA 7354 FLIGHT 5766 FLOOR PATH EMERGENCY LIGHTS ARE INOPERABLE ROWS 2-5. REPLACED THE FLEXIBLE LAMP. 2L72 4F RTA21EA 20030430000732003043000073SO 2003 4 30 SIMA200308405 120030321A531514522463001 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21800AE 145425 ABI - DURING A MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 CORRODD BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERRNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM (SRM EMB 145.1142 REV 20) CHAPTERS 53-21-10 FIG 201. (M) 2L72 4F RTT00011AT 20030430000882003043000088SO 2003 4 30 SIMA200309013 120030307A532014521725615 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION AFT SILL PLATE CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DOOR SILL IAW EMB 135 51-40-02. (M) 2L72 4F RTT00011AT 20030430000952003043000095EU 2003 4 30 USAASA03028 120030325A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19709UW 0997 LGA - THE EMEGENCY LIGHTS SYSTEM FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE BATTERY AT THE RIGHT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030430000962003043000096EU 2003 4 30 USAASA03024 120030318A3350321430 BATTERY PACK AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19704US 0922 PHL - THE EMERGENCY POWER SUPPLY UNIT, FORWARD BATTERY PACK, WAS INOPERATIVE IN THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACK. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030430001062003043000106NM 2003 4 30 03116428 120030426A3397 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCONNECTED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27428FJ 3193 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISCOVERED THE FOWARD SECTION OF THE EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL RESCURED A CONNECTOR AND PERFORMED AN OPERATIONAL CHECK THAT WAS GOOD. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030430001072003043000107NM 2003 4 30 QXEA0300509 120030427A2120 SMOKE DHAV DHC8 DHC8202 2809007NM COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09345PH 476 SEA - FLIGHT 2246 - FLIGHT ATTENDANT AND FIRST OFFICER REPORTED SMOKE AND HAZE IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND GROUND RAN BOTH ENGINES. BOTH ENGINES WERE RAN SEPARATELY AND AT VARIOUS POWER SETTINGS WITH THE BLEEDS OPERATING. COULD NOT DUPLICATE WRITEUP. AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20030430001082003043000108CE 2003 4 30 GLBA2003057 120030428A5270 SWITCH BEECH 1900 1900D 1154162CE CARGO DOOR OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03150GL UE150 CARGO DOOR ILLUM IN FLIGHT, CLEANED CARGO DOOR SWITCHES PERFORMED ADJUSTMENT PROCEDURES OPS CHECKED GOOD. 2L72 4T RTA24CE 20030430001102003043000110NM 2003 4 30 CALA0300228 120030427A2120 SMOKE BOEING757 757224 1384958NM COCKPIT DETECTED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0958101 27291 ENROUTE FROM EWR TO LIM THE AIRCRAFT DIVERTED TO GCM FOR SMOKE IN THE CABIN. NO EICAS MESSAGES DISPLAYED. PERFORMED FIM FOR OVERBOARD EXHAUST VALVE AND COOLING TEST. NO PROBLEMS NOTED. INSPECTED RECIRC FANS (LEFT AND RIGHT), INSPECTED AND CLEANED ALL SMOKE DETECTORS, INSPECTED TUNNEL AREA FOR EVIDENCE OF RUNNING PACKS. UNABLE TO DUPLICATE PROBLEM. PERFORMED ENGINE RUN-UP AND INSPECTED SUPPLY FANS, RECIRC FANS, FILTERS, AUX FAN, DETECTORS, EQUIPMENT RACK, AND ALL POSSIBLE WIRING AND COMPONENTS IN THE TUNNEL AREAS. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT PERFORMED AN EVALUATION FLIGHT WITH NO DISCREPANCIES NOTED. ALL ELECTRICAL AND COOLING SYSTEMS CHECK NORMAL. 2L72 4F RTA2NM 20030430001292003043000129 2003 4 30 SWAA030920 420030421A2565D31354 INDICATOR BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030430001682003043000168 2003 4 30 SWAA030866 420030417A2565D31354 SLIDE BOEING737 7373H4 1384600NM PAX DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030430001792003043000179NM 2003 4 30 SWAA030900 120030420A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED (6 EA) AT BS 639 AT STR 4L, BS 727D AT STR 7L, BS 727D AT STR 3L, BS 727E AT STR 3L, BS 500D AT STR 5L & BS 520 AT STR 7L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030430001802003043000180NM 2003 4 30 SWAA030899 120030420A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED (7 EA) AT BS 597 AT STR 3R, BS 639 AT STR 4R, BS 727 AT STR 6R, BS 867 AT STR 4R, BS 867 AT STR 5R, BS 500D AT STR 8R & BS 520 AT 6R. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030430001962003043000196NM 2003 4 30 SWAA030930 120030427A53306545768 SKIN BOEING737 737317 138447PNM FUSELAGE BULGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN BULGED AT BS 380, BETWEEN STR 16L & STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430002232003043000223SO 2003 4 30 SWIA200311915 120030425A2751 WARNING LIGHT EMB 120 EMB120ER 3260203SO TE FLAPS ILLUMINATED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07214SW 120280 IN FLIGHT CLIMBING THROUGH 7,000 FEET, THE FLAP DISAGREEMENT LIGHT ILLUMINATED. COULD NOT CLEAR VIA QRH. RETURNED TO SLC. INSPECTED FLAPS. NO DEFECTS FOUND. PERFORMED FLAP FUNCTIONAL CHECKS IAW MM 27-50-00. OPERATIONAL CHECKS SATISFACTORY. NO DEFECTS NOTED AT THIS TIME. 2L72 4T RTA31SO 20030430002342003043000234NM 2003 4 30 XNOA01111 120030411A5270 CONNECTOR BOEING727 727227 1384078NM MLG DOOR MALFUNCTIONED A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL2376753 ON DEPARTURE FROM ICT RT MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLE LANDING GEAR PER CHECK LIST. DOOR LIGHT OUT. CLEANED AND RECONNECTED CONNECTOR ON RT DOOR SWITCH. OPS CHECK GOOD IAW 727 MM 32-10-00. 2L73 4F A3WE 20030430002372003043000237EU 2003 4 30 2003F00224 120030413A5630MBK117241006 WINDOW BOLKMS117 BK117B2 5626013EU CREW DOOR SEPARATED E GVNAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 SW09220HH 7215 DURING CLIMB OUT, GOING THROUGH 600 FT, THE SLIDING WINDOW OF THE PILOT'S DOOR WINDOW DEPARTED THE AIRCRAFT. MAINTENANCE FOUND THE TRACK WHERE THE SLIDING WINDOW RIDES WAS DEBONDED FROM THE WINDOW. TRACK WAS REGLUED WITH EPOXY RESIN AND SECURED TO THE WINDOW WITH PANHEAD SCREWS AND NUTS. SOME DEBONDING DETECTED ON WINDOW TRACKS OF OTHER BK117S IN THE FLEET. ALL WINDOW TRACKS ON ALL WINDOWS ON ALL BK117S AND BO105 IN THE FLEET WERE INSPECTED, REBONDED AS NEEDED AND SECURED WITH SCREWS AND NUTS. 1G72 3U NCH13EU 20030430002402003043000240NM 2003 4 30 AWXA200300367 120030327A5320654795712 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK THE AFT CARGO DOOR CUTOUT LOWER SUPPORT WEB ANGLE AT BS 837, STR 25 RT WAS FOUND DAMAGED. MAINTENANCE CUT OUT DAMAGED SECTION OF AFT CARGO DOOR CUTOUT LOWER SUPPORT WEB ANGLE AT BS 837, STR 25 RT; FABRICATED A FILLER AND 2 EACH PLATES; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-12, PG 1-3, & 6, FIG 1. 2L72 4F RTA16WE 20030430002422003043000242WP 2003 4 30 MWEA030168 120030414A57555910055501 SKIN DOUG DC9 DC915 3022036WP SPOILER DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 LEFT WING GROUND SPOILER HAS A DENT 2 X .058 INCH DEEP. CUT OUT DAMAGE, HOT BOND ON REPAIR DOUBLER. 2L72 4F A6WE 20030429000562003042900056NM 2003 4 29 DHL2003743009 120030411A2611 SMOKE DETECTOR BOEING727 727225 1384077NM INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 THE 6R SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED STATION 6R SMOKE DETECTOR IAW M/M 26-16-01. OPS CHECKED GOOD. 2L73 4F A3WE 20030429000692003042900069SO 2003 4 29 QE52003F00000 120030324A28108402917 TANK PIPER PA46 PA46350P 7104602SO LYC O540 TIO540* 41532EA FUEL SYS LEAKING B QE5RO OTHER K FLUID LOSS NRNOT REPORTED 1 NM07775RD 4622174 THE TANK WAS BROUGHT FOR WELD REPAIR OF LEAKING WELD SEAMS. THE TANK WAS SUCCESSFULLY REPAIRED AND PASSED PRESSURE TEST. WHILE ACCOMPLISHING THE WELD REPAIR, THE DEPTH OF WELD PENETRATION OF ORIGINAL WELD WAS OBSERVED. THE AMOUNT OF PENETRATION IS MINIMAL AT BEST. BECAUSE THIS IS A FUEL TANK, THIS CRS BELIEVES THERE IS A POTENTIAL FOR FIRE AND CATASTROPHIC FAILURE. I WOULD SUGGEST THAT A NDT INSPECTION BE PERFORMED TO DETERMINE THE DEPTH OF WELD PENETRATION TO ENSURE SOUND WELD JOINTS. 1L71 3O3 ORTA25SO E14EA 20030429000772003042900077NM 2003 4 29 P5CA0300822 120030410A5347 SEAT TRACK BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 SEAT TRACK STA 970 LBL 98.58 LEVEL 1 CORROSION. REPAIRED SRM 53-10-05 1A. 2L74 4F A20WE 20030430000362003043000036EA 2003 4 30 COMA0360217 120030425A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01920CA7791 979 7022 FLIGHT 5786 LANDING GEAR DISAGREE WARNING, NOSE LANDING GEAR DID NOT EXTEND. COULD NOT DUPLICATE, LANDING GEAR OPERATION NORMAL. REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. 2L72 4F RTA21EA 20030430000532003043000053NM 2003 4 30 2003UALA00384 120030416A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 A GOUGE WAS FOUND ON THE FWD LOWER CORNER OF THE FUSELAGE SKIN AT APPROXIMATELY BS 300-S17R. 2L72 4F4 FRTA16WE E2GL 20030430000612003043000061NM 2003 4 30 USAA030033 120030326A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US 22959 PIT - FOUND SKIN CRACKED 1.5 INCHES, AT ICE LIGHT, BS 727D AT S23R. DAMAGED SKIN CUTOUT, INSTALLED REPAIR DOUBLER AND TRIPLER PER EA 87064A. (M) 2L72 4F RTA16WE 20030430001562003043000156 2003 4 30 SWAA030879 420030420A2565 GIRT BAR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20030430002102003043000210 2003 4 30 VNAA0304015 420030417A3418 CONTROLLER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT STALL WARNINGFAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07430JS 3044 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND PUSHER AND AOA FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGES CLEARED AND FLIGHT 4154 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4154 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002202003043000220SO 2003 4 30 C2XA03IA042 120030427A32221170C000004 STRUT EMB 145 EMB145LR 3260212SO NLG UNDERSERVICED A C2XAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW2713553 145585 IAH- FLIGHT 2538, THE CREW NOTED AFTER TAKEOFF THAT THE LANDING GEAR WOULD NOT RETRACT, AIR/GROUND SENSOR FAILURE ON EICAS. FOLLOWED QRH. THE CREW RETURNED THE AIRCRAFT TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE SERVICED THE NOSE LANDING GEAR SHOCK ABSORBER IAW EMB 145 AMM 32-20-01,PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION, AND, RETRACTION IAW EMB145 AMM 32-30-00, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030430002322003043000232EU 2003 4 30 BAQA085883 120030401A641011731743 BLADE BOLKMS117 BK117A1 5626010EU TAIL ROTOR PEELING E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME1411 7243 TAIL ROTOR BLADE HAS PAINT PEELING OFF. UNABLE TO BALANCE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030430002452003043000245WP 2003 4 30 MWEA030173 120030414A57525910047501 STRUCTURE DOUG DC9 DC915 3022036WP AILERON TAB DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 LEFT AILERON TAB HAS A DENT LOCATED AFT OF THE THIRD HINGE OUTBOARD TRAILING EDGE DENT 2 X .080 INCH DEEP. REPAIRED AND BALANCED AILERON CONTROL TAB. 2L72 4F A6WE 20030430002472003043000247WP 2003 4 30 MWEA030167 120030414A575559100055512 PANEL DOUG DC9 DC915 3022036WP SPOILER DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 RIGHT CENTER SPOILER PANEL HAS A DENT 2.5 X .052 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE AND BOND EXISTING DOUBLER. 2L72 4F A6WE 20030430002572003043000257NM 2003 4 30 SWAA030818 120030411A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F A16WE 20030430002632003043000263NM 2003 4 30 SWAA030824 120030410A335057771 CAP BOEING737 7372H4 138448CNM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP BROKEN IN FWD CABIN. REMOVED AND REPLACED EEPLS END CAP PER MM. 2L72 4F A16WE 20030430002692003043000269NM 2003 4 30 VNAA0304007 120030412A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07430JS17308565 3044 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 1D WAS NOT ILLUMINATING. MAINTENANCE INSPECETED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030501000072003050100007WP 2003 5 1 AALA20030240 120030210A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21461AA 49566 TUL - FOUND LONGERON 4L AT STATION 200 CRACKED IN RADIUS LONGERON 4L CRACKED TWO PLACES AT INBOARD AND OUTBOARD FASTENERS ATTACHED TO FRAME STATION 160. REMOVED AND REPLACED LONGEORN 4L FROM STATION 148.55 TO STATION 218 PER B/P SRM 53-02-00. (M) 2L72 4F A6WE 20030501000242003050100024WP 2003 5 1 AALA20030235 120030129A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 TUL - FOUND CRACK FS 503. INSTALLED REPAIR DOUBLER ON FRAME REF SRM 53-10-00-30. (M) 2L72 4F A6WE 20030501000292003050100029WP 2003 5 1 AALA20030196 120030204A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21417AA 49328 TUL - FOUND CRACK IN FUSELAGE SKIN AT RIVET STATION 1380 BETWEEN L14 AND L15 LEFT SIDE. STOP DRILLED CRACK SPECIFIED QA242. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M) 2L72 4F A6WE 20030501000452003050100045EA 2003 5 1 ASOA03102 120030311A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11913EV 7731 FLT 4414 - DURING A GROUND INSPECTION IN MGM, THE RIGHT EXTERIOR EMERGENCY LIGHT ADJACENT TO THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT LAMP ADJACENT TO THE SERVICE DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030501000462003050100046EU 2003 5 1 ASOA03114 120030316A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11633AS15383 344 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030501000662003050100066WP 2003 5 1 GTIA030196 120030218A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND CABIN FLOORBOARD STATION 826-864, DELAMINATED. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20030501000672003050100067WP 2003 5 1 GTIA020197 120030218A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND CABIN FLOOR PANEL STATION 886-927 DELAMINATED. FABRICATED FLOOR PANEL. (M) 2L72 4F RTA6WE 20030501000682003050100068WP 2003 5 1 GTIA030202 120030304A5553 ANGLE DOUG DC9 DC983 3022083WP VERTICAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND RIGHT DORSAL FIN ATTACH ANGLE INNER ANGLE CRACKED IN RADIUS. REMOVED RIGHT DORSAL FIN ATTACHED INNER ANGLE. DRILL AND LOCATE NEW INNER ANGLE. INSTALLED NEW INNER ANGLE. UPON REMOVAL OF RIGHT DORSAL FIN ANGLE FOUND LEFT GUSSET TO BE CRACKED. REMOVED CRACKED GUSSET. LOCATED AND DRILLED NEW GUSSET. INSTALLED NEW GUSSET. (M) 2L72 4F RTA6WE 20030501000842003050100084SW 2003 5 1 2003F00238 120030104A5230 MECHANISM FRCHLDSA227 SA227DC 3377521SW CARGO DOOR LACK OF LUBE A BSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM05453LA DC852B FLT 2561 - OLF - DURING CLIMB, THE CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHT CAME ON AT CABIN PRESSURE OF 2 PSID. PASSENGER REPORTED NOISE FROM AFT OF AIRCRAFT. CREW RETURNED TO STATION, LIGHT WENT OUT AS ENGINES WERE SHUT DOWN. DOOR CLOSING PROCEDURES OR DOOR HARD TO CLOSE. CLEANED AND LUBED CLICKS, ADJUSTED LOWER AFT CLICK CLACK AND REINDEXED LINKAGE. (M) 2L72 4T RTA18SW 20030424000602003042400060EA 2003 4 24 JBXA03002 120030319A3620356024310 SENSOR CNDAIRCL600 CL6002B19 1900309EA NR 1 ENGINE MALFUNCTIONED A JBXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO05592ML 7410 FLT 5135 TYS - BHM. ON CLIMB HAD L 14TH DUCT FAIL MSG ON EICAS. PERFORMED EMER 6-4 CHECKLIST, SHUTDOWN NR 1 ENG. DIVERTED BACK TO TYS. REMOVED AND REPLACED LT PYLON SENSING ELEMENT IAW CRJ MM 36-21-04. OPS CHECK GOOD. 2L72 4F RTA21EA 20030424000642003042400064NE 2003 4 24 MALA030204 220030212A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT MALFUNCTIONED A MALAB EMER. DESCENT YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 GL15443XJ 340B443 DURING DESCENT TO MSP AT 12,500 FT, POPPING SOUND CAME FROM RT ENGINE FOLLOWED BY SIMULTANEOUS ENGINE OVER-TEMP AND IGNITION LIGHT ILLUMINATION. ITT WENT TO 1058 (FOR 10 SECONDS) TORQUE AT 20 PERCENT NG WAS NORMAL ALONG WITH ALL OTHER ENGINE INDICATIONS. CONDUCTED MEMORY ITEMS FOR ENGINE FAILURE INFLIGHT. AS SOON AS RIGHT POWER LEVER WAS RETARDED ENGINE RESTORED ITSELF WITH ALL INDICATIONS BEING NORMAL. OAT WAS -14 DEGREES CELSIUS, WITH CLEAR CONDITIONS THE ENTIRE FLIGHT ENGINE OPERATED NORMAL FOR REMAINED OF FLIGHT. MAINTENANCE REPLACED RT ENGINE REFERENCE WORK PACKAGE 2/12/03 FOR DETAILS. 2L72 4T4 TRTA52EU E8NE 20030424000702003042400070NM 2003 4 24 IU62003F00004 120030221A291065477821 HOUSING BOEING737 737* NM HYD VALVE ERODED B IU6RO OTHER K FLUID LOSS NRNOT REPORTED 1 NM01 PIN HOLE EROSION FROM INSIDE UNIT TO EXTERNAL CAUSING LEAKAGE. EROSION. (CA2 NR 174742) 2L72 4F RTA16WE 20030424000762003042400076NM 2003 4 24 UPS03440339 120030306A5314 KEELBEAM BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:N/A FX - KEEL BEAM BOX EXTERIOR I/B SURFACE FOUND SURFACE CORROSION AT STA 1416 TO STA 1456 LBL 7. (DEPTH 0.055 INCH, WIDTH .75 INCH, LENGTH .75 INCH). CORROSION REMOVED AND REPROTECTED AS PER SRM AND SRM 51-10-02 BLEND OUT DEPTH 0.009 INCH, WIDTH 1 INCH, LENGTH 3 INCHES WITHIN SRM 53-10-01 LIMITS. 2L74 4F RTA20WE 20030424000822003042400082NM 2003 4 24 HNAA0300015 120030323A25202B11261AJE STRUCTURE DHAV DHC8 DHC8201 2809001NM F/A SEAT CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07994HA1574215742 459 DURING MAINTENANCE, THE INBOARD POST OF THE FLIGHT ATTENDANT SEAT WAS FOUND SEVERELY CORRODED AT THE BASE. A NEW POST WAS INSTALLED. THIS AIRCRAFT HAS THE HUNTING INTERIOR. 2H72 4T RTA13NM 20030424001012003042400101EA 2003 4 24 SWIA200311842 120030320A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM DIRTY A SWIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07924SW 7681 STAB TRIM AND MACH TRIM CAUTION MESSAGE RECEIVED IN FLIGHT. RETURNED TO BOI. CLEANED STAB TRIM DISCONNECT SWITCHES. PERFORMED FUNCTIONAL CHECK OF STAB TRIM SYSTEM. FUNCTION CHECKS GOOD IAW 27-40-00. 2L72 4F RTA21EA 20030424001042003042400104CE 2003 4 24 THG2003F00000 120030317A3222HMX5FGM ROD END BEECH 36 A36 1151604CE CONT O520 TSIO520UB 17040SO NLG INOPERATIVE D THGSO OTHER O OTHER NRNOT REPORTED 1 NM0936WP EA13 527577 PILOT HEARD LOUD NOISE DURING FLIGHT AS MAIN LANDING GEAR WAS ACCUATED TO UP POSITION, GOT UNSAFE LANDING GEAR WARNING LIGHT. PILOT ASKED FOR ASSISTANCE FROM LOCAL FBO. ON FLY-BY, PERSONNEL ON GROUND NOTICED THAT NOSE GEAR WAS NOT LOCKED IN DOWN POSITION; BUT WAS SWINGING BACK AND FORTH IN AIRSTREAM. PILOT THEN TRIED TO MANEUVER A/C SO NOSEGEAR WOULD LOCK INTO DOWN POSITION, BUT WITH NO SUCCESS. AS A/C CAME IN FOR LANDING, GEAR WAS CYCLED ONE MORE TIME AND AT THAT TIME .5000 INCH PIECE OF ROD END (REMAINING ON END OF BRAZE/PLUNGER ROD ASSEMBLY), JUST HAPPENED TO ALIGN AND CONNECT WITH REMAINING ROD END BEARING PIECE (LT ON ACCUATOR ARM), AND LOCKED NOSE GEAR INTO DOWN LOCKED POSITION. A/C LANDED SAFELY. 1L71 3O3 O 3A15 E8CE 20030424001152003042400115SO 2003 4 24 LD22003F00001 120030306A32401159SC15043 BRAKE ASSY GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE ROTORS DAMAGED B LD2RK NONE MJ OVER TEMP WARNING INDICATION ININSP/MAINT 1 GL1523M 1442 579 11261 DURING POST FLIGHT INSPECTION, A BRAKE TEMPERATURE OF 980 WAS NOTED ON THE NR 4 BRAKE. THE WHEEL WAS REMOVED AND THE NR 1 ROTOR HAS SEVERAL DRIVE CLIPS COMING OFF. THE BRAKE WAS REPLACED WITH A NEW UNIT. THE NR 4 MAIN WHEEL WAS REMOVED AND SENT OUT FOR INSPECTION DUE TO HIGH TEMP. 2L72 4F4 FRTA12EA E00057EN 20030424001182003042400118NM 2003 4 24 UPS03440341 120030305A5312 FITTING BOEING747 747200 1384847NM BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, LT BS 1480 BULKHEAD CRACK REVEALED ON EXTENSION FITTING HOLE NR 5 APPROX 0.06 INCH LONG RUNNING UPWARD. PLS REFER FIGURE ATTACH. LT 1480 BULKHEAD EXTENSION FITTING HOLE NR 5 REWORKED TO 0.800 AND BUSHING INSTALLED AS PER RS 53-34989. 2L74 4F RTA20WE 20030424001272003042400127WP 2003 4 24 UPS03840350 120030303A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, LONG 17R AND END FITTING ARE CRACKED AT STA 1766. REMOVED, FABRICATED AND REPLACED LONGERON 17R AND END FITTING IAW DWG 5649327 AND 4772397 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20030424001292003042400129WP 2003 4 24 UPS03840352 120030303A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, LONGERON 17L AND END FITTING ARE CRACKED AT STA 1766. REMOVED LONGERON AND END FITTING, FABRICATED LONGERON IAW DWG 5649327. REPLACED FITTING AND INSTALLED LONGERON IAW DWG 4772397 AND SRM 51-1-20D. 2L74 4F RT4A25 20030424001322003042400132WP 2003 4 24 UPS03840355 120030301A52202702833 SHAFT DOUG DC8 DC873F 302199FWP EMERG EXIT HANDLCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C 2, LEFT OVERWING EMERGENCY EXIT DOOR HANDLE AFT LATCH SHAFT FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 2702833 AND SRM 51-3-0. 2L74 4F RT4A25 20030424001392003042400139NM 2003 4 24 F3LA200300114 120030310A5551 FITTING BOEING737 7372Y5 1384554NM HORIZONTAL STAB CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED RT. HORIZONTAL STAB CENTER SECTION, AFT UPPER ATTACH CLEVIS, AFT LUG, CORRODED. REPAIRED PER EA 55-737-077. 2L72 4U RTA16WE 20030424001402003042400140EA 2003 4 24 QXEA0300350 120030226A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 FOUND TWO CRACKS BY LPI IN AFT PRESSURE BULKHEAD. REPAIRED IAW CRJ 700 MM TACK 51-23-00-390-810-A01 AND RO R-29-07. 2L72 4F RTA21EA 20030424001512003042400151EU 2003 4 24 MALA030190 120030309A5270 SWITCH SAAB SF340 340B 7860101EU PAX DOOR OUT OF ADJUST A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15443XJ 340B443 INFLIGHT ON FLIGHT 3294, AT 14,000 FT MAIN DOOR HANDLE CAUTION LIGHT ILLUMINATED, REMAINED ON. COMPLETED QRH, FLIGHT DIVERTED FROM BMI TO AZO DUE TO THE MAIN CABIN DOOR LIGHT ILLUMINATING INFLIGHT. LIGHT OUT THROUGH 10,000 FT. F/A STATED BOTH INDICATORS OFF ALIGNMENT .25 INCH. A/C FERRIED TO DTW FOR REPAIR. MAINTENANCE INSPECTED DOOR HANDLE CAUTION LIGHT SYSTEM, AND ADJUSTED SWITCH IAW SF340 AMM CHAP 52-70. OPERATIONS CHECK GOOD. 2L72 4T RTA52EU 20030428001842003042800184NM 2003 4 28 AWXA200300356 120030323A53136546877143 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.375 INCH CRACK WAS FOUND ON AFT END OF RT STRINGER 18A WEB AT BS 727. MAINTENANCE TRIMMED OUT CRACK AT AFT END OF RT STRINGER 18A SHEAR WEB, BS 727; PERFORMED HFEC INSPECTION OF VERIFY NO CRACKS EXIST. FABRICATED A FILLER AND RADIUS BLOCK; INSTALLED REPAIR PARTS IAW AWA ER 03-5363-03097-TB3. 2L72 4F RTA16WE 20030428001852003042800185SO 2003 4 28 RAIA0030388 120030326A3297D3899921KA98SN CONNECTOR EMB 145 EMB145LR 3260212SO NLG CORRODED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03816HK 145055 STL- THUMPING NOISE COMING FROM NOSE WHEEL WELL. MAINTENANCE INSPECTED AND FOUND LEFT HAND DOWN LOCK PROX SWITCH CONNECTOR CORRODED. REMOVED AND REPLACED CONNECTOR, OPS CHECK OK. 2L72 4T RTT00011AT 20030428001882003042800188 2003 4 28 RAIA00303093 420030330A34207003360948 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU NR 2 AHRS FAULTY A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03551HK114002393 41040 STL- HEADING COMPARATOR ERROR WARNING. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER, OPS CK OK. 2L72 4T RTA41NM 20030428001922003042800192SO 2003 4 28 RAIA00303097 120030401A3350 LIGHT EMB 145 EMB145 3260210SO CABIN DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03801HK 145053 PIT- CABIN EMERGENCY LIGHTS INOP. RE-SECURED WIRE AT EMERGENCY LIGHT TRACK, OPS CHECK OK. 2L72 4F RTT00011AT 20030429000012003042900001 2003 4 29 MALA030231 420030407A3445071015075203 TRANSPONDER SAAB SF340 340B 7860101EU TCAS SYS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15369PX 340B295 INFLIGHT ON FLIGHT 3327, TRANSPONDER INOP. AIR RETURN TO MSP. MAINTENANCE REPLACED TRANSPONDER/TCAS CONTROL HEAD P/N 071015075203, SN/OFF2018, SN/ON1544. TCAS OPS CHECKS GOOD IAW SF340 MM CHAP 34. NR 1 & NR 2 TRANSPONDER CHECK GOOD IAW SF340 MM CHAP 34 AND FAR 43 APP F. ALT REPORTING SYSTEM TESTED GOOD IAW FAR 43 APP E PAR C. 2L72 4T RTA52EU 20030429000042003042900004CE 2003 4 29 DXTA200300007 120030210A2497M22759 WIRE CESSNA500 560CESSNA 2076750CE DC POWER CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07330QS7331 5600329 DURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY ADJACENT TO A SHROUDED FUEL CROSSFEED LINE, AND CABIN OUTFLOW VALVES. SHOULD A FIRE START, IT IS POSSIBLE THAT IT COULD GO UNNOTICED UNTIL THE CROSSFEED SHROUD AND LINE IS BREACHED. 2L72 4F RTA22CE 20030429000052003042900005NM 2003 4 29 P5CA0300791 120030203A5347 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 UPPER LOBE MAIN DECK, CORROSION ON SEAT TRACK LBL 11 BETWEEN STA 1940-1960. CORRODED PORTION SEAT TRACK REMOVED, REINFORCED WITH NEW SEAT TRACK PER SRM 53-11-25 FIG -7. 2L74 4F A20WE 20030429000112003042900011NM 2003 4 29 P5CA0300787 120030216A5730 SKIN BOEING747 747283B 1384867NM RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RT WING L/E LWR SURFACE CORROSION IN LWR SURFACE WS 1280. DAMAGED AREA TRIMMED OUT, REINFORCED WITH DOUBLER PER SRM 57-30-03 FIG -9. 2L74 4F A20WE 20030429000182003042900018NM 2003 4 29 P5CA0300795 120030204A5347 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 STA 1817 / LBL 98 / WL 208 CRACK ON SEAT TRACK. DAMAGED AREA TRIMMED OUT, REINFORCED WITH NEW SEAT TRACK PER SRM 53-10-05. 2L74 4F A20WE 20030429000222003042900022NM 2003 4 29 P5CA0300805 120030405A2720 PEDAL BOEING747 74746NF 13848BTNM RUDDER DISPLACED A P5CAO OTHER O OTHER CRCRUISE 1 WP23450PA 30808 WITH RUDDER SURFACES NEUTRAL RUDDER PEDALS WERE DISPLACED 1-8 UNITS (RIGHT). OPERATIONAL CHECKED PER AMM 27-21-00. OPS CHECK NORMAL. SUSPECT LARGE LATERAL IMBALANCE AS INDICATED ON W/B FORMS. 2L74 4F RTA20WE 20030425000232003042500023SO 2003 4 25 SWIA200311852 120030323A3233 ACTUATOR EMB 120 EMB120ER 3260203SO RT MLG MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07224SW 120294 ON DEPARTURE, RT MAIN GEAR DISAGREEMENT. A & B LIGHTS REMAIN ON AND RIGHT MAIN GEAR WOULD NOT RETRACT AS OBSERVED BY TOWER. RECYCLED THE GEAR 3 TIMES BEFORE RIGHT MAIN GEAR WOULD RETRACT. A & B DISAGREEMENT LIGHTS THEN EXTINGUISHED. RETURNED TO SLC. REPLACED MAIN LANDING GEAR ACTUATOR ON RIGHT SIDE PER MM 32-32-10. OPS CHECK GOOD. 2L72 4T RTA31SO 20030425000252003042500025EA 2003 4 25 SWIA200311854 120030324A3397 GROUND WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSLOOSE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07449SW 7699 EMERGENCY LIGHTS DO NOT COME ON WHEN F/A SWITCH IN ON POSITION. REMOVED CLOSET. INSPECTED GROUNDING STUD N3141 AND TIGHTENED STUD. OPS CHECK GOOD. REINSTALLED GALLEY CLOSET. 2L72 4F RTA21EA 20030425000562003042500056SW 2003 4 25 TU32003F00001 120030318A6420 BEARING BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL TAIL ROTOR DEBONDED B TU3RO OTHER O OTHER NRNOT REPORTED 1 WP07303PS271 23016 ELASTOMERIC DEBONDED FROM BEARING HOUSING. (SN/ LK0326, LK1013, LK0308, LK0810) 1G72 3U3 UNCH9SW E1GL 20030425000892003042500089NM 2003 4 25 QXEA0300396 120030320A5420 DEFLECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND LOWER COWL OIL COOLER AIR DEFLECTOR LEFT HAND FORWARD LIP IS CHAFING ON LOWER COWL. REPAIRED IAW HORIZON AIR EA 6-71-80 AND RD 8/4-71-047. 2H72 4T RTA13NM 20030428001382003042800138EU 2003 4 28 DHL2003367003 120030408A2611 CONTROL BOX AIRBUS300 A300B4203 3930306EU SMOKE DETECTION MALFUNCTIONED A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01367DH 265 CARGO FORWARD COMPARTMENT SMOKE LIGHT CAME ON DURING PUSHBACK. RESET SMOKE DETECTOR BOX. OPS CHECKED GOOD IAW M/M 26-14-00. 2L72 4F RTA35EU 20030424001522003042400152EU 2003 4 24 WRNA200300009 120030317A33404173763 LANDING LIGHT AIRBUS300 A300B4203 3930306EU FAILED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05821SC 211 RT LANDING LIGHT INOP, POPS CONTROL CIRCUIT BREAKER R&R LANDING LIGHT ASSY IAW 33-42-11. OPS CK SATISFACTORY 2L72 4F RTA35EU 20030424001572003042400157SO 2003 4 24 LR7A03012 120030313A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WORN A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND RT FS 891- 902 SKIN PANEL WITH MULTIPLE PATCHES AT RBL 61, WL 200. SKIN SECTION REPLACED IAW SRM SMP 583 51-60 & 51-70 USING .050 2024 T3 PER ED 03-002-5. DOUBLER INSTALLED IAW 51-140-12. NR 2002. 2H74 4T A1SO 20030424001672003042400167SO 2003 4 24 LR7A03022 120030313A5312 DOUBLER LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND LT FS 924 BULKHEAD UPPER WEB REPAIR DOUBLER CRACKED AT LBL 66, WL 270. DOUBLER REPLACED IAW SRM SMP 583 51-140-12. NR 2157. 2H74 4T A1SO 20030424001752003042400175SO 2003 4 24 LR7A03030 120030313A5730 SKIN LKHEED382 382G 526414USO LT & RT WING CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5711 FOUND UPPER SURFACE OWS 173-241 T/E PANELS CRACKED LT AND RT. SKIN PANELS REPLACED IAW LAC MEA 382-57-03-020. NR 2232. 2H74 4T A1SO 20030424001812003042400181SO 2003 4 24 LR7A03036 120030313A5310 STRUT LKHEED382 382G 526414USO FUSELAGE DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE FS 814 STRUT DENTED AT RBL 61, WL 215. REPAIRED IAW LAC MEA 382-53-03-027. NR 2325. 2H74 4T A1SO 20030424001842003042400184WP 2003 4 24 ZW0A0303403 120030323A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BURNED OUT A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139628W 53598 THE EGRESS LIGHTS WERE INOPERATIVE AT THE FIRST ROW, ROW 8, ROW 20 TO 26, AND ROW 31. REPLACED LAMP P/N 7732 AT FIRST ROW, REINSTALLED LAMP AT ROW 8, RESEATED BATTERY ROW 20 TO 26, AND REINSTALLED LAMP AT ROW 31. CHECK-C 12-23-2002 STL. 2L72 4F RTA6WE 20030423000362003042300036NM 2003 4 23 AUS20030270 120030102A5711 SPAR BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING REAR LOWER SPAR CONTAINED LEVEL 3 CORROSION AT WS 200. FOUND DURING CPCP INSPECTION IAW C57-581-03. 2L73 4F4 FRTA3WE E2EA 20030423000682003042300068 2003 4 23 BAQA085814 420030324A34105209130004 INDICATOR BOLKMS117 BK117A3 5626015EU HSI MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UB511 7062 HSI VERTICAL FLAG WILL NOT PULL. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030423001202003042300120EU 2003 4 23 U30A200300007 120030302A3350 LIGHT AIRBUS320 A320212 3930322EU EMERGENCY MALFUNCTIONED A U30AO OTHER O OTHER CRCRUISE 1 EA17265AV 427 DURING CRUISE ON FLT 307 CUN-PIT, THE LEFT MID CABIN & AFT EMERGENCY EXIT LIGHTS (OVER EXITS) WENT INOP. ON GROUND IN PIT RECYCLED EMERGENCY LIGHT ARM SWITCH & CIRCUIT BREAKER. OPERATIONALLY CHECKED ALL EMERGENCY LIGHTS GOOD PER TASK 33-51-00-710-060 AND AMM 33-51-00-401. 2L72 4F RTA28NM 20030423001212003042300121 2003 4 23 U30A200300008 420030310A2210B546CAM0103 COMPUTER AIRBUS320 A320214 3930316EU ZONE 128 FAULTY A U30AO OTHER J WARNING INDICATION CRCRUISE 1 EA17262AV1572 1572 1725 DURING CRUISE ON FLT 0441 CUN-CLE, NR 2 FMGC WILL NOT RESET AND AUTOPILOT NR 2 WOULD NOT ENGAGE AS A RESULT. DEFERRED PER MEL 22-10-01. ON MARCH 11, 2003, REPLACED NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) IAW AMM 22-83-34-400-001. TESTED AFS OK. PERFORMED CROSSLOAD IAW AMM 22-70-00-610-007. PERFORMED RETURN TO SERVICE REQUIREMENTS FOR RVSM. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030423001342003042300134EU 2003 4 23 U30A200300009 120030312A3350 LIGHT AIRBUS320 A320212 3930322EU EMERGENCY MALFUNCTIONED A U30AO OTHER O OTHER CRCRUISE 1 EA17265AV 427 IN CRUISE DURING FLT 315 RSW-BWI AND THEN ON DESCENT, THE EMERGENCY EXIT LIGHTS IN REAR OF AIRCRAFT AND ON AFT DOORS NOT LIGHT, INOPERATIVE. OTHERS AT MID CABIN AND FWD WORK. PERFORMED BITE TEST ON THE CABIN INTERCOMMUNICATIONS DATA SYSTEM (CIDS) PER TASK 23-73-00-740-003 (EMERGENCY BATTERY CAPACITY TEST). RECYCLED EMERGENCY EXIT LIGHT SWITCH IN COCKPIT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030423001472003042300147WP 2003 4 23 ZW0A0303007 120030306A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 AT STA 169 THE FRAME WAS DAMAGED AT LONGERON 19R TO 20R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030423001562003042300156NM 2003 4 23 UPS03M40284 120030214A5347S4929147707576 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP INSPECTION TYPE: C CABIN CORROSION ON SEAT TRACK BETWEEN STA 1721-1761 AS MARKED ON X=8.5. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 32 AT SEAT TRACK STA 1721-1761, X-8.5 EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1 REV 32. DAMAGED PORTION OF SEAT TRACK REMOVED AND NEW SEAT TRACK INSTALLED. 2L73 4F RTA22WE 20030423002062003042300206NM 2003 4 23 UPS03240306 120030214A5310 FLANGE BOEING727 727108C 1384039NM LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, LEFT MAIN WHEEL WELL BS 930 FITTING SUSPECT CRACK ON I/B VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-04, 53-10-3, 53-10-4, 51- 10-02 & 51-40-3 & DRAWINGS 65-16336 & 65C15732. 2L73 4F A3WE 20030424000692003042400069NE 2003 4 24 MWEA030143 220030321A7320226195 PACKING DOUG DC9 DC914 3022034WP PWA JT8 JT8D7B 52053NE ENGINE LEAKING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31700ME 45696 EPR DROPPED DOWN TO DOWN SLIGHTLY ADVANCED THROTTLE, POWER CAME ON BACK AFTER A FEW MORE MINUTES, POWER STARTER FALLING AGAIN. REMOVED AND REPLACED RIGHT PRESSURE AND DUMP VALVE LINE PACKING. 2L72 4F4 F A6WE E2EA 20030428002022003042800202NM 2003 4 28 0300766739 120030405A5414 SKIN BOEING747 747251F 1384898NM NR 3 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01639US 23887 DURING H-CHECK, FOUND CRACK IN SKIN OF NR 3 PYLON AT ACCESS PANEL NR 473CL CUTOUT. REPAIRED PER EA 67-165062. 2L74 4F A20WE 20030429000242003042900024NM 2003 4 29 PCA0300816 120030130A5320 PANEL BOEING747 747283B 1384867NM CABIN CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 UPPER DECK SIDE WALL CRACKS ON CLIPS 500-520 RT SIDE STRINGER 8, 9, 10, 10A, 11A & 12. FABRICATED NEW CLIPS PER SRM 51-40-03, 51-10-02, 51-30-02, 51-11-01. 2L74 4F A20WE 20030429000402003042900040EA 2003 4 29 COMA0370010 120030407A3610GG670803203 GASKET CNDAIRCL600 CL6002C10 1390015EA BLEED AIR DUCT MISINSTALLED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01374CA25 10090 FLIGHT 5814 LT BLEED AIR DUCT WARNING. REPLACED IMPROPERLY INSTALLED GASKET ON EXTERNAL AIR CONNECTOR. 2L72 4F RTA21EA 20030429000432003042900043EA 2003 4 29 COMA0360188 120030409A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01977CA 7157 FLIGHT 5485 LT ENGINE REVERSER UNLOCKED MESSAGE. SECURED T/R AND DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20030429000442003042900044NE 2003 4 29 DXTA200300009 220030316A7261 ENGINE BRAERO1000 HAWKER1000 7450005EU PWA 305 PW305 NE LT & RT ENGINE OVERSERVICED E DXTAA UNSCHED LANDING WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07551QS 259051 IN FLIGHT DENSE BLACK SMOKE CAME OUT OF THE COPILOTS AIR CONDITIONER VENT. SHORTLY AFTER THAT REAR BAGGAGE SMOKE ANNUNCIATOR ON THE MASTER WARNING PANEL ILLUMINATED. 2L72 4F4 FRTA3EU E35NE 20030429000542003042900054EA 2003 4 29 03101622A 120030411A335060205 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHT AT THE LOWER LEFT OF THE CABIN SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030429000632003042900063EA 2003 4 29 SWIA200311869 120030403A4930 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA APU FIRE A SWIAF ACTIVATE FIRE EXT. BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 NM07591SW 7079 ON POSTFLIGHT, NOTICED SMOKE COMING FROM APU VENT. POWERED UP AIRPLANE AND APU FIRE BELL WITH LIGHT CAME ON FOR ABOUT FIVE SECONDS. POWER FUEL SWITCH WAS IN; I PRESSED OUT THE SWITCH. BOTTLE FIRED WHEN A/C WAS ADDED. REMOVED APU, INSPECTED FUEL MANIFOLD. REPLACED BOTH IGNITERS. PERFORMED LEAK CHECK WITH AIR OF FUEL SYSTEM. NO DEFECTS NOTED ON FUEL FEED SYSTEM. REINSTALLED APU PER CRJ MM 49-10-00. 2L72 4F RTA21EA 20030429000752003042900075NM 2003 4 29 P5CA0300823 120030410A5753 WEB BOEING747 747283B 1384867NM TE FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RIGHT WING INBOARD MID FLAP INBOARD WEB CRACKED. SPRING ROD CUT OUT, REPAIRED PER SRM 51-40-02 FIG 01. 2L74 4F A20WE 20030429000792003042900079NM 2003 4 29 P5CA0300826 120030410A5414 ACCESS PANEL BOEING747 747283B 1384867NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 NR 3 PYLON ACCESS PANEL CUTOUT LWR AFT CORNER CRACKED. REPAIRED PER SRM 54-34-03 FIG 23. 2L74 4F A20WE 20030429000882003042900088WP 2003 4 29 03FDEA00433 120030411A5310 STRUCTURE DOUG DC10 DC1030 3023501WP LT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 LEFT MLG W/W AFT O/B STRUCTURE HAS CRACKED L-ANGLE. CLOSING ACTION ON 04/11/03. REMOVED ANGLE IAW SRM 51-31-01, FAB ANGLE ON TRAVLER T2/325914. INSTALLED ANGLE IAW SRM 51-31-01. 2L73 4F A22WE 20030429000922003042900092CE 2003 4 29 GVR2003F00001 120030225A25105519009 SEAT CESSNA500 550 2076604CE PWA JT15 JT15D1 52060NE CABIN CRACKED B GVRRO OTHER O OTHER NRNOT REPORTED 1 CE05187TA 5500257 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. 1L72 4F4 F A22CE E1NE 20030429000952003042900095NM 2003 4 29 CH1A200395010 120030410A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON LBL 45 SEAT TRACK FS 1000 TO FS 1140. 2L73 4F A3WE 20030429001122003042900112SO 2003 4 29 RAIA00304100 120030403A2760M83536 RELAY EMB 145 EMB145 3260210SO SPOILER WARNING FAILED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03803HK 145077 PIT- SPOILER FAIL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED RELAY K0362, OPS CHECK OK. 2L72 4F RTT00011AT 20030429001262003042900126CE 2003 4 29 CWQ2003F00004 120030221A32106521642 BRACKET CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE MLG UPLOCK BROKEN B CWQRK NONE O OTHER ININSP/MAINT 1 GL05800QS 785 5600598 DURING ROUTINE INSP OF GEAR CYCLE AND UPLOCK CHECKS NOTICED THAT RT MAIN GEAR HAD PROBLEMS IN UP AND LOCKED POSITION. UPON FURTHER INSP FOUND (PN 6521641-2) UPLOCK HOOK ATTACH BRACKET CRACKED 2.25 INCHES, STARTING FROM LOWER EDGE OF BACKET MOVING IN VERTICAL DIRECTION UPWARD THRU 3 OF 4 ATTACH FASTENERS(HI-LOCKS). BRACKET IS MOUNTED ON VERTICAL STRINGER ON REAR FACE OF FORWARD SPAR. SINCE CRACK STARTS FROM BOTTOM AND MOVE UPWARD IT APPEARS THAT GEAR WAS HITTING IT ON UPWARD STROKE DURING RETRACTION AND NOT CAUSED BY WEIGHT OF GEAR RESTING IN THE HOOK WHEN UP AND STOWED. REMOVED MAIN GEAR ACTUATOR AND BROKEN BRACKET AND SENT TO MFG FOR EVALUATION, AWAITING RESULTS. 2L72 4F4 FRTA22CE E00053EN 20030429001372003042900137NM 2003 4 29 AUS20030290 120030212A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 30 CONTAINED LEVEL 2 IN AREA LOCATED AT BS1010. FOUNDDURING INSPECTION IAW CPCP C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030424000842003042400084NM 2003 4 24 F3LA200300106 120030228A5320 CHANNEL BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED SUPPORT CHANNEL CORRODED IN FWD CARGO COMPARTMENT FROM STA. 380 TO STA. 500D, LBL 24. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-01, FIG. 3 AND SRM 51-10-02, PARA. 7, SRM 53-30-53, FIG. 203, AND SRM 51-20-01. 2L72 4F RTA16WE 20030424000872003042400087NM 2003 4 24 QXEA0300385 120030321A521085217008101 SEAL BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DAMAGED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09403QX 4037 SEA-ON FLIGHT NUMBER 2398, ON CLIMBOUT, FLIGHT ATTENDANT REPORTED LOUD RUSHING NOISE COMING FROM MAIN CABIN DOOR. NOTICED AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO FIELD. INSPECTED MAIN CABIN DOOR SEAL AND FOUND SEVERAL CUTS. REMOVED AND REPLACED SEAL. GROUND RAN AND PRESSURIZED AIRCRAFT. SEAL INFLATES, NO LEAKS NOTED AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424001052003042400105WP 2003 4 24 MWEA030144 120030326A53209912243228 SHEAR TIE DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 SHEAR TIE IS CRACKED AT FRAME STATION 1309 ABOVE LONGERON 16 RIGHT. FABRICATED AND INSTALLED TWO SHIMS AND NEW SHEAR TIE. 2L72 4F A6WE 20030424001232003042400123WP 2003 4 24 UPS03840340 120030322A3350 BATTERY DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 EMERGENCY EXIT LIGHTS INOP. REMOVED NAD REPLACED BATTERY AND RELAY UNIT AND OPS CHECKED GOOD PER MM 33-50-01. 2L74 4F RT4A25 20030424001442003042400144NM 2003 4 24 QXEA0300372 120030313A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - TOP WING TO FUSELAGE AFT APERTURE FOR PANEL 261HT IS CHAFED. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030424001862003042400186WP 2003 4 24 ZW0A0303404 120030323A3350 COVER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT MISSING A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139628W 53598 THE LEFT SIDE NUMBER 2 CABIN DOOR EMERGENCY LIGHT COVER WAS MISSING, AND BOTH OVERWING EXIT LIGHTS WERE INOPERATIVE AT ROW 21. REPLACED MISSING LIGHT COVER P/N 0105610, AND RESEATED THE BATTERIES FOR THE OVERWING EXIT LIGHTS. CHECK-C 12-23-2002 STL. 2L72 4F RTA6WE 20030424001912003042400191WP 2003 4 24 MWEA030150 120030328A5420 COVER DOUG DC9 DC981 3022081WP LT ENGINE ISO CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LEFT ENGINE UPPER ISOLATOR COVER PLATE HAS LITE CORRSION ON THE TOP. REMOVED AND INSTALLED ISOLATOR COVER PLATE. 2L72 4F A6WE 20030424002072003042400207WP 2003 4 24 UPS03840367 120030312A5310 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, EMPANAGE RT FITTING CRACKED FROM RBL2 - RBL 8 SECOND J-BEAM FROM BELLY SKIN. PERFORMED HFEC IAW NDT SPM 06-10-01, .001 CRACK FOUND ON FITTING. REMOVED FITTING TO FOM. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030425000042003042500004WP 2003 4 25 UPS03840383 120030313A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, EMPENNAGE L17R END FITTING AND LONGERON CRACKED FROM FS 1768-1778. REMOVE L17 RT LONGERON AND FITTING REMOVED SHEAR CLIP AND TEAR STRIP AT FS 1766 & 1708. LOCATED AND DRILLED NEW LONGERON SECTION AND FITTING. INSTALLED LONGERON END FITTING SHEAR CLIP AND TEAR STRAP IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030425000092003042500009WP 2003 4 25 UPS03840390 120030301A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, A/C ACCESSORY BETWEEN STA 55 TO 70 BETWEEN LONG 24L TO 25L FRAME 55 IS CRACKED AT SUPPORT ROD. REPAIRED FRAME 55 BY THE FABRICATION AND INSTALLATION OF FRAME SECTION AND SPLICES IAW DC8 SRM 53-2-0 51-1-21 AND 51-1-21D. 2L74 4F RT4A25 20030425000152003042500015EU 2003 4 25 MALA030211 120030327A26131734362450 SENSOR SAAB SF340 340B 7860101EU TAILPIPE HOT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15423XJ 340B423 AFTER TAKEOFF OF FLIGHT 3082, RT TAILPIPE HOT LIGHT CAME ON. FOLLOWED QRH TURNED OFF BLEED. RIGHT TAILPIPE HOT LIGHT WENT OUT AND BACK ON 3 TIMES. THEN OUT FOR GOOD. NO OTHER ABNORMAL ENGINE INDICATIONS. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED ALL THREE TAILPIPE SENSORS P/N 17343-62-450. OPS CHECKS GOOD IAW AMM 26-12-05-2. 2L72 4T RTA52EU 20030425000222003042500022NM 2003 4 25 KPVA20039 120030226A256010005511 LIGHT DHAV DHC8 DHC8103 1386005NM COCKPIT INOPERATIVE A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13806WP 357 COCKPIT PORT EMERGENCY LIGHT, LOW BATTERY CHARGE. REMOVED AND REPLACED PORT EMERGENCY LIGHT. OPS CHECK GOOD. 2H72 4T RTA13NM 20030425000422003042500042WP 2003 4 25 ZW0A0303502 120030326A3350408822101 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY SIGN INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139302B 49528 THE FWD OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 10-1-02 STL. 2L72 4F RTA6WE 20030425000472003042500047NM 2003 4 25 UPS03440396 120030309A5210 SKIN BOEING747 747200 1384847NM PAX DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, MAIN DOOR - R4 DOOR UPPER HINGE CUTOUT LOWER WEB FOUND CORROSION CRACKED. M/D - R4 DOOR UPPER HINGE CUTOUT LWR WEB REPLACED AS PER SRM 51-10-01 P8. 2L74 4F RTA20WE 20030425000582003042500058SW 2003 4 25 TU32003F00004 120030318A6220222310503101 BEARING BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL MAIN ROTOR DEBONDED B TU3RO OTHER O OTHER NRNOT REPORTED 1 WP07303PS2469 23016 RUBBER DEBONDED BEYOND LIMITS. 1G72 3U3 UNCH9SW E1GL 20030425000662003042500066CE 2003 4 25 ZES2003F00000 120030301A5397 WIRE RAYTHNDH125 HAWKER800 7450004CE GARRTTTFE731TFE7312B WP FUSELAGE SHORTED E ZESAO OTHER O OTHER NRNOT REPORTED 1 EA03258SP3053 258258 DURING ENGINE START, LT ENGINE WOULD MOTOR TO 20 PERCENT NR, THEN START CONTROL CIRCUIT BREAKER B4, 5 AMP WOULD TRIP. FOUND SHORTED WIRE IN THE IGNITION SYSTEM IN CABIN JUST FORWARD OF THE LEFT WHEEL WELL CONTACTING THE STRUCTURE WHERE IT PASSED THROUGH THE KEEL BEAM. ALSO FOUND ANTI CHAFE STRIP PULLED AWAY REPAIRED WIRE AND CHAFE STRIP. CHECKED AIRCRAFT. 2L72 4F4 FRTA3EU E6WE 20030423001362003042300136NM 2003 4 23 QXEA0300335 120030309A3230 LANDING GEAR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 LACK OF LUBE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09407QX 4049 YYC - FLIGHT 2331 - AIRCREW RETURNED TO FIELD WHEN AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. THE CHECKLIST WAS RUN BUT THE GEAR STILL FAILED TO RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND INTERROGATED THE PSEU. THE PSEU REPORTED -NWCENT UNREASONABLY FAR-. THE NOSE GEAR PROXIMITY SENSOR WAS FOUND TO BE IN RIG. NO OTHER DISCREPANCIES WERE NOTED. MAINTENANCE CLEANED AND LUBED THE NOSE GEAR SWITCHES AND SENSORS, PERFORMED OPERATIONAL CHECKS, AND RETURNED THE AIRCRAFT BACK TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20030423001392003042300139WP 2003 4 23 MWEA030132 120030313A3241421396 CONTROL BOX DOUG DC9 DC932 3022066WP COCKPIT INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31209ME 47730 WHILE ARMING ANTI-SKID RIGHT OUTBOARD AND INBOARD LIGHTS REMAINED ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX. 2L72 4F A6WE 20030423001482003042300148WP 2003 4 23 ZW0A0303008 120030306A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 FOUND DENT IN FUSELAGE SKIN AT STA 167, ABOVE LONGERON 20R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030423001712003042300171NM 2003 4 23 F3LA200300097 120030228A5311 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED FWD PRESSURE BULKHEAD SIDE FRAME AT LOWER FUSELAGE, STA. 178, WL 207, RBL 28, CRACKED. REPLACED RT. FRAME PER BOEING SERVICE BULLETIN 737-53A1173, REV. 3, SECTION III, PART XI, POINT I, FIGURES 71 AND 72. 2L72 4F RTA16WE 20030423002002003042300200EA 2003 4 23 QXEA0300365 120030316A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 PDX- DENT BELOW RIGHT SIDE STATIC PORT. REPAIRED IAW CRJ SRM 51-25-16 AND HORIZON AIR EA R-53-81/REO 670-53-21-032. 2L72 4F RTA21EA 20030424000292003042400029WP 2003 4 24 ZW0A0303205 120030319A335057761 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139401W 53137 THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 24 AND AFT. REPLACED THE BATTERY PACK BATTERIES. CHECK-C 11-16-02 STL. 2L72 4F RTA6WE 20030424000782003042400078WP 2003 4 24 ZW0A0303301 120030321A3350 LIGHT DOUG DC9 DC983 3022083WP EMERGENCY EXIT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139405T 53141 BOTH FORWARD EMERGENCY EXIT LIGHTS, AND THE EGRESS LIGHT AT ROW 14, WERE REPORTED INOPERATIVE. THE OVERWING EXIT LIGHTS OPERATED NORMAL AND THE EGRESS LIGHT OPERATED NORMAL. CHECK-C 10-19-2002 STL. 2L72 4F RTA6WE 20030424000952003042400095EA 2003 4 24 SWIA200311836 120030221A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07908SW 7540 FS 280 RBL AND LBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED. FOUND DURING C-CHECK INPSECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21 AND 51-23-00. 2L72 4F RTA21EA 20030424000972003042400097EA 2003 4 24 SWIA200311838 120030221A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07908SW 7540 FS 625 STR 14 LT AND 14 RT INTERCOSTAL ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-51. 2L72 4F4 FRTA21EA E15NE 20030424001132003042400113NM 2003 4 24 PCAA0303060 120030304A534785310066 SEAT TRACK DHAV DHC8 DHC8102 2809003NM COCKPIT WORN A PCAAK NONE O OTHER ININSP/MAINT 1 EA13847EX 333 DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING AN A LEVEL INSPECTION, CAPTAINS AND FIRST OFFICERS SEAT RAILS WERE FOUND TO BE WORN. ON 22 MARCH 2003 MAINTENANCE REPAIRED THE CAPTAINS AND FIRST OFFICERS SEAT RAILS BY INSTALLING A STAINLESS STEEL WEAR STRIP IN ACCORDANCE WITH DEHAVILLAND DASH 8 SERVICE BULLETIN 8-53-53. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424002012003042400201NM 2003 4 24 PCAA0303061 120030327A2930 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM HYD SYSTEM ILLUMINATED A PCAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA13979HA 373 LGA-YUL. FLIGHT 3978 CREW REPORTED THAT THE NR 1 HYDRAULIC ISOLATION VALVE AND INBOARD ROLL SPOILER LIGHTS HAD ILLUMINATED IN FLIGHT. AFTER FLAP UP LANDING IN YUL NORMAL BRAKING SYSTEM HAD FAILED. MAINTENANCE HAD INSPECTED THE AIRCRAFT FOR HYDRAULIC LEAKS AND NONE WERE FOUND. THE NR 1 HYDRAULIC SYSTEM WAS SERVICED. CREW RAN THE AIRCRAFT AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030425000182003042500018NE 2003 4 25 HALA0300082 220030214A72007202388 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LEFT STALLED A HALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 WP13478HA 55123 ATB-TWO LOUD BANGS, FROM LEFT ENGINE, LOW OIL PRESSURE, COMPRESSOR STALL, LEFT ENGINE SHUT DOWN, RETURNED TO HNL, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LEFT ENGINE IAW MM. 2L72 4F4 FTRA6WE E00061EN 20030425000762003042500076EU 2003 4 25 MALA030216 120030331A8010501113775008 MOTOR BAC 146 AVRO146RJ85A1500097EU STARTER FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15506XJ E2314 DURING FLIGHT 3401, STARTER OPERATING LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE STARTER MOTOR P/N ON OFF 501-1-13775-008, S/N ON TE2389, S/N OFF TE2601 IAW AMM 80-10-11. RAN ENGINE, OPS CHECK GOOD. 2H74 4F RTA49EU 20030425000792003042500079NM 2003 4 25 QXEA0300386 120030319A2720 HINGE BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 300 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - FORE RUDDER AFT LOWER HINGE BRACKET UPPER SURFACE WORN AROUND ATTACH HOLE. REPAIRED IAW HORIZON AIR EA 6-55-25. 2H72 4T RTA13NM 20030425001012003042500101NE 2003 4 25 P5CA0300785 220030331A7520773863 TUBE BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 4 ENGINE RUPTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 688856 NR 4 ENG 13TH STAGE TURBINE CASE COOLING DUCT RUPTURED AND BLEW THRU LT REVERSER HALF. REPLACED 13TH STAGE COOLING DUCT & LT REVERSER HALF. 2L74 4F4 F A20WE E3NE 20030425001042003042500104NM 2003 4 25 DLM88030210 120030304A2420 CSD DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE UNDERSERVICED A DALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO27919DL 49584 725959 LEFT CSD OVERTEMP IN FLIGHT. GENERATOR TURNED OFF AND TEMP DROPPED. SERVICED CSD. 2L72 4F4 FRTA6WE E9NE 20030425001112003042500111NM 2003 4 25 DL78K030220 120030306A29101550127114 FITTING BOEING737 737832 13844CFNM NR 2 ENGINE DAMAGED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO273730B 30538 876591 NR 2 ENG HYD QTY DECREASING ON CLIMBOUT. REPLACED NR 2 ENG HYD PUMP PRESSURE HOSE AND QUICK DISCONNECT FITTING AND CASE DRAIN HOSE AT ENG PUMP. 2L72 4F RTA16WE 20030425001172003042500117NM 2003 4 25 DLM88030240 120030313A2530 OVEN DOUG MD88 MD88 3023688NM GALLEY OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27902DE 53379 FWD GALLEY OVEN OVERHEATS AND SMOKES. REPLACED SAME. 2L72 4F RTA6WE 20030428000092003042800009WP 2003 4 28 ZW0A0303602 120030327A335058222 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13905TW 49157 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 25 THRU 31. REPLACED THE POWER SUPPLY. CHECK-C 12-3-02 STL. 2L72 4F A6WE 20030428000232003042800023NM 2003 4 28 QXEA0300419 120030331A521085210263101 STRUT DHAV DHC8 DHC8202 2809007NM ZONE 800 BROKEN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09345PH 476 SEA- MAIN CABIN DOOR FORWARD STAY STRUT IS BROKEN. REMOVED AND REPLACED STRUT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030428000302003042800030WP 2003 4 28 GTIA030175 120030306A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 PAX CABIN LT SIDE INBOARD STA 927 TO STA 1003 FILLER PNL CRACKED & DAMAGED. FLOORBOARD FAB. 2L72 4F4 FRTA6WE E2EA 20030428000412003042800041WP 2003 4 28 GTIA030167 120030223A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO STA 148, RBL 8 INCHES CORRODED ON TRACK. REMOVED FLOOR TRACK SUPPORT STA 148 TO 200 RBL 8. FABRICATED NEW TRACK. INSTALLED NEW TRACK. 2L72 4F4 FRTA6WE E2EA 20030428000502003042800050NM 2003 4 28 OZIA200343001 120030102A5320001A534C4061338 FLOOR SUPPORT DORNERDO32 DO328300 NM PWA 306 PW306B NE FUSELAGE CORRODED A OZIAK NONE O OTHER ININSP/MAINT 1 CE05430Z 6656 3127 FORWARD SIDE OF LAVATORY FLOOR SUPPORT (FRAME 35) CORRODED. 2H72 4T4 FRTA55NM E35NE 20030428000612003042800061WP 2003 4 28 MWEA030158 120030404A55513912033503 BUSHING DOUG DC9 DC981 3022081WP HORIZONTAL STAB CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 LEFT OUTBOARD LOBE FOR HORIZONTAL STABILIZER PIVOT BEARING CORRODED. FABRICATED AND INSTALLED BUSHING. 2L72 4F A6WE 20030428000782003042800078SO 2003 4 28 IKDC2003001 220030403A8520VU933 CRANKSHAFT CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO ENGINE BROKEN E IKDCA UNSCHED LANDING RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CRCRUISE 1 AL01109SW U20603799 WHILE CRUISING AT 6500 FT, THE ENGINE MOMENTARILY RAN ROUGH AND QUIT, NO WARNING INDICATIONS. THE AIRCRAFT SUCCESSFULLY LANDED ON A ROAD WITH NO INJURIES OR DAMAGE. AFTER LANDING, IT WAS NOTED THAT THE PROPELLER COULD NOT BE ROTATED. THE SUBSEQUENT ENGINE TEAR DOWN FOUND THE CRANKSHAFT TO BE BROKEN JUST FORWARD OF THE TWO REAR CYLINDERS ROD CONNECTIONS. CRANKSHAFT NUMBERS ON THE PROPELLER ATTACH FLANGE: (V/U 93-3 NOLHA 333) 1H71 3O3 O A4CE E5CE 20030428000842003042800084NM 2003 4 28 DHL2003741518 120030320A5330 SKIN BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS DENTS AT BS 1090 STR'S 18, 19, AND 20 L. C/A: 1) REMOVED PAINT I.A.W. B-727 M.M. 51-20-01. 2) EVALUATE 5 EACH DENTS, 2 EACH OUT OF LIMITS, 3 EACH IN LIMITS WITH A/Y RATIOS OF 1/.013 =76, .6/.009 = 66.6, .5/.013= 38.4 IAW B-727 SRM 53-30-1 FIG 1. 3) CUT-OUT 2 EACH DAMAGED AREAS ONE 3.5 X 2.3 AND THE OTHER 2.7 X 1.6 AND FAB DOUBLER IAW 2024- T3 .063 P.O. NR 9912102 DIM. 15.5 X 12.5 IAW B-727 SRM 53-30-3 FIG. 1. 4) DOUBLER TREATED AND PRIMED IAW B-727 SRM 51-10-2. 5) DOUBLER INSTALLED IAW B-727 SRM 53-30-3 FIG. 1. 2L73 4F4 FRTA3WE E2EA 20030428000902003042800090EU 2003 4 28 MALA030224 120030403A3230 UPLOCK BAC 146 AVRO146RJ85A1500097EU LT MLG CONTAMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15513XJ E2329 DURING FLIGHT 3621, GEAR UNSAFE LIGHT DURING GEAR RETRACTION FROM MISSED APPROACH. RECYCLED THREE TIMES. AIR RETURN TO DTW. JACKED AC FOR GEAR SWINGS, NOTED EXCESSIVE MOISTURE RT, LT DOOR AND GEAR UPLOCKS. CLEANED AND LUBED LOCKS IAW AVRO AMM CH 12. SUSPECT ICE BUILD-UP. PERFORMED MULTIPLE GEAR SWINGS. ALL CHECKS GOOD IAW CH 32. 2H74 4F RTA49EU 20030428000932003042800093NM 2003 4 28 PCAA0304065 120030402A2710 SERVO DHAV DHC8 DHC8102 2809003NM LT AILERON FAILED A PCAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA13804EX19955193 227 ACFT HAD DEAD SPOT LT AILERON ROLL. PITCH TRIM STIFF & OVER RESPONSIVE TO UP. MX OP CHECKED ROLL SPOILERS & CHECKED RIGGING OF AILERON CABLE CIRCUIT. CABLE TENSION ADJ FROM CONTROL WHEEL TO SPLITTER QUADRANT. TRIM CABLES, TRAVELS & RIGGING CHECKED. AILERON TRAVELS CHECKED ALONG WITH OPS CHECK OF SPOILER CUTOUT AT 140 KTS. AILERON CONTROL CIRCUIT UNDER COCKPIT FLOOR CHECKED & VISUALLY INSPECTED. WINGS VISUALLY INSPECTED, NO DEFECTS. AILERONS & TRIMS VISUALLY INSPECTED. ACFT TEST FLT UNSATISFACTORY. ACFT ROLLS ABNORM LT PASSING THRU 10 DEG LT BANK. ACFT ROLLS RT NORM. MX CHECKED AILERON CABLE TENSION IN WINGS AND LT & RT AILERON BALANCE. REPLACED LT AILERON & SERVO. TEST FLT SATISFACTORY. 2H72 4T RTA13NM 20030428000962003042800096NM 2003 4 28 VNAA0303032 120030329A21505413C000 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE TEMP CONTROL FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07426JS14888 3038 DURING TAKEOFF CREW REPORTED AOA, SHAKER AND PUSHER FAIL. MESSAGE CLEARED AFTER EXITING RUNWAY. THEN CREW REPORTED LT PACK WOULD NOT COOL IN EITHER MODE. AIRCRAFT WAS FERRIED TO DAY WHERE THE LT TEMP CONTROL VALVE WAS REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL 21-62-05 AND OPS CHECKED GOOD. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030429001672003042900167NE 2003 4 29 CA030319005 220030313A73206078T55P13 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN) MAINTENANCE FOUND EXCESSIVE FUEL LEAK FROM NR 2 ENGINE FCU. UPON EXAMINATION FOUND THAT FUEL WAS LEAKING FROM AROUND THROTTLE SPLINE SHAFT. FCU WAS REPLACED. 2L72 4F4 FRTA21EA E15NE 20030428000272003042800027WP 2003 4 28 GTIA030173 120030324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FLOORBOARD AT STA 1309-1260 CENTER DAMAGED. FAB PANEL. 2L72 4F4 FRTA6WE E2EA 20030428000282003042800028NM 2003 4 28 HNAA0300017 120030331A323183231020003 SPRING DHAV DHC8 DHC8102 2809003NM MLG DOOR BROKEN A HNAAO OTHER J WARNING INDICATION CRCRUISE 1 EA07934HA47721 139 NR 2 MLG AFT INBOARD GEAR DOOR CAME OPEN IN FLIGHT. FOUND DOOR ACTUATOR ROD AND ALT EXTENSION SPRING BROKEN. REPLACED ROD AND SPRING. 2H72 4T RTA13NM 20030428000702003042800070SW 2003 4 28 EHI0404 120030404A291041000633 SPRING BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA SERVO FAILED B LCFAO OTHER EF VIBRATION/BUFFET FLT CONT AFFECTED ININSP/MAINT 1 NM0959633547 547 30676 HYDRAULIC SYSTEM FEEDBACK FELT AND AUDIBLY OBSERVED WHILE IN ALL OPERATIONAL GROUND AND FLIGHT PROFILES. DURING MAINTENANCE TROUBLESHOOTING THE SUBJECT SERVO SPRING WAS FOUND FATIGUED/BROKEN. 1G71 4U4 U H4SW E22EA 20030428000952003042800095NM 2003 4 28 VNAA0303033 120030330A2730 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ELEVATOR FAILED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL07433JS 3047 DURING FLIGHT CONTROL CHECK THE ELEVATOR CONTROLS BECAME STUCK. MAINTENANCE INSPECTED THE ELEVATOR CONTROL SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-31-00 AND FOUND LOOSE INSULATION IN THE FRAME 45 ELEVATOR PULLEY. THE INSULATION WAS REMOVED AND RESECURED. OPERATIONAL CHECKS WERE COMPLETED AND NO FURTHER BINDING WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030428001562003042800156EU 2003 4 28 DHL2003367004 120030408A2611 CONNECTOR AIRBUS300 A300B4203 3930306EU SMOKE DETECTOR DIRTY A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01367DH 265 FORWARD COMPARTMENT SMOKE LIGHT CAME ON STEADY AND REMAINED ON. DEFERRED FORWARD COMPARTMENT SMOKE DETECTION PER MEL 26-14-02-1. ASSIGNED DMI 12501. PLACARDS INSTALLED. REF DMI 12501. FORWARD COMPARTMENT SMOKE LIGHT CAME ON STEADY AND REMAINED ON. CLEANED CONNECTORS ON BOTH FORWARD COMPARTMENT SMOKE DETECTORS REF 26-11-00. NO FAULTS DETECTED. THIS CLEARS DMI 12501. PLACARD REMOVED. MAINTENANCE CONTROL NOTIFIED. 2L72 4F RTA35EU 20030428001742003042800174WP 2003 4 28 03FDEA00403 120030408A5420 ANGLE DOUG DC10 DC1030 3023501WP NR 3 PYLON CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 3 PYLON ANGLE CHAFED THROUGH AT AFT RIB SUPPORT FOR PANEL 487FL. CLOSING ACTION ON 04/07/03. REMOVED RIB SUPPORT IAW SRM 51-31-01. FAB NEW RIB SUPPORT ON TRAVELER T2/325651. LOCATED AND DRILLED NEW PART IAW SRM 51-31-01. TREATED AND PRIMED RIB SUPPORT IAW SRM 51-21-01. INSTALLED NEW RIB SUPPORT IAW SRM 51-31-01. 2L73 4F A22WE 20030429000412003042900041NM 2003 4 29 AT0300010 120030407A2120 ODOR BOEING717 717200 1383700NM CABIN DETECTED A ZZDAO OTHER J WARNING INDICATION APAPPROACH 1 SO15943AT 55006 LAVATORY SMOKE EAD ALERT. FLIGHT ATTENDANT COMPLAINED OF ABNORMAL A/C HEAT, FAINT A/C ODOR IN COCKPIT. ISOLATED OIL ODOR TO AUXILIARY POWER UNIT. PERFORMED B717 FIM 49-50 TASK 807. CHECKED LEFT AND RIGHT WATER SEPARATOR COALESCER BAGS FOR OIL CONTAMINATION. COALESCER BAGS OK. RAN LEFT AND RIGHT AIR CONDITIONING PACKS WITH APU AND ENGINES FOR EXTENDED PERIOD OF TIME REF B717 AMM 21-00-00. NO SMOKE OR ODOR NOTED. A/C OK FOR SERVICE. 2L72 4F TRA6WE 20030429001282003042900128CE 2003 4 29 CWQ2003F00005 120030303A21206512072101 DUCT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA CRACKED A CWQRK NONE O OTHER ININSP/MAINT 1 GL05396QS5965 5600396 DURING ROUTINE INSPECTION, LOOKED INTO NACA DORSAL SCOOP AND FOUND THE LOWER AIR VANE (PN 6512072-12) CRACKED .5000 INCH WITH CRACK STARTING FROM THE CENTER OF (V) CUT MOVING OUTBOARD. GAINED ACCESS FROM TAIL BAGGAGE AREA AND REMOVED CRACKED VANE. REMOVED EA 9309 IAW MFG STANDARD PRACTICES, UPON REMOVAL NOTICED THAT THE V CUT APPEARS TO HAVE BEEN CUT WITH HAND SNIPS AND THERE WAS NO RELIEF HOLE AT BOTTOM OF CUT, ALSO THERE WAS VERY LITTLE EA 9309 SECURING INTO PLACE. INSTALLED NEW PART AND CLOSED UP AREA. WILL SEND BAD PART TO MFG FOR EVALUATION. (SCR NR 91291)(PTRS 7647) 2L72 4F4 FRTA22CE E25EA 20030429001932003042900193CE 2003 4 29 CA030409016 120030401A561010138402522 WINDSHIELD BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043NE HARTZLHCB4M HCB4MP3 GL COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) DURING CRUISE FLIGHT, RT COCKPIT WINDSHIELD CRACKED, EMERGENCY WAS CALLED AND THE AIRCRAFT LANDED SAFELY . FOUND INNER PLY OF WINDSHIELD CRACKED. WINDSHIELD WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20030429002142003042900214EU 2003 4 29 DHL2003365003 120030412A26123500813 CONTROLLER AIRBUS300 A300B4203 3930306EU FIRE DETECTION WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01365DH 149 LT HAND MANIFOLD FAULT LIGHT LOOP-A WILL NOT TEST. REMOVED AND REPLACED LT HAND CFD CONTROL UNIT IAW M/M 26-16-11 AND CHECKED OK. 2L72 4F RTA35EU 20030429002292003042900229NM 2003 4 29 SWAA030767 120030403A3350207377 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 EEPLS LENS LOOSE BETWEEN ROWS 7 AND 9. SECURED EEPLS LENS PER MM. 2L72 4F RTA16WE 20030430000022003043000002NM 2003 4 30 S03427016 120030413A2760 HANDLE BOEING747 747400 NM PWA 4056 PW4056 NE SPOILERS MALFUNCTIONED W SAJFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP03 24309 B-18271 ABORTED TAKEOFF (GS 70 KTS) DUE TO EICAS MSG (WARNING MSG) CONFIGURATION SPOILER. CHK CMC PRESENT LEG FAULT AND EXIST FAULT NO ANY FAULT WAS FOUND. IAW AMM 27-62-00 AUTO SPEED BRK FUNCTION TEST NML AND SPEED BRAKE HANDLE FUNCTION CHECK NML. DFDR DATA READOUT FOUND CONFIG SPOILER WARNING ACTIVATED BY ARM SWITCH S217. SPEED BRAKE HANDLE ARM AWITCH REPLACED AND TAKEOFF CONFIG WARNING TEST PASS. 2L74 4F4 FRTA20WE E24NE 20030430000042003043000004NM 2003 4 30 QXEA0300494 120030411A5320 FAIRING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - WING TO FUSELAGE FAIRINGS, PANEL 262FT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030430000242003043000024NM 2003 4 30 AWXA200300445 120030415A53126546568 BULKHEAD BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK 4 EACH 1/2 INCH CRACKS WERE FOUND AT RIVET HOLES ON REAR PRESSURE BULKHEAD AT BS 1016, AFT OF STR 7 L/H. MAINTENANCE CUTOUT DAMAGED PORTION OF WEB ON REAR PRESSURE BULKHEAD AT BS 1016, AFT OF STR 7 L/H; FABRICATED A FILLER, DOUBLER, TRIPLER, AND TAPERED SHIM; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-4, FIG. 15. 2L72 4F RTA16WE 20030424000752003042400075NM 2003 4 24 UPS03440338 120030306A5314 KEELBEAM BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 KEEL BEAM BOX EXTERIOR LOWER I/B SURFACE FOUND SURFACE CORROSION AT STA 1383 TO STA 1405 LBL 7. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02, BLEND OUT DEPTH 0.008 INCH, WIDTH 1 INCH, LENGTH 3 INCHES WITHIN SRM 53-10-01 LIMITS. (DEPTH 0.040 INCH, WIDTH 1 INCH, LENGTH 2 INCHES). 2L74 4F RTA20WE 20030424000962003042400096EA 2003 4 24 SWIA200311837 120030221A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING TE FLAP DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07908SW 7540 LEFT WING NR 4 FROM INBOARD FLEXIBLE DRIVE SHAFT IS DAMAGED AT HEX END. FOUND DURING C-CHECK INSPECTION. FLEX DRIVE REPLACED IAW CRJ MM 27-53-10-400-803. P/N: 11045D100-401, S/N OFF: 4864, S/N ON: 8082. 2L72 4F4 FRTA21EA E15NE 20030424001412003042400141NM 2003 4 24 QXEA0300370 120030313A5410 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 UPPER ANGLE IS CRACKED AT FORWARD END OF LEFT HAND LOWER COWL. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030424001692003042400169SO 2003 4 24 LR7A03024 120030313A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND FS 924 BULKHEAD UPPER WEB CRACKED AT LBL 61, WL 256. REPAIRED IAW SRM SMP 583 51-140-17. NR 2159. 2H74 4T A1SO 20030425000652003042500065CE 2003 4 25 ZSE2003F00002 120030319A531210143002141 BULKHEAD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A60A 52043NE FUSELAGE CRACKED D ZSEAO OTHER O OTHER NRNOT REPORTED 1 CE01498AC8301 BB287 2 INCH CRACK AT LOWER AFT CENTER OF BULKHEAD RUNNING SIDE TO SIDE. 1L72 4T4 T A24CE E4EA 20030425000872003042500087NM 2003 4 25 QXEA0300394 120030320A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - TWO CRACKS COMING OUT OF MOUNTING HOLES IN SKIN PANEL 85327152 FOR HOLDING THE NR 2 VHF ANTENNA. REPAIRED IAW HORIZON AIR EO/EA 6-53-162. 2H72 4T RTA13NM 20030425001092003042500109NM 2003 4 25 DL76L030217 120030304A361079275516 CONTROLLER BOEING767 767332 1382001NM RIGHT ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27196DN 28453 RIGHT PRV INOPERATIVE. SWAPPED HPSOV AND PRV. AFTER TAKEOFF RIGHT ENG BLEED FAILED. DUE TO FORECAST WEATHER IN JFK DECISION WAS MADE TO DIVERT TO FRA. FOUND PRV CONTROLLER AT FAULT. REPLACED PRV CONTROLLER, OPS CHECK ON R/U OK. 2L72 4F RTA1NM 20030425001142003042500114NM 2003 4 25 DLM88030230 120030309A3350 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27920DL 49644 EMERGENCY LIGHTS INOP LAST 8 ROWS. REPLACED POWER SUPPLY. 2L72 4F RTA6WE 20030428000052003042800005NM 2003 4 28 ZW0A0303604 120030330A3350 LIGHT BOEING757 7572Q8 1384972NM CABIN INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13710TW 28169 THE MOST FORWARD EGRESS LIGHT STRIP IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPAIRED BROKEN FEEDER SYSTEM. CHECK-C 11-14-01 MCI. 2L72 4F RTA2NM 20030428000292003042800029WP 2003 4 28 GTIA030174 120030324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 PAX CABIN CENTER FLOOR PANEL STA 826 TO STA 886 SOFT/MUSHEY AND SEVERAL INSERTS BROKEN OUT. FABRICATED NEW FLOOR PANEL. 2L72 4F4 FRTA6WE E2EA 20030428000322003042800032WP 2003 4 28 GTIA030177 120030307A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 INTERCOSTAL DAMAGED/CRACKED DURING WEB REPAIR AT FS 179 LBL 12 CABIN FLOOR AREA. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS. 2L72 4F4 FRTA6WE E2EA 20030428001072003042800107NM 2003 4 28 UPS03640413 120030405A3350 LIGHT BOEING767 76734AF 1385212NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01315UP 27743 INSPECTION TYPE: ASV, EMERGENCY LIGHT ABOVE LT SUPERNUMERARY SEAT INOP. RELAMPED, OPS CHECKS OK. 2L72 4F RTA1NM 20030428001282003042800128WP 2003 4 28 ZW0A0303905 120030402A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13925TW 49357 THE FUSELAGE SKIN WAS DAMAGED AT STA 588 TO 555, LONGERON 26R TO 26L. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 4. CHECK-C 8-15-02 STL. 2L72 4F A6WE 20030428001372003042800137 2003 4 28 DHL2003364007 420030408A2565 SLIDE AIRBUS300 A300B4203 3930306EU STARBOARD SIDE MALFUNCTIONED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 STARBOARD SIDE SLIDE WILL NOT ARM. REMOVED DEBRIS FROM AFT SLIDE ENGAGEMENT SLOT. OPS CHECKED OK PER 52-10-11. 2L72 4F RTA35EU 20030428001392003042800139NM 2003 4 28 CALA0300181 120030407A5230 SKIN BOEING777 777224 1385225NM CARGO DOOR DEFORMED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778008 29478 INSPECTION FOUND AFT CARGO DOOR FORWARD LOWER CORNER SKIN DEFORMED. REPAIRED IAW SRM 52-30-01, FIGURE 202, REPAIR 17, SHEET 5. 2L72 4F RTT00001SE 20030428001552003042800155EU 2003 4 28 DHL2003368002 120030408A3260 PROXIMITY SWITCH AIRBUS300 A300B4203 3930306EU MLG DIRTY A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01506TA 207 UNABLE TO RAISE LANDING GEAR LEVER PAST THE OFF POSITION FOR GEAR RETRACTION. TROUBLESHOT PER FIM 32-30-00. SYSTEM NR 1, SENSORS NR 4 & NR 7, FAIL BITE TEST. SYSTEM NR 2 OPS CHECKED OK PER FIM 32-30-00. SYSTEM NR 1 TRANSFERRED TO DMI 12494, PER MEL 32-31-01-1 CAT-B. REF DMI 12494 UNABLE TO RAISE LANDING GEAR LEVER PAST THE OFF POSITION FOR GEAR RETRACTION. THIS CLEARS DMI 12494, MAINTENANCE CONTROL NOTIFIED. CLEANED PROXIMITY SWITCH, RIGHT-HAND SHOCK ABSORBER DETECTOR, AND RE-RACKED DETECTOR MODULE 54GB. SYSTEM CHECKED IAW 32-61-12. 2L72 4F RTA35EU 20030428001762003042800176WP 2003 4 28 IXXA0300030O 120030409A7722 WIRE HARNESS DOUG DC8 DC873F 302199FWP EGT DIRTY A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11605AL91916892 46106 AFTER TAKEOFF IN CLIMBOUT FROM BDL TO EWR, NR 3 EGT REACHED 999 AND WAS ERRATIC. CREW DIVERTED TO TOL DUE TO NO MAINTENANCE IN EWR. CREW ARRIVED IN TOL WITH AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE THERMOCOUPLE WIRING HARNESS FOR CRACKS AND NO DEFECTS WERE NOTED. MAINTENANCE CLEANED PINS FOR THERMOCOUPLE HARNESS AND INSTALLED A NEW HARNESS IN ACCORDANCE WITH CFM MAINTENANCE MANUAL. ENGINES WERE RUN IN ACCORDANCE WITH ATI ENGINE RUN HANDBOOK. ENGINE PARAMETERS WERE NORMAL. OPERATIONAL CHECK WAS GOOD IN ACCORDANCE WITH ATI GENERAL MAINTENANCE MANUAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030428001822003042800182NM 2003 4 28 AWXA200300354 120030408A3397BMS13311122 WIRE BOEING737 7373Y0 1384671NM EMERGENCY LIGHT SHORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTS FROM SEAT ROW 11 LT AFT WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND SHORTED WIRES UNDER SEAT ROW 18 LT, SPLICED WIRES PER SWPM 20, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030428001862003042800186SO 2003 4 28 RAIA00303090 120030328A3412102AU1AF PROBE EMB 145 EMB145LR 3260212SO TAT SENSOR INOPERATIVE A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03820HK9632 145064 SGF- TOTAL AIR TEMP NR 2 INOP WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 2 TAT, OPS CHECK OK. 2L72 4T RTT00011AT 20030429000032003042900003CE 2003 4 29 DXTA200300008 120030314A324177B62 PRESSURE SWITCH CESSNA500 560CESSNA 2076750CE BRAKE ASSY FAILED E DXTAD RETURN TO BLOCK JS WARNING INDICATION AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07323QS 5600323 BRAKE PUMP RUNS CONTINUOUSLY WHEN BRAKES ARE APPLIED. LOW BRAKE PRESS ANNUNCIATOR ILLUMINATES. 2L72 4F RTA22CE 20030429000082003042900008NM 2003 4 29 P5CA0300794 120030203A5347 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 STA 1760-1880 LBL & RBL 11 WL 208 CORROSION ON SEAT TRACK AND FLOORBEAM. DAMAGED AREA TRIMMED OUT, REINFORCED PER SRM 51-30-02 & 53-10-05 FIG 1 A. 2L74 4F A20WE 20030429000152003042900015NM 2003 4 29 P5CA0300793 120030204A5315 FLOORBEAM BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 STA 2320 / LBL 20 WL 208 CORROSION ON FLOORBEAM UPPER TEE. CORRODED AREA TRIMMED OUT, REINFORCED AREA PER SRM 53-11-25. 2L74 4F A20WE 20030429000172003042900017NM 2003 4 29 P5CA0300811 120030126A5320 PANEL BOEING747 747283B 1384867NM CABIN CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 UPPER DECK SIDE WALL CRACK ON THE CLIPS AT FRAME STA 500/L AT CONNECTION TO STR 10, 10A, 11A, 12. CRACKED CLIPS REMOVED AND NEW FABRICATED 7075 TG 0.050 THK PER SRM 53-10-20 & SRM 51-40-03 FIG -4. PROTECTED PER SRM 51-10-02 AND INSTALLED RIVETS PER SRM 51-30-02. 2L74 4F A20WE 20030429000272003042900027NM 2003 4 29 P5CA0300813 120030126A5320 BRACKET BOEING747 747283B 1384867NM FLOOR SUPPORT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LWR-LOBE AFT CRG CRACKS ON TWO BRACKETS AT THE FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1900-1920. CRACKED 2 BRACKETS REMOVED, NEW BRACKETS FABRICATED PER SRM 53-11-25 & PER SAMPLE PROTECTED WITH ANODIZE PER SRM 51-10-02, FASTENERS INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 20030429000362003042900036NM 2003 4 29 03FDEA00413 120030409A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION (C53-111-01, 3) ON FRAME BS 950F LBL 8-11 WL 148. REPAIRED FRAME IAW SRM 53-10-4 FIG 15 AND EA 7-5310-69652. 2L73 4F RTA3WE 20030425000022003042500002WP 2003 4 25 UPS03840379 120030327A2611 BATTERY DOUG DC8 DC873F 302199FWP SMOKE DETECTOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 REF M 256938 LOWER SMOKE DETECTOR BATTERY MSG AD 3746. REMOVED AND REPLACED TWO EACH SMOKE DETECTION BATTERY ON PIT 34 AD 3746 AS PER MM 26-18-02. CLEARED M256938, OPS CHECK GOOD. 2L74 4F RT4A25 20030425000922003042500092NM 2003 4 25 QXEA0300399 120030318A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - EXTERNAL FUSELAGE BELLY SKIN A NICK FSX-8.00 AND .5 INCH INBOARD OF STRINGER 33P. REPAIRED IAW 51-25-10, PAGE 201-205 AND HORIZON AIR EA 6-53-211. 2H72 4T RTA13NM 20030425000942003042500094NM 2003 4 25 QXEA0300401 120030320A5414 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 400 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - NR 1 NACELLE INBOARD AT STATION X449.500 HAS SCRATCH AND DENT IN SKIN. REPAIRED IAW DHC-8 400 SRM 51-25-05 AND HORIZON AIR EA 6-54-216. 2H72 4T RTA13NM 20030428000162003042800016EA 2003 4 28 QXEA0300417 120030402A2611 COVER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX- FORWARD CARGO BAY ENTRY WAY SMOKE DETECTOR PROTECTIVE COVER IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030428000382003042800038WP 2003 4 28 GTIA030164 120030318A5230 BEAM DOUG DC9 DC932 3022066WP CARGO DOOR CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL2312536 47113 EDDY CURRENT INSPECTION REVEALED 2.25 INCH CRACKS EMANATING FROM FASTENER HOLE IN OUTER PAN OF AFT LOWER CARGO DOOR FWD EDGE AT BEAM 1. STOP DRILLED CRACKS AND INSTALLED PATCH ON AFT CARGO DOOR. 2L72 4F A6WE 20030428000742003042800074NM 2003 4 28 DHL2003741507 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS OIL CANNING FWD BS 1050 AT STR'S 23, 24, AND 25R. CUT OUT DAMAGE AREA DIM 2.90 X 2.60 INCH 2024 T-3 IAW B-727 SRM 53-30-3 FIG 4. FAB FILLER DIM AREA 2.90 X 2.60 INCH .063 PO 9912350 AND FAB DOUBLER, SHIM FROM 2024-T-3 .071 INCH DIM DOUBLER ARE 11.5 X 8.25 INCH SHIM DIM ARE 1 X 6 INCH PO 9912182 .071 IAW B-727 SRM. TREAT AND PRIMED, INSTALL ALL PART IAW B-727 SRM 51-10-2, 53-30-3 FIG 4, AND 53-30-2 FIG 1. 2L73 4F RTA3WE 20030430000342003043000034EA 2003 4 30 COMA0360219 120030427A5610NP1393222 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER DEDESCENT 1 SO01988CA12756 7204 FLIGHT 5855 CO PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW. 2L72 4F RTA21EA 20030430000512003043000051EU 2003 4 30 2003UALA00386 120030420A3260 BRACKET AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG SENSOR DAMAGED A UALAA UNSCHED LANDING CF F.O.D. FLT CONT AFFECTED CLCLIMB 1 WP29497UA 1847 RETURN TO FIELD DUE TO LANDING GEAR SHOCK ABSORBER FAULT INDICATIONS. REPLACED SENSOR BRACKET FOR LANDING GEAR EXTENSION SENSOR (24GA & 25GA) CAUSED BY FOD. 2L72 4F4 FRTA28NM E40NE 20030430000622003043000062NM 2003 4 30 USAA030032 120030319A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU50845 23381 PIT - FOUND SKIN PANEL CRACKED TWO PLACES 1.25 INCH AND .750 INCH, STATION 685 BL 0 AT KEELBEAM. STOP DRILLED CRACKS, INSTALLED EXTERNAL DOUBLER PER EA 53683E. (M) 2L72 4F RTA16WE 20030430000662003043000066NM 2003 4 30 USAASB03026 120030215A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US 23311 PIT - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROW 15 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 15. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030430000692003043000069NM 2003 4 30 USAABB03051 120030317A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 PHL - FOUND EXIT IDENTIFIERS AT L1 AND R4 DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030430000912003043000091SO 2003 4 30 SIMA200309006 120030307A532014522461011 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030428001132003042800113SO 2003 4 28 C2XA03CL085 120030404A3234 SELECTOR EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL MLG FAULTY A C2XAO OTHER J WARNING INDICATION APAPPROACH 1 SW2714938 145029 MSP FLIGHT 2779 CREW REPORTED LANDING GEAR DISAGREE MESSAGE. RED NOSE INDICATION ON EICAS. COULD ALSO HEAR THAT NOSE GEAR WAS DOWN. GEAR RECYCLED OK. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTT00011ATTE6CH 20030428001162003042800116WP 2003 4 28 EIA2003051 120030307A5311 FRAME DOUG DC9 DC933F 302207AWP PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09944F 47194 FORWARD CARGO PIT FRAME AT STA 351, SIDE AT BEND RADIUS. CORRODED BETWEEN LONGERON 30-29 R. INSTALLED REPAIR ON STA 351 FRAME SRM 51-30-02,1 AND 53-03 FIG 2A. HEAT TEATED AND FABRICATED DOUBLERS IAW SRM 53-03 PG 4E AND 4J. 2L72 4F4 F A6WE E2EA 20030428001192003042800119NM 2003 4 28 CALA0300167 120030403A5210 ANGLE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE PAX DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND L-ANGLE ATTACHED TO Z-ANGLE AT R-1 DOOR CORRODED. THE L-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20030428001502003042800150SO 2003 4 28 C2XA03BT049 120030408A326014521495403 WIRE HARNESS EMB 145 EMB145ER 3260211SO MLG DEFECTIVE A C2XAB EMER. DESCENT N FALSE WARNING LDLANDING 1 SW2712946 145052 EWR---CO2809, CREW REPORTED, LANDING / AIR GROUND FAILURE INFLIGHT AND ENGINE NR 1 & NR 2 THRUST REVERSER DISAGREEMENT INFLIGHT. DECLARED EMERGENCY AND LANDED IN EWR UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED NOSE GEAR AIR GROUND PROXIMITY SWITCH HARNESS, OPS CHECKED GOOD IAW EMB145 MM 32-65-05 AND EMB 145 MM 78-31-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030428001572003042800157NM 2003 4 28 UPS03240416 120030323A5330 SKIN BOEING727 727173C 1384059NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, EVIDENCE OF CORROSION AT CIRCUMFERENTIAL JOINT BS 480 RT BETWEEN ST R10 AND 14 RT. LFEC C/W MATERIAL LOSS INDICATIONS MARKED. PAINT STRIPPED AND FASTENERS REMOVED IAW SRM 51-30-2. DAMAGED AREA CUT OUT, CUTOUT HFEC AND NDF, HOLES HFEC AND NDF. REPAIR ACCOMPLISHED UPS EO B727-53-20106. 2L73 4F A3WE 20030428001622003042800162EA 2003 4 28 03098643 120030408A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27643BR 7363 DURING MAINTENANCE INSPECTION, A RT EXTERIOR AND THE AFT CABIN EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030428001992003042800199NM 2003 4 28 0300776739 120030404A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01639US 23887 DURING H-CHECK, FOUND CRACK IN FRAME WEB AT BS 440 S15L. REPAIRED PER EA 67-165052. 2L74 4F A20WE 20030429000252003042900025NM 2003 4 29 P5CA0300806 120030206A5730 SKIN BOEING747 747283B 1384867NM RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RIGHT WING L/E LWR SURFACE CORROSION IN LWR SURFACE WAS 1280. DAMAGED AREA TRIMMED OUT, REINFORCED WITH DOUBLER PER SRM 57-30-03 FIG -9. 2L74 4F A20WE 20030429001092003042900109SW 2003 4 29 VH22003F00000 120030331A74102714087017 CONTROL BOX SWRNGNSA226 SA226T 8780122SW GARRTTTPE331TPE331* 01514WP IGNITION SYS FAILED B VH2RO OTHER O OTHER NRNOT REPORTED 1 SW17240NM14 T240 ON MARCH 15, 2003 FAS INSTALLED AUTO CONTINUOUS IGNITION SYSTEM IAW AD AND SB WHICH INSTALLED A NEW IGNITION CONTROL BOX LATEST VARIANT OF THIS UNIT. SYSTEM OPS CHECK WERE GOOD. ON MARCH 25,2003, THE FAILED UNIT (PN 27014087-017) SN FAS 1147 WAS REPLACED WITH A NEW (PN 2714087-001M (MODIFIED EQUIVILENT OF PN 27-14087-017)). NEW SN FAS-1055 ON. SYSTEM OPS CHECKS WERE GOOD. THE FAILED UNIT SN FAS-1147 HAD 2 BURNED CIRCUIT BOARD TRACES. ENTIRE SYSTEM WAS CHECKED AND NO OTHER DEFECTS WERE NOTED. 2L72 4T3 TRTA5SW E2WE 20030429001182003042900118SO 2003 4 29 RAIA00304110 120030410A272015793101 PRESSURE SWITCH EMB 145 EMB145 3260210SO RUDDER FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03803HK8672 145077 PIT- RUDDER NR 2 FAIL WARNING. MAINTENANCE REMOVED AND REPLACED NR 2 RUDDER PRESSURE SWITCH, OPS CK GOOD. 2L72 4F RTT00011AT 20030429002212003042900221 2003 4 29 SWAA030805 420030409A2565 GAUGE BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030430000582003043000058NM 2003 4 30 USAABB03047 120030320A33508731002511REV15 LIGHT BOEING757 7572B7 1384964NM EXIT SIGN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19629AU 27807 BDL - FOUND R1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030430000802003043000080SO 2003 4 30 SIMA200309008 120030308A532014522459003 BRACKET EMB 135 EMB135LR 3260305SO FLOOR SUPPORT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION PASSENGER DOOR FORWARD FLOOR SUPPORT BRACKET CORRODED. REMOVED AND INSTALLED FLOOR SUPPORT IAW EMB 135/145 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030430000942003043000094NM 2003 4 30 USAASB03041 120030318A2420915F2125 GCU BOEING737 737401 1384701NM NR 1 GENERATOR FAILED A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19420US20762156 23987 CLT - FLT 799 - SHORTLY AFTER TAKEOFF FROM ORD, EN ROUTE TO CLT, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED. CREW PLACED THE NR 1 GENERATOR BACK ON LINE, WHERE IT STAYED FOR A COUPLE OF MINUTES, BEFORE DROPPING OFF LINE AGAIN. FREQUENCY AND VOLTS WERE NORMAL. CREW STARTED AND USED THE APU. THEN, THE NR 1 GENERATOR OPERATED NORMAL. FLIGHT CONTINUED ONTO CLT. UPON LANDING INTO CLT, THE NR 1 GENERATOR DROPPED OFF LINE AGAIN. THE COCKPIT WENT DARK ON THE LEFT SIDE AND THE CREW WAS UNABLE TO RESTORE ANY POWER. MAINTENANCE FOUND THE NR 1 GENERATOR CONTROL UNIT UNLATCHED AND DISCONNECTED. RESET THE NR 1 GENERATOR CONTROL UNIT. RAN ENGINE. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030430001042003043000104NM 2003 4 30 03118410 120030428A3350 SIGN DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27410FJ 3165 DURING PREFLIGHT INSPECTION THE FLIGHT CREW DISCOVERED THE FOWARD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND COULD NOT DUPLICATE THE DEFECT. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030430001092003043000109EA 2003 4 30 QXEA0300508 120030426A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 100 FAILED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09613QX2441 10045 BOI - CREW RECEIVED A FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE INTERROGATED THE MAINTENANCE DIAGNOSTICS COMPUTER AND FOUND FAULT AS FORWARD SMOKE DETECTOR WORD 352 BIT 20. MAINTENANCE REPLACED THE NR 3 SMOKE DETECTOR IN THE FORWARD CARGO BAY AND THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030430001172003043000117NM 2003 4 30 03FDEA00608 120030426A2613 WARNING LIGHT BOEING727 727200 138407ENM WING/BODY OVHT ILLUMINATED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25222FE 20933 ON CLIMB OUT OF MAO APPROX 5,000 FT. NR 3 STRUT OVERHEAT LIGHT CAME ON. UPON RETARDING POWER APPROX. .20 EPR LIGHT WENT OUT. AFTER COMPLYING WITH QRH PROCEDURES, POWER WAS RESTORED TO NORMAL WITH NO FURTHER INDICATIONS. BASED ON CREW REPORT, AND VERBAL DEBRIEF UPON ARRIVAL IN MIA, AFTER THE ENGINE PWR WAS REDUCED AND THE LIGHT EXTING,THE PILOT RESTORED THE POWER SETTING TO NORM, AND THE STRUT OVERHEAT LIGHT STAYED OUT THE REMAINDER OF THE FLT, AFTER 5 HOURS NO REPEAT, I'LL TAKE AS AN ANOMALLY. RAN ENG AND PER JET RUN HANDBOOK, NO FAULTS NOTED,CHECKED SYSTEM IAW M/M 26-12-011-5 AND 26-14-001-2 ALL CHECKED OK. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20030430001332003043000133NM 2003 4 30 SWAA030916 120030424A5754 STRUCTURE BOEING737 7373H4 1384600NM RT WING LE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED C4 CHECK, FOUND RT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. R&R RT INBD FOREFLAP PER MM. 2L72 4F RTA16WE 20030430001342003043000134NM 2003 4 30 SWAA030915 120030423A57536546435 STRUCTURE BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED C2 CHECK, FOUND LT OTBD AFT T/E FLAP DELAMINATED AT INBD LOWER CORNER. R&R LT OTBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030430001442003043000144NM 2003 4 30 SWAA030905 120030423A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 EEPLS SECTION MISSING AT ROW 21. INSTALLED EEPLS PER MM. 2L72 4F A16WE 20030430001552003043000155 2003 4 30 SWAA030880 420030420A2565D31354 SLIDE BOEING737 7373H4 1384600NM PAX DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030430001632003043000163NM 2003 4 30 SWAA030872 120030419A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS ( 2 EA ) AT STR 4L, BS 350 TO BS 360 & BS 259 TO BS 278. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030430001652003043000165NM 2003 4 30 SWAA030869 120030417A32136561740 STRUT BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG UPPER OUTER CYLINDER CORRODED. REMOVED AND REPLACED LT MLG UPPER OUTER CYLINDER PER MM. 2L72 4F RTA16WE 20030430001672003043000167 2003 4 30 SWAA030867 420030418A25656567380 LENS BOEING737 7373H4 1384600NM ESCAPE SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND COVER LENS LOOSE. SECURED COVER LENS PER MM. 2L72 4F RTA16WE 20030501000852003050100085WP 2003 5 1 GTIA030199 120030217A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND MID PIT UPPER WEB LONGEORN 18L FROM STATION 712 TO STATION 769 AT 4 LOCATIONS CORRODED. REMOVED WEB AT FS 712 TO 788. LOCATED AND DRILLED NEW WEB. INSTALLED NEW WEB. (M) 2L72 4F RTA6WE 20030501000902003050100090SW 2003 5 1 2003F00240 120030205A7933 INDICATOR FRCHLDSA227 SA227DC 3377521SW NR 2 ENG OIL INOPERATIVE A BSAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM05853LS DC853B FLT 2565 - BIL - FOUND NR 2 ENGINE OIL TEMP WAS HIGH DURING CLIMB-OUT. CREW RETURNED TO STATION. INDICATION SYSTEM MALFUNCTION. REPLACED TEMP PROBLE DUE OT SUSPECTED OIL INFILTRATION FROM CONNECTOR SIDE, REPAIRED OIL TEMP BULB CONNECTOR, AND REPLACED VENRNATHERM VALVE. OIL SAMPLE WAS TAKEN, OIL WAS CHECKED FOR BURNING OR BURNED ODOR, NONE WAS NOTED. HALF HOUR GROUND RUN WAS PERFORMED, FOLLOWED BY A TEST FLIGHT. NO FURTHER DISCREPANCIES WERE NOTED. (M) 2L72 4T RTA18SW 20030501000922003050100092NM 2003 5 1 KPVA200314 120030319A3241 WARNING LIGHT DHAV DHC8 DHC8103 1386005NM ANTI SKID SYS ILLUMINATED A KPVAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP13808WP 026 FLT 1550 - HNL - INBOARD AND OUTBOARD ANTI-SKID CAUTION LIGHTS ILLUMINATED ON TAXI. PERFORMED ANTI-SKID SELF TEST. NO MALFUNCTION DEFECT CODES NOTED. TESTED SYSTEM IAW DHC-8 MM 32-46-00, PARAGRAPH 3, PAGE 3. (M) 2H72 4T RTA13NM 20030430000162003043000016SO 2003 4 30 LR7A03040 120030426A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 658 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND FS 869 SKIN DENTED AT LBL 82, WL 200. REPAIRED IAW SRM SMP 583 51-140-12. NR 0008. 2H74 4T A1SO 20030430000212003043000021EU 2003 4 30 AWXA200300448 120030417A5320D5323003020000 FITTING AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1/2 INCH CRACK WAS FOUND ON FITTING AT AFT SIDE OF FORWARD CARGO DOOR FRAME CUTOUT. MAINTENANCE REMOVED DAMAGED FITTING AT AFT SIDE OF FORWARD CARGO DOOR FRAME CUTOUT FR 28, STR 35 R/H; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 5-6. 2L72 4F RTA28NM 20030430000572003043000057NM 2003 4 30 USAABB03048 120030320A2120 ODOR BOEING757 7572B7 1384964NM COCKPIT DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19632AU 27810 CLT - FLT 1160 - CREW REPORTED STRONG ELECTRICAL ODOR AND SMOKE WHEN RADAR IN USE. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE RADAR TRANSCEIVER WAS REPLACED AS A PRECAUTION. (M) 2L72 4F RTA2NM 20030430000592003043000059NM 2003 4 30 USAABB03046 120030319A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19624AU 27245 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030430000712003043000071NM 2003 4 30 USAA030021 120030303A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU 22205 CLT - FOUND FRAME WITH TWO CRACKS .625 INCH LONG, .281 INCH LONG, FORWARD CARGO DOOR AFT FRAME BS 620 UNDER NR 6 DOOR STEP FT. CUTOUT DAMAGE AREA, FABRICATED REPLACEMENT WEB, INSTALLED WEB PER EA 87103. (M) 2L72 4F RTA2NM 20030430000782003043000078SO 2003 4 30 SIMA200309001 120030325A3350 BATTERY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21844AE 145682 DFW - FLT 3951 - CREW REPORTED THE OVERWING EMERGENCY LIGHT AND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 9, 10 AND IT WILL NOT ILLUMINATE. MAINTENANCE RESECURED THE BATTERY AT POWER SUPPLY NR 4. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030430000832003043000083SO 2003 4 30 SIMA200308401 120030318A5310 WINDOW FRAME EMB 135 EMB135LR 3260305SO COCKPIT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 ABI - DURING AN IMBV INSPECTION, THE LEFT WINDSHIELD LOWER OUTBOARD 14 SCREW HOLES WERE FOUND TO BE CORRODED. THE SCREW HOLES WERE REAMED TO REMOVE CORROSION. THREE HOLES REQUIRED REAMING A SECOND TIME. THREE BUSHINGS WERE FABRICATED AND INSTALLED. REPAIRED IAW EMB STATEMENT IC2003-145/0899, GST-1578/02-B AND ETN EB-53-035. (M) 2L72 4F RTT00011AT 20030430001022003043000102EU 2003 4 30 0311833003 120030428A33506040751 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PEROSNNEL DISCOVERED THE EMERGENCY EXIT SIGN AT THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE POWER SUPPLY FOR THE NR 1 EMERGENCY BATTERY AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030430001132003043000113NM 2003 4 30 03FDEA00604 120030425A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FRAME BS 660 LBL 25 WL 149. 2L73 4F RTA3WE 20030430002482003043000248WP 2003 4 30 MWEA030170 120030414A57555910055512 PANEL DOUG DC9 DC915 3022036WP SPOILER DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 RIGHT CENTER SPOILER PANEL HAS DENT 1.5 X .033 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE BONDED EXISTING DOUBLER. 2L72 4F A6WE 20030501000432003050100043EA 2003 5 1 ASOA03100 120030310A2752853D10014 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAP INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11847AS 7335 FLT 4810 - DURING APPROACH INTO SYR FROM ATL, THE CREW RECEIVED A FLAP FAILURE MESSAGE. WHEN SELECTING THE FLAPS TO EIGHT DEGREES THEY DID NOT MOVE. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT LANDED SAFELY IN SYR. THE LOCAL MECHANIC COMPILED WITH AD 98-20-01 RESETTING THE FLAP SYSTEM AND CYCLING THE FLAPS WITH NO DEFECTS NOTED. THE FLAPS ELECTRONIC CONTROL UNIT CODES SHOWED THE TOP THREE WERE JAMMED. MAINTENANCE REMOVED AND REPLACED THE NR 3 RIGHT OUTBOARD FLAP INBOARD ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030501000722003050100072WP 2003 5 1 GTIA030206 120030303A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FS 160-200 CABIN FLOOR SUPPORT CORRODED IN RADIUS. FABRICATED NEW FLOOR SUPPORT. REMOVED FLOOR SUPPORT. FLOOR SUPPORT WILL BE INSTALLED ON WO NR B68 18-N-566. (M) 2L72 4F RTA6WE 20030501001182003050100118EA 2003 5 1 03101628 120030411A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THREE EMERGENCY EXIT LIGHT BATTERIES. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030501001232003050100123NM 2003 5 1 ASAA0310022 120030221A53306545775 SKIN PANEL BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 854, STRINGER 17R-18R GOUGED. REPAIRED SKIN PANELS PER SRM. (M) 2L72 4F RTA16WE 20030501001302003050100130NM 2003 5 1 ASAA0310091 120030305A57306546419501 SKIN BOEING737 737298C 1384490NM RT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND RT WING LEADING EDGE SKIN AT WING STATION 337-367 CHAFED AND DENTED. REMOVED DAMAGED AREA AND REPAIRED SKIN PER SRM. (M) 2L72 4F RTA16WE 20030501001352003050100135NM 2003 5 1 ASAA0310042 120030225A532065555741 WEB BOEING737 737210C 1384459NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 4 FLAP TRACK FAIRING VERTICAL WEB AT BS 700, LEFT BUTTOCK LINE 65 GOUGED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F A16WE 20030501001562003050100156 2003 5 1 ASAA0380119 420030204A25653961896501 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01953AS 49386 SEA - DURING PREFLIGHT CHECK, FOUND LEFT FORWARD (L-1) PASSENGER DOOR GIRT-TO-SLIDE COVER LANYARD DISCONNECTED. RETATTACHED LANYARD. (M) 2L72 4F A6WE 20030501001572003050100157NM 2003 5 1 ASAA0310052 120030227A54106570193503 GUSSET BOEING737 737298C 1384490NM NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL GUSSET AT NACELLE STATION 236, CHAFED. REMOVED AND REPLACED GUSSET PER SRM. (M) 2L72 4F RTA16WE 20030501001802003050100180NM 2003 5 1 ASAA0310068 120030301A53136545775558 STRINGER BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGERS 17R-18R AT BS 854, GOUGED. BLENDED OUT DAMAGE AND INSTALLED REPAIRS PER SRM. (M) 2L72 4F RTA16WE 20030501001912003050100191NM 2003 5 1 ASAA0310059 120030301A532065558434 SUPPORT ANGLE BOEING737 737298C 1384490NM FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SUPPORT ANGLES AT BS 986, STRINGER 23L-24L BENT. REMOVED AND REPLACED SUPPORT ANGLES PER SRM. (M) 2L72 4F RTA16WE 20030501001952003050100195EU 2003 5 1 USAASA03026 120030322A335032145410 POWER SUPPLY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19187US 1704 CLT - THE EMERGENCY EXIT SIGN WILL NOT ILLUMINATE AT THE R-3 DOOR. MAINTENANCE REPLACED THE R-3 DOOR EMERGENCY POEWR SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030501002012003050100201NM 2003 5 1 ASAA0310034 120030225A5320654198624189 PAD BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, STANSION PAD AT BS 578, RIGHT BUTTOCK LINE 50 CORRODED. REMOVED AND REPLACED STANSION PAD PER SRM. (M) 2L72 4F RTA16WE 20030501002092003050100209WP 2003 5 1 ASAA0380270 120030317A5320993061267 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 OAK - DURING C-CHECK, RT CABIN FLOOR MEMBRANE IS CORRODED BETWEEN FS 1193 AND 1211. INSTALLED DOUBLER PER SRM 53-01, 51-30-3, AND 51-10-3. (M) 2L72 4F RTA6WE 20030501002112003050100211WP 2003 5 1 ASAA0380268 120030317A5532593614317 SKIN DOUG DC9 DC983 3022083WP VERTICAL STAB GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OAK - ON 15K CHECK, VERTICAL STABILIZER SKIN GOUGED ON LEFT SIDE AT LOWER FORWARD END OF CUTOUT FOR HORIZONTAL STABILIZER. BLENDED GOUGE AND INSTALLED DOUBLER PER SRM 55-01. (M) 2L72 4F RTA6WE 20030501002132003050100213EA 2003 5 1 ASOA03117 120030319A7920J221P136 O-RING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ENG OIL FILTER CUT A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11852AS 7369 FLT 4673 - DUIRNG CLIMB-OUT FROM ATL-SHV, THE CREW EXPERIENCED LOW OIL PRESSURE ON THE RIGHT ENGINE WITH IT DROPPING TO 21 PSI. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO GTR, LANDING SAFELY. MAINTENANCE REPLACED A CUT O-RING ON THE OIL FILTER BOWL AND SERVICED THE ENGINE WITH SIX QUARTS OF OIL. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20030501002162003050100216NM 2003 5 1 2003F00245 120030325A291065178851 O-RING BOEING727 727225 1384077NM HYD SYSTEM WORN A RYNAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CE07801EA 22432 DURING APPROACH TO AUSTIN AT 29,000 FEET, BOTH B-HYDRAULIC LOW PRESSURE LIGHTS CAME ON. B-SYSTEM PRESSURE INDICATED ZERO AND SYSTEM QUANTITY NORMAL. EMERGENCY PROCEDURES WERE FOLLOWED. AIRCRAFT LANDED AT AUSTIN WITHOUT INCIDENT. REPLACED O-RING AND TIGHTENED BLEEDER PLUG ON BRAKE INTERCONNECT MODULE. LEAK CHECKED GOOD. (M) 2L73 4F A3WE 20030430000982003043000098EU 2003 4 30 USAASA03021 120030305A2121EVT3454H FAN AIRBUSA321 A321211 3930370EU AVIONICS BAY SEIZED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19187US 1704 PHL - FLT 125 - EN ROUTE PHL-DEN, ON TAKEOFF, AIRCRAT HAD A FLOOR VIBRATION, ALONG WITH A BLOWER EXTRACT FAULT AND AN ODOR OF SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACD THE AVIONICS COOLING BLOWER FAN. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030430001492003043000149NM 2003 4 30 SWAA030886 120030417A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT RBL 8, BS 813, BS 827, BS 825, BS 845 & BS 847. REPAIRED FLOOR BEAMS PER SWA EA. 2L72 4F RTA16WE 20030430001522003043000152NM 2003 4 30 SWAA030883 120030417A531365C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 4 EA ) AT BS 500C AT STR 7R, BS 520 AT STR 7R, BS 663 AT STR 10R & BS 663 AT STR 10L. R&R STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030430001972003043000197NM 2003 4 30 SWAA030929 120030426A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED C2 CHECK, FOUND LT INBOARD AFT T/E FLAP DELAMINATED AT OUTBOARD CORNER. REMOVED AND REPLACED LT INBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030430002162003043000216NM 2003 4 30 VNAA0304021 120030422A3350321473 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07434JS6771 6151 3051 THE CREW REPORTED THAT THE 5LK EMERGENCY LIGHT POWER SUPPLY WAS BAD. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002282003043000228NM 2003 4 30 AWXA200300435 120030426A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM LAVATORY DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28833AW 1844 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD NR 2 POSITION EMERGENCY FLASHLIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE FORWARD NR 2 POSITION EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030430002392003043000239EU 2003 4 30 AWXA200300366 120030329A5315D5311283620200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y189, AFT SIDE OF FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM TRACK Y189, FR 20; FABRICATED A NEW REPLACEMENT FLOORBEAM TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 18, PG 39-42. 2L72 4F RTA28NM 20030501000252003050100025SO 2003 5 1 SIMA200302204 120030119A532014521725013 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE 145160 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS IN THREE AREAS. COMPLETELY REMOVED CORROSION FROM AREAS BY BLENDING. PERFORMED AN EDDY CURRENT INSPECTION OF BLENDED AREA. NO DEFECTS NOTED. FABRICATED TWO REPAIR DOUBLERS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-40-06 EMB IC2003-145/0137 AND INFORMATION CONTAINED IN AEAI ETN NR EM 53-0361 PAGE 7 FIG 5 ITEM 3. (M) 2L72 4T RTT00011AT 20030501000642003050100064WP 2003 5 1 GTIA030194 120030218A5520 BALANCE WEIGHT DOUG DC9 DC983 3022083WP RT ELEVATOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND RIGHT ELEVATOR BALANCE WEIGHT AND FASTENERS HAVE CORROSION. RECIEVED NEW RIGHT ELEVATOR BALANCE WEIGHT. LOCATED AND DRILLED NEW BALANCE WEIGHT. INSTALLED NEW BALANCE WEIGHT. (M) 2L72 4F RTA6WE 20030501000872003050100087WP 2003 5 1 GTIA030201 120030216A5710 STRUCTURE DOUG DC9 DC983 3022083WP LT WING TO BODY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND LEFT WING, WING TO FUSELAGE CORROSION AT FORMER STATION 807. REMOVED DAMAGED SECTION. FORMED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20030501001322003050100132WP 2003 5 1 ASAA0380134 120030216A33500105603 LIGHT DOUG DC9 DC983 3022083WP FWD CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01965AS 53079 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE FORWARD OF ROW 2. REPLACED DAMAGED CONNECTOR SEGMENT. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030501001372003050100137NM 2003 5 1 ASAA0310070 120030303A55306554842U19 ANGLE BOEING737 737210C 1384459NM VERTICAL STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND VERTICAL STABILIZER SKATE ANGLE AT BS 1016-1138, CHAFED. REMOVED AND REPLACED SKATE ANGLE PER SRM. (M) 2L72 4F A16WE 20030501001522003050100152WP 2003 5 1 ASAA0380117 120030203A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01977AS 53453 SEA - DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE AT ROW 9. REPLACED POEWR SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030501001632003050100163NM 2003 5 1 ASAA0310050 120030227A542065466115 ANGLE BOEING737 737298C 1384490NM NR 1 NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL Z-ANGLE AT NACELLE STATION 159, CHAFED. REMOVED AND REPLACED CHANNEL PER SRM. (M) 2L72 4F RTA16WE 20030501001932003050100193EU 2003 5 1 USAASA03025 120030321A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19729US 1170 TPA - THE AFT EMERGENCY POWER SUPPLY UNIT FAILS THE EMERGENCY LIGHTS TESTS. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALL CHECKS OK. (M) 2L72 4F RTA28NM 20030502000292003050200029SO 2003 5 2 SIMA200309007 120030307A532014522459003 SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION FLOOR BOARD RAMPS SUPPORT CORRODED. REMOVED AND INSTALLED NEW RAMP SUPPORTS IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-04. (M) 2L72 4F RTT00011AT 20030502000462003050200046WP 2003 5 2 ASAA0380146 120030222A52805930583193 DOOR DOUG DC9 DC982 3022082WP MLG CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, RIGHT MLG DOOR AFT OUTBOARD CORNER CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05. (M) 2L72 4F A6WE 20030502000492003050200049WP 2003 5 2 ASAA0380158 120030224A5320993653443 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, LEFT FORWARD FLOOR SUPPORT CORRODED. REPLACED DAMAGED FLOOR SUPPORT PER SRM 51-10-2, 10-3, 30-2 AND 53-14-1. (M) 2L72 4F A6WE 20030502000502003050200050WP 2003 5 2 ASAA0380160 120030225A53119911505 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FRAME CRACKED AT FS 83.5. STOP DRILLED CRACK, AND INSTALLED DOUBLER PER SRM 53-03. (M) 2L72 4F A6WE 20030502000582003050200058WP 2003 5 2 ASAA0380170 120030228A53209911520213 ATTACH ANGLE DOUG DC9 DC982 3022082WP FS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FORWARD CARGO BAY BULKHEAD LOWER GILINER ATTACH ANGLE IS CRACKED AT FS 218. STOP DRILLED CRACK AND INSTALLED STACKED DOUBLER AND TRIPLER PER SRM 53-01. (M) 2L72 4F A6WE 20030502000602003050200060WP 2003 5 2 ASAA0380172 120030301A532199665115 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS CORRODED INSERTS AT FS 1079-1117. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030502000612003050200061WP 2003 5 2 ASAA0380173 120030301A532199579185 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, FLOOR PANEL IS CORRODED ON UPPER SURFACE AT FS 1022. REMOVED CORROSION AND INSTALLED DOUBLER AND HAT CHANNEL PER SRM 51-30-2 AND 53-05. (M) 2L72 4F A6WE 20030502000642003050200064WP 2003 5 2 ASAA0380176 120030301A532039146353 PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND COCKPIT LT SIDE PANEL IS CRACKED. REINFORCED PANEL WITH BONDED FIBERGLASS DOUBLER PER MM 25-00-00. (M) 2L72 4F A6WE 20030502000842003050200084NM 2003 5 2 AWXA200300371 120030414A5753113N280063 SKIN BOEING757 757225 1384959NM LT TE FLAP MISSING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 LAS - FLIGHT CONTROL - FLT 0055 - ON POST FLIGHT WALK AROUND MAINTENANCE FOUND A 6' BY 6" SECTION OF BONDED MATERIAL MISSING FROM THE UPPER SURFACE OF THE LT INBOARD AFT TRAILING EDGE FLAP. MAINTENANCE INSPECTED THE UPPER SURFACE OF THE LT INBOARD AFT TRAILING EDGE FLAP AND FOUND DAMAGE NOT TO REQUIRE MONITOR IAW NOTE B OF 757-200 SRM 57-53-01. AIRCRAFT WAS FLOWN TO PHX WHERE THE DAMAGED FILLER WAS REMOVED, AREA WAS PRIMED, AND A NEW REPLACEMENT FILLER WAS INSTALLED. AREA WAS SANDED TO CONTOUR, PRIMED, AND PAINTED IAW 757-200 SRM 51-21-10. 2L72 4F RTA2NM 20030502000992003050200099EU 2003 5 2 AWXA200300385 120030329A5315D5311282600101 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF RAIL Y-503, BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED RAIL Y-503, BETWEEN FR 14 AND FR 16. FABRICATED A NEW REPLACEMENT RAIL. INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 35. 2L72 4F RTA28NM 20030502001032003050200103NE 2003 5 2 P5CA03000858 220030415A7200 ENGINE BOEING747 747200 1384847NM PWA JT9 JT9D7 52054NE NR 4 OUT OF RIG A P5CAO OTHER O OTHER CRCRUISE 1 WP23524UP 21446 662533 NR 4 ENG CHECKED PART PWR RIGGING CHECKED PS4 WIRE FOR LEAKS, LINE TO AND FROM PT2 SENSOR. UNABLE TO DETERMINE AT THIS TIME, BUT THROTTLE RIG WAS PERFORMED ON ALL FOUR ENGS. 2L74 4F4 FRTA20WE E20EA 20030502001052003050200105NM 2003 5 2 PCA0300836 120030411A5347 SEAT TRACK BOEING747 747249F 1384849NM FUSELAGE BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 SEAT TRACK CROWN BROKEN OFF STA 340-360. REPAIRED PER SRM 53-10-05. 2L74 4F A20WE 20030502001092003050200109NM 2003 5 2 PCA0300840 120030410A5522 SKIN BOEING747 747249F 1384849NM ELEVATOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 RIGHT OUTBOARD ELEVATOR SKIN CRACK STA 360. REPAIR AS PER SRM 51-40-01. 2L74 4F A20WE 20030502001302003050200130NM 2003 5 2 AT0300013 120030414A29337972189502 LINE BOEING717 717200 1383700NM NR 2 ENGINE UNSERVICEABLE A ZZDAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO15985AT 55090 LOST RIGHT HYDRAULIC FLUID AFTER TAKEOFF, HYDRAULIC LOW QUANTITY ALERT ILLUMINATED, HYDRAULIC QUANTITY INDICATES ZERO. RTB PERFORMED, MANUAL GEAR EXTENSION, NORMAL LANDING AND ROLL OUT, TOWED TO GATE. REPLACED NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE IAW MM 29-10, LEAK CHECK. REMOVED AND REPLACED RIGHT AND LEFT MAIN LANDING GEAR DOORS FOR DAMAGE, PROVIDED CLEARANCE ON THE NEW DOORS. OPS CHECK GOOD MM 3200. 2L72 4F TRA6WE 20030501000692003050100069WP 2003 5 1 GTIA030203 120030301A5210 CLIP DOUG DC9 DC983 3022083WP PAX DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - L-1 DOOR HAS TWO CLIPS CRACKED AT TOP OF DOOR STRUCTURE. REMOVED CLIPS. FORMED NEW CLIPS. INSTALLED CLIPS. (M) 2L72 4F RTA6WE 20030501001242003050100124NM 2003 5 1 ASAA0310071 120030303A5320655056825 WEB BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND AFT ENTRY DOOR THRESHOLD WEB AT BS 967, LEFT BUTTOCK LINE 52 CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F A16WE 20030501001972003050100197NM 2003 5 1 ASAA0310054 120030301A5347 SEAT TRACK BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SEAT TRACK AT BS 727-867, RIGHT BUTTOCK LINE 22 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20030430001782003043000178NM 2003 4 30 SWAA030901 120030421A53106935365 SHEAR TIE BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R & STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030430001812003043000181 2003 4 30 SWAA030898 420030421A2565D31354 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030430001832003043000183NM 2003 4 30 SWAA030896 120030421A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430001892003043000189NM 2003 4 30 SWAA030937 120030425A53126545413201 BULKHEAD BOEING737 7373H4 1384600NM AC BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C1 CHECK, FOUND SECONDARY HEAT EXCHANGER OUTBOARD SUPPORT BULKHEAD WEB CRACKED, BS 585 & LBL 40.875. REPAIRED BULKHEAD WEB PER SWA EA. 2L72 4F RTA16WE 20030430001982003043000198 2003 4 30 SWAA030928 420030426A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030430002012003043000201NM 2003 4 30 SWAA030925 120030425A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29787SA 29812 DURING SCHEDULED C4 CHECK, FOUND NUMEROUS EEPLS COVERS CRACKED BETWEEN ROW NR 2 & ROW NR 23. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20030430002042003043000204NM 2003 4 30 VNAA0304017 120030418A2612 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT ENGINE FIRE FALSE INDICATIONA VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07440JS 3058 EN ROUTE, THE CREW RECEIVED A RT ENGINE FIRE INDICATION. UPON ARRIVAL AT TYS, OUTSTATION MAINTENANCE INSPECTED THE RIGHT HAND ENGINE AND FOUND NO VISUAL INDICATIONS OF A FIRE. THEN MAINTENANCE INSPECTED THE RIGHT HAND ENGINE FIRE LOOPS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00 AND FOUND NO DEFECTS. THE AIRCRAFT WILL REMAIN IN TYS OVERNIGHT AWAITING PARTS AND MECHANICS FROM DAY. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002072003043000207NE 2003 4 30 VNAA0304011 220030415A7320 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE IBV VALVE FAILED A VNAAO OTHER J WARNING INDICATION LDLANDING 1 GL07463PS 3087 ON FINAL, THE CREW RECEIVED AN ECU FAIL MESSAGE AT APPROX 100 FEET AGL. HEAVY BRAKING WAS NEEDED AFTER TOUCHDOWN DUE TO THE LACK OF REVERSE THRUST DUE TO THE FAILED ECU. WHILE TAXIING THE CREW HEARD A LOUD NOISE FROM THE RIGHT SIDE OF THE AIRCRAFT AND TAXIIED TO THE RUN UP PAD. THE PASSENGERS WERE THEN DEPLANED AND BUSSED TO THE GATE. MAINTENANCE WAS THEN CALLED OUT TO THE THE RUN UP LOCATION. MAINTENANCE INSPECTED AND CLEANED THE IBV VALVE CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. MAINTENANCE ALSO INSPECTED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00, NO DEFICIENCIES WERE NOTED. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002082003043000208NM 2003 4 30 VNAA0304016 120030418A2120 SMOKE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT DETECTED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07434JS 3051 THE CREW REPORTED SMOKE IN THE COCKPIT OVERHEAD PANEL OR LIGHT ON APU START. OUTSTATION MAINTENANCE INSPECTED THE APU AND FOUND NO DEFECTS, INSPECTED THE OVERHEAD PANEL AND FOUND NO DEFECTS, INSPECTED THE ELECTRICAL SYSTEM AND FOUND NO DEFECTS, ENSURED HX FAN CIRCUIT BREAKERS WERE IN, THEN GROUND RAN THE AIRCRAFT WITH THE CREW AND COULD NOT DUPLICATE ANY SMOKE IN THE COCKPIT, ALL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 49-00-00. AFTER THE GROUND RUN UP WITH THE CREW AND NO DEFECTS WERE NOTED, THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002182003043000218NM 2003 4 30 VNAA0304024 120030427A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07433JS19442276 3047 THE CREW REPORTED THAT THE LAST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002362003043000236SO 2003 4 30 ZKG2003F00002 120030224A275082905002 BELLCRANK PIPER PA46 PA46310P 7104605SO PWA PT6 PT6A34 52043EA LT FLAP BROKEN B ZKGRO OTHER O OTHER NRNOT REPORTED 1 NE059100Z 4608014 PILOT REPORTED A ROLL OF THE AIRCRAFT WHEN THE FLAPS WERE SELECTED DOWN, INSPECTION FOUND LEFT FLAP BELLCRANK BROKEN. THE FAILED PART WAS PREVOUSLY INSPECTED IAW MFG SB 1062 AND FOUND TO BE IN COMPLIANCE. THE BRAKE WAS NOT IN THE AREA OF INSPECTION OF THE SB. THE BRAKE WAS AROUND THE SHAFT. 1L71 3O4 TRTA25SO E4EA 20030429000942003042900094NM 2003 4 29 CH1A200395009 120030408A5320 MOUNT BOEING727 727290 138408WNM GLIDE SLOPE ANT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 GLIDE SLOPE ANTENNA MOUNTING BOX IS CRACKED AT LOWER LT ATTACH ANGLE (INSIDE NOSE RADOME) 2L73 4F A3WE 20030429001402003042900140NM 2003 4 29 AUS20030294 120030212A5311 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME LOCATED IN BILGE AREA AT BS 970 BETWEEN STRINGER28R AND STRINGER 29R CONTAINED LEVEL 2 CORROSION ON THE LOWER LEG. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030429001792003042900179GL 2003 4 29 CA030404010 120030404A2720SL24P SLEEVE DIAMONDA20 DA20A1 2990000GL ROTAX 912 ROTAX912F3 EU HOFMANHOV352HOV352F NE YOKE ASSY INOPERATIVE W A UNSCHED LANDING DF INFLIGHT SEPARATION FLT CONT AFFECTED CRCRUISE 1 CA (CAN) WHEN RIGHT RUDDER WAS APPLIED TO RECOVER FROM A LEFT HAND SPIN A BANG WAS HEARD. THE PILOT FLYINGS (FROM THE RIGHT SEAT) RIGHT RUDDER PEDAL FOLDED TO THE FLOOR. SUBSTANTIAL SLACK WAS NOTED IN THE RIGHT HAND RUDDER CABLE WHERE IT MEETS THE PEDAL. THE PILOT NOT FLYINGS RUDDER PEDALS WERE NOT AFFECTED. AFTER LANDING IT WAS DISCOVERED THAT THE RIGHT SEAT FORWARD OUTBOARD RUDDER CONTROL CABLE (P/N SF12579) HAD PULLED THROUGH THE OVAL SLEEVE AT THE RUDDER YOKE ASSEMBLY END. 1L71 3O3 ONTTA4CH E00051EN5 CTP5BO 20030430000122003043000012NM 2003 4 30 QXEA0300488 120030417A1430 FASTENER BOMBDRDHC8 DHC8401 1390041NM ZONE 600 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - PANEL 622AT HAS TWO GOUGES IN TWO INBOARD FASTENERS ON RIGHT WING. REPAIRED IAW HORIZON AIR EA 6-57-134 AND RD-8/4-57-162 2H72 4T RTA13NM 20030430000412003043000041SO 2003 4 30 C2XA03CL095 120030425A2913971808MODA PUMP EMB 145 EMB145 3260210SO NR 1 ENGINE LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2731131117 145705 THE CREW REPORTED A NR 1 HYDRAULIC LOW QUANTITY AND A ENGINE NR 1 HYDRAULIC PUMP FAIL MESSAGE ON THE EICAS AFTER TAKEOFF.THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE HYDRAULIC PUMP LEAKING BETWEEN THE PUMP HOUSING AND VALVE PLATE.THE PUMP WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030430001422003043000142NM 2003 4 30 SWAA030907 120030422A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 820, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030430001722003043000172NM 2003 4 30 SWAA030862 120030416A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, BELOW STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430001882003043000188 2003 4 30 SWAA030891 420030420A2565D31354 GIRT BAR BOEING737 7373Y0 1384671NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030430002562003043000256NM 2003 4 30 SWAA030817 120030411A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 EEPLS STRIP LOOSE IN CABIN. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030430002602003043000260 2003 4 30 SWAA030821 420030410A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030430002612003043000261NM 2003 4 30 SWAA030822 120030410A32106546113 PIN BOEING737 737317 138447PNM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030430002672003043000267NM 2003 4 30 SWAA030828 120030413A52106918187 ROD BOEING737 7377H4 1384404NM PAX DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29758SW 27873 AFT ENTRY DOOR HARD TO OPEN. FOUND, AFT ENTRY DOOR LOWER GATE ACTUATING ROD BROKEN. REMOVED AND REPLACED ACTUATING ROD PER MM. 2L72 4F RTA16WE 20030430002712003043000271WP 2003 4 30 AALA20030266 120030219A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21585AA 53248 TUL - FOUND RIGHT CUSP HAS CRACKS TWO PLACES STATION 1309 BETWEEN LIGHTENING HOLES APPROX 2.5 INCHES AND AT LIGHTENING HOLES STATION 1291-1297 APPROX 3.5 INCHES. REPLACED CUSP PANEL FROM STATION 1250 TO 1310 RIGHT AARD 53-00-00-07 AND SRM 53-05-00 FIG 97. (M) 2L72 4F A6WE 20030501000012003050100001NE 2003 5 1 ASOA03098 220030310A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LEFT MALFUNCTIONED A O OTHER EJ VIBRATION/BUFFET WARNING INDICATION APAPPROACH 1 SO11708EV 10060 965347 DURING APPROACH INTO DAB FROM ATL, THE LT ENGINE COMPRESSOR STALLED THREE TIMES WITH AIR SPEED OF 180 KTS AT APPROX 4,000 FEET AND FLAPS SELECTED AT 8 DEGREES. THE CREW REDUCED THE POWER ON THE LEFT ENGINE TO IDEL AND THEN AN AMBER LEFT FULL AUTHORITY DIGITAL ELECTRONIC CONTROL MESSAGE CAME ON AND THEN WENT OUT. AN EMERGENCY WAS DECLARED AN THE AIRCRAFT LANDED SAFELY IN DAB. MAINTENANCE REMOVED AND REPLACD THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA EOOO63EN 20030501000042003050100004WP 2003 5 1 AALA20030232 120030212A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 TUL - FOUND FS 1485 CANT FRAME CRACKED, TOP LEFT AFT SIDE. INSTALLED DOUBLER ON FRAME PER AARD 53-10-00-32. (M) 2L72 4F A6WE 20030501000112003050100011WP 2003 5 1 AALA20030271 120030220A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 TUL - FOUND FORWARD RIGHT EMERGENCY EXIT DOOR JAMB UPPER WEB CRACKED AT STATION 872, 876 (TWO PLACES). INSTALLED DOUBLER ON FORWARD RIGHT EMERGENCY EXIT DOOR JAMB UPPER, PER SRM 53-05 FIG 32. (M) 2L72 4F RTA6WE 20030501000282003050100028WP 2003 5 1 AALA20030270 120030220A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 TUL - FOUND FORWARD LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB CRACKED AT STATION 872, 876. INSTALLED DOUBLER ON FORWARD LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB PER SRM 53-05 FIG 32. (M) 2L72 4F RTA6WE 20030501000622003050100062NM 2003 5 1 2003F00237 120030326A7500800347 GASKET BOEING727 727276 138408RNM PWA JT8 JT8D15 52051NE NR 1 ENGINE FAILED A FX7AA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO19908PG 20951 NR 1 ENGINE HAS AN INTERMITTENT FIRE WARNING LIGHT AND HORN AFTER DEPARTURE FROM KMIA USING REDUCED THRUST FOR TAKEOFF. THROTTLE WAS RETARDED TO HALF-WAY POINT AND THE FIRE WARNING EXTINGUISHED. TESTED THE FIRE WARNING SYSTEM AND FOUND IT TO BE OK. DID NOT SHUT DOWN ENGINE, ONLY LOW THRUST SETTING BACK INTO KMIA, WITH NO FURTHER OCCURRENCE. FOUND AIR LEAK AT FUEL HEAT VALVE GASKET. REMOVED FAULTY GASKET AND REINSTALLED VALVE PER MM 75-09-01. RAN ENGINE AT BLAST FENCE AT TAKEOFF POWER FOR 3 MINUTES, ENGINES RAN NORMAL PER MM 71-00. NO WARNINGS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F4 FRTA3WE E2EA 20030501000752003050100075WP 2003 5 1 GTIA030215 120030314A7830 DOOR DOUG DC9 DC983 3022083WP THRUST REVERSER CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND LEFT, T/R, S/N 49914 TOPSIDE DOOR HAS CRACK. FABRICATED 1 DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20030501000942003050100094WP 2003 5 1 GTIA030216 120030218A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND CABIN FLOOR PANEL STATION 886-946 DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030501000962003050100096WP 2003 5 1 GTIA030218 120030301A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND MAIN CABIN STATION 1003 RIGHT SIDE WEB PANEL CRACKED/DAMAGED AT HATS SECTION TWO, PEELING OFF RUB STRIP AND MISSING A PIECE 13 .375 INCH. FABRICATE NEW WEB PANEL. (M) 2L72 4F RTA6WE 20030429002002003042900200CE 2003 4 29 CWQ2003F00006 120030303A21206512072101 DUCT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA CRACKED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05316QS 5600516 DURING ROUTINE INSP LOCKED INTO NACA DORSAL SCOOP AND FOUND THE LOWER AIR VANE PN 6512072-12 CRACKED 1.50 INCH IN A CIRCLE PATTERN AND READY TO BREAK OFF. FOUND SEVERAL OTHER AIRCRAFT OF THIS SAME MODEL WHERE THE PART HAS BROKEN OFF AND BEEN FOUND DOWN STREAM (2 EA PIECES IN DUCT WORK AND 1 EA WEDGED IN FRESH AIR CHECK VALVE, 1 EA MADE IT PAST FRESH AIR CHECK VALVE AND OVERHEAD BLOWER FAN IN CABIN WEDGED INTO AFT BULKHEAD VERTICAL DUCT WORK). REMOVED VANE AND ALSO NOTICED THE LACK OF EA 9309 SECURING INTO PLACE AND THAT V NOTCH WAS CUT WITH HAND SNIPS WITH NO RELIEF HOLE AT INTERSECTION. INSTALLED NEW PART IAW MFG SP. SENT TO MFG FOR EVALUATION. (SCR 91292) 2L72 4F4 FRTA22CE E25EA 20030430000262003043000026NM 2003 4 30 AWXA200300443 120030414A53156545808 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER CAP OF FLOORBEAM AT BS 294.5, RBL 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED TO ACCESS DAMAGED AREA SEAT TRACKS BS 294.5, RBL 45, BS 274.5, RBL 45, BS 274.5, RBL 20, FLOOR SUPPORT BS 274.5 TO BS 294.5, RBL 20, AND TEE CHORD SUPPORT BS 274.5 TO BS 294.5, RBL 15; CUTOUT DAMAGED SECTION OF FLOOR BEAM UPPER TEE CAP; FABRICATED A NEW SECTION OF TEE CHORD, 2 EACH REPAIR ANGLES, AND SHIMS; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-9, FIG. 5, AND REINSTALLED PARTS REMOVED FOR ACCESS IAW B737-200 SRM 51-30-2, PG. 2, & 4-5. 2L72 4F RTA16WE 20030430000382003043000038EA 2003 4 30 COMA0360215 120030424A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01721CA 7259 FLIGHT 5083 ANTI-SKID CAUTION MESSAGE WHEN LANDING GEAR EXTENDED. COULD NOT DUPLICATE, SYSTEM TEST NORMAL. 2L72 4F RTA21EA 20030430000442003043000044WP 2003 4 30 MWEA030189 120030428A5320591014167 PAN DOUG DC9 DC981 3022081WP CARGO BAY GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 MID CARGO BAY DOOR PAN RADIUS AND HUCK FASTNER HEAVILY GOUGED FORWARD SIDE OF DOOR PAN. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030430000562003043000056NM 2003 4 30 USAA030028 120030321A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US49042 23314 PIT - FOUND SKIN CRACKED 1 INCH IN LENGTH, AFT SERVICE DOOR, UPPER HINGE CUTOUT. REMOVED CRACK AND INSTALLED DOUBLER PER TR 52-10-13 AND EA 75742. (M) 2L72 4F RTA16WE 20030430001152003043000115NM 2003 4 30 03FDEA00606 120030425A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FLOORBEAM UPPER FLANGE BS 312, LBL 23, WL 208. 2L73 4F RTA3WE 20030430001222003043000122NM 2003 4 30 03FDEA00555 120030421A5311 FRAME BOEING727 727200 138407ENM FUSELATGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 BS 1050 FRAME PUNCTURED BY FLOOR PANEL FASTENER, RBL 21, WL 156. BS 1050 FRAME RBL 21 W/L 156 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED & INSTALLED REPAIR DOUBLER AT BS 1050, RBL 21, WL 156 IAW SRM 51-30-2. 2L73 4F RTA3WE 20030430001252003043000125NM 2003 4 30 03FDEA00596 120030424A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FLOORBEAM UPPER FLANGE B/S 344, LBL 25-45, WL 208. REMOVED CORROSION ON SEAT TRACK FLANGE BS 460, LBL 25, WL 208. FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED & REPLACED SEAT TRACK BS 344 TO 480, LBL 25, WL 208 PER SRM 51-30-02, 53-10-05. 2L73 4F RTA3WE 20030430001272003043000127NM 2003 4 30 SWAA030922 120030423A5753 STRUCTURE BOEING737 737301 1384611NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED A2 CHECK, FOUND RT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. R&R RT INBD FOREFLAP PER MM. 2L72 4F RTA16WE 20030430001312003043000131 2003 4 30 SWAA030918 420030423A2565 INDICATOR BOEING737 7372H4 138448CNM AFT CABIN DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2L72 4F A16WE 20030430001322003043000132NM 2003 4 30 SWAA030917 120030424A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT STR 26L, BS 395, BS 430 & BS 455. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430001452003043000145NM 2003 4 30 SWAA030890 120030419A79301163P181 PRESSURE SWITCH BOEING737 7372T4 1384492NM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 707403 NR 2 ENGINE OIL FILTER BY-PASS LIGHT ILLUMINATED. R&R NR 2 ENG OIL FILTER & OIL FILTER BY-PASS PRESS SW PER MM. 2L72 4F4 F A16WE E2EA 20030430001482003043000148NM 2003 4 30 SWAA030887 120030421A5315654681143 FLOORBEAM BOEING737 7373H4 1384600NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 996.5, LBL 21. REPAIRED FLOOR BEAM PER SWA EA. 2L72 4F RTA16WE 20030430001822003043000182NM 2003 4 30 SWAA030897 120030422A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED FROM BS 380 TO BS 420, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20030430002242003043000224EA 2003 4 30 SWIA200311914 120030426A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07498SW 7483 ON DEPARTURE, WE RECEIVED A STAB CH 1 INOP STATUS MESSAGE. STAB TRIM WILL RE-ENGAGE, BUT ONLY FOR A FEW SECONDS BEFORE FAILING AGAIN. INTERROGATED MDC AND FOUND HSTCU CH NR 1 FAILED. REMOVED AND REPLACED HSTCU IAW 27-40-00. 2L72 4F RTA21EA 20030430002512003043000251 2003 4 30 SWAA030812 420030412A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030430002552003043000255 2003 4 30 SWAA030816 420030410A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29071SW 22358 AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030430002702003043000270NM 2003 4 30 VNAA0304008 120030412A5210 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR FAILED A VNAAO OTHER O OTHER CRCRUISE 1 GL07472PS 3008 DURING CRUISE, THE CREW RECEIVED A MAIN CABIN DOOR LIGHT ON THE RED WARNING PANEL. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR ROD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030501000182003050100018SO 2003 5 1 SIMA200307601 120030314A2560P2010009120 FLASHLIGHT EMB 135 EMB135LR 3260305SO GALLEY SHORTED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21735TS 145386 BWI - FLT 4834 - CREW REPORTED A SMOKE ODOR COMING FROM THE EMERGENCY EXIT SIGN AT FLIGHT ATTENDANT STATION. CONTRACT MX INSPECTED AND FOUND THAT DE-ICE FLUID HAD SHORTED OUT THE FLIGHT ATTENDANT FLASH LIGHT CHARGER ASSEMBLY. THE CHARGER ASSEMBLY WAS PUT ON MEL AT THIS TIME. MX REMOVED AND REPLACED THE FLIGHT ATTENDANT FORWARD FLASHLIGHT ASSEMBLY IAW. THE EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030501001102003050100110WP 2003 5 1 ASAA0380140 120030223A3350MISC060 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030501001152003050100115WP 2003 5 1 ASAA0380124 120030209A5320593597515 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OAK - DUIRNG C-CHECK, FOUND MID CARGO BAY LEFT FLOOR SUPPORT CRACKED AT TRACK ATTACH RIVET. REPLACED FLOOR SUPPORT AT FS 712 PER SRM 51-10-4 AND 30-2. (M) 2L72 4F RTA6WE 20030501001252003050100125NM 2003 5 1 ASAA0310072 120030303A53206573746 FLOOR SUPPORT BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 947-967, LEFT BUTTOCK LINE 18, RIGHT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20030501001332003050100133WP 2003 5 1 ASAA0380098 120030122A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OAK - DURING C-CHECK, RIGHT WING TO BODY AFT FILLET PANEL LOWER RUB STRIP HAS LIGHT SURFACE CORROSION AROUND FASTENER AND RUBSTRIP. CUT OUT CORRODED SECTION AND INSTLALED DOUBLER AND TRIPLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20030501001402003050100140NM 2003 5 1 ASAA0310084 120030304A54146547966 DOUBLER BOEING737 737210C 1384459NM NR 2 NACELLE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL LATCH PIN DOUBLER AT NACELLE STATION 181 CRACKED. REMOVED AND REPLACED DOUBLER PER SRM. (M) 2L72 4F A16WE 20030501001442003050100144NM 2003 5 1 ASAA0310023 120030221A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 727-727A, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20030501001462003050100146WP 2003 5 1 ASAA0380129 120030212A33500105603 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01973AS 53449 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 25 INOPERATIVE. REINSTALLED, RECONNECTED LIGHT ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030501001472003050100147WP 2003 5 1 ASAA0380130 120030212A33500105603 LIGHT DOUG DC9 DC983 3022083WP ROW 2 DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01973AS 53449 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT MISSING AT ROW 2. REPLACED LIGHT ASSEMBLY, THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030501001552003050100155WP 2003 5 1 ASAA0380127 120030209A5320 DRAIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OAK - DURING C-CHECK, FOUND CORROSION AROUND BELLY DRAINS IN AFT CARGO BAY. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AT FS 1231 PER SRM 53-04. (M) 2L72 4F RTA6WE 20030501001622003050100162NM 2003 5 1 ASAA0310049 120030227A5420657377327 CHANNEL BOEING737 737298C 1384490NM NR 2 NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL CHANNEL AT NACELLE STATION 147, CHAFED. REMOVED AND REPLACED CHANNEL PER SRM. (M) 2L72 4F RTA16WE 20030501001672003050100167NM 2003 5 1 ASAA0310078 120030304A53106549914543 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SHEAR TIE AT BS 1016, STRINGER 24L CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. (M) 2L72 4F RTA16WE 20030501001722003050100172NM 2003 5 1 ASAA0310057 120030301A531069374176 MOUNT BOEING737 737298C 1384490NM DOOR HINGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO DOOR HINGE MOUNT PLATES AT BS 456, STRINGER 18R CORRODED. REMOVED AND REPLACED MOUNT PLATES PER SRM. (M) 2L72 4F RTA16WE 20030501001752003050100175NM 2003 5 1 ASAA0310081 120030304A5320655584311 DRAIN MAST BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND DRAIN MAST PAN AT BS 986, STRINGER 23L-24L CORRODED. REMOVED AND REPLACED DRAIN MAST PAN PER SRM. (M) 2L72 4F RTA16WE 20030501001922003050100192NM 2003 5 1 ASAA0310060 120030301A531069396801 STRINGER CLIP BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DUIRNG D-CHECK, FOUND STRINGER TIE AT BS 1156, STRINGER 12L CRACKED. REMOVED AND REPLACED STRINGER TIE PER SRM. (M) 2L72 4F RTA16WE 20030501002062003050100206NM 2003 5 1 ASAA0310039 120030225A532065319601 PAD BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, STANSION PAD AT BS 500A, RIGHT BUTTOCK LINE 55 CORRODED. REMOVED AND REPLACED STANSION PAD PER SRM. (M) 2L72 4F RTA16WE 20030430001122003043000112NM 2003 4 30 03FDEA00603 120030425A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 N00516 CORROSION (C53-111-01) ON FRAME B.S 640, RBL 4, WL 148. 2L73 4F RTA3WE 20030430001432003043000143NM 2003 4 30 SWAA030906 120030422A335007912 COVER BOEING737 7372H4 138448CNM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER MISSING AT ROW 5. INSTALLED COVER PER MM. 2L72 4F A16WE 20030430002352003043000235NM 2003 4 30 XNOA01112 120030411A2612 CONNECTOR BOEING727 727227 1384078NM FIRE DETECTION DIRTY A XN0AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL23793A 20774 ON TAKEOFF ROLL, FIRE BELL SOUNDED, NO LIGHT INDICATION. BELL COULD ONLY BE SILENCED BY HOLDING IN BELL CUTOUT SWITCH. WHEN RELEASED BELL CONTINUE TO RING. CLEANED CONNECTOR ON FIRE DETECTION BOXES. OPS CHECK GOOD IAW 26-11-00. 2L73 4F A3WE 20030430002622003043000262NM 2003 4 30 SWAA030823 120030413A53306545776 SKIN BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20030430002662003043000266NM 2003 4 30 SWAA030827 120030410A2910272A4452 LINE BOEING737 7373H4 1384600NM HYD SYS LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW29396SW 27690 DIVERSION, A-SYSTEM HYDRAULICS QUANTITY DROPPED TO BETWEEN .25 & .5. FOUND GROUND SPOILER HYD LINE LOOSE. TIGHTENED HYD LINE, LEAK & OPS CHECK GOOD. PER MM 2L72 4F RTA16WE 20030501000062003050100006WP 2003 5 1 AALA20030234 120030130A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 TUL - FOUND CRACK IN FRAME STATION 1174 AT LONGERON 6 LEFT. INSTALLED FRAME DOUBLER AT STATION 1174, L6L PER AARD 53-10-00-30. (M) 2L72 4F A6WE 20030501001422003050100142NM 2003 5 1 ASAA0310025 120030221A5320BAC1513295 SHROUD BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND CARGO BAY CEILING SUPPORT SHROUD AT BS 500A-500B, LEFT BUTTOCK LINE 43 CORRODED. REMOVED AND REPLACED SUPPORT SHROUD PER SRM. (M) 2L72 4F A16WE 20030501001432003050100143NM 2003 5 1 ASAA0310024 120030221A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 663-720, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20030428001332003042800133NM 2003 4 28 DHL2003740002 120030405A5210 HANDLE BOEING727 7272Q9 138448MNM PAX DOOR LACK OF LUBE A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01740DH 21930 MAIN ENTRY DOOR HANDLE EXTREMELY HARD TO TURN TO LOCKED POSITION FROM THE INSIDE. LUBED MAIN ENTRY DOOR HANDLE AND LATCHES OK PER M/M 52-11-01. 2L73 4F RTA3WE 20030428001412003042800141NM 2003 4 28 DHL2003741522 120030401A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, LT FUSELAGE SKIN BS 1270 IS DENTED ABOVE STR 21L. REMOVED 2 EACH PNEUMATIC DUCTS FOR ACCESS MM 36-00-01. CHEMICALLY REMOVED PAINT MM 51-20-01. REMOVED FASTENER AS REQUIRED SRM 51-30-2. CUT OUT DAMAGE AREA 1.25 X 1 INCH SRM 53-30-3 FIG 5. FABRICATED DOUBLER REPAIR 2024 T-3 .063 PO 9912380 9.25 X 8 INCH AND FILLER 2024 T3 .050 PO 9912380- 11.25 X 2 INCH SRM 53-30-3 FIG 5. ALODINED AND PRIMED SRM 51-10-2. INSTALLED COUNTERSINK REPAIR WASHER SRM 51-30-8. INSTALLED DOUBLER AND FILLER REPAIR SRM 51-30-2 AND 53-30-3 FIG 5. SEALED AREA 51-20-4, REINSTALLED 2 PNEUMATIC DUCTS MM 36-00-01. 2L73 4F RTA3WE 20030428001642003042800164WP 2003 4 28 03FDEA00418 120030409A5240AKC70111 HINGE DOUG DC10 DC1030 3023501WP TAIL CONE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC 7011-1. CLOSING ACTION ON 04/09/03. COMPLIED WITH EA 8-5240-68763, TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC 7011-1. 2L73 4F A22WE 20030429000392003042900039NE 2003 4 29 00087 220030407A7200 HOSE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE ASPIRATOR DAMAGED E HAEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05324TW 324 251710A PILOT REPORTED RT ENGINE FLAMED OUT AT 390, ENGINE RELIGHT AT 250, UNEVENTFUL LANDING AT ADS. MAINTENANCE REPLACED P2 ASPIRATOR HOSE PERFORMED GROUND RUNS, CHECK GOOD. 2L72 4J4 J A10CE 1E16 20030429000492003042900049 2003 4 29 GLBA2003046 420030410A3414 INDICATOR BEECH 1900 1900D 1154162CE AIRSPEED STUCK A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM03240GL UE240 NR 1 AIRSPEED IND STUCK AT ZERO. 2L72 4T RTA24CE 20030429000572003042900057NM 2003 4 29 EIA2003054 120030408A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 MAIN DECK STATION 1241 BL 72 LT UPPER LOBE WEB HAS CORROSION. REPAIRED CANTED WEB PER ECRA 471-53-210-2. 2L74 4F A20WE 20030429000622003042900062EA 2003 4 29 SWIA200311868 120030403A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07906SW 7510 DURING APPROACH TO FAT, ATTEMPTED TO EXTEND FLAPS. FLAPS FAIL CAUTION MESSAGE ILLUMINATED AND FLAPS REMAINED AT ZERO DEGREES. FOLLOWED QHR PROCEDURE. LANDED WITH FLAPS AT ZERO DEGREES. RESET CIRCUIT BREAKERS FOR FLAPS CONTROLLER CHANNELS 1 & 2 (CB1 & 2F4). FLAPS FAIL MESSAGE WENT AWAY. CYCLED FLAPS THROUGH SEVERAL CYCLES. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20030429000702003042900070 2003 4 29 372PA0021 420030411A2230 COMPUTER BOEING737 737306 13844BGNM AUTO THROTTLE MALFUNCTIONED A PIDAO OTHER O OTHER CRCRUISE 1 SO05372PA 23546 AUTO THROTTLE DROPPED OFF LINE IN FLIGHT & WOULD NOT RESET. RESET AUTO THROTTLE COMPUTER AND RAN AUTO THROTTLE BITE TEST PER MM 22-31-00. TEST OK. 2L72 4F RTA16NE 20030429000732003042900073NM 2003 4 29 P5CA0300821 120030410A5347 SEAT TRACK BOEING747 747249F 1384849NM FUSELAEG CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 SEAT TRACK STA 1046 RBL 99.0 LEVEL 1 CORROSION. REPAIR PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20030429000782003042900078NM 2003 4 29 P5CA0300824 120030410A5730 SKIN BOEING747 747283B 1384867NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LEFT WING NR 2 STRUT 11B, SKIN CRACKED. FUEL EMERGENCY DRAIN REPAIRED PER SRM 54-34-03 FIG 23. 2L74 4F A20WE 20030429000872003042900087NM 2003 4 29 AWXA200300364 120030328A532065528941 CHANNEL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 LCQ - EES - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON CABIN FLOOR SUPPORT CHANNEL AT BS 520, LBL 4. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT CHANNEL BS 520, LBL 4 - 21; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 16-17. 2L72 4F RTA16WE 20030429001052003042900105SO 2003 4 29 C2XA03SH102 120030413A531014522226003 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV - DURING C-CHECK, THE CENTER BUTT STRAP BETWEEN FRAMES 60 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030429001292003042900129NM 2003 4 29 03FDEA00191 120030301A5753ARC2512504 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING I/B FLAP O/B HINGE PIVOT HOLE LUG CORRODED. SNRM N0582 - RT WING I/B FLAP O/B HINGE PIVOT HOLE LUG HOLE OVERSIZED TO 1.250 INCH AS PER SRM 51-31-01 VOL II AND REPROTECTED AS PER SRM 51-21-01 VOL II. COMPLIED WITH FEDEX EA 1-5750-68593 WINGS- RIGHT INBOARD TRAILING EDGE FLAP- HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20030429001302003042900130NE 2003 4 29 AUS20030251 120030224A53207620123014138 ANGLE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE TAILBOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE TEE SECTION CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN). CRACK IS LOCATED IN AREA IMMEDIATELY ABOVE THE TOP LT TAIL BOOM ATTACHMENT FITTING AND APPEARS TO HAVE INITIATED FROM THE RADIUS CUT AT THE END OF THE STRINGER. 1G72 3U3 UNCH1NE E19EU 20030429001322003042900132NM 2003 4 29 AUS20030269 120030207A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE STRINGER 18A LOCATED AT STN 930 RT CONTAINED LEVEL 2 CORROSION BETWEEN THE FASTENERS ON THE LOWER LEG OF THE TEE SECTION. FOUND DURING INSPECTION IAW CPCP C53-100-01. 2L73 4F4 FRTA3WE E2EA 20030429001332003042900133NM 2003 4 29 AUS20030284 120030212A5311 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME FLANGE LOCATED AT BS 720A CONTAINED LEVEL 2 CORROSION IN AREA BETWEEN STRINGER 27R AND 28R. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030429001412003042900141NM 2003 4 29 AUS20030296 120030212A5320 BRACKET BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CLIP BRACKET JOINING STRINGER 27L TO FRAME AT LOCATION BS 1130 CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INVESTIGATION IAWC53-113-01. 2L73 4F4 FRTA3WE E2EA 20030425000882003042500088NM 2003 4 25 QXEA0300395 120030316A5420 SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND LONGITUDINAL SUPPORT ALONG UPPER END OF FOD DOOR ACTUATOR IS CRACKED AT AFT END. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030428000132003042800013EA 2003 4 28 QXEA0300415 120030401A2611 SCREEN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09605QX 10022 BOI- FORWARD CARGO BAY CENTER CHIMNEY SCREEN IS DAMAGED. REPAIRED IAW REO 670-53-32-001. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030428000682003042800068NM 2003 4 28 QXEA0300427 120030401A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FUSELAGE BELLY SKIN SCRATCHED AT STATION X32.40 BETWEEN STRINGERS 30P AND 31P. REPAIRED IAW RD 8/4-53-489. 2H72 4T RTA13NM 20030428000802003042800080 2003 4 28 CH1A200381011 420030405A3442 RECEIVER BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE WEATHER RADAR INOPERATIVE A C1HAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15681CA 22020 DURING FLIGHT WEATHER, RADAR WOULD TEST BUT NOT PAINT WEATHER. DIVERTED INTO MCO TO REPAIR WEATHER RADAR. 2L73 4F4 F A3WE E2EA 20030428000942003042800094NM 2003 4 28 VNAA0303034 120030330A30607013348937 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT PROPELLER FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07426JS3972 3038 AFTER TAKEOFF THE RIGHT PROPELLER HEAT FAILED. THE FLIGHT CREW RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE RIGHT DATA ACQUISTION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-42-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030428001512003042800151NM 2003 4 28 DHL2003746005 120030407A2612 WARNING HORN BOEING727 727224 1384076NM APU FIRE INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01746DH 22252 APU FIRE WARNING HORN, IN NOSE GEAR WELL, IS INOPERATIVE. TRANSFERRED TO DMI 12489 PER MEL 26-11-2 CAT-C. REF DMI 12489 APU FIRE WARNING HORN IN NOSE GEAR WELL IS INOPERATIVE. TROUBLESHOT PER WDM 49-41-0, FOUND HORN INOPERATIVE. REMOVED AND REPLACED HORN, OPS CHECKED NORMAL. THIS CLEARS DMI 12489. 2L73 4F A3WE 20030428001612003042800161WP 2003 4 28 ZW0A0304002 120030408A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13964TW 53614 THE EGRESS LIGHT WAS INOPERATIVE AT ROW 22. RESEATED THE LAMP. CHECK-C 5-25-2002. 2L72 4F RTA6WE 20030428001712003042800171WP 2003 4 28 03FDEA00407 120030408A5410 SEAL DOUG DC10 DC1030 3023501WP NR 3 ENGINE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 3 ENGINE O/B CORE COWL UPPER SEAL AFT OF AFT HINGE GOUGED. CLOSING ACTION ON 04/07/03. REMOVED DAMAGED SEAL IAW SRM 51-35-01. FAB NEW SEAL ON TRAVELER T2/304970. INSTALLED SEAL IAW SRM 51-35-01. 2L73 4F A22WE 20030429000982003042900098NM 2003 4 29 CH1A200395013 120030409A5280 HINGE BOEING727 727290 138408WNM LT MLG DOOR CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LT MLG WING DOOR UPPER FWD HINGE (2 EACH) CRACKED AND LOOSE HARDWARE PULLING THROUGH 2L73 4F A3WE 20030429001762003042900176NE 2003 4 29 CA030404006 220030325A7420T20016 HARNESS AIRTRCAT400 AT401 0390204SW ORENDAOE600AOE600A NE IGNITION DAMAGED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) UPON PERFORMING THE SCHEDULED 200 HOUR ENGINE INSPECTION, THE IGNITION HARNESS ASSEMBLY WAS FOUND TOBE DAMAGED DUE TO EXCESSIVE HEAT. THE DAMAGE WAS LOCATED AT THE B5 SPARK PLUG LEAD. DIRECT EXPOSURE TO EXHAUST GASES WAS RULED OUT AS THE CAUSE OF THE DAMAGE, AS NO EXHAUST LEAKS WERE FOUND. THE IGNITION HARNESS WAS REPLACED. INVESTIGATION INTO THE CAUSE, AND FORMULATION OF CORRECTIVE ACTION CONTINUES. MORE DETAILS TO FOLLOW. 1L71 3R3 V A17SW E0006A 20030429002012003042900201NM 2003 4 29 CALA0300189 120030411A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND KEELBEAM LOWER CHORD CORRODED AT BS 500B-520, S28L. REPAIRED IAW SRM 53-30-12, FIGURE 202. 2L72 4F RTA16WE 20030429002282003042900228NM 2003 4 29 SWAA030766 120030406A32306546113 TRUNNION BOEING737 7375H4 138449DNM LT MLG W/W CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030430000082003043000008NM 2003 4 30 QXEA0300490 120030411A5350 FAIRING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - WING TO FUSELAGE FAIRINGS, PANEL 261LT FUSELAGE ATTACH FLANGE. HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030430000102003043000010NM 2003 4 30 QXEA0300486 120030419A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - MULTIPLE SCRATCHES AND GOUGES AT X61 AND STRINGER 31R. REPAIRED IAW HORIZON AIR EA 6-53-242 AND RD 8/4-53-529. 2H72 4T RTA13NM 20030430000132003043000013EA 2003 4 30 QXEA0300510 120030426A497041410284 VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09615QX 10065 PDX- ON FLIGHT 2438 OUT OF 10,000 FEET ON ARRIVAL TO PDX, RECIEVED A "APU FAULT" CAUTION MESSAGE. APU OPERATED NORMALLY. BEGAN TO RUN ABNORMAL CHECKLIST AND MESSAGE WENT OUT AFTER TWO MINUTES. REMOVED AND REPLACED DEPRIME SELINOID VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030430000272003043000027NM 2003 4 30 AWXA200300442 120030428A3350BR964411 LIGHT BOEING737 737300 1384610NM SEAT ROW 20 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LAS - EEL - EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 20 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 20 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030430000402003043000040EA 2003 4 30 COMA0370012 120030424A3260895303 PROXIMITY SENSOR CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01355CA1015 10067 FLIGHT 5679 LANDING GEAR DISAGREE WARNING, GEAR DID NOT RETRACT. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT 2L72 4F RTA21EA 20030430000432003043000043WP 2003 4 30 MWEA030190 120030428A533059102285 SKIN DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 FUSELAGE SKIN IS CRACKED AT STATION 1437 BETWEEN LONGERON 3&4 RIGHT. -- FABRICATED AND INSTALLED FILLER. COUNTERSUNK DOUBLER AND INSTALLLED. 2L72 4F A6WE 20030430000452003043000045WP 2003 4 30 MWEA030188 120030428A53203926046501 FITTING DOUG DC9 DC981 3022081WP CARGO BAY CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 MID CARGO BAY DOOR FITTING CRACKED, LOWER AREA. LOCATED, DRILLED AND INSTALLED FITTING. 2L72 4F A6WE 20030430000492003043000049EU 2003 4 30 2003UALA00390 120030423A2497 CABLE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ELECTRICAL BURNED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29463UA 1282 FLIGHT DIVERTED DUE TO SMOKE ODOR IN THE CABIN. FOUND PIN 'A' OF CONNECTOR 400VCA SEVERELY BURNED, ALONG WITH RECEPTICLE. REPLACED IDG POWER CABLE AND PYLON POWER CABLE. 2L72 4F4 FRTA28NM E40NE 20030430000522003043000052EU 2003 4 30 2003UALA00385 120030417A2131 COMPUTER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29475UA 1495 DIVERSION DUE TO LOSS OF CABIN PRESSURE. AIRCRAFT EXPERIENCED DUAL BLEED SYSTEM FAILURE - LT BLEED LEAK & ENG 2 BLEED FAULT. THE BLEED MANAGEMENT COMPUTER WAS REPLACED FOR THE REPORTED BLEED LEAK (NO LEAKS WERE FOUND) AND THE FAN AIR THERMOSTAT WAS REPLACED FOR THE NR 2 BLEED SYSTEM FAULT. 2L72 4F4 FRTA28NM E40NE 20030430000602003043000060NM 2003 4 30 USAABB03045 120030318A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19633AU 27811 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS ARE ROWS 1, 4, 6, 26 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030430000762003043000076NE 2003 4 30 MEX2003098 220030327A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LEFT FOD A ASMFK NONE O OTHER ININSP/MAINT 1 SW23160PL 49763 MID-MEX - DURING TRANSIT CHECK, A FOREIGN OBJECT DAMAGE ON LEFT ENGINE WAS DETECTED. DURING INSPECTION DETECTED 7 BLADES WITH DAMAGE AND TWO BLADES OUT OF LIMITS. SHOP MECHANICS, SENT TO BLADE CHANGE AND BORESCOPE INSPECTION. (M) 2L72 4F4 FRTA6WE E9NE 20030430000842003043000084SO 2003 4 30 SIMA200308407 120030320A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND INSTALLED NEW SILL IAW EMB REPAIR STATEMENT IC2003-145/0818. (M) 2L72 4F RTT00011AT 20030428001682003042800168NM 2003 4 28 03FDEA00411 120030409A7710 COMPRESSOR BOEING727 727100 1384036NM NR 3 ENGINE STALLED A FDEAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO25188FE 19081 RIGHT AFTER ROTATION AND LIFT OFF, NR 3 ENGINE HAD 3 LARGE COMPRESSOR STALLS WITH EPR DROP TO 1.2/1.4. RAMP PERSONNEL SAW FLAMES OUT REAR OF ENGINE. SHUT DOWN NR 3 ENGINE IAW QRH AND COMPLIED WITH REMAINING QRH PROCEDURES. UNEVENTFUL LANDING. R&R'D NR 3 ENGINE PER ENGINE CHANGE WORK CARD 70T0501-03 UP TO ITEM 6. J. COMPLETED ENGINE CHANGE WORK CARD 70T0501-03 AND ENGINE RUN WORK CARD 70T0301-03. ALL SYSTEMS OPS CHECK NORMAL. 2L73 4F RTA3WE 20030428001802003042800180NM 2003 4 28 F3LA200300115 120030406A21337110033 OUTFLOW VALVE BOEING737 73736E 138443ANM CABIN PRESSURE FAILED A F3LAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03315FL 215 25159 FLIGHT CREW REPORTED TOTAL LOSS OF PRESSURIZATION AT CRUISE ALTITUDE. INOPERATIVE IN STANDBY AND MANUAL. MAX CABIN ALTITUDE 18,500/2,000 FPM. NO RAPID DECOMPRESSION. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED AFT OUTFLOW VALVE, CABIN PRESSURE CONTROLLER, AND OVERHEAD SELECTOR PANEL. PERFORMED OPERATIONAL TEST, CHECKED NORMAL. OXYGEN GENERATORS USED AT ROWS 12 DEF, 15 ABC, 16 ABC, 16 DEF, 17 ABC, 17 DEF, 18 ABC, 18 DEF, 19 DEF, 20 ABC, AND 22 ABC. REPLACED SAME. 2L72 4F RTA16WE 20030429000142003042900014NM 2003 4 29 P50300797 120030129A5320 INTERCOSTAL BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 FWD CGR SHEARED RIVETS ON SEAT TRACK AND CRACK ON INTERCOSTAL BETWEEN LBL 25-LBL45. DAMAGED INTERCOSTAL REMOVED, NEW FABRICATED H/F 2024 T30.050 THK PER SAMPLE PER SRM 53-10-21. PROTECTED AREA PER SRM 51-10-02. RIVETED PER SRM 51-30-02. 2L74 4F A20WE 20030429000712003042900071NM 2003 4 29 P5CA0300828 120030410A5320 INTERCOSTAL BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 BODY GEAR W/W STA 1438 1460 1 INCH CRACK AT INTERCOSTAL AT LONGERON BOX. REPAIR PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20030429000842003042900084NM 2003 4 29 AWXA200300360 120030410A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 16 BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28325AW 23260 PHX - EEL - FLIGHT CREW REPORTED THAT THE EMERGENCY ESCAPE PATH LIGHT WAS BROKEN OFF SEAT ROW 16 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030429001352003042900135NM 2003 4 29 AUS20030288 120030212A5311 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME LOCATED AT BS 1050 STRINGER 27R CONTAINED LEVEL 3 CORROSION ON THE TOP FLANGE. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030430000062003043000006NM 2003 4 30 QXEA0300492 120030411A5350 FAIRING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - WING TO FUSELAGE FAIRING, PANEL 261FT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030430000292003043000029NM 2003 4 30 AWXA200300440 120030427A5210 BOTTLE AIRBUSA319 A319132 3930340NM PAX DOOR DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28832AW 1643 LAS - EES - DURING INSPECTION MAINTENANCE FOUND THE R-1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R-1 DOOR ASSIST BOTTLE TO PROPER PRESSURE. 2L72 4F RTA28NM 20030430000812003043000081SO 2003 4 30 SIMA200307602 120030316A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN FAILED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21624AE 145111 CMH - FLT 3213 - CREW REPORTED THE MOST AFT SECTIONS OF FLOOR PROXIMITY EMERGENCY LIGHTS DO NOT ILLUMINATED. MAINTENANCE REPLACED THE AFT FLOOR PROXIMITY STRIP LIGHTS IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030430000862003043000086NM 2003 4 30 USAA030026 120030309A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19371US50906 22950 CLT - FOUND SKIN CRACKED 2 INCH, BS 727E AND S24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20030430000922003043000092NM 2003 4 30 USAA030035 120030312A5320 WEB BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU58629 22198 CLT - FOUND WEB CRACKED .250 INCH, BS 1440 S26R. DAMAGED REMOVED, INSTALLED SPLICE REPAIR AND DOUBLER PER EA 86992. (M) 2L72 4F RTA2NM 20030430001012003043000101EU 2003 4 30 55691 120030429A2841 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE COCKPIT MALFUNCTIONED A UHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL17149SZ 340A149 369353 AFTER TAXING AWAY FROM THE GATE NOTICED THE NR 2 FUEL FLOW GAUGE WAS INOP AND THE NR 1 PROP OIL GAUGE INDICATING JUST ABOVE ZERO. THE AIRCRAFT RETURNED TO THE GATE 2L72 4T4 TRTA52EU E8NE6 20030430001192003043000119WP 2003 4 30 03FDEA00601 120030424A5710 HINGE DOUG DC10 DC1030 3023501WP WINGS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR S 32 C/W E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 04/18/03. COMPLIED WITH E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK. 2L73 4F A22WE 20030430001372003043000137NM 2003 4 30 SWAA030912 120030423A2751113A3910 BELLCRANK BOEING737 7377H4 1384404NM FLAP DRIVE BROKEN A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29723SW 27855 WHEN FLAPS EXTENDED, AIRCRAFT ROLLS LEFT. FOUND, NR 1 AFT FLAP DRIVE INBD BELLCRANK BROKEN. R&R NR 1 AFT FLAP BELLCRANK PER MM. 2L72 4F RTA16WE 20030430001512003043000151NM 2003 4 30 SWAA030884 120030419A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430001582003043000158NM 2003 4 30 SWAA030877 120030418A53126517583 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, WL201 AT LBL 5.5 & BS 178, WL 213 AT RBL 6.5. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030430001602003043000160NM 2003 4 30 SWAA030875 120030419A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 262 TO BS 270, STR 14R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030430001612003043000161NM 2003 4 30 SWAA030874 120030419A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 264 TO BS 275, STR 14L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030430001662003043000166NM 2003 4 30 SWAA030868 120030416A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKS (2 E ) AT BS 912 BELOW STR 24R & BS 940 ABOVE STR 24L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030430001692003043000169NM 2003 4 30 SWAA030865 120030416A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030430001862003043000186NM 2003 4 30 SWAA030893 120030420A53126517582 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 227 & LBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM. 2L72 4F RTA16WE 20030430001992003043000199 2003 4 30 SWAA030927 420030427A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030430002022003043000202NM 2003 4 30 SWAA030924 120030427A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030430002032003043000203NM 2003 4 30 DHL2003727004 120030429A4930 FUEL BOWL BOEING727 727228 1384083NM APU FUEL SYS LEAKING A DHLAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01727DH 20204 VERY STRONG ODOR OF JET FUEL IN COCKPIT. FOUND SMALL APU FUEL FILTER LEAKING. TRANSFERRED TO DMI 12706 IAW MEL 49-1 CAT-C. PLACARDS INSTALLED. REF DMI 12706 VERY STRONG ODOR OF FUEL IN COCKPIT. REMOVED AND REPLACED HIGH PRESSURE FUEL BOWL AND TESTED IAW 727 M/M CHAPTER 49-00. NO LEAKS NOTED AT THIS TIME. THIS CLEARS DMI 12706. PLACARD REMOVED. 2L73 4F RTA3WE 20030430002062003043000206 2003 4 30 VNAA0304013 420030416A3418 STALL WARNING DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07458PS 3068 DURING TAKEOFF, THE CREW RECEIVED A PUSHER, TAKEOFF CONFIGURATION, AND A FLAP CAS MESSAGES AND ABORTED TAKEOFF. OUTSTATION MAINTENANCE RESET THE STICK PUSHER AND RERACKED THE FLAP CONTROL AND BOTH IAC'S IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR A FERRY FLIGHT. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002112003043000211NM 2003 4 30 VNAA0304009 120030414A3350PS835C POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07472PS168501324 3008 THE CREW REPORTED THAT THE EMERGENCY BATTERY WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002172003043000217NM 2003 4 30 VNAA0304023 120030426A5210 BOLT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR OUT OF ADJUST A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07431JS 3028 EN ROUTE, THE CREW RECEIVED A DOORS LIGHT ON THE RED WARNING PANEL. WHEN THE FLIGHT ATTENDANT CHECKED THE DOOR, THE LIGHT EXTINGUISHED. THE FLIGHT WAS AT 25,000 FEET. FLIGHT 4094 LANDED AT CLT WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED, MEASURED AND ADJUSTED THE SHOOT BOLT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. THE AIRCRAFT WAS THEN TAKEN FOR A FUNCTIONAL CHECK FLIGHT IN WHICH THERE WERE NO DEFECTS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002222003043000222SO 2003 4 30 SWIA200311916 120030426A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07223SW 120291 NACELLE FLAPS DROP SLIGHTLY (UNCOMMANDED). REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECK GOOD. NO HYDRAULIC LEAKS NOTED. S/N OFF: 0187. 2L72 4T RTA31SO 20030430002252003043000225EU 2003 4 30 AWXA200300439 120030415A5210 BOTTLE AIRBUS320 A320232 3930326EU PAX DOOR DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 PHX - EES - DURING INSPECTION MAINTENANCE FOUND THE L-1 DOOR EMERGENCY ASSIST BOTTLE PRESSURE LOW. SERVICED L-1 DOOR EMERGENCY ASSIST BOTTLE IAW AMM 52-10-00-301. 2L72 4F RTA28NM 20030430002272003043000227NM 2003 4 30 AWXA200300436 120030426A5610 WINDSHIELD BOEING757 7572G7 1384963NM COCKPIT FAILED A AWXABA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 WP28908AW 24233 EN ROUTE, THE CAPTAINS FORWARD WINDSHIELD BEGAN TO MAKE A POPPING SOUND, WINDOW CRACKED, DESCENDED TO LOWER ALTITUDE AND SLOWER SPEED FOR FEAR OF LOSING WINDOW, DIVERTED TO ONT. MAINTENANCE REMOVED AND REPLACED LT FORWARD WINDSHIELD IAW AMM 56-11-01, PG. 401. AS PRECAUTION, REPLACED WINDOW HEAT CONTROLLER LT FRONT IAW AMM 30-41-01, PG. 401. VENDOR FUNCTIONAL TEST OF WINDOW HEAT CONTROL S/N 107C-1046 WAS NO FAULT FOUND. UNIT PASSED BENCH TEST IAW HONEYWELL CMM 30-41-07, REV 12, AND WAS RETURNED TO SERVICE. VENDOR CONFIRMED FAILURE OF WINDSHIELD S/N 908AWCPT1, FAILURE ANALYSIS NOT ACCOMPLISHED, WINDSHIELD SCRAPPED AT VENDOR. 2L72 4F RTA2NM 20030429000502003042900050EA 2003 4 29 03099680 120030409A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27680BR 7679 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT HALF OF THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 4 INVERTER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030429000612003042900061EA 2003 4 29 SWIA200311867 120030331A5753601R146991 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT TE FLAPS BURNED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07445SW 7651 LEFT OUTBOARD FLAP TRAILING EDGE HAS SEVERAL BURNED AREAS AS A RESULT OF A LIGHTNING STRIKE. INSTALLED SERVICEABLE FLAP ON LEFT OUTBOARD POSITION IAW 27-54-01 AND 27-54-05. S/N OFF: SB/RJ/731. 2L72 4F4 FRTA21EA E15NE 20030429001892003042900189NM 2003 4 29 CA030409009 120030409A792128E99X OIL COOLER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ENGINE OIL LEAKING W EA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) AIRCRAFT LOST OIL PRESSURE ON NR 2 ENGINE. ENGINE SHUTDOWN AND SECURED IAW QRH AND FLIGHT DIVERTED TO YXT. OIL COOLER FOUND TO BE CRACKED WITHIN THE COOLING CORE. THIS WAS AN OVERHAUL UNIT FROM THE MANUFACTURE TO POST SB CONFIGURATION. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030502000202003050200020WP 2003 5 2 ASAA0380137 120030215A532199365485 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL FOND TO HAVE 4 CORRODED INSERTS FROM FS 110-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030502000342003050200034WP 2003 5 2 ASAA0380139 120030215A5347SR095301157001 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, SEAT TRACK CORROSION AT FS 200-255. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 53-05. (M) 2L72 4F A6WE 20030502000802003050200080GL 2003 5 2 03FDEA00578 220030422A7200 ENGINE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 3 FLAMED OUT A FDEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO256804950886 47803 NR 3 ENGINE OIL STRAINER CLOG LIGHT CAME ON AT FL 330. AS WE WERE ABOUT TO START THE RED TABS CHECK LIST FOR THIS PROBLEM NR 3 ENGINE FLAMED OUT. AT TIME OF FLAME OUT ALL ENGINE INDICATIONS WERE NORMAL. RED TABS COMPLETED. AIRCRAFT DIVERTED TO KDEN FOR PRECAUTIONARY LANDING. REMOVED AND REPLACED #3 ENGINE IAW FEDEX WORKCARDS . 2L73 4F4 F A22WE E23EA 20030502000982003050200098EU 2003 5 2 AWXA200300384 120030329A5310D5348002069601 SHEAR TIE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK, A 1 INCH CRACK WAS FOUND ON SHEAR WEB AFT SIDE OF FR 68 AND OUTBOARD OF Y-1292 LT. MAINTENANCE REMOVED CRACKED SHEAR WEB AFT SIDE OF FR 68, Y1292 LT; FABRICATED A NEW REPLACEMENT SHEAR WEB. INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 21-22 & 35. 2L72 4F RTA28NM 20030502001602003050200160NM 2003 5 2 DHL2003741532 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS A SHARP DENT AT BS 420 BELOW STR 18L. CUT OUT DAMAGE AREA 1.90 X 1.60 INCH AT BS 420 BELOW STR 18L IAW B-727 SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER 10 X 7.375 INCH 2024 T-3 -.071 PO 9912598 IAW B-727 SRM 53-30-3 FIG 3. TREATED AND PRIMED IAW B-727 SRM 51-10-6. INSTALLED REPAIR DOUBLER IAW B-727 53-30-3 FIG 3. 2L73 4F RTA3WE 20030502001632003050200163SO 2003 5 2 C2XA03BT053 120030417A2750 CONNECTOR EMB 145 EMB145 3260210SO TE FLAPS DIRTY A C2XAO OTHER S AFFECT SYSTEMS APAPPROACH 1 SW2713956 145078 EWR---CO2546, CREW REPORTED FLAP FAILED, DECLARED EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTED FLAPS AND CHECKED ELECTRICAL CONTINUITY IN ALL CONNECTOR PINS FOR LEFTHAND AND RIGHTHAND FLAP TRANSMISSION BRAKES AND FLAP VELOCITY SENSORS. INCLUDING PINS 46, 47, 92, 93, 42, 43, 45, 88, 89, 91, 8, 9, 115, 116, 17, 16, 44, 107, 106 AND 90 IN CONNECTOR P1104. ALL CHECKED GOOD. CLEANED CONNECTOR P1247, P1248, FLAP VELOCITY SENSOR CONNECTOR AND P1105, P1106, P1107 AND P1108. OPS CHECKED FLAP SYSTEM GOOD IAW EMB145 MM 27-53-00 AND EMB145 WM 27-53-51. NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030502001652003050200165NM 2003 5 2 03FDEA00575 120030422A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 WHILE WORKING CARD N00303 FOUND CORROSION ON STR 27 LT FROM BS 1130-1040. \ 2L73 4F RTA3WE 20030502002032003050200203NM 2003 5 2 UPS03M40439 120030320A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT RBL 8.5 BETWEEN STA 784-939 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK RBL 8.5 STA 784-939 & FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK REWORKED AND HOLES PICK UP AS PER SRM 53-70-00 VOL I REV 32, PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK FASTENER INSTALLED AS PER 53-70-00 VOL I REV 32 STA STA 784-939 RBL 8.5 2L73 4F RTA22WE 20030502002322003050200232EA 2003 5 2 QXEA0300445 120030410A2120 FAN CNDAIRCL600 CL6002C10 1390015EA CABIN AIR FAILED A QXEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09608QX 10026 PDX-ON FLIGHT NUMBER 2449, FAINT ODOR OF BURNING PLASTIC IN COCKPIT AND CABIN. RECIRCULATING FAN CIRCUIT BREAKER POPPED. TURNED OFF RECIRCULATING FAN, ODOR DISAPPEARED. PLACED ON RSI 326845. 2L72 4F RTA21EA 20030501001502003050100150WP 2003 5 1 ASAA0380096 120030120A5610MS210434 NUT DOUG DC9 DC983 3022083WP COCKPIT WINDOW LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 PDX - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE DIFFICULT TO OPEN. AFT TRACK BLOCK SECURING NUT HAD BECOME LOOSE. RESECURED AFT TRACK BLOCK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030502000112003050200011WP 2003 5 2 ASAA0380136 120030215A532199365445 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, CABIN FLOOR PANEL TO HAVE 16 CORRODED INSERTS FROM FS 160 TO 200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030502000402003050200040WP 2003 5 2 ASAA0380152 120030224A532059134217 WEB DOUG DC9 DC982 3022082WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND WEB IS CHAFED AT AFT END OF RIGHT NLG DOOR. MATERIAL LOSS IS IN EXCESS OF 20 PERCENT. REPLACED NLG DOOR JAMB GUSSET PER SRM 51-10-2, 10-4, 30-2, AND 30-5. (M) 2L72 4F A6WE 20030502000572003050200057WP 2003 5 2 ASAA0380169 120030228A5320993053839 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, RIGHT CUSP WEB IS CRACKED AT FS 218. REPLACED CUSP WEB PER SRM 51-10-2, 10-4, 30-2, AND 30-5. (M) 2L72 4F A6WE 20030502001152003050200115NM 2003 5 2 UPS03M40437 120030320A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT LBL 8.5 BETWEEN STA 791-840 FOUND CORRODED. CORROSION REMOVED AT STA 791-840 LBL 8.5 & FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK REWORKED AND HOLES PICKED OUT AS PER AS PER SRM 53-70-00 VOL I REV 32, PROTECTED PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 VOL I REV 32 AT STA 791-840 LBL 8.5. 2L73 4F RTA22WE 20030502001542003050200154NM 2003 5 2 HNAA0300020 120030415A541087140303007 CONE DHAV DHC8 DHC8102 2809003NM NR 1 NACELLE BROKEN A HNAAO OTHER C F.O.D. NRNOT REPORTED 1 EA07931HA 132 CREW REPORTED A WHISTLE SOUND FROM NR 1 ENGINE WHENEVER POWER WAS APPLIED. FOUND A PIECE OF THE NR 1 LOWER COWL AFT CONE HAD BROKEN OFF CAUSING FOD DAMAGE TO NR 1 ENGINE. REPLACED ENGINE AND LOWER COWL. 2H72 4T RTA13NM 20030502001552003050200155NM 2003 5 2 03FDEA00473 120030417A5320 PANEL BOEING727 727200 138407ENM CARGO BAY TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CABIN STA 400 LEFT SIDEWALL PANEL IS TORN IN UPPER AREA. 2L73 4F RTA3WE 20030502001812003050200181NM 2003 5 2 AWXA200300376 120030415A53302024T3 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - MAJOR REPAIR - DURING INSPECTION A 3.875 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT LAP SEAM BS 737, STR 24 LT. MAINTENANCE TRIMMED OUT DAMAGE ON SKIN AT BS 737, STR 24 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 210 PG 227-230. 2L72 4F RTA16WE 20030502002532003050200253WP 2003 5 2 03FDEA00586 120030423A5230 BRACKET DOUG DC10 DC1030 3023501WP CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25317FE 46835 AFT CARGO DOOR HAS LWR AFT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DC10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20030502002562003050200256EA 2003 5 2 COMA0360212 120030422A322016050105 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG FLAT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01964CA16651 7129 FLIGHT 5758 LANDING GEAR DISAGREE WARNING, NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NOSE LANDING GEAR STRUT PISTON ASSEMBLY. 2L72 4F RTA21EA 20030502002642003050200264NM 2003 5 2 03FDEA00442 120030415A3260 SWITCH BOEING727 727100 1384036NM ZONE 700 CORRODED A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25188FE 19081 DURING FIRST FLIGHT GEAR EXTENSION GOT NO GREEN NOSE GEAR INDICATOR (NO RED ONE EIGHTER) LIGHTS CHECKED GOOD, LONG AFTER OTHER MAIN GEAR INDICATION ON S/O PANEL, A PRESSURE WAS NORMAL. AFTER RECYCLING GEAR GOT NORMAL GEAR IND. LANDED UNEVENTFULLY. FOUND WATER AND CORROSION ON POSITION SWITCH ELECTRICAL CONNECTOR. REMOVED CORROSION AND WATER, OPS CHECKED IAW B727-100 M/M 32-61-021-5. ALL CHECKS GOOD AT THIS TIME. 2L73 4F RTA3WE 20030502002732003050200273NM 2003 5 2 SWAA030852 120030416A5315BAV1509 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 727D + 5, RBL 3 & BS 727B + 3, LBL 3. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20030502002832003050200283NM 2003 5 2 751PA0015 120030417A3350 LIGHT BOEING757 757200 1384950NM EXTERIOR INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 R-1 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK OK. 2L72 4F RTA2NM 20030505000062003050500006NE 2003 5 5 03FDEA00448 220030415A7520 MANIFOLD DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE ENGINE AIR SYS DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 1 ENGINE SIDE LONGITUDINAL CDP AIR 14TH STAGE MANIFOLD FWD END 90 DEG ELBOW PART HAS 2 EA ADJACENT DENTS. CLOSING ACTION ON 04/14/03. ON N/R 00425. REMOVED AND REPLACED CDP AIR TUBE MANIFOLD AT 14TH STAGE IAW M/M 75-00-04-4. 2L73 4F4 F A22WE E23EA 20030505000122003050500012 2003 5 5 GTIA030136 420030307A256511331DGDME SLIDE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE CABIN INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23826NK 49391 L1 SLIDE PRESS IN RED BAND. REMOVED AND REPLACED L-1 SLIDE EVAC. 2L72 4F4 FRTA6WE E2EA 20030505000152003050500015NM 2003 5 5 SWAA030859 120030415A27316545166 ROD END BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB AFT ROD END ASSY PER MM. 2L72 4F RTA16WE 20030505000182003050500018EA 2003 5 5 COMA0360208 120030420A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS DEDESCENT 1 SO01973CA20274 7146 FLIGHT 5839 LANDING GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030505000202003050500020SO 2003 5 5 C2XA03TY050 120030416A2620270541 HANDLE EMB 135 EMB135LR 3260305SO EXTINGUISHER SHORTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27155273995 145413 TYS- DURING A SCHEDULED 1-C INSPECTION THE FIRE HANDLE NR 2 WOULD NOT LIGHT UP DURING THE FIRE DETECTION TEST. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FIRE SHUTOFF AND EXTINGUISHING HANDLE. OPS CHECK WAS GOOD. A/C WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030505000242003050500024WP 2003 5 5 MWEA030178 120030416A2731 PRESSURE SWITCH DOUG DC9 DC915 3022036WP ELEVATOR OUT OF ADJUST A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31300ME 45718 ELEVATOR POWER ON ANNUNCIATOR DOES NOT ILLUMINATE WITH M-FUNCTION. INSPECTED SWITCH & PERFORMED ADJUSTMENT TEST OF ELEVATOR POWER CONTROL PRESSURE SWITCH NO DEFECTS NOTED TEST GOOD. 2L72 4F A6WE 20030505000282003050500028NM 2003 5 5 2003UALA00289 120030316A3246 WHEEL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NLG VIBRATION A UALAO OTHER E VIBRATION/BUFFET TOTAKEOFF 1 WP29922UA 26642 AIRCRAFT LANDED AT A STATION UNDER AMBER ALERT DUE TO NOSE GEAR VIBRATION DETECTED DURING TAKEOFF. *S/D* REPLACED BOTH NOSE TIRES. PERFORMED VISUAL INSPECTION OF NOSE LANDING STRUT, NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E2GL 20030505000352003050500035CE 2003 5 5 GLBA2003044 120030405A2731503801253 CLUTCH BEECH 1900 1900D 1154162CE ELEVATOR TRIM STUCK A GLBAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM03211GL UE211 ELEVATOR TRIM STUCK. REMOVED AND REPLACED ELEVATOR ELECTRIC TRIM MAGNETIC CLUTCH AND CONNECTING CABLE PULLEYS, OPS CK GOOD. 2L72 4T RTA24CE 20030505000422003050500042NM 2003 5 5 SWAA030837 120030414A32106546113 PIN BOEING737 7373H4 1384600NM LT MLG TRUNION CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED SERVICE CHECK, FOUND LEFT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LEFT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030505000462003050500046EU 2003 5 5 G1F2003F00001 120030402A3210S25WS4037 TRUNNION BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP LT & RT MLG CORRODED B G1FRO OTHER O OTHER NRNOT REPORTED 1 GL13241RT7739 257057 CORRISION DETECTED ON LEFT AND RIGHT MAIN LANDING GEAR TRUNNIONS DURING THE MFG 125 SERIES 700 FLEX MAINT PROGRAM. INSPECTION CODE 570010 REQUIREMENTS. THIS INSPECTION IS CURRENTLY A DETAILED VISUAL INSPECTION AT FOUR YEAR INTERVALS. THE CORROSION RESULTED IN REMOVAL AND REPLACEMENT OF BOTH LEFT AND RIGHT TRUNNIONS. PN S25WS4037 AND S25WS4038 RESPECTIVELY. 2L72 4F4 F A3EU E6WE 20030505000492003050500049NM 2003 5 5 AWXA200300377 120030402A5210 CABLE BOEING757 757225 1384959NM PAX DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - EMERGENCY EVACUATION SYSTEM - DURING C-08 CHECK THE R-2 DOOR FAILED EMERGENCY POWER ACTUATION TEST FOR TRAVEL OF ACTUATION CABLE. MAINTENANCE ADJUSTED THE R-2 DOOR EMERGENCY POWER ACTUATION CABLE IAW BMM 52-11-32 PG 404 & 408, CABLE TRAVEL CHECKED GOOD IAW T/C F1C52608. 2L72 4F RTA2NM 20030505000632003050500063NM 2003 5 5 CALA0300209 120030406A5522 SKIN BOEING737 737524 1384721NM ELEVATOR PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2737615 27328 THE AIRCRAFT SUFFERED HAIL DAMAGE IN THE FORM OF A SMALL PUNCTURE TO THE LT ELEVATOR UPPER SKIN PANEL AT APPROXIMATELY ELEVATOR STATION 128.79. THE HOLE WAS APPROXIMATELY 17.5 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE CLEAN UP REQUIRED REMOVAL OF ALL PLIES AND CORE. THE SKIN WAS REPAIRED IAW ECRA 5520-01328. 2L72 4F RTA16WE 20030505000652003050500065NM 2003 5 5 CALA0300211 120030406A5522 SKIN BOEING737 737524 1384721NM ELEVATOR PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0937615 27328 AIRCRAFT SUFFERED HAIL DAMAGE TO THE RT ELEVATOR UPPER SKIN PANEL. THE HAIL IMPACT CAUSED A SMALL PUNCTURE AT APPROXIMATELY ELEVATOR STATION 129.4 AND 9.25 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE WAS THROUGH ALL PLIES AND TO THE CORE. THE SKIN WAS REPAIRED IAW ECRA 5520-01331. 2L72 4F RTA16WE 20030505000682003050500068NM 2003 5 5 03FDEA00219 120030303A5510ALC8104 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 17L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. SNRM N0676 - COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505000772003050500077NM 2003 5 5 03014 120030331A5210 STRUCTURE BOEING BOEING747 747132 1384882NM PAX DOOR DAMAGED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23709CK 000344 20247 ON THRU FLIGHT INSPECTION, FOUND L-2 DOOR FORWARD LOWER EDGE BELOW BOTTOM HINGE TO LOWER -R- STRAP PULLED LOOSE AND TORN. APPROX SIZE 10 INCH ON FRONT; BOTTOM BROKE LOOSE APPROX 6 INCH AFT; SHEET METAL IS TORN UPWARD APPROX 6 INCHES. 2L74 4F A20WE 20030502000042003050200004EA 2003 5 2 ASOA03119 120030319A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11845AS 7324 FLT 4414 - DURING A GROUND INSPECTION AT MGM, THE AFT EMERGENCY CEILING LIGHT NEXT TO THE LAVATORY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP NEXT OT THE LAVATORY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030502000092003050200009SO 2003 5 2 SIMA200309015 120030314A532014521725615 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR AFT SILL CORRODED. REMOVED SERVICE DOOR AFT SILL AND INSTALLED NEW SERVICEABLE SILL IAW EMB 135 SRM 51-40-02, 51-40-06, 51-40-04 AND 51-20-03. (M) 2L72 4F RTT00011AT 20030502000692003050200069WP 2003 5 2 ASAA0380181 120030301A532199366023 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO BAY FLOOR PANEL IS DELAMINATED, PUNCTURED, AND CORRODED ON TOP AND BOTTOM SIDES. REPLACED PANEL PER SRM 51-10-2, 10-3, AND 10-4. (M) 2L72 4F A6WE 20030502000702003050200070WP 2003 5 2 ASAA0380182 120030301A532199365859 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT FLOOR PANEL UPPER SURFACE IS WORN TO METAL. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030502000772003050200077NM 2003 5 2 ASAA0240023 120030124A5751654646047 BRACKET BOEING737 7374Q8 138447QNM RT WING AILERON CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01782AS 25113 PAE - DURING C-CHECK, FOUND CRACKED BRACKET RIGHT AILERON INBOARD BALANCE BAY OUTBOARD RIB FITTING AND WEB. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030502000902003050200090NM 2003 5 2 AWXA200300380 120030402A5210 CABLE BOEING757 757225 1384959NM PAX DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - EMERGENCY EVACUATION SYSTEM - DURING C-08 CHECK THE L-4 DOOR FAILED EMERGENCY POWER ACTUATION TEST FOR TRAVEL OF ACTUATION CABLE. MAINTENANCE ADJUSTED THE L-4 DOOR EMERGENCY POWER ACTUATION CABLE IAW BMM 52-11-32 PG 404 & 408, CABLE TRAVEL CHECKED GOOD IAW T/C F1C52609. 2L72 4F RTA2NM 20030502001232003050200123EA 2003 5 2 SWIA200311877 120030411A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA LT WING SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07435SW4373 4373 7555 SPOILERONS FAULT STATUS MESSAGE ILLUMINATED IN FLIGHT. REMOVED AND REPLACED THE LEFT WING SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. P/N OFF: 270007 S/N OFF: MAL 4704 S/N ON: MAL 5034. 2L72 4F RTA21EA 20030502001532003050200153WP 2003 5 2 GTIA030180 120030302A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 160 TO STA 200 LBL 44 FLOOR SUPPORT HAS GOUGED/ DAMAGED CORRODED. FABRICATED NEW FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030502001682003050200168EA 2003 5 2 COMA0360200 120030416A2420 GENERATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 INOPERATIVE A COMAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01721CA 7259 FLIGHT 5261 GENERATOR NR 2 OFF-LINE DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030502001952003050200195EA 2003 5 2 A6WA200340042 120030331A2420761341 GCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ADG FAILED A A6WAO OTHER L NO TEST NRNOT REPORTED 1 GL31405AW5970 7362 PERFORM ADG DEPLOYMENT TEST FLIGHT. ADG FAILED TO POWER AC ESS BUS TEST FLIGHT UNSATISFACTORY. REPLACED GCU, (S/N OFF: 0212, S/N ON: 0290). COMPLETED TEST FLIGHT REQUIREMENTS. NO DEFECTS NOTED. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF). 2L72 4F4 FRTA21EA E15NE 20030502002672003050200267NM 2003 5 2 03FDEA00438 120030414A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 EXTERIOR SKIN OIL CANNED BS 1139 BETWEEN STR 23 AND 24 RT. OIL CANNED EXTERIOR SKIN BS 1139 BETWEEN STR 23 AND 24 RH FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REMOVED DAMAGE IN AN AREA OF 3.6" X 4.4 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3. 2L73 4F RTA3WE 20030505000852003050500085NM 2003 5 5 372PA0023 120030416A3350363674 LAMP BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 FLOOR PATH LIGHTING LAMP IN AFT SECTION PARTIALLY INOP. REMOVED AND REPLACED EMERGENCY FLOOR PATH FLEX LAMP PER MM 33-51-81. OPS CHECK NORMAL. 2L72 4F RTA16NE 20030505001252003050500125NM 2003 5 5 03FDEA00212 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 8L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505001282003050500128NM 2003 5 5 03FDEA00486 120030417A5411 FRAME BOEING727 727200 138407ENM NR 1 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 1 ENGINE UPPER NACELLE SKIN HAS CRACK FORWARD OF PIN LATCH CUTOUT AREA. REMOVED, FABRICATED AND INSTALLED ANGLE IAW BOEING 727 SRM 51-30-2. 2L73 4F RTA3WE 20030505001352003050500135NM 2003 5 5 03FDEA00636 120030427A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 UPON REMOVAL OF RT NR 2 LEADING EDGE OUTBOARD MOST SEAL FOUND SLAT UPPER SKIN TRAILING EDGE AFT MOST HOLE CRACKED. RT WING NR 2 LEADING EDGE OUTBOARD SLAT UPPER SKIN TRAILING EDGE REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II AND DWG NRB6225. 2L73 4F RTA22WE 20030505001472003050500147NM 2003 5 5 03FDEA00490 120030417A3220 COVER BOEING727 727200 138407ENM NLG VAVLE DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NOSE LANDING GEAR METERING VALVE COVER HAS DELAMINATION ON UPPER SURFACE. REPAIRED NOSE LANDING METERING VALUE COVER IAW BOEING CMM 25-00-67. 2L73 4F RTA3WE 20030505001522003050500152NM 2003 5 5 03FDEA00496 120030417A5414 SKIN BOEING727 727200 138407ENM NR 2 NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 2 ENGINE RIGHT AFT NACELLE SKIN LOWER AFT CORNER BENT AND CHAFED. *S/D* REPAIRED BENT CORNER AND CHAFED EDGE IAW BOEING 727-200 SRM 54-10-03. 2L73 4F RTA3WE 20030505001552003050500155NM 2003 5 5 03FDEA00499 120030417A5710 STRUCTURE BOEING727 727200 138407ENM AILERON TAB TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT WING AILERON TRIM TAB INBOARD UPPER SURFACE DISBONDED AND TORN ON HONEYCOMB MATERIAL. 2L73 4F RTA3WE 20030505001632003050500163NM 2003 5 5 03FDEA00465 120030416A5414 SKIN BOEING727 727200 138407ENM NR 3 NACELLE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE UPPER NACELLE EXTERIOR SKIN GOUGED NEXT TO NR 1 LATCH. *S/D* REPAIRED NR 3 ENGINE NACELLE IAW BOEING 727-200 SRM 54-30-03. 2L73 4F RTA3WE 20030505001662003050500166SO 2003 5 5 C2XA03SH107 120030421A532014521725001 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 18 AND 21 WAS FOUND TO HAVE PITTING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030505001762003050500176NM 2003 5 5 DHL2003741547 120030320A5230 SKIN BOEING727 727200 138407ENM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, C1 DOOR SKIN HAS MANY DENTS ALL ARE MARKED. AREA FOUND TO BE OUT OF LIMITS IAW B-727 SRM 52-00-2. CUT OUT DAMAGED AREA OF SKIN DIM 59 X 14.75 INCHES AND FABBED NEW SKIN FROM 2024-T3 .071 PO 9912398 (59 X 14.75 INCHES) AND 8 EACH SPLICE PLATES FROM 2024-T3 .080 PO 9912380 DIM 9.5 X 5 INCHES, 7 X 5 INCHES, 9 X 5 INCHES 11 X 5 INCHES, 5 X 5.5 INCHES, 9 X 5 INCHES, 7 X 2.5 INCHES IAW SRM 52-20-3 FIG 2. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 52-00-1 FIG 2. 2L73 4F RTA3WE 20030505001772003050500177SO 2003 5 5 C2XA03SH112 120030421A531514522499003 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 SHV-DURING C-CHECK THE CENTER FLOORBEAM ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030505001812003050500181NM 2003 5 5 03FDEA00491 120030417A5320 WEB BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 AFT AIRSTAIR AREA AT STA 1223 RIGHT SIDE UPPER LIGHTENING HOLE IS CRACKED IN TAIL COMPARTMENT VERTICAL WEB. REPAIRED CRACK IN LIGHTENING HOLE WEB BY INSTALLING A DOUBLER PLATE IAW BOEING 727-200 SRM 53-10-02. 2L73 4F RTA3WE 20030505001862003050500186NM 2003 5 5 03FDEA00217 120030303A5510ALC8104 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 15L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505001982003050500198EA 2003 5 5 03108623 120030408A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 DURING MAINTENANCE INSPECTION, THE LT WING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505002032003050500203NM 2003 5 5 UPS03M40436 120030320A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT RBL 27.5 BETWEEN STA 791-840 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK RBL 27.5 STA 791-840 FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK & SPLICE REWORKED AS PER SRM 53-70-00 VOL I REV 32, HOLES PICK OUT AND PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK & SPLICE FITTING INSTALLED AS PER 53-70-00 VOL I REV 32 AT STA 791-840 RBL 27.5. 2L73 4F RTA22WE 20030505002122003050500212NM 2003 5 5 03FDEA00503 120030417A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FORWARD CARGO PIT RIGHT AFT BULKHEAD ANGLE HAS NUMEROUS AREAS OF CORROSION. *S/D* REPAIRED RT FWD CARGO PIT BULKHEAD ANGLE IAW B727-200 SRM 51-40-03. 2L73 4F RTA3WE 20030505002222003050500222NM 2003 5 5 03FDEA00551 120030421A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION WHILE WORKING CARD N00622 FOUND CORROSION ON STRINGER 26 RT BS 1166 TO BS 1148. 2L73 4F RTA3WE 20030505002252003050500225NM 2003 5 5 03FDEA00548 120030421A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION WHILE WORKING CARD N00303 FOUND CORROSION ON STRINGER RT BS 1090 AND BS 1110. 2L73 4F RTA3WE 20030505002292003050500229NM 2003 5 5 DHL2003741542 120030320A5330 SKIN BOEING727 727100 1384036NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS A DENT FWD BS STR 18R. REMOVED PAINT IN AFFECTED AREA IAW B-727 MM 51-20-01. DAMAGED AREA OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 1 X 1 INCH AND FABBED REPAIR DOUBLER THAT INCORPORATED NR 43432, 43434, 43435, FROM 2024-T3 .063" PO 9912495 DIM 62.5 X 16 IAW B-727 SRM 53-30-3 FIG 1, 53-30-2 FIG 2. DOUBLER WAS TREATED, PRIMED AND INSTALLED IAW B-727 SRM 51-10-2, 53-30-1 FIG 1, 53-30-2 FIG 2. 2L73 4F RTA3WE 20030505002402003050500240EU 2003 5 5 AWXA200300389 120030329A5315D53470940100 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM Y-512 ON FORWARD SIDE OF FR 66 TO FR 66 + 127MM. MAINTENANCE BLENDED OUT CORROSION ON UPPER SURFACE OF FLOORBEAM Y-512, FORWARD SIDE OF FR 66; PERFORMED 10 X VISUAL AND HFEC INSPECTION TO VERIFY NO CRACKS EXIST. TREATED DAMAGED AREA, PRIMED, APPLIED TOP COAT; REPAIR ACCOMPLISHED IAW AWA ER 26-5343-03104-SS1. 2L72 4F RTA28NM 20030505002432003050500243EA 2003 5 5 COMA0360201 120030415A3230462 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01973CA15160 7146 FLIGHT 5806 LANDING GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030505002632003050500263EA 2003 5 5 03108621 120030418A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 DURING MAINTENANCE INSPECTION, THE LT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505002642003050500264WP 2003 5 5 03FDEA00534 120030418A2750D425TB PULLEY DOUG DC10 DC1030 3023501WP RT WING BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 RT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. R/R PULLEY BRACKET & PULLEY. 2L73 4F A22WE 20030505002702003050500270EA 2003 5 5 03109639 120030419A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 DURING MAINTENANCE INSPECTION, THE NR 2 LT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505002722003050500272EU 2003 5 5 0303081 120030308A6123 CONTROL UNIT SAAB SF340 SF340A 7850100EU AUTOCOARSEN SHUTDOWN A UHLAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 GL1719XS 340A019 ON 03/08/03 AIRCRAFT N19XS ON FLT 4485 WAS ON APPROACH INTO TOL, WITHIN 5-10 SECONDS BEFORE TOUCHDOWN THE CREW EXPERIENCED AN UNCOMMANDED AUTOCOARSEN OF THE RT ENGINE. CREW CONTINUED LANDING THE AIRCRAFT. ONCE ON THE RUNWAY THE CREW SHUT DOWN THE RT ENGINE. 2L72 4T RTA52EU 20030506000012003050600001EU 2003 5 6 03FDEA00545 120030418A7722 INDICATOR AIRBUS310 A310 EU NR 1 EGT ECAM INOPERATIVE A FDEAB EMER. DESCENT O OTHER TOTAKEOFF 1 SO25420FE 339 ON ROTATION ECAM WARNING ACTIVATED AND NR 1 ENGINE EGT SPIKES TO OVER 900 DEG AND NR 1 ENG N2 SPIKES TO NEAR 119 PERCENT. RETURN FOR LANDING WITH NR 1 ENG AT IDLE. REMOVED AND REPLACED NR 1 EGT INDICATOR AND NR 1 N2 INDICATOR PER A310 MM 77-21-21-4 AND MM 77-12-21-4, AND PERF ENGINE IDLE AND HIGH POWER RUN PER A310 JRH, ALL PARAMETERS NORMAL. PROBLEM ON NR 1 EGT AND NR 1N2 INDICATION DUPLICATED ON GROUND. DURING MX ENG RUN PRIOR BOTH INDICATOR CHANGE. 2L72 4F RTA35EU 20030506000022003050600002EU 2003 5 6 139262 120030411A2613 SENSOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT TAILPIPE CONTAMINATED A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17108CQ 340A108 348 FLIGHT 4471 BED-TTN JUST AFTER TAKE-OFF, DURING CLIMB THE RT TAILPIPE HOT LIGHT ILLUMINATED. THE CREW REDUCED POWER 20-30 PERCENT AND THE LIGHT WENT OUT 2 MINUTES LATER. AFTER ABOUT A MINUTE WITH THE POWER STILL REDUCED, THE LIGHT CAME BACK ON FOR A FEW SECONDS THEN WENT BACK OUT. WEATHER CONDITIONS WERE HEAVY RAIN. THE A/C TURNED AROUND AND RETURNED TO BED. A/C TAKEN OUT OF SERVICE 4-11-03. 2L72 4T4 TRTA52EU E8NE6 20030506000052003050600005NM 2003 5 6 CALA0300219 120030425A53156546811 FLOORBEAM BOEING737 7373T0 1384582NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914320 23371 I-BEAM AT STATION 986.5 AFT GALLEY HAS CORROSION THROUGHOUT ENTIRE LENGTH MARKER (8 INCHES). REMOVED CORROSION, REPAIRED FLOORBEAM PER SRM 53-30-51. 2L72 4F RTA16WE 20030501001602003050100160NM 2003 5 1 ASAA0310062 120030301A532065596581 INTERCOSTAL BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AFT AIRSTAIR TORQUE BOX INTERCOSTAL AT BS 947-967, LT BUTTOCK LINE 51 CRACKED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20030501001892003050100189NM 2003 5 1 ASAA0310032 120030225A5320 PAD BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, STANSION PAD AT BS 685, RIGHT BUTTOCK LINE 51 CORRODED. REMOVED AND REPLACED STANSION PAD PER SRM. (M) 2L72 4F RTA16WE 20030502000052003050200005NM 2003 5 2 2003F00249 120030325A3297 CONNECTOR BOEING727 727222 1384073NM MLG INDICATOR DAMAGED A RYNAO OTHER N FALSE WARNING LDLANDING 1 CE077639U 19912 DURING LANDING AT WICHITA, THE NOSE LANDING GEAR SAFE LIGHT FAILED TO ILLUMINATE WHEN GEAR WAS EXTENDED. EMERGENCY CHECKLIST PROCEDURES WERE FOLLOWED WITH A CONFIRMED VISUAL DOWN INDICATION. AIRCRAFT LANDED AT ICT WITHOUT INCIDENT. SECURED LOOSE PIN AND RELAMPED LIGHT ASSEMBLY. OPERATIONAL CHECKED NORMAL. AIRCRAFT CONTINUED TO HOUSTON (IAH) AND THE LIGHT ASSEMBLY WAS REPLACED FOR PRECAUTION. (M) 2L73 4F A3WE 20030502000312003050200031SO 2003 5 2 SIMA200309003 120030307A532014522460013 BEAM EMB 135 EMB135LR 3260305SO CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145164 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED NEW CENTER BEAM GUSSET IAW EMB 135/145 SRM 51-40-02, 51-40-04, 51-40-06 AND CPM 51-21-04. (M) 2L72 4F RTT00011AT 20030502000622003050200062WP 2003 5 2 ASAA0380174 120030301A53219366007 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FLOOR PANEL IS CRACKED AT FS 731-786.5. REPLACED PANEL PER SRM 51-10-2, 10-3, AND 10-4. (M) 2L72 4F A6WE 20030502000742003050200074WP 2003 5 2 ASAA0380185 120030302A53215936591 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND MID CARGO BAY CENTER FLOOR PANEL ATTACH ANGLE IS CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-2 AND 30-2. (M) 2L72 4F A6WE 20030502000762003050200076WP 2003 5 2 ASAA0380188 120030302A57549937498501 SKIN DOUG DC9 DC982 3022082WP LT WING LE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND LEFT WING LEADING EDGE CRACKED JUST OUTBOARD OF VORTILON. INSTALLED SPLICE PER SRM 51-10-2, 10-4, 30-2 AND 30-5. (M0 2L72 4F A6WE 20030502000782003050200078NM 2003 5 2 ASAA0240022 120030124A5320654957315 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01782AS 25113 PAE DURING C-CHECK, FOUND LEFT AFT RAM AIR INLET PLENUM OUTBOARD ATTACH SKATE ANGLE IS CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030502000812003050200081WP 2003 5 2 ZW0A0304302 120030414A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13982TW 53632 THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 8 TO 10. RESEATED BATTERIES IN THE BATTERY PACK AT ROW 8. CHECK-C 11-19-02 STL. 2L72 4F RTA6WE 20030502000852003050200085NM 2003 5 2 AWXA200300372 120030403A5315 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM SUPPORT ANGLE BS 405, RBL 26-47. MAINTENANCE REMOVED DAMAGED FLOORBEAM SUPPORT ANGLE BS 405, RBL 26-47; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 3-4. 2L72 4F RTA2NM 20030502001072003050200107NM 2003 5 2 PCA0300838 120030411A5310 STRUCTURE BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 BS 1700 S13R - BS 1780 S13R CRACK. REPAIR PER SRM 53-10-04 FIG 88. TIME LIMIT REPAIR COI. 2L74 4F A20WE 20030502001102003050200110NM 2003 5 2 PCA0300841 120030410A5347 SEAT TRACK BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FWD CARGO AT BS 680 RBL 45.5 SEAT TRACK CRACK / TOP CHORD PUNCTURE. SEAT TRACK REPAIR SRM 53-10-05 FI 5 FLOOR STRUCTURE 51-40-03 FIG 1. 2L74 4F A20WE 20030502001122003050200112WP 2003 5 2 UPS03840428 120030415A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED SHIPS EMERGENCY LIGHT BATTERY PACK PER 33-50-01, OPS CKS NORMAL. 2L74 4F RT4A25 20030502001132003050200113 2003 5 2 371PA0020 420030412A2230 COMPUTER BOEING737 737306 13844BGNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO05371PA 23543 AUTO THROTTLE SWITCH WOULD NOT STAY ARMED DURING TAKEOFF ROLL. DURING CLIMB WITH AUTO THROTTLE ARMED, NR 1 N1=94.7, NR 2 N1= 91.5 AT FL290. PERFORMED AUTO THROTTLE BITE AND RANGE CHECK ON FMS. NO FAULTS NOTED. OK FOR SERVICE PER MM 22-30-01. 2L72 4F RTA16NE 20030502001142003050200114WP 2003 5 2 GTIA030141 120030312A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 CABIN FLOOR PANEL STA 826-864 DELAMINATED, BENT, PUNCTURED. FABRICATED NEW FLOOR. 2L72 4F4 FRTA6WE E2EA 20030502001182003050200118EA 2003 5 2 SWIA200311872 120030406A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07418SW 7446 RECEIVED FLAP FAIL CAUTION MESSAGE AT 11,000 FT. ON DOWNWIND, FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU UPON ARRIVAL AT GATE. NO FAILURES LISTED. PERFORMED VISUAL INSPECTION OF FLAPS AND BPSU RIG CHECK AND SYSTEM CHECKS IAW CL600 MM 27-51-00 & 27-51-05. ALL SYSTEMS PASS CHECKS. FLAP OPERATION AND INDICATION CHECK GOOD. 2L72 4F RTA21EA 20030502001202003050200120SO 2003 5 2 SWIA200311874 120030410A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07567SW 120342 WIRES PULLED OUT OF EMERGENCY EXIT LIGHTS ON LEFT ROW. REPLACED AFT MOST EMERGENCY FLOOR LIGHT ASSEMBLY. OPS CHECK GOOD. 2L72 4T RTA31SO 20030502001252003050200125EA 2003 5 2 SWIA200311879 120030414A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A SWIAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 NM07918SW3 3 7645 WITH BOTH ENGINES RUNNING AND NORMAL HYDRAULIC PRESSURE ON ALL 3 SYSTEMS, FLT SPLICER FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES ON ED2 (STATUS). RETURNED TO THE GATE. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD. 2L72 4F RTA21EA 20030502001262003050200126NM 2003 5 2 DHL2003741525 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, FUSELAGE SKIN HAS 2 DENTS FWD AND AFT BS 1148 ABOVE STR 19L. BLENDED AREA (PREVIOUS) 2 EACH FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA DIM 2.4 X 1.4 AND FAB REPAIR DOUBLER FROM MAT ID 2024-T3 .063 PO 9912380 DIM 11.5 X 8.75 AND FILLER FROM MAT ID 2024 T-3 .050 PO 9912380 DIM 2.4 X 1.4 IAW B-727 SRM 53-30-3 FIG 3. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. FAB AND INSTALLED REPAIR WASHERS IAW B-727 SRM 51-30-8 FIG 2. INSTALLED DOUBLER AND FILLER IAW B-727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20030502001372003050200137NM 2003 5 2 CALA0300197 120030406A5522 SKIN BOEING737 737524 1384721NM RT ELEVATOR PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715659 28920 THE RT ELEVATOR UPPER SKIN WAS DAMAGED DURING A HAIL STORM. THE DAMAGE CONSISTED OF ONE PUNCTURE AND 10 SMALL DENTS. THE SKIN WAS REPAIRED IAW ECRA 5520-01326. 2L72 4F RTA16WE 20030502001392003050200139GL 2003 5 2 C2XA03CL091 220030415A720023070401 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 LEAKING A C2XAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW27139558859 145075 CAE311169 STL FLIGHT 2462 CREW REPORTED NUMBER TWO ENGINE LOW OIL PRESSURE AND QUANTITY IN FLIGHT. IN FLIGHT COMMANDED SHUTDOWN OF NUMBER TWO ENGINE. CREW DIVERTED TO CLE. MAINTENANCE FOUND ENGINE TO BE LEAKING INTERNALLY. NUMBER 2 ENGINE WAS REMOVED AND REPLACED. GROUND RUNS AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20030430002432003043000243WP 2003 4 30 MWEA030169 120030414A57555910055501 SKIN DOUG DC9 DC915 3022036WP SPOILER DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 LEFT WING INBOARD FLIGHT SPOILER HAS DENT 2.375 X .059 INCH DEEP. CUT OUT DAMAGE, HOT BOND DOUBLER. 2L72 4F A6WE 20030501000192003050100019EA 2003 5 1 ASOA03116 120030318A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030501000372003050100037WP 2003 5 1 AALA20030268 120030214A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 TUL - FOUND SMALL AREA OF CORROSION LEFT CUSP STATION 545 EXTENDING FROM BELOW BRACKET. INSTALLED DOUBLER AT STATION 545 LEFT SIDE CUSP PER AARD 53-00-00-02. (M) 2L72 4F RTA6WE 20030501000612003050100061EU 2003 5 1 USAASA03022 120030307A2120EVT3454H FAN AIRBUS320 A320214 3930316EU AVIONICS BAY OVERHEATED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19124US 1314 BDL - FLT 1261 - EN ROUTE BOS-CLT, DURING FLIGHT, AN ODOR OF SMOKE BECAME PRESENT IN THE COCKPIT AND FORWARD GALLEY AREA. THE FLIGHT DIVERTED TO BDL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS EXTRACT FAN AND FILTER. OPS CHECKED OK. (M) 2L72 4F RTA28NM 20030501000802003050100080WP 2003 5 1 GTIA030227 120030313A5553 ANGLE DOUG DC9 DC983 3022083WP VERTICAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND DORSAL FIN AT BOTH LT AND RT SIDE CRACKED. REMOVED BOTH LT AND RT SIDE. LOCATED AND DRILLED ANGLE 5912188036. INSTALLED ANGLE P/N 5912158036. FABRICATED LOCATED AND DRILLED NEW 5910242-121. INSTALLED NEW 5910242-121. (M) 2L72 4F RTA6WE 20030501001052003050100105NM 2003 5 1 ASAA0310030 120030225A5320697878149 BRACKET BOEING737 737298C 1384490NM FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOND FRAME BRACKET AT BS 1040, LEFT BUTTOCK LINE 12 BROKEN. REMOVED AND REPLACED BRACKET PER SRM. (M) 2L72 4F RTA16WE 20030501001272003050100127NM 2003 5 1 ASAA0310074 120030303A54116573771 RIB BOEING737 737210C 1384459NM NR 2 NACELLE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL RIB AT NACELLE STATION 152.25, GOUGED. REMOVED DAMAGED AREA AND REPAIRED RIB PER SRM. (M) 2L72 4F A16WE 20030501001652003050100165NM 2003 5 1 ASAA0310080 120030304A5330 SKIN BOEING737 737298C 1384490NM FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND APU CUTOUT SKIN AT BS 1156, STRINGER 20R BENT. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20030501001732003050100173NM 2003 5 1 ASAA0310069 120030301A53306545775558 SKIN PANEL BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN PANEL AT BS 901-906, STRINGER 23R CRACKED TWO EACH. CUT OUT DAMAGED AND INSTALLED DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20030501001962003050100196NM 2003 5 1 ASAA0310056 120030301A53216545833524 FLOORBOARD BOEING737 737298C 1384490NM CABIN CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOORBOARD AT BS 255-270, BUTTOCK LINE 0 CRACKED AND CORRODED. REMOVED AND REPLACED FLOORBOARD PER SRM. (M) 2L72 4F RTA16WE 20030501001992003050100199NM 2003 5 1 ASAA310086 120030305A53206993075 RETAINER BOEING737 737298C 1384490NM FS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND L1 DOOR PRESSURE SEAL RETAINER AT BS 344, STRINGER 7L CRACKED. REMOVED AND REPLACED PRESSURE SEAL RETAINER PER SRM. (M) 2L72 4F RTA16WE 20030502000542003050200054WP 2003 5 2 ASAA0380166 120030228A53219936583 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND LEFT FLOOR PANEL SURFACE IS PUNCTURED AT FS 408. REPLACED FLOOR PANEL PER SRM 53-20-1, AND 53-05. (M) 2L72 4F A6WE 20030502000792003050200079WP 2003 5 2 ASAA0380186 120030302A53405928885516 FITTING DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, LEFT OVERHEAD STOWAGE BIN MOUNT FITTING IS BROKEN. REPLACED MOUNT FITTING PER MM 20-10-12 AND 30-01. (M) 2L72 4F A6WE 20030502000872003050200087NM 2003 5 2 P5CA0300854 120030412A5311 FRAME BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FRAME CRACK 1740 S13R. REPAIRED PER SRM 51-40-03. 2L74 4F A20WE 20030502001002003050200100NM 2003 5 2 03FDEA00472 120030417A5321 FLOOR PANEL BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 AFT CARGO PIT STA 1030 TO 1070 FORWARD CENTER FLOOR PANEL HAS SEVERAL GOUGES AND A PREVIOUS REPAIR. 2L73 4F RTA3WE 20030502001412003050200141 2003 5 2 SWAA030829 420030413A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 FWD SERVICE DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030502001522003050200152WP 2003 5 2 GTIA030145 120030221A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE INSERTS,STA200 CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO 160 LBL 44 TO 53 INCHES (9 X 40) FLOOR PNL SOFT/ MUSHY CORRODED INSERTS. FABBED NEW CABIN FLOORBOARD, STA 200-160 LBL 53. 2L72 4F4 FRTA6WE E2EA 20030502001572003050200157NM 2003 5 2 03FDEA00475 120030417A5414 SKIN BOEING727 727200 138407ENM NR 3 NACELLE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE LOWER COWLING EXTERIOR SKIN FORWARD MID AND AFT HAS 7 DENTS. 2L73 4F RTA3WE 20030502001592003050200159NM 2003 5 2 03FDEA00477 120030417A2612 WARNING LIGHT BOEING727 727200 138407ENM NR 1 ENG FIRE FALSE ACTIVATIONA FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25212FE 22934 DURING DESCENT INTO MEM, FIRE WARNING BELL CAME ON 3 TIMES. DURATION WAS 2-3 SECONDS, DURING THIRD INCIDENT NR 1 FIRE LIGHT ILLUMINATED BRIEFLY. LIGHT TESTED GOOD DURING TEST. REMOVED AND REPLACED ENGINE FIRE DETECTION CONTROLLER, PER MM 26-11-000-4, OPS CHECK GOOD, OK FOR SERVICE. 2L73 4F RTA3WE 20030502001612003050200161NM 2003 5 2 03FDEA00478 120030417A5411 FRAME BOEING727 727200 138407ENM NR 3 NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE UPPER COWLING NR 5 UPPER LATCH FRAME STIFFENER HAS CHAFING CONDITION. 2L73 4F RTA3WE 20030502001732003050200173NM 2003 5 2 03FDEA00462 120030416A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT FUSELAGE STA 277 FORWARD TOILET SERVICE PANEL SKIN HAS DEEP DENT. REPAIRED IAW FEDEX EA 5330-69463 2L73 4F RTA3WE 20030502001842003050200184EU 2003 5 2 AWXA200300410 120030327A5320D53911670200 ATTACH ANGLE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A .75 INCH CRACK WAS FOUND ON PARTITION FRAME IN AFT CARGO COMPARTMENT FORWARD BULKHEAD, UPPER LT CORNER. MAINTENANCE PERFORMED HFEC INSPECTION TO DETERMINE WHERE CRACK ENDS; STOP DRILLED CRACK; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 26-5314-00011-JS4. 2L72 4F RTA28NM 20030502001862003050200186EU 2003 5 2 AWXA200300412 120030328A5320D53471123 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK 2 AREAS OF CORROSION WERE FOUND ON LOWER SURFACE OF SHEAR WEB FR 69+331MM, FORWARD SIDE OF FR 70, RBL 1275. MAINTENANCE BLENDED OUT CORROSION LOWER SURFACE OF SHEAR WEB FR 69+331MM, FORWARD SIDE OF FR 70, RBL 1275; MATERIAL LOSS WITHIN LIMITS. PERFORMED HFEC TO VERIFY NO CRACKS EXIST. TREATED, PRIMED AND TOP COATED AREA. REPAIR ACCOMPLISHED PER AWA ER 26-5341-03097-TB2. 2L72 4F RTA28NM 20030502001922003050200192WP 2003 5 2 ZW0A0304401 120030415A2150 ACM DOUG DC9 DC983 3022083WP LEFT OVERSERVICED A ZW0AO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CE139403W 53139 DURING PREFLIGHT SMOKE IN CABIN DUE TO OVERSERVICE OF AIR CONDITIONING PRESSURIZATION LT ACM. REPLACED LT ACM PER MM 21-51-01 AND COMPLETED MD9-49-06. CHECK-C 9-11-02 STL. 2L72 4F RTA6WE 20030429002072003042900207EU 2003 4 29 03101316 120030411A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030429002162003042900216CE 2003 4 29 CWQ2003F00008 120030303A21206512072101 DUCT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA CRACKED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05308QS 5600277 DURING ROUTINE INSPECTION LOOKED INTO NACA DORSAL SCOOP AND FOUND THE LOWER AIR VANE PN 651207212 CRACKED .3750 INCH WITH THE CRACK STARTING FROM THE CENTER OF V CUT STRAIGHT AFT. GAINED ACCESS FROM TAIL BAGGAGE AREA AND REMOVED CRACKED VANE. REMOVED EA 9309 IAW MFG STANDARD PRACTICES, UPON REMOVAL NOTICED THAT THE V CUT APPEARS TO HAVE BEEN CUT WITH HAND SNIPS AND THERE WAS ON RELIEF HOLE AT BOTTOM OF CUT, ALSO THERE WAS VERY LITTLE EA 9309 SECURING INTO PLACE. INSTALLED NEW PART AND CLOSE UP AREA. WILL SEND BAD PART TO MFG FOR EVALUATION. (SCR 91284) (PTRS 7641) 2L72 4F4 FRTA22CE E25EA 20030429002232003042900223NM 2003 4 29 SWAA030807 120030409A5520BACB28AK04 BUSHING BOEING737 7373T0 1384582NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 AND NR 2 HINGE HARDWARE AND BUSHINGS PER MM. 2L72 4F RTA16WE 20030429002242003042900224 2003 4 29 SWAA030808 420030409A2565D31354 SLIDE BOEING737 7373T0 1384582NM FWD CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030430000112003043000011NM 2003 4 30 QXEA0300489 120030420A5230 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - CHAFE MARKS AROUND SUPPORT ROLLER BRACKET, FORWARD LOWER BRACKET ON AFT BAGGAGE DOOR. REPAIRED IAW DHC-8 400 SRM 51-14-00, PAGE 221 AND SRM 51-25-05. 2H72 4T RTA13NM 20030430000892003043000089SO 2003 4 30 SIMA200309011 120030311A532014525422007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO CARGO BAY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, RIGHT FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-20-03, 51-40-02, 51-40-06. (M) 2L72 4F RTT00011AT 20030430001262003043000126NM 2003 4 30 SWAA030923 120030423A2760654645268A HINGE FITTING BOEING737 737301 1384611NM LT WING SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED A2 CHECK, FOUND BROKEN HINGE FITTING ON NR 4 GROUND SPOILER UPPER SIDE. R&R NR 4 GROUND SPOILER & OTBD ACTUATOR PER MM. 2L72 4F RTA16WE 20030430001462003043000146NM 2003 4 30 SWAA030889 120030421A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 500C & BS 500D, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20030430001912003043000191NM 2003 4 30 SWAA030935 120030427A3110M564 MODULE BOEING737 7373H4 1384600NM INSTRUMENT PANELFAULTY A SWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW29640SW 27713 DECLARED EMERGENCY. NUMEROUS CAUTION WARNING LIGHTS INOP IN COCKPIT. REMOVED AND REPLACED M564 MASTER DIM MODULE PER MM. 2L72 4F RTA16WE 20030429002322003042900232SW 2003 4 29 20035 120030411A7603 LOCK SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP CONDITION LEVER WORN E STZAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL03505FS AC591B AFTER TAKEOFF AT APPROXIMATELY 600 FEET AGL, PILOT REPORTED THAT BOTH LEFT AND RIGHT FUEL BY-PASS ANNUNCIATORS ILLUMINATED, ACOMPANIED WITH PRONOUNCED ENGINE SURGING. AIRCRAFT RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. MAINTENANCE LATER DETERMINED THAT THE CONDITION LEVER FRICTION LOCKS HAD NOT BEEN APPLIED, ALLOWING THE CONDITION LEVERS TO CREEP BACK TOWARD THE LOW RPM STOP. 2L72 4T4 TRTA8SW E4WE 20030430000152003043000015SO 2003 4 30 LR7A03042 120030426A5350339336L LONGERON LKHEED382 382G 526414USO LT MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 658 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WW POD WL 200 LONGERON CRACKED AT FS 477, LBL 80. REPLACED LONGERON IAW SRM SMP 583 51-70. NR 0015, 02/REP/61 AND 02/REP/62. 2H74 4T A1SO 20030430000772003043000077NM 2003 4 30 MEX2003099 120030328A3230392492 VALVE DOUG MD80 MD83 3023681NM MLG FAILED A ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23831LF 53050 MEX-GDL - DURING TRANSIT, DETECTED HYDRAULIC LEAK FROM LT MLG IN ANTI-SKID SYSTEM DUAL VALVE. VALVE WAS REPLACED IAW MM 32-43-03 AND HYDRAULIC SYSTEM WAS REFILLED, TESTS CORRECT. (M) 2L72 4F RT 20030430000992003043000099NM 2003 4 30 USAA030034 120030312A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 CLT - FOUND FRAME CRACKED .5 INCH, BS 1380 AFT CARGO DOOR CUTOUT FRAME WEB CRACKED, BELOW NR 6 DOOR STOP. INSTALLED WEB SPLICE REPAIR PER EA 87119. (M) 2L72 4F RTA2NM 20030430001472003043000147NM 2003 4 30 SWAA030888 120030421A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 872, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430001642003043000164NM 2003 4 30 SWAA030870 120030417A32106546113 TRUNNION BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030430002682003043000268NM 2003 4 30 VNAA0304006 120030411A2731 RELAY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ELEVATOR TRIM FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07429JS 3043 DURING CLIMBOUT, THE CREW NOTICED THAT THE ELEVATOR TRIM STOPPED WORKING. AFTER CONFERRING WITH MAINTENANCE CONTROL, FLIGHT 4156 RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE 49CC RELAY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030501001092003050100109NM 2003 5 1 ASAA0390001 120030219A5610 ROLLER BOEING737 737990 NM COCKPIT WINDOW LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01305AS 0305 30013 SEA - DURING LINE MAINTENANCE, THE CAPTAINS SLIDING WINDOW HARD TO CLOSE. TIGHTENED AFT ROLLER. SLIDING WINDOW OPERATES NORMALLY. (M) 2L74 4F RTA16WE 20030501001112003050100111WP 2003 5 1 ASAA0380114 120030129A53305936667501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OAK - DURING C-CHECK, FUSELAGE SKIN IS CREASED & DENTED AT FS 1183 AT 6 O'CLOCK POSITION. INSTALLED DOUBLER PRE SRM 51-10-3 AND 51-103B. (M) 2L72 4F RTA6WE 20030501001312003050100131NM 2003 5 1 ASAA0310047 120030226A53106545813501 DOOR FRAME BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND R1 DOOR FRAME AT BS 328, STRINGER 11R-12R CRACKED. STOP DRILLED CRACKS IN DOOR FRAME PER SRM. (M) 2L72 4F RTA16WE 20030501001342003050100134WP 2003 5 1 ASAA0380115 120030131A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01976AS 53452 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING REMAINED ON WITH BATTERY SWITCH OFF. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030430002092003043000209NM 2003 4 30 VNAA0304018 120030418A24201180001 GCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT GENERATOR FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07429JS20713 3043 DURING CLIMBOUT, THE CREW RECEIVED A RIGHT HAND AC VOLT FAIL INDICATION AND RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002492003043000249NM 2003 4 30 SWAA030810 120030413A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030430002502003043000250NM 2003 4 30 SWAA030811 120030413A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030430002542003043000254NM 2003 4 30 SWAA030815 120030412A3350604222 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT ENTRY & AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20030501000092003050100009WP 2003 5 1 AALA20030272 120030214A5347 GALLEY TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 TUL - FOUND CORROSION ON FORWARD GALLEY TIE DOWN FITTING. REPLACED WITH NEW TIE DOWN FITTING PER SRM 51-01. (M) 2L72 4F RTA6WE 20030501000172003050100017SO 2003 5 1 SIMA200302201 120030116A531514525381003 FLOORBEAM EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21653AE 145433 ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE CENTER FLOORBEAM AT FRAME 20. REMOVED CORRODED AREA BY CUTOUT. FABRICATED AN EXTERNAL U-SHAPED DOUBLER. REPAIR DONE IAW EMB-145 SRM (145/1142, REV 20) 53-21-10 PARA 5 FIG 204 SHEET 2, AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030501000212003050100021WP 2003 5 1 AALA20030278 120030304A5320 FITTING DOUG DC9 DC982 3022082WP FLAP ACTUATOR CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21203AA 49145 TUL - FOUND .25 INCH CRACK AT INBOARD FLAP ACTUATOR FORWARD ATTACH FITTING CRACK IS AT EDGE OF CUTOUT WHERE HYDRAULIC LINES PASS THROUGH. REPAIRED CRACK ON FITTING PER ESO80559 DATED 03-03-03. (M) 2L72 4F A6WE 20030501000632003050100063WP 2003 5 1 GTIA030205 120030228A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - L1 DOOR UPPER FRAME FORWARD OUTER RADIUS CRACKED. STOP DRILLED CRACK. (M) 2L72 4F RTA6WE 20030501000732003050100073WP 2003 5 1 GTIA030213 120030217A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND MID PIT LONGEORN 28R AT STATION 598 CORRODED. REMOVED LONGERON 28R STATION 588 TO 630. FABRICATED NEW LONGERON 28 SECTION. INSTALLED LONGERON SECTION. (M) 2L72 4F RTA6WE 20030501000742003050100074WP 2003 5 1 GTIA030214 120030220A5320 FLANGE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND AFT PIT CORRODED BEAM FLANGE AT FS 1145-1155 7 INCHES RBL. FORMED NEW STRAP REPAIR IAW EA 5310-0304. INSTALLED STRAP REPAIR. (M) 2L72 4F RTA6WE 20030506000082003050600008NM 2003 5 6 CALA0300221 120030427A575465507579 RIB BOEING737 7373T0 1384582NM LE FLAP GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977303 23354 LEFT WING NUMBER TWO MID FLAP GOUGED AT MID SPAR CENTER FORE FLAP TRACK GUIDE. REPLACED RIB AT MID FLAP SPAR CENTER FORE FLAP TRACK GUIDE NUMBER TWO MID FLAP PER SRM 51-10-02. 2L72 4F RTA16WE 20030502001962003050200196NM 2003 5 2 03FDEA00513 120030418A5320 PANEL BOEING727 727200 138407ENM CARGO BAY TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CABIN 2 EA GILLINER PANELS TORN AT LEFT SIDE STA 1160. *S/D* FABRICATED GILLINER IAW FED EX SRZ 25-005C. 2L73 4F RTA3WE 20030502002272003050200227NM 2003 5 2 EIA2003065 120030417A5730 SKIN BOEING747 747273C 1384896NM RT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 RIGHT UPPER WING UPPER SURFACE OF LOWER SKIN HAS HEAVY CORROSION AT FWD SPAR LOWER CHORD AT WS 1323. REMOVED DAMAGE, INSPECTED AND NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 471-57-217-2 REV-A. 2L74 4F A20WE 20030505000192003050500019WP 2003 5 5 DHL2003805007 120030423A2611 FIRE DETECTOR DOUG DC8 DC873F 302199FWP CARGO BAY WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01805DH 46125 NR 7 MAIN DECK CARGO COMPARTMENT FIRE DETECTOR DOES NOT TEST. DEFERRED NR 7 FIRE DETECTOR AS PER MEL 26-6-1 ASSIGNED DMI 12660 PLACARD PANEL. REF DMI 12660, NR 7 MAIN DECK CARGO COMPARTMENT FIRE DETECTOR DOES NOT TEST. OPS CHECKED NR 7 SMOKE DETECTOR PER DACO 26-10-. NO DEFECTS NOTED. THIS CLEARS DMI 12660 PLACARD REMOVED. 2L74 4F RT4A25 20030505000272003050500027EU 2003 5 5 0300813224 120030313A5315 FLOORBEAM AIRBUS320 A320211 3930320EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01324US 273 DURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT BEAM AT FRAME 20 LBL 30. REPAIRED PER EA 32-193626. 2L72 4F RTA28NM 20030505000322003050500032NM 2003 5 5 2003UALA00373 120030410A5320 THRESHOLD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 AFT PIT DOOR THRESHOLD WEB BS 749 TO 847 HAS LEVEL 1 CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED THE WEB. 2L72 4F4 FRTA16WE E2GL 20030505000692003050500069NM 2003 5 5 DHL2003741552 120030322A5280 WEB BOEING737 737200A 1384416NM MLG DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, LT MLG W/W STA 950 LOWER AFT MLG DOOR STOP AT LATCH POINT, WEB IS CRACKED. REMOVED NR 1 & 2 HYD SYS B-PUMPS. DISCONNECTED 3 HYD LINES LT MLG W/W STA 950 FOR ACCESS. REMOVED FUEL DRAIN STA 950, AFT CLOSE OUT W/W PANEL, HYD PUMP BRACKETS FOR ACCESS & DRAIN MAST. CUT OUT DAMAGED AREA DIM 1.5 X 3 INCH, FABBED 1 FILLER DIM 1.5 X 3 INCH & 1 DOUBLER DIM 5 X 10 INCH. ALODINED & PRIMED PARTS. INSTALLED WEB REPAIR. FABRICATED 2 ANGLES DIM 1 X 1 X 3 INCH FOR FWD SIDE TOP BRACKETS. ALODINED & PRIMED ANGLES. FABRICATED 1 T-ANGLE DIM 2 X 53 INCH. ALODINED, PRIMED T-ANGLE AND INSTALLED. INSTALLED NR 1 & 2 HYD SYS B-PUMPS, 3 HYD LINES LT MLG W/W STA 950 & FUEL DRAIN STA 950. 2L72 4F RTA16WE 20030505001712003050500171NM 2003 5 5 SWAA030843 120030414A53106935365 SHEAR TIE BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L & STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030505001852003050500185NM 2003 5 5 03FDEA00215 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 11L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505002322003050500232WP 2003 5 5 UPS03840448 120030413A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED AT STA 1766 RBL 35 AT APPROX 66 INCHES ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER IAW SRM 53-2-5 FIG 14A, FOUND TO BE WITHIN RANGE LIMITS OF PREVIOUSLY INSTALLED REPAIR IAW SRM 53-2-5 FIG 14A. 2L74 4F RT4A25 20030505002512003050500251NM 2003 5 5 CALA0300204 120030419A5347 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717306 23357 INSPECTION FOUND A 4 INCH CRACK IN RT TIE DOWN RAIL AT STA 492. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030505002572003050500257NM 2003 5 5 03FDEA00541 120030418A2780 PANEL BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT WING LEADING EDGE ACCESS PANEL AT INBOARD STOP NR 7 SLAT HAS APPROXIMATELY .375 INCH CRACK AT UPPER CORNER OF CUTOUT FOR STOP. INSTALLED DOUBLER REPAIR IAW BOEING 727-200 SRM 57-50-3. 2L73 4F RTA3WE 20030506000072003050600007EA 2003 5 6 03111656 120030421A2560601R464015 ESCAPE ROPE CNDAIRCL600 CL6002B19 1900309EA COCKPIT MISSING A VTZAK NONE O OTHER ININSP/MAINT 1 EA27656BR 7485 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE HOOK FOR THE EMERGENCY ESCAPE ROPE WAS MISSING. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY ESCAPE ROPE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030506000092003050600009NM 2003 5 6 CALA0300222 120030426A53476940352 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977303 23354 SEAT TRACK CORRODED STATION 277 - 294 AT RBL 42. REMOVED AND REPLACED DAMGED SEAT TRACK PER SRM 51-40-02. 2L72 4F RTA16WE 20030506000152003050600015NM 2003 5 6 DHL2003741548 120030401A5340 FITTING BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, BS 1050 STR 27R END FITTING CORRODED. REMOVED FITTING BS 1050 STR 26R FOR REPAIR. REMOVED FASTENERS FOR ACCESS ON STR 27R KEEL BEAM EXTENSION ANGLE. UPON REMOVAL OF STR FITTING FOUND KEELBEAM T-ANGLE CORRODED AND CRACKED. REMOVED PREVIOUS KEEL BEAM ANGLE SPLICE AT BS 1010 AND REMOVED T-ANGLE FOR REPAIR. CUT OUT FRAME SECTION AT BS 1030 FOR T-ANGLE PANEL DIM 4 X 4 INCHES. FABBED NEW T-ANGLE USING 65-56135-30 PO 3077170 AND INSTALLED NEW PIECE. FAB FRAME REPAIR USING 7075-T6 .071 PO 9912182 IAW SRM 51-40-3 FIG 3. ALODINED AND PRIMED ALL REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED FRAME REPAIR T-ANGLE SPLICE AND NEW END FITTING P/N 65-56185-1, PO 3077192 IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030506000172003050600017EA 2003 5 6 COMA0360196 120030417A2613355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA RT UNRELIABLE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01467CA 7637 FLIGHT 5914 RT 14TH STAGE DUCT OVERHEAT WARNING. REPLACED THE PYLON LEAK SENSIGN ELEMENT. 2L72 4F RTA21EA 20030506000302003050600030EA 2003 5 6 SWIA200311881 120030414A2750 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07924SW 7681 FLAP FAIL MESSAGE IN FLIGHT. PERFORMED A NO FLAP LANDING. PULLED AND RESET FLAP CIRCUIT BREAKERS. OPS CHECK OF FLAPS GOOD. UPDATE 3/18/2003: FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WHEN SELECTING FLAPS 8 DEGREES, FLAPS FAILED AT 0 DEGREES. FLAPS FAILED MESSAGE CLEARED AND OPERATIONAL CHECK GOOD. FECU TESTED AND ALL LINE REPLACEABLE UNITS TESTED PASSED. 2L72 4F4 FRTA21EA E15NE 20030506000342003050600034NM 2003 5 6 CALA0300231 120030430A52306547953 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CANNING A CALAK NONE O OTHER ININSP/MAINT 1 SW0977303 23354 C2 DOOR SKIN OIL CANNING APPROXIMATELY 32 INCHES FROM TOP OF DOOR AND 7 INCHES FROM FORWARD EDGE. FABRICATED AND INSTALLED REPAIR PER SRM 52-00-01. 2L72 4F RTA16WE 20030506000372003050600037EU 2003 5 6 03FDEA00657 120030430A5753A5797065000151 VANE AIRBUS310 A310 EU ZONE 600 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE32906 281 RT INBOARD FLAP VANE TOP SURFACE 6 INCHES INBOARD FROM OUTBOARD HOIST POINT IS AN AREA GOUGED AND WORN 2 X 2.5 X .012 INCH (BEEN CHAFING ON NR 2 SPOILER ACTUATOR DRIP PAN). BLENDED OUT DAMAGE IAW SRM 51-73-10. NDT BLENDOUT IAW NTM 51-10-08. FILLED REWORK AREA WITH EA 934 A&B IAW EA 6-5750-69671. FABRICATED AND INSTALLED BONDED STEEL DOUBLER PER SRM 57-52-12 FIG 202 AND FAX 942-023683/005/2003 AND EA 6-5750-69671. 2L72 4F RTA35EU 20030506000532003050600053WP 2003 5 6 UPS03840457 120030411A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, FWD ACCESSORY COMPARMENT AT STA 55 & L24L FRAME IS CRACKED. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51-1-21. HEAT TREATED FRAME SECTION AND SPLICES IAW TPS-1003 REV A. FABBED AND LOCATED FRAME SECTION AND SPLICES IAW DC8 SRM 53-2-24. ALODINED AND PRIMED ALL REPAIR PARTS IAW DC8 SRM 51-1-8 AND INSTALLED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030506000582003050600058EA 2003 5 6 COMA0360199 120030416A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01933CA 7040 FLIGHT 5276 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030506000712003050600071NM 2003 5 6 03FDEA00572 120030422A5720 BRACKET BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT WING TIP UPPER SUPPORT BRACKET FOR NAVIGATION LIGHT LENS HAS 1.5 INCH CRACK IN RADIUS OF BRACKET. FABRICATED AND INSTALLED BRACKET IAW BOEING 727 SRM 51-20-1 AND 51-30-2. 2L73 4F RTA3WE 20030506000832003050600083NM 2003 5 6 03FDEA00580 120030423A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FLOORBEAM UPPER FLANGE BS 620, RBL 25 TO LBL 45, WL 208. CORROSION ON FLOORBEAM UPPER FLANGE BS 620, RBL 25. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AND REPAIR FLOORBEAM UPPER FLANGE AT BS 620, RBL 25 IAW SRM 53- 10-8. 2L73 4F RTA3WE 20030506000952003050600095NM 2003 5 6 CALA0300216 120030424A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977303 23354 INSPECTION FOUND A HOLE MEASURING APPROXIMATELY 4 INCHES X 5 INCHES IN FUSELAGE SKIN BETWEEN STA 986.5 AND 1006 BETWEEN S3L AND S4L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210. 2L72 4F RTA16WE 20030506001122003050600112NM 2003 5 6 DHL2003755006 120030425A5754 STRUCTURE BOEING727 727225 1384077NM NR 5 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 RT WING L/E STA 464 APPROX HAS APPROX 5 INCH CRACK ABOVE NR 5 SLAT. CLEANED AREA OF PAINT AT STA 444 AND 454. PERFORMED DYE PENETRANT OF SUSPECTED AREAS AND CONFIRMED SKIN CRACKS AT STA 444 & 454. CUT OUT AREA SIZE 3 X 4 INCH ON STA 444 LT WING L/E AND CUT OUT 3 X 5 INCH STA 454 IAW B727 SRM 57-30-4 FIG 4. FABRICATED FILLERS FROM 2024-T3 1040 SIZE 3 X 4 INCH AND 3 X 5 INCH PO 9912571 AND DOUBLERS FROM 2024-T3 .505 SIZE 3 X 7 INCH AND 4 X 7 INCH AND 3 X 9 INCH AND 4 X 9 INCH PO 9912495 IAW B727 SRM 57-30-4 FIG 4. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIRS AT STA 444 AND 454 IAW B727 SRM 57-30-4 FIG 4. 2L73 4F A3WE 20030506001182003050600118NM 2003 5 6 CALA0300224 120030425A53476546815120 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAO OTHER O OTHER NRNOT REPORTED 1 SW0977303 23354 RIGHT OUTBOARD SEAT TRACK HAS CORROSION AT AFT END STATION 927. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-2. 2L72 4F RTA16WE 20030505001402003050500140NM 2003 5 5 03FDEA00631 120030428A5312 BULKHEAD BOEING727 727200 138407ENM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT MLG WHEEL WELL STATION 870 BULKHEAD IS CRACKED AT LBL 42 APPROXIMATELY W/L 185.5 AND BELOW HORIZONTAL CHORD REPAIRED IN ACCORDANCE WITH FEDEX EA 7-5310- 69465. 2L73 4F RTA3WE 20030505002042003050500204NM 2003 5 5 03FDEA00511 120030418A5720 INTERCOSTAL BOEING727 727200 138407ENM LT WING BENT A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25218FE 21101 INTERCOSTAL BENT ON LEFT WING LOWER SURFACE AT ATTACH POINT FOR WING ACCESS PANEL 12 INCHES INBOARD OF MAIN LANDING GEAR FORWARD TRUNNION. 2L73 4F RTA3WE 20030505002072003050500207NM 2003 5 5 03FDEA00508 120030417A5321 FLOOR PANEL BOEING727 727200 138407ENM CABIN MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FORWARD AUXILARY FUEL TANK FLOOR ACCESS PANEL AT STA 720E RIGHT SIDE HAS AREAS OF FILLING COMPOUND MISSING ON 3 OF 4 EDGES. *S/D* REPAIRED FLOORBOARD ACCESS PANEL IAW FED EX SRZ 25-005C. 2L73 4F RTA3WE 20030505002082003050500208NM 2003 5 5 03FDEA00507 120030417A5321 FLOOR PANEL BOEING727 727200 138407ENM CABIN DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 AFT CARGO PIT FLOOR PANEL STA 960E TO 990 HAS GILLINER PATCH WITH HOLE PUNCTURED THROUGH. *S/D* REPAIRED FLOOR PANEL IAW BOEING SRM 727-200 53-10-07. 2L73 4F RTA3WE 20030506000062003050600006NM 2003 5 6 CALA0300220 120030426A534765E80736156 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977303 23354 AFT CARGO RIGHT TIE DOWN RAIL CORRODED IN NUMEROUS PLACES BETWEEN STATIONS 727 AND 787 UPPER SURFACE. REMOVED AND REPLACED WITH NEW TRACK PER 53-60-53 AND INSTALLED SPLICE AND FASTENERS PER SRM 53-00-53. 2L72 4F RTA16WE 20030506000392003050600039 2003 5 6 03FDEA00655 420030430A34426225132120 TRANSCEIVER BOEING727 727200 138407ENM ZONE 100 FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO25482FE 21464 WEATHER RADAR INDICATOR DISPLAYS A FAIL MESSAGE IN WX, MAP & TEST MODES. REMOVED AND REPLACED RADAR TRANSCEIVER PART 622-1532-101, S/N 4416 (ON) PART 622-5132-120, S/N 4511(OFF), OP'S CHECK GOOD IAW M/M 34-41-041-4. 2L73 4F RTA3WE 20030506000472003050600047WP 2003 5 6 UPS03840451 120030412A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, REMOVE L2 UPPER AFT CORNER STEEL DOUBLER PER EO DC8-5330-12073-H STA 1660 LONG 10L. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED DOUBLER AND TRIPLER, REINSTALLED FILLER AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 17. 2L74 4F RT4A25 20030506000992003050600099NM 2003 5 6 03FDEA00641 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND CORRODED. 2L73 4F RTA22WE 20030506001392003050600139WP 2003 5 6 GTIA030190 120030223A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 180 RBL 9 INCH TO 42 INCH SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030506001412003050600141WP 2003 5 6 GTIA030169 120030223A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE SUB FLOOR CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 168.7 RBL ( CORRODED AT DOUBLER ( BELOW THERMAL BARRIER) FABRICATED NEW SUB FLOOR WEB. REMOVED SUB FLOOR WEB DOUBLER. FABRICATED NEW WEB DOUBLER. FABRICATED SPLICE DOUBLER. INSTALLED SPLICE ON WEB STA. INSTALLED SUB FLOOR. INSTALLED SUB FLOOR WEB DOUBLER. 2L72 4F4 FRTA6WE E2EA 20030506001662003050600166WP 2003 5 6 ASAA0380224 120030307A575459304942 VANE DOUG DC9 DC982 3022082WP LE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT FLAP VANE DENTED ON LEADING EDGE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM. (M) 2L72 4F A6WE 20030506001762003050600176WP 2003 5 6 ASAA0380244 120030307A531357242886 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND LONGERON 28L IS CORRODED AT FLANGE OF REPAIR SPLICE. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM. (M) 2L72 4F A6WE 20030506001872003050600187WP 2003 5 6 ASAA0380193 120030302A57555930976501 SKIN DOUG DC9 DC982 3022082WP SPOILER DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT WING GROUND SPOILER IS DISBONDED. REMOVED DAMAGED AREA AND REBONDED WITH FIBERGLASS PER SRM 51-70-1B. (M) 2L72 4F A6WE 20030506002032003050600203NM 2003 5 6 ASAA0310018 120030216A52206396002 PLATE BOEING737 737298C 1384490NM EMERGENCY EXIT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT DOOR STOP PLATE AT BS 616, STRINGER 14R CRACKED. REMOVED AND REPLACED STOP PLATE PER SRM. (M) 2L72 4F RTA16WE 20030506002132003050600213WP 2003 5 6 ASAA0380240 120030307A532059360262 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO AREA INTERCOSTAL IS CRACKED. REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F A6WE 20030506002172003050600217WP 2003 5 6 ASAA0380196 120030303A5310993061291 BRACKET DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT SERVICE (L-2) DOOR EMERGENCY SLIDE AFT GIRT BAR FLOOR BRACKET IS CORRODED. REPLACED BRACKET PER SRM 53-01. (M) 2L72 4F A6WE 20030506002192003050600219WP 2003 5 6 ASAA0380202 120030304A5320993053425 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CENTER FLOOR SUPPORT CORRODED AT FS 200. REPLACED SUPPORT PER SRM 53-01. (M) 2L72 4F A6WE 20030506002372003050600237WP 2003 5 6 ASAA0380264 120030314A56105613217519 WINDOW DOUG DC9 DC983 3022083WP COCKPIT JAMMED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OAK - DURING PREFLIGHT CHECK, FOUND CAPTAINS CLEARVIEW WINDOW JAMMED IN CLOSED POSITION. ADJUSTED WINDOW PER MM 56-10-03. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030506002392003050600239WP 2003 5 6 ASAA0380258 120030309A53159936534165 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OAK - DUIRNG C-CHECK, FOUND FLOORBEAM CORRODED ON OUTBOARD OF PANEL F-6, FS 160-196. REPLACED SUPPORT BEAM PER SRM 51-10-4 AND 51-30-2. (M) 2L72 4F RTA6WE 20030506002452003050600245WP 2003 5 6 ASAA0380261 120030309A5320991015193 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OAK - FOUND DURING C-CHECK, LEFT PASSENGER FLOOR WEB MEMBRANE CORRODED BETWEEN FS 826-845. INSTALLED DOUBLER PER SRM 51-10-3 AND 53-01. (M) 2L72 4F RTA6WE 20030501000812003050100081WP 2003 5 1 GTIA030228 120030312A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND PASSENGER CABIN RIGHT SIDE STAITON 541 TO STATION 617 FLOOR PANEL CRACKED/DAMAGED AT CORNER/INSERTS BROKEN OUT. REPAIRED FLOOBOARD. (M) 2L72 4F RTA6WE 20030501000882003050100088WP 2003 5 1 GTIA030211 120030218A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CARGO DOOR LOWER AFT SKIN WORN. FABRICATED, LOCATED AND DRILLED ONE DOUBLER. INSTALLED DOUBLER EDGE REPAIR. (M) 2L72 4F RTA6WE 20030501001412003050100141NM 2003 5 1 ASAA0310083 120030304A5320654585545 WEB BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOOR WEB AT BS 950-993, RIGHT BUTTOCK LINE 55 CORRODED. REMOVED AND REPLACED FLOOR WEB PER SRM. (M) 2L72 4F A16WE 20030501001532003050100153WP 2003 5 1 ASAA0380125 120030209A5320 DRAIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OAK - DURING C-CHECK, FOUND CORROSION AROUND MID CARGO BAY BELLY DRAIN. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04, 51-30-2, AND 51-30-5. (M) 2L72 4F RTA6WE 20030501001592003050100159NM 2003 5 1 ASAA0310092 120030305A53206549815265 SUPPORT ANGLE BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SUPPORT ANGLE AT BS 244-264, RIGHT BUTTOCK LINE 11, RIGHT BUTTOCK LINE 30 CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20030501001662003050100166NM 2003 5 1 ASAA0310079 120030304A5320BAC150524624 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND T-ANGLE AT BS 847, STRINGER 19R CORRODED. REMOVED AND REPLACED T-ANGLE PER SRM. (M) 2L72 4F RTA16WE 20030501001692003050100169NM 2003 5 1 ASAA0310076 120030304A53106935352U14 SHEAR TIE BOEING737 737298C 1384490NM FS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SHEAR TIE CLIP AT BS 827, STRINGER 13L CRACKED. REMOVED AND REPLACED SHEAR TIE CLP PER SRM. (M) 2L72 4F RTA16WE 20030501001792003050100179NM 2003 5 1 ASAA0310061 120030301A5320BAC1506626 STIFFENER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND APU AIR INLET CUTOUT STIFFENER AT BS 1104-1156, STRINGER 17R CORRODED. REMOVED AND REPLACED STIFFENER PER SRM. (M) 2L72 4F RTA16WE 20030501001822003050100182NM 2003 5 1 ASAA0310066 120030301A5320655965818 DOUBLER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AFT AIRSTAIR INTERCOSTAL DOUBLER AT BS 947-967, LEFT BUTTOCK LINE 50 CORRODED. REMOVED AND REPLACED DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20030501001842003050100184NM 2003 5 1 ASAA0310090 120030305A5320656739370 ATTACH ANGLE BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIR TORQUE BOX ATTACH ANGLE AT BS 947-967, LEFT BUTTOCK LINE 50 CRACKED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20030501001882003050100188NM 2003 5 1 ASAA0310020 120030221A53306545775 SKIN PANEL BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 887, STRINGER 19R-20R DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20030501002022003050100202NM 2003 5 1 ASAA0310035 120030225A532065419868 PAD BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, STANSION PAD AT BS 500A, LEFT BUTTOCK LINE 55 CORRODED. REMOVED AND REPLACED STANSION PAD PER SRM. (M) 2L72 4F RTA16WE 20030501002122003050100212EA 2003 5 1 ASOA03122 120030320A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 FLT NR 4414 - DURING A GROUND INSPECTION AT MGM, THE EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP T ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030501002192003050100219NM 2003 5 1 KPVA200316 120030331A2697 WIRE DHAV DHC8 DHC8103 1386005NM SMOKE DETECTOR BROKEN A KPVAO OTHER N FALSE WARNING APAPPROACH 1 WP13808WP 026 SMOKE WARNING LIGHT INTERMITTENT ON LANIDNG APPROACH. AIRCRAFT AIRCRAFT WAS INSPECTRED BY MX AND FERRIED BACK TO HNL, INSPECTION REVEALED A BROKEN WIRE AT NR 2 SMOKE DETECTOR. WIRE REPAIRED AND SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2H72 4T RTA13NM 20030501002202003050100220 2003 5 1 ASAA0380271 420030317A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01977AS 53453 SEA - DURING LINE CHECK, FORWARD LEFT L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD PER MM 25-62-00. (M) 2L72 4F RTA6WE 20030430001052003043000105EU 2003 4 30 031184301 120030428A33508GS00599705 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 DURING PREFLIGHT INSPECTION THE FLIGHT CREW DISCOVERED THE EMERGENCY LIGHT A ROW 6C WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE BULB AND PERFORMED AN GOOD OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030502001992003050200199NM 2003 5 2 AWXA200300417 120030405A5347654N02438 SEAT TRACK BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND SEAT TRACK BS 365 TO BS 418, RBL 24. MAINTENANCE REMOVED SEAT TRACK BS 365 TO BS 418, RBL 24; FABRICATED A NEW REPLACEMENT SEAT TRACK SUPPORT ASSEMBLY AND SHEAR TIE; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-40-02 PG 7-8 & 39. 2L72 4F RTA2NM 20030502002122003050200212EU 2003 5 2 AWXA200300395 120030404A5347D5311278220200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF RT OUTBOARD CABIN SEAT TRACK FORWARD END AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED RT OUTBOARD CABIN SEAT TRACK FORWARD END AT FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-44-11 PG 1, 19, & 20, FIG 2, AND SRM 51-42-11 PG 1, 7, 21, 22, 28, & 39, FIG 8 & 12. 2L72 4F RTA28NM 20030502002282003050200228NM 2003 5 2 EIA2003066 120030417A5710 STRUCTURE BOEING747 747273C 1384896NM RT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 RIGHT WING STA 1323 AFT OF NR 23 VARIABLE CAMBER FLAP LOWER T-CHORD CORRODED. REMOVED CORROSION, TRIMMED DAMAGE, INSPECTED AND NDT, FABRICATED REPAIR AND INSTALL PER ECRA 471-57-217-2 REV-A. 2L74 4F A20WE 20030502002342003050200234WP 2003 5 2 ABXA030133 120030409A3230 UPLOCK DOUG DC8 DC863 302198AWP MLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION CRCRUISE 1 GL23820AX 46155 GEAR UPLATCH FAILED TWICE. RECYCLED AND FOLLOWED ABNORMAL PROCEDURES. SUSPECT CABLE TO NOSE GEAR. TRIED AGAIN ON FINAL APPROACH AND UPLATCH CHECK WAS NORMAL. AIRCRAFT FERRIED TO ILN. INSPECTED UPLATCH ASSEMBLY. GROUND OPS SEVERAL TIMES. LUBRICATED UPLATCH ASSEMBLY. VERIFIED OVERCENTER MEASUREMENTS IAW DC-8 MM 32-31-06. GROUND OPS NORMAL. 2L74 4F 4A25 20030502002422003050200242WP 2003 5 2 IXXA0300032O 120030415A3260 WARNING LIGHT DOUG DC8 DC873F 302199FWP MLG ILLUMINATED A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11606AL 46044 DURING CLIMB FROM KEWR TO KTOL GEAR RETRACTION DOOR NOT LATCHED LIGHT STAYED ILLUMINATED. CREW USED MAIN GEAR ISOLATION SWITCHES SELECTED TO LT AND LATCH LIGHT WENT OUT. RT SELECTED LATCHED LIGHT STAYED ON AND THE ALTERNATE MAIN LANDING GEAR DOOR LIGHTS REMAINED OUT. GEAR WAS CYCLED. INSPECTION IS ON GOING. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. 2L74 4F RT4A25 20030502002432003050200243WP 2003 5 2 MWEA030186 120030425A2421ITL113D SWITCH DOUG DC9 DC932 3022066WP COCKPIT DIRTY A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31302ME 47102 ON PUSHBACK AFTER ENGINE START THE RIGHT DC VOLTS SHOWED ZERO. CLEANED VOLT SELECT SWITCH IN COCKPIT OVERHEAD. OPERATION CHECK GOOD. 2L72 4F A6WE 20030502002452003050200245NM 2003 5 2 XNOA01113 120030411A5270 WARNING LIGHT BOEING727 727227 1384078NM MLG DOOR ILLUMINATED A XN0AO OTHER J WARNING INDICATION CLCLIMB 1 GL2376753 21249 ON DEPARTURE FROM ICT RT MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLE PER CHECK LIST. DOOR LIGHT OUT. 2L73 4F A3WE 20030501001132003050100113WP 2003 5 1 ASAA0380122 120030209A5320S000925 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OAK - DURING C-CHECK, FOUND MID CARGO BAY LEFT FLOOR SUPPORT CRACKED AT TRACK ATTACH RIVET. REPLACED FLOOR SUPPORT AT FS 579 PER SRM 51-10-4 AND 30-2. (M) 2L72 4F RTA6WE 20030501001212003050100121NM 2003 5 1 ASAA0310029 120030225A5330 SKIN BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN PANEL AT BS 251, STRINGER 21L DENTED. REPAIRED DAMAGED SECTION PER SRM. (M) 2L72 4F RTA16WE 20030501002042003050100204NM 2003 5 1 ASAA0310040 120030225A532065466115 FLOOR SUPPORT BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOORBOARD SUPPORT CHANNEL AT BS 540, LEFT BUTTOCK INE 45- LEFT BUTTOCK LINE 65 CORRODED. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM. (M) 2L72 4F RTA16WE 20030502000232003050200023NE 2003 5 2 USAASB03040 220030316A7200 COMPRESSOR BOEING737 7373B7 1384580NM GE CFM56 CFM563BUS 13802NE NR 1 ENGINE LEAKING A USAAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA19512AU 23595 724773 ATL - FLT 1037 - SHORTLY AFTER THRUST WAS SET FOR TAKEOFF OUT OF PHL, A STRONG OIL SMELL WAS NOTICED THROUGH OUT THE CABIN. THERE WAS ALSO SOME HAZE IN THE CABIN. FLIGHT CONTINUED ONTO ATL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A HIGH POWER ENGINE RUN. FOUND THE LEFT PACK EMITTING SMOKE INTO THE CABIN THROUGH THE NR 1 ENGINE BLEED. NO EXTERNAL LEAKS WERE NOTED. AIRCRAFT WAS RELEASED ON MEL 21-1A. MAINTENANCE IN PIT ACCOMPLISHED A NR 1 ENGINE BOROSCOPE THROUGH BLEED VALVES AND 5TH STAGE HIGH PRESSURE COMPRESSOR. FOUND EVIDENCE OF OIL LEAKAGE IN COMPRESSOR. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY. OPERATIONAL CHECK AND LEAK CHECK GOOD. CLEARED MEL 21-1A. (M) 2L72 4F4 FRTA16WE E2GL 20030502000442003050200044WP 2003 5 2 ASAA0380156 120030224A5347SR095301157003 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, SEAT TRACK SECTION IS CORRODED. REPLACED DAMAGED SECTION PER SRM 53-05. (M) 2L72 4F A6WE 20030502001512003050200151WP 2003 5 2 041103 220030411A7320 COMPUTER LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP FUEL SYSTEM FAILED E ESUAEA ENGINE SHUTDOWN UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 CE03274JS 274 74756 RIGHT FUEL COMPUTER FAILED, OPERATED ENGINE IN MANUAL MODE, OIL PSI NORMAL, NR 2 N2 FLUCTUATED, NR 2 ITT GAUGE FAILED MOMENTARILY, ABOUT 20 MINUTES LATER ENGINE FLAMED OUT AT FL390. AIRCRAFT LANDED WITHOUT INCIDENT. STAGE OF OPERATION PART 91, EMPTY. GARRET THE ENGINE MANUFACTURE IS TROUBLESHOOTING THE ENGINE. A LOANER ENGINE HAS BEEN INSTALLED. 2L72 4F4 F A10CE E6WE 20030502001832003050200183EU 2003 5 2 AWXA200300409 120030331A5311D53570303206 FRAME AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A .125 INCH CRACK WAS FOUND AT THE SIXTH FASTENER HOLE DOWN ON FRAME 39, BETWEEN STR 14-15 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME 39 BETWEEN STR 14-15 LT; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA EO 53-14-20. 2L72 4F RTA28NM 20030502002112003050200211NM 2003 5 2 AWXA200300394 120030419A351089151114 BOTTLE AIRBUSA319 A319132 3930340NM ZONE 125 DISCHARGED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28805AW 1049 OMA - DIVERSION - FLT 0012 - APPROXIMATELY 1 HOUR AND 30 MINUTES INTO FLIGHT EN ROUTE FROM PHX TO JFK CREW OXYGEN WENT DOWN TO 20 PSI AND REGULATOR PRESSURE WAS LOW, FLIGHT DIVERTED TO OMA. EMERGENCY OXYGEN SWITCH WAS STUCK IN 100 PERCENT POSITION AFTER GROUND TEST, MASK WAS NOT STOWED PROPERLY CAUSING OXYGEN TO DEPLETE. CONTRACT MAINTENANCE REMOVED AND REPLACED CREW OXYGEN BOTTLE IAW T/C S2A35301, PERFORMED LEAK CHECK, NO LEAKS NOTED. 2L72 4F RTA28NM 20030502002472003050200247WP 2003 5 2 MWEA030172 120030415A575359121551 DOUBLER DOUG DC9 DC915 3022036WP TE FLAP DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 LEFT FLAP FOUND DENT 1 X .068 INCH DEEP AT STATION XRS 320. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030502002492003050200249NM 2003 5 2 03FDEA00591 120030423A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LOWER FORWARD CARGO BILGE AREA LONGERON 52 FOUND WITH CORROSION BETWEEN STA Y = 6-70 TO 6-90. LOWER FORWARD CARGO BETWEEN STA Y=6-70 TO 6-90 LONGERON 52 REPAIRED AS PER SRM 53-10-00, FIG.1, VOL.I. 2L73 4F RTA22WE 20030502002502003050200250NM 2003 5 2 03FDEA00590 120030423A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 6-90 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK CORRODED AT STA 6-90 LT X = 75.25. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG. 1 VOL. I. 2L73 4F RTA22WE 20030502002522003050200252NM 2003 5 2 03FDEA00589 120030421A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK CRACKED AT STA 755 LBL 47.5 BETWEEN FLOOR PANELS NR 241BF, 241CF AND 241JF. CABIN STA 645 TO STA 765 LBL 47.5 SEAT TRACK REPAIRED AS PER SRM 53-70- 00, VOL.I, FIG.1. 2L73 4F RTA22WE 20030502002632003050200263NM 2003 5 2 03FDEA00443 120030415A261265249203 CONTROL UNIT BOEING727 727200 138407ENM E&E BAY FALSE INDICATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25494FE 21532 AT FL 190 AND CLIMBING (310 KIAS) THE FIRE WARNING BELL & MASTER FIRE LIGHT WENT OFF CONTINUOUSLY WITH NO OTHER INDICATIONS. THE BELL WOULD ONLY SILENCE WHEN ANY SILENCING BUTTON WAS HELD IN. BELL AND LIGHT WENT OUT ON DESCENT, CAME BACK ON AS AIRCRAFT BLOCKED IN. BELL AND LIGHT WERE STILL ON UPON ACFT ARRIVAL, CONNECTED EXTERNAL PWR, DURING DEBRIEF WITH CREW, EXTERNAL PWR DROPPED OFF-STARTED APU, APPLIED PWR AND THE BELL AND LIGHT DID NOT COME BACK ON. COULD NOT GET THE PROBLEM TO DUPLICATE. T/S TO FIRE AND OVERHEAT DETECT OR ACCESSORY BOX IN E/E. REMOVED AND REPLACED FIRE DETECTOR BOX PER SMP'S. FIRE SYSTEM TEST NORMAL PER JRH CHAPTER 5 . 2L73 4F RTA3WE 20030502002652003050200265NM 2003 5 2 03FDEA00440 120030415A2612 WARNING LIGHT BOEING727 727200 138407ENM ENG FIRE DETECT ILLUMINATED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25498FE 20867 ON CLIMBOUT OF HARLINGEN ,THE FIRE BELL AND GLARESHIELD LIGHT CAME ON INTERMTTENTLY. NO OTHER INDICATION (MOMENTARY/ INSTANTANEOUS THEN OUT). PERFORM ENGINES FIRE TEST NORMAL, NO DEFECT NOTED. CAN'T DUPLICATE PROBLEM. NO HISTORY. OK FOR SERVICE. 2L73 4F RTA3WE 20030502002702003050200270NM 2003 5 2 SWAA030849 120030415A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 834, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030502002772003050200277NM 2003 5 2 SWAA030856 120030415A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 2 INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 2. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20030505000112003050500011SO 2003 5 5 C2XA03SH115 120030422A531514530628001 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030505000342003050500034NE 2003 5 5 2003UALA00375 220030410A7261 NUT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE LOOSE A UALAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 WP29648UA 25285 A/C EXPERIENCED DROP IN NR 1 ENGINE OIL QTY AND PRESSURE. ENGINE WAS REMOVED FROM A/C AND HOC RUN PERFORMED AT TEST CELL. FOUND NR 1 & 2 OIL SCAVENGE TUBE LEAKING AT 'B' NUT. REPLACED TUBE. IDG CARBON SEAL AT THE MAIN GEAR BOX WAS REPLACED DUE TO THE IDG BEING REPLACED. NO HOC REPORTED AFTER TEST. 2L72 4F4 FRTA1NM E24NE 20030505000372003050500037SO 2003 5 5 C2XA03BT050 120030414A213320996011100 OUTFLOW VALVE EMB 135 EMB135LR 3260305SO CABIN PRESSURE FAULTY A C2XAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SW2727506 145206 EWR---CO2342, CREW REPORTED THAT PRESSURIZATION FLUCTUATED PLUS AND MINUS 1500 FEET PER MINUTE. UNCONTROLLABLE IN AUTO OR MANUAL MODES AIRCRAFT AIR RETURNED TO EWR AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE PNEUMATIC OUTFLOW VALVE (P/N 92185A010100, S/N 00239) IAW EMB135 MM 21-31-04 AND REMOVED AND REPLACED THE DIGITAL PRESSURE CONTROLLER (P/N 20996011100, S/N 01470) IAW EMB135 MM 21-31-01. OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030505000382003050500038WP 2003 5 5 ARWA20030402 120030411A274230042502 ROTARY ACTUATOR DOUG DC8 DC862 3021970WP TRIM SERVO JAMMED A ARWAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO19802BN 45909 RIGHT SUIT CASE HANDLE JAMMED IN FORWARD POSITION AND COULD NOT BE MOVED EVEN WITH C/B PULLED. REMOVED AND REPLACED RIGHT LONGITUDINAL TRIM SERVO ACTUATOR IAW MM 27-41-10. OPERATIONAL CHECK NORMAL IAW MM 27-40-0. 2L74 4F 4A25 20030505000402003050500040SO 2003 5 5 C2XA03TY049 120030415A531012003832001 SHEAR TIE EMB 135 EMB135LR 3260305SO FUSELAGE BENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715527 145413 TYS, DURING A SCHEDULED INSPECTION A DENT WAS FOUND ON THE LEFT FORWARD FUSELAGE BETWEEN FRAMES 10 AND 11 AND BETWEEN STRINGERS 13L AND 15L. MAINTENANCE REMOVED THE DAMAGED SHEAR CLIP, RESTORED SKIN AND INSTALLED A NEW SHEAR CLIP IAW EC5330-01246. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030505000572003050500057NM 2003 5 5 CALA0300199 120030417A5320 STRUCTURE BOEING737 7373T0 1384582NM SUBFLOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717306 23357 INSPECTION FOUND A 3 INCH CRACK IN SUBFLOOR AT STA 1024, RBL 10. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030505000582003050500058NM 2003 5 5 CALA0300200 120030417A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714307 23358 INSPECTION FOUND CABIN FLOORBEAM CORRODED AROUND NUT PLATE HOLE AT STA 344, LBL 35. REPAIRED ONE FLANGE OF THE FLOORBEAM UPPER CHORD IAW SRM 53-10-51, FIGURE 206, SHEET 4. 2L72 4F RTA16WE 20030505000762003050500076EU 2003 5 5 AWXA200300402 120030405A5315D5311146020200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-81 FROM FORWARD SIDE OF FR 18 TO FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-81 FROM FORWARD SIDE OF FR 18 TO FR 20; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 21-22, 28-30, 32, & 39-41, FIG 8, 12, 13 & 18. 2L72 4F RTA28NM 20030505000812003050500081SO 2003 5 5 SWIA200311886 120030412A27503471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER G MULTIPLE FAILURE APAPPROACH 1 NM07196SW6082 6082 120151 BOTH OUTBOARD FLAPS FLUTTER UP TO 5 DEGREES WHEN IN THE 15 DEGREE AND 25 DEGREE POSITIONS. NO FAILURE INDICATED ON THE FLAP CONTROL PANEL. REPLACED FCU AND ANNUNCIATOR WITH VERSION II. OPS CHECK GOOD. 2L72 4T RTA31SO 20030505000962003050500096NM 2003 5 5 PCA0300834 120030411A5311 FRAME BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 CORROSION BS 2200 S42L-S45L FRAME WEB. REPAIRED PER SRM 51-40-02. 2L74 4F A20WE 20030505000982003050500098NM 2003 5 5 PCA0300843 120030410A5320 SUPPORT BOEING747 747249F 1384849NM FWD CARGO BAY CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEVEL 1 CORROSION FWD CARGO DIVIDED / CEILING SUPPORT. REPAIR PER SRM 51-40-03. 2L74 4F A20WE 20030505001072003050500107NM 2003 5 5 03FDEA00210 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 6L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505001092003050500109NM 2003 5 5 AWXA200300427 120030405A5347654N02438 SEAT TRACK BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK INTERGRANULAR CORROSION WAS FOUND ON SEAT TRACK AT BS 365, RBL 45. MAINTENANCE REMOVED SEAT TRACK AT RBL 45 FROM BS 365 TO BS 418; FABRICATED A NEW REPLACEMENT SEAT TRACK PER DWG 141N5130; INSTALLED REPAIR PART IAW B757-200, SRM 51-40-02 PG 11-12. 2L72 4F RTA2NM 20030505001122003050500112EU 2003 5 5 AWXA200300430 120030329A5320D5361018720200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR PANEL SUPPORT ANGLE FORWARD OF FR 13, INBOARD AND OUTBOARD OF FLOORBEAM Y-1292. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT ANGLE FR 13, INBOARD AND OUTBOARD OF FLOORBEAM Y-1292; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT ANGLE PER DWG D53610187; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20030502000102003050200010SO 2003 5 2 SIMA200309016 120030314A532014524131009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION PASSENGER DOOR FORWARD FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED PASSENGER DOOR FORWARD FLOOR SUPPORT IAW EMB 135 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20030502001752003050200175EA 2003 5 2 COMA0360191 120030414A5210601R31903305 MECHANISM CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR CORRODED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01963CA 7127 FLIGHT 5865 CABIN DOOR OUTER HANDLE WILL NOT STOW. REPLACED THE CABIN DOOR BELL CRANK MECHANISM. 2L72 4F RTA21EA 20030502002172003050200217EA 2003 5 2 A6WA200340045 120030416A2420761339D ADG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ELECTRICAL WILL NOT TEST A A6WAO OTHER L NO TEST NRNOT REPORTED 1 GL31411ZW 7569 MAINTENANCE CHECK FLIGHT REQUIRED FOR ADG DEPLOY INFLIGHT FUNCTION TEST. REMOVED AND REPLACED ADG (S/N OFF: 0598) (S/N ON:0736). PERFORMED ADG FLIGHT TEST, TEST OK. ADG COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF). 2L72 4F4 FRTA21EA E15NE 20030502002182003050200218EA 2003 5 2 COMA0360189 120030413A7600 SWITCH CNDAIRCL600 CL6002B19 1900309EA RT ENGINE FAILED A COMAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO01819CA 7415 FLIGHT 5884 RT ENGINE ROLL BACK DURING T/O AND LATER DURING CLIMB. DEFERRED SPEED CONTROL PER MEL. 2L72 4F RTA21EA 20030502002572003050200257NM 2003 5 2 2003UALA00252 120030309A2797 WIRE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLAT FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29664UA 29236 CREW RECEIVED L/E SLAT ASYMMETRY DISAGREEMENT EICAS MESSAGE. FOUND WIRES FOR 12R OUTBOARD SLAT SKEW LOSS SW S2314 AND FLEX CONDUIT BROKEN APPROXIMATELY 3 FEET INBOARD OF SWITCH. REPAIRED WIRES AND INSTALLED INTERIM CONDUIT. ENTERED CF ITEM TO MAKE PERMANENT REPAIR. 2L72 4F4 FRTA1NM E24NE 20030505000442003050500044EU 2003 5 5 G1F2003F00000 120030402A5312 BULKHEAD BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP FUSELAGE SCORED B G1FRO OTHER O OTHER NRNOT REPORTED 1 GL13241RT7739 257057 TOOL SCORING DETECTED ON REAR PRESSURE BULKHEAD SEGMENTS (PN 25-7FC-31-1 UPPER LEFT, 25-7FC-31-55 UPPER RIGHT AND 25-7FC-31-57 LOWER SEGMENTS) DURING THE EIGHT YEAR INSPECTION CODE 530024 OF MFG 125 SERIES 700 FLEX MAINT PROGAM. REAR PRESSURE BULKHEAD LOCATED BETWEEN FRAMES 19(STA423.5) AND 20A(STA436) FABRICATED FROM .028 2024T ALUMINUM, WAS DRESSED TO REMOVE SCORING, MAPPED, MEASURED AND SUBMITTED TO MFG ENGINEERING. ENGINEERING DETERMINED ALL SEGMENTS WERE BEYOND SERVICEABLE LIMITS. ALL SEGMENTS TO BE REMOVED AND REPLACED. 2L72 4F4 F A3EU E6WE 20030505000922003050500092NM 2003 5 5 03FDEA00482 120030417A5411 FRAME BOEING727 727200 138407ENM NR 3 NACELLE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE NACELLE HAS A GOUGE AT FRAME NR 7. REPAIRED COWLING FRAME IAW BOEING 727 SRM 54-10-2 FIGURE 5. 2L73 4F RTA3WE 20030505000942003050500094NM 2003 5 5 PCA0300832 120030411A5315 FLOORBEAM BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FLOORBEAM TOP CHORD LWR SURFACE AT BS 2240 LBL 40 CORROSION. REPAIRED PER SRM 53-10 FIG 12. 2L74 4F A20WE 20030430001232003043000123NM 2003 4 30 03FDEA00577 120030422A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 WHILE WORKING FOUND SHEAR TIE CRACKED AT BS 950D LBL 6 WL 147. REMOVED DAMAGED SHEAR TIE AT BS 950D LBL 6 WL 147 FABRICATED, ALODINE, PRIMED AND INSTALLED REPAIR IAW 53-10-4 FIG 15 AND FED EX EA 7-5310-69479. 2L73 4F RTA3WE 20030430001282003043000128NM 2003 4 30 SWAA030921 120030424A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 4 EA ) AT BS 730 BELOW STR 19R, BS 727E ABOVE STR 23L, BS 764 ABOVE STR 20L & BS 730E BELOW STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430001412003043000141NM 2003 4 30 SWAA030908 120030422A335020121 BATTERY PACK BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM. 2L72 4F RTA16WE 20030430001772003043000177NM 2003 4 30 SWAA030902 120030422A278069598894 ARM BOEING737 7372H4 138448CNM RT WING LE FLAP BROKEN A SWAAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SW29095SW 23054 EXCESSIVE LT RUDDER & AILERON TRIM REQUIRED TO MAINTAIN WINGS LEVEL. FOUND, RT INBOARD KRUEGER FLAP HINGE ARM BROKEN. REMOVED AND REPLACED RT INBOARD KRUEGER FLAP HINGE ARM PER MM. 2L72 4F A16WE 20030430001852003043000185 2003 4 30 SWAA030894 420030421A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030430001952003043000195NM 2003 4 30 SWAA030931 120030427A5315BAC1790 FLOORBEAM BOEING737 737317 138447PNM AFT CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1006, WL 208 & LBL 9. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20030430002642003043000264 2003 4 30 SWAA030825 420030411A256565C19901 CABLE BOEING737 7372H4 138448CNM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030501000262003050100026SO 2003 5 1 ASOA03101 120030310A2611 BATTERY EMB 120 EMB120RT 3260202SO SMOKE DETECTOR INOPERATIVE A ASOAO OTHER N FALSE WARNING CRCRUISE 1 SO11258AS 120131 FLT 4903 - DURING CRUISE FROM IAH-DFW, THE LAVATORY SMOKE DETECTOR GAVE RANDOM FALSE ALARMS. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030501000972003050100097SW 2003 5 1 2003F00242 120030201A792031080811 LINE FRCHLDSA227 SA227DC 3377521SW LT ENGINE OIL CRACKED A I7WAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM051119K DC830B DURING DESCENT, CREW OBSERVED THE LEFT ENGINE OIL PRESSURE LIGHT CAME ON, THIS WAS VERIFIED BY LT OIL PRESSURE INDICATION LOW, CREW THEN SHUT DOWN LEFT ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. OIL LEAK IN PROP GOVERENOR AREA. REPLACED LINE AND RE-ALIGNED PROP GOVERNOR REVERSE LOCK OUT 90 DEGREE ELBOW FITTING. FOUND END OF LINE TO BE STRESSED FROM THE JAM NUT BEING TIGHTENED AND BENDING THE LINE JUST AFT OF THE B-NUT FERRULE. (M) 2L72 4T RTA18SW 20030501001282003050100128NM 2003 5 1 ASAA0310046 120030226A531165465678 FRAME BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FRAME AT BS 1006, LEFT BUTTOCK LINE 39 CORRODED. REMOVED DAMAGE AND INSTALLED FABRICATED FRAME SECTION PER SRM. (M) 2L72 4F A16WE 20030501001862003050100186NM 2003 5 1 ASAA0310088 120030305A53306545J866588 ACCESS PANEL BOEING737 737298C 1384490NM FS 663-727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND KEELBEAM ACCESS PANEL, THREE, AT BS 663-727, BUTTOCK LINE 0 CORRODED. REMOVED AND REPLACED ACCESS PLATES PER SRM. (M) 2L72 4F RTA16WE 20030502000012003050200001NE 2003 5 2 ASAA0380113 220030127A7261806685 SEAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 4 BEARING LEAKING A ASAAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM01954AS 49387 P717371D EN ROUTE BUR-PDX, WITH DIVERSION TO SMF, IN FLIGHT SHUTDOWN AND DIVERSION DUE TO INDICATION OF PRECIPITOUS DECREASE IN OIL QUANTITY (FROM 13.5 TO 10 QUARTS) DURING THE FIRST 30 MINUTES OF FLIGHT. ENGINE REPLACED. SHOP TEARDOWN INVESTIGATION REVEALED DISENTIGRATED NR 4 BEARING CARBON SEAL AS CAUSE OF OIL LOSS. ENGINE CURRENTLY UNDER REPAIR. 2L72 4F4 F A6WE E9NE 20030502000082003050200008SO 2003 5 2 SIMA200309010 120030311A531014525381003 DOUBLER EMB 135 EMB135LR 3260305SO CARGO FLOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 THIS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, LEFT DOUBLER CORRODED BETWEEN FRAME 65 AND 68. REMOVD AND INSTALLED NEW LEFT DOUBLER BETWEEN FRAMES 65 AND 68 IAW EMB135/145 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06 AND CPM 51-21-04. (M) 2L72 4F RTT00011AT 20030502000212003050200021SO 2003 5 2 SIMA200309004 120030307A531014522461011 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION AFT DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 135 51-40-02. (M) 2L72 4F RTT00011AT 20030502000242003050200024NM 2003 5 2 USAABB03053 120030331A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 26 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19610AU 27122 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030505001112003050500111NM 2003 5 5 AWXA200300429 120030402A5310146N8711 DOOR FRAME BOEING757 757225 1384959NM CARGO DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR FRAME WEB AT BS 1380, FROM STR 21 TO 26 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT DOOR FRAME WEB AT BS 1380, FROM STR 21 TO 26 RT; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B757-200, SRM 53-00-07 FIG 202. 2L72 4F RTA2NM 20030505001222003050500122EU 2003 5 5 AWXA200300406 120030405A5350D53230281200 ATTACH ANGLE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON LT FORWARD BELLY FAIRING VERTICAL ATTACH ANGLE BS 1483.4, 13 INCHES FROM OUTBOARD GROUND AIR CONDITIONING ATTACH POINT. MAINTENANCE REMOVED CRACKED LT FORWARD BELLY FAIRING VERTICAL ATTACH ANGLE BS 1483.4; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11 PG 1, 2, PARA 5 & 6, SRM 51-42-11, PG 8-11, FIG 2, PG 17, FIG 5, AND PG 25, 29, FIG 9. 2L72 4F RTA28NM 20030505001242003050500124NM 2003 5 5 03FDEA00216 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 13L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505001362003050500136NM 2003 5 5 03FDEA00635 120030427A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING FOUND INBOARD FLAP, OUTBOARD HINGE WING SIDE WITH PIVOT HOLE WITH MINOR CORROSION. MINOR CORROSION ON RT WING, INBOARD FLAP, OUTBOARD HINGE WING SIDE, PIVOT HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-07, FIG. 401. 2L73 4F RTA22WE 20030505001372003050500137NM 2003 5 5 03FDEA00634 120030428A5712 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- NR 16 L/E SLAT TRACK I/B SUPPORT RIB FOUND CRACKED. 2L73 4F RTA22WE 20030505001382003050500138NM 2003 5 5 03FDEA00633 120030428A5712 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- NR 16 L/E SLAT TRACK I/B SUPPORT RIB FOUND CRACKED. 2L73 4F RTA22WE 20030505001432003050500143NM 2003 5 5 03FDEA00624 120030426A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE (1 EACH) FLAP SIDE FOUND WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69223 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT INBD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030505001512003050500151NM 2003 5 5 03FDEA00495 120030417A5414 SKIN BOEING727 727200 138407ENM NR 2 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 2 ENGINE LEFT AFT NACELLE LOWER FORWARD CORNER SKIN HAS A CRACK AND CHAFING. REPAIRED NR 2 ENGINE COWLING FWD LOWER CORNER IAW BOEING 727-200 SRM 54-10-03. 2L73 4F RTA3WE 20030505001562003050500156WP 2003 5 5 MWEA030181 120030424A272099579969 RIB DOUG DC9 DC981 3022081WP RUDDER CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LOWER END OF RUDDER HAS RIB ASSEMBLY THAT HAS CORROSION AT FLANGE. REMOVED DAMAGE AND INSTALLED NEW RIB. 2L72 4F A6WE 20030505001722003050500172NM 2003 5 5 SWAA030844 120030411A53106935365 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030505001842003050500184NM 2003 5 5 03FDEA00214 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 10L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505001962003050500196EA 2003 5 5 COMA0360194 120030416A2560P2070001214 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY SHORTED A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01982CA 7168 FLIGHT 5794 - FLIGHT ATTENDANT REPORTED EMERGENCY FLASHLIGHT DID NOT ILLUMINATE AFTER TAKING IT OUT OF HOLDER. AFTER ABOUT 40 SECONDS IT STARTED SMOKING AND BECAME HOT TO THE TOUCH. CREW DEACTIVATED IT BY REMOVING THE BATTERY. LATER INVESTIGATION SHOWED THAT THE CONTROLLING CIRCUIT BOARD HAD SHORTED OUT. 2L72 4F RTA21EA 20030505002052003050500205NM 2003 5 5 03FDEA00510 120030418A5321 FLOOR PANEL BOEING727 727200 138407ENM FUSELAGE TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CARGO DECK FLOOR PANEL AT BS 950 RBL 45 INBOARD EDGE TORN. *S/D* REPAIRED IAW FED EX BOEING 727 SR 27-51-002. 2L73 4F RTA3WE 20030505002142003050500214NM 2003 5 5 03FDEA00516 120030418A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION (C53-113-01), FWD CARGO BAY INNER SURFACE OF OUTER SKIN AT BS 699 RBL 3 WL 148 AT NUT PLATE. 2L73 4F RTA3WE 20030505002182003050500218EA 2003 5 5 03105631 120030415A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27631BR 7261 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT ONE SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE INVERTER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505002352003050500235EU 2003 5 5 03114318 120030424A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DIRTY A VTZAK NONE O OTHER ININSP/MAINT 1 EA27318UE 41041 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE VESTIBULE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE ELECTRICAL CONTACTS AT THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030505002412003050500241EU 2003 5 5 AWXA200300390 120030405A5315D53112091202 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-765 AT FR 16. MAINTENANCE REMOVED CORROSION ON UPPER SURFACE OF FLOORBEAM Y-765 AT FR 16 AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF FLOORBEAM; FABRICATED A NEW SECTION OF FLOORBEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 PG 8-10, 12, 28-30, & 32, FIG 2, 3, 12 & 13. 2L72 4F RTA28NM 20030505002422003050500242EU 2003 5 5 03108316 120030418A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHT SECTION. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030505002562003050500256NM 2003 5 5 03FDEA00542 120030418A5320 BRACKET BOEING727 727200 138407ENM FUSELAGE ELONGATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CARGO DOOR BRACKET AT STA 480 FOR CORNER REVEAL HAS TWO EACH RIVET HOLES ELONGATED. FABRICATED NEW BRACKET IAW BOEING 727-200 SRM 51-20-01. 2L73 4F RTA3WE 20030505002672003050500267EA 2003 5 5 03109670 120030419A79301153P0012 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA RT ENGINE OIL FAILED A VTZAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA27670BR 7561 DURING CRUISE, THE CREW REPORTED THAT THE RT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED AND OIL PRESSURE INDICATED ZERO. THE CREW COMPLIED WITH THE QRH AND SHUT DOWN THE RT ENGINE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE RT ENGINE OIL PRESSURE SWITCH. ENGINE RUN OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505002682003050500268EA 2003 5 5 03111692 120030421A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27692BR 7759 DURING MAINTENANCE INSPECTION, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030502001772003050200177NM 2003 5 2 AWXA200300374 120030415A53302024T3050 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW 23219 PHX - MAJOR REPAIR - DURING INSPECTION A 2.625 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 740, STR 19 RT. MAINTENANCE PERFORMED TEMPORARY REPAIR BY CUTTING OUT DAMAGED AREA OF SKIN; FABRICATING A REPAIR PLATE; INSTALLING REPAIR PART AND BLIND RIVET REPAIR IAW B737-300 SRM 53-00-01 PG 204-206 FIG 202. REPAIR TO BE REINSPECTED EVERY 2500 FLIGHT HOURS, PERMANENT REPAIR TO BE ACCOMPLISHED WITH 20,000 FLIGHT HOURS. 2L72 4F RTA16WE 20030502001792003050200179CE 2003 5 2 GLBA2003042 120030403A5270 SWITCH BEECH 1900 1900D 1154162CE CARGO DOOR OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03195GL UE195 CARGO DOOR ANNUN ILLUM IN FLIGHT. ADJUSTED CARGO DOOR DOORSILL SWITCH. 2L72 4T RTA24CE 20030502001932003050200193NM 2003 5 2 DHL2003741535 120030402A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, LT FUSELAGE SKIN AT BS 208 HAS A SHARP DENT ABOVE LT PITOT TUBE. LT FUSELAGE SKIN AT BS 208 HAS A SHARP DENT OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA DIM 1 INCH IAW B-727 SRM 53-30-3 FIG 13. FABRICATED DOUBLER REPAIR FROM 2024-T3 .050 PO 9912380 DIM 3.80 INCH AND FILLER FROM 2024-T3 .040 DIM 1 INCH IAW B-722 SRM 53-30-3 FIG 12 AND 53-30-2 FIG 2. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030502002012003050200201EU 2003 5 2 AWXA200300419 120030329A5347D5347209001100 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF SEAT TRACK Y-1292 AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF BEAM Y-1292 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6, 7 & 88. 2L72 4F RTA28NM 20030502002302003050200230EA 2003 5 2 QXEA0300446 120030408A26109847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 BOI- SCREEN TORN ON CENTER CHIMNEY OF FORWARD CARGO COMPARTMENT. INSTALLED NEW CHIMNEY AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030502002382003050200238NM 2003 5 2 03FDEA00594 120030423A5350 FRAME DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 FORWARD TAIL CONE MOST AFT MAIN FRAME LT SIDE FOUND WITH CRACK. FWD TAIL CONE MOST AFT MAIN FRAME LH SIDE CRACK REPAIRED AS PER DWG. AKC7539 AND SRM 53-00-01, VOL.II. 2L73 4F RTA22WE 20030502002402003050200240NM 2003 5 2 03FDEA00592 120030423A5310 STANCHION DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LOWER FORWARD CARGO AFT BULKHEAD STANCHION P/N A6A7094-9 AT STA X = 9.0 FOUND CORROSION (4 PLACES) ON FASTENERS HOLES. 2L73 4F RTA22WE 20030502002692003050200269NM 2003 5 2 DHL2003741529 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, FUSELAGE SKIN HAS A DENT BS 345 AT STR 21 L. FUSELAGE SKIN BS 345 STR 21L HAS A DENT OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 1 X 1.75 INCH IAW B-727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER EXTERNAL REPAIR FROM MAT 2024-T-3 .063 PO 9912380 DIM 10.75 INCH X 7.5 INCH IAW B-727 SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBLER EXTERNAL REPAIR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030502002712003050200271NM 2003 5 2 SWAA030850 120030415A53306545800 SKIN BOEING737 7372K6 1364440NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29129SW 22340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK (2 EA) AT BS 360, LOWER AFT CORNER OF NR 1 PAX WINDOW, RT SIDE. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030502002752003050200275NM 2003 5 2 SWAA030854 120030415A53116516301 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME OUTER CHORD CRACKED AT BS 188, WL 207 & RBL 30. REMOVED AND REPLACED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20030502002762003050200276NM 2003 5 2 SWAA030855 120030416A531365C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 500D, STR 7R & STR 6L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030502002812003050200281NM 2003 5 2 DHL2003741541 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS A DENT FWD BS 1133 BELOW STR 19 R. DAMAGED FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 1 X 1 INCH AND FABBED REPAIR DOUBLER THAT INCORPORATES NR 43432, 43433, 43435, FROM 2024 T3 .063 PO 9912495 DIM 62.5 X 16 INCHES IAW B-727 SRM 53-30-1 FIG 1, 53-30-2 FIG 2. DOUBLER WAS TREAT, PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-30-1 FIG 1, 53-30-2 FIG 2. 2L73 4F RTA3WE 20030505000102003050500010SO 2003 5 5 C2XA03SH114 120030422A531514521700001 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE LT FLOORBEAM BETWEEN FRAMES 20 AND 21 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-30-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030505000162003050500016NM 2003 5 5 HNAA0300019 120030415A3320BV033021148 SOCKET DHAV DHC8 DHC8201 2809001NM CABIN LIGHT OVERHEATED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07987HA18375 425 CREW REPORTED SMOKE COMING FROM THE OVERHEAD CABIN LIGHT AT ROW 1 D/F. FOUND AFT LIGHT SOCKET OVERHEATED. REPLACED SOCKET. 2H72 4T RTA13NM 20030505000472003050500047CE 2003 5 5 WVE2003F00007 120030310A242130728692 SPLINE ADAPTER LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312B WP ALTERNATOR CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09407FX2203 090 DURING 600 HOUR INSPECTION OF THE ALTERNATOR SPLINE ADAPTER, DISCOVERED ADAPTER TO BE CRACKED IN FOUR LOCATIONS. PROBABLE CAUSE, FATIGUE. (2003B0665) 2L72 4F4 FRTT00008WIE6WE 20030505000702003050500070EU 2003 5 5 AWXA200300399 120030405A5315D5347218820200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292, FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-1292, FORWARD SIDE OF FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 39-41, FIG 18, SRM 51-42-11 PG 6-7 AND SRM 51-49-00 PG 24. 2L72 4F RTA28NM 20030505000722003050500072EU 2003 5 5 03115305 120030425A33508GS00599705 LAMP JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27305UE 41019 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD BULKHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030505000742003050500074EU 2003 5 5 AWXA200300400 120030405A5315D5347218920200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292, FORWARD AND AFT SIDE OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-1292, FORWARD AND AFT SIDE OF FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 39-41, FIG 18, SRM 51-72-11 PG 1-2. 2L72 4F RTA28NM 20030505001032003050500103NM 2003 5 5 03FDEA00206 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 2L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505001672003050500167 2003 5 5 SWAA030839 420030415A2565D31354 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030505001992003050500199WP 2003 5 5 UPS03840445 120030416A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT WILL NOT TEST A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT TEST. REMOVED AND REPLACED SHIPS EMERGENCY LIGHT BATTERY PACK PER 33-50-01, OPS CHECK NORMAL. 2L74 4F RT4A25 20030505002172003050500217NM 2003 5 5 03FDEA00554 120030421A5320 SPLICE BOEING727 727200 138407ENM STRINGER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-111-01) ON STRINGER SPLICE BS 585-595 STR 26L. 2L73 4F RTA3WE 20030505002462003050500246NM 2003 5 5 03FDEA00525 120030418A5753 FAIRING BOEING727 727200 138407ENM RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RT WING NR 8 FLAP TRACK MOVABLE FAIRING PREVIOUS REPAIR GOUGED ON INNER SURFACE AT FORWARD OUTBOARD AREA. *S/D* REPAIRED FAIRING IAW BOEING 727-200 SRM 57-20-04. 2L73 4F RTA3WE 20030505002582003050500258NM 2003 5 5 03FDEA00540 120030418A5753 STIFFENER BOEING727 727200 138407ENM LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LT WING NR 2 FLAP TRACK MOVABLE FAIRING GOUGED ON 2ND FROM FORWARD INTERNAL STIFFENER OUTBOARD EDGE. REMOVED AND REPLACED FORWARD INTERNAL STIFFENER IAW BOEING 727-200 SRM 51-30-02. 2L73 4F RTA3WE 20030506000102003050600010WP 2003 5 6 MWEA030179 120030421A2741 SWITCH DOUG DC9 DC932 3022066WP HORIZONTAL STAB DIRTY A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31209ME 47730 AFTER THROTTLE ADVANCEMENT, TAKEOFF WARNING HORN SOUNDED. ALL INDICATIONS NORMAL. HORIZONTAL STABILIZER SWITCH FOUND STICKING. CLEANED SWITCH. 2L72 4F A6WE 20030506000182003050600018EA 2003 5 6 03112659 120030422A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030506000212003050600021NM 2003 5 6 03FDEA00557 120030421A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-111-01) ON STRINGER 27L BS 700. 2L73 4F RTA3WE 20030506000232003050600023NM 2003 5 6 03FDEA00523 120030418A5753 FAIRING BOEING727 727200 138407ENM LT WING BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT WING NR 4 FLAP TRACK FAIRING FORWARD EXTERNAL DOUBLER BROKEN. *S/D* REPAIRED FAIRING IAW BOEING 727-200 SRM 57-20-04. 2L73 4F RTA3WE 20030506000412003050600041EU 2003 5 6 03FDEA00653 120030429A5410A54612100 PYLON AIRBUS310 A310 EU NR 1 ENGINE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 NR 1 ENGINE PYLON HAS I/B CENTER SECTION AT CENTER T/R HINGE POINT BOWED INWARD APPROX 17 INCHES HIGH AND 20 INCHES LONG WITH 1 INCH DEPTH. SUBSEQUENT DISASSEMBLY AND INSPECTION REVEALED, I/B SIDE OF SKIN AT RIB 7 HAD DEFORMED GUSSET, PYLON PLANK FROM RIB 1 TO RIB 8 BEND, I/B T/R SEAL CHANNEL AT RIB 4 12:00 POSITON GOUGED 1 INCH X 0.25 DEEP, INBOARD T/R FWD HINGE POINT CRACKED, INBOARD T/R CENTER HINGE BRACKET BEARING BROKEN, HYD/FUEL LINE ANGLE BRACKETS AT L/E RIB 3 BENT, I/B SIDE OF PYLON AT RIB 3 HAD 3 RIVETS SHEARED. R/R NR 1 PYLON ON S00010 PER E.A. 6-5450-69698. 2L72 4F RTA35EU 20030506000542003050600054WP 2003 5 6 UPS03840458 120030330A5320 SUPPORT ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, AFT PIT RT AFT DOOR SUPPORT ANGLE CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030506000592003050600059NM 2003 5 6 03115409 120030425A5610001A561A0000219 WINDSHIELD DORNERDO32 DO328300 NM COCKPIT CRACKED A VTZAO OTHER O OTHER DEDESCENT 1 EA27409FJ 3161 DURING DESCENT, THE CREW REPORTED THAT THE RT COCKPIT SIDE WINDOW HAD CRACKED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE WINDOW. WINDOW HEAT AND PRESSURIZATION CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030506000632003050600063NM 2003 5 6 03FDEA00648 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND WITH CORROSION. SURFACE CORROSION ON LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-07, FIG. 401. 2L73 4F RTA22WE 20030506000682003050600068NM 2003 5 6 03FDEA00587 120030420A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK AT RT 47.5 STA 1199 - 1280 CRACKED AND CROWN AREA WORN. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG. 1 VOL. I. 2L73 4F RTA22WE 20030506000762003050600076NM 2003 5 6 03FDEA00567 120030421A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION WHILE WORKING CARD N00319 FOUND CORROSION ON - 27 LT AT BS 950D+6 AND +18, BS 950E+10, BS 950F+10. REPAIRED STR 27 LT IAW SRM 53-10-3. 2L73 4F RTA3WE 20030506000982003050600098NM 2003 5 6 03115427 120030425A2611 WARNING LIGHT DORNERDO32 DO328300 NM SMOKE DETECT ILLUMINATED A VTZAO OTHER N FALSE WARNING DEDESCENT 1 EA27427FJ 3192 DURING DESCENT, THE CREW REPORTED THAT THE -LAV SMOKE- CAS MESSAGE HAD ILLUMINATED, NO SMOKE HAD BEEN DETECTED UPON INSPECTION. MAINTENANCE PERSONNEL PERFORMED A VISUAL INSPECTION FOR SMOKE WITH NO FINDINGS. DURING POWER UP OF THE AIRCRAFT THE CAS MESSAGE DID NOT REAPPEAR. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030506001082003050600108NM 2003 5 6 DHL2003748005 120030426A2121 GASPER FAN BOEING727 727225 1384077NM CABIN INOPERATIVE A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01748DH 22440 NOXIOUS BURNING ODOR COMING FROM GASPER OUTLETS. DEFERRED GASPER FAN PER MEL 21-24 DMI 12684 CAT-D. CIRCUIT BREAKER PULLED AND CONNECTOR REMOVED AT GASPER FAN. REF DMI 12684 - NOXIOUS BURNING ODOR FROM GASPER OUTLETS. REMOVED AND REPLACED GASPER FAN AS PER M/M 21-23-1. OPS CHECKS NORMAL. THIS CLEARS DMI 12684. PLACARDS REMOVED. 2L73 4F A3WE 20030506001112003050600111NM 2003 5 6 CALA0300223 120030425A53156545810 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAO OTHER O OTHER NRNOT REPORTED 1 SW0977303 23354 THREE FASTENERS CORRODED IN FLOORBEAM. REPLACED UPPER STRUCTUREAS REQUIRED IN SRM 53-10-51. 2L72 4F RTA16WE 20030506001132003050600113EU 2003 5 6 AWXA200300420 120030404A5320D539740620200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND AT NUT PLATE RIVET HOLE ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT FR 53, LBL 16. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT (PROFILE JOINT) AT FR 53, LBL 16; FABRICATED A NEW REPLACEMENT PROFILE JOINT IAW DWG 17D539 74706; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-8. 2L72 4F RTA28NM 20030506001202003050600120NM 2003 5 6 CALA0300226 120030425A534765C80736158 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977303 23354 AFT BAG BIN CARGO TIE DOWN RAIL HAS CORROSION AT STATION 947. REMOVED AND REPLACED TIE DOWN TRACK STATION 877 - 947 PER SRM 51-40-02 AND 53-60-53. 2L72 4F RTA16WE 20030502002552003050200255NM 2003 5 2 2003UALA00284 120030316A521042367 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE PAX DOOR ODOR A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29646UA 25283 ACRID AND BURNING RUBBER ODOR ON THE FLIGHT DECK. THE SOURCE OF THE ODOR WAS THE FLIGHT DECK DOOR LATCH ASSEMBLY. REPLACED THE LATCH ASSEMBLY AND THE SYSTEM OPS CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20030502002742003050200274NM 2003 5 2 SWAA030853 120030416A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030502000262003050200026EU 2003 5 2 USAABA03007 120030329A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 0370 PHL - FOUND FAULTY BATTERIES IN THE AFT EPSU. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20030502000392003050200039WP 2003 5 2 ASAA0380150 120030222A532059134217 WEB DOUG DC9 DC982 3022082WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND WEB IS CHAFED AT AFT END OF LEFT NLG DOOR. MATERIAL LOSS IS IN EXCESS OF 20 PERCENT. REPLACED NLG DOOR JAMB GUSSET PER SRM 51-10-2, 10-4, 30-2 AND 30-5. (M) 2L72 4F A6WE 20030502000412003050200041WP 2003 5 2 ASAA0380149 120030222A532099557735 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FORWARD LEFT PAX ENTRANCE INTERCOSTAL CRACKED INBOARD OF HOLD-OPEN HANDLE RELEASE. REPLACED RELEASE (CLIP) PER SRM 51-30-2 AND 51-30-5. (M) 2L72 4F A6WE 20030502000472003050200047WP 2003 5 2 ASAA0380147 120030222A5320593607027 SILL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FORWARD CARGO BAY DOOR JAMB SILL PLATE EDGE CRACKED. STOP DRILLED CRACK AND INSTALLED PLUG RIVET PER SRM 51-01. (M) 2L72 4F A6WE 20030502000512003050200051WP 2003 5 2 ASAA0380161 120030228A5320993061267 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND LEFT CUSP WEB UPPER SURFACE CORRODED AT FS 1250. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-70-4. (M) 2L72 4F A6WE 20030502000712003050200071WP 2003 5 2 ASAA0380183 120030301A53219957918162 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT FLOOR PANEL UPPER SKIN IS CRACKED AT AFT FASTENER HOLE. INSTALLED DOUBLER PER SRM 53-05. (M) 2L72 4F A6WE 20030502000732003050200073WP 2003 5 2 ASAA0380171 120030301A532199525233 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS BROKEN INSERTS AT FS 200-256. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030502000932003050200093SO 2003 5 2 C2XA03IA037 120030414A3260 WARNING LIGHT EMB 145 EMB145LR 3260212SO MLG FALSE ACTIVATIONA C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2729917 145414 STL- FLIGHT 2463, ON CLIMB THE CREW NOTED THAT THE LANDING GEAR WILL NOT RETRACT MESSAGE APPEARED ON THE EICAS. THE CREW RETURNED THE AIRCRAFT TO STL AND LANDED WITHOUT INCIDENT. STL- MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030502000962003050200096NM 2003 5 2 AWXA200300382 120030327A533065757783 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A 9.5 INCH CREASE WAS FOUND AT FRAMED EDGE OF EXTERNAL FUSELAGE SKIN AT BS 807, STR 27 LT TO STR 27 RT. MAINTENANCE CUT OUT DAMAGED AREA OF EXTERNAL FUSELAGE SKIN AT BS 807, STR 27 LT TO STR 27 RT; REMOVED EXISTING REPAIR BS 796 TO BS 810, STR 26-27 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED 3 EACH FILLERS AND A DOUBLER. INSTALLED REPAIR PARTS IAW AWA ER 03-5300-03104-SS2. 2L72 4F RTA16WE 20030502001112003050200111NM 2003 5 2 UPS03240426 120030410A5313 LONGERON BOEING727 727180C 138406GNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 INSPECTION TYPE: C2, WHILE WORKING EO B727-5330-17160-A, STA 366.65 LONGERON S1 IS CRACKED. REMOVED FASTENERS, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED REPAIR CHANNEL AND FILLER IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 2. 2L73 4F A3WE 20030502001312003050200131NM 2003 5 2 373PA0012 120030412A3350873100212 LIGHT BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 FWD RIGHT EMERGENCY LIGHT IDENTIFIER IS INOP. REMOVED AND REPLACED FWD RT LIGHT IDENTIFIER. OPS CHECK OK PER MM 33-51-51. 2L72 4F RTA16WE 20030502001342003050200134NM 2003 5 2 751PA0014 120030412A3350 WIRE BOEING757 757200 1384950NM EMERGENCY LIGHT LOOSE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05751PA 23928 EMERGENCY LIGHTS ROW 17ABC ON FLOOR BROKEN OFF BY PASSENGER. REINSTALLED AND REPAIRED LOOSE WIRING ON EMERGENCY LIGHTING ROW 17ABC PER MM 33-50-00. 2L72 4F RTA2NM 20030502001352003050200135NM 2003 5 2 CALA0300195 120030406A5751 SKIN BOEING737 737524 1384721NM LT AILERON DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715659 28920 THE LT AILERON UPPER SKIN WAS DENTED BY HAIL. ONE DENT MEASURED 0.027 INCH DEEP AND 1.25 INCH DIAMETER. THE OTHER MEASURED 0.031 INCH DEEP AND 0.75 INCH DIAMETER. THE DAMAGED SKIN WAS REPAIRED IAW ECRA 5760-01007. 2L72 4F RTA16WE 20030502001362003050200136NM 2003 5 2 CALA0300196 120030406A5751 SKIN BOEING737 737524 1384721NM RT AILERON DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715659 28920 THE RT AILERON SKIN WAS DENTED IN THREE PLACES BY HAIL. THE DENTS MEASURED 0.023 INCH DEEP X 0.75 INCH DIAMETER, 0.031 INCH DEEP X 0.75 INCH DIAMETER, AND 0.028 INCH DEEP X 1 INCH DIAMETER. THE SKIN WAS REPAIRED IAW ECRA 5760-01008. 2L72 4F RTA16WE 20030502001382003050200138NM 2003 5 2 CALA0300198 120030406A5522 SKIN BOEING737 737524 1384721NM LT ELEVATOR PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715659 28920 THE LT ELEVATOR UPPER SKIN WAS DAMAGED BY HAIL. THE DAMAGE CONSISTED OF ONE PUNCTURE AND THREE DENTS. THE SKIN WAS REPAIRED IAW ECRA 5520-01325. 2L72 4F RTA16WE 20030430002442003043000244WP 2003 4 30 MWEA030171 120030414A57555910055512 SKIN DOUG DC9 DC915 3022036WP SPOILER DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 RIGHT CENTER SPOILER PANEL HAS DENT 1.75 X .037 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE AND BOND DOUBLER. 2L72 4F A6WE 20030501000302003050100030WP 2003 5 1 AALA20030239 120030205A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21461AA 49566 TUL - FOUND CRACKS RADIATING OUT OF THREE RIVET HOLES ABOVE L14R AT STATION 1401. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-01-00 FIG 2. (M) 2L72 4F A6WE 20030501001172003050100117WP 2003 5 1 ASAA0380100 120030122A21501941101 HEAT EXCHANGER DOUG DC9 DC983 3022083WP A/C PACK CLOGGED A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM01965AS 53079 OAK - HOT INSULATION ODOR AND BLUE HAZE IN CABIN WITH APU ON AND AIR CON PACKS ON. REPLACED BOTH PRIMARY AND SECONDARY (P/N 18406032, S/N 46-5085) HEAT EXCHANGERS, BOTH HAD INGESTED INSULATION BLANKET MATERIAL. OPS CHECK OK. (M) 2L72 4F RTA6WE 20030501001192003050100119WP 2003 5 1 ASAA0380095 120030118A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE IN 1ST CLASS CABIN. REPAIRED, RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030501001262003050100126NM 2003 5 1 ASAA0310073 120030303A53116546573 FRAME BOEING737 737210C 1384459NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FRAME AT BS 1104, RIGHT BUTTOCK LINE 27 CHAFED. REMOVED DAMAGED AREA AND REPAIRED FRAME PER SRM. (M) 2L72 4F A16WE 20030501001392003050100139NM 2003 5 1 ASAA0310085 120030305A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 867-947, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED DAMAGED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20030501002142003050100214NE 2003 5 1 A6WA200360004 220030328A732077390017 FUEL CONTROL BAC 146 146200A 1500266EU LYC ALF502ALF502R 41580NE NR 3 ENGINE MALFUNCTIONED A A6WAO OTHER J WARNING INDICATION CRCRUISE 1 GL31607AW E2052 AT FL280, OAT -40 DEGREES C, TMS OFF, ANY REDUCTION IN POWER OF NR 3 ENGINE FUEL FLOW WOULD DROP TO 300 NR A FEW SECONDS. OTHER ENGINE INSTRUMENTS WOULD DROP ACCORDINGLY. REMOVED AND REPLACED NR 3 FUEL CONTROL ASSEMBLY. OPS AND LEAK CHECKS GOOD AT THIS TIME. (M) 2H74 4F4 F A49EU E6NE 20030502000032003050200003EU 2003 5 2 ASOA03120 120030320A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING HANGAR MAINTENANCE AT MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030502000282003050200028NM 2003 5 2 AMTA200300388 120030321A3350 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 EMERGENCY EGRESS FLOOR PATH LIGHTS NOPERTIVE NEXT TO ROW TWO. SECURED LOOSE CONNECTION. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030502000302003050200030SO 2003 5 2 SIMA200309022 120030325A5610163500112 WINDSHIELD EMB 135 EMB135KL 3260302SO COCKPIT FAILED A SIMAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21807AE 145506 DFW - FLT 3813 - DURING CRUISE FLIGHT, THE FIRST OFFICERS WINDSHIELD SHATTERED. AIRCRAFT RETURNED TO DFW WITH NO FURTHER INCIDENT REPORTED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030502000322003050200032SO 2003 5 2 SIMA200309017 120030318A531014522459003 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION, GALLEY CENTER BEAM RAMP SUPPORT CORRODED. REMOVED AND INSTALLED NEW GALLEY CENTER BEAM RAMP SUPPORT IAW EMB 135 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04. (M) 2L72 4F RTT00011AT 20030502000352003050200035WP 2003 5 2 ASAA0380142 120030222A57519957968501 PANEL DOUG DC9 DC982 3022082WP AILERON HINGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, RIGHT AILERON HINGE PANEL NR 3 IS CRACKED AT DRAIN HOLE. STOP DRILLED CRACK AND VERIFIED CONTAINMENT BY EDDY CURRENT INSPECTION PER SRM 51-01. (M) 2L72 4F A6WE 20030502000372003050200037WP 2003 5 2 ASAA0380144 120030222A53203936903505 SUPPORT BRACKET DOUG DC9 DC982 3022082WP MLG WW CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, LEFT MLG WHEEL WELL HYDRAULIC LINE SUPPORT BRACKET CRACKED. REPLACED BRACKET PER MM 20-30-01. (M) 2L72 4F A6WE 20030502000522003050200052WP 2003 5 2 ASAA0380164 120030228A5321539321402400 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL SUPPORT HAT CHANNEL IS CORRODED AT FS 1098-1211. REPLACED SUPPORT PER SRM 51-10-2, 10-3, 10-4 AND 30-1. (M) 2L72 4F A6WE 20030502000562003050200056WP 2003 5 2 ASAA0380168 120030228A57545922500506 SKIN DOUG DC9 DC982 3022082WP NR 1 SLAT SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT NR 1 SLAT LEADING EDGE IS SCRATCHED. REMOVED SCRATCHES AND INSTALLED DOUBLER PER SRM 57-09. (M) 2L72 4F A6WE 20030502000862003050200086EU 2003 5 2 AWXA200300407 120030405A5315D5347207500100 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1732, FORWARD SIDE OF FR 66. MAINTENANCE REMOVED CORROSION ON UPPER SURFACE OF FLOORBEAM Y-1732, AND DOOR SILL FITTING FORWARD SIDE OF FR 66; MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-1732 AND CUT OUT DAMAGED SECTION OF DOOR SILL FITTING; FABRICATED A NEW REPLACEMENT FLOORBEAM, A FILLER, AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 PG 7-41, FIG 2-18, SRM 53-41-14 PG 202-213 FIG 201. 2L72 4F RTA28NM 20030505000232003050500023WP 2003 5 5 MWEA030177 120030415A3000 CIRCUIT BREAKER DOUG DC9 DC981 3022081WP GALLEY TRIPPED A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31803ME 48029 DRAIN MASTER HEATER CIRCUIT BREAKERS POPPED. PERFORMED OPERATIONAL CHECK OF DRAIN MAST HEATER PER MM 30-72-01, RESET CIRCUIT BREAKERS. 2L72 4F A6WE 20030505000252003050500025NM 2003 5 5 DHL2003741539 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN PREVIOUS REPAIR AT BS 1050 TO 1070 HAS DENTS AT EACH END ALONG STR 28R. REMOVED PREVIOUS REPAIR BS 1050 TO 1070 TO INCORPORATE NEW REPAIR IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIMENSIONS 40 X 17.5 INCHES. FABRICATED ONE DOUBLER DIMENSIONS 48 X 19 INCHES USING 2024-T3 .071 PO 9912182 ONE SHIM USING 2024-T3 .063 DIM 40 X 1 INCH AND 4 SHIMS DIMENSIONS 6 X 1 INCH USING .063 2024-T3 PO FOR ALL SHIMS 9912102 IAW B-727 SRM 51-30-3 FIG 1. ALODINED AND PRIMED ALL REPAIR PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED ALL PARTS BS 1050 - 1070 IAW B-727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20030505000432003050500043NM 2003 5 5 SWAA030838 120030414A3213656174010 STRUT BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED SERVICE CHECK, FOUND LEFT MLG STRUT OUTER CYLINDER CORRODED. REMOVED AND REPLACED LEFT MLG OUTER CYLINDER PER MM. 2L72 4F RTA16WE 20030505001312003050500131NM 2003 5 5 03FDEA00489 120030417A2510 PANEL BOEING727 727200 138407ENM COVER PANEL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 BENEATH CIRCUIT BREAKER PANEL FLIGHT CONTROL, APU, HYDRAULIC SYSTEM COVER PANEL IS CRACKED. *S/D* REPAIRED CIRCUIT BREAKER PANEL IAW BOEING CMM 25-00-61. 2L73 4F RTA3WE 20030505001732003050500173NM 2003 5 5 SWAA030845 120030411A53136551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (4 EA) AT BS 360, STR 4R, BS 360, STR 14R, BS 540, STR 14R & BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030505002102003050500210NM 2003 5 5 03FDEA00504 120030417A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FORWARD CARGO PIT AFT BULKHEAD LEFT LOWER ANGLE HAS NUMEROUS AREAS OF CORROSION. *S/D* REPAIRED LT BOTTOM FWD CARGO PIT AFT BULKHEAD ANGLE IAW BOEING 727-200 SRM 51-40-03. 2L73 4F RTA3WE 20030505002202003050500220NM 2003 5 5 03FDEA00553 120030421A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 LWR FUSELAGE EXTERIOR SURFACE BS 450 STR 21R - 22R SKIN OIL CANNING. DENT AT BS 450, STR 21 - 22 RT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REPAIRED DENT PER FED EX EA 7-5330-54488. 2L73 4F RTA3WE 20030505002482003050500248NM 2003 5 5 CALA0300201 120030418A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717306 23357 INSPECTION FOUND CHANNEL CORRODED AT DRAIN MAST, STA 986-1006, L26L TO L27L. THE CHANNEL WAS REPAIRED IAW SRM 51-40-2. 2L72 4F RTA16WE 20030506000032003050600003EA 2003 5 6 COMA0360198 120030416A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01977CA 7157 FLIGHT 5706 LT THRUST REVERSER UNLOCK CAUTION. SECURED T/R AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030506000332003050600033EA 2003 5 6 SWIA200311885 120030413A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07916SW 7634 OVERHEAD EMERGENCY LIGHT IN CABIN (SECOND ONE) IS OUT. REMOVED AND REPLACED LIGHT BULB AS INDICATED PER MM 33-51-16. OPS CHECK GOOD. 2L72 4F RTA21EA 20030506000552003050600055WP 2003 5 6 UPS03840461 120030402A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, R2 UPPER AFT DOOR JAMB CORNER HAS 2 EA CRACKS AT L11R APPROX 1.25 INCH AND 2 INCH LONG. CUT OUT CRACKS IN INNER DOUBLER, FABRICATED DOUBLER, TRIPLER, AND SKIN FILLER IAW DC8 SRM 53-2-0 FIG 16 TR 53-156. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOULBER, TRIPLER AND SKIN FILLER IAW DC8 SRM 53-2-0 FIG 16 TR 53-156. 2L74 4F RT4A25 20030506000602003050600060NM 2003 5 6 DHL2003754004 120030424A3231 ROD BOEING727 727223 1384074NM NLG DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01754DH 22008 IN CRUISE FLIGHT AT FL 310, INTERMITTENT BANGING NOISE HEARD BENEATH COCKPIT FLOOR AND ACCOMPANIED BY NOSE GEAR DOOR ANNUNCIATOR LIGHT. ADJUSTED LEFT AND RIGHT NOSE LANDING GEAR WHEEL WELL DOOR ACTUATION ROD, LEFT AND RIGHT FORWARD AND AFT DOOR STOPS IAW B727 M/M 32-22-1. OPS CHECKED GOOD. 2L73 4F A3WE 20030506000692003050600069NM 2003 5 6 DHL2003741554 120030423A5730 SKIN BOEING727 727200 138407ENM LT WING LE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, LEFT WING I/B LEADING EDGE SKIN IS CREASED WBL 92.8. CUT OUT DAMAGED AREA 6 X 2.25 INCH AND FABBED FILLER FROM 2024-T3 .063 PO 9912380 AND DOUBLER FROM 2024-T3 .080 PO 9912495 DIM 10 X 7.5 INCH IAW B-727 SRM 57-30-4 FIG 2. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 57-30-4 FIG 2. INSTALLED SKIN REPAIR IAW B-727 SRM 57-30-2. RE-INSTALLED ANTI-ICE DUCT IAW B-727 M/M 30-11-81. RE-INSTALLED ACCESS PANEL IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030506000782003050600078NM 2003 5 6 03FDEA00643 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) UPPER ATTACHMENT TO WING REAR SPAR HOLE (2 EACH) FOUND CORRODED. CORROSION ON LH WING, OUTBD FLAP, OUTBD HINGE (WINGSIDE) UPPER ATTACHMENT TO WING REAR SPAR HOLES (2 EACH) AREA REMOVED AS PER CMM 57-44-09 PAGE 403 AND FOUND WITHIN LIMIT AS PER DWG. NO. ARC0503. 2L73 4F RTA22WE 20030506000792003050600079NM 2003 5 6 03FDEA00585 120030423A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 DENT IN FUSELAGE SKIN BS 430, STR 20-21 RT. 2L73 4F RTA3WE 20030506000922003050600092NM 2003 5 6 03FDEA00645 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO WING REAR SPAR LOWER FITTING BORE HOLE (2 EACH) FOUND CORRODED. CORROSION ON LH WING OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO WING REAR SPAR LOWER FITTING BORE HOLE ( 2 EACH )AREA REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-08 FIG. 401 AND DWG NO. ARC0502. REPAIR CARRIED OUT AS PER CMM 57-44-08 FIG. 401. 2L73 4F RTA22WE 20030502000892003050200089NM 2003 5 2 DHL2003741528 120030404A5330 SKIN BOEING727 727200 138407ENM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, FUSELAGE SKIN BULGED AROUND FASTENERS AT BS 1050 STR 27L. REMOVED FASTENERS SRM 51-30-2 WITH CORE FOUND TO BE OUT OF LIMITS SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 5 X 5 INCH. FABRICATED DOUBLER 2024 T-3 .063 PO 9912495 DIM 13.5 X 11.5 INCH FILLER 2024 T-3 .050 PO 9912380 SRM 53-30-3 FIG 3. STRINGER 27L CORRODED OUT OF LIMITS SRM 53-10-1 FIG 1. CUT OUT DAMAGE STR DIM 19.5 INCH, FABRICATED STR SAME MAT PO 3001104 DIM 19.5 INCH 2 EACH SPLICES BAC 1498-131 PO 3001104 SRM 53-10-3. REMOVED WEB AT BS 1050-1070 SRM 51-30-2. INSTALLED REPAIR PARTS SRM 51-30-2. REINSTALLED WEB 51-30-2 AND SEALED AREA SRM 51-20-4. 2L73 4F RTA3WE 20030502001022003050200102NM 2003 5 2 P5CA0300856 120030412A5311 FRAME BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FRAME CRACK STA 1660 S-12R. REPAIRED PER SRM 51-30-02. 2L74 4F A20WE 20030502001042003050200104NE 2003 5 2 P5CA03000857 220030415A7230 COMPRESSOR BOEING747 747200 1384847NM PWA JT9 JT9D7 52054NE NR 3 ENGINE STALLED A P5CAO OTHER O OTHER CRCRUISE 1 WP23524UP 21446 702000 NR 3 ENG COMPRESSOR STALLED WHEN SETTING CRUISE PWR NR 3 ENG CHECKED EVC FILTER FOR WATER. CHECKED BLEEDS INLET AND EXHAUST. NO DEFECTS NOTED CHECKED BLEEDS AND RIGGING PER 72-00-00. UNABLE TO DETERMINE AT THIS TIME, BUT THROTTLE RIG WAS PERFORMED ON ALL FOUR ENGS. 2L74 4F4 FRTA20WE E20EA 20030502001062003050200106NM 2003 5 2 PCA0300837 120030411A5753 SKIN BOEING747 747249F 1384849NM TE FLAP PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEFT WING INBOARD TRAILING EDGE MID FLAP UPPER PNL 577IT PUNCTURE. REPAIRED PER SRM 51-40-06 REV 96. 2L74 4F A20WE 20030502001402003050200140NM 2003 5 2 DHL2003741527 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, FUSELAGE SKIN HAS A DENT AFT BS 1070 BELOW STR 20L. REMOVED FASTENERS FOR ACCESS BS 1070 STR 20 L IAW B-727 SRM 51-30-2. REMOVED AFT LT SIDE WALL AIR DUCT FOR ACCESS IAW B-727 SRM 36-00-01. CUT OUT DAMAGED AREA IAW B-727 SRM 53-30-3 FIG 2 DIMENSION 1.5 X 1.4. FABRICATED ONE DOUBLER DIMENSION 11.5 X 10 USING 2024 T-3 .071 INCH, PO 9912441 AND ONE FILLER DIMENSION 1.5 X 1 USING .063 2024 T-3 PO 9912380 IAW B-727 SRM 53-30-3 FIG 2. ALODINED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 53-30-3 FIG 2. REINSTALLED AIR DUCT REMOVED FOR ACCESS IAW B-727 SRM 36-00-01. 2L73 4F RTA3WE 20030502001422003050200142NM 2003 5 2 SWAA030830 120030414A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29730SW 27862 EEPLS COVER MISSING IN AFT CABIN. INSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030502001432003050200143NM 2003 5 2 SWAA030831 120030414A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 21L. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20030502001472003050200147NM 2003 5 2 SWAA030835 120030414A275265445517 ACTUATOR BOEING737 7373H4 1384600NM LT WING TE FLAP FAULTY A SWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29614SW 28033 AIR TURNBACK - LEFT OUTBOARD L/E FLAP REMAINED EXTENDED DURING FLAP RETRACTION. REMOVED AND REPLACED LEFT OUTBOARD L/E FLAP ACTUATOR PER MM. 2L72 4F RTA16WE 20030502001672003050200167NM 2003 5 2 2003UALA00365 120030407A3350 CONNECTOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHT DIRTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29670UA 29240 AFT GALLEY CROSS AISLE EMERGENCY LIGHT INOP. SECURED AND CLEANED CONNECTOR. 2L72 4F4 FRTA1NM E24NE 20030502001692003050200169NM 2003 5 2 PCAA0304067 120030415A2120 ODOR DHAV DHC8 DHC8102 2809003NM DETECTED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13844EX 339 HPN-FLIGHT 3571, CREW REPORTED AT LOW POWER SETTINGS HAD A STRONG OIL ODOR IN THE BLEEDS. MAINTENANCE INSPECTED BOTH ENGINES, GROUND RAN AIRCRAFT WITH CREW, NO ODOR WAS EVIDENT. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030502001742003050200174EU 2003 5 2 03FDEA00460 120030415A5320D58522 SUPPORT AIRBUS300 A300F4605R 3930327EU ZONE 700 INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25662FE 761 LANDING GEAR WOULD NOT RETRACT, NR 1 SYSTEM - NR 2 DEFERRED. ACN RELEASED FOR SERVICE PER MEL/CDL: 32-30-01. LANDING GEAR RETRACTION MECHANISM INOP. MAX SPEED 255 KIAS/0.65 M. DO NOT USE FMS PROFILE MODE. REMOVED BROKEN PROX SENSOR SUPPORT (IPC 32-14-64-06 ITEM 10) FROM INSIDE LT SHOCK STRUT ABOVE BOGIE BEAM. L/G VMO/MMO SELECT SWITCH PLACED IN L/G DOWN POSITION SEE AMM 32-00-00-4. NO OVERWEIGHT LANDING INSPECTION REQUIRED PER 05-51-11. 2L72 4F RTA35EU 20030502001852003050200185EU 2003 5 2 AWXA200300411 120030327A5320D53911631200 ATTACH ANGLE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A .75 INCH CRACK WAS FOUND ON PARTITION FRAME IN AFT CARGO COMPARTMENT FORWARD BULKHEAD, UPPER RT CORNER. MAINTENANCE PERFORMED HFEC INSPECTION TO DETERMINE WHERE CRACK ENDS; STOP DRILLED CRACK; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 26-5314-00011-JS4. 2L72 4F RTA28NM 20030502001882003050200188NM 2003 5 2 AWXA200300414 120030401A5313BAC1493787 STRINGER BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK A BULGE WAS NOTED ON FUSELAGE SKIN AT STRINGER 28 LT, BS 1460. UPON FURTHER EVALUATION CORROSION WAS FOUND ON STRINGER 28 LT, AT BS 1455. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 28 LT BS 1430 TO 1460; FABRICATED A NEW SECTION OF REPLACEMENT STRINGER; INSTALLED REPAIR PART IAW AWA ER 19-5314-03107-TB1. 2L72 4F RTA2NM 20030502001912003050200191NM 2003 5 2 03FDEA00453 120030416A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION AT STA 990, LBL 7, WL 140 FRAME HAS CORROSION. CORROSION ON FRAME BS 990 LBL 7 WL 140 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FRAME IAW SRM 53-10-4 FIG 13. 2L73 4F RTA3WE 20030502002022003050200202NM 2003 5 2 UPS03M40438 120030315A5347AFA7789545 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT LBL 67 STA 2007 ATTACHMENT BOLT HOLE FOUND CORRODED. CORRODED SEAT TRACK FASTENER REMOVED & SPLICE CUT CARRIED OUT AT ST A1751 X=67 PER SRM 53-70-00 FIG 1 VOL I REV 32. NEW SEAT TRACK AFA7789545 HOLES PICK UP & SPLICE HAT, SPLICE PLATE FABRICATED PER SRM 53-70-00 FIG 1 VOL I & NEW SEAT TRACK AFA7789-545, SPLICE HAT & PLATE INSTALLED AT CABIN STA 1751-2007 X=67 PER SRM 53-70-00 FIG 1 VOL I REV 32. 2L73 4F RTA22WE 20030502002042003050200204NM 2003 5 2 UPS03M40440 120030315A53157075T6511 FLOORBEAM DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C GALLEY FLOORBEAM SUPPORT AT LBL 46 STA 2007 ATTACHMENT FOUND CORRODED. CORROSION AREA REMOVED AT LBL 46 STA 2007 GALLEY FLOORBEAM SUPPORT FOUND EXCEED LIMIT PER SRM 51-21-01 VOL II & 53-00-01 VOL I REV 32. NEW T-CHORD & SPLICE FABRICATED AS PER SRM 53-40-00 VOL I FIG 6 REV 32. SPLICE ANGLE HEAT TREATED AS DPS700-1. NEW T-CHORD & SPLICE ANGLE HOLES PICK OUT PER SRM 51-31-01 VOL II REV 32 & INSTALLED PER 53-40-00 VOL I FIG 6 REV 32. 2L73 4F RTA22WE 20030502002092003050200209EU 2003 5 2 AWXA200300392 220030420A73203352615000 LINE BOEING737 7373S3 1384711NM CFMINTCFM56 CFM563B2 13802EU NR 2 ENGINE BROKEN A AWXACD ABORTED TAKEOFF RETURN TO BLOCK S AFFECT SYSTEMS TOTAKEOFF 1 WP28315AW 23734 724466 PHX - ABORTED TAKEOFF - FLT 0126 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR MKE AT 110 KTS THE NR 2 ENGINE LOST POWER, ABORTED TAKEOFF. AFTER TAXIING OFF RUNWAY THE NR 2 ENGINE EGT STAYED AT 750. MOVED NR 2 THROTTLE THROUGH FULL RANGE OF MOTION, HAD NO EFFECT ON ANY INSTRUMENTS, SHUT DOWN NR 2 ENGINE. MAINTENANCE INSPECTED THE NR 2 ENGINE IAW 71-00-42 FIG 106 AND FOUND THE COMPRESSOR DISCHARGE PRESSURE (CDP) TUBE BROKEN OFF OF THE MAIN ENGINE CONTROL. REMOVED AND REPLACED CDP TUBE IAW BMM 71-00-59 PG 110, PERFORMED POWER ASSURANCE RUN, LEAK CHECK GOOD. COMPLIED WITH HIGH ENERGY STOP INSPECTION PER T/C F8M32001 FOR A 20 MILLION FOOT-POUND ENERGY ABSORPTION PER WHEEL STOP. NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E21EU 20030502002212003050200221NM 2003 5 2 EIA2003059 120030416A5312 BULKHEAD BOEING747 747273C 1384896NM LT MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 LEFT WING MAIN LANDING GEAR WELL BS 1241 VERT BULKHEAD CORROSION AT LBL 94 UNDER HORIZ ANGLE AT VERT CANTED SPLICE. REMOVED CORROSION, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRS 471-57-209-2. 2L74 4F A20WE 20030502002222003050200222NM 2003 5 2 EIA2003060 120030416A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 FRAME OUTER CHORD CORRODED AT STA 1260L BELOW FLOOR LINE (MAIN DECK). REMOVED CORROSION PER BOEING 747-SRM 51-10-01 PAGES 13-14. MATERIAL LOSS WITHIN LIMITS PER BOEING 747-SRM 53-10-01 FIG 1 SHEET 2 AND 3 NOTE B AND SHEET 6 DETAIL II. REPAIRED SHORT EDGE MARGIN FASTENERS PER ECRA 471-57-219-2. 2L74 4F A20WE 20030502002242003050200224NM 2003 5 2 EIA2003062 120030416A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE WORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 RIGHT FUSELAGE SKIN STA 2280-2416 WORN AT INTERFACE OF VERT STAB. TRIMMED OUT DAMAGE, INSPECTED AND NDT AREA, FABBED AND INSTALLED REPAIR PARTS PER ECRA 471-53-221-2. 2L74 4F A20WE 20030502002262003050200226NM 2003 5 2 EIA2003064 120030416A5414 SKIN BOEING747 747121 1384871NM NR 3 PYLON CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 NR 3 PYLON INBOARD SIDE SKIN CRACKED TO UPWARD ABOVE PLATE 473CL. PERMANENT REPAIR INSTALLED PER ECRA 480-54-158-1 PER 8110-3 FROM BOEING. 2L74 4F A20WE 20030502002352003050200235WP 2003 5 2 ABXA030134 120030415A5610 LOCK DOUG DC9 DC931 3022065WP COCKPIT WINDOW STICKING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 FIRST OFFICER'S CLEAR VIEW WINDOW WOULD NOT OPEN. FOUND UPPER WINDOW LOCK STICKING. CLEANED AND LUBRICATED LOCK. OPS CHECKED GOOD IAW DC-9 MM 56. 2L72 4F A6WE 20030502002372003050200237NM 2003 5 2 03FDEA00595 120030424A2611774001 SMOKE DETECTOR BOEING727 727200 138407ENM MAIN CARGO MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25479FE 21461 INFLIGHT RECEIVED MAIN CARGO SMOKE ALARM IN SECTION NR 3 COMPLIED WITH RED TABS AND LIGHT EXTINGUISHED. A/C RECEIVED INTO GATE NO FIRE OR SMOKE NOTED AT ARRIVAL. INSPECTED MAIN CARGO DECK SECTION NR 3, NO INDICATION OF FIRE ANYWHERE. DEMI CAN AYY 5070 HAD APPX 180 LBS OF DRY ICE FOR MEDICAL EQUIPMENT AT SECTION NR 3 RT. PERFORMED MC SMOKE DETECTION SYS ADJ/TEST PER MM 26-16-001-5, OP'S CHECKS NORMAL. REMOVED AND REPLACED NR 3 SMOKE DETECTOR AS A PRECAUTIONARY PER MM 26-16-001-4, SYS OPS CHECKS NORMAL PER MM 26-16-001-5. 2L73 4F RTA3WE 20030502002442003050200244NM 2003 5 2 DHL2003741551 120030323A5210 HINGE BOEING727 727200 138407ENM MAIN CABIN DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, MCD HINGE CRACKED (FWD LWR SECTION AND AFT UPPER SECTION) NDT CONFIRMED. REMOVED DAMAGED HINGES AND INSTALLED NEW P/N MS20001-16, PO 307742 IAW AEI B-727 MM CHAPTER 52 FIGURE 5201C. OPS CHECK GOOD IAW AEI B-727 MM CHAPTER 52 PAGE 65. 2L73 4F RTA3WE 20030501001362003050100136NM 2003 5 1 ASAA0310044 120030226A53106955131 DOOR FRAME BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DUIRNG C-CHECK, FOUND APU ACCESS DOOR FRAME AT BS 1100, WATERLINE 220 CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED FRAME PER SRM. (M) 2L72 4F A16WE 20030501001452003050100145NM 2003 5 1 ASAA0310019 120030221A53106545783501 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500A, STRINGER 28L-28R CORRODED. FABRICATED AND REPLACED SHEAR TIE PER SRM. (M) 2L72 4F RTA16WE 20030501001582003050100158NM 2003 5 1 ASAA0310064 120030301A532065549241 ANGLE BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND MAIN CARGO DOOR UPPER ATTACH ANGLE AT BS 434, STRINGER 14L CRACKED. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20030501001642003050100164NM 2003 5 1 ASAA0310051 120030227A54206552263110 GUSSET BOEING737 737298C 1384490NM NR 1 NACELLE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE FAIRING GUSSET AT NACELLE STATION 227, CRACKED. REMOVED AND REPLACED GUSSET PER SRM. (M) 2L72 4F RTA16WE 20030502000172003050200017SO 2003 5 2 SIMA200309018 120030314A532014524131011 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, PASSENGER DOOR AFT FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE PASSENGER DOOR AFT FLOOR SUPPORT IAW EMB 35 SRM 51-40-02, 51-20-03. (M) 2L72 4F RTT00011AT 20030502000422003050200042WP 2003 5 2 ASAA0380154 120030224A5321993653911 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030506001422003050600142CE 2003 5 6 CGO2003F00005 120030327A246050284003 CONTROL PANEL BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE DC GROUND FAULT INOPERATIVE B CGORO OTHER O OTHER NRNOT REPORTED 1 GL03740TA3336 RK123 INVESTIGATED PILOT COMPLAINT OF UNSUCCESSFUL BATTERY FEEDER PREFLIGHT TESTS. PROBLEM RECTIFIED AFTER TROUBLESHOOTING BY REPLACEMENT OF PN 50284-003 DC GROUND FAULT PROTECTION PANEL (MFG) PART TSN/TSOH UNKNOWN. HAVE NOTED THIS PART PREVIOUSLY TO BE SOURCE OF SIMILAR COMPLAINTS. A/C TT:3336.1 HRS/2693 CYCLES. 2H72 4F4 FRTA16SW E25EA 20030506001502003050600150SO 2003 5 6 CSA2003F00000 120030415A26121734362 FIRE DETECTOR PIPER PA31T PA31T3 7103128SO PWA PT6 PT6A11 52043NE RT ENGINE BROKEN E CSAAO OTHER O OTHER NRNOT REPORTED 1 AL01217CS18002 31T8275014 PCE10429 ON 11 APR 03, THE RIGHT ENGINE FIRE LIGHT CAME ON INTERMITTENTLY IN FLIGHT. THE AIRCRAFT WAS LANDED IN WBB WITHOUT INCIDENT, AND THE FIRE LIGHT CAME ON STEADY AT TOUCHDOWN. NO OTHER SIGN OF FIRE PRESENT, AND ENGINE WAS SHUT DOWN AT FIRST SAFE OPPORTUNITY. THE STARTER/GEN MOUNTED THERMOCOUPLE SENSOR WAS PHYSICALLY BROKEN, WITH THE INSULATED BACKSHELL OF THIS UNIT HANGING FREE. FIRE DETECTION SYSTEM OPERATION WAS NORMAL AFTER REPLACING SENSOR. 1L72 3T3 T A8EA E4EA 20030506001622003050600162WP 2003 5 6 ASAA0380220 120030307A53203925817502 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOOR SUPPORT CRACKED. REPLACED DAMAGED CABIN FLOOR SUPPORT PER SRM. (M) 2L72 4F A6WE 20030506001642003050600164WP 2003 5 6 ASAA0380222 120030307A5347292235714400 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO TRACK CORROSION AT FASTENER HOLES. REPLACED DAMAGED TRACK PER SRM. (M) 2L72 4F A6WE 20030506001732003050600173WP 2003 5 6 ASAA0380250 120030307A575353960262 ATTACH FITTING DOUG DC9 DC982 3022082WP LT TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, LEFT OUTBOARD FLAP HINGE ATTACH LUG IS GOUGED. BLENDED PER ASA EA 5750-01803. (M) 2L72 4F A6WE 20030506001802003050600180EA 2003 5 6 A6WA200340038 120030323A2751 INDICATOR CNDAIRCL600 CL6002B19 1900309EA RT TE FLAP MALFUNCTIONED A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31422AW 7341 RIGHT FLAP INDICATOR FLASHES BETWEEN 8 DEGREES AND 10 DEGREES WITH FLAPS SET AT 10 DEGREES. MEL M ACTION CAUSES FAULTS. REMOVED AND REPLACED FLAP POSITION TRANSMITTER. (M) 2L72 4F RTA21EA 20030506001922003050600192WP 2003 5 6 ASAA0380219 120030307A534795300082 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM. (M) 2L72 4F A6WE 20030506001942003050600194EA 2003 5 6 A6WA200340053 120030413A4900 APU CNDAIRCL600 CL6002B19 1900309EA FIRE A A6WAF ACTIVATE FIRE EXT. A FLAME/FIRE NRNOT REPORTED 1 GL31434AW 7322 AFTER APU SHUTDOWN FIRE WAS NOTED IN THE INTAKE. AGENTS USED HALON/DRY CHEMICAL TO EXTINGUISH. REMOVED AND REPLACED THE APU, SUSPECT CAUSE AS EITHER THE LOAD CONTROL VALVE OR THE FUEL SHUTOFF VALVE. (M) 2L72 4F RTA21EA 20030506001952003050600195WP 2003 5 6 ASAA0380227 120030307A53103924827511 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND SHEAR TIE CORRODED. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR SPLICE PER SRM. (M) 2L72 4F A6WE 20030506002042003050600204NM 2003 5 6 ASAA0310017 120030216A5320654962411 STRAP BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DUIRNG SCHEDULED D-CHECK, FOUND TRANSITION STRAP AT BS 851-947, STRINGER 21R-23R CORRODED. REMOVED AND REPLACED TRANSITION STRAP PER SRM. (M) 2L72 4F RTA16WE 20030506002072003050600207WP 2003 5 6 ASAA0380232 120030307A534759366631 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND MID CARGO TRACK LEFT SIDE LOWER SURFACE HAS FASTENER WITH SHORT EDGE MARINE. INSTALLED SPLICE PLATE ON CARGO TRACK. (M) 2L72 4F A6WE 20030506002342003050600234WP 2003 5 6 ASAA0380214 120030304A52805936793 DOOR DOUG DC9 DC982 3022082WP MLG CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - OFUND DURING 30K CHECK, LEFT MLG STRUT DOOR IS CORRODED ON LOWER OUTER SURFACE. REMOVED DAMAGED SECTION AND INSTALLED BONDED ALUMINUM FILLER AND DOUBLER PER EA 3110-01126. (M) 2L72 4F A6WE 20030506002352003050600235WP 2003 5 6 ASAA0380215 120030304A533059535804 PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT FUSELAGE AFT PANEL 2207 IS CRACKED AT THE FORWARD END. REPAIRED PANEL WITH FIBERGLASS OVERLAY PER SRM 51-70-1. (M) 2L72 4F A6WE 20030506002362003050600236NM 2003 5 6 ASAA0310014 120030214A33508821004 BATTERY PACK BOEING737 737290C 138448VNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - DURING PREFLIGHT INSPECTION, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON PALLET NR 2. REMOVED AND REPLACED BATTERY PACK, THEN LIGHT OPERATED NORMALLY. (M) 2L72 4F A16WE 20030506002442003050600244WP 2003 5 6 ASAA0380263 120030312A53105936038501 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OAK - FOUND DURING C-CHECK, AFT CARGO BAY LOWER DOOR BEAM EDGE CORRODED ON HORIZONTAL LEG. REPLACED LOWER BEAM PER SRM 51-30-2 AND 30-6. (M) 2L72 4F RTA6WE 20030505001682003050500168NM 2003 5 5 SWAA030840 120030415A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 EEPLS COVER LOOSE AT ROW NR 2. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030505001912003050500191NM 2003 5 5 EIA2003070 120030418A5230 FITTING BOEING747 747273C 1384896NM CARGO DOOR CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 NR 4R NOSE CARGO DOOR LATCH FITTING ON NR 3 BOLT HOLE LOCATION IS CHAFED. REAMED HOLE FROM .530 TO .671 PER EO 53-747-1633-01 REV-C, FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED. 2L74 4F A20WE 20030505002262003050500226WP 2003 5 5 03FDEA00547 120030418A7500 GASKET DOUG DC10 DC1010 3022110WP NR 3 ENGINE BLOWN A FDEAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION DEDESCENT 1 SO2568057 48264 AT TOP OF DESCENT GOT INTERMITTENT THEN STEADY LOOP A LT NR 3 ENG FOLLOWED RED TABS TESTED LOOP-B TEST FAILED FOLLOWED ENG FIRE SEVERE DAMAGE CHECKLIST SHUTDOWN NR 3 ENG FIRE INDICATIONS CONTINUED UNTIL AFTER SHUTDOWN. FOUND 9TH STAGE METAL GASKET BLOWN OUT, WHICH CAUSED HOT AIR TO BE BLOWN ON THE -A- AND -B- FIRE LOOPS. REMOVED AND REPLACED GASKET PER STANDARD MAINT PRACTICES. FOUND NO FAULTS WITH -B- LOOP, OPS CHECK NORM PER M/M 26-10-00-5. INSP TIN FOIL ON DUCT JOINTS, NO DAMAGE FOUND. NR 3 ENG WAS RAN PER JRH, NO FAULTS NOTED ON IDLE ENG RUN. REOPENED ENG AND INSP DUCTS, NO FAULTS NOTED, ENG COWLINGS ARE CLOSED PER M/M 71-00-00-2. OK FOR SVC. 2L73 4F A22WE 20030505002452003050500245NM 2003 5 5 03FDEA00524 120030418A5753 FAIRING BOEING727 727200 138407ENM RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT WING NR 5 FLAP TRACK MOVABLE FAIRING LEADING EDGE DAMAGED. *S/D* REMOVED AND REPLACED SKIN IAW BOEING 727-200 SRM 51-20-01. 2L73 4F RTA3WE 20030505002622003050500262NM 2003 5 5 03FDEA00533 120030418A5245 BUSHING BOEING727 727200 138407ENM AC PACK DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT PACK COOLING DOOR ACTUATOR ROD OPENING ELONGATED AND GOUGED. REMOVED AND REPLACED BUSHINGS IAW BOEING 727 SOPM 20-50-03 AND REMOVED AND REPLACED SKIN IAW BOEING 727-200 SRM 51-30-02. 2L73 4F RTA3WE 20030506000442003050600044EA 2003 5 6 COMA0360205 120030418A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01458CA1246 7613 FLIGHT 5102 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20030506000752003050600075WP 2003 5 6 03FDEA00568 120030421A5330 FINGER DOUBLER DOUG DC10 DC1030 3023501WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 MAIN DECK UNDER F/R STRUCTURE STA 515 TO 535 LBL 8.5 TO RBL 8.5 FINGER DOUBLER CORRODED AND FASTENER HEADS CORRODED AND BROKEN OFF. CLOSING ACTION ON 04/20/03. REMOVED AND REPLACED FINGER DOUBLER IAW SRM 53-12-01 AND SRM 51-31-01. FAB NEW DOUBLER IAW SRM 53-12-01, TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED DOUBLER IAW SRM 51-31-01. 2L73 4F A22WE 20030506001222003050600122NM 2003 5 6 CALA0300230 120030429A532069429013 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAO OTHER O OTHER NRNOT REPORTED 1 SW0977303 23354 AFT CARGO COMPARTMENT INTERCOSTAL CORRODED INBOARD OF CARGO DOOR JAMB STATION 807 AND 827. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-00. 2L72 4F RTA16WE 20030506001532003050600153CE 2003 5 6 SVV2003F00000 120030422A32303581507715 UPLOCK BRACKET BEECH 36 A36 1151604CE CONT O520 IO520* 17032SO RT MLG WW FAILED E SVVAO OTHER O OTHER NRNOT REPORTED 1 AL059468Q E314 ACTUATOR ROD TO RT GEAR FAILED. APPARENT CAUSE MAY HAVE BEEN FAILURE OF UPLOCK SYSTEM TO RELEASE. FOUND ALOT OF DIRT IN UPLOCK ROLLER AND POSSIBLE WORN UPLOCK BRACKET. 1L71 3O3 O 3A15 E5CE 20030506001742003050600174WP 2003 5 6 ASAA0380251 120030307A5753591921810 HINGE FITTING DOUG DC9 DC982 3022082WP RT TE FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT WING FLAP HOLE FOR BEARING ASSEMBLY IS CORRODED. REMOVED CORROSION. INSTALLED REPAIR SLEEVE AND BUSHING PER EA 5750-01796. (M) 2L72 4F A6WE 20030506001812003050600181WP 2003 5 6 ASAA0380254 120030307A531153960262 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO AREA HAS FRAME CORRODED. REMOVED FRAME CORROSION AND INSTALLED REPAIR ANGLES PER SRM. (M) 2L72 4F A6WE 20030506002232003050600223NM 2003 5 6 ASAA0310008 120030125A52416552873 TORQUE TUBE BOEING737 737290C 138448VNM R2 DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 SEA - CREW REPORTED THE R2 DOOR WAS DIFFICULT TO OPERATE THROUGH THE OPEN AND CLOSE CYCLE. S/D REMOVED AND REPLACED AFT GALLEY DOOR TORQUE TUBE (P/N 65-45849-160) AND RIGGED R2 DOOR, THEN DOOR OPERATED WITHIN LIMITS. (M) 2L72 4F A16WE 20030507000172003050700017CE 2003 5 7 AUS20030323 120030313A27316627401000001 ACTUATOR LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312 01518WP ELEVATOR TAB FAULTY W O OTHER F FLT CONT AFFECTED APAPPROACH 1 AUS (AUS) HORIZONTAL STABILISER TRIM ACTUATOR INTERNAL FAILURE. 2L72 4F4 FRTT00008WIE6WE 20030507000222003050700022 2003 5 7 AUS20030328 420030318A2230 SWITCH FOKKERF27 F27MK50 EU PWA PWA120PW125B NE AUTOTHROTTLE SYSFAULTY W O OTHER O OTHER CLCLIMB 1 AUS 21553 (AUS) ENGINE RATING SELECT PANEL (ERSP) FAULTY. SUSPECT CLIMB MODE SWITCH WORN INTERNALLY. 2H72 4T4 TRTA817 E20NE 20030507000282003050700028NM 2003 5 7 AUS20030331 120030314A5753 BOLT BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU TE FLAP TRACK SHEARED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT OUTBOARD TRAILING EDGE FLAP INBOARD FLAP TRACK FAIRING ADRIFT. INSPECTION FOUND A BOLT SHEARED WHICH THEN ALLOWED THE FLAP FAIRING CAM FOLLOWERS TO SEPARATE FROM THE TRACK. 2L72 4F4 FRTA16WE E21EU 20030502001162003050200116EA 2003 5 2 SWIA200311870 120030416A5720 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA WING MISSING A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 STRINGER CLIP AT WS 106.4 LOWER WING PLANK, FORWARD INTEGRAL STRINGER MISSING. FOUND DURING C-CHECK INSPECTION. 2L72 4F RTA21EA 20030502002062003050200206WP 2003 5 2 DHL2003807005 120030415A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP CARGO BAY MALFUNCTIONED A DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01807DH 45990 LOWER CARGO LIGHT ILLUMINATED. RESET LOWER CARGO SMOKE DETECTOR PER SMM 26-15-0. 2L74 4F RT4A25 20030502002132003050200213EU 2003 5 2 AWXA200300396 120030405A5320D5347112420100 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF WEB BETWEEN FR 69 AND FR 70, AND AFT OF BEAM Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED SHEAR PLATE WEB BETWEEN FR 69 AND FR 70, AFT OF BEAM Y-1292, BETWEEN STR 23 AND STR 24 RT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 53-00-14, PG 101-102, SRM 51-44-11, PG 16, 19-20, FIG 2, AND SRM 51-42-11, PG 8-12, 21, 22, FIG 2, 3, & 8. 2L72 4F RTA28NM 20030502002462003050200246EA 2003 5 2 COMA0360211 120030422A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01977CA 7157 FLIGHT 5857 LEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20030502002582003050200258 2003 5 2 2003UALA00280 420030315A344206650008405 TRANSCEIVER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE WX RADAR SYS INTERMITTENT A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29841UA 1545 DIVERTED DUE TO INOPERATIVE WEATHER RADAR. REPLACED WEATHER RADAR TRANSCEIVER, SYSTEM GROUND CHECKS OK AND CFDS SELF TEST NORMAL. 2L72 4F4 FRTA28NM E40NE 20030502002612003050200261EA 2003 5 2 03101638 120030411A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505000012003050500001NM 2003 5 5 XNOA01115 120030416A5270 SWITCH BOEING727 727227 1384078NM MLG DOOR DIRTY A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL2376753 21249 ON DEPARTURE FROM BWI RT MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLED PER CHECK LIST. DOOR LIGHT OUT. CLEANED & INSPECTED RT MAIN GEAR DOOR SWITCH. DOOR OPS CHECK GOOD IAW B727 MM 52-81-0. 2L73 4F A3WE 20030505000042003050500004WP 2003 5 5 03FDEA00445 120030415A5347 SEAT TRACK DOUG DC10 DC1030 3023501WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 MAIN DECK SEAT TRACK STA 595 TO 675 AND STR FOR FLOORBOARDS BAD. CLIP NUTS HOLES CORRODED TOP AND BOTTOM. BLENDED DAMAGE TRACK IAW SRM 53-10-00 STA 595 TO 620 FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR SECTIONS AND SPLICES IAW SRM 53-70-00. 2L73 4F A22WE 20030505000072003050500007WP 2003 5 5 03FDEA00447 120030415A7830 STRUCTURE DOUG DC10 DC1030 3023501WP T/R SUPPORT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 COMPLY WITH EA 8-7832-68786 NR 1 ENGINE RM T/R-DISPOSITION OF CRACK IN T/R FWD SUPPORT EXTRUSION. CLOSING ACTION ON 04/15/03. COMPLIED WITH EA 8-7830-68786. NR 1 ENGINE RT T/R-DISPOSITION OF CRACK IN T/R FWD SUPPORT EXTRUSION. 2L73 4F A22WE 20030505000312003050500031NM 2003 5 5 2003UALA00372 120030409A5270 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE PAX DOOR ILLUMINATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29104UA 26902 A/C RECEIVED DOOR UNLOCKED WARNING FOR 5R. 2L74 4F4 FRTA20WE E24NE 20030505000362003050500036CE 2003 5 5 GLBA2003047 120030411A7500 TUBE BEECH 1900 1900D 1154162CE LT BLEED AIR DAMAGED A GLBAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 NM03219GL UE219 NR 1 ENG ITT WAS HOT ON CLIMBOUT. REMOVED AND REPLACED LT BLEED AIR TUBE FROM PRSOV TO PRECOOLER, GROUND RUN OPS CK GOOD. 2L72 4T RTA24CE 20030505000502003050500050NM 2003 5 5 AWXA200300378 120030402A5210 CABLE BOEING757 757225 1384959NM PAX DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - EMERGENCY EVACUATION SYSTEM - DURING C-08 CHECK THE L-2 DOOR FAILED EMERGENCY POWER ACTUATION TEST FOR TRAVEL OF ACTUATION CABLE. MAINTENANCE ADJUSTED THE L-2 DOOR EMERGENCY POWER ACTUATION CABLE IAW BMM 52-11-32 PG 404 & 408, CABLE TRAVEL CHECKED GOOD IAW T/C F1C52607. 2L72 4F RTA2NM 20030505000512003050500051NM 2003 5 5 DHL2003752001 120030416A2611160117301 BATTERY BOEING727 727223 1384074NM SMOKE DETECTOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01752DH 22466 AFT LOWER CARGO SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED BATTERY IN NR 2 AFT CARGO SMOKE DETECTOR. PERFORMED CHARACTERIZATION OF DETECTOR, OPS CHECKED GOOD IAW 727 ADVANCED M/M SUPPLEMENT 26-16-01. 2L73 4F A3WE 20030505000532003050500053EU 2003 5 5 AUS20030242 120030228A531341L STRINGER AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER NR 41L LOCATED BELOW FORWARD CARGO AREA BETWEEN FRAME 30 AND FRAME 31 CONTAINED LEVEL 2 CORROSION. AREA OF CORROSION 127MM (5IN) BY 25.4MM (1IN) AND 0.8636MM (0.034IN) DEEP. FOUND DURING INSPECTION IAW MRBR 53.21.80. 2L72 4F4 FRTA28NM E29NE 20030505000612003050500061NM 2003 5 5 CALA0300207 120030406A5522 SKIN BOEING737 737524 1384721NM ELEVATOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2737615 27328 THE AIRCRAFT SUFFERED HAIL DAMAGE TO THE UPPER SKIN PANEL OF THE LT ELEVATOR. THE HAIL IMPACT CAUSED A SMALL DENT AT APPROXIMATELY ELEVATOR STATION 86.8. THE DAMAGE CLEAN UP REQUIRED REMOVAL OF ALL PLIES. THE DENT WAS APPROXIMATELY 15.5 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE SKIN PANEL WAS REPAIRED IAW ECRA 5520-01330. 2L72 4F RTA16WE 20030505000642003050500064NM 2003 5 5 CALA0300210 120030406A5522 SKIN BOEING737 737524 1384721NM ELEVATOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0937615 27328 AIRCRAFT SUFFERED HAIL DAMAGE TO THE RT ELEVATOR UPPER SKIN PANEL. THE HAIL IMPACT CAUSED A SMALL DENT AT APPROXIMATELY ELEVATOR STATION 88.9 AND 10.25 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE CLEAN UP REQUIRED REMOVAL OF ALL PLIES AND THE CORE. THE SKIN WAS REPAIRED IAW ECRA 5520-01332. 2L72 4F RTA16WE 20030505000662003050500066NM 2003 5 5 CALA0300212 120030422A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914320 23371 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016 FROM RBL 10 TO LBL 35. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS PERFORMED IAW SRM 53-00-51, FIGURE 202. 2L72 4F RTA16WE 20030505000782003050500078EU 2003 5 5 MALA030240 120030418A215011341041 MOTOR SAAB SF340 340B 7860101EU FAILED A MALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15434XJ 340B434 DURING TAXI IN ON FLIGHT 3230, SMOKE FILLED CABIN DURING TAXI INTO GATE. AFTER NORMAL LANDING IN TRL CREW NOTICED A STRONG ELECTRICAL ODOR WHILE TAXIING TO THE GATE THE CABIN FILLED WITH SMOKE, THERE WERE NO VISIBLE SIGNS OF FIRE AND THE CAUSE OF SMOKE WAS UNKNOWN. MAINTENANCE REMOVED AND REPLACED SUPPLEMENTAL AC MOTOR IAW R134, AC CONDI SYSTEM MAINTENANCE MANUAL SAAB 340 SAAB 340 A/B, ALL CHECKS GOOD PN ON/OFF 1134104-1, SN/ON 1032, SN/OFF 673. REMOVED FROM DMR MXC NOTIFIED. 2L72 4T RTA52EU 20030505000822003050500082SO 2003 5 5 SWIA200311887 120030414A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO RT FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07196SW6891 6812 120151 CONTROL FAULT RECEIVED ON OUTBOARD FLAPS. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-53-01 AND 27-53-05. NO LEAKS NOTED. OPS CHECK GOOD. 2L72 4T RTA31SO 20030505000842003050500084EA 2003 5 5 SWIA200311889 120030416A274070607 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07903SW 7425 STAB FAIL MESSAGE RECEIVED ON EICAS. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT. S/N OFF 865. 2L72 4F RTA21EA 20030505000902003050500090NM 2003 5 5 03FDEA00480 120030417A5414 SKIN BOEING727 727200 138407ENM NR 3 NACELLE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE UPPER NACELLE EXTERIOR SKIN HAS 1 DENT APPROXIMATELY 24 INCHES FROM AFT EDGE. INSTALLED FLUSH REPAIR IAW BOEING 727 SRM 54-30-2. 2L73 4F RTA3WE 20030505001002003050500100NM 2003 5 5 PCA0300845 120030412A5730 PANEL BOEING747 747249F 1384849NM RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 RIGHT WING TRAILING EDGE FIXED PNL (DELAMINATION). REPAIRED PER SRM 51-30-02, MM 51-30-02, 57-22-01. 2L74 4F A20WE 20030505001022003050500102NM 2003 5 5 PCA0300847 120030412A5730 PANEL BOEING747 747249F 1384849NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEFT WING OUTBOARD COVE LP PNL DELAMINATION INOP TRAILING EDGE. REPAIRED PER SRM 51-40-12. 2L74 4F A20WE 20030505001062003050500106NM 2003 5 5 03FDEA00209 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 5L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505001162003050500116NM 2003 5 5 DHL2003741530 120030408A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, IN AFT PIT BS 1050 FRAME HAS 3 EACH DENTS IN THE RADIUS BETWEEN STRINGERS 25L-27L. REMOVED FRAME SPLICES IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA APPROX 3 INCHES IAW B-727 SRM 51-40-3. FABRICATED NEW SPLICE DOUBLER FOR FRAME BS 1050 BETWEEN STR 25L AND 27L MAT USED 7075-T6 .063 PO 9911326 DIMENSIONS 18.5 X 4 INCHES IAW B-727 SRM 51-40-3. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED SPLICE DOUBLER AT BS 1050 BETWEEN STR 25L-27L IAW B-727 SRM 51-30-2 AND 51-40-3 FIG 1. 2L73 4F RTA3WE 20030502000062003050200006NM 2003 5 2 USAASB03048 120030401A3297BACR13CG2AB RELAY BOEING737 7374B7 1384702NM MLG FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19426US 24548 BDL - FLT 1087 - AFTER TAKEOFF FROM BDL, CREW REPORTED THE LANDING GEAR LEVER WOULD NOT RETRACT. CREW FOLLOWED QUICK REF HANDBOOK PROCEDURES AND RETURNED TO FIELD AT BDL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. AFTER LANDING, MAINTENANCE ADVISED THAT THE AIRCRAFT IS NOT SWITCHING TO THE AIR MODE. MAINTENANCE REMOVED AND REPLACED THE R276 AIR SENSING RELAY AND THE LANDING GEAR LEVER LATCH SOLENOID (P/N A420-060283-05). OPS CHECK GOOD PER MM. (M) 2L72 4F RTA16WE 20030502000662003050200066WP 2003 5 2 ASAA0380178 120030301A532059360759 SUPPORT ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO BAY SUPPORT ANGLE CORRODED AT FS 1218. REPLACED ANGLE PER SRM 51-30-5 AND 53-14-3. (M) 2L72 4F A6WE 20030502000722003050200072WP 2003 5 2 ASAA0380184 120030302A5320993653429 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, FORWARD CENTER FLOOR PANEL MOUNTING SUPPORT IS CORRODED AT FS 200. REPLACED SUPPORT PER SRM 51-30-5. (M) 2L72 4F A6WE 20030502001192003050200119SO 2003 5 2 SWIA200311873 120030413A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS LEAKING A SWIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM07189SW7608 7520 120048 ON DEPARTURE OUT OF SLC HAD FLAP, ADVANCED SWS AND CONTROL FAULT LIGHTS FLASHING. PERFORMED QRH. DID NOT CLEAR THE PROBLEM. RETURNED TO SLC. FOUND LEFT NACELLE FLAP ACTUATOR LEAKING. INSTALLED NEW ACTUATOR IAW MM 27-50-00. 2L72 4T RTA31SO 20030502001212003050200121SO 2003 5 2 SWIA200311875 120030412A5753 STRUCTURE EMB 120 EMB120ER 3260203SO RT TE FLAPS DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07567SW 120342 SEVERAL LOOSE RIVETS FOUND ON UNDERSIDE OF RT NACELLE FLAP TRAILING EDGE. ALSO UNUSUAL LARGE DRAIN HOLE IN UNDERSIDE AT UPPER CORNER. FOUND DURING LINE INSPECTION. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-02. 2L72 4T RTA31SO 20030502001272003050200127EU 2003 5 2 VTZ2003F00000 120030410A3350 SOCKET JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE LAMP IN THE LIGHT SOCKET. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030502001642003050200164NM 2003 5 2 03FDEA00576 120030422A5311 FRAME BOEING727 727200 138407ENM FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 FRAME UPPER CHORD IS PUNCTURED BS 1070 RBL 24 WL 150. 2L73 4F RTA3WE 20030502001702003050200170NM 2003 5 2 03FDEA00458 120030416A5310 FRAME BOEING727 727200 138407ENM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 CRACK AT LIGHTENING HOLE IN HORIZONTAL FRAME AT BS 1183 RBL 44 WL 194.0. FABRICATED AND INSTALLED FRAME SECTION IAW BOEING 727-200 SRM 51-30-2 PG 2 AND 3 ITEM B AND 51-30-2 PG 8 ITEM D. 2L73 4F RTA3WE 20030502002072003050200207NM 2003 5 2 UPS03M40442 120030315A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE: C, SEAT TRACK AT RBL 75.5 STA 914-946 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK AT RBL 75.5 STA 914-946 AS PER SRM 51-2 1-01 VOL II REV 32 & FOUND EXCEED LIMIT. NEW SEAT TRACK & SPLICES REWORK AS PER SRM 53-70-00 VOL I REV 32 & HOLES PICKED OUT AS PER SRM 51-21-01 VOL 11 REV 32. NEW SEAT TRACK AND SPLICES INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 914-946 RBL 75.5. 2L73 4F RTA22WE 20030505000262003050500026NM 2003 5 5 DHL2003741545 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS 3 DENTS BETWEEN BS 1133 AND 1148 BELOW STR 19R. REMOVED PAINT IAW B-727 MM 51-20-01. DAMAGED AREAS FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA (2 DENTS IN 1 CUTOUT) DIM 1.75 X 1.25 INCH AND 5.5 X 2.5 INCH IAW B-727 SRM 53-30-3 FIG 1. FABBED REPAIR DOUBLER THAT INCORPORATES NR 43433, 43434, 43435, FROM 2024-T3 .063 PO 9912495 DIM 62.5 X 16 INCHES IAW B-727 SRM 53-30-3 FIG 1, 53-30-2 FIG 2. DOUBLER TREATED, PRIMED AND INSTALLED IAW B-727 SRM 51-10-2, 53-30-1 FIG 1, 53-30-2 FIG 2. 2L73 4F RTA3WE 20030505000802003050500080EU 2003 5 5 MALA030238 120030416A6120 TRANSDUCER SAAB SF340 340B 7860101EU PGB OIL FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15438XJ 340B438 DURING FLIGHT 3119, RT PROP OIL PRESSURE FLUCUATED THEN DROPPED TO ZERO INFLIGHT. TEMPERATURE AND LIGHT OPERATED NORMAL. RT PROP OIL PRESSURE FLUCTUATION BETWEEN 0-200 PSI OCCASIONALLY STEADY AT 100 PSI IN THE GREEN ARC. THEN WENT TO PSI AND STAYED. AIR RETURN TO MSP. MAINTENANCE REPLACED RT PGB OIL PSI X-DUCER PER SAAB AMM 79-30-5-4 AND REMOVED AND RE-INSTALLED RT OIL FILTER PGB FOR ACCESS. LEAK AND OPS CHECK GOOD. ALSO OHMED WIRING AT RT INDICATOR TO X-DUCER CHECK GOOD. 2L72 4T RTA52EU 20030505000882003050500088NM 2003 5 5 PCA0300849 120030412A5330 SKIN BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 BS 2200 S40R LEVEL 1 CORROSION. SRM 53-10-01 CLEANUP 51-10-02 REPROTECTED. 2L74 4F A20WE 20030505000912003050500091NM 2003 5 5 03FDEA00481 120030417A3234 HANDLE BOEING727 727100 1384036NM MLG FAILED A FDEAO OTHER O OTHER CLCLIMB 1 SO25124FE 19360 LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. PROCEEDED WITH LANDING GEAR LEVER LATCH FAILED TO RELEASE RED TAB CHECKLIST. AFTER PULLING AND RESETTING SAFETY RELAY/ LEVER LATCH CB, GEAR RAISED NORMALLY. REMOVED AND REPLACED R-91 AND R-93 LANDING GEAR SAFETY RELAYS. ALSO FOUND CONTROL HANDLE LOCKING VLV SOLENOID DIRTY. CLEANED OPS CK LANDING GEAR HANDLE AS PER M/M 32-31-00-5, OPS CHECK GOOD. 2L73 4F RTA3WE 20030505001172003050500117SO 2003 5 5 C2XA03SH109 120030421A531514521713005 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE CENTER FLOORBEAM BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030505001272003050500127NM 2003 5 5 03FDEA00485 120030417A5330 DOUBLER BOEING727 727200 138407ENM FUSELAGE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LOWER FUSELAGE JUST FORWARD OF AIRSTAIR RIGHT SIDE HAS LOOSE DOUBLER. *S/D* FABRICATED REPLACEMENT DOUBLER IAW BOEING 727 SRM 51-51-2 AND 51-30-2 AND 51-20-1. 2L73 4F RTA3WE 20030505001292003050500129NM 2003 5 5 03FDEA00487 120030417A5414 SKIN BOEING727 727200 138407ENM NR 1 NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 1 ENGINE UPPER NACELLE EXTERIOR SKIN HAS A NICK AT BOTTOM OF AFT PIN LATCH CUTOUT. 2L73 4F RTA3WE 20030505001342003050500134EU 2003 5 5 03107302 120030417A33508GS00599705 LAMP JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27302UE 41013 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT EXTERIOR EMERGENCY EXIT LIGHT AND THE CENTER CABIN EMERGENCY EXIT SIGN WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030505001442003050500144NM 2003 5 5 03FDEA00623 120030426A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE (1 EACH) FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69223 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH INBD. FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030505001482003050500148NM 2003 5 5 03FDEA00492 120030417A5420 STRUCTURE BOEING727 727200 138407ENM NR 2 NACELLE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 2 ENGINE RIGHT FORWARD COWLING RAIN GUTTER BENT. REPAIRED NR 2 ENGINE RIGHT HAND COWLING RAIN GUTTER IAW BOEING 727-200 SRM 51-40-01. 2L73 4F RTA3WE 20030505001602003050500160NM 2003 5 5 03FDEA00468 120030417A5754 SKIN BOEING727 727200 138407ENM RT WING DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT WING LEADING EDGE HAS A DENT ABOUT 6 FEET OUTBOARD OF THE FUSELAGE. 2L73 4F RTA3WE 20030505001612003050500161NM 2003 5 5 03FDEA00467 120030417A2750MS9391130ZE4C MOTOR BOEING727 727200 138407ENM ZONE 600 FAILED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25220FE 20934 AFTER T/O FLAP RETRACTION - OUTBOARD T/E FLAPS STAYED AT 5 DEG WHEN FLAPS WERE RETRACTED TO 2 DEGREES. USED ALT FLAP MASTER SWITCH TO RETRACT FLAPS PER QRH PROCEDURE. PERF T/S AND FOUND OUTBOARD FLAP STUCK FROM 5 TO 2, RESET USING ALTERNATE. COULD NOT GET IT STUCK AGAIN BUT THEN WAS VERIFIED THAT THE MOVEMENT FROM 5 UP TO ZERO WAS NOT CONSISTENT; THE TORQUE TUBE WAS MOVING AS IT WAS GRABING. VERIFIED BY-PASS VLV AND FOUND WORKING PROPERLY. REMOVED AND REPLACED FLAP POWER UNIT HYD MOTOR AS PER B727-200 MM 27-51-062-4. RAN SYS SEVERAL TIMES AND NOW IT'S WORKING CONSISTENTLY. ACFT IS OKAY TO FLY. 2L73 4F RTA3WE 20030505001652003050500165NM 2003 5 5 03FDEA00463 120030416A5720 STIFFENER BOEING727 727200 138407ENM LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT WING NR 3 FLAP TRACK MOVEABLE FAIRING I/B FORWARD INTERNAL STIFFENER GOUGED. *S/D* REMOVED AND REPLACED RIB STIFFENER IAW BOEING 727-200 SRM 57-20-03. 2L73 4F RTA3WE 20030505001822003050500182NM 2003 5 5 DHL2003741537 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK. FUSELAGE SKIN BS 472 BELOW STR 17L HAS A DENT OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA DIAMETER .875 INCH IAW B-727 SRM 53-30-3 FIG 1. FAB DOUBLER REPAIR DIAMETER 3.80 INCH FROM MAT 2024-T-3 .050 PO 9912140 AND FILLER DIAMETER .875 INCH FROM 2024 T3 .040 PO 9912380 IAW B-727 SRM 53-30-3 FIG 13 AND 53-30-2 FIG 2. TREATED AND PRIMED DOUBLER REPAIR AND FILLER IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AND FILLER IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030505001832003050500183SO 2003 5 5 C2XA03SH110 120030421A532014524131009 SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE PASSENGER DOOR THRESHOLD SUPPORTS WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030505002532003050500253NM 2003 5 5 03FDEA00521 120030418A5230 PANEL BOEING727 727200 138407ENM CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CARGO DOOR UPPER PANEL DETERIORATED. *S/D* FABRICATED NEW PANEL IAW FED EX SRZ 25-005C. 2L73 4F RTA3WE 20030505002552003050500255NM 2003 5 5 03FDEA00543 120030418A2822 SHROUD BOEING727 727200 138407ENM FUEL SYSTEMS DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FORWARD AUXILARY FUEL TANK SUMP SHROUD HAS DAMAGE. SUMP SHROUD OK FOR SERVICE IAW FED EX EA7-2810-68041. 2L73 4F RTA3WE 20030505002602003050500260NM 2003 5 5 03FDEA00531 120030418A5240 RETAINER BOEING727 727200 138407ENM DOOR SEAL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT FORWARD SERVICE DOOR FUSELAGE FRAME SEAL RETAINER HAS 3 CRACKS AND SEVERAL BENT AREAS FORWARD AND AFT SIDES. REPAIRED SEAL RETAINER IAW BOEING 727-200 SRM 51-40-03. 2L73 4F RTA3WE 20030505002652003050500265NM 2003 5 5 MWEA030182 120030424A216011508801 CONTROLLER BOEING717 717200 1383700NM CABIN TEMP DEFECTIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31902ME 55166 AFTER ENGINE START LEFT COCKPIT TEMPERATURE HIGH AND THEN LEFT PACK OVERHEAT ALERT CAME ON AND OFF AS TEMPERATURE WENT UP AND DOWN. REMOVED AND REPLACED COCKPIT AIR TEMPERATURE CONTROLLER. 2L72 4F TRA6WE 20030502001452003050200145NM 2003 5 2 SWAA030833 120030412A5753113A37007 SKIN BOEING737 7377H4 1384404NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 DURING SCHEDULED A2 CHECK, FOUND LEFT OUTBOARD T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SURFACE. REMOVED AND REPLACED LEFT OUTBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20030502002412003050200241EA 2003 5 2 03101638A 120030411A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 DURING MAINTENANCE INSPECTION, THE RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030502002602003050200260NM 2003 5 2 2003UALA00282 120030315A2760NAS6304 BOLT BOEING747 747422 1384935NM PWA 4056 PW4056 NE AILERON MISSING A UALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP29180UA52398 25224 EXCESSIVE AILERON TRIM, 1.5 UNITS, REQUIRED TO MAINTAIN LEVEL FLIGHT. INVESTIGATION FOUND LEFT INBOARD AILERON POWER CONTROL PACKAGE INPUT CONTROL ROD WAS DETACHED AT ONE END. BOLT, NUT & WASHER ON PCP END OF ROD WERE MISSING AND REPLACED BEFORE RETURN TO SERVICE. NO FURTHER DAMAGE OR MISSING HARDWARE WAS DETECTED. 2L74 4F4 FRTA20WE E24NE 20030502002682003050200268WP 2003 5 2 IXXA0300031O 120030409A3260 PROXIMITY SWITCH DOUG DC8 DC873F 302199FWP MLG OUT OF ADJUST A IXXAO OTHER N FALSE WARNING CLCLIMB 1 SW11606AL894541206 46044 DURING CLIMB FROM KTOL TO KMCO THE CREW RAISED GEAR DOOR AND THE NOT LATCHED LIGHT STAYED ILLUMINATED. GEAR WAS RECYCLED, LEFT LIGHT WENT OUT AND RIGHT LIGHT STAYED ON. MAINTENANCE REMOVED RIGHT MAIN LANDING GEAR DOOR PROXIMITY SWITCH AND BRACKET. FABRICATED AND INSTALLED DOUBLER AND FILLER FOR PROXIMITY SWITCH. THEN SWAPPED PROXIMITY BOXES, REINSTALLED AND OPERATIONALLY CHECKED PROXIMITY SWITCH IN ACCORDANCE WITH DOUGLAS AIRCRAFT MAINTENANCE MANUEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20030502002842003050200284WP 2003 5 2 DHL2003804002 120030413A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP NR 2 MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01804DH 46124 NR 2 SMOKE DETECTOR INOPERATIVE. MEL 26-6-1 DMI 12559 CAT-C PLACARD INSTALLED. REFER TO DMI 12559. NR 2 SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED NR 2 SMOKE DETECTOR AS PER M/M 26-10-5. OPS CHECKED GOOD. THIS CLEARS DMI 12559. 2L74 4F RT4A25 20030505000022003050500002CE 2003 5 5 6022004082003 120030408A3230 SELECTOR VALVE LEAR 60 60LEAR 5170707CE MLG ACTIVATED E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05255FX990 990 220 CAPTAIN SELECTED GEAR UP. GEAR DID NOT RETRACT, GEAR DOORS REMAINED OPEN, AND 3 UNSAFE GEAR LIGHTS ILLUMINATED. CYCLED GEAR 3 TIMES AND SITUATION DID NOT CHANGE. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN GEAR SELECTOR VALVE. OPS CHECK NORMAL. 2L72 4F RTA10CE 20030505000212003050500021NM 2003 5 5 DHL2003741538 120030402A5310 FRAME BOEING727 727200 138407ENM RAM AIR DOOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, A/C BAY AT BS 720 HAS CORROSION AT BOTH LT AND RT SIDE OF RAM AIR DOOR ATTACH FRAME. CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG 1. REMOVED SKIN FOR ACCESS IAW B-727 SRM 51-30-2 AND CUT OUT 2 EACH DAMAGED AREAS DIM 3 INCHES EACH AND FABBED FILLERS FROM BAC 1490-2785 PO 9912243 DIM 3 INCHES EACH AND ANGLE DOUBLERS FROM 7075 T6 .050 PO 9912146 DIM 13 X 3 INCHES EACH IAW B-727 SRM 51-40-3 FIG 1 AND 53-50-1 FIG 2. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED IAW B-727 SRM 51-40-3 FIG 1. SKIN REINSTALLED IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030505000752003050500075EU 2003 5 5 AWXA200300401 120030405A5315D5347217220390 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292, FORWARD AND AFT SIDE OF FR 67. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-1292, FORWARD AND AFT SIDE OF FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 39-41 FIG 18, SRM 51-72-11 PG 1-2. 2L72 4F RTA28NM 20030505001792003050500179EA 2003 5 5 03109642 120030419A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY FLOOR TRACK LIGHT STRIP WAS FOUND TO BE DAMAGED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505001902003050500190NM 2003 5 5 EIA2003069 120030418A5230 STRUCTURE BOEING747 747273C 1384896NM CARGO DOOR LATCHCORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 NR 3L NOSE CARGO DOOR LATCH BOLT HOLE NR 2 HAS CORROSION. REAMED HOLE NR 2 FROM 0.623 TO 0.733 PER EO 53-747-1633-01 REV-C, FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED. 2L74 4F A20WE 20030505001952003050500195SO 2003 5 5 C2XA03IA041 120030421A27613604401003 ACTUATOR EMB 145 EMB145LR 3260212SO SPOILER LEAKING A C2XAO OTHER K FLUID LOSS DEDESCENT 1 SW2713914 145430 IAH- FLIGHT 2751, THE CREW DECLARED EMERGENCY DUE TO NR 2 HYDRAULIC LOW QUANTITY AND LANDED AT IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 2 GROUND SPOILER ACTUATOR, SERVICED THE HYDRAULIC SYSTEM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030505002312003050500231WP 2003 5 5 UPS03840447 120030412A5754 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, RT WING L/E UPPER RIB IS CRACKED AT FASTENER END AT XFS 826.750. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED STACK ANGLE DOUBLER REPAIR IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030505002542003050500254EA 2003 5 5 COMA0360193 120030414A2913MPEV0122B PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01973CA14593 7146 FLIGHT 5026 GEAR DISAGREE WARNING. REPLACED HYDRAULIC ACMP NR 3B. 2L72 4F RTA21EA 20030506000492003050600049WP 2003 5 6 UPS03840453 120030414A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP CENTER SUBFLOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C1 STA 960-980 AT LBL 66 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-1-0, 53-2-0 FIG 1F, 51-1-21. 2L74 4F RT4A25 20030506000642003050600064NM 2003 5 6 03FDEA00647 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) ACTUATOR FITTING (2 EACH) BORE HOLE FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69242 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030506000672003050600067WP 2003 5 6 UPS03840463 120030405A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD WEB FOWARD SIDE CRACKED AT RBL 26 TO 28 AND RBL 34 TO 38 ABOVE FLOOR LINE. CUT OUT CRACKED AREA IAW DC8 SRM 53-2-5. REMOVED 5772638-48 ATTACK ANGLE, FABBED -11, -19, -9, & 25-27 DOUBLERS IAW DC8 SRM 53-2-5 & DAC DWG SR08530007. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED -9,- 11,-19 FILLERS & 25-27 DOULBERS -30 ANGLE IAW DC8 SRM 51-1-20D. INSTA LLED HAT CHANNEL, GILLINER ATTACH ANGLE IAW DC8 SRM 51-1-21 & 51-3-0. 2L74 4F RT4A25 20030506000822003050600082NM 2003 5 6 03FDEA00581 120030423A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FLOORBEAM UPPER FLANGE BS 328, LBL 33 TO LBL 23, WL 208. 2L73 4F RTA3WE 20030506000852003050600085NM 2003 5 6 AWXA200300432 120030413A572069475423 ANGLE BOEING737 73733A 1384673NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND ON THE RT WING INBOARD TRAILING EDGE UPPER FIXED PANEL LOWER SUPPORT ANGLE WBL 72.25. MAINTENANCE REMOVED CRACKED LOWER SUPPORT ANGLE AT WBL 72.25; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 26, & 45. 2L72 4F RTA16WE 20030506000882003050600088NM 2003 5 6 03FDEA00501 120030417A2120 DUCT BOEING727 727200 138407ENM AIR CONDITIONINGCRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 OVERHEAD CABIN AIR CONDITIONING DUCT STA 450 TO 670 HAS NUMEROUS AREAS OF DELAMINATION AND CRACKING. *S/D* REPAIRED OVERHEAD A/C DUCT IAW BOEING CMM 25-00-67. 2L73 4F RTA3WE 20030506000892003050600089NM 2003 5 6 03FDEA00610 120030419A5740 FITTING DOUG MD11 MD11 3023602NM RIGHT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RIGHT WING FOUND L/E NR 16 TRACK INBOARD SUPPORTING FITTING CRACKED. RT WING LEADING EDGE NR 16 TRACK INBOARD SUPPORTING FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II AND DWG ARB2850. 2L73 4F RTA22WE 20030506001002003050600100EA 2003 5 6 03113670 120030423A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27670BR 7561 DURING MAINTENANCE INSPECTION, THE LT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030506001092003050600109NM 2003 5 6 375PA0014 120030427A3350 BULB BOEING737 73739A 138447PNM EMERGENCY LIGHT BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 THREE EACH BULBS NOT WORKING ON EMERGENCY EXIT LIGHT TEST ON SERVICE CHECK. RECONNECTED WIRING AT SOCKETS. ALL LIGHTS OPS CHECK GOOD PER MM 33-50-00. 2L72 4F RTA16WE 20030506001212003050600121NM 2003 5 6 CALA0300229 120030429A26124739551 MODULE BOEING737 737924 13848A1NM FIRE DETECTION FALSE INDICATIONA CALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0979402 30119 AIRCRAFT EN ROUTE FROM IAH TO OAK DIVERTED TO MAF DUE TO FORWARD CARGO FIRE WARNING. AIRCRAFT INSPECTED WITH NO EVIDENCE OF FIRE. FIRE WARNING SYSTEM CHECKED AND DISCHARGED FIRE BOTTLE REPLACED. 2L74 4F RTA16WE 20030505000222003050500022NM 2003 5 5 MWEA030176 120030416A801059382541 DUCT DOUG MD88 MD88 3023688NM ENGINE START DEFECTIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31601ME 49762 LEFT START VALVE WILL NOT OPEN. REMOVED AND REPLACED LEFT ENGINE PNEUMATIC STARTER DUCT. 2L72 4F RTA6WE 20030505000392003050500039WP 2003 5 5 ARWA20030403 120030412A3231 ARM DOUG DC8 DC862F 3021972WP NLG DOOR BROKEN A ARWAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO19791AL 46150 AFTER GEAR RETRACTION NOISE AND VIBRATION FROM NOSE GEAR AREA. POST FLIGHT INSPECTION FOUND GEAR DOOR ARM BROKEN WITH DAMAGE TO FUSELAGE AT DOOR HINGE AREA. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER REPAIR IAW DC8 SRM 53-2-1 FIG 7 PAGE 111. REMOVED AND REPLACED ROD ON NOSE LANDING GEAR (NLG) FIX DOOR LT SIDE IAW DC8 MM 32-30-0 PAGE 201. 2L74 4F 4A25 20030505001012003050500101NM 2003 5 5 PCA0300846 120030412A5730 PANEL BOEING747 747249F 1384849NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEFT WING TRAILING EDGE FIX PNL DELAMINATION. REPAIRED PER SRM 51-30-02 MM 51-30-02, 57-22-01. 2L74 4F A20WE 20030505001452003050500145NM 2003 5 5 03FDEA00622 120030426A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING FOUND OUTBOARD FLAP, INBOARD HINGE WING SIDE WITH PIVOT HOLE LOCATION CORRODED. CORROSION ON RT WING, OUTBOARD FLAP, INBOARD HINGE WING SIDE, PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-08, FIG.401. 2L73 4F RTA22WE 20030505001532003050500153NM 2003 5 5 03FDEA00497 120030417A5313 STRINGER BOEING727 727200 138407ENM CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FORWARD CARGO PIT HAS 1 INCH CRACK AT BS 520 STRINGER 27R . *S/D* REPAIRED IAW BOEING 727-200 SRM 51-40-3. 2L73 4F RTA3WE 20030505001592003050500159NM 2003 5 5 03FDEA00469 120030417A5321 FLOOR PANEL BOEING727 727200 138407ENM LOWER CARGO DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 A .75 X 3.5 INCH HOLE IN FLOOR OF AFT LOWER CARGO COMPARTMENT STATION 1020. 2L73 4F RTA3WE 20030505001782003050500178NM 2003 5 5 03109406 120030419A3397 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27406FJ 3156 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE FROM SEAT ROW 4 THROUGH 6. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030505001972003050500197EA 2003 5 5 03105621 120030415A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE INVERTER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030505002012003050500201NM 2003 5 5 UPS03M40434 120030320A5347S492914770T5T65 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT LBL 8.5 BETWEEN 879-899 FOUND CORRODED. CORROSION REMOVED AT STA 879-899 LBL 8.5 & FOUND EXCEED LIMIT AS PER SRM 53-70-00 VOL I REV 32 & 51-21-01 VOL II REV 32. NEW SEAT TRACK & SPLICE FITTING REWORK & HOLES PICKOUT AS PER SRM 53-70-00 VOL I REV 32, PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK & SPLICE FITTING INSTALLED AS PER SRM 53-70-00 VOL I REV 32 AT STA 879-899 AT LBL 8.5. 2L73 4F RTA22WE 20030505002062003050500206NM 2003 5 5 03FDEA00509 120030417A5330 PANEL BOEING727 727200 138407ENM FUSELAGE BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE PANEL 3354 FORWARD INBOARD CORNER BROKEN. *S/D* REPAIRED IAW BOEING 727-200 SRM 51-40-09. 2L73 4F RTA3WE 20030505002092003050500209NM 2003 5 5 03FDEA00506 120030417A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT FLOOR SUPPORT BETWEEN STA 720 AND STA 720D HAS NUMEROUS ARES OF CORROSION. *S/D* REMOVED AND REPLACED FLOOR SUPPORT IAW BOEING 727-200 SRM 51-30-02. 2L73 4F RTA3WE 20030505002112003050500211NM 2003 5 5 03FDEA00505 120030417A5320 RETAINER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CARGO DOOR FUSELAGE FRAME SEAL RETAINER HAS A CRACK AT UPPER AFT SIDE. *S/D* INSTALLED DOUBLER IAW BOEING 727-200 SRM 51-40-3. 2L73 4F RTA3WE 20030505002492003050500249NM 2003 5 5 CALA0300202 120030418A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN WHERE COUNTER BALANCE CABLE EXITS DOOR. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER AND STRAP WERE INSTALLED IAW ECRA 5232-01025. 2L72 4F RTA16WE 20030505002692003050500269GL 2003 5 5 GLBA2003049 320030418A6140503890571 TACH GENERATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL LT PROPELLER FLUCTUATES A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM0394GL 24190 UE94 LEFT PROP GAUGE FLUCUATES. REMOVED AND REPLACED LEFT TACK GEN. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20030506000202003050600020NM 2003 5 6 03FDEA00558 120030421A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-111-01) ON SKIN BS 720A LBL 2 WL 148. 2L73 4F RTA3WE 20030506000252003050600025NM 2003 5 6 03FDEA00528 120030418A5753 STIFFENER BOEING727 727200 138407ENM LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT WING NR 3 FLAP TRACK MOVABLE FAIRING INBOARD FORWARD INTERNAL STIFFENER GOUGED. REMOVED AND REPLACED RIB STIFFENER IAW BOEING 727-200 SRM 57-20-03. 2L73 4F RTA3WE 20030506000422003050600042NM 2003 5 6 03FDEA00652 120030429A3412403024 INDICATOR BOEING727 727200 138407ENM TAT FAILED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25236FE 21330 TAT INDICATOR INTERMITTANT. INDICATOR FAILED ON CLIMBOUT WITH OFF FLAG CYCLING FOR 30 SEC. THEN FAILED WITH SOLID OFF FLAG FOR 60 MIN. INDICATOR CAME BACK ON DURING APPROACH. REMOVED AND REPLACED TAT INDICATOR & OPS CHECKED PER 727-200 MM 34-13-000-5. ALL INDICATIONS NORMAL. 2L73 4F RTA3WE 20030506001302003050600130EU 2003 5 6 AWXA200300424 120030419A5313D53480047200 STRINGER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON STRINGER 31 RT AT FR 65. MAINTENANCE REMOVED TREATED CORROSION ON STRINGER 31 RT AT FR 65; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW A320 SRM 53-00-13 PG 207-209, & 211-213. 2L72 4F RTA28NM 20030506001312003050600131EU 2003 5 6 AWXA200300425 120030405A5350D5323022620000 PANEL AIRBUS320 A320232 3930326EU WING TO BODY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON WING TO BODY FAIRING CLOSING PLATE AT FR 34, LBL 64. MAINTENANCE REMOVED DAMAGED CLOSING PLATE AT FR 34, LBL 64; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 21-22 AND SRM 51-42-11 PG 9-10 & 12. 2L72 4F RTA28NM 20030506001342003050600134WP 2003 5 6 MEX2003134 120030412A801138334221 STARTER DOUG DC9 DC982 3022082WP PWA JT8 JT8D15 52051NE RT ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW231003X282397489 48067 AIRCRAFT RETURNED TO PLATFORM, DURING RIGHT ENGINE STARTING WERE NOT N1, N2 AND OIL PRESSURE INDICATIONS. DURING REVISION WAS DETECTED THAT SHAFT COUPLING STARTER WAS BROKEN. IT WAS REPLACED IAW MM, TESTS CORRECT. 2L72 4F4 F A6WE E2EA 20030506001382003050600138WP 2003 5 6 GTIA030189 120030223A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 160 TO 200 RBL 44 INCHES SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABBED AND INSTALLED NEW FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030506001442003050600144CE 2003 5 6 B4Z2003F00000 120030415A3110AN54A BOLT BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE LT PEDESTAL MISSING E B4ZAO OTHER O OTHER NRNOT REPORTED 1 SO11685BC215 FL355 ON TAKEOFF ROLL, BOTH ENGINES WOULD NOT DEVELOP FULL POWER. AIRCRAFT TAXIED BACK TO RAMP. FURTHER INSPECTION BY TECH FOUND BOLT PN AN5-4A FROM LEFT SIDE OF PEDESTAL LYING ON FLOOR AFTER REMOVING LEFT PEDESTAL SIDE COVER. (ATTACHMENT) 2L72 4T4 TRTA24CE E4EA 20030506001542003050600154CE 2003 5 6 JGV2003F00001 120030327A551062321809 SCISSORS CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP HORIZONTAL STAB DAMAGED B JGVRO OTHER O OTHER NRNOT REPORTED 1 CE0977LX 6507051 WHILE PERFORMING, PHASE 5 INSPECTION, ITEM CODE: D274000, TASK: HORIZONTAL STABILIZER SCISSORS FREE PLAY CHECK, THE FREE PLAY WAS FOUND OUT OF LIMITS. THE UPPER AND LOWER SCISSORS( PN 62321809 & 10) WERE REMOVED TO REPLACE THE BUSHINGS IN EACH ASSEMBLY. THE SCISSORS WERE REINSTALLED AND SUBSEQUENT MOVEMENTS OF THE HORIZONTAL STABILIZER TRIM ACTUATOR CAUSED DAMAGE TO THE UPPER AND LOWER SCISSORS AT CENTER PIVOT BOLT AREA. IT WAS DETERMINED THAT THE LOWER SCISSORS ASSEMBLY HAD BEEN INSTALLED UPSIDE DOWN. MM DOES NOT CONTAIN ANY NOTES OR WARNINGS THAT TELL THE MECHANIC THAT THE SCISSORS ASSEMBLY MUST BE ORIENTED PROPERLY TO PREVENT DAMAGE TO THE ASSEMBLY. 2L72 4F4 F A9NM E6WE 20030506001552003050600155SO 2003 5 6 EWG2003F00000 220030415A8530TISN71 CYLINDER CESSNA414 414 2075908CE CONT O520 TSIO520NB 17040SO NR 2 SEPARATED E EWGAO OTHER O OTHER NRNOT REPORTED 1 SO05716P 196 4140944 521098 PILOT REPORTS THE INABILITY TO THROTTLE BACK THE LEFT ENGINE. UPON INSPECTION OF THE LEFT ENGINE, NOTED THE NR 2 RAM CYLINDER (PN TISN71.2BCA221) HAD SEPERATED. THE CYLINDER HAD SEPARATED AT THE TOP OF THE BAREL WHERE THE HEAD AND COMBUSTION CHAMBER MEETS. NO DAMAGE TO THE AIRCRAFT WAS NOTED AT THE TIME OF INSPECTION. CYLINDER WAS REMOVED AND REPLACED AND THE AIRCRAFT/ENGINE RETURNED TO SERVICE. CAUSE OF DEFECT UNKNOWN. 1L72 3O3 ORTA7CE E8CE 20030506001602003050600160WP 2003 5 6 ASAA0380234 120030307A55325910256517 SKIN DOUG DC9 DC982 3022082WP VERTICAL STAB GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RUDDER LEADING EDGE UPPER SKIN GOUGED AND CREASED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM. (M) 2L72 4F A6WE 20030506001692003050600169WP 2003 5 6 ASAA0380242 120030307A57545937551 CAP DOUG DC9 DC982 3022082WP RT WING LE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE END CAP GOUGED. BLENDED, PERFORMED WELD REPAIR PER EA 5740-01344. (M) 2L72 4F A6WE 20030506001862003050600186WP 2003 5 6 ASAA0380274 120030322A56105613217520 WINDOW DOUG DC9 DC983 3022083WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS30705 53448 LAX - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE DIFFICULT TO OPEN. LUBRICATED WINDOW. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030506001902003050600190WP 2003 5 6 ASAA0380217 120030307A5320995107031 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND TAIL CONE RELEASE PANEL SUPPORT ARM CRACKED. APPLIED FIBERGLASS OVERLAY TO SUPPORT ARM PER SRM. (M) 2L72 4F A6WE 20030506002102003050600210WP 2003 5 6 ASAA0380236 120030307A5320591014199 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FORWARD CARGO DOOR FORWARD ANGLE IN CENTER FORWARD EDGE IS CRACKED. REMOVED AND REPLACED DAMAGED ANGLE PER SRM. (M) 2L72 4F A6WE 20030506002122003050600212WP 2003 5 6 ASAA0380239 120030307A5313593643443 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND LONGERON AND 29R AFT OF STATION 579 HAVE CORROSION AROUND FASTENERS. REMOVED DAMAGED DOUBLER. INSTALLED NEW REPAIR DOUBLER AND STRAP PER ASA EA 5330-01195. (M) 2L72 4F A6WE 20030506002202003050600220WP 2003 5 6 ASAA0380203 120030304A53219957828 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FLOOR PANEL IS CORRODED AT FS 148-200. REPLACED PANEL PER SRM 53-01. (M) 2L72 4F A6WE 20030506002212003050600221WP 2003 5 6 ASAA0380204 120030304A53202936534139 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200. REPLACED SUPPORT PER SRM 53-01. (M) 2L72 4F A6WE 20030506002252003050600225WP 2003 5 6 ASAA0380198 120030303A5310991556531 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, AFT PASSENGER DOOR LOWER FRAME HAS GOUGES. REPLACED FRAME PER SRM 52-01. (M) 2L72 4F A6WE 20030506002302003050600230WP 2003 5 6 ASAA0380210 120030304A53205910369501 CHANNEL DOUG DC9 DC982 3022082WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND APU SHROUD RIGHT AFT HAT CHANNEL FRETTING AT FS 1361-1390. REMOVED DAMAGED SECTION AND REPAIRED WITH FILLER AND DOUBLER PER SRM 51-70-5. (M) 2L72 4F A6WE 20030506002402003050600240WP 2003 5 6 ASAA0380259 120030309A5320593064413 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OAK - FOUND DURING C-CHECK, FLOOR SUPPORT CORRODED BETWEEN INBOARD AND OUTBOARD SEAT TRACK AT FS 1155 ON RIGHT SIDE. REPLACED SUPPORT PER SRM 51-10-4 AND 51-30-5. (M) 2L72 4F RTA6WE 20030506002412003050600241NM 2003 5 6 ASAA0240125 120030310A33978100022602 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01772AS 25105 SEA - DURING SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROW 17. REATTACHED WIRE, OPERATIONAL CHECKED GOOD, RELEASED. (M) 2L72 4F RTA16WE 20030505001502003050500150NM 2003 5 5 03FDEA00494 120030417A5414 SKIN BOEING727 727200 138407ENM NR 2 NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 2 ENGINE FORWARD COWLING LOWER AFT CORNER INTERIOR SKIN CHAFED. *S/D* REPAIRED SKIN IAW BOEING 727-200 SRM 54-30-01. 2L73 4F RTA3WE 20030505001932003050500193EA 2003 5 5 COMA0360207 120030420A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01472CA2030 7667 FLIGHT 5196 LANDING GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030505002162003050500216NM 2003 5 5 DHL2003749005 120030422A3260 WARNING LIGHT BOEING727 727200 138407ENM MLG MALFUNCTIONED A DHLAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01749DH 22013 ON FINAL APPROACH LANDING GEAR EXTENDED LIGHTS INDICATION 3 MAIN GREEN, AND 3 RED MAIN/NOSE LIGHTS. GEAR RECYCLED, SHOWED 3 MAIN GREEN NORMAL LANDING. INSPECTED NOSE & MLG UP LOCK & DOWN LOCK SWITCHES, LANDING GEAR ACTUATION UNIT, AND LIGHT ON WHEELS SWITCH & LINKAGE. NO DEFECTS NOTED. LANDING GEAR INDICATION SYSTEM OPS CHECKED NORMAL AT THIS TIME PER M/M 32-61-00. 2L73 4F RTA3WE 20030505002442003050500244EA 2003 5 5 COMA0360202 120030416A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01964CA 7129 FLIGHT 5715 RT THRUST REVERSER UNLOCK CAUTION MESSAGE. SECURED T/R AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030505002732003050500273NE 2003 5 5 61771 220030404A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE NR 2 FLUCTUATES A UHLAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 GL17138SD 138 DURING T/O ROLL OF FLT 4476 TTN-BED RIGHT ENGINE TORQUE HAD LARGE FLUCTUATIONS. INITIAL TROUBLE SHOOTING FOUND IT TO BE A FAULT IN CTOT SYSTEM. CTOT SYSTEM MEL'D. 2L72 4T4 TRTA52EU E8NE 20030506000572003050600057NM 2003 5 6 03FDEA00651 120030429A3260 SWITCH BOEING727 727100 1384036NM ZONE 700 FAILED A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25188FE 19081 UPON LOWERING GEAR FOR LANDING, GREEN GEAR NOSE LIGHT DID NOT ILLUMINATE (TESTED OK). NO AMBER GEAR LIGHT. CYCLED GEAR AND NOSE GEAR LIGHT ILLUMINATED ON SECOND EXTENSION OF GEAR. REMOVED AND REPLACED NOSE LANDING GEAR LOCK SWITCH PER 727 MM 32-61-021-4. PERFORMED ADJUSTMENT/TEST PER 727 MM 32-61-021-5. OPS CHECKED NORMAL. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20030506000722003050600072WP 2003 5 6 03FDEA00571 120030421A5320 ANGLE DOUG DC10 DC1030 3023501WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 995 AFT CARGO AFT WALL LWR SUPPORT ANGLE IS CORRODED LBL 25 TO LBL 60 STA 1967. CLOSING ACTION ON 04/16/03 ON N/R 00995. REMOVED CORROSION, FOUND ANGLE TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED ANGLE IAW SRM 51-35-01. FAB ANGLE ON TRAVELER T2/326614, INSTALLED IAW SRM 51-31-01. 2L73 4F A22WE 20030506000932003050600093NM 2003 5 6 03FDEA00617 120030423A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR FITTING HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69216 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030506001672003050600167EA 2003 5 6 A6WA200340039 120030402A2910 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM CHAFED A A6WAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL31422AW 7341 HYDRAULIC 2 LOW PRESSURE MESSAGE ON EICAS, NO QUANTITY NOTED. REMOVED AND REPLACED NR 2 EDP (HYD) AND CHAFED LINE IN PYLON (HYD). OPS AND LEAK CHECK GOOD. (M) 2L72 4F RTA21EA 20030507000112003050700011EU 2003 5 7 CA030407005 120030404A324223203500 ROTOR PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL BRAKE ASSY BROKEN W O OTHER O OTHER ININSP/MAINT 1 CA (CAN) DUE TO PREVIOUS BRAKE FAILURES, WE NOW DISSASSEMBLE AND INSPECT THE BRAKE ASSY AT 1000 CYCLES.ON INSPECTION OF THIS ASSY. WE FOUND OUTER ROTOR DISK BROKEN AT RELIEF HOLES. WEAR PINS INDICATE HALF LIFEON ASSY. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030507000522003050700052NM 2003 5 7 AUS20030351 120030322A8011GRTA3966 SEAL HONEYWELL BOEING737 7377BX 13844D2NM GE CFM56 CFM567B24 NE ENGINE STARTER FAILED W O OTHER EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS GRTA3966 (AUS) NR 1 ENGINE STARTER FAILED. OIL COMING FROM STARTER EXHAUST. INVESTIGATION FOUND TURBINE OIL SEAL LEAKING. 2L72 4F4 FRTA16WE E00055EN 20030507000592003050700059SO 2003 5 7 AUS20030358 120030206A760389307000 ROD END PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA HARTZLHCC2Y HCC2YK2 GL POWER LEVER FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT ENGINE GOVERNOR RODEND FAILED UNDER LIGHT TORQUE DURING INSTALLATION. 1L72 3O3 O A7SO 1E10 5 CP920 20030507000602003050700060CE 2003 5 7 AUS20030359 120030220A3230128050981 TUBE CESSNA210 210L 2073448CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL MLG LOOSE W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) LANDING GEAR DOWN LINE FITTING LOOSE AT FIREWALL END. 1H71 3O3 O 3A21 E5CE 5 CP47GL 20030507000652003050700065WP 2003 5 7 CA030410006 220030409A72308943825 TUBE SWRNGNSA227 SA227* SW GARRTTTPE331TPE33111U 01514WP MCAULY4HFR344HFR34C652 NE ENGINE P3 FRACTURED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CA (CAN) LH AND RH ENGINE WOULD NOT DEVELOP TARGET TORQUE OF THE DAY.LH ENGINE HAD A BROKEN P3 TUBE ALLOWING EXCESSIVE COMPRESSOR LEAK.RH ENGINE HAD POWER PERFORMANCE PROBLEM DUE TO TEMPERATURE OF THE DAY.RH ENGINE WAS REPLACED AND P3 TUBE WAS REPLACED ON LH ENGINE. NOTE: TIMES ON P3 TUBE ARE NOT TRACKED 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20030507000762003050700076EU 2003 5 7 CA030411005 120030331A2913704A33690004 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HYDRAULIC PUMP CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING ROUTINE INSPECTION AME DISCOVERED HYDRAULIC PUMP BELT TO BE CRACKED (APPROXIMATELY HALF WIDTH). BELT WAS REPLACED AND A/C RETURNED TO SERVICE. 1G71 3U3 UNCH9EU E19EU 20030507000772003050700077GL 2003 5 7 CA030411006 120030408A2720SL24P CONTROL CABLE DIAMONDA20 DA20A1 2990000GL ROTAX 912 ROTAX912F3 EU RUDDER FAILED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) WHILE INVESTIGATING A PREVIOUS RUDDER CABLE FAILURE IT WAS DISCOVERED THAT THE OVAL SLEEVE ON THE LT OUTBOARD RUDDER CABLE, AT THE RUDDER PEDAL END, WAS IMPROPERLY SWAGED. NONE OF THE THREE COMPRESSIONS WERE SUFFICIENT. MAINTENANCE RECORDS DID NOT INDICATE THAT THE CABLE HAD BEEN REPLACED SINCE NEW. 1L71 3O3 ONTTA4CH E00051EN 20030507000882003050700088SW 2003 5 7 AUS20030376 120030313A3213NAS517416 SCREW SWRNGNSA227 SA227* SW MLG STRUT LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR TRUNNION FITTING SCREWS WORKING. FOUND WHEN LT MAIN LANDING GEAR STRUT WAS REMOVED FOR ACCESS. 2L72 4T RTA5SW 20030507000922003050700092NE 2003 5 7 CA030415001 220030409A8530 NUT DOUG A26 A26BSHIELDS 3020504WP PWA R2800 R280079 52026NE NR 2 CYLINDER LOOSE W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) AFTER TAKEOFF OIL/SMOKE WAS NOTICED COMING FROM RT ENGINE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. ROCKER JAM NUT FOUND BACKED OFF ON CYLINDER NR 2 INTAKE. 2M72 4R4 R L34 5E8 20030507000942003050700094NM 2003 5 7 AUS20030377 120030328A291366087 PUMP BOEING737 73776N 13844CHNM GE CFM56 CFM567B24 NE HYDRAULIC FAILED W O OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 AUS (AUS) ENGINE DRIVEN HYDRAULIC PUMP FAILED. CASE DRAIN FILTERCONTAMINATED. 2L72 4F4 FRTA16WE E00055EN 20030507000982003050700098EU 2003 5 7 AUS20030381 120030401A5711NOTKNOWN SPAR CAP FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING FORWARD LOWER SPAR CAP CONTAINED TWO AREAS OF EXFOLIATION CORROSION LOCATED BETWEEN RIB 12375 AND RIB 12975. AREAS OF CORROSION APPROXIMATELY 50.8MM BY 25.4MM (2IN BY 1IN) AND 76.2MMBY 25.4MM (3IN BY 1IN). 2L72 4F4 FRT E25NE 20030507001212003050700121NM 2003 5 7 CA030418001 120030415A3297 CONNECTOR BOEING737 737275C NM PWA JT8 JT8D9A 52048NE MLG INDICATOR DAMAGED W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) FLT CREW REPORTED NLG GREEN DOWNLOCK INDICATION WOULD NOT EXTINGUISH WHEN MLG SELECTED UP. MLG DID RETRACT. GREEN LIGHT WOULD NOT EXTINGUISH. MLG CYCLED 3 TIMES, NO JOY . RETURNED TO BASE. ABLE TO DUPLICATE FAULT ON GROUND. NLG DOWNLOCK SENSOR REPLACED, NO JOY. MLG ACCESSORY UNIT REPLACED, ALSO NO JOY. CONDUIT LEADING FROM DOWNLOCK SENSOR TO MLG ACCESSORY UNIT MOVED WHICH EXTINGUISHED LIGHT. CONDUIT & WIRING REMOVED. WIRING INSPECTED. UNABLE TO FIND FAULT WITH WIRING. WIRING & CONDUIT WERE REINSTALLED, NEW CONNECTORS FOR TERMINAL BLOCK. MLG SWUNG SEVERAL TIMES WITHOUT FAULT. SYS WIRING INSPECTED SEVERAL MORE TIMES & TESTED, NO PROBLEMS FOUND. 2L72 4F4 F A16WE E2EA 20030506000132003050600013WP 2003 5 6 03FDEA00537 120030418A5320 CHANNEL DOUG DC10 DC1030 3023501WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 FWD CARGO PIT CEILING PANEL HAT TRACK CRACKED AT FS 970 RBL 48. CLOSING ACTION ON 04/14/03. HAT TRACK REMOVED IAW SRM 53-31-01. NEW HAT TRACK FAB ON TRAVELER T2/325808. NEW HAT INSTALLED IAW SRM 51-31-01. 2L73 4F A22WE 20030506000262003050600026NM 2003 5 6 03FDEA00527 120030418A5413 LONGERON BOEING727 727200 138407ENM NR 3 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE NACELLE INBOARD SKIN CHAFED AND CRACKED. REMOVED AND REPLACED LONGERON IAW BOEING 727-200 SRM 51-30-02. 2L73 4F RTA3WE 20030506000402003050600040NM 2003 5 6 03FDEA00654 120030430A2612 CONNECTOR BOEING727 727200 138407ENM NR 3 ENGINE LOOSE A FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25484FE 21466 ON DESCENT THE NR 3 ENGINE FIRE DETECTION WARNING LIGHT ILLUMINATED. UPON LANDING, THE LIGHT FLICKERED AND REMAINED ON. TROUBLESHOT IAW MM 26-11-000-1 FOUND CONNECTOR TO THE RESPONDER IN THE FWD SECTION LOOSE. INSPECTED CONNECTOR AND ALL OTHER COMPONENTS IN THE SYSTEM. TIGHTENED, REINSTALLED CONNECTOR AND OPS CHECK SYS, ALL TEST NORM IAW MM 26-11-000- 5, NO HISTORY 90 DAYS. 2L73 4F RTA3WE 20030506002462003050600246WP 2003 5 6 ASAA0380230 120030307A52109955763U11 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND L1 DOOR HANDLE SUPPORT BOX AFT INTERCOSTAL CRACKED. REPLACED DAMAGED INTERCOSTAL PER SRM. (M) 2L72 4F A6WE 20030505001702003050500170NM 2003 5 5 SWAA030842 120030414A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030506000282003050600028EU 2003 5 6 DHL2003364008 120030417A2751 CONNECTOR AIRBUS300 A300B4203 3930306EU FLAP SYSTEM DIRTY A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01364DH 141 FLAP INDICATOR INDICATED 0 WITH FLAP HANDLE AT 15. T/S PER FIM 27-50-00. CK'D CONTACTS ON FLAP CONTROL UNIT IAW MM 27-52-11 AND TESTED PER MM 27-55-00. INSPECTED & CLEANED FLAP POSITION INDICATOR CONNECTOR. SYS OPS CK'D OK PER MM 27-55-00. 2L72 4F RTA35EU 20030506000842003050600084NM 2003 5 6 249TR0017 120030422A3350 BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 DURING PRE-AMP CHECK, FOUND L1 & R1 EMERGENCY SLIDE LIGHTS INOP. RELAMPED L1 DOOR SLIDE LIGHT, REPLACED R1 DOOR SLIDE LIGHT ASSEMBLY AND REPLACED TWO BATTERY PACKS PER MM 33-51-81. 2L72 4F RTA16WE 20030506001172003050600117NM 2003 5 6 03FDEA00519 120030418A5320 PANEL BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CARGO SIDEWALL PANEL STA 560 TO 748 DETERIORATED. 2L73 4F RTA3WE 20030506001282003050600128NM 2003 5 6 AWXA200300422 120030416A532069353521 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN AFT CARGO COMPARTMENT AT THE FORWARD SIDE OF BS 887, STR 22 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 887, STR 22 RT, FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 10-11, & 38 FIG 8 AND SRM 51-40-05 PG 1. 2L72 4F RTA16WE 20030507000382003050700038EU 2003 5 7 CA030409012 120030327A2400911TS08Y CONTROL UNIT UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) SMOKE IN CABIN, LANDED, CAUTION LIGHTS ON, VEMD SCREENS WENT OUT, NO ELECTRICAL POWER. 1G72 3U3 UNCR0001RD E34NE 20030507000572003050700057EU 2003 5 7 AUS20030356 120030321A21709599020143 SEPARATOR PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL HUMIDITY CONTROLCONTAMINATED W O OTHER J WARNING INDICATION DEDESCENT 1 AUS 1831 (AUS) WATER SEPARATOR BAG CLOGGED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030507000692003050700069CE 2003 5 7 AUS20030361 120030305A3213CM268932 CLIP CESSNA402 402A 207590MCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL MLG FAULTY W O OTHER O OTHER LDLANDING 1 AUS (AUS) LH MAIN LANDING GEAR OLEO CIRCLIP FAILED. LANDING GEAR OLEO EXTENDED BEYOND LIMITS AND WAS ONLY HELD TOGETHER BY THE TORQUE LINKS. DAMAGE CAUSED TO RETRACTION MECHANISM, LANDING GEAR ANDLANDING GEAR DOOR. WHEN SELECTED DOWN, GEAR EXTENDED AND LOCKED OK. RH MAIN LANDING GEAR OLEO CIRCLIP WAS INSPECTED AND SPRINGTENSION WAS FOUND TO HAVE DETERIORATED. 1L72 3O3 O A7CE E8CE 5 CP22EA 20030507000992003050700099 2003 5 7 AUS20030382 420030317A256531841101 SLIDE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE ESCAPE SLIDE FAULTY W K NONE L NO TEST ININSP/MAINT 1 AUS (AUS) ESCAPE SLIDE FAULTY. SLIDE DEPLOYED AND INFLATED CORRECTLY BUT FAILED TO DROP TO THE GROUND. THE RAFT WAS TWISTED APPROXIMATELY 45 DEGREES AROUND THE LONG AXIS WITH THE INBOARD END IN CONTACT WITH THE OUTSIDE OF THE DOOR FRAME/FUSELAGE. 2L72 4F4 FRT E25NE 20030507001022003050700102NM 2003 5 7 AUS20030384 120030401A2150 A/C PACK BOEING767 767338 1385151NM GE CF6 CF680C2* GL CABIN COOLING SYSMOKE W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AUS (AUS) SMOKE IN CABIN AND FLIGHT DECK. RT AIRCONDITIONING PACK FAULTY. 2L72 4F4 FRTA1NM E23EA 20030507001052003050700105CE 2003 5 7 CA030416002 120030414A27305052443929 CONTROL CABLE BEECH 90 C90 1152913CE PWA PT6 PT6A21 52043EA ELEVATOR OBSTRUCTED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) FWD ELEVATOR BELLCRANK, AFT STOP BOLT WAS NOT CONTACTING ITS PROPER STOP. OUTBOARD MOUNTING BOLT FOR MLG MOTOR RELAY WAS INSTALLED THROUGH UNDER FLOOR BULKHEAD WITH SHANK FORWARD & BOLT EXCESSIVELY LONG. ELEVATOR CABLE-LOCKING TAB WAS STRIKING RELAY-MOUNTING BOLT HARD & ACTING AS A STOP. FULL ELEVATOR CONTROL TRAVEL WAS STILL ACHIEVED AT PRIMARY STOPS ON EMPENNAGE. PROPER LENGTH AN-4 BOLT WAS INSTALLED TO SECURE LANDING GEAR RELAY WITH SHANK ORIENTED AFT. WITH NORMAL CLEARANCE BEING RESTORED ELEVATOR BELLCRANK AFT STOP BOLT WAS RIGGED AS PER MM SPECS. IF LOCKING TAB HAD TRAVELED PAST MISINSTALLED RELAY MOUNTING BOLT, POSSIBILITY EXISTS THAT CONTROL COLUMN COULD HAVE JAMMED IN FULL AFT POSITION. 1L72 3T4 T 3A20 E4EA 20030507001352003050700135EA 2003 5 7 CA030419002 120030130A5754601R120445 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING LE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACKS FOUND IN LT WING LEADING EDGE MID SECTION. CRACK IS APPROX. 10 - 15 CM VERTICAL AND IS CONNECTED TO THE RIVETS IN THE MIDDLE OF THE L.E. ASSY.IN ADDITION TO THIS CRACK, 2 SMALLER CRACKS WERE FOUND ON EACH SIDE OF THIS CRACK, BOTH OF THESE CRACKS ARE STARTING FROM RIVETS . 2L72 4F4 FRTA21EA E15NE 20030506000142003050600014EA 2003 5 6 COMA0360203 120030418A78301267587 PDU CNDAIRCL600 CL6002B19 1900309EA LT ENGINE T/R MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01977CA20025 7157 FLIGHT 5830 LT ENGINE THRUST REVERSER UNLOCKED MESSAGE. REPLACED THE PDU. 2L72 4F RTA21EA 20030506001022003050600102WP 2003 5 6 DHL2003806006 120030426A2611 LAMP DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01806DH 46002 NR 5 SMOKE DETECTOR WILL NOT TEST. DEFERRED NR 5 SMOKE DETECTOR PER MEL 26-6-2, ASSIGNED CONTROL 12688, CAT-C. PLACARD INSTALLED. REFER TO DMI 12688. NR 5 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 5 SMOKE DETECTOR AND TESTED GOOD AS PER M/M 26-10-5. THIS CLEARS DMI 12688. 2L74 4F RT4A25 20030506001752003050600175WP 2003 5 6 ASAA0380252 120030307A524039522381 HINGE DOUG DC9 DC982 3022082WP SERVICE DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01953AS 49386 OKC - DURING 30K CHECK, FOUND AFT GALLEY SERVICE DOOR HINGE FITTING GOUGED. BLENDED GOUGE PER ASA EA 5240-01102. (M) 2L72 4F A6WE 20030507000212003050700021EU 2003 5 7 AUS20030327 120030317A5713D57252463200 STRINGER AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING NR 3 STRINGER FORWARD LOWER FLANGE CONTAINED LEVEL 2 CORROSION LOCATED ON THE LOWER SKIN BETWEEN RIB BAY 5 AND RIB BAY 6. FOUND DURING INSPECTION IAW J9-IA57-0806. 2L72 4F4 FRTA46NM E29NE 20030507000712003050700071EU 2003 5 7 AUS20030363 120030323A3213HC321B0052000 PIN BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502* 41580EA MLG DAMAGED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR DIRECTIONAL LINK UPPER ATTACHMENT PIN FOUND TO BE MIGRATING FROM THE LUG LOCATED AT FRAME 29. LOCKING PLATE AND PIN INCORRECTLY FITTED. MAIN LANDING GEAR IS A NEWLYOVERHAULED UNIT AND HAD ONLY JUST BEEN FITTED TO THE AIRCRAFT 48CYCLES PREVIOUSLY. PERSONNEL/MAINTENANCE ERROR. 2H74 4F4 FRTA49EU E6NE 20030507000722003050700072CE 2003 5 7 AUS20030364 120030326A53471412144 SEAT TRACK CESSNA337 337 2075702CE CONT O360 IO360C 17025SO MCAULY2AF34CD2AF34C306 GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SEAT TRACK CRACKED AT REAR SEAT STOP. ON REMOVAL ANOTHER CRACK WAS FOUND AT THE SEAT REMOVAL CUTOUT. 1H72 3O3 O A6CE E1CE 5 CP5EA 20030507001062003050700106EA 2003 5 7 CA030416003 220030406A7320212060745001 BELLCRANK BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA DROOP COMP FAILED W O OTHER E VIBRATION/BUFFET APAPPROACH 1 CA (CAN) DURING APPROACH THE DROOP COMPENSATOR SYSTEM FAILED TO RESPOND AND ENGINE RPM INCREASED AS THE COLLECTIVE WAS LOWERED. PILOT ADJUSTED ENGINE RPM USING THE ELECTRICAL TRIM SYSTEM, (BEEP SWITCH). SUBSEQUENT INSPECTION FOUND THAT THE ENGINE GOVERNOR CONTROL, SAFETY BELL CRANK SHEAR RIVET, HAD SHEARED. NO BINDING COULD BE FOUND IN THE GOVERNOR CONTROL SYSTEM LINKAGES. FAILURE OF THE SHEAR RIVET IS LIKELY THE RESULT OF FATIGUE. 1G71 4U4 U H4SW E22EA 20030507001412003050700141EA 2003 5 7 CA030421006 120030418A3234750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE MLG DEFECTIVE W O OTHER J WARNING INDICATION NRNOT REPORTED 1 CA 16903 (CAN) GEAR DISAGREE MESSAGE ON APPROACH, NOSE GEAR SHOWED DOWN & GREEN, MAIN SHOWED UP & WHITE, GEAR HANDLE CYLCLED TWICE WITH SAME INDICATION, HYD INDICATION OK. MANUAL EXTENSION COMPLETED AS PER QRH. THIS WAS THE ORIGINAL PART FROM THE MANUFACTURER. 2L72 4F4 FRTA21EA E15NE 20030507001502003050700150EU 2003 5 7 ALG2003F00055 120030213A2697 WIRE UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE COMPRESSOR SENSOBROKEN E ALGAO OTHER N FALSE WARNING APAPPROACH 1 SW03523AL 1262 34281 DURING SHORT FINAL. THE ENGINE FIRE WARNING LIGHT ILLUMINATED SHORT FINAL ON HELIDECK. THE PILOT SHUT THE AIRCRAFT DOWN AND NOTIFIED MAINTENANCE. UPON INSPECTION THE MECHANIC FOUND THE NEGATIVE LEAD TO THE COMPRESSOR SENSOR WIRE TERMINAL BROKEN. REPAIRED THE TERMINAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 UNCR0001RD E34NE 20030507001912003050700191NE 2003 5 7 ALG2003F00057 120030320A2930 WARNING LIGHT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL HYD SYS ILLUMINATED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03741SW 760070 DURING TAKE OFF, THE NR 1 HYDRAULIC LIGHT ILLUMINATED. THE PILOT FOLLOWED THE CHECKLIST AND LANDED ON HI 389. THE MECHANIC CHECKED THE NR 1 HYDRAULIC SYSTEM PRESSURE CONTROL AND WARNING SYSTEM COMPLIED WITH GROUND RUN AND OPS CHECK. NO DEFECT NOTED. 1G72 3U3 U H1NE E1GL 20030507002042003050700204NM 2003 5 7 CH1A2003017 120030410A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON FLOORBEAM LBL 45 TO LBL 62 AT BS 1067. 2L73 4F A3WE 20030507002062003050700206NM 2003 5 7 CH1A200395019 120030410A5754 SKIN BOEING727 727290 138408WNM RT WING LE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 RT WING LE CRACK IN UPPER SURFACE SKIN AT NR 5 SLAT INBD.UPHOOK CUTOUT, AT AFT END. 2L73 4F A3WE 20030507002112003050700211NM 2003 5 7 CH1A200395031 120030410A5313 SKIN BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 SKIN BULGING AT BS 1050 TO BS 1070 STR 30 2L73 4F A3WE 20030507002162003050700216NE 2003 5 7 CH1A200392001 220030411A7230 COMPRESSOR BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE ENGINE STALLED A C1HAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL15292AS 21458 ON TAKEOFF, AN ENGINE EXPERIENCED COMPRESSOR STALL AT 1.2 EPR WINDS 300 AT 5. NO OTHER INDICATIONS 2L73 4F4 F A3WE E2EA 20030508000032003050800003NE 2003 5 8 P5CA0300874 220030430A72307344441 COMPRESSOR BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE NR 3 ENGINE STALLED A P5CAO OTHER K FLUID LOSS DEDESCENT 1 WP23524UP 21446 702000 AT FL 330 NR 3 ENG COMPRESSOR STALLED. EPR WENT FROM 1.45 - 1.56 WITH 120 DEGREES RISE IN TEMP. INSP INLET AND EXHAUST (2) PERFORMED CHIP DETECTOR INSP (3) PERFORMED BORESCOPE INSPECTION. NO DEFECTS NOTED (4) REPLACED TT2 SENSOR PRECAUTIONARY. AMM 73-21-04 2L74 4F4 FRTA20WE E20EA 20030508000102003050800010NM 2003 5 8 S03425011 120030309A2530416100149 COFFEEMAKER BOEING747 747400 NM PWA 4056 PW4056 NE GALLEY 3 ODOR W SAJFO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP03 28711 B-18203 IN FLT BURING ODOR CAME OUT ONCE AT GALLEY UNIT 3 AND THEN PULL OUT ALL C/B OF UNIT 3. CHECKED ALL GALLEY 3 EQUIPMENT FOUND BURNING ODOR COME FROM COFFEEMAKER 309. COFFEEMAKER 309 REPLACED AND ALL GALLEY. EQUIPMENTS FUNCTION CHK NML. 2L74 4F4 FRTA20WE E24NE 20030508000122003050800012CE 2003 5 8 CGO2003F00007 120030407A54141229100713 PANEL BEECH 2000 2000 1152000CE PWA PT6 PT6* 52043EA LT NACELLE CRACKED B CGORO OTHER O OTHER NRNOT REPORTED 1 GL038283S2470 NC41 FOUND CRACK/ DELAMINATED AREA IN PRODUCTION LAP JOINT BETWEEN MOLDED HALVES OF CLOSEOUT PANEL AT APPROX 6 OCLOCK POSITION BELOW SPINNER CUT-OUT AND ABOVE OIL COOLER EXIT DUCT. AREA USUALLY DIRTY/GREASY, HAVE TO CLEAN THOROUGHLY AND FLEX PARTS TO INSPECT ADEQUATELY. SUSPECT CAUSAL FACTOR NORMAL AIRFRAME/PROPELLER VIBRATION LEVELS AND/OR HEAT THIS LOCATION. FIELD REPAIR FR-SS-00044 AND RETURNED TO SERVICE. SUGGEST CLOSE INSPECTION OF THIS AREA DURING SCHEDULED INSPECTIONS ONCE AIRCRAFT APPROACHES 2000 HOUR TTAF. 1L72 4T3 TRTA38ACE E2NE 20030508000142003050800014EA 2003 5 8 JUJ2003F00000 220030411A8520 SEAL PIPER PA32 PA32R301T 7103220SO LYC O540 TIO540* 41532EA CRANKSHAFT INOPERATIVE B JUJRO OTHER K FLUID LOSS NRNOT REPORTED 1 SO07834CC 32R8329007 ENGINE WAS TROUBLE SHOT DUE TO EXCESS OIL LOSS. EXAMINATION FOUND THE CRACKSHAFT SEAL TO BE PARTIALLY UNSEATED, ALLOWING OIL TO FLOW PAST AND OUT OF THE ENGINE. UPON FURTHER EXAMINATION, THE ENGINE WAS FOUND TO EXHIBIT AN UNUSUALLY HIGH AMOUNT OF CRANKCASE PRESSURE. AN APPROVED AFTER MARKET AIR/OIL SEPARATOR HAD BEEN PREVIOUSLY INSTALLED. THE RUBBER HOSES OF UKNOWN PN WERE USED FOR INSTALLATION OR REPLACEMENT. ONE HOSE WAS FOUND TO BE BENT AT SUCH AN THE OTHER HOSE WAS FOUND TO BE APPROXIMATELY 85 PERCENT BLOCKED DUE TO COLLAPSE. REMOVAL OF THE SUSPECT HOSES AND AIR/OIL SEPARATOR, AND INSTALLATION OF OEM BREATHER HOSE PROVIDED NORMAL OPERATION OF ENGINE WITH NORMAL CRACKCASE PRESSURE. 1L71 3O3 O A3SO E14EA 20030508000152003050800015NM 2003 5 8 DL73K030336 120030404A2613896798 ELEMENT BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE MALFUNCTIONED A DALAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO27377DL 23604 709186 NR 1 ENGINE OVERHEAT ON CLIMBOUT.PERFORMED PROCEDURES IAW POM. LIGHT STAYED ON UNTIL AFTER SE LANDING - REPLACED LOWER LOOP AND FIRE DETECTOR ACCESSORY UNIT 2L72 4F4 F A16WE E2EA 20030508000282003050800028WP 2003 5 8 DHL2003873008 120030430A3350 SWITCH DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT STUCK A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01873SJ 46091 EMERGENCY LIGHT DISARM LIGHT STUCK ON. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW DC-8 M/M 33-10-0. OPS CHECKED GOOD. 2L74 4F RT4A25 20030508000302003050800030WP 2003 5 8 DHL2003805008 120030501A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP COCKPIT DIRTY A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01805DH 46125 SECOND OFFICERS SEAT DOES NOT SLIDE EASILY ON THE FLOOR RAILS. CLEANED SEAT TRACKS AND LUBED S/O'S SEAT ROLLERS. CHECKED GOOD AS PER M/M 25-11-6. 2L74 4F RT4A25 20030508000312003050800031EA 2003 5 8 COMA0360221 120030502A2710600908002 PULLEY CNDAIRCL600 CL6002B19 1900309EA RIGHT WING FROZEN A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01971CA 7145 FOUND AILERON CABLE PULLEY FROZEN IN RIGHT WING NEAR THE INBOARD AILERON HINGE POINT. W.S. 282.0 DURING E.O. 27-081A. REMOVED DEFECTIVE PULLEY AND INSTALLED A SERVICEABLE PULLEY. 2L72 4F RTA21EA 20030508000322003050800032EA 2003 5 8 COMA0360222 120030425A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN AIR DIRTY A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01447CA 7552 FLIGHT 5297 VISABLE SMOKE IN CABIN CLEANED THE ACM WATER SERPERTOR BAGS. GROUND RAN SYSTEM, NO ODOR NOTED. 2L72 4F RTA21EA 20030506001362003050600136WP 2003 5 6 GTIA030186 120030223A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 LBL 6 INCHES TO RBL 6 INCHES SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABBED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030506002272003050600227WP 2003 5 6 ASAA0380200 120030304A53109936534101 FITTING DOUG DC9 DC982 3022082WP GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, LEFT FORWARD PASSENGER L-1 DOOR EMERGENCY SLIDE GIRT BAR AFT FLOOR FITTING IS CORRODED AT FS 180. REPLACED FITTING PER SRM 53-01. (M) 2L72 4F A6WE 20030507000042003050700004NM 2003 5 7 AUS20030317 120030226A1430 BOLT BOEING737 737800* NM GE CFM56 CFM567B24 NE FUEL CONTROL MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 ENGINE FAN INLET TEMPERATURE SENSOR (T12) BOLTS (2OFF) MISSING. THE TWO MISSING BOLTS WERE LOCATED WITHIN THE ENGINE COWL ACCESS PANEL. 2L72 4F4 FRTA16WE E00055EN 20030507000842003050700084NM 2003 5 7 AUS20030372 120030325A2721658D1005 ACTUATOR BOEING767 767338 1385151NM GE CF6 CF680C2* GL RUDDER TAB FAILED W O OTHER F FLT CONT AFFECTED DEDESCENT 1 AUS 451 637A (AUS) RUDDER TRIM ACTUATOR FAILED. 2L72 4F4 FRTA1NM E23EA 20030507000932003050700093NE 2003 5 7 CA030415003 120030327A6710 CONTROL QUADRANT SKRSKYS61 S61N 8142104NE GE CT58 CT581401 30011NE COLLECTIVE STUCK W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN) PILOT PULLED THE COLLECTIVE UP ON FINAL APPROACH TO THE HELIDECK, THE COLLECTIVE JAMMED AND COULD NOT BE MOVED UP ANY FURTHER. THE AIRCRAFT CONTINUED TO DESEND OVER THE DECK AND AS GROUND CUSHION WAS ENCOUNTERED THE AIRCRAFT STOPPED DESCENDING AND CAME TO A STOP IN A 10 FOOT HOVER. 2G72 4U4 U 1H15 1E3 20030507000972003050700097SO 2003 5 7 AUS20030380 220030131A73101 LINE CESSNA421 421B 2076014CE CONT O520 GTSIO520H 17032SO MCAULY3AF34C3AF34C92 GL ENGINE FUEL DISTLOOSE W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) LT ENGINE NR 5 CYLINDER FUEL INJECTION LINE LOOSE AT ATTACHMENT TO FLOW DIVIDED. 1L72 3O3 O A7CE E7CE 5 CP22EA 20030507001012003050700101GL 2003 5 7 CA030415004 220030414A726123031459 PUMP SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE OIL FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) AIRCRAFT MASTER CAUTION LIGHT ' NR 2 OIL PRESSURE ' ILLUMINATED IN CRUISE. THE OIL PRESSURE GAUGE WAS AT 50 PSI AND THE NR 2 ENGINE TORQUE METER GAUGE WAS READING LOW AND FLUCTUATING. THE FLIGHT CREW BROUGHT THE ENGINE TO FLIGHT IDLE AND DID A PRECAUTIONARY LANDING AT VANCOUVER AIRPORT. THE TORQUE SYSTEM AND ENGINE OIL SYSTEM WERE INSPECTED AND THE OIL FILTER/ REGULATOR VALVE ASSY WAS CHANGED. A GROUND RUN AND TEST FLIGHT WERE SATISFACTORY. APPROX. 1 HR LATER SAME HAPPENED AGAIN. THE ENGINE GEAR BOX WITH THE SUSPECT PUMP IN IT WERE REMOVED AND A SERVICEABLE GEAR BOX WAS INSTALLED GROUND RUNS AND TEST FLIGHTS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20030507001252003050700125SO 2003 5 7 AUS20030392 120030331A2460460620 FILTER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL DC POWER SHORTED W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) ALTERNATOR FILTER SHORT CIRCUITED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20030506001582003050600158WP 2003 5 6 ASAA0380112 120030130A33500105603 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01977AS 53453 SEA - DURING PREFLIGHT CHECK, RED EMERGENCY TRACK LIGHTING IN FIRST CLASS WAS FOUND INOPERATIVE. REPLACED HARNESS ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20030506001592003050600159 2003 5 6 ASAA0380132 420030213A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 SEA - DURING LINE CHECK, FOUND EMERGENCY SLIDE LANYARD 'NOT ROOTED' (DISCONNECTED) AT AFT LEFT SERVICE L-2 DOOR. 'ROOTED', REATTACHED, LANYARD. (M) 2L72 4F RTA6WE 20030506001992003050600199WP 2003 5 6 ASAA0380260 120030309A5320993061215 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OAK - DUIRNG C-CHECK, FOUND AFT CARGO BAY FLOOR MEMBRANE CORRODED AT FS 1070. INSTALLED DOUBLER PER SRM 51-10-3 AND 53-01. (M) 2L72 4F RTA6WE 20030506002112003050600211WP 2003 5 6 ASAA0380237 120030307A5510991840173 CHANNEL DOUG DC9 DC982 3022082WP HORIZONTAL STAB PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT HORIZONTAL STABILIZER AFT SPAR HINGE CHANNEL SUPPORT PUNCTURED. REPLACED DAMAGED CHANNEL PER SRM. (M) 2L72 4F A6WE 20030506002152003050600215WP 2003 5 6 ASAA0380195 120030303A53205937669505 STRAP DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FRAME SUPPORT (STRAP) IS CORRODED AT FS 1127. REPLACED FRAME PER SRM 51-10-4 AND 30-5. (M) 2L72 4F A6WE 20030506002312003050600231WP 2003 5 6 ASAA0380207 120030304A5320993653473 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FLOOR PANEL MOUNTING SUPPORT TRACK IS CORRODED AT FS 160-200. REPLACED SUPPORT TRACK PER SRM 53-01. (M) 2L72 4F A6WE 20030507000792003050700079CE 2003 5 7 CA030414002 120030414A5510KNKDL428 INSERT BEECH 100 B100 1152919CE GARRTTTPE331TPE3316252B 01514WP HORIZONTAL STAB STRIPPED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED INSPECTION, REPLACING THE HORIZONTAL STAB AFT ATTACHMENT POINTS. WE REMOVED THE BOLTS THAT ATTACH TO THE CASTING TO GAIN ACCESS, THREE OF THE 12 BOLTS WOULD JUST SPIN IN PLACE.AFTER REMOVING THESE BOLTS WE FOUND THAT THE NUTS (INSERTS) WERE STRIPPED. WE COULD ONLY SUSPECT THAT THEYWERE OVERTORQED IN PAST. ALL INSERTS WERE INSPECTED AND ALL SUSPECT ONES REPLACED WITH NEW. ALL NEW BOLTS, LT AND RT INSTALLED. 1L72 4T4 T A14CE E2WE 20030507001232003050700123SW 2003 5 7 AUS20030390 120030329A8097 WIRE HARNESS SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C663 NE STARTER CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT STARTER WIRING CHAFING ON STARTER RELAY BUS. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20030507001272003050700127SO 2003 5 7 AUS20030394 120030311A57514019000 DOUBLER PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE2Y HCE2YK2 GL AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AILERON SPAR OUTBOARD HINGE DOUBLER CRACKED. FOUND DURING INSPECTION IAW AD/PA31/118. 1L72 3O3 O A20SO E14EA 5 CP9EA 20030507001462003050700146GL 2003 5 7 CZQ2003F00000 220030401A72006843362 BEARING BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE FAILED E CZQAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA2533QP 2753 CAE835121 DURING FLIGHT, ENG CHIP LIGHT ACTIVATED. MAGNETIC OIL PLUGS REMOVED AND INSPECTED AND WERE FOUND TO HAVE METAL PARTICLES ATTACHED. ENG WAS REMOVED AND THE GEARBOX REMOVED FROM THE COMPRESSOR AND TURBINE. ENG 1.5 ROLLER BEARING PN 6843362 FAILED. ROLLER CAGE WAS IN A FAILED CONDITION, INNER RACE PN 23034786B FAILED. GEARSHAFT HAS 2 GEARS ATTACHED, PRESUMED TO BE WELDED TO SHAFT, SMALLER GEAR, WHICH DRIVES THE FUEL CONTROL SEPARATED AT THE RADIUS ATTACH POINT. THE STEEL INSERT(CAGE) PN 6843362 WHICH RECEIVES THE BRG PN 23005749 IN THE GEARBOX COVER WAS FOUND TO BE ROTATING THE STEEL LOCKPIN WHICH HOLDS THE STEEL INSERT(CAGE) IN ALUMINUM COVER WAS FOUND TO BE SHEARED. 1G71 3U3 U H2SW E4CE 20030507001482003050700148SO 2003 5 7 SL52003F00000 120030402A7810646463184 EXHAUST GATE PIPER PA46 PA46310P 7104605SO CONT O520 TSIO520BE 17040SO ENGINE CRACKED B SL5RO OTHER O OTHER NRNOT REPORTED 1 NE036920K61 468508083 DURING MAINTENANCE, CHECKING EXHAUST FOR POSSIBLE LEAKS, FOUND RIGHT HAND EXHAUST TEE ABOVE RIGHT TURBOCHARGER CRACKED HALF WAY AROUND, THE CRACK IS NOT VISIBLE FROM OUTSIDE AND WAS FOUND BY PRESSURIZING EXHAUST AND SOAP AND WATER. 1L71 3O3 ORTA25SO E8CE 20030507001632003050700163 2003 5 7 CGO2003F00003 420030324A2562 CASE CESSNA500 550 2076604CE PWA 530 PW530A NE ELT BATTERY CRACKED B CGORO OTHER O OTHER NRNOT REPORTED 1 GL03770JM506 5500902 WHILE INSPECTING ELT BATTERY IN CONJUNCTION WITH PHASE 18. 12 MONTH EMERGENCY EQUIPMENT INSPECTIONS AND FAR 91.207(D); NOTED: ELT BATTERY CASE CRACKED, CORROSION FROM LEAKING BATTERY MATERIAL ON INTERIOR OF SAME AREA. BATTERY MFG, EXPIRATION DATE OF 7/2003, WO NR 33883. 1L72 4F4 F A22CE E00053EN 20030507001962003050700196NM 2003 5 7 CH1A200395024 120030411A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOORBEAM AT BS 344 BETWEEN RBL 22 & RBL 62 HAS CORROSION IN NUMEROUS PLACES. 2L73 4F A3WE 20030507002022003050700202NM 2003 5 7 CHA1200395015 120030410A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON LBL 55 SEAT TRACK BS 1070 TO BS 1140. 2L73 4F A3WE 20030507002142003050700214NE 2003 5 7 S03471012 220030307A7200 ENGINE BOEING747 747400 NM PWA 4056 PW4056 NE NR 3 FAILED W SAJFC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 WP03 24311 B-18273 MAX THRUST T/O, DURING ROTATION A LOUD "BANG" WAS HEARD. ENGINE NR 3 EPR INDICATION SWING UP AND DOWN MOMENTARILY. ENGINE NR 3 WAS RECOVERED AUTOMATICALLY AND OPERATED NORMALLY IN THE REST FLIGHT. REPLACE NR 3 ENGINE AT AMS. 2L74 4F4 FRTA20WE E24NE 20030507001832003050700183WP 2003 5 7 GTIA030187 120030223A5321 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 160 RBL 12 INCHES TO RBL 44 INCHES SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABBED AND INSTALLED NEW FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030507002052003050700205NM 2003 5 7 CH1A200395018 120030410A5320 CHANNEL BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON HAT CHANNEL SECTION UPPER SURFACE AT LBL 55 AT BS 1030 2L73 4F A3WE 20030507002082003050700208NM 2003 5 7 CH1A200395027 120030410A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON CABIN FLOORBEAM AT LBL 12 BS 1070 TO BS 1090. 2L73 4F A3WE 20030508000182003050800018NM 2003 5 8 DL72S030340 120030404A571165249661 SPAR BOEING727 727225A 1384077NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805EA 22436 THE LOWER STRUCTURE AND WEB OF THE LT WING AUX SPAR BEAM WERE FOUND CRACKED NEAR THE NR 7 INBD SPOILER ACTUATOR SUPPORT FITTING. THE LOWER STRUCTURE WAS CUT AND THE CRACKED SECTION REMOVED. A NEW SECTION WAS SPLICED IN WITH STEEL REPAIR ANGLES. THE WEB WAS CUT AND THE CRACKED SECTION REMOVED. A NEW SECTION WAS SPLICE IN WITH AN ALUMINUM REPAIR DOUBLER.THE WORK WAS ACCOMPLISHED PER ER/A 384781-14, REV A. 2L73 4F RTA3WE 20030508000192003050800019 2003 5 8 DL76G030341 420030407A2330251009137 PROJECTOR BOEING767 7673P6 1385105NM CABIN FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27154DL 25241 ENROUTE ATL/SCL FLT 147/06 REPORT STRONG ODOR OF BURNED PLASTIC FWD B/C SEATS FIRST 2 ROWS OF SEATS ON THE LT SIDE OF THE CABIN. CREW TURNED OFF IFE AND UTILITY BUSSES. ODOR DISSIPATED. CREW ELECTED TO CONTINUE TO SCL./C MTC FOUND THE FWD PROJECTOR INTERNALLY SHORTED. PROJECTOR DEACT AND MCO TO COVER. REF LOG C/N 328878001. REPLACED PROJECTOR. OPS NOW NORMAL. MCO AND PLACARD REMOVED. 2L72 4F RTA1NM 20030508000402003050800040NM 2003 5 8 CH1A200395035 120030412A5330 SKIN BOEING727 727290 138408WNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 4 CRACKS AT LOWER ROW OF FASTNERS STR 26L FROM F.S. 480 TO 500. 2L73 4F A3WE 20030508000522003050800052NM 2003 5 8 DLM88030350 120030410A53125910130285 BULKHEAD DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27905DL 49536 THE BEARINGS IN THE THRUST REVERSER VALVE ACTUATING MECHANISM DETERIORATED ALLOWING THE P-DOME INSULATION BLANKET GUARD TO WEAR INTO THE P-DOME SKIN. ADDITIONALY, A SCREW ON THE VALVE CAM FOLLOWER CRANK ASSY WORE THROUGH THE P-DOME SKIN AND FWD DOUBLER. THE DAMMAGE IS AT Z=-23 AND RBL 35 ON THE STA 1338 P-DOME BULKHEAD. TWO DOUBLERS WERE INSTALLED ON THE FWD SIDE OF THE P-DOME PER ER/A 420372-14 TO REPAIR THE DAMAGE. 2L72 4F RTA6WE 20030508000532003050800053NM 2003 5 8 DLM90030351 120030410A29107963941502 LINE DOUG MD90 MD9030 3023690NM LT WHEEL WELL LEAKING A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO27916DN 53396 LT HYDRAULIC QUANITY FELL TO 6 QUARTS IN FLIGHT AT 33000 FT. TURNED OFF HYD PUMP PER ABNORMAL PROCEDURES CHECKLIST. RETURNED TO NORMAL LEVEL AFTER 10 MIN. FOUND GOUND SPOILER VALVE LINE LEAKING. INSTALLED APPROVED TEMP LINE PER M/M GOOD FOR 350 HRS FROM FLIGHT 1172/10. 2L72 4F RTA6WE 20030508000592003050800059WP 2003 5 8 MWEA0302001 120030505A57553936845501 BUSHING DOUG DC9 DC981 3022081WP SPOILER CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 RIGHT GROUND SPOILER CRANK ASSEMBLY ATTACH BOLT HOLE HAS PITTING CORROSION IN IT. FABRICATED AND INSTALLED TWO EACH BUSHINGS IN CRANK. 2L72 4F A6WE 20030508000682003050800068 2003 5 8 DL76L030356 420030415A34604058650930 CDU BOEING767 767332 1382001NM COCKPIT INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27181DN 25986 LEFT FMC CDU DISPLAY INOP. REPLACED CAPT. CDU. CONFIRMED BLOWER OK. 10 MINS AFTER REPLACEMENT CAPT CDU BLANKED OUT. INSTALLED ORIGINAL CDU. CYCLED C.B. E8 SEVERAL TIMES CDU RECOVERED AND REMAINED ACTIVE. FWD TO MCO/PLAC PRECAUTIONARY. 2.5 AMP C.B. LISTED IF REQUIRED. 2L72 4F RTA1NM 20030508000702003050800070NM 2003 5 8 DL76G030358 120030415A2780 RELAY BOEING767 767332 1382001NM LE FLAPS FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO271603 29695 ON DEPARTURE AFTER FLAPS SHOWED UP, RECEIVED AN LE SLAT ASSY EICAS MESSAGE. FOLLOWED QRN PROCEDURES, LIGHT STAYED ON DURING LANDING. REMOVED RELAY K2307 FROM P37 PANEL, FLAPS SLATS NOW NML. 2L72 4F RTA1NM 20030508000742003050800074NM 2003 5 8 DL733030363 120030417A5753 WEDGE BOEING737 737347 1384647NM RT WING DELAMINATED A DALAO OTHER O OTHER NRNOT REPORTED 1 SO273301 23181 RT INBOARD AFT FLAP TE WEDGE DISBONDED. REPAIRED PER ER/A 422820-14 2L72 4F RTA16WE 20030508000782003050800078NM 2003 5 8 2003UALA00396 120030427A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29567UA 26673 EMERGENCY SLIDE LIGHT OUTSIDE AFT CARGO DOOR INOPERATIVE. RELAMPED. 2L72 4F4 FRTA2NM E17NE 20030508000852003050800085NM 2003 5 8 AWXA200300471 120030410A5310654695713 SPLICE BOEING737 737277 1384570NM CREASE BEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON CREASE BEAM STRUCTURE SPLICE PLATE AT BS 530, LBL 64. MAINTENANCE REMOVED AND REPLACED SPLICE PLATE AT BS 530, LBL 64 IAW B737-200 SRM 51-10-1, PG. 8. 2L72 4F RTA16WE 20030903001332003090300133WP 2003 9 3 ASAA0380038A 120030105A33500105606 LIGHT DOUG DC9 DC982 3022082WP CABIN DISLODGED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02953AS 49386 DURING PREFLIGHT CHECK DISCOVERED (1ST WHITE) EMERGENCY LIGHT POPPED OUT OF STRIP. REPAIRED GROUND. LIGHT THEN OPERATIVE PROPERLY. 2L72 4F A6WE 20030508000952003050800095NM 2003 5 8 QXEA0300519 120030418A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - SCRATCH ON FUSELAGE BELLY SKIN AT X246 AND STRINGER 32L. REPAIRED IAW DHC-8 400 SRM 51-21-10 AND SRM 51-25-200, PAGES 202-205, PARAGRAPH 5. 2H72 4T RTA13NM 20030508001032003050800103NE 2003 5 8 DL764030366 220030417A7200 ENGINE BOEING767 767 UTILUSENM GE CF6 CF680C2B7 NE NR 1 STALLED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27833MH7357 29706 716192 JUST PRIOR TO LIFT OFF ATL 27 RT, LT ENGINE COMPRESSOR STALLED REPETITIVELY ABOUT 7 TIMES BEFORE THROTTLE WAS REDUCED AF TER TAKEOFF. FLT ATTENDANTS NOTED FLAMES COMING OUT OF LEFT ENGINE WHILE THIS POPPING WAS OCCURING. N1 AND EGT FLUCUATED. TAKEOFF POWER WAS DERATED 55 DEG. OPERATED OK THROUGH LANDING. NO EXCEEDANCES. INDICATIONS NORMAL. REPLACED ENGINE ON TRANS 14T103 2L72 4F4 FRTA1NM E13NE 20030508001052003050800105NM 2003 5 8 DLM11030367 120030416A2913 PUMP DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE NR 2 HYD SYS UNSERVICEABLE A DALAO OTHER O OTHER NRNOT REPORTED 1 SO27811DE 48566 723924 ON ARRIVAL TO ATL HAD NR 2 ENGINE HYDRAULIC PUMP HIGH TEMP INDICATION. AFTER TROUBLE SHOOTING CAUSE FOUND CHECK VALVE HAD FAILED, CONTAMINATING THE ENTIRE SYSTEM AND INTERNAL FAILURE OF THE PUMPS, METAL IN ALL THE FILTER BODIES NO.2 SYSTEM. REPLACED PUMPS, FILTERS, FLUSHED SYSTEM, RESERVICED 2L73 4F4 FRTA22WE E24NE 20030508001172003050800117NM 2003 5 8 HOC2003F00015 120030429A53206519606198 SUPPORT BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK, CORROSION WAS NOTED ON AFT LAV PAN AND SUPPORT. 2L72 4F4 FRTA16WE E2EA 20030508001212003050800121 2003 5 8 MALA030250 420030429A2565D31003107 GIRT BAR BAC 146 AVRO146RJ85A1500097EU PAX DOOR SLIDE LACK OF LUBE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15520XJ E2345 FA REPORTS LT FWD DOOR GIRT BAR IS HARD TO ENGAGE. LEFT FORWARD PASSENGER DOOR, IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE SWAPPED LT FRONT W/RT REAR SLIDES PN ON/OFF D31003-107. LT FRONT SN 1547. RIGHT REAR SN 1407. LUBED DOOR AND GIRT BARS. OPS CHECK GOOD 2H74 4F RTA49EU 20030508001312003050800131NM 2003 5 8 UPS03440626 120030414A533065B0500064 DOOR FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C M/D - R5 DR FWD FX CUTOUT UPPER REVEAL FOUND CRACKED AT STR 16. DOOR CUTOUT REVEAL FRAME REPAIRED AS PER SRM 51-40-03 FIG.1 2L74 4F A20WE 20030508001352003050800135EU 2003 5 8 U30A200300014 120030502A5210 RESERVOIR AIRBUS320 A320212 3930322EU PAX DOOR LOW A U30AK NONE O OTHER ININSP/MAINT 1 EA17265AV 427 DURING DAILY INSPECTION AFTER FLT 313 IN BWI, THE L2 CREW PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. REPLACED DIAPHRAM PN FE240-221-001 AND ASSOCIATED PACKINGS & SERVICED CYLINDER IAW AMM 52-10-00-610-001. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030508001552003050800155NM 2003 5 8 QXEA0300517 120030410A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 FUSELAGE SKIN GOUGED AT X5 AND STRINGER 26R. REPAIRED IAW DHC-8 400 SRM 51-14-00-350-803. 2H72 4T RTA13NM 20030507001672003050700167SO 2003 5 7 TVM2003F00000 220030402A8570653608 PUMP CESSNA414 414A 2075907CE CONT O550 TSIOL550A SO NR 1 ENGINE LEAKING E TVMAO OTHER O OTHER NRNOT REPORTED 1 EA05500AA 47 414A0313 800652 PUMP WAS LEAKING COOLANT FROM DRAIN AND WOULD NOT MAINTAIN SYSTEM PRESSURE. 1L72 3O3 O A7CE E4SO 20030507001842003050700184EU 2003 5 7 XSF2003F00000 120030401A2913S40 COUPLING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HYD PUMP DRIVE WORN E XSFAO OTHER O OTHER NRNOT REPORTED 1 WP13702SA405 3551 9880 PILOT EXPERIENCED HYDRAULIC FAILURE IN FLIGHT. SPLINES BETWEEN HYDRAULIC PUMP AND DRIVING PULLEY FOUND WORN. SPLINES ARE GREASED EVERY 500 HOURS. TT 409.5 HOURS. SPLINE MAY NOT HAVE BEEN GREASED SUFFICIENTLY. WHEN AIRCRAFT WAS ASSEMBLED. 1G71 3U3 U H9EU E19EU 20030508000022003050800002NM 2003 5 8 P5CA0300872 120030424A2830125613A NOZZLE BOEING747 7472U3B 1384846NM LT WING LEAKING A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23922FT 22768 DURING FUELING LEAK WAS OBSERVED FROM LT WING FUEL JETTISON NOZZLE VALVE. REPLACED LT FUEL JETTISON NOZZLE VALVE. 2L74 4F RTA20WE 20030508000512003050800051SO 2003 5 8 C2XA03SH126 120030502A532014521721005 STRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 SHV DURING C CHECK THE CENTER BUTTSRAP BETWEEN FRAMES 14 AND 19 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030508000582003050800058WP 2003 5 8 MWEA030185 120030506A5230995766438 FITTING DOUG DC9 DC981 3022081WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 MID CARGO DOOR LOWER AFT STOP SUPPORT FITTINGS ATTACH ANGLE CRACKED. FABRICATED AND INSTALLED TEE SUPPORT. 2L72 4F A6WE 20030508000992003050800099EA 2003 5 8 QXEA0300635 120030423A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 PDX-SKIN CHAFED AT FS319.00 ON LT SIDE, MID FUSELAGE JUST FORWARD OF CUTOUT FOR MAIN CABIN DOOR. REPAIRED IAW CRJ-700 SRM 51-25-16 AND HORIZON AIR EA R53-95 AND EO 670-53-21-035. 2L72 4F RTA21EA 20030508001112003050800111NM 2003 5 8 DLM90030374 120030418A256061020 BATTERY PACK DOUG MD90 MD9030 3023690NM FLASHLIGHT DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27906DA 53386 FWD FLT ATTN STATION EMERGENCY FLASHLIGHT FAILS LED. REPLACED EMERGENCY FLASHLIGHT BATTERY PACK PER M/M CKS GOOD 2L72 4F RTA6WE 20030509000032003050900003EU 2003 5 9 CX7A194J42 120030507A26121734362450 DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE CONTAMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03303CE 340B194 RT TAIL PIPE HOT ON T/O ROLL PRIOR TO V1. MODERATE PRECIPITATION. 2L72 4T RTA52EU 20030509000112003050900011WP 2003 5 9 GTIA030240 120030317A5753 SKIN DOUG DC9 DC983 3022083WP TE FLAPS DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW- FOUND RIGHT INBOARD FLAP LOWER SURFACE DENTED ON FRAME. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. INSTALLED NEW SKIN PANEL, FOUND NO DAMAGE TO FRAME. (M) 2L72 4F RTA6WE 20030509000142003050900014SO 2003 5 9 SIMA200309607 120030403A531014522178005 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING DAMAGE CENTER SILL AND INSTALL NEW SILL IAW EMBL 145 SRM 145/1142 REV 21, CHAPTERS 51-40-02, 51-40-06, AND 51-20-03. (M) 2L72 4T RTT00011AT 20030509000322003050900032WP 2003 5 9 GTIA030246 120030402A5410 LINER DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 ENGINE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 725463 DTW - ACCOUSTIC LINER DELAMINATED IN NR 2 ENGINE FAN DISCHARGE TURBINE EXHAUST SECTION OUTER DUCT. REMOVED AND REPLACED NR 2 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20030509000732003050900073NM 2003 5 9 HOC2003F00007 120030420A5347 SEAT TRACK BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON SEAT TRACK AND FLOOR SUPPORTS AT STA 380-420, RBL 10-20. 2L72 4F4 FRTA16WE E2EA 20030509000832003050900083GL 2003 5 9 BZP2003F00001 120030215A2497MS272227 CONTACTOR BOMBDRBD700 BD7001A10 1390006GL RROYCEBR700 BR700710A110 NE PANEL ARCED B BZPRO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO11949GP137 57 9049 TERMINAL C2 OF CONTACTOR KPB101 WAS NOT TORQUED PROPERLY. THIS TERMINAL IS SUBJECTED TO HIGH ELECTRICAL LOADING AND AS SUCH EXPERIENCED ARCING DUE TO ITS BEING LOOSE. ARCING CAUSED CONTACTOR TERMINAL COVER, (PN MS272436), TO MELT NEAR TERMINAL C2. PLASTIC PART OF LUG AT THE CONNECTION POINT OF WIRE NR 3PB113A16 ALSO MELTED. OF BIGGER CONCERN IS WIRE 3PV100B6 THAT CONNECTS TO C1 OF THIS CONTACTOR. THIS IS A NR 6 WIRE THAT HAS AN APPRX 15 FT RUN FROM TRANSFORMER RECTIFIER UNIT(TRU) AXV100. THERE IS NO WIRE PROTECTION INSTALLED FOR THIS WIRE RUN(NOR IS THERE ANY FOR THE NR10 WIRE THAT RUNS FROM C2 TO ROW N OF THE COCKPIT CIRCUIT BREAKER PANEL). NOTE: HALF OF TERMINALS ON CONTACTOR WERE MISSING LOCK WASHERS. 2L72 4F4 FRTT00003NYE00057EN 20030509001232003050900123EU 2003 5 9 I05R086283 120030425A771478899811 INDICATOR UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE ENGINE NG INTERMITTENT B I05RO OTHER O OTHER NRNOT REPORTED 1 WP0526LB 400 3514 INSTRUMENT INTERMITTENT, THE PERMENENT FAILURE REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H9EU E00054EN 20030509001382003050900138EA 2003 5 9 COMA0360231 120030506A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM WEAK A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01821CA6454 7420 FLIGHT 5345 LANDING GEAR DISAGREE WARNING, USED EMREGENCY FREE FALL SYSTEM TO LOWER NLG. REPLACED HYDRAULIC PUMP 3A. 2L72 4F RTA21EA 20030509001462003050900146WP 2003 5 9 AMTA200300458 120030325A5347 FLOORBEAM LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 C-2 COMPARTMENT FLOORBEAM CORRODED FS 1685 LBL 40. FABRICATED NEW CARGO FLOOR TRACK SECTION LBL 40 FS 1685-1725. INSTALLED CARGO FLOOR TRACK IAW 51-40-01 SRM. (M) 2L73 4F A23WE 20030509001512003050900151SO 2003 5 9 SIMA200309201 120030401A3411 DRAIN EMB 135 EMB135LR 3260305SO PITOT STATIC BROKEN A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21730KW 145346 AFTER TAKEOFF CREW REPORTED THE PITCH TRIM 1 AND 2 FAILED AND FIRST OFFICERS AIRSPEED WAS APPROXIMATELY 50 KNOTS LOW. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF PITCH TRIM SYSTEM WAS SATISFACTORY IAW EMB MM. A PITOT STATIC SYSTEM OPERATIONAL CHECK WAS COMPLIED WITH NO DEFECTS NOTED. A BROKEN PITOT STATIC DRAIN WAS FOUND AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030509001542003050900154NM 2003 5 9 USAASB03054 120030409A3260MS253831 SWITCH BOEING737 737301 1384611NM MLG INDICATOR FAILED A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19574US 23739 EWR - FLT 505 - ON GEAR EXTENSION INTO EWR, CREW RECEIVED THREE GREN AND THREE RED GEAR INDICATION LIGHTS. CREW ACCOMPLISHED GO-AROUND TO CONFIRM GEAR WAS DOWN AND LOCKED. QUICK REFERENCE HANDBOOK PROCEDURES WERE ALSO PERFORMED. ALL THREE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED WITH GEAR DOWN UNTIL THE GEAR HANDLE WAS MOVED AROUND. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE S78 LANDING GEAR LEVER SWITCH. OPERATIONAL CHECK AND GEAR SWING CHECKS GOOD. (M) 2L72 4F RTA16WE 20030509001582003050900158NM 2003 5 9 AMTA200300446 120030403A3350S417N50914 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 FOUND FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE FROM ROW 35 THROUGH ROW 37. REPLACED FLOOR PATH LIGHT ASSEMBLY AT ROW 35 PER AMM 33-51-11-3, OPS CHECK GOOD MFG P/N S417N509-14. (M) 2L72 4F RTA2NM 20030507001742003050700174WP 2003 5 7 GTIA030183 120030301A5320 ANGLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK33528 49503 MAIN CABIN STA 769 TO STA 826 RT SIDE WEB PANEL. RT SIDE HAS CRACKED/DAMAGED AT HATS SECTION (2EA) AND RUB STRIP PEELING OFF, CORRODED ON EDGE. CUT OUT DAMAGED AREA OF CRACK NR 1. STOP DRILLED CRACKED NR 2. FABRICATED REPAIR ANGLES FOR CRACKS NR 1 AND NR 2. INSTALLED REPAIR ANGLES. 2L72 4F4 FRTA6WE E2EA 20030507001772003050700177WP 2003 5 7 GTIA030193 120030218A5311 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 AFT ASSEMBLY COMPT CANT FRAME 1485 CORRODED AND CRACKED RBL 20 INCH, WL(-6). REMOVED DAMAGED AREA. FABRICATED FRAME SECTION. FABRICATED DOUBLER FRAME. INSTALLED FRAME SECTION DOUBLER. 2L72 4F4 FRTA6WE E2EA 20030507001822003050700182WP 2003 5 7 GTIA030182 120030303A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FLOOR PANEL BETWEEN AFT LAVS HAS HOLE PUNCTURE. ALSO HAS DAMAGED INSERTS AND MISSING CORE. FABRICATED NEW PANEL. 2L72 4F4 FRTA6WE E2EA 20030508000562003050800056NM 2003 5 8 DL757030354 120030412A2530831610403M0DA OVEN BOEING757 757232 1384965NM MID GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27690DL 27585 PER CREW OVEN BURNING ODOR ON TAKEOFF AND CLIMB IN COCKPIT AND CABIN, ALL OVEN CBS PULLED CABIN ODOR STOPPED.THIS WAS ON FLT 1241 FROM ATL TO BWI. REMOVED AND REPLACED OVENS 2L72 4F RTA2NM 20030509000292003050900029EU 2003 5 9 A6WA200360008 120030411A5753 FLAP TRACK BAC 146 146200A 1500266EU NR 1 WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 FLAP TRACK WEAR NR 2 RIGHT, NR 1 RIGHT AND LEFT NR 1. REPAIR REQUESTED FROM BAE SYSTEMS REF AVMAX FAX 1538-6080003. (M) 2H74 4F A49EU 20030509001592003050900159NM 2003 5 9 AMTA200300473 120030407A2622898052 EXTINGUISHER BOEING757 75723N 1384973NM CABIN DISCHARGED A AMTAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11520AT 27976 PORTABLE HALON FIRE EXTNIGUISHER FROM LEFT FORWRAD OVERHEAD BIN DISCHARGED IN FLIGHT INTO THE MIDDLE OVEN IN THE FORWARD GALLEY. DUE TO SMOKE FROM PAPER IN OVEN. REPLACED PORTABLE HALON FIRE EXTINGUISHER, LEFT FORWARD OVERHEAD, SECURED OK FOR SERVICE. NO DEFECTS NOTED WITH THE OVEN. (M) 2L72 4F RTA2NM 20030509001732003050900173NM 2003 5 9 USAABB03058 120030409A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU 22199 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030513000142003051300014NM 2003 5 13 250TR0015 120030429A5320 STIFFENER BOEING737 7372K5 138448XNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 HOLE IN STIFFENER AT STR 26RT BETWEEN BS420 AND BS440. FABRICATED NEW WEB PER DWG 65-20726 AND INSTALLED PER SRM 51-10-1. 2L72 4F RTA16WE 20030513000242003051300024EA 2003 5 13 03131644 120030511A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27644BR 7379 DURING MAINTENANCE INSPECTION, THE NR 1 AND 3 EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513000252003051300025SO 2003 5 13 UZ22003F00000 220030417A8530 CYLINDER BEECH 55 95A55 1152704CE CONT O470 IO470L 17026SO ENGINE SEPARATED B UZ2RO OTHER O OTHER NRNOT REPORTED 1 SW179648Y 1200 TC383 CS1923889LR NR 4 CYLINDER TOP CAME OFF OF BARREL IN FLIGHT UNKNOWN CAUSE OR HOW TO PREVENT. 1L72 3O3 O 3A16 3E1 20030513000392003051300039NM 2003 5 13 03FDEA00706 120030508A5754 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP L/E STOP BOLT SUPPORT ISLAND FOUND CRACKED. 2L73 4F RTA22WE 20030513000462003051300046 2003 5 13 SWIA200311954 420030428A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NR 1 YAW DAMPER MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07426SW7086 7086 7468 NR 1 YAW DAMPER WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW LINEAR ACTUATOR WITH A SERVICEABLE UNIT IAW MM 22-22-01. PERFORMED OPS CHECK IAW MM 22-22-01. 2L72 4F RTA21EA 20030513000572003051300057NE 2003 5 13 ASOA03125 220030323A73208108001002 EEC AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE INOPERATIVE A ASOAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11637AS 383 127027 DURING TAKEOFF, AT APPROXIMATELY 3,000 FT WHILE INCREASING TO CLIMB POWER, THE RT ENGINE SPEED WENT TO 102.5 PERCENT. THE CREW REDUCED THE ENGINES TO 86 PERCENT WITH 1 INCH SPLIT IN THE LEVERS, THEN THE RT ENGINE DECREASED TO 83 PERCENT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ELECTRONIC ENGINE CONTROL UNIT. ENGINE RUNS AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20030513000582003051300058EA 2003 5 13 ASOA03124 120030323A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11861AS 7445 DURING APPROACH INTO ATL FROM SWF,WITH THE FLAPS SELECTED TO 8 DEGREES, THE CREW RECEIVED A FLAPS FAILED MESSAGE. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT LANDED SAFELY IN ATL WITH THE FLAPS TO ZERO. MAINTENANCE COMPLIED WITH AD 98-20-01 AND RESET THE FLAPS SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030513000622003051300062EA 2003 5 13 03129668 120030509A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27668BR 7544 DURING MAINTENANCE INSPECTION, THE LT AFT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513000732003051300073EU 2003 5 13 RAIA00304123 120030427A3397 WIRE AEROSPATR42 ATR42300 8680920EU EMERGENCY LIGHT BROKEN A RAIAO OTHER L NO TEST NRNOT REPORTED 1 CE03421TE 102 EMERGENCY EXIT LIGHT ON STAIRS INOPERATIVE. REPAIRED BROKEN WIRE, OPS CK OK. 2H72 4T RTA53EU 20030513000782003051300078 2003 5 13 RAIA00305128 420030504A34257003360948 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AHRS FALSE INDICATIONA RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03560HK138086203 41076 HEADING COMPARATOR ERROR MESSAGE. MAINTENANCE REMOVED AND REPLACED THE NR 2 AHRS COMPUTER, OPS CK OK. 2L72 4T RTA41NM 20030513000792003051300079EU 2003 5 13 RAIA00305129 120030504A3010 BOOT AEROSPATR72 ATR72202 8680940EU DEICE SYSTEM DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03722TE 220 AIRFRAME DE-ICE FAULT INDICATION. MAINTENANCE INSTALLED DE-ICE BOOT PATCHES AND OPS CK SYS OK. 2H72 4T RTA53EU 20030513000822003051300082NM 2003 5 13 UPS03240661 120030509A3350 LIGHT BOEING727 727185C 138406NNM CABIN INOPERATIVE A IPXAO OTHER L NO TEST ININSP/MAINT 1 SO01954UP 19827 EMERGENCY EXIT LIGHT AT CREW ENTRY DOOR INOPERATIVE. PERFORMED ADJ/TEST OF EMERGENCY LIGHTS IAW MM 33-50-01. OPS CHECK GOOD. NO DEFECTS NOTED. 2L73 4F A3WE 20030513000872003051300087NM 2003 5 13 UPS03240668 120030415A5311 FRAME BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, SUSPECT CRACK ON FRAME ADJACENT TO HINGE STRUCTURE AT FWD END OF FWD CARGO BAY DOOR. ON REMOVAL OF STIFFENER IN PREPARATION FOR REPAIR A NEW CRACK WAS FO UND WHICH WAS OUTSIDE THE PERMITED REPAIR AREA. FRAME WAS REMOVED IAW SRM 51-30-02. FRAME FABRICATED IAW SRM 51-30-02 FRAME INSTALLED IA W SRM 51-30-02. REPAIR CARRIED OUT IAW SRM 51-10-1 2L73 4F A3WE 20030513000962003051300096NM 2003 5 13 AWXA200300498 120030411A5322654653835136 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING C-15 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT FORWARD OUTBOARD FRAME WEB AND SHEAR TIE BS 599, LBL 70 & RBL 70. MAINTENANCE CUTOUT CRACKS AT FRAME WEB AND SHEAR TIE BS 599, LBL 70 & RBL 70 AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5362-03119-SS4. 2L72 4F RTA16WE 20030513001202003051300120NM 2003 5 13 UPS03240677 120030417A5230 ANGLE BOEING727 727185C 138406NNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C&SI, CRACK ON ANGLE AFT CARGO DOOR INTERIOR, JUST ABOVE FWD DOOR STOP FITTING REMOVED CRACKED ANGLE, AFTER DE-RIVETING AREA IAW SRM 51-30-2 FABRIC ATED NEW ANGLE IAW SRM 51-20-1 FIG 7. INSTALLED NEW ANGLE & REPAIRED IAW SRM 51-40-3 2L73 4F A3WE 20030508000572003050800057EA 2003 5 8 COMA0360223 120030429A5610NP1393221 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER APAPPROACH 1 SO01924CA13789 7026 FLIGHT 5861 PILOTS SIDE WINDOW SHATTERED. REPLACED WINDOW. 2L72 4F RTA21EA 20030508001342003050800134EA 2003 5 8 03118620 120030428A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27620BR 7179 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISCOVERED AN EMERGENCY CEILING LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030509000432003050900043SO 2003 5 9 SIMA200309602 120030331A531014525480003 SILL EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 20 CHAPTERS 51-40-02, 51-40-04, 51-40-06, 51-20-01, 51-20-03, AND EMB CPM 51-21-04, 51-21-05 AND 51-21-06. (M) 2L72 4T RTT00011AT 20030509000772003050900077SW 2003 5 9 FTU2003F00011 120030424A5520440000246 COLLAR GULSTM690TP 695A 7630519SW GARRTTTPE331TPE331* 01514WP TORQUE TUBE LOOSE B FTURO OTHER O OTHER NRNOT REPORTED 1 NE057812 96089 DURING A NORMAL PERIODIC INSPECTION, BOTH LEFT AND RIGHT ELEVATORS WERE FOUND LOOSE. CLOSER INSPECTION REVEALED WORKING RIVETS WHICH HOLD COLLARS (PN 440000-246) TO THE ELEVATOR TORQUE TUBES (PN 440000-96). HOLES WERE DAMAGED BEYOND ALLOWABLE LIMITS AND BOTH LEFT AND RIGHT ASSEMBLIES WERE REPLACED WITH NEW PARTS. IF THE WORKING RIVETS WERE FOUND AT AN EARLIER INSPECTION, THIS CONDITION MAY NOT HAVE OCCURED. 1H72 4T3 T 2A4 E2WE 20030509001302003050900130CE 2003 5 9 5868 120030425A273155654506 SPROCKET CESSNA CESSNA500 550 2076604CE ACTUATOR DETACHED B ESEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO11117TA 116 012603 5500464 AIRCRAFT PITCH TRIM CONTROL FROZE IN PLACE, DURING FLIGHT, DUE TO THE RIGHT PITCH TRIM ACTUATOR CHAIN SPROCKET PN 556450-6 BECOMING DISLODGED FROM ACTUATOR DUE TO ATTACHMENT PIN FOR THE SPROCKET PN S2637-6Z11 COMING OUT OF THIS SPROCKET TO SHAFT ATTACHMENT. ACTUATOR WAS REPLACED WITH ANOTHER, SAME PN, OVERHAULED UNIT. PITCH TRIM SYSTEM RIGGING SET AND OPERATIONAL TESTED GOOD.DETAILED INFORMATION ON THIS REPAIR IS ON FILE ON W.O. 5868. 1L72 4F A22CE 20030513000282003051300028WP 2003 5 13 0300929621 120030510A2150 DUCT DOUG DC9 DC932 3022066WP LT ACM SEPARATED A NWAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01621NW 47544 CRUISING AT FL 330 CREW NOTICED THE CABIN ALTITUDE AT 9300' AND CLIMBING AT 450FPM. COM PROCEDURES DID NOT ARREST CABIN CLIMB AND CREW PERFORMED AN EMERGENCY DESCENT TO A LOWER ALTITUDE WHERE THEY WERE ABLE TO REGAIN CONTROL OF CABIN PRESSURIZATION. FLIGHT DIVERTED TO MKE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A DUCT FROM THE LEFT ACM SEPARATED AND REINSTALLED IT. THE NR 1 CONTROLLER BITE SHOWED FAULT CODE 016, NR 2 HAD NO FAULTS. AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20030513000352003051300035NM 2003 5 13 03FDEA00710 120030507A5754 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413 WINGS- LT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030513000422003051300042 2003 5 13 SWIA200311950 420030503A31706229820009 COMPUTER CNDAIRCL600 CL6002B19 1900309EA NR 2 DCU MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07930SW 7713 IAPS DEGRADED STATUS MESAGE WOULD NOT CLEAR. REMOVED AND REPLACED NR 2 DCU IAW CRJ MM 31-41-04. OPS CHECK GOOD PER CRJ MM 31-41-00. 2L72 4F RTA21EA 20030513000972003051300097NM 2003 5 13 AWXA200300500 120030429A53226545409602 ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING C-15 CHECK A 1 1/2 INCHES CRACK WAS FOUND ON VERTICAL ATTACH ANGLE BELOW CABIN SEAT TRACK AT RBL 24.75, BS 663.75. MAINTENANCE CUTOUT DAMAGED SECTION OF CHORD AT RBL 24.75, BS 663.75; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SECTION OF CHORD AND SPLICE REPAIR ANGLES; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5312-03120-KB2. 2L72 4F RTA16WE 20030513001072003051300107NM 2003 5 13 AWXA200300459 120030501A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28802AW 924 FLIGHT CREW REPORTED THE AFT LT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030513001082003051300108NM 2003 5 13 AWXA200300460 120030429A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW7508 924 DURING INSPECTION THE LT FORWARD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-38-400. 2L72 4F RTA28NM 20030513001092003051300109NM 2003 5 13 AWXA200300461 120030420A5320BAC1509100146 CHANNEL BOEING737 73733A 1384673NM CABIN FLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT CHANNEL, BS 859, RBL 7. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR PANEL SUPPORT CHANNEL; FABRICATED A CHANNEL FILLER AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG. 201-202, FIG. 201. 2L72 4F RTA16WE 20030513001352003051300135NM 2003 5 13 03126428 120030506A3350321431 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27428FJ 3193 DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY BATTERIES 4LK, 5LK, 6LK AND 7LK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030513001462003051300146NM 2003 5 13 CH1A200395044 120030416A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON CABIN FLOOR SUPPORT BS 420 BETWEEN RBL 45 AND RBL 62 2L73 4F A3WE 20030513001482003051300148NM 2003 5 13 CH1A200395046 120030417A5313 STRINGER BOEING727 727290 138408WNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 3 CRACKS ON STR 26L LOWER ROW OF FASTENERS FROM BS 540 TO BS 560 2L73 4F A3WE 20030513001502003051300150NM 2003 5 13 CH1A200395048 120030417A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOOR SUPPORT AT BS 418 BETWEEN RBL 22 TO RBL 44 IS EXFOLIATED 2L73 4F A3WE 20030513001632003051300163EA 2003 5 13 QXEA0300465 120030419A26129847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 BOI- FORWARD CARGO COMPARTMENT CENTER SMOKE DETECTOR CHIMNEY SCREEN TORN. REMOVED AND REPLACED CENTER CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513001682003051300168NM 2003 5 13 2003UALA00376 120030412A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 FWD NOSE COMPARTMENT STATION 284 STR 23R IS CORRODED ON TOP OUTBOARD SIDE. INSTALLED NEW STRINGER SECTION A CLIPS. 2L72 4F4 FRTA16WE E2GL 20030513001712003051300171NE 2003 5 13 2003UALA00379 220030411A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29568UA 26674 AIRCRAFT LOST NR 2 ENGINE AT ROTATION. 2L72 4F4 FRTA2NM E17NE 20030513001802003051300180NM 2003 5 13 QXEA0300471 120030421A7930APT761000100DW TRANSMITTER DHAV DHC8 DHC8202 2809007NM ENGINE OIL MALFUNCTIONED A QXEAO OTHER K FLUID LOSS CLCLIMB 1 NM09364PH3201 3201 524 ON FLIGHT 2149 ON CLIMBOUT THROUGH 8,000 NR 1 OIL PRESSURE GAUGE FELL TO 25 POUNDS MOMENTARILY, THEN TO ZERO. NO ASSOCIATED CAUTION LIGHTS. ALL OTHER INDICATIONS NORMAL. INDICATOR STAYED AT ZERO POUNDS FOR 12 TO 15 MINUTES AND THEN RETURNED TO NORMAL. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513001822003051300182EA 2003 5 13 SWIA200311891 120030417A2740 COMPUTER CNDAIRCL600 CL6002B19 1900309EA HSCU MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07597SW 7293 STAB TRIM AND MACH TRIM BOTH DISCONNECTED IN FLIGHT AND UPON TOUCHDOWN. RE-RACKED HSCU COMPUTER. PERFORMED BIT CHECK, NO FAULTS NOTED. CHECKS GOOD. 2L72 4F RTA21EA 20030513002002003051300200EA 2003 5 13 QXEA0300476 120030404A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 ON AFT PRESSURE BULKHEAD LOOKING FORWARD LOWER LEFT SIDE JUST BELOW STRINGER 17BL RIVET HOLE ELONGATED. REPAIRED IAW HORIZON AIR EA R-53-85 AND WVAC EO 601R-53-3915. 2L72 4F RTA21EA 20030513002052003051300205NM 2003 5 13 QXEA0300481 120030421A3230 YOKE BOMBDRDHC8 DHC8401 1390041NM ZONE 700 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 RIGHT HAND MAIN LANDING GEAR UPPER OUTBOARD LEG OF YOKE, SMALL RETRACT ACTUATOR HYDRAULIC TUBE IS RUBBING YOKE LEG. REPAIRED IAW HORIZON AIR EA 6-32-226. 2H72 4T RTA13NM 20030513002072003051300207NM 2003 5 13 QXEA0300483 120030412A5753 FLAP TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 LEFT HAND NACELLE HAS DIAPHRAGM CRACKED JUST ABOVE NR 3 FLAP TRACK. REPARIED IAW DHC-8 400 SRM TASKS 51-42-05-330-801, PAGES 201-218 AND 51-40-15-330-801, PAGES 201-229. 2H72 4T RTA13NM 20030513002172003051300217 2003 5 13 GLBA2003054 420030423A34426227337001 TRANSMITTER BEECH 1900 1900D 1154162CE WX RADAR SYS MALFUNCTIONED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03184UX5618 UE184 RADAR WILL NOT PAINT, R & R WX RADAR OPS CHECK GOOD. 2L72 4T RTA24CE 20030513002262003051300226SO 2003 5 13 C2XA03SH117 120030425A532014525480003 SILL EMB 145 EMB145LR 3260212SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 SHV DURING C CHECK THE CARGO DOOR SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-20-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030513002362003051300236NE 2003 5 13 42403 220030424A8530116733 CYLINDER HEAD DOUG DC3 DC3C 3021457WP PWA R1830 R183090D 52020NE ENGINE SPLIT E VLLAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL0536AP 5701 799 13439 CP355054 AT CLIMB POWER IN ROUTE HZY-UDG RIGHT ENGINE DEVELOPED A VIBRATION AND A SLIGHT LOSS OF POWER. AIRCRAFT DIVERTED TO MWO. FOUND NR 1 CYLINDER HEAD SEPARATED FROM BARREL. 2L72 4R4 R A669 5E4 20030513002382003051300238EA 2003 5 13 ASOA03174 120030420A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL AT FS 574 AND FS 621 IAW SRM 51-00 AND SRM 53-00. (M) 2L72 4F RTA21EA 20030513002432003051300243 2003 5 13 A6WA200340054 420030417A2220 ACCELEROMETER CNDAIRCL600 CL6002B19 1900309EA NR 1 ENGINE MALFUNCTIONED A A6WAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL31422AW 7341 DURING TAKEOFF ROLL AT 70 KNOTS, OBSERVVED N2 ENGINE VIBE 'ICON' ON NR 1 ENGINE BTMS. ALL GREEN BANDS ON ABORTED TAKEOFF. PERFORMED PARTIAL ENGINE BORESCOPE. NO DAMAGE NOTED. REMOVED AND REPLACED NR 1 ENGINE ACCELEROMETER. NO DEFECTS NOTED. (M) 2L72 4F RTA21EA 20030513002442003051300244EA 2003 5 13 A6WA200340060 120030417A5755 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA SPOILER DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 FOUND LEFT FLIGHT SPOILER HAS A DENT THAT IS 1 INCH IN DIAMETER AND .038 INCH DEEP. PERFORMED INSPECTION AND EDDY CURRENT OF AREA IAW WVAC EO 601R-57-3945. (M) 2L72 4F RTA21EA 20030513002512003051300251EA 2003 5 13 ASOA03153 120030410A5210601R3198041 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING A C-CHECK IN MCN, THE UPPER HINGE AT THE TOP STEP OF THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE UPPER HINGE AT THE TOP STEP OF THE PASSENGER DOOR IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030513002792003051300279SO 2003 5 13 ASOA03143 120030401A3350D36604001 BATTERY PACK EMB 120 EMB120RT 3260202SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11281AS 120224 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS IN THE AFT SECTION OF THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE AFT SECTION OF THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030509000372003050900037WP 2003 5 9 GTIA030237 120030314A5320 ATTACH ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND MID PIT STATION 522 CORRODED AT ANGLE SUPPORT BULKHEAD, AFT FACE AND FORWARD SIDE LBL 18 LBR 18. FABRICATED NEW ATTACH ANGLE. PRIOR TO STEOP 4 REMOVED ATTACH ANGLE. INSTALLED ANGLE. (M) 2L72 4F RTA6WE 20030509000852003050900085NM 2003 5 9 IU62003F00016 120030402A291065446924 HOUSING BOEING737 737* NM HYD SYSTEM CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 7306337037 1134 LARGE CRACK IN (D) PORT. PROBABLE CAUSE: FATIGUE CRACK. (MECHANIC FSX, JOB NR 175957) 2L72 4F RTA16WE 20030509000892003050900089NM 2003 5 9 HOC2003F00017 120030429A5313 STRINGER BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK, STRINGER AT 15L, STA 720B-720 WAS FOUND CRACKED. 2L72 4F4 FRTA16WE E2EA 20030509001472003050900147WP 2003 5 9 AMTA200300461 120030404A52101281T10033 ACTUATOR LKHEED1011 10113853 5265020WP PAX DOOR INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 FOUND L1 DOOR FAILS TO CLOSE ELECTRICALLY. REMOVED AND REPLACED L1 DOOR ACTUATOR ASSEMBLY IAW MM 52-12-01. OPS NORMAL. (M) 2L73 4F A23WE 20030509001532003050900153NM 2003 5 9 AMTA200300466 120030406A33508100022608 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11522AT 29330 EGRESS FLOOR TRACK INOPERATIVE FROM ROW 35 BACK. REMOVED AND REPLACED LIGHT ASSEMBLY ROW 35 IAW AMM 33-51-11, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030509001692003050900169NM 2003 5 9 USAA030038 120030410A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU35259 27124 CLT - FOUND FLOORBEAM CORRODED .5 INCH BY .75 INCH, STATION 1640 LBL 40, RBL 30 UPPER SURFACE. FULL REPLACEMENT OF UPPER STRUCTURE, ADDED WEIGHT OF REPAIR 4.3 LBS PER TR 53-15-01. (M) 2L72 4F RTA2NM 20030513000032003051300003 2003 5 13 ABXA030140 420030502A221025866865 COMPUTER DOUG DC9 DC931 3022065WP E & E BAY MALFUNCTIONED A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23948AX81 47065 AUTOPILOT PITCHED UP AND DOWN 1500 FT./MIN., THEN MADE AN UNCOMMANDED 30 DEGREES RIGHT TURN. AUTOPILOT CHECKED GOOD ON GROUND. REMOVED AND REPLACED PITCH AXIS COMPUTER AS PRECAUTION. PITCH COMPUTER CHECKED GOOD IAW DC-9 MM 22-13-01. 2L72 4F A6WE 20030513000062003051300006CE 2003 5 13 W0107481 120030311A243523080023 STARTER GEN LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP LEFT FAILED E HGPAO OTHER O OTHER NRNOT REPORTED 1 SW1510J 063 UNSCHEDULED LANDING. LT STARTER/GEN FAILED IN FLIGHT. UPON VISUAL INSPECTION IT WAS NOTICED THAT 50 PERCENT OF THE FAN BLADES WERE MISSING. IT ALSO APPEARS THAT A BEARING FAILURE TOOK PLACE DUE TO SHAFT BEING SIEZED. 2L72 4F4 FRTT00008WIE6WE 20030513000362003051300036NM 2003 5 13 03FDEA00709 120030507A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030513000502003051300050EU 2003 5 13 00089 120030509A2822 PUMP AMD FALCONFALCON20 2730103EU RT FUEL BOOST FAILED E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05699TW 050 PILOT REPORTED THAT DURING CLIMBOUT, RIGHT BOOST PUMP FAILED. RETURNED TO ADS FOR MAINTENANCE. R & R RT BOOST PUMP LEAK AND OPS CHECKS GOOD. 2L72 4F RTA7EU 20030513000642003051300064NM 2003 5 13 CALA0300236 120030509A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM STA 992-1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 992-1006, RBL 7. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030513001192003051300119EA 2003 5 13 QXEA0300467 120030413A5320 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 INTERCOSTAL IMMEDIATELY FORWARD OF REAR PRESSURE BULKHEAD IS CRACKED AT HYDRUALIC LINE FEED THROUGH OF LEFT HAND SIDE. REPAIRED IAW HORIZON AIR EO R-29-07. 2L72 4F RTA21EA 20030513001412003051300141NM 2003 5 13 CH1A200395043 120030416A5320 DOUBLER BOEING727 727290 138408WNM LAVATORY FLOOR CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FWD. LAV. FLOOR PAN DOUBLER LOCATED BETWEEN BS300 AND BS 312 AT RBL 44 TO RBL 52 CORRODED 2L73 4F A3WE 20030513002152003051300215WP 2003 5 13 ABXA030138 120030418A5250AR25291GR41 LOCK DOUG DC8 DC863F 302198FWP COCKPIT DOOR BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 AFTER PRE-DEPARTURE CHECK WAS COMPLETED. CREW WAS UNABLE TO OPEN COCKPIT DOOR. FOUND DOOR LOCK PLUNGER BROKEN IN LOCKED POSITION. INSTALLED SLIDE LOCK ON FLIGHT COMPARTMENT SIDE OF COCKPIT DOOR. VERIFIED THAT LOCK WAS OPERABLE FROM INSIDE THE COCKPIT. REPLACED COCKPIT DOOR HANDLE IAW REA D852-47190. COCKPIT DOOR HANDLE OPS CHECKED GOOD WHEN DOOR OPENED AND CLOSED. 2L74 4F 4A25 20030513002302003051300230SO 2003 5 13 C2XA03SH120 120030425A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 DURING C CHECK STRINGER 19 RIGHT AT FRAME 52 WAS FOUND CHAFFED. MAITENANCE REMOVED DAMAGE AND REPAIRED AFFECTED STRINGER IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030513002422003051300242EA 2003 5 13 ASOA03158 120030411A5315601R53037D2A FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOORBEAMS AT BL 9 IN THE SERVICE DOOR AREA WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT FLOORBEAMS (P/N'S 601R53-037K2A AND 601R53-037K3A) AT BL 9 IN THE SERVICE DOOR AREA, IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20030513003012003051300301EA 2003 5 13 ASOA03163 120030415A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 FLT 4425 - DURING A GROUND INSPECTION IN ATL, THE FORWARD EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-CONNECTED THE FORWARD EMERGENCY FLOOR LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030513003042003051300304EA 2003 5 13 ASOA03166 120030418A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURNG A C-CHECK IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030513003052003051300305EA 2003 5 13 ASOA03167 120030418A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE RIGHT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 AND BETWEEN 13 AND 14 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 AND BETWEEN 13 AND 14 IAW ASA EO 600-53-0069 AND ASA EO 600-53-0088. (M) 2L72 4F RTA21EA 20030514000062003051400006NM 2003 5 14 AALA20030360 120030320A3397 WIRE BOEING767 767223 1385123NM EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21338AA 22335 DURING OVERNIGHT MAINTENANCE, MID GALLEY RIGHT EMERGENCY EXIT FLOOR FLOOD LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030514000152003051400015EA 2003 5 14 ASOA03181 120030425A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION CRCRUISE 1 SO11906EV 7642 DURING CRUISE THE FLAPS FAILED AT ZERO DEGREES. THE CREW COMPLIED WITH QRH PROCEDURES BUT WAS UNABLE TO CLEAR THE FLAP FAILURE PROBLEM. AN EMERGENCY WAS DECLARED AND TH AIRCRAFT LANDED SAFELY IN CAK. MAINTENANCE COMPLIED WITH AD 98-20-01, PERFORMED FIVE OPERATIONAL CHECKS OF THE FLAPS SYSTEM AND RESET THE FLAPS. OP CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514000232003051400023SO 2003 5 14 ASOA03129 120030325A571312016085002 STRINGER EMB 120 EMB120ER 3260203SO RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11267AS 120198 DURING AN 'A' CHECK IN TXK, THE RIGHT WING STRINGER NR 10 LOCATED CLOSE TO RIB NR 3 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WING STRINGER NR 10 CLOSE TO RIB NR 3 IAW SRM 57-20-03. (M) 2L72 4T RTA31SO 20030514000252003051400025NM 2003 5 14 AALA20030312 120030313A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 19B INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 19B ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030514000262003051400026EU 2003 5 14 AALA20030364 120030320A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211455K 11467 DURING OVERNIGHT MAINTENANCE, RIGHT REAR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT REAR OVERWING EMERGENCY LIGHT ASSEMBLY. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030514000332003051400033NM 2003 5 14 AALA20030372 120030326A3350 BALLAST BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21339AA 22336 DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LEFT OVERWING EMERGENCY EXIT LIGHTS BALLAST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030507000122003050700012EU 2003 5 7 AUS20030321 120030312A21507786833 HEAT EXCHANGER FOKKERF27 F27MK50 EU PWA PWA120PW125B NE CABIN COOLING ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) SMOKE AND FUMES EVIDENT IN CABIN. INVESTIGATION COULD FIND NO CAUSE BUT THE LT HEAT EXCHANGER HAD BEEN REPLACED PRIOR TO THE FLIGHT. THE AIR CONDITIONING SYSTEM WAS OPERATED ON THE GROUND FOR TWENTY MINUTES UNTIL THE SMOKE/ODOR DISAPPEARED. 2H72 4T4 TRTA817 E20NE 20030507000192003050700019NM 2003 5 7 AUS20030325 120030312A324226123121 BRAKE BOEING737 737800* NM GE CFM56 CFM567B24 NE LT MLG FAILED W O OTHER O OTHER LDLANDING 1 AUS (AUS) LT MAIN LANDING GEAR INBOARD BRAKE ASSEMBLY FAILED. 2L72 4F4 FRTA16WE E00055EN 20030507000202003050700020EU 2003 5 7 AUS20030326 120030318A5315D53112692200000 FLOORBEAM AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FLOORBEAM CONTAINED LEVEL 2 CORROSION IN AREA LOCATED AT THE AFT END OF THE DUMMY RAIL AT FRAME 16. AREA OF CORROSION 63.5MM BY 50.8MM WITH A DEPTH OF 2.54MM (2.5IN BY 2IN BY 0.10IN DEEP). FOUND DURING INSPECTION IAW J9-IA53-0410. 2L72 4F4 FRTA46NM E29NE 20030507000302003050700030 2003 5 7 AUS20030334 420030314A34604052506941 FMC BOEING767 767338 1385151NM GE CF6 CF680C2* GL COCKPIT FAILED W O OTHER O OTHER CLCLIMB 1 AUS 95108447 (AUS) FLIGHT MANAGEMENT COMPUTER (FMC) FAILED. BOTH UNITS AFFECTED. 2L72 4F4 FRTA1NM E23EA 20030507000332003050700033 2003 5 7 AUS20030337 420030209A34189754421421 TRANSMITTER PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL STALL WARNING FAILED W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) ANGLE OF ATTACK (AOA) TRANSMITTER FAULTY. INSPECTION FOUND THEVANE BEARING ROUGH TO ROTATE AND VANE STICKING. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030507000452003050700045NM 2003 5 7 AUS20030344 120030311A276165448517 ACTUATOR BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU DRAG CONTROL LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) GROUND SPOILER ACTUATOR LEAKING. 2L72 4F4 FRTA16WE E21EU 20030507000562003050700056CE 2003 5 7 AUS20030355 120030227A275014601007 CONTROL CABLE CESSNA337 337B 2075706CE CONT O360 IO360D 17025SO MCAULY2AF34CD2AF34C59 GL TE FLAPS FRAYED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT INBOARD FLAP CABLE CONTAINED BROKEN STRANDS LOCATED IN AREA APPROXIMATELY 25.4MM TO 38.1MM (1IN TO 1.5IN) FROM THE INBOARD BELLCRANK TURNBUCKLE. 1H72 3O3 O A6CE E1CE 5 CP5EA 20030507000702003050700070EU 2003 5 7 AUS20030362 120030321A21409803811824 POTENTIOMETER PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL HEATING SYSTEM OUT OF ADJUST W O OTHER J WARNING INDICATION DEDESCENT 1 AUS 1831 (AUS) AIRCRAFT HEATING SYSTEM POTENTIOMETER INCORRECTLY SET. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030507000862003050700086EU 2003 5 7 AUS20030374 120030326A2822S2653005 CIRCUIT BREAKER BAC 146 146100A 1500260EU LYC ALF502ALF502R3A 41580NE FUEL BOOST FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) RT OUTER FUEL BOOST PUMP CIRCUIT BREAKER OVERHEATED AND BURNED. HEAT FROM THE BURNED CB DAMAGED THE ADJACENT BRAKE FAN CIRCUIT AND CAUSED FUMES IN THE FLIGHT DECK AND CABIN. 2H74 4F4 FRTA49EU E6NE 20030507000892003050700089CE 2003 5 7 CA030414003 120030414A771231017253 TORQUE SENSOR BEECH 100 B100 1152919CE GARRTTTPE331TPE3316252B 01514WP ENGINE MALFUNCTIONED W O OTHER O OTHER CRCRUISE 1 CA (CAN) TORQUE SPLIT IN FLIGHT. INCREASE TO APPROX 160 FT/LBS GREATER ON LT SIDE. ON RUN UP LOST TORQUE INDICATION COMPLETLY ON RT ENGINE. TROUBLESHOOTING: INSTALL TEST GAUGE BETWEEN TORQUE SENSOR AND TORQUE TRANSDUCER. ONLY GET APP 15 PSIOUT OF UNIT. SHOULD BE 18.5PSI AT 150 FT/LBS 60 PSI AT 1875 FT/LBS.TORQUE SENSOR REPLACED ON RT ENG. RT ENG IS IN PROCESS OF LAB TESTING FOR DSC SHEET. WILL DO A LAB TEST ON LT ENGINE TO MAKE SURE NOTHING CHANGED FROM DSC SHEETS, (REASON TO CHECK THE LAB TESTER IS HERE.) BACKGROUND ON SENSOR ENGINE AT 3532.0 TSO 2867 CSN AUG. 29/2002 ENGINE DISSEMBLED TO COMPLETE WITH HSI, GBL, & S/B UPGRADE. ENG REASSEMBLED USING LIFE LIMITED PARTS :SENSOR TSO 2734.7 HRS AT INSTALLATION. 1L72 4T4 T A14CE E2WE 20030507001032003050700103EA 2003 5 7 CA030311006 120030305A2520269A55125 BELT SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA DRIVE SYSTEM CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) BELTS CRACKED TO FABRIC. BELT SET REPLACED. 1G71 3U3 O0 4H12 1E10 20030507001132003050700113CE 2003 5 7 AUS20030389 120030402A7720 PROBE CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE ENGINE TEMP SEPARATED W O OTHER EM VIBRATION/BUFFET OVER TEMP CLCLIMB 1 AUS (AUS) LT ENGINE T1 PROBE SHEARED. PROBE ENTERED ENGINE CAUSING DAMAGE TO SPINNER, FAN BLADES AND BYPASS STATORS. SUSPECT PROBE SHEARED DUE TO FOD. SMALL PIECES OF YELLOW PLASTIC MATERIAL WERE FOUND IN THE CORE STATOR VANES UPON ENGINE DISASSEMBLY. 1L72 4F4 F A22CE E1NE 20030507001332003050700133NM 2003 5 7 AUS20030400 120030406A3040 TERMINAL BOEING747 747438 NM RROYCERB211 RB211524G19 NE WINDSHIELD BROKEN W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) FIRST OFFICER'S NR 1 WINDOW TERMINAL BROKEN. WINDOW CHANGED. 2L74 4F4 FRTA20WE E30NE 20030506000292003050600029EA 2003 5 6 SWIA200311880 120030417A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSCONTAMINATED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07910SW 7566 FRONT HALF OF EMERGENCY LIGHT STRIP ON CABIN FLOOR DOES NOT ILLUMINATE. CLEANED MOISTURE FROM WIRE STRIP CONNECTIONS ON EMERGENCY LIGHTS. OPS CHECK NORMAL. 2L72 4F RTA21EA 20030514000392003051400039NM 2003 5 14 PCAA0304070 120030427A323382910016009 ACTUATOR DHAV DHC8 DHC8102 2809003NM NLG SLUGGISH A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13807EX29407 292 AFTER SELECTING GEAR DOWN, NOSE GEAR MADE STRANGE NOISE. RED UNSAFE LIGHT STAYED ILLUM 10 SEC AFTER MAIN GEAR INDICATING GREEN. AFTER NOISE STOPPED NOSE GEAR EXTENDED. MX INSPECTED ACFT & BLED NR 2 HYD SYS. TEST FLT SATIFACTORY. ACFT RETURNED TO SERVICE. NOSE GEAR DID NOT EXTEND NORMALLY AN ALTERNATE EXTENSION PERFORMED. MX PERFORMED TEST ON PROXIMITY SENSOR ELECTRONICS UNIT & INSPECTED NOSE GEAR. LANDING GEAR SWUNG, COULD NOT DUPLICATE. TEST FLT UNSATISFACTORY. CREW REPORTED THE NOSE GEAR WAS VERY SLOW TO RESPOND. MX REPLACED NOSE GEAR DOOR ACTUATOR, NOSE GEAR SELECTOR VALVE UNDER COCKPIT FLOOR & REPLACED RELAY 3261-K7. OPS & LEAK CHECK GOOD. GEAR SWUNG, NO DEFECTS NOTED. TEST FLT SATISFACTORY. 2H72 4T RTA13NM 20030514000682003051400068NM 2003 5 14 SWAA030967 120030430A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR FUSELAGE SKIN CRACKED AT LOWER FWD CORNER, BS 955 AT STR 20L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030514000692003051400069 2003 5 14 SWAA030968 420030429A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030514000702003051400070NM 2003 5 14 SWAA030969 120030429A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT ENTRY & AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH AFT ENTRY AND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20030514000722003051400072NM 2003 5 14 SWAA030938 120030427A56105717623122 WINDOW BOEING737 7372H4 138448CNM COCKPIT LEAKING A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29089SW 22904 AIR TURNBACK. FIRST OFFICER'S SLIDING WINDOW LEAKING EXCESSIVELY. FOUND, WINDOW PRESS SEAL FAILED. REMOVED AND REPLACED FIRST OFFICER'S SLIDING WINDOW PER MM. 2L72 4F A16WE 20030514000732003051400073 2003 5 14 SWAA030939 420030428A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030514000792003051400079NM 2003 5 14 SWAA030945 120030427A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CRACKED AT LBL 24, BS 669 & BS 672. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20030514000852003051400085NM 2003 5 14 SWAA030986 120030501A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP IN CABIN. REMOVED AND REPLACED EEPLS RECEPTICAL PER MM. 2L72 4F RTA16WE 20030514000932003051400093NM 2003 5 14 SWAA030994 120030504A52306547952 SKIN BOEING737 7373G7 1384595NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT END OF HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030514000952003051400095NM 2003 5 14 SWAA030996 120030504A52416545871 DOOR BOEING737 7377H4 1384404NM AFT SERVICE BINDING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 AFT SVC DOOR BINDING. REPAIRED AFT SVC DOOR PER SWA EA. 2L72 4F RTA16WE 20030514000962003051400096NM 2003 5 14 SWAA030997 120030505A2910A5116080260 LINE BOEING737 7377H4 1384404NM HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW29716SW 27850 DIVERSION, HYDRAULIC A-SYS FLUID QTY LOSS NR HYD A-SYS MODULE AND ACOUSTIC FILTER. REMOVED AND REPLACED HYD LINE PER MM. 2L72 4F RTA16WE 20030513000122003051300012NM 2003 5 13 250TR0013 120030429A5320 ANGLE BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION ON LEFT TRANSITION ANGLE BS440 TO BS480 (FORWARD CARGO BIN). REPLACED CORRODED SECTION OF TRANSITION ANGLE PER EA53-114. 2L72 4F RTA16WE 20030513000712003051300071EU 2003 5 13 RAIA00304121 120030425A2612ETCEU CONVERTER JETAIRJETSTMJETSTM4101 1500501EU FIRE DETECTOR FAILED A RAIAO OTHER N FALSE WARNING LDLANDING 1 CE03564HK3468 41081 AFT CARGO FIRE WARNING INDICATION DURING DECENT INTO STL. MAINTENANCE REMOVED AND REPLACED AFT CARGO FIRE WARNING CONVERTER. OPS CK OK. 2L72 4T RTA41NM 20030513001382003051300138NM 2003 5 13 F3LA200300116 120030411A5320 FLOOR SUPPORT BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 3468 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORTS BETWEEN STA. 847 AND 867. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53. 2L72 4F RTA16WE 20030513001592003051300159NM 2003 5 13 QXEA0300461 120030415A243511521062 STARTER GEN BOMBDRDHC8 DHC8401 1390041NM NR 1 INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09405QX603 4047 ON FLIGHT NUMBER 2328, EN-ROUTE, DC BUS CAUTION LIGHT ILLUMINATED. ALSO NR 1 GEN, AUX BATTERY AND STANDBY BATTERY ILLUMINATED. SYSTEMS RESET PER CHECKLIST BUT NR 1 STALL FAIL, NR 2 SYSTEM FAIL AND PUSHER SYSTEM FAIL CAUTION LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED NR 1 DC STARTER GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030506000512003050600051WP 2003 5 6 UPS03840455 120030331A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, AFT FUSE L17R AT END FITTING CRACKED. REMOVED L17RT END FITTING TO FOM RECEIVED NEW LONG PO 5649327-44. LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW L17RT & END FITTING IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030506001032003050600103EU 2003 5 6 MALA030243 120030423A27708377M7 ACTUATOR SAAB SF340 SF340A 7850100EU GUST LOCK MALFUNCTIONED A MALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL1568XJ 340A068 PILOT STATED WHILE OUT ON RUNWAY PRECEDING FLIGHT 3183, RUDDER GUST LOCK DID NOT RELEASE UNTIL 20 SECONDS LATER FROM RELEASING HANDLE. ONCE FULL TRAVEL ON RUDDER WAS PRESENT THE LIGHT WENT OUT. TAXIED OFF RUNWAY AND RETURNED TO GATE. MAINTENANCE REPLACED THE RUDDER GUST LOCK ACTUATOR PN/OFF 8618M16, PN/ON 8377M7, SN/OFF 95110060, SN/ON M343 IAW AMM 27-72-10. OPS CHECKS GOOD. 2L72 4T RTA52EU 20030506001052003050600105EU 2003 5 6 MALA030245 120030424A5220 COVER SAAB SF340 340B 7860101EU EMERGENCY DOOR DISLODGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15445XJ 340B445 RT EMERENCY DOOR COVER FELL OFF (DOOR HANDLE COVER). MAINTENANCE RESECURED COVER. 2L72 4T RTA52EU 20030506001062003050600106NM 2003 5 6 DHL2003751008 120030427A2612 POWER UNIT BOEING727 727264 138408MNM FIRE DETECTOR FAILED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 APU FIRE TEST INOPERATIVE. TROUBLESHOT TO FIRE DETECTOR POWER UNIT. REPLACED PER B-727 M/M 26-15-0. CHECKED GOOD. 2L73 4F A3WE 20030506001722003050600172WP 2003 5 6 ASAA0380249 120030307A531359360281 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, STATION 1015 LONGERON 30 CORROSION AT FASTENER HOLES. SPOT FACED CORROSION PER EA 5310-02158. (M) 2L72 4F A6WE 20030506001782003050600178WP 2003 5 6 ASAA0380246 120030307A574059541709 MOUNT DOUG DC9 DC982 3022082WP PANEL GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, RIGHT WING NR 1 INBOARD SLAT CLOSE OUT MOUNT BROKEN. REPLACED BRACKET PER SRM. (M) 2L72 4F A6WE 20030506001832003050600183WP 2003 5 6 ASAA0380256 120030307A53305920323555 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DUIRNG 30K CHECK, FOUND FUSELAGE SKIN DAMAGED BETWEEN LONGERONS 19R AND 20R AT STATION 365. INSTALLED REPAIR DOUBLER PER SRM. (M) 2L72 4F A6WE 20030506001882003050600188WP 2003 5 6 ASAA0380194 120030302A5347SRO95301157001 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND SEAT TRACK UPPER SURFACE INCLUDING INBOARD AND OUTBOARD FLANGES ARE CORRODED. REPLACED DAMAGED TRACK SECTION PER SRM 53-05. (M) 2L72 4F A6WE 20030507000432003050700043CE 2003 5 7 AUS20030342 120030320A8120 BEARING CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL TURBOCHARGER FAILED W O OTHER E VIBRATION/BUFFET CLCLIMB 1 AUS 562 (AUS) TURBOCHARGER BEARING FAILED. TURBINE RUBBING ON HOUSING. 1L72 3O3 O A7CE E8CE 5 CP22EA 20030507001042003050700104CE 2003 5 7 CA030416001 120030415A30209091009913 TUBE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA ANTI ICE SYS CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) RT OUTBOARD ANTI-ICE FLEX TUBE FOUND CRACKED BOTH TOP AND BOTTOM AT ATTACH ANGLES. REPLACED WITH NEW PART. 1L72 3T4 TRT3A20 E4EA 20030507001642003050700164WP 2003 5 7 GTIA030140 120030312A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DETERIORATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 MAIN CABIN STA 807 TO STA 826 CENTER FLOORBOARD HAS SOFT/ MUSHY AND DETERIORATED. FABRICATED NEW FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20030507001662003050700166CE 2003 5 7 FPI2003F00009 120030326A57110024300185 SPAR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO WING CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO151844712810 TH883 AT ANNUAL INSPECTION, CRACKS WERE FOUND IN FORWARD AND AFT CARRY THRU SPAR WEB FACES. THE CRACKS WERE FOUND ABOVE THE INSTALLED WEB REPAIR KITS AT THE UPPER SPAR FITTINGS. THESE NEW CRACKS APPEAR TO HAVE BEEN CAUSED BY THE INSTALLATION OF THE WEB REPAIR ITS TRANSFERING STRESS TOT HE UPPER CORNERS OF THE WEB. IAW AD. 1L72 3O3 O 3A16 E5CE 20030507001682003050700168WP 2003 5 7 GTIA030147 120030221A5330 PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE FUSELAGE DETERIORATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO ST 256 LBL 44 INCHES (21X56) FLOOR PANEL SOFT/ MUSHEY, DETERIORATED CORR. INSERTS. 2L72 4F4 FRTA6WE E2EA 20030507001732003050700173NM 2003 5 7 MEX2003129 120030410A2425 SYMBOL GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE MALFUNCTIONED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23169PL 53175 AIRCRAFT RETURNED TO PLATFORM, AT FIRST OFFICIAL SIDE DURING ENGINES STARTING WERE OF ND AND PFD INDICATIONS OFF. THE SYMBOL GENERATOR DIGITAL COMPUTER WAS RESEATED IAW MM, TESTS CORRECT. 2L72 4F4 FRTA6WE E2EA 20030507001752003050700175WP 2003 5 7 GTIA030184 120030226A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE SUB FLOOR CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK33528 49503 PAX CABIN STA 160 RBL 50 SUB FLOOR CORRODED. REMOVED WEB. FABRICATED NEW WEB AND DOUBLER. INSTALLED WEB AND DOUBLER. 2L72 4F4 FRTA6WE E2EA 20030513001722003051300172NE 2003 5 13 2003UALA00380 220030412A7230 COMPRESSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A UALAEC ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29593UA 28144 NR 2 ENGINE COMPRESSION STALL ON TAKEOFF 2L72 4F4 FRTA2NM E17NE 20030513002352003051300235CE 2003 5 13 GLBA2003055 120030424A2840 TRANSMITTER BEECH 1900 1900D 1154162CE FUEL FLOWMETER FAILED A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03195GL3199 UE195 RT FUEL FLOW INDICATOR SHOWS ZERO INOP, R&R RT FUEL FLOW TRANSMITTER 2L72 4T RTA24CE 20030513002762003051300276WP 2003 5 13 AALA20030194 120030211A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21218AA 49168 FOUND CRACK IN FUSELAGE SKIN STATION 138 LONGERON 13L. STOP DRILLED END OF CRACK AND APPLIED NON-PRESSURIZED DOUBLER PATCH PER SRM 53-01-00 FIG 2 SHEET 3, SRM 53-34-00 PAGE 17 FIG 4 SHEET 2, PAGE 16 FIG 4 SHEET 1, SRM 51-01-00 PAGE 1, AND AARD 53-30-00-02 PAGE 1. (M) 2L72 4F A6WE 20030514000562003051400056NM 2003 5 14 SWAA030979 120030501A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, FWD END OF NR 2 RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030514000612003051400061NM 2003 5 14 SWAA030960 120030429A259765C19901 CABLE BOEING737 7373H4 1384600NM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030514000872003051400087 2003 5 14 SWAA030988 420030504A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030514000992003051400099NM 2003 5 14 SWAA031000 120030505A3350 LENS BOEING737 737301 1384611NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. 2L72 4F RTA16WE 20030514001052003051400105NM 2003 5 14 SWAA031006 120030505A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030514001112003051400111NM 2003 5 14 PCAA0305073 120030512A2930 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM HYD SYSTEM ILLUMINATED A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13817EX 191 SYR-FLIGHT 3992. CREW REPORTED ROLL SPOILER INBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED DURING FLIGHT FOLLOWED BY NR 1 ISOLATION VALVE CAUTION LIGHT. MAINTENANCE INSPECTED AND RAN AIRCRAFT WITH ALL HYDRAULIC SYSTEMS OPERATING FOR 1 HOUR. NO LEAKS WERE NOTED. ALL SYSTEMS OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030514001212003051400121NM 2003 5 14 SWAA031032 120030507A5753 SKIN BOEING737 7373K2 13844BANM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV BN778 23738 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED ON INBOARD SIDE. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20030514001362003051400136NM 2003 5 14 SWAA031022 120030507A29106544580 MODULE BOEING737 7373Q8 1384670NM RT MLG WW LEAKING A SWAABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29685SW 23401 DIVERSION, DECLARED EMERGENCY. A SYSTEM HYDRAULICS FAILED, PRESSURE / QUANTITY ZERO. REMOVED AND REPLACED A SYSTEM MODULE O-RING AND REMOVED AND REPLACED CASE DRAIN FILTERS PER MM. 2L72 4F RTA16WE 20030514001422003051400142NM 2003 5 14 SWAA031042 120030508A57546573714 SKIN BOEING737 7373Q8 1384670NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT CRACKED ON LOWER SKIN JUST BELOW RETRACT ACTUATOR. REPAIRED NR 4 L/E SLAT PER SRM. 2L72 4F RTA16WE 20030514001532003051400153NM 2003 5 14 SWAA031053 120030511A5311 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND OUTER FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030514001562003051400156NE 2003 5 14 VNAA0305004 220030502A73208110993 HMU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE FAILED A VNAAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL07441JS175869203 3059 AT 13,000, THE CREW BEGAN GETTING A LEFT HAND ENGINE SURGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL. THE CREW THEN DIVERTED TO PHL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY AT PHL. TWO MECHANICS FROM PIT WERE SENT TO INSPECT THE AIRCRAFT. MAINTENANCE THEN REPLACED THE HYDROMECHANICAL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030514001662003051400166NE 2003 5 14 P5CA0300859 220030412A7200 ENGINE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 WP23920FT 22237 662258 ENGINE START NR 4 ENGINE HAS OIL LEAKING INTO TAILPIPE NR 4 FROM BEARING COMPARTMENT. REPLACED NR 4 ENGINE. 2L74 4F4 F A20WE E3NE 20030514001802003051400180NM 2003 5 14 377PA0016 120030505A3350 LIGHT BOEING737 7373L9 1384470NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05377PA 23718 FLOOR PATH LIGHTING INOP ROWS 18-26. REPLACED LAST SECTION OF FLOOR PATH LIGHT STRIP. 2L72 4F RTA16WE 20030514001812003051400181 2003 5 14 372PA0025 420030505A2230 COMPUTER BOEING737 737306 13844BGNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 SO05372PA 23546 AUTO THROTTLES DISCONNECT WHEN SETTING TAKEOFF POWER (SEEMS TO HAVE 5 PERCENT LESS N1 ON NR 2 ENGINE) CRUISE WORKS FINE. COMPLETED FMS BITE TEST FOUND FAILURE CODE FOR CABLE SYSTEM. INSPECTED ENGINE CABLE SYSTEM AND LUBRICATED. CHECKS GOOD PER MM 22-04-10. 2L72 4F RTA16NE 20030514001822003051400182NM 2003 5 14 03FDEA00682 120030505A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 CABIN- EXFOLIATION CORROSION OBSERVED ON SEAT TRACK UPPER LEG AT STA 1383 RBL 9. 2L73 4F RTA22WE 20030514001862003051400186NM 2003 5 14 03FDEA00663 120030501A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 THE FUSELAGE OUTER SKIN IS CHAFED AT BS 720D+13 INCHES STR 19L. BLENDED CHAFED AREA 1 X 2 X .027 FROM ORIGINAL .064 OUTER SKIN BS 720D+13 INCHES STR 19L. FOUND OUT OF LIMITS PER SRM 53-30-01. REPAIRED CHAFED AREA PER SRM 53-30-03 AND FED EX SR 27-57-056. 2L73 4F RTA3WE 20030514001962003051400196NM 2003 5 14 03FDEA00700 120030507A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING - O/B FLAP I/B HINGE (FLAP SIDE), LWR PIVOT, I/B LUG HOLE CORRODED. RT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT, I/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68415 WINGS- RIGHT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030514002022003051400202NM 2003 5 14 03FDEA00687 120030506A5320 WEB BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 WHILE WORKING FED EX NRC N00312 FOUND CORROSION ON WEB AT RBL 6, BS 1146-1166, WL 146. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED WEB PER SRM 51-30-2. 2L73 4F RTA3WE 20030514002042003051400204NM 2003 5 14 03FDEA00716 120030430A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING, FOUND OUTBOARD FLAP, INBOARD HINGE FITTING, FLAP SIDE TO FLAP MOUNTING HOLES LOCATION QTY 6 EACH CORRODED. CORROSION ON LH WING , O/B FLAP I/B HINGE FITTING, FLAP SIDE TO FLAP MOUNTING HOLES REMOVED AS PER SRM 51-21-01 VOL II & SRM 51-31-01 VOL II. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69254 WINGS- LT OUTBOARD FLAP INBOARD AFT OVERSIZE HOLES- REPAIR. 2L73 4F RTA22WE 20030514002122003051400212NM 2003 5 14 03FDEA00582 120030424A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 BS 1090 FRAME PUNCTURED BY FLOOR PANEL FASTENERS, LBL 21 WL 156. INSTALLED THE FABRICATED DOUBLER AT BS 1090 FRAME LBL 21 WL 156 IAW SRM 51-40-3. REINSTALLED STANTION PER SRM 51-30-2. 2L73 4F RTA3WE 20030514002152003051400215NM 2003 5 14 03FDEA00661 120030501A2611 SMOKE DETECTOR BOEING727 727200 138407ENM MAIN CARGO MALFUNCTIONED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25486FE 21489 NR 5 MAIN CARGO SMOKE DETECTOR CAME ON, ON T/O ROLL AT APPROX 20 KTS. REMOVED AND REPLACED NR 5 MAIN CARGO SMOKE DETECTOR IAW FED EX M/M 26-16-001-4. 2L73 4F RTA3WE 20030515000052003051500005EA 2003 5 15 03132621 120030512A2560P4010021 BATTERY CNDAIRCL600 CL6002B19 1900309EA FLASHLIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BATTERY IN THE EMERGENCY FLASHLIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513001492003051300149NM 2003 5 13 CH1A200395047 120030417A5313 STRINGER BOEING727 727290 138408WNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 6 CRACKS ON STR 26L LOWER ROW OF FASTENERS FROM BS 520 TO BS 540 2L73 4F A3WE 20030513002252003051300225NE 2003 5 13 UIAFAA9202 220030424A7314 PUMP DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 2 ENGINE FAILED Z A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 TW0015223 404 12372 NR 2 ENG FAILURE AFTER TAKE-OFF; IAW PWC MM 72-01-40RPL NO.2 ENG FMC AND FUEL PUMP AND IAW AMM 71-00-00 GROUND ENGINE RUNUP CHECK NORMAL. 2H72 4T4 TRTA13NM E20NE 20030513002292003051300229SO 2003 5 13 C2XA03SH119 120030425A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 DURING C CHECK STRINGER 19 LEFT AT FRAME 52 WAS FOUND CHAFED. MAITENANCE REMOVED DAMAGED SECTION AND REPAIRED STRINGER IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030513002832003051300283WP 2003 5 13 AALA20030195 120030211A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21218AA 49168 FOUND TWO CRACKS AT FASTENERS THROUGH FUSELAGE SKIN STATION 1380, LONGERON 14 RT. .25 INCH STOP DRILLED END OF TWO CRACKS AT STATION 1380 RIGHT DYE CHECK. END OF STOP DRILLED VERIFIED BY QA, 006, INSTALLED DOUBLER PER SRM CH 53-01-00 FIG 2 SHEET 3 AND AARD 53-30-00-2. (M) 2L72 4F A6WE 20030513002902003051300290WP 2003 5 13 AALA20030213 120030205A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21574AA 53151 FOUND CORROSION ON CUSP WEB ABOVE MID-CARGO DOOR AT STATION 661. CUTOUT CORRODED SECTION OF CUSP AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. (M) 2L72 4F A6WE 20030513002972003051300297NM 2003 5 13 USAASB03032 120030301A3397 WIRE BOEING737 7374B7 1384702NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 CLT - MAINTENANCE REPORTED THE SMALL ROUND EMERGENCY LIGHT, WHICH IS SEAT MOUNTED AT ROW 12C, WILL NOT ILLUMINATE. MAINTENANCE FOUND THE WIRES DISCONNECTED. RECONNECTED WIRES. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030507001762003050700176WP 2003 5 7 GTIA030185 120030226A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 PAX CABIN STA 160 RBL 54 FLOOR SUPPORT CORRODED. FABED NEW FLOOR SUPPORT. REMOVED FLOOR SUPPORT, INSTALLED FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030507001882003050700188SO 2003 5 7 YEB2003F00000 120030401A2421 SLIP RING PIPER PA46 PA46350P 7104602SO PWA PT6 PT6A34 52043EA ALTERNATOR FAILED A YEBRO OTHER O OTHER NRNOT REPORTED 1 CE05881DB8 4622067 PCERB0062 INSTALLED NEW STANDBY ALTERNATOR MANUFACTURED. ALTERNATOR FAILED AFTER 8.1 HOURS TIME IN SERVICE. TEARDOWN INSPECTION REVEALED THAT THE CARBON BRUSH IN THE AFT POSITION WAS COMPLETELY WORN OUT AND THE BRUSH SPRING HAD WRAPPED AROUND THE SLIP RING AND SHAFT AND HAD DAMAGED THE SLIP RING. ALTERNATOR RETURNED TO MFG FOR WARRANTY REPAIRS. 1L71 3O4 TRTA25SO E4EA 20030507001952003050700195NM 2003 5 7 CH1A200395023 120030411A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOORBEAM AT BS 312 HAS CORROSION AROUND FASTENER HOLES BETWEEN RBL 12 TO LBL 62. 2L73 4F A3WE 20030507001972003050700197NM 2003 5 7 CH1A200395025 120030411A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON BS 1030 FLOORBEAM UPPER STRUCTURE AROUND FASTENER HOLES LBL 24 & RBL 24. 2L73 4F A3WE 20030507001982003050700198NM 2003 5 7 CH1A200395021 120030411A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOORBEAM STABILIZER STRAP AT BS 358 LBL 23 IS CRACKED. 2L73 4F A3WE 20030507002012003050700201NM 2003 5 7 CH1A200395028 120030410A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON BS 1090 FLOORBEAM UPPER STRUCTURE AT LBL 12. 2L73 4F A3WE 20030508000062003050800006NM 2003 5 8 DLM88030335 120030404A2150 TRANSDUCER DOUG MD88 MD88 3023688NM AC PACKS CONTAMINATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27901DL 49532 ON CLIMBOUT FROM ATL TO PIT CREW SMELLED SOMETHING BURNING. COUULD NOT IDENTIFY SOURCE. ODOR WAS STRONGER IN AFT CABIN THEN IN FWD CABIN. ALSO VERY STRONG IN COCKPIT. (ELECTRICAL ODOR) - PERFORMED DUCT BURNOUT 2L72 4F RTA6WE 20030508000092003050800009CE 2003 5 8 042703 120030427A3241 BRAKE ASSY LEAR 35 35A 5170602CE ANTI SKID FAILED E ESUAO OTHER O OTHER TXTAXI/GRND HDL 1 CE0372LL 275 WHILE TAXING ON THE RAMP, BOTH BRAKES AND STEERING FAILED. CREW USED EMERGANCY BRAKES TO STOP THE AIRCRAFT. NOSE OF AIRCRAFT BUMP INTO THE RAILING. MAINTENANCE SUSPECTS ANTI-SKID SYSTEM. 2L72 4F A10CE 20030508000132003050800013NM 2003 5 8 QXEA0300532 120030504A5210 SCREW DHAV DHC8 DHC8202 2809007NM HANDRAIL LOOSE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09358PH 506 PDX- ON FLIGHT 2191 MAIN CABIN DOOR OPENED PARTIALLY. ONLY 25 PERCENT. FOUND NUT MISSING AND SCREW BACKED OUT FROM AFT HANDRAIL LINKAGE. REPLACED NUT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030508000382003050800038CE 2003 5 8 GLBA2003059 120030504A561010138402524 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT CRACKED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03261GL1293 1293 UE261 RT WINDSHIELD CRACKED IN FLIGHT. 2L72 4T RTA24CE 20030508000412003050800041NM 2003 5 8 CH1A200395036 120030414A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON CABIN FLOOR SUPPORT AT LBL 12 BS 1030 TO 1050 2L73 4F A3WE 20030508000462003050800046NM 2003 5 8 03FDEA00673 120030503A2612 SMOKE DETECTOR BOEING727 727200 138407ENM MAIN CARGO DECK FALSE INDICATIONA FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25479FE 21461 MAIN CARGO SMOKE LIGHT NR 4 CAME ON WITH ASSOCIATED ALARM WHILE ON FINAL APPROACH. LIGHT EXTINGUISHED ON ITS OWN AFTER APPROX. I MINUTE. COMPLIED WITH RED TABS AND LANDED UNEVENTFULLY. INTIAL MAIN DECK ( PRE-OFFLOAD ) INSPECTION REVEALED NO SMOKE, FUMES, OR ODOR. DOWN LOADED & CHECKED ALL CONTAINERS NO PROBLEMS FOUND, PERFORMED CARGO SMOKE OPS CHECK PER M/M 26-16-001-5, CHECK GOOD, NOTE: DRY-ICE SHIPPED IN POSITIONS 7 & 8 SUSPECTED CAUSE. 2L73 4F RTA3WE 20030508000472003050800047NM 2003 5 8 03FDEA00672 120030502A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25485FE 21488 DENT IN EXTERNAL FUSE SKIN AT BS 1105 BETWEEN STR 28 LEFT AND 29. FOUND DENT ON EXTERNAL FUSE SKIN AT BS 1105 BETWEEN STR 28 LEFT AND 29 TO BE OUT OF LIMITS. CUT OUT DAMAGED SKIN. FABRICATED REPAIR DOUBLER FOR SKIN. CUT OUT AT BS 1105 BETWEEN STR. 28 LEFT AND 29. ALODINED, PRIMED & INSTALLED IAW SRM 53-30-3. 2L73 4F RTA3WE 20030506001432003050600143CE 2003 5 6 AKG2003F00000 120030407A21213521000 MOTOR BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA VENT BLOWER FAILED B AKGRO OTHER O OTHER NRNOT REPORTED 1 CE05902PL1097 LJ1583 CREW HAD SMOKE IN THE CABIN AT CRUISE FLIGHT. TURNING THE VENT BLOWER OFF CLEARED THE SMOKE FROM THE CABIN. AFTER REMOVEING THE BLOWER ASSEMBLY FROM THE AIRCRAFT INSPECTION FOUND THAT THE MOTOR WAS LOCKED UP AND THE BRUSHES BURNED. 1L72 3T4 TRT3A20 E4EA 20030506001512003050600151NM 2003 5 6 TX22003F00000 120030415A49401152426245 STARTER BOEING737 737100 1384404NM GE CFM56 CFM56* 13802NE APU FAILED A TX2RO OTHER O OTHER NRNOT REPORTED 1 SW05108MS27 088C0343 33102 NPRM STATES TO REMOVE PART NUMBERS AND SERIES NUMBER AND REPLACE THESE ITEMS WITH A SERIES 7 OR GREATER. THE SERIES 7 UNIT WHEN INSTALLED FAILED. WHEN AN APU START WAS ATTEMPTED USING A SERIES 7 START CONVERTER UNIT. THE NEW UNIT EXPERIENCED A COMPLETE ELECTRICAL FAILURE. 2L72 4F4 F A16WE E2GL 20030514000102003051400010EU 2003 5 14 ASOA03130 120030326A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE EXTERIOR PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030514000312003051400031EU 2003 5 14 AALA20030256 120030301A3397 WIRE FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211411G 11369 DURING OVERNIGHT MAINTENANCE, NR 4 OVERHEAD 28 VOLT CENTER AISLE EMERGENCY STANDBY LIGHTING INOPERATIVE. REPAIRED NR 4 OVERHEAD 28 VOLT CENTER AISLE EMERGENCY STANDBY LIGHTING WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030514000472003051400047EA 2003 5 14 COMA0360235 120030509A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01716CA10679 7250 FLIGHT 5259 LANDING GEAR DISAGREE WARNING, NLG INDICATED UNSAFE. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030514000652003051400065NM 2003 5 14 SWAA030964 120030429A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 277 AT STR 15R & BS 360 AT STR 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030514000672003051400067NM 2003 5 14 SWAA030966 120030430A324426078251 TIRE BOEING737 7373H4 1384600NM NLG FAILED A SWAABA EMER. DESCENT UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SW29640SW 27713 AIR TURNBACK, DECLARED EMERGENCY. AFTER TAKEOFF DURING GEAR RETRACTION, SUSPECT BLOWN TIRE. FOUND, LT NLG TIRE TREAD SECTION MISSING. REMOVED AND REPLACED BOTH NR 1 & 2 NLG WHEEL AND TIRE ASSY PER MM. 2L72 4F RTA16WE 20030514000742003051400074NM 2003 5 14 SWAA030940 120030428A53116546569 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1006, STR 17R. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20030514000822003051400082NM 2003 5 14 SWAA030983 120030502A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 869, ABOVE STR 19L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030514000862003051400086 2003 5 14 SWAA030987 420030503A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030514000972003051400097 2003 5 14 SWAA030998 420030505A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF POSITION. REPOSITIONED EVACUATION SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030514001012003051400101NM 2003 5 14 SWAA031002 120030505A53146545866 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND KEELBEAM WEB CORRODED, BS 663 TO BS 727A RT SIDE. REPAIRED KEELBEAM PER SRM. 2L72 4F RTA16WE 20030514001152003051400115NM 2003 5 14 SWAA031026 120030508A3350610478 BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20030514001652003051400165NM 2003 5 14 P5CA0300864 120030412A5320 SPLICE BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LT BS 1480 WEB SPLICE PLATE 16 INCH CRACK NR 18 HOLE. REPAIRED PER SRM 51-30-02. 2L74 4F A20WE 20030514001922003051400192NM 2003 5 14 03FDEA00704 120030509A5330 TRIPLER BOEING727 727200 138407ENM MAIN CARGO DOOR WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 MAIN CARGO DOOR TRIPLER WEAR. COMPLIED WITH EA 7-5330-70376 BLENDED AREA, EDDY CURRENT INSP, NO CRACKS NOTED. OK FOR SERVICE. 2L73 4F RTA3WE 20030514002382003051400238WP 2003 5 14 GTIA030142 120030312A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 AFT PIT CRACKED FLOOR WEB AT FS1289-1309 LONG 18R. FAB DOUBLER. INSTALLED DOUBLER. 2L72 4F4 FRTA6WE E2EA 20030514002402003051400240SW 2003 5 14 ALGA086242 120030423A6230406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL UNIVERSAL ROUGH E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03607AL689 53264 FOUND BEARINGS ROUGH AND RATCHETING. 1G71 3U3 UO H2SW E1GL 20030515000242003051500024EA 2003 5 15 SWIA200311945 120030331A5411 RIB CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 LEFT PYLON RIB AT FS 605.00 CRACKED LOWER OUTBOARD FLANGE. FOUND DURING C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-21, AND 51-23-00. 2L72 4F RTA21EA 20030515000292003051500029EA 2003 5 15 03123671 120030503A339759465 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27671BR 7572 DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A WIRING CABLE FOR THE EMERGENCY FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515000352003051500035EA 2003 5 15 03121667 120030501A33508GS00542405 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27667BR 7535 DURING MAINTENANCE INSPECTION, THE FORWARD CABIN EMERGENCY EXIT SIGN WAS FOUND TO HAVE ONE LAMP INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515000392003051500039EA 2003 5 15 SWIA200311908 120030303A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 LEFT LOWER WING PLANK WS 148.019 FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA OF LEFT WING PLANK IAW REO 601R-57-21-130 REV D AND REO 601R-57-21-131 REV NC. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-131. NO CRACKS NOTED. 2L72 4F RTA21EA 20030515000422003051500042NM 2003 5 15 03122403 120030502A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27403FJ 3149 DURING PREFLIGHT INSPECTION THE CREW DISCOVERED THE 2ND SECTION OF EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030515000432003051500043EA 2003 5 15 03121628 120030501A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 DURING PREFLIGHT INSPECTION THE CREW DISCOVERED A CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030515000442003051500044SO 2003 5 15 SWIA200311918 120030425A3260 PLUNGER EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE MLG OUT OF ADJUST A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07224SW 120294 DURING TAKEOFF RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR DOWN AND RECEIVED ALL GEAR DOWN INDICATIONS. RETURNED TO LAX. ADJUSTED RIGHT GEAR DOOR PLUNGER. SWUNG GEAR NUMEROUS TIMES. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20030515000452003051500045EA 2003 5 15 03119632 120030429A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISCOVERED AN EMERGENCY EXIT SIGN AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030515000592003051500059SO 2003 5 15 C2XA03IA045 120030502A213314520402431 LINE EMB 135 EMB135LR 3260305SO OUTFLOW VALVE LOOSE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2717521 145378 THE CREW NOTED AN UNCONTROLABLE PRESSURE RISE ON TAKEOFF. THE CREW RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAINTENANCE TIGHTENED A LINE ON THE PNEUMATIC OUTFLOW VALVE, PERFORMED A OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030515000612003051500061CE 2003 5 15 DXTA200300025 120030502A3240 BRAKE CESSNA500 560CESSNA 2076750CE ANTI SKID SYS MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07306QS 5600266 NO BRAKING ACTION WITH LT OR RT PEDALS. ANTI-SKID LIGHT ILLUMINATED ONCE EMERGENCY BRAKING WAS SELECTED. FOUND FAULTY LT ANTI-SKID TRANSDUCER, REPLACED AND BLED SYSTEM. 2L72 4F RTA22CE 20030515000622003051500062WP 2003 5 15 DXTA200300027 220030503A7200 ENGINE RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP RIGHT SHUTDOWN E DXTAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL07886QS4236 258486 P107226 AT ALTITUDE WHEN RT THROTTLE FOR DESCENT THE RT ENGINE HAD UNNCOMMANDED SHUTDOWN IN FLIGHT, RESTART NO HELP. 2L72 4F4 FRTA3EU E6WE 20030515000652003051500065SO 2003 5 15 C2XA03CL097 120030501A3234745501 LEVER EMB 145 EMB145LR 3260212SO MLG INTERMITTENT A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2713553 145585 SYR FLIGHT 3181 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF. THE CREW CYCLED THE GEAR AND CONTINUED AS NORMAL. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030515000812003051500081SO 2003 5 15 C2XA03SH130 120030505A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713908 145465 SHV - DURING C-CHECK EXTERNAL REINFORCING ANGLE STIFFENER ON STRINGER 19R WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGE AND PERFORMED ANGLE REPAIR ON AFFECTED STRINGER IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030515000842003051500084NM 2003 5 15 C1HA200395059 120030510A2613 WARNING LIGHT BOEING727 727290 138408WNM NR 3 ENGINE ILLUMINATED A C1HAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15295AS 22147 ON CLIMBOUT ENGINE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. 2L73 4F A3WE 20030515000852003051500085SO 2003 5 15 C2XA03IA044 120030503A2131 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW2711547 145563 CAPT LOST PRESSURIZATION, MANUAL MODE WAS WORKING. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030508000052003050800005EA 2003 5 8 COMA0360227 120030503A7930601509199 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01420CA6039 7451 FLIGHT 5690 LT ENGINE OIL PRESSURE CAUTION MESSAGE. REPLACED THE OIL PRESSURE TRANSDUCER. 2L72 4F RTA21EA 20030508000112003050800011NM 2003 5 8 EVAS092011 120030410A5730 SKIN BOEING747 74745E 1384947NM RT WING CORRODED W QOCFK NONE O OTHER ININSP/MAINT 1 WP0316409 28093 DURING C08 CHECK, FOUND CORROSION ON RT WING EXTENTION LOWER SKIN UPPER SURFACE AT ERSS STA 1635. REMOVE THE CORROSION AND PERFORM NDI INSPECTION, ON FURTHER DEFECTS FOUND 2L74 4F RTA20WE 20030508000222003050800022NM 2003 5 8 DLM88030344 120030408A2150 A/C PACK DOUG MD88 MD88 3023688NM AFT ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27977DL 53258 ON TAKEOFF FROM SDF FLIGHT ATTENDANTS IN AFT CABIN SAID THEY SMELLED FUMES. NO FUMES IN FWD CABIN OR FLIGHT DECK ALL INDICATIONS NORM. LINE CHECK PILOT IN AFT CABIN SAID FUMES SMELLED LIKE RESIDUE BURNING OFF OF PNEUMATIC DUCTS. ODOR DISAPPATED QUICKLY WHEN CLIMB POWER SELECTED. REMAINDER OF FLIGHT UNEVENTFUL. CORR. PERFORMED OPN 5088 AND 5099 DUCT BURNOUT 2L72 4F RTA6WE 20030508000422003050800042NM 2003 5 8 CH1A200395037 120030414A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON CABIN FLOOR SUPPORT AT LBL 12 BS 1050 TO BS 1070 2L73 4F A3WE 20030506001232003050600123NM 2003 5 6 03FDEA00471 120030417A5321 FLOOR PANEL BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 AFT CARGO PIT AT STA 960E TO 990 FORWARD FLOOR PANEL HAS A HOLE. 2L73 4F RTA3WE 20030506002282003050600228WP 2003 5 6 ASAA0380205 120030304A53405910142 ATTACH ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND GILLINER ATTACH ANGLE IS CRACKED AT FS 617. REPAIRED CRACKED ANGLE WITH COLD BOND FIBERGLASS OVERLAY PER SRM 51-70-1. (M) 2L72 4F A6WE 20030506002422003050600242NM 2003 5 6 ASAA0370001 120030314A33508100022608 LIGHT BOEING737 737790 13844CNNM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01609AS 29752 OAK - DURING MAINTENANCE CHECK, THE MID CABIN EMERGENCY TRACK LIGHTS WERE INOPERATIVE. ADJUSTED THE EMERGENCY TRACK LIGHT WIRES. THE TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA16WE 20030507000032003050700003NM 2003 5 7 AUS20030316 120030309A2420735511A CSD BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU NR 1 ENGINE FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 1 ENGINE CONSTANT SPEED DRIVE (CSD) INPUT DRIVESHAFT SPLINE DISENGAGED DUE TO RETAINING RING AND SPACER COMING ADRIFT. 2L72 4F4 FRTA16WE E21EU 20030507000132003050700013EA 2003 5 7 CA030407007 220030405A8530 ENGINE ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA VIBRATION W A UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 CA (CAN) DURING CRUSE FLIGHT AT 400FT. PILOT HEARD A LOUD 'BANG' A/C BEGAN TO VIBRATE AND THERE WAS A POWER LOSS HOWEVER THE ENGINE WAS STILL RUNNING. A/C WAS LANDED WITH NO SUBSEQUENT DAMAGE AND ENGINE SHUT OFF. ON INSPECTION IT WAS DISCOVERED THAT SOMETHING IN NUMBER FOUR PISTON HAD FAILED CAUSING A HOLE TOPOF THE CRANKCASE. ENGINE WAS REMOVED AND WILL BE SENT TO A OVERHAUL SHOP FOR FUTHER INVESTIGATION. 1G71 3O3 O H11NM E295 20030507000312003050700031EU 2003 5 7 AUS20030335 120030320A5315 FLOORBEAM AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FLOORBEAMS CONTAINED LEVEL 2 CORROSION. 2L72 4F4 FRTA46NM E29NE 20030507000952003050700095EU 2003 5 7 AUS20030378 120030320A323399101399 ACTUATOR REIMS 406 F406 7535723EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL MLG FAULTY W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) NOSE LANDING GEAR ACTUATOR FAULTY. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20030507001292003050700129NM 2003 5 7 AUS20030396 120030403A6310A1902 BELT ROBSINR22 R22BETA 7640110NM LYC O360 O360J2A 41514EA XMSN DRIVE DISTORTED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE TO TRANSMISSION DRIVE BELTS STRETCHED BEYOND LIMITS. 1G71 3O3 O H10WE E286 20030507001302003050700130NM 2003 5 7 AUS20030397 120030403A7921C3094 BRACKET ROBSINR22 R22BETA 7640110NM LYC O360 O360J2A 41514EA OIL COOLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OIL COOLER BRACKET ASSEMBLY CRACKED IN SEVERAL LOCATIONS. 1G71 3O3 O H10WE E286 20030507001312003050700131NM 2003 5 7 AUS20030398 120030404A6310A1681 RETAINER ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA FREE WHEEL UNIT CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FREE WHEEL ASSEMBLY BACKING PLATE CRACKED FROM BOLT HOLE TO EDGE. 1G71 3O3 O H10WE E274 20030507001612003050700161CE 2003 5 7 CTU2003F00003 120030410A1430AN414 BOLT CESSNA340 340CESSNA 2076404CE CONT O520 TSIO520* 17040SO ELEVATOR BENT B CTURO OTHER O OTHER NRNOT REPORTED 1 GL21812V 7116 3400157 (NOTE: SUBMITTER HAS SEVERAL AIRCRAFT OF SAME MAKE AND MODEL). AFTER FAILURE OF BOLT PRIOR TO FLIGHT MAINTENANCE FACILITY PERFORMED INSPECTION OF BOLT WHICH THE ELEVATOR BELLCRANK ROTATES ON. BOLT HAVE BEEN STRESSED AND BENT. MFG SHOULD HAVE BOLT OF LARGER SIZE INSTALLED AND RECURRING INSTALLED OF BEARING. 1L72 3O3 O 3A25 E8CE 20030507001702003050700170SO 2003 5 7 C852003F00002 120030401A2842550698 TRANSMITTER PIPER PA31 PA31325 7103105SO LYC O540 TIO540* 41532EA LT WING CORRODED B C85RK NONE O OTHER ININSP/MAINT 1 NE014039L3858 318112013 DURING ANNUAL INSPECTION, FUEL LEAK WAS NOTED FROM LT WING. EXTENSIVE CHECKING SHOWED LEAKS FROM BOTH INBOARD AND OUTBOARD FUEL SENDERS. SENDERS WERE FOUND TO BE BADLY ROTTED AND CORRODED, BUT WERE STILL OPERATING AND INDICATING PROPERLY. REPLACING SENDER UNITS AND GASKETS CORRECTED THE FUEL LEAK PROBLEM. CAUSE, DETERIORATION OF SEALANT USED WHEN FACTORY BUILT. 1L72 3O3 O A20SO E14EA 20030507001782003050700178WP 2003 5 7 GTIA030192 120030221A2910 LINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE HYD SYSTEM GOUGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 RT T/R HYDRAULIC LINE GOUGING INTO LONGERON 19R STA 1384 (LONGERON AND HYDRAULIC LINE DAMAGED) DRILLED FASTENER LOCATION INTO REPAIR SPLICE. INSTALLED REPAIR SPLICE. 2L72 4F4 FRTA6WE E2EA 20030507002172003050700217NM 2003 5 7 CH1A200395033 120030410A5754 SKIN BOEING727 727290 138408WNM RT WING LE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 RT WING LE CRACKED IN UPPER SURFACE SKIN AT NR 5 SLAT INBD UPHOOK CUTOUT AFT END 2L73 4F A3WE 20030508000482003050800048EU 2003 5 8 03FDEA00671 120030502A3610 TUBE AIRBUS AIRBUS300 A300B4605R 3930308EU PRECOOLER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25682FE 19984 800 NR 1 ENGINE PRECOOLER CRACKED AT COOLING TUBE INSTALLED PRECOOLER IAW W/C 64S0202 WO 22877 AT MAE. 2L72 4F RTA35EU 20030508000552003050800055NM 2003 5 8 DL733030353 120030411A3350BPS73 POWER SUPPLY BOEING737 737347 1384647NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27308WA 23441 AFT CABIN EMERGENCY LIGHT INOPERATIVE, RELAMPED NO HELP R & R POWER SUPPLY LIGHT OPS NORMAL. 2L72 4F RTA16WE 20030508000652003050800065NM 2003 5 8 CH1A200395056 120030426A5320 SUPPORT BOEING727 727290 138408WNM TRUNNION CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 RT FWD. TRUNNION BEARING SUPPORT HAS CORROSION. 2L73 4F A3WE 20030508000822003050800082EU 2003 5 8 A6WA200360025 120030501A2710 WARNING LIGHT BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA RUDDER VALVE ILLUMINATED A A6WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL31292UE E2087 MWS RUDDER VALVE LIGHT IS ILLUMINATED IN FLIGHT AFTER DEPARTURE. AIR RETURN TO ORD. RESET ABD, TESTED IAW. 2H74 4F4 F A49EU E6NE 20030508000862003050800086NM 2003 5 8 AWXA200300472 120030414A53206545895 SPLICE BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON SPLICE AT AFT CARGO COMPARTMENT BILGE, BS 900, STR 27 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AT BS 900, STR 27 L/H, AND TRIMMED AWAY CORROSION ON STRINGER ENDS; PERFORMED HFEC INSPECTION OF TRIM TO VERIFY NO CRACKS EXIST; FABRICATED SHIMS, AND A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-45776; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5361-03119-SS3. 2L72 4F RTA16WE 20030508000872003050800087NM 2003 5 8 AWXA200300473 120030411A532065C218084 STRUCTURE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1" CRACK WAS FOUND ON STRUCTURE BELOW FLAP CONTROL CABLE FAIRLEADS AT OUTBOARD SEAT TRACK, BS 560, HFEC CONFIRMED. MAINTENANCE REMOVED CRACKED CHORD AT BS 560; FABRICATED A NEW REPLACEMENT STRUCTURE PER DWG 65C21808; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5362-03119-SS2. 2L72 4F RTA16WE 20030508000892003050800089NM 2003 5 8 AWXA200300475 120030410A53126516300 BULKHEAD BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND AT HOLE ON VERTICAL WEB, AFT SECTION OF BS 178 BULKHEAD, AT RBL 17, WL 188. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AT AFT SECTION OF BS 178 BULKHEAD, AT RBL 17, WL 188; FABRICATED A WEB SPLICE AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-11, PG. 89-101, FIG. 11. 2L72 4F RTA16WE 20030508001012003050800101EA 2003 5 8 QXEA0300537 120030423A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 PDX-TWO NICKS IN FUSELAGE SKIN EDGE ON AFT SIDE OF PASSENGER DOOR CUTOUT. REPAIRED IAW CRJ-700 SRM 51-25-16 AND SRM 51-00-01. HORIZON AIR EA R53-95, R53-93 AND EO 370-53-21-035. 2L72 4F RTA21EA 20030508001122003050800112NM 2003 5 8 DL76G030376 120030419A2781S283T0067 SENSOR BOEING767 767332 1382001NM SLAT UNSERVICEABLE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO271610D 30594 DURING CLIMBOUT, CLEAN CONFIGURATION, LE SLAT ASYM EICAS MSGACOMPLISHED QRH PROCEDURE. AIRCRAFT LANDED WITH ZERO SLATS AND 20 DEG FLAPS. 173 KT LANDING SPEED. REPLACED S279 PROX SENSOR. CHECKS OK. PERFORMED HIGH ENERGY STOP INSPECTION NO DEFECTS. 2L72 4F RTA1NM 20030508001132003050800113NM 2003 5 8 HOC2003F00008 120030420A5320 FLOOR SUPPORT BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK, CORROSION WAS NOTED ON OUTBOARD FLOOR SUPPORT BRACKET FOR FORWARD LAV. STA 314-344, RBL 5-10. 2L72 4F4 FRTA16WE E2EA 20030508001242003050800124NM 2003 5 8 UPS03440619 120030409A5730 SKIN BOEING747 747121 1384871NM RT WING BULGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, RT WING UPPER SURFACE RABBET AREA FOUND BULGED AT WS 1460 ( AFT NO.26 V/C FLAP ). CORR BLEND OUT 0.087 X 2 X 4 INCHES. REMAINING THICKNESS RANGED FROM .050 TO .071 INCH. RHW.UPPER.SKIN.SURFACE.REPAIR.AS PER.RS.R57-25-35006.A .WS.1460.AND.UPS.ENG'R.FILE.747-57-20040. 2L74 4F A20WE 20030508001382003050800138NM 2003 5 8 DL76K030380 120030419A2121S210T17027 FAN BOEING767 767332 1382001NM EXHAUST SEIZED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27176DZ 29697 DURING APPROACH 15MIN PRIOR TO LANDING EICAS MESSAGE -FWD EQ EXH FAN- DISPLAYED WITH STRONG NOXIOUS ELECTRICAL SMELL NOTED IN COCKPIT ONLY. EMERGENCY EQUIPMENT DISPATCHED. TROUBLESHOT PER F.I.M. REPLACED RELAY K345 DUE TO NO POWER TO FAN. CIRCUIT BREAKER NOW POPS. FOUND EXHAUST FAN DAMAGED. REPLACED SAME. FORWARD EQUIPMENT COOLING EXHAUST FAN OP CHECKS GOOD. 2L72 4F RTA1NM 20030506001682003050600168WP 2003 5 6 ASAA0380241 120030307A53102620717 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, AFT CARGO AREA HAS CORRODED SHEAR TIE. REPLACED SECTION OF DAMAGED SHEAR TIE PER SRM. (M) 2L72 4F A6WE 20030506002292003050600229WP 2003 5 6 ASAA0380209 120030304A5347S00062 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO BAY TRACK CORRODED AT FS 1007-1155. REPLACED TRACK PER SRM 51-30-1. (M) 2L72 4F A6WE 20030506002332003050600233WP 2003 5 6 ASAA0380212 120030304A532199365859 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRUSHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS CRUSHED AREA AT FS 259-313. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030506002532003050600253CE 2003 5 6 WDA2003F00000 120030329A322204425035 FORK CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA NLG INOPERATIVE B WDARK NONE O OTHER ININSP/MAINT 1 SO09603TC306 18280712 L2732348A DURING AN ANNUAL INSPECTION, WE REMOVED THE NOSE WHEEL PANT TOP ATTACHING BOLT AND THE LOWER FORK WITH THE TIRE ON IT FELL OFF OF THE STRUT ASSEMBLY. WE CALLED MFG TO VERIFY THAT FORK IS PRESSED ON THE STRUT ASSEMBLY. MFG REQUESTED THE FORK ASSEMBLY FOR FURTHER INSPECTION. 1H71 3O3 ONT3A13 1E4 20030507000632003050700063CE 2003 5 7 CA030410004 120030401A5310121340615 DOOR FRAME CESSNA206 U206C 2073332CE CONT O520 IO520F 17032SO FUSELAGE CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) UPON ANNUAL INSPECTION OF AIRCRAFT THE FORWARD LT DOOR POST WAS FOUND CRACKED ALMOST 1/2 WAY AROUND THE STRUCTURE. THE AIRCRAFT IS OPERATED ON WIPLINE FLOATS SO CONDITIONS FROM ROUGH WATER IS A POSSIBLE CONTRIBUTING FACTOR. THE AIRCRAFT HAS BEEN MAINTAINED AT A COMMERCIAL STANDARD AND ALL APPLICABLE AD'S AND NECESSARY SB'S COMPLIED WITH. 1H71 3O3 O A4CE E5CE 20030507001122003050700112NM 2003 5 7 AUS20030388 120030329A7830 LEVER BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU THRUST REVERSER JAMMED W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) NR 2 ENGINE THRUST REVERSER LEVER JAMMED. 2L72 4F4 FRTA16WE E21EU 20030507002002003050700200NM 2003 5 7 CH1A200395026 120030411A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 SURFACE CORROSION FOUND ON FLOORBEAM BETWEEN LBL 45 TO LBL 62 AT BS 1035 2L73 4F A3WE 20030508000042003050800004NM 2003 5 8 03FDEA00677 120030504A5330 SKIN BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 DRAIN BAY AT STA. 295 TO 280 WL 147.5 BS 27L HAS SKIN FRAYING AND CHIPPING IN DRAIN BAY. REPAIRED DRAIN BAY STRUCTURE IN ACCORDANCE WITH FEDEX E.A. 7-5310-69487 2L73 4F RTA3WE 20030508000542003050800054NM 2003 5 8 DLM88030352 120030408A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27943DL 49816 THE AFTERBODY FUSELAGE SKIN WAS FOUN WITH A CRACK AT FS 1418 JUST INBD OF THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT LONGERON 1R. THE CRACK WAS REMOVED WITH A 2.5 X 1 INCH CUTOUT AND REPAIRED WITH A TITANIUM REPAIR DOUBLER PER ER/A 384848-14, REV A. 2L72 4F RTA6WE 20030508000622003050800062EA 2003 5 8 COMA0360228 120030503A335059465 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR DAMAGED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01455CA 7592 FLIGHT 5799 ORANGE SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. REPLACED CONNECTOR WIRE. 2L72 4F RTA21EA 20030508000722003050800072NM 2003 5 8 DLM88030360 120030415A2120 ODOR DOUG MD88 MD88 3023688NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27957DL 49976 STRONG BURNING RUBBER ODOR IN CABIN AFTER T/O AND LANDING. PERFORMED DUCT BURNOUT, NO ODOR NOTED 2L72 4F RTA6WE 20030508000752003050800075NM 2003 5 8 DL73G030364 120030415A531265C3759029 BULKHEAD BOEING737 73735B 13844BMNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27224DA 24269 INSPECTION OF THE FS 178 BULKHEAD WEB PER AD 2000-05-29 REVEALED SEVERAL CRACKS IN THE CENTER WEB BETWEEN WL 219 & 226 AND BETWEEN LBL 12 & RBL 5.7. THE CENTER WEB WAS REMOVED AND A WEB INSTALLED TO CORRECT THE PROBLEM. THE REPLACEMENT WAS ACCOMPLISHED PER BAC S/B 737-53-1173 AND PER ER/A 384870-14AD. 2L72 4F RTA16WE 20030508000762003050800076NM 2003 5 8 DL73S030365 120030415A53109078224 DOUBLER BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 THE 'H' DOUBLER AROUND THE LOWER HINGE CUTOUT FOR THE L1 DOOR CUTOUT FWD FRAME WAS FOUND WITH A 3/8 INCH CRACK IN THE CORNER RADIUS. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A TITANIUM REPAIR DOUBLER PER ER/A 384891-14, REV B. 2L72 4F RTA16WE 20030508000772003050800077NM 2003 5 8 DHL2003750001 120030502A5347 SEAT TRACK BOEING727 7272M7 138407SNM FUSELAGE BROKEN A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01750DH 21951 THE REAR STOP ON THE S/O'S CHAIR SLIDING TRACK BROKEN/MISSING. REMOVED AND REPAIR SCREW ON TRACK STOP. CHECKED GOOD IAW 20-80-1. 2L73 4F A3WE 20030508000792003050800079EU 2003 5 8 A6WA200360022 120030425A5523 STRUCTURE BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA ELEVATOR TAB DENTED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31290UE E2080 DENTS OUT OF LIMITS ON THE RT ELEVATOR AND TABS. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584. 2H74 4F4 F A49EU E6NE 20030508001442003050800144NM 2003 5 8 QXEA0300496 120030420A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PANEL 262AT HAS CHAFE DAMAGE ON LOWER SURFACE. REPARIED IAW RD 8/4-53-521. 2H72 4T RTA13NM 20030508001462003050800146NM 2003 5 8 QXEA0300498 120030420A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PANEL 262HT HAS CHAFE DAMAGE ON LOWER SURFACE. REPAIRED IAW RD 8/4-53-521. 2H72 4T RTA13NM 20030508001482003050800148NM 2003 5 8 QXEA0300500 120030418A5240 SKIN BOMBDRDHC8 DHC8401 1390041NM SERVICE DOOR NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 RT AFT SERVICE DOOR SKIN HAS TWO SMALL NICKS AT THE LOWER FORWARD CORNER. REPAIRED IAW DHC-8-400 SRM 51-14-350-502 AND Q400 AMM 51-25-31-370-801. 2H72 4T RTA13NM 20030508001492003050800149NM 2003 5 8 QXEA0300511 120030421A5510 SHIM BOMBDRDHC8 DHC8401 1390041NM ZONE 300 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - SHIM AT FORWARD RIGHT HAND HORIZONTAL STAB ATTACH FITTING IS MIGRATING. REPAIRED IAW DHC-8 400 AMM TEMPORARY REVISION 55-10-00, PAGE 3-5. 2H72 4T RTA13NM 20030508001562003050800156NM 2003 5 8 QXEA0300501 120030414A5310 SILL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 FORWARD PASSENGER DOOR SILL HAS CORROSION IN NUMEROUS PLACES. REPAIRED IAW DHC-8 SRM 51-42-05-330-801, PAGES 201-218, PARAGRAPH 1-4. 2H72 4T RTA13NM 20030714000012003071400001NM 2003 7 14 CALA0300338 120030627A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717644 28905 INSPECTION FOUND A .125 INCH CRACK IN INTERCOSTAL AT FORWARD ENTRY STA 328-344, LBL 50.5. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030507000392003050700039SW 2003 5 7 CA030409013 120030328A5532 STRUCTURE BELL 206 206A 1181508SW ALLSN 250C 250C20 03013GL VERTICAL FIN CRACKED W A UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 CA (CAN) WHILE IN CRUISE FLIGHT THE PILOT NOTICED A YAW TO THE RIGHT. UPON LANDING HE NOTICED THAT THE TAIL FELT TWITCHY AND SHUTDOWN TO INVESTIGATE. WHEN HE GOT OUT HE NOTICED THE TOP HALF OF THE VERTICAL STABILIZER BENT OVER TO THE RIGHT HANGING ON BY THE RT SKIN. THE CRACK PROPAGATED FROM A SMOKING RIVET WITHIN ATTACHES LT TRAILING EDGE TO FIN. 1G71 3U3 U H2SW E4CE 20030507001322003050700132NM 2003 5 7 AUS20030399 120030404A6420A0082 HUB ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA TAIL ROTOR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL ROTOR HUB CORRODED AROUND STEEL BUSHINGS. TAIL ROTOR BLADE TIP CAPS CONTAINED EXFOLIATION CORROSION. 1G71 3O3 O H10WE E274 20030507001392003050700139SW 2003 5 7 CA030421004 120030131A5302204032806079A LONGERON BELL 204 204B 1181404SW LYC T53 T5311B 41549NE TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 17138 (CAN) UPPER LT ATTACH LONGERON CRACKED AFT OF HOT BONDED DOUBLER. CRACK APPEARS TO HAVE STARTED AT A RIVET HOLE. THE CRACK WAS DISCOVERED DURING A ENGINE REMOVAL WHERE THE AFT ENGINE COWL WAS REMOVED EXPOSING THE LONGERON. THE CRACK MEASURES APPROX 3 INCHES IN LENGTH. THE CRACK WAS ORIENTED IN A LATERAL PLANE TO THE LENGTH OF THE PART. 1G71 4U4 U H1SW E1EA 20030507002152003050700215SO 2003 5 7 CHQ000247 120030415A2913 PUMP EMB 145 EMB145 3260210SO NR 1 HYD SYSTEM LEAKING A CHQAO OTHER K FLUID LOSS CRCRUISE 1 GL11263 HYDRAULIC SYSTEM FAILURE. NO OTHER INDICATIONS NOTED. COCKPIT RECIEVED NO MASTER CAUTION CHIME WHEN MESSAGES CAME UP ON EICAS. FOUND HOSE ASSY. TO NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. RR'D HOSE ASSY. R & R NR 1 ENGINE DRIVEN HYDRAULIC PUMP. PERFORMED INSPECTION OF THE HYD.FLUID FILTERS. NO CONTAMINATION NOTED. SERVICED AND BLED NR 1 HYD. SYSTEM. PERFORMED ENGINE RUN AT MAX POWER FOR THREE MINUTES. NR 1 HYD SYS. OPERATES NORMALLY. 2L72 4F RTT00011AT 20030508000292003050800029WP 2003 5 8 DHL2003802003 120030501A2612 FIRE LOOP DOUG DC8 DC873 302199CWP NR2 ENGINE SHORTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH 46076 NR 2 ENGINE FIRE LOOP "A" INDICATES A SHORT. "B" LOOP OK. ENTERED ON DMI 12760 IAW MEL 26-2-3 CAT. "C". REF. DMI 12760 NR 2 ENGINE FIRE LOOP "A" INDICATES A SHORT. "B" LOOP OK. NR 2 ENGINE COWL OPEN TO FACILITATE MAINTENANCE. INSPECTED ALL LOOPS AND RE-SECURED LOOP CONNECTORS ON NR 2 ENGINE FIRE DETECTOR SYSTEM. OPS NORMAL PER M/M 26-10-0. THIS CLEARS DMI 12760. PLACARD REMOVED. 2L74 4F RT4A25 20030508000832003050800083EU 2003 5 8 AWXA200300469 120030505A335032145410 BATTERY PACK AIRBUS320 A320232 3930326EU EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW13875 1079 PHX - EEL - DURING INSPECTION OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM FAILED USING CIDS PANEL. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL) AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030508001292003050800129NM 2003 5 8 UPS03440624 120030412A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C M/D - BS 1500 RH STR 12R TO 13R, SHEAR TIE BRACKET FOUND CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030508001502003050800150NM 2003 5 8 QXEA0300512 120030418A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 SCRATCHES IN FUSELAGE SKIN BETWEEN THE FORWARD BAG DOOR AND THE EMERGENCY EXIT DOOR. REPAIRED IAW RD 8/4-53-505. 2H72 4T RTA13NM 20030509000092003050900009WP 2003 5 9 GTIA030235 120030306A5310 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND MID LOWER CARGO LOWER DOOR JAMB CUTOUT OUTBOARD BEAM CORRODED STATION 693-636. REMOVED CARGO DOOR JAMB BEAM. DRILLED AND LOCATED HOLES IN NEW DOOR JAMB BEAM. INSTALLED NEW DOOR JAMB BEAM. (M) 2L72 4F RTA6WE 20030630000102003063000010NM 2003 6 30 DHL2003747511 120030511A5521 SPAR BOEING727 727224 1384076NM RT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING "C" CHECK N/R 53401 RT. ELEVATOR REAR SPAR AT ELEVATOR STATION 99.79 HAS A CRACK IN THE LOWER RADIUS. ( VERIFIED WITH HFEC) REMOVED AND REPLACED RT ELEVATOR REAR SPAR IAW S/B 727-55-0059 P/N 65C30825-24 PO 312612. 2L73 4F A3WE 20030508001042003050800104WP 2003 5 8 ZW0A0304601 120030425A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139617R 53564 THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 3, 5, 7, AND 11. RESEATED THE LAMPS AT ALL 4 POSITIONS. CHECK-C 9-11-02 STL. 2L72 4F RTA6WE 20030508001142003050800114NM 2003 5 8 HOC2003F00011 120030429A5320 FLOOR SUPPORT BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK, CORROSION WAS NOTED ON CABIN FLOOR SUPPORT BRACKET AT STA 1070, LEFT. 2L72 4F4 FRTA16WE E2EA 20030508001192003050800119EA 2003 5 8 COMA0360224 120030429A7830 SWITCH CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF ADJUST A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01977CA 7157 FLIGHT 5837 LEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE. ADJUSTED THE STOW SWITCH TO M/M SPECIFICATIONS. 2L72 4F RTA21EA 20030508001202003050800120EU 2003 5 8 MALA030249 120030429A2120 ODOR BAC 146 AVRO146RJ85A1500097EU CABIN DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15513XJ E2329 FA SMELLED FUMES IN THE CABIN OF FLIGHT 3554. A/C DIVERTED TO SDF. MAINTENANCE INSPECTED A/C BAY, HYDRAULIC BAY, AND E&E BAY, NO FUMES OR SMOKE NOTED. RAN APU NR 1 & 2 PACKS INDEPENDENTLY, FOUND NO LEAKS OR FUMES PRESENT. RAN ALL FOUR ENGINES WITH ENGINE AIR PACKS SELECTED ON. COULD NOT DUPLICATE DISCREPANCY. 2H74 4F RTA49EU 20030508001272003050800127NM 2003 5 8 UPS03440622 120030414A531065B0831517 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C M/D - BS 1301 LT STR 16L SHEAR TIE FOUND CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030508001362003050800136NM 2003 5 8 DL76S030378 120030419A7930CF680A2 ENGINE BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 LEAKING A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27127DL43511 24077 580356 ENROUTE TO EWR LT ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DROP. QUANTITY REACHED 0.SHUT DOWN ENGINE WHEN LOW OIL PRESSURE LIGHT CAME ON AT APPROXIMATELY 10-11 PSI. FOUND OIL LEAK FROM OIL INLET PRESSURE TUBE. REMOVED AND REPLACED SCAVENGE TUBE ON NBR 6 BEARING HOUSING PER MM . LE CK GOOD. 2L72 4F4 FRTA1NM E13NE 20030508001422003050800142NM 2003 5 8 03FDEA00668 120030501A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CORROSION ON SHEAR TIE STA 950E BETWEEN STR 29R AND 30R. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM 53-10-4, 53-10-1, 51- 10-6. 2L73 4F RTA3WE 20030508001432003050800143NM 2003 5 8 03FDEA00667 120030501A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CORROSION BS 1166 RBL 15 WL 146 ON FRAME, FWD & AFT SIDES. REPAIRED FRAME AT BS 1166, RBL 3 - RBL 15, WL 146 PER SRM 53-10-1. 2L73 4F RTA3WE 20030508001512003050800151NM 2003 5 8 QXEA0300513 120030418A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PANEL 261LT HAS CHAFE DAMAGE ON LOWER SURFACE. REPARIED IAW RD 8/4-53-521, PAGES 4-5. 2H72 4T RTA13NM 20030507001492003050700149CE 2003 5 7 XGN2003F00000 120030301A2421X4087 BEARING BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO ALTERNATOR FAILED E XGNAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW051096W172 CE436 IN FLIGHT, AIRCRAFT LANDED WITHOUT INCIDENT. THE ALTERNATOR DRIVE END BEARING FAILED CAUSING THE ALTERNATOR ROTOR ASSEMBLY WITH THE DRIVEN GEAR TO EXTEND INTO THE ALTERNATOR DRIVE GEAR. THE MISALIGNMENT OF THESE TWO GEARS CAUSED THE ATTACH BOLTS ON THE ALTERNATOR DRIVE GEAR TO SHEAR. METAL FROM THE FAILED BEARINGS AND DAMAGE TO THE CRANKCASE CONTAMINATED THE ENGINE AND RUINED THE OIL PUMP GEARS AND HOUSING. 1L71 3O3 O 3A15 E5CE 20030507001512003050700151CE 2003 5 7 WVE2003F00008 120030310A242130728692 SPLINE ADAPTER LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP ALTERNATOR CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09430FX1043 166 DURING 600 HOUR INSPECTION OF THE ALTERNTOR SPLINE ADAPTER, DISCOVERED ADAPTER TO BE CRACKED IN TWO LOCATIONS. PROBABLE CAUSE: FATIGUE. (2003B0666) 2L72 4F4 FRTT00008WIE6WE 20030507001552003050700155CE 2003 5 7 CTU2003F00004 120030410A1430AN414 BOLT CESSNA340 340A 2076405CE CONT O520 TSIO520* 17040SO ELEVATOR BENT B CTURO OTHER O OTHER NRNOT REPORTED 1 GL21340FR5298 340A0039 AFTER FAILURE OF BOLT PRIOR TO FLIGHT OPERATOR CHOSE TO PERFORM INSPECTION OF OTHER 340 AIRCRAFT IN FLEET. BOLT MUST BE REMOVED FOR INSPECTION. THIS BOLT IS THE ELEVATOR BOLT, CRANK PIVOT BOLT. IT ALSO HAS A BEARING WHICH IS SOMETIMES WORN AS WELL. 1L72 3O3 O 3A25 E8CE 20030508000252003050800025NM 2003 5 8 DHL2003783004 120030501A3260 MODULE BOEING727 727227 1384078NM MLG FAILED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01766AT 21999 UPON GEAR RETRACTION RIGHT GEAR RED LIGHT REMAINED ILLUMINATED. CHECKED ABNORMAL PROCEDURE DISCUSSED WITH MAINTENANCE, PROCEDED DIRECTLY TO KCVG. LANDED AT KCVG NORMALLY. WITH RED RIGHT GEAR LIGHT ILLUMINATED DOOR LIGHTS WERE OUT AND RIGHT GREEN GEAR DOWN LIGHT WAS OUT AND WOULD NOT PRESS TO TEST NOR WOULD IT TEST WITH LIGHT TEST SWITCH. RELAMPED RIGHT GREEN GEAR DOWN LIGHT - NO HELP, WOULD NOT TEST.TESTED THE OPERATION OF BOTH RT MAIN GEAR UPLOCK AND DOWNLOCK SENSORS IAW B-727 M/M 32-61-81 AND 32-61-91, NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR ELECTRONIC MODULE AS A PRECAUTIONARY IAW B-727 M/M 32-09-121. OPS CHECKED GOOD. 2L73 4F A3WE 20030508000802003050800080SO 2003 5 8 C2XA03SH127 120030505A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 SHV DURING C CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO HAVE CORROSION UNDER COMPOSITE CROSSBEAM AT FRAME 20. MAITENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR TO AFFECTED BEAM IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APRROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030509000172003050900017WP 2003 5 9 GTIA030223 120030218A5241 PAN DOUG DC9 DC983 3022083WP FWD GALLEY TORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD GALLEY DOOR AT FORWARD PAN CORNER TORN. VISIBLE THROUGH LIGHTING HOLE. ON REMOVAL OF PAN, FOUND DOOR FRAME, CUT IN RADIUS AND SECONDARY HOLE AND CRACK FROM HOLE TO HOLE IN RADIUS. REMOVED DOOR PAN. AFTER REMOVING PANE FOUND CORROSION ON CUSP ANGLE. REMOVED CUSP ANGLE SECTION. FABRICATED CUSP ANGLE. INSTALLED CUSP. FABRICATED 21 AND 19 SPLICE ANGLE. INSTALLED 21 ND 19 SPLICE ANGLES. LOCATED AND DRILLED NEW R1 DOOR PAN. INSTALLED NEW PAN. (M) 2L72 4F RTA6WE 20030509000182003050900018WP 2003 5 9 GTIA030231 120030325A5410 LINER DOUG DC9 DC983 3022083WP NR 2 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FLL - NR 2 ENGINE NOSE COWL ACCOUSTIC LINER DAMAGE. NR 2 ENGINE NOSE COWL AND T/R ASSEMBLY, REMOVED AND REPLACED. (M) 2L72 4F RTA6WE 20030509000192003050900019WP 2003 5 9 GTIA030234 120030130A5230 INTERCOSTAL DOUG DC9 DC981 3022081WP CARGO DOOR GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND MID CARGO DOOR HEAVY GOUGE INBOARD SIDE OF DOOR FORWARD LOWER RIGHT CORNER. REMOVED INTERCOSTAL. FABRICATED REPAIR DOUBLER. FABRICATED REPAIR INTERCOSTAL. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20030509000272003050900027EU 2003 5 9 A6WA200360010 120030409A5311 FRAME BAC 146 146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31290UE E2080 FRAME 32 MLG WHEEL WELL RIGHT AFT BULKHEAD CRACKED IN TWO PLACES IN LOWER FALSE DIAPHRAGM FOR FAIRING ATTACHMENT. PATCH TWO ABOVE AREAS PER SRM 51-71-11. DOUBLE ROW RIVETS 2024 T3 .050 ALUM. (M) 2H74 4F A49EU 20030509000282003050900028EU 2003 5 9 A6WA200360007 120030411A5755 SKIN BAC 146 146200A 1500266EU AIR BRAKE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 DENT IN LT AND RT AIR BRAKE OUT OF LIMITS OF SRM. REPAIR REQUESTED FROM BAE SYSTEMS REF AVMAX FAX 1538-6080004. (M) 2H74 4F A49EU 20030509000362003050900036WP 2003 5 9 GTIA030236 120030320A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND LEFT INBOARD SEAT TRACK BETWEEN G-4 GALLEY SEAT 33 STATION 1212 TO 1309 NUMEROUS NICKS, GOUGES, BARE METAL AND CORROSION. SEAT TRACK FOUND OUT OF LIMITS AT STATION 1277 AND 1280. CUT OUT SEAT TRACK FROM STATION 1261-1297. FABRICATED NEW SEAT TRACK. INSTALLED SEAT TRACK REPAIR. (M) 2L72 4F RTA6WE 20030509000392003050900039WP 2003 5 9 GTIA030251 120030322A5755 PANEL DOUG DC9 DC983 3022083WP SPOILER CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND LEFT WING INBOARD FLIGHT SPOILER PANEL CRACKED AT INBOARD AFT CORNER. REMOVED LEFT INBOARD FLIGHT SPOILER PANEL. REPAIRED LEFT WING FLIGHT SPOILER. INSTALLED WING INBOARD FLIGHT SPOILER. (M) 2L72 4F RTA6WE 20030509000562003050900056EA 2003 5 9 FTU2003F00006 220030414A8500 ENGINE GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA NACELLE CONTAMINATED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE059038N 3050 DURING A ROUTINE OIL CHANGE WHEN OIL FILTER WAS CUT OPEN FOR INSPECTION, A LARGE AMOUNT OF SILVER PARTICILES WERE FOUND. OIL SUMP SCREEN WAS REMOVED FOR INSPECTION AND LARGE PIECES OF SILVER MATERIAL WAS FOUND. ALL CYLINDERS WERE REMOVED FOR INTERNAL INSPECTION, FOUND NOTHING OBVIOUS, THE OIL SUMP WAS REMOVED AND LARGE THICK SILVER FLAKES WERE FOUND. REMOVED ACCESSORY CASE REMOVED NO OBVIOUS PROBLEMS FOUND. ENGINE WAS REMOVED FROM THE AIRCRAFT AND RETURNED TO MFG FOR INVESTIGATION AND REPAIR. IT HAS BEEN SUSPECTED TO BE A BEARING PROBLEM. 1H72 3O3 O 6A1 1E4 20030509000572003050900057EU 2003 5 9 K9GR490Y 120030416A2810 FUEL TANK BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE331* 01514WP LT & RT WING LEAKING B K9GRO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19492UE 790 TOTAL AIRCRAFT TIME: 20,351.2, TOTAL CYCLES: 24, 497 FUEL LEAKS AT W/S 38 AND 83, LT AND RT WINGS. UPON OPENING WINGS FOR FUEL TANK REPAIR, CORROSION WAS NOTED AROUND THE FUEL SUMPS. SOME SKIN SEPARATION DUE TO EXPANSION OF CORROSION PRODUCTS WAS FOUND AND CRACK WERE NOTED VISUALLY. WHEN EXAMINED WITH ZYGLO, NUMEROUS CRACKS WERE FOUND IN ALL WING STATIONS NOTED ABOVE. SUBSEQUENT INSPECTION OF A/C HAD BEEN IN SERVICE ON THE EAST COAST PRIOR TO LEASE RETURN AND STORAGE. 2L72 4T3 TRTA56EU E2WE 20030509000642003050900064CE 2003 5 9 FTU2003F00007 120030424A3020674101 VALVE CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE LT ANTI ICE AIR CORRODED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE05126QS S5500126 DURING REPLACEMENT OF PERI SEALS ON THE FORWARD SIDE OF THE ENGINE ANTI ICE SYSTEM, THE ANTI ICE VALVE HAD TO BE REMOVED. WHILE REMOVING THE ELECTRICAL CONNECTOR, DIFFICULTY WAS ENCOUNTERED BECAUSE THE CONNECTOR WAS OVER TORQUED OR CORROSION HAD CREATED A PROBLEM. IN THE PROCESSES OF REMOVING THE PLUG, THE SOCKET ON THE ELECTRICAL SOLENOID VALVE SEPARATED FROM THE BODY. THIS RESULTED INTO BEING AN EXPENSIVE REPAIR WHEN THE UNIT WAS SENT BACK TO THE MFG. IT IS HIGHLY RECOMMENDED TO BE SURE THE THREADS ON THE CONNECTORS ARE CLEAN AND PROPER TORQUE USED WHEN SECURING THE ELECTRICAL CONNECTOR. THE REPAIRED UNIT WAS REINSTALLED AND OPS CHECKED GOOD. 1L72 4F4 FRTA22CE E1NE 20030509000742003050900074NM 2003 5 9 HOC2003F00012 120030429A5320 INTERCOSTAL BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON LOWER FLANGE COMMON TO FLOORBEAM STRAP AND INTERCOSTAL. STA 1130, LBL 24. 2L72 4F4 FRTA16WE E2EA 20030509000782003050900078NE 2003 5 9 RU32003F00002 220030430A7200 ENGINE BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE RIGHT FAILED A RU3AA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW1567 FF2 PCE95331 RIGHT ENGINE FAILED SHORTLY AFTER TAKE-OFF (1940Z) CLIMBING THROUGH 2,500 FT. EMERGENCY PROCEDURES ACCOMPLISHED, AND LANDED WITHOUT FURTHER INCIDENT. ENGINE WAS REMOVED AND SENT TO O/H FACILITY. ENGINE TEARDOWN REPORT INDICATES THE INFLIGHT SHUTDOWN WAS MOST LIKELY CAUSED BY THE UNCOUPLING OF THE ACCESSORY GEAR BOX TO THE COMPRESSOR. FAILURE OF THE SPADE LOCK SYSTEM ALLOWED THE INPUT SHAFT TO MOVE BACK INTO ITS BEARING, SCORING ITS JOURNAL. THIS REDUCED THE INTER-PLAY OF THE SPLINE AND OVER TORSIONED THE SPLINE CONTACT CAUSING THE UNCOUPLING. 2L72 4T4 T A24CE E4EA 20030509001332003050900133 2003 5 9 COMA0370014 420030506A3417 ADC CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01331CA 10061 FLIGHT 6899 ADC NR 1 FAILED. RESET ADC, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20030509001342003050900134NM 2003 5 9 CALA0300234 120030508A52306546921528 SKIN BOEING737 7373T0 1384582NM CARGO DOOR MISREPAIRED A CALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW0977303 23354 C1 DOOR IMPROPERLY REPAIRED ON INNER SKIN AT CENTER LINE NR 4 HOLE. INSTALLED REPAIR PER ECRA 5232-01028. 2L72 4F RTA16WE 20030509001372003050900137NE 2003 5 9 ARWA20030501 220030509A7230 COMPRESSOR DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 1 ENGINE STALLED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO19791AL 46150 643740 NR 1 ENGINE COMPRESSOR STALLED, REDUCED POWER 1.50 EPR, N1 TACH FLUX AND MAX "O". OIL TEMP INCREASING. ENGINE SHUT DOWN 05:30Z WINDMILLING OIL PRESSURE 16 PSI. NOTE: PRELIMINARY INSPECTION REVEAL C1 BEARING FAILURE. CORRECTIVE ACTION: 2L74 4F4 F 4A25 1E8 20030509001432003050900143EU 2003 5 9 142141 120030509A26131734362450 SENSOR SAAB SF340 SF340A 7850100EU TAIL PIPE CONTAMINATED A UHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL17108CQ 340A108 FLT4488 DURING TAKEOFF ROLL TAILPIPE OVERTEMP WARNING LIGHT ILLUMINATED TAKEOFF ABORTED AND RETURNED TO GATE MAINTENANCE DISPATCHED TO AIRCRAFT CLEANED AND DRIED OFF CONNECTIONS RESEALED RAN AIRCRAFT NO FURTHER PROBLEMS NOTED AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 20030507001652003050700165WP 2003 5 7 GTIA030143 120030219A5310 FITTING DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 AFT CARGO FS 1336 STR 28R END FITTING CORRODED. REMOVED STR 28R END FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED STRINGER 28R END FITTING. 2L72 4F4 FRTA6WE E2EA 20030508000242003050800024NM 2003 5 8 DL73K030348 120030409A5730654549517 SKIN BOEING737 737232 1384475NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 THE LT WING UPPER SKIN WAS FOUND WITH A 1.5 INCH CRACK EXTENDING FWD FROM THE AFT EDGE OF THE SKIN AT THE REAR SPAR AT WBL 170. THE CRACK WAS REMOVED WITHA 2 X 1 INCHES CUTOUT IN THE SKIN AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384859-14, REV A. 2L72 4F RTA16WE 20030508000922003050800092NM 2003 5 8 2003UALA00404 120030430A2131 CONTROLLER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN PRESSURE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29947UA 26688 AIRCRAFT DIVERTED ENROUTE BECAUSE THE CABIN PRESSURE BECAME UNCONTROLLABLE. CABIN PRESSURE CONTROLER (CPC) FAILED DUE TO INTERNAL FAULT. REPLACED THE CABIN PRESSURE CONTROLER, THAN PRESSURIZED AIRCRAFT USING APU IN AUTO, STANDBY AND MANUAL TO ENSURE CORRECT OPERATION. NO DEFECT NOTED. 2L72 4F4 FRTA16WE E2GL 20030508001532003050800153NM 2003 5 8 QXEA0300515 120030418A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PANEL 261CT HAS CHAFE DAMAGE ON LOWER SURFACE. REPAIRED IAW RD 8/4-53-521, PAGES 4-5, STEPS 9-12. 2H72 4T RTA13NM 20030509000422003050900042NM 2003 5 9 USAASB03044 120030323A3234 HANDLE BOEING737 737301 1384611NM MLG FAILED A USAAO OTHER O OTHER APAPPROACH 1 EA19574US 23739 PIT - FLT 542 - ON APPROACH INTO PIT FROM ATL, AT APPROXIMATELY 2,500 TO 3,000 FT, CREW RECEIVED THREE GEAR DISAGREEMENT LIGHTS WHEN PLACING GEAR HANDLE DOWN. CREW REPORTED THEY FELT THE GEAR GO DOWN. CAPTAIN OPTED TO ACCOMPLISH A FLYBY WHERE THE TOWER CONFIRMED THE GEAR WAS IN THE DOWN POSITION. CAPTAIN ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND FOUDN THAT THE GEAR HANDLE WAS NOT COMPLETELY ENGAGED. CREW THEN RECEIVED THREE GEAR GREEN LIGHTS, CONTINUED APPROACH AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT TAXIED TO THE GATE. NO EMERGENCY WAS DECLARED. CAPTAIN CONFIRMED TO MAINTENANCE THAT THE GEAR HANDLE WAS NOT FULLY ENGAGED. ONCE GEAR HANDLE WAS PLACED ALL THE WAY DOWN, THREE GREEN GEAR LIGH2L72 4F RTA16WE 20030509000482003050900048WP 2003 5 9 GTIA030250 120030311A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND AFT PIT FS 1231 FRAME CORROSION. FORMED REPAIR CHANNEL. FABRICATED 13'S. CUT OUT FRAME FOR REPAIR. INSTALLED REPAIR PARTS. (M) 2L72 4F RTA6WE 20030509001672003050900167NM 2003 5 9 USAABB03060 120030413A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19625VJ 27246 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030509001682003050900168NM 2003 5 9 USAABB03059 120030411A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 26 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030509001752003050900175EU 2003 5 9 USAASA03029 120030326A335032145410 PSU AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19715UW 1051 PHL - THE EMERGENCY EXIT LIGHT ON THE AIRCRAFT RIGHT SIDE, MID CABIN, WAS INOPERATIVE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030513000042003051300004NM 2003 5 13 250TR0012 120030429A5320 PANEL BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 WEB PANEL CRACKED LEFT SIDE UNDER TRANSITION ANGLE AT BS460 (FORWARD CARGO BIN). FABRICATED NEW WEB IAW DWG 69C41473 AND INSTALLED. 2L72 4F RTA16WE 20030513000072003051300007CE 2003 5 13 DXTA200300031 120030510A3260 WARNING LIGHT CESSNA650 650 2076802CE NLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07715QS 6507105 UPON GEAR EXTENSION, NOSE GEAR GREEN DOWN & LOCKED LIGHT FAILED TO COME ON, HOWEVER THE NOSE STEERING ARM LIGHT CAME ON. CONFIRMATION TESTS (THROTTLES TO IDLE & FLAPS PAST 20 DEGREES) WERE DONE & NO GEAR UNLOCKED HORN SOUNDED. GEAR WAS RECYCLED AND WE RECEIVED NO NOSE GEAR LIGHT AGAIN. ABOUT 2 MINUTES LATER THE NOSE GEAR GREEN LIGHT CAME ON. 2L72 4F A9NM 20030513000092003051300009EA 2003 5 13 QXEA0300545 120030506A5610 WINDOW CNDAIRCL600 CL6002C10 1390015EA ZONE 100 BURNED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 SEVERAL BURN MARKS BELOW FIRST OFFICERS SIDE WINDOW. REPAIRED IAW HORIZON AIR EA R-53-100 AND SRM 51-42-06 AND SRM 51-20-06. 2L72 4F RTA21EA 20030513000112003051300011NM 2003 5 13 250TR0011 120030429A5347 CARGO TRACK BOEING737 7372K5 138448XNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 RIGHT CARGO TIE DOWN TRACK CRACKED AT BS 460 (FORWARD CARGO BIN).REPAIRED PER SRM 51-40-4. 2L72 4F RTA16WE 20030513000322003051300032NM 2003 5 13 03FDEA00713 120030430A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING FOUND OUTBOARD FLAP, INBOARD MOST HINGE FITTING FLAP SIDE, AFT MOST HOLE LOCATION QTY. 1 EACH OUTBOARD MOST FACE WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69246 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RH OUTBOARD FLAP/INBOARD FLAP HINGE SUPPORT - REPAIR. 2L73 4F RTA22WE 20030513000412003051300041EA 2003 5 13 SWIA200311949 120030508A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07926SW 7687 FLYING AT CRUISE 28,000 WE RECEIVED A HIGH SPEED CLACKER, CABIN CHIME AND FLAPS FAIL CAUTION ALL AT THE SAME TIME. LANDED FLAPS 0 DEGREES AT LAX. HIGH SPEED WARNING AND CHIME INTERMITTANT. RIGGED LEFT BPSU IAW MM 27-54-00. PERFORMED FUNCTIONAL CHECK ON GROUND, OPS CHECK GOOD. FLIGHT TEST GOOD. 2L72 4F RTA21EA 20030513000432003051300043EA 2003 5 13 SWIA200311951 120030508A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07493SW 7450 RT WING EXTERIOR EMERGENCY LIGHTS HAVE FORWARD LIGHT OVER WING AND LIGHT JUST AFT OF SERVICE DOOR INOP. REPLACED LAMPS FOR FORWARD EXTERIOR EMERGENCY LIGHT AT WING AND LIGHT JUST AFT OF SERVICE DOOR IAW MM 33-51-21. OPS CHECK GOOD. 2L72 4F RTA21EA 20030513000472003051300047CE 2003 5 13 051003 120030510A329716001260 CIRCUIT BREAKER BEECH 1900 1900C 1154161CE LANDING GEAR INOPERATIVE E YADAO OTHER J WARNING INDICATION APAPPROACH 1 AL0345GL UC45 PILOT REPORTED THAT HE HAD TO MANUALY EXTEND THE LANDING GEAR. 2L72 4T RTA24CE 20030513000482003051300048NM 2003 5 13 P5CA0300876 120030511A5497 WIRE BOEING747 747249F 1384849NM PYLON CHAFED A P5CAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP23920FT 22237 AFTER PUSHBACK NR 4 BLEED OVERHEATED LIGHT ILLUMINATED. FOUND CHAFED WIRE IN PYLON, REPAIRED PER MM 20-10-13, REPOSITION CLAMP & WIRE, CHECKED FOR AIRLEAKS - NONE FOUND 2L74 4F A20WE 20030513000672003051300067NM 2003 5 13 CALA0300239 120030511A3350BR963180 WIRE BOEING757 757224 1384958NM SEAT 22A BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2733103 27293 INSPECTION FOUND THE SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 16-25 INOPERATIVE DUE TO A BROKEN WIRE. THE WIRE AT SEAT 22A WAS REPAIRED IAW WD BR2013-P-7572CO AND OPERATION OF THE LIGHT WAS RESTORED. 2L72 4F RTA2NM 20030513000772003051300077SO 2003 5 13 RAIA00305127 120030503A3250 STEERING SYS EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03819HK 145062 AIRCRAFT PULLED HARD TO LEFT DURING TAKE-OFF ROLL. MAINTENANCE ADJUSTED NOSE WHEEL STEERING SYSTEM, OPS CK OK. 2L72 4T RTT00011AT 20030513000802003051300080SO 2003 5 13 C2XA03CL098 120030506A323023092900001 UPLOCK EMB 145 EMB145 3260210SO NOSE GEAR FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714960 145100 THE CREW REPORTED AFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT.THE CREW RECYCLED THE GEAR WITH NO SUCCESS. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030513000892003051300089NM 2003 5 13 UPS03240671 120030414A5315 FLOORBEAM BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, CORROSION UNDER ANCHOR CLIP ON LWR SIDE OF FLOORBEAM TOP STRUCTURE BS 344 LBL 12 APPROX. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7 2L73 4F A3WE 20030513000992003051300099NM 2003 5 13 AWXA200300502 120030419A5330654577870 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING C-15 CHECK A 3/4 INCHE CRACK WAS FOUND ON R-2 DOOR FUSELAGE SKIN UPPER HINGE CUTOUT BS 957. MAINTENANCE CUTOUT CRACK ON R-2 DOOR FUSELAGE SKIN UPPER HINGE CUTOUT BS 957; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-3, FIG. 21A. 2L72 4F RTA16WE 20030513001062003051300106 2003 5 13 730PA0003 420030503A2210 DAMPER BOEING737 7373L9 1384470NM YAW MALFUNCTIONED A PIDAK NONE O OTHER CRCRUISE 1 SO05730PA 27924 YAW DAMPER WILL NOT ENGAGE. PERFORMED YAW DAMPER SYSTEM BITE TEST. ALL FAULTS CLEARED. NO CURRENT FAULTS PRESENT. 2L72 4F RTA16WE 20030513001152003051300115NM 2003 5 13 QXEA0300452 120030416A3233465507 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM MLG INOPERATIVE A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09412QX2742 4059 ON FLIGHT, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. SHOWED AMBER AND RED LIGHTS. CHECKLIST BROUGHT ALL GREEN UP NORMAL. LANDING WAS NORMAL. REMOVED AND REPLACED RETRACTION ACTUATOR. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513001272003051300127WP 2003 5 13 UPS03840678 120030424A574037048411 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, LT WING AT STA. XRS 74 OB SIDE STRINGER 51 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3704841, AND SRM. 51-1-20D 2L74 4F RT4A25 20030513001292003051300129NM 2003 5 13 CALA0300232 120030503A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912318 23369 LEFT PRESSURE DECK IN WHEEL WELL CRACKED (1 INCH). REPAIRED PRESSURE DECK PER SRM 53-60-51. 2L72 4F RTA16WE 20030513001312003051300131NM 2003 5 13 DL757030386 120030425A5531175N20012 PANEL BOEING757 757232 1384965NM VERTICAL FIN PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27613DL 22820 VERTICAL STABILIZER LT LOWER FWD SKIN (FWD TORQUE BOX) WAS DAMAGED DUE TO GROUND DAMAGE. REPAIRED PER ERA 423002-14 2L72 4F RTA2NM 20030513001322003051300132NM 2003 5 13 DL76S030387 120030425A3260849704 FSEU BOEING767 767332 1382001NM E/E BAY INTERMITTENT A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27134DL 25123 AFTER T/O AMBER PROBE HEAT STATUS. AFTER CLEANING UP A/C GOTRED FLAP AURAL WARNING W/FLAPS UP. ON LWR STATUS HAD AIR/GRD DISAGREE, LDG GEAR MON, AND NOSE A/G DISAGREE. CLEANED S244 - S245 - S246. CHECKED CONDUIT AND WIRING FOR S244 S245 AND S246. ALL CHECKS GOOD. REPLACED FSEU AND RAN SYS TEST OF FSEU PER MM ALL CHECKS NORMAL 2L72 4F RTA1NM 20030508000972003050800097EA 2003 5 8 QXEA0300533 120030415A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 PDX-GOUGE IN UPPER FUSELAGE SKIN AT FS 394.00 ON LT SIDE. REPAIRED IAW CRJ700 SRM 53-00-01, SRM 51-21-11 AND SRM 51-21-16. 2L72 4F RTA21EA 20030508000902003050800090NM 2003 5 8 AWXA200300476 120030422A53106546527 SHEAR TIE BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR TIE AT BS 500B BETWEEN STR 28 LT AND 28 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF SHEAR TIE AT BS 500B BETWEEN STR 28 LT AND 28 RT; FABRICATED A REPAIR ANGLE AND DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07, PG. 213. 2L72 4F RTA16WE 20030509000022003050900002 2003 5 9 XNOA01117 420030507A3442 DISPLAY BOEING727 727227 1384078NM WX RADAR SYS MALFUNCTIONED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23793A 20774 RADAR PAINTED ERRONEOUS DISPLAY IN ALL CONDITIONS OTHER THAN STATIC. REMOVED & REPLACED WEATHER RADAR R/T. OPS CHECK GOOD AT THIS TIME. MM 727-200 MM 34-21-00. 2L73 4F A3WE 20030509000062003050900006SO 2003 5 9 C2XA03IA047 120030506A3350MS27473E10F355 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN DIRTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717560 145605 ON PREFLIGHT THE CREW NOTED THAT THE FORWARD EMERGENCY EXIT SIGN WAS INOP. MAINTENANCE CLEANED THE INVERTER CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMREGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030509000082003050900008WP 2003 5 9 GTIA030245 120030329A54105930645501 COWLING DOUG DC9 DC982 3022082WP NR 2 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 LGA - NR 2 ENGINE ACCOUSTIC LINER MATERIAL MISSING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED RN 2 ENGINE NOSE COWL. (M) 2L72 4F A6WE 20030509000122003050900012WP 2003 5 9 GTIA030241 120030331A7800 LINER DOUG DC9 DC941 302207NWP RT ENGINE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23130NK 47604 FOUND RT ENGINE HAS A SECTION OF ACCOUSTIC LINER MISSING AND CRACKED TAILPIPE 2 O'CLOCK POSITION. REMOVED AND REPLACED THRUST REVERSER SPACER. OPS AND LEAK CHECK GOOD. (M) 2L72 4F A6WE 20030509000152003050900015WP 2003 5 9 G60A069 120030305A2611 SMOKE DETECTOR DOUG DC10 DC1030F 3023504WP CARGO BAY FALSE ACTIVATIONA G6OAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27609GC 46932 NR 3 LOWER FORWARD CARGO SMOKE DETECTOR ILLUMINATED WITH ASSOCIATED LIGHTS, ACCOMPLISHED CHECKLIST E-23 AND DISCHARGED NR 1 AND NR 2 CARGO FIRE BOTTLES. INSPECTED CARGO COMP, NO FAULTS FOUND. REF TAFI 26-14BC. DETECTOR FAULT, MEL 26-15-1, CONTROL NR M80312. DDG 26-15 C/W. (M) 2L73 4F RTA22WE 20030509000302003050900030WP 2003 5 9 GTIA030225 120030215A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FOUND KEELBEAM STATION 826-905 HAS CORROSION AT SEVERAL PLACES, BARE METAL. SEVERAL AREAS BETWEEN STATION 826-850 OUT OF LIMITS. FABRICATED 1 DOUBLER, 1 TRIPLER. DURING REPAIR OF LOWER KEEL BEAM SKIN FOUND LEFT INTERCOSTAL AT STATION 845 TO BE DEEPLY GOUGED. REMOVED LEFT INTERCOSTAL. LOCATED AND DRILLED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. INSTALLED TWO DOUBLER AND 1 TRIPLER. (M) 2L72 4F RTA6WE 20030509000312003050900031WP 2003 5 9 GTIA030238 120030312A5753 VANE DOUG DC9 DC983 3022083WP TE FLAPS DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FOUND LEFT INBOARD FLAP VANE LOWER SIDE HAS NUMEROUS DENTS. DUE PEN INSPECTION OF DENTS REVEAL 9 CRACKS IN SKIN. REPAIRED CRACKS ON LEFT INBOARD FLAP VANE USING 7075-T6 .020 ETCHED SKIN AND DOUBLER. FILM ADHESIVE. (M) 2L72 4F RTA6WE 20030509000342003050900034 2003 5 9 GTIA030248 420030405A2565 SLIDE DOUG DC9 DC981 3022081WP PAX DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FLL - FLT 765 - L1 SLIDE PACK FELL OFF. RE-INSTALLED L1 SLIDE PACK. (M) 2L72 4F A6WE 20030509000402003050900040SO 2003 5 9 SIMA200309604 120030402A5313 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 DURING A IMBV INSPECTION, STRINGER 19L AT JUNCTION OF CENTER FUSELAGE 3 AND 4 BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED A NDT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21 CHAPTERS 53-24-02 FIG 201. (M) 2L72 4T RTT00011AT 20030509000622003050900062NM 2003 5 9 HOC2003F00009 120030426A5320 SUPPORT BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE BULKHEAD CORRODED B HOCRK NONE O OTHER ININSP/MAINT 1 WP0754348 21967 DURING A (C) CHECK, CORROSION WAS NOTED AT STA 1166, AFT BULKHEAD SUPPORT. (CENTER/ TOP). 2L72 4F4 FRTA16WE E2EA 20030509000662003050900066EA 2003 5 9 B2E2003F00000 220030224A7414 BRUSH BLOCK PIPER PA28 PA28RT201 7102818SO LYC O360 IO360C1C6 41514EA MAGNETOR DAMAGED B B2ERO OTHER O OTHER NRNOT REPORTED 1 EA232218Z809 00101735 28R7918117 REMOVED SLICK MAGNETO IAW INSPECTION. FOUND DISTRIBUTOR GEAR MISSING CARBON BRUSH AND SPRING IN VERY POOR CONDITION. ALSO DISTRIBUTOR BEARING BAR WAS BURNED AND MELTED. 1L71 3O3 O 2A13 1E10 20030509000802003050900080CE 2003 5 9 CNQ2003F00001 120030317A21206512072101 VANE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA SCOOP CRACKED B CNQRO OTHER O OTHER NRNOT REPORTED 1 CE07379QS 5600479 DURING ROUTINE INSPECTION, LOOKED INTO NACA SCOOPS AND SAW THE UPPER VANE PN 651207211 AND LOWER VANE PN 651207212 MISSING 1 INCH X 1 INCH AND A 1 INCH X 2 INCH PART OF VANE. BOTH CRACKS STARTED AT (V CUT). PARTS WERE FOUND DOWN STREAM PAST THE FRESH AIR CHECK VALVE AND THE OVERHEAD BLOWER WEDGED IN DUCT WORK. REPLACED BROKEN VANES WITH NEW AND SECURED IN PLACE WITH EA9309 IAW MM. BEFORE REINSTALLATION, WE DRILLED A RELIEF HOLE AT THE BOTTOM OF (V). AS WITH OTHER SCR`S, CONCERNED WITH THE BROKEN PARTS BECOMING WEDGED IN THE FRESH AIR CHECK VALVE (WHICH WOULD NOT ALLOW CABIN TO HOLD PRESSURE) AND OR THE OVERHEAD BLOWER FAN. 2L72 4F4 FRTA22CE E25EA 20030509000822003050900082NM 2003 5 9 HOC2003F00002 120030425A5320 INTERCOSTAL BOEING727 727231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON OUTBOARD LWR INTERCOSTAL, STA 1070-STGR30, RBL 2.0. 2L73 4F4 F A3WE E2EA 20030509001112003050900111SW 2003 5 9 ALGA086246 120030423A6220406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR SEIZED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL350 53265 FOUND BEARING WORN, RATCHETING AND SEIZED IN SMALL ARC OF TRAVEL. BEARING REPLACED BY (FIELD) MAINT. 1G71 3U3 UO H2SW E1GL 20030508001062003050800106NM 2003 5 8 DL73S030368 120030417A3350BPS73 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27308DL 23080 ON LAYOVER FOUND EMERGENCY LIGHTS OUT ROW 1-4 - REPLACED POWER SUPPLY 2L72 4F RTA16WE 20030509000212003050900021EU 2003 5 9 A6WA200360006 120030411A7603 LEVER BAC 146 146200A 1500266EU NR 3 ENGINE OUT OF RIG A A6WAO OTHER O OTHER TXTAXI/GRND HDL 1 GL31609AW E2070 NR 3 THRUST LEVER NEEDS TO BE RE-RIGGED. UNABLE TO SET BELOW 40 PERCENT N1. (M) 2H74 4F A49EU 20030509000252003050900025 2003 5 9 MEX2003137 420030415A2565 ARM BOEING757 7572Q8 1384972NM ESCAPE SLIDE JAMMED A ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23802AM 26270 CAPTAIN REPORTED THAT WAS NOT POSSIBLE TO ARM THE EMERGENCY SLIDE OF DOOR NR 4 IT WAS JAMMED. AIRCRAFT WAS SENT TO THE HANGAR WHERE WAS TESTED AND ADJUSTED THE MECHANISM WAS ADJUSTED IAW MM 52-11-20, ALL CORRECT. (M) 2L72 4F RTA2NM 20030509000552003050900055SO 2003 5 9 FTU2003F00008 220030424A74141051324 SPRING BEECH 36 A36 1151604CE CONT O520 IO520B 17032SO IMPULSE COUPLINGBROKEN B FTURO OTHER O OTHER NRNOT REPORTED 1 NE05951LH884 E2300 CUSTOMER WAS COMPLAINING OF A ROUGH RUNNING ENGINE DUE TO A BAD LEFT MAGNETO, REMOVED MAGNETO AND FOUND THE IMPULSE COUPLING SPRING WAS BROKEN. COUPLING SPRING REPLACED WITH A NEW PART, REINSTALLED MAGNETO AND TIMED TO ENGINE. GROUND RAN ENGINES AND NO FURTHER PROBLEM FOUND. 1L71 3O3 O 3A15 E5CE 20030509000762003050900076NM 2003 5 9 A6WA200330009 120030424A3350321431 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE EMERGENCY LIGHTSINOPERATIVE A O OTHER O OTHER NRNOT REPORTED 1 GL31329MX1814 1814 3049 EMERGENCY LIGHT GO DIM AND THEN OUT. REMOVED AND REPLACED BATTERY AS REQUIRED IAW JOB INSTRUCTION CARD. NO FURTHER OCCURRANCES, NO REPEATS, NO TRENDS. SUSPECT LOW BATTERY POWER. (M) 2H72 4T4 TRTA45NM E20NE 20030509001192003050900119EU 2003 5 9 I05R086278 120030416A3310013020020010 POWER SUPPLY UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE LIGHT FAILED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0526LB 550 3514 POWER SUPPLY HAD PARTIAL FAILURE, POWER SUPPLY REMOVED AND REPLACED 1G72 3U3 U H9EU E00054EN 20030509001392003050900139EU 2003 5 9 DHL2003363003 120030507A3240 HOSE AIRBUS300 A300B4203 3930306EU BRAKE SYS FAILED A DHLAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SO01363DH 85 AT THE BEGINNING OF THE TAKE-OFF ROLL THE GREEN SYSTEM (HYDRAULIC) LEVEL LOW LIGHT ILLUMINATED. THE TAKE-OFF WAS REJECTED AT 70 KNOTS, 260000 LBS, OAT 14ØC, -10 FT P.A., AND A MAXIMUM BRAKE TEMPERATURE OF 150ØC WAS REACHED. REPLACED BLOWN HOSE WITH LIKE UNIT. SERVICED GREEN SYSTEM AND PRESSURE CHECKED PER 29-21-00. NO LEAKS NOTED. MAX BRAKING, REJECTED TAKEOFF INSPECTION DUE. MAX BRAKE TEMPERATURE OF 450ØC NOT MET. INSPECTED BRAKES AND TIRE PLUGS IAW 32-41-00 AND 32-42-27. ALL SYSTEMS OK. 2L72 4F RTA35EU 20030509001762003050900176EU 2003 5 9 USAASA03031 120030404A3350321430 BATTERY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19111US 1114 LGA - AIRCRAFT FAILED THE EMERGENCY LIGHT TEST. MAINTENANCE REPLACED THE BATTERY IN THE EMERGENCY POWER SUPPLY UNIT AT THE RIGHT OVERWING EMERGENCY EXIT. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030513000012003051300001WP 2003 5 13 AALA20030370 120030325A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21567AM 53293 FOUND CORROSION ON DOOR AFT CARGO JAMB BEAM UPPER AND LOWER LEG OF BEAM VARIOUS PLACES. TREATED, PRIMED, PAINTED AND BLENDED AREA. INSTALLED DOUBLER PER ESO 80559 DATED 3-14-03. (M) 2L72 4F RTA6WE 20030513000852003051300085NM 2003 5 13 UPS03240666 120030414A5210 ATTACH FITTING BOEING727 72722C 138400FNM RT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, RT MLG WING DOOR ACTUATING ROD ATTACH FITTING CRACKED FITTING REPLACED IAW EO B727-3210-2583-G APP. D, E, F & G 2L73 4F A3WE 20030513000932003051300093NM 2003 5 13 C8GA20030012 120030507A7920453953 LINE BOEING727 727225 1384077NM PWA JT8 JT8D9A 52048NE ENGINE OIL CRACKED A C8GAE ENGINE SHUTDOWN K FLUID LOSS DEDESCENT 1 SO15808EA 22439 666344 THE NR 1 OIL QUANTITY DROPPED TO A .25 GALLON ON DOWNWIND FOR RUNWAY 12R INTO KMSP. INFLIGHT SHUT DOWN OF THE NR 1 ENGINE AS PRECAUTIONARY IN ACCORDANCE WITH CCIA PROCEDURES, ADVISED ATC AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND AN OIL PRESSURE LINE LEAKING AT THE FUEL/OIL COOLER IN THE NR 1 ENGINE. REMOVED AND REPLACED OIL LINE IAW STC INSTALL PROCEDURES IM-727S3HW. OPERATIONAL AND LEAK CHECK NORMAL PER MM 72-00, AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20030513001172003051300117NM 2003 5 13 QXEA0300518 120030418A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 GOUGE ON FUSELAGE SKIN AT X47 AND STRINGER 24R. REPAIRED IAW HORIZON AIR EA 6-53-243. 2H72 4T RTA13NM 20030513001402003051300140NM 2003 5 13 F3LA200300118 120030411A5320 FLOOR SUPPORT BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 3468 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT STA. 727D + 5. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53. 2L72 4F RTA16WE 20030513001452003051300145NM 2003 5 13 CH1A200395042 120030415A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOOR SUPPORT AT BL 0 BETWEEN BS400-BS420 IS GOUGED AND CORRODED AROUND FASTENER HOLES 2L73 4F A3WE 20030513001562003051300156NM 2003 5 13 QXEA0300459 120030402A5230 GUIDE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 FORWARD BAGGAGE DOOR FORWARD LOWER ROLLER GUIDE DENTED WITH UPSET METAL AT LEADING EDTE. REPAIRED IAW RD 8/4-52-025. 2H72 4T RTA13NM 20030509001362003050900136NM 2003 5 9 0300916638 120030507A2120 ODOR BOEING747 747251B 1384892NM CABIN DETECTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL01638US 23549 DURING DESCENT A BURNING ODOR EMITTED BY DOOR 5L. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. ODOR DISSIPATED AFTER LANDING. CHECKED ELECTRICAL SYSTEMS BY DOOR 5L WITH NO FAULTS FOUND. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030509001442003050900144NM 2003 5 9 DHL2003754005 120030507A2613 WARNING LIGHT BOEING727 727223 1384074NM OVERHEAT WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 LOWER AFT BODY OVERHEAT WILL NOT TEST. DEFERRED PER MEL 26-20-2 CAT. "C". SPECIAL PROCEDURE COMPLIED WITH. DMI 12836 PLACARD INSTALLED. MAINTENANCE CONTROL NOTIFIED. REF. DMI 12836, LOWER AFT BODY OVERHEAT WILL NOT TEST. REPLACED LOWER AFT BODY CORRY LIGHT ASSEMBLY IAW B-M/M 33-10-51. OPS CHECKED GOOD. THIS CLEARS DMI 12836. PLACARD REMOVED. 2L73 4F A3WE 20030509001522003050900152NM 2003 5 9 AMTA200300475 120030408A3350SG9930 LIGHT BOEING737 73783N 13844HINM CABIN LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11320TZ 32610 EGRES LIGHTING STRIP NEEDS TO BE RESECURED AT MOST FORWARD LOCATION. REMOVED AND REPLACED FORWARD 3.5 FOOT EGRESS STRIP SECTION PER MM REF 33-51-15-902, OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030509001552003050900155NM 2003 5 9 USAASB03052 120030406A3260MS253831 SWITCH BOEING737 7374B7 1384702NM MLG INDICATOR FAILED A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19426US 24548 CLT - FLT 1953 - ON GEAR EXTENSION INTO CLT, CREW RECEIVED THREE RED AND THREE GREEN GEAR INDICATION LIGHTS. CREW DECLARED AN EMERGENYC AND ACCOMPLISHED TOWER FLYBY TO DETERMINE GEAR WAS DOWN. CREW ALSO VERIFIED GEAR WAS LOCKED THROUGH LANDING GEAR VIEWING PORTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAITNENANCE PINNED GEAR AND THE AIRCRAFT TAXIED TO GHE GATE. MAINTENANCE FOUND THE S78 CONTROL LEVER SWITCH OUT OF ADJUSTMENT. READJUSTED SWITCH PER MM 32-61-11. ALSO, LUBRICATED LEVER LATCH RELEASE TRIGGER WHICH WAS FOUND TO BE STICKING TO HANDLE ASSEMBLY. ACCOMPLISHED GEAR SWING. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20030509001602003050900160 2003 5 9 AMTA200300441 420030402A3417 PITOT HEAD BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE MISSING A AMTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL11554TZ 32588 31817 ON CLIMB SIGNIFICANT SURGE IN ALL PARAMETERS ON THE RIGHT ENGINE. COMPLETED ENGINE SURGE/STALL CHECKLIST AND REVIEWED. ENGINE EEC LIGHT ILLUMINATED CHECKLIST CONDITIONS PERSISTED AT ALL POWER SETTINGS. PERFORMED FIM TASK 71-06-00 FIG 102. FOUND PITOT HEAD ON PF RAKE MISSING. ACCOMPLISHED M/M 77-11-04-2 BLANK INSTALLATION. RAN ENGINE SEVERAL EPR SETTINGS, OPS NORMAL. (M) 2L72 4F4 FRTA2NM E12EU 20030508000332003050800033 2003 5 8 IL32003F00000 420030331A34185038040 PITOT TUBE BEECH 36 B36TC 1151609CE CONT O520 TSIO520* 17040SO LT WING BROKEN B IL3RO OTHER O OTHER NRNOT REPORTED 1 WP076554K504 EA324 AIRCRAFT BROUGHT IN FOR 24 MONTH ALTIMETER/TRANSPONDER CERTIFICATION. WHILE TROUBLESHOOTING LEAKS, THE SOLID NUMBER 4 COPPER LINE FROM THE PITOT TUBE ASSEMBLY WAS FOUND TO BE BROKEN FLUSH WITH THE ASSEMBLY CASTING. THE LINE HAD BEEN EPOXIED BACK ON TO THE ASSEMBLY CASTING BY FILLING THE CAVITY BEHIND AND INTO THE CASTING AND FORMING THE EPOXY AROUND THE LINE USING SOME KINK OF FLEXIBLE FORM. IT LOOKS LIKE DUCT TAPE WAS USED TO FORM THE EPOXY AND ADHESIVE WAS STILL ON IT. THE TUBE ASSEMBLY HAD BEEN INSTALLED (NEW) ON 9/5/92 WITH 887.7 HOURS ON THE AIRCRAFT. 1L71 3O3 O 3A15 E8CE 20030508000362003050800036NM 2003 5 8 QXEA0300531 120030426A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX- EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 1. REMOVED AND REPLACED LIGHT ASSEMBLY AT FORWARD SECTION OF TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030508000442003050800044EU 2003 5 8 03FDEA00675 120030503A7830FXCOMP233T ANGLE AIRBUS300 A300F4605R 3930327EU THRUST REVERSER GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25682FE 800 NR 233 NR 2 ENG I/B THRUST REVERSER LOWER CORE STRUCTURE ANGLE GOUGED 4 AREAS. R/R ANGLE PER IAW SRM 51-40-21 SRM 51-40-21 AT MAE. 2L72 4F RTA35EU 20030508001092003050800109NM 2003 5 8 DLM88030371 120030418A3230MS288892 VALVE DOUG MD88 MD88 3023688NM NLG LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27988DL 53339 UPON GEAR RETRACTION NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUM. HAD NOISE INDICATING GEAR NOT FULLY RETRACTED. AIR RETURN TO IAD. MAINTENANCE FOUND NLG STRUT FLAT. UPPER SHRAEDER VALVE LEAKING. REPALCING SAME AND SERVICING STRUT. 2L72 4F RTA6WE 20030508001222003050800122EU 2003 5 8 MALA030251 120030428A4900 APU BAC 146 AVRO146RJ85A1500097EU SHUTDOWN A MALAO OTHER O OTHER CLCLIMB 1 GL15526XJ E2351 DURING CLIMBOUT OF FLIGHT 3567, APU AUTOSHUTDOWN. APU AUTOSHUTDOWN DURING CLIMB THRU 24000 FT. NO RESTART ATTEMPTED. MAINTENANCE GROUND RAN 45 MINUTES, UNABLE TO DUPLICATE. 2H74 4F RTA49EU 20030508001372003050800137NM 2003 5 8 DLM88030379 120030420A27804952287503 SWITCH DOUG MD88 MD88 3023688NM COCKPIT MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27985DL 53312 DURING CLIMB OUT SLAT DISAGREE LIGHT ILLUMINATED WITH SLAT HANDLE IN UP POSITION AND GOOD INDICATION . REPLACED FLAP HANDLE POSITION SWITCH SLAT OPERATION AND INDICATION NORMAL RAN BITE ON PSEU NO FAULTS 2L72 4F RTA6WE 20030509000332003050900033WP 2003 5 9 GTIA030247 120030406A33501001191 LIGHT DOUG DC9 DC983 3022083WP CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 ACY - FOUND FORWARD EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT ASSEMBLY FUNCTIONAL CHECK GOOD. (M) 2L72 4F RTA6WE 20030509000352003050900035WP 2003 5 9 GTIA030249 120030306A5310 BEAM DOUG DC9 DC983 3022083WP CARGO DOORWAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND AFT LOWER CARGO, LOWER JAMB DOOR CUTOUT OUTBOARD BEAM CORRODED STATION 1155 TO STATION 1211. FABRICATED 1 DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20030509000382003050900038WP 2003 5 9 GTIA030233 120030201A5753 VANE DOUG DC9 DC981 3022081WP TE FLAP GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FOUND LT WING CENTER FIXED VANE OUTBOARD FLAP HAS 2 PLACES GOUGES. BLENDED GOUGES. MATERIAL LOSS FOUND TO BE OT OF LIMITS. REPAIRED LEFT WING CENTER FIXED VANE. (M) 2L72 4F A6WE 20030509000652003050900065EA 2003 5 9 W0P2003F00000 120030325A5521C2TE103AND RIB DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985* 52008NE ELEVATOR CORRODED E W0PCO OTHER O OTHER NRNOT REPORTED 1 AL059290Z 1387 UPON COMPLYING WITH AD, FOUND CORROSION TO HAVE SEVERELY EATEN AWAY THE TIP RIB ON FOUR DIFFERENT ELEVATORS. 1H71 3R3 R A806 5E1 20030509000672003050900067NM 2003 5 9 HOC2003F00001 120030420A5347 SEAT TRACK BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON SEAT TRACK STA 1070-1130 LT. 2L72 4F4 FRTA16WE E2EA 20030509000682003050900068NM 2003 5 9 HOC2003F00003 120030425A5315 FLOORBEAM BOEING727 727231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON FLOORBEAM TOP SURFACE STA 440, 12 LBL-12 RBL. 2L73 4F4 F A3WE E2EA 20030509001482003050900148NE 2003 5 9 AMTA200300419 220030330A7200 ENGINE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RIGHT MALFUNCTIONED A AMTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL11524AT 30233 31677 RT ENGINE WOULD NOT REACH MAX TAKEOFF EPR WITH EEC AND ENG LIMITER ON STD TAKEOFF EPR NORMAL. ENGINE PARAMETERS NORMAL FOR LOW EPR. TAKEOFF WITH EEC AND ENGINE LIMITER OFF NOT CHECKED. FOLLOWED FIM 73-21-00, STEP 1-21 PER FIM NO FURTHR ACTION REQUIRED OK FOR SERVICE. (M) 2L72 4F4 FRTA2NM E12EU 20030509001632003050900163NM 2003 5 9 USAASB03050 120030403A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT ROW 11DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AT STATION 634L. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030509001712003050900171NM 2003 5 9 USAA030036 120030407A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US35261 24812 FOUND SKIN CRACKED 3 INCHES, RIGHT SKIN BETWEEN STATION 727E-727F AT STATION 25R. REMOVED CRACK SECTION OF SKIN AND INSTALLED .63 INCHES EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20030509001772003050900177NM 2003 5 9 USAABB03055 120030403A3310141T480149 WINDSHIELD BOEING757 7572B7 1384964NM LEFT SMOKE A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19632AU4094 27810 DEN - FLT 607 - APPROXIMATELY FORTY MILES EAST OF DENVER, SMOKE BEGAN TO POUR FROM THE AREA OF THE CAPTAIN'S GLARESHIELD. CREW DONNED SMOKE GOGGLES AND OXYGEN MASKS. FLIGHT DIVERTED TO DENVER AND LANDED WITHOUT FURTHER INCIDENT. S/D - MAINTENANCE FOUND THE J5 CONNECTOR AND SENSOR FOR LEFT WINDSHIELD BURNED. THE WINDSHIELD WAS REPLACED, AS WELL AS THE WINDSHIELD HEAT CONTROLLER. (M) 2L72 4F RTA2NM 20030513000182003051300018EU 2003 5 13 AALA20030224 120030223A3397 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2141063 506 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON SEAT 27G INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030513000492003051300049EA 2003 5 13 03130673 120030510A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGNECY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27673BR 7599 DURING MAINTENANCE INSPECTION, THE RT FWD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513000532003051300053NM 2003 5 13 AALA20030357 120030321A3350 BATTERY BOEING757 757223 1384957NM EMERGENCY LIGHT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21624AA 24582 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. CLEANED BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030513000662003051300066NM 2003 5 13 CALA0300238 120030510A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2746625 27529 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-30-51. 2L72 4F RTA16WE 20030513000752003051300075SO 2003 5 13 RAIA00304125 120030429A3350RSP1B POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTPINOPERATIVE A RAIAO OTHER L NO TEST NRNOT REPORTED 1 CE03815HK838 145048 OVER-WING EMERGENCY LIGHT INOP BOTH SIDES. REMOVED AND REPLACED POWER SUPPLY, OPS CK OK. 2L72 4T RTT00011AT 20030513000812003051300081EU 2003 5 13 AWXA200300507 120030506A3250 CONTROL UNIT AIRBUS320 A320232 3930326EU BRAKE SYSTEM MALFUNCTIONED A AWXAO OTHER J WARNING INDICATION APAPPROACH 1 WP28619AW 527 ON APPROACH INTO PHL EN ROUTE FROM PHX RECEIVED BRAKE STEERING CONTROL UNIT (BSCU) FAULT CHANNEL NR 1; SYSTEM PREVIOUSLY WAS MEL'D IN SNA (MEL 32-42-03, COND. 1 "BSCU SYS NR 1 INOP"). DECLARED EMERGENCY AND LANDED WITHOUT EVENT, AIRCRAFT ABLE TO TAXI TO GATE. MAINTENANCE REMOVED AND REPLACED BSCU IAW AWA T/C R2A32301. VENDOR FUNCTIONAL TEST OF BSCU S/N 118 WAS UNABLE TO CONFIRM REASON FOR REMOVAL (NO FAULT FOUND). PERFORMED SERVICE BULLETIN C20216-32-3229, PART NUMBER CONVERTED TO C202163382D32. UNIT TESTED AND RETURNED TO SERVICE IAW CMM 32-47-27. 2L72 4F RTA28NM 20030513000832003051300083NM 2003 5 13 UPS03240664 120030428A5711 FRAME BOEING727 72722C 138400FNM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, FRAME ASSY ON LWR SURFACE OF APU EXHAUST PANEL ON RT WING IS CORRODED. FRAME ASSY REPLACED IAW DRAWING 6562837 & SRM 51-30-32 2L73 4F A3WE 20030513000912003051300091NM 2003 5 13 UPS03240674 120030415A5320 SUPPORT BOEING727 727185C 138406NNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C&SI, SUSPECT CORROSION UNDER 2 STRIP PANELS EITHER SIDE OF FEEL COMPUTER BOTH PANELS HAVE SUSPECT BULGES IN AREAS AROUND FASTENERS TO FACILITATE ACCESS LT & RT PANELS NT 9703 & 9704 REMOVED IAW SR M 51-30-5 REMOVED LT & RT TEE SUPPORTS IAW SRM 51-30-2 LT & RT T-CHORD SUPPORTS REPLACED IAW DRAWING 65-72786 2L73 4F A3WE 20030513000942003051300094NM 2003 5 13 AWXA200300496 120030507A3397BMS13311122 WIRE BOEING737 737301 1384611NM SEAT ROW 17 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING INSPECTION A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE WAS FOUND AT THE SPLICE UNDER CENTER OF SEAT ROW 17 L/H. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 17 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030513001042003051300104NM 2003 5 13 377PA0015 120030503A3350 WIRE BOEING737 7373L9 1384470NM EMERGENCY LIGHT DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05377PA 23718 EMERGENCY LIGHTING INOP. ROW 18 AFT. REPAIRED WIRING IAW SP CHPT.20. TEST OK 2L72 4F RTA16WE 20030513001122003051300112NM 2003 5 13 CH1A200395058 120030426A5753 SLAT TRACK BOEING727 727290 138408WNM LT WING CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LT WING L/E CUTOUT FOR NR 4 SLAT I/B TRACK IS CRACKED AT AFT EDGE. 2L73 4F A3WE 20030513001282003051300128WP 2003 5 13 UPS03840682 120030413A5711 SPAR DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, HFEC HOLE INSPECTION DETECTED A CRACK ON THE RT WING FORWARD LOWER SPAR BETWEEN STA. XFS 515-XFS 526.76 IN HOLE NR 8 (PG. 15 OF E.O. DC8-5710-14184-D) COINED 10 EA. HOLES IN CONDITION 1, COLD WORKED 1 HOLE IN CONDITION 2 NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED FLUSH REPAIR BUSHING IAW DWG.4709980, E.O. DC8-5710-14184APPX. E,DWG. J060232,AND SRM. 51-3-5 2L74 4F RT4A25 20030508000642003050800064NM 2003 5 8 2003UALA00401 120030429A3350 CABLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT SHORTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29550UA 25398 EEL LIGHTING OUT AT SEAT 23 TO 31. REPLACED TRACK FEEDER CABLE. 2L72 4F4 FRTA2NM E17NE 20030508001252003050800125NM 2003 5 8 UPS03440620 120030414A531065B0831519 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C M/D - BS 1283 LT STR 16L SHEAR TIE FOUND CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030508001472003050800147NM 2003 5 8 QXEA0300499 120030420A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM TE FLAPS SEPARATED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 RT OUTBOARD FLAP TRAILING EDGE HAS SEPARATION AND LOOSE RIVETS ALONG AFT EDGE BETWEEN YW371 AND 407. REPAIRED IAW DHC-8-400 SRM TASK 51-25-15-370-801. 2H72 4T RTA13NM 20030509000262003050900026EA 2003 5 9 A6WA200340052 120030414A5245 PANEL CNDAIRCL600 CL6002B19 1900309EA DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 RIGHT BUTE DOOR PANEL 694PB, HAS ELONGATED HOLE REAMED HOLE, FABRICATED FREEZE PLUG, INSTALLED FREEZE PLUG. ALL WORK ACCOMPLISHED IAW WVAC EO 601R-57-3931. (M) 2L72 4F RTA21EA 20030509000442003050900044SO 2003 5 9 SIMA200308408 120030322A5313 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21626AE 145117 ABI - FOUND AIRCRAFT ARRIVED FOR PERMANENT REPAIR OF TDMI NR 626MQ530307 DENT ON LEFT FUSELAGE BETWEEN FRAMES 8 AND 9 AND BETWEEN STRINGERS 15L AND 17L. PERFORMED A 3 INCH BY 1.5 INCH CUTOUT OF DAMAGED AREA. CLEANED AND TREATED CUT OUT. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB SRM, SRM EMB 145 1142 REV 20, CHAPTERS 53-10-01 FIG 201. (M) 2L72 4T RTT00011AT 20030509001412003050900141EU 2003 5 9 MALA030263 120030507A3260006WS00 WEU SAAB SF340 SF340A 7850100EU COCKPIT MALFUNCTIONED A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL1598XJ 340A098 RT MLG LIGHT TAKES AN EXTRA MINUTE FOR LIGHT TO COME ON DURING EXTENSION. RT MAIN WHEEL INDICATOR WOULD NOT ILLUMINATE IN TRAN. LIGHT WAS OUT, PUMP NOT RUNNING TRIED MOVING INDICATOR NO HELP 1 MINUTE LATER LIGHT CAME ON. MAINTENANCE REPLACED WEU PN 006WS00, SN/OFF 1632, SN/ON 1634. REPLACED LANDING GEAR CONTROL UNIT PN D494-12-001 SN/OFF 619/10-96, SN/ON 606/04-96. IAW SAAB AMM CHAP 32. 2L72 4T RTA52EU 20030509001502003050900150NM 2003 5 9 USAABB03057 120030322A49005835239003 PACKING BOEING757 7572B7 1384964NM GEARBOX LEAKING A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19633AU 27811 EN ROUTE PHL-PHX, WITH THE LFT GENERATOR ON MEL AND APU OPERATING, THE CREW NOTED A DECREASE IN THE APU OIL FROM 'FULL' TO .'50' TO 'REFILL'. SHORTLY THEREAFTER THE APU PERFORMED AN AUTO SHUTDOWN. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN DEN REPLACED THE APU OIL LINE. MAINTENANCE IN PHX (FL 9242) RAN THE APU AND COULD NOT FIND AN OIL LEAK. ON THE SUBSEQUENT FLIGHT (FL 162, 3/23/03), THE APU WAS AGAIN OPERATING DUE TO THE LEFT GENERATOR MEL, AND THE APU LOST OIL AGAIN. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACD THE APU. UPON TESTING THE APU UNDER PRESSURIZED CONDITIONS, OIL LEAKED FROM THE SPLIT LINE BETWEEN THE LOAD COMPRESSOR AND TH2L72 4F RTA2NM 20030509001622003050900162NM 2003 5 9 USAASB03049 120030402A2612659401 MODULE BOEING737 7373B7 1384580NM E/E BAY INOPERATIVE A USAAO OTHER N FALSE WARNING CRCRUISE 1 EA19528AU 24410 CLT - FLT 560 - EN ROUTE FROM PIT-CLT, CREW REPORTED THE FIRE LIGHTS/BELL CUTOUT LIGHTS ON BOTH SIDES OF THE GLARESHIELD ILLUMINATED TWICE DURING FLIGHT. NO OTHER BELLS, FIRE HANDLE LIGHTS OR MASTER CAUTION LIGHTS WERE REPORTED TO HAVE SOUNDED/ILLUMINATED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE ENGINE AND APU FIRE DETECTION M279 MODULE. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20030513000152003051300015NM 2003 5 13 AMTA200300317 120030306A3610312N53217 DUCT BOEING757 75728A 1384976NM RT ENGINE DAMAGED A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11521AT 24368 EICAS STATUS MESSAGE RIGHT STRUT O/H DET 1 DISPLAYED. REMOVED AND REPLACED RIGHT ENGINE SUPPLY HIGH PRESSURE DUCT IAW MM 36-11-01. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030513000522003051300052WP 2003 5 13 AALA20030356 120030321A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DIRTY A AALAK NONE O OTHER ININSP/MAINT 1 SW21463AA 49593 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD WG HATCH RIGHT AND LEFT SIDE INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030513000612003051300061NM 2003 5 13 PCAA0305071 120030505A33506104789 BATTERY DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DISCHARGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13839EX 226 CREW REPORTED NUMEROUS FLOOR PROXIMITY EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513001372003051300137 2003 5 13 MDAS092019 420030416A2210 SWITCH BOEING737 737800* NM NR 1 FCC FAILED W Q0MFC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 WP03 28236 ON APRIL 16, EXPERIENCED ABORTED TAKEOFF DUE TO FCC INTERMITTENT FAULT. TO/GA DIDN'T SHOW AND FD DISAPPEARED FROM BOTH MONITORS AFTER PUSHED THE AUTO-THROTTLE TO/GA SWITCHES DURING TAKEOFF. THE CREW FOLLOWED QRH AND DECIDED TO ABORT TAKEOFF. IAW AMM 22-11-00, CHECK FOUND NR 1 FCC FAULT. REMOVED NR 1 FCC FOR PIN CLEANING. REINSTALLED IT AND FUNCTIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO DISPATCH. 2L72 4F RTA16WE 20030513001542003051300154NM 2003 5 13 QXEA0300457 120030405A5420 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM RT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 RIGHT HAND LOWER COWL CONE SUPPORT BRACKET UPPER ANGLE CRACKED AT FORWARD THREE RIVETS. REPAIRED IAW Q400 MM 71-61-01, TR 71-054. 2H72 4T RTA13NM 20030513001572003051300157NM 2003 5 13 QXEA0300460 120030402A5230 GUIDE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FORWARD BAGGAGE DOOR AFT LOWER ROLLER GUIDE WORN AT LEADING EDGE. REPAIRED IAW RD 8/4-52-025. 2H72 4T RTA13NM 20030513001662003051300166EU 2003 5 13 NSVA20030024 120030420A2611 CONNECTOR SAAB SF340 340B 7860101EU LAVATORY DIRTY A NSVAK NONE N FALSE WARNING CRCRUISE 1 EA27299CJ 340B299 LAVATORY SMOKE WARNING ANNUNICATOR GIVES FALSE ALARMS INFLIGHT. AIRCRAFT PERFORMED NORMAL SCHEDULED LANDING IN PVD. MAINTENANCE WAS DISPATCHED, TROUBLESHOT AND CLEANED THE CANNON PLUG ON THE LAVATORY SMOKE DETECTOR. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 20030513001752003051300175NM 2003 5 13 QXEA0300469 120030420A3260 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM MLG DIRTY A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09400QX 4030 AFTER TAKE OFF, THE NOSE GEAR GREEN LIGHT REMAINED ON AFTER THE GEAR WAS RETRACTED. THE GEAR WAS CYCLED AND HAD THE SAME RESULT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED, CLEANED, AND REINSTALLED THE CONNECTOR TO THE LANDING GEAR CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD AND THE RII INSPECTION WAS COMPLIED WITH. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20030513001782003051300178NE 2003 5 13 GLBA2003052 220030422A7412 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE IGNITER TRIPPED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03170GL UE170 RT IGNITER POWER CIRCUIT BREAKER POPPED W/N RESET, R&R RT IGNITER CB 2L72 4T4 TRTA24CE E26NE 20030513001812003051300181SO 2003 5 13 SWIA200311890 120030414A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER FAILED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07251YV6 6 120251 AFTER TAKEOFF, DISCOVERED WE HAD VERY LIMITED RIGHT RUDDER AUTHORITY. RIGHT RUDDER PEDAL WOULD ONLY DEPRESS ABOUT 1 1/2 INCHES. LEFT PEDAL TRAVEL NORMAL AND ALL COCKPIT INDICATIONS NORMAL. INSPECTED RUDDER FOR FREEDOM OF MOVEMENT, CHECKED GOOD. BLUE SYSTEM RUDDER ACTUATOR FAILED HEALTH CHECK. REPLACED RUDDER ACTUATOR IAW MM 27-22-02. OPS AND LEAK CHECKED GOOD. 2L72 4T4 TRTA31SO E20NE 20030513001832003051300183EA 2003 5 13 SWIA200311892 120030417A3350 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07588SW 7069 FLOOR TRACK EMERGENCY LIGHTING AT ROW 9-13 IS INOP.REMOVED AND REPLACED NR 4 INVERTER IAW MM 33-51-07. OPS CHECK GOOD. 2L72 4F RTA21EA 20030513001892003051300189SO 2003 5 13 SWIA200311898 120030418A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07289YV7607 7607 120289 NACELLE FLAPS SLOW TO RESPOND WHEN FLAP HANDLE POSITIONED UP, AND WE GET A DISAGREEMENT ON THE FLAP ANNUNCIATOR PANEL. INSTALLED SERVICEABLE LEFT NACELLE FLAP ACTUATOR. OPS CHECKS GOOD/LEAK CHECKS GOOD. NO FURTHER FAULTS NOTED. 2L72 4T RTA31SO 20030513002102003051300210SO 2003 5 13 C2XA03CL092 120030416A3350110049 CHARGER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT FAULTY A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2714945 145049 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING AT ROW 7-12 WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY CHARGER.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030513002232003051300223WP 2003 5 13 ZW0A0304503 120030419A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13966TW 53616 DURING OVERNITE INSPECT EMERGENCY LITE AT 27D INOP. RE-INSTALLED LITE BULB AT 27D. OPS CHECK NORMAL PER MM 33-53-00. CHECK-C 6-7-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030513002462003051300246EU 2003 5 13 A6WA200360012 120030421A5313 LONGERON BAC 146 146200A 1500266EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31290UE E2080 FORWARD CARGO DOOR CUTOUT LOWER LONGEORN CORROSION DAMAGE COMPLETELY THROUGH THE FACE LONGERON. REPAIR REQUESTED FOR BEE SYSTEM REF AVMAX-FAX 1584-60000. (M) 2H74 4F A49EU 20030513002552003051300255EA 2003 5 13 ASOA03177 120030420A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE FLOORBEAM BRACKET AT RBL 9 AND FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOORBEAM BRACKET AT RBL 9 AND FS 280 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030513002612003051300261EA 2003 5 13 ASOA03140 120030401A5343 SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING AN 'A' CHECK AT MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20030513002642003051300264NE 2003 5 13 RU3A03004 220030308A7200 ENGINE BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE RIGHT FAILED A RU3AA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW2167 FF2 PCE95331 RIGHT ENGINE FAILED SHORTLY AFTER TAKEOFF, CLIMBING THROUGH 2,500 FT EMEGENCY PROCEDURES ACCOMPLISHED, AND LANDED WITHOUT FURTHER INCIDENT. (M) 2L72 4T4 T A24CE E4EA 20030508001572003050800157NM 2003 5 8 QXEA0300450 120030414A5210 HANDLE BOMBDRDHC8 DHC8401 1390041NM PAX DOOR LACK OF LUBE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09401QX 4031 BOI - FLIGHT ATTNEDANT REPORTS THAT THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR HANDLE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030509000692003050900069NM 2003 5 9 HOC2003F00005 120030420A53206549606101 SPLICE BOEING727 727231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON TENSION TIE FITTING AND SPLICE ANGLE AT STA 1183, STR 17R. 2L73 4F4 F A3WE E2EA 20030513001602003051300160NM 2003 5 13 QXEA0300462 120030419A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT BURNED OUT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH248 514 RIGHT HAND AFT EGRESS LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513001642003051300164NM 2003 5 13 QXEA0300466 120030417A335010126271 SOCKET DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX- LEFT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED SOCKET AND BULBS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513001672003051300167CE 2003 5 13 AMWA19 120030407A5346 PLATE BEECH 1900 1900D 1154162CE TRUSS CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0715YV UE15 WHILE PERFORMING AN "A" CHECK ON THE LEFT AND RIGHT SIDE OF ENGINE TRUSSES, THE LEFT AND RIGHT PRESSURE PLATES HAVE RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE CHAFING. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030513001762003051300176NM 2003 5 13 QXEA0300470 120030419A335061047811 BATTERY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH6822 264 514 RT HAND AFT EGRESS LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY P54. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513002022003051300202EA 2003 5 13 QXEA0300477 120030407A5340 CLIP CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 AT FS 1108 LEFT HAND SIDE LOOKING FORWARD CLIP LOWER FASTENER HOLE ELONGATED. REPAIRED IAW HORIZON AIR EO R-53-44B, EA 53-89 AND EO 601R-53-3923. 2L72 4F RTA21EA 20030513002032003051300203EA 2003 5 13 QXEA0300479 120030416A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 AIRCRAFT SKIN HAS LIGHT SURFACE CORROSION AT UPPER TCAS ANTENNA MOUNT POINT.REPAIRED IAW CRJ NDT 51-20-06. 2L72 4F RTA21EA 20030513002042003051300204NM 2003 5 13 QXEA0300480 120030410A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 SCRATCHES IN FUSELAGE SKIN BETWEEN THE FORWARD BAG DOOR AND THE EMERGENCY EXIT DOOR. REPAIRED IAW SR, 51-20-10-150-001. 2H72 4T RTA13NM 20030513002082003051300208NM 2003 5 13 QXEA0300484 120030414A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 GOUGE ON FUSELAG BELLY SKIN AT X260 AND STRINGER 27L. REPAIRED IAW DHC-8-400 SRM TASK 51-25-15-370-801. 2H72 4T RTA13NM 20030513002272003051300227SO 2003 5 13 C2XA03SH116 120030425A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 DURING C CHECK THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND NOT TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY BATTERY POWER SUPPLY POWERING AFFECTED LIGHT. PERFORMED AN OPERATIONAL CHECK. OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030513002312003051300231SO 2003 5 13 C2XA03BT056 120030423A527057275 SWITCH EMB 145 EMB145LR 3260212SO SERVICE DOOR OUT OF ADJUST A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW2716954 145072 SERVICE DOOR OPEN WARNING LIGHT INFLIGHT. REMOVED AND REPLACED SWITCH 57275 AND READJUSTED SWITCH 57246 IAW EMB MM 52-74-01. OPS CHECK GOOD. 2L72 4T RTT00011AT 20030513002372003051300237EA 2003 5 13 ASOA03173 120030420A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOORBEAM AT LBL 27 AND FS 589 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOORBEAM AT LBL 27 AND FS 589 IAW SRM 51-00 AND SRM 53-00. (M) 2L72 4F RTA21EA 20030513002502003051300250EA 2003 5 13 ASOA03171 120030420A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE SERVICE DOOR SILL STRINGER BETWEEN FS 310 AND FS 349 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE SERVICE DOOR SILL STRINGER BETWEEN FS 310 AND FS 349 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030513002522003051300252EA 2003 5 13 ASOA03152 120030410A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING A C-CHECK IN MCN, THE FORWARD ATTACHING ANGLE ON THE RIGHT SIDE FLOORBEAM BELOW THE COCKPIT DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD ATTACHING ANGLE ON THE RIGHT SIDE FLOORBEAM BELOW THE COCKPIT DOOR IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030513002532003051300253EU 2003 5 13 ASOA03156 120030412A33507012210 BULB AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030513002742003051300274EA 2003 5 13 ASOA03139 120030331A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 DURING A GROUND INSPECTON IN DFW, THE EXTERIOR SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR SERVICE DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030513002802003051300280EU 2003 5 13 A6WA200360018 120030423A5730 SKIN BAC 146 146200A 1500266EU LT WING LE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LEFT WING INBOARD LEADING EDGE HAS 1 HOLE ENLARGED IN TOP SKIN ABOVE NR 2 PYLON. REPAIRED IAW RIL HC572H9066 AND FAX BARA/AVR/6362/03-DC. (M) 2H74 4F A49EU 20030509000132003050900013 2003 5 9 GTIA030243 420030402A2565 SLIDE DOUG DC9 DC941 302207NWP CABIN DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23130NK 47604 EMERGENCY SLIDE PACK FELL OFF. REINSTALLED LANYARD SLIDE CHECK OK. (M) 2L72 4F A6WE 20030509000162003050900016EA 2003 5 9 A6WA200340051 120030415A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 RT INBOARD FLAP, FLAP VANE HAS CHAFE DEEPER THAN PRESCRIBED LIMITS PER REO 601R-57-52-004, .014 DEEP. REMOVED AND REPLACED DEFECTIVE SECTION OF RIGHT FLAP VANE IAW WVAC EO 601R-57-3940. (M) 2L72 4F RTA21EA 20030509001022003050900102 2003 5 9 AC2A086263 420030410A3421430375002107 DISPLAY BELL 430 430 1182150SW ALLSN 250C 250C* GL EFIS INOPERATIVE E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH5442 49037 EFIS DISPLAY DIMS AND FLASHES. REPLACED TUBE. 1G72 3U3 URTH9SW E4CE 20030509001452003050900145EU 2003 5 9 USAASA03030 120030401A33501012887 LIGHT AIRBUSA319 A319112 3930323EU PAX CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19745UW 1289 THE EMERGENCY RED LIGHTS AT ROW 8 A/C RIGHT ARE MISSING, ALONG WITH THE LENS. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030513000442003051300044EA 2003 5 13 SWIA200311952 120030507A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07493SW 7450 ONE FLOOR LEVEL EMERGENCY LIGHT STRIP IS INOP. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY LIGHT STRIP IAW 33-51-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20030513000922003051300092NM 2003 5 13 UPS03240675 120030422A5350 FRAME BOEING727 727185C 138406NNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3431, AFT FORMED SECTION HAS HEAVY CORROSION UNDER FLOATING ANCHOR NUTS REMOVED FASTENERS ON FRAME IAW SRM 51-30-02. CORRODED SECTION OF FRAME FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01 FIG 1 & CORRODED SECT ION OF FRAME REMOVED IAW SRM 51-10-06 REPAIRED FRAME IAW SRM 51-40-3 2L73 4F A3WE 20030513001162003051300116NM 2003 5 13 QXEA0300503 120030421A5510 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZONTAL STAB LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 SHIM AT FORWARD RIGHT HAND HORIZONTAL STAB ATTACH FITTING IS MIGRATING. REPAIRED IAW DHC-8 400 AMM 55-10-00-400-801. 2H72 4T RTA13NM 20030513001182003051300118WP 2003 5 13 ABXA030136 120030418A3260 PROXIMITY SENSOR DOUG DC9 DC931 3022065WP MLG DOOR OUT OF ADJUST A ABXAB EMER. DESCENT N FALSE WARNING CRCRUISE 1 GL23944AX 47550 GEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. GEAR RECYCLED. EMERGENCY DECLARED. LIGHT REMAINED ILLUMINATED UNTIL DESCENT. CREW VERBAL GEAR UPLATCH CHECK WAS NORMAL. COULD NOT DUPLICATE. VERIFIED RIGHT MAIN LANDING GEAR DOOR POSITION SENSOR WAS OUT OF RIG. RIGGED TARGET AND SENSOR TO SPECS IAW DC-9 AMM 32-60-03-2-0201. FINAL DOOR INDICATION WAS NORMAL. 2L72 4F A6WE 20030513001532003051300153NM 2003 5 13 QXEA0300456 120030403A5210 SKIN BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 FORWARD ENTRY DOOR SHELL HAS A DENT APPROXIMATELY 6 INCHES FROM LOWER EDGE. REPAIRED IAW Q400 SRM 51-25-05, PAGE 208, PARAGRAPH F-4-A-D. 2H72 4T RTA13NM 20030513001622003051300162EA 2003 5 13 QXEA0300464 120030418A2840D98C09602 PRESSURE SENSOR CNDAIRCL600 CL6002C10 1390015EA RT ENGINE FAILED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09602QX2578 2578 10010 AFTER STARTING RT ENGINE, RIGHT MAIN EJECTOR MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513001692003051300169NM 2003 5 13 2003UALA00377 120030414A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29363UA 24532 CABIN STATION 942 FLOORBEAM CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM CAP. 2L72 4F4 FRTA16WE E2GL 20030513002772003051300277EU 2003 5 13 A6WA200360013 120030415A2751 WARNING LIGHT BAC 146 146200A 1500266EU TE FLAPS ILLUMINATED A A6WAO OTHER F FLT CONT AFFECTED LDLANDING 1 GL31291UE E2084 FLAP FAULT LIGHT ILLUMINATED. ZERO FLAP LANDING. 74K LBS, TOUCHDOWN SPEED 170 KNOTS, MODERATE BRAKING, BRAKES APPLIED 80 KNOWTS, BRAKE TEMP MAX 470 DEGREES, BRAKE FANS ON. RESET FLAP SYSTEM, PERFORMED F/C AND SAFETY LANE 2 TEST. COULD NOT DUPLICATE. OK FOR SERVICE PER AMM 27-50-00. NO FURTHER INSPECTIONS REQUIRED PER MOM 14-40-13, TR 108. (M) 2H74 4F A49EU 20030513002852003051300285NM 2003 5 13 USAASB03036 120030305A2780189929 SENSOR BOEING737 7374B7 1384702NM NR 3 L/E SLAT MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19777AU 24979 DURING CLIMB-OUT, WHEN FLAPS WERE RETRACTED TO THE FULL UP POSITION, THE LEADING FLAPS TRANSIT LIGHT AND THE NR 3 SLAT FULL EXTEND LIGHT REMAINED ILLUMINATED. NO ADVERSE CONTROL PROBLEMS WERE REPORTED BUT THE CAPTAIN ELECTED TO RETURNT TO FIELD AT CLT FROM MAINTENANCE TO CHECK THE PROBLEM. FLIGHT LANDED AT CLT WITHOT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND HIGH RESISTANCE ACROSS THE NR 3 SLAT FULL EXTEND SENSOR S166, LEG W252-223-20R. REMOVED AND REPLACED S166 FULL EXTEND SENSOR PER MM 27-88-11. ALSO, REPLACED INTERMITTENT NR 3 SLAT ROD END WIRING W252-052-20 AND W252-127-20 ALONG TELESCOPING TUBE. ACCOMPLISHED SATISFACTORY OPERATIONAL TEST OF LEADING EDGE DEVICE INDICATION PER MM 2L72 4F RTA16WE 20030513003062003051300306EA 2003 5 13 ASOA03168 120030418A5346 SUPPORT CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOEWR WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20030513003072003051300307EA 2003 5 13 ASOA03172 120030420A5260 HINGE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE STEP CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP HINGE BETWEEN FS 310 AND FS 349 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR TOP STEP HINGE BETWEEN FS 310.00 AND FS 349 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030514000212003051400021EA 2003 5 14 A6WA200340058 120030410A7830 BLOCKER DOOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 RT ENGINE THRUST REVERSER BLOCKER DOOR NR 2 IS CRACKED AT DOOR HINGE MOUNTING POINT. REMOVED AND INSTALLED NEW SERVICEABLE DOOR IAW CRJ AMM 78-33-21-400-801. 9M) 2L72 4F RTA21EA 20030514000272003051400027EA 2003 5 14 ASOA03146 120030402A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING AN 'A' CHECK IN MCN, FRAME FS 640 BETWEEN STRINGERS 13R AND 14R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING FRAME FS 640 BETWEEN STRINGERS 13R AND 14R IAW ASA EO 600-53-0088. (M) 2L72 4F RTA21EA 20030514000322003051400032WP 2003 5 14 AALA20030371 120030326A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21591AA 53254 DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY EXIT LIGHTS AFT OF ROW 22 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT LEFT OVERWATER SIDE MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030514000372003051400037SO 2003 5 14 RAIA00304113 120030415A3297 WIRE EMB 145 EMB145 3260210SO WOW SWITCH DETERIORATED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03801HK 145053 5284-RIC- LANDING GEAR AIR/GRN FAIL MESSAGE. MAINTENANCE REPAIRED BAD WIRE ON NR 2 WOW CONNECTOR RIGHT GEAR. OPS CHECK GOOD. 2L72 4F RTT00011AT 20030514000452003051400045EA 2003 5 14 COMA0360233 120030508A783022850200140 TORQUE BOX CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01959CA18263 7116 RIGHT HAND THRUST REVERSER TORQUE BOX WAS FOUND CRACKED AT 6:30 O'CLOCK POSITION. REMOVED AND INSTALLED SERVICEABLE TORQUE BOX. 2L72 4F RTA21EA 20030514000462003051400046EA 2003 5 14 COMA0360234 120030510A32347179015 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01973CA16318 7146 FLIGHT 5300 LANDING GEAR DISAGREE WARNING, NLG INDICATED UNSAFE. REPLACED THE LANDING GEAR CONTROL HANDLE. 2L72 4F RTA21EA 20030514000632003051400063NM 2003 5 14 SWAA030962 120030429A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20030514000832003051400083NM 2003 5 14 SWAA030984 120030501A57536546435333 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030514000942003051400094NM 2003 5 14 SWAA030995 120030502A53126545819121 PRESSURE PANEL BOEING737 7373H4 1384600NM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SPECIAL VISIT, FOUND UPPER NLG W/W SKIN CRACKED AT AFT OUTBOARD LT CORNER OF NOSE TIRE BRAKE PAD. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030513000562003051300056EA 2003 5 13 ASOA03126 120030323A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM INOPERATIVE A ASOAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO11870AS 7530 FLT 4785 - DURNG CRUISE, THE CREW RECEIVED A RIGHT HYDRAULIC HIGH TEMPERATURE CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE RT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE DRIVEN PUMP, RT HYDRAULIC MANIFOLD FILTER, RETURN FILTER, BOTH CASE DRAIN FILTERS, AND THE HYDRAULIC RESERVOIR FLUID. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030513001222003051300122CE 2003 5 13 DXTA200300030 120030507A7830 WARNING LIGHT CESSNA560 560XL 2076702CE PWA 545 PW545A NE THRUST REVERSER ILLUMINATED E DXTAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL07665QS 5605165 RIGHT "T/R ARM LIGHT" , "HYD PRESS" & "MASTER WARNING" LIGHT ILLUMINATED WHILE CRUSING LEVEL AT FL330, MACH 7.0. ENGAGED EMERGENCY STOW SWITCH AND DECLAIRED AN EMERGENCY WHILE SLOWING TO 200 KTS INDICATED. NOTICED NO UNSUAL AIRCRAFT MOVEMENT OR ANY DAMAGE. MADE AN EMERGENCY LANDING AT TEB WITHOUT INCIDENT. ITEM IS UNDER INVESTIGATION. FOUND T/R STOW SWITCH SE006 AND T/R DEPLOY SWITCH SE004 LOOSE. PERFORMED T/R DEPLOY AND STOW SWITCH ADJUSTMENT. SAFETIED SWITCHES AS REQUIRED. PERFORMED T/R LUBRICATION PROCEDURE. AND PERFORMED THRUST REVERSER SYSTEM FUNCTIONAL TEST. 2L72 4F4 FRTA22CE E00059EN 20030513001242003051300124NM 2003 5 13 UPS03240681 120030416A5753 FLAP TRACK BOEING727 727185C 138406NNM WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C&SI, NR 7 FLAP TRACK - LIGHT SURFACE CORROSION IN HORIZ. HOLES I & J. NR 2 FLAP TRACK INSTALLED IN NR 7 FLAP TRACK POS. IAW MM 27-51-31 2L73 4F A3WE 20030513001422003051300142NM 2003 5 13 CH1A200395039 120030414A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON CABIN FLOOR SUPPORT AT LBL 12 BS 1030 TO 1050 2L73 4F A3WE 20030513001522003051300152NM 2003 5 13 QXEA0300455 120030403A5210 HINGE BOMBDRDHC8 DHC8401 1390041NM PAX DOOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 AFT PASSENGER DOOR MAIN HINGE IS CHAFED ON LOWER OUTBOARD HINGE. REPAIRED IAW HORIZON AIR EA 6-52-263. 2H72 4T RTA13NM 20030513001992003051300199EA 2003 5 13 QXEA0300475 120030405A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 BULKHEAD WEB STRUCTURE AT FS 1098.20 RIGHT HAND, EVIDENCE OF CRACK WITH NDT AROUND FITTINGS. REPAIRED IAW DRJ700 NDTM 51-20-06 AND BOMBARDIER AEROSPACE REO 670-53-61-034 2L72 4F RTA21EA 20030509001562003050900156SO 2003 5 9 SIMA200309614 120030403A5313 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED BELOW SRM LIMITS BETWEEN FRAME 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED A NDT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A REPAIR ANGLE, SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M) 2L72 4T RTT00011AT 20030513000372003051300037NM 2003 5 13 03FDEA00708 120030507A5754 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE FOUND CORRODED. LOWER ATTACHING PIVOT O/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68412 WINGS- LT O/B FLAP- O/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030513000692003051300069NM 2003 5 13 CALA0300241 120030512A5312 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD CORRODED JUST AFT OF FS 1016 AT LBL 6 TO RBL 6. REPAIRED APB IAW DRAWING 65C28106-1. 2L72 4F RTA16WE 20030513000982003051300098NM 2003 5 13 AWXA200300501 120030429A53226545409602 ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1" CRACK WAS FOUND ON VERTICAL ATTACH ANGLE BELOW CABIN FLOOR SEAT TRACK AT LBL 24.75, BS 663.75. MAINTENANCE CUTOUT DAMAGED SECTION OF CHORD AT LBL 24.75, BS 663.75; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SECTION OF CHORD AND SPLICE REPAIR ANGLES; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5312-03120-KB2. 2L72 4F RTA16WE 20030513001022003051300102EU 2003 5 13 AWXA200300505 120030427A5210D5211021420300 FITTING AIRBUS320 A320231 3930325EU R1 DOOR BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - EES - DURING C-03 CHECK THE R-1 DOOR REDUCER SHAFT MECHANISM RIG PIN FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR REDUCER SHAFT MECHANISM RIG PIN FITTING PER AIRBUS INDUSTRIES CMM 52-11-15, PG. 319, 745, FIG. 308. 2L72 4F RTA28NM 20030513001052003051300105 2003 5 13 249TR0018 420030426A2210 CIRCUIT BREAKER BOEING737 7372K5 138448XNM AUTOPILOT TRIPPED A PIDAO OTHER O OTHER CRCRUISE 1 SO05249TR 22598 NO AUTO PILOT TRIM. FOUND AUTO PILOT TRIM CIRCUIT BREAKER POPPED. RESET BREAKER. OPS CHECKED OK PER MM 22-11-01. 2L72 4F RTA16WE 20030513001302003051300130NM 2003 5 13 CALA0300233 120030503A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912318 23369 RIGHT PRESSURE DECK IN WHEEL WELL CRACKED (1.5 INCH). REPAIRED PRESSURE DECK PER SRM 53-60-51. 2L72 4F RTA16WE 20030513001792003051300179SO 2003 5 13 C2XA03BT054 120030420A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715555 145594 DURING SEVICE/ROUTINE CHECK FOUND PSU EMERGENCY LIGHT OUT AT 12A. REMOVED AND REPLACED EMERGENCY LIGHT AT 12A IAW EMB MM 33-50-07. OPS CHECK GOOD. 2L72 4T RTT00011AT 20030513001862003051300186SO 2003 5 13 SWIA200311895 120030403A275012064207615 SWITCH EMB 120 EMB120RT 3260202SO FLAP SELECTOR MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07593SW1817 1817 120191 WITH FLAPS SELSECTED TO 15 DEGREES FLAP CONTROL FAULT. REMOVED AND REPLACED FLAP SELECTOR HANDLE WITH SERVICEABLE UNIT. RAN FLAPS FULL SCALE MULTIPLE TIMES. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030513002572003051300257EU 2003 5 13 ASOA03180 120030423A2750350A503000100 COMPUTER AEROSPATR72 ATR72212 8680945EU COCKPIT INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11636AS1631 375 FLT 4331 - DURING APPROACH INTO GPT FROM ATL, THE CREW RECEIVED A FLAP UNLOCK MESSAGE WITH THE FLAPS SELECTED AT THIRTY DEGREES. A GO AROUND WAS INITIATED WITH THE FLAPS RETRACTED TO FIFTEEN DEGREES AND THE MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT MAD A ZERO DEGREE SAFE LANDING IN GPT. MAINTENANCE REMOVED AND REPLACED THE MULTIFUNCTION COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030513002862003051300286WP 2003 5 13 AALA20030215 120030205A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21574AA 53151 TUL - FOUND CORROSION ON CUSP WEB ABOVE MID CARGO DOOR CUTOUT STA 636-641. CUT OUT CORRODED CUSP AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. (M) 2L72 4F A6WE 20030513003022003051300302EU 2003 5 13 ASOA03164 120030416A3320EO38711 LAMP AEROSPATR72 ATR72 EU CABIN BURNED OUT A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11640AS 405 DURING FINAL APPROACH INTO VPS FROM ATL, THE FLIGHT ATTENDANT NOTICED SMOKE AND A SMOKE ODOR IN THE AFT CABIN AREA. THE AIRCRAFT LANDED SAFELY IN VPS. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD LAMP ABOVE SEAT 16 C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030514000032003051400003EA 2003 5 14 ASOA03184 120030426A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11901EV 7616 FLT 4694 - DURING A GROUND INSPECTION IN DFW, THE AFT SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-CONNECTED THE AFT SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514000142003051400014WP 2003 5 14 AALA20030359 120030321A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21572AA 49458 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 14D INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030514000412003051400041NM 2003 5 14 ABXA030139 120030430A2760252T14013 ACTUATOR BOEING767 767231 1385131NM SPOILER DEFECTIVE A ABXAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL23708AX 22571 SPOILERS LIGHT ILLUMINATED EICAS MESSAGE SPOILERS DISPLAYED WITH SPOILERS SELECTED DOWN. THIS HAPPENED IMMEDIATELY AFTER TAKEOFF. AT FL 350, CONTROL WHEEL DISPLAYED AN UNCOMMANDED 45 DEGREES WITH AUTOPILOT ENGAGED. AUTOPILOT WAS DISCONNECTED AND THE UNCOMMANDED CONTROL DISPLACEMENT REMAINED AT FLIGHT LEVEL 240. ALL CONTROL INPUTS APPEARED NORMAL. FOUND CONNECTOR D161 SLIGHTLY BURNED. REMOVED AND REPLACED CONNECTOR D161 AND THREE SOCKETS IAW B767 WDM 27-61-13. REMOVED AND REPLACED SPOILER ACTUATOR NR 12 IAW B767 MM 27-61-02-4. 2L72 4F RTA1NM 20030514000512003051400051 2003 5 14 SWAA030974 420030430A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29071SW 22358 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030513002242003051300224CE 2003 5 13 DXTA200300013 120030422A3260 WARNING LIGHT CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07305QS 5600261 DURING APPROACH AT IAH, LT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. PERFORMED ABNORMAL CHECK LIST AND BLEW GEAR DOWN, STILL DID NOT HAVE INDICATION. AIRCRAFT LANDED SAFELY AT IAH. 2L72 4F RTA22CE 20030513002342003051300234CE 2003 5 13 DXTA200300012 120030420A3241 BRAKE CESSNA500 560CESSNA 2076750CE ANTI SKID SYS MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07313QS 5600325 DURING TAXI OUT FOR DEPARTURE CO-PILOT FELT THE BRAKES MOMENTARILY DISENGAGED. PILOT TOOK CONTROL AND HAD SAME EXPERIENCE. AIRCRAFT RETURNED TO BLOCK. PERFORMED ANTI-SKID SYSTEM CHECK ON GROUND AND SYSTEM PERFORMED NORMALLY. 2L72 4F RTA22CE 20030513002402003051300240SO 2003 5 13 ASOA03179 120030423A335012021299001 LIGHT EMB 120 EMB120ER 3260203SO RT OVERWING INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11268AS 120202 FLT 4132 - DURING A GROUND INSPECTION IN DFW, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030513002562003051300256EA 2003 5 13 ASOA03161 120030414A3230521153 ARM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DISCONNECTED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11717EV 10088 FLT 4192 - DURING CLIMB-OUT FROM SAT-DFW, THE CREW RECEIVED A PROXIMITY SENSOR FAULT ONE STATUS MESSAGE ON THE ENGINE INDICATION AND CREW ALERT SYSTEM. SHORTLY AFTERWARDS A WEIGHT ON WHEELS CAUTION MESSAGE APPEARED ON THE ENGINE INDICATION AND CREW ALERT SYSTEM. THE NOSE GEAR WOULD NOT RETRACT AND REMAINED IN THE DOWN POSITION FOR THE DURATION OF THE FLIGHT. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT LANDING SAFELY IN DFW. MAINTENANCE FOUND THE NOSE LANDING GEAR TORQUE LINKS DISCONNECTED AND RECONNECTED THEM. MAINTENANCE ALSO REMOVED AND REPLACED THE NOSE GEAR WHEEL AND TIRE ASSEMBLIES AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECKS AND VISUAL INSPECTIONS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030513002632003051300263NM 2003 5 13 GAIA03013OP 120030312A33501000677 LIGHT BOEING727 727223 1384074NM COCKPIT LOOSE A GAIAO OTHER O OTHER NRNOT REPORTED 1 SW076833 20186 FLT 743 - MEM-TOL - COCKPIT EMERGENCY EXIT LIGHT CAME ON AND WOULD NOT TURN OFF. FOUND COCKPIT EMERGENCY EXIT LIGHT NOT FULLY SECURED IN BASE. REINSTALLED THE EMERGENCY EXIT LIGHT. OPS CHECK GOOD. (M) 2L73 4F A3WE 20030514001292003051400129NM 2003 5 14 SWAA031015 120030507A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 8L, BS 380 & BS 400. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030514001442003051400144NM 2003 5 14 SWAA031044 120030509A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 930 AT STR 24L, BS 520 AT STR 15R & BS 930 AT STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030514001482003051400148NM 2003 5 14 SWAA031048 120030510A2560 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 LEFT FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED LT FWD EMERGENCY FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20030514001492003051400149 2003 5 14 SWAA031049 420030509A256565C19901 CABLE BOEING737 7373H4 1384600NM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030514001632003051400163NM 2003 5 14 P5CA0300870 120030412A533081103 SKIN BOEING747 747249F 1384849NM FUSELAGE PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FUSELAGE SKIN PUNCTURE BS 2598 BETWEEN 525R / 526R. JACKING INCIDENT DURING C-CHECK AT SIN. 2L74 4F A20WE 20030514001692003051400169NM 2003 5 14 P5CA0300862 120030412A573081103 SKIN BOEING747 747249F 1384849NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEVEL 1 CORROSION STA 1240 LBL 950 APPROX 3.0 X .5. REPAIR PER SRM 57-30-01 REWORK PER 8110-3 PAO-SIN-03-00017F, PAO - SIN - 0700013H. 2L74 4F A20WE 20030514001712003051400171NM 2003 5 14 P5CA0300866 120030325A5330 SKIN BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 SKIN BS 1480 CRACKED NR 9, 11 L/E, NR 11 R/S. REPAIRED PER SB 747 53A 2390 R1 CONTINUE REINSPECTION 1600 FLT CYCLES COI 920. 2L74 4F A20WE 20030514001832003051400183NM 2003 5 14 03FDEA00681 120030505A5310 STRUCTURE DOUG MD11 MD11 3023602NM CARGO FLOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 DURING REMOVAL OF CARGO HANDLING TRAY CORROSION OBSERVED ON FLOOR STRUCTURE AT STA 1961 LBL 58 IN CABIN. 2L73 4F RTA22WE 20030514001842003051400184EU 2003 5 14 03FDEA00680 120030505A7830491B1220000019 DOOR GE CF680C2 AIRBUS300 A300F4605R 3930327EU NR 1 ENG T/R GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25682FE R634034 800 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR. COMPLIED WITH EA 8-7832-68795 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR AT MAE. 2L72 4F RTA35EU 20030514001932003051400193NM 2003 5 14 03FDEA00703 120030507A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING - O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE FOUND CORRODED. RT WING- O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-69232 WINGS- TRAILING EDGE & TRAILING EDGE DEVICES- RH OUTBD FLAP OUTBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030514001952003051400195NM 2003 5 14 03FDEA00701 120030507A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING - O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT, I/B LUG I/B FACE CORRODED. RT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT, I/B LUG I/B FACE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68415 WINGS- RIGHT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030514001972003051400197NM 2003 5 14 03FDEA00699 120030507A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING - O/B FLAP I/B HINGE (FLAP SIDE), LWR PIVOT O/B LUG HOLE CORRODED. RT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT O/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68415 WINGS- RIGHT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030514001982003051400198WP 2003 5 14 03FDEA00697 120030508A5320 COVER DOUG DC10 DC1010 3022110WP COCKPIT WINDOW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 CAPT'S SLIDING WINDOW LWR TRACK, FWD ATTACH COVER CRACKED. REMOVED PANEL IAW SRM 51-31-01. FAB NEW PANEL IAW DWG ABN7039. FROM 6061- 0.0.032. INSTALLED NEW PANEL IAW SRM 51-31-01. 2L73 4F A22WE 20030514002002003051400200WP 2003 5 14 03FDEA00695 120030508A5312 DOUBLER DOUG DC10 DC1010 3022110WP BULKHEAD CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 IN CENTER ACCESSORY COMPT STA 1156, BULKHEAD BETWEEN LONGERONS L50-49, LT LOWER CORNER OF BATTERY HAS CORROSION AT DOUBLER. REMOVED DOUBLER IAW SRM 51-31-01. FAB NEW DOUBLER ON TRAVELER 2/330509. INSTALLED NEW DOUBLER IAW SRM 51-33-01. PAINTED AREA IAW SRM 51-21-01. 2L73 4F A22WE 20030514002062003051400206WP 2003 5 14 03FDEA00698 120030508A3620350082 WARNING LIGHT DOUG DC10 DC1010 3022110WP PNEUMATIC SYSTEMILLUMINATED A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25358FE 46633 AIR SYS 2 OFF ALERT ILLUMINATED AND WITHIN SECONDS, THE AIR MANF 2 FAIL ALERT ILLUMINATED. RETURNED TO MEMPHIS. NO OTHER SECONDARY INDICATIONS. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02 CATEGORY: C EXPIRATION: 18MAY03 MEL 36-23-01-02: NR 2 MANIFOLD FAIL DETECTION LOOP INOP. MX MUST CLEAR ALERT PRIOR TO EACH DISPATCH. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START. CATEGORY -C- EXPIRATION DATE 18 MAY 03. *S/D* REPLACED MANIFOLD FAILURE CTRL, ALL LOOPS CHECK GOOD WITH TESTER AMM 36-23-01. 2L73 4F A22WE 20030514002102003051400210NM 2003 5 14 03FDEA00686 120030506A5320 WEB BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 WHILE WORKING FED EX NRC N00312, FOUND CORROSION ON WEB AT LBL 10, BS 1146-1166, WL 146. REMOVED CORRODED WEB AND REPAIRED PER SRM 51-30-5, 51-30-2. 2L73 4F RTA3WE 20030514002112003051400211NM 2003 5 14 03FDEA00685 120030506A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CORROSION (C53-113-01) ON STR 29L KEEL BEAM O/B FLANGE FROM STA 950D TO 950E. REMOVED CORROSION ON STR 19L KEEL BEAM O/B FLANGE FROM BS 950D TO 950E FOUND TO BE OUT OF LIMITS IAW SRM 51-10-3. INSTALLED REPAIR STRAP ON STR 29L KEEL BEAM IAW FED EX DRAWING SR 27-53-023A. 2L73 4F RTA3WE 20030514002132003051400213NM 2003 5 14 03FDEA00561 120030421A5310 STRUCTURE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION AROUND FASTENER HOLES, BS 740-759, LBL 6-RBL 6, WL 138. REPAIRED PER SRM 53-10-1, 53-10-2, AND 51-40-2. 2L73 4F RTA3WE 20030514002142003051400214NM 2003 5 14 03FDEA00562 120030421A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-224-01, 3) ON BS 1176 FRAME, WL 208, LBL 60 TO SKIN. REPAIRED PER 51-30-2, 51-30-5 AND 65C33557, FEDEX MM 36-00-01. 2L73 4F RTA3WE 20030515000112003051500011EA 2003 5 15 SWIA200311934 120030430A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A SWIAO OTHER N FALSE WARNING LDLANDING 1 NM07906SW 7510 FLAPS FAIL CAUTION MESSAGE ON LANDING. FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU PER FIM 27-50. ALL LRU'S PASSED ALL TESTS. OPS CHECK GOOD ON GROUND. OPERATED FLAPS SEVERAL TIMES ON GROUND. NO PROBLEMS NOTED. 2L72 4F RTA21EA 20030513001472003051300147NM 2003 5 13 CH1A200395045 120030417A5313 STRINGER BOEING727 727290 138408WNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 7 CRACKS ON STR 26L LOWER ROW OF FASTENERS FROM BS 560 TO BS 580 2L73 4F A3WE 20030513002482003051300248EA 2003 5 13 ASOA03154 120030410A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP UPPER HINGE NUT PLATE ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR TOP STEP UPPER HING NUT PLATE ANGLE IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030513002582003051300258EA 2003 5 13 ASOA03159 120030411A5315601R53037K1A FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOORBEAMS AT BL 27 IN THE SERVICE DOOR AREA WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT FLOORBEAMS (P/N'S 601R53-037K1A AND 601R53-037K4A) AT BL 27 IN THE SERVICE DOOR AREA, IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20030513003002003051300300EA 2003 5 13 ASOA03162 120030415A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 FLT 4437 - DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY FLOOR LIGHTING STRIP WAS FOUND TO HAVE A LOOSE CONNECTION. MAINTENANCE REMOVED AND REPLACED THE FORWARD FIRST SECTION EMERGENCY FLOOR LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514000192003051400019EA 2003 5 14 ASOA03150 120030408A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11830AS 7236 DURING TAKEOFF AND LANDING FROM DFW-RDU, THE RIGHT PACK BECAME UNCONTROLLABLE IN AUTOMATIC OR MANUAL MODES AND SHOWED 17 PSI IN THE RIGHT TENTH STAGE ONLY. A BURNING ODOR ALSO OCCURRED IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN RDU. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514000222003051400022EA 2003 5 14 ASOA03151 120030409A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING A C-CHECK IN MCN, THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20030514000602003051400060 2003 5 14 SWAA030959 420030429A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD ENTRY AND FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030514000712003051400071NM 2003 5 14 SWAA030970 120030429A33506556633 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD CEILING EMERGENCY EXIT LIGHT LOOSE AT OVERWING EXITS. SECURED CEILING EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030514000782003051400078NM 2003 5 14 SWAA030944 120030424A53116546529 FRAME BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, BETWEEN STR 27L & STR 28L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030514000882003051400088 2003 5 14 SWAA030989 420030504A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2L72 4F RTA16WE 20030514000922003051400092NM 2003 5 14 SWAA030993 120030502A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030513000342003051300034NM 2003 5 13 03FDEA00711 120030507A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG I/B FACE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG I/B FACE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030513001132003051300113NM 2003 5 13 QXEA0300502 120030421A5510 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZONTAL STAB LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 SHIM AT FORWARD RT HORIZONTAL STAB ATTACH FITTING IS MIGRATING. REPAIRED IAW DHC-8 400 AMM TEMPORARY REVISION 55-10-00, PAGES 1-3. 2H72 4T RTA13NM 20030513001362003051300136WP 2003 5 13 NACA20030081 120030415A792131534 ACTUATOR DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 3 ENGINE INOPERATIVE A NACAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 AL03779TA3264 3264 45529 P34011 NR 3 ENGINE SHUT DOWN DUE TO OIL COOLER DOOR NOT OPERATING. REPLACED OIL COOLER DOOR ACTUATOR. 2L74 4R4 R 6A3 5E8 20030513001442003051300144NM 2003 5 13 CH1A200395041 120030414A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOOR SUPPORT AT RBL 12 BETWEEN BS400-BS420 HAS CORROSION 2L73 4F A3WE 20030513001882003051300188SO 2003 5 13 SWIA200311897 120030420A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP LEAKING A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM07236SW8155 8155 120312 UPON DEPLOYING FLAPS 15 DEGREES, FLAPS DISAGREEMENT LIGHT CAME ON, FOLLOWED BY LOW LEVEL LIGHT FOR RT/BLUE HYDRAULIC PUMP, LOW PRESS, MAIN PUMP LOW PRESS AND ELECTRIC PUMP LIGHT. UPON POSTFLIGHT, FOUND SIGNIFICANT FLUID LEAK. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-00. REPLACED RT ENGINE DRIVEN PUMP AND ALL FOUR FILTERS IAW EMB120 MM 29-10-00. OPS AND LEAK CHECK GOOD. 2L72 4T RTA31SO 20030513001912003051300191NM 2003 5 13 QXEA0300472 120030413A5260 SEAL BOMBDRDHC8 DHC8401 1390041NM PAX DOOR LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09409QX 4051 AFT PASSENGER DOOR IS STIFF AND DIFFICULT TO OPEN. CLEANED AND LUBED DOOR SEAL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513002212003051300221WP 2003 5 13 ZW0A0304501 120030420A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN WORN A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13972TW 53622 EMERGENCY FLOOR LITE ESCAPE PATH AT 5E INOP DUE TO WEAR. RE-INSERTED LOOSE LAMP AT 5E. EMERGENCY LITE CHECK OK. CHECK-C 7-18-02 MCI. --CLOSED-- 2L72 4F RTA6WE 20030514000022003051400002EA 2003 5 14 ASOA03170 120030420A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE LT AND RT 9 AND 27 FLOORBEAMS BETWEEN FS 280 AND FS 379 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT 9 AND 27 FLOORBEAMS BETWEEN FS 280 AND FS 379 IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20030514000362003051400036EU 2003 5 14 RAIA00304112 120030410A2797 WIRE AEROSPATR72 ATR72202 8680940EU RUDDER TRIM DISCONNECTED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03722TE 220 5540-STL- RUDDER TRIM CD POPPED. MAINTENANCE REPLACED WIRE VAD 5055VC, OPS CHECK GOOD. 2H72 4T RTA53EU 20030514000762003051400076NM 2003 5 14 SWAA030942 120030427A57536546435277 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED ON LOWER SKIN. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030514001032003051400103 2003 5 14 SWAA031004 420030504A2565D31354 SLIDE BOEING737 7372H4 138448CNM PAX DOOR DISLODGED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29095SW 23054 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F A16WE 20030514001092003051400109NM 2003 5 14 SWAA031010 120030506A53116546543 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STRINGER 9R, BS 440 & BS 867. REPAIRED FUSELAGE FRAMES PER BFG ER. 2L72 4F RTA16WE 20030514001192003051400119NM 2003 5 14 SWAA031030 120030508A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED, BS 360, STRINGER 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030514001232003051400123NM 2003 5 14 SWAA031034 120030508A575565C25256 FITTING BOEING737 7373H4 1384600NM SPOILER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED PM CHECK, FOUND RT WING INBOARD GROUND SPOILER ACTUATOR OUTBOARD ATTACH FITTING BROKEN. REMOVED AND REPLACED SPOILER ASSY PER MM. 2L72 4F RTA16WE 20030514001242003051400124NM 2003 5 14 SWAA031035 120030508A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED PM CHECK, FOUND 2.5 INCH LONG CRACK, BS 727D, STRINGER 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030514001332003051400133NM 2003 5 14 SWAA031019 120030507A552065C25798 HINGE FITTING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE FITTING PER MM. 2L72 4F RTA16WE 20030514001462003051400146NM 2003 5 14 SWAA031046 120030508A3350PH22300L TRACK BOEING737 7375H4 138449DNM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS PHOTOLUMINESCENT SECTIONS CRACKED BETWEEN ROW 10 DEF & ROW 19 DEF. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20030514001472003051400147NM 2003 5 14 SWAA031047 120030508A3350AD20131A BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29718SW 27852 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACKS FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20030514001502003051400150NM 2003 5 14 SWAA031050 120030510A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 873 & BS 876, STR 22R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030514001602003051400160 2003 5 14 RAIA00304117 420030417A3417700070095 ADC AEROSPATR72 ATR72202 8680940EU NR 2 FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03722TE3843 1581 220 5590-STL- ADC NR 2 FAIL. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA COMPUTER, OPS CHECK GOOD. 2H72 4T RTA53EU 20030514001622003051400162SO 2003 5 14 RAIA00304119 120030421A323023092900001 UPLOCK EMB 145 EMB145LR 3260212SO NLG FAILED A RAIAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 CE03813HK8626 3251 145044 5710-STL- NOSE LANDING GEAR DOES NOT INDICATE UP AND LOCKED AFTER RETRACTION. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK ASSEMBLY, OPS CHECK GOOD. 2L72 4T RTT00011AT 20030514001762003051400176EU 2003 5 14 03FDEA00678 120030504A5280A531057600101 HINGE AIRBUS310 A310 EU NLG DOOR CRACKED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25429FE 364 ON GEAR RETRACTION AFTER T/O NOSE GEAR DOOR AMBER LIGHT ON, WITH VIBRATION IN THE AREA BEHIND COCKPIT DOOR. WHEN GEAR EXTENDED FOR LANDING THE NOSE GEAR WAS ON. DID MANUAL GEAR EXTENSION. ALL GEAR GREEN LIGHTS ON. REMOVED AND REPLACED R/H NOSE GEAR DOOR ACTUATOR FITTING, DOOR ACTUATOR & DOOR SEQUENCE VALVE. REF EA. 6-5300-71217. A310 MM 32-31-18 & 32-31-16, DOOR RIG AND OPS CHECK NORMAL. PERFORMED GEAR RETRACTION TEST REF 32-31-00-5 OPS CHECK NORMAL. 2L72 4F RTA35EU 20030514001772003051400177NM 2003 5 14 03FDEA00665 120030501A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 WHILE WORKING FUSELAGE 5081, N00285, FOUND SHEAR TIE TO BE CORRODED OUT OF LIMITS BS 620, WL 138, LBL 3. 2L73 4F RTA3WE 20030514002162003051400216NM 2003 5 14 03FDEA00714 120030430A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING: OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO FLAP LOWER FWD HOLE (4 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP. 2L73 4F RTA22WE 20030514002172003051400217NM 2003 5 14 03FDEA00718 120030430A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE FLAP SIDE AFT HOLES LOCATION QTY 2 EA WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69244 WINGS- TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD FLAP HINGE BRACKET - STRUT REPAIR. 2L73 4F RTA22WE 20030514002192003051400219NM 2003 5 14 03FDEA00721 120030428A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING: O/B FLAP O/B HINGE (WING SIDE) LWR ATTACHMENT TO WING REAR SPAR FOUND WITH HOLE (2 EACH) CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030514002342003051400234GL 2003 5 14 AC2A086269 220030421A72006854424 SHAFT SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL NR 2 ENGINE LEAKING E AC2AO OTHER K FLUID LOSS ININSP/MAINT 1 SO077266K 760283 890392 PART IS LEAKING OIL. OIL SEAL HAD BECOME DISPLACED FROM FUEL PUMP DRIVE SEAL BORE IN ENGINE GEARBOX. OIL WAS COMING OUT OF THE FUEL PUMP CASE DRAIN, THROUGH THE DRAIN HOSE AND OUT OF THE DRAIN CLUSTER ON THE BELLY OF THE AIRCRAFT. FUEL PUMP WAS REMOVED, THE DRIVE SEAL WAS REPLACED WITH NEW SEAL AND THE FUEL PUMP WAS REINSTALLED. 1G72 3U3 U H1NE E1GL 20030513001842003051300184 2003 5 13 SWIA200311893 420030402A22156225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER BINDING A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07220SW 120288 RUDDER PEDALS MAKE A LOUD GRINDING NOISE WHEN THEY ARE MOVED. REMOVED RUDDER TO INSPECT. FOUND SERVO TO MAKE GRINDING NOISE AND ALSO FOUND IT TO BE BINDING. REPLACED SERVO WITH SERVICEABLE UNIT. AUTOPILOT OP CHECKS GOOD. 2L72 4T RTA31SO 20030513002112003051300211SO 2003 5 13 C2XA03CL093 120030415A335066367 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2716520 145372 THE CREW REPORTED 2 EMERGENCY FLOOR LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REPLACED NR 3 INVERTER AND A AISLE PATH EMERGENCY LIGHT STRIP.OPERATIONAL CHECKS WERE GOOD.INVERTER P/N 7824-1 2L72 4F RTT00011AT 20030513002782003051300278NM 2003 5 13 WRLA200304 120030315A275096010211 TRANSMITTER DOUG MD11 MD11 3023602NM FLAP HANDLE FAILED A WRLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA27271WA 48518 AIRLERON DEFLECT DISAGREE IN FLIGHT. RETURNED TO DEPARTING STATION YOKOTA JAPAN. REPLACED FLAP HANDLE POSITION TRANSMITTER. (M) 2L73 4F RTA22WE 20030514000572003051400057NM 2003 5 14 SWAA030980 120030501A52306547952 SEAL BOEING737 7373H4 1384600NM CARGO DOOR LOOSE A SWAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29363SW 26574 DIVERSION, DECLARED EMERGENCY. UNABLE TO CONTROL CABIN PRESSURE. REINSTALLED AFT LOWER CORNER SEAL IN AFT CARGO DOOR AND REINSTALLED APU DUCT BOOT CLAMP IN KEEL BEAM PER MM. 2L72 4F RTA16WE 20030514001172003051400117NM 2003 5 14 SWAA031028 120030508A3350610478 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED A2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030514001892003051400189NM 2003 5 14 250TR0016 120030429A5311 FRAME BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CRACK IN FRAME AT BS 480 AT LEFT TRANSITION ANGLE (FORWARD CARGO BIN). REPAIRED PER SRM 51-40-3. 2L72 4F RTA16WE 20030514002242003051400224WP 2003 5 14 03FDEA00728 120030513A5753ANB74141 SUPPORT DOUG DC10 DC1010 3022110WP TE FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 LEFT INBOARD FLAP - INBOARD ACTUATOR LEVER ARM, SUPPORT STRUCTURE HAS DEEP WEAR/CHAFING AT PREVIOUS REPAIR. REQUEST ENGR EVALUATION. COMPLIED WITH EA-85750-67549 HINGE BRACKET SHIM INSTALL ALSO COMPLIED WITH EA- 8-5310-66485 WING- LT I/B T/E FLAP SUPPORT PANEL DAMAGE REPAIR. (REF. ITEM CHANGED PER ENGINEERING REQUEST FLAP CONTROL VALVE, RESTRICTROS, I/B & O/B ACTUATORS AND FLAP BUS CABLES. 2L73 4F A22WE 20030515000192003051500019SO 2003 5 15 SWIA200311940 120030503A3297 WIRE EMB 120 EMB120ER 3260203SO MLG CORRODED A SWIAO OTHER S AFFECT SYSTEMS CLCLIMB 1 NM07578SW 120346 FLIGHT IDLE UNLOCK LIGHTS, AUTO PRESSURIZATION AND TCAS IN STANDBY AFTER GEAR RETRACTION. INSPECTED AND FOUND CORROSION AT WIRE CONNECTOR J0318 AND EXPOSED WIRE SHIELD INBOARD OF WIRE CONNECTOR J0318. REPLACED CONNECTOR J0318 AND APPLIED PROTECTIVE COVER TO AFFECTED AREA OF WIRE I/B OF CONNECTOR J03318. PERFORMED GEAR CYCLE. OPS CHECK GOOD. 2L72 4T RTA31SO 20030515000212003051500021EA 2003 5 15 SWIA200311942 120030331A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 RIGHT AND LEFT ELECTRICAL BAY FLOOR PANELS AT FS 193 CRACKED. FOUND DURING C-CHECK INSPECTION. NDT HFEC CARRIED OUT IAW REO 601R-53-11-081. NO CRACKS NOTED. REPAIRED DAMAGED FLOOR IAW CRJ REO 601R-53-11-245 REV NC. 2L72 4F RTA21EA 20030515000312003051500031EA 2003 5 15 03124703 120030504A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 DURING MAINTENANCE INSPECTION, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515000372003051500037EA 2003 5 15 SWIA200311906 120030303A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 PILOTS BULKHEAD FS 280 RDL 9.0 FLOORBEAM CRACKED. FOUND DURING C-CHECK INSPECTION. HFEC INSPECTION COMPLIED WITH ON CUT OUT REPAIR AREA AS REQUIRED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-11-137 REV NC. 2L72 4F RTA21EA 20030515000482003051500048WP 2003 5 15 ZW0A0304701 120030507A3350408822101 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13953U 49267 THE EMERGENCY OVERHEAD LIGHTS FROM ROWS 23 THRU 27, AND THE EMERGENCY OVERHEAD LIGHTS JUST FWD OF AFT TAIL CONE EXIT DOOR, WERE INOPERATIVE. REPLACED THE BATTERIES IN POWER SUPPLY B5-106 FOR ROWS 23 THRU 27, AND REPLACED THE BATTERIES IN POWER SUPPLY B5-28 FOR AFT TAIL CONE EXIT DOOR LIGHTS. CHECK-C 2-18-03 STL. 2L72 4F A6WE 20030515000522003051500052CE 2003 5 15 GLBA2003060 120030512A2810 CAP BEECH 1900 1900D 1154162CE FUEL STORAGE LEAKING A GLBAO OTHER K FLUID LOSS CLCLIMB 1 NM03192GL UE192 LEFT O/B FUEL CAP LEAKS. REMOVED AND REPLACED FUEL CAP, OPS CHECK GOOD. 2L72 4T RTA24CE 20030514000492003051400049NM 2003 5 14 SWAA030972 120030501A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 EEPLS COVER CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030514000902003051400090NM 2003 5 14 SWAA030991 120030504A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 722B + 9 & BS 752, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030514001582003051400158SO 2003 5 14 RAIA00304115 120030415A32501170A180001 POTENTIOMETER EMB 145 EMB145LR 3260212SO NLG STEERING DEFECTIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03819HK4777 3956 145062 5710-STL- AIRCRAFT PULLS HARD RIGHT. MAINTENANCE REMOVED AND REPLACED STEERING FEEDBACK POTENTIOMETER, OPS CHECK GOOD. 2L72 4T RTT00011AT 20030514001882003051400188NM 2003 5 14 373PA0014 120030509A335086210066 BATTERY PACK BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 EMERGENCY LIGHT INOP ON SEAT 6D. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK PER MM 33-51-51. 2L72 4F RTA16WE 20030514002222003051400222NM 2003 5 14 03FDEA00638 120030423A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK AT RT X = 47.5 STA 1321 - 1361 CORRODED. CABIN - STA 1270 TO STA 1390 RT X=47.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00, VOL I, FIG 1. 2L73 4F RTA22WE 20030514002322003051400232EU 2003 5 14 NXT2003F00001 120030326A5302109037305105 RIB AGUSTAA109 A109E 0260119EU VERTICAL STAB CRACKED E O OTHER O OTHER NRNOT REPORTED 1 SW19143CF364 11142 A CRACK WAS FOUND IN THE INTERIOR OF THE LEFT SIDE OF THE VERTICAL FIN. THE CRACKS WERE LOCATED ON HORIZONTAL RIBS AT WL 235.2 AT STATION 9725.0 MM. LOWER CRACK IS APPROXIMATELY 4 INCHES LONG. SECOND CRACK IS APPROX. 1.25 INCH LONG. MFG WAS CONTACTED FOR SERVICEABILITY INSTRUCTIONS. A LETTER WAS INSSUED PERMITTING OPERATION FOR 100 HOURS PROVIDED DAILY AND 25 HOUR INSPECTIONS WERE COMPLIED WITH INSTRUCTIONS. 1G72 3U RTH7EU 20030514002392003051400239GL 2003 5 14 ALGA086239 220030422A724023008614 COMBUSTION LINER CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C* GL ENGINE CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 .020 INCH GAP BETWEEN AREA (A) AND AREA (B). CRACKS IN DEFLECTOR PLATE. 1Q71 3R3 U 2A6 E4CE 20030515000102003051500010EA 2003 5 15 SWIA200311933 120030502A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07413SW3300 3300 7102 EN ROUTE, STATUS MESSAGE OF FLT SPLRS FAULT AND IB GROUND SPLR FAULT UPON DEPLOYMENT. ON THE GROUND, RECEIVED A CAUTION MESSAGE OF GLD UNSAFE. ALL GLD'S DID DEPLOY ON LANDING. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD. 2L72 4F RTA21EA 20030515000172003051500017EA 2003 5 15 SWIA200311911 120030303A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 RIGHT LOWER WING PLANK WS 148.019 FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-13 IAW WS 148.019. NO CRACKS NOTED. DAMAGED AREA OF RIGHT LOWER WING PLANK REPAIRED IAW REO 601R-57-21-130 REV D AND REO 601R-57-21-131 REV NC. 2L72 4F4 FRTA21EA E15NE 20030515000262003051500026EA 2003 5 15 SWIA200311947 120030331A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FS 589.00 FLOORBEAM LEFT SIDE CRACKED BETWEEN LBL 42.5 AND 45.0. FOUND DURING C-CHECK INSPECTION. NDT-HFEC CARRIED OUT IAW NDTM PART 1 51-20-01. NO CRACKS NOTED. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-694 REV NC. CARGO DOOR CLEARANCES CHECKED IAW CRJ AMM 52-31-00-820-801. 2L72 4F RTA21EA 20030515000282003051500028SO 2003 5 15 SWIA200311913 120030423A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSBROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07224SW 120294 RED EMERGENCY LIGHTS ON FLOOR (BOTH) AT MAIN CABIN DOOR ARE INOP. REWIRED BROKEN WIRES ON FORWARD EMERGENCY RED LIGHTS ON THE FLOOR. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030515000512003051500051WP 2003 5 15 ZW0A0304704 120030508A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13982TW 53632 FOUND A DENT ON THE LEFT SIDE OF THE FUSELAGE BETWEEN LONGERON L18 AND L19, AT STA 237. REPAIRED DENT PER ARA 18325. CHECK-C 11-19-02 STL. 2L72 4F RTA6WE 20030515000532003051500053CE 2003 5 15 GLBA2003061 120030513A3150 CONNECTOR BEECH 1900 1900D 1154162CE MASTER CAUTION DAMAGED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03210UX UE210 MASTER CAUTION GOING OFF IN FLIGHT. REPAIRED LOOSE PIN ON CONNECTOR, OPS CHECK GOOD. 2L72 4T RTA24CE 20030515000542003051500054NM 2003 5 15 ZW0A0304802 120030512A3350767 BULB BOEING757 7572Q8 1384972NM EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13701TW 28160 THE EXTERNAL EMERGENCY LIGHT AT THE LEFT SIDE NUMBER 4 CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 5-27-02 MCI. 2L72 4F RTA2NM 20030515000562003051500056 2003 5 15 DXTA200300018 420030428A2210 MOTOR CESSNA560 560XL 2076702CE AUTOPILOT LACK OF LUBE E DXTAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL07610QS 5605210 CLIMBING THROUGH 35,000 FT YOKE JERKED ABRUPTLY, AUTOPILOT WAS DISCONNECTED AND AIRCRAFT NEED NOSE DOWN TRIM. FIFTEEN SECONDS LATER WITH AUTOPILOT OFF SECOND JERK OCCURRED IN YOKE. 2L72 4F RTA22CE 20030515000982003051500098NM 2003 5 15 03FDEA00621 120030426A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING FOUND OUTBOARD FLAP, OUTBOARD HINGE WING SIDE WITH PIVOT HOLE LOCATION WITH CORROSION. CORROSION ON RT WING, OUTBOARD FLAP, OUTBOARD HINGE WING SIDE, PIVOT HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-09, FIG.401. 2L73 4F RTA22WE 20030515001262003051500126NM 2003 5 15 AWXA200300535 120030415A5330654580027 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK HFEC INSPECTION INDICATED A .25 INCH CRACK AT FASTENER HOLE ON FUSELAGE SKIN FORWARD OF L-1 DOOR LOWER HINGE CUTOUT. MAINTENANCE TRIMMED OUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW ER 03-5300-03129-ES2. 2L72 4F RTA16WE 20030515001372003051500137NM 2003 5 15 AWXA200300481 120030422A53206520726 SILL BOEING737 73733A 1384673NM CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND SCREW HOLES ON FORWARD CARGO DOOR SCUFF PLATE BS 460. MAINTENANCE MECHANICALLY REMOVED CORROSION FROM FORWARD CARGO DOOR SCUFF PLATE (SILL WEB) BS 460, AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SILL WEB; FABRICATED A NEW REPLACEMENT SILL WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-30-01, PG 12. 2L72 4F RTA16WE 20030515001392003051500139NM 2003 5 15 AWXA200300483 120030429A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 210, RBL 6. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 210, RBL 6; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG 275-280, FIG 210. 2L72 4F RTA16WE 20030515001402003051500140NM 2003 5 15 AWXA200300484 120030429A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 213, LBL 11. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 213, LBL 11; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND 2 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG 265-272, FIG 209. 2L72 4F RTA16WE 20030527000382003052700038NM 2003 5 27 2003UALA00394 120030426A335064641 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DEFECTIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29301UA 23642 EMERGENCY EXIT LIGHTING (EEL) AFT OF ROW 16 WAS INOPERATIVE. *S/D* REPLACED 18 FT SECTION OF EEL CABLE. 2L72 4F4 FRTA16WE E2GL 20030527000572003052700057WP 2003 5 27 AALA20030260 120030302A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217541A 49995 ORD - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS FROM ROW 22-26 INOPERATIVE. SECURED CEILING EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000622003052700062EU 2003 5 27 AALA20030417 120030405A3350 LIGHT FOKKERF28 F28MK0100 4990807EU WING INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211403M 11354 DFW - DURING OVERNIGHT MAINTENANCE, LEFT WING EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT WING EXTERNAL EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030527000772003052700077WP 2003 5 27 AALA20030352 120030320A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21258AA 49288 STL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECTOR UNDER SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527001092003052700109EA 2003 5 27 2003F00319 120030228A275183141020000 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A MASAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW0777302 7302 FFCM AT 20 UNITS ON APPROACH, FLAPS 30 SELECTED. EMERGENCY DECLARED. SAFE LANDING. CONTRACT MAINTENANCE PERFORMED PART 'A'. THE AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE COMPLIED WITH PART 'B'. MAINTENANCE REPLACED THE BPSU. OP CHECKS GOOD. (M) 2L72 4F RTA21EA 20030528000512003052800051EU 2003 5 28 BAQA086414 120030514A6210L621M1010054 BLADE UROCOPEC135 EC135T1 5620026EU MAIN ROTOR DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01511ME2371 0143 SUSPECTED WATER IN BLADE. REPLACED WITH REPAIRED, SERVICEABLE UNIT. 1G72 3U H88EU 20030528000582003052800058EU 2003 5 28 HEEA086744 120030522A8000845UN01Q4AA5F SWITCH SNIAS 350 AS350B3 8680954EU ENGINE STARTER FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03973AE 3229 ENGINE WOULD NOT MOTOR OR START WHEN IDLE WAS SELECTED. TO BE SENT TO VENDOR. 1G71 3U H9EU 20030528000642003052800064EU 2003 5 28 BAQA086347 120030507A6200L673M20A1005 ACTUATOR UROCOPEC135 EC135T1 5620026EU MAIN ROTOR LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01118WS1589 0089 MAIN ROTOR ACTUATOR LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030528000782003052800078CE 2003 5 28 2003F00300 120030425A3244 TIRE CESSNA750 750 2076810CE MLG DEFLATED A UG8ACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL235115 7500018 DEPARTING DENVER THE NO TAKEOFF WARNING ANNUNCIATED AND THE TAKEOFF WAS ABORTED. THE RIGHT LANDING GEAR WHEELS, BOTH INBOARD AND OUTBOARD, DEFLATED AFTER TAXI IN DUE OT HEAT BUILD UP CAUSED BY HEAVY BRAKING. MAINTENANCE CREW DISPATCHED FROM AACI MAIN BASE AT KDTW TO INVESTIGATE THE PROBLEM. NO FURTHER INFORMATION IS AVAILABLE AT THIS TIME AND A SUPPLEMENTAL REPORT WILL BE FOLLOWING UPON COMPLETION OF REQUIRED MAINTENANCE. (M) 2L72 4J RTT00007WI 20030530000872003053000087NM 2003 5 30 DL76L030482 120030520A2120 ODOR BOEING767 767332 1382001NM EXHAUST FAN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27188DN 27583 RECEIVED FWD EQUIP COOLING EXHAUST FAN EICAS MSG WITH STRONG FUMES IN COCKPIT. FWD C/B TRIPPED AND FWD EQUIP COOLING EXHAUST FAN INOP WITH AND ACRID ODOR. FWD FAN TO MCO PER MEL. 2L72 4F RTA1NM 20030530000922003053000092NM 2003 5 30 SWAA031098 120030515A272065C25927 BEARING BOEING737 7372T4 1384492NM AILERON WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED A2 CHECK, FOUND AILERONS DIFFICULT TO MOVE OUT OF CENTER DETENT. REMOVED AND REPLACED 4 EA BEARINGS ON AILERON CONTROL DRUM PER MM. 2L72 4F A16WE 20030530001032003053000103EA 2003 5 30 CA030505008 120030505A5534C6TP103927 SPAR DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING CHANGE OVER CRACKS WERE OBSERVED UNDER THE FORWARD ATTACHMENT POINT. NEW SPAR MANUFACTURED. NO PARTS AVAILABLE FROM MANUFACTURE. 1H72 3T4 TRTA9EA E4EA 6 CP15EA 20030530001082003053000108EA 2003 5 30 CA030507001 120030501A5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER DEDESCENT 1 CA (CAN) DURING DESCENT AT APPROXIMATELY 11000 FT, THE CAPTAIN'S WINDSHIELD SHATTERED. QRH PROCEDURE FOLLOWED, FLIGHT CONTINUED AND LANDED SAFELY. AIRCRAFT RETURNED TO SERVICE FOLLOWING THE WINDSHIELD REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20030602000102003060200010EU 2003 6 2 2003F00356 120030512A2434153912B CONTROL PANEL FOKKERF27 F27MK600 4990706EU DC GENERATOR MALFUNCTIONED A COEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM13730FE 10386 AIRCRAFT DEPARTED SEA FOR JNU, RIGHT GENERATOR FAIL LIGHT ILLUMINATED AND UNABLE TO RESET. PILOT ADVISED TO RETURN TO SEA. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT DC CONTROL PANEL. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T A817 20030602000152003060200015NM 2003 6 2 USAA030050 120030506A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU 23514 FOUND SKIN CORRODED 1 INCH AREA AND .5 INCH AREA, AROUND FASTENER, BL 0 STATION 1016 RADIAL STIFFENER. CORROSION LEVEL 1. REMOVED DAMAGED END OF STIFFENER, INSTALLED NEW SECTION AND SPLICE PER BOEING DRAWING 65C28106. (M) 2L72 4F RTA16WE 20030602000392003060200039EU 2003 6 2 AUS20030410 120030409A2760 SPEED BRAKE BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502* 41580EA FAULTY W O OTHER O OTHER CRCRUISE 1 AUS (AUS) UNCOMMANDED AIRBRAKE OPERATION. EXTENSIVE INVESTIGATION AND TESTING COULD FIND NO CAUSE FOR THE PROBLEM. 2H74 4F4 FRTA49EU E6NE 20030527001102003052700110EA 2003 5 27 2003F00320 120030310A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A MASAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0717175 7175 DIVERTED TO PHX AND DECLARED AN EMERGENCY DUE TO CAPTAIN WINDOW SHATTERED AT 35,000, BELIEVED TO BE FROM A BIRDSTRIKE. MAINTENANCE REPLACED THE WINDSHIELD. (M) 2L72 4F RTA21EA 20030528000172003052800017SW 2003 5 28 HEEA086582 120030428A2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL WARN SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 SIGNAL CONDITIONING UNIT CAUSES TRANSFER CAUTION LIGHT TO FLICKER. 1G72 4U H4SW 20030529000372003052900037EU 2003 5 29 BAQA086395 120030512A6240L771M40C1003 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE TACH MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01135MH6 0131 ROTOR INDICATION DROPS OFF LINE LESS THAN ZERO. INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030529000582003052900058SW 2003 5 29 HEEA086645 120030521A3213412321104 CROSSTUBE BELL 412 412 1182202SW MLG SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R1943 36007 CROSSTUBE CENTER SUPPORT IS SEPERATED. 1G72 4U H4SW 20030529000652003052900065NE 2003 5 29 HEEA086510 120030521A32462070A900 WHEEL SKRSKYS76 S76A 8143006NE NLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH8071 760078 DRY ROTTEN. REPLACED 2 EACH BEARING CONE P/N 1780 DUE TO CORROSION. REPAIRED. 1G72 3U H1NE 20030530000152003053000015NE 2003 5 30 HEEA086531 220030522A73200164348730 FUEL CONTROL SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE NR 2 ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 2650 760166 NR 2 ENGINE LIGHTS OFF BUT WILL NOT ACCELERATE PAST 30 PERCENT N1. 1G72 3U3 U H1NE E19EU 20030530000242003053000024SW 2003 5 30 HEEA086678 120030522A7120 BEARING BELL 412 412 1182202SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 ENGINE MOUNT HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20030530000272003053000027SW 2003 5 30 HEEA086681 120030522A6730 BUSHING BELL 412 412 1182202SW T/R SERVO WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 1838 36002 INPUT LEVER BUSHINGS WORN AND LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20030530000542003053000054WP 2003 5 30 AMTA200300581 120030322A5311 FRAME LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND FORWARD FUSELAGE SECTION, FRAME, REPAIR DOUBLERS, FS 449 CORRODED. DOUBLER ON RIGHT SIDE WAS REPLACED PER LAC DRAWING NR 164 2621 AND SRM 51-40-01. (M) 2L73 4F A23WE 20030530000652003053000065NM 2003 5 30 2003F00340 120030102A551065245711 SUPPORT BOEING727 72721 1384003NM HORIZONTAL STAB CORRODED A XP0BO OTHER O OTHER NRNOT REPORTED 1 SO35727PX 19261 LEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM, AFT LOWER FLANGE, AT 21 INCHES AND 30 INCHES FROM INBOARD END. ELEVATOR STATION 17.20 TO 47.20, CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-06. (M) 2L73 4F A3WE 20030602000622003060200062EU 2003 6 2 CA030424001 120030418A27101F11792 LEVER BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU MOUNTING TAB FRACTURED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA (CAN) DEPARTING THE CREW FOUND ABNORMAL CONTROL INPUT WAS REQUIRED TO MAINTAIN THE AIRCRAFT LEVEL. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WHERE MAINTENACE FOUND A BROKEN LT AILERON CONTROL LEVER. THE MOUNTING FOOT ONTHE FORWARDOUTBOARD CORNER WAS FRACTURED. THE PART WAS REPLACED, AN INSPECTION FOR EXCESS WIND CONDITION EXPOSURE WAS PERFORMED AND NTO5 AILERON PERFORMANCE FLIGHT TEST WAS CONDUCTED PRIOR TO THE AIRCRAFT RETURNING TO SERVICE. 2L72 3T4 T A24EU A196 20030602000692003060200069EA 2003 6 2 CA030514011 120030505A21331037729 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA ISOLATION BLANKEOBSTRUCTED W O OTHER W INADEQUATE Q C CRCRUISE 1 CA (CAN) DURING FIRST PRODUCTION FLT TEST, WHILE PERFORMING PRESSURIZATION TESTING AT FL300, CABIN PRESSURE WAS LOST & CREW HAD TO MAKE AN EMERGENCY DESCENT. ON GROUND TECHNICIAN FOUND A SMALL ISOLATION BLANKET OF APPROXIMATELY 10 INCHES SQUARE STUCKED IN RT OUTFLOW VALVE. BLANKET CAME OFF FROM FS 605 RT STR 17. IT WAS FOUND THAT THE BLANKET WAS NOT INSTALLED WITH DOUBLE FACE TAPE A REQUESTED DURING ASSEMBLY. BLANKET WAS NOT DAMAGED & THEN WAS REINSTALLED PER ASSEMBLY INSTRUCTIONS. AREA WAS REINSPECTED FOR ANY OTHER LOOSE BLANKETS. THE PRESSURE CONTROL PANEL WAS REPLACED AND THE SYSTEM WAS TESTEDSERVICEABLE.THE AIRCRAFT WAS REDISPATCHED FOR FLT AND THE PRESSURIZATION SYSTEM WAS FUNCTIONING SATISFACTORILY. 2L72 4F RTA21EA 20030602000812003060200081CE 2003 6 2 CA030514016 120030507A5310TU206G DOOR FRAME CESSNA206 TU206G 2073357CE CONT O550 IO550F 17042SO MCAULYD3A34 D3A34C402 GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A CESSNA CONTINUED AIRWORTHINESS PROGRAM INSPECTION 53-10-02 A 2 INCH CRACK WAS NOTED IN THE DOOR POST AT THE BOTTOM LEFT OF THE WINDOW. A REPAIR HAD TO BE COMPLETED IN ACCORDANCE WITH CESSNA SEB 93-4 BY INSTALLING THE DOORPOST MODIFICATION KIT SK206-41. 1H71 3O3 O A4CE E3SO 5 CP47GL 20030602000832003060200083NM 2003 6 2 DL738030484 120030521A2910S274A005 FUSE BOEING737 737800* NM MLG WW DAMAGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27383DN 30346 AFTER T/O AND FLAP RETRACTION L/E FLAPS LIGHT REMAINED ILLUMINATED AMBER L/E DEVICES POSITION IND CONFIRMED SEVERAL L/E FLAP INTRANSIT CONDITION. PERFORMED TEST PER FIM 27-81 TASK 803 FAULT CODE 27-81224 FOUND RETRACT HYD FUSE SET. RESET FUSE PERFORMED FIM 27-81 TASK 803 AOO, TEST OK. FLAP/SLAT OPERATION AND IND CHECKED NORMAL. 2L72 4F RTA16WE 20030602000842003060200084NM 2003 6 2 DL73S030485 120030522A53306545800602 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 FUSELAGE SKIN FS 344, S-19R TO S-20R - DENT: A DENT WAS REPORTED APPROXIMATELY 2 INCHES BELOW THE LOWER EDGE OF THE UPPER SKIN OF THE LAP SPLICE AT S-19R. THE DENT MEASURED 2.2 X 1.5 X 0.057 INCH DEEP. THE SKIN PANEL IS 0.036 INCH SKIN WITH A 0.036 INCH INTERNAL BONDED DOUBLER. DAL ER/A 384904-14 CUTS OUT THE DENT, WHICH AFFECTS ONLY THE 0.036 INCH SKIN (NOT THE BONDED DOUBLER), AND INSTALLS A 0.040 INCH 2024-T3 CLAD SHEET REPAIR DOUBLER THAT EXTENDS ACROSS THE S-19R LAP SPLICE. 2L72 4F RTA16WE 20030602000922003060200092NM 2003 6 2 SWAA031184 120030528A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE IN FWD CABIN. SECURED LENS PER MM. 2L72 4F RTA16WE 20030602001062003060200106 2003 6 2 SWAA031174 420030525A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030602001212003060200121 2003 6 2 SWAA031159 420030525A256565C19901 CABLE BOEING737 7373H4 1384600NM ESCAPE SLIDE FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2L72 4F RTA16WE 20030602001242003060200124 2003 6 2 SWAA031162 420030524A2565D31354 SLIDE BOEING737 7373L9 1384470NM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030602001252003060200125NM 2003 6 2 SWAA031163 120030523A5520183A8300 HINGE BOEING737 7377H4 1384404NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29417WN 29822 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB NR 3 AND NR 4 HINGES WORN. REMOVED AND REPLACED HARDWARE ON NR 3 AND NR 4 HINGES PER MM. 2L72 4F RTA16WE 20030602001282003060200128NM 2003 6 2 SWAA031166 120030522A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 672, RBL 36. REPAIRED PRESS WEB PER SRM. 2L72 4F RTA16WE 20030602001312003060200131NM 2003 6 2 SWAA031169 120030524A53126517583 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179.5, WL 177 AT LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SRM. 2L72 4F A16WE 20030602001362003060200136NM 2003 6 2 SWAA031147 120030521A53306545766 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT PAX WINDOW CUTOUT, BS 357, STRINGER 13R. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030602001562003060200156NM 2003 6 2 VNAA0305015 120030521A5320 GASKET DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FWD FUSELAGE LOOSE A VNAAO OTHER O OTHER CLCLIMB 1 GL07424JS 3033 DURING THE CLIMBOUT, THE CREW HEARD A BANGING NOISE ON THE FUSELAGE AND RETURNED TO DAY. MAINTENANCE INSPECTED AND FOUND A PIECE OF WEATHER STRIPPING LOOSE AT THE FORWARD FUSELAGE. MAINTENANCE THEN TRIMMED THE STRIPPING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00 AND THEN PLACED IT ON THE DMI LIST. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030602001572003060200157NM 2003 6 2 VNAA0305013 120030520A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07463PS15534152 3087 THE CREW REPORTED THAT THE FLIGHT ATTENDANTS EMERGENCY SIGN AND FLOOR LIGHTING AT ROW 5 WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030602001732003060200173NM 2003 6 2 AALA20030490 120030422A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21783AN 30004 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 3G INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 3G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030602001802003060200180NM 2003 6 2 AALA20030517 120030422A2420GEN3005 IDG BOEING757 757223 1384957NM GENERATOR FAILED A AALAO OTHER H ELECT. POWER LOSS-50 PC DEDESCENT 1 SW21688AA 25730 OGG - FLT 161 - DURING DESCENT, LEFT GEN CONT OFF LIGHT ILLUMINATED, RAN CHECKLIST UNABLE TO RESTORE GENERATOR. REMOVED AND REPLACED LEFT IDG PER MM, OPS AND LEAK CHECK OK. (M) 2L72 4F RTA2NM 20030604000142003060400014EA 2003 6 4 A6WA200340066 120030510A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 RIGHT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. REMOVED CRACKED PORTION OF ANGLE AND INSTALLED NEW ANGLE IAW BOMARDIER AEROSPACE REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20030529000332003052900033EU 2003 5 29 BAQA086393 120030512A6321L635M1022101 BRAKE UROCOPEC135 EC135T1 5620026EU MAIN ROTOR INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01511ME132 0143 ROTOR BRAKE HAS INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030530000202003053000020SW 2003 5 30 HEEA086674 120030522A6720 BEARING BELL 412 412 1182202SW T/R LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 11008 33113 TAIL ROTOR LINK HAS BEARINGS WORN. REPAIRED. 1G72 4U H4SW 20030602000752003060200075NM 2003 6 2 AUS20030422 120030415A2822568126713005 PUMP BOEING737 737400 138449ANM CFMINTCFM56 CFM563C 13802EU FUEL BOOST MALFUNCTIONED W K NONE O OTHER ININSP/MAINT 1 AUS 1323A (AUS) NR 1 FORWARD FUEL BOOST PUMP SURGING AND CAUSING LOW PRESSURE INDICATIONS. 2L72 4F4 FRTA16WE E21EU 20030602001012003060200101NM 2003 6 2 SWAA031170 120030527A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29762SW 27876 EEPLS COVERS LOOSE AT ROWS NR 1 AND NR 2. SECURED COVERS PER MM. 2L72 4F RTA16WE 20030602001742003060200174NM 2003 6 2 AALA20030491 120030422A3350 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21388AA 27448 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 34B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030604000062003060400006SO 2003 6 4 SIMA200311312 120030417A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 ABI - DURING AN IMBV INSPECTION, THE GALLEY FORWARD FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED SECTION OF THE FORWARD FLOORBEAM. FABRICATED A REPAIR STRAP, SHIM AND TWO DOUBLERS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21 CHAPTERS 53-21-10 FIG 203. (M) 2L72 4F RTT00011AT 20030604000192003060400019SO 2003 6 4 SIMA200311313 120030417A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 DURING AN IMBV INSPECTION, THE CARGO DOOR OPENING LOWER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SILL AND CLEANED AREA. INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 21 CHAPTERS 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20030604000212003060400021SO 2003 6 4 SIMA200312706 120030415A532013500469401 STRUCTURE EMB 135 EMB135LR 3260305SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION CABIN EXTENSION PROFILER RIGHT CORRODED. REMOVED AND INSTALLED SERVICEABLE CABIN EXTENSION PROFILE IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030604000362003060400036SO 2003 6 4 SIMA200312709 120030416A532014524131007 SUPPORT EMB 135 EMB135LR 3260305SO PAX DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, PASSENGER DOOR OPENING AFT THRESHOLD SUPPORT HAS CORROSION. REMOVED CORRODED DOOR OPENING AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030604000532003060400053WP 2003 6 4 UPS03840468 120030405A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, AFT PRESSURE BULKHEAD WEB FWD SIDE CRACKED AT LBL 23 TO 27 AND LBL 3 3 TO 37. 65 INCHES ABOVE FLOORLINE. REMOVED DAMAGE, FABRICATED -25, -27 DOUBLERS AND -29 ANGLE, -9, -11, -19 FILLERS IAW DAC DWG SR 08530007. ALODINED AND PRIMED REPAIRS IA W DC8 SRM 51-1-8. INSTALLED REPAIR IAW DAC DWG SR 08530007. 2L74 4F RT4A25 20030604000552003060400055WP 2003 6 4 UPS03840470 120030417A531037544731N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, STATION 380-400 LONGERON 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 3754473 AND SRM. 51-1-20D 2L74 4F RT4A25 20030515000732003051500073 2003 5 15 DXTA200300021 420030430A3441 WARNING LIGHT CESSNA750 750 2076810CE INERTAIL GUIDANAILLUMINATED E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07971QS 7500071 ON TAKEOFF MASTER CAUTION LIGHT CAME ON FOR FGC B-CHANNEL FAIL, ABORTED TAKEOFF. 2L72 4J RTT00007WI 20030515000772003051500077SO 2003 5 15 SWIA200311927 120030430A3260 CONNECTOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE MLG SHORTED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07216SW 120285 AFTER TAKEOFF LANDING GEAR (ALL 3 WHEELS) WOULD NOT RETRACT. ALL SIX A & B GREEN LIGHTS REMAINED ILLUMINATED. ONLY RIGHT GEAR -A- LIGHT EXTINGUISHED. WITH LANDING GEAR LEVER IN THE DOWN POSITION ALL RED LIGHTS EXTINGUISHED. REMOVED AND REPLACED CONNECTOR P1548 & P0950 AT RIGHT OVERWING FUSELAGE (CONNECTOR INTERNALLY SHORTED), REF EMB120 W/M 20-20-00, 20-50-01 & 32-61-00. CYCLED GEAR NUMEROUS TIMES. NO FAULTS NOTED. OPS CHECK GOOD. P/N: MS3470L8-33S AND P/N: M83723/761415N. 2L72 4T4 TRTA31SO E20NE 20030515000872003051500087SO 2003 5 15 C2XAO3SH131 120030505A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713908 145465 SHV - DURING C-CHECK EXTERNAL REINFORCING ANGLE STIFFENER ON STRINGER 19L WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGE AND PERFORMED ANGLE REPAIR ON AFFECTED STRINGER IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030515000902003051500090SO 2003 5 15 C2XA03SH124 120030502A531514522459003 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 SHV - DURING C-CHECK RAMP ANGLE ON CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION ON AFT END AT FRAME 20. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030515000932003051500093NM 2003 5 15 03FDEA00723 120030426A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING, FOUND OUTBOARD FLAP, INBOARD HINGE WITH MOUNTING HOLES QTY 6 EACH WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69242 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030515000962003051500096EA 2003 5 15 03130678 120030510A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27678BR 7653 DURING MAINTENANCE INSPECTION, THE RT FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515000972003051500097NM 2003 5 15 03131403 120030511A3350362624 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27403FJ 3149 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS FROM SEAT ROW 4 TO 6 WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIPS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030515001042003051500104NM 2003 5 15 03FDEA00618 120030423A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FITTING HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69217 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES LH OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030515001072003051500107CE 2003 5 15 CH1A200393049 120030424A5313 STRINGER CESSNA337 T337G 2075726CE FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293 P3370226 STRINGER 26R CRACKED AT BS 46. 1H72 3O A6CE 20030515001092003051500109NM 2003 5 15 CH1A200395051 120030425A5753 SKIN BOEING727 727290 138408WNM TE FLAP DELAMINATED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LEFT INBOARD FORE FLAP LOWER SURFACE (APPROX MID-WAY) DELAMINATED. 2L73 4F A3WE 20030515001182003051500118EA 2003 5 15 SWIA200311932 120030501A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07941SW 7750 RUDDER TRIM WILL NOT MOVE LEFT. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL PANEL. OPS CHECKS GOOD. FUNCTIONS IN BOTH DIRECTIONS. 2L72 4F RTA21EA 20030515001312003051500131WP 2003 5 15 ZW0A0304803 120030512A3350408822101 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13978TW 53628 BOTH UPPER LAMPS AT EMERGENCY LIGHT TRIPLE FIXTURE IN CONE SLIDE AREA, THE EMERGENCY OVERHEAD LIGHT ON RT SIDE OF TAIL CONE SLIDE, AND THE EMERGENCY OVERHEAD LIGHT IN CATWALK IN TAIL CONE, WERE ALL INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK. CHECK-C 8-17-02 MCI. 2L72 4F RTA6WE 20030515001452003051500145NM 2003 5 15 AWXA200300530 120030512A2932501310000 PRESSURE SENSOR AIRBUSA319 A319132 3930340NM NR 1 ENGINE FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28814AW 1281 CMH - DIVERSION - FLT 0045 - AFTER CLIMBOUT OF DCA EN ROUTE FOR PHX NOTICED HYDRAULIC POWER TRANSFER UNIT ON ECAM AFTER THRUST REDUCTION. ALSO DISPLAYED ECAM MESSAGE NR 1 ENGINE HYDRAULIC PUMP. DIVERTED TO CMH AS PRECAUTION. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP PRESSURE SWITCH (1074GK) IAW AMM TASK 29-11-17-000-010, OPERATIONAL AND LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20030523001282003052300128NM 2003 5 23 QXEA0300579 120030515A2910 LINE DHAV DHC8 DHC8202 2809007NM HYD SYSTEM LEAKING A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM09365PH 526 OTH-ON FLIGHT NUMBER 2156, LOSS NR 2 HYDRAULIC QUANTITY ON DESCENT. NR 2 HYDRAULIC PUMP CAUTION ILLUMINATED WHEN GEAR EXTENDED BY NORMAL PRESSURE. CAUTION LIGHT ILLUMINATED FOR A MAX OF 5-8 MINUTES. ON TAXI NR 2 MAIN HYDRAULIC PRESSURE FLUCTUATED 1800-3000 PSI. INSPECTED NR 2 (EPD). REMOVED AND REPLACED DRAG STRUT ACTUATOR UP FLEX LINE. REPLACED CASE DRAIN FILTER. GROUND RAN AIRCRAFT FOR 10 MINUTES. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030527000682003052700068WP 2003 5 27 AALA20030262 120030303A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21400AA 49311 DURING OVERNIGHT MAINTENANCE, AFT STAIR WALL EMERGENCY EXIT LIGHTS ON LEFT WALL COVER WILL NOT STAY ILLUMINATED. REPLACED AFT STAIR WALL EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030604000732003060400073NM 2003 6 4 UPS03240546 120030411A5260 STRUCTURE BOEING727 72722C 138400FNM AIRSTAIR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, CRACK AT BELLED HOLE ON VERTICAL WEB ON LT SIDE OF AIRSTAIRS AT STA . 1306 (LOWER HOLE). CRACKS STOP DRILLED IAW SRM 51-10-1. HFEC INSP. CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4 RESULTS - NDF CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM 51-40-2 2L73 4F A3WE 20030604000772003060400077NM 2003 6 4 UPS03440491 120030411A5320 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 M/D - FLOOR SUPPORT HEAD SECTION FOUND CORROSION AT LOWER FACE AS MARKED. CORRODED HAT SECTION REPLACED AS PER SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 2 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604000812003060400081NM 2003 6 4 UPS03440495 120030411A5314 SUPPORT BRACKET BOEING747 747121 1384871NM KEEL BEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 KEEL BEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1226 LBL 9. BRACKET REPLACED AS PER SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604000922003060400092NM 2003 6 4 UPS03440506 120030411A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, SEAT TRACK O/B FLANGE UNDER SURFACE CORROSION. BS 670 - 810 RBL 11 SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 14. CORROSION BLEND OUT 0.030 X 1 X 1 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604001042003060400104NM 2003 6 4 UPS03440519 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 660 LT STR - 24 L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001122003060400112NM 2003 6 4 UPS03440527 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 760 LT STR 16L FRAME FOUND CRACKED. FRAME REPAIRED AT BS 760 BETWEEN S14L TO S17L AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001212003060400121NM 2003 6 4 UPS03440536 120030415A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 940 FRAME CRACK AT S24R AS MARKED. BS 940 FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001522003060400152NM 2003 6 4 UPS03440572 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 960, BET S7-8R FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 53-10-04. 2L74 4F A20WE 20030530000832003053000083NM 2003 5 30 DL757030474 120030517A275118196917 TRANSMITTER BOEING757 757232 1384965NM RT TE FLAPS MALFUNCTIONED A DALAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO27680DA UNK 26956 UPON SELECTING FLAPS 1 DEG T/E FLAP ASYM MESSAGE AND AMBER TRAILING EDGE LIGHT, FOLLOWED PROCEDURE AND LANDED WITH L/E AND 1/2 DEG FLAPS. TROUBLESHOT PER FIM FOUND RT POSITION TRANSMITTER 20 DEG OUT OF LIMITS. POSITIONED TRANSMITTER TO CORRECT VALUE PER M/M, CYCLED FLAPS TO FULL DOWN 30 DEG SEVERAL TIMES, NO FAULTS. OPS CHECKS GOOD. 2L72 4F RTA2NM 20030530000842003053000084NM 2003 5 30 DL767030475 120030518A25605027451162251 SEAT BELT BOEING767 767232 1385132NM SEAT 36C DISCONNECTED A DALAO OTHER O OTHER CRCRUISE 1 SO27102DA 22214 DURING TURBULENCE PASSENGER SEAT BELT AT 36C BECAME DISCONNECTED FROM SEAT, CAUSING A PASSENGER TO BE EJECTED FROM THE SEAT. THE SEAT BELT WAS REMOVED AND REPLACED. THEN BELT WAS SENT TO ATL. 2L72 4F RTA1NM 20030530000912003053000091NE 2003 5 30 050849 220030520A7250 GAS GENERATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE FAILED A AMWAO OTHER O OTHER DEDESCENT 1 CE07171ZV9415 9415 UE171 114157 ON APPROACH ON FLIGHT 5547 ARRIVING FROM PITTSBURGH PENNSYLVANIA TO WATERTOWN NEW YORK, THE LEFT ENGINE ITT EXCEEDED LIMITS. THE ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T4 TRTA24CE E26NE 20030602000062003060200006SO 2003 6 2 SIMA200312716 120030420A532014521725013 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL CORRODED. REMOVED CORRODED FORWARD SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030602000292003060200029NE 2003 6 2 CA030514005 220030505A7230 COMPRESSOR ARRIEL1B SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE DAMAGED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) AIRCRAFT WAS BEING GROUND RUN AFTER ASSEMBLY FROM MAJOR MAINT INSPECTION. ALL ENGINE PARAMETERS WERE NORMAL. ENGINE REAR VIBERATION CHECK IAW AWD 1990-064 (A)R1 6MM/S (ACCEPTABLE). ENGINE COAST DOWN 45 SEC. AFTER GROUND RUN AN ENGINE OIL FLOW WAS IN PROGRESS ON A HOT ENGINE WHEN AT 12 SEC INTO OIL FLOW THE ENGINE STARTED MAKING A LOUD METALIC RUBBING SOUND AND THE ENGINE DRAGGED DOWN THE STARTER AND NG DECREASED. AFTER THE ENGINE STOPPED THE COMPRESSOR WAS TURNED BY HAND AND THERE WAS A METALIC RUBBING SOUND AND THE COMPRESSOR WAS HARD TO TURN. WHEN THE ENGINE COOLED TO AMBIENT TEMP THE COMPRESSOR TURNED FREELY AND NO NOISE. ENGINE WAS REMOVED AND SENT FOR REPAIR. 1G71 3U3 UNCH9EU E19EU 20030602000702003060200070GL 2003 6 2 AUS20030417 220030412A7200695687 ENGINE BOEING767 767338 1385151NM GE CF6 CF680C2* GL RIGHT SURGES W O OTHER E VIBRATION/BUFFET CLCLIMB 1 AUS 3838 (AUS) RT ENGINE SURGED. A LOUD THUMP WAS FELT AND PASSENGERS REPORTED SEEING AN ORANGE FLASH. HIGH VIBRATION LEVELS INDICATED FOLLOWING THRUST REDUCTION. 2L72 4F4 FRTA1NM E23EA 20030602000902003060200090NM 2003 6 2 DLM88030491 120030526A7603 CONTROL CABLE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE RESTRICTED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27968DL 53161 726980 DURING TAXI, RT ENGINE THROTTLE WOULD INITIALLY NOT GO PAST APPROX 1-2 INCHES OF TRAVEL. FOUND INSULATION WRAPPED AROUND RT ENGINE THRUST REVERSER CONTROL CABLE PULLEY. REF FOR PULLEY 78-30-00-1B SHEET 1 ITEM 185. AFTER REMOVAL OF INSULATION THROTTLE MOVEMENT NORMAL. 2L72 4F4 FRTA6WE E9NE 20030602001092003060200109NM 2003 6 2 SWAA031177 120030527A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 7L, BS 727B AND BS 727D. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030602001422003060200142NM 2003 6 2 SWAA031153 120030522A2497W0804 WIRE BOEING737 737317 138447PNM RT WING ROOT CHAFED A SWAAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW29698SW 23176 ABORTED TAKEOFF, WITH 80 PERCENT N2, NR 2 ENG WENT BACK TO IDLE. REPAIRED WIRING AT BUNDLE NR W804 PER WDM. OPS CK GOOD PER MM. 2L72 4F RTA16WE 20030602001452003060200145 2003 6 2 SWAA031133 420030521A2565 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030604000242003060400024GL 2003 6 4 SIMA200313206 220030505A720023073300 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL LEFT FAILED A SIMAO OTHER O OTHER TOTAKEOFF 1 SW21824AE 145584 AFTER TAKEOFF WHEN PACK WAS SELECTED ON THE COCKPIT FILLED WITH SMOKE AND CONTINUED UNTIL NR 1 PACK WAS SHUT OFF BY CREW. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20030604000542003060400054WP 2003 6 4 UPS03840469 120030331A53476015176 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, CABIN SEAT TRACK F CRACKED AT STA 1571. REMOVED AND REPLACED SEAT SECTION IAW DC8 SRM 53-2-3 AND UPS EO DC8- 5320-5167. 2L74 4F RT4A25 20030604000792003060400079NM 2003 6 4 UPS03440493 120030411A532065B38600318 STRINGER CLIP BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 BULK CARGO COMPT - BS 2020 STR 34L STRINGER CLIP UPPER EDGE FOUND CRACKED. BS 2020 STR 34L STRINGER CLIP REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030604000992003060400099NM 2003 6 4 UPS03440514 120030412A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 1700 RT FRAME BTN S-3R AND S-4R SHEAR TIE FOUND CRACKED AS MARKED. SHEAR TIE REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030604001232003060400123NM 2003 6 4 UPS03440538 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 540 LT BET STRINGER 22L AND 23L FRAME INNER CHORD FOUND CRACKED. FRAME REPAIRED AS PER HX RS R53-22-35011 AND ENGINEERING FILE NUMBER 747-53-20135. 2L74 4F A20WE 20030604001482003060400148NM 2003 6 4 UPS03440568 120030411A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2180, BET STRINGER 25-26L FRAME WEB FOUND CRACK. M/D FX FRAME WEB REPAIRED AT BS 2180 BTN STR 25L AND STR 26L PER SRM 53-10-04 FIG.39. 2L74 4F A20WE 20030604001512003060400151NM 2003 6 4 UPS03440571 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 BS 540 LT STR 25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER HX RS R53-22-35011 & UPS RA 747-53-20135 REF NRC FF76313 FOR DETAIL. 2L74 4F A20WE 20030604001732003060400173NM 2003 6 4 UPS03440593 120030412A575365B078831 RIB BOEING747 747121 1384871NM NR 9 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 9 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1,2,3,6,7 & 8 (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-5740-18687-A 2L74 4F A20WE 20030604001762003060400176NM 2003 6 4 UPS03440596 120030413A575365B078712 RIB BOEING747 747121 1384871NM NR 20 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT WING - NR 20 VC FLAP O/B I/B ROTARY ACTUAOTR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 4 , 5 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND EO B747-5740-18687-A. 2L74 4F A20WE 20030604001922003060400192NM 2003 6 4 UPS03440617 120030428A5414 SKIN BOEING747 747200 1384847NM NR 4 PYLON WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: P/S, NR 4 PYLON I/B SIDE HAS HOLE WORN IN PREVIOUS REPAIR. ***OPEN*** 2L74 4F RTA20WE 20030604001942003060400194WP 2003 6 4 UPS03840547 120030411A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, FWD ACCESSORY COMPARTMENT AT STA 55 & L24L FRAME IS CRACKED. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51-1-21. MAT ID 7075-0 .07 1 PO 401846.1 FABBED AND LOCATED FRAME SECTION AND SPLICES IAW DC8 S RM 53-2-0, 51-2-24. ALODINED AND PRIMED ALL REPAIR PARTS IAW DC8 SRM 51-1-8 AND INSTALLED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20030604002022003060400202EA 2003 6 4 2003FA0000454 120030502A4930 SOLENOID CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU FUEL STUCK B A6WRO OTHER O OTHER NRNOT REPORTED 1 WP28434AW P1017 7322 DURING ENGINE MAINTENANCE, SMOKE WAS NOTED COMING FROM THE APU INLET DOOR. MECHANICS TRIED TO DRY MOTOR THE APU TO EXTINGUISH THE FLAMES, BUT WERE UNSUCCESSFUL. DRY CHEMICAL WAS USED TO EXTINGUISH THE FLAMES. DURING INVESTIGATION AND TEARDOWN OF THE APU AT THE MFG REPAIR STATION, THE APU FUEL SOLENOID FAILED FUNCTIONAL CHECK AND WAS FOUND TO BE STUCK IN THE OPEN POSITION. TESTING OF THE SOLENOID IS ON-GOING WITH THE INVESTIGATION. 2L72 4F4 FRTA21EA E15NE 20030604002042003060400204NM 2003 6 4 UPS03440632 120030404A783065B97235143 SLEEVE BOEING747 747121 1384871NM NR 1 ENGINE DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, NR 1 ENGINE - FAN THRUST REVERSER SLEEVE DEBOND REVEALED AT EXTERNAL SKIN BETWEEN 8 AND 9 O'CLOCK POSITION. NR 1 ENGINE THRUST REVERSER SLEEVE REPAIRED AS PER RS R-78-30-35003 AND UPS UPS EO B747-7830-18689-A. 2L74 4F A20WE 20030604002062003060400206WP 2003 6 4 UPS03840614 120030414A55405644210505 STRUCTURE DOUG DC8 DC873F 302199FWP RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, UPPER LT SIDE OF RUDDER LE. AREA HAS A 1.5 INCH CRACK AT ZR 298.1255 3.5 INCHES FWD. OF HINGE LINE STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER,CALCULATED RUDDER BALANCE,CALCULATED IN LIMITS AND UPDATED TAG WITH NEW MOMENT OF 2532.127 IN/LBS IN LIMITS,I.A.W. SRM. 55-2-0,51-4-6,51-4-8 2L74 4F RT4A25 20030604002132003060400213CE 2003 6 4 BAQA086230 120030422A3233232710018 ACTUATOR LEAR 55 55LEAR 5170702CE MLG MALFUNCTIONED W BAQAO OTHER N FALSE WARNING NRNOT REPORTED 1 FS0140DK 1180 092 ACTUATOR WOULD NOT INDICATE DOWN AND LOCKED. REPLACED WITH SERVICEABLE UNIT. 2L72 4F A10CE 20030604002302003060400230WP 2003 6 4 UPS03840635 120030410A5711 SPAR DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C-3, WHEN INSPECTING LWR FRONT SPAR ON RT WING, FOUND PREVIOUSLY REPAIRED HOLES TO EXCEED LIMITATIONS CALLED OUT IN EO. FABBED & INSTALLED RPR BUSHINGS FOR HOLES 3,5,&11. FABBED RPR ANGLES J060232-53/56/58/60.LOCATED, DRILLED, AND STRESS COINED REQ'D HOLES IN SPAR AND RPR STRAP & RPR ANGLES.ALODINED & PRIMED.INSTALLED RPR STRAP & RPR ANGLES.ALL IAW DAC DWG 4709980, J060232, REO G09212, DC8 SRM 51-1-25, 51-1-24, 51-1-8, 51-1-20D, & DPS 3.67-56 2L74 4F RT4A25 20030604002312003060400231WP 2003 6 4 UPS03840636 120030414A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, HFEC INSP. OF L-1 DOOR FWD. UPPER CORNER DETECTED A CRACK COMING FROM THE EDGE OF THE CUTOUT EXTENDING FWD AND UP APPROX. 2.375 INCHES AT STA. 25 LONG. 10L REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER,TRIPLER, AND FILLER IAW SRM. 53-2-0 FIG. 15 AND SAA SK 808-031 2L74 4F RT4A25 20030604002332003060400233WP 2003 6 4 UPS03840643 120030415A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, R-2 DOOR UPER AFT CORNER FOUND 1.450 INCHES AND 1.740 INCHES CRACKS IN SKIN AND LONG. 11R AT STA. 1660 CUTOUT DAMAGEIN SKIN AND STOP DRILLED CRACK IN LONG. 11R,NDT VERIFIED NO CRACKS AT CUTOUT AND STOP DRILL TERMINATES CRACK IN LONG., FABRICATED AND INSTALLED DOUBLER,TRIPLER,FILLER AND STRAP I.A.W. SRM 53-2-0 FIG. 21 AND SAA SK 808-475 2L74 4F RT4A25 20030604002392003060400239EU 2003 6 4 CX7A194J41 120030504A26121734362450 SENSOR SAAB SF340 340B 7860101EU TAILPIPE MALFUNCTIONED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03307CE 340B204 DURING TAKEOFF GOT A TAILPIPE HOT ON THE NR 1 ENGINE ABORTED TAKEOFF, TAXIED OFF RUNWAY AND WARNING EXTINGUISHED. 2L72 4T RTA52EU 20030605000242003060500024EU 2003 6 5 2003F00358 120030521A3350 BATTERY BAG JETSTMJETSTM3101 1500215EU EMERGENCY LIGHT DISCHARGED A B16AK NONE L NO TEST ININSP/MAINT 1 NE05536PA 681 EMERGENCY LIGHT BATTERIES DEAD. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT POEWR SUPPLIES IAW AMM 33-50-00. LIGHT OPS CHECKED SATISFACTORY. SUSPECT EMERGENCY LIGHTS WERE SELECTED AND LEFT ON INADVERTENTLY. (M) 2L72 4T RTA21EU 20030605000322003060500032EA 2003 6 5 A6WA200340072 120030513A5753 VANE CNDAIRCL600 CL6002B19 1900309EA LT TE FLAP CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 LEFT OUTBOARD FLAP VANE HAS A CHAFE APPROX .004 INCH DEEP BLENDED DAMAGED AREA IAW WVAC EO 601R-57-3998. (M) 2L72 4F RTA21EA 20030605000332003060500033EA 2003 6 5 A6WA200340071 120030506A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT ARE CRACKED. REMOVED AND REPLACED OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT SIDES IAW CRJ SRM 51-42-06. (M) 2L72 4F RTA21EA 20030605000372003060500037SO 2003 6 5 SIMA200302103 120030112A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SILL, INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142 REV 20, CHAPTERS 51-40-02, 51-20-03, 51-40-06. (M) 2L72 4F RTT00011AT 20030605000422003060500042NM 2003 6 5 AMTA200300683 120030520A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 EGRESS LIGHTING AT ROW 32 AND ROW 33 WILL NOT ILLUMINATE. RECONNECTED WIRES TO LIGHT ASSEMBLY, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030602000852003060200085NM 2003 6 2 DL76S030486 120030522A2780 WIRE HARNESS BOEING767 767332 1382001NM LE FLAP SENSOR DAMAGED A DALAA UNSCHED LANDING N FALSE WARNING LDLANDING 1 SO27133DN 24982 LEADING EDGE FLAP LIGHT AND EICAS MSG WHEN FLAPS WERE PUT TO 20 DEGREES. REPAIRED S301 SENSOR WIRING. 2L72 4F RTA1NM 20030602001142003060200114NM 2003 6 2 SWAA031182 120030526A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS 460, BS 500C AND BS 500D. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030602001232003060200123NM 2003 6 2 SWAA031161 120030524A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030602001372003060200137 2003 6 2 SWAA031148 420030521A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20030602001552003060200155NE 2003 6 2 VNAA0305016 220030522A7320311835602 SIGNAL COND UNIT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE FAILED A VNAAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL07437JS19212 3055 DURING TAKEOFF, THE LT HAND ENGINE WAS ONLY PRODUCING 85 PERCENT TORQUE AND THE CREW ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND TORQUE SIGNAL CONDITIONER AND LEFT HAND TORQUE PROBE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. POWER ASSURANCE RUNS WERE PERFORMED AND NO DEFECTS WERE NOTED. THE AIRCRAT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030604000042003060400004SO 2003 6 4 SIMA200311804 120030422A531112010732001 FRAME EMB 135 EMB135LR 3260305SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND FRAME 81 DAMAGED ON LOWER EDGE. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW EMB 135, SRM 145/1142 CHAPTER 51, REV 21, 51-40-02, 51-20-03, 51-20-01 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030604001072003060400107NM 2003 6 4 UPS03440522 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 960 BET S24 - 25R FRAME FOUND CRACK. REF NRC 7379 FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001882003060400188NM 2003 6 4 UPS03440609 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2060 BET STR 25-26L, FRAME WEB FOUND CRACK. FRAME WEB REPAIRED AT BS 2060 BTN STR 25L AND STR 26L AS PER SRM 53-10-04 FIG 39. 2L74 4F A20WE 20030605000042003060500004NM 2003 6 5 AUS20030429 120030419A29127592113101 FILTER BOEING737 73776N 13844CHNM GE CFM56 CFM567B24 NE HYD POWER CONTAMINATED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) HYDRAULIC RESERVOIR PRESSURISATION MODULE FILTER CONTAMINATED.SYSTEM A CASE DRAIN FILTER CONTAINED TRACES OF METAL. 2L72 4F4 FRTA16WE E00055EN 20030605000382003060500038NM 2003 6 5 USAABB03067 120030501A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 FOUND FLOOR LEVEL EMERGENCY LIGHTS WEAK AT ROWS 4, 13, 29 AND 33. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030605000522003060500052CE 2003 6 5 75M032903 120030329A2140 MUFFLER CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO HEATER CONTAMINATED E UATAA UNSCHED LANDING CB F.O.D. SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL039475M 20700695 SMOKE IN COCKPIT AFTER TAKEOFF. RETURNED TO AIRPORT AND LANDED. REMOVED PLASTIC SHRINK WRAP FROM HEAT MUFFLER. PROPELLER SUCKED A PIECE OF PLASTIC WRAP OFF OF THE RAMP AND INTO THE ENGINE COMPARTMENT. 1H71 3O3 O A16CE E5CE 20030605000782003060500078WP 2003 6 5 ABXA030142 120030510A2997 WIRE DOUG DC9 DC933F 302207AWP HYD PUMP BURNED A ABXAK NONE A FLAME/FIRE ININSP/MAINT 1 GL23933AX3167 MX187512A 47291 RIGHT AUXILIARY HYDRAULIC PUMP POWER WIRES BURNED THROUGH. REMOVED AND REPLACED THE RIGHT AUXILIARY PUMP. OPS CHECKED GOOD IAW DC-9 AMM 29-10-06-2-0001. 2L72 4F A6WE 20030605000922003060500092NM 2003 6 5 UPS03240686 120030423A5350 RIB BOEING727 72722C 138400FNM W/B FAIRING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3430, FWD FORMED SECTION SUPPORT RIB HAS EVIDENCE OF HEAVY CORROSION UNDER ANCHOR NUT PLATES, JUST FWD OF GRND MOVER DOOR CUT OUT DOOR REMOVED IAW SRM 51-30-02. FRAME REMOVED IAW SRM 51-30-02. CORR OSION REMOVED FROM SKIN IAW SRM 51-10-01 FOUND WITHIN LIMITS. FRAME FOUND OUT OF LIMITS IAW SRM 51-10-01 FABRICATED NEW FORMED SECTION IAW SRM 51-20-1. INSTALLED NEW SECTION IAW SRM 51-30-2 2L73 4F A3WE 20030605000952003060500095NM 2003 6 5 UPS03240690 120030430A5755 HINGE FITTING BOEING727 72722C 138400FNM NR 5 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, SUSPECT CRACK FOUND ON NR 5 SPOILER CENTRE HINGE FITTING HFEC INSP. CARRIED OUT ON NR 5 SPOILER CENTER HINGE FITTING IAW B727 N DTM PT 6 51-00-00 FIG 4 RESULT: CRACK CONFIRMED. CENTER HINGE FITTI NG REPLACED IAW SRM 51-30-02 2L73 4F A3WE 20030605000982003060500098WP 2003 6 5 UPS03840691 120030513A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01818UP 46108 EMERGENCY EXIT LIGHTS INOPERATIVE, FOUND ON PREDEPARTURE CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS PER M/M 33-50-01. OPS CKS GOOD. 2L74 4F RT4A25 20030605001082003060500108EU 2003 6 5 HDN2003F00002 120030330A7931DK040 TRANSMITTER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENG OIL PRESSUREINOPERATIVE D HDNAO OTHER O OTHER NRNOT REPORTED 1 SW03105SE S769 INSTALLED NEW PART, INOPERATIVE NEEDLE ON GAUGE WENT TO THE RED LIMIT. (REG NR CHANGED FROM 911VH TO 105SE RESERVED N-NUMBER). 1G72 3U3 U H3EU E4CE 20030605001322003060500132CE 2003 6 5 BLI2003F00000 120030331A3244 TIRE CESSNA500 500CESSNA 2076602CE PWA JT15 JT15D1 52060NE MLG FAILED E BLIAO OTHER O OTHER NRNOT REPORTED 1 GL1758TC 5000261 CONTACTED LOCAL MAINTENANCE TO RECOVER A/C NOT WHEEL AND REPLACE TIRE. RETURNED TO SERVICE. 1L72 4F4 F A22CE E1NE 20030605001412003060500141SO 2003 6 5 SWIA200311967 120030511A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSBURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07215SW 120281 FLOOR LEVEL RED COURTESY LIGHT BY FLIGHT ATTENDANT'S SEAT IS INOP. REMOVED AND REPLACED BULB IN FLOOR LEVEL RED COURTESY LIGHT WITH SERVICEABLE UNIT. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20030605001542003060500154NE 2003 6 5 BAQA086399 220030512A7310 TRANSFER TUBE BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE FUEL MANIFOLD BENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01117UB733 430168701 7062 TRANSFER TUBES BENT. REPLACED WITH SERVICEABLE UNIT. 5/13/03 1G72 3U3 U H13EU E5NE 20030605001552003060500155NE 2003 6 5 BAQA086308 220030430A753297914211 VALVE BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE BLEED SOV FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01932CJ 7024 VALVE WILL NOT ACTUATE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030605001562003060500156EU 2003 6 5 BAQA086350 120030508A3340G83857 LANDING LIGHT BOLKMS117 BK117A1 5626010EU EXTERIOR INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01136AE58 7234 LANDING LIGHT RETRACT INOP. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030605001712003060500171NM 2003 6 5 03139405 120030517A3350 LIGHT DORNERDO32 DO328300 NM CABIN INTERMITTENT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27405FJ DURING PREFLIGHT INSPECTION, CREW REPORTED THAT EMERGENCY LIGHT OUTSIDE OF GALLEY WAS INOPERABLE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030605001732003060500173NM 2003 6 5 03139411 120030517A3397 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27411FJ DURING PREFLIGHT INSPECTION, CREW REPORTED THAT EMERGENCY TRACK FLOOR LIGHTING WAS INOPERABLE. MAINTENANCE PERSONNEL RESECURED A LOOSE CONNECTOR, AN OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE 2H72 4T RTA55NM 20030604000412003060400041SO 2003 6 4 SIMA200312719 120030418A531014522460013 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21709GB 145211 THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION GALLEY AREA CENTER BEAM GUSSET HAS CORROSION. REMOVED AND REPLACED CENTER BEAM GUSSET IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030604000882003060400088NM 2003 6 4 UPS03440502 120030409A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 AFT CARGO COMPT - BS 1540 STRINGER 34 RT FOUND CORRODED. AFT CARGO COMPT BS 1540 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20030604000952003060400095NM 2003 6 4 UPS03440509 120030411A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2180 RT STR 25R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 39. 2L74 4F A20WE 20030604001252003060400125NM 2003 6 4 UPS03440540 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 640 LT STR - 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001342003060400134NM 2003 6 4 UPS03440554 120030413A5313 LONGERON BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 M/D - BS 1235 S8L STRINGER END CRACKED. BS 1235 S8L STRINGER REPAIRED AS PER HX RS R53-21-35017 & UPS RA 747-53-20138. 2L74 4F A20WE 20030604001582003060400158NM 2003 6 4 UPS03440578 120030412A575365B106301 RIB BOEING747 747121 1384871NM NR 3 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 3 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2 & 3 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030604001932003060400193WP 2003 6 4 UPS03840487 120030428A5200 DOOR DOUG DC8 DC873F 302199FWP AIR START CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 LT FUSELAGE SECONDARY AIR START DOOR CRACKED. REPAIRED PER EO DC8-5330-18680-A 2L74 4F RT4A25 20030604001972003060400197EA 2003 6 4 JBXA03004 120030428A2100 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A JBXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05571ML 7209 AIR RETURN FLIGHT 5116 DISCREPANCY : ON LIFTOFF HAD OVERBOARD COOL CAUTION MESSAGE ALSO OVERBOARD COOL FAIL STATUS MESSAGE. CYCLED SERVICE DOOR AND MAIN CABIN DOOR OPERATIONAL CHECK OF OVERBOARD EXHAUST VALVE GOOD I-A-W AMM 21-24-34 2L72 4F RTA21EA 20030605001292003060500129NE 2003 6 5 MEX2003115 220030404A7230 BLADE DOUG MD80 MD83 3023681NM PWA JT9 JT9D* NE NR 2 ENGINE DAMAGED W ASMFO OTHER O OTHER NRNOT REPORTED 1 GL23881LF 53051 A/C UNSCHEDULED LANDING DUE TO ALL PARAMETERS OSCILLATION AND VIBRATION IN BOTH ENG. DURING CLIMB AT FL 310, AFTER ENG AND WING-TAIL DE-ICING WAS SHUTTING OFF, VIBRATION WITHOUT DETONATIONS AND BOTH ENG PARAMETERS OSCILLATED BETWEEN 1.80 TO 2.05 EPRS; VARIATION STOPPED AT POWER REDUCTION WHEN LEVELED AT FL 310. 40 MINUTES LATTER CLIMBING AT FL 350 SAME PROBLEMS WERE SHOWN, ENG REACHED APPROX 1.95 TO 2.00 EPRS. DURING FAN BLADES INSP WERE FOUND LT ENG WITH 11 BLADES DAMAGED AND RT ENG WITH 28 BLADES DAMAGED. BOROSCOPE INSP WAS ACCOMPLISHED TO BOTH ENG NO ADDITIONAL DAMAGE WAS FOUND. DISC C-1 OFF RIGHT ENG WAS REPLACED IAW MM AND LEFT FAN BLADES WERE REPAIRED IAW MM. ENG WERE TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRT E20EA 20030605001722003060500172EA 2003 6 5 03139631 120030516A3350 LIGHT CNDAIRCL600 CL600* EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27631BR DURING MAINTENANCE INSPECTION, CEILING EMERGENCY LIGHT WAS INOPERABLE. MAINTENANCE PERSONNEL RELAMPED CEILING EMERGENCY LIGHT, AN OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20030606000172003060600017NM 2003 6 6 03FDEA00757 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B FWD BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000192003060600019NM 2003 6 6 03FDEA00755 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR 2L73 4F RTA22WE 20030606000202003060600020NM 2003 6 6 03FDEA00754 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHING POINT, O/B AFT BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR 2L73 4F RTA22WE 20030606000682003060600068EU 2003 6 6 03FDEA00782 120030520A5311 FRAME AIRBUS300 A300B4605R 3930308EU FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 DENT IN EXT. FUSELAGE AFT OF BULK CARGO DOOR, AT FRAME 72 AND APPROX. STRINGER 38R. DENT HAS CREASE IN CENTER. DENT MEASURES 1.53 IN LONG, 1.125 IN WIDE AND .093 IN DEEP AT CREASE. CUTOUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER IAW A300-600 SRM 53-10-12. NDT INSPECTED CUT OUT PER NTM 51-10-08, WITH NO CRACK FOUND. INSTALLED REPAIR DOUBLER IAW A300-600 SRM 51-40-23. 2L72 4F RTA35EU 20030606000692003060600069GL 2003 6 6 03FDEA00780 220030520A7261 ENGINE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 3 MALFUNCTIONED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25386FE 46620 451244 CRUISE ALT (FL370) ANC -- SEA 2+19 ENROUTE TIME "ENG NR 3 OIL PRESS LOW" ALERT. FOLLOWED APPROPRIATE CHECKLIST & LANDED AT DESTINATION. EMERGENCY DECLARED. FOUND ANGLE GEARBOX LOOSE ON HORIZONTAL SHAFT ANGLE GEARBOX CASE SEALS BLOWN, SEVERAL OIL LINES SHEARED FROM VIBRATION. TOWER SHAFT SHEARED FROM ANGLE GEARBOX AND VERTICAL SHAFT HOUSING DISINTERGRATED. ALSO NOTED METAL ON A,G & D SCAVANGE MAG PLUGS. REMOVED AND REPLACE THE #3 ENGINE. 2L73 4F4 F A22WE E23EA 20030606000702003060600070WP 2003 6 6 03FDEA00781 120030520A5710 HINGE DOUG MD10 MD1010F WP RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 S 16 COMPLY WITH E.A.8-5740-70384. WINGS INBD FLAP OUTBD HINGE SUPPORT FITTING TO WING ATTACH HOLES REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740-70384. 2L73 4F RTA22WE 20030606000792003060600079NM 2003 6 6 03FDEA00770 120030513A5710 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B CTR BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000842003060600084NM 2003 6 6 03FDEA00765 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP I/B HINGE (FLAP SIDE) AFT ATTACHMENT POINT FWD BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606001022003060600102EU 2003 6 6 CX7A194J43 120030510A7931 WARNING LIGHT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENG OIL ILLUMINATED A CX7AE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL03316CE 340B348 785542 IN CRUISE GOT A RIGHT HAND ENGINE OIL PRESSURE LIGHT WITH RIGHT ENGINE OIL PRESSURE BELOW 30 PSI. APPLIED RIGHT HAND ENGINE SHUTDOWN PER CHECKLIST. NO OTHER DEFECTS NOTED. 2L72 4T4 TRTA52EU E8NE 20030606001032003060600103EU 2003 6 6 CX7A194J0345 120030520A26121734362450 DETECTOR SAAB SF340 340B 7860101EU TAILPIPE FALSE ACTIVATIONA CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03303CE 340B194 TAILPIPE HOT ILLUMINATED ON T/O ROLL ABORTED T/O. RAN CHECKLIST LIGHT OUT AFTER POWER REDUCTION. 2L72 4T RTA52EU 20030609000012003060900001WP 2003 6 9 WRNA200300010 120030521A2612 FIRE LOOP LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 3 ENGINE FALSE ACTIVATIONA WRNAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05311EA 193A1012 10414 AFTER TAKE OFF AND DURING CLIMB OUT A FULL FIRE INDICATION ON NR 3 ENGINE. LOOP A & B ON, FIRE HANDLE ON, FIREBELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATION OFF IMMEDIATLY AFTER ENGINE SHUTDOWN. FIRE BOTTLES NOT FIRED. FUEL DUMPED (APPROX. 8800 GALLONS) AIRCRAFT RETURNED TO FIELD, LANDED NORMAL. INSPECTED ALL PYLON DUCTS AND CAMPS. RETORQUED ALL CONNECTIONS DUE TO RESCENT ENGINE CHANGE PER 36-12-00. RAN ENGINE TO 1.20 IEPR, 45 PSI DUCT PRESSURE, NO FIRE WARNING FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 20030609000122003060900012EA 2003 6 9 SWIA200311980 120030516A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07498SW 7483 STAB TRIM CH1 INOP STATUS MESSAGE INFLIGHT - WILL NOT RESET. REPLACED HSTA AND MCU IAW MM 27-42-01 AND 27-42-05. OPS CHECK OF SYSTEM TEST OK, REF. MM 27-40-00. ACTUATOR P/N: 8396-3 S/N OFF: 698 MCU P/N: 7082-3 S/N OFF: 734. 2L72 4F RTA21EA 20030609000182003060900018WP 2003 6 9 ARWA20030213 120030215A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198968U 46069 DURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 380, STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 380 IAW STC SA1063SO AND SA1377SO. 2L74 4F 4A25 20030609000202003060900020WP 2003 6 9 ARWA20030215 120030215A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198968U 46069 DURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 420 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 420 IAW STC SA1063SO AND SA1377SO. 2L74 4F 4A25 20030609000222003060900022WP 2003 6 9 ARWA20030217 120030215A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198968U 46069 DURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOOR BEAM SPLICE PLATES AT STATION 460 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 460 IAW STC SA1063SO AND SA1377SO. 2L74 4F 4A25 20030609000422003060900042NM 2003 6 9 C1HA200396007 120030520A5347 SEAT TRACK BOEING727 7272J4 1384006NM FUSELAGE GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 GOUGING ON NR 1 SEAT TRACK AT LBL 44 BETWEEN BS 344 & 380. 2L73 4F RTA3WE 20030609000532003060900053WP 2003 6 9 DHL2003807007 120030519A2910000AA5060324 LINE DOUG DC8 DC873F 302199FWP HYD SYSTEM LEAKING A DHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01807DH 45990 AFTER T/O UPON GEAR RETRACTION HYD SYS PX WENT TO ZERO , HYD QTY WENT TO HALF FULL. AILERON CONTROL MANUAL LIGHT ILLUMINATED. COMPLETED HYD PX ABNORMAL. ABNORM PROCEDURE, PX DID NOT INCREASE HYD QTY DECREASED TO AUX LEVEL. COMPLETED HYD QTY LOSS ABNORMAL PROCEDURE, FLAPS WOULD NOT EXTEND HYD PX DID NOT INCREASE, HYD QTY DROPPED TO JUST ABOVE EMER. LEVEL. COMPLETED HYD SYS FAILED EMERGENCY CHECKLIST AND LANDED BACK AT SDQ. T/S SYSTEM FOUND FLEX HYD LINE BROKEN. R&R FLEX LINE IAW MM 29-10-0 ON LH BOGIE TRIM ACTUATOR. SERVICED MAIN HYD. SYSTEM I/A/W/ MM 12-30-1 AND RAN NR 2 AND 3 ENGS I/A/W/ JRH. NO LEAKS NOTED. SYSTEM NORMAL. 2L74 4F RT4A25 20030609000562003060900056WP 2003 6 9 ZW0A0305001 120030521A3350408822101 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139402W 53138 THE CEILING EMERGENCY LIGHT WAS INOPERATIVE ABOVE SEAT 18B, 19B, AND 20B. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 9-4-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030609000752003060900075EA 2003 6 9 QXEA0300627 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS 394, 1 INCH ABOVE STRINGER 15R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000812003060900081EA 2003 6 9 QXEA0300633 120030517A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 FASTENER DAMAGED AT 4 INCHES AFT OF FS549 AND 7 INCHES ABOVE STRINGER 12R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-20, PG 13-22. 2L72 4F RTA21EA 20030604001802003060400180NM 2003 6 4 UPS03440600 120030412A575365B078782 RIB BOEING747 747121 1384871NM NR 19 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT WING - NR 19 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1 TO 8. (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO 747-5740-18687-A 2L74 4F A20WE 20030604001842003060400184NM 2003 6 4 UPS03440604 120030413A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, AFT CARGO DOOR CUTOUT FWD UPPER CORNER FOUND BEAR STRAP CRACK APPROX 3/16 INCHES LONG FROM EDGE. AFT CARGO DOOR CUTOUT FWD CUTOUT UPPER CORNER REPAIRED AS PER SRM 53-30-03 FIG 62 AND REFER NRC 6407 FOR WORK DETAIL. CAT B REPAIR REQUIRES REPEAT INSPECTION THRESHOLD AT 15,000 CYCLES AFTER REPAIR INSTALLATION AND REPEAT AT 3000 CYCLES INTERVAL PER SRM. 2L74 4F A20WE 20030604001952003060400195WP 2003 6 4 UPS03840548 120030402A53105597646 FRAME DOUG DC8 DC873F 302199FWP CUSP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, BS 55 L21L CUSP FRAME CRACKED APPROX 6 INCH LONG. REMOVED FWD CORNER PAN AND FWD LOWER WEB FOR ACCESS FABBED NEW FRAME IAW DAC DWG 5597646. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTAL LED IAW DAC DWG 5597646, 51-1-21, AND 51-1-20D. REINSTALLED FWD LOWE R WEB AND FWD LOWER CORNER PAN IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030604002012003060400201NM 2003 6 4 C8GA20030010 120030429A3244 TIRE BOEING727 727223 1384074NM MLG FAILED A C8GAO OTHER O OTHER LDLANDING 1 SO15715AA 22470 FLIGHT 002 FROM MPTO TO MIA. AFTER NORMAL LANDING AND NORMAL TOUCHDOWN, AND WITHOUT APPLICATION OF BRAKES ON TOUCHDOWN THE MAIN TIRES BLEW AND AIRCRAFT CAME TO A COMPLETE STOP. THE MIA TOWER INFORMED US OF FIRE OR SMOKE COMING FROM RIGHT WHEEL WELL AND WE REQUESTED EMERGENCY ASSISTANCE. FIRE DEPARTMENT RESPONDED AND AIRCRAFT WAS SECURE. THE AIRCRAFT WAS INSPECTED AND PREPARED FOR A SPECIAL MAINTENANCE FERRY FLIGHT FROM MIA TO JAX TO BE WORK AT THE FLIGHTSTAR REPAIR FACILITY IN JACKSONVILLE, FLORIDA. 2L73 4F A3WE 20030605000122003060500012EU 2003 6 5 AUS20030437 120030417A8011 MOTOR AIRBUS330 A330202 3930316EU GE CF6 CF680 30025NE STARTER FAILED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS (AUS) ENGINE STARTER MOTOR FAILED. EXTERNAL DAMAGE TO ENGINE. 2L72 4F4 FRTA46NM E13NE 20030605000272003060500027SO 2003 6 5 SIMA200302106 120030101A5310 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 ABI - FOUND DUIRNG AN IMBV INSPECTION, EXTENSION AT CENTER BEAM BETWEEN FRAME 22 AND 23 CORRODED. REMOVED AND INSTALLED SERVICEABLE EXTENSION IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030605000342003060500034EA 2003 6 5 A6WA200340070 120030520A5755 SKIN CNDAIRCL600 CL6002B19 1900309EA SPOILER DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 RIGHT INBOARD GROUND SPOILER HAS A DENT ON TOP SKIN INSPECTED AND NDT'ED DENT IAW WVAC EO 601R-57-4039A. (M) 2L72 4F RTA21EA 20030605000462003060500046 2003 6 5 2003F00360 420030518A2312 CONTROL PANEL BOEING747 747122 1384872NM NR 1 & 2 VHF COMFAILED A KCSAO OTHER O OTHER CRCRUISE 1 GL23712CK 19754 NR 1 VHF AND NR 2 VHF WILL NOT RECEIVE. REMOVED AND REPLACED NR 1 AND NR 2 VHF COMM PANEL IAW 747 MM 2320. OPERATIONS CHECKS GOOD. (M) 2L74 4F A20WE 20030605001122003060500112EA 2003 6 5 03134633 120030514A3350363782 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27633BR 7274 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030605001172003060500117WP 2003 6 5 MEX2003145 120030427A5754 SLAT DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE WINGS OUT OF ADJUST W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23216AM 49586 DURING TAKE OFF THE SLAT LIGHT DISAGREE TURN ON WITH 13 DEGREES OF ADJUSTMENT ON SLATS, DISAGREE LIGHT TURN ON BEFORE V1. THE FLAP/SLAT BAR AND POSITION WERE ADJUSTED IAW MM. 2L72 4F4 FRTA6WE E2EA 20030605001512003060500151SO 2003 6 5 CHQA000409 120030517A3230 CONTROL UNIT EMB 145 EMB145 3260210SO MLG FAILED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11266 AIR GROUND FAIL LANDING GEAR WOULD NOT RETRACT. REPLACED LGEU. 2L72 4F RTT00011AT 20030606000042003060600004EA 2003 6 6 03139706 120030517A3350 LIGHT CNDAIRCL600 CL600* EA NR 2 INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27706BR DURING MAINTENANCE INSPECTION, RT FUSELAGE NR 2 EMERGENCY LIGHT WAS INOPERABLE. MAINTENANCE PERSONNEL RELAMPED NR 2 EMERGENCY LIGHT, AN OPERATIONAL CHECK SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20030606000162003060600016NM 2003 6 6 03FDEA00758 120030513A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP I/B HINGE (FLAP SIDE), FWD ATTACHING POINT, I/B FWD BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000722003060600072NM 2003 6 6 03FDEA00777 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B CTR BOLT HOLE FOUND CORRODED. ** S/D ** COMING 2L73 4F RTA22WE 20030606000782003060600078NM 2003 6 6 03FDEA00771 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT I/B CTR BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR . 2L73 4F RTA22WE 20030606000912003060600091NM 2003 6 6 COOSDR030018 120030501A5755 SKIN BOEING727 727200 138407ENM NR 14 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG 363 20725 RIGHT WING, FLIGHT SPOILER NR 14, PN 65-17347-54, SN 363, WITH DELAMINATION. 2L73 4F RTA3WE 20030606000972003060600097WP 2003 6 6 ABXA030146 120030519A793142D491C PRESSURE SWITCH DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3B 52039NE NR 3 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 GL23819AX38 45927 645695 AT FL 330, RAT -15, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH 51 PSI AND OIL TEMP. OF 110 DEG. DURING IDLE, TEMP WAS 115 DEGREES, RPESSURE OF 48 PSI. OIL PRESSURE LIGHT FLICKERED AT IDLE. PERFORMED ENGINE SECURING PROCEDURE. NR 3 ENGINE N2 40 PERCENT AND OIL PRESSURE OF 30 PSI WITH ENGINE SECURED. REPLACED NR 3 ENGINE OIL STRAINER. INSPECTED FOR METAL, NONE FOUND. REPLACED LOW OIL PRESSURE SWITCH AND OIL PRESSURE DIFFERENTIAL SWITCH. RUN UP AND LEAK CHECKED GOOD IAW DC-8 MM 79-20-04-2. 2L74 4F4 F 4A25 1E8 20030609000132003060900013SO 2003 6 9 SWIA200311981 120030518A3260 CONNECTOR EMB 120 EMB120ER 3260203SO PROX SENSOR CONTAMINATED A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07579SW 120347 PILOT REPORTS ON TAKE OFF, GEAR WOULD NOT RETRACT UNLESS OVER-RIDDEN, ALSO BOTH FLIGHT - IDLE UNLOCK LIGHT CAME ON AND WOULD GO OUT 3-6 MINS INTO FLIGHT.INSPECTED ALL GEAR PROX SENSORS AND CANNON-PLUG CONNECTIONS, FOUND LT MAIN LANDING GEAR WOW PROX SENSOR CONNECTOR BEHIND GEAR IN NACELLE, FULL OF WATER. CLEANED CANNON PLUG AND PERFORMED MULTIPLE GEAR SWINGS. ALL OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED. 2L72 4T RTA31SO 20030609000242003060900024SO 2003 6 9 C2XA03TY071 120030520A531214547494403 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP RIGHT HAND MOUNT. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EC 5330-01250, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030609000332003060900033WP 2003 6 9 03FDEA00788 120030521A5230 SKIN DOUG DC10 DC1010 3022110WP CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 COMPLY WITH E.A.8-5350-70377.FUSELAGE- LOWER CARGO DOOR- LOWER JAMB SKIN GOUGE REWORK. CLOSING ACTION ON 05/21/03. COMPLIED WITH E.A.8-5350-70377. 2L73 4F A22WE 20030609001012003060900101SO 2003 6 9 C2XA03SH143 120030523A531014526437007 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 DURING C-CHECK THE RIGHT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030609001032003060900103SO 2003 6 9 C2XA03SH145 120030523A531014525480003 THRESHOLD EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 DURING C-CHECK THE BAGGAGE DOOR THRESHOLD LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030609001082003060900108SO 2003 6 9 C2XA03SH150 120030523A531014522460013 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030609001162003060900116NM 2003 6 9 03141405 120030522A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27405FJ DURING MAINTENANCE INSPECTION, AFT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED AFT EXTERIOR EMERGENCY LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T RTA55NM 20030609001402003060900140CE 2003 6 9 GLBA2003062 120030516A249770B46B056R1024 SWITCH BEECH 1900 1900D 1154162CE COCKPIT BURNED OUT A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM03245GL UE245 ELECTRICAL SMOKE FROM BEHIND FO'S AVIONICS PANEL.REPLACED AVIONICS ANNUCIATOR DIM SWITCH, OP/C GOOD.CLOSED. 2L72 4T RTA24CE 20030609001422003060900142NE 2003 6 9 UPS03640696 220030520A7230 COMPRESSOR BOEING767 767300 1385204NM GE CF6 CF680C2B6F 30025NE NR 2 ENGINE VIBRATION A IPXAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO01330UP 27756 704909 AT FL 330 RT ENG COMPRESSOR STALLED. 1ST STALL RT ENG VIB WAS 3.2 / 2ND VIB WAS 5.0. ENG THRUST WAS RETARDED TO IDLE. ON SHUTDOWN ENG READINGS WERE N1L 28.3 R28.7 EGTL 411 R480 N2L 69.0 R 72.0 FFL 1.3 R1. 5. R/R NR 2 ENG PER TC 6002 AND TC 6001. NO DEFECTS NOTED. OPS CK GOOD. 2L72 4F4 FRTA1NM E13NE 20030609001472003060900147SO 2003 6 9 C2XA03SH151 120030525A531514522459003 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV-DURING C-CHECK THE SUPPORT RAMP ON THE CENTER FLOORBEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECT SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030609001792003060900179NE 2003 6 9 CA030501006 220030415A7250 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE FAILED W CD ABORTED TAKEOFF RETURN TO BLOCK XTJENGINE FLAMEOUT ENGINE CASE PENETRATION WARNING INDICATION TOTAKEOFF 1 CA (CAN) FAILURE OCCURRED DURING THE TAKE OFF ROLL AT 65 KNOTS, AIRCRAFT RETURNED TO THE GATE. THE RUNWAY WAS SHUTDOWN FOR A BRIEF PERIOD TO ALLOW FOR DEBRIS TO BE CLEANED UP. A/C 714 EXPERIENCE FAILU RE OF NR 1 LT ENGINE DURING THE TAKEOFF ROLL. A LOUD BANG FOLLOWED BY LEFT ENGINE FAILED EPR 1.0 AND TGT 1148. VISUAL INSPECTION OF THE ENGINE REVEALED A LARGE QUANTITY OF DEBRIS IN TAIL PIPE. DURING STRIP OF ENGINE ALL OF THE BLADES AND STATORS FROM STAGE 4 REARWARDS ARE GONE. 2L72 4F4 FTRA6WE E00061EN 20030609001802003060900180NE 2003 6 9 CA030501007 220030428A7261AS3209017 O-RING DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A135 52043NE HARTZLHCB3T HCB3TN3 GL ENGINE OIL SPLIT W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) IN CRUISE PILOT OBSERVED OIL SPRAYING ONTO THE WINDSCREEN. AS HE WAS CLOSE TO A MAINTENANCE BASE HE ELECTED TO LAND AND HAVE IT LOOKED AT. AT LANDING HE NOTICED OIL PRESSURE HAD DROPPED TO YELLOW (70 PSI AND THE LOW OIL PRESSURE LIGHT HAD FLICKERED ONCE. AFTER NORMAL SHUTDOWN THE MECHANIC FOUND A DEFECTIVE O-RING AT THE TUBE UNION AT THE ENGINE C-FLANGE. O-RING WAS REPLACED , 4 LITERS OF OIL ADDED AND GROUND RUN NORMAL. CHIP DETECTOR AND OIL SCREEN WAS CHECKED CLEAN. 1H71 3R4 T A815 E4EA 6 CP15EA 20030609002022003060900202 2003 6 9 HEEA086575 420030522A34578144002241D GPS SKRSKYS76 S76C 8143008NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 WILL NOT READ RAIM, UNRELIABLE. TO BE SENT TO VENDOR. 1G72 3U NCH1NE 20030605001032003060500103NM 2003 6 5 S03457018 120030422A5730 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE RT WING CORRODED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 24310 DURING C-CHECK, CORROSION FOUND ON THE RT WING LOWER SKIN FRONT SPAR CAVITY UPPER SURFACE, FSSO 1188 - 1197. AFTER REMOVING ATTACHED FITTING, PERFORM AN HFEC SURFACE AND OPEN HOLE INSPECTION. TO VERIFY NO DAMAGE EXISTS. THE BLENDED OUT DIMENSIONS ARE 2.5IN (W) X 11IN (L) WITH A MAX. TAPERED BLEND OF 0.181IN ON THE NON-PADDED AREA. MAKE A PERMANENT REPAIR IAW THE INSTRUCTIONS OF EO 744-57-20-0005/BOEING CHI-TPE-03-00283H. 2L74 4F4 FRTA20WE E24NE 20030605001072003060500107EU 2003 6 5 HDN2003F00001 120030330A7931DK040 TRANSMITTER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENG OIL PRESSUREINOPERATIVE D HDNAO OTHER O OTHER NRNOT REPORTED 1 SW03105SE S769 CAE821660 INSTALLED NEW PART, INOPERATIVE NEEDLE ON GAUGE, STILL WENT TO RED LIMIT. (HDNA610E) (REG NR CHANGED FROM 911VH TO 105SE RESERVED N-NUMBER) 1G72 3U3 U H3EU E4CE 20030606000462003060600046CE 2003 6 6 2003F00285 120030520A2410ALV9510 ALTERNATOR CESSNA310 310R 2074245CE CONT O520 IO520* 17032SO LEFT ENGINE LOOSE E DUFAK NONE O OTHER ININSP/MAINT 1 GL271533T 202 310R0111 THE AIRCRAFT WAS SQUAWKED WITH AN INTERMITTENT ALTERNATOR. THE ALTERNATOR WAS REMOVED FOR REPLACEMENT WHEN IT WAS DISCOVERED THAT THE FORWARD DRIVE BEARING HAD EXCESSIVE PLAY. ALTHOUGH IT CANNOT BE DETERMINED FOR SURE IF THIS WAS THE CAUSE FOR THE ALTERNATOR FALLING OFF LINE. THE FAILURE OF THIS BEARING, HAD IT REMAINED UNDETECTED, WOULD HAVE CAUSED SEVERE DAMAGE TO THE ENGINE WITHIN A FEW MORE HOURS OF OPERATION. 1L72 3O3 O 3A10 E5CE 20030606000542003060600054EA 2003 6 6 COMA0360238 120030517A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01420CA3172 7451 FLIGHT 5082 EMERGENCY LIGHT STATUS MESSAGE WITH EMERGENCY SWITCH IN OFF POSITION. REPLACED ALL FOUR DISCHARGED EMERGENCY BATTERY PACKS (SAME P/N). 2L72 4F RTA21EA 20030606000812003060600081NM 2003 6 6 03FDEA00768 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030609000472003060900047 2003 6 9 CALA0300261 420030521A2565416N242460 CARRIAGE BOEING757 757224 1384958NM SLIDE LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714120 27562 THE RT OFF WING ESCAPE SLIDE CARRIER FAILED TO OPERATE/DEPLOY DURING TEST. THE RT OFFWING SLIDE CARRIER OPERATING CRANK ASSEMBLY WAS FOUND TO HAVE EXCESSIVE PLAY. ALL PINS AND BEARINGS WERE REPLACED IN THE CRANK HANDLE IAW MM 25-65-00. 2L72 4F RTA2NM 20030609000602003060900060EA 2003 6 9 QXEA0300645 120030521A7830TY214810A VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 400 FAILED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09607QX 10024 BOI ON FLIGHT 9851 ON TAKEOFF ROLL ADVANCED POWER TO TAKEOFF GOT LEFT REVERSER FAULT CAUTION LOW SPEED ABORT (60 KNTS). LEFT REVERSER FAULT MESSAGE NO LONGER SHOWING AT GATE ON SHUTDOWN. REMOVED AND REPLACED ISOLATION CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030609000712003060900071EA 2003 6 9 QXEA0300623 120030517A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 19R, 17 INCHES AFT OF FS250. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 25-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000852003060900085EA 2003 6 9 QXEA0300638 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 8R, 4.5 INCHES AFT OF FS 724.08. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-46-06, PG 1-8. 2L72 4F RTA21EA 20030609000922003060900092EU 2003 6 9 AWXA200300573 120030521A3510MF100511 OXYGEN MASK AIRBUS320 A320231 3930325EU FLIGHT DECK LEAKING A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28632AW414514265 81 FLIGHT CREW REPORTED THE FIRST OFFICERS OXYGEN MASK IS LEAKING. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS OXYGEN MASK IAW T/C R1B35301, OPERATIONAL CHECK WAS GOOD. VENDOR LEAK TEST OF OXYGEN MASK S/N 23208 FOUND NO LEAKS, REASON FOR REMOVAL WAS NOT CONFIRMED. A FULL INSPECTION OF MASK WAS ACCOMPLISHED IN WHICH NUMEROUS DEFECTIVE PARTS WERE REPLACED. THESE ITEMS INCLUDE A FRAYED PNEUMATIC HARNESS (P/N MXH30), 10 EACH O-RINGS (P/N R03460X240A20B6), GASKET SEAL (P/N 553008), AND VISOR (P/N 446268). 2L72 4F RTA28NM 20030609000972003060900097SO 2003 6 9 C2XA03IA052 120030520A335078241 INVERTER EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718114 145664 DURING POSTFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT ON ROW SEAT TWELVE (12) FORWARD EXIT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030610000022003061000002 2003 6 10 HEEA086721 420030521A23129210121 TRANSCEIVER SNIAS 350 AS350B 8680801EU COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 NR 2 AND 5 KEYPAD BUTTONS MISSING. FOUND FACEPLATE BAD AND NR 2 AND 5 BUTTONS MISSING. REPLACED. BENCH CHECK GOOD. 1G71 3U H9EU 20030610000112003061000011WP 2003 6 10 MWEA030231 120030527A535059114037 DOUBLER DOUG DC9 DC982 3022082WP RADOME CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 SKIN DOUBLER AROUND LEFT RADOME CUTOUT IS CRACKED. -- REMOVED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030610000122003061000012WP 2003 6 10 MWEA030232 120030527A531059101419 PAN DOUG DC9 DC982 3022082WP CARGO DOORWAY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 AFT CARGO DOOR FORWARD END HAS MODERATE CORROSION ON INNER PAN BETWEEN NR 2 AND 3 BEAMS. -- BLENDED CORROSION AND INSTALLED TWO EACH RIVETS. 2L72 4F A6WE 20030610000172003061000017NM 2003 6 10 2003UALA00418 120030509A2133VFT300BA1 VALVE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN PRESSURE MALFUNCTIONED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29841UA 1545 ABORTED TAKEOFF DUE TO A VENT AVIONIC FAULT. ABORTED A 2ND TIME FOR THE SAME REASON. SUPPLEMENTAL DATA UPDATE SKIN AIR OUTLET VALVE SUBSEQUENTLY REPLACED (AFTER BEING FAULTED) AND NO FURTHER DISCREPANCIES REPORTED. 2L72 4F4 FRTA28NM E40NE 20030610000242003061000024CE 2003 6 10 4144W1 120030520A32303540121 DRAG LINK BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO HARTZLHCA3V PHCA3VF4 GL MLG CRACKED E ESUAO OTHER O OTHER CRCRUISE 1 CE034144W TH554 IT WAS NOTICED THAT THE NLG DOORS WOULD NOT CLOSE UPON MLG RETRACTION. RETRACTION MECHANISM WAS INSPECTED WITH NO ABNORMAL INDICATION EVIDENT. A/C JACKED & GEAR RETRACT TEST BEGUN SO THAT MLG WOULD BE UP & NLG PIN ENGAGED WITH NGL DOORS ACTUATOR HOOK. NOTICED THAT UPPER (REAR) DRAG BRACE BROKEN AT LEAST 75 PERCENT AROUND TUBE STRUCTURE THAT WOULD ONLY OPEN BREAK WHEN THE LANDING GEAR WOULD ENGAGE NGL DOOR ACTUATOR HOOK. CRACK STARTED FROM DRIVE RIVET IN TUBE. DRIVE RIVET IS USED TO PLUG CORROSION PREVENT HOLE IN TUBE. BREAK HAS EXSISTED FOR SOME TIME & ONLY RECENTLY STARTED TO "RUN" AS EVIDENCED BY CORROSION AND FRESH BREAK INDICATION ON TUBE. NEW KIT WAS INSTALLED. 1L72 3O3 O 3A16 E5CE 5 CP6EA 20030610000272003061000027EA 2003 6 10 QXEA0300650 120030525A3010 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 ILLUMINATED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09604QX 10019 ON FLIGHT NUMBER 2423, COWL AND ANTI ICE ON, CLIMBING THROUGH 290,000 FFET, SELECT WING ANTI ICE OFF AND GET NR 1 ENGINE BLEED CAUTION. HALFWAY THROUGH CHECKLIST, GET A RT PACK MESSAGE. INTERROGATED MDC, NO ASSOCIATED FAULTS IN FAULT HISTORY. COMPLIED WITH OPERATIONAL TEST OF WING ANTI ICE CONTROL AND INDICATING SYSTEM. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030610000292003061000029SO 2003 6 10 LR7A03045 120030523A272237202111 BOOSTER LKHEED382 382G 526414USO RUDDER ACTUATOR BINDING A LR7AL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 AL03403LC 7793 4590 DURING APPROACH TO BET FLT CREW REPORTED RUDDER WOULD NOT MOVE PAST NEUTRAL TO THE RT. INITIATED GO AROUND. ON SECOND APPROACH SOME RT RUDDER CONTROL WAS REGAINED WITH FLAPS AT 50 PERCENT AND IAS 150 KTS. FLEW ABNORMAL PATTERN AND USED DIFFERENTIAL POWER TO MAINTAIN RUNWAY ALIGNMENT. ON ROLL OUT RUDDER REACTED NORMALLY BELOW 60 KTS. INSPECTED RUDDER CONTROL SYSTEM FOR FREEDOM OF MOVEMENT. NO DEFECTS NOTED. NOTED INTERNAL POPPING SOUND FROM RUDDER BOOSTER ASSY DURING MOVEMENT. REPLACED RUDDER BOOSTER ASSY IAW SMP 581 27-20 PG 217-219, LEAK AND OPS CHECK NORMAL. AIRCRAFT RELEASED FOR TEST FLIGHT TO CONFIRM CORRECTIVE ACTION. TEST FLIGHT SATISFACTORY. LP 12179, ITEM 1. 2H74 4T A1SO 20030610000462003061000046WP 2003 6 10 ABXA030156 120030325A5310591013044 SHEAR TIE DOUG DC9 DC932 3022066WP AFT CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 FS 996 BETWEEN LONGERON 18 RIGHT - LONGERON 19 RIGHT, SHEAR TIE CRACKED. REPLACED SHEAR TIE AT STA 996, LONGERON 18 RIGHT - LONGERON 19 RIGHT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030610000482003061000048WP 2003 6 10 ABXA030160 120030403A53209911840112 BRACKET DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 BULKHEAD AT STA 1087 HAD CRACKED ATTACH BRACKET LOCATED ON AFT FACE UPPER FLANGE AT 12:00 POSITION. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030610000492003061000049WP 2003 6 10 ABXA030161 120030403A55105918000515 CAP DOUG DC9 DC931 3022065WP HORIZONTAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 HORIZONTAL STABILIZER LEFT LOWER T-CAP CRACKED AT OUTER TIP. REPAIRED AREA IAW DC-9 SRM 55-02. 2L72 4F A6WE 20030610000502003061000050WP 2003 6 10 ABXA030162 120030421A57555910055514 SKIN DOUG DC9 DC933F 302207AWP RT WING SPOILER DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 LARGE AREA OF DELAMINATION ON UPPER AND LOWER SURFACE OF THE RIGHT WING INBOARD SPOILER PANEL. REPLACED SPOILER IAW DC-9 MM 27-61-01-4-0001. 2L72 4F A6WE 20030610000612003061000061SO 2003 6 10 C2XA03IA051 120030521A3210 LANDING GEAR EMB 145 EMB145 3260210SO MAIN MALFUNCTIONED A C2XAO OTHER O OTHER TOTAKEOFF 1 SW2712122 145684 AFTER TAKEOFF FROM IAH, THE CREW NOTED THAT THE LANDING GEAR FAILED TO RETRACT. THE FLIGHT CONTINUED TO DAL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSTALLED THE LANDING GEAR SAFETY PINS AND, SAFTIED THE PINS. A MAINTENANCE FERRY FLIGHT WAS FLOWN FROM DAL TO IAH. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. DIFFICULTY DATE WAS 5/21/2003, NOT 2/21. UPDATED 5/27/03 2L72 4F RTT00011AT 20030610000622003061000062EA 2003 6 10 COMA0360246 120030521A2721 PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A COMAK NONE O OTHER ININSP/MAINT 1 SO01739CA 7273 RUDDER TRIM INTERMITTENTLY STICKS WHEN SELECTIG TO THE RIGHT. REPLACED THE RUDDER TRIM PANEL, SUSPECT TRIM SWITCH WORN. 2L72 4F RTA21EA 20030610000672003061000067NM 2003 6 10 DL733030408 120030501A5311654583392 FRAME BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272310 23596 FUSELAGE / COCKPIT FLOOR STRUCTURE / CRACKED WEB AND INTERCOSTAL / STA 178, WL 207, RBL 28, THE INTERCOSTAL OUTBOARD STRUCTURE AND HORIZONTAL WEB WERE FOUND CRACKED. BOTH ARE LOCATED IMMEDIATELY AFT OF THE STA 178 BULKHEAD. THE CRACK WAS TRIMMED OUT OF THE STRUCTURE AND A NEW BULKHEAD ATTACH CLIP WAS INSTALLED WHICH PICKS UP ADDITIONAL FASTENERS ON THE CHORD AND WEB. THE WEB WAS REPLACED. ALL WORK WAS ACCOMPLISHED PER ER/A 384917-14AD. 2L72 4F RTA16WE 20030610000882003061000088NE 2003 6 10 DLM88030430 220030506A7261 STRAINER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE CLOGGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27923DL31682 725779 49705 725779 DURING DEPARTURE RT OIL STRAINER CLOGGED MSG CAME ON. FOLLOWED CHECK LIST RETARDED TO IDLE LIGHT REMAINED ON. CONTINUED TO OPERATE AT IDLE. .OIL TEMP REACHED 114 BEFORE THROTTLES WERE RETARDED TO IDLE. DURING TAXI IN EGT ON RT ENG WAS 423. COMPARED T0 330 ON LT ENG. REPLACED DELTA P SWITCH RAN ENG LK CKD GOOD OIL PRESS/TEMP GOOD AT ALL ENG SETTINGS. REPLACED OIL FILTER NO DEBRIS FOUND ON OIL FILTER OR MCD.OIL TEMP PLACARDS OK AS WELL AS EGT WITHIN LIMITS 2L72 4F4 FRTA6WE E9NE 20030527000742003052700074WP 2003 5 27 AALA20030383 120030327A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21452AA 49553 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWELL WALL MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000762003052700076WP 2003 5 27 AALA20030250 120030227A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21437AA 49455 DFW - RIGHT OVERHEAD EMERGENCY PATH LIGHT AT ROW 7 INOPERATIVE. REPAIRED LOOSE GROUND WIRE AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030527001202003052700120EU 2003 5 27 Z8R2003F00000 120030311A3222212422001 BUSHING CASA C212 C212CC 2410204EU GARRTTTPE331TPE331* 01514WP NLG WORN E Z8RAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA23352CA 342 190 WHILE LANDING, NOSE GEAR HAD EXTREME VIBRATION CAUSING TORQUE ARM PINS TO POP OUT AND DAMAGING THE BUSHINGS. 2H72 4T3 T A43EU E2WE 20030527001272003052700127NM 2003 5 27 CW12003F00001 120030501A3020 PRESSURE SWITCH AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE NACELLE CRACKED A CW1RO OTHER O OTHER NRNOT REPORTED 1 EA11790M 4894 19 WHILE PERFORMING A ROUTINE ENGINE INSPECTION A BLEED AIR TAP FOR NACELLE ANTI-ICE PRESSURE SWITCHES WAS FOUND TO BE CRACKED AT THE WELD LOCATION. PROBABLE CAUSE WAS VIBRATION. THIS COULD BE PREVENTED BY INSTALLING SUPPORT BRACKET AND NOTING SPECIFIC AREA FOR INSPECTION DURING INSPECTION. 2K73 4F4 FRTA50NM E44NE 20030528000072003052800007EU 2003 5 28 HEEA086733 120030522A3340356H2802 POWER SUPPLY SNIAS 350 AS350B2 8680813EU STROBE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH 3248 STROBE LIGHT POWER SUPPLY HASN`T ANY POWER OUTPUT. TO BE SENT TO VENDOR. 1G71 3U H9EU 20030528000132003052800013GL 2003 5 28 ERAA086435 220030424A7323252466715 GOVERNOR BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL ENGINE SPLIT E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01 11427 DOES NOT KEEP SPEED CAUSING TORQUE SPLIT. OVERHAULED IAW HONEYWELL OHM FORM 15-1095A. 1G72 3U3 UNCH3EU E4CE 20030528000232003052800023SW 2003 5 28 HEEA086589 120030512A2821 FILTER BELL 206 206B3 1181506SW FUEL SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 TORQUE DROPPED TO 50 PERCENT, N1 DROPPED, PILOT LOWERED COLLECTIVE AND ALL RETURNED TO NORMAL. REPLACED FUEL SYSTEM COMPONENTS: F/C, GOVERNOR, FUEL NOZZLE AND FUEL FILTER. 1G71 3U H2SW 20030528000622003052800062EU 2003 5 28 BAQA086416 120030514A6210L621M1010054 BLADE UROCOPEC135 EC135P1 8680990EU MAIN ROTOR CONTAMINATED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01135ME2907 0009 SUSPECTED WATER IN BLADE. INSTALLED REPAIRED SERVICEABLE UNIT. 1G72 3U O H88EU 20030528000802003052800080NM 2003 5 28 KPVA200321 120030427A2611 WARNING LIGHT DHAV DHC8 DHC8103 1386005NM CARGO SMOKE ILLUMINATED A KPVAO OTHER N FALSE WARNING APAPPROACH 1 WP13808WP 026 BAGGAGE SMOKE WARNING IN FLIGHT. COMPLIED WITH WALK AROUND AND HAVE DETERMINED THE AIRCRAFT TO BE SAFE FOR FERRY FLIGHT FROM MKK TO HNL ONLY IAW GMM CHAPTER 4 PAGE 4.7 TO 4.10. RE-LAMPED NR 2 BAGGAGE SMOKE DETECTOR IAW 8 CMM 26-10-21 SECTION 60 PAGE 7. OPS CHECK GOOD IAW 8 MM 26-12-00 PAGE 201 SECTION A. NO DEFECTS FOUND. (M) 2H72 4T RTA13NM 20030528001082003052800108SW 2003 5 28 HEEA086616 120030521A6710212076015001 CHECK VALVE BELL 412 412 1182202SW RT CYCLIC SERVO LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032014K 33020 RT CYCLIC SERVO CHECK VALVE LEAKING. 1G72 4U H4SW 20030529000192003052900019GL 2003 5 29 15HA0358002 220030423A72616794516 LINE CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL NR 4 BEARING OILBROKEN A I5HAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL23582P 475 WHILE EN ROUTE BETWEEN CVG AND PIT, THE CAPTAIN NOTICED A DROP FROM 65 PSI TO 50 PSI IN THE LEFT POEWR SECTION OIL PRESSURE, FLUCTUATING REDUCTION GEARBOX OIL PRESSURE AND A THREE GALLON DROP IN OIL QTY. THE CAPTAIN PULLED THE LEFT 'E' HANDLE AND SECURED THE ENGINE. THE CREW DIVERTED TO THE COLUMBUS MAINTENANCE FACILITY AT LCK. A BROKEN EXTERNAL OIL PRESSURE LINE SERVICING THE NR 4 BEARING WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE FAILURE OF THE OIL LINE MAY HAVE BEEN CAUSED BY A VIBRATING REDUCTION GEARBOX THAT HAD RECENTLY BEEN REPLACED ON THAT ENGINE. (M) 2L72 4R4 T 6A6 E282 20030529000262003052900026NE 2003 5 29 HEEA086624 220030521A7532312320301 BLEED VALVE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 BLEED VALVE DOES NOT SEAT PROPERLY WHEN CLOSED. CAUSING HIGH ITT. 1G72 4U4 U H4SW E22EA 20030529000312003052900031SW 2003 5 29 HEEA086629 120030521A6220 BEARING BELL 412 412 1182202SW PENDULUM ASSY. ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 PHI702 36003 MAIN ROTOR PENDULUM ASSY BEARING HAS ROUGHNESS. REPAIRED. 1G72 4U H4SW 20030530000302003053000030SW 2003 5 30 HEEA086682 120030522A2911212076007003 ACCUMULATOR BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03107X 33113 ACCUMULATOR LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20030530000452003053000045SW 2003 5 30 HEEA086690 120030522A6220412010182101 BEARING BELL 412 412 1182202SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214981809 36003 MAIN ROTOR GEARBOX HAS BEARING WEAR. SCRAPPED. 1G72 4U H4SW 20030530000472003053000047SW 2003 5 30 HEEA086692 120030522A6230412010406115 BEARING BELL 412 412 1182202SW M/R LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214983711 36003 MAIN ROTOR LINK HAS BEARING WEAR. REPAIRED. 1G72 4U H4SW 20030530000722003053000072SO 2003 5 30 SIMA200311806 120030425A532014525480003 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 21, CHAPTERS 51-40-02, 51-40-06, 51-20-03. (M) 2L72 4T RTT00011AT 20030530000892003053000089NE 2003 5 30 050683 220030514A7320 ROD BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FUEL CONTROL DISCONNECTED A AMWAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CE07242YV UE242 WHILE EN ROUTE ON FLIGHT 5598 FROM MORGANTOWN PENNSYLVANIA TO PITTSBURGH PENNSYLVANIA, THE RIGHT ENGINE DISPLAYED RAPIDLY INCREASING AND UNCONTROLLABLE RISE IN TORQUE AND FUEL FLOW. THE CREW EVALUATED THE SITUATION AND AGREED TO PERFORM A PRECAUTIONARY ENGINE SHUT DOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND 8 .25 INCH ROD DISCONNECTED AT THE FUEL CONTROL UNIT. MAINTENANCE REINSTALLED THE ROD. THE AIRCRAFT DID A GROUND RUN AND THEN WAS RETURNED TO SERVICE. NO PARTS WERE USED THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T4 TRTA24CE E26NE 20030530001052003053000105EA 2003 5 30 CA030505009 120030505A5531C6TP103931 SPAR DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING CHANGE OVER CRACKS WERE OBSERVED UNDER THE AFT ATTACHMENT POINT. NEW SPAR MANUFACTURED. NO PARTS AVAILABLE FROM MANUFACTURE. POOR PRODUCT SUPPORT. 1H72 3T4 TRTA9EA E4EA 6 CP15EA 20030530001252003053000125NE 2003 5 30 BJNA030501 220030506A7260717000 GEARBOX BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE RT ENGINE LEAKING A BJNAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP11344TM 23044 709406 NR 2 ENGINE DEVELOPED OIL LEAK IN FLIGHT, ENGINE SHUT DOWN, AIRCRAFT LANDED WITHOUT INCIDENT. FOND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED, OIL LEAKING AROUND THE PORTS BANJO FITTING FOR THE OIL PRESSURE SWITCH'S OIL LINE. INSTALLED A HELICAL COIL IAW PW STANDARD PRACTICES MANUAL, PN 585005, TASK 70-00-00-350-002 SPOP 415. ENGINE LEAK CHECKED OK. (M) 2L72 4F4 FRTA16WE E2EA 20030602000022003060200002SO 2003 6 2 ASOA03195 120030502A3350 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11268AS 120202 DURING A GROUND INSPECTION IN DFW, THE RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030602000112003060200011CE 2003 6 2 2003F00357 120030424A2910NAS161216 PACKING CESSNA500 560CESSNA 2076750CE HYD POWERPACK LEAKING A IMJAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA2515SK 5600395 ON FINAL APPROACH TO KTEB, BOTH THE POEWR BRAKE AND ANTI-SKID LIGHTS ILLUMINATED. DIVERTED TO KEWR, TO TAKE ADVANTAGE OF GREATER RUNWAY LENGTH. AFTER LANDING MAINTENANCE, FOUND THE O-RING SEALING THE HYDRAULIC FILTER IN THE POEWR BRAKE UNIT PROTRUDING CAUSING FLUID LOSS. (M) 2L72 4F RTA22CE 20030602000142003060200014NM 2003 6 2 USAA030049 120030506A530069353521 CLIP BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US40013 23990 PIT - FOUND STRINGER ATTACH CLIP CRACKED .25 INCH, STATION 578, S4R. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-00-03. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-00-03. (M) 2L72 4F RTA16WE 20030602000172003060200017NM 2003 6 2 USAASB03056 120030428A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHTSLOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 PIT - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS, AT SEAT ROWS 17 THROUGH 22, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE SPLICE IN SEAT ROW 20, LEFT SIDE. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20030602000512003060200051EA 2003 6 2 CA030514008 120030513A2612261030013A22 WIRE DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL FIRE LOOP BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 32910 (CAN) DURING HEAVY MAINT INSPECT FOUND TWO WIRES CHAFED & BROKEN AT DETERIORATED CLAMPS IN LOWER AFT FIREWALL AREA. RUBBER CUSHION HAD TORN AWAY ALLOWING METAL CLAMP TO WEAR WIRES. THESE WIRES ARE FOR FIRE LOOP SYSTEM ON NR 3 ENGINE, WHICH WAS WORKING WHEN AIRCRAFT WAS TAKEN DOWN FOR MAINT. ONLY SUPPORT CLAMPS WERE HOLDING WIRES TOGETHER. FIRE LOOP SYSTEM HAS BEEN SNAGGED MANY TIMES IN THE PAST, IT WOULD FAIL PRE-FLIGHT TEST THREE OR FORE TIMES PER YEAR, MOSTLY ON COLD WINTER MORNINGS. IT WAS USUALLY REPAIRED BY CLEANING/REPLACING CONNECTIONS IN THE FIRE LOOP. I SUSPECT THAT THE BAD CONNECTION IN THESE CHAFED & BROKEN WIRES MAY HAVE INCREASED THE RESISTANCE IN SYSTEM AND CAUSED TEST TO FAIL IN THE SYSTEM. 2H74 4T4 T A20EA E4EA 6 CP1NE 20030528000202003052800020EU 2003 5 28 ERAA086440 120030425A3212D24762101 FLOAT BOLKMS105 BO105CBS 5626008EU MLG LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01130EH1347 558 7 HOLES FOUND AS INDICATED ON BAG, PATCHED ALL PINHOLES IAW 25-60-95 1G72 3U NCH3EU 20030528000862003052800086SW 2003 5 28 HEEA086600 120030521A7160209062214001 ACTUATOR BELL 412 412 1182202SW ENG INTAKE STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 ACTUATOR STUCK AND CIRCUIT BREAKER KEEPS POPPING. 1G72 4U H4SW 20030529000082003052900008NM 2003 5 29 AALA20030432 120030410A5320 FLOOR SUPPORT BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21621AM 24579 FOUND TOP OF AFT FLOOR SUPPORT CORRODED CENTER, FS 1640-1660. REMOVED AFT FLOOR SUPPORT. INSTALLED NEW AUX FLOOR SUPPORT PER SRM 51-70. (M) 2L72 4F RTA2NM 20030529000842003052900084SW 2003 5 29 HEEA086658 120030521A6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 TAIL ROTOR HAS WORN BUSHINGS; VIBRATION IN TAIL ROTOR. REPAIRED. 1G72 4U H4SW 20030530000372003053000037 2003 5 30 HEEA086543 420030522A3455071121805 CONTROL UNIT SKRSKYS76 S76A 8143006NE ADF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 ADF CONTROL UNIT IS UNREADABLE. IN SHOP REPAIR. 1G72 3U H1NE 20030602000192003060200019NM 2003 6 2 USAA030044 120030428A5311 FRAME BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US40460 23885 PIT - FOUND FRAME CRACKED .5 INCH, FS 480 S8R S9R. COMPLETED REPAIRS FOR TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20030602000492003060200049NM 2003 6 2 AUS20030415 120030411A4970D4934J CONNECTOR BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU APU INDICATOR LOOSE W O OTHER N FALSE WARNING CLCLIMB 1 AUS (AUS) APU INOPERATIVE, LIGHT FAULTY. INVESTIGATION FOUND BACKSHELL ON CONNECTOR D4934J LOOSE. 2L72 4F4 FRTA16WE E21EU 20030602000612003060200061EU 2003 6 2 CA030403002 120030331A7712311629401 LIMITER PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TORQUE MALFUNCTIONED W O OTHER RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CRCRUISE 1 CA (CAN) DURING TROUBLESHOOTING FOR A 2-3 LB. FLUCTUATION IN TQ.AND NP. AND NG., IT WAS DEEMED THAT THE FCU WAS AT FAULT AND REPLACED. RUN UP PARAMETERS APPEARED TO BE NORMAL & A TEST FLIGHT WAS INITIATED. AFTER APPX. 10 MIN IN CRUISE & MULTIPLE POWER LEVER MOVEMENTS FROM 25-40 LBS. TQ. A/C APPEARED TO BE OPERATING AS PER NORMAL. UPON RETURNING TO BASE POWER LEVER WAS MOVED AHEAD FOR LANDING & THERE WAS A 3 LB REDUCTION IN TQ INSTEAD, ATTEMPTS WERE MADE AT INCREASE TQ. & EACH TIME POWER WOULD REDUCE. POWER LEVER LEFT ALONE & A UNEVENTFUL LANDING WAS MADE.AFTER TOUCHDOWN THERE WAS NO RESPONSE IN EITHER FORWARD OR REVERSE MODE BY POWER LEVER. POST FLIGHT TROUBLESHOOTING IDENTIFIED TORQUE LIMITER TO BE AT FAULT WHEN 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030602000632003060200063CE 2003 6 2 CA030424002 120030424A32334377113 CAP BEECH 99 99A 1154003CE PWA PT6 PT6A28 EA NLG ACTUATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 19264 (CAN) ACTUATOR WAS REMOVED FOR ANOTHER REASON AND SENT IN FOR OVERHAUL. UPON LPI OF END CAP CRACK INDICATIONS WERE NOTED IN THE EXTEND END CAP. THIS WILL BE THE THIRD FAILURE. CRACK WAS IN THE SAME PLACE AS 2 PREVIOUS MAJOR FRACTURES 1L72 3T4 T A14CE E4EA 20030602000732003060200073EU 2003 6 2 AUS20030420 120030414A324250135042 BRAKE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE MAIN ROTOR FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BRAKE ROTOR AND STATOR INNER DRIVE LUGS FAILED. SEVERAL SMALL STONES WERE FOUND IN THE DEBRIS. SUSPECT CAUSED BY LOOSE GRAVEL FROM OUTBACK AIRSTRIPS. 2L72 4F4 FRT E25NE 20030602000792003060200079 2003 6 2 CA030514014 420030505A34254056510903 DISPLAY HONEYWELL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FLT DIRECTOR FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA 95043025 (CAN) CAPTAIN'S PRIMARY FLIGHT DISPLAY FLARED BRIGHT THEM WENT OUT FOLLOWED IMMEDIATELY BY ODOR OF SMOKE AND SOON AFTER BLUE SMOKE EMANATED FROM PDF AREA. PART SENT FOR OVERHAUL. 2L72 4F4 FRTA6WE E9NE 20030602000802003060200080EU 2003 6 2 CA030514015 120030512A26213473641 HEAD BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FIRE EXTING CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THIS DUAL OUTLET, FORWARD NR 1 CARGO BAY EXTINGUISHER WAS RECEIVED FOR OVERHAUL AFTER HAVING BEEN DISCHARGED THROUGH ONE OUTLET. UPON REMOVAL OF THE SAFETY CAP FROM THE DISCHARGE HEAD OF THE UNFIRED OUTLET, THE INTERIOR OF THE DISCHARGE OUTLET WAS FOUND TO BE TIGHTLY PACKED WITH AN UNIDENTIFIED COARSELY CRYSTALLINE SUBSTANCE THAT APPEARS TO HAVE CORRODED THE INTERNAL COMPONENTS OF THE DISCHARGE HEADASSEMBLY, INCLUDING THE EXPLOSIVE CARTRIDGE. 2H74 4F4 F A49EU E6NE 20030602000892003060200089NM 2003 6 2 DL757030490 120030525A3222 AXLE BOEING757 757232 1384965NM NLG DAMAGED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27675DL 25980 ON TAXI OUT TO RUNWAY LT NOSE WHEEL ASSY BEARING AND OUTER RACE FAILED. REPLACED NLG AXLE AND WHEEL ASSEMBLY. 2L72 4F RTA2NM 20030602000962003060200096NM 2003 6 2 SWAA031188 120030528A3350100885 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS SECTION INOP IN AFT CABIN. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030602001102003060200110NM 2003 6 2 SWAA031178 120030523A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 178, WL 232. REMOVED AND REPLACED FRAME PER SRM. 2L72 4F RTA16WE 20030602001162003060200116NM 2003 6 2 SWAA031154 120030523A5313BAC1498 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE STRINGERS CORRODED (2 EA) BS 967 AT STR 26L AND BS 967 TO BS 977 AT STR 25L. REPAIRED STRINGERS PER SRM. 2L72 4F A16WE 20030602001382003060200138NM 2003 6 2 SWAA031149 120030521A551265C25727 SKIN BOEING737 7372H4 138448CNM TAIL CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C4 CHECK, FOUND 14 EA CRACKS AT RT HORIZONTAL STAB LOWER SKIN EMANATING FROM FASTENERS HOLES, BETWEEN STA 107 AND STA 173. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030602001442003060200144 2003 6 2 SWAA031132 420030521A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030602001472003060200147 2003 6 2 SWAA031135 420030521A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030602001482003060200148 2003 6 2 SWAA031136 420030519A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030602001522003060200152NM 2003 6 2 SWAA031140 120030520A53126516300 BULKHEAD BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 213 AND RBL 6.5. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030602001582003060200158NM 2003 6 2 VNAA0305014 120030521A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07462PS13727148 3084 THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT ROWS 3, 4, AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030602001622003060200162NM 2003 6 2 VNAA0305011 120030517A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07433JS1172029 3047 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 7 - 9 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030602001692003060200169EA 2003 6 2 A6WA200340063 120030430A5320 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOORFRAME DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 PREVIOUS PASSENGER DOOR SEALS STRIKER REPAIR IS DAMAGED, FS 310. REPAIRED DAMAGED AREA IAW BOMBARDIER INC REO 601R-52-11-008 REV B. (M) 2L72 4F RTA21EA 20030604000112003060400011NM 2003 6 4 AALA20030494 120030424A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21774AN 29581 DURING OVERNIGHT MAINTENANCE, FORWARD RIGHT FORWARD FACING LOWER EMERGENCY EXIT PATH LIGHT ON THE G3 GALLEY WALL INOPERATIVE. REPLACED FORWARD RIGHT FORWARD FACING LOWER EMERGENCY EXIT PATH LIGHT ON THE G3 GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030604000122003060400012NM 2003 6 4 USAASB03063 120030507A335020131A BATTERY PACK BOEING737 737301 1384611NM FWD CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US 23742 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE FORWARD RIGHT SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030529000732003052900073NE 2003 5 29 HEEA086515 120030521A243231999001 BATTERY SKRSKYS76 S76A 8143006NE MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03764P 760276 BATTERY DEAD. REPAIRED. 1G72 3U H1NE 20030529000892003052900089SW 2003 5 29 HEEA086663 120030522A243230703002 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 BATTERY DEAD. REPAIRED. 1G72 4U H4SW 20030530000322003053000032 2003 5 30 HEEA086538 420030522A3455066104701 TRANSCEIVER SKRSKYS76 S76A 8143006NE ADF INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 ADF TRANSCEIVER INOPERATIVE. IN SHOP REPAIR. 1G72 3U H1NE 20030602000082003060200008NM 2003 6 2 2003F00355 120030509A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM CARGO BAY MALFUNCTIONED A KPVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP13805WP 353 SMOKE WARNING LIGHT ON WHILE ON GROUND. TROUBLESHOT SYSTEM, FOUND TOP SMOKE DETECTOR TO BE FAULTY. DISCONNECTED CONNECTOR AND SECURED. DEFERRED PER MEL 26-8-1. PLACARD INSTALLED. CAT C 5/9/03, DUE 5/19/03. CLEARED MEL 26-8-1 SMOKE WARNING LIGHT ON BAGGAGE. REMOVED AND REPLACED BAGGAGE SMOKE DETECTOR CEILING, OPS CHECK GOOD IAW DHC 8MM 26-12-00 PAGE 201 PARA 1A. PLACARDS REMOVED 5/10/03 0400 HRS. (M) 2H72 4T RTA13NM 20030602001182003060200118 2003 6 2 SWAA031156 420030523A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030602001392003060200139NM 2003 6 2 SWAA031150 120030521A551265C25727 SKIN BOEING737 7372H4 138448CNM TAIL CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C4 CHECK, FOUND 4 EA CRACKS AT LT HORIZONTAL STAB LOWER SKIN EMANATING FROM FASTENERS HOLES, BETWEEN STA 124 AND STA 173. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030604000092003060400009NM 2003 6 4 AALA20030481 120030421A3397 CONNECTOR BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21329AA 22329 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25 RIGHT SIDE INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR UNDER SEAT 25A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030604000292003060400029EA 2003 6 4 A6WA200340061 120030505A2434 IDG CNDAIRCL600 CL6002B19 1900309EA RT GENERATOR UNDERSERVICED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31414ZW 7586 RT IDG CAUTION FOLLOWED BY RT GEN OFF LINE ON TAKEOFF SERVICED IDG. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030604000322003060400032SO 2003 6 4 SIMA200313201 120030507A3260852701 UPLOCK SWITCH EMB 135 EMB135LR 3260305SO NLG INOPERATIVE A SIMAO OTHER N FALSE WARNING APAPPROACH 1 SW21713AE 145249 BGR - FLT 4626 - CREW REPORTED THE NOSE LANDING GEAR DOOR OPENED UNCOMMANDED DURING DESCENT. AIRCRAFT LANDED WITH NO FURTHER INCIDENT REPORTED. MAINTENANCE FOUND AN INOPERATIVE UPLOCK PROXIMITY SWITCH. THE UPLOCK SWITCH WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030604000432003060400043SO 2003 6 4 SIMA200312702 120030430A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21709GB 145211 DURING AN IMBV INSPECTION, THE LEFT SECTION OF THE FORWARD FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 6 INCHES BY 3.5 INCHES SECTION OF THE LEFT SECTION OF THE FORWARD FLOORBEAM BY CUTOUT. FABRICATED A REPLACEMENT FORWARD FLOORBEAM CENTER SECTION AND FABRICATED ONE DOUBLER. REPAIR DONE IAW EMB 145 REPAIR STATEMENT IC2003-145/1380 PARA 1 PRINCIPLES OF EMB 145/1142 CHAPTERS 53, REV 21, 53-21-10 PARA 4 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030604000482003060400048NM 2003 6 4 UPS03640464 120030408A53207075T62 STIFFENER BOEING767 76734AF 1385212NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01304UP 27242 INSPECTION TYPE: C4, WHILE WORKING BS 246 FLOORBEAM INSPECTION IAW S/B767-53-0093 FOUND STIFFENER CRACKED AT BS 246. LBL40, WL 200. REMOVED CRACKED PART. REPAIRED BY FABRICATION AND INSTALLATION OF NE W PART PER S/B 767-53-0093, GOODRICH ER 032003 AND FAA 8110-3 FORM S IGNED 14APRIL2003 2L72 4F RTA1NM 20030604000562003060400056WP 2003 6 4 UPS03840471 120030331A53476015176 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, CABIN SEAT TRACK F CRACKED AT STA 1571. REMOVED AND REPLACED SEAT SECTION IAW DC8 SRM 53-2-3 AND UPS EO DC8- 5320-5167 2L74 4F RT4A25 20030604000642003060400064WP 2003 6 4 UPS03840479 120030407A57203645611U FITTING DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, NR 1 ALT AFT BOOST PUMP MOUNT FITTING IS CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D RECEIVED NEW FITTING P/ N 3645611U PO SP094626. LOCATED, DRILLED, AND DEBURRED IAW DC8 SRM 5 1-1-24. INSTALLED IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030604000822003060400082NM 2003 6 4 UPS03440496 120030412A5314 SUPPORT BRACKET BOEING747 747121 1384871NM KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1225 LBL 9. SUPPORT BRACKET REINSTALLED AS PER SRM 51-30-2 AND BRACKET REPLACED AS PER SRM 51-10-01 P.8 REFER NRC 6878. CORROSION BLEND OUT 0.040 X 1 X 1 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604000842003060400084NM 2003 6 4 UPS03440498 120030413A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:N/A M/D - BS 760 LBL 40 FLOORBEAM UPPER SURFACE FOUND CORRODED. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 3. CORROSION BLEND OUT 0.060 X 2 X 2 INCHES, EXCEED SRM LIMIT. 2L74 4F A20WE 20030604000962003060400096NM 2003 6 4 UPS03440510 120030412A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FWD CARGO COMPT - STA 840 STR - 45R TO 46R FRAME SHEAR TIE CORROSION CRACK REVEALED. FWD CARGO COMPT STA 840 S45R - S46R FRAME SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2L74 4F A20WE 20030604001002003060400100NM 2003 6 4 UPS03440515 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE DEFORMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 1800 RT BETWEEN STRINGER 20 - 22R FRAME FOUND DEFORMED. M/D BS 1800 RT BTN STR 20 AND STR 22 FRAME REPAIRED AS PER SRM 53-10-04 FIG 87. 2L74 4F A20WE 20030604001022003060400102NM 2003 6 4 UPS03440517 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 940 LT STR 24L FRAME FOUND CRACKED. BS 940 BETWEEN S24L TO S25L FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001172003060400117NM 2003 6 4 UPS03440532 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 960 FRAME CRACKED AT STR 9L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54. 2L74 4F A20WE 20030604001192003060400119NM 2003 6 4 UPS03440534 120030413A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 820 - 860 LBL 11 SEAT TRACK RT LIP FOUND CORRODED. BS 810 - 890 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. CORROSION BLEND OUT 0.050 X 1 X 10 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604001242003060400124NM 2003 6 4 UPS03440539 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2100, BET STR 25 - 26L FRAME WEB FOUND CRACK. M/D FX FRAME WEB REPAIRED AT BS 2100 BTN STR 25L AND STR 26L AS PER SRM 53-10-04 FIG 39. 2L74 4F A20WE 20030604001272003060400127NM 2003 6 4 UPS03440542 120030406A5711 SPAR BOEING747 747121 1384871NM NR 4 SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING UPPER SURFACE FRONT SPAR RABBET PANEL FOUND BULGE AT NR 4 SLAT O/B AREA AS MARKED. LT WING UPPER SURFACE FRONT SPAR REPAIRED AS RS R57-25-35006 AND ENGINEERING FILE NUMBER : 747-57-20040 AT NR 4 SLAT O/B AREA WS 1294. 2L74 4F A20WE 20030604001322003060400132NM 2003 6 4 UPS03440552 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C M/D - BS 920 LH STR - 24L FRAME FOUND CRACKED. BS 920 BETWEEN S24L TO S25L FRAME REPAIRED AS PER SRM 53-10-04 FIG.35. 2L74 4F A20WE 20030604001442003060400144NM 2003 6 4 UPS03440564 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 760, BET STR 14 - 15R FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R-53-22-35013 AND ENGINEERING FILE NUMBER 747-53-20132. 2L74 4F A20WE 20030604001542003060400154NM 2003 6 4 UPS03440574 120030410A5320 SUPPORT BRACKET BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, KEELBEAM PANEL SUPPORT ATT BRACKET FOUND SURFACE CORROSION AT STA 1285 TO STA 1286 RBL 8 TO RBL 9. CORROSION BLEND OUT ( 0.030 X 1 X 1 INCHES) BRACKET REPLACED AS PER SRM 51-10-01. 2L74 4F A20WE 20030604001562003060400156NM 2003 6 4 UPS03440576 120030412A575365B106331 RIB BOEING747 747121 1384871NM NR 2 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING, NR 2 VC FLAP I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NO.1, 2, 3 & 4 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030602000532003060200053WP 2003 6 2 CA030521003 220030518A73218978017 FUEL CONTROL SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP ENGINE MALFUNCTIONED W O OTHER WE INADEQUATE Q C VIBRATION/BUFFET TXTAXI/GRND HDL 1 CA (CAN) UPON STARTING OF ENG RPM WHICH SHOULD HAVE STABILIZED AT 70 PERCENT AT IDLE CONTINUED TO ACCELLERATE TO APPROXEMATLY 90-94 PERCENT BEFORE IT STABILIZED. ATTEMPTS TO REDUCE RPM USING ENG CONTROLS WERE UNSUCCESSFUL. ABOUT 30-40 SECONDS AFTER STABILIZING AT 90-94 PERCENT RPM BEGAN TO DECREASE ITSELF & EVENTUALLY STOPPED AT 70 PERCENT. ENG SHUTDOWN TO CHECK CONTROLS & RIGGING OF ENG WITH NO PROBLEMS FOUND. IN CONSULTING WITH PERIMETER'S TURBINE SHOP THEY SUSPECTED THAT UNDERSPEED FUEL GOVERNOR WAS STUCK & NOT LIMITING FUEL FOR A PROPER IDLE SPEED. ENG STARTED AGAIN & SAME PROBLEM OCCURED BUT RPM REDUCED BACK TO IDLE WITHIN ABOUT 20 SECONDS. FUEL CONTROL UNIT WAS REMOVED & REPLACED WHICH RECTIFIED PROBLEM. 2L72 4T4 TRTA8SW E4WE 20030602000592003060200059WP 2003 6 2 CA030425009 120030424A6710369A7339 SUPPORT HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL COLLECTIVE BROKEN W O OTHER F FLT CONT AFFECTED CRCRUISE 1 CA (CAN) PILOT HEARD A LOUD BANG AND SUCCESSFULLY LANDED WITHOUT INCIDENT. INVEST REVEALED THAT THE COLLECTIVE SUPPORT BRACKET WAS BROKEN. SUPPORT BRACKET WAS REPLACED WITH A 369N2650 AS PER MM. FURTHER INVEST INTO CAUSE REVEALED THAT PLUNGER IN SLEEVE OF COLLECTIVE BUNGEE ASSEMBLY WAS BINDING. A REVIEW OF MM REVEALED THAT THERE IS A LUBRICATION OF COLLECTIVE BUNGEE REQUIRED AT INSTALL BUT NO RECURRING LUBRICATION SPECIFIED EITHER IN MM. SERVICING. SEVERAL OTHER COLLECTIVE BUNGEES ON OTHER AIRCRAFT WERE INSPECTED AND FOUND TO BE DRY AND VERY WORN.AS THE MM IS NOT CLEAR ON THE INTERVAL OF LUBRICATION, 1G71 3U3 U H3WE E4CE 20030602000602003060200060WP 2003 6 2 CA030428001 120030421A35104019374 HOSE LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE OXYGEN SYS LEAKING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CREW REPORTED OXYGEN CYLINDER PRESSURE LOW ON ARRIVAL. DURING INVESTIGATION MAINTENANCE FOUND THE LP OXYGEN LINE LEAKING AT THE BOTTLE. LINE WAS REPLACED . SUSPECT DAMAGE WAS CAUSED DURING CYLINDER REPLACEMENT. 2L73 4F4 F A23WE E12EU 20030602000762003060200076NM 2003 6 2 AUS20030423 120030415A2697 CONNECTOR BOEING737 737400 138449ANM CFMINTCFM56 CFM563C 13802EU FIRE PROTECTION CONTAMINATED W O OTHER N FALSE WARNING CRCRUISE 1 AUS (AUS) NR 1 ENGINE FIRE DETECT/OVERHEAT FAULT LIGHT ILLUMINATED DURING FLIGHT. LOOP (A) FAULT LIGHT WAS INTERMITTENT AND LOOP (B) FAULT LIGHT WAS ON CONTINUOUSLY. THE CORE DETECTOR WIRING WAS INSPECTED AND CONNECTOR D1208 WAS FOUND CONTAMINATED. 2L72 4F4 FRTA16WE E21EU 20030602000992003060200099NM 2003 6 2 SWAA031191 120030527A5310672036 BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND RT OUTBD LOWER VERTICAL BEAM CRACKED AT BS 188, WL 203 TO WL 214 AT RBL 30. REPAIRED VERTICAL BEAM PER SRM. 2L72 4F RTA16WE 20030602001002003060200100NM 2003 6 2 SWAA031192 120030527A3260 WARNING LIGHT BOEING737 7377H4 1384404NM MLG MALFUNCTIONED A SWAAO OTHER N FALSE WARNING TOTAKEOFF 1 SW29410WN 27897 DURING TAKEOFF AFTER RAISING GEAR, THE RED NLG LIGHT FLICKERED. RECYCLED GEAR, LIGHT FLICKERED SEVERAL MORE TIMES AND EXTINGUISHED. C/W BITE CHECK, RESET FAULT, OPS CK GOOD PER FIM TASK. 2L72 4F RTA16WE 20030602001332003060200133 2003 6 2 SWAA031144 420030522A25651061323 BOTTLE BOEING737 7373H4 1384600NM ESCAPE SLIDE DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED EVACUATION SLIDE PER MM. 2L72 4F RTA16WE 20030602001512003060200151 2003 6 2 SWAA031139 420030520A256565C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINER HOOK BROKEN. REMOVED AND REPLACED RETAINER HOOK PER MM. 2L72 4F RTA16WE 20030602001632003060200163NM 2003 6 2 USAASB03058 120030501A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA19591US 23936 CLT - FLT 337 - PILOT REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 22 AND AT THE AFT RIGHT SERVICE DOOR ILLUMINATED DURING PUSHBACK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THAT SECTION OF EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030604000282003060400028NM 2003 6 4 USAASB03060 120030503A3610 CONTROL VALVE BOEING737 7373B7 1384580NM PRECOOLER FAILED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19391US 23313 AT FL330, NR 2 ENGINE BLEED TRIPPED. LT PACK WOULD NOT HOLD CABIN AT FL330. CREW INITIATED RAPID DESCENT TO FL180 WHERE CABIN PRESSURE STABILIZED. NR 2 ENGINE BLEED RESET WHILE PASSING THROUGH FL250. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT PIT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED ENGINE RUN FOR BLEED TRIP PROBLEM. NO BLEED TRIPS NOTED AND PRESSURE WAS NORMAL. REMOVED AND REPLACED NR 2 ENGINE PRECOOLER CONTROL VALVE SENSOR AND 450 DEGREE BLEED AIR OVERTEMP THERMOSTAT SENSOR AS PRECAUTIONARY. LEAK CHECK AND OPERATIONAL CHECK NORMAL. ACCOMPLISHED SINGLE PACK CONFIDENCE CHECK PER JOB PROCEDURE CARD. BOTH PACKS CHECK GOOD. (M) 2L72 4F RTA16WE 20030604000662003060400066WP 2003 6 4 UPS03840481 120030413A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C2, AT STA. 1723 CANTED FRAME, LONG.14L IS CRACKED. CUT OUT DAMAGED LONG. SECTION FABRICATED AND REPLACED LONGERON SECTION I.A.W. SRM. 53-2-03 FIG. 10 2L74 4F RT4A25 20030604000972003060400097NM 2003 6 4 UPS03440512 120030412A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FLOORBEAM UPPER STRUCTURE FOUND CORRODED. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 3. CORROSION BLEND OUT 0.050 X 1 X 1 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604001012003060400101NM 2003 6 4 UPS03440516 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 960 LT BET STR 23L TO 24L FRAME FOUND CRACKED. BS 960 BETWEEN S23L TO S24L FRAME REPAIRED AS PER SRM 53-10-04 FIG 4 . 2L74 4F A20WE 20030604001632003060400163NM 2003 6 4 UPS03440583 120030409A5312 BULKHEAD BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FX - LOWER FUSELAGE BULKHEAD ATTACH WEB FOUND CRACKED AT STA 1480 RBL 90 WL 120 ( AS MARKED). WEB REPAIRED AS PER SRM 51-40-02 FIG.1. 2L74 4F A20WE 20030604001782003060400178NM 2003 6 4 UPS03440598 120030412A575365B078861 RIB BOEING747 747121 1384871NM NR 10 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 10 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 3,4,5 & 6. (VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030604001862003060400186NM 2003 6 4 UPS03440607 120030414A5310 CREASE BEAM BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 980 S4-5L CREASE BEAM CRACKED. CREASE BEAM WEB REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030604001992003060400199 2003 6 4 ARWA20030406 420030428A22202099006010 SENSOR LKHEED1011 1011385115 5265015WP AOA FAILED A ARWAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19307GB 193U1131 STALL WARNING NR 1 CHANEL FAILED IN FLIGHT, CONTINOUS STICK SHAKER IN FLIGHT. DE-SELECTED NR 1 CHANEL AND RETURNED TO MIAMI AS ADVISED BY FLIGHT CONTROL. DUMPED FUEL 1508Z-1520Z DOWN TO LANDING WEIGHT. REMOVED AND REPLACED NR 1 ANGLE OF ATTACK SENSOR IAW MM 22-31-06; PERFORMED STALL WARNING TEST IAW MM 22-17-05, FOUND ALL SYSTEMS NORMAL. 2L73 4F A23WE 20030604002192003060400219EU 2003 6 4 XG3R086326 120030502A334010003 LIGHT UROCOPEC120 EC120B 8680987EU STROBE BROKEN W XG3RO OTHER O OTHER NRNOT REPORTED 1 FS0126LB 825 3514 LIGHT BROKEN, REPLACE WITH NEW PART. 1G72 3U NCR0001RD 20030604002262003060400226NM 2003 6 4 UPS03240640 120030417A5230 SKIN BOEING727 72722C 138400FNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, CRACK ON AFT CARGO DOOR INNER SKIN AT HOLE CUT OUT FOR BALANCE MECHANISM CABLE PULLEY. STOP DRILLED HOLE IAW SRM 51-10-1 REPAIR WAS THEN CARRIED OUT IAW SR M 51-40-2 REPROTECTED IAW SRM 51-10-2 2L73 4F A3WE 20030604002292003060400229NM 2003 6 4 UPS03440634 120030502A3232 ACTUATOR BOEING747 747123 1384873NM RT MLG DOOR INTERMITTENT A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01672UP 20324 DURING GEAR RETRACTION RED GEAR LIGHT AND RED DOOR LIGHT ILLUMINATED RE CYCLED NO HELP PREFORMED EMERGENCY PROCEDEURE I/A/W QRH-NO HELP R ETURNED TO BASE. F/E PANEL SHOWED RT WING DOOR OPEN IN BOTH PRI + ALT. RESEQUENCE NO HELP. REPLACED RT WING GEAR DOOR ACTUATOR (PRECAUTIONARY) FOR INTERMITENT GEAR DOOR LIGHT. GARY ABBOTT 00263 5-3-03 / CK'D REQ OF RH WING GEAR DOOR EQUENCE VLV PER MM 32-32-02 OPS NORMAL 99432 5-3-03 ONT/ SEE L OG 059864 ITEM 1 FOR CONTINUATION. 2L74 4F A20WE 20030604002352003060400235SO 2003 6 4 LR7A03044 120030504A531233914912L SPLICE LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 623 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WW FS 617 AFT BULKHEAD LOWER PANEL SPLICE CRACKED AT OUTBD END, LBL 80, WL 150. REPLACED LOWER SPLICE IAW LOCKHEED DWG 339149. NR 0031. 2H74 4T A1SO 20030604002382003060400238EU 2003 6 4 CX7A194J40 120030430A26121734362450 SENSOR SAAB SF340 340B 7860101EU TAILPIPE MALFUNCTIONED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03303CE 340B194 EXPERIENCED TAILPIPE HOT INDICATION DURING TAKEOFF ROLL ON RIGHT ENGINE. 2L72 4T RTA52EU 20030605000032003060500003NM 2003 6 5 AUS20030428 120030417A29127592113101 FILTER BOEING737 7377BX 13844D2NM GE CFM56 CFM56* 13802NE HYD SYSTEM CONTAMINATED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) HYDRAULIC RESERVOIR PRESSURISATION MODULE AIR FILTER CONTAMINATED. 2L72 4F4 FRTA16WE E2GL 20030605000082003060500008NM 2003 6 5 AUS20030433 120030424A29127592113101 FILTER BOEING737 73776N 13844CHNM GE CFM56 CFM567B24 NE HYD SYSTEM CONTAMINATED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) HYDRAULIC SYSTEM RESERVOIR CHARGE FILTER HAD EVIDENCE OF MOISTURE IN THE FILTER HOUSING. 2L72 4F4 FRTA16WE E00055EN 20030605000302003060500030NE 2003 6 5 SIMA200304301 220030208A72003SAH11773AZ RELAY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE INOPERATIVE A SIMAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 SW21386AE 340B386 DFW - FLT 3572 - CREW REPORTED THE RIGHT ENGINE FAILED ON FINAL APPROACH TO DFW. DURING TROUBLESHOOTING AS PER A SAAB MX FOUND RELAY 68KF TO BE AT FAULT. RELAY WAS REPLACED AND OPERATIONAL CHECK WERE COMPLIED WITH. AIRCRAFT WAS RELEASED FOR FCF. CHECK FLIGHT WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20030605000482003060500048NM 2003 6 5 USAA030052 120030510A5320 ANGLE BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 FOUND 4 CRACKS .125 INCH, SCREW HOLES CRACKS, BS 1200-1220 AT BL 0. FABRICATED NEW ANGLE PER SRM 53-60-51 AND SRM 53-10-2. (M) 2L72 4F RTA2NM 20030602001052003060200105 2003 6 2 SWAA031173 420030527A2565 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030602001222003060200122NM 2003 6 2 SWAA031160 120030523A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030604000022003060400002EU 2003 6 4 SIMA200313209 120030508A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21356AE 340B356 LAX - FLT 3255 - DURING PREFLIGHT, CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT 22LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030604000072003060400007NM 2003 6 4 AALA20030468 120030418A3397 CONNECTOR BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139364 24045 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BY 1L AND 1R DOOR INOPERATIVE. SECURED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030604000232003060400023GL 2003 6 4 SIMA200312602 220030503A720023072309 CARBON SEAL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A SIMAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21723AE 145288 CREW REPORTED FOUL ODOR IN COCKPIT IN CABIN DURING FLIGHT. MAINTENANCE FOUND THE LT ENGINE LEAKING OIL FROM SPINNER. THE ZERO CARBON SEAL WAS REPLACED IAW ENGINE MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20030604001142003060400114NM 2003 6 4 UPS03440529 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 1640 S-13L FRAME CRACKED. M/D FRAME REPAIRED AT BS 1640 BTN STR 12L AND STR 14L AS PER SRM 51-40-03 FIG 2. 2L74 4F A20WE 20030604001462003060400146NM 2003 6 4 UPS03440566 120030413A5313 LONGERON BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 1002-1004- S2R, STR END FOUND CRACK. BS 1002 - 1004 S2R STRINGER REPAIRED AS PER HX RS R53-21-35017 & UPS RA 747-53-20138. 2L74 4F A20WE 20030604001912003060400191NM 2003 6 4 UPS03440612 120030406A5414 SKIN BOEING747 747121 1384871NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, NR 3 PYLON EXTERIOR SURFACE SKIN NAC STA 218.9 LHS 1EA RIVET HOLE UPPER AND LOWER EDGE SUSPECT CRACKS ARE FOUND AS MARKED. NR 3 PYLN EXTERIOR SKIN REPAIRED AT I/B SIDE AS PER RS R54-50-35005 AND UPS EO B747-5410-18686-A DVI THE REPAIRED AREA FOR CRACKS OR DAMAGE AT 18 MOUTHS INTERVAL. 2L74 4F A20WE 20030604001982003060400198WP 2003 6 4 ARWA20030405 120030427A5243 ACCESS PANEL LKHEED1011 1011385115 5265015WP LEAKING A ARWAA UNSCHED LANDING O OTHER CLCLIMB 1 SO19307GB 193U1131 WITH BOTH OUTFLOW VALVES CLOSED, MAX PRESSURE DIFFERENTIAL 4.5 INCHES CABIN CLIMBING. CHECK FOR PNEU LEAK. RETURNED TO MIA. SECURED INNER PANEL ON C-2 FOR HTE UNLOCK ACTUATOR ACCESS. AIRCRAFT WILL HOLD PRESSURATION OK FOR SERVICE IAW MM # 21-31-00, PAGE 122. 2L73 4F A23WE 20030604002202003060400220 2003 6 4 BAQA086232 420030422A34215040017907 INDICATOR BEECH 90 C90 1152913CE ATTUTUDE MALFUNCTIONED W BAQAO OTHER O OTHER NRNOT REPORTED 1 FS0190LF 44 LJ852 ATTITUDE INDICATOR DRIFTS SIDE TO SIDE. REPLACED WITH SERVICEABLE UNIT. 1L72 3T 3A20 20030604002282003060400228NM 2003 6 4 UPS03240642 120030414A5350 RADOME BOEING727 72722C 138400FNM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, RADOME FAILED MOISTURE CHECK. RADOME REPLACED IAW MM 53-15-00. RESISTANCE CHECK CARRIED OUT ON RADOME IAW MM 53-15-00. CHECK FOUND TO BE SATISFACTORY 2L73 4F A3WE 20030605000262003060500026SO 2003 6 5 SIMA200302107 120030101A532014522459003 RAMP EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 ABI - THIS IS LEVEL 2 FINDING ON CRIC NR 29272, FOUND DURING AN IMBV INSPECTION, GALLEY CENTER BEAM RAMP CORRODED. REMOVED AND INSTALLED SERVICEABLE BEAM RAMP IAW EMB 135 SRM 51-40-02 AND 51-40-03. (M) 2L72 4F RTT00011AT 20030605000392003060500039NM 2003 6 5 AMTA200300665 120030518A3350 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11523AT 30232 FLOOR TRACK EGRESS LIGHTS INOPERATIVE AT ROW 10. RECONNECTED WIRES ON LIGHT ASSEMBLY, OPS NORMAL. (M) 2L72 4F RTA2NM 20030605000552003060500055EU 2003 6 5 NXT2003F00002 120030326A5302109037305105 RIB AGUSTAA109 A109E 0260119EU PWA PW206 PW206B 0 NE VERTICAL FIN CRACKED E NXTAK NONE O OTHER ININSP/MAINT 1 SW19144CF293 11144 PCEBC0321 A CRACK WAS FOUND DURING A 300 HOUR INSPECTION OF THE VERTICAL FIN. THE CRACK WAS FOUND ON THE RIB AT APPROX. WL 235.2 MM, STA 9725.0 MM, AND RAN FROM STA 9623.4 MM TO 98266 MM. THE MANUFACTURER WAS CONTACTED FOR INSTRUCTIONS ON SERVICEABILITY. A LETTER FROM ENGINEERING PERMITTED THE AIRCRAFT TO BE FLOWN AN AUDITIONAL 100 HOURS PROVIDED DAILY AND 25 HOUR INSPECTIONS WERE PERFORMED. 1G72 3U3 URTH7EU E42NE 20030605000732003060500073NM 2003 6 5 MEX2003149 120030429A2910S271N5013 SHUTOFF VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE HYD SYSTEM FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23801AM 25624 AIRCRAFT SUSPENDS TAKE OFF DUE TO EICAS (L FLT CONT HYD) MESSAGE. THE HYDRAULIC SHUTOFF VALVE WAS VERIFIED AND IT WAS CORRECT. FIM PROCEDURE WAS ACCOMPLISHED AND NON FAILURE INDICATION WAS DETECTED. DURING OVERNIGHT SERVICE THE HYDRAULIC SHUTOFF VALVE WAS REPLACED IAW MM, TEST OK. 2L72 4F4 FRTA2NM E17NE 20030605000882003060500088EU 2003 6 5 GXP2003F00001 120030424A2131 CONTROLLER AMD FALC20FALCOND 2720304EU GE CF700 CF700* 30010NE CABIN PRESSURE MALFUNCTIONED E GXPAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL23618GA 211 AIRCRAFT RETURNED BACK TO JVY (IN) AFTER TAKEOFF DUE TO PRESSURIZATION, INOPERATIVE. AIRCRAFT DOWN DUE TO PARTS ON ORDER. 2L72 4F4 F A7EU E7EA 20030605000972003060500097WP 2003 6 5 UPS03840689 120030513A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 ON DEPARTURE THE EMERGENCY EXIT LIGHTS WERE DEAD, FOUND BATTERY PACK POWER LOW AFTER TIME OF CHARGER. NEED BATTERY PACK REPLACED. REMOVED & REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-60-00. LIGHT OPS CK GOOD. 2L74 4F RT4A25 20030605000992003060500099CE 2003 6 5 GVR2003F00002 120030429A2510551900921 SEAT CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE CABIN CRACKED B GVRRO OTHER O OTHER NRNOT REPORTED 1 CE05390AJ 5500326 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW ST01042WI STRUCTURAL SEAT REPAIR. 1L72 4F4 F A22CE E1NE 20030605001102003060500110WP 2003 6 5 IXXA0300033O 120030506A2752 WARNING HORN DOUG DC8 DC862 3021970WP TE FLAPS FALSE ACTIVATIONA IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11799AL727462470 45922335 ON TAKE OF, FROM TOL TO WRI, WITH FLAPS RETRACTING, TAKE OFF WARNING HORN SOUNDS UNTIL PTC IS PLACED IN NORMAL. CREW DID AN AIR TURN AROUND TO TOL. MAINTENANCE PERFORMED A TEST OF FLAP TAKEOFF WARNING SWITCH AND ALL OPERATIONAL CHECKS ARE GOOD AT THIS TIME IN ACCORDANCE WITH DOUGLAS DC-8 MAINTENANCE MANUAL. 2L74 4F 4A25 20030605001152003060500115NM 2003 6 5 UPS03240693 120030514A3350 BATTERY BOEING727 72721C 138400MNM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 COCKPIT DOOR EMERG LT INOPERATIVE. R/R BATTERIES P/N S106. IAW MM 3307. OPS CK OKAY. 2L73 4F A3WE 20030605001212003060500121NE 2003 6 5 MEX2003141 220030424A7200 WARNING LIGHT DOUG MD80 MD83 3023681NM PWA JT8 JT8D NE LT ENGINE ILLUMINATED W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23946AS 49658 AIRCRAFT RETURN TO PLATFORM, BECAUSE OF OSCILATION OF 0.08 IN LEFT ENGINE EPR INDICATOR. THE TX EPR WAS REPLACED IAW MM, TEST CORRECT. 2L72 4F4 FRT E2EA 20030605001222003060500122WP 2003 6 5 IXXA0300035O 120030516A2797 WIRE DOUG DC8 DC871F 302199DWP RUDDER CHAFED A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11823BX839412111 46064 ON CLIMB OUT FROM TOL TO ATL CREW REPORTED RUDDER MANUAL REVERSION LIGHT CAME ON. THE CREW REPORTED THAT THE RUDDER WAS POWERED BUT THE LIGHT WAS STAYING ON. CREW RETURNED TO TOL. MAINTENANCE VERIFIED HYDRAULIC PRESSURE AND QUANTITY ARE OKAY. MAINTENANCE FOUND BROKEN WIRE AT MANUEL REVERSION SWITCH, AND REPAIRED WIRE AT REVERSION SWITCH IN ACCORDANCE WITH DOUGLAS DC-8 MAINTENANCE MANUEL. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030605001312003060500131NM 2003 6 5 MEX2003109 120030401A2720 GEARBOX DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE HORIZONTAL STAB INOPERATIVE W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23169PL 53175 AIRCRAFT ARRIVED WITH REPORT PRIMARY HORIZONTAL STABILIZER WITHOUT MOVEMENT, IT WAS NECESSARY TO COMPENSATE WITH ELEVATOR DURING FINAL APPROACH. THE GEARBOX ASSEMBLY TRIM AND ALTERNATE ENGINE WERE REPLACED IAW MM AND RELAY LONGITUDINAL TRIM WAS REPLACED IAW MM, TESTS CORRECT. 2L72 4F4 FRTA6WE E2EA 20030605001342003060500134SO 2003 6 5 CA030318006 120030318A76032489418 THROTTLE CABLE PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA MCAULY3DF36CB3DF36C526 GL LT ENGINE SEIZED W E ENGINE SHUTDOWN E VIBRATION/BUFFET LDLANDING 1 CA (CAN) LT THROTTLE CABLE ASSEMBLY WAS SEIZED AND FROZEN WITH ICE, ON THE WING BETWEEN THE FUSELAGE. 1L72 3O3 O A20SO E14EA 5 C 20030605001422003060500142EA 2003 6 5 SWIA200311968 120030510A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER LF NO TEST FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07588SW5629 5629 7069 THE OUTBOARD GROUND SPOILERS FAULT DURING TEST. REMOVED AND REPLACED NR 1 SECU IAW CRJ AMM 27-61-05. PERFORMED OPS CHECK IAW CRJ AMM 27-61-05 AND 27-64-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20030605001462003060500146 2003 6 5 SWIA200311972 420030510A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07442SW3867 3867 7609 BEFORE PUSH BACK, NR 1 YD INOP STATUS MESSAGE CAME ON. REPLACED NR 1 YAW DAMPER ACTUATOR WITH SERVICEABLE UNIT IAW MM 22-22-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20030605001482003060500148SO 2003 6 5 SWIA200311974 120030505A2750 CONTROL HANDLE EMB 120 EMB120ER 3260203SO FLAP CONTROL OBSTRUCTED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07217SW 120286 FLAPS WILL NOT GO TO THE 45 DEGREE POSITION. COMMAND BARS SHOW CORRECTLY, BUT THE FLAPS WILL NOT GO PAST 25 DEGREES. REMOVED DEBRIS OBSTRUCTING FLAP HANDLE MOVEMENT TO 45 DEGREES. CYCLED FLAPS. OPS CHECK GOOD, NO DEFECTS NOTED. 2L72 4T RTA31SO 20030605001502003060500150NM 2003 6 5 S03227021 120030503A2750 DRIVE LINK BOEING747 747200 1384847NM PWA JT9 JT9D7R4G2 52054NE TE FLAPS LOOSE W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 22299 DAILY CHECK FOUND T/E FLAP NR 7 FAIRING SIDEOLAY. CHECK FOUND FIXED DRIVE LINK ATTACHMENT FITTING LOOSEN ON NR 7 T/E FLAP TRACK. IAW AMM 27-51-45 T/E FLAP NR7 TRACK FAIRING B ATTACHMENT BOLTS RETORQUE AND FITTING SEALANT. REMOVED ATTACHMENT FITTING AND SENT TO SHOP FOR CLOSE VISUAL INSPECTIN ON 05/09/2003. THE CONDITION OF ATTACHMENT FITTING IS NORMAL, BUT THE CORROSION IN NR 7 TRACK WAS FOUND. EON 742-57-632472-021 WAS ISSUED TO REPAIR THE DAMAGE TRACK. 2L74 4F4 FRTA20WE E3NE 20030605001612003060500161NM 2003 6 5 F3LA200300119 120030516A2611PPA110100 SMOKE DETECTOR AIRBUSA319 A319111 3930336NM AFT CARGO BAY FAILED A F3LAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03904FR 273 1579 AIR TURN BACK. FLIGHT CREW REPORTED AFT CARGO SMOKE/HEAT ECAM WARNING. NO SMELL OF SMOKE, CARGO FLOOR WAS NOT HOT. DISCHARGED AFT CARGO BOTTLE. NOTE: THIS WAS A WARNING INDICATION ONLY, NOT AN ACTUAL FIRE. TROUBLESHOT SMOKE DETECTION SYSTEM AND REPLACED SENSOR. REPLACED AFT CARGO EXTINGUISHER BOTTLE. SYSTEM TESTED OKAY. 2L72 4F RTA28NM 20030605001662003060500166WP 2003 6 5 2003FA0000504 120030410A6230 WASHER HUGHES369 369D 4470706WP M/R MAST WRONG PART B EOORO OTHER O OTHER NRNOT REPORTED 1 AL03CGPHC 180257D INCORRECT WASHERS, DAMAGED BOLD RADIUS. 1G71 3U H3WE 20030605001692003060500169CE 2003 6 5 AW42003F00000 120030428A561010138402515 WINDSHIELD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A60 52043NE COCKPIT CRACKED E AW4RO OTHER O OTHER NRNOT REPORTED 1 WP1131WC BB465 FOLLOWING DEPARTURE, PILOT`S WINDSHIELD INNER GLASS PANE CRACKED. AIRCRAFT RETURNED TO DEPARTURE WHERE WINDSHIELD WAS REPLACED. 1L72 4T4 T A24CE E4EA 20030606000052003060600005NM 2003 6 6 03139417 120030517A3350 LIGHT DORNERDO32 DO328300 NM ROWS 4-6 INTERMITTENT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27417FJ DURING PREFLIGHT INSPECTION, CREW REPORTED THAT EMERGENCY TRACK LIGHTING - ROWS 4 - 6 WERE INOPERABLE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030606000142003060600014WP 2003 6 6 03FDEA00760 120030519A5753 HINGE DOUG MD10 MD1010F WP TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 S 14 C/W E.A.8-5740-70390. WINGS-RT INBD FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 05/17/03. COMPLIED WITH E.A.8-5740-70390.WINGS R/H INBD FLAP HINGE ASSY CORROSION REWORK. 2L73 4F RTA22WE 20030604000672003060400067WP 2003 6 4 UPS03840482 120030416A572097532978 ANGLE DOUG DC8 DC873F 302199FWP RT WING L/E CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, RT WING CENTER LE. SUPPORT ANGLE AT XS 520 IS CRACKED. REMOVED,FABRICATED AND REPLACED ANGLE IAW DWG. 9753297,AND SRM. 51-1-20D 2L74 4F RT4A25 20030604001052003060400105NM 2003 6 4 UPS03440520 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 600 LT STR 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001092003060400109NM 2003 6 4 UPS03440524 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 600 LT STR 19L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35 AT BS 600 BETWEEN STR 18L - 20L. 2L74 4F A20WE 20030604001392003060400139NM 2003 6 4 UPS03440559 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 920 BET S24-25R FRAME FOUND CRACKED. REF NRC 7377 FRAME REPAIRED AS PER SRM 53-10-04 FIG.35. 2L74 4F A20WE 20030604001712003060400171NM 2003 6 4 UPS03440591 120030412A575365B078781 RIB BOEING747 747121 1384871NM NR 8 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 8 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2,3,4,6,7 & 8 (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-5740-18607-A. 2L74 4F A20WE 20030604002032003060400203NM 2003 6 4 UPS03440627 120030414A53157075T6511 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, U/D - FLOORBEAM UPPER STRUCTURE FOUND CORROSION AT BS 340 BL 0 - LBL 40 FLOORBEAM UPPER STRUCTURE REPAIRED AS PER SRM 53-10-07 FIG.23 CORROSION BLEND OUT SIZE 0.038 X 1 X 3 INCHES. 2L74 4F A20WE 20030604002072003060400207WP 2003 6 4 UPS03840615 120030412A572098874277 STIFFENER DOUG DC8 DC873F 302199FWP RT WING TE. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, RIGHT WHEEL WELL AT STA. XW 5 AFT T-CAP STRUT FOR TE. IS CRACKED REMOVED,FABRICATED AND REPLACED STIFFENER I.A.W. 9887427,AND SRM. 51-1-20D 2L74 4F RT4A25 20030604002162003060400216 2003 6 4 BAQA086293 420030430A3421 LIGHT UROCOPEC135 EC135T1 5620026EU INDICATOR INOPERATIVE W BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01118WS1579 6561 0089 INDICATOR LIGHTING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030605000442003060500044CE 2003 6 5 2003F00359 120030520A2720 LIMITER CESSNA750 750 2076810CE RUDDER FAILED A UG8AO OTHER J WARNING INDICATION ININSP/MAINT 1 GL235116 7500019 DURING PILOT'S PREFLIGHT, WITH APU RUNNING, THE 'RUDDER LIMIT FAIL' RED CAS MESSAGE ANNUNCIATED. ANOTHER AIRCRAT WAS UTILIZED FOR THE TRIP. THE RUDDER LIMITER FAILED TO ACTUATE DUE TO A FAULT IN THE ELECTRICAL COMPONENTS OF THE SYSTEM. AIRCRAFT WAS DE-POWERED AND RESET. NO FAULTS WERE NOTED WHEN POWERED UP A SECOND TIME. NO ACTIVE FAULTS WERE NOTED IN IMT. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L72 4J RTT00007WI 20030606000342003060600034WP 2003 6 6 ABXA030145 120030514A2760 CONTROL CABLE DOUG DC8 DC863 302198AWP SPOILER BROKEN A ABXAO OTHER O OTHER CRCRUISE 1 GL23818AX 46075 SPOILER CABLE S-23 BROKEN IN LT WHEEL WELL. REPLACED CABLES S-23 AND S-24. COMPLIED WITH SPOILER ADJ/TEST IAW WORK PACK 60172912. PERFORMED VISUAL INSPECTION OF SPOILER HYDRAULIC CONTROL LIMIT SWITCH CONNECTOR, P1-1036. FOUND CONNECTOR AND WIRING NEAR CONNECTOR DEGRADED. REPLACED P1-1036 AND SPLICED IN NEW SECTION OF WIRING IAW DC-8 WDM 27-62-01. OPS CHECKED ON ADJ/TEST. 2L74 4F 4A25 20030606000442003060600044NE 2003 6 6 00091 220030515A7200 ENGINE LEAR 24 24B 5170306CE GE CJ610 CJ6106 30006NE RIGHT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05233TW 24B221 251210A AIRCRAFT DEPARTED ADS DURING CLIMB TO FL430 RH ENGINE FLAMED OUT, ENGINE RELET AND AIRCRAFT LANDED AT LRD, DURING POST FLIGHT INSPECTION NO EVIDENCE OF FOD DAMAGE OR LEAKS FOUND. AIRCRAFT ROUTED TO ADS FOR INSPECTION MAINTENANCE TIGHTENED P3 LINE TO FUEL CONTROL AND PERFORMED ALL GROUND CKS PER GE M/M SEI-186 72-00 PAGE 139 AND FIGURE 101. AIRCRAFT RETURNED TO SERVICE. 2L72 4J4 J A10CE 1E16 20030606000482003060600048CE 2003 6 6 NE52003F00001 120030515A3710442CW PUMP CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 1 VACUUM INOPERATIVE B NE5RO OTHER O OTHER NRNOT REPORTED 1 GL13596DM 43 402C0255 VACUUM PUMP INOPERATIVE. 1L72 3O3 O A7CE E8CE 20030606000662003060600066WP 2003 6 6 03FDEA00784 120030520A5710 HINGE DOUG DC10 DC1010 3022110WP LT WING TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 S 26 COMPLY WITH E.A.8-5740-70391. WINGS LT I/B FLAP HINGE ASSY ATTACH LUG REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740-70391 2L73 4F A22WE 20030606000712003060600071EU 2003 6 6 03FDEA00778 120030520A2920 RAM AIR TURB AIRBUS300 A300B4605R 3930308EU HYD SYSTEM INOPERATIVE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25657FE 748 WHILE PERFORMING RAT EXTENSION, COULD NOT DEPLOY RAT WITH CONTROL HANDLES, BOTH CONTROL HANDLES IN FLIGHT COMPARTMENT. TROUBLESHOT PER A300-600 AMM 29-25-00-5, NO DEFECTS NOTED. OPS CK GOOD. 2L72 4F RTA35EU 20030606000822003060600082NM 2003 6 6 03FDEA00767 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000862003060600086NM 2003 6 6 03FDEA00763 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030609000082003060900008SO 2003 6 9 SWIA200311975 120030518A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07188SW7365 2864 120039 CREW REPORTS THE LEFT OUTBOARD FLAP IS SLOW DEPLOYING TO 45 DEGREES. REMOVED FAULTY FLAP ACTUATOR ON LEFT OUTBOARD FLAP AND REPLACED WITH A SERVICEABLE UNIT AS REQUIRED BY EMB MM 27-50-09. OPS CHECK GOOD. NO LEAKS NOTED. 2L72 4T RTA31SO 20030609000262003060900026SO 2003 6 9 C2XA03TY073 120030520A532014521718003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 DURING A SCHEDULED INSPECTION THE LOWER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE LOWER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030609000272003060900027SO 2003 6 9 C2XA03TY074 120030521A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713903 145479 DURING A SCHEDULED INSPECTION THE CENTER RAMP ANGLE WAS FOUND TO CORRODED IN SEVERAL AREAS AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030609000342003060900034NM 2003 6 9 03FDEA00787 120030521A5315 FLOORBEAM BOEING727 727100 1384036NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON FLOORBEAM AT STA 312 APPROX RBL 18 AT WL 208.1 IN LAVATORY AREA. REMOVED, FABRICATED REPAIR PARTS AND INSTALLED IAW BOEING DRAWING 65-17593 AND BOEING 727-100 SRM 51-40-4 AND 51-30-2 2L73 4F RTA3WE 20030609000362003060900036NM 2003 6 9 03FDEA00785 120030513A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE CORRODED. R/R PER EA 1-5750-69247. 2L73 4F RTA22WE 20030609000402003060900040NM 2003 6 9 C1HA200396012 120030520A5347 SEAT TRACK BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 AFT CABIN SEAT TRACK RBL 45 HAS NUMEROUS AREAS OF PITTING CORROSION BETWEEN BS 955F AND 1070 2L73 4F RTA3WE 20030609000452003060900045NM 2003 6 9 C1HA200396010 120030520A5347 SEAT TRACK BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 PITTING CORROSION AND GOUGING ON NR 3 SEAT TRACK AT RBL 22 BETWEEN BS 690 & 740. 2L73 4F RTA3WE 20030609000522003060900052EU 2003 6 9 MALA030273 120030517A3520 OXYGEN MASK SAAB SF340 340B 7860101EU CABIN MISSING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15454XJ 340B454 PAX 02 MASK IS MISSING. MAINTENANCE INSTALLED PAX O2 MASK.A/C OK FOR SERV.P/N 801808-02 2L72 4T RTA52EU 20030609000592003060900059NM 2003 6 9 QXEA0300644 120030521A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM ZONE 400 MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09346PH 477 SEA ON FLIGHT 2239 ABORTED TAKEOFF DUE TO DURING TAKEOFF ROLL ADDED POWER AND AUTOFEATHER DID NOT ARM. THIS SDR IS AWAITING FURTHER INFORMATION. 2H72 4T RTA13NM 20030609000662003060900066SO 2003 6 9 SWIA200311989 120030520A3397 WIRE EMB 120 EMB120ER 3260203SO EXIT SIGN LOOSE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07234SW 120308 EXIT SIGN ON SEAT 1 C&B OUT.SECURED LOOSE WIRE CONNECTION ON EXIT SIGN AT SEAT 1 CB. OPS CHECK GOOD. 2L72 4T RTA31SO 20030609000692003060900069EA 2003 6 9 QXEA0300621 120030517A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 BURN MARK ON SKIN .2 INCHES BELOW BOTTOM EDGE OF ADG DOOR, 9 INCHES AFT OF FS169. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000792003060900079EA 2003 6 9 QXEA0300631 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 13R, 1 INCH AFT OF FS501. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000842003060900084EA 2003 6 9 QXEA0300637 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS693, 4 INCHES BELOW STRINGER 8R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-03, PG 1-8. 2L72 4F RTA21EA 20030604001852003060400185NM 2003 6 4 UPS03440605 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 540 LT STR 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R53-22-35011 REFER NRC FF76313 FOR DETAIL. AND ENGR FILE NBR 747-53-20135. 2L74 4F A20WE 20030604001892003060400189NM 2003 6 4 UPS03440610 120030411A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2120 BET STR 25 - 26L FRAME WEB FOUND CRACK. M/D FX FRAME WEB REPAIRED AT BS 2120 BTN STR 25L AND STR 26L AS PER SRM 53-10-04 FIG 39. 2L74 4F A20WE 20030604002222003060400222EU 2003 6 4 BAQA086304 120030430A6330L633M2010101 MOUNT UROCOPEC135 EC135P1 8680990EU GEARBOX LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 FS01577LF468 0140 GEARBOX MOUNT LEAKING. PLUNGER RECESSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030605000212003060500021NM 2003 6 5 UPS03240654 120030414A5320 WEB BOEING727 72722C 138400FNM BS WL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, NOSE WHEEL WELL LT SIDE AT STA 992 WL 140 TWO SMALL CRACKS ON HORIZONTAL WEB. HORIZONTAL WEB REMOVED & REPLACED IAW SRM 51-20-01 & 51-30-02 2L73 4F A3WE 20030605001002003060500100CE 2003 6 5 GVR2003F00003 120030505A2510551900921 SEAT CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE CABIN CRACKED B GVRRO OTHER O OTHER NRNOT REPORTED 1 CE0537MH 5500153 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. ALSO PREVIOUS INAPPROPRIATE REPAIR. SOMEONE PUT A GUSSET IN AREA MARKED 2. CHAIR WAS REPAIRED IAW ST01042WI STRUCTURAL SEAT REPAIR. 1L72 4F4 F A22CE E1NE 20030605001702003060500170NE 2003 6 5 GLBA2003064 220030518A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT & RT MALFUNCTIONED A GLBAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 NM03219GL UE219 BOTH ENGINE WILL NOT MAKE TAKEOFF POWER, REMOVED LT PT STATOR. 2L72 4T4 TRTA24CE E26NE 20030606000032003060600003EU 2003 6 6 03139316 120030517A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27316UE 41055 DURING MAINTENANCE INSPECTION, EMERGENCY FLOOR TRACK LIGHTS AT ROWS 6B/C WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY LAMP ON EXIT ROW, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTA41NM 20030606000582003060600058EA 2003 6 6 COMA0360242 120030519A3020601970977 VALVE CNDAIRCL600 CL6002B19 1900309EA LEFT ENGINE DEFECTIVE A COMAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO01781CA9661 7312 FLIGHT 5485 RECEIVED A LEFT ENGINE COWL ANTI-ICE CAUTION DURING TAKE OFF ROLL, AIRCRAFT RETURNED TO THE GATE. REPLACED THE LEFT ENGINE ANTI-ICE VALVE. 2L72 4F RTA21EA 20030609000352003060900035WP 2003 6 9 03FDEA00738 120030516A3260D103200103 PROXIMITY SENSOR DOUG DC10 DC1030 3023501WP ZONE 700 INOPERATIVE A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25319FE3997116862 47820 UPON GEAR RETRACTION AFTER DEPARTURE, FRONT DISPLAY (F/O) LT MAIN GEAR LIGHT REMAINED RED, ALL OTHERS EXTINGUISHED. RECYCLED GEAR IAW RED TAB PROCEDURE- GEAR RETRACTED NORMALLY; ALL LIGHTS EXTINGUISHED. R/R PROX BOX. 2L73 4F A22WE 20030609000942003060900094NM 2003 6 9 AWXA200300575 120030521A3397BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 19 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 DURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14 AND 19 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 14 LT, AND REPAIRED A BROKEN WIRE AT SEAT ROW 19 LT. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. PART NAME; LIGHT ASSEMBLY, MFG; GRIMES, P/N; 10-1272-1, LOC; SEAT ROW 14 LT. 2L72 4F RTA16WE 20030609000982003060900098SO 2003 6 9 C2XA03SH140 120030523A531014522461007 DOUBLER EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV-DURING C-CHECK THE DOUBLER AT FRAME 17 STRINGER 17R WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030609001002003060900100SO 2003 6 9 C2XA03SH142 120030523A531014522460013 BUTT STRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030609001052003060900105SO 2003 6 9 C2XA03SH147 120030523A531014522226003 BUTTSTRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030609001092003060900109NE 2003 6 9 WRNA200300011 220030521A72507476604 PRESSURE SWITCH LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 3 ENGINE LEAKING A WRNAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05311EA1974 1974 193A1012 10414 DURING CLIMB/CRUISE FULL FIRE INDICATION ON ENG NR 3, LOOP A&B ON, FIRE HANDLE ON, FIRE BELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATIONS OFF IMMEDIATELY AFTER ENGINE SHUTDOWN. FIRE BOTTLE NOT FIRED. APPROX 8800 GALS. OF FUEL DUMPED. A/C RETURNED TO FIELD, LANDED NORMAL. REPOSITIONED V BAND COUPLING AT HP SEAL, NR 3 ENG. IAW 20-36-01. REMOVED AND REPLACED HP OVERPRESSURE SWITCH IAW 36-11-44. RAN ENGINE AT TAKE OFF POWER SEVERAL TIMES IAW 71-00-00 NO ABNORMALITIES NOTED, OP'S CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 20030609001132003060900113NM 2003 6 9 DHL2003747508 120030512A5311 FRAME BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING "C" CHECK DISCREPANCY AS FOLLOWS, "CABIN INTERIOR TOP OF WING CENTER SECTION RT FRAME AT BS 826 GUSSET ANGLE CRACKED. NDT CONFIRMED. REMOVED AND REPLACED GUSSET RT SIDE BS 826 USING P/N 69-45596 2L73 4F A3WE 20030609001192003060900119WP 2003 6 9 ABXA030150 120030502A552339180757 BRACKET DOUG DC9 DC932 3022066WP ELEVATOR HINGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 DURING A LINE MAINTENANCE VISIT, FOUND THE RT ELEVATOR GEARED TAB CENTER HINGE BEARING BRACKET CRACKED. REPLACED RIGHT GEARED TAB IAW DC-9 MM 27-30-04-2-0001. 2L72 4F A6WE 20030609001262003060900126EU 2003 6 9 MALA030275 120030504A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15525XJ E2350 DURING C-CHECK IN CVG, NR 4 SEAT TRACK FORWARD FROM FRAME 18 TO 20A HAS CORROSION. MAINTENANCE REMOVED AND REPLACED SEAT TRACK IAW EO A53026. REF 409 118105 FOR DETAIL. A/C RELEASE DATE 5/21/03. 2H74 4F RTA49EU 20030515000572003051500057CE 2003 5 15 DXTA200300019 120030428A2131 CONTROLLER CESSNA750 750 2076810CE CABIN PRESSURE MALFUNCTIONED E DXTAG O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL07982QS 7500182 JUST AFTER STARTING A DESCENT FROM FL 410 CABIN RAPIDLY OVERPRESSURIZED . PRESSURE WENT TO BELOW ZERO AND CABIN DPSI WAS RIGHT AT REDLINE. DUE TO RATE AND PRESSURE, CHOSE TO CABIN DUMP. AS A RESULT OXYGEN MASKS DEPLOYED. OPS CHECKED PRESSURISATION SYSTEM ON GROUND WITH APU AND ENGINES, NO FAULTS FOUND. 2L72 4J RTT00007WI 20030515000602003051500060CE 2003 5 15 DXTA200300026 120030502A3297 WIRE CESSNA650 650 2076802CE MLG BROKEN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07789QS3835 6507089 GEAR WOULD NOT RETRACT AFTER TAKEOFF, ACCOMPLISHED AIR TURNBACK TO MKE. 2L72 4F A9NM 20030515000632003051500063SO 2003 5 15 C2XA03IA048 120030510A324039807 CONTROL VALVE EMB 145 EMB145LR 3260212SO BRAKE SYS FAULTY A C2XAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW2715983 145239 IAH - FLT 2711 - CREW REPORTED THAT THE OUTBOARD BRAKES FAIL MESSAGE ILLUMINATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURN TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE OUTBOARD BRAKE CONTROL VALVE TO BE FAULTING. THE VALVE WAS REMOVED AND REPLACED, THE BRAKE SYSTEM OPERATIONALLY TESTED, AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030515000662003051500066EU 2003 5 15 DXTA200300028 120030505A7931 OIL CAP ISRAELGALAXYGALAXY 4500307EU PWA 306 PW306B NE RT ENGINE LOOSE E DXTAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL07700QS 052 PCECC0105 ON CLIMBOUT RIGHT ENGINE LOW OIL PRESSURE MESSAGE CAME ON. RETARDED THROTTLE TO IDLE AND ENGINE PRESS DROPPED TO ZERO. SHUTDOWN THE RIGHT ENGINE PER CHECKLIST AND LANDED SAFELY AT CMH. 2L72 4F4 FRTA53NM E35NE 20030515000722003051500072SO 2003 5 15 SWIA200311926 120030501A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07562SW 120336 SECOND FROM FRONT RED EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED RED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030515000822003051500082NM 2003 5 15 C1HA200394008 120030509A2612182518003752 ELEMENT BOEING727 727290 138408WNM NR 1 FIRE MALFUNCTIONED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15294AS 22146 WHEN TEST SWITCH PLACED ON ENG/WW NR 1 FIRE HANDLE DOES NOT TEST. 2L73 4F A3WE 20030515001012003051500101NM 2003 5 15 03FDEA00614 120030423A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING FOUND OUTBOARD FLAP, INBOARD MOST HINGE, OUTBOARD & INBOARD HOLE WITH CORROSION (FLAP SIDE PIVOT HOLE). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69218 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RH OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030515001162003051500116SO 2003 5 15 SWIA200311930 120030504A3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO LEFT MLG BROKEN A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07569SW 120344 GNS AFIS FUNCTION DOES NOT RECORD OFF OR ON TIMES AND CREW HAD TO USE THE DOWNLOCK RELEASE BUTTON TO RETRACT THE GEAR. INSPECTED LANDING GEAR SYSTEM. FOUND LEFT MLG GROUND PROX SENSOR TO BE BROKEN. REMOVED AND REPLACED PROXIMITY SENSOR WITH A SERVICEABLE UNIT AND ACCOMPLISHED NUMEROUS GEAR SWINGS WITH NO FURTHER DEFECTS. OPS CHECK GOOD. VERIFIED CORRECT OUT, OFF, ON AND IN TIMES. GNS OPS CHECK GOOD. 2L72 4T RTA31SO 20030515001252003051500125 2003 5 15 AWXA200300534 420030514A2565D31038186 SLIDE BOEING757 7572S7 1384962NM PAX DOOR BINDING A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28902AW43004471 23322 FLIGHT CREW REPORTED THE R-1 DOOR EVACUATION SLIDE ARMING LEVER WAS BINDING. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR EMERGENCY EVACUATION SLIDE IAW AWA T/C R1C25602, OPERATIONAL CHECK OF R-1 DOOR ARMING LEVER WAS NORMAL. VENDOR OVERHAULED SLIDE, TEARDOWN REPORT DESCRIBED ONLY PARTS ON PACKING LIST, NO MENTION OF DISCREPANCIES. 2L72 4F RTA2NM 20030515001442003051500144EU 2003 5 15 AWXA200300529 120030504A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU SEAT ROW 7 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT READS OPEN. MAINTENANCE SPLICED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT IAW ESPM 20-43-11 PG 9, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030523001402003052300140WP 2003 5 23 DHL2003804883 120030127A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 496.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS 496.250 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON LT WING CTR L/E FORMER IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20030523001412003052300141WP 2003 5 23 DHL2003604516 120030427A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD L/E FORMER AT STA XFS 735.000 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE-DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030527000062003052700006WP 2003 5 27 DHL2003604521 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING INBOARD L/E FORMER CRACKED (0.500 INCH) STA XFS 628.750. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000292003052700029 2003 5 27 DL76G030323 420030402A256520131A BATTERY BOEING767 7673P6 1385105NM OVERWING SLIDE DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27152DL 24984 WHILE PERFORMING AN ETOPS PRE-DEPARTURE CHECK THE EMERGENCY ESCAPE LEFT OVERWING SLIDE SQUIB FAILED. REPLACED BATTERY CHECKS GOOD. 2L72 4F RTA1NM 20030527000412003052700041WP 2003 5 27 DHL2003801045 120030412A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 379.000 AND 385.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2- FIG 38. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. DRILLED NEW HOLES ON DOUBLER IAW SRM 51-1-22 PG 1. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030610000922003061000092NM 2003 6 10 DL733030435 120030406A524065528547 ARM BOEING737 737347 1384647NM REAR DOOR BROKEN A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27303WA 23183 WHEN CATERING ATTEMPTED TO OPEN THE LEFT REAR SERVICE DOOR . IT WOULD NOT OPEN. REPLACED BROKEN ARM ASSEMBLY 2L72 4F RTA16WE 20030610000992003061000099NM 2003 6 10 DLM88030450 120030508A531499305384 STRUCTURE DOUG MD88 MD88 3023688NM KEELBEAM CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27908DE 53417 THE OUTER FRAME OF THE LONGERON 18R CUSP BEAM WAS FOUND WITH AN AREA OF CORROSION ON THE HORIZONTAL FLANGE AT FS 683. THE CORROSION WAS REMOVED WITH A CUTOUT TO THE FLANGE AND REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384979-14, REV B. 2L72 4F RTA6WE 20030513003082003051300308SO 2003 5 13 ASOA03185 120030426A33501317 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11638AS 120282 DURING A GROUND INSPECTION IN ATL, THE RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030514000072003051400007NM 2003 5 14 AALA20030361 120030322A3350 BATTERY BOEING737 737823 13844BZNM EMERGENCY LIGHT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21913AN 29514 DUIRNG OVERNIGHT MAINTENANCE, EMERGENCY EXIT SLIDE LIGHT AT L1 DOOR INOPERATIVE. CLEANED BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030514000162003051400016EU 2003 5 14 ASOA03178 120030423A33507012210 BULB AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING AN "A" CHECK IN MCN, THE AFT EMERGENCY LIGHT WOULD NOT LIGHT UP WHEN THE TWO MINUTE BUTTON WAS ACTIVATED. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030514000382003051400038NM 2003 5 14 PCAA0304069 120030426A2910 O-RING DHAV DHC8 DHC8102 2809003NM SHUTOFF VALVE LEAKING A PCAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA13844EX 339 RIC-PHL FLIGHT 3792. CREW REPORTED ALL CONTENTS OF NR 1 HYDRAULIC SYSTEM WERE LOST. EMERGENCY WAS DECLARED. MAINTENANCE REPLACED AN O-RING ON THE HYDRAULIC SHUT OFF VALVE AND REPLACED THE NR 1 HYDRAULIC PUMP. CASE DRAIN PRESSURE AND RETURN FILTERS WERE ALSO REPLACED. HYDRAULIC SYSTEM WAS SERVICED AND BLED. OPERATION AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030514000522003051400052NM 2003 5 14 SWAA030975 120030501A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT SVC & AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH AFT SVC & AFT ENTRY EMERGENCY EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20030514001542003051400154NE 2003 5 14 VNAA0305006 220030511A7297 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE IBV VALVE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE CANNON PLUG ON THE IBV VALVE AND INSPECTED THE ENGINE HARNESS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-00-00. GROUND RUNS WERE THEN PERFORMED WITH THE CREW AND NO DEFICIENCIES WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030514002232003051400223NM 2003 5 14 03FDEA00637 120030429A5711 SPAR CAP DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING, FOUND WING REAR SPAR UPPER CAP UPPER SURFACE WITH CORROSION FROM XORS 830 TO XORS 1090. OUTER LT WING/REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIRED FROM XORS 830 TO XORS 1090 AS PER FEDEX EA 1-5720-69229, SRM 57-20-00 FIG. 16 VOL. I AND FEDEX EA 1-5720-69230. 2L73 4F RTA22WE 20030515000162003051500016EA 2003 5 15 03121657 120030501A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 DURING MAINTENANCE INSPECTION, THE RT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515001002003051500100SO 2003 5 15 C2XA03SH125 120030502A531014525480003 BEAM EMB 135 EMB135LR 3260305SO CARGO DOORWAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030515001112003051500111NM 2003 5 15 CH1A200395053 120030426A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOORBEAM AT STA 380 HAS CORROSION AROUND HOLES BETWEEN BL 0 AND RBL 62 (AS MARKED). 2L73 4F A3WE 20030515001122003051500112NM 2003 5 15 CH1A200395054 120030426A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FLOORBEAM AT STA 340 BETWEEN RBL 12 AND LBL 62 IS CORRODED AND CRACKED AT LBL 26 (UPPER CHORD). 2L73 4F A3WE 20030515001322003051500132EU 2003 5 15 142012 120030429A2910L38710SA SWIVEL SAAB SF340 SF340A 7850100EU HYD SYSTEM BROKEN A UHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL17108CQ 340A108 FLIGHT 4456, SHORTLY AFTER TAKEOFF NOTICED THE HYD LIGHT ILLUMINATED AFTER THE LANDING GEAR RETRACTED. ALSO NOTICED A UNSAFE INDICATION IN THE GEAR HANDLE AND THE HYD PRESSURE AND QTY GAUGE LOW. BLEW THE GEAR, THEN PERFORMED SAFE CHECKS BEFORE LANDING. 2L72 4T RTA52EU 20030515001492003051500149EU 2003 5 15 AWXA200300465 120030425A5210D0001019200000 ROD AIRBUS320 A320231 3930325EU R-1 DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - EES - DURING C-04 CHECK THE R-1 DOOR PLUNGER TO STRIKE LEVER CLEARANCE WAS FOUND OUT OF LIMITS BETWEEN DIMENSIONS A (J) AND B (J2). MAINTENANCE ADJUSTED THE R-1 DOOR PLUNGER TO STRIKE LEVER CLEARANCE IAW AMM TASK 52-11-14-820-002, SUB TASK 52-11-14-820-052, AND FIG 501, SHT 1. 2L72 4F RTA28NM 20030527000452003052700045NM 2003 5 27 DL733030331 120030402A53306545775594 SKIN BOEING737 737347 1384647NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 DURING HMV INSPECTIONS, THREE (3) DENTS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FS 757 AND 767 IN THE BAY BETWEEN STRINGERS 20R AND 21R. ADDITIONALLY, FOUR (4) DENTS WERE FOUND BETWEEN FS 757 AND 767 IN THE BAY BETWEEN STRINGERS 21R AND 22R. ALL DENTS WERE WITHIN SRM LIMITS EXCEPT ONE (1) DENT JUST ABOVE STRINGER 22R, WHICH WAS CUTOUT. THE THREE (3) REMAINING DENTS BETWEEN S21R AND 22R WERE REWORKED AND A DOUBLER WAS INSTALLED OVER THE FOUR (4) DAMAGE LOCATIONS BETWEEN S21R AND 22R PER DAL ER/A 412529-14. 2L72 4F RTA16WE 20030527000602003052700060WP 2003 5 27 AALA20030425 120030408A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217535A 49989 TPA - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FORWARD EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000672003052700067WP 2003 5 27 AALA20030386 120030329A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21406A 49317 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE COMPARTMENT INTERIOR TAILCONE RELEASE HANDLE EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE IN TAILCONE FOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527001132003052700113NM 2003 5 27 MEX2003155 120030503A2720 ACTUATOR BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RUDDER INOPERATIVE W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23806AM 26273 AIRCRAFT RETURN TO PLATFORM DUE TO RUDDER PCA EICAS MESSAGE. THE RUDDER MODULE WAS VERIFIED AND THE ALARM WAS FOUND IN RIGHT RUDDER RATIO. IN HANGER THE FIM 27-21-00 PROCEDURE WAS ACCOMPLISHED. BEING ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20030528000022003052800002EU 2003 5 28 HEEA086727 120030522A6220 BEARING SNIAS 350 AS350B2 8680813EU STARFLEX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 WORN BEARINGS. REPLACED WITH SERVICEABLE PARTS. 1G71 3U H9EU 20030528000432003052800043EU 2003 5 28 HE66086398 120030512A2910105450121 POWERPACK BOLKMS105 BO105LSA1 5626021EU HYD SYSTEM DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 FS01202LF3915 2014 HYDRAULIC PACK LEAKING, REPLACED. 1G72 3U H3AU 20030528000672003052800067SW 2003 5 28 AC2A086460 120030509A2435M20021 BRUSHES BELL 430 430 1182150SW STARTER GEN CHIPPED E AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH321 97101 49037 PART IS CHIPPED. BRUSHES CHIPPED AT TRAILING EDGE AND EVIDENCE OF OVERHEATING. SPRING CLIP RIVIT COMES LOOSE AND CLIP FALLS OFF UPON BRUSH REMOVAL. REPLACED BRUSHES. 1G72 3U RTH9SW 20030529000302003052900030SW 2003 5 29 HEEA086628 120030521A6220412010216105 BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03415A 814 36257 PLAY IN BEARING OF MAIN ROTOR HEAD. REPAIRED. 1G72 4U H4SW 20030529000362003052900036EU 2003 5 29 BAQA086472 120030521A7712G555674 TRANSDUCER BOLKMS117 BK117A1 5626010EU TORQUE INDICATORMALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME1385 7243 NR 1 TORQUE INDICATOR FLUCTUATES 20 TO 40 PERCENT. REPLACED WITH SERVICEABLE UNIT. ORDERED TO REPLACE STOCK. 5/21/03 1G72 3U H13EU 20030530000012003053000001 2003 5 30 HEEA086526 420030521A2300 CAP SKRSKYS76 S76C 8143008NE SIREN AMP LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 2315 760505 INTERNAL FUSE CAP LOOSE. UNIT OPERATES INTERMITTENTLY. 1G72 3U NCH1NE 20030530000732003053000073SO 2003 5 30 SIMA200311807 120030424A532014522178005 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 ABI - DURING AN IMBV INSPECTION, THE SERVIE DOOR CENTER SILL WAS FOND TO BE CORRODED BEYOND SRM LIMITS. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL IAW EMB SRM, SRM EMB-145/1142 REV 21, CHAPTERS 51-40-02, 51-40-03, 51-40-06 AND CPM 51-21-04. (M) 2L72 4T RTT00011AT 20030530000752003053000075SO 2003 5 30 SIMA200312711 120030421A532014524381003 GUSSET EMB 145 EMB145LR 3260212SO CARGO BAY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 THIS IS A LEVEL 2 FINDING, FOUND ON AN IMBV INSPECTION CARGO ENTRY GUSSET HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02/06, 51-20-03. (M) 2L72 4T RTT00011AT 20030530001112003053000111EU 2003 5 30 CA030507005 220030403A7250EU24036 BOLT GULSTMG1159 G1159B 3953535SO RROYCESPEY SPEY5118 54523EU ENGINE BROKEN W O OTHER O OTHER NRNOT REPORTED 1 CA 10219 (CAN) ENGINE IS AT RRC FOR REPAIR DUE TO HIGH VIBRATION ON WING. VIBRATION ON THE REAR PICK UP WAS CONFIRMED ON A TEST BED RUN AT RRC. DURING THE STRIP OF THE TURBINE SECTION IT WAS NOTED THAT 2 OF BOLTS HAVE RELEASE THEMSELVES FROM THE LP TURBINE INNER SEAL HOUSING. THE BOLTS WERE FOUND UNDERNEATH THE BALANCING FLANGE OF THE HP TURBINE DISC STAGE 2 AND THE NUTS FOUND ON THE BALANCING WIRE FLANGE OF THE LP 1 TURBINE DISC. THE BOLTS AND NUTS WERE IDENTIFIED TO BE THE CAUSE FOR THE HIGH VIBRATION OF THE ENGINE. THE BOLTS AND NUTS ARE EXPENDABLE PARTS AS PER THE SPEY ENGINE MANUAL, AND NEW ONES ARE INSTALLED AT EACH BUILD. 2L72 4F4 FRTA12EA E2EU 20030530001192003053000119SO 2003 5 30 SIMA200312714 120030420A532014529150001 ANGLE EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION GALLEY CROSSBEAM AND PROFILE CORRODED. REMOVED AND REPLACED CROSSBEAM AND PROFILE IAW EMB 145 SRM 51-40-02/04, 51-20-03. (M) 2L72 4T RTT00011AT 20030530001262003053000126NM 2003 5 30 HALA0300285 120030425A4940 STARTER BOEING767 767300 1385204NM APU FAILED A HALAK NONE O OTHER ININSP/MAINT 1 WP13585HA 24257 ETOPS SIGNIFICANT SYSTEM, APU FAULT LIGHT ON, NO ROTATION, NO EGT RISE. REPLACED STARTER PER MM 49-41-06 AND REPLACED STARTER CLUTCH PER MM 49-41-01. OPS AND LEAK CHECK OK. (M) 2L72 4F RTA1NM 20030515001502003051500150EU 2003 5 15 122561 120030503A2420 WARNING LIGHT SAAB SF340 SF340A 7850100EU AC GENERATOR ILLUMINATED A UHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL17123XS 123 FLT 4506 PULLED OUT OF THE GATE, LEFT ENGINE WAS IN FEATHER, WHEN PUTTING POWER ON THE ENGINE THE LEFT A/C GEN LIGHT WOULD NOT GO OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET CIRCUIT BREAKERS IN COCKPIT AND NOSE WHEEL WELL. INSPECTED LEFT A/C GEN. PERFORMED OPS CHECK OF A/C GEN. OPS CHECKED GOOD. A/C RETURNED TO SERVICE. 2L72 4T RTA52EU 20030515001552003051500155NM 2003 5 15 SWAA031071 120030510A2710BACB10A829 BEARING BOEING737 7372T4 1384492NM AILERON WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND AILERON CONTROL WHEEL SLOW WHEN RETURNING FROM LEFT TURN. REMOVED AND REPLACED AILERON CONTROL UPPER SHAFT BEARING PER MM. 2L72 4F A16WE 20030515001602003051500160NM 2003 5 15 SWAA031076 120030512A33506556633 LIGHT BOEING737 7373K2 13844BANM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED C4 CHECK, FOUND LT AFT CABIN SIDEWALL EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20030515001682003051500168NM 2003 5 15 AWXA200300486 120030429A53126925753 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD FLOOR WEB AT WL 207, LBL 24. MAINTENANCE REMOVED CRACKED FLOOR WEB BS 178 BULKHEAD, WL 207, LBL 24, AND DISCOVERED A CRACKED ATTACH ANGLE. REMOVED CRACKED ATTACH ANGLE; FABRICATED A NEW REPLACEMENT FLOOR WEB AND ATTACH ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-30-01, PG 12. 2L72 4F RTA16WE 20030515001742003051500174EU 2003 5 15 AWXA200300493 120030427A5315D5347209001000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, FORWARD OF FR 66. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7, SRM 51-76-11 PG 9-10 FIG 4. 2L72 4F RTA28NM 20030515001752003051500175EU 2003 5 15 AWXA200300494 120030427A5315D5347218820200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, AT FR 68. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7, SRM 51-76-11 PG 9-10, FIG 4. 2L72 4F RTA28NM 20030515001802003051500180NM 2003 5 15 AWXA200300523 120030511A259765C1990115 CABLE BOEING737 7373Y0 1384671NM R-2 DOOR FRAYED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 PHX - EES - DURING INSPECTION THE R-2 DOOR SLIDE RELEASE CABLE WAS FOUND FRAYED. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR SLIDE RELEASE CABLE, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030515001822003051500182NM 2003 5 15 AWXA200300525 120030506A532069265553 CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON AFT LOWER WEB CLIP AT L-1 DOOR CUTOUT BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED AFT LOWER WEB CLIP AT L-1 DOOR CUTOUT BS 344, STR 16; FABRICATED AND NEW REPLACEMENT WEB CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 10-11. 2L72 4F RTA16WE 20030515001872003051500187NM 2003 5 15 AWXA200300512 120030410A52106079454 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .5 INCH CRACKS WERE FOUND ON L-1 DOOR INTERIOR SKIN AND AFT EDGE BEAM AT AFT DOOR STOP PIN CUTOUTS. MAINTENANCE TRIMMED OUT CRACKS ON L-1 DOOR INTERIOR SKIN AND AFT EDGE BEAM AT AFT DOOR STOP PIN CUTOUTS; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST. FABRICATED A DOUBLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW ER 03-5362-03126-SS2. 2L72 4F RTA16WE 20030515001952003051500195NM 2003 5 15 AWXA200300457 120030414A531565468123 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CAP AT BS 1016, LBL 27.75. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CAP AT BS 1016, LBL 27.75; FABRICATED A NEW SECTION OF UPPER CAP, 2 EACH SUPPORT ANGLES AND STRAPS PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-9 FIG 2 PG 7-11. 2L72 4F RTA16WE 20030515001962003051500196NM 2003 5 15 AWXA200300458 120030401A5523657379946 STRUCTURE BOEING737 737277 1384570NM ELEVATOR TAB DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK THE RT ELEVATOR TAB WAS FOUND DELAMINATED AT THE INBOARD END TRAILING EDGE, STAB STA 80. MAINTENANCE PERFORMED COMPOSITE REPAIR ON RT ELEVATOR TAB AT INBOARD END TRAILING EDGE, STAB STA 80 IAW B737-200 SRM 51-40-9 FIG 1 PG 4, PARA 4C, TABLE II. 2L72 4F RTA16WE 20030520000032003052000003EA 2003 5 20 CA030421008 120030416A5302S612066120002 FITTING CARSONS61 S61LSKRSKY EA GE CT58 CT581401 30011NE PYLON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA H1044 (CAN) DURING VISUAL INSPECTION, A CRACK WAS DETECTED ON LT LOWER PYLON HINGE WEB AREA, ORIGINATING FROM A TOOLING HOLE, AND PROGRESSING TOWARD THE OUTBOARD SIDE. 2G72 4U4 U H8EA 1E3 20030520000152003052000015NM 2003 5 20 AMTA200300571 120030428A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11520AT 27976 TWO LIGHTS INOPERATIVE ON EMERGENCY EGRESS TRACK AT SEAT 1C. FOUND WIRE TERMINAL DISCONNECTED, RECONNECTED TERMINAL, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030520000252003052000025EU 2003 5 20 SIMA200311801 120030425A5610 WINDSHIELD SAAB SF340 340B 7860101EU COCKPIT FAILED A SIMAO OTHER O OTHER DEDESCENT 1 SW21376AE 340B376 CREW REPORTED A LARGE BIRD STRUCK THE RIGHT FORWARD WINDSHIELD. WINDSHIELD SHATTERED. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION IN THE AREA AND REPLACED THE WINDSHIELD IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030520000272003052000027WP 2003 5 20 GTIA030257 120030404A5297 WIRE DOUG DC9 DC983 3022083WP DOOR LIGHT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 L1 DOOR EXIT MARKER DOES NOT ILLUMINATE WITH EMERGENCY POWER ON. TROUBLESHOT EMERGENCY LIGHTING. FOUND WIRE SPLICE DEFECTIVE. REPLACED DEFECTIVE SPLICE. (M) 2L72 4F RTA6WE 20030520000282003052000028WP 2003 5 20 GTIA030258 120030405A5410 LINER DOUG DC9 DC983 3022083WP RT NACELLE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FOUND RT ENGINE INLET CASE ACOUSTIC LINER DAMAGED IN 4 PLACES. REPAIRED RIGHT ENGINE INLET AT DAMAGED AREAS. (M) 2L72 4F RTA6WE 20030520000332003052000033SO 2003 5 20 SIMA200309608 120030328A532014522459001 SUPPORT EMB 135 EMB135KL 3260302SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 THIS IS A LEVEL TWO FINDING, FOUND DURING A MBV INSPECTION, INBOARD GALLEY RAMP SUPPORT CORRODED. REMOVED AND INSTALLED NEW INBOARD GALLEY RAMP SUPPORT IAW EMB 140 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030520000402003052000040 2003 5 20 2003F00255 420030116A3100 INDICATOR CESSNA207 207 2073602CE CO2 FALSE INDICATIONA YADAO OTHER N FALSE WARNING CRCRUISE 1 AL0136CF 20700269 PILOT REPORTED THAT THE INSTRUMENT PANEL MOUNTED, PASSIVE-TYPE, CARBON MONOXIDE INDICATOR DISK TURNED BLACK WHILE EN ROUTE AND TEN MINUTES FROM LANDING. MAINTENANCE HAS NOT LOOKED INTO THE PROBLEM AT THE TIME THAT THIS REPORT IS BEING GENERATED. INSPECTED EXHAUST SYSTEM AND FOUND NO LEAKS. REPLACED CO INDICATOR AND TEST FLEW SATISFACTORY. (M) 1H71 3O A16CE 20030520000412003052000041SO 2003 5 20 2003F00256 120030219A32134550404 TUBE PIPER PA31 PA31350 7103110SO PISTON OVERSIZED A YAAAO OTHER O OTHER NRNOT REPORTED 1 AL03509FN 317952162 PILOT REPORTED RT MLG OLEO STRUT STICKING IN THE EXTENDED POSITION & NOT READILY COMPRESSING. AFTER REMOVAL FROM A/C, RT MLG WAS DISASSEMBLED TO DISCOVER THAT RETAINING PINS THAT SECURED TOP BEARING TO STRUT PISTON TUBE HAD PASSED CLEAR THROUGH INTO PISTON TUBE BORE & WERE BINDING UP ON ORFICE TUBE AND HAD MIGRATED TO BETWEEN PISTON TUBE & TRUNNION BORE, BINDING THERE ALSO. FURTHER INVEST CLEARLY REVEALED THAT A PREVIOUS OWNER/OPERATOR HAD ENLARGED RATAINING PIN HOLES IN TOP OF CHROME PISTON TUBE FROM FACTOR SPECS OF .250 IN DIAMETERS TO IN EXCESS OF .310 IN DIAMETER WHICH ALLOWED RETAINING PINS TO BECOME DISLODGED INSTEAD OF BEING LOCKED IN PLACE. LT MLG WAS REMOVED & DISASSEMBLED TO DISCOVER SAME CONDITION1L72 3O A20SO 20030514001182003051400118NM 2003 5 14 SWAA031029 120030508A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND 3.5 INCH LONG FUSELAGE SKIN CRACK, BS 275, STRINGER 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030514001262003051400126NM 2003 5 14 SWAA031012 120030506A259765C19901 CABLE BOEING737 7372H4 138448CNM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030514001372003051400137EU 2003 5 14 SWAA031037 220030508A75327064004 BLEED VALVE BOEING737 7375H4 138449DNM CFMINTCFM56 CFM562AFR 13802EU NR 2 ENGINE FAULTY A SWAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW29522SW 26564 AIR TURNBACK, NR 2 ENGINE WOULD NOT MAKE CLIMB POWER. REMOVED AND REPLACED BLEED VALVE PER MM. 2L72 4F4 FRTA16WE E21EU 20030514001402003051400140NM 2003 5 14 SWAA031040 120030509A335065C27093 LIGHT BOEING737 7372H4 138448CNM MID CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F A16WE 20030514001432003051400143NM 2003 5 14 SWAA031043 120030508A57536546435 SKIN BOEING737 7373Q8 1384670NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED 1/4D CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED. REPAIRED LT OUTBOARD AFT T/E FLAP PER SRM. 2L72 4F RTA16WE 20030514001552003051400155NM 2003 5 14 VNAA0305005 120030508A3150 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT ILLUMINATED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND AC VOLT FAIL INDICATION AND ABORTED TAKEOFF. WHILE TAXIING TO THE GATE THE INDICATION CLEARED AND THE CREW CALLED MAINTENANCE CONTROL. THE CREW WAS THEN INSTRUCTED TO ATTEMPT ANOTHER TAKEOFF AND DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030514001612003051400161SO 2003 5 14 RAIA00304118 120030420A324238793500 SHUTOFF VALVE EMB 145 EMB145 3260210SO BRAKE SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03806HK8458 145112 OUTBOARD BRAKE FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE SHUTOFF VALVE, OPS CHECK GOOD. 2L72 4F RTT00011AT 20030514001742003051400174 2003 5 14 372PA0024 420030428A22303200940010 SENSOR BOEING737 737306 13844BGNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO05372PA 23546 AUTO THROTTLE DISENGAGES ON TAKEOFF AND CLIMB. CLIMB NR 2 N1 3 PERCENT LESS THAT NR 1 N1. REMOVED AND REPLACED N1 SENSOR ENGINE NR 2 PER MM 77-12-01. TEST OK. 2L72 4F RTA16NE 20030514002052003051400205NM 2003 5 14 03FDEA00717 120030430A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING, FOUND OUTBOARD FLAP, INBOARD HINGE FITTING FLAP SIDE TO FLAP MOUNTING HOLES LOCATION CORRODED. CORROSION ON LH WING, O/B FLAP I/B HINGE FITTING FLAP SIDE TO FLAP MOUNTING HOLES REMOVED AS PER SRM 51-21-01, VOL II. AND SRM 51-31-01, VOL II. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69254 WING - LT OUTBOARD FLAP INBOARD AFT HINGE OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030515000752003051500075CE 2003 5 15 DXTA200300023 120030430A3260 BULB CESSNA500 560CESSNA 2076750CE MLG INDICATOR BURNED OUT E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07366QS 5600466 UNSAFE INDICATION ON LEFT MAIN GEAR, BLEW GEAR DOWN. FOUND BOTH LIGHT BULBS ON MLG PANLE BURNED OUT, REPLACED BULBS. 2L72 4F RTA22CE 20030515000922003051500092NM 2003 5 15 03FDEA00724 120030505A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25602FE 48402 RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE TO FLAP LOWER SURFACE WITH HOLES FLAP SIDE QTY 4 EACH CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69251 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030515000942003051500094EU 2003 5 15 03129315 120030509A3230 VALVE JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27315UE 41033 AFTER TAKEOFF, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL RESEATED THE UNDERCARRIAGE RELEASE VALVE. OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030520000342003052000034WP 2003 5 20 GTIA030263 120030223A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CABIN, STATION 180 LBL 13 INCHES TO 38 INCHES FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT AT STATION 180 LBL 13 - LBL 38. FABRICATED NEW FLOOR SUPPORT AT STATION 180 LBL 13 - LBL 38. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20030520000492003052000049SO 2003 5 20 SIMA200311304 120030326A532014521725001 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, THE LEFT FLOORBOARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE FLOORBOARD SILL IAW EMB 145 SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030520000522003052000052SO 2003 5 20 SIMA200311306 120030331A5320 SUPPORT BRACKET EMB 145 EMB145LR 3260212SO PAX DOORWAY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION PASENGER DOOR CUTOUT CENTER SILL SUPPORT BRACKETS (P/N 145-24131-007 AND 145-24131-009) SERVICEABLE CENTER SILL IAW EMB 145 SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030520000752003052000075NM 2003 5 20 AMTA200300497 120030412A2613579601 OVERHEAT SENSOR BOEING757 75723N 1384973NM NR 1 NACELLE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11514AT 27971 EICAS STATUS MESSAGE, L ENG OH LP2 DISPLAYED. REMOVED AND REPLACED NR 1 ENGINE NACELLE OVERHEAT DETECTOR. OPS NORMAL PER MM 26-11-01. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20030520000792003052000079CE 2003 5 20 2003F00258 120030329A2697 WIRE BEECH 1900 1900D 1154162CE FIRE BOTTLE LOOSE A GUUAF ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 SO1981556 UE239 FLT 9205 - NAS/FLL - DURING FLIGHT, NR 1 FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED. CONTINUED TO FLL. SECURED LOOSE WIRE AT NR 1 FIRE BOTTLE SQUIB. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20030520000822003052000082NM 2003 5 20 AMTA200300507 120030415A3350 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 EGRESS OVERHEAD LIGHT OUT AT ROW 37 ABC. RECONNECTED QUICK DISCONNECT DO7274. PERFORMED OPS CHECK, NORMAL. (M) 2L72 4F RTA2NM 20030520001072003052000107NM 2003 5 20 AALA20030439 120030409A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21389AA 27449 DFW - DUIRNG OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT 40B INOPERATIVE. RECONNECTED EMERGENCY EXIT PATH LIGHTING CONNECTOR AT 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520001282003052000128EA 2003 5 20 ASOA03191 120030429A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11850AS 7355 FLT 4134 - DURING A GROUND INSPECTION IN SHV, THE EXTERIOR LEFT OVERWING AFT EMEGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR LEFT OVERWING AFT EMEGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030520001292003052000129NM 2003 5 20 KPVA200317 120030406A33506104784 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A KPVAK NONE O OTHER ININSP/MAINT 1 WP13807WP 023 EMERGENCY EXIT EGRESS LIGHT ON RIGHT SIDE AND ONE AT CENTER CEILING AISLE LIGHT INOPERATIVE. REMOVED AND REPLACED AFFECTED POWER SUPPLY. OPERATIONAL CHECK OF SYSTEM GOOD. WORK IAW DHC-8 MM 33-51-00, PAGES 201-202. (M) 2H72 4T RTA13NM 20030520001312003052000131EU 2003 5 20 ASOA03187 120030421A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK FROM FRAME 37 TO 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK FROM FRAME 37 TO 41 IAW SRM 51-25-02 AND SRM 51-25-04. (M) 2H72 4T RTA53EU 20030520001342003052000134NM 2003 5 20 2003F00267 120030123A5315 FLOORBEAM BOEING727 727222 1384073NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 1130, LBL 0. REMOVED CORROSION FROM FLOORBEAM AT FUSELAGE STATION 1130 BL 0. REMOVED UPPER T-CAP LBL 60 TO RBL 60, STATION 1130. FABRICATED NEW T-CAP. TREATED, PRIMED AND INSTALLED NEW UPPER T-CAP LBL 60 TO RBL 60 FUSELAGE STATION 1130. (M) 2L73 4F A3WE 20030520001352003052000135NM 2003 5 20 2003F00268 120030123A5315 FLOORBEAM BOEING727 727222 1384073NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM AT STATION 1130, RBL 45. REMOVED UPPER T-CAP FROM LBL 60 TO RBL 60. FABRICATE, TREAT, PRIME AND INSTALLED NEW T-CAP. (M) 2L73 4F A3WE 20030520001362003052000136NM 2003 5 20 2003F00269 120030120A5312652368723 FRAME BOEING727 727222 1384073NM BULKHEAD CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND NR 2 ENGINE BULKHEAD AT FUSELAGE STATION 1342, ENGINE COWL LIP SEAL CRACKED FROM 1 O'CLOCK TO 4 O'CLOCK POSITION. INSTALLED NEW COWL SEAL RETAINER NR 2 ENGINE AT FUSELAGE STATION 1342, STRINGER 6L TO STRINGER 6R. (M) 2L73 4F A3WE 20030520001502003052000150NM 2003 5 20 2003F00278 120030120A5320 PANEL BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND STRINGER 5L, FUSELAGE STATION 350, SUPPORT PANEL IS CRACKED. REMOVED AND REPLACED PANEL STATION 350, STRINGER 5L. (M) 2L73 4F A3WE 20030520001552003052000155SO 2003 5 20 2003F00283 220030401A8520632018 GEAR CESSNA421 421A 2076012CE CONT O520 GTSIO520C 17032SO CRANKSHAFT BROKEN A MNOAO OTHER O OTHER NRNOT REPORTED 1 WP05421A 421A0132 REMOVED RIGHT INOPERATIVE ALTERNATOR FOR REPAIR AND NOTED. CRANKCASE DAMAGED, ALTERNATOR FACE GEAR, BROKEN AND LOOSE. FACE GEAR ATTACH BOLTS, DAMAGED AND LOOSE. (M) 1L72 3O3 O A7CE E7CE 20030602000072003060200007SO 2003 6 2 SIMA200313202 120030506A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21644AE 145204 DURING AN IMBV INSPECTION, STRINGER 19R BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS NOTED. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M) 2L72 4T RTT00011AT 20030602000122003060200012SO 2003 6 2 ASOA03193 120030501A335012021299001 LIGHT EMB 120 EMB120RT 3260202SO RT OVERWING INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11274AS 120229 DURING A GROUND INSPECTION IN DFW, THE RIGHT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030602000212003060200021NM 2003 6 2 USAA030048 120030505A5330 SKIN BOEING737 737301 1384611NM WINDOW POST CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US42530 23555 FOUND WINDOW POST SKIN CRACKED .375 INCH LONG, CAPTAIN WINDSCREEN OUTBOARD POST, TOP OUTBOARD CORNER. CUT OUT DAMAGED, INSTALLED FILLER AND DOUBLER PER SRM 53-10-01 FIG 210. (M) 2L72 4F RTA16WE 20030602000432003060200043EA 2003 6 2 CA030514001 120030509A5610601R3303313 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER APAPPROACH 1 CA (CAN) DURING THE APPROACH, THE PILOT REPORTED THE LT WINDSHIELD OUTER PANE CRACKED. THE AIRCRAFT LANDEDUNEVENTFULLY. FOLLOWING THE WINDSHIELD REPLACEMENT, THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030602000452003060200045SO 2003 6 2 AUS20030411 120030211A2897 WIRE HARNESS EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE FUEL BOOST PUMP WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LEFT FORWARD BOOST PUMP LOOM CHAFED AGAINST RIGID FUEL LINE PN 120-08735-047 LOCATED IN THE TANK. LOOM INCORRECTLY ROUTED. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20030602000502003060200050EU 2003 6 2 CA030514006 120030509A3411900000 MOISTURE TRAP AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE7315BR WP STANDBY PITOT CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) OVER THE PAST FEW YEARS WE HAVE NOTICED A TENDENCY OF THE PLASTIC MOISTURE TRAPS IN THE STANDBY PITOT-STATIC SYSTEM TO CRAZE AND CRACK. THIS HAS CAUSED LEAKAGE AND IN ONE INSTANCE THE TRAP FRACTURED AND FELL OFF DURING INSPECTION. AFTER SOME INVESTIGATION WE FOUND THAT THE PLASTIC MATERIAL WAS NOT COMPATIBLE WITH ISOPROPYL ALCOHOL WHICH IS USED TO REMOVE TRACES OF HYDRAULIC FLUID FROM THE ADJACENTAREA. WE EXPOSED A TEST PART TO ALCOHOL AND WITHIN A FEW MINUTES IT HAD CRAZED, CRACKED AND THE PLASTIC HAD EXFOLIATED, COMING OFF IN LAYERS LIKE MICA SHEETS. A CAUTIONARY NOTE IN THE MM WOULD HELP AVOID THIS PROBLEM. 2L73 4F4 FRTA46EU E6WE 20030602000572003060200057EA 2003 6 2 CA030425007 120030419A6220269A54985 SHAFT SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA MAIN ROTOR UNDERSIZE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FORWARD BEARING INNER RACE TURNING ON SHAFT. 1G71 3U3 O0 4H12 1E10 20030527001152003052700115 2003 5 27 G5S2003F00000 420030430A25657A14124 SLIDE BOEING747 747400 NM UPPER DECK DOOR INOPERATIVE W G5SAO OTHER L NO TEST NRNOT REPORTED 1 EA29493MC 1 29254 DURING AN OPERATIONAL CHECK OF THE INFLATABLE EVACUATION SYSTEM AT THE UPPER DECK DOOR RT, THE SLIDE WAS LIFED AND HAS BEEN FALLEN OUT OF THE DOOR FRAME. SUDDENLY THE SLIDE STOPPED ROTATING AND STUCK. AFTER WAITING SEVERAL SECONDS THE MECHANIC OPENED THE VELCRO TAPES, WHICH CONNECT THE ASPIRATORS WITH THE GIRT. AFTER THIS THE SLIDE TURNED TO THE END POSITION AND INFALATED PROPERLY. INVESTIGATION OF THE VIDEO RECORD HAS SHOWN THAT THE FORWARD RELEASE CABLE WAS TIGHT WHEN THE SLIDE STUCK. THE LAST RELEASE PIN WAS LAYING BENEATH THE GIRT. OPENING OF THE VELCRO TAPES INCREASED THE FORCE AND THE RELEASE CABLE GOT FREE. AFTER THIS MANUAL RELEASE, THE SLIDE INFLATED PROPERLY. 2L74 4F RTA20WE 20030528000242003052800024NE 2003 5 28 HEEA086590 220030512A72615034T70P04 SEAL BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 2 ENGINE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 FIFTY TWO MINUTES AFTER TAKEOFF, NR 2 ENGINE OIL LIGHT ILLUMINATED WITH COINCIDING PRESSURE DROP OF NR 2 ENGINE OIL PRESSURE GAUGE. PRESSURE WENT TO ZERO WHILE NR 2 ENGINE WAS SHUT DOWN IN FLIGHT. 2G72 4U4 U H10SW E8NE 20030528000342003052800034SW 2003 5 28 ERAA086444 120030425A6510212040600005 HANGER ASSY BELL 412 412 1182202SW T/R DRIVESHAFT VIBRATION E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01169EH14970 33064 HANGER ASSY HAS HIGH FREQUENCY VIBRATION COUPLING AND BEARING HANGER HAD PRIMER COAT. NO DEFECTS NOTED TO CAUSE HIGH FREQUENCY. DISASSEMBLED, STRIPPED PRIMER, CLEANED & VISUALLY INSPECTED ALL PARTS. HAD CAD PLATING TOUCHED UP ON COUPLING. REASSEMBLED, TORQUED & SAFTIED IAW 412-CR&O INSTALLING NEW SEAL & PURGED BEARING WITH MOBIL 28 AND REPACKED FLEX COUPLING WITH GREASE DATED 9-20-01. 1G72 4U H4SW 20030528000522003052800052EU 2003 5 28 HEEA086738 120030522A7931642790041 TRANSMITTER AEROSPAS355 AS355* EU OIL PRESSURE FLUCTUATES E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03855PH 3351 OIL PRESSURE FLUCTUATING. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H11EU 20030528000702003052800070WP 2003 5 28 AALA20030449 120030411A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21408AA 49319 - DURING OVERNIGHT MAINTENANCE, BOTH FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. TIGHTENED FORWARD OVERWING EMERGENCY EXIT LIGHT BATTEYR CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030528001022003052800102SW 2003 5 28 HEEA086611 120030521A7120 BEARING BELL 412 412 1182202SW ENGINE MOUNT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03415A 36257 FWD TRIPOD BEARING BAD. REPLACED. 1G72 4U H4SW 20030529000352003052900035EU 2003 5 29 BAQA086455 120030519A6500741C000005 ACTUATOR BOLKMS117 BK117B2 5626013EU TAIL ROTOR MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS011174U2812 7146 CAUSING SEVERE KICKING EVEN WITH YAW-CSAS DISENGAGED. SEALS LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030529000522003052900052EU 2003 5 29 HEEA086507 120030521A77200301037070 HARNESS AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1D1 NE PYROMETRIC FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03974AE 2653 9586 PROBE BECAME UNSOLDERED AT PROBE ATTACH NUT AND CAME OUT OF ENGINE. 1G72 3U3 U H11EU E19EU 20030529000552003052900055SW 2003 5 29 HEEA086642 120030521A3212412050013115 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 MLG EMERGENCY FLOAT BAG LEAKING. 1G72 4U H4SW 20030530000092003053000009SW 2003 5 30 HEEA086671 120030522A5210209031816105 DOOR BELL 412 412 1182202SW CREW DOOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 CREW DOOR WORN THROUGH AT TOP. REPLACED DOOR. 1G72 4U H4SW 20030530000212003053000021SW 2003 5 30 HEEA086675 120030522A6510212040600005 HANGER ASSY BELL 212 212 1181420SW T/R DRIVE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736J18343 31140 PITTING ON OUTPUT FLANGE. REPLACED 4 EACH CLAMPS 204-040-811-001 DUE TO CORROSION. REPAIRED. 1G71 4U H4SW 20030530000482003053000048NE 2003 5 30 HEEA086545 120030522A6220 BEARING SKRSKYS76 S76C 8143008NE M/R HEAD ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH BFG3050BIC 760505 MAIN ROTOR HEAD ROD HAS A WORN BEARING. 1G72 3U NCH1NE 20030530000552003053000055EA 2003 5 30 2003F00332 120030326A5210601R31911501 STRUT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR INOPERATIVE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0797325 7325 AIRCRAFT MAIN CABIN DOOR WILL NOT CLOSE. MAINTENANCE TROUBLESHOT. REPLACED THE GAS SHOCK STRUT AND RE-RIGGED MAIN CABIN DOOR. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20030602000162003060200016NM 2003 6 2 USAASB03062 120030505A2750 CIRCUIT BREAKER BOEING737 737401 1384701NM TE FLAPS TRIPPED A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19409US 23879 CLT - FLT 859 - ON APPROACH INTO CLT, THE FLAP INDICATION DID NOT GO BEYOND 10 DEGREES. CREW COMMENCED WITH A MISSED APPROACH AND DECLARED AN EMERGENCY. ALTERNATE FLAP EXTENSION PROCEDURE WAS INITIATED AND A NORMAL FLAP LANDING WAS MADE WITH FLAP INDICATION READING ZERO. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE RESET POPPED FLAP POSITION TRAILING EDGE INDICATION CIRCUIT BREAKER. PERFORMED FLAP INDICATION TEST PER MM 27-51-00. OPERATIONAL TEST GOOD. (M) 2L72 4F RTA16WE 20030602000782003060200078GL 2003 6 2 AUS20030425 320030417A6111A2202A BEARING HARTZL PIPER PA32 PA32R300 7103213SO LYC O540 IO540* 41532EA HARTZLHCC2Y HCC2YK1 GL PROPELLER BLADE FRACTURED W K NONE O OTHER ININSP/MAINT 1 AUS 879 CH14311 (AUS) PROPELLER BLADE BEARING FRACTURED. 1L71 3O3 O A3SO 1E4 5 CP920 20030602000822003060200082NM 2003 6 2 DLM90030483 120030520A33508039251 POWER SUPPLY DOUG MD90 MD9030 3023690NM CABIN INOPERATIVE A DALAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO27903DA 53383 F/C EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2L72 4F RTA6WE 20030602001032003060200103NM 2003 6 2 DLM88030492 120030526A335060030451 POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27911DL 49542 ON POWER DOWN EMERGENCY EXIT LIGHTS STAY ON. REPLACED POWER SUPPLY. 2L72 4F RTA6WE 20030602001042003060200104NM 2003 6 2 SWAA031172 120030527A3350BR2013 LIGHT BOEING737 7373H4 1384600NM MID CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 EEPLS SECTION INOP AT MID CABIN. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20030602001082003060200108NM 2003 6 2 SWAA031176 120030524A53116546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, WL 14 AND RBL 9. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030602001112003060200111NM 2003 6 2 SWAA031179 120030525A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND STUB FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030602001132003060200113NM 2003 6 2 SWAA031181 120030526A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) BS 294 AT STR 14L, BS 520 AT STR 12R, BS 787 AT STR 23L AND BS 807 AT STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030602001172003060200117NM 2003 6 2 SWAA031155 120030523A53126445819 WEB BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C1 CHECK, FOUND NLG W/W BOTH LT/RT UPPER WEB CRACKED AT ACCESS PANEL CUTOUT TIRE STOP. REPAIRED UPPER WEB PER SWA EA. 2L72 4F RTA16WE 20030602001352003060200135NM 2003 6 2 SWAA031146 120030522A3350BR2013 LIGHT BOEING737 7377H4 1384404NM MID CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 EEPLS INOP AT MID CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030602001402003060200140NM 2003 6 2 SWAA031151 120030522A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, STRINGER 5R, BS 727B AND BS 727E. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030602001612003060200161NM 2003 6 2 VNAA0305021 120030529A3240 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMER BRAKE ILLUMINATED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07438JS 3056 EN ROUTE, THE CREW HAD A EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE THAT WOULD NOT EXTINGUISH. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO ELM. AT 50 FEET ABOVE GROUND ON LANDING THE MESSAGE EXTINGUISHED. OUTSTATION MAINTENANCE INSPECTED AND SERVICED THE EMERGENCY PARKING BRAKE ACCUMULATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-12-00. THE SYSTEM WAS CHARGED AND OPERATIONAL CHECKS WERE PERFORMED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030602001642003060200164NM 2003 6 2 USAASB03059 120030502A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ABOVE THE FORWARD ENTRY DOOR AND ABOVE SEAT 2A REMAIN ILLUMINATED FOR A SHORT PERIOD OF TIME DURING TESTING. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030602001652003060200165GL 2003 6 2 I5HA0358003 220030507A7200 ENGINE CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL LEFT MALFUNCTIONED A I5HAO OTHER O OTHER TOTAKEOFF 1 GL23582P 475 ON THE TAKEOFF ROLL DEPARTING CVG, EN ROUTE TO CLE THE LEFT ENGINE WOULD ONLY PRODUCE 888 DEGREES, NOMINAL IS 971 DEGREES. THE PILOT ABORTED THE TAKEOFF. THE TEMPERATURE DATRUM (TD) SYSTEM WAS NULLED AND FULL POWER WAS THEN AVAILABLE. THE TD SYSTEM WAS DEFERRED AND THE FLIGHT CONTINUED UNEVENTFULLY TO CLE WITH THE TD SYSTEM IN THE NULL POSITION. (M) 2L72 4R4 T 6A6 E282 20030602001662003060200166EA 2003 6 2 ASOA03190 120030429A2910AE2460010H0264 LINE CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYS CHAFED A ASOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11837AS 7271 FLT 4496 - DURING CLIMB-OUT FROM DFW-CHS, AT APPROXIMATELY 22,000 FEET THE CREW RECEIVED A NR 2 HYDRAULIC LOW PRESSURE WARNING MESSAGE WITH THE SYNOPTIC PAGE SHOWING NO HYDRAULIC FLUID IN THE RESERVOIR. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN PUMP PRESSURE LINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030602001702003060200170EA 2003 6 2 A6WA200340062 120030423A5200 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 PASSENGER DOOR SEAL STRIKER IS DAMAGED AT FS 310 AND FS 349 AT MIDDLE LATCH LOCATION. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 310 AND 349 IAW REO 601R-52-11-008 ISSUE B. (M) 2L72 4F RTA21EA 20030602001812003060200181NM 2003 6 2 AALA20030525 120030502A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 21HJ INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRE AT 31HJ. SYTSEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030604000162003060400016NM 2003 6 4 AALA20030510 120030429A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21A INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 21A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030529000572003052900057SW 2003 5 29 HEEA086644 120030521A3246412050015112 SKID BELL 412 412 1182202SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 33115 SKID TUBE MACHINED SURFACE DAMAGE UNDER SKID NEAR SADDLE TO A DEPTH OF .035. SENT TO DRAKE AIR FOR WARRANTY REPAIR. 1G72 4U H4SW 20030529000722003052900072NE 2003 5 29 HEEA086514 120030521A243230126002S BATTERY SKRSKYS76 S76A 8143006NE MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03764P 760276 BATTERY DEAD. REPAIRED. 1G72 3U H1NE 20030529000762003052900076 2003 5 29 HEEA086518 420030521A34427021450601 COMPUTER SKRSKYS76 S76A 8143006NE COCKPIT WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03763P 760166 COMPUTER FAILS SELF TEST. 1G72 3U H1NE 20030530000172003053000017NE 2003 5 30 HEEA086533 220030522A73200174025120 VALVE SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE FUEL SYSTEM INTERFERENCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 VALVE HAS INTERMITTENT OPERATION DURING ENGINE STARTS. 1G72 3U3 U H1NE E19EU 20030530000742003053000074SO 2003 5 30 SIMA200312704 120030429A5320 SUPPORT EMB 145 EMB145LR 3260212SO PAX DOOR FRAME CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 ABI - DURING AN IMBV INSPECTION, THE PASSENGER DOOR LOWER SEALING SUPPORT FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE LOWER SEALING SUPPORT AND ATTACHED STRUCTURE. FABRICATED A REPLACEMENT SUPPORT. FABRICATION AUTHORITY CONTAINED IN EMB STATEMENT IC2003-145/1435. REPAIR DONE IAW EMB STATEMENT IC2003-145/1435, EMB SRM, SRM 145/1142 REV 21, 51-20-03, 51-40-02, 51-40-06, EMB CPM, CPM 145/1132 REV 8, 51-21-04, 51-21-05, 51-21-06, AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030530001222003053000122NM 2003 5 30 AMTA200300637 120030511A3350 LIGHT BOEING757 75723N 1384973NM ESCAPE SLIDE INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 R1 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED R1 FORWARD GIRT BAR PROX SENSOR PER MM 25-66-11 AND SWPM CHAP 20. OPS NORMAL. (M) 2L72 4F RTA2NM 20030602000232003060200023NM 2003 6 2 USAA030042 120030417A5414 SKIN BOEING737 7373B7 1384580NM LT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19523AU47983 23858 FOUND SKIN CRACKED 1 INCH LONG, LEFT ENGINE PYLON AT ACCESS PANEL S724L CUTOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 54-50-07. (M) 2L72 4F RTA16WE 20030520001562003052000156NM 2003 5 20 2003F00284 120030120A5411652368723 FRAME BOEING727 727222 1384073NM NR 2 NACELLE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND NR 2 ENGINE BULKHEAD AT FUSELAGE STATION 1342 ENGINE COWL LIP SEAL IS CRACKED AT 10 O'CLOCK TO 11 O'CLOCK POSITION. INSTALLED NEW COWL SEAL LIP RETAINER NR 2 ENGINE AT STATION 1342 FROM STRINGER 6L TO STRINGER 6R. (M) 2L73 4F A3WE 20030521000072003052100007WP 2003 5 21 DHL2003801056 120030407A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING CTR L/E UPPER SKIN CORRODED FROM XFS 322.750 TO XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION FROM RT WING CTR L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED AREA IAW SRM 57-2-1 PG 1 FIG 38. FABRICATED FILLER AND DOUBLER (7075-T6 0.063) IAW SRM 57-2-1 PG 1 FIG 38. CLEANED, TREATED AND PRIMED DOUBLER AND FILLER INNER SIDE IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 PG 1 FIG 38 AND SRM 51-1-21 PG 1. REFER TO N/R 2146 FOR RT WING CTR L/E REMOVAL/ REINSTALLATION. 2L74 4F RT4A25 20030521000082003052100008WP 2003 5 21 DHL2003804905 120030121A5754 SKIN DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING T/E TOP EXTERIOR SKIN SURFACE DELAMINATED (STA 5.000-47.000). CUT OUT DAMAGED AREA IAW SRM 57-2-3 PG 4 PAR 1. FABRICATED FILLER AND DOUBLER (7075-T6 AL0.032) IAW SRM 57-2-3 PG 4 PAR 11. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INNER SURFACE IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 51-1-9 PG 2-3 PAR 2-3. 2L74 4F RT4A25 20030521000122003052100012WP 2003 5 21 DHL2003801016 120030503A573056110101 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING LOWER SURFACE- T/E LWR PANEL OUTER SKIN DELAMINATED STA XW 5.000- XW 47.000. REMOVED AND REPLACED LT WING T/E LWR PANEL BETWEEN STA XW 5.000 - XW 47.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521000162003052100016WP 2003 5 21 DHL2003604505 120030428A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING - CTR L/E INNER PART FORMER CRACKED 1.000, XFS 502.500 (UPPER PART). STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON RT WING CTR L/E FORMER (XFS 502.500) IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000172003052100017WP 2003 5 21 DHL2003801077 120030429A5710 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01801DH78807 46033 LT WING L/E INBOARD VANE SLOT PLATING HOLES ELONGATED AT STA XILD 0.7095 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL-030412, ED3258. TRIMMED OUT ELONGATED HOLES SKIN AREA IAW EO DHL-030412, ED3258. FABRICATED DOUBLER (7075-T6 0.071) AND INTERNAL DOUBLER (7075-T6 0.050) AND FILLER (7075-T6 0.063) IAW EO DHL-030412, ED3258. CLEANED, TREATED AND PRIMED INNER SIDE OF FILLER, DOUBLER AND INTERNAL DOUBLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLERS IAW EO DHL-030412, ED3258, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030521000202003052100020WP 2003 5 21 DHL2003801060 120030409A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E FORMER CRACKED 0.500 INCH AT XFS 354.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-00. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE AND NEW FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521000242003052100024WP 2003 5 21 DHL2003604512 120030424A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD L/E FORMER AT STA XFS 797.500 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLED DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030515000302003051500030EU 2003 5 15 03124317 120030504A2910141910013 HOSE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM CHAFED A VTZAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27317UE 41031 DURING CRUISE OF THE FLIGHT FROM ROA TO IAD, THE CREW REPORTED HAVING LOST HYDRAULIC PRESSURE AND THAT HYDRAULIC QUANTITY HAD DROPPED TO ZERO. AN EMERGENCY WAS DECLARED AND THE FLIGHT CONTINUED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS STOPPED AND DEPLANED ON THE RUNWAY AND TOWED TO THE GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE RT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE HOSE (CHAFED)AND SERVICED THE HYDRAULIC SYSTEM. OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030515000672003051500067EA 2003 5 15 SWIA200311921 120030425A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07935SW 7725 ON APPROACH TO SBA, THE RIGHT FLIGHT SPOILER MESSAGE ANNUNCIATED WITH A SLIGHT ROLL TO THE LEFT. UPON LANDING, THE RIGHT SPOILER DID NOT DEPLOY WITH GLDS. PERFORMED FUNCTIONAL CHECK OF FLIGHT SPOILERONS AND GROUND SPOILERS SEVERAL TIMES. ALL CHECKS NORMAL WITH NO FURTHER DISCREPANCIES AT THIS TIME. 2L72 4F RTA21EA 20030515000702003051500070 2003 5 15 SWIA200311924 420030429A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO NR 1 AUTOPILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07393SW6644 6644 120330 CAPTAIN'S AUTOPILOT SPONTANEOUSLY DISENGAGES WITH CORRESPONDING RED A/P LIGHTS AND AURAL WARNING. CAPTAIN FLIGHT DIRECTOR AND F/O'S A/P OPERATE NORMALLY. REPLACED NR 1 APC-65B. OPS CHECK GOOD. 2L72 4T RTA31SO 20030515001412003051500141NM 2003 5 15 AWXA200300499 120030411A5310654687781 BEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON SHEAR BEAM WEB, RT MAIN LANDING GEAR WHEEL WELL STRINGER 18A RT, BS 706. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; INSTALLED REPAIR KIT PARTS IAW BOEING SERVICE BULLETIN 737-53-1066, EO 53-14-09, PART III, PARA D2. 2L72 4F RTA16WE 20030515001532003051500153 2003 5 15 SWAA031069 420030513A2565D31354 SLIDE BOEING737 7373H4 1384600NM PAX DOOR DISLODGED A SWAAO OTHER O OTHER TXTAXI/GRND HDL 1 SW29624SW 27934 UPON ARRIVAL TO THE GATE, FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030606000562003060600056EA 2003 6 6 COMA0360240 120030516A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01956CA 7105 FLIGHT 5575 DURING TAKE OFF ROLL RECEIVED A STABILIZER TRIM CAUTION, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE LEFT AND RIGHT PITCH TRIM DISCONNECT SWITCHES. 2L72 4F RTA21EA 20030606000572003060600057EA 2003 6 6 COMA0360241 120030516A3260 ROLLER CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01920CA 7022 FLIGHT 5927 DURING APPROACH RECEIVED A GEAR DISAGREE CAUTION. ADJUSTED THE NLG UPLOCK ROLLER 2L72 4F RTA21EA 20030606000742003060600074NM 2003 6 6 03FDEA00775 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP I/B HINGE (FLAP SIDE) AFT ATTACHMENT POINT AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030609000052003060900005WP 2003 6 9 ARWA20030504 120030514A2910 LINE DOUG DC8 DC861 3021952WP NR 2 ENGINE LEAKING A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO1929UA 46159 DURING CRUISE, LOST HYDRAULIC QUANTITY FOLLOWED THE LOSS OF HYDRAULIC FLUID OR PRESSURE. ABNORMAL OR EMERGENCY CHECKLIST. REMOVED AND REPLACED FLEX HYDRAULIC LINE ON NR 2 ENGINE PER MM 29-10-12. RUN UP CHECK ACCOMPLISHED AS PER MM 71-00-0 NO LEAK FOUND IT AT NORMAL. 2L74 4F 4A25 20030609000212003060900021WP 2003 6 9 ARWA20030216 120030215A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198968U 46069 DURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 440 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 440 IAW STC SA1063SO AND SA1377SO. 2L74 4F 4A25 20030609000442003060900044NM 2003 6 9 C1HA200396009 120030520A5347 SEAT TRACK BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 PITTING CORROSION AND GOUGING ON NR 2 SEAT TRACK AT LBL 22 BETWEEN BS 480 & 620. 2L73 4F RTA3WE 20030609000732003060900073EA 2003 6 9 QXEA0300625 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 PDX-RIVET DAMAGED AT FS 364, 3 INCHES ABOVE STRINGER 17R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609001412003060900141NM 2003 6 9 DHL2003780009 120030520A5270 CAM BOEING727 727223 1384074NM PAX DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01780DH 22006 FORWARD ENTRY DOOR LIGHT ILLUMINATED ON LANDING. ADJUSTED MOST UPPER FORWARD CAM HOUSING PER BMM CHAPTER 52-11-01, OPS CHECKED GOOD ON GROUND. 2L73 4F A3WE 20030609001852003060900185NM 2003 6 9 CA030515002 120030304A2913570347 PUMP DHAV DHC8 DHC8315 2809010NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE HYD SYSTEM FAILED W O OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CA (CAN) DURING APPROACH TO AIRPORT, NR 2 LIGHT HYD PUMP FAULT. LOSS OF HYD NR 2 FLUID (QTY 4). PAN-PAN CALL DECLARED & A/C RETURNED TO DEPARTURE AIRPORT. QRH PROCEDURE FOLLOWED & A/C LANDED WITHOUT EVENT. EDP NR 2 FAILURE OR PRESSURE MANIFOLD FAILURE (LEAKAGE) UNIT CLEANED & VISUALLY INSPECTED. ROTATION CHECK CARRIED OUT, SATISFACTORY. UNIT RELEASED FOR CONFIRMATION TEST, RETURNED FOR DRAFT SEAL LEAK. UNIT PARTIALLY DISASSEMBLED TO INVESTIGATE FAULT. PARENT THREADS STRIPPED IN HOUSING. MATING RING & ELEMENT WORN, PISTON SHOES WORN. EDP NR 2 REPLACED. SYS NR 2 RETURN FILTER REPLACED. SYS NR 2 PRESSURE MANIFOLD REPLACED. CASE DRAIN FILTER REPLACED. SYS NR 2 BLEEDING & REFILLING.A/C RELEASED INTO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030610000052003061000005 2003 6 10 HEEA086724 420030522A2312064105430 TRANSCEIVER BOLKMS105 BO105S 5626006EU VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 TRANSCEIVER WON'T TRANSMIT. IN SHOP REPAIR. 1G72 3U H3EU 20030610000372003061000037NM 2003 6 10 P5CA0300880 120030524A2160 CONTROLLER BOEING747 74746NF 13848BTNM CABIN MALFUNCTIONED A P5CAO OTHER O OTHER CRCRUISE 1 WP23454PA 30812 ZONE TEMP: CABIN FILLER WITH SMOKE - RESET - TEMP STARTED DOWN - TEMP TO 36 SMOKE AGAIN. T/S SYSTEM ORDERED ZONE TEMP CONTROLLER DEFERRED TRIM AIR SYSTEM MEL 21-61-9B CATC. INSPED TRIM AIR DUCTS AND VLVS. NO DEFECTS NOTED. FAULTY ZONE TEMP CONTROLLER 2L74 4F RTA20WE 20030611000212003061100021WP 2003 6 11 GTIA030331 120030503A5730 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE LT WING CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23800NK 49144 LT WING LE PANEL 1117C CORROSION AT FASTENER HOLES. FABRICATED DOUBLER. INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20030611000252003061100025WP 2003 6 11 GTIA030320 120030414A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 MID CARGO FS 695, INTERCOASTAL CORRODED AND TOOL MARKS STR 29L. FABRICATED NEW INTERCOSTAL. PRIOR TO STEP 5, REMOVED DAMAGED INTERCOSTAL. INSTALLED INTERCOSTAL. 2L72 4F4 F A6WE E2EA 20030611000352003061100035WP 2003 6 11 MEX2003163 120030508A7711LG80E1 INDICATOR DOUG DC9 DC987 3022087WP EPR FAILED W ASMFED ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23803ML 49726 AIRCRAFT RETURN TO PLATFORM DUE TO LT ENGINE EPR INDICATION FAILURE. DURING REVISION THE INDICATION ON EDP IS LESS THAN 1, THEREFORE, THE LT ENGINE WAS SHUTDOWN. THE EPR TRANS WAS REPLACED IAW MM, TEST CORRECT. 2L72 4F RTA6WE 20030611000452003061100045GL 2003 6 11 CA030409002 220030211A726123063371 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE DISINTEGRATED W D RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) UPON INSTALLATION OF OVERHAULED ENGINE, DURING INITIAL GROUND RUN, AME NOTICED EXCESSIVE OIL LEAK FROM OIL COOLER BLOWER PAD (FRONT SPARE ACCESSORY DRIVE PAD). ENGINE WAS SHUT DOWN.UPON INSPECTION, WHEN OIL COOLER BLOWER WAS REMOVED, IT WAS FOUND THAT THE RESERVOIR WASFULL OF OIL AND THE SEAL HAD APPROXIMATELY .333 OF ITS LIP EITHER CRACKED OR MISSING (SEE ATTACHED PHOTO). IT WAS NOTED THAT THE SEAL HAD BEEN MODIFIED TO P/N 23063371 IAW CEB 72-3260, BY REMOVINGTHE SEAL SPRING.IT WAS ALSO DETERMINED THAT THE ENGINE HAD UNDERGONE A FULL TEST BUT THE SEAL FAILURE HAD NOT BEEN DISCOVERED BECAUSE THE SPARE ACCESSORY PAD WAS BLANKED OFF AND SEALED. 1G72 3U3 U H1NE E1GL 20030611000612003061100061CE 2003 6 11 CA030515005 120030414A2425ALV9407 ALTERNATOR CESSNA414 414 2075908CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C93 GL ENGINE FAILED W D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 CA (CAN) ON TAKEOFF ROLL ALTERNATOR (RT) FAIL LIGHT CAME ON. TAKE-OFF ABORTED PRIOR TO BECOMING AIRBORNE. 1L72 3O3 ORTA7CE E8CE 5 CP22EA 20030611000682003061100068NE 2003 6 11 HEEA086552 120030522A261247320501 FIRE DETECTOR SKRSKYS76 S76C 8143008NE ENGINE INOPERATIVE W HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 FIRE DETECTOR INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20030602000682003060200068 2003 6 2 CA030424008 420030414A22972C610Y20RD WIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE AUTOPILOT SYS CHAFED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA (CAN) AUTO PILOT AND AUTO THROTTLE DISENGAGES C/B C-18 POP OUT. THE DFGS AND AILERON SERVO WERE REPLACED AND FUNCTIONAL CHECK WERE CARRIED OUT, AIRCRAFT RETURN TO SERVICE. ON THE SECOND FLIGHT AUTO PILOT NR 1 TRIP ALONG WITH THE AUTO THROTTLE AND C/B C18 POP OUT. AIRCRAFT STARTED TO OSCILLATED IN FLIGHT. QR A COMPLETED YAW DAMPER OFF RUDDER HYD LEVER - MAN. OSCILLATION STOP.WIRE 2C610Y20RD FOUND SHAFING ATUPPER SECTION OF VERTICAL FIN (28 VAC FEED FOR RT ELEVATOR POSITION SENSOR). WIRE ISOLATED AND AREPAIRED. SYSTEM CHECK SERVICEABLE IAW MM 22-00-00 P202. 2L72 4F4 FRTA6WE E9NE 20030602000872003060200087NM 2003 6 2 DL73S030488 120030523A7933 BULB BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 ENG TEMP MALFUNCTIONED A DALAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO27307DL75536 695240 23079 695240 NR 1 OIL TEMP ERRATIC FLUX PLUS OR MINUS 10 DEGREES UPPER GREEN BAND, THEN WENT INTO YELLOW BAND. ALL AREAS PLUS OR MINUS 10 DEGREES. FLUX STAYED IN YELLOW UP TO 15 MINUTES. PRECAUTIONARY SHUTDOWN PER POM. REPLACED OIL TEMP BULB. 2L72 4F4 FRTA16WE E2EA 20030602000952003060200095 2003 6 2 SWAA031187 420030527A256565C19901 CABLE BOEING737 7373Q8 1384670NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030602001682003060200168EA 2003 6 2 A6WA200340064 120030504A5320 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 DAMAGE AT EXISTING REPAIR ON PAX DOOR SEAL STRIKER FS 310, LOWER FRAME LATCH. REMOVED DAMAGED SECTION OF SEAL STRIKER AND INSTALLED A NEW SECTION OF SEAL STRIKER IAW REO 601R-52-11-008 ISSUE B. (M) 2L72 4F RTA21EA 20030602001712003060200171NM 2003 6 2 AALA20030482 120030420A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 28B INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030602001762003060200176NM 2003 6 2 AALA20030535 120030421A3397 WIRE BOEING767 767323 1385205NM CABIN CHAFED A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21372AA 25199 SFO - DURING OVERNIGHT MAINTENANCE CHECK OF THE FORWARD CARGO LOADING SYSTEM A CIRCUIT BREAKER WAS POPPING. WHEN RESET IT WAS OBSERVED THAT THE SMOKE WAS COMING FROM THE RIGHT LOWER SIDEWALL AREA. REMOVED PANEL AND NOTED A DAMAGED WIRE BUNDLE. POSSIBLE FUSELAGE REPAIR MAY HAVE CAUSED THE WIRES TO CHAF. INSTALLED TWO NEW CONNECTOR PLUGS AND FABRICATED BRACKET FOR CONNECTOR PLUGS. (M) 2L72 4F RTA1NM 20030602001782003060200178NM 2003 6 2 AALA20030522 120030503A3350 SOCKET BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21755AN 30263 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 35G INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SOCKET AT 35G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030604000182003060400018SO 2003 6 4 SIMA200311311 120030419A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 DURING AN IMBV INSPECTION A PREVIOUS REPAIR ON THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR AND CLEANED THE AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB-145/1142 REV 21, CHAPTERS 53-21-10 FIG 201. (M) 2L72 4F RTT00011AT 20030604000222003060400022EA 2003 6 4 SIMA200302702 120030124A24344120T07P01 ALTERNATOR CNDAIRCL600 CL6002C10 1390015EA LT ENGINE INOPERATIVE A SIMAE ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 SW21503AE 10021 DURING TAXI CREW REPORTED AND UNCOMMANDED ENGINE SHUTDOWN OF THE LEFT ENGINE. CREW FOLLOWED CHECKLIST AND RESTARTED ENGINE. ENGINE SHUTDOWN AGAIN AFTER APPROXIMATELY SIX MINUTES. AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE FOUND THE PERMANENT MAGNET ALTERNATOR TO BE INOPERATIVE. PMA WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030604000252003060400025SO 2003 6 4 SIMA200312601 120030430A27503631101007 LEVER EMB 135 EMB135LR 3260305SO TE FLAP INOPERATIVE A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21711PH 145235 DURING APPROACH CREW REPORTED THE FLAPS FAILED. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030604000302003060400030NM 2003 6 4 USAA030046 120030428A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 CLT - FOUND INTERCOSTAL WEB CRACKED, STATION 660 AT S14L. FABRICATED WEB PER BOEING DRAWING 143N8339 PER SRM 53-30-15. (M) 2L72 4F RTA2NM 20030604000372003060400037SO 2003 6 4 SIMA200312710 120030415A531014522460013 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 THIS IS A LEVEL 2 FINDING FOUND DURNG AN IMBV INSPECTION, CENTER FLOORBEAM GUSSET CORRODED IN GALLEY. REMOVED AND INSTALLED SERVICEABLE CENTER FLOOR GUSSET IN GALLEY IAW EMB 135 SRM 51-40-02/06, 51-20-03. (M) 2L72 4F RTT00011AT 20030604000442003060400044SO 2003 6 4 SIMA200310608 120030416A2913YB203A PUMP EMB 135 EMB135LR 3260305SO HYD SYSTEM INOPERATIVE A SIMAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SW21704PG 145174 DURING LANDING CREW REPORTED LOSING HYD SYSTEM 1 AND HAD PROBLEM GETTING GEAR DOWN AND LOCKED. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. AIRCRAFT WAS TOWED TO THE GATE FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE NR 4 HYDRAULIC PUMP IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030604000512003060400051WP 2003 6 4 UPS03840466 120030415A53204772397U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, STATION 1700 LONGERON 11L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 4772397 AND SRM. 51-1-20D 2L74 4F RT4A25 20030604000522003060400052WP 2003 6 4 UPS03840467 120030407A2810 FITTING DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, NR 4 ALT FWD AND AFT BOOST PUMP MOUNT FITTINGS ARE CRACKED (2EA FITTIN GS) REMOVED FWD AND AFT CRACKED BOOST PUMP FITTINGS IAW DC8 SRM 51-1-20D . LOCATED, DRILLED AND DEBURRED 2 EA NEW FITTINGS P/N 3645612U PO SP O903876 AND 3645611U PO SPO903618 IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20030609001282003060900128EU 2003 6 9 MALA030280 120030521A61208210163 GOVERNOR SAAB SF340 SF340A 7850100EU OVERSPEED MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1579XJ 340A079 RT PROP RPM SLOWED AFTER TAKEOFF. RT PROP RPM UNDERSPEED NOTICED AFTER TAKEOFF (1280 RPM) PROCEEDED IN ACCORDANCE WI/QRH AND RETURNED FOR LANDING. TORQUE MOTOR LOCKOUT WAS ACHIEVED, BOTH CONDITION LEVERS WERE AT MAX PRIOR TO THIS. AIR RETURN TO CRW. MAINTENANCE REPLACED RT PROP OVERSPEED GOVERNOR IAW SF340 MM CHAP. 61. ALL CHECKS GOOD AT THIS TIME. PN 8210-163, SN/ON 2163906. 2L72 4T RTA52EU 20030609001302003060900130EU 2003 6 9 MALA030277 120030504A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15525XJ E2350 DURING C-CHECK INSPECTION IN CVG, NR 1 SEAT TRACK HAS CORROSION FROM FRAMES 18-20A. MAINTENANCE REPAIRED SEAT TRACKS IAW EO A53026. REF 409 118107 FOR DETAIL. A/C RELEASE DATE 5/21/2003 2H74 4F RTA49EU 20030513002942003051300294NM 2003 5 13 USAASB03031 120030228A335030043229 LIGHT BOEING737 7373B7 1384580NM EXTERIOR FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US 22958 ATL - MAINTENANCE REPORTED THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACD THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT/SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030514000182003051400018EA 2003 5 14 A6WA200340056 120030409A2621 BOTTLE CNDAIRCL600 CL6002B19 1900309EA NR 2 FIRE DISCHARGED A A6WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL31424AW 7656 ENGINE FIRE NR 2 LOW LOW PSI CAS MESSAGE. REMOVED AND REPLACED ENGINE NR 2 FIRE BOTTLE IAW 26-20, PERFORMED OPS TEST OF BOTTLE/SYSTEM. (M) 2L72 4F RTA21EA 20030514000202003051400020EA 2003 5 14 ASOA03144 120030402A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING AN 'A' CHECK AT MCN, THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20030514001042003051400104 2003 5 14 SWAA031005 420030505A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT PAX DOOR DISLODGED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29370SW 26597 AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030514001162003051400116 2003 5 14 SWAA031027 420030508A2565 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20030514001512003051400151NM 2003 5 14 SWAA031051 120030510A5754 SKIN BOEING737 737317 138447PNM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT CRACKED AT LOWER T/E AFT ROW OF FASTENERS. REPAIRED NR 6 L/E SLAT PER SWA EA. 2L72 4F RTA16WE 20030514001682003051400168NM 2003 5 14 P5CA0300869 120030412A5532 PANEL BOEING747 747249F 1384849NM VERICAL STAB DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 VERTICAL STAB AUX SPAR PANEL FIN STA 395 TO FIN 420 DELAMINATED. REPAIRED PER SRM 51-30-02 BOEING PAO SIN 03-00011M. 2L74 4F A20WE 20030514001852003051400185NM 2003 5 14 03FDEA00662 120030501A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-224-01) ON FLOORBEAM UPPER FLANGE BS 480 LBL 25 TO LBL 45 WL 208. REPAIRED PER EA 7-5310-69493. 2L73 4F RTA3WE 20030514001902003051400190NM 2003 5 14 250TR0017 120030429A5321 FLOOR PANEL BOEING737 7372K5 138448XNM CARGO BAY DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 HOLE IN NR 2 FLOOR PANEL IN FORWARD CARGO BIN. REPAIRED PER SRM 51-40-2 FIG 1. 2L72 4F RTA16WE 20030515000072003051500007EA 2003 5 15 03126654 120030506A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 DURING MAINTENANCE INSPECTION, THE NR 3 RT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515000152003051500015SO 2003 5 15 SWIA200311938 120030429A5210 SWITCH EMB 120 EMB120ER 3260203SO PAX DOOR OUT OF POSITION A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07186SW 120034 HYDRAULIC LOCK ON MAIN CABIN DOOR WITH OCCASIONAL FORWARD ACTUATOR LIGHT ON OVERHEAD PANEL. PERFORMED QRH PROCEDURE AND THE DOOR OPENED. REPOSITIONED SWITCH IN HOUSING. TESTED AND DOOR WORKS OK. WORK PERFORMED IAW EMB MM 52-12-00. 2L72 4T RTA31SO 20030515000552003051500055CE 2003 5 15 DXTA200300017 120030421A3260327 INDICATOR CESSNA500 560CESSNA 2076750CE MLG INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07305QS 5600261 LEFT MLG INDICATOR LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION ON FINAL TO IAH. PERFORMED EMERGENCY CHECKLIST AND BLEW GEAR DOWN. 2L72 4F RTA22CE 20030515000642003051500064CE 2003 5 15 GLBA2003056 120030425A561010138402522 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03255GL2194 UE255 FIRST OFFICER`S WINDSHIELD SHATTERED. REMOVED AND REPLACED RT WINDSHIELD. 2L72 4T RTA24CE 20030515000952003051500095EA 2003 5 15 03130649 120030510A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27649BR 7414 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515001512003051500151EU 2003 5 15 141801 120030501A3500 OXYGEN SYSTEM SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE LEAKING A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17152CQ 152 FLIGHT 4463 TTN-BED. SHORTLY AFTER TAKEOFF A/C LEVELED OFF AT 13,000 FT CREW NOTICED THE OXYGEN PRESSURE BLEEDING OFF. PRESSURE STARTED AT 1500 PSI AND BLED DOWN TO 500 PSI IN ABOUT 20 MINUTES. THE LOW LEVEL OXYGEN LIGHT ILLUMINATED. THE CREW SHUT OFF THE OXYGEN SYSTEM AT 500 PSI AND THE SYSTEM PRESSURE CONTINUED TO BLEED OFF DOWN TO ABOUT 400 PSI. A/C RETURNED TO TTN AND TAKEN OUT OF SERVICE AT 1320. CREW DID NOT DECLARE AN EMERGENCY, NO OTHER SYSTEMS NOTABLY EFFECTED. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030515001572003051500157NM 2003 5 15 SWAA031073 120030510A53106558280 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA SHEAR TIES CRACKED AT BS 360, STRINGERS 14L & 14R. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20030515001662003051500166NM 2003 5 15 AWXA200300468 120030414A531069717701 SHEAR TIE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON VERTICAL ATTACH ANGLE (SHEAR TIE) AT FORWARD AND AFT SIDES OF BS 597, RT OUTBOARD SIDE. MAINTENANCE TRIMMED OUT DAMAGE ON SHEAR TIE AND FRAME AT FLANGE BEND; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS AND REPAIR ANGLES PER DWG 69-71770; INSTALLED REPAIR PARTS IAW AWA ER 15-5362-03119-SS4. 2L72 4F RTA16WE 20030515001702003051500170EU 2003 5 15 AWXA200300488 120030424A5414D54630462201 PANEL AIRBUS320 A320231 3930325EU LT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-03 CHECK A 1.25 INCH CRACK WAS FOUND ON LT PYLON INBOARD SIDE AT FORWARD UPPER CORNER OF PANEL 414CR ATTACH POINT, STA 537. MAINTENANCE CUT OUT DAMAGED SECTION OF EXTRUSION PROFILE AT PYLON STA 537; FABRICATED A FILLER AND REPAIR SPLICE; INSTALLED REPAIR PART IAW A320 SRM 54-52-12 PG 215-220 FIG 203. 2L72 4F RTA28NM 20030515001842003051500184EU 2003 5 15 AWXA200300506 120030427A5311D53370239200 FRAME AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-03 CHECK A .0625 INCH CRACK WAS FOUND AT THE FIFTH FASTENER HOLE DOWN ON FRAME 39, STR 14 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME 39 AT STR 14 LT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA EO 53-14-20 FIG 3R. 2L72 4F RTA28NM 20030515001912003051500191EU 2003 5 15 AWXA200300516 120030426A5330D53470410208 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 60 AND 61, AT BL 0, UNDER ANTENNA CUTOUT. MAINTENANCE CUT OUT CORROSION ON EXTERNAL SKIN BETWEEN FRAMES 60 AND 61, AT BL 0; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11 PG 203, 208, 210-212 FIG 203. 2L72 4F RTA28NM 20030515001922003051500192EU 2003 5 15 AWXA200300517 120030426A5330D5347040820000 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 62 AND 63, STR 42-43 LT, UNDER IFPC ANTENNA. MAINTENANCE CUT OUT CORROSION ON EXTERNAL SKIN BETWEEN FRAMES 62 AND 63, STR 42-43 LT, UNDER IFPC ANTENNA; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11 PG 203, 209-214 FIG 203. 2L72 4F RTA28NM 20030515001992003051500199NM 2003 5 15 AWXA200300455 120030422A53106546527 SHEAR TIE BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR TIE AT BS 500B, BETWEEN STR 28 LT AND 28 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF SHEAR TIE AT BS 500B, BETWEEN STR 28 LT AND 28 RT; FABRICATED A REPAIR ANGLE AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, PG 213. 2L72 4F RTA16WE 20030520000052003052000005EA 2003 5 20 CA030401007 120030327A29106047523865 LINE CNDAIRCL604 CL604 1900301EA GE CF34 CF343B1 NE HYD SYSTEM CHAFED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) NR 1 EDP HYDRAULIC CASE DRAIN LINE WAS CHAFING AGAINST NR 1 EDP HYDRAULIC PX LINE, DUE TO INSUFFICIENT CLEARANCE/SYSTEM VIBRATION. CHAFING OCCURRED OVER A LENGTH OF APPROXIMATELY 4 INCHES, AND WAS BEYOND ALLOWABLE LIMITS. 2L72 4F4 FRTA21EA E15NE 20030520000062003052000006SW 2003 5 20 CA030421009 120030403A28106875224 ACCUMULATOR BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUEL SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING AIR LEAK CHECK & AFTER FUEL SYSTEM MAINTENANCE, A LEAK WAS DETECTED AT END OF ACCUMULATOR, WHERE MALL ADAPTER IS ATTACHED. 1G71 3U3 U H2SW E4CE 20030520000082003052000008EU 2003 5 20 CA030422002 120030417A7603A552326 CONTROL CABLE STBROSSD3 SD360 8100606EU PWA PT6 PT6A65AR 52043NE POWER LEVER BROKEN W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 CA (CAN) ON APPROACH THE PILOT COULD NOT GET RT ENGINE POWER LOW ENOUGH FOR APPROACH POWER SETTING. A/C LANDED AT HIGHER THAN NORMAL POWER SETTING AND AFTER LANDING NEITHER BETA OR REVERSE SELECTIONS WERE POSSIBLE. MAINT FOUND POWER LEVER MOVEMENT IN COCKPIT LIMITED IN FORWARD DIRECTION AND NO MOVEMENT IN EITHER DIRECTION WAS VISIBLE AT ENGINE. INVESTIGATION REVEALED THE RT POWER CONTROL TELEFLEX CABLE HAD BROKED INSIDE ITS CONDUIT. LOCATION OF BREAK WAS AT A 180 DEGREE BEND IN CABLE JUST BELOW ENGINE CONTROL CAM CLUSTER. 2H72 4T4 T A41EU E4EA 20030520000222003052000022WP 2003 5 20 GTIA030271 120030413A5532 PANEL DOUG DC9 DC983 3022083WP VERTICAL STAB CHAFED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 FOUND RIGHT VERTICAL STAB ACCESS PANEL CHAFING ON INTERIOR. FABRICATED DOUBLER. LOCATED AND DRILLED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20030520000242003052000024SO 2003 5 20 SIMA200309612 120030325A531014522459003 BEAM EMB 135 EMB135KL 3260302SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21804AE 145487 THIS IS A LEVEL TWO FINDING FOUND DURING AN MBV INSPECTION, CENTER BEAM RAMP IS CORRODED AT FRAME 20. REMOVED CORRODED CENTER BEAM RAMP AND INSTALLED NEW SERVICEABLE RAMP IAW EMB 140 SRM 51-40-02, 51-20-03. (M) 2L72 4F RTT00011AT 20030520000302003052000030WP 2003 5 20 GTIA030264 120030220A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - AFT PIT CORRODED INTERCOSTAL AT FS 1145-1155 4 INCHES RBL. REMOVED INTERCOSTAL FROM AFT PIT FS 1145-1155 RBL 4 INCHES. FABRICATED INERCOSTAL. INSTALLED INTERCOSTAL AT STATION 1145-1155 RBL 4. (M) 2L72 4F RTA6WE 20030520000322003052000032SO 2003 5 20 SIMA200309902 120030407A5610NP15131111 WINDSHIELD EMB 135 EMB135LR 3260305SO COCKPIT CRACKED A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21713AE 145249 JFK - FLT 4583 - DURING CLIMB, CREW REPORTED THE CAPTAINS WINDSHIELD CRACKED. CREW DIVERTED TO JFK AND LANDED SAFELY WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030514001272003051400127NM 2003 5 14 SWAA031013 120030506A335065C27093 LIGHT BOEING737 7372T4 1384492NM MID CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F A16WE 20030514001392003051400139 2003 5 14 SWAA031039 420030509A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030515000232003051500023EA 2003 5 15 SWIA200311944 120030331A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FS 484 RBL 36 RT INTERCOSTAL O/B FL6 CRACKED. FOUND DURING C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 -A-. NDT-HFEC CARRIED OUT IAW REO 601R-53-41-059. NO CRACKS NOTED. 2L72 4F RTA21EA 20030515000402003051500040EA 2003 5 15 SWIA200311909 120030303A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 LEFT WING FUEL PANEL REBATES HAVE CORROSION UNDER PANELS 510AB, 540AB, 540CB, 540DB, 540FB, 550AB. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-57-21-030 REV A UNDER PANEL 510AB MAX MAT'L LOSS .002, 540CB MAX MAT'L LOSS .008, 540DB MAX MAT'L LOSS .004, 540FB MAX MAT'L LOSS .003, 550AB MAX MAT'L LOSS .004, 540AB DAMAGE BEYOND LIMITS OF THIS REPAIR. HFEC INSPECTION C/O ON BLEND WING FUEL TANK LID REBATES AS REQUIRED IAW REO 601R-57-21-030. NO CRACKS FOUND. 2L72 4F4 FRTA21EA E15NE 20030515001052003051500105NM 2003 5 15 03FDEA00619 120030423A2752 FITTING DOUG MD11 MD11 3023602NM ACTUATOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR FITTING (2 EACH) FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69217 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030515001652003051500165NM 2003 5 15 AWXA200300467 120030410A53126516300 BULKHEAD BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON WEB DURING ULTRASONIC INSPECTION OF FORWARD PRESSURE BULKHEAD BS 178, 2 INCHES ABOVE WL 195 AT LBL 5.7. MAINTENANCE CUTOUT DAMAGED SECTION OF WEB; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-11, FIG 1, PG 1-8. 2L72 4F RTA16WE 20030515001942003051500194NM 2003 5 15 AWXA200300519 120030508A3260 ACTUATOR BOEING757 757225 1384959NM LT MLG FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 ON CLIMBOUT RECEIVED MLG DOOR DISAGREE INDICATION AFTER MLG RETRACTION. PERFORMED MLG DISAGREE CHECKLIST: LT MLG GREEN WITH GEAR HANDLE OFF, NOSE & RT MAIN BLANK. ACFT FEEL INDICATED LT MLG NEVER RETRACTED, TURNED BACK & LANDED WITHOUT EVENT. MX R & R MLG DOOR-OPERATED GEAR SEQUENCE VALVE, DID NOT CORRECT PROBLEM. AFTER DUPLICATING PROBLEM & GETTING MLG TO RETRACT BY APPLYING WEIGHT TO BACK OF TRUCK, MX REPLACED LT MLG TRUCK POSITIONER ACT, AS A PRECAUTION REPLACED LT TRUCK TILT PROXIMITY SENSORS 1 & 2, PROBLEM STILL PERSISTS. R & R DOWNLOCK ACTUATOR, OPS & LEAK CK GOOD, GEAR CYCLED W/O DEFECT. VENDOR BENCH TEST & TEARDOWN OF DOWNLOCK ACTUATOR CONFIRMED FAILURE OF UNIT. 2L72 4F RTA2NM 20030515001982003051500198NM 2003 5 15 AWXA200300454 120030423A53206552878 WEB BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 3 INCH CRACK WAS FOUND ON CUSP WEB AT BS 1003, LBL 62. MAINTENANCE REMOVED CRACKED CUSP WEB AND ATTACH ANGLE AT BS 1003, LBL 62; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR WEB AND REMOVED ATTACH ANGLE IAW B737-300 SRM 51-40-02 PG 11-12. 2L72 4F RTA16WE 20030520000442003052000044NM 2003 5 20 AMTA200300535 120030421A3350 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11516AT 27972 EMERGENCY EGRESS FLOOR PATH LIGHTING SYSTEM INOPERATIVE FROM ROW 11 TO ROW 13. RECONNECTED LOOSE WIRING TO TERMINAL PER WDM 20. (M) 2L72 4F RTA2NM 20030520000452003052000045SO 2003 5 20 SIMA200311308 120030331A531014522459003 BEAM EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION GALLEY CENTER BEAM RAMP SUPPORT CORRODED. REMOVED AND REPLACED RAMP SUPPORT IAW EMB 145 51-40-02. (M) 2L72 4T RTT00011AT 20030520000542003052000054WP 2003 5 20 GTIA030273 120030409A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 FTW - FOUND MAIN CABIN STATION 1041 TO STATION 1060 FLOOR PANEL DETERIORATED. FABRICATED A NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030520000612003052000061NM 2003 5 20 AMTA200300495 120030414A3350 SIGN BOEING737 73783N 13844HINM EMERGENCY LIGHTSBROKEN A AMTAK NONE O OTHER ININSP/MAINT 1 GL11308TZ 28244 R-2 EMERGENCY EXIT SIGN ABOVE FLOOR IS BROKEN. REPLACED EXIT LIGHT ASSEMBLY. CHECK GOOD. REF MM 33-50-00. (M) 2L72 4F RTA16WE 20030520000662003052000066SO 2003 5 20 SIMA200309609 120030328A532014522461011 GUSSET EMB 135 EMB135KL 3260302SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 THIS IS A LEVEL TWO FINDING FOUND DURING A MBV INSPECTION, GALLEY FORWARD DIAMOND GUSSET CORRODED. INSTALLED NEW DIAMOND GUSSET IN GALLERY AREA IAW EMB 140 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030520000702003052000070EU 2003 5 20 SIMA200311103 120030419A61207901996 ACTUATOR SAAB SF340 340B 7860101EU NR 2 PROP BROKEN A SIMAE ENGINE SHUTDOWN E VIBRATION/BUFFET APAPPROACH 1 SW21350CF 340B350 SGF - FLT 3617 - DURING APPROACH THE RIGHT ENGINE STARTED TO VIBRATE SEVERLY. CREW SHUT DOWN THE ENGINE AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO OTHER INCIDENTS. DURING POST FLIGHT ONE BLADE ON THE RIGHT PROPELLER DID NOT GO INTO FEATHER. MAINTENANCE REMOVED AND REPLACED THE RIGHT PROPELLER ASSEMBLY IAW W/C 47173. OPS AND LEAK CHECK WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. UPON TEAR DOWN OF THE PROPELLER MAINTENANCE FOUND ONE OF THE PROPELLER ACTUATOR YOKE ARMS HAD BROKEN OFF. (M) 2L72 4T RTA52EU 20030520000782003052000078CE 2003 5 20 2003F00257 120030401A2750100384040 MOTOR BEECH 1900 1900D 1154162CE TE FLAPS SHORTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO1987557 UE246 AFTER LANDING, DURING POST FLIGHT, BURNING ELECTRICAL ODOR COMING FROM CARGO AREA. REMOVED AND REPLACED FLAP MOTOR. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20030604000582003060400058WP 2003 6 4 UPS03840473 120030412A531046198102 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, RIGHT WHEEL WELL OUTBOARD STA. 940 UPPER BEAM FITTING IS CRACKED AT LONG. 24R REMOVED AND REPLACED FITTING I.A.W. DWG 4619810,AND SRM. 51-1-20D 2L74 4F RT4A25 20030604000602003060400060WP 2003 6 4 UPS03840475 120030421A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3 L-1 DOOR LWR AFT CORNER SKIN CRACKED 2 EA BY CUTOUT MARKED. REPAIRED LOWER AFT DOOR CORNER IAW DC8 SRM 53-2-0 FIG 15, TR 53-128, TR 53-155 AND REO G09193 2L74 4F RT4A25 20030604000712003060400071SO 2003 6 4 125401 120030425A55131159CSH205009 TAB GULSTMG1159 GIV 3980115SO LT ELEVATOR DELAMINATED E ERYAK NONE O OTHER ININSP/MAINT 1 CE07920DS5148 1254 DURING SCHEDULED MX, FOUND LT ELEVATOR TRIM TAB INBOARD TOP AND BOTTOM SIDE DELAMINATED BEYOND LIMITS. REMOVED TRIM TAB, REPAIRED IAW CHAPTER 27-04-00 AND RE-INSTALLED TRIM TAB 2L72 4F RTA12EA 20030604000742003060400074NM 2003 6 4 UPS03440488 120030411A5310 STRUCTURE BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 M/D - HAT SECTION FWD FLANGE UPPER AND LOWER SURFACE CORROSION. CORRODED HAT SECTION REPLACED AS PER SRM 51-10-01 PAGE 8. CORROSION BLEND OUT 0.030 X 1 X 1 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604000832003060400083NM 2003 6 4 UPS03440497 120030413A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 BS 1474 S-12L STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20030604000862003060400086NM 2003 6 4 UPS03440500 120030406A5414 SKIN BOEING747 747121 1384871NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 NR 3 PYLON ACCESS PANEL 473EL CUTOUT UPPER EDGE RIVET HOLE LOWER EDGE SUSPECT CRACK REVEALED AS MARKED. SKIN REPAIRED PER SRM 54-30-03 FIG 17B. 2L74 4F A20WE 20030604000892003060400089NM 2003 6 4 UPS03440503 120030410A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 BS 2320 FRAME CRACKED AT STRINGER 26L AS MARKED. BS 2320 BTN STR 24L - 34L FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2L74 4F A20WE 20030604000902003060400090NM 2003 6 4 UPS03440504 120030410A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, SEAT TRACK FOUND CORROSION AT BS 560 - 565 LBL 65. SEAT TRACK REPAIRED AT U/D BS 530 - 570 LBL 65 AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.040 X 1 X 10 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604001112003060400111NM 2003 6 4 UPS03440526 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 760 LT STR 16L FRAME FOUND CRACKED. FRAME REPAIRED AT BS 760 BETWEEN S-14L TO S-17L AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001312003060400131NM 2003 6 4 UPS03440551 120030413A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 1000 - 1020, S6L STRINGER CRACKED. BS 1000 S-6L STRINGER REPAIRED AS PER HX RS R53-21-35017 AND ENGINEERING FILE NUMBER ; 747-53-20138. 2L74 4F A20WE 20030604001362003060400136NM 2003 6 4 UPS03440556 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 M/D - BS 680 LT STR 17L FRAME INNER STRUCTURE FOUND CRACKED. FRAME REPAIRED AS PER HX RS R53-22-35010 & UPS RA 747-53-20131. 2L74 4F A20WE 20030604001412003060400141NM 2003 6 4 UPS03440561 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D BS 920 BET S23-24R FRAME FOUND CRACKED. BS 920 BETWEEN S23L TO S25L FRAME REPAIRED AS PER SRM 53-10-04 FIG.35. 2L74 4F A20WE 20030604001422003060400142NM 2003 6 4 UPS03440562 120030412A5320 SUPPORT BRACKET BOEING747 747121 1384871NM KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1095 LBL 9. CORROSION BLEND OUT (0.040 X 1 X 1 INCHES) SUPPORT BRACKET REPLACED AS PER SRM 51-10-01 P.8 2L74 4F A20WE 20030604001532003060400153NM 2003 6 4 UPS03440573 120030412A5320 STRINGER CLIP BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 540 LT STRINGER 15L, 16L & 17L TIE CLIP FOUND CORRODED. CORROSION BLEND OUT ( 0.009 X 1 X 3 INCHES) AT M/D BS 540 LT STR 15L TO 17L EXCEEDS LIMITATION. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG.8. 2L74 4F A20WE 20030530000702003053000070NM 2003 5 30 UIEA200300002 120030122A5710 BEAM BOEING747 747243B 1384830NM RT WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15516MC83946 22507 DURING CURRENT C-CHECK AT SIA, FOUND RT WING LE BEAM WEB CRACKED AT OLES 1200. CRACK REMOVED BY CUTTING THE WEB AT OLES 1190 AND DISCARDING THE INBOARD SECTION FROM OLES 1190 TO 1200. PERFORMED HFEC INSPECTION OF CUT EDGE TO ENSURE CRACK FREE CONDITION. NO ADDITIONAL CRACKING FOUND. FABRICATED REPLACEMENT WEB AND REINFORCING DOUBLERS. INSTALLED REPLACEMENT PARTS WITH REVETS PER SRM 57-20-03 FIG 7. (M) 2L74 4F A20WE 20030530000862003053000086NM 2003 5 30 DL733030478 120030519A5343 FITTING BOEING737 737347 1384647NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO272310 23596 CORROSION WAS FOUND IN THE LUG BORE AND AFT LUG FACE OF THE LT MLG SIDE STRUT FITTING AT FS 685. THE BORE WAS OVERSIZED AND THE FACE SPOTFACED TO REMOVE ALL CORROSION. A REPAIR BUSHING WAS INSTALLED IN THE BORE AND A WASHER INSTALLED TO FILL THE SPOTFACE. THE REPAIR WAS ACCOMPLISHED PER ER/A 385080-14. 2L72 4F RTA16WE 20030602000092003060200009SO 2003 6 2 SIMA200312712 120030420A532014522178005 CHANNEL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR SILL HAS CORROSION. REMOVED DAMAGED SILL AND INSTALLED NEW SERVICE DOOR SILL IAW EMB 145 SRM 51-20-03, 51-40-02/06 AND EMB CPM 5-21-04. (M) 2L72 4T RTT00011AT 20030602000562003060200056SW 2003 6 2 CA030425003 120030331A6320205040249003 BEARING BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA MAIN ROTOR MAKING METAL W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING 600 HR TRANSMISSION INSPECTION INPUT QUILL WAS REMOVED TO FACILITATE MAINTENANCE. BEARING DEFECTS WERE IDENTIFIED THAT REQUIRED REPLACEMENT PRIOR TO AIRCRAFT WAS RETURNED TO SERVICE. 1G71 4U4 U H4SW E22EA 20030602000862003060200086NM 2003 6 2 DL76L030487 120030523A2750 FCU BOEING767 767332 1382001NM TE FLAPS MALFUNCTIONED A DALAO OTHER N FALSE WARNING DEDESCENT 1 SO27188DN 27583 ON APPROACH AS FLAPS WERE GOING BETWEEN 5 AND 15 RECEIVED T/E FLAP DISAGREE EICAS AND DISCRETE LIGHT. C/W ABNORMAL CKLIST AND LANDED W/ FLAPS 20 AS JPER CK LIST. T/S PER FIM 27-51-00 FIG 105. TEST OK. NO FAULTS FSEU. 2L72 4F RTA1NM 20030602001152003060200115NE 2003 6 2 SWAA031183 220030527A72206497823000 PIN BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE NR 2 ENGINE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29428WN 29844 890279 DURING SCHEDULED A1 CHECK, SWA SI 11165-72, NR 2 ENGINE RETAINING RING PINS AND MID FLANGE FAN DISK PINS FAILED TORQUE PIN CHECK. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030602001262003060200126NM 2003 6 2 SWAA031164 120030522A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 747 AT STR 23R AND BS 970 AT STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030602001752003060200175NM 2003 6 2 USAASB03061 120030505A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 ATL - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 20, LEFT SIDE, RANDOMLY ILLUMINATE AT TIMES. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK, LOCATED IN THE AFT GALLEY, LEFT OF OVERHEAD LIGHT. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20030604000272003060400027EU 2003 6 4 USAASA03038 120030503A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19733UW 1205 DCA - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT IN THE AFT POSITION. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030604000352003060400035SO 2003 6 4 SIMA200312708 120030416A532014524131009 SUPPORT EMB 135 EMB135LR 3260305SO PAX DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 PASSENGER DOOR OPENING FORWARD THRESHOLD SUPPORT HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030604000652003060400065WP 2003 6 4 UPS03840480 120030414A53204750419501N STRINGER CLIP DOUG DC8 DC873F 302199FWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, STATION 1153 AT LONGERON 19R INSIDE HOLE HAS A CRACKED STRINGER CLIP. REMOVED AND REPLACED CLIP IAW DWG. 4750419 AND SRM. 51-1-20D 2L74 4F RT4A25 20030604001222003060400122NM 2003 6 4 UPS03440537 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 620, BET S17-18R, FRAME I/B STURCTUREFOUND CRACK. FRAME REPAIRED AS PER HX RS R53-22-35012 AND 747-53-20136. 2L74 4F A20WE 20030604001642003060400164NM 2003 6 4 UPS03440584 120030413A5610 FORGING BOEING747 747121 1384871NM RT WINDOW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 620 - 640 RT WINDOW FORGING FOUND CORROSION AT CUTOUT SKIN AFT AREA. CORROSION BLEND OUT (0.028 X 1 X 1 INCHES). WINDOW FORGING REINSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20030604001652003060400165NM 2003 6 4 UPS03440585 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 540 BET S24-25R FRAME FOUND CRACK. M/D BS 540 STR 24R - STR 26R FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20030604001662003060400166NM 2003 6 4 UPS03440586 120030414A532065B0500063 REVEAL BOEING747 747121 1384871NM PAX DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, L5 DOOR FWD FX CUTOUT UPPER REVEAL CRACKED AT STR 16. DOOR CUTOUT REVEAL FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20030604001682003060400168NM 2003 6 4 UPS03440588 120030408A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FWD CARGO COMPT - BS 500 S-39R TO 40R FRAME SHEAR TIE SURFACE CORROSION REVEALED. SHEAR TIE REPAIRED AT BS 500 STR 39 - 40R AS PER SRM 53-10-04 FIG 3. CORROSION BLEND OUT 0.030" X 1" X 1". 2L74 4F A20WE 20030604001752003060400175NM 2003 6 4 UPS03440595 120030412A575365B078801 RIB BOEING747 747121 1384871NM NR 9 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 9 VC FLAP O/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2,3 & 6. (VIEW FROM I/B). BOLT HOLES CORROSION REVEALED REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030520000802003052000080CE 2003 5 20 2003F00259 120030407A2697 WIRE BEECH 300 300BEECH 1152930CE BLEED AIR MELTED A RU3AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2174 FF9 CLIMBING THROUGH16,500 FT MSL, LT BLEED AIR LIGHT FLASHED THEN STEADY. FOLLOWED EMERGENCY PROCEDURE AND LANDED. DURING DESCENT, BLEED AIR FAIL LIGHT EXTINGUISHED. INVESTIGATION REVEALED THAT THE BLEED AIR SENSING LINE HAD A MELTED PLACE, WHICH CAUSED THE BLEED AIR LIGHT TO COME ON. SENSING LINE WAS REPLACED, AND SYSTEM OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T A24CE 20030520000862003052000086NM 2003 5 20 2003F00261 120030410A2611100064901 SMOKE DETECTOR BOEING727 727230 1384080NM UPPER CARGO DECKDEFECTIVE A RYNAO OTHER J WARNING INDICATION APAPPROACH 1 CE07303FV 21619 ON APPROACH INTO DAY, A MOMENTARY ACTIVATION OF MAIN CARGO FIRE SYSTEM, FOLLOWED IMMEDIATELY BY THE GREEN SYSTEM NORMAL LIGHT AND THEN YELLOW MAINTENANCE LIGHT. NO ACCOMPANING FIRE OR SMOKE NOTED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SMOKE DETECTOR IN POSITION 12, LEFT UPPER CARGO DECK. (M) 2L73 4F A3WE 20030520000882003052000088EU 2003 5 20 USAASA03034 120030421A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU PAX CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19714US 1046 THE AFT EMERGENCY POWER SUPPLY UNIT SHOWS FAULT. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. SYSTEM CHECKS OK. (M) 2L72 4F RTA28NM 20030520000902003052000090NM 2003 5 20 USAABB03061 120030416A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030520001042003052000104NM 2003 5 20 AALA20030419 120030405A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21750AN 30259 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LEFT LOWER FORWARD FACING EMERGENCY EXIT PATH LIGHTING IN THE G3 GALLEY COAT CLOSET WALL IS BROKEN. REPLACED FORWARD LEFT LOWER FORWARD FACING EMERGENCY EXIT PATH LIGHT ASSEMBLY ON THE G3 GALLEY COAT CLOSET WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030520001102003052000110NM 2003 5 20 AALA20030424 120030408A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139364 24045 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BY 1L AND 1R DOOR INOPERATIVE. SECURED EMERGENCY EXIT LIGHTS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520001242003052000124 2003 5 20 USAASA03033 420030421A2565D31516113 SLIDE AIRBUSA321 A321211 3930370EU RIGHT DEFECTIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19186US 1701 DURING TROUBLESHOOTING FOR AN 'EPSU EXT LOAD FWD L' FAULT MESSAGE, FOUND THE FORWARD RIGHT EMERGENCY ESCAPE SLIDE ALSO DEFECTIVE FOR HIGH RESISTANCE OF THE SLIDE LIGHTS. MAINTENANCE REPLACED THE R1 SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030520001412003052000141EA 2003 5 20 2003F00271 120030404A7830 SWITCH CNDAIRCL604 CL604 1900301EA THRUST REVERSER MALFUNCTIONED A UG8AO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23599DA 5498 RIGHT THRUST REVERSER UNLOCKED ON ENGINE START. BOTH THRUST REVERSER STOW SWITCHES WERE LEFT IN THE DEPRESSED POSITION. PLACED BOTH THRUST REVERSER STOW SWITCHES IN THE NORMAL POSITION. THRUST REVERSERS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030520001462003052000146EU 2003 5 20 ASOA03188 120030421A5320 ANGLE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN BNA, THE MAIN PASSENGER DOOR FORWARD THRESHOLD 'T' ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE MAIN PASSENGER DOOR FORWARD THRESHOLD 'T' ANGLE IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20030520001572003052000157EA 2003 5 20 ASOA03186 120030428A3350MS33386839 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 FLT 4480 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANTS ANNUNCIATOR EMERGENCY BLUE LIGHT ON THE CEILING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS ANNUNCIATOR EMERGENCY LIGHT LAMP ON THE CEILING EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030521000012003052100001EU 2003 5 21 MALA030266 120030510A36109303688100 HOSE SAAB SF340 340B 7860101EU BLEED AIR LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15411XJ 340B411 DURING CLIMBOUT ON FLIGHT NR 3105, RIGHT BLEED AIR LEAK LIGHT ON THE OVERHEAT A/C PANEL ILLUMINATED. QRH- LIGHT EXTINGUISHED AFTER BLEEDS WERE CLOSED. MAINTENANCE TRANSFERRED TO 409 NR 181703. REPLACED RT SIDE BLEED AIR FUSELAGE HOSE P/N 9303688-100 IAW AMM 36-11-00-2, PERFORMED ENGINE RUN WITH BLEEDS ON. OPS CHECK GOOD. 2L72 4T RTA52EU 20030521000042003052100004NM 2003 5 21 DHL2003783005 120030511A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01766AT 21999 ENGINE NR 3 ENGINE DETECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. DEFERRED PER DHL MEL 26-9 CAT-C NR 12894. REF DMI 12894; ENGINE NR 3 ENGINE DETECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. REPOSITIONED FIRE DETECTION LOOP NR 3 ENGINE FOR CLEARANCE PER M/M 26-11-00, OPS CHECKED OK. 2L73 4F A3WE 20030521000102003052100010WP 2003 5 21 DHL2003801009 120030419A5710576998591 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01801DH78807 46033 LT WING L/E INBOARD VANE SKIN SHOWS ELONGATED HOLES AT STA XS. 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030413, ED3259. REMOVED FASTENERS IAW SRM 51-1-21 PG 2. CUT OUT DAMAGED AREA IAW EODHL 030413, ED3259. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6 0.063), INNER DOUBLER (7075-T6 0.050) AND DOUBLER (7075-T6 0.071) IAW EODHL 030413, ED 3259. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INNER PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON SPLICE SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL 030413, ED 3259, SRM 51-1-21 PG 2, SRM 51-1-20D PG 9, SRM 51-3-0 PG 2 AND SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030515000862003051500086SO 2003 5 15 C2XA03SH129 120030505A532014522459003 SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713908 145465 SHV - DURING C-CHECK THE SUPPORT RAMP ON CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030515001342003051500134NM 2003 5 15 AWXA200300478 120030422A53106546564 SHEAR TIE BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BASE OF FRAME BS 927, STR 27 LT TO STR 27 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF SHEAR TIE; FABRICATED A REPAIR ANGLE AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07 FIG 205 PG 213. 2L72 4F RTA16WE 20030520000172003052000017NM 2003 5 20 AMTA200300563 120030425A4900 APU BOEING757 75733N 1384931NM MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11551TZ 32585 APU WOULD NOT START, 3 ATTEMPTS, RPM UP TO 15 PERCENT. PERFORMED APU BITE IAW MM 39-61-05. NO FAULTS DISPLAYED STARTED APU IAW MM 49-11-00. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030604002082003060400208WP 2003 6 4 UPS03840616 120030417A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, REPAIR DOUBLER AT FS 237 AT LONG. 5R HAS BLIND FASTENERS AND DOES NOT COMPLY WITH SRM. PER. EO. DC8-5330-12800-D REMOVED EXISTING DOUBLER,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED DOUBLER,FILLER,AND FINGER DOUBLER I.A.W. SRM. 53-2-1 FIG. 7 2L74 4F RT4A25 20030604002092003060400209WP 2003 6 4 UPS03840628 120030417A53204758514520N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, INTERCOSTAL ATTACH FITTING IS CRACKED AT STA. 1230 LONG. 33R REMOVED AND REPLACED FITTING IAW DWG. 4758514,AND SRM. 51-1-20D 2L74 4F RT4A25 20030604002212003060400221SW 2003 6 4 BAQA086329 120030505A7410106149501 IGNITER BOX BELL 206 206L3 1182108SW ENGINE INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01206CJ2390 51579 IGNITER BOX HAS INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20030604002242003060400224EU 2003 6 4 BAQA086234 120030422A6330L633M2010101 MOUNT UROCOPEC135 EC135P1 8680990EU GEARBOX FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01137MH91 0179 GEARBOX MOUNT HAS AN INTERNAL FAILURE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030604002272003060400227NM 2003 6 4 UPS03240641 120030417A5320 ANGLE BOEING727 72722C 138400FNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, CRACK ON ANGLE, AFT CARGO DOOR INTERIOR, ABOVE AFT DOOR STOP. REMOVED ANGLE FROM DOOR INTERIOR IAW SRM 51-30-2 FABRICATED NEW ANGL E IAW SRM 51-20-1 FIG 7 INSTALLED NEW ANGLE IAW SRM 51-30-2 2L73 4F A3WE 20030604002322003060400232WP 2003 6 4 UPS03840637 120030423A574046403091 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, LT WING FITTING AT REAR SPAR AT XRS 446 AT REAR SPAR REMOVED,FABRICATED AND REPLACED FITTING I.A.W. DWG. 4640309 AND SRM. 51-1-20D 2L74 4F RT4A25 20030604002342003060400234EU 2003 6 4 NSVA20030025 120030502A3350387 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A NSVAK NONE O OTHER ININSP/MAINT 1 EA27299CJ 340B299 THIRD FLIGHT OF THE DAY PILOT REPORTED ROW 4 AND 11 FLOOR LEVEL EMERGENCY LIGHT WERE INOP. MAINTENANCE WAS DISPATCHED TO AIRCRAFT FOUND 2 BULBS BURNED OUT REMOVED AND REPLACED BULBS OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 20030605000022003060500002CE 2003 6 5 AUS20030427 120030411A5312 BULKHEAD BEECH 200 B200T 1152929CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN3 GL FUSELAGE DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) REAR PRESSURE BULKHEAD DAMAGED. A SMALL DENT APPROXIMATELY 10.1MM (0.4IN) LONG CONTAINING A SHARP INDENT WAS FOUND TO BE CRACKED. SUSPECT CAUSED DURING EQUIPMENT LOADING SOME TIME PREVIOUSLY. 1L72 4T4 T A24CE E4EA 6 CP15EA 20030605000142003060500014NM 2003 6 5 AUS20030439 120030428A78303272621 GEARBOX RROYCE BOEING747 747438 NM RROYCERB211 RB211524G19 NE THRUST REVERSER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE THRUST REVERSER GEARBOX DETACHED. THRUST REVERSER SLEEVE TWISTED AND NOT FULLY RETRACTED. DAMAGE CAUSED TO ASSOCIATED STRUCTURE AND MECHANISM. 2L74 4F4 FRTA20WE E30NE 20030605000252003060500025 2003 6 5 A6WA200340074 420030520A2210 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA YAW DAMPER MALFUNCTIONED A A6WAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31410AW 7490 YAW DAMPER NR 2 WILL NOT STAY ENGAGED WHEN MOVING AIRCRAFT. YAW DAMP INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR. CHECKS OK. (M) 2L72 4F RTA21EA 20030605000352003060500035EA 2003 6 5 A6WA200340069 120030520A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 FUSELAGE SKIN IS DAMAGED AT PASSENGER DOOR CUTOUT FS 310. REPAIRED DAMAGE AT PASSENGER DOOR CUTOUT FS 310 IAW BOMBARDIER INC REO 601R-53-21-160A. (M) 2L72 4F RTA21EA 20030605000472003060500047WP 2003 6 5 WX030004 120030415A33500105601003PA57 COVER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT MISSING A WX0AO OTHER O OTHER TXTAXI/GRND HDL 1 WP17860GA 49786 DURING ACCOMPLISHMENT OF A SERVICE CHECK, MAINTENANCE FOUND SOME EMERGENCY FLOOR TRACK LIGHTING WIRES EXPOSED. MAINTENANCE SPLICED IN A NEW SECTION OF TRACK COVER AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20030602001322003060200132NM 2003 6 2 SWAA031143 120030522A335065C27093 LENS BOEING737 7372H4 138448CNM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F A16WE 20030602001432003060200143NM 2003 6 2 DL73S030400 120030429A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 0 23075 MAJOR REPAIR TO FUSELAGE SKIN WHERE CRACKS WERE FOUND DUE TO INSPECTION EO 5-75366-12AD. A/C WILL BE REPAIRED PER ERA 384984-14. 2L72 4F RTA16WE 20030602001462003060200146 2003 6 2 SWAA031134 420030520A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030604000202003060400020SO 2003 6 4 SIMA200311315 120030422A531112010732001 FRAME EMB 135 EMB135LR 3260305SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND FRAME 18 DAMAGED ON LOWER EDGE. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW EMB 135 SRM 145/1142 CHAPTER 51, REV 21, 51-40-02, 51-20-03, 51-20-01. 2L72 4F RTT00011AT 20030604000402003060400040SO 2003 6 4 SIMA200312701 120030429A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21709GB 145211 ABI - DURING AN MBV INSPECTION, THE CENTER SECTION OF THE FORWARD FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 15.375 INCH BY 21.5 INCH SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPLACEMENT FORWARD FLOORBEAM CENTER SECTION AND TWO DOUBLRR AND SHIMS. REPAIR DONE IAW EMB 145/ SRM 145/1142, CHAPTER 53, REV 21-10 PARA 4 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030604000912003060400091NM 2003 6 4 UPS03440505 120030410A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, SEAT TRACK FOUND CORROSION AT 520 - 575 LBL 46. SEAT TRACK REPAIRED AT U/D BS 480 - 590 LBL 46 AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.045 X 1 X 10 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604000932003060400093NM 2003 6 4 UPS03440507 120030411A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, SEAT TRACK O/B FLANGE CORROSION. SEAT TRACK REPAIR AT BS 670 - 810 RBL 11. REF NRC 6876. CORROSION BLEND OUT 0.050 X 1 X 2 INCHES. 2L74 4F A20WE 20030604001382003060400138NM 2003 6 4 UPS03440558 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 580 LT STRINGER 24L FRAME FOUND CRACKED. FRAME REPAIRED AT BS 580 BETWEEN S23L TO S25L AS PER SRM 53-10-04 FIG.35. 2L74 4F A20WE 20030604001612003060400161NM 2003 6 4 UPS03440581 120030412A575365B106221 RIB BOEING747 747121 1384871NM NR 5 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING, NR 5 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 5 AND 6 ( VIEW FROM I/B ). BOLT HOLE CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030604002142003060400214 2003 6 4 BAQA086227 420030422A34006226521016 CONTROL HEAD BELL 222 222U 1182140SW NAV DISPLAY INTERMITTENT W BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01277LF8659 47520 DISPLAY INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H9SW 20030604002252003060400225NM 2003 6 4 UPS03240639 120030417A5330 PANEL BOEING727 72722C 138400FNM FUSELAGE ERODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, AIRSTAIRS COMPARTMENT, CLOSE OUT PANEL AT STA 1223 LOBE THAT JOINS TO EXTERNAL SKIN IS SHOWING SIGNS OF ERROSION ALONG ITS EDGE ON LT SIDE. AREA REPAIRED IAW SRM 51-40-3 FIG 1 2L73 4F A3WE 20030605000052003060500005EA 2003 6 5 AUS20030430 220030409A8530EYP138 CYLINDER PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA HARTZLHCE2Y HCE2YK2 GL ENGINE DAMAGED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS 60 (AUS) RH ENGINE NR 4 AND NR 6 CYLINDERS EXTENSIVELY HEAT DAMAGED. SUSPECT EXHAUST HAD SEPARATED FROM CYLINDER. 1L72 3O3 O 1A10 1E4 5 CP9EA 20030605000232003060500023NM 2003 6 5 WRLA200310 120030514A302032138684 VALVE DOUG MD11 MD11F 3023600NM NR 2 ANTI ICE FAILED A WRLAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA27276WA 48632 NR 2 ENGINE ANTI-ICE DISAGREE LIGHT FOLLOWED BY LEVEL 3 NR 2 ENGINE DUCT LIGHT. SECURED NR 2 ENGINE. SHUT DOWN NR 2 ENGINE DUMPED FUEL AND RETURNED TO CHARLESTON. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE VALVE. REMOVED AND REPLACED NR 2 ENGINE BURST ELEMENT PERFORMED AIR TEST ALL TEST PASSED. GROUND RAN AT 1.3 EPR WITH ANTI-ICE ON AND OFF NO ALERTS. REPLACED ANTI-ICE VALVE. (M) 2L73 4F RTA22WE 20030605000402003060500040WP 2003 6 5 AMTA200300679 120030507A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 INTERIOR AREA AT LOWER END BETWEEN EXTERIOR SKIN AND INTERIOR CLOSE OUT PANEL CORROSION ON ANGLE 19 INCHES FROM AFT END EDGE OF DOOR. REPLACED ANGLE IAW LKHD DRWG 1503517 AND SRM 51-40-01. (M) 2L73 4F A23WE 20030605000502003060500050NM 2003 6 5 AMTA200300602 120030505A2600 WARNING LIGHT BOEING757 75723N 1384973NM LT ENGINE ILLUMINATED A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11514AT 27971 LT ENGINE OH LPS DISPLAYED. DISCONNECTED, INSPECTED AND RESECURED C/P C41072 AND D2402 PER WM SD PRACTICES. PERFORMED AFOLTS TEST PER MM 26-12-00-71, 5-001. OPS CHECK SATISFACTORY. VERIEFIED OPS CHECK GOOD FLIGHT 933. (M) 2L72 4F RTA2NM 20030605000632003060500063NM 2003 6 5 C8GA20030014 120030513A3232 ACTUATOR BOEING727 727223 1384074NM NLG DOOR FAILED A C8GAO OTHER J WARNING INDICATION APAPPROACH 1 SO15715AA 22470 FLIGHT 002 FROM PTO TO MIA. ON APPROACH TO MIA, THE NOSE LANDING GEAR DOORS OPEN AND THE NOSE GEAR FAILED TO LOWER. RECYCLED SYSTEM TWICE BEFORE THE NOSE GEAR CAME DOWN. NO EMERGENCY ACTION WAS TAKEN AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NOSE GEAR UNLOCK ACTUATOR, TRANSFER CYLINDER AND TWO WAY RESTRICTOR WERE REPLACED. OPERATED THE NOSE LANDING GEAR SYSTEM SEVERAL TIMES AND NO DEFECTS WERE NOTED. ALL WORK DONE IAW MM 32-33-11, 32-33-41, 32-33-0, AND 32-34-0. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030605000892003060500089NM 2003 6 5 UPS03240683 120030411A5752 TAB BOEING727 72722C 138400FNM LT WING AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, LT WING, I/B AILERON TAB HAS 2 ARMS OF DELAMINATION ON UPPER SURFACE. I/B AILERON TAB REMOVED IAW MM 27-10-05. FITTED NEW AILERON TAB IAW MM 27-10-05. I/B AILERON TAB BALANCE CHECKED IAW SRM 51-80-03. ADJ /TEST CARRIED OUT IAW MM 27-10-05 2L73 4F A3WE 20030605001012003060500101NM 2003 6 5 PCAA0305074 120030513A323054C546347 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003NM NLG INOPERATIVE A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13843EX 335 CREW REPORTED THAT THE NOSE GEAR FAILED TO EXTEND WITH NORMAL EXTENSION. MAINTENANCE REPLACED THE NOSE LANDING GEAR SOLENOID SEQUENCE VALVE. GEAR WAS SWUNG, OPERATIONAL AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030605001042003060500104EA 2003 6 5 03134675 120030514A2910601R7523659 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A VTZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA27675BR 7635 DURING THE CLIMB, THE CREW REPORTED THAT THE HYDRAULIC NR 3 PRESSURE DROPPED TO ZERO WITH A GEAR DISAGREE MESSAGE AND A "HYD3A" MESSAGE. THE FLIGHT RETURNED TO ORD, LANDED WITHOUT FURTHER INCIDENT, AND WAS TOWED TO THE GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A HYDRAULIC BRAKE LINE. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030605001112003060500111EU 2003 6 5 03134324 120030514A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27324UE 41017 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE LIGHTING SECTION. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030605001252003060500125WP 2003 6 5 ZW0A0304902 120030515A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139401W 53137 THE EGRESS LIGHT AT ROW 25, AND THE EGRESS LIGHTS FROM ROW 27 THROUGH 29, WERE INOPERATIVE. REINSERTED LAMP AT ROW 25, AND CLEANED LAMP ASSEMBLY SOCKETS AT ROW 29. CHECK-C 11-16-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030605001302003060500130NM 2003 6 5 MEX2003107 120030331A27204372505 GEARBOX DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE HORZIZONTAL STABSTUCK W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23169PL 53175 DURING FINAL APPROACH LONG TRIM WAS STUCKED, THE NOSE COMPENSATION UP WAS NOT POSSIBLE. THE PRIMARY ACTUATOR ENGINE WAS REPLACE. THE GEAR BOX ASSY TRIM AND ALTRENATE ENGINE WERE REPLACED IAW MM AND RELAY LONGITUDINAL TRIM WAS REPLACED IAW, TESTS CORRECT. 2L72 4F4 FRTA6WE E2EA 20030605001382003060500138 2003 6 5 ARWA20030503 420030513A34212587909903 INDICATOR DOUG DC8 DC863 302198AWP ATTITUDE FAILED A ARWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO19345JW 46042 CAPTAIN'S ATTITUDE INDICATOR FAILED, TAKE OFF ABORTED. REMOVED & REPLACED NR 1 VG OPS CK GOOD IAW DC8 MM 34-25-0 , REMOVED AND REPLACED NR 1 INSTRUMENT AMPLIFIER RACK AND NR 1 HORIZON INDICATOR OPS CHECKED GOOD IAW DC8 MM 34-5-0. 2L74 4F 4A25 20030605001442003060500144 2003 6 5 SWIA200311970 420030508A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07939SW 7742 AT CRUISE, AIRCRAFT BEGAN YAW SERIES LEFT AND RIGHT WITH AUTHORITY. AFTER SEVERAL SECONDS, YD2 INOP STATUS MESSAGE APPEARED AND AIRCRAFT RETURNED TO NORMAL FLIGHT. AT CRUISE, AUTOPILOT ON, AND YD2 OFF, AIRCRAFT BEGAN YAW SERIES LEFT AND RIGHT AFTER SEVERAL SECONDS AND RETRIMMING OF RUDDER, AIRCRAFT WOULD STABILIZE IN NORMAL FLIGHT. SEVERAL OCCURENCES. REMOVED AND REPLACED NR 1 AND 2 FCC'S IAW CRJ MM 22-12-14. PERFORMED OPERATIONAL CHECKS IAW CRJ MM 22-11-00. S/N OFF: 128VV. 2L72 4F RTA21EA 20030514000012003051400001EA 2003 5 14 ASOA03183 120030425A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11861AS 7445 DURING APPROACH FROM RDU-DFW, THE FLAPS FAILED AT ZERO DEGREES. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE COMPLIED WITH AD 98-20-01 AND RESET THE FLAPS SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514000082003051400008WP 2003 5 14 AALA20030362 120030323A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21937AN 53286 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030514000502003051400050NM 2003 5 14 SWAA030973 120030430A53306545800700 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29071SW 22358 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT NR 1 RT PAX WINDOW LOWER AFT CUTOUT, BS 360. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030514000662003051400066 2003 5 14 SWAA030965 420030429A2565 GIRT BAR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29412WN 29818 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030514000772003051400077NM 2003 5 14 SWAA030943 120030428A53116546543 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW STR 17L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030514000892003051400089NM 2003 5 14 SWAA030990 120030503A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030514001082003051400108NM 2003 5 14 SWAA031009 120030506A3350BR2013 LIGHT BOEING737 7375H4 138449DNM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C4 CHECK, FOUND EEPLS SECTION INOP IN AFT CABIN. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20030514001142003051400114NM 2003 5 14 SWAA031025 120030508A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 EEPLS COVER LOOSE AT FWD END. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030514001302003051400130NM 2003 5 14 SWAA031016 120030506A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, ABOVE STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030611000722003061100072NE 2003 6 11 HEEA086557 120030522A32437025001004101 VALVE SKRSKYS76 S76A 8143006NE BRAKE SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 VALVEWILL NOT HOLD PARK. 1G72 3U H1NE 20030611000742003061100074NE 2003 6 11 HEEA086559 120030522A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03223429573 760096 TRAILING EDGE OF PADDLE "A" NEAR THE TIP HAS SOME SEPERATION. 1G72 3U H1NE 20030611000792003061100079NE 2003 6 11 HEEA086564 120030522A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 THE CRESENT SHAPE DOUBLER UPPER AND LOWER SIDE IS SEPARATED. 1G72 3U H1NE 20030611000932003061100093SW 2003 6 11 HEEA086701 120030522A63226038T59P02 BLOWER BELL 214 214ST 1182106SW NR 2 ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 NR 2 ENGINE BLOWER OFF CAUTION LIGHT ILLUMINATED IN FLIGHT. TO BE SENT TO VENDOR FOR REPAIR. 2G72 4U H10SW 20030611000952003061100095SW 2003 6 11 HEEA086703 120030522A632194501031 BRAKE ASSY BELL 412 412 1182202SW MAIN ROTOR STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 BRAKE ASSY HAS STICKING PISTON IN CALIPER. SHOP REPAIR. 1G72 4U H4SW 20030611001012003061100101EU 2003 6 11 I05R086497 120030512A28229A2045 PUMP UROCOPEC135 EC135P1 8680990EU FUEL BOOST INTERMITTENT H I05RO OTHER O OTHER NRNOT REPORTED 1 FS01551BA 188 BOOST PUMP OPERATION INTERMITTENT REMOVED AND REPLACED PUMP 1G72 3U O H88EU 20030611001142003061100114EU 2003 6 11 HEEA086718 120030521A243651565000R VOLT REGULATOR BOLKMS105 BO105S 5626006EU NR 1 ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 NR 1 ENGINE VOLTAGE REGULATOR QUIT WHILE SETTING NR 2 GENERATOR VOLTAGE AFTER WIRE REPAIR. SENT FOR WARRANTY REPAIR. 1G72 3U H3EU 20030609001142003060900114NM 2003 6 9 03139500 120030519A3350 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27500FJ DURING MAINTENANCE INSPECTION, LAVATORY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED LAVATORY EMERGENCY LIGHT BULB. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED. 2H72 4T RTA55NM 20030609001542003060900154SO 2003 6 9 C2XA03SH158 120030525A532014524131007 SUPPORT EMB 145 EMB145LR 3260212SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV- DURING C-CHECK THE AFT PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030610000042003061000004EU 2003 6 10 HEEA086723 120030521A2822D105318E PUMP BOLKMS105 BO105S 5626006EU FUEL BOOST INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 NR 1 SUPPLY BOOST PUMP INOPERATIVE. 1G72 3U H3EU 20030610000822003061000082NE 2003 6 10 DLM88030423 220030505A7314 SHAFT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE FUEL PUMP SHEARED A DALAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO27966DL 53115 725998 RIGHT ENGINE FLAMED OUT AT APPROXIMATELY 60 KTS. MTC IN PROGRESS ON NR 2 ENGINE. FOUND FUEL PUMP SHAFT SHEARED. REPLACED PUMP AND CONTROL 2L72 4F4 FRTA6WE E9NE 20030611000782003061100078NE 2003 6 11 HEEA086563 120030522A62107615009000049A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR CHIPPED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 7609 760060 TRAILING EDGE CHIPPED 1.5 IN. FROM TRIM TAB. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20030611001022003061100102EU 2003 6 11 I05R086498 120030512A6340430106202 PICKUP UROCOPEC135 EC135P1 8680990EU M/R GEARBOX INOPERATIVE H I05RO OTHER O OTHER NRNOT REPORTED 1 FS01551BA519 188 LOSS OF N/R INDICATION, REPLACED SPEED PICKUP. OPS CHECKED GOOD. 1G72 3U O H88EU 20030611001362003061100136EA 2003 6 11 ASOA03196 120030513A4930AP258S04 ELBOW CNDAIRCL600 CL6002B19 1900309EA FUEL LINE LEAKING A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO11835AS 7258 FLT 4481 - DURING CRUISE FROM LEX-ATL AT APPROX 26,000 FEET, WHEN THE CREW INCREASED THE COCKPIT TEMPERATURE TO 43 DEGREES CELSIUS A FUEL SMELL OCCURRED. THE SMELL DIMINISHED BUT REMAINED NOTICEABLE WHEN THE CREW DECREASED THE TEMPERATURE TO 3 DEGREES CELSIUS. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT FUEL LINE ELBOW. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030611001622003061100162SO 2003 6 11 SWIA200312004 120030521A2422 INVERTER EMB 120 EMB120ER 3260203SO AUTOPILOT FAILED A SWIAO OTHER I FLT. ATTITUDE INST. APAPPROACH 1 NM07299SW 120329 F/O'S AUTO PILOT FAILED ON THE APPROACH MODE. RED AP LIGHT ON MAP AND FCP. REMOVED AND REPLACED NR 1 INVERTER WITH SERVICEABLE UNIT IAW MM 24-22-00. OPS CHECK GOOD. P/N OFF: AL-251-1G, S/N OFF: 6074. 2L72 4T RTA31SO 20030612000042003061200004EA 2003 6 12 SWIA200312012 120030524A2760270007 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA LT SPOILERS MALFUNCTIONED A SWIAO OTHER O OTHER CRCRUISE 1 NM07426SW3194 3194 7468 RECEIVED A SPOILERON FAULT MESSAGE IN FLIGHT. TESTED THE SYSTEM AND FOUND THE LEFT INBOARD SPOILER PCU TO BE NON-FUNCTIONAL. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU IAW 27-62-01. OPS CHECK GOOD, LEAK CHECK GOOD. 2L72 4F RTA21EA 20030612000082003061200008SO 2003 6 12 SWIA200312016 120030425A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07295SW 120322 CORROSION ON FLOORBEAM IN LAVATORY AREA. FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED BUTT STRAP WITH SERVICEABLE UNIT, LAV TO CARGO, RIGHT SIDE. 2L72 4T4 TRTA31SO E20NE 20030612000232003061200023NM 2003 6 12 P5CA0300884 120030528A3610BACC10EY600A CLAMP BOEING747 7472U3B 1384846NM HEAT EXCHANGER LOOSE A P5CAO OTHER O OTHER CLCLIMB 1 WP23922FT 22768 BOTH A&B NR 2 NACELLE TEMP SPIKING RETARDED THROTTLE NACELLE INDICATIONS NORMAL. ON LEAK CK FOUND FAILED DUCT CLAMP BETWEEN HEAT EXCHANGER & ENG DUCT. INSTALLED NEW CLAMP AND ON LEAK CHECK NIL LEAKS NOTED. THREADS STRIPPED ON HOLDING BOLT FOR CLAMP. 2L74 4F RTA20WE 20030612000242003061200024SO 2003 6 12 C2XA03SH165 120030528A3260852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO LT MLG OUT OF ADJUST A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW2714945 145049 SHV - DURING TEST FLIGHT 3160, A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. THE PILOT USED THE DOWNLOCK RELEASE TO CYCLE THE GEAR. THE AIRCRAFT COMPLETED THE TEST FLIGHT AND RETURNED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR PROXIMITY SWITCH AND OPERATIONAL CHECKED GOOD IN ACCORDANCE WITH EMB-145 MM 32-63-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030612000352003061200035EA 2003 6 12 SWIA200312027 120030521A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 FS 280 FLOORBEAM LEFT OUTBOARD ATTACH ANGLE LBL 9.0 CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACE ANGLE IAW CRJ SRM 51-40-11. P/N: 601R31113-57 2L72 4F RTA21EA 20030612000462003061200046WP 2003 6 12 ABXA030181 120030520A53155910137459 FLOORBEAM DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 EXFOLIATED FLOORBEAM IN FORWARD LOWER CARGO, FS 313 AT RIGHT BUTT LINE 6. REPAIRED CORRODED FLOORBEAM IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030612000492003061200049WP 2003 6 12 ABXA030172 120030523A275057726913 MECHANISM DOUG DC8 DC863 302198AWP RT WING TE FLAPSBROKEN A ABXAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL23820AX 46155 WHEN FLAPS WERE EXTENDED TO THE 12 DEG POSITION, THE LEFT FLAP POSITION INDICATED 12 DEG AND THE RIGHT FLAP INDICATED 7 DEG. THE AIRCRAFT ROLLED TO THE LEFT. RETRACTED FLAPS AND RE-EXTENDED, OPS NORMAL. VERIFIED, FOUND RIGHT INBOARD FLAP ACTUATOR MECH ASSEMBLY BROKEN. REPLACED FLAP ACTUATOR ASSEMBLY IAW DC-8 MM 27-51-09-4. LEAK CHECKED GOOD. PERFORMED ADJ/TEST IAW DC-8 MM 27-50-00-5. OPS CHECKED GOOD. REPLACED DAMAGED FLAP STOP ASSEMBLY IAW DC-8 MM 27-51-09. ADJUSTED STOP IAW DC-8 MM 27-50-00. OPS CHECKED GOOD. REPLACED DAMAGED RIGHT WING INBOARD TRAILING EDGE PANEL IAW DC-8 MM 57-10-00. REPLACED RIGHT WING INBOARD FLAP ACTUATOR EXTEND HYDRAULIC LINE IAW DC-8 MM 27-50-00. OPS AND LEAK CHECKED GOOD. 2L74 4F 4A25 20030612000532003061200053WP 2003 6 12 ABXA030176 120030429A5553591214130 ATTACH ANGLE DOUG DC9 DC932 3022066WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 RIGHT AFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS CRACKED. REPAIRED ANGLE IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030612000772003061200077WP 2003 6 12 UPS03840700 120030521A534047504192 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1220 LONG 19R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612000792003061200079WP 2003 6 12 UPS03840702 120030521A534047504191N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT LONG 1180 LONG 18R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612000912003061200091SO 2003 6 12 C2XA03IA055 120030529A32347455501 LEVER EMB 145 EMB145LR 3260212SO MLG INTERMITTENT A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2719554 145587 IAH- FLIGHT 2548, THE CREW NOTED INTERMITTENT LANDING GEAR LEVER DISAGREE IN FLIGHT. HANDLE IN THE UP POSITION ALL GEAR INDICATORS SHOW UP, BUT BOXED IN RED. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, IAW ERJ 145-MM-32-32-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030612000942003061200094WP 2003 6 12 200300285 120030529A276139545571 DRIVE LINK DOUG DC9 DC915F 3022037WP LT SPOILER CRACKED B EIAAK NONE O OTHER ININSP/MAINT 1 WP07915F 47061 LT INBOARD FLIGHT SPOILER DRIVE LINK SHOWS CRACKED DURING ULTRASONIC INSPECTION. REMOVED AND REPLACED LEFT HAND INBOARD FLIGHT SPOILER DRIVE LINK PER EO DC9-826--91 REV A. 2L72 4F A6WE 20030612000952003061200095WP 2003 6 12 ABXA030183 120030514A5553591214129 ATTACH ANGLE DOUG DC9 DC941 302207NWP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23964AX 47781 VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED, LEFT SIDE OF VERTICAL AFT END. REPAIRED ANGLE IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030612000982003061200098NM 2003 6 12 CALA0300273 120030530A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND FLOORBEAM CORRODED ON TOP SIDE IN TWO PLACES AT STA 986, RBL 15-44. REPLACED T-CAP IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030612001082003061200108NM 2003 6 12 UPS03240746 120030519A5754 BRACKET BOEING727 727185C 138406NNM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, NR 3 SLAT, STRUCTURE SUPPORT ANGLE IS CRACKED JUST I/B OF WHERE ACTUATOR EYE END ATTACHES TO SLAT. BRACKET REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. BRACKET INSTALLED IAW SRM 57-50-03 & SRM 51-30-02. 2L73 4F A3WE 20030612001142003061200114NM 2003 6 12 UPS03240752 120030520A5754 ANGLE BOEING727 727185C 138406NNM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, NR 6 SLAT, O/B TRACK TO SLAT ATTACH ANGLE IS CRACKED. ANGLE FABRICATED IAW SRM 51-20-01. ANGLE INSTALLED IAW SRM 51-20-02. 2L73 4F A3WE 20030612001182003061200118NM 2003 6 12 UPS03440762 120030515A5313BAC14935227075 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, AFT CARGO STA 1745 S41L STRINGER FOUND CRACKED AT FASTENER HOLE. AFT CARGO BS 1740-1760 S41L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. 2L74 4F RTA20WE 20030612001202003061200120NM 2003 6 12 UPS03440764 120030509A532065B280814 ANGLE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, NLG W/W STA 320 RBL 30 PRESSURE DECK RT UPPER ANGLE AREA CRACKED AS MARK. NLG W/W PRESSURE DECK RT UPPER CORNER ANGLE AT RBL 30 REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030612001222003061200122NM 2003 6 12 UPS03440766 120030519A5313BAC14981327075 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 1940 - 1960 STR 8R STRINGER END CRACKED. M/D BS 1940-1960 STR 8R STRINGER REPLACED AS PER SRM 53-10-03 FIG 12. 2L74 4F RTA20WE 20030610000532003061000053WP 2003 6 10 ABXA030165 120030414A531599115451 FLOORBEAM DOUG DC9 DC931 3022065WP CARGO BAY CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 FLOORBEAM WAS EXFOLIATED AT FS 408 DIRECTLY ABOVE FORWARD LOWER CARGO DOOR CUTOUT AND OUTBOARD OF RIGHT BUTT LINE 54. REPAIRED AREA IAW REA D953-47171 AND DC-9 SRM. 2L72 4F A6WE 20030610000812003061000081NM 2003 6 10 DLM88030422 120030504A33506011779 BATTERY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27994DL 53346 OVERWING EMERGENCY LTS. COME ON WHEN COCKPIT EMERGENCY LIGHT SWITCH IS PLACED IN THE OFF POSITION. REPLACED OVERWING EMERGENCY LIGHT BATTERY RACK-OPS NORMAL. 2L72 4F RTA6WE 20030610001032003061000103GL 2003 6 10 HEEA086997 220030604A732023072725 HMU BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03510PH 53209 FUEL LEAKING FROM SHAFT SEAL DRAIN ON HMU. 1G71 3U3 UO H2SW E4CE 20030610001252003061000125SW 2003 6 10 HEEA087022 120030604A6230406012129101 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 MAIN ROTOR PITCH LINK BEARING FROZEN. 1G71 3U O H2SW 20030611000322003061100032NM 2003 6 11 MEX2003159 120030505A3150 WARNING LIGHT BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE COCKPIT ILLUMINATED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23301AM 30045 AIRCRAFT RETURNED TO PLATFORM DUE TO MACH SPEED TRIM MESSAGE ILLUMINATION. THE BITE TEST ON P61 ADC WAS ACCOMPLISHED AND LIGHT ILLUMINATION IN OVERHEAD P11. FLIGHT CONTROLS TEST WAS ACCOMPLISHED AND LT ELEV PCU MESSAGE ILLUMINATED. THE MESSAGE APPEARED ONLY WHEN THE THREE HYDRAULIC SYSTEMS ARE OPERATIN. THE LT ELEV-PCU MESSAGE IS DEFERRED BY MEL 27-21-2. 2L72 4F4 FRTA2NM E17NE 20030611000882003061100088SW 2003 6 11 HEEA086696 120030522A3246412050015109 SKID BELL 412 412 1182202SW MLG CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MLG SKID CRACKED AT FWD CROSSTUBE SADDLE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030611001352003061100135SO 2003 6 11 ASOA03206 120030510A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11268AS 120202 DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030611001412003061100141EA 2003 6 11 ASOA03197 120030507A3397487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 FLT 4761 - DURING A GROUND INSPECTION IN ATL, THE FORWARD EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE POWER STRIP CONNECTORS TO THE FORWARD EMERGENCY FLOOR LIGHTS WET. MAINTENANCE DRIED, CLEANED AND RECONNECTED THE EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030611001492003061100149EA 2003 6 11 2003F00370 120030323A2700 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA COCKIT ILLUMINATED A FDKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07504MJ 10066 FLT 6604 - PHX-LAX, AFTER TAKEOFF, PILOT RECEIVED A GROUND LIFT DUMPING UNSAFE CAUTION MESSAGE. FOLLOWED CFM PROCEDURES AND RETURNED TO PHX WITH NO PROBLEMS. MAINTENANCE RESET SYSTEM AND FOUND NO DEFECTS. AIRCRAFT CONTINUED ITS FLIGHT WITH NO FURTHER DIFFICULTIES RELATED TO THE OCCURRENCE. (M) 2L72 4F RTA21EA 20030611001582003061100158NM 2003 6 11 UPS03440697 120030511A5310141U11071 BEAM BOEING747 747200 1384847NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, NLG WW TUNNEL - LT BS 280 VERTICAL BEAM WEB FOUND CRACK AT LOWER STANDOFF HOLE BETWEEN 1ST AND 2ND STIFFENER CLIP (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED WITH SERVICEABLE NEW PART AS PER SRM 51-10-01 PG 8 AN AREA PAINT TOUCH UP PER MM 51-24-11. 2L74 4F RTA20WE 20030612000542003061200054WP 2003 6 12 ABXA030177 120030512A53109955756501 BEAM DOUG DC9 DC931 3022065WP PAX DOORWAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 MAIN ENTRY DOOR HORIZONTAL BEAM ABOVE UPPER HINGE ATTACH POINT WAS CRACKED. REPAIRED MAIN ENTRY DOOR BEAM PLANE NR 5 IAW DC-9 SRM 52-05. 2L72 4F A6WE 20030612001162003061200116NM 2003 6 12 UPS03240754 120030516A5522 SKIN BOEING727 727185C 138406NNM LT ELEVATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, LT ELEV UPPER SURFACE, CORROSION BENEATH I/B & 2ND FROM I/B STATIC DISCHARGE BASES. DISCHARGE BASE REMOVED IAW SRM 51-30-02 ON 2ND FROM I/B STATIC BASE. CORROSION REMOVED AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 55-20-1. REPAIRS CARRIED OUT IAW SRM 55-20-3 FIG 2. STATIC DISCHARGERS INSTALLED IAW MM 23-61-00. TEST CARRIED OUT PER MM 23-61-00, FOUND TO BE SATISFACTORY. 2L73 4F A3WE 20030612001352003061200135WP 2003 6 12 UPS03840723 120030503A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, R1 DOOR JAMB UPPER AFT CORNER CRACKED 2 EACH, FOUND WITH NDT. REMOVED DAMAGE IAW DC8 SRM 53-2-0, FABBED FILLER, DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0, TR 53-126 & ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 53-2-0 AND TR 53-126. 2L74 4F RT4A25 20030612001462003061200146WP 2003 6 12 UPS03840735 120030503A5310559764631 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, BS 50 - 54 S-21L CUSP FRAME CRACKED APPROX 4.5 INCH LONG. FABBED -31 FRAME IAW DAC DWG 5597646. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -31 FRAME IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030612001492003061200149WP 2003 6 12 UPS03840738 120030505A5510 CAP DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, RT HORIZONTAL STAB INBD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. PERFORMED E/C INSP OF LOWER TEE CAP IAW NDT SPM 06-10-01.001 CRACKED AT RADIUS. REMOVED ANGLE LOCATED AND DRILLED NEW ANGLE IAW DC8 SRM 5 1-1-24, INSTALLED NEW ANGLE IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20030612001512003061200151WP 2003 6 12 UPS03840740 120030506A53206449722 FITTING DOUG DC8 DC873F 302199FWP STRINGER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, NR 56 STRINGER HAS AFT STRINGER END FITTING CRACKED, NR 4 ALT. REC'D NEW FABBED FITTING, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. DRILLED, LOCATED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030612001612003061200161WP 2003 6 12 UPS03840759 120030521A53404772397U1 FITTING DOUG DC8 DC871F 302199DWP AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, STA 1781 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612001662003061200166EA 2003 6 12 SWIA200312039 120030524A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07459SW 7782 MAIN CABIN DOOR EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB. OPS CHECK GOOD. (P/N 1308) 2L72 4F4 FRTA21EA E15NE 20030612001722003061200172 2003 6 12 SWIA200312045 420030525A3425 FUSE EMB 120 EMB120ER 3260203SO INDICATOR LOOSE A SWIAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 NM07224SW 120294 TEN MINUTES AFTER TAKEOFF F/O'S ADI & EHSI WENT INOP WITH ALL FLAGS, ATT DISPLAY CAUTION LIGHT ILLUMINATED. AP WOULD NOT ENGAGE, AND TCAS WAS INOP. RETURNED TO FIELD. FOUND FUSE F0029 NOT SECURE IN FUSE HOLDER. VERIFIED FUSE GOOD AND REINSTALLED INTO FUSE HOLDER AND REPLACED AUX GEN 2 BUS 2 CONTROL RELAY K0396. F/O'S ADI, EHSI, AUTOPILOT AND TCAS, OPS CHECK GOOD. 2L72 4T RTA31SO 20030612001742003061200174EA 2003 6 12 SWIA200312047 120030529A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 EMERGENCY EXIT SIGN (FLOODLIGHT) AT SERVICE DOOR BROKEN. REPLACED EMERGENCY EXIT SIGN BY SERVICE DOOR AND REPLACED THE ELECTRICAL CONNECTOR. DISCOVERED DURING MAINTENANCE INSPECTION. 2L72 4F4 FRTA21EA E15NE 20030612001762003061200176SO 2003 6 12 C2XA03TY080 120030601A533014520551003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE PUNCTURED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713979 145181 A PUNCTURE WAS FOUND IN THE EXTERIOR SKIN APPROX 12 INCHES AFT OF THE SERVICE DOOR. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A DOUBLER AND FILLER, AND INSTALLED. ALODINED, PRIMED AND PAINTED. PRESSURE CHECKED GOOD I/A/W-EMB-SRM-53-21-01, CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4T RTT00011AT 20030612001922003061200192WP 2003 6 12 EIA2003079 120030429A5330 SKIN DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09915F 47061 EXTERNAL SKIN AT STA 918, STRINGER 4R (EMPENNAGE ON RT SIDE) HAS A 2 INCH LONG CRACK. REMOVED CRACKED SECTION OF SKIN, FABRICATED REPAIR DOUBLER, (2) FILLERS, (2) FINGER DOUBLERS, ALODINED, PRIMED & INSTALLED PER DC9 SRM 53-04 FIGURE 12B, PG 54, 56, 60 BV, 60JC, 53-30-0, PG 18-21, 51-10-3, PG 20, & 23-24. REPETITIVE INSPECTION REQUIRED EVERY 8,000 CYCLES PER DC9 SRM 53-04 FIGURE 12B, PG 33, PAR B. 2L72 4F A6WE 20030613000082003061300008EA 2003 6 13 SWIA200312061 120030421A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 FS 235 FUSELAGE SKIN RBL 6.0 NLG CUTOUT CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-048 REV B. 2L72 4F4 FRTA21EA E15NE 20030613000102003061300010EA 2003 6 13 SWIA200312063 120030421A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 SERVICE DOOR SILL PLATE CORRODED. DISCOVERED DURING C-CHECK. DAMAGE FOUND TO BE OUT OF LIMITS. REPLACED SERVICE DOOR SILL PLATE WITH NEW PART IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20030613000222003061300022NM 2003 6 13 UPS03440785 120030509A5314 STRUCTURE BOEING747 747200 1384847NM KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FX - KEEL BEAM BOX INTERIOR LOWER STRUCTURE FOUND HEAVY CORROSION AT STA 1450 TO STA 1465 LBL 6 TO LBL 8. CORROSION BLEND OUT 0.149 X .75 X 1.5 INCH. REPAIRED CARRIED OUT AS PER HX RS R53-49-35025 UPS ENG'R FILE 747- 53-20139. 2L74 4F RTA20WE 20030613000252003061300025NM 2003 6 13 UPS03440788 120030515A5320 TEE FITTING BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, LT MLG WW STA 1241 BL 0 VERTICAL TEE FITTING CORROSION CRACK REVEALED. CORROSION BLEND OUT 0.063 X 2 X 10. BL 0 STIFFENER AT BS 1241 CTR SECTION REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030613000302003061300030NM 2003 6 13 CALA0300283 120030521A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND THE AFT CARGO DOOR INNER SKIN CRACKED AT THE EDGE OF A LIGHTENING HOLE. THE DOOR SKIN WAS REPAIRED IAW ECRA 5232-01029. 2L72 4F RTA16WE 20030613000362003061300036WP 2003 6 13 ABXA030188 120030604A3231 ROLLER DOUG DC9 DC932 3022066WP RT MLG DOOR OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23928AX 47392 FOUND GEAR UPLATCH CHECK GEAR DOOR OPEN LIGHT AND RIGHT MAIN UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR AS PER ABNORMAL PROCEDURE. GEAR UPLATCH CHECK SATISFACTORY. UPON INSPECTION, FOUND RIGHT UPLATCH ROLLER NEEDED ADJUSTED. ADJUSTED DOOR ROLLER CLEARANCES AND PERFORMED UPLATCH ADJUSTMENT TEST IAW DC-9 AMM 32-60-0. OPS CHECKED GOOD AND INDICATION GOOD. UPLATCH TEST OKAY. 2L72 4F A6WE 20030610001052003061000105GL 2003 6 10 HEEA086999 220030604A732023072725 HMU BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 2596 ONE OF THE PLUGS BENT ON ONE SIDE AND MECHANICAL DAMAGE TO HMU NEXT TO AREA WHERE PLUG IS LOCATED. 1G71 3U3 UO H2SW E4CE 20030611000462003061100046WP 2003 6 11 CA030425002 220030424A732189356117 FUEL CONTROL SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCE4N HCE4N3 NE RT ENGINE FAILED W O OTHER EW VIBRATION/BUFFET INADEQUATE Q C CRCRUISE 1 CA (CAN) DURING CRUISE FLT CREW NOTICED RT ENGINE EGT, TORQUE & FUEL FLOW STARTING TO SURGE AS WELL AS NOTICING A CORRESPONDING INCREASE, DECREASE IN ENGINE POWER. ENGINE WAS ALSO FUEL LIMITED DURING CRUISE PORTION OF FLIGHT. SURGING WAS CONTROLLABLE AND DID NOT REQUIRE ANY MAJOR ACTION. UPON DECENT, PULLING BACK THROTTLE RESULTED IN A MOMENTARY INCREASE IN ENG POWER & THEN STARTED DECREASING NORMALLY. PRIOR TO TAKEOFF & CLIMB WERE ALL NORM, CREW STATED THAT ENG FUNCTIONED NORM WITH GOOD POWER FOR TAKEOFF. LANDING WAS CARRIED OUT NORMALLY WITH NO PROBLEMS REPORTED FROM CREW. INSPECTION OF ENG & CONTROLS REVEALED NO PROBLEMS. FCU WAS REPLACED, TEST FLIGHT CARRIED OUT. 2L72 4T4 TRTA8SW E4WE 5 CP10NE 20030611000492003061100049EU 2003 6 11 CA030428008 120030428A7830FGFB583800308 SEAL AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE7315BR WP THRUST REVERSER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE PERFORMING THE BASIC (MONTHLY) INSPECTION, FOUND SEAL/SHIELD P/N FGFB 583800308 CRACKED, BRACKETS BROKEN. BECAUSE OF THE BROKEN BRACKETS CAUSED THE SEAL/SHEILD TO CHAFE ON THE INNER FORWARD SKIN OF BOTH THRUST REVERSER DOORS IN THE STOWED POSITION. THE DAMAGED ON THE INNER SKIN WAS BLENDED OUT IAW SRM AND ALL THREE PARTS REPLACED WITH NEW. 2L73 4F4 FRTA46EU E6WE 20030611000662003061100066NM 2003 6 11 CA030516004 120030516A323282970015005 CYLINDER MESSIER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ACTUATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2823420742 LI0215 (CAN) ACTUATOR FOUND LEAKING, OVERHAULED, AND CYLINDER ASSY REPLACED. CYLINDER CRACKED AT BOTTOM OPPOSITE SIDE OF IN & OUT FITTINGS. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030611000762003061100076NE 2003 6 11 HEEA086561 120030522A67207610305018104 SUPPORT SKRSKYS76 S76A 8143006NE TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 TAIL ROTOR BOOST WOULD NOT STAY ON. SCRAPPED. 1G72 3U H1NE 20030611000822003061100082NE 2003 6 11 HEEA086567 120030522A24227655003007105 INVERTER SKRSKYS76 S76A 8143006NE AC SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 INTERMITTENT INVERTER WARNING LIGHT. SENT FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030611001532003061100153EA 2003 6 11 ASOA03200 120030508A28427689602 PROBE CNDAIRCL600 CL6002C10 1390015EA FUEL QTY MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION CRCRUISE 1 SO11717EV 10088 FLT 4205 - DURNG CRUISE FROM DCA-DFW, THE CREW RECEIVED A LEFT AND TOTAL FUEL QUANTITY AMBER INDICATION, ALONG WITH AN AUTO CROSS FLOW INHIBIT STATUS MESSAGE. THE CREW COMPLIED WITH QRH PROCEDURES AND DECLARED AN EMERGENCY. DURING APPROACH WHEN DESCENDING THROUGH 5,000 FEET THE INDICATION PROBLEM CORRECTED ITSELF, BUT AT 500 FEET A 1,000 LB IMBALANCE INDICATION APPEARED. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE LEFT WING NR 3 FUEL QUANTITY PROBE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030611001632003061100163EA 2003 6 11 SWIA200312005 120030520A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB FAILED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07924SW2967 2967 7681 ON TAXI OUT FOR STAB CH1 INOP STATUS MESSAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW 27-42-01. OPS CHECK GOOD ON GROUND. P/N OFF/ON 8396-3, S/N OFF 221. 2L72 4F RTA21EA 20030612000012003061200001SO 2003 6 12 SWIA200312009 120030522A5713 STRINGER EMB 120 EMB120ER 3260203SO LEFT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07214SW 120280 CRACKED STRINGER LEFT INBOARD WING LOWER SURFACE AFT OF INBOARD FUEL CELL ACCESS PANEL. FOUND DURING A CHECK INSPECTION. COMPLIED WITH WING STRINGER REPAIR AT LEFT INBOARD WING LOWER SURFACE STRINGER NR 8 AT RIB NR 5 PER SRM 57-20-03. 2L72 4T RTA31SO 20030612000122003061200012 2003 6 12 SWIA200312020 420030523A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO NR 1 AUTOPILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07291SW5963 5963 120318 THE CAPTAIN'S FLIGHT DIRECTOR INOP WITH AN INTERMITTENT COMPUTER FLAG INDICATION ON THE ADI, FOLLOWED BY TRIM AND AP INDICATIONS ON THE FCP. REPLACED NR 1 AUTOPILOT COMPUTER FLIGHT DIRECTOR. OPS CHECK NORMAL. 2L72 4T RTA31SO 20030612000152003061200015EA 2003 6 12 SWIA200312023 120030417A2750 FLEX DRIVE CNDAIRCL600 CL6002B19 1900309EA TE FLAP BENT A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 LEFT OUTBOARD FLAP FLEX DRIVE (NR 5) IS BENT AT ENDS. FOUND DURING C-CHECK INSPECTION. LEFT OUTBOARD FLEX DRIVE NR 5 HAS BEEN REPLACED IAW AMM 27-53-10. 2L72 4F RTA21EA 20030612001212003061200121NM 2003 6 12 UPS03440765 120030509A532065B280813 ANGLE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, NLG WW STA 320 LBL 30 PRESSURE DECK LT UPPER ANGLE AREA CRACKED AS MARK. NLG WW LT PRESSURE DECK UPPER ANGLE AT LBL 30 FROM BS 260-340 REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030612001522003061200152WP 2003 6 12 UPS03840741 120030508A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766 - 1806 LONG 17R IS CRACKED. REMOVED L17R AND END FITTING TO FOM. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED L17R & END FITTING IAW DC8 SRM 51-1-21/51-1-20D. 2L74 4F RT4A25 20030612001822003061200182 2003 6 12 2003UALA00399 420030526A2565 FITTING BOEING757 757222 1384956NM PWA 2037 PW2037 NE GIRT BAY SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 DOOR 3R GIRT BAR SHOE FITTING SEPARATED FROM GIRT BAR ASSEMBLY. REINSTALLED SHOE ASSY. 2L72 4F4 FRTA2NM E17NE 20030613000162003061300016WP 2003 6 13 ABXA030185 120030105A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 AFT PAX DOOR UPPER AFT CORNER HAD 4 CRACKS FOUND WITH NDT L-2. REMOVED DAMAGE IAW DC-8 SRM 53-2-0, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0, 51-1-20D, AND 51-1-21. 2L74 4F 4A25 20030613000492003061300049SO 2003 6 13 C2XA03IA058 120030603A2910AE71379016 LINE EMB 145 EMB145LR 3260212SO HYD PUMP LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2715910 145455 THE CREW NOTED THAT HYDRAULIC NR 1 LOW QTY MESSAGE APPEARED ON EICAS WITH HYDRAULIC LEAK. (NOTE: THE FLIGHT WAS DIVERTED TO BNA. MAINTENANCE REMOVED AND REPLACED THE SUCTION AND PRESSURE HYDRAULIC LINES AT THE ENGINE DRIVEN HYDRAULIC PUMP, NR 1 ENGINE, SERVICED THE NR 1 HYDRAULIC SYSTEM, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000672003061300067SO 2003 6 13 C2XA03BT064 120030606A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING 3A INSPECTION MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-00. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20030613000742003061300074SO 2003 6 13 C2XA03SH170 120030608A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 SHV-DURING C-CHECK THE REPAIR DOUBLER ON T-REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000792003061300079SO 2003 6 13 C2XA03SH175 120030608A532014525422001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 SHV-DURING C-CHECK THE LEFT HAND SILL AT FRAME 65 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000882003061300088EU 2003 6 13 MALA030292 120030606A29110884230011 ACCUMULATOR SAAB SF340 340B 7860101EU HYD SYSTEM LEAKING A MALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15451XJ 340B451 EN ROUTE MSP-ATW HYDRAULIC CAUTION ON CWP CAME ON. QUANTITY IS NORMAL MAIN PRESSURE NORMAL. EMERGENCY PRESSURE WAS LOW. OB/IB BRAKE PRESSURE NORMAL. CYCLED HYDRAULIC SWITCH TO OVERRIDE PUMPED UP BOTH MAIN AND EMERGENCY, BUT EMERGENCY STARTED SLOW LEAK DOWN. A/C DIVERTED TO CWA. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY, FOUND BOTH MAIN AND EMERGENCY QUANTITY NORMAL. NO LEAKAGE, HYDRAULIC SYSTEM OPS CHECKED GOOD ON THE GROUND AND ON THE JACKS IAW LC1 HYDRAULIC SYSTEM FUNCTION CHECKS. NO BLEED DOWN NOTED. MAINTENANCE REPLACED EMERGENCY HYDRAULIC ACCUMULATOR P/N 0884230011, S/N OFF 8423-10104, S/N ON 8423-7909 IAW SF340 AMM 29-10-20. ALL CHECKS GOOD. 2L72 4T RTA52EU 20030613000902003061300090EA 2003 6 13 COMA0360257 120030530A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01710CA11918 7241 FLIGHT 5830 GEAR DISAGREE WARNING DURING GEAR EXTENSION AND RETRACTION. REPLACED HYDRAULIC PUMP 3B. 2L72 4F RTA21EA 20030613001012003061300101NM 2003 6 13 UPS03440816 120030521A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - L3 DOOR CUTOUT AFT UPPER CORNER FOUND CRACK AT FX SKIN AND TRIPLER RUNNING FROM EDGE TO FASTENER HOLE. M/D - L3 DOOR CUTOUT AFT UPPER CORNER SKIN AND TRIPLER REPAIRED AS PER HX RS R-53-41-35034 AND UPS EO B747-5310-18865-A. 2L74 4F RTA20WE 20030613001042003061300104NM 2003 6 13 UPS03440820 120030509A5313 LONGERON BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FX - KEEL BEAM BOX INTERIOR LOWER STRUCTURE FOUND HEAVY CORROSION AT STA 1450 TO STA 1465 RBL 6 TO RBL 8. LONGERON REPAIRED AT BS 1456 TO 1480 RT AS PER HX RS R53-49-35025 ITEM 1 TO ITEM 19 AND ENG'R FILE NUMBER 747-53-20139. CORROSION BLEND OUT 158 X .75 X 1 INCH EXCEED SRM LIMIT. 2L74 4F RTA20WE 20030613001222003061300122 2003 6 13 SWAA031197 420030529A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030613001322003061300132NM 2003 6 13 SWAA031238 120030603A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, BETWEEN STR 26L AND STR 27L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030617000072003061700007EU 2003 6 17 AUS20030474 120030320A5311FR16FR20 FRAME AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAMES FR 16 AND FR 20 LOCATED ADJACENT TO FLOOR AND LT SERVICE DOOR CONTAINED LEVEL 2 CORROSION. 2L72 4F4 FRTA46NM E29NE 20030617000082003061700008NE 2003 6 17 AUS20030475 220030422A725034005991809210 SHROUD BOEING737 737800* NM GE CFM56 CFM567B24 NE TURBINE SECTION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE FAN FRAME OUTER SHROUD CRACKED. CRACK LENGTH APPROXIMATELY 127MM (5IN). AIRCRAFT IS FOREIGN REGISTERED 5W-SAM. 2L72 4F4 FRTA16WE E00055EN 20030617000122003061700012EU 2003 6 17 CA030526005 120030522A274247145131 ACTUATOR AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE STABILIZER MALFUNCTIONED W K NONE J WARNING INDICATION ININSP/MAINT 1 CA (CAN) HOLDING AT FL200 200KTS ELAC2 PITCH FAULT FOLLOWED BY A/P OFF, ALTN LAW AND ELAC 1PITCH FAULT. ECAM SHOWED STAB JAM BUT MAN. PITCH TRIM OK. DIR LAW ON MLG DOWN PITCH TRIM IN MAN STILL AVAIL. A/C HANDLING QUALITY WAS GOOD. NO FAULT LTS ON ELAC2/1 ON O/HEAD PANEL 2L72 4F4 FRTA28NM E29NE 20030514001342003051400134NM 2003 5 14 SWAA031020 120030506A5520BACB28AKM07 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C1 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHING AT NR 1 ELEVATOR TAB HINGE ATTACH POINT PER MM. 2L72 4F RTA16WE 20030514002252003051400225NM 2003 5 14 03FDEA00727 120030512A3620 MANIFOLD DOUG MD11 MD11 3023602NM PNEUMATIC SYSTEMDAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25578FE 48458 IN CRUISE (FL320) AFTER 5+30 FLIGHT, AIR MANF 2 FAIL WARNING ILLUMINATED, NR 2 PACK SHUTDOWN AUTOMATICALLY. DIVERTED TO NFFN. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 22MAY03. MEL 36-10-02-A: PNEUMATIC SUPPLY SYS NR 2 - INOP. PNEU MANF DECAY CHECK C/OUT PER MM 36-00-01 - WITHIN MM LIMIT. (ACTUAL 28 SECS 25- 15 PSI MIN 19.2 SECS). 22MAY03 SFS MX R/R'D D1-126 SENSING ELEMENT I.A.W. AMM 36-23-07-04. OPS OK. 2L73 4F RTA22WE 20030515000022003051500002GL 2003 5 15 ALGA086259 220030425A725023055438 NOZZLE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C* GL TURBINE FLAKING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO FOUND METAL FLAKING OFF ON 1ST STAGE BLADE PATH. 1Q71 3R3 U 2A6 E4CE 20030515000132003051500013SO 2003 5 15 SWIA200311936 120030501A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07224SW 120294 EMERGENCY FLOOR LIGHT AT 6A BURNED OUT. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N OL-3071 BPE. 2L72 4T RTA31SO 20030515000992003051500099SO 2003 5 15 C2XA03SH122 120030502A531014522460015 BUTT STRAP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 SHV- DURING C-CHECK LEFT HAND BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030515001132003051500113NM 2003 5 15 CH1A200395055 120030426A5330 SKIN BOEING727 727290 138408WNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FUSELAGE SKIN CRACKED 2 PLACES BS 647 STR 4L. CRACK AT 9:00 POSITION, LOWER ROW OF RIVETS. 2L73 4F A3WE 20030515001292003051500129WP 2003 5 15 ZW0A0304801 120030513A3350200200001SMI LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13966TW 53616 THREE EGRESS LAMPS WERE INOPERATIVE AT THE FLOOR BETWEEN FIRST CLASS AND COACH. REPLACED ONE LAMP, REPLACED ONE COVER, AND RE-INSERTED LAMP AT ROW 5. CHECK-C 6-7-02 STL. 2L72 4F RTA6WE 20030515001302003051500130WP 2003 5 15 ZW0A0304804 120030512A33507732 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13978TW 53628 THE EGRESS LIGHT JUST AHEAD OF CABIN ROW 6, AND THE EGRESS LIGHT JUST FORWARD OF ROW 31, WERE INOPERATIVE. REPLACED BOTH BULBS. CHECK-C 8-17-2002 MCI. 2L72 4F RTA6WE 20030515001332003051500133NM 2003 5 15 AWXA200300477 120030423A5313BAC1498157 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND AT END FASTENER OF STRINGER 16 LT, BS 504C. MAINTENANCE REMOVED FASTENER AND CUT OUT DAMAGED SECTION OF STRINGER 16 LT, AT BS 504C; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR CHANNEL, 2 EACH HAT SECTIONS, AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201, PG 203. 2L72 4F RTA16WE 20030515001422003051500142NM 2003 5 15 AWXA200300527 120030512A3397BMS13311122 WIRE BOEING737 737301 1384611NM SEAT ROW 12 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 PHX - EEL - DURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 TO 16 LT INOPERATIVE. REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030515001472003051500147NM 2003 5 15 AWXA200300463 120030502A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM SEAT ROW 7 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - EEL - DURING INSPECTION MAINTENANCE FOUND A DAMAGED EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT. REPAIRED DAMAGED EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030515001542003051500154NM 2003 5 15 SWAA031070 120030512A32216546288 LINK BOEING737 7373A4 1384585NM NLG LOOSE A SWAAO OTHER E VIBRATION/BUFFET LDLANDING 1 SW29676SW 23288 SEVERE VIBRATION FELT FROM NOSE GEAR UPON LANDING. REMOVED AND REPLACED BOTH NLG UPPER & LOWER TORSION LINKS PER MM. 2L72 4F RTA16WE 20030515001582003051500158NM 2003 5 15 SWAA031074 120030510A53116545785 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW FRAME CRACKED AT BS 470 LT SIDE. REMOVED AND REPLACED WINDOW FRAME PER ERO. 2L72 4F RTA16WE 20030515001612003051500161NM 2003 5 15 SWAA031078 120030512A575465C26686 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030515001642003051500164NM 2003 5 15 AWXA200300466 120030504A793147385 CONTROLLER BOEING757 757225 1384959NM NR 2 ENGINE FAULTY A AWXAE ENGINE SHUTDOWN HJSELECT. POWER LOSS-50 PC WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 WP28915AW4861041502 22209 EN ROUTE, RT IDG FAILED WITH LOSS OF BOTH UTILITY BUSSES, NR 2 ENG ALSO LOST ALL OIL PRESSURE, SHUTDOWN NR 2 ENG PER FLIGHT REFERENCE HANDBOOK. MAINTENANCE PERFORMED EEC BLEED VALVE CONTROL UNIT, & TRANSIENT PRESSURE UNIT BITE CHECKS THAT RESULTED WITH EEC CODE 07, AND TPU CODE 90. INSPECTED CONNECTIONS ON FCU, & PERFORMED RESISTANCE CHECK ON ALTERNATOR, ALL CHECKS GOOD. REPLACED NR 2 LOWER POWER CONDITIONING CONTROLLER, OPS CHECK GOOD IAW BMM 73-21-10-4. VENDOR PRETEST OF POWER CONDITIONING CONTROLLER WAS NO FAULT FOUND. TEARDOWN OF UNIT IDENTIFIED 4 CRACKED ISOLATORS, 4 DETERIORATED GASKETS AND A WORN CABLE ASSY. UNIT WAS OVERHAULED AND TESTED IAW CMM 73-21-10. 2L72 4F RTA2NM 20030515001812003051500181NM 2003 5 15 AWXA200300524 120030414A531569366565 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK 5 EACH CRACKS WERE FOUND ON FLOORBEAM SHEAR WEB BS 927 TO BS 947, BL 0. MAINTENANCE REMOVED CRACKED FLOORBEAM SHEAR WEB FROM BS 927 TO BS 947, AND ATTACH ANGLE; FABRICATED AND NEW REPLACEMENT SHEAR WEB PER DWG 69-36656-5, AND ATTACH ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-05 PG 4 FIG 2 AND SRM 51-40-02 PG 3-4 & 38 FIG 8. 2L72 4F RTA16WE 20030515001892003051500189NM 2003 5 15 AWXA200300514 120030414A5313655297832 STRINGER BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH AREA OF EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT, AT BS 967 WATER TANK COMPARTMENT. MAINTENANCE CUTOUT CORROSION ON STRINGER 27 LT AT BS 967; FABRICATED A REPAIR SPLICE (HAT CHANNEL); INSTALLED REPAIR PART IAW B737-200 SRM 53-10-3 FIG 1 PG 3-8. 2L72 4F RTA16WE 20030515001972003051500197NM 2003 5 15 AWXA200300453 120030423A5313BAC1498139 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT END OF STRINGER 16 RT, AT BS 504C. MAINTENANCE CUTOUT CRACKED AREA OF STRINGER 16 RT, AT BS 504C; FABRICATED 2 EACH REPAIR ANGLES, A HAT SECTION, AND CHANNEL; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 PG 11-12. 2L72 4F RTA16WE 20030520000112003052000011NE 2003 5 20 UIEA200300017 220030411A7261 WARNING LIGHT BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 4 ENGINE ILLUMINATED A UIEAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA15808MC 21048 530280 INFLIGHT ENGINE SHUTDOWN, DURING CRUISE, NR 4 ENGINE SHUTDOWN IN FIGHT DUE TO 'OIL FILTER BYPASS LIGHT. OIL TEMPEARTURE AND PRESSURE NORMAL AT 49 PSI/120 DEGREES AND N2 AT 94 PERCENT. WITH THRUST AT IDEL (75 PERCENT N2) PRESSURE WAS 30 PSI AND TEMPERATURE ROSE TO 140 DEGREES. LIGHT WAS STILL ON. LIGHT REMAINED ON STEADY AFTER SHUTDOWN. REMOVED AND REPLACED NR 4 ENGINE PER B747 MM 71-00-02 AND FORM NR 01-AA-45. COMPLIED WITH ALL PROCEDURES WITHIN. ENGINE RUNUP, LEAK CHECK AND ALL SYSTEMS CHECK SATISFACTORY. (M) 2L74 4F4 F A20WE E23EA 20030520000122003052000012NM 2003 5 20 UIEA200300018 120030424A2612 WARNING LIGHT BOEING747 747243B 1384830NM NR 2 ENGINE FALSE INDICATIONA UIEAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA15516MC 22507 INFLIGHT ENGINE SHUTDOWN, NR 2 ENGINE WAS SHUTDOWN DUE TO FIRE DETECTION LIGHT AND FAULT LIGHT. NR 2 FIRE DETECTION 'A' LOOP WOULD NOT TEST. COMPLETED ENGINE SHUTDOWN CHECKLIST. HYDRAULIC SYSTEM SHUTDOWN FOR 20 MINUTES. INCIDENT TIME FRAME, AIRCRAFT DEPARTED ANC 22:15Z. IRREGULARITY OCCURRED 07:15Z. AIRCRAFT BLOCKED IN AT PVG TO 07:48Z. FOR NR 2 ENGINE FIRE DETECTION 'A' CORRECTIVE ACTION, REF WDW WIRING CHECK FOR INSULATION AND RESISTANCE, FOUND OK. CLEANED ALL ELEMENT CONNECTORS. INSTALLED BACK. GROUND TEST OK PER MM 26-11-02. (M) 2L74 4F A20WE 20030520000142003052000014NM 2003 5 20 UIEA200300020 120030428A3230 TRUNNION BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NLG LACK OF LUBE A UIEAO OTHER WJ INADEQUATE Q C WARNING INDICATION APAPPROACH 1 EA15523MC 21782 NOSE LANDING GEAR WOULD NOT EXTEND NORMALLY. EXTENDED OK WITH ALTERNATE SWITCH. LUBRICATED NOSE LANDING GEAR TRUNNIONS PER MM 12-21-01. JACKED AIRCRAFT PER MM 7-11-02. RESET ALTERNATE GEAR SYSTEM PER 32-36-00 AND ACCOMPLISHED NOSE LANDING GEAR SWING PER 32-34-00. OPS CHECK NORMAL. (M) 2L74 4F4 FRTA20WE E23EA 20030520000182003052000018NM 2003 5 20 AMTA200300545 120030422A4900 APU BOEING757 75733N 1384931NM MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11551TZ 32585 APU WOULD NOT START, 3 ATTEMPTS RPM GOT UP TO 14 PERCENT. PERFORMED APU BITE, NO DEFECTS NOTED IAW FIM 49-11-00-2. OPERATIONAL CHECK 3 TIMES NORMAL PER MM 49-11-00-802. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20030520000292003052000029NM 2003 5 20 GTIA030262 120030418A1100 SIGN DOUG MD80 MD83 3023681NM CABIN DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 GLO-PATH EXIT SIGNS ARE UNREADABLE AT ALL FOUR OVERWING EXITS AND L2 DOOR. REMOVED AND REPLACED EXIT SIGNS AT ALL FOUR OVERWING EXITS AND L2 DOOR FOR GLO-PATH LIGHTING, AFE-T-GLO. (M) 2L72 4F RT 20030520000352003052000035SO 2003 5 20 SIMA200309601 120030402A532014521725001 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED NUTPLATE AND BLENDED THE CORRODED AREA OF THE CENTER SILL AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER. REPAIR DONE IAW AEA ETN EM-53-036R1 AND STANDARD EMB SRM, SRM 145/1142 REV 20, PRACTICES. (M) 2L72 4F RTT00011AT 20030520000432003052000043NM 2003 5 20 AALA20030382 120030327A3350 SWITCH BOEING767 767223 1385123NM EMERGENCY LIGHT FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21317AA 22319 SFO - EN ROUTE JFK-SFO, DURING CLIMB-OUT, EMERGENCY EXIT LIGHT ILLUMINATED AND STAYED ON. LANDED SFO WITHOUT INCIDENT. TIGHTENED EMERGENCY EXIT LIGHT SWITCH IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030514001022003051400102NM 2003 5 14 SWAA031003 120030505A53116546540 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AND CRACKED AT BS 639, BETWEEN WL 208 & WL 212 RT SIDE. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030514002182003051400218NM 2003 5 14 03FDEA00719 120030430A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE FLAP SIDE AT FLAP LOWER SURFACE AFT HOLE QTY 2 EACH WITH CORROSION. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP. 2L73 4F RTA22WE 20030515000042003051500004EA 2003 5 15 03134657 120030514A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 DURING MAINTENANCE INSPECTION, THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515000332003051500033EA 2003 5 15 03133630 120030513A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE BOARDING AREA, AND CABIN EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515000792003051500079EU 2003 5 15 03119303 120030429A33506040751 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27303UE 41015 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISCOVERED THE AFT EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE NR 4 POWER SUPPLY AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030520000202003052000020WP 2003 5 20 GTIA030265 120030419A3260 UPLOCK SENSOR DOUG DC9 DC983 3022083WP MLG FAILED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23826NK 49391 AFTER TAKEOFF, GEAR RETRACTION LEFT MAIN LIGHT REMAINED ILLUMINATED UNTIL LEVEL OFF AT 10,000 FEET, ACCOMPLISHED QRH TIMES. INSPECTED THE LMG STRUCTURE AND RETRACT MECHANISM AND DETERMINED NO VISABLE DAMAGE. INSPECTED THE LMG PROX SENSORS AND FOUND LMG UPLOCK PROX SENSOR DAMAGED. REMOVED AND REPLACED THE LMG UPLOCK SENSOR AND AJUSTED THE GAP. OPS CHECK GOOD ON PROX TEST. (M) 2L72 4F RTA6WE 20030520000552003052000055WP 2003 5 20 GTIA030255 120030414A73338TJ85GBA2 TRANSMITTER DOUG DC9 DC981 3022081WP FUEL FLOW FAILED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23806NK 48051 RSW - FLT 1504 - LEFT ENGINE HAD EXCESSIVE FUEL FLOW 5100 NR/HR AT CRUISE ALT 31,000 FEET DID QRH FOR HIGH FUEL FLOW. TROUBLESHOT TO FUEL FLOW TRANSMITTER, REMOVED AND REPLACED LEFT FUEL FLOW TRANSMITTER. OPS AND LEAK CHECK GOOD. (M) 2L72 4F A6WE 20030521000302003052100030WP 2003 5 21 DHL2003804892 120030207A5553 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 CORROSION ON JOINT ANGLE BETWEEN FUSELAGE AND VERTICAL STABILIZER, STA 1766.000, L-3L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 PG 44A-44B FIG 16A. REMOVED CORROSION ON ANGLE IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED AREA IAW SRM 53-2-5 PG 44A-44B. FABRICATED FILLER (7075-T6AL 0.160) AND SHIM (7075-T6AL-0.125) AND REINFORCEMENT ANGLE (STEEL 177-PH-0.080) IAW SRM 53-2-5 PG.44A-44B. CLEANED, TREATED AND PRIMED FILLER AND SHIM AT INNER AREA IAW SRM 51-1-8B. INSTALLED FILLER, SHIM AND REINFORCEMENT ANGLE ON JOINT ANGLE BETWEEN FUSELAGE AND VERTICAL STAB STA 1766.000, L-3L IAW SRM 53-2-5 PG 44A-44B FIG-16A, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1 (PRC). 2L74 4F RT4A25 20030521000332003052100033WP 2003 5 21 MWEA030209 120030514A53509911500283 PIN DOUG DC9 DC981 3022081WP RADOME CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 RADOME RIGHT UPPER GUIDE PIN LOWER CRACKED. INSTALLED DOUBLER. 2L72 4F A6WE 20030521000372003052100037NM 2003 5 21 DHL2003783002 120030429A2121219201 GASPER FAN BOEING727 727227 1384078NM CABIN ODOR A DHLAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01766AT 21999 GASPER FAN POPS CIRCUIT BREAKER AND HAS ELECTRICAL ODOR. REPLACED GASPER FAN IAW MM 21-23-1. OPS CHECKED GOOD. 2L73 4F A3WE 20030521000382003052100038WP 2003 5 21 DHL2003604527 120030501A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING - OUTBOARD STUB WING FORMER CRACKED 0.500 AT XS 539.000. STOP DRILLED CRACK AT XS 539.000 AND FABRICATED DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000412003052100041WP 2003 5 21 DHL2003804901 120030125A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E FORMER AT STA XFS 354.000 WITH 1.500 INCH CRACK. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER ANGLE INNER SIDE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AND NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000492003052100049EU 2003 5 21 MALA030253 120030501A3150 WARNING LIGHT SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15449XJ 340B449 FLIGHT IDLE STOP WAS PULLED AND CONFIG WARNING HORN DID NOT ILLUMINATE OR GO OFF WHEN LT ENGINE WAS STARTED DURING FLIGHT 3111. FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED WHEN A/C WENT WHEELS UP. NO OTHER INFORMATION AT THIS TIME. NO FLIGHT INTERUPTION NOTED FROM LOG PAGE 1085858-10/11. 2L72 4T RTA52EU 20030521000532003052100053EU 2003 5 21 MALA030257 120030418A5553 ANGLE BAC 146 AVRO146RJ85A1500097EU WING TO STAB CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 LEFT VERTICAL STABILIZER TO FUSELAGE CLOSING ANGLE CRACKED. MAINTENANCE REPAIRED PER EO A53112. 2H74 4F RTA49EU 20030521000672003052100067WP 2003 5 21 MWEA030208 120030514A53305910228210 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 CRACKS FOUND AT CANTED FRAME STATION 1474 LOCATED APPROXIMATELY BETWEEN LONGERON 14R & 15R. INSTALLED DOUBLER. 2L72 4F A6WE 20030521000782003052100078WP 2003 5 21 DHL2003804904 120030121A534752772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 MAIN CARGO COMPT NR 1 RT TRACK LUG WORN STA 1670.000 - STA 1770.000. REMOVED DAMAGED TRACK AREA IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SECTION WITH NEW FASTENERS ON MAIN CARGO COMPT 1 RT TRACK STA 1670.000 - STA 1770.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521000792003052100079WP 2003 5 21 DHL2003801011 120030427A575457696004 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT OUTER WING INBOARD L/E OUTER PLATING CORRODED AT STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030405, ED 3260. REMOVED FASTENERS IAW SRM 51-1-21 PG 2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT CORRODED AREA IAW EODHL 030405, ED 3260. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6 0.050) AND DOUBLER (7075-T6 0.063) IAW EODHL 030405, ED3260. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INNER PART IAW SRM 51-1-8B. APPLIED ON SPLICE SURFACE IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL 030405, ED 3260, SRM 51-1-21 PG 2, SRM 51-1-20D PG 9 AND SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030521000802003052100080WP 2003 5 21 DHL2003801020 120030418A57105769933184 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING L/E OUTBOARD VANE SHOWS ELONGATED HOLES AT STA XOLDO 67.0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030410, ED-3265 CUT OUT DAMAGED AREA IAW EO DHL 030410, ED 3265. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6 0.063) AND INNER DOUBLER (7075-T6 0.050) AND OUTER DOUBLER (7075-T6 0.071) IAW EO DHL 030410, ED -3265. CLEANED, TREATED AND PRIMED INNER SIDE OF FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLERS WITH NEW FASTENERS IAW EO DHL 030410, ED 3265, SRM 51-1-21 PG 1 SRM 51-1-20D PG 9 SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030521000842003052100084WP 2003 5 21 MWEA030206 120030509A7120 COVER DOUG DC9 DC981 3022081WP ENGINE ISOLATOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LEFT LOWER FORWARD ISOLATOR COVER HAS LITE CORROSION IN THE ATTACH BOLT HOLES AND ON MOUNTING SURFACE. REMOVED AND REPLACED LEFT LOWER FORWARD ISOLATOR. 2L72 4F A6WE 20030521001002003052100100NM 2003 5 21 HNAA0300022 120030512A3397 CONNECTOR DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT LOOSE A HNAAO OTHER O OTHER NRNOT REPORTED 1 EA07966HA 452 CREW REPORTED THAT THE FIRST TWO FLOOR EMERGENCY LIGHTS WERE INOP. RESEATED CONNECTOR ON EMERGENCY LIGHTS POWER SUPPLY. 2H72 4T RTA13NM 20030521001132003052100113WP 2003 5 21 DHL2003801043 120030413A5210 SKIN DOUG DC8 DC873F 302199FWP PAX DOOR WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 FWD PASSENGER DOOR- EXTERNAL SKIN AROUND HANDLE SHOWS WEAR OUT OF LIMITS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1. FABRICATED NEW SKIN (2024-T6 AL0.050) IAW SRM 52-3-1 PG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SKIN IAW SRM 52-3-1 PG 2, SRM 51-1-21 PG 1 AND SRM 51-1-15 PG 1. REFER TO N/R 2026 FOR FWD PASSENGER DOOR REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20030521001262003052100126NM 2003 5 21 DHL2003783006 120030514A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 GROUNDED A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01766AT 21999 FOLLOWING LANDING, THE NR 3 DETECTOR CIRCUIT GROUND ON THE P6 3 V-PANEL ILLUMINATED. FOUND LOOP TOUCHING SUPPORT BRACKET. RE-SECURED LOOP. OPS CHECKED GOOD PER 26-21-0. 2L73 4F A3WE 20030521001312003052100131NM 2003 5 21 DHL2003726004 120030514A2612 FIRE LOOP BOEING727 727228 1384083NM NR 3 SHORTED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01726DH 20409 ENGINE NR 3 SYSTEM B-FIRE DETECTION LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE CHECK LIST. SWITCHED TO SYSTEM-A SYSTEM TESTED NORMALLY. FOUND SHIELD FOR FIRE LOOP CONTACTING B-LOOP. CLEARED SHIELD, OPS TESTED NORMALLY. 2L73 4F RTA3WE 20030521001322003052100132NE 2003 5 21 DHL2003781003 220030515A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE NR 3 MALFUNCTIONED A DHLACD ABORTED TAKEOFF RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO01768AT 21996 707130 RTO: 158,500 LBS, 80 KTS, 26 DEGREE C, 570 FT PA, BRAKE ENERGY ZONE NORMAL. ENGINE NR 3 WOULD NOT MAKE T/O THRUST 2.04 ACTUAL EPR 2.16 TARGET 93 PERCENT N, ACTUAL, 100 DEG TARGET, EGT 645 DEG (FF 10,000). ENGINE NR 1 AND NR 2 NORMAL 216, 218, 100 PERCENT. ENGINE NR 3 THRUST LEVER FIRE WALLED. PERFORMED ENGINE TRIM ON NR 3 ENGINE. ADJUSTED FUEL CONTROL IAW DHL JRH CHAPTER 7.7, ENGINE TRIM PROCEDURES. FILED OUT ENGINE TRIM RECORD AND FUEL CONTROL ADJUSTMENT RECORD. OPS CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20030521001572003052100157WP 2003 5 21 DHL2003604507 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBOARD L/E FORMER WITH 0.500 INCH CRACK STA XFS 578.750. STOP DRILLED CRACK AT STA XFS 578.750 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, 51-1-21 PG 1. 2L74 4F RT4A25 20030521001642003052100164NM 2003 5 21 SWAA031084 120030514A52106547952 SKIN BOEING737 7372H4 138448CNM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA ACO. 2L72 4F A16WE 20030609001332003060900133NM 2003 6 9 AWXA200300578 120030521A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 LAS - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD ENTRY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD ENTRY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030609001362003060900136NM 2003 6 9 AWXA200300581 120030504A5313146N5447 STRINGER BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 3. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 3; FABRICATED A NEW SECTION OF FLOOR SUPPORT STRINGER, AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030609001492003060900149SO 2003 6 9 C2XA03SH153 120030525A532014524131009 SUPPORT EMB 145 EMB145ER 3260211SO THRESHOLD CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE FORWARD PASSANGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030609001782003060900178EA 2003 6 9 CA030501005 120030501A3251750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NLG STEERING FAILED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) AFTER TAKE OFF GOT A STEERING INOP MESSAGE FOLLOWED BY GEAR DISAGREE , WITH NOSE GEAR NOT IND IN THE UP POSITION, AIRCRAFT RETURNED WITH NO INCIDENT TOTAL TIME 10992 HRS. 2L72 4F4 FRTA21EA E15NE 20030609001842003060900184EU 2003 6 9 CA030502003 120030430A7603LN93556X32 BOLT BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL N2 LEVER LOOSE W O OTHER EJ VIBRATION/BUFFET WARNING INDICATION APAPPROACH 1 CA (CAN) ON APPROACH, PILOT APPLIED COLLECTIVE PITCH AND NOTICED NR 1 TORQUE SPLIT AWAY FROM NR 2 ENG TORQUE. FURTHER APPLICATION MADE MATTERS WORSE. AFTER LANDING , MAINTENANCE PERSONNEL INVESTIGATED AND FOUND THE BOLT ATTACHING THE N2 LINKAGE TO THE AFT SIDE OF THE DUAL HYDRAULIC UNIT HAD BACKED OUT. THIS ALLOWED THE NR 1 LINKAGE ROD END TO DISCONNECT. THE NR 2 CONNECTOR REMAINED IN PLACE WITH THE BOLT NOT ALL THE WAY BACKED OUT. THE BOLT WAS REINSTALLED THROUGH BOTH LINKAGE ROD ENDS AND CHECKED TO MAKE SURE THAT IT WAS IN SAFETY. IT WAS NOTED DURING INSTALLATION OF THE BOLT THAT THERE WAS DRAG TORQUE PRESENT BETWEEN THE BOLT AND THE NUT PLATE. THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H3EU E4CE 20030609001862003060900186EU 2003 6 9 CA030516005 120030516A2910D133756E01 MANIFOLD BOLKMS105 BO105CBS 5626008EU HYD SYSTEM FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THIS UNIT WAS RECEIVED FOR REPAIR. DURING INCOMING FUNCTIONAL CHECK IT WAS NOTED THAT THE CHANGE OVER FROM SYSTEM 1 TO 2 WAS VERY SLUGGISH & STIFF. DISASSEMBLY OF THE VALVE BODY MANIFOLD REVEALED CORROSION INSIDE THE THREADED PLUGS OF BOTH SYSTEMS. THE MOISTURE MAY HAVE BEEN TRAPPED AS A RESULT OF PRESSURE WASHING THIS UNIT, COMBINED WITH AN ACCUMULATION OF DIRT AND OIL BLOCKING THE DRAIN HOLE. THE DRAIN HOLES ARE NOT EASILY ACCESSIBLE FOR INSPECTION CLEANING. MAINTENANCE PERSONNEL SHOULD BE MORE DILIGENT NOT TO USE PRESSURE WASHING EQUIPMENT IN THIS AREA. 1G72 3U NCH3EU 20030609001872003060900187EU 2003 6 9 CA030516006 120030513A2750 FLEX COUPLING PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TE FLAPS DAMAGED W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 CA (CAN) ON APPROACH THE FLAP CAWS LIGHT CAME ON WHEN FLAPS WERE SELECTED DOWN FOR APPROACH. THE AIRCRAFT LANDED WITH 0 FLAP SETTING. MAINTENANCE WAS ABLE TO PRODUCE AN ASSYMETRIC FLAP CONDITION ON THE GROUND THRU THE USE OF THE FLAP MAINTENANCE SWITCH. INSPECTION REVEALED THE LT INBOARD FLAP FLEX DRIVE SHAFT SHEARED IN TWO PIECES INSIDE THE HOUSING. A NEW DRIVESHAFT WAS INSTALLED AND FLAP SYSTEM RIGGED. FURTHER INSPECTION OF THE 3 REMAINING DRIVESHAFTS FOUND EXCESS CORROSION ON THE CABLE. THE AIRCRAFT WAS GROUNDED UNTIL REPLACEMENT DRIVESHAFTS WERE INSTALLED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030609001942003060900194CE 2003 6 9 CA030520005 120030520A323050410051 SPRING CESSNA310 310L 2074230CE CONT O470 IO470VO 17026SO DOWNLOCK BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING WALK-AROUND PRIOR TO FLIGHT, PIC NOTICED DOWNLOCK SPRING HANGING FROM ONE ATTACH POINT AND UPON INSPECTION WAS FOUND BROKEN AT ATTACH POINT ABOUT 1/2 AN INCH ABOVE SPRING BODY. SPRING WAS REPLACED NEW. 1L72 3O3 O 3A10 3E1 20030609001982003060900198 2003 6 9 HEEA086571 420030522A22107690001812102 BRAKE SKRSKYS76 S76A 8143006NE AUTOFLIGHT STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROLL MAG BRAKE STICKS IN LATERAL MODE. TO BE SENT TO VENDOR. 1G72 3U H1NE 20030605000912003060500091NM 2003 6 5 UPS03240685 120030417A5310 DOOR FRAME BOEING727 72722C 138400FNM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, SUSPECT CRACK AT NR 1 STOP FITTING CUT OUT ON FWD FRAME OF AFT CARGO DOOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-30-02 & SMRO EO 2003-025-021 UPS ENGINEERING FILE NO. B727-5330-18744-A 2L73 4F A3WE 20030515000802003051500080EA 2003 5 15 03117679 120030427A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISCOVERED AN EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030515001032003051500103NM 2003 5 15 03FDEA00616 120030423A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FITTING HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69216 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030515001692003051500169NM 2003 5 15 AWXA200300487 120030502A532069353521 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN AFT CARGO COMPARTMENT AT BS 727D, STR 23 LT. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 727D, STR 23 LT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 38, FIG 8 AND SRM 51-40-05 PG 7 FIG 4. 2L72 4F RTA16WE 20030515001722003051500172EU 2003 5 15 AWXA200300490 120030429A5321261NF FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN CENTER OF FLOOR PANEL 261NF. MAINTENANCE PERFORMED COMPOSITE REPAIR OF CRACK IN CENTER OF FLOOR PANEL 261NF IAW A320 SRM 53-02-00 PG 203-207 FIG 202. 2L72 4F RTA28NM 20030515001732003051500173EU 2003 5 15 AWXA200300491 120030427A5320D53112091200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND AT FASTENER HOLE ON FLOOR SUPPORT Y1292, FR 18. MAINTENANCE CUTOUT DAMAGED AREA ON FLOOR SUPPORT Y1292, AT FR 18; FABRICATED 2 EACH REPAIR ANGLES AND A FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 201-210 FIG 201, SRM 51-21-11 PG 5-7, SRM 51-23-11 PG 20 AND SRM 51-42-11 PG 8-12 FIG 2-3. 2L72 4F RTA28NM 20030520000232003052000023WP 2003 5 20 GTIA030272 120030411A5553 ANGLE DOUG DC9 DC983 3022083WP VERTICAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 RIGHT INNER DORSAL FIN ANGLE CRACKED AT FS 1437. REMOVED RIGHT DORSAL FIN INNER ANGLE. LOCATED AND DRILLED NEW DORSAL FIN INNER ANGLE. INSTALLED INNER DORSAL FIN ANGLE. (M) 2L72 4F RTA6WE 20030520000262003052000026SO 2003 5 20 SIMA200309613 120030325A524014521725001 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21804AE 145487 THIS IS A LEVEL TWO FINDING FOUND DURING AN MBV INSPECTION SERVICE DOOR CENTER SILL CORRODED. BLENDED OUT CORROSION ON SERVICE DOOR SILL. FABRICATED 3 REPAIR DOUBLERS AND INSTALLED IAW ETN NR EB-53-032R1 AND IC2003-145-1094. (M) 2L72 4F RTT00011AT 20030520000422003052000042NM 2003 5 20 AALA20030378 120030328A3397 CONNECTOR BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21330AA 22330 DURING OVERNIGHT MAINTENANCE, LAST THREE EMERGENCY LIGHTS ON EXTERIOR FUSELAGE INOPERATIVE. REATTACHED CONNECTOR FOR EMERGENCY LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520000472003052000047SO 2003 5 20 SIMA200311302 120030402A532014521725615 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, AFT SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-20-01/03, 51-40-02/04/06. (M) 2L72 4T RTT00011AT 20030520000642003052000064NM 2003 5 20 AMTA200300546 120030422A360010746016 PILOT VALVE BOEING757 75733N 1384931NM RT ENGINE FAILED A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11553TZ 32587 RIGHT ENGINE HIGH STAGE EICAS MESSAGE. REMOVED AND REPLACED HIGH STAGE PILOT PER FIM 36-10-00-1 FIG 111. OPS CHECKS GOOD. REF MM 36-11-08-4. (M) 2L72 4F RTA2NM 20030520000842003052000084WP 2003 5 20 AMTA200300476 120030321A5310 SHEAR TIE LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 AFT FUSELAGE SECTION, F/S 1792, CORROSION ON LOWER FRAME SHEAR TIE. REPAIRED DAMAGED AREA IAW SRM 53-12-00 FIG 805. (M) 2L73 4F A23WE 20030520000872003052000087CE 2003 5 20 2003F00262 120030330A2697 TERMINAL BEECH 1900 1900D 1154162CE BOTTLE SQUIB LOOSE A GUUAO OTHER N FALSE WARNING CRCRUISE 1 SO1987555 UE234 DURING FLIGHT, FIRE EXTINGUISHER DISCHARGE LIGHT FLASHES ON AND OFF. CONTINUED TO FLL. SECURED LOOSE TERMINAL AT LEFT SQUIB. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20030520000922003052000092NM 2003 5 20 AALA20030429 120030409A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 28-30HJ INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520000932003052000093NM 2003 5 20 AALA20030452 120030412A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21795AN 30257 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY LOWER LEFT CORNER BROKEN. REPLACED EMERGENCY EXIT LIGHT AT FORWARD GALLEY LOWER LEFT CORNER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030520001002003052000100NM 2003 5 20 AALA20030350 120030316A2420GEN5103 IDG BOEING767 767323 1385205NM RT ENG GEARBOX FAILED A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW2139364 24045 OGG - FLT 7 - DURING CRUISE, THE RIGHT GEN DRIVE LIGHT ILLUMINATED PERFORMED CHECKLIST PROCEDURE RAN APU AND CONTINUED TO DESTINATION, NO FURTHER PROBLEMS. REMOVED AND REPLACED RIGHT ENGINE IDG PER MM, OPS AND LEAK CHECK GOOD, OK FOR SERVICE. (M) 2L72 4F RTA1NM 20030520001052003052000105NM 2003 5 20 AALA20030402 120030401A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21786AN 30250 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING ON LEFT SIDE OF FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030605000942003060500094NM 2003 6 5 UPS03240688 120030414A5311 FRAME BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, CORROSION ON FRAME TIE ANGLE BS 351.2 S24L - S25L. DAMAGE REMOVED IAW SRM 51-10-01 FOUND OUTSIDE LIMITS. REPAIR SECTIO N FABRICATED IAW FLAP PATTERN LAYOUT AS PER SRM 51-20-1. 2L73 4F A3WE 20030605001062003060500106EU 2003 6 5 HDN2003F00000 120030330A7931DK040 TRANSMITTER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 2 OIL PRESS INOPERATIVE D HDNAO OTHER O OTHER NRNOT REPORTED 1 SW03105SE S769 CAE821660 WHEN ENGINE OIL PRESSURE TRANSMITTER IS INSTALLED ON AIRCRAFT, PORT WAS INOPERATIVE, THE PRESSURE GAUGE WENT TO THE RED ON THE GAUGE. (REG NR CHANGED FROM 911VH TO 105SE RESERVED N-NUMBER) 1G72 3U3 U H3EU E4CE 20030605001582003060500158CE 2003 6 5 DXTA200300032 120030516A3230 LANDING GEAR CESSNA500 560CESSNA 2076750CE MAIN MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07308QS 5600277 GEAR WOULD NOT RETRACT AFTER TAKEOFF . HAD NO PROBLEM EXTENDING FOR LANDING DID NOT USE EMERGENCY BLOW DOWN . NOSE ANNUNCIATER REMAINED GREEN AND RED ANNUN REMAINED ON. 2L72 4F RTA22CE 20030606000392003060600039NM 2003 6 6 IU62003F00018 120030410A2761654494713 HOUSING BOEING BOEING737 737* NM ACTUATOR BROKEN B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 9406 ACTUATOR HOUSING HAS A BROKEN LUG, CAUSED BY FATIGUE. 2L72 4F RTA16WE 20030606000492003060600049CE 2003 6 6 NE52003F00002 120030515A3710442CW PUMP CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 2 ENGINE VACUINOPERATIVE B NE5RO OTHER O OTHER NRNOT REPORTED 1 GL13596DM 48 402C0255 VACUUM PUMP INOPERATIVE. 1L72 3O3 O A7CE E8CE 20030606000802003060600080NM 2003 6 6 03FDEA00769 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP I/B HINGE (FLAP SIDE) AFT ATTACHING POINT BOTH FWD AND AFT BOLT HOLES CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000922003060600092NM 2003 6 6 COOSDR030019 120030501A5755 SKIN BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 9 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG 22 20725 RT WING, FLIGHT SPOILER NR 9, PN 65-17348-66, SN 22, WITH DELAMINATION. 2L73 4F4 FRTA3WE E2EA 20030606000932003060600093NM 2003 6 6 COOSDR030020 120030501A5755 SKIN BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 7 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG 196 20725 LEFT WING, GROUND SPOILER NR 7, PN 65-17348-66, SN 196, WITH DELAMINATION. 2L73 4F4 FRTA3WE E2EA 20030606000952003060600095NM 2003 6 6 COOSDR030022 120030501A5755 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 8 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG 220 20725 RIGHT WING, GROUND SPOILER NR 8, PN 65-17348-83, SN 220, WITH DELAMINATION. 2L73 4F4 FRTA3WE E2EA 20030609000102003060900010SO 2003 6 9 SWIA200311977 120030512A7997 WIRE EMB 120 EMB120ER 3260203SO NR 1 ENG OIL CHAFED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07233SW 120307 ABORTED TAKEOFF FOR AURAL WARNING ''OIL'' WITH LIGHT FLASHING ON MAP (OIL PRESS). PERFORMED AURAL WARNING RESET AND STATIC RUN UP. STILL RECEIVED ''OIL'' AURAL WARNING. FOUND AND REPAIRED A CHAFED WIRE ON NR 1 ENGINE OIL PRESSURE SWITCH. GROUND RUN UP OPS CHECK GOOD. 2L72 4T RTA31SO 20030609000292003060900029WP 2003 6 9 0301029151 120030520A5210 SEAL DOUG DC9 DC914 3022034WP PAX DOOR LEAKING A NWAAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL018909E 45770 CLIMBING THROUGH FL 270 THE "CABIN PRESSURE" WARNING ILLUMINATED. CABIN WAS AT 10,000 AND 4.2 PSI DIFFERENTIAL WITH OUTFLOW VALVE FULLY CLOSED. BOTH PACKS WERE INDICATING NORMAL PRESSURE. CREW INITIATED AN EMERGENCY DESCENT WITH POWER ON TO FL 170 UNTIL CABIN CONTROL WAS REGAINED. CABIN ALTITUDE WAS MAINTAINED AT 8000 WITH A 3.4 PSI DIFFERENTIAL. FLIGHT ATTENDANT REPORTED A LOUD AIR LEAK AT AFT CABIN PLUG DOOR. LANDING AT CMH WAS UNEVENTFUL AND MAINTENANCE RESEATED THE PLUG DOOR. AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20030609000492003060900049NM 2003 6 9 CALA0300263 120030521A5230 SKIN BOEING737 7373T0 1384582NM C-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND A 1/2 INCH CRACK IN C-2 DOOR INNER SKIN AT ACCESS PANEL CUTOUT BELOW HANDLE. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01029. 2L72 4F RTA16WE 20030609000612003060900061EA 2003 6 9 SWIA200311979 120030514A77145071T98P02 AMPLIFIER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 1 ENGINE FAULTY A SWIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 NM07594SW 7285 APPROXIMATELY 2 MINUTES AFTER TAKEOFF THE RIGHT ENGINE ROLLED BACK AND WOULD NOT PRODUCE POWER. TRIED TO RESTART, BUT RELIGHT FAILED. RETURNED TO IAH.TROUBLESHOOTING SYSTEM DETERMINED THE RIGHT ENGINE N1 AMPLIFIER TO BE FAULTY. SUPPLEMENTAL REPORT FORTHCOMING. UPDATE: 5/20/03 SLC: REMOVED AND REPLACED NR 2 RT AMPLIFIER IAW MM 73-21-03. RUN RT ENGINE IAW MM 71-00-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030609000652003060900065EA 2003 6 9 SWIA200311988 120030520A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB FAILED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07407SW3381 3021 7034 STAB CHI INOP ON CLIMB OUT. AGAIN ON DESCENT. REMOVED AND REPLACED MCU AND HSTA . TESTS GOOD. 2L72 4F RTA21EA 20030609000912003060900091EA 2003 6 9 QXEA0300647 120030519A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09608QX 10026 AFT LAVATORY SMOKE DETECTOR MESSAGE. TESTED AND FOUND TO BE GOOD FOR SERVICE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030611001332003061100133EA 2003 6 11 2003F00361 120030515A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA NR 2 ENGINE FAILED A FDKAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07510MJ 10101 FRL - FLT 6570 - SAN-TUS, RETURNED TO FIELD DUE TO LOSS OF NR 2 ENGINE EDP HYD PRESSURE. MAINTEANCE PERFORMED MAINTENANCE ACTION FOR MEL 29-11-01 AND RETURNED A/C TO SERVICE. MAINTENANCE REPLACED THE PUMP. (M) 2L72 4F RTA21EA 20030611001652003061100165EA 2003 6 11 SWIA200312007 120030526A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07412SW 7101 CENTER STEP BOARDING LIGHT IS INOP. REPLACED LIGHT BULBS IN CENTER STEP BOARDING LIGHT PER MM 33-45-01. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030612000172003061200017SO 2003 6 12 C2XA03SH161 120030528A531514530627001 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM HAS CORROSION UNDER THE COMPOSITE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030612000432003061200043EU 2003 6 12 MALA030284 120030528A7930522794 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE ENG OIL PRESS FLUCTUATES B MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15115XJ DURING FLIGHT 2754, RECURRING LT ENGINE OIL PRESS FLUCTUATES/CONSUMPTION. LEFT ENG OIL PRESSURE FLUCTUATES BETWEEN 50 AND 80 PSI, NO RELATED INDICATIONS BELIEVED TO BE GAUGE NOT ENGINE. DECLARED EMERGENCY. MAINTENANCE REPLACED LT ENG OIL PSI GAUGE P/N 522794, S/N OFF 04871374, S/N ON B592A, IAW AMM 79-50-15, OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20030612000632003061200063EA 2003 6 12 SWIA200312037 120030525A2910 LINE CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYS LEAKING A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM07595SW 7292 ON A 10 MILE FINAL TO RUNWAY 26 - HYD 2B LOW PRESS MESSAGE APPEARED. HYD 2B RESERVOIR APPEARS TO BE EMPTY. REMOVED AND REPLACED HYDRAULIC LINE ON NR 2 HYDRAULIC SYSTEM SERVICE PORT IAW CL600 20-22-00. OPS CHECK GOOD. RESERVICED HYDRAULIC SYSTEM RESERVOIR IAW CL600 12-12-29. 2L72 4F RTA21EA 20030612000872003061200087WP 2003 6 12 UPS03840711 120030528A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 EMERGENCY EXIT LIGHTS WERE LEFT IN ARMED POSITION. BATTERY IS DEAD. CHECKED EMERGENCY LIGHTS. FOUND BATTERY PACK DISCHARGED AND ONE BATTERY SPLIT OPEN. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL 33-50-00. 2L74 4F RT4A25 20030612001332003061200133WP 2003 6 12 UPS03840721 120030503A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C-2 FWD PIT RBL 45 STA 70 FLOORBEAM CORRODED. BLENDED OUT CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED REPAIR ANGLE AND FILLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE AND FILLER IAW DC8 SRM 51-1-21 & 51-3-0. RESECURED SEAT TRACK AND INSTALLED 4 EA FLOORBOARDS IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030612001702003061200170SO 2003 6 12 SWIA200312043 120030531A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07196SW1350 157 120151 FLAP PANEL INDICATES ASYMMETRY, CONTROL FAULT & DISAGREEMENT AT SAME TIME ALONG WITH MECHANICAL FLAP INDICATOR AT 15 DEGREES AND ADVANCED SWS & FLAP AMBER LIGHTS ON MAP. FLAPS DO NOT TEST AND DO NOT RESET AND DO NOT FUNCTION. REMOVED AND REPLACED FLAP ANNUNCIATOR WITH SERVICEABLE UNIT. FUNCTIONAL TEST OK, BITE TEST OK - RST OK. FLAP GAP CHECK OK. OPS CHECK GOOD IAW 27-50-05. 2L72 4T RTA31SO 20030613000062003061300006EA 2003 6 13 SWIA200312059 120030421A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 FS 193 ELECTRICAL BAY RT FLOOR CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE IAW CRJ REO 601R-53-11-245 REV NC. 2L72 4F RTA21EA 20030613000202003061300020NM 2003 6 13 UPS03440783 120030520A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 2180-2200 STR 12L STRINGER CRACKED. M/D BS 2180-2200 STR 12L REPAIRED AS PER HX RS 53-61-35030 & UPS ENG 'R FILE 747-53-20140. 2L74 4F RTA20WE 20030613000382003061300038SO 2003 6 13 C2XA03CL104 120030605A335066903 LIGHT EMB 135 EMB135ER 3260203SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715509 145238 CLE FLIGHT 2083, THE CREW REPORTED AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030613000722003061300072SO 2003 6 13 C2XA03SH168 120030608A532014522178005 THRESHOLD EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613001242003061300124 2003 6 13 SWAA031199 420030528A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030613001452003061300145NM 2003 6 13 SWAA031226 120030602A33506556633 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29732SW 27864 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030617000472003061700047EU 2003 6 17 CA030527003 120030520A53021090372441 BULKHEAD AGUSTAA109 A109A2 0260120EU ALLSN 250C 250C20B 03013GL TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A SCHEDULE INSPECTION, IT WAS REVEALED ON A PREVIOUS REPAIR, WITH LESS THAN 302 HOURS, BULKHEAD AND REPAIRED DOUBLER WERE CRACKED. AS WELL 2 FURTHER CRACKS WERE FOUND APPROXIMATELY 5 INCHES ABOVE INITIAL CRACK IN BULKHEAD. ALL CRACKS DESCRIBED ABOVE IS BETWEEN STA. 9036.0 TO STA 9248.7 & WL 18950.0 TO WL 1547.5 AMD AT BL 0.00 TO RBL 800. 1G72 3U3 U H7EU E4CE 20030617000482003061700048NM 2003 6 17 CA030527004 120030526A5610NP1653114 WINDSHIELD AIRBUSA319 A319114 3930350NM COCKPIT FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) F/O'S WNDSHIELD STARTED ARCING IN BETWEEN LAMINATES OF GLASS. THEN MULTILE CRACKING OCCURED. QRH PROCEDURE CARRIED OUT AND FLIGHT DIVERTED. WINDSHIELD TOTAL TIME 16,782HRS (ORIGINAL). 2L72 4F RTA28NM 20030617000662003061700066EA 2003 6 17 QXEA200300666 120030524A7120 MOUNT CNDAIRCL600 CL6002C10 1390015EA NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - YOKE HAS SEVERAL GOUGES AND SMALL DENTS AROUND LOWER MOUNT. REPAIRED IAW HORIZON AIR EA R-71-35. 2L72 4F RTA21EA 20030617000692003061700069EA 2003 6 17 QXEA200300668 120030520A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA PAX DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - MAIN CABIN DOOR LOWER AFT INNER SKIN IS DENTED AND SCRATCHED. REPAIRED IAW CRJ SRM 51-42-13 AND 51-42-06. 2L72 4F RTA21EA 20030617000762003061700076EA 2003 6 17 CA030526007 120030415A5511CFTP57 SPAR DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) INSPECTED STABILIZER FRONT SPAR AS PER 2 YEAR INSPECTION REQUIREMENTS OF A/D CF91-42. SPAR WAS FOUND CRACKED UNDER ATTACH BRACKET. CRACK STARTED AT UPPER BOLT HOLE FOR RIGHT ATTACH BRACKET. SPAR REPLACED WITH NEW PART AND AIRCRAFT RETURNED TO SERVICE 1H71 3R3 R A806 5E1 20030617000972003061700097 2003 6 17 ERAA087088 420030516A349740008330208 CABLE SKRSKYS61 S61N 8142104NE GE CT58 CT58* 30011GL IN1407B INOPERATIVE E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01561EH165 61471 SCREEN IN INOPERATIVE (NOT COMING ON). FOUND DEFECTIVE CABLE ON DATA PROCESSING BOARD. REPLACED CABLE AND TESTED. 2G72 4U4 U 1H15 1E3 20030617001052003061700105NM 2003 6 17 QXEA200300682 120030608A7921 DEFLECTOR BOMBDRDHC8 DHC8401 1390041NM OIL COOLER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - NR 1 OIL COOLER AIR DEFLECTION FOIL HAS CHAFE ON RIGHT HAND SIDE FROM LOWER COWL ANGLE. REPAIRED IAW Q400 PART 6, 51-00-02. 2H72 4T RTA13NM 20030617001192003061700119NM 2003 6 17 QXEA200300672 120030530A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM AFT PAX JAMMED A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09413QX 4060 BTM-ON FLIGHT NUMBER 2381, AFT PASSENGER DOOR JAMMED IN FRAME, WILL NOT OPEN OR CLOSE. RESET DOOR. OPERTED DOOR SEVERAL TIMES NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617001212003061700121NM 2003 6 17 QXEA200300673 120030602A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM NLG OUT OF ADJUST A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09414QX 4061 SEA-ON FLIGHT NUMBER 9801, AFTER ENGINE START, NOSE GEAR DOORS OPENED FOR 5 SECONDS AND THEN CLOSED ON THEIR OWN. NOSE GEAR UNSAFE LIGHT ILLUMINATED. FOUND NOSE GEAR DOWN 1 PROX SENSOR TOO FAR. ADJUSTED PROX SENSOR TO PROPER INDUCTANCE VALUE. GROUND RAN AIRCRAFT, MOVED NOSE WHEEL STEERING FRON SIDE TO SIDE. GEAR DOORS DID NOT OPEN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617001342003061700134NM 2003 6 17 QXEA0300651 120030527A2910 HYDRAULIC LINE BOMBDRDHC8 DHC8401 1390041NM HYD SYSTEM CHAFED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09400QX4625 4030 SEA-SUP-ON FLIGHT NUMBER 2328, AFTER TAKEOFF NR 2 HYDRAULIC SYSTEM FAILED. NOSE WHEEL CAME UP THE REST OF THE GEAR DID NOT. FLIGHT RETURNED TO FIELD, CREW DID ALTERNATE GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED FLEX LINE ON NR 2 MAIN LANDING GEAR UPLOCK ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617001452003061700145NE 2003 6 17 ERAA087101 120030520A64107610105101042 BLADE SKRSKYS76 S76 8143010NE TAIL ROTOR CRACKED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01574EH1369 760369 SPAR HAS A FIBERGLASS SPLINTER STICKING OUT AND LEADING EDGE STRIP IS CRADKED ON ONE BLADE. AREA OF SPLINTER UT INSPECTED PER 2ATI 3098, NO DELAMINATION FOUND SPLINTER REMOVED AND REPAIRED BY CTI. 1G72 3U H1NE 20030617001522003061700152NM 2003 6 17 QXEA200300709 120030604A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - DENTS DUE TO ICE DAMAGE ON FUSELAGE SKIN BETWEEN STATIONS X281 - X301. REPAIRED IAW HORIZON AIR EA 6-55-152B. 2H72 4T RTA13NM 20030617001532003061700153NM 2003 6 17 QXEA200300710 120030605A3213 STRUT BOMBDRDHC8 DHC8401 1390041NM LT MLG CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - LEFT MAIN LANDING GEAR STRUT IS CHAFED AT FOUR LOCATIONS ADJACENT TO UPPER ENDS OF AFT FAIRING. REPAIRED IAW CMM 32-11-03, PAGE 602, 2A 3A 1-6. 2H72 4T RTA13NM 20030612001302003061200130NM 2003 6 12 UPS03440776 120030519A5310 REVEAL BOEING747 747200 1384847NM DOOR FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - R5 DOOR FWD CUTOUT REVEAL CRACK AT S-16 AS MARKED. REPAIRED AS PER SRM 53-10-04 FIG 91 AT M/D R5 DOOR FWD CUT REVEAL AT S-16. 2L74 4F RTA20WE 20030612001842003061200184NM 2003 6 12 2003UALA00445 120030523A7500 SWITCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT BLEED MALFUNCTIONED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29676UA 30028 LT BLEED FAILED ON TAKEOFF ROLL. CREW WAS DOING A PACKS OFF TAKEOFF WITH ENG BLEED SWITCHES ON AND ALL ISOLATION VALVES OPEN. NORMAL CONDITION TO GET BLEED OFF ON ONE SIDE OR THE OTHER DUE TO DUAL BLEED PROTECTION. 2L72 4F4 FRTA1NM E24NE 20030613000372003061300037WP 2003 6 13 ABXA030189 120030604A5210 HANDLE DOUG DC9 DC941 302207NWP PAX DOOR BINDING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23972AX 47631 MAIN CABIN LEFT FORWARD ENTRY DOOR WOULD NOT OPEN. FOUND DOUBLER ON EXTERIOR DOOR BINDING EXTERIOR HANDLE, CHAMFERRED DOUBLE ON MAIN CABIN LEFT FORWARD ENTRY DOOR, NO BINDING NOTED. DOOR OPEN/CLOSED OKAY IAW DC-9 AMM 52-11-00. 2L72 4F A6WE 20030613000412003061300041EA 2003 6 13 SWIA200311997 120030514A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07433SW 7550 FLOORBEAM ATTACH ANGLES AT FS 280 RBL 9 ARE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11 PAR 4, 51-42-20, 51-42-06 & RII53-401. 2L72 4F4 FRTA21EA E15NE 20030613000962003061300096NM 2003 6 13 UPS03440809 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D- BS 1488 S10R STRINGER END FOUND CRACKED AS MARKED. M/D - BS 1488 S10R STRINGER END REPAIRED AS PER HX RS R53-61-35035 AND ENG'R FILE NUMBER 747-53-20146. 2L74 4F RTA20WE 20030613001002003061300100NM 2003 6 13 UPS03440813 120030516A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - FRAME FOUND CRACKED AT BS 360 BETWEEEN STR 14R AND 15R. FRAME REPAIRED AS PER RS 53-12-35026 AND UPS EO B747-5310-18852-A. 2L74 4F RTA20WE 20030613001182003061300118 2003 6 13 SWAA031193 420030529A2565 BOTTLE BOEING737 7377H4 1384404NM ESCAPE SLIDE DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29752SW 0110 29804 FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATION OUT OF LIMITS. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030617000392003061700039NE 2003 6 17 AUS20030492 220030430A7210311657901 GEAR DHAV DHC8 DHC8315 2809010NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE REDUCTION G/B FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 12223 (AUS) NR 1 ENGINE REDUCTION GEARBOX CHIP DETECTOR ACTIVATION. THE CHIP DETECTOR WAS REMOVED AND CONTAINED A FRAGMENT OF GEAR TOOTH. BOROSCOPE INSPECTION FOUND DAMAGE TO A SECOND STAGE REDUCTION GEAR TOOTH. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030617000642003061700064GL 2003 6 17 CA030605017 320030430A6114B1894 NUT DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE HARTZLHCB3R HCB3R304 GL PROP HUB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PROP REMOVED FOR ENGINE CHANGE, FOUND NUT HOLDING PROP TO CRANKSHALF CRACKED. NUT WAS CRACKED FROM NOTCH FOR INSTALL TOOL TO A HOLE FOR LOCKING CLIP. CRACK WAS NOT INTO THREADS OF NUT. REPLACED NUT WITH NEW PART, PROP THEN REINSTALLED & AIRCRAFT RETURNED TO SERVICE. 1H71 3R3 R A806 5E1 5 CP28EA 20030617000672003061700067NE 2003 6 17 CA030605018 220030403A8520126299 CASE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE MAGNETO PAD CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING MAINTENANCE TO FIND SOURCE OF OIL LEAK ON ENGINE IT WAS FOUND THAT THE REAR ENGINE CASE WAS CRACKED. THE REAR ENGINE CASE WAS CRACKED AT LEFT MAGNETO PAD WHICH HAS ENGINE OIL RUNNING UNDER IT, THIS CAUSED THE OIL LEAK. ENGINE WAS REMOVED AND REAR CASE AND BLOWER ASSY CHANGED WITH OVERHAULED UNIT. ENGINE WAS REINSTALLED GROUND RUN & RETURNED TO SERVICE 1H71 3R3 R A806 5E1 20030617000702003061700070EA 2003 6 17 QXEA200300669 120030520A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA PAX DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - MAIN CABIN DOOR LOWER FORWARD INNER SKIN IS DENTED AND SCRATCHED. REPAIRED IAW CRJ SRM 51-42-13 AND 51-42-06. 2L72 4F RTA21EA 20030617000872003061700087NM 2003 6 17 QXEA200300664 120030530A2120 SMOKE DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09352PH 494 RDM- ON FLIGHT 2055 AT 20,000 FEET, DURING DESCENT UNKNOWN SOURCE OF SMOKE FILLED CABIN AND COCKPIT TO A "HAZE" LEVEL WITH ASSOCIATED BURINING SMELL OF POSSIBLY OIL. THIS DECREASED AS THE FLIGHT CONTINUED. INSPECTED BOTH ENGINE OIL LEVELS. GROUND RAN EACH ENGINE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617001502003061700150NM 2003 6 17 QXEA200300707 120030610A5551 FITTING BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB SCORED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - LEFT HAND MIDDLE FITTING FOR HORIZONTAL STAB MOUNT IS SCORED. REPAIRED IAW RD 8/4-55-92, PAGE 6, STEP4. 2H72 4T RTA13NM 20030617001602003061700160SW 2003 6 17 HEEA087300 120030611A6300407010206103 BEARING BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH4449 53393 MAIN ROTOR DRIVE HAS A BEARING WORN OUT. 1G71 3U O H2SW 20030617001662003061700166SW 2003 6 17 HEEA087467 120030612A282070079H000Y150 HOSE BELL 407 407 1182206SW FUEL SYS KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 INLET FUEL HOSE KINKED. REPLACED HOSE. 1G71 3U O H2SW 20030617001772003061700177NM 2003 6 17 QXEA200300690 120030603A7110 BRACKET BOMBDRDHC8 DHC8401 1390041NM LT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - LEFT LOWER COWL CONE SUPPORT BRACKET UPPER ANGLE CRACKED AT FORWARD THREE RIVETS. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030617001812003061700181NM 2003 6 17 QXEA200300588 120030508A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - SHIMS BETWEEN FORWARD LEFT HAND H-STAB TO V-STAB ATTACH POINTS ARE EXTRUDING. REPAIRED IAW HORIZON AIR EA 6-55-31. 2H72 4T RTA13NM 20030617001842003061700184NM 2003 6 17 QXEA200300591 120030430A7110 CHANNEL BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - NR 1 ENGINE LOWER COWL V-CHANNEL IS CRACKED. FABRICATED AND INSTALLED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030617001982003061700198EU 2003 6 17 ERAA087107 120030521A2842VT044 TRANSMITTER BOLKMS105 BO105A EU FUEL QUANTITY ERRATIC E ERAAO OTHER N FALSE WARNING NRNOT REPORTED 1 FS01135EH S675 FUEL PROBE HAS ERRATIC INDICATION. REPLACED CASE ASSEMBLY AND TESTED. 1G72 3U H3EU 20030617002272003061700227EA 2003 6 17 QXEA200300701 120030521A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 CKB - TOP EDGE OF AFT BAGGAGE DOOR SKIN IS CHAFED AT APPROXIMATELY FS 1029.00. REPAIRED IAW HORIZON AIR EA R-52-97 AND REO 670-52-31-003. 2L72 4F RTA21EA 20030617002302003061700230GL 2003 6 17 HEEA087458 220030612A72616892846 LINE BELL 407 407 1182206SW ALLSN 250C 250C* GL NR 1 BEARING CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 NR 1 BEARING PRESSURE LINE RUSTED AND CRACKED. REPLACED TUBE ASSY. 1G71 3U3 UO H2SW E4CE 20030617002412003061700241NM 2003 6 17 QXEA200300660 120030528A32607002537 CONTROL BOX DHAV DHC8 DHC8202 2809007NM E/E BAY MALFUNCTIONED A QXEAK NONE N FALSE WARNING CLCLIMB 1 NM09363PH101921795 520 ALW- ON FLIGHT 2045 PRIMARY NOSE GEAR INDICATOR INDICATES NOSE GEAR DOWN AFTER RETRACTION. ALTERNATE INDICATOR INDICATES NORMAL RETRACTION. REMOVED AND REPLACED ADVISORY CONTROL BOX. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617002452003061700245EU 2003 6 17 BAQA086756 120030529A6330L633M2010103 MOUNT UROCOPEC135 EC135P1 8680990EU GEARBOX LEAKING H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01577LF53 0140 PLUNGER IN ALL THE WAY. FLUID LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030617002502003061700250NM 2003 6 17 QXEA200300586 120030515A5311 FRAME BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - FUSELAGE FRAME LOCATED AT STATION X-30 AND STINGER 7P HAS CHAFING. REPAIRED IAW HORIZON AIR EA 6-53-255. 2H72 4T RTA13NM 20030617002532003061700253NM 2003 6 17 QXEA200300595 120030503A5240 HINGE BOMBDRDHC8 DHC8401 1390041NM SERVICE DOOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT SERVICE DOOR MAIN HINGE ASSEMBLY CHAFED/GOUGED ON BOTTOM EDGE FORWARD OF AFT END. REPAIRED IAW HORIZON AIR EA 6-52-287. 2H72 4T RTA13NM 20030617002592003061700259SW 2003 6 17 HEEA087480 120030612A2432CTJ620E061513 CONNECTOR BELL 407 407 1182206SW BATTERY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 LOCKING TABS WORN AT CONNECTOR. SCRAPPED. 1G71 3U O H2SW 20030617002622003061700262NM 2003 6 17 QXEA200300603 120030430A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - FORWARD SUPPORT FLANGE FOR 262FT IS CHAFED. REPAIRED IAW DHC-8-400 RD 8/4-53-451. 2H72 4T RTA13NM 20030617002752003061700275NM 2003 6 17 QXEA200300609 120030505A5230 FITTING BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT BAG DOOR, LOWER FORWARD GUIDE ROLLER FITTING IS GOUGED. REPAIRED IAW HORIZON AIR EA 6-52-289. 2H72 4T RTA13NM 20030617002812003061700281NM 2003 6 17 QXEA200300676 120030604A2434 GENERATOR BOMBDRDHC8 DHC8401 1390041NM NR 1 ENGINE MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM09539DS 4016 PDX- NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED DURING TAKEOFF ROLL. PERFORMED CHECKLIST AFTER END OF CRITICAL FLIGHT PHASE. GENERATOR RESET AND FUNCTIONED NORMALLY FOR REMAINDER OF FLIGHT. PERFORMED OPERATIONAL CHECK IAW Q400 AMM TASK 24-31-00-710-802. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617002902003061700290WP 2003 6 17 GTIA030340 120030508A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND LEFT AFT LAVATORY STATION 1338 HAS CORROSION AT BRACKET AND SUPPORT FLOOR. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030613001462003061300146NM 2003 6 13 SWAA031227 120030602A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT ROW NR 1. SECURED COVER PER MM. 2L72 4F RTA16WE 20030617000052003061700005NM 2003 6 17 AUS20030472 120030502A5250 SOLENOID BOEING767 767238 1385114NM PWA JT9 JT9D7R4E 52054NE COCKPIT DOOR FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) FLIGHT DECK DOORLOCK SOLENOID FAULTY. 2L72 4F4 FRTA1NM E3NE 20030617000182003061700018WP 2003 6 17 AUS20030482 120030327A6310269A55593 COUPLING HUGHES269 269B 4470502WP LYC O360 HIO360D1A 41514EA ENGINE/XMSN WORN W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS 6862 (AUS) ENGINE TO TRANSMISSION DRIVE LOWER COUPLING WORN. COUPLING HAS A DIFFERENT SERIAL NUMBER TO THE LOGBOOK ENTRY. SUSPECT UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. 1G71 3O3 O 4H12 1E10 20030617000462003061700046EA 2003 6 17 QXEA200300654 120030520A5280 RIB CNDAIRCL600 CL6002C10 1390015EA RT MLG DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - RIGHT MAIN GEAR DOOR LOWER DOOR ASSEMBLY RIB IS CRACKED. REPAIRED IAW MFG EO R-31-04. 2L72 4F RTA21EA 20030617000582003061700058EA 2003 6 17 QXEA200300656 120030520A5311 FRAME CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - RIGHT 1108 FRAME RIVET HOLE ELONGATED BELOW STRINGER 9 AND STRINGER 8. REPAIRED IAW MFG EA R-53-108. 2L72 4F RTA21EA 20030617000812003061700081EA 2003 6 17 AUS20030500 120030424A2710C6CW10311 CONTROL CABLE DHAV DHC6 DHC6200 2802620EA PWA PT6 PT6A20 52043EA HARTZLHCB3T HCB3TN3 GL AILERON FRAYED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AILERON CABLES PNO C6CW1031-1 (2OFF) AND PNO C6CW1032-1 CONTAINED BROKEN STRANDS IN AREA OF WING ROOT FAIRLEADS. 1H72 3T3 TRTA9EA E4EA 6 CP15EA 20030617001032003061700103SW 2003 6 17 HEEA087288 120030611A6710407001523101 IDLER ASSY BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR BINDING E O OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 MAIN ROTOR CONTROL IDLER ASSY BEARINGS BINDING. REPAIRED. 1G71 3U3 UO H2SW E1GL 20030617001272003061700127SW 2003 6 17 HEEA087465 120030612A282070061H000Y114A HOSE BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUEL SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 FUEL HOSE HAS CORROSION AT SLEEVE ON BOTH ENDS. REPLACED HOSE. 1G71 3U3 UO H2SW E1GL 20030617002012003061700201NM 2003 6 17 QXEA200300727 120030611A2120 SMOKE DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09345PH 476 LMT-ON FLIGHT NUMBER 2130, AFTER ENGINE START AND BLEEDS ON, NOTICED HAZE IN COCKPIT AND CABIN. CHECKED NR 1 AND NR 2 ENGINE OIL LEVELS. NO DEFECTS NOTED. QUANTITY GOOD. GROUND RAN NR 1 AND NR 2 ENGINE. NO SMOKE OR OIL SMELL. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617002072003061700207NM 2003 6 17 QXEA200300713 120030601A5512 SKIN BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FORWAD SPAR CAP AND Y605D-26.40. REPAIRED IAW Q400 SRM 51-21-10, PAGE 204-205 AND SRM 51-25-10, PAGE 201-205. 2H72 4T RTA13NM 20030617002932003061700293WP 2003 6 17 GTIA030345 120030507A5544 HINGE BRACKET DOUG DC9 DC982 3022082WP RUDDER CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - VERTICAL STAB RUDDER HINGE CENTER 'V' BRACKET ASSEMBLY HAS CORROSION STATION ZR 97.207. REMOVED VERTICAL STAB RUDDER HINGE CENTER 'V' BRACKET. INSTALLED BRACKET ASSEMBLY. (M) 2L72 4F A6WE 20030617003022003061700302NM 2003 6 17 SWAA031246 120030604A3350AD20131A BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29712SW 27846 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030617003062003061700306NM 2003 6 17 SWAA031262 120030606A335065C27093 LIGHT BOEING737 7373A4 1384585NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030617003202003061700320NM 2003 6 17 SWAA031271 120030605A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 7L. REPAIRED BULKHEAD PER SRM. 2L72 4F RTA16WE 20030617003262003061700326SW 2003 6 17 HEEA087039 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030617003332003061700333SW 2003 6 17 HEEA087044 120030604A6220406312103101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 MAIN ROTOR LINK WORN. 1G71 3U O H2SW 20030617003362003061700336SW 2003 6 17 HEEA087325 120030611A6230 SEAL BELL 407 407 1182206SW M/R MAST ASSY LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03405PH4346 53038 53207 MAST SEAL LEAKING OIL. REPAIRED. 1G71 3U O H2SW 20030618000042003061800004SW 2003 6 18 HEEA087329 120030611A6510 BEARING BELL 407 407 1182206SW T/R DRIVESHAFT SCORED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH A1006 53147 T/R DRIVESHAFT BEARING SURFACE SCORED. REPLACED. 1G71 3U O H2SW 20030520001082003052000108NM 2003 5 20 AALA20030427 120030409A3350 SOCKET BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21343AN 33082 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT LEFT SIDE JUST FORWARD OF AFT SERVICE DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520001212003052000121NM 2003 5 20 USAABB03065 120030427A33508731002511REV15 SIGN BOEING757 757225 1384959NM L3 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU 22198 PHL - FOUND EXIT IDENTIFIER AT L3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030520001272003052000127NM 2003 5 20 KPVA200318 120030406A33506104784 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A KPVAK NONE O OTHER ININSP/MAINT 1 WP13807WP 023 EMERGENCY EXIT EGRESS LIGHT AT RIGHT FORWARD POSITION AND ONE AT THE FORWARD CEILING AISLE LIGHT INOPERATIVE. REMOVED AND REPLACED AFFECTED POWER SUPPLY. OPERATIONAL CHECK OF SYSTEM GOOD. IAW DHC-8 MM 33-51-00, PAGES 201-202. (M) 2H72 4T RTA13NM 20030520001322003052000132CE 2003 5 20 2003F00265 120030329A7160CEETS4266 HOSE LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE NR 1 INLET DAMAGED A CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05273CA 039 251622A THE AIRCRAFT EXPERIENCED A FLAME OUT ON THE NR 1 ENGINE AT FL400. ENGINE RESTARTED AT FL250, THE AIRCRAFT ARRIVED IN PHX WITHOUT FURTHER INCIDENT. ENGINE INSPECTED FOR FOD. NONE FOUND. INSPECTED ENGINE PER CJ610 M/M. FOUND ASPIRATOR HOSE BAD. REPLACED HOSE, TEST FLEW AC, NO PROBLEM FOUND. (M) 2L72 4J4 J A10CE 1E16 20030520001372003052000137NM 2003 5 20 2003F00270 120030120A5412652368723 FRAME BOEING727 727222 1384073NM BULKHEAD CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND NR 2 ENGINE FORWARD BULKHEAD, ENGINE COWL LIP SEAL, CRACKED AT FUSELAGE STATION 1342, 6 O'CLOCK POSITION. INSTALLED NEW COWL SEAL RETAINER, NR 2 ENGINE, STRINGER 6L TO STRINGER 6R. (M) 2L73 4F A3WE 20030520001422003052000142SO 2003 5 20 2003F00272 120030404A2720 ACTUATOR GULSTMGV GULFSTREAMGV3980116SO RUDDER MALFUNCTIONED A UG8AO OTHER O OTHER NRNOT REPORTED 1 GL23920DC 534 UNUSUAL NOISE COMING FROM RUDDER ACTUATOR DURING MANUAL OPERATION. RUDDER QUADRANT BELLCRANK RUBBING ON CABLE GUIDE. SUPPORT MOUNT HOLE TOO BIG FOR PIVOT BUSHING. GULFSTREAM RESEARCHING REASON FOR DEFECT. (M) 2L72 4F RTA12EA 20030520001582003052000158EU 2003 5 20 CA030502005 120030501A6320350A37118322 LOCK SNIAS 350 AS350D 8680803EU LYC LTS101LTS101600A3 41560NE MAIN ROTOR BROKEN W O OTHER J WARNING INDICATION ININSP/MAINT 1 CA (CAN) LOCK FOR BEARING, FOUND BROKEN BY CUSTOMER. UNITS RETURNED FOR METAL CONTAMINATION. ROTOR SHAFT REPAIRED AND BEVEL GEARBOX AND EPICYCLIC OVERHAULED. BEARING PRELOAD IS IMPORTANT DURING REASSEMBLY TO ENSURE LOCK AND THRUST WASHER ARE PROPERLY UNDER LOAD. 1G71 3U3 U H9EU E5NE 20030520001612003052000161GL 2003 5 20 CA030505004 320030425A6140AG34 DRIVE SHAFT MTSBSIMU2 MU2B60 5780460CE HARTZLHCB4T HCB4TN5 GL TACH GENERATOR SHEARED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE PROP INDICATION WAS INTERMITTENT. MAINTENANCE FOUND THE DRIVE SHEARED OFF INSIDE THE TACHOMETER GENERATOR WHERE THE ROLL PIN SECURES THE DRIVE. 1H72 3T RTA10SW 6 CP40EA 20030521000132003052100013WP 2003 5 21 DHL2003801018 120030418A57305769857381 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E LWR PLATING SHOW ELONGATED HOLES AT STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030411, ED3266. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (7075-T6 AL0.063) IAW EODHL 030411, ED 3266. CLEANED, TREATED AND PRIMED INTERNAL SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED DOUBLER WITH NEW FASTENERS IAW EODHL 030411, ED 3266, SRM 51-1-21 PG 1 AND SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030521000192003052100019WP 2003 5 21 DHL2003801054 120030408A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 466.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000212003052100021WP 2003 5 21 DHL2003801062 120030409A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01801DH78807 46033 LT WING- CTR L/E FORMER CRACKED 0.500 INCH AT XFS 372.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030515000182003051500018EA 2003 5 15 SWIA200311939 120030504A7830 PDU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07406SW 7030 ON LANDING THE RIGHT THRUST REVERSER DID NOT DEPLOY, 14TH STAGE POPOUT VALVE WAS IN AND THRUST REVERSER WAS ARMED. MANUALLY RESET THE THRUST REVERSER PDU. OPERATED THE RIGHT THRUST REVERSER SEVERAL TIMES WITH NO FURTHER PROBLEMS. 2L72 4F4 FRTA21EA E15NE 20030515000412003051500041EA 2003 5 15 SWIA200311910 120030303A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA LT & RT WING CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 LEFT AND RIGHT WING FUEL PANELS 610AB, 650AB, 640AB, 640CB, 640DB, 640FB, 540CB, 510AB, 540AB, 540DB, 540FB, 550AB HAVE CORROSION. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-57-21-079 REV NC. PANEL 640FB CORROSION BEYOND LIMITS, 650AB CORROSION BEYOND LIMITS, 510AB MAT'L LOSS NEGLIGABLE, 540CB MAT'L LOSS .004, 540AB MAX MAT'L LOSS .008, 640 DB MAX MAT'L LOSS .018, 550AB MAX MAT'L LOSS .016, 640CB MAX MAT'L LOSS .014, 610AB MAX MAT'L LOSS .006, 640AB MAX MAT' L LOSS .007, 540FB MAX MAT'L LOSS .013. NEW FUEL LIDS FOR 640FB AND 650AB INSTALLED P/N OFF: 601R10. 2L72 4F RTA21EA 20030515000502003051500050WP 2003 5 15 ZW0A0304703 120030507A3350408822101 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13941AS 49925 THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN SEAT ROWS 7 TO 11 AND JUST AFT OF ROW 31, AND THE FIRST CLASS EGRESS LIGHTS WERE DIM. REPLACED THE BATTERIES FOR THE BATTERY PACK FOR BOTH OF THE CEILING LIGHTS, AND CLEANED MOISTURE FROM FLOOR TRACK FOR THE DIM EGRESS LIGHTS. CHECK-C 2-9-03 STL. 2L72 4F A6WE 20030515000682003051500068EA 2003 5 15 SWIA200311922 120030428A27507455001 LEVER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07595SW3112 3112 7292 FLAPS FAIL CAME ON FINAL, 7 MILES OUT. WHEN FLAPS WERE AT 20 DEGREES, SELECTED 30 DEGREES AND FLAPS FAIL MESSAGE ILLUMINATED. INTERROGATED FECU. FECU INDICATED FLAP HANDLE FAILURE. REMOVED AND REPLACED FLAP HANDLE. FLAPS OPS CHECK GOOD. 2L72 4F RTA21EA 20030618000142003061800014SW 2003 6 18 HEEA087330 120030611A6510407040330101 BEARING BELL 407 407 1182206SW T/R DRIVE SHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X4272 A1136 53267 ROUGH BEARINGS. REPLACED SHAFT 407040330101, S/N A2975 DUE TO BEARING JOURNAL GROOVED AND BEARING 407340339101, S/N ZV11198 DUE TO ROUGH. REPAIRED. 1G71 3U O H2SW 20030618000252003061800025 2003 6 18 SWAA031320 420030611A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT CABIN DOORS OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2L72 4F A16WE 20030618000312003061800031NM 2003 6 18 SWAA031325 120030613A33506104789 CHARGER BOEING737 7375H4 138449DNM CARGO BAY INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED RON, FOUND LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER M1135 PER MM. 2L72 4F RTA16WE 20030618000342003061800034NM 2003 6 18 SWAA031328 120030615A261233007505 FIRE LOOP BOEING737 7375H4 138449DNM APU FAULTY A SWAAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW29526SW 26568 DIVERSION, APU FIRE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH FIRE BOTTLES, FIRE LIGHT WENT OUT AND THEN RE-ILLUMINATED. REMOVED AND REPLACED APU LOWER FIRE DETECTOR LOOP AND BOTH FIRE BOTTLES PER MM. 2L72 4F RTA16WE 20030618000392003061800039NM 2003 6 18 SWAA031332 120030614A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM CORRODED AT BS 727, LBL 7. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20030618000402003061800040SW 2003 6 18 HEEA087335 120030611A6510407040302107 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 TAIL ROTOR DRIVESHAFT SPLINE COATING GONE. REPLACED. 1G71 3U O H2SW 20030618000432003061800043NM 2003 6 18 SWAA031335 120030615A3350AD20131A BATTERY BOEING737 7372T4 1384492NM CARGO BAY DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED PM CHECK, FOUND AFT CABIN DOORS EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM. 2L72 4F A16WE 20030515001622003051500162NM 2003 5 15 SWAA031079 120030513A57436545321 FITTING BOEING737 737317 138447PNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND LT MLG FITTING UPPER REAR SPAR D-HOLE CRACKED. REMOVED AND REPLACED LT MLG ATTACK FITTING PER ER, SRM, & BAC DRAWING. 2L72 4F RTA16WE 20030520000102003052000010NM 2003 5 20 CA030423001 120030318A792187900014103 FITTING LORINORDAM DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE HAMSTD14SF 14SF7 NE OIL COOLER BROKEN W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DURING FLIGHT LOW OIL PRESURE WARNING LIGHT CAME ON, PILOT INITIATED THE ENGINE SHUT DOWN PROCEDURE AND DIVERTED FLIGHT TO YQB. AFTER INVESTIGATION WE FOUND THAT THE FITTING WAS BROKEN AT OUTBOARD FLANGE WHAT CAUSED THE OIL LEAK. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030520000672003052000067WP 2003 5 20 GTIA030270 120030422A3260 PROXIMITY SENSOR DOUG DC9 DC981 3022081WP LT MLG FAILED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23806NK 48051 RED LIGHT REMAINED ON IN LEFT MAIN GEAR AFTER RAISING HANDLE. RECYCLED GEAR ALL INDICATIONS NORMAL. RAISED GEAR AND LEFT MAIN RED LIGHT ON AGAIN. NO VIBRATIONS RUMBLINGS OR WARNINGS ABOVE 300 KIAS. LEFT ALL HYDRAULIC PUMPS ON HIGH AS A PRECAUTION AND CONTINUED FLIGHT. GEAR INDICATIONS NORMAL WITH GEAR DOWN. TROUBLESHOT AND FOUND LEFT MAIN GEAR UPLOCK SENSOR D1-26 AT FAULT. REMOVED AND REPLACED D1-26 PROX SENSOR AS PER MM 32-60-05. OPS NORMAL ON GORND AS PER MM 32-60-05. (M) 2L72 4F A6WE 20030520000692003052000069SO 2003 5 20 SIMA200309610 120030328A524014521725615 DOUBLER EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 THIS IS A LEVEL TWO FINDING FOUND DURING A MBV INSPECTION, SERVICE DOOR CENTER SILL CORRODED. INSTALLED SERVICEABLE DOUBLER IAW ETN NR EM-53-036R1. (M) 2L72 4F RTT00011AT 20030520000732003052000073WP 2003 5 20 GTIA030253 120030410A5270833703 SENSOR DOUG DC9 DC983 3022083WP MLG DOOR MALFUNCTIONED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 GEAR DOOR LIGHT CAME ON AT ALTITUDE OUT WHEN DESCENT STARTED. INSTALLED SERVICABLE GEAR DOOR SENSOR. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20030520000892003052000089EU 2003 5 20 USAABA03009 120030422A4920 APU AIRBUS330 A330323 3930335EU APU BAY MALFUNCTIONED A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19671UW 0323 AT APPROXIMATELY 55N, 020 W, THE LEFT IDG FAULTED AND WOULD NOT RESET. THE CREW ALSO COULD NOT GET THE APU START. THE FLIGHT DIVERTED TO LGW. EN ROUTE TO LGW, THE APU WAS STARTED. FLIGHT LANDED AT LGW WITH NO FURTHER INCIDENT. MAINTENANCE SWAPPED THE APU AND LEFT IDG GCU'S. AN ENGINE RUN WAS PERFORMED AND THE LEFT GENERATOR OPERATED NORMALLY, AS DID THE APU GENERATOR. THE FLIGHT DEPARTED LGW WITH THE APU RUNNING. EN ROUTE, THE LEFT IDG FAULTED AGAIN. THE FLIGHT CONTINUED AND LANDED IN PHL WITHOUT FURTHER INCIDENT. (M) 2L72 4F RTA46NM 20030520000972003052000097NM 2003 5 20 USAABB03063 120030427A33509221009 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU 22198 PHL - FOUND EXIT IDENTIFIERS AT L4 AND R4 DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M) 2L72 4F RTA2NM 20030520001262003052000126WP 2003 5 20 GTIA030269 120030408A5320 WEB DOUG DC9 DC983 3022083WP SUBFLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 FTW - FOUND CORROSION AT E/E CABIN SUBFLOOR FS 207, 24 INCHES RBL. CUT OUT WEB. FABRICATED 1 REPAIR DOUBLER. FABRICATED 1 FILLER. INSTALLED 1 DOUBLER REPAIR AND FILLER IN WEB. (M) 2L72 4F RTA6WE 20030605001492003060500149WP 2003 6 5 DHL2003801049 120030409A5280 FRAME DOUG DC8 DC873F 302199FWP NLG DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 NLG W/W DOOR FORMER CRACKED 1.000 STA 93.000 (LT). REMOVED FORMER CRACKED IAW SRM 51-1-21 PG 1. FABRICATED FORMER (2024-T3 AL0.063) IAW SRM 52-5-1 PG 1-4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FORMER ON NLG W/W DOOR STA 93.000 IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030606000112003060600011NM 2003 6 6 CW12003F00000 120030501A3020F2MA724602300A2 LINE AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE NACELLE ANTI ICECRACKED B CW1RO OTHER O OTHER NRNOT REPORTED 1 EA11790M 4894 19 WHILE PERFORMING A ROUTINE ENGINE INSPECTION A BLEED AIR TAP FOR NACELLE ANTI-ICE PRESSURE SWITCHES WAS FOUND TO BE CRACKED AT THE WELD LOCATION. PROBABLE CAUSE WAS VIBRATION. THIS COULD BE PREVENTED BY INSTALLING SUPPORT BRACKET AND NOTING SPECIFIC AREA FOR INSPECTION DURING INSPECTIONS. 2K73 4F4 FRTA50NM E44NE 20030604000622003060400062WP 2003 6 4 UPS03840477 120030413A5320577384444 BRACKET DOUG DC8 DC873F 302199FWP CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, RT LONGERON 6R FWD OF PRESSURE BULKHEAD AT STA 1766 BRACKET IS BROKEN REMOVED,FABRICATED AND REPLACED BRACKET I.A.W. DWG.5773844 AND SRM. 51-1-20D 2L74 4F RT4A25 20030604001132003060400113NM 2003 6 4 UPS03440528 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 1680 FRAME CRACK AT STR 13L I/B AREA. FRAME REPLACED AS PER SRM 51-10-01 PAGE 8 AT CABIN STA 1680 BTN STR 12L AND STR 16L. 2L74 4F A20WE 20030604001152003060400115NM 2003 6 4 UPS03440530 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 560 LT STR 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030604001292003060400129NM 2003 6 4 UPS03440544 120030412A5321 WEB BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FLOOR WEB AT BS 520 RBL 83 FOUND CORROSION. WEB REPAIRED AS PER RS NR : R52-25-35007 AND ENGINEERING FILE NUMBER 747-53-20130. 2L74 4F A20WE 20030605000102003060500010SO 2003 6 5 AUS20030435 120030424A55114012202 SPAR PIPER PA31 PA31325 7103105SO LYC O540 TIO540F2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT TAILPLANE OUTBOARD SPAR CRACKED AT HINGE POINT. FOUND DURING INSPECTION IAW AD. 1L72 3O3 O A20SO E14EA 5 CP33EA 20030605000162003060500016NM 2003 6 5 UPS03240644 120030411A3210 ATTACH FITTING BOEING727 72722C 138400FNM LT MLG SWIVEL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C/SI, LT MLG SWIVEL VALVE LINK ARM ATTACH BRACKET CRACKED AT UPPER ATTACH POINT. BRACKET REPLACED IAW SRM 51-20-1 2L73 4F A3WE 20030605001432003060500143EA 2003 6 5 SWIA200311969 120030510A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07920SW 7660 EMERGENCY LIGHT, FORWARD - CENTER - CEILING, IS INOP. REMOVED AND REPLACED FORWARD - CENTER - CEILING EMERGENCY LAMP IAW CRJ MM 33-51-16. OPS CHECK GOOD. 2L72 4F RTA21EA 20030605001672003060500167NM 2003 6 5 UPS03440695 120030516A3350 FUSE BOEING747 747200 1384847NM EMERGENCY LIGHT BLOWN A IPXAO OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SO01520UP 1 INSPECTION TYPE: AS-E, EMERGENCY LIGHT FIXTURE L1854 IN L1 DOOR SILL INOPERATIVE. RELAMP NO HELP. REPLACED FUSE IN EMERGENCY LIGHT ASSY AND OPS CHECKED NORMAL IAW MM33-51 -07. 2L74 4F RTA20WE 20030606000252003060600025NM 2003 6 6 03FDEA00736 120030508A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP I/B HINGE (AIRCRAFT SIDE), ACTUATOR I/B AND O/B LUG HOLES CORRODED. TRAILING EDGE & TRAILING EDGE DEVICES- LH OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030606000262003060600026NM 2003 6 6 03FDEA00735 120030518A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING OUTBOARD FLAP INBOARD HINGE (AIRCRAFT SIDE) ACTUATOR INBOARD AND OUTBOARD LUG HOLES CORRODED AREA REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69233 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030606000292003060600029NM 2003 6 6 03FDEA00731 120030514A5320 CHANNEL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 LT WHEEL WELL HAS CORROSION AT STRINGER 18A CHANNEL BS 939 & 912 UPR SURFACE. REMOVED AND REPLACED SILL CHANNEL BS 870-940, LBL 65, WL 190 AT STR 18A PER SRM 51- 30-5, 51-30-2. 2L73 4F RTA3WE 20030606000322003060600032WP 2003 6 6 03FDEA00733 120030515A5753 HINGE DOUG DC10 DC1010 3022110WP RT WING TE FLAP INOPERATIVE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 46613 COMPLY WITH E.A. 8-5740-70384 WINGS- RT OUTBD FLAP, INBD HINGE ASSY P/N ARC1984. FACT 13MAY03 22:27 BFM R COMPLIED WITH E.A.# 8-5740-70384. 2L73 4F A22WE 20030606000382003060600038CE 2003 6 6 DXTA200300033 120030513A2120 ODOR CESSNA560 560XL 2076702CE CABIN DETECTED E DXTAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07699QS 5605199 WHILE ENROUTE AT FL280 NOTICED STRONG ODOR IN COCKPIT + CABIN. PIC + SIC DEVELOPED HEADACHE + BURNING EYES. USED O2. ONCE AT 3000' , SELECTED OFF ON PRESSURIZATION SOURCE. ODOR DIMINISHED. ITEM IS UNDER INVESTIGATION 2L72 4F RTA22CE 20030521000272003052100027WP 2003 5 21 DHL2003804889 120030209A57405769589504 FITTING DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING CTR L/E UPPER PART CORRODED, STA XW 257.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030106, ED-3212. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON RT WING CTR L/E UPPER PART IAW SRM 51-1-8B PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16, FABRICATED A REPAIR DOUBLER (7075-T6AL-0.071) AND FILLER (7075-T6AL-0.063) IAW EODHL030106, ED3212. CLEANED TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER AT RT WING CTR L/E UPPER PART (STA XW 257.000) WITH NEW FASTENERS IAW EODHL 030106, ED-3212 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000362003052100036WP 2003 5 21 MWEA030191 120030429A339739564823 WIRE DOUG DC9 DC914 3022034WP COCKPIT LIGHT ARCED A MWEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31700ME 45696 A BURNING ODOR WAS NOTICED IN THE COCKPIT AND SMOKE WAS OBSERVED COMING OUT OF THE FIRST OFFICERS MAP LIGHT AREA. FOUND GROUND WIRE TO RHEOSTAT BROKEN CAUSING WIRE TO ARC. REMOVED AND REPLACED FIRST OFFICER'S LIGHT ASSEMBLY. 2L72 4F A6WE 20030521000552003052100055EU 2003 5 21 DHL2003368005 120030519A3230 RELAY AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01368DH 207 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REFERRED TO LANDING GEAR HANDLE CANNOT BE RAISED ABNORMAL PROCEDURE, AND SELECTED SYSTEM 1 ON THE LEVER LOCK & WARNING SYSTEM. GEAR RETRACTED NORMALLY. REMOVED AND REPLACED PROXIMITY DETECTION BOX AND RELAY 14GB IAW M/M 32-61-12 & ESPM. 2L72 4F RTA35EU 20030521000632003052100063WP 2003 5 21 DHL2003801013 120030418A57535642960507 SKIN DOUG DC8 DC873F 302199FWP LT WING TE FLAP CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING INBOARD FLAP UPPER SKIN CORRODED STA XW 2.000 TO XW 91.000 LT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030407, ED 3263, REMOVED CORROSION IAW SRM 51-1-8 PAGES 17, 18 FOUND OUT OF LIMITS IAW SRM 57-2-0 PAGE 16. REMOVED CORRODED SKIN IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN (2024-T3 0.050) IAW EO DHL 030407 ED 3236, CLEANED TREATED AND PRIMED NEW SKIN INNER PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON SPLICE SURFACE IAW 51-1-15 PAGE 1. INSTALLED NEW SKIN WITH NEW FASTENERS IAW EO DHL 030407 ED 3263 SRM 51-1-21 PAGE 1, SRM 51-1-15 PAGE 1. 2L74 4F RT4A25 20030521000682003052100068EU 2003 5 21 MALA030247 120030414A5280 DOOR BAC 146 AVRO146RJ85A1500097EU LT MLG TORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15505XJ E2313 AIRCRAFT TO BE FERRIED FROM MSP TO CVG FOR REPAIRS TO THE ABOVE MENTIONED DAMAGES (LT MLG DOOR UPPER PANEL TORN AT UPPER AFT EDGE). NR 4 ENGINE LT AND RT ATTENUATED PANELS 7 SCREWS PULLED THROUGH AND FWD CARGO BAY FWD LT AND RT BULKHEADS DAMAGED A42BR AND 141BL. MAINTENANCE COMPLIED WITH ALL DISCREPANCIES. 2H74 4F RTA49EU 20030521000852003052100085WP 2003 5 21 MWEA03207 120030509A7120 COVER DOUG DC9 DC981 3022081WP ENGINE ISOLATOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 RIGHT LOWER FORWARD ENGINE ISOLATOR COVER HAS LITE CORROSION ON MATING SURFACE. BLENDED CORROSION, INSTALLED NEW PLATE. 2L72 4F A6WE 20030521000922003052100092WP 2003 5 21 DHL2003801033 120030415A5311 FRAME DOUG DC8 DC873F 302199FWP TAIL CONE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 TAIL CONE LT FRAME WITH 2.000 CRACK IN STA 1937.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA 1937.000 IAW SRM 53-2-0 PG 1B. FABRICATED DOUBLER (2024-T3 AL 0.040) IAW SRM 53-2-0 PG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000972003052100097WP 2003 5 21 DHL2003801036 120030410A5751 SKIN DOUG DC8 DC873F 302199FWP LT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT OUTBOARD AILERON NOSE PLATING WITH TWO CRACKS OF 1.000 AND 0.500 INCH BETWEEN STA XA 674.000 AND 752.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-8-1 PG 9 FIG 4. REMOVED DAMAGED NOSE PLATING SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-T3 0.032) IAW SRM 57-8-1 PG 9 FIG 4. CLEANED, TREATED AND PRIMED NEW SKIN INNER SIDE PG 9 FIG 4 AND SRM 51-1-21 PG 1. REFER TO N/R 2058 FOR REBALANCING. 2L74 4F RT4A25 20030521001012003052100101NM 2003 5 21 HNAA0300023 120030512A33506104791X POWER SUPPLY DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT INOPERATIVE A HNAAO OTHER O OTHER NRNOT REPORTED 1 EA07966HA9286 452 CREW REPORTED THAT THE CENTER OVERHEAD EMERGENCY EXIT SIGN, THE CENTER AFT EMERGENCY CEILING LIGHT AND THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WERE INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY PS4. 2H72 4T RTA13NM 20030521001052003052100105WP 2003 5 21 DHL2003801024 120030421A573057696003 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT OUTER WING INBOARD L/E OUTER PLATING CORRODED AT STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030402, ED3253. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT DAMAGED AREA IAW EODHL 030402, ED 3253. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063), A FILLER (7075-T6 AL 0.050) IAW EODHL-030402, ED3253. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER ON LT OUTER WING INBOARD L/E OUTER PLATING WITH NEW FASTENERS IAW EODHL-030402, ED3253 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001062003052100106WP 2003 5 21 DHL2003801069 120030424A53404641324N FITTING DOUG DC8 DC873F 302199FWP ACCESSORY BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 AFT ACCY COMPT - SPLICE FITTING CRACKED 1.000 INCH FS 1690.000 L-18L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED DAMAGED SPLICE FITTING SRM 51-1-21 PG 1. CLEAN, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521001182003052100118WP 2003 5 21 MWEA030213 120030516A523059101419 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FORWARD CARGO COMPARTMENT DOOR INNER PAN HAS APPROXIMATELY A 2 INCH CRACK LOCATED OUTBOARD OF THE TORQUE TUBE CAM HOOK AFT SIDE OF DOOR. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030521001222003052100122NM 2003 5 21 DHL2003751009 120030506A2697 WIRE BOEING727 727264 138408MNM FIRE LOOP BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01751DH 22982 NR 1 ENGINE FIRE LOOP AT FORWARD END HAS 1 WIRE BROKEN OFF. REMOVED AND REPLACED FIRE LOOP CONNECTOR ASSEMBLY, P/N 878581-01, PER BSWP MAN 20-62-16. FIRE TEST NORMAL PER B727 M/M 26-11-00. 2L73 4F A3WE 20030521001432003052100143EU 2003 5 21 MALA030259 120030502A5511 SPAR SAAB SF340 340B 7860101EU HORIZONTAL STAB DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING C1 INSPECTION IN CWA, LT HORIZONTAL STABILIZER UPPER FWD SPAR CUP FWD WEB WAS DAMAGED. MAINTENANCE COMPLETED REPAIR IAW EO 55034. 2L72 4T RTA52EU 20030521001492003052100149WP 2003 5 21 MWEA030195 120030501A53479957871515 SEAT TRACK DOUG DC9 DC981 3022081WP COCKPIT DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 CAPTAIN'S AFT SEAT TRACKS HOLES ARE ENLONGATED. DRILLED UP, INSTALLED REPAIR. 2L72 4F A6WE 20030521001612003052100161NM 2003 5 21 SWAA031081 120030513A551165C25727 SKIN BOEING737 7372H4 138448CNM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED C3 CHECK, FOUND LT HORIZ STAB SKIN CRACKED (11 EA) ON LOWER SURFACE RADIATING FWD OUT OF FWD RIVET ROW. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030521001622003052100162NM 2003 5 21 SWAA031082 120030513A551165C25727 SKIN BOEING737 7372H4 138448CNM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED C3 CHECK, FOUND RT HORIZ STAB SKIN CRACKED (3 EA) ON LOWER SURFACE RADIATING FWD OUT OF FWD RIVET ROW. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030521001632003052100163NM 2003 5 21 SWAA031083 120030513A575465C26686 SKIN BOEING737 7373Q8 1384670NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED 1/4D CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED ON LOWER SKIN AROUND ACTUATOR CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030521001742003052100174WP 2003 5 21 DHL2003604508 120030429A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING INBOARD L/E FORMER CRACKED 0.500 INCH, STA XFS 622.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20 PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030520000312003052000031SO 2003 5 20 SIMA200309606 120030325A532014521725015 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21804AE 145487 THIS IS LEVEL TWO FINDING FOUND DURING A MBV INSPECTION, THE SERVICE DOOR AFT SILL WAS FOUND CORRODED. REMOVED AND INSTALLED NEW SERVICE DOOR SILL IAW EMB 140 SRM 51-40-02, 51-20-03 AND 51-40-06. (M) 2L72 4F RTT00011AT 20030520000382003052000038NM 2003 5 20 AMTA200300565 120030425A3350 WIRE BOEING757 75733N 1384931NM EMERGENCY LIGHT DIRTY A AMTAK NONE O OTHER ININSP/MAINT 1 GL11557TZ 32591 R4 EMERGENCY LIGHT INOPERATIVE. CLEAN WIRE TERMINAL AS REQUIRED. (M) 2L72 4F RTA2NM 20030520000952003052000095NM 2003 5 20 WRLA200307 120030408A32604305990040 TRANSMITTER DOUG MD11 MD11 3023602NM NR 2 WHEEL FAILED A WRLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27277WA 48743 ABORTED TAKEOFF AT 80 KNOTS DUE TO TIRE PRESSURE ANNUNCIATION ON TIRE NR 2. INTERROGATED BTMTP NO CURRENT FAULTS SHOWN. FAULT HISTOR SHOWS NR 2 TIRE FAILURE. INSPECTED NR 2 MWA AND NR 2 MWA TIRE PRESSURE, BOTH NORMAL AND WITHIN LIMITS. PLACED TIRE PRESSURE INDICATION ON MEL 32-46-1-2 DMI M32AP08-16 INSTALLED PLACARD CAT C ITEM ENTERED IN DMI LOG BTM/TPI SYSTEM CIRCUIT BREAKER PULLED AND COLLARED PER MEL. REPLACED TIRE PRESSURE TRANSMITTER. (M) 2L73 4F RTA22WE 20030520001062003052000106NM 2003 5 20 AALA20030422 120030405A7830 WARNING LIGHT BOEING757 757223 1384957NM LT REVERSER ILLUMINATED A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW21690AA 25696 HNL - ON CLIMB-OUT, LEFT ENGIE REVERSE AMBER LOCK LIGHT. LEFT REVERSER PLACARDED INOPERATIVE PER MEL. ENTERED IN MIC MPM 78-01 COMPLIED WITH. REINSTALLED NUT PLUS WASHER FOR MECHANICAL LINKAGE COMMON TO OUTBOARD PROXIMITY SWITCH. OPS CHECK GOOD CLEARED MIC SHEET PLUS MEL. (M) 2L72 4F RTA2NM 20030520001152003052000115NM 2003 5 20 AALA20030403 120030403A3397 CONNECTOR BOEING777 777223 1385213NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21762AN 31479 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SEAT 3D INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT CONNECTOR ON SEAT 3D. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030520001512003052000151NM 2003 5 20 2003F00279 120030120A5347 SEAT TRACK BOEING727 727222 1384073NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND SEAT TRACK CORRODED AT STATION 1110 TO 1120, RBL 45. REMOVED CORROSION ON SEAT TRACK FLANGE. MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK. TREATED AND PRIMED. (M) 2L73 4F A3WE 20030521000142003052100014WP 2003 5 21 DHL2003801023 120030418A5730576954589 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT OUTER WING OUTBOARD L/E OUTER PLATING CORRODED AT STA XFS 710.000. PERFORMED MAJOR REPAIR IAW EODHL 030401, ED3255. REMOVED CORROSION ON LT WING OUTBOARD L/E STA XFS 710.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT CORRORED AREA IAW EODHL 030401, ED3255. FABRICATED FILLER (7075-T6 0.050) AND DOUBLER (7075-T6 0.063) IAW EODHL 030401, ED3255. CLEANED, TREATED AND PRIMED INNER SIDE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL 030401, ED3255, SRM 51-1-21 PG 1 SRM 51-1-20D PG 9 AND SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030521000812003052100081WP 2003 5 21 DHL2003801021 120030418A57545769933184 VANE DOUG DC8 DC873F 302199FWP LT WING LE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING L/E OUTBOARD VANE UPPER SKIN SHOWS ELONGATED HOLES AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030408, ED-3264. CUT OUT DAMAGED AREA IAW ED DHL 030408, ED-3264. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED FILLER (7075-T6 0.063) AND INNER DOUBLER (7075-T6 0.050) AND OUTER DOUBLER (7075 T-6 0.071) IAW EO DHL 030408, ED 3264. CLEANED, TREATED AND PRIMED INNER SIDE OF FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1 AND INSTALLED FILLER AND DOUBLERS IAW EO DHL 030408, ED-3264, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030521000942003052100094WP 2003 5 21 DHL2003801032 120030409A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E FORMER WITH 2.000 INCH CRACK AT STA XOLDI 6.225. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED 2.000 CRACK ON LT WING CTR L/E IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE (STEEL-301 0.25H-0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE USING NEW FASTENERS IAW SRM 51-1-21M PG 1. 2L74 4F RT4A25 20030521001302003052100130NM 2003 5 21 DHL2003726003 120030514A2612 CONNECTOR BOEING727 727228 1384083NM FIRE LOOP DIRTY A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01726DH 20409 ENGINE SYSTEM-B FIRE DETECTION LIGHT ILLUMINATED. SWITCHED TO SYSTEM-A FIRE DETECTION LIGHT TESTED NORMALLY. CLEANED NR 3 FIRE LOOP CONNECTOR AND RESET B-SYSTEM TEST BUTTON OPS CHECKED NORMAL IAW 727 M/M 26-11-0. 2L73 4F RTA3WE 20030521001792003052100179WP 2003 5 21 DHL2003801074 120030509A3230 LANDING GEAR DOUG DC8 DC873F 302199FWP HUNG UP A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 WHEN SELECTING EMERGENCY, LT GEAR HANGS UP FOR 3 SECONDS AND DOES NOT RELEASE PROPERLY. PERFORMED ADJUSTMENT AND TEST OF LT MLG MECH CONTROL SYSTEM IAW MM 32-31-0 PG 201. OPS CHECKED LANDING GEAR IN NORMAL AND EMERGENCY GOOD IAW MM 32-30-0 PG 201. 2L74 4F RT4A25 20030521001912003052100191EU 2003 5 21 AWXA200300542 120030429A5320D5391379020002 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 28, RBL 11. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT FR 28, RBL 11; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 51-44-21, TABLE 3, PG 5. 2L72 4F RTA28NM 20030609000962003060900096EU 2003 6 9 AWXA200300577 120030428A5320D53230256201 ANGLE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK A 3 INCH CRACK WAS FOUND ON ATTACH ANGLE AT FR 34 ON SUPPORT STRUCTURE AT AFT UPPER EDGE OF PANEL 191AB. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT FR 34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW AWA E.R. 26-5323-03128-TB1. 2L72 4F RTA28NM 20030609001102003060900110WP 2003 6 9 IXXA0300036 120030521A7797 CONNECTOR DOUG DC8 DC873F 302199FWP NR 4 ENG EGT LOOSE A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW11606AL460441646 46044 DURING CRUISE FROM TOL ENROUTE TO DFW NR 4 EGT ROSE ABNORMALLY, THEN DROPPED TO "0". AS A PRECAUTIONARY MEASURE FLIGHT CREW ELECTED TO SHUTDOWN NR 4 ENGINE. AN UNEVENTFUL LANDING WAS MADE IN DFW. UPON INSPECTION MAINTENANCE DISCOVERED LOOSE CONNECTOR ON HARNESS. THIS WAS SECURED AND SYSTEM OPERATIONALLY CHECKED GOOD. ALL WORK COMPLETED PER APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030609001232003060900123WP 2003 6 9 ABXA030152 120030517A5420591326238 ATTACH ANGLE DOUG DC9 DC932 3022066WP NR 2 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23984AX 47258 THE RIGHT LOWER PYLON ATTACH ANGLE WAS FOUND CRACKED WHILE PERFORMING AN INSPECTION OF THE NR 2 PYLON FOR AN ENGINE CHANGE. REPAIRED ATTACH ANGLE IAW DC-9 SRM 54-04, FIG 10. 2L72 4F A6WE 20030609002042003060900204 2003 6 9 HEEA086577 420030522A3442MI585200 TRANSCEIVER SKRSKYS76 S76A 8143006NE WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 NO DISPLAY MAP AND WEATHER MODE. SHOP REPAIR. 1G72 3U H1NE 20030609002052003060900205EU 2003 6 9 HEEA086719 120030521A243651565000R VOLT REGULATOR BOLKMS105 BO105S 5626006EU FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 VOLT REGULATOR PRODUCING OVERVOLTAGE NO REGULATION. 1G72 3U H3EU 20030610000032003061000003 2003 6 10 HEEA086722 420030521A23129210121 TRANSCEIVER AEROSPAS355 AS355* EU VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 VHF TRANSCEIVER DOES NOT TRANSMIT. 1G72 3U H11EU 20030610000132003061000013EU 2003 6 10 03123327 120030523A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27327UE 41080 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT ON HALF OF THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030610000152003061000015EU 2003 6 10 03143328 120030523A33501317 LAMP JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27328UE 41083 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS ON THE FORWARD BULKHEAD HAD LAMPS THAT WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE INOPERATIVE LAMPS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030610000232003061000023NM 2003 6 10 DHL2003781004 120030523A33501000677 LIGHT BOEING727 727227 1384078NM COCKPIT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01768AT 21996 COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY IAW B-727 M/M 33-50-101. OPS CHECKED GOOD. 2L73 4F A3WE 20030610000252003061000025NM 2003 6 10 DHL2003720006 120030524A3220 LANDING GEAR BOEING727 727228 1384083NM NOSE LACK OF LUBE A DHLAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01720DH 19544 AFTER LOWERING LANDING GEAR HANDLE NOSE GEAR RED LIGHT STAYED ON. WENT AROUND. NEXT TIME GEAR CAME DOWN NORMALLY. INSPECTED AND LUBED NOSE GEAR AND PERFORMED TEST IAW 727 M/M CHAPTER 32-33-0 CYCLED NOSE GEAR SEVERAL TIMES. NO FAULTS FOUND. 2L73 4F RTA3WE 20030610000262003061000026EA 2003 6 10 QXEA0300649 120030525A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX3134 1921 10033 MAINTENANCE DISCOVERED A BROKEN WELD ON THE FORWARD CARGO BAY SMOKE DETECTOR AND REPLACED THE SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030610000342003061000034EA 2003 6 10 03144683 120030524A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27683BR 7692 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030610000362003061000036SO 2003 6 10 C2XA03CL103 120030524A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711565 145621 CLE FLIGHT 2104 THE CREW REPORTED THE FIRST SECTION OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030610000382003061000038NM 2003 6 10 P5CA0300879 120030522A5330 SKIN BOEING747 74746NF 13848BTNM FUSELAGE GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23451PA 30809 AFT FUSELAGE SKIN AT STA 2392 THRU 2394 DEEP GOUGE. CUT OUT DAMAGE, FABRICATED & INSTALLED REPAIR DOUBLER & FILLER AS PER SRM 53-00-01 FIF 201. 2L74 4F RTA20WE 20030610000572003061000057WP 2003 6 10 MWEA030233 120030525A3150S1141 SWITCH DOUG DC9 DC9 3022002WP COCKPIT DIRTY A MWEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL31206ME 47791 RECEIVED TAKEOFF WARNING HORN WHILE ADVANCING THROTTLES. -- CLEANED STICKY SWITCH. 2L72 4F A6WE 20030521001972003052100197 2003 5 21 SWAA031060 420030512A2565D31354 SLIDE BOEING737 7373G7 1384595NM AFT CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH AFT CABIN DOOR SLIDES PER MM. 2L72 4F RTA16WE 20030521002012003052100201NM 2003 5 21 SWAA031064 120030509A57536546435278 SKIN BOEING737 737317 138447PNM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C4 CHECK, FOUND RIGHT OUTBOARD AFT T/E FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED RIGHT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030522000042003052200004NM 2003 5 22 0300956632 120030502A5414 SKIN BOEING747 747251B 1384892NM PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 23112 DURING H-CHECK FOUND CRACK IN NR 3 PYLON INBOARD SKIN AT CUTOUT OF SLOT SEAL AT NACELLE STATION 178. REPAIRED PER EA 66-164978. 2L74 4F A20WE 20030522000072003052200007NM 2003 5 22 GTIA030282 120030426A4990 OIL SYSTEM DOUG MD80 MD83 3023681NM APU OVERSERVICED A GTIAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 GL23828NK 49823 DIVERTED TO MYR, CRUISE FLIGHT, APU OIL TEMP HIGH ILLUMINATED. FOLLOWED QRH PROCEDURES AND CONSULTED WITH DISPATCH/ DIVERTED TO MYR. FOUND APU OIL OVERSERVICED, DRAINED OIL FROM TANK TO FULL MARK. STARTED APU AND NO FURTHER DEFECTS NOTED. LOADED APU WITH ELECTRICAL AND AIR. 2L72 4F RT 20030522000142003052200014SO 2003 5 22 C2XA03TY064 120030517A531514525480003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR LOWER BEAM IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000222003052200022NM 2003 5 22 2003UALA00414 120030505A5230 ANGLE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE DOOR ACCESS BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29810UA 843 ANGLE SUPPORTS ARE BENT UNDER THE LOWER ACCESS PANEL ON AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SUPPORT ANGLES. 2L72 4F4 FRTA28NM E40NE 20030522000342003052200034WP 2003 5 22 GTIA030287 120030420A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 FLOORBOARD (CABIN) AT STA 826-886 (CENTER) FWD LT CORNER BROKEN. REMOVED DAMAGED CORRECTED ON FLOORBOARD. FABRICATED NEW COVER. INSTALLED NEW COVER. 2L72 4F4 FRTA6WE E2EA 20030522000572003052200057SO 2003 5 22 C2XA03TY069 120030517A532014522459003 SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 TYS, DURING A SCHEDULED INSPECTION THE LEFT HAND GALLEY RAMP SUPPORT FLOOR WAS CRACKED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT IAW EMB-135/145 CPM-51-21-04/05. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000692003052200069SO 2003 5 22 C2XA03TY054 120030517A531514522226003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 TYS, DURING A SCHEDULED INSPECTION SURFACE OXIDATION WAS FOUND AROUND FASTENERS ON LAV FLOOR CENTER BEAM. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM TOP CAP IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000732003052200073SO 2003 5 22 14952 120030518A532014525991003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV DURING C-CHECK LEFT HAND LOWER LINING CARGO SUPPORT AT FRAME 61 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030522000792003052200079SO 2003 5 22 C2XA03SH139 120030518A531114525664003 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV DURING C-CHECK A DENT WAS FOUND AT FRAME 67 STRINGER 15 RIGHT. MAINTENANCE REMOVED DAMAGE AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-00-04. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030522000802003052200080WP 2003 5 22 GTIA030291 120030416A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 CORRODED WEB L18R AT FS 256-313, FS 503-522, FS 541-560, AND FS 674-712. MAT ON FS 275-313 IS OUT OF LIMITS. CUT OUT DAMAGED AREA. FORMED NEW DOUBLER REPAIR. INSTALLED NEW DOUBLER REPAIR. 2L72 4F4 FRTA6WE E2EA 20030522000982003052200098 2003 5 22 SWAA031092 420030514A2565 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030522001022003052200102NM 2003 5 22 DHL2003783009 120030515A2612 FIRE DETECTOR BOEING727 727227 1384078NM NR 3 ENGINE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01766AT 21999 ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. REPLACED LOWER DETECTOR ELEMENT SUPPORT CLAMP DUE TO WORN SYSTEM. TESTED IAW M/M 20-11-00, OPS NORMAL. GROUND FAULT LIGHT IS OFF. 2L73 4F A3WE 20030522001032003052200103NM 2003 5 22 DHL2003783010 120030516A2697 WIRE BOEING727 727227 1384078NM FIRE DETECTOR SHORTED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01766AT 21999 ENGINE NR 3 DETECTOR CIRCUIT GROUND FAULT LIGHTS ILLUMINATED AT P6 CIRCUIT BREAKER PANEL. DEFERRED PER DHL MEL 26-9-1 CAT-C. ASSIGNED CONTROL 12957. PLACARD INSTALLED. REF DMI 12957 ENGINE NR 3 DETECTOR GROUND CIRCUIT FAULT LIGHT ILLUMINATED. FOUND POOR INSTALLATION. REINSTALLED IAW B727 OHM 71-02-01. OPS CHECKED NORMAL. THIS CLEARED DMI 12957. 2L73 4F A3WE 20030522001122003052200112NM 2003 5 22 AWXA200300550 120030516A7711LG14C14 TRANSMITTER BOEING737 737277 1384570NM NR 2 ENGINE EPR MALFUNCTIONED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28182AW30035369 22649 PHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR TUS, SETTING REDUCED FOR POWER 1.96, NR 2 ENGINE EPR DID NOT COME UP TO POWER, EPR STAGNATED AT 1.45 EPR WHILE THRUST LEVER ADVANCED. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT WIRING AND COULD NOT DUPLICATE PROBLEM, REMOVED AND REPLACED EPR TRANSMITTER IAW BMM 77-11-21, PG 401, OPERATIONAL CHECK WAS GOOD. VENDOR BENCH TEST OF EPR TRANSMITTER S/N P100 CONFIRMED FAILURE OF UNIT. UNIT WAS FOUND TO BE OUT OF CALIBRATION DUE TO DRIVE TRAIN GEAR CONTAMINATION. CLEANED DRIVE TRAIN GEARS AND BEARINGS; RESET CALIBRATION ON MECHANISM ASSEMBLY IAW CMM 77-10-01. 2L72 4F RTA16WE 20030522001152003052200115 2003 5 22 CALA0300252 420030517A2565D31393109 SLIDE AIRCRUISERS BOEING757 757224 1384958NM LEFT LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW27191177720 27559 INSPECTION FOUND LT OVERWING ESCAPE SLIDE UNLACED. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-60-00 AND WORK CARD 19-2560-1-0901. 2L72 4F RTA2NM 20030520000602003052000060NM 2003 5 20 AMTA200300515 120030417A3350 BULB BOEING737 73783N 13844HINM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11312TZ 32579 L2 DOOR EGRESS SIGN HAS ONE BULB INOPERATIVE. REMOVED AND REPLACED L2 DOOR EGRESS EXIT SIGN INDICATOR IAW 737 AMM 33-51-01, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030521000022003052100002EU 2003 5 21 MALA030265 120030508A211011341041 MOTOR SAAB SF340 340B 7860101EU COMPRESSOR FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15426XJ 340B426 DURING FLIGHT 2786 SMOKE FILLED CABIN WITH SUPP A/C ON. NO PAX BOARDED AT THIS TIME. SMOKE FILLED CABIN WITH SUPP AC ON. SHUT SUPP AC OFF AND SMOKE STOPPED. MAINTENANCE FOUND COMPRESSOR MOTOR BURNT AND FAN SHROUD BURNT. REPLACED COMPRESSOR MOTOR AND SHROUD IAW SF340, R-134A AIR CONDITIONING SYSTEM MM, ALL CHECKS GOOD AT THIS TIME. MOTOR P/N ON & OFF P/N 1134104-1, S/N OFF 494, S/N ON 117, SHROUD P/N 1250611. REMOVED FROM DMR MXC NOTIFIED. 2L72 4T RTA52EU 20030521000622003052100062WP 2003 5 21 DHL2003804906 120030215A571457066751 PANEL DOUG DC8 DC873F 302199FWP CENTER WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING - NR 728 CTR WING LOWER PANEL INNER SKIN DELAMINATED, STA 779.000 - STA 810.000. REMOVED AND REPLACED CTR WING LWR PANEL NR 728 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521001022003052100102NM 2003 5 21 DHL2003754007 120030514A2613 OVERHEAT SENSOR BOEING727 727223 1384074NM WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 PRE-FLIGHT, LOWER AFT BODY OVERHEAT WILL NOT TEST. BULB TESTED GOOD. TRANSFERRED TO DMI 12918 IAW B727 MEL 26-10-2 CAT-C, PLACARDS INSTALLED. REF DMI 12918 LOWER AFT BODY OVERHEAT WILL NOT TEST. BULB TESTED OK. CLEANED AND RESEATED CONNECTOR AS PER WPM 20-60-1. SYSTEM TESTED GOOD IAW M/M 26-14-01. THIS ACTION CLEARS DMI 12918. 2L73 4F A3WE 20030521001112003052100111WP 2003 5 21 DHL2003801055 120030412A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 341.500 AND 347.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. DRILLED NEW HOLES ON DOUBLER IAW SRM 51-1-22 PG 1. INSTALLED DOUBLER USING NEW FASTENERS IAW SRM 57-2-1 FIG 38 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001142003052100114WP 2003 5 21 DHL2003801007 120030429A57405769859164 FITTING DOUG DC8 DC873F 302199FWP RT STUB WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT STUB WING UPPER SURFACE ZEE PAN AT STA XS 250.089 WITH 2.000 INCH CRACK. REMOVED AND REPLACED RT STUB WING UPPER SURFACE ZEE PAN FITTING AT XS 250.089 IAW SRM 51-1-21 PG 1 AND SRM 51-1-21D PG 9. 2L74 4F RT4A25 20030521001202003052100120NE 2003 5 21 DHL2003721001 220030515A7200 ENGINE BOEING727 727228 1384083NM PWA JT8 JT8D7 52053NE NR 3 MALFUNCTIONED A DHLACDO ABORTED TAKEOFF RETURN TO BLOCK OTHER O OTHER TOTAKEOFF 1 SO01721DH 19545 REJECTED TAKEOFF - UNABLE TO MAKE EPR ON NR 3. T/O EPR READINGS 1.94; 1.96; 1.83. UTILIZED EMERGENCY PROCEDURE 5.4.1, REJECTED TAKEOFF FLOW CHART, AND BRAKE ENERGY CHART AS PER FN NR 2, ENGINE, AIRCRAFT, WEATHER CONDITIONS WERE: 165.3, SPEED 80 KTS, TEMP 27C, PA AT 29.82 160 FT. BRAKE ENERGY CHART IN NORMAL RANGE EGTS 520; 520; 520. ENGINE NR 3 WAS SLOW TO SPOOL UP AND DID NOT MAKE T/O EPR WHILE NR 1 AND NR 2 WERE AT T/O POWER. RII REQUIRED. FOUND ALL ENGINES OUT OF TRIM. TRIMMED ALL 3 ENGINES IAW B727 MM 71-00-30 & DHL JRH. RUN SHEET COMPLETED, NO DEFECTS NOTED. C/W REJECTED TAKEOFF INSPECTION. REJECTED TAKEOFF INSPECTION IAW DHL GMM 5.6 & B727 M/M 05-51-121. NO DEFECTS NOTED. 2L73 4F4 FRTA3WE E2EA 20030521001922003052100192EU 2003 5 21 AWXA200300543 120030502A5320D5397470900000 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT AT FR 63, LBL 406MM. MAINTENANCE REMOVED DAMAGED FLOOR PANEL SUPPORT AT FR 63, LBL 406MM; FABRICATED A NEW REPLACEMENT FLOOR PANEL SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-12 & 22 FIG 2, 3 & 8. 2L72 4F RTA28NM 20030521001962003052100196 2003 5 21 SWAA031059 420030511A25656519901 CABLE BOEING737 7373G7 1384595NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030521002022003052100202WP 2003 5 21 DHL2003804876 120030208A5754576998591 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 SLOT VANE UPPER SKIN HOLES ELONGATED AT STA XS 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 03112, ED-3217. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EO DHL 030112, ED-3217. FABRICATED A REPAIR DOUBLER (7075 T6AL-0.071), FILLER (7075T6AL-0.063) AND INTERNAL DOUBLER (7075T6AL-0.050) IAW EO DHL03112, ED-3217. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER AT LT INBOARD SLOT VANE UPPER SKIN WITH NEW FASTENERS IAW EO DHL 03112, ED-3217 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030522000032003052200003NM 2003 5 22 0300936632 120030507A5412 BULKHEAD BOEING747 747251B 1384892NM NACELLE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 23112 DURING H-CHECK, FOUND CRACK IN NR 3 PYLON REAR MOUNT BULKHEAD WEB AT NACELLE STATION 227. REPAIRED PER EA 66-165065. 2L74 4F A20WE 20030522000282003052200028WP 2003 5 22 GTIA030279 120030428A7160 LINER DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE NR 2 ENGINE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23801NK 48048 NR 2 ENGINE INLET HAS TWO CUTS ON ACCOUSTIC LINING AT 4 AND 6 O`CLOCK POSITION. REPAIRED NR 2 ENGINE INLET ACCOUSTIC LINING. NO OTHER DEFECTS NOTED AT THIS TIME. 2L72 4F4 F A6WE E2EA 20030522000772003052200077SO 2003 5 22 C2XA03TY070 120030517A531014520600001 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 TYS, DURING A SCHEDULED INSPECTION THE LEFT FLOOR SUPPORT JUST AFT OF MAIN CABIN DOOR WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030606000432003060600043NE 2003 6 6 00090 220030514A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05221TW 221 304152B AIRCRAFT DEPARTED ADS WHILE CLIMBING FROM FL360 TO FL 370 LEFT ENGINE FLAMED OUT, ENGINE RELET AND CONTINUED TO DESTINATION, ON POST FLIGHT INSPECTION NO FOD DAMAGE OR LEAKS FOUND. NO FURTHER PROBLEM ON NEXT LEG. 2L72 4F4 F A7EU E7EA 20030606000592003060600059EA 2003 6 6 COMA0370015 120030516A3260533405 VALVE CNDAIRCL600 CL6002C10 1390015EA NLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01371CA775 10082 FLIGHT 5071 DURING CLIMB OUT RECEIVED A GEAR DISAGREE WARNING WHEN GEAR WAS SELECTED UP, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20030606000762003060600076NM 2003 6 6 03FDEA00773 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B CTR BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000832003060600083NM 2003 6 6 03FDEA00766 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000902003060600090NM 2003 6 6 COOSDR030017 120030501A5755651734754 SKIN BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 4 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG 20725 LEFT WING, FLIGHT SPOILER NR 4, PN 65-17347-54, SN BN378 WITH DELAMINATION. 2L73 4F4 FRTA3WE E2EA 20030606000992003060600099CE 2003 6 6 DRU2003F00000 120030210A301040653481 BLANKET LEAR 25 25B 5170511CE GE CJ610 CJ6108 30006NE HORZ STAB DEICE BURNED E DRUAO OTHER O OTHER NRNOT REPORTED 1 GL257810W7695 117 DURING INSP BY MECH, A BLACK STREAK (FORE TO AFT) WAS NOTICED ON LT HORIZ STAB, THAT BOOT LOOKED BURNT ON L.E. EXAMINATION REVEALED THAT BOOT MUST HAVE SHORTED AGAINST L.E., BURNING BOTH BOOT AND HORIZ STAB CONSISTED OF NICKEL SIZE HOLE BEING COMPLETELY BURNT THROUGH. NO OTHER INTERNAL STRUCTURES WERE DAMAGED. BOTH BOOT AND L.E. SKIN WERE REMOVED AND REPLACED BY NEW COMPONENTS. LAST SCHEDULED INSP OF TAIL REVEALED NO ANNOMOLIES. AN INSPECTION OF STAB DE-ICE SYST WAS ACCOMPLISHED, INCLUDING SEQUENCE TIMER, WIRING, CIRCUIT BREAKERS, CURRENT LIMITER, TERMINAL BLOCKS, SYST SWITCH, AND CAUTION LIGHT. PILOTS REPORTED NO DISCREPANCIES. CIRCUIT BREAKERS AND CURRENT LIMITER HAD NOT BLOWN PREVENTING THIS MALFUCTION. 2L72 4J4 J A10CE 1E16 20030609000032003060900003EA 2003 6 9 COMA0360244 120030520A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01914CA23084 7012 WHILE ACCOMPLISHING TASK 53-160-610, THREE CRACKS WERE FOUND ON THE FUSELAGE PRESSURE FLOOR SKIN, ONE AT FS 459.5 BETWEEN LBL 0.0 AND RBL 9.0, AND TWO AT FS 462.0 BETWEEN LBL 9.0 AND RBL 9.0 THE CRACKS MEASURE 2.25, 2.50 AND 3.25 INCHES IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102 DATED 18-13-2002 AND COMAIR E.A. 10-5330-00194 DATED MAY 15, 2003. 2L72 4F RTA21EA 20030609000042003060900004WP 2003 6 9 ARWA20030210 120030215A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198968U 46069 DURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 340, STRINGER 21. REMOVED AND REPLACED FLOOR BEAM SPLICE PLATES AT STA 340 IAW STC SA1063SO AND SA1377SO. 2L74 4F 4A25 20030609000072003060900007SO 2003 6 9 C2XA03BT059 120030520A3350 FUSE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BLOWN A C2XAO OTHER L NO TEST ININSP/MAINT 1 SW2716919 145393 EWR---CO2196, CREW REPORTED, EMERGENCY EXIT LIGHT STRIP INOPERATIVE.....MAINTENANCE REMOVED AND REPLACED FUSES IN GALLEY EMERGENCY LIGHT BATTERY IAW EMB145 CMM #25-60-03 AND 33-50-00, OPS. CHECKED EMERGENCY LIGHT STRIP GOOD. 2L72 4T RTT00011AT 20030609000142003060900014SO 2003 6 9 SWIA200311982 120030520A3150 WARNING LIGHT EMB 120 EMB120ER 3260203SO STAB TRIM ILLUMINATED A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07561SW 120335 ON TAKEOFF ROLL, GOT A ''TRIM WARNING''. ABORTED TO AND RETURNED TO THE BOX.FOUND AURAL WARNING CB'S POPPED. RESET CB'S AND ALL TEST GOOD. 2L72 4T RTA31SO 20030609000572003060900057WP 2003 6 9 ZW0A0305002 120030521A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13905TW 49157 THE EGRESS LIGHT AT ROW 7 AND THE EMERGENCY LIGHTS ABOVE THE L1 AND L2 DOORS WERE INOPERATIVE. REINSERTED THE LAMP INTO THE MODULE FOR THE EGRESS LIGHT, REPLACED THE LAMP ASSEMBLY PN L20191-9 ABOVE THE L2 CABIN DOOR, AND CLEANED THE CONTACTS AND REPLACED THE LAMP PN 1315 ABOVE THE L1 CABIN DOOR. CHECK-C 12-3-02 STL. --CLOSED-- 2L72 4F A6WE 20030609000672003060900067EA 2003 6 9 SWIA200311990 120030520A3241750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07499SW5465 5465 7398 UPON TAKEOFF, RECEIVED ANTI-SKID INBOARD CAUTION MSG FOLLOWED BY A GEAR DISAGREE WARNING AND PARKING BRAKE SOV CAUTION. FOLLOWED QRH PROCEDURE AND RETURNED TO THE AIRPORT.REMOVED AND REPLACED MLG SELECTOR VALVE IAW MM 32-32-10. OPS CHECK GOOD. LEAK CHECK GOOD. 2L72 4F RTA21EA 20030609000702003060900070EA 2003 6 9 QXEA0300622 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 18R, 6 INCHES AFT OF FS 235. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000762003060900076EA 2003 6 9 QXEA0300628 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS 409, 2 INCHES ABOVE STRINGER 15R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000802003060900080EA 2003 6 9 QXEA0300632 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 12R, 4 INCHES FORWARD OF FS533. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000822003060900082EA 2003 6 9 QXEA0300634 120030517A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 FASTENER DAMAGED, 3 INCHES FORWARD OF FS597 AND 2 INCHES ABOVE STRINGER 10R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-20, PG 13-22. 2L72 4F RTA21EA 20030604001822003060400182NM 2003 6 4 UPS03440602 120030410A5410 FRAME BOEING747 747121 1384871NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, NR 2 PYLON REAR ENGINE MOUNT BULKHEAD AFT FRAME FOUND CRACKED AT 4 & 5 O/C POSITION ( LOOKING FORWARD ). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD I/B AFT FRAME REPAIRED AS PER RS 54-53-35009 AND UPS REPAIR AUTHORIZATION 747-54-20035 INSPECTIONS OF DVI AND HFEC TO CONTINUE PER UPS EO B747-5410-13908 AND SB 747-54A2202. 2L74 4F A20WE 20030604001962003060400196WP 2003 6 4 UPS03840613 120030414A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, AFT FUSELAGE INSIDE 60 HOLE LONG. 17R IS CRACKED AT STA. 1776 APPROX REMOVED,FABRICATED AND REPLACED LONGERON IAW SRM. 53-5-0,51-1-20D AND DWG. 5649327 2L74 4F RT4A25 20030604002002003060400200NM 2003 6 4 C8GA20030011 120030430A7930 WARNING LIGHT BOEING727 727227 1384078NM NR 2 & 3 ENG ILLUMINATED A C8GAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO15308AS 22002 FLIGHT 201 FROM MIA TO PTY. ABORTED TAKE OFF ROLL DUE TO NR 2 AND 3 ENGINE OIL BYPASS LIGHT CAME ON AT 90 KNOTS. AIRCRAFT RETURNED TO BLOCKS WITHOUT INCIDENT. REMOVED AND INSPECTED NR 2 AND 3 ENGINE OIL FILTERS, BOTH FILTERS WERE FOUND TO BE CLEAN. INSTALLED NEW FILTERS IN BOTH ENGINES, PERFORMED ENGINE RUNS, LEAK CHECKS WAS GOOD AND BOTH NR 2 AND 3 LOW OIL PRESSURE BYPASS LIGHTS WENT OUT AND WORKED NORMALLY PER B727 MM 79-30-00. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030604002122003060400212WP 2003 6 4 UPS03840631 120030430A5610 WINDOW DOUG DC8 DC871F 302199DWP COPILOT OUT OF ADJUST A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: PFLT, COPILOTS SIDE WINDOW WILL NOT OPEN DISCOVERED ON POST FLIGHT ADJUSTED WINDOW GUIDE AT TOP FORWARD CORNER OF F/O SLIDING WINDOW. 2L74 4F RT4A25 20030605000282003060500028SO 2003 6 5 SIMA200302105 120030101A531014522461011 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 FOUND DUIRNG A IMBV INSPECTION, DIAMOND GUSSET ON RIGHT BEAM AT FRAME 22 CORRODED. REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET IAW EMB 145/135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030605001092003060500109NM 2003 6 5 SCNA03002 120030513A3350D71702001 POWER SUPPLY BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL1580SY 5661 30332 FLOOR PATH LIGHTING AT SEATS 17-23 ABC INOP. REPLACED POWER SUPPLY PER AMM 33-51-06-960-805 SYSTEM CKED NORMAL. 2L72 4F RTA16WE 20030605001182003060500118NM 2003 6 5 P5CA0300877 120030514A7920 LINE BOEING747 747237B 1384858NM PWA JT9 JT9D7J 52054NE NR 1 ENG OIL LEAKING A P5CAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23524UP 21446 662348 DURING CRUISE NR 1 ENG OIL QTY SLOWLY PROGRESSED TOWARD ZERO, LOW OIL PRESS LIGHT ILLUM. FOUND OIL LEAKING FROM NR 1 ENG GEN TRANSFER TUBE PER MM 24-11-00 GEN & CSD REMOVED FOR FLT P/N 2MIT60B00010 KIT INSTALLED PERFORMED ENG RUN - NO LEAKS NOTICED. OIL LEAKING INTO THE TRANSFER TUBE FROM THE GEAR CASE AND GOING OVERBOARD 2L74 4F4 FRTA20WE E20EA 20030605001262003060500126 2003 6 5 MEX2003119 420030405A34526227878201 TRANSPONDER DOUG MD88 MD88 3023688NM ATC FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 GL23XATPM2770 2770 49671 CAPTAIN REPORTED ATC TRANSPONDER OUT OFF SERVICE. WITH ATC TRANSPONDER FAILURE WAS REQUESTD TO FAA ATCA TO OPERATE IAW MEL34-22 (AUTHORIZATION NR ZFWZM04052003). DURING OVERNIGHT SERVICE BOTH ATC TRANSPONDERS, LOWER ANTENNA AND TRANSFERENCE RELAY WERE REPLACED IAW MM, TESTS CORRECT. 2L72 4F RTA6WE 20030606000602003060600060EU 2003 6 6 MALA030268 120030515A3260 DOWNLOCK SWITCH SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15370PX 340B300 ON FINAL APPROACH WITH GEAR SELECTEDDOWN THERE WAS NO RT MAIN GREEN LIGHT INDICATION. THERE WAS NO AMBER DIWSAGREEMENT LIGHT. A GO-AROUND WAS INITIATED. WHEN FLAPS WERE SELECTED UP THE RT MAIN GEAR LIGHT CAME ON. A/C LANDED WITHOUT INCIDENT. INSPECTED A/C AND FOUND SAFE FOR FERRY FLIGHT FROM SCE TO DTW FOR RT MLG INDICATION. MAINTENANCE REPLACED MLG DOWNLOCK SWITCH (RT) IAW SAAB 340 AMM CHAP 32-61. ALL CHECKS GOOD. 2L72 4T RTA52EU 20030606000882003060600088WP 2003 6 6 03FDEA00761 120030519A5753ARC0502 HINGE DOUG DC10 DC1010 3022110WP RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 S 20 COMPLY WITH E.A.8-5750-70378. WINGS-OUTBD FLAP RT-INBD HINGE BRACKET- ACTUATOR ATTACH HOLE REPAIR P/NARC0502. CLOSING ACTION ON 05/13/03 COMPLIED WITH .8-5750-70378. WINGS-OUTBD FLAP R/H-INBD HINGE BRACKET-ACTUATOR ATTACH HOLE REPAIR P/N ARC0502. 2L73 4F A22WE 20030609000632003060900063EA 2003 6 9 SWIA200311986 120030515A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WORN A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07589SW 7072 ON FINAL, FLAPS 45 SELECTED. ''FLAP FAIL'' MESSAGE BOTH FLAPS INDICATING 45 DEGREES. FLAPS WOULD NOT RETRACT AFTER LANDING.TROUBLESHOT FLAP SYSTEM. LT INBOARD FLAP ACTUATORS WORN AND BINDING. REPLACED THE LT INBOARD FLAP ACTUATORS AND RIGGED LT AND RT FLAP SYSTEMS. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20030609000872003060900087EA 2003 6 9 QXEA0300640 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS 830.4, 2 INCHES ABOVE STRINGER 10R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000892003060900089EA 2003 6 9 QXEA0300642 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS 953, 2 INCHES ABOVE STRINGER 12R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030609000952003060900095NM 2003 6 9 AWXA200300576 120030502A5320146N53236 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT 2 EACH NUT PLATES UNDER CABIN FLOOR PANEL BS 1708, RBL 50. MAINTENANCE REMOVED NUT PLATE CLIPS FROM FLOOR SUPPORT ANGLE BS 1708, RBL 50, AND FOUND FLOOR SUPPORT ANGLE TO ALSO BE CORRODED; REMOVED CORROSION AND FOUND MATERIAL LOSS BEYOND LIMITS; REMOVED DAMAGED FLOOR SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART AND NEW NUT PLATE CLIPS IAW B757-200 SRM 51-70-11, PG. 1-7, FIG 1. 2L72 4F RTA2NM 20030609000992003060900099SO 2003 6 9 C2XA03SH141 120030523A531112010732001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV-DURING C-CHECK THE APU FIREWALL LOWER FRAME 81 WAS FOUND TO HAVE A CRACK. MAINTENANCE PERFORMED A DOUBLER REPAIR AT FRAME 81 IAW EC 5310-01238. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030609001122003060900112NM 2003 6 9 DHL2003747507 120030512A5312 BULKHEAD BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING "C" CHECK DISCREPANCY AS FOLLOWS, "AFT. PRESS. BULKHEAD BS 1183 RBBL 36.4 VERTICAL BEAM IS CRACKED FROM INB/OUT AFT. FLANGES. STOP DRILLED CRACKS AND INSTALLED REPAIR PARTS PER S/B 727-53-0192 REV. 1, FIG. 2. 2L73 4F A3WE 20030609001172003060900117NM 2003 6 9 CALA0300264 120030521A5310 DOOR FRAME BOEING777 777224 1385225NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777014 29862 MAINTENANCE DISCOVERED DAMAGE IN THE FORM OF A DENT AND 1.1 INCH LONG CRACK IN THE AFT CARGO DOOR UPPER BEAM ASSEMBLY WEB WHILE AIRCRAFT WAS ON RON AT IAH. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5230-01723 AND A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 365 CALENDAR DAYS. 2L72 4F RTT00001SE 20030609001202003060900120WP 2003 6 9 ABXA030147 120030502A532039203202N ANGLE DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 DURING A LINE MAINTENANCE VISIT, FOUND THE LT WHEEL WELL SLANT PANEL INBOARD ATTACH ANGLE CRACKED AND EXFOLIATED. CRACK WAS APPROXIMATELY 3" LONG. REPLACED ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 20030609001252003060900125WP 2003 6 9 ABXA030149 120030502A552339180755 BRACKET DOUG DC9 DC932 3022066WP LT ELEVATOR TAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 DURING A LINE MAINTENANCE VISIT, FOUND THE RIGHT ELEVATOR GEARED TAB INBOARD HINGE BEARING BRACKET CRACKED. REPLACED RIGHT GEARED TAB IAW DC-9 MM 27-30-04-2-0001. 2L72 4F A6WE 20030609001312003060900131EU 2003 6 9 MALA030278 120030504A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15525XJ E2350 DURING C-CHECK INSPECTION IN CVG, NR 2 SEAT TRACK ON FRAME 18 HAS CORROSION. MAINTENANCE REPAIRED SEAT TRACK IAW EO A53026. REF TO 409 118111 FOR DETAIL. A/C RELEASE DATE 5/21/03. 2H74 4F RTA49EU 20030609001392003060900139NE 2003 6 9 AWXA200300584 220030523A7320 CONTROL UNIT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ENGINE MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28650AW 856 ON TAKEOFF AT LAS EN ROUTE FOR CMH WITH THRUST SET TO FLEX, NR 2 WENT TO TOGA, AND NR 1 WENT TO FLEX OR REDUCED SETTING (10 O'CLOCK ON GAUGE). HAD ECAM MESSAGE NO FLEX TEMP SET, BUT FLEX WAS SET AT IDLE. UPPER ECAM POWER INDICATOR VARIED FROM TOGA TO CLIMB WITH NO CREW INPUT. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED BITE TEST THROUGH CENTRAL FAULT DISPLAY SYSTEM ON FULL AUTHORITY DIGITAL ENGINE CONTROL NR 1 & 2, A & B CHANNELS, NO FAULTS WERE NOTED. PERFORMED BITE TEST OF ENGINE INTERFACE UNIT NR 1 & 2, NO FAULTS NOTED. PERFORMED ENGINE RUN TO TAKEOFF POWER WITH NO DEFECTS NOTED. 2L72 4F4 FRTA28NM E40NE 20030609001432003060900143SO 2003 6 9 SWIA200312000 120030519A27523203001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07268UE5888 3387 120207 CREW REPORTS CONTROL FAULT ON INBOARD FLAPS.REMOVED AND REPLACED RT IB FLAP ACTUATOR IAW 27-50-07. REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW 27-50-01. PN OFF/ON 120-64207-615 SN OFF 280040-316. FUNCTIONAL TEST AND OPS CHECK GOOD. 2L72 4T RTA31SO 20030609001512003060900151SO 2003 6 9 C2XA03SH155 120030525A532014525681007 ANGLE EMB 145 EMB145ER 3260211SO CARGO RAMP CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE LOWER ATTACH ANGLE FOR THE CARGO RAMP AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030609001722003060900172EU 2003 6 9 CA030430008 120030430A324615702100 FAIRING PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL MLG WHEEL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FAIRING HAS CRACKS NOTED ADJACENT SCREW HOLES. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030609001762003060900176EA 2003 6 9 CA030501003 120030425A2916 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYD SYSTEM LEAKING W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DIVERSION DUE TO MECHANICAL. CREW REPORTED 'HYD 2 LOW PRESS LIGHT CAME ON IN FLIGHT(FL330) HYDRAULIC PRESSURE READ 0 PSI. ENGINE WAS RUN FOR 33 MINUTES ENROUTE TO DIVERSION LANDING KFWA. 'NIL HYDRAULIC QUANITY. LANDING COMPLETED WITH OUT INCIDENT. MAINTENANCE FOUND HYD RESERVOIR LEAKING FROM STAND PIPE AT ATTACH POINT TO BOTTOM OF RESERVOIR.RESEVOIR REPLACED. ENGINE DRIVEN HYD PUMP REPLACED DUE TO BEING RUN WITH HYDRAULIC SYSTEM EMPTY. RETURN LINE FOR PUMP SUBSEQUENTLY FOUND LEAKING AND REPLACED. SUSPECT ALSO AFFECTED BY PUMP BEING RUN WHILE DRY. 2L72 4F4 FRTA21EA E15NE 20030609001812003060900181CE 2003 6 9 CA030501008 120030501A32301153800025 MOTOR BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA MLG FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER REPLACING GEAR ACTUATORS, MOTOR CONTROLLER AND GEAR BOX AND COMPLETING 15 GEAR SWINGS. THE AIRCRAFT WENT ON A TRAINING FLIGHT. WHILE TRAINING THE GEAR WAS SELECTED UP. THE GEAR STOPPED MID TRAVEL AND DID NOT RESPOND TO GEAR DOWN SELECTION. A MANUAL GEAR EXTENSION WAS COMPLETED AND THE AIRCRAFT LANDED SAFELY. THE LANDING GEAR CIRCUIT BREAKER WAS TRIPPED. THE CB WAS RESET AND THE GEAR SWUNG SEVERAL TIMES WITHOUT INCIDENT. SUSPECTED MOTOR TRIPPING C/B WHEN SUBJECT TO AIR LOADS. THE MOTOR AND THE CIRCUIT BREAKER WILL BE REPLACED. 1L72 4T4 T A24CE E4EA 20030605000712003060500071EU 2003 6 5 XNOA01118 120030513A5610 PIN AIRBUS300 A300B4203 3930306EU WINDOW LATCH OUT OF ADJUST A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23370PC 134 DURING TAXI CHECK F/O'S WINDOW WILL NOT LATCH. RESET PIN LATCH MECHANISM ON F/O'S WINDOW. OPS CHECK GOOD IAW A300 MM 56-12-00. NO OTHER DEFECTS. 2L72 4F RTA35EU 20030605000722003060500072NM 2003 6 5 MEX2003157 120030504A2740 MODULE DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE H/S INDICATOR MALFUNCTIONED W ASMFA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23160PL 49763 A/C RETURN TO PLATFORM , TAKE OFF WARNING ACTIVATED ON FLAPS MODE. THE FLIGHT WAS CANCELLED. DURING OVERNIGHT SERVICE THE TAKE OFF WARNING WAS VERIFIED IAW MM. THE HORIZONTAL STABILIZER POSITION INDICATOR MODULE WAS TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030605001272003060500127SO 2003 6 5 CHQA000249 120030516A2611 WARNING LIGHT EMB 145 EMB145 3260210SO LAVATORY SMOKE ILLUMINATED A CHQAO OTHER J WARNING INDICATION CRCRUISE 1 GL11266 LAV SMOKE WARNING. WILL SEND UPDATE WHEN MORE INFORMATION IS AVAILABLE ON A CORRECTIVE ACTION. 2L72 4F RTT00011AT 20030605001332003060500133CE 2003 6 5 BLI2003F00001 120030331A2421 SPACER CESSNA421 421B 2076014CE CONT O520 GTSIO520F 17032SO ALTERNATOR WRONG PART E BLIAO OTHER O OTHER NRNOT REPORTED 1 GL1765AE 421B0953 WHILE REPLACING AN ALTERNATOR, NOTICED THAT DRIVE GER RETAINING NUT WOULD NOT RUN DOWN SUFFICIENTLY TO INSTALL SAFETY. DISCOVERED 2 DIFFERENT SPACER SIZES ON OLD AND NEW AACT. REMOVED CORRECT SIZE SPACER FROM ANOTHER OHC ALTERNATOR AND INSTALLED. CONTACTED FACILITY TO INFORM AND ACQUIRE CORRECT REPLACEMENT SPACER. 1L72 3O3 O A7CE E7CE 20030606000062003060600006NE 2003 6 6 03128410 220030508A7200PWC306B ENGINE DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT FAILED A VTZAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA27410FJ4268 3165 PCECD0136 DURING CLIMB, THE CREW REPORTED THAT THE LT ENGINE HAD FAILED. THE ENGINE WAS SECURED AND THE FLIGHT RETURNED TO CVG WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT ENGINE. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030606000312003060600031NM 2003 6 6 03FDEA00734 120030514A5753 STRUCTURE DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- L/E XORS 805, CRACK FOUND APPROX 12 INCHES FROM TOP TO LOWER SURFACE. REPAIR CARRIED OUT AT LT WING L/E XORS 805 TOP TO LOWER SURFACED AREA AS PER SRM 57-10-00 FIG.7 VOL.I. 2L73 4F RTA22WE 20030609001382003060900138NM 2003 6 9 AWXA200300583 120030504A5320146N530093 CHANNEL BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SHEAR DECK HAT CHANNEL BS 1714-1716, RBL 12. MAINTENANCE REMOVED DAMAGED HAT CHANNEL BS 1714-1716, RBL 12; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-05, PG. 1, 2, & 5. 2L72 4F RTA2NM 20030609001902003060900190CE 2003 6 9 CA030520001 120030516A3260 WIRE CESSNA650 650 2076802CE GARRTTTPE731TFE7313C WP UPLOCK SWITCH BROKEN W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) AFTER THE AIRCRAFT TOOK-OFF PILOT SELECTED THE GEAR HANDLE TO THE UP POSITION. DURING CLIMB PILOT REPORT LT MAIN LANDING INDICATION STILL SHOWN GEAR DOWN AND LOCK, PASSENGER HEARD A RUMBLE AROUND LT GEAR AREA. AIRCRAFT RETURN TO YUL MAINTENANCE BASE. MAINTENANCE FOUND A BROKEN WIRE AT THE LT UPLOCK SWITCH. WIRE REPAIRED AS PER MANUFACTURER INSTRUCTION. AIRCRAFT RETURN TO SERVICE. 2L72 4F4 F A9NM E6WE 20030610000072003061000007NE 2003 6 10 CALA0300265 220030525A7321 HMU BOEING737 737824 13844BZNM CFMINTCFM56 CFM567B26US NE NR 2 ENGINE FAILED A CALAO OTHER Y ENGINE STOPPAGE APAPPROACH 1 SW2712221 28930 875908 THE NR 2 ENGINE AUTO SHUTDOWN WHILE AT 6,000 FEET ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. BITE TESTS ON THE HMU AND EEC INDICATED THAT BOTH NEEDED TO BE CHANGED. THE NR 2 ENGINE HMU AND NR 2 ENGINE EEC WERE REMOVED AND REPLACED. SUPPLEMENT ADDS PART INFORMATION FOR HMU. 2L72 4F4 FRTA16WE E00055EN 20030610000142003061000014SO 2003 6 10 C2XA03BT061 120030524A335020131A BATTERY EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727512 145274 CREW (DURING WALKAROUND) NOTICED THE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES AND OPS CHECKED SYSTEM GOOD. 2L72 4F RTT00011AT 20030610000192003061000019NM 2003 6 10 2003UALA00438 120030516A3397 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 EMERGENCY LIGHTS ARE INOP AT EXTERIOR AT DOOR 4L AND EEL LIGHTS, EXIT SIGN AND BULLNOSE LIGHTS BETWEEN ROWS 20-30. RELAMPED AT DOOR 4L AND RESEATED CONNECTORS ON POWER SUPPLIES. 2L72 4F4 FRTA2NM E17NE 20030610000302003061000030SO 2003 6 10 C2XA03CL102 120030523A3397 CONNECTOR EMB 145 EMB145ER 3260211SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715932 145015 CLE FLIGHT 2256, THE CREW REPORTED THE EXIT LIGHT OUT AT ROW 12A. MAINTENANCE INSPECTED AND RESECURED LOOSE CONNECTOR AT THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030610000312003061000031EU 2003 6 10 03144324 120030524A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSLOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27324UE 41017 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT 3 LAMPS IN THE FWD. EMERGENCY FLOOR TRACK LIGHTS WERE INOP. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE EMERGENCY FLOOR LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030610000332003061000033EA 2003 6 10 03144637 120030524A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27637BR 7308 DURING MAINTENANCE INSPECTION, THE LT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030610000442003061000044WP 2003 6 10 ABXA030169 120030415A533059114162 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 FUSELAGE EXTERIOR SKIN HAD BULGE AT APPROXIMATELY STA 589, LONGERON 18 RIGHT. REPAIRED AREA IAW REA D958-47172MR AND DC-9 SRM 51-10-3. 2L72 4F A6WE 20030610000552003061000055WP 2003 6 10 ABXA030155 120030324A532099105035 WEB DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 CUSP WEB CRACKED AT STA 889 TO 929, LEFT SIDE. REPLACED CUSP WEB FROM LEFT BUTT LINE 55, FS 900 - FS 965 IAW DC-9 SRM. 2L72 4F A6WE 20030610000712003061000071NM 2003 6 10 DL73S030412 120030501A53106547952524A DOOR FRAME BOEING737 737232 1384475NM CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 THE UPPER FRAME PORTION OF THE FWD FRAME ON THE C2 CARGO DOOR WAS FOUND WITH A CRACK IN THE LOWER FASTENER ROW OF THE FRAME AT THE LAP JOINT BETWEEN THE UPPER AND LOWER FRAME. THE CRACK WAS STOP DRILLED AND REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 384999-14, REV A. 2L72 4F RTA16WE 20030610000762003061000076NM 2003 6 10 DL733030417 120030503A36101828203 HEAT EXCHANGER BOEING737 737347 1384647NM RT CRACKED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO273301 23181 RIGHT WING BODY OVERHEAT LIGHT CAME ON DURING CLIMB RAN PROCEDURE BUT LEFT PACK WOULD NOT HOLD CABIN ALTITUDE CABIN UNDER CONTROL AT 18000 MAX CABIN ALT 9500. FOUND FIBERGLASS PLENUM AT HEAT EXCHANGER BLOWN OUT ON LOWER SEAM ALSO FOUND BOTH HEAT EXCHANGERS CRACKED AT OUTBOARD FLANGE REPLACED BOTH HEAT EXCHANGERS 2L72 4F RTA16WE 20030610000892003061000089NM 2003 6 10 DL73S030431 120030506A2120 VALVE BOEING737 737232 1384475NM E&E BAY STUCK A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27304DL 23076 IR: 20KFT CABIN ALTITUDE HORN WENT OFF.CBN ALT AT 11 KFT. STARTED DESCENT SWITCHED TO STBY CBN WOULD NOT PRESS. MANUAL MODE ALSO INOP. REPLACED E & E COOLING EXHAUST VALVE. ALSO FOUND LEFT ENGINE 450 DEG THERMOSTAT SENSE LINE BACKED OFF. TIGHTENED SAME,RAN ENGINES ACFT PRESSURIZED TO 5 PSID. 2L72 4F RTA16WE 20030610000912003061000091NM 2003 6 10 DL733030434 120030507A53306545767129 SKIN BOEING737 737347 1384647NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO272310 23596 FUSELAGE / SKIN / DENTING AND CREASE AT STA 380 BETWEEN STRINGERS 17L AND 18L. DENTED AND CREASED SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 384851-14. 2L72 4F RTA16WE 20030610000962003061000096NM 2003 6 10 DLM90030441 120030507A275008BHG36ABJF733 TRANSMITTER DOUG MD90 MD9030 3023690NM ELEVATOR CORRODED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27902DA 53382 PYLON FLAP FAULT EOAP MESSAGE ILLUMINATED AT 100KTS ON TAKEOFF ROLL. AIRCRAFT TAKEOFF REJECTED AND RETURNED TO BLOCK AT GATE C-10. FOUND LEFT ELEVATOR POSITION SENSOR OUT OF RIG AND CAUSING INTERMITTENT ILLUMINATION OF PYLON FLAP FAULT. REPLACED SENSOR PER AMM. PERFORMED ADJ/TEST AND RETURN TO SERVICE TESTS. ALL CHECKED GOOD. OK FOR SERVICE. 2L72 4F RTA6WE 20030610001002003061000100NM 2003 6 10 DL76S030453 120030509A2751 INDICATOR BOEING767 767332 1382001NM TE FLAPS INOPERATIVE A DALAO OTHER J WARNING INDICATION CRCRUISE 1 SO27133DN 24982 AT FL350 FLAP INDICATOR NEEDLES JUMPED TO .5 DEG AND FLUCTUATED TO 0 AND BACK L/E ASSY LIGHT AND MESSAGE. BIT PSEU/FSEU FAULTS NBR 11 I/B SLAT SENSOR..301.. CKD GAPS AND SENSORS W/ELDEC CKS GOOD. RESET PSEU AND OP FLAPS SEV TIMES. NO FAULTS. REPLACED FSEU MM OK FOR SERVICE. 2L72 4F RTA1NM 20030515001172003051500117SO 2003 5 15 SWIA200311931 120030429A3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07250YV 120250 GEAR RETRACTION NORMAL. IN FLIGHT THE B-DISAGREEMENT LIGHTS ILLUMINATED FOR ABOUT 15 SECONDS. UPON GEAR EXTENSION, THE LEFT AND NOSE GEAR EXTENDED NORMALLY, THE RIGHT GEAR REQUIRED ABOUT 7 SECONDS BEFORE THE DISAGREEMENT LIGHT EXTINGUISHED. REPLACED RIGHT MAIN GEAR INBOARD DOOR SEQUENCE VALVE. OPS CHECK, LEAK CHECK GOOD, GEAR SWING GOOD. 2L72 4T4 TRTA31SO E20NE 20030515001282003051500128NM 2003 5 15 AWXA200300537 120030424A5330507945164 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND AT FASTENER HOLE ON L-1 DOOR UPPER INNER SKIN BS 339, STR 9 LT. MAINTENANCE CUTOUT DAMAGE ON L-1 DOOR UPPER INNER SKIN BS 339, STR 9 LT; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, PG 1-3 FIG 1. 2L72 4F RTA16WE 20030515001672003051500167NM 2003 5 15 AWXA200300485 120030421A531465621258 KEELBEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON KEEL BEAM LOWER ANGLE IN RT AIR CONDITIONING BAY, BS 540. MAINTENANCE REMOVED 2 EACH ANGLE SUPPORTS FOR ACCESS AND FOUND CORROSION INDICATIONS IN ALL SIX HOLES; REAMED OUT HOLES AND PERFORMED HFEC INSPECTION, 5 HOLES, NO CRACK INDICATION. CRACK FOUND IN AFT HOLE OF HORIZONTAL FLANGE; CUT OUT CRACKED AREA ON KEEL BEAM LOWER ANGLE; PERFORMED ANOTHER HFEC INSPECTION, NO CRACK NOTED. FABRICATED A REPAIR ANGLE, FILLER, STRAP, AND SHIMS; INSTALLED REPAIR PARTS IAW AWA ER 15-5313-03119-SS1. 2L72 4F RTA16WE 20030515001762003051500176EU 2003 5 15 AWXA200300495 120030427A5315D5347217220290 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, AT AFT SIDE OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7, SRM 51-76-11 PG 9-10 FIG 4. 2L72 4F RTA28NM 20030515001772003051500177NM 2003 5 15 AWXA200300520 120030510A3350321430 BATTERY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1350 DURING INSPECTION THE AFT CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK ON EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM TASK 33-51-58-000-001, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030520000392003052000039NM 2003 5 20 AALA20030398 120030401A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21784AN 29588 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SEAT LIGHT AT 2D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT 2D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030520000632003052000063WP 2003 5 20 AMTA200300477 120030325A5347 CARGO TRACK LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 C-3 CARGO COMPARTMENT TRACK CORRODED, 53 FUSELAGE 10 MAIN FRAME. REPAIRED C-3 TRACK AS PER SRM 53-24-00 AND ALODINED PRIMED AND PAINTED AREA AS PER SRM 51-21-02. (M) 2L73 4F A23WE 20030520000852003052000085NM 2003 5 20 AMTA200300220 120030214A3350 LIGHT BOEING737 73783N 13844HINM CABIN DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11314TZ 30640 AFT LEFT SECTION OF EGRESS TRACK DAMAGED APPROX 1 FOOT LONG. CLEANED EGRESS TRACK. TRACK OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20030520001162003052000116WP 2003 5 20 GTIA030267 120030409A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 FTW - FOUND FORWARD CABIN RIGHT SIDE STATION 200 TO STATION 256, FLOOR PANEL SOFT/MUSHEY DETERIORATED INSERTS CORRODED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030521000262003052100026WP 2003 5 21 DHL2003801067 120030503A2697 CONNECTOR DOUG DC8 DC873F 302199FWP RT WING LOOSE A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01801DH78807 46033 RT WING NR 3 ENG FIRE EXT BOTTLE SQUIB CARTRIDGE (POS NR 5) ELECT CONNECTION HAS LOOSE PINS. REMOVED AND REPLACED ELECT CONNECTOR FROM NR 3 ENG FIRE EXT BOTTLE SQUIB CARTRIDGE (POS NR 5) IAW MM 20-50-1 PG 213. SEE J/C 8-26-20-003 FOR OPS CK. 2L74 4F RT4A25 20030521000292003052100029WP 2003 5 21 DHL2003804890 120030215A57305769589505 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING - L/E UPPER SKIN CORRODED AROUND STA XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030108, ED-3214. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EODHL-30108, ED-3214. FABRICATED A REPAIR DOUBLER (7075-T6AL-0.071) AND THREE FILLERS (7075-T6AL-0.063) IAW EODHL-30108,ED-3214. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED DOUBLER AND FILLERS AT LT WING L/E UPPER SKIN WITH NEW FASTENERS IAW EODHL-30108, ED-3214, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030610000592003061000059WP 2003 6 10 ZW0A0305101 120030525A335058222 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ZW0AO OTHER O OTHER CRCRUISE 1 CE13919TW 49368 THE EGRESS LIGHTS AT THE OVERWING EMERGENCY EXITS, CAME ON IN FLIGHT WITH THE SWITCH IN ARM POSITION. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-28-03 STL. 2L72 4F A6WE 20030610000602003061000060SO 2003 6 10 C2XA03IA053 120030511A335020131A BATTERY EMB 145 EMB145 3260210SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713964 145123 DURING SCHEDULED MAINTENANCE THE AFT AISLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030610000642003061000064NE 2003 6 10 DLM88030401 220030429A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 LEAKING A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27912DL25959 49543 726916 PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL QTY..WIND- MILL TIME 15 MIN...MIN OIL PRESS 8 PSI...MAX OIL TEMP 162- FOR LESS THAN 5 MIN. REPLACED NR 1 ENGINE PER TRANSMITTAL 9T102 ... 2L72 4F4 FRTA6WE E9NE 20030610000752003061000075NM 2003 6 10 DLM88030416 120030502A3350 BATTERY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27968DL 53161 SEAT 22ED EMERGENCY LIGHT INOP. REPLACED BATTERY PACK ASSY. 2L72 4F RTA6WE 20030610000782003061000078NM 2003 6 10 DLM88030419 120030504A33506011779 BATTERY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27994DL 53346 OVERWING EMERGENCY LTS COME ON WHEN COCKPIT EMERGENCY LIGHT SWITCH IS PLACED IN THE OFF POSITION. REPLACED OVERWING EMERGENCY LIGHT BATTERY RACK. OPS NML. 2L72 4F RTA6WE 20030610000832003061000083NM 2003 6 10 DL757030424 120030503A5330146N33705 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27613DL 22820 THE FUSELAGE SKIN AND UNDERLYING BEAR STRAP WERE FOUND DENTED AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT FS 1380 BETWEEN STRINGERS 22R & 23R. THE DAMAGE WAS REMOVED WITH A TRIMOUT AT THE DOOR EDGE. THE TRIMOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384808-14, REV A. 2L72 4F RTA2NM 20030610000972003061000097NM 2003 6 10 DL73G030444 120030508A331010604506 RELAY BOEING737 737330 13844BJNM COCKPIT FAILED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27242DL 23834 ABORTED TAKEOFF AT 90 KTS. WHEN APPROX. 40 LIGHTS ANUNNICATED ON OVERHEAD PANEL AND CONSOLE. FOUND ALL LIGHTS ILLUMINATED COMMON TO MASTER CAUTION SECT. A. RECYCLED MASTER TEST SW. LIGHTS EXTINGUISH.REPLACED MASTER TEST RELAY R33. ALL MASTER DIM AND TEST FUNCTIONS CHK GOOD PER AMM. 2L72 4F RTA16WE 20030606000212003060600021NM 2003 6 6 03FDEA00753 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B FWD BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR 2L73 4F RTA22WE 20030606000232003060600023NM 2003 6 6 03FDEA00737 120030508A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP O/B HINGE (AIRCRAFT SIDE), ACTUATOR I/B AND O/B LUG HOLES CORRODED. AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-69234 WINGS- TRAILING EDGE & TRAILING EDGE DEVICES- LH OUTBD FLAP OUTBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030606000412003060600041NM 2003 6 6 IU62003F00020 120030507A2910511532 HOUSING PNEUDRAULICS BOEING737 737200 1384453NM SHUTTLE VALVE OVERTORQUED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 675 CRACKED INSIDE THE MOUNTING HOLE. OVER-TORQUED OR OVER-PRESSURIZED. EVALUATE THE DESIGN/ MATERIAL HOUSING IS MADE FROM. 2L72 4F A16WE 20030606000502003060600050CE 2003 6 6 NE52003F00003 120030515A3710442CW PUMP CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 1 ENG VACUUM INOPERATIVE B NE5RO OTHER O OTHER NRNOT REPORTED 1 GL13596DM 61 402C0255 VACUUM PUMP INOPERATIVE. 1L72 3O3 O A7CE E8CE 20030606000512003060600051CE 2003 6 6 NE52003F00004 120030515A3710442CW PUMP CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 1 ENG VACUUM INOPERATIVE B NE5RO OTHER O OTHER NRNOT REPORTED 1 GL13596DM 42 402C0255 VACUUM PUMP INOPERATIVE. 1L72 3O3 O A7CE E8CE 20030609000502003060900050NM 2003 6 9 DHL2003747506 120030513A5311 FRAME BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING "C" CHECK IN AFT. CARGO FRAME BS 1030 HAS A DENT INTO THE RADIUS BELOW STR 26L. CUT-OUT DAMAGE AREA APROX 1 INCH FRAME 1030 STR 26 L IAW B-727 S.R.M. 51-40-3. 2) REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2. 3) 2L73 4F A3WE 20030609000622003060900062SO 2003 6 9 SWIA200311985 120030515A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07233SW8 8 120307 NUMEROUS FLOOR EMERGENCY LIGHTS (REAR ROWS) DO NOT ILLUMINATE ON TEST AND EMERGENCY LIGHT SIGNS AT ROW 9 DO NOT ILLUMINATE ON TEST.REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY IAW MM 33-00-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030610000562003061000056WP 2003 6 10 ABXA030159 120030402A53119919619503 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 MAIN FRAME AT STA 737 LEFT WAS CRACKED BETWEEN Z-ANGLE ATTACH FASTENERS. INSTALLED REPAIR DOUBLER ON FRAME STA 737 LEFT IAW DC-9 SRM 51-30-1 AND DWG 5935650. 2L72 4F A6WE 20030610000632003061000063EA 2003 6 10 COMA0360245 120030522A5610601R3303310 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01999CA12444 7230 FLIGHT 5517 DURING CRUISE FLIGHT THE RIGHT WINDSHIELD CRACKED, AIRCRAFT DIVERTED TO IAD. REPLACED THE RIGHT WINDSHIELD. 2L72 4F RTA21EA 20030611000202003061100020WP 2003 6 11 GTIA030328 120030408A5310 BEAM DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE CARGO DOORWAY CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 MID LOWER CARGO, LWR DOOR JAMB OB BEAM CORRODED. REMOVED DOOR JAMB BEAM L28R STA 598 TO 733. DRILLED AND LOCATED HOLES IN NEW BEAM, INSTALLED DOOR JAMB BEAM. 2L72 4F4 F A6WE E2EA 20030611000292003061100029WP 2003 6 11 GTIA030316 120030417A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FORWARD ENTRY DOOR HOLD OPEN PIN CUTOUT SKIN DAMAGED, REPAIRS. UPON FURTHER INSPECTION THE PAN COMMON TO THE ENTRY DOOR HOLD PIN ASSY WAS FOUND TO BE CRACKED. FABBED -13, -11 DOUBLERS, -3 PLATE. LOCATED AND DRILLED NEW PAN. INSTALLED FORWARD ENTRY DOOR HOLD OPEN PIN ASSY AND REPAIR PARTS NOTED IN STEP NR 1. 2L72 4F4 F A6WE E2EA 20030611000332003061100033 2003 6 11 MEX2003161 420030506A34604034241974 COMPUTER DOUG MD80 MD83 3023681NM COCKPIT FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23XASWW 49848 THE DIGITAL FLIGHT GUIDANCE COMPUTER DFGC FAILED DUE TO THE MACH SPEED INDICATOR DOES NOT APPEAR AND ALTITUDE HOLD INDICATOR WAS AFFECTED. THE DFGC WAS DEFERRED BY MEL 22-15. DURING OVERNIGHT SERVICE THE DFGC WAS REPLACED IAW MM 22-01-01 AND WIRING WAS VERIFIED IAW WDM 22-16-11, TEST CORRECT. 2L72 4F RT 20030611000422003061100042NM 2003 6 11 EVAE092014 120030525A3233 ACTUATOR BOEING747 74745E 1384947NM MLG LEAKING W QOCFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP0316462 27173 CAPTAIN REPORT: (GEAR TILT) MESSAGE,LANDING GEAR CANNOT RETRACT,AIRCRAFT AIR TURN BACK TO TPE. MAINTENANCE CHECK, FOUND THE HYDRAULIC TUBE OF RIGHT BODY GEAR TRUCK POSITION ACTUATOR LEAKING AND HYDRAULIC FUSE ACTIVED. REPLACED THE HYDRAULIC TUBE AND LEAK CHECK NORMAL. 2L74 4F RTA20WE 20030611000472003061100047NE 2003 6 11 CA030428003 220030427A7261LK58367 OIL CAP LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE NR 3 ENGINE LEAKING W O OTHER K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) DURING ENGINE START NR 3 ENGINE OIL CAP WAS LEAKING FROM THE CENTER. OIL CAP WAS REPLACED AND SYSTEM CHECKED SERVICEABLE. 2L73 4F4 F A23WE E12EU 20030611000732003061100073NE 2003 6 11 HEEA086558 120030522A32437025001004101 VALVE SKRSKYS76 S76A 8143006NE BRAKE SYS LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW031546G 760076 BRAKE VALVE LEAKING. 1G72 3U H1NE 20030611000802003061100080NE 2003 6 11 HEEA086565 120030522A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 FIBERGLASS SEPERATED NEAR THE AFT END OF THE DOUBLER. 1G72 3U H1NE 20030611000872003061100087SW 2003 6 11 HEEA086695 120030522A6230412010405109 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214983697 36003 MAIN ROTOR MAST LINK HAS BEARING WEAR. SHOP REPAIR. 1G72 4U H4SW 20030611000972003061100097 2003 6 11 HEEA086705 420030522A2330 SWITCH BELL 412 412 1182202SW SIREN BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 1292 33112 POWER SWITCH BROKEN OFF. EXT/INT SWITCH BENT. FOUND SWITCHES S401, S402 AND FUSE F101 BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030611001032003061100103EU 2003 6 11 I05R086499 120030512A3040B391571227 SPLINE ADAPTER UROCOPEC135 EC135P1 8680990EU WIPER ARM SHEARED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05551BA700 188 WINDSHIELD WIPER SPLINES SHEARED, REPLACED WIPER ARM ASSY. 1G72 3U O H88EU 20030611001102003061100110EU 2003 6 11 HEEA086714 120030521A642011731822 BEARING BOLKMS117 BK117A1 5626010EU PITCH LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911TL 7198 PITCH LINK ASSY HAS WORN BEARINGS. REPLACED 2 EACH 11-3943P BEARINGS DUE TO WORN AND 2 EACH 11-6488P BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H13EU 20030609001182003060900118NE 2003 6 9 00092 220030521A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05324TW 24D324 251718A AIRCRAFT INROUTE FROM MNM TO RWI CLIMBING TO FL450 INCOUNTERED LIGHT TURBULANCE, SPEED DECREASED BELOW .72 LT ENGINE FLAMED OUT. NO EMERGENCY WAS DECLARED REQUESTED LOWER FOR RELIGHT, ENGINE RELIGHT AND CLIMB BACK TO FL410. AIRCRAFT CONTINUED TO DESTINATION,, INSPECTION FOR FOD DAMAGE AND LEAKS PERFORMED, NO DEFECTS NOTED AT THIS TIME. 2L72 4J4 J A10CE 1E16 20030609001452003060900145EA 2003 6 9 SWIA200312002 120030520A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07932SW1281 1281 7714 STAB TRIM CH 1 INOP STATUS IN FLIGHT. RESET PER QRH.MDC CODE INDICATED HTSCU FAILED. REPLACED HSTCU PER MM 27-41-01. OPS CHECK GOOD OF STAB TRIM SYSTEM. 2L72 4F RTA21EA 20030609001482003060900148SO 2003 6 9 C2XA03SH152 120030525A531014529150003 CROSSBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE LOWER CROSSBEAM ANGLE FROM THE CENTER BEAM TO THE RIGHT HAND BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030609001612003060900161EU 2003 6 9 CA030405001 120030401A63204638302023 BEARING BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL M/R GEARBOX SPALLED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) GEARBOX RECEIVED FROM A CUSTOMER IN THE USA. RT INPUT SPLIT INNER RACE BEARING PEELING/SPALLING. METAL CONTAMINATION CAUSED DAMAGE TO OTHER INTERNAL BEARINGS. 1G72 3U3 UNCH3EU E4CE 20030609001962003060900196CE 2003 6 9 CA030521002 120030508A55201016100191 TORQUE TUBE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA ELEVATOR CORRODED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING A SCHEDULED INSPECTION, CORROSION WAS DETECTED ON THE LT ELEVATOR TORQUE TUBE. THE PAINT WAS LIFTED IN THE AREA ADJACENT TO THE LOWER AFT MOUNTING BOLT. A POWDER COATING AND MINOR FLACKING WAS EVIDENT. CLOSER INSPECTION AND CLEANING DETERMINED THAT THE TUBE SHOULD BE REPLACED. A FLEET CAMPAIGN WAS INITIATED TO INSPECT ALL OTHER TORQUE TUBES IN THE SYSTEM. 1L72 4T4 T A24CE E4EA 20030609002002003060900200 2003 6 9 HEEA086573 420030522A34578143902240B GPS SKRSKYS76 S76A 8143006NE COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 GPS FAILED IN FLIGHT. UNABLE TO ACQUIRE SIGNALS. SHOP REPAIR. 1G72 3U H1NE 20030610000102003061000010WP 2003 6 10 MWEA030230 120030527A53119912243241 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 AFT CARGO COMPARTMENT FRAME AT STATION 1309 HAS AREA OF CORROSION ON AFT AND LOWER SIDES BETWEEN LONGERON 29 LEFT AND 29 RIGHT. -- FABRICATED AND INSTALLED ALL REPAIR PARTS. 2L72 4F A6WE 20030611000412003061100041NE 2003 6 11 MEX2003174 220030513A7200 ENGINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23801AM 25624 AIRCRAFT RETURN TO PLATFORM DUE TO NR 1 ENGINE DID NOT START. STARTER VALVE WAS CHECKED AND IGNITION WAS CORRECT. TESTS PERFORMED IAW MM 74-21-0. AFTER THIS CHECK LEFT ENGINE STARTING WAS CORRECT IAW MM 80-10-00. 2L72 4F4 FRTA2NM E17NE 20030611000572003061100057EA 2003 6 11 CA030514018 120030425A783022850741115 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE THRUST REVERSER OUT OF ADJUST W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA (CAN) (L REV UNLOCK) WARNING MESSAGE POSTED WHILE IN CRUISE. AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. FOLLOWING READJUSTMENT OF THE THRUST REVERSER STOW SWITCH, THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030611000652003061100065NM 2003 6 11 CA030516003 120030516A323282970018009 CYLINDER MESSIER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF* NE DOOR ACTUATOR CORRODED W K NONE K FLUID LOSS ININSP/MAINT 1 CA 3916639166 0166 (CAN) FOUND TO BE LEAKING. PART OVERHAULED AND CYLINDER ASSY. REPLACED S.B.8-32-109 AND 8-32-84 ACCOMPLISHED. CHANGED P/N TO -013 FROM -009 CYLINDER ASSY FOUND CORRODED AND WORN. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030611001132003061100113EU 2003 6 11 HEEA086717 120030521A243651565000R VOLT REGULATOR BOLKMS105 BO105S 5626006EU VOLT REGULATOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 VOLTAGE REGULATOR PRODUCING UNCONTROLLED VOLTAGE. SENT FOR INSPECTION AND REPAIR. 1G72 3U H3EU 20030611001382003061100138EA 2003 6 11 ASOA03198 120030507A3350YAD4F RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11716EV 10084 FLT 4712 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS WHEN THE SWITCH WAS IN THE ARMED POSITION, TURNED ON AND OFF INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS RELAY AT JUNCTION BOX ELEVEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030611001442003061100144EA 2003 6 11 2003F00365 120030323A26136007300 SENSOR CNDAIRCL600 CL6002C10 1390015EA BRAKE OVERHEAT MALFUNCTIONED A FDKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07503MJ 10058 FLT 6574 - PHX-ABQ, AFTER TAKEOFF, PILOT RECEIVED A MASTER WARNING BRAKE OVERHEAT FOR THE RIGHT INBOARD BRAKE. PILOT FOLLOWED CFM PROCEDURES TO EXTINGUISH THE WARNING MESSAGE TO NO AVAIL. RETURNED TO PHX WITH NO PROBLEMS. MAINTENANCE FOUND THE NR 3 BRAKE TEMP SENSOR AT FAULT AND CHANGED IT. AIRCRAFT CONTINUED ITS FLIGHT WITH NO FURTHER DIFFICULTIES. (M) 2L72 4F RTA21EA 20030611001472003061100147EA 2003 6 11 2003F00368 120030202A5220 DOOR CNDAIRCL600 CL6002C10 1390015EA ESCAPE DOOR UNSECURE A FDKAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07507MJ 10077 FRL - FLT 6624 - PHX-ELP - CREW REPORTED RIGHT EMERGENCY EXIT CAUTION MESSAGE ON DOOR PAGE. MAINTENANCE REINSTALLED DOOR NO FURTHER DEFECTS WERE NOTED A/C RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030611001502003061100150NM 2003 6 11 2003F00371 120030402A2611A7251 SMOKE DETECTOR DOUG MD88 MD88 3023688NM LAVATORY WILL NOT TEST A A4JAK NONE O OTHER ININSP/MAINT 1 SO3512FQ 49766 DURING A-CHECK, FOUND RIGHT AFT LAVATORY SMOKE DETECTOR DOES NOT TEST. REPLACED RIGHT AFT LAVATORY SMOKE DETECTOR IAW MM 26-14-00. CHECK NORMAL. (M) 2L72 4F RTA6WE 20030611001522003061100152EA 2003 6 11 ASOA03202 120030509A335017563 BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 FLT 4726 - DURING A GROUND INSPECTION IN MSY, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MAIN AIRCRAFT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030611001572003061100157WP 2003 6 11 0301039995 120030523A27805919526508 DUCT DOUG DC9 DC931 3022065WP SLATS DAMAGED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL018978E 47327 WHEN SLATS WERE SELECTED AT APPROXIMATELY 220 KTS, THE AIRCRAFT ROLLED TO THE RIGHT. THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE AND THE AMBER SLAT DISAGREEMENT LIGHT DID NOT EXTINGUISH. AS FLIGHT CREW INITIATED COM PROCEDURES AND THE AIRCRAFT SLOWED TO 175 KTS THE SLAT EXTEND DID ILLUMINATE AND THE SLAT DISAGREEMENT WENT OUT. THE LANDING AT MSP WAS NORMAL AND UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT T-DUCT AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F A6WE 20030612000022003061200002EA 2003 6 12 SWIA200312010 120030524A3234750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07941SW 7750 GEAR DOWN DISAGREE ON APPROACH - LEFT MAIN GEAR. PERFORMED QRH PROCEDURE, LEFT MAIN GEAR EXTENDED NORMALLY. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE WITH SERVICEABLE UNIT IAW CRJ MM 32-32-10. LEAK CHECK AND OPS CHECK GOOD. 2L72 4F RTA21EA 20030612000032003061200003 2003 6 12 SWIA200312011 420030519A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07197SW1352813528 120186 BOTH AUTPILOTS TURN RIGHT, UNCOMMANDED, DO NOT FOLLOW COMMAND BARS. REPLACED APP-65. OPS CHECK GOOD IAW AMM 22-00-00. 2L72 4T RTA31SO 20030612000282003061200028EA 2003 6 12 COMA0370016 120030523A3234533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01340CA1583 10062 FLIGHT 5207 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20030612000292003061200029EA 2003 6 12 COMA0370017 120030526A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01379CA126 10102 FLIGHT 5812 FORWARD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY BATTERY. 2L72 4F RTA21EA 20030612000332003061200033EA 2003 6 12 SWIA200312025 120030417A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 FS 625.3 RIGHT ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED FS 625.3 ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F RTA21EA 20030612000372003061200037EA 2003 6 12 SWIA200312029 120030521A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL ANGLE IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-52 2L72 4F RTA21EA 20030612000382003061200038EA 2003 6 12 SWIA200312030 120030521A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 FS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV. ''A''. REPAIR ANGLE P/N: 601R-53-61-117-3 2L72 4F RTA21EA 20030612000392003061200039NM 2003 6 12 CALA0300268 120030528A5320 ATTACH ANGLE BOEING737 737524 1384721NM DOORWAY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714639 28900 INSPECTION FOUND Z-ATTACH ANGLE CORRODED AT L-2 DOOR ENTRYWAY. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030612000422003061200042EU 2003 6 12 MALA030283 120030526A2560 ESCAPE ROPE BAC 146 AVRO146RJ85A1500097EU COCKPIT LOOSE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15534XJ E2370 DURING FLIGHT 3645, ESCAPE ROPE PANEL KEEPS FALLING DOWN. MAINTENANCE APPLIED NEW HOOK AND LOOP TO THE AFFECTED AREA AS NEEDED SEC CHECKS GOOD. 2H74 4F RTA49EU 20030612000522003061200052WP 2003 6 12 ABXA030175 120030430A541249125392 FITTING DOUG DC9 DC932 3022066WP PYLON BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 AFT LOWER INBOARD FITTING CRACKED FS 965 PYLON BULKHEAD RIGHT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20030612000692003061200069SO 2003 6 12 C2XA03BT063 120030529A2611 SMOKE DETECTOR EMB 145 EMB145ER 3260211SO CARGO BAY MALFUNCTIONED A C2XAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2714925 145004 CREW REPORTED, DECLARED EMERGENCY FOR BAGGAGE AREA SMOKE WARNING IN FLIGHT, DIVERTED TO RDU, FIRE EXTINGUISHER BLOWN. MAINTENANCE DISPATCHED TO AIRCRAFT, INSPECTED AND FOUND NO EVIDENCE OF SMOKE. PLACED BAGGAGE SMOKE DETECTOR AND BAGGAGE FIRE EXTINGUISHER ON MEL. REMOVED AND REPLACED NR 1 AND 2 BAGGAGE SMOKE DETECTORS (P/N: 473597-13) OPS.CHECKED GOOD IAW EMB145 MM 26-23-00 AND REMOVED AND REPLACED NR 1 AND 2 FIRE BOTTLES FOR BAGGAGE COMPARTMENT (P/N:33700027-1) IAW EMB145 MM 26-23-01. BOTH MEL'S CLEARED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030612000732003061200073NM 2003 6 12 UPS03440716 120030511A5320141U109212 CLIP BOEING747 747200 1384847NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, NWW TUNNEL - RT BS 300 VERTICAL BEAM 3RD STIFFENER CLIP FOUND CRACKED (COUNT FROM TOP). CLIP REPLACED AS PER SRM 51-10-01 PAGE 8 AND AN AREA PAINT TOUCHED UP PER MM 51-24-11. 2L74 4F RTA20WE 20030612000832003061200083WP 2003 6 12 UPS03840706 120030521A53404750419501N FITTING DOUG DC8 DC871F 302199DWP FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1160 LONG 18R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612000852003061200085WP 2003 6 12 UPS03840708 120030520A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, AT STATION 1730 CANTED FRAME LONGERON 14L IS CRACKED. REMOVED LONGERON SECTION STATION 1710-1760, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20030612000962003061200096NM 2003 6 12 CALA0300271 120030530A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND A 2 INCH CRACK IN PRESSURE DECK WEB AT STA 663.75 IN RT WHEEL WELL JUST O/B OF J-BOX. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, PAGE 214-221. 2L72 4F RTA16WE 20030612000992003061200099NM 2003 6 12 CALA0300274 120030530A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 312, RBL 38 TO LBL 20. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2L72 4F RTA16WE 20030612001062003061200106WP 2003 6 12 ZW0A0305301 120030529A49903812761 APU DOUG DC9 DC983 3022083WP APU BAY LEAKING A ZW0AO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE139403W 53139 CREW REPORTED HAZE IN CABIN AND HAD ODOR, MOST NOTICEABLE ON THE GROUND. REPLACED THE APU DUE TO INTERNAL OIL LEAK. CHECK-C 9-11-02 STL. 2L72 4F RTA6WE 20030612001242003061200124NM 2003 6 12 UPS03440768 120030510A5312 BULKHEAD BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C, FX - STA 1480 PRESSURE BULKHEAD LEFT O/B LOWER WEB FOUND CRACKED AT LBL 90 TO LBL 92 HI-LOK AREA. FX STA 1480 PRESSURE BULKHEAD LEFT O/B LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1 JUST AT LBL 90 TO LBL 92. 2L74 4F RTA20WE 20030610000682003061000068NM 2003 6 10 DL73S030409 120030430A5330654577416 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 THE FUSELAGE SKIN WAS FOUNE WITH A 2 INCH CRACK RUNNING ALONG THE BONDED WAFFLE DOUBLER EDGE AT STRINGER 17L AND FS 790. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384984-14. 2L72 4F RTA16WE 20030610000872003061000087NM 2003 6 10 DL757030428 120030503A5310143N85119 FRAME BOEING757 757232 1384965NM FS 560, S-22R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27604DL 22811 THE INNER STRUCTURE AND WEB OF THE C1 DOOR CUTOUT FWD FRAME AT FS 560 WERE FOUND CRACKED BETWEEN STRINGERS 21R & 22R. THE CRACKS ARE TYPICAL OF AD 2002-24-02 AND BAC S/B 757-53A0080.THE OUTER CHORD WAS DAMAGED DURING THE REPAIR. ALL CRACKS AND DAMAGES WERE TRIMMED OUT. THE CHORDS WERE REPAIRED WITH ALUMINUM REPAIR ANGLES AND THE WEB WITH A DOUBLER. THEREPAIRS WERE ACCOMPLISHED PER ER/S 384900-14AD. 2L72 4F RTA2NM 20030611000312003061100031WP 2003 6 11 GTIA030314 120030429A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CABIN DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FORWARD LAV ENTRY STA 256 FLOOR PANEL DELAMINATED. REMOVED FLOOR PANEL. FABBED FLOOR PANEL. INSTALLED NEW FLOOR PANEL. 2L72 4F4 F A6WE E2EA 20030612000062003061200006EA 2003 6 12 SWIA200312014 120030526A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07443SW 7638 RT WING FORWARD EMERGENCY LIGHT INOP. REPLACED BULB PER CRJ MM 33-51-21. OPS CHECK GOOD. 2L72 4F RTA21EA 20030612000182003061200018SO 2003 6 12 C2XA03SH162 120030528A531514521700003 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO HAVE CORROSION AT RAMP SUPPORT ANGLE BETWEEN FRAMES 19 AND 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR ON AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030612000212003061200021NM 2003 6 12 P5CA0300882 120030528A5312 BULKHEAD BOEING747 7472U3B 1384846NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CRACK FOUND ON 1480 LWR BULKHEAD RT SIDE. REPAIRED PER S/B 53-2390. 2L74 4F RTA20WE 20030612000672003061200067 2003 6 12 ABXA030182 420030528A221025866878 COMPUTER DOUG DC9 DC931 3022065WP AUTOPILOT DEFECTIVE A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23948AX975 47065 AUTOPILOT ROLLED INTO A 30 DEGREES LEFT BANK UNCOMMANDED. REPLACED THE ROLL AXIS COMPUTER. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 22-10-00. 2L72 4F A6WE 20030612000752003061200075NM 2003 6 12 UPS03440719 120030515A5540 BULKHEAD BOEING747 747200 1384847NM RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, UPPER RUDDER ASSY LWR BHD INTERIOR WEB SKIN CRACKED TWO LOCATIONS AT RED MARKED. UPPER RUDDER ASSY LOWER BULKHEAD WEB INT SKIN WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F RTA20WE 20030612001002003061200100NM 2003 6 12 CALA0300275 120030530A5530 ANGLE BOEING737 737524 1384721NM VERTICAL STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719638 28899 INSPECTION FOUND L-ANGLE AT LT VERTICAL STABILIZER BOTTOM INSIDE PANEL 9507 GOUGED. THE GOUGED SECTION OF L-ANGLE WAS REMOVED AND REPLACED IAW ECRA 5380-01013. 2L72 4F RTA16WE 20030612001132003061200113NM 2003 6 12 UPS03240751 120030519A5330 SKIN BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C SUSPECT CRACK AT FWD ENTRY DOOR CUTOUT AT FWD UPPER CORNER AS MARKED. HFEC INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460-D. REPAIR AT FWD ENTRY DOOR REPAINTED IAW MM 51-20-91. 2L73 4F A3WE 20030612001192003061200119NM 2003 6 12 UPS03440763 120030522A52807075T60050IN SKIN BOEING747 747200 1384847NM MLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, LT BODY MLG WW - BODY MLG I/B STRUT DOOR EXTERNAL SURFACE SKIN FOUND CRACKED AT REAR UPPER CORNER. SKIN REPAIRED AS PER SRM 52-80-02 FIG 1. 2L74 4F RTA20WE 20030612001372003061200137WP 2003 6 12 UPS03840725 120030505A53403649114U ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, MAIN CABIN CORRODED FITTING CENTER WING BOX TO SHEAR WEB ATTACH FITTING STA 920 RBL 66 APX. REMOVED AND REPLACED FITTING AND INSTALLED IAW DC8 SRM 51-3-2 AND 51-1-20D. 2L74 4F RT4A25 20030612001382003061200138WP 2003 6 12 UPS03840726 120030514A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, MAIN CABIN FLOORBEAM T-CAP FOUND BLENDED ON FROM AN EXISTING REPAIR STA 1620 LBL 48. FABBED REPAIR ANGLE IAW DC8 SRM 53-2-0 FIG 1B. ALODINED & PRIMED ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030612001472003061200147WP 2003 6 12 UPS03840736 120030503A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, L2 LWR FWD DOOR JAMB CORNER, DOOR PAN AND DOOR SEAL CRACKED. REMOVED SEAL DEPRESSOR, DOOR PAN. FABBED REPAIR DOUBLER FOR DRAINPAN AND FABBED NEW SEAL DEPRESSOR. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20030612001542003061200154WP 2003 6 12 UPS03840743 120030519A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, AFT PIT FS 1127 AT RBL 49 LOWER FLANGE OF SEAT TRACK IS CRACKED. REMOVED DAMAGED SEAT TRACK. REC'D NEW SEAT TRACK, DRILLED IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030612001582003061200158WP 2003 6 12 UPS03840756 120030521A53404611159501N FITTING DOUG DC8 DC871F 302199DWP A/C BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C1 A/C BAY STA 70 LONG FRAME FITTING 34L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611159 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612001642003061200164WP 2003 6 12 UPS03840780 120030520A5240 ANGLE DOUG DC8 DC871F 302199DWP R-1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, 1 INCH CRACK ON ANGLE DOUBLER INNER FRAME OF R-1 DOOR AT STA 160 LONG 15R-17R ON DOOR. REMOVED, FABRICATED AND INSTALLED ANGLE DOUBLER IAW DWG 5615762, AND SRM 51-1-21, 51-1-21A, 51-3-0. 2L74 4F RT4A25 20030612001672003061200167EA 2003 6 12 SWIA200312040 120030526A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM DIRTY A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07589SW 7072 DURING FIRST FLIGHT OF DAY CHECKS, F/O'S NOSE DOWN STAB TRIM INOP USING CH1 AND CH2. CLEANED F/O YOKE SWITCH. OPS CHECKS GOOD PER MM 27-41-05. 2L72 4F RTA21EA 20030612001682003061200168EA 2003 6 12 SWIA200312041 120030415A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 625 LEFT INTERCOSTAL ANGLE STRINGER 146 CRACKED. REPLACED ANGLE IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20030612001872003061200187NE 2003 6 12 2003UALA00451 220030530A7261 BEARING AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 5 LEAKING A UALAF ACTIVATE FIRE EXT. KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 WP29462UA 1272 NUMBER 1 ENGINE OIL LEAK IN FLIGHT. QUANTITY DECREASED FROM 10.5 TO 3.5. SMOKE IN TAILPIPE AND TURBINE AREA AFTER SHUTDOWN. OIL LEAK CAUSED BY OIL LEAKING FROM NR 5 BEARING COMPARTMENT INTO HOT GASPATH AREA, GENERATING SMOKE AT ENGINE SHUTDOWN. LEAK CAUSED BY EXCESSIVE OIL "COKING" DEPOSITS IN BEARING COMPARTMENT AREA. OSV HAS REVIEWED AND CORRECTED PROCESS THAT ALLOWED THIS OVERSIGHT. 2L72 4F4 FRTA28NM E40NE 20030612001932003061200193EA 2003 6 12 COMA0360250 120030529A3260 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01917CA 7017 FLIGHT 5295 GEAR DISAGREE WARNING ON APPROACH. ADJUSTED THE NLG UPLOCK ASSY. 2L72 4F RTA21EA 20030612001952003061200195EA 2003 6 12 COMA0360252 120030531A325016736105 SERVO VALVE CNDAIRCL600 CL6002B19 1900309EA NLG STEERING MALFUNCTIONED A COMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01924CA11385 7026 FLT 5501 COULD NOT MAINTAIN DIRECTIONAL CONTROL DURING T/O WITH FULL LT RUDDER AIRCRAFT PULLED TO THE RT. REPLACED THE ELECTRO HYDRAULIC SERVO VALVE. 2L72 4F RTA21EA 20030612001982003061200198EA 2003 6 12 SWIA200311993 120030507A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW 7555 FS 621 LEFT FLOORBEAM ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117 REV A. 2L72 4F4 FRTA21EA E15NE 20030612002002003061200200SO 2003 6 12 SWIA200312049 120030530A5753 BRACKET EMB 120 EMB120ER 3260203SO TE FLAPS BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07581SW 120349 LEFT OUTBOARD FLAP MOVEABLE ROLLER BRACKET BROKEN ON INBOARD SIDE. REMOVED AND REPLACED LEFT OUTBOARD FLAP MOVEABLE CHANNEL INBOARD ROLLER SUPPORT BRACKET IAW EMB SRM 51-40-02. 2L72 4T RTA31SO 20030613000052003061300005SO 2003 6 13 SWIA200312058 120030602A6120 SWITCH EMB 120 EMB120ER 3260203SO AUTOFEATHER SYS STUCK A SWIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NM07214SW 120280 PILOT REPORTS THAT RIGHT ENGINE AUTO FEATHERED ON TAKEOFF ROLL WITH LT ENGINE TQ FLUCTUATION, BUT ENGINE DID NOT FOLLOW FLUCTUATION. FOUND LEFT ENGINE AUTO FEATHER TEST SWITCH STUCK IN THE TEST POSITION. REMOVED AND REPLACED SWITCH. RAN A/C, OPS CHECKED GOOD. 2L72 4T RTA31SO 20030613000112003061300011EA 2003 6 13 SWIA200312064 120030421A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 FS 484 RT INTERCOSTAL O/B FLG RBL 3G CRACKED. DISCOVERED DURING C-CHECK. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-11-059. 2L72 4F RTA21EA 20030613000172003061300017WP 2003 6 13 ABXA030186 120030105A53135750198502 LONGERON DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 LONGERON 24 RIGHT CRACKED JUST UNDER BOTTLE BOLT IN BATH TUB AREA. ACCOMPLISHED LONGERON 24 RIGHT REPLACEMENT IAW ABX REA D853-46001-MR AND JOB CARD 90453100 (TIMCO). 2L74 4F 4A25 20030613000182003061300018WP 2003 6 13 ABXA030187 120030204A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 CLEAN, TREAT AND PRIME SKIN UNDER C4 SCUFF PLATE. CLEANED CORROSION, TREATED, PRIMED SKIN. FABRICATED AND INSTALLED FILLERS, DOUBLERS AND TRIPLERS IAW DC-8 REA D853-46013-MR, AND THE SRM. 2L74 4F 4A25 20030613000332003061300033EA 2003 6 13 COMA0360256 120030602A2420755469E IDG CNDAIRCL600 CL6002B19 1900309EA RT ENGINE FAILED A COMAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO01958CA141501373 7111 FLIGHT 5781 RT ENGINE IDG MESSAGE. REPLACED THE RT IDG. 2L72 4F RTA21EA 20030613000422003061300042EA 2003 6 13 SWIA200311998 120030514A5315 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07433SW 7550 CABLE FAIRLEAD INTERCOSTAL AT FS 484 IS CRACKED AT RBL 36. DISCOVERED DURING C-CHECK. REPAIRED INTERCOSTAL IAW CRJ REO 601R53-41-059 REV A (RII53-401). 2L72 4F4 FRTA21EA E15NE 20030613000482003061300048SO 2003 6 13 SWIA200312069 120030603A5753 FLAP TRACK EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS DAMAGED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07214SW 120280 AFTER DEPARTURE FLAPS WOULD NOT RETRACT PAST 10 DEGREES. FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING 10 DEGREES. RETURNED TO FIELD. REPLACED RIGHT OUTBOARD FLAP INNER FIXED TRACK IAW EMB MM 57-53-03. INSTALLED SERVICEABLE TRACK ON RIGHT WING, OUTBOARD FLAP AT OUTBOARD POSITION. 2L72 4T4 TRTA31SO E20NE 20030613000512003061300051NM 2003 6 13 PCAA0306076 120030603A5610NP15790113 WINDSHIELD DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA13844EX1096 339 FLIGHT 3647 FROM LGA-BTV DESCENDING THROUGH 5000 FT, CREW FIRST SMELLED SOMETHING BURNING . THEN SAW SMOKE COMING FROM WINDSHIELD HEAT TERMINALS. SELECTED HEAT OFF AND LEFT WINDSHIELD CRACKED. CREW DONNED OXYGEN MASKS, DECLARED EMERGENCY. THEN LANDED WITHOUT INCIDENT. CREW REPORTED TO MAINTENANCE THAT SMOKE CAME FROM WINDSHIELD TERMINALS. SELECTED HEAT OFF AND WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED LT WINDSHIELD, IAW M/M CHAPTER 56-10-11. CHECKED WIRE TERMINALS ENDS. GROUND RAN AIRCRAFT AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030613000542003061300054CE 2003 6 13 NSVA200300006 120030219A3310 ODOR BEECH 1900 1900C 1154161CE COCKPIT DETECTED A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27207CJ UC107 DURING FLIGHT THE LIGHTS/FLIGHT CIRCUIT BREAKER POPPED OUT. CIRCUIT BREAKER WAS RESET AND THEN POPPED AGAIN. THEN A STRONG ODOR OF ELECTRICAL DISCHARGE. THE BACKLIGHTING OF THE CAPTAIN AND CO-PILOTS INSTRUMENTS THEN WENT OUT. 2L72 4T RTA24CE 20030611000302003061100030WP 2003 6 11 GTIA030315 120030429A5321 FLOORBOARD DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CABIN DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FORWARD ENTRY STA 200 FLOOR PANEL DELAMINATED. REMOVED FLOOR PANEL. FABRICATED NEW FLOORBOARD. INSTALLED NEW FLOORBOARD. 2L72 4F4 F A6WE E2EA 20030611000482003061100048EU 2003 6 11 CA030428007 120030414A2913704A33690004 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HYD PUMP TORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION AME DISCOVERED THAT THE HYDRAULIC PUMP BELT WAS TORN (APPROXIMATELY .3333 OF THE WIDTH) AT LAP JOINT AREA. BELT REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 UNCH9EU E19EU 20030611000702003061100070NE 2003 6 11 HEEA086555 120030522A28206531703006110 VALVE SKRSKYS76 S76A 8143006NE FUEL SYS LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW034253S 760035 FUEL VALVE LEAKING. REPLACED WITH SERVICEABLE VALVE. 1G72 3U H1NE 20030611000832003061100083NE 2003 6 11 HEEA086568 120030522A24207655009005104 CONTROL UNIT SKRSKYS76 S76A 8143006NE GENERATOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 AC GENERTOR DELAYED COMING ON LINE. SENT FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030611001002003061100100SW 2003 6 11 HEEA086708 120030522A6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 TAIL ROTOR WORN BUSHINGS. REPAIRED. 1G72 4U H4SW 20030611001122003061100112EU 2003 6 11 HEEA086716 120030521A243651565000R VOLT REGULATOR BOLKMS105 BO105S 5626006EU ELECTRICAL INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 VOLTAGE REGULATOR PRODUCING UNCONTROLLED VOLTAGE. SENT FOR WARRANTY REPAIR. 1G72 3U H3EU 20030612000442003061200044WP 2003 6 12 ABXA030179 120030514A531359114279 LONGERON DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 LONGERON 17 RIGHT CRACKED BEHIND SPLICE SECTION AT FS 965 BEHIND FORWARD PYLON BULKHEAD. REPAIRED AREA IAW DC-9 SRM 53-02. 2L72 4F A6WE 20030612000512003061200051WP 2003 6 12 ABXA030174 120030430A531199196171 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 LT FORWARD MAIN FRAME FS 699 CRACKED ON FORWARD FLANGE FROM BOLT IN RADIUS. REPLACED FRAME ON JOB CARD EA 53400321-001. 2L72 4F A6WE 20030612000802003061200080WP 2003 6 12 UPS03840703 120030521A53404750418U FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1152 LONG 19R. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D. 2L74 4F RT4A25 20030613000242003061300024NM 2003 6 13 UPS03440787 120030519A5313 LONGERON BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C AFT CARGO BS 1745 S49R STRINGER SPLICE FITTING CORROSION CRACK. CORROSION BLEND OUT 0.063 X 1.5 X 4 INCH. STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030613000432003061300043EA 2003 6 13 SWIA200311999 120030514A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07433SW 7550 FS 621.00 LBL 36 FLOOR ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE AREA IAW CRJ REO 601R-53-61-117 REV A & RII53-401. 2L72 4F4 FRTA21EA E15NE 20030613000622003061300062NM 2003 6 13 UPS03440796 120030520A532065B3860034 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, AFT CARGO COMPT - BELOW FLOOR STRINGER ATT TIE CLIP FOUND CORROSION AT STA 1696 TO STA 1700 STR 48R. DUE TO COR TIE CLIP OUT OF SRM 53-10-01 FIG 1 LIMIT NEED TO BE CHANGED BLENDED AERA .75 X .5 INCH AND MAT'L REMAIN 0.020 INCH. AFT CARGO COMPT STA 1696 TO STA 1700 STRINGER S48R ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030613000762003061300076SO 2003 6 13 C2XA03SH172 120030608A532014522459003 SUPPORT ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 SHV-DURING C-CHECK THE SUPPORT ANGLE ON THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613001072003061300107 2003 6 13 SWAA031248 420030604A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030613001082003061300108NM 2003 6 13 SWAA031249 120030605A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 761, BELOW STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030613001092003061300109NM 2003 6 13 SWAA031250 120030605A27316545166 ROD END BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB ROD END ASSY'S PER MM. 2L72 4F RTA16WE 20030613001122003061300112NM 2003 6 13 SWAA031253 120030605A21307207375 VALVE BOEING737 7373L9 1384470NM CABIN PRESSURE FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29657SW 23331 AIR TURNBACK, UNABLE TO PRESSURIZE CABIN. REMOVED AND REPLACED CABIN PRESSURE RELIEF SAFETY VALVE PER MM. 2L72 4F RTA16WE 20030613001152003061300115NM 2003 6 13 SWAA031256 120030605A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030613001362003061300136NM 2003 6 13 SWAA031242 120030603A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 540, STR 4R AND STR 10R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030613001382003061300138NM 2003 6 13 SWAA031244 120030603A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AT ROW NR 8. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030613001512003061300151NM 2003 6 13 SWAA031232 120030603A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030617000132003061700013NM 2003 6 17 CA030527002 120030523A79301163P181 BYPASS VALVE BOEING737 737275 1384485NM PWA JT8 JT8D9A 52048NE NR 1 ENG OIL MALFUNCTIONED W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 1206 (CAN) ON TOP OF CLIMB NR 1 ENGINE OIL FILTER BY-PASS CAME ON STEADY. CHECK LIST WAS PERFORMED AND LIGHT REMAINED ON. ENGINE SHUT DOWN HAD TO BE COMPLETED AS PER QRH, AIRCRAFT RETURNED TO TORONTO. 2L72 4F4 F A16WE E2EA 20030617000142003061700014EU 2003 6 17 AUS20030478 120030414A67201054537110 BEARING BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101750B1 41560NE TAIL ROTOR FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LONGITUDINAL CONTROL SYSTEM ROD END BEARING TEFLON LINER FAULTY. 1G72 3U3 UNCH13EU E5NE10 20030617000202003061700020GL 2003 6 17 CA030527009 220030503A7321 SHAFT BENDIX BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL FUEL CONTROL SHEARED W O OTHER W INADEQUATE Q C DEDESCENT 1 CA 322475 (CAN) ONE MINUTE AFTER TAKEOFF DURING A FLIGHT TEST FOR COMPRESSOR STALL, THE NR 2 ENGINE OVER SPEED. THE AIRCRAFT FLEW BACK TO BASE IMMEDIATELY WITH NO FURTHER INCIDENT. THE ENGINE WAS REMOVED FROM THE AIRCRAFT. WHEN THE FCU WAS REMOVED IT WAS NOTICED THAT THE SHAFT WAS SHEARED. IT WAS ALSO FOUND THAT ONE WASHER BETWEEN FCU & GEARBOX WAS NOT INSTALLED. THIS MAY HAVE LED TO THE FCU SHAFT SHEARING. A NEW FCU WAS INSTALLED AND THE ENGINE RAN NORMALLY. 1G72 3U3 U H3EU E4CE 20030611001482003061100148EA 2003 6 11 2003F00369 120030319A2840 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA FUEL PUMP ILLUMINATED A FDKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07508MJ 10087 FRL - FLT 6633 - PHX - AIRCRAFT RETURNED TO FIELD FOR FUEL PUMP CAUTION MESSAGE. MAINTENANCE RESET THE SYSTEM. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030612000162003061200016SO 2003 6 12 C2XA03SH160 120030528A523014529610003 STOP EMB 145 EMB145ER 3260211SO CARGO DOOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE CARGO DOOR STOP LIP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED STOP IAW EMB 145 SRM 52-30-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030521000312003052100031WP 2003 5 21 DHL2003804894 120030207A5553 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 VERT STAB AND RT FUSE- ATTACHING ANGLE CORRODED BETWEEN STA 1766.000 - STA 1800.382 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 PG 44A-44B, FIG 16A. REMOVED CORROSION ON ANGLE IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED AREA IAW SRM 53-2-5 PG 44A-44B. FABRICATED FILLER (7075-T6-0.160), SHIM (7075-T6-0.125) AND REINFORCEMENT ANGLE (STEEL-P4-0.080) IAW SRM 53-2-5 PG 44A-44B. CLEANED, TREATED AND PRIMED FILLER, SHIM AND INNER AREA IAW SRM 51-1-8B. INSTALLED FILLER, SHIM AND REINFORCEMENT ANGLE ON ATTACHING ANGLE OF VERTICAL STAB AND FUSELAGE RT STA 1766.00 - STA 1800.382 IAW SRM 53-2-5 PG 44A-44B FIG 16A, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1 (PRC). 2L74 4F RT4A25 20030521000432003052100043WP 2003 5 21 DHL2003804911 120030127A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING- CTR L/E FORMER CRACKED 1.000, STA XFS 490.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK AT STA XFS 490.000 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LT WING CTR L/E FORMER UPPER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000542003052100054EU 2003 5 21 MALA030258 120030418A5330 ACCESS PANEL BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 FUEL ACCESS PANEL 6110B CORRODED. SUSPECT FRETTING CORROSION, MAINTENANCE REPLACED PANEL FOR CORRECTIVE ACTION. 2H74 4F RTA49EU 20030521000712003052100071WP 2003 5 21 MWEA030203 120030507A5312 BULKHEAD DOUG DC9 DC981 3022081WP FUSELAGE GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 AFT PRESSURE BULKHEAD SKIN HAS A GOUGE ON THE RIGHT SIDE LOCATED AT ABOUT THE 7:00 POSITION (LOOKING FROM THE AFT SIDE) FROM THE CENTER SECTOR. BLENDED GOUGE, PERFORMED THICKNESS CHECK. THICKNESS WITHIN LIMITS. 2L72 4F A6WE 20030521000762003052100076NM 2003 5 21 DHL2003720005 120030516A2611 LAMP BOEING727 727228 1384083NM SMOKE DETECTOR BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01720DH 19544 NR 3 SMOKE DETECTOR (RT) WILL NOT TEST. RE-LAMPED, OPS CHECKED NORMAL IAW M/M 26-17-000. 2L73 4F RTA3WE 20030521000862003052100086NM 2003 5 21 DHL2003747500 120030511A5321 WEB BOEING727 727224 1384076NM CABIN FLOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN FLOOR SUPPORT WEB AT BS 870 LT SIDE OUTBOARD BY THE EMERGENCY EXIT LBL 60 IS CRACK (MKD). REMOVED FLOOR SUPPORT FOR REPAIR IAW B-727 SRM 51-30-2. CUT-OUT AREA DIM 1.5 INCH X 1 INCH AND FABRICATED ONE FILLER 1.5 INCH X 1 INCH AND ONE ANGLE DOUBLER DIMENSIONS 6.5 INCH X 2 INCH USING 7075 T-6 .040 PO 9912249 IAW B-727 SRM 51-40-3. ALODINED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-40-3. 2L73 4F A3WE 20030521000892003052100089WP 2003 5 21 DHL2003802004 120030502A5347 SEAT TRACK DOUG DC8 DC873 302199CWP COCKPIT LACK OF LUBE A DHLAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SO01802DH 46076 S/O SEAT VERY HARD TO MOVE WHEN USING FORWARD SEAT EDGE RELEASE HANDLE. LUBRICATED GUIDE RAILS, OPS CHECKED GOOD PER M/M 25-11-2. 2L74 4F RT4A25 20030521000932003052100093WP 2003 5 21 DHL2003801025 120030419A573057696004 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT OUTER WING INBOARD L/E OUTER PLATING SHOWS CORROSION AT XFS 710.000. PERFORMED MAJOR REPAIR IAW EODHL-030403, ED3261. REMOVED FASTENERS, REMOVED CORROSION FROM RT OUTER WING INBOARD L/E OUTER PLATING. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT CORRODED AREA IAW EODHL-030403, ED3261. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER (7075-T6 0.050) (7075-T6AL 0.063) IAW EODHL-030403, ED 3261. CLEANED,TREATED AND PRIMED FILLER AND DOUBLER INNER PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL-030403, ED 3261, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9 AND SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030521000982003052100098WP 2003 5 21 DHL2003801026 120030423A534036169482 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 MAIN CARGO COMPT FITTING ATTACHING FRAME TO RT CUSP EXTRUSION AT STA 702.875 WITH 2.000 INCH CRACK. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521000992003052100099WP 2003 5 21 DHL2003801029 120030422A52304656392N FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 D-BELLY DOOR INTERNAL STRUCTURE HINGE SUPPORT FITTING CRACKED. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON D-BELLY DOOR INTERNAL STRUCTURE HINGE SUPPORT IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001102003052100110WP 2003 5 21 DHL2003801044 120030412A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E UPPER SKIN HOLES ELONGATED, XFS 335.250 TO XFS 335.250 TO XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 1. FABRICATED DOUBELR (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. DRILLED NEW HOLES ON DOUBLER IAW SRM 51-1-22 PG 1. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001162003052100116EA 2003 5 21 COMA0360237 120030512A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01982CA 7168 FLIGHT 5240 FLAPS FAILED AFTER LANDING. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030521001352003052100135WP 2003 5 21 DHL2003801031 120030414A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L\E FORMER CRACKED 1.000 INCH AT XS 454.000. REMOVED FASTENERS IAW SRM 51-121 PG 1. FABRICATED REINFORCING ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001662003052100166NM 2003 5 21 SWAA031086 120030514A575360B00178 ROLLER BOEING737 7372H4 138448CNM LT WING TE FLAP WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29071SW 22358 T/E FLAPS CAUSED SHUDDER DURING EXTENSION. REMOVED AND REPLACED LEFT T/E MID FLAP PIVOT ROLLER PER MM. 2L72 4F A16WE 20030521001682003052100168NM 2003 5 21 SWAA031088 120030512A53306546882 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BOTH LT & RT VERTICAL STAB AFT ATTACH POINTS, BS 1138. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030515001562003051500156NM 2003 5 15 SWAA031072 120030510A53306545768 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH LONG FUSELAGE SKIN CRACK, BS 520, STRINGER 16R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030612000762003061200076WP 2003 6 12 UPS03840699 120030517A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, REMOVE DOUBLER FROM L-1 DOOR UPPER FWD CORNER, DOUBLER DOES NOT CONFORM TO SRM. REPAIR PER SRM 53-2-0 FIG 15 ST STA 60 LONG 10L. REMOVED EXISTING REPAIR, CUTOUT CRACK DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 15. 2L74 4F RT4A25 20030612000782003061200078WP 2003 6 12 UPS03840701 120030520A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, STATION 1730 LONG 14R IS CRACKED. REMOVED LONGERON STA 1720 TO 1760, FABRICATED AND INSTALLED LONGERON SECTION IAW DWG 5649327 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20030612001102003061200110NM 2003 6 12 UPS03240748 120030517A5320 SUPPORT BRACKET BOEING727 727185C 138406NNM WX RADAR SYS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, WEATHER RADAR TX MOUNTING PLATE, SUPPORT BRACKET AFT LEFT SIDE IS CRACKED. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1 SHEET 1. 2L73 4F A3WE 20030612001252003061200125NM 2003 6 12 UPS03440771 120030519A5313 LONGERON BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D- BS 1940-1960 STRINGER 1R STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 6. 2L74 4F RTA20WE 20030612001482003061200148WP 2003 6 12 UPS03840737 120030504A5230 LATCH DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, C-PIT CROSS SLIDE DOOR LOWER JUST AFT OF CENTER LATCH HOOK CRACKED. REMOVED FASTENERS IN WEB IAW DC8 SRM 51-1-21 & 51-3-0 FOR ACCESS. REMOVED CRACKED LATCH HOOK IAW DC8 SRM 51-1-21. INSTALLED LATCH HOOK AND WEB IAW DC8 SRM 51-1-21, 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20030613000472003061300047EA 2003 6 13 SWIA200312068 120030601A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07952SW 7805 FLOOR EMERGENCY LIGHTS ALONG ROWS 6, 7 & 8 WILL NOT ILLUMINATE. FOUND 1 GROUND PIN (R3) PULLED OUT OF TB104. SECURED AND ALL EMERGENCY LIGHTS OPS CHECKS GOOD AT THIS TIME. 2L72 4F RTA21EA 20030613000852003061300085 2003 6 13 MALA030295 420030608A34426227337001 CONTROLLER SAAB SF340 340B 7860101EU WEATHER RADAR MALFUNCTIONED A MALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL15411XJ 340B411 DURING FLIGHT 3259, WEATHER RADAR CANNOT PAINT. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED WX RADAR RT PN/ON/OFF 622-7337-001, SN/ON 1547, SN/OFF 1042. ALL CHECKS GOOD IAW SF 340 MM CHAP 34. 2L72 4T RTA52EU 20030613000862003061300086EU 2003 6 13 MALA030296 120030608A30006068T56P01 VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ANTI ICE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15434XJ 340B434 DURING FLIGHT 3529, RT AIR VALVE LIGHT ILLUMINATED QRH WAS PERFORMED LIGHT STAYED ON. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RT ANTI-ICE BLEED START VALVE IAW GE 75-00-00. PERFORMED OPS TEST GOOD IAW GE MM 72-00-00 TEST PARA G P/N 6068T56P01, S/N OFF GRTG1292, ON/GRTB9914. 2L72 4T4 TRTA52EU E8NE 20030613001192003061300119NM 2003 6 13 SWAA031194 120030529A3350073123 LENS BOEING737 7377H4 1384404NM CABIN FLOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 FWD EEPLS LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030613001572003061300157NM 2003 6 13 SWAA031216 120030601A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C4 CHECK, FOUND RT OUTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030617000262003061700026EU 2003 6 17 CA030602006 120030523A6200LN93556X32 BOLT BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL HYDRAULIC PACK WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) WHILE COMPLYING WITH FLEET CAMPAIGN NOTICE 351-73-20-12 IT WAS FOUND THAT THE BOLT CONNECTING THE TWO N2 GOVERNOR CABLES TOO THE HYD PACK WAS TOO SHORT, ONLY ONE THREAD WAS SHOWING THROUGH THE ANCHOR NUT. A NEW BOLT WAS INSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H3EU E4CE 20030617000402003061700040GL 2003 6 17 AUS20030493 120030507A2750B190956 CONTROL CABLE PAC CT4 CT4B GL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED CLCLIMB 1 AUS 7297 (AUS) FLAP LEVER INTERLINK CABLE BROKEN. LT (SLAVE) FLAP LEVER DISCONNECTED FROM RT (MASTER) LEVER. 1L71 3O3 ORTA9PC E1CE 5 CP920 20030617000542003061700054NM 2003 6 17 CA030603008 120030524A792120008A OIL COOLER ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA ENGINE LEAKING W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) NOTED A SMALL BIT OF OIL ACCUMULATING ON UNDER SIDE OF COOLER. NO EVIDENCE OF IAT RUNNING FROM ANYWHERE ELSE. 1G71 3O3 O H10WE E274 20030617000902003061700090NM 2003 6 17 AUS20030507 120030506A2520 SEAT BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU CABIN LOOSE W O OTHER O OTHER CRCRUISE 1 AUS (AUS) PASSENGER SEAT 1A-C OUTBOARD LEG ADRIFT FROM SEAT TRACK. 2L72 4F4 FRTA16WE E21EU 20030617000982003061700098 2003 6 17 ERAA087090 420030516A344240008310103 RECEIVER SKRSKYS61 S61N 8142104NE GE CT58 CT58* 30011GL WX RADAR FAILED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01561EH 61471 RADAR DOES NOT PAINT RAIN. ONCE YOU'RE WITHIN 10 MILES OF VERY HEAVY RAIN, IT STARTS TO PAINT LIGHT RAIN. 2G72 4U4 U 1H15 1E3 20030515001862003051500186NM 2003 5 15 AWXA200300509 120030411A53206517684 INTERCOSTAL BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL AT STR 12 LT, BETWEEN BS 294 AND BS 305. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT STR 12 LT, BETWEEN BS 294 AND BS 305; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-200 SRM 51-10-1 PG 8. 2L72 4F RTA16WE 20030520000132003052000013NM 2003 5 20 UIEA200300019 120030427A3040 HEATER BOEING747 74747UF 1384949NM WINDSHIELD SMOKE A UIEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15498MC 29259 SMOKE IN COCKPIT, 30 MINUTES AFTER TAKEOFF, ELECTRICAL LEAD ON LOWER LEFT SIDE OF CAPTAINS WINDSHIELD STARTED TO SMOKE. WINDOW HEAT LEFT WAS TURNED OFF. SMOKE STOPPED AND REMAINED OFF FOR THE REST OF THE FLIGHT. FOUND L1 WINDOW HEAT ELECTRICAL LEAD AND TERMINAL CONTACT POOR. TERMINAL CLEANED AND INSTALLED PER MM 56-11-01. WINDOW HEAT WIRE CHECK PERFORMED PER WD 30-41-11. ALL SATISFACTORY. (M) 2L74 4F RT1384945 20030520001492003052000149NM 2003 5 20 2003F00277 120030120A5320 STRINGER CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND STRINGER 4L, STATION 720D, HAS CRACKED CLIP. FABRICATED, TREATED, PRIMED AND INSTALLED NEW CLIP AT STATION 720D, STRINGER 4. (M) 2L73 4F A3WE 20030521000282003052100028WP 2003 5 21 DHL2003804893 120030205A534037502571 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 AFT CARGO COMPT FITTING CRACKED 3.000 BETWEEN STA 1040.000 AND 1060.000 NEAR TO L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 AND FAX BOEING-SEV-LIM-03-00-0003H, DATE: JAN. 20, 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON AFT CARGO COMPT BETWEEN STA 1040.000 AND STA 1060.000, L-31R IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521000472003052100047WP 2003 5 21 DHL2003801022 120030418A5730576954589 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT OUTER WING OUTBOARD L/E UPPER PLATING CORRODED AROUND STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030414, ED 3267. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT DAMAGED AREA IAW EODHL 030414, ED 3267. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) A FILLER (7075-T6 AL0.050) IAW EODHL 030414, ED 3267. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B, APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER ON LT OUTER WING OUTBOARD L/E UPPER PLATING AROUND STA XFS 710.000 USING NEW FASTENERS IAW EODHL030414, ED3267 AND SRM 51-1-212L74 4F RT4A25 20030521000592003052100059WP 2003 5 21 DHL2003801008 120030421A57305769857387 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E SKIN SHOW ELONGATED HOLES AND INTERIM REPAIR AT XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030409, ED 3257. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW EO DHL 030409, ED 3257. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER (7075-T6 0.063) IAW EODHL 030409, ED 3257. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INNER PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON SPLICE SURFACE IAW SRM 51-1-5 PG 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL 030409, ED 3257, SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521000642003052100064WP 2003 5 21 DHL2003801014 120030425A5753 FITTING DOUG DC8 DC873F 302199FWP LT TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT FLAP HINGE SUPPORT FITTING LWR SUPPORT ANGLE AT STA XF 97.000 CRACKED. REMOVED AND REPLACED LT FLAP HINGE SUPPORT FITTING LWR SUPPORT ANGLE AT XF 97.000 IAW MM 20-16-0 PG 207. REFER O N/R 0075 FOR OPS CHECK. 2L74 4F RT4A25 20030521000702003052100070EU 2003 5 21 MALA030248 120030426A3350 LIGHT SAAB SF340 340B 7860101EU ROW 8 INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15362PX 340B258 ROW NR 8 FLOOR TRACK LIGHT INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY WITH NEW UNIT OPS CHECK GOOD IAW SAAB AMM 33-50-20-2. 2L72 4T RTA52EU 20030521000722003052100072WP 2003 5 21 MWEA030204 120030507A5312 BULKHEAD DOUG DC9 DC981 3022081WP FUSELAGE GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 AFT PRESSURE BULKHEAD HAS A GOUGE ON THE RIGHT SIDE LOCATED AT ABOUT 11:00 POSITION (LOOKING FROM THE AFT SIDE) FROM THE CENTER OF THE THRUST REVERSE SECTOR, THE GOUGE IS ABOUT 3.5 FROM THE CENTER OF THE SECTOR. BLENDED OUT GOUGE, PERFORMED THICKNESS TEST FOUND WITHIN LIMITS. 2L72 4F A6WE 20030521001412003052100141WP 2003 5 21 DHL2003801040 120030404A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 MAIN CARGO COMPT NR 4 TRACK PLUG LUGS WORN AT STA 952.000. REMOVED AND REPLACED NR 4 TRACK PLUG AT STA 952.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521001482003052100148WP 2003 5 21 MWEA030194 120030501A53479957871517 SEAT TRACK DOUG DC9 DC981 3022081WP COCKPIT DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 FIRST OFFICER'S AFT SEAT TRACK HOLES ARE ENLONGATED. REMOVED TOP LEG OF FIRST OFFICER'S AFT SEAT TRACK AND TOP LEG OF PILOT'S SEAT, DRILLED UP SEAT TRACK AND INSTALLED TOP LEG SEAT TRACK AND TOP LEG OF PILOTS SEAT TRACK. 2L72 4F A6WE 20030521001712003052100171 2003 5 21 SWAA031054 420030512A25656557450478 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29314SW 23336 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED WHEN OPENING DOOR. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM. 2L72 4F RTA16WE 20030521001772003052100177WP 2003 5 21 DHL2003801072 120030508A5230 PIN DOUG DC8 DC873F 302199FWP DOOR CRANK BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 UPPER CARGO DOOR NR 4 LOCKPIN CRANK ASSY BROKEN. REMOVED CRANK ASSY ON NR 4 LOCKPIN (UPPER CARGO DOOR) IAW OHM 52-3-10 PG 1, 2, 8, 11, 17 AND 18. 2L74 4F RT4A25 20030521001942003052100194NM 2003 5 21 SWAA031057 120030511A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 798, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030522000082003052200008NM 2003 5 22 0300976312 120030517A2530 OVEN BOEING747 747451 1384940NM GALLEY SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01672US 30267 DURING FLIGHT SMOKE EMITTED FROM THE 3-28 OVEN IN THE NR 4 GALLEY. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND CONTROLLER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030522000112003052200011SO 2003 5 22 C2XA03TY060 120030517A531514521699003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE DIGITAL PLATE AT FR20 & 22 WAS FOUND CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PLATE IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000192003052200019SO 2003 5 22 C2XA03BT058 120030519A33501317 LAMP EMB 145 EMB145LR 3260212SO CABIN INTERIOR BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716999 145307 DURING SERVICE/ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 12A TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LAMP AT SEAT 12A IAW EMB145 AMM 33-50-50. OPS CHECKED EMERGENCY LIGHTS GOOD. 2L72 4T RTT00011AT 20030522000442003052200044WP 2003 5 22 GTIA030303 120030425A2497 STUD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE GROUND INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 BOTH OVERHEAD EMERGENCY LIGHTS AT STA 636 ARE INOPERATIVE. REMOVED AND REPLACED GROUND STUDS 5221 AND 5222. 2L72 4F4 FRTA6WE E2EA 20030522000582003052200058SO 2003 5 22 C2XA03SH136 120030518A541014576057621 STRUCTURE EMB 145 EMB145LR 3260212SO LT NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV DURING C-CHECK LEFT HAND ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO HAVE RUB MARKS. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030522000632003052200063WP 2003 5 22 GTIA030292 120030416A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 CORRODED WEB AT L18R FS 769-788, FS 788-807, FS 826-845 AND FS 886-905. FS 788-807, FS 826-845 AND FS 881-905 FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA AT L18R STA 826 TO 845. CUT OUT DAMAGED AREA AT L18R STA 886-905. CUT OUT DAMAGED AREA AT L18R STA 788-807. FABRICATED 3 EA DOUBLERS. INSTALLED 3 EA DOUBLERS. 2L72 4F4 FRTA6WE E2EA 20030522000662003052200066SO 2003 5 22 C2XA03SH133 120030518A541014576631622 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV DURING C-CHECK, THE RIGHT HAND LOWER ENGINE COWLING HAS RUB MARKS ON THE MOST AFT INBOARD STIFFENER. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STIFFENER IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030522000702003052200070SO 2003 5 22 C2XA03SH132 120030518A531514522459003 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV DURING C-CHECK THE RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED RAMP ANGLE IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030522000752003052200075SO 2003 5 22 C2XA03TY056 120030517A531514525480003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEAM, IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000852003052200085WP 2003 5 22 GTIA030308 120030421A5310 STRUCTURE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE SUBFLOOR CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 CABIN STA 218, LBL 43, SUBFLOOR CORRODED. CUT OUT DAMAGE. DRILL AND LOCATE DOUBLER. INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20030522000922003052200092WP 2003 5 22 GTIA030294 120030427A3260 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE LT MLG DIRTY A GTIAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23826NK 49391 UPON GEAR RETRACTION LEFT LANDING GEAR RED UNSAFE LIGHT, TOOK APPROXIMATELY ONE MINUTE TO EXTINGUISH. FOUND GREASE ON TARGET, CLEANED AND INSPECTED LT PROX SWITCH AND TARGET AND TESTED. OPS CHECK GOOD. 2L72 4F4 FRTA6WE E2EA 20030522000942003052200094NM 2003 5 22 SWAA031066 120030512A53116546546 FRAME BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CORRODED (2 EA) AT BS 794, WL 157 AT RBL 21 & BS 786, WL 153 AT RBL 14. REPAIRED FUSELAGE FRAMES PER SRM. 2L72 4F RTA16WE 20030522001052003052200105NM 2003 5 22 CALA0300256 120030519A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR INNER SKIN ABOVE HANDLE ON LIGHTENING HOLE. THE SKIN WAS REPAIRED IAW ECRA 5232-01015. 2L72 4F RTA16WE 20030522001132003052200113NM 2003 5 22 AWXA200300552 120030515A3520417N3100293SP OXYGEN MASK BOEING737 73733A 1384673NM SEAT ROW 19 MISINSTALLED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - EMERGENCY EQUIPMENT - DURING C-17 CHECK OF EMERGENCY OXYGEN SYSTEM THE PASSENGER SERVICE UNIT OXYGEN MASK AT SEAT ROW 19 LT FAILED DROP CHECK. MAINTENANCE FOUND OXYGEN MASK LANYARD AT SEAT ROW 19 LT MISROUTED, CORRECTLY ROUTED LANYARD, DROP TEST WAS GOOD PER AWA T/C S1C35002. 2L72 4F RTA16WE 20030522001232003052200123 2003 5 22 SWAA031125 420030519A256565C19901 CABLE BOEING737 7373H4 1384600NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030522001252003052200125NM 2003 5 22 SWAA031127 120030519A33506104781 BATTERY BOEING737 7375H4 138449DNM MID CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030522001302003052200130NM 2003 5 22 SWAA031109 120030516A212165771 BLOWER BOEING737 7375H4 138449DNM E/E COMP FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29523SW 26565 EN ROUTE, ELECTRIC TYPE BURNING SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACED SECONDARY EQUIPTMENT COOLING BLOWER PER MM. 2L72 4F RTA16WE 20030520000462003052000046SO 2003 5 20 SIMA200311101 120030417A21508152403 ACM EMB 145 EMB145 3260210SO NR 2 INOPERATIVE A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21613AE 145081 ORD - FLT 4246 - DURING CLIMB CREW REPORTED AN ELECTRICAL/SULPHUR ODOR IN THE COCKPIT AND THE FLIGHT ATTENDANT REPORTED A SMALL AMOUNT OF SMOKE IN THE CABIN. THE AIRCRAFT WAS RETURNED TO ORD AND THE SMOKE DISSIPATED DURING THE LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ACM IAW EMB MM. OPERAITONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030520000482003052000048SO 2003 5 20 SIMA200311303 120030326A532014521725615 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, SERVICE DOOR AFT SILL CORRODED. REMOVED AFT SERVICE DOOR SILL AND INSTALLED SERVICEABLE AFT SILL IAW EMB 145 SRM 51-40-002. (M) 2L72 4T RTT00011AT 20030520000622003052000062NM 2003 5 20 AMTA200300494 120030414A3350 LIGHT BOEING737 73783N 13844HINM EMERGENCY EXIT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11308TZ 28244 L-1 DOOR EMERGENCY EXIT LIGHT NOT LIGHTED. CLEANED LAMP SOCKET IAW CH 33-51-00 OF THE AMM. (M) 2L72 4F RTA16WE 20030520001132003052000113NM 2003 5 20 AALA20030444 120030411A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21352AA 24033 STL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 23B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520001392003052000139NM 2003 5 20 BJNA03041 120030407A33503626624 LIGHT BOEING737 737282 13844ATNM CABIN DISCONNECTED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 EMERGENCY FLOOR PROXIMITY LIGHTING (FROM PASSENGER ROWS 14 THROUGH 17) NOT LIGHTING DURING OPERATIONAL CHECK. MAINTENANCE DISCOVERED THAT THE LIGHTING STRIP FOR THIS SECTION HAD BECOME DISCONNECTED FROM ITS POWER SOCKET. LIGHT STRIP WAS REATTACHED AND OPERATIONALLY TESTED NORMAL PER LUMINESCENT COMPONENT MM 33-51-01. (M) 2L72 4F RTA16WE 20030521000352003052100035WP 2003 5 21 MWEA030192 120030429A212039347101 ADAPTER DOUG DC9 DC932 3022066WP AIR CONDITIONINGLEAKING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31602ME 48133 AT 33,000 FEET MASTER WARNING AND CABIN PRESSURE ANNUNICATOR CAME ON AND THE OXYGEN MASK DROPPED. REMOVED AND REPLACED WATER SEPARATOR DUCT BOOT. 2L72 4F A6WE 20030521000502003052100050EU 2003 5 21 MALA030255 120030416A5753HC579L0884004 HINGE BAC 146 AVRO146RJ85A1500097EU TE FLAP CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 WHILE COMPLYING WITH FLAP EO AD020307 FOUND LT O/B FLAP HINGE AFT PIN HC579L0884-004, LT I/B FLAP HINGE PINS HC579L0884-000 AND HC579L0884-002 AND LT I/B FLAP LINK PIN HC579L0871-000 WITH CORROSION. REPLACED PINS FOR CORRECTIVE ACTION. 2H74 4F RTA49EU 20030521001152003052100115WP 2003 5 21 MWEA030211 120030516A53505911403501 SKIN DOUG DC9 DC982 3022082WP RADOME DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 SKIN DAMAGE ON FUSELAGE AT RADOME LEFT HINGE. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F A6WE 20030521001542003052100154WP 2003 5 21 DHL2003801076 120030414A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 FWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL CRACKED 1.500 AT STA 640.000, LBL-40. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA 640.000, LBL-40 IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER (2024-T3 AL0.050) IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030522000092003052200009NM 2003 5 22 0300986302 120030513A2530 CONTROLLER BOEING747 747451 1384940NM OVENS FAILED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01662US 23720 DURING FLIGHT A ELECTRICAL ODOR WAS NOTICED AT THE TOP OF THE STAIRS LEADING TO THE UPPER DECK AND IN THE MAIN CABIN BY THE VIDEO CONTROLS. TURNED OFF GALLEY POWER AND VCR'S. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED 2-33/34 OVENS/CONTROLLERS AND REPOSITIONED 2-23 OVEN VENT HOLE. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030522000172003052200017NM 2003 5 22 375PA0015 120030512A3350 BULB BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 FWD EMERGENCY FLOOR PATH LIGHTING HAS ONE LIGHT INOP AT ROW 1. MOVED FLOOR PATH LENS FROM ROW 7 TO ROW 1. ROW ONE OPS NORMAL. RELEASED ON MEL 33-19-1. ROW 7 HAS 1 FLOOR PATH LIGHT BULB INOP. 05/15/2003: REPLACED BULB AND REINSTALLED LENS ON ROW 7. SYSTEM OPS, CHECKS GOOD PER MM 33-51-02. CLEARED MEL. 2L72 4F RTA16WE 20030522000512003052200051NE 2003 5 22 GTIA030275 220030424A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 2 SMOKE A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23812NK 48021 709901 AIR RETURN, ON TAKEOFF AFT CABIN FILLED WITH SMOKE. AFT LAV SMOKE ALARMS WENT OFF. RETURNED TO DTW. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK AND LEAK GOOD, NO DEFECTS NOTED. 2L72 4F4 F A6WE E9NE 20030522000722003052200072SO 2003 5 22 C2XA03TY066 120030517A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE OMEGA BEAM BETWEEN FR20 AND 23 WAS FOUND CORRODED IN SEVERAL PLACES. MAINTENANCE CUT OUT THE DAMAGED AREAS, FABRICATED AND INSTALLED ANGLES, SHIMS, FILLER AND PLATE IAW EMB-135/145 SRM 53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000972003052200097 2003 5 22 SWAA031091 420030516A2565 BOTTLE BOEING737 7372H4 138448CNM ESCAPE SLIDE DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F A16WE 20030522001072003052200107NM 2003 5 22 CALA0300258 120030520A5414 SKIN BOEING737 7373T0 1384582NM NR 1 NACELLE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND A .5 INCH CRACK IN NR 1 I/B PYLON SKIN AT FORWARD UPPER CORNER OF PANEL 5724. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204. 2L72 4F RTA16WE 20030617001162003061700116SW 2003 6 17 HEEA087295 120030611A6220407010114101 CONE SEAT BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR HEAD CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 CONE SEAT HAS CORROSION AROUND CENTER LINE. TO BE SENT TO MFG. 1G71 3U3 UO H2SW E1GL 20030617001172003061700117SW 2003 6 17 HEEA087296 120030611A6220407310104105 SPRING BROKEN BELL 407 407 1182206SW ALLSN 250C 250C* GL FRAHM ASSY BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH LK61 53396 FRAHM ASSY HAS A BROKEN SPRING. REPLACED SPRING (2 EA) 407310104105 DUE TO BROKEN. REPAIRED. 1G71 3U3 UO H2SW E4CE 20030617001232003061700123GL 2003 6 17 HEEA087461 220030612A74216899084 IGNITER BELL 407 407 1182206SW ALLSN 250C 250C47M 03013GL ENGINE CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 ENGINE LIGHT OFF LATE. IGNITER HAS CARBON BUILD UP. REPLACED IGNITER. 1G71 3U3 UO H2SW E1GL 20030617001282003061700128EA 2003 6 17 QXEA200300674 120030604A2820D98C07606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX3221 10033 BOI- FUEL LEAKING FROM MAIN LANDING WHEEL BINS. FOUND RIGHT ENGINE INLET PRESSURE SENSOR LEAKING. REPLACED SENSOR. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030617001312003061700131SW 2003 6 17 HEEA087297 120030611A6220407010150109A FRAHM BELL 407 407 1182206SW MAIN ROTOR HEAD BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 FRAHM ASSY HAS A BROKEN SPRING. SHOP REPAIR. 1G71 3U O H2SW 20030617001392003061700139GL 2003 6 17 ERAA087098 220030520A753223053176 BLEED VALVE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL COMPRESSOR STALLED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01298EH4798 S845 BLEED VALVE PRODUCING COMPRESSOR STALLS. OVERHAULED BLEED VALVE; CHANGED ALL NECESSARY PARTS AS LISTED ON WORK FORM. 1G72 3U3 U H3EU E4CE 20030617001492003061700149NM 2003 6 17 QXEA200300706 120030610A5551 FITTING BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - LEFT HAND FITTING FOR HORIZONTAL STAB MOUNT IS GOUGED FROM INSTALLATION OF BARREL NUT. REPAIRED IAW RD 8/4-55-92, PAGE 6, STEP 4. 2H72 4T RTA13NM 20030617001572003061700157SW 2003 6 17 HEEA087298 120030611A6220407010150109A FRAHM BELL 407 407 1182206SW MAIN ROTOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 FRAHM ASSY HAS A BROKEN SPRING. REPLACED SPRING (2 EA) 407310104105 DUE TO BROKEN. REPAIRED. 1G71 3U O H2SW 20030613000322003061300032EA 2003 6 13 COMA0360255 120030602A261324403615 ELEMENT CNDAIRCL600 CL6002B19 1900309EA MLG FALSE INDICATIONA COMAO OTHER N FALSE WARNING DEDESCENT 1 SO01472CA 7667 FLIGHT 5313 MLG OVERHEAT MESSAGE. REPLACED THE LT MLG OVERHEAT SENSING ELEMENT. 2L72 4F RTA21EA 20030613000712003061300071SO 2003 6 13 C2XA03SH167 120030608A531014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 15. MAINTENANCE REPAIRED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000822003061300082NM 2003 6 13 P5CA03000885 120030530A2612 WARNING LIGHT BOEING747 7472U3B 1384846NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE ILLUMINATED A P5CAO OTHER N FALSE WARNING TOTAKEOFF 1 WP23922FT 22768 702238 ON T/O NR 4 ENG FIRE DET A-LOOP ILLUMINATED FIRE LIGHT. B-LOOP NORMAL. ITEM WAS DEFERRED PER THE DDPG AFTER IT WAS DETERMINED THAT ONE LOOP WAS OPERATIONAL. DEFECTIVE A-LOOP. 2L74 4F4 FRTA20WE E20EA 20030613000922003061300092NM 2003 6 13 UPS03440803 120030517A5320 REVEAL BOEING747 747200 1384847NM L5 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C M/D - L5 DOOR FUSELAGE FWD CUTOUT REVEAL FOUND CRACKED AT BS 2232 BETWEEN 16L - 17L. M/D L5 DOOR FWD CUTOUT REVEAL S-16 REPAIRED AS PER SRM 53-10-04 FIG 91. 2L74 4F RTA20WE 20030613001112003061300111NM 2003 6 13 SWAA031252 120030604A5520BACB28AM07 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING. 2L72 4F RTA16WE 20030613001172003061300117NM 2003 6 13 SWAA031258 120030604A33406944578 SWITCH BOEING737 7372H4 138448CNM COCKPIT FAULTY A SWAAO OTHER O OTHER APAPPROACH 1 SW29090SW 22905 ELECTRICAL ODOR IN COCKPIT. REMOVED AND REPLACED LT INBD LANDING LIGHT SWITCH PER MM. 2L72 4F A16WE 20030613001252003061300125NM 2003 6 13 SWAA031200 120030529A53306523693 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED A2 CHECK, FOUND 2 LONG FUSELAGE SKIN CRACK, BS 349, STRINGER 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030522001142003052200114NM 2003 5 22 AWXA200300553 120030516A3350BR964411 LIGHT BOEING757 757225 1384959NM SEAT ROW 16 INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28913AW 22207 JFK - EEL - DURING 8-DAY CHECK AT JFK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS FOUND INOPERATIVE. MAINTENANCE ISSUED MEW 33-51-3, COND 1 FLOOR PROX EMERGENCY ESCAPE PATH LIGHT INOPERATIVE SEAT 16 LT. 05/19/2003 - PHX - MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030522001182003052200118EU 2003 5 22 MALA030267 120030510A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING INSPECTION IN CWA, RT FUSELAGE AT STA 316 HAS DENTS BETWEEN SL1616 AND SK1618. MAINTENANCE COMPLETED REPAIR IAW EO S53150. REF 409 NR 177298 FOR DETAIL. A/C RELEASE DATE 5/12/2003. 2L72 4T RTA52EU 20030522001282003052200128NM 2003 5 22 SWAA031130 120030519A53106969854 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT CUTOUT FOR NR 5 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030523000092003052300009NM 2003 5 23 2003F00292 120030120A5313 STRINGER BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND STRINGER, 8L AT FUSELAGE STATION 380 CRACKED. REMOVED DAMAGED AREA FROM FRAME AT FUSELAGE STATION 380, STRINGER 8L. FABRICATE REPAIR DOUBELR. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M) 2L73 4F A3WE 20030523000222003052300022EA 2003 5 23 QXEA0300567 120030515A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX-DAMAGED RIVET AT STATION 613.00 TWO INCHES BELOW STRINGER 6R ON RIGHT HAND SIDE ABOVE WINDOW 9. REPAIRED IAW CRJ-700 SRM 51-42-06 AND 51-25-16. 2L72 4F RTA21EA 20030523000362003052300036NM 2003 5 23 DL73G030392 120030425A5330654580026 SKIN BOEING737 73735B 13844BMNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27224DA 24269 A CRACK WAS FOUND IN THE SKIN AND BONDED DOUBLER AT THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1 INCH CUTOUT IN THE CORNER. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384787-14, REV A. 2L72 4F RTA16WE 20030523000372003052300037NM 2003 5 23 DL73S030393 120030426A5330654577518 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK AT THE BONDED SKIN DOUBLER LINE ALONG STRINGER 19R AT FS 767. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384968-14. 2L72 4F RTA16WE 20030523000412003052300041NM 2003 5 23 DLM88030397 120030427A53125910130387 BULKHEAD DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27918DL 49583 TOOL DAMAGE (DRILL MARKS) WERE FOUND ON AFT PRESSURE BULKHEAD LOWER CAP NEAR SKIN DRAIN HOLES. REPAIRED BY BLENDING 0.007 INCH DEPTH LHS AND 0.009 INCH DEPTH RHS PER FAA DER APPROVED REPAIR INSTRUCTIONS. 2L72 4F RTA6WE 20030523000552003052300055NM 2003 5 23 SWAA031116 120030519A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030523000642003052300064NM 2003 5 23 QXEA0300528 120030504A33506138001 POWER SUPPLY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09412QX 4059 PDX- DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM FOUND AFT TWO CEILING LIGHTS, AFT WALL EXIT LIGHT AND GALLEY CEILING EXIT LIGHT ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523000662003052300066NM 2003 5 23 SWAA031122 120030519A53126516300 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234, LBL 8.5 AND LBL 9.5. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F A16WE 20030523000732003052300073NM 2003 5 23 CALA0300244 120030510A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716339 23577 THE LT FUSELAGE SKIN HAD A DENT LOCATED BETWEEN STA 211.80 AND 219.80, WL 200, (S19L LAP SPLICE). THE AREA PREVIOUSLY HAD AN INTERIM REPAIR INSTALLED AND WAS PLACED ON DIP. THE SKIN WAS PERMANENTLY REPAIRED IAW ECRA 5330-03253 WHILE AIRCRAFT WAS IN 1C CHECK AT MCO. 2L72 4F RTA16WE 20030618000802003061800080NE 2003 6 18 SWAA031303 220030611A7200 ENGINE BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE NR 1 FAILED A SWAAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 SW29731SA 27863 875775 IN-FLIGHT SHUTDOWN, DECLARED EMERGENCY, AIR TURNBACK, NR 1 ENGINE FAILURE, AUTO SHUTDOWN IN-FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030617001302003061700130GL 2003 6 17 ERAA087095 220030519A7323252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE SURGES E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01292EH 562 ENGINE SURGES AND OSCILLATES AT HIGH POWER. OIL CONTAMINATION INTERNALLY. REPAIRED AND TESTED IAW HONEY WELL OHM FORM 15-1095A 1G72 3U3 U H3EU E4CE 20030617001552003061700155NM 2003 6 17 QXEA200300712 120030601A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - NICK ON EDGE OF FUSELAGE SKIN CUT-OUT FOR FORWARD BAG DOOR - AFT OF CUT-OUT 2 INCHES BELOW LATCH ROLLER TRACK. REPAIRED IAW Q400 SRM 51-14-00, FIGURE 203, PAGE 215 AND SRM 51-25-05, PAGE 208. 2H72 4T RTA13NM 20030617001892003061700189NM 2003 6 17 QXEA200300724 120030612A5230 LATCH BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR LACK OF LUBE A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09409QX 4051 RETURNED TO FIELD, ON CLIMBOUT MASTER WARNING "FUSELAGE DOOR" WARNING LIGHT ILLUMINATED. SYSTEM PAGE SHOWED FORWARD BAGGAGE DOOR NOT CLOSED. PERFORMED CHECKLIST AND RETURNED TO BOI. CLEANED AND LUBED FORWARD CARGO DOOR LATCH AND SHAFT. DOOR OPENS AND CLOSES NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617002572003061700257SW 2003 6 17 HEEA087479 120030612A2497BD131 CONNECTOR BELL 407 407 1182206SW CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 CONNECTOR CORRODED. SCRAPPED. 1G71 3U O H2SW 20030617002662003061700266SW 2003 6 17 HEEA087026 120030604A7120206064105101 LEG ASSY BELL 206 206L3 1182108SW ENG MOUNT MISINSTALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FOUND END FITTING IMPROPERLY LOCATED, LEG WILL NOT FIT WORK AID. SENT FOR CREDIT. 1G71 3U H2SW 20030617002692003061700269NM 2003 6 17 QXEA200300607 120030429A7110 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - NR 2 ENGINE LOWER COWLING HAS ANGLE SUPPORT CRACKED JUST BELOW OIL COOLER AFT MOUNTING BOLT. REMOVED AND REPLACED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030617003072003061700307NM 2003 6 17 SWAA031263 120030608A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030618000522003061800052SW 2003 6 18 HEEA087337 120030611A6510206061432117 BEARING BELL 407 407 1182206SW BLOWER SHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH PHI0004 53399 FWD BEARING ROUGH. REPLACED IMPELLER 206061432117 DUE TO BENT; BEARING (2 EA) 407-340-339-101, S/N ZV14826 AND ZV14885 DUE TO ROUGH. REPAIRED. 1G71 3U O H2SW 20030618000682003061800068NM 2003 6 18 SWAA031309 120030611A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234, LBL 13. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030618000782003061800078SW 2003 6 18 HEEA087341 120030611A6510407340339101 BEARING BELL 407 407 1182206SW BLOWER SHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH PHI0026 53159 BEARING ROUGH. REPLACED BEARING (2 EA) 407340339101, S/N ZV15265 AND ZV14832 DUE TO ROUGH. REPAIRED. 1G71 3U O H2SW 20030618001002003061800100NM 2003 6 18 SWAA031285 120030608A53206545819 GUSSET BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED RON, FOUND NLG ACTUATOR UPPER SUPPORT GUSSET FITTING CRACKED. REMOVED AND REPLACED NLG ACTUATOR UPPER SUPPORT FITTING PER BAC DRAWING. 2L72 4F RTA16WE 20030618001152003061800115 2003 6 18 SWAA031291 420030608A2565D31354 SLIDE BOEING737 7377H4 1384404NM FWD CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29758SW 27873 DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030618001212003061800121SW 2003 6 18 HEEA087350 120030611A7120407060111101 MOUNT BELL 407 407 1182206SW ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 ENGINE MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030618001232003061800123NM 2003 6 18 SWAA031294 120030608A2710BACC2AB CONTROL CABLE BOEING737 7373H4 1384600NM AILERON WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 NO DEFLECTION ON RT AILERON DURING CONTROL INPUT. REMOVED AND REPLACED (3 EA) AILERON BUS CABLES, ABSB-4, ABSA-3 AND ABSB-3 PER MM. 2L72 4F RTA16WE 20030618001272003061800127NE 2003 6 18 HEEA087136 120030610A67107640003006054 LINK SKRSKYS76 S76A 8143006NE CYCLIC DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 IDLER LINK AT LATERAL FORCE GRADIENT DUE TO STILL CYCLIC LATERAL MOVEMENTS. SHOP REPAIR. 1G72 3U H1NE 20030618001282003061800128EA 2003 6 18 COMA0360260 120030607A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01989CA 7215 FLIGHT 5882 GEAR DISAGREE WARNING DURING CRUISE FLIGHT. REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR. 2L72 4F RTA21EA 20030618001352003061800135SW 2003 6 18 HEEA087351 120030611A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 EXHAUST STACK CRACKED AT AFT WELD GOING UP ALONG WELD IN CENTER OF DUCT. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030522001102003052200110EU 2003 5 22 AWXA200300549 120030516A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 221 DEFECTIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28669AW3531 1792 PHX - EEL - FLIGHT CREW REPORTED THE FORWARD OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED WITH THE EMERGENCY EXIT LIGHT SYSTEM IN ARMED POSITION; NO OTHER EMERGENCY LIGHTS WERE ON. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-38-04, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030522001312003052200131NM 2003 5 22 SWAA031110 120030519A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 520, BETWEEN STR 15R AND STR 16R, STR 16L BETWEEN BS 474 AND BS 477. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030523000172003052300017NE 2003 5 23 2003F00298 220030317A7230 BLADE BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE COMPRESSOR DAMAGED A PCSAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO17794AJ 21243 688672 IN FLIGHT NR 3 ENGINE COMPRESSOR STALLED TWICE AND HAD HIGH EGT INDICATION. ENGINE NR 3 WAS SHUTDOWN IN FLIGHT AND FLIGHT CONTINUED TO KMIA WITHOUT FURTHER INCIDENT. MIA MAINTENANCE INSPECTED ENGINE NR 3 AND FOUND THE C-9 THROUGH C-13 BLADES DAMAGED. ENGNE WAS REMOVED AND REPLACED IAW AMJ FORMS B-48 AND B-49. MAINTENANCE PERFORMED LEAK CHECKS AND OPERATIONAL CHECKS NORMAL IAW AMJ FORM B-41. AIRCRAFT WAS RETURND TO SERVICE. (M) 2L73 4F4 F A3WE E2EA 20030523000192003052300019NM 2003 5 23 SWAA031112 120030519A53306545785 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT RT WINDOWS NR 1, NR 4 AND NR 6. REPAIRED CUTOUT SKINS PER SRM. 2L72 4F RTA16WE 20030523000242003052300024NM 2003 5 23 QXEA0300550 120030512A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09345PH21207699 476 LWS- ON FLIGHT 2209 AFTER NORMAL STARTUP NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. UPON CYCLING NR 1 AC GENERATOR SWITCH PER CHECKLIST, CAUTION LIGHT MOMENTARILY EXTINGUISHED THEN RE-ILLUMINATED. REMOVED AND REPLACED NR 1 AC GENERATOR AND GCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030606000642003060600064NM 2003 6 6 03FDEA00613 120030423A5753NRC6055507 SKIN DOUG MD11 MD11 3023602NM TE FLAP DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT INBOARD FLAP LOWER SKIN SURFACE LOWER SECTION FOUND WITH SEVERAL DENTS (BETWEEN 54 - 66 INCHES FROM INBOARD EDGE). LT INBOARD FLAP LOWER SKIN SURFACE LOWER SECTION DENT SKIN REPAIRED AS PER SRM 57-10-00 VOL. II. 2L73 4F RTA22WE 20030609000232003060900023CE 2003 6 9 051603 120030516A2820RA5326 DIAPHRAGM BEECH 1900 1900C 1154161CE FUEL PUMP RUPTURED E YADAK NONE K FLUID LOSS ININSP/MAINT 1 AL031566C 955 B427 UC36 LOW PSI FUEL PUMP FOUND LEAKING ON RAMP - RUPTURED DIAPHRAGM 2L72 4T RTA24CE 20030609000642003060900064EA 2003 6 9 SWIA200311987 120030518A2750 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07927SW 7693 ''FLAP FAIL'' CAUTION MESSAGE AFTER FLAP RETRACTION AFTER LANDING IN SLC. REMOVED AND REPLACED RIGHT BPSU IAW 27-51-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20030609000902003060900090NM 2003 6 9 QXEA0300646 120030519A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09364PH 524 ON FLIGHT 9800 LAVATORY SMOKE DETECTOR WENT ON WHEN IN ROUTE. NO VISUAL SMOKE OR ODOR NOTED. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030609001562003060900156SO 2003 6 9 C2XA03SH157 120030525A532014524131005 SUPPORT EMB 145 EMB145LR 3260212SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 DURING C-CHECK THE FORWARD PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030609001602003060900160EA 2003 6 9 CA030404009 120030402A2121101270 FLAPPER VALVE TECHNOFAN AE0804AA2 CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DAMAGED W O OTHER J WARNING INDICATION CRCRUISE 1 CA 13399 509 (CAN) AT CRUISE ALTITUDE 'ARINC COOL' & 'DISPLAY COOL'MESSAGES WERE GIVEN. FLIGHT ALTERNATE AND STANDBY SELECTIONS WERE TRIED BUT MESSAGE STAYED ON.AIRCRAFT PLANNED TO DIVERT BUT AT LOWER ALTITUDETHE MESSAGE WENT AWAY SO FLIGHT CONTINUED TO ORIGINAL DESTINATION.MAINTENANCE FOUND FLAPPER VALVE ON LOWER COOLING FAN STUCK OPEN. VALVE HAD GROOVE WORN ON HINGE ARM CAUSING IT TO HANG UP ON HINGE PIN MOUNT. 2L72 4F4 FRTA21EA E15NE 20030610000422003061000042WP 2003 6 10 ABXA030167 120030414A5312991015541 PRESSURE PANEL DOUG DC9 DC931 3022065WP RT MLG WW CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 ONE SHEARED FASTENER AND SKIN BULGED AT DOUBLER RIGHT WHEEL WELL UPPER PRESSURE PANEL, STA 716, RIGHT BUTT LINE 56. REPAIRED AREA IAW REA D953-47174. 2L72 4F A6WE 20030610000542003061000054WP 2003 6 10 ABXA030154 120030325A531359203031 LONGERON DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 LONGERON 30 HEAVILY PITTED AT FS 756. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030610000692003061000069NM 2003 6 10 DL757030410 120030502A2150 CLAMP BOEING757 757232 1384965NM A/C PACK LOOSE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27602DL 22809 LT DUCT LEAK. EICAS MSG. WITH CORRESPONDING DUCT LEAK LT ON AIR CONDITIONING PANEL. FOUND PNEUMATIC DUCT LT WING LEAKING. RESECURED. NO FURTHER LEAKS NOTED 2L72 4F RTA2NM 20030610000982003061000098NM 2003 6 10 DL73S030445 120030507A5330654577519 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK RUNNING ALONG THE MILL/BONDED DOUBLER LINE OF STRINGER 23R AT FS 867. THE CRACK IS TYPICAL OF BAC S/B 737-53A1210. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 384995-14, REV A. 2L72 4F RTA16WE 20030613001272003061300127NM 2003 6 13 SWAA031202 120030529A2121215201 MOTOR BOEING737 7373L9 1384470NM GASPER FAN OVERHEATED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29657SW 23331 DIVERSION TO BOI, BURNING ODOR IN CABIN. REMOVED AND REPLACED GASPER AIR FAN PER MM. 2L72 4F RTA16WE 20030613001412003061300141NM 2003 6 13 SWAA031222 120030602A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 663, STR 1R AND STR 2R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030521001762003052100176WP 2003 5 21 DHL2003604506 120030428A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING CTR L/E INNER PART FORMER CRACKED 1.000 INCH, XFS 316.500. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON RT WING CTR L/E FORMER (XFS 316.500) IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030520001192003052000119NM 2003 5 20 USAA030040 120030407A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 FOUND SKIN CRACKED 3 INCHES, RIGHT FUSELAGE SKIN BETWEEN STATION 727E-727F AT STATION 25R. REMOVED CRACKED SECTION OF SKIN AND INSTALLED .063 INCH EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20030520001472003052000147NM 2003 5 20 2003F00275 120030120A5320 STRINGER CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND STRINGER 8R, FUSELAGE STATION 460 RIGHT SIDE, HAS CRACKED CLIP. REMOVED AND REPLACED CLIP. TREATED AND PRIMED AREA AT STARINGER 8R, FUSELAGE STATION 460. (M) 2L73 4F A3WE 20030521000602003052100060WP 2003 5 21 DHL2003801010 120030418A57535642960507 VANE DOUG DC8 DC873F 302199FWP LT WING TE FLAP CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING INBOARD FLAP VANE UPPER PLATING CORRODED STA XW 104.000 - XW 115.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030406, ED 3282. REMOVED CORROSION ON INBOARD FLAP UPPER PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED CORRODED SKIN IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED (03 EA) INNER FILLERS (01 EA WITH 2024-T3 0.016 AND 02 EA WITH 0.025) AND NEW SKIN (2024-T3 0.063) IAW EODHL 030406, ED 3262. CLEANED, TREATED AND PRIMED FILLER INNER PART AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT ON SPLICE SURFACES IAW SRM 51-1-15 PG 2. INSTALLED FILLER AND NEW SKIN IAW EODHL 030406, ED 3262, SRM 51-1-21 PG 2 AND SRM 51-2L74 4F RT4A25 20030521000882003052100088WP 2003 5 21 DHL2003804913 120030213A573056488971 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING UPPER SURFACE T/E UPPER ACCESS PANEL 510 SHOWS EXTERNAL SKIN DELAMINATED STA XA 475.000- XA 507.000. REMOVED AND REPLACED T/E UPPER ACCESS PANEL 510 ON LT WING UPPER SURFACE, STA XA 475.000- XA 507.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521000952003052100095NM 2003 5 21 DHL2003747503 120030513A5311 FRAME BOEING727 727224 1384076NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR FRAME AT BS 580 SHOW GOUGE AREA BETWEEN ST 17R/16R. BLENDED AREA FOUND WITH OUT LIMITS IAW B-727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7-75 T-6 .063 DIM 7 X 6.5 INCH PO 9912495. TREATED AND PRIMED ALL PARTS AND AREAS IAW B-727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B-727 SRM 51-40-3 AT FRAME BS 580 BETWEEN ST 17R/16R. 2L73 4F A3WE 20030521001472003052100147NM 2003 5 21 SWAA031056 120030511A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 3, ABOVE STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030521001562003052100156WP 2003 5 21 DHL2003604510 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBOARD L/E FORMER AT STA XFS 597.000 WITH 0.500 INCH CRACK. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001852003052100185WP 2003 5 21 DHL2003604520 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING INBOARD L/E FORMER CRACKED 0.500 INCH, STA XFS 641.250. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001882003052100188EU 2003 5 21 AWXA200300539 120030515A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 221 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28667AW 1710 DURING 4-DAY CHECK THE FORWARD CABIN EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) BATTERY PACK IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030521001902003052100190EU 2003 5 21 AWXA200300541 120030427A5320D53070011 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y254, FR-16 -17, RBL 254MM. UPON FURTHER INSPECTION A .625 INCH CRACK WAS FOUND IN SAME LOCATION; MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM Y254, FR-16 -17, RBL 254MM; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 211-212 FIG 202. 2L72 4F RTA28NM 20030521001992003052100199NM 2003 5 21 SWAA031062 120030512A53156546804 FLOORBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, WL 208 & LBL 5. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20030522000052003052200005NM 2003 5 22 0300946632 120030507A5412 BULKHEAD BOEING747 747251B 1384892NM NACELLE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 23112 DURING H-CHECK FOUND CRACK IN NR 4 PYLON REAR MOUNT BULKHEAD WEB AT NACELLE STATION 221. REPAIRED PER EA 66-165066. 2L74 4F A20WE 20030522000122003052200012SO 2003 5 22 C2XA03TY061 120030517A531514522159003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE RIGHT SIDE OF RAMP AT FR20 AND CROSSBEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2L72 4T RTT00011AT 20030610001182003061000118SW 2003 6 10 HEEA087015 120030604A6230406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH625 53147 WORN BUSHINGS. REPLACED 4 EACH BUSHINGS 406310406101 DUE TO WORN. REPAIRED. 1G71 3U O H2SW 20030610001222003061000122SW 2003 6 10 HEEA087019 120030604A6230406010427109 GIMBAL RING BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 CORROSION BLEEDING OUT OF STEEL BUSHINGS THAT ARE INSERTED INTO THE ALUMINUM GIMBAL. TO BE SENT TO BELL FOR CREDIT. 1G71 3U O H2SW 20030610001232003061000123SW 2003 6 10 HEEA087020 120030604A6230406010428109 BUSHING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR HEAD BUSHINGS WORN. 1G71 3U O H2SW 20030611000172003061100017WP 2003 6 11 GTIA030325 120030506A3397 WIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE EMERGENCY LIGHT BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 AFT STAIRWAY OVERHEAD EMERGENCY LIGHT IS INOPERATIVE DUE TO A BROKEN WIRE. REPAIRED WIRE AT AFT STAIRWAY OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL. 2L72 4F4 FRTA6WE E2EA 20030611000192003061100019WP 2003 6 11 GTIA030327 120030429A5321 FLOORBOARD DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE CABIN CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FLOORBOARD MAIN CABIN STA 826-927 LT, CRACKED. STOP DRILLED CRACK. FABBED REPAIR DOUBLER. INSTALLED REPAIR PARTS. 2L72 4F4 F A6WE E2EA 20030611000362003061100036 2003 6 11 MEX2003164 420030508A34604034233901 COMPUTER DOUG MD88 MD88 3023688NM COCKPIT FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW03XATXC 49389 AIRCRAFT RETURN TO PLATFORM DUE TO LOSS OF FLIGHT DIRECTOR BUS. THE DFGC BRAKERS WERE RESET AND THE CODE FAIL INDICATES CADC NR 1 AND LEADING ANGLE TRANSMITTOR NR 1 DAMAGED. THE DFGC NR 1 WAS REPLACED IAW MM 22-01-01. DURING OVERNIGHT SERVICE BOTH DFGC WERE TESTED IAW MM 22-01-03, ALL CORRECT. 2L72 4F RTA6WE 20030611000672003061100067 2003 6 11 HEEA086551 420030522A3413457400MA1311 INDICATOR SKRSKYS76 S76A 8143006NE VERT SPEED INOPERATIVE B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 INDICATOR INTERMITTENTLY INOPERATIVE AND WILL READ 300 FEET PER MINUTE ERROR. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030611000962003061100096 2003 6 11 HEEA086704 420030522A2340A3016W INTERPHONE BELL 412 412 1182202SW COMM SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 RPM AUDIO WEAK. SHOP REPAIR. 1G72 4U H4SW 20030611000992003061100099 2003 6 11 HEEA086707 420030522A3442MI585202 PEDESTAL BELL 412 412 1182202SW PWA PT6 PT6* 52043EA ANTENNA INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 ANTENNA PEDESTAL INTERMITTENT ANT FAULT WITH BLANK SCREEN. SHOP REPAIR. 1G72 4U3 T H4SW E2NE 20030611001042003061100104EU 2003 6 11 I05R086500 120030512A65407052A3632279 CHIP DETECTOR UROCOPEC135 EC135P1 8680990EU T/R GEARBOX INOPERATIVE E I05RO OTHER O OTHER NRNOT REPORTED 1 FS01135BP45 0197 TAIL ROTOR GEARBOX CHIP CONTINUITY CAUTION, REPLACED DETECTOR. 1G72 3U O H88EU 20030611001062003061100106EU 2003 6 11 HEEA086710 120030521A642010531821 BEARING BOLKMS105 BO105S 5626006EU CONTROL ROD ASSYWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037170D S840 CONTROL ROD HAS WORN BEARINGS. REPLACED 2 EACH 11-6488P BEARINGS DUE TO WORN; 2 EACH 11-3943P BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030611001072003061100107EU 2003 6 11 HEEA086711 120030521A642010531821 BEARING BOLKMS105 BO105S 5626006EU CONTROL ROD ASSYWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037170D S840 CONTROL ROD HAS WORN BEARINGS. REPLACED 1 EACH 116488P BEARINGS DUE TO WORN; 1 EACH 11-3943P BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030611001152003061100115EU 2003 6 11 2003FA0000534 120030512A2710 BEARING GROB 120 G120A 1660208EU AILERON LEVER FAILED B VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP07861AF841 85001 DURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING. PROBABLE CAUSE IS A DESIGN FLAW IN THE CONTROL ROD DEFLECTION TO EXCEED THE DESIGN LIMIT OF THE BEARING. RECOMMEND DESIGN CHANGE OR REPLACE BEARING WITH ONE THAT HAS BETTER LIMITS AND LOAD HANDLING CAPABILITIES. 1L71 3O RTA49CE 20030609001062003060900106SO 2003 6 9 C2XA03SH148 120030523A531514522461011 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE DOUBLER ON THE RIGHT HAND FLOORBEAM AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030609001112003060900111EU 2003 6 9 03139332 120030519A3350 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27332UE 41100 DURING MAINTENANCE INSPECTION, PASSENGER DOOR EMERGENCY SIGN DIDN'T ILLUMINATE. MAINTENACE PERSONNEL REMOVED AND REPLACED POWER SUPPLY UNIT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTA41NM 20030522000272003052200027WP 2003 5 22 0300969861 120030508A2780 CONTROL CABLE DOUG DC9 DC951 3022051WP NR 1 & 2 SLATS OUT OF RIG A NWAAK NONE O OTHER ININSP/MAINT 1 GL01770NC 47758 ON INITIAL SLAT EXTENSION THE AIRCRAFT ROLLED TO THE RIGHT AND THE BLUE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE SLAT EXTEND INDICATOR DID NOT ILLUMINATE. AFTER ABOUT 45 SECONDS THE EXTEND DID LIGHT UP AND THE DISAGREE EXTINGUISHED. FLIGHT CONTROL WAS NORMAL AFTER THAT AND THE LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE SLAT CONTROL CABLES HAD LOW TENSION AND THE NR 2 SLAT DRIVE STOP WAS HITTING. ALL OF THE SLAT CABLES WERE RIGGED AND THE STOPS ADJUSTED. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F RTA6WE 20030522000322003052200032WP 2003 5 22 0301011226 120030517A3350 BATTERY PACK DOUG DC10 DC1030 3023501WP EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01226NW 46583 ZONE-B EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERHEAD BATTERY PACK AT DOOR 3L. 2L73 4F A22WE 20030522000552003052200055SO 2003 5 22 C2XA03TY053 120030517A532014522460015 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 TYS, DURING A SCHEDULED INSPECTION THE AFT GUSSET IN THE GALLEY WAS FOUND CORRODED AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB-135/145 SRM 51-40-02 AND CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000652003052200065SO 2003 5 22 C2XA03TY059 120030517A531514521718003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE LOWER RAMP ANGLE ON OMEGA BEAM WAS FOUND CORRODED AT FR20. MAINTENANCE REMOVED AND REPLACED THE LOWER RAMP ANGLE IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000742003052200074SO 2003 5 22 C2XA03TY055 120030517A531514525422001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE LEFT AFT OUTBOARD FLOORBEAM IN LAV HAS CORRODED INSERTS AND SURFACE OXIDATION. MAINTENANCE REMOVED AND REPLACED THE CARBON FLOORBEAM IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000822003052200082WP 2003 5 22 GTIA030301 120030417A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 FORWARD LAV PARTITION MODULE ASSEMBLY CORRODED AT LOWER BASE PANEL SUPPORT. FABRICATED NEW FLOOR PANEL SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030522000872003052200087WP 2003 5 22 GTIA030311 120030414A5320 WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT PIT STA 1150 TO STA 1220 WEB CORRODED. FAB NEW WEB. 2L72 4F4 F A6WE E2EA 20030522000882003052200088NM 2003 5 22 0300835810 120030422A3397 WIRE BOEING757 757351 1384991NM EMERGENCY LIGHT SHORTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01490NW 32990 DURING LINE CHECK EMERGENCY SEAT LIGHTS ROW 26-30 WERE INOPERATIVE. FOUND SHORTED WIRE ON SEAT FRAME 27C. REPAIRED AND REROUTED WIRE AND SYSTEM TESTED GOOD. 2L72 4F RTA2NM 20030522001002003052200100NM 2003 5 22 SWAA031094 120030515A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030522001162003052200116 2003 5 22 CALA0300253 420030518A2565D31393109 SLIDE BOEING757 757224 1384958NM LEFT OVERWING LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW271412015493 27562 INSPECTION FOUND LT OVERWING SLIDE UNLACED AT TOP DURING SYSTEM OPERATION CHECK. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-65-01. 2L72 4F RTA2NM 20030522001262003052200126 2003 5 22 SWAA031128 420030520A256561621469 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030520000502003052000050SO 2003 5 20 SIMA200311305 120030327A5310 BEAM EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY CROSSBEAM (P/N 145-29150-001) AND PROFILE (P/N 145-29150-003) HAVE CORROSION. INSTALLED SERVICEABLE CROSSBEAM AND PROFILE IAW EMB 145 SRM 51-40-06, 51-20-03 AND 51-40-02. (M) 2L72 4T RTT00011AT 20030520001032003052000103NM 2003 5 20 AALA20030442 120030410A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139356 24037 MIA - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520001092003052000109NM 2003 5 20 AALA20030391 120030401A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21360AA 24041 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS 11B, 12B, AND 13B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030520001532003052000153NM 2003 5 20 2003F00281 120030121A5320 RESTRAINT BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND RBL 60, FUSELAGE STATION 680 HAS CRACKED SIDE RESTRAINT. FABRICATED DOUBLER REPAIR. TREATED, PRIMED AND INSTALLED AT FUSELAGE STATION 680, RBL 60. (M) 2L73 4F A3WE 20030522000152003052200015SO 2003 5 22 C2XA03CL100 120030519A33503025101 LIGHT EMB 145 EMB145LR 3260212SO FUSELAGE INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713969 145141 DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT DID NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030522000682003052200068SO 2003 5 22 C2XA03SH135 120030518A532014522460015 STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV DURING C-CHECK THE BUTTSTRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030522000892003052200089 2003 5 22 159PL0030 420030511A2565 BOTTLE BOEING737 737242 1384477NM ESCAPE SLIDE DISCHARGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05159PL 21186 L2 SLIDE PRESSURE READS ZERO. REMOVED AND REPLACED L2 SLIDE PER MM 25-61-311. 2L72 4F A16WE 20030522001172003052200117NM 2003 5 22 CALA0300254 120030518A261320035008300 OVERHEAT SENSOR BOEING737 737824 13844BZNM MLG WW INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW271221811995 28778 THE WHEEL WELL FIRE LIGHT ILLUMINATED WITH THE LANDING GEAR RETRACTED AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE OVERHEAT DETECTION UNIT WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20030523000392003052300039NM 2003 5 23 DL76S030395 120030428A5751 SKIN BOEING767 767332 1382001NM LT AILERON DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27116DL 23275 DELAMINATED SPOT ON LEFT OUTBOARD AILERON. REPAIRED AILERON. 2L72 4F RTA1NM 20030523000452003052300045EA 2003 5 23 QXEA0300572 120030515A5350 LATCH CNDAIRCL600 CL6002C10 1390015EA RADOME DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX- DAMAGED RIVET AT STATION 169.00 ON BOTTOM, ONE INCH LEFT OF LOWER RADOME LATCH .5 INCH AFT OF FRAME FRONT. REPAIRED IAW CRJ-700 SRM 51-25-16 AND 51-42-13. 2L72 4F RTA21EA 20030523000492003052300049NM 2003 5 23 2003UALA00409 120030502A5610 WINDSHIELD BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALAO OTHER O OTHER DEDESCENT 1 WP29542UA 25276 1R COCKPIT WINDSHIELD CRACKED. FIRST OFFICERS WINDSHIELD STARTED ARCING IN LOWER CORNER AND PROGRESSED INTO THE WINDOW UNTIL THE WINDOW SHATTERED. FOD DAMAGED OUTER LAYER OF FIRST OFFICER'S NR 1 WINDSHIELD NEAR CENTER OF WINDSHIELD. THIS DAMAGE RESULTED IN STRESS CONCENTRATION THAT CAUSED OUTER PLY TO FAIL (CRACKED). SUBSEQUENT TO THIS FAILURE, ARCING OCCURRED AT THE BUS-BAR FOLLOWED BY SHATTERING OF OUTER WINDSHIELD PLY AND "R FWD WINDOW HEAT" EICAS MESSAGE. REPLACED FIRST OFFICER'S NR 1 WINDSHIELD ASSEMBLY. NO VISIBLE SIGNS OF MOISTURE INGRESSION WERE PRESENT THAT MAY HAVE CAUSED WINDOW FAILURE. 2L72 4F4 FRTA2NM E17NE 20030523000512003052300051NM 2003 5 23 2003UALA00411 120030505A3350362624 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29904UA 25004 EEL FLOOR LIGHTING INOPERATIVE FROM ROW 15ABC THROUGH AFT GALLEY. *S/D* REPLACED EEL 4 EACH LIGHTS AND EEL CABLE. OPS CHECK OK. 2L72 4F4 FRTA16WE E2GL 20030523000592003052300059 2003 5 23 SWAA031120 420030518A25656567380 LENS BOEING737 7377H4 1384404NM SLIDE COVER LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29700GS 27835 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030523000712003052300071NM 2003 5 23 SWAA031103 120030515A5711654544555 RIB BOEING737 7373H4 1384600NM LT/RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND BOTH LT/RT WINGS RIBS CRACKED ON THE LOWER SECTION AT WBL 135.5. REPAIRED LOWER CHORDS PER SWA EA. 2L72 4F RTA16WE 20030523000772003052300077NM 2003 5 23 SWAA031105 120030516A53156545410366 FLOORBEAM BOEING737 7373H4 1384600NM AFT CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 661, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030523000892003052300089EA 2003 5 23 QXEA0300549 120030511A2612 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 ILLUMINATED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09613QX 10045 PDX-ON FLIGHT NUMBER 2298, FIRE SYSTEM FAULT STATUS MESSAGE. PLACED ON MEL. 2L72 4F RTA21EA 20030523001122003052300112NM 2003 5 23 2003UALA00420 120030512A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29524UA 24977 SKIN DAMAGED AT STA 470 AT STR 23 RT. MAJOR REPAIR - FILLER AND DOUBLER INSTALLED. 2L72 4F4 FRTA2NM E17NE 20030521000422003052100042WP 2003 5 21 DHL2003804903 120030125A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LT WING CTR L/E FORMER UPPER PART AT XFS 297.500 IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000732003052100073WP 2003 5 21 DHL2003804899 120030125A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E FORMER LWR PART WITH CRACK AT STA XFS 297.500. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER ANGLE INNER SIDE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE IAW SRM 57-2-0 PG 9 - 10. 2L74 4F RT4A25 20030521001242003052100124NM 2003 5 21 C1HA200395060 120030514A3350900835A BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FWD RT OVERWING EMERGENCY EXIT LIGHT IS INOP. 2L73 4F A3WE 20030521001532003052100153WP 2003 5 21 DHL2003801017 120030507A5755 PANEL DOUG DC8 DC873F 302199FWP SPOILER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING UPPER SURFACE- LT NR 2 SPOILER UPPER AND LWR SKIN DELAMINATED. REMOVED DELAMINATED LT NR 2 SPOILER IAW MM 27-61-1 PG 201-206. CLEANED AFFECTED AREA IAW SRM 51-1-9 PG 1. FABRICATED PLUG AND DOUBLER (ALUMINUM SPLICE CORE) (7075-T6 AL0.016) IAW SRM 57-2-3 PG 14, PG 6D. BONDED AND CURED IAW SRM 51-1-9 PG 1, PG 4. REINSTALLED LT NR 2 SPOILER IAW MM 27-61-1 PG 204-206. 2L74 4F RT4A25 20030521001582003052100158WP 2003 5 21 DHL2003604502 120030505A535056563512 PANEL DOUG DC8 DC873F 302199FWP WING TO BODY DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING UPPER SURFACE - NR 708 FILLET OUTER SKIN DELAMINATED STA 980.000 - 1040.000. REMOVED AND REPLACED NR 708 FILLET ON RT WING UPPER SURFACE, STA 980.000 - STA 1040.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030522000162003052200016WP 2003 5 22 GTIA030286 120030416A5311 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 CANT 1474 LEFT IN AFT ACCESSORY COMPARTMENT CRACKED FRAME. STOP DRILLED CRACK. FABRICATED DOUBLERS. INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA6WE E2EA 20030522001272003052200127NM 2003 5 22 SWAA031129 120030520A57536546435 SKIN BOEING737 7373T5 1384608NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED C1 CHECK, FOUND RT OUTBOARD AFT T/E FLAP DELAMINATED AT NR 7 FAIRING. REMOVED AND REPLACED RT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030523000202003052300020EA 2003 5 23 QXEA0300565 120030515A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX- DAMAGED RIVET 2 INCHES AFT OF STATION 533.00 ON STRINGER R7 ABOVE RIGHT HAND WINDOW 6. REPAIRED IAW CRJ-700 SRM 51-42-06 AND 51-25-16. 2L72 4F RTA21EA 20030523000502003052300050NM 2003 5 23 2003UALA00410 120030503A4920 APU BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE APU BAY FIRE A UALAO OTHER A FLAME/FIRE ININSP/MAINT 1 WP29957UA 26707 APU CAUGHT ON FIRE AT GATE. AFTER REMOVAL THE APU DISPLAYED VERY LITTLE EVIDENCE OF FIRE. THE FADEC CONTROL UNIT WAS CAPTURED FOR THE DOWN LOAD OF THE NON-VOLITILE MEMORY. DATA INDICATED NO UNUSUAL OCCURENCES DURING THE OPERATION OF THE ENGINE AT THE TIME DOF THE INCIDENT. TEST CELL RUNS TO DATE HAVE PROVEN NO ABNORMAL FUNCTIONING. FURTHER TESTING CONTINUES WITH INTRODUCTION OF THERORETICAL IMPLENTATIONS (INCLUDING SIMULATED TAIL WIND GUSTS) TO PIN POINT CAUSE. THESE ACTION WILL BE FOLLWED BY A COMPLETE DISASSEMBLY AND INSPECTION OF LRU'S. ESTIMATED COMPLETION DATED: JUNE 23, 03. 2L72 4F4 FRTA16WE E2GL 20030523000682003052300068NM 2003 5 23 SWAA031100 120030516A3350101114 LENS BOEING737 7373H4 1384600NM MID CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C1 CHECK, FOUND BOTH LT/RT OVERWING EMERGENCY EXIT LIGHT LENSES MISSING. INSTALLED LENSES PER MM. 2L72 4F RTA16WE 20030523000812003052300081EA 2003 5 23 QXEA0300522 120030426A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 600 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 CKB - UPPER AFT RIGHT WING HAS A RIVET MISSING AT WS 170.83. REPAIRED IAW DRJ 700 SRM 51-42-06. 2L72 4F RTA21EA 20030523000952003052300095EA 2003 5 23 QXEA0300556 120030514A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09613QX1465 1465 10045 BOI - FLIGHT 02457 - CREW RETURNED TO FIELD WHEN THE FORWARD CARGO BAY SMOKE DETECTOR SOUNDED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF SMOKE IN THE CARGO AREA. MAINTENANCE DID FIND THE NUMBER 2 SMOKE DETECTOR CANNON PLUG DISCONNECTED AND RECONNECTED SAME. MAINTENANCE ALSO REPLACED THE NUMBER 3 SMOKE DETECTOR UNIT. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030523001082003052300108NM 2003 5 23 QXEA0300521 120030428A5230 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX-1 INCH LONG GOUGE IN PATCH IN UPPER AFT CORNER OF CARGO DOOR. REPAIRED IAW RD8-52-021 AND DHC8 SRM 51-40-00. 2H72 4T RTA13NM 20030523001242003052300124NM 2003 5 23 2003UALA00432 120030515A3397 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29590UA 28708 EEL LIGHT AFT SECTION FROM ROW 28 IS INOP. POWER FEEDER, BROKEN AT SIDE WALL. REPLACED POWER FEEDER. 2L72 4F4 FRTA2NM E17NE 20030523001382003052300138WP 2003 5 23 DHL2003804880 120030210A5720 ANGLE DOUG DC8 DC873F 302199FWP LT STUB WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT STUB WING CTR L/E ATTACH ANGLE AT STA XS 515.750 WITH 2.000 INCH CRACK. REMOVED DAMAGED ANGLE IAW SRM 51-3-0 PAGE 1. FABRICATED ANGLE (7075-T6 AL 0.080) IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20030523001392003052300139WP 2003 5 23 DHL2003804882 120030203A5754 INTERCOSTAL DOUG DC8 DC873F 302199FWP LT WING LE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E INTERCOSTAL LWR PART WITH 3.000 INCH CRACK STA XFS 10.250 - 335.250. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED INTERCOSTAL ( 7075-T6AL 0.071) IAW SRM 57-2-0 PG 8-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED INTERCOSTAL IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030523001432003052300143WP 2003 5 23 DHL2003804884 120030208A5753 VANE DOUG DC8 DC873F 302199FWP LT WING ELONGATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING OUTBOARD VANE SLOT UPPER SKIN HOLE ELONGATED AT XOLDO 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030110, ED-3221. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, TRIMMED OUT DAMAGED SKIN IAW EODHL 030110, ED-3221, FABRICATED A REPAIR DOUBLER (7075T6 0.071) AND FILLER (7075T6 AL 0.063) IAW EODHL 030110, ED-3221. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER AT LT WING OUTBOARD VANE SLOT UPPER SKIN WITH NEW FASTENERS IAW EODHL 030110, ED-3221 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000012003052700001WP 2003 5 27 DHL2003604517 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBOARD L/E FORMER WITH 0.500 INCH CRACK STA XFS 610.000. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000082003052700008WP 2003 5 27 DHL2003801075 120030410A5751 SKIN DOUG DC8 DC873F 302199FWP LT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING LT AILERON T/E CRACKED 0.500 INCH BETWEEN STA XA 622.00 AND STA XA 662.000. REMOVED AILERON T/E (CRACKED) IAW SRM 51-1-21A PG 3-4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW T/E (2024-T3 AL0.020) IAW SRM 57-8-1 PG 8. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. INSTALLED NEW T/E WITH NEW FASTENERS IAW SRM 51-1-21A PG 3-4. 2L74 4F RT4A25 20030527000132003052700013WP 2003 5 27 DHL2003801034 120030415A5350 FRAME DOUG DC8 DC873F 302199FWP TAIL CONE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 TAIL CONE LT FRAME WITH 0.500 INCH CRACK IN STA 1961.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA 1961.000 IAW SRM 53-1-0 FIG 1B. FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000162003052700016NM 2003 5 27 SWAA031097 120030514A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED FROM BS 390 TO BS 500B, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20030527000182003052700018NM 2003 5 27 VNAA0305008 120030512A5210 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07431JS 3028 DURING CLIMBOUT, THE CREW RECEIVED A MAIN CABIN DOOR LIGHT ON THE RED WARNING PANEL AND RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE MAIN CABIN DOOR ROD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030527000252003052700025NM 2003 5 27 DLM88030319 120030402A2120 ODOR DOUG MD88 MD88 3023688NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27940DL 49813 FOLLOWING TAKEOFF IN ATLANTA AT 6000 FEET AGL FLIGHT ATTENDANT NOTICED STRONG ACRID ODOR OF SMOKE THROUGHOUT CABIN. PERFORMED DUCT BURNOUT PROCEDURE. 2L72 4F RTA6WE 20030527000272003052700027NM 2003 5 27 DL733030321 120030401A53306545767130 SKIN BOEING737 737347 1384647NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 REPAIR OF DENTA DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STRINGER 17L AND 18L AT STA 360. THE DENTED MATERIAL WAS CUT OUT AND TWO EXTERNAL ALUMINUM DOUBLERS WERE INSTALLED PER ER/A 384678-14. 2L72 4F RTA16WE 20030527000332003052700033WP 2003 5 27 DHL2003802005 120030503A2612 CONNECTOR DOUG DC8 DC873 302199CWP NR 2 FIRE LOOP DIRTY A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01802DH 46076 NR 2 ENGINE FIRE SHORT CIRCUIT LIGHT FLASHED ON LOOP-A, LOOP-B OK. INSPECTED ALL LOOPS AND CLEANED CONNECTOR. OPS CHECKED GOOD IAW M/M 26-10-0. 2L74 4F RT4A25 20030527000392003052700039NM 2003 5 27 2003UALA00395 120030426A3620 SHUTOFF VALVE BOEING757 757222 1384956NM PWA 2037 PW2037 NE BLEED AIR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29546UA 25367 RECEIVED LT HI-STG LIGHT AND EICAS MSG. REPLACED HI PRESSURE CONTROLLER AND HPSOV. CONTROLLER OVERPRESUURE SWITCH MALFUNCTIONED. HPSOV HAD NFF. 2L72 4F4 FRTA2NM E17NE 20030527000422003052700042NM 2003 5 27 DL733030328 120030401A533065458001205 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 DURING ACCOMPLISHMENT OF PERMANENT REPAIR OF FUSELAGE SKIN/DOUBLER CRACKING, ADDITIONAL CRACK WAS FOUND IN BOTH. THE DAMAGE WAS TRIMMED OUT AND TWO EXTERNAL DOUBLERS WERE INSTALLED WITH SOLID FASTENERS PER ER/A 366481-14, REV C. 2L72 4F RTA16WE 20030527000542003052700054WP 2003 5 27 DHL2003801053 120030408A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 460.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000582003052700058WP 2003 5 27 AALA20030454 120030413A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21510AM 49804 DFW - DURING OVERNIGHT MIANTENANCE, CEILING EMERGENCY EXIT LIGHTS BY AFT GALLEY DOOR INOPERATIVE. RESEATE CEILING EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000752003052700075WP 2003 5 27 AALA20030286 120030306A33501001191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21575AM 53152 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000862003052700086WP 2003 5 27 AALA20030313 120030313A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2173444 49470 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMEGENCY EXIT PATH LIGHTING AT SEAT 9B INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 9B ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030617001152003061700115EA 2003 6 17 QXEA200300671 120030603A3620 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA BLEED AIR SYS MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09613QX 10045 SJC-ON FLIGHT 2571 RETURNED TO FIELD DUE TO LEFT BLEED DUCT WARNING MESSAGE WITH AURAL MESSAGE. MESSAGE REMAINED ON AFTER 60 SECONDS. AIRCRAFT LANDED WITHOUT INCIDENT. INTEROGATED MDC AND FOUND LEFT BLEED LOOP B OPEN CURCUIT MT138. PERFORMED CONTINUITY CHECK OF LEFT BLEED LOOP AT MT138,MT140,MT203 AND MT142. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030610000202003061000020NM 2003 6 10 2003UALA00439 120030515A3397 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DEFECTIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29658UA 27113 FROM SEAT 30F TO RIGHT AFT LAV AND AFT GALLEY CROSS AISLE FLOOR PROX LIGHTING INOP. REPLACED CABLE - LEAD WIRE. 2L72 4F4 FRTA1NM E24NE 20030630000032003063000003NE 2003 6 30 MALA030184 220030303A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT MALFUNCTIONED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL15451XJ 340B451 AFTER TAKEOFF OF FLIGHT NR 3172 PLN-DTW. RT ENGINE WAS SHUTDOWN BY THE CREW. AIR RETURN TO PLN. AFTER TAKEOFF ABOUT 500 FT AND AS CTOT WAS BEING DIALED DOWN, THE RT ENGINE STARTED MAKING POPPING NOISE. CREW SAW THAT THERE WAS STILL NG, BUT ITT WAS CLIMBING (AT LEAST 960 DEGREES) ALSO GOT MASTER WARNING LIGHT AND RT ENGINE AUTO COARSENED. CREW FOLLOWED QRH AND SHUTDOWN ENGINE. FDR WILL BE DOWNLOADED. SOUNDS LIKE A DECEL STALL. NO OTHER INFORMATION AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20030610000392003061000039EU 2003 6 10 03145327 120030525A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27327UE 41080 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS AT SEAT ROW 2 WERE INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030610000522003061000052WP 2003 6 10 ABXA030164 120030415A55115918000518 SPAR CAP DOUG DC9 DC931 3022065WP HORIZONTAL STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 LEFT HORIZONTAL STABILIZER REAR UPPER SPAR CORRODED JUST INBOARD OF XHS 68. REPAIRED AREA IAW REA D955-47165 AND DC-9 SRM. 2L72 4F A6WE 20030611000342003061100034 2003 6 11 MEX2003162 420030507A2340 HANDSET DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE COCKPIT FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23160PL 49763 THE INTERCOMMUNICATION BETWEEN COCKPIT AND AFTER GALLEY IS NOT CLEAR AND ONLY INTERFERENCE IS HEARD. THE REPORT IS DEFERRED BY MEL 23-8-1, CAT B. 2L72 4F4 FRTA6WE E2EA 20030611000382003061100038NE 2003 6 11 MEX2003170 220030510A7314 FILTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE FUEL PUMP FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW231075T 49724 AIRCRAFT RETURN TO PLATFORM DUE TO LOW ACCELERATION ON ENGINE NR 1. SERVICE ON ACCELERATION CAMERA WAS ACCOMPLISHED IAW MM 73-20-01. DURING OVERNIGHT SERVICE THE FUEL PUMP FILTER PS3 WAS REPLACED AND TEST WAS ACCOMPLISHED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20030611000922003061100092 2003 6 11 HEEA086700 420030522A3421504001790116 GYRO BELL 412 412 1182202SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 GYRO PRECESSES 20 DEGREES. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030611001462003061100146EA 2003 6 11 2003F00367 120030428A2760C16221AA02 INDICATOR CNDAIRCL600 CL6002C10 1390015EA SPOILER FAILED A FDKAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW07504MJ 10066 FRL - FLT 6617 - PHX-OMH, AIRCRAFT RETURNED TO GATE FOR SPOILER/STAB FAULT AND RUDDER LIMITER STATUS MESSAGE. MAINTENANCE REPLACED THE DUAL STANDBY INDICATOR. AIRCRAFT DEPARTED WITH NO OTHER FAILURES. (M) 2L72 4F RTA21EA 20030612000452003061200045WP 2003 6 12 ABXA030180 120030519A5412991224381 BULKHEAD DOUG DC9 DC931 3022065WP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 LEFT FORWARD PYLON BULKHEAD WEB HAD CRACK AT ATTACH FASTENER 20 INCHES FROM FLOOR, LEFT BUTT LINE 54. REPAIRED IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030612000482003061200048WP 2003 6 12 ABXA030171 120030528A2613 CONNECTOR DOUG DC9 DC932 3022066WP OVERHEAT DETECT DAMAGED A ABXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23980AX 47176 AFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURE CHECKLIST AND ANNUNCIATOR REMAINED ILLUMINATED. LANDED WITHOUT INCIDENT. REPLACED CONNECTOR P1-387, AFTER FINDING WIRES SHORTED AND TOUCHING EACH OTHER. TAIL COMPARTMENT WAS COOL UPON ARRIVAL. OPS CHECKED GOOD AT ILN. 2L72 4F A6WE 20030612000602003061200060SO 2003 6 12 SWIA200312034 120030528A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07236SW 120312 RIGHT RUDDER LIMITED TO APPROXIMATELY 1/3 OF FULL TRAVEL DURING INITIAL CLIMB. RUDDER WORKS CORRECTLY WITH BLUE SYSTEM SWITCH TURNED OFF. REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB 120 MM 27-22-02. OPS CHECK GOOD IAW EMB MM 27-20-00. NO DEFECTS NOTED. S/N OFF 0671. 2L72 4T RTA31SO 20030612000662003061200066SO 2003 6 12 C2XA03TY078 120030530A532014525422001 SILL EMB 145 EMB145LR 3260212SO LAV AREA CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 TYS DURING A SCHEDULED 2C INSPECTION THE LT FLOOR SILL IN THE LAV AREA HAD SOME CORROSION. MAINT REMOVED AND REPLACED THE LT FLOOR SILL IN THE LAV, REMOVED AND REPLACED LT CARBON FIBER IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030612000712003061200071NM 2003 6 12 UPS03440714 120030516A5320 INTERCOSTAL BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, COCKPIT - BS 360 - 380 S1 - 2R INTERCOSTAL AFT WEB CRACKED. SUPPORT WEB REPAIRED AS PER SRM 51-40-03 FIG 3. 2L74 4F RTA20WE 20030612000742003061200074NM 2003 6 12 UPS03440717 120030516A531069B031461 SHEAR TIE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C M/D - BS 1500, BET STR 20 - 22R FRAME ATT SHEAR TIE FOUND CRACK. SHEAR TIE REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F RTA20WE 20030612000812003061200081WP 2003 6 12 UPS03840704 120030521A53404750419501N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1200 LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D. 2L74 4F RT4A25 20030617001442003061700144EA 2003 6 17 QXEA0300580 120030510A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - NR 3 COCKPIT SEAT TRACK HAS A NICK IN THE INBOARD EDGE FORWARD OF THE AFT END OF THE TRACK. REPAIRED IAW HORIZON AIR EA R-53-102. 2L72 4F RTA21EA 20030617001752003061700175NM 2003 6 17 QXEA200300688 120030531A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - AFT BAGGAGE DOOR SURROUND, FUSELAGE SKIN EDGE GOUGED APPROXIMATELY 18 INCHES FROM TOP ON AFT EDGE. REPAIRED IAW Q400 SRM 51-25-05, PAGE 208. 2H72 4T RTA13NM 20030617001782003061700178NM 2003 6 17 QXEA200300691 120030603A7110 CHANNEL BOMBDRDHC8 DHC8401 1390041NM LT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - LEFT HAND LOWER COWL (412AB) HAS TWO (LT AND RT HAND) CHANNELS CRACKED AT LOWER END NEAR COWL FLAP ACTUATOR. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030617001902003061700190SW 2003 6 17 HEEA087473 120030612A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW FLOAT BOTTLE BLOWN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 FUSIBLE PLUG BLOWN. 1G71 3U O H2SW 20030617002002003061700200EU 2003 6 17 ERAA087108 120030521A2842VT044 TRANSMITTER BOLKMS105 BO105A EU FUEL QUANTITY MALFUNCTIONED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01291EH S842 FUEL PROBE HAS INCORRECT READINGS. REPLACED CASE ASSEMBLY AND TESTED. 1G72 3U H3EU 20030617002042003061700204SW 2003 6 17 HEEA087306 120030611A6410 BLADE BELL 407 407 1182206SW T/R HUB ASSY PEELING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH5036 53006 53142 PAINT PEELING OFF BLADES. REPAIRED. 1G71 3U O H2SW 20030617002102003061700210SW 2003 6 17 HEEA087309 120030611A6410 BLADE BELL 407 407 1182206SW T/R HUB ASSY DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53209 53198 SEPARATION ON TRAILING EDGE AT THE TIP. REPAIRED. 1G71 3U O H2SW 20030617002162003061700216EA 2003 6 17 QXEA200300694 120030605A5720 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - RIGHT HAND WING AT WS 178.00 HAS CHAFE IN THE WING LEADING EDGE. REPAIRED IAW HORIZON AIR EA R-57-36 AND WVAC EO 601R-57-4070. 2L72 4F RTA21EA 20030617002182003061700218EA 2003 6 17 QXEA200300698 120030531A5754 PANEL CNDAIRCL600 CL6002C10 1390015EA L/E SLAT CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - RIGHT HAND WING SLAT PANEL 1 CHAFED ON OUTBOARD EDGE AFT SIDE. REPAIRED IAW CRJ 700 SRM 51-25-01. 2L72 4F RTA21EA 20030617002212003061700221NM 2003 6 17 QXEA200300733 120030613A1430 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM STRESS PANEL BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX- STRESS PANEL 622CT HAS SPINNING SCREW AND NUTPLATE AT AFT ROW, SIX FASTENERS INBOARD FROM AFT OUTBOARD CORNER. REPAIRED IAW DHC-8 Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030617002242003061700224NM 2003 6 17 QXEA200300736 120030613A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX- LEFT HAND NR 4 FLAP TRACK HAS WEAR OR PITTING ALONG THE INBOARD SURFACE OF TRACK AREA E. WEAR IS LOCATED 13 INCHES AFT OF FLAP FAIRING BRACKET TO 18 INCHES AFT OF FAIRING BRACKET. REPAIRED IAW DHC-8 RD 8-57-988. 2H72 4T RTA13NM 20030617002462003061700246NM 2003 6 17 QXEA200300605 120030501A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - FUSELAGE SKIN HAS SCRAPE THROUGH INTO METAL AT X305, X140-X145 LT. REPAIRED IAW DHC-8 400 RD 8/4-53-505. 2H72 4T RTA13NM 20030617002642003061700264SW 2003 6 17 HEEA087025 120030604A6520406040406109 CASE BELL 407 407 1182206SW T/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH536 53435 TAIL ROTOR GEARBOX CASE HAS EXCESSIVE CORROSION IN AREAS AROUND CHIP PLUG. TO BE SENT FOR CREDIT. 1G71 3U O H2SW 20030617002772003061700277NM 2003 6 17 QXEA200300610 120030506A5753 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - A CHAFE EXISTS OUTBOARD FROM INBOARD FLAP END ON LEFT HAND OUTBOARD FLAP. REPAIRED IAW DHC-8 400 RD 84/57-167. 2H72 4T RTA13NM 20030617002852003061700285SW 2003 6 17 HEEA087319 120030611A5610407030115125 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 WINDSHIELD IS CRAZED. REPLACED WINDSHIELD. 1G71 3U O H2SW 20030613001302003061300130NM 2003 6 13 SWAA031236 120030603A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030612001012003061200101NM 2003 6 12 CALA0300276 120030530A5240 ANGLE BOEING737 737524 1384721NM R-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719638 28899 INSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030612001072003061200107NM 2003 6 12 AT0300016 120030531A3520 OXYGEN MASK BOEING717 717200 1383700NM CABIN DEPLOYED A ZZDAO OTHER O OTHER TOTAKEOFF 1 SO15994AT 55138 IMMEDIATELY AFTER TAKEOFF ALL PASSENGER'S OXYGEN MASKS DEPLOYED. REPACKED PASSENGER'S OXYGEN MASKS AM 35-23 AND PERFORMED FUNCTIONAL TEST OF PASSENGER MASK RELEASE SYSTEM, OPS NORMAL AMM 35-22 AND FIM 35-20 TASK 804. 2L72 4F TRA6WE 20030612001112003061200111NM 2003 6 12 UPS03240749 120030515A5312 WASHER BOEING727 727185C 138406NNM PRESSURE PANEL MISSING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, AIR LEAK AT NWW PRESSURE PANEL, RT FWD PANEL. PANEL REMOVED IAW MM 20-80-01. FIBRE WASHERS FOUND TO BE MISSING & REPLACED IAW IPC 25-53-00. ON FURTHER INVESTIGATION CRACK FOUND ON NWW SIDE WALL. AREA CUT OUT IAW SRM 51-40-2. REPAIRED AREA IAW SRM 51-40-2. LEAK CHECKED REPAIR AREA AND PANEL IAW MM 21-30-01. NO LEAKS FOUND. 2L73 4F A3WE 20030612001172003061200117NM 2003 6 12 UPS03440761 120030519A531069B028035 SHEAR TIE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 1020 FRAME SHEAR TIE FOUND CRACKED BETWEEN S-9R AND S-11R. M/D BS 1020 S9R-S11R FRAME SHEAR TIE (2EA) REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030612001272003061200127NM 2003 6 12 UPS03440773 120030519A5310 SHEAR TIE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 1020 FRAME SHEAR TIE FOUND CRACKED BETWEEN S-8R AND S-9R. M/D BS 1020 FRAME SHEAR TIE 1 EA REPLACE AS PER SRM 51-10-01 BETWEEN S-8R AND S-9R. 2L74 4F RTA20WE 20030612001282003061200128NM 2003 6 12 UPS03440774 120030513A5510 WEB BOEING747 747200 1384847NM HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, EMP - LT HORIZONTAL STAB TIP FAIRING SUPPORT STRUCTURE VERTICAL WEB IS FOUND CRACKED AT APPROX 10 INCHES AFT OF HS REAR SPAR AT HSBL 421.5. EMP - LT HORIZONATAL STAB TIP FAIRING SUPPORT STRUCTURE VERTICAL WEB REPAIRED AS PER HX RS R55-13-35021 (UPS EO 747-55-20001). 2L74 4F RTA20WE 20030612001292003061200129NM 2003 6 12 UPS03440775 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 2340 - 2360 STR 12R STRINGER END CRACKED. CRACKED STRINGER TRIMMED OUT AS PER SRM 51-10-01 AND PERFORM STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F RTA20WE 20030610000012003061000001EU 2003 6 10 HEEA086720 120030521A243651565000R VOLT REGULATOR BOLKMS105 BO105S 5626006EU INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 VOLTAGE REGULATOR INOPERATIVE. 1G72 3U H3EU 20030610000082003061000008NM 2003 6 10 CALA0300266 120030524A4900380029815 APU BOEING757 757224 1384958NM APU BAY SHUTDOWN A CALAO OTHER J WARNING INDICATION CRCRUISE 1 SW27141202189910494 27562 THE APU AUTO SHUTDOWN ON TWO START ATTEMPTS AT FL 35. APU START WAS SUCCESSFUL AT FL 15. THE APU ASSEMBLY WAS REMOVED AND REPLACED IAW MM 49-11-01. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20030610000842003061000084NM 2003 6 10 DL757030425 120030503A5330143N33203 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27609DL 22816 THE SKIN WAS FOUND WITH 4 DENTS BETWEEN FS 601 & 630 AND BETWEEN STRINGERS 15L & 16L. THE DENTS WERE REMOVED WITH 4 SMALL CUTOUTS AND REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384778-14, REV A. 2L72 4F RTA2NM 20030610001012003061000101GL 2003 6 10 HEEA086995 220030603A732023007827 VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 VALVE ASSY STUCK IN OPEN POSITION. REPLACED. 1G71 3U3 UO H2SW E1GL 20030611000062003061100006CE 2003 6 11 FDJ2003F00000 120030515A215012503273 WHEEL CESSNA208 208B 2073701CE PWA PT6 PT6A11 52043NE BLOWER ASSY FAILED E FDJAO OTHER O OTHER NRNOT REPORTED 1 SO15126AR303 208B1004 PILOT REPORTED NO AIR MOVEMENT FROM EYE BALL VENTS WHEN AIR CONDITION WAS SELECTED. TROUBLESHOOTING REVEALED LEFT AND RIGHT WHEEL ASSEMBLIES HAD FAILED AT BLOWER ASSEMBLY SHAFT ATTACHMENTS. THE WHEEL IS MANUFACTURED FROM LIGHT/THIN ALUMINUM AND THE PLATE THAT ATTACHES TO BLOWER SHAFT APPEARS UNABLE TO SUPPORT THE VIBRATION EXPERIENCED DURING NORMAL USE. 1H71 3T3 T A37CE E4EA 20030611000232003061100023WP 2003 6 11 GTIA030321 120030414A5313 STRINGER DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FORWARD CARGO STRINGER 28L CORRODED FS 428. FAB STRAP. INSTALLED STRAP. 2L72 4F4 F A6WE E2EA 20030611000272003061100027WP 2003 6 11 GTIA030318 120030415A5310 DOOR FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT PIT STA 1155 FORWARD DOOR FRAME CORRODED. REMOVED DAMAGED AREA. FORMED REPAIR. INSTALLED 2 REPAIR PIECES. 2L72 4F4 F A6WE E2EA 20030611001612003061100161NE 2003 6 11 MALA030282 220030524A7530211C119136A PRESSURE SWITCH SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15453XJ 340B453 DURING FLIGHT 3009, RT HP BLEED VALVE LIGHT ILLUMINATED. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RT BLEED PRESSURE SWITCH P/N 211C119-136A, IAW AMM 36-22-10-2. OPS CHECKS GOOD. REMOVED FROM DMR MXC NOTIFIED. 2L72 4T4 TRTA52EU E8NE 20030612000892003061200089WP 2003 6 12 UPS03840713 120030528A3350 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 EMERGENCY EXIT LIGHT COME ON AND GO OFF DURING FLIGHT. ALL OTHER INDICATIONS NORMAL. TROUBLESHOT EMERGENCY EXIT LIGHTS. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AND RELAY UNIT. PERFORMED OPERATIONAL TEST PER MM 33-50-01. OK FOR SERVICE. 2L74 4F RT4A25 20030612001342003061200134WP 2003 6 12 UPS03840722 120030505A53405643483502N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, MAIN CABIN - FLOORBEAM TO FUSE ATTACHMENT FRAME STA 915 RBL 66 APX CORRODED. REMOVED CORROSION ON FRAME FITTING, OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED FITTING, LOCATED, DRILLED, AND DEBURRED FITTING IAW DAC DWG 5643483. INSTALLED FRAME FITTING IAW DC8 SRM 51-1-20D, 51-3 -0 AND DAC DWG 5643483. 2L74 4F RT4A25 20030612001442003061200144WP 2003 6 12 UPS03840733 120030503A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, L2 DOOR JAMB UPPER AFT CORNER CRACKED 1 EA MARKED FOUND WITH NDT. FAB AND INSTALLED -11, -13 DOUBLERS AND -23 FILLER IAW DC8 SRM 53-2- 0 FIG 18. ALSO, INSTALLED INTERCOSTAL TO SKIN ATTACH ANGLE WEB AND 2 END FITTINGS AT APPROX L10L-L11L FS 1640 LT. 2L74 4F RT4A25 20030612001562003061200156WP 2003 6 12 UPS03840745 120030514A5510 CAP DOUG DC8 DC873F 302199FWP L/H HORZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C-2 LT HORIZ STAB INBOARD LOWER CAP CRACKED. REMOVED LT HORIZ L/E CAP, PERFORMED HEFC IAW NDT SPM 06-10-001.01. LOCATED & DRILLED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21/51-1-20D. 2L74 4F RT4A25 20030612001622003061200162WP 2003 6 12 UPS03840760 120030521A53404750419U501 ATTACH FITTING DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED STA 1152 LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612001632003061200163WP 2003 6 12 UPS03840779 120030520A5240 WEB DOUG DC8 DC871F 302199DWP R-1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, 1.25 INCH CRACK UPPER LEFT INNER WEB R-1 DOOR AT STA 156 LONG 12R TO 13R ON DOOR. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 52-2-0 FIG 1B. 2L74 4F RT4A25 20030612001812003061200181NM 2003 6 12 2003UALA00368 120030409A5720 SEAL BOEING777 777222 1385219NM PWA PW4077PW4077 NE RT WING DETERIORATED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29771UA30715 26932 SMOKE APPEARING FROM RIGHT WING. SMOKE WAS ACTUALLY ONE END OF A RUBBER SEAL THAT HAD BECOME DISLODGED AND WAS FLUTTERING AT 500 MPH. DISLODGED PART OF THE SEAL END WAS CUT AND SURFACE REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030612002012003061200201EA 2003 6 12 SWIA200312050 120030530A2751855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07433SW4735 4735 7550 ON TAXI IN RETRACTING FLAPS FROM 30 DEGREES TO 20 DEGREES, RECEIVED FLAPS FAIL MESSAGE AND FLAPS REMAINED AT 30 DEGREES. REMOVED AND REPLACED RIGHT BPSU IAW MM 27-51-10. 2L72 4F RTA21EA 20030612002022003061200202EA 2003 6 12 SWIA200312051 120030526A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07916SW 7634 EMERGENCY LIGHT INOP IN CEILING OF PAX CABIN. INSTALLED NEW BULB, OPS CHECK GOOD. 2L72 4F RTA21EA 20030612002032003061200203SO 2003 6 12 SWIA200312052 120030525A326012041890015 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO MLG FAILED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07235SW 120310 ON GEAR RETRACTION RIGHT MAIN SYSTEM-A GREEN LIGHT REMAINS ILLUMINATED. REMOVED AND REPLACED RIGHT MAIN GEAR DOWNLOCK PROX SENSOR IAW MM 32-61-01. OPS CHECK GOOD. P/N 120-41127-001. 2L72 4T RTA31SO 20030613000042003061300004EA 2003 6 13 SWIA200312057 120030529A2751855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAP FAILED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07945SW504 504 7770 ON TAXI TO THE TERMINAL, FLAP FAIL MESSAGE APPEARED. REPLACED RIGHT BRAKE POSITION SENSOR UNIT AND RIGGED IAW 27-51-10. FLAP SYSTEM TEST GOOD. 2L72 4F RTA21EA 20030613000122003061300012 2003 6 13 MALA030285 420030519A34256226342022 DISPLAY SAAB SF340 340B 7860101EU COCKPIT INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15439XJ 340B439 DURING FLIGHT 2935 A/C REPORTED THE F/O'S EADI SCREEN WENT BLANK INFLIGHT. OVERFLEW ABR TO GET INTO MSP. A/C DIVERTED TO MSP. MAINTENANCE REPLACED NR 2 EADI (P/N 622-6342-022) (S/N OFF 5241) (S/N ON 3641). NR 2 EFIS CHECKS GOOD. 2L72 4T RTA52EU 20030613000232003061300023NM 2003 6 13 UPS03440786 120030519A5310 SHEAR TIE BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, AFT CARGO STA 1840 STR 45R TO 46R SHEAR TIE CORROSION REVEALED. CORROSION BLEND OUT 0.040 X 1 X 2 INCH. SHEAR TIE BRACKET REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030613000272003061300027WP 2003 6 13 UPS03840790 120030603A3350 BATTERY DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND RELAY UNIT PER MM 33-50-01. 2L74 4F RT4A25 20030613000442003061300044SO 2003 6 13 SWIA200312065 120030424A5753 BRACKET EMB 120 EMB120ER 3260203SO TE FLAPS CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07220SW 120288 RIGHT INBOARD LOWER FLAPWELL, INBOARD ROLLER BRACKET CRACKED. DISCOVERED DURING C-CHECK. REPLACED AFFECTED BRACKET IAW EMB120 SRM 51-10-02. 2L72 4T RTA31SO 20030613001552003061300155NM 2003 6 13 SWAA031214 120030602A5313BAC1498 STRINGER BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 179, STR 17L. REPAIRED STRINGER PER SRM. 2L72 4F A16WE 20030617000432003061700043EA 2003 6 17 QXEA200300652 120030513A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA LT WING GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - LEFT WING, LOWER WING SKIN AT WS 128.00 HAS A GOUGE. REPAIRED IAW AMM 51-25-01. 2L72 4F RTA21EA 20030617000612003061700061EA 2003 6 17 QXEA200300658 120030523A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - LEFT PRESSURE BULKHEAD WEB BL 34-41 STRINGER 8-9 CRACKED. REPAIRED IAW CRJ 700 AMM TASK 21-21-00-710-801 AND REO 670-53-61-034. 2L72 4F RTA21EA 20030617001012003061700101NM 2003 6 17 QXEA200300681 120030608A7110 WEB BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - NR 1 LOWER COWL AFT CONE VERTICAL WEB UPPER LEG CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030617001372003061700137GL 2003 6 17 ERAA087097 220030520A7323252466715 GOVERNOR BOLKMS105 BO105A EU ALLSN 250C 250C20B 03013GL ENGINE STIFF E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01135EH S675 GOVERNOR HITS MAX STOP WITH MAX BEEP AND UP COLLECTIVE AND ARM VERY STIFF. HEAVY WEAR ON INTERNAL COMPONENTS MAY BE DUE TO EXTERNAL VIBRATION SOURCES. WORK SCOPE CHANGED TO OVERHAUL DUE TO SEVERITY OF WORN COMPONENTS. OVERHAULED IAW HONEYWELL OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20030617001542003061700154NM 2003 6 17 QXEA200300711 120030608A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - DENT ON FUSELAGE SKIN EXTERIOR, RIGHT SIDE OF AIRCRAFT. REPAIRED IAW RD 8/4-53-606. 2H72 4T RTA13NM 20030617001562003061700156NM 2003 6 17 QXEA200300715 120030601A5512 SKIN BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FRONT SPAR AND Y605D-52.96. REPAIRED IAW Q400 SRM 51-21-10, PAGES 204-205 AND SRM 51-25-10, PAGES 201-205. 2H72 4T RTA13NM 20030617001992003061700199NM 2003 6 17 QXEA200300725 120030612A5210D5D592395926 STRUT DHAV DHC8 DHC8202 2809007NM PAX DOOR WORN A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09363PH114271122 520 SEA-ON FLIGHT NUMBER 2185, FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED GAS STRUTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617002712003061700271SW 2003 6 17 HEEA087029 120030604A6310406040500131FM FREEWHEEL UNIT BELL 407 407 1182206SW MAIN ROTOR VIBRATES E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW03457PH3195 53147 HIGH FREQ VIBRATION. REPLACED BEARING 406-040-532-103, S/N 0507 DUE TO WEAR LINE ON ROLLERS AND ROUGH; SEAL 214-040-841-101 DUE TO LEAKING. REPAIRED. 1G71 3U O H2SW 20030617002802003061700280SW 2003 6 17 HEEA087315 120030611A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH385 53038 BLADE APPEARS CRACKED AT ROOT END OF BLADE WHERE PROTECTIVE LEADING EDGE STRIP BEGINS. 1G71 3U O H2SW 20030617002962003061700296SW 2003 6 17 HEEA087036 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030617002982003061700298WP 2003 6 17 GTIA030363 120030505A5730 PANEL DOUG DC9 DC982 3022082WP LT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND LEFT WING INNER WING UPPER AFT TRAILING EDGE TRAP PANEL CRACKED/DAMAGE TO COMPOSITE MATERIAL. REPAIRED CRACK/DAMAGED AREA. (M) 2L72 4F A6WE 20030617003092003061700309NM 2003 6 17 SWAA031265 120030605A3350BR2013 STRIP BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29400WN 27891 DURING SCHEDULED C3 CHECK, FOUND EEPLS SECTION CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20030617003152003061700315SW 2003 6 17 HEEA087482 120030612A6321D01641 BOLT BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 ROTOR BRAKE BOLT WORN. 1G71 3U O H2SW 20030617003162003061700316NM 2003 6 17 SWAA031269 120030607A33506104789 BATTERY BOEING737 7372T4 1384492NM CARGO BAY DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030613000462003061300046SO 2003 6 13 SWIA200312067 120030424A5330 SKIN EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07220SW 120288 ANGLE BEHIND CAPTAIN'S DV WINDOW CUTOUT CRACKED. DISCOVERED DURING C-CHECK. REPLACED BRACKET IAW SRM 120 51-10-02. 2L72 4T RTA31SO 20030613000592003061300059NM 2003 6 13 UPS03440793 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, BULK CARGO STA 1960 S47R STRINGER END CORROSION CRACKED. STRINGER REPAIRED AT BS 1960 - 1990 STR 47R AREA AS PER SRM 53-10-03 FIG 1 DUE TO CORROSION CRACK .3125 INCH LENGTH OUT OF SRM FIG 1 LIMITATION. 2L74 4F RTA20WE 20030613000612003061300061NM 2003 6 13 UPS03440795 120030520A531465B15069418 STIFFENER BOEING747 747200 1384847NM KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FX KEELBEAM BOX RT STIFFENER FOUND CORROSION CRACKED AT STA 1460 RBL 6. FX KEEL BEAM BOX AT RBL 6 STA 1460 STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. DUE TO CORROSION CRACK TO STIFFENER OUT OF SRM 53-10-01 FIG LIMITED NEED TO BE CHANGED. DAMAGED AREA .75 X 1.5 X 0.032 INCH MAT'L REMAINED. 2L74 4F RTA20WE 20030611000622003061100062EA 2003 6 11 CA030515006 120030514A2910 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE CHAFED W O OTHER KE FLUID LOSS VIBRATION/BUFFET NRNOT REPORTED 1 CA (CAN) THE CREW REPORTED AN ENGINE VIBRATION ON ENGINE NR 2. MAINTENANCE CARRIED OUT A VISUAL INSPECTION OF THE AFT EQUIPMENT BAY AND FOUND HYDRAULIC LINES AND A WIRE CHAFING. THE DAMAGED LINES AND FAIRLEAD WERE REPLACED, THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030611001392003061100139EA 2003 6 11 2003F00362 120030121A7830M8353622025M RELAY CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER FAILED A FDKAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07506MJ 10073 ASH - FLT 6627 - PHX-ELP, ABORTED TAKEOFF, RIGHT THRUST REVERSER UNSAFE MESSAGE. MAINTENANCE REPLACED GROUND RELAY. PERFORMED OPS CHECK OF NR 2 T/R. OPS CHECKED GOOD. (M) 2L72 4F RTA21EA 20030611001552003061100155EA 2003 6 11 JBXA03007 120030527A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A JBXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05593ML 7465 FLIGHT NUMBER 5117 DEPARTING FROM LGA BOUND FOR RDU DIVERTED INTO PHL FOR OUTER DOOR HANDLE MESSAGE AND PAX DOOR LIGHT. OPS CHECKED PAX DOOR AND PRESSURE SYSTEM. OPS CHECKED GOOD IAW 52-11-00. 2L72 4F RTA21EA 20030612000072003061200007SO 2003 6 12 SWIA200312015 120030425A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07295SW 120322 CORROSION ON LEFT INBOARD FLOORBEAM AND SEAT TRACK AT FORWARD END OF SEAT TRACK. FOUND DURING C-CHECK INSPECTION. REPAIRED CORROSION ON LEFT INBOARD FLOORBEAM AND SEAT TRACK AT FORWARD END OF SEAT TRACK. REPAIRED FLOORBEAM IAW SRM 53-00-03 AND REPAIRED SEAT TRACK IAW EMB EST 186/96. NO DEFECTS NOTED. 2L72 4T4 TRTA31SO E20NE 20030612000142003061200014EA 2003 6 12 SWIA200312022 120030417A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 FS 484 LEFT AND RIGHT INTERCOSTALS OUTBOARD FLG LBL 36 CRACKED. FOUND DURING C-CHECK INSPECTION. INTERCOSTALS REPAIRED IAW CRJ REO 601R53-41-059. HFEC C/O IAW 51-20-06/REO 601R-53-41-059 ON REPAIRED AREAS AND BRACKET RADIUS. NO CRACKS NOTED. 2L72 4F RTA21EA 20030612000362003061200036EA 2003 6 12 SWIA200312028 120030521A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 FS 484 LEFT INTERCOSTAL OUTBOARD FLG LBL 36 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-41-059 REV ''A''. 2L72 4F RTA21EA 20030612000472003061200047WP 2003 6 12 ABXA030170 120030524A32604700775 SEAL DOUG DC8 DC863F 302198FWP MLG TORN A ABXAO OTHER O OTHER CRCRUISE 1 GL23811AX 46113 GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. CYCLED GEAR AND LIGHT WENT OUT. RIGHT MAIN LANDING GEAR DOOR IDENTIFIED ON FLIGHT ENGINEER'S LANDING GEAR AND DOOR LATCHING PANEL. CLEANED UP LATCH SWITCH. OPS CHECKED GOOD IAW DC-8 AMM 32-60-00-2. ON WALKAROUND, ALSO FOUND SEAL ON RIGHT MAIN LANDING GEAR TORN. REPLACED TORN SEAL IAW DC-8 MM 32-10-0. 2L74 4F 4A25 20030612000592003061200059 2003 6 12 SWIA200312033 420030526A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07453SW 7743 STALL FAIL CAUTION MESSAGE ILLUMINATED IMMEDIATELY AFTER TAKEOFF. RETURNED TO SLC. REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK GOOD. S/N OFF 982. 2L72 4F RTA21EA 20030612001032003061200103NM 2003 6 12 CALA0300278 120030601A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006 FROM LBL 24 TO LBL 28. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030612001422003061200142WP 2003 6 12 UPS03840731 120030503A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, L1 DOOR FRAME UPPER FWD CORNER CRACKED 4 EA MARKED FOUND WITH NDT. REMOVED CRACKED AREAS IAW DC8 SRM 53-2-0 FIG 15 AND TR 53-128. FABBED DOUBLER, TRIPLER AND FILLER IAW D8 SRM 53-2-0 FIG 15. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED DOUBLER, TRIPLER, & FILLER IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20030612001452003061200145WP 2003 6 12 UPS03840734 120030503A53476015176 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, FWD PIT STA 320 LBL 27 FLOORBOARD, TRACK CORRODED. REMOVED CORROSION, WITHIN LIMITS IAW DC8 SRM 53-2-3. FOUND SCALLOP ON UPPER SURFACE WORN BEYOND LIMITS IAW DC8 SRM 53-2-3. REMOVED AND REPLACED TRACK SECTION IAW DC8 SRM 51-3-0, 53-2-3 FIG 14 AND UPS DWG 53B-0 03. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED UPS SPLICE DC8- 53B-003-501 IAW UPS DWG DC8-53B-003. 2L74 4F RT4A25 20030612001572003061200157WP 2003 6 12 UPS03840755 120030519A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, L-1 UPPER AFT CORNER DOUBLER,TRIPLER DOES NOT CONFORM TO SRM 53-2-0 FIG 15, STA 60 AT LONG 10L. REMOVED EXISTING DOUBLER AND TRIPLER, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 15. 2L74 4F RT4A25 20030617003252003061700325NM 2003 6 17 SWAA031276 120030607A3350BP573 BATTERY BOEING737 7373K2 13844BANM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030617003322003061700332SW 2003 6 17 HEEA087043 120030604A6220406312103101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 MAIN ROTOR LINK WORN. 1G71 3U O H2SW 20030618000052003061800005SW 2003 6 18 HEEA087483 120030612A5320ETCB6A2114X CASE BELL 407 407 1182206SW FUSELAGE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 CORRODED UNDER HEAT SHRINK, UNABLE TO DETECT UNTIL REMOVED. 1G71 3U O H2SW 20030618000162003061800016EU 2003 6 18 HE66087112 120030613A67104012373916 ACTUATOR BOLKMS105 BO105LSA1 5626021EU PITCH DEFECTIVE H HEEAO OTHER O OTHER NRNOT REPORTED 1 FS01202LF 2014 PITCH CSAS FAILED REPLACED ACTUATOR. 1G72 3U H3AU 20030618000202003061800020NE 2003 6 18 HEEA087122 220030610A72500292727180 CHECK VALVE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE ENGINE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 ENGINE LEAKS OIL STATICLY FROM BURNER CAN. 1G72 3U3 UNCH1NE E19EU 20030618000232003061800023SW 2003 6 18 HEEA087332 120030611A6510 BEARING BELL 407 407 1182206SW T/R DRIVE SHAFT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH3063 A1855 53378 BEARING MOUNT AREA HAS DAMAGE. REPLACED. 1G71 3U O H2SW 20030618000472003061800047 2003 6 18 SWAA031315 420030611A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT CABIN DOORS OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2L72 4F A16WE 20030618000512003061800051NM 2003 6 18 SWAA031337 120030615A335065C27093 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT MID CABIN INOP. REMOVED AND REPLACED EMERGENCY LIGHT BASE ASSY PER MM. 2L72 4F A16WE 20030618000542003061800054NM 2003 6 18 SWAA031338 120030614A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT OVERWING EXIT. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030618000572003061800057SW 2003 6 18 HEEA087339 120030611A6510206061432117 BEARING BELL 407 407 1182206SW BLOWER SHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH PHI0009 53399 FWD BLOWER BEARING ROUGH. REPLACED SHAFT ASSY. 1G71 3U O H2SW 20030618000592003061800059SW 2003 6 18 HEEA087340 120030611A6510407040303119A SHAFT BELL 407 407 1182206SW T/R BLOWER OVERHEATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 BLACK GREASE. REPAIRED. 1G71 3U O H2SW 20030618000722003061800072NM 2003 6 18 SWAA031296 120030609A551265C25727 SKIN BOEING737 7375H4 138449DNM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED C4 CHECK, FOUND BOTH LEFT AND RIGHT HORIZ STAB SKIN CRACKED ON LOWER SURFACE AT REAR SPAR ATTACHMENT POINT, LEFT AND RIGHT AT STA 145 AND RT AT STA 152. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030618000732003061800073NE 2003 6 18 HEEA087130 120030610A632140004769R CALIPER SKRSKYS76 S76A 8143006NE ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 WORN PUCKS - SLOW TO RELEASE. SHOP REPAIR. 1G72 3U H1NE 20030618000932003061800093SW 2003 6 18 HEEA087347 120030611A6320407040628101 TUBE BELL 407 407 1182206SW M/R GB OIL SYS KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 MAIN ROTOR GEARBOX OIL TUBE KINKED NEAR RADIUS. 1G71 3U O H2SW 20030617000382003061700038CE 2003 6 17 AUS20030490 120030508A7797 FUSE BBAVIA8 8KCAB 2110612CE LYC O360 AEIO360* EA AMTR C8289 C8289 GL HOURMETER DISCONNECTED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE HOURMETER INLINE FUSE HOLDER DISCONNECTED. 1H71 3O3 O A21CE 1E10 5 NEXPP5N 20030617000792003061700079NE 2003 6 17 AUS20030498 220030509A7310AE7074221 HOSE AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE ENGINE FUEL DISTLEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE MAIN FUEL FEED HOSE LEAKING THOUGH UPPER BRAIDED AREA. 2L72 4F4 FRTA46NM E29NE 20030617001402003061700140EA 2003 6 17 QXEA200300583 120030507A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA LT WING LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - LOOSE RIVET ON LT HAND WING, OUTBOARD OF THE OUTBOARD SPOILER. REPAIRED IAW CRJ-700 SRM 51-42-06, PAGES 1-18. 2L72 4F RTA21EA 20030617001412003061700141GL 2003 6 17 ERAA087099 220030520A72506898735 COMBUST CHAMBER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE CRACKED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01125EH12230 S562 TURBINE HAS LOW POWER. HAS CRACKED ARMPIT ON COMBUSTION CASE. INSTALLED SERVICEABLE COMBUSTION CASE. 1G72 3U3 U H3EU E4CE 20030617001422003061700142EA 2003 6 17 QXEA200300584 120030511A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - FORWARD PASSENGER DOOR HAS SCRATCHES IN PAINT AROUND DOOR ON FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA R-53-100. 2L72 4F RTA21EA 20030617002232003061700223NM 2003 6 17 QXEA200300735 120030613A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX- LEFT HAND NR 4 FLAP TRACK HAS TWO LOW AREAS OF WEAR ON LOWER SURFACE OF TRACK. WEAR POINTS ARE .50 & 7.00 INCHES AFT OF FLIP FAIRING SUPPORT BRACKET. REPAIRED IAW DHC-8 RD 8-57-988. 2H72 4T RTA13NM 20030617002262003061700226EA 2003 6 17 QXEA200300696 120030531A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA RT AILERON CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - RIGHT HAND AILERON LEADING EDGE UPPER SURFACE CHAFED. REPAIRED IAW CRJ 700 SRM 51-25-01. 2L72 4F RTA21EA 20030617002352003061700235EA 2003 6 17 QXEA200300693 120030604A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - FOUND CRACKS IN AFT BULKHEAD WHILE PERFOMING HYDRAULIC FLEX INSTALL ON RIGHT HAND WEB. REPAIRED IAW HOEIZON AIR EO R-53-114. 2L72 4F RTA21EA 20030617002722003061700272SW 2003 6 17 HEEA087030 120030604A6220406310404101 ROD END BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH4419 53038 MAIN ROTOR HEAD ROD END WORN BEYOND LIMITS. SERIAL NUMBERS REMOVED ARE NH4636, NH4933, NH5056 AND NH5090. TO BE SENT TO MFG FOR CREDIT. 1G71 3U O H2SW 20030618000372003061800037 2003 6 18 SWAA031330 420030613A2565D31354 SLIDE BOEING737 7373Q8 1384670NM ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030618000552003061800055NM 2003 6 18 SWAA031339 120030615A531065C31308 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 STOP. REPAIRED AFT FRAME PER SRM AND SWA TYPICAL REPAIR T1. 2L72 4F RTA16WE 20030618000902003061800090SW 2003 6 18 HEEA087346 120030611A6320407040623101 TUBE BELL 407 407 1182206SW M/R GB OIL SYS LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03501PH 53401 FLARE IS WORN AND UNABLE TO STOP LEAK. 1G71 3U O H2SW 20030618000962003061800096NM 2003 6 18 SWAA031281 120030607A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN FWD CABIN. REMOVED AND REPLACED EEPLS IN FWD CABIN PER MM. 2L72 4F RTA16WE 20030618000982003061800098NM 2003 6 18 SWAA031283 120030609A25606557463 ATTACH FITTING BOEING737 7373H4 1384600NM FWD ENTRY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT ATTACH FITTING CORRODED. REPAIRED FITTING PER SRM. 2L72 4F RTA16WE 20030618001012003061800101NM 2003 6 18 SWAA031286 120030605A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, BETWEEN STR 8L AT STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030618001032003061800103SW 2003 6 18 HEEA087349 120030611A7120407060111101 MOUNT BELL 407 407 1182206SW ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 ENGINE MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030612001602003061200160WP 2003 6 12 UPS03840758 120030521A571446473651 FITTING DOUG DC8 DC871F 302199DWP CENTER WING BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, LT STA 980 FITTING IS CRACKED NEXT TO FUSELAGE ON WING BOX. REMOVED AND REPLACED FITTING IAW DWG 4647365 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612001772003061200177SO 2003 6 12 C2XA03TY081 120030602A532014521725013 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE CLEANED THE AREA, FILLED WITH EPOXY RESIN, FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED A DOUBLER I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-10-02, 51-21-04/05/06 AND GST1927/02A. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030612001782003061200178SO 2003 6 12 C2XA03TY082 120030602A575314568000431 SKIN EMB 145 EMB145LR 3260212SO TE FLAP DELAMINATED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING A SCHEDULED INSPECTION THE LEFT WING INBOARD FLAP BOTTOM SIDE HAS TWO AREAS OF DELAMINATION. MAINTENANCE REPAIRED THE DAMAGED AREAS I/A/W-EC5750-01195, EMB-CMP-51-21-03/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030613000642003061300064NM 2003 6 13 UPS03440800 120030516A5320 REVEAL BOEING747 747200 1384847NM PAX DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - R4 PAX DOOR CUTOUT FWD REVEAL FOUND CRACKED AT LOWER PORTION BETWEEN S-23 AND S-24 AS MARKED. M/D - R4 DOOR CUTOUT FWD REVEAL PANEL BETWEEN S-23R AND S-24R CRACKED REPAIRED AS PER SRM 53-10-04 FIG 84. 2L74 4F RTA20WE 20030613000652003061300065NM 2003 6 13 UPS03440801 120030515A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FX - AIR CONDITIONING BAY REAR FAIRING SKIN SURFACE FOUND CORROSION AT STA 1235 TO STA 1255 RBL 9 TO LBL 9. SKIN REPLACED AS PER SRM 51-10-01 PAGE 8. CORROSION BLEND OUT 0.012 X 4 X 4 INCH. 2L74 4F RTA20WE 20030613000802003061300080SO 2003 6 13 C2XA03SH176 120030608A531514522461003 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR ON THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000812003061300081SO 2003 6 13 C2XA03SH177 120030608A532014522459001 ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 SHV-DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000832003061300083EU 2003 6 13 MALA030294 120030607A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15517XJ E2335 AFTER TAKEOFF OF FLIGHT NR 3546, GREEN SYSTEM HIGH TEMP ILLUMINATED INFLIGHT. USED EMERGENCY GEAR HANDLE. AIR RETURN TO DTW. MAINTENANCE REPLACED NR 3 EDP P/N 521449. RAN AIRCRAFT, ALL CHECKS GOOD AT THIS TIME. ALL IAW ARJ 85 AMM. 2H74 4F RTA49EU 20030613000872003061300087EU 2003 6 13 MALA030297 120030608A2910OFFHTE9531101 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15514XJ E2330 DURING CRUISE ON FLIGHT 3548 HYDRAULIC GREEN SYSTEM HI TEMP LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED GREEN SYSTEM ISOLATION VALVE P/N OFF HTE9531-101, P/N ON HTE9531-3, S/N FRTR010AW. AMM REF 29-36-00-1 RAN ENGINE NR 3 EDP FOR 40 MINUTES, NO GREEN SYSTEM LIGHT. LEAK CHECK AND NO LEAKS. 2H74 4F RTA49EU 20030613000892003061300089EU 2003 6 13 MALA030293 120030606A2910 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15517XJ E2335 DURING CLIMBOUT OF FLIGHT 3478, FROM DTW GREEN HYDRAULIC HI TEMP CAME ON FOLLOWED QRH. AIR RETURN TO DTW. MAINTENANCE GROUND RAN PRESSURIZED HYDRAULIC ON GROUND FOR 1 HOUR AND 20 MINUTES AT NO TIME DID THE GREEN HI TEMP LIGHT ILLUMINATE. INSPECTED GREEN SYSTEM, ALSO COULD NOT DUPLICATE DISC AT THIS TIME. AC OK FOR CONTINUED SERVICE. 2H74 4F RTA49EU 20030613000942003061300094NM 2003 6 13 UPS03440805 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D CROWN - S4R STR END CORROSION CRACKED AT BS 1238. M/D STRINGER BN BS 1210 AND BS 1240 S4R REPAIRED AS PER SRM 53-10-03 FIG 5 DUE TO COR CRACK LENGTH .5 INCH FROM EDGE TO 2ND FASTENER HOLE AREA EXCEEDED SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F RTA20WE 20030613001202003061300120 2003 6 13 SWAA031195 420030528A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM. 2L72 4F A16WE 20030613001232003061300123NM 2003 6 13 SWAA031198 120030529A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 668, RBL 24. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030613001292003061300129NM 2003 6 13 SWAA031235 120030604A53106935365 SHEAR TIE BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 27R AND STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F A16WE 20030613001312003061300131NM 2003 6 13 SWAA031237 120030604A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20030613001332003061300133NM 2003 6 13 SWAA031239 120030601A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20030613001342003061300134NM 2003 6 13 SWAA031240 120030603A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 500C + 14, STR 16R. REPAIRED STR PER SRM. 2L72 4F RTA16WE 20030613001352003061300135 2003 6 13 SWAA031241 420030603A2565D31591 INDICATOR BOEING737 7373H4 1384600NM SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030613001372003061300137NM 2003 6 13 SWAA031243 120030604A53116935365 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030613001472003061300147 2003 6 13 SWAA031228 420030603A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 1846 26585 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030613001492003061300149NM 2003 6 13 SWAA031230 120030603A5314BAC1503 STIFFENER BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL STIFFENER CRACKED AY BS 663, LBL 6.15. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM. 2L72 4F A16WE 20030613001532003061300153 2003 6 13 SWAA031212 420030601A25656557463 GIRT BAR BOEING737 7372T4 1384492NM ESCAPE SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTINGS (FWD AND AFT) CORRODED. REMOVED AND REPLACED BOTH ATTACH FITTINGS PER MM. 2L72 4F A16WE 20030613001562003061300156NM 2003 6 13 SWAA031215 120030601A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING LE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT OUTBD T/E FLAP DELAMINATED. REMOVED AND REPLACED OUTBD T/E FLAP PER MM. 2L72 4F RTA16WE 20030611001592003061100159NM 2003 6 11 UPS03440698 120030511A5310141U11072 BEAM BOEING747 747200 1384847NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, NLG WW TUNNEL - RT BS 280 VERTICAL BEAM WEB FOUND CRACK AT LOWER STANDOFF HOLE BETWEEN 1ST & 2ND STIFFENER CLIP (COUNT FROM TOP). DEFECT WEB REMOVED AND SERVICEABLE WEB REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030612000112003061200011SO 2003 6 12 SWIA200312019 120030425A5320 CLIP EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07295SW 120322 LEFT AND RIGHT FRAME 9 CLIPS CRACKED IN COCKPIT. FOUND DURING C-CHECK INSPECTION. COMPLIED WITH SB 120-53-0073. 2L72 4T4 TRTA31SO E20NE 20030612000272003061200027EA 2003 6 12 COMA0360247 120030526A78105083T69G05 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENG EXAUST CRACKED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01420CA 7451 807466 FLIGHT 5016 RT ENGINE LOW OIL PRESSURE WARNING. REPLACED CRACKED EXHAUST FRAME. 2L72 4F4 FRTA21EA E15NE 20030612000582003061200058SO 2003 6 12 SWIA200312032 120030528A3350 LIGHT EMB 120 EMB120ER 3260203SO ROW 6A BROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07568SW 120343 EXIT LIGHT AT ROW 6A IS BROKEN. INSTALLED NEW EXIT LIGHT ASSEMBLY AT ROW 6A. OPS CHECK GOOD. 2L72 4T RTA31SO 20030612000932003061200093SO 2003 6 12 C2XA03IA057 120030530A33503025103 LIGHT EMB 145 EMB145 3260210SO OVERWING INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713965 145125 DURING PREFLIGHT THE CREW NOTED THAT THE RIGHT HAND EMERGENCY OVERWING LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND EMERGENCY OVERWING LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030612001022003061200102NM 2003 6 12 CALA0300277 120030601A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND LEFT O/B FLOOR SUPPORT CORRODED BETWEEN STA 1006-1016, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030612001322003061200132NM 2003 6 12 UPS03440778 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D CROWN - S-4R STR CORRODED AT BS 1338. CORROSION BLEND OUT (0.033 X .5 X 2 INCH) STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. 2L74 4F RTA20WE 20030613000142003061300014NE 2003 6 13 MALA030287 220030529A73208346001 PRESSURE SWITCH SAAB SF340 SF340A 7850100EU GE CT7TS CT72A 30030NE FUEL SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15106XJ 340A106 DURING CLIMBOUT ON FLIGHT 3183, RT MAIN PUMP LIGHT ILLUMINATED AFTER TAKEOFF. AIR RETURN TO MSP. MAINTENANCE REPLACED MAIN FUEL PRESSURE SWITCH P/N 8346-001, OPS AND LEAK CHECK GOOD. 2L72 4T4 URTA52EU E8NE 20030613000282003061300028NM 2003 6 13 CALA0300281 120030602A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L AT BS 500C + 4, JUST FORWARD OF LEFT ICE LIGHT HOUSING. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20030613000702003061300070SO 2003 6 13 C2XA03SH166 120030608A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 DURING C-CHECK THE LEFT HAND FORWARD EMERGENCY LIGHT WAS FOUND TO BE NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE BULB IAW EMB 145 IPC 33-50-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000972003061300097NM 2003 6 13 UPS03440810 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 1720- 1740 STR 9R STRINGER END CRACKED. M/D - BS 1720-1740 STR 9R STRINGER END REPAIRED AS PER HX RS R-53-61-35035 AND ENG'R FILE NUMBER 747-53-20146. 2L74 4F RTA20WE 20030613000992003061300099NM 2003 6 13 UPS03440812 120030517A5220 HINGE BOEING747 747200 1384847NM EMERGENCY EXIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - L5 DOOR T/T LWR HINGE LWR BEARING ASSY MOUNTING SUPPORT AREA CORROSION. CORROSION BLEND OUT (0.040 X 1 X 1 INCH). M/D L5 DOOR LWR HINGE LWR SUPPORT WEB REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20030613001032003061300103NM 2003 6 13 UPS03440819 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 BS 1940 - 1960 STR 2R STRINGER END CRACKED. M/D BS 1940 - 1960 STR 2R STRINGER END REPAIRED AS PER HX RS R-53-61-35035 AND ENG'R 747-53-20146. 2L74 4F RTA20WE 20030613001132003061300113NM 2003 6 13 SWAA031254 120030604A575465C26603 SLAT BOEING737 7373H4 1384600NM LT WING OUT OF RIG A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 NR 4 L/E SLAT VISUALLY NOT ALIGNED WITH OTHER SLATS. REMOVED AND REPLACED NR 4 L/E SLAT AND OUTBD GUIDE STOP. 2L72 4F RTA16WE 20030617000232003061700023SW 2003 6 17 CA030530003 120030428A6210212015501115 BLADE BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ANNUAL M/R BLADE INSPECTION AME DISCOVERED A SMALL CORROSION PIT IN BLADESKIN LOCATED AT BLADE STATION 13.7 & 5.5 FROM LEADING EDGE.(SEE ATTACHED PHO TOS)FOUR CRACKS WERE FOUND ORIGINATING FROM THE PIT.THE LONGEST CRACK WAS 14 INCH CHORDWISE, TWO SMALLER CRACKS PROGRESSING TOWARDS THE LEADING EDGE AT APPROXIMATELY 45 DEG FROM THE MAIN CRACK.THE FOURTH CRACK WAS PROGRESSING STRAIGHT TOWARDS THE LEADING EDGE. THE PIT WAS APPROXIMATELY 1/16 IN DIAMETER AND APPROXIMATELY 0.015 DEEP. M/R BLADE WAS REPLACED AND A/C RETURNED TO SERVICE. 1G71 4U4 U H4SW E22EA 20030617000242003061700024 2003 6 17 CA030530008 420030514A2340 RADIO PIPER PA44 PA44180 7104402SO NR 2 INTERCOMM FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) INSTRUCTOR AND STUDENT ON BOARD, TRAINING FLT. NOTICED ODORS AND A LITTLE SMOKE SEEMINGLY TO COME FROM JUST BY CO-PILOTS POSITION, UNDER PANEL. ALL ELECTRICS SWITCHED OFF. MINIMUM ELECTRICS ON, NO FURTHER PROBLEMS, RETURNED TO BASE. A/C INSPECTED, NO FAULTS FOUND. ALL SYSTEMS APPEARED OK. AIRCRAFT RELEASED. AIRCRAFT DISPATCHED. DURING PRE-FLIGHT, NOTED THAT INTERCOMM ON PILOTS SIDE UNSERV ICEABLE. (HAD BEEN REPORTED SERVICEABLE ON PREVIOUS TRIP TO BASE.) INTERCOMM REPLACED AND FUNCTION CHECKED SERVICEABLE. NOTICED AT THIS TIME, THE NR 2 COMM DIGITAL DISPLAY WORKED BUT THIS RADIO WOULD NOT TRANSMIT. 1L72 3O A19S0 20030617000272003061700027EA 2003 6 17 CA030603001 120030531A325016480101 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NLG STEERING FAILED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CA 23052 (CAN) ON TAKE OFF ROLL, THE FLIGHT CREW REPORTED THAT THEY COULD NOT MAINTAIN RUNWAY CENTERLINE. HAD TO USE FULL LT RUDDER DEFLECTION. AIRCRAFT PULLED TO RT.ABORTED TAKE OFF AT 60 KTS (WIND WAS STRAIGHT DOWN THE RUNWAY). AFTER REPLACING THE NOSE WHEEL STEERING ELECTRO HYDRAULIC SHUT OFF VALVE (EHSV), NO FURTHER DISCREPANCY WAS NOTED DURING THE HIGH SPEED TAXI TEST AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030617000292003061700029CE 2003 6 17 CA030603003 120030603A30209091009913 TUBE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA ANTI ICE SYS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING DAILY SERVICEABILITY CHECK THE LT ENGINE SHORT ANTI-ICE FLEX TUBES WAS FOUND TO BE CRACKED. THERE WAS NO EVIDENCE OF AN EXHAUST LEAK INSIDE THE COWLING. THE TUBE WAS CRACKED APPROX. HALF OF IT S CIRCUMFERENCE. CRACKED TUBES WAS REPLACED. LT TUBE TSN 341 HOURS. 1L72 3T4 TRT3A20 E4EA 20030617000742003061700074SW 2003 6 17 CA030523001 120030522A6220407010105101 STUD BELL BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R HEAD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA A144 (CAN) CRACKS FOUND AT OVERHAUL ON MAIN ROTOR HEAD. 1G71 3U3 UO H2SW E1GL 20030617000782003061700078NM 2003 6 17 CA030502001 120030501A53504426X210 RADOME DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NOSE BIRD STRIKE W O OTHER O OTHER CLCLIMB 1 CA (CAN) CREW REPORTED ' BIRD STRIKE LT SIDE OF NOSE CONE ON DEPARTURE CLIMBING THROUGH 1500' INDICATED, IE 1000 FT AGL. ALL ENGINE INDICATIONS, FLT CONTROLS ETC NORMAL.RADAR ANT LIGHT CONTINUOUSLY FLASHING, IE RADAR ANTENNA WILL NEED TO BE READJUSTED. MAINTENANCE COMPLETED BIRD STIKE INSPECTION PER CH 5-50-26 OF DASH 8 MM 8-1-8-2. RADOME REPLACED DUE TO DAMAGE ON LT SIDE. W/R ANTENNA ASSY P/N MI-585353, RADAR DISH P/N MI585066, AND W/R R/T P/N MI585350-5 ALSO REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030617000802003061700080NE 2003 6 17 AUS20030499 120030511A67307826002 SERVO SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE TAIL ROTOR LEAKING W O OTHER KF FLUID LOSS FLT CONT AFFECTED CRCRUISE 1 AUS 853 (AUS) TAIL ROTOR SERVO PISTON SEALS LEAKING. LOSS OF NO1 HYDRAULICSYSTEM FLUID. 1G72 3U3 UNCH1NE E19EU 20030617000962003061700096 2003 6 17 ERAA087087 420030516A342040008330207 INDICATOR BELL 412 412 1182202SW RADAR FLUCTUATES E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01418EH UNIT FLASHES ON AND OFF IN FLIGHT. UNIT WORKED WELL ON BENCH. HAS CORROASION ON INTERCONNECT BOARD. REMOVED CORROSION AND TESTED UNIT. 1G72 4U H4SW 20030617001042003061700104SW 2003 6 17 HEEA087456 120030612A249765003061513 CONNECTOR BELL 407 407 1182206SW ALLSN 250C 250C* GL ELECTRICAL BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 LOCKING TABS BROKEN OFF OF CONNECTOR. TO BE SENT TO MFG FOR CREDIT. 1G71 3U3 UO H2SW E4CE 20030617001102003061700110SW 2003 6 17 HEEA087291 120030611A6710 BUMPER BLOCK BELL 407 407 1182206SW ALLSN 250C 250C47B GL BELLCRANK DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 RUBBER BUMPER UNBONDED FROM BELLCRANK. TO BE SENT TO MFG. 1G71 3U3 UO H2SW E1GL 20030617001122003061700112SW 2003 6 17 HEEA087293 120030611A6220407010100115 BEARING BELL 407 407 1182206SW M/R HUB DELAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH3807 53283 RED FEATHERING BEARING DELAMINATED. REPAIRED. 1G71 3U O H2SW 20030617001182003061700118SW 2003 6 17 HEEA087457 120030612A24976500306N CONNECTOR BELL 407 407 1182206SW ELECTRICAL BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 LOCKING TABS BROKEN OFF OF CONNECTOR. 1G71 3U O H2SW 20030617001292003061700129NM 2003 6 17 QXEA200300675 120030607A3260MS25237387 LIGHT DHAV DHC8 DHC8202 2809007NM COCKPIT INOPERATIVE A QXEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 NM09350PH 488 BOI-ON FLIGHT NUMBER 2203, FLIGHT DID A GO-AROUND ON APPROACH AT BOI DUE TO NORMAL NOSE GEAR LIGHT DID NOT ILLUMINATE. ALTERNATE GEAR LIGHT SHOWED DOWN. CREW LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR DOWN AND LOCKED LIGHT SOCKET LOOSE. ONE LIGHT BULB BURNT OUT. RESECURED SOCKET ASSEMBLY, RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617001322003061700132EA 2003 6 17 QXEA200300290 120030220A2820D98C07606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM MALFUNCTIONED A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09614QX1532 10049 PDX-BOOST PUMPS CYCLING INFLIGHT. MAINTENANCE INSPECTED AND REPLACED THE ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030617001382003061700138NM 2003 6 17 QXEA200300723 120030602A5420 BRACKET BOMBDRDHC8 DHC8401 1390041NM NR 1 NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - NR 1 NACELLE ANGLE BRACKET BETWEEN FORWARD FRAME ASSEMBLY LEFT HAND SIDE AND TOP, LEFT HAND HEAT SHIELD SUPPORT FRAME IS CRACKED. REPAIRED IAW Q400 SRM 51-42-05. AND SRM 54-10-06, FIGURE 1, ITEM 3. 2H72 4T RTA13NM 20030617001462003061700146EA 2003 6 17 QXEA200300581 120030510A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - NR 1 COCKPIT SEAT TRACK HAS A NICK IN THE INBOARD EDGE 8 INCHES FORWARD OF AFT END OF TRACK. REPAIRED IAW HORIZON AIR EA R-53-101. 2L72 4F RTA21EA 20030612001392003061200139WP 2003 6 12 UPS03840728 120030503A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, MAIN CABIN TRACK CORRODED ON LOWER SIDE IN CARGO PIT RT TUNNEL STA 1243 RBL 62. REMOVED EXISTING SEAT TRACK SECTION. LOCATED, DRILLED & DEBURRED NEW SECTION OF TRACK AND SPLICES (P/N 60-15176), DC8-53B-003-502 (2) IAW DC8 SRM 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20030612001592003061200159WP 2003 6 12 UPS03840757 120030521A53404641324U501 FITTING DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, STATION 1690 LONG 28L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612001732003061200173EA 2003 6 12 SWIA200312046 120030529A5220 PIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OVERWING EXIT WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 LEFT AND RIGHT OVERWING EXIT HINGE SUPPORT PINS SHOWING SIGNS OF WEAR AND SURFACE CORROSION. REPLACED PINS IAW STANDARD MAINTENANCE PRACTICES. DISCOVERED DURING MAINTENANCE INSPECTION. 2L72 4F4 FRTA21EA E15NE 20030612001902003061200190WP 2003 6 12 EIA2003077 120030521A5320 WEB DOUG DC9 DC915F 3022037WP FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09915F 47061 EXFOLIATED CORRROSION AT BS 218-228, RBL 52 (APPROX) AFT OF SERVICE DOOR. REMOVED AND REPLACED CUSP WEB PER EO 53-DC9-978-00 REV B, & DC9 SRM 51-30-2, PG 1-4. 2L72 4F A6WE 20030613000022003061300002EA 2003 6 13 SWIA200312055 120030530A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07411SW 7067 AFTER LANDING AND CLEARING RUNWAY, TRANSFERED BLEEDS TO APU OPEN AND COCKPIT FILLED WITH SMOKE AND A STRONG BURNING ODOR. RAN ENGINES EXCESSIVELY WITH BOTH PACKS ON. NO SMOKE OR BURNING ODOR. TRANSFERRED BLEEDS OVER TO APU. RAN FOR 1/2 HR, NO SMOKE OR BURNING ODOR. OPS CHECK GOOD. UNABLE TO DUPLICATE. 2L72 4F RTA21EA 20030613000262003061300026NM 2003 6 13 UPS03540789 120030603A5610 MECHANISM BOEING757 75724APF 1384969NM WINDOW CRANK INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01473UP 28846 RT NR 2 WINDOW CRANK MECHANISM STRIPPED WINDOW WILL NOT OPEN FOR EGRESS FROM INSIDE OR OUTSIDE. REMOVED ANGLE DRIVE GEARBOX ASSY REF M/M 56-11-04-4. INSTALLED ANGLE DRIVE GEARBOX ASSY AS PER MM 56-11-04-4. OPS CK NORMAL. 2L72 4F RTA2NM 20030613000352003061300035 2003 6 13 0301076717 420030602A3460 ANNUNCIATOR BOEING747 747251F 1384898NM COCKPIT SMOKE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01617US 21121 DURING CLIMB SMOKE EMITTED FROM THE CAPTAIN'S FLIGHT DIRECTOR/PERFORMANCE MANAGEMENT SYSTEM LIGHT UNDER THE GLARESHIELD. AIRCRAFT RETURNED TO SEA AND LANDED WITHOUT INCIDENT. REPLACED THE PERFORMANCE MANAGEMENT SYSTEM ANNUNCIATOR PANEL AND SWITCHING UNIT. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030613000572003061300057NM 2003 6 13 UPS03440791 120030519A5330 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, AREA AFT OF BULK CARGO STA 2180-2200 S50L STRINGER END CORROSION CRACK FOUND. AFT OF BULK CARGO BS 2180-2200 S50L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F RTA20WE 20030613000692003061300069SO 2003 6 13 C2XA03IA060 120030606A3260 PROXIMITY SWITCH EMB 135 EMB135LR 3260305SO MLG MALFUNCTIONED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2728529 145512 AFTER TAKEOFF THE CREW NOTED THAT THE LANDING GEAR AURAL WARNING WAS SOUNDING AFTER GEAR RETRACTION. THE CREW RETURNED THE AIRCRAFT TO CLL, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE PROX SWITCHES AND RERACKED THE AWU. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030613000732003061300073SO 2003 6 13 C2XA03SH169 120030608A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 SHV-DURING C-CHECK THE DOUBLER ON T-REINFORCEMENT ON STR 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613001022003061300102NM 2003 6 13 UPS03440817 120030512A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, AFT CARGO DOOR CUTOUT AFT UPPER CORNER AREA FOUND FOUND 1EA HOLE CRACK AT SKIN AND BEARSTRAP APPROX .0625 INCH RUNNING UPWARD AND DOWNWARD. AFT CARGO DOOR CUTOUT AFT UPPER CORNER HINGE CAP 1EA BOLT HOLE REPAIRED AS PER BOEING MSG UPS-HKG-03-00105H RS R53-61-35020 AND UPS EO B747-5330-18849-A. REF TAR S/N 103610. 2L74 4F RTA20WE 20030613001162003061300116NM 2003 6 13 SWAA031257 120030605A53116935365 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030613001542003061300154NM 2003 6 13 SWAA031213 120030601A53116546536 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BETWEEN STR 7L AND STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030617000422003061700042EU 2003 6 17 AUS20030496 120030409A5347D33830403 SEAT TRACK FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE FLT ATTENDANT CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AFT FLIGHT ATTENDANT SEAT SUPPORT BRACKET CORRODED. 2L72 4F4 FRT E25NE 20030617001632003061700163SW 2003 6 17 HEEA087302 120030611A6300407010206103A ROD END BELL 407 407 1182206SW M/R DRIVE DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 RUBBER AT ROD END IS OIL SOAKED AND DETERIORATED. 1G71 3U O H2SW 20030617001692003061700169GL 2003 6 17 HEEA087469 220030612A731070079H100F210 HOSE BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUEL FILTER CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 HOSE ASSY HAS BEEN CHAFED TO THE STEEL BRAIDS FROM THE ENGINE COWLING SUPPORT. REPLACED HOSE. 1G71 3U3 UO H2SW E1GL 20030617001722003061700172 2003 6 17 HEEA087471 420030612A3457 BATTERY BELL 407 407 1182206SW GPS SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 8270245 53401 BATTERY FAILED. FOUND MEMORY BATTERY BAD AND CORROSION ON PRINTED CIRCUIT BOARDS. REPLACED MEMORY BATTERY AND CLEANED CORROSION. BENCH CHECK GOOD. 1G71 3U O H2SW 20030617001882003061700188NM 2003 6 17 QXEA200300661 120030529A32346131001001 SELECTOR VALVE BOMBDRDHC8 DHC8401 1390041NM MLG FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09407QX2804 2804 4049 GEG- ON FLIGHT 2359 AFTER LIFTOFF NOSE GEAR RETRACTED NORMALLY BUT BOTH MAIN GEAR FAILED TO RETRACT. CREW WENT THROUGH CHECKLIST. GEAR CYCLED AGAIN. NOSE GEAR WORKED FINE, BUT STILL RECIEVED YELLOW AND RED ON BOTH MAIN GEAR ON GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617001962003061700196EU 2003 6 17 ERAA087105 120030521A2840VT044 TRANSMITTER BOLKMS105 BO105S 5626006EU FUEL QTY FLUCTUATES E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01292EH 562 QUANTITY INDICATION FLUCTUATES. COMPONENT TESTED PRIOR TO DISASSEMBLY. REPLACED CASE ASSEMBLY AND TESTED. 1G72 3U H3EU 20030617001972003061700197EU 2003 6 17 ERAA087106 120030521A2842VT044 TRANSMITTER BOLKMS105 BO105S 5626006EU FUEL QUANTITY FLUCTUATES E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01152EH S701 GAUGE FLUCTUATING. REPLACED CASE ASSEMBLY AND TESTED. 1G72 3U H3EU 20030617002032003061700203NM 2003 6 17 QXEA200300728 120030611A5320 MOUNT BRACKET BOMBDRDHC8 DHC8401 1390041NM FUSELAGE TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX- .5 INCH TO .1875 INCH WIDE TEAR IN LOWER FORWARD CORNER OF THE MOUNTING BRACKET FOR THE PARK BRAKE CONTROL VALVE. REPAIRED IAW HORIZON AIR EA 6-53-267 AND RD8/4-53-616. 2H72 4T RTA13NM 20030617002052003061700205EA 2003 6 17 QXEA200300730 120030612A3297 WIRE HARNESS CNDAIRCL600 CL6002C10 1390015EA RT MLG FAULTY A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09612QX 10042 PDX-ON FLIGHT NUMBER 2438, MAIN LANDING GEAR FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT GEAR DOWNLOCK HARNESS ASSEMBLY. REPAIRED IAW CRJ MM, 32-61-05 AND CRJ MM 32-61-00-710-801-A01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030617002122003061700212SW 2003 6 17 HEEA087310 120030611A6420 BEARING BELL 407 407 1182206SW T/R HUB ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH4275 53230 53461 TAIL ROTOR FEATHERING BEARINGS WORN. REPAIRED. 1G71 3U O H2SW 20030617002422003061700242NM 2003 6 17 QXEA200300600 120030430A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT SUPPORT FLANGE FOR 261HT IS CHAFED. REPAIRED IAW DHC-84 RD 8/4-53-451. 2H72 4T RTA13NM 20030617002482003061700248SW 2003 6 17 HEEA087477 120030612A1430APC230321586 CLAMP BELL 407 407 1182206SW ELECTRICAL TWISTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 WIRE HAS TWISTED CLAMP. SCRAPPED. 1G71 3U O H2SW 20030617002512003061700251NM 2003 6 17 QXEA200300593 120030502A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - LOWER FUSELAGE SKIN AT LOWER TCAS ANTENNA HAS CORROSION IN SEVERAL SPOTS. REPAIRED IAW Q400 SRM TASK 51-21-00-350-301. 2H72 4T RTA13NM 20030617002522003061700252NM 2003 6 17 QXEA200300594 120030507A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT FUSELAGE CARGO DOOR CUTOUT CHAFE AT UPPER AFT CORNER. REPAIRED IAW HORIZON AIR EA 6-52-252. 2H72 4T RTA13NM 20030617002542003061700254NM 2003 6 17 QXEA200300598 120030430A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT SUPPORT FLANGE FOR 261CT IS CHAFED. REPAIRED IAW DHC-8 Q400 RD 8/4/53-451. 2H72 4T RTA13NM 20030617002792003061700279SW 2003 6 17 HEEA087314 120030611A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH3487 53400 WATER LEAKING FROM TRAILING EDGE ROOT OF BLADE. 1G71 3U O H2SW 20030617002822003061700282SW 2003 6 17 HEEA087316 120030611A5610407030115123 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 WINDSHIELD IS CRAZED. REPLACED WINDSHIELD. 1G71 3U O H2SW 20030617002862003061700286SW 2003 6 17 HEEA087320 120030611A5610407030118105 CHIN BUBBLE BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 WINDOW CRAZED AROUND OUTER EDGE. REPLACED WINDOW. 1G71 3U O H2SW 20030617002922003061700292SW 2003 6 17 HEEA087035 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030613001402003061300140NM 2003 6 13 SWAA031221 120030602A3350BR2013 WIRE BOEING737 7377H4 1384404NM EMERGENCY LIGHT EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED C4 CHECK, FOUND EEPLS WIRES EXPOSED. SECURED WIRES PER MM. 2L72 4F RTA16WE 20030613001442003061300144NM 2003 6 13 SWAA031225 120030603A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 21R. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20030613001482003061300148NM 2003 6 13 SWAA031229 120030602A53106545871 DOOR FRAME BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT EDGE FRAME CRACKED NEAR STOP FITTING CUTOUT. REPAIRED FRAME PER SRM. 2L72 4F A16WE 20030617000252003061700025EU 2003 6 17 CA030530013 120030512A321322201TK080015X BOLT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MLG SHEARED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) UPON REINSTALLING THE LANDING GEAR SHOCK ABSORBERS, THE LOWER BOLT HOLDING THE FORWARD CROSSTUBE SHOCK CLAMPS IN PLACE SHEARED WHEN BEING TORQUED TO MANUFACTURERS RECOMMENDATIONS. THE BOLT SHEARED JUST BEFORE REACHING THE 132.7 IN LBS OF TORQUE LISTED IN THE MAINTENANCE MANUAL. THIS BOLT AND OTHER SIDE CLAMP BOLT REPLACED TO PRECLUDE SIMILAR FAILURE. MANUFACTURER NOTIFIED OF OCCURRENCE. 1G71 3U3 U H9EU E19EU 20030617000312003061700031SO 2003 6 17 CA030528009 120030527A271062701123 CABLE PIPER PIPER PA44 PA44180 7104402SO AILERON CONTROL FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN EVENT NR 3 INSPECTION THE LT AILERON BALANCE CABLE WAS FOUND TO BE FRAYED WHERE IT CROSSES THE INBOARD PULLEY AT THE WING ROOT. THE PULLEY WAS REMOVED AND INSPECTED AND THE BEARING WAS FOUND TO BE IN GOOD WORKING ORDER, THE BEARING WAS LUBED AND THE PULLEY WAS REINSTALLED. THE CABLE WAS REPLACED WITH NEW AND THE AILERON SYSTEM RIGGED.THIS CABLE WAS ORIGINAL FROM NEW.ALL OTHER CABLES WERE INSPECTED AND NO WEAR WAS FOUND. 1L72 3O A19S0 20030617000362003061700036CE 2003 6 17 AUS20030488 120030424A2434642985 BRACKET CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL DC ALTERNATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ALTERNATOR CAPACITOR RETAINING BRACKET FAILED. CAPACITOR SHORTCIRCUITING ON POSITIVE PLATE. 1L72 3O3 O A25CE E7CE 5 CP45GL 20030617000562003061700056EA 2003 6 17 QXEA200300655 120030521A5280 RIB CNDAIRCL600 CL6002C10 1390015EA LT MLG DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - LEFT MAIN GEAR DOOR LOWER DOOR ASSEMBLY HAS A CRACK IN MOST INBOARD RIB. REPAIRED IAW CRJ 700 AMM 32-12-01-400-801. 2L72 4F RTA21EA 20030617001132003061700113NM 2003 6 17 QXEA200300737 120030613A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX- RIGHT HAND NR 4 FLAP TRACK HAS THREE LOCAL AREAS .125 INCH THAT ARE WORN ON TRACK C. REPAIRED IAW DHC-8 RD 8-57-988. 2H72 4T RTA13NM 20030617001202003061700120GL 2003 6 17 HEEA087459 220030612A73136899001 FUEL NOZZLE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE INTERMITTENT E O OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 FUEL NOZZLE HAS INTERMITTENT DELAYED STARTS. REPLACED FUEL NOZZLE. 1G71 3U3 UO H2SW E1GL 20030617001682003061700168NM 2003 6 17 QXEA200300718 120030606A5730 DOUBLER BOMBDRDHC8 DHC8401 1390041NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - CHAFING ON DOUBLER AT OUTBOARD FLAP, LEFT HAND WING, INBOARD END, UPPER SIDE. REPAIRED IAW HORIZON AIR EA 6-57-141. 2H72 4T RTA13NM 20030617001922003061700192SW 2003 6 17 HEEA087475 120030612A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 RT FLOAT BOTTLE FUSIBLE PLUG LEAKING. 1G71 3U O H2SW 20030617001942003061700194SW 2003 6 17 HEEA087304 120030611A6220407010207101 STOP BELL 407 407 1182206SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 MAIN ROTOR STOP SEPARATED. 1G71 3U O H2SW 20030617002022003061700202SW 2003 6 17 HEEA087305 120030611A6420 BEARING BELL 407 407 1182206SW T/R HUB ASSY GALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH1002 A639 53327 TAIL ROTOR FEATHERING BEARINGS GALLED. REPAIRED. 1G71 3U O H2SW 20030617002442003061700244NM 2003 6 17 QXEA200300601 120030430A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT SUPPORT FLANGE FOR 261LT IS CHAFED. REPAIRED IAW DHC-8 400 RD 8/4-53-451. 2H72 4T RTA13NM 20030617002582003061700258NM 2003 6 17 QXEA200300611 120030506A5753 MOUNT BOMBDRDHC8 DHC8401 1390041NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - RIGHT HAND WING OUTBOARD FLAP MOUNT LUG AT NR 4 CARRIAGE, FORWARD, LEFTHAND MOUNT FRAME CONTACTS NR 4 FLAP BEAM DURING OPERATION AT FORWARD END OF TRAVEL, INBOARD OF THE TOP CENTER ROLLER SURFACE. REPAIRED IAW HORIZON AIR EA 6-57-139. 2H72 4T RTA13NM 20030617003112003061700311SW 2003 6 17 HEEA087038 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH1181 53199 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030617003192003061700319 2003 6 17 BAQA087063 420030611A34214021541791 INDICATOR BOLKMS117 BK117A1 5626010EU COCKPIT MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME415 7243 NR 1 AND NR 2 MISCOMPARE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030618000082003061800008SW 2003 6 18 HEEA087486 120030612A6240M835362028M RELAY BELL 407 407 1182206SW ROTOR HORN MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03501PH 53401 RELAY CAUSING DEGRADE LIGHT. 1G71 3U O H2SW 20030618000152003061800015EU 2003 6 18 I05R086818 120030529A5210677110123 SPRING SNIAS 350 AS350* EU CREW DOOR LATCH MISSING H I05RO OTHER O OTHER NRNOT REPORTED 1 FS0129LB 287 3560 PILOTS DOOR WILL NOT CLOSE PROPERLY REPLACED MISSING SPRING. 1G71 3U H9EU 20030618000322003061800032 2003 6 18 SWAA031326 420030612A2565D31354 SLIDE BOEING737 7375H4 138449DNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION AND CABLE MISROUTED. REPOSITIONED SLIDE AND REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030618000332003061800033NM 2003 6 18 SWAA031327 120030614A575411411106 SKIN BOEING737 7377H4 1384404NM L/E FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 NR 4 L/E FLAP SKIN CRACKED AT WEB STIFFENER. REMOVED AND REPLACED NR 4 L/E FLAP PER MM. 2L72 4F RTA16WE 20030618000452003061800045 2003 6 18 SWAA031313 420030611A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030618000462003061800046NM 2003 6 18 SWAA031314 120030611A256010C801 LATCH BOEING737 7372H4 138448CNM COCKPIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 F/O'S EMERGENCY ESCAPE ROPE DOOR LATCH BROKEN. REPAIRED LATCH ASSY PER MM. 2L72 4F A16WE 20030618000492003061800049 2003 6 18 SWAA031316 420030611A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030618000582003061800058 2003 6 18 HEEA087124 420030610A2312064102300 TRANSCEIVER SKRSKYS76 S76A 8143006NE VHF SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 VHF TRANSCEIVER HAS A POPPING SOUND. SHOP REPAIR. 1G72 3U H1NE 20030618000602003061800060 2003 6 18 SWAA031305 420030611A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSY OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030618000692003061800069NM 2003 6 18 SWAA031310 120030611A53206517583 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND LT VERTICAL CHORD CRACKED AT BS 179, LBL 5.7. REPAIRED VERTICAL CHORD PER SRM. 2L72 4F RTA16WE 20030618000752003061800075NM 2003 6 18 SWAA031297 120030609A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 500 + 15, STR 26R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030617000452003061700045EA 2003 6 17 QXEA200300653 120030514A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - RIGHT WING LEADING EDGE HAS A GOUGE ON THE TOP SIDE AT WS 163. REPAIRED IAW QX4 SUPPLEMENT 51-12-00. 2L72 4F RTA21EA 20030617000492003061700049EU 2003 6 17 CA030528016 120030526A33409728769401 LANDING LIGHT PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL EXTERIOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE RT LANDING LIGHT HAS A HISTORY OF FAILING WITHIN A VERY SHORT PERIOD OF TIME FOLLOWING REPLACEMENT OF BULB. THE LASTEST INCIDENT OCCURRED WITHIN 5 HOURS OF FLYING TIME. MAINTENANCE FOUND THAT THE SEALED LAMP WAS CRACKING AT THE TOP OF THE LENSE ON A CONSISTANT BASIS. LOCATATE AT THE TOP OF THE LIGHT ASSEMBLY A RE (3) RIVETS, WHICH WERE COMING IN CONTACT WITH THE BACK OF THE SEALED LAMP. ANTI-CHAFE TAPE WAS ADDED TO THE INSIDE DIAMETER OF THE LIGHT HOUSING, EFFECTIVELY ADDING A SHIM. THIS HAS PROVIDED ENOUGH CLEARANCE BETWEEN THE HOUSING AND LIGHT TO CORRECT THE PROBLEM. THE AIRCRAFT HAS NOT EXPERIENCED ANOTHER LIGHT FAILURE SINCE THE MAINTENANCE ACTION WAS ACCOMPLISHED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030617000502003061700050EA 2003 6 17 QXEA200300657 120030523A5500 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA EMPANNAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - RIGHT LUNCHBOX CRACKED AT NR 10 FITTING AT FS 1070 1088. REPAIRED IAW QX SUPP AND SRM 51-40-00, 51-40-15. 2L72 4F RTA21EA 20030523000272003052300027NM 2003 5 23 AWXA200300568 120030505A5347146N544059 CARGO TRACK BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND UNDER NUT PLATES ON AFT CARGO COMPARTMENT TIE DOWN FITTING AT BS 1360, RBL 36. MAINTENANCE REMOVED AND REPLACED DAMAGED TIE DOWN FITTING AT BS 1360, RBL 36 IAW B757-200 SRM 51-40-02, PG 11. 2L72 4F RTA2NM 20030523000282003052300028NM 2003 5 23 AWXA200300569 120030504A5320146N5417 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT IN SEVERAL SPOTS BETWEEN BS 1380 AND BS 1405, RBL 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AFT CARGO COMPARTMENT FLOOR SUPPORT BETWEEN BS 1380 AND BS 1405, RBL 20; FABRICATED A REPAIR SUPPORT ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG 1-7. 2L72 4F RTA2NM 20030523000302003052300030EU 2003 5 23 AWXA200300571 120030519A5321D5362005500000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 MCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 242GF WAS FOUND DELAMINATED. MAINTENANCE REMOVED CABIN FLOOR PANEL 242GF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70055; INSTALLED NEW PANEL IAW AWA T/C R1C25306, AND A320 SRM 53-02-00, PG 233-236, FIG 209. 2L72 4F RTA28NM 20030523000322003052300032NM 2003 5 23 QXEA0300615 120030519A6120 CONTROLLER DHAV DHC8 DHC8202 2809007NM ZONE 400 MALFUNCTIONED A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09364PH 524 PSC ON FLIGHT 2101 ABORTED TAKEOFF DUE TO AUTOFEATHER DOES NOT ARM AT TAKEOFF POWER. PERFORMED AUTOFEATHER SYSTEM AND POWER UPTRIM TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523000472003052300047EA 2003 5 23 QXEA0300575 120030515A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX- DAMAGED RIVET ON STRINGER 9R ONE INCH AFT OF FUSELAGE 409.00 ABOVE RIGHT HAND WINDOW 2. REPAIRED IAW HORIZON AIR EA R-53-106, REO 670-53-00-036, CRJ SRM 51-25-16 AND 51-12-00. 2L72 4F RTA21EA 20030618001362003061800136SW 2003 6 18 HEEA087352 120030611A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20030618001382003061800138SW 2003 6 18 HEEA087353 120030611A5320407064807119 SUPPORT BELL 407 407 1182206SW FUSELAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 SUPPORT HAS MOUNTING HOLES ELONGATED. 1G71 3U O H2SW 20030618001412003061800141EA 2003 6 18 COMA0360265 120030610A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO01712CA11740 7244 FLIGHT 5686 UNCONTROLLED MOMENTARY ROLL DURING CRUISE FLIGHT, FOLLOWED BY SPOILERONS FAULT MESSAGE. REPLACED THE RT INBOARD SPOILERON PCU. 2L72 4F RTA21EA 20030618001472003061800147NE 2003 6 18 COMA0360271 220030611A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT OVERTEMP A COMAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO01984CA 7171 807384 FLIGHT 5879 RIGHT ENGINE OVER TEMPERATURE, INDICATED 901 DEGREES CELSIUS. REPLACED ENGINE. 2L72 4F4 FRTA21EA E15NE 20030618001482003061800148EA 2003 6 18 COMA0360272 120030611A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01815CA 7397 FLIGHT 5142 FLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20030618001502003061800150SW 2003 6 18 HEEA087356 120030611A5320407070620111 TRIM PANEL BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 TRIM PANEL CRACKED ALONG EDGES BEYOND REPAIR. 1G71 3U O H2SW 20030618001662003061800166GL 2003 6 18 HEEA087144 220030613A725023068265 BOLT BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL TURBINE ASSY DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032753F569 CAT25276 2729 CAE800819F TURBINE WAS REMOVED FOR 1750 HOUR INSPECTION. UPON INSPECTION OF PARTS NOTED FRETTING MUTE ON TIE BOLT. PART SCRAPPED. 1G71 3U3 U H2SW E4CE 20030618001832003061800183SW 2003 6 18 HEEA087150 120030609A6710206001053005 BEARING BELL 206 206L1 1182107SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035014V 45217 BELLCRANK ASSY HAS WORN BEARINGS. REPLACED BEARING (2 EACH) 206001053005 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618001872003061800187SW 2003 6 18 HEEA087154 120030609A6710206001763001 BELLCRANK BELL 206 206L3 1182108SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 BELLCRANK WORN. REPLACED BELLCRANK MS276474 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618001922003061800192SW 2003 6 18 HEEA087158 120030609A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW M/R HEAD STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 FLAP RESTRAINT ARM STICKING. REPAIRED. 1G71 3U H2SW 20030618002052003061800205EU 2003 6 18 HEEA087522 120030610A2913A5026780 PUMP AEROSPAS355 AS355* EU HYDRAULIC VIBRATION E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW03974AE 2653 NOISE AND VIBRATION IN THE TAIL ROTOR SYSTEM. REPLACED HYD PUMP. 1G72 3U H11EU 20030618002082003061800208SW 2003 6 18 HEEA087163 120030609A3212206030104023 FITTING BELL 206 206L3 1182108SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 FITTING ASSY IS WORN AND RUBBER MISSING. SCRAPPED. 1G71 3U H2SW 20030523000762003052300076NM 2003 5 23 SWAA031104 120030516A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 794, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030523000922003052300092WP 2003 5 23 MWEA030224 120030519A523059360641 CLIP DOUG DC9 DC982 3022082WP MID CARGO GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 MID CARGO DOOR LOWER FORWARD CORNER CLIP GOUGED. FABRICATED AND INSTALLED CLIP. 2L72 4F A6WE 20030523001202003052300120NM 2003 5 23 2003UALA00426 120030512A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29590UA 28708 AFT EEL STRIP FRONT OF FWD AFT LAV INOP. REPLACED EEL STRIP. 2L72 4F4 FRTA2NM E17NE 20030521000402003052100040WP 2003 5 21 DHL2003801070 120030512A57305654693403 PANEL DOUG DC8 DC873F 302199FWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 LT LWR PANEL NR 723 AT STA 750.000 SHOWS DELAMINATED INTERNAL/EXTERNAL SKIN. REMOVED AND REPLACED LT LWR PANEL 723 AT STA 750.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521000462003052100046WP 2003 5 21 DHL2003804896 120030214A531351616757 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LWR FUSE INNER STRUCTURE, L-17L CRACKED 3.00, STA 1772.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3, PG 16, FIG 5, SRM 51-2-0 FIG 50, DPS 4.710. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521001192003052100119WP 2003 5 21 MWEA030214 120030516A5230591014167 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FORWARD CARGO COMPARTMENT DOOR OUTER PAN HAS APPROXIMATELY A .375 INCH CRACK LOCATED OUTBOARD OF THE TORQUE TUBE CAM HOOK AFT SIDE, INNER AND OUTER PAN ARE BENT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030521001392003052100139WP 2003 5 21 DHL2003801046 120030412A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E UPPER SKIN HAS ELONGATED HOLES BETWEEN STA XOLDI 6.225 AND XS 466.651 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 AND SRM 57-3-3 FIG 5. REMOVED DAMAGED CTR L/E UPPER SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6 AL0.063) IAW SRM 57-3-3 FIG 5. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. INSTALLED NEW SKIN ON LT WING CTR L/E UPPER SKIN SURFACE (STA XOLDI 6.225 AND XS 466.651) IAW SRM 57-3-3 FIG 5 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001812003052100181WP 2003 5 21 DHL2003804908 120030214A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FWD ACCY COMPT FRAME CRACKED 1.000 INCH, STA 55.000 L-23L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 PG 2U/2V FIG 2 (SHEET 2). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 PG 2U/2V FIG 2 (SHEET 2). FABRICATED NEW FRAME SEGMENT AND SPLICES (7075-0-0.071/0.080) IAW SRM 53-2-0 PG 2U/2V FIG 2 (SHEET). HEAT TREATED IAW SRM 51-1-1 PG 1-17, SRM 51-1-4 PG 1-3, DPS 1-05.3. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND SPLICES WITH NEW FASTENERS IAW SRM 53-2-0 PG 2U/2V FIG 2 (SHEET 2). SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. FOR PNE DUCTS REMOVAL/REINSTALLATION AND LEAK CHECK SEE N/R 1835. 2L74 4F RT4A25 20030521001982003052100198 2003 5 21 SWAA031061 420030512A2565D31354 SLIDE BOEING737 7373G7 1384595NM FWD SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030522000212003052200021NM 2003 5 22 2003UALA00413 120030505A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ROW 15 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29904UA 25004 EEL FLOOR LIGHTING INOPERATIVE FROM ROW 15 THROUGH AFT GALLEY. REPLACED 4 EEL LIGHTS AND ONE EEL CABLE. OPS CHECK OK. 2L72 4F4 FRTA16WE E2GL 20030522000252003052200025NM 2003 5 22 2003UALA00417 120030505A2910 CHECK VALVE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE HYD SYSTEM LEAKING A UALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP29817UA 873 YELLOW SYSTEM LOW LEVEL LIGHT ILLUMINATED AND ECAM SHOWS 0 QUANTITY. FOUND LEAK AT HYD CHECK VALVE IN PTU MANIFOLD REPLACED CHECK VALVE AND FILLED YELLOW SYSTEM AND LEAK CHECKED SYSTEM NO LEAKS FOUND. 2L72 4F4 FRTA28NM E40NE 20030522000452003052200045WP 2003 5 22 GTIA030305 120030414A5320 WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CARGO BAY CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FORWARD CARGO CEILING AREA WEB CORRODED FS 226, STR 18R. FABRICATED WEB DOUBLER. INSTALLED DOUBLER AND FILLER. 2L72 4F4 F A6WE E2EA 20030522000532003052200053SO 2003 5 22 C2XA03IA050 120030513A261147359713 SMOKE DETECTOR EMB 145 EMB145 3260210SO CARGO BAY INOPERATIVE A C2XAO OTHER N FALSE WARNING APAPPROACH 1 SW2714974 145161 IAH- FLIGHT 2085, DURING FINAL ARRIVAL AND APPROACH BEGINNING, EICAS WARNING FOR BAGGAGE SMOKE ILLIMINATED WITH OVERHEAD EXTG BUTTON. EICAS MESSAGE CAME ON/WENT OUT/ CAME ON/ WENT OUT A TOTAL OF THREE (3) TIMES IN ONE MINUTE AND STAYED OUT. IAH- MAINTENANCE REMOVED AND REPLACED FORWARD BAGGAGE SMOKE DETECTOR. PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO EVIDENCE OF FIRE OR SMOKE IN THE BAGGAGE COMPAPTMENT. 2L72 4F RTT00011AT 20030522000902003052200090WP 2003 5 22 GTIA030289 120030411A5312 BULKHEAD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 AFT ACC AREA BULKHEAD CRACKED AT STA 1463 CANT APPROX LONGERON 3L. REMOVED 2 PART WEB ASSY. FABBED WEB AND DOUBLER ASSY. INSTALLED WEB AND DOUBLER ASSY. 2L72 4F4 FRTA6WE E2EA 20030522000932003052200093WP 2003 5 22 GTIA030295 120030414A5320 WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 E AND E BAY FS 162 CEILING AREA WEB CORRODED LBL 51. DRILL AND LOCATED DOUBLER. INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20030523000122003052300012 2003 5 23 2003F00294 420030501A3460701030031203 COMPUTER CESSNA750 750 2076810CE NR 1 FAILED A UG8AO OTHER O OTHER CRCRUISE 1 GL235115 7500018 DURING FLIGHT, Y/D FAILED, AUTOPILOT DISENGAGED, AND FGC 'A' AND FGC 'B' FAILED. AIRCRAFT CONTINUED ON TO DESTINATION AS SCHEDULED. NR 1 IAC (INTEGRATED AVIONICS COMPUTER) FAILED. REPLACED THE NR 1 IAC AND OPERATION WAS NORMAL. (M) 2L72 4J RTT00007WI 20030523000142003052300014NM 2003 5 23 2003F00295 120030119A7120 MOUNT BRACKET BOEING727 727222 1384073NM NR 2 ENGINE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND NR 2 ENGINE CASCADE VANE HAS CRACKED MOUNT BRACKET. WELDED CRACKED MOUNT BRACKET PER AMS STD-1595 AND BAC5975. (M) 2L73 4F A3WE 20030523000482003052300048NM 2003 5 23 2003UALA00408 120030503A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29324UA 23956 BELLY SKIN AREA OF THE AFT FUSELAGE DRAIN MAST IS GOUGED. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE, FILLER & DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030523001252003052300125NM 2003 5 23 2003UALA00433 120030421A575465C26602302 WEDGE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 5 SLAT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 HAIL DAMAGE OCCURRED TO T/E WEDGE, NR 5 SLAT. REPAIRED T/E WEDGE, SLAT NR 5. 2L72 4F4 FRTA16WE E2GL 20030523001262003052300126NM 2003 5 23 2003UALA00434 120030421A575465C26601382 WEDGE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 6 SLAT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 HAIL DAMAGE OCCURRED TO T/E WEDGE, NR 6 SLAT. REPAIRED T/E WEDGE, SLAT NR 6. 2L72 4F4 FRTA16WE E2GL 20030523001332003052300133NM 2003 5 23 QXEA0300505 120030419A5310 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX-DENT DAMAGE BETWEEN X281.0 AND X301.0, SRINGER 12 AND STRINGER 11. REPAIRED IAW HORIZON AIR EA 6-53-171 AND RD84-53-440. 2H72 4T RTA13NM 20030523001342003052300134WP 2003 5 23 DHL2003804886 120030205A53203754473501 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 AFT CARGO COMPT SPLICE FITTING CRACKED AT STA 1320.000, L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 AND FAX BOEING SEU-LIM-03-00002H DATE JUN 20, 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON AFT CARGO COMPT AT STA 1320.000 L-31L IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030527000052003052700005WP 2003 5 27 DHL2003604525 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBOARD L/E FORMER AT STA XFS 691.250 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000122003052700012WP 2003 5 27 DHL2003801066 120030406A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING INBOARD L/E FORMER WITH 1.000 INCH CRACK AT STA XFS 578.750. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED NEW DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-20D PG 21. 2L74 4F RT4A25 20030527000192003052700019NM 2003 5 27 VNAA0305007 120030512A3010851003 EJECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ANTI ICE SYSTEM FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07442JS1872789 3060 DURING CLIMBOUT, THE CREW RECEIVED AN AIRFOIL DE-ICE FAIL INDICATION. FLIGHT 4176 THEN RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 17HH EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030527000222003052700022NM 2003 5 27 DHL2003754006 120030510A2613 PANEL BOEING727 727223 1384074NM OVERHEAT PROTECTMALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 LOWER AFT BODY OVERHEAT WILL NOT TEST. TRANSFERRED TO DMI LOG IAW DHL MEL 26-10-2. THIS IS DMI 12873 PLACARDS INSTALLED TEST ONLY. REF DMI 12873, LOWER AFT BODY OVERHEAT WILL NOT TEST. REMOVED AND REPLACED FIRE AND OVERHEAT PROTECTION PANEL, OPS CHECKED GOOD IAW BMM CHAPTER 26-14-0. 2L73 4F A3WE 20030527000342003052700034WP 2003 5 27 DHL2003804874 120030120A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING CTR L/E FORMER UPPER PART AT STA XFS 372.000 WITH .500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED .500 CRACK ON CENTER L/E FORMER UPPER PART IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE 2024T3 AL.032 IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON CTR L/E FORMER UPPER PART, STA XFS 372.000 IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20030527000482003052700048NM 2003 5 27 CALA0300245 120030512A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND L-2 DOOR ENTRYWAY Z-ANGLE CORRODED AT STA 943-987. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-2. 2L72 4F RTA16WE 20030527000592003052700059WP 2003 5 27 AALA20030388 120030330A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT CHAFED A AALAK NONE O OTHER ININSP/MAINT 1 SW21490AA 49683 BOS - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT FROM ROW 1-9 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000612003052700061WP 2003 5 27 AALA20030261 120030228A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21269AA 49292 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER FORWARD OVERWING HATCHES INOPERATIVE. SECURED EMERGENCY EXIT LIGHT WIRE ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000722003052700072WP 2003 5 27 AALA20030447 120030411A3397 HARNESS DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21510AM 49804 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT IGHT AT 10D INOPERATIVE. REPLACED EMERGENCY LIGHT PIGTAIL ASSEMBLY AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000832003052700083WP 2003 5 27 AALA20030413 120030406A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2176201 53291 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS FROM ROW 17-21 INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030527000852003052700085WP 2003 5 27 AALA20030317 120030317A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217535A 49989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 20D INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT BATTERY IN FORWARD AND MID CABINS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000892003052700089WP 2003 5 27 AALA20030381 120030328A25601001191 FLASHLIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21258AA 49288 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT ARM INDICATOR INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527001042003052700104NM 2003 5 27 C7WA200200042 120030328A29106517844250 LINE BOEING727 7272J7 138400ENM HYD SYSTEM LEAKING A C7WAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17128NA 20879 LOST SYSTEM A HYDRAULIC. ENGINE NR 1 PUMP LOW PRESSURE LIGHT FOLLOWED BY FLUID LOSS IN FLIGHT. REMOVED AND REPLACED TWO EACH HYDRAULIC LINES, P/N 65-17844-250 AND 65-17844-17, LEAK CHECK GOOD. (M) 2L73 4F A3WE 20030521001802003052100180WP 2003 5 21 DHL2003804907 120030120A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 M/C COMPT NR 3 LT TRACK LUG WORN, STA 785.000. REMOVED NR 3 LT TRACK DAMAGED AREA IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521001842003052100184WP 2003 5 21 DHL2003604509 120030429A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBOARD L/E FORMER AT STA XFS 585.000 WITH 0.500 INCH CRACK. STOP DRILLED CRACK AT STA XFS.585.000, FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030522000012003052200001 2003 5 22 372PA0026 420030508A3444959960714931 ALTIMETER BOEING737 737306 13844BGNM COCKPIT INOPERATIVE A PIDAO OTHER O OTHER CLCLIMB 1 SO05372PA 23546 RADIO ALTIMETER INOP. COMMAND BARS DISAPPEAR WHEN HITTING TOGA TRIGGERS ON TAKEOFF, ALSO DISAPPEAR WHEN VOR/LOC ENGAGES. BANK ANGLE NEVER EXCEEDS 5 DEGREES IN HDG OR LNAV MODE DURING TURNS. ALTITUDE ALERT HORN DOES NOT WORK. CLEANED CONNECTORS ON ANALOGUE TO DIGITAL ADAPTERS AND OPS CHECKED PER MM 34-31-02. REMOVED AND REPLACED NR 1 AND NR 2 RADIO ALTIMETERS AND OPS CHECKED PER MM 34-31-02. 2L72 4F RTA16NE 20030522000132003052200013SO 2003 5 22 C2XA03TY063 120030517A531514525422001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION, CORRODED INSERTS AND SURFACE OXIDATION WAS FOUND ON FLOORBEAM, LEFT OUTBOARD AFT IN LAV. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IN LAV IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000502003052200050WP 2003 5 22 GTIA030299 120030501A216160715211 SELECTOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE CABIN TEMP INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23815NK 49415 IN AUTO RIGHT, AC WENT FULL HOT, SMOKE IN CABIN LAVATORY, ALARMS WENT OFF. SWITCHED TO FULL COLD IN MANUAL, CABIN CLEARED, ALARMS OFF. TRIED AUTO MODE AGAIN, ONLY HELD FULL COLD IN ANY POSITION. OPERATES NORMAL IN MANUAL. REMOVED AND REPLACED CABIN TEMP SELECTOR, OPS CHECK GOOD. 2L72 4F4 FRTA6WE E2EA 20030522000622003052200062SO 2003 5 22 C2XA03TY068 120030517A531514525393003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 TYS, DURING A SCHEDULED INSPECTION THE CARGO FLOOR LONGITUDINAL BEAM JUST AFT OF LOADING RAMP WAS GOUGED. MAINTENANCE BLENDED THE DAMAGED AREA ON FLOOR SUPPORT AT FR68, FABRICATED AND INSTALLED A DOUBLER, ALODINED, PRIMED AND PAINTED IAW EC5320-01096. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000642003052200064WP 2003 5 22 GTIA030293 120030425A3260 TARGET DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE PROXIMITY SWITCHDIRTY A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23820NK 49126 GEAR DOOR OPEN LIGHT (AMBER) CAME ON IN CRUISE FOR ABOUT 5 MIN AND THEN WENT OUT FOR DURATION OF FLIGHT. NO GEAR RED LIGHTS WERE ON AT ANY TIME. PERFORMED BITE CHECK ON ELECTRONICS PRO BOX, NO FAULTS FOUND. INSPECTED PROX SWITCH AND TARGET FOR GEAR DOORS, FOUND LEFT MAIN TARGET DIRTY, CLEANED SAME. OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20030522000672003052200067SO 2003 5 22 C2XA03SH134 120030518A532014521725001 BEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV DURING C-CHECK LEFT HAND CROSSBEAM AT FRAME 19 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030522000992003052200099NM 2003 5 22 SWAA031093 120030514A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACK (2 EA ) AT STR 15R, BS 500C & BS 500D. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030522001012003052200101 2003 5 22 SWAA031095 420030515A25656557463 GIRT BAR BOEING737 7373Q8 1384670NM AFT SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. SECURED ATTACH FITTING PER MM. 2L72 4F RTA16WE 20030523000212003052300021EA 2003 5 23 QXEA0300566 120030515A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX- DAMAGED RIVET ON STRINGER 7 BETWEEN STATION 565.00 AND 581.00 BETWEEN RIGHT HAND WINDOWS 7 & 8. REPAIRED IAW CRJ-700 SRM 51-42-06 AND 51-25-16. 2L72 4F RTA21EA 20030523000582003052300058NM 2003 5 23 SWAA031119 120030518A335065C27093 LIGHT BOEING737 7372H4 138448CNM SERVICE DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGHENCY EXIT LIGHT ASSY PER MM. 2L72 4F A16WE 20030523000832003052300083EA 2003 5 23 QXEA0300554 120030502A2150 BLADE CNDAIRCL600 CL6002C10 1390015EA ZONE 300 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 CKB - RIGHT HAND AFT FUSELAGE VENT IS MISSNG ONE RAM AIR EXHAUST DUCT BLADE. REPAIRED IAW WVAC EO 601R-21-3960. 2L72 4F RTA21EA 20030523000912003052300091WP 2003 5 23 MWEA030223 120030519A5230591014167 ANGLE DOUG DC9 DC982 3022082WP NR 5 DOOR CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FORWARD CARGO COMPARTMENT DOOR OUTER PAN IS CHAFED UNDER THE FORWARD NUMBER 5 DOOR STOP PAD. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F A6WE 20030523001012003052300101 2003 5 23 AWXA200300545 420030515A256565C1990116 CABLE BOEING737 737375 13844BNNM ESCAPE SLIDE FRAYED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 PHX - EES - DURING INSPECTION THE R-2 DOOR EMERGENCY ESCAPE SLIDE CABLE WAS FOUND FRAYED. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW T/C I1C25009. 2L72 4F RTA16WE 20030523001032003052300103NM 2003 5 23 AWXA200300547 120030507A5340146N872216 FITTING BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON RT CORNER FITTING AT BS 1720. MAINTENANCE REMOVED CORRODED RT CORNER FITTING AT BS 1720; FABRICATED A NEW REPLACEMENT CORNER FITTING PER DWG 146N8722; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 1-2. 2L72 4F RTA2NM 20030523001272003052300127NM 2003 5 23 QXEA0300578 120030517A2720 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09351PH8676 490 SEA-ON FLIGHT NUMBER 2008, ON CLIMBOUT THROUGH 8,000 FEET, RUDDER PRESSURE AND RUDDER PRESSURE CAUTION LIGHTS ILLUMINATED. REMOVED AND REPLACED DUAL LEVEL PRESSURE REGULATOR. PERFORMED OPERATIONAL CHECK OF DUAL PRESSURE REGULATOR VALVE. OPERATIONAL/LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523001312003052300131NM 2003 5 23 2003UALA00436 120030514A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29917UA 25384 FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. 2L72 4F4 FRTA16WE E2GL 20030523001352003052300135WP 2003 5 23 DHL2003804879 120030207A535057103692N FAIRING DOUG DC8 DC873F 302199FWP RT WING DELAMINATED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 RT WING NR 709 AFTER WING FUSELAGE FILLET EXTERNAL SKIN DELAMINATED STA 108.000 - STA 120.000. REMOVED DELAMINATED PANEL (RT WING STA 108.000 - 1120.000) IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, INSTALLED NEW PANEL (FROM USA) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030527000462003052700046NM 2003 5 27 DLM88030332 120030403A5270833703 SENSOR DOUG MD88 MD88 3023688NM RT MLG WW INOPERATIVE A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27937DL 49810 LANDING GEAR DOOR OPEN LIGHT ON AT FL330, STAYED ON WITH CLB TO FL350. LIGHT STAYED ON APPROX 20 MINUTES THEN WENT OUT. STAYED OUT REMAINDER OF FLT. REPLACED RIGHT MLG DOOR PROX SWITCH AND ADJUSTED PER M/M 32-60-05. GEAR DOOR INDICATION NOW TESTS NORMAL. 2L72 4F RTA6WE 20030527001012003052700101WP 2003 5 27 2003F00312 120030306A3260BZE712NT1 SWITCH CVAC 340 340CVAC 242270AWP NLG MALFUNCTIONED A VGCAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO17151FL 51 NO GEAR NOSE GEAR INDICATION. MADE FLYBY AT CMH. GEAR APPEARED TO BE DOWN AND LOCKED. PERFORMED VISUAL FROM COCKPIT. GEAR APPERAED TO BE LOCKED. LANDED WITHOUT ANY INCIDENT. ADJUST NOSE GEAR SWITCH. SING NOSE GAR PER CH 11 FIG 11-6-102 CONVAIR MM. ALL INDICATIONS NORMAL. (M) 2L72 4R 6A6 20030528000042003052800004EU 2003 5 28 HEEA086730 120030522A243523032048 STARTER GEN BOLKMS105 BO105S 5626006EU ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 STARTER GENERATOR HAS UNCONTROLLED VOLTAGE. SHOP REPAIR. 1G72 3U H3EU 20030528000412003052800041 2003 5 28 HEEA086595 420030521A3452071119208 DISPLAY BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 DISPLAY TOO DIM TO READ DURING DAYLIGHT. REPLACED V101 PHOTOCELL, DISPLAY LENS. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030528000562003052800056NE 2003 5 28 HEEA086742 220030522A7314P94B12209 PUMP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH1790 3248 FUEL PUMP DOES NOT RUN. TO BE SENT TO VENDOR. 1G71 3U3 U H9EU E19EU 20030528000592003052800059GL 2003 5 28 ERAA086448 220030425A753023053176 BLEED VALVE BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL COMPRESSOR FAILED E ERAAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 FS01133EH5342 598 BLEED VALVE / COMPRESSOR STALL : OVERHAULED BLEED VALVE CHANGED NECESSARY PARTS.. 1G72 3U3 UNCH3EU E4CE 20030528000652003052800065EU 2003 5 28 BAQA085218 120030321A6710L673M40A1001 ACTUATOR UROCOPEC135 EC135T1 5620026EU FENESTRON LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01118WS583 0089 FENESTRON ACTUATOR HAS PLAY IN CONTROL ARM AND LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030528000742003052800074WP 2003 5 28 AALA20030252 120030227A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21437AA 49455 RIGHT LIGHT ASSEMBLY AT OVERHEAD ROW 7 IS BROKEN. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M0 2L72 4F RTA6WE 20030528000942003052800094GL 2003 5 28 ALGA086457 220030520A731347104R SHROUD CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C20B 03013GL FUEL NOZZLE MISMANUFACTURED E ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO 0615 FOUND PART TO BE MACHINED WRONG. RETURNED PART TO MANUFACTURER. FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E4CE 20030523000622003052300062NM 2003 5 23 QXEA0300557 120030515A6120M390166105L RELAY DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09346PH 477 PDX-ON FLIGHT NUMBER 2173, ON TAKEOFF WITH BOTH POWER LEVERS AT TAKEOFF POSITION AND BOTH TORQUES APPROX 97 PERCENT, AUTOFEATHER ARM LIGHT FAILED TO ILLUMINATE. DUPLICATED PROBLEM, AUTOFEATHER WOULD NOT ARM OR TEST, REPLACED RELAYS 6121 K-5 & 6121 K-19. OPERATIONALLY TESTED AUTOFEATHER CIRCUITS. AUTOFEATHER ARMED & POWER UPTRIM OPERATED NORMAL. BOTH PROPS WHEN SELECTED AUTOFEATHERED NORMALLY. SYSTEM OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523000962003052300096WP 2003 5 23 MWEA030215 120030519A5347SRO953011113 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 CAPTAINS AFT OUTBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED TRACK. 2L72 4F A6WE 20030523001042003052300104NM 2003 5 23 QXEA0300506 120030425A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH* 444 528 SEA- RIGHT HAND AFT OUTSIDE EMERGENCY LIGHT, AFT OVERHEAD EMERGENCY LIGHT, AND CENTER OVERHEAD EXIT SIGN ARE INOPERATIVE. REMOVED AND REPLACED NR 5 EMERGENCY BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523001052003052300105NM 2003 5 23 QXEA0300540 120030506A30804100S00501 VALVE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 FAILED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09413QX1532 1532 4060 SEA- ON FLIGHT 2330 DEICE PRESSURE CAUTION LIGHT. PERFORMED EMERGENCY CHECKLIST. FOUND RIGHT OUTBOARD WING BOOT SLOW TO INFLATE WITH LOWER PRESSURE THAN LEFT SIDE. REMOVED AND REPLACED DUAL DISTRIBUTION VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523001092003052300109EA 2003 5 23 QXEA0300617 120030519A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 BOI-CENTER CHIMNEY DAMAGED FORWARD CARGO BAY. INSTALLED NEW CENTER CHIMNEY IN FORWARD CARGO BAY IAW TASK 268100Q01 ON LINE 1 CHECK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030523001102003052300110NM 2003 5 23 QXEA0300618 120030517A5270 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 800 ILLUMINATED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09413QX 4060 PDX-ON FLIGHT NUMBER 2355, LEFT HAND REAR PASSENGER DOOR WARNING CAME ON AT 5,000 FEET DURING DESCENT. CABIN PRESSURIZATION LOST AND CABIN CLIMBED TO 4,000 FEET. INSPECTED PASSENGER DOOR (AFT) PERFORMED PROXIMITY OPERATIONAL TEST 31-62-00-710-001 AND FUNCTIONAL TEST OF AFT PASSENGER DOOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523001192003052300119NM 2003 5 23 CALA0300251 120030515A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND U-CHANNEL FOR DRAIN MAST CORRODED AT STA 986.5 BETWEEN S24L AND S25L. INSTALLED DRAIN MAST IAW MM 30-71-00, PAGE 501-503. 2L72 4F RTA16WE 20030521000392003052100039WP 2003 5 21 DHL2003801068 120030506A535056563501 PANEL DOUG DC8 DC873F 302199FWP WING TO BODY DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING TO FUSELAGE UPPER FILLET NR 706 INTERNAL SKIN DELAMINATED (STA 912.000-980.000). REMOVED AND REPLACED LT WING TO FUSELAGE UPPER FILLET NR 706 (STA 912.000-980.000) IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000872003052100087NM 2003 5 21 DHL2003747501 120030511A5754 STRUCTURE BOEING727 727224 1384076NM LT WING FLAP CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK DISCREPANCY AS FOLLOWS, DEEP CHAFE MARK ON DOUBLER OUTBOARD LEADING EDGE OF INBOARD FOREFLAP LT. REMOVED OLD DOUBLER AND FABBED NEW DOUBLER IAW B-727 SRM 57-50-4 FIG 1 FROM 2024-T3 .050 PO 9912495 2. DOUBLER DIMENSIONS 4 INCH X 4 INCH. ALODINED AND PRIMED DOUBLER AND MATING SURFACE IAW B-727 SRM 51-10-2. INSTALLED DOUBLER IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20030521001172003052100117WP 2003 5 21 MWEA030212 120030516A5230591014167 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 MID CARGO DOOR OUTER PAN IS CRACKED FORWARD END ADJACENT TO INNER PAN. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030521001292003052100129NM 2003 5 21 DHL2003755007 120030508A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01755DH 21857 FUSELAGE HAS HOLE IN LEFT SIDE, FORWARD OF AFT PRESSURE BULKHEAD, BY GROUND VEHICLE. ACCOMPLISHED REPAIR ON DAMAGED SKIN AS PER B727 SRM 53-30-3. PERFORMED PRESSURE CHECK, CHECKS OK. PATCH REPAIRED NEEDS TO BE PAINTED. TRANSFERRED TO DMI 12871E OK PER GMM 3.5 CAT-2. DOES NOT EFFECT SAFE OPS OF THE A/C. AFT LOWER CARGO GILL LINER REMOVED FOR INSPECTION AND REPAIR OF DAMAGED SKIN AND STRINGER. GILL LINER REPLACED FOLLOWING STRUCTURAL REPAIRS M/M 25-52. FURTHER INSPECTION ON ITEM 1M L/P 331006 FOUND STRINGER 24 BETWEEN STATION 1130 AND 1148 BROKEN. PERFORMED REPAIR ON STRINGER AS PER B727 SRM 53-10-3 DETAIL 1. PERFORMED PRESSURE CHECK. CHECKED OK. 2L73 4F A3WE 20030521001382003052100138WP 2003 5 21 DHL2003801042 120030409A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 EXTERNAL FUSE CRACKED 1.000 INCH STA 1743.000 - STA 1746.000 BETWEEN L-16R AND L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6 0.063), DOUBLER (7075-T6 0.071) AND FINGER DOUBLER (7075-T6 0.040) IAW SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 51-1-8B. INSTALLED CONICAL SPACER IAW SRM 51-1-26 FIG 1. INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7, SRM 51-1-15 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521001512003052100151WP 2003 5 21 MWEA030197 120030501A5230995766440 CLIP DOUG DC9 DC981 3022081WP CARGO DOOR MISALIGNED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 MID CARGO DOOR ATTACH CLIP DOES NOT LINE UP WITH NEW SKIN REPAIR. FABRICATED AND INSTALLED NEW CLIP. 2L72 4F A6WE 20030521001672003052100167NM 2003 5 21 SWAA031087 120030513A53306545785 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED C3 CHECK, FOUND RIGHT NR 1 PAX WINDOW CUTOUT CRACKED AT LOWER AFT CORNER. REPAIRED WINDOW SKIN PER SWA EA. 2L72 4F A16WE 20030522000182003052200018WP 2003 5 22 GTIA030285 120030415A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 PAX CABIN FLOOR INTERCOSTAL CRACKED AT FS 1041 OBL. REMOVED DAMAGE INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. 2L72 4F4 FRTA6WE E2EA 20030528000992003052800099SW 2003 5 28 HEEA086608 120030521A6520212040506005 CASE BELL 412 412 1182202SW GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z AHP52789 36019 TAIL ROTOR GEARBOX CASE CORRODED. 1G72 4U H4SW 20030528001042003052800104 2003 5 28 BAQA086477 420030522A3451066106900 INDICATOR BOLKMS117 BK117A3 5626015EU DME INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01932CJ1485 7024 DME INOPERATIVE USING NR 2 NAV. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030523000102003052300010NM 2003 5 23 2003F00293 120030119A52306559948502 DOOR BOEING727 727222 1384073NM CARGO CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND NR 2 AFT CARGO DOOR, LOWER AFT CORNER IS CRACKED. REMOVED AND REPLACED LOWER AFT DOOR CORNER, NR 2 CARGO DOOR. (M) 2L73 4F A3WE 20030523000262003052300026NM 2003 5 23 AWXA200300567 120030507A5320146N53363 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT BETWEEN BS 1680 AND BS 1700, LBL 50. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT BETWEEN BS 1680 AND BS 1700, LBL 50; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 7. 2L72 4F RTA2NM 20030523000702003052300070NM 2003 5 23 SWAA031102 120030516A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 500C + 16, LBL 19. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20030523001162003052300116NM 2003 5 23 2003UALA00424 120030513A5230 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29654UA 25392 BULK CARGO DOOR EXTERNAL SKIN DENTED. MAJOR REPAIR - INSTALLED EXTERNAL DOUBLER. 2L72 4F4 FRTA1NM E24NE 20030527000102003052700010WP 2003 5 27 DHL2003801059 120030408A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING - CTR L/E FORMER CRACKED 0.500 INCH AT XS 484.895. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE AND NEW FASTENERS IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000652003052700065WP 2003 5 27 AALA20030392 120030402A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2170529 49921 DFW - DURING OVERNIGHT MAINTENANCE, CEILING PANEL EMERGENCY EXIT LIGHT ABOVE CATWALK IN AFT SECTION INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000702003052700070WP 2003 5 27 AALA20030285 120030306A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21493AA 49731 EMERGENCY EXIT LIGHT ABOVE EXIT DOORS ROW A AND B AT 20 DEF INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000802003052700080NM 2003 5 27 AMTA200300596 120030502A33503020421 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11516AT 27972 L1 DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 335106. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030527001142003052700114SW 2003 5 27 SVB2003F00000 120030202A2910 SEAL BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL HYD SERVO LEAKING D SVBAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL2730SV 2768 23002 RAPID SERVO LEAK EMPTIED NR 1 HYDRAULIC SYSTEM IN LESS THAN 6 MINUTES. COLLECTIVE CYCLIC SERVO CONTINUED TO FUNCTION ON NR 2 HYDRAULIC SYSTEM BUT TAIL ROTOR CONTROLS WERE INOPERATIVE REQUIRING A FORCED LANDING. 1G72 3U3 UNCH9SW E1GL 20030528000052003052800005EU 2003 5 28 HEEA086731 120030522A6220 SPRING AEROSPAS355 AS355* EU VIBE ABSORBER BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH2347 M1733 3352 BROKEN SPRING FOUND ON VIBRATION ABSORBER DURING INSPECTION. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030529000322003052900032SW 2003 5 29 HEEA086630 120030521A6220 BEARING BELL 412 412 1182202SW PENDULUM ASSY. WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03415A 814 A4187 36257 MAIN ROTOR PENDULUM ASSY HAS PLAY IN BEARING. REPAIRED. 1G72 4U H4SW 20030529000392003052900039NE 2003 5 29 HEEA086503 220030521A72000292005250 ENGINE SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1A1 60030NE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 7947 760166 ENGINE PRODUCING LOW POWER. 1G72 3U3 U H1NE E19EU 20030529000422003052900042SW 2003 5 29 HEEA086633 120030521A6230412010405111 FITTING BELL 412 412 1182202SW M/R LINK CLOGGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 PLUGGED GREASE FITTING, WON'T TAKE GREASE. REPAIRED. 1G72 4U H4SW 20030522000312003052200031WP 2003 5 22 GTIA030284 120030407A7160 SCREEN DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NR 1 ENGINE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 NR 2 ENGINE NOSE COWL ACOUSTIC DELAMINATING, 11:00 O`CLOCK AS MARK. REPAIRED NR 1 INLET ACOUSTIC SCREEN. 2L72 4F4 FRTA6WE E2EA 20030522000412003052200041 2003 5 22 372PA0028 420030511A2210 COMPUTER BOEING737 737306 13844BGNM AUTOPILOT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05372PA 23546 ALTITUDE ALERT HORN DOES NOT WORK. COMPLETED OPERATIONAL CHECKS PER MM 22-11-01 AND PERFORMED BITE CHECK USING FMC DFCS. NO DEFECTS NOTED. 2L72 4F RTA16NE 20030522000422003052200042 2003 5 22 801DM0009 420030503A2210163000105 SERVO BOEING757 757200 1384950NM AILERONS MALFUNCTIONED A PIDAO OTHER O OTHER CRCRUISE 1 SO05801DM 26240 NO LAND 3 AILERON SERVO FCCR MESSAGE ON MCDP. REMOVED AND INSTALLED SERVICEABLE AILERON LATERAL CONTROL SERVO. ADJUSTMENT, TEST, LEAK AND OPS CHECK GOOD IAW MM 22-13-03. 2L72 4F RTA2NM 20030522000612003052200061SO 2003 5 22 C2XA03TY052 120030517A531014522460009 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE PUNCTURED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 TYS, DURING A SCHEDULED INSPECTION THE CENTER BEAM IN IN GALLEY, TOP CAP HAS A PUNCTURE AT THE END. MAINTENANCE FABRICATED A DOUBLER AND INSTALLED IAW EC5320-01095. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030523000292003052300029 2003 5 23 AWXA200300570 420030515A256560592101 FITTING AIRBUS320 A320231 3930325EU ZONE 150 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW251248625 271 MCN - EES - DURING C-01 CHECK THE LT OVERWING HATCH SLIDE BOTTLE CABLE FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING HATCH SLIDE BOTTLE IAW AMM SUBTASK 25-62-46-020-050-A, AND 25-62-46-420-050-A, OPERATIONAL CHECK WAS GOOD IAW AMM 25-62-46-710-052. 2L72 4F RTA28NM 20030523000442003052300044EA 2003 5 23 QXEA0300507 120030425A2611 COMPUTER CNDAIRCL600 CL6002C10 1390015EA SMOKE DETECTOR FALSE INDICATIONA QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09613QX 10045 SEA - FLIGHT 2501 - CREW RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A FWD SMOKE DETECTOR 3 FAILED CMD ON THE MAINTENANCE DIAGNOSTICS COMPUTER. A FIRE DETECTION SYSTEM TEST WAS PERFORMED AND CHECKED GOOD. NO MORE FAULTS LISTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030523000742003052300074NM 2003 5 23 QXEA0300538 120030430A5414 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - LEFT HAND NACELLE LOWER COWL AFT CONE SUPPORT APPEARS TO HAVE CRACKS. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030523001442003052300144WP 2003 5 23 DHL2003604515 120030426A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD L/E FORMER AT STA XFS 866.250 CRACKED 0.500 INCH. STOP DRILLED CRACK AT XFS 866.250. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030523001462003052300146WP 2003 5 23 MWEA030205 120030509A712059357041 YOKE DOUG DC9 DC981 3022081WP ENGINE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LEFT ENGINE YOKE UPPER ISOLATOR COVER BOLT HAVE CORROSION INSIDE, HOLES ON YOKE. INSTALLED NEW YOKE ISOLATORS AND ABSORBERS. 2L72 4F A6WE 20030527000042003052700004WP 2003 5 27 DHL2003604519 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING INBOARD L/E FORMER CRACKED 0.500 INCH, STA XFS 635.00. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000152003052700015NM 2003 5 27 DHL2003747504 120030513A5311 FRAME BOEING727 727224 1384076NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR FRAME AT BS 540 HAS A GOUGE BETWEEN ST 17R/16R. BLENDED AREA FOUND WITH OUT LIMITS IAW SRM B-727 51-10-1. FABRICATED AND INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-40-3 FIG 1. TREATED AND PRIMED IAW 51-10-2 NOT DIMENSIONS 10 X 6.52, 7075 T-6 .063 INCH MAT P/O 9912495. 2L73 4F A3WE 20030527000212003052700021NM 2003 5 27 VNAA0305010 120030515A30604E29473 TIMER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE DE-ICE FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07427JS18547677 3039 EN ROUTE, THE CREW RECEIVED A LEFT HAND PROP HEAT FAIL INDICATION AND WAS ADVISED TO DIVERT TO PIT. MAINTENANCE THEN INSPECTED AND REPLACED THE DE-ICE TIMER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030527000302003052700030NM 2003 5 27 DL72S030324 120030402A7710 SEAL BOEING727 727225A 1384077NM PWA JT8 JT8D15 52051NE NR 1 TACH GEN LEAKING A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO278890Z61916 21859 687469 FUMES IN THE CABIN REPORTED BY F/A. FOUND NR 1 ENG TACH GENERATOR SEAL LEAKING. REPLACED SEAL, LEAK CKS OK. NO ODORS DET. 2L73 4F4 FRTA3WE E2EA 20030527000352003052700035NM 2003 5 27 0300906631 120030404A5311 FRAME BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01631US 23111 DURING H-CHECK A CRACK WAS FOUND IN THE FRAME WEB AT BS 1265. REPAIRED PER EA 66-193812. 2L74 4F A20WE 20030527000492003052700049NM 2003 5 27 CALA0300246 120030512A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716339 23577 INSPECTION FOUND A CRACK IN RT PRESSURE DECK AT STA 665-675, RBL 35-45. THE PRESSURE DECK WAS REPAIRED IAW ECRA 5312-01021. 2L72 4F RTA16WE 20030527000692003052700069WP 2003 5 27 AALA20030284 120030305A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217526A 49918 ORD - EMERGENCY EXIT LIGHT AT FORWARD ENTRY, FORWARD GALLEY, AND OVER LEFT SEATS 26-29 DIM. CLEANED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000732003052700073WP 2003 5 27 AALA20030446 120030411A3397 HARNESS DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21510AM 49804 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 7D INOPERATIVE. REPLACED EMERGENCY LIGHT PIGTAIL ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000812003052700081NM 2003 5 27 AMTA200300594 120030502A3350BPS73 BATTERY BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND R1 EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER FOR THE FORWARD RIGHT EMERGENCY LIGHTS IAW B757 MM 33-51-07. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030527000822003052700082WP 2003 5 27 AALA20030418 120030406A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21582AA 53159 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 28-29 AND LEFT SERVICE DOOR IN CEILING PANEL INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR ROWS 22-29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000942003052700094EA 2003 5 27 2003F00304 120030219A3260G601R3261011 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0797325 7325 FLT 6012 - PHX-PSP, RETURN TO FIELD FOR GEAR DISAGREE MESSAGE ON TAKEOFF. MAINTENANCE REPLCED THE PROX SENSOR. AIRCRAFT BACK IN SERVICE. (M) 2L72 4F RTA21EA 20030527001002003052700100EA 2003 5 27 2003F00310 120030319A5320601R8500239 BRACKET CNDAIRCL600 CL6002B19 1900309EA NLG PROX SENSOR OUT OF POSITION A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW0777278 7278 WHILE IN FLIGHT, NOSE LANDING GEAR DOOR ON EICAS SHOWED GEAR DOOR OPEN. MAINTENANCE IS TROUBLESHOOTING. MAINTENANCE ADJUSTED CENTER PROX SENSOR BRACKET. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20030527001022003052700102CE 2003 5 27 2003F00313 120030422A3240A41130 SWITCH CESSNA750 750 2076810CE PARKING BRAKE BROKEN A UG8AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL235112 7500010 DURING TAXI TO TAKEOFF, THE NO TAKEOFF CAUTION APPEARED ON THE EICAS. SIMULATNEOUSLY, THE PARK BRAKE PRESS LOW MESSAGE WAS ILLUMINATED. THE CREW TAXIED BACK TO GM BASE AND ANOTHER AIRCRAFT WAS UTILIZED FOR THE FLIGHT. UPON TROUBLESHOOTING, THE PARK BRAKE SWITCH WAS FOUND TO BE FAULTY. THE CONTACT PLUNGER HAD DETERIORATED, THUS NOT ACTUATING THE CONTACTS. SWITCH HAS BEEN REQUESTED. (M) 2L72 4J RTT00007WI 20030522000302003052200030WP 2003 5 22 GTIA030277 120030427A3260 CONNECTOR DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE MLG UPLOCK INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23818NK 48018 WITH GEAR UP ON DESCEND INTO LGA THE RED NOSE GEAR LIGHT ILLUMINATED SEVERAL TIMES-OUT FOR LANDING. PERFORMED BITE ON PSEU OF NOSE GEAR LOCKED AND NOSE GEAR UP POSITION SENSORS, BOTH PASS. CLEANED AND RESET CONNECTOR UPSTREAM OF D1-31 NOSE GEAR UP POSITION SENSOR. OPS CHECKED NORMAL. 2L72 4F4 F A6WE E2EA 20030522000522003052200052SO 2003 5 22 C2XA03TY058 120030517A532014521725001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 DURING A SCHEDULED INSPECTION THE LT SILL WAS FOUND CORRODED IN SEVERAL PLACES BETWEEN FR 19 AND 20. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND SILL IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030527000662003052700066WP 2003 5 27 AALA20030384 120030328A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21465A 49595 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAILCONE AND SEATS ROWS 21-31 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY, CLEANED CONTACTS, AND REPLACED WIRE FROM SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527001062003052700106NE 2003 5 27 2003F00316 220030226A7261693905B OIL CAP BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE NR 2 ENGINE LOOSE A PCSAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17794AJ 21243 FLT 835 - KMIA/UVF - CAPTAIN REPORTED, NR 2 ENGINE OIL QUANTITY INDICATED 1.5 WHILE INFLIGHT. LOW OIL QUANTITY LIGHT DID NOT ILLUMINATE. AIRCRAFT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE OIL CAP NOT SECURED. ENGINE OIL WAS SERVICED. OIL CAP REPLACED AND SECURED WITH SAFETY WIRE IAW MM 12-13-01. AIRCRAFT RETURNED BACK SERVICE. (M) 2L73 4F4 F A3WE E2EA 20030527001222003052700122SW 2003 5 27 CYX2003F00000 120030430A6220407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR ROUGH A CYXRO OTHER O OTHER NRNOT REPORTED 1 CE01407LG225 53143 THIS BEARING WAS REMOVED DURING A ROUTINE SCHEDULED INSPECTION. IT WAS ROUGH AND NOISY COMPARED TO THE OTHER FIVE BEARINGS IN THE TAIL ROTOR DRIVE SYSTEM. IF NOT FOR THE PORBLEMS THIS MODEL HELICOPTER HAS HAD IN THIS AREA, THE BEARING WOULD PROBABLY BEEN LEFT IN SERVICE. THE BEARING WAS NOT REALLY THAT BAD. 1G71 3U O H2SW 20030528000062003052800006EU 2003 5 28 HEEA086732 120030522A6320350A32310121 FRICTION RING SNIAS 350 AS350B3 8680954EU M/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03973AE 3229 TRANSMISSION POWER TAKE OFF SEAL LEAKING. TO BE SENT TO VENDOR. 1G71 3U H9EU 20030528000082003052800008EU 2003 5 28 HEEA086734 120030522A3340356H2801 POWER SUPPLY SNIAS 350 AS350B2 8680813EU STROBE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH 3248 STROBE LIGHT POWER SUPPLY HASN`T ANY POWER OUTPUT. TO BE SENT TO VENDOR. 1G71 3U H9EU 20030528000122003052800012GL 2003 5 28 ERAA086434 220030424A7323252466715 GOVERNOR BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01125EH9642 S562 GOVERNOR HITS MAX STOP AT FULL BEEP WHEN COLLECTIVE IS UP. DROOPING, OVERSPEEDING EARLY, STIFF THROTTLE. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1G72 3U3 UNCH3EU E4CE 20030618001172003061800117SW 2003 6 18 HEEA087500 120030612A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 BLOWER ASSY WORN SPLINES. REPLACED. 1G71 3U O H2SW 20030618001222003061800122SW 2003 6 18 HEEA087502 120030612A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 BLOWER ASSY HAS A BEARING ROUGH. REPLACED. 1G71 3U O H2SW 20030618001332003061800133 2003 6 18 HEEA087140 420030610A2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 ICS MAKING LOUD SQUEALING NOISE. SHOP REPAIR. 1G72 3U H1NE 20030618001552003061800155SW 2003 6 18 HEEA087504 120030612A6710SL504ASP5 NUT BELL 407 407 1182206SW CYCLIC WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 LOW CYCLIC FRICTION - COULD NOT ADJUST DUE TO WORN THREADS. SCRAPPED. 1G71 3U O H2SW 20030618001602003061800160EA 2003 6 18 COMA0360279 120030614A2750860D10018ABC CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01982CA12866 7168 FLIGHT 5778 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 20030618001702003061800170SW 2003 6 18 HEEA087363 120030611A5320407070620125 PANEL BELL 407 407 1182206SW COLLECTIVE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 COLLECTIVE PANEL CRACKED. 1G71 3U O H2SW 20030618001722003061800172SW 2003 6 18 HEEA087510 120030612A6710214001347005 ACTUATOR BELL 412 412 1182202SW FLT CONTROLS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 FORCE TRIM NOT RELEASING INTERMITTENTLY. SHOP REPAIR. 1G72 4U H4SW 20030618001842003061800184SW 2003 6 18 HEEA087151 120030609A6710206001053005 BEARING BELL 206 206L1 1182107SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0383MT 45492 BELLCRANK ASSY HAS WORN BEARINGS. REPLACED BEARING (2 EACH) 206001053005 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618001942003061800194SW 2003 6 18 HEEA087160 120030609A6420206011724109 TUBE BELL 407 407 1182206SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 TAIL ROTOR HAS WEAR ON OUTBOARD END OF SHAFT. SENT TO H-S TOOLS & PARTS FOR INSPECTION AND REPAIR. 1G71 3U O H2SW 20030618002012003061800201SW 2003 6 18 HEEA087370 120030611A5320407070620150 TRIM PANEL BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 TRIM PANEL CRACKED. 1G71 3U O H2SW 20030618002152003061800215SW 2003 6 18 HEEA087168 120030609A6320206031594003 BEARING BELL 206 206B3 1181506SW FITTING ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322751 MS1600 3627 WORN BEARING. REPLACED BEARING 206031594003 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618002172003061800217SW 2003 6 18 HEEA087170 120030609A6330206033509003 BEARING BELL 206 206L3 1182108SW XMSN RESTRAINT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038592X LK0089 51508 WORN BEARINGS. REPLACED BEARINGS (2 EA) 206033509003 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030619000032003061900003SW 2003 6 19 HEEA087174 120030609A6320206040140013 BEARING BELL 206 206L3 1182108SW GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 BEARING SEAT WORN. SENT TO ABLE ENGINEERING FOR PARTIAL REPAIR. 1G71 3U H2SW 20030527000962003052700096NM 2003 5 27 2003F00306 120030428A3600379561 GASKET BOEING727 727212 138407GNM NR 3 WORN A PCSAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO17598AJ 21947 CREW REPORTED NR 3 STRUT OVERHEAT LIGHT CAME ON IMMEDIATELY AFTER LIFT OFF. CAPTAIN FOLLOWED AMERIJET NORMAL PROCEDURES AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEAK AT 13TH STAGE INBOARD DUCT. REMOVED AND REPLACED GASKETS. IN ADDITION, OFUND 2ND LEAK AT THE 13TH STAGE CHECK VALVE FORWARD CLAMP. TORQUE CLAMP, TESTED NR 3 ENGINE AT TAKEOFF AND PART POWER NO LEAKS NOTED. ACCOMPLISHED AMERIJET PROCEDURES FORM B-41 AND TESTED ENGINE PER MM 71-00. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L73 4F A3WE 20030527000992003052700099EA 2003 5 27 2003F00309 120030317A5320G601R3261011 BRACKET CNDAIRCL600 CL600* EA NLG PROX SENSOR DAMAGED A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07MASA 7264 ASH - FLT 6138 - PHX-MRY - RETURNED TO FIELD FOR NOSE GEAR DISAGREE MESSAGE AND NOSE GEAR DOOR. MAINTENANCE REPLACED NOSE GEAR PROX BRACKET AND OPS CHECKED AIRCRAFT, RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030522000022003052200002NM 2003 5 22 NACA20030085 120030508A575465185338 HINGE BOEING727 72723 1384004NM KRUEGER FLAP CORRODED A NACAK NONE O OTHER ININSP/MAINT 1 AL03930FT 19387 LT WING KRUEGER FLAP MOUNT BRACKET HINGE ASSEMBLY CORRODED. REMOVED AND REPLACED HINGE ASSEMBLY. 2L73 4F A3WE 20030522000392003052200039NE 2003 5 22 NACA20030083 220030503A8530356996 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 11 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA1459 1459 45529 37244 NR 2 ENGINE BACK FIRING AT FULL RICH AND LOSS OF BMEP. REPLACED NR 2 ENGINE, NR 11 CYLINDER. 2L74 4R4 R 6A3 5E8 20030522000402003052200040WP 2003 5 22 GTIA030290 120030415A5311 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE GOUGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 FRAME IS GOUGED AND CRACKED STA 207 BETWEEN STR 5L-6L. FABRICATED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS. 2L72 4F4 FRTA6WE E2EA 20030522001092003052200109NM 2003 5 22 AWXA200300548 120030516A3350BR964411 LIGHT BOEING737 737300 1384610NM ROW 13 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030522001322003052200132NM 2003 5 22 SWAA031111 120030519A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED (2 EA) AT STR 11R, BS 390 AND BS 500A. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030523000082003052300008NM 2003 5 23 2003F00291 120030120A5330 PANEL BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND STRINGER 5L, FUSELAGE STATION 360, SUPPORT PANEL 6F, CRACKED. REMOVED AND REPLACED PANEL STATION 360, STRINGER 5L. (M) 2L73 4F A3WE 20030523000252003052300025EU 2003 5 23 AWXA200300566 120030520A33501012661 LIGHT AIRBUS320 A320232 3930326EU SEAT ROW 10 BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28605AW 543 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT AT SEAT ROW 10 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030523000842003052300084EA 2003 5 23 QXEA0300527 120030504A29136619501 PUMP CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09612QX1142 1142 10042 PDX - FLIGHT 2402 - CREW REPORTED THE NUMBER 3 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 3 HYDRAULIC PUMP. OPERATIONAL CHECKS AND GEAR SWINGS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030523000852003052300085WP 2003 5 23 MWEA030228 120030521A274095906 MOTOR DOUG DC9 DC981 3022081WP STABILIZER DEFECTIVE A MWEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31804ME 48030 PRIMARY TRIM PROBLEM. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR AND FIRST OFFICERS YOKE TRIM SWITCH AND REPLACED CONNECTORS. 2L72 4F A6WE 20030523001002003052300100NM 2003 5 23 QXEA0300559 120030512A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX-DENT IN RIGHT HAND FUSELAGE SB 299.500 BETWEEN STRINGER 19 AND 20. REPAIRED IAW HORIZON AIR EA 6-53-253. 2H72 4T RTA13NM 20030527000322003052700032NM 2003 5 27 DLM88030326 120030402A2910P240002080240HH HOSE DOUG MD88 MD88 3023688NM LT HYD SYS LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27934DL 49721 ON CLIMBOUT LT HYD QTY AND PRESS DROPPED TO ZERO QTY BEGAN TO RISE ON ARRIVAL CVG, 4 QTS APPROACH 9 QTS ON SHUTDOWN PUMP OFF. REPLACING LINE P/N 299600044 LT ENG PRESS FLEX LINE. 2L72 4F RTA6WE 20030527000512003052700051NM 2003 5 27 CALA0300248 120030514A5320 STIFFENER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND STIFFENER AFT OF STA 1016, BL 0 CORRODED ON BOTH RIGHT AND LEFT SIDES. LEFT AND RIGHT STIFFENERS AND SPLICES WERE INSTALLED IAW EA 5310-04045 AND DRAWING 65C28106. 2L72 4F RTA16WE 20030528000102003052800010EU 2003 5 28 HEEA086736 120030522A6240614764031 INDICATOR SNIAS 350 AS350B2 8680813EU NR STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 NR NEEDLE STUCK AT 120 RPM AND NTL NEEDLE FLUCTUATES. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H9EU 20030528000192003052800019 2003 5 28 HEEA086578 420030522A2300N0001553 ANTENNA SKRSKYS76 S76A 8143006NE OUTERLINK MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035435V 760158 ANTENNA MALFUNCTIONED, OUTERLINK WON'T TRANSMIT. TO BE SENT TO VENDOR. 1G72 3U H1NE 20030528000282003052800028GL 2003 5 28 ALGA086422 220030515A723023051123 MOUNT CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30P 03013GL COMPRESSOR MISMANUFACTURED E ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO FOUND MOUNT PADS HEIGHT DIMENSION UNDER LIMITS. 1Q71 3R3 U 2A6 E1GL 20030528000212003052800021SW 2003 5 28 HEEA086586 120030430A2400214175131103 RELAY BELL 214 214ST 1182106SW ELECTRICAL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 NR 2 BATTERY WILL NOT GO INTO SERIES. 2G72 4U H10SW 20030528000362003052800036NE 2003 5 28 ERAA086446 120030425A6240 CONNECTOR SKRSKYS61 S61N 8142104NE TRANSDUCER CORRODED E ERAAO OTHER N FALSE WARNING NRNOT REPORTED 1 FS01561EH 486 61471 BIM LIGHT ON INTERMITTENT PRESSURE IN BLADE CHECKED GOOD. OPENED DIRTY CIRCUIT, CONNECTOR PLUG CORRODED. CIRCUIT REPAIRS AND CLEANING; NEW CONNECTOR PLUG; LEAK TESTED; CIRCUIT WAS FUNCTION TESTED. 2G72 4U 1H15 20030528000382003052800038EU 2003 5 28 HEEA086592 120030516A6240222375021113 INDICATOR BOLKMS117 BK117A1 5626010EU TRIPLE TACH MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03230H 7136 NR 2 NEEDLE DROPS TO ZERO WHEN INDICATOR IS TAPERED. SENT TO BELL FOR WARRANTY REPAIR. REFERENCE: 1G72 3U H13EU 20030528000492003052800049EU 2003 5 28 BAQA086408 120030514A7330L284M30C1003 SENSOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE FUEL INDICATION MALFUNCTIONED E BAQAO OTHER N FALSE WARNING NRNOT REPORTED 1 FS01575ME1093 0157 SENSOR PRODUCING A FUEL DEGRADE LIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H88EU E34NE 20030528000502003052800050EU 2003 5 28 BAQA086412 120030514A6240L771M40C1005 INDICATOR UROCOPEC135 EC135P1 8680990EU TRIPLE TACH INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01137MH111 0179 TRIPLE TACH HAS INTERMITTENT ROTARY RPM. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030528000602003052800060 2003 5 28 HEEA086596 420030521A34251113025 INDICATOR BELL 412 412 1182202SW HSI MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 COPILOT HSI COURSE HEADING KNOB BINDING. 1G72 4U H4SW 20030528000662003052800066NE 2003 5 28 AC2A086459 220030509A723023065591 IMPELLER BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE NR 1 ENGINE BROKEN E AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CM4240 CAC44298 49090 CORNER OF IMPELLER BLADE IS BROKEN OFF. BROKEN AREA MEARURES 1/4 X 1/2 INCH. BROKE IMPELLER PIECE WAS FOUND IN THE TURBINE. REMOVED ENGINE FROM AIRCRAFT AND REPLACED IMPELLER. 1G72 3U3 URTH9SW E1GL 20030528000682003052800068NE 2003 5 28 AC2A086461 120030511A2435M20021 BRUSHES SKRSKYS76 S76A 8143006NE STARTER GEN CHIPPED E AC2AO OTHER O OTHER NRNOT REPORTED 1 FS017266K528 5569 760283 BRUSHES ARE CHIPPED. THE TRAILING EDGE OF THE BRUSHES HAVE BEEN BREAKING OFF. THE LEAD WIRE THAT IS RIVITED AND SOLDERED COMES LOOSE POSSIBLY DUE TO OVERHEATING. REPLACED BRUSHES. 1G72 3U H1NE 20030528000822003052800082 2003 5 28 C7WA200200041 420030314A2210G4103 CONTROL PANEL BOEING727 7272J7 138400ENM PEDESTAL SHORTED A C7WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO17128NA 20879 WHEN ENGAGING AUTOPILOT, CRUISE STABILIZER TRIMS TO THE FULL NOSE DOWN POSITION. WITH AUTOPILOT DISCONNECTED, AFTER LEVEL OFF AT FL350, AN ELECTRICAL OVERHEAT ODOR STARTED TO FILL THE COCKPIT. CHECKLIST PERFORMED, ODOR STOPPED. REMOVED AND REPLACED RIGHT ELEVATOR POSITION SENSOR PER MM 22-11-71. OPS CHECK GOOD PER MM 22-11-0, P/N 2588838. FOR OVERHEAT ODOR FOUND CENTER PEDESTAL LIGHTS POPS CIRCUIT BREAKER. REMOVED AND REPLACED NR 1 AUDION NAV/COMM CONTROL PANEL PER M/M 33-11-0 AND 23-21-0. OPS CHECK GOOD, P/N INSTLALED G1982B. (M) 2L73 4F A3WE 20030528000982003052800098SW 2003 5 28 HEEA086607 120030521A6420212011701101FM1 BEARING BELL 412 412 1182202SW TAIL ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03330088262 36004 WORN FEATHERING BEARINGS. REPLACED 4 EACH BEARINGS 205-012-710-001 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030529000062003052900006EU 2003 5 29 AALA20030400 120030402A3350 WIRE AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114061 471 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 9G INOPERATIVE. SECURED EMERGENCY EXIT LIGHT WIRE CONNECTOR AT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030529000092003052900009EU 2003 5 29 2003F00326 120030304A5220SD3110853XU DOOR STBROSSD3 SD330 8100602EU EMERGENCY EXIT DAMAGED A DATAK NONE O OTHER ININSP/MAINT 1 GL13390GA SH3077 DURING THE BEFORE START CHECKLIST, THE MAIN CARGO DOOR MI INDICATED CROSSHATCHED. THE FLIGHT CREW STOPPED THE CHECKLIST AND THE FIRST OFFICER OPENED AND CLOSED THE MAIN CARGO DOOR. THE ALL 7 DOORS MI'S INDICATED SHUT. THE FLIGHT CREW CONTINUED THE CHECKLIST. ALL 7 DOORS MI'S INDICATED SHUT DURING TAKEOFF AND THE FLIGHT. THE FORWARD LEFT EMERGENCY EXIT DOOR INADVERTANTLY OPENED DURING LANDING AT ALBANY, NY. THE FLIGHT CREW EXPERIENCED NO UNUSUAL FLIGHT CHARACTERISTICS AT ALL. THE DIRECTOR OF MAINTENANCE HAD A MAIN DOOR, PART NUMBER SD3-11-2255 AND A LEFT EMERGENCY DOOR ASSEMBLY, PART NR SD3-11-053XU SENT TO ALBANY, NY TO REPLACE THE DAMAGED DOORS. (M) 2H72 4T A41EU 20030523000722003052300072NM 2003 5 23 CALA0300242 120030424A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717306 23357 MAINTENANCE DISCOVERED A SMALL TRIM-OUT IN THE INNER SKIN OF THE FORWARD CARGO DOOR AT A LIGHTENING HOLE. THE DAMAGED AREA WAS REPAIRED IAW ECRA 5232-01026. 2L72 4F RTA16WE 20030523000782003052300078NM 2003 5 23 SWAA031106 120030514A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030523001222003052300122NM 2003 5 23 2003UALA00430 120030421A575465C26602301 WEDGE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 2 SLAT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 HAIL DAMAGE OCCURRED TO T/E WEDGE, NR 2 SLAT. REPAIRED T/E WEDGE, SLAT NR 2. 2L72 4F4 FRTA16WE E2GL 20030528000312003052800031SW 2003 5 28 ERAA086441 120030425A6230412010402111FM BEARING BELL 412 412 1182202SW SWASHPLATE WORN E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01421EH13678 33067 SWASHPLATE HAS WORN GIMBAL RING BEARINGS. NEARING O/H, GIMBAL BEARING WORN, BEARING COVER SCRAP. 2 SUPPORT BUSHINGS WORN, SWASHPLATE BEARING WORN. ACTION TAKEN: COMPLETELY DISASSEMBLED FOR OVERHAUL. COMPLIED WITH VISUAL & NDT INSEPCTIONS. REPLACED GIMBAL BOLTS BEARINGS, COVER, 2 SUPPORT BUSHINGS & SWASHPLATE BEARING. SENT PARTS OUT FOR PRIMER & PAINT. RE-TORQUE OUTER RING BOLTS IAW TB 412-84-40. REASSEMBLED NEW SEALS & HARDWARE. PURGE , LUBED BEARINGS. 1G72 4U H4SW 20030528000422003052800042EU 2003 5 28 BAQA086397 120030512A6240430106202 PICKUP BOLKMS117 BK117A1 5626010EU ROTOR SPEED MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME 7243 PICKUP CAUSING ERRATIC READINGS AND ENGINE LOW LIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030528000552003052800055SW 2003 5 28 HEEA086741 120030522A2810FT17521E FUEL CELL BOLKMS105 BO105CB* SW FUSELAGE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 FUEL CELL LEAKING. TO BE SENT TO VENDOR. 1G72 4U H3EU 20030528000772003052800077WP 2003 5 28 AALA20030430 120030409A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21413AA 49324 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 1721 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030528000832003052800083SW 2003 5 28 HEEA086597 120030521A6710204001045009 BUSHING BELL 212 212 1181420SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736J 31140 GUIDE BUSHINGS WORN. REPLACED 2 EACH 204-001-036-001 GUIDES DUE TO WORN AND BEARING MS27643-4 DUE TO WORN. REPAIRED. 1G71 4U H4SW 20030528001092003052800109SW 2003 5 28 HEEA086618 120030521A6320214040013115FM GEARBOX BELL 214 214ST 1182106SW MAIN ROTOR MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M1416 28102 GEARBOX MAKING METAL. REPAIRED. 2G72 4U H10SW 20030528001112003052800111SW 2003 5 28 HEEA086620 120030521A243230126002 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030523001152003052300115NM 2003 5 23 2003UALA00423 120030509A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29648UA 25285 EMERGENCY EXIT LIGHT FWD UPPER CORNER OF DOOR 2R AND 2L INOP. REPLACED BATTERY CHARGER AND BATTERY PACK ASSEMBLY. 2L72 4F4 FRTA1NM E24NE 20030527000032003052700003WP 2003 5 27 DHL2003604522 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBOARD L/E FORMER AT STA XFS 672.500 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030528000712003052800071WP 2003 5 28 AALA20030440 120030410A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPAIR EMERGENCY EXIT LIGHT WIRE SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030529000032003052900003NM 2003 5 29 AALA20030420 120030403A5312 PRESSURE PANEL BOEING757 757223 1384957NM MLG WW CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21621AM 24579 IN THE LT MAIN LANDING GEAR WHEEL WELL, INBOARD WALL BETWEEN STATION 1100 AND 1120 THERE IS AN AREA OF CORROSION. BLENDED CORROSION PER SRM 53-40-12-1. ALODINED AND PRIMED AND PAINTED. (M) 2L72 4F RTA2NM 20030529000122003052900012NM 2003 5 29 AMTA200300576 120030429A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 RED EGRESS LIGHT INOPERATIVE AT 29D. RECONNECTED LOOSE WIRE TO LAMP ASSEMBLY. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030529000172003052900017EU 2003 5 29 AALA20030379 120030328A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211466A 11498 DURING OVERNIGHT MAINTENANCE, FORWARD OF SEAT ROW 8 EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT TRACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030529000202003052900020SW 2003 5 29 ALGA086489 120030522A6220406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR DEFECTIVE H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01457AL609 53151 UNIVERSAL STICKING, RATCHETY AND WORN. REPLACED WITH A SERVICABLE PART. 1G71 3U O H2SW 20030529000252003052900025SW 2003 5 29 HEEA086623 120030521A243230703001 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0333008 36004 BATTERY WON'T HOLD CHARGE. REPAIRED. 1G72 4U H4SW 20030527000242003052700024NM 2003 5 27 DL733030317 120030330A5330654577572 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 THE FUSELAGE SKIN WAS FOUND DENTED AND CRACKED AT THE LOWER FWD CORNER OF THE C2 DOOR OPENING. THE DAMAGE WAS REMOVED WITH A 1.5 X 1 INCH CUTOUT TO THE CORNER THROUGH THE BONDED SKIN ASSY AND UNDERLYING BEAR STRAP. THE CORNER WAS REPAIRED WITH MULTIPLE ALUMINUM REPAIR DOUBLERS PER ER/A 384702-14. 2L72 4F RTA16WE 20030527000312003052700031NM 2003 5 27 DLM88030325 120030402A2120 ODOR DOUG MD88 MD88 3023688NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27963DL 49982 PASSENGERS AND CREW REPORT BURNING ODOR IN CABIN AROUND ROW 22A/B/C SHORTLY AFTER T/O ATL. ODOR DISSIPATED QUICKLY. PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20030527000632003052700063WP 2003 5 27 AALA20030410 120030404A3397 CONTACTOR DOUG DC9 DC982 3022082WP EMERGENCY BATTERINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217533A 49987 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONTACTS ON EMEGENCY EXIT LIGHT BATTERY CHARGER POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527000932003052700093NM 2003 5 27 AMTA200300600 120030502A26124739551 MODULE BOEING737 73783N 13844HINM COCKPIT INOPERATIVE A AMTAO OTHER N FALSE WARNING DEDESCENT 1 GL11302TZ 32576 FORWARD CARGO FIRE WARNING LIGHT ILLUMINATED INFLIGHT WITHOUT A MASTER FIRE WARNING LIGHT OR FIRE WARNING BELL. ACCESSED CARGO PIT, NO EVIDENCE OF SMOKE, BAGGAGE CHECK AS UNLOADED NOTHING FOUND. BITE TEST CEU PER 26-16-00-810-801. NO FAULTS NOTED. REMOVED AND REPLACED CARGO FIRE CONTROL PANEL PER 26-00-02-4 OF BOEING AMM. OPS CHECK GOOD PER AMM 26-16-00-5. (M) 2L72 4F RTA16WE 20030527000952003052700095EA 2003 5 27 2003F00305 120030219A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A MASAO OTHER J WARNING INDICATION CLCLIMB 1 SW0777195 7195 MOMENTARY GEAR DISAGREE MESSAGE ON TAKEOFF, THEN MESSAGE REAPPEARED AFTER GEAR EXTENDED FOR LANDING AT DESTINATION. MAINTENANCE REPLACED THE PRIORITY VALVE. AIRCRAFT BACK IN SERVICE. (M) 2L72 4F RTA21EA 20030527001172003052700117 2003 5 27 MEX2003148 420030428A34426225135001 TRANSMITTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE RADAR SYS FAILED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW23803ML 49726 AIRCRAFT AIR TURNBACK DUE TO RADAR FAIL. TX RADAR WAS REPLACED IAW MM, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20030528000292003052800029NE 2003 5 28 BAQA086426 220030516A7320430121106 FUEL CONTROL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ENGINE MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01967LS56 7067 ENGINE STARTS HOT. REMOVED FROM ENG NR: REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030528000812003052800081NM 2003 5 28 BJNA03042 120030422A33501000679 LIGHT BOEING737 737282 13844ATNM CABIN INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 DURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT OVER THE R-2 DOOR WOULD NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, SYSTEM CHECKS NORMALLY. (M) 2L72 4F RTA16WE 20030528000902003052800090SW 2003 5 28 AC2A086463 120030515A7830206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE CRACKED E AC2AK NONE O OTHER ININSP/MAINT 1 FS0117237807 51478 EXHAUST STACK IS CRACKED AT REAR WELD SEAM. REPLACED EXHAUST ASSY. 1G71 3U3 U H2SW E1GL 20030528000962003052800096SW 2003 5 28 HEEA086605 120030521A2612209075395001 FIRE LOOP BELL 412 412 1182202SW NR 2 ENGINE FAILED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW032014K 33020 NR 2 ENGINE FIRE HARNESS CONTROL UNIT INTERMITTENTLY WON'T TEST OR LIGHT DELAYS. 1G72 4U H4SW 20030528001102003052800110SW 2003 5 28 HEEA086619 120030521A6510 SEAL BELL 214 214ST 1182106SW HANGER ASSY LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0359806 A427 28140 HANGER ASSY SEAL LEAKS. REPLACED INNER COUPLING 214-040-603-005, S/N A293 DUE TO CORROSION AND WORN SEAL RIDE AREA. REPAIRED. 2G72 4U H10SW 20030529000132003052900013CE 2003 5 29 2003F00329 120030330A2910NAS161216 PACKING CESSNA500 560CESSNA 2076750CE HYD POWERPACK LEAKING A IMJAO OTHER O OTHER TXTAXI/GRND HDL 1 EA2515SK 5600395 ON TAXI OUT, PILOTS AND CO-PILOTS BRAKES FAILED. FOUND HYDRAULIC FLUID LEAK AT THE HYDRAULIC POWER PACK FILTER BOWL. (M) 2L72 4F RTA22CE 20030617000732003061700073EA 2003 6 17 QXEA200300670 120030517A5420 PAINT CNDAIRCL600 CL6002C10 1390015EA NR 1 NACELLE DETERIORATED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - NR 1 NACELLE LOWER FORWARD CORE COWL ALUMINIZED PAINT IS MISSING AND DETERIORATED FROM VARIOUS LOCATIONS. PAINTED AS REQUIRED IAW CRJ 700 SRM 51-25-01, FIGURE 1-13 QX4. 2L72 4F RTA21EA 20030617000822003061700082EA 2003 6 17 QXEA200300663 120030531A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX- CENTER FIRE PROTECTION CHIMNEY IN THE FORWARD CARGO BAY IS DAMAGED. REMOVED AND REPLACED CENTER CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030617001002003061700100 2003 6 17 ERAA087092 420030519A344240005040301 DRIVE SYSTEM SKRSKYS61 S61N 8142104NE GE CT58 CT58* 30011GL WX RADAR SYS DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01561EH 61471 UNIT MAKING GROWLING NOISE AND STICKING. WATER DAMAGE. REPLACED WATER DAMAGED MOTOR, REMOVED CORROSION, ALIGNED AND TESTED. COMPLIED WITH SERVICE LETTER SL-T-03-001. 2G72 4U4 U 1H15 1E3 20030617001142003061700114SW 2003 6 17 HEEA087294 120030611A6220407010100115 BEARING BELL 407 407 1182206SW ALLSN 250C 250C20 03013GL M/R HUB ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH2958 53147 WORN DAMPER BEARING. REPAIRED. 1G71 3U3 UO H2SW E4CE 20030617002972003061700297SW 2003 6 17 HEEA087037 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030617003032003061700303 2003 6 17 SWAA031259 420030606A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29427WN 29831 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030617003132003061700313EU 2003 6 17 BAQA083524 120030117A31507008138903 COMPUTER BOLKMS117 BK117A1 5626010EU COCKPIT MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME2681 7243 "TRIM" CAUTION LIGHT ON IN FLIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030617003292003061700329SW 2003 6 17 HEEA087040 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH1190 53199 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030618000022003061800002SW 2003 6 18 HEEA087327 120030611A6510 BEARING BELL 407 407 1182206SW T/R DRIVESHAFT VIBRATION E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH3767 A624 53147 HIGH FREQ VIBRATION. BEARING ROUGH. REPLACED BEARING 407040339101, S/N ZV12038 DUE TO ROUGH. REPAIRED. 1G71 3U O H2SW 20030618000352003061800035 2003 6 18 SWAA031304 420030611A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030618000632003061800063 2003 6 18 HEEA087125 420030610A3451066107800 RECEIVER SKRSKYS76 S76A 8143006NE DME ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 DME OUTPUT IS ERRATIC. SHOP REPAIR. 1G72 3U H1NE 20030618000772003061800077 2003 6 18 SWAA031312 420030611A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030618000892003061800089NM 2003 6 18 SWAA031302 120030610A33506128251 CHARGER BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOORS LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER BASE PER MM. 2L72 4F RTA16WE 20030618000992003061800099 2003 6 18 SWAA031284 420030607A2565D313591 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED SPECIAL VISIT, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030618001052003061800105 2003 6 18 HEEA087494 420030612A2561PHI10090 LIFE VEST BELL 407 407 1182206SW CABIN LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 LIFE VEST LEAKING. REPLACED. 1G71 3U O H2SW 20030618001372003061800137EA 2003 6 18 COMA0360263 120030610A3230 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01807CA 7364 FLIGHT 5581 GEAR DISAGREE WARNING DURING EXTENSION. COULD NOT DUPLICATE PROBLEM. CLEAN AND LUBED NLG AND ADJUSTED NLG UPLOCK HOOK TO NEW T/R M/M SPECIFICATIONS. 2L72 4F RTA21EA 20030618001422003061800142EA 2003 6 18 COMA0360266 120030610A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA A/C BAY MALFUNCTIONED A COMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01981CA20428 7163 FLIGHT 5816 LT A/C PACK STUCK IN FULL HOT, BURNING SMELL AND LOUD SQUEALING NOISE. REPLACED THE LT ACM. 2L72 4F RTA21EA 20030618001572003061800157 2003 6 18 COMA0360278 420030614A34426229302003 RADAR CNDAIRCL600 CL6002B19 1900309EA E/E BAY INOPERATIVE A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01986CA138801 7174 FLIGHT 5359 WEATHER RADAR IS INOPERABLE IN-FLIGHT. REPLACED THE WEATHER RADAR. 2L72 4F RTA21EA 20030529000432003052900043SW 2003 5 29 HEEA086634 120030521A6230 BEARING BELL 412 412 1182202SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 MAIN ROTOR LINK HAS WORN BEARINGS. REPLACED 4 EACH BEARINGS 412-310-400-107 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030529000532003052900053NE 2003 5 29 HEEA086508 120030521A32462070A900 WHEEL SKRSKYS76 S76A 8143006NE NLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03223421352 760096 NOSE WHEEL ASSY WORN. REPLACED BEARING CONE P/N 1780 DUE TO MECH DAMAGE. REPAIRED. 1G72 3U H1NE 20030529000882003052900088NE 2003 5 29 HEEA086521 120030521A62107615009100053 BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X7112 760050 THE C BLOCK HAS EXCESSIVE CORROSION AROUND THE ATTACHMENT BOLT. THE SKIN ON THE LOWER SIDE NEAR STA. 44 HAS SOME SEPERATION OVER THE SPAR. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030530000022003053000002 2003 5 30 HEEA086664 420030522A3452066011430201 TRANSPONDER BELL 230 230 1182149SW ATC INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RC 23037 ATC TRANSPONDER FOUND FAULTY. INTERMITTENT OPERTION. CONTROL HEAD WILL DISPLAY "FAIL". IN SHOP REPAIR. 1G72 3U NCH9SW 20030530000062003053000006SW 2003 5 30 HEEA086668 120030522A5230205032809035 PANEL BELL 412 412 1182202SW CARGO DOOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 CARGO DOOR HAS SEPERATION IN UPPER AFT CORNER OF PANEL. IN REPAIR. 1G72 4U H4SW 20030530000122003053000012 2003 5 30 HEEA086528 420030521A2300N0010001 CONTROL UNIT SKRSKYS76 S76A 8143006NE COMMS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 FAILS TO REPORT. SENT TO OUTERLINK FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030530000132003053000013NE 2003 5 30 HEEA086529 120030521A6220SS40CT28A140180 HOSE SKRSKYS76 S76C 8143008NE M/R DAMPER CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 MAIN ROTOR DAMPER HOSE CHAFED. SCRAPPED. 1G72 3U NCH1NE 20030530000182003053000018NE 2003 5 30 HEEA086534 120030522A78100401287410 EXHAUST STACK SKRSKYS76 S76C 8143008NE ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 LT EXAHAUST HAS CRACKS. 1G72 3U NCH1NE 20030530000232003053000023SW 2003 5 30 HEEA086677 120030522A7600212061101001 BEARING BELL 412 412 1182202SW ENGINE CONTROLS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 ENGINE CONTROLS HAVE WORN BEARING. SCRAPPED. 1G72 4U H4SW 20030530000292003053000029 2003 5 30 HEEA086536 420030522A2312064100900 TRANSCEIVER KTR905 SKRSKYS76 S76A 8143006NE COCKPIT VHF WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 VHF TRANSCEIVER WEAK. IN SHOP REPAIR. 1G72 3U H1NE 20030530000312003053000031 2003 5 30 HEEA086537 420030522A2312064102302 TRANSCEIVER KTR908 SKRSKYS76 S76A 8143006NE VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 VHF TRANSCEIVER INOPERATIVE. IN SHOP REPAIR. 1G72 3U H1NE 20030530000422003053000042SW 2003 5 30 HEEA086687 120030522A6220412010182101 BEARING BELL 412 412 1182202SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214982278 36003 MAIN ROTOR GEARBOX HAS BEARING WEAR. SCRAPPED. 1G72 4U H4SW 20030530000462003053000046SW 2003 5 30 HEEA086691 120030522A6230 BEARING BELL 412 412 1182202SW M/R LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214983817 A2045 36003 MAIN ROTOR LINK HAS BEARING WEAR. REPAIRED. 1G72 4U H4SW 20030530000612003053000061NM 2003 5 30 AMTA200300575 120030429A3320100477112 LIGHT LKHEED1011 1011 N/A-SDRNM LAVATORY OVERHEATED A AMTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL11195AT 193C1041 BURNED ELECTRICAL ODOR EMINATING FROM RIGHT FORWARD LAVATORY. FOUND X-FORMER ON OVERHEAD LIGHT ASSEMBLY OVERHEATED. REMOVED AND REPLACED RIGHT FORWARD LAVATORY OVERHEAD LIGHT ASSEMBLY PER MM 33-27-01. OPS CHECK NORMAL. (M) 2L73 4F RTA23WE 20030617001712003061700171NM 2003 6 17 QXEA200300719 120030605A542085414131101 DIAPHRAGM BOMBDRDHC8 DHC8401 1390041NM NR 2 NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - DIAPHRAGM ON NR 1 NACELLE FAIRING IS CRACKED ON LOWER FLANGE. REPAIRED IAW Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030617001802003061700180NM 2003 6 17 QXEA200300587 120030508A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - SHIMS BETWEEN FORWARD RIGHT HAND H-STAB TO V-STAB ATTACH POINTS HAVE COMPLETELY EXTRUDED. REPAIRED IAW HORIZON AIR EA 6-55-31. 2H72 4T RTA13NM 20030617001862003061700186NM 2003 6 17 QXEA200300596 120030502A5320 FLANGE BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - 261FT HAS CHAFED FLANGE. REPAIRED IAW Q400 AMM 51-25-31-370-801 AND RD 8/4-53-521, PAGE 5. 2H72 4T RTA13NM 20030617001872003061700187NM 2003 6 17 QXEA200300597 120030502A5320 FLANGE BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - 261HT HAS CHAFED FLANGE. REPAIRED IAW Q400 AMM 51-25-31-370-801 AND RD 8/4-53-521. 2H72 4T RTA13NM 20030617002892003061700289SW 2003 6 17 HEEA087322 120030611A2510407030211101 COVER BELL 407 407 1182206SW COLLECTIVE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 COLLECTIVE COVER CRACKED. REPLACED. 1G71 3U O H2SW 20030617002942003061700294WP 2003 6 17 GTIA030349 120030514A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FLOORBOARD STATION 1056-1136 LBL 44-54 CRACKED AND DELAMINATED IN SEVERAL AREAS. REPAIRED FLOORBOARD. (M) 2L72 4F A6WE 20030617002992003061700299WP 2003 6 17 GTIA030365 120030503A5720 SUPPORT DOUG DC9 DC982 3022082WP RT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND RIGHT WING LEADING EDGE STATION XFS 624 CRACKED AND BENT, SUPPORT. REMOVED SUPPORT. LOCATED AND DRILLED NEW SUPPORT. INSTALLED THE NEW SUPPORT. (M) 2L72 4F A6WE 20030618000132003061800013SW 2003 6 18 HEEA087046 120030604A6320406340100101 PUMP BELL 407 407 1182206SW XMSN OIL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 TRANSMISSION OIL PUMP HAS SPLINE WEAR. 1G71 3U O H2SW 20030618000282003061800028NM 2003 6 18 SWAA031322 120030613A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED JUST OF BS 440, ABOVE STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030618000612003061800061NM 2003 6 18 SWAA031306 120030610A3350604222 BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C3 CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030618000822003061800082NM 2003 6 18 SWAA031298 120030610A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030618000842003061800084SW 2003 6 18 HEEA087344 120030611A6510 SHAFT BELL 407 407 1182206SW FLYWHEEL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 TAIL ROTOR FLYWHEEL SHAFT HAS WORN SPLINES. 1G71 3U O H2SW 20030618001432003061800143EA 2003 6 18 COMA0360267 120030610A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01999CA 7230 FLIGHT 5498 FLAPS FAILED AT 27 DEGREES. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030618001712003061800171SW 2003 6 18 HEEA087364 120030611A5210407070620137 PANEL BELL 407 407 1182206SW CREW DOOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 CREW DOOR PANEL BROKEN. 1G71 3U O H2SW 20030618001912003061800191SW 2003 6 18 HEEA087157 120030609A6220206011117003 RESTRAINT BELL 206 206L1 1182107SW M/R HEAD STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0327766 45312 FLAP RESTRAINT STICKING. REPAIRED. 1G71 3U H2SW 20030619000112003061900011 2003 6 19 AC2A086760 420030521A3425430375002109 DISPLAY BELL 430 430 1182150SW COCKPIT MALFUNCTIONED E AC2AO OTHER O OTHER CRCRUISE 1 SO07430CM1339 49090 FOUND CIRCUIT BREAKER POPPED FOR EFIS UNIT. WOULD NOT RESET. REPLACED EFIS UNIT WITH NEW. 1G72 3U RTH9SW 20030619000132003061900013SW 2003 6 19 AC2A086763 120030524A2910222380020001 MODULE BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE NR 1 HYD SYS GALLED H AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CT1397 49089 HYDRAULIC MODULE FILTER HOUSING THREADS GALLED ON THE RETURN SIDE. REPLACED HYDRAULIC MODULE ASSEMBLY. 1G72 3U3 URTH9SW E1GL 20030619000252003061900025SW 2003 6 19 HEEA087374 120030611A2510407070620155 PANEL BELL 407 407 1182206SW SEAT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 SEAT PANEL CRACKED. 1G71 3U O H2SW 20030619000452003061900045 2003 6 19 HEEA087195 420030609A34424000038001 CONTROL UNIT BELL 206 206L3 1182108SW WX RADAR SYS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 LOOSE KNOB. FOUND SELECTOR KNOB CRACKED AND VOLUME CONTROL BAD. REPLACED SELECTOR KNOB AND VOLUME CONTROL. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030619000482003061900048 2003 6 19 HEEA087198 420030609A2561501819409 SEAT BELT BELL 206 206L3 1182108SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 LAP SEAT BELT WORN. SENT TO AIRCRAFT BELTS FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20030619000612003061900061SW 2003 6 19 HEEA087402 120030611A6510407340339101 BEARING BELL 407 407 1182206SW TAIL ROTOR ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 TAIL ROTOR DRIVE BEARING ROUGH. 1G71 3U O H2SW 20030619000702003061900070SW 2003 6 19 HEEA087215 120030609A6720PHI206L3957 BEARING BELL 206 206L3 1182108SW PITCH CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 WORN BEARING ON TOP LEVER. REPAIRED. 1G71 3U H2SW 20030619000722003061900072SW 2003 6 19 HEEA087406 120030611A6510407340339101 BEARING BELL 407 407 1182206SW T/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 BEARING HAS EXCESSIVE AMOUNT OF AXIAL PLAY. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030619000802003061900080SW 2003 6 19 HEEA087415 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TAIL ROTOR DISC PACK PITTING AND FRETTING CORROSION BEYOND LIMITS. 1G71 3U O H2SW 20030619000852003061900085SW 2003 6 19 HEEA087220 120030609A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D23 51106 MAIN BATTERY DEAD. 1G71 3U H2SW 20030619000962003061900096SW 2003 6 19 HEEA087420 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030620000042003062000004SW 2003 6 20 HEEA087230 120030610A6220206011100105 ROTOR HEAD BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW036251X6693 51552 MAIN ROTOR HEAD SLINGING GREASE. SHOP REPAIR. 1G71 3U H2SW 20030620000072003062000007SW 2003 6 20 HEEA086934 120030603A6420206011728001 TRUNNION BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH 53278 TAIL ROTOR TRUNNION HAS EXCESSIVE WEAR ON BEARING SPINDLES. TO BE SENT TO MFG. 1G71 3U O H2SW 20030620000092003062000009SW 2003 6 20 HEEA086936 120030603A5302206020113255A STRUCTURE BELL 407 407 1182206SW TAILBOOM FIN CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 TAIL BOOM HAS CORROSION ON FIN ASSY. REPAIRED. 1G71 3U O H2SW 20030620000182003062000018 2003 6 20 HEEA087237 420030610A34424000023 TRANSCEIVER BELL 206 206L3 1182108SW WX RADAR SYS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 WEATHER RADAR SYS INTERMITTENT. SHOP REPAIR. 1G71 3U H2SW 20030620000232003062000023SW 2003 6 20 HEEA086945 120030603A3212206050247135 COVER BELL 407 407 1182206SW FLOAT ASSY TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 FLOAT COVER ASSY TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030620000262003062000026SW 2003 6 20 HEEA086948 120030603A3212206050247138 COVER BELL 407 407 1182206SW FLOAT ASSY TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 FLOAT COVER ASSY TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030529000292003052900029SW 2003 5 29 HEEA086627 120030521A6210412010216105 BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03415A 814 36257 MAIN ROTOR HEAD HAVE PLAY IN BEARING. REPAIRED. 1G72 4U H4SW 20030529000342003052900034SW 2003 5 29 HEEA086631 120030521A6220 BEARING BELL 412 412 1182202SW PENDULUM ASSY. WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03415A 814 A4192 36257 MAIN ROTOR PENDULUM ASSY HAS PLAY IN BEARING. REPAIRED. 1G72 4U H4SW 20030529000402003052900040NE 2003 5 29 HEEA086505 220030521A73140292958050 VALVE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1A1 60030NE FUEL SYSTEM ODOR E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 FUEL ODOR IN COCKPIT DURING START. 1G72 3U3 UNCH1NE E19EU 20030529000452003052900045SW 2003 5 29 HEEA086636 120030521A6230412010408101 BUSHING BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03415A 814 36257 BUSHING HAS WORN TEFLON. REPLACED BUSHING 412010420101 DUE TO TEFLON WORN. REPAIRED. 1G72 4U H4SW 20030529000602003052900060SW 2003 5 29 HEEA086647 120030521A2841412375001105 INDICATOR BELL 412 412 1182202SW FUEL QTY FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 FUEL QUANTITY INDICATOR FLUCTUATES. 1G72 4U H4SW 20030529000872003052900087SW 2003 5 29 HEEA086661 120030521A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T344 28101 BATTERY HAS WEAK VOLTAGE. 2G72 4U H10SW 20030529000922003052900092 2003 5 29 HEEA086524 420030521A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS CHATTERING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 AFCS ACTUATOR CHATTERS CONTINUOUSLY WITH CHANNEL ON. INSPECTED BY ACCESSORY SHOP AND FOUND UNIT TO CHATTER WHEN TESTED AND POTENTIOMETERS OUT ON STRIP CHART. SENT TO HELICOPTER SUPPORT, INC. FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030530000042003053000004 2003 5 30 HEEA086666 420030522A34161003511424 ALTIMETER BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ALTIMETER LAGGING. IN SHOP REPAIR. 1G72 4U H4SW 20030530000052003053000005SW 2003 5 30 HEEA086667 120030522A6320 SEAL BELL 412 412 1182202SW QUILL LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0321498 A1763 36003 MAIN ROTOR QUILL ASSY SEAL LEAKS. IN REPAIR. 1G72 4U H4SW 20030530000102003053000010 2003 5 30 HEEA086527 420030521A2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 CAUSING STATIC IN PILOTS HEADSET. FOUND UNIT TO HAVE VERY WEAK AND NOISY TRANSMIT AUDIO. CLEANED S1 SWITCH. REPLACED C30 AND C31 CAPACITORS. REPLACED Q8 AND Q10 TRANSISTORS. STRAIGHTENED BENT TERMINAL ON S1 TRANSMIT SELECTOR SWITCH AND RESOLDERED WIRE TO TERMINAL. REPAIRED. BENCH CHECK GOOD. 1G72 3U H1NE 20030530000282003053000028EU 2003 5 30 HEEA086726 120030522A291010545028 POWERPACK BOLKMS105 BO105S 5626006EU HYD SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 FAILED 12 MONTH INSPECTION. PRESSURE RELIEF VALVE CHECK OF NR 2 VALVE BODY MANIFOLD (STUCK IN BYPASS AND COULD NOT GET IT TO UNSTICK) IN SHOP REPAIR. 1G72 3U H3EU 20030530000402003053000040NE 2003 5 30 HEEA086685 220030522A74124040T18P02 EXCITER BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N 28106 EXCITER PRODUCES SLOW LIGHT OFF. REPLACED. 2G72 4U4 U H10SW E8NE 20030530000412003053000041SW 2003 5 30 HEEA086686 120030522A79214068T96P01 PRESSURE SWITCH BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 2 ENGINE MALFUNCTIONED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0359806 28140 NR 2 ENGINE BLOWER LIGHT CAME ON AFTER ENGINE START. REPLACED. 2G72 4U4 U H10SW E8NE 20030530000432003053000043SW 2003 5 30 HEEA086688 120030522A6220412010182101 BEARING BELL 412 412 1182202SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214981809 36003 MAIN ROTOR GEARBOX HAS BEARING WEAR. SCRAPPED. 1G72 4U H4SW 20030617001652003061700165NM 2003 6 17 QXEA200300717 120030601A5512 SKIN BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FRONT SPAR AND F605D-75.20. REPAIRED IAW Q400 WRM 51-21-10, PAGES 204-205 AND SRM 51-25-10, PAGES 201-205. 2H72 4T RTA13NM 20030620000492003062000049SO 2003 6 20 ASOA03226 120030520A3397M22759209 WIRE EMB 120 EMB120RT 3260202SO EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11258AS 120131 FLT 4939 - DURING A GROUND INSPECTION IN DFW, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE DEFECTIVE WIRE SPLICE ON THE RIGHT AFT EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030617003102003061700310NM 2003 6 17 SWAA031266 120030605A3397BR2013 WIRE BOEING737 7377H4 1384404NM CABIN DISCONNECTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29738CB 27870 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW NR 1. RECONNECTED EEPLS WIRES PER MM. 2L72 4F RTA16WE 20030617003212003061700321NM 2003 6 17 SWAA031272 120030607A256010C801 DOOR LATCH BOEING737 7373H4 1384600NM COCKPIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 FO'S ESCAPE ROPE DOOR LATCH INOP. REMOVED AND REPLACED DOOR LATCH ASSY PER MM. 2L72 4F RTA16WE 20030618000012003061800001SW 2003 6 18 HEEA087326 120030611A6510407040302101 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 WORN BEARING MOUNT SURFACE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030618000942003061800094NM 2003 6 18 SWAA031279 120030607A3350D71701100 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29717SA 27851 DURING SCHEDULED PM CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER MM. 2L72 4F RTA16WE 20030618001082003061800108SW 2003 6 18 HEEA087496 120030612A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 BLOWER ASSY FWD BEARING ROUGH. REPLACED. 1G71 3U O H2SW 20030618001962003061800196SW 2003 6 18 HEEA087162 120030609A3212206030104023 FITTING BELL 206 206L3 1182108SW EMERGENCY FLOAT CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 EMERGENCY FLOAT FITTING IS CHAFED. SCRAPPED. 1G71 3U H2SW 20030619000202003061900020SW 2003 6 19 HEEA087183 120030609A2910206076665101 LINE BELL 206 206L3 1182108SW HYD SYSTEM CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03979BH 51403 HYD RESERVOIR RETURN LINE CHAFED. SCRAPPED. 1G71 3U H2SW 20030619000402003061900040SW 2003 6 19 HEEA087385 120030611A3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 153 53188 LEAKING AT INTERCONNECT FITTING. 1G71 3U O H2SW 20030619000912003061900091SW 2003 6 19 HEEA086931 120030603A6420206011728001 TRUNNION BELL 407 407 1182206SW ALLSN 250C 250C20 03013GL TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 TAIL ROTOR TRUNNION SPINDLES ARE WORN. TO BE SENT TO MFG. 1G71 3U3 UO H2SW E4CE 20030620000122003062000012SW 2003 6 20 HEEA086939 120030603A3212206050247131 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 FLOAT COVER TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030620000632003062000063NM 2003 6 20 USAA030079 120030522A5540 ANGLE BOEING737 737301 1384611NM RUDDER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND RUDDER CRACKED .5 INCH, RUDDER LOWER FORWARD SEAL PLATE ANGLE. INSTALLED WET LAYUP REPAIR PER EA 76293, SRM 51-70-17 AND 51-60-00. (M) 2L72 4F RTA16WE 20030620000672003062000067WP 2003 6 20 MEX2003197 120030531A26136712152180 SWITCH DOUG DC9 DC987 3022087WP TAIL OVERHEAT FAILED A ASMFO OTHER N FALSE WARNING TOTAKEOFF 1 SW23755RA 49727 AFTER TAKEOFF ON CUU STATION TAIL COMP TEMP HIGH LIGHT COMES ON. DURING OVERNIGHT SERVICE, TAIL COMP OVERHEAT SENSORS WERE REPLACED IAW MM 36-20-02 AND WIRING SENSORS WERE VERIFIED IAW WDM 36-23-00, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030620000682003062000068NM 2003 6 20 USAA030067 120030516A521065535954 STRIKER BOEING737 737401 1384701NM DOOR SEAL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 PIT - FOUND SEAL DEPRESSOR CRACKED 2 INCHES, UPPER FORWARD CORNER FORWARD SERVICE DOOR SEAL DEPRESSOR. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2L72 4F RTA16WE 20030620000802003062000080NM 2003 6 20 MEX2003200 120030601A2761 ACTUATOR DOUG MD88 MD88 3023688NM AUTO SPOILER MALFUNCTIONED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23168PL 53174 AIRCRAFT RETURNED TO GATE, DURING TAXI TAKEOFF, ALARM AND AUTO SPOILERS VOICE APPEARED. AIRCRAFT DID FLY UNDER MEL 27-19 CAT C. DURING OVERNIGHT SERVICE THE SPOILER AUTOMATIC ACTUATOR WAS REPLACED IAW MM 27-62-05, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030617001732003061700173NM 2003 6 17 QXEA200300684 120030505A5320 BRACKET BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - CHAFE DAMAGE TO BRACKET OF VERTICAL WALL OF AFT CARGO BAY UPPER, LOWER DECK. REPAIRED IAW HORIZON AIR EA 6-54-249. 2H72 4T RTA13NM 20030617001742003061700174SW 2003 6 17 HEEA087472 120030612A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 FUSIBLE PLUG LEAKING. 1G71 3U O H2SW 20030617001792003061700179NM 2003 6 17 QXEA200300705 120030610A5551 FITTING BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - RIGHT HAND FORWARD FITTING FOR HORIZONTAL STAB MOUNT IS GOUGED FROM INSTALLATION OF BARREL NUT. REPAIRED IAW RD 8/4-55-92, PAGE 6, STEP4. 2H72 4T RTA13NM 20030617001932003061700193EU 2003 6 17 ERAA087103 120030520A65204619002003 GEARBOX BOLKMS105 BO105S 5626006EU TAIL ROTOR MAKING METAL E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01292EH1220 562 INT GEARBOX MAKING METAL. C/W PRE INSPECTION. NO DEFECTS NOTED. DISASSEMBLED GEAR BOX FORMS NECESSARY FOR REPAIR. CLEANED & VISUALLY INSPECTED ALL PARTS. NO DEFECTS NOTED. REASSEMBLED G/B WITH NEW O RINGS, ORIGINAL PARTS & HARDWARE. SAFTIED ALL REQUIRED HARDWARE, PROSEALED & PAINTED GEAR BOX REQUIRED. COMPLIED WITH ASB 105-30-111. FOUND NO OBVIOUS REASON FOR G/B TO MOVE. COMPLIED WITH METAL INSPECTION IAW REM 304 TT 12193.9 TSO 242.7 1G72 3U H3EU 20030617002152003061700215SW 2003 6 17 HEEA087312 120030611A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X4293 53267 CORROSION AT WEIGHT POCKET. SERIAL NUMBERS REMOVED ARE A1353, A1369, A1383 AND A1405. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030617002762003061700276SW 2003 6 17 HEEA087032 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 MAIN ROTOR DRIVE UNIVERSAL WORN. 1G71 3U O H2SW 20030617002952003061700295WP 2003 6 17 GTIA030355 120030510A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND DENTS AT FS 265-313 AT LONGRONS 21R. CUT OUT DAMGAED AREA. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED NEW 11 SKIN, FINGER DOUBLER, AND 5 DOUBLER. (M) 2L72 4F A6WE 20030617003012003061700301NM 2003 6 17 SWAA031219 120030602A3350AD20131A BATTERY BOEING737 7373H4 1384600NM CABIN FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS ILLUMINATING WHEN SWITCH IS OFF. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER FOR FWD CABIN DOOR EMERGENCY EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20030617003042003061700304NM 2003 6 17 SWAA031260 120030605A3350BR2013 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C3 CHECK, FOUND EEPLS SECTION INOP AND AFT CABIN END CAP MISSING. RELAMPED EEPLS AND INSTALLED END CAP PER MM. 2L72 4F A16WE 20030618000062003061800006SW 2003 6 18 HEEA087484 120030612A7714LTX1965002 LAMP BELL 407 407 1182206SW COCKPIT INOPERATIVE E HEEAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SW03498PH 53399 LOW ROTOR RPM CAUTION LIGHT INOPERATIVE. TO BE SENT TO BELL HELICOPTER FOR CREDIT. 1G71 3U O H2SW 20030618000562003061800056NE 2003 6 18 SWAA031340 220030615A7230 BLADE BOEING737 7372H4 138448CNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE BENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 687882 DURING WALK AROUND INSP, FOUND BENT FAN BLADES (6 EA) ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 F A16WE E2EA 20030618001532003061800153EA 2003 6 18 COMA0360277 120030613A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01915CA23093 7013 DURING COMPLIANCE TASK 022-53-160-610, THREE CRACKS WERE FOUND IN PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL 9.0 AND RBL 9.0. THE CRACKS RANGE FROM 2.5 INCH TO 3.375 INCH IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV B, DATED 6-8-2003, AND REO 601R-53-41-162, DATED 6-9-2003. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20030618001652003061800165 2003 6 18 HEEA087143 420030611A22157690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS JAMMED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 ACTUATOR JAMMED. REPLACED WITH SERVICEABLE PART. 1G72 3U NCH1NE 20030618001932003061800193SW 2003 6 18 HEEA087159 120030609A6220206011117003 RESTRAINT BELL 206 206L4 1182110SW M/R HEAD STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0362127 52023 FLAP RESTRAINT STICKS DOWN. REPAIRED. 1G71 3U NCH2SW 20030618001972003061800197SW 2003 6 18 HEEA087366 120030611A2510407070620140 PANEL BELL 407 407 1182206SW COCKPIT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 HEADLINER CRACKED BEYOND REPAIR. 1G71 3U O H2SW 20030619000052003061900005SW 2003 6 19 HEEA087176 120030609A6330206040270101 SUPPORT BELL 206 206L3 1182108SW GEARBOX LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 AFT SUPPORT LEAKING. REPLACED UNION (3 EA) AN8333D DUE TO SEAT AND THREAD DAMAGE; NUT (3 EA) AN924-3D DUE TO THREADS STRIPPED; HOUSING SUPPORT 206-040-241-001 (4 EA) DUE TO CORROSION IN BOLT HOLES. REPAIRED. 1G71 3U H2SW 20030619000552003061900055GL 2003 6 19 HEEA087204 220030609A7320DPUA0101 COMPUTER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE CONTROL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206LS 51070 ENGINE CONTROL COMPUTER COULD NOT DOWNLOAD SYSTEM. 1G71 3U3 U H2SW E1GL 20030619000812003061900081SW 2003 6 19 HEEA086933 120030603A6420206011728003 TRUNNION BELL 407 407 1182206SW PITCH CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 PITCH CONTROL TRUNNION HAS WORN SPINDLES. TO BE SENT TO MFG. 1G71 3U O H2SW 20030619000822003061900082SW 2003 6 19 HEEA087216 120030609A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 MAIN BATTERY WEAK. REPAIRED. 1G71 3U H2SW 20030619000892003061900089 2003 6 19 HEEA086928 420030529A2210214001347005 ACTUATOR BELL 412 412 1182202SW AFCS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 WOULD NOT AUTO TRIM WITH AFCS. SENT TO MFG FOR WARRANTY REPAIR. 1G72 4U H4SW 20030619000902003061900090SW 2003 6 19 HEEA086930 120030603A6710206001396001 SHAFT BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 LOW CYCLIC FRICTION - COULD NOT ADJUST FRICTION DUE TO WORN THREADS. TO BE SENT TO MFG. 1G71 3U O H2SW 20030619000982003061900098SW 2003 6 19 HEEA087422 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030619001012003061900101SW 2003 6 19 HEEA087425 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 TAIL ROTOR DISC PACK HAS CORROSION PITS BEYOND LIMITS. 1G71 3U O H2SW 20030620000012003062000001 2003 6 20 HEEA087227 420030610A3422066304607 GYRO BELL 206 206L4 1182110SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 DG PRECESSES 35 DEGREES IN 15 MINUTES. SHOP REPAIR. 1G71 3U NCH2SW 20030620000052003062000005SW 2003 6 20 HEEA087231 120030610A6340206075681117 INDICATOR BELL 206 206L3 1182108SW DUAL TACH MISMARKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 RANGE MARKINGS ARE INCORRECT, 99 TO 101 PERCENT IS FOR A -123 INDICATOR ONLY. THIS ONE SHOULD BE 97 TO 100 PERCENT. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030620000252003062000025SW 2003 6 20 HEEA086947 120030603A3212206050247137 COVER BELL 407 407 1182206SW FLOAT ASSY TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 FLOAT COVER ASSY TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030620000292003062000029SW 2003 6 20 HEEA087427 120030612A3212407350300101 FLOAT BELL 407 407 1182206SW MLG FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03491PH 53386 FAILED 6 MONTH INSPECTION. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030620000422003062000042NM 2003 6 20 USAABB03077 120030516A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030620000482003062000048SO 2003 6 20 ASOA03223 120030518A5610NP1513111 WINDSHIELD EMB 120 EMB120RT 3260202SO FUSELAGE SEPARATED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11258AS 120131 FLT 4888 - DURING CLIMB-OUT FROM AEX-GTR, AT APPROXIMATELY 14,000 FEET THE CABIN PRESSURE BEGAN TO CLIMB AT 2,000 FEET PER MINUTE. THE AIRCRAFT DESCENDED TO 10,000 FEET DURING WHICH TIME THE CAPTIAN NOTICED A GAP HAD OCCURRED BETWEEN HIS WINDSHIELD AND THE AIRCRAFT ALONG THE LOWER EDGE. THE CREW COMPLIED WITH QRH PROCEDURES, DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO AEX, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD. SPEED TAPE WAS APPLIED TO EXPEDITE CURE TIME IAW MM 56-10-01. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030620000572003062000057WP 2003 6 20 GTIA030401 120030519A5310 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND MID PIT STATION 636 FRAME END FITTING CORRODED. LOCATED AND DRILLED HOLES NEW FITTING. (M) 2L72 4F A6WE 20030623000222003062300022NM 2003 6 23 USAA030074 120030520A5310 CREASE BEAM BOEING757 757225 1384959NM BS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 CLT - FOUND CREASE BEAM WEB CRACKED 1 INCH, BS 1368 STRINGER 17L. REPLACED WEB PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20030623000242003062300024NM 2003 6 23 USAASB03072 120030531A33501012721 LIGHT BOEING737 7373B7 1384580NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 PILOT REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 12C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030623000262003062300026NM 2003 6 23 USAA030085 120030601A53206552878V97 SILL BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US40013 23990 FOUND SILL ASSEMBLY CORRODED 1.5 INCH AREA, AFT ENTRY DOOR LOWER SILL ASSEMBLY FROM STATON 907 PLUS 6 INCHES, STATION 1006. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20030623000272003062300027NM 2003 6 23 USAA030084 120030521A5200AN201KP4A BEARING BOEING737 737401 1384701NM DOOR FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US40808 23986 FOUND FAILURE IN TERMINAL OF ROLLER BEARING, AFT CARGO DOOR AND DEEP GOUGES IN LATCHING FITTING AND COVER PLATE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2L72 4F RTA16WE 20030623000462003062300046WP 2003 6 23 GTIA030341 120030510A5320 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - ATTACH ANGLE STATION 592 MID PIT CORRODED. WHILE REMOVING CORROSION, ATTACH ANGLE WAS FOUND TO BE CRACKED. FABRICATED REPLACEMENT CLIP. (M) 2L72 4F A6WE 20030623000552003062300055WP 2003 6 23 GTIA030343 120030506A5342 ATTACH ANGLE DOUG DC9 DC982 3022082WP VERTICAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 LEFT DORSAL FIN VERTICAL ATTACH ANGLE HAS CRACK IN VERTICAL LEG. REMOVED LEFT DORSAL FIN VERTICAL ATTACH ANGLE. LOCATED AND DRILLED NEW DORSAL FIN VERTICAL ANGLE. INSTALLED LEFT DORSAL FIN OUTSIDE ATTACH ANGLE. (M) 2L72 4F A6WE 20030623000632003062300063NM 2003 6 23 2003F00378 120030319A335010005511 LIGHT DHAV DHC8 DHC8103 1386005NM CABIN MALFUNCTIONED A KPVAK NONE O OTHER ININSP/MAINT 1 WP13805WP 353 PORTABLE EMERGENCY LIGHT DIM. REMOVED PORTABLE EMERGENCY LIGHT AND RE-INSTALLED SERVICEABLE PORTABLE EMERGENCY LIGHT BY RESECURING INTO LOCKING SOCKET. (M) 2H72 4T RTA13NM 20030623000652003062300065SO 2003 6 23 ASOA03209 120030513A335012021299001 LIGHT EMB 120 EMB120ER 3260203SO FUSELAGE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11268AS 120202 DURING A GROUND INSPECTION IN DFW, THE EXTERIOR LEFT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR LEFT AFT EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030623000682003062300068CE 2003 6 23 2003F00379 120030516A2910510011194 LINE CESSNA402 402C 207590RCE HYD SYSTEM CRACKED A CRJAO OTHER O OTHER LDLANDING 1 CE016764C 402C0628 THE PILOT WAS UNABLE TO NORMALLY EXTEND THE LANDING. EMERGENCY GEAR EXTENSION PROCEDURES WERE SUCCESSFUL. SUBSEQUENT INSPECTION REVEALED THAT THE RIGHT GEAR EXTENSION PRESSURE LINE HAD DEVELOPED A .5 INCH CRACK JUST PRIOR TO THE LANDING GEAR UPLOCK ACTUATOR. THE AIRCRAFT LOST HYDRAULIC FLUID. THE CRACK IN A LOCATION WERE THE LINE MADE A 180 DEGREE BEND. THE CRACK APPEARS TO BE CAUSED BY FATIGUE. THE LINE WAS THE ORIGINAL LINE AND WAS 21 YEARS. THE LINE WAS REPLACED. (M) 1L72 3O A7CE 20030623000732003062300073EA 2003 6 23 ASOA03207 120030510A5720CC670170811 FITTING CNDAIRCL600 CL6002C10 1390015EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11705EV 10051 DURING HANGAR MAINTENANCE IN BTR, THE RIGHT WING INBOARD SPOILER HINGE FITTING AT STATION WS 185.11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE RIGHT WING INBOARD SPOILER HINGE FITTING AT STATION WS 185.11 UPON ARRIVAL OF THE REPLACEMENT PART. (M) 2L72 4F RTA21EA 20030623000752003062300075NM 2003 6 23 2003F00383 120030524A3610 CLAMP BOEING727 727225 1384077NM BLEED AIR LOOSE A MYWAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO19803MA 22434 ON CLIMB-OUT FROM MIA, PASSING THROUGH F/ 29 LOWER AFT BODY OVERHEAT LIGHT CAME ON. FOLLOWED AOM AND ISOLATION PROCEDURES. RETURNED TO MIA FOR MAINTENANCE ACTION. T/S PER MM 26-14-0. FOUND LOOSE CLAMP IN AFT CARGO COMPARTMENT SIDEWALL FORWARD CORNER. SECURED LOOSE CLAMP AND LEAK CHECK. NO FURTHER LEAKS NOTED AND SYSTEM OPS NORMAL AT 2.06 EPR FOR 5 MINUTES. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030623000772003062300077CE 2003 6 23 2003F00385 120030512A5531 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1953545 UE185 AT SCHEDULED ROUTINE INSPECTION, VERTICAL STABLIZER FORWARD TOP RIB HAS TWO CRACKS ON STRESS RELIEF HOLES. REPAIRED VERTICAL STABILIZER FORWARD TOP RIB BY INSTALLING TWO REPAIR DOUBLERS AT THE END OF CRACKS IAW BEECH 1900D STRUCTURAL REPAIR MANUAL 51-70-17, FIGURE 1, PAGE 2 JUNE/99. (M) 2L72 4T RTA24CE 20030618001162003061800116NM 2003 6 18 SWAA031292 120030608A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29758SW 27873 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED IN SEVERAL AREAS. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030618001182003061800118NM 2003 6 18 SWAA031293 120030609A52306547952 DOOR SEAL BOEING737 7373H4 1384600NM CARGO DOOR DAMAGED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29356SW 25251 AIR TURNBACK, UNABLE TO PRESSURIZE CABIN. REMOVED AND REPLACED AFT CARGO DOOR SEAL AND LOWER OVER PRESSURE SAFETY VALVE PER MM. 2L72 4F RTA16WE 20030618001442003061800144EA 2003 6 18 COMA0360268 120030611A335059465 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN FAULTY A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01924CA 7026 FLIGHT 5464 EMERGENCY FLOOR LIGHTS FORWARD OF ROW 8 ARE INOPERABLE. REPLACED WIRING CONNECTOR AT ROW 1. 2L72 4F RTA21EA 20030617003302003061700330SW 2003 6 17 HEEA087041 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030618000112003061800011 2003 6 18 HEEA087489 420030612A3457N0002000 GPS BELL 407 407 1182206SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 GPS OUTERLINK RECEIVES INTERMITTENTLY. REPAIRED. 1G71 3U O H2SW 20030618000872003061800087 2003 6 18 SWAA031300 420030609A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030618001072003061800107 2003 6 18 SWAA031288 420030608A2565D31593 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030618001252003061800125NE 2003 6 18 HEEA087135 120030610A76007630103901102 ACTUATOR SKRSKYS76 S76A 8143006NE ENGINE ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 ACTUATOR OPERATES ERRATICALLY AND HESITATES DURING MID TRAVEL. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030618001302003061800130EA 2003 6 18 COMA0360261 120030606A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01959CA 7116 FLIGHT 5738 GEAR DISAGREE WARNING. CLEANED AND LUBED THE NLG. COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA21EA 20030618001342003061800134EA 2003 6 18 COMA0360262 120030608A5754601R120448 PANEL CNDAIRCL600 CL6002B19 1900309EA L/E SLAT CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01967CA17122 7134 RIGHT WING LEADING EDGE PANEL ASSEMBLY 630JL HAS A 3.0 INCH VERTICAL CRACK AT WS 190.0. REMOVED RIGHT WING LEADING EDGE PANEL 630JL, FITTED AND INSTALLED NEW SERVICEABLE RIGHT WING LEADING EDGE ASSEMBLY IAW CRJ AMM 57-41-01-400-804. 2L72 4F RTA21EA 20030618001522003061800152EA 2003 6 18 COMA0360275 120030612A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01729CA12759 7265 FLIGHT 5733 GEAR DISAGREE WARNING AFTER TAKE-OFF. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 20030618001622003061800162 2003 6 18 HEEA087141 420030610A2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE CABIN MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 CAUSING STATIC IN CABIN ICS. SHOP REPAIR. 1G72 3U H1NE 20030618001852003061800185SW 2003 6 18 HEEA087152 120030609A6710206001053005 BEARING BELL 206 206L3 1182108SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038591X 51495 BELLCRANK ASSY HAS WORN BEARINGS. REPLACED BEARING (2 EACH) 206001053005 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618001952003061800195SW 2003 6 18 HEEA087161 120030609A6400 BEARING BELL 206 206L3 1182108SW ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 WORN BEARINGS. SCRAPPED. 1G71 3U H2SW 20030619000272003061900027SW 2003 6 19 HEEA087376 120030611A5320407070620156 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 HEADLINER PANEL CRACKED. 1G71 3U O H2SW 20030619000332003061900033SW 2003 6 19 HEEA087187 120030609A29002111328 FILTER ELEMENT BELL 206 206L3 1182108SW FUEL SYSTEM CLOGGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 RETURN BYPASS BUTTON POPS. REPAIRED. 1G71 3U H2SW 20030619000432003061900043SW 2003 6 19 HEEA087387 120030611A3397407076502103S CONNECTOR BELL 407 407 1182206SW COCKPIT CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 DECK CONNECTOR CORRODED. 1G71 3U O H2SW 20030619000872003061900087SW 2003 6 19 HEEA087416 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 AFT COUPLING DISK PACK CRACKED. 1G71 3U O H2SW 20030620000032003062000003 2003 6 20 HEEA087229 420030610A34570845000000 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F WILL NOT MAINTAIN PRESET WAYPOINTS AFTER POWER IS REMOVED FROM THE AIRCRAFT. SHOP REPAIR. 1G71 3U H2SW 20030620000552003062000055NE 2003 6 20 ASOA03233 220030526A72614047T95P01 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ENGINE LEAKING A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11834AS 7254 872360 FLT 4383 - DURING CLIMB-OUT FROM MGM-DFW, AT APPROXIMATELY 22,000 FEET THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE MASTER WARNING MESSAGE WITH THE OIL PRESSURE DROPPING RAPIDLY TO ZERO PSI. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE RIGHT ENGINE. THE AIRCRAFT DIVERTED TO MLU AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN MLU. MAINTENANCE FOUND THE RIGHT ENGINE MAIN OIL TANK EMPTY, REMOVED AND REPLACED THE SCAVENGE PUMP LINE AND REDUCER FITTINGS. OPERATIONAL AND LEAK AND CHECKS GOOD. AIRCRAFT OK FOR SERVICE. THE AIRCRAFT WAS FERRIED TO MCN AND THE RIGHT ENGINE WAS REMOVED AND REPLACED FOR TEARDOWN INSPECTION OF THE MAIN LINE BEARING AS A PRECAUTION2L72 4F4 FRTA21EA E15NE 20030620000642003062000064NM 2003 6 20 USAA030088 120030524A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US42211 23876 CLT - FOUND CRACK IN SKIN 3.5 INCHES, STATION L 495, L STRINGER 17, SKIN. INSTALLED DOUBLER AND TRIPLER PER EA 87256. (M) 2L72 4F RTA16WE 20030623000062003062300006NM 2003 6 23 USAA030061 120030529A53106545871523 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US46845 23232 DOOR STOP CUTOUTS CRACKED .0180 INCHES IN LENGTH, WL 240 AND WL 250 OF DOOR STOPS, FORWARD GALLEY DOOR AFT FRAME. TEMP REPAIR, TRIM TO REMOVE CRACKS, DEBURR AND BREAK SHARP EDGES PER EA 74896. (M) 2L72 4F RTA16WE 20030623000092003062300009WP 2003 6 23 AMTA200300659 120030507A5312 BULKHEAD LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 COMPARTMENT AFT BULKHEAD CORRODED FS 1685 LBL 24 TO LBL 28 JUST ABOVE CARGO FLOOR. REPAIRED BULKHEAD IAW SRM 51-50-07. (M) 2L73 4F A23WE 20030623000112003062300011NM 2003 6 23 AMTA200300655 120030516A3350 STRIP BOEING737 73783N 13844HINM ESCAPE STRIP CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11321TZ 28249 THE FLOOR EGRESS FROM SEATS 2-3 DEF IS CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF PHOTOLUMINESCENT STRIP REF MM 33-51-15-2. (M) 2L72 4F RTA16WE 20030623000352003062300035EA 2003 6 23 A6WA200340075 120030527A2910401R4523559 LINE CNDAIRCL600 CL6002B19 1900309EA NLG LEAKING A A6WAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL31426AW 7669 WHILE TAXIING AIRCRAFT LOST NR 3 HYDRAULIC. FLUID LEAKING AROUND NOSE LANDING GEAR. REMOVED AND REPLACED RIGHT INBOARD LINE IN NOSE COMPARTMENT. (M) 2L72 4F RTA21EA 20030623000412003062300041WP 2003 6 23 GTIA030350 120030514A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND CORROSION AT PAX CABIN FLOOR SUPPORT FS 200. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030623000452003062300045WP 2003 6 23 GTIA030336 120030415A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 AFT PIT CORRODED AT FRAME, STATION 1079 - 1309. REMOVED CORROSION ON FRAME STATION 1231-1271 AND 1309. FOUND OUT OF LIMITS. CUTOUT DAMAGE IF FRAME FROM STATION 1231. INSTALLED NEW SECTION OF FRAME. SPLICE REPAIR STATION 1231. CUTOUT DAMAGE AREA OF FRAME STATION 1271. LOCATED AND DRILLED NEW SECTION OF FRAME. FABRICATED 4 REPAIR SPLICES AND 4 PLATES. INSTALLED SECTION OF FRAME AND SPLICES REPAIR ON FRAME STATION 1271. LOCATED AND DRILLED NEW FRAME. FOUR ANGLES REPAIRS 5, 9 FOR SPLICE REPAIR. FABRICATED FOUR PLATES. INSTALLED NEW SECTION OF FRAME STATION 1309 L28R AND L28L. INSTALLED FRAME SPLICES. (M) 2L72 4F A6WE 20030623000492003062300049WP 2003 6 23 GTIA030356 120030511A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND DENT AT 58 JUST ABOVE FLOOR LEVEL. REMOVED DAMAGED SKIN SECTION AT FS BT STRINGER 17-18 LEFT, CUT OUT IS 5375 BY 8.75. FABRICATED REPAIR PARTS 5 BBL, 9 FINGER BDL 15 SKIN SEC INSTALLED ALL REPAR PARTS. (M) 2L72 4F A6WE 20030623000502003062300050WP 2003 6 23 GTIA030358 120030511A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - AFT FUSELAGE STATION 1380 RIGHT SIDE CORRODED AT INTERCOSTAL AND ANGLE SUPPORT 'T' CAP. DRILLED AND LOCATED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2L72 4F A6WE 20030623000622003062300062NM 2003 6 23 2003F00377 120030319A3010 BOOT DHAV DHC8 DHC8103 1386005NM LT LE SEPARATED A KPVAK NONE O OTHER ININSP/MAINT 1 WP13805WP 353 FOUND LEFT LEADING EDGE DE-ICE BOOT SEPARATED FROM LEADING EDGE. RE-SEALED LEFT LEADING EDGE 513BL DE-ICE BOOT IAW MM 30-10-46 PAGE 225-230. (M) 2H72 4T RTA13NM 20030623000692003062300069EA 2003 6 23 ASOA03219 120030517A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING AN A-CHECK IN BTR, THE RIGHT EXTERIOR EMERGENCY LIGHT AFT OF THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT LAMP AFT OF THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030623000762003062300076CE 2003 6 23 2003F00384 120030224A712012991004717 TRUSS BEECH 1900 1900D 1154162CE ENGINE CHAFED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1917534 UE141 AT SCHEDULED ROUTINE MAINTENANCE, CHAFING DAMAGE AT 2.75 INCHES AFT OF FIRE SEAL FLANGE ON INBOARD SIDE. PERFORMED TRUSS REPAIR TO CHAFED AREA IAW FAA APPROVED DATA CONTAINED IN RAYTHEON FIELD REPAIR FR-CO-00830 REV A. (M) 2L72 4T RTA24CE 20030623000792003062300079SO 2003 6 23 2003F00387 120030524A29101159SCH5125 VALVE GULSTMGV GULFSTREAMGV3980116SO HYD SYSTEM MALFUNCTIONED A UG8AO OTHER J WARNING INDICATION APAPPROACH 1 GL235101 550 UNABLE TO GET NORMAL LANDING GEAR EXTENSION. PERFORMED EMERGENCY LANDING GEAR EXTENSION. T/S LANDING GEAR SYSTEM INDICATED A MALFUNCTION OF THE LANDING EAR HYDRAULIC SELECTOR VALVE LOCATED IN THE MAIN WHEEL WELL. REPLACED LANDING GEAR HYDRAULIC SELECTOR/DUMP VALVE. LANDING GEAR OPERATIONAL CHECKS NORMAL IAW GULFSTREAM MM. (M) 2L72 4F RTA12EA 20030618001022003061800102SW 2003 6 18 HEEA087348 120030611A7120 BEARING BELL 407 407 1182206SW MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 ENGINE MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030619000152003061900015SW 2003 6 19 AC2A086765 120030528A622050047C632 BOLT BELL 430 430 1182150SW ALLSN 250C 250C* GL MAIN ROTOR GALLED E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH 49037 BOLT IS GALLED. THREADS OF BOLTS FOUND GALLED DURING ROUTINE MAINTENANCE. REPLACED BOLTS. 1G72 3U3 URTH9SW E4CE 20030619000392003061900039SW 2003 6 19 HEEA087383 120030611A6320407040624101 TUBE BELL 407 407 1182206SW GEARBOX OIL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 FRETTING CORROSION AT FLARE UNDER "B" NUT. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030619000562003061900056 2003 6 19 HEEA087206 420030609A2562ELP362D ELT BELL 206 206L3 1182108SW CABIN WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0321497 51518 ELT WOULD NOT TEST. SENT TO RJE INTERNATIONAL FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20030620000192003062000019SW 2003 6 20 HEEA086941 120030603A3212206050247132 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 EMERGENCY FLOAT COVER TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030620000222003062000022SW 2003 6 20 HEEA086944 120030603A3212206050247135 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 FLOAT COVER ASSY TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030620000372003062000037SW 2003 6 20 HEEA087436 120030612A2560407370720101 RESTRAINT BELL 407 407 1182206SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 SEAT BELT WORN. 1G71 3U O H2SW 20030620000542003062000054WP 2003 6 20 GTIA030382 120030516A5320 STRUCTURE DOUG DC9 DC981 3022081WP SUBFLOOR GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - SUBFLOOR GOUGED STATION 180 RBL 34. MATERIAL FOUND TO BE CRACKED. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F A6WE 20030623000152003062300015NM 2003 6 23 AMTA200300632 120030512A3350 LIGHT BOEING737 73783N 13844HINM CABIN BROKEN A AMTAK NONE O OTHER ININSP/MAINT 1 GL11322TZ 32611 FORWARD LEFT SEAT 1ABC FLOOR PROXIMITY LIGHTING STRIP BROKEN. REMOVED AND REPLACED PROXIMITY STRIP PER MM 33-51-15. (M) 2L72 4F RTA16WE 20030623000742003062300074EA 2003 6 23 ASOA03208 120030328A261223410400 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA LT ENGINE INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11858AS 7417 FLT 4766 - DURING CLIMB-OUT DFW-AUS, THE CREW RECEIVED A LEFT ENGINE 14TH STAGE DUCT MESSAGE AT APPROXIMATELY 14,000 FEET. QRH AND EMERGENCY PROCEDURES WERE COMPLIED WITH. THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE 14TH STAGE PYLON FIRE LOOP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030623000822003062300082EU 2003 6 23 USAASA03042 120030516A335032145410 LIGHT AIRBUSA319 A319112 3930323EU CABIN FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW11788 0890 EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE LEFT MID EPSU. (M) 2L72 4F RTA28NM 20030623001022003062300102NM 2003 6 23 USAASB03070 120030526A2133322684003 OUTFLOW VALVE BOEING737 737301 1384611NM E/E BAY LEAKING A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19573US 23560 EN ROUTE FROM MCI TO CLT, AT FL290, THE CABIN BEGAN CLIMBING AT OVER 1,000 FEET PER MINUTE. BLEED PRESSURE WAS NORMAL AND THE OUTFLOW VALVE WAS CLOSED. CABIN STABILIZED ONCE AIRCRAFT DESCENDED TO FL240. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT CLT. MAINTENANCE FOUND AIR LEAKS AT THE FORWARD OUTFLOW VALVE, E/E COMPARTMENT DOOR AND APU DUCT PRESSURE SEAL AT AFT BULKHEAD. REPLACED FORWARD OUTFLOW VALVE PER MM 21-43-11. OPERATIONAL CHECK NORMAL. REPLACED PRESSURE SEAL FOR APU BLEED DUCT. LEAK CHECK GOOD. FOUND SEAL ROLLED ON E/E COMPARTMENT DOOR. REPOSITIONED SEAL. PERFORMED LEK RATE CHECK PER MM 05-51-01. LEAK CHECKS WITHIN LIMITS. (M) 2L72 4F RTA16WE 20030623001122003062300112EA 2003 6 23 A6WA200340082 120030520A5755 SKIN CNDAIRCL600 CL6002B19 1900309EA SPOILER DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 RIGHT INBOARD GROUND SPOILER HAS A DENT ON TOP SKIN INSPECTED AND NOTED DENT IAW WVAC EO 601R-57-4039A. (M) 2L72 4F RTA21EA 20030623001162003062300116EA 2003 6 23 A6WA200340084 120030527A3242601R4523559 LINE CNDAIRCL600 CL6002B19 1900309EA RT BRAKE CRACKED A A6WAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 GL31426AW 7669 WHILE TAXIING AIRCRAFT LOST NR 3 HYD FLUID LEAKING AROUND NLG. REMOVED AND REPLACD RIGHT INBOARD BRAKE LINE IN NOSE COMPARTMENT. (M) 2L72 4F RTA21EA 20030624000032003062400003WP 2003 6 24 GTIA030373 120030507A5320 CLIP DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND AFT PIT CORRODED AND CRACKED ANGLE CLIP AT FS 1250 LONGERON 23L-24L. REMOVED CLIP. INSTALLED NEW CLIP. (M) 2L72 4F A6WE 20030624000122003062400012WP 2003 6 24 GTIA030410 120030519A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND DENT AT FS 321 BETWEEN LONGERONS 25 AND 26R, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20030624000172003062400017NM 2003 6 24 USAABB03080 120030522A33501640487 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030624000192003062400019NE 2003 6 24 VNAA0306005 220030608A7532 BLEED VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ENGINE FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07458PS 3068 AFTER DEPARTURE, THE CREW RECEIVED A LEFT HAND LOW PRESSURE BLEED VALVE FAILED CLOSED INDICATION AND RETURNED TO CAK. MAINTENANCE INSPECTED AND SWAPPED THE LEFT HAND ENGINE LOW PRESSURE AND HIGH PRESSURE BLEED VALVES FOR TROUBLESHOOTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00 AND THE LOW PRESSURE BLEED VALVE CHECKED GOOD. HOWEVER, THE HIGH PRESSURE BLEED VALVE REMAINED CLOSED AND WAS DEFERRED, 36-1 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030624000302003062400030NM 2003 6 24 CALA0300312 120030613A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 8 AND LBL 12. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5320-01603. 2L72 4F RTA16WE 20030624000452003062400045NM 2003 6 24 CALA0300298 120030608A551065C251564 FITTING BOEING737 7373T0 1384582NM HORIZONTAL STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, RBL 10. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02, FIGURE 12, SHEET 2. 2L72 4F RTA16WE 20030624000512003062400051NM 2003 6 24 CALA0300288 120030606A575365C372631 SUPPORT BOEING737 737524 1384721NM NR 1 FLAP TRACK GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719638 28899 INSPECTION FOUND NR 1 FLAP TRACK FAIRING SUPPORT GOUGED AT I/B HINGE LUG. A NEW TRACK FAIRING SUPPORT WAS INSTALLED IAW MM 27-51-71. 2L72 4F RTA16WE 20030624000642003062400064NM 2003 6 24 CALA0300307 120030611A575465C26601180 SKIN BOEING737 7373T0 1384582NM NR 6 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 2 INCH CRACK IN NR 6 SLAT PANEL SKIN AT LOWER RIVET LOCATED JUST O/B OF I/B AUX TRACK, RIGHT SLAT STA 300. A REPAIR WAS INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20030624000702003062400070EA 2003 6 24 COMA0370019 120030614A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01368CA 10075 FLIGHT 5877 LEFT THRUST REVERSER UNSAFE MESSAGE DURING TAKE-OFF, ABORTED AND RETURNED TO THE GATE. DEFERRED LEFT THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20030619000162003061900016SW 2003 6 19 HEEA087179 120030609A6320206040270101 SUPPORT BELL 206 206L3 1182108SW GEARBOX LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 MAIN ROTOR GEARBOX AFT SUPPORT LEAKING. REPAIRED. 1G71 3U H2SW 20030619000222003061900022SW 2003 6 19 HEEA087185 120030609A3210206323202 SUPPORT BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 MLG SUPPORT WORN AND CORRODED. SCRAPPED. 1G71 3U H2SW 20030619000242003061900024SW 2003 6 19 HEEA087373 120030611A2510407070620152 PANEL BELL 407 407 1182206SW SEAT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 SEAT PANEL CRACKED. 1G71 3U O H2SW 20030619000932003061900093SW 2003 6 19 HEEA087417 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030619001042003061900104 2003 6 19 HEEA087226 420030610A3425066304604 INDICATOR BELL 206 206L3 1182108SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 WON'T HOLD HEADING, PRECESSES. SHOP REPAIR. 1G71 3U H2SW 20030623000332003062300033WP 2003 6 23 MEX2003185 120030519A2430976J2528 GENERATOR DOUG DC9 DC987 3022087WP RIGHT FAILED A ASMFO OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SW231075T 49724 AIRCRAFT ARRIVED WITH REPORT RIGHT GENERATOR OUT OF SERVICE, GENERATOR WAS REPLACED AND AFTER ENGINES STARTING CAPTAIN INFORMS THAT SAME CONDITION CONTINOUS. AIRCRAFT ARRIVED BY ITS OWN IMPULSE TO THE POSITION S-7, ENGINES WERE SHUTDOWN AND WIRING WERE VERIFIED, ALL CORRECT. GENERATOR WAS REPLACED AGAIN IAW TO MM 24-10-00, TESTS CORRECT. (M) 2L72 4F RTA6WE 20030624000402003062400040NM 2003 6 24 CALA0300322 120030606A5522 SKIN BOEING777 777224 1385225NM RT ELEVATOR TORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2777006 29476 MAINTENANCE FOUND A TEAR APPROXIMATELY 1 INCH LONG IN RT ELEVATOR TRAILING EDGE SKIN. THE TEAR WAS CENTERED 195 INCHES FROM THE I/B END OF THE ELEVATOR. THE TEAR WAS 2.25 INCH LONG AND SPANNED THREE FASTENERS. THE ELEVATOR WAS REPAIRED IAW ECRA 5520-01333. 2L72 4F RTT00001SE 20030624001122003062400112NM 2003 6 24 XNOA01121 120030528A7603 THROTTLE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE OUT OF ADJUST A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL2376753 21249 ON TAKEOFF ENG NR 2 & 3 NORMAL. ENG NR 1 THROTTLE 4 KNOBS MORE OUT OF ALIGN WITH 2.2 EPR AND 88 PERCENT N1. TAKEOFF REJECTED. FOUND NR 1 EPR INACCURATE. TRANSFERRED TO DMI 3383 IN ACCORDANCE WITH MEL 77-1-2. PLACARDS INSTALLED. 2L73 4F4 F A3WE E2EA 20030625000112003062500011WP 2003 6 25 03FDEA00804 120030524A5230AKC7288 RUB STRIP DOUG DC10 DC1010 3022110WP DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 LT PATIO DOOR UPPER STAINLESS STRIP CRACKED AND CRUSHED. CLOSING ACTION ON 05/24/03. REMOVED CLOSEOUT STRIP IAW SRM 51-31-01.FAB NEW RUB STRIP ON TRAVLER T2/33374, LOCATED AND DRILLED NEW PART IAW SRM 51-31-01.INSTALLED RUB STRIP IAW SRM 51-31-01 2L73 4F A22WE 20030625000132003062500013WP 2003 6 25 03FDEA00802 120030524A5754ARB1242 SKIN DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 NR S 17 COMPLY WITH E.A.8-5710-70392.WINGS-RT-FIXED LEADING EDGE BEADED DOUBLER REPAIR ACB 1242. CLOSING ACTION ON 05/23/03. COMPLIED WITH E.A.8-5710-70392. 2L73 4F A22WE 20030625000312003062500031NM 2003 6 25 AWXA200300586 120030527A3411C16195AA PITOT HEAD AIRBUSA319 A319132 3930340NM ZONE 120 DAMAGED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28829AW6336 1563 ON TAKEOFF ROLL AT YYC EN ROUTE, THE CAPTAINS AIRSPEED IND READS 20 KTS LOWER THAN 1ST OFFICERS & STANDBY AIRSPEED IND. T/O REJECTED AT SPEED OVER 100 KTS. MAINT INSTALLED PITOT STATIC TESTER, BOTH PILOTS & 1ST OFFICERS ALTIMETERS TESTED GOOD UP TO 1200 FT. WATER FOUND & DRAINED FROM CAPTAINS PITOT STATIC SYSTEM. A FUP WAS WRITTEN TO PERFORM AN INSPECTION OF THE CAPTAINS PITOT PROBE PER AMM TASK 34-11-15-200-001, AND FUNCTIONAL TEST ENTIRE SYSTEM PER 34-13-00-720-009. WHEN THE AIRCRAFT ARRIVED BACK IN PHX, MAINTENANCE REMOVED AND REPLACED THE LT PITOT PROBE IAW AMM 34-11-15-401. OPERATIONAL CHECK WAS GOOD IAW AMM 30-31-00-710. VENDORS FUNCTIONAL TEST OF PITOT PROBE S/N 4911 CONFIRMED FAILURE OF UNIT. 2L72 4F RTA28NM 20030625000412003062500041EU 2003 6 25 AWXA200300595 120030518A5411D54630462202 STRUCTURE AIRBUS320 A320231 3930325EU RT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-03 CHECK A 1/2 INCH CRACK WAS FOUND ON RT PYLON ATTACH ANGLE (EXTRUSION PROFILE) AT THE INBOARD FORWARD CORNER OF PANEL 4230 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF ATTACH ANGLE; FABRICATED A FILLER AND REPAIR SPLICE; INSTALLED REPAIR PARTS IAW A320 SRM 54-52-12, PG. 215-220, FIG 203. 2L72 4F RTA28NM 20030625000452003062500045EU 2003 6 25 AWXA200300599 120030519A5321D5367005600100 FLOOR PANEL AIRBUS320 A320231 3930325EU CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 MCN - MAJOR REPAIR - DURING C-01 CHECK CENTER WING FLOOR PANEL 242FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 242FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70055; INSTALLED REPAIR PART IAW AWA T/C R1C25306. 2L72 4F RTA28NM 20030625000492003062500049NM 2003 6 25 03FDEA00823 120030528A3260189915 SENSOR BOEING727 727200 138407ENM MLG UP&DOWN LOCKINOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25467FE 21449 ON TAKE OFF, LANDING GEAR LEVER WOULD NOT RETRACT PAST THE OFF DETENT. PERFORMED QRH PROCEDURE FOR LANDING GEAR LEVER LATCH FAILED TO RELEASE. T/S PER 727-200 WDM 32-31-01. OHM CHECKED ENTIRE AIR & GROUND SENSOR CIRCUITS FROM L/G ACCESSORY RACK PLUG AND CONFIRMED AN OPEN CIRCUIT INSIDE THE AIR SENSING PROX SWITCH WHEN COMPARED TO A KNOWN NEW SWITCH. R&R'D THE AIR SENSING PROX SWITCH SENSOR LOCATED ON LT GEAR PER 727-200 MM 32-09- 221-4 & OPS CHECKED AIR GROUND SENSE & LEVER LOCK CIRCUITS PER MM 32-09-221-5 AND 32-31-016-4. AIR SENSE MODE NOW FULLY FUNCTIONAL. LEVER LOCK RELEASES ON TEST & L/G LEVER MOVES UP. 2L73 4F RTA3WE 20030625000502003062500050WP 2003 6 25 03FDEA00822 120030528A5312 BULKHEAD DOUG DC10 DC1010 3022110WP ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 COMPLY WITH E.A.8-5310-70387. FUSELAGE-MAINFRAME-REPAIR OF STA 1987 BULKHEAD P/N AJC7066-1. CLOSING ACTION ON 05-27-03 ON N/R C00019. COMPLIED WITH E.A.8-5310-70387. 2L73 4F A22WE 20030625000542003062500054NM 2003 6 25 03FDEA00748 120030507A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- I/B FLAP O/B HINGE (FLAP SIDE), LWR PIVOT I/B LUG HOLE CORRODED. SNRM N1013 - RH WING- I/B FLAP O/B HINGE (FLAP SIDE) LWR PIVOT I/B LUG HOLE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-68411, WING- RIGHT INBOARD TRAILING EDGE FLAP- HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20030626000082003062600008CE 2003 6 26 GLBA2003050 120030421A5270 SENSOR BEECH 1900 1900D 1154162CE CARGO DOOR OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03150GL UE150 CARGO DOOR ANNUN ILLUM, ADJUSTED DOOR AJAR SENSOR SWITCH OPS CHK GOOD 2L72 4T RTA24CE 20030626000162003062600016NE 2003 6 26 MALA030221 220030402A7200 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 4 SMOKE A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15535XJ E2371 DURING FLIGHT 3407, CREW REPORTED SMOKE IN THE COCKPIT. AIR RETURN TO DTW. REFER TO SDR MALA030225 FOR ADDITIONAL INFORMATION. MAINTENANCE REPLACED NR 4 ENGINE. 2H74 4F4 FRTA49EU E6NE 20030626000212003062600021WP 2003 6 26 IXXA0300026O 120030315A5280 HINGE DOUG DC8 DC873F 302199FWP MLG DOOR WORN A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11606AL894321184 46044 DURING TAKEOFF FROM KTOL TO KLAX ON GEAR RETRACTION HANDLE UP DOOR UNLATCHED LIGHT STAYS ILLUMINATED. UP LATCH CHECK LIGHT STAYED ILLUMINATED AND REMAINED ILLUMINATED WITH HANDLE UP. INSPECTION IS ON GOING AND AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED MULTIPLE PARTS. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH THE DOUGLAS AIRCRAFT MAINTENANCE MANUEL. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20030626000222003062600022NM 2003 6 26 DHL2003753003 120030415A2612 SWITCH BOEING727 727223 1384074NM APU WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01753DH 22468 APU FIRE TEST IS INOPERATIVE. TRANSFERRED TO DMI LIST IAW MEL 26-11 CAT-C. SPECIAL PROCEDURES APPLY REF CONTROL 12585. DOES NOT EFFECT SAFE OPERATION OF AIRCRAFT. 2L73 4F A3WE 20030630000072003063000007EU 2003 6 30 CX7A194J37 120030404A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03300CE 340B184 LT TAILPIPE HOT LIGHT ILLUMINATED ON T/O ROLL. 2L72 4T RTA52EU 20030630000342003063000034EU 2003 6 30 AWXA200300610 120030502A5311D53370241200 FRAME AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK AFTER FIRST OVERSIZE OF FASTENER HOLE COMMON TO SKIN A 1/8 INCH CRACK WAS FOUND ON FRAME 41, THIRD FASTENER HOLE BELOW STR 14 LT. MAINTENANCE REAMED OUT HOLE TO SECOND OVERSIZE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; CUTOUT DAMAGED SECTION OF FRAME 41 AT THIRD FASTENER HOLE BELOW STR 14 LT; FABRICATED A REPAIR ANGLE AND FRAME FILLER; INSTALLED REPAIR PARTS IAW E.O. 53-14-20. 2L72 4F RTA28NM 20030630000382003063000038EU 2003 6 30 AWXA200300614 120030502A5320D5397470700000 PROFILE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR PROFILE FR 58, LBL 660MM TO RBL 660MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PROFILE FR 58, LBL 660MM TO RBL 660MM IAW AWA E.R. 26-5341-03142-TB5. 2L72 4F RTA28NM 20030620000732003062000073NM 2003 6 20 USAA030069 120030516A5320654580734 ANGLE BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 PIT - FOUND ANGLE WITH .5 INCH CRACK, UPPER SIDE S9R AT STATION 291.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2L72 4F RTA16WE 20030623000312003062300031EU 2003 6 23 USAASA03036 120030501A3260848401 PROXIMITY SWITCH AIRBUS320 A320214 3930316EU MLG BAY INOPERATIVE A USAAA OUNSCHED LANDING OTHER N FALSE WARNING CLCLIMB 1 EA19106US 1044 AFTER TAKEOFF, CREW RECEIVED ECAM INDICATIONS OF 'GEAR NOT UPLOCKED', 'ENG 2 REVERSER FAULT', AND 'CAPT PITOT'. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A PROXIMITY SWITCH, FIN 23GA. LANDING GEAR SYSTEMS CHECK WAS NORMAL. (M) 2L72 4F RTA28NM 20030623000482003062300048WP 2003 6 23 GTIA030338 120030501A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FOUND CORRODED FRAME IN AFT LEFT LAVATORY AT FS 1338 LEFT SIDE APPROX 6 INCHES ABOVE CUSP LINE. FABRICATED 3 ANGLE AND 5 SPLICE ANGLE. INSTALLED 3 ANGLE AND 5 SPLICE REPAIR. (M) 2L72 4F A6WE 20030623001072003062300107NM 2003 6 23 USAASB03066 120030516A335020121 CHARGER BOEING737 7374B7 1384702NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 MAINTENANCE FOUND SEVERAL EMERGENCY EXIT LIGHTS, AT VARIOUS LOCATIONS THROUGHOUT THE CABIN, INOPERATIVE. MAINTENANCE FOUND THE M1479 BATTERY CHARGER ASSEMBLY BAD. REMOVED AND REPLACED THE M1479 BATTERY CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030624000222003062400022NM 2003 6 24 VNAA0306001 120030601A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DOOR FAILED A VNAAO OTHER O OTHER CRCRUISE 1 GL07431JS 3028 THE CREW RECEIVED A DOORS LIGHT ON THE RED WARNING PANEL AND RETURNED TO PIT. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND ADJUSTED THE PROXI SENSORS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030624000472003062400047NM 2003 6 24 CALA0300300 120030609A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 787 TO 850 AT STRINGER 25R. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030624000542003062400054NM 2003 6 24 CALA0300291 120030606A5320C226020491015 MOUNT BOEING737 737524 1384721NM GALLEY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719638 28899 INSPECTION FOUND RT AFT GALLEY FLOOR MOUNT CORRODED. THE FLOOR MOUNT WAS REPLACED IAW ECRA 2540-01305. 2L72 4F RTA16WE 20030624000672003062400067NM 2003 6 24 CALA0300324 120030617A5210654N02449 LOCK BOEING757 757224 1384958NM PAX DOOR INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714121 27563 THE L-2 DOOR HOLD OPEN LOCK FAILED TO OPERATE. THE HOLD OPEN LOCK WAS REPLACED IAW MM 52-11-02. 2L72 4F RTA2NM 20030624000812003062400081SO 2003 6 24 SWIA200312077 120030606A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP FAILED A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM07217SW8141 8141 120286 SHORTLY AFTER SELECTING FLAPS 15 DEGREES FOR LANDING, RECEIVED A FLAP DISAGREEMENT ON THE INBOARD & NACELLE FLAPS. WITHIN A FEW SECONDS, LOST THE ENTIRE BLUE HYD SYSTEM AS NOTED BY NO FLUID QUANTITY AND SUBSEQUENT WARNING LIGHTS. INSTALLED SERVICEABLE HYD ACTUATOR ON RT NACELLE FLAP. OPS CHECK AND LEAK CHECKS GOOD IAW 27-50-00. 2L72 4T RTA31SO 20030625000142003062500014WP 2003 6 25 03FDEA00801 120030524A7830 CONTROL VALVE DOUG DC10 DC1010 3022110WP THRUST REVERSER FAILED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 N 860 #2 O/B T/R FAILS TO AUTO-RESTOW CHECK. CLOSING ACTION ON 05/24/03. REMOVED AND REPLACED DIRECTI0NAL CONTROL VALVE IAW M/M 78-31-11-2, LEAK TO BE ACCOMPLISHED ON W/C 78X3501CMR. 2L73 4F A22WE 20030625000572003062500057NM 2003 6 25 03FDEA00751 120030513A5753NRC6066 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING, O/B FLAP I/B HINGE (FLAP HINGE SIDE), AFT ATTACHING POINT, BOTH FWD AND AFT BOLT HOLE CORRODED. LT WING, O/B FLAP I/B HINGE (FLAP HINGE SIDE) AFT ATTACHING POINT, BOTH FWD AND AFT BOLT HOLE REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413, WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT COOROSION. 2L73 4F RTA22WE 20030626000052003062600005WP 2003 6 26 UPS03840431 120030418A3530 SMOKE BARRIER DOUG DC8 DC871F 302199DWP COCKPIT TORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: PFLT, MAIN CARGO DECK SMOKE CURTAIN HAS A 8 INCH TEAR & HAS COME UNSCURED BOTH IN THE LOWER LT OUTBOARD SIDE. PERFORMED INTERIM REPAIR EO DC8 -2550-1872B TRASFERD TO D-258389 FINAL SMOKE CURTAIN REPAIR ACCOMPLISHED PER UPS E.O. #DC8-2550-1872, APPENDIX 8.3, OK FOR SERVICE.THIS CLEARS D258389 2L74 4F RT4A25 20030630000082003063000008EU 2003 6 30 CX7A194J38 120030404A26131734362450 DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT TAILPIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03302CE 340B193 LT TAILPIPE HOT LIGHT ILLUMINATED ON TAKEOFF ROLL. 2L72 4T4 TRTA52EU E8NE 20030630000652003063000065SW 2003 6 30 ALGA087781 120030626A8011214060056109 STARTER BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE ENGINE MALFUNCTIONED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03391AL 28103 WILL NOT ENGAGE EVERYTIME. REQUEST WARRANTY REPAIR. RO 33256 DMR 719713 2G72 4U4 U H10SW E8NE 20030630000802003063000080SW 2003 6 30 HEEA087842 120030613A6230406010429101 PIN BELL 407 407 1182206SW GIMBAL RING WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 PIN WORN AND STUCK IN GIMBAL RING. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030618001102003061800110NM 2003 6 18 SWAA031319 120030612A552365C26384 HINGE BOEING737 7373A4 1384585NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C3 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20030618001142003061800114SW 2003 6 18 HEEA087499 120030612A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 METAL PARTICLES IN GREASE ON FRONT BEARING. REPLACED BEARING 407-340-339-101, S/N ZV10970 DUE TO ROUGH; BEARING 407-340-339-101, S/N ZV10935 DUE TO ROUGH. REPAIRED. 1G71 3U O H2SW 20030618001772003061800177SW 2003 6 18 HEEA087515 120030613A3210407030112103 FITTING BELL 407 407 1182206SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 MLG FITTING WORN BEYOND LIMITS. CAUSED BY CONTACT BETWEEN ROCKING BEAM AND FITTING. REPLACED. 1G71 3U O H2SW 20030619000442003061900044 2003 6 19 HEEA087194 420030609A34424000038 CONTROL HEAD BELL 206 206B3 1181506SW WX RADAR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 VOLUME KNOB INOPERATIVE. REPLACED VOLUME POTENTIOMETER. REPAIRED. ALSO REPLACED VOLUME KNOB, SELECTOR KNOB AND FACEPLATE. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030619000772003061900077SW 2003 6 19 HEEA087412 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030620000382003062000038GL 2003 6 20 HEEA087000 220030604A732023072725 HMU BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 SHOWED BAD ON PLA DATA. SENT FOR INSPECTION AND REPAIR. 1G71 3U3 UO H2SW E4CE 20030620000832003062000083EU 2003 6 20 ASOA03224 120030518A5320S53970716357 BRACKET AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT UPPER AND LOWER ATTACHMENT BRACKETS FOR THE BANANA SEAL PANEL WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT UPPER AND LOEWR ATTACHMENT BRACKETS FOR THE BANANA SEAL PANEL IAW SRM 53-91-42. (M) 2H72 4T RTA53EU 20030623000232003062300023NM 2003 6 23 USAA030056 120030516A5315 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 FOUND FLOORBEAM CORROSION 1 INCH BY 3 INCH AREA, UPPER SURFACE FLOORBEAM UPPER CHORD BS 1320, LBL 24. FLOORBEAM UPPER CHORD REPAIR, UPPER CHORD REPLACEMENT LBL 54-RBL 36 PER T/R 53-15-01. (M) 2L72 4F RTA2NM 20030623000362003062300036WP 2003 6 23 GTIA030334 120030517A3260 UPLOCK SENSOR DOUG DC9 DC983 3022083WP LT MLG DAMAGED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23826NK 49391 LT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION, UNTIL CLIMBING OUT OF 1500 FEET AGL. BOTH PILOTS HEARD A THUMP AND THEN THE LIGHT WENT OUT. NO FURTHER ABNORMAL INDICATIONS. PERFORMED GEAR RETRACTION TEST. FOUND LEFT UPLOCK SENSOR OUT OF LIMITS. READJUSTED. (M) 2L72 4F RTA6WE 20030623000562003062300056WP 2003 6 23 GTIA030353 120030510A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND DENT AT FS 598 BETWEEN LONGERONS 21 AND 22R. REMOVED DAMAGED AREA. FABRICATED NEW SECTION OF SKIN 29, 19 FINGER DOUBLER, 27 DOUBLERS, 23 DOUBLERS. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20030623000902003062300090 2003 6 23 GTIA030414 420030601A2565 BRACKET DOUG DC9 DC982 3022082WP ESCAPE SLIDE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 SLIDE PACK BRACKET ON R-1 DOOR WILL NOT HOLD SLIDE PACK GIRT BAR. REPOSITIONED AFT GIRT BAR HOOK ON R-1 SLIDE PACK. GIRT BAR OPERATION NORMAL. (M) 2L72 4F A6WE 20030623000922003062300092WP 2003 6 23 GTIA030405 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND TWO SMALL FLOOR SUPPORTS LBL 53 AND 1 LONG SUPPORT LBL 57 STATION 160-200 ARE CORRODED. REMOVED LONG FLOOR SUPPORT. REMOVED SMALL FLOOR SUPPORT. FABRICATED LONG AND 1 SMALL FLOOR SUPPORT. INSTALLED 1 SMALL FLOOR SUPPORT LBL 53 AND 1 LONG FLOOR SUPPORT. (M) 2L72 4F A6WE 20030623000932003062300093WP 2003 6 23 GTIA030411 120030519A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND DENT AT FS 350 BETWEEN LONGERONS 25 AND 26R. DENT WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED WITH SOLID FASTENERS. (M) 2L72 4F A6WE 20030623000962003062300096WP 2003 6 23 GTIA030403 120030514A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND CORROSION AROUND FASTENER HOLES AT STATION 237 ON WEB AT RBL 47 TWO PLACES. CUT OUT DAMAGED AREA. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030623000992003062300099EU 2003 6 23 USAABA03016 120030522A3350321430 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 EMERGENCY LIGHT BATTERY 11WL FAILS EPSU CAPACITY TEST. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA46NM 20030618001682003061800168SW 2003 6 18 HEEA087146 120030609A6220206301051101 BEARING BELL 206 206L3 1182108SW PIVOT ASSY UNSTAKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 UPPER BEARING UNSTAKED. REPLACED BEARING 206301051101 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618001742003061800174SW 2003 6 18 HEEA087512 120030612A79218543909 OIL COOLER BELL 206 206L3 1182108SW ENGINE OIL MALFUNCTIONED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW03141BH 51303 OIL COOLER PRODUCING HIGH OIL TEMP. SHOP REPAIR. 1G71 3U H2SW 20030618001862003061800186SW 2003 6 18 HEEA087153 120030609A6710206001554001 SUPPORT BELL 206 206L3 1182108SW M/R CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N 51512 SUPPORT HAS OUTBOARD BUSHING WORN. REPLACED BUSHING 214-001-917-003 DUE TO WORN; BUSHING 21-010-16-10 DUE TO WORN; BUSHING 22-008-23-24-20 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618002002003061800200SW 2003 6 18 HEEA087369 120030611A2510407070620149 PANEL BELL 407 407 1182206SW SEAT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 SEAT PANEL CRACKED. 1G71 3U O H2SW 20030618002022003061800202 2003 6 18 HEEA087519 420030610A3421504001790116 GYRO BOLKMS105 BO105S 5626006EU COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 HORIZON GYRO PRECESSES. SHOP REPAIR. 1G72 3U H3EU 20030618002032003061800203GL 2003 6 18 HEEA087520 220030610A72406870992 CASE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL COMBUSTION SEC CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 OUTER COMBUSTION CASE CRACKED. REPLACED CASE. 1G72 3U3 U H3EU E4CE 20030618002132003061800213SW 2003 6 18 HEEA087166 120030609A6320 BEARING BELL 206 206B3 1181506SW DRAG PIN ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G B127256 3610 DRAG PIN ASSY BEARING WORN. REPAIRED. 1G71 3U H2SW 20030618002162003061800216SW 2003 6 18 HEEA087169 120030609A6320 BUSHING BELL 206 206L3 1182108SW ARM ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N 51512 BUSHINGS WORN; BUFFER PADS UNBONDED. REPAIRED. 1G71 3U H2SW 20030619000012003061900001SW 2003 6 19 HEEA087172 120030609A6330206033542003 MOUNT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 TRANSMISSION MOUNT BEARING JOURNALS WORN. REPAIRED. 1G71 3U H2SW 20030529000152003052900015NM 2003 5 29 AALA20030460 120030414A3350 SOCKET BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21780AN 29956 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 36G INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT 36G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030529000182003052900018NE 2003 5 29 2003F00330 220030321A7200 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE NR 2 STALLED A P9RAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO11919PG 22604 P708804 NR 2 ENGINE WENT INTO A CONTINUOUS COMPRESSOR STALL SHORTLY AFTER LANDING GEAR RETRACTION ON TAKEOFF AT MSP. EGT CLIMBED INTO AND STABILIZED IN THE RED ARC FOR 1 MINUTE, RETARDED ENGINE THROTTLE TO IDLE POSITION AND ENGINE STABILIZED, ALL OTHER SYSTEMS NORMAL. AIRCRAFT RETURNED TO MSP WITH THE ENGINE AT IDLE. ENGINE WAS SHUTDOWN UPON RETURN TO GATE. TOTAL ENGINE OPERATION WAS 48 MINUTES. FOUND NOSE DOME ASSEMBLY PART NR 65196842 DETACHED FROM FRONT ACCESSORY COVER P/N 633758. PROBABLE CAUSE OF DETACHMENT ATTRIBUTED TO OVER TORQUE OF STUD P/N AN126294. C1 BLADE DAMAGE FOUND. ENGINE BOROSCOPE REVEALED NO FURTHER DAMAGE. C1 DISK REPLACD IAW MM 723000. (M) 2L73 4F4 FRTA3WE E2EA 20030529000642003052900064 2003 5 29 HEEA086651 420030521A237080510800001 DATA BOX BELL 412 412 1182202SW SKYWATCH FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032148K 36001 SKYWATCH DATA BOX FAILS OPERATIONAL CHECK AFTER 5 MINUTES. 1G72 4U H4SW 20030529000672003052900067EU 2003 5 29 BAQA086229 120030422A622057911100 THRUST BEARING AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR CORRODED E BAQAO OTHER O OTHER NRNOT REPORTED 1 SW03199SM1081 6396 THRUST BEARING CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE UNITS. 1G72 3U3 U H10EU E19EU 20030529000692003052900069 2003 5 29 HEEA086511 420030521A3416212070238003 INDICATOR SKRSKYS76 S76A 8143006NE COPILOT ALT INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 COPILOT ALTIMETER READS 100 FEET DIFFERENT. REPAIRED. 1G72 3U H1NE 20030529000752003052900075 2003 5 29 HEEA086517 420030521A34427000839901 INDICATOR SKRSKYS76 S76A 8143006NE RADAR ALT ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 RADAR ALTIMETER INDICATOR IS ERRATIC AND HAS UNRELIABLE NEEDLE MOVEMENT. SENT TO HONEYWELL, TEXAS FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030623001032003062300103EA 2003 6 23 A6WA200340080 120030520A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 FUSELAGE SKIN IS DAMAGED AT PAX DOOR CUTOUT FS 349. REPAIRED FUSELAGE SKIN AT PAX DOOR CUTOUT FS 349 IAW BOMBARDIER INC REO 601R-53-21-078. (M) 2L72 4F RTA21EA 20030623001042003062300104NM 2003 6 23 USAASB03065 120030511A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT FAILED A USAAO OTHER N FALSE WARNING CRCRUISE 1 EA19591US 23936 EN ROUTE FROM BUF-PHL, PILOT REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 17 THROUGH 20 ILLUMINATED INTERMITTENTLY DURING ENTIRE FLIGHT. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20030623001092003062300109WP 2003 6 23 AMTA200300714 120030523A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 FOUND 7 INCH CRACK IN SKIN PANEL FS 1725 AFT OF REMOVEABLE PANEL 313A LEFT SIDE, TOP OF NR 2 ENG'S DUCT. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW ERA L1011-53R-5188, NO FURTHER INSPECTION REQUIRED. (M) 2L73 4F A23WE 20030624000132003062400013NM 2003 6 24 USAABB03073 120030515A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4 AND 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030624000162003062400016NM 2003 6 24 USAABB03075 120030515A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19621AU 27200 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030624000182003062400018NM 2003 6 24 USAABB03079 120030520A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19633AU 27811 PIT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 1 MISSING. MAINTENANCE HAD PREVIOUSLY REPLACED THE SEAT ROW AND NOT INSTALLED THE LIGHT. LIGHT WAS INSTALLED. (M) 2L72 4F RTA2NM 20030624000212003062400021NM 2003 6 24 VNAA0306003 120030606A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07463PS 3087 THE CREW REPORTED THAT THE FLIGHT ATTENDANTS EMERGENCY LIGHTING WAS INOP. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030624000242003062400024SO 2003 6 24 SWIA200312079 120030608A2750 ROD EMB 120 EMB120ER 3260203SO NACELLE FLAP OUT OF ADJUST A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07297SW 120327 EXCESSIVE SLACK NOTED IN MOVEMENT OF LEFT NACELLE FLAP. REPLACED LEFT NACELLE FLAP ACTUATOR ROD END IAW EMB 120 MM 27-50-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030624000392003062400039NM 2003 6 24 CALA0300321 120030602A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND UPPER SECTION OF FLOORBEAM CORRODED AT BS 328. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01145. 2L72 4F RTA16WE 20030624000422003062400042NM 2003 6 24 CALA0300296 120030607A5754 SKIN BOEING737 7373T0 1384582NM NR 5 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT PANEL AT I/B AUX TRACK. REPAIRED SLAT SKIN IAW SRM 57-43-01, FIGURE 206, SHEETS 1-4. 2L72 4F RTA16WE 20030624000632003062400063NM 2003 6 24 CALA0300306 120030611A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND A .5 INCH CRACK AND UPPER SHIM DAMAGE IN FLOOR PANEL SUPPORT AT STA 540, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030624000662003062400066NM 2003 6 24 CALA0300309 120030612A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603. 2L72 4F RTA16WE 20030624000792003062400079SO 2003 6 24 SWIA200312075 120030607A2751 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAP IND FAILED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07268UE 120207 INBOARD FLAPS DISAGREEMENT ON LIGHT BAR, CONTROL FAULT ILLUMINATED ON O/H PANEL, FLAP INDICATOR SHOWED ZERO DEGREES (ALL DURING TAXI OUT). REPLACED CONNECTOR P1756 AND P1757 AS REQUIRED. ALSO MEGGED SYSTEM WIRING. NO DEFECTS NOTED. SYSTEM OPS CHECK GOOD IAW 27-50-00. 2L72 4T RTA31SO 20030624000802003062400080SO 2003 6 24 SWIA200312076 120030607A3260 WIRE HARNESS EMB 120 EMB120ER 3260203SO MLG UNSERVICEABLE A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07187SW 120037 WHEN LANDING GEAR LEVER WAS MOVED DOWN, RIGHT RED TRANSITION -A- LIGHT STAYED ON, RIGHT GREEN -A- LIGHT DID NOT COME ON. REMOVED AND INSTALLED SERVICEABLE WIRE HARNESS. OPS CHECK GOOD ON GEAR SWING IAW EMB MM 32-61-01. P/N OFF/ON 120-22623-501. 2L72 4T RTA31SO 20030624000862003062400086NM 2003 6 24 DLM88030459 120030512A5220 SEAL DOUG MD88 MD88 3023688NM OVERWING EXIT LEAKING A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27996DL 53363 LEFT SIDE SQUEAL REPORTED BY FLIGHT ATTENDANT AFTER T/O. REMOVED LEFT FOWARD OVERWING EXIT DOOR CLEARED SEAL INSPECTED SEAL AND DOOR NO FURTHER DEFECTS NOTED PERFORMED OVERWING EMERGENCY EXIT CHECK ON LEFT FORWARD DOOR PER M/M. 2L72 4F RTA6WE 20030624000922003062400092NM 2003 6 24 DL73S030466 120030514A2760654496116 ACTUATOR BOEING737 737232 1384475NM LT WING CRACKED A DALAO OTHER K FLUID LOSS LDLANDING 1 SO27317DL 0352 23089 AFTER LANDING ROLL OUT, LOSS OF SYSTEM -A- QUANTITY PRESSURE FOUND NR 1 SPOILER ACTUATOR CRACKED. REPLACED ACTUATOR 2L72 4F RTA16WE 20030619000232003061900023SW 2003 6 19 HEEA087372 120030611A2510407070620152 PANEL BELL 407 407 1182206SW SEAT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 SEAT PANEL CRACKED. 1G71 3U O H2SW 20030619000592003061900059SW 2003 6 19 HEEA087400 120030611A6510407340339101 BEARING BELL 407 407 1182206SW COOLER ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 FWD BEARING ROUGH ON OIL COOLER BLOWER SHAFT. 1G71 3U O H2SW 20030620000312003062000031SW 2003 6 20 HEEA087429 120030612A3212407350302101 FLOAT BELL 407 407 1182206SW MLG LEAKING E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03493PH 53393 LEAKING AROUND FWD INSIDE RELIEF VALVE. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030620000392003062000039NM 2003 6 20 USAABB03083 120030603A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030620000712003062000071NM 2003 6 20 USAA030080 120030522A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US49058 23316 FOUND SKIN CRAKCED .75 INCH LONG CRACK, SKIN AFT ENTRY DOOR LOWER HINGE CUTOUT STATION 947.5, STRINGER 14L. DOUBLER AND TRIPLER INSTALLED AND PAINTED PER SRM 53-60-01 AND EA 76329. (M) 2L72 4F RTA16WE 20030623000522003062300052WP 2003 6 23 GTIA030360 120030508A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND CORRODED LONGERON STRAP AND ATTACHMENT HARDWARE AFT BAG BIN STATION 1320-1338 L23R TO L25R. REMOVED TWO LONGERON STRAP AT STATION 1320-1338 L24R-L23R. INSTALLED NEW LONGERON STRAP FITTING, L24R STATION 1320-1338. INSTALLED NEW LONGERON STRAP FITTING L23R STATION 1320-1338. (M) 2L72 4F A6WE 20030623000872003062300087WP 2003 6 23 GTIA030406 120030515A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND FLOOR SUPPORT STATION 148-200 RBL 7 HAS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030623000982003062300098WP 2003 6 23 GTIA030408 120030515A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLOOR SUPPORT HAS CORROSION STATION 160-200 RBL 43. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030624000072003062400007EU 2003 6 24 A6WA200360029 120030523A5320 CONDUIT BAC 146 146300A 1500267EU FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 FLANGED CONDUIT P/N HC535B0285-000 IS KINKED AND HAS TWO HOLES. MAINTENANCE WELDED CONDUIT IAW BAE FAX BARA/AVR/6411/03-DC. (M) 2H74 4F RTA49EU 20030624000292003062400029WP 2003 6 24 EIA2003081 120030504A5330 SKIN DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09915F 47061 PER N5339, LT ENTRY DOOR, UPPER AFT CORNER SKIN CRACKED BETWEEN LONGERONS 8 & 9, BS 200. REMOVED DAMAGE 7 INSTALLED FABRICATED FILLERS & DOUBLERS PER SRM 53005, PGS 540, 551, 552. REPEAT INSPECTIONS PER W/C N5343 AT OR BEFORE 28,000 CYCLES. 2L72 4F A6WE 20030624000612003062400061NM 2003 6 24 CALA0300304 120030606A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 1 INCH CRACK IN VERTICAL ANGLE ON BOTTOM END AT BS 616, LBL 65 OF MAIN CABIN, TOP OF WING CENTER SECTION. THE ANGLE FORMS I/B SECTION OF BS 616 FORGING AT EXIT HATCH. REPAIRED IAW ECRA 5311-01150. 2L72 4F RTA16WE 20030625000202003062500020NM 2003 6 25 DHL2003726006 120030528A2782 SLAT BOEING727 727228 1384083NM NR 2 MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01726DH 20409 DURING CLIMB, UPON FLAP RETRACTION NR 2 SLAT FAILED TO RETRACT. PERFORM ABNORMAL PROCEDURES. DID NOT FIX PROBLEM. AIRCRAFT TURNED BACK AND RETURNED TO BASE. INSPECTED NR 2 L/E SLAT ROLLERS TRACKS ACTUATOR ATTACH POINTS IAW B-727 MM. NO DEFECTS NOTED. INSP. LT WING L/E NR 2 SLAT WIRING AND OPS CONNECTIONS IAW B-727 WDM. L/E SLAT POSITION INDICATOR SWITCH OP'S CHECKED NORMAL ADJ. IAW B-727 MM. OPERATED L/E SLATS THRU NUMEROUS CYCLES ON GROUND. NO DEFECTS NOTED. OP'S CHECK ACCOMPLISHED IAW B-727 MM. 2L73 4F RTA3WE 20030625000332003062500033NM 2003 6 25 AWXA200300587 120030504A5320146N5318 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT CABIN SHEAR DECK BS 1701 TO BS 1720, STR 17 LT TO STR 17 RT. MAINTENANCE REMOVED SHEAR DECK WEB FROM BS 1680 TO BS 1720; FABRICATED REPLACEMENT SHEAR DECK WEB PER DWG 146NB5318; INSTALLED REPAIR PART IAW 51-40-02, PG. 4, 11, & 16. 2L72 4F RTA2NM 20030625000342003062500034NM 2003 6 25 AWXA200300588 120030505A5315146N5246U8 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-O9 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT BS 1640 TO BS 1660, RBL 70. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR SUPPORT BS 1640 TO BS 1660, RBL 70; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW 51-40-02, PG. 7. 2L72 4F RTA2NM 20030625000372003062500037NM 2003 6 25 AWXA200300591 120030504A5315BAC15172226 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM AT BS 1469, RBL 16. MAINTENANCE FOUND CORROSION TO BE ON EXISTING REPAIR ANGLE; REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT LIMITS; REMOVED CORRODED REPAIR ANGLE AT BS 1469, RBL 16; FABRICATED A NEW REPLACEMENT REPAIR ANGLE; INSTALLED REPAIR PART IAW 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030625000392003062500039NM 2003 6 25 AWXA200300593 120030509A5320143N8328 SUPPORT ANGLE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION FOUND ON L-4 DOOR THRESHOLD SUPPORT ANGLE AT B/S 1681. MAINTENANCE REMOVED L-4 DOOR THRESHOLD SUPPORT ANGLE AT B/S 1681; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE PER DWG 143N8328; INSTALLED REPAIR PART IAW B757 SRM 51-70-11 PAGES 1-7. 2L72 4F RTA2NM 20030625000472003062500047EU 2003 6 25 AWXA200300601 120030519A5321D536700500000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 DURING C-01 CHECK CENTER WING FLOOR PANEL 241EF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241EF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306. 2L72 4F RTA28NM 20030625000482003062500048NM 2003 6 25 DHL2003726007 120030528A2781 ACTUATOR BOEING727 727228 1384083NM NR 2 SLAT MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01726DH 20409 UPON FLAP RETRACTION NR 2 FLAP FAILED TO RETRACT PERFORMED ABNORMAL PROCEDURE DID NOT FIX PROBLEM. PERFORMED DETAILED CHECK OF SLAT SYSTEM WIRING. FOUND NO DEFECTS IAW B-727 WDM 27-81-02. REMOVED AND REPLACED NR 2 SLAT ACTUATOR IAW B-727 MM 27-81-0. OP'S CHECK OF SLAT SYSTEM CHECKS GOOD ON GROUND TEST IAW B-727 MM 27-81-0. 2L73 4F RTA3WE 20030625000522003062500052EU 2003 6 25 03FDEA00815 120030527A5310 DOOR FRAME AIRBUS300 A300B4605R 3930308EU CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 COMPLY WITH E.A. 6-5313-70393 "FUSELAGE-MAIN FRAME-LWR FWD CARGO DOOR FRAME/FUSELAGE SKIN REPAIR AT FRAME 20A FACT 27MAY03 11:35 BFM U COMPLIED WITH E.A. 6-5313-70393 FUSELAGE-MAIN FRAME- LWR FWDCARGO DOOR FRAME/FUSELAGE SKIN REPAIR AT FR20A. 2L72 4F RTA35EU 20030625000852003062500085NM 2003 6 25 UPS03440187 120030214A5414 SKIN BOEING747 747200 1384847NM NR 3 NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01528UP 24071 INSPECTION TYPE:PFLT NR 3 ENG PYLON INBOARD SIDE AFT ENG MOUNT ACCESS CUT PANEL PREVIOUS DOUBLER HOLE CHAFED THROUGH, HOLE CHAFED APPROX 2 INCHES AFT OF CUTOUT. REMOVED PREVIOUS REPAIR TO INBOARD SIDE OF PYLON. REPAIRED ACCESS DOOR/TAB SPACER,REMOVED FASTENER AND STARTED DRILLING HOLES. TRIMMED REPAIR DOUBLER AND COUNTERSUNK HOLES. INSTALLED DOUBLER, COMPLETED INSTALLATION OF REPAIR 54-34-03. 2L74 4F RTA20WE 20030626000062003062600006WP 2003 6 26 ABXA030132 120030411A30404TL1593 SWITCH DOUG DC9 DC932 3022066WP ANTI ICE SYS SHORTED A ABXAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23900AX 47380 SAW SMOKE IN BEHIND CAPTAIN'S OVERHEAD MAP LIGHT AND SMELLED ELECTRICAL. DONNED OXYGEN AND JUMP SEATER CHECKED NO SMOKE/FIRE IN UPPER DECK. NO FIRE/SMOKE INDICATOR LIGHTS, ALL PANEL INDICATIONS NORMAL AND COULDN'T IDENTIFY SOURCE, SMOKE SUBSIDED, THEN LESS THAN 60 SECONDS LATER WE SMELLED AGAIN, ALMOST AS MUCH AS INITAILLY. STARTED ELECTRICAL SMOKE CHECKLIST AND EMERGENCY LANDED VFR IN MEMPHIS. FOUND EVIDENCE OF BURNED WIRE AND SMOKE AT STATION 45 IN OVERHEAD CENTER PANEL AREA. WINDSHIELD HEAT SWITCH FOUND TO BE BURNED AND CRACKED. FOUND CENTER WINDSHIELD WIRE H589A16 BURNED 2 INCHES FROM WINDSHIELD, CUT H589A16 BACK TO REMOVE DAMAGED WIRE AND INSTALLED NEW TERMINAL ON SAME, REPLACED WINDSHIELD HEAT SWITCH IAW 2L72 4F A6WE 20030627000042003062700004CE 2003 6 27 TXHA6881BB 120030420A32005045213 TUBE CESSNA402 402A 207590MCE MGL DRIVE INOPERATIVE A TXHAA UNSCHED LANDING O OTHER CLCLIMB 1 WP134544Q 402A0044 DEPARTED OUT OF HNL, BUT COULD NOT RETRACT RIGHT MAIN LANDING GEAR. GREEN DOWN AND LOCKED INDICATION LIGHT REMAINED ILLUMINATED. PILOT NOTIFIED THE TOWER AND RETURNED BACK TO BASE. MAINTENANCE WAS NOTIFIED AND UPON INSPECTION DISCOVERED RIGHT OUTBOARD DRIVE TUBE END BROKEN. FURTHER INSPECTION REVEALED NO OTHER DAMAGE TO PARTS OR AIRFRAME. REPLACED AND FULL RETRACTION TEST CARRIED OUT IAW CESSNA MM SECTION 4-19 THROUGH 4-26 AND AIRCRAFT RETURNED TO SERVICE. (M) 1L72 3O A7CE 20030630000042003063000004NE 2003 6 30 UPS03440287 220030313A7200 ENGINE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE NR 2 OVERHEATED A IPXAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SO01523UP 22381 NR 2 ENGINE TEMPERATURE 1100 DEGREES. NR 2 ENGINE SHUT DOWN, EMERGENCY DECLARED. 2L74 4F4 FRTA20WE E3NE 20030630000242003063000024EU 2003 6 30 DHL2003365009 120030529A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU CABIN MALFUNCTIONED A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01365DH 149 AFTER NR 1 ENGINE START SEVERAL CABIN SMOKE DETECTORS, AND BATTERIES SMOKE LIGHT ILLUMINATED. RAN PACKS TILL SMOKE LIGHTS EXTINGUISHED. GROUND OPS CHECKED OK IAW M/M 26-10-0. 2L72 4F RTA35EU 20030630000422003063000042EU 2003 6 30 AWXA200300618 120030502A5320D5327470400000 PROFILE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR PROFILE FR 59, LBL 660 MM TO RBL 660 MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PROFILE FR 59, LBL 660MM TO RBL 660MM IAW AWA E.R. 26-5341-03142-TB5. 2L72 4F RTA28NM 20030630000442003063000044NM 2003 6 30 AWXA200300620 120030504A5320146N530093 CHANNEL BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR DECK HAT CHANNEL BS 1716, BL 0. MAINTENANCE REMOVED CORRODED HAT CHANNEL BS 1716, BL 0; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-05, PG. 1-2, & 5. 2L72 4F RTA2NM 20030623000042003062300004NM 2003 6 23 MEX2003194 120030528A29101474252 VALVE DOUG MD80 MD83 3023681NM HYD SYSTEM980470FAILED A ASMFO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW23945AS 49643 DURING TRANSIT CHECK, DETECTED HYDRAULIC LEAK AT RIGHT MLG, HYDRAULIC TEST WAS ACCOMPLISHED DETECTING LEAK AT SHUTOFF AND SPOILER DEPRESSURIZATION VALVE. VALVE WAS REPLACED IAW MM 29-10-26, ALL TESTS CORRECT. (M) 2L72 4F RT 20030623001062003062300106NM 2003 6 23 USAASB03064 120030510A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGNECY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU 23594 MAINTENANCE FOUND THE EMERGENCY LIGHTS ABOVE THE AFT SERVICE DOOR, THE AFT GALLEY CENTER EXIT LIGHT AND THE LIGHT AFT OF THE AFT ENTRY DOOR, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030624000262003062400026NM 2003 6 24 HNAA0300027 120030529A335052891 CONTROL PANEL DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT INTERMITTENT A HNAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA07997HA8005 5525 507 CREW REPORTED THAT THE FOLLOWING EMERGENCY LIGHTS FLICKER IN FLIGHT: ROW 4 EXIT LIGHTS, ROW 1 SMALL EXIT SIGN, ROWS 1 & 7 CEILING LIGHT, GALLEY LIGHT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM BUT DID REPLACE THE F/A CONTROL PANEL AND CLEANED THE CONNECTOR BEHIND THE F/A PANEL. 2H72 4T RTA13NM 20030624000372003062400037NM 2003 6 24 CALA0300319 120030602A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND A GOUGE IN FUSELAGE SKIN AT THE FORWARD LOWER CORNER OF THE L2 DOOR, STA 965, S17L. THE GOUGE MEASURED 2 X 1.4 INCH THE AREA WAS REPAIRED IAW ECRA 5330-03257. A DIP WAS ISSUED TO ACCOMPLISH AN HFEC INSPECTION AND GV INSPECTION AT A THRESHOLD OF 60,000 TOTAL AIRFRAME CYCLES AND SUBSEQUENT INTERVALS OF 24,000 CYCLES. 2L72 4F RTA16WE 20030624000502003062400050NM 2003 6 24 CALA0300287 120030606A575365C372631 ARM BOEING737 737524 1384721NM RT WING TE FLAP GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719638 28899 INSPECTION FOUND FAIRING SUPPORT ARM GOUGED AT RIGHT O/B MID FLAP CARRIAGE.REPLACED ARM IAW MM 27-51-34. 2L72 4F RTA16WE 20030624000912003062400091NM 2003 6 24 DLM88030465 120030514A3020759702324 DUCT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27974DL 53242 725638 FOUND ON ARRIVAL DFW NR 2 ENGINE UPPER ENG COWL DAMAGED UPON FURTHER INVESTIGATION FOUND NBR 2 ENG ANTI-ICE DUCT BLOWN C/A RPLCD BOTH SECTIONS OF VSV ANTI-ICE DUCT AND VALVE. LEAKS CHECKS GOOD. 2L72 4F4 FRTA6WE E9NE 20030624001052003062400105WP 2003 6 24 IXXA0300037O 120030525A2133 OUTFLOW VALVE DOUG DC8 DC862 3021970WP CABIN PRESSURE CONTAMINATED A IXXAG O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW11728PL459181066 45918 DURING CRUISE AT FLIGHT LEVEL 28K CABIN ALTITUDE BEGAN TO CLIMB. CREW ELECTED TO DEPLOY PASSENGER O2 MASKS. FLIGHT CONTINUED TO WSAP AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MAINTENANCE CLEANED OUTFLOW VALVE, INSPECTED DUCTING AND OPERATIONALLY CHECKED THE AIRCRAFT PRESSURIZATION SYSTEM. ALL CHECKS INDICATED NORMAL OPERATION. ALL WORK WAS COMPLETED PER APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20030625000402003062500040NM 2003 6 25 AWXA200300594 120030509A5320146N83276 FITTING BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON L-4 DOOR THRESHOLD SUPPORT FITTING AT BS 1675, LBL 68. MAINTENANCE REMOVED L-4 DOOR THRESHOLD SUPPORT FITTING AT BS 1675, LBL 68; FABRICATED A NEW REPLACEMENT THRESHOLD SUPPORT FITTING; INSTALLED REPAIR PART IAW 51-40-05, PG. 5-8. 2L72 4F RTA2NM 20030625000462003062500046EU 2003 6 25 AWXA200300600 120030519A5321D536716100000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 MCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 241FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306. 2L72 4F RTA28NM 20030630000712003063000071EU 2003 6 30 BAQA087537 120030620A6330L633M2010104 MOUNT UROCOPEC135 EC135T1 5620026EU GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03485AE13 0273 GEARBOX MOUNT LEAKING. PART ONLY LASTED 13.0 HOURS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030630000752003063000075SW 2003 6 30 HEEA087837 120030623A243231908001 BATTERY BELL 407 407 1182206SW ALLSN 250C 250C47B GL MASTER BURNED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH 53278 BATTERY CELL BURNED ON CHARGE. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030701000052003070100005SW 2003 7 1 HEEA087859 120030614A6320407040627101 TUBE BELL 407 407 1182206SW MRGB OIL SYS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR GEARBOX OIL TUBE HAS CORROSION FOUND UNDER ADEL CLAMP NOT VISIBLE UNTIL REMOVED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000082003070100008SW 2003 7 1 HEEA087862 120030619A3213407050201115 CROSSTUBE BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW038595X 53267 MLG CROSSTUBE HAS CORROSION DUE TO IMPROPER PROTECTION DURING MANUFACTURING PROCESS NEAR STRAP ASSY. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000092003070100009SW 2003 7 1 HEEA087863 120030611A2510407070728103 HEADREST BELL 407 407 1182206SW COCKPIT OUT OF ADJUST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 HEADREST WILL NOT ADJUST. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000142003070100014SW 2003 7 1 HEEA087868 120030617A3411407075037101 STATIC LINE BELL 407 407 1182206SW PITOT/STATIC CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03491PH 53386 STATIC LINE HAS DEVELOPMENT OF CORROSION DUE TO TREATMENT USED DURING MANUFACTURE PROCESS. REPLACED TUBE. 1G71 3U O H2SW 20030701000392003070100039SW 2003 7 1 HEEA086956 120030603A2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH878 53398 STARTER GEN WILL NOT COME ON LINE. REPAIRED. 1G71 3U O H2SW 20030702000032003070200003NM 2003 7 2 AMTA200300761 120030610A21503989083 VALVE BOEING737 73783N 13844HINM LT A/C PAC MALFUNCTIONED A AMTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL11304TZ 30675 LEFT PACK TRIP LIGHT, WOULD NOT RESET. FOUND ON RECALL. REMOVED AND REPLACED LEFT PACK TCV VALVE PER MM 21-51-10-4. OPS CHECK GOOD. LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030702000142003070200014EU 2003 7 2 SIMA200316403 120030612A21507769106 ACM SAAB SF340 340B 7860101EU ACM BAY INOPERATIVE A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21341SB 340B341 AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMELL OF SMOKE COMING FROM CABIN ENTS. AIRCRAFT RETURNED TO LAX. DECLARED EMERGENCY FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030702000212003070200021NM 2003 7 2 USAASB03075 120030609A27511817387 TRANSMITTER BOEING737 7373B7 1384580NM TE FLAP INOPERATIVE A USAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA19389US 23311 ON APPROACH INTO PIT, CAPTAIN REPORTED THE AIRCRAFT ENCOUNTERED AN ASYMMETRICAL TRAILING EDGE FLAP INDICATION. CREW DECLARED AN EMERGENCY, COMPLIED WITH EMERGENCY CHECKLIST AND EXECUTED A NO FLAPS LANDING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT FLAP POSITION TRANSMITTER INOPERATIVE. REMOVED AND REPLACED RIGHT FLAP POSITION TRANSMITTER PER MM TASK 27-58-12-404-006. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030701000072003070100007SW 2003 7 1 HEEA087861 120030610A3213407050201101 CROSSTUBE BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MLG CROSSTUBE CORRODED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000102003070100010SW 2003 7 1 HEEA087864 120030611A2510407070731101 HEADREST BELL 407 407 1182206SW COCKPIT OUT OF ADJUST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 HEADREST WILL NOT ADJUST. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000172003070100017SW 2003 7 1 HEEA087871 120030615A2822407362013101 PRESSURE SWITCH BELL 407 407 1182206SW ENGINE STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 ENGINE PRESSURE SWITCH STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000232003070100023SW 2003 7 1 HEEA087877 120030614A291070061H000V122A LINE BELL 407 407 1182206SW HYD SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 HYDRAULIC LINE HAS DEVELOPMENT OF CORROSION UNDER SLEEVE DUE TO DISSIMILAR METALS USED DURING MANUFACTURE PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000242003070100024SW 2003 7 1 HEEA087878 120030614A291070061J175W216A LINE BELL 407 407 1182206SW HYD SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 HYDRAULIC LINE HAS DEVELOPMENT OF CORROSION UNDER SLEEVE DUE TO DISSIMILAR METALS USED DURING MANUFACTURE PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000302003070100030EU 2003 7 1 HEEA087882 120030624A280023053192 VALVE BOLKMS105 BO105S 5626006EU FUEL SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 FUEL VALVE INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G72 3U H3EU 20030701000322003070100032EU 2003 7 1 HEEA087884 120030623A2432RG380E40 BATTERY BOLKMS105 BO105S 5626006EU MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381832123 S828 MAIN BATTERY VOLTAGE TOO LOW TO ACTIVATE RELAY. BATTERY WEAK. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H3EU 20030702000022003070200002 2003 7 2 AMTA200300773 420030613A2565 CONTAINER BOEING737 73783N 13844HINM ESCAPE SLIDE LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11319TZ 30643 FOUND DOOR L2 SLIDE CONTAINER LOOSE. SECURED 2L DOOR CONTAINER. OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030702000052003070200005NM 2003 7 2 AMTA200300768 120030612A2560 BATTERY BOEING737 73783N 13844HINM FLASHLIGHT DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11324TZ 32882 EMERGENCY FLASHLIGHT AFT GALLEY INOPERATIVE. REMOVED AND REPLACED BATTERY FOR FLASHLIGHT. (M) 2L72 4F RTA16WE 20030702000382003070200038 2003 7 2 2003F00391 420030603A3441701030031203 COMPUTER CESSNA750 750 2076810CE FLIGHT GUIDANCE FAILED A GTIAO OTHER O OTHER CRCRUISE 1 GL235113 7500013 'A' CHANNEL OF FGC (FLIGHT GUIDANCE COMPUTER) FAILED DURING FLIGHT. 'A' CHANNEL OF FGC TRIPPED OFF LINE. FLIGHT CREW WAS ABLE TO RESET SYSTEM. IMT WAS INTERROGATED AND NO FAULTS WERE FOUND. PERFORMED OPERATIONAL CHECK PER HONEYWELL MM. SYSTEM SELF TEST OK AND NO FAULTS WERE NOTED. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4J RTT00007WI 20030623000942003062300094WP 2003 6 23 GTIA030412 120030519A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND DENT AT FS 218 BETWEEN LONGERON 15 AND 16L, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030623001182003062300118WP 2003 6 23 GTIA030369 120030510A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE BENT A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND L-1 DOOR JAMB HAS SKIN EDGES BENT OUT AND REQUIRES REPAIR. PERFORMED DYE PENETRANT INSPECTION, FOUND CRACK IN SKIN. REMOVED CRACK IN SKIN. FABRICATED 19 TRIP. FABRICATED 21 DOUBLER. INSTALLED NEW REPAIR. (M) 2L72 4F A6WE 20030624000532003062400053NM 2003 6 24 CALA0300290 120030606A534065B578393 FITTING BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0970352 23590 INSPECTION FOUND FITTING O/B OF STRINGER 18R AT STA 1016 CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030624000892003062400089NM 2003 6 24 DL757030463 120030512A5330146N35317 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27609DL 22816 FUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE COMMON TO THE VHF ANTENNA CUTOUT AND THE REINFORCING DOUBLERS AT FS 1470 AND BL 0. THE EXISTING DOUBLERS WERE REMOVED AND THE ANTENNA CUTOUT ENLARGED TO REMOVE THE CORROSION. TWO LARGER ALUMINUM EXTERNAL DOUBLERS WERE INSTALLED TO REPAIR THE AREA PER ER/A 384844-14, REV A. 2L72 4F RTA2NM 20030626000122003062600012NM 2003 6 26 03FDEA00457 120030416A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 STRINGER HAS CORROSION ON STR 29L BS 950E TO BS 1020. REMOVED AND REPLACED STR 29L (KEEL BEAM) IAW FED EX E.A. 7-5310-69472. 2L73 4F RTA3WE 20030626000182003062600018NE 2003 6 26 UPS03840423 220030409A7230 COMPRESSOR DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE NR 3 ENGINE STALLED A IPXAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 SO01705UP 45949 692129 NR 3 ENGINE COMPRESSOR STALL IFSD AT FL350 WHEN POWER WAS REDUCED FROM 85 TO 77 N & CONTINUED TO STALL IN DESCENT WHEN POWER WAS REDUCED BELOW 72N NR 3 ENG SHUTDOWN IN FLIGHT DUE TO CONTINUED COMPRESSOR STALLS IN LEVEL FLIGHT WITHOUT MOVING THROTTLE. REMOVED AND REPLACED NR 3 ENG IAW MAINT TC 9071 6 STEP 1-4(82586) RIGGED VSV & VBV PER TC 9071 7(09326) BAD FROM STOCK MEC PARTS ON ORDER (99610) BOROSCOPED NR 3 HPT AND LPT BOTH LOW AND HIGH PER MM 72-00-00, CKS OK ON ALL STAGES. 2L74 4F4 FRT4A25 E2GL 20030630000192003063000019NM 2003 6 30 AWXA200300604 120030513A5320654541041 WEB BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND AT RIVET HOLE ON INTERNAL FUSELAGE CENTER WEB BS 706, BL 0. MAINTENANCE REMOVED CRACKED AREA OF CENTER WEB BS 706, BL 0; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND FILLER PLATES; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-2, FIG. 1. 2L72 4F RTA16WE 20030630000232003063000023EU 2003 6 30 DHL2003365008 120030529A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU CARGO BAY MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01365DH 149 CABIN SMOKE DETECTORS SEVERAL CAME ON. WITH CARGO CABIN OPEN COOLED LIGHTS EXTINGUISHED OPS CHECKED OK IAW M/M 26-10-0. 2L72 4F RTA35EU 20030630000292003063000029SO 2003 6 30 CHQA00411 120030528A2611 SMOKE DETECTOR EMB 145 EMB145 3260210SO CARGO BAY INOPERATIVE A CHQAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL11834 BAGGAGE SMOKE WARNING LIGHT ILLUMINATED ON FINAL- NO OTHER INDICATION OF FIRE. REMOVED AND REPLACED REAR BAGGAGE SMOKE DETECTOR, OPS CHECK GOOD 2L72 4F RTT00011AT 20030702000512003070200051WP 2003 7 2 GTIA030306 120030415A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FOUND AFT PIT STATION 1174 CORRODED AT SKIN WITH INNER/OUTER DOUBLER, LOWER DOOR JAMB. INNER SKIN FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLERS. INSTALLED 2 DOUBLERS. (M) 2L72 4F A6WE 20030626000132003062600013NM 2003 6 26 03FDEA00455 120030416A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 N00344 CORROSION FWD CARGO BAY INNER SKIN AT B/S 720B+12 RBL 25. REPAIRED EXTERNAL SKIN AT B.S. 720B+12", RBL 25, WL 148 IAW SRM 53-30-3 AND FED EX E.A. 7-5330-54470. 2L73 4F RTA3WE 20030707000282003070700028NM 2003 7 7 AALA20030593 120030522A3397 CONNECTOR BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21363AA 24044 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 12 AB AND 24 HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030707000312003070700031NM 2003 7 7 AALA20030112 120030124A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21941AN 29534 DURING OVERNIGHT MAINTENANCE, LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LT AFT OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030707000432003070700043WP 2003 7 7 AALA20030622 120030531A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21485AA 49678 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GORND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707000502003070700050SO 2003 7 7 AALA20030119 120030127A3350 LIGHT PIPER PA23 PA23250 7102308SO CABIN MISSING A AALAK NONE L NO TEST ININSP/MAINT 1 SW21952AN 272862 MIA - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHTS ON SEAT 14D MISSING. INSTALLED MISSING FORWARD EMERGENCY EXIT LIGHTS ON SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 1L72 3O 1A10 20030707000522003070700052NM 2003 7 7 AALA20030594 120030522A3397 CONNECTOR BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 33H INOPERATIVE. REPLACED EMERGENCY EXIT ILGHT PIN IN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030707000632003070700063NM 2003 7 7 2003UALA00491 120030612A3350 LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29530UA 25043 EXTERIOR EMERGENCY SLIDE LIGHT, INOPERATIVE AT DOOR 4L. RELAMPED. 2L72 4F4 FRTA2NM E17NE 20030707000692003070700069WP 2003 7 7 UPS03840856 120030616A5754 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LT WING LE LOWER RIB IS CRACKED AT XFS 385, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLERS I.A.W. SRM. 57-2-0 FIG.2 2L74 4F4 FRT4A25 E2GL 20030707000882003070700088NM 2003 7 7 2003UALA00480 120030605A5310 SHEAR TIE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 BS 1335, BETWEEN STRINGERS 33R AND 34R, SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2L72 4F4 FRTA1NM E3NE 20030707000902003070700090NM 2003 7 7 DL73S030596 120030628A3350276005 FUSE BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27303DL 23075 EMERGENCY SEAT LIGHTS INOPERATIVE, FROM CLOSET 1R THROUGH ROW 10. RPLCD FUSE AT D1133. CLOSET LIGHTS STILL INOPERATIVE. REPAIRED BROKEN WIRES AT CLOSET BULKHEAD. NOW OPS NORMAL. 1L EMERGENCY SLIDE LIGHT, INOPERATIVE, RELAMPED, CKS GOOD. 2L72 4F RTA16WE 20030707000922003070700092NM 2003 7 7 DL767030598 120030629A5330146T32212 SKIN BOEING767 767232 1385132NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27101DA 22213 SKIN DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS 1263 NEAR STRINGER 37L, DUE TO CONTACT WITH GROUND EQUIPMENT. THE DENT WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER IAW ER/A 385345-14 REV B. 2L72 4F RTA1NM 20030707000992003070700099GL 2003 7 7 6462003F00000 120030601A672028163511 CONTROL CABLE ENSTRMF28 280C 3300505GL LYC O360 HIO360* 41514EA TAIL ROTOR WORN D H90GO OTHER O OTHER NRNOT REPORTED 1 NM09646H 300 1099 BOTH LEFT AND RIGHT TAIL ROTOR CONTROL CABLES SHOW EXCESS WEAR, WHERE THEY PASS THRU THE FAIRLEADS IN THE AFT TALL CONE BULKHEAD. CABLES HAVE BEEN WEARING IN THIS LOCATION CONSTANTLY EVERY 300 TO 400 HOURS. SUGGEST A WIDER CONTACT SURFACE AREA AT THE FAIR LEAD TO REDUCE THE CONCENTRATION OF FRICTION. 1G71 3O3 O H1CE 1E10 20030707001022003070700102NE 2003 7 7 R7S2003F00000 220030602A7320 FUEL CONTROL SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE L R7SLO OTHER O OTHER NRNOT REPORTED 1 SW17747R 3341 FUEL CONTROL UNIT BECOMES OUT OF PHASE WITH THE DIGITAL ENGINE CONTROL UNIT (DECU). REINITIALIZATION IS REQUIRED AT MORE FREQUENT INTEVALS THAN AC CERTIFICATED. MFG ISSUED SERVICE LETTER TO REQUIRE ENGINE SHUTDOWN DURING REFUELING CAUSING REINITIALIZATION. 1G71 3U3 U H9EU E19EU 20030707001052003070700105WP 2003 7 7 UPS03840858 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 791. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001202003070700120WP 2003 7 7 UPS03840866 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 622. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001242003070700124NM 2003 7 7 AWXA200300735 120030612A53156546812193 FLOORBEAM BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM AT BS 994, LBL 13-44, WL 208. MAINTENANCE REMOVED FLOORBEAM BS 994, LBL 13-44, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10, FIG. 2. 2L72 4F4 FRTA16WE E2GL 20030707001262003070700126WP 2003 7 7 CALA0300326 120030621A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733817 49371 INSPECTION FOUND LONGERON 22R CORRODED AND SKIN BULGING AT STA 168. THE LONGERON SECTION WAS REMOVED AND REPLACED IAW SRM 53-02, PAGE 1-2 AND 53-02, PAGE 48-50. 2L72 4F A6WE 20030707001372003070700137NM 2003 7 7 AWXA200300710 120030608A5320654585531 ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK .4375 CRACK WAS FOUND IN RADIUS OF STIFFENER ANGLE AT BS 1004, RBL 47, WL 208. MAINTENANCE REMOVED CRACKED STIFFENER ANGLE AT BS 1004, RBL 47, WL 208; FABRICATED A NEW REPLACEMENT STIFFENER ANGLE PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 610. 2L72 4F RTA16WE 20030707001432003070700143WP 2003 7 7 UPS03840868 120030616A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LEFT WING LE UPPER RIBS ARE CRACKED AT XFS 826.75,XFS 847.5 AND XFS 822.5. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILL TERMINATES CRACKS, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030714000222003071400022NM 2003 7 14 SWAA031394 120030623A3350101114 LENS BOEING737 7373G7 1384595NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT LENS CLOUDED. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030714000912003071400091NM 2003 7 14 SWAA031349 120030616A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 26R, BS 787 AND BS 792. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030714001012003071400101 2003 7 14 CALA0300346 420030627A34512594625902 INDICATOR BOEING737 7373T0 1384582NM RMI/DME INOPERATIVE A CALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW27633052022820042 23356 SMOKE BEGAN COMING FROM THE F/O'S RMI WHILE EN ROUTE TO ATL. THE APPROPRIATE C/B WAS PULLED AND THE SMOKE CEASED. THE AIRCRAFT LANDED SAFELY AT ATL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RMI AT FAULT. THE F/O'S RMI/DME(DUAL UNIT) WAS REMOVED AND REPLACED IAW MM 34-28-81. A SYSTEM TEST WAS PERFORMED AND OPERATION CHECKED NORMAL. ALL C/P'S AND WIRES WERE INSPECTED WITH NO DEFECTS NOTED. 2L72 4F RTA16WE 20030714001032003071400103NM 2003 7 14 CALA0300348 120030630A3350252005 FUSE BOEING737 737524 1384721NM BATTERY PACK BLOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND THE LAST FOUR ROWS OF EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. THE RT AFT BATTERY PACK 5 AMP FUSE WAS REMOVED AND REPLACED IAW MM 33-51-51 AND OPERATION OF THE LIGHTS WAS RESTORED. 2L72 4F RTA16WE 20030714001052003071400105CE 2003 7 14 GLBA2003096 120030629A3230 POWERPACK BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0397UX UE97 GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR HANDLE & POWER PACK. 2L72 4T RTA24CE 20030716000282003071600028NM 2003 7 16 2003F00420 120030314A5320 FLOOR SUPPORT BOEING727 727222 1384073NM FUSELAGE DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 17. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLER AND FILLER AT AFT CARGO FLOOR SUPPORT RBL 17 STATION 950F PLUS 2 INCHES. (M) 2L73 4F A3WE 20030716000912003071600091NM 2003 7 16 USAABB03090 120030613A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND L2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030716001172003071600117 2003 7 16 HEEA088047 420030619A2320N0001553 ANTENNA SKRSKYS76 S76A 8143006NE OUTERLINK INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 OUTERLINK ANTENNA INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030717000382003071700038SW 2003 7 17 HEEA088013 120030619A3213407050102101 CROSSTUBE BELL 407 407 1182206SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MLG CROSSTUBE T-BOLT WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000902003071700090EU 2003 7 17 I05R087967 120030527A6320L623M4003101 LEVER UROCOPEC135 EC135P1 8680990EU M/R GEARBOX WORN E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05551BA 188 MAIN ROTOR GEARBOX HAS A WORN BEARING, REPLACED PARTS 1G72 3U O H88EU 20030718000112003071800011NM 2003 7 18 TSAA0353120 120030506A53306573742 SKIN BOEING737 73725A 1384481NM FUSELAGE DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DENT DISCOVERED ON FUSELAGE SKIN BETWEEN BS 981 AND 996 ALONG STRINGER 14L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED A REPAIR DOUBLER AND TRIPLER. ALODINE, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48 SHEET 46. (M) 2L72 4F RTA16WE 20030718000232003071800023 2003 7 18 WRLA200312 420030603A221037590286 CONTROL PANEL DOUG DC10 DC10 N/A-SDRNM GLARE SHIELD INOPERATIVE A WRLAO OTHER O OTHER NRNOT REPORTED 1 EA27541SA 46541 AUTOPILOTS 1 AND 2 FAILED TO ENGATE RETURNED TO LAX, THE AIRCRAFT RETURNED TO THE DEPARTING STATION LAX FOR REPAIR. ALIGNED INU'S PRESSURIZED HYDRAULICS, YAW UPPER AND LOWER YAW ON, FD'S ON FLAGS IN VIEW PERFORMED TEST TO SYSTEM. OPERATIONAL CHECKED OK REPLACED PITCH CONTROL PANEL. FMA CHECKED OK PER MM 22-10-00. REPLACED PITCH GUIDANCE CONTROL PANEL. (M) 2L73 4F RTA22WE 20030718000292003071800029NM 2003 7 18 USAASB03087 120030618A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU 23595 MAINTENANCE REPORTED THE FLOOR PATH EMERGENCY LIGHT AT SEAT 14C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT FLOOR PATH EMERGENCY LIGHT AT SEAT 14C. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030718000302003071800030EU 2003 7 18 USAASA03063 120030612A36002293B010000 CHECK VALVE AIRBUSA319 A319112 3930323EU NR 2 ENG FAILED A USAAE ENGINE SHUTDOWN RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET DEDESCENT 1 EA19705UW 0929 AT APPROX FL260, DURING DESCENT, NR 2 ENG STALLED & LOST POWER. FELT A VIBRATION AS N1 DECREASED FROM 90 TO 50 PERCENT. THROTTLE PULL BACK STOPPED VIBRATION. COMMAND INDICATED APPROX 40 PERCENT, BUT ENGINE THRUST INDICATED 20 PERCENT. THROTTLE ADVANCED SLOWLY, NO RESPONSE RECEIVED FROM OTHER INDICATIONS. RECEIVED A 'ENG 2 STALL' ECAM MESSAGE. SHUTDOWN NR 2 ENG. FLT CONTINUED & LANDED WITHOUT INCIDENT. TOTAL SINGLE ENG TIME 15 MINS. MX REPLACED NR 2 ENG IP CHECK VALVE. INSPECT NR 2 ENG MAG CHIP DETECT FOR METAL, DUE TO POPPED CHIP DETECTOR. NO METAL FOUND. RESET CHIP DETECTOR. PERFORMED AN ENG BORESCOPE. NO FAULTS FOUND. RAN ENG & OPS CHECKED BLEED SYSTEM. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030718000372003071800037NM 2003 7 18 USAASB03082 120030614A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU 23704 MAINTENANCE REPORTED THE EMERGENCY LIGHTING AT SEAT 12 ABC WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED WIRING ON SEAT 12ABC PER STANDARD WIRING PRACTICES MANUAL 20-10-13. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030630000122003063000012NM 2003 6 30 DHL2003780010 120030529A5270 SWITCH BOEING727 727223 1384074NM PAX DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01780DH 22006 "FWD ENTRY" LIGHT CAME ON DURING TOUCHDOWN ON S/O PANEL AND STAYED ON. REMOVED AND REPLACED FORWARD ENTRY DOOR SWITCH IAW B-M/M 52-70-01. OPS CHECKED GOOD. 2L73 4F A3WE 20030630000432003063000043EU 2003 6 30 AWXA200300619 120030502A5320D53974705000 PROFILE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-60, RBL 686 MM. MAINTENANCE REMOVED DAMAGED AFT CARGO COMPARTMENT CORNER PROFILE FR 59-60, RBL 686MM, FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW AWA E.R. 26-5341-03142-TB5. 2L72 4F RTA28NM 20030630000622003063000062SW 2003 6 30 ALGA087748 120030624A6220406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR ROUGH B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03477AL135 53203 UNIVERSAL BEARING WORN, RATCHETY, ROUGH AND BINDING. REMOVED AND REPLACED. 1G71 3U O H2SW 20030630000642003063000064SW 2003 6 30 ALGA087771 120030620A6210412015300109 BLADE BELL 412 412EP 1182205SW MAIN ROTOR PEELING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW037022F21 36318 PAINT PEELING AND NO HIGH VIZ PAINT. HAS WATER COMING FROM LEADING EDGE AT BLADE ROOT AS MARKED. ORIGINAL BLADE RECEIVED WITH NEW AIRCRAFT SN 36318. WARRANTY REPAIR AND RETURN REQUESTED. 1G72 4U H4SW 20030702000102003070200010NM 2003 7 2 TSAA0352106 120030427A53106546921528 DOOR FRAME BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13816AL 23122 REMOVED DAMAGED INBOARD DORR FRAME AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED AN ANGLE DOUBLER FROM .063 INCH 2024-T3 CLAD MATERIAL. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED ANGLED DOUBLER PER FIGURE B. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 1763, DEVIATION A. (M) 2L72 4F RTA16WE 20030702000202003070200020NM 2003 7 2 USAA030089 120030522A5315 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND FLOORBEAM CORRODED APPROX 6 INCHES BY 1 INCH, FLOORBEAM BETWEEN STATION 344 AND 360 10 INCHES LBBL. MANUFACTURED AND INSTALLED T-CAP PER EA 76223 SRM CHAPTER 51. (M) 2L72 4F RTA16WE 20030707000422003070700042WP 2003 7 7 AALA20030554 120030511A3397 CONNECTOR DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21430AA 49342 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT 21D AND AFT INOPERATIVE. SECURED EMERGENCY EXIT SEAT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707000462003070700046WP 2003 7 7 AALA20030635 120030604A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21470AA 49600 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707000732003070700073EA 2003 7 7 03160667 120030609A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27667BR 7535 DURING MAINTENANCE INSPECTION, THE LT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030707001152003070700115CE 2003 7 7 DXTA200300038 120030601A3260327 LAMP CESSNA500 560CESSNA 2076750CE MLG INDICATOR INOPERATIVE E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07352QS 5600352 DID NOT GET 3 GREEN LIGHTS UPON GEAR EXTENSION. RAN CHECKLIST AND CONFIRMED DOWN AND LOCKED. BLEW EMERGENCY BOTTLE TO COMPLETE CHECKLIST. RT MAIN GEAR DID NOT ILLUMINATE. RELAMPED LANDING GEAR INDICATOR MODULE WITH 4 NEW LAMPS IAW M.M. 33-1-01. 2L72 4F RTA22CE 20030707001162003070700116WP 2003 7 7 DHL2003801078 120030407A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 MAIN CARGO COMPT. NR 2 CARGO TRACK LUGS BETWEEN STA. 1553 AND STA. 1620, WORN, CORRODED. REMOVED NR 2 WORN TRACK SEGMENT IAW SRM 53-2-3 PG. 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED 3 SPLICES IAW SRM 53-2-3 PG.49-50. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG. 49-50. 2L74 4F4 FRT4A25 E2GL 20030707001522003070700152NM 2003 7 7 UPS03540851 120030614A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01423UP 25325 2 AFT OBS SMOKE GOGGLES CRACKED. REMOVED AND REPLACED AFT OBS SMOKE GOGGLES. 2L72 4F RTA2NM 20030707001542003070700154NM 2003 7 7 03FDEA00990 120030627A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D NE CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 WHILE WORKING FOUND AREA OF OIL CANNING ON FWD CARGO DOOR LOWER SKIN 10 INCHES FROM FRONT. REPAIRED FWD CARGO DOOR LOWER SKIN IAW SRM 52-00-3 FIG 3. 2L73 4F4 FRTA3WE E2EA 20030707001552003070700155EU 2003 7 7 03FDEA00989 120030627A5310 FLANGE AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 REPAIR OF SLIGHT GOUGES ON FR 28, INNER FLANGE. FACT 27JUN03 06:44 BFMR WORK COMPLIED WITH ON E.A. 6-5310-70955 FUSELAGE-MAINFRAME REPAIR OF SLIGHT GOUGES ON FR 28, INNER FLANGE. 2L72 4F4 FRTA35EU E13NE 20030707001572003070700157 2003 7 7 AWXA200300720 420030620A2565 GIRT BAR BOEING757 7572S7 1384962NM ESCAPE SLIDE DAMAGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28905AW281592743 23567 FLIGHT CREW REPORTED THE L-4 DOOR SLIDE ARMING HANDLE JAMS, DOOR EVACUATION SLIDE ARMING LEVER DIFFICULT TO POSITION TO ENGAGE POSITION. MAINTENANCE FOUND GIRT BAR FORWARD TANG BROKEN, REMOVED AND REPLACED L-4 DOOR SLIDE ASSEMBLY IAW T/C R1C25602, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030707001592003070700159EU 2003 7 7 AWXA200300722 120030610A5320D5323022720000 ANGLE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK A .2500 INCH CRACK WAS FOUND ON ANGLE AT FR 34, STR 31 LT. MAINTENANCE REMOVED ANGLE AT FR 34, STR 31 LT; PROCURED AND DRILLED NEW ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 28-30, 39-41, FIG. 12 & 18. 2L72 4F RTA28NM 20030707001642003070700164NE 2003 7 7 AWXA200300631 220030601A7323FFG021BH GOVERNOR BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE NR 1 ENGINE INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28913AW416495824 22207 ON CLIMB OUT, NR 1 ENG WAS UNABLE TO MAINTAIN FULL CLIMB POWER, THRUST LEVERS SPLIT APPROX 5 INCHES, NR 2 ENG WAS ABLE TO MAINTAIN FULL CLIMB POWER, NR 1 ENG FULL FWD AGAINST STOPS. CLIMB WAS 1.54, NR 1 ENG INDICATED 1.44, FL 230. ENG LIMITER INOP LIGHT ILLUMINATED WITH EICAS MESSAGE (L ENG LIMIT) DISPLAYED. TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINT REMOVED AND REPLACED THE NR 1 ENG FUEL FLOW GOVERNOR IAW T/C R5M73603, TRIM PERFORMED IAW T/C F5M73601. MAINT ALSO REPLACED NR 1 ENGINE ELEC SPEED AND TEMP LIMITER IAW T/C R2A73601. ENG RUN PERFORMED AT TAKEOFF POWER THRUST LEVERS OPERATED NORMALLY, NO BITE FAULTS. 2L72 4F4 FRTA2NM A12EU 20030707001772003070700177WP 2003 7 7 ARWA20030605 120030605A5310 DOOR FRAME DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAO OTHER O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING MAINTENANCE INSPECTION THE FOLLOWING WAS FOUND, FORWARD ENTRY DOOR FRAME, BOTTOM AFT CORNER HFEC INSPECTION REVEALED .1250 INCH CRACK. ACCOMPLISHED REPAIRS AT FORWARD ENTRY DOOR AFT LOWER CORNER IAW SB 53-075 AND DRAWING NR SR08530021. 2L74 4F 4A25 20030707001822003070700182NM 2003 7 7 AWXA200300749 120030607A53126545409245 WEB BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE PRESSURE PANEL CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK 2 EACH CRACKS WERE FOUND LT WHEEL WELL PRESSURE WEB AT OUTBOARD SIDE OF FORMED CHANNEL BS 664, LBL 32. MAINTENANCE CUTOUT DAMAGE ON LT W/W PRESSURE WEB BS 664, LBL 32; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A -6 STIFFENER, -8 DOUBLER, 2 EACH -9 FILLERS, A -10 FILLER, AND -11 FILLER; INSTALLED REPAIR PARTS IAW SRM 53-60-51, PG. 213-217, FIG. 203. 2L72 4F4 FRTA16WE E2GL 20030708000382003070800038WP 2003 7 8 UPS03840898 120030602A5340 FITTING DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3B 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3, AFT PIT BETWEEN STA 1260 AND STA 1280 STR 31L CRACKED REMOVED CRACKED LONGERON SPLICE IAW SRM 51-1-20D. REC'D, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 5 1-1-20D 2L74 4F4 FRT4A25 1E8 20030630000512003063000051SW 2003 6 30 HEEA087834 120030617A2520206072334105 SEAT BELL 407 407 1182206SW ALLSN 250C 250C47B GL CABIN TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 SEAT TORN. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030701000132003070100013SW 2003 7 1 HEEA087867 120030617A3411407075036101 STATIC LINE BELL 407 407 1182206SW PITOT/STATIC SYSCORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03491PH 53386 STATIC LINE HAS DEVELOPMENT OF CORROSION DUE TO TREATMENT USED DURING MANUFACTURE PROCESS. REPLACED TUBE. 1G71 3U O H2SW 20030529000832003052900083SW 2003 5 29 HEEA086657 120030521A6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 TAIL ROTOR WORN BUSHING. REPAIRED. 1G72 4U H4SW 20030530000082003053000008SW 2003 5 30 HEEA086670 120030522A5302209031816103 COVER BELL 412 412 1182202SW PYLON MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 VERTICAL PYLON COVER DID NOT FIT PROPERLY. IN REPAIR. 1G72 4U H4SW 20030530000142003053000014NE 2003 5 30 HEEA086530 120030522A733312281301 INDICATOR SKRSKYS76 S76A 8143006NE NR 1 FUEL FLOW READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 NR 1 FUEL FLOW INDICATOR READS LOW. 1G72 3U H1NE 20030530000162003053000016NE 2003 5 30 HEEA086532 220030522A73200164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 ENGINE WON'T START - TROUBLESHOOTING. 1G72 3U3 U H1NE E19EU 20030530000262003053000026SW 2003 5 30 HEEA086680 120030522A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 STEP ACTUATION ONLY COMES UP HALF WAY. SENT ACTUATOR TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030530000332003053000033 2003 5 30 HEEA086539 420030522A2312071101215 TRANSCEIVER KFS590B SKRSKYS76 S76A 8143006NE VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 TRANSCEIVER`S TRANSMITION IS GARBLED. IN SHOP REPAIR. 1G72 3U H1NE 20030530000442003053000044SW 2003 5 30 HEEA086689 120030522A6220412010182101 BEARING BELL 412 412 1182202SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214981809 36003 MAIN ROTOR GEARBOX HAS BEARING WEAR. SCRAPPED. 1G72 4U H4SW 20030530000502003053000050GL 2003 5 30 HEEA086547 220030522A726023063372 SEAL CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL GEARBOX LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAG97616 CAE900116 SEAL LEAK ON TEST CELL RUN. INSPECTION OF PART REVEALED SEAL SPLIT. INSTALLED NEW SEAL. 1Q71 3R3 U 2A6 E1GL 20030530000512003053000051NE 2003 5 30 HEEA086548 120030522A2435 COMMUTATOR SKRSKYS76 S76A 8143006NE STARTER GEN DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 1601 760060 RECEIVED FOR COMMUTATOR SPOT. INSPECTED BY ACCESSORY SHOP FOUND UNIT HAD EXCESSIVE BRUSH WEAR. 1G72 3U H1NE 20030530000522003053000052NE 2003 5 30 HEEA086549 120030522A26123020726 FIRE DETECTOR SKRSKYS76 S76A 8143006NE WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW031546G 760076 FIRE DETECTOR WILL NOT TEST. 1G72 3U H1NE 20030617002192003061700219EU 2003 6 17 BAQA086808 120030605A2435524031 STARTER GEN AEROSPSA365 SA365N 8680669EU ENGINE NOISY E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM689 6396 EXCHANGE. STARTER GENERATOR EMITS EXCESSIVE STATIC NOISE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030617002322003061700232EA 2003 6 17 QXEA200300692 120030604A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - FOUND CRACKS IN AFT BULKHEAD WHILE PERFORMING HYDRAULIC FLEX INSTALL ON THE LEFT HAND WEB. REPAIRED IAW REO 670-53-61-034. 2L72 4F RTA21EA 20030617002372003061700237EA 2003 6 17 QXEA200300699 120030531A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - RIGHT HAND WING FIXED LEADING EDGE CHAFED AT OUTBOARD END OF SLAT PANEL 1. REPAIRED IAW CRJ 700 SRM 51-25-01. 2L72 4F RTA21EA 20030617002472003061700247NM 2003 6 17 QXEA200300606 120030508A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - FUSELAGE SKIN IS DENTED AT X297, Z134 LT. REPAIRED IAW DHC-8 400 RD 8/4-53-0552. 2H72 4T RTA13NM 20030618000762003061800076NE 2003 6 18 HEEA087132 120030610A64107610105501042 BLADE SKRSKYS76 S76C 8143008NE TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 HOLE IN BLADE. REPLACED TAIL ROTOR ASSEMBLY. 1G72 3U NCH1NE 20030618001582003061800158SW 2003 6 18 HEEA087506 120030612A3310SM20ACD300A21 RELAY BELL 407 407 1182206SW COCKPIT LIGHT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 COCKPIT LIGHT RELAY WILL NOT COMPLETE CIRCUIT. 1G71 3U O H2SW 20030619000372003061900037SW 2003 6 19 HEEA087381 120030611A5210407070620218 PANEL BELL 407 407 1182206SW DOOR TRIM BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 DOOR TRIM PANEL BROKEN. 1G71 3U O H2SW 20030619000502003061900050GL 2003 6 19 HEEA087200 220030609A75106899080 VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL BLEED AIR SYS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 ANTI ICE SYSTEM INTERMITTENT. REPAIRED. 1G71 3U3 U H2SW E1GL 20030619000642003061900064 2003 6 19 HEEA087209 420030609A3420PA1129 HEADSET BELL 206 206L3 1182108SW COCKPIT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 HEADSET BROKEN. SCRAPPED. 1G71 3U H2SW 20030619000952003061900095SW 2003 6 19 HEEA087419 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030620000062003062000006SW 2003 6 20 HEEA087232 120030610A6240209075325011 INDICATOR BELL 412 412 1182202SW RPM BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 RPM INDICATOR LAMP ASSY WILL NOT REMAIN INTACT. SHOP REPAIR. 1G72 4U H4SW 20030620000162003062000016GL 2003 6 20 HEEA087235 220030610A732125490926 FUEL CONTROL CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C20B 03013GL ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAX STOP ON FUEL CONTROL IS BENT OR CROSS THREADED. SHOP REPAIR. 1Q71 3R3 U 2A6 E4CE 20030620000302003062000030SW 2003 6 20 HEEA087428 120030612A3212407350301101 FLOAT BELL 407 407 1182206SW MLG LEAKING E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03408PH 53228 LEAKING ON 6 MONTH INSPECTION. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030620000322003062000032SW 2003 6 20 HEEA087431 120030612A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03457PH 53147 LEFT FUEL TRANSFER LIGHT DOES NOT ILLUMINATE WHEN THE SWITCH IS TURNED OFF. 1G71 3U O H2SW 20030620000342003062000034SW 2003 6 20 HEEA087433 120030612A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 INTERMITTENT. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030620000352003062000035SW 2003 6 20 HEEA087434 120030612A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 PRESSURE SWITCH INTERMITTENT. 1G71 3U O H2SW 20030620000362003062000036SW 2003 6 20 HEEA087435 120030612A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 LT FUEL TRANSFER CAUTION LIGHT DOES NOT ILLUMINATE WHEN SWITCH IS TURNED ON. 1G71 3U O H2SW 20030620000412003062000041NM 2003 6 20 USAABB03085 120030603A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19630AU 27808 FOUND EXIT IDENTIFIER AT L2 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030620000472003062000047EA 2003 6 20 ASOA03222 120030517A5320601R3111357 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING A C-CHECK IN MCN, THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 IAW SRM 51-42-20. (M) 2L72 4F RTA21EA 20030620000602003062000060EA 2003 6 20 ASOA03230 120030522A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11849AS 7347 FLT 4557 - DURING FINAL APPROACH INTO MLB FROM ATL, A GEAR DISAGREEMENT WARNING MESSAGE WAS RECEIVED. THE CREW COMPLIED WITH THE QRH PROCEDURES, PERFORMED A GO AROUND AND CYCLED THE GEARS. THREE GREEN LIGHTS WERE RECEIVED INDICATING THE GEAR WAS DOWN. EMERGENCY TRUCKS WERE REQUESTED AND THE AIRCRAFT LANDED SAFELY IN MLB. MAINTENANCE REMOVED AND REPLACD THE ELECTRIC MOTOR DRIVEN PUMP. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030701000362003070100036SW 2003 7 1 HEEA086953 120030603A3246206053184122 SKID BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 DISSIMILAR METAL CORROSION AROUND THE FLOAT BAG MOUNT INSERTS. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030702000322003070200032NM 2003 7 2 TSAA0353110 120030423A53116545808 FRAME BOEING737 73725A 1384481NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 FOUND BS 244 FRAME CRACKED AT RIGHT CREASE BEAM. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-40-3, FIGURE 1. (M) 2L72 4F RTA16WE 20030702000332003070200033EA 2003 7 2 A6WA200340090 120030528A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA DOOR SEAL DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 PASSENGER DOOR SEAL STRIKER AT FS 310 IS DAMAGED MIDWAY TOP TO BOTTOM. REPAIRED DAMAGED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-52-11-008 REV B. (M) 2L72 4F RTA21EA 20030702000442003070200044WP 2003 7 2 GTIA030392 120030524A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND L-1 AND R-1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE AND EMERGENCY PASSAGEWAY LIGHTING INOPERATIVE. FOUND CONNECTOR LOOSE AT L1- AND R1 EMERGENCY BATTERY PACK RE-CONNECTED. FOUND BROKEN COPPER TERMINAL GROUND FOR EMERGENCY PASSAGEWAY LIGHTING RE-TERMINATED. (M) 2L72 4F A6WE 20030702000462003070200046CE 2003 7 2 2003F00393 120030602A5280 LATCH CESSNA750 750 2076810CE NLG DOOR UNSECURE A UG8AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL235114 7500017 NOSE DOOR OPEN R, CAS MESSAGE ILLUMINATED AFTER TAKEOFF. INSPECTED RIGHT NOSE DOOR AND FOUND LATCH OPEN. INSPECTED LATCH AND TEE BOLT FOR DEFECTS AND FOUND NONE. RELATCHED DOOR IAW PROCEDURES OUTLINED IN CESSNA MM. CAS MESSAGE EXTINGUISHED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030707000822003070700082 2003 7 7 372PA0031 420030529A22303200940010 TRANSMITTER BOEING737 737306 13844BGNM NR 1 & 2 ENGINESINOPERATIVE A PIDAO OTHER J WARNING INDICATION CLCLIMB 1 SO05372PA 23546 AUTO THROTTLE INOPERATIVE. DISENGAGES ON TAKE OFF. N1 LIMIT FROM FMC INOPERATIVE. N1 WILL NOT SET IN GAUGES. DEFERRED IAW MEL 22-4. 6/7/2003: REPLACED NR 2 ENGINE NR 1 TRANSMITTER IAW MM 77-12-02. RECALLED FLIGHT HISTORY ON ALL NR 1 TACH DISCONNECTS. CHECKED WIRING AND ASSOCIATED CONNECTORS. NO DEFECTS. ALL AUTO THROTTLE BITE TESTS PASS. 2L72 4F RTA16NE 20030707000842003070700084NM 2003 7 7 QXEA200300757 120030621A5720 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 RIGHT INBOARD FLAP SHROUD HAS BROKEN L ANGLE ATTACHING CONNECTOR TO SPAR. REPAIRED IAW HORIZON AIR EA 6-57-158. 2H72 4T RTA13NM 20030707001002003070700100CE 2003 7 7 DYV2003F00000 120030605A325059420011 BELLCRANK CESSNA421 421C 2076016CE NLG STEERING CRACKED E DYVAO OTHER O OTHER NRNOT REPORTED 1 NM07215MP7214 421C1231 COULD BE OVER STEERING ON TUG MOTOR OR EXCESSIVE USE. FOUND ON INSPECTION. 1L72 3O A7CE 20030707001462003070700146WP 2003 7 7 UPS03840871 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE UPPER RIB IS CRACKED AT XS448 STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001782003070700178NM 2003 7 7 AWXA200300745 120030618A53126516300 BULKHEAD BOEING737 7373G7 138447JNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-13 CHECK 3 EACH 1 INCH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT RBL 5, WL 197.75 - 198.75, WL 201 - 201.75, AND RBL 6.25, WL 200.75 - 201.5. MAINTENANCE STOP DRILLED CRACKS ON BS 178 BULKHEAD WEB AT RBL 5, WL 197.75 - 198.75, WL 201 - 201.75, AND RBL 6.25, WL 200.75 - 201; PERFORMED HFEC INSPECTION OF STOP DRILL HOLES TO VERIFY CRACKS ARE CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 210, PG. 275-278. 2L72 4F4 FRTA16WE E2GL 20030707001862003070700186EU 2003 7 7 RAIA00305152 120030528A261351228801 OVERHEAT LOOP JETAIRJETSTMJETSTM4101 1500501EU FALSE INDICATIONA RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03560HK 41076 RIGHT OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 OVERHEAT LOOP. 2L72 4T RTA41NM 20030708000212003070800021NM 2003 7 8 03175403 120030624A3350 LIGHT DORNERDO32 DO328300 NM NR 4 CTR AISLE INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27403FJ 3149 DURING MAINTENANCE INSPECTION, NR 4 CENTER AISLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 4 EMERGENCY CENTER AISLE LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T RTA55NM 20030708000672003070800067NM 2003 7 8 ABXA030197 120030610A5230146T69341 SKIN BOEING767 767281 1385109NM CARGO DOOR GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 CARGO DOOR GOUGE WAS FOUND IN THE PART AT BULK CARGO DOOR INNER SKIN, STA. 1439, WL 131, P/N 146T6334-1, GOUGE ON INNER SKIN. REPAIRED AREA IAW REA MR. 2L72 4F RTA1NM 20030708000692003070800069NM 2003 7 8 ABXA030192 120030610A5410311T14002 STRUT BOEING767 767281 1385109NM MLG GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 2 ENGINE STRUT RIGHT SKIN PANEL NEAR ACCESS DOOR CUT OUT. MAXIMUM DEPTH OF BLENDED OUT REQUIRED TO COMPLETELY REMOVE DAMAGE, 0.025 INCH. REPAIRED AREA IAW REA . 2L72 4F RTA1NM 20030708000772003070800077NM 2003 7 8 AWXA200300648 120030513A53156545410224 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - MAJOR REPAIR - DURING C-15 CHECK 2 EACH 1INCH CRACKS WERE FOUND ON FLOORBEAM STRUCTURE AT AFT END OF AILERON TOWER SHAFT QUADRANT CUTOUT BS 676, LBL 24.5. MAINTENANCE REMOVED ANGLE AND STIFFENER AT BS 676, RBL 24.5; FABRICATED DOUBLERS; INSTALLED REPAIR PARTS IAW SB 737-57-1139 & E.O. 5715-01007. 2L72 4F RTA16WE 20030708000882003070800088NM 2003 7 8 UPS03M40882 120030624A2611 SMOKE DETECTOR DOUG MD11 MD11F 3023600NM CABIN FAILED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01270UP 48576 CLIMBING THROUGH 26000 FT, CABIN SMOKE LEVEL 3 ALERT ILLUMINATED. 1 SENSOR TOP DECK. MECHANIC FOUND NR 3 SENSOR SHOWING FAILED. 0 STOCK MECHANIC DEFERRED IAW MEL REF M2 61900. 2L73 4F RTA22WE 20030708000972003070800097WP 2003 7 8 ARWA20030304 120030312A5230AE245012 SPLICE DOUG DC8 DC863 302198AWP DOOR FRAME CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO DOORS JAMMED, AFT SECTION INTERIOR STA. 280 BETWEEN L-20 AND L-21 WITH 5 INCH CRACK. C/A: REPLACED SIDE BEAM SECTION FROM PRODUCTION SPLICE TO L-21L P/N AE2450-12 IAW SRM 51-1-21. 2L74 4F 4A25 20030630000682003063000068EU 2003 6 30 BAQA087578 120030611A243245043006 BATTERY UROCOPEC135 EC135T1 5620026EU MASTER DISCHARGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH2147 0131 FAULT CODES. BATTERY DISCHARGE LIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030630000892003063000089SW 2003 6 30 HEEA087851 120030624A6320 CASE BELL 407 407 1182206SW CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH A123 53198 TRANSMISSION ASSY HAS CORROSION AT LOWER CASE MATING FLANGE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030630000902003063000090SW 2003 6 30 HEEA087852 120030523A6510407040302113 SHAFT BELL 407 407 1182206SW TAIL ROTOR SCORED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH4479 53147 SCORED SURFACE ON BEARING. REPLACED BEARING 407040339101 DUE TO SCORED SURFACE; SHAFT 407-040-330-101, S/N A2193 DUE TO WORN SHAFT JOURNAL; ADAPTER 406-040-328-103, S/N AFS1172 DUE TO CORROSION ON INNER FLANGE. REPAIRED. 1G71 3U O H2SW 20030707000342003070700034WP 2003 7 7 AALA20030630 120030602A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21244AA 49256 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT L1 DOOR STAYS ON WITH SWITCH IN OFF POSITION. REPLACED EMERGENCY EXIT PATH LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707001422003070700142WP 2003 7 7 UPS03840867 120030616A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LEFT WING OB LE LOWER RIBS ARE CRACKED AT XFS 772.5 AND XFS 822.5. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001802003070700180EU 2003 7 7 AWXA200300747 120030609A5420D5745008320200 ATTACH FITTING AIRBUS320 A320231 3930325EU NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK A .5000 INCH CRACK WAS FOUND ON LT WING LEADING EDGE ACCESS PANEL ATTACH FITTING, OUTBOARD OF NR 1 PYLON. MAINTENANCE REMOVED CRACKED ATTACH FITTING; FABRICATED A NEW REPLACEMENT ATTACH FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6-7. 2L72 4F RTA28NM 20030708000372003070800037WP 2003 7 8 DHL2003801080 120030407A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 MAIN CARGO COMPT. NR 2 TRACK PLUG LUGS AT STA. 219.000 WORN. REMOVED WORN PLUG AT STA. 219.000 IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG AND CHANNEL IAW SRM 53-2-3 PG.17-19. 2L74 4F4 FRT4A25 E2GL 20030708000822003070800082NM 2003 7 8 UPS03440881 120030623A3350 SOCKET BOEING747 747200 1384847NM PWA JT9 JT9D* NE EMERGENCY LIGHT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01528UP 24071 INSPECTION TYPE:PFLT FWD ENTRY DOOR AFT EMERGENCY LIGHT SOCKET ASSY PUSHED THROUGH DOOR FRAME. UNABLE TO RELAMP. SECURED SOCKET ASSY TO LIGHT ASSY TO DOOR FRAME. 2L74 4F4 FRTA20WE E20EA 20030708000902003070800090WP 2003 7 8 UPS03840926 120030608A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, COMPLY WITH MPI P 14035: IAW M REPAIR TO AIRSTART DOOR CUTOUT AT 100Y CYCLES OR 3 MONTHS WHICHEVER COMES FIRST IAW EO DC8-5330-0793, STATION 25 TO 55 LONG. 28L-30L AT DOOR CUTOUT REMOVED EXISTING FILLERS,NDT VERIFIED NO CRACKS AT EXISTING CUTOUTS, FABRICATED AND INSTALLED DOUBLER AND FILLERS IAW DC8-5330-0795, SRO 8530020,AND SRM. 53-2-0 FIG. 13 2L74 4F4 FRT4A25 E2GL 20030708001042003070800104EU 2003 7 8 AWXA200300706 120030501A5740D5725267000390 FITTING AIRBUS320 A320231 3930325EU WING ARCED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK A HOLE WAS FOUND BURNT INTO THE INBOARD EDGE OF NR 2 PYLON TO WING ATTACH FITTING, ARCING CAUSED FROM NR 2 IDG FEEDER CABLE. MAINTENANCE REMOVED SPIGOT FITTING AND FORWARD INBOARD PYLON ATTACH FITTING; FABRICATED A NEW REPLACEMENT INBOARD PYLON ATTACH FITTING; INSTALLED SPIGOT FITTING AND FORWARD INBOARD PYLON ATTACH FITTING IAW AWA ER 26-5716-03163-ES1. 2L72 4F RTA28NM 20030708001152003070800115WP 2003 7 8 GTIA030426 120030519A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 SCRATCH WITH DENT AT FS 800 BETWEEN LONGERONS 5 AND 6R REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20030709000072003070900007WP 2003 7 9 GTIA030435 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 EPC PANEL LOWER FLANGE HAS CORROSION STATION 160 LBL 13-57. UPON REMOVAL OF THE EPC PANEL LOWER FLANGE, THE FLOOR SUPPORT BELOW EPC PANEL IS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030709000092003070900009WP 2003 7 9 AALA20030579 120030518A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21271AA 49293 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS 19-21 INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT WIRE ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000122003070900012NM 2003 7 9 AALA20030571 120030515A2120 ODOR BOEING757 757223 1384957NM CABIN DETECTED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21689AA 25731 AT CRUISE AFTER 1 PLUS 40 FLIGHT TIME CABIN REPORTED ODOR OF ELECTRIC FUMES IN VICINITY OF ROWS 16 THROUGH 18. ODOR INTENSIFIED. UTILITY BUSES DE-ENERGIZED, RIGHT RECIRC FAN OFF, RIGHT PACK OFF AND ODOR SUBSIDED. OPERATED ALL LIGHTING AT FULL INTENSITY, OPERATED POWER PORTS, HAD BOTH UTILITY BUSES ON, OPERATED PACKS, BOTH LEFT AND RIGHT RECIRC FANS ON, RAN ENGINES AND INSPECTED BEHIND CEILING PANELS IN AREA OF ROWS 16 THROUGH 18. NO DISCREPANCY NOTED. UNABLE OT DUPLICTE. (M) 2L72 4F RTA2NM 20030709000172003070900017WP 2003 7 9 AALA20030576 120030516A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21596AA 53286 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 7 MISSING. REPLACED EMERGENCY EXIT LIGHT AT SEAT 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030709000222003070900022WP 2003 7 9 AALA20030524 120030502A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21571AA 49353 DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. SECURED AFT EMERGENCY EXIT DOOR LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030709000272003070900027WP 2003 7 9 AALA20030542 120030507A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21248AA 49259 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000362003070900036WP 2003 7 9 AALA20030550 120030509A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21494AA 49732 DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000372003070900037WP 2003 7 9 AALA20030527 120030502A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGNECY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21224AA 49174 DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHTS COMMON TO EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707001652003070700165NM 2003 7 7 AWXA200300632 120030513A57546546422294 SLAT BOEING737 737277 1384570NM RT WING DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW12397 22645 DURING C-15 CHECK THE NR 5 SLAT OUTBOARD TRAILING EDGE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT IAW AWA T/C R3M27008. 2L72 4F RTA16WE 20030708000232003070800023NM 2003 7 8 03163425 120030612A3350 LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE ROW 4-6 INTERMITTENT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27425FJ 3189 DURING PREFLIGHT INPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT BETWEEN ROWS 4-6, INTERMITTENT. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T4 FRTA55NM E35NE 20030708000922003070800092WP 2003 7 8 UPS03840928 120030623A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, C-PIT DOOR LOWER AFT CORNER, REMOVED EXISTING REPAIR TO ACCOMPLISH AND SATISFY REPAIR REQUIREMENTS OF SRM, FOR DOOR CORNER REPAIRS AT STATION 1220 LONG 33R. NDT VERIFIED NO CRACKS AT EXISTING CUTOUTS, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG. 22. 2L74 4F4 FRT4A25 E2GL 20030708001072003070800107EU 2003 7 8 DHL2003366508 120030522A5311R5397405420692 FRAME AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 CORROSION ON AFT CARGO FORWARD DOOR FRAME, FRAME 59A WHERE FRAME MEETS SILL BEAM AT BOTTOM. REMOVED INTERCOSTAL AND GUSSETS TO GAIN ACCESS,CUT OUT DAMAGED LOWER FRAME SECTION IAW A NR SRM 53-17-00. TRIMMED ,LOCATED ABD DRILLED LOWER FRAME SECTION AND COUPLING IAW A300 SRM 53-17-00. INSTALLED LOWER FRAME SECTION COUPLING,INTERCOSTAL AND GUSSETS IAW A300 SRM 53-17-00 AT FRAMES 59A AFT CARGO. 2L72 4F RTA35EU 20030709000472003070900047WP 2003 7 9 GTIA030443 120030521A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLOORBOARD STATION 1156-1254 LBL 44 STIFFENERS CRACKED AND DEBONDED. REPAIRED FLOORBOARD. (M) 2L72 4F A6WE 20030709000612003070900061EA 2003 7 9 03150307 120030530A3397 WIRE CNDAIRCL600 CL600* EA EMERGENCY LIGHT BROKEN A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27683BR SEVERAL FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT EXIT SIGN AT GALLEY SERVICE DOOR PER CRJ MM 33-51-13, OPS CHECK OK. 2L72 4F RTA21EA 20030709000652003070900065NE 2003 7 9 MWEA030238 220030530A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE VIBRATION A MWEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL31807ME 48033 FLIGHT ATTENDANT REPORTED EXCESSIVE ENGINE VIBRATION. COMPLIED WITH ENGINE VIBRATION TEST, VIBRATION IS WITHIN LIMITS. 2L72 4F4 F A6WE E9NE 20030709000782003070900078EA 2003 7 9 03156632 120030605A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGNECY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030709000832003070900083EU 2003 7 9 MALA030290 120030531A5400 LATCH SAAB SF340 SF340A 7850100EU NACELLE DOOR MALFUNCTIONED A MALAO OTHER O OTHER CRCRUISE 1 GL1599XJ 340A099 DURING FLIGHT 2928 LT ENGINE COWL CAME LOOSE ON FWD CORNER. MAINTENANCE INSPECTED LATCHES FOR CONDITION AND SECURITY. CHECKS OK. INSPECTED HINGES VISUALLY, CHECKS OK. RESECURED LATCH. 2L72 4T RTA52EU 20030709001002003070900100WP 2003 7 9 MWEA030243 120030609A2740920710296 CONTACTOR DOUG DC9 DC981 3022081WP HORZ STAB TRIM INOPERATIVE A MWEAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL31804ME 48030 PRIMARY TRIM INOPERATIVE. REMOVED AND REPLACED NOSE DOWN PRIMARY LONGITUDINAL TRIM CONTACTOR. 2L72 4F A6WE 20030709001032003070900103WP 2003 7 9 ZW0A0305401 120030609A324026088921 BRAKE DOUG DC9 DC982 3022082WP NR 2 WHEEL LOCKED A ZW0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE13957U 49702 WHILE TAXIING TO GATE AFTER NORMAL LANDING AND NORMAL BRAKING THE LEFT INBOARD BRAKE LOCKED UP. PASSENGERS WERE DEPLANED WITH THE AIRCRAFT ON TAXI WAY. THE BRAKE WAS REPLACED ALONG WITH NUMBER 1 AND 2 WHEEL ASSEMBLIES. THE NUMBER 2 WHEEL TRANSDUCER WAS ALSO REPLACED PRECAUTIONARY. CHECK-C 11-23-02 STL. 2L72 4F A6WE 20030709001062003070900106CE 2003 7 9 GLBA2003070 120030601A2130 FILTER BEECH 1900 1900 1154160CE PRES CONTROLLER DIRTY A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03247UE 247UE AIRCRAFT WILL NOT PRESSURIZE. CLEANED PRESSURE CONTROLLER FILTER, OPS CHECK GOOD. 2L72 4T RTA24CE 20030709001192003070900119NM 2003 7 9 371PA0022 120030603A3350 LIGHT BOEING737 737306 13844BGNM CABIN INOPERATIVE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 EMERGENCY FLOOR LIGHT ROW NR 1 ELEMENT BAD. INSTALLED NEW LIGHT ELEMENT. 2L72 4F RTA16NE 20030709001262003070900126EA 2003 7 9 03165633 120030614A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27633BR 7274 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE AT SEAT ROWS 11 AND 12. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030709001332003070900133CE 2003 7 9 GLBA2003082 120030615A351035961G12 OXYGEN MASK BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 NM0394GL 9306 UE94 CAPTS O2 MASK HOSE BURST. REPLACED O2 MASK/ HOSE ASSY. 2L72 4T RTA24CE 20030710000102003071000010EU 2003 7 10 ASOA03240 120030521A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11634AS 370 DURING A C-CHECK IN BNA, THE RIGHT SEAT TRACK BETWEEN FRAMES 39 AND 40 ON THE TOP AND BOTTOM SIDES AROUND THE NUT PLATES WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACK BETWEEN FRAMES 39 AND 40 ON THE TOP AND BOTTOM SIDES AROUND THE NUT PLATES IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20030710000212003071000021EU 2003 7 10 ASOA03234 120030527A3350 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11535AS 464 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT ON THE CABIN DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY LIGHT ON THE CABIN DOOR AND FOUND IT TO FUNCTION PROPERLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030710000222003071000022NM 2003 7 10 TSAA0351148 120030504A532065317875 CHANNEL BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 FOUND CORROSION ON C-CHANNEL UPPER STRUCTURE LOCATED BETWEEN BS 312 AND BS 344 AT WL 208, LBL 57. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 312 AND BS 344. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-40-3. (M) 2L72 4F RTA16WE 20030710000272003071000027 2003 7 10 USAASA03035 420030422A2565 FITTING AIRBUSA319 A319112 3930323EU GIRT BAR DAMAGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19743UW 1277 THE OPERATIONAL TEST OF THE FORWARD GIRT BAR FITTING ON THE L1 DOOR DURING SCHEDULED MAINTENANCE WAS FOUND UNSATISFACTORY. MAINTENANCE REMOVED THE GIRT BAR FITTING, CLEANED ALL OF THE COMPONENTS, AND THEN INSTALLED THE GIRT BAR FITTING BACK INTO ITS ORIGINAL POSITION. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030710000312003071000031WP 2003 7 10 GTIA030447 120030506A5730 PANEL DOUG DC9 DC982 3022082WP RT WING DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 RIGHT WING INNER WING UPPER FORWARD TRAP PANEL DELAMINATING. FITTED AND DRILLED NEW RT WING INNER UPPER FORWARD TRAP PANEL. INSTALLED NEW RT WING INNER UPPER PANEL. (M) 2L72 4F A6WE 20030710000412003071000041 2003 7 10 USAASA03046 420030520A2565D5211044000700RDGIRT BAR AIRBUS320 A320214 3930316EU PAX CABIN FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19121UW 1294 BOS - DURING INSPECTION OF THE AFT RIGHT SLIDE/RAFT GIRT BAR, THE GIRT BAR WAS FOUND TO HAVE IMPROPER CLEARANCE BETWEEN THE DOUBLER/STOP AND THE GIRT BAR. MAINTENANCE REPLACED THE AFT RIGHT SLIDE/RAFT GIRT BAR. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030710000492003071000049NM 2003 7 10 DHL2003747516 120030513A5313 STRINGER BOEING727 727224 1384076NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK, N/R 53605 IN AFT CARGO STR 27L HAS CORROSION FROM BS 950 A TO BS 1070. CUT-OUT DAMAGED SECTION OF STR 27 L FROM STA 950A PLUS 10 TO 1080 IAW B-727 SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER USING BAC1498-145 4 PIECES AT 21 INCHES, TWO EACH AT 19 INCHES AND ONE PIECE 20 INCHES PO 312634. FABRICATED AFT SECTION STRINGERS USING BAC 1498-147 TWO PIECES 20 INCHES AND ONE PIECE 26.5 INCHES LONG, PO 312634. FABRICATED SPLICES USING BAC1498-131 PO 312634 THREE PIECES 10 INCHES, ONE PIECE 14 INCHES, AND 6 PIECES 13 INCHES. ALODINED AND PRIMED ALL PARTS IAW B-727 SRM 51-10-2. INSTALLED ALL REPAIR PARTS IAW B-727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20030710000502003071000050EU 2003 7 10 DHL2003365007 120030528A2170 COALESCER BAG AIRBUS300 A300B4203 3930306EU AIR DIST CONTAMINATED A DHLAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01365DH 149 ON TAXI, SMOKE LIGHT NR 5, 7, 9, & 10 ILLUMINATED ON FLIGHT ENGINEER PANEL, AND SMOKE AT MASTER WARNING PANEL CONTINUED CHIME. APPROPRIATE EMERGENCY CHECK LIST ACCOMPLISHED. REMOVED AND REPLACED NR 7 SMOKE DETECTOR UNIT AS PER M/M 26-11-00. ALSO REMOVED AND REPLACED BOTH ACM COALESCER BAGS AS A PRECAUTION M/M 21-51-16. CHECKED ON GROUND, OPS NORMAL. 2L72 4F RTA35EU 20030710000592003071000059WP 2003 7 10 DHL2003807009 120030530A52701EN32R SWITCH DOUG DC8 DC873F 302199FWP CARGO DOOR FAILED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01807DH 45990 BELLY DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. PRESSURIZATION NORMAL. REMOVED AND REPLACED -A- BELLY DOOR WARNING MICRO SWITCH. OPS CHECKED GOOD IAW 52-31-1. 2L74 4F RT4A25 20030710000632003071000063NM 2003 7 10 DHL2003741004 120030605A3150 WARNING HORN BOEING727 7272Q9 138448MNM ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01741DH 21931 REJECTED TAKEOFF CVG DUE TO TAKEOFF WARNING HORN. TOGW 128.4, KIAS 0-2K, OAT 17 DEGREES C, PA 900, BRAKE ENERGY CHART, NORMAL STAB TRIM FOR T/O SET AT 2.8 PRIOR TO NEXT T/O, RECYCLED STAB TRIM FULL NOSE DOWN AND FULL NOSE UP, THEN BACK TO 2.8. NO FURTHER PROBLEM. OPS CHECKED T/O CONFIGURATION SYSTEM IAW 727 M/M 31-26-00. OPS CHECKED SYSTEM OK. 2L73 4F RTA3WE 20030710000932003071000093SO 2003 7 10 GLBA2003081 120030609A3697 WIRE EMB 120 EMB120ER 3260203SO RT DUCT DAMAGED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03299UX 120299 RIGHT DUCT LEAK LIGHT ILLUM AT 6000 FT. REPAIRED WIRING AT 50345 AND 50319, PERFORMED GROUND RUN CK ON RIGHT PACK, OPS CK AND LEAK CK GOOD. 2L72 4T RTA31SO 20030710000952003071000095WP 2003 7 10 DHL2003802009 120030615A2510 SEAT DOUG DC8 DC873 302199CWP COCKPIT BINDING A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01802DH 46076 CAPTAIN'S SEAT BINDS DURING FORE AND AFT ADJUSTMENT. ADJUSTED CAPTAIN'S FORE AND AFT SEAT LEVER. SEAT OPS GOOD IAW 25-11-1. 2L74 4F RT4A25 20030708001082003070800108EU 2003 7 8 DHL2003366509 120030525A5320 FLOOR SUPPORT AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 FWD PIT FLOOR SUPPORT ANGLE CORRODED ON LOWER SURFACE AT FRAME 35,BETWEEN RBL 39 TO RBL56. C/A: REMOVED EXFOLIATION CORR. IAW A300 SRM 51-10-10, OUT OF LIMITS. FABRICATED NEW REPAIR ANGLES IAW A300 SRM 53-10-10. MAT. ID FOR REPAIR 2024T3 IAW A300 SRM 51-41-0. ALODINED AN PRIMED IAW A300 SRM 51-40-12. ORIGINAL THICKNESS DETERMINED TO BE .047,REMOVED .047,REMAINING .000 IAW A300 SRM 51-10-10,INSTALLED REPIAR IAW A300 SRM 53-10-10. 2L72 4F RTA35EU 20030709000192003070900019WP 2003 7 9 AALA20030581 120030518A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217530 49922 DURING OVERNIGHT MAINTENANCE, COCKPIT AND FORWARD GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED COCKPIT AND FORWARD GALLEY EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000212003070900021WP 2003 7 9 AALA20030519 120030503A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 23-28 INOPERATIVE. REPAIRED EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 23-28 CONNECTION. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000522003070900052WP 2003 7 9 GTIA030438 120030515A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP COCKPIT DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLIGHT COMPARTMENT CENTER FLOOR PANEL AND SUPPORT DAMAGED DELAMINATED. FABRICATED FLOOR PANEL. (M) 2L72 4F A6WE 20030709000572003070900057WP 2003 7 9 GTIA030386 120030530A490038003681 APU DOUG DC9 DC983 3022083WP APU BAY LEAKING A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 ABOUT 2 MIN AFTER SELECTING AIRFOIL ANTI-ICE A BURNING ODOR ENTERED THE CABIN AND WAS DETECTABLE IN THE COCKPIT. SMELL WENT AWAY WHEN AIRFOIL ANTI-ICE WAS TURNED OFF. ODOR WAS APPARENT ALSO WHEN TAIL DE-ICE WAS SELECTED. REMOVED AND REPLACED APU. OPS AND LEAK CHECK GOOD. (M) 2L72 4F RTA6WE 20030709001232003070900123NE 2003 7 9 MALA030302 220030611A7320219333010 HYDROMECH UNIT BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE ENGINE MALFUNCTIONED A MALAE ENGINE SHUTDOWN Y ENGINE STOPPAGE NRNOT REPORTED 1 GL15513XJ E2329 DURING FLIGHT 3465, NR 4 ENGINE WENT TO SUB IDLE-CREW SHUTDOWN ENGINE. NR 4 ENGINE APPEARED TO GO INTO SUB IDLE, ON APPROX 15 MIN FINAL. THE GEN FELL OFF LINE AND ENGINE NR 4 AIR VALVE ANNUNCIATORS CAME ON. THE N2 INDICATED 37 PERCENT AND EGT 433 DEGREES. THIS WAS WITH THE THRUST LEVER ABOVE 50 PERCENT TRAVEL THE ENGINE WAS SHUTDOWN AS A PRECAUTION. MAINTENANCE REPLACED HMU P/N 2-193-330-10, SN/OFF 98AGU722, SN/ON 4AGU275 IAW JOB CARD 7310-502. ALL CHECKS GOOD. RAN ENGINE, ALL OPS CHECK GOOD. 2H74 4F4 FRTA49EU E6NE 20030710000032003071000003EU 2003 7 10 ASOA03243 120030521A5320 SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11634AS 370 DURING A C-CHECK IN BNA, THE FLOOR SUPPORT FLANGE AT FRAME 36 FROM THE LEFT SIDEWALL TO THE RIGHT SIDEWALL ON THE OTP AND BOTTOM SIDES AROUND THE NUT PLATES, AND AT FRAME 40 BETWEEN THE LEFT SEAT TRACK AND THE RIGHT SIDEWALL ON THE TOP AND BOTTOM SIDES AROUND THE NUT PLATES WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT FLANGE AT FRAME 36 FROM THE LEFT SIDEWALL TO THE RIGHT SIDWALL ON THE OTP AND BOTTOM SIDES AROUND THE NUT PLATES AND AT FRAME 40 BETWEEN THE LEFT SEAT TRACK AND THE RIGHT SIDEWALL ON THE TOP AND BOTTOM SIDES AROUND THE NUTPLATES IAW ASA EO 72-53-0139. (M) 2H72 4T RTA53EU 20030710000512003071000051NM 2003 7 10 DHL2003721002 120030522A31509643 WARNING HORN BOEING727 727228 1384083NM APU MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01721DH 19545 DURING APU FIRE TEST EXTERNAL HORN WAS NOT HEARD. WARNING BELL AND LIGHT ON FLIGHT DECK OPERATED NORMALLY. TRANSFERRED TO DMI 13032 MEL REF 26-11-2 CAT C. REFER TO DMI 13032; REMOVED AND REPLACED APU WARNING HORN AND PERFORMED ADJ/TEST PER BMM 26-15-0. OPS CHECKED NORMAL. THIS CLEARS DMI 13032, PLACARD REMOVED. 2L73 4F RTA3WE 20030710000542003071000054WP 2003 7 10 DHL2003873009 120030523A3350313 LAMP DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01873SJ 46091 EMERGENCY EXIT LIGHT DISARM LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT DISARM LIGHT IAW M/M 33-10-1, OPS CHECKED NORMAL. 2L74 4F RT4A25 20030710000702003071000070NM 2003 7 10 DHL2003752002 120030611A2612 FIRE DETECTOR BOEING727 727223 1384074NM APU INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01752DH 22466 APU FIRE TEST INOPERATIVE. DEFERRED TO DMI 13227 MEL 26-11-1. PLACARDS INSTALLED. REF DMI 13227 APU FIRE TEST INOPERATIVE. CLEANED PLUG AT CONTROL BOX. OPS CHECKED GOOD PER M/M 20-11-25/49-00. THIS CLEARS DMI 13227. 2L73 4F A3WE 20030710001042003071000104SO 2003 7 10 C2XA03IA063 120030612A3397487191 CONNECTOR EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2728529 145512 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EXIT SIGN ABOVE SEAT 1A OVERHEAD DOES NOT ILLUMINATE. IAH- MAINTENANCE RESECURED THE FEMALE CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030710001132003071000113EU 2003 7 10 DHL2003362009 120030617A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 1 ENGINE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01362DH 84 ENGINE NR 1 A LOOP CAME ON IN FLIGHT. ABNORMAL PROCEDURE PERFORMED. UNABLE TO DUPLICATE CONDITION ON GROUND. SYSTEM OPS CHECKED GOOD PER M/M 26-12-00. 2L72 4F RTA35EU 20030710001162003071000116NM 2003 7 10 DHL2003748006 120030618A2510 SEAT BOEING727 727225 1384077NM COCKPIT DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01748DH 22440 F/O'S SEAT FORWARD - AFT ADJUSTMENT LEVER DOES NOT FULLY DISENGAGE LOCKING PIN WHEN ADJUSTING POSITION. LUBED AND OPERATED SEVERAL TIMES, OPS CHECKED NORMAL IAW M/M 25-10-41. 2L73 4F A3WE 20030710001222003071000122EA 2003 7 10 03169667 120030618A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27667BR 7535 DURING MAINTENANCE INSPECTION, THE RIGHT FORWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030620000612003062000061EA 2003 6 20 ASOA03229 120030521A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 FLT 4853 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHT STRIP AT ROWS FOUR AND FIVE WAS FOUND TO BE MISSING. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROWS FOUR AND FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030620000622003062000062NM 2003 6 20 USAA030082 120030427A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND FRAME CRACKED .1875 INCH, SMALL CRACK IN FRAME AT RIVET STATION 360 LEFT, BETWEEN 58-59. REMOVED DAMAGED AND INSTALLED DOUBLERS PER TR 53-10-20A. (M) 2L72 4F RTA16WE 20030617003182003061700318NM 2003 6 17 SWAA031270 120030606A52106918187 GUIDE ARM BOEING737 7377H4 1384404NM ENTRY DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 FWD ENTRY DOOR WOULD NOT OPEN. REPAIRED FWD ENTRY UPPER GUIDE ARM PER MM. 2L72 4F RTA16WE 20030618000532003061800053SW 2003 6 18 HEEA087338 120030611A6510 BEARING BELL 407 407 1182206SW BLOWER SHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X PHI0006 53267 BEARING ROUGHNESS. REPLACED SHAFT ASSY. 1G71 3U O H2SW 20030618000832003061800083SW 2003 6 18 HEEA087343 120030611A6510 SHAFT BELL 407 407 1182206SW FLYWHEEL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 FLYWHEEL SHAFT HAS WORN SPLINES. 1G71 3U O H2SW 20030618001812003061800181SW 2003 6 18 HEEA087148 120030609A6710206010470101 BEARING BELL 206 206L3 1182108SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038587X RE1259 51464 BELLCRANK ASSY HAS WORN BEARINGS. REPLACED BEARING (2 EACH) 206010470101 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030619000212003061900021SW 2003 6 19 HEEA087184 120030609A3213206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MLG CROSSTUBE CORROSION. SCRAPPED. 1G71 3U H2SW 20030619000522003061900052SW 2003 6 19 HEEA087388 120030611A5260407301109 STEP BELL 407 407 1182206SW AIR STAIR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 CORROSION BEYOND LIMITS DUE TO IMPROPER PROTECTION DURING MFG PROCESS. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030619000972003061900097SW 2003 6 19 HEEA087421 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030620000532003062000053WP 2003 6 20 GTIA030379 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND FLOOR SUPPORTS FOUR EACH AT STATION 200 RBL 5-57 ARE CORRODED. REMOVED FOUR EACH FLOOR SUPPORTS. FABRICATED NEW FLOOR SUPPORTS. INSTALLED FLOOR SUPPORTS. (M) 2L72 4F A6WE 20030620000702003062000070NM 2003 6 20 USAA030060 120030522A5310 BELTFRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND BELTFRAME CRACKED .1875 INCH, BELTFRAME CRACKED AT STATION 303.9 STRINGER 13L. DOUBLER INSTALLED PER EA 76233. (M) 2L72 4F RTA16WE 20030620000722003062000072NM 2003 6 20 USAA030059 120030425A551065C2526503 FITTING BOEING737 737301 1384611NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 FOUND FITTING CRACKED 1.5 INCHES LONG, FITTING IN HORIZONTAL STABILIZER CENTER SECTION OF RIGHT THRUST BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2L72 4F RTA16WE 20030620000762003062000076NM 2003 6 20 USAA030072 120030516A5300 STRINGER CLIP BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 PIT - FOUND CLIP CRACKED 1 INCH, STATION 360 STRIGNER 11R. INSTALLED FABRICATED CLIP PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20030620000822003062000082EU 2003 6 20 ASOA03225 120030518A21211103P060301 PRESSURE SWITCH AEROSPATR72 ATR72 EU FAN INOPERATIVE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11641AS 387 DURING FINAL APPROACH FROM AVL-ATL, THE FLIGHT ATTENDANT NOTICED A MIST AND UNUSUAL SMELL IN THE CABIN. THE CREW ALSO NOTICED A FAINT OIL ODOR IN THE COCKPIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RT PACK TURBO FAN PRESSURE AND HEAR EXCHANGER OVERTEMP SWITCHES. OPERATIONAL CHECKS GOOD AND AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030620000902003062000090EA 2003 6 20 A6WA200340076 120030525A3510 LINE CNDAIRCL600 CL6002B19 1900309EA OXYGEN MASK FAILED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31440AW 7766 OXYGEN MASK SUPPLY LINE FAILED. COCKPIT 02 SUPPLY DEPLETED. INSTALLED NEW SUPPLY HOSE FROM OBSERVERS OXYGEN STORAGE BOX AND RECHARGED OXYGEN SYTEM TO 1520 PSI. NO FURTHER LEAKS NOTED. (M) 2L72 4F RTA21EA 20030620000922003062000092NM 2003 6 20 USAA030064 120030516A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19584US47825 23743 PIT - FOUND SKIN CRACKED .375 INCH LONG, RIGHT AFT SERVICE DOOR LOWER HINGE CUTOUT STATION 951. (M) 2L72 4F RTA16WE 20030710001352003071000135EU 2003 7 10 MALA030308 120030607A5530 FRAME BAC 146 AVRO146RJ85A1500097EU VERTICAL STAB DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15505XJ E2313 DURING C-CHECK INSPECTION IN CVG, VERTICAL STAB FRAME ASSEMBLY ITEM NR 1 (HC553314HO138-000) AT RIB 20 WAS DAMAGED DUE TO ITS AFT BUSHING WORN AND CAUSING THE FRAME ASSEMBLY TO DROP AND CHAFE ON RUDDER HINGE ASSEMBLY AT RIB 20. REPLACEMENT OF ITEM 1 & 2 (HC5540017-000) WAS PERFORMED TO REPAIR DAMAGED PARTS. NEW BUSHING WAS PRE-INSTALLED ON NEW FRAME ASSEMBLY. TO GAIN ACCESS TO RUDDER HINGE A CUTOUT WAS PERFORMED TO RUDDER SKIN. SEE EO A55025 FOR WORK PERFORMED. REF 409 NR 127753 AND 127755 FOR DETAIL. 2H74 4F RTA49EU 20030710001362003071000136 2003 7 10 MALA030314 420030615A34406228971020 COMPUTER BAC 146 AVRO146RJ85A1500097EU TCAS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15521XJ E2346 EN ROUTE TO CLT, ON FLIGHT NR 3478, WEATHER RADAR STARTED TO PAIN SPIKES THEN GOT PROGRESSIVELY WORSE. THERE WERE THUNDERSTORMS AHEAD. AIR RETURN TO DTW. MAINTENANCE REPLACED TCAS COMPUTER P/N/OFF & ON 622-8971-020, SN/OFF 6770 SN/ON 5613. ALL CHECKS GOOD AT THIS TIME IAW RH-85 MM CHAP 34. 2H74 4F RTA49EU 20030710001372003071000137EU 2003 7 10 MALA030304 120030601A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4K INSPECTION IN CWA, LT CENTER AISLE SEAT TRACK HAS CORROSION. MAINTENANCE REPLACED SEAT TRACK SECTION LBL 18/3 STA 297-352 IAW EO S53060. REF 409 NR 179529 FOR DETAIL. A/C RELEASE DATE 6/6/03. 2L72 4T RTA52EU 20030710001412003071000141EU 2003 7 10 MALA030313 120030614A243023080031 GENERATOR SAAB SF340 340B 7860101EU DC SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15406XJ 340B406 OUTBOUND ON FLIGHT 3273 RIGHT DC GEN FELL OFF LINE. RAN QRH COULD NOT RESET, BUS TIE LIGHT ON, NO C/B POPPED. AIR RETURN TO MSP. MAINTENANCE REPLACED RIGHT DC GEN IAW JOB CARD 243103 SEE CONT ADN 409S 071301 P/N ON/OFF 23080-031, SN/OFF 99951, SN/ON 99294. ALL OPS CHECK GOOD. SEE JOB CARD 243103 FOR DETAIL OF WORK PERFORMED. 2L72 4T RTA52EU 20030710001432003071000143NM 2003 7 10 EIA2003088 120030614A5512 SKIN BOEING747 747SR46 1384816NM HORIZONTAL STAB CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 SEVERAL SMALL AREAS OF SURFACE CORROSION ON LOWER SURFACE LT HORIZONTAL STAB APPROX STA 410 AT STR 7. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER B747 SRM 51-10-01, 51-20-01, 51-30-00, 51-10-02 AND 55-10-03. 2L74 4F RTA20WE 20030710001462003071000146NM 2003 7 10 EIA2003084 120030614A5312 BULKHEAD BOEING747 747SR46 1384816NM RT WING MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 RIGHT WING GEAR W/W BS 1241 CANTED BULKHEAD WEB AND VERTICAL STIFFENER CORRODED RBL 55-75. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-53-143-2. 2L74 4F RTA20WE 20030710001502003071000150NM 2003 7 10 DHL2003742009 120030613A525065703691 LATCH BOEING727 727225 1384077NM COCKPIT DOOR BROKEN A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01742DH 21290 COCKPIT DOOR WON'T OPEN. TRANSFERRED TO DMI 13250 PER MEL 52-14 CAT C PLACARD INSTALLED. REF DMI 13250 COCKPIT DOOR KNOB BROKEN OFF. REMOVED AND REPLACED COCKPIT DOOR IAW M/M 52-00. THIS CLEARS DMI 13250. 2L73 4F A3WE 20030710001512003071000151WP 2003 7 10 MWEA030247 120030620A53475936594527 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 VARIOUS SPOTS OF LIGHT CORROSION ON MID-PIT RIGHT SIDE CARGO TIE DOWN RAIL FROM FRAME STATION 693-788. FABRICATED AND INSTALLED NEW SECTION RAIL. 2L72 4F A6WE 20030711000032003071100003NM 2003 7 11 DHL2003726008 120030604A3260 CONNECTOR BOEING727 727228 1384083NM MLG LOOSE A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01726DH 20409 LEFT GEAR DOOR LIGHT DOES NOT ILLUMINATE ON S/O'S ANNUNCIATOR PANEL DURING GEAR RETRACTION OR EXTENSION. LIGHT TESTS OK. CLEANED AND RE-SECURED CONNECTOR. OPS CHECKED GOOD IAW B727 M/M 32-62. 2L73 4F RTA3WE 20030711000122003071100012NE 2003 7 11 DHL2003755009 220030619A7320 MOISTURE TRAP BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE CONTAMINATED A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO01755DH 21857 700311 DURING T/O AND CLIMB NR 1 EPR AND FUEL FLOW CONTINUALLY FLUCTUATES .04 AND 400 LBS RESPECTIVELY. PERFORMED ABNORMAL PROCEDURES. FLUCTUATIONS STOPPED PRIOR TO PRECAUTIONARY ENGINE SHUT DOWN. FOUND MOISTURE IN THE NR 1 ENGINE FUEL CONTROL MOISTURE TRAP. DRAINED SMALL AMOUNT OF MOISTURE. PERFORMED ENGINE RUN TO WHITE LINE. NO FLUCTUATIONS NOTED REF JRH 7.7. 2L73 4F4 F A3WE E2EA 20030711000142003071100014CE 2003 7 11 GLBA2003088 120030619A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03170GL UE170 CRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED CRACK IAW BEECH SRM. 2L72 4T RTA24CE 20030711000232003071100023SO 2003 7 11 C2XA03SH200 120030623A553214522562403 SKIN EMB 145 EMB145LR 3260212SO VERTICAL STAB LEDAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK THE VERTICAL STABILIZER LEADING EDGE WAS FOUND TO HAVE COMPOSITE DAMAGE. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 51-70-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000252003071100025EU 2003 7 11 DHL2003366506 120030523A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 FWD CABIN FLOOR FR 16 BL 61R SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK AT FR 16 BL 61R IAW A300 SRM 51-40-11. ORIGINAL THICKNESS .200 REMOVED .027 AND .030 FOUND TO BE WITHIN LIMITS IAW A300 SRM 53-10-00. ALODINED AND PRIMED IAW A300 SRM 51-40-11. 2L72 4F RTA35EU 20030711000352003071100035NM 2003 7 11 DHL2003753004 120030614A2420905D9774 VOLT REGULATOR BOEING727 727223 1384074NM NR 1 GENERATOR FAILED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01753DH 22468 REJECTED T/O, 10 KTS, 132,500 GW., 21 C, & 880 PRESS ALT. THIS WAS NOT AN HIGH ENERGY STOP PER MX. MULTI-LIGHT TRIP OFF OF NR 3 GEN WITH BUSS TIE BREAKERS TRIPPING OFF. OVER EXCITATION ON NR 1 GEN. OVER EXCITATION ON NR 2 GSU, UNDER EXCITATION ON NR 3 GEN ONLY NR 3 FIELD TRIPPED. DEFERRED NR 3 GEN PER MEL 24-1, DMI 13257 ASSIGNED BY MX CONTROL, ACCOMPLISHED MX PROCEDURE PER MEL. VERIFIED NORMAL OPERATION NR 1 & 2 GEN FULL LOAD AND NO WATER IN E&E COMPT. MULTI-LIGHT TRIP OFF OF NR 3 GEN, WITH B & B'S TRIPPING OFF OVER EXCITATION ON NR 2 GEN UNDER EXCITATION ON NR 3 GEN. ONLY NR 3 FIELD TRIPPED. REMOVED AND REPLACED NR 3 ENGINE GEN VOLTAGE REGULATOR. SYSTEM OPS CHECKED GOOD ON ENGINE RUN. 2L73 4F A3WE 20030711000412003071100041NM 2003 7 11 219PA0007 120030623A2560 BATTERY PACK BOEING737 737222 1384473NM FLASHLIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05219PA 19956 FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. REPLACED FWD FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT BATTERY PACK PER MM 33-51-21. 2L72 4F A16WE 20030711000482003071100048EU 2003 7 11 DHL2003366518 120030522A5310A53978300 DOOR FRAME AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 CORROSION ON AFT CARGO FWD DOOR FRAME, FR 59A STRINGER 44R (MARKED). REMOVED WEB AND ANGLE PERFORMED ACID TEST IAW ASTM 1A76-97 MAT ID 2024T3 .050 AND ANGLE 2024T3 .083. FAB WEB AND ANGLE IAW A300 SRM 51-10-40, ALODINED AND PRIMED IAW A300 SRM 51-40-12. SENT ANGLE TO HEAT TREATED IAW TIMCO LOAD HT061603-1 TO 2024T4. PAINTED WEB AN ANGLE IAW A300 SRM 51-40-12. INSTALLED WEB AN ANGLE IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20030711000622003071100062WP 2003 7 11 MWEA030253 120030624A534799578712 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 FIRST OFFICER'S AFT OUTBOARD SEAT TRACK IS WORN BEYOND LIMITS. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20030711000642003071100064EA 2003 7 11 03173662 120030622A3620355924400 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DUCT WARNING INSTALLED A VTZAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27662BR 7526 873042 DURING CRUISE FROM EWR AT 16000 FT THE LT 14TH STAGE DUCT WARNING MESSAGE APPEARED. CREW DECLARED EMERGENCY AND SHUT DOWN LT ENGINE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL SWAPPED 14 STAGE FENWAL DUCT WARNING LOOPS AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030711000772003071100077CE 2003 7 11 GLBA2003094 120030625A5712 RIB BEECH 1900 1900D 1154162CE CENTER WING CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03192GL UE192 MAINTENANCE INSPECTION FOUND LT INBOARD KEEL RIB CRACK .625 INCH LONG. PENDING CORRECTIVE ACTION. 2L72 4T RTA24CE 20030711000802003071100080SO 2003 7 11 C2XA03BT068 120030619A32343631101007 SELECTOR EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2748901 145501 CREW REPORTED, LANDING GEAR AURAL WARNING REPEATEDLY WHEN LANDING GEAR RETRACTED. MAINTENANCE REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW EMB 145 MM 27-53-03 AND OPS CHECKED GOOD. GEAR SWING PERFORMED AND OPS CHECKED GOOD REFERENCE EMB145 MM 32-32-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030709000032003070900003WP 2003 7 9 GTIA030431 120030411A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND CABIN LEFT MIDDLE SEAT TRACK CORRODED FS 1309-1214. CUT OUT SEAT TRACK. DRILL AND LOCATED NEW SECTION OF SEAT TRACK. DRILL AND LOCATED SPLICE REPAIR. INSTALLED MID SEAT TRACK FS 1204-1309 AND SPLICE REPAIR. (M) 2L72 4F A6WE 20030709000682003070900068EA 2003 7 9 03152645 120030601A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27645BR 7383 DURING MAINTENANCE INSPECTION, THE LT EXTERIOR OVERWING AND LT FWD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030709000922003070900092SO 2003 7 9 C2XA03CL106 120030606A32347455501 CONTROL HANDLE EMB 135 EMB135ER 3260203SO COCKPIT FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714505 145192 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030710000122003071000012EU 2003 7 10 ASOA03242 120030521A5320 SILL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11634AS 370 DURING A C-CHECK IN BNA, FLOOR SILL PLATE AT THE RIGHT SIDEWALL BETWEEN FRAMES 39 AND 41 ON THE TOP AND BOTTOM SIDES AROUND THE NUT PLATES WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL PLATE AT THE RIGHT SIDEWALL BETWEEN FRAMES 39 AND 41 ON THE TOP AND BOTTOM SIDES AROUND THE NUT PLATES IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20030710000822003071000082EU 2003 7 10 DHL2003366503 120030523A5520 STRUCTURE AIRBUS300 A300B4203 3930306EU ELEVATOR SPLIT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 LT ELEV IS CORRODED/SPLITTING ALONG THE TE. REMOVED 2 EACH BASES AND 5 EACH STATIC ELEMENATORS FOM. REMOVED CORROSION IAW A300-B4-200 SRM 51-40-11, FOUND TO BE OUT OF LIMITS IAW A300 SRM 55-20-00. FABBED DOUBLER IAW A300 SRM 55-20-00. PAA'D DOUBLER IAW TPS-1001-REV E, PRIMED AREA, BONDED REPAIR, ALODINED REPAIR, EDGE SEALED, REINSTALLED 2 EACH BASES AND 5 EACH STATIC ELEMENATORS ALL IAW A300 SRM 55-20-00. PERFORMED ELECTRICAL CHECK IAW AMM 23-60-00. 2L72 4F RTA35EU 20030710001522003071000152WP 2003 7 10 MWEA030248 120030620A5320991555416 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 LITE CORROSION ON TOP OF INTERCOSTAL BETWEEN STATION 769-788 AND BETWEEN LONGERON 27-28 RIGHT. FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F A6WE 20030711001012003071100101NM 2003 7 11 DHL2003746507 120030531A53206518636378 STIFFENER BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH55185 22252 DURING C-CHECK, N/R 54037 RT WHEEL WELL BS 870 AND INTERSECTION TO KEEL BEAM VERTICAL STIFFENER IS CRACKED. REMOVED DAMAGED ANGLE AND INSTALLED NEW P/N 65-18636-378 PO 316031 IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20030711001032003071100103NM 2003 7 11 VNAA0306008 120030613A5270 PROXIMITY SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE GALLEY DOOR FAILED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07472PS 3008 AT 10,000 FEET, THE CREW RECEIVED A GALLEY DOORS LIGHT OPEN AND CLOSING INDICATION. THE AIRCRAFT WOULD NOT PRESSURIZE AND FLIGHT 4158 THEN DIVERTED TO IAD. MAINTENANCE INSPECTED AND CLEANED THE GALLEY DOOR PROXY SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030711001082003071100108NM 2003 7 11 VNAA0306011 120030622A2420 GENERATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RH FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07425JS 3037 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. THE CREW RESET THE SYSTEM AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030711001172003071100117WP 2003 7 11 MWEA030257 120030627A5320991199219 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 CRACK ON ANGLE SUPPORT BRACKET AT RIGHT SIDE AT STATION 1488 JUST AFT OF CANTED FRAME STATION 1485. FABRICATED AND INSTALLED ANGLE. 2L72 4F A6WE 20030623000022003062300002NM 2003 6 23 USAASB03071 120030531A3260189929 SENSOR BOEING737 737401 1384701NM RT MLG WW MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19406US 23876 AFTER TAKEOFF FROM CLT, CREW WAS UNABLE TO RETRACT THE LANDING GEAR AS GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. QUICK REFERENCE HANDBOOK PROCEDURES WERE FOLLOWED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE LANDING GEAR AIR SAFETY SENSOR S106 OPEN. REMOVED AND REPLACED AIR SAFETY SENSOR S106 PER MM 32-09-01. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030623000072003062300007EA 2003 6 23 ASOA03216 120030517A5315601R3111357 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING HANGAR MAINTENANCE IN SHV, THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR BY STOP DRILLING THE ENDS OF THE CRACKS OF THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 IAW ASA EO 600-53-0100. (M) 2L72 4F RTA21EA 20030623000132003062300013NM 2003 6 23 AMTA200300657 120030516A3350 STRIP BOEING737 73783N 13844HINM CABIN DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11321TZ 28249 THE FLOOR EGRESS IN FRONT OF THE AFT RIGHT LAV IS DISCOLORED. REMOVED AND REPLACED DAMAGED SECTION OF PHOTOLUMINESCENT STRIP REF MM 33-51-15-2. (M) 2L72 4F RTA16WE 20030623000182003062300018NM 2003 6 23 USAA030066 120030516A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US46845 23232 PIT - FOUND SKIN CRACKED .375 INCH, INNER SKIN, LOWER FORWARD CORNER. DOUBLER INSTALLED PER EA 74690. (M) 2L72 4F RTA16WE 20030623000422003062300042WP 2003 6 23 GTIA030351 120030514A7120 ISOLATOR DOUG DC9 DC982 3022082WP NACELLE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - RIGHT AFT VIBRATION ISOLATOR CAD PLATING CORRODED. REMOVED RIGHT AFT VIBRATION ISOLATOR. INSTALLED RIGHT AFT VIBRATION ISOLATOR. (M) 2L72 4F A6WE 20030623000472003062300047WP 2003 6 23 GTIA030337 120030414A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FOUND MID CARGO FS 690 STATION STRINGER 30-29L SKIN CORRODED. AFTER FURTHER EVALUATION, MORE DAMAGE FOUND ON EXTERNAL SKIN. FABRICATED EXT DOUBLER. FABRICATED INT DOUBLER. INSTALLED REPAIR DOUBLERS. (M) 2L72 4F A6WE 20030623000512003062300051WP 2003 6 23 GTIA030359 120030506A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND MID CARGO LOWER DOOR JAMB BEAM CORRODED. REMOVED MID CARGO LOWER DOOR JAMB BEAM. LOCATE AND DRILLED NEW JAMB BEAM. INSTALLED NEW JAMB BEAM IN MID CARGO. (M) 2L72 4F A6WE 20030623000582003062300058WP 2003 6 23 GTIA030362 120030509A7120K22199SA31 ISOLATOR DOUG DC9 DC982 3022082WP NACELLE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND LOWER RIGHT FORWARD VIBRATION ISOLATOR ALIGNMENT MARKS BEYOND LIMITS. REMOVED RIGHT FORWARD LOWER VIBRATION ISOLATOR. INSTALLED RIGHT FORWARD LOWER VIBRATION ISOLATOR. (M) 2L72 4F A6WE 20030623000642003062300064 2003 6 23 COEA0301730 420030417A8300GD202 DRIVE SHAFT FOKKERF27 F27MK600 4990706EU LT GEARBOX FAILED A COEAO OTHER O OTHER APAPPROACH 1 NM13730FE 10386 NR 1 ENGINE ACCESSORY GEARBOX DRIVESHAFT FAILED DURING AIRCRAFT APPROACH TO SEA. FLIGHT CREW PERFORMED PRECAUTIONARY ENGINE IN FLIGHT SHUT DOWN AND LANDED AT SEA WITHOUT FURTHER INCIDENT. ENGINE NACELLE AND FIREWALL SUSTAINED SUBSTANTIAL DAMAGE. ENGINE, ACCESSORY GEARBOX, ACCESSORY GEARBOX DRIVE SHAFT REPLACED. DAMAGED STRUCTURE REPAIRED. ACCESSORY GEARBOX DRIVESHAFT SENT TO NTSB LAB. (M) 2H72 4T A817 20030623000722003062300072CE 2003 6 23 2003F00382 120030512A712012991004717 TRUSS BEECH 1900 1900D 1154162CE RIGHT ENGINE CRACKED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1953545 UE185 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT ENGINE TRUSS BRACKETS FOR COWLING CRACKS AT EXISTING WELD, LEFT UPPER, LEFT LOWER, RIGHT UPPER BRACKETS. REMOVED ENGINE TRUSS AND REPAIRED IAW FAA APPROVED DATA CONTAINED IN RAYTHEON KIT 129-9017, STEPS 17 THROUGH 22. (M) 2L72 4T RTA24CE 20030623000812003062300081 2003 6 23 USAASA03043 420030517A2565D5211044000600RDGIRT BAR AIRBUS320 A320214 3930316EU ESCAPE SLIDE FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19120US 1286 WHILE ACCOMPLISHING THE OPERATIONAL TEST OF THE AFT LEFT PASSENGER DOOR SLIDE, THE GIRT BAR FAILED TO STAY ENGAGED IN THE FLOOR FITTINGS OF THE AIRCRAFT. THE FAILURE ALLOWED THE SLIDE TO DETACH FROM THE AIRCRAFT. THE SLIDE CONTINUED TO INFLATE AFTER IT LANDED ON THE GROUND. MAINTENANCE REPLACED THE GIRT BAR ASSEMBLY WHEN THE NEW SLIDE WAS INSTALLED. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030623000842003062300084NE 2003 6 23 USAABA03017 220030526A73208162004026 EEC AIRBUS330 A330323 3930335EU PWA 4168 PW4168 NE LEFT ENGINE MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19677UW 0380 PHL - FLT 196 - EN ROUTE, CREW RECEIVED THE ECAM WARNING 'ENG 1 FADEC A FAULT.' FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE EEC. (M) 2L72 4F4 FRTA46NM E36NE 20030623000862003062300086EU 2003 6 23 USAABA03015 120030519A3350 LIGHT AIRBUS330 A330323 3930335EU CABIN MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 FCO - EMERGENCY EXIT LIGHTS OVER DOORS R3 AND L3 AND OVERHEAD EXIT LIGHTS ILLUMINATED DURING FILGHT AND STAYED ON. MAINTENANCE PERFORMED THE EMERGENCY LIGHTS TEST. NO FAULTS FOUND. (M) 2L72 4F RTA46NM 20030623000892003062300089WP 2003 6 23 GTIA030413 120030519A5330 SKIN DOUG DC9 DC981 3022081WP FS DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND DENT AT FS 350 BETWEEN LONGERONS 26 AND 27R. DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DUOBLER. (M) 2L72 4F A6WE 20030618001262003061800126EA 2003 6 18 COMA0360259 120030604A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01916CA23469 7014 DURING COMPLIANCE OF TASK 002-53-160-610, THREE CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL 9.0 AND RBL 9.0. THE CRACKS RANGE FROM 2.625 TO 3.125 INCH IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, DATED 8-13-2002, AND REO 601R-53-41-160, DATED 6-2-2003. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20030714000142003071400014WP 2003 7 14 DHL2003801050 120030621A3260H2024B SWITCH DOUG DC8 DC873F 302199FWP MLG MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01801DH 46033 DOORS NOT LATCHED AND LEFT AND RIGHT DOOR UNSAFE LIGHTS REMAIN ILLUMINATED AFTER DEPARTURE. FOLLOWED DOOR NOT LATCHED LIGHT ILLUMINATED PROCEDURE. LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED LEFT AND RIGHT MAIN GEAR DOOR SWITCHES AND LUBED DOOR ROLLERS. OPS CHECKED GOOD PER 32-31-4. OK FOR SERVICE. 2L74 4F RT4A25 20030714000312003071400031 2003 7 14 SWAA031403 420030623A2565 INDICATOR BOEING737 7372H4 138448CNM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030714000322003071400032NM 2003 7 14 SWAA031404 120030624A532065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) BS 663 AT STR 10R, AND BS 633 AT STR 10L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030714000672003071400067NM 2003 7 14 SWAA031369 120030619A56105893543130 WINDOW BOEING737 7373H4 1384600NM COCKPIT DELAMINATED A SWAAO OTHER O OTHER CRCRUISE 1 SW29398SW 27692 R1 WINDOW DELAMINATED AND ARCING IN FLIGHT. REMOVED AND REPLACED R1 WINDOW AND R1 WINDOW HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20030714000862003071400086NM 2003 7 14 SWAA031344 120030614A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR 8L AND STR 9L, BS 727E, BS 807 AND BS 847. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030714001092003071400109EU 2003 7 14 MALA030324 120030627A2730 SWITCH SAAB SF340 SF340A 7850100EU ELEVATOR MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL1599XJ 340A099 DURING FLIGHT 3372, PUSHER SYSTEM DISARM WARNING LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE RESET CIRCUIT BREAKER L-4 (PUSHER DISARM), PERFORMED OPS CHECK OF AOA AND PUSHER DISARM SWITCHES PER TASK 273503. ALL SYSTEMS CHECKED GOOD. BREAKERS STAYED RESET. OK FOR SERVICE. AOA TASK 273504. 2L72 4T RTA52EU 20030714001272003071400127WP 2003 7 14 DHL2003801082 120030701A3297 TERMINAL DOUG DC8 DC873F 302199FWP MLG LOOSE A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 AFTER GEAR RETRACTION, RED GEAR LIGHT WAS ILLUMINATED. LIGHT EXTINGUISHED AFTER UP LATCH CHECK, AND WIGGLING THE GEAR HANDLE (GEAR NOT LATCHED LIGHT). TIGHTENED LOOSE TERMINAL ON GEAR NOT LATCHED LIGHT SOCKET. TEST GOOD PER M/M 32-60-0. 2L74 4F RT4A25 20030709000502003070900050WP 2003 7 9 GTIA030436 120030514A5320 INTERCOSTAL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND AFT PIT INTERCOSTAL CRACKED AT FS 1309-1320 LONGERON 28R. REMOVED INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. (M) 2L72 4F A6WE 20030709000622003070900062NE 2003 7 9 03148426 220030528A7230 BLADE DORNERDO32 DO328300 NM PWA 306 PW306B NE COMPRESSOR SEPARATED A VTZAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA27426FJ DURING CLIMB, THE CREW REPORTED A RT ENGINE ITT EXCEEDANCE. THE FLIGHT RETURNED TO RDU AND LANDED WITHOUT INCIDENT. FOUND HPT NR 1 BLADE SEPARATION. MAINTENANCE PERSONNEL REMOVED AND REPLACED RT ENGINE. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RELEASE FOR SERVICE. (TT SINCE SHOP VISIT 449.0) 2H72 4T4 FRTA55NM E35NE 20030709000722003070900072CE 2003 7 9 GLBA2003074 120030602A7712 INDICATOR BEECH 1900 1900D 1154162CE TORQUE STUCK A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03118GL UE118 LEFT TORQUE GAUGE STICKS AT 500 LBS. REMOVED AND REPLACED TORQUE INDICATOR. 2L72 4T RTA24CE 20030709000862003070900086EA 2003 7 9 03159705 120030608A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTS FROM SEAT ROW 2 TO 5 WERE FOUND TO BE DIM. MAINTENANCE PERSONNEL CLEANED THE CONNECTOR FOR THE LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030710000652003071000065NM 2003 7 10 DHL2003747517 120030513A7160 INTAKE DUCT BOEING727 727224 1384076NM NR 2 ENGINE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK, N/R 53639 EMP STA 1303 WEB ABOVE NR 2 ENGINE INTAKE DUCT IS CRACKED, LOWER RT CORNER. REMOVED FASTENERS FOR ACCESS PER B-727 SRM 51-30-2. STOP DRILL AT WEB STA 1303 PER SERVICE BULLETIN 727-53-0094, REV 3 HFEC PER 727 NDT PT6-51-00-00 FIG 23. CRACK ENDS IN STOP HOLE. RE-INSTALLED FASTENERS IAW B-727 SRM 51-30-2. DHL INSPECTION NOTE: A RFES WAS REQUIRED AND WRITTEN TO AF. ENGINE TO CREATE AN MSI FOR 2400 CYCLE RE-INSPECTION. 2L73 4F A3WE 20030710000672003071000067NM 2003 7 10 DHL2003745012 120030606A3260 PROXIMITY SENSOR BOEING727 727224 1384076NM RT MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 WHEN SELECTING GEAR LEVER TO OFF, AFTER GEAR RETRACTION, RIGHT MAIN GEAR DOOR LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES. INSPECTED RIGHT GEAR DOOR SWITCH AND WIRING. ADJUSTED DOOR SWITCH AND TESTED PER B727 M/M 32-62-11. NO DEFECTS NOTED. 2L73 4F A3WE 20030710001082003071000108SO 2003 7 10 C2XA03SH189 120030618A3350110049 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 811XW WAS FOUND TO BE NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 BATTERY POWER SUPPLY CHARGER IAW EMB 145 AMM 33-50-04-801-A. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030710001242003071000124SO 2003 7 10 C2XA03CL113 120030618A335078241 INVERTER EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716525 145403 CLE FLIGHT NR 2153, THE CREW REPORTED THE EXIT SIGN OVER THE SERVICE DOOR NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE NR 2 INVERTER AND EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. EXIT SIGN P/N 7444-1. 2L72 4F RTT00011AT 20030702000292003070200029NM 2003 7 2 TSAA0333112 120030501A33509221009 BATTERY PACK BOEING737 7372S2C 138448GNM PAX CABIN INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13806AL 21927 REPLACED RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO FAILING TEST. OPS CHECK OK. AIRCAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030702000312003070200031NM 2003 7 2 TSAA0333109 120030426A335086210066 BATTERY PACK BOEING737 737230 1384401NM PAX CABIN DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 REPLACED AFT ENTRY IDENTICAL POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030623001002003062300100EU 2003 6 23 USAASA03048 120030523A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT WILL NOT TEST A USAAK NONE L NO TEST ININSP/MAINT 1 EA19753US 1326 DURING EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE AFT EPSU BATTERIES. (M) 2L72 4F RTA28NM 20030623001152003062300115EU 2003 6 23 A6WA200360027 120030512A5512 PANEL BAC 146 146300A 1500267EU STABILIZER CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 CHAFE DAMAGE TO LEFT STABILIZER PANEL 275CL. MAINTENANCE BLENDED AND POLISHED DAMAGE AREA IAW BAE FAX BARA/AVR/3037/03-DC. (M) 2H74 4F RTA49EU 20030624000012003062400001WP 2003 6 24 GTIA030371 120030519A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP COCKPIT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - HIDDEN DAMAGE COCKPIT FLIGHT OFFICERS FLOOR PANEL DIRECTLY UNDER SEAT CORRODED. FABRICATED NEW PANEL. (M) 2L72 4F A6WE 20030625000042003062500004NM 2003 6 25 03147414 120030527A3350F13T5WW LAMP DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27414FJ 3169 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACKS LIGHTS AT SEAT ROWS 8 AND 9 WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030625000072003062500007NM 2003 6 25 IU62003F00021 120030515A3240511531 HOUSING BOEING737 737* NM BRAKE VALVE CRACKED B IU6RO OTHER K FLUID LOSS NRNOT REPORTED 1 NM01 HOUSING CRACKED IN BOLT HOLE. PROBABLE CAUSE: FATIGUE / WEAK HOUSING. 2L72 4F RTA16WE 20030625000122003062500012WP 2003 6 25 03FDEA00803 120030524A5320AJC702817 CLIP DOUG DC10 DC1010 3022110WP ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 AFT FUSELAGE PENTHOUSE CANTED FRAME AT Y=2029.88. HAS REPAIRS, SHOULD BE REPLACED PER E.O.8-5310-7-5000.PT 1. CLOSING ACTION ON 02/22/03. REMOVED AND REPLACED CLIP IAW E.O.8-5310-7-5000.PT1 AND SRM 51-31/01. 2L73 4F A22WE 20030625000442003062500044EU 2003 6 25 AWXA200300598 120030521A33971703302 TERMINAL AIRBUS320 A320231 3930325EU EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 DURING C-01 CHECK THE EMERGENCY EXIT LIGHT BETWEEN THE L/H OVER-WING HATCHES WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED A BROKEN EMERGENCY EXIT LIGHT TERMINAL LUG BETWEEN L/H OVER-WING EXITS IAW A320 ESPM 20-48-14, PG. 1-3, OPERATIONAL CHECK WAS GOOD IAW AMM SUBTASK 33-51-00-710-051. 2L72 4F RTA28NM 20030625000562003062500056NM 2003 6 25 03FDEA00752 120030514A5753NRC6066 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING, O/B FLAP O/B HINGE (FLAP HINGE SIDE) AFT ATTACHING POINT, AFT BOLT HOLE CORRODED. O/B FLAP O/B HINGE (FLAP HINGE SIDE) AFT ATTACHING POINT AFT BOLT HOLE REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68412 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT COOROSION. 2L73 4F RTA22WE 20030626000072003062600007CE 2003 6 26 GLBA2003048 120030416A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS LACK OF LUBE A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03249GL UE249 FLAPS WILL NOT RETRACT, CLEANED LUBED & OPS CHK FLAP SAFETY SWITCHES OPS CHECKS GOOD. 2L72 4T RTA24CE 20030626000092003062600009NM 2003 6 26 UPS03640444 120030420A7920RR37100D PUMP BOEING767 767300 1385204NM LT ENG SCAV OIL LEAKING A IPXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO01319UP 27758 INSPECTION TYPE:ETOP LEFT ENGINE OIL QTY DECREASE IN FLIGHT, DIVERSION TO CTS EMERGENCY DECLARED. FOUND OIL LEAKING FROM LT ENGINE SCAV OIL PUMP OUTLET PORT TO THE OIL PRESS TRANSMITTER, R/R LUB AND SCAV OIL PUMP ASSY AND REDUCER-TUBE AND OIL LEAK CHECK OK WITH ENG RUN PER MM79-21--03 2L72 4F RTA1NM 20030626000172003062600017EU 2003 6 26 CX7A194J36 120030404A26131734362450 SENSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE TAILPIPE CONTAMINATED A CX7AEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL03314CE 340B335 RT TAILPIPE HOT LIGHT ILLUMINATED IN FLIGHT. 2L72 4T4 TRTA52EU E8NE 20030630000282003063000028WP 2003 6 30 03FDEA00820 120030527A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 MAIN CARGO CORROSION FOUND AT BS 1371, LBL 85 AT REAR SPAR TOP OF FUEL TANK WILL NEED TO HAVE FASTENERS REMOVED. R/R SKIN PER E.A. 8-5710-69306. 2L73 4F A22WE 20030701000332003070100033SW 2003 7 1 HEEA086951 120030603A3211206052105035 STRAP BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 STRAP ASSY CORRODED, UNABLE TO DETECT CORROSION UNTIL PAINT REMOVAL. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030702000172003070200017NM 2003 7 2 AMTA200300748 120030503A5753 SKIN BOEING737 73783N 13844HINM TE FLAP DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11316TZ 32609 RIGHT WING INBOARD TRAILING EDGE MAIN FLAP SKIN DENTED 8 INCHES FROM EDGE. REPAIRED SKIN IAW SRM 51-70-10-2-2. (M) 2L72 4F RTA16WE 20030702000522003070200052NM 2003 7 2 AMTA200300733 120030518A2530 OVEN BOEING737 73783N 13844HINM GALLEY MALFUNCTIONED A AMTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11302TZ 32576 OVEN GLIDES IN FORWARD AND AFT GALLEY CREATE BILLOWING CLOUDS OF SOOT AND BLACK SMOKE WHEN COOKING ENTREE'S, AS REPORTED BY SR F/A. CATERING REMOVED AND REPLACED INSERTS AND GUIDES. OVENS IN FORWARD AND AFT GALLEY, OP CHECKED GOOD AMM 25-00-00. (M) 2L72 4F RTA16WE 20030702000542003070200054EU 2003 7 2 USAASA03058 120030601A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19756US 1340 THE AIRCRAFT CABIN RIGHT SIDE EMERGENCY LIGHTS WERE FOUND BLINKING. MAINTENANCE REPLCD THE MID CABIN RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030702000932003070200093CE 2003 7 2 AUS20030533 120030522A28204528203431001 LINE LEAR 45 45LEAR 5170805CE FUEL SYSTEM DAMAGED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) LOW PRESSURE FUEL SUPPLY LINE LEAKING FROM AREA APPROXIMATELY MIDWAY BETWEEN TWO END FITTINGS. LINE IS IN CONTACT WITH TWO FLEXIBLE TOILET SERVICING LINES IN THIS AREA. SUSPECT TUBE CORRODED THROUGH. INVESTIGATION BY MANUFACTURER FOUND THE DAMAGE TO BE CAUSED BY ELECTRICAL ARCING FROM THE TOILET SERVICE PANEL SWITCH. 2L72 4F RTT00008WI 20030716000722003071600072SO 2003 7 16 SIMA200313903 120030513A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21808AE 145519 DURING AN MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND EXTERNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-21-10 FIG 201. (M) 2L72 4F RTT00011AT 20030624000982003062400098NM 2003 6 24 DL76G030472 120030518A33501000677 LIGHT BOEING767 7673P6 1385105NM COCKPIT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27156DL 25354 COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY. 2L72 4F RTA1NM 20030707000292003070700029NM 2003 7 7 AALA20030627 120030529A2420GEN5103 GENERATOR BOEING767 767223 1385123NM RT ENGINE FAILED A AALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SW21320AA 22321 DRIVE LIGHT CAME ON WITH ASSOCIATED EICAS MESSAGE DISCONNECTED AS PER CHECK LIST. EICAS MESSAGE DISTINGUISHED BITE MAINTENANCE PANEL FOR FAULTS. VISUALLY INSPECTED GEN NO FAULTS NOTED ON THE GROUND. RAN ENGINE FOUND IDG TO BE LEAKING. DEFERRED RIGHT IDG INOPERATIVE PER MEL ACCOMPLISHED MPM 24-1 ENT IN MIC SHEET. REMOVED AND REPLACED NR 2 ENGINE IDG. LEAK AND OPS CHECK GOOD. REMOVED PLACARD CLEARED MIC SHEET. (M) 2L72 4F RTA1NM 20030707000382003070700038NM 2003 7 7 AALA20030591 120030520A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21763AN 31480 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROWS 11-13 DEF INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHTS AT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030707000392003070700039NM 2003 7 7 AALA20030596 120030521A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21796AN 30796 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT INTERIOR FORWARD LEFT G3 CLOSET INOPERATIVE. REPLACED EMERGENCY EXIT INTERIOR FORWARD LEFT G3 CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030707000402003070700040NM 2003 7 7 AALA20030629 120030601A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21752AN 30260 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT PATH ASSEMBLY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030707000412003070700041WP 2003 7 7 AALA20030555 120030512A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21590AA 53253 DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030707000512003070700051NM 2003 7 7 AALA20030586 120030518A3397 WIRE BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21362AA 24043 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9 H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 9 H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030707000652003070700065NM 2003 7 7 2003UALA00493 120030612A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29364UA 24533 EXTERNAL FUSELAGE SKIN AT B.S. 928 BETWEEN STR. 17L AND 18L IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030707000662003070700066SO 2003 7 7 CX2A03RI002 120030625A2120 ODOR EMB 145 EMB145ER 3260211SO CABIN DETECTED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2714940 145033 CREW REPORTED AFTER TAKE OFF SMOKE ODOR IN FLIGHT DECK. THE CREW RETURNED TO RIC WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE BLEED AIR SYSTEM, AND PERFORMED A HIGH POWER ENGINE RUNS. ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030707000682003070700068NM 2003 7 7 03FDEA00897 120030617A5710 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RT WING O/B FLAP STOP FITTING (NR 2 FLAP VANE TRACK) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-67554 PT 1 - WINGS OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR 2L73 4F RTA22WE 20030707000772003070700077EA 2003 7 7 COMA0360299 120030626A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE LACK OF LUBE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01936CA 7043 FLIGHT 5833 GEAR DISAGREE WARNING. CLEANED AND LUBED NOSE LANDING GEAR. 2L72 4F RTA21EA 20030707000852003070700085NM 2003 7 7 QXEA200300758 120030621A5720 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 RIGHT SIDE INBOARD FLAP SHROUD HAS BROKEN L ANGLE ATTACHING CONNECTION CHANNEL TO SPAR (VERY OUTBOARD) REPAIRED IAW HORIZON AIR EA 6-57-158. 2H72 4T RTA13NM 20030707001182003070700118NE 2003 7 7 ALG2003F00065 120030312A2930 CONNECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL HYD SYSTEM MALFUNCTIONED A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03741SW 760070 DURING CLIMB OUT, NR 1 SERVO CAUTION LIGHT ILLUMINATED, THE PILOT THEN FOLLOWED THE CHECKLIST PROCEDURES. IT REOCCURRED AGAIN BEFORE LANDING. THE INDICATION WAS A MOMENTARY SERVO JAM, UPON LANDING THE MECHANIC FOUND CONNECTORS CORRODED ON NR 1 HYDRAULIC MODULE AND NR 1 SIDE OF MAIN ROTOR AFT SERVO, CLEANED THE CONNECTORS AND CHECKED THE HYDRAULIC SYSTEM WITH THE HYDRAULIC MULE IAW MM, FOLLOWED BY AN OPERATION CHECK AND FOUND TO BE SERVICEABLE. THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20030707001212003070700121EA 2003 7 7 COMA0360282 120030621A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01920CA 7022 FLIGHT 5683 FLAPS FAIL MESSAGE DURING TAXI. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20030707001342003070700134NM 2003 7 7 AWXA200300707 120030617A2823 ACTUATOR BOEING737 73733A 1384673NM CROSSFEED VALVE ERRATIC A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28166AW 9567 23627 ON DEPARTURE, FUEL CROSSFEED VALVE BECAME UN CONTROLLABLE CYCLING TO OPEN AND CLOSED POSITION ON ITS OWN. DISAGREEMENT LIGHT ILLUMINATED IN BOTH SWITCH POSITIONS, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FUEL CROSSFEED VALVE ACTUATOR IN RT WING FUEL TANK IAW BMM 28-22-21, PG. 401. CYCLED VALVE SEVERAL TIMES, OVERHEAD AGREEMENT LIGHT AGREED WITH VALVE POSITIONS. 2L72 4F RTA16WE 20030711000982003071100098EA 2003 7 11 COMA0360296 120030625A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAL ABORTED APPROACH JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01936CA13785 7043 FLIGHT 5786 NLG FAILED TO EXTEND WHEN SELECTED DOWN. REPLACED THE PSEU. 2L72 4F RTA21EA 20030711001142003071100114EU 2003 7 11 DHL2003362010 120030627A2697 CONNECTOR AIRBUS300 A300B4203 3930306EU FIRE LOOP DIRTY A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01362DH 84 IN FLIGHT ENGINE NR 1 LOOP -A- LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. OPS NORMAL NR 1 LOOP MOVED TO -B- LOOP. REPOSITIONED -A- LOOP AND CLEANED CONNECTOR. SYSTEM OPS CHECKED NORMAL. OK FOR SERVICE. 2L72 4F RTA35EU 20030714000092003071400009EA 2003 7 14 COMA0360303 120030626A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LT TE FLAPS DEFECTIVE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01986CA3056 7174 FLIGHT 5584 DURING DESCENT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY. REPLACED THE LEFT BRAKE POSITION SENSING UNIT. 2L72 4F RTA21EA 20030714000202003071400020NM 2003 7 14 SWAA031392 120030622A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED BETWEEN BS 807 AND BS 815, STR 26R. REMOVED AND REPLACED CORRODED SECTION OF STRINGER PER SRM. 2L72 4F RTA16WE 20030714000762003071400076NM 2003 7 14 SWAA031391 120030621A552065C35943 BEARING BOEING737 7377H4 1384404NM ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED SPECIAL VISIT, BOTH LT AND RT ELEVATORS FAILED OUTPUT TORQUE TUBE BUS LINKAGE TEST. REMOVED AND REPLACED BOTH LEFT AND RT ELEVATOR TORQUE TUBE CRANK BEARINGS MM. 2L72 4F RTA16WE 20030714001152003071400115CE 2003 7 14 GLBA2003092 120030622A21301143641407 CONTROLLER BEECH 1900 1900D 1154162CE ENVIRO SYS MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03195GL UE195 RIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED A317 PCB, OPS CHECK GOOD. 2L72 4T RTA24CE 20030714001562003071400156 2003 7 14 BAQA087566 420030701A2312069102525 TRANSCEIVER AEROSPAS355 AS355F2 8680812EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03941MS104 5495 TRANSCEIVER DOES NOT POWER UP. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030714001712003071400171EU 2003 7 14 BAQA086803 120030701A7931IPT70RT11000250GTRANSDUCER BOLKMS117 BK117B1 5626012EU ENGINE OIL ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME1287 7235 PRESSURE ERRATIC. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030716000112003071600011WP 2003 7 16 GTIA030457 120030514A57535910042504 VANE DOUG DC9 DC981 3022081WP RT FLAP DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND RT OUTBOARD FLAP MIDDLE VANE LOWER SIDE DELAMINATED. RIGHT OUTBOARD REMOVED FLAP MIDDLE VANE. VANE DELAMINATED BEYOND BOEING DC-9 MD-80 ACCEPTABLE REPAIR LIMITS AND TRAILING EDGE HAS HEAVY CORROSION. INSTALLED NEW RIGHT OUTBOARD FLAP MIDDLE VANE. (M) 2L72 4F A6WE 20030716000212003071600021EA 2003 7 16 A6WA200340099 120030618A2840 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA FUEL SHUTOFF ILLUMINATED A A6WAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL31446AW 7806 LEFT TRANSFER SHUTOFF VALVE CAUTION AMBER FUEL FAILED OPEN, CHECKED FUEL COMPUTER FOR FAULT CODES, NO CODES NOTED. NO EVIDENCE OF LEFT TRANSFER SHUTOFF VALVE CAUTION. OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030716000302003071600030 2003 7 16 USAASA03056 420030528A2565 BOTTLE AIRBUSA319 A319112 3930323EU ESCAPE SLIDE DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 THE FORWARD SERVICE DOOR SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE R1 SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030716000342003071600034NM 2003 7 16 USAABB03082 120030523A7720 WARNING LIGHT BOEING767 7672B7 1385107NM RT ENGINE ILLUMINATED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19651US 24764 EN ROUTE, CREW NOTED HIGH EGT AND LOW OIL PRESSURE ON RIGHT ENGINE. CREW REDUCED THRUST TO IDLE POWER. FLIGHT DIVERTED TO YHZ AND LANDED WITHOUT FURTHER INCIDENT. INFORMATION ON THE FDR SHOWED THAT THE FUEL FLOW TO THE ENGINE DROPPED TO ZERO ON APPROACH, APPROXIMATELY 1000 FEET AGL. (M) 2L72 4F RTA1NM 20030716000682003071600068NM 2003 7 16 2003F00424 120030602A49901605501 CONTROL VALVE BOEING737 737800* NM APU INOPERATIVE A MYWAO OTHER MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SO19733MA 30619 DURING TURN AROUND IN MIA, APU INOPERATIVE. HIGH OIL TEMPERATURE FAULT. TROUBLE SHOT SYSTEM. REMOVED AND REPLACED APU TEMP CONTROL VALVE. OPS CHECK AND LEAK CHECKED GOOD IAW 49-91-21. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030716000732003071600073SO 2003 7 16 SIMA200313207 120030511A783083990139 SWITCH EMB 135 EMB135KL 3260302SO THRUST REVERSER INOPERATIVE A SIMAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SW21810AE 145525 WHEN BOTH ENGINES WERE ADVANCED FOR TAKEOFF, THE NR 2 ENGINE REACHED N1 OF 70 PERCENT AND THEN DROPPED TO IDLE SPEED, THEN JUMBED BACKUP TO 70 PERCENT N1. THE CREW NOTICED A YAW MOTION ON THE AIRCRAFT. THE TAKEOFF WAS ABORTED. MAINTENANCE REMOVED AND REPLACED THE ENGINE TWO THRUST REVERSER LOWER DEPLOY SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030716000982003071600098EU 2003 7 16 XG3R087956 120030711A3340 BULB UROCOPEC130 EC130B4 EU EXTERIOR LIGHT BURNED OUT B XG3RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 353 3320 3560 PART KEPT BURNING OUT BULB AND SYSTEM FUSE. REPLACED PART. 1G72 3U H9EU 20030716001022003071600102NE 2003 7 16 HEEA087971 120030509A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S11329 760035 TAIL ROTOR BLADE PRIMARY RUBBER TORN BEYOND LIMITS. 1G72 3U H1NE 20030717000182003071700018SW 2003 7 17 HEEA087995 120030626A6220406010429101 PIN BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 MAIN ROTOR PIN WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000482003071700048 2003 7 17 HEEA088024 420030625A34225050010902 GYRO BELL 407 407 1182206SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 GYRO PRECESSING. UPON REMOVAL HEARD PART RATTLING INSIDE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030718000072003071800007NM 2003 7 18 TSAA0357117 120030507A575465453203 WEB BOEING737 73725A 1384481NM NR 6 SLAT CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 CORROSION DISCOVERED ON RIGHT WING SPAR WEB AT FSS 540-552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED SECTION OF WEB. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED AND INSTALLED REPAIR PART WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 57-10-6, FIGURE 1. (M) 2L72 4F RTA16WE 20030718000162003071800016NM 2003 7 18 USAA030095 120030606A5310 DOOR FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU58984 22199 FOUND FRAME CRACKED .25 INCH, BS 144 AFT CARGO DOOR FRAME NR 6 STOP HOLE. WEB REPLACEMENT/SPLICED IN PER EA 87279. (M) 2L72 4F RTA2NM 20030718000172003071800017NM 2003 7 18 USAA030094 120030606A5310 DOOR FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU58984 22199 FOUND FRAME CRACKED .25 INCH, BS 1380 AFT CARGO DOOR FRAME NR 6 STOP HOLE. WEB REPLACEMENT/SPLICED. (M) 2L72 4F RTA2NM 20030718000242003071800024NE 2003 7 18 GAIA03021OP 220030625A7314371900 PUMP BOEING727 727251 138408HNM PWA JT8 JT8D9A 52048NE FUEL SYSTEM FAILED A GAIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW07252US 19971 687788 DURING CLIMB-OUT FROM EWR AT 6500 FEET, THE NR 3 ENGINE QUIT. THE AIRCRAFT RETURNED TO EWR. AN UNEVENTFUL LANDING WAS MADE. INSPECTION FOUND THE DRIVE SHAFT SHEARD ON THE ENGINE DRIVEN FUEL PUMP. THE FUEL PUMP AND FUEL CONTROL WERE REPLACED. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F4 F A3WE E2EA 20030718000332003071800033WP 2003 7 18 GTIA030478 120030518A5310 DOOR FRAME DOUG DC9 DC981 3022081WP MLG DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND LT-RT MLG DOOR JAMB HINGE SUPPORT CORRODED. FABRICATED NEW LT FITTING. LOCATED AND DRILLED NEW LT AND RT HINGE SUPPORTS FOR DOOR JAMB. INSTALLED NEW LT AND RT HINGE SUPPORTS FOR DOOR JAMB. REMOVED LT HINGE SUPPORT. INSTALLED LT HINGE SUPPORT. (M) 2L72 4F A6WE 20030718000442003071800044WP 2003 7 18 AMTA200300745 120030430A5751 STRUCTURE LKHEED1011 10113853 5265020WP RT AILERON DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 RT INBOARD AILERON INBOARD SUPPORT FITTING ATTACHMENT HOLE GOUGED. REPAIRED FITTING IAW ER/A L10-57R-5157. (M) 2L73 4F A23WE 20030718000872003071800087WP 2003 7 18 CA030708006 220030120A725031081642 TURBINE WHEEL BAG JETSTMJETSTM3212 1500217EU GARRTTTPE331TPE33110UG 01514WP MCAULY4HFR344HFR34C652 NE ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 11453 (CAN) ENG SUSPECT INTERNAL VIBRATION. SOURCE OF VIBRATION WAS 6, BROKEN BY STRESS RUPTURE, P/N 3101512-6 BLADES ON FIRST STAGE T-WHEEL ASSY. P/N 3101512-6 BLADES ARE NO LONGER BEING INSTALLED. IT IS NOTED THAT 6 P/N 3101512-6 BLADES WERE REPLACED DURING A PROP STRIKE INSP AT ENGINE TSO 166:09. P/N 3108125-1 BLADES ARE BLADES THAT ARE INSTALLED NOW. DOWNSTREAM IMPACT DAMAGE CAUSED BY BROKEN BLADES EXITING ENGINE VIA GAS PATH AND SUBSEQUENT VIBRATION RELATED DAMAGES ARE MAJOR EXPENSE IN THIS REPAIR. A HOT SECTION AND GEARBOX INSP CAN BE SIGNED OFF WITH THIS REPAIR. ENGINE WILL REQUIRE TEST CELL RUNS FOR RECOMPENSATION, VIBRATION SURVEY, TORQUE CALIBRATION, LEAK AND FUNCTION CHECKS. 2L72 4T4 TRTBA15CAA E4WE 6 C3PNE 20030721000052003072100005NM 2003 7 21 AUS20030561 120030611A492038007021 BLEED VALVE HONEYWELL BOEING737 737800* NM GE CFM56 CFM567B24 NE APU ENGINE CONTAMINATED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AUS P6256 (AUS) APU BLEED VALVE CONTAMINATED WITH MOBIL JET 2. ODORS IN CABIN. 2L72 4F4 FRTA16WE E00055EN 20030618001462003061800146EA 2003 6 18 COMA0360270 120030611A3230 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01959CA 7116 FLIGHT 5301 GEAR DISAGREE WARNING DURING APPROACH. ADJUSTED NOSE LANDING GEAR UPLOCK TO NEW T/R M/M SPECIFICATIONS. 2L72 4F RTA21EA 20030618001562003061800156SW 2003 6 18 HEEA087505 120030612A6710SL505ASP6 NUT BELL 407 407 1182206SW CYCLIC WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 LOW CYCLIC FRICTION - COULD NOT ADJUST DUE TO WORN THREADS. SCRAPPED. 1G71 3U O H2SW 20030618001632003061800163 2003 6 18 HEEA087509 420030612A3421066304604 COMPASS BELL 206 206L3 1182108SW COCKPIT STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 COMPASS CARD STICKING. SHOP REPAIR. 1G71 3U H2SW 20030618001692003061800169SW 2003 6 18 HEEA087147 120030609A6710206010470101 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D RE1009 51106 BELLCRANK HAS WORN BEARINGS. REPLACED BEARING (2 EACH) 206010470101 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030618001902003061800190SW 2003 6 18 HEEA087156 120030609A6720 BUSHING BELL 206 206L3 1182108SW DRIVE LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 WORN BUSHING. REPAIRED. 1G71 3U H2SW 20030618002112003061800211SW 2003 6 18 HEEA087164 120030609A3212206030104023 FITTING BELL 206 206L3 1182108SW MLG FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 FITTING ASSY RUBBER MISSING. SCRAPPED. 1G71 3U H2SW 20030619000752003061900075SW 2003 6 19 HEEA087409 120030611A6510407340339107 BEARING BELL 407 407 1182206SW T/R DRIVE TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 TAIL ROTOR DRIVE BEARING GREASE SEAL TORN. 1G71 3U O H2SW 20030619001022003061900102 2003 6 19 HEEA087426 420030611A344280510890001 DISPLAY BELL 206 206B3 1181506SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322751 3627 WEATHER RADAR NOT PICKING UP OUTSIDE 1/4 MILE. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030619001032003061900103 2003 6 19 HEEA087225 420030610A2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 TRANSMITS WEAK AND GARBLED. SHOP REPAIR. 1G72 4U H4SW 20030620000442003062000044WP 2003 6 20 GTIA030380 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND FLOOR SUPPORTS FOUR EACH STATION 200 LBL 9-57 ARE CORRODED. FLOOR SUPPORTS AT STATION 200 LBL 16 TO 43, 44-53, 55-57 OUT OF LIMITS. REMOVED FLOOR SUPPORTS. FABRICATED NEW FLOOR SUPPORTS. INSTALLED FLOOR SUPPORTS. (M) 2L72 4F A6WE 20030620000662003062000066NM 2003 6 20 USAA030058 120030527A532065516982 SPLICE BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US40316 23988 PIT - FOUND STRINGER SPLICE WITH TWO CRACKS .25 IN LENGTH, BS 907 STRINGER 4 LEFT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-30-01. (M) 2L72 4F RTA16WE 20030620000812003062000081EA 2003 6 20 ASOA03220 120030517A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11904EV 7628 DURNG A GROUND INSPECTION IN DFW, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030620000872003062000087NM 2003 6 20 C7WA200300043 120030424A7500451077 TUBE BOEING727 7272M7 138407SNM NR 3 ENGINE BROKEN A C7WAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO17742RW 21952 AIR TURNBACK, ENGINE NR 3 HAD MULTIPLE COMPRESSOR STALLS. FOUND BROKEN LINE AT PRESSURE BLEED CONTROL VALVE REMOVED AND REPLACED TUBE IAW MM 20-10-05 ACCOMPLISHED ENGNE RUN IAW MM 71-00-00, ALL PARAMTERS NORMAL. (M) 2L73 4F A3WE 20030623000192003062300019 2003 6 23 MEX2003198 420030601A34142594466901 INDICATOR DOUG DC9 DC982 3022082WP AIRSPEED FAILED A ASMFCD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW231003Y 48068 AIRCRAFT SUSPENDS TAKEOFF DUE TO AIRSPEED INDICATIONS SHOWED A 40 KNOTS DIFFERENCE AND SPEED FLAG APPEARED. THE MACH AND AIRSPEED INDICATOR NR 2 WERE REPLACED IAW MM 34-13-01, ALL TESTS CORRECT. (M) 2L72 4F A6WE 20030623000202003062300020NM 2003 6 23 USAA030054 120030515A5330654577678 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US42530 23555 FOUND WALKAROUND SKIN CORRODED, 8 INCHES BY 8 INCHES, STATION 727 FROM STRINGER 27 RIGHT-27 LEFT. CUT OUT DAMAGED AREA, INSTALLED TRIPLER PER EA 76192. (M) 2L72 4F RTA16WE 20030623000382003062300038WP 2003 6 23 GTIA030347 120030514A5520 STRUCTURE DOUG DC9 DC982 3022082WP ELEVATOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND LEFT ELEVATOR STATION XHR 11 TWO DOUBLER CRACKED, DAMAGE. REMOVED DAMAGED UPPER AND LOWER TWO DOUBLERS. FABRICATED TWO DOUBLERS. INSTALLED FABRICATED DOUBLERS. (M) 2L72 4F A6WE 20030623001102003062300110WP 2003 6 23 AMTA200300720 120030528A3350 LIGHT LKHEED1011 10113853 5265020WP CABIN MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 AFT RIGHT EGRESS LIGHTING EXTREMELY DIM. REMOVED WATER MOISTURE AND DIRT FROM EGRESS LIGHTING STRIP END WITH LPS CFC CLEANER AS REQUIRED, OPS CHECK OK. (M) 2L73 4F A23WE 20030623001112003062300111EA 2003 6 23 A6WA200340081 120030520A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 FUSELAGE SKIN IS DAMAGED AT PAX DOOR CUTOUT FS 310. REPAIRED DAMGE AT PAX DOOR CUTOUT FS 310 IAW BOMBARDIER INC REO 601R-53-21-160A. (M) 2L72 4F RTA21EA 20030623001192003062300119WP 2003 6 23 GTIA030370 120030511A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND T-CHORD SUPPORT ANGLE IS CRACKED IN RADIUS. REMOVED SUPPORT ANGLE. INSTALLED CLIP. (M) 2L72 4F A6WE 20030624000022003062400002WP 2003 6 24 GTIA030372 120030505A5730 PANEL DOUG DC9 DC982 3022082WP LT WING DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND LT WING LOWER TRAP PANEL DELAMINATING. REPAIRED LEFT WING LOWER TRAP PANEL AT DELAMINATED. (M) 2L72 4F A6WE 20030624000102003062400010WP 2003 6 24 GTIA030377 120030513A5310 DOOR FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND LT MLG FORWARD DOOR JAMB IS CRACKED AT T-CAP DOUBLER. REMOVED DOUBLER. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20030624000432003062400043NM 2003 6 24 CALA0300285 120030606A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 940-992. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 53-60-15. 2L72 4F RTA16WE 20030624000442003062400044NM 2003 6 24 CALA0300297 120030607A5230143A61101 SKIN BOEING737 737724 13844BYNM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND A DENT IN OUTER SKIN OF FORWARD CARGO DOOR AT AFT CENTER EDGE, BS 487.65. THE DENTED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01724 AND SRM 51-20-01. 2L72 4F RTA16WE 20030624000522003062400052NM 2003 6 24 CALA0300289 120030606A5320C22101129001 MOUNT BOEING737 737524 1384721NM LAVATORY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719638 28899 INSPECTION FOUND FORWARD LAV MOUNT CORRODED AT DOOR THRESHOLD AFT CORNER. THE AFT CORNER MOUNT WAS REPLACED IAW ECRA 2540-01436. 2L72 4F RTA16WE 20030624000582003062400058NM 2003 6 24 CALA0300295 120030607A53306545778 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 1 INCH CRACK IN EXTERIOR FUSELAGE SKIN AT R-2 DOOR UPPER HINGE ARM CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-60-01. 2L72 4F RTA16WE 20030624000592003062400059NM 2003 6 24 CALA0300302 120030610A53306518420 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A .5 INCH CRACK IN LT WINDSHIELD POST SKIN. THE CRACK WAS ROUTED OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-10-01, FIGURE 210. 2L72 4F RTA16WE 20030624000742003062400074SO 2003 6 24 SWIA200312070 120030604A27503203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07187SW7745 6512 120037 INFLIGHT FLAP CONTROL FAULT INDICATION WOULD NOT CLEAR. RETURNED TO FIELD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS AND LEAK CHECKS GOOD IAW MM 27-50-09. 2L72 4T RTA31SO 20030624000772003062400077SO 2003 6 24 SWIA200312073 120030604A275012064207615 SWITCH EMB 120 EMB120RT 3260202SO FLAP SELECTOR MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07593SW2534 2534 120191 WHEN FLAPS 15 WERE SELECTED FCU INDICATES CONTROL FAULT WITH FLAP AND ASWS LIGHTS ON MAP. REMOVED AND REPLACED FLAP HANDLE WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030624000822003062400082EA 2003 6 24 SWIA200312078 120030608A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A SWIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM07920SW 7660 DETECTED SMOKE IN THE CABIN AT 500 FT AFTER T/O. SMOKE WAS NOT THICK BUT SMELLED LIKE PLASTIC. SMOKE DISSIPATED UPON RETURN TO FIELD. INSPECTED AFT EQUIPMENT BAY, GEAR BAY, AVIONIC BAY, ALL INTERIOR LIGHTS AND BALLAST. NO MESSAGES ON ECAS. EVERYTHING WORKS, ALL CHECKS GOOD. 2L72 4F RTA21EA 20030624000842003062400084NM 2003 6 24 DL73S030455 120030510A5330655298890 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27321DL 23093 AFT ENTRY DOOR CUTOUT, UPPER HINGE CUTOUT CRACK REPAIR THE UPPER HINGE CUTOUT OF THE L2 DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK THROUGH THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385034-14, REV A. 2L72 4F RTA16WE 20030624000872003062400087NM 2003 6 24 DL73K030460 120030512A3350 POWER SUPPLY BOEING737 737247 138448DNM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27243WA 23517 EMERGENCY FLOOR LIGHTING INOP AT ROWS 1 THRU 4. REPLACED POWER SUPPLY 2L72 4F A16WE 20030630000782003063000078SW 2003 6 30 HEEA087840 120030613A6230406010427109 GIMBAL RING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 GIMBAL RING WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000202003070100020SW 2003 7 1 HEEA087874 120030610A2510407370721105 RESTRAINT BELL 407 407 1182206SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 RESTRAINT WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030702000432003070200043WP 2003 7 2 GTIA030390 120030508A5310 STRUCTURE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND AFT FUSELAGE LEFT SIDE STATION 1429 TO 1418 HAS CORROSION AT SUPPORT FORWARD VENTRAL STAIRWAY. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030707000942003070700094NM 2003 7 7 DLM88030600 120030701A335020131A BATTERY PACK DOUG MD88 MD88 3023688NM AFT CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27993DL 53345 ON L/O CHECK FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. 2L72 4F RTA6WE 20030707001682003070700168NM 2003 7 7 P5CA0300886 120030611A3250 SWITCH BOEING747 7472D3B 1384805NM NLG STEERING MALFUNCTIONED A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23505MC 21251 ON TOW OUT RT LANDING GEAR TURNED SIDEWAYS. OPS CHECKED BODY GEAR STEERING SYSTEM IAW MM 32-53-00. OPS CK OK A/C BACK TO CONFIGURATION. SUSPECT RT BODY GEAR UNLOCK SWITCHES MALFFUNCTIONED. 2L74 4F RTA20WE 20030707001702003070700170EA 2003 7 7 03164701 120030613A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA RT OVRWING LIGHTBURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27701BR 7448 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT OVERWING EMERGECNY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL CHANGED THE BULB AND PERFORMED A SATISFOACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030707001902003070700190WP 2003 7 7 UPS03840822 120030520A5712 RIB DOUG DC8 DC871F 302199DWP LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, LEFT WING LE. UPPER RIB IS CRACKED AT XFS 697.5 STOPDRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED STACK ANGLE REPAIR IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707002022003070700202WP 2003 7 7 UPS03840877 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 747. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030708000012003070800001EU 2003 7 8 DXTA200300056 120030703A7331 ENGINE BRAERO1000 BAE1251000 1500287EU RIGHT MALFUNCTIONED E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07514QS NA1005 DURING TAKEOFF ROLL AT APPROX 100KTS A/C STARTED YAWING TO THE RIGHT ENGINE GUAGES REVEALED LEFT N1 98.4 PERCENT RIGHT N1 94 PERCENT LEFT ENGINE FUEL FLEW 2300 LBS/HR AND RIGHT 1900 LB/HR APR ARMED. 2L72 4F RTA3EU 20030708000252003070800025NM 2003 7 8 0301126312 120030616A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01672US 30267 DURING LINE CHECK FOUND ZONE B-FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030708000262003070800026EU 2003 7 8 03FDEA00894 120030616A7830491B1220002005 BRACKET AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE THRUST REVERSER CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 N 120 NR 1 ENG THRUST REVERSER LOWER AFT CLOSE OUT PANNEL LEADING EDGE, CHAFED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-21 PG 7 @ MAE. 2L72 4F4 FRTA35EU E13NE 20030708000442003070800044NM 2003 7 8 EVAS092015 120030528A3310 SWITCH DOUG MD11 MD11F 3023600NM LIGHT DIMMER OVERHEATED W QOCFB EMER. DESCENT MJ OVER TEMP WARNING INDICATION CRCRUISE 1 WP03 48786 DURING CRUISE FROM TPE TO ANC, CAPTAIN REPORT THERE IS SOME STRANGE ODOR IN THE COCKPIT, CAPTAIN DECIDE DIVERT TO HND. ON GROUND CHECK,FOUND THE DIMMER OVERHEATED, REPLACED DIMMER AND OPERATIONAL CHECK NORMAL. AIRCRAFT REGISTRATION IS B16110. 2L73 4F RTA22WE 20030708000472003070800047WP 2003 7 8 UPS03840826 120030525A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, MAIN CABIN L-2 DOOR TORQUE BOX WEB HAS A RIVNUT INSTALLED NEXT TO HI -LOCK WITH NO EDGE DISTANCE STA. 1660 LONG. 10L. REMOVED WEB AND REMOVED DAMAGE FROM FRAME,FABRICATED AND INSTALLED DOUBLER ON FRAME AND WEB AT STA. 1660 LONG.10L IAW SRM. 53-2-0 FIG. 23. 2L74 4F RT4A25 20030630000482003063000048SW 2003 6 30 HEEA087831 120030614A2810206064263101 TUBE BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUEL SYSTEM CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03491PH 53386 FUEL SYSTEM TUBE HAS CORROSION PITTING UNDER SLEEVE DUE TO IMPROPER PROTECTION DURING MANUFACTURING PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030630000502003063000050SW 2003 6 30 HEEA087833 120030609A2520206072219107 BRACKET BELL 407 407 1182206SW ALLSN 250C 250C47B GL PAX SEAT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 SEAT BRACKETS BROKEN. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030710001302003071000130NM 2003 7 10 03169416 120030618A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27416FJ 3171 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM SEAT ROWS 1 TO 4. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AND THE BATTERY AT LOCATION 4LK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030710001472003071000147NM 2003 7 10 EIA2003085 120030614A5315 FLOORBEAM BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 UPPER DECK FLOORBEAM BS 380 RT BL 45 TO RT FRAME INTERFACE WEB HAS MULTIPLE CRACKS, ELONGATED HOLES AND DENTS. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-53-142-2. 2L74 4F RTA20WE 20030711000962003071100096EA 2003 7 11 COMA0360294 120030625A301011513361 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ANTI ICE MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01785CA20843 7326 FLIGHT 5129 WING OVERHEAT WARNING DURING T/O. REPLACED THE ANTI-ICE CONTROLLER. 2L72 4F RTA21EA 20030714000512003071400051NM 2003 7 14 SWAA031376 120030620A53306546881 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030714000782003071400078NM 2003 7 14 SWAA031413 120030625A53126517583 BEAM BOEING737 7372H4 138448CNM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SRM. 2L72 4F A16WE 20030714000882003071400088NM 2003 7 14 SWAA031346 120030616A55306547450 DRAG ANGLE BOEING737 7373H4 1384600NM VERTICAL FIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN ATTACH CLEVIS DRAG ANGLES CORRODED LT SIDE (2 EA). REMOVED AND REPLACED VERTICAL FIN DRAG ANGLES PER SRM. 2L72 4F RTA16WE 20030714001142003071400114CE 2003 7 14 GLBA2003091 120030621A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS OUT OF ADJUST A GLBAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM03179GL UE179 FLAPS INOPERATIVE. CND ADJUSTED RIGHT FLAP SPLIT SWITCH. 2L72 4T RTA24CE 20030714001422003071400142 2003 7 14 ALGA087896 420030701A8300E6893672 PINION GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL GEARBOX GALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL263 CAG47416 53240 CAE847064 ENGINE REMOVED DUE TO METAL IN OIL. CAUSE FOUND TO BE GALLING ON PINION GER TEETH. REMOVED AND REPLACED PINION GEAR. 1G71 3U3 UO H2SW E1GL 20030714001452003071400145 2003 7 14 HEEA088082 420030702A2565350A25153202 HANDLE AEROSPAS355 AS355* EU SLIDE BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03971AE 3230 SLIDE HANDLE HAS BROKEN PIN. REPLACED. 1G72 3U H11EU 20030714001492003071400149EU 2003 7 14 HEEA088086 120030702A772250061036 INDICATOR BOLKMS105 BO105S 5626006EU EXHAUST TEMP READS HIGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 EXHAUST TEMP INDICATOR READS HIGH. SHOP REPAIR. 1G72 3U H3EU 20030714001502003071400150EU 2003 7 14 HEEA088087 120030705A770070BMB01020 CONTROL UNIT AEROSPAS355 AS355* EU ENGINE INTERFERENCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE 3234 INTERMITTENT RED GOV LIGHT AND ENGINE WOULD NOT TURN WHEN SWITCH SET TO ON POSITION EVEN WITH NO RED GOV LIGHT. REPLACED. 1G72 3U H11EU 20030714001622003071400162 2003 7 14 BAQA087945 420030630A3421501121001 GYRO AGUSTAA109 A109E 0260119EU COCKPIT TUMBLES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109UP132 11061 VERTICAL GYRO UNIT HAS ONLY 132.4 HOURS ON IT. TUMBLES AND THUMPS IN PITCH. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH7EU 20030714001652003071400165EU 2003 7 14 BAQA087778 120030626A28221176415103 PUMP BOLKMS117 BK117A1 5626010EU FUEL BOOST INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03967LS1381 7067 FUEL BOOST PUMP INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030714001682003071400168 2003 7 14 BAQA086344 420030616A3160L316M30C1003 DISPLAY UROCOPEC135 EC135P1 8680990EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME3760 0009 DISPLAY IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 7/3/03 1G72 3U O H88EU 20030714001732003071400173EU 2003 7 14 BAQA087776 120030630A6330L633M2010102 MOUNT UROCOPEC135 EC135P1 8680990EU TRANSMISSION LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03577LF63 0140 MOUNT LEAKING AND COLLAPSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030715000112003071500011 2003 7 15 USAASA03054 420030526A2565 LANYARD AIRBUSA319 A319112 3930323EU ESCAPE SLIDE CUT A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW 1033 THE LEFT AFT DOOR SLIDE LANYARD WAS FOUND FRAYED AND CUT. MAINTENANCE REPLACED THE LEFT AFT SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030715000162003071500016 2003 7 15 USAASA03065 420030615A2565 SLIDE AIRBUS320 A320214 3930316EU PAX DOOR LOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW 0863 THE LEFT MID ENTRY DOOR SLIDE COVER WAS FOUND LOOSE. MAINTENANCE FOUND THE SLIDE PACK SAGGING, AND HOLDING THE BUSTLE AWAY FROM LATCH. REPLACED THE SLIDE PACK AND ADJUSTED THE SLIDE COVER. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030716000142003071600014 2003 7 16 USAASA03051 420030524A2565 SLIDE AIRBUSA319 A319112 3930323EU PAX DOOR DISLODGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW 1019 THE FORWARD LEFT ENTRY DOOR ESCAPE SLIDE/RAFT WAS FOUND SEPARATING FROM THE MOUNTING. MAINTENANCE REPLACED THE ESCAPE SLIDE. OK FOR SERVICE. THE REPAIR SHOP FOUND THAT THE SLIDE REQUIRED REPACKING. THE SLIDE WAS REPACKED AND RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 20030716000172003071600017NM 2003 7 16 2003F00410 120030314A5730 ACCESS PANEL BOEING727 727222 1384073NM RT WING CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON RIGHT WING, NR 6 SLAT LOWER ACCESS PANEL NR 6589. FABRICATED NEW PANEL. ALODINED, PRIMED AND INSTALLED NEW ACCESS PANEL AT RIGHT LOWER NR 6 SLAT. (M) 2L73 4F A3WE 20030716000272003071600027NM 2003 7 16 2003F00419 120030314A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 660, STRINGER 23R/24R. FABRICATE REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRAME STATION 660 STRINGER 23R AND 24R. (M) 2L73 4F A3WE 20030716000292003071600029NM 2003 7 16 USAABB03095 120030623A335092110551 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 FOUND L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030716000602003071600060WP 2003 7 16 GTIA030467 120030508A5320 SPLICE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT PIT CORRODED FASTENERS ALL AT FS 1193-1212, 14 AT 25L, 14 AT 24L, 14 AT 231, 2 AT 221, 15 AT 241, 14 AT 201, 14 AT 19L. UPON FURTHER INSPECTION AT FS 1193-1212 L23L SPLICE IS FOUND TO BE CORRODED OUT OF LIMITS. REMOVED SPLICE. FABRICATE NEW LONGERON SPLICE. INSTALLED NEW LONGERON SPLICE. (M) 2L72 4F A6WE 20030716000622003071600062SO 2003 7 16 SIMA200316007 120030529A531514522461003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21809AE 145521 DURING AN MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT A 4 INCH SECTION OF DAMAGE FLOORBEAM AND TREATED THE BARE METAL. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTERS 53-21-10 FIGURE 201 SHEET 1. (M) 2L72 4F RTT00011AT 20030710001452003071000145NM 2003 7 10 EIA2003083 120030614A5514 ATTACH FITTING BOEING747 747SR46 1384816NM STRING TO SKIN CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 CORRSION ON UPPER SKIN TO STR ATTACH AREA IN RT HAND HORIZONTAL INTERIOR MAIN BOX 5 INCHES INBOARD OF RIB AT STAB STATION 235 ON 5TH STR AFT OF FWD SPAR ON FWD END. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-55-1582. 2L74 4F RTA20WE 20030711000272003071100027EU 2003 7 11 DHL2003366511 120030523A5411ASL0602501 LONGERON AIRBUS300 A300B4203 3930306EU NACELLE DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 NR 1 ENGINE O/B CORE NACELLE DOOR UPPER HINGE, CRACK ACCESS LONGITUDNAL SUPPORT ANGLE DOT C3158. REMOVED DAMAGED LONGERON ASSY & INSTALLED NEW LONGERON ASSY IAW DAC WSL6361. 2L72 4F RTA35EU 20030711000382003071100038 2003 7 11 COMA0360280 420030617A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01487CA 7729 FLIGHT 5792 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20030711000432003071100043NM 2003 7 11 751PA0016 120030620A3397 WIRE BOEING757 757200 1384950NM EMERGENCY LIGHT BROKEN A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 L1 FLOOR EMERGENCY LIGHT INOP (RED). FIRST IN LINE. SPLICED BROKEN WIRE. OPS CHECKS NORMAL. 2L72 4F RTA2NM 20030711000692003071100069SO 2003 7 11 C2XA03SH205 120030626A531014522226003 BUTTSTRAP EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030711001062003071100106NM 2003 7 11 VNAA0306013 120030622A24371030200 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE GENERATOR FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07425JS3935 3037 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND HALL EFFECT SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030714000042003071400004NM 2003 7 14 CALA0300341 120030627A5512 SKIN BOEING737 737524 1384721NM HORIZONTAL STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714660 28921 INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE DENTED WITH A SHARP CREASE IN THE CENTER OF THE DENT AT LEADING EDGE STA 184. REPAIRED IAW SRM 55-10-01 AND ECRA 5510-01647. 2L72 4F RTA16WE 20030714000382003071400038NM 2003 7 14 SWAA031410 120030624A5330BAC1498 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED PM CHECK, FOUND STRINGER CRACKED AT BS 945, STR 21R. REPAIRED STRINGER PER SRM. 2L72 4F A16WE 20030714000412003071400041NM 2003 7 14 SWAA031356 120030617A335065C27093 LIGHT BOEING737 7373H4 1384600NM FWD ENTRY DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030714000432003071400043NM 2003 7 14 SWAA031358 120030617A3350D71702001 HOUSING BOEING737 7377H4 1384404NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29701GS 27836 DURING SCHEDULED RON, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY HOUSING PER MM. 2L72 4F RTA16WE 20030714000592003071400059NM 2003 7 14 SWAA031361 120030618A53136551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030714000682003071400068NM 2003 7 14 SWAA031383 120030622A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED RON, FOUND BS 1016 BULKHEAD WEB CRACKED (2 EA) BETWEEN STR 7L AND STR 8L. REPAIRED BULKHEAD WEB PER SWA EA. 2L72 4F RTA16WE 20030714000852003071400085NM 2003 7 14 SWAA031343 120030615A53126516300 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 12.0. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030714001072003071400107CE 2003 7 14 GLBA2003098 120030630A3297 WIRE BEECH 1900 1900D 1154162CE MLG DAMAGED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0397UX UE97 GEAR WOULD NOT RETRACT. REPAIRED WIRING FROM P522 TO J168, OPS CK GOOD. 2L72 4T RTA24CE 20030714001512003071400151 2003 7 14 HEEA088088 420030705A2350A3016W INTERPHONE BOLKMS105 BO105S 5626006EU COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 INTERPHONE BOX FM SIDE INOPERATIVE. SHOP REPAIR. 1G72 3U H3EU 20030716000202003071600020NM 2003 7 16 2003F00413 120030314A5320 FLOOR SUPPORT BOEING727 727222 1384073NM FUSELAGE DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 13. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED REPAIR AT AFT CARGO FLOOR SUPPORT RBL 13 STATION 950F. (M) 2L73 4F A3WE 20030716000532003071600053WP 2003 7 16 GTIA030460 120030513A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FLIGHT COMPARTMENT, RIGHT FLOOR PANEL CRACKED, BACKSIDE HAS SURFACE CORROSION AND BARE METAL. CUT OUT CRACK IN PANEL, FABRICATED NEW PLATE AND DOUBLER. INSTALLED PLATE AND DOUBLER. (M) 2L72 4F A6WE 20030716000992003071600099GL 2003 7 16 HEEA087968 220030628A72606898642 GEARSHAFT BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL GEARBOX SHEARED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P823 51530 CAE895023 ENGINE WAS REMOVED DUE TO GEAR PROBLEM. STARTER TURNS BUT COMPRESSOR NOT ENGAGED TO STARTER. TEARDOWN INSPECTION REVEALED A SHEARED SHAFT BETWEEN THE FORWARD AND AFT GEARS OF CENTRIFUGAL BREATHER GEAR. PART IS BEING HELD FOR FAILURE ANALYSIS. 1G71 3U3 U H2SW E1GL 20030716001042003071600104NE 2003 7 16 HEEA087973 120030627A63107636104008103 COUPLING SKRSKYS76 S76C 8143008NE MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 ENGINE TO ROTOR COUPLING CORRODED BEYOND .0005 INCHES. TO BE SENT TO VENDOR. 1G72 3U NCH1NE 20030716001082003071600108 2003 7 16 HEEA088036 420030703A2312064102302 TRANSCEIVER SKRSKYS76 S76A 8143006NE VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 TRANSCEIVER EMITS LOUD POPPING SOUND AND TRANSMITS AND RECEIVES GARBLED. SHOP REPAIR. 1G72 3U H1NE 20030716001192003071600119SW 2003 7 16 HEEA087975 120030628A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S15911 36002 OUTBOARD ABRASION STRIP HAS SEVERAL EROSION HOLE THROUGH THE STRIP. 1G72 4U H4SW 20030717000082003071700008SW 2003 7 17 HEEA087985 120030622A30006035T95G04 DUCT BELL 214 214ST 1182106SW ANTI ICE SYS CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 ANTI ICE BLEED VALVE DUCT CHAFED. REPLACED DUCT. 2G72 4U H10SW 20030624000942003062400094 2003 6 24 DL738030468 420030516A23005145142 CONTROL PANEL BOEING737 737832 13844CFNM COCKPIT BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27373DA 29621 FIRST OFFICER AUDIO CONTROL PANEL GOT VERY WARM AND STARTED SMOKING SLIGHTLY. COUL DNOT DESELECT VHF NMBR 3 AND HF1. REPLACED F/O AUDIO SELECT PANEL 2L72 4F RTA16WE 20030619000302003061900030SW 2003 6 19 HEEA087379 120030611A5320407070620213 PANEL BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 TRIM PANEL CRACKED. 1G71 3U O H2SW 20030619000712003061900071SW 2003 6 19 HEEA087405 120030611A6510407340339101 BEARING BELL 407 407 1182206SW T/R DRIVE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 TAIL ROTOR DRIVE BEARING EMITTING BLACK GREASE. 1G71 3U O H2SW 20030620000892003062000089EA 2003 6 20 ASOA03214 120030507A274170608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11907EV 7648 FLT 4295 - DURING CLIMB-OUT FROM DFW-JAX, THE STABILIZER AND MACH TRIMS DISENGAGED AT APPROXIMATELY 400 FEET. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030623000172003062300017NM 2003 6 23 USAA030062 120030516A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US46845 23232 FOUND SKIN CRACKED .875 INCH, MED CUTOUT BS 304 WL 259. DOUBLER INSTALLED PER EA 74808A. (M) 2L72 4F RTA16WE 20030624000232003062400023NM 2003 6 24 VNAA0305023 120030531A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ROW 4 FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07457PS 3048 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP AT ROW 4 AND 5 WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030624001112003062400111EU 2003 6 24 DXTA200300035 120030522A3242 MASTER CYLINDER BRAERO1000 BAE1251000A 1500104EU BRAKE ASSY OVERSERVICED E DXTAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 GL07523QS NA1010 NO BRAKING ACTION FROM CO-PILOT'S RIGHT BRAKE PEDAL (ONLY 300-400 PSI REGISTERED ON BRAKE PRESS. GAUGE). - BLED HYDRAULIC SYSTEM AND SERVICED MASTER CYLINDER TO PROPER FLUID LEVEL. 2L72 4F RTA3EU 20030625000162003062500016EU 2003 6 25 03FDEA00799 120030524A5753 SKIN AIRBUS300 A300B4605R 3930308EU TE FLAP DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25657FE 748 RT CENTER FLAP BOTTOM SKIN HAS 3 CREASED DENTS RANGING FROM 1/4"W TO 1/2"W, 1/2" L TO 6"L ON T/E JUST I/B OF #4 FLAP TRACK. REPAIRED BOTTOM SKIN BY INSTALLING DOUBLER I/A/W FEDEX EA 6-5750-2003 2L72 4F RTA35EU 20030625000172003062500017EU 2003 6 25 03FDEA00798 120030524A5330 SKIN AIRBUS300 A300B4605R 3930308EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25657FE 748 FUSELAGE EXTERIOR SKIN AT FR 43-44 STR 53L-55L HAS BLEND OUT AREA OUT OF LIMITS BY 0.006. PERFORMED HFEC OF AREA, DVI, AND REMOVED 4 FASTENERS. ROTOTESTED 4 HOLES, O/S TO 6.31MM AND INSTALLED HL11VF8/HL70-8 HILOC FASTENERS. PRIMED AND PAINTED. ALL WORK COMPLETED I/A/S FEDEX EA 6-5315-71314 RELEASED 5/22/03 2L72 4F RTA35EU 20030625000192003062500019EU 2003 6 25 03FDEA00796 120030523A7830491B1220000029 BLOWOUT DOOR AIRBUS300 A300B4605R 3930308EU NR 2 ENGINE T/R WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 COMPLY WITH E.A. 6-7830-70395 EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029) FACT 23MAY03 03:28 BFM R COMPLIED IAW/E.A. 6-7830-70395 -EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029. 2L72 4F RTA35EU 20030625000602003062500060EA 2003 6 25 03149637 120030529A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA LT OVERWING INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27637BR 7308 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030625001392003062500139SW 2003 6 25 AUS20030511 120030514A32602782186057 BULB SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UHR WP MLG INDICATOR FAILED W O OTHER P NO WARNING INDICATION LDLANDING 1 AUS (AUS) LT MAIN LANDING GEAR DOWN INDICATOR BULBS BLOWN. 2L72 4T4 TRTA5SW E4WE 20030626000102003062600010 2003 6 26 U30A200300013 420030415A3460B546CAM0103 COMPUTER AIRBUS320 A320214 3930316EU ZONE 128 INOPERATIVE A U30AO OTHER O OTHER TXTAXI/GRND HDL 1 EA17261AV2797 1595 1615 NR 2 FMGC FAILED PRIOR TO DEPARTURE.(FLT 256 EWR-PUJ)DEFERRED PER MEL 22-83-01.{REVISION TO THE REPORT SUBMITTED 4/28/03}. AFTER FLT 105, PUJ-PHL, ON 4/15/03, AT PHL; REMOVED & REPLACED NR 2FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC)I/A/W AMM 22-83-34-401, OPPS CK'D OK. COMPLIED WITH RVSM RETURN SERVICE REQUIREMENTS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030626000142003062600014NM 2003 6 26 03FDEA00441 120030415A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 BS 560 FRAME AND SHEAR TIE HAVE TWO FASTENER HOLES THAT HAVE BEEN DRILLED UP INTO THE VERTICAL PORTION OF THE FRAME LBL 12 WL 148. REPAIRED B.S. 560, LBL 12, W.L. 148 SHEAR TIE IAW SRM 53-10-4 FIG 13 AND FED EX E.A. 7-5310-54467. 2L73 4F RTA3WE 20030630000022003063000002NE 2003 6 30 00097 220030608A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE LEFT FLAMED OUT E HAEABA EMER. DESCENT UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05977TW 13 PILOT REPORTED LT ENGINE FLAMED OUT WHILE CLIMBING FROM FL360 TO 370, DECENDED AND RESTART AND CLIMB BACK TO FL330 AND COMPLETED LEG. WILL UPDATE AFTER MAINTENANCE.COMPLIED WITH SEI 187 FLOW CHART FOR FLAME OUT CK OUT CF700 NO DEFECTS NOTED. 2L72 4F4 F A7EU E7EA 20030630000162003063000016EU 2003 6 30 DHL2003365006 120030528A2150 ACM AIRBUS300 A300B4203 3930306EU CABIN COOLING CONTAMINATED A DHLAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01365DH 149 ON TAXI, SMOKE LIGHT ILLUMINATED ON MASTER WARNING PANEL, SMOKE SENSOR ON FLIGHT ENGINEER PANEL ILLUMINATED IN NR 6 & 7. APPROPRIATE EMERGENCY CHECK LIST ACCOMPLISHED. RETURN TO BLOCKS. ON RETURN TO BLOCK, FOUND DURING DUAL PACK OPERATION OF WATER VAPOR EXITING FROM OVERHEAD DUCTING. OPERATED PACKS IN HEAT MODE TO CLEAR WATER VAPOR. THEN COOLED CABIN, AND PERFORMED MAIN DECK SMOKE DETECTION ADJUST. 2L72 4F RTA35EU 20030630000222003063000022 2003 6 30 MWEA030237 420030528A34189650449002 COMPUTER DOUG MD88 MD88 3023688NM STALL WARNING MALFUNCTIONED A MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31601ME 49762 WHEN ADDING POWER FOR TAKE-OFF STALL INDICATION FAILURE LIGHT ILLUMINATED. REMOVED AND REPLACED STALL WARNING COMPUTER. 2L72 4F RTA6WE 20030630000252003063000025NE 2003 6 30 XNOA01120 220030527A7320 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 OUT OF RIG A XN0AO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23373PC 218 NO THROTTLE RESPONSE ON NR 1 ENGINE. RIG VSV AND VBV IAW ENGINE MANUAL 72-00-00. POWER RUN CHECK GOOD. 2L72 4F4 FRTA35EU E23EA 20030630000362003063000036EU 2003 6 30 AWXA200300612 120030502A5320D5347047821000 STRUCTURE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 58 - 59, LBL 686 MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT CORNER PROFILE FR 58-59, LBL 686 MM IAW A320 SRM 53-41-14, FIG. 24, PG. B31-B32. 2L72 4F RTA28NM 20030630000372003063000037EU 2003 6 30 AWXA200300613 120030502A5320D53974705000 PROFILE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-61, LBL 686MM. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-61, LBL 686MM; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND A SPLICE DOUBLER; INSTALLED REPAIR PARTS IAW AWA E.R. 26-05341-03142-TB5. 2L72 4F RTA28NM 20030630000472003063000047SW 2003 6 30 HEEA087830 120030615A3212206050247135 COVER BELL 407 407 1182206SW ALLSN 250C 250C47B GL FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 RT INSIDE TORN AND DETERIORATED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030630000522003063000052NE 2003 6 30 BAQA087531 220030608A7314430201407 PUMP BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE FUEL SYSTEM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03219HM1790 47573 FUEL PUMP DOESN'T TURN FREELY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H9SW E5NE 20030630000592003063000059NE 2003 6 30 ALGA087758 120030625A6520SB8208102 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL T/R GEARBOX LEAKING B ALGAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03917QS A12600345 760217 TAIL ROTOR GEARBOX OUTPUT SEAL LEAKED WHEN RUN-UP ON TEST STAND. 1G72 3U3 U H1NE E1GL 20030620000742003062000074NM 2003 6 20 USAA030070 120030516A5320654580730 ANGLE BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 PIT - FOUND ANGLE CRACKED .5 INCH, UPPER SIDE OF 13R STATION 291.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART N/R. (M) 2L72 4F RTA16WE 20030623000052003062300005EA 2003 6 23 ASOA03215 120030517A5315601R3111357 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING HANGAR MAINTENANCE, FLOORBEAM CLIPS AT BULKHEAD FS 280 LBL AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR BY STOP DRILLING THE ENDS OF THE CRACKS OF THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 IAW ASA EO 600-53-0100. (M) 2L72 4F RTA21EA 20030623000322003062300032WP 2003 6 23 ZIAA03003 120030521A2450A718JL RELAY LKHEED188 188A 5262602WP NR 2 SYSTEM OVERHEATED A ZIAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL235512 188A1017 LANDED IN TORONTO DUE TO ELECTRICAL SMOKE COMING FROM BEHIND COCKPIT CIRCUIT BREAKER PANEL. REMOVED AND REPLACED NR 2 MAIN DC BUS REVERSE CURRENT CUTOUT RELAY IAW L-188 MM CPT 24-0. ALL SYSTEM CHECK NORMAL. (M) 2L74 4T RT4A22 20030623000442003062300044WP 2003 6 23 GTIA030357 120030510A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND DENT AT FS 245 BETWEEN LONGERONS 18L AND 19L. FABRICATED REPAIR DOUBLERS AND FILLERS. UPON FURTHER EVALUATION. FOUND SHEAR TIE FRAME SECTION AT STATION 237 L18 - L20L TO BE CRACKED. REMOVED SHEAR TIE SECTION AT FS 237 L18L TO L20L. FABRICATED NEW SHEAR TIE SECTION. I NSTALLED SHEAR TIE. INSTALLED FABRICATED REPAIR DOUBELRS AND FILLERS. (M) 2L72 4F A6WE 20030623000672003062300067 2003 6 23 UIEA200300022 420030430A2565 CABLE BOEING747 74747UF 1384949NM ESCAPE SLIDE STUCK A UIEAK NONE O OTHER ININSP/MAINT 1 EA15493MC 292254 DURING C-04 CHECK IN FRA AND WHILE PERFORMING AN OPERATIONAL CHECK OF THE INFLATABLE EVACUATION SYSTEM AT THE UPPER DECK DOOR RIGHT SIDE AS PER WO A230102GTI, THE SLIDE WAS LIFTED AND HAD FALLEN OUT OF THE DOOR FRAME. SUDDENLY THE SLIDE STOPPED ROTATING AND STUCK. AFTER WAITING SEVERAL SECONDS THE MECHANIC OPENED THE VELCRO TAPES WHICH CONNECT THE ASPIRATORS WITH THE GIRT. AFTER THIS THE SLIDE TURNED TO THE END POSITION AND INFLATED PROPERLY. INVESTIGATION OF THE VIDEO RECORD HAD SHOWN THAT THE FORWARD RELEASE CABLE WAS TIGHT WHEN THE SLIDE STUCK. THE LAST RELEASE PIN WAS LAYING BENEARTH THE GIRT. OPENING THE VELCRO TAPES INCREASED THE FORCE AND THE RELEASE CABLE GOT FREE. AFTER THIS MANUAL RELEASE, THE 2L74 4F RT1384945 20030624000322003062400032NM 2003 6 24 CALA0300314 120030614A5730 SKIN BOEING737 7373T0 1384582NM WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 1 INCH CRACK IN NR 4 SLAT ACTUATOR CUTOUT ON RT FIXED LEADING EDGE SKIN AT WBL 325. A DOUBLER WAS INSTALLED IAW SRM 57-41-01. 2L72 4F RTA16WE 20030624000342003062400034NM 2003 6 24 CALA0300316 120030616A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A GOUGE IN CENTER OF AFT BAGGAGE BIN DOOR EXTERIOR SKIN ABOUT 12 INCHES ABOVE HANDLE. THE SKIN WAS REPAIRED IAW SRM 52-00-01, PAGE 203. 2L72 4F RTA16WE 20030624000352003062400035NM 2003 6 24 CALA0300317 120030527A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM STA CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND CRACKS IN PRESSURE DECK WEB AT STA 665 TO 675, RBL 35 TO 45. A WEB STIFFENER WAS INSTALLED IAW ECRA 5312-01022. 2L72 4F RTA16WE 20030624000462003062400046NM 2003 6 24 CALA0300299 120030609A55126554821 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716339 23577 A DENT WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER SKIN 15 INCHES O/B OF FUSELAGE ON LEADING EDGE AT STA 60. THE DENTED AREA PREVIOUSLY HAD AN INTERIM REPAIR INSTALLED AND HAD BEEN PLACED ON DIP. A PERMANENT REPAIR WAS PERFORMED BY INSTALLING AN EXTERNAL DOUBLER IAW ECRA 5510-01679. 2L72 4F RTA16WE 20030624000832003062400083EU 2003 6 24 HCM2003F00001 120030430A2821 WARNING LIGHT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL SYSTEM ILLUMINATED E O OTHER J WARNING INDICATION NRNOT REPORTED 1 WP13982BH 2876 9043 1.4 HOURS INTO A SIGHT SEEING FLIGHT, THE (FUEL FILTER) LIGHT ILLUMINATED ON THE CAUTION PANEL. THE PILOT MADE A PRECAUTIONARY LANDING AS SOON AS POSSIBLE. A MECHANIC WAS SENT TO THE HELICOPTER AND CHANGED THE FUEL CONTROL AND THE AIRFRAME FUEL FILTER. THE HELICOPTER WAS THEN RETURNING TO BASE WHEN THE (FUEL FILTER) LIGHT ILLUMINATED AGAIN. THE PILOT LANDED AT THE HILO MAINTENANCE FACILITY. BOTH FUEL BOOST PUMPS, THE FULE FILTER AND BYPASS INDICATOR ASSEMBLY AND THE FUEL CONTROL UNIT WERE ALL CHANGED AT THIS TIME. THE FUEL FILTER BOWL HAD A FOREIGN SUSSTANCE INTHE BOTTOM OF THE BOWL. IT WAS NOT MAGNETIC. THE FUEL SAMPLE HAS BEEN SENT OUT FOR EVALUATION. 1G71 3U3 U H9EU E19EU 20030624000952003062400095NM 2003 6 24 DLM88030469 120030516A5350530700500 RADOME DOUG MD88 MD88 3023688NM NOSE DAMAGED A DALAO OTHER O OTHER NRNOT REPORTED 1 SO27933DL 49720 ON ARRIVAL DFW FOUND RADOME DAMAGED. LOWER LEFT CENTER. APPROX 6 INCHES IN DIAMETER, SPONGY FEELING. REPLACED RADOME 2L72 4F RTA6WE 20030625000182003062500018EU 2003 6 25 03FDEA00797 120030523A7830491B1220000029 BLOWOUT DOOR AIRBUS300 A300B4605R 3930308EU NR 2 ENGINE T/R WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 COMPLY WITH E.A. 6-7830-70395 EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029) FACT 23MAY03 03:28 BFM R COMPLIED IAW/E.A. 6-7830-70395 -EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029. 2L72 4F RTA35EU 20030625000422003062500042NM 2003 6 25 AWXA200300596 120030516A53306545765 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-17 CHECK 9 EACH CRACKS WERE FOUND ON LOWER ROW OF FASTENERS OF LAP SEAM AT BS 492 - BS 502, STR 4 RT. MAINTENANCE REMOVED FASTENERS AT STR 4 RT BETWEEN BS 485 AND BS 508; CUTOUT DAMAGED AREA OF FUSELAGE SKIN FROM BS 487.5 TO BS 506.5; FABRICATED 3 EACH FILLERS, AND 4 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, PG. 362, FIG. 228. 2L72 4F RTA16WE 20030626000032003062600003NM 2003 6 26 2003UALA00370 120030404A3350FU305 FUSE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 DURING PREFLIGHT INSPECTION CREW REPORTED EEL (AISLE) LIGHTS INOP ROW 15 TO REAR OF CABIN. REPLACED FUSES ON AFT BATTREY PACK 2L72 4F4 FRTA16WE E2GL 20030630000742003063000074SW 2003 6 30 HEEA087836 120030607A791023066697 FILTER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE OIL BYPASSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 OIL FILTER BYPASS BUTTON POPPING. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030630000762003063000076SW 2003 6 30 HEEA087838 120030617A243231908001 BATTERY BELL 407 407 1182206SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 BATTERY WEAK. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000112003070100011SW 2003 7 1 HEEA087865 120030614A3212206676901103 VALVE BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 196 53266 FLOAT BOTTLE VALVE LEAKING. REPLACED VALVE 206-373-901-103 DUE TO LEAKING AT PILOT VALVE VENT. REPAIRED. 1G71 3U O H2SW 20030702000062003070200006EA 2003 7 2 A6WA200340093 120030607A2621 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA NR 1 ENGINE DISCHARGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31424AW 7656 FOUND FIRE BOTTLE EMPTY, REMOVED BOTTLE REMOVED AND REPLACED NR 1 ENGINE FIRE EXTINGUISHER CONTAINER IAW AMM 26-21-07. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030702000252003070200025NM 2003 7 2 AMTA200300751 120030516A5753 SKIN BOEING737 73783N 13844HINM LT WING TE FLAP DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11317TZ 28246 FOUND LEFT WING INBOARD TRAILING EDGE AFT FLAP LOWER SKIN DENTED. REPAIRED SKIN IAW SRM 51-70-10-2. (M) 2L72 4F RTA16WE 20030702000342003070200034NM 2003 7 2 USAASB03074 120030607A2120 ODOR BOEING737 7373B7 1384580NM CABIN DETECTED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19394US 23316 TEN MINUTES AFTER TAKEOFF FROM CLT, FLIGHT ATTENDANT REPORTED AN ELECTICAL ODOR ALONG WITH A SLIGHT HAZE IN THE CABIN FROM SEAT ROWS 4 THROUGH 14. AS A PRECAUTION, CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE CHECKED E/E COMPARTMENT FOR SMOKE ODOR. RAN PACKS FULL HOT AND FULL COLD WHILE RUNNING ENGINES AT TAKEOFF POWER. COULD NOT DUPLICATE ELECTRICAL ODOR OR HAZE. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030702000352003070200035WP 2003 7 2 GTIA030394 120030506A5753 SKIN DOUG DC9 DC982 3022082WP RT WING TE FLAP GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND RIGHT WING INBOARD FLAP GOUGED AT NOSE CAP 3RD HINGE FROM INBOARD. MATERIAL ID 2014-T6.090. MATERIAL SUB 2014-T6.090 TO 7075-T6.090. FABRICATED WEB DOUBLER REPAIR. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20030702000392003070200039WP 2003 7 2 GTIA030384 120030527A3260833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23826NK 49391 NOSE GEAR RED ON RETRACTION WITH MAINS OUT NLG INDICATOR RETRACTED NO ABNORMAL INDICATION, VIBRATION ETC. AFTER 2 MINUTES LIGHT WENT OUT THEN 1 MINUTE LATER CAME BACK ON FOR 10 MINUTES, THEN OUT. APPEAR TO BE MORE SWITCH PROBLEM. ON APPROACH LIGHT CAME ON AT 10,000 FEET, STAYED ON UNTIL GEAR DOWN. NOSE GEAR UNSAFE INDICATION ON GEAR RETRACTION. CYCLED GEAR AND CLEARED. REMOVED AND REPLACED NOSE GEAR UP POSITION PROX SENSOR D1-31. RESHIMMED NOSE GEAR PROX SWITCH. CYCLED NOSE GEAR SEVERAL TIMES. YSTEM OP CHECKS GOOD. (M) 2L72 4F RTA6WE 20030630000532003063000053NE 2003 6 30 BAQA087055 220030608A7314430201407 PUMP BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE ENGINE FUEL FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03219HM1529 47573 FUEL PUMP WOULD NOT TURN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H9SW E5NE 20030630000562003063000056NE 2003 6 30 ALGA087751 120030624A6520SB8207102 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL T/R GEARBOX LEAKING B ALGAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03519AL A12600128 760058 MULTIPLE INPUT SEALS LEAKING WHEN RUN-UP ON TEST STAND. REPLACED SEALS WITH NEW. 1G72 3U3 U H1NE E1GL 20030630000572003063000057EU 2003 6 30 BAQA087752 120030520A760025013482 METER BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE SLAVING INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03932CJ 7024 SLAVING METER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030701000012003070100001SW 2003 7 1 HEEA087855 120030617A6510407340339107 BEARING BELL 407 407 1182206SW BLOWER SHAFT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH PHI0009 53188 UNABLE TO BALANCE. REPLACED BEARING 407-340-339-107, S/N ZV16525 DUE TO SCRAPPED WITH HANGER; AFT HOUSING 407-040-322-101, S/N 74613-130 DUE TO BOLT BORE WORN OUT. REPAIRED. 1G71 3U O H2SW 20030701000032003070100003SW 2003 7 1 HEEA087857 120030415A6320407040623101 LINE BELL 407 407 1182206SW MRGB OIL SYS CORRODED E HEEAK NONE O OTHER NRNOT REPORTED 1 SW03491PH 53386 CORROSION CAUSED BY DISSIMILAR METALS USED IN MANUFACTURING PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000212003070100021SW 2003 7 1 HEEA087875 120030610A2510407370723103 SEAT BELT BELL 407 407 1182206SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 SEAT BELT WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000432003070100043SW 2003 7 1 HEEA086960 120030603A7810206064203101 DUCT BELL 407 407 1182206SW EXHAUST CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 DUCT IS EXCESSIVELY CRACKED IN SEVERAL PLACES. REPLACED DUCT. 1G71 3U O H2SW 20030702000092003070200009EA 2003 7 2 A6WA200340048 120030328A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31431AW 7256 ONE LIGHTENING STRIKE DAMAGE AREA IN OPEN BAY AT FS 250 BETWEEN STRINGERS L25 AND L26. TRIMMED OUT DAMAGED AREA OF SKIN PANEL. COMPLIED WITH EDDY CURRENT INSPECTION OF CUT LINE FROM DAMAGE REMOVAL. NO INDICATION NOTED AT THIS TIME. FABRICATED FILLER. COMPLIED WITH WVAC RO 601R-53-3910. COMPLIED WITH STEP 15 OF WVAC EO 601R-53-3910. (M) 2L72 4F RTA21EA 20030702000232003070200023NM 2003 7 2 USAA030090 120030603A5320 WEB BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU58984 22199 FOUND WEB CRACKED .5 INCH, BS 560 STRINGER 20 RT. DAMAGE REMOVED, INSTALLED FABRICATED WEB SECTION AND REPAIR DOUBLERS PER SRM 53-00-07 FIG 202 AND EA 87. 2L72 4F RTA2NM 20030707000272003070700027NM 2003 7 7 AALA20030584 120030518A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21760AN 31477 DURING OVERNIGHT MAINTENANCE, LEFT FORWARD GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT FORWARD GALLEY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030707000712003070700071SW 2003 7 7 HEEA0029439 120030521A7920209062010001 VALVE BELL 412 412 1182202SW ENGINE OIL INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 PLATE LOOSE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20030707000952003070700095NM 2003 7 7 DLM88030601 120030627A2410 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE DEFECTIVE A DALAA UNSCHED LANDING M OVER TEMP CRCRUISE 1 SO27902DL 49533 718103 AS WE REACHED CRUISE ALT NOTICED RIGHT CSD OUTLET OIL TEMP ABOVE RED ARC FOLLOWED POM PROCEDURE. TURNED RIGHT GEN OFF, STABILIZED ABOUT 130 DEG. FREQ 394 398 WITH GEN SW OFF. CSD RISE IN CAUTION UNTIL GEN TURNED OFF/ T/S NR 2 ENGINE IAW MM 24-10-00-01 R/R TEMP SENSOR IAW MM RAN ENGINE FOR 5-7 MINS OPS CKS NORMAL. 2L72 4F4 FRTA6WE E9NE 20030707000972003070700097NM 2003 7 7 QXEA200300773 120030617A5410 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 INSIDE OF LOWER NACELLE LEFT HAND LOWER AFT CONE BRACKET CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030707001292003070700129NM 2003 7 7 CALA0300329 120030623A2121732591F FAN BOEING767 767224 1385170NM E & E BAY INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27731529709 9709 30431 AN ELECTRICAL SMOKE ODOR WAS DETECTED ON THE FLIGHT DECK AND IN THE VICINITY OF SEAT 3B OVERHEAD. THE UTILITY BUSSES AND RECIRCULATION FANS WERE TURNED OFF AND THE EQUIPMENT COOLING SELECTOR WAS TURNED TO STANDBY IAW CHECKLIST. THE ODOR DISSIPATED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE COOLING AIR FAN AND FAN CONTROL CIRCUIT CARD. OPERATIONAL CHECKS WERE GOOD WITH NO ODORS DETECTED. 2L72 4F RTA1NM 20030707001332003070700133NE 2003 7 7 E7J2003F00000 220030505A7230 COMPRESSOR WHEEL GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE ENGINE DAMAGED E E7JAO OTHER O OTHER NRNOT REPORTED 1 NE03507QS1861 625 11320 WHILE PERFORMING AD 203-07-11, ENGINE FAN DISK ULTRASONIC INSPECTION, THREE FAN BLADE TRAILING EDGES WERE FOUND WITH UNACCEPTABLE DAMAGE. THE FAN DISK RING SHOWED GOUGING IN THE AREAS CORRESPONDING WITH THE DAMAGED BLADES. (REPORT NR: 625-01-03) (PTRS: NE03200305670) 2L72 4F4 FRTA12EA E00057EN 20030702000452003070200045CE 2003 7 2 2003F00392 120030611A2820 TRANSFER VALVE CESSNA750 750 2076810CE FUEL SYSTEM FAILED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL235113 7500013 RT TANK O'FILL, VENTED FUEL OPERATED IAW CESNA LETTER QTY WAS LESS THAN 32000 LBS. A FUEL TRANSFER CHECK WAS PERFORMED BY MAINTENANCE PER CESSNA MM. NO DEFECTS FOUND, SYSTEM FUNCTIONED NORMALLY. (M) 2L72 4J RTT00007WI 20030702000552003070200055EA 2003 7 2 A6WA200340087 120030604A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 RIGHT SIDE UNDER FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621 RBL 33, WL 73 DAMAGED STRUCTURE WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW REO 601R-53-61-004 REV B. (M) 2L72 4F RTA21EA 20030623000972003062300097WP 2003 6 23 GTIA030404 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLOOR SUPPORT STATION 218 LBL 13-RBL 10 HAS CORROSION. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030624000052003062400005WP 2003 6 24 GTIA030375 120030519A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND MID CARGO FS 693 FRAME AND FITTING CORRODED AT JAMB BEAM. LOCATE AND DRILLED NEW FITTING. (M) 2L72 4F A6WE 20030624000152003062400015NM 2003 6 24 USAABB03078 120030519A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 23 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030624000382003062400038NM 2003 6 24 CALA0300320 120030602A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND CORROSION ALONG THE FLOORBEAM AT STA 294.5, RBL 31.5. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01147. 2L72 4F RTA16WE 20030624000492003062400049NM 2003 6 24 CALA0300286 120030606A7120S302A0053 ISOLATOR BOEING737 737524 1384721NM NR 2 ENGINE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW27196381681416814 28899 INSPECTION FOUND A 1 INCH CRACK IN RIGHT ENGINE AFT ISOLATOR ELASTOMER. THE NR 2 ENGINE AFT MOUNT WAS REMOVED AND REPLACED IAW MM 54-42-11. 2L72 4F RTA16WE 20030624000562003062400056NM 2003 6 24 CALA0300293 120030607A532069353654 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 2 INCH CRACK AT SCREW HOLE OF INTERCOSTAL AT BS 500D-520, MAIN CABIN FLOOR CENTERLINE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030626000012003062600001NM 2003 6 26 03FDEA00514 120030418A5753 STRUCTURE BOEING727 727200 138407ENM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT WING INBOARD MID FLAP HAS 2 EACH AREAS OF CORROSION. REPAIRED AREAS IAW FED EX SR 27-51-002. 2L73 4F RTA3WE 20030627000012003062700001WP 2003 6 27 GTIA03025N 120030404A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - AFT ACCESSORIED TAIL CONE EMERGENCY LIGHTS INOPERATIVE. T/S TAILCONE EMERGENCY LIGHTS FOUND WIRES DISCONNECTED AND LIGHT ASSEMBLY BROKEN. CONNECTED WIRES TO LIGHT ASSEMBLY. REMOVED BROKEN LIGHT ASSEMBLY. INSTALLED EMERGENCY LIGHT ASSEMBLY. (M) 2L72 4F RTA6WE 20030630000172003063000017NM 2003 6 30 AWXA200300602 120030514A53156546540 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND ON FLOORBEAM WEB AT BS 639, RBL 45-50. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM; FABRICATED A FILLER, DOUBLER, AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-2, FIG. 1, PG. 1. 2L72 4F RTA16WE 20030630000792003063000079SW 2003 6 30 HEEA087841 120030613A6230406010428109 BUSHING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 MAIN ROTOR HEAD BUSHING SET WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000402003070100040SW 2003 7 1 HEEA086957 120030603A2435303001383 BRUSHES BELL 407 407 1182206SW STARTER GEN FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH3754 95175 53378 STARTER GEN WILL NOT START. REPLACED 4 EACH BRUSHES 30300-1383 DUE TO WORN. REPAIRED. 1G71 3U O H2SW 20030624001022003062400102NM 2003 6 24 DL73K030481 120030520A3350S283T0143 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27323DL 23095 DOOR 1L EMERGENCY OVERHEAD LIGHT INOPERATIVE. REPLACED M1133 POWER SUPPLY. 2L72 4F RTA16WE 20030625000052003062500005EA 2003 6 25 03147621 120030527A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 DURING MAINTENANCE INSPECTION, THE RT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030625000222003062500022EU 2003 6 25 106459B 120030521A6510C635C1003203 DISC UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE TAIL ROTOR DRIVEINOPERATIVE C SC0MO OTHER O OTHER NRNOT REPORTED 1 WP25255SD500 1102 FOUND DURING 500 HOUR INSPECTION: VISIBLE WEAR STEP, REPLACED IAW MFG TECH. NOTE: DISC FREE FLOATS ON MAIN GEAR BOX TAILROTOR OUTPUT SHAFT. (P/N: 632A2108102) WHICH SEES INCREASED WEAR. 1G72 3U3 UNCR0001RD E34NE 20030625000532003062500053EU 2003 6 25 03FDEA00813 120030526A2910 LINE AIRBUS310 A310 EU HYD SYSTEM LEAKING A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25422FE 346 DURING CRUISE, ECAM SIGNALED GREEN HYD RSVR LO LEVEL. GREEN HYD QUANTITY GAUGE AT RED DOT. FOLLOWED ECAM AND QRH PROCEDURES FOR HYD RSVR LO LEVEL, HYD SYS LO PR, AND L/G EXTENDED USING ALTERNATE GEAR EXTENSION. PERFORMED LEAK CHECK FOUND HYD FLUID LEAKING FROM UNION OF KRUEGER SELECTOR SOLENOID VALVE (ITEM 60 IPC 27-88-03-03/PAGE 1). PACKING ITEM 40 OF IPC 27-88-03-03 SEEKING FOR REPLACEMENT IF AVAILABLE. REF IPC 27-88-03-03 FIGURE 03 SHEET 1 ITEM 40 PACKING P/N NAS1612-6 IAW AMM 27-88-12-4 AND LEAK CHECKED OK. GREEN HYDRAULIC FLUID TOP-UP TO SERVICE LEVEL. RESTORATION OF LANDING GEAR ACTUATING SYSTEM TO NORMAL OPERATING CONDITION ACC TO AMM 32-33- 00-2. 2L72 4F RTA35EU 20030707000242003070700024NM 2003 7 7 AALA20030643 120030608A3350 CONNECTOR BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21322AA 22323 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 20AB INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE CONNECTOR SEAT 20AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030707000352003070700035NM 2003 7 7 AALA20030502 120030424A2120 FILTER BOEING757 757223 1384957NM CABIN DIRTY A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21657AM 24615 EN ROUTE, ACRID FUMES NOTED IN FIGHT DECK AND CABIN. COMPLETED CHECKLIST. THE RIGHT RE-CIRCULATION FAN WAS OBSERVED TO BE OFF. DIVERTED MSY AND LANDED WITHOUT INCIDENT. CLEANED LOOSE DUST FROM RE-CIRCULATION FAN FILTER. REINSTALLED CANNON PLUG ON RE-CIRCULATION FAN. RESET CIRCUIT BREAKERS. PERFORMED RE-CIRCULATION TEST AS REQUIRED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030707000532003070700053WP 2003 7 7 AALA20030632 120030503A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21410AA 49321 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-711 THROUGH L2-715 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707000542003070700054WP 2003 7 7 AALA20030518 120030503A3397 CONTACTOR DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2159523 49915 DURING OVERNIGHT MAINTENANCE, CABIN EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 18-21 INOPERATIVE. RESEATED CABIN EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 18-21 BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707000642003070700064NM 2003 7 7 2003UALA00492 120030612A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE SEAT 1E INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29775UA 26947 BOTH EEL LIGHTS ON SEAT 1E ARE INOPERATIVE. 2L72 4F4 FRTT0001SE E46NE 20030707000722003070700072EA 2003 7 7 QXEA200300769 120030624A4900 APU CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE APU BAY LEAKING A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09606QX 10023 AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED AN AFT LAVATORY SMOKE DETECTOR WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND OIL IN MIXING MANIFOLD AND VERIFIED THAT THE APU WAS LEAKING OIL. DUCTING WAS CLEANED AND MEL WAS CONTINUED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030707000812003070700081NE 2003 7 7 00093 220030528A7200 ENGINE LEAR 24 24E 5170316CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05330TW 330 251458 AIRCRAFT CLIMBING FROM FL410 LT ENGINE FLAMEOUT, RELIGHT AT FL250, CLIMB BACK TO FL330 TO DESTINATION, WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE PERFORMED FLAMEOUT INSPECTION IAW MFG/ MM SEI-186 AND R & R P2 LINE. OPS CK GOOD. 2L72 4J4 J A10CE 1E16 20030707000832003070700083 2003 7 7 03170674 420030619A222070609 CONTROL BOX CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT INOPERATIVE A VTZAO OTHER F FLT CONT AFFECTED LDLANDING 1 EA27674BR 7601 WHILE ON DESCENT WITH AUTOPILOT ENGAGED, STAB FAIL AND MACH FAIL MESSAGES APPEARED. THE STAB AND MACH TRIM WOULD NOT REENGAGE, EMERGERNCY DECLARED AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REPLACED THE HSTCU AND PERFOREMED A SATISFACTORY OPERTIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030707000862003070700086EA 2003 7 7 COMA0360286 120030622A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HYD SYSTEM UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01965CA15966 7131 FLIGHT 5704 GEAR DISAGREE WARNING WHEN GEAR EXTENDED. REPLACED HYDRAULIC PUMP 3A. 2L72 4F4 FRTA21EA E15NE 20030707000912003070700091NM 2003 7 7 DL76L030597 120030628A5714111T501217 RIB BOEING767 767332 1382001NM CENTER WING GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27196DN 28453 LOWER STRUCTURAL DAMAGE REPAIR THE LOWER STRUCTURE OF THE LBL 62.05 LOWER BEAM OF THE CENTER WING WAS BADLY GOUGE TO A BLOWN DUCT FROM FS 915-919. THE DAMAGED SECTION OF CHORD WAS CUT AND REMOVED. A NEW SECTION OF STRUCTURE WAS SPLICED IN WITH STEEL REPAIR ANGLES IAW ER/A 385317-14, REV A. 2L72 4F RTA1NM 20030707001032003070700103EA 2003 7 7 COMA0360293 120030625A3230 DRAG BRACE CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01978CA 7158 FLIGHT 5172 GEAR DISAGREE WARNING AFTER TAKEOFF. LUBRICATED NLG DRAG BRACE. RETRACT CHECK WAS NORMAL. 2L72 4F RTA21EA 20030707001102003070700110WP 2003 7 7 UPS03840863 120030616A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LEFT WING LE LOWER RIB IS CRACKED AT XFS 766.25 STOPDRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001122003070700112WP 2003 7 7 UPS03840865 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE. UPPER RIB IS CRACKED AT XFS 872. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030708000222003070800022EA 2003 7 8 03180671 120030630A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27671BR 7572 DURING MAINTENANCE INSPECTION, EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED WIRE TO EMERGENCY FLOOR TRACK LIGHTING, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030708000612003070800061SO 2003 7 8 SWIA200312098 120030519A532012006158002 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07296SW 120325 CORROSION ON RT FLOOR SUPPORT BUTT STRAP AND OUTBOARD FLOOR CHANNEL UNDER TOILET APPROX. FS 13500. (DISCOVERED DURING C-CHECK.) REMOVED BUTT STRAP AND CHANNEL ADJACENT TO LAV. INSTALLED TWO NEW BUTT STRAPS IAW SRM 51-10-02. P/N: 120-06158-002, 120-06159-501 2L72 4T RTA31SO 20030708000632003070800063EU 2003 7 8 YENA200307 120030607A24003042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15550JB 1891 STRONG BURNING RUBBER ODOR IN CABIN. INSPECTED AREA WHERE ODOR WAS REPORTED TO ORIGINATE FOUND BURNT ODOR FROM SEB (SEAT ELECTRONIC BOX) AT SEAT 9E. INSPECTED WIRES NO DEFECTS NOTED. SEB CONNECTIONS REMOVED AND STOWED, LTV SYSTEM DEACTIVATED AND PLACED ON MEL. PERSONNEL REMOVED AND REPLACED SEB AT 9E AND 10. SYSTEM REACTIVATED OPS CK O.K., MEL CLEARED. 2L72 4F RTA28NM 20030708000662003070800066NM 2003 7 8 ABXA030196 120030610A5511181T41104 STRINGER BOEING767 767281 1385109NM HORIZONTAL STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 RIGHT HORIZONTAL STAB. LOWER STRINGER NO. 10 LOWER HORZ. FLANGE RBL 56, P/N 181T4110-4, FOUND CORROSION DURING INSPECTION ON STRINGER P/N 181T4110-4 COMMON TO SKIN PANEL REMAIN THICKNESS MATERIAL OF 0.135 INCH ORIGINAL THICKNESS WAS 0.165 INCH. THE TOTAL BLENDED AREA WAS APPROXIMATELY 2.5 INCH AND 1 INCH WIDE. REPAIRED AREA IAW REA B655-46297MR. 2L72 4F RTA1NM 20030708000682003070800068NM 2003 7 8 ABXA030198 120030610A5311145T10032 FRAME BOEING767 767281 1385109NM FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 RIGHT STA. 883.5 FRAME SEGMENT P/N 145T1003-2 FAIL SAFE FRAME AT STR. 18 RIGHT WAS FOUND CORRODED. THE ORIGINAL THICKNESS OF FRAME WAS 0.200 INCH AFTER BLENDED OUT CORROSION THE REMAINING THICKNESS WAS 0.170 INCH. REPAIRED AREA IAW REA B653-46282, REV. 'A'. 2L72 4F RTA1NM 20030708000782003070800078NM 2003 7 8 AWXA200300649 120030514A5311654655219 FRAME BOEING737 737277 1384570NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A .5000 INCH CRACK WAS FOUND ON FUSELAGE LOWER LOBE FRAME AT BS 827, LBL 22. MAINTENANCE TRIMMED OUT DAMAGE ON FUSELAGE LOWER LOBE FRAME AT BS 827, LBL 22, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED FILLER, RADIUS FILLER, SHEAR TIE, AND TIE CLIP; INSTALLED REPAIR PARTS IAW SRM 53-10-4, FIG. 11. 2L72 4F RTA16WE 20030708000792003070800079NM 2003 7 8 AWXA200300650 120030516A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 4.7, WL 201-202. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW SRM 53-10-08, PG. 270-280. 2L72 4F RTA16WE 20030708000932003070800093WP 2003 7 8 UPS03840929 120030618A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE ACCESSORY BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, AFT ACCESSORY COMPT. STA. 1600-1620 AT RBL 45 SEAT TRACK REPAIR IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION STATION 1590-1610 AT RBL 45, AND REPLACED SEAT TRACK SPLICE STATION 1600-1620 IAW SRM 53-2-3 FIG. 14 2L74 4F4 FRT4A25 E2GL 20030708000952003070800095WP 2003 7 8 UPS03840931 120030616A531057729103 DOOR FRAME DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3 52039NE FUSELAGE MISLOCATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C, MAIN CABIN AT STA 1660-R2 DOOR JAMB WEB HAS DOUBLE DRILLED HOLES. REM FASTENERS FROM DOOR JAMB WEB. REM AIR GRILL AND R2 DOOR DRAIN PAN. TRIMMED OUT DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 DWG DC8-53A-01 0 AND UPS EO DC8-5310-11728-A FAB 99 ANGLE, REP STRAP AND NEW DOOR JAMB WEB IAW DAC DWG 5772756 AND REO G09326. ALOD PRIMED IAW SRM 51-1-8. INSTALL WEB AND REPAIR STRAP IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F4 FRT4A25 1E8 20030630000832003063000083SW 2003 6 30 HEEA087845 120030621A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 BLADE CLIMBS IN FLIGHT; UNABLE TO TRACK. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030630000862003063000086SW 2003 6 30 HEEA087848 120030615A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03741PH 53457 MAIN ROTOR BLADE LEADING EDGE CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030630000872003063000087SW 2003 6 30 HEEA087849 120030614A5610407030115123 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 WINDSHIELD CRAZED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701001542003070100154EA 2003 7 1 A6WA200340088 120030609A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA TE FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 LEFT OUTBOARD FLAP HAS A DENT ON THE INBOARD SIDE OF THE FLAP VANE. REMOVED AND REPLACED DAMAGED LEFT OUTBOARD FLAP VANE, P/N 601R14571-7 IAW CRJ 200 SRM 51-42-11, 51-23-00, 51-25-16, 51-42-21 AND WVAC EO 601R-57-4088. (M) 2L72 4F RTA21EA 20030702000482003070200048WP 2003 7 2 GTIA030397 120030518A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND PASSENGER CABIN FLOOR PANEL AT FS 1250-1303 CENTER, PANEL HONEY COMB EDGE BROKEN. FABRICATED FLOOR PANEL. (M) 2L72 4F A6WE 20030702000502003070200050WP 2003 7 2 GTIA030399 120030513A5340 FITTING DOUG DC9 DC981 3022081WP NLG WW CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND NOSE WHEEL WELL, STATION 70 LBL 16 AND RBL 16, TWO FITTINGS CRACKED. REMOVED TWO FITTINGS. LOCATED AND DRILLED HOLES ON TWO NEW FITTINGS. INSTALLED TWO NEW FITTINGS. (M) 2L72 4F A6WE 20030707000362003070700036NM 2003 7 7 AALA20030560 120030411A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21773AN 29583 DURING OVERNIGHT MAINTENANCE, FORWARD LT LOWER FORWARD FACING EMERGENCY EXIT PATH LIGHTING IN THE G3 GALLEY COAT CLOSET WALL IS BROKEN. REPLACED FORWARD LEFT LOWER FORWARD FACING EMERGENCY EXIT PATH LIGHTING ASSEMBLY ON THE G3 GALLEY COAT CLOSET WALL. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030707000962003070700096NM 2003 7 7 DL738030603 120030701A3350 LIGHT BOEING737 737832 13844CFNM CABIN INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO273754A 29626 FOUND ON L/O EMERGENCY AISLE FLOOR LIGHTS FROM SEAT 10DEF TO 15DEF INOPERATIVE. REPLACED FUSE F1 AT BATTERY POWER SUPPLY. RECONNECTED ALL 10 SEAT LIGHT ASSEMBLY HARNESS. OPN GOOD 2L72 4F RTA16WE 20030707001362003070700136NM 2003 7 7 AWXA200300709 120030609A53156546812189 FLOORBEAM BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOORBEAM AT BS 996, LBL 38, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOORBEAM BS 996, LBL 38, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW SRM 51-40-02, PG. 10 AND 11, FIG. 12. 2L72 4F4 FRTA16WE E2GL 20030707001392003070700139SO 2003 7 7 SMT2003F00001 120030512A243437D22355 DRIVE BELT PIPER PA32 PA32R301 7103218SO LYC O540 IO540K1G5 41532EA ALTERNATOR FAILED E SMTRO OTHER O OTHER NRNOT REPORTED 1 EA174148010 3246147 L3704348A AIRCRAFT HAS BEEN SUBJECT TO NUMEROUS ALTERNATOR AND AIR CONDITIONING COMPRESSOR DRIVE V BELT FAILURES. SOME WITH LESS THAN 10 HOURS TIME IN SERVICE WITH FIRST FAILURE OCCURRING AT 25 HOURS AIRCRAFT TOTAL TIME SINCE NEW. THE AIR CONDITIONING COMPRESSOR HAS BEEN REPLACED. PULLEY ALIGNMENT AND IDLER PULLEY CONDITION HAVE BEEN INSPECTED WITH NO DEFECTS NOTED. WITH THE LATEST FAILURE THE ALTERNATOR PULLEY WAS REPLACED DUE TO SCORING AND DISCOLORATION AND A NEW SET OF DRIVE BELTS AND WERE INSTALLED. BELT TENSION WAS ADJUSTED IAW MM. AIRCRAFT WAS GROUND RUN AND BELT TENSION RECHECKED AND FOUND TO BE WITHIN LIMITS. BELT TENSION AND CONDITION HAS SINCE BEEN RECHECKED AFTER 10 HOURS TIS WITH NO DEFECTS NOTED. 1L71 3O3 O A3SO 1E4 20030707001512003070700151CE 2003 7 7 DXT2003F00000 120030610A323099146371 MANIFOLD CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL SOLENOID SHORTED E DXTAO OTHER O OTHER NRNOT REPORTED 1 GL07964QS951 7500164 AFTER TAKEOFF LANDING GEAR FAILED TO RETRACT AND OPENED LEFT MLG BREAKER. RSETTING BREAKER OPEN AGAIN. EMERGENCY GEAR BLOW-DOWN INITIATED AND LANDED AT AIRPORT HANGER. OPERATIONAL CHECK CONFIRMED DISCREPANCY. FOUND SHORTED SOLENOID IN GEAR CONTROL MODULE. REPLACEMENT OPERATION CHECK SATISFACTORY. 2L72 4J4 FRTT00007WITE6CH 20030707001692003070700169NM 2003 7 7 P5CA0300887 120030611A3250 ACTUATOR BOEING747 7472D3B 1384805NM NLG STEERING BROKEN A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23505MC 21251 LEFT BODY GEAR LIGHT "UNLOCKED" WOULD NOT COME ON IN PRIMARY OR ALTERNATE ON TAXI BACK LIGHTS CAME ON. ITEM TRANSFERRED TO DMI NR 30932 IAW DDPG 32-17-C BODY GEAR STEERING ACTUATORS VERIFIED LOCKED. REQUIRES FURTHER TROUBLE SHOOTING 2L74 4F RTA20WE 20030707001742003070700174WP 2003 7 7 ARWA20030604 120030611A2910 LINE DOUG DC8 DC861 3021952WP HYD SYSTEM LEAKING A ARWAO OTHER K FLUID LOSS CRCRUISE 1 SO1929UA 46159 LOSS OF HYDRAULIC FLUID DOWN TO STAND-PIPE. LOSS OF HYDRAULIC CHECK LIST COMPLETED. INSPECTED NR 3 PYLON FOR EVIDENCE OF HYDRAULIC LEAK, FOUND RIGID LINE DAMAGED INSIDE PYLON AREA; REMOVED AND REPLACED RIGID LINE ASSEMBLY AS REQUIRED IAW MM 20-12-0; OPERATIONAL CHECK NORMAL IAW MM 29-00 AND MM 29-10-12; NO LEAKS FOUND. SERVICED RESERVOIR IAW 12-30-1. 2L74 4F 4A25 20030708000962003070800096WP 2003 7 8 UPS03840932 120030603A531457504121N ANGLE DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3 52039NE KEELBEAM COVER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C, R/W/W KEEL BEAM INSIDE ACCESS DOVER STA 935, BEAM IS CRACKED REM MLG LT AND RT DOOR ACTUATORS, LT AND RT W/W WEBS TO FOM. LOC DRI LLED AND INSTALLED NEW SPLICE ANGLE IAW DAC DWG 5750371 P/N 5750042- 1N. FAB -51, -53, -55, -57 AND -59 REPAIR PARTS IAW DAC DRAWING 575041 2. INSTALLED REP PARTS, ATT COMPONENTS AND NEW SECTION OF WEB IAW DAC DWG 5750412, DC8 SRM 51-1-20D. INST MLG LT AND RT ACTUATORS. 2L74 4F4 FRT4A25 1E8 20030708001112003070800111WP 2003 7 8 GTIA030428 120030519A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND DENT AT FS 359 BETWEEN LONGERONS 20 AND 21R. DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED ONE DOUBLER. INSTALLED ONE DOUBLER REPAIR. (M) 2L72 4F A6WE 20030709000112003070900011NE 2003 7 9 AALA20030617 220030530A7200 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE LEFT SURGES A AALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW21197AN 32391 ON TAKEOFF ROLL AT ORD, LEFT ENGINE AT STD POWER SETTING STARTED SURING BETWEEN 1.5 AND 1.6 EPR SEVERAL TIMES ABORTED TAKEOFF. (M) 2L72 4F4 FRTA2NM E12EU 20030709000182003070900018WP 2003 7 9 AALA20030574 120030516A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21577AA 53154 DURING OVERNIGHT MAINTENANCE, AFT TAIL OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED AFT TAIL OVERHEAD EMERGENCY EXIT ILGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000282003070900028WP 2003 7 9 AALA20030520 120030503A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217514A 49891 DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT LIGHTS COMMON TO EMERGENCY EXIT LIGHT BATTERY PACK B5 101 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000312003070900031WP 2003 7 9 AALA20030488 120030423A3350 CONTACTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21454AA 49559 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT LAVATORY ARE INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000402003070900040WP 2003 7 9 AALA20030483 120030421A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21271AA 49293 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 18-21 INOPERATIVE. REPAIRED CEILING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000452003070900045WP 2003 7 9 GTIA030441 120030516A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLOORBOARD, OUTBOARD LEFT AFT, STATION 1250 TO 1361, STIFFENER DISBONDED. INSULATION MISSING AND TORN. REPAIRED FLOORBOARD. (M) 2L72 4F A6WE 20030707001612003070700161NM 2003 7 7 AWXA200300724 120030610A53206545834260 STIFFENER BOEING737 7373Y0 1384671NM FLOOR SUPPORT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT STIFFENER AT BS 318, LBL 10, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED CORRODED FLOOR SUPPORT STIFFENER BS 318, LBL 10, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11. 2L72 4F RTA16WE 20030707001882003070700188WP 2003 7 7 UPS03840924 120030617A5340 SEAT TRACK DOUG DC8 DC873F 302199FWP CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, MAIN CABIN SEAT TRACK IS CRACKED AT STA. 1000 AT RBL 45 REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION STATION 990 TO 1110 IAW SRM. 53-2-3 FIG. 14 2L74 4F RT4A25 20030707002032003070700203WP 2003 7 7 UPS03840878 120030616A5754576958927 DOUBLER DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335 REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG.5769589,AND SRM. 51-1-20D,51-1-21 2L74 4F RT4A25 20030708000202003070800020EA 2003 7 8 03178661 120030627A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ROW 5 INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27661BR 7520 DURING MAINTENANCE INSPECTION, EMERGENCY LIGHT AT ROW 5 WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED FUSELAGE EMERGENCY LIGHT, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030708000322003070800032EU 2003 7 8 DHL2003366517 120030607A5311R5397405820000 FRAME AIRBUS300 A300B4203 3930306EU GE CF6 CF680 30025NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 FOUND CORRODED AT L45. RECEIVED NEW FRAME R5397405421093 FOR A/C 366DH AND FRAME COUPLING R5397405820000, SEGMENT 64 FOUND TO BE OUT OF LIMITS IAW SRM 53-17-00. ORG. THICKNESS .068 REMAINING THICKNESS .0, REMOVED DAMAGE SEGMENT FR. 64 IAW A300 SRM 53-17-00,LOCATED, DRILLED NEW FRAME R5397405421093 AND FRAME COUPLING R5397405820000 IAW SRM 53-17-00 PAGE 765/766 FIG. 713, INSTALLED NEW FRAME AND COUPLING IAW SRM 53-17-00,REMOVED AN INSTALLED PANEL IAW SRM 51-30-30. 2L72 4F4 FRTA35EU E13NE 20030708000572003070800057SO 2003 7 8 SWIA200312094 120030609A27503471001001 PANEL EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FLAP ANNUNCIATORMALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07214SW7358 7358 120280 AFTER TAKEOFF, OUTBOARD FLAPS WOULD NOT COMPLETELY RETRACT AND FLAP DISAGREEMENT INDICATED. QRH, RECYCLED AND WOULD NOT CORRECT. FLAPS CAME DOWN FINE BUT WILL NOT RETRACT IN AIR. ON GROUND THEY RETRACT COMPLETELY. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL WITH SERVICEABLE UNIT IAW MM 27-50-05. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20030708000602003070800060SO 2003 7 8 SWIA200312097 120030519A5753 BRACKET EMB 120 EMB120ER 3260203SO LT NACELLE FLAP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07296SW 120325 LT NACELLE FLAP BRACKET CRACKED INSIDE. (DISCOVERED DURING C-CHECK.) REPLACED INSIDE OUTBOARD BRACKET ON LEFT NACELLE FLAP. 2L72 4T RTA31SO 20030709000532003070900053WP 2003 7 9 GTIA030423 120030511A5320 PANEL DOUG DC9 DC981 3022081WP INTERIOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND AFT ACCY COMPARTMENT OVERHEAD INTERNAL WEB PANEL CRACKED AT AFT END AT FS 1485 CANT FRAME 24 INCHES LBL. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030709000882003070900088SO 2003 7 9 C2XA03CL105 120030606A3230355022002MOD2 ELECTRICAL BOX EMB 135 EMB135ER 3260203SO LANDING GEAR FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714505 145192 CLE FLIGHT 2226 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030709000902003070900090NM 2003 7 9 371PA0021 120030607A3350 LIGHT BOEING737 737306 13844BGNM ROW 23 TO 26 INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05371PA 23543 EMERGENCY EXIT LIGHTS ROW 23 TO 26 INOP. RESECURED LAST STRIP OF FLOOR LIGHTING. OPS CHECKS GOOD IAW MM 33-51-02. 2L72 4F RTA16NE 20030709000982003070900098SO 2003 7 9 C2XA03IA062 120030610A2120 SMOKE EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714977 145175 THE CREW NOTED SMOKE IN THE COCKPIT. THE CREW DECLARED EMERGENCY AND DIVERTED TO MEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF SMOKE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709000992003070900099GL 2003 7 9 C2XA03BT066 220030609A7230 BLADE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE DIRTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW27115485381 653 145565 CAE311316 CREW REPORTED ON POST FLIGHT FOUND TAR ON FAN BLADES OF NR 1 ENGINE. MAINTENANCE PERFORMED INSPECTION FOR FOD ON THE NR 1 ENGINE FAN BLADES, FAN BYPASS VANES. FOUND TAR RESIDUE PASSED CLEAR OF INTERNAL SURFACES. CLEANED FAN BLADES AND FAN BYPASS VANES. PERFORMED BOROSCOPE INSPECTION OF THE COMPRESSOR SECTION IAW REFERENCE AE3007 MM 72-30-00-200-801, UP TO AND INCLUDING INLET GUIDE VANES. FOUND NO EVIDENCE OF FOD INGESTION. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20030709001022003070900102CE 2003 7 9 GLBA2003078 120030607A27501015210303 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS INOPERATIVE A GLBAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM03247GL UE247 FLAPS WOULD NOT RETRACT BEYOND 17 DEG. REPLACED THE SPLIT FLAP LINKS ON BOTH SIDES. 2L72 4T RTA24CE 20030709001092003070900109SO 2003 7 9 C2XA03SH179 120030612A541014576057621 STRUCTURE EMB 145 EMB145LR 3260212SO NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK THE NUMBER ONE UPPER COWLING AFT EDGE MEMBER WAS FOUND CHAFED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709001252003070900125EA 2003 7 9 03164672 120030613A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27672BR 7594 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030707001282003070700128NM 2003 7 7 CALA0300328 120030623A5330 SKIN BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711651 28912 INSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN OUTBOARD OF EE ACCESS DOOR AT STA 338 BETWEEN STRINGER 24R AND 25R. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5330-03260. 2L72 4F4 FRTA16WE E2GL 20030707001302003070700130NM 2003 7 7 CALA0300330 120030602A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 1 INCH CRACK IN THE INNER CHORD OF THE LT FRAME AT STA 616. REPAIRED IAW ECRA 5311-01150. 2L72 4F RTA16WE 20030707001322003070700132NM 2003 7 7 CALA0300331 120030513A5330 SKIN BOEING737 737724 13844BYNM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND TWO DENTS IN FUSELAGE SKIN AT BS 385, BETWEEN S17L AND 18L. THE DENTED AREA WAS REPAIRED IAW ECRA 5331-01126. 2L72 4F RTA16WE 20030711001232003071100123WP 2003 7 11 MWEA030262 120030630A5755S124681014016 SKIN DOUG DC9 DC982 3022082WP RT WING SPOILER DEBONDED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RIGHT WING GROUND SPOILER HAS A PREVIOUS REPAIR ON TOP SURFACE AT OUTBOARD AFT CORNER THAT IS DEBONDING. FABRICATED AND BONDED NEW DISC TO SPOILER. 2L72 4F A6WE 20030714000212003071400021NM 2003 7 14 SWAA031393 120030622A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 520 AT STR 16L AND BS 727E AT STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030714000602003071400060NM 2003 7 14 SWAA031362 120030618A33506104781 BATTERY BOEING737 7372T4 1384492NM EMERGNECY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030714000792003071400079NM 2003 7 14 SWAA031414 120030625A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030714000902003071400090NM 2003 7 14 SWAA031348 120030616A53106545871 DOOR FRAME BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR FRAME LOWER HINGE CUTOUT CRACKED. REPAIRED FRAME PER SRM. 2L72 4F A16WE 20030714001222003071400122NM 2003 7 14 CALA0300355 120030701A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND A 2 INCH CRACK IN CENTER FLOOR SUPPORT AT STA 540 LEFT OF CENTER. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030716000012003071600001NM 2003 7 16 2003F00403 120030314A5320 FLOOR SUPPORT BOEING727 727222 1384073NM FUSELAGE DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND DENT ON AFT CARGO COMPARTMENT FLOOR SUPPORT, STATION 950E, LBL 10. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED PARTS ON AFT CARGO FLOOR SUPPORT LBL 10 STATION 950E. (M) 2L73 4F A3WE 20030716000022003071600002NM 2003 7 16 2003F00404 120030314A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND DENTS ON FORWARD CARGO FRAME AT BS 700, STRINGER 24L/25L. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATION 700 STRINGER 24L AND 25L. (M) 2L73 4F A3WE 20030716000242003071600024NM 2003 7 16 2003F00416 120030313A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, OFUND CRACK ON LOWER LEFT PANEL MOUNT FRAME AT LOWER END, BS 720. FABRICATE REPAIR ANGLE. ALODINED, PRIMED AND INSTALLED NEW ANGLE AT LOWER LEFT PANEL MOUTN FRAME STATION 720. (M) 2L73 4F A3WE 20030717000132003071700013 2003 7 17 HEEA087990 420030629A34427007700614 DISPLAY BELL 214 214ST 1182106SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M 28102 WEATHER RADAR DISPLAY SCREEN DARK AND FUZZY. TO BE SENT TO VENDOR FOR REPAIR. 2G72 4U H10SW 20030701000412003070100041SW 2003 7 1 HEEA086958 120030603A2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X4352 53267 STARTER GEN FELL OFF LINE AND THEN STARTER WOULD NOT MOTOR. REPAIRED. 1G71 3U O H2SW 20030702000402003070200040WP 2003 7 2 GTIA030393 120030520A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND AFT ACCY COMPARTMENT WEB CRACKED AT FS 1485 APPROX 20 INCHES RBL. REMOVED CRACKED WEB. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. UPON FURTHER INSPECTION FOUND CHAFING AND CRACK. STOP DRILLED CRACK. NO DOUBLER REQUIRED. INSTALLED REPAIR WEB. (M) 2L72 4F A6WE 20030702000472003070200047WP 2003 7 2 GTIA030395 120030509A5543 TAB DOUG DC9 DC982 3022082WP RUDDER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND RUDDER TAB AREAS OF DELAMINATED. REPAIRED DAMAGE ON RUDDER TAB. (M) 2L72 4F A6WE 20030707001502003070700150NM 2003 7 7 QXEA200300772 120030624A5210 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM PAX DOOR INOPERATIVE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09413QX 4060 THE CREW REPORTED THAT THE REAR PASSENGER DOOR WILL NOT OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED AND LUBED THE DOOR LOCK AND ACTUATING SYSTEM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20030707001672003070700167NM 2003 7 7 AWXA200300634 120030513A5755654645161B PANEL BOEING737 737277 1384570NM SPOILER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - FLIGHT CONTROL - DURING C-15 CHECK THE NO. 8 SPOILER WAS FOUND DELAMINATED AT THE MID CENTER AFT EDGE. MAINTENANCE REMOVED AND REPLACED THE NR 8 SPOILER PANEL IAW BMM 27-62-91, PG. 401. 2L72 4F RTA16WE 20030707001812003070700181EU 2003 7 7 AWXA200300748 120030611A5315D5347209800000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND AT TWO PLACES ON UPPER SURFACE OF FLOORBEAM AT FR 66, Y-915. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOORBEAM Y-915, FROM FR 65 TO FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 28-30. 2L72 4F RTA28NM 20030707001852003070700185EU 2003 7 7 RAIA00305151 120030527A3350AML44 BULB AEROSPATR42 ATR42300 8680920EU EMERGENCY LIGHT BURNED OUT A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03422TE 106 AFT EMERGENCY LIGHTS AT F/A SEAT AND CEILING INOP. REMOVED AND REPLACED BULBS. 2H72 4T RTA53EU 20030707001872003070700187NM 2003 7 7 UPS03440840 120030515A5320 STRAP BOEING747 747200 1384847NM PAX DOORFRAME CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - R1 DOOR FRAME LWR HINGE CUTOUT STRAP FOUND CRACKED AS MARKED. LOWER HINGE CUTOUT REPAIRED IAW SRM 52-10-02 FIG.12. 2L74 4F RTA20WE 20030708000042003070800004 2003 7 8 GLBA2003100 420030703A34256229681001 DISPLAY BEECH 1900 1900D 1154162CE EFIS INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03169GL14544 UE169 FO EHSI WENT BLANK, REMOVED AND REPLACED FO LOWER EFIS DISPLAY. OPS CHECKED GOOD. 2L72 4T RTA24CE 20030708000092003070800009NM 2003 7 8 DHL2003746009 120030703A5410 FIRE SEAL BOEING727 727224 1384076NM NR 1 ENGINE UNSECURE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01746DH 22252 1) NR 1 FIRE FAULT LOOP LIGHT ILLUMINATED. 2) FOUND NR 1 ENGINE FIRE LOOP UNSECURED NEXT TO FCU. RESECURED FIRE LOOP AND OPS CHECKED SERVICEABLE IAW M/M 26-11-00. 2L73 4F A3WE 20030708000102003070800010NM 2003 7 8 DHL2003750004 120030704A3350 BATTERY BOEING727 7272M7 138407SNM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01750DH 21951 BOTH EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE DURING THE STANDBY POWER CHECK. REPLACED BATTERIES IN BOTH EXIT LIGHTS IAW 727 M/M 33-50-111 OPS CHECKED NORMAL. 2L73 4F A3WE 20030708000162003070800016EA 2003 7 8 COMA0360302 120030625A5297K601R507474S WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE DOOR UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01798CA 7348 FLIGHT 5481 CABIN DOOR STOW HANDLE CAUTION MESSAGE. REPLACED DOOR WIRE HARNESS. 2L72 4F4 FRTA21EA E15NE 20030708000172003070800017NM 2003 7 8 03179411 120030628A3350 LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE LAVATORY INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27411FJ 3166 DURING MAINTENANCE INSPECTION, LAVATORY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED LAVATORY EMERGENCY LIGHT, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 FRTA55NM E35NE 20030708000192003070800019EA 2003 7 8 03180705 120030630A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27705BR 7470 DURING MAINTENANCE INSPECTION, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM ROW 2 THRU 5. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY FLOOR LIGHT TRACK COVER, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030708000242003070800024EA 2003 7 8 03164636 120030613A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27636BR 7307 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISCOVERED THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030708000362003070800036WP 2003 7 8 DHL2003801079 120030408A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 MAIN CARGO COMPT. NR 6 TRACK LUGS WORN (STA. 280.000 - STA. 321.000) REMOVED NR 6 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG.49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG. 49-50. 2L74 4F4 FRT4A25 E2GL 20030708000392003070800039WP 2003 7 8 UPS03840900 120030602A52104751734 DOUBLER DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3B 52039NE PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3, L2 DOOR UPPER FWD CORNER SHOWS CRACK INDICATION WITH XRAY INSPECTION. REMOVED CRACKED INTERNAL SKIN DOUBLER AND PARTIALLY REMOVED WEB TO FOM. FAB NEW INTERNAL SKIN SPLICE DOULBER IAW DWG NR 4751734 AND PRIMED IAW DC8 SMR 51-1-8, THEN INSTALLED DOUBLER AND WEB IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-21A, 51-1-17 AND DAC DWG 4751734 2L74 4F4 FRT4A25 1E8 20030709001272003070900127NM 2003 7 9 03165405 120030614A2697 WIRE DORNERDO32 DO328300 NM FIRE LOOP LOOSE A VTZAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27405FJ 3155 DURING TAXI, THE CREW REPORTED THAT THE RT ENGINE FIRE INDICATION HAD ILLUMINATED AND DISCHARGED THE EXTINGUISHER BOTTLES. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPAIRED LOOSE WIRE SHIELDING ON THE RT ENGINE FIRE DETECTOR INNER LOOP. AN ENGINE RUN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030710000132003071000013EU 2003 7 10 ASOA03239 120030521A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11634AS 370 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FRAMES 36 AND 41 ON THE TOP AND BOTTOM SIDES AROUND THE NUT PLATES WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED LEFT SEAT TRACK BETWEEN FRAMES 36 AND 41 ON THE OTP AND BOTTOM SIDES AROUND THE NUT PLATES IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20030710000232003071000023EU 2003 7 10 ASOA03236 120030527A215022051204 ACM AEROSPATR72 ATR72 EU FUSELAGE INOPERATIVE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11640AS 405 DURING CRUISE, A BURNING ODOR OCCURRED IN THE CABIN AND THE RT PACK BECAME INOPERATIVE. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE ACM INCLUDING THE CLAMPS ON THE TWO BELLOWS OF THE HEAT EXCHANGER. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030710000342003071000034NM 2003 7 10 USAABB03087 120030603A2750849701 PSEU BOEING767 7672B7 1385107NM TE FLAPS MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19655US 25257 APPROXIMATELY 2 HOURS AFTER DEPARTURE, THE CONFIGURATION LIGHT ILLUMINATED AND THE CREW RECEIVED THE EICAS MESSAGE 'FLAPS'. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TRIED THE BITE ON THE PSEU AND RECEIVED NO RESPONSE. THE PSEU WAS REPLACED. (M) 2L72 4F RTA1NM 20030710000482003071000048NM 2003 7 10 DHL2003747515 120030513A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK, N/R 53604 IN AFT CARGO FRAME BS 1050 HAS A DENT INTO THE RADIUS BELOW STR 26 L. CUT OUT DAMAGED AREA DIM 1 INCH X 1 INCH AND FABRICATED ONE DOUBLER DIMENSIONS 10 INCH X 6 INCH USING 7075-T6 .071 PO 9912380 IAW B-727 SRM 51-40-3 FIG 1. ALODINED AND PRIMED REPAIR DOUBLER IAW B-727 SRM 51-10-3. INSTALLED BS 1050 FRAME REPAIRS IAW B-727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20030710000722003071000072NM 2003 7 10 DHL2003746501 120030601A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE HAS DENT AT STR. 21L-22L BETWEEN STA 400-420. FOUND DENT TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT-OUT DAMAGE AREA DIM 1 INCH CIRCULE IAW B-727 SRM 53-30-1 FIG 1 AND 53-30-3 FIG 13. FAB DOUBLER INTERNAL REPAIR MAT 2024-T3 .050 PO 9912624 DIM CIRCULE 3.875 INCH AND FILLER MAT 2024-T3 .040 PO 9912182 DIM .875 INCH CIRCULE IAW B-727 SRM 53-30-3 FIG 13 AND 53-30-2 FIG 2. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBLER INTERNAL REPAIR IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20030710000872003071000087NM 2003 7 10 DHL2003721005 120030607A26111601173 BATTERY BOEING727 727228 1384083NM SMOKE DETECTOR INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01721DH 19545 LOWER CARGO SMOKE DETECTOR FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERIES IN SMOKE DETECTOR S/N: 4530. OPS CHECKED GOOD IAW B727 M/M 26-16-01. 2L73 4F RTA3WE 20030710000912003071000091 2003 7 10 375PA0016 420030614A2210 CONNECTOR BOEING737 737317 138447PNM FUEL METERING DIRTY A PIDAO OTHER J WARNING INDICATION CRCRUISE 1 SO05375PA 23812 VARIOUS ANOMALOUS (SIC) INDICATIONS FROM FMA/MCP. A/T ANN RAPIDLY CHANGES MODES, SPURIOUS ALTITUDES APPEAR. IN ALT HOLD A/C CLIMBS & DESCENDS +/- 300 FT. VS MODE CYCLES, ALT HOLD CYCLES. CLEANED AND CHECKED EFIS RT AND CLEANED CONNECTOR TO THE FMA. PERFORMED CHECK THRU CDU. NO DUPLICATE FAILURES PER MM 22-10-00. 2L72 4F RTA16WE 20030710000942003071000094CE 2003 7 10 GLBA2003072 120030602A2150 PRESSURE SWITCH BEECH 1900 1900 1154160CE MALFUNCTIONED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03245UE 245UE RIGHT EVIR ILLUM, ON T/O ROLL. CHECKED THE PRESSURE SOLENOID FOR OPERATION AND LEAKAGE AND RIGHT PROP PRESSURE SWITCH FOR PROPER OPERATION, BOTH GOOD. CHECKED RIGHT ENVIR TEMP AND PRESSURE, OPS CHECK GOOD. 2L72 4T RTA24CE 20030710000982003071000098CE 2003 7 10 GLBA2003084 120030616A7712 INDICATOR BEECH 1900 1900D 1154162CE RT TORQUE STUCK A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03184GL UE184GL RIGHT TORQUE INDICATOR STUCK AT 300 LBS. SWAPPED IND SIDE TO SIDE FOR TROUBLESHOOTING PURPOSES, OPS CK GOOD ON GROUND RUN. 2L72 4T RTA24CE 20030710001012003071000101EA 2003 7 10 03160699 120030609A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FAULTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27699BR 7801 DURING CLIMB, THE CREW REPORTED AN INDICATION OF SMOKE IN THE CARGO COMPARTMENT THE CARGO FIRE BOTTLES WERE BLOWN. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED CARGO SMOKE DETECTORS AS A PRECAUTIONARY MEASURE AND INSTALLED NEW FIRE BOTTLES. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030710001032003071000103WP 2003 7 10 DHL2003806010 120030615A2611327 LAMP DOUG DC8 DC873F 302199FWP SMOKE DETECTOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01806DH 46002 NR 6 UPPER DECK SMOKE DETECTOR WILL NOT TEST. DEFERRED NR 6 SMOKE DETECTOR IAW MEL 26-6-2 CAT C. DMI 13267 PLACARD IS INSTALLED. REF DMI 13267 NR 6 UPPER DECK SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 6 MAIN CARGO COMPARTMENT SMOKE DETECTOR AS PER MM 26-10-5. OPS NORMAL. THIS CLEARS DMI 13267. 2L74 4F RT4A25 20030710001062003071000106SO 2003 7 10 C2XA03SH187 120030618A531014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030710001102003071000110SO 2003 7 10 C2XA03SH191 120030618A532014522460015 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK THE AFT BUTTSTRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030708000522003070800052SO 2003 7 8 CY42003F00000 220030331A8530TIST712ACA CYLINDER HEAD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE SEPARATED A CY4RO OTHER O OTHER NRNOT REPORTED 1 AL036492H87 20700544 247848R CYLINDER HEAD SEPARATED FROM THE BARREL. 1H71 3O3 O A16CE E5CE 20030709000132003070900013WP 2003 7 9 AALA20030539 120030506A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21406A 49317 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHTING AFT OF ROW 23 INOPERATIVE. REPLACED EMERGENCY EXIT AISLE LIGHT ASSEMBLY BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030710000252003071000025EU 2003 7 10 ASOA03241 120030521A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11634AS 370 DURING A C-CHECK, THE FLOOR SUPPORT FLANGE INBOARD OF THE SERVICE DOOR THRESHOLD PLATE BETWEEN FRAMES 36 AND 39 ON THE OTP AND BOTTOM SIDES AROUND THE NUT PLATES WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT FLANGE INBOARD OF THE SERVICE DOOR THRESHOLD PLATE BETWEEN FRAMES 36 AND 39 ON THE TOP AND BOTTOM SIDES AROUND THE NUT PLATES IAW SRM 53-81-00 AND SRM 51-25-02. (M) 2H72 4T RTA53EU 20030710000552003071000055NM 2003 7 10 DHL2003745011 120030523A2510808737631 SEAT BOEING727 727224 1384076NM COCKPIT MALFUNCTIONED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01745DH 20665 FIRST OFFICERS SEAT WILL NOT LOCK INTO PLACE WHEN ADJUSTED FORWARD OR AFT. REMOVED AND REPLACED F/O'S SEAT. OPS CHECKED GOOD IAW M/M 25-10. 2L73 4F A3WE 20030710001072003071000107SO 2003 7 10 C2XA03SH188 120030618A531014522178005 THRESHOLD EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030710001192003071000119SO 2003 7 10 C2XA03CL112 120030618A33977287500601 WIRE HARNESS EMB 145 EMB145 3260210SO CABIN BURNED A C2XAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW2715973 145159 CLE FLIGHT 2109 THE CREW REPORTED A BURNING ODOR WHILE TAXIING AND 2BC SIDEWALL LIGHT ASSEMBLY WAS INOPERATIVE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE SIDEWALL LIGHT HARNESS ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030710001272003071000127CE 2003 7 10 GLBA2003086 120030618A2120 ODOR BEECH 1900 1900D 1154162CE CABIN DETECTED A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM03255GL UE255 SMOKE ODOR IN CABIN. INSPECTED A/C, NO DISCREPANCIES NOTED. OPERATIONAL CK FLIGHT SATISFACTORY. 2L72 4T RTA24CE 20030710001312003071000131EU 2003 7 10 MALA030303 120030601A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4K INSPECTION IN CWA, CENTER AISLE SEAT TRACK HAS CORROSION. MAINTENANCE REPLACED SEAT TRACK BL 0 STA 294-329. REF 409 NR 179528 FOR DETAIL. A/C RELEASE DATE 6/6/03. 2L72 4T RTA52EU 20030710001332003071000133EU 2003 7 10 MALA030311 120030616A3520 GUARD BAC 146 AVRO146RJ85A1500097EU SWITCH FAULTY A MALAG O2 MASK DEPLOYED O OTHER NRNOT REPORTED 1 GL15513XJ E2329 AFTER BOARDING FLIGHT A/C FOR NR 3417, ALL O2 MASKS FELL DOWN. BELIEVE CAUSED BY FAULTY PROTECTIVE SWITCH COVER, CAP SIDE. MAINTENANCE ADJUSTED CAPT SWITCH GUARD. OPS CHECK GOOD STOWED ALL PAX O2 MASK. SECURITY CHECK GOOD. 2H74 4F RTA49EU 20030710001342003071000134EU 2003 7 10 MALA030305 120030603A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4K INSPECTION IN CWA, LT FUSELAGE HAS SEVERAL DENTS BETWEEN STA 352-363. MAINTENANCE REPAIRED DENTS WITH DOUBLER/TRIPLER IAW EO 53009. REF 409 NR 179479 FOR DETAIL. A/C RELEASE DATE 6/6/03. 2L72 4T RTA52EU 20030711000072003071100007EU 2003 7 11 MTNA20032 120030402A6123 PROPELLER RROYCE FOKKERF27 F27MK500 4990629EU RROYCEDART DART5327R 54509NE LT ENGINE MALFUNCTIONED A MTNAO OTHER Y ENGINE STOPPAGE CRCRUISE 1 SO33728FE248464448 14182 10657 14182 IN FLIGHT FROM CRW TO LCK THE LEFT ENGINE AUTO-FEATHERED. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED UNEVENTFULLY AT LCK. THE CAUSE IS UNKNOWN AT THIS TIME. 2H72 4T4 T A817 E297 20030711000082003071100008EA 2003 7 11 JBXA03009 120030612A32445010571 TIRE CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A JBXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05571ML 7209 FLIGHT 5188 FROM DCA TO JAX DIVERTED INTO RDU FOR BLOWN NR 1 TIRE ON TAKEOFF. ON ARRIVAL MX FOUND THE NR 1 TIRE SHREDDED WITH DAMAGE TO THE GEAR DOOR AND A CUT IN THE INBOARD FLAP. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY AND FERRIED A/C TO REPAIR FACILITY TO FACILITATE REQUIRED REPAIRS. 2L72 4F RTA21EA 20030711000112003071100011EA 2003 7 11 JBXA03012 120030617A3260 DISPLAY CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A JBXAO OTHER N FALSE WARNING LDLANDING 1 SO05261BD 7137 NOSE WHEEL LIGHT YELLOW/RED WITH GEAR LEVER DOWN DISPLAYED ON EICAS. RELEASED PER MEL 32-30-01 AND ASSIGNED TO DMI NUMBER 12916. 2L72 4F RTA21EA 20030711000162003071100016SO 2003 7 11 C2XA03SH193 120030622A532014521725615 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO HAVE CORROSION AROUND NUT PLATES. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000262003071100026EU 2003 7 11 DHL2003366510 120030610A5330 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 FR 63A AND SKIN CORRODED BETWEEN L40 AND L41. REMOVED FASTENERS AT FR63A TO GAIN ACCESS. REMOVED CORROSION IAW A300 SRM 51-40-11, ORIGINAL THICKNESS .315 ON SKIN, REMAINING .257, MATERIAL REMOVED .058, FOUND WITHIN LIMITS IAW A300 SRM 53-17-00 FIG 115, 53-10-00 FIG 206A. NO CORROSION NOTED ON FRAME. ALODINED SKIN IAW A300 SRM 51-40-11, PRIMED IAW A300 SRM 51-40-12, TOPCOATED IAW A300 SRM 51-40-12. INSTALLED FASTENERS IAW A300 SRM 51-30-30. SEALED AREA IAW A300 SRM 51-40-20. 2L72 4F RTA35EU 20030711000332003071100033EU 2003 7 11 DHL2003366514 120030530A5411ASL0605537 FRAME AIRBUS300 A300B4203 3930306EU NACELLE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 NR 1 O/B CORE NACELLE L/E FRAME, EXISTING REPAIR WORN THROUGH. REMOVED WORN FRAME AND INSTALLED NEW FRAME IAW BAC DWG NSL6361. 2L72 4F RTA35EU 20030708000412003070800041WP 2003 7 8 UPS03840902 120030602A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3, R2 DOOR UPPER AFT CORNER SHOW CRACK INDICATION WITH S RAY INSPECTION. REMOVED DAMAGE IN SKIN AND INTERNAL DOUBLER IAW SRM 53-2-0. REMOVED WEB STA 1650-1660 L9-15 RT AND INTERCOSTAL STA 1620-1640 BTWN L10- 11R FAB DOUBLER, TRIPLER, AND FILLERS IAW SRM 53-2-0. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED DOUBLER, TRIPLER, FILLERS, AND INTERCOSTAL IAW SRM 51-1-20D AND 53-2-0. 2L74 4F RT4A25 20030630000322003063000032NM 2003 6 30 AWXA200300607 120030528A3397BMS13311122 WIRE BOEING737 737301 1384611NM SEAT ROW 7 SHORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHTS FROM SEAT ROWS 4-9 WERE INOPERATIVE. MAINTENANCE REPAIRED A SHORTED EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030630000552003063000055 2003 6 30 ALGA087724 420030624A8300E6898785 GEAR BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL GEARBOX PTO DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0360WJ 704 CAG70698 45276 CAE860696 AS PER MANDATORY BULLETIN T-075. REMOVED AND REPLACED. SUBMITTED BY: PRESTON BARZARE 1G71 3U3 U H2SW E1GL 20030630000852003063000085SW 2003 6 30 HEEA087847 120030612A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH4429 53399 MAIN ROTOR BLADE CRACKED LEADING EDGE CORROSION STRIP. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030630000912003063000091SW 2003 6 30 HEEA087853 120030522A6510407040302113 SHAFT BELL 407 407 1182206SW TAIL ROTOR SCORED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH3706 53147 SCORED SURFACE ON BEARING. REPLACED BEARING 407-040-339-101, S/N ZV1109 DUE TO SCORED SURFACE; SHAFT 407-040-330-101, S/N A2193 DUE TO WORN SHAFT JOURNAL; ADAPTER 406-040-328-103, S/N AFS2193 DUE TO CORROSION. REPAIRED. 1G71 3U O H2SW 20030701000042003070100004SW 2003 7 1 HEEA087858 120030415A6320407040624101 TUBE BELL 407 407 1182206SW MRGB OIL SYS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR GEARBOX OIL TUBE HAS CORROSION CAUSED BY DISSIMILAR METALS USED IN MANUFACTURING PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030701000192003070100019SW 2003 7 1 HEEA087873 120030610A2510407370721101 RESTRAINT BELL 407 407 1182206SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 RESTRAINT WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030702000192003070200019NM 2003 7 2 BJNA030601 120030610A2120 ODOR BOEING737 737282 13844ATNM COCKPIT DETECTED A BJNAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP11344TM 23044 BURNING ODOR IN COCKPIT AND CABIN ON TAKEOFF. INSPECTED AIRCRAFT, RAN ENGINES, CHECKED AIR CONDITIONING PACKS AND VENTILATION SYSTEM. UNABLE TO DUPLICATE, NO FAULTS FOUND. (M) 2L72 4F RTA16WE 20030707001012003070700101NM 2003 7 7 371PA0024 120030624A339758782 POWER CABLE BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING SYSTEM INOP. REPLACED POWER CABLE ASSY. OPS CHECK NORMAL. 2L72 4F RTA16NE 20030707001752003070700175EA 2003 7 7 03167634 120030616A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27634BR 7287 DURING MAINTENANCE INSPECTION, THE CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030707001832003070700183WP 2003 7 7 UPS03840891 120030616A5730 ACCESS PANEL DOUG DC8 DC873F 302199FWP RT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING IB. AILERON LOWER ACCESS PANEL NR 541 CUTOUT IS CRACKED. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED DOUBLER IAW SRM. 57-2-0 FIG. 2H. 2L74 4F RT4A25 20030708000032003070800003CE 2003 7 8 DXTA200300057 120030704A3230 LANDING GEAR CESSNA500 560CESSNA 2076750CE MAIN INOPERATIVE E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07303QS 5600343 NORMAL GEAR EXTENSION INOPOPERATIVE, HANDLE DOWN WITH NO HYDRAULIC PRESSURE INDICATOR , NO GEAR UNLOCK EMERGENCY EXTENSION COMPLIED WITH IAW CHECKLIST, LANDING UNEVENTFULL. SECURED LOOSE CONNECTOR "P160" FOR MLG CONTROL HANDLE IN COCKPIT. RESET THE PNEUMATIC EMERGENCY MLG CONTROL SYS AND BOTTLE TO THE NORMAL POSITION, CYCLED MLG 12 TIMES NORMALLY. MLG EXTENTION AND RETRACTION OPS CHECKED NORMAL IAW CE560 MM. 2L72 4F RTA22CE 20030708000152003070800015EA 2003 7 8 COMA0360301 120030626A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS WEAK A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01999CA11401 7230 FLIGHT 5544 FLAPS FAIL, CAUTION MESSAGE. REPLACED THE PDU. 2L72 4F4 FRTA21EA E15NE 20030708000502003070800050WP 2003 7 8 UPS03840844 120030521A53103750891504 SHEAR TIE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, C-PIT STA. 1120 BELOW LONG. 21R SHEARTIE IS CRACKED REMOVED, FABRICATED AND REPLACED SHEARTIE I.A.W. UPS ENGINEERING FILE NUMBER ,SAA SK 705-061 AND SRM. 51-1-20D. 2L74 4F RT4A25 20030708000642003070800064NM 2003 7 8 ABXA030191 120030610A5411314T1210333 FRAME BOEING767 767281 1385109NM NACELLE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 NR 2 ENGINE RIGHT CORE COWL FRAME NAS STA. 304.60 AND NAC WL 73, DAMAGE WAS FOUND ON FRAME P/N 314T1210-333. REPAIRED AREA IAW REA B671-46254MR. 2L72 4F RTA1NM 20030711000392003071100039SO 2003 7 11 C2XA03IA065 120030615A2750 CONTROL UNIT EMB 145 EMB145LR 3260212SO TE FLAPS MALFUNCTIONED A C2XAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW2748901 145501 CREW NOTED THAT THE FLAPS FAILED IN FLIGHT, DECLARED EMERGENCY, DID AN EMERGENCY DESCENT AND LANDED WITHOUT INCIDENT. THE CREW CONTACTED MAINTENANCE CONTROL, PERFORMED FLAP RESET, OPS CHECK GOOD. 2L72 4T RTT00011AT 20030711000402003071100040NM 2003 7 11 HNAA0300029 120030619A242031708011A GENERATOR DHAV DHC8 DHC8201 2809001NM NR 1 ENGINE FAILED A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07983HA316111312 478 TAKE-OFF ABORTED DUE TO NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATING. REMOVED AND REPLACED NR 1 AC GENERATOR. 2H72 4T RTA13NM 20030711000442003071100044WP 2003 7 11 DHL2003804005 120030621A2611327 LAMP DOUG DC8 DC873F 302199FWP SMOKE DETECTOR BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01804DH 46124 NR 12 SMOKE DETECTOR INOPERATIVE, WON'T TEST UPPER CARGO. DMI 13326 ASSIGNED CVG MAINTENANCE CONTROL PER MEL 26-6-1. PLACARD INSTALLED. RELAMPED NR 12 SMOKE DETECTOR BEACON IAW 26-10-5. OPS CHECKED NORMAL. THIS CLEARS DMI 13326. PLACARD REMOVED. 2L74 4F RT4A25 20030711000492003071100049EA 2003 7 11 COMA0360281 120030620A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING FAILED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01458CA 7613 FLIGHT 5336 FLAPS FAILED DURING TAXI. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030711000542003071100054EU 2003 7 11 MALA030315 120030613A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 DURING 4K CHECK IN CWA, RT FUSELAGE CABIN SKIN HAS .039 INCH DEEP DENT, 1.25 INCH AT STA 340.5, 2.5 INCH BELOW SL 1615. MAINTENANCE REPAIRED RT CABIN SKIN DENT IAW EO S53009. A/C RELEASE DATE 6/19/03. REF 409 NR 179659 FOR DETAIL. 2L72 4T RTA52EU 20030711000582003071100058NE 2003 7 11 MALA030321 320030623A614010223N01R00 INDICATOR SAAB SF340 340B 7860101EU ROTOL R390 R3904123F27 NE PROP RPM FAILED A MALAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL15415XJ 340B415 AFTER TAKEOFF OF FLIGHT 3237, RIGHT HAND PROP RPM INDICATOR FAILED. AIR RETURN TO ABR. MAINTENANCE REPLACED PROP SPEED INDICATOR P/N 10223N01R00, SN/OFF B604, SN/ON 9703632. IAW SAAB AMM 61-40-05-2, OPS CHECK GOOD. 2L72 4T RTA52EU 6 CP31NE 20030711000592003071100059EU 2003 7 11 MALA030320 120030622A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15444XJ 340B444 DURING FLIGHT 2703, AVIONICS SMOKE LIGHT ILLUMINATED INFLIGHT. DECLARED EMERGENCY. MAINTENANCE REMOVED AND REPLACED AVIONICS SMOKE DETECTOR P/N ON/OFF 72-111211-000, SN/OFF A5276, SN/ON B5550. INSTALLED SERVICEABLE DOOR. ALL CHECKS GOOD SEE 409 NR 167819 FOR ADDITIONAL INFO. 2L72 4T RTA52EU 20030711000702003071100070SO 2003 7 11 C2XA03SH202 120030626A531014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 SHV-DURING C-CHECK THE RIGHT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000852003071100085NM 2003 7 11 CALA0300334 120030622A2897 WIRE HARNESS BOEING737 737524 1384721NM BOOST PUMP BURNED A CALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW2714664 1585AC 28925 THE AFT FUEL BOOST PUMP LOW PRESSURE LIGHT LEFT SIDE ILLUMINATED AFTER LANDING AT DFW. WHILE TROUBLESHOOTING THE PUMP THE WIRE BUNDLE AT STA 254 IN COCKPIT WAS FOUND BURNED. OVERHEATING OF THE PUMP WAS SUSPECTED TO BE THE CAUSE OF THE BURNT WIRING. THE FUEL BOOST PUMP WAS REPLACED AS A PRECAUTIONARY MEASURE. THE DAMAGED WIRING WAS SPLICED IAW STANDARD WIRING PRACTICES MANUAL 20-30-12. THE WIRING BUNDLES WERE REROUTED, SECURED, AND ATTACHED TO AFT CLAMP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20030711000912003071100091WP 2003 7 11 MWEA030255 120030625A52805910557504 DOOR DOUG DC9 DC932 3022066WP MLG INOPERATIVE A MWEAO OTHER L NO TEST CLCLIMB 1 GL31502ME 48132 GEAR UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED MAIN LANDING GEAR RIGHT INBOARD DOOR. 2L72 4F A6WE 20030708001022003070800102EU 2003 7 8 AWXA200300704 120030425A5320D53911670200 PLATE AIRBUS320 A320231 3930325EU FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK 2 EACH .5000 INCH CRACKS WERE FOUND ON AFT CARGO COMPARTMENT FORWARD BULKHEAD, LT UPPER CORNER FRAME PLATE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED, FABRICATED A REPAIR DOUBLER AND SHIMS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5314-00011-JS4. 2L72 4F RTA28NM 20030709000252003070900025WP 2003 7 9 AALA20030557 120030512A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21248AA 49259 DURING OVERNIGHT MAINTENANCE, CEILING AISLE EMERGENCY EXIT LIGHTS FROM ROWS 8 THROUGHT 11 INOPERATIVE. INSTALLED NEW EMERGENCY EXIT LIGHT BATTERY GROUND WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000442003070900044WP 2003 7 9 GTIA030440 120030516A5320 STIFFENER DOUG DC9 DC981 3022081WP FLOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLOORBOARD, RIGHT OUTBOARD FS 928-1003, LOWER STIFFENER CRACKED. REMOVED DAMAGED AREA. FABRICATED DOUBLR AND FILLER. INSTALLED DOUBLER AND FILLER. (M) 2L72 4F A6WE 20030709001072003070900107SO 2003 7 9 GLBA2003069 120030529A73301111102 INDICATOR EMB 120 EMB120ER 3260203SO FUEL SYSTEM FALSE INDICATIONA GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03299UX 120299 RIGHT FUEL FILTER ILLUM. REMOVED AND REPLACED HP AND LP FUEL FILTERS, OPS CK GOOD. 2L72 4T RTA31SO 20030710000602003071000060NM 2003 7 10 DHL2003755008 120030522A5270766001 SWITCH BOEING727 727225 1384077NM PAX DOOR LACK OF LUBE A DHLAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO01755DH 21857 FORWARD ENTRY DOOR LIGHT NOT ILLUMINATED WITH FORWARD ENTRY DOOR OPEN. LUBED SWITCH IN DOOR JAMB. OPS GOOD IAW M/M 52-11-01. 2L73 4F A3WE 20030710000642003071000064WP 2003 7 10 DHL2003807011 120030602A52701EN32R SWITCH DOUG DC8 DC873F 302199FWP CARGO DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01807DH 45990 AT FL 390, BELLY DOOR OPEN WARNING LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. PRESSURIZATION NORMAL. CONTINUED NORMAL OPERATION. ASSIGNED DMI 13146 MEL 52-1 COMPLIED WITH SPECIAL PROCEDURES. REF DMI 13146 BELLY DOOR OPEN WARNING LIGHT ILLUMINATED (A-PIT). RII REQUIRED. REMOVED AND REPLACED BELLY DOOR OPEN WARNING SWITCH. OPS CHECKED GOOD IAW M/M 52-70-0. MAINTENANCE CONTROL NOTIFIED. THIS CLEARS DMI 13146. 2L74 4F RT4A25 20030710000762003071000076WP 2003 7 10 DHL2003801004 120030611A3231 CYLINDER DOUG DC8 DC873F 302199FWP MLG DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 UPON LANDING GEAR RETRACTION DOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHTS ILLUMINATED APPROPRIATE ABNORMAL PROCEDURE PERFORMED LIGHTS REMAINED ON GEAR NOT LATCHED LIGHT ILLUMINATED IN CVG PATTERN RIGHT DOOR UNSAFE LIGHT ILLUMINATED. ADJUSTED LEFT GEAR DOOR ACTUATING CYLINDER ADJUSTABLE LINK PER DC-8 M/M 32-32-7. JACKED A/C AND SWUNG LANDING GEAR PER DC-8 32-11-1. OPS CHECKED SERVICEABLE. NO DEFECTS NOTED. 2L74 4F RT4A25 20030710000852003071000085EU 2003 7 10 DHL2003366507 120030520A5330 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 LT FWD FUSELAGE FRAME 11 EXTERNAL SKIN IS DENTED. FOUND DENT TO BE OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED DAMAGE AND FABBED REPAIR DOUBLER AND FILLER IAW A300 SRM 53-12-00 FIG 709. ALODINED AND PRIMED IAW A300 SRM 51-40-12. INSTALLED REPAIR IAW A300 SRM 53-12-00 FIG 709 AND A300 SRM 51-30-30. 2L72 4F RTA35EU 20030711000052003071100005CE 2003 7 11 MTNA135031 120030305A261247790008 CONTROL BOX CESSNA208 208B 2073701CE FIRE WARNING FALSE INDICATIONA MTNAO OTHER J WARNING INDICATION CRCRUISE 1 SO33917FE3468 208B0017 APPROXIMATELY 20 MILES FROM JAX THE ENGINE FIRE WARNING LIGHT ILLUMINATED AND THE HORN SOUNDED. THE PILOT COMPLETED THE EMERGENCY CHECK LIST AND THEN DECLARED AN EMERGENCY WITH ATC. THE AIRCRAFT LANDED WITH ON OTHER PROBLEMS. AFTER TROUBLESHOOTING THE SYSTEM THE MECHANIC REMOVED AND REPLACED A CONTROL BOX AND A FIRE LOOP. THE AIRCRAFT WAS RETURNED TO SERVICE. 1H71 3T A37CE 20030711000462003071100046SO 2003 7 11 C2XA03CL114 120030617A3350 LIGHT EMB 145 EMB145ER 3260211SO OVERWING INTERMITTENT A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2715941 145035 CLE FLIGHT 2917 THE CREW REPORTED THE EMERGENCY LIGHTS FOR THE MAIN CABIN DOOR AND OVERWING EXIT LIGHT DID NOT WORK. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030711000522003071100052EU 2003 7 11 MALA030318 120030618A5753 SPAR SAAB SF340 340B 7860101EU LT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 DURING 4K INSPECTION IN CWA, LT FLAP REAR SPAR CRACKED AT WS 142. MAINTENANCE COMPLETED REPAIR IN REAR SPAR AT WS 142 IAW EO 57007. A/C RELEASE DATE 6/19/03. REF TO 409 NR 179691 FOR DETAIL. 2L72 4T RTA52EU 20030711000552003071100055EU 2003 7 11 MALA030316 120030614A5330 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 DURING 4K INSPECTION IN CWA, DENT FOUND UNDER RT ICE SHIELD FWD OF STA 319, BETWEEN SL1618 AND SL1620. MAINTENANCE COMPLETED DOUBLER REPAIR IAW EO NR 53005. REF TO 409 NR 179654 FOR DETAIL. A/C RELEASE DATE 6/19/03. 2L72 4T RTA52EU 20030711001042003071100104NM 2003 7 11 VNAA0306006 120030612A32502304000001 CONTROLLER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NLG STEERING FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07424JS19259277 3033 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC STEERING CONTROL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030711001052003071100105NM 2003 7 11 VNAA0306007 120030613A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL07463PS1217651 3087 THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT ROWS 3 TO 7 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030711001072003071100107NM 2003 7 11 VNAA0306012 120030622A24301180001 GCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RIGHT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07425JS197551019 3037 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030711001102003071100110NM 2003 7 11 DHL2003783013 120030626A7930388062 O-RING BOEING727 727227 1384078NM PWA JT8 JT8D17A 52049NE OIL FILTER BROKEN A DHLAEDO ENGINE SHUTDOWN RETURN TO BLOCK OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO01766AT 21999 AFTER ENGINE START LOST ALL OIL QUANTITY FOLLOWED OIL PRESSURE ON ENGINE NR 1. COMPLETED LOW OIL PRESSURE ABNORMAL AND SHUT DOWN ENGINE NR 1 AT 35 PSI. FOUND O-RING ON OIL FILTER BROKEN. REMOVED AND REPLACED O-RING AND FILTER. OPS CHECKED NORMAL IAW M/M 79-33-0. SERVICED OIL IAW M/M 12-13-1. CAP RE-SECURED. 2L73 4F4 F A3WE E2EA 20030711001202003071100120WP 2003 7 11 MWEA030259 120030627A5534591218836 ANGLE DOUG DC9 DC982 3022082WP VERTICAL STAB CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 STATION 1429 RIGHT SIDE INNER VERTICAL STABILIZER TO FUSELAGE FITTING IS CRACKED. FABRICATED AND INSTALLED NEW ANGLE. 2L72 4F A6WE 20030711001242003071100124WP 2003 7 11 MWEA030266 120030628A524049157601 PAN DOUG DC9 DC981 3022081WP SERVICE DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 FORWARD GALLEY SERVICE DOOR HOOK PAN ASSEMBLY IS CRACKED. REMOVED AND REPLACED CRACKED PAN ASSEMBLY. 2L72 4F A6WE 20030714000072003071400007NM 2003 7 14 CALA0300344 120030628A5320 ANGLE BOEING737 737524 1384721NM DOOR FRAME CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717644 28905 INSPECTION FOUND ZEE ANGLE I/B OF L-2 DOOR CORRODED. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030714000112003071400011EA 2003 7 14 COMA0360305 120030627A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01999CA 7230 FLIGHT 5215 DURING TAKEOFF ROLL RECEIVED A FLIGHT SPOILER CONFIGURATION WARNING, ABORTED AND RETURNED THE GATE. PERFORMED SYSTEM RESET. 2L72 4F RTA21EA 20030714000152003071400015NM 2003 7 14 SWAA031418 120030625A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 767 AND BS 769, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030714000172003071400017 2003 7 14 SWAA031420 420030626A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030714000282003071400028NM 2003 7 14 SWAA031400 120030624A53206546804 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 1006 AND BS 1016, BETWEEN LBL 5 AND LBL 10, WL 208. REPAIRED FLOOR SUPPORT PER SRM. 2L72 4F RTA16WE 20030714000342003071400034NM 2003 7 14 SWAA031406 120030624A53126517582 BEAM BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 230 AND RBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM. 2L72 4F A16WE 20030714000372003071400037NM 2003 7 14 SWAA031409 120030623A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 767 AT STR 24L AND BS 870 AT STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030714000462003071400046NM 2003 7 14 SWAA031371 120030620A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 811, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030714000492003071400049 2003 7 14 SWAA031374 420030621A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030714000542003071400054 2003 7 14 SWAA031379 420030620A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030714000562003071400056NM 2003 7 14 SWAA031381 120030620A324426078251 TIRE BOEING737 7373H4 1384600NM NLG FAILED A SWAAA UNSCHED LANDING DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 SW29314SW 23336 AIR TURNBACK, AT ROTATION FELT NOSE VIBRATION, HEARD MATERIAL IMPACTING FUSELAGE. FOUND, TREAD LOSS AT NR 1 NLG TIRE. REMOVED AND REPLACED BOTH NOSE TIRE AND WHEEL ASSY PER MM. 2L72 4F RTA16WE 20030714000692003071400069 2003 7 14 SWAA031384 420030622A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 1628 27933 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030714000812003071400081NM 2003 7 14 SWAA031416 120030623A3350BR2013 LIGHT BOEING737 7375H4 138449DNM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP LOOSE AT ROW NR 12. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20030714000892003071400089 2003 7 14 SWAA031347 420030616A256561620468 SLIDE BOEING737 7373Q8 1384670NM SERVICE DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030714000982003071400098NM 2003 7 14 371PA0026 120030628A335058674 POWER SUPPLY BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 EMERGENCY EXIT SIGN AT L2 DOOR INOP AND COVER BROKEN. REPLACED POWER SUPPLY IAW MM 33-51-41 AND EXIT SIGN IAW MM 33-51-11. OPS CHECKS NORMAL. 2L72 4F RTA16NE 20030714001122003071400112CE 2003 7 14 GLBA2003099 120030701A261224412886 FIRE LOOP BEECH 1900 1900D 1154162CE NR 1 ENGINE MALFUNCTIONED A GLBAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 NM03179GL UE179 NR 1 FIRE HANDLE ILLUM IN FLIGHT. REMOVED AND REPLACED FWD FIRE LOOP. 2L72 4T RTA24CE 20030714001182003071400118NM 2003 7 14 CALA0300351 120030701A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND L-1 DOOR JAMB ZEE ANGLE CORRODED FROM BS 306-344. THE ZEE ANGLE WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030708000732003070800073NM 2003 7 8 AWXA200300644 120030513A5320654797322 WEB BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A .7500 INCH CRACK WAS FOUND ON FUSELAGE INTERIOR SHEAR WEB BELOW THE RT EMERGENCY ESCAPE HATCH CUTOUT. MAINTENANCE REMOVED DAMAGED SHEAR WEB BELOW THE RT EMERGENCY ESCAPE HATCH CUTOUT BS 616 TO BS 639, STR 27 RT; FABRICATED A NEW REPLACEMENT SHEAR WEB IAW DWG 65-47973; INSTALLED REPAIR PART IAW SRM 51-10-1, PG. 8. 2L72 4F RTA16WE 20030708000742003070800074NM 2003 7 8 AWXA200300645 120030513A5755654645258B PANEL BOEING737 737277 1384570NM SPOILER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK THE NO. 5 SPOILER WAS FOUND DELAMINATED AT THE INBOARD AFT EDGE. MAINTENANCE REMOVED AND REPLACED THE NO.5 SPOILER PANEL IAW BMM 27-62-12, PG. 401. 2L72 4F RTA16WE 20030630000672003063000067EU 2003 6 30 BAQA087569 120030601A243523081043 STARTER GEN BOLKMSBK117 BK117C1 5626025EU ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117NC752 7517 STARTER GENERATOR INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030701000342003070100034SW 2003 7 1 HEEA087238 120030610A6220412010216107 BEARING BELL 412 412 1182202SW PENDULUM WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 BLUE TRAILING EDGE WORN. SHOP REPAIR. 1G72 4U H4SW 20030701000382003070100038SW 2003 7 1 HEEA086955 120030603A2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH875 53207 STARTER GEN FIELD CIRCUIT BREAKER POPS. REPAIRED. 1G71 3U O H2SW 20030702000152003070200015NM 2003 7 2 AMTA200300719 120030528A3233273A12011 ACTUATOR BOEING737 73783N 13844HINM NOSE GEAR MALFUNCTIONED A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11301TZ 28239 AFTER TAKEOFF, UPON GEAR RETRACTION RED NOSE GEAR AND GREEN NOSE GEAR LIGHTS REMAINED ILLUMINATED. LOUD AIR NOISE HEARD AND RETURNED TO PHL. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR IAW AMM 32-33-21-4. CYCLED GEAR 5 TIMES. LEAK AND OPS CHECK GOOD. NO RED LIGHT. (M) 2L72 4F RTA16WE 20030702000422003070200042WP 2003 7 2 GTIA030389 120030519A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP COCKPIT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND FLIGHT COMP, F/O'S RIGHT FORWARD FLOOR PANEL BROKEN. REMOVED FLOORBOARD. FABRICATED NEW FLOORBOARD. INSTALLED F/B RIGHT. (M) 2L72 4F A6WE 20030707000302003070700030NM 2003 7 7 AALA20030146 120030203A3397 WIRE BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21968AN 30095 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT PLUG ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030707000702003070700070NM 2003 7 7 2003UALA00495 120030613A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29198UA 28716 DENT TOP FLOORBEAM BS600 RBL43. MAJOR REPAIR ACCOMPLISHED. REPLACED TOP TEE CHORD. 2L74 4F4 FRTA20WE E24NE 20030707001082003070700108WP 2003 7 7 UPS03840861 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 822. STOP DRILLED RIB,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001622003070700162NM 2003 7 7 AWXA200300629 120030530A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030707001632003070700163NM 2003 7 7 AWXA200300630 120030513A335090055 CHARGER BOEING737 737277 1384570NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK EMERGENCY LIGHT BATTERY CHARGER M1051 LOCATED IN AFT AISLE CEILING HAS NO OUTPUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER M1051, OPERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33005. 2L72 4F RTA16WE 20030708000022003070800002CE 2003 7 8 DXT200300057 120030704A3230 LANDING GEAR CESSNA500 560CESSNA 2076750CE MAIN INOPERATIVE E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07303QS 5600343 NORMAL GEAR EXTENSION INOPERATIVE, HANDLE DOWN WITH NO HYDRAULIC PRESSURE INDICATOR , NO GEAR UNLOCK EMERGENCY EXTENSION COMPLIED WITH IAW CHECKLIST, LANDING UNEVENTFULL. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20030708000052003070800005CE 2003 7 8 GLBA2003101 120030703A2750 LINK BEECH 1900 1900D 1154162CE TE FLAP STUCK A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03169GL UE169 FLAPS STUCK AT 17 DEG, R&R RT FLAP SAFETY LINK OPS CHECKED GOOD. 2L72 4T RTA24CE 20030708000062003070800006CE 2003 7 8 DXTA200300058 120030705A3246 WHEEL CESSNA750 750 2076810CE NLG INOPERATIVE E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TXTAXI/GRND HDL 1 GL07903QS 7500162 NOSE WHEEL BEGAN SHAKING VIOLENTLY PASSING THROUGH 60 KNOTS DURING TAKEOFF ROLL. REPLACED LT & RT NOSE TIRE & WHEEL ASSY IAW 750 M/M 32-41-01. 2L72 4J RTT00007WI 20030714001192003071400119NM 2003 7 14 CALA0300352 120030701A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT NUTPLATE HOLES BETWEEN STA 344 AND 360, LBL 10. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-40. 2L72 4F RTA16WE 20030714001212003071400121NM 2003 7 14 CALA0300354 120030701A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND STRINGER 27L CORRODED AT STA 1006. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20030709000662003070900066EU 2003 7 9 03152316 120030601A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE GROUND WIRE AT THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030709001042003070900104CE 2003 7 9 GLBA2003076 120030605A21632066645 FILTER BEECH 1900 1900D 1154162CE TEMP SENSE LINE FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03245GL UE245 LEFT ENVIRO FAIL WOULD NOT RESET UNABLE TO PRESSURIZE. REPLACED LT PRECOOLER TEMP SENSE LINE FILTER. 2L72 4T RTA24CE 20030709001132003070900113SO 2003 7 9 C2XA03SH184 120030613A541414576616043 SKIN EMB 145 EMB145LR 3260212SO NR 1 NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK NUMBER ONE ENGINE LOWER COWLING SKIN WAS FOUND GOUGED BY FRAME 7. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709001162003070900116NM 2003 7 9 CALA0300310 120030612A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND A .5 INCH CRACK IN MAIN WHEEL WELL PRESSURE DECK AT STA 673, LBL 31. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51, FIGURE 203. 2L72 4F RTA16WE 20030709001222003070900122EU 2003 7 9 MALA030301 120030610A5270 SWITCH BAC 146 AVRO146RJ85A1500097EU PAX DOOR DIRTY A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15512XJ E2326 ON TAKEOFF ROLL OF FLIGHT 3555, LOWER DOOR NOT SHUT LIGHT ILLUMINATED. MAINTENANCE VERIFIED ALL DOOR CLOSED. CLEANED AFT CARGO DOOR OPEN SWITCH, OPS CHECK GOOD. LIGHT OUT. RETURN TO SERVICE. 2H74 4F RTA49EU 20030710000022003071000002NM 2003 7 10 KPVA200325 120030608A33506104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHTSINOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13807WP 023 FOUND LEFT AND RIGHT FORWARD EGRESS LIGHT OUT AND ONE FORWARD CEILING AISLE LIGHT EMERGENCY LIGHT OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLIES 3351-PS1 AND 3351-PS2. OPS CHECK GOOD IAW DHC 8 MM 33-51-00 PAGE 202. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030710001202003071000120EA 2003 7 10 03168648 120030617A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27648BR 7406 DURING MAINTENANCE INSPECTION, THE LEFT EXTERIOR AFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE POWER SUPPLY FOR THE EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030710001542003071000154NM 2003 7 10 DHL2003750003 120030619A5220 SKIN BOEING727 7272M7 138407SNM EMERGENCY EXIT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 RT FORWARD OVERWING HATCH VERY HARD TO OPEN. OUTBOARD UPPER SKIN DAMAGED. HATCH IN WRONG POSITION. INSTALLED IN CORRECT POSITION. WORKS FINE. BURNISHED OUT MINOR SCRATCH IAW B727 SRM 51-10-6. 2L73 4F A3WE 20030711000092003071100009EA 2003 7 11 JBXA03010 120030615A323316520101 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NLG LEAKING A JBXAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO05261BD 7137 NOSE GEAR UNSAFE. REMOVED AND REPLACED NOSE GEAR ACTUATOR IAW AMM 32-33-01, OPS CHECK GOOD. 2L72 4F RTA21EA 20030711000832003071100083EA 2003 7 11 COMA0360290 120030624A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01785CA 7326 FLIGHT 5298 WING OVERHEAT MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030714000022003071400002NM 2003 7 14 CALA0300339 120030627A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717644 28905 INSPECTION FOUND A .125 INCH CRACK IN INTERCOSTAL AT FORWARD ENTRY STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-10-51 AND 51-70-11. 2L72 4F RTA16WE 20030714000052003071400005NM 2003 7 14 CALA0300342 120030627A5347 GALLEY TRACK BOEING737 7373T0 1384582NM BS CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND CORROSION ON GALLEY TRACK BETWEEN BS 277 AND 294, RBL 44. THE GALLEY TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030714000122003071400012 2003 7 14 MWEA030268 420030628A3442 DISPLAY DOUG DC9 DC981 3022081WP WX RADAR SYS FAILED A MWEAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 GL31805ME 48031 CAPTAIN'S RADAR INDICATOR WON'T TEST AND IS BLANK. SELF TEST WEATHER RADAR SYSTEM CHECKED GOOD. 2L72 4F A6WE 20030714000262003071400026NM 2003 7 14 SWAA031398 120030623A52106918187 GUIDE ARM BOEING737 7373H4 1384600NM PAX DOOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 FWD ENTRY DOOR DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED DOOR GUIDE ARM PER MM. 2L72 4F RTA16WE 20030708000492003070800049WP 2003 7 8 UPS03840842 120030521A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, RADIOGRAPHIC (X-RAY)INSPECTION DETECTED 4 CRACKS ON THE R-2 DOOR UPPER AFT CORNER AT STA. 1660 LONG. 11R CUTOUT DAMAGE AND REMOVED DAMAGE AT LONG. 11R,NDT VERIFIED NO CRACKS AT CUTOUT AND DAMAGE REMOVAL, FABRICATED AND INSTALLED DOUBLER, TRIPLER,FILLER AND STRAP I.A.W. E.O. SAA SK 705-086 AND SRM. 53-2-0 FIG. 16 2L74 4F RT4A25 20030708000542003070800054EA 2003 7 8 SWIA200312091 120030605A5411 RIB CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 605 LT PYLON RIB CRACKED. (DISCOVERED DURING C-CHECK) REPLACED RIB IAW CRJ SRM 51-40-11 P/N: 601-37004-85 2L72 4F RTA21EA 20030708000562003070800056SO 2003 7 8 SWIA200312093 120030613A3397 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07217SW 120286 EMERGENCY LIGHTS INOPERATIVE, IN CABIN. RESECURED CENTER LIGHTS BATTERY PACK CONNECTOR PLUG. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 20030708000582003070800058SO 2003 7 8 SWIA200312095 120030519A5420 CLIP EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT WING NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07296SW 120325 LT WING OB NACELLE RIB NR 15 LOWER CENTER CLIP CRACKED. (DISCOVERED DURING C-CHECK.) INSTALLED NEW LEFT WING OB NACELLE RIB NR 15 LOWER CENTER CLIP IAW MM 28-10-00. 2L72 4T4 TRTA31SO E20NE 20030708000762003070800076NM 2003 7 8 AWXA200300647 120030513A53156545410224 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK 2 EACH 1 INCH CRACKS WERE FOUND ON FLOOR BEAM UPPER STRUCTURE AT AFT END OF AILERON QUADRANT CUTOUT BS 676, RBL 24.5. MAINTENANCE CUTOUT DAMAGE ON FLOORBEAM UPPER STRUCTURE BS 676, RBL 24.5; FABRICATED 3 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW SB 737-57-1139 & E.O. 5715-01007. 2L72 4F RTA16WE 20030708000982003070800098EU 2003 7 8 YENA200311 120030615A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN FAILED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15517JB10471 1327 WHILE ACCOMPLISHING WEEKLY CHECK, EMERGENCY LIGHT FAILED TEST; T/S TO EPSU AT RIGHT EMERGENCY EXIT. REPLACED EPSU AT RIGHT EMERGENCY EXIT WITH BORROWED PART FROM UAL; NO DELAY INCURRED. 2L72 4F RTA28NM 20030708001002003070800100NM 2003 7 8 AWXA200300702 120030616A521080330034 RESERVOIR BOEING757 757225 1384959NM PAX DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING 4-DAY CHECK FOUND THE L-2 DOOR EMERGENCY POWER RESERVOIR PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR EMERGENCY POWER RESERVOIR IAW BMM 52-11-30. 2L72 4F RTA2NM 20030708001052003070800105 2003 7 8 252TR0005 420030623A22102590650901 COUPLER BOEING737 737228 13844AGNM MACH TRIM INOPERATIVE A PIDAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO05252TR 23001 AUTO PILOT AT 315 KTS TRIM ROLLS BACK AND FORTH 3 TURNS EACH DIRECTION. REPLACED MACH TRIM COUPLER IAW MM 22-21-0. OPS TEST NORMAL. 2L72 4F RTA16WE 20030709000052003070900005WP 2003 7 9 GTIA030433 120030514A5320 ANGLE DOUG DC9 DC981 3022081WP DOOR FRAME CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 MID PIT DOOR OPENING LOWER AFT CORNER STATION 693 FRAME CORRODED. REMOVED LOWER 6 INCH OF FS 693 FRAME. FABRICATED FILLER AND REPAIR ANGLE. INSTALLED FILLER AND REPAIR ANGLE. (M) 2L72 4F A6WE 20030709000142003070900014WP 2003 7 9 AALA20030585 120030518A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21446AA 49472 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000152003070900015WP 2003 7 9 AALA20030592 120030521A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21286AA 49298 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROWS 12-17 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY AT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000342003070900034WP 2003 7 9 AALA20030549 120030509A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21494AA 49732 DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707001922003070700192WP 2003 7 7 UPS03840824 120030526A57203704841501 FITTING DOUG DC8 DC871F 302199DWP RIGHT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, STRINGER END FITTING IS CRACKED INBOARD SIDE OF XRS 74 AT STRINGER 51 AFT SIDE IN NR 3 MAIN TANK. REMOVED AND REPLACED FITTING IAW DWG. 3704841 AND SRM. 51-1-20D 2L74 4F RT4A25 20030707002002003070700200WP 2003 7 7 UPS03840875 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 797. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030708000652003070800065NM 2003 7 8 ABXA030195 120030610A5420311T11155 FITTING BOEING767 767281 1385109NM NACELLE ELONGATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 DURING INSPECTION, ON LEFT STRUT FORWARD UPPER SPAR FITTING, FOUND FOUR BOLT HOLES SHOULD BE .4375 INCH ARE ALREADY OVERSIZED TO 0.515 INCH AND BACB 30 MT8X ARE INSTALLED. SB GIVES A MAXIMUM OVERSIZE OF 4692 INCH FOR THOSE HOLES. REWORKED AREA IAW REA B654-46255MR. 2L72 4F RTA1NM 20030714000442003071400044NM 2003 7 14 SWAA031359 120030617A53106545871 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CRACKED AT AFT FRAME ON 5TH FROM TOP STOP PIN CUTOUT. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20030714000932003071400093NM 2003 7 14 SWAA031351 120030615A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030714001282003071400128NE 2003 7 14 C1HA200381014 220030623A7530658385 BLEED VALVE BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE ENGINE MALFUNCTIONED A C1HAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION APAPPROACH 1 GL15681CA 22020 ON APPROACH INTO PVR ADVANCED THRUST LEVERS FROM IDLE TO APPROX 1.4 EPR NOTICED A COMPRESSOR STALL. THIS HAPPENED TWICE ON APPROACH. SUSPECT NR 2 ENGINE BECAUSE THE EPR'S JUMPED ERRATICALLY. ALL OTHER INDICATIONS WERE NORMAL. 2L73 4F4 F A3WE E2EA 20030714001402003071400140SW 2003 7 14 ALGA087894 120030701A6320206040032001 BEARING BELL 206 206B3 1181506SW TRANSMISSION SPALLED B O OTHER O OTHER NRNOT REPORTED 1 SW03158H BKW10097 2974 TRANSMISSION REMOVED FOR METAL IN OIL, FOUND BEARING BREAKING DOWN. 1G71 3U H2SW 20030714001482003071400148EU 2003 7 14 HEEA088085 120030618A6230350A37118101 GUIDE AEROSPAS355 AS355* EU SWASHPLATE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 3004 EXCESSIVE WEAR ON GUIDE AT SWASHPLATE BALL JOINT AREA. REPLACED. 1G72 3U H11EU 20030714001542003071400154 2003 7 14 BAQA086475 420030521A22109910991 CONTROL HEAD UROCOPEC135 EC135T1 5620026EU AUTO FLIGHT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME 132 RC-550, AFTER ENTERING FREQUENCY THEN TRYING TO TRANSMIT. ALL ENTERED INFORMATION IS DUMPED FROM SCREEN TO DEFAULT SETTINGS. 7/2/03 1G72 3U H88EU 20030714001572003071400157 2003 7 14 BAQA087929 420030707A3421060001301 GYRO UROCOPEC135 EC135T1 5620026EU COCKPIT PRECESSES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118WS 0089 GYRO INTERMITTENTLY PRECESSES 90 DEGREES WHEN IN THE SLAVE MOD. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030716000092003071600009WP 2003 7 16 GTIA030455 120030615A7820782160 MUFFLER DOUG DC9 DC983 3022083WP ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 DURING DAILY INSPECTION, FOUND HOLE IN EXHAUST NOISE SUPPRESSOR AT THE 7 O'CLOCK POSITION. REPLACED MIXER. (M) 2L72 4F RTA6WE 20030716000372003071600037NM 2003 7 16 TSAA0353152 120030613A53306546549 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 REPAIRED FUSELAGE SKIN CRACK AT BS 767, STRINGER 19 RIGHT. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN. VERIFIED CRACK REMOVED USING HFEC METHOD. FABRICATED AND INSTALLED A REPAIR FILLER AND PLATE FROM 2024-T3 MATERIAL IAW SRM 53-30-3, FIGURE 3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030716000382003071600038NM 2003 7 16 TSAA0353153 120030608A53306546549 SKIN BOEING737 7372S2C 138448GNM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13806AL 21927 FUSELAGE SKIN CRACKED AT BS 767, STRINGER 17. TRIMMED OUT DAMAGE AREA. HFEC INSPECTION AROUND CUTOUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED .50 INCH 2024-T3 FILLER AND .063 INCH CRES DOUBLER WITH CHAMFERED EDGES, REMOVED ALL NICKS, BURRS, SCRATCHES, GOUGES AND SHARP EDGES FROM SKIN AND ALL REPAIR PARTS, CLEANED AND TREATED ALL EXPOSED AREAS WITH ALODINE AND PRIMER, APPLIED BMS 5-95 SEALANT TO ALL REPAIR PARTS IAW SRM 53-30-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030716000412003071600041SO 2003 7 16 SIMA200316002 120030608A261147359713 SMOKE DETECTOR EMB 135 EMB135KL 3260302SO FWD CARGO BAY INOPERATIVE A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21806AE 145503 DURING CLIMB, CREW REPORTED A FIRE WARNING FOR THE AFT BAGGAGE COMPARTMENT. AN EMERGENCY WAS DECLARED AND QRH PROCEDURES WERE FOLLOWED. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CARGO SMOKE DETECTOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE AFTER FIRE BOTTLE WAS REPLACED. (M) 2L72 4F RTT00011AT 20030716000422003071600042SO 2003 7 16 SIMA200316903 120030614A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21710TB 145224 DURING AN IMBV INSPECTION, THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS BETWEEN FRAMES 65-67. REMOVED EXISTING SILL. CLEANED AND TREATED THE AREA. INSTALLED NEW SILL IAW EMB SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20030716000462003071600046NM 2003 7 16 USAABB03092 120030614A33509221009 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19603AU 22198 FOUND EXIT IDENTIFIER AT THE L3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030716000472003071600047NM 2003 7 16 GAIA03020OP 120030619A33501000677 LIGHT BOEING727 727223 1384074NM CABIN INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07858AA 21085 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030716000512003071600051WP 2003 7 16 GTIA030458 120030514A5753 VANE DOUG DC9 DC981 3022081WP RT FLAP DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND RIGHT INBOARD FLAP OUTBOARD VANE DENTED AND DELAMINATED. REPAIRED RIGHT INBOARD FLAP OUTBOARD VANE DENTS AND DELAMINATION THREE PLACES. (M) 2L72 4F A6WE 20030708001142003070800114WP 2003 7 8 GTIA030421 120030513A5320 ANGLE DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 NOSEWHEEL WELL, STATION 40 LBL 5 AND RBL 5, TWO ANGLES CRACKED AT AFT END IN RADIUS. REMOVED TWO ANGLES. FABRICATED TWO ANGLES. INSTALLED TWO ANGLES. (M) 2L72 4F A6WE 20030709000202003070900020WP 2003 7 9 AALA20030580 120030517A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21587AA 53250 DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FORWARD CABIN EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000322003070900032WP 2003 7 9 AALA20030476 120030421A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21298AA 49310 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT ROW 18-29 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000492003070900049WP 2003 7 9 GTIA030445 120030528A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP GALLEY DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND PASSENGER CABIN UNDER G-4 GALLEY FLOOR PANEL DELAMINATED, INSERTS BAD. FABRICATED NEW PANEL. INSTALLED FLOOR PANEL. (M) 2L72 4F A6WE 20030709000552003070900055WP 2003 7 9 GTIA030425 120030613A5710 STRUCTURE DOUG DC9 DC981 3022081WP RT WING BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 RIGHT WING LEADING EDGE LIP AT RE-FUELING PANEL OPENING IS BROKEN OFF AT INBOARD LATCH. TRIMMED OUT DAMAGE. FABRICATED 11 DOUBLER. FABRICATED 13 FILLER. I NSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F A6WE 20030709000642003070900064 2003 7 9 372PA0030 420030526A2230 CONTROL UNIT BOEING737 737306 13844BGNM NR 2 ENGINE MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05372PA 23546 AUTO THROTTLE INTERMITTENTLY DISCONNECTS, WHEN ENGAGED REDUCES NR 2 ENGINE N1 BY 3 PERCENT, REVERTS TO A/T COMPUTER. RELEASED UNDER MEL 22-4. 5/27/2003: ADJUSTED NR 2 ENGINE POWER LEVEL ANGLE SYNCHRO IAW MM 22-31-11. 2L72 4F RTA16NE 20030709000672003070900067EA 2003 7 9 03152633 120030601A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27633BR 7274 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT CABIN EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030709000762003070900076EA 2003 7 9 03155656 120030604A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27656BR 7485 DURING MAINTENANCE INSPECTION, THE NR 3 RT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030709000852003070900085WP 2003 7 9 MWEA030241 120030603A5610564324502 RETAINER DOUG DC9 DC981 3022081WP WINDOW CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 RIGHT UPPER COCKPIT WINDOW RETAINER IS CORRODED IN LOWER FORWARD CORNER. REMOVED DAMAGE AND INSTALLED FILLER AND EXTERNAL DOUBLER. 2L72 4F A6WE 20030709001082003070900108SO 2003 7 9 C2XA03SH183 120030612A532014524131009 CHANNEL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK U-CHANNEL WAS FOUND TO HAVE CORROSION UNDER MAIN THRESHOLD. MAINTENANCE REMOVED AND REPLACED AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709001152003070900115SO 2003 7 9 C2XA03SH186 120030613A540014576038003 STRUCTURE EMB 145 EMB145LR 3260212SO NR 2 NACELLE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK THE NUMBER TWO UPPER COWLING INBOARD EDGE MEMBER WAS FOUND DENTED. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709001282003070900128EA 2003 7 9 03166661 120030615A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGNECY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27661BR 7520 DURING MAINTENANCE INSPECTION, THE RT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030710000052003071000005EA 2003 7 10 ASOA03246 120030531A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 FLT 4134 - DURING A GROUND INSPECTION IN SHV, THE LEFT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030710000082003071000008NM 2003 7 10 KPVA200327 120030609A3350 BATTERY PACK DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT WEAK A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13805WP 63564 353 PORTABLE EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT. OPS CHECK GOOD IAW DHC 8 MM 33-51-00 PAGE 201-202. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030710000262003071000026NM 2003 7 10 TSAA0333144 120030609A33509221009 BATTERY PACK BOEING737 7372S2C 138448GNM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13806AL 21927 REPLACED FORWARD SERVICE DOOR IDENT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030710000302003071000030NM 2003 7 10 USAA030078 120030516A5311 FRAME BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU33879 27199 CLT - FOUND 2 INCHES OF CORROSION, STATION 1400 BETWEEN S28L-S27L ON OUTER FRAME. REMOVED CORROSION AND INSTALLED REPAIR FASTENERS PER EA 87238. (M) 2L72 4F RTA2NM 20030710000402003071000040 2003 7 10 USAASA03041 420030514A2565D5211044000600 GIRT BAR AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW 1019 CLT - DURING INSPECTION, THE L2 DOOR WAS FOUND TO HAVE IMPROPER CLEARANCE BETWEEN DOUBLER/STOP AND GIRT BAR. MAINTENANCE REPLACED THE GIRT BAR. INSPECTED INSTALLATION AND FOUND SERVICEABLE. (M) 2L72 4F RTA28NM 20030710000462003071000046NM 2003 7 10 DHL2003747513 120030512A5320 STIFFENER BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK, RIGHT WHEEL WELL BS 870 AND KEEL BEAM, VERTICAL STIFFENER IS CRACKED. RUNNING FROM UNDERNEATH REINFORCE PLATE. REMOVED PNEUMATIC DUCTS RT A/C BAY AT FLOW MULTIPLIER IAW B-727 SRM 36-00-01. REMOVED STIFFENER DAMAGED IAW B-727 SRM 51-30-2, DRILLING NEW ANGLE P/N 65-18636-378 PO 312626 IAW B-727 SRM 51-30-5. TREATED AND PRIMED NEW HOLES IAW B-727 SRM 51-10-2. INSTALLED NEW ANGLE IAW B-727 SRM 51-30-2. REINSTALLED PNEUMATIC DUCTS RT A/C BAY AT FLOW MULTIPLIER IAW B-727 MM 36-00-01. LEAK CHECK FOUND NORMAL IAW B-727 MM 21-51-0 AND 36-00-01. 2L73 4F A3WE 20030710000472003071000047NM 2003 7 10 DHL2003747514 120030512A5312 BEAM BOEING727 727224 1384076NM PRESS BULKHEAD CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK, AFT PRESS BULKHEAD BS 1183 LBL 36.4 VERTICAL BEAM CRACK INDICATION WL 149 APPROX IS ABOUT 1 INCH LONG NDT, CONFIRMED. STOP DRILLED CRACK IAW B-727 SRM 51-10-1. AREA HFEC INSPECTED AND VERIFIED CRACKS END IN STOP DRILL HOLES. INSTALLED S/B REPAIR PARTS IAW S/B 727-53-0192 REV 1 FIG 2. P/N 65C34488-2 PO 312649, 65C34488-3 PO 312660. 2L73 4F A3WE 20030710000582003071000058WP 2003 7 10 DHL2003807010 120030531A52701EN32R SWITCH DOUG DC8 DC873F 302199FWP CARGO DOOR BROKEN A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01807DH 45990 AT FL 330 BELLY DOOR OPEN LIGHT ILLUMINATED PERFORMED ABNORMAL PROCEDURE. PRESSURIZATION NORMAL. CONTINUED NORMAL OPERATIONS. FOUND A PIT CARGO DOOR SWITCH BROKEN. REMOVED AND REPLACED SWITCH, OP CHECKS GOOD PER DC8 M/M 52-70-0 AND WDM 52-3-0. 2L74 4F RT4A25 20030710000752003071000075NM 2003 7 10 DHL2003741003 120030603A2611302842 SMOKE DETECTOR BOEING727 7272Q9 138448MNM MAIN CABIN WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01741DH 21931 NR 6 SMOKE DETECTOR IN MAIN CABIN DOES NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR IAW B-727 26-16-01. 2L73 4F RTA3WE 20030710000772003071000077WP 2003 7 10 DHL2003806009 120030611A2820 SEAL DOUG DC8 DC873F 302199FWP NR 3 PYLON LEAKING A DHLAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO01806DH 46002 FUEL LEAK UNDER WING BETWEEN NR 3 & 4 PYLON. TORQUED GAMMA SEAL JUST OUTBOARD NR 3 PYLON LEAK CHECKED GOOD IAW M/M 28-21-14. 2L74 4F RT4A25 20030710000802003071000080EU 2003 7 10 DHL2003366501 120030525A5753UNK RIB AIRBUS300 A300B4203 3930306EU FLAP TRACK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 LW AFT FLAP TRACK FAIRING 533AM, RIB CRACKED AT LIGHTENING HOLE. STOP DRILLED CRACK IAW A300 SRM 51-41-10. ROUTED OUT REMAINING CRACK IN EDGE IAW A300 SRM 51-41-20. MAT VERIF 2024T3 .040 IAW A300 SRM 57-36-11 & SRM 51-21-00. FAB REPAIR DOUBLER IAW A300 SRM 51-41-20. MAT USED 2024T3, .040 PO 411449.1. INSTALLED REPAIR DOUBLER IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20030710000862003071000086NM 2003 7 10 DHL2003746504 120030603A5320 STIFFENER BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 DURING C-CHECK DISCREPANCY AS FOLLOWS, N/R 54232 L/W WS 92.8 LOWER SECTION OF VERTICAL STIFFENER IS CRACKED, EMANATING FROM RIVET. CUT-OUT CRACK L-ANGLE 4.4 IAW B-727 SRM 51-40-3 FIG 1. FABBED 1 EACH L-ANGLE AND L-ANGLE DOUBLE MAT 7075-T6 .032, 7075-T6 .040 PO 209041 AND 9912240 IAW B-727 SRM 57-20-2 FIG 1 51-40-3 FIG 1. TREAT AND PRIME L-ANGLE AND DOUBLER IAW B-727 SRM 51-30-2 AND INSTALLER L-ANGLE AND DOUBLER IAW B-727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20030710000902003071000090NM 2003 7 10 DHL2003745013 120030607A33501000679 LIGHT BOEING727 727224 1384076NM CABIN INTERMITTENT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01745DH 20665 EMERGENCY EXIT LIGHT AT L1 DOOR WORKS INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR IAW M/M REF 33-50-01. GROUND OPS CHECKED GOOD. 2L73 4F A3WE 20030710000992003071000099SO 2003 7 10 C2XA03CL109 120030614A3260852701 SWITCH EMB 145 EMB145ER 3260211SO LANDING GEAR FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2714947 145054 ROC FLIGHT 2033 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LEFT NR 1 AND RIGHT NR 2 MAIN GEAR PROXIMITY SWITCHES. ALSO REPLACED THE LEFT MAIN GEAR TRAILING ARM TARGET. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030710001002003071000100SO 2003 7 10 C2XA03CL110 120030612A3397 WIRE EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT BROKEN A C2XAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW2714505 145192 CLE FLIGHT 2008 THE CREW REPORTED AISLE PATH LIGHTING STRIP INOPERATIVE BY LAVATORY. MAINTENANCE REPAIRED BROKEN WIRE ON LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030708000722003070800072NM 2003 7 8 AWXA200300643 120030513A53116546538551 FRAME BOEING737 737277 1384570NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A .5000 INCH CRACK WAS FOUND ON RADIUS OF SIDE FRAME AT BS 597, LBL 70. MAINTENANCE TRIMMED OUT DAMAGE AT BEND OF THE FLANGE ON SIDE FRAME AT BS 597, LBL 70; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW E.R. 15-5362-03150-ES1. 2L72 4F RTA16WE 20030708000832003070800083NE 2003 7 8 A301037 220030323A7313430167601C MANIFOLD BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE FUEL SYS FAILED A OLRAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP11911WJ 7050 ON 12 MINUTE FLIGHT NR2 ENGINE. FUEL MANIFOLD STARTED SLOW DRIP LEAK AT 10 OCLOCK NOZZLE. MEDICAL CREW REPORTED STRONG SMELL OF FUEL ON SHORT FINAL. PILOT GROUNDED AIRCRAFT MAINTENANCE INSPECTION AND FOUND LEAK. MAIN RECOMMENDS INSTALLATION OF FLEXIBLE NOZZLE INTERCONNECT TUBE MAINIFOLDS LIKE MFG. 1G72 3U3 U H13EU E5NE 20030708000872003070800087WP 2003 7 8 UPS03840883 120030625A2611 SMOKE DETECTOR DOUG DC8 DC871F 302199DWP CARGO BAY MALFUNCTIONED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01703UP 45939 DURING CLIMB OUT MAIN CARGO COMPARTMENT SMOKE INDICATOR ILLUMINATED. REMOVED AND REPLACED NR 6 SMOKE DETECTOR ASSEMBLY REF 26-10-07, ADJ/TEST OPS GOOD. 2L74 4F RT4A25 20030709000802003070900080WP 2003 7 9 MWEA030240 120030606A5230591014167 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 MID CARGO DOOR PAN IS CRACKED AFT END JUST BELOW TORQUE TUBE FITTINGS. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030716000662003071600066SO 2003 7 16 SIMA200316005 120030524A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21810AE 145525 DURING AN MBV, THE CENTER FLOORBEAM LOWER FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAME 26 AND 27. BLENDED THE DAMAGED AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA WITH NO DEFECTS NOTED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW EMB STATEMENT IC2003-145/1766, EMB SRM, SRM EMB 145/1142 REV 21, 53-21-10 PARA 9 FIG 208 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030710001152003071000115NM 2003 7 10 DHL2003749007 120030616A2613 SENSOR BOEING727 727200 138407ENM OVERHEAT WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01749DH 22013 LOWER AFT BODY OVERHEAT WILL NOT TEST. DEFERRED PER MEL 26-10-2. SP 26-10-2 COMPLIED WITH. DMI 13274 PLACARD INSTALLED. MAINTENANCE CONTROL NOTIFIED. REF DMI 13274; LOWER AFT BODY OVERHEAT WILL NOT TEST. TROUBLESHOT AND TESTED SYSTEM IAW BMM 26-14-00. NORMAL OPERATIONS. THIS CLEARS DMI 13274, PLACARDS REMOVED. 2L73 4F RTA3WE 20030711000172003071100017SO 2003 7 11 C2XA03SH194 120030622A532014525382003 SILL EMB 145 EMB145LR 3260212SO CARGO DOOR SCRATCHED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 SHV DURING C-CHECK CARGO COMPARTMENT LT SILL LIFT AT FRAME 73 WAS FOUND TO HAVE SCRATCHES. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000282003071100028NM 2003 7 11 PCAA0306078 120030619A2910NAS16128 O-RING DHAV DHC8 DHC8102 2809003NM HYD SYSTEM FAILED A PCAAB EMER. DESCENT K FLUID LOSS APAPPROACH 1 EA13832EX 280 FLIGHT 3867 FROM SYR TO LGA ON APPROACH TO LGA CREW NOTICED NR 2 HYDRAULIC ISOLATION VALVE CONTENTS WERE CLOSE TO ZERO. CREW DECLARED AN EMERGENCY. PUT THE GEAR DOWN MANUALLY AND LANDED WITHOUT FURTHER INCIDENT. LGA MECHANIC INSPECTED AND FOUND O-RING ON ONE LINE TO POWER TRANSFER UNIT LEAKING. REMOVED AND REPLACED O-RING. SERVICED AND BLED NR 2 HYDRAULIC SYSTEM, LEAK CHECKED GOOD IN ACCORDANCE WITH MAINTENANCE MANUAL CHAPTER 29-11-00. 2H72 4T RTA13NM 20030711000472003071100047SO 2003 7 11 C2XA03CL115 120030620A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716919 145393 DURING ROUTINE MAINTENANCE NR 2 AND NR 3 EMERGENCY AISLE PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030711000732003071100073NM 2003 7 11 C1HA200382007 120030626A2611824PY SMOKE DETECTOR BOEING727 7272S7 138407ZNM LAVATORY MALFUNCTIONED A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15682CA 22019 SMOKE DETECTOR FWD LAV ACTIVATES OCCASIONALLY WHEN DOOR IS SHUT. 2L73 4F A3WE 20030711000892003071100089NM 2003 7 11 EIA2003091 120030626A28206070334 CHECK VALVE BOEING747 747212B 1384886NM FUEL SYSTEM BENT A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 JETTISON PUMP CHECK VALVE FOUND BENT. INSTALLED NEW VALVE. PART NUMBER 60-703137. 2L74 4F A20WE 20030711000902003071100090SO 2003 7 11 C2XA03IA067 120030625A3350 POWER SUPPLY EMB 145 EMB145 3260210SO EMERGENCY LIGHT MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713965 145125 DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS WERE INOP. MAINTENANCE RESET THE EMERGENCY LIGHTING POWER SUPPLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030714000032003071400003NM 2003 7 14 CALA0300340 120030627A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717644 28905 INSPECTION FOUND A .125 INCH CRACK IN INTERCOSTAL AT FORWARD ENTRY, STA 312-328, LBL 50.5. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030714000952003071400095NM 2003 7 14 SWAA031353 120030615A3260FCA410 RELAY BOEING737 7373Q8 1384670NM NLG LATCH FAULTY A SWAAO OTHER J WARNING INDICATION CLCLIMB 1 SW29317WN 24068 GEAR HANDLE RAISED, NLG RED UNSAFE LIGHT DID NOT EXTINGUISH. CYCLED GEAR ALL GREEN LIGHTS ILLUMINATED, RED LIGHT EXTINGUISHED. REMOVED AND REPLACED S845 SWITCH AND R375 NLG LATCHING RELAY PER MM. 2L72 4F RTA16WE 20030714000962003071400096NM 2003 7 14 SWAA031354 120030616A21317638102 CONTROLLER BOEING737 7373Q8 1384670NM COCKPIT FAILED A SWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW29688SW 23254 CABIN PRESSURE ALTITUDE WARNING HORN SOUNDED AT 35K, INITIATED PROCEDURES WITH EMERGENCY DESCENT. FOUND, PRESSURE CONTROLLER FAILURE. REMOVED AND REPLACED PRESSURE CONTROLLER PER MM. 2L72 4F RTA16WE 20030714000972003071400097WP 2003 7 14 DHL2003801081 120030701A2612 FIRE LOOP DOUG DC8 DC873F 302199FWP NR 3 ENGINE WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01801DH 46033 NR 3 ENGINE -A- FIRE LOOP DOES NOT TEST. PLACED NR 3 ENGINE -A- LOOP ON DMI 13406 AS PER MEL 26-2-3. REF DMI 13406 NR 3 ENGINE -A- FIRE LOOP DOES NOT TEST. CHECKED FIRE LOOP. FOUND FIRE LOOP TOUCHING ENGINE CASE. REPOSITIONED FIRE LOOP. OPS CHECKED GOOD AT THIS TIME M/M DC-8 26-10-0. THIS CLEARS DMI 13406. PLACARDS REMOVED. 2L74 4F RT4A25 20030714001132003071400113 2003 7 14 GLBA2003090 420030620A3442 INDICATOR BEECH 1900 1900D 1154162CE WX RADAR SYS INOPERATIVE A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03255GL UE255 WEATHER RADAR INOP. OPS CHK WX RADAR, OPS CK GOOD. 2L72 4T RTA24CE 20030715000182003071500018NM 2003 7 15 2003F00402 120030313A5320 CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACKED STRINGER FRAME ATTACH CLIP AT STATION 570, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT STATION 560 STRINGER 5R. (M) 2L73 4F A3WE 20030716000552003071600055WP 2003 7 16 GTIA030462 120030514A5340 FITTING DOUG DC9 DC981 3022081WP BULKHEAD CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND STRINGER 29L APB TEE NUTS NOT SELF CENTERING IAW SB-53-201 AND REQUIRE GOUGE INSPECTION UPON REMOVAL. AFTER REMOVAL OF NUTS DISCOVERED CORROSION ON TEE FITTING. REMOVED TEE FITTING. LOCATED AND DRILLED NEW TEE FITTING. INSTALLED TEE FITTING. (M) 2L72 4F A6WE 20030716000782003071600078WP 2003 7 16 GTIA030470 120030511A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 MAIN CABIN FS 754 RIGHT CENTER FLOOR PANEL HAS BROKEN INSERT. REMOVED PANEL. FABRICATED PANEL. INSTALLED FLOORBOARD. (M) 2L72 4F A6WE 20030716000792003071600079NM 2003 7 16 2003F00426 120030305A5720 WEB BOEING727 727222 1384073NM FS 870 CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND RT MLG WW FORWARD BULKHEAD INBOARD WEB CRACKED, STATION 870. STOP DRILLED CRACK AT INBOARD SIDE OF STATION 870, RIGHT WHEEL WELL. HFEC VERIFIED STOP DRILL. FABRICATED REPAIR DOUBLER FOR AFT SIDE OF STATION 870 BULKHEAD WEB AND REPAIR DOUBLER FOR FORWARD SIDE OF BULKHEAD WEB. TREATED AND PRIMED DOUBLERS AND AREA. INSTLALED DOUBLERS ON FORWARD AND AFT SIDES OF STATION 870 BULKHEAD. (M) 2L73 4F A3WE 20030716000882003071600088NM 2003 7 16 USAABB03097 120030622A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 18 AND 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030716000972003071600097EU 2003 7 16 HE66087954 120030709A6340 NEEDLE BOLKMS105 BO105LSA1 5626021EU TRIPLE TACH DEFECTIVE B HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03202LF 028 2014 TRIPLE TACH NEEDLES WERE STICKING REPLACED TRIPLE TACH 1G72 3U H3AU 20030716001102003071600110NE 2003 7 16 HEEA088039 120030703A62207610608000050 DAMPENER SKRSKYS76 S76A 8143006NE MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 MAIN ROTOR DAMPER WORN. REPLACED DAMPER. 1G72 3U H1NE 20030716001142003071600114NE 2003 7 16 HEEA088044 120030706A24207655009005105 GENERATOR SKRSKYS76 S76A 8143006NE ELECTRICAL INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 GENERATOR INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030717000032003071700003SW 2003 7 17 HEEA087980 120030701A6420 BEARING BELL 412 412 1182202SW TAIL ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH9091 TR030299 33150 FEATHERING BEARINGS WORN. SHOP REPAIR. 1G72 4U H4SW 20030717000052003071700005 2003 7 17 HEEA087982 420030629A2215412001700101 SERVO BELL 412 412 1182202SW AFCS YAW ACTUATOINOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 AFCS YAW ACTUATOR CHANNEL INOPERATIVE. TO BE SENT TO VENDOR. 1G72 4U H4SW 20030717000272003071700027SW 2003 7 17 HEEA088004 120030626A6220407010150109 FRAHM BELL 407 407 1182206SW MAIN ROTOR VIBRATION E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 FRAHM ASSY HAS ONE PER REV VIBRATION. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000412003071700041SW 2003 7 17 HEEA088016 120030626A2510407070731103 HEADREST BELL 407 407 1182206SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 DISSENGAGE PINS WILL NOT DISSENGAGE FOR HEADREST ADJUSTMENT. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000682003071700068GL 2003 7 17 HEEA088081 220030702A753223053176 BLEED VALVE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 BLEED VALVE PRODUCING ENGINE HIGH TOT. SHOP REPAIR. 1G72 3U3 U H3EU E4CE 20030717000712003071700071SW 2003 7 17 HEEA088063 120030608A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032260812101 33075 MAIN ROTOR BLADE FRETTING PAD ON THE LOWER SIDE HAS SOME SEPERATION. FIBERGLASS CRACKED NEAR THE INBOARD TRIM TAB. 1G72 4U H4SW 20030717000722003071700072 2003 7 17 HEEA088064 420030621A344280511400003 CONTROL UNIT BELL 412 412 1182202SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 WEATHER RADAR INDICATOR R/T RANGE FAIL. 1G72 4U H4SW 20030717000732003071700073SW 2003 7 17 HEEA088065 120030703A79218543909 OIL COOLER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 ENGINE TEMPS WERE RUNNING NEAR THE UPPER RED LINE. REPLACED OIL COOLER. 1G71 3U3 U H2SW E1GL 20030717000752003071700075SW 2003 7 17 HEEA088067 120030703A2620A344T EXTINGUISHER BELL 206 206L3 1182108SW CABIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 FIRE EXTINGUISHER HAS LOW PRESSURE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030717000762003071700076SW 2003 7 17 HEEA088068 120030701A6730C4264144 SEAT CLARK 1000 1000CLARK 2230102SW CYLINDER LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 RH1636 CAUSING EXCESSIVE INTERNAL LEAKAGE. REPLACED WITH SERVICEABLE PART. 1Q71 3R 2A6 20030709000822003070900082 2003 7 9 MALA030289 420030530A34146225353011 INDICATOR SAAB SF340 340B 7860101EU AIRSPEED MALFUNCTIONED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15427XJ 340B427 DURING FLIGHT 3323 CAPT AIRSPEED INDICATOR BARBERPOLE SPINNING CONTINUOUSLY INFLIGHT. INDICATION FOR AIRSPEED SEEMS NORMAL. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED NR 1 AIRSPEED INDICATOR REF AMM 34-10-00. P/N ON/OFF 622-5353-011. S/N OFF 381. S/N ON 133. OPS TEST OK. 2L72 4T RTA52EU 20030709001112003070900111SO 2003 7 9 C2XA03SH181 120030612A531514522461011 DOUBLER EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709001302003070900130EA 2003 7 9 03167652 120030616A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27652BR 7429 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN ENTRY DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030710000012003071000001NM 2003 7 10 KPVA200323 120030608A33506104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13807WP 023 EMERGENCY EXIT FLOOR PATH LIGHTS ALL OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLIES 3352-PSI AND 3352-PS2. OPS CHECK GOOD IAW DHC 9 MM 33-51-00 PAGE 202. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030710000352003071000035NM 2003 7 10 USAA030051 120030508A532065458078 INTERCOSTAL BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US40013 23990 PIT - FOUND WEB INTERCOSTAL CRACKED .5 INCH, FS 277-294.5 AT S-14R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20030710000382003071000038NM 2003 7 10 USAA030087 120030523A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 FOUND FRAME WEB CRACKED .25 INCH, STATION 1440. INSTALLED TEMPORARY TIME LIMITED REPAIR PER EA 87186. (M) 2L72 4F RTA2NM 20030710000692003071000069NM 2003 7 10 DHL2003780011 120030606A5270 DOOR BOEING727 727223 1384074NM PAX OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01780DH 22006 FORWARD ENTRY LIGHT ILLUMINATED ON LANDING. PERFORMED ADJUSTMENT OF MAIN FORWARD ENTRY DOOR IAW B-727 M/M 52-11-01. OPS CHECKED SERVICEABLE. 2L73 4F A3WE 20030710000742003071000074NM 2003 7 10 DHL2003746503 120030603A5311 FRAME BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 DURING C-CHECK DISCREPANCY AS FOLLOWS N/R 54181, IN FWD CARGO FRAME BS 680 HAS 5 DENTS INTO THE RADIUS BETWEEN STR 26L AND STR 24L. CUT-OUT DAMAGED AREA OF FRAME BS 680 DIMENSIONS 10 INCHES X 1 INCH AND FABRICATED ONE DOUBLER REPAIR DIMENSIONS 22 INCHES X 4 INCHES USING 7075-T6 .063 PO 9912495 IAW B-727 51-40-3 FIG 3 AND 53-10-2 FIG 3. ALODINED AND PRIMED REPAIR DOUBLER IAW B-727 51-10-2. INSTALLED REPAIR AT FRAME BS 680 IAW B-727 SRM 51-40-3 FIG 3. 2L73 4F A3WE 20030710000832003071000083EU 2003 7 10 DHL2003366504 120030605A5320 INTERCOSTAL AIRBUS300 A300B4203 3930306EU FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 LT SIDE INTERCOSTAL BETWEEN FRAME 83-84 BENT. REMOVED INTERCOSTAL BETWEEN FR 83 & 84 (STR 30) M ID FOR THE INTERCOSTAL IS CLAD 2024T3 .040. FABBED JOINING SECTION IAW A300 SRM 51-41-30. ALODINED IAW A300 SRM 51-40-12, PRIMED AND PAINTED IAW A300SRM 51-40-12. INSTALLED REPAIR (JOINING SECTION) IAW A300 SRM 51-30-30 AND REINSTALLED INTERCOSTAL IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20030710001482003071000148NM 2003 7 10 EIA2003086 120030614A5753 FLAP TRACK BOEING747 747SR46 1384816NM WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 NR 1 FLAP TRACK FWD O/B SIDE FIRST 4 BOLT HOLES ARE CORRODED AND SOME CAD PLATING MISSING. REWORKED NR 1 FLAP TRACK O/B HOLES 1-4 PER SB 747-57-2256 PAGE 1-52. 2L74 4F RTA20WE 20030711000182003071100018SO 2003 7 11 C2XA03SH195 120030622A532014521725013 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK SERVICE DOOR FOWARD SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000202003071100020SO 2003 7 11 C2XA03SH197 120030622A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO DOORWAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000212003071100021SO 2003 7 11 C2XA03SH198 120030622A541114576057621 RIB EMB 145 EMB145LR 3260212SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK NUMBER TWO UPPER COWLING WAS FOUND TO HAVE A GOUGE AT THE AFT RIB. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED RIB IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000312003071100031NE 2003 7 11 MWEA030251 220030619A732176960615 FUEL CONTROL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE ENGINE INOPERATIVE A MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31601ME 49762 P725404D AFTER APPLYING TAKEOFF POWER RIGHT FUEL FLOW FLASHED AND INDICATED APPROXIMATELY 11,00 POUNDS PER HOUR, EXHAUST GAS TEMPERATURE FLASHED & INDICATED IN YELLOW ARC. AFTER VISUAL INSPECTION REMOVED AND REPLACED RIGHT ENGINE FUEL CONTROL. 2L72 4F4 FRTA6WE E9NE 20030711000322003071100032EU 2003 7 11 DHL2003366513 120030524A5411 RIB AIRBUS300 A300B4203 3930306EU NACELLE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 NR 1 ENG O/B CORE NACELLE INTERIOR AFT RIB IS DAMAGED. ROUTED OUT DAMAGE AREA AN INSTALLED REPAIR DOUBLER IAW TIMCO REO G09306. 2L72 4F RTA35EU 20030711000342003071100034WP 2003 7 11 DHL2003801006 120030621A3260 CONNECTOR DOUG DC8 DC873F 302199FWP MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 AFTER TAKEOFF & GEAR RETRACTION RED DOOR NOT LATCHED LIGHT AND RIGHT DOOR UNSAFE LIGHT WERE ILLUMINATED. GEAR DOOR NOT LATCHED LIGHT ILLUMINATED ABNORMAL PROCEDURE FOLLOWED, LIGHTS REMAINED ILLUMINATED. CLEANED AND RESEATED CONNECTOR ON RIGHT GEAR DOOR SWITCH PER DC-8 M/M 32-60-0. JACKED AIRCRAFT AND SWUNG LANDING GEAR PER DC-8 M/M 32-11-1. OPS CHECKED SERVICEABLE ON GROUND. 2L74 4F RT4A25 20030711000362003071100036EU 2003 7 11 DHL2003366516 120030525A7830 ANGLE AIRBUS300 A300B4203 3930306EU THRUST REVERSER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 NR 1 ENG I/B THRUST REVERSER ANGLE FOR THE UPPER T/R HINGE ACCESS PANEL CRACKED. REMOVED ANGLE TO FOM, MAT ID 224T3 .040 PO 411449.1, FABBED REPAIR ANGLES IAW A300 SRM 51-41-30, ALODINED AND PRIMED IAW A300 SRM 51-40-12. INSTALLED REPAIRS IAW A300 SRM 51-30-30, REINSTALLED ANGLE IN A/C IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20030711000422003071100042 2003 7 11 371PA0023 420030622A3460 COMPUTER BOEING737 737306 13844BGNM FLT MANAGEMENT INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05371PA 23543 NR 1 FMC CLIMB PAGE INOP. UNABLE TO ACCESS. NR 1 FMC/CDU CLIMB FUNCTION KEY INOP. DEFERRED PER MEL 34-36-3. 2L72 4F RTA16NE 20030711000632003071100063SO 2003 7 11 C2XA03CL116 120030623A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2716919 145393 CLE FLIGHT 2058 THE CREW REPORTED DURING PREFLIGHT THE EMERGENCY EXIT LIGHT WAS INOPERATIVE AT ROW 12. MAINTENANCE REPLACED THE NR 6 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030711000652003071100065NM 2003 7 11 CALA0300332 120030623A2420 CIRCUIT BREAKER BOEING737 737524 1384721NM NR 1 ENGINE FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27176142598425984 8071 27327 A HEAVY ELECTRICAL ODOR WAS NOTICED IN THE CABIN WHILE EN ROUTE TO DCA. THE ODOR WAS ACCOMPANIED BY FAILURE OF CABIN LIGHTS, OVEN, AND AUTOPILOT AND THE NR 1 ENGINE GENERATOR BUS OFF LIGHT, AND RIGHT EQUIP COOLING SUPPLY OFF LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 TRANSFORMER RECTIFIER (TR) C/B POPPED. THE NR 1 TR CIRCUIT BREAKER WAS REMOVED AND REPLACED. THE NR 1 TRANSFORMER RECTIFIER WAS REMOVED AND REPLACED IAW MM 24-21-31. ALL OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTA16WE 20030711000682003071100068SO 2003 7 11 C2XA03SH204 120030626A532013500322001 SILL EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030711000822003071100082EA 2003 7 11 COMA0360289 120030624A2410 IDG CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAC ABORTED TAKEOFF JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01949CA 7080 FLIGHT 5304 LEFT IDG CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030711000872003071100087NM 2003 7 11 CALA0300336 120030625A5330 SKIN BOEING737 737824 13844BZNM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 INSPECTION FOUND A HOLE PUNCTURED INTO THE FUSELAGE SKIN THREE FEET BELOW THE L-2 DOOR AT BS 958, S22L-S23L. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5330-03261. 2L72 4F RTA16WE 20030709000392003070900039WP 2003 7 9 AALA20030500 120030426A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW213515 49892 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTING FROM ROW 13-17 INOPERATIVE. REPOSITIONED CEILING EMERGENCY EXIT LIGHTING BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000412003070900041WP 2003 7 9 AALA20030513 120030430A3350 BULB DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21490AA 49683 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED LIGHT FROM 3EE-19D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BULB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000892003070900089 2003 7 9 250TR0018 420030606A34202591092904 INDICATOR BOEING737 7372K5 138448XNM COCKPIT MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 F/O'S ADI JUMPS & TURNS. REPLACED F/O'S ADI. OPERATIONAL TEST NORMAL PER MM 34-22-0. 2L72 4F RTA16WE 20030710000092003071000009SO 2003 7 10 ASOA03244 120030531A3397M22759209 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11266AS 120188 FLT 4925 - DURING A GROUND INSPECTION IN DFW, THE LEFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE WIRE SPLICE ON THE LEFT EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030710000162003071000016NM 2003 7 10 TSAA0333146 120030607A33508610062 BATTERY PACK BOEING737 73725A 1384481NM PAX CABIN INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030710000182003071000018NM 2003 7 10 TSAA0353149 120030504A53106545875070 CREASE BEAM BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 FOUND CORROSION ON RIGHT CREASE BEAM AROUND NUT PLATE HOLES BETWEEN BS 290 AND 358. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 290 AND BS 358. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-2. (M) 2L72 4F RTA16WE 20030710000322003071000032NM 2003 7 10 USAA030077 120030529A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU59253 22202 CLT - FOUND 1.25 INCH CRACK, BS 1440 FRAME BETWEEN S 26R AND S 27R. INSTALLED NEW FRAME SECTION AND REPAIR SPLICES PER EA 87211, 87187A, 87230. (M) 2L72 4F RTA2NM 20030710000392003071000039EU 2003 7 10 SIMA200314701 120030522A3230HP848430621 CONTROL VALVE SAAB SF340 340B 7860101EU MLG INOPERATIVE A SIMAO OTHER J WARNING INDICATION LDLANDING 1 SW21373AE 340B373 ON APPROACH TO SPS LANDING GEAR WOULD NOT EXTEND. CREW RETURNED TO DFW AND DID AN EMERGENCY EXTENSION AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE IAW SAAB MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE AFTER REPLACEMENT OF EXPLOSIVE BLOTS IN THE MAIN GEAR. (M) 2L72 4T RTA52EU 20030711000372003071100037NM 2003 7 11 DHL2003754011 120030621A3260 SWITCH BOEING727 727223 1384074NM RT MLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01754DH 22008 UPON GEAR RETRACTION, RED DOORS LIGHT ON PILOTS FORWARD PANEL & AMBER RIGHT GEAR DOOR LIGHT STAYED ILLUMINATED ON SECOND OFFICER'S ANNUNCIATOR PANEL. NO VIBRATIONS FELT IN AIRCRAFT. CLEANED AND ADJUSTED RT MAIN LANDING GEAR DOOR SWITCH IAW M/M 32-62-11. OPS CHECKED NORMAL. OK FOR SERVICE. 2L73 4F A3WE 20030711000502003071100050EA 2003 7 11 COMA0360283 120030620A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HANDLE ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01966CA 7132 FLIGHT 5099 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. AIRCRAFT DID NOT PRESSURIZE. COULD NOT DUPLICATE. DOOR OPERATES NORMAL, AIRCRAFT PRESSURIZES NORMAL. 2L72 4F RTA21EA 20030711000512003071100051EA 2003 7 11 COMA0360285 120030622A2750860D10018ABCD COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01458CA3915 7613 FLIGHT 5514 FLAPS FAIL MESSAGE DURING TAXI. REPLACED THE FECU. 2L72 4F RTA21EA 20030711000782003071100078NM 2003 7 11 DHL2003745014 120030623A3233651783013 ACTUATOR BOEING727 727224 1384076NM MLG MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 AFTER TAKEOFF AFTER GEAR RETRACTION LEFT MAIN RED GEAR DOOR LIGHT, RED DOORS LIGHT LEFT & RIGHT AMBER ON S/O PANEL WITH GEAR HANDLE UP. RAN ABNORMAL PROCEDURE. RETURNED TO SAN 3 GREEN. AS SOON AS GEAR HANDLE WAS PLACED DOWN THE LEFT MAIN GEAR LIGHT (GREEN) CAME ON. REMOVER AND REPLACED LEFT GEAR ACTUATOR IAW B727 M/M 32-32-2. OPS CHECKED IAW WITH ALTERNATE METHOD IAW B727 M/M 32-00-11. OPS AND LEAK CHECKED GOOD. 2L73 4F A3WE 20030711001192003071100119WP 2003 7 11 MWEA030258 120030627A53475956594521 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 MODERATE CORROSION ON MID-PIT LEFT SIDE TIE RAIL FROM FRAME STAION 541 AFT TO FRAME STATION 788. FABRICATED AND INSTALLED SPLICE FOR TIE DOWN RAIL, FABRICATED AND INSTALLED AFT SLPICE. 2L72 4F A6WE 20030711001222003071100122WP 2003 7 11 MWEA030261 120030630A55315910242115 FRAME DOUG DC9 DC982 3022082WP VERTICAL STAB DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 STATION 1420 FRAME LOCATED INSIDE THE VERTICAL STABILIZER IS DAMAGED ON BOTH LOWER ENDS. REMOVED AND REPLACED FORMER. 2L72 4F A6WE 20030714000062003071400006NM 2003 7 14 CALA0300343 120030627A5347 GALLEY TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND GALLEY TRACK CORRODED BETWEEN BS 328 AND 360 AT RBL 44. THE FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030714000132003071400013WP 2003 7 14 MWEA030269 120030629A324495502676 WHEEL DOUG DC9 DC981 3022081WP MLG VIBRATION A MWEAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL31805ME 48031 NOSE WHEEL VIBRATION. REMOVED AND REPLACED LT AND RT NOSE TIRE AND WHEEL ASSEMBLY. 2L72 4F A6WE 20030714000192003071400019NM 2003 7 14 SWAA031422 120030626A27316959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB INPUT ROD HARDWARE AND BUSHING. 2L72 4F RTA16WE 20030714000302003071400030NM 2003 7 14 SWAA031402 120030624A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030714000422003071400042NM 2003 7 14 SWAA031357 120030617A3350AD20131A BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY LOW. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030714000452003071400045NM 2003 7 14 SWAA031370 120030620A3350BCREF4146 LIGHT BOEING737 7372H4 138448CNM COCKPIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY PER MM. 2L72 4F A16WE 20030714000472003071400047NM 2003 7 14 SWAA031372 120030619A335020131H BALLAST BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST AND BATTERY PER MM. 2L72 4F RTA16WE 20030714000482003071400048NM 2003 7 14 SWAA031373 120030619A3350101114 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C3 CHECK, FOUND AFT CABIN CENTER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030714000582003071400058NM 2003 7 14 SWAA031360 120030618A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20030714000622003071400062NM 2003 7 14 SWAA031364 120030618A2560P2070001 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED RON, FOUND AFT CABIN LOWER EMERGENCY FLASH LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20030714000712003071400071 2003 7 14 SWAA031386 420030621A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030714000732003071400073NM 2003 7 14 SWAA031388 120030621A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SURFACES. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030714000772003071400077NM 2003 7 14 SWAA031412 120030625A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHTLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 EEPLS COVER LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030714000842003071400084NM 2003 7 14 SWAA031342 120030615A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 562, STR 4R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030714000922003071400092NM 2003 7 14 SWAA031350 120030615A3350311500 LENS BOEING737 7373Y0 1384671NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030709000692003070900069EA 2003 7 9 03153646 120030602A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27646BR 7392 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 3 CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030709000772003070900077EA 2003 7 9 03155706 120030604A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT FWD OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030709000962003070900096SO 2003 7 9 C2XA03TY085 120030611A575314568000432 SKIN EMB 145 EMB145LR 3260212SO FLAP DELAMINATED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING A SCHEDULED INSPECTION THE RIGHT INBOARD FLAP LOWER TRAILING EDGE DELAMINATED. MAINTENANCE REPAIRED THE DELAMINATED AREA I/A/W-EC5750-01196, PRIMED AND PAINTED I/A/W-CMP-51-21-03/05/05. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030710000142003071000014NM 2003 7 10 TSAA0351143 120030505A53136573744 STRINGER BOEING737 73725A 1384481NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DAMAGED STRINGER 2 RIGHT WHILE REMOVING STRINGER CLIP. CUTOUT DAMAGED STRINGER SECTION BETWEEN BS 360 AND BS 389. FABRICATED NEW STRINGER SECTION, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 3. (M) 2L72 4F RTA16WE 20030710000562003071000056NM 2003 7 10 DHL2003754008 120030523A261318U1 CIRCUIT BREAKER BOEING727 727223 1384074NM OVERHEAT SYSTEM FAILED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 LOWER AFT BODY OVERHEAT WILL NOT TEST. LOWER AFT BODY OVERHEAT TEST FEATURE AT FLIGHT DECK DEFERRED PER MEL 26-10-2 CAT C. DMI 13038 SPECIAL PROCEDURE 26-10-2, COMPLIED WITH, PLACARD INSTALLED. REF DMI 13038 LOWER AFT BODY HEAT WILL NOT TEST. PER MEL REQUIREMENT PERFORMED SP 26-10-2. SYSTEM INDICATION NORMAL. DMI 13038 STILL IN EFFECT. REF DMI CONTROL NR 13038 MEL 26-10-2 LOWER AFT BODY OVERHEAT WILL NOT TEST. REMOVED AND REPLACED OVERHEAD DETECTION CIRCUIT BREAKER IAW M/M CHAPTER 20. SYSTEM TEST CHECKED GOOD IAW M/M 26-14-0. THIS CLEARS DMI 13038. PLACARD REMOVED. 2L73 4F A3WE 20030710000732003071000073NM 2003 7 10 DHL2003746502 120030601A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 DURING C-CHECK DISCREPANCY AS FOLLOWS, N/R 54096 FUSELAGE HAS (2) DENTS BETWEEN STA 1070-1090 BETWEEN STR 17L-18L. CUT-OUT 1 EACH DENT AREA DIM 1.0 X 1.0 IAW B-727 SRM 53-30-3 FIG 3. EVALUATION OF SECOND DENT IS WITHIN LIMITS BY A/Y RATIO A .039 DIVIDED BY Y 1.54 = 38.46 IAW B-727 SRM 53-30-1. FAB DOUBLER FORM 2024-T3 .071 PO 9912441 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20030710000882003071000088NM 2003 7 10 DHL2003746505 120030603A5310 SHEAR TIE BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 DURING C-CHECK DISCREPANCY AS FOLLOWS, N/R 54183 RT SHEAR WEB CRACKED AND CORRODED AT BS 1169 RBL 17 MARKED IN RED. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 7075 T-6 .050 PO 9912380 DIM 5 X 7.5 AND DOUBLER FROM 7075 T-6 .063 PO 9912495 DIM 7.5 X 7.5 IAW 727 SRM 51-40-2 FIG 1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. PARTS INSTALLED IAW B-727 SRM 51-40-2 FIG 1. 2L73 4F A3WE 20030711000292003071100029NM 2003 7 11 EIA2003072 120030430A5313 STRINGER BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 CORROSION DAMAGED STRINGER S42L BS 585 IN FORWARD CARGO PIT AREA. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-03, PAGE 1-4. 2L74 4F RTA20WE 20030711000612003071100061WP 2003 7 11 MWEA030252 120030624A534799578711 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 CAPTAINS AFT OUTBOARD SEAT TRACK IS WORN BEYOND LIMITS. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20030711000672003071100067SO 2003 7 11 C2XA03TY086 120030623A5330 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2716112 145660 MAINTENANCE FOUND DAMAGE SKIN ON THE LT FORWARD FUSELAGE BETWEEN FR 1 AND FR 3 BETWEEN STR 13L AND 15L. MAINTENANCE REMOVED THE DAMAGE SECTION OF STR 13L AND SPLICED IN A NEW SECTION. RECONTOURED FR 3. REMOVED AND REPLACED THE SKIN ON THE LT FWD FUSELAGE IAW EC 2003-145/2122; SRM 51-40-02;03;06. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED BACK TO SERVICE. 2L72 4T RTT00011AT 20030711001132003071100113 2003 7 11 373PA0016 420030626A221010620383 COMPUTER BOEING737 7373Y0 1384671NM AUTOPILOT MALFUNCTIONED A PIDAO OTHER O OTHER CRCRUISE 1 SO05373PA 23749 WHEN AUTO PILOT -B- ENGAGED, HDG SELECT ONLY GIVES 10 DEGREES OF BANK. PLACED ON MEL 22-15-8. 6/28/2003: RAN AUTO PILOT BITE TEST IAW MM 22-11-00. OPS CHECKS NORMAL AT THIS TIME. SWAPPED FCC'S AS A PRECAUTION. 2L72 4F RTA16WE 20030714000642003071400064 2003 7 14 SWAA031366 420030618A2565 INDICATOR BOEING737 7372H4 138448CNM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2L72 4F A16WE 20030714001112003071400111EA 2003 7 14 COMA0360307 120030628A3260601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG DEFECTIVE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01959CA17802 7116 FLIGHT 5803 WHEN LOWERING LANDING GEAR RECEIVED GEAR DISAGREE CAUTION. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20030714001202003071400120NM 2003 7 14 CALA0300353 120030701A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT NUT PLATE HOLES BETWEEN STA 344 AND 360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-40. 2L72 4F RTA16WE 20030714001302003071400130NM 2003 7 14 C1HA200395063 120030630A3350900835A BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LEFT FWD OVERWING EMERGENCY EXIT LIGHT INOP. 2L73 4F A3WE 20030714001322003071400132NM 2003 7 14 C1HA200395065 120030630A3350900835A BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LEFT FWD OVERWING OUTSIDE EMERGENCY EXIT LIGHT INOP. 2L73 4F A3WE 20030714001582003071400158NE 2003 7 14 ALGA087937 120030708A6320SB11061 BEARING SKRSKYS76 S76A 8143006NE M/R GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03741SW A08100051 760070 MAIN GEARBOX REMOVED FOR METAL IN OIL, FOUND BEARING BREAKING DOWN. 1G72 3U H1NE 20030714001692003071400169EU 2003 7 14 BAQA081100 120030523A672041800876800 ACTUATOR UROCOPEC135 EC135T1 5620026EU TAIL ROTOR WILL NOT TEST B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME1217 132 WILL NOT TEST AND ACTUATUION WITH A CORRESPONDING Y ON PFD. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030714001702003071400170EU 2003 7 14 BAQA086456 120030517A372041800876800 ACTUATOR UROCOPEC135 EC135T1 5620026EU TAIL ROTOR INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME1277 132 ACTUATOR INOPERATIVE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030715000122003071500012NM 2003 7 15 2003F00397 120030314A5315 FLOORBEAM BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON AFT CARGO FLOORBEAM AT STATION 950B, BL 0. FABRICATE NEW ANGLE. TREATED, PRIMED AND INSTALLED NEW ANGLE AT STATION 950B BL 0. (M) 2L73 4F A3WE 20030715000132003071500013NM 2003 7 15 2003F00398 120030313A5320 CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720A, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT STATION 720A STRINGER 5L. (M) 2L73 4F A3WE 20030715000152003071500015NM 2003 7 15 2003F00400 120030313A5320 CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720, STRINGER 3L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720 STRINGER 3L. (M) 2L73 4F A3WE 20030716000052003071600005NM 2003 7 16 2003F00406 120030611A49901605501 CONTROL VALVE BOEING737 737800* NM APU INOPERATIVE A MYWAO OTHER M OVER TEMP TXTAXI/GRND HDL 1 SO19733MA 30619 APU SHUT DOWN DUE TO HIGH OIL TEMPERATURE. REMOVED AND REPLACED APU OIL TEMP BULB IAW 49-94-11. NO HELP. REMOVED AND REPLACED OIL COOLER IAW 49-91-41. NO HELP. REMOVED AND REPLACED APU TEMP CONTROL VALVE IAW 49-91-21. OPS CHECKED GOOD ON RUN UP. FULLY LOADED APU FOR 30 MINUTES. NO DEFECTS NOTED. PLACARD REMOVED AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030716000162003071600016NM 2003 7 16 2003F00409 120030314A5754 BRACKET BOEING727 727222 1384073NM NR 6 SLAT BROKEN A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BRACKET BROKEN. REPLACD NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BOLT BRACKET. (M) 2L73 4F A3WE 20030716000182003071600018NM 2003 7 16 2003F00411 120030305A5280 HINGE BOEING727 727222 1384073NM RT MLG DOOR CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND HINGE FLANGE CRACKED AT RIGHT WING DOOR, FORWARD LOCATION. REMOVED AND REPLACED HINGE HALF ON RIGHT MAIN LANDING GEAR WING DOOR. (M) 2L73 4F A3WE 20030716000192003071600019NM 2003 7 16 2003F00412 120030314A5320 FLOOR SUPPORT BOEING727 727222 1384073NM FUSELAGE DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 9. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLER AND FILLER AT AFT CARGO FLOOR SUPPORT RBL 9 STATION 950F. (M) 2L73 4F A3WE 20030716000322003071600032NM 2003 7 16 USAABB03089 120030612A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2L72 4F RTA2NM 20030716000502003071600050SO 2003 7 16 SIMA200316003 120030524A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21810AE 145525 ABI - DURING AN MBV, THE CENTER FLOORBEAM LOEWR FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAME 24 AND 25. BLENDED THE DAMGED AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA WITH NO DEFECTS NOTED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW EMB STATEMENT IC2003-145/1766, EMB SRM 145/1142 REV 21, 53-21-10 PARA 9, FIG 208 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030716000582003071600058WP 2003 7 16 GTIA030465 120030504A5730 PANEL DOUG DC9 DC982 3022082WP RT WING CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND RIGHT WING LEADING EDGE PANEL 1248C CORROSION AT FASTENER HOLES AND NUMEROUS GOUGES. MATERIAL OUT OF LIMITS. RECEIVED NEW R/W L/E PANEL. (M) 2L72 4F A6WE 20030716000652003071600065NM 2003 7 16 2003F00422 120030313A5320 STRINGER CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720E, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720E, STRINGER 5L. (M) 2L73 4F A3WE 20030716000692003071600069 2003 7 16 USAASA03069 420030623A2565 SLIDE AIRBUSA319 A319112 3930323EU CABIN MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19725UW 1135 NO EMERGENCY LIGHTS DID NOT ILLUMINATE ON THE AFT RIGHT SLIDE WHEN THE SLIDE WAS DEPLOYED FOR AN OPERATIONAL CHECK. MAINTENANCE REPLACED THE ESCAPE SLIDE. OPERATIONALLY CHECKED EMERGENCY LIGHTS SYSTEM. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030716000712003071600071SO 2003 7 16 SIMA200311301 120030421A27503631001007 CONTROL UNIT EMB 135 EMB135KL 3260302SO TE FLAPS INOPERATIVE A SIMAO OTHER O OTHER DEDESCENT 1 SW21847AE 145707 AMA - FLT 3733 - DURING DESCENT, CREW REPORTED A FLAP FAIL MESSAGE ON EICAS WHEN FLAPS WERE SELECTED TO NINE DEGREES. FLAP INDICATOR SHOWED A YELLOW DASH AND ZERO FLAP MOVEMENT WAS CONFIRMED. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT AND THE FLAP DRIVE MOTOR (P/N 3632501003 S/N 01867) IAW EMB MM. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030710001322003071000132EU 2003 7 10 MALA030306 120030603A5310 STRUCTURE SAAB SF340 340B 7860101EU LYC LF507 LF5071F NE FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4K INSPECTION IN CWA, LT FUSELAGE HAS DENTS UNDER ICE SHIELD AT STA 341 ABOVE FUSELAGE REINFORCEMENT. MAINTENANCE COMPLETED TRIPLER/DOUBLER REPAIR IAW EO 53009. REF 409 NR 179480 FOR DETAIL. A/C RELEASE DATE 6/6/03. 2L72 4T4 FRTA52EU E6NE 20030711000102003071100010EA 2003 7 11 JBXA03011 120030617A3620 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA BLEED AIR DUCT FALSE INDICATIONA JBXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO05592ML 7410 LEFT 14TH STAGE DUCT MSG AT CLIMB PWR RETARDED LEFT PWR LEVER LEVELED OFF AT 25,000. FOLLOWED QRH PROCEDURE LANDED AT DCA. DUCT MSG DISAPPEARED WITHIN FEW SECONDS OF PULLING LEFT PWR LEVER TO RETARD, IT DID NOT RE-ILLUMINATE FOR THE REMAINDER OF THE FLIGHT. PERFORMED OPERATIONAL CHECK OF 14TH STAGE BLEED AIR SYSTEM AND GROUND LEAK TEST OF 14TH STAGE BLEED SYSTEM IAW CRJ AMM 36-12-00 AND 36-21-00, ALL CHECKS GOOD. 2L72 4F RTA21EA 20030714000162003071400016 2003 7 14 SWAA031419 420030626A2565 INDICATOR BOEING737 7373Q8 1384670NM SLIDE BOTTLE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 1900 24068 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030714000252003071400025NM 2003 7 14 SWAA031397 120030623A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 SEVERAL EEPLS COVERS MISSING IN CABIN. INSTALLED COVERS PER MM. 2L72 4F RTA16WE 20030714000722003071400072 2003 7 14 SWAA031387 420030621A25656567380 CONTAINER BOEING737 7373H4 1384600NM ESCAPE SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED CONTAINER PER MM. 2L72 4F RTA16WE 20030714001232003071400123NM 2003 7 14 DHL2003742010 120030630A33505708458505 LIGHT BOEING727 727225 1384077NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01742DH 21290 MAIN ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND OPS CHECKED OK IAW B727 M/M 33-50-71. 2L73 4F A3WE 20030714001252003071400125WP 2003 7 14 DHL2003802010 120030628A2611327 LAMP DOUG DC8 DC873 302199CWP SMOKE DETECTOR BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01802DH 46076 NR 5 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 5 SMOKE DETECTOR. OPS NORMAL PER M/M 26-10-0. 2L74 4F RT4A25 20030714001722003071400172 2003 7 14 BAQA087943 420030507A3160L316M30C1003 DISPLAY UROCOPEC135 EC135P1 8680990EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME300 0009 TOT READING IS 2000 DEGREES CELSIUS WHEN ENGINE IS RUNNING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030716000442003071600044NM 2003 7 16 TSAA0333114 120030510A33506013211 BATTERY PACK BOEING737 7372S2C 138448GNM PAX CABIN INOPERATIVE A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13806AL 21927 REPLACED AFT EXTERIOR EMERGENCY LIGHT BATTERY PACK DUE TO FAILING TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030716000542003071600054WP 2003 7 16 GTIA030461 120030513A5280 STRUCTURE DOUG DC9 DC981 3022081WP NLG DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND RIGHT FORWARD NOSE GEAR DOOR, EXCESSIVE PLAY IN AFT HINGE. UPON FURTHER INSPECTION, FOUND STIFFENER JUST OUTBOARD OF AFT HALF HINGE FOR RT NLG FORWARD DOOR TO BE CRACKED. FABRICATED NEW STIFFENER. INSTALLED NEW AFT HALF HINGE AND NEW OUTBOARD STIFFENER. (M) 2L72 4F A6WE 20030717000622003071700062SW 2003 7 17 HEEA088055 120030704A2913206076030101 PUMP BELL 206 206L3 1182108SW HYD SYSTEM NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03129MR 51129 HYD PUMP PRODUCING A HIGH PITCH SQUEAL. SHOP REPAIR. 1G71 3U H2SW 20030717000872003071700087SW 2003 7 17 HEEA088079 120030710A2820214066226103 CHECK VALVE BELL 214 214ST 1182106SW FUEL SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAUSING TRANSFER LIGHT TO STAY ON. 2G72 4U H10SW 20030717000912003071700091EU 2003 7 17 HEEA088033 120030629A2822D107318D1 PUMP BOLKMS105 BO105S 5626006EU FUEL SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 WP053071K S859 FUEL PUMP PRODUCES ZERO PRESSURE AND POPS CIRCUIT BREAKER. TO BE SENT TO VENDOR. 1G72 3U H3EU 20030717000962003071700096NM 2003 7 17 TSAA0333116 120030508A33508100037901 LIGHT BOEING737 73776N 13844CHNM CABIN INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13740AL 28640 REPLACED EMERGENCY OVERWING EXIT LIGHT DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030717001012003071700101EU 2003 7 17 USAASA03067 120030619A3397 CONNECTOR AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19187US 1704 THE AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. FAILURE MESSAGE, 'EPSU INT LOAD EXIT R', WAS PRESENT. MAINTENANCE DISCONNECTED THE MID CABIN, RIGHT SIDE, EMERGENCY POWER SUPPLY UNIT CONNECTOR, THEN RECONNECTED. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030718000042003071800004NM 2003 7 18 TSAA0333127 120030529A33508610066 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHTSINOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13823AL 23154 REPLACED RIGHT OVERWING EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030718000062003071800006NM 2003 7 18 TSAA0351124 120030505A53206545774 STRINGER CLIP BOEING737 73725A 1384481NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 CLIP DISCOVERED CRACKED OR TORN ON STRINGER 2R LOCATED AT BS 380. REMOVED DAMAGED CLIP. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS. REPAIR COMPLETED IAW SRM 51-30-2, FIGURE 1. (M) 2L72 4F RTA16WE 20030718000282003071800028NM 2003 7 18 USAASB03078 120030612A3397 WIRE BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19785AU 25024 MAINTENANCE REPORTED THE AISLE MARKER EMERGENCY LGIHT AT SEAT 19 A INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE SEAT CONNECTOR. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030718000322003071800032WP 2003 7 18 GTIA030479 120030514A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 LT CUSP CORRODED STA 200-229. PRIOR TO STEP 7, FOUND CORRODED WEB TO BE BEYOND ECONOMICAL REPAIR. REMOVED L1 DOOR WEB STATION 200-208. CORRODED ON CUSP WAS FOUND TO BE OUT OF LIMITS. FABRICATED CUSP, WEB WAS FOUND TO BE OUT OF LIMITS. REMOVED CORROSION ON WEB STATION 218-236 LBL 44 TO LBL 54. WEB WAS FOUND TO BE OUT OF LIMITS. FABRICATED WEBS STATION 218-236 AND 200-218. REMOVED COROSION ON L1 DOOR WEB. INSTALLED NEW SECTION OF CUSP STATION 180 TO 230. INSTALLED L1 DOOR WEB STATION 200-208. INSTALLED WEB STATION 200-218. INSTALLED WEB STATION 218-236. (M) 2L72 4F A6WE 20030718000352003071800035NM 2003 7 18 USAABB03104 120030625A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 FOUND R3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030718000432003071800043WP 2003 7 18 AMTA200300746 120030322A5250 DOOR LKHEED1011 10113853 5265020WP COCKPIT DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 RT AND LT FLIGHT DECK DOOR PARTITIONS DAMAGED. REPLACED PARTITIONS IAW ER/A L10-53F-5117 AND EO L10-52CS-27 18B. (M) 2L73 4F A23WE 20030718000732003071800073EA 2003 7 18 CA030612009 120030610A2761270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE SPOILERON FAILED W O OTHER J WARNING INDICATION CRCRUISE 1 CA (CAN) NOTICED AN UNCOMMANDED MOMENTARY ROLL IN CRUISE. THIS WAS FOLLOWED BY A SPOILERON FAULT STATUS MSG, WHICH REMAINED ON. LANDING PERFORMED UNEVENTFULLY. MAINTENANCE FOUND RIGHT SPOILERON INBOARD PCU FAILED. FOLLOWING THE PCU REPLACEMENT, THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030716000772003071600077WP 2003 7 16 GTIA030469 120030506A5320 PAN DOUG DC9 DC982 3022082WP FWD CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND FORWARD CARGO LOWER DOOR JAMB BEAM CORRODED. REMOVED FORWARD CARGO DOOR JAMB PAN. REPLACED FORWARD CARGO DOOR JAMB PAN. LOCATE AND DRILLED FORWARD CARGO DOOR JAMB PAN. FABRICATED SPLICE REPAIR. INSTALLED SPLICE REPAIR ON STAITON 370 PLUS STATION 427. (M) 2L72 4F A6WE 20030716000872003071600087 2003 7 16 USAASA03052 420030524A2565 SLIDE AIRBUSA319 A319112 3930323EU LEFT MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW 1019 THE LT FORWARD ENTRY DOOR SLIDE WILL NOT ARM. THE ARMING LEVER SPRINGS BACKUP AFTER ARMING. MAINTENANCE REMOVED, INSPECTED, THEN INSTALLED THE SAME SLIDE BACK ONTO THE LEFT FORWARD ENTRY DOOR. NO DEFECTS WERE NOTED. THE GIRT BAR AREA AT DOOR FRAME CORNERS WERE CLEANED. THE ARMING HANDLE WAS OPERATIONALLY CHECKED. ALL CHECKS WERE OK. (M) 2L72 4F RTA28NM 20030717000892003071700089EU 2003 7 17 I05R087964 120030601A6420350A33318000 TORSION BAR SNIAS 350 AS350* EU TAIL ROTOR WORN B I05RO OTHER O OTHER NRNOT REPORTED 1 WP0526LB 485 3514 PREMATURE WEAR OF LAMINATED TORSION BARS. REPLACED LAMINATED TORSION BARS. 1G71 3U H9EU 20030717000942003071700094EU 2003 7 17 BAQA087888 120030627A74109550176020 GENERATOR AEROSPSA365 SA365N 8680669EU HIGH ENERGY INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911UF3051 6338 HIGH ENERGY GENERATOR PRODUCING INTERMITTENT SPARK. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030107000782003010700078NM 2003 1 7 CALA0300002 120030103A5320 STIFFENER BOEING737 7373T0 1384582NM STA 500-500A CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0976355 23593 INSPECTION FOUND A 1" CRACK IN FORWARD CARGO COMPARTMENT STIFFENER AT STA 500-500A, LBL 3. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030107000802003010700080NM 2003 1 7 CALA0300004 120030106A5414 SKIN BOEING737 7373T0 1384582NM L/H PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0976355 23593 INSPECTION FOUND A 2" CRACK IN L/H ENGINE PYLON SKIN AT PANEL #5727L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV. B. 2L72 4F RTA16WE 20030116001822003011600182SO 2003 1 16 C2XA03BT003 120030104A3260852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO LT MLG FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2715926 145005 CREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS ON TAKEOFF FROM NEWARK. AIRCRAFT AIR RETURNED TO EWR, LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR PROXIMITY SWITCH IAW EMB145 MM 32-63-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030108000372003010800037NM 2003 1 8 QXEA0300012 120030107A33506038443 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09364PH 524 BOI- TWO OVERHEAD EMERGENCY LIGHTS AND ONE LEFT HAND OUTSIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PS3 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030108000482003010800048EA 2003 1 8 COMA0360007 120030104A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01484CA498 7702 FLIGHT 5343 FLAPS FAIL MESSAGE DURING TAXI OPS.REPLACED THE PDU 2L72 4F RTA21EA 20030109000712003010900071NM 2003 1 9 MWEA030021 120030108A5310993053875 DOUBLER DOUG MD88 MD88 3023688NM STA 389-408 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RIGHT CUSP MEMBRANE HAS CORROSION BETWEEN STATION 389 TO 408. -- REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030109000762003010900076SO 2003 1 9 C2XA03BT004 120030108A323023092300505 ACTUATOR EMB 145 EMB145ER 3260211SO FAULTY A C2XAO OTHER S AFFECT SYSTEMS UKUNKNOWN 1 SW2715926 145005 EWR---CO3628, CREW REPORTED, "LEFTHAND MAIN GEAR WOULD NOT RETRACT." MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED #1 MAIN LANDING GEAR UNLOCK ACTUATOR IAW #32-33-09 (REFERENCE M-602 #430342). OPS.CHECKED GOOD.. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030109000782003010900078NM 2003 1 9 159PL0025 120030106A3350 BATTERY BOEING737 737242 1384477NM A PIDAK NONE O OTHER UKUNKNOWN 1 SO05159PL 21186 Fwd entry door, L1 emergency pack light inop. Replaced batteries per MM 33-50-00. Test OK 2L72 4F A16WE 20030109001212003010900121EA 2003 1 9 QXEA0300013 220030106A7200312162701 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 MALFUNCTIONED A QXEAE ENGINE SHUTDOWN X ENGINE FLAMEOUT TOTAKEOFF 1 NM09402QX3690 4032 PCEFA0011 SEA - FLIGHT #2311, #2 ENGINE FAILED AT ROTATION WITH SUBSEQUENT AUTO FEATHER. CAPTAIN HEARD TWO LOUD BANGS LIKE A COMPRESSOR STALL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED #2 ENGINE. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE SENT TO PRATT & WHITNEY FOR ROOT CAUSE OF FAILURE. 2H72 4T4 TRTA13NM E00062EN 20030109001282003010900128EA 2003 1 9 SWIA200311679 120030101A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A SWIAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07447SW 7677 FLAPS FAIL CAUTION ON APPROACH. ONLY 20 DEGREES FLAPS WAS OBTAINED. WENT AROUND AND DID QRH. LANDED WITH FLAPS AT 20 DEGREES. RIGGED FLAPS PER MM 27-51-00. REMOVED AND REPLACED LEFT BPSU IAW CRJ MM 27-51-10. CYCLED MULTIPLE TIMES, NO FURTHER FAILURES. OPS CHECK GOOD. 2L72 4F RTA21EA 20030110000402003011000040EA 2003 1 10 03003661 120030103A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27661BR 7520 DURING PREFLIGHT INSPECTION EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. AIRCRAFT WAS FERRIED AND MAINTENANCE PERSONNEL REMOVED AND REPLACED NR 2 INVERTER, AN OPERATIONAL CHECK WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030110000422003011000042EA 2003 1 10 03005668 120030105A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27668BR 7544 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT OVERWING EXIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030327000872003032700087GL 2003 3 27 C2XA03BT007 220030108A729723062387 HARNESS EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 1 ENGINE SHORTED A C2XAO OTHER XF ENGINE FLAMEOUT FLT CONT AFFECTED APAPPROACH 1 SW2717928 145007 CAE311181 CREW REPORTED NR 1 ENGINE UNCOMMANDED SHUTDOWN ON APPROACH TO SYR, CONTINUED INTO SYR, LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED NR 1B FADEC ENGINE HARNESS IAW RR AE3007 MM #71-00-00 AND REMOVED AND REPLACED FADEC NR 1B DUE TO SHORT IN HARNESS AND DAMAGE TO FADEC #1B IAW EMB145 MM #73-22-01. OPERATIONAL CHECKED ENGINE AND AIRCRAFT GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CLOSED. 2L72 4F4 FRTT00011ATTE6CH 20030717000122003071700012 2003 7 17 HEEA087989 420030625A3442MI585202 PEDESTAL BELL 412 412 1182202SW RADAR ANTENNA MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 RADAR FLASHES ANTENNA. SHOP REPAIR. 1G72 4U H4SW 20030717000372003071700037SW 2003 7 17 HEEA088012 120030623A5610407030645116 WINDOW BELL 407 407 1182206SW PAX DOOR CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 PAX DOOR WINDOW IS CRAZED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000392003071700039SW 2003 7 17 HEEA088014 120030620A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 ENGINE BIPOD MOUNT HAS WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000442003071700044SW 2003 7 17 HEEA088019 120030619A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 TAIL ROTOR DISC PACK CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000582003071700058 2003 7 17 HEEA088051 420030704A3422060001500 GYRO BELL 206 206L3 1182108SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 GYRO HAS INTERMITTENT OPERATION. 1G71 3U H2SW 20030717000642003071700064SW 2003 7 17 HEEA088057 120030703A3210206513219 GAS CYLINDER BELL 206 206L3 1182108SW MLG BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MLG GAS CYLINDER BROKEN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030717000652003071700065SW 2003 7 17 HEEA088058 120030703A6210212015501115 BLADE BELL 212 212 1181420SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03278053210 31106 MAIN ROTOR BLADE SKIN SEPERATION OUTBOARD END LOWER SURFACE FROM TIP INBOARD APPROXIMATELY 2.25 INCHES AND AFT FROM LEADING EDGE APPROXIMATELY 2 INCHES. REPLACED WITH SERVICEABLE PART. 1G71 4U H4SW 20030717000672003071700067SW 2003 7 17 HEEA088060 120030701A8011214060056109 STARTER BELL 214 214ST 1182106SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 STARTER KICKS OFF DURING START. 2G72 4U H10SW 20030717000692003071700069SW 2003 7 17 HEEA088061 120030702A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 STARTER WILL NOT MOTOR. 1G72 4U H4SW 20030717000882003071700088SW 2003 7 17 HEEA088080 120030711A5610407030115125 WINDSHIELD BELL 407 407 1182206SW COCKPIT MISMARKED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 WRONG IDENTIFICATION ON WINDOW -- R/H; IT IS L/H. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 3U O H2SW 20030718000012003071800001 2003 7 18 USAASA03064 420030615A256561639103 BOTTLE AIRBUSA321 A321211 3930370EU ESCAPE SLIDE READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19170US7451 1462 A CABIN INTERCOMMUNICATION DATA SYSTEM RED LIGHT ILLUMINATED FOR THE MID RIGHT SERVICE DOOR ESCAPE SLIDE INFLATION RESERVOIR. MAINTENANCE REPLACED THE MID RIGHT SERVICE DOOR ESCAPE SLIDE INFLATION RESERVOIR. BITE CHECKED OK. (M) 2L72 4F RTA28NM 20040413000452004041300045NM 2004 4 13 ASAA0240157 120030319A532069165004 INTERCOSTAL BOEING737 7374Q8 138447QNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 727A-B, RBL 20 AND WL 156. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030108000022003010800002NM 2003 1 8 PCAA0301009 120030107A33506104789 BATTERY PACK DHAV DHC8 DHC8102 2809003NM POSITION 100 DISCHARGED A PCAAK NONE L NO TEST NRNOT REPORTED 1 EA13804EX 227 LGA- FLIGHT#3806. CREW REPORTED ROW 4 OVERHEAD EMERGENCY EXIT SIGN NOT ILLUMINATING. MAINTENANCE REPLACED 3 EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030108000042003010800004SO 2003 1 8 C2XA02SH174 120030108A530014520551001 SKIN EMB 145 EMB145LR 3260212SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV DURING C CHECK FUSELAGE SKIN WAS FOUND GOUGED JUST AFT OF LOWER AFT CORNER OF SERVICE DOOR CUT OUT. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01209. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030108000112003010800011WP 2003 1 8 MWEA030004 120030107A52805930583276 DOUBLER DOUG DC9 DC981 3022081WP RH MLG CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 RIGHT MAIN LANDING GEAR DOOR HAS MODERATE CORROSION ALONG AFT EDGE. -- BLENDED OUT CORROSION DRILLED REMAINING HOLES IN REPAIR DOUBLERS AND INSTALLED FASTENERS. 2L72 4F A6WE 20030108000142003010800014WP 2003 1 8 MWEA030007 120030107A5280593058378 INTERCOSTAL DOUG DC9 DC981 3022081WP STA Y962 Y970 TOOL DAMAGE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 RIGHT MAIN LANDING GEAR INTERCOSTAL BETWEEN STATION Y962.717 & Y970.343 AT X34.651 HAS A DEEP TOOL MARK. -- FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F A6WE 20030110000612003011000061NM 2003 1 10 QXEA0300017 120030104A36208209082 SWITCH BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAK NONE J WARNING INDICATION CRCRUISE 1 NM09403QX 4037 SEA-ON FLIGHT NUMBER 2361, #2 BLEED HOT CAUTION LIGHT ILLUMINATED INFLIGHT. CAUTION LIGHT EXTINGUSHED ABOUT 5 MINS AFTER EMERGENCY/ABNORMAL CHECK LIST COMPLETED. BLEED TURNED OFF. INTERROGATED CDS, FOUND FAULT CODES 7001 & 7005 FOR RIGHT HAND SIDE. REMOVED AND REPLACED BLEED OVERTEMP SWITCH. GROUND RAN ENGINES, CYCLED BLEED AIR ON. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030110000692003011000069NE 2003 1 10 0301091 320030109A6140IPTE1191000200 TRANSMITTER SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE ROTOL R389 R3894123F26 NE LH PGB SATURATED A UHLAK NONE J WARNING INDICATION CRCRUISE 1 NE03148SD UDAG0487 340A148 132 DRG189389 During Flight 4501 from PIT to LEX L ENG oil press light illum in flight + L prop PSI fluctuating between 0-100 psi. Removed + cleaned canon plug on oil pressure transmitter IAW SAAB AMM 73-00-00 ops check good. 2L72 4T4 TRTA52EU E8NE 6 CP30NE 20030113000402003011300040EU 2003 1 13 03013312 120030113A801123095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU A VTZAF ACTIVATE FIRE EXT. O OTHER TXTAXI/GRND HDL 1 EA27312UE 41025 During taxi, the crew reported a L/H engine fire. The crew shut down the L/H engine and activated the engine fire extinguisher. The aircraft returned to the gate without further incident. Maintenance personnel removed and replaced the L/H engine starter-generator. An operational check was satisfactory and the aircraft was returned to service. 2L72 4T RTA41NM 20030113000452003011300045CE 2003 1 13 GLBA2003003 120030111A560010138402524 WINDSHIELD BEECH 1900 1900D 1154162CE A GLBAD RETURN TO BLOCK O OTHER CLCLIMB 1 NM03201GL999 UE201 FO'S WINDOW CRACKED, R&R FO'S WINDSHIELD 2L72 4T RTA24CE 20030113000882003011300088WP 2003 1 13 DHL2003807002 120030110A2130 DOOR SEAL DOUG DC8 DC873F 302199FWP A DHLAO OTHER O OTHER CRCRUISE 1 SO01807DH 45990 1) IN CRUISE AT FL370 A SUDDEN POP AND THE SOUND OF RUSHING AIR WAS HEARD. THE CABIN BEGAN A SLOW CLIMB OF 100 FPM. WE DESCENDED TO FL290 AND THE CABIN PRESSURE STABILIZED AND THE SOUND OF LEAKING AIR STOPPED.2) FOUND SECTION OF LINE FWD CARGO DOOR SEAL NOT SECURE. REINSTALLED SEAL IN RETAINER IAW 52-36-8. PERFORMED PRESSURIZATION CHECK IAW 21-30-0. OPS CHECKED GOOD. 2L74 4F RT4A25 20030113000902003011300090WP 2003 1 13 ZW0A0300501 120030112A33507732 LAMP DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13964TW 53614 THE CABIN EGRESS LIGHTING WAS INOPERATIVE FROM ROW 26 TO 31. REPLACED LAMP AND SECURED LIGHTS. CHECK-C 5-25-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030113000912003011300091NM 2003 1 13 ZW0A0300502 120030109A33501315 LAMP DOUG MD80 MD83 3023681NM A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951TW 53470 THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE ABOVE THE AFT FLIGHT ATTENDANT POSITION AND AT CABIN ROW 11. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 5-28-02 STL. --CLOSED-- 2L72 4F RT 20030324000262003032400026NM 2003 3 24 374PA0002 120030112A2560P4010021 BATTERY BOEING737 73736M 138443BNM FLASHLIGHT DISCHARGED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05374PA 28333 FWD FLIGHT ATTENDANT JUMPSEAT OUTBOARD EMERGENCY FLASHLIGHT LED WILL NOT FLASH. ITEM DEFERRED PER MEL 25-12, CONTROL NR 0112001. 1/15/2003. R & R BATTERY POWER UNIT AS REQUIRED. OPS CHECK NORMAL. CLEARED MEL 25-12, CONTROL NR 0112001 2L72 4F RTA16WE 20030113001432003011300143SO 2003 1 13 C2XA03CL009 120030113A3260852701 SWITCH EMB 145 EMB145ER 3260211SO NOSE GEAR CONTAMINATED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2717928 145007 CLE FLIGHT#2408 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF FOLLOWED BY ENGINE 1-2 REV. DISAGREE.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR AIR/GROUND PROXIMITY SWITCH.THE NOSE STRUT WAS ALSO SERVICED TO PROPER LIMITS.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030114000272003011400027NM 2003 1 14 VNAA0301001 120030101A240020040 ALTERNATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LH FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07439JS190653602 3057 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND ALTERNATOR FAIL INDICATION AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND ALTERNATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030102000312003010200031NM 2003 1 2 CALA0300001 120030101A5330 SKIN BOEING737 7373T0 1384582NM BS 727E CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND A 1.5" CRACK IN R/H FUSELAGE SKIN AFT OF TRAILING EDGE OF FLAP, BS 727E, S18R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01 AND ECRA 5330-03191. 2L72 4F RTA16WE 20030103000602003010300060SO 2003 1 3 C2XA03BT001 120030102A3350 LAMP EMB 145 EMB145 3260210SO CABIN FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2714972 145151 EWR---CO3453, CREW REPORTED ON POSTFLIGHT CHECK, EMERGENCY LIGHT NEAR EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB IAW EMB145 MM 33-50-00. OPS.CHECKED SYSTEM GOOD. 2L72 4F RTT00011AT 20030103000632003010300063NM 2003 1 3 AWXA200300006 120030103A3250271N61191 HOSE BOEING757 7572S7 1384962NM ZONE 700 - LANDIRUPTURED A AWXAO OTHER GSKMULTIPLE FAILURE AFFECT SYSTEMS FLUID LOSS TXTAXI/GRND HDL 1 WP28902AW0 0 23322 PHX - NOSE WHEEL STEERING FAILURE - FLT 0716 - AFTER NORMAL LANDING AT PHX EN ROUTE FROM LAS NOSE WHEEL STEERING FAILED ON TAXIWAY, AND L/H HYDRAULIC QUANTITY DECREASED TO ZERO WITH SYSTEM PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE FOR L/H HYDRAULIC SYSTEM DISPLAYED. AIRCRAFT REQUIRED TOW TO GATE. MAINTENANCE FOUND L/H LANDING GEAR DOWN LOCK ACTUATOR FLEX LINE RUPTURED. REMOVED AND REPLACED L/H LANDING GEAR DOWN LOCK ACTUATOR FLEX LINE; LEAK CHECK COMPLIED WITH IAW BMM 32-32-02, PG. 407, STEP 11 & 12. 2L72 4F RTA2NM 20030103000702003010300070NE 2003 1 3 RAIA00301005 220030102A7200PW120 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE FAILED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03423TE125976254 119 121372 5639-STL- FLIGHT ATTENDANT REPORTED SPARKS COMING FROM LEFT ENGINE TAIL PIPE. ALL ENGINE PARAMETERS WERE OK. MAINTENANCE INVESTIGATED, FOUND INTERNAL ENGINE FAILURE, AND REMOVED AND REPLACED THE LEFT ENGINE, OPS AND LK CK OK. 2H72 4T4 TRTA53EU E20NE 20030106001432003010600143GL 2003 1 6 BAQA082774 220030103A73210164248860 FUEL CONTROL AEROSPAS365 AS365N2 8680815EU ALLSN 250C 250C* GL ENGINE FAILED H BAQAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 FS01915ME1470 6417 ENGINE "FLAMES OUT" AT FLIGHT IDLE WHEN BOOST PUMPS ARE TURNED OFF. REMOVED FROM ENGINE NR 12046. REPLACED FUEL CONTROL WITH SERVICEABLE UNIT. 1G72 3U3 URTH10EU E4CE 20030108000322003010800032WP 2003 1 8 MWEA030014 120030107A531399196513 SKIN DOUG DC9 DC981 3022081WP STA 237 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 FORMERS AT STATION 237 BETWEEN LONGERONS 5 AND 4 LEFT AND 9 AND 8 LEFT REQUIRES REMOVAL TO FACILITATE SKIN REPAIR. -- LOCATED AND DRILLED NEW FORMER, FABRICATED AND INSTALLED SPLICE PLATE. 2L72 4F A6WE 20030108000352003010800035EA 2003 1 8 COMA0360003 120030103A5610NP13932110 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA R/H BROKEN A COMAK NONE O OTHER UKUNKNOWN 1 SO01954CA2982 7100 FLIGHT 6029 COPILOTS WINDSHIELD SHATTERED.REPLACED WINDSHIELD 2L72 4F RTA21EA 20030207000722003020700072NE 2003 2 7 NACA20030066 220030104A7421URHB32E SPARK PLUG PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 11 CYLINDER CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL031377K 355 575575 44596 NK510186 NR 3 ENGINE SHUT DOWN FOR NR 11 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED FRONT AND REAR SPARK PLUGS. 2L74 4R4 R A781 5E8 20030108000652003010800065WP 2003 1 8 ARWA20030101 120030102A57405615057503 SPAR CAP DOUG DC8 DC863F 302198FWP A ARWAO OTHER O OTHER ININSP/MAINT 1 SO19441J 74553 45688 LOG PAGE # 503179. DISCREPANCY: DURING 1A CHECK THE FOLLOWING WAS FOUND; ITEM # 128M: L/H WING AUXILIARY SPAR INBD. UPPER LOG WITH CRACK. GENERATED BY J/C # 51-020-04-06-1. CORRECTIVE ACTION: ACCOMPLISHED TEMPORARY REPAIR IN ACCORDANCE WITH BOEING MESSAGE INW-LIM-03-00004H, DATED 01/03/02. APPROVAL FOR THE REPAIR WAS GRANTED ON 8110-3. REPETITIVE INSPECTION UNTIL REPLACEMENT IS PART OF THE APPROVAL. 2L74 4F 4A25 20030109000692003010900069NM 2003 1 9 MWEA030017 120030108A5310993061221 DOUBLER DOUG MD88 MD88 3023688NM STA 1155-1174 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CUSP MEMBRANE CORRODED RIGHT SIDE STATION 1155-1174. -- FABRICATED AND INSTALLED NEW DOUBLER AND NEW FILLERS. 2L72 4F RTA6WE 20030110000012003011000001SO 2003 1 10 C2XA03BT006 120030109A5300 SKIN EMB 145 EMB145LR 3260212SO DENTED A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2714998 145302 BTV---CO2002, DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND FUSELAGE DAMAGED ON LEFTHAND SIDE AT FRAME #22. MAINTENANCE REMOVED DAMAGED CLIP AT FRAME #22 AND ATTACHING FLOOR CROSS MEMBER, PERFORMED SKIN REPAIR IAW EMB145 SRM #53-21-00, FABRICATED SKIN CLIP IAW EMB LETTER IC2003-145/0103-B, REINSTALLED FABRICATED SKIN CLIP AND FLOOR CROSS MEMBER, AND PRESSURIZATION CHECKED/OPS.CHECKED AIRCRAFT GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030110000382003011000038NM 2003 1 10 03003404 120030103A3350 POWER SUPPLY DORNERDO32 DO328300 NM CABIN MALFUNCTIONED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27404FJ 3150 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT EMERGENCY BATTERIES WERE INOPERATIVE. MAINTENANCE PERSONNEL INSPECTED EMERGENCY POWER SUPPLY AND PERFORMED OPERATIONAL CHECK, OPS CHECK WAS GOOD AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T RTA55NM 20030110000452003011000045WP 2003 1 10 CALA0300006 120030109A5313 LONGERON DOUG DC9 DC982 3022082WP STA 1415 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0935832 49492 INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT AFT SIDE OF BELTFRAME, STA 1415. A LONGERON SPLICE WAS INSTALLED IAW SRM 53-02. 2L72 4F A6WE 20030113000862003011300086NM 2003 1 13 UPS03440012 120030105A5730 PANEL BOEING747 747259B 1384804NM LH WLG BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C LH WLG BAY AREA MOST I/B SKIN PNL (TRIANGLE SHAPE) EDGE SHOCK STRUT DOOR CUTOUT EDGE SEAL RETAINER EDGE CORROSION FOUND AT 3 LOCATIONS. SEAL RETAINER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG.2. 2L74 4F RTA20WE 20030113001372003011300137EU 2003 1 13 03007309 120030107A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27309UE 41022 DURING MAINTENANCE INSPECTION, RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED RIGHT AFT EMERGENCY LIGHT, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T3 TRTA41NM E2WE 20030113001422003011300142SO 2003 1 13 C2XA03CL010 120030110A3620M1195175242 SWITCH EMB 145 EMB145LR 3260212SO AFT WING TO FUSEDEFECTIVE A C2XAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW2716919 145393 CLE FLIGHT#2316 THE CREW REPORTED AFTER TAKEOFF A BLEED LEAK INDICATION OCCURED.THE CREW TURNED OFF THE #2ENGINE BLEED AND THE MESSAGE CLEARED.SHORTLY AFTER THE MESSAGE RETURNED AND THE CREW SHUTDOWN THE #2 ENGINE.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE BLEED AIR THERMAL SWITCH SO220.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030114000312003011400031NM 2003 1 14 SWAA030045 120030108A2750AV13J5144 BYPASS VALVE BOEING737 7373H4 1384600NM LT MLG W/W FAULTY A SWAAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 SW29311SW 23333 DIVERSION, T/E FLAPS WOULD NOT EXTEND. REMOVED AND REPLACED FLAP BYPASS VALVE PER MM. 2L72 4F RTA16WE 20030114000342003011400034NM 2003 1 14 SWAA030021 120030105A575465C26602 SLAT BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20030114000362003011400036NM 2003 1 14 SWAA030024 120030106A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED SERVICE CHECK, SWA SI 11075, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHING AT NR 1 HINGE ATTACH POINT PER MM. 2L72 4F RTA16WE 20030114000382003011400038NM 2003 1 14 SWAA030026 120030106A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 6, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030106001532003010600153NE 2003 1 6 HEEA082804 120030102A63217665009803103 POWERPACK SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 POWER CYCLES ON APPROX. EVERY 5 SECONDS, POWER PACK WILL NOT HOLD PRESSURE. 1G72 3U H1NE 20030106001552003010600155NE 2003 1 6 HEEA082806 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 ROTOR BRAKE MODULE WILL NOT PRESSURE UP. 1G72 3U H1NE 20030106001562003010600156NE 2003 1 6 HEEA082807 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 ROTOR BRAKE WON'T RELEASE. 1G72 3U H1NE 20030106001592003010600159NE 2003 1 6 HEEA082810 120030102A63217665009803103 POWERPACK SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROTOR BRAKE WILL NOT STOP CYCLING. 1G72 3U H1NE 20030106001602003010600160NE 2003 1 6 HEEA082811 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROTOR BRAKE CYCLING ON AND OFF WHEN IN THE ON POSITION. 1G72 3U H1NE 20030106001612003010600161NE 2003 1 6 HEEA082812 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROTOR BRAKE KEEPS MOTORING. 1G72 3U H1NE 20030106001672003010600167NE 2003 1 6 HEEA082818 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035426U 760167 ROTOR BRAKE CYCLES CONTINUOUSLY. 1G72 3U H1NE 20030123000772003012300077NM 2003 1 23 QXEA0300113 120030121A30804100S00501 VALVE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09404QX1881 1881 4046 GEG ON FLIGHT 2355- AFTER SELECTING AIRFRAME DEICE BOOT SELECTION TO FAST, RECIEVED DEICE PRESSURE MASTER CAUTION. RAN EMERGENCY CHECKLIST, NO ABNORMAL DEICE PRESSURE INDICATED ON EITHER SIDE. NO.5 GREEN LIGHT ON OVERHEAD DEICE PANEL ON FIRST OFFICERS SIDE STAYS ON AFTER IT SHOULD GO OUT. NO.6 GREEN LIGHT CAME ON AND NO.5 LIGHT ON FIRST OFFICERS SIDE STILL STAYS ON GOING TO SLOW OR MANUAL DOES NO GOOD. REMOVED AND REPLACED NO.5 DUAL DISTRIBUTION VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030124000042003012400004EU 2003 1 24 MALA030104 120030104A3242201298302 BRAKE BAC 146 AVRO146RJ85A1500097EU LT MLG FIRE A MALAO OTHER AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15522XJ E2347 WHILE PARKING AFTER FLIGHT, LT O/B BRAKE FAN APPEARS TO BE ON FIRE, MAKING SMOKE, FLAMES AND SPARKS. WHILE PARKING AT GATE LT O/B BRAKE FAN PRODUCING SPARKS AND FLAMES, STILL SMOKING 20 MIN AFTER. LEFT BRAKE TEMP 250 C MAX. MX REPLACED LT AXLE P/N 201298302, S/N ON 13808/01, LT I/B BRAKE P/N AHA2331-2, S/N ON VX102, S/N OFF WY099, LT I/B TIRE PH AHA1489 S/N ON VL065, S/N OFF VE006. LT O/B TIRE P/N 1489, S/N ON WU052, S/N OFF VU076. BRAKE FAN MOTOR P/N AHM9050, S/N ON 467138, ANTI-SKID TRANDUCER P/N ACM28076, S/N ON VC042 AND BRAKE FAN MOTOR HOUSING P/N AHM8109 IAW MAIN WHEEL TC 3240-502, BRAKE TC 3240-501, BRAKE FAN MOTOR AMM32-43-11-201 SKID TRANSDUCER AMM 32-41-44-201 AXLE AMM 32-10-31-401, OPS CK GOOD. 2H74 4F RTA49EU 20030124000082003012400008NM 2003 1 24 DHL2003742005 120030124A2611 LAMP BOEING727 727225 1384077NM A DHLAKO NONE OTHER L NO TEST NRNOT REPORTED 1 SO01742DH 21290 1) POSITION #2 SMOKE DETECTOR WILL NOT TEST.2) REMOVED AND REPLACED TEST LAMP ON SMOKE DETECTOR, OPS CHECKED GOOD IAW BMM 26-17-0. 2L73 4F A3WE 20030124001042003012400104NM 2003 1 24 AWXA200300072 120030104A53206550568 SUPPORT ANGLE BOEING737 7373G7 1384595NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW0 0 24712 LCQ - MAJOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON LOWER SURFACE NUT PLATES OF L-2 DOOR THRESHOLD SUPPORT ANGLE, BS 967 TO BS 969. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED L-2 DOOR THRESHOLD SUPPORT ANGLE; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11, PG. 3, FIG. 1. 2L72 4F RTA16WE 20030127000042003012700004 2003 1 27 HEEA083580 420030114A34424000038 CONTROL HEAD BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 WEATHER RADAR CONTROL HEAD WILL NOT HOLD POSITION. SHOP REPAIR. 1G72 4U H4SW 20030127000062003012700006 2003 1 27 HEEA083582 420030114A3421 LIGHT BELL 412 412 1182202SW ATTITUDE IND INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 4556 33076 ATTITUDE INDICATOR LIGHT INOPERATIVE. SHOP REPAIR. 1G72 4U H4SW 20030127000202003012700020 2003 1 27 HEEA083596 420030114A3442MI5851352 INDICATOR BELL 412 412 1182202SW RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 RADAR SYSTEM WON'T PAINT NOISE BAND. SHOP REPAIR. 1G72 4U H4SW 20030127000232003012700023 2003 1 27 HEEA083599 420030114A3442MI585200 RADAR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 "WAIT" COMES ON THEN SCREEN GOES BLANK. SHOP REPAIR. 1G72 4U H4SW 20030114000412003011400041NM 2003 1 14 SWAA030030 120030106A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT ANTENNA CUTOUT, BS 406 AND BS 446, BL 0. REPAIRED SKIN PER BOEING SERVICE BULLETIN. 2L72 4F RTA16WE 20030114000592003011400059NM 2003 1 14 SWAA030007 120030102A5520BACB28AK07 BUSHING BOEING737 7377H4 1384404NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29751SW 29803 DURING SCHEDULED A2 CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2 AND NR 3 HINGE ATTACH POINTS WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 3 HINGE ATTACH POINTS PER MM. 2L72 4F RTA16WE 20030114000602003011400060NM 2003 1 14 SWAA030010 120030105A33506545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 26L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030114000642003011400064NM 2003 1 14 SWAA030014 120030105A5751654645423 AILERON BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C2 CHECK, FOUND LT AILERON DELAMINATED ON LOWER SKIN BETWEEN NR 2 AND NR 3 HINGES. REMOVED AND REPLACED LT AILERON PER MM. 2L72 4F RTA16WE 20030114000672003011400067NM 2003 1 14 SWAA030017 120030105A80113502945 STARTER BOEING737 7377H4 1384404NM CFM56 CFM56* 13802NE NR 1 ENGINE LEAKING A SWAAEB ENGINE SHUTDOWN EMER. DESCENT JK WARNING INDICATION FLUID LOSS DEDESCENT 1 SW29420WN 29825 888304 IN-FLT SHUTDOWN, DECLARED EMERGENCY, DURING CRUISE NR 1 ENGINE OIL QUANTITY DROPPED TO 0, OIL PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE STARTER PER MM. 2L72 4F4 FRTA16WE E2GL 20030114001152003011400115 2003 1 14 SWAA030002 420030101A256522D22901151 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F A16WE 20030114001162003011400116NM 2003 1 14 SWAA030006 120030102A57536546430100 SKIN BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C2 CHECK, FOUND RT T/E INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED RT T/E INBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20030114001172003011400117NM 2003 1 14 SWAA030008 120030104A2560P2070001 BATTERY BOEING737 737317 138447PNM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29693SW 23174 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20030114001322003011400132NM 2003 1 14 SWAA030034 120030107A3350 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT CEILING LIGHT AT OVERWING EXIT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030114001422003011400142NM 2003 1 14 SWAA030046 120030102A7603315A1044 CONTROL QUADRANT BOEING737 7375H4 138449DNM GE CFM56 CFM56* 13802NE NR 1 ENGINE OBSTRUCTED A SWAAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 SW29515SW 25154 720727 IN-FLT SHUTDOWN, PRIOR TO DESCENT, NR 1 ENGINE THRUST LEVER WOULD NOT RETARD. FOUND DEBRIS INSIDE THROTTLE QUADRANT, REMOVED DEBRIS AND OPS CK GOOD PER MM. 2L72 4F4 FRTA16WE E2GL 20030114002102003011400210NM 2003 1 14 VNAA0301005 120030106A2840 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FUEL SYSTEM DIRTY A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07432JS 3045 EN ROUTE TO TYS, THE CREW RECEIVED A FUEL FEEDER TANK LOW CAS MESSAGE. THE CREW CALLED MAINTENANCE CONTROL AND THE DECISION WAS MADE TO DIVERT TO ROA. OUTSTATION MAINTENANCE THEN INSPECTED THE FUEL LEVEL WHICH CHECKED GOOD AND THEN CLEANED THE CONNECTORS ON THE REFUEL/DEFUEL PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030114002132003011400213 2003 1 14 VNAA0301007 420030107A3418 WARNING SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07472PS 3008 DURING TAKEOFF, THE CREW RECEIVED AN AOA CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGE EXTINGUISHED WHEN THE AIRCRAFT CLEARED THE RUNWAY. THE CREW CALLED MAINTENANCE CONTROL AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4058 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030114002492003011400249EA 2003 1 14 COMA0360017 120030110A2711 AILERON CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 SO01981CA 7163 FLIGHT 5360 AILERON CONFIG WARNING DURING T/O.ADJUSTED AILERON TRIM INTO T/O RANGE. 2L72 4F RTA21EA 20030114002532003011400253EA 2003 1 14 COMA0360021 120030111A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01983CA12999 7169 FLIGHT 5819 GEAR DISAGREE WARNING WHEN SELECTED DOWN.REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030114002562003011400256EA 2003 1 14 COMA0360024 120030112A3397 SPLICE CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01965CA 7131 FLIGHT 5748 ONE SEGMENT OF EMERGENCY FLOOR LIGHTING IS INOP. REPAIRED WIRE SPLICE AT ROW 8. 2L72 4F RTA21EA 20030127000272003012700027 2003 1 27 HEEA083603 420030114A3457N0002000 GPS BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 GPS TAKES 30 MINUTES TO OPERATE PROPERLY. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030127000382003012700038 2003 1 27 HEEA083615 420030114A2300100005430 HEADSET BELL 407 407 1182206SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 MIC ON HEADSET BROKEN. REPAIRED. 1G71 3U O H2SW 20030127000482003012700048SW 2003 1 27 HEEA083625 120030114A52103160202 HANDLE BELL 407 407 1182206SW CREW DOOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 CREW DOOR LEVER ON HANDLE WORN. TO BE SENT TO BELL FOR CREDIT. 1G71 3U O H2SW 20030127000532003012700053SW 2003 1 27 HEEA083631 120030114A243231908001 BATTERY BELL 407 407 1182206SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 BATTERY HAS NO VOLTAGE WHEN SWITCH IS TURNED ON. REPAIRED. 1G71 3U O H2SW 20030127000582003012700058 2003 1 27 HEEA083636 420030114A342150400179015 INDICATOR BELL 407 407 1182206SW ADI MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 ADI INDICATES 30 DEGREES BANK AFTER 5 MINUTES STRAIGHT AND LEVEL FLIGHT. REPAIRED. 1G71 3U O H2SW 20030127000592003012700059 2003 1 27 HEEA083637 420030114A342150400179015 INDICATOR BELL 407 407 1182206SW ADI PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 ADI PRECESSES IN FLIGHT. REPAIRED. 1G71 3U O H2SW 20030127000622003012700062 2003 1 27 HEEA083640 420030114A34225050031904 GYRO BELL 407 407 1182206SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 DIRECTIONAL GYRO DRIFTS (PRECESSES). REPAIRED. 1G71 3U O H2SW 20030127000632003012700063 2003 1 27 HEEA083641 420030114A34225050031904 GYRO BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 DIRECTIONAL GYRO HAS TO BE RESET SEVERAL TIMES. REPAIRED. 1G71 3U O H2SW 20030127000742003012700074SW 2003 1 27 HEEA083648 120030114A7910 B-NUT BELL 407 407 1182206SW HOSE ASSY CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 HOSE ASSY HAS CORROSION ON INSIDE OF B-NUT ON THREADS. 1G71 3U O H2SW 20030127000892003012700089NM 2003 1 27 SWAA030077 120030110A53206551268 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SPECIAL VISIT, FOUND BS 180 FLOOR WEB CRACKED AT RBL 24, WL 207. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20030127000902003012700090 2003 1 27 HEEA083655 420030114A344278806059008 DISPLAY BELL 407 407 1182206SW WX RADAR SYS ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 WEATHER RADAR INDICATOR ERRATIC DURING FLIGHT. 1G71 3U O H2SW 20030127000972003012700097EA 2003 1 27 COMA0360042 120030126A5320601350125152 ANGLE CNDAIRCL600 CL6002B19 1900309EA FS621.0 CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01967CA16116 7134 L/H AND R/H OBLIQUE ANGLES AT FS 621.0 STR 14 ARE CRACKED.PERFORMED A MAJOR REPAIR BY REPLACING CRACKED OBLIQUE ANGLES AT FS 621.0 STR 14 L/H AND R/H SIDE I/A/W CRJ SRM 51-42-21 AND WVAC EO 601R-53-3804. 2L72 4F RTA21EA 20030127001022003012700102EA 2003 1 27 COMA0360047 120030123A2620 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA 7241 FLIGHT 5292 CARGO FIRE BOTTLE LOW MESSAGE.COULD NOT DUPLICATE. INPSECTED BOTTLE AND WIRING - NO DEFECTS. 2L72 4F RTA21EA 20030127001042003012700104EA 2003 1 27 COMA0360050 120030123A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO01940CA 7048 FLIGHT 5173 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030127001052003012700105 2003 1 27 HEEA083659 420030114A344280510800001 CONTROL BOX BELL 407 407 1182206SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 WEATHER RADAR CONTROL BOX DATA FAILED MESSAGE. 1G71 3U O H2SW 20030127001282003012700128SW 2003 1 27 HEEA083672 120030115A3212206050247131 COVER BELL 407 407 1182206SW EMERGENCY FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 EMERGENCY FLOAT COVER HOOK AND LOOP WILL NOT HOLD ANYMORE. 1G71 3U O H2SW 20030127001372003012700137SW 2003 1 27 HEEA083678 120030115A3212206050247135 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20030127001442003012700144SW 2003 1 27 HEEA083682 120030115A3212206050247137 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20030127001522003012700152SW 2003 1 27 HEEA083686 120030115A3246206053184122 SKID BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 SKID TUBE CORRODED BEYOND LIMITS. 1G71 3U O H2SW 20030127001712003012700171SW 2003 1 27 HEEA083692 120030115A2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH533 98142 53283 STARTER GEN BRUSHES WORN. REPAIRED. 1G71 3U O H2SW 20030127001762003012700176SW 2003 1 27 HEEA083693 120030115A2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 99092 53188 STARTER GEN BRUSHES WORN. REPAIRED. 1G71 3U O H2SW 20030127002072003012700207SW 2003 1 27 HEEA083699 120030115A5310206064515103 SUPPORT BELL 407 407 1182206SW OIL TANK CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 FWD ENGINE OIL TANK SUPPORT CRACKED AT FWD RT MOUNT BOLT. 1G71 3U O H2SW 20030127002102003012700210SW 2003 1 27 HEEA083701 120030115A7160206064819005 DOOR BELL 407 407 1182206SW ENG COWL CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 ENGINE COWL DOOR CRACKED. 1G71 3U O H2SW 20030127002212003012700221SW 2003 1 27 HEEA083709 120030115A7160206064909101 INTAKE BELL 407 407 1182206SW BELLMOUTH CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 BELLMOUTH INTAKE HAS CORROSION. 1G71 3U O H2SW 20030127002282003012700228SW 2003 1 27 HEEA083714 120030115A2913206076030117FM PUMP BELL 407 407 1182206SW HYD SYSTEM NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 HYD PUMP MAKING NOISE INTERMITTENTLY. 1G71 3U O H2SW 20030127002292003012700229SW 2003 1 27 HEEA083715 120030115A2913 SHAFT BELL 407 407 1182206SW HYD PUMP SPLINESWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH K0070 53386 HYD PUMP HAS WORN SPLINES. 1G71 3U O H2SW 20030127002422003012700242SW 2003 1 27 HEEA083723 120030115A2810206362002103 CAP BELL 407 407 1182206SW FUEL STORAGE BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 FUEL STORAGE CAP TAB IS BROKEN OFF OF CAP. 1G71 3U O H2SW 20030127002472003012700247SW 2003 1 27 HEEA083726 120030115A3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 EMERGENCY FLOAT SOLENOID VALVE LEAKING. 1G71 3U O H2SW 20030127002482003012700248SW 2003 1 27 HEEA083727 120030115A5210206513211 ACTUATOR BELL 407 407 1182206SW PAX DOOR WEAK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 ONE NOT STRONG ENOUGH TO OPEN THE DOOR. THE OTHER ONE HAS ONE OF THE END CLIP HOLES WORN THROUGH THE METAL. SCRAPPED. 1G71 3U O H2SW 20030127002512003012700251WP 2003 1 27 MWEA030015 120030107A5320993053815 WEB DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 FLOOR WEB OUTBOARD OF NR 1 SEAT TRACK AT FRAME STATION 313 HAS AN OBLONG HOLE. LOCATED AND DRILLED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20030127002532003012700253NM 2003 1 27 MWEA030018 120030108A5320993061221 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CUSP MEMBRANE CORRODED RIGHT SIDE STATION 1193 AREA AND STATION 1212. BLENDED CORROSION FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F RTA6WE 20030127002562003012700256SW 2003 1 27 HEEA083731 120030115A3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03723PH 53283 EMERGENCY FLOAT PRESSURE GAUGE FACE PLATE TURNS INSIDE GAUGE, PRESSURE INDICATION NOT RELIABLE. 1G71 3U O H2SW 20030127002612003012700261SW 2003 1 27 HEEA083736 120030115A2821222366621103 FILTER BELL 407 407 1182206SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03408PH 53228 FILTER LIGHT OFFSHORE AND WOULD NOT TEST. 1G71 3U O H2SW 20030127002712003012700271GL 2003 1 27 HEEA083747 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH 53401 CAUSING HIGHER THAN NORMAL MGT READINGS. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030127002852003012700285NM 2003 1 27 03FDEA00026 120030115A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 BS 500, FRAME IS DENTED ABOVE STR 22L UPPER FLANGE. REMOVED DAMAGE AREA OF BS 500 FRAME AND FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW SRM. 2L73 4F RTA3WE 20030127002902003012700290NM 2003 1 27 03FDEA00030 120030115A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 FRAME, BS 1050 LBL 26 WL 155 HAS A DENT. DENT FOUND TO BE OUT OF LIMITS PER SRM. REPAIRED AREA IAW SRM, E.A. 2L73 4F RTA3WE 20030128000042003012800004GL 2003 1 28 ALGA084030 220030123A73202539688 COVER CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C* GL FUEL CONTROL DEFECTIVE H ALGAK NONE O OTHER ININSP/MAINT 1 FS01PARTO 326726 ON ASSEMBLY FOUND COVER LEAKING EXCESSIVE. REMOVED. 1Q71 3R3 U 2A6 E4CE 20030128000082003012800008EU 2003 1 28 BAQA084012 120030121A6321L635M1025229 BRAKE DISC UROCOPEC135 EC135T1 5620026EU MAIN ROTOR WARPED W O OTHER O OTHER NRNOT REPORTED 1 FS01522ME 0144 BRAKE DISC WARPED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030128000112003012800011GL 2003 1 28 HEEA083763 220030115A742123060816 LEAD BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE IGNITER DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 IGNITER LEAD DELAYED ENGINE STARTS. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000132003012800013GL 2003 1 28 HEEA083765 220030115A742123060816 LEAD BELL 407 407 1182206SW ALLSN 250C 250C* GL IGNITER DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH 53461 IGNITER LEAD DELAYED LIGHT OFFS. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000172003012800017GL 2003 1 28 HEEA083769 220030115A726023063370 SEAL BELL 407 407 1182206SW ALLSN 250C 250C* GL FORWARD PTO LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 ENGINE AND TRANSMISSION TRANSFERRING OIL. REPLACED FWD PTO SEAL WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000362003012800036SW 2003 1 28 HEEA083789 120030115A282123066697 FILTER BELL 407 407 1182206SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 FILTER BYPASS INDICATOR POPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128000392003012800039SW 2003 1 28 HEEA083792 120030115A282123066697 FILTER BELL 407 407 1182206SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 FILTER BYPASS INDICATOR POPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128000402003012800040SW 2003 1 28 HEEA083794 120030115A7120 BEARING BELL 407 407 1182206SW MOUNT SEPARATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 10679 53188 BEARING SEPARATED FROM ENGINE MOUNT. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128000412003012800041SW 2003 1 28 HEEA083795 120030115A7120 BEARING BELL 407 407 1182206SW REAR MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 12630 53159 REAR ENGINE MOUNT HAS A WORN SPHERICAL BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128000442003012800044EU 2003 1 28 0301181 120030118A61201103P2671 PRESSURE SWITCH SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE FROZEN A UHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 NE03158SD 158 flt# 4479 during takeoff did not get autocoursen arm light. Crew aborted take off and returned to gate. mechanic performed ground run. iaw 61-22-00-5. ops checked good. A/C returned to service without further incident 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030128000482003012800048GL 2003 1 28 HEEA083801 220030115A732023072725 HYDROMECH UNIT BELL 407 407 1182206SW ALLSN 250C 250C* GL FUEL CONTROL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03723PH 53283 FUEL FOUND DRIPPING OUT OF CONNECTOR PLUG RECEPTICLE. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000502003012800050 2003 1 28 HEEA083804 420030116A34424000023 TRANSCEIVER BELL 407 407 1182206SW WX RADAR SYS DAMAGED E O OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 FM SUDDENLY WOULD NOT TRANSMIT OR RECEIVE. FOUND BROKEN SOLDER JOINT ON POWER SUPPLY BOARD. REPAIRED. PROBLEM. BENCH CHECK GOOD. 1G71 3U O H2SW 20030128000512003012800051EU 2003 1 28 0301281 120030128A6120 LAMP SOCKET SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE UNSECURE A UHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 NE03152CQ 152 FLT # 4499. durning takeoff did not get autocoursen arm light. crew aborted take-off and returned to gate. found light assy loose in socket. pilot did not notice durning lights check. Mechanic resecured light assy and performed ground run. IAW 61-22-00-5. Ops checked good. A/C returned to service without further notice. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030128000572003012800057SW 2003 1 28 HEEA083811 120030116A6220406010117115 PLATE BELL 407 407 1182206SW ROTOR HEAD CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH2281 A347 53142 MAIN ROTOR HEAD LOWER PLATE HAS CORROSION BEYOND LIMITS. CORROSION ON LOWER PLATE NEAR STAINLESS STEEL LOCK PLATE ON RED ARM. 1G71 3U O H2SW 20030128000622003012800062SW 2003 1 28 HEEA083816 120030116A6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03408PH333 53228 MAIN ROTOR SWASHPLATE HAS GREASE LEAKING PAST UPPER SEAL INTO BOOT. REPAIRED. 1G71 3U O H2SW 20030128000632003012800063SW 2003 1 28 HEEA083817 120030116A6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03496PH 53398 MAIN ROTOR SWASHPLATE HAS GREASE IS LEAKING FROM UPPER SEAL. REPAIRED. 1G71 3U O H2SW 20030128000642003012800064SW 2003 1 28 HEEA083818 120030116A6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03724PH 53327 UNIBALL SATURATED WITH GREASE FROM MAIN ROTOR SWASHPLATE. REPAIRED. 1G71 3U O H2SW 20030128000672003012800067SW 2003 1 28 HEEA083821 120030116A6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03498PH 53399 MAIN ROTOR SWASHPLATE LEAKING GREASE FROM TOP SEAL. REPAIRED. 1G71 3U O H2SW 20030128000692003012800069SW 2003 1 28 HEEA083823 120030116A6230406010413117 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03719PH 53266 MAIN ROTOR PITCH LINK HAS CORROSION. 1G71 3U O H2SW 20030128000702003012800070SW 2003 1 28 HEEA083824 120030116A6300406010417101 BEARING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 MAIN ROTOR BEARING WORN. 1G71 3U O H2SW 20030128000792003012800079SW 2003 1 28 HEEA083833 120030116A6230406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH2493 53401 MAIN ROTOR LINK ASSY WORN. 1G71 3U O H2SW 20030128000842003012800084EA 2003 1 28 03026622 120030126A3260162253 BRACKET CNDAIRCL600 CL6002B19 1900309EA A VTZAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA27622BR NOSE GEAR DISAGREE LIGHT. R&R TARGET BRACKET P/N 16225-3 OP'S CK'D GEAR SYSTEM CK'D OK. 2L72 4F RTA21EA 20030128000852003012800085EA 2003 1 28 03026621 120030126A3260162253 BRACKET CNDAIRCL600 CL6002B19 1900309EA A VTZAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA27621BR NOSE GEAR DISAGREE LIGHT ILLUMINATED ON TAKEOFF, R&R TARGET BRACKET, P/N 16225-3, OP'S CK'D GOOD. 2L72 4F RTA21EA 20030128000912003012800091NM 2003 1 28 03FDEA00033 120030115A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 MECHANICAL DAMAGE ON FRAME, BS 980, STR 7R. REMOVED MECHANICAL DAMAGE. FABRICATED, DRILLED, ALOINDED, PRIMED, AND INSTALLED REPAIR DOUBLER IAW SRM. 2L73 4F RTA3WE 20030128000922003012800092SW 2003 1 28 HEEA083840 120030116A6230406010428109 BUSHING BELL 407 407 1182206SW M/R HEAD SET WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH3602 53399 MAIN ROTOR HEAD BUSHING SET WORN. 1G71 3U O H2SW 20030115000252003011500025EA 2003 1 15 SWIA200311685 120030111A2797 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA J6CD SHORTED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07929SW 7703 STAB TRIM CH. 2 WILL NOT ENGAGE. FOUND BURNED AND SHORTED PIN B AT J6CD. REPLACED CONNECTOR AND REPAIRED WIRING. STAB TRIM OPS CHECKS GOOD. 2L72 4F RTA21EA 20030115000902003011500090SW 2003 1 15 AC2A082963 120030104A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK H AC2AK NONE L NO TEST ININSP/MAINT 1 FS0117238357 51492 BATTERY IS WEAK ON STARTS. "LOW VOLTAGE ON STARTS" REPLACED BATTERY. 1G71 3U H2SW 20030115000922003011500092SW 2003 1 15 AC2A082964 120030107A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK H AC2AK NONE L NO TEST ININSP/MAINT 1 FS0153702498 51249 BATTERY IS WEAK. "BATTERY HAS LOW VOLTAGE DURING START" REPLACED BATTERY. BATTERY WAS RECHARGED, A CAPACITY CHECK WAS PERFORMED AND BATTERY FAILED. BATTERY WAS RECHARGED WITH A CONDITIONING CHARGE AND A CAPACITY CHECK WAS PERFORMED AGAIN. BATTERY FAILED A SECOND CHECK. RECHARGED BATTERY. ALL WORK DONE IAW INSTRUCTIONS FOR CONTINUED AIRWORTHINESS MAINTENANCE MANUAL SUPPLEMENT FOR VALVE REGULATED LEAD-ACID MAIN BATTERY. MANUAL: M1 REVISION: F JUNE 20, 2002 1G71 3U H2SW 20030115000932003011500093EU 2003 1 15 0301021 120030102A2611CGAB120101 SMOKE DETECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE E/E BAY DIRTY A UHLAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NE03121CQ1396 1396 340A121 FLIGHT 4501, AIRCRAFT WAS TAXIING TO TAKEOFF WHEN THE AVIONICS SMOKE WARNING LIGHT ILLUMINATED ON THE CWP. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MECHANIC INSPECTED AND CLEANED THE AVIONICS SMOKE DETECTOR. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030115000992003011500099EU 2003 1 15 0301131 120030113A143040S57 CAMLOCK SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE RT NACELLE MISSING A UHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NE03340SZ 340A004 401 DRG189789 FLT 4534, HANGER, UPON TAXI TO DEICE LINEUP THE FLIGHT ATTENDANT NOTICED A CAMLOCK MISSING FROM THE TOP FORWARD COWLING ON THE RIGHT ENGINE. THE AIRCRAFT RETURNED TO THE GATE AND SHUT DOWN SO MECHANIC COULD REPLACE THE MISSING HARDWARE. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030115001012003011500101SW 2003 1 15 ALGA082913 120030110A6230407040038101A MAST BELL 407 407 1182206SW MAIN ROTOR CRACKED H ALGAK NONE O OTHER ININSP/MAINT 1 FS01582364028 53069 FOUND MAST SHAFT CRACKED, BELOW SPLINES, MIDDLE OF SHAFT. 1G71 3U O H2SW 20030115001052003011500105WP 2003 1 15 03FDEA00003 120030103A3620 PRESSURE SWITCH DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL PNEUMATIC SYS FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25389FE 46623 PNEUMATIC SYSTEM 3 MANIFOLD FAILURE, IN FLIGHT. COMPLETED RED TABS, LIGHT WENT OUT. CREW REPORTED FAILURE OCCURRED ON DESCENT, APPX 30-40 MILES OUT. REMOVED AND REPLACED RIGHT WING PRESSURE SWITCH IAW MM. OPS CHECK NORMAL IAW TAFI. 2L73 4F4 F A22WE E23EA 20030115001062003011500106NM 2003 1 15 03FDEA00006 120030108A2752MS9391130ZE4C MOTOR BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE T/E FLAP FAILED A FDEAO OTHER K FLUID LOSS APAPPROACH 1 SO25244FE 21647 COMPLETE LOSS OF SYSTEM A HYDRAULIC FLUID JUST PRIOR TO FLAP EXTENSION. SPOILERS HAD BEEN USED JUST PRIOR TO LOSS. REPLACED RIGHT OUTBOARD FLAP MOTOR IAW MM, SERVICED HYDRAULIC SYSTEM TO FULL LEVEL. OPERATED FLAPS UP AND DOWN SEVERAL TIMES, ALL INDICATIONS NORMAL. 2L73 4F4 FRTA3WE E2EA 20030115001162003011500116 2003 1 15 BAQA082896 420030108A3425656767 COMPENSATOR BOLKMS117 BK117A3 5626015EU COCKPIT HSI CRACKED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911NH8149 7030 COMPENSATOR CRACKED AND HAS WATER DAMAGE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030115001222003011500122NM 2003 1 15 03FDEA00010 120030108A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 OIL CAN DENT IN SKIN AT BS 211, RBL 23, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR IAW SRM 53-30-3. 2L73 4F4 FRTA3WE E2EA 20030115001532003011500153 2003 1 15 ERAA082936 420030103A22107659506 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01578EH3628 760099 UNIT INOPERATIVE. ARMATURE AND BRUSHES WERE BOTH WORN, REQUIRING OVERHAUL. REPLACED MOTOR, CLUTCH WASHER, POTENTIOMETERS, SEAL, PACKING, GROMMETS, GROUND STRAP, AND BEARING. CALIBRATED FOR OPTIMUM PERFORMANCE. REPAIRED AS REQUIRED. 1G72 3U H1NE 20030115001592003011500159SW 2003 1 15 ERAA082940 120030103A6420 BEARING BELL 412 412 1182202SW TAIL ROTOR WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01415EH307 HB837 33009 FEATHER BEARINGS WORN. FOUND FEATHER BEARINGS ARE IN LIMITS, TRUNNION LOOSE. RE SHIMMED TRUNNION, COMPLIED WITH TRUNNION CENTERING IAW 412 CR&O. INSPECTED T/R BLADES, CLEANED AND WAXED. INSPECTED FEATHER BEARINGS. FOUND TO BE IN LIMITS. REASSEMBLED T/R ASSY, MARVEL BALANCED AND TORQUED IAW 412 CR&O. 1G72 4U H4SW 20030115001972003011500197SW 2003 1 15 ERAA082945 120030106A6230412010402111 SWASHPLATE BELL 412 412 1182202SW MAIN ROTOR WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01412EH5819 33001 SWASHPLATE HAS WORN GIMBAL RING AND S/P LINK BEARINGS. ALSO TWO TRUNNIONS WORN, DISASSEMBLED TO FACILITATE GIMBAL BEARING REPLACEMENT. REPLACED GIMBAL RING BEARINGS AND BOLTS AND REPLACED 2 TRUNNIONS. VISUALLY INSPECTED AND FOUND NO ADDITIONAL DEFECTS. REASEMBLED, TORQUED AND SEATED AS REQUIRED. COMPLIED WITH ASB412-02-110 ON 2 GIMBAL BOLTS. LUBED BRGS WITH MOBIL 28 GREASE. REPAIRED IAW 412 CR&O CH 62, MM 62, & SPM TT 5819.2 TSO 1294.9 1G72 4U H4SW 20030115002102003011500210NM 2003 1 15 DL733030027 120030106A5311654581327 FRAME BOEING737 737347 1384647NM R1 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307WA 23440 CORROSION WAS FOUND ON THE INNER FLANGE OF THE R-1 DOORWAY AFT FRAME JUST ABOVE THE FLOORLINE. THE CORROSION WAS REMOVED TO A MAX DEPTH OF .017". ADDITIONALLY, A GOUGE WAS REMOVED 4" ABOVE THE CORROSION TO A MAX DEPTH OF .021". A REPAIR ANGLE WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2L72 4F RTA16WE 20030115002112003011500211NM 2003 1 15 DL733030028 120030106A5330654577350 SKIN BOEING737 737347 1384647NM 757 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307WA 23440 THREE AREAS OF PRE-EXISTING DAMAGES WERE REPORTED. THE FIRST TWO WERE PREVIOUS BLENDS AT FS 757 AT STR 15R AND JUSTBELOW STR 14R. THE FINAL DAMAGE WAS JUST AFT AT STR 15R. ALL OF THE DAMAGES WERE REMOVED WITH TWO CUTOUTS. THE DAMAGE AT FS 757 RESULTED IN A 9" X 5" CUTOUT AND THE REMAINING INA 6.25 X 2.25" CUTOUT. AN EXTERNAL DOUBLER WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2L72 4F RTA16WE 20030102000512003010200051SO 2003 1 2 C2XA02CL253 120030101A304016311112 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT BURNED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714907 145468 DURING FLIGHT 3432 THE CREW REPORTED A BURNING ODER DURING ICING CONDITIONS, MAINTENANCE REPLACED THE FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT AND HAD THE AIRCRAFT TEST FLOWN.DURING THE TEST FLIGHT IT WAS DISCOVERED THE RIGHT WINDSHIELD WAS SMOKING.MAINTENANCE REPLACED THE RIGHT WINDSHIELD. 2L72 4T RTT00011AT 20030103000012003010300001SO 2003 1 3 C2XA02SH166 120030103A530014521725615C SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV- DURING C CHECK SILL BY SERVICE DOOR FOUND TO HAVE CORRSION BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED AFFECTED SILL IAW EMB SRM 145 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030103000682003010300068 2003 1 3 RAIA00301003 420030102A34207011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03572HK7927 10 41091 5371-BWI-CAPTAIN'S FLIGHT INSTRUMENTS ALL WENT BLANK. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SYMBOL GENERATOR, OPS CK OK. 2L72 4T RTA41NM 20030104000012003010400001SO 2003 1 4 C2XA02SH170 120030104A530013500400013 STRINGER EMB 145 EMB145LR 3260212SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV-DURING C CHECK THE T REINFORCEMENT ON STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030105000012003010500001SO 2003 1 5 C2XA03CL002 120030103A361014530046403 TUBE EMB 145 EMB145ER 3260211SO ENGINE 1 PYLON LEAKING A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2714940 145033 CLE FLIGHT 3091 THE CREW REPORTED BLEED 1 LEAK INDICATION ON EICAS,THEN RETURNED TO CLE .AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PYLON BLEED TUBE ASSEMBLY AND IT LEAK CHECKED GOOD. 2L72 4F RTT00011AT 20030106001002003010600100WP 2003 1 6 DHL2003805001 120030104A2611 LAMP DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01805DH 46125 1) DURING PREFLIGHT #12 SMOKE DETECTOR DOES NOT PRESS TO TEST.2) ITEM TRANSFERRED TO DMI LOG PER 26-6-1 DMI #11487 PLACARD INSTALLED.3) DMI #11487 DURING PREFLIGHT #12 SMOKE DETECTOR DOES NOT PRESS TO TEST.4) REMOVED AND REPLACED LAMPS TO #12 SMOKE DETECTOR IAW M/M 26-10-6. TESTED OK. THIS CLEARS DMI #11487. 2L74 4F RT4A25 20030106001302003010600130SW 2003 1 6 ALGA082781 120030103A6320204040132001 BEARING RACE BELL 206 206L3 1182108SW M/R GEARBOX GALLED H ALGAK NONE O OTHER ININSP/MAINT 1 FS01355AL 51444 FOUND RACE BREAKING DOWN WHEN GEARBOX DISASSEMBLED FOR OVERHAUL. 1G71 3U H2SW 20030106001452003010600145EU 2003 1 6 BAQA082793 120030106A2435524031 STARTER GEN AEROSPAS365 AS365N2 8680815EU ENGINE MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME416 6417 STARTER GENERATOR KICKED OFF LINE. WOULD NOT RESET. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030106001692003010600169NM 2003 1 6 ZW0A0300201 120030105A33507732 LAMP DOUG MD80 MD83 3023681NM A ZW0AK NONE O OTHER NRNOT REPORTED 1 CE139414W 53189 THE EGRESS LIGHT AT CABIN ROW 31 WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 11-6-02 STL. --CLOSED-- 2L72 4F RT 20030106001872003010600187NE 2003 1 6 HEEA082820 120030102A63217665009803103 POWERPACK SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911UK 760275 ROTOR BRAKE POWERPACK SLOW TO STOP ROTOR. 1G72 3U H1NE 20030124000062003012400006NE 2003 1 24 NACA20030069 220030123A8530356993 CYLINDER PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE 4 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA525 525 NK510318 45529 NK510318 DISCREPANCY: #4 ENGINE PRECAUTIONARY SHUT DOWN DUE TO BACK FIRING, ANALYZER READS #4 CYLINDER LOW COMPRESSION BOTH SIDES.CORRECTIVE ACTION: REPLACED #4 ENGINE #4 CYLINDER. 2L74 4R4 R A781 5E8 20030124000072003012400007NM 2003 1 24 DHL2003751001 120030123A5210 GUIDE ARM BOEING727 727264 138408MNM A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01751DH 22982 1) FOUND FORWARD ENTRY DOOR OPEN LATCH (LOCK LEVER) BROKEN.2) REMOVED AND REPLACED FORWARD ENTRY DOOR GUIDE ARM AND ROLLER ASSEMBLY IAW M/M 52-11-22. DOOR OPS CHECKED GOOD. 2L73 4F A3WE 20030124000112003012400011SO 2003 1 24 C2XA03BT014 120030123A4900 APU EMB 145 EMB145LR 3260212SO TAILPIPE ODOR A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2711544 145557 EWR---CO2517, CREW REPORTED, "FUEL ODOR WHEN OPERATING AIRCONDITIONING PACKS WITH APU RUNNING." MAINTENANCE PERFORMED OPERATIONAL CHECK OF AIRCONDITIONING SYSTEM (WITH APU RUNNING)IAW EMB145 AMM #21-51-00. OPS.CHECKED GOOD. NO ABNORMAL ODORS NOTED. AIRCRAFT RETURNED TO SERVICE. (SUSPECT WINDS BLOWING UP THE APU TAILPIPE.) 2L72 4T RTT00011AT 20030124000792003012400079NM 2003 1 24 EIA2003005 120030123A330065B475291 CARD BOEING747 747121 1384871NM BURNED A EIAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09480EV FEC128 20348 DURING CLIMB OUT WE SMELLED STRONG ELECTRICAL FUMES FROM COCKPIT SOMEWHERE AROUND FE's PANEL.fOUND PC CARD A16 AND TYPE II LAMP DIMMER CARD A14 BURNT. REPLACED CARD IAW MM 33-11-01. FOR PRECAUTIONARY REPLACED DIMMER AND TRANSFORMER FE LIGHT CONTROL PANEL IAW MM 33-11-01 OPS NORMAL 2L74 4F A20WE 20030124000802003012400080NM 2003 1 24 EIA2003003 120030122A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 FRAME WEB CRACKED FS 1580 ABOVE STR. 43R. REMOVED DAMAGE, NDT AREA, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER B747 SRM 53-10-01 FIG. 70 2L74 4F A20WE 20030128000932003012800093SW 2003 1 28 HEEA083841 120030116A6230406010429101 PIN BELL 407 407 1182206SW M/R DRIVE LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 MAIN ROTOR DRIVE LINK PIN WORN. 1G71 3U O H2SW 20030128000992003012800099SW 2003 1 28 HEEA083845 120030116A6230 BUSHING BELL 407 407 1182206SW PC LEVER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH AFS2155 53401 MAIN ROTOR PITCH CHANGE LEVER BUSHINGS WORN. 1G71 3U O H2SW 20030128001012003012800101SW 2003 1 28 HEEA083846 120030116A6230 BUSHING BELL 407 407 1182206SW PC LEVER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH AFS2156 53401 MAIN ROTOR PITCH CHANGE LEVER BUSHINGS WORN. 1G71 3U O H2SW 20030314000262003031400026NM 2003 3 14 03FDEA00046 120030115A5712ARB2850505 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING NR 16 SLAT TRACK INBOARD STRUCTURAL RIB FOUND CRACKED (CRACK LENGTH APPROX 0.5 INCHES). REMOVED DAMAGED RIB NR 16 AND REPLACED NEW RIB NR 16 AT LT WING TRACK INBOARD STRUCTURAL AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20030128001172003012800117SW 2003 1 28 HEEA083857 120030116A6310406040316101 SPLINE ADAPTER BELL 407 407 1182206SW ENG/MRGB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 MAIN ROTOR ENGINE TO GEARBOX SPLINE ADAPTER WORN. 1G71 3U O H2SW 20030128001182003012800118SW 2003 1 28 HEEA083858 120030116A6310406040316101 SPLINE ADAPTER BELL 407 407 1182206SW ENG/MRGB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 MAIN ROTOR ENGINE TO GEARBOX SPLINE ADAPTER HAS WORN SPLINES. 1G71 3U O H2SW 20030128001192003012800119SW 2003 1 28 HEEA083859 120030116A6310406040316101 SPLINE ADAPTER BELL 407 407 1182206SW ENG/GB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 ENGINE TO GEARBOX SPLINE ADAPTER HAS WORN SPLINES. 1G71 3U O H2SW 20030128001222003012800122SW 2003 1 28 HEEA083861 120030116A6310406040316101 SPLINE ADAPTER BELL 407 407 1182206SW ENGINE TO GB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 ENGINE TO GEARBOX SPLINE ADAPTER HAS WORN SPLINES. 1G71 3U O H2SW 20030128001272003012800127SO 2003 1 28 000238 120030113A2130 COUPLING EMB 145 EMB145 3260210SO CABIN PRESSURE LOOSE A CHQAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL11275 RAPID DECOMPRESSION, FOUND SPLIT FLEXIBLE COUPLING ON NR 2 PACK AND NR 1 LOOSE FLEX COUPLING. REPLACED SPLIT COUPLING AND TIGHTENED LOOSE ONE AS REQUIRED. NR 2 PACK LEAK CHECKS OK. RAN NR 1 PACK COULD NOT DUPLICATE PACK NR 1 OVHT EICAS MESSAGE. 2L72 4F RTT00011AT 20030128001282003012800128EU 2003 1 28 00070 120030110A3260A23870101 SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE LANDING GEAR FAILED E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05977TW 13 PILOT REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE, RETURNED FOR MAINTENANCE. MAINTENANCE ADJUSTED MICROSWITCH AND SWUNG GEAR CK GOOD. AIRCRAFT DEPARTED GEAR WOULD NOT RETRACT, RETURN TO DEPARTURE AIRPORT, MAINTENANCE R/R 17G1 MICROSWITCH PERFORMED GEAR SWINGS AND RETURN AIRCRAFT TO SERVICE. NO FURTHER PROBLEMS ON NEXT FLIGHTS. 2L72 4F4 F A7EU E7EA 20030128001452003012800145SW 2003 1 28 HEEA083868 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001512003012800151SW 2003 1 28 HEEA083871 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001582003012800158SO 2003 1 28 C2XA02SH181 120030122A532014521721005 BUTT STRAP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712519 145366 SHV-DURING C CHECK THE LT BUTTSTRAP (FWD DIGITAL) JUST AFT OF FRAME 16 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE SECTION AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS EC 5320-01074. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030128001702003012800170WP 2003 1 28 ZW0A0300805 120030108A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT DAMAGED AT STA 905, LBL 12. REMOVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01. 2L72 4F A6WE 20030128001742003012800174WP 2003 1 28 ZW0A0300807 120030110A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT FOUND CRACK IN LOWER DOOR BEAM AT LOWER HINGE CUTOUT. FWD SERVICE DOOR. REPLACED FRAME PER SRM SPM 6-70-01. 2L72 4F A6WE 20030716000932003071600093 2003 7 16 USAASA03055 420030528A2565 SLIDE AIRBUS320 A320214 3930316EU PAX DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19120US 1286 PHL - THE AFT RIGHT SLIDE WAS FOUND UNRAVELED DURING MAINTENANCE. MAINTENANCE REPLACED THE AFT RIGHT SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030716001062003071600106 2003 7 16 HEEA088034 420030701A2312064100900 TRANSCEIVER SKRSKYS76 S76A 8143006NE VHF SYSTEM WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035435V 760158 TRANSCEIVER TRANSMITS AND RECEIVES WEAK. SHOP REPAIR. 1G72 3U H1NE 20030717000012003071700001SW 2003 7 17 HEEA087978 120030626A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW MAIN ROTOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03129MR 51129 MAIN ROTOR ACTUATOR INOPERATIVE. 1G71 3U H2SW 20030717000192003071700019SW 2003 7 17 HEEA087996 120030627A6720 BEARING BELL 407 407 1182206SW LINK DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH HBFS24 53399 TAIL ROTOR LINK BEARING DEFECTIVE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000222003071700022SW 2003 7 17 HEEA087999 120030622A6710407001523101 IDLER ASSY BELL 407 407 1182206SW M/R CONTROL DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR IDLER ASSY BEARING OUTER RACE TURNING IN IDLER. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000252003071700025SW 2003 7 17 HEEA088002 120030621A6220407010104109 CONE BELL 407 407 1182206SW MAIN ROTOR PEELING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR HEAD LOWER CONE HAS TEFLON COATING PEELING OFF OF INNER RACE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000262003071700026SW 2003 7 17 HEEA088003 120030628A6220407010150107 FRAHM BELL 407 407 1182206SW MAIN ROTOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 FRAHM ASSY HAS A SPRING BROKEN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000302003071700030SW 2003 7 17 HEEA088007 120030622A5610407030118107 CHIN BUBBLE BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 RIGHT CHIN BUBBLE CRAZED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000322003071700032SW 2003 7 17 HEEA088009 120030622A5630407030635101 WINDOW BELL 407 407 1182206SW CREW DOOR CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 CRAZED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000342003071700034GL 2003 7 17 AC2A087916 220030602A751023007827 VALVE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL ENGINE DEFECTIVE B AC2AK NONE O OTHER ININSP/MAINT 1 SO077266K 760283 PART IS DEFECTIVE.THE GREEN ANTI -ICE ADVISORY LIGHT WAS REMAINING ON REGARDLESS OF SWITCH POSITION. THE ANTI -ICE SOLENOID VALVE WAS REPLACED BUT DID LIGHT REMAINED ON. THE ANTI-ICE SOLENOID WAS REPLACED AGAIN AND THE PROBLEM WAS CURED. SOLENOID WAS REPLACED. 1G72 3U3 U H1NE E1GL 20030717000502003071700050SW 2003 7 17 HEEA088026 120030619A6320206040156001 MAGNETIC SEAL BELL 407 407 1182206SW XMSN INPUT LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03493PH 53393 TRANSMISSION INPUT SEAL LEAKING. REPLACED MAG SEAL 206040156001 DUE TO PITTING. REPAIRED. 1G71 3U O H2SW 20030717000532003071700053 2003 7 17 HEEA088029 420030702A2215214001540113 ACTUATOR BELL 214 214ST 1182106SW SCAS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N 28106 CAUSING SCAS ROLL TO DISENGAGE. 2G72 4U H10SW 20030717000542003071700054 2003 7 17 HEEA088030 420030626A34427007700614 DISPLAY BELL 412 412 1182202SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 WEATHER RADAR DISPLAY FAILED. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030717000612003071700061SW 2003 7 17 HEEA088054 120030609A6210206015001115 BLADE BELL 206 206L3 1182108SW MAIN ROTOR LIGHTNING STRIKEE HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128546 51134 MAIN ROTOR BLADE INVOLVED IN LIGHTNING STRIKE. FOUND SOME SMALL AREA ALONG THE SEAM THAT APPEARS TO BE FROM LIGHTNING. 1G71 3U H2SW 20040413000482004041300048NM 2004 4 13 ASAA0240168 120030322A5345651612910 SHELF BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND RADAR TRANSCEIVER SHELF IS CRACKED BELOW AFT END OF LEFT MOUNT CHANNEL. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030124000862003012400086NM 2003 1 24 UPS03240066 120030106A5520 ELEVATOR BOEING727 72721C 138400MNM L/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE:C SUSPECT CRACK ON LH ELEVATOR REAR SPAR @ 2 ND HINGE FROM O/B @ TOP I /B CORNER DUE TO UNAVAILABILITY OF REAR SPAR REPLACEMENT KIT. REPLACED L/H ELE VATOR IAW MM 27-30-01 2L73 4F A3WE 20030124000872003012400087NM 2003 1 24 UPS03440041 120030102A5310 WEB BOEING747 747259B 1384804NM LH WLG W/W CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C L/H WLG W/W FWD BULKHEAD WEB UPPER AREA BS 1241 LBL 60-100 CORROSION REVEALED. CORROSION REMOVED IAW SRM51-10-01, CORROSION DEPTH 0.038", WIDTH 1", LENGTH 2". 2L74 4F RTA20WE 20030204002832003020400283NM 2003 2 4 F3LA200300015 120030118A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM FASTENER CORRODED AND FROZEN IN PLACE AT STA 294.5, LBL 5. DETERMINED CORROSION TO BE OUT OF LIMITS PER SRM 53-10-15. REPAIRED FLOORBEAM UPPER CHORD FROM LBL 22 - RBL 59 PER SRM 53-10-51, FIG 205, SRM 51-40-2 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030127000022003012700002SW 2003 1 27 HEEA083575 120030113A6730212076003005 SERVO BELL 412 412 1182202SW ROTOR SERVO SYS LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033893L 33006 ROTOR SERVO SYSTEM LEAKING AT PILOT VALVE. REPLACED SERVO. 1G72 4U H4SW 20030127000032003012700003 2003 1 27 HEEA083579 420030114A34424000038 CONTROL HEAD BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 WEATHER RADAR CONTROL HEAD WILL NOT HOLD POSITION. SHOP REPAIR. 1G72 4U H4SW 20030127000052003012700005 2003 1 27 HEEA083581 420030114A23124000106010 CONTROL UNIT SKRSKYS76 S76A 8143006NE VHF SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792CH 760193 VHF CONTROL UNIT TONE CODES ARE INTERMITTENT. SHOP REPAIR. 1G72 3U H1NE 20030127000072003012700007 2003 1 27 HEEA083583 420030114A3421504001790116 GYRO BELL 412 412 1182202SW COCKPIT INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 HORIZON GYRO HAS A 20 DEGREE TILT IN LEVEL FLIGHT. SHOP REPAIR. 1G72 4U H4SW 20030127000132003012700013SW 2003 1 27 HEEA083589 120030114A243651589002R VOLT REGULATOR BELL 412 412 1182202SW DC SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 VOLT REGULATOR HAS UNEVEN AMP. DRAW. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030127000182003012700018 2003 1 27 HEEA083594 420030114A3442MI5851345 INDICATOR BELL 412 412 1182202SW RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 RADAR SCREEN TURNS DARK IN FLIGHT. SHOP REPAIR. 1G72 4U H4SW 20030127000252003012700025 2003 1 27 HEEA083601 420030114A3442MI585202 PEDESTAL BELL 412 412 1182202SW RADAR ANTENNA INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 RADAR ANTENNA PEDESTAL WILL NOT TILT. SHOP REPAIR. 1G72 4U H4SW 20030127000332003012700033 2003 1 27 HEEA083609 420030114A2312064105430 TRANSCEIVER BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 TRANCEIVER KEEPS FLICKING OFF. TURNING THE KNOB OFF THEN BACK ON GETS IT TO WORK AGAIN. REPLACED BAD S901 VOLUME CONTROL SWITCH AND MHZ SWITCH HOUSING. REPAIRED. CLEANED SELECTOR CONTACTS. BENCH CHECK GOOD. 1G71 3U O H2SW 20030127000352003012700035 2003 1 27 HEEA083611 420030114A3452066106200 TRANSPONDER BELL 407 407 1182206SW ATC SYS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 TRANSPONDER KNOB BROKEN. FOUND FACEPLATE ASSY AND CATHODE PULSE OSCILLATOR V101 BAD. REPLACED. BENCH CHECK GOOD. 1G71 3U O H2SW 20030127000412003012700041 2003 1 27 HEEA083618 420030114A345713824120234 GPS BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 GPS RECEIVER LOSES MEMORY. FOUND BATTERY VOLTAGE GOOD. REPLACED BAD MESSAGE BUTTON BACKLIGHT BULB AND BAD BUTTONS. BENCH CHECK GOOD. 1G71 3U O H2SW 20030127000442003012700044 2003 1 27 HEEA083621 420030114A345713824120234 GPS BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 GPS RECEIVER NOT HOLDING MEMORY. SENT TO ASM FREEFLIGHT FOR INSPECTION AND REPAIR. 1G71 3U O H2SW 20030127000492003012700049SW 2003 1 27 HEEA083626 120030114A52103160201 HANDLE BELL 407 407 1182206SW CREW DOOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 CREW DOOR HANDLE WORN. TO BE SENT TO BELL FOR CREDIT. 1G71 3U O H2SW 20030127000562003012700056 2003 1 27 HEEA083634 420030114A342150400179015 INDICATOR BELL 407 407 1182206SW ADI MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 IN CRUISE FLIGHT THE ADI INDICATOR PITCHES UP LIKE THE AIRCRAFT IS IN A CLIMB WHEN IT IS NOT. REPAIRED. 1G71 3U O H2SW 20030128001752003012800175WP 2003 1 28 ZW0A0300808 120030110A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT IN THE FWD CABIN, FOUND CORROSION ALONG THE FLOOR SUPPORT AT STA 148 TO 200, 8 INCHES LBL, UNDER NUMBER 5 FLOOR PANEL. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01. 2L72 4F A6WE 20030128001782003012800178WP 2003 1 28 ZW0A0300811 120030113A5320 BRACKET DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT FOUND FWD SERVICE DOOR AFT SILL BRACKET CORRODED, STA 197 AND RBL 53. REPLACED BRACKET PER DOUGLAS DRAWING 9911516 AND SPM 6-70-01 FASTENER SUBSTITUTION, 51-50-01 SRM. 2L72 4F A6WE 20030128001832003012800183WP 2003 1 28 ZW0A0301102 120030123A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ZW0AK NONE O OTHER LDLANDING 1 CE13973TW 53623 SEVERAL SEGMENTS OF EGRESS LIGHTING WERE INOP. REPLACED BATTERIES IN POWER SUPPLY AT ROW 21 AND RECONNECTED FEED CABLE AT ROW 29. OPS CHECK GOOD. 2L72 4F RTA6WE 20030128001862003012800186WP 2003 1 28 ZW0A0301105 120030117A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139629H 53599 DURING CHECK-C CRACK AT LEFT HAND MAIN GEAR DOOR CUTOUT FORWARD 11B CORNER FORWARD OF DOOR ACTUATOR ASSEMBLY RUNNING OUTBOARD FROM CORNER TURNING UPWARD. ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER IAW SRM 51-20-5. 2L72 4F RTA6WE 20030128001912003012800191NM 2003 1 28 QXEA0300125 120030126A2910570347 PUMP DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09366PH7562 510 PDX-ON FLIGHT NUMBER 2189, AFTER TAKEOFF, AFTER GEAR RETRACTION, LEFT MAIN NOSE AND NOSE GEAR DOOR DID NOT CLOSE. #2 HYDRAULIC PRESSURE ZERO, QUANTITY AND STANDBY PUMPS OK. RETURNED TO FIELD AFTER ALTERNATE GEAR EXTENSION. REMOVED AND REPLACED #2 ENGINE HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030128001972003012800197EU 2003 1 28 DHL2003362005 120030118A3230286467 SERVO VALVE AIRBUS300 A300B4203 3930306EU MLG FAILED A DHLACO ABORTED TAKEOFF OTHER J WARNING INDICATION TOTAKEOFF 1 SO01362DH 84 NR 7 BRAKE HOT LIGHT ILLUMINATED ON TAKEOFF ROLL AIRCRAFT WEIGHT: 25,100, 60 KTS, 11 C, AND PRESSURE ALTITUDE 288 FT. TRANSFERRED TO DMI #11676 IAW MEL 32-42-09 COMPLIED WITH SECURING PROCEDURES. NR 7 BRAKE DEACTIVATED. REF. DMI 11676 - NR 7 BRAKE HOT LIGHT ILLUMINATED ON TAKEOFF ROLL, A/C WEIGHT 251,000, 60 KNOTS, 11 DEGREES C, AND PRESSURE ALTITUDE 288. REMOVED AND REPLACED NR 7 GREEN SYSTEM SERVO VALVE WITH SERVICEABLE UNIT IAW A-300M/M 32-42-48 BLOCK 501. THIS CLEARS DMI #11676. 2L72 4F RTA35EU 20030128002352003012800235SW 2003 1 28 HEEA083886 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002362003012800236NM 2003 1 28 AWXA200300046 120030112A5320654797321 WEB BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK A .5 INCH CRACK WAS FOUND ON CUSP WEB AT LT SIDE BS 617 TO BS 637. MAINTENANCE REMOVED THE CRACKED CUSP WEB BS 617 TO BS 637; FABRICATED A NEW REPLACEMENT CUSP WEB; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 38, FIG 8, AND PG 3, 5, 51, FIG 13. 2L72 4F RTA16WE 20030128002392003012800239SW 2003 1 28 HEEA083889 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002462003012800246SW 2003 1 28 HEEA083894 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002542003012800254SW 2003 1 28 HEEA083901 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH NHFS6025 53159 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030128002552003012800255SW 2003 1 28 HEEA083902 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH NHFS6113 53159 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030128002572003012800257SW 2003 1 28 HEEA083904 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030128002702003012800270NM 2003 1 28 C1HA200384001 120030116A3350 BATTERY PACK BOEING727 7272S7 138407ZNM CABIN DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15684CA 22491 EMER FLOOR TRACK LIGHTING FROM ROW 14 FWD INOP. REMOVED & REPLACED EMER FLOOR TRACK LIGHTING BATTERY PACK & POWER SUPPLY AT STATION 480 IN REF TO M/M CH 33-50-23. OPS CHECK OK. 2L73 4F A3WE 20030129000062003012900006SW 2003 1 29 HEEA083916 120030117A6220407001526105 BELLCRANK BELL 407 407 1182206SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 MAIN ROTOR HEAD BELLCRANK BEARING WORN AND WEAR PAD RUBBER TORN AND UNBONDED. 1G71 3U O H2SW 20030129000072003012900007SW 2003 1 29 HEEA083917 120030117A6220407001526101 BELLCRANK BELL 407 407 1182206SW M/R HEAD DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 BELLCRANK RUBBER IS DEBONDED. 1G71 3U O H2SW 20030127000672003012700067GL 2003 1 27 HEEA083645 220030114A72616895090 HOUSING BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE OIL DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 FLUCTUATING OIL PRESSURE. REPAIRED. 1G71 3U3 UO H2SW E1GL 20030127000732003012700073SW 2003 1 27 HEEA083647 120030114A282070061H000V112A HOSE BELL 407 407 1182206SW FUEL DIST KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 FUEL HOSE KINKED. 1G71 3U O H2SW 20030127000772003012700077SW 2003 1 27 HEEA083650 120030114A282070079E000D176 HOSE BELL 407 407 1182206SW FUEL DIST CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 FUEL HOSE ASSY CHAFED. 1G71 3U O H2SW 20030127000802003012700080NM 2003 1 27 PCAA0301019 120030117A3350 CONNECTOR DHAV DHC8 DHC8102 2809003NM CABIN DISCONNECTED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13830EX 155 DURING ROUTINE MAINTENANCE VISIT 3 EMERGENCY FLOOR LIGHTS WERE FOUND INOPERATIVE AT ROW 5. AFTER REMOVING CENTER FLOORBOARD, WIRING FOR LIGHTS FOUND TO BE UNPLUGGED. CONNECTOR RECONNECTED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030127000842003012700084 2003 1 27 SWAA030058 420030110A256565C19901 CABLE BOEING737 7373H4 1384600NM SERVICE DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030127000862003012700086 2003 1 27 SWAA030060 420030110A25656567380 COVER BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 AFT SVC DOOR EMERGENCY EVAC SLIDE COVER FELL OFF. REINSTALLED COVER PER MM. 2L72 4F RTA16WE 20030127000942003012700094SW 2003 1 27 HEEA083658 120030114A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 EMERGENCY FLOAT FUSIBLE PLUG LEAKING. TO BE SENT TO BELL. 1G71 3U O H2SW 20030127001012003012700101EA 2003 1 27 COMA0360046 120030123A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT UNRELIABLE A COMAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION APAPPROACH 1 SO01940CA3528 7048 FLIGHT 5608 FLAPS FAILED DURING APPROACH.REPLACED THE L/H BPSU. 2L72 4F RTA21EA 20030127001062003012700106 2003 1 27 HEEA083660 420030114A344280510800001 CONTROL BOX BELL 407 407 1182206SW WX RADAR SYS UNRELIABLE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 DATA BOX SKYWATCH UNRELIABLE. 1G71 3U O H2SW 20030127001102003012700110 2003 1 27 HEEA083663 420030114A34578143802240D GPS BELL 407 407 1182206SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 GPS SYSTEM FREEZES UP. 1G71 3U O H2SW 20030127001142003012700114GL 2003 1 27 HEEA083665 220030114A732095704 CHECK VALVE BELL 407 407 1182206SW ALLSN 250C 250C30 03013GL ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 CHECK VALVE FLARE END NICKED CAUSING LEAK. REPAIRED. 1G71 3U3 UO H2SW E1GL 20030127001172003012700117SW 2003 1 27 HEEA083667 120030115A6710206001396001 SHAFT BELL 407 407 1182206SW CYCLIC STICK DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 CYCLIC STICK SHAFT FINE THREADS GALLED AND STRIPPED. 1G71 3U O H2SW 20030127001302003012700130SW 2003 1 27 HEEA083673 120030115A3212206050247131 COVER BELL 407 407 1182206SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 EMERGENCY FLOAT COVER TORN. 1G71 3U O H2SW 20030127001322003012700132SW 2003 1 27 HEEA083675 120030115A3212206050247132 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033193E 53276 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20030127001392003012700139SW 2003 1 27 HEEA083679 120030115A3212206050247135 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20040416000062004041600006NM 2004 4 16 ASAA0240172 120030322A53306546555 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND DAMAGE UNDER FRAME FLANGE AT BS 847. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040416000052004041600005NM 2004 4 16 ASAA0240176 120030322A533065C312403 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON FRAME INNER DOUBLER AT BS 794. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030108000032003010800003SO 2003 1 8 C2XA02SH173 120030108A520014533395001 SKIN EMB 145 EMB145LR 3260212SO DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV DURING C CHECK THE PASSENGER DOOR WAS FOUND TO HAVE A DENT JUST FOWARD OF DOOR'S WINDOW. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5210-01070. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030108000102003010800010WP 2003 1 8 MWEA030003 120030107A5313593058386 INTERCOSTAL DOUG DC9 DC981 3022081WP Y958 & Y962 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 CRACKED INTERCOSTAL BETWEEN FRAMES Y958.117 AND Y962.717 14 INCHES OUTBOARD OF HINGE. -- FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F A6WE 20030108000302003010800030WP 2003 1 8 MWEA030011 120030107A532099234845 WEB DOUG DC9 DC981 3022081WP STA 180 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 INTERCOSTAL WEB CRACKED BETWEEN LEFT FLOOR BEAM AT FRAME STATION 180. -- FABRICATED AND INSTALLED WEB. 2L72 4F A6WE 20030108000312003010800031WP 2003 1 8 MWEA030013 120030107A533059366673 DOUBLER DOUG DC9 DC981 3022081WP STA 1250 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 FUSELAGE SKIN IS DENTED STATION 1250 BETWEEN LONGERONS 30 AND 29 LEFT. -- FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030108000332003010800033EA 2003 1 8 COMA0360001 120030102A291073031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA #3 UNRELIABLE A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01982CA13566 7168 FLIGHT 6811 GEAR DISAGREE WARNING - L/H MLG INDICATED INTRANSIT.REPLACED THE #3 HYDRAULIC RESERVOIR 2L72 4F RTA21EA 20030108000342003010800034EA 2003 1 8 COMA0360002 120030103A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR INOPERATIVE A COMAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO01957CA 7109 FLIGHT 5751 FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOP.REPLACED THE LIGHT STRIP 2L72 4F RTA21EA 20030108000492003010800049EA 2003 1 8 COMA0360008 120030106A5270 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01973CA 7146 FLIGHT 9801 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.ADJUSTED HANDLE PROXIMITY SWITCH (PS2MB). 2L72 4F RTA21EA 20030108000602003010800060EA 2003 1 8 COMA0360010 120030101A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01941CA13595 7050 FLIGHT 5495 LANDING GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030109000012003010900001NM 2003 1 9 PCAA0301010 120030106A3230574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM INOPERATIVE A PCAAO OTHER J WARNING INDICATION LDLANDING 1 EA13841EX208616 249 HPN- FLIGHT#3665. CREW REPORTED LANDING GEAR WOULD NOT EXTEND NORMALLY, GEAR HANDLE SELECTED AND ONLY RED IN-TRANSIT LIGHTS CAME ON, MAIN AND NOSE GEAR WOULD NOT EXTEND. ALTERNATE EXTENSION PERFORMED. MAINTENANCE INSPECTED WIRING AT INHIBIT SWITCH, SELECTOR VALVE AND WING ROOT. VERIFIED POWER AT SELECTOR VALVE WITH GEAR HANDLE UP AND DOWN. DEICE FLUID CLEANED FROM VALVE, AND WING ROOT CANNON PLUGS. PROBLEM REOCCURED FLIGHT#9381. MAINTENANCE REPLACED GEAR SELECTOR VALVE PANEL. PROBLEM REOCCURED FLIGHT#6841. MAINTENANCE OPERATIONAL CHECKED GEAR AND INSPECTED WIRING AND CANNON PLUGS. NO DEFECTS WERE NOTED. LANDING GEAR SELECTOR VALVE REPLACED FOR TROUBLESHOOTING. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED 2H72 4T RTA13NM 20030320000732003032000073NM 2003 3 20 2003UALA00001 120030101A5610NP1653115 WINDSHIELD AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE LEFT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29804UA17385 759 CAPTAINS WINDSHIELD OUTER PANE CRACKED. SUPPLEMENTAL DATA UPDATE LOWER BUS BAR ARCED DUE TO DELAMINATION AND WATER INGRESSION CAUSED BY WEATHER SEAL DETERIORATION. WINDSHIELD WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20030109000662003010900066NM 2003 1 9 2003UALA00002 120030101A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 CABIN FLOORBEAM UPPER CHORD CORRODED, STA 365, RBL 5-15. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLES. 2L72 4F4 FRTA2NM E17NE 20030109000702003010900070NM 2003 1 9 MWEA030019 120030108A5310993053873 DOUBLER DOUG MD88 MD88 3023688NM STA 560 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CUSP MEMBRANE CORREDED LEFT SIDE STATION 560 AREA. -- REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOULBER. 2L72 4F RTA6WE 20030109000722003010900072NM 2003 1 9 MWEA030022 120030108A53109930612100 DOUBLER DOUG MD88 MD88 3023688NM STA 984-1003 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CUSP MEMBRANE CORRODED RIGHT SIDE STATION 984-1003. -- REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER AND FILLERS AND REPAIR PARTS. 2L72 4F RTA6WE 20030127001482003012700148SW 2003 1 27 HEEA083684 120030115A3212206050247138 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033193E 53276 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20030127001602003012700160SW 2003 1 27 HEEA083689 120030115A2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH574 Y10304 53199 STARTER GEN BRUSHES WORN. REPAIRED. 1G71 3U O H2SW 20030127001612003012700161EA 2003 1 27 03024680 120030124A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27680BR EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE MID TO AFT OF CABIN. REMOVED AND REPLACE P/N 2013-1A BATTERY. OPS CHECKED GOOD 2L72 4F RTA21EA 20030127002042003012700204SW 2003 1 27 HEEA083696 120030115A7810206064203101 DUCT BELL 407 407 1182206SW EXHAUST CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 EXHAUST DUCT CRACKED AT BOTH ENDS. 1G71 3U O H2SW 20030127002152003012700215SW 2003 1 27 HEEA083705 120030115A5320206064902035S CHANNEL BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 FUSELAGE CHANNEL CRACKED. SCRAPPED. 1G71 3U O H2SW 20030127002262003012700226SW 2003 1 27 HEEA083712 120030115A2913206076030111 PUMP BELL 407 407 1182206SW HYD SYSTEM FAILED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03402PH 53159 PUMP FAILED DURING LET DOWN HYDRAULIC LIGHT ILLUMINATED AND WHINING NOISE WAS NOTICED WHILE LIGHT WAS ON. 1G71 3U O H2SW 20030127002322003012700232SW 2003 1 27 HEEA083717 120030115A2821 HOUSING BELL 407 407 1182206SW FUEL FILTER LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03742PH 1534 53461 FUEL FILTER HOUSING LEAKING. 1G71 3U O H2SW 20030127002332003012700233SW 2003 1 27 HEEA083718 120030115A6730206076062107 SERVO BELL 407 407 1182206SW CYCLIC LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03405PH 53207 CYCLIC SERVO LEAKING. 1G71 3U O H2SW 20030127002382003012700238SW 2003 1 27 HEEA083721 120030115A6310206340300105 DRIVE SHAFT BELL 407 407 1182206SW M/R GEARBOX CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH771 53266 MAIN ROTOR GEARBOX DRIVE SHAFT IS PITTED ON FLEX FRAMES AND INSIDE OF SHAFT. 1G71 3U O H2SW 20030127002452003012700245SW 2003 1 27 HEEA083725 120030115A3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 EMERGENCY FLOAT SOLENOID VALVE LEAKING. 1G71 3U O H2SW 20030127002492003012700249WP 2003 1 27 MWEA030009 120030107A2922AC7031H8K2 FILTER DOUG DC9 DC932 3022066WP HYD SYSTEM DEFECTIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31216ME 47740 RIGHT HYDRAULIC SYSTEM FLUID QUANTITY DEPLETED AND LOST PRESSURE. REMOVED AND REPLACED AUXILIARY LINE FILTER HOUSING AND FILTERS. 2L72 4F A6WE 20030127002502003012700250SW 2003 1 27 HEEA083728 120030115A521020898421 LATCH BELL 407 407 1182206SW PAX DOOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 PAX DOOR LATCH WORN. 1G71 3U O H2SW 20030127002542003012700254NM 2003 1 27 MWEA030023 120030108A53209930538U23 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RIGHT CUSP MEMBRANE REQUIRES REMOVAL FROM STATION 598 TO 712 DUE TO CORROSION. REMOVED, DRILLED UP AND INSTALLED MEMBRANE. 2L72 4F RTA6WE 20030127002552003012700255SW 2003 1 27 HEEA083730 120030115A3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH 53461 EMERGENCY FLOAT PRESSURE GAUGE HAS WATER INTRUSION AND INACCURATE INDICATIONS. 1G71 3U O H2SW 20030127002592003012700259SW 2003 1 27 HEEA083734 120030115A2821222366621103 FILTER BELL 407 407 1182206SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03492PH 53390 CLOGGED INDICATOR WOULD NOT RESET. 1G71 3U O H2SW 20030127002692003012700269GL 2003 1 27 HEEA083745 220030115A725023001832 NOZZLE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE BENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 ENGINE NOZZLE BENT. SCRAPPED. 1G71 3U3 UO H2SW E1GL 20030127002722003012700272GL 2003 1 27 HEEA083748 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 HIGH TOT. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030127002732003012700273GL 2003 1 27 HEEA083749 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH10297 53003 HIGH MGT. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030127002752003012700275GL 2003 1 27 HEEA083751 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 53188 OCCASIONAL HIGH MGT WITH POWER CHANGES AND POSSIBLE INTERNAL CONTAMINATION. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030127002762003012700276GL 2003 1 27 HEEA083752 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 HIGH ENGINE OPERATING TEMP. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030127002792003012700279GL 2003 1 27 HEEA083755 220030115A753223007827 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03457PH 53147 ANTI ICE LIGHT ILLUMINATES DURING START. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030127002862003012700286GL 2003 1 27 HEEA083759 220030115A724023030911 CASE BELL 407 407 1182206SW ALLSN 250C 250C* GL COMBUSTION CHAM CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 FUEL NOZZLE BOSS CRACKED. REPLACED WITH SERVICEABLE CASE. 1G71 3U3 UO H2SW E4CE 20030127002872003012700287SW 2003 1 27 HEEA083760 120030115A282123056451 FILTER BELL 407 407 1182206SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 BYPASS INDICATOR POPPED. SCRAPPED. 1G71 3U O H2SW 20030127002892003012700289SW 2003 1 27 HEEA083761 120030115A282123056451 FILTER BELL 407 407 1182206SW FUEL SYSTEM CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 FUEL FILTER CONTAMINATED. SCRAPPED. 1G71 3U O H2SW 20030625000672003062500067CE 2003 6 25 NSVA200300003 120030122A52201015141961 HANDLE BEECH 1900 1900C 1154161CE EMERGENCY DOOR LOOSE A NSVAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 EA27207CJ29978 UC107 IN FLIGHT, INSIDE DOOR HANDLE FELL OFF. 2L72 4T RTA24CE 20030127002922003012700292GL 2003 1 27 HEEA083762 220030115A742023060816 LEAD BELL 407 407 1182206SW ALLSN 250C 250C* GL IGNITER BURNED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 IGNITER LEAD END CORRODED AND BURNED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030127002932003012700293SO 2003 1 27 C2XA03IA007 120030125A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716951 145063 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY (OVERHEAD GALLEY LOCATION), PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2L72 4T RTT00011AT 20030128000072003012800007EU 2003 1 28 BAQA082952 120030113A7714L771M40C1003 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE TACH STICKING H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01136MH410 0161 TRIPLE TACH NR 1 AND 2 N2 NEEDLES RANDOMLY STICK. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030128000212003012800021GL 2003 1 28 HEEA083773 220030115A723023063392 ENGINE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENG BAY DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH 53399 CAE847434 ENGINE HAS A HOLE IN LEFT HAND COMPRESSOR ARM PIT. REPLACED WITH SERVICEABLE ENGINE. 1G71 3U3 UO H2SW E1GL 20030128000232003012800023SW 2003 1 28 HEEA083775 120030115A7700 SHAFT BELL 407 407 1182206SW PMA SHEARED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 FADEC FAULT IN FLIGHT. FOUND PMA SHAFT SHEARED DUE TO FAILED BEARING IN PMA. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030109000752003010900075NM 2003 1 9 MWEA030028 120030109A5310993053812 DOUBLER DOUG MD88 MD88 3023688NM STA 522-541 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RIGHT CUSP MEMBRANE HAS CORROSION BETWEEN STATION 522-541. -- CLEANED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030109001242003010900124NM 2003 1 9 AWXA200300017 120030108A3350ABS0374A24 CABLE AIRBUSA319 A319132 3930340NM SEAT ROW 12 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW0 0 1088 CMH - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES ON ESCAPE PATH LIGHT AT SEAT ROW 12 L/H; SPLICED BROKEN WIRES; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030128001942003012800194NM 2003 1 28 AWXA200300021 120030106A532069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND ON THE FORWARD SIDE OF STRINGER TIE CLIP AT BS 1064, STR 5 RT. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 1064, STR 5 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-30-01PG. 5-6, AND SRM 51-40-02, PG. 10-11. 2L72 4F RTA16WE 20030110000292003011000029EA 2003 1 10 COMA0360015 120030108A2150 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01964CA 7129 FLIGHT 5716 TOILET SMOKE WARNING.CLEANED COALESCER SOCKS AND RAN SYSTEM TO CLEAR OIL FUMES FROM PREVIOUS APU FAILURE. 2L72 4F RTA21EA 20030110000302003011000030EA 2003 1 10 COMA0360013 120030108A2421 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 LOW A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01477CA 7670 FLIGHT 9490 NR 1 IDG CAUTION MESSAGE DURING T/O. SERVICED IDG OIL TO PROPER LEVEL. 2L72 4F RTA21EA 20030110000372003011000037EU 2003 1 10 03001302 120030101A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN BROKEN A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27302UE 41013 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL INSTALLED A SPLICE ON A BROKEN WIRE IN THE FORWARD SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20030110000432003011000043EA 2003 1 10 03006635 120030106A3350 COVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27635BR 7295 DURING PREFLIGHT INSPECTION CREW REPORTED THAT EMERGENCY FLOOR TRACK LIGHTING WAS LOOSE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EEL LIGHT STRIP COVER, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030110000442003011000044EU 2003 1 10 03007303 120030107A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27303UE 41015 DURING MAINTENANCE INSPECTION, EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL SECURED LOOSE CONNECTOR, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T3 TRTA41NM E2WE 20030401001762003040100176WP 2003 4 1 DHL2003806002 120030109A56105887276502 WINDSHIELD DOUG DC8 DC873F 302199FWP COCKPIT CRACKED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01806DH 46002 FIRST OFFICER WINDSHIELD CRACKED AT DEPARTURE TIME. DEFERRING F/O'S WINDSHIELD PER GMM 3.5 CAT I; IAW DC-8 M/M TEMP. REMOVED AND REPLACED FO'S WINDSHIELD IAW DC-8 M/M 56-10-2. OPERATIONAL CHECK SERVICEABLE. THIS CLEARS DMI #11530E. REF. DMI #11531 (DUE TO F/O'S WINDSHIELD OUTER PANE CRACKED, DE-ACTIVATED WINDOW HEAT TO F/O'S WINDSHIELD). REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER IAW DC8 M/M 30-41-0, OPERATIONAL CHECK SERVICEABLE. THIS CLEARS DMI #11531. 2L74 4F RT4A25 20030113000392003011300039NM 2003 1 13 0300035509 120030107A5311 FRAME BOEING757 757251 1384970NM CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01509US 23198 During "H" check found corrosion damage on lower sill frame of aft cargo doorway. Repaired per EA 55-193454. 2L72 4F RTA2NM 20030113000872003011300087WP 2003 1 13 DHL2003807001 120030110A56105887276502 WINDSHIELD DOUG DC8 DC873F 302199FWP A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01807DH 45990 1) F/O'S WINDSHIELD EMITS FREQUENT, BUT INTERMITTENT ELECTRICAL DISCHARGES ON THE INTERIOR OF WINDSHIELD. THIS ARCING CAN BE SEEN MOSTLY AT THE TOP AND BOTTOM OF WINDSHIELD WHERE IT MEETS THE WINDOW FRAME.2) REF. ITEM 3P THIS LOG PAGE (#312079) FOR CORRECTIVE ACTION.3) F/O'S WINDSHIELD IS CRACKED.4) REMOVED AND REPLACED F/O'S WINDSHIELD IAW M/M 56-10-2.5) REPLACE R/H FORWARD WINDOW HEAT CONTROLLER DUE TO WINDOW FAILURE. REF. ITEM 3P LOG PAGE #312079.6) REMOVED AND REPLACED FORWARD R/H WINDOW HEAT CONTROLLER IAW DC-8 M/M 30-41-0, OPERATIONAL CHECKED SERVICEABLE. 2L74 4F RT4A25 20030113000892003011300089WP 2003 1 13 DHL2003801001 120030110A3260H2024B SWITCH DOUG DC8 DC873F 302199FWP A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01801DH 46033 1) DOORS NOT LATCHED LIGHT ILLUMINATED. LEFT DOOR UNSAFE LIGHT ILLUMINATED. PERFORMED "GEAR OR DOOR NOT LATCHED LIGHT ILLUMINATED" ABNORMAL PROCEDURE LIGHTS REMAINED ILLUMINATED.2) REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR SWITCH. OPS CHECKED GOOD PER DC8 M/M 32-60-0. 2L74 4F RT4A25 20030113001502003011300150NM 2003 1 13 AWXA200300029 120030112A53302024T3071 SKIN BOEING737 73733A 1384673NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW0 0 23625 PHX - MAJOR REPAIR - DURING INSPECTION A 2 1/2" CRACK WAS FOUND ON SKIN AT BS 767 BELOW EMERGENCY EXIT LIGHT ON R/H SIDE OF AIRCRAFT. MAINTENANCE CUTOUT CRACK; PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER AND FILLER; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG. 201. 2L72 4F RTA16WE 20030114000322003011400032NM 2003 1 14 SWAA030019 120030103A3350311500 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 14 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030114000332003011400033NM 2003 1 14 SWAA030020 120030105A575465C26601 SLAT BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED NR 1 L/E SLAT PER MM. 2L72 4F RTA16WE 20030128000262003012800026GL 2003 1 28 HEEA083778 220030115A741223064130 IGNITER BOX BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 A/C FAILED TO START. REPLACED WITH SERVICEABLE IGNITER BOX. 1G71 3U3 UO H2SW E4CE 20030128000282003012800028GL 2003 1 28 HEEA083780 220030115A723023064570 LINER BELL 407 407 1182206SW ALLSN 250C 250C* GL COMPRESSOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 COMPRESSOR LINER DELAYED STARTS. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000422003012800042SW 2003 1 28 HEEA083796 120030115A7120 BEARING BELL 407 407 1182206SW REAR MOUNT UNSTAKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 14473 53396 REAR MOUNT BEARING IS UNSTAKED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128000542003012800054SW 2003 1 28 HEEA083807 120030116A2430214175131103 RELAY BELL 214 214ST 1182106SW DC SYSTEM ARCED E HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03 DC RELAY CONTACTS ARCED. 2G72 4U H10SW 20030128000602003012800060SW 2003 1 28 HEEA083814 120030116A6210406010120101 BOLT BELL 407 407 1182206SW M/R BLADE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 MAIN ROTOR BLADE BOLT SHANK HAS TWO WORN SPOTS. 1G71 3U O H2SW 20030128000662003012800066SW 2003 1 28 HEEA083820 120030116A6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03494PH2729 53396 MAIN ROTOR SWASHPLATE IS LEAKING GREASE. REPAIRED. 1G71 3U O H2SW 20030128000722003012800072SW 2003 1 28 HEEA083826 120030116A6300406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH1571 53399 MAIN ROTOR LEVER ASSY WORN. 1G71 3U O H2SW 20030128000732003012800073SW 2003 1 28 HEEA083827 120030116A6300406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 MAIN ROTOR LEVER ASSY WORN. 1G71 3U O H2SW 20030128000772003012800077SW 2003 1 28 HEEA083831 120030116A6230406010426101 LINK BELL 407 407 1182206SW SWASHPLATE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH680 53003 MAIN ROTOR SWASHPLATE LINK WORN. 1G71 3U O H2SW 20030128000802003012800080SW 2003 1 28 HEEA083834 120030116A6230406010427109 GIMBAL RING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH3602 53399 MAIN ROTOR GIMBAL RING WORN. 1G71 3U O H2SW 20030128000812003012800081SW 2003 1 28 HEEA083835 120030116A6230406010427109 GIMBAL RING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH2754 53003 MAIN ROTOR GIMBAL RING WORN. 1G71 3U O H2SW 20030128000982003012800098EU 2003 1 28 MALA030129 120030120A2610310108 FIRE LOOP BAC 146 AVRO146RJ85A1500097EU A MALAK NONE JN WARNING INDICATION FALSE WARNING DEDESCENT 1 GL15516XJ E2334 ON DECENT INTO MSP, NWS DIM FAIL LIGHT ILLUMINATED. SEL OVRD AND ENGINE #2 LOOP FAULT ILLUMINATED SE LOOP B AND LIGHT WENT OUT. MAINTENANCE REPLACED #2 ENGINE ZONE 1 FIRE LOOP PN 3101-08 IAW AMM 26-11-11 OPS CHECK GOOD PERFORMED OPS CHECK OF NWS IAW AMM CHAP 31 OPS CHECK GOOD, COULD NOT DUPLICATED PROBLEM. 2H74 4F RTA49EU 20030128001002003012800100WP 2003 1 28 03FDEA00041 120030115A7714 SENSOR DOUG MD10 MD1010F WP GE CF6 CF6* 30020GL NR 2 ENGINE ERRATIC A FDEAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO25363FE 48263 DURING LEVEL CRUISE AT FL 330, CREW OBSERVED A LEVEL 2 ALERT (ENGINE 2 RPM LO) CONSIDERED SEVERE DAMAGE DUE TO NR 1 AND NR 2 RPM SPLIT WITH VERY ERRATIC NR 2 RPM. CREW ACCOMPLISHED SEVERE DAMAGE CHECKLIST IN QRH. PRESHUTDOWN PARAMETERS: NR 1 (94 PERCENT), EGT NORMAL, NR2 (32 PERCENT) PLUS OR MINUS 10 PERCENT AND ERRATIC, FF NORMAL, POST SHUTDOWN PARAMETERS: N1 (0), EGT LOW TEMP, NR 2 (8 PERCENT), FF 0 OIL PRESSURE 6-8 PSI APX. INSPECTED INLET AND EXHAUST; NO DISCREPANCIES FOUND. AFTER C/W MD1010 MM. RAN NR 2 ENG AND DUPLICATED MALFUNCTION. REMOVED AND REPLACED CORE SPEED SENSOR IAW MM. RAN NR 2 ENGINE OPS CHECKED NORMAL. 2L73 4F4 FRTA22WE E23EA 20030128001022003012800102SW 2003 1 28 HEEA083847 120030116A6230 BUSHING BELL 407 407 1182206SW PC LEVER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH AFS2195 53400 MAIN ROTOR PITCH CHANGE LEVER BUSHINGS WORN. 1G71 3U O H2SW 20030128001112003012800111SW 2003 1 28 HEEA083853 120030116A6230406010129101 ROD BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 MAIN ROTOR ROD ASSY WORN. 1G71 3U O H2SW 20030128001142003012800114SW 2003 1 28 HEEA083855 120030116A6320406040030107 BEARING BELL 407 407 1182206SW MRGB TRIPLEX SETCORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 A121 RECEIVED WITH EXCESSIVE CORROSION NEAR THE V INDEX MARK ON OUTER RACES OF TRIPLEX BEARING SET OF MAIN ROTOR GEARBOX. 1G71 3U O H2SW 20030128001232003012800123SW 2003 1 28 HEEA083862 120030116A6520406040416101 SHAFT BELL 407 407 1182206SW TRGB OUTPUT CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH805 A694 53228 TAIL ROTOR GEARBOX OUTPUT SHAFT HAS EXCESSIVE PITTING ON SPLINES. 1G71 3U O H2SW 20030128001242003012800124SW 2003 1 28 HEEA083863 120030116A6520407040416101 SHAFT BELL 407 407 1182206SW TRGB OUTPUT CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH2127 A1109 53401 TAIL ROTOR GEARBOX OUTPUT SHAFT HAS EXCESSIVE PITTING ON SPLINES. OUTPUT CAP 406040408101, SN AFS1424 BEARING LINER WORN BEYOND LIMITS. REPAIRED. 1G71 3U O H2SW 20030128001252003012800125SW 2003 1 28 HEEA083864 120030116A6310 MOUNT BELL 407 407 1182206SW FREEWHEEL UNIT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH A3456 53199 FREEWHEEL UNINT MOUNT BROKEN FOR LT LOWER ROTOR BRAKE MOUNT BOLT. 1G71 3U O H2SW 20030128001382003012800138SW 2003 1 28 HEEA083867 120030116A6310406040500131 FREEWHEEL UNIT BELL 407 407 1182206SW MAIN ROTOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH338 53393 FREEWHEEL UNIT CAUSING ENGINE VIBRATION FWD END AND ALSO FWD SEAL LEAKING. REPLACED FWU. 1G71 3U O H2SW 20030128001542003012800154SW 2003 1 28 HEEA083872 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH 53278 UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001652003012800165SW 2003 1 28 HEEA083877 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001662003012800166NM 2003 1 28 ZW0A0300801 120030116A335060030451 POWER SUPPLY DOUG MD80 MD83 3023681NM CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139414W 53189 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 1 TO 6. REPLACED THE POWER SUPPLY. 2L72 4F RT 20030128001712003012800171SW 2003 1 28 HEEA083878 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001792003012800179SW 2003 1 28 HEEA083880 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001812003012800181NE 2003 1 28 ZW0A0301002 220030120A7261 SCAVENGE PUMP BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE LEAKING A ZW0AEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE13712TW 27624 4960 DURING CRUISE OIL QTY DROPPED FROM 11 QTS TO 5 QTS WITH CONTINUING DROP UNTIL RIGHT ENGINE OIL PRESSURE EICAS MESSAGE. PERFORMED ENGINE FAILURE CHECKLIST. SHUT DOWN ENGINE AND DIVERTED TO TAMPA. FOUND OIL LEAKING FROM SCAVENGE PUMP NIPPLE. REPLACED SCAVENGE PUMP ASSEMBLY. ACCOMPLISHED 757 MM 72-61-08 AND PERFORMED TEST 11 OK FOR SERVICE. 2L72 4F4 FRTA2NM E17NE 20030128001872003012800187SW 2003 1 28 HEEA083882 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001982003012800198 2003 1 28 AWXA200300026 420030111A2565D30664105 SLIDE AIRBUS320 A320231 3930325EU L1 DOOR FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW310092724 65 PHX - EMERGENCY EVACUATION - DURING INSPECTION THE FORWARD FLIGHT ATTENDANT PANEL EMERGENCY SYSTEM TEST FAILED FOR L-1 DOOR. MAINTENANCE REMOVED AND REPLACED DEFECTIVE L-1 DOOR SLIDE IAW T/C R1C25304, EMERGENCY SYSTEM TEST GOOD. 2L72 4F RTA28NM 20030128002232003012800223EU 2003 1 28 AWXA200300035 120030107A5310D5347112420100 CREASE BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON THE LOWER SURFACE OF RT CREASE BEAM (SHEAR PLATE) FROM BS 69 TO BS 70. MAINTENANCE REMOVED DAMAGED CREASE BEAM; FABRICATED A REPLACEMENT CREASE BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-11-42, PG 10 & 12, AND SRM 51-42-11 FIG 59-62, PG 20-27. 2L72 4F RTA28NM 20030128002242003012800224EU 2003 1 28 AWXA200300036 120030105A5320D53475529204 STRUCTURE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON AFT CARGO DOOR CUTOUT LOWER SILL JUST FORWARD OF FRAME SUPPORT FITTING NR 7, FR 52A. MAINTENANCE REMOVED DAMAGED SEALING PROFILE AT AFT CARGO DOOR CUTOUT LOWER SILL; FABRICATED A NEW REPLACEMENT SEALING PROFILE; INSTALLED REPAIR PART IAW A320 SRM 51-44-11, PG. 16-20, FIG. 2. 2L72 4F RTA28NM 20030128002262003012800226EU 2003 1 28 AWXA200300038 120030112A3350ABS0374A24 TERMINAL AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28627AW 66 EWR - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE AT SEAT ROW 19 LT. MAINTENANCE REPAIRED BROKEN TERMINAL AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 19 LT, OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20030128002282003012800228NM 2003 1 28 AWXA200300040 120030109A532069353654 FLOOR SUPPORT BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK A .75 INCH CRACK WAS FOUND AT FASTENER HOLES OF CABIN FLOOR SUPPORT BS 500D TO BS 520, BL 0. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT BS 500D TO BS 520, BL 0; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 38, FIG 8, AND SRM 51-40-05, PG 4-6, & 9, FIG 3 & 4. 2L72 4F RTA16WE 20030128002292003012800229SW 2003 1 28 HEEA083883 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002302003012800230NM 2003 1 28 AWXA200300041 120030113A33501012721 LIGHT BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 PHX - EEL - FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 9 LT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030128002312003012800231NM 2003 1 28 AWXA200300042 120030115A3350900835A BATTERY PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - EEL - DURING INSPECTION THE VERTICAL EMERGENCY EXIT LIGHT AT THE L2 DOOR AND OVER WING EXIT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030128002342003012800234SW 2003 1 28 HEEA083885 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002482003012800248SW 2003 1 28 HEEA083896 120030117A6230406310411101 BOOT BELL 407 407 1182206SW MAIN ROTOR TORN E O OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 MAIN ROTOR BOOT IS TORN AND RIPPED. 1G71 3U O H2SW 20030128002562003012800256SW 2003 1 28 HEEA083903 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH NHFS6120 53188 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030128002622003012800262NM 2003 1 28 C1HA200395004 120030119A3350 BATTERY PACK BOEING727 727290 138408WNM CABIN DISCHARGED A C1HAK NONE L NO TEST TXTAXI/GRND HDL 1 GL15295AS 22147 OVERHEAD EMERGENCY LIGHT AT ROW 11 WILL NOT ILLUMINATE. REMOVED & REPLACED PASS CABIN CEILING EMER LIGHT BATTERY PACK AT ROW 11 IN REF 33-50-01 OPS CHECK OK 2L73 4F A3WE 20030128002632003012800263NM 2003 1 28 C1HA200381001 120030111A2611 SMOKE DETECTOR BOEING727 7272S7 138407ZNM A C1HAO OTHER N FALSE WARNING UKUNKNOWN 1 GL15681CA 22020 FWD LAV SMOKE DETECTOR WENT OFF WITH NO INDICATION OF SMOKEREMOVED AND REPLACED FWD LAV SMOKE DETECTOR AS REQ OPS CHECK GOOD 2L73 4F A3WE 20030128002642003012800264EA 2003 1 28 COMA0360052 120030127A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01931CA 7037 FLIGHT 5887 CABIN DOOR EMERGENCY WARNING.ADJUSTED DOOR LATCH MECHANISM. 2L72 4F RTA21EA 20030328000812003032800081 2003 3 28 COMA0360049 420030123A31706229820009 DCU CNDAIRCL600 CL6002B19 1900309EA AVIONICS FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01779CA13874 7306 FLIGHT 5560 SMOKE TOILET MESSAGE AFTER T/O. REPLACED THE NR 1 DCU. 2L72 4F RTA21EA 20030221000472003022100047EU 2003 2 21 AWXA200300074 120030125A5350 SEAL AIRBUS320 A320231 3930325EU WING/BODY FAIRINTORN A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 WP28621AW 053 ENROUTE A FLIGHT ATTENDANT NOTICED CONSIDERABLE VIBRATION DURING ENTIRE FLT BETWEEN ROWS 11-17. REPORTS INDICATE VIBRATIONS COULD BE FELT ABOVE AND BELOW 290 KTS. MAINTENANCE FOUND LT UPPER MID WING TO BODY FAIRING SEAL HAD OLD STYLE OF OF SEAL INSTALLED AND TORN ABOUT 3 INCHES. MAINTENANCE REMOVED AND REPLACED SEAL ON LT UPPER MID WING TO BODY FAIRING WITH NEW PER A320 SRM 51-42-21. ADDITIONALLY, MAINTENANCE FOUND HYD LINE FROM PTU TO MAIN GREEN MANIFOLD 90 DEGREE UNION GOING THROUGH WEB, NUT BACKED OFF AND EVIDENCE OF VIBRATING . MAINTENANCE TIGHTENED NUT AS REQUIRED AND SUBSEQUENT LEAK CHECK OF THE FITTING WAS FOUND GOOD. 2L72 4F RTA28NM 20030128002732003012800273EU 2003 1 28 AWXA200300084 120030107A5315D53112087203 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND FLOORBEAM AT FR 16, THIRD BEAM FROM OUTBOARD RT SIDE. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, PG. 213-219, FIG. 203, SHT 1 & 2. 2L72 4F RTA28NM 20030129000012003012900001SW 2003 1 29 HEEA083907 120030117A6320406360500101 OIL COOLER BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW034999 53323 MAIN ROTOR GEARBOX OIL COOLER LEAKING. 1G71 3U O H2SW 20030129000022003012900002SW 2003 1 29 HEEA083908 120030117A6320406360500101 OIL COOLER BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03494PH 53396 MAIN ROTOR OIL COOLER LEAKING. 1G71 3U O H2SW 20030114000402003011400040NM 2003 1 14 SWAA030029 120030106A53206546536 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND STUB BEAM WEB CRACKED AT BS 695, WL 206 AND RBL 62. REPAIRED STUB BEAM WEB PER SRM. 2L72 4F RTA16WE 20030114000432003011400043 2003 1 14 SWAA030036 420030106A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030114000442003011400044NM 2003 1 14 SWAA030038 120030107A53126545819139 WEB BOEING737 7373H4 1384600NM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED BC CHECK, FOUND NLG WHEEL WELL RT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20030114000612003011400061NM 2003 1 14 SWAA030011 120030104A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 556, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030114000662003011400066NM 2003 1 14 SWAA030016 120030104A78301U1225 VALVE BOEING737 7372H4 138448CNM LT ENGINE LEAKING A SWAAAD UNSCHED LANDING RETURN TO BLOCK K FLUID LOSS CLCLIMB 1 SW29103SW 23109 AIR TURNBACK, F/A REPORTED FLUID SMELL IN FWD CABIN. FOUND NR 1 ENGINE TR ISOLATION VALVE LEAKING. REMOVED AND REPLACED NR 1 ENGINE TR ISOLATION VALVE PER MM. 2L72 4F A16WE 20030114001192003011400119NM 2003 1 14 SWAA030018 120030103A1430 FASTENER BOEING737 7373H4 1384600NM ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED FASTENERS PER SRM. 2L72 4F RTA16WE 20030114002142003011400214NM 2003 1 14 VNAA0301008 120030108A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY EXIT OUT OF ADJUST A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07461PS 3075 EN ROUTE, THE CREW RECEIVED A 9A EMERGENCY DOOR LIGHT INDICATION ON THE RED WARNING PANEL. FLIGHT DESCENDED TO 9000 FEET AND THE LIGHT WENT OUT. MAINTENANCE INSPECTED, CLEANED, AND RESEATED THE DOOR AND PROXY SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030114002502003011400250EA 2003 1 14 COMA0360018 120030109A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01821CA 7420 FLIGHT 5794 FLAPS FAIL MESSGE WHEN SELECTED TO 30 DEGREES.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030114002552003011400255EA 2003 1 14 COMA0360023 120030111A2510010841301 SEAT BELT CNDAIRCL600 CL6002B19 1900309EA COPILOT SEAT BROKEN A COMAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO01963CA 7127 FLIGHT 5485 COPILOTS SEAT BELT BROKEN.REASSEMBLED CABLE FOR BELT LOCK. 2L72 4F RTA21EA 20030114002592003011400259EA 2003 1 14 COMA0360016 120030110A2740 COMPUTER CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01473CA 7668 FLIGHT 5804 STAB TRIM AND MACH TRIM CAUTION MESSAGES.RESET CIRCUIT BREAKS, FAULT CLEARED. 2L72 4F RTA21EA 20030114002632003011400263NM 2003 1 14 ZW0A0300602 120030113A33501317 LAMP BOEING757 757231 1384950NM A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13705TW 28479 ONE EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 5L AND ONE AT ROW 25R. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 12-6-02 MCI. --CLOSED--- 2L72 4F RTA2NM 20030115000372003011500037NM 2003 1 15 2003UALA00017 120030105A5313 WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 CABIN FLOOR STRUCTURE AT STATION 998 TO 1002 LBL 67 AT STRINGER 17L CREASE BEAM WEB CORRODED ON UPPER SURFACE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW WEB. 2L72 4F4 FRTA2NM E17NE 20030115000442003011500044EU 2003 1 15 010903 120030109A5240257PT1091A BRACKET HAWKERBAE125BAE125700B 7450007EU DOOR CRACKED E ESUAK NONE O OTHER ININSP/MAINT 1 CE03414RF10393 257060 A CRACK WAS FOUND IN A BRACKET THAT IS INSTALLED ON THE HELL HOLE DOOR DURING PREFLIGHT. THE CRACKED BRACKET WAS REMOVED AND REPLACE WITH A NEW BRACKET. 2L72 4F RTA3EU 20030115000722003011500072EA 2003 1 15 CA030104001 120030104A2820CC670621041 LINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUEL FEED CRACKED W A UNSCHED LANDING KFJFLUID LOSS FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 CA (CAN) IN CRUISE, CREW RECEIVED SEVERAL FUEL IMBALANCE MESSAGES THAT THE CREW WAS ABLE TO CORRECT, CENTER TANK FILED WITH FUEL VERY RAPIDLY. DISPATCH AND MOC CONCURRED WITH THE CREW TO LAND AT THE NEAREST AIRPORT. NO EMERGENCY WAS DECLARED BUT CFR DID ROLL DO TOO FUEL SPILLAGE. AC LANDED WITH 4800 POUNDS IN THE CENTER TANK AND FUEL WAS VENTING FROM THE OVERFILL VENTS. ON INVESTIGATION, IT IS REPORTED THAT A CRACK WAS FOUND ALONG THE WELDED AREA OF THE TRANSFER TUBE BOSS ON THE SUBJECT TUBE. THE AFFECTED FUEL TUBE WAS REPLACED. REPLACED THE WYE DUCTS (LT AND RT) DUE TO CHAFING AT THE FERRULE. RT ENGINE FEED LINE WAS ALSO REPLACED AS PRECAUTION. 2L72 4F4 FRTA21EA EOOO63EN 20030115000862003011500086NM 2003 1 15 0300046314 120030112A3397 WIRE BOEING747 747451 1384940NM CABIN DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01674US 30269 DURING LINE CHECK FOUND LEFT B ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REINSTALLED WIRE, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030115000882003011500088NM 2003 1 15 0300056627 120030113A3350 POWER SUPPLY BOEING747 747251B 1384892NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01627US 21709 DURING LINE CHECK FOUND C ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030115000912003011500091EU 2003 1 15 0301012 120030101A3230AIR131330 SPRING SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE RT MLG BROKEN A UHLAK NONE O OTHER ININSP/MAINT 1 NE03123CQ FLIGHT 4554, AFTER LANDING AND UPON POST FLIGHT WALK AROUND. THE CREW FOUND THE RIGHT OUTBOARD LANDING GEAR ASSISTER SPRING TO BE BROKEN AT THE GEAR LEG END. MECHANIC REMOVED AND REPLACED SPRING WITH A SERVICEABLE PART. THE NR 4 TIRE WAS AFFECTED WITH MULTIPLE DEEP CUTS TO THE TOP TREAD. MECHANIC REMOVED AND REPLACED THE NR 4 WHEEL WITH A SERVICEABLE PART. INSPECTION OF SURROUNDING AREA FOUND NO FURTHER DAMAGE. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030115000962003011500096SW 2003 1 15 ALGA082879 120030107A6320206040030003 BEARING BELL 206 206L1 1182107SW M/R GEARBOX SPALLED H ALGAK NONE O OTHER ININSP/MAINT 1 FS013194P 45788 DISASSEMBLED MAIN ROTOR GEARBOX FOR OVERHAUL AND FOUND TRIPLEX BEARING BREAKING DOWN. 1G71 3U H2SW 20030115000982003011500098NE 2003 1 15 0301041 320030104A6140 CONNECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE TRANSDUCER DIRTY A UHLAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 NE03148CQ 148 182 DRG189389 ON FINAL APPROACH, FLIGHT 4477 EXPERIENCED PROPELLER OIL FLUCTUATIONS FROM 0-60 PSI. INFLIGHT SHUTDOWN OF LEFT ENGINE PERFORMED. FLIGHT LANDED WITHOUT INCIDENT. MECHANIC CLEANED CONNECTOR PLUGS ON PRESSURE TRANSDUCER AND COCKPIT INDICATOR. OPERATIONAL CHECKS, GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030115001032003011500103WP 2003 1 15 03FDEA00002 120030103A3620831651 PRESSURE SWITCH DOUG DC10 DC1030 3023501WP GE CF6 CF6* 30020GL PNEUMATIC SYS FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25302FE 46801 ON TAKEOFF, WITH WING ANTI-ICE ON NR 1, PNEUMATIC FAIL LIGHT ILLUMINATED, RAN RED TABS IAW TAFI, FOUND PRESSURE SWITCH FAULT, LEFT WING. REPLACED MANIFOLD FAILURE DET PRESSURE SWITCH. OPERATIONS AND LEAK CHECK, GOOD IAW MM. 2L73 4F4 F A22WE E23EA 20030115001132003011500113EU 2003 1 15 BAQA082882 120030107A6410365A12002002 BLADE AEROSPSA365 SA365N 8680669EU TAIL ROTOR DEBONDED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM504 6396 TAIL ROTOR BLADE DEBONDING NEAR ROOT. EXCESSIVE PLAY IN SPOOL. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030115001182003011500118EU 2003 1 15 BAQA082899 120030108A6220117775P BALL JOINT AEROSPSA365 SA365N 8680669EU STARFLEX WORN H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911UF114 6338 BALL JOINT WORN. BEARING CAME OF ON STARFLEX IN THE POSITION OF THIS BALL JOINT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030115001252003011500125NM 2003 1 15 03FDEA00019 120030113A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT BORE NR 26L FOUND CORROSION ON BEARING SURFACE AND BORE REAMED BEYOND MAXIMUM OVERSIZE LIMIT IAW EO 1-5510-7-5000 AND SB MD11-55-023. 2L73 4F RTA22WE 20030115001552003011500155NE 2003 1 15 ERAA082938 120030103A242051530006B GCU SKRSKYS76 S76A 8143006NE AC SYSTEM INOPERATIVE H ERAAO OTHER HN ELECT. POWER LOSS-50 PC FALSE WARNING NRNOT REPORTED 1 FS01579EH 760274 GENERATOR WILL NOT COME ON LINE; BUSS TIE LIGHT NOT ILLUMINATED. Q7 SHORTED 3 OTHER UNITS FROM SAME SHIP HAVE SAME CONDITION. CHECKED WIRING ASSOCIATED WITH CAUTION LIGHT CIRCUIT AND BUSS TIE CIRCUITS FOR HELICOPTERS. TESTED & TROUBLESHOT AND REPLACED Q7. CALIBRATED AND BENCH TESTED IAW LEAR SIEGLER MANUAL. 1G72 3U H1NE 20030115001582003011500158SW 2003 1 15 ERAA082939 120030103A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01422EH14632 33068 MAIN ROTOR BLADE HAS CRACK IN LEADING EDGE AND FIBERGLASS. INSPECTED, PERFORMED 2500 HOUR INSPECTION, REPAIRED SKIN AT STA 131 TO STA 153 AND STA148 TO STA 152 ON LOWER SURFACE REPLACED OUTBOARD ABRASION STRIP. REPLACED INBOARD AND OUTBOARD SPLICE COVERS REPLACED POLY ROOT TAPE APPLIED HIGH VIS PER CUSTOMER REQUIREMENT; STATIC BALANCED. 1G72 4U H4SW 20030115001932003011500193GL 2003 1 15 ERAA082943 220030106A72606894171 GEARBOX BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE LEAKING A ERAAK NONE K FLUID LOSS ININSP/MAINT 1 AL03292EH3032 562 FOUND GEARBOPX SPLITLINE LEAKING. TWO STUDS NOT HOLDING TORQUE ON GEARBOX. RE-SEALED GEARBOX SPLIT LIND WITH EC776 GLUE. RE-SEATED TWO STUDS. 1G72 3U3 U H3EU E4CE 20030115001952003011500195EU 2003 1 15 0300063247 120030113A3350321431 BATTERY PACK AIRBUS320 A320212 3930322EU FWD LEFT FAILED A NWAAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01347NB 408 On take off EMERGENCY LIGHTS/CABIN circuit breaker popped and emergency lights came on. Returned to MSP and landed uneventfully. Reset circuit breaker. Emergency light system test gave FWD L BATT LOW message. Replaced battery pack at forward left power supply. Emergency light system test OK. Aircraft returned to service. 2L72 4F RTA28NM 20030115002082003011500208 2003 1 15 DL777030001 420030101A2330UNK MONITOR BOEING777 777232 1385232NM SEAT 30J UNSERVICEABLE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27864DA 29736 FRC-257-8930J PASSENGER SEAT 30J INSEAT VIDEO MONITOR INOP WONT TURN ON. REPLACED AVU AND LOADED SOFTWARE. CHECKS GOOD BUT VIDEO MONITOR IS INOP AND HAS A STRONG ELECTRICAL SMELL. REMOVED MONITOR. ALL MOUNTING HARWARE STILL PRESENT ON ARM. STOWED ARM AND LOCKED OUT. CONT ON MCO NEEDS MONITOR NIS ATL ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2L72 4F RTT00001SE 20030115002122003011500212NM 2003 1 15 DL733030032 120030107A5343654654322 FITTING BOEING737 737347 1384647NM FRAME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307WA 23440 THE RHS MLG SIDE STRUT SUPPORT FITTING HAD CORROSION IN THE BORE AND FORWARD AND AFT FACES OF THE FITTING AT FS 685, WL 188.5. THE BORE WAS OVERSIZED AND REPAIR BUSHINGS INTALLED. CORROSION WAS BLENDED FROM THE FACES. THE DAMAGE WAS FOUND AT HMV. 2L72 4F RTA16WE 20030115002132003011500213NE 2003 1 15 DLM88030044 220030110A7310320115DALFH VALVE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE #1 ENGINE INOPERATIVE A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27901DE 53378 725774 IRR- LEFT ENG FUEL HEAT VALVE INOP FLIGHT DIVERTED TO JAX UNABLE TO CONTINUE TO ORIGINAL DESTINATION. CORR.ACT.- REPLACED VALVE PER M/M ALTERNATE PART NBR USED 320115 2L72 4F4 FRTA6WE E9NE 20030129000042003012900004SW 2003 1 29 HEEA083914 120030117A6220407001524105 BELLCRANK BELL 407 407 1182206SW M/R HEAD DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 MAIN ROTOR HEAD BELLCRANK BUFFER WASHER, RUBBER DEBONDING. T 1G71 3U O H2SW 20030129000112003012900011SW 2003 1 29 HEEA083921 120030117A6720407001732101 BELLCRANK BELL 407 407 1182206SW T/R CONTROL WORN E O OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 TAIL ROTOR CONTROL BELLCRANK ASSY HAS A WORN BEARING. 1G71 3U O H2SW 20030129000132003012900013SW 2003 1 29 HEEA083923 120030117A6220 BEARING BELL 407 407 1182206SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH A282 53199 MAIN ROTOR HEAD ORANGE ARM SHEAR BEARING SEPARATED AND HAS A VIBRATION. REPAIRED. 1G71 3U O H2SW 20030129000152003012900015SW 2003 1 29 HEEA083925 120030117A6220 BEARING BELL 407 407 1182206SW M/R HEAD DELAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X A351 53267 MAIN ROTOR HEAD HAS A BAD FEATHERING BEARING, DELAMINATED. REPAIRED. 1G71 3U O H2SW 20030129000212003012900021SW 2003 1 29 HEEA083931 120030117A6220 SPRING BELL 407 407 1182206SW FRAHM ASSY CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH A714 53003 MAIN ROTOR HEAD FRAHM ASSY HAS A CRACKED SPRING. 1G71 3U O H2SW 20030129000252003012900025SW 2003 1 29 HEEA083935 120030117A6300407010201105 BEAM BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH1479 53283 BEAM ASSY HAS MECHANICAL DAMAGE. 1G71 3U O H2SW 20030129000352003012900035SW 2003 1 29 HEEA083948 120030117A6420407012101111 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR OUT OF BALANCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH3601 53207 UNABLE TO BALANCE TAIL ROTOR HEAD. REPAIRED. 1G71 3U O H2SW 20030129000382003012900038SW 2003 1 29 HEEA083951 120030117A6420 BEARING BELL 407 407 1182206SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53390 53288 FEATHERING BEARINGS WORN. REPAIRED. 1G71 3U O H2SW 20030129000452003012900045SW 2003 1 29 HEEA083958 120030117A3246407012204 SKID BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 MLG SKID CORRODED. 1G71 3U O H2SW 20030129000822003012900082SW 2003 1 29 HEEA083986 120030117A7810407062021101 DUCT BELL 407 407 1182206SW EXHAUST CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 EXHAUST DUCT CRACKED. 1G71 3U O H2SW 20030129000962003012900096SW 2003 1 29 HEEA083990 120030117A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20030129001082003012900108SW 2003 1 29 HEEA083995 120030117A5200407064807117 SUPPORT BELL 407 407 1182206SW ENG BAY DOOR DAMAGED E O OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 ENGINE BAY DOOR SUPPORT, THE HOLES FOR PIN ELONGATED. 1G71 3U O H2SW 20030129001112003012900111SW 2003 1 29 HEEA083996 120030117A5200407064807117 SUPPORT BELL 407 407 1182206SW ENG BAY DOOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 ENGINE BAY DOOR SUPPORT BRACE MOUNTING HOLE ELONGATED. 1G71 3U O H2SW 20030204002842003020400284NM 2003 2 4 F3LA200300016 120030120A5320 SUPPORT ANGLE BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED 5TH RIB BACK FROM FWD BULKHEAD IN LT SIDE OF AFT CARGO COMPARTMENT CORRODED. REMOVED AND REPLACED DAMAGED SIDEWALL SUPPORT ANGLE PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20030204002852003020400285NM 2003 2 4 F3LA200300017 120030121A5320 WEB BOEING737 7373M8 1384615NM FUSELAGE PUNCTURED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FLOOR WEB PUNCTURED AT STA 986.5 TO 1016. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-60-51, FIG 101. 2L72 4F RTA16WE 20030129001792003012900179NM 2003 1 29 UPS03240095 120030110A5310 SUPPORT BOEING727 72722C 138400FNM BS 850-870 RBL62CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI CORROSION ON SEAT TRACK SUPPORT BS 850 - 870 RBL 62.5 SUPPORT REPLACED IAW SRM 51-30-02 2L73 4F A3WE 20030129001812003012900181NM 2003 1 29 UPS03240097 120030103A5755 HINGE BOEING727 72722C 138400FNM #13 SPOILER PANECRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI #13 SPOILER PANEL I/B HINGE CRACKED REMOVED #13 SPOILER PANEL IAW MM 27-61-01 . REPLACED I/B HINGE IAW O HM 57-53-01 REPLACED I/B CENTER SPOILER HINGE BEARING DUE TO WEAR IA W OHM 57-53-01 PG 402. INSTALLED #13 PANEL IAW MM 27-61-01 2L73 4F A3WE 20030129002192003012900219SO 2003 1 29 LR7A03004 120030124A5312 SKIN LKHEED382 382G 526414USO FS 478 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 489 4698 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB3202 FOUND RMLG BAY SIDEWALL SKIN CRACKED .25 IN. AT FS 478, RBL 61, WL 170.REPLACED SKIN PANEL FS 477 TO 517 AND WL 150 IAW SRM SMP 583 53-40-02 AND DWG 34203. NR 0096. 2H74 4T A1SO 20030410002462003041000246NM 2003 4 10 F3LA200300028 120030125A5320 FLOOR SUPPORT BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT LBL 8.10 CORRODED AT NUMEROUS LOCATIONS FROM AFT BULKHEAD TO FWD BULKHEAD, BOTH TOP AND BOTTOM. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-20-53, 51-40-02, 53-00-53 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030130000752003013000075NM 2003 1 30 P5CA0300729 120030119A5411NONE FRAME BOEING747 7472U3B 1384846NM #4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CRACK FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD FRAME ASSY BELOW NAC WL 167.0 ON L/H FWD, R/H FWD & AFT AT FASTENER HOLE. REPLACEMENT OF CRACKED FRAME ASSY CARRIED OUT AS PER SRM 51-10-01 2L74 4F RTA20WE 20030130000762003013000076NM 2003 1 30 P5CA0300730 120030120A5412NONE SUPPORT ANGLE BOEING747 7472U3B 1384846NM #4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CRACK APPROX. 2-3/4" FOUND #4 PYLON AFT ENG. BULKHEAD FRAME AT NAC STA 221.90 MID SPARE WEB LWR LATERAL SUPPORT ANGLE AT MID SECTION & JOINTING 3 FASTENERS. REPLACEMENT OF CRACKED LATERAL SUPPORT ANGLE CARRIED OUT PER SRM 51-10-01. 2L74 4F RTA20WE 20030130000802003013000080NM 2003 1 30 P5CA0300735 120030123A5411NONE FRAME BOEING747 7472U3B 1384846NM #1 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CRACK FOUND #1 PYLON REAR ENG. MOUNT BULKHEAD L/H FWD FRAME APPROX. 1/2" FROM TOP RADIUS. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3. 2L74 4F RTA20WE 20030130000822003013000082NM 2003 1 30 P5CA0300737 120030123A5411NONE FRAME BOEING747 7472U3B 1384846NM #3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CRACK 1-1/2" FOUND #3 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FWD FRAME REAPIR ANGLE, STARTING FROM TOP EDGE RADIUS. FRAME REPAIR ANGLE REPLACED PER SRM 54-10-03 & FAA FORM 8110-3. 2L74 4F RTA20WE 20030130001592003013000159NM 2003 1 30 F3LA200300008 120030117A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED TOP SURFACE OF I-BEAM AT STA 986.5 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-51, FIG 101. REMOVED DAMAGED UPPER CAP OF FLOORBEAM PER SRM 53-00-51, FIG 202. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-51, FIG 202 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030410002482003041000248NM 2003 4 10 F3LA200300031 120030127A5320 STRAP BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK INSPECTION REPORTED AFT STRAP IN AFT CARGO COMPARTMENT, RBL 20, INBOARD OF DOOR SILL WEB CORRODED FROM FWD TO AFT. REPLACED STRAP AND BOTH LOWER FILLERS PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20030131000722003013100072SO 2003 1 31 C2XA03TY013 120030131A33501317 BULB EMB 145 EMB145LR 3260212SO CABIN BLOWN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716919 145393 TYS, During a scheduled inspection the first aisle emergency light was found inoperative. Maintenance removed and replaced the bulb. operiational checked good, aircraft released to service. 2L72 4T RTT00011AT 20030131000732003013100073SO 2003 1 31 C2XA03TY014 120030131A533014521725615 SILL EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 TYS, During a scheduled inspection the service door aft sill was found corroded. Maintenance removed and replaced the sill I/A/W-EMB-SRM-51-40-02. Aircraft will be released to service upon complection of inspection. 2L72 4T RTT00011AT 20030131000812003013100081SO 2003 1 31 C2XA03TY016 120030131A553014520736003 HOUSING EMB 145 EMB145LR 3260212SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 TYS, During a scheduled inspection the right vertical stab spherical bearing housing support has internal gouges at 1 and 8 oclock position. Maintenance reamed the hole and installed a bushing I/A/W-EMB-EC5510-01049. Aircraft will be released to service upon complection of inspection. 2L72 4T RTT00011AT 20030131001062003013100106CE 2003 1 31 CA030107003 120030103A5740901100351 FITTING BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA WING SPAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A ROUTINE INSPECTION, AME NOTICED AN OILY STREAK ON THE FITTING. AFTER CLEANING, IT APPEARED TO BE A DEEP SCRATCH. THE AREA WAS CLEANED WITH SOLVENT AND REEXAMINED, WHICH LOOKED LIKE A CRACK. AN NDT. (LIQUID PENETRANT) WAS PERFORMED TO CONFIRM THE CRACK. IT WAS ESTABLISHED THAT IT WAS A CRACK.A FLEET-WIDE INSPECTION WAS PERFORMED ON ALL FITTINGS. NO DEFECTS WERE FOUND. THE MANUFACTURER WAS INFORMED AND PROBLEM WAS DISCUSSED AT LENGTH. AWAITING PARTS FOR REPLACEMENT. 1L72 3T4 TRT3A20 E4EA 20030131001322003013100132SO 2003 1 31 C2XA03BT018 120030128A3230GS02550C BLOCK EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2713553 145585 EWR---CO2297, CREW REPORTED, "ON CLIMB AFTER TAKEOFF, WE GOT A LANDING GEAR DISAGREEMENT MESSAGE ON EICAS MESSAGE WITH LANDING GEAR INDICATION SHOWING UP IN RED. GEAR WAS UP AND CAME DOWN NORMALLY WITH THE LANDING GEAR LEVER." MAINTENANCE FOUND BAD GROUND TO PINS 1,5,9,AND 10 AT LANDING GEAR LEVER GROUND BLOCK. REMOVED AND REPLACED LANDING GEAR LEVER GROUND TERMINAL BLOCK IAW EMB145 MM #20-13-05 AND EMB145 WM #32-33-50. OPS.CHECKED OF LANDING GEAR IAW EMB145 MM #32-30-00. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030116000032003011600003EU 2003 1 16 BAQA082903 120030108A651010531803 ROTOR SHAFT BOLKMS117 BK117B1 5626012EU TAIL ROTOR BENT H BAQAK NONE O OTHER ININSP/MAINT 1 FS01945ME5943 7235 TAIL ROTOR SHAFT BENT. WILL NOT BALANCE ON AIRCRAFT. BUSHING MISSING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030116000112003011600011 2003 1 16 HEEA082968 420030107A34142002011293 INDICATOR SKRSKYS76 S76A 8143006NE AIRSPEED INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03476X 760436 INDICATES 77 KNOTS WHEN CALIBRATED PITOT-STATIC TEST SET INDICATES 70 KNOTS. INDICATES 7 KNOTS FASTER THAN COPILOT AIRSPEED INDICATOR. REPLACED WITH SERVICEABLE INDICATOR. 1G72 3U H1NE 20030116000192003011600019 2003 1 16 HEEA082976 420030107A31407007700614 INDICATOR SKRSKYS76 S76A 8143006NE ECAS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 ECAS DISPLAY SCREEN SHRINKS IN FLIGHT. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030116000202003011600020NE 2003 1 16 HEEA082977 120030107A6220 BEARING SKRSKYS76 S76A 8143006NE M/R DAMPER LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ A06101870 760231 MAIN ROTOR DAMPER BEARING LOOSE IN ROD END BORE. REPAIRED. 1G72 3U H1NE 20030116000212003011600021NE 2003 1 16 HEEA082978 120030107A30207630407900112 HEATER SKRSKYS76 S76A 8143006NE FIREWALL INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 FIREWALL HEATER IS INOPERATIVE DUE TO ONE TEMP SENSOR SHOWING AN OPEN LEAD CONDITION. 1G72 3U H1NE 20030116000282003011600028 2003 1 16 HEEA082985 420030107A23709806020023 CVR SKRSKYS76 S76A 8143006NE COCKPIT FAULTY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 COCKPIT VOICE RECORDER TEST LIGHT FLASHES ON CONTINUOSLY. 1G72 3U H1NE 20030116000332003011600033GL 2003 1 16 HEEA082991 220030109A725023053299 TURBINE WHEEL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P1986 51530 CAE895174 ENGINE REMOVED DUE TO TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION ON ALL 1ST STAGE TURBINE WHEEL BLADES. SCRAPPED WHEEL. 1G71 3U3 U H2SW E1GL 20030116000392003011600039SW 2003 1 16 HEEA082998 120030106A7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0354641 51184 UNABLE TO COMMUNICATE TO COMPUTER. 1G71 3U H2SW 20030116000402003011600040SW 2003 1 16 HEEA082999 120030106A7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 COMPUTER INCORRECTLY RECORDED OVER TORQUE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116000422003011600042SW 2003 1 16 HEEA083001 120030106A7797DPUK0414 WIRE HARNESS BELL 206 206L4 1182110SW INTELASTART COMPFAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0362127 52023 PROCESSOR HAD ENGINE TORQUE FAULT. TROUBLESHOT WIRING IN AIRCRAFT, FOUND SPLICE AT J3 BAD, CAUSE FUSE TO BLOW. INSTALLED SOLDER SLEEVE ON SHIELDED WIRES AND REPINNED CONNECTOR. 1G71 3U NCH2SW 20030116000462003011600046 2003 1 16 HEEA083005 420030106A2562ELT10 ELT BELL 206 206L3 1182108SW CABIN WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03205FC 51130 ELT WOULD NOT TEST ON MONTHLY INSPECTION. 1G71 3U H2SW 20030116000502003011600050SW 2003 1 16 HEEA083009 120030106A2140ES392501 CONTROL CABLE BELL 206 206L3 1182108SW DEFROST HEATER BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 FLEX CABLE FOR DEFROST HEATER VALVE BROKEN. SCRAPPED. 1G71 3U H2SW 20030116000622003011600062SW 2003 1 16 HEEA083021 120030106A6320PHI206052 MAGNETIC SEAL BELL 206 206B3 1181506SW ROTOR HEAD LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032275Y 3626 MAIN ROTOR MAGNETIC SEAL LEAKING. REPLACED WITH SERVICEABLE SEAL. 1G71 3U H2SW 20030116000682003011600068SW 2003 1 16 HEEA083028 120030106A5520PHI206L17001 BUSHING BELL 206 206L3 1182108SW ELEVATOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 PLASTIC BUSHING WORN IN RIGHT HAND ELEVATOR. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116000712003011600071SW 2003 1 16 HEEA083031 120030106A7714SC628 WARNING SYSTEM BELL 206 206B3 1181506SW LOW ROTOR INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 LOW ROTOR ALARM INTERMITTENTLY INOPERATIVE. SCRAPPED. 1G71 3U H2SW 20030116000752003011600075SW 2003 1 16 HEEA083035 120030106A2430SM20ACD200A21 RELAY BELL 206 206L1 1182107SW DC SYSTEM STUCK E O OTHER O OTHER NRNOT REPORTED 1 SW035007Q 45187 BATTERY RELAY STICKING. 1G71 3U H2SW 20030116000852003011600085 2003 1 16 HEEA083045 420030106A2312064101902 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0320898 45721 TRANSCEIVER RECEIVES WEAK AND BROKEN. FOUND RECEIVER AUDIO CUTTING OUT INTERMITTENTLY. REPLACED BAD C147 CAPACITOR. REPAIRED. FOUND MODULATION DISTORTED. REPLACED C609 AND C607 CAPACITORS. REPAIRED MODULATION BUT POWER OUT WAS WEAK AT 118 MHZ. REPLACED R181 RESISTOR. REPAIRED. FOUND KHZ KNOB INTERMITTENTLY SWITCHING TO PRESET CHANNELS WHEN TURNED. CLEANED SW102 SWITCH. REPAIRED. ADJUSTED CARRIER SQUELCH, MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20030116000922003011600092CE 2003 1 16 046605 120030109A6120 SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA COCKPIT OUT OF ADJUST A AMWAK NONE O OTHER APAPPROACH 1 CE0710675 10675 UPON APPROACH ON FLIGHT 5490, THE AUTOFEATHER SWITCH ARMED ANNUNCIATOR FAILED TO ILLUMINATE. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE PEDESTAL SWITCHES. NO PARTS WERE USED. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T3 TRTA24CE E4EA 20030116001022003011600102 2003 1 16 HEEA083055 420030107A34570110005400 GPS BELL 206 206B3 1181506SW COCKPIT DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03103PH 3000 GPS INTERNAL BATTERY WEAK. 1G71 3U H2SW 20030116001032003011600103 2003 1 16 HEEA083056 420030107A34570110005400 GPS BELL 206 206L4 1182110SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 GPS ENTER BUTTON IS INTERMITTENT. 1G71 3U NCH2SW 20030116001072003011600107 2003 1 16 HEEA083059 420030107A233002000002 AMPLIFIER BELL 206 206L3 1182108SW ENTERTAIN SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 ENTERTAINMENT SYSTEM AMPLIFIER IS BLOWING FUSES. FOUND Q7, Q8 TRANSISTORS BAD. REPLACED AND REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001122003011600112 2003 1 16 HEEA083062 420030107A2312064101900 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 TRANSCEIVER LOSES PROGRAMMING FREQUENCY OVERNIGHT. REPLACED I112 MEMORY CHIP TO REPAIR. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001172003011600117 2003 1 16 HEEA083066 420030107A2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610C 51425 VHF TRANSCEIVER IS INOPERATIVE. POWER OUT WAS ABOUT 2 WATTS LOW. REPLACED C623 AND C624 ON TRANSMIT BOARD. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001322003011600132 2003 1 16 HEEA083077 420030108A2312064105430 TRANSCEIVER BELL 206 206B3 1181506SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03103PH 3000 VHF TRANSCEIVER BREAKS SQUELCH INTERMITTENTLY. REPLACED LENS ON FACEPLATE. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001342003011600134 2003 1 16 HEEA083079 420030108A3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 RADAR ALTIMETER INOPERATIVE. SHOP REPAIR. 1G71 3U H2SW 20030116001472003011600147 2003 1 16 HEEA083091 420030108A2312069102405 TRANSCEIVER KX155 BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 COMM RADIO DIGITAL READOUT INOPERATIVE. IN SHOP REPAIR. 1G71 3U H2SW 20030116001762003011600176SO 2003 1 16 C2XA02SH172 120030104A531313500400019 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715912 145439 SHV- DURING C-CHECK T REINFORCEMENT AT STRINGER 19R WAS FOUND CHAFFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116001882003011600188 2003 1 16 HEEA083099 420030108A345713824120234 RECEIVER BELL 206 206L3 1182108SW GPS ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036161A 51611 GPS RECEIVER DIRECT BUTTON ERRATIC. DIRECT BUTTON, WPT, APT/VOR AND MSG BUTTONS ERRATIC. ALSO FOUND DISPLAY NOT DIMMING AND BUTTONS UNREADABLE. REPLACED SAME. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001892003011600189 2003 1 16 HEEA083100 420030108A345713824120234 RECEIVER BELL 206 206L1 1182107SW GPS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035014Y 45219 GPS HAS DIM DISPLAY. FOUND FILTER BAD AND REPLACED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001902003011600190 2003 1 16 HEEA083101 420030108A345713824120234 RECEIVER BELL 206 206L3 1182108SW GPS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034282Z 51499 GPS LOSES DATA. FOUND UNIT WOULD NOT PASS GPS TEST. 1G71 3U H2SW 20030131001472003013100147SO 2003 1 31 C2XA03BT023 120030128A3350110049 BATTERY PACK EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2714568 145628 EWR---CO2561, CREW REPORTED, RIGHTHAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK CHARGER IAW EMB145 AMM 33-50-04. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20030131001712003013100171NM 2003 1 31 UPS03240107 120030130A5330 SKIN BOEING727 72722C 138400FNM BS360 I/B STR.4 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C+SI 5 MM CRACK FOUND PROPAGATING FROM THE SIXTH FASTENER I/B OF STR.4 R AT BS360 AFT SKIN AFT FASTENER ROW. FASTENERS REMOVED IAW SRM 51-30-02. CRACK TRIMED OUT IAW SRM 51-10-06 REPAIR CARRIED IAW EO.B727-5310-1371+DRG.NO.69-62161. 2L73 4F A3WE 20030131001912003013100191NM 2003 1 31 P5CA0300741 120030126A5320NONE BRACKET BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACKS FOUND ON 2 BRACKETS AT FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1800-1920, "LOWER LOBE AFT CARGO". CRACKED BRACKETS REMOVED. NEW FABRICATED HF 7075T651 PER SRM 53-11-25 & PER SAMPLE. PROTECTED W/ ANODIZE PER SRM 51-10-02. FASTENER INSTL PER SRM 51-30-02. 2L74 4F A20WE 20030131001922003013100192NM 2003 1 31 P5CA0300742 120030126A5320NONE CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND ON CLIP AT FRAME STA 500/R AT CONNECTION TO STR 10-10A-11A-12. UPPER DECK SIDEWALL PANEL. NEW CLIP FABRICATED PER SRM 53-10-20 & SRM 51-40-03, FIG. 4. PROTECTED PER SRM 51-10-02, RIVETS PER SRM 51-30-02. 2L74 4F A20WE 20030131001932003013100193NM 2003 1 31 P5CA0300747 120030128A5753NONE FLAP BOEING747 747200 1384847NM R/H WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 CRACK, 1" LONG, IN O/B AFT FLAP, INBD SIDE, 4" FROM AFT EDGE. REPAIR CARRIED OUT IAW SRM 51-40-14, FIG. 10. 2L74 4F RTA20WE 20030201000022003020100002SO 2003 2 1 C2XA02SH185 120030201A531313500400013 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAO OTHER K FLUID LOSS ININSP/MAINT 1 SW2713913 145438 SHV DURING C CHECK GOUGE WAS FOUND ON STRINGER 19L ON T REINFORCEMENT AT FRAME 52. MAINTENANCE REMOVED AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030201000042003020100004SO 2003 2 1 C2XA02SH188 120030201A531214547494003 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713913 145438 SHV- DURING C CHECK APU FIREWALL CRACKED AT TOP RIVET OF RIGHT HAND VERTICAL REINFORCEMENT. MAINTENANCE REMOVED DAMAGE AND REPAIRED CRACK IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030203000202003020300020WP 2003 2 3 CA030113004 120030109A29101564213139 TUBE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) HYDRAULIC LEAK RT SIDE FLAP WELL NEAR NR 1 SPOILER ACTUATOR. SPOILER NR 1 PRESSURE HYDRAULIC TUBE, SYSTEM B REPAIRED PER AMM 20-29-02, P801. 2L73 4F4 F A23WE E12EU 20030203000722003020300072 2003 2 3 MEX2003003 420030105A3416 INDICATOR DOUG DC9 DC982 3022082WP COCKPIT FAILED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW23491SH 49150 AIRCRAFT RETURNED TO PLATFORM DUE TO FIRST OFFICER ALTIMETER OFF FLAG. ALTIMETER WAS RESET BUT FLAG CONTINUES. BOTH CADCS WERE INTERCHANGED, TESTS WERE PERFORMED IAW MM. AFTER TESTS, 130 FT DIFFERENCE BETWEEN ALTIMETERS APPEARS. PNEUMATIC CONNECTIONS WERE DRAINED AND CLEANED, ALL OPERATED IN A CORRECT WAY. 2L72 4F A6WE 20030203001062003020300106NM 2003 2 3 PCAA0302031 120030102A56107802 WINDSHIELD DHAV DHC8 DHC8102 2809003NM LEFT CRACKED A PCAAO OTHER Z SIGNIFICANT FAILURE REPORT CRCRUISE 1 EA13814EX8521 318 BGM-PIT FLIGHT#3568. CREW REPORTED THAT THE CAPTAINS WINDSHIELD HAD CRACKED DURING FLIGHT. EMERGENCY WAS DECLARD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CAPTAINS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. AIRCRAFT WAS GROUND RAN, OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030203001502003020300150CE 2003 2 3 AWK2003F00000 120030103A2820583801091 SELECTOR VALVE BEECH 58 58 1152740CE CONT O550 IO550* SO FUEL SYSTEM LEAKING B AWKRK NONE K FLUID LOSS ININSP/MAINT 1 WP25729F 39 TH2020 ON WALK AROUND INSPECTION FOUND FUEL STAINING ON LEFT INBOARD LANDING GEAR DOOR RUNNING DOWN TO WINGROOT. FUTHER INSPECTION REVEALED LEFT WING FUEL SELECTOR LEAKING FUEL. REPLACED WITH NEW. 1L72 3O3 O 3A16 E3SO 20030203001702003020300170WP 2003 2 3 DHL2003803002 120030131A2611 LAMP DOUG DC8 DC873 302199CWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01803DH 46123 1) DURING PREFLIGHT #7 SMOKE DETECTOR WOULD NOT TEST.2) RELAMPED SMOKE DECTETOR OPS CK GOOD PER MM 26-10-0. 2L74 4F RT4A25 20030203001722003020300172CE 2003 2 3 FFS2003F00009 120030113A5530EWB22514 BOLT BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE VERT STABILIZER UNDERTORQUED A FFSAK NONE O OTHER ININSP/MAINT 1 AL01575D 20267 UE24 WHILE PERFORMING AN INSPECTION OF THE TAIL SECTION, THE UPPER FOUR ATTACH BOLTS FOR THE VERTICAL STABILIZER FORWARD SPAR WERE SMOKING AND THE WASHERS WERE LOOSE UNDER THE RT SIDE BOLT HEADS. ALL FOUR BOLTS WERE BELOW MINIMUM TORQUE SPECS. 2L72 4T4 TRTA24CE E26NE 20030203001842003020300184SW 2003 2 3 GLR2003F00000 120030103A7810 CLAMP GULSTM112 112TC 7630306SW LYC O360 TO360C1A6 41514EA NR 3 EXHAUST WRONG PART A GLRSK NONE W INADEQUATE Q C ININSP/MAINT 1 NM0949AB 259 13066 L21269A EXHAUST SLIP JOINT SEIZED AFTER COMPLIANCE WITH SB, CAUSING BUCKLING OF NR 3 STACK. WRONG CLAMP WAS PROVIDED BY MFG AND FIT ONLY ON THE SLIP JOINT. SHOWED CLAMP ON SLIP JOINT AND MAY HAVE CAUSED SEIZING AND BUCKLING. 1L71 3O3 O A12SO E26EA 20030203001982003020300198CE 2003 2 3 GUU2003F00003 120030110A32404500SA1 VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA PARKING BRAKE LOCKED A GUUAO OTHER O OTHER TXTAXI/GRND HDL 1 SO1781556 UE239 DURING TAXI, BRAKES STUCK. REMOVED AND REPLACED PARKING BRAKE VALVES. OPERATIONAL CHECK GOOD. 2L72 4T3 TRTA24CE E2NE 20030203002342003020300234EA 2003 2 3 COMA0360065 120030130A5320 SUPPORT BRACKET CNDAIRCL600 CL6002B19 1900309EA A COMAK NONE O OTHER ININSP/MAINT 1 SO01989CA 7215 THE PREVIOUS REPAIR AT THE R/H SIDE FS 621, WL73.5 BETWEEN RBL36 AND RBL42 UNDER FLOOR SUPPORT STRUCTURE WAS CRACKED.REMOVED THE CRACKED PREVIOUS REPAIR PARTS AND INSTALLED NEW REPAIR PARTS I/A/W REO 601R-53-61-004 REV B 2L72 4F RTA21EA 20030204000112003020400011NM 2003 2 4 LI32003F00001 120030121A49304950084 MANIFOLD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE APU FUEL BROKEN B LI3RO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP09338UA 24242 FUEL LEAK APU AUTO SHUTDOWN. APU DEFERRED. C/B PULLED. FOUND LEAK AT FUEL HEATER. HEATER NOT LEAKING. MAIN FUEL MANIFOLD CRACKED AT 11:00 O`CLOCK POSITION AT FUEL NOZZLE (INJECTOR) MANIFOLD HAS 14 FUEL TUBES. ONE HAS A BROKEN TUBE BETWEEN THE FLEXIBLE FIRE SLEEVE AND THE B-NUT TO THE FUEL INJECTOR. PART SENT TO LAB FOR ANALYSIS. 2L72 4F4 FRTA16WE E2GL 20030204000292003020400029NM 2003 2 4 SWAA030186 120030124A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000302003020400030NM 2003 2 4 SWAA030187 120030123A53116546536 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, WL 209 & RBL 70. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030204000322003020400032NM 2003 2 4 SWAA030189 120030126A3220162A31083 CONTROL ROD BOEING737 7377H4 1384404NM NLG W/W WORN A SWAAAD UNSCHED LANDING RETURN TO BLOCK EP VIBRATION/BUFFET NO WARNING INDICATION CLCLIMB 1 SW29715SW 27849 AIR TURNBACK, DECLARED EMERGENCY, DURING DEPARTURE LOUD POP AND EXCESS VIBRATION NOTED FROM NLG AREA, CYCLED GEAR NORMALLY. REMOVED AND REPLACED LT NLG DOOR CONTROL ROD PER MM. 2L72 4F RTA16WE 20030204000342003020400034NM 2003 2 4 SWAA030225 120030129A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 490, RBL 11. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000412003020400041 2003 2 4 SWAA030212 420030129A256565C19901 CABLE BOEING737 7372H4 138448CNM L1 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030204000422003020400042NM 2003 2 4 SWAA030213 120030129A53156545410 BEAM BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 716 - BS 706, BBL 0, WL 208. REPAIRED BEAM PER SRM AND BFG ER. 2L72 4F RTA16WE 20030204000452003020400045NM 2003 2 4 SWAA030216 120030129A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED, BS 294, RBL 55, WL 208 -211. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030204000462003020400046NM 2003 2 4 SWAA030217 120030128A5710115A81618 FRAME BOEING737 7377H4 1384404NM LT WING T/E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29719SW 27853 DURING SCHEDULED 5Y CHECK, FOUND LT WING T/E SUPPORT FRAME CRACKED, WBL 413.18. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20030204000472003020400047NM 2003 2 4 SWAA030218 120030129A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM RT ELEV WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 DURING SCHEDULED SERVICE CHECK, (SI 11038-55), RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 3 AND NR 4 HINGE BUSHINGS PER MM. 2L72 4F RTA16WE 20030204000532003020400053NM 2003 2 4 SWAA030203 120030128A53116545871 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 STOP FITTING. REPAIRED DOOR FRAME PER SWA T1. 2L72 4F RTA16WE 20030204000632003020400063NM 2003 2 4 SWAA030175 120030123A3211654611320 PIN BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED C3 CHECK, FOUND LT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED TRUNION PIN PER MM. 2L72 4F RTA16WE 20030204000642003020400064 2003 2 4 SWAA030176 420030123A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2L72 4F RTA16WE 20030204000782003020400078NM 2003 2 4 SWAA030165 120030122A3211656337823 LINK BOEING737 7373H4 1384600NM RH MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED C1 CHECK, FOUND RT MLG TRUNION LINK CORRODED. REMOVED AND REPLACED TRUNION LINK PER MM. 2L72 4F RTA16WE 20030204000802003020400080NM 2003 2 4 SWAA030132 120030117A57536546435 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBD AFT T/E FLAP DELAMINATED AT LOWER SKIN. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000812003020400081NM 2003 2 4 SWAA030138 120030120A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAMS UPPER SURFACE AT BS 312, LBL 10, AND UPPER AND LOWER SURFACE AT BS 328, RBL 9 - RBL 58. REPAIRED CORRODED SECTION OF FLOORBEAMS PER SRM. 2L72 4F RTA16WE 20030204000842003020400084NM 2003 2 4 SWAA030142 120030117A3350079123 COVER BOEING737 7377H4 1384404NM CABIN FLOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 EEPLS COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20030204000932003020400093NM 2003 2 4 SWAA030152 120030121A2560PL2230LH00 STRIP BOEING737 7375H4 138449DNM CABIN FLOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 11 DEF. SECURED STRIP PER MM. 2L72 4F RTA16WE 20030204000942003020400094NM 2003 2 4 SWAA030108 120030117A531365C27314 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND CORROSION ON SHEAR TIE BS 360 STR 18R AND STR 28L. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20030204000962003020400096NM 2003 2 4 SWAA030115 120030117A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D STR 10L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000972003020400097NM 2003 2 4 SWAA030116 120030117A53116516323 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SPV CHECK, FOUND CRACK AT MAIN FRAME BS 360 BETWEEN STR 14R AND STR 15R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030204000992003020400099NM 2003 2 4 SWAA030123 120030119A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 188 STR 17R. REMOVED AND REPLACED CRACKED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20030204001022003020400102NM 2003 2 4 SWAA030096 120030116A532065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, BS 663, STRINGERS 9L AND 9R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030204001082003020400108NM 2003 2 4 SWAA030085 120030115A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK 4 INCHES LONG AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204001352003020400135EU 2003 2 4 VJ32003F00018 120030105A2750120A4283 MOTOR GROB 120 G120A 1660208EU TE FLAPS NOISY B VJ3RA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP07862AF 85002 DURING FLIGHT, FLIGHT CREW HEAR LOUD NOISE FROM CARGO AREA WHILE USING FLAPS. MAINTENANCE TROUBLESHOOT AND FOUND THAT THE MOTOR OF THE FLAP UNIT WAS EXTREMELY NOISY. REPLACE FLAP MOTOR UNIT AND NOISE WHEN AWAY. EXPECT THAT BEARING IN UNIT ARE DRY OR INTERNAL GEARS WEARING. RECOMMENDATION AT TIME THIS IS TO CHECK MANUFACTURE PROCESS. 1L71 3O RTA49CE 20030204001632003020400163WP 2003 2 4 MWEA030045 120030107A3242500432114 BRAKE DOUG DC9 DC981 3022081WP MLG WORN A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31803ME 48029 FLIGHT ATTENDANTS IN REAR HEARD METAL ON METAL AND SCRAPING NOISE. REMOVED AND REPLACED NR 3 MAIN LANDING BRAKE, WHEEL AND TIRE ASSEMBLY. 2L72 4F A6WE 20030204001672003020400167 2003 2 4 SWAA030092 420030115A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. REPOSITIONED ESCAPE SLIDE PER M/M. 2L72 4F A16WE 20030204001762003020400176NE 2003 2 4 011703N792MA 220030117A732132447593 FUEL CONTROL CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE ENGINE MALFUNCTIONED G FGPAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA01792MA1028566 5500302 70728 THE AIRCRAFT ENCOUNTERED SEVER TURBULENCE, AT WHICH TIME THE ENGINE WENT TO 38 PERCENT N1/MIN FLOW. UPON REMOVAL OF FUEL CONTROL, IT WAS NOTED THAT IT RATTLED. FUEL CONTROL TO BE INSPECTED BY MFG. 1L72 4F4 F A22CE E1NE 20030204001772003020400177 2003 2 4 SWAA030103 420030116A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED C1 CHECK, FOUND THE R1 DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED THE R1 DOOR ESCAPE SLIDE PER M/M. 2L72 4F RTA16WE 20030116001972003011600197GL 2003 1 16 HEEA083109 220030108A7261174000101 FILTER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE OIL DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 FILTER ASSY BYPASS BUTTON REMAINS PARTIALLY EXTENDED AT ALL TIMES. TO BE SENT TO VENDOR. 1G71 3U3 U H2SW E1GL 20030116001982003011600198SW 2003 1 16 HEEA083110 120030108A28222C271 CARTRIDGE BELL 206 206L3 1182108SW FUEL SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 FUEL PUMP CARTRIDGE INOPERATIVE. 1G71 3U H2SW 20030105000022003010500002SO 2003 1 5 C2XA03IA002 120030104A5610163500109 WINDSHIELD EMB 135 EMB135LR 3260305SO COCKPIT CRACKED A C2XAO OTHER O OTHER DEDESCENT 1 SW2728518 145334 IAH- DURING DESCENT THE CREW NOTED THAT THE PILOTS WINDSHIELD CRACKED, EMERGENCY WAS DECLAIRED, AND, THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED, and, REPLACED THE CAPTAIN'S WINDSHIELD, PERFORMED A OPERATI9ONAL CHECK,and, LEAK CHECK, NO DEFECTS NOTED, and, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030106000892003010600089EU 2003 1 6 MALA030103 120030104A33506013211 POWER SUPPLY SAAB SF340 SF340A 7850100EU A MALAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 GL1589XJ 340A089 DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS 7LN, 31LN, 25LN, 35LN, AND 51LN INOP. MAINTENANCE REPLACED POWER SUPPLY PN ON/OFF 60-1321-1, INSTALLED BATTERY PN 61-0478-9. OPS CHECK GOOD. 2L72 4T RTA52EU 20030106001572003010600157NE 2003 1 6 HEEA082808 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 ROTOR BRAKE WON'T ENGAGE. 1G72 3U H1NE 20030106001622003010600162NE 2003 1 6 HEEA082813 120030102A63217665009803103 POWERPACK SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROTOR BRAKE WILL NOT STOP MOTORING. 1G72 3U H1NE 20030106001632003010600163NE 2003 1 6 HEEA082814 120030102A63217665009803103 POWERPACK SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROTOR BRAKE POWERPACK KEEPS CYCLING. 1G72 3U H1NE 20030106001652003010600165NE 2003 1 6 HEEA082816 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K 760082 ROTOR BRAKE PUMP MOTORS WITH NO PRESSURE. 1G72 3U H1NE 20030106001662003010600166NE 2003 1 6 HEEA082817 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K 760082 ROTOR BRAKE LIGHT WILL NOT GO OUT. LOW PRESSURE SWITCH BAD. 1G72 3U H1NE 20030106001682003010600168NE 2003 1 6 HEEA082819 120030102A6321 O-RING SKRSKYS76 S76A 8143006NE POWERPACK CUT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 633 ROTOR BRAKE POWERPACK O-RING CUT. 1G72 3U H1NE 20030106002292003010600229EU 2003 1 6 AWXA200300011 120030102A3232D5337061320200 FITTING AIRBUS320 A320232 3930326EU CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW0 0 448 MCN - MAJOR REPAIR - DURING C-07 CHECK HFEC INSPECTION INDICATED 2 EACH CRACKS ON THE L/H MAIN LANDING GEAR DOOR ACTUATOR FITTING, AFT 6TH FASTENER HOLE FROM THE TOP IN KEEL BEAM, 12 AND 6 O'CLOCK POSITION. MAINTENANCE ENLARGED THE AFT 6TH L/H MAIN LANDING GEAR DOOR ACTUATOR FITTING FASTENER HOLE PER E.O. 53-15-17. HFEC INSPECTION VERIFIED NO CRACKS EXIST. 2L72 4F RTA28NM 20030107000012003010700001NM 2003 1 7 PCAA0301006 120030103A291082950010351 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003NM CRACKED A PCAAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 EA13846EX 326 PIT- FLIGHT#3847. CREW REPORTED #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED ON GROUND.FLUID LOSS ON #2 SIDE, DOWN TO 3/4 OF A QUART. MAINTENANCE FOUND HYDRAULIC LINE PART NUMBER 82950010-351 CRACKED. INTERIM FLEX LINE INSTALLED AND SECURED. LEAK CHECK GOOD AT THIS TIME. HYDRAULIC SYSTEM SERVICED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030107000182003010700018EU 2003 1 7 DHL2003366001 120030103A2612AUL71221 DETECTOR AIRBUS300 A300B4203 3930306EU A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01366DH 249 1) LOOP "A" FOR ENGINE #1 ON THE FIRE DETECT LOOPS PANEL WILL NOT TEST.2) DEFERRED PER MEL 26-13-03. CONTROL #11472. PLACARD INSTALLED.3) REF. DMI #11472, LOOP "A" FOR ENGINE #1 ON THE FIRE DETECT LOOPS WILL NOT TEST.4) REF. WD 26-12-11 PAGE 5, FOUND PYLON FIRE LOOPS 23WD/25WD READING 105 OHMS ON CONTINUITY CHECK (SHOULD BE ONLY A FEW OHMS). FIRE LOOP "A" TESTS OK WHEN JUMPER IS USED BETWEEN PINS "A" & "B" OF CONNECTOR 595VC.5) REF. DMI #11472 LOOP "A" FOR ENGINE #1 IN THE FIRE LOOP PANEL WILL NOT TEST.6) REMOVED AND REPLACED FORWARD PYLON LOWER CAP FIRE SENSING ASSEMBLY IAW A300 AMM 26-12-12. OPS CHECKED GOOD IAW A300 AMM 26-12-00 PAGE 501. THIS CLEARS DMI #11472. 2L72 4F RTA35EU 20030123000762003012300076NE 2003 1 23 WRNA200300001 220030117A7200CF650C2 ENGINE AIRBUS A300B4 AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE OVERTEMP A WRNAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING EJMVIBRATION/BUFFET WARNING INDICATION OVER TEMP CLCLIMB 1 SO05820SC427752664 154 154 528271 During climb out of flt level 75, time 0540Z, heard an expolosion from #1 engine, confirmed #1 engine failure, #1 engine EGT went to max indication, followed emergency and abnormal procedure, fuel dump procedure was followed down to max landing weight. A/C returned to field, landing normal.Corrective Action: Removed and replaced engine I/A/W engine change paperwork. Run up checks satisfactory. Aircraft returned to service. 2L72 4F4 FRTA35EU E23EA 20030204002812003020400281NM 2003 2 4 F3LA200300013 120030118A5320 SHIM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTALS BETWEEN STA 986.5 AND 967 CORRODED ON TOP SIDE. FLOOR SUPPORT SHIM AT LBL 15.5 AND RBL 15.5 FOUND TO BE OUT OF LIMITS PER SRM 53-60-51, FIG 101. FABRICATED SHIMS PER EA 53-737-199. INSTALLED SHIMS TO FLOOR SUPPORTS AND REINSTALLED FLOOR SUPPORTS PER SRM 51-40-02. 2L72 4F RTA16WE 20030124000052003012400005WP 2003 1 24 MWEA030044 120030124A278059365321 PULLEY DOUG DC9 DC981 3022081WP PULLEY BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 SLAT FOLLOW UP CABLE PULLEY IN THE SLAT SEQUENCE CONTROL MECHANISM HAS A SECTION BROKEN OFF. -- BLENDED DAMAGE. 2L72 4F A6WE 20030124000092003012400009SO 2003 1 24 C2XA03BT013 120030123A4900 APU EMB 145 EMB145LR 3260212SO TAILCONE ODOR A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2729906 145472 EWR---CO2679, CREW REPORTED, "WHEN STARTING APU THERE WAS A STRONG FUEL SMELL." MAINTENANCE REPOSITIONED AIRCRAFT FROM "TAILWIND" CONDITION. RAN APU. NO FAULTS OR SMELLS NOTED IAW EMB145 MM 49-00-00. AIRCRAFT RETURNED TO SERVCIE. 2L72 4T RTT00011AT 20030124000812003012400081NM 2003 1 24 EIA2003004 120030122A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 FUSELAGE INTERIOR RIGHT SIDE F.S. 1760 CRACK IN FRAME AT STRINGER 13 UPPER FLANGE OF FRAMECUT OUT DAMAGED SECTION FABRICATED FRAME SECTION AND REPAIR SPLICES(2EA) PER B747 SRM 51-40-06 PG. 2 SHEET 1-4, ALODINED, PRIMED AND INSTALLED REPAIR PER B747 SRM 51-30-02 PG 1-15. 2L74 4F A20WE 20030124000822003012400082NM 2003 1 24 UPS03240049 120030107A5310 BRACKET BOEING727 72721C 138400MNM BS 740 S17R BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE:C FLAT BRACKET BROKEN ON FUSELAGE SKIN AT BS 740 AT INTERSECTION WITH STR. 17R NEW PLATE FABRICATED IAW SRM 51-20-01 FIG 7 INSTALLED IAW SRM 51-30-02 2L73 4F A3WE 20030124000852003012400085NM 2003 1 24 UPS03240065 120030106A5310 FITTING BOEING727 72721C 138400MNM BS 950 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE:C CRACK INDICATION IN 2 HOLES BS 950 L/H HOLES LOCATED ON ROWS 2ND FRO M FWD EDGE OF FITTING AND 2ND HOLES FROM BOTTOM OF SPLICE PLATE JUST BELOW STR. 6 L/H BS 950 BULKHEAD FITTING REPLACED IAW EO B727-5310-3012 & DRAWING 65C18332 AND 2MIT65C15732-25 2L73 4F A3WE 20030127000082003012700008 2003 1 27 HEEA083584 420030114A3421 LIGHT BELL 412 412 1182202SW HORIZON GYRO INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 1748 36002 HORIZON GYRO LIGHTING INOPERATIVE. SHOP REPAIR. 1G72 4U H4SW 20030127000102003012700010 2003 1 27 HEEA083586 420030114A34215040017928 INDICATOR BELL 412 412 1182202SW STANDBY ATTITUDEPRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 STANDBY ATTITUDE PRECESSES. SHOP REPAIR. 1G72 4U H4SW 20030127000122003012700012 2003 1 27 HEEA083588 420030114A34215040017928 INDICATOR BELL 412 412 1182202SW STANDBY ATTITUDEPRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 STANDBY ATTITUDE PRECESSES. SHOP REPAIR. 1G72 4U H4SW 20030127000142003012700014SW 2003 1 27 HEEA083590 120030114A67207001482 CONTROL ROD BELL 412 412 1182202SW TAIL ROTOR DAMAGED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW035759N 33002 CONTROL ROD DAMAGED CAUSING AFCS CAUTION LIGHT TO COME ON INTERMITTENTLY. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030127000162003012700016 2003 1 27 HEEA083592 420030114A2350A3016R MIXER BOX BELL 412 412 1182202SW COMMS SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 MIXER BOX CAUSING BUZZING NOISE IN HEADSET. SHOP REPAIR. 1G72 4U H4SW 20030127000262003012700026 2003 1 27 HEEA083602 420030114A3457N0002000 GPS BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 GPS DOES NOT ADKNOWLEDGE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030127000282003012700028 2003 1 27 HEEA083604 420030114A3457N0002000 GPS BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 GPS WILL NOT ACKNOWLEDGE RECEPTION. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030127000292003012700029 2003 1 27 HEEA083605 420030114A2312069102435 RECEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 VHF RECEIVER HAS STATIC ON ALL FREQUENCIES. SENT TO SHOP FOR REPAIR. 1G71 3U H2SW 20030127000312003012700031SW 2003 1 27 HEEA083607 120030114A2820206362002101 CAP BELL 206 206L3 1182108SW FUEL STORAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 FUEL CAP AND ADAPTER ASSY HANDLE WILL NOT STAY LOCKED, WORN. SENT TO SHOP FOR REPAIR. 1G71 3U H2SW 20030127000322003012700032 2003 1 27 HEEA083608 420030114A34570110050400 GPS BELL 407 407 1182206SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 GPS INTERMITTENTLY DISPLAYS "NO DATA" AND CODE 429. 1G71 3U O H2SW 20030127000362003012700036SW 2003 1 27 HEEA083613 120030114A28221C2710 CARTRIDGE BELL 407 407 1182206SW FUEL BOOST INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 CARTRIDGE DOES NOT OPERATE WITH POWER APPLIED. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030204001842003020400184 2003 2 4 SWAA030111 420030117A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED BC1 CHECK, FOUND R2 DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED ESCAPE SLIDE PER MM. 2L72 4F RTA16WE 20030204001852003020400185NM 2003 2 4 SWAA030113 120030117A25606551463 ATTACH FITTING BOEING737 7373H4 1384600NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND CORROSION ON THE L1 GIRT BAR ATTACH FITTINGS BS 312 AND BS 344. REMOVED AND REPLACED THE L1 GIRT BAR ATTACHED FITTINGS PER MM. 2L72 4F RTA16WE 20030204001862003020400186NM 2003 2 4 SWAA030114 120030117A5220507978 HANDLE BOEING737 7373H4 1384600NM EMERGENCY EXIT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED BC2 CHECK, FOUND THE RT OVERWING EMERGENCY EXIT INSIDE HANDLE DAMAGED. REMOVED AND REPLACED THE INSIDE EXIT HANDLE PER MM. 2L72 4F RTA16WE 20030204001882003020400188NM 2003 2 4 SWAA030119 120030118A2560PH22301 STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 PORTION OF THE EEPLS SELF ILLUMINATION STRIP NOT SECURED. SECURED THE EEPLS STRIP PER MM. 2L72 4F RTA16WE 20030204001912003020400191 2003 2 4 SWAA030121 420030118A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED BC4 CHECK, FOUND R2 DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED R2 DOOR ESCAPE SLIDE PER MM. 2L72 4F RTA16WE 20030204001972003020400197SO 2003 2 4 2003F00101 120030117A8120LW127996S100 LINE PIPER PA31 PA31325 7103105SO LYC O540 TIO540F2BD 41532EA TURBOCHARGER OILLEAKING E EA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL0959815822 822 317612041 L499061A DEVELOPED OIL LEAK FROM LT ENGINE DURING RETURN FLIGHT. OIL TEMP WAS HOLDING, BUT OIL PRESSURE HAD STARTED TO DECAY. PILOT SHUT ENGINE DOWN AND FEATHERED AS A PRECAUTIONARY MEASURE. FOUND PIN HOLE IN TURBOCHARGER OIL SUPPLY LINE AND REPLACED WITH NEW ON 1/21/03. REMOVED OIL FILTER AND CHECKED FOR METAL CONTAMINATION, NONE FOUND. 1L72 3O3 O A20SO E14EA 20030204002002003020400200NM 2003 2 4 SWAA030129 120030119A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500A STR 4L, BS 520 STR 7R, STR 8R AND STR 12L, BS 597 STR 3L, BS 616 STR 3R, BS 727A STR 8L, 727B STR 8L, BS 727D STR 3R & STR 4L AND BS 727E STR 7L. REMOVED AND REPLACED CRACKED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030204002102003020400210NM 2003 2 4 SWAA030144 120030121A2560P2070001 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29314SW 23336 FWD OUTBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20030204002122003020400212 2003 2 4 SWAA030157 420030122A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29071SW 22358 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20030204002192003020400219NM 2003 2 4 SWAA030168 120030122A3230A42006028305 SOLENOID BOEING737 7373H4 1384600NM COCKPIT INOPERATIVE A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29614SW 28033 AIR TURNBACK, LANDING GEAR LEVER WOULD NOT MOVE UP PAST THE OFF POSITION. LANDING GEARS WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR LEVER LOCK SOLENOID PER MM. 2L72 4F RTA16WE 20030204002262003020400226NM 2003 2 4 SWAA030190 120030125A335065C27093 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 RT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030204002272003020400227NM 2003 2 4 SWAA030192 120030125A3350071701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29764SW 27878 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL MID INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED MID CABIN BATTERY PACK PER MM. 2L72 4F RTA16WE 20030204002322003020400232NM 2003 2 4 SWAA030199 120030126A32116546113 TRUNNION PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED A2 CHECK, SWA SI 11251-32, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030204002402003020400240NM 2003 2 4 SWAA030222 120030129A2910R291206EE025OT HYDRAULIC LINE BOEING737 7373K2 13844BANM LT MLG LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29345SA 23786 AIR TURNBACK/DECLARED EMERGENCY, LOST HYD A-SYS PRESSURE AND QUANTITY INDICATIONS AFTER TAKEOFF. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR HYD LINE PER MM. 2L72 4F RTA16WE 20030204002422003020400242 2003 2 4 SWAA030224 420030130A25651061323433 SLIDE BOEING737 7375H4 138449DNM AFT ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2L72 4F RTA16WE 20030204002432003020400243 2003 2 4 SWAA030230 420030129A2565D31354 SLIDE BOEING737 7373Q8 1384670NM CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030204002442003020400244NM 2003 2 4 SWAA030231 120030130A335007912 COVER BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 EEPLS COVER DAMAGED AT ROW NR 16. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030204002492003020400249NM 2003 2 4 VNAA0301013 120030112A7603 SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE POWER LEVER MALFUNCTIONED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION HORN AND RED WARNING PANEL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE POWER LEVER MICRO SWITCH RACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002692003020400269NM 2003 2 4 VNAA0301017 120030115A3260870004MODB PSEU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LANDING GEAR FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07470PS16917318 3006 EN ROUTE, THE CREW RECEIVED A PROXY SYSTEM FAIL INDICATION ON THE HYDRAULICS PAGE AND CALLED MAINTENANCE CONTROL. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE INSTRUCTED TO DIVERT TO PIT. MAINTENANCE INSPECTED AND FOUND SEVERAL CODES IN THE PSEU. MAINTENANCE THEN REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002732003020400273NM 2003 2 4 VNAA0301021 120030121A3240 METERING VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BRAKE SYS CONTAMINATED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07470PS 3006 THE CREW REPORTED THAT THE FIRST OFFICER'S BRAKES WERE EXTENDED WITH LIGHT TO NO BRAKING ACTION. MAINTENANCE INSPECTED AND BLED THE BRAKE METERING UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002762003020400276NM 2003 2 4 VNAA0301025 120030123A3250 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NLG STEERING DIRTY A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07430JS 3044 THE CREW ADVANCED POWER FOR TAKEOFF AND RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE THEN ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE CANNON PLUGS ON THE BACK OF THE NOSE WHEEL STEERING MANIFOLD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002772003020400277NM 2003 2 4 VNAA0301026 120030124A2611 SMOKE WARNING DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07470PS 3006 THE CREW REPORTED THAT THE LAV SMOKE CAS MESSAGE FLASHED AND THEN CLEARED. THE CREW CALLED MAINTENANCE CONTROL JUST TO REPORT IT AND WERE INSTRUCTED TO CONTINUE SINCE IT DID NOT REPEAT. FLIGHT 4064 WAS COMPLETED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002782003020400278NM 2003 2 4 VNAA0301027 120030124A5270 PROXIMITY SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DOOR OUT OF ADJUST A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07426JS 3038 EN ROUTE, THE MASTER CAUTION LIGHT ILLUMINATED AND THE PRESSURE CHECKED GOOD. THE CREW DESCENDED AND SLOWED TO 150 KIAS. AT FL180 THE LIGHT EXTINGUISHED. UPON ARRIVAL AT DCA, MAINTENANCE INSPECTED AND ADJUSTED THE OVER CENTER PROXI SWITCH CLEARANCE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030205000042003020500004CE 2003 2 5 208000103 120030120A275226111441 STRUCTURE CESSNA CESSNA208 208B 2073701CE FLAP ACTUATOR CRACKED E ENHRK NONE O OTHER ININSP/MAINT 1 AL031276P2858 208B00852 SUPPORT ASSEMBLY-FLAP ACTUATOR FAILURE. PILOT REPORTED FLAPS SELECTED 10 DEG FLAPS WENT TO 10 DEGREE STOPPED AT THE NEXT FLAP SELECTION CIRCUIT BREAKER TRIPPED, CIRCUIT BREAKER WOULD NOT RESET. STANDBY FLAP SW WAS NOT USED AND BREAK-AWAY WIRE INTACT. FURTHER VISUAL INSPECTION OF THE FLAP SYSTEM PERFORMED BY MAINTENANCE PERSONNEL FOUND THE FLAP ACTUATOR SUPPORT BRACKETS CRACKED AND BROKEN. 1H71 3T A37CE 20030205000362003020500036NM 2003 2 5 SROM200300003 120030103A5311652072328 FRAME BOEING737 737205 1384456NM ZONE 100 CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND FWD CARGO DOOR CUT OUT AFT FRAME CRACKED AT NR 5 STOP FITTING. RECEIVED, DRILLED AND INSTALLED FWD CARGO DOOR AFT FRAME REPAIR PARTS PER 51-40-03, FIG. 1, PARA. 1,2 & 3. MAJOR REPAIR 2L72 4F RTA16WE 20030205000382003020500038NM 2003 2 5 SROM200300005 120030103A5320654582942 WEB BOEING737 737205 1384456NM ZONE 200 CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND CORROSION AT E & E BAY, RT SIDE OF DOOR CUTOUT ABOVE LATCH PLATE. REMOVED AND REPLACED WEB PER SRM 51-30-2, 53-10-1. MINOR REPAIR. FINDING NOT A CPCP ITEM. 2L72 4F RTA16WE 20030205000402003020500040NM 2003 2 5 SROM200300007 120030105A5320 INTERCOSTAL BOEING737 737205 1384456NM ZONE 100 CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND CORROSION ON UPPER FLANGE OF INTERCOSTAL AT STA 967, RBL20, CARGO FLOOR LEVEL. REMOVED INTERCOSTAL AND REPLACED WITH NEW PER SRM 53-10, 53-30-2, 51-10-2 AND 57-20-1. MINOR REPAIR. NOT A CPCP GENERATED FINDING. 2L72 4F RTA16WE 20030205000422003020500042NM 2003 2 5 SROM200300009 120030105A781065522631018 CHANNEL BOEING737 737205 1384456NM ZONE 400 CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND NR 2 ENGINE I/B FIXED FAIRING MOST AFT I/B CHANNEL STIFFENER CRACKED. REPAIRED NR 2 ENGINE I/B FIXED FAIRING AFT I/B CHANNEL PER SRM 51-20-1 & 51-30-2. MINOR REPAIR. 2L72 4F RTA16WE 20030205000442003020500044NM 2003 2 5 SROM200300011 120030105A54147075T6 SKIN BOEING737 737205 1384456NM ZONE 400 DENTED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 2 ENGINE IB NACELLE SKIN DENTED. REPAIRED NR 2 ENGINE IB NACELLE SKIN BY FABRICATING REPAIR PARTS FOR SKIN AND INSTALLING ON NACELLE AFTER REMOVING DAMAGE PER SRM 54-10-3. MINOR REPAIR. 2L72 4F RTA16WE 20030205000462003020500046NM 2003 2 5 SROM200300013 120030116A5411657377482 RIB BOEING737 737205 1384456NM ZONE 400 CHAFED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 2 ENGINE OB NACELLE NR 10 RIB CHAFED 8 INCHES FROM LOWER EDGE. CUT OUT DAMAGE 1 X 3 INCHES, FABRICATED REPAIR DOUBLER, ALODINED, PRIMED PART AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3 AND 54-30-1. MINOR REPAIR. 2L72 4F RTA16WE 20030205000512003020500051NM 2003 2 5 SROM200300019 120030120A541065279583 DOUBLER BOEING737 737205 1384456NM ZONE 400 CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 1 ENGINE OB NACELLE FWD IB BREATHER CUT OUT IS CRACKED. REMOVED AND REPALCED BREATHER CUT OUT WITH NEW PART PER SRM 51-30-5, 51-10-2, 51-30-3 AND MM 51-21-17. 2L72 4F RTA16WE 20030205000532003020500053EU 2003 2 5 VJ32003F00021 120030124A7714 INDICATOR GROB 120 G120A 1660208EU ENGINE RPM ERRATIC A VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP07862AF701 009 85002 THE RPM INDICATOR IS ERRATIC AND STICKS DURING FLIGHT. PROBABLE CAUSE MAY BE INTERNAL MECHANISM FAILING. 1L71 3O RTA49CE 20030205000542003020500054EA 2003 2 5 WO105501 120030109A783022850808125 THRUST REVERSER CNDAIRCL600 CL6002B16 1900305EA LT ENGINE BROKEN B H DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE NRNOT REPORTED 1 NE03343KA6723 5086 LT THRUST REVERSER 8 O'CLOCK MAIN TRACK FITTING WAS FOUND SEPERATED AT THE MAIN TRACK ATTACHMENT FORK END. INITIAL VISUAL INSPECTION FOUND ATTACHMENT FITTING HAD PENETRATED LT ENGINE LOWER FAN COWL AND DAMAGED THE FAN BLADE CONTAINMENT CASE RING. FURTHER INSPECTION FOUND THE FOLLOWING COMPONENTS DAMAGED: 8 O'CLOCK MAIN TRACK FITTING, LT FAN CONTAINMENT RING, LT THRUST REVERSER POWER DRIVE UNIT, LT THRUST REVERSER ACTUATOR, LT 4 O'CLOCK MAIN TRACK FITTING, LT 2 O'CLOCK ACTUATOR, LT 2 O'CLOCK CASCADE, LT INLET COWL, AND THE LT 8 O'CLOCK MAIN TRACK. 2L72 4F RTA21EA 20030205000592003020500059SO 2003 2 5 C2XA03CL028 120030202A26123601133500230 DETECTOR EMB 135 EMB135ER 3260203SO #2 ENGINE FAILED A C2XAK NONE J WARNING INDICATION DEDESCENT 1 SW2715509 145238 CLE FLIGHT#2083 THE CREW REPORTED A ENGINE #2 FIRE DETECTOR FAIL MESSAGE INTERMITTENTLY ON THE DESCENT.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #2 ENGINE FIRE DETECTOR LOOP ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030205001042003020500104NM 2003 2 5 PCAA0302034 120030203A533085310346 ANGLE DHAV DHC8 DHC8102 2809003NM CRACKED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13824EX 387 DURING ROUTINE MAINTENANCE VISIT, NOSE LANDING GEAR TRUNNION RIGHT SIDEWALL ANGLE AT APPROXIMATE STATION OF X101 FOUND CRACKED WHILE PERFORMING A 4 INSPECTION. ALSO, NOSE WHEEL WELL SKIN PART NUMBER 85310056 WAS FOUND CRACKED AT AREA OF INTERSECTION OF STATION X96.19 AND Y9.00. CRACKS WERE REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWINGS RD8-53-3630 AND RD8-53-698. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030206000452003020600045NE 2003 2 6 DLM11030052 220030111A7320 EEC DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE NR 2 ENGINE MALFUNCTIONED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27812DE42279 48601 723904 ON TO ROLL SELECT FADEC ALTN ILLUMINATED AGAIN ABORTED TO APPROXIMATELY 60 KTS MESSAGE OCCURS SHORTLY AFTER TAKEOFF POWER IS SET NORMAL FULL POWER USED ON BOTH TAKEOFFS. REPLACED NR 2 ENGINE EEC. 2L73 4F4 FRTA22WE E24NE 20030206000462003020600046NM 2003 2 6 SWAA030271 120030204A27512061141 INDICATOR BOEING737 7372H4 138448CNM COCKPIT FAULTY A SWAAAD UNSCHED LANDING RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29094SW 23053 AIR TURNBACK, AFTER TAKEOFF T/E FLAPS WOULD NOT RETRACT. REMOVED AND REPLACED FLAP INDICATOR PER MM. 2L72 4F A16WE 20030206000472003020600047 2003 2 6 SWAA030273 420030203A256565C19901 CABLE BOEING737 7375H4 138449DNM AFT ENTRY DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030206000482003020600048 2003 2 6 SWAA030274 420030203A25656557463 FITTING BOEING737 7373H4 1384600NM FWD SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED C3 CHECK, FOUND LOOSE RIVETS AT FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING RIVETS PER SRM. 2L72 4F RTA16WE 20030206001322003020600132EA 2003 2 6 COMA0360071 120030203A324017300124 HARNESS CNDAIRCL600 CL6002B19 1900309EA R/H MLG DEFECTIVE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01811CA 7380 FLIGHT 5697 OUTBD ANTI SKID INOP CAUTION MESSAGE.REPLACED THE R/H MLG WIRE HARNESS. 2L72 4F RTA21EA 20030206001372003020600137EA 2003 2 6 COMA0360076 120030131A3350276005 FUSE CNDAIRCL600 CL6002B19 1900309EA CABIN BLOWN A COMAO OTHER O OTHER ININSP/MAINT 1 SO01917CA 7017 FLIGHT 5530 FWD EXTERIOR EMERGENCY LIGHTS ARE INOP.REPLACED BATTERY CHARGER FUSE. 2L72 4F RTA21EA 20030206001542003020600154WP 2003 2 6 ZW0A0301302 120030127A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C, IN THE AFT CARGO COMPT FOUND BULKHEAD FRAME CORRODED AT STRINGER 1320, RBL 6, LBL 40. REMOVED OLD FRAME AND REPLACED PER SPM 6-70-01. 2L72 4F A6WE 20030206001892003020600189NM 2003 2 6 AWXA200300105 120030128A5320146N872215 FITTING BOEING757 7572S7 1384962NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CORNER FITTING ABOVE L/H CUSP WEB AT BS 1720. MAINTENANCE REMOVED CORRODED CORNER FITTING ABOVE L/H CUSP WEB AT BS 1720; FABRICATED A NEW REPLACEMENT CORNER FITTING; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 11-12. 2L72 4F RTA2NM 20030207000162003020700016NM 2003 2 7 DLM88030049 120030112A322039567851 LINK DOUG MD88 MD88 3023688NM NLG DOOR FAILED A DALAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO27972DL 53215 VIBRATION. AFTER GEAR RETRACTION, GEAR RECYCLED SAME RESULT. CAME ON TO ATL. AT ARRIVAL IN ATL FOUND LT NOSE GEAR DOOR OPEN. REPLACED LT FWD NOSE GEARDOOR LINK. JACKED NOSE GEAR AND CYCLED GEAR, OPERATION, CHECKS GOOD. 2L72 4F RTA6WE 20030127000372003012700037SW 2003 1 27 HEEA083614 120030114A28221C2710 CARTRIDGE BELL 407 407 1182206SW FUEL BOOST INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 CARTRIDGE INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030127000402003012700040 2003 1 27 HEEA083617 420030114A2562110324 ANTENNA BELL 407 407 1182206SW ELT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 ELT ANTENNA WHIP BROKEN. REPAIRED. 1G71 3U O H2SW 20030127000462003012700046SW 2003 1 27 HEEA083623 120030114A52103160201 HANDLE BELL 407 407 1182206SW CREW DOOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 CREW DOOR LEVER ON HANDLE IS WORN. 1G71 3U O H2SW 20030127000472003012700047SW 2003 1 27 HEEA083624 120030114A52103160201 HANDLE BELL 407 407 1182206SW CREW DOOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 CREW DOOR HANDLE WORN. TO BE SENT TO BELL FOR CREDIT. 1G71 3U O H2SW 20030127000502003012700050SW 2003 1 27 HEEA083628 120030114A243231908001 BATTERY BELL 407 407 1182206SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 BATTERY WEAK DURING START. REPAIRED. 1G71 3U O H2SW 20030127000522003012700052SW 2003 1 27 HEEA083630 120030114A243231908001 BATTERY BELL 407 407 1182206SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 BATTERY WEAK AND NEGATIVE PIN CORRODED. REPAIRED. 1G71 3U O H2SW 20030127000552003012700055 2003 1 27 HEEA083633 420030114A342150400179015 INDICATOR BELL 407 407 1182206SW ADI MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 ADI WON'T CAGE. REPAIRED. 1G71 3U O H2SW 20030127000602003012700060 2003 1 27 HEEA083638 420030114A34225050010902 GYRO BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 GYRO CARD ROTATES - WILL NOT STABILIZE. REPAIRED. 1G71 3U O H2SW 20030127000642003012700064 2003 1 27 HEEA083642 420030114A34225050031904 GYRO BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 DIRECTIONAL GYRO SPINS. REPAIRED. 1G71 3U O H2SW 20030127000682003012700068EU 2003 1 27 MALA030106 120030110A2161 CONTROLLER SAAB SF340 SF340A 7850100EU CABIN TEMP MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1599XJ 340A099 DURING FLIGHT 3196, RT DUCT OVERTEMP/BLEED FAULTED. AUTO AND MANUAL MODE. AIR RETURN TO MSP. MAINTENANCE CHECKED MANUAL MODE TEMP CONTROL, OPS CHECK GOOD. DEFERRED AUTO TEMP CONTROL AS PER MEL 21-60-2 (C) TRANSFERRED TO DMR MXC NOTIFIED. NO OTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20030127000752003012700075NM 2003 1 27 PCAA0301017 120030119A2910 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE LEAKING A PCAAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 EA13836EX 297 YUL-FLIGHT 3974 CREW REPORTED NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL, PRESSURE DROPPED TO ZERO WITH FLUID LEAKING OUT OF NR 2 ENGINE NACELLE. MAINTENANCE FOUND OUTBOARD ACTUATOR LINE LEAKING. LINE REPLACED WITH AN INTERIM FLEX LINE IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 20-50-52. NR 2 HYDRAULIC PUMP REPLACED. AIRCRAFT GROUND RAN, OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030127000762003012700076SW 2003 1 27 HEEA083649 120030114A282070061J175W216A HOSE BELL 407 407 1182206SW FUEL DIST KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 FUEL HOSE ASSY KINKED. 1G71 3U O H2SW 20030127000782003012700078SW 2003 1 27 HEEA083651 120030114A282070079H000Y150 HOSE BELL 407 407 1182206SW FUEL DIST KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 FUEL HOSE ASSY KINKED. 1G71 3U O H2SW 20030127000812003012700081NM 2003 1 27 PCAA0301020 120030117A3397 WIRE DHAV DHC8 DHC8102 2809003NM CABIN BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13824EX 387 DURING ROUTINE MAINTENANCE VISIT 6TH EMERGENCY FLOOR LIGHT FROM FRONT FOUND INOPERATIVE. WIRE WAS BROKEN IN LIGHT TRACK. BROKEN WIRE REPAIRED GOING TO LIGHT SEGMENT IN TRACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030127000882003012700088NM 2003 1 27 SWAA030074 120030113A32116546113 TRUNNION PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED 1/2D CHECK, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030127000922003012700092SW 2003 1 27 HEEA083656 120030114A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 EMERGENCY FLOAT FUSIBLE PLUG LEAKING. 1G71 3U O H2SW 20030207000802003020700080NE 2003 2 7 NACA20030071 220030206A7421URHB32E SPARK PLUG PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE 10 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA133 133 A701WTVN 45529 37244 DISCREPANCY: #2 ENGINE SHUT DOWN DUE TO #10 CYLINDER DOUBLE SHORTED SECONDARY AND RUNNING ROUGH.CORRECTIVE ACTION: REPLACED FRONT AND REAR SPARK PLUGS. 2L74 4R4 R A781 5E8 20030207000862003020700086NM 2003 2 7 QXEA03000008 120030106A2910 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007NM HYD SYSTEM LEAKING A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM09347PH 480 PDX - FLIGHT 2069 - UPON GEAR SELECTION DOWN, THE NR 2 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED AND THE NR 2 HYDRAULIC FLUID WENT TO 0. MAINTENANCE INSPECTED THE AIRCRAFT AND THE NUMBER 2 HYDRAULIC SYSTEM AND REPLACED THE NUMBER 2 ENGINE DRIVEN PUMP AND A HYDRAULIC LINE BETWEEN THE PRESSURE FILTER AND THE PUMP. 2H72 4T RTA13NM 20030207000902003020700090EA 2003 2 7 QXEA0300003 120030103A2820D98C07606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAILED A QXEAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 NM09605QX2355 2355 10022 BOI ON FLIGHT 2447- CENTER WING SECTION HAS FUEL DRIPPING OUT. REMOVED AND REPLACED ENGINE FUEL PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030207000912003020700091NM 2003 2 7 03FDEA00029 120030115A2910 HYDRAULIC LINE BOEING727 727200 138407ENM PWA JT8 JT8D* NE HYD SYSTEM OUT OF POSITION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 HYDRAULIC LINE CHAFING ON STRUCTURE STA 1150, STR 22L, AFT CARGO REPAIRED FRAME IAW EA 7-5310-68161, SRM 51-40-3 FIG 1. 2L73 4F4 FRTA3WE E2EA 20030207000942003020700094EU 2003 2 7 03FDEA00048 120030119A5530 STRUCTURE AIRBUS310 A310203 3930313EU GE CF6 CF680 30025NE VERTICAL STAB DAMAGED A FDEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO25426FE 245 AT 23,000 FT WHILE ACCEL, FELT AIRFRAME VIB AND RETURNED. FOUND NR 1 VERT, LE, FIN ASSY DAMAGED. COAX ENDS PULLED FROM MOUNT, NUMEROUS FIBERGLASS SUPPORTS BROKEN, ANTENNA CONDUIT BENT AND STANDOFFS BROKEN. THIS INCLUDES ANTENNA ITSELF. FOUND STIFFENER 4.5 AND 5 BENT AND STIFFENER 5 CRACKED. STRAIGHTENED 4.5 STIFFENER AND AWAITING EA FOR STOP DRILL REPAIR OF NR 5 STIFFENER. FIN ASSY BUTT STRAP AND SUPPORT WEB BENT AND TORN. FIN ASSY UPPER EDGE FASTENER HOLES TORN THROUGH. REMOVED VERT STAB ACCESS PANELS, REMOVED DAMAGED FIN ASSY AND VERTICAL LE. DRILLED UP NEW FIN ASSY. INSTALLED DORSAL FIN ASSY. INSTALLED FWD, LEFT AND RIGHT VERTICAL STABILIZER SIDE FAIRINGS. 2L72 4F4 FRTA35EU E13NE 20030207000982003020700098NM 2003 2 7 03FDEA00053 120030118A3610652244143 DUCT BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 1 ENGINE BLOWN A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25257FE 20939 DURING CLIMBOUT WITH STANDARD TAKEOFF POWER SET, NR 1 ENGINE FIRELIGHT ILLUMINATED WITH HORN ON. SHUT DOWN ENGINE IAW WITH CHECKLIST. REMOVED AND REPLACED MAIN OIL STRAINER DUE TO INFLIGHT SHUT DOWN OF NR 1 ENGINE. ENGINE WINDMILLED FOR APPROXIMATELY 10 MINUTES. WORK DONE IAW AMM. LEAK CHECKED GOOD. REMOVED AND REPLACED 13TH STAGE SADDLE DUCT IAW AMM. LEAK CHECKED GOOD. AWAITING UPPER ENGINE COWL. INSTALLED UPPER ENGINE COWLING IAW AMM. OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20030207001012003020700101NM 2003 2 7 03FDEA00056 120030117A5313A6A71281 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CAC COMPARTMENT - BETWEEN BS 1139 - 1159, LONGERON 48L EDGE CORRODED. REPAIRED AS PER FEDEX EA NR 1-5310-63144. 2L73 4F RTA22WE 20030207001032003020700103NM 2003 2 7 03FDEA00059 120030116A5511 SPAR CAP DOUG MD11 MD11 3023602NM HORIZ STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT HORIZONTAL STABILIZER UPPER SPAR CAP AFT PLANK NR 33L BORE REAMED TO ALLOWABLE OVERSIZE DIA 1.178 INCHES IAW SB FOUND WITH 02 EA. 2L73 4F RTA22WE 20030207001062003020700106NM 2003 2 7 03FDEA00063 120030122A5320 WEB BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION, FORWARD CARGO DOORWAY LOWER SILL BEAM WEB, STA 560-620 STR 26R, NUMEROUS AREAS OUTBOARD SIDE. REMOVED, FABRICATED, AND INSTALLED FORWARD CARGO DOOR LWR BEAM WEB IAW SRM 53-10-1, 51-20-1, 51-30-2. 2L73 4F4 FRTA3WE E2EA 20030207001072003020700107NM 2003 2 7 03FDEA00064 120030122A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 AFT CARGO BAY BS 1130 FRAME IS DENTED AT LBL 27 UPPER FLANGE. DENT IN FRAME BS 1130 AFT CARGO BAY LBL 27 UPPER FLANGE TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 53-10-1, SRM 51-30-2, SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20030207001132003020700113EU 2003 2 7 03FDEA00073 120030124A7830 WARNING LIGHT AIRBUS310 A310222 3930315EU PWA JT9 JT9D* NE COCKPIT ILLUMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25447FE 251 715438 ON TAKEOFF, POWER APPLICATION NR 1 REV UNLOCK LIGHT ILLUMINATED. REJECTED TAKE OFF AND RETURNED TO RAMP, WHEN POWER REDUCED, LIGHT WENT OUT. AC RELEASED FOR SERVICE IAW MEL/CDL 78-31-01 CATEGORY C. ENGINE NR 1 REV UNLK - INOPERATIVE. AFFECTED THRUST (1 OR 2) REVERSER DEACTIVATED. 2L72 4F4 FRTA35EU E20EA 20030207001282003020700128WP 2003 2 7 ZW0A0301503 120030201A3397 WIRE HARNESS DOUG DC9 DC982 3022082WP CABIN DISCONNECTED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13960TW 49231 THE FIRST CLASS EGRESS LIGHTING WAS INOPERATIVE. RECONNECTED FEEDER CABLE. 2L72 4F A6WE 20030207001362003020700136EU 2003 2 7 QXEA0300007 120030103A33503006253 LIGHT FOKKERF28 F28MK4000 4990810EU CABIN INOPERATIVE A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09493US 11161 PDX- RIGHT HAND FORWARD EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT HAND FORWARD EGRESS LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20030207001392003020700139NM 2003 2 7 QXEA0300008 120030106A2913570347 PUMP DHAV DHC8 DHC8202 2809007NM HYD SYSTEM FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09347PH7472 480 SUP - PDX - FLIGHT 2069 - UPON GEAR SELECTION DOWN, THE NR 2 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED AND THE NR 2 HYDRAULIC FLUID WENT TO 0. MAINTENANCE INSPECTED THE AIRCRAFT AND THE NUMBER 2 HYDRAULIC SYSTEM AND REPLACED THE NUMBER 2 ENGINE DRIVEN PUMP AND A HYDRAULIC LINE BETWEEN THE PRESSURE FILTER AND THE PUMP. OPERATIONAL AND LEAK CHECKS WERE PERFORMED AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030207001582003020700158SO 2003 2 7 C2XA03BT027 120030207A335066368 LIGHT EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2714916 145415 BTV---CO2002, DURING 2A INSPECTION, MAINTENANCE FOUND FLOOR EMERGENCY LIGHT STRIP 2ND FROM THE REAR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED #7 FLOOR PROXIMITY EMERGENCY LIGHT STRIP IAW EMB145 AMM #33-50-12. OPS. CHECKED GOOD. 2L72 4T RTT00011AT 20030129000162003012900016SW 2003 1 29 HEEA083926 120030117A6220 BEARING BELL 407 407 1182206SW M/R HEAD FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH A391 53378 MAIN ROTOR HEAD GREEN BLADE GRIP SHEAR BEARING FAILED. 1G71 3U O H2SW 20030129000262003012900026SW 2003 1 29 HEEA083936 120030117A6300407010201105 BEAM BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH1074 53207 NR PICKUP WIRING BUNDLE CHAFED PYLON BEAMS. DAMAGE .035 OF AN INCH IN AREA WITH NO DAMAGE ALLOWED. 1G71 3U O H2SW 20030129000332003012900033SW 2003 1 29 HEEA083946 120030117A6420407012101111 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 TAIL ROTOR HEAD TRUNNION CLICKS WHEN FLAPPING BLADES. REPAIRED. 1G71 3U O H2SW 20030129000372003012900037SW 2003 1 29 HEEA083950 120030117A6420 BEARING BELL 407 407 1182206SW T/R HEAD SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53324 53283 TAIL ROTOR HEAD BEARING HAS RUBBER SEPERATION. REPAIRED. 1G71 3U O H2SW 20030129000402003012900040SW 2003 1 29 HEEA083953 120030117A6420 BEARING BELL 407 407 1182206SW T/R HEAD DELAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53397 53159 TAIL ROTOR HEAD FLAPPING BEARINGS DELAMINATED. REPAIRED. 1G71 3U O H2SW 20030129000442003012900044SW 2003 1 29 HEEA083957 120030117A3246407012203 SKID BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 MLG SKID CORRODED. 1G71 3U O H2SW 20030129000492003012900049SW 2003 1 29 HEEA083962 120030117A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 MAIN ROTOR BLADE HAS SEPARATION AT TIP. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030129000552003012900055SW 2003 1 29 HEEA083968 120030117A5321407030713103 FLOOR PANEL BELL 407 407 1182206SW CARGO DECK CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 CARGO DECK FLOOR PANEL CORRODED AND SEPARATED. 1G71 3U O H2SW 20030129000592003012900059SW 2003 1 29 HEEA083973 120030117A6320407040623101 LINE BELL 407 407 1182206SW M/R GEARBOX OIL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 MAIN ROTOR GEARBOX OIL LINE CORRODED UNDER SLEEVE. 1G71 3U O H2SW 20030129000602003012900060SW 2003 1 29 HEEA083974 120030117A6320407040623101 LINE BELL 407 407 1182206SW M/R GEARBOX OIL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 MAIN ROTOR GEARBOX OIL LINE CORRODED UNDER B-NUT SLEEVE. 1G71 3U O H2SW 20030129000642003012900064SW 2003 1 29 HEEA083978 120030117A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 ENGINE BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030129000652003012900065SW 2003 1 29 HEEA083979 120030117A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 ENGINE BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030129000682003012900068SW 2003 1 29 HEEA083982 120030117A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 ENGINE BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030129000752003012900075NM 2003 1 29 2003UALA00076 120030121A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29646UA 25283 EXTERNAL LOWER FUSELAGE SKIN HAS DENT AT BS 654 + 66, STRINGER 31R. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH DOUBLER AND FILLER. 2L72 4F4 FRTA1NM E24NE 20030129000772003012900077SW 2003 1 29 HEEA083983 120030117A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030207001602003020700160EA 2003 2 7 COMA0360084 120030205A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01916CA 7014 FLIGHT 5797 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2L72 4F RTA21EA 20030208000082003020800008EU 2003 2 8 RAIA00301028 120030129A3220AH54474 TIRE AEROSPATR72 ATR72202 8680940EU OUT OF BALANCE A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03722TE 220 5602-STL- SEVERE VIBRATION FROM NOSE TIRES ON TAKE OFF. MAINTENANCE REMOVED AND REPLACED THE NOSE TIRES, TAXI CK OK. 2H72 4T RTA53EU 20030210000502003021000050NM 2003 2 10 QXEA0300033 120030103A3620 SWITCH BOMBDRDHC8 DHC8401 1390041NM BLEED AIR SYS FAULTY A QXEAO OTHER N FALSE WARNING TOTAKEOFF 1 NM09403QX 4037 SEA ON FLIGHT 2315- NR 2 BLEED HOT CAUTION ILLUMINATED SHORTLY AFTER TAKEOFF. RAN ABNORMAL CHECK LIST, CAUTION LIGHT REMAINED ILLUMINATED. REPINNED 9811-P20 ON NR 2 ENGINE BLEED AIR OVER TEMPERATURE SWITCH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030210000562003021000056EA 2003 2 10 QXEA0300040 120030109A2820D98C07606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAILED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09608QX2755 2755 10026 BOI ON FLIGHT 2551- RIGHT FUEL LOW PRESSURE CAUTION MESSAGE AFTER ENGINE START. REMOVED AND REPLACED NR 2 ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030210000572003021000057EA 2003 2 10 QXEA0300041 120030113A2820D98C07606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09612QX338 338 10042 SEA- LEFT FUEL PRESSURE LOW CAUTION MESSAGE. REMOVED AND REPLACED NR 1 FUEL LOW PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030210001112003021000111NM 2003 2 10 QXEA0300059 120030111A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX-FORWARD FLANGE OF PANEL 262FT IS CHAFED. REPAIRED IAW DHC-84 SRM 51-21-10, SRM 51-25-10 AND HORIZON AIR EA 6-53-173. 2H72 4T RTA13NM 20030210001122003021000112NM 2003 2 10 QXEA0300060 120030110A5320 THRESHOLD BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX-MAIN CABIN DOOR BOTTOM THRESHOLD CORRODED AT SCREW HOLE. REPAIRED IAW DHC-84 SRM 51-42-05 AND 51-21-10. 2H72 4T RTA13NM 20030210001252003021000125NM 2003 2 10 QXEA0300068 120030107A7110 BRACKET BOMBDRDHC8 DHC8401 1390041NM RT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- CENTER BRACKET CRACKED BELOW UPPER DECK OF RIGHT HAND LOWER COWL 422AB. REPAIRED IAW DHC-8 400 SRM 71-61-01, 71-61-01 AND RD 8/4-71-016. 2H72 4T RTA13NM 20030210001302003021000130NM 2003 2 10 QXEA0300072 120030107A7110 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM LT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- LEFT HAND LOWER ENGINE COWL 412AB RIGHT HAND UPPER BYPASS DOOR SUPPORT BRACKET IS CRACKED. REPAIRED IAW DHC-8 400 SRM 71-61-01, 71-61-06 AND RD 8/4-71-016. 2H72 4T RTA13NM 20030210001362003021000136NM 2003 2 10 CALA0300028 120030210A5230 SKIN BOEING737 737524 1384721NM AFT CARGO DR GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914605 27318 INSPECTION FOUND GOUGE AND DENT IN AFT CARGO DOOR SKIN AT AFT SIDE. REPAIRED DOOR IAW SRM 53-00-01 AND 52-30-01. 2L72 4F RTA16WE 20030210001582003021000158NM 2003 2 10 AWXA200300115 120030125A531565528941 FLOORBEAM BOEING737 7373G7 138447JNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK 2 EACH 1/2" CRACKS WERE FOUND ON MAIN CABIN FLOOR BEAM BS 540, TRANSVERSE BEAM WEB IS CRACKED AT BOTH ENDS BL "0" AND LBL 24.75. MAINTENANCE REMOVED TRANSVERSE BEAM BS 540; FABRICATED A NEW REPLACEMENT TRANSVERSE BEAM PER DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030210001612003021000161NM 2003 2 10 UPS03440146 120030124A5330 SKIN BOEING747 747200 1384847NM STA 975-987 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C FX - LOWER FUSELAGE EXTERNAL SKIN EDGE FOUND CORRROSION CRACKED AT STA 983 STRG 42L. FX - LOWER FUSELAGE STA 975 TO STA 987 S42L EXTERNAL SKIN REPAIRED AS PER SRM 53-30-03 FIG.1. 2L74 4F RTA20WE 20030328000862003032800086EA 2003 3 28 COMA0360086 120030205A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01814CA 7387 FLIGHT 5174 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030210001622003021000162EA 2003 2 10 COMA0360083 120030206A301011513361 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01932CA14131 7038 FLIGHT 5631 ANTI-ICE DUCT WARNING DURING T/O.REPLACED THE ANTI-ICE CONTROLLER. 2L72 4F RTA21EA 20030210001632003021000163GL 2003 2 10 NSVA200300005 320030206A61111299600327 PROPELLER BEECH 1900 1900D 1154162CE HARTZLHCB4M HCB4M GL A NSVAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 EA27191CJ138612677 UE19 HJ89A During climb out from LGA, @ approximately 1000 ft., crew noted that a ring of sparks were coming from the RH engine. With engine indications normal crew reduced power-sparks continued. In flight emergency was declared-air return to LGA. Aircraft landing was uneventful. Upon taxi to gate, maintenance concluded that sparks were coming from prop blade(s). Upon closer examination, maintenance noted a heating element on one blade had burn marks. Suspect de-ice boot was arcing. R&R prop. Op's check good. Aircraft returned to service. 2L72 4T RTA24CE 6 CP56GL 20030207001092003020700109NM 2003 2 7 03FDEA00068 120030122A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 AFT CARGO BAY BS 950F FRAME IS DENTED ABOVE STR 26L. FOUND FRAME OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION OF FRAME, AND REPAIRED WITH DOUBLER. WORK DONE IAW SRM 51-40-3 FIG 1. REMOVED DAMAGED AREA OF FRAME FED-EX EA 7-5310-68168. 2L73 4F RTA3WE 20030129000812003012900081SW 2003 1 29 HEEA083985 120030117A7810407062021101 DUCT BELL 407 407 1182206SW EXHAUST CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 EXHAUST DUCT IS CRACKED NEXT TO BLOWER HOUSING. 1G71 3U O H2SW 20030129000992003012900099SW 2003 1 29 HEEA083992 120030117A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20030129001052003012900105SW 2003 1 29 HEEA083994 120030117A5200407064807103 SUPPORT BELL 407 407 1182206SW ENG BAY DOOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 ENGINE BAY DOOR BRACE MOUNTING HOLE ELONGATED. 1G71 3U O H2SW 20030129001172003012900117SW 2003 1 29 HEEA083999 120030117A7810407065203101 DUCT BELL 407 407 1182206SW EXHAUST SYS CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 EXHAUST DUCT CRACKED. 1G71 3U O H2SW 20030401001052003040100105NE 2003 4 1 DHL2003803001 220030124A7261 B-NUT DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE NR 4 ENGINE OIL CRACKED A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO01803DH 46123 NR 4 ENGINE LOST 4 QUARTS OF OIL IN FLIGHT FROM MEX APPROXIMATELY 1/2 QUART EVERY HALF HOUR. FOUND OIL TUBE SUPPLY TGB CRACKED AT B-NUT. REMOVED FOR FABRICATION. NR 4 ENGINE QUIT ON DESCENT. OIL PRESSURE AND TEMPERATURE NORMAL. ENGINE CONTINUED WINDMILLING. N2 INCREASED TO 80 PERCENT AFTER FLAMEOUT THEN OSCILLATED. REF ITEM 3P LOG PAGE 326249, NR 4 ENGINE QUIT ON DESCENT. OIL PRESSURE AND TEMPERATURE NORMAL. ENGINE CONTINUED WINDMILLING. N2 INCREASED TO 80 PERCENT AFTER FLAMEOUT THEN OSCILLATED. PERFORMED ENGINE PERFORMANCE RUN AND SHEET. ALL PARAMETERS NORMAL. NASH PUMP PRESSURE NORMAL PER 71-00-00, DC-8 JRH CHAPTER 11 ITEM 3P LOG PAGE 326249 STILL OPEN. 2L74 4F4 FRT4A25 E2GL 20030129001482003012900148NM 2003 1 29 DHL2003751003 120030127A33501000679 BATTERY BOEING727 727264 138408MNM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01751DH 22982 1) COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE.2) REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IAW B727 MM 33-50-01. OPS CHECKED GOOD. 2L73 4F A3WE 20030129001522003012900152EU 2003 1 29 HEEA084004 120030113A2840S1120021090 PRESSURE SWITCH AEROSPAS355 AS355* EU COCKPIT WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03975AE 2777 FUEL PRESSURE CAUTION LIGHT DOES NOT FUNCTION TEST CORRECTLY. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030129001532003012900153 2003 1 29 HEEA084005 420030114A34570110005400 GPS BOLKMS105 BO105S 5626006EU COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03135AE S838 PILOT REPORTS GPS IS INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H3EU 20030129002182003012900218NM 2003 1 29 QXEA0300131 120030129A5270 LATCH BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DIRTY A QXEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM09412QX 4059 FCA - FLIGHT 2347 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE CREW GOT A FUSELAGE DOOR WARNING LIGHT FOR THE FORWARD BAGGAGE DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE LATCHING MECHANISM STICKING. THE LATCHING MECHANISM WAS CLEANED AND LUBED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030206001792003020600179NM 2003 2 6 F3LA200300021 120030122A5320 SHIM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON TOP SIDE OF THREE INTERCOSTALS BETWEEN STA 986.5 AND 1006. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS. FOUND SHIM OUT OF LIMITS PER SRM 53-60-51. FABRICATED REPLACEMENT SHIM PER EA 53-737-193. INSTALLED SHIM AND SUPPORT PER SRM 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030206001802003020600180NM 2003 2 6 F3LA200300022 120030122A5320 SHIM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED ALL INTERCOSTALS BETWEEN STA 986.5 AND 967 CORRODED ON TOP SIDE. BLENDED CORROSION FROM FLOOR SUPPORTS/INTERCOSTALS. FOUND NO CORROSION AT STA 967 TO 986.5, BL 0. FLOOR SUPPORT SHIMS AT LBL 15.5 AND RBL 15.5 FOUND TO BE OUT OF LIMITS PER SRM 53-60-51, FIG. 101. FABRICATED SHIMS PER EA 53-737-198. INSTALLED SHIMS TO FLOOR SUPPPORTS AND REINSTALLED FLOOR SUPPORTS PER SRM 51-40-02. 2L72 4F RTA16WE 20030130000432003013000043EA 2003 1 30 COMA0360057 120030128A301032144424 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA L/H MALFUNCTIONED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01811CA4543 7380 FLIGHT 5749 LEFT WING ANTI ICE DUCT WARNING.REPLACED THE L/H MODULATING SHUT OFF VALVE. 2L72 4F RTA21EA 20030410002442003041000244NM 2003 4 10 F3LA200300026 120030122A5320 SHIM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON TOP SIDE OF THREE INTERCOSTALS BETWEEN STA 951 AND 967, INBOARD OF L-2 DOOR. FOUND CORROSION ON SHIM OUT OF LIMITS. FABRICATED AND INSTALLED REPLACEMENT SHIM PER SRM 53-60-51, 51-40-02, FIG 12, AND EA 53-737-193. 2L72 4F RTA16WE 20030130000772003013000077NM 2003 1 30 P5CA0300731 120030120A5730NONE PANEL BOEING747 7472U3B 1384846NM L/H WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 DELAMINATION FOUND L/H WING LEADING EDGE TOP PANEL AT FSSD 1550 (O/B MOST). PANEL REPAIR CARRIED OUT PER SRM 51-40-12 & SRM 51-30-20. 2L74 4F RTA20WE 20030130000782003013000078NM 2003 1 30 P5CA0300733 120030122A5210NONE SKIN BOEING747 7472U3B 1384846NM 1 R/H DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 EVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 R/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN REPAIR CARRIED OUT IAW SRM 52-10-02, FIG. 9. 2L74 4F RTA20WE 20030130001492003013000149EU 2003 1 30 MALA030136 120030126A5320 WEBBING SAAB SF340 340B 7860101EU A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING E-CHECK IN CWA, WEBBING AT STA 288-294 HAS CORROSION. MAINTENANCE REPLACED WEBBING. RELEASE DATE 1/28/03. REF 409 #175563 FOR DETAIL. 2L72 4T RTA52EU 20030130001612003013000161NM 2003 1 30 F3LA200300009 120030117A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CABIN FLOORBEAM AT STA 987.5, RBL 24.25 TO LBL 45.50, SHOWED SIGNS OF CONTAMINATION AND BLUE WATER CONTAMINATION. BLENDED CORROSION ON FLOORBEAM UPPER CAP AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-51, FIG 101. FABRICATED AND INSTALLED UPPER CAP PER SRM 53-00-51, FIG 202, AND SOPM 20-41-02. 2L72 4F RTA16WE 20030130001672003013000167NM 2003 1 30 AWXA200300087 120030129A3350BMS13311122 WIRE BOEING757 7572S7 1384962NM SEAT ROW 17 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW0 0 23321 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOUND UNDER THE SEAT ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030130001682003013000168NM 2003 1 30 F3LA200300033 120030127A5320 MOUNT BRACKET BOEING737 7373M8 1384615NM STA. 989 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT GALLEY MOUNT BRACKET CORRODED AT STA. 989, RBL 30. FABRICATED AND INSTALLED REPLACEMENT BRACKET PER EA 53-737-19C, STEP 1, SRM 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030331001182003033100118NM 2003 3 31 DHL2003726001 120030125A2612 FIRE DETECTOR BOEING727 727228 1384083NM APU BAY WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01726DH 20409 APU FIRE WARNING WILL NOT TEST. TROUBLESHOT SYSTEM, VERIFIED INTEGRITY OF THE SENSOR/RESPONDER, TEST SWITCH, OPERATING POWER UNIT, AND WIRING UP TO SENSOR/RESPONDER PER B727 MM 26-15-00. PLACED ITEM ON DEFERRAL, DMI NR 11766, PER MEL 26-11-1 C. 2L73 4F RTA3WE 20030131001492003013100149SO 2003 1 31 C2XA03BT024 120030130A33501317 LAMP EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2712924 145311 BTV--CO2002, DURING 3A INSPECTION MAINTENANCE FOUND EMERGENCY EXIT LIGHT OVER RIGHTHAND ESCAPE HATCH (WING) TO BE INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AS NECESSARY IAW EMB145 AMM #33-50-07. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20030131001552003013100155EU 2003 1 31 CA030108010 120030107A2720 SHAFT BAG JETSTMJETSTM3212 1500217EU GARRTTTPE331TPE33112UHR WP ROTOL R333 R333482F12 GL RUDDER PEDAL LOOSE W K NONE O OTHER ININSP/MAINT 1 CA 1227412274 (CAN) DURING BRIDGING INSPECTION, FOUND THAT THE CO-PILOTS LT RUDDER PEDAL TORQUE SHAFT, TORQUE LEVER ASSY. VERY LOOSE. FASTENERS ATTACHING BOTH ASSY'S LOOSE AND ELONGATIN G TORQUE TUBE HOLES. VISUALLY INSPECTED AND REPAIRED ASSY'S AS REQUIRED. NEW OVERSIZE FASTENERS INSTALLED. DUPLICATE INSPECTIONS CARRIED OUT. 2L72 4T4 TRTBA15CAA E4WE 6 CP61GL 20030131001682003013100168NM 2003 1 31 UPS03240104 120030107A5310 SHEAR TIE BOEING727 72722C 138400FNM BS 322 BL 0 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI FLOOR BEAM SHEAR TIE CRACKED AT BS 322 APPROX AND BL0 FLOOR BEAM SHEAR TIE AT BS 322 AND BL 0 REPAIRED IAW SRM 53-10-8 FIG 6 2L73 4F A3WE 20030131001742003013100174NM 2003 1 31 UPS03240114 120030114A5310 STRINGER BOEING727 72722C 138400FNM AIRSTAIR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI CRACK IN AIRSTAIR CENTRE STRINGER AT LWR END OF 2ND BAY FROM TOP OF STAIR REPAIR CARRIED OUT AS REQUIRED IAW SRM 53-10-3 2L73 4F A3WE 20030131001752003013100175NM 2003 1 31 UPS03240116 120030106A5330 SKIN BOEING727 72722C 138400FNM BS 360 S4R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI 5MM CRACK FOUND PROPAGATING FROM THE FASTENER I/B OF STR.4R AT BS 36 0 AFT SKIN AFT SIXTH FASTENER ROW REPAIR CARRIED OUT IAW EO B727-5310-1371 7 DRAWING 69-62161 2L73 4F A3WE 20030131001772003013100177NM 2003 1 31 UPS03240122 120030103A5310 FRAME BOEING727 72722C 138400FNM BS 930 R/H W/W CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI CRACK FOUND ON BS 930 FRAME R/H W/W REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-04 FIG 1, 53-10-3 FIG 1, DRAWING 65C15732, 65-16336 AND SRM 51-30-05 2L73 4F A3WE 20030131001802003013100180NM 2003 1 31 UPS03240128 120030109A5753 FLAP TRACK BOEING727 72722C 138400FNM NO.3 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C+SI NO.3 FLAP TRACK HAS CORROSION ON PAD B, BETWEEN HOLES G AND F AND AL SO ON THE LWR FLANGE AROUND HOLE G. REPAIRED IAW SMRO EO 2003-003-010 AND EO 2003-003-003. 2L73 4F A3WE 20030131001832003013100183NM 2003 1 31 ANCF200300003 120030130A5600141T480013 WINDSHIELD BOEING767 767383 1385214NM CRACKED W ANCFD RETURN TO BLOCK O OTHER CRCRUISE 1 SO23984AN 24357 DURING FLIGHT WAS FOUND 1L WINDOW CRACKED (windshield outer panel). AIRCRAFT RETURNED TO BOGOTACORRECTIVE ACTION:1L WINDOW WAS REPLACED IN ACCORDING TO AMM 56-11-01 PAG 401 TO 411, AND WINDOW HEATING SYSTEM CHECKED IAW AMM-30-41-00/501 WITH SATISFACTORY RESULTS 2L72 4F RTA1NM 20030131001852003013100185EA 2003 1 31 SWIA200311745 120030127A322016050105 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07587SW 7062 AFTER TAKE OFF FROM OKC THE NOSE GEAR DISAGREEMENT WARNING WENT OFF, PERFORMED QRH PROCEDURE AND RETURNED FOR LANDING AT OKC. REMOVED AND REPLACED NLG IAW 32-21-01. 2L72 4F RTA21EA 20030211000012003021100001EA 2003 2 11 SWIA200311763 120030204A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERG EXIT SIGN CONTAMINATED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07413SW 7102 LEFT EMERGENCY LIGHT (FORWARD LOWER) EXIT SIGN DOES NOT ILLUMINATE. CLEANED ELECTRICAL CONNECTOR ON LEFT EMERGENCY DOOR EXIT SIGN. OPS CHECK GOOD. 2L72 4F RTA21EA 20030211000032003021100003EA 2003 2 11 03024621 120030124A3260 TARGET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG DAMAGED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27621BR 7186 NLG DISAGREE LIGHT ILLUMINATED ON TAKEOFF. REPAIRED TARGET BRACKET, OPS CHECKED GOOD. 2L72 4F4 FRTA21EA E15NE 20030211000042003021100004EA 2003 2 11 03025663 120030125A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LAVATORY ACTIVATED A VTZAK NONE J WARNING INDICATION CRCRUISE 1 EA27663BR 7274 LAV SMOKE DETECTOR WARNING IN FLIGHT WITH SYSTEM DEFERRED, INSPECTED APU, ACM UNITS AND ASSOCIATED DUCTING/VALUES, RAN ENGINES WITH APU RUNNING AND NO DEFECT NOTED. 2L72 4F4 FRTA21EA E15NE 20030211000122003021100012NM 2003 2 11 2003UALA00131 120030130A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29567UA 26673 DENT LEFT SIDE OF A/C BETWEEN STRINGER 14 & 15 AT STATION 1615. A OVER Y IS 32. DIA 3-64 BY 1.5 INCHES. HFEC ACCOMPLISHED/NO CRACKS NOTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20030320001402003032000140NM 2003 3 20 2003UALA00132 120030130A5414 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 NR 1 PYLON STRUT OUTBOARD SIDE SKIN IS CRACKED AT FORWARD ACCESS HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH DOUBLERS. 2L72 4F4 FRTA2NM E17NE 20030212000312003021200031NM 2003 2 12 AUS20030044 120030120A5315 FLOORBEAM BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLOORBEAM CORRODED AT BS 950 AND RBL 70. 2L73 4F4 FRTA3WE E2EA 20030327000922003032700092SO 2003 3 27 C2XA03BT031 120030211A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145 3260210SO LAVATORY FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714960 145100 EWR---CO2260, LAV SMOKE WARNING PASSING THROUGH 7500 FEET. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR IAW EMB145 AMM 26-44-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030212000652003021200065EA 2003 2 12 CA030116007 120030116A2701CR431364 RIVET CNDAIR CNDAIRCL215 CL2151A10 1900320EA PWA R2800 CA3 52026NE HAMSTD43E 43E60 NE CONTROL COLUMN WORN W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) ALL RIVETS LOOSE IN CAPTAIN`S CONTROL COLUMN. RIVETS WITH INCORRECT LENGTH INSTALLED FROM FACTORY. 2H72 4R4 RRTA14EA E231 6 CP871 20030212000682003021200068EA 2003 2 12 CA030117004 120030115A27106007510017 PCU CNDAIRCL604 CL604 1900301EA GE CF34 CF343B1 NE RT AILERON LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) WHILE IN THE HANGAR, HYDRAULIC FLUID WAS NOTICED ON THE WING UNDERSIDE LEAKING FROM THE AILERON PCU DRAIN HOLES. DURING SUBSEQUENT LEAK CHECKS WITH THE PCU INSPECTION PANEL REMOVED NO SIGNIFICANT LEAKAGE NOTICED. DURING SHORT TURN AROUND FLIGHTS NO EVIDENCE OF LEAKAGE NOTED, HOWEVER, WHEN THE A/C SAT FOR MORE THAN A COUPLE OF HOURS AFTER A HIGH LEVEL, COLD FLIGHT AND / OR REMAINED OUTSIDE IN 0 DEGREE CELCIUS WEATHER THE LEAKAGE WAS AT ITS WORST. 2L72 4F4 FRTA21EA E15NE 20030212000722003021200072EA 2003 2 12 CA030119003 120030110A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) EN ROUTE, LEFT WINDOW CRACKED. FERRY FLIGHT PERFORMED.LEFT WINDOW REPLACED PER AMM. 2L72 4F4 FRTA21EA E15NE 20030212000742003021200074EA 2003 2 12 CA030119006 120030110A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) UPON LANDING IT WAS NOTICED THE CAPT'S SIDE WINDOW WAS CRACKED. CAPT'S SIDE WINDOW REPLACED AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030212000772003021200077EU 2003 2 12 WRNA200300003 120030207A2700NSA931300030 CIRCUIT BREAKER AIRBUS300 A300B4203 3930306EU COCK PIT UNSERVICEABLE A WRNAK NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO05820SC 154 Flight control servo control lever lock circuit breaker tripsCorrective Action: R&R'd circuit breaker I/A/W MM 20-16-00 Op's check good 2L72 4F RTA35EU 20030212000792003021200079CE 2003 2 12 CA030120003 120030120A5500 FRAME CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE EMPENNAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACKS FOUND AT FUSELAGE FRAME RIVETS FOR VENTRAL FIN POSSIBLE REASON RIVET SPACING TO SMALL CRACKS AT RIVETS WHERE FRAME AND VENTRAL FIN JOIN. 1H71 3T3 T A37CE E4EA 20030212000822003021200082NM 2003 2 12 CALA0300031 120030210A5320 STIFFENER BOEING737 7373T0 1384582NM STA 1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND STIFFENER CORRODED AT LEFT SIDE AND RIGHT SIDE OF BL0 BELOW FLOOR LINE AT STA 1016. REPAIRED IAW EA 5310-04045, POS 2. 2L72 4F RTA16WE 20030212000872003021200087NM 2003 2 12 CALA0300038 120030211A5230 SKIN BOEING737 7373Q8 1384670NM BS 827 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914384 26313 INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED AT BS 827. REPAIRED IAW SRM 52-00-01, FIGURE 202. 2L72 4F RTA16WE 20030212000952003021200095NM 2003 2 12 AWXA200300120 120030206A531369353521 TIE CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 5/16" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 2 L/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 2 L/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 38, FIG. 8, AND SRM 51-40-05, PG. 1-4, FIG. 1-2, PG. 7, FIG. 4. 2L72 4F RTA16WE 20030212000982003021200098NM 2003 2 12 AWXA200300124 120030204A531265163007 WEB BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW0 0 23713 MCN - MAJOR REPAIR - DURING C-16 CHECK , A BULKHEAD WEB WAS FOUND CRACKED AT B.S. 178. CRACK WAS CONFIRMED WITH HFEC. MAINTENANCE REMOVED DAMAGED AREA OF BULKHEAD WEB BS 178; FABRICATED A REPAIR DOUBLER, FILLER, AND 3 EACH SHIMS; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG. 287-288J, FIG. 211. 2L72 4F RTA16WE 20030212001052003021200105NM 2003 2 12 PCAA0302040 120030210A33506038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM POSITION 300 INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13836EX 297 DURING ROUTINE MAINTENANCE VISIT LEFT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. EMERGENCY LIGHT BATTERY AND POWER SUPPLY WERE REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030213000012003021300001NM 2003 2 13 CA030120009 120030120A2910DSC252B40124 HOSE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM LEAKING W A UNSCHED LANDING K FLUID LOSS CLCLIMB 1 CA 3906139061 (CAN) AFTER DEPARTURE FLIGHT CREW REPORTED LOSS OF NR 2 HYDRAULIC SYSTEM FLUID. AIRCRAFT RETURNED TO DEPARTURE AIRPORT FOR NORMAL LANDING. ( ALTERNATE GEAR EXTENSION USED) INSPECTION FOUND NLG UPLOCK/RETRACTION ACTUATOR FLEX HOSE LEAKING THROUGH BRAID ON HOSE CAUSING THE LOSS OF HYDRAULIC FLUID . HOSE DOES NOT SHOW ANY PHYSICAL DAMAGE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030213000222003021300022EU 2003 2 13 CA030125001 120030123A6210117151311 BLADE BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101750B1 41560NE MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CHORDWISE CRACK FOUND ON RED MAIN ROTOR BLADE 100MM CUFF S/N 806, 80MM OUTBOARD OF BLADE FITTING. MAIN ROTOR BLADES (4) REPLACED, MANUFACTURER NOTIFIED. 1G72 3U3 UNCH13EU E5NE10 20030213000302003021300030EA 2003 2 13 CA030129003 220030113A8520SL18840 CAMSHAFT HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA ENGINE DAMAGED W O OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 CA L3490836A (CAN) THE ENGINE HAD 6 HOURS TTSO. THE PILOTS NOTICED AN ENGINE VIBRATION, AND STARTING WAS BECOMING EVER MORE DIFFICULT. THE AME THEN PROCEEDED IN REPLACING THE TWO MAGNETOS AND THE CARBURETOR. AFTER A FEW HOURS OF FLIGHT THE PROBLEM PERSISTED. THE AME THEN CONDUCTED AN INTERNAL INSPECTION, IT WAS REVEALED THAT THE INTAKE VALVE IN CYLINDER NR 1 AND THE EXHAUST VALVE IN CYLINDER NR 3 WERE NOT OPENING COMPLETELY. AN INSPECTION OF THE CAMSHAFT WAS CARRIED OUT, 2 LOBES OF THE CAM WERE DAMAGED. THE ENGINE WAS REMOVED FROM THE HELICOPTER AND THEN THE CAMSHAFT WAS REPLACED UNDER MANUFACTURERS WARRRANTY. 1G71 3O3 OO 4H12 E286 20030213000392003021300039NM 2003 2 13 CA030131004 120030124A5230AE4664100 BLOCK BOEING727 727200 138407ENM CARGO DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FOUND MINOR CRACKING OCCURRING FROM THE LOCK WIRE HOLE ON LOWER PIVOT BLOCK OF CARGO DOORS. WE HAVE REPLACED APPROXIMATELY 10 OF THOSE PIVOT BLOCKS OVER A 2-3 YEAR PERIOD. THE MANUFACTURER DOES NOT PUBLISH ANY LIMITS OR REPAIR STANDARD. MANUFACTURER HAS BEEN ADVISED OF THIS PROBLEM. 2L73 4F RTA3WE 20030213000452003021300045GL 2003 2 13 CA030204014 220030120A7320206064713101 LEVER BELL 206 206L 1181522SW ALLSN 250C 250C28 03013GL FUEL CONTROL FAILED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) REQUIRED BOLT PN NAS6604D8 (AS PER 206L IPC) WOULD NOT FIT IN EXISTING HOLE OF FUEL CONTROL LEVER PN 206064713101 WITHOUT ENLARGING HOLE. 1G71 3U3 U H2SW E1GL 20030213000462003021300046NE 2003 2 13 CA030204015 120030130A6520B538A3 CHIP DETECTOR SKRSKY SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL T/R GEARBOX SHORTED W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA A126000220 (CAN) IN CRUISE FLIGHT AT 5000 FT, TAIL ROTOR GEARBOX HOT/CHIP LIGHT CAME ON. FLIGHT CREW ASKED FOR AND RECEIVED IMMEDIATE DESCENT INTO CYYJ. THE AIRCRAFT LANDED AND WAS SHUTDOWN NORMALLY. THE ENGINEER REMOVED CHIP PLUG AND FOUND NO METAL. WHEN REINSTALLED THE CAUTION LIGHT CAME ON AGAIN. A NEW TEMP/CHIP PLUG WAS INSTALLED. NO CAUTION LIGHT CAME ON. THE AIRCRAFT WAS GROUND RUN AND LEAK CHECKED AND NO FAULT FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20030213000542003021300054SW 2003 2 13 CA030210004 120030130A2910206076062003 SERVO BELL 206 206L 1181522SW ALLSN 250C 250C20R2 GL HYD SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) HYDRAULIC SERVO LEAKING. REMOVED FOR REPAIR. 1G71 3U3 U H2SW E4CE 20030213000562003021300056NM 2003 2 13 EVAS092006 120030205A5312 BULKHEAD DOUG MD11 MD11F 3023600NM FUSELAGE CRACKED W QOCFK NONE O OTHER ININSP/MAINT 1 WP0316108 48778 DURING CARGO LOADING , 2.5 INCH DIAMETER HOLE FOUND WITH RADAL CRACK ON LT LOWER CORNER OF PRESSURE BULKHEAD. PERFORM REPAIR BY FINGER DOULBER AND TEE AT STATION 2007 X=-10 AND X=-70 RESPECTIVELY PERFORM CABIN PERSSURE LEAKAGE CHECK. 2L73 4F RTA22WE 20030213000572003021300057NE 2003 2 13 00072 220030118A7200 ENGINE LEAR 24 24B 5170306CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05233TW 24B221 251013A PILOT REPORTED ENGINE LT FLAMEOUT DURING CLIMB AT FL400. DESCENDED AND NORMAL RESTART AT FL220, RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE. WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE COMPLIED WITH FLAMEOUT FLOW CHART FROM CJ610 MM SEI 186 FIG 101, NO DEFECTS NOTED. 2L72 4J4 J A10CE 1E16 20030213000622003021300062EU 2003 2 13 00077 120030205A7930 CONNECTOR AMD FALC20FALCONE 2720305EU OIL TEMP IND DIRTY E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05285TW 285 PILOT REPORTED OIL TEMP INDICATION ON LT ENGINE HIGHER THAN NORMAL, PILOT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REMOVED AND CLEANED OIL TEMP CONNECTOR PLUG RESEATED AND OPS CHECKED NORMAL. 2L72 4F A7EU 20030213000642003021300064NE 2003 2 13 0065187 320030123A61117826853 BLADE EMB 120 EMB120 3260201SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE PROPELLER CRACKED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 857358 PROPELLER BLADE CRACKED IN LEADING EDGE SHIELD. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20030213000722003021300072NM 2003 2 13 03006 120030127A3260 WARNING LIGHT BOEING747 7472B4B 138481BNM COCKPIT ILLUMINATED A KCSAO OTHER J WARNING INDICATION CLCLIMB 1 GL23713CK 21099 AFTER GEAR RETRACTION, WITH GEAR LEVER OFF, BOTH RT BODY DOOR OPEN LIGHTS ILLUMINATED IN PRIMARY AND ALTERNATE POSITIONS. 2L74 4F RTA20WE 20030213000732003021300073EU 2003 2 13 0301161 120030116A61201103P2671 PRESSURE SWITCH SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE AUTOCOURSEN FROZEN A UHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 NE03158SD 158 FLT 4476, DURING TAKEOFF ROLL, DID NOT GET AUTOCOURSEN ARM LIGHT. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED GROUND RUNS IAW MM. AFTER AIRCRAFT WARMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030213000872003021300087WP 2003 2 13 ABXA030072 120030126A5230995766412 WEB DOUG DC9 DC941 302207NWP FWD. CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23957AX 47759 FORWARD LOWER CARGO DOOR UPPER AFT HINGE INTERCOSTAL WEB CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20030213000942003021300094EA 2003 2 13 COMA0360091 120030207A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01783CA 7315 FLIGHT 5718 FLAPS FAILED AFTER LANDING.COULD NOT DUPLICATE. INSPECTED FLAPS PER AD 98-20-01 - NO FAULTS FOUND. 2L72 4F RTA21EA 20030213000992003021300099EA 2003 2 13 COMA0360096 120030209A33506464 POWER CABLE CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR UNRELIABLE A COMAO OTHER O OTHER ININSP/MAINT 1 SO01914CA 7012 FLIGHT 5919 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED POWER STRIP AT ROW 1. 2L72 4F RTA21EA 20030213001072003021300107EA 2003 2 13 COMA0360098 120030210A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01986CA7084 7174 FLIGHT 5109 GEAR DISAGREE WARNING DURING RETRACTION.REPLACED THE PSEU 2L72 4F RTA21EA 20030213001082003021300108EA 2003 2 13 COMA0360099 120030210A3030 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01965CA 7131 FLIGHT 5554 LT AOA, LT STATIC, LT PITOT HEAT CAUTION.RESET C/B, COULD NOT DUPLICATE PROBLEM, SYSTEM TEST NORMAL. 2L72 4F RTA21EA 20030213001122003021300112NM 2003 2 13 2003F00083 120030106A33507024091007 LENS BOEING737 73783N 13844HINM GE CFM56 CFM56* 13802NE CABIN MISSING A AMTAK NONE O OTHER ININSP/MAINT 1 GL11303TZ 28648 (ORIGINAL CLOSED) EMERGENCY PATH FLOOR PROXIMITY LIGHT AFT OF RIGHT NR 2 OVERWING EXIT MISSING LENS; INSTALLED EXIT LENS AS REQUIRED. OK FOR SERVICE.. 2L72 4F4 FRTA16WE E2GL 20030625000752003062500075NM 2003 6 25 F3LA200300049 120030129A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT RBL 3 CORRODED. FOUND TO BE OUT OF LIMIT PER SRM 53-60-53. REPLACED FLOOR SUPPPORT CHANNEL PER SRM 51-40-02. 2L72 4F RTA16WE 20030214000092003021400009NM 2003 2 14 2003F00094 120030101A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE CABIN DISCONNECTED G K NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 (ORIG-CLOSED) DURING SCHEDULED MAINTENANCE EMERGENCY EGRESS LIGHTS AT ROW 29 INOPERATIVE. MAINTENANCE RECONNECTED WIRE AT EGRESS LIGHT ASSEMBLY ROW 29. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA2NM A12EU 20030214000392003021400039NM 2003 2 14 CALA0300043 120030206A5330 SKIN BOEING737 7373T0 1384582NM STA 727D-727E CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914358 23943 INSPECTION FOUND A 1.5" CRACK IN FUSELAGE SKIN BETWEEN STA 727D +9.9 AND STA 727E JUST ABOVE S23L. THE SKIN WAS REPAIRED IAW ECRA 5330-03205. 2L72 4F RTA16WE 20030214000412003021400041WP 2003 2 14 CALA0300046 120030213A5311 FRAME DOUG DC9 DC982 3022082WP STA 1418 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0972822 49482 INSPECTION FOUND A 1" CRACK IN FUSELAGE FRAME AT STA 1418, LONGERON 1L. REPAIRED IAW SRM 53-03, PAGE 5. 2L72 4F A6WE 20030625000792003062500079NM 2003 6 25 F3LA200300051 120030129A5320 SHIM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA 312 AND 328, LBL 10, CORRODED. REMOVED INTERCOSTAL BETWEEN STA 312 AND 328 AND FOUND CORROSION TO BE ON SHIM ONLY. REMOVED SHIM, FABRICATED AND INSTALLED NEW SHIM PER SRM 51-40-02, SRM 51-40-02 AND EA 53-737-195. 2L72 4F RTA16WE 20030625000782003062500078NM 2003 6 25 F3LA200300052 120030129A5320 SHIM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL, FLOORBEAM AND HAT SECTION CORRODED BETWEEN STA 328 AND STA 344, LBL 11 TO RBL 12. REMOVED INTERCOSTAL BETWEEN STA 328 AND STA 344 AND FOUND CORROSION TO BE ON SHIM ONLY. REMOVED SHIM, FABRICATED AND INSTALLED REPLACEMENT SHIM PER SRM 51-40-02, SRM 51-40-02 AND EA 53-737-195. 2L72 4F RTA16WE 20030214000482003021400048NM 2003 2 14 P5CA0300758 120030203A5320NONE SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LEVEL 1 CORROSION FOUND ON UPPER LOBE MAIN DECK SEAT TRACK LBL 11 BWTN STA 1940-1960. CORRODED PORTION SEAT TRACK REMOVED. REINFORCED WITH NEW SEAT TRACK PER SRM 53-11-25 FIG.7. 2L74 4F A20WE 20030214000522003021400052SO 2003 2 14 C2XA03BT032 120030213A335066364 LIGHT EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2713955 145075 BTV---CO3180, MAINTENANCE FOUND "AFT EMERGENCY LIGHT STRIP INOPERATIVE, REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP IAW EMB145 MM 33-50-12. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20030214000702003021400070NM 2003 2 14 DHL2003720002 120030214A26121014A POWER UNIT BOEING727 727228 1384083NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01720DH 19544 1) APU FIRE DETECTION SYSTEM WILL NOT RESET AFTER FIRE TEST - INTERMITTENT.2) REPLACED APU FIRE DETECTION OPERATING POWER UNIT. FIRE DETECTION SYSTEM RESETS CONSISTENTLY. APU OPERATION NORMAL. M/M 26-15-00. 2L73 4F RTA3WE 20030214000722003021400072WP 2003 2 14 ABXA030029 120030110A27613654074 LINK DOUG DC8 DC863F 302198FWP GROUND SPOILER BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 DURING SERVICE CHECK, FOUND THE NR 5 INBOARD GROUND SPOILER WITH 2 EACH CENTER CRANK ASSEMBLIES AND INBOARD SPOILER OVERCENTER LINK BROKEN. REMOVED THE LEFT WING NR 5 SPOILER PANEL AND REPLACED BOTH SPOILER CRANK ASSEMBLIES IAW AMM. OPS CHECKED GOOD. INSTALLED SPOILER PANEL NR5. OPS CHECKED GOOD. 2L74 4F 4A25 20030214000762003021400076WP 2003 2 14 ARWA20030102 120030119A324039069B VALVE DOUG DC8 DC862 3021970WP ANTI SKID INOPERATIVE A ARWAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO19802BN 45905 DURING TAXI, BEFORE TAKEOFF, ANTI SKID INOPERATIVE LIGHT ON WITH SWITCH IN (ON) POSITION. REMOVED AND REPLACED RT MAIN LANDING GEAR OUTBOARD ANTI SKID DUAL SERVO VALVE. BLED SYSTEM, OPS CHECKED AND FOUND NORMAL IAW MM. 2L74 4F 4A25 20030214000802003021400080WP 2003 2 14 ASAA0380052 120030105A5753593591929 RUB STRIP DOUG DC9 DC983 3022083WP T/E FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING FLAP FLEX JOINT UPPER PANEL CHAFE STRIPS WORN IN SEVERAL AREA. REPLACED RUB STRIP PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20030214000822003021400082WP 2003 2 14 ASAA0380054 120030105A361059363957 SUPPORT DOUG DC9 DC983 3022083WP PNEUMATIC SYS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, PNEUMATIC DUCT ANGLE SUPPORT CRACKED AT AFT END OF WHEELWELL IN KEEL BEAM. REPLACED ANGLE PER SRM 51-10-2 AND 51-10-4. (M) 2L72 4F RTA6WE 20030214000992003021400099EU 2003 2 14 0300153243 120030201A2131 CONTROLLER AIRBUS320 A320212 3930322EU GE CFM56 CFM56* 13802NE CABIN PRESSURE MALFUNCTIONED A NWAAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL01343NW 387 DURING CLIMB RECEIVED CABIN PRRESSURE EXCESS CABIN ALTITUDE MESSAGE AT 10,000 FT. LEVELED OFF AT 11,000 FT AND MESSAGE WENT AWAY. CLIMBED TO 12,800 FT AND MESSAGE RETURNED. LEVELED OFF AT 12,000 FT AND MESSAGE CLEARED FOLLOWED SHORTLY BY THE SAFETY VALVE OPENING, MASKS DEPLOYED. WHILE RETURNING, RECEIVED CAB PR SYS 1 FAULT MESSAGE. TEST OF CABIN PRESSURE CONTROLLER 1 AND 2 CHECKED GOOD. REPLACED OUTFLOW VALVE AND OPERATIONALLY TESTED GOOD. DISCREPANCY RETURNED DURING FERRY FLT. REMOVED DUST CAP FROM THE AMBIENT PRESSURE PORT OF CABIN PRESSURE CONTROLLER 1. SYSTEM TESTED GOOD AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA28NM E2GL 20030214001002003021400100NM 2003 2 14 0300216636 120030205A3350 LIGHT BOEING747 747251B 1384892NM PWA JT9 JT9D* NE CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01636US 23547 DURING LINE CHECK FOUND HALF OF THE LT AISLE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRE AND OPERATIONAL CHECK GOOD. 2L74 4F4 F A20WE E20EA 20030214001112003021400111WP 2003 2 14 ASAA0380059 120030106A5320S1242886 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, LONGERON SPLICE HAS CORRODED FASTENERS AT FS 1201. REPAIRED DAMAGED AREA PER SRM 53-01. (M) 2L72 4F RTA6WE 20030214001352003021400135EA 2003 2 14 03042624 120030211A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 During preflight inspection, the crew reported that the forward emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the forward emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030214001362003021400136NM 2003 2 14 P5CA0300765 120030207A304029155 CONTROLLER BOEING747 74746NF 13848BTNM 1R WINDOW FAULTY A P5CAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP23451PA 30809 AFTER TWO HOURS OF FLT SMOKE WAS OBSERVED COMING FROM RT SIDE COCKPIT. AOM PROCEDURE COMPLIED W/. SMOKE SOURCE TRACED TO LWR AREA OF NUMBER 1 RT WINDOW. WINDOW HEAT 1R SWITCHED OFF, SMOKE STOPPED. AREA OF GREASE WAS OBSERVED ALONG LWR PART OF WINDOW. REMOVED AND REPLACED 1R WINDOW HEAT CONTROL UNIT AS PER MM 30-41-01. OPS CHECKS NORMAL. 2L74 4F RTA20WE 20030216000072003021600007EU 2003 2 16 RAIA00302041 120030206A2730C850176 SENSOR JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03550HK1546615466 41039 5623-STL- LEFT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE LEFT STALL WARNING SENSOR. 2L72 4T RTA41NM 20030217000032003021700003SO 2003 2 17 C2XA03CL040 120030214A3350 CONNECTOR EMB 145 EMB145ER 3260211SO CABIN DIRTY A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2715941 145035 CLE FLIGHT#2025 THE CREW REPORTED EMERGENCY LIGHTING OVERHEAD IN FORWARD GALLEY WAS INOPERATIVE.MAINTENANCE INSPECTED AND CLEANED CONNECTOR FOR LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030217000042003021700004SO 2003 2 17 C2XA03CL041 120030214A3350 WIRE EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2716918 145397 IAH FLIGHT#2829 THE CREW REPORTED THE EMERGENCY EXIT LIGHT WAS INOPERATIVE.MAINTENANCE INSPECTED AND RECONNECTED WIRE FOR THE EMERGENCY EXIT LIGHT.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030217000052003021700005SO 2003 2 17 C2XA03CL042 120030216A2611 GROUND WIRE EMB 145 EMB145 3260210SO LAV LOOSE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2714960 145100 CLE FLIGHT#2131 THE CREW REPORTED A LAV SMOKE WARNING DURING CLIMB.THE CREW CONFIRMED NO SMOKE PRESENT.MAINTENANCE INSPECTED AND REPLACED LAV SMOKE DETECTOR PANEL.MAINTENANCE ALSO RESECURED A LOOSE GROUND WIRE ON THE LAV SMOKE DETECTOR.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030217000092003021700009NM 2003 2 17 UPS03440177 120030206A5210 FRAME BOEING747 747200 1384847NM DOOR #1R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C CRACK REVEALED AT PASSENGER DOOR #1R AT THE DOOR FRAMES FWD BOTTOM CORNER VERTICAL RADIUS. THE CRACK RUNNING UPWARD WITH LENGTH 3" LONG APPROX. AND A STOP HOLE DRILLED AT UPPER CRACK END. #1R DOOR FWD VERTICAL FRAME CRACKED AT RADIUS PREVIOUS STOP DRILLED C/OUT. HFEC C/OUT NIL CRACK BEYOND STOP DRILLED AND CRACKED FRAME PREVIOUS REPAIRED PER SRM 52-10-02 FIGURE 10. 2L74 4F RTA20WE 20030217000102003021700010NM 2003 2 17 UPS03540175 120030215A2560MXP21000 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01455UP 25476 INSPECTION TYPE:N/A CAPT. SMOKE GOGGLES LENSE CRACKED. REPLACED.CAPT. SMOKE GOGGLES. 2L72 4F RTA2NM 20030217000132003021700013NM 2003 2 17 AWXA200300146 120030213A5315BAC1520792 SEAT TRACK BOEING737 73733A 1384673NM MISALIGNED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW0 0 23634 LCQ - MAJOR REPAIR - DURING C-18 CHECK THE L/H OUTBOARD SEAT TRACK SPLICE WAS FOUND INTERFERING WITH THE SEAT ATTACH POINT BS 847. MAINTENANCE REMOVED SEAT TRACK FROM BS 807 TO BS 847, LBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-52, PG. 210, FIG. 204. 2L72 4F RTA16WE 20030218000042003021800004NM 2003 2 18 03041423 120030210A2120 SMOKE DORNERDO32 DO328300 NM PWA 306 PW306B NE COCKPIT DETECTED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27423FJ AFTER TAKE OFF, FROM ROA TO CVG; CREW REPORTED SMOKE IN FLIGHT DECK. AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 FRTA55NM E35NE 20030218000072003021800007NM 2003 2 18 03FDEA00085 120030105A5753ARC2515502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 SNRM N0566 - RT WING INBOARD T/E FLAP AT OUTBOARD SIDE OF THE FLAP SIDE OF THE HINGE PIVOT BORE HOLE FOUND CORROSION. ** S/D ** COMING 2L73 4F RTA22WE 20030218000122003021800012NM 2003 2 18 03FDEA00105 120030203A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 N01087) CORROSION ON FLOORBEAM ( BS 344, LBL 25 TO RBL 25, WL 208). REMOVED CORROSION FROM FLOORBEAM (BS 344 LBL 25 TO RBL 25) MATERIAL REMOVED .035 INCH X 1 X 20 INCH, O.T. .100 INCH DETERMINED TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED NEW UPPER CHORD AND REPAIR ANGLE SPLICES IAW SR 27-53-007. INSTALLED NEW UPEPR CHORD AND ANGLE SPLICES IAW SR 27-53-007. 2L73 4F4 FRTA3WE E2EA 20030218000132003021800013NM 2003 2 18 03FDEA00106 120030204A5315 FLOORBOARD BOEING727 727200 138407ENM PWA JT8 JT8D NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 N01110) FLOORBEAM UPPER FLANGE HAS A FIGURE EIGHT FASTENER HOLE. (BS 500, RBL 1, WL 208) REMOVED DAMAGED FLOORBEAM SECTION AND REPAIRED. (BS 500 FLOOR BEAM AT RBL 1, WL 208 IAW SRM 53-10-8 2L73 4F4 FRTA3WE E2EA 20030314000312003031400031NM 2003 3 14 03FDEA00115 120030207A5210 STRUCTURE BOEING727 727200 138407ENM PAX DOOR DAMAGED A FDEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO25480FE 21462 PASSING APPROX 10,000 FT MSL NOTICED CABIN VVI FLUCTUATED BETWEEN CLIMB AND DESCENT. AROUND 13,000 FT HEARD AND FELT 2 LOAD BANGS COMING FROM VICINITY OF FORWARD ENTRY DOOR. DOOR WAS DIFFICULT TO CLOSE AND OPEN. *S/D* REPAIRED L1 DOOR UPPER AFT CORNER PER SRM 52-10-1 & 51-40-4. NO OTHER ACTION WILL BE REQUIRED. 2L73 4F RTA3WE 20030218000422003021800042CE 2003 2 18 LX52003F00000 120030124A30801013810125 VALVE BEECH B300 B300 1159232CE PWA PT6 PT6A11 52043NE BRAKE DEICE STICKING B LX5RO OTHER O OTHER NRNOT REPORTED 1 GL19981LL 190 FL265 THERE IS A PERSISTANT PROBLEM WITH THIS SERIES BRAKE DEICE VALVE STICKING IN THE OPEN POSITION. THIS PROBLEM SEEMS TO BE GREATER DURING THE WINTER (EXTREME COLD) BUT IT DOES OCCUR AT ALL TIMES OF THE YEAR. 2L72 4T3 TRTA24CE E4EA 20030218000512003021800051SO 2003 2 18 2003F00107 220030210A7414BL6006061 MAGNETO CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO LEFT FAILED E DUFAK NONE L NO TEST ININSP/MAINT 1 GL27500FS 310R0630 826046 RECEIVED A FACTORY REBUILT ENGINE FROM TCM AND INSTALLED. DURING THE GROUND RUNS IT WAS DISCOVERED THAT THE LT MAGNETO WAS DEAD. FURTHER INSPECTION REVEALED THE PROBLEM TO BE IN THE MAGNETO ITSELF. A REPLACEMENT MAGNETO WAS ORDERED AND INSTALLED WHICH CHECKED OK. 1L72 3O3 O 3A10 E5CE 20030218000682003021800068NM 2003 2 18 AALA20021902 120030102A3397 WIRE BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21366AA 25193 DFW - DURING OVERNIGHT MAINTENANCE, PATH LIGHT AT SEAT 38H INOPERATIVE. REPAIRED EMERGENCY PATH LIGHTING WIRE AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030218000852003021800085NM 2003 2 18 AMTA200300141 120030124A2841 INDICATOR BOEING757 75723N 1384973NM COCKPIT MALFUNCTIONED A AMTAK NONE J WARNING INDICATION CRCRUISE 1 GL11526AT 30735 FLT 438 - AT LEVEL OFF FOR CRUISE RIGHT FUEL QUANTITY INDICATOR WENT BLANK. HAD LOWER STATUS MESSAGE 'FUEL QUANTITY INDICATOR'. FUEL QUANTITY TEST OK. PERFORMED FIM 28-41-00 FIG 104, NO FAULTS FOUND, OK FOR SERVICE. (M) 2L72 4F RTA2NM 20030218000862003021800086NM 2003 2 18 AMTA200300151 120030128A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 FOUND L1 EXTERIOR EMERGENCY DOOR LIGHT INOPERATIVE. CHANGE BATTERY PACK IAW 33-51-07-902-003-001. (M) 2L72 4F RTA2NM 20030218001172003021800117NM 2003 2 18 DHL2003780002 120030218A3350 LIGHT BOEING727 727223 1384074NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01780DH 22006 1) FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT CHECK.2) REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT IAW M/M 33-50-01. OPS CHECKED GOOD. 2L73 4F A3WE 20030218001322003021800132EU 2003 2 18 DHL2003365001 120030218A2750615500017 INDICATOR AIRBUS300 A300B4203 3930306EU A DHLAO OTHER O OTHER APAPPROACH 1 SO01365DH 149 1) WHEN FLAPS SELECTED TO 8 DEGREES, INDICATOR DID NOT SHOW ANY FLAP MOVEMENT. RAN ABNORMAL PROCEDURE.2) REPLACED FLAP POSITION INDICATOR IAW M/M 27-55-11. OPS CHECKED GOOD. 2L72 4F RTA35EU 20030218001452003021800145EA 2003 2 18 COMA0360100 120030216A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER O OTHER ININSP/MAINT 1 SO01938CA 7046 FLIGHT 5616 FLAPS FAILED AT ZERO, AT GATE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030218001472003021800147EA 2003 2 18 COMA0360101 120030213A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER O OTHER ININSP/MAINT 1 SO01486CA 7707 FLIGHT 5829 EMERGENCY FLOOR PATH LIGHTING FWD SECTION IS INOP.CLEANED ELECTRICAL CONNECTIONS - SYSTEM TEST NORMAL. 2L72 4F RTA21EA 20030218001762003021800176NM 2003 2 18 QXEA0300168 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 4 SEAT TRACK HAS SCRATCHES AT STATION 370. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001802003021800180NM 2003 2 18 QXEA0300172 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 2 SEAT TRACK HAS LIGHT PITTING AT STATION 488. REPAIRED IAW RD 8-53-1342, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001872003021800187NM 2003 2 18 QXEA0300179 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 6 SEAT TRACK HAS SCRATCHES AT STATION 540-545. REPAIRED IAW RD 8-53-4936, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001882003021800188NM 2003 2 18 QXEA0300180 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 6 SEAT TRACK HAS SCRATCHES AT STATION 597. REPAIRED IAW RD 8-53-4936, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218002032003021800203 2003 2 18 SWAA030323 420030210A2565D31591475 SLIDE BOEING737 7373H4 1384600NM FWD SVC DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030218002072003021800207NM 2003 2 18 SWAA030329 120030210A5315BAC1509 FLOORBEAM BOEING737 7373G7 1384595NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT RBL 8, BS 845 AND BS 825. REPAIRED FLOORBEAM PER SWA RA. 2L72 4F RTA16WE 20030218002112003021800211 2003 2 18 SWAA030302 420030206A25656557463 BRACKET BOEING737 7373G7 1384595NM FWD ENTRY DOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED GIRT BAR BRACKET PER MM. 2L72 4F RTA16WE 20030218002122003021800212NM 2003 2 18 SWAA030303 120030207A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 727D + 14 AT STR 22L AND BS 770 AT STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030218002242003021800224 2003 2 18 SWAA030289 420030205A2565D31354 SLIDE BOEING737 7373H4 1384600NM SVC DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD AND AFT SVC DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH SLIDES PER MM. 2L72 4F RTA16WE 20030218002252003021800225NM 2003 2 18 SWAA030290 120030205A335065C33304 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LENS MISSING AT ROW NR 11 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030218002262003021800226 2003 2 18 SWAA030291 420030205A2565D31354 SLIDE BOEING737 7373A4 1384585NM FWD SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD AND AFT SVC DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030218002272003021800227NM 2003 2 18 SWAA030292 120030206A53306545772 SKIN BOEING737 7373G7 1384595NM FUSELAGE BULGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN BULGED BETWEEN BS 727 AND BS 727A, ABOVE STR 8L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030218002292003021800229NM 2003 2 18 SWAA030295 120030206A53146962014 STIFFENER BOEING737 7373H4 1384600NM LT MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD STIFFENER CRACKED AT LT MLG W/W, BS 663 AND LBL 6.15. REMOVED AND REPLACED STIFFENER PER SRM. 2L72 4F RTA16WE 20030218002482003021800248NM 2003 2 18 SWAA030245 120030131A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 4R, BS 629, BS 689 AND BS 690. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030218002502003021800250NM 2003 2 18 SWAA030247 120030201A533065C27287 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF FWD SVC DOOR. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030218002592003021800259NM 2003 2 18 SWAA030360 120030212A55206959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB MAST HARDWARE AND BUSHING AND NR 1 TAB HINGE BUSHING PER MM. 2L72 4F RTA16WE 20030218002652003021800265SW 2003 2 18 ALG2003F0218 120030116A5412206064902036 CHANNEL BELL 407 407 1182206SW ALLSN 250C 250C47B GL FIREWALL CRACKED B ALGRK NONE O OTHER ININSP/MAINT 1 SW03617AL 53265 DURING DAILY INSPECTION, 3 INCH CRACK IN RADIUS OF CHANNEL, WAS FOUND. CRACK STARTS BOTTOM OF CHANNEL AND GOES UP 3 INCHES JUST ABOVE RECEPTACLE DOUBLER. C/A: INSTALL STAINLESS STEEL DOUBLER. 1G71 3U3 UO H2SW E1GL 20030219000022003021900002NE 2003 2 19 ALG2003F00024 120030117A77149580115900 SENSOR SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE MAG OVERSPEED FAILED E ALGAO OTHER O OTHER TXTAXI/GRND HDL 1 SW03521AL 760132 15550TEC DURING GROUND RUN, WITH NR 1 ENGINE RUNNING AT GROUND IDLE (70 PERCENT NR1) AND ROTOR BRAKE ENGAGED, THE ENGINE SHUT ITSELF OFF AFTER RUNNING ABOUT 3-5 MINUTES. THE MECHANIC REMOVED AND REPLACED THE MAG OVERSPEED SENSOR AND THE AIRCRAFT RETURNED TO SERVICE. 1G72 3U3 U H1NE E19EU 20030219000102003021900010SO 2003 2 19 OG52003F00001 120030117A2140FR10E214EL COMBUST CHAMBER PIPER PA31T PA31T 7103124SO PWA PT6 PT6* 52043EA HEATER FAILED A OG5RK NONE O OTHER ININSP/MAINT 1 GL2125ND 159 31T8020005 DURING TROUBLESHOOTING OF HEATING DISCREPANCY THE COMBUSTION TUBE OF HEATER WAS FOUND SEVERELY COMPRESSED AROUND ITS UNSUPPORTED CIRCUMFERENCE. NO VISABLE CRACKS OR LEAKAGE WERE NOTED. SUSPECT WEAK WALLS FOR A PRESSURIZED INSTALLATION HEATER ASSEMBLY WAS REPLACED WITH FACTORY REBUILT ASSEMBLY. 1L72 3T3 T A8EA E2NE 20030219000112003021900011SO 2003 2 19 OG52003F00002 120030117A21402300475 REGULATOR PIPER PA44 PA44180 7104402SO LYC O360 O360* 41514EA HEATER LEAKING B OG5RO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL21299ND1160 4496077 PILOT SQUACKED FUEL ODOR WHEN HEATER WAS TURNED ON. UPON INVESTIGATION FOUND FUEL REQ. AND SHUT OFF VALVE WAS SPRAYING FUEL OUT OF WEEP HOLE WHENEVER HEATER WAS TURNED ON. AD 2001-17-13 ADDRESSES LEAKAGE OF THIS UNIT BUT NOT IN THE AREA WHERE THIS ONE WAS LEAKING. UNIT WAS REPLACED AND FUNCTION RETURNED TO NORMAL. AD WAS SIGNED OFF BY MFG. 1L72 3O3 O A19S0 E286 20030219000132003021900013NM 2003 2 19 SROM200300021 120030207A335058791 LIGHT BOEING737 737205 1384456NM CABIN INOPERATIVE C SROMK NONE L NO TEST ININSP/MAINT 1 AL03733PA 6 23466 DURING TEST OF FLOOR EGRESS LIGHTING SECTION BETWEEN ROWS 11 & 16 FOUND TO BE INOPERATIVE. REPLACED LEAD-IN CABLE. OPS CHECKED NORMAL. 2L72 4F RTA16WE 20030219000152003021900015EA 2003 2 19 COMA0360103 120030214A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA 7017 FLIGHT 5620 CABIN DOOR WARNING MESSAGE.COULD NOT DUPLICATE. INSPECTED DOOR, OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA21EA 20030219000192003021900019SW 2003 2 19 Y2T2003F00000 120030103A6230206040576105 BEARING BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL MAST FAILED A YT2RO OTHER O OTHER NRNOT REPORTED 1 WP01401CJ262 51326 BEARING FAILED, 262.6 HOURS, AFTER INSTALLATION. 1G71 3U3 U H2SW E1GL 20030219000262003021900026NM 2003 2 19 2003UALA00159 120030209A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29647UA 25284 AFT CARGO PIT AT BS 1087 AND RBL 26, INTERCOSTAL ATTACH ANGLE TO FRAME, IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE. 2L72 4F4 FRTA1NM E24NE 20030219000292003021900029NM 2003 2 19 2003UALA00170 120030211A5311 ATTACH ANGLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29647UA 25284 AFT CARGO PIT AT BS 1087 AND LBL 26, INTERCOSTAL ATTACH ANGLE TO FRAME, IS CRACKED MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE. 2L72 4F4 FRTA1NM E24NE 20030219000352003021900035WP 2003 2 19 MWEA030104 120030214A5330591143351 DOUBLER DOUG DC9 DC981 3022081WP STA 1354 - 1354 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FUSELAGE SKIN IS DAMAGED FROM FRAME STATION 1338 - 1354 LONGERON 10 RIGHT TO LONGERON 12 RIGHT. -- FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030219000362003021900036WP 2003 2 19 MWEA030090 120030213A533059364365 SKIN DOUG DC9 DC981 3022081WP STA 1338 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FORWARD SIDE OF FRAME STATION 1338 SKIN IS DAMAGED. -- FABRICATED AND INSTALLED NEW SKIN AND REPAIR DOUBLER. 2L72 4F A6WE 20030219000382003021900038WP 2003 2 19 MWEA030094 120030213A533059364365 FINGER DOUBLER DOUG DC9 DC981 3022081WP STA 1322 & 1338 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FINGER DOUBLER LOCATED ON THE SKIN PANEL REPAIR BETWEEN STATION 1322 & 1338 ARE DAMAGED THIS REPAIR IS BETWEEN LONGERON 13 RIGHT AND 7 RIGHT. -- FABRICATED AND INSTALLED FINGER DOUBLER. 2L72 4F A6WE 20030219000532003021900053WP 2003 2 19 MWEA030103 120030217A53125910130287 SPLICE DOUG DC9 DC981 3022081WP LONG 12 & 9 RH CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 RIGHT OUTBOARD SIDE OF AFT PRESSURE BULKHEAD IS DENTED AND CRACKED BETWEEN LONGERON 12 AND 9 RIGHT. -- FABRICATED AND INSTALLED NEW SPLICE AND AFT PRESSURE BULKHEAD. 2L72 4F A6WE 20030219000542003021900054WP 2003 2 19 MWEA030097 120030217A53125910130287 DOUBLER DOUG DC9 DC981 3022081WP DOOR JAMB INSTALLED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 AFT PRESSURE BULKHEAD RIGHT SIDE SPLICE AT VENTRAL DOOR JAMB, REQUIRES DOUBLER INSTALLATION. -- FABRICATED AND INSTALLED REPAIR PART. 2L72 4F A6WE 20030219000572003021900057NM 2003 2 19 RYN2003F00000 120030123A27821U109592 ACTUATOR BOEING727 727225 1384077NM PWA JT8 JT8D5 52046NE NR 7 LE SLAT DEFECTIVE A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07815EA 22552 DURING CLIMBOUT, NR 7 LEADING EDGE SLAT WOULD NOT RETRACT. EMERGENCY FLAP PROCEDURES FOLLOWED. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. 2L73 4F4 F A3WE E2EA 20030219000632003021900063WP 2003 2 19 MWEA030067 120030212A5313991857215 DOUBLER DOUG DC9 DC981 3022081WP STA 1338 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 STATION 1338 RIGHT AFT PRESSURE BULKHEAD DOUBLER LONGERON 7-12 IS DAMAGED. -- FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030219000662003021900066WP 2003 2 19 MWEA030086 120030212A53209915558232 CLIP DOUG DC9 DC981 3022081WP STA Z34 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 AFT PRESSURE BULKHEAD FORMER OUTBOARD LOWER CLIP STATION Z34 IS CRACKED ON THE OUTBOARD END. -- REMOVED AND INSTALLED LOWER CLIP. 2L72 4F A6WE 20030219000682003021900068WP 2003 2 19 MWEA030060 120030212A5313591016378 SHEAR TIE DOUG DC9 DC981 3022081WP LONG 12 & 9 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 SHEAR TIES ARE DAMAGED BETWEEN LONGERON 12 AND 9 RIGHT SIDE OF STATION 1338 FUSELAGE, FORWARD OF AFT PRESSURE BULKHEAD. -- REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED TWO EACH SHIMS AND INSATLLED SHEAR TIE AND REMAINING FASTENERS. 2L72 4F A6WE 20030219000692003021900069WP 2003 2 19 MWEA030065 120030212A53229915558230234 SUPPORT ANGLE DOUG DC9 DC981 3022081WP STA 248 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 UPPER ANGLE SUPPORT FOR AFT PRESSURE BULKHEAD FORMER IS DAMAGED RIGHT OUTBOARD FORWARD SIDE OF AFT PRESSURE BULKHEAD THIRD FORMER DOWN FROM TOP AT STATION 248. -- FABRICATED AND INSTALLED NEW ANGLE SUPPORT AND CLIP. 2L72 4F A6WE 20030219000722003021900072NM 2003 2 19 SWAA030251 120030202A3350604222 BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT SVC AND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030219000762003021900076NM 2003 2 19 SWAA030255 120030201A3350100885 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29714CB 27848 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROW NR 6 AND ROW NR 8. RECHARGED BATTERY PER MM. 2L72 4F RTA16WE 20030219000802003021900080WP 2003 2 19 MWEA030063 120030217A5311591016373 FRAME DOUG DC9 DC981 3022081WP STA 1338 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FRAME AT STATION 1338 IS CRACKED IN THREE PLACES BETWEEN LONGERON 12 AND 9 RHIGHT SIDE OF FUSELAGE FORWARD OF AFT PRESSURE BULKHEAD. -- REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED ANGLE SPLICE FRAME SECTION. 2L72 4F A6WE 20030219000862003021900086NM 2003 2 19 SWAA030301 120030207A33506556633 LIGHT BOEING737 7375H4 138449DNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030219000882003021900088NM 2003 2 19 SWAA030306 120030207A3350D71701100 CHARGER BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PER MM. 2L72 4F RTA16WE 20030219000892003021900089NM 2003 2 19 SWAA030310 120030209A5610589354 WINDOW BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29639SW 27712 DURING CRUISE R1 COCKPIT WINDOW CRACKED WITH ASSOCIATED ARCING. REMOVED AND REPLACED R1 COCKPIT WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20030219000902003021900090NM 2003 2 19 SWAA030311 120030207A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030219000962003021900096NM 2003 2 19 SWAA030313 120030209A53126546568 DOUBLER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND LOWER CHORD DOUBLER CORRODED AT BS 1016, WL 191 AND LBL 5. REPAIRED DOUBLER PER SRM. 2L72 4F RTA16WE 20030219000972003021900097NM 2003 2 19 SWAA030314 120030208A53126546568 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND BULKHEAD SKIN CORRODED AT BS 1016, WL 192 AND BL 0. REPAIRED BULKHEAD SKIN PER SRM. 2L72 4F RTA16WE 20030219000992003021900099 2003 2 19 SWAA030319 420030208A2565D31591475 SLIDE BOEING737 7373Q8 1384670NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030219001192003021900119NM 2003 2 19 SWAA030347 120030212A3350 CONNECTOR BOEING737 7373H4 1384600NM AFT ENTRY DOOR DIRTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LIGHT INOP. CLEANED SLIDE LIGHT CONNECTOR AND OPS CK GOOD PER MM. 2L72 4F RTA16WE 20030219001232003021900123NM 2003 2 19 SWAA030352 120030212A27316545166 ROD END BOEING737 7377H4 1384404NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29738CB 27870 DURING SCHEDULED C4 CHECK, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB PUSH RODS HARDWARE PER MM. 2L72 4F RTA16WE 20030219001242003021900124NM 2003 2 19 SWAA030354 120030212A2560PH22300L STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROWS NR 6 AND NR 8 ABC. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20030219001262003021900126WP 2003 2 19 CALA0300053 120030217A5313 LONGERON DOUG DC9 DC982 3022082WP STA 1418 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0915841 49581 INSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. REPAIRED IAW ECRA 5311-01132. 2L72 4F A6WE 20030219001302003021900130 2003 2 19 SWAA030355 420030212A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030219001352003021900135NM 2003 2 19 USAA020010A 120030116A5320 STIFFENER BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US41260 23876 PIT - FOUND STIFFENER CRACKED .5 INCH, LEFT STRINGER LBBL 6.15 STATION 663.75 WL 170.4. INSTALLED REPAIR ANGLES PER EA 75658. (M) 2L72 4F RTA16WE 20030219001402003021900140NM 2003 2 19 USAA030003 120030107A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19447US34029 24874 CLT - FOUND SKIN CRACKED 1.5 INCHES LONG, STATION 727E AT STRINGER 23 RIGHT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-03. (M) 2L72 4F RTA16WE 20030219001422003021900142NM 2003 2 19 USAA030006 120030116A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19523AU 23858 CLT - FOUND SKIN CRACKED 1 INCH, BS 727E AT STRINGER 23 RIGHT. INSTALLED DOUBLER AND TRIPLER PER EA 86987. (M) 2L72 4F RTA16WE 20030219001432003021900143NM 2003 2 19 USAA030007 120030113A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US47082 23742 PIT - FOUND SKIN CRACKED 1.875 INCH CRACK, BETWEEN STATION 727E AND 727E AT STRINGER 23R AFT BELLY SKIN. DOUBLER INSTALLED PER SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20030219001442003021900144NM 2003 2 19 USAA030008 120030114A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US51682 22956 PIT - FOUND SKIN CRACKED 1.5 INCH, BS 735 AT STRINGER 23L. DOUBLER INSTALLED PER SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20030219001482003021900148EU 2003 2 19 USAABA03001 120030121A335032146210 POWER SUPPLY AIRBUS330 A330323 3930335EU L3 DOOR FAULTY A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19672UW 0333 PHL - THE EPSU AT DOOR L3 FAULTED. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA46NM 20030219001532003021900153NM 2003 2 19 USAABB03012 120030117A33509221009 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 BDL - FOUND EXIT IDENTIFIER AT DOOR L4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030219001572003021900157NM 2003 2 19 USAABB03017 120030125A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19628AU 27806 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2L72 4F RTA2NM 20030219001582003021900158EU 2003 2 19 USAASA02008 120030126A335032145510 POWER SUPPLY AIRBUSA321 A321211 3930370EU CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19187US 1704 LAX - THE EMERGENCY POWER SUPPLY UNIT BY THE L-2 DOOR FAILED THE EMERGENCY LIGHT TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030219001732003021900173WP 2003 2 19 MWEA030079 120030217A53204912515523 CLIP DOUG DC9 DC981 3022081WP STATION 1338 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LONGERON 11 RIGHT SHOVEL CLIP (AFT OF STATION 1338 TEE) IS DAMAGED. -- REMOVED AND REPLACED SHOVEL CLIP. 2L72 4F A6WE 20030219001752003021900175NM 2003 2 19 AWXA200300162 120030201A53122024T3032 WEB BOEING737 73733A 1384673NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW0 0 23634 LCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB, APPROXIMATELY WL 196.75 TO WL 198, AT APRON OF RBL 5. MAINTENANCE CUTOUT CRACKS AT RBL 5, WL 196.75 AND WL 202; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND 3 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 210, PG. 275 - 279. 2L72 4F RTA16WE 20030220000062003022000006EU 2003 2 20 BMAC030002 120030202A3150 WARNING LIGHT BAG JETSTMJETSTM3101 1500215EU COCKPIT ILLUMINATED A B16AO OTHER N FALSE WARNING NRNOT REPORTED 1 NE05536PA 681 PILOT REPORTED UPON CLIMBING THRU 11200 FT, DOOR LIGHT ILLUMINATED. FOLLOWED EMERGENCY CHECKLIST. LIGHT REMAINED ON UNTIL LANDING. MAINTENANCE CYCLED CIRCUIT BREAKER FOR DOOR CONTROL LIGHT IAW MM. OPS CHECKED, OK. 2L72 4T RTA21EU 20030220000072003022000007WP 2003 2 20 BMAC030003 220030204A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RIGHT MALFUNCTIONED A B16AC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NE05536PA 681 PILOT REPORTED TAKEOFF ABORTED DUE TO RT ENGINE NOT GENERATING POWER. MAINTENANCE CHECKED ALL CONNECTOR PLUGS AND C/W TWO HIGH SPEED TAXI RUNS. SYSTEM OPS CHECKED NORMAL ON GROUND IAW MM. 2L72 4T4 TRTA21EU E4WE 20030220000122003022000012NM 2003 2 20 0300236314 120030214A3397 WIRE BOEING747 747451 1384940NM CABIN DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01674US 30269 DURING LINE CHECK FOUND LT ZONE B FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRE, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030220000182003022000018EU 2003 2 20 03044312 120030213A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT UNSECURE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27312UE 41025 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE BETWEEN SEAT ROWS 3 AND 4. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030220000282003022000028NM 2003 2 20 03FDEA00124 120030213A5320 SUPPORT BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 CORROSION ON SEAT TRACK SUPPORT AT BS 760-850, LBL 25, WL 208. ** SD ** COMING 2L73 4F RTA3WE 20030220000302003022000030NM 2003 2 20 03FDEA00126 120030214A217022D10 COALESCER BAG BOEING727 727100 1384036NM ZONE 100 CONTAMINATED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25107FE 19202 AFTER GEAR RETRACTION, CREW BECAME AWARE OF AN ACRID ODOR WHICH INTENSIFIED. INITIAL ODOR WAS OF BURNING RUBBER OR A SMOLDERING WIRE BUNDLE. CREW WENT ON OXYGEN AND RETURNED TO IND. PERFORMED FIRE, SMOKE, FUMES AND ODOR CHECKLIST. REPLACED BOTH WATER SEPARATOR SOCKS. FOUND LT SOCK EXTREMELY DIRTY AND SMELLED OF DE-ICE FLUID. CHECKED ACM OIL LEVELS, FOUND NORMAL. RAN ALL 3 ENGINES IAW JRH. RUN WAS NORMAL. NO ODOR PRESENT. REF. M/M 21-51-032. 2L73 4F RTA3WE 20030220000442003022000044WP 2003 2 20 ABXA030045 120030123A33505708458503 BATTERY PACK DOUG DC8 DC863 302198AWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23818AX 46075 EMERGENCY EXIT LIGHTS EXTREMELY DIM. NOTICED AFTER POWER LOAD. REPLACED EMERGENCY BATTERY PACK IAW DC-8 MM 33-50-01-2. OPS CHECKED GOOD. 2L74 4F 4A25 20030220000542003022000054WP 2003 2 20 ABXA030054 120030130A4930 SOLENOID VALVE DOUG DC9 DC931 3022065WP APU LEAKING A ABXAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23906AX 47072 AIRCRAFT HAD STRONG JET FUEL ODOR IN COCKPIT AND CABIN AREA. FOUND FUEL SOLENOID VALVE ON APU LEAKING. REMOVED AND REPLACED ALL O-RINGS ON VALVE AND REINSTALLED. LEAK CHECKED GOOD IAW DC-9 MM 49-30-03-2-003. REPLACED LT COALESCAR BAG AS PRECAUTIONARY. FOUND BAG CLEAR. NO FUEL ODOR. LEAK CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 20030220000552003022000055WP 2003 2 20 ABXA030056 120030129A3150 WARNING HORN DOUG DC9 DC915 3022036WP CONFIGURATION ACTIVATED A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23927AX 45717 AFTER TAKE-OFF OUT OF ILN, AIRCRAFT FAILED TO PRESSURIZE AND CONFIGURATION WARNING HORN SOUNDED. CHECKED LT OLEO SWITCH, EXERCISED SWITCH SEVERAL TIMES. CLEANED AND RESEATED CONNECTOR. CREW ASSISTED IN GROUND OPS CHECK OF PRESSURIZATOIN AND CONFIG. WARNING SYSTEM. GROUND SHIFT SYSTEM OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 20030220000672003022000067WP 2003 2 20 ABXA030068 120030209A5210 MECHANISM DOUG DC8 DC861 3021952WP PAX DOOR LACK OF LUBE A ABXAO OTHER O OTHER NRNOT REPORTED 1 GL23843AX 46017 FORWARD CABIN DOOR BINDED DURING OPENING AND CLOSING. CLEANED AND LUBRICATED FORWARD CABIN ENTRY DOOR. OPERATED DOOR THROUGH SEVERAL CYCLES. NO DISCREPANCIES NOTED. 2L74 4F 4A25 20030220000722003022000072WP 2003 2 20 ABXA030075 120030218A21215007025381 FAN DOUG DC8 DC861 3021952WP CABIN DEFECTIVE A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23842AX12857 46015 LT RECIRCULATION FAN STALLED WITH ODOR OF WIRE BURNING AND ELECTRICAL SURGE ON AIRCRAFT. REMOVED AND REPLACED LT RECIRCULATION FAN IAW DC-8 MM 21-21-01-2. OPS CHECKED GOOD IAW DC-8 MM. 2L74 4F 4A25 20030220000732003022000073EA 2003 2 20 QXEA0300005 120030102A2130 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA CABIN PRESSURE MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09610QX 10033 SJC ON FLIGHT 2458- RECEIVED A AMBER CABIN ALTITUDE MESSAGE IN CLIMB FOLLOWED BY A RED CABIN ALTITUDE MESSAGE. LEVELED AT 12,000 FEET, CABIN WAS AT 10,800 FEET. FOLLOWED CHECKLIST, WAS UNABLE TO CONTROL CABIN PRESSURE UP OR DOWN. INSPECTED AFT BAY DOOR. NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220000762003022000076NM 2003 2 20 QXEA0300042 120030113A3230 DOOR DHAV DHC8 DHC8202 2809007NM MLG OPEN A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09349PH 486 SEA-ON FLIGHT NUMBER 2396, RETURNED TO FIELD FOR GEAR DID NOT RETRACT DUE TO ALT RELEASE HANDLE DOOR BEING OPEN. CLOSED MAIN LANDING GEAR ALT DOOR. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030131001862003013100186EA 2003 1 31 COMA0360060 120030129A4990 APU CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 SO01941CA 7050 FLIGHT 5729 APU LOW OIL PRESSURE WARNING.ADDED 2.5 QUARTS OF OIL TO APU. 2L72 4F RTA21EA 20030131001892003013100189NM 2003 1 31 P5CA0300739 120030126A532065B0300131 CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACKS FOUND ON THE CLIP AT FRAME STA 500/L, UPPER DECK SIDEWALL, AT CONNECTION TO STR 10-10A-11A-12. CRACKED CLIPS REMOVED & NEW ONES FABRICATED HF 7075T6 0.050 THK PER SRM 53-10-20 & SRM 51-40-03, FIG. 4. PROTECTED PER SRM 51-10-02 & INSTALL RIVETS PER SRM 51-30-02. 2L74 4F A20WE 20030131001902003013100190NM 2003 1 31 P5CA0300740 120030126A5320NONE BRACKET BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND ON BRACKET AT FLOOR TRACK SUPPORT RBL-25 BETWEEN STA 1900-1920, "LOWER LOBE AFT CARGO." CRACKED BRACKET REMOVED. NEW FABRICATED HF 7075T651 PER SRM 53-11-25 & PER SAMPLE. PROTECTED W/ ANODIZE PER SRM 51-10-02. FASTENER INSTL PER SRM 51-30-02. 2L74 4F A20WE 20030203000012003020300001WP 2003 2 3 CA030110001 220030106A7260307000315 GEARBOX BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP ACCESSORY LEAKING W EA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) LOW OIL PRESSURE INDICATION IN FLT ON LT, NR 1 ENGINE. PILOT SHUT DOWN NR 1 ENGINE AND CONDUCTED EMERGENCY LANDING. INITIAL VISUAL INSPECTION SHOWED OIL HAD SPEWED OVER COWLING. FURTHER INVESTIGATION LATER SHOWED EVIDENCE OF EXCESSIVE HIGH ENGINE GEARBOX PRESSURE AS INDICATED BY OIL FILTER HOUSING BEING PULLED OUT OF GEARBOX. ENGINE WAS INSPECTED PREVIOUSLY FOR INTERMITTENT OIL LOSS BETWEEN FLIGHTS. AT ONE TIME 4 QUARTS WERE LOST IN ONE 3 HOUR LEG. INVESTIGATION AT THAT TIME PRESUMED POSSIBLE LOSS OF OIL FROM ALTERNATOR AND STARTER GEN PAD SEALS. SEALS WERE REPLACED. ENGINE REMOVED FOR INVESTIGATION AND REPAIR. LOANER ENGINE INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20030203000142003020300014CE 2003 2 3 CA030112008 120030108A52601144000301 SEAL BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA AIRSTAIR FAILED W BA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) DURING MAINTENANCE CHECK FLT, BEECHCRAFT 1900 HAD AN UNCOMMANDED DEPRESSURIZATION. DESCRIPTION OF THE EVENT WERE AS FOLLOWS, WHILE CLIMBING THROUGH AN ALTITUDE OF 10500 FT. FORWARD CABIN DOOR ENUNCIATOR LIGHT ILLUMINATED AND WHILE COMPLETING THE EMERGENCY CHECKS, A LOUD BANG WAS HEARD WITH A LOSS OF PRESSURIZATION. AT THIS TIME, THE FLIGHT CREW ADVISED ATC OF THE EMERGENCY AND COMMENCED A GRADUAL DESCENT AND PRIORITY APPROACH WAS REQUESTED. THE AIRCRAFT LANDING WAS UNEVENTFUL AND SUBSEQUENTLY RETURNED TO THE MAINTENANCE FACILITY. THE CONTRACTED AMO INFORMED US THAT THE UPPER SECTION OF THE DOOR SEAL GAVE WAY WITH THE CABIN PRESSURE AT 3.7. 2L72 4T4 TRTA24CE E4EA 20030203000232003020300023EA 2003 2 3 CA030113008 220030112A7310LW120980100 LINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA FUEL NOZZLE BROKEN W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB, PILOTS NOTICED PARTIAL POWER LOSS ON THE LT ENGINE. THE AIRCRAFT RETURNED TO BASE AND LANDED SAFELY. MAINTENANCE INVESTIGATED PROBLEM AND FOUND THE LT ENGINE NR 4 CYLINDER FUEL NOZZLE LINE BROKEN AT FLANGE.THE LINE WAS REPLACED AND AD 2002-26-01 CARRIED OUT. A GROUND RUN WAS CARRIED OUT AND THE AIRCRAFT WAS RETURNED FOR SERVICE. 1L72 3O3 O A20SO E14EA 20030203000252003020300025NM 2003 2 3 CA030113010 120030111A2910DSC252A40230 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM CHAFED W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) ON STARTUP NR 2 HYDRAULIC SYSTEM QUANTITY BLED TO 1 QT. PUDDLE OF FLUID OBSERVED AROUND LT MAIN GEAR. AIRCRAFT SHUT DOWN. NR 1 MAIN BRAKE FLEX LINE REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030203000262003020300026NM 2003 2 3 CA030113011 120030111A3810 COMPRESSOR BOEING757 757251 1384970NM RROYCERB211 RB211535E43754555NE POTABLE WATER MALFUNCTIONED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CA (CAN) STRONG BURNING ODOR AND LIGHT SMOKE IN AFT CABIN. FAULT TRACED TO POTABLE WATER COMPRESSOR. CB FOUND POPPED. DEFERRED FOR REPLACEMENT. ELECTRICAL CONNECTOR REMOVED FROM COMPRESSOR. 2L72 4F4 FRTA2NM E12EU 20030203000602003020300060EA 2003 2 3 03033662 120030202A261247269801 CIRCUIT CARD CNDAIRCL600 CL6002B19 1900309EA A VTZAFO ACTIVATE FIRE EXT. OTHER N FALSE WARNING LDLANDING 1 EA27662BR 7526 On landing touchdown, the crew noted a R/H engine fire indication and bell. The engine was shut down with the fire handle and the #2 fire extinguisher was discharged. Maintenance personnel removed and replaced the R/H engine fire detection circuit card. An operational check was satisfactory, the engine fire extinguisher was replaced and the aircraft was returned to service. 2L72 4F RTA21EA 20030203000682003020300068CE 2003 2 3 CA030120010 120030116A270050110002 HINGE PIN BEECH 99 99A 1154003CE PWA PT6 PT6A28 EA LT WING FRACTURED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TIME ON PIN IS UNKNOWN IT WAS NOTICED THAT THE SKIN FORWARD OF THE LT UPPER FORWARD WING SPAR NEAR THE WING FITTING WAS SOFT AND EASILY MOVED. DURING CLOSER INSPECTION THE PIN WAS FOUND NOT TO BE ENGAGED IN THE LAST 2 FT OF THE HINGE BY THE WING FITTING. THE WING TIP WAS REMOVED AND IT WAS FOUND THAT THE HINGE PIN BROKE WHERE IT BENDS TO GO UNDER THE SAFETY PLATE. AS A RESULT THE PIN WORKED ITS WAY OUT AND CURLED UP INSIDE THE WING TIP. 1L72 3T4 T A14CE E4EA 20030203000712003020300071NM 2003 2 3 MDAS092002 120030113A5730 SKIN BOEING737 737800* NM WINGS CHAFED W Q0MFK NONE O OTHER ININSP/MAINT 1 WP0316805 30636 BOEING 737-800 EXPERIENCED CHAFING DAMAGE TO THE LOWER SKIN AND FUEL ACCESS DOORS IN THE AREA OF THE PYLON BLADE SEAL CONTACT DURING MAINTENANCE VISIT. IT APPEARS THAT THE STRUT SEALS HAVE BEEN RIDING ON THE ACCESS PANELS, ACCESS PANEL RINGS, AND THE LOWER SURFACE OF THE WING SKIN. THE ACCESS PANELS ARE LOCATED ON EACH OUTBOARD SIDE OF THE STRUTS AT WING STA 255-277 LT AND RT, BETWEEN RIB 7 AND 8. MDN TAKE AN INTERIM REPAIR THAT BLEND OUT THE NOTED GROVES IN THE ACCESS PANELS, ACCESS PANEL RINGS, AND WING LOWER SURFACES WITH REFERENCE TO SRM AND SERVICE BULLETIN 737-57-1268. THE INTERIM REPAIR WITH RUB STRIPS INSTALLED PER SB IS STRUCTURALLY SATISFACTORY. 2L72 4F RTA16WE 20030203000822003020300082EU 2003 2 3 BAQA083527 120030120A6330L633M2010101 MOUNT UROCOPEC135 EC135P1 8680990EU TRANSMISSION LEAKING H BAQAK NONE K FLUID LOSS ININSP/MAINT 1 FS01577LF340 0140 TRANSMISSION MOUNT LEAKING FLUID. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030203000892003020300089EU 2003 2 3 BAQA084058 120030130A28229A2045 PUMP UROCOPEC135 EC135P1 8680990EU FUEL SYSTEM INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911TS644 0167 FUEL PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030203001082003020300108EU 2003 2 3 2003FA0000067 120030115A6410109813129101 GRIP AGUSTAA109 A109E 0260119EU T/R BLADE LOOSE B LN3RK NONE O OTHER ININSP/MAINT 1 EA0312VW 366 11074 GRIP BUSHINGS WERE ROTATING INSIDE OF GRIP CAUSING GRIP INSIDE DIAMETER TO WEAR BEYOND LIMITS. 1G72 3U RTH7EU 20030203001432003020300143NM 2003 2 3 PCAA0301030 120030131A531585310380 FLOORBEAM DHAV DHC8 DHC8102 2809003NM X97.0 CRACKED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13849EX 337 MDT- DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING A 3 INSPECTION, CRACK WAS FOUND ON FRAME SECTION 85310380 IN FLOOR BEAM FRAME AT STATION X97.0, NOSE GEAR WELL. CRACK WAS REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-4521 AS AN INTERIM REPAIR. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030203001522003020300152WP 2003 2 3 BKJ2003F00000 120030111A32409540976 BRAKE ASSY CVAC 440 440 2422902WP PWA R2800 R2800* 52026NE RT INBOARD LEAKING B BKJRO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SW1724DR 393 DURING LANDING CHECK, UPON ARRIVAL TO AIRPORT. PILOTS NOTICED LOW HYDRAULIC RESEVOIR LEVEL. TOWER WAS NOTIFIED AND A NORMAL LANDING WAS MADE. AS A PRECAUTION, THE AIRCRAFT WAS TOWED TO PARKING. INSPECTION REVEALED A LEAKING BRAKE ASSEMBLY. 2L72 4R4 R 6A6 5E8 20030203001532003020300153CE 2003 2 3 BSY2003F00002 120030107A76035038901223 THROTTLE CABLE BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO LT ENGINE BROKEN A BSYAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL071653W TH252 LT ENGINE, NO THROTTLE CONTROL, SHUT ENGINE DOWN, LANDED NO PROBLEM. FOUND THROTTLE CABLE BROKEN, REMOVED AND REPLACED THROTTLE CABLE, OPS CHECKED GOOD. 1L72 3O3 O 3A16 E5CE 20030203001642003020300164WP 2003 2 3 DTH2003F00000 220030102A7200 ENGINE BEECH 100 B100 1152919CE GARRTTTPE331TPE331* 01514WP RIGHT FLAMED OUT E DTHAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 GL2575AP BE57 27154 RT ENGINE FLAMED OUT DURING DESCENT TO LANDING. AUTO IGNITION RELIT, NORMAL OPERATION. YET TO DETERMINE IF MECHANICAL OR OPERATIONAL PROBLEM. 1L72 4T3 T A14CE E2WE 20030203001652003020300165CE 2003 2 3 DYT2003F00000 120030110A322008421024 BELLCRANK CESSNA310 T310Q 2074244CE CONT O520 TSIO520* 17040SO NLG IDLER BROKEN B DYTRO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO158108G 310Q1047 PILOT REPORTED BANG COMING FROM UNDER HIS FEET WHEN GEAR WAS RETRACTED. WHEN GEAR WAS EXTENDED THE NOSE GEAR DID NOT LOCK. AIRCRAFT LANDED AND NOSE GEAR COLLAPSED. INVESTIGATION FOUND THAT NOSE GEAR IDLER BELLCRANK, BROKEN. 1L72 3O3 O 3A10 E8CE 20030203001822003020300182CE 2003 2 3 FPI2003F00002 120030114A3233 HOUSING CESSNA210 210N 2073453CE ACTUATOR CRACKED A FPIAK NONE O OTHER ININSP/MAINT 1 SO156195N 21062966 FOUND LANDING GEAR ACTUATOR CRACKED IAW SB. 1H71 3O 3A21 20030203001862003020300186CE 2003 2 3 GUU2003F00002 120030112A55301015240133 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA VERTICAL STAB CRACKED A GUUAK NONE O OTHER ININSP/MAINT 1 SO178155612096 UE239 AT SCHEDULED INSPECTION, THE LT RUDDER TORQUE SHAFT SUPPORT BRACKET WAS FOUND TO BE CRACKED. REMOVED AND REPLACED LT RUDDER TORQUE SHAFT SUPPORT BRACKET. 2L72 4T3 TRTA24CE E2NE 20030328000832003032800083EA 2003 3 28 COMA0360059 120030129A2740601R923019 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO01934CA12636 7042 FLIGHT 5780 STAB TRIM AND MACH TRIM CAUTION MESSAGE. REPLACED THE HSTCU. 2L72 4F RTA21EA 20030203002402003020300240SO 2003 2 3 C2XA03TY019 120030203A510014529150009 BEAM EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 TYS DURING A SCHEDULED 2-C INSPECTION THE FORWARD FLOOR SUPPORT BEAM FOR PANEL 242AF WAS FOUND CORRODED. MAINT. CLEANED AREA,FAB.,ALLODINED AND PRIMED A DOUBLER AND INSTALL IAW EMB 135/145 SRM-51-10-02 AND CMP-51-21-04/05/06.ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030204000122003020400012NE 2003 2 4 M7K2003F00000 220030107A7200 ENGINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MAKING METAL E M7KAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 WP1943MH 4725 1732 2856 9378 UPON ENGINE START ENGINE CHIP LIGHT ILLUMINATED ON THE CENTRAL WARNING PANEL. ENGINE IMMEDIATELY SHUT DOWN. CHIP DETECTORS AND OIL FILTER FOUND WITH METAL CONTAMINATION. ENGINE REMOVED. UNUSUAL NOISE EMINATES FROM THE FREE TURBINE WHEN ROTATED BY HAND. ENGINE SENT FOR TEARDOWN AND REPAIR. 1G71 3U3 U H9EU E19EU 20030204000232003020400023NM 2003 2 4 VNAA0301024 120030122A3200870004MODB PSEU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FAILED A VNAAO OTHER O OTHER CLCLIMB 1 GL07471PS15648 3007 WHILE CLIMBING THROUGH 12,000 FEET, THE CREW NOTICED THE GEAR INDICATION LIGHTS WERE INTERMITTENTLY COMING ON. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE ADVISED TO RETURN TO DAY. MAINTENANCE INSPECTED AND REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204000252003020400025NM 2003 2 4 SWAA030180 120030123A335007912 COVER BOEING737 7375H4 138449DNM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030204000282003020400028NM 2003 2 4 SWAA030185 120030124A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 530, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000352003020400035NM 2003 2 4 SWAA030226 120030130A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A + 17, WL 208 AND RBL 27.5. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20030204000382003020400038NM 2003 2 4 SWAA030229 120030130A531365C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030127000932003012700093SW 2003 1 27 HEEA083657 120030114A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 EMERGENCY FLOAT FUSIBLE PLUG LEAKING. 1G71 3U O H2SW 20030127000952003012700095 2003 1 27 VNAA0301011 420030111A3418 STALL WARNING DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07472PS 3008 DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE SYSTEM RESET ITSELF AND FLIGHT 4043 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030127000962003012700096NM 2003 1 27 DHL2003745004 120030124A3231 SWITCH BOEING727 727224 1384076NM A DHLAKO NONE OTHER O OTHER CLCLIMB 1 SO01745DH 20665 1) THE RED DOORS LIGHT AND THE RIGHT GEAR DOOR LIGHT CAME ON WHEN THE LANDING GEAR HANDLE WAS MOVED TO OFF AFTER GEAR RETRACTION. THE LIGHTS WENT OUT WHEN THE GEAR HANDLE WAS MOVED TO UP. SEE LOG PAGES 323267 AND 323259.2) DEFERRED RIGHT GEAR DOOR INDICATION PER MEL 32-1 CONTROL #11736 ASSIGNED, PLACARD INSTALLED.3) REF DMI # 11736 - RED DOORS LIGHT AND THE RIGHT GEAR LIGHT CAME ON WHEN GEAR HANDLE WAS MOVED TO OFF AFTER GEAR RETRACTION. THE LIGHT WENT OUT WHEN HANDLE WAS MOVED TO UP.4) REMOVED AND REPLACED RH MAIN GEAR DOOR LIGHT SWITCH AND OPS CHECKED PER B727 M/M 32-12-01. OPS CHECKED GOOD. THIS CLEARS DMI #11736. PLACARD REMOVED. 2L73 4F A3WE 20030127001002003012700100EA 2003 1 27 COMA0360045 120030126A53116003603331 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FS718 CRACKED A COMAO OTHER O OTHER ININSP/MAINT 1 SO01967CA16115 7134 LEFT FS 718 FRAME AND DOUBLER CRACKED BETWEEN STRINGERS 10 AND 12.REPAIRED FRAME AND REPLACED DOUBLER I/A/W BOMBARDIER REO 601R-53-61-193A. 2L72 4F RTA21EA 20030127001072003012700107 2003 1 27 HEEA083661 420030114A344280510800001 CONTROL BOX BELL 407 407 1182206SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 DATA BOX SKYWATCH UNREADABLE CAUSING FALSE TARGETS TO DISPLAY. COULD NOT DUPLICATE PROBLEM. BENCH CHECK GOOD. 1G71 3U O H2SW 20031027001102003102700110NM 2003 10 27 ASAA0240232 120030407A5320654795113 THRESHOLD BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND AFT CARGO BAY UPPER THRESHOLD PLATE IS CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030127001202003012700120SW 2003 1 27 HEEA083668 120030115A5302 SKIN BELL 407 407 1182206SW TAILBOOM FIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH BP3069 53199 SKIN CRACKED AT LOW LT SIDE AT STINGER BLOCK FWD END. IN SHOP REPAIR. 1G71 3U O H2SW 20030127001222003012700122SW 2003 1 27 HEEA083669 120030115A6320206040156001 SEAL BELL 407 407 1182206SW M/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR GEARBOX SEAL REMOVED DUE TO OIL LEAK. 1G71 3U O H2SW 20030127001262003012700126SW 2003 1 27 HEEA083671 120030115A3212206050247131 COVER BELL 407 407 1182206SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 EMERGENCY FLOAT COVER TORN. 1G71 3U O H2SW 20030127001312003012700131SW 2003 1 27 HEEA083674 120030115A3212206050247131 COVER BELL 407 407 1182206SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 EMERGENCY FLOAT COVER WORN, TORN, VELCRO LOOSE. 1G71 3U O H2SW 20030127001352003012700135SW 2003 1 27 HEEA083677 120030115A3212206050247132 COVER BELL 407 407 1182206SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 EMERGENCY FLOAT COVER END CAP WORN AND TORN. TO BE SENT TO BELL FOR CREDIT. 1G71 3U O H2SW 20030127001412003012700141SW 2003 1 27 HEEA083680 120030115A3212206050247137 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033193E 53276 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20030127001632003012700163SW 2003 1 27 HEEA083690 120030115A2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH3700 97148 53393 STARTER GEN BRUSHES WORN. REPAIRED. 1G71 3U O H2SW 20031027001152003102700115NM 2003 10 27 ASAA0240198 120030329A53306548240 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND EMPENNAGE SKIN HAS CHAFING DAMAGE AT RIGHT LOWER AFT HORIZONTAL STAB SEAL. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030127001962003012700196SW 2003 1 27 HEEA083694 120030115A2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 95189 53401 STARTER GEN BRUSHES WORN. 1G71 3U O H2SW 20030204000402003020400040NM 2003 2 4 SWAA030234 120030130A32106546109 ARM BOEING737 7373H4 1384600NM LT/RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, SWA SI 11251-32, FOUND LT AND RT MLG CLEVIS BEAM ARMS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG CLEVIS BEAM ARMS PER MM. 2L72 4F RTA16WE 20030204000432003020400043NM 2003 2 4 SWAA030214 120030129A57406559886 BEAM BOEING737 7373H4 1384600NM LT WING T/E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND LT MLG BEAM REAR SPAR CHORD CRACKED. REPAIRED BEAM PER SWA ACO. 2L72 4F RTA16WE 20030204000482003020400048NM 2003 2 4 SWAA030219 120030129A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT ELEV WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 DURING SCHEDULED SERVICE CHECK, (SI 11038-55), LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 3 AND NR 4 HINGE BUSHINGS PER MM. 2L72 4F RTA16WE 20030204000492003020400049NM 2003 2 4 SWAA030220 120030129A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SPECIAL VIST, FOUND A 1.25 LONG FUSELAGE SKIN CRACK, BS 767+7, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000572003020400057NM 2003 2 4 SWAA030208 120030125A32106582770 FITTING BOEING737 7373H4 1384600NM LT MLG W/W CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD WALKING BEAM SUPPORT FITTING CORRODED. REMOVED AND REPLACED LT MLG FWD WALKING BEAM SUPPORT FITTING PER MM. 2L72 4F RTA16WE 20030204000622003020400062NM 2003 2 4 SWAA030174 120030123A53116546541 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 FRAME CRACKED AT STR 2R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030204000712003020400071NM 2003 2 4 SWAA030154 120030121A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 FUSELAGE SKIN CRACKED, BS 394, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030204000722003020400072NM 2003 2 4 SWAA030155 120030121A53306545772 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED, BS 715, STR 10L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030204000742003020400074NM 2003 2 4 SWAA030158 120030122A55306546874 ANGLE BOEING737 7373H4 1384600NM VERT STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB LEFT AND RT DRAG ANGLES CORRODED. REMOVED AND REPLACED ANGLES PER SRM. 2L72 4F RTA16WE 20030204000752003020400075NM 2003 2 4 SWAA030161 120030122A531165C25229 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED, BS 727D, STR 13R. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20030204000762003020400076NM 2003 2 4 SWAA030163 120030122A57536546431280 FLAP BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED C1 CHECK, FOUND RT WING T/E OUTBD FORE FLAP LOWER SKIN CRACKED. REMOVED AND REPLACED FORE FLAP PER MM. 2L72 4F RTA16WE 20030204000792003020400079NM 2003 2 4 SWAA030166 120030122A3211654611325 PIN BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED C1 CHECK, FOUND RT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED TRUNION PIN PER MM. 2L72 4F RTA16WE 20030204000832003020400083 2003 2 4 SWAA030141 420030120A25656557463 HOOK BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR ESCAPE SLIDE COVER FWD HOOK LOOSE. SECURED L1 DOOR ESCAPE SLIDE COVER FWD HOOK PER MM. 2L72 4F RTA16WE 20030204000882003020400088NM 2003 2 4 SWAA030147 120030121A53116558280 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 14R AND 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030204000892003020400089 2003 2 4 SWAA030148 420030121A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030127002032003012700203SW 2003 1 27 HEEA083695 120030115A2823206063640109 VALVE BELL 407 407 1182206SW FUEL SHUTOFF INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 FUEL SHUTOFF VALVE WILL NOT OPEN. VALVE WILL MOTOR BUT STAYS CLOSED. 1G71 3U O H2SW 20030127002142003012700214NE 2003 1 27 PCAA0301024 220030126A7261311859701 GARLOCK SEAL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LEFT LEAKING A PCAAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 EA13805EX 228 121153 BGM-PIT FLIGHT#3569. CREW REPORTED #1 ENGINE OIL PRESSURE WENT TO BETWEEN 40 AND 45 PSI IN FLIGHT. CHECKLIST COMPLIED WITH AND ENGINE SHUT DOWN. EMERGENCY DECLARED, AND AIRCRAFT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED #1 ENGINE STARTER GARLOCK SEAL IN ACCORDANCE WITH PRATT AND WHITNEY MAINTENANCE MANUAL 72-20-00. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030127002182003012700218SW 2003 1 27 HEEA083707 120030115A5320206064902036S CHANNEL BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 FUSELAGE CHANNEL CRACKED. SCRAPPED. 1G71 3U O H2SW 20030127002202003012700220SW 2003 1 27 HEEA083708 120030115A5412206064902127 FIREWALL BELL 407 407 1182206SW ENG BAY CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 ENGINE BAY FIREWALL CRACKED. 1G71 3U O H2SW 20030127002242003012700224SW 2003 1 27 HEEA083711 120030115A2913206076030111 PUMP BELL 407 407 1182206SW HYD SYSTEM MALFUNCTIONED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03402PH 53159 PUMP PRODUCING HYD PRESSURE ABOVE MANUFACTURERS LIMITS. 1G71 3U O H2SW 20030127002272003012700227SW 2003 1 27 HEEA083713 120030115A2913206076030111 PUMP BELL 407 407 1182206SW HYD SYSTEM NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 HYD PUMP MAKING ABNORMAL NOISE. 1G71 3U O H2SW 20030127002442003012700244SW 2003 1 27 HEEA083724 120030115A3212 BOTTLE BELL 407 407 1182206SW SOLENOID VALVE DISCHARGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH 212 53399 EMERGENCY FLOAT SOLENOID VALVE BOTTLE WILL NOT HOLD CHARGE. 1G71 3U O H2SW 20030127002582003012700258SW 2003 1 27 HEEA083733 120030115A6310214040841101 SEAL BELL 407 407 1182206SW FREEWHEEL UNIT LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03496PH 53398 FREEWHEEL UNIT SEAL AFT CAP LEAKING. 1G71 3U O H2SW 20030127002622003012700262SW 2003 1 27 HEEA083737 120030115A2821 WARNING LIGHT BELL 407 407 1182206SW FUEL BYPASS FALSE INDICATIONE HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03495PH 53397 FUEL FILTER BYPASS LIGHT WOULD NOT GO OUT. 1G71 3U O H2SW 20030127002632003012700263SW 2003 1 27 HEEA083738 120030115A2821 WARNING LIGHT BELL 407 407 1182206SW FUEL BYPASS FALSE INDICATIONE HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03612PH 53199 FUEL FILTER BYPASS LIGHT WOULD NOT GO OUT. 1G71 3U O H2SW 20030127002652003012700265SW 2003 1 27 HEEA083740 120030115A2820222366649101 VALVE BELL 407 407 1182206SW SUMP DRAIN MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 SUMP DRAIN VALVE STAYS OPEN. 1G71 3U O H2SW 20030127002662003012700266SW 2003 1 27 HEEA083741 120030115A2820222366652003 FITTING BELL 407 407 1182206SW FUEL DISTRIB CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 SMALL END OF FITTING IS CORRODED. SCRAPPED. 1G71 3U O H2SW 20030127002672003012700267SW 2003 1 27 HEEA083742 120030115A2844222375077115 TRANSDUCER BELL 407 407 1182206SW FUEL INDICATOR FLUCTUATES E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03612PH 53199 FUEL INDICATOR TRANSDUCER HAS FLUCTUATION IN FLIGHT. 1G71 3U O H2SW 20030127002802003012700280NM 2003 1 27 MWEA030025 120030109A5320993053873 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RIGHT CUSP MEMBRANE HAS CORROSION BETWEEN STATION 370 TO 389. BLENDED OUT CORROSION, FABRICATED AND INSTALLED DOUBLER AND FILLER AND INSTALLED RIGHT PANEL. 2L72 4F RTA6WE 20030127002822003012700282NM 2003 1 27 MWEA030032 120030107A575499194471 PANEL DOUG MD88 MD88 3023688NM L/E SLAT TORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31212ME 49762 NR 3 LEFT SLAT PANEL TORN AT LOWER SURFACE UPPER RIGHT CORNER. REMOVED DAMAGE AND INSTALLED INTERNAL DOUBLER AND FILLER. 2L72 4F RTA6WE 20030204001012003020400101NM 2003 2 4 SWAA030095 120030116A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH LONG AT BS 500D, STRINGER 10L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204001442003020400144CE 2003 2 4 XA12003F00000 120030102A499058491661 FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP APU CLOGGED B XA1RK NONE O OTHER ININSP/MAINT 1 SW09754TA 258406 THE INLINE FILTER INSTALLED UNDER SB 21-3485 CLOGS UP. THERE IS NO TIME INTERVAL TO CLEAN THIS FILTER. THE SB SIMPLY STATES TO INSTALL THE FILTER, IT DOES NOT MENTION AN INTERVAL TO CLEAN OR REPLACE IT. THE CLOGGED FILTER CAUSED THE PRESSURIZATION TO GET A 3000 FPM BUMP DURING TAKEOFF CLIMB. 2L72 4F4 FRTA3EU E6WE 20030204001572003020400157 2003 2 4 03FDEA00015 420030110A34174059060901 ADC DOUG MD11 MD11 3023602NM E/E BAY FAULTY A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25584FE 48436 AFTER TO AIRSPEED COPILOTS SIDE 20 KTS OFF. SUSPECT CADC FAIL. RAN AIRSPEED: LOST, SUSPECT OR ERRATIC CHECK LIST. RETURNED TO KIX. CHECKED BOTH CADC-1/-2, DURING CADC-2 TEST FOUND CADC FAIL IND INTERMITTENTLY CAME ON SEVERAL TIMES. REMOVED AND REPLACED CADC-2 PER MM 34-16-01-4. CADC-2 ALL TESTED AND SATISFACTORY PER MM 34-16-01-5. A/C OK FOR SERVICE. 2L73 4F RTA22WE 20030204001602003020400160NM 2003 2 4 MWEA030031 120030111A7711 INDICATOR DOUG MD88 MD88 3023688NM COCKPIT READS LOW A MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31601ME 49762 CREW NOTICED RIGHT AND LEFT ENGINE PRESSURE RATIO SYSTEM INDICATIONS READ ZERO. INSPECTED PRESSURE TOTAL 2 AND PRESSURE TOTAL 7 LINES FOR WATER, APPLIED GROUND HEAT TO LEFT AND RIGHT ENGINES, VERIFIED ENGINE PRESSURE RATIO SYSTEM WORKING NORMALLY. 2L72 4F RTA6WE 20030204001612003020400161WP 2003 2 4 MWEA030041 120030116A553259670321 SKIN DOUG DC9 DC981 3022081WP VERTICAL STAB CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 LEFT SIDE OF VERTICAL STABILIZER IS CHAFED FROM LEADING EDGE OF HORIZONTAL STABILIZER RUB STRIP/SEAL. CUT OUT DAMAGE, INSTALLED INTERNAL TITANIUM DOUBLER AND FILLER. 2L72 4F A6WE 20030204001652003020400165NM 2003 2 4 SWAA030089 120030115A5320BAC1498 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER SPLICES BS 360 STR 28L AND STR 28R. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030204001792003020400179NM 2003 2 4 SWAA030106 120030117A3350BR2013 CAP BOEING737 7372H4 138448CNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED BC3 CHECK, FOUND THE EEPLS FWD END CAP MISSING. INSTALLED THE EEPLS FWD END CAP PER MM. 2L72 4F A16WE 20030204001822003020400182NM 2003 2 4 SWAA030109 120030117A53206545409 STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND SWAY STRAP CRACKED AT BS 312 RBL 45 AND LBL 45 AND BS 328 BBL 0 WL 200. REMOVED AND REPLACED SWAY STRAPS PER SRM. 2L72 4F RTA16WE 20030204001832003020400183NM 2003 2 4 SWAA030110 120030117A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B STR 2L AND 727C STR 6R AND STR 7L AND BS 727D STR 6R AND STR 7R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030204001902003020400190NM 2003 2 4 SWAA030120 120030118A53306545890 BEAR STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND LOWER HOLE IN BEARSTRAP CRACKED AT BS 303.9 LBL 62, WL 238. REPAIRED CRACK IN BEARSTRAP PER SRM. 2L72 4F RTA16WE 20030204001932003020400193 2003 2 4 SWAA030122 420030119A2565D31591478 SLIDE BOEING737 7373H4 1384600NM L1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 L1 DOOR ESCAPE SLIDE PRESSURE IS LOW. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE PER MM. 2L72 4F RTA16WE 20030204001942003020400194NM 2003 2 4 SWAA030124 120030119A3397BR2013 WIRE BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 EEPLS WIRING ON THE LT SIDE AT ROW 9 IS NOT SECURE. SECURED THE EEPLS WIRING AT ROW 9 PER MM. 2L72 4F RTA16WE 20030204002032003020400203NE 2003 2 4 SWAA030131 220030117A72301663M24P BLADE BOEING737 7373L9 1384470NM GE CFM56 CFM56* 13802NE NR 2 ENGINE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 857307 DURING POST FLIGHT, FOUND NR 2 ENG FAN BLADES NR 2 CRACKED AND NR 4 TIP CURLED. REMOVED AND REPLACED NR 2 ENG FAN BLADES NR 2, NR 4, NR 21 AND NR 23 PER MM. 2L72 4F4 FRTA16WE E2GL 20030204002052003020400205 2003 2 4 SWAA030134 420030120A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 L1 DOOR ESCAPE SLIDE PARTIALLY FELL OUT OF CONTAINER. REINSTALLED THE L1 ESCAPE SLIDE PER MM. 2L72 4F RTA16WE 20030204002172003020400217NM 2003 2 4 SWAA030167 120030122A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. RELAMPED PER MM. 2L72 4F RTA16WE 20030127002842003012700284GL 2003 1 27 HEEA083757 220030115A724023030911 CASE BELL 407 407 1182206SW ALLSN 250C 250C* GL COMBUST CHAMB DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH 53461 IGNITER BOSS HAS STRIPPED THREADS. REPAIRED. 1G71 3U3 UO H2SW E4CE 20030127002882003012700288NM 2003 1 27 03FDEA00028 120030115A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION ON LOWER FLOORBEAM CORD, AROUND NUTPLATES, STA 1070, 0 BL - RBL 45, WL 200. BLENDED CORROSION ON BS 1070 LOWER CHORD AND FOUND OUT OF LIMITS AT RBL 11 TO RBL 34. REMOVED LOWER CHORD FROM RBL 11 TO RBL 34. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS ALL WORK DONE IAW SRM. 2L73 4F RTA3WE 20030128000032003012800003SW 2003 1 28 ALGA084011 120030120A6320407040076101 BOLT BELL 407 407 1182206SW TRANSMISSION SCORED H ALGAK NONE O OTHER ININSP/MAINT 1 FS01697AL2457 A388 53374 ON DISSASSEMBLY FOUND 30 BOLTS ON GEAR SHAFT LOOSE, MATING SURFACE FRETTED BEYOUND LIMITS IN CR&O MANUAL. THIS WAS THE FIRST TIME UNIT WAS DISSASSEMBLED SINCE NEW. REMOVED AND REPLACED BOLTS. 1G71 3U O H2SW 20030128000052003012800005GL 2003 1 28 ALGA084031 220030123A73202539688 COVER CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C* GL FUEL CONTROL DEFECTIVE H ALGAK NONE O OTHER ININSP/MAINT 1 FS01PARTO 326726 ON ASSEMBLY FOUND COVER LEAKING EXCESSIVE. REMOVED. 1Q71 3R3 U 2A6 E4CE 20030128000062003012800006 2003 1 28 BAQA082897 420030108A3420 LIGHT AEROSPSA365 SA365N 8680669EU HSI INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM 6396 CO-PILOT EMERGENCY LIGHT ON HSI. SELECT PANEL INOPERATIVE. 1G72 3U H10EU 20030128000092003012800009EU 2003 1 28 BAQA084013 120030121A2822P94C16606 PUMP AEROSPAS365 AS365N2 8680815EU FUEL BOOST INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME694 6417 BOOST PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030128000152003012800015GL 2003 1 28 HEEA083767 220030115A725023062752 SHIELD BELL 407 407 1182206SW ALLSN 250C 250C* GL NR 1 NOZZLE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH 53401 NR 1 NOZZLE SHIELD CRACK AT CENTER OF SHIELD DOME. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000162003012800016GL 2003 1 28 HEEA083768 220030115A726023063369 SEAL BELL 407 407 1182206SW ALLSN 250C 250C* GL ENG/XMSN LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03496PH 53398 ENGINE AND TRANSMISSION TRANSFERRING OIL. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000192003012800019GL 2003 1 28 HEEA083771 220030115A720023063392 ENGINE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENG BAY MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 ENGINE MAKING METAL. REPLACED WITH SERVICEABLE ENGINE. 1G71 3U3 UO H2SW E1GL 20030128000252003012800025GL 2003 1 28 HEEA083777 220030115A741223064130 IGNITER BOX BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 IGNITER BOX HAS NO OUTPUT. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000312003012800031GL 2003 1 28 HEEA083784 220030115A720023064570 LINER BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 LINER HAS CRACKS AND FUEL NOZZLE GUIDE WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000372003012800037SW 2003 1 28 HEEA083790 120030115A282123066697 FILTER BELL 407 407 1182206SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 FILTER BYPASS INDICATOR POPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128000492003012800049 2003 1 28 HEEA083803 420030116A34424000023 TRANSCEIVER BELL 407 407 1182206SW WX RADAR SYS MALFUNCTIONED E O OTHER O OTHER NRNOT REPORTED 1 SW03740PH 53435 TRANSCEIVER HAS A LOUD SQUEAL IN HEADSET. BENCH CHECK GOOD. 1G71 3U O H2SW 20030128000592003012800059SW 2003 1 28 HEEA083813 120030116A6220406010120101 BOLT BELL 407 407 1182206SW M/R BLADES DAMAGED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03719PH 53266 MAIN ROTOR BLADE BOLTS HAVE MECHANICAL DAMAGE AT TOP OF SHANK AT GROOVE. 1G71 3U O H2SW 20030128000712003012800071SW 2003 1 28 HEEA083825 120030116A6300406010421103 SPACER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 MAIN ROTOR SPACER WORN. 1G71 3U O H2SW 20030128000742003012800074SW 2003 1 28 HEEA083828 120030116A6300406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH2754 53003 MAIN ROTOR LEVER ASSY WORN. 1G71 3U O H2SW 20030128000762003012800076SW 2003 1 28 HEEA083830 120030116A6300406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 1202 53323 MAIN ROTOR LEVER ASSY WORN. 1G71 3U O H2SW 20030128000822003012800082SW 2003 1 28 HEEA083836 120030116A6230406010427109 GIMBAL RING BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH2040 53461 MAIN ROTOR GIMBAL RING CORRODED UNDER BUSHINGS. 1G71 3U O H2SW 20030128000892003012800089WP 2003 1 28 03FDEA000040 120030115A1430 BOLT DOUG MD10 MD1010F WP GE CF6 CF6* 30020GL LT MLG OUT OF ADJUST A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25372FE 46610 ON GEAR RETRACTION LEFT MAIN GEAR LIGHT REMAINED RED. SECONDARY LEFT MAIN GEAR LIGHT REMAINED RED ALSO. RAN CHECKLIST FOR MAIN GEAR NOT UP AND LOCKED, LOWERED GEAR IAW CHECKLIST AND RETURNED FOR LANDING. FOUND DOOR LATCH ROLLER LINK PIVOT WITH EXCESSIVE TIGHTNESS, SPRINGS WOULD NOT RETURN LINK TO STOP. LOOSENED PIVOT BOLT AND RESAFTIED, MM. DOOR LATCH ROLLER LINK NOW RETURNS PROPERLY. OK FOR SERVICE. 2L73 4F4 FRTA22WE E23EA 20030128000942003012800094NM 2003 1 28 03FDEA00039 120030115A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION ON FLOORBEAM BS 312 AT FASTENER HOLES WL 207. 2L73 4F4 FRTA3WE E2EA 20030128001042003012800104SW 2003 1 28 HEEA083848 120030116A6230 BUSHING BELL 407 407 1182206SW PC LEVER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH AFS2197 53400 MAIN ROTOR PITCH CHANGE LEVER BUSHINGS WORN. 1G71 3U O H2SW 20030207000932003020700093NM 2003 2 7 03FDEA00044 120030116A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION ON FLANGE AND BEAM OB SIDE OF LT KEELBEAM STA 950A AFT CARGO BAY. REPAIRED KEELBEAM BS 950A + 2 STR 29L IAW SRM 27-53-023A. 2L73 4F RTA3WE 20030128001072003012800107SW 2003 1 28 HEEA083851 120030116A6230406010129101 ROD BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 MAIN ROTOR ROD ASSY WORN. 1G71 3U O H2SW 20030128001132003012800113EU 2003 1 28 03FDEA00047 120030119A2730 BEARING AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE ELEVATOR WORN A FDEAK NONE F FLT CONT AFFECTED CRCRUISE 1 SO25665FE 769 ON ROTATION FOR TAKEOFF ELEVATOR RESPONSE WAS VERY SLUGGISH AS IF A/P WAS ON IN CONTROL WHEEL STEERING. NO CHANGE IN HOW THE ELEV FELT AT 250 KIAS AND 320 KIAS. NO WARNING LIGHTS ILLUMINATED AT ANY TIME. DURING APPROACH ELEV RESPONSE FELT THE SAME FOUND CAPT AND FIRST OFFICERS VERTICAL TORQUE TUBES IN AFT FUSELAGE HAD SIGNIFICANT STIFFNESS DURING ROTATION. REMOVED VERTICAL TORQUE TUBES IAW AMM 27-31-21-4, REPLACED BEARINGS IAW CMM 27-31-38. REINSTALLED TORQUE TUBES IAW AMM 27-31-21-4. C/W MECHANICAL CONTROL AND PITCH UNCOUPLING ADJ AND TEST IAW AMM 27-31-00-5. 2L72 4F4 FRTA35EU E13NE 20030128001262003012800126SW 2003 1 28 HEEA083865 120030116A6310 SEAL BELL 407 407 1182206SW FREEWHEEL UNIT LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03493PH3020 A3910 53393 FREEWHEEL UNINT FWD AND AFT SEAL LEAKING OIL. REPLACED FREEWHEEL UNIT. 1G71 3U O H2SW 20030128001462003012800146SW 2003 1 28 HEEA083869 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001562003012800156SW 2003 1 28 HEEA083873 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001572003012800157SO 2003 1 28 C2XA02SH179 120030118A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2736915 145421 SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 INBOARD SIDE WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030128001592003012800159SW 2003 1 28 HEEA083874 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128001612003012800161SW 2003 1 28 HEEA083875 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030204002332003020400233NM 2003 2 4 SWAA030202 120030128A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 362, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030204002532003020400253NM 2003 2 4 VNAA0301016 120030115A3150 WARNING SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CALLED MAINTENANCE CONTROL AND THE MESSAGE HAD CLEARED. MAINTENANCE CONTROL HAD THE CREW RUN THE AIRCRAFT AT 100 PERCENT AND THE MESSAGE DID NOT RETURN. FLIGHT 4108 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002672003020400267WP 2003 2 4 ZW0A0301501 120030203A33502232 LAMP DOUG DC9 DC982 3022082WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13953U 49267 THE LEFT OVERWING EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 2-8-02 STL. --CLOSED-- 2L72 4F A6WE 20030204002752003020400275NM 2003 2 4 VNAA0301023 120030122A32347178011 CONTROL HANDLE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT FAULTY A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07471PS10257 3007 WHILE CLIMBING OUT, THE CREW NOTICED THE GEAR INDICATION LIGHTS HAD CAME BACK ON. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE ADVISED TO RETURN TO DAY. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL HANDLE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002902003020400290EA 2003 2 4 SWIA200311755 120030108A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA FS 484 CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07430SW 7523 FS 484 LBL 36.0 INTERCOSTAL ATTACH FLANGE CRACKED. FOUND DURING C CHECK INSPECTION. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-41-059. NDT-HFEC CARRIED OUT IAW REO 601R-53-41-059. NO CRACKS NOTED. 2L72 4F RTA21EA 20030205000012003020500001SO 2003 2 5 C2XA02SH190 120030205A533014523055005 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713913 145438 SHV- DURING C CHECK REAR FUSELAGE SKIN WAS FOUND TO HAVE A GOUGE JUST BELOW CENTER OF CARGO DOOR BUMPER PLATE. MAINTENANCE REPAIRED GOUGE IN AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5330-01219. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030205000342003020500034NM 2003 2 5 SROM200300001 120030104A7810 FAIRING BOEING737 737205 1384456NM NR 1 ENG TAILPIPGOUGED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 1 ENGINE TAIL PIPE FAIRING DAMAGED CORNER (LOWER) REPAIRED PER SRM 51-40-3. MINOR REPAIR. 2L72 4F RTA16WE 20030205000582003020500058NE 2003 2 5 NACA20030070 220030124A8530356993 CYLINDER PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE #6 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL037919C1453 1453 P36225 43554 P36225 DISCREPANCY: #3 ENGINE FEATHERED FOR BACKFIRING & VIBRATION.CORRECTIVE ACTION: REPLACED #6 CYLINDER. 2L74 4R4 R A781 5E8 20030205000632003020500063SO 2003 2 5 C2XA03CL029 120030203A3320BR900022 BALLAST EMB 145 EMB145ER 3260211SO CABIN FAULTY A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2714925 145004 CLE FLIGHT#2267 THE CREW REPORTED A ELECTRICAL BURNING SMELL COMING FROM ABOVE THE FLIGHT ATTENDANT CALL PANEL.MAINTENANCE INSPECTED AND REPLACED THE DIMMING BALLAST FOR THE CEILING LIGHTS ABOVE SEAT 1A.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030205001032003020500103NM 2003 2 5 PCAA0302033 120030203A554285540001003 RUDDER DHAV DHC8 DHC8102 2809003NM CRACKED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13824EX305178232 387 DURING ROUTINE MAINTENANCE VISIT, FORE RUDDER WAS FOUND CRACKED AT UPPER RIGHT SIDE WHILE PERFORMING A 4 INSPECTION. PATCH TO RUDDER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-335. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030205001372003020500137NM 2003 2 5 CALA0300023 120030117A5230 SKIN BOEING737 737824 13844BZNM FWD CARGO DR GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0927213 28773 INSPECTION FOUND A GOUGE AND DENT IN THE FORWARD CARGO DOOR EXTERNAL SKIN. THE GOUGE WAS APPROXIMATELY 6 INCHES IN LENGTH. THE DAMAGED AREA OF DOOR SKIN WAS REPAIRED IAW ECRA 5230-01709 AND SRM 52-00-01, REPAIR 3. 2L72 4F RTA16WE 20030205001392003020500139NM 2003 2 5 QXEA0300236 120030131A3230301450201 SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 FAILED A QXEAA UNSCHED LANDING O OTHER TOTAKEOFF 1 NM09404QX 4046 SEA ON FLIGHT 2311 AFTER TAKEOFF GEAR WOULD NOT RETRACT. CREW PERFORMED CHECKLIST AND RETURNED TO SEA. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030206000032003020600003NE 2003 2 6 DL76P030008 220030102A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 BIRD INGESTION A DALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO27143DA49810 25991 724151 BIRDSTRIKE AT APPROX 800 FT ON RIGHT ENGINE. ENGINE IMMEDIATLY STARTED MAKING A HUMMING NOISE AND ENGINE VIBS SHOWED 5.0. RETARDED ENGINE TO IDLE AND NOISE WENT AWAY. APPAND LANDING WERE MADE WITH ENGINE AT IDLE. FOUND SEVERAL BLADES AND EXIT GUIDE VANES DAMAGED. DAMAGED BLADES AND VANES REPLACED. 2L72 4F4 FRTA1NM E24NE 20030206000152003020600015NM 2003 2 6 DL76S030036 120030107A3350767 BULB BOEING767 767332 1382001NM LT OVERWING BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27134DL 25123 LT AFT OVERWING EMERGENCY LIGHT INOPERATIVE RELAMPED CKS GOOD 2L72 4F RTA1NM 20030206000162003020600016NE 2003 2 6 DL76S030048 220030111A75209295M25G07 DUCT BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 ENGINE CRACKED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27118DL 23277 580292 PILOT REPORTED NR 1 ENGINE HAD OVERHEAT LOOP 1 EICAS MSG AMD ALSO HAD OVERHEAT LOGHT ON PEDESTAL FLICKERING, CLOSED BLEED VALVE, LIGHT STILL FLICKERS, WENT OUT AFTER RETARDING THROTTLE. ON ENGINE INSPECTION FOUND TURBINE CASE COOLING DUCT CRACKED, REPLACED SAME. 2L72 4F4 FRTA1NM E13NE 20030206000392003020600039NM 2003 2 6 0300176718 120030128A5412 BULKHEAD BOEING747 747251F 1384898NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 During "L" Check found crack on #2 pylon rear engine mount bulkhead. Repaired per EA 67-165032. 2L74 4F A20WE 20030206001352003020600135EA 2003 2 6 COMA0360074 120030131A2740 DEBRIS MONITOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 SO01781CA 7312 FLIGHT 5376 STAB TRIM AND MACH TRIM CAUTION MESSAGE.CLEANED DEBRIS FROM STAB TRIM ENGAGE SWITCH. 2L72 4F RTA21EA 20030206001362003020600136EA 2003 2 6 COMA0360075 120030201A3040 WINDOW CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01986CA 7174 FLIGHT 5608 LEFT WINDOW HEAT CAUTION MESSAGE.SWITCHED TEMP SENSOR LEADS TO BACK UP SENSORS. 2L72 4F RTA21EA 20030206001382003020600138EA 2003 2 6 COMA0360077 120030201A2610 TERMINAL CNDAIRCL600 CL6002B19 1900309EA A COMAE ENGINE SHUTDOWN JN WARNING INDICATION FALSE WARNING CRCRUISE 1 SO01999CA 7230 FLIGHT 5433 LEFT ENGINE JETPIPE OVERHEAT WARNING.REPOSITIONED ALL 4 TERMINAL ENDS FOR JET PIPE LOOPS. 2L72 4F RTA21EA 20030206001442003020600144NM 2003 2 6 03FDEA00023 120030115A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 DENT IN EXTERNAL SKIN BS 1033 STR 22-23R. REPAIR PER SRM 53-30-3, SKIN AT BS 1033 STR 22-23R. 2L73 4F4 FRTA3WE E2EA 20030206001522003020600152EA 2003 2 6 COMA0360080 120030204A335036378 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR UNRELIABLE A COMAO OTHER O OTHER ININSP/MAINT 1 SO01916CA 7014 FLIGHT 5124 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED STRIP LIGHTS 2L72 4F RTA21EA 20030206001562003020600156WP 2003 2 6 ZW0A0301401 120030129A33503300016031 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139625W 53595 THE CEILING EMERGENCY LIGHTS AT ROW 25 TO THE AFT CABIN WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. 2L72 4F RTA6WE 20030206001582003020600158EA 2003 2 6 A6WA200340015 120030110A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A A6WAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 GL31424AW 7656 FLAP FAIL CAS MESSAGE FLAP FAIL AT ZERO DEGREES. NO FLAP LANDING. COMPLIED WITH QRH. REPLACED LEFT BPSU. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030206001822003020600182EU 2003 2 6 USAASA03002 120030101A3350 BATTERY PACK AIRBUSA319 A319112 3930323EU CABIN DISCHARGED A K NONE L NO TEST ININSP/MAINT 1 EA19727UW 1147 THE EXIT SIGN AT DOOR 2R WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE LIGHT ASSEMBLY AT THE AFT RIGHT DOOR. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030206001862003020600186NE 2003 2 6 A6WA200360001 220030104A7200 FIRE BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 1 ENGINE DETECTED A A6WAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 GL31183US E2043 WHILE STARTING NR 1 ENGINE, AGENTS SAW FLAMES. MOVED NR 1 THRUST HANDLE TO 'FUEL OFF'. AGENTS INDICATED FIRE PERSISTS. PULLED NR 1 FIRE HANDLE AND SHOT NR 1 BOTTLE, FIRE WENT OUT. NO COCKPIT INDICATION OF FIRE. OPS REPORTED A SUBSTANTIAL TAIL WIND DURING START MAINTENANCE INSPECTED TAILPIPE, TMS AND FCU RIGGING, NO DEFECTS NOTED. STARTED ENGINE 3 TIMES AND SUCCESSFULLY RAN. OVERSPEED AND FUEL SOV OPS NORMAL OK FOR CONTINUED SERVICE. (M) 2H74 4F4 F A49EU E6NE 20030206001912003020600191WP 2003 2 6 MWEA030057 120030203A533059114065 SKIN DOUG DC9 DC982 3022082WP STATION 168 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FORWARD PASSENGER ENTRY DOOR JAMB UPPER FORWARD CORNER SKIN CRACKED. -- CUTOUT DAMAGE AND FABRICATED AND INSTALLED DOUBLERS. 2L72 4F A6WE 20030207000182003020700018NM 2003 2 7 DLM88030056 120030114A7920 O-RING DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENG OIL CUT A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27965DL 49984 725772 LT ENGINE OIL QTY DECREASED TO ZERO IN FLIGHT. OTHER ENGINE INDICATIONS NORMAL. REPLACED CUT O-RING ON OIL TRANSFER TUBE. 2L72 4F4 FRTA6WE E9NE 20030207000962003020700096NM 2003 2 7 03FDEA00051 120030120A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 FRAME CRACKED IN THE FWD CARGO BAY. REMOVED DAMAGED FRAME FLANGE. FABRICATED, & INSTALLED REPAIR PARTS IAW SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20030207000992003020700099NM 2003 2 7 03FDEA00054 120030120A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION ON SEAT TRACK OB FLANGE BS 650-660 LBL 25 WL 208. R&R SEAT TRACK PER SRM 51-30-2. 2L73 4F RTA3WE 20030207001082003020700108NM 2003 2 7 03FDEA00065 120030122A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 CORROSION ON FLOORBEAM LOWER CHORD UPPER SURFACE STA 1130, RBL 4, WL 201. REMOVED CORROSION ON FLOORBEAM LOWER CHORD UPPER SURFACE BS 1130, RBL 1-RBL 8, WL 201, IAW SRM. 100 PERCENT MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED LOWER FLANGE OF FLOORBEAM IAW SRM. 2L73 4F RTA3WE 20030207001112003020700111NM 2003 2 7 03FDEA00071 120030122A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 DENT IN SKIN AT FRAME BS 460 BETWEEN STR 20R - 21R. FOUND SKIN TO BE WITHIN LIMITS. SHEAR TIE AT BS 460 STR 20R-21R OUT OF LIMITS. REPAIRED SHEAR TIE IAW SRM 51-40-3 FIG 1 AND EA 7-5310-54395. 2L73 4F RTA3WE 20030207001152003020700115NM 2003 2 7 03FDEA00074 120030125A3260 POSITION SWITCH BOEING727 727100 1384036NM PWA JT8 JT8D1 52044NE NLG FAULTY A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25188FE 19081 INFLIGHT, NO NOSE GEAR DOWN INDICATION. (GREEN LIGHTS). REPLACED BOTH BULBS NO EFFECT. CYCLED GEAR, TESTED BULBS, DID NOT WORK, REPLACED BOTH BULBS, AGAIN A VERY WEAK LIGHT, GOOD INDICATION, WENT TO BRIGHT, WORKED. BACK TO DIM AND WAS INTERMITTENT, LANDING NORMAL IN ALL RESPECTS. REMOVED AND REPLACE THE NOSE GEAR POSITION SWITCH IAW MM 32-61-021-4. CLEANED CONNECTOR PLUG. OPS CHECKED NORMAL. AIRCRAFT OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20030207001162003020700116NM 2003 2 7 03FDEA00077 120030127A5311 FRAME BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 AFT CARGO BAY BS 950C, STR 26L IS DENTED IN UPPER FLANGE. NO DENTS ALLOWED IN FRAMES. DETERMINED OUT OF LIMITS IAW SRM 53-10-1. REMOVED DENTED MATERIAL AT BS 950C, STR 26L, IAW SRM 51-40-3 FIG 1. SSI INSPECTION PERFORMED IAW BOEING D6-48040-1. FABRICATED, DRILLED, COUNTERSUNK, ALODINED, PRIMED AND INSTALLED REPAIR PART IAW SRM 51-40-3 FIG 1. 2L73 4F4 F A3WE E2EA 20030207001192003020700119NM 2003 2 7 03FDEA00082 120030129A2781 SWITCH BOEING727 727200 138407ENM L/E FLAP FAULTY A FDEAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25286FE 22623 AFTER TAKEOFF WHEN RETRACTING FLAPS FROM 5 DEGREES THE PILOTS L/E FLAP AMBER LIGHT ILLUMINATED. S/O PANEL SHOWED THE NR 1 L/E FLAP WAS AMBER. RAN RED TABS RETURNED TO MEM AFTER DUMPING APPROX 4000 LBS FUEL. R&R NR 1 L/E FLAP SWITCH REF B727 MM 27-82-001-4. 2L73 4F RTA3WE 20030207001202003020700120NM 2003 2 7 03FDEA00087 120030130A5320 SPLICE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION ON FWD CARGO BAY STRINGER SPLICE BS 485 STRINGER 28 LT. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3. 2L73 4F RTA3WE 20030207001212003020700121NM 2003 2 7 03FDEA00088 120030130A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION BS 1130 WL 201 LBL 37 - RBL 51, CORROSION AROUND NUT PLATE HOLES ON LWR FLOORBEAM CHORD AFT CARGO BAY. 2L73 4F RTA3WE 20030207001222003020700122NM 2003 2 7 03FDEA00098 120030203A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION ON FLOORBEAM UPPER FLANGE. 2L73 4F RTA3WE 20030207001312003020700131WP 2003 2 7 ZW0A0301601 120030204A3350408822101 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139402W 53138 THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 27 TO 29. REPLACED BATTERIES FOR THE EMERGENCY LIGHTS. 2L72 4F RTA6WE 20030207001522003020700152WP 2003 2 7 ZW0A0301701 120030206A3350408822101 BATTERY DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139405T 53141 THE EGRESS LIGHTS BETWEEN ROWS 21 AND 26, AND BOTH AFT OVERWING EXIT LOWER EXIT LIGHTS, WERE INOPERATIVE. REPLACED THE BATTERIES IN BOTH BATTERY PACKS. CHECK-C 10-19-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030207001542003020700154NM 2003 2 7 ZW0A0301703 120030206A79308D1497 SWITCH BOEING757 757231 1384950NM PWA 2037 PW2037 NE A ZW0AAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE13725TW 30338 4946 AFTER DEPARTING SFO THE RH ENGINE OIL FILTER STATUS MESSAGE APPEARED. THE RH ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO SFO. THE ENGINE DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. CHECK-C 1-16-02 MCI. ---CLOSED--- 2L72 4F4 FRTA2NM E17NE 20030207001562003020700156SO 2003 2 7 C2XA03BT025 120030202A3230 MODULE EMB 145 EMB145LR 3260212SO FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW2712540 145537 EWR---CO2095, CREW REPORTED, " UPON TAKEOFF, GEAR HANDLE MOVED UP, GEAR CAME UP WITH AURAL WARNING. CONTINUOUSLY SOUNDED." AIRCRAFT AIRTURNED TO EWR. MAINTENANCE REMOVED AND REPLACED LANDING GEAR MODULE IAW EMB145 MM #32-32-02. SWUNG LANDING GEAR AND CLEANED UPLOCK SWITCHES. OPERATIONAL TEST OF LANDING GEAR GOOD IAW EMB145 MM #32-30-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030207001572003020700157SO 2003 2 7 C2XA03BT026 120030203A3200 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO FAULTY A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2714938 145029 EWR---CO 2143, CREW REPORTED, " LANDING GEAR/ GROUND FAILURE MESSAGE ON EICAS WHEN GEAR DOWN IS SELECTED." MAINTENANCE REMOVED AND REPLACED LEFTHAND LANDING GEAR SHOCK ABSORBER PROXIMITY SWITCH, OPS. CHECKED GOOD IAW EMB145 MM #32-63-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030207001622003020700162NM 2003 2 7 NACA20030073 120030206A2450ZL2790A VOLT REGULATOR BOEING727 727100 1384036NM PWA JT8 JT8D NE 1 TRIPPED A NACAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 AL03930FT33 33 19387 P657108 DISCREPANCY: ON TAKE OFF ROLL LOST #1 ENG GEN ESSENTIAL POWER WITH #3 ENGINE GENERATOR SELECTED.CORRECTIVE ACTION: REPLACED #1 VOLTAGE REGULATOR. 2L73 4F4 FRTA3WE E2EA 20030207001632003020700163CE 2003 2 7 047632 120030206A75003031829 TUBE BEECH 1900 1900D 1154162CE CRACKED A AMWAO OTHER R PARTIAL RPM/PWR LOSS APAPPROACH 1 CE07218YV UE218 UPON APPROACH FOR LANDING ON FLIGHT 5441 IN CHARLOTTE NORTH CAROLINA, THE LEFT ENGINE TORQUE FELL TO BETWEEN 0-500LBS. ALL THE OTHER ENGINE INDICATIONS WERE NORMAL. THE CREW THEN SHUT DOWN THE ENGINE. THE CREW ALSO DID THE EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED LEFT HAND PNUEMATIC TUBE ASSEMBLY P3 AIR FRONT TUBE. NO TEARDOWN WILL BE REQUIRED. 2L72 4T RTA24CE 20030208000012003020800001EU 2003 2 8 RAIA00301018 120030118A261351228318 SENSOR JETAIRJETSTMJETSTM4101 1500501EU FALSE INDICATIONA RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03558HK 41071 5516-STL- RIGHT HAND OVER HEAT LOOP WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVER HEAT SENSOR, OPS CK OK. 2L72 4T RTA41NM 20030128001642003012800164NM 2003 1 28 QXEA0300127 120030126A33506138001 BATTERY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX3373 0 4032 PDX- WHILE PERFORMING EMERGENCY LIGHT SYSTEM CHECK, RIGHT HAND FORWARD SIDEWALL AND FORWARD PIT WALL LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED BOTH BATTERY PACKS. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030128001722003012800172WP 2003 1 28 ZW0A0300806 120030110A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT FOUND CORROSION ALONG FLOOR SUPPORT AT STA 148 TO 200, 8 INCHES RBL, UNDER NUMBER 4 FLOOR PANEL. INSTALLED NEW FLOOR SUPPORT, FABRICATED FROM EXTRUSION PER SPM 6-70-01. 2L72 4F A6WE 20030128001852003012800185WP 2003 1 28 ZW0A0301104 120030117A5230 BRACKET DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C CRACKED BRACKET FOR LOWER AFT DOOR STOP FORWARD CARGO DOOR. REPLACED BRACKET PER SRM 52-03. 2L72 4F A6WE 20030128001952003012800195EU 2003 1 28 AWXA200300023 120030109A3320325060 BALLAST AIRBUS320 A320231 3930325EU CABIN MALFUNCTIONED A AWXAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28620AW 052 PHX - BURNING SMELL - BURNING ELECTRICAL ODOR OBSERVED AROUND ROW 20. MAINTENANCE REMOVED AND REPLACED CEILING LIGHT BALLAST SEAT ROW 20 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030128002002003012800200NM 2003 1 28 AWXA200300028 120030111A3350900835A BATTERY BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 AUS - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS AND BATTERY PACK ON EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030128002032003012800203NM 2003 1 28 DHL2003727001 120030128A2900 VALVE BOEING727 727228 1384083NM A DHLADO RETURN TO BLOCK OTHER O OTHER TXTAXI/GRND HDL 1 SO01727DH 20204 1) DURING PUSH BACK THE HYDRAULIC BRAKE PRESSURE STARTED TO DECREASE TO 2100 PSI.2) FOUND LEAKING SHRAEDER VALVE FOR BRAKE ACCUMULATOR. REPLACED VALVE AND RESERVICED ACCUMULATOR. OPS CHECKED GOOD IAW 29-12-42 AND 12-15-01. 2L73 4F RTA3WE 20030128002402003012800240EU 2003 1 28 AWXA200300053 120030119A276031077100 SERVO AIRBUS320 A320231 3930325EU SPOILER MALFUNCTIONED A AWXAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP28633AW4178119237 082 EWR - EL - FLT 685 IN CRUISE FLIGHT, AN ECAM MESSAGE FLT CTL SPLR FAULT ILLUMINATED SPOILER NR 1. MAINTENANCE REPLACED RT NR 1 SPOILER SERVO CONTROL IAW MM 27-64-51-401. 2L72 4F RTA28NM 20030128002412003012800241SW 2003 1 28 HEEA083890 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002432003012800243SW 2003 1 28 HEEA083892 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002472003012800247SW 2003 1 28 HEEA083895 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030128002522003012800252SW 2003 1 28 HEEA083899 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH NHFS5396 53390 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030128002582003012800258SW 2003 1 28 HEEA083905 120030117A6320406340100101 PUMP BELL 407 407 1182206SW GEARBOX OIL LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03495PH 53397 MAIN ROTOR GEARBOX OIL PUMP LEAKING. 1G71 3U O H2SW 20030128002612003012800261NM 2003 1 28 C1HA200395003 120030119A3350 BATTERY PACK BOEING727 727290 138408WNM CABIN DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15295AS 22147 OVERHEAD EMERGENCY LIGHT AT ROW 24 (STA 950) INOP.REMOVED & REPLACED PASS CABIN CEILING EMER LIGHT BATTERY PACK AT ROW 24 STA 950 IN REF TO M/M CH 33-50-01 OPS CHECK OKAY 2L73 4F A3WE 20030128002662003012800266EA 2003 1 28 COMA0360054 120030125A3030 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING S AFFECT SYSTEMS TOTAKEOFF 1 SO01989CA 7215 FLIGHT 5562 TAT AND R/H PITOT HEAT CAUTION MESSAGE.RESET SYSTEM CIRCUIT BREAKERS, FAULT CLEARED. 2L72 4F RTA21EA 20030128002672003012800267EA 2003 1 28 COMA0360055 120030126A5220 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF K FLUID LOSS TOTAKEOFF 1 SO01952CA 7092 FLIGHT 5850 DURING T/O A LARGE AMOUNT OF FLUID DRAINED FROM THE LIGHT CONTROL PANEL.RESEALED THE CREW DITCHING HATCH. 2L72 4F RTA21EA 20030128002682003012800268EA 2003 1 28 COMA0360056 120030124A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01917CA 7017 FLIGHT 5938 FLAPS FAIL MESSAGE DURING TAXI.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030220000772003022000077NM 2003 2 20 QXEA0300073 120030107A7110 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM LT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- LEFT HAND ENGINE LOWER COWL 412AB LEFT HAND UPPER BYPASS DOOR SUPPORT BRACKET IS CRACKED AT RIVET. REPAIRED IAW DHC-8 400 RD 8/4-71-016. 2H72 4T RTA13NM 20030220000802003022000080WP 2003 2 20 ABXA030076 120030218A2760 DRAIN DOUG DC9 DC941 302207NWP SPOILERS FROZEN A ABXAB EMER. DESCENT F FLT CONT AFFECTED APAPPROACH 1 GL23951AX 47616 DEPLOYING SPOILERS CREATED A LT ROLL OF 5 DEGREES PER SECOND. AILERONS BINDED DURING APPROACH, AILERONS HEAVY DURING APPROACH. FOUND SLAT PANEL DRAINS BLOCKED BY ICE, WATER LEAKED OUT OF SLANT PANEL AND DOWN ONTO AILERON AND SPOILER CABLES, FREEZING THEM UP. THAWED ALL AND CHECKED. OPS CHECKED GOOD IAW DC-9 MM CHAPTER 27. 2L72 4F A6WE 20030220000812003022000081EA 2003 2 20 QXEA0300077 120030111A3080 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09611QX 10041 SEA ON FLIGHT 2507- RIGHT WING ANTI-ICE CAUTION MESSAGE WITH WING ANTI-ICE SELECTED ON. PERFORMED CHECKLIST AND MESSAGE REMAINED ON. INTEROGATED MDC, NO FAULTS FOUND. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220000842003022000084NE 2003 2 20 QXEA0300082 220030114A72504124T3P03 TURBINE BLADES GE CF348C1 CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX GEE965223 10009 965223 PDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE HPT 1 BLADE 2/3 MISSING AND TWO BLADES CRACKED. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION OF THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCLERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEE DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030220000932003022000093NM 2003 2 20 QXEA0300089 120030116A5230 SPRING BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR STICKING A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 PDX - FLIGHT 2329 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A FORWARD BAGGAGE DOOR CAUTION LIGHT AND THE AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE DOOR SPRING STICKING. THE DOOR AND SPRING WAS CLEANED AND LUBRICATED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20030220000992003022000099EU 2003 2 20 QXEA0300094 120030112A5312 ANGLE FOKKERF28 F28MK4000 4990810EU FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09492US 11159 PDX- FORWARD PRESSURE BULKHEAD BOTTOM CONNECTION ANGLE HAS A THREE INCH LONG CRACK IN RADIUS, AFT SIDE OF BULKHEAD FS1550 THROUGH 3 INCHES LEFT OF BL0. REPAIRED IAW FOKKER SRM 53-02-18 AND HORIZON AIR EA 4-53-1578. 2L72 4F RTA20EU 20030220001022003022000102EU 2003 2 20 QXEA0300096 120030111A5720 CHANNEL FOKKERF28 F28MK4000 4990810EU LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09497US 11173 PDX- LEFT HAND WING LOWER STATION 2230 RIB 'U' CHANNEL HAS EXFOLIATION CORROSION ON THE INTERIOR AT STRINGER 2.13 APPROXIMATELY .5 INCHES LONG. REPAIRED IAW FOKKER SRM 57-01-01. 2L72 4F RTA20EU 20030220001042003022000104EA 2003 2 20 QXEA0300098 120030110A2820 B-NUT CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM LOOSE A QXEAK NONE K FLUID LOSS ININSP/MAINT 1 NM09603QX 10011 BOI- FOUND LEAK OUT OF LEFT FORWARD FUEL SUMP DRAIN IN CENTER TANK DURING TESTING OF EO R-28-96. FOUND PRIMARY EJECTOR FUEL-FEED TUBE 'B' NUT LOOSE. RETORQUED 'B' NUT IAW AMM TR 28-0152. 2L72 4F RTA21EA 20030220001052003022000105NM 2003 2 20 QXEA0300100 120030117A3260 SENSOR BOMBDRDHC8 DHC8401 1390041NM RT MLG OUT OF ADJUST A QXEAK NONE J WARNING INDICATION CRCRUISE 1 NM09411QX 4055 GEG-MAIN LANDING GEAR DOORS SHUFFLE INFLIGHT OPEN PARTIALLY THEN CLOSE. THE AMBER GEAR LIGHT COMES ON FOR A SPLIT SECOND AND YOU CAN FEEL A VIBRATION IN AIRCRAFT. ADJUSTED RIGHT GEAR DOOR CLOSED SENSOR. GAP CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001062003022000106NM 2003 2 20 QXEA0300101 120030118A3230465005 UPLOCK BOMBDRDHC8 DHC8401 1390041NM RT MLG MALFUNCTIONED A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09411QX2607 4055 SEA-AFTER TAKEOFF, LANDING GEAR CYCLED SEVERAL TIMES. GEAR HANDLE LIGHT CAME ON AND LEFT AND RIGHT GEAR UNSAFE AND LEFT AND RIGHT DOOR LIGHTS CYCLED ON AND OFF. REMOVED AND REPLACED RIGHT HAND MAIN LANDING GEAR UPLOCK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001122003022000112EA 2003 2 20 QXEA0300107 120030119A5310 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA FUSELAGE BIRD STRIKE A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09613QX 10045 SMF - FLIGHT 2493 - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF A BIRD STRUCK THE AIRCRAFT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF DAMAGE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220001242003022000124EA 2003 2 20 COMA0360107 120030218A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01966CA 7132 FLIGHT 5587 R/H THRUST REVERSER UNLOCKED MESSAGE DURING T/O.SECURED T/R AND DEFERRED MAINT. PER MEL. 2L72 4F RTA21EA 20030220001272003022000127NM 2003 2 20 QXEA0300121 120030122A2612 CONNECTOR DHAV DHC8 DHC8202 2809007NM NR 2 ENGINE NOT SEATED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09366PH 510 SEA ON FLIGHT 2029- NR 2 ENGINE CHECK FIRE DETECTION LIGHT ILLUMINATED WITH MASTER WARNING. RAN CHECKLIST. RESEATED CANNON PLUG ON NR 2 ENGINE LOOP A CONNECTION. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001282003022000128EA 2003 2 20 COMA0360105 120030217A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01932CA20705 7038 FLIGHT 5647 GEAR DISAGREE WARNING AFTER T/O.REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030115002182003011500218EA 2003 1 15 COMA0360030 120030110A5346601R5361366 WEB CNDAIRCL600 CL6002B19 1900309EA BEAM CRACKED A COMAO OTHER O OTHER ININSP/MAINT 1 SO01796CA8345 7338 THE ENGINE SUPPORT BEAM LOWER WEB L/H SIDE WAS CRACKED AT FS 628, WL111 AND LBL37.REMOVED THE CRACKED AREA, PEFROMED EDDY CURRENT TO ENSURE ALL DAMAGE WAS REMOVED AND INSTALLED REPAIR PAERTS I/A/W REO 601R-53-61-366 REV E. 2L72 4F RTA21EA 20030116000042003011600004SW 2003 1 16 ERAA082946 120030106A6230412010402111FM SWASHPLATE BELL 412 412 1182202SW MAIN ROTOR WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01 13561 SWASHPLATE ASSY HAS WORN GIMBAL RING BEARINGS. DISASSEMBLED TO FACILITATE GIMBAL RING BEARING REPLACEMENT. REPLACED GIMBAL RING BEARINGS AND GIMBAL RING BOLTS, 1 TRUNNION, AND INSTALLED MAG PICKUP BRACKET & SENSOR. COMPLIED WITH RETORQUED IAW TB 412-84-40. COMPLIED WITH ASB412-02-110 NEW BOLTS IN GIMBAL RING. REASSEMBLED SWASHPLATE ASSY, TORQUED & SAFETY WIRED AS REQUIRED. LUBED WITH MOBILE 28. REPAIRED IAW 412 CR&O CH 62 MM 62 SRM & APPLICABLE BULLETINS COMPLIED WITH TB412-84-40, ASB 412-02-110. 1G72 4U H4SW 20030116000062003011600006GL 2003 1 16 ERAA082948 220030106A7321252464431 FUEL CONTROL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE CONTAMINATED H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01292EH13409 562 ENGINE WILL NOT START, FUEL WON'T GO TO NOZZLE, HAS NEW SCREEN. FCU CONTAMINATED, REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-602E (FUEL SIDE OF FCU FLUSHED DUE TO CONTAMINATION) 1G72 3U3 U H3EU E4CE 20030116000102003011600010NE 2003 1 16 HEEA082967 120030107A3246 TIRE SKRSKYS76 S76A 8143006NE WHEEL ASSY WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW035426U PHI0031 760167 MAIN LANDING GEAR WHEEL HAS A WORN TIRE. REPAIRED. 1G72 3U H1NE 20030116000132003011600013 2003 1 16 HEEA082970 420030107A3416212070238003 INDICATOR SKRSKYS76 S76A 8143006NE ALTIMETER INACCURATE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034253S 760035 COPILOT SIDE ALTIMETER INDICATOR IS 200 FT. DIFFERENT FROM PILOTS SIDE. IN SHOP REPAIR. 1G72 3U H1NE 20030116000162003011600016NE 2003 1 16 HEEA082973 120030107A673041004077 HOUSING SKRSKYS76 S76A 8143006NE M/R SERVO LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033122G 0775 760232 PIN PLUG IN MAIN ROTOR SERVO HOUSING LEAKED DURING FINAL TEST. 1G72 3U H1NE 20030116000182003011600018 2003 1 16 HEEA082975 420030107A34447001840913 TRANSCEIVER SKRSKYS76 S76A 8143006NE RADAR ALTIMETER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 RADAR ALTIMETER INDICATES 50 FEET AT ALL ALTITUDES AND TEST AT 130 FEET. IN SHOP REPAIR. 1G72 3U H1NE 20030116000242003011600024NE 2003 1 16 HEEA082981 120030107A21207650007901102 BLOWER SKRSKYS76 S76A 8143006NE AIR DISTRIBUTIONINOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 VENT BLOWER INOPERATIVE - POPS BLOWER POWER CIRCUIT BREAKER. 1G72 3U H1NE 20030116000302003011600030 2003 1 16 HEEA082987 420030107A3442MI585202 ANT PEDESTAL SKRSKYS76 S76A 8143006NE RADAR SYS DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 RADAR STOPS WORKING - DISPLAYS "ANT" FAULT. SHOP REPAIR. 1G72 3U H1NE 20030116000322003011600032 2003 1 16 HEEA082990 420030107A2564PHI10090 LIFE VEST SKRSKYS76 S76A 8143006NE CABIN LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 LIFE VEST LEAKING. 1G72 3U H1NE 20030116000342003011600034GL 2003 1 16 HEEA082992 220030109A725023053299 TURBINE WHEEL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N1135 51512 CAE890024 ENGINE REMOVED DUE TO EXCESSIVE OIL CONSUMPTION. TURBINE WAS REPAIRED DUE TO EXCESSIVE OIL CONSUMPTION AND OIL QUENCHED 1ST STAGE WHEEL. SCRAPPED WHEEL. 1G71 3U3 U H2SW E1GL 20030116000382003011600038SW 2003 1 16 HEEA082997 120030106A7740DPUA0101 COMPUTER BELL 206 206L4 1182110SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0362127 52023 COMPUTER FAILS ENGINE TORQUE VALUES, READINGS INDICATE ALL 9'S. 1G71 3U NCH2SW 20030116000412003011600041SW 2003 1 16 HEEA083000 120030106A7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 51029 COMPUTER HAS MULTIPLE NR FAULTS. 1G71 3U H2SW 20030116000432003011600043SW 2003 1 16 HEEA083002 120030106A7797DPUK0414 WIRE HARNESS BELL 206 206L4 1182110SW INTELASTART COMPFAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 COMPUTER HAS CONTINUOUS ANNUNCIATION ON INTELLISTART LIGHT ASSY DUE TO FAULT. TROUBLESHOT WIRING IN AIRCRAFT, FOUND PINS 25 AND 26 SWAPPED WITH PINS 35 AND 36. ALSO REPLACED PROCESSOR DUE TO THE MISPLACEMENT OF PINS. 1G71 3U NCH2SW 20030116000532003011600053SW 2003 1 16 HEEA083012 120030106A6420LB21010202 BEARING BELL 206 206L3 1182108SW ROTOR HEAD SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03129MR1830 HB22 51129 BEARING ELASTOMER SEPARATED AROUND TRUNNION SPINDLE AREA. 1G71 3U H2SW 20030116000542003011600054SW 2003 1 16 HEEA083013 120030106A3220M206SW9371 PLENUM BELL 206 206L3 1182108SW MLG MISMANUFACTURED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW036748D 51106 PLENUM BOXES DO NOT FIT CONTOUR OF NOSE PANEL. OUTBOARD AFT EDGE HAS 1/4 INCH GAP BETWEEN PANEL AND PLENUM BOX. DIMENSION ON NEW PLENUM BOX DOES NOT MATCH THE PLENUM BOX THAT WAS REMOVED. ALSO REMOVED -2 PLENUM. SHIMMED THE GAP ON BOTH AIRBOXES ON INSTALLATION. 1G71 3U H2SW 20030116000642003011600064SW 2003 1 16 HEEA083023 120030106A6320PHI206052 MAGNETIC SEAL BELL 206 206L3 1182108SW M/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033116P 51530 MAIN ROTOR GEARBOX MAGNETIC SEAL LEAKING. REPLACED WITH SERVICEABLE SEAL. 1G71 3U H2SW 20030116000732003011600073SW 2003 1 16 HEEA083033 120030106A2430SM20ACD200A21 RELAY BELL 206 206L3 1182108SW DC SYSTEM BURNED E O OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 RELAY STUCK CLOSED AND BURNED. 1G71 3U H2SW 20030116000862003011600086 2003 1 16 HEEA083046 420030106A2312064101902 TRANSCEIVER CLARK 1000 1000CLARK 2230102SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TRANSCEIVER INTERMITTENT RECEPTION. REPLACED Q309, Q310 AND Q315 TRANSISTORS AND REALIGNED RECEIVER. ADJUSTED CARRIER SQUELCH, FREQUENCY. REPAIRED. BENCH CHECK GOOD. 1Q71 3R 2A6 20030116000892003011600089CE 2003 1 16 046484 120030106A3260 ANNUNCIATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA COCKPIT DAMAGED A AMWAK NONE N FALSE WARNING APAPPROACH 1 CE07174YV UE174 UPON ARRIVAL,FLIGHT 5481, THE LANDING GEAR HANDLE WAS DOWN. THERE WAS NO GREEN INDICATION ON THE NOSE. THE CREW THEN PERFORMED A MANUAL EXTENSION. THE TOWER CONFIRMED THAT THE GEAR APPEARED DOWN. THE CREW LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPAIRED THE NOSE LANDING GEAR ANNUNCIATOR, THEREFORE NO PARTS WERE USED. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T3 TRTA24CE E2NE 20030116000972003011600097SW 2003 1 16 HEEA083052 120030107A5302212030156023S DOUBLER BELL 412 412 1182202SW TAIL BOOM MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 DOUBLER DOES NOT HAVE THE PROPER FITTING AT THE RADIUS. REPLACMENT APPEARS TO HAVE STRAIGHT LINE BEND CONTOUR AND NOT THE REQUIRED AIRFRAME STRUCTURE CONTOUR TO FIT THE FUSELAGE AFT BULKHEAD AT THE LOWER T/B MOUNTING BOLT AREAS. 1G72 4U H4SW 20030116001162003011600116 2003 1 16 HEEA083065 420030107A2312064101902 TRANSCEIVER BELL 206 206L1 1182107SW VHF SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0320898 45721 TRANSCEIVER RECEIVES INTERMITTENTLY. FOUND NO RECEIVER AUDIO DUE TO BAD C147 CAPACITOR. REPLACED. REPAIRED PROBLEM. REALIGNED RECEIVER AND ADJUSTED C/N SQUELCH, MIC GAIN AND SIDETONE. CLEANED FACEPLATE AND BENCH CHECK GOOD. 1G71 3U H2SW 20030116001182003011600118 2003 1 16 HEEA083067 420030107A2312064101902 TRANSCEIVER BELL 206 206L1 1182107SW VHF SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031076Y 45380 VHF TRANSCEIVER LED WOULD NOT DISPLAY. REPLACED DS501 DISPLAY AND LENS. REPAIRED. FOUND RECEIVER A LITTLE WEAK AT 118 MHZ. ALIGNED RECEIVER AND ADJUSTED C/N SQUELCH. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001212003011600121 2003 1 16 HEEA083070 420030107A2312064101905 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038591X 51495 VHF TRANSCEIVER DISPLAY HAS BURNED OUT DIGITS. REPLACED BAD DISPLAY. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001222003011600122 2003 1 16 HEEA083071 420030107A2312064101905 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0349EA 51507 SELECTOR KNOB STICKING. FOUND SW101 TRANSFER SWITCH AND BUTTON BROKEN. ALSO FOUND FACEPLATE CRACKED AND RECEIVER BOARD HINGES BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001262003011600126WP 2003 1 16 MWEA030033 120030116A53135910493533 DOUBLER DOUG DC9 DC932 3022066WP STA 965 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 FUSELAGE DENT AFT OF CARGO DOOR STATION 965 BETWEEN LONGERON 25-26 RIGHT. -- FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030116001302003011600130 2003 1 16 HEEA083075 420030108A2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 VHF TRANSCEIVER TRANSMITS WEAK. FREQUENCY OFF ABOUT 500 HZ. ADJUSTED FREQUENCY AND SIDETONE. REPLACED BAD DISPLAY LENS. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001352003011600135 2003 1 16 HEEA083080 420030108A3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 AT 1800 FEET RADAR ALTIMETER DISPLAYS 400-500 FT. SHOP REPAIR. 1G71 3U H2SW 20030116001392003011600139 2003 1 16 HEEA083083 420030108A3452066106200 TRANSPONDER BELL 206 206B3 1181506SW ATC SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 ATC TRANSPONDER INOPERATIVE. REPLACED Q415 TRANSISTOR, R477 RESISTOR AND V101 CAVITY OSCILLATOR. REPAIRED. ADJUSTED FREQUENCY AND PULSE WIDTH. CLEANED CODE SELECTORS. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001432003011600143 2003 1 16 HEEA083087 420030108A3452066106200 TRANSPONDER BELL 206 206L3 1182108SW ATC SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F ATC TRANSPONDER INOPERATIVE. 1G71 3U H2SW 20030116001492003011600149 2003 1 16 HEEA083093 420030108A2312071104302 TRANSCEIVER KFS570B BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 TRANSCEIVER KNOB TURNS 360 DEGREES. STRAIGHTENED BENT ON/STBY/OFF SELECTOR SWITCH STOP. BENCH CHECK GOOD. 1G71 3U H2SW 20030129000082003012900008SW 2003 1 29 HEEA083918 120030117A6220407001526101 BELLCRANK BELL 407 407 1182206SW M/R HEAD DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 MAIN ROTOR HEAD BELLCRANK RUBBER IS DEBONDED. 1G71 3U O H2SW 20030129000102003012900010SW 2003 1 29 HEEA083920 120030117A6720407001731101 LINK BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 LINK ASSY HAS A ROUGH AND DAMAGED BEARING. 1G71 3U O H2SW 20030129000142003012900014SW 2003 1 29 HEEA083924 120030117A6220 BEARING BELL 407 407 1182206SW M/R HEAD SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH3284 A345 53400 MAIN ROTOR HEAD SPINDLE BEARING SEPARATED. REPAIRED. 1G71 3U O H2SW 20030129000172003012900017SW 2003 1 29 HEEA083927 120030117A6220407010100115 ROTOR HEAD BELL 407 407 1182206SW MAIN ROTOR MISALIGNED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03407PH 53003 UNABLE TO INSTALL ON MAST DUE TO SPLINE MISALIGNMENT. REPAIRED. 1G71 3U O H2SW 20030129000182003012900018SW 2003 1 29 HEEA083928 120030117A6320407010104109 CONE BELL 407 407 1182206SW M/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 MAIN ROTOR GEARBOX LOWER CONE PITTED ON FACE. 1G71 3U O H2SW 20030129000202003012900020SW 2003 1 29 HEEA083930 120030117A6220 SPRING BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH A654 53393 MAIN ROTOR HEAD FRAHM ASSY HAS THREE CRACKED SPRINGS. 1G71 3U O H2SW 20030129000232003012900023SW 2003 1 29 HEEA083933 120030117A6220 SPRING BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH LK66 53400 MAIN ROTOR HEAD FRAHM ASSY HAS A BROKEN SPRING. 1G71 3U O H2SW 20030129000242003012900024SW 2003 1 29 HEEA083934 120030117A6220 SPRING BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH A324 53398 MAIN ROTOR HEAD FRAHM ASSY HAS A BROKEN SPRING. 1G71 3U O H2SW 20030129000292003012900029SW 2003 1 29 HEEA083942 120030117A6420407012101111 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR OUT OF BALANCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 UNABLE TO BALANCE TAIL ROTOR HEAD. REPAIRED. 1G71 3U O H2SW 20030129000322003012900032SW 2003 1 29 HEEA083945 120030117A6420407012101111 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 TAIL ROTOR HEAD MAKING A CLICKING NOISE WHEN BLADE IS FLAPPED. REPAIRED. 1G71 3U O H2SW 20030129000342003012900034SW 2003 1 29 HEEA083947 120030117A6420407012101111 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR NOISY E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW03612PH 53199 TAIL ROTOR HEAD PRODUCING A HIGH FREQUENCY AT HOVER. REPAIRED. 1G71 3U O H2SW 20030129000422003012900042SW 2003 1 29 HEEA083955 120030117A6420407012109101 CROSSHEAD BELL 407 407 1182206SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 TAIL ROTOR HEAD CROSSHEAD HAS SPLINES WORN. 1G71 3U O H2SW 20030129000482003012900048SW 2003 1 29 HEEA083961 120030117A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 MAIN ROTOR BLADE HAS SEPARATION ON BOTTOM OF BLADE. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030129000502003012900050SW 2003 1 29 HEEA083963 120030117A5320407023800128S ANGLE BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH 53278 FUSELAGE ANGLE IS CRACKED. 1G71 3U O H2SW 20030129000522003012900052SW 2003 1 29 HEEA083965 120030117A5302 STRUCTURE BELL 407 407 1182206SW HORIZONTAL STAB DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH BP4 53003 STRUCTURE DEBONDED UPPER RT SIDE OF HORIZONTAL STABILIZER. 1G71 3U O H2SW 20030129000542003012900054SW 2003 1 29 HEEA083967 120030117A5610407030115125 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 RT WINDSHIELD CRAZED. 1G71 3U O H2SW 20030129000562003012900056NE 2003 1 29 HEEA083969 220030117A7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 1 OVERTEMP E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S4684 36002 CPPS62276 COMPRESSOR STALL ON NR 1 ENGINE. NR 1 N1 ENGINE DROPPED OFF LINE ON SHORT FINAL. MAINTENANCE DETERMINED THROUGH HUMS DATA RETRIEVED THAT THE NR 1 ENGINE ITT HAD EXCEEDANCE 1006 DEGREES FOR 15 SECONDS. REPLACED ENGINE. 1G72 4U4 U H4SW E22EA 20030129000582003012900058SW 2003 1 29 HEEA083971 120030117A6510 BEARING BELL 407 407 1182206SW T/R SHAFT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH A1934 53397 TAIL ROTOR SEGMENTED DRIVE SHAFT ASSY HAS WORN BEARING. 1G71 3U O H2SW 20030129000612003012900061SW 2003 1 29 HEEA083975 120030117A6320407040624101 LINE BELL 407 407 1182206SW MRGB OIL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 MAIN ROTOR GEARBOX OIL LINE CORRODED UNDER B-NUT SLEEVE. 1G71 3U O H2SW 20030129000632003012900063SW 2003 1 29 HEEA083977 120030117A3213407050201103 CROSSTUBE BELL 407 407 1182206SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 MLG CROSSTUBE SPREAD. 1G71 3U O H2SW 20030129000662003012900066SW 2003 1 29 HEEA083980 120030117A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 ENGINE BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030129000732003012900073NM 2003 1 29 2003UALA00070 120030118A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 LH EXTERNAL FUSELAGE SKIN HAS DENT 6" AFT OF CABIN PRESSURE STATIC PORT BETWEEN STRINGER 22L-23L, STA. 1370. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20030129000762003012900076EU 2003 1 29 03FDEA00067 120030121A7810 TAILPIPE AIRBUS310 A310 EU GE CF6 CF680 30025NE NR 2 ENGINE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25430FE 394 SIGNIFICANT TAIL PIPE FIRE DAMAGE FOUND ON POSTFLIGHT WALKAROUND, ON INBOARD AILERON, AND BOTH CANOE FAIRINGS ADJACENT TO THE AILERON ON THE NR 2 ENGINE SIDE (INWORK) WORKING IN CONJUNCTION WITH WRI 73-10/4991, CHECKED COMBUSTER DRAIN VALVE IAW M/M. NO DEFECTS NOTED. REMOVED AND REPLACED COMBUSTOR DRAIN VALVE PRECAUTIONARY IAW M/M. NO FUEL NOTED IN DRAIN LINE. IAW MOCC, NR 2 ENG MEC REQUIRES CHANGING PRIOR TO NEXT ENGINE START. 2L72 4F4 FRTA35EU E13NE 20030129000922003012900092SW 2003 1 29 HEEA083989 120030117A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20030129001202003012900120EU 2003 1 29 HEEA084000 120030113A651010531803 DRIVE SHAFT BOLKMS105 BO105S 5626006EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0350293 S677 TAIL ROTOR DRIVE SHAFT WORN EXCESSIVELY. 1G72 3U H3EU 20030129001292003012900129EU 2003 1 29 HEEA084002 120030113A7714614764021 INDICATOR AEROSPAS355 AS355* EU ROTOR RPM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 ROTOR RPM INDICATOR DECREASES 120 RPM DURING OPERATION. ROTOR NEEDLE GOES FROM 380 RPM INDICATED WITHOUT AN ACTUAL DROP IN ROTOR RPM. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030401001792003040100179WP 2003 4 1 DHL2003873001 120030128A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP CARGO BAY INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01873SJ 46091 LOWER CARGO SMOKE DETECTOR SYSTEM INOPERATIVE. MAINTENANCE MESSAGE AD1681 SHOWING. DEFERRED IAW MEL REF. 26-10-1-A1. CONTROL 11771 ASSIGNED. PLACARD INSTALLED. 2L74 4F RT4A25 20030129001422003012900142WP 2003 1 29 DHL2003801002 120030128A2611302314 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01801DH 46033 1) #3 SMOKE DETECTOR MAIN CABIN WOULD NOT TEST. RELAMPED NO HELP.2) REMOVED AND REPLACED #3 SMOKE DETECTOR SYSTEM. OPS CHECKED OK IAW M/M 26-15-00. 2L74 4F RT4A25 20030129001502003012900150 2003 1 29 HEEA084003 420030113A2300N0001553 ANTENNA AEROSPAS355 AS355* EU OUTERLINK COMMS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 3004 OUTERLINK HAD COMM/FAILURE MESSAGE. SCRAPPED. 1G72 3U H11EU 20030129001542003012900154 2003 1 29 HEEA084006 420030114A3452066106200 TRANSPONDER BOLKMS117 BK117A1 5626010EU COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RZ 7092 DOES NOT GENERATE SIGNAL. REPLACED BAD F401 FUSE, BAD V101 CAVITY AND BAD R477 RESISTOR. REPAIRED PROBLEM. ADJUSTED PULSE WIDTH AND FREQUENCY. FOUND DYNAMIC RANGE BAD. ALIGNED PRESELECTOR AND IF SECTION. REPAIRED PROBLEM. ALSO REPLACED FACEPLATE AND V301 PHOTOCELL AND CLEANED CODE SELECTOR WAFER SWITCHES. BENCH CHECK GOOD. 1G72 3U H13EU 20030401000912003040100091NM 2003 4 1 DHL2003747002 120030128A2612 FIRE DETECTOR BOEING727 727224 1384076NM NR 1 ILLUMINATED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01747DH 22253 FIRE PROTECTION DETECTOR CIRCUIT GROUND LIGHT NR 1 ILLUMINATED. TRANSFERRED NR 1 GROUND FAULT FIRE PROTECTION TO DMI 11778 IAW M/M 26-9-1. PLACARD INSTALLED. 2L73 4F A3WE 20030129001822003012900182NM 2003 1 29 UPS03240100 120030110A5310 BRACKET BOEING727 72722C 138400FNM BS 580 S2L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI BRACKET CRACKED AT MAIN CARGO DOOR SUPPORT BEAM BS 580 STR. 2 L/H REPAIR CARRIED OUT IAW SMRO EO 2003-003-008 UPS ENGINEERING FILE NO. 727-55-20034 2L73 4F A3WE 20030204002862003020400286NM 2003 2 4 F3LA200300018 120030121A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 1016, RBL 29. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-30-51, PAGES 203-208. 2L72 4F RTA16WE 20030204002872003020400287NM 2003 2 4 F3LA200300019 120030121A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 312 CORRODED FROM LBL 1 TO LBL 31. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-51, PARA 114, DETAIL XI. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-51 AND 51-40-02. 2L72 4F RTA16WE 20030220001312003022000131NM 2003 2 20 F3LA200300024 120030122A5340 ATTACH ANGLE BOEING737 7373M8 1384615NM FUSELAGE DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED LT MLG WHEELWELL CUTOUT AFT FAIRING ATTACH ANGLE HAD SEVERAL FASTENER HOLES WORN AND DAMAGED. REPLACED FAIRING ATTACH ANGLE PER SRM 53-43-01. 2L72 4F RTA16WE 20030130001322003013000132NE 2003 1 30 A6WA200340016 220030109A73216078T55P13 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE MALFUNCTIONED A A6WAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 GL31431AW 7256 RIGHT ENGINE INFLIGHT FLAMED OUT WITH RIGHT ENGINE OIL PRESSURE CAS MESSAGE ON ED1. REMOVED AND REPLACED NR 2 FUEL CONTROL UNIT. NO DEFECTS NOTED. REPLACED FUEL FILTER, RIG CHECKED, TANKS SUMPED, NO DEFECTS. (M) 2L72 4F4 FRTA21EA E15NE 20030131000182003013100018GL 2003 1 31 CA030103015 220030103A732323065125 GOVERNOR BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED W O OTHER EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 CA (CAN) TORQUE SPLIT OF 8 PERCENT REPORTED IN CRUISE. TEST FLIGHT REVEALED THAT BOTH GOVENORSWERE CAUSING THEIR RESPECTIVE N1 TO FLUCTUATE. BOTH GOVENORS WERE REPLACED ON BOTH ENGINES. A/C RETURNED TO SERVICE. 1G72 3U3 U H3EU E4CE 20030131000202003013100020WP 2003 1 31 CALA0300021 120030130A5313 LONGERON DOUG DC9 DC982 3022082WP STA 1418 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0972825 49485 INSPECTION FOUND A 1/2" CRACK IN LONGERON 2R AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW ECRA 5311-01132. 2L72 4F A6WE 20030131000572003013100057NE 2003 1 31 CA030106005 220030101A7230 ENGINE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE NR 2 SURGES W EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) ENGINE NR 2 SURGED ON CLIMBOUT. ENGINE SHUT DOWN AND AIRCRAFT RETURNED TO DEPARTURE STATION. BLADE DAMAGE FOUND ON SUBSEQUENT BOROSCOPE CHECK. NR 2 ENGINE REPLACED AS PER AMM. 2L72 4F4 FRTA28NM E29NE 20030131000882003013100088 2003 1 31 ABXA030055 420030130A2210258668911ABX1 CONTROL PANEL DOUG DC9 DC931 3022065WP COCKPIT DEFECTIVE A ABXAK NONE E VIBRATION/BUFFET CRCRUISE 1 GL23908AX72 47008 AIRCRAFT SHOOK VIOLENTLY WHEN AUTO PILOT TURNED ON. TURNED OFF AND TRIED AGAIN. SAME RESULTS. TURNED OFF AUTO PILOT, NOTICED NO YOKE MOVEMENT. REMOVED AND REPLACED AUTO PILOT CONTROLLER. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 22-10-00-5. 2L72 4F A6WE 20030131001272003013100127SO 2003 1 31 C2XA03BT017 120030129A3350 CHARGER EMB 145 EMB145LR 3260212SO CABIN AREA OPEN A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2712924 145311 CLE---COCO2351, CREW REPORTED, EMERGENCY EXIT DOOR SIGN LIGHT INOPERATIVE. MAINTENANCE REALIGNED PIN ON CHARGER BASE. OPS.CHECKED GOOD IAW EMB145 AMM #33-50-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030131001352003013100135SO 2003 1 31 C2XA03BT019 120030129A3350 LIGHT EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2713979 145181 CLE---CO2245, CREW REPORTED, EMERGENCY LIGHTS ROWS 8AND9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP IAW EMB145 AMM #33-50-10. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20030131001392003013100139NM 2003 1 31 CA030107019 120030106A3246BACB30MT826 BOLT BOEING757 757236 1384971NM RROYCERB211 RB211535E43754555NE WHEEL BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING WALK AROUND IN YMX, MTCE FOUND NR 8 MAIN WHEEL ASSY WITH ONE BOLT BROKEN (NUT WITH PORTION OF BOLT MISSING). THE MLG WHEEL ASSY WAS REPLACED I.A.W. AMM 32-45-01 (REF., DEF. 58871). 2L72 4F4 FRTA2NM E12EU 20030131001412003013100141SO 2003 1 31 C2XA03BT021 120030130A3350110049 BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN AREA FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2714542 145547 BTV---CO2002, DURING ROUTINE INSPECTION, MAINTENANCE FOUND AFT OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTERY PACK CHARGER IAW EMB145 AMM #33-50-00. OPS. CHECKED GOOD. 2L72 4T RTT00011AT 20030131001502003013100150WP 2003 1 31 MWEA030047 120030131A5320591142831 DOUBLER DOUG DC9 DC981 3022081WP BYPASS DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 RIGHT THRUST REVERSER BYPASS DOOR CUT OUT HAS AN INTERNAL DOUBLER THAT IS CRACKED IN THREE LOCATIONS. -- LOCATED, DRILLED AND INSTALLED NEW DOUBLER. 2L72 4F A6WE 20030116001512003011600151 2003 1 16 HEEA083094 420030108A3444071111400 ANTENNA BELL 206 206L3 1182108SW RADAR ALTIMETER DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 RADAR ALTIMETER ERRATIC INDICATION. DAMAGED ANTENNA. 1G71 3U H2SW 20030116001552003011600155 2003 1 16 HEEA083096 420030108A34251113025 INDICATOR BELL 206 206L3 1182108SW HSI INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 HSI INDICATOR COURSE NEEDLE WILL NOT MOVE. 1G71 3U H2SW 20030116001722003011600172SO 2003 1 16 C2XA02SH167 120030103A532014521721005 BUTT STRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV- DURING C-CHECK FOWARD DIGITAL BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 14 AND 19. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED FOWARD DIGITAL BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116001742003011600174SO 2003 1 16 C2XA02SH169 120030103A531514521713003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED DAMAGE AREA AND REPAIRED AFFECTED OMEGA BEAM IAW EMB SRM 145 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116001772003011600177SO 2003 1 16 C2XA02SH175 120030108A521014533395001 SKIN EMB 145 EMB145LR 3260212SO PAX DOOR SCRATCHED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV - DURING C-CHECK THE PASSENGER DOOR WAS FOUND TO HAVE SEVERAL SCRATCHES ON SKIN. MAINTENANCE REMOVED DAMAGED AREAS AND REPAIRED AFFECTED SECTIONS IAW CONTINENTAL EXPRESS EC 5210-01070. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116001782003011600178SO 2003 1 16 C2XA02SH176 120030108A531114524061001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV - DURING C-CHECK HOLES ON FRAME 15 WHERE COCKPIT TO CABIN LEFT FORWARD PORTION ATTACHES WERE FOUND ELONGATED. MAINTENANCE REPAIRED ELONGATED HOLES IAW CONTINENTAL EXPRESS EC 5340-01050. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116001912003011600191 2003 1 16 HEEA083102 420030108A345713824120234 RECEIVER BELL 206 206L3 1182108SW GPS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251V 51404 GPS FAILING TO HOLD MEMORY. WILL NOT MESSAGE "RECEIVER FAIL AND BATTERY BACKUP FAIL". FOUND UNIT WOULD NOT PASS GPS TEST. 1G71 3U H2SW 20030116001962003011600196 2003 1 16 HEEA083108 420030108A34571624820 ANTENNA BELL 206 206B3 1181506SW GPS SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 FAILS TO RECEIVE GPS SIGNALS. REPLACED ANTENNA. 1G71 3U H2SW 20030116002002003011600200SW 2003 1 16 HEEA083115 120030108A523020184401 LATCH BELL 206 206L3 1182108SW LITTER DOOR LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 LITTER DOOR LIGHT STAYS ON CAUTION PANEL. FOUND STUD THAT CONNECTS LOWER ROD TO LEVER CAME LOOSE. TO BE SENT TO VENDOR. 1G71 3U H2SW 20030116002032003011600203SW 2003 1 16 HEEA083118 120030108A6700 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N 51512 ROTORCRAFT FLIGHT CONTROL BELLCRANK HAS WORN BEARINGS. SCRAPPED. 1G71 3U H2SW 20030116002072003011600207SW 2003 1 16 HEEA083122 120030108A6700206001552001 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038590X 51494 WITH SLIGHT FORWARD DISPLACEMENT OF THE CYCLIC ON THE GROUND AT FLIGHT RPM AIRCRAFT WOULD DEVELOP A DIVERGENT LONGITUDINAL BOUNCE. FOUND ONE SIDE OF BEARING FAILED ON COLLECTIVE BELLCRANK LOCATED AT TRANSMISSION SUPPORT. THERE WAS NO INDICATION OF WEAR OR LOOSE BEARING ON DAILY PRIOR TO FAILURE. SCRAPPED. 1G71 3U H2SW 20030116002082003011600208SW 2003 1 16 HEEA083123 120030108A6700 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 ROTORCRAFT FLIGHT CONTROLS BELLCRANK HAS A WORN CENTER BEARING. REPAIRED. 1G71 3U H2SW 20030116002162003011600216EU 2003 1 16 QXEA0300080 120030114A491038075412 APU FOKKERF28 F28MK4000 4990810EU ZONE 200 FAILED A QXEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09497US* 1265 11173 PDX- CLIMBING THROUGH 10,000 FEET, FLIGHT ATTENDANT REPORTED THAT SMOKE ALARM IN LAVATORY WAS SOUNDING AND THAT SMOKE WAS VISABLE. TURNED OFF APU IN FLIGHT AND SMOKE WAS DISSIPATING. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20030116002222003011600222SW 2003 1 16 HEEA083128 120030108A6220206011105001 BEARING BELL 206 206B3 1181506SW TRUNNION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 YELLOW MAIN ROTOR TRUNNION BEARING WORN. SCRAPPED. 1G71 3U H2SW 20030116002332003011600233SW 2003 1 16 HEEA083133 120030108A6220206011117003 RESTRAINT BELL 206 206B3 1181506SW MAIN ROTOR FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032275Y 3626 MAIN ROTOR FLAP RESTRAINT STICKING IN DOWN POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116002432003011600243WP 2003 1 16 ZW0A0300301 120030106A3260 WARNING SYSTEM DOUG DC9 DC982 3022082WP COCKPIT ACTIVATED A ZW0AL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CE13928TW 48012 WHEN THE LANDING GEAR WAS EXTENDED FOR APPROACH THE NOSE GEAR RED LIGHT STAYED ILLUMINATED. CREW DID A TOWER FLY BY THEN RECYCLED THE LANDING GEAR. THE INDICATION WAS THEN NORMAL. MAINTENANCE CYCLED THE LANDING GEAR SEVEN TIMES, CHECKED SECURITY OF THE NOSE GEAR DEFLECTOR, AND CHECKED STRUT EXTENSION. ALL WAS NORMAL. 2L72 4F A6WE 20030116002652003011600265NM 2003 1 16 ABXA030024 120030106A5310140T2102249 SHEAR TIE BOEING767 767281 1385109NM FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE, CORRODED SHEAR TIE AT STA 742, BETWEEN STRINGERS 36 - 37 LEFT. CORRODED SHEAR TIE REMOVED, NEW SHEAR TIE INSTALLED IAW SRM. 2L72 4F RTA1NM 20030116002662003011600266NM 2003 1 16 ABXA030025 120030106A5310141T122427 SHEAR TIE BOEING767 767281 1385109NM FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE, CORRODED SHEAR TIE AT STA 412, BETWEEN STRINGERS 39 LEFT - 39 RIGHT. CORRODED SHEAR TIE REMOVED AND INSTALLED NEW SHEAR TIE IAW SRM. 2L72 4F RTA1NM 20030116002732003011600273SW 2003 1 16 HEEA083135 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MAIN ROTOR FLAP RESTRAINT STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116002762003011600276SW 2003 1 16 HEEA083137 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 MAIN ROTOR FLAP RESTRAINT STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116002822003011600282SW 2003 1 16 HEEA083142 120030108A6220206011139001 ARM BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR HEAD ARM RUBBER IS SWOLLEN. 1G71 3U H2SW 20030117000092003011700009SW 2003 1 17 HEEA083154 120030108A3213206030104023 FITTING BELL 206 206L3 1182108SW MLG CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 MLG CROSSTUBE FITTING ASSY WORN AND CORRODED. SCRAPPED. 1G71 3U H2SW 20030117000102003011700010SW 2003 1 17 HEEA083155 120030108A6320206031509101 DRAG PIN BELL 206 206B3 1181506SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MAIN ROTOR DRAG PIN BEARING WORN AND UNSTAKED. REPAIRED. 1G71 3U H2SW 20030117000162003011700016NM 2003 1 17 CALA0300014 120030116A5242 SKIN BOEING737 7373T0 1384582NM E&E DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917321 23372 INSPECTION FOUND A 1/2" CRACK IN E&E DOOR OUTER SKIN AT R/H SIDE. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030117000192003011700019SW 2003 1 17 HEEA083159 120030108A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 TRANSMISSION RESTRAINT WORN. REPAIRED. 1G71 3U H2SW 20030117000342003011700034SW 2003 1 17 HEEA083167 120030108A6320206033518007 STOP BELL 206 206L3 1182108SW M/R GEARBOX TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 MAIN ROTOR GEARBOX STOP HAS TORN RUBBER. TO BE SENT TO VENDOR. 1G71 3U H2SW 20030117000482003011700048SW 2003 1 17 HEEA083169 120030108A6330 BUSHING BELL 206 206L3 1182108SW MOUNT ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 BUSHINGS WORN. REPAIRED. 1G71 3U H2SW 20030117000502003011700050SW 2003 1 17 HEEA083170 120030108A6330 BUSHING BELL 206 206L3 1182108SW MOUNT ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 MAIN ROTOR TRANSMISSION MOUNT BUSHINGS WORN. REPAIRED. 1G71 3U H2SW 20030117000522003011700052SW 2003 1 17 HEEA083171 120030108A6330 BUSHING BELL 206 206L3 1182108SW MOUNT ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 BUSHINGS WORN. REPAIRED. 1G71 3U H2SW 20030117000692003011700069SW 2003 1 17 HEEA083181 120030108A6510 BEARING BELL 206 206L3 1182108SW T/R DRIVESHAFT WORN E O OTHER O OTHER NRNOT REPORTED 1 SW0331801 A1301032 51074 TAIL ROTOR DRIVE SHAFT HAS A WORN BEARING. REPAIRED. 1G71 3U H2SW 20030117000752003011700075SW 2003 1 17 HEEA083184 120030108A3212206050247103 COVER BELL 206 206B3 1181506SW EMERGENCY FLOAT DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 EMERGENCY FLOAT COVERS DETERIORATED. 1G71 3U H2SW 20030320000752003032000075EU 2003 3 20 2003UALA00015 120030104A2910SC47003 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE YAW DAMPER SERVOLEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29450UA 857 LOSS OF GREEN HYDRAULIC SYSTEM INFLIGHT. GREEN HYD RSVR LOW LEVEL ECAM. REPLACED GREEN SYSTEM RETURN FILTER ELEMENT AND YAW DAMPER SERVO ACTUATOR. RESERVICED HYDRAULIC SYSTEM. THE EVENT REOCCURED ON THE NEXT FLIGHT. AN INTERNAL HYD LEAK CHECK AND A VERIFICATION TEST FLIGHT WAS PERFORMED TO ISOLATE LEAK. NO LEAKS WERE FOUND NOR WAS THE PROBLEM DUPLICATED. RUDDER SERVO CONTROL (GREEN SYSTEM) AND THE T.H.S. HYDRAULIC MOTOR ACTUATOR WERE REPLACED PRECAUTIONARY. 2L72 4F4 FRTA28NM E40NE 20030117000932003011700093NM 2003 1 17 2003UALA00019 120030106A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 BODY STATION 867, STRINGER 9R, FUSELAGE FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030117000992003011700099SW 2003 1 17 HEEA083189 120030108A3212206050248115 FLOAT BELL 206 206L3 1182108SW EMERGENCY FLOAT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036251Y 51556 FLOAT BAG ASSY FAILED 6 MONTH INSPECTION. 1G71 3U H2SW 20030117001022003011700102SW 2003 1 17 HEEA083192 120030108A3213206050288101 CROSSTUBE BELL 206 206B3 1181506SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322751 3627 FOUND CROSSTUBE CORRODED BEYOND LIMITS NEAR AND UNDER SADDLES. SCRAPPED. 1G71 3U H2SW 20030117001072003011700107SW 2003 1 17 HEEA083194 120030108A3246206050298101 SKID BELL 206 206B3 1181506SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032753F 2729 EXCESSIVE CORROSION ON ENTIRE LENGTH OF SKID TUBE. SCRAPPED. 1G71 3U H2SW 20030117001232003011700123SW 2003 1 17 HEEA083201 120030108A2821206061634003 VALVE BELL 206 206L3 1182108SW FUEL FILTER STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 FUEL FILTER VALVE STICKING. REPAIRED. 1G71 3U H2SW 20030117001242003011700124SW 2003 1 17 HEEA083202 120030108A2810206061675001 FUEL CELL BELL 206 206B3 1181506SW FUSELAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032753F 2729 BLISTERS FILLED WITH FLUID IN AND OUTSIDE OF CELL. 1G71 3U H2SW 20030117001262003011700126SW 2003 1 17 HEEA083203 120030108A7120206062102013 LEG ASSY BELL 206 206B3 1181506SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MOUNT LEGS WORN. SCRAPPED. 1G71 3U H2SW 20030117001352003011700135SW 2003 1 17 HEEA083208 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 ACTUATOR DOES NOT EXTEND OR RETRACT. 1G71 3U H2SW 20030117001652003011700165NM 2003 1 17 252TR0002 120030103A33501000679 LIGHT BOEING737 737228 13844AGNM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 Emergency exit light over L1 door does not work. Replaced emergency exit light over L1 door. 2L72 4F RTA16WE 20030117001702003011700170NM 2003 1 17 AWXA200300049 120030103A5320BAC1509100146 FLOOR SUPPORT BOEING737 7373G7 138447JNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 LCQ - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND UNDER NUTPLATE ON AFT CARGO COMPARTMENT FLOOR SUPPORT "L" ANGLE BS 771, LBL 2. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; CUTOUT DAMAGED PORTION OF FLOOR SUPPORT; FABRICATED REPAIR ANGLES PER B737-300 SRM 53-00-53, PG. 201-203; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG. 201-203, FIG. 201 2L72 4F RTA16WE 20030117001712003011700171NM 2003 1 17 AWXA200300050 120030105A5315BAC1520792 SEAT TRACK BOEING737 7373G7 1384595NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW0 0 24712 LCQ - MAJOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON R/H OUTBOARD CABIN SEAT TRACK AT BS 649 TO BS 706. MAINTENANCE REMOVED CORRODED SEAT TRACK AT RBL 44 FROM BS 536 TO BS 727; FABRICATED A NEW REPLACEMENT SEAT TRACK; AND INSTALLED REPAIR PART IAW B737-300 SRM 53-00-52, PG. 221-223, FIG. 207 2L72 4F RTA16WE 20030117001722003011700172NM 2003 1 17 AWXA200300051 120030109A5712654544556 RIB BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW0 0 24712 LCQ - MAJOR REPAIR - DURING C-13 CHECK 1 1/2" CRACK WAS FOUND ON R/H WING #3 FUEL TANK INTERNAL AFT RIB LOWER LEG, WBL 135.5. MAINTENANCE CUTOUT CRACKED SECTION OF RIB AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR "T" ANGLE; AND INSTALLED REPAIR PART IAW AWA E.R. 03-5712-03014. 2L72 4F RTA16WE 20030118000022003011800002SO 2003 1 18 C2XA02SH180 120030118A53121454749003 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2736915 145421 SHV-DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT FAR RIGHT FASTENER HOLE OF 2ND HORIZONTAL REINFORCEMENT FROM TOP. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030131001622003013100162NE 2003 1 31 CA030109001 220030105A7321 SHAFT BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE FUEL CONTROL SHEARED W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) DURING TAXI OUT IN YYZ ON NR 1 ENGINE, THROTTLES WERE ADVANCED FOR TAXI AND ENGINE WENT TO 80 PERCENT N2 WITH RISE IN EGT & F/F. THROTTLE MOVED BACK TO IDLE & ALL PARAMATERS NORMAL. ADVANCED THROTTLE AGAIN AND SAME PROBLEM HAPPENED WITH RISE IN ALL PARAMETERS. MAINTENANCE REMOVED FCU AND FOUND SHAFT SHEARED. FCU REPLACED AND ENGINE RUN CHECKED SERVICEABLE.TIME 55069.02 CYCLES 52105. 2L72 4F4 F A16WE E2EA 20030131001702003013100170NM 2003 1 31 UPS03240106 120030108A5755 ANGLE BOEING727 72722C 138400FNM #3 SPOILER. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C+SI NO.3 SPOILER SUPPORT FITTING I/B FITTING ATTACH ANGLE FOUND TO BE DA MAGED.CRACK FOUND IN LWR. MOUNT BOLT HOLE PROPRAGATING TO EDGE.EXIST ING REPAIR ALSO CRACKED FROM LWR BOLT HOLE TO FREE EDGE. CRACKED ANGLE REMOVED IAW SRM 51-30-2. INSTALLED NEW ANGLE IAW SRM 51-30-2 + DRG.65-16201. 2L73 4F A3WE 20030131001722003013100172NM 2003 1 31 UPS03240110 120030112A5310 STIFFENER BOEING727 72722C 138400FNM BS 233 RL 16 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI CORROSION AT FLOOR LEVEL I/B STIFFENER BS 233 APPROX RBL 16 APPROX U NDERNEATH 1ST OFFICERS SEAT SUPPORTS CORROSION REMOVED AND FOUND OUTSIDE LIMITS OF SRM 51-10-6 & 51-10-1 STIFFENER CHANNEL REPLACED IAW SRM 51-30-2 2L73 4F A3WE 20030131001762003013100176NM 2003 1 31 UPS03240120 120030113A5310 FLANGE BOEING727 72722C 138400FNM BS 930 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI R/H W/W BS 930 HORIZ. INTERCOSTAL COMMON TO BS 930 FRAME EVIDENCE OF CORROSION ON HORIZ. AND VERTICAL FLANGE REPAIR CARRIED OUT IAW SMRO EO 2003-003-013 UPS ENGINEERING FILE NO. 727-53-20093 2L73 4F A3WE 20030131001812003013100181WP 2003 1 31 MWEA030048 120030128A532059100911 DOUBLER DOUG DC9 DC982 3022082WP RH RADOME DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RIGHT RANDOME HINGE CUT-OUT IS DAMAGED. -- CUT-OUT DAMAGE FABRICATED FILLER AND DOUBLER. 2L72 4F A6WE 20030131001842003013100184EA 2003 1 31 SWIA200311742 120030125A2721 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07923SW 7664 RUDDER TRIM INOP, RUDDER TRIM STUCK IN THE FULL RIGHT POSITION. REMOVED AND REPLACED TRIM PANEL IAW CRJ MM 27-12-10. OPS CHECK GOOD.PN ON 601R51226-23/01. 2L72 4F RTA21EA 20030131001872003013100187EA 2003 1 31 COMA0360061 120030129A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO01936CA20773 7043 FLIGHT 5242 EMERGENCY LIGHTS INOP - SWITCH LEFT ON.REPLACED EMERGENCY BATTERIES. 2L72 4F RTA21EA 20030203000052003020300005EU 2003 2 3 CA030110005 120030107A7120 MOUNT BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU RT ENGINE LOOSE W K NONE O OTHER ININSP/MAINT 1 CA 14673 (CAN) WHILE CARRYING OUT AN ENGINE INSPECTION, THE RT LOWER ENGINE MOUNTING FOOT WAS FOUND TO BE PULLING AWAY FROM THE COMPRESSOR CASE. 3 OUT OF 8 STUDS THAT SECURE THE MOUNT FOOT TO THE FLANGE HAD MISSING NUTS. THERE WAS A 0.75 GAP BETWEEN THE FORWARD PART OF THE MOUNT FOOT AND THE COMPRESSOR CASING, THE MAINTENANCE MANUAL ALLOWING A MAXIMUM GAP OF 0.2. THE MAINTENANCE MANUAL DETAIL INSPECTION CRITERIA FOR THIS LOCATION. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 3T4 T A24EU A196 20030203000242003020300024EA 2003 2 3 CA030113009 220030112A7310LW120980100 LINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA FUEL NOZZLE BROKEN W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB, PILOTS NOTICED PARTIAL POWER LOSS ON THE LT ENGINE. THE AIRCRAFT RETURNED TO BASE AND LANDED SAFELY. MAINTENANCE INVESTIGATED PROBLEM AND FOUND THE LT ENGINE NR 4 CYLINDER FUEL NOZZLE LINE BROKEN AT FLANGE. THE LINE WAS REPLACED AND AD 2002-26-01 CARRIED OUT.A GROUND RUN WAS CARRIED OUT AND THE AIRCRAFT WAS RETURNED FOR SERVICE. 1L72 3O3 O A20SO E14EA 20030203000342003020300034CE 2003 2 3 CA030115003 120030113A3260404EN16 SQUAT SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE MLG MALFUNCTIONED W O OTHER N FALSE WARNING APAPPROACH 1 CA (CAN) DURING APPROACH, FLT CREW SELECTED GEAR DOWN, HEARD GEAR ACTUATE BUT INDICATION DID NOT IDENTIFY THREE GREEN. CREW WAS CONFIDENT THAT GEAR WAS DOWN BUT SELECTED AND PERFORMED MANUAL GEAR EXTENSION AS PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. LT MAIN SQUAT SWITCH WAS REPLACED, GEAR SYSTEM CHECKED AND THE AIRCRAFT RELEASED. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030203000662003020300066NM 2003 2 3 PCAA0301029 120030130A3230574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM ONLY INTERMITTENT A PCAAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 EA13845EX3105313173 344 LGA-FLIGHT#3695. CREW REPORTED GEAR WOULD NOT RETRACT. GEAR RECYCLED, THEN GEAR RETRACTED. MAINTENANCE REPLACED GEAR SELECTOR VALVE IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. AFTER PERFORMING SEVERAL GEAR RETRACTIONS AND EXTENSIONS OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030203000702003020300070NM 2003 2 3 EVA92012402 120030123A5343 FITTING DOUG MD11 MD11F 3023600NM MLG CORRODED W QOCFK NONE L NO TEST ININSP/MAINT 1 WP0316107 48546 CORROSION WAS FOUND ON THE LANDING GEAR TRUNNION SUPPORT FITTING THE SHEAR PIN HOLES OF BOTH FITTING ARE REAMED TO 1.636 INCH & LOCAL BLENDING WAS PERFORMED TO CLEAN THE CORROSION. IN BOTH FITTING, 501/-502, THE 3 BOLTS HOLES ARE REAMED TO SIZES LARGER THAN 1.385 INCH. 2L73 4F RTA22WE 20030203001512003020300151CE 2003 2 3 AWK2003F00001 120030103A2820583801091 SELECTOR VALVE BEECH 58 58 1152740CE CONT O550 IO550* SO FUEL SYSTEM LEAKING B AWKRK NONE K FLUID LOSS ININSP/MAINT 1 WP25658DG18 TH2032 ON WALK AROUND INSPECTION, FOUND FUEL STAINING ON LT INBOARD LANDING GEAR DOOR RUNNING DOWN TO WING ROOT. FURTHER INSPECTION REVEALED LT WING FUEL SELECTOR LEAKING FUEL. REPLACED WITH NEW. 1L72 3O3 O 3A16 E3SO 20030203001662003020300166CE 2003 2 3 E712003F00000 120030109A56201014400424 WINDOW BEECH 200 200BEECH 1152920CE FUSELAGE SEPARATED E E71AO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 EA17200SV BB1187 RIGHT REAR BAGGAGE COMPARTMENT WINDOW SEPARATED FROM AIRCRAFT IN FLIGHT AT 17,500FT. AN EXAMINATION OF THE AIRCRAFT OR THE WINDOW REMAINS HAS NOT BEEN CONDUCTED YET. THE AIRCRAFT IS TO BE RECOVERED SOON. MFG HAS BEEN CONTACTED ABOUT THE INCIDENT AND AN ENGINEERING REPORT HAS BEEN REQUESTED TO FERRY THE AIRCRAFT TO 40N. 1L72 4T A24CE 20030203001762003020300176CE 2003 2 3 FFS2003F00012 120030121A55201016100196 RIVET BEECH 1900 1900C 1154161CE PWA PT6 PT6* 52043EA TORQUE TUBE LOOSE A FFSAK NONE O OTHER ININSP/MAINT 1 AL01575Z 17319 UC136 SLIGHT MOVEMENT DETECTED BETWEEN TORQUE ADAPTER AND TORQUE TUBE WHEN ELEVATORS WERE LOADED IN OPPOSITE DIRECTIONS. 2L72 4T3 TRTA24CE E2NE 20030203001992003020300199CE 2003 2 3 GUU2003F00004 120030114A32331143800419 ACTUATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT MLG BYPASSING A GUUAO OTHER J WARNING INDICATION APAPPROACH 1 SO17695473295 UE189 DURING APPROACH WHEN LANDING GEAR IS SELECTED DOWN THE AIRCRAFT JOLTS AS THE LEFT GEAR LIGHTS ILLUMINATE. REMOVED AND REPLACED LEFT MLG ACTUATOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20030203002312003020300231EA 2003 2 3 COMA0360062 120030130A335064641 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR UNRELIABLE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01962CA 7123 FLIGHT 5785 ROW 1 EMERGENCY FLOOR LIGHTING IS INOP.REPLACED THE FLOOR LIGHT POWER STRIP. 2L72 4F RTA21EA 20030203002352003020300235EA 2003 2 3 COMA0360068 120030130A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA A COMAK NONE O OTHER ININSP/MAINT 1 SO01989CA 7215 L.H. F.S. 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 IS CRACKED.REPAIRED L H F.S. 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 I/A/W WVAC E.O. 601R-53-3826. 2L72 4F RTA21EA 20030203002362003020300236NM 2003 2 3 PCAA0302032 120030201A2910AN81510D FITTING DHAV DHC8 DHC8102 2809003NM #2 ENGINE DRIVENCRACKED A PCAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 EA13825EX 388 BGM-PHL FLIGHT#3577. AIRCRAFT RETURNED TO FIELD DUE TO #2 HYDRAULIC QUANTITY GOING TO ZERO ON CLIMB OUT. EMERGENCY WAS DECLARED. MAINTENANCE REPLACED O RINGS ON PRESSURE WARNING SWITCH, PRESSURE TRANSMITTER, AND LOW PRESSURE WARNING SWITCH. AN O RING WAS ALSO REPLACED ON FITTING FOR INLET PRESSURE ON RIGHT PRESSURE MANIFOLD. RIGHT ENGINE DRIVEN HYDRAULIC PUMP ALSO REPLACED. STANDBY HYDRAULIC PUMP RAN IN HANGAR FOR 15 MINUTES. NO LEAKS WERE NOTED. AIRCRAFT GROUND RAN AND HYDRAULIC SYSTEM CYCLED. NO LEAKS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. FLIGHT#9383. CREW REPORTED HYDRAULIC QUANTITY ON #2 SIDE WAS LOST IN FLIGHT WHEN GEAR WAS SELECTED DOWN. MAINTENANCE FOUND A CRACKED A.N. FITTING ON #2 ENGINE DRIVEN PUM2H72 4T RTA13NM 20030203002382003020300238NM 2003 2 3 QXEA0300213 120030131A3230401020101 SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX 4046 PDX-ON FLIGHT NUMBER 2311, RETURNED TO FIELD. GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED NOSE WHEEL CENTER PROXIMITY SENSOR AND RIGGED. LANDING EXTENSION AND RETRACTION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030204000022003020400002CE 2003 2 4 IZ22003F00003 120030106A1430NAS5779A12A NUT MTSBSIMU2 MU2B36A 5780413CE GARRTTTPE331TPE331* 01514WP RTWING CRACKED B IZ2RK NONE O OTHER ININSP/MAINT 1 SW15338CM7494 703SA DURING INSPECTION, FOUND UPPER WING INBOARD/OUTBOARD ATTACH BOLT WOULD NOT PROPERLY TIGHTEN TO TORQUE VALUE. INVESTIGATION REVEALED RIGHT UPPER FORWARD BARREL NUT WAS CRACKED. FURTHER INVESTIGATION REVEALED RIGHT LOWER FORWARD BARREL NUT WAS ALSO CRACKED. 1H72 3T3 T A10SW E2WE 20030204000082003020400008SO 2003 2 4 KRT2003F00000 120030107A1430NAS464P427 BOLT PIPER PIPER PA44 PA44180 7104402SO LYC O360 O360* 41514EA DRAG LINK SHEARED B KRTRO OTHER O OTHER LDLANDING 1 SO092088K5942 447995175 UPON TOUCH DOWN OD THE NOSE GEAR DURING LANDING THE NOSE GEAR COLLAPSED RESULTING IN DAMAGE TO THE NOSE OF THE AIRCRAFT, BOTH ENGINES AND BOTH PROPELLERS. AFTER EXAMINATION OF THE NOSE GEAR IT WAS NOTED THAT THE CENTER DRAG LINK BOLT WAS SHEARED IN THE CENTER AND THE DOWN LOCK HOOK WAS BROKEN IN HALF. NOSE LANDING GEAR DOWN LOCK BUSHING REPLACEMENT 2/11/81, TT 2698.86. 1L72 3O3 O A19S0 E286 20030204000212003020400021SO 2003 2 4 R2J2003F00001 220030108A7414K3056 DISTRIBUTOR GEARSLICK PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO MAGNETO ARCED B R2JRK NONE O OTHER ININSP/MAINT 1 EA21113DK569 00030950 347870151 WHILE COMPLETEING RECOMMENDED 500 HOURS INTERNAL MAGNETO INSPECTION ON MAGNETO. 569 HOURS SINCE NEW; INSPECTOR FOUND DISTRIBUTOR GEAR ELECTRODE DAMAGED DUE TO ARCING AND OVERHEATING. MAGNETO WAS OPERATING NORMALLY, WAS SOON TO MISFIRE IF ELECTRODE BROKE FROM ITS MOUNT, WHICH WOULD CAUSE MAGNETO TO JUMP TIME. THIS COULD CAUSE LOSS OF ENGINE POWER. NEW GEAR INSTALLED-INSPECTION COMPLETE SUGGEST 500 HOUR INSPECTION BE MADE MANDATORY. 1L72 3O3 O A7SO E9CE 20030204000242003020400024NM 2003 2 4 VNAA0301028 120030126A24001060003 BPCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07432JS16750 3045 DURING TAKE OFF, THE CREW PUSHED THE THROTTLES FORWARD AND RECEIVED A RIGHT HAND DC GENERATOR FAILED MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204000332003020400033NM 2003 2 4 SWAA030223 120030130A3350101073 LENS BOEING737 7375H4 138449DNM FWD ENTRY DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030204000392003020400039NM 2003 2 4 SWAA030233 120030130A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410 AFT OF LRRA ANTENNA. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000522003020400052NM 2003 2 4 SWAA030201 120030127A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND AFT SVC DOOR LOWER HINGE CUTOUT SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000542003020400054NM 2003 2 4 SWAA030204 120030128A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030204000562003020400056NM 2003 2 4 SWAA030206 120030127A53306545890 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000592003020400059NM 2003 2 4 SWAA030171 120030123A3350417N5213 COVER BOEING737 7377H4 1384404NM CABIN FLOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 EEPLS TRACK COVER LOOSE. SECURED TRACK COVER PER MM. 2L72 4F RTA16WE 20030204000652003020400065NM 2003 2 4 SWAA030177 120030123A3350101114 LENS BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SPECIAL VISIT, FOUND RT FWD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030204000692003020400069NM 2003 2 4 SWAA030196 120030125A551065C25727 SKIN BOEING737 7373H4 1384600NM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT AFT SPAR RIVET ROW, CENTER BALANCE BAY. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000702003020400070NM 2003 2 4 SWAA030197 120030125A53116546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED RON, FOUND SHEAR TIE CRACKED AT BS 907, BETWEEN STR 20L AND STR 21L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030204000852003020400085 2003 2 4 SWAA030143 420030121A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29071SW 22358 AFT ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F A16WE 20030204000862003020400086 2003 2 4 SWAA030145 420030121A2565D31354 SLIDE BOEING737 7373T5 1384608NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 FWD ENTRY DOOR EVACUATION SLIDE LOOSE. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030204000982003020400098 2003 2 4 SWAA030117 420030117A25656567380 LENS BOEING737 7373H4 1384600NM CABIN CRAZED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED BC2 CHECK, FOUND THE L1 DOOR EMERGENCY ESCAPE SLIDE LENS CRAZED. REMOVED AND REPLACED THE L1 ESCAPE SLIDE LENS PER MM. 2L72 4F RTA16WE 20030204001042003020400104 2003 2 4 SWAA030098 420030116A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20030204001052003020400105NM 2003 2 4 SWAA030101 120030116A335007912 LENS BOEING737 7373H4 1384600NM CABIN FLOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 EELPS LENS BROKEN AT FWD ENTRY AREA. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030204001072003020400107NM 2003 2 4 SWAA030104 120030116A3350101114 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT SIGN LENS MISSING AT ROW 23. REMOVED AND REPLACED EMERGENCY EXIT SIGN AT ROW 23 PER M/M. 2L72 4F RTA16WE 20030204001102003020400110NM 2003 2 4 SWAA030087 120030115A53116546551 FRAME BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BIN ATTACH BRACKETS BS 807 AND BS 827 BETWEEN STR 8L AND STR 9L AND FRAME CRACK AT BIN ATTACH BRACKET BS 807 BETWEEN STR 8R AND STR 9R. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20030204001152003020400115CE 2003 2 4 UG8AG0342 120030103A5753 FLAP TRACK CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LT AND RT CONTAMINATED E UG8AA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL235112 7500010 AFTER SELECTING FLAPS UP, AMBER FLAPS FALL LIGHT CAME ON. UNABLE TO RESET. RETURN TO DTW. SLATS OK. ZERO FLAPS. ICE, WATER AND SAND FOUND IN THE LT AND RT INBOARD FLAP WELLS AND FLAP TRACKS. CAUSED FLAP MOTOR OVERCURRENT DURING FLAP ACTUATION. 2L72 4J4 FRTT00007WITE6CH 20030204001172003020400117CE 2003 2 4 UQRR0301 120030107A3260 WIRE CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP MLG UPLOCK FAILED B UQRRA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 WP01398CW7555 6500098 A BROKEN GROUND WIRE AT PIN "F" OF THE LT MLG UPLOCK SWITCH CONNECTOR CAUSED THE LT MLG UPLOCK TO CLOSE AND LOCK BEFORE THE LANDING GEAR WAS FULLY RETRACTED. THIS ACTION RESULTED IN THE UPLOCK HOUSING ASSEMBLY AND UPLOCK MECHANISM TO BE SMASHED BY THE RETRACTING LANDING GEAR. THE FLIGHT CREW HEARD A LOUD BANG AND THE GEAR UNLOCKED ANNUNCIATOR REMAINED ON. THE CREW THEN PUT THE LANDING GEAR HANDLE DOWN AND CONFIRMED 3 GREEN GEAR SAFE ANNUNCIATORS AND SAFELY LANDED THE AIRCRAFT. 2L72 4F4 F A9NM E6WE 20030204001392003020400139GL 2003 2 4 W592003F00000 320030114A6111B24231 CYLINDER PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC2Y HCC2YR2 GL PROP BLADE LOOSE B W59RK NONE O OTHER ININSP/MAINT 1 WP07573ER298 4496149 AV10886B PROPELLER WAS SUBMITTED FOR REPAIR DUE TO A SEIZED SPINNER ATTACH PN A24053 WHILE ATTEMPTING TO REMOVE THE NUT. IT WAS NOTED THAT THE ENTIRE CYLINDER ASSEMBLY WAS LOOSE AND UNSCREWING FROM THE HUB. THIS PART SHOULD HAVE BEEN TORQUED TO 180 FT LBS. THIS IS A NEW PROPELLER ASSY AND WE HAVE RECENTLY SEEN NUMEROUS PROBLEMS WITH THE LOW STOP ASSY AND SPINNER MOUNTING NUTS ON SEVERAL NEW, LOW TIME PA-44S. 1L72 3O3 O A19S0 E286 5 CP920 20030204001412003020400141NE 2003 2 4 WVE2003F00000 220030110A7261WF336354 OIL FILTER CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE CAP ASSY MISMANUFACTURED B K NONE W INADEQUATE Q C ININSP/MAINT 1 EA09309FX 5306 DURING A MAINTENANCE CHECK, WHILE ATTEMPTING TO REPLACE THE OIL FILTER THE PACKING ON THE OIL FILTER CAP ASSEMBLY (OIL FILTER SHAFT) WAS CUT. DURING INVESTIGATION THE OIL FILTER END CAP INNER LIP WAS FOUND ROUGH AND HAD SHARP EDGES. 2L72 4F4 FRTA21EA E15NE 20030204001422003020400142CE 2003 2 4 WVE2003F00001 120030110A2110135155033 BRACKET LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP A/C COMPRESSOR CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09427FX1067 163 DURING 1200 HOUR MAINTENANCE CHECK THE AIR CONDITIONER COMPRESSOR MOUNT BRACKET WAS FOUND CRACKED. 2L72 4F4 FRTT00008WIE6WE 20030208000022003020800002SO 2003 2 8 RAIA00301019 120030119A36208166101 VALVE EMB 145 EMB145LR 3260212SO MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03818HK1019 145059 5721-STL - RIGHT ENGINE BLEED OVERTIME INDICATION. MAINTENANCE REMOVED AND REPLACED THE #2 FAN AIR VALVE, OPS CK OK. 2L72 4T RTT00011AT 20030208000042003020800004EU 2003 2 8 RAIA00301021 120030121A24351030032 SENSOR AEROSPATR42 ATR42300 8680920EU MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03426TE 228 5679-STL- RIGHT HAND GENERATOR WILL NOT COME DON LINE. MAINTENANCE REMOVED AND REPLACED RIGHT HALL EFFECTS SENSOR, OPS CK OK. 2H72 4T RTA53EU 20030208000092003020800009EU 2003 2 8 RAIA00301030 120030131A7710331EDP12 PANEL JETAIRJETSTMJETSTM4101 1500501EU READS HIGH A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03561HK13071102 41077 5558-STL - RIGHT ENGINE IDLE TORQUE 23%. MAINTENANCE REMOVED AND REPLACED THE ENGINE INSTRUMENT PANEL, OPS CK OK. 2L72 4T RTA41NM 20030210000322003021000032EA 2003 2 10 QXEA0300018 120030104A2612 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA FIRE DETECTION MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09606QX 10023 TUS-ON FLIGHT NUMBER 2535, INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE, USUALLY ASSOCIATED WITH LIGHT TURBULENCE AT FL370 AND FL390. INTERROGATED MDC, NO FAULT FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030210000472003021000047NM 2003 2 10 QXEA0300031 120030106A5210 BUSHING DHAV DHC8 DHC8202 2809007NM PAX DOOR BACKED OUT A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09360PH 515 BOI- MAIN CABIN DOOR WILL NOT OPEN. FOUND AFT HANDRAIL EXTENSION PIVOT BUSHING BACKED OUT. RESECURED BUSHING. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030210001082003021000108NM 2003 2 10 QXEA0300056 120030107A7110 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM RT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX-RIGHT HAND LOWER COWL CENTER CONE SUPPORT BRACKET LOWER FLANGE CRACKED. REPAIRED IAW RD8-4-71-016. 2H72 4T RTA13NM 20030210001092003021000109NM 2003 2 10 QXEA0300057 120030111A5210 HINGE BRACKET BOMBDRDHC8 DHC8401 1390041NM PAX DOOR WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX-AFT PASSENGER DOOR HINGE BRACKET AT DOOR IS WORN/LOOSE. REPAIRED IAW DHC-84 MM 52-12-16-400-501 AND 52-12-00-830-801. 2H72 4T RTA13NM 20030210001222003021000122NM 2003 2 10 QXEA0300065 120030111A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- PANEL 262AT FORWARD BOTTOM FLANGE IS CHAFED THE ENTIRE LENGTH. REPAIRED IAW DHC-8 400 SRM TASK 51-14-00-350-801, DHC-8 400 SRM 51-21-10, 51-25-10 AND HORIZON AIR EA 6-53-173. 2H72 4T RTA13NM 20030210001242003021000124NM 2003 2 10 QXEA0300067 120030109A5320 THRESHOLD BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- MAIN CABIN DOOR THRESHOLD IS CORRODED AROUND NUTPLATES. REPAIRED IAW DHC-8 400 SRM 51-00-02, 51-42-05 AND HORIZON AIR EA 6-53-176. 2H72 4T RTA13NM 20030210001262003021000126NM 2003 2 10 QXEA0300069 120030109A5752 SKIN BOMBDRDHC8 DHC8401 1390041NM AILERON DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- DENT IN TRAILING EDGE OF GROUND ADJUSTABLE TAB ON OUTBOARD END. REPAIRED IAW DHC-8 400 SRM 51-00-02, TASK 27-14-01-400-801 AND RD 8/4-57-114. 2H72 4T RTA13NM 20030210001282003021000128NM 2003 2 10 QXEA0300071 120030107A5420 WEB BOMBDRDHC8 DHC8401 1390041NM LT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- CRACK IN DIAPHRAGM ON LEFT HAND NACELLE OUTBOARD SIDE AT XN200. REPAIRED IAW DHC-8 Q400 SRM 51-40-10, 51-42-05 AND 51-42-45. 2H72 4T RTA13NM 20030210001562003021000156 2003 2 10 C2XA03BT028 420030210A3420 DISPLAY EMB 145 EMB145 3260210SO COCKPIT AREA ODOR A C2XAK NONE O OTHER CRCRUISE 1 SW2713118 145675 EWR---CO2006, CREW REPORTED "PLASTIC/RUBBER SMELL CONTINUING INFLIGHT ON FLIGHT DECK. NO SMOKE DETECTED." MAINTENANCE FOUND EICAS CAUSING SMOKE SMELL. REMOVED AND REPLACED EICAS DISPLAY UNIT IAW EMB145XR AMM 34-22-01. OPS.CHECKED GOOD. 2L72 4F RTT00011AT 20030211000082003021100008SO 2003 2 11 C2XA03CL034 120030208A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714542 145547 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE.MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY AND BATTERY CHARGER.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030211000112003021100011NM 2003 2 11 ANCF200300005 120030203A3220 NUT DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE NLG UNDERTORQUED W ANCFC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO23190AN 53190 THERE WAS A VERY STRONG VIBRATION OF THE NOSE WHEELS DURING TAKE OFF ROLL. TAKE OFF WAS ABOTED BELOW 60 KTS. WAS VERIFCATED TORQUE IN NUT STRUT IAW AMM 32-21-02 PAG 404 WAS ADJUSTED DEFLECTOR IAW AMM 32-20-02 PAG 202 AND NOSE WHEELS WERE REPLACED IAW AMM 32-40-02 PAGE 202 2L72 4F4 FRT E9NE 20030211000132003021100013NM 2003 2 11 2003UALA00135 120030202A5330 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29669UA 30025 GOUGE JUST BELOW AFT CARGO DOOR CUTOUT ON FUSELAGE. LENGTH: 9.75" BY .25" STARTS AT LOWER FWD CORNER STAINLESS STEEL CUFF PLATE. THE FIRST 2.5" EXTENDS IN DEPTH THRU SCUFF PLATE AND APPROX. .031" DEEP ONTO FUSE SKIN. THE REMAINING 7.25" OF GOUGE IS .125". MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER INSTALLED. 2L72 4F4 FRTA1NM E24NE 20030211000152003021100015NM 2003 2 11 ZW0A0301903 120030209A3350767 LAMP BOEING757 757231 1384950NM A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13726TW 30339 THE LEFT SIDE NUMBER 4 CABIN DOOR FUSELAGE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-1-02 MCI. --CLOSED-- 2L72 4F RTA2NM 20030212000182003021200018SW 2003 2 12 AUS20030002 120030101A73302764024117 LINE SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UHR WP FUEL INDICATOR BROKEN W O OTHER EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 AUS 96 (AUS) RT ENGINE FUEL BYPASS WARNING LIGHT ILLUMINATED. INVESTIGATION FOUND THAT THE FUEL LINE TO THE DIFFERENTIAL PRESSURE TRANSMITTER WAS BROKEN AT THE CONNECTOR END FITTING. 2L72 4T4 TRTA5SW E4WE 20030212000212003021200021NM 2003 2 12 AUS20030018 120030110A5753NAS577B8A NUT BOEING737 737377 NM TE FLAP TRACK CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TRAILING EDGE FLAP TRACK RETAINING BOLTS LOCATED AT THE LT OUTBOARD FLAP, INBOARD TRACK, INBOARD RETAINING BOLT THREADS WERE NOT IN SAFETY. BOLT AND BARREL NUT WERE REMOVED AND INSPECTED WITH THE NUT FOUND TO BE CRACKED. 2L72 4F RTA16WE 20030212000232003021200023WP 2003 2 12 AUS20030023 120030114A571151762561 SPAR CAP DOUG DC4 C54E 3021530WP RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT OUTER WING UPPER SPAR CAP CORRODED BETWEEN WS 399 AND WS 421. 2L74 4R A762 20030212000262003021200026WP 2003 2 12 AUS20030026 120030114A54145234753136 SKIN DOUG DC4 C54E 3021530WP NACELLE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT NACELLE UPPER INBOARD SKIN CORRODED BETWEEN SKIN AND SUPPORTING STRUCTURE. 2L74 4R A762 20030212000292003021200029NM 2003 2 12 AUS20030041 120030120A5315 FLOORBEAM BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FLOORBEAM LOCATED AT BS 1130 LBL 71 AND RBL 71 CORRODED. 2L73 4F4 FRTA3WE E2EA 20030212000322003021200032NM 2003 2 12 AUS20030045 120030120A5315 FLOORBEAM BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLOORBEAM CORRODED AT BS 1030 FL AND RBL 70. 2L73 4F4 FRTA3WE E2EA 20030212000402003021200040EU 2003 2 12 CA030106012 120030103A261231072 ECU PACIFICSCIEN FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU FIRE SUPPRESSIONMALFUNCTIONED W F ACTIVATE FIRE EXT. H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 CA (CAN) THE SUBJECT AIRCRAFT HAVE BAGGAGE COMPARTMENT SMOKE DETECTION AND FIRE SUPPRESSION SYSTEM INSTALLED, SUPLEMENTAL TYPE CERTIFICATE SA02-134. THE FIRE SUPPRESSION SYSTEM INCLUDES TWO HALON BOTTLES, DIVERTER VALVES, AND ASSOCIATED PIPING AND HALON NOZZLES. DISCHARGE OF THE HALON BOTTLES IS MANUALLY CONTROLLED BY MEANS OF PUSHBUTTON SWITCHES IN THE COCKPIT. THE OPERATOR HAS OBSERVED THAT THE 60 SECOND COUNTDOWN TIMER IS INTERMITTENTLY TRIGGERED BY SELECTING THE BATTERY MASTER FROM OFF TO ON. THIS RESULTS IN UNCOMMANDED DISCHARGE OF THE NR 2 HALON BOTTLE. 2L72 4F4 FRTA20EU E2EU 20030410002512003041000251NM 2003 4 10 F3LA200300035 120030127A5320 FLOOR SUPPORT BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT AT STA 772, RBL 8.1 CORRODED. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 55-60-53, 53-60-53, 53-00-53 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030212000502003021200050NM 2003 2 12 QXEA0300241 120030206A21308201003004 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09410QX2669 4053 SUP- FLIGHT 397 - AIRCRAFT DIVERTED WHEN THE CREW WAS UNABLE TO PRESSURIZE OVER 1.0. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ELECTRONIC CONTROL UNIT AND THE ENVIRONMENTAL CONTROL SYSTEM CONTROLLER. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030410002522003041000252NM 2003 4 10 F3LA200300036 120030127A5320 FLOOR SUPPORT BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT STA 860, RBL 8.1. REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-60-53, 53-00-53, 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030212000512003021200051EA 2003 2 12 CA030114002 120030106A4930388273010 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE APU LEAKING W O OTHER BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CRCRUISE 1 CA (CAN) PILOTS REPORTED THAT IN FLIGHT THEY HAD A STRONG FUEL ODOR FROM THE BLEEDS WITH THE APU AIR ON. UPON LANDING, APU ACCESS PANEL WAS OPENED AND STRONG FUEL ODOR AND EVIDENCE OF SPRAY WAS NOTED. MAINTENANCE COMFIRMED MAJOR FUEL LEAKAGE FROM APU COMBUSTOR CAN. APU FUEL CONTROL UNIT WAS REPLACED. 2L72 4F4 FRTA21EA E15NE 20030212000552003021200055NE 2003 2 12 CA030114008 220030110A7230 COMPRESSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE DAMAGED W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA J49 (CAN) DURING CLIMB RIGHT ENGINE ITT ROSE TOWARDS 860 DEG. THROTTLES PULLED BACK AND ITT RISE RESTORED. UNABLE TO GET CRUISE POWER BELOW 860 DEG ITT FL 310 IN CRUISE 860 DEG AT 94 PERCENT CRUISE 93.2 PERCENT AT FL 330. MAINTENANCE BOROSCOPED ENGINE AND FOUND THREE COMPRESSOR SECTIONS WITH BLADE DAMAGE ENGINE REPLACED AS PER AMM. 2L72 4F4 FRTA21EA E15NE 20030212000712003021200071EA 2003 2 12 CA030119001 120030111A2820CC670621041 LINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUEL FEED CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHEN A/C WAS BEING FUELED, CENTER TANK WAS FILLED TO 2000 LBS AND WINGS FILLED TO 5500 LBS. ALSO CREW GOT A FUEL IMB CAUTION ON CLIMB OUT ABOUT 5 MIN AFTER TAKE OFF. USED PUMPS AND GRAVITY TO REMOVE FUEL FROM CENTER TANK ASSY. INSPECTED LT CENTER TANK AND FOUND FUEL TUBE ASSY CRACKED. RAI LT CENTERLINE FUEL TUBE ASSY. LEAK AND OPS CHECKED GOOD PER CRJ AMM 28-13-25 2L72 4F4 FRTA21EA EOOO63EN 20030212000782003021200078EA 2003 2 12 CA030120002 120030111A2820601R6226135 TUBE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUEL SYSTEM CHAFED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) A SUSPECTED BOOST PUMP INDICATION DEFECT WAS BEING WORKED WHEN IT WAS NOTICED THAT CENTRE FUEL TANK QUANTITY WAS INCREASING DURING PERIODS OF PUMP ACTIVITY. ON INSPECTION THE LT BOOST PUMP PRESSURE INDICATION LINE PT 601R6226135 WAS FOUND TO HAVE BEEN COMPLETELY CHAFED THROUGH AFTER RUBBING AGAINST LT MAIN FUEL FEED LINE PT 601R62272-21. FURTHER TO THAT, IT WAS ALSO NOTICED THAT THE BOOST PUMP CROSS FEED LINE PT 601R62299-3 WAS IN CONTACT WITH AND CHAFING AGAINST THE MAIN DIVIDING SPAR BETWEEN THE LT AND RT SIDES OF THE CENTRE FUEL TANK WHERE THE PIPE PASSED THROUGH IT. 2L72 4F4 FRTA21EA E15NE 20030212000802003021200080NM 2003 2 12 UPS03240156 120030128A5310 FITTING BOEING727 72725C 138400HNM TAIL SKID BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C R/H LWR. TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED FITTING IAW SRM 51-30-02. FABRICATED NEW FITTING IAW DRAWING NO.65-85208 INSTALLED FABRICATED FITTING IAW DRAWING NO.65-25992 2L73 4F A3WE 20030212000842003021200084NM 2003 2 12 CALA0300033 120030210A5311 FRAME BOEING737 7373Q8 1384670NM STA 1121 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914384 26313 INSPECTION FOUND INNER FORMED FRAME CHORD DENTED AT STA 1121, LBL 28, WL 292. REPAIRED IAW SRM 51-70-11, FIGURE 1. 2L72 4F RTA16WE 20030212000962003021200096NM 2003 2 12 AWXA200300121 120030206A531369353521 TIE CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 2 R/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 2 R/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 38, FIG. 8, AND SRM 51-40-05, PG. 1-4, FIG. 1-2, PG. 7, FIG. 4. 2L72 4F RTA16WE 20030212000992003021200099NM 2003 2 12 AWXA200300129 120030124A53306545800 SKIN BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW0 0 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK A 3/4" CRACK WAS FOUND ON FUSELAGE SKIN AT THE FORWARD CORNER OF THE LOWER HINGE CUTOUT OF R-1 DOOR. MAINTENANCE STOP DRILLED CRACK ON FUSELAGE SKIN AT THE FORWARD CORNER OF THE LOWER HINGE CUTOUT OF R-1 DOOR AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, FIG. 208. 2L72 4F RTA16WE 20030212001002003021200100NM 2003 2 12 AWXA200300132 120030126A53126516300 WEB BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW0 0 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK 2 EACH 1/2" CRACKS WERE FOUND ON 178 BULKHEAD RADAR ANTENNA ATTACH BRACKET, R/H SIDE AT UPPER INBOARD AND OUTBOARD ATTACH POINTS. MAINTENANCE STOP DRILLED CRACKS ON 178 BULKHEAD RADAR ANTENNA ATTACH BRACKET, R/H SIDE AT UPPER INBOARD AND OUTBOARD ATTACH POINTS, AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 210, PG. 276. 2L72 4F RTA16WE 20030212001042003021200104NM 2003 2 12 PCAA0302041 120030211A335028VS200Y4DH RECTIFIER DHAV DHC8 DHC8102 2809003NM LEFT INTERMITTENT A PCAAK NONE S AFFECT SYSTEMS CRCRUISE 1 EA13806EX29739 263 SYR FLIGHT#3884. CREW REPORTED EMERGENCY LIGHTS FLICKER INTERMITTANTLY ON GROUND AND IN FLIGHT. MAINTENANCE CYCLED EMERGENCY LIGHTS ON AND OFF. AIRCRAFT GROUND RAN. PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. PHL FLIGHT#3562. CREW REPORTED EMERGENCY LIGHTS FLICKER ON APPROACH AND ON GROUND. MAINTENANCE REPLACED THE EMERGENCY LIGHTS CONTROL BOX. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. PHL FLIGHT#3634. CREW REPORTED EMERGENCY LIGHTS FLICKERED ON AND OFF ON TAKE-OFF AND ON GROUND. MAINTENANCE CYCLED EMERGENCY LIGHT CIRCUIT BREAKERS. AIRCRAFT GROUND RAN, AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. ABE FLIGHT#3508. CREW REPORTED EMERGENCY LIGHTS FLICKER RIGHT BEFORE 2H72 4T RTA13NM 20030213000112003021300011EU 2003 2 13 CA030122009 120030114A3220AN617 BOLT MESSIER AIRBUS310 A310300 3930305EU GE CF6 CF680C2* GL NLG STRIPPED W K NONE O OTHER ININSP/MAINT 1 CA L596 (CAN) DURING A CHECK ROUTING INSPECTION THE FOUR BOLTS (AN6-17) AT THE ATTACHMENT OF THE SHOCK ABSORBER OFTHE UPPER PART OF THE BARREL HAVE BEEN FOUND STRIPPED AND THE NUTS LOOSE. INSTALLATION OF THE BOLTS HAS TO BE CARRIED OUT IAW INSTRUCTIONS GIVEN IN THE MESSIER SB 470-32-708 AND MESSIER SB 470-32-709. 2L72 4F4 FRTA35EU E23EA 20030213000152003021300015CE 2003 2 13 CA030123007 120030123A5280508201834 HINGE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA MCAULY4HFR344HFR34C754 NE NLG DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 14112 (CAN) WHEN CONDUCTING GEAR RETRACTION AS PART OF PHASE INSPECTION FORWARD PORTION OF RT NOSE GEAR DOOR DID NOT FAIR IN WITH THE FUSELAGE. A MORE DETAILED INSPECTION WAS CARRIED OUT, REVEALING THE FORWARD HINGE CRACKED AT THE FIRST RIVET AS THE FITTING ENTERS THE DOOR ASSEMBLY. HINGE REPLACED. 1L72 4T4 T A24CE E4EA 6 C3PNE 20030213000172003021300017NE 2003 2 13 CA030123010 220030123A72603036777 CARBON SEAL BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE LT ENGINE CRACKED W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE, CREW NOTICED OIL PRESSURE DROPPING AND ELECTED TO SHUTDOWN THE LT ENGINE AS A PRECAUTION. THE FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE AGB WAS REMOVED TO INVESTIGATE OIL LOSS THRU THE OVERBOARD VENT AND THE STARTER GENERATOR SPLINE, CARBON SEAL WAS FOUND CRACKED ALLOWING OIL TO VENT. SIX QUARTS WERE DISPLACED CAUSING THE OIL PRESSURE DROP. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030213000202003021300020CE 2003 2 13 CA030124003 120030123A5610101384025 WINDSHIELD BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043NE COCKPIT FAILED W BA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) WHILE LEVELING AS FL 270, TEMP -44, IFR A LOUD BANG WAS HEARD AND THE CO-PILOTS WINDSHIELD SHATTERED. SOME SMALL PIECES OF GLASS WERE ON THE CO-PILOTS SHIRT AND PANTS. CRACKED WINDSHIELD CHECK LIST WAS COMPLETED AND DECENT TO 4000 FT. WAS MADE AND AND EMERGENCY DECLARED. NO OTHER DAMAGE. 2L72 4T4 TRTA24CE E4EA 20030213000232003021300023GL 2003 2 13 CA030127001 220030113A725023038160 TURBINE BELL 206 206L 1181522SW ALLSN 250C 250C20R2 GL ENGINE SEIZED W E ENGINE SHUTDOWN YDJENGINE STOPPAGE INFLIGHT SEPARATION WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) DURING FIRST START OF THE ENGINE, FOLLOWING A TURBINE CHANGE, MAIN ROTOR BLADES INITIALLY STARTED TURNING BUT THEN STOPPED BEFORE ENGINE ACCELERATED TO IDLE SPEED. THE START WAS ABORTED.AME ATTEMPTED TO TURN THE MAIN ROTOR BLADES BACKWARDS BUT WAS UNABLE TO DO SO. THE PT (N2) TURBINE WAS SEIZED. THE A/C WAS BROUGHT INTO THE HANGAR. AFTER APPROXIMATELY 45 MINUTES A LOUD BANG WAS HEARD AND THE N2 TURBINE BROKE FREE. THE TURBINE WAS REMOVED AND RETURNED TO STANDARD AERO. ENGINEERING REPORT WAS REQUESTED. 1G71 3U3 U H2SW E4CE 20030213000272003021300027NM 2003 2 13 CA030128001 120030127A3246315731 WHEEL BOMBDRDHC8 DHC8400 NM PWC 150 PW150A EA MLG DEPARTED W O OTHER DB INFLIGHT SEPARATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA (CAN) AT OR RIGHT AFTER THE TAKE OFF FROM BASE, THE AIRCRAFT LOST THE NR 3 MLG WHEEL AND TIRE ASSEMBLY. THE FLIGHT CONTINUED TO NEXT BASE. AFTER LANDING THE NR 3 BRAKE FELL OFF OF THE AXAL AND WAS DRAGGED BEHIND THE AIRCRAFT. THIS WAS RECOGNIZED BY SOME PASSENGERS DUE TO SPARKS WHICH HAVE BEEN CAUSED BY THE BRAKE TOUCHING THE RUNWAY. THE PILOTS RECOGNIZED THE PROBLEM AFTER A WALK AROUND. A NUMBER OF PARTS ON THE STRUT ASSY WERE FOUND DAMAGED BY THE HEAT. PARTS PLACED ON ORDER. 2H72 4T4 TRTA13NM E00062EN 20030213000352003021300035NE 2003 2 13 CA030130005 220030112A7200 ENGINE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE NR 1 VIBRATION W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 CA (CAN) DURING TAKE OFF, CREW REPORTED NR 1 ENG HIGH VIBRATION, VIBRATION REACHED 5 UNITS ON BOTH CHANNELS. THE ENGINE WAS SHUTDOWN AS PER QRH. ESN 14858 HAD SHOWN AN INCREASE IN N1 VIBRATION TREND IN THE 2 WEEKS PREVIOUS TO THE EVENT AND A FAN CLEAN AND RELUBRICATION WAS PERFORMED ON JANUARY 8. THE TREND WENT FROM 1.0 ACU DOWN TO .6 - .7 ACU FOLLOWING THIS FAN MAINTENANCE (8 FLIGHTS). FOLLOWING IFSD DUE TO5.0 ACU VIBRATION THE MCD AND FILTER CHECK INDICATED BY QUANTITY AND LOCATION OF DEBRIS FOUND (INTERNAL WHEEL CASE MCD AND OTHERS) THAT THIS EVENT WAS CAUSED BY INTERNAL FAILURE- MOST LIKELY A LOCATION BEARING. 2L73 4F4 F A23WE E12EU 20030213000402003021300040NM 2003 2 13 CA030203002 120030131A3246 BEARING DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE WHEEL ASSY SEIZED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) AFTER PUSHBACK FROM GATE, CREW REPORTED THAT TUG HAD DIFFICULTLY PUSHING AIRCRAFT AS IF BRAKES FROZE. MAINTENANCE FOUND FAILURE OF I/B AND O/B WHEEL BEARINGS ON NR 2 MAIN WHEEL ASSY. LT MLG SHOCK STRUT, NR 1 AND NR 2 MAIN WHEEL ASSYS, AND NR 2 BRAKE ASSY REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030118000052003011800005SO 2003 1 18 C2XA03TY008 120030118A534014522461003 DOUBLER EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 TYS, During a scheduled inspection corrosion was found on doubler of right omega beam at frame 20 and 22. Maintenance cleaned doubler at FR20 and found to be within limits and removed and replaced the doubler for omega beam at FR22, alodined, primed and painted. I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-21-04/05/06. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2L72 4T RTT00011AT 20030220001332003022000133WP 2003 2 20 ZW0A0301801 120030208A335069030451 POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13925TW 49357 THE TAIL CONE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY. 2L72 4F A6WE 20030220001452003022000145EA 2003 2 20 A6WA200340010 120030104A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FOUND FLOOR SUPPORT STRUCTURE AT FS 621, CRACKED AT LEFT AND RIGHT SIDES COMPLIED WITH REO 601R-53-6-004 REV B. (M) 2L72 4F RTA21EA 20030220001712003022000171WP 2003 2 20 ARWA20030105 120030125A79207755259519 LINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE ENGINE OIL LEAKING A ARWAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19441J 45988 671243 NR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO FLUCTUATING OIL PRESSURE AND INTERMITTENT PRESSURE WARNING LIGHT AT 1555Z WINDMILLING OIL PRESSURE 15-25 PSI. INSPECTED NR 2 ENGINE, FOUND RIGID LINE BETWEEN MAIN OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH DAMAGED (LEAKING). REMOVED AND REPLACED RIGID LINE IAW DC8 MM 20-12-0 AND 79-20-6. OPERATIONS CHECK NORMAL IAW MM 71-00. NO LEAKS FOUND. ALSO NR 2 ENGINE MAIN OIL FILTER WAS INSPECTED IAW DC8 MM 79-20-7; NO CONTAMINATION FOUND. 2L74 4F4 F 4A25 1E8 20030220001892003022000189NM 2003 2 20 AWXA200300164 120030201A53122024T3032 WEB BOEING737 73733A 1384673NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW0 0 23634 LCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT LBL 5, WL 200 TO WL 201.25. MAINTENANCE CUTOUT CRACKS ON BS 178 BULKHEAD WEB AT LBL 5, WL 200 TO WL 201.25; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND 3 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG. 275-279, FIG. 210. 2L72 4F RTA16WE 20030625000762003062500076 2003 6 25 IXXA0300014O 420030211A22102588787904 COMPUTER DOUG DC8 DC871F 302199DWP YAW DAMPER FAILED A IXXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW11827BX84346199 45971 AFTER DEPARTURE FROM MCO DURING CLIMBOUT DESTINED FOR TOL AIRCRAFT EXPERIENCED YAW ABNOMALY. CREW ELECTED TO RETURN TO MCO. AFTER UNEVENTFUL LANDING IN MCO MAINTINANCE INSPECTED SYSTEM AND TRANSFERRED THE YAW DAMPNER TO MEL. ALL WORK COMPLETED PER APPLICABLE MANUALS AND AIRCRAFT RETURNED TO SERVICE WITH YAW DAMP SYSTEM DEFERRED. FURTHER TROUBLESHOOTING ON 2/12/2003 IN IAH REVEALED YAW DAMPNER COMPUTER FAULTY. THIS COMPONENT WAS REPLACED AND SYSTEM OPERATIONALLY CHECKED NORMAL. IAH MAINTENANCE COMPLETED ALL TASKS PER APPLICABLE MANUALS, CLEARED MEL ITEM AND RETURNED AIRCRAFT TO SERVICE. 2L74 4F RT4A25 20030221000102003022100010EU 2003 2 21 AWXA200300059 120030107A5320D534711242000 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE LOWER SURFACE OF LT SHEAR PLATE BETWEEN FR 69 AND 70. MAINTENANCE FOUND CORROSION ON LOWER SURFACE OF LT SHEAR PLATE BETWEEN FR 69 AND 70 TO BE BEYOND 50 PERCENT OF MATERIAL LOSS; REMOVED SHEAR PLATE; FABRICATED NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 53-41-17, PG. 8 & 16. 2L72 4F RTA28NM 20030221000122003022100012EA 2003 2 21 QXEA0300128 120030127A3620GG43620041 SENSOR CNDAIRCL600 CL6002C10 1390015EA BLEED AIR SYS FAILED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09606QX 10023 PDX ON FLIGHT 2446- AFTER TAKE OFF LEFT ENGINE BLEED CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PACK INLET PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030221000132003022100013NM 2003 2 21 AWXA200300061 120030102A5414311A1450 SKIN BOEING737 737300 1384610NM NR 1 ENG PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C-14 CHECK A 7/8 INCH CRACK WAS FOUND ON SKIN OF NR 1 ENGINE PYLON AT INBOARD SIDE, FORWARD ACCESS PANEL, FORWARD EDGE. MAINTENANCE STOP DRILLED CRACK ON SKIN OF NR 1 ENGINE PYLON AT INBOARD SIDE, FORWARD ACCESS PANEL, FORWARD EDGE; PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW AWA E.R. 03-5433-00158-JL2A. 2L72 4F RTA16WE 20030221000142003022100014EU 2003 2 21 AWXA200300062 120030108A5320D53472075001 BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF CREASE BEAM AT FORWARD EDGE OF RT AFT SERVICE DOOR ENTRANCE AT RT AFT LAVATORY ATTACH STUD, FR 66, STR 23 RT. MAINTENANCE FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS WITH 100 PERCENT MATERIAL LOSS AT ATTACHMENT HOLE; REMOVED DAMAGED SECTION OF CREASE BEAM; FABRICATED 2 EACH REPAIR ANGLES AND A FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, PG. 103, FIG. 101, PG. 202-204, 209-210, FIG. 201. 2L72 4F RTA28NM 20030221000252003022100025NM 2003 2 21 QXEA0300133 120030128A335010005511 SIGN DHAV DHC8 DHC8202 2809007NM CABIN FAULTY A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX- FORWARD RIGHT HAND EMERGENCY EXIT SIGN IN FRONT OF SEATS 1DE DIM WHEN SELECTED. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030221000262003022100026EA 2003 2 21 QXEA0300134 120030128A2612 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09601QX 10009 SMF-ON FLIGHT NUMBER 2496, RIGHT FIRE FAIL CAUTION MESSAGE. COMPLIED WITH SYSTEM TEST AND RIGHT FIRE FAIL CAUTION EXTINGUISHED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030221000302003022100030EA 2003 2 21 QXEA0300138 120030114A5320 SPACER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 CKB- RADIO ALTIMETER ANTENNA SPACER HAS SURFACE CORROSION AT STATION 1012.00, BL 2.500 PORT. REPAIRED IAW CRJ SRM 51-21-06. 2L72 4F RTA21EA 20030221000342003022100034EA 2003 2 21 QXEA0300145 120030113A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 CKB- AT FRAME 1126 SECOND OUTBOARD RIVET HOLE THROUGH SKIN ELONGATED STRINGER 12L. REPAIRED IAW HORIZON AIR EA R-53-67. 2L72 4F RTA21EA 20030221000362003022100036NM 2003 2 21 QXEA0300147 120030124A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- LEFT HAND WING NR 1 FLAP TRACK, UPPER TRACK, LOWER SURFACE HAS DIVOTS. REPAIRED IAW DHC-8 RD 8-57-985 AND SRM 51-00-06. 2H72 4T RTA13NM 20030213000502003021300050EU 2003 2 13 CA030205007 120030108A6420355A09103601 BEARING CAGE UROCOP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR TORN W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 CA 7845 (CAN) VIBRATION, COULDN'T STROBE OUT (1.2 IPS). CHECKED 1/2 SHELL BEARINGS AND NOTICED 2 BEARINGS TORN. REMOVED TAIL ROTOR ASSY AND CHANGED 4 BEARINGS, 1 SET PN 355A09103601 AND TWO PN 350A33215300 DUE TO WEAR. TAIL ROTOR SPAR INSPECTED AND NO DAMAGE FOUND. TAIL ROTOR REINSTALLED AND BALANCED TO BELOW 0.1 IPS. 1G71 3U3 UNCH9EU E19EU 20030213000592003021300059EU 2003 2 13 00074 120030123A5270 SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE CARGO DOOR DIRTY E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05165TW 65 PILOT REPORTED AFTER DEPARTURE FROM BHM CLIMBING THRU 5000 FT DOOR LIGHT WARNING CAME ON , LEVELED OFF AT 5000 FT REDUCED POWER LIGHT WENT OUT, RETURN TO DEPARTURE AIRPORT. MAINTENANCE CLEANED DOOR LIGHT SWITCH AND OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2L72 4F4 F A7EU E7EA 20030213000632003021300063CE 2003 2 13 0019 120030121A52101300308 SEAL LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP PAX DOOR TORN E CIEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03222BE61 489 DURING CLIMB TO ASSIGNED ALTITUDE, PILOT HEARD AN AUDIBLE AIR LEAK FROM AROUND ENTRY DOOR AT APPROXIMATELY 4.5 CABIN PSI. THE CABIN WOULD NOT PRESSURIZE BEYOND 5.5 CABIN PSI. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. CABIN DID NOT DEPRESSURIZE. LOWER AFT SECTION OF ENTRY DOOR SEAL WAS FOUND TO BE ROLLED AND TORN. SUSPECT SEAL WAS ROLLED DURING CLOSURE OF LOWER DOOR. DAMAGED SECTION OF THE DOOR SEAL WAS REPLACED IAW MM. AIRCRAFT WAS PRESSURIZED ON THE GROUND AND CHECKED GOOD. 2L72 4F4 F A10CE E6WE 20030213000652003021300065GL 2003 2 13 0065225 320030131A6114D50172 LATCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MCAULY5JFR C5JFR36C1104GL PROPELLER CRACKED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 951175 PROPELLER HUB LATCH PAWL CRACKED. 2L72 4T3 TRTA41NM E2WE 5 CP15NE 20030213000672003021300067NM 2003 2 13 0300096313 120030117A3350 CONNECTOR BOEING747 747451 1384940NM LIGHT DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK FOUND UPPER DECK STAIR AND ZONE C, RT AISLE EMERGENCY LIGHTS INOPERATIVE. RECONNECTED CONNECTOR PLUG TO POWER SUPPLY OVER DOOR 2L. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030213000682003021300068NM 2003 2 13 0300106313 120030117A2530 COFFEEMAKER BOEING747 747451 1384940NM NR 5 GALLEY ODOR A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01673US 30268 DURING FLIGHT A STRONG BURNING ODOR EMITTED IN THE AREA OF THE NR 5 GALLEY. PULLED THE GALLEY CIRCUIT BREAKERS AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CLEANED AREA OF COFFEEMAKERS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030213000702003021300070NE 2003 2 13 0300123248 220030121A7320 SEAL AIRBUS320 A320212 3930322EU CFMINTCFM56 CFM565A3 NE HMU LEAKING A NWAAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL01348NW 410 731970 DURING CRUISE FLGHT ENGINE NR 2 N1 DETERIORATED TO 72 PERCENT N1 AND TEN MINUTES LATER ENGINE NR 2 FLAMED OUT. RELIGHT UNSUCCESSFUL. FLIGHT CREW PERFORMED AN UNEVENTFUL LANDING AT DESTINATION AIRPORT. MAINTENANCE FOUND A FUEL LEAK AT THE HMU. MAINTENANCE REPLACED THE SEAL PLATE AT HMU TO FUEL FLOW TRANSMITTER. 2L72 4F4 FRTA28NM E29NE 20030213000772003021300077WP 2003 2 13 MWEA030072 120030212A8011 DRIVE SHAFT DOUG DC9 DC932 3022066WP ENGINE SHEARED A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31209ME 47730 WHEN ATTEMPTING TO START #2 ENGINE THE N2 WENT TO 10% THEN DROPPED OFF TO ZERO. -- REMOVED AND REPLACED STARTER DRIVE SHAFT. 2L72 4F A6WE 20030213000792003021300079NM 2003 2 13 03FDEA00049 120030115A5753 VANE DOUG MD11 MD11 3023602NM TE FLAP FAILED A FDEAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO25583FE 48421 NR 2 HYDRAULIC SYSTEM FAILED ON TAXI IN. DURING POST FLIGHT INSPECTION, FOUND LEFT, INBOARD FORE FLAP SPLIT IN HALF AT MID TRACK POSITION (LEFT HALF SEPARATED FROM AIRCRAFT). THIS CAUSED FLAP TO CONTINUE BEYOND ITS STOP DURING RETRACTION AND CONTINUED INTO WING INNER TRAILING EDGE STRUCTURE AND HYDRAULIC LINES. LT INBD FLAP VANE INBD TRACK ASSY REPLACED LT INBD FLAP VANE CENTER TRACK & SPRING CARTRIDGE ASSY. REPLACED LT INBD FLAP VANE OTBD TRACK ASSY REPLACED LT INBD FLAP VANE ASSY R & R DAMAGED STRUTS MPN ARC0457507 & 507 ON WING TE STRUCTURE PER MD11 SRM/SMP. AIRCRAFT OK FOR SERVICE. LT INBD FLAP VANE ASSY ADJUSTMENT AND TEST CARRIED. 2L73 4F RTA22WE 20030213000922003021300092EA 2003 2 13 COMA0360090 120030209A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01986CA7084 7174 FLIGHT 5109 GEAR DISAGREE WARNING DURING RETRACTION.REPLACED THE PSEU 2L72 4F RTA21EA 20030213000972003021300097EA 2003 2 13 COMA0360094 120030208A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO01924CA 7026 FLIGHT 5395 WHEN FLIGHT SPOILERS DEPLOYED, AIRCRAFT ROLLED TO LEFT.COULD NOT DUPLICATE. FOUND NO DEFECTS WTIH SPOILER SYSTEM. 2L72 4F RTA21EA 20030213001012003021300101WP 2003 2 13 2003F00073 120030107A335058721 COVER LKHEED1011 10113853 5265020WP SEAT 33 BROKEN G K NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 EGRESS LIGHT COVER BROKE AT LT SIDE AFT AT SEAT 33. REMOVED AND REPLACED LIGHT COVER. 2L73 4F A23WE 20030213001102003021300110WP 2003 2 13 2003F00078 120030105A335058791 LIGHT LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE CABIN INOPERATIVE G AMTAK NONE L NO TEST ININSP/MAINT 1 GL11164AT 1238 EMERGENCY LIGHTING AT FORWARD GALLEY AND ROW 2HJK INOPERATIVE. REMOVED AND REPLACED LEAD ASSEMBLY AT SEAT 2 HJK FROM WALL TO EGRESS LITE. 2L73 4F4 F A23WE A12EU 20030213001132003021300113NM 2003 2 13 2003F00086 120030106A2421727792M GENERATOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RT ENGINE INOPERATIVE G AMTAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL11523AT1212212122 30232 31672 (ORIG-CLOSED) FLT NR 576. DURING CRUISE RT GENERATOR OFF DISPLAYED. RT GENERATOR OFF LIGHT ILLUMINATED. GENERATOR SWITCH RESET DID NOT CORRECT CONDITION. CREW DEACTIVATED SYSTEM. MAINTENANCE INSTALLED SERVICABLE RIGHT ENGINE GENERATOR DRIVE ASSY IAW MM. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA2NM E12EU 20030213001142003021300114EA 2003 2 13 SWIA200311769 120030205A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERG LTS, #2 CRACKED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07413SW 7102 FLOOR LEVEL EXIT ROW LIGHT AND FLOOR TRACK LIGHTS ARE INOP. FOUND BATTERY PACK #2 CRACKED. REMOVED AND REPLACED #2 ELBP AND #2 EMERGENCY LIGHTING INVERTER IAW MM 33-51-04 & 33-51-07. OPS CHECK GOOD. 2L72 4F RTA21EA 20030204001512003020400151EA 2003 2 4 ZSE2003F00000 220030114A7200 ENGINE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA RIGHT FAILED E ZSEAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 CE01498AC8198 2745 BB287 PCE80614 DESCENDING FOR LANDING, TORQUE DROPPED ON RT ENGINE WITH TEMPERATURE INCREASING. ENGINE SHUT DOWN AND LANDED WITHOUT INCIDENT. 1L72 4T4 T A24CE E4EA 20030204001622003020400162NE 2003 2 4 MWEA030042 220030121A7200JT8D219 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RIGHT SHUTDOWN A MWEAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 GL31810ME 48072 P725366D FLIGHT EXPERIENCED LOUD BANG FOLLOWED BY A ROLL BACK OF RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE. 2L72 4F4 F A6WE E2EA 20030204001662003020400166NM 2003 2 4 SWAA030090 120030115A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED RON, FOUND AFT CABIN EELPS INOP. REMOVED AND REPLACED BATTERY PACK PER M/M. 2L72 4F RTA16WE 20030204001732003020400173 2003 2 4 SWAA030099 420030116A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030204001752003020400175 2003 2 4 SWAA030100 420030116A256522D22900131 SLIDE BOEING737 7372H4 138448CNM R1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F A16WE 20030204001812003020400181NM 2003 2 4 SWAA030107 120030117A57546573714 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND NR 6 LE SLAT LOWER SKIN CRACKED .5 INCHES. SLAT SKIN CRACK REPAIRED PER SRM. 2L72 4F RTA16WE 20030204001872003020400187 2003 2 4 SWAA030118 420030117A2565D31354 SLIDE BOEING737 7377H4 1384404NM CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29789SW 29816 DURING SCHEDULED BC3 CHECK, FOUND THE R2 EMERGENCY ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED THE R2 ESCAPE SLIDE PER MM. 2L72 4F RTA16WE 20030204001922003020400192CE 2003 2 4 200301 120030115A36001H7514 REGULATOR CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA ZONE 400 BINDING E S4WAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP0795NA 3868 208B0666 DURING CRUISE FLIGHT, PILOT NOTICED A BURN ODOR IN COCKPIT. PILOT THEN NOTED THAT DOOR POST TRIM PANEL WAS DISCOLORED. RETURNED TO AIRPORT AND NOTIFIED MECHANIC. MECHANIC FOUND THE PRESSURE REGULATOR TO BE FAULTY. FURTHER INVESTIGATION LED TO REPLACEMENT OF THE PRESSURE RELIEF VALVE AND ALL THREE DEICE SOLENOIDS (PRECAUTIONARY MEASURE). PERFORMED MECHANIC FLIGHT AFTER, NO FURTHER DEFECTS NOTED. 1H71 3T3 T A37CE E2NE 20030204001982003020400198NM 2003 2 4 SWAA030126 120030119A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN LT FWD, RT FWD AND RT AFT CLEVIS LUG FACES CORRODED. REPAIRED THE VERTICAL FIN LUG FACES PER SWA ER. 2L72 4F RTA16WE 20030204002042003020400204 2003 2 4 SWAA030133 420030120A34255224655001 CONTROL PANEL BOEING737 7372T4 1384492NM COCKPIT MALFUNCTIONED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29702ML 22054 BOTH FLIGHT DIRECTORS WENT TO GA MODE AND ARCED SMELL IN COCKPIT. REMOVED AND REPLACED SELECTOR FLIGHT DIRECTOR MODE CONTROL PANEL PER MM. 2L72 4F A16WE 20030204002072003020400207NM 2003 2 4 SWAA030136 120030120A2560P2070004 RETAINER BOEING737 7372H4 138448CNM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED A2 CHECK, FOUND FWD LOWER EMERGENCY FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED EMERGENCY FLASHLIGHT HOLDER PER MM. 2L72 4F A16WE 20030204002082003020400208NM 2003 2 4 SWAA030137 120030120A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 597, STR 7L, BS 616, STR 5R, AND BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030204002112003020400211NM 2003 2 4 SWAA030153 120030121A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED C2 CHECK, FOUND EEPLS DAMAGED AT ROWS 10, 19, AND AFT END. REPAIRED EEPLS PER MM. 2L72 4F A16WE 20030204002212003020400221 2003 2 4 SWAA030178 420030126A2565D31354 SLIDE BOEING737 7375H4 138449DNM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030204002242003020400224NM 2003 2 4 SWAA030181 120030124A53116545807 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR CUTOUT FWD CENTER STUB FRAME CRACKED. REPAIRED STUB FRAME PER SWA EA. 2L72 4F RTA16WE 20030204002252003020400225NM 2003 2 4 SWAA030182 120030126A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030204002302003020400230NM 2003 2 4 SWAA030198 120030125A2560P2070001 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED SERVICE CHECK, FOUND UPPER AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030204002392003020400239NM 2003 2 4 SWAA030211 120030129A3397BR2013 WIRE BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29719SW 27853 EEPLS SECTION BROKEN. SECURED EEPLS STRIP, RELAMPED AND REPAIRED WIRING PER MM. 2L72 4F RTA16WE 20030204002522003020400252NM 2003 2 4 VNAA0301015 120030115A5310 STRUCTURE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FUSELAGE VIBRATION A VNAAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07458PS 3068 DURING TAKEOFF, THE CREW FELT A STRONG VIBRATION AT APPROXIMATELY 60 KNOTS AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND FOUND NO DISCREPANCIES. MAINTENANCE THEN PERFORMED HIGH SPEED TAXI RUNS WITH THE CREW AND COULD NOT DUPLICATE THE PROBLEM AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002602003020400260NM 2003 2 4 HNAA0300007 120030130A335082410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003NM CABIN DEFECTIVE A HNAAO OTHER O OTHER CRCRUISE 1 EA07908HA4593845838 015 Emergency light over pax door and forward right hand side emergency door flicker on and off during flight. Removed and replaced emergency light control box, operational check good. 2H72 4T RTA13NM 20030204002612003020400261NM 2003 2 4 2003UALA00105 120030125A5700 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 SCRAPE ON BOTTOM SURFACE OF RIGHT WING, 3 FEET INBD FROM TIP. FOUND DENT 3 BY 6 INCHES WITH DELAM. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED QUADRUPLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20030204002702003020400270NM 2003 2 4 VNAA0301018 120030118A5270 PROXIMITY SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DOOR FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07426JS 3038 EN ROUTE, THE CREW RECEIVED A OPEN DOOR INDICATION ON THE RED WARNING PANEL FOR THE PASSENGER DOOR. THERE WAS NO LOSS OF PRESSURE AND THE DOOR WAS SECURE. FLIGHT 4195 THEN DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 8MC OVER THE CENTER PROXIMITY SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030204002912003020400291EA 2003 2 4 SWIA200311756 120030108A5315 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOOR, FS 621 LHCRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07430SW 7523 FS 621 LH FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV ''A''. ANGLE P/N: 601R53-61-117-1 REPAIR ANGLE P/N: 601R53-61-117-3. 2L72 4F RTA21EA 20030205000282003020500028CE 2003 2 5 ENHA200300001 120030121A275226111441 SUPPORT CESSNA CESSNA208 208B 2073701CE FLAP ACTUATOR CRACKED E ENHAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 AL031276P2858 00852 FLAP ACTUATOR STRUCTURE SUPPORT ASSY FAILURE. PILOT REPORTED FLAPS SELECTED TO 10 DEGREE, FLAPS DEPLOYED TO 10 DEGREE. AT THE NEXT FLAP SELECTION, FLAP C/B TRIPPED, C/B WOULD NOT RESET. STANDBY FLAP SWITCH WAS NOT USED AND BREAKAWAY WIRE INTACT. INSPECTION OF FLAP SYSTEM BY MAINTENANCE PERSONNEL FOUND THE FLAP ACTUATOR SUPPORT BRACKETS CRACKED AND BROKEN. 1H71 3T A37CE 20030205000392003020500039NM 2003 2 5 SROM200300006 120030105A78106573771 FAIRING BOEING737 737205 1384456NM ZONE 400 DENTED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 2 ENGINE O/B TAILPIPE COWLING DENTED 30 INCHES FROM FWD END AND 22 INCHES FROM BOTTOM. REMOVED & REPAIRED DENTED SECTION PER SRM 51-40-02 PG. 1-3 FIG. 1. MINOR REPAIR. 2L72 4F RTA16WE 20030205000412003020500041NM 2003 2 5 SROM200300008 120030107A781065522631017 GUSSET BOEING737 737205 1384456NM NR 1 TAILPIPE FAGOUGED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND NUMBER ONE ENGINE O/B FIXED FAIRING AFT UPPER GUSSET GOUGED. REPAIRED #1 ENGINE O/B FIXED FAIRING AFT UPPER GUSSET PER SRM 54-10-1, 51-20-1 AND 51-30-2. MINOR REPAIR 2L72 4F RTA16WE 20030205000432003020500043NM 2003 2 5 SROM200300010 120030114A54106573771 WEB BOEING737 737205 1384456NM ZONE 400 TORN C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND LOWER AFT NR 2 PYLON WEB TORN AT AFT T/R HYDRAULIC LINE HOLE. REPAIRED WEB PER SRM 51-40-2. MINOR REPAIR 2L72 4F RTA16WE 20030205000452003020500045NM 2003 2 5 SROM200300012 120030116A541065C140941 SKIN BOEING737 737205 1384456NM ZONE 400 CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND NR 1 ENGINE SLIPPER FAIRING INBOARD AFT CORNER SKIN TORN. REMOVED DAMAGE AREA 1.1 X 0.8 INCH, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-30-2, 51-10-2, 51-10-1, 51-40-2 AND 54-30-1. MINOR REPAIR. 2L72 4F RTA16WE 20030205000482003020500048NM 2003 2 5 SROM200300015 120030116A5413657010426 LONGERON BOEING737 737205 1384456NM ZONE 400 CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND NR 1 ENGINE IB FIXED FAIRING AFT UPPER LONGERON ANGLE BROKE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 54-10-1, 51-30-2 & 51-20-1. MINOR REPAIR. 2L72 4F RTA16WE 20030205000502003020500050NM 2003 2 5 SROM200300017 120030120A53106566213 SHROUD BOEING737 737205 1384456NM APU BAY CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND LOWER APU SHROUD CRACKED 3.5 INCHES AFT OF PREVIOUS REPAIRED AREA. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED ON SHROUD PER EA 4910-01089 & 4910-01077. MONOR REPAIR 2L72 4F RTA16WE 20030221000452003022100045NM 2003 2 21 QXEA0300156 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 1 SEAT TRACK HAS PITTING CORROSION AT STATION 424. REPAIRED IAW DHC-8 SRM 51-20-16, 51-00-06 AND 51-20-36. 2H72 4T RTA13NM 20030221000462003022100046NM 2003 2 21 QXEA0300157 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 1 SEAT TRACK HAS PITTING CORROSION AT STATION 405-408. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-16, 50-20-36 AND RD 8-53-1342. 2H72 4T RTA13NM 20030221000492003022100049NM 2003 2 21 AWXA200300076 120030125A3350BR964411 LIGHT BOEING737 73733A 1384673NM SEAT ROW 15 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030221000522003022100052NM 2003 2 21 QXEA0300158 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 1 SEAT TRACK HAS PITTING CORROSION AT STATION 390. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-16, 51-20-36 AND RD 8-53-1342. 2H72 4T RTA13NM 20030221000542003022100054NM 2003 2 21 QXEA0300159 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 1 SEAT TRACK HAS LIGHT PITTING AT STATION 340-345. REPAIRED IAW DHC-8 SRM 51-20-16, 51-00-06, 51-20-36 AND RD 8-53-1342. 2H72 4T RTA13NM 20030221000582003022100058NM 2003 2 21 QXEA0300162 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 1 SEAT TRACK HAS LIGHT PITTING AT STATION 295-298. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-16, 51-20-36 AND RD 8-53-1342. 2H72 4T RTA13NM 20030221000772003022100077NM 2003 2 21 AWXA200300171 120030129A5315146N5444 FRAME BOEING757 7572S7 1384962NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT FRAME BS 1510, LBL 11. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT FRAME BS 1510, LBL 11; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030221000782003022100078NM 2003 2 21 AWXA200300172 120030129A5315146N5444 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT FRAME BS 1510, LBL 07 IN THE AFT CARGO COMPARTMENT . MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT FRAME BS 1510, LBL 07; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030221000872003022100087NM 2003 2 21 CALA0300058 120030219A5347 SEAT TRACK BOEING737 7373T0 1384582NM BS 907-947.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND L/H O/B SEAT TRACK AT BS 907-947.5 CORRODED. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. 2L72 4F RTA16WE 20030221000912003022100091SW 2003 2 21 AC2A084144 120030207A6500430310101107 RESTRAINT BELL 430 430 1182150SW TAIL ROTOR DEBONDED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2883 49037 SHEAR RESTRAINT IS DISBONDED. PIN IS SEPARATED FROM RUBBER. REPLACED SHEAR RESTRAINT. 1G72 3U RTH9SW 20030221000972003022100097NM 2003 2 21 0300265642 120030218A7920 PWA BOEING757 757251 1384970NM PWA 2037 PW2037 NE A NWAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01542US 26489 716410 During cruise flight the aircraft cabin and cockpit were cold. Flight crew switched to manual and then to auto pack temp control. The cabin began to fill with smoke and the left aft lav alarm sounded. Smoke stopped when standby pack control reselected. Maintenance replaced the Zone Temp Controller. 2L72 4F4 FRTA2NM E17NE 20030625000922003062500092NM 2003 6 25 F3LA200300069 120030218A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, LBL 3, AT NUT PLATE ON UNDERSIDE OF FLANGE. FABRICATED AND INSTALLED FLOOR SUPPORT AND SPLICE PER SRM 53-10-3, FIG 11, AND SOPM 20-41-02. 2L72 4U RTA16WE 20030625000932003062500093NM 2003 6 25 F3LA200300071 120030218A5320 SEAT TRACK BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT STA 290, RBL 16. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-2 AND 53-10-2. 2L72 4U RTA16WE 20030625000942003062500094NM 2003 6 25 F3LA200300073 120030218A5320 ANGLE BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON BULKHEAD ANGLE AT STA. 947.5 LOWER ANGLE. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-1, 53-20-01, FIG. 5, DETAIL II, 51-30-02 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030625000952003062500095NM 2003 6 25 F3LA200300074 120030218A5313 STRINGER BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON STRINGER 18-R AT STA. 727B + 16. REPAIRED DAMAGED SECTION OF STRINGER PER SRM 53-10-1, PAGE 6, DETAIL VI, SRM 53-10-3, PAGE 10, DETAIL VII AND SOPM 20-41-02. 2L72 4U RTA16WE 20030223000062003022300006SO 2003 2 23 C2XA03SH016 120030222A530014525994001 CROSSBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND RIGHT FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030205000572003020500057WP 2003 2 5 DHL2003804500 120030116A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING L/E INNER FORMER CRACKED 1/2 IN AT XFS 598.000. REMOVED FASTNERS PER SRM 51-1-20D PG 21,STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 0.032. CLEANED, TREATED AND PRIMED PER SRM 51-1-8 B.INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030205000642003020500064 2003 2 5 DL76L030003 420030101A34206227998003 INDICATOR BOEING767 767332 1382001NM COCKPIT FAILED A DALAO OTHER O OTHER CRCRUISE 1 SO27171DN 3366 24759 COPILOTS ADI FAILED ENROUTE. ALTN EFIS NO HELP. REPLACED COPILOTS ADI. TEST OK. OK FOR SERVICE. 2L72 4F RTA1NM 20030205000812003020500081NE 2003 2 5 DL76L030006 220030102A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 STALLED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO271200K25559 724741 28457 724741 NR 1 ENGINE 2 AUDIBLE COMPRESSOR STALLS ON T/O FROM DUB...ACFT RETURNED MTC IN PROGRESS. REPLACING NR 1 ENGINE. 2L72 4F4 FRTA1NM E24NE 20030206000372003020600037NM 2003 2 6 0300196718 120030128A5311 WEB BOEING747 747251F 1384898NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 During "L" check found crack in frame web at BS 380 S23R. Repaired per EA 67-165035. 2L74 4F A20WE 20030206000402003020600040NM 2003 2 6 0300166718 120030128A5412 BULKHEAD BOEING747 747251F 1384898NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 During "L" check found crack on #4 pylon rear engine mount bulkhead. Repaired per EA 67-165031. 2L74 4F A20WE 20030206000412003020600041NM 2003 2 6 0300205511 120030124A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01511US 23199 DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-193436. 2L72 4F RTA2NM 20030206000532003020600053EA 2003 2 6 COMA0390001 120030203A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA WING MALFUNCTIONED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01331CA544 10061 FLIGHT 5097 LANDING GEAR DISAGREE WARNING.REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20030206001302003020600130EA 2003 2 6 COMA0360070 120030202A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAO OTHER S AFFECT SYSTEMS UKUNKNOWN 1 SO01982CA2751 7168 FLIGHT 5242 EMERGENCY LIGHTS ARE INOPREPLACED EMERGENCY BATTERIES 2L72 4F RTA21EA 20030206001332003020600133EA 2003 2 6 COMA0360072 120030203A3260172825 TARGET CNDAIRCL600 CL6002B19 1900309EA L/H MLG LOOSE A COMAA UNSCHED LANDING NS FALSE WARNING AFFECT SYSTEMS CLCLIMB 1 SO01952CA 7092 FLIGHT 5156 GEAR DISAGREE WARNING.TIGHTENED LOOSE TARGET ONTHE L/H MLG UPLOCK. 2L72 4F RTA21EA 20030206001402003020600140EA 2003 2 6 COMA0360079 120030202A21331037729 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01477CA1378 7670 FLIGHT 5241 AIRCRAFT WOULD NOT PRESSURIZE. REPLACED THE NR 2 OUTFLOW VALVE. 2L72 4F RTA21EA 20030206001772003020600177NM 2003 2 6 CALA0300009 120030112A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917321 23372 INSPECTION FOUND A 3 INCH CRACK IN CENTER FLOOR SUPPORT BETWEEN STA 500D AND 520. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030206001782003020600178NM 2003 2 6 CALA0300010 120030113A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917321 23372 INSPECTION FOUND KEEL BEAM CORRODED AFT OF STA 500D INSIDE AIR CONDITIONING DISTRIBUTION BAY. A KEEL BEAM REPAIR WAS INSTALLED IAW SRM 53-30-12. 2L72 4F RTA16WE 20030206001842003020600184EU 2003 2 6 USAASA03004 120030114A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19728UW 1155 TPA - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030206001922003020600192SO 2003 2 6 C2XA03IA016 120030206A32307455501REVF CONTROL HANDLE EMB 145 EMB145LR 3260212SO COCKPIT INTERMITTENT A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2713988 145265 IAH- FLIGHT 2088, LANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE, ATTEMPTED TO RECYCLE GEAR TWICE WITH NO CHANGE. THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030207000122003020700012NM 2003 2 7 DLM88030020 120030104A25304110001131 COFFEEMAKER DOUG MD88 MD88 3023688NM R-1 GALLEY OVERHEATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27985DL 53312 ON ENTRY INTO AIRCRAFT FIRST OFFICER AND FLIGHT ATTENDENT SMELLED ELECTRICAL TYPE ODOR IN AIRCRAFT. FOUND R1 GALLEY COFFEEMAKER OVERHEATING. REPLACED. 2L72 4F RTA6WE 20030224000122003022400012GL 2003 2 24 ALGA084136 220030219A7200 BEARING RACE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL PT SHAFT CORRODED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO SG10056 FOUND CORROSION PITTING ON INNER POWER TURBINE SHAFT BEARING RACE. 1Q71 3R3 U 2A6 E1GL 20030224000142003022400014SW 2003 2 24 ALGA084141 120030220A6520214040009109 GEARBOX BELL 214 214ST 1182106SW TAIL ROTOR WORN H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01390AL3642 28198 MOUNT HOLE ON GEARBOX ELONGATED AND WORN AT CONTACT POINT. 2G72 4U H10SW 20030625000962003062500096NM 2003 6 25 F3LA200300076 120030219A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT SCREW HOLE, STA. 328, LBL 29. REMOVED TOP CAP REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE TO TOP CAP PER SRM 51-40-02. 2L72 4U RTA16WE 20030224000302003022400030NE 2003 2 24 HEEA084149 220030211A7532 BELLOWS SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE BLEED VALVE RUPTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K FF34600 760082 DOES NOT OPEN ON TEST RUN. REPLACED BELLOWS PN 6893483 DUE TO RUPTURED AND PITTED. REPAIRED BLEED VALVE. 1G72 3U3 U H1NE E19EU 20030224000312003022400031NE 2003 2 24 HEEA084151 120030211A63007610205001047 PLATE SKRSKYS76 S76A 8143006NE MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 PILOT BUSHINGS HAS GROOVES. REPLACED PILOT 76101-05022-103 DUE TO WORN; SCRAPER S11065-17 DUE TO WORN; AND LINER 300SSDRML DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030224000332003022400033NE 2003 2 24 HEEA084154 120030211A6320 BEARING SKRSKYS76 S76A 8143006NE M/R GEARBOX ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH10562 A08100316 760078 MAIN ROTOR GEARBOX HAS A WORN GENERATOR DRIVE AND ROUGH BEARINGS. 1G72 3U H1NE 20030224000352003022400035NE 2003 2 24 HEEA084156 120030211A21407650007904101 PRESSURE SWITCH SKRSKYS76 S76A 8143006NE HEATER INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 PRESSURE SWITCH INOPERATIVE. SCRAPPED. 1G72 3U H1NE 20030224000372003022400037 2003 2 24 HEEA084158 420030212A2312064100900 TRANSCEIVER SKRSKYS76 S76A 8143006NE VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 TRANSCEIVER HAS GARBLED TRANSMISSION. ADJUSTED TRANSMIT COMPRESSOR. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G72 3U H1NE 20030224000392003022400039 2003 2 24 HEEA084160 420030212A34211113034 INDICATOR SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 ATTITUDE INDICATOR JUMPS AND JIGGLES IN FLIGHT. 1G72 3U H1NE 20030224000432003022400043 2003 2 24 HEEA084164 420030212A34215040017928 INDICATOR SKRSKYS76 S76A 8143006NE STANDBY ATTITUDEPRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 STANDBY ATTITUDE INDICATOR PRECESSES IN FLIGHT, NOT ON GROUND. IN SHOP REPAIR. 1G72 3U H1NE 20030224000452003022400045 2003 2 24 HEEA084166 420030212A34427007700614 INDICATOR SKRSKYS76 S76A 8143006NE WX RADAR SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 WEATHER RADAR PICTURE IS NOT BRIGHT ENOUGH. 1G72 3U H1NE 20030224000472003022400047 2003 2 24 HEEA084168 420030212A34427021450601 INDICATOR SKRSKYS76 S76A 8143006NE WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 WEATHER RADAR SCREEN GOES BLANK. 1G72 3U H1NE 20030224000482003022400048NE 2003 2 24 HEEA084169 120030212A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 14124 760166 TAIL ROTOR BLADE PRIMARY RUBBERS ON BOTH PADDLES TORN. 1G72 3U H1NE 20030224000522003022400052NE 2003 2 24 HEEA084173 120030212A6700 BEARING SKRSKYS76 S76A 8143006NE BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 WORN BEARINGS. REPLACED 4 EACH BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030224000532003022400053NE 2003 2 24 HEEA084174 120030212A6700 BEARING SKRSKYS76 S76A 8143006NE BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K 760082 FLT CONTROL BELLCRANK HAS WORN BEARINGS. REPAIRED. 1G72 3U H1NE 20030207000132003020700013NM 2003 2 7 DLM88030026 120030105A3350BR9279103 LIGHT DOUG MD88 MD88 3023688NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27977DL 53258 ON INSPECTION FOUND EMERGENCY LIGHT IN FWD AREA OF AFT AIRSTAIR INOPERATIVE. FOUND WIRING TO LIGHT ASSY DAMAGED. REPLACED LIGHT ASSY AND QUICK DISCONNECT SPLICES. OPERATION OF LIGHT NORMAL. 2L72 4F RTA6WE 20030207000192003020700019NE 2003 2 7 DLM88030057 220030114A7261 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 LEAKING A DALAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27965DL 49984 INBOUND CREW REPORTS OIL FUMES IN CABIN. FOUND OIL LEAK ON NR 1 ENGINE. REPAIRED SAME 2L72 4F4 FRTA6WE E9NE 20030207000212003020700021NM 2003 2 7 DLM88030062 120030109A55315911384506 SPAR CAP DOUG MD88 MD88 3023688NM VERTICAL STAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27974DL 53242 DURING HMV-2, REPLACEMENT OF THE RT INNER & OUTER HINGE PLATES, TOOLING DAMAGE WAS INCURRED AT A SINGLE FASTENER LOCATION ON ANGLE PN 3912080504 AND REAR SPAR CAP PN 5911384506.THE HOLE WAS OVERSIZED AND BUSHED ON EACH PART. 2L72 4F RTA6WE 20030207000392003020700039NM 2003 2 7 DLM90030037 120030106A322059632541 PISTON DOUG MD90 MD9030 3023690NM NLG STRUT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27916DN 53396 NOSE GEAR UNSAFE ON TAKE OFF. COMPLIED WITH POM PROCEDURE CYCLED GEAR STILL UNSAFE UP. NOISE LEVEL WAS VERY HIGHT INDICATING DOOR AND OR GEAR WAS EXTENDED. ALSO AUTO SPOILER FAIL MSG. F/D WENT OF VIEW. STALL INDICATOR FAILURE. REPLACED NOSE LANDING GEAR STRUT PISTON ASSY PER MM PERFORMED OPERATIONAL CHECK OF NOSE LANDING GEAR PER MM. CHECKED GOOD. PERFORMED ACS RTS TEST, PASSED 2L72 4F RTA6WE 20030207000402003020700040NM 2003 2 7 DLM90030046 120030111A273008BHG36ABJF733 SENSOR DOUG MD90 MD9030 3023690NM RT ELEVATOR FAILED A DALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO27907DA 53387 AT CRUISE FL330 EOAP MESSAGE ELEVATOR SPLIT & PYLON FLAP FAULT ILLUMINATED. ALSO NO AUTOLAND ILLUMINATED ON FMA. RAN RTS ON DFGC 1 & 2. GO ON BOTH. RAN ACS TEST. NO FAULTS FOUND ELEVATOR POSITION SENSOR NR 2 ON DFGC 2. REPLACED RT ELEVATOR POSITION SENSOR IAW AMM 27-34-01-5. 2L72 4F RTA6WE 20030207000872003020700087NM 2003 2 7 QXEA0300001 120030101A5270 SENSOR BOMBDRDHC8 DHC8401 1390041NM DOOR LACK OF LUBE A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09414QX 4061 BTM - FLIGHT 381 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE REAR PASSENGER DOOR AND FORWARD CARGO DOOR INDICATED OPEN. MAINTENANCE INSPECTED BOTH DOORS, CLEANED AND LUBED SENSORS, AND PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS WERE GOOD AND NO FURTHER DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030207000882003020700088EA 2003 2 7 QXEA03000011 120030104A2820D98C09602 PRESSURE SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM LEAKING A QXEAO OTHER K FLUID LOSS UKUNKNOWN 1 NM09604QX2378 10019 FAT - FUEL WAS FOUND LEAKING FROM THE PRIMARY EJECTOR PRESSURE SENSORS WEEP HOLES. MAINTENANCE REPLACED BOTH PRIMARY EJECTOR PRESSURE SENSORS AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030207000892003020700089NM 2003 2 7 QXEA0300002 120030101A1430 BOLT DHAV DHC8 DHC8202 2809007NM PAX DOOR LOOSE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09359PH 514 SEA- FLIGHT ATTENDANT REPORTS THAT MAIN CABIN DOOR STICKS, MAKING IT VERY DIFFICULT TO OPEN. FOUND LOOSE ATTACHMENT BOLT AND NUT IMPEDING DOOR OPENING AND CLOSING. TIGHTENED BOLT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030207000952003020700095NM 2003 2 7 03FDEA00050 120030120A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 CORROSION ON FLOORBEAM LWR CHORD UPPER SURFACE STA 1130 RBL 4 WL 201. 2L73 4F RTA3WE 20030207001182003020700118NM 2003 2 7 03FDEA00081 120030129A5210 DOOR BOEING727 727200 138407ENM CREW ENTRY OPEN A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25267FE 21673 DURING CLIMB A/C PRESS FAIL, RAN THE RED TABS AND IT WAS NO HELP. S/O OPENED COCKPIT DOOR AND FOUND EITHER CREW ENTRY OR CARGO DOOR WAS SUSPECTED OPEN. DECLARED EMERGENCY AND DIVERTED INTO AFW. FOUND CREW ENTRY DOOR PARTIALLY OPEN WHEN AIRCRAFT BLOCKED AT AFW. REMOVED DOOR LINER AND SLIDE, REMOVED AND REPLACED UPPER HINGE GUIDE ARM ASSY AND LOWER HINGE SNUBBER, AND REINSTALLED DOOR LINER AND SLIDE IAW 727 AMM 52-11-061-4 2L73 4F RTA3WE 20030207001242003020700124NM 2003 2 7 03FDEA00100 120030203A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION ON SHEAR TIE AT BS 1166, RBL 3, WL 152, AFT CARGO BAY. 2L73 4F RTA3WE 20030207001262003020700126NM 2003 2 7 03FDEA00102 120030203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO BAY FRAME IS GOUGED AT BS 680 LBL 50 WL 172. 2L73 4F RTA3WE 20030207001292003020700129WP 2003 2 7 ZW0A0301504 120030201A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN DISCONNECTED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13960TW 49231 THE EGRESS EMERGENCY EXIT LIGHT STRIP AT THE AFT GALLEY DOOR EXIT WAS INOPERATIVE. RECONNECTED CONNECTOR ON TERMINAL STRIP. 2L72 4F A6WE 20030207001452003020700145NE 2003 2 7 QXEA0300015 220030106A72504124T31P03 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 ENGINE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX2860 10010 965263 CKB - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE WITH MISSING MATERIAL. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVETIGATION AT GE.INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THIS REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030210000362003021000036EA 2003 2 10 QXEA0300021 120030107A2820D98C09602 PRESSURE SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS UKUNKNOWN 1 NM09601QX100 10009 LGB-ON FLIGHT NUMBER 2502, FUEL LEAK NOTED FROM CENTER OF TWO INSPECTION PANELS. REMOVED AND REPLACED NR 1 PRIMARY EJECTOR SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030224000552003022400055NE 2003 2 24 HEEA084176 120030212A21407650007904101 SWITCH SKRSKYS76 S76A 8143006NE NR 2 ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 NR 2 ENGINE HEATER SAFETY SWITCH INOPERATIVE; HEATER INOPERATIVE. IN SHOP REPAIR. 1G72 3U H1NE 20030224000602003022400060NE 2003 2 24 HEEA084181 220030212A74209550168600 IGNITION LEAD SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE ENGINE CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 IGNITION LEAD CHAFED. 1G72 3U3 U H1NE E19EU 20030224000622003022400062NE 2003 2 24 HEEA084183 220030212A74129550176020 GENERATOR SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE HIGH ENERGY INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 HIGH ENERGY GENERATOR IS INOPERATIVE. 1G72 3U3 U H1NE E19EU 20030224000672003022400067 2003 2 24 HEEA084188 420030212A2340PHI20004 MIXER BOX SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X 760050 VHF SWITCHES WILL NOT MUTE AUDIO. FOUND SWITCH S1 BAD. REPLACED. BENCH CHECK GOOD. 1G72 3U H1NE 20030224000712003022400071GL 2003 2 24 HEEA084191 220030213A75329550161210 BLEED VALVE AEROSPAS355 AS355* EU ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 BLEED VALVE WILL NOT CLOSE. 1G72 3U3 U H11EU E4CE 20030224000772003022400077NE 2003 2 24 HEEA084198 120030213A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 TRAILING EDGE HAS SEPARATION AND A 5 INCH CRACK. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20030224000842003022400084 2003 2 24 HEEA084205 420030213A34578143902240B GPS SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 GPS HANGS UP WITH BUTTONS PUSHED ON NAV, WPT, ENT. BUTTONS AT TIMES TAKES 2 0R 3 PUSHES TO ACTIVATE. ALSO DROPS TERMINAL DATA AND UNABLE TO USE SOME APPROACHES WITHOUT RESTARTING. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20030224000852003022400085 2003 2 24 HEEA084206 420030214A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S12887 760035 AFCS ACTUATOR KICKS IN FLIGHT. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030224000892003022400089SW 2003 2 24 HEEA084210 120030120A5320407070620112 TRIM PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 CABIN TRIM PANEL CRACKED. 1G71 3U O H2SW 20030224001032003022400103EA 2003 2 24 COMA0360111 120030220A2420AE7098291 LINE CNDAIRCL600 CL6002B19 1900309EA LT ENGINE LEAKING A COMAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO01976CA 7151 FLIGHT 5015 #1 IDG AND GENERATOR FAULT MESSAGE.REPLACED LEAKING OIL LINE ON IDG. 2L72 4F RTA21EA 20030224001052003022400105SW 2003 2 24 HEEA084220 120030120A5320407070620140 HEADLINER BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 HEADLINER CRACKED. 1G71 3U O H2SW 20030224001142003022400114NM 2003 2 24 CALA0300064 120030223A5320 WEB BOEING737 7373T0 1384582NM STA 791-800 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND VERTICAL WEB CORRODED IN AFT BAGGAGE BIN AT STA 791-800, RBL 20. A NEW WEB WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20030224001162003022400116NM 2003 2 24 CALA0300066 120030223A5320 STRAP BOEING737 7373T0 1384582NM STA 780-800 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND STRAP CORRODED UDER VERTICAL WEB AT STA 780-800, RBL 20. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030224001182003022400118NM 2003 2 24 CALA0300068 120030223A5311 FRAME BOEING737 7373T0 1384582NM STA 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND R/H O/B FRAME CORRODED AT STA 986, RBL 40. REPAIRED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030224001202003022400120EA 2003 2 24 COMA0360112 120030220A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA 3A WEAK A COMAL ABORTED APPROACH S AFFECT SYSTEMS APAPPROACH 1 SO01934CA7085 7042 FLIGHT 5847 GEAR DISAGREE WARNING.REPLACED THE 3A HYDRAULIC PUMP. 2L72 4F RTA21EA 20030214000052003021400005NM 2003 2 14 2003F00090 120030108A2421734284F GCU BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE E/E BAY FAILED G C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 GL11523AT 30232 (ORIG-CLOSED) FLT 431. ON TAKEOFF ROLL BELOW 40 KTS, RT GENERATOR TRIPPED OFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE RT GCU IAW MM. PERFORMED GENERATOR CONTROL ADJUSTMENT AND TEST IAW AMM OPERATIONAL CHECKS NORMAL. 2L72 4F4 FRTA2NM A12EU 20030214000072003021400007NM 2003 2 14 2003F00092 120030105A3397 WIRE BOEING757 75723N 1384973NM CABIN DISCONNECTED G K NONE L NO TEST TXTAXI/GRND HDL 1 GL11514AT 27971 (ORIG-CLOSED) FLT 337. DURING GROUND HANDLING AFT SECTION OF EMERGENCY PATHWAY LIGHTING INOPERATIVE. MAINTENANCE FOUND WIRE LOOSE AT ROW 30, RECONNECTED WIRE. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20030214000082003021400008NM 2003 2 14 2003F00093 120030101A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE CABIN DISCONNECTED G K NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 (ORIG-CLOSED) DURING SCEDULED MAINTENANCE EMERGENCY EGRESS LIGHTS AT ROW 38 INOPERATIVE. MAINTENANCE RECONNECTED WIRE AT ROW 38 EGRESS LIGHTS ASSEMBLY. OPERATIONAL CHECK NORMAL. 2L72 4F4 FRTA2NM A12EU 20030214000142003021400014 2003 2 14 2003FA0000033 420030114A2210501126402 SERVO LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP YAW CHAFED B JGVAK NONE O OTHER ININSP/MAINT 1 CE09520SC8168 600 087 THE SECONDARY YAW SERVO CABLE KEEPER WAS RUBBING THE PRIMARY YAW SERVO CABLE ON THE RT SIDE CAUSING EXCESSIVE WEAR ON BOTH COMPONENTS. 2L72 4F4 F A10CE E6WE 20030214000152003021400015EU 2003 2 14 2003FA0000050 120030110A7160C42RDB502017 INLET BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP ENGINE CRACKED E MNZAK NONE O OTHER ININSP/MAINT 1 CE0312OJC6846 NA0247 DURING ROUTINE INSPECTION, IT WAS NOTED THAT THE ENGINE INLET ASSEMBLY WAS CRACKED AT THE SOUND DAMPENING SCREEN AND A COUPLE OF FASTENERS (RIVETS) WERE MISSING. THE PART WAS REMOVED & REPLACED WITH A NEW OR OVERHAULED PART. 2L72 4F4 F A3EU E6WE 20030214000202003021400020NM 2003 2 14 2003FA0000147 120030107A2761654494710 HOUSING BOEING BOEING737 737* NM ACTUATOR BROKEN B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 52748 4423 ACTUATOR HOUSING BROKEN AT BEARING LUG. 2L72 4F RTA16WE 20030320000812003032000081NM 2003 3 20 2003UALA00049 120030110A38300123FJ SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE LAVATORY 'K' FAILED A UALAA UNSCHED LANDING AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29551UA586 25399 FIRE IN THE LEFT AFT LAV UNDER THE SEAT SHROUD. LIQUID LEVEL SENSOR FAILED INTERNALLY CAUSING A FIRE THAT DAMAGED THE SENSOR ITSELF ALONG WITH THE TOILET SEAT SHROUD AND A NEARBY AIR VENT. REPLACED LIQUID LEVEL SENSOR, TOILET SHROUD, AND VENT ASSEMBLY AND RETURNED LAVATORY TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20030214000312003021400031WP 2003 2 14 ASAA0280031A 120030104A573039615971 ACCESS PANEL DOUG DC9 DC983 3022083WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT GROUND SPOILER ACCESS PANEL 1627A IS CRACKED. REPLACED PANEL PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20030214000382003021400038NM 2003 2 14 CALA0300042 120030204A5542 SKIN PANEL BOEING737 737524 1384721NM RUDDER L/E GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0937615 27328 INSPECTION FOUND THE LOWER L/H SIDE OF RUDDER LEADING EDGE SKIN PANEL GOUGED. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5540-01162. 2L72 4F RTA16WE 20030214000402003021400040NM 2003 2 14 CALA0300044 120030212A5330 SKIN BOEING737 7373T0 1384582NM STA 727D CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0969348 23586 INSPECTION FOUND A 3" CRACK IN FUSELAGE SKIN AT STA 727A, S23L. REPAIRED IAW ECRA 5330-03090. 2L72 4F RTA16WE 20030625000802003062500080NM 2003 6 25 F3LA200300053 120030129A5320 SHIM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL CORRODED BETWEEN STA 312 AND STA 328, RBL 12. REMOVED INTERCOSTAL BETWEEN STA 312 AND STA 328 AND FOUND CORROSION TO BE ON SHIM ONLY. REMOVED SHIM, FABRICATED AND INSTALLED REPLACEMENT SHIM PER SRM 51-40-02, 51-40-02 AND EA 53-737-195. 2L72 4F RTA16WE 20030214000442003021400044NM 2003 2 14 P5CA0300750 120030127A5320NONE INTERCOSTAL BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LEVEL 1 CORROSION, DISTORTION AND SEVERAL TEARS FOUND LOWER LOBE AFT CARGO BTWN STATION STA 1800-1900, RH 58 LBL 58. DAMAGE INTERCOSTAL REMOVED AND FABRICATED HF 2024T3.0050 THK PER SAMPLE & SRM 53-11-25. PROTECTED AREA PER SRM 51-10-02. RIVETED PER SRM 51-3-02. 2L74 4F A20WE 20030214000452003021400045NM 2003 2 14 P5CA0300751 120030127A5320NONE SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK ON SEAT TRACK RH-25 STA 910. DAMAGED PORTION FLOOR TRACK REMOVED. NEW PORTION FABRICATION H/F 78-71511 EXTRU.BAC 1580-1658 PER SRM 58-11-25 FIG. 7R ANGLE PER SRM 51-40-02 (7075 T6 TM560). RIVETED PER SRM 51-30-02. 2L74 4F A20WE 20030214000502003021400050WP 2003 2 14 ABXA030002 120030101A3397 WIRE DOUG DC9 DC931 3022065WP PWA JT8 JT8D* NE CHART HOLDER UNSECURE A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23945AX 47551 FIRST OFFICERS YOKE LIGHT SPARKED WHEN LIFTED. SECURED WIRING TO CHART HOLDER IAW MM. OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20030214000632003021400063WP 2003 2 14 ASAA0380044 120030105A5321993659913 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL HAS DAMAGED EDGE. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030214000682003021400068NM 2003 2 14 ABXA030026 120030106A5320214T03311 TUBE BOEING767 767281 1385109NM FUSELAGE WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE, BETWEEN STA. 325 - 347, LT BUTT LINE 21, LT BUTT LINE 48.65 AND RT BUTT LINE 44.45, 6 EACH TUBES WORN OUT. DAMAGED TUBES REMOVED AND NEW TUBES INSTALLED IAW SRM. 2L72 4F RTA1NM 20030214000742003021400074WP 2003 2 14 ASAA0380049 120030105A573099375792 PANEL DOUG DC9 DC983 3022083WP RT WING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING LOWER PANEL 1219C COUNTERSINK HOLES ARE ELONGATED. INSTALLED DOUBLER PER SRM 57-06A. (M) 2L72 4F RTA6WE 20030214000782003021400078WP 2003 2 14 ASAA0380051 120030105A575359359201 ACCESS PANEL DOUG DC9 DC983 3022083WP T/E FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT WING FLAP LOWER FLEX JOINT ACCESS PANEL IS CHAFED IN SEVERAL PLACES. REPLACED PANEL PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20030214000832003021400083SO 2003 2 14 C2XA03CL038 120030211A5210 HANDLE EMB 145 EMB145ER 3260211SO MAIN DOOR LOOSE A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2715948 145056 SYR FLIGHT#2886 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE.MAINTENANCE INSPECTED AND RESECURED THE INSIDE HANDLE ON THE MAIN CABIN DOOR.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030214000842003021400084NM 2003 2 14 UPS03240161 120030129A5330 DOUBLER BOEING727 72725C 138400HNM BS1180 S6L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C SMALL AREA OF EXFOLIATION CORROSION FOUND ON FUSELAGE SKIN BS1180 JU ST ABOVE STR.6L REPAIR FILLER AND NEW DOUBLER TO INCORPORATE NEW AND EXISTING REPAIR FABRICATED IAW SRM 53-30-03 FIG.3A. REPAIR PARTS INSTALLED IAW SRM 53-30-03. 2L73 4F A3WE 20030214000862003021400086SO 2003 2 14 C2XA03CL039 120030213A335020131A BATTERY EMB 135 EMB135ER 3260203SO CABIN DEFECTIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727506 145206 DURING ROUTINE MAINTENANCE THE EMERGENCY FLOOR LIGHTING BETWEEN ROW 1 AND ROW 8 DID NOT TURN OFF.MAINTENANCE INSPECTED AND REPLACED THE #2 EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030214000982003021400098WP 2003 2 14 ASAA0380056 120030105A523059101417 RUB STRIP DOUG DC9 DC983 3022083WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO DOOR LOWER PAN FORE AND AFT RUB BLOCKS ARE CHAFED. REPAIRED PAN PER EA 5230-01185. (M) 2L72 4F RTA6WE 20030214001012003021400101NM 2003 2 14 0300226641 120030210A2597 WIRE BOEING747 747212B 1384886NM PWA JT9 JT9D* NE COFFEE MAKER MISROUTED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01641NW 21941 DURING FLIGHT SMOKE EMITTED FROM THE LEFT AFT GALLEY COFFEE MAKER. PULLED CIRCUIT BREAKER AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REROUTED CROSSED WIRES ON COFFEE MAKER TERMINAL STRIP AND REPLACED COFFEE MAKER. OPERATIONAL CHECK GOOD. 2L74 4F4 F A20WE E20EA 20030625000812003062500081NM 2003 6 25 F3LA200300054 120030201A5340 ATTACH ANGLE BOEING737 7373M8 1384615NM FUSELAGE WORN A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED SEVERAL FASTENER HOLES WORN AND DAMAGED ON RT MLG WHEEL WELL CUTOUT AFT FAIRING ATTACH ANGLE. REPLACED ATTACH ANGLE PER SRM 51-40-02. 2L72 4F RTA16WE 20030214001122003021400112WP 2003 2 14 ASAA0380060 120030106A52304926022 PAN DOUG DC9 DC983 3022083WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY DOOR PAN CHAFED AT FORWARD AND AFT LOWER RUB BLOCKS. BLENDED DAMAGED AREAS PER EA 5230-01187 AND BAC TLX AOC-OKC-02-00125H AND -00126H. (M) 2L72 4F RTA6WE 20030214001132003021400113WP 2003 2 14 ASAA0380061 120030106A532059360501 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, LONGERON 30 SPLICE IS CORRODED AT FS 1201. BLENDED SPLICE PER EA 5310-02153 AND BAC TLX AOC-OKC-02-00159H. (M) 2L72 4F RTA6WE 20030625000822003062500082NM 2003 6 25 F3LA200300055 120030129A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 312 CORRODED FROM BL 0 TO RBL 12. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-51, PARA 114, DETAIL XI. FABRICATED REPAIR PART PER SRM 53-10-51 AND INSTALLED PER SRM 53-10-51 AND SRM 51-40-02. 2L72 4F RTA16WE 20030214001382003021400138SO 2003 2 14 LR7A03008 120030202A5311 DOUBLER LKHEED382 382G 526414USO FS 902 MISSING A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 581 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0504 FOUND PREVIOUS FRAME REPAIR REQUIRING REWORK TO CONFORM TO SRM SMP 583 53-50-17, DUE 1 EA. MISSING DOUBLER FS 902, LBL 62, WL 200. CAUSE LIKELY MISINTERPRETATION AND APPLICATION OF 53-50-16 REPAIR - NO OUTBD DOUBLER REQUIRED.INSTALLED DOUBLER ON OUTBOARD SURFACE OF INNER TEE IAW SRM SMP 583 53-50-17. NR 0071. 2H74 4T A1SO 20030214001392003021400139SO 2003 2 14 LR7A03009 120030214A71006714802 VANE LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL #4 FAILED A LR7AE ENGINE SHUTDOWN C F.O.D. CRCRUISE 1 AL03405LC 2514 5025 550353 #4 ENG. DECOUPLED IN-FLIGHT 25,000 FT APPROX 11,000 LB. TORQ. ENG. SHUTDOWN IAW QRH.SUSPECT INGESTION FROM PART OF 2ND STAGE COMPRESSOR VANE.REMOVED AND REPLACED #4 ENGINE ASSY PER JOB CARD HN71136 AND TEST RAN PER JC 7101. ENGINE OPS CHECKS GOOD AND LEAK CHECKS GOOD. 2H74 4T4 T A1SO E282 20030216000032003021600003EU 2003 2 16 RAIA00302035 120030203A3200350A52006011 CONTROLLER AEROSPATR72 ATR72202 8680940EU MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03723TE80 80 283 5452-MLI- LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE #1 MULTI FUNCTION CONTROL, OPS CK OK. 2H72 4T RTA53EU 20030216000062003021600006NE 2003 2 16 RAIA00302040 220030205A7200PW120 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE LEAKING A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03421TE26864 102 120540 5548-STL- SMOKE HASE IN CABIN AND COCKPIT. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE. 2H72 4T4 TRTA53EU E20NE 20030216000092003021600009EU 2003 2 16 RAIA00302043 120030211A2730C850176 SENSOR JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03555HK9749 9749 41072 5608-STL- LEFT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED LEFT STALL SENSOR, OPS CK OK. 2L72 4T RTA41NM 20030217000022003021700002NE 2003 2 17 ANCF200300007 220030215A7311ACB093F2480Y7 FILTER BOEING767 767259 1385136NM PWA 4056 PW4056 NE DIRTY W ANCFD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 SO23985AN 24618 EICAS(STATUS)MSG L ENG.FUEL FILTER DISPLAYED.ACTION. WAS REPLACED FUEL FILTER ELEMENT ENG.LH IN ACCORDING AMM 73-11-02/401.IT WAS CLEANED FUEL DISTRIBUTION VALVE STRAINER FILTER IAW AMM 73-11-04 PAG 401. TEST IAW AMM 71-00-00 PAG.501 2L72 4F4 FRTA1NM E24NE 20030217000142003021700014EU 2003 2 17 QXEA0300275 120030212A33506008905 POWER SUPPLY FOKKERF28 F28MK4000 4990810EU ZONE 200 FAILED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09492US 11159 PDX- EMERGENCY EGRESS LIGHTS AT ROW 5, 6 AND 8 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20030218000052003021800005NM 2003 2 18 03FDEA00083 120030129A2613 WARNING LIGHT BOEING727 727200 138407ENM BODY OVERHEAT ILLUMINATED A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 SO25288FE 21850 LOWER AFT BODY OVERHEAT ILLUMINATED IN FLIGHT AT FL280. ACCOMPLISHED LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED (CHECKLIST) IAW QRH INDICATED SOURCE OF OVERHEAT AS ENGINE NR 3 LOW STAGE BLEED AIR SUPPLY TO THE MAIN WING ANTI-ICE VALVE. LIGHT EXTINGUISHED AND TESTED GOOD. TESTS NORMAL. RAN ENGINES IWA JRH APPROX 1 HR. REMOVED ACCESS PANEL FOR KEELBEAM AREA. INSPECTED FOR LEAKS WITH LASER HEAT DETECTOR IN AFT STAIRWELL,AFT CGO COMPARTMENT, KEELBEAM AREA, FOUND NONE. CHECKED FOR CLEARANCE ON ACCESSIBLE LOOPS. FOUND OK. INSTALLED KEEL BEAM ACCESS PNL. PRIOR HISTORY SHOWS T/S FOR FALSE ALARM. PERFORMED IAW MM 26-14-000-1 HAS BEEN C/W. REPLACED DET CONT. IAW MM. TESTS OK. 2L73 4F RTA3WE 20030218000082003021800008NM 2003 2 18 03FDEA00095 120030120A5753NRC6055508 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 SNRM N0957 - RT WING INBOARD FLAP, INBOARD AND OUTBOARD BORE OF THE FLAP SIDE OF THE HINGE BRACKET PIVOT BORES FOUND WITH CORROSION. ** S/D ** COMING 2L73 4F RTA22WE 20030218000142003021800014NM 2003 2 18 03FDEA00109 120030205A2613 WARNING LIGHT BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE NR 3 ENGINE ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25212FE 22934 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT. COMPLETED PROCEDURES IAW QRH. LIGHT EXTINGUISHED AFTER NR 3 BLEED CLOSED - R PACK OFF - NR 3 THRUST LEVER TO IDLE. NR 3 THRUST LEVER RESTORED WITH NO REOCCURANCE. ***S/D COMING **** 2L73 4F4 FRTA3WE E2EA 20030218000362003021800036NM 2003 2 18 AWXA200300014 120030105A71602607MK2 ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE VARI STATOR VANEINOPERATIVE A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28660AW9664 1234 FLT 0660, ON TAKEOFF ROLL EN ROUTE RECEIVED ECAM MESSAGE (ENG 1 COMPRESSOR VANE); REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306. LUBRICATED VSV, PERFORMED MAINTENANCE GROUND RUN, OPERATIONAL AND LEAK CHECK GOOD. 2L72 4F4 FRTA28NM E311NE 20030218000712003021800071NM 2003 2 18 AMTA200300107 120030118A2612710127 FIRE LOOP BOEING757 75733N 1384931NM LT ENGINE FAULTY A AMTAK NONE J WARNING INDICATION ININSP/MAINT 1 GL11556TZ 32590 STATUS MESSAGE LT ENG FIRE LOOP 2. REMOVED AND REPLACED LEFT ENGINE LOOP NR 2 IAW MM 26-11-01-4. SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030218001072003021800107NM 2003 2 18 VNAA0302015 120030216A3300501122803 POWER SUPPLY 501122803 DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FORWARD FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07459PS187292561 7531 3070 THE CREW REPORTED THE EMERGENCY AND BACK UP BATTERIES FAIL TO TEST. MAINTENANCE INSPECTED AND REPLACED BOTH EMERGENCY POWER SUPPLIES IN ACCORDANCE WITH DONIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030218001182003021800118NM 2003 2 18 VNAA0301029 120030126A24301180001 GCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RIGHT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07432JS19446 3045 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030218001282003021800128NM 2003 2 18 GAIA03001OP 120030117A28246563 VALVE BOEING727 7272J0 138407ENM FUEL SYSTEM MALFUNCTIONED A GAIAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07281KH 21105 FLT 884 - ONT-FWA - DURING CLIMB CREW DISCOVERED A PROBLEM WITH THE FUEL PANEL. THE NR 2 CROSSFEED VALVE WAS NOT OPEN. CREW DECLARED AN EMERGENCY AND DIVERTED TO PHX. DEFERRED NR 2 CROSSFEED VALVE PER MEL 28-7. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20030218001732003021800173NM 2003 2 18 QXEA0300165 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 4 SEAT TRACK HAS SCRATCHES AT STATION 310-325. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001752003021800175NM 2003 2 18 QXEA0300167 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 4 SEAT TRACK HAS SCRATCHES AT STATION 344-360. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001792003021800179NM 2003 2 18 QXEA0300171 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 3 SEAT TRACK HAS LIGHT PITTING AT STATION 514. REPAIRED IAW RD 8-53-3644, DHC-8-200 SRM 51-40-11 AND SRM 51-40-00. 2H72 4T RTA13NM 20030625000992003062500099NM 2003 6 25 F3LA200300080 120030219A5347 SEAT TRACK BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND SCREW HOLES AT SEAT TRACK BETWEEN STA. 328 AND STA. 344, RBL 54. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-3. 2L72 4U RTA16WE 20030224001242003022400124NM 2003 2 24 P5CA0300768 120030224A5320NONE SEAT TRACK BOEING747 7472U3B 1384846NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23923FT 22769 LEVEL 1 CORROSION FOUND UPPER LOBE MAIN DECK SEAT TRACK LBL 1133, RT STA 1480-1660. DAMAGE SEAT TRACK PORTION REMOVED. NEW FABRICATE M/F 7075T6SM EXTRU BAC 1520-1889 PER DWG 866-17-19743-SH-2. 2L74 4F RTA20WE 20030224001252003022400125NM 2003 2 24 P5CA0300769 120030224A5330NONE SKIN BOEING747 7472U3B 1384846NM FUSELAGE DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23923FT 22769 DENT PUSHED INBD AT EXT FUSELAGE SKIN STA 400 LH - STR 27. DAMAGE AREA TRIMMED OUT. REINFORCED AREA W/ DOUBLER PER SRM 53-30-03, FIG. 1. 2L74 4F RTA20WE 20030224001312003022400131WP 2003 2 24 ZW0A0302603 120030219A3350105606003 HARNESS DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139620D 53591 DURING OVERNIGHT INSPECTION ROW 21 FLOOR PATH LIGHTING INOP. REPLACED BROKEN HARNESS 105606-003 CPN 4096971 BETWEEN ROW 22 AND 23. OPS CHECK NORMAL PER MD80 MM33-53-01. CHECK-C STL 10-19-02. --CLOSED-- 2L72 4F RTA6WE 20030224001342003022400134NM 2003 2 24 AWXA200300184 120030128A5320146N5447 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1471, STR 29R. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AREA OF FLOOR SUPPORT BS 1471, STR 29R; FABRICATED REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1-7. 2L72 4F RTA2NM 20030224001472003022400147NM 2003 2 24 AWXA200300199 120030218A5313693535214 TIE CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW0 0 24060 YVR - MAJOR REPAIR - DURING C-11 CHECK A 3/8" CRACK WAS FOUND UNDER RIVET HEAD ON STRINGER TIE CLIP BS 727D, STR 6 L/H. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 727D, STR 6 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3 & 6. 2L72 4F RTA16WE 20030225000052003022500005SO 2003 2 25 C2XA03SH025 120030225A530014521713005 BEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 24.MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030225000092003022500009SW 2003 2 25 HEEA084228 120030120A2510407070620152 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 SEAT PANEL CRACKED. 1G71 3U O H2SW 20030225000102003022500010SW 2003 2 25 HEEA084229 120030120A5320407070620153 PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030225000122003022500012SW 2003 2 25 HEEA084231 120030120A5320407070620155 PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030225000162003022500016SW 2003 2 25 HEEA084235 120030120A5210407070620157 PANEL BELL 407 407 1182206SW PAX/CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 PAX/CREW DOOR PANEL CRACKED. 1G71 3U O H2SW 20030225000172003022500017SW 2003 2 25 HEEA084236 120030120A5210407070620157 PANEL BELL 407 407 1182206SW PAX/CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 PAX/CREW DOOR PANEL CRACKED. 1G71 3U O H2SW 20030225000212003022500021SW 2003 2 25 HEEA084240 120030120A5320407070620179 PANEL BELL 407 407 1182206SW CABIN BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 CABIN INTERIOR PANEL BROKEN. 1G71 3U O H2SW 20030225000242003022500024SW 2003 2 25 HEEA084243 120030120A2701407070620183 PANEL BELL 407 407 1182206SW CONTROL COLUMN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 CONTROL COLUMN PANEL CRACKED. 1G71 3U O H2SW 20030225000272003022500027SW 2003 2 25 HEEA084246 120030120A2510407070620207 STRUCTURE BELL 407 407 1182206SW HAT BIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 HAT BIN STRUCTURE CRACKED. 1G71 3U O H2SW 20030210000512003021000051NM 2003 2 10 QXEA0300034 120030112A36208209732 SWITCH BOMBDRDHC8 DHC8401 1390041NM BLEED AIR SYS MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09403QX 4037 PDX ON FLIGHT 2353- NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED DURING FLIGHT. TURNED OFF NR 2 BLEED PER CHECKLIST. CAUTION LIGHT REMAINED ILLUMINATED FOR THE REST OF THE FLIGHT. REMOVED AND REPLACED NR 2 BLEED OVER TEMPERATURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030210000542003021000054EA 2003 2 10 QXEA0300037 120030111A2820D98C07606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09608QX239 239 10026 PDX ON FLIGHT 2474- LEFT FUEL LOW PRESSURE CAUTION MESSAGE WHEN LEFT BOOST PUMP SELECTED. REMOVED AND REPLACED ENGINE PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030210000552003021000055NM 2003 2 10 QXEA0300038 120030111A3010 DEICE SYSTEM BOMBDRDHC8 DHC8401 1390041NM LT WING MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX 4046 SEA ON FLIGHT 2389- RETURNED TO FIELD DUE TO DEICE PRESSURE CAUTION LIGHT. LEFT HAND OUTBOARD BOOT WOULD NOT FULLY INFLATE. RIGHT HAND INBOARD TAIL LIGHT WOULD NOT GO OUT WHEN OUTBOARD WERE ILLUMINATED. CYCLED DEICE PRESSURE SYSTEM NUMEROUS TIMES AND OPERATIONAL CHECKS OF DUAL DISTRIBUTION VALVES. NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030210000972003021000097NM 2003 2 10 QXEA0300047 120030105A1430 FASTENER BOMBDRDHC8 DHC8401 1390041NM FUSELAGE MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 CKB-FORWARD BAGGAGE DOOR FUSELAGE AND AFT SERVICE DOOR FUSELAGE TOP FORWARD AND AFT CORNERS HAVE FASTENERS MISSING. REPAIRED IAW HORIZON AIR EA 653-168AND RD8-4-53-342. 2H72 4T RTA13NM 20030210001072003021000107NM 2003 2 10 QXEA0300055 120030107A7110 BRACKET BOMBDRDHC8 DHC8401 1390041NM LT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX-LEFT HAND ENGINE LOWER COWL UPPER DECK TO CONE SUPPORT AND BRACKET TOP FLANGE IS CRACKED AT AFT END. REPAIRED IAW RD8-4-71-016. 2H72 4T RTA13NM 20030210001132003021000113NM 2003 2 10 QXEA0300061 120030105A5320 CLIP BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- ANGLE CLIP CRACKED FOR SUPPORT STRUCTURE FOR VHF ANTENNA AT AFT OUTBOARD INSIDE CORNER. REPAIRED IAW HORIZON AIR EO 6-53-162. 2H72 4T RTA13NM 20030210001142003021000114NM 2003 2 10 QXEA0300062 120030107A5320 CLIP BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- CRACKED CLIP ON SUPPORT STRUCTURE FOR VHF ANTENNA AT FORWARD OUTBOARD INSIDE CORNER STATION Z81.00. REPAIRED IAW HORIZON AIR EO 6-53-162. 2H72 4T RTA13NM 20030210001172003021000117NM 2003 2 10 QXEA0300063 120030107A5320 CLIP BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- CRACKED CLIP AT SUPPORT STRUCTURE OF VHF ANTENNA AT FORWARD OUTBOARD OUTSIDE CORNER STATION Z81.00. REPAIRED IAW HORIZON AIR EO 6-53-162. 2H72 4T RTA13NM 20030210001372003021000137NM 2003 2 10 CALA0300029 120030210A5330 SKIN BOEING737 7373T0 1384582NM STA 880 GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND THE R/H UPPER FUSELAGE SKIN GOUGED BELOW FORWARD R/H SIDE DORSAL FIN MOUNT POINT AT STA 880, STRINGER 2R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01. 2L72 4F RTA16WE 20030210001592003021000159NM 2003 2 10 AWXA200300117 120030128A532065C105922 FLOOR SUPPORT BOEING737 7373G7 138447JNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CABIN FLOOR INTERCOSTAL AT BS 947-967, RBL 8. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT BS 947-967, RBL 8; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65C10592; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030210001602003021000160NM 2003 2 10 AWXA200300118 120030120A53146545866588 PANEL BOEING737 73733A 1384673NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW0 0 23634 LCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH 1" CRACKS WERE FOUND ON KEEL BEAM PANEL BETWEEN WHEEL WELLS AT FORWARD END BS 685. MAINTENANCE REMOVED EXISTING DOUBLER AT BS 660 TO BS 690; STOP DRILLED CRACKS AND PERFORMED HFEC INSP TO VERIFY CRACKS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-12, FIG. 202, PG. 204. 2L72 4F RTA16WE 20030211000022003021100002NM 2003 2 11 02603427 120030126A3242 BRAKE DORNERDO32 DO328300 NM PWA 306 PW306B NE LT MLG CONTAMINATED A VTZAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA27427FJ 3192 FLIGHT CREW REPORTED SMOKE COMING FROM THE LT MAIN LANDING GEAR DURING LANDING. AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE PERSONNEL INSPECTED LT BRAKES AND FOUND TRACES OF DEICING FLUID ON BRAKES. FLUID WAS REMOVED FROM THE BRAKES AND AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 FRTA55NM E35NE 20030211000052003021100005EA 2003 2 11 03027625 120030127A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27625BR 7214 ON TAKEOFF, RECEIVED NOSE GEAR DISAGREE AND NOSE DOOR MESSAGE WITH AURAL WARNING. ADJUSTED NOSE GEAR PROX SWITCH. OPS CHECKED OK. 2L72 4F4 FRTA21EA E15NE 20030211000102003021100010NM 2003 2 11 ANCF200300004 120030201A5270 WARNING LIGHT BOEING757 757236 1384971NM CARGO DOOR FALSE ACTIVATIONW ANCFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO23227AN 23227 DURING TAKE OFF EICAS MSG AFT CARGO DOOR DISPLAYED AND CARGO DOOR OPEN LIGHT ILLUMINATED. TAKE OFF WAS REJECTED. AFT CARGO DOOR WAS INSPECTED AND FOUND LOCKED AND CLOSED; CARGO DOOR INDICATION WAS DEFERRED UNDER MEL 52-71-1 CAT "C" AND MAINTENANCE ACTIONS WERE ACCOMPLISHED. 2L72 4F RTA2NM 20030212000172003021200017EU 2003 2 12 AUS20030001 120030101A77123039242 SENSOR FOKKERF27 F27MK50 EU PWA PWA120PW125B NE TORQUE INDICATORFAILED W O OTHER EJIVIBRATION/BUFFET WARNING INDICATION FLT. ATTITUDE INST. TOTAKEOFF 1 AUS (AUS) RT ENGINE TORQUE INDICATOR TAPE CONTINUED TO INCREASE ABOVE THE EEC SETTING DURING TAKEOFF. THE EEC AND MFC WIRING WAS CHECKED AND CLEANED, TORQUE GAUGES WERE SWAPPED AND THE ENGINE RATING PANEL REPLACED. SEVERAL FLIGHTS LATER THE RT TORQUE WAS REPORTED FLICKERING UP TO 6 PERCENT AND THE EEC DEGRADE LIGHT ILLUMINATED. INVESTIGATION SHOWED A FAULT CODE 65 IDENTIFYING THE NR 1 NH SENSOR AS THE PROBLEM. 2H72 4T4 TRTA817 E20NE 20030225000322003022500032SW 2003 2 25 HEEA084251 120030120A5320407070620210 PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030225000532003022500053SW 2003 2 25 HEEA084275 120030211A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M507 28102 MAIN BATTERY WEAK. BATTERY SCRAPPED AT VENDOR 1/17/03. 2G72 4U H10SW 20030225000572003022500057SW 2003 2 25 HEEA084279 120030211A6720206001058101 CONTROL ROD BELL 206 206L3 1182108SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 CONTROL ROD HAS SURFACE DAMAGE UNDER SLEEVE. SCRAPPED TAIL ROTOR CONTROL ROD DUE TO CORROSION. 1G71 3U H2SW 20030225000612003022500061SW 2003 2 25 HEEA084283 120030211A6710206001053005 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E O OTHER O OTHER NRNOT REPORTED 1 SW038594X 51531 MAIN ROTOR FLT CONTROL BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS. REPAIRED. 1G71 3U H2SW 20030225000632003022500063SW 2003 2 25 HEEA084285 120030211A6220206011100105 ROTOR HEAD BELL 206 206L4 1182110SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03621278754 52023 MAIN ROTOR HEAD IS SLINGING GREASE FROM END OF GRIP. REPLACED 4 NUTS EB902514 DUE TO CORROSION AND RETAINER 206011129003 DUE TO BEING WORN. REPAIRED. 1G71 3U NCH2SW 20030225000732003022500073NM 2003 2 25 DHL2003747005 120030222A7830 ANNUNCIATOR BOEING727 727224 1384076NM COCKPIT SHORTED A DHLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01747DH 22253 AFTER DEPARTING CVG IN HEAVY RAIN, ESSENTIAL POWER WARNING LIGHT STARTED TO PARTIALLY ILLUMINATE FOLLOWED BY ALL 3 REVERSER LIGHTS, THEN GEAR LIGHTS. NO OTHER INDICATIONS OF ACTUAL PROBLEMS THOUGH. CYCLED WARNING LIGHTS TEST SWITCH TO BRIGHT AND LIGHTS WENT OUT. THEN CYCLED TEST SWITCH BACK TO DIM AND ALL LIGHTS CONNECTED WITH THAT TEST SWITCH ILLUMINATED AND STAYED ON. UNABLE TO GET LIGHTS TO GO OUT AFTER. CONFIRMED NR 2 THRUST REVERSER ANNUNCIATOR INTERNALLY SHORTED. REPLACED SAME. ALL INSTRUMENT PANEL ANNUNCIATORS CHECK GOOD IAW B727 M/M 33-10-41. ANNUNCIATOR REPLACEMENT DONE IAW B727 M/M 33-10-51. 2L73 4F A3WE 20030225000822003022500082SW 2003 2 25 HEEA084296 120030211A6330407310203101 MOUNT BELL 407 407 1182206SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 MAIN ROTOR GEARBOX MOUNT WORN. 1G71 3U O H2SW 20030225000902003022500090SW 2003 2 25 HEEA084303 120030211A6510407340339101 BEARING BELL 407 407 1182206SW T/R DRIVESHAFT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 TAIL ROTOR DRIVESHAFT HANGER BEARING SLINGING BLACK GREASE. 1G71 3U O H2SW 20030625001072003062500107NM 2003 6 25 F3LA200300089 120030225A5320 SILL BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR RT. MOP SILL CORRODED AT VARIOUS POINTS ALONG ENTIRE LENGTH OF MOP SILL. REPLACED DAMAGED MOP SILL PER SRM 51-30-2 AND BOEING DRAWING 65-45855. 2L72 4U RTA16WE 20030625001082003062500108NM 2003 6 25 F3LA200300090 120030225A5320 MOUNT BRACKET BOEING737 7372Y5 1384554NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED FWD FUSELAGE VHF 2 ANTENNA MOUNT BRACKET CRACKED AT STA. 500, RBL 2. REPLACED BRACKET PER SRM 51-10-1 AND 51-30-2. 2L72 4U RTA16WE 20030625001092003062500109NM 2003 6 25 F3LA200300091 120030225A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM AT STA. 772, LBL 12, AT FLOOR PANEL SPLICE STRIP, BOTTOM SIDE OF UPPER FLANGE. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-5 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030225001002003022500100NM 2003 2 25 P5CA0300771 120030225A7600NONE THROTTLE BOEING747 747341 13848AMNM # 4 ENG STUCK A P5CAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 WP23355MC 23395 # 4 ENG. SHUT DOWN ON DESCENT INTO PIK - THROTTLE STUCK AT 2.0 ON THROTTLE QUANDRANT ENG PARAMETERS NORMALS 75% M ONE MORE THIS HAPPENED ON DESCENT OIL PRESSURE AT LAST FEW MIN. OF FLT THROTTLE OK AFTER LANDING. ENG SHUT DOWN CHECKLIST COMPLIED WITH A/C CURRENTLY IN A-CK CORRECTIVE ACTION TO FOLLOW. 2L74 4F RTA20WE 20030226000042003022600004 2003 2 26 ALGA084686 420030221A83006893672 PINION GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL ACCESSORY G/B WORN H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01547AL1496 CAG47047 53240 CAE847064 FOUND PINION GEARS SHOWING HEAVY WEAR ON DRIVE SIDE. THIS IS A REOCCURRING EVENT. 1G71 3U3 UO H2SW E1GL 20030226000052003022600005NE 2003 2 26 BAQA084101 220030210A753297914211 BLEED VALVE BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE ENGINE DAMAGED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01117CJ53 7051 BLEED VALVE CONNECTOR PLUG RECEPTICLE CORRODED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030226000072003022600007SW 2003 2 26 HEEA084305 120030211A6510407340340101 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 TAIL ROTOR DRIVE DISC PACK CRACKED. 1G71 3U O H2SW 20030212000252003021200025WP 2003 2 12 AUS20030025 120030114A57115145975500 SPAR DOUG DC4 C54E 3021530WP LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING REAR LOWER SPAR CAP ANGLE CORRODED IN AREA BETWEEN WS 318 AND WS 357. 2L74 4R A762 20030212000272003021200027EU 2003 2 12 AUS20030027 120030112A5302109037043205 STRUCTURE AGUSTAA109 A119 0261102EU TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL BOOM ASSEMBLY CRACKED. LIMITED INFORMATION PROVIDED. 1G72 3U H7EU 20030212000282003021200028CE 2003 2 12 AUS20030030 120030107A289799102326 WIRE HARNESS CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL FUEL WIRING CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING FUEL CAPACITANCE LOOM CHAFING ON THE UPPER SURFACE OFTHE LOWER WING SKIN AT THE INBOARD END. 1L72 3O3 O A7CE E8CE 5 CP22EA 20030212000302003021200030NM 2003 2 12 AUS20030043 120030120A5315 FLOORBEAM BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FLOORBEAM CORRODED AT BS 1110 LBL 68 AND RBL 68 WL 208. 2L73 4F4 FRTA3WE E2EA 20030212000332003021200033NM 2003 2 12 AUS20030047 120030120A5315 FLOORBEAM BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLOORBEAM CORRODED AT BS 72 LBL 65 AND RBL 65. 2L73 4F4 FRTA3WE E2EA 20030212000342003021200034NM 2003 2 12 AUS20030048 120030120A5315 FLOORBEAM BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLOORBEAM CORRODED AT BS 620 LBL 62 AND RBL 62. 2L73 4F4 FRTA3WE E2EA 20030212000432003021200043WP 2003 2 12 ARWA20030108 120030127A2611100064901 SMOKE DETECTOR DOUG DC8 DC862 3021970WP CARGO BAY MALFUNCTIONED A ARWAO OTHER J WARNING INDICATION CRCRUISE 1 SO19810BN 45905 LOWER CARGO SMOKE AND FIRE DETECTION MAINTENANCE LIGHT ON; CODE F15231: FALSE ALARM. LOWER CARGO AND FIRE DETECTOR MAINTENANCE LIGHT ON; ENTERED ON DMI 17416 IAW MEL 26-10-1-R-A CAT "C". REMOVED AND REPLACED SMOKE DETECTOR FORWARD CENTER; OPERATIONAL CHECK OK, IAW STC 00746LA-D. CLEARED DMI 17416. 2L74 4F 4A25 20030410002502003041000250NM 2003 4 10 F3LA200300034 120030127A5320 FLOOR SUPPORT BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT STA 727D+5, RBL 8. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-60-53, SRM 53-00-53, AND SOPM 20-41-02. 2L72 4F RTA16WE 20030212000482003021200048NE 2003 2 12 NACA20030074 220030210A8530356994 CYLINDER PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE 15 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA1748 1748 36210 45529 36210 DISCREPANCY: #3 ENGINE SHUT DOWN DUE TO BACK FIRING.CORRECTIVE ACTION: REPLACED #15 CYLINDER. 2L74 4R4 R A781 5E8 20030212000532003021200053NE 2003 2 12 NACA20030075 220030211A7421URHB32E SPARK PLUG PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE #2 CYLINDER CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL034387254 54 858218 44665 1841 DISCREPANCY: #2 ENGINE SHUT DOWN DUE TO LOW BMEP.CORRECTIVE ACTION: REPLACED #2 CYLINDER REAR SPARK PLUG AND RETORQUED COIL AND LEAD. 2L74 4R4 R A781 5E8 20030212000602003021200060NE 2003 2 12 CA030116001 220030113A7200CF343B1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT FAILED W O OTHER LJ NO TEST WARNING INDICATION CRCRUISE 1 CA 873612 (CAN) PRODUCTION FLIGHT TEST 1 (2002-12-21) UNABLE TO AIRSTART RT ENGINE EITHER WINDMILL OR WITH AIR TURBINE START. N2 REMAINED AT 0 PERCENT EVEN WITH ATS ENGAGED. RNC (RAPPORT DE NON CONFORMANCE) C302087572 RAISED. PILOTS TO CARRIED OUT DISPOSITION OF RNC AS PER PROPULSION ENGINEERING ON NEXT FLIGHT. PRODUCTION FLIGHT TEST 2 (2002-12-23) REPEAT OF SNAG FLIGHT NR 1. RT ENGINE N2 TURNED FREELY AFTER LANDING DURING MOTORING ON APU BLEED. ON NEXT FLIGHT, BREAK-IN PROCEDURE CARRIED OUT PRIOR TO RESTART ATTEMPT. AFTER BREAK-KN PROCEDURE REPEAT WINDMILL RELIGHT PROCEDURE PER PROPULSION ENGINEERING DISPOSITION. PRODUCTION FLIGHT TEST #3 (2002-12-23) WINDMILL PORTION OF WEAR IN PROCEDURE UNSUCCESSFUL. ATS RELIGHT AFT2L72 4F4 FRTA21EA E15NE 20030212000622003021200062CE 2003 2 12 CA030116003 120030113A8011631847 SHAFT CESSNA421 421A 2076012CE CONT O520 GTSIO520D 17032SO MCAULY3AF34C3AF34C92 GL STARTER CLUTCH BROKEN W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) ON DEPARTURE, ENGINE START RT ENGINE NO ROTATION. PILOT CALL MAINTENANCE. MAINTENANCE FOUND THAT STARTER CLUTCH WAS LOOSE. DISMANTLE, FOUND BAD GEAR ON SHAFT THAT IS RUNNING ON CRANKSHAFT GEAR. ENGINE REMOVED AND SEND TO REPAIR SHOP. 1L72 3O3 O A7CE E7CE 5 CP22EA 20030410002542003041000254NM 2003 4 10 F3LA200300038 120030128A5320 SUPPORT BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON ZEE SUPPORT, RT SIDE OF AFT CARGO COMPARTMENT, FROM STA 727 TO 767. FABRICATED AND INSTALLED REPLACEMENT ZEE SUPPORT PER SRM 53-60-53, 51-40-05, 51-40-02, MM 51-21-41 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030212000752003021200075NM 2003 2 12 NACA20030076 120030211A7997JT8D7B ENGINE BOEING727 727100 1384036NM PWA JT8 JT8D NE #1 SHORTED A NACAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL03930FT4189341893 19387 P657108 DISCREPANCY: ABORTED TAKE OFF DUE TO #1 ENGINE OIL PRESSURE LIGHT ILLUMINATED.CORRECTIVE ACTION: REMOVED MOISTURE FROM OIL DIFFERENTIAL PRESSURE SWITCH CANNON PLUG. 2L73 4F4 FRTA3WE E2EA 20030212000832003021200083NM 2003 2 12 CALA0300032 120030210A5320 STIFFENER BOEING737 7373Q8 1384670NM STA 1104 BENT A CALAK NONE O OTHER ININSP/MAINT 1 SW0914384 26313 INSPECTION FOUND FUSELAGE SECTION 48 HORIZONTAL STIFFENER BENT AT STA 1104, LBL 24. REPAIRED IAW SRM 51-70-11, FIGURE 1. 2L72 4F RTA16WE 20030212000932003021200093NE 2003 2 12 CA030120008 220030116A7310523994 LINE BOEING737 7372Q9 138448MNM PWA JT8 JT8D9A 52048NE FUEL SYS CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) NR 1 ENGINE FUEL LINE FROM FUEL CONTROL UNIT TO FUEL FLOW TRANSMITTER CHAFING ON TOP OF MAIN OIL TANK. FUEL LINE AND OIL TANK REPLACED. 57134.39 HOURS. 54518 CYCLES. 2L72 4F4 F A16WE E2EA 20030212001012003021200101NM 2003 2 12 AWXA200300134 120030123A575465C26601271A SLAT BOEING737 7373G7 1384595NM NO. 1 POSITION DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW148410 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK THE NO. 1 SLAT WAS FOUND DELAMINATED ON THE TRAILING EDGE WEDGE. MAINTENANCE REMOVED AND REPLACED THE NO. 1 SLAT ASSEMBLY IAW BMM 27-81-21. 2L72 4F RTA16WE 20030212001022003021200102NM 2003 2 12 AWXA200300135 120030123A575365C6602217 SLAT BOEING737 7373G7 1384595NM POS NO. 2 DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW148410 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK THE NO. 2 SLAT WAS FOUND DELAMINATED IN SEVERAL PLACES ON THE AFT TRAILING EDGE WEDGE. MAINTENANCE REMOVED AND REPLACED THE NO. 2 SLAT ASSEMBLY IAW BMM 27-81-21. 2L72 4F RTA16WE 20030212001032003021200103NM 2003 2 12 AWXA200300136 120030127A575465C26602218 SLAT BOEING737 7373G7 1384595NM POS NO. 5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW148410 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM FASTENER HOLES ON THE LOWER SURFACE OF THE NO. 5 SLAT. MAINTENANCE REMOVED AND REPLACED THE NO. 5 SLAT ASSEMBLY IAW BMM 27-81-21. 2L72 4F RTA16WE 20030213000072003021300007EA 2003 2 13 CA030122001 120030119A5210600314983 FITTING CNDAIRCL601 CL6012A12 1900303EA GE CF34 CF341A NE PAX DOOR BROKEN W A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 CA (CAN) DOOR TENSION FITTING (UPPER FORWARD) BROKEN IN FLIGHT. 2L72 4F4 FRTA21AE E15NE 20030213000092003021300009EA 2003 2 13 CA030122007 120030120A792128E997 OIL COOLER DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE NR 2 LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) NR 2 OIL COOLER FOUND LEAKING. OIL COOLER REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030213000122003021300012EA 2003 2 13 CA030123003 120030124A5610NP1393221 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED W B EMER. DESCENT D INFLIGHT SEPARATION DEDESCENT 1 CA (CAN) DESCENDING THROUGH APPROXIMATLY 18000 FT, HEARD A THUD, LOOKING TO MY LT, NOTICED THAT THE LT SIDE WINDOW HAD NUMUROUS CRACKS. THERE WERE NO AIR SOUNDS AND THE CABIN PRESSURE WAS NORMAL. QRH PROCEDURE, ADVISE ATC OF THE SITUATION AND REQUESTED LOWER. AS THERE DID NOT SEEM TO BE ANY FURTHER DETERIATION OF THE WINDOW, DID NOT FEEL IT NECESSARY TO DECLAIR AN EMERGENCY, AND MADE A NORMAL APPROACH AND LANDING IN DENVER. R & R LT WINDOW, OPS CHECK & LEAK CHECK GOOD PER AMM. 2L72 4F4 FRTA21EA E15NE 20030213000132003021300013EU 2003 2 13 CA030123004 120030123A63204638303008 BEARING BOLKMS105 BO105CBS 5626008EU GEARBOX SPINNING W K NONE O OTHER ININSP/MAINT 1 CA 1301 (CAN) UNIT RECEIVED FROM THE USA. COLLECTOR GEAR ASSY BALL BEARING PN 4619303083 SPINNING IN BUSHING. INDICATION PICKED UP ON ELECTRICAL CHIP DETECTOR. 1G72 3U NCH3EU 20030213000292003021300029EA 2003 2 13 CA030129002 120030122A3213585926L FITTING DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE FLOAT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 58010L (CAN) INTERGRANULAR CORROSION AT FORWARD FLOAT STRUT ATTACH HOLE ON 585926. LT FITTING FOUND DURING ROUTINE 100 HOUR INSPECTION. FLOAT DATE OF MANUFACTURE 1-11-51 HOUR ON PART UNKNOWN. TTAF 11,951.4 HOURS. 1H71 3R3 R A806 5E1 20030213000412003021300041NM 2003 2 13 DHL2003755003 120030213A7920 SEAL BOEING727 727225 1384077NM A DHLAEO ENGINE SHUTDOWN OTHER O OTHER DEDESCENT 1 SO01755DH 21857 1) DESCENDING THRU 8000' INTO CVG #1 ENGINE LOW OIL PRESSURE LIGHT CAME ON. NOTED OIL QUANTITY AT "0". SHUT DOWN #1 IN FLIGHT.2) FOUND GEAR BOX TO OIL COOLER TUBE LINE LEAKING AT B-NUT. REPLACED RUBBER SEAL, TIGHTENED LINE, AND RAN ENGINE NO LEAKS NOTED IAW M/M 79-20-11. 2L73 4F A3WE 20030213000552003021300055NM 2003 2 13 EVA92012401 120030110A5754 STRINGER DOUG MD11 MD11F 3023600NM LT & RT WING LE CRACKED W QOCFK NONE O OTHER ININSP/MAINT 1 WP0316107 48546 CRACK FOUND ON RT & LT WING FIXED LE STRINGER DOUBLER AT STA XOS 906, INSTALLATION OF INTERNAL DOUBLERS AT STA XOS906 WILL REDUCE THE POTENTIALITY OF CRACK IN THIS SECTION. 2L73 4F RTA22WE 20030213000582003021300058NE 2003 2 13 00073 220030118A7200 ENGINE LEAR 24 24B 5170306CE GE CJ610 CJ6106 30006NE FLAMED OUT E HAEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05233TW 24B221 251210A PILOT REPORTED ENGINE FLAME OUT DURING CLIMB, AT FL400, DECEND AND NORMAL RESTART AT FL220, RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE. WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE COMPLIED WITH FLAME OUT FLOW CHART FROM CJ610 MM SEI 186 FIG 1011 NO DEFECTS NOTED. 2L72 4J4 J A10CE 1E16 20030213000602003021300060EU 2003 2 13 00075 120030129A3260 SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE LT MLG INOPERATIVE E HAEAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW05165TW 65 PILOT REPORTED NO DOWN LOCK INDICATION FOR THE LEFT MAIN GEAR WHILE ON APPROACH, DECLARED EMERGENCY AND LANDED DTW WITHOUT INCIDENT. WILL UPDATE THIS REPORT AFTER MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LT MLG DOWN LOCK SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F4 F A7EU E7EA 20030213000762003021300076EU 2003 2 13 03034306 120030203A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN UNSECURE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27306UE 41020 DURING PREFLIGHT INSPECTION, CREW REPORTED THAT A SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE ELECTRICAL CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTING SECTION. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20030226000122003022600012SW 2003 2 26 HEEA084310 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030226000162003022600016EA 2003 2 26 03057661 120030226A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27661BR 7520 R/H Exterior Emergency Light inoperative. Maintenance personnel relamped emergency light. operational check good. aircraft released for continued service 2L72 4F RTA21EA 20030226000192003022600019SW 2003 2 26 HEEA084312 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030226000232003022600023SW 2003 2 26 HEEA084316 120030211A3212407350301101 FLOAT BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 LEFT FLOAT BAG LEAKING. 1G71 3U O H2SW 20030226000292003022600029SW 2003 2 26 HEEA084319 120030211A2842407362005103 SWITCH BELL 407 407 1182206SW FUEL LOW MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 FUEL LOW LEVEL LIGHT STAYS ON. 1G71 3U O H2SW 20030226000332003022600033SW 2003 2 26 HEEA084322 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 BOOST PUMP LIGHT NOT ILLUMINATING. REPLACED FUEL CELL PRESSURE SWITCH. 1G71 3U O H2SW 20030226000402003022600040SW 2003 2 26 HEEA084329 120030211A2842407362005103 SWITCH BELL 407 407 1182206SW LOW FUEL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 FUEL LOW LEVEL SWITCH WILL NOT GO OUT. 1G71 3U O H2SW 20030226000412003022600041SW 2003 2 26 HEEA084330 120030211A2520407370721105 SEAT BELT BELL 407 407 1182206SW PAX SEAT STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 PASSENGER COMPARTMENT SEAT, SEAT BELT INERTIA REEL STICKING. 1G71 3U O H2SW 20030226000492003022600049SW 2003 2 26 HEEA084338 120030211A7712407375003107 INDICATOR BELL 407 407 1182206SW ENGINE TORQUE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 ENGINE TORQUE INDICATOR INDICATED TORQUE EXCEEDENCE. 1G71 3U O H2SW 20030226000532003022600053SW 2003 2 26 HEEA084342 120030211A6340407375005101 INDICATOR BELL 407 407 1182206SW XMSN OIL PRESS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 GEARBOX OIL PRESSURE INDICATOR SCALE IS BLANK, NO BARS ILLUMINATED. 1G71 3U O H2SW 20030226000632003022600063SW 2003 2 26 HEEA084351 120030211A7697407375012101 WIRE HARNESS BELL 407 407 1182206SW FADEC SYS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 FADEC TO ENGINE WIRE HARNESS OIL SOAKED AND TORN. 1G71 3U O H2SW 20030226000662003022600066SW 2003 2 26 HEEA084353 120030211A2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 SIGNAL COND UNIT MALFUNCTIONED, PRODUCING FUEL LOW LEVEL LIGHTS. 1G71 3U O H2SW 20030226000722003022600072SW 2003 2 26 HEEA084359 120030211A2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL QTY SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 SIGNAL COND UNIT READS 23 POUNDS LOW OF PROPER RANGE AT FULL LEVEL. 1G71 3U O H2SW 20030227000032003022700003SW 2003 2 27 HEEA084360 120030211A6340407375021103 SENSOR BELL 407 407 1182206SW ROTOR RPM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 LOW ROTOR HORN COMES ON BETWEEN IDLE AND FLY POSITIONS ON COLLECTIVE DURING START UP. 1G71 3U O H2SW 20030227000052003022700005SW 2003 2 27 HEEA084362 120030211A6710407375038101 PANEL BELL 407 407 1182206SW COLLECTIVE STICKBROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 START SWITCH LIGHTED PANEL ON COLLECTIVE STICK BROKEN. 1G71 3U O H2SW 20030227000102003022700010CE 2003 2 27 NSVA200300009 120030222A260024412886 FIRE LOOP BEECH 1900 1900D 1154162CE INOPERATIVE A NSVACD ABORTED TAKEOFF RETURN TO BLOCK JLPWARNING INDICATION NO TEST NO WARNING INDICATION TOTAKEOFF 1 EA27240CJ UE40 PWM-On take off roll, LH Fuel Fire-wall S/O Valve light in handle illuminated. Amp Detect (LH Side) fails to illuminate the fire-wall Fuel S/O valve handle. Take off was aborted, aircraft returned to gate. MX found no eveidence of fire. Trouble shooting of system revealed Amp and Loop test portion inop. R&R LH Engine Fire Loop Detector. OP's check good. Aircraft returned to service. 2L72 4T RTA24CE 20030227000122003022700012GL 2003 2 27 HEEA084369 220030211A73135233600 FUEL NOZZLE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 DELAYED LIGHT OFFS. IN SHOP REPAIR. 1G71 3U3 UO H2SW E4CE 20030227000232003022700023 2003 2 27 HEEA084370 420030211A344278806059008 DISPLAY BELL 407 407 1182206SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 DISPLAY IMAGE BOUNCES AND INTERMITTENTLY DISAPPEARS. IN SHOP REPAIR. 1G71 3U O H2SW 20030227000372003022700037SW 2003 2 27 HEEA084374 120030211A6320AAB060RVP1Y1 BYPASS VALVE BELL 407 407 1182206SW GEARBOX OIL SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 MAIN ROTOR GEARBOX OIL SYSTEM BYPASS VALVE INDICATOR BUTTON WILL NOT STAY IN. 1G71 3U O H2SW 20030227000432003022700043 2003 2 27 HEEA084376 420030211A2350AMS44 KNOB BELL 407 407 1182206SW AUDIO CONTROL STRIPPED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 AUDIO CONTROL SELECTOR KNOB STRIPPED. FOUND TRANSMIT SELECTOR SHAFT ON S302 LOOSE. TIGHTENED SHAFT AND REPAIRED. BENCH CHECK GOOD. 1G71 3U O H2SW 20030227000822003022700082 2003 2 27 HEEA084388 420030212A3120 LIGHT BELL 407 407 1182206SW CLOCK INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 02837 53396 CLOCK LIGHT INOPERATIVE. 1G71 3U O H2SW 20030227000892003022700089SW 2003 2 27 HEEA084395 120030212A6510 BEARING BELL 407 407 1182206SW BLOWER ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH PHI0035 53114 NR 2 SHAFT AND BLOWER ASSY HAS A ROUGH BEARING. REPAIRED. 1G71 3U O H2SW 20030227000932003022700093 2003 2 27 HEEA084397 420030212A2340PM212302 SWITCH BELL 407 407 1182206SW CYCLIC STICK STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 CYCLIC STICK TRIGGER ICS/RADIO SWITCH STICKS IN ICS MODE. 1G71 3U O H2SW 20030227001062003022700106SW 2003 2 27 HEEA084412 120030212A6510214040606005 BEARING BELL 214 214ST 1182106SW HANGER ASSY DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03598064324 A1633 28140 HIGH AVMS READING. REPLACED BEARING DUE TO FLAT SPOTS FELT ON ROTATION. REPAIRED. 2G72 4U H10SW 20030227001112003022700111SW 2003 2 27 HEEA084417 120030212A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806676 28140 MAIN BATTERY DISCHARGED, WON'T START AIRCRAFT. 2G72 4U H10SW 20030227001242003022700124 2003 2 27 HEEA084430 420030213A3444066106103 ALTIMETER BELL 206 206L3 1182108SW COCKPIT ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 RADAR ALTIMETER IS ERRATIC. IN SHOP REPAIR. 1G71 3U H2SW 20030227001252003022700125 2003 2 27 HEEA084431 420030213A3452066106200 TRANSPONDER BELL 206 206L3 1182108SW VOR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 WHEN GOING FROM ON THE ALTIMETER UNIT SHUTS OFF. REPLACED SWITCH ASSY. REPAIRED. ALSO REPLACED RESISTOR R477, FACEPLATE. ADJUSTED FREQUENCY. BENCH CHECK GOOD. 1G71 3U H2SW 20030227001292003022700129SW 2003 2 27 HEEA084435 120030213A6710206001526001 BELLCRANK BELL 206 206B3 1181506SW CYCLIC CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032275Y 3626 CYCLIC CONTROL BELLCRANK HAS A WORN PIVOT BEARING. IN SHOP FOR REPAIR. 1G71 3U H2SW 20030228000062003022800006SW 2003 2 28 HEEA084443 120030213A6230 BUSHING BELL 206 206L3 1182108SW IDLER LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 IDLER LINK HAS WORN BUSHINGS. REPAIRED. 1G71 3U H2SW 20030228000072003022800007NM 2003 2 28 SWAA030422 120030223A3250G69617858 BEARING BOEING737 7373H4 1384600NM NLG DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 AFTER TURING TILLER WOULD NOT RETURN TO CENTER. R&R NLG STEERING COLLAR BEARING PER MM. 2L72 4F RTA16WE 20030228000082003022800008NM 2003 2 28 SWAA030424 120030222A33506104781 BATTERY BOEING737 7377H4 1384404NM MID CABIN FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 DURING SCHEDULED RON, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. RESET POWER TO BATTERY PACK PER MM. 2L72 4F RTA16WE 20030228000092003022800009 2003 2 28 SWAA030429 420030221A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030228000162003022800016NM 2003 2 28 SWAA030396 120030219A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29737JW 27869 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20030228000222003022800022NM 2003 2 28 SWAA030382 120030216A2130106223111 MODULE BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 SW29611SW 27697 DECLARED EMERGENCY. CABIN PRESSURIZATION CONTROLLER FAILED, COULD NOT MAINTAIN CABIN PRESSURE. RAPID DECOMPRESSION OCCURRED. FWD F/A'S O2 MASK DID NOT FALL DOWN. PRESSURIZATION CONTROLLER OPERATED PARTIALLY DURING SHORT FINAL. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, OVERHEAD MODULE, AND OUTFLOW VALVE. OPS CHECK GOOD PER MM. 2L72 4F RTA16WE 20030228000312003022800031SW 2003 2 28 HEEA084446 120030213A6220 BEARING BELL 206 206L4 1182110SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03621275889 TR011797 52023 TAIL ROTOR HEAD HAS WORN BEARINGS. REPAIRED. 1G71 3U NCH2SW 20030228000842003022800084WP 2003 2 28 ASAA0380007 120030103A575359100433 VANE DOUG DC9 DC983 3022083WP T/E FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP VANE GOUGED ON LEADING EDGE. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-60-0, 51-70-2, AND 50-14. (M) 2L72 4F RTA6WE 20030228000902003022800090WP 2003 2 28 ASAA0380012 120030103A57535919218508 HINGE FITTING DOUG DC9 DC983 3022083WP T/E FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING HARDWARE AND BEARING BOLT HOLES CORRODED. REMOVED CORROSION AND REPAIRED BOLT HOLES BY INSTALLING BUSHINGS PER EA 5750-01756. (M) 2L72 4F RTA6WE 20030228001002003022800100WP 2003 2 28 ASAA0380014 120030103A53471D0025B CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY TRACK CORRODED AT FS 1212-1322. REPLACED TRACK PER SRM 51-30-01. (M) 2L72 4F RTA6WE 20030228001012003022800101WP 2003 2 28 ASAA0380015 120030103A53219936602 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL IN PUNCTURED AT FS 1117-1155. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030228001082003022800108SW 2003 2 28 HEEA084463 120030213A6730C4264215 SLIDE & SLEEVE BELL 206 206L3 1182108SW SERVO ACTUATOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03 RH0159 SLIDE AND SLEEVE CAUSING EXTERNAL LEAKAGE OF SERVO DURING TESTING. FOUND DEFECTIVE LAPPING. 1G71 3U H2SW 20030228001092003022800109SW 2003 2 28 HEEA084464 120030213A7740 BATTERY BELL 206 206L3 1182108SW COMPUTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 0367 51556 PROCESSOR HAS LOW INTERNAL BATTERY VOLTAGE. 1G71 3U H2SW 20030228001102003022800110SW 2003 2 28 HEEA084465 120030213A7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW E/E BAY MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 PROCESSOR WILL NOT COMMUNICATE WITH LAPTOP. 1G71 3U H2SW 20030228001182003022800118SW 2003 2 28 HEEA084469 120030213A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 MAIN BATTERY WEAK. SHOP FOR REPAIR. 1G71 3U H2SW 20030228001202003022800120WP 2003 2 28 ABXA030091 120030203A5300995823870 SHEAR TIE DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 SHEAR TIE AT F.S. 1019, LONGERON 14 - 15 RIGHT, CRACKED. REPLACED SHEAR TIE IAW DC-9 SSRM K05159. 2L72 4F A6WE 20030303000162003030300016NE 2003 3 3 HEEA084484 220030214A732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENG TORQUE SURGES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 CONTROL UNIT CAUSING TORQUE SURGES WHEN POWER IS APPLIED. IN SHOP FOR REPAIR. 1G72 4U4 U H4SW E22EA 20030213000812003021300081NM 2003 2 13 03FDEA00076 120030127A5230 SKIN BOEING727 727233 138408ANM PWA JT8 JT8D* NE CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 NR 3 CARGO DOOR EXTERIOR SKIN HAS A GOUGE 15 INCHES FROM FWD EDGE 28 INCHES FROM LOWER EDGE. GOUGE ON NR 3 CARGO DOOR EXTERIOR SKIN FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. REMOVED AND REPLACED NR 3 CARGO DOOR EXTERIOR SKIN IAW EA NR7-5230- 68160, FUNCTIONAL CHECKED IAW MM 52-35-051-4 STEP 4, CHECKED GOOD. 2L73 4F4 FRTA3WE E2EA 20030213000822003021300082NM 2003 2 13 03FDEA00078 120030127A2611W462A4220 WIRE BOEING727 727247 138408FNM PWA JT15 JT15D1 52060NE SMOKE DETECTION CHAFED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25233FE 21327 MAIN CARGO SMOKE CONTROL, ACTIVATED IN FLIGHT (FL290) RESET, REACTIVATED, THEN ALARM SILENCED. ZONE 6 LIGHT REMAINED ON. DECLARED AN EMERGENCY AND LANDED. ALARM ACTIVATED FOUR TO SIX MORE TIMES DURING RECOVERY. NO SMOKE OR FUMES WERE DETECTED AT ANYTIME. DUE TO PREVIOUS NOTE ON JAN. 27 ABOUT WIRE BUNDLE RESTING ON SCREW (GROUND STUD) REMOVED WIRE W462-A42-20 BETWEEN D3828 AND D5370. INSPECTED WIRE FOR DEFECTS WITH NO DEFECTS NOTED. INSTALLED NEW WIRE FROM D3828 PIN 12 AND D5370 PIN 11 IAW MFG SWPM 20-10-11 AND 727-200 WDM 26-16-01. CARGO SMOKE TEST NORMAL, IAW B727-200 MM 26-16-001-5. 2L73 4F4 F A3WE E1NE 20030213000862003021300086WP 2003 2 13 ABXA030070 120030123A53403915132501 FITTING DOUG DC9 DC941 302207NWP RT. WHEEL WELL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23957AX 47759 FLOOR BEAM TO KEEL FITTING, STA. 775 WAS CRACKED. REPLACED FITTING, STA. 775, IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 20030213000932003021300093WP 2003 2 13 2003F00071 120030106A29162690039M3 RESERVOIR LKHEED1011 10113851 5265010WP HYD SYTEM FAILED G A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11197AT 193P1082 "B" SYSTEM QUANITY SLOWLY DECREASED, SHUT OFF ENGINE. PUMPS AND SYSTEM CONTINUED TO DECREASE TO .2500 FULL AND HELD STEADY. REMOVED AND REPLACED (B) SYSTEM RESERVIOR ASSEMBLY. 2L73 4F A23WE 20030213000962003021300096NE 2003 2 13 COMA0360093 220030208A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01984CA 7171 FLIGHT 5115 LEFT ENGINE N2 VIBE MESSAGE DURING T/O.COULD NOT DUPLICATE, INSPECTED ENGINE, FOUND NO DEFECTS. 2L72 4F4 FRTA21EA E15NE 20030213001022003021300102WP 2003 2 13 2003F00074 120030102A3350 LIGHT LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE ROW 1-5 INOPERATIVE G K NONE L NO TEST ININSP/MAINT 1 GL11162AT 1220 EGRESS PATHWAY LIGHTING AT ROW 1-5 RIGHT, INOPERATIVE INCLUDING FORWARD GALLEY. REMOVED MOISTURE AND CLEANED CONTACTS ON EGRESS PATHWAY LIGHTING ROW 5 THRU FORWARD GALLEY RIGHT SIDE. 2L73 4F4 F A23WE A12EU 20030213001092003021300109EA 2003 2 13 COMA0360089 120030208A261247259701 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AVIONICS FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01988CA12162 7204 FLIGHT 9488 AFTER T/O ALL FIRE WARNINGS ON.REPLACED THE FIRE AND OVERHEAT CONTROL UNIT. 2L72 4F RTA21EA 20030410002562003041000256NM 2003 4 10 F3LA200300040 120030128A2550 PANEL BOEING737 7373M8 1384615NM CARGO BAY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED RT TRANSITION PANEL FROM STA 867 - 947.3 CORRODED AT NUT PLATE HOLES. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-60-53. FABRICATED AND INSTALLED REPLACEMENT ZEE CHANNEL PER SRM 53-60-53 AND 51-40-02. 2L72 4F RTA16WE 20030410002582003041000258NM 2003 4 10 F3LA200300042 120030128A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED Z-ANGLE AT L-1 THRESHOLD CORRODED FROM STA 312 TO STA 344, OUTBOARD OF MOP SILL. REPLACED Z-CHANNEL PER SRM 51-40-02. 2L72 4F RTA16WE 20030625000722003062500072NM 2003 6 25 F3LA200300045 120030129A5320 PANEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED TRANSITION PANEL IN AFT CARGO COMPARTMENT AT STA 847 - 867, STR 25R, CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-60-53 AND 53-60-15. REPLACED PANEL PER SRM 51-40-02, 53-60-15 AND SOPM 21-40-02. 2L72 4F RTA16WE 20030214000232003021400023CE 2003 2 14 45164012020 120030115A3233 ACTUATOR LEAR 45 45LEAR 5170805CE LT MLG FAILED E J7SAO OTHER N FALSE WARNING LDLANDING 1 SW05428FX1300 1300 164 ON DESCENT, LT MLG INDICATED NO DOWN AND LOCKED INDICATION. AIRCRAFT PERFORMED FLY-BY OF TOWER TO VERIFY GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. LT MLG ACTUATOR REPLACED, AS THE SWITCH IS BUILT INTO THE ACTUATOR AND IS NOT A LRU. SUBSEQUENT GEAR SWINGS SATISFACTORY. AIRCRAFT APPROVED FOR RETURN TO SERVICE 2L72 4F RTT00008WI 20030214000322003021400032WP 2003 2 14 ASAA0280032A 120030104A5310 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, SHEAR TIE CORRODED AT FS 1174. REPLACED SHEAR TIE PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20030214000332003021400033WP 2003 2 14 ASAA0280034A 120030104A2560 FITTING DOUG DC9 DC983 3022083WP FWD ENTRY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE GIRT BAR ATTACH FITTING IS CORRODED. REPLACED FITTING PER SRM 51-30-1. (M) 2L72 4F RTA6WE 20030214000342003021400034WP 2003 2 14 ASAA0280040A 120030105A5230592000335 HINGE DOUG DC9 DC983 3022083WP BARRIER DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY BARRIER DOOR HINGE IS CRACKED. REPLACED HINGE PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20030214000372003021400037NM 2003 2 14 CALA0300041 120030203A5330 BEAR STRAP BOEING737 737524 1384721NM C DOOR CUTOUT CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0937615 27328 INSPECTION FOUND CORROSION AT THE INSIDE SURFACE OF THE BEAR STRAP AT THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR CUTOUT. THE CORROSION WAS REMOVED AND REPAIR WAS PERFORMED IAW ECRA 5331-01121. 2L72 4F RTA16WE 20030303000182003030300018SW 2003 3 3 HEEA084486 120030214A6320412010182101 BEARING BELL 412 412 1182202SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MAIN ROTOR GEARBOX HAS A WORN BEARING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000202003030300020CE 2003 3 3 GLBA2003026 120030226A560010138402517 WINDSHIELD BEECH 1900 1900D 1154162CE A GLBAD RETURN TO BLOCK O OTHER CRCRUISE 1 NM03195GL2085 UE195 #1 WINDSHIELD CRACKED, REPLACED #1 WINDSHIELD 2L72 4T RTA24CE 20030303000292003030300029SW 2003 3 3 HEEA084495 120030214A6220412310400101 ROD END BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 MAIN ROTOR ROD END BEARING IS WORN. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000312003030300031SW 2003 3 3 HEEA084496 120030214A6220412310400101 ROD END BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z3410 36019 MAIN ROTOR ROD END BEARING IS WORN. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000432003030300043SW 2003 3 3 HEEA084502 120030214A33407028521 LIGHT BELL 412 412 1182202SW STROBE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 ANTI COLLISION LIGHT INTERNAL MECHANISM INOPERATIVE. IN SHOP REPAIR. 1G72 4U H4SW 20030303000652003030300065NM 2003 3 3 SWAA030401 120030219A3211656337811 LINK BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED RON, FOUND RT MLG FWD TRUNNION LINK TRUNNION LUGS CORRODED. REMOVED AND REPLACED RT MLG TRUNNION LINK, BEARING AND BEARING BOLT PER MM. 2L72 4F RTA16WE 20030303000762003030300076NM 2003 3 3 SWAA030427 120030224A3350BR2013 TRACK BOEING737 7372T4 1384492NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 EEPLS LENS LOOSE IN FWD CABIN. REMOVED AND REPLACED TRACK SECTION & LENS PER MM. 2L72 4F A16WE 20030303000782003030300078NM 2003 3 3 SWAA030430 120030221A32116541633 TRUNNION PIN BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C3 CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030303000792003030300079 2003 3 3 SWAA030431 420030224A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030303000812003030300081NM 2003 3 3 SWAA030434 120030226A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICES CRACKED (2 EA) AT STR 4L, BS 360 & BS 908. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030303000842003030300084 2003 3 3 SWAA030439 420030225A25656557463 BRACKET BOEING737 7373H4 1384600NM SERVICE DOOR MISINSTALLED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR HOLD DOWN BRACKET INSTALLED BACKWARD. INSTALLED FLOOR BRACKET CORRECTLY PER MM. 2L72 4F RTA16WE 20030303000882003030300088NE 2003 3 3 HEEA084519 220030214A732325249995 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE OSCILLATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 GOVERNOR CAUSING OSCILLATION WHEN POWER IS APPLIED. REPAIRED. 1G72 4U4 U H4SW E22EA 20030303001052003030300105NM 2003 3 3 0300336744 120030227A5412 BULKHEAD BOEING747 747212F NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01644NW 24177 During "H" check found crack in #4 pylon aft torque bulkhead chord at the top fastener hole common to the lower spar fitting. Repaired per EA 67-165046. 2L74 4F RTA20WE 20030303001062003030300106NM 2003 3 3 0300346744 120030227A5412 WEB BOEING747 747212F NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01644NW 644NW During "H" check found cracks in #4 pylon rear engine mount outboard forward and aft frame webs. Repaired per EA 67-165042. 2L74 4F RTA20WE 20030303001082003030300108SO 2003 3 3 C2XA03CL057 120030301A335014532843401 CONTROL MODULE EMB 145 EMB145LR 3260212SO CABIN INTERMITTENT A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2714902 145496 CLE FLIGHT#2865 THE CREW REPORTED THE EMERGENCY LIGHTS IN THE CABIN WOULD INTERMITTENTLY ILLUMINATE IN THE ARM POSITION.MAINTENANCE INSPECTED AND REPLACED RELAY KO275 AND THE OVERHEAD LIGHT CONTROL MODULE.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030214000472003021400047NM 2003 2 14 P5CA0300755 120030130A5300NONE SKIN BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND ON F/S 360 RH BWTN STR 8 TO STR 10. DAMAGE AREA TRIMMED OUT REINFORCED WITH SEGMENT AND SPLICE PER SRM 53-10-04, 51-10-02 & 51-30-02. 2L74 4F A20WE 20030214000562003021400056WP 2003 2 14 ASAA0380039 120030105A53219936600 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY FLOOR PANEL PUNCTURED AT FS 427-465. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030214000592003021400059WP 2003 2 14 ASAA0380042 120030105A53219936599505 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL IS PUNCTURED. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030214000602003021400060WP 2003 2 14 ABXA030004 120030107A33105956888503 CONTROL PANEL DOUG DC9 DC932 3022066WP PWA JT8 JT8D NE COCKPIT DEFECTIVE A ABXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23903AX 47427 AT CRUISE, SAW SMOKE COMING OUT AROUND CENTER INSTRUMENT AND PEDESTAL LIGHT PANEL. TURNED LIGHTS OFF. DECLARED EMERGENCY, RAN CHECKLIST AND RETURNED AIRPORT, AFTER SMOKE STOPPED. ISOLATED BURNING ODOR TO CENTER INSTRUMENT PANEL LIGHTING CONTROL PANEL. REPLACED PANEL IAW AMM AND PERFORMED VISUAL INSPECTION OF WIRING IN SURROUNDING AREA. NO WIRING DEFECTS NOTED. REPLACED THE FOLLOWING CIRCUIT BREAKERS AS PRECAUTION: B1-306, B1-307, B1-308, B1-309 AND B1-271. REF. W.D. NR 33-13-03, 33-13-06 AND 33-14-02. ALL CENTER INSTRUMENT PANEL AND PEDESTAL LIGHTING CHECKED GOOD. NO SMOKE OR ODOR PRESENT. REPLACED ALL CIRCUIT BREAKERS IAW AMM. 2L72 4F4 F A6WE E2EA 20030214000652003021400065WP 2003 2 14 ASAA0380046 120030105A532199366023 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL UPPER SKIN IS DISBONDED. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030214000772003021400077WP 2003 2 14 ASAA0380050 120030105A575359306132 ACCESS PANEL DOUG DC9 DC983 3022083WP T/E FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING FLAP FLEX JOINT UPPER ACCESS PANEL UPPER SURFACE IS GOUGED. REPAIRED PANEL PER SRM 51-70-1. (M) 2L72 4F RTA6WE 20030214000792003021400079NE 2003 2 14 ARWA20030103 220030119A7250UL19659 BLADE LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B40254555NE COMPRESSOR DAMAGED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO19307GB 193U1131 14613 NR 3 ENGINE AT 370 FEET, BOTH CHANNEL A AND B 2.7 CAUTION LIGHT ON. SHUTDOWN ENGINE 1200Z. FEELING THE VIBRATION ON THE FLOOR. REMOVED AND INSPECTED MASTER AND INTERNAL GEAR-BOX MAGNETIC CHIP DETECTOR AND OIL FILTERS IAW MM. NO EVIDENCE OF INTERNAL FAILURE. VISUALLY INSPECTED AIR INTAKE, LP COMPRESSOR AND EXHAUST FOR EVIDENCE OF FOD OR DEBRIS, NO EVIDENCE OF DAMAGE. PERFORMED BOROSCOPE INSPECTION. LP ROTOR STAGE 7, HP ROTOR 6 STAGE AND HPT BLADES REAR, NO DAMAGE FOUND. REMOVED AND REPLACED NR 3 ENGINE NR 31 L/P. BLADE IAW MM. PREFORMED VIBRATION SURVEY AND FOUND LEVEL ON NORMAL RANGE IAW MM. 2L73 4F4 F A23WE E12EU 20030214001022003021400102EU 2003 2 14 0301282 120030128A6120 CONTROLLER SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE AUTOCOARSEN INOPERATIVE A UHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NE03152CQ 152 FLIGHT NR 4511 DID NOT GET THE AUTOCOARSEN ARM LIGHT DURING TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. A/C WAS FERRIED TO PIT AND TAKEN OUT OF SERVICE AT 1200. A/C ARRIVED IN PIT AT 1520. PIT MECHANIC REMOVED AND REPLACED AUTOCOARSEN STATUS LIGHT, PERFORMED OPERATIONAL CHECK OF AUTOCOARSENING SYSTEM. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030625000832003062500083NM 2003 6 25 F3LA200300056 120030201A5320 INTERCOSTAL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT LBL 11, BETWEEN STA 294.5 AND STA 312, HAS A CORRODED ANCHOR FIXTURE WITH BOLT SHANK IN IT. REPLACED INTERCOSTAL PER SRM 51-40-2. 2L72 4F RTA16WE 20030214001372003021400137SO 2003 2 14 LR7A03006 120030202A53123391499R SKIN PANEL LKHEED382 382G 526414USO FS 617 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 581 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3202 FOUND RMLG WHEEL WELL FS 617 AFT BULKHEAD SKIN CRACKED .5 IN. AT CENTER OF PANEL RBL 69, WL 184.REPLACED SKIN PANEL IAW SRM SMP 583 53-40-02 AND DWG 339149. NR 0040. 2H74 4T A1SO 20030217000012003021700001WP 2003 2 17 IXXA0300011O 120030204A7100JT3D ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7A 52039NE #2 WORN A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11867BX361264292 46049 671062 AFTER DEPARTURE FROM KBFI ENROUTE TO KPDX CREW NOTICED OIL QUANTITY IN NUMBER 2 ENGINE DROPPED ABNORMALLY. AS A PRECAUTIONARY MEASURE THE #2 ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO KBFI FOR AN UNEVENTFUL LANDING. POSITIVE OIL PRESSURE WAS MAINTAINED THRU OUT FLIGHT. AIRCRAFT DEPARTED KBFI ON 2/5/2003 UNDER A FERRY PERMIT TO KTOL, AIRCRAFT MADE AN UNEVENTFUL LANDING IN KTOL.REPLACED ENGINE AND OPERATION CHECKS GOOD ALL WORK COMPLETED PER APPLICABLE MANUALS AND AIRCRAFT RETURNED TO SERVICE 2L74 4F4 F 4A25 1E8 20030217000062003021700006WP 2003 2 17 CALA0300048 120030215A5313 LONGERON DOUG DC9 DC982 3022082WP STA 1418 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0915841 49581 INSPECTION FOUND A 2" CRACK IN LONGERON 2R AT STA 1418. A SECTION OF LONGERON WAS SPLICED IN IAW ECRA 5311-01132. 2L72 4F A6WE 20030217000152003021700015WP 2003 2 17 ARWA20030205 120030213A243051508000 GCU DOUG DC8 DC863F 302198FWP NR 2 GEN FAILED A ARWAH DEACTIVATE SYST/CIRCUITS O OTHER TXTAXI/GRND HDL 1 SO19784AL 46135 WHEN GENERATORS ARE PARARELLED NR 2 GENERATOR UNPARELLED, NO VOLTS, NO FREQS AND LOAD. REMOVED AND REPLACED GENERATOR CONTROL UNIT (GCU) IAW MM 24-20-6. OPERATIONAL CHECK NORMAL IAW MM 24-20-1. 2L74 4F 4A25 20030218000112003021800011NM 2003 2 18 03FDEA00104 120030203A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 N01056) CORROSION AT BS 1070, WL 208, RBL 30 UPPER SURFACE ON FLOORBEAM. FOUND PREVIOUS REPAIR TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED NEW REPAIR ANGLE AND FILLER FROM BAC 490-2883 7075T6 .090" LOT NR 179279 AND BAC 1505-100880, LOT NR458274. INSTALLED REPAIR PARTS, ALL DONE IAW SRM 53-10-8 AND 51-30-2. 2L73 4F4 FRTA3WE E2EA 20030218000152003021800015NM 2003 2 18 03FDEA00110 120030205A5310 SUPPORT ANGLE BOEING727 727200 138407ENM PWA JT8 JT8D NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION A/C BAY, STA 740, LBL 12, WL 140 AT LOWER FRAME OF BULKHEAD. REMOVED AND REPLACED LOWER SUPPORT ANGLE BS 740 LBL 12 WL 140 IAW SRM 51-30-2 AND 51-20-4. 2L73 4F4 FRTA3WE E2EA 20030218000172003021800017NM 2003 2 18 03FDEA00112 120030206A5511ALC81782 RIB DOUG MD11 MD11F 3023600NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT HORIZONTAL STAB AT STA XE 122.594, FWD RIB, ONE HORIZONTAL MACHINED ANGLE FOUND A CRACKED, LINE MEASURED APPROX. 1 INCH IN LENGTH. HORIZONTAL STABILIZER UPPER FORWARD RIB XE 122.594 REPAIRED AS PER FEDEX EA 1-5510-63146 - STABILIZERS - HORIZONTAL STABILIZER - UPPER FORWARD RIB CRACKED AT XE =122.594 2L73 4F RTA22WE 20030218000192003021800019EU 2003 2 18 03FDEA00114 120030205A7920 FITTING AIRBUS310 A310222 3930315EU PWA JT9 JT9D3 52050NE OIL FILTER HOUSELOOSE A FDEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO25417FE 333 NR 1 ENGINE SHUT DOWN ON DESCENT DUE TO ZERO OIL QUANTITY AND FLUCTUATING OIL PRESSURE. ECAM ADVISORY ENGINE NR 1 OIL QTY LOW ADVISORY CAME ON AT LEVEL OFF ALT OF FL300. THE NR 1 THROTTLE WAS REDUCED TO IDLE FOR REMAINDER OF FLT UNTIL THE OIL PRESSURE FLUCTUATED IN THE DESCENT. ENGINE OIL LOW PRESSURE CHECK LIST AND PROCEDURE WITH SINGLE ENGINE OPERATION WERE ACCOMPLISHED. ATT CPH MTC. PLS PERFORM ENGINE WIND MILLING INSPECTION IAW A310-200 M/M BUS DESK FACT LEAK TRACED TO LOOSE FITTING ON ENGINE OIL FILTER HOUSING AT OIL FILTER PX DIFFERENTIAL SWITCH RESTRICTOR. INSERT FOUND DAMAGED. REPAIR CARRIED IAW MM. 2L72 4F4 FRTA35EU E20EA 20030218000322003021800032EU 2003 2 18 AWXA200300007 120030102A3350321430 BATTERY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28631AW 077 DURING INSPECTION RECEIVED A (CIDS) FAULT FOR EMERGENCY EXIT LIGHT BATTERY AT L-1 DOOR. MAINTENANCE REMOVED AND REPLACED THE FORWARD LT EMERGENCY LIGHT BATTERY IAW AMM, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030218000332003021800033EU 2003 2 18 AWXA200300008 120030103A3230 UPLOCK SENSOR AIRBUS320 A320232 3930326EU MLG OUT OF ADJUST A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28639AW 471 AIR TURN BACK AFTER TAKEOFF EN ROUTE RETRACTED LANDING GEAR, NLG REMAINED DOWN. PERFORMED ECAM PROCEDURES, CYCLED LANDING GEAR; NO CHANGE, NLG REMAINED DOWN AND LOCKED, MAIN GEAR INDICATED UNSAFE. RECYCLED GEAR, ALL GEAR ASSY RETRACTED, BUT LT, RT MAIN GEAR DOORS REMAINED OPEN. LWRD GEAR AND TURNED BACK. MAINT REMOVED AND REPLACED LANDING GEAR SAFETY VALVE IAW AMM, NLG UPLOCK ASSY IAW T/C R4N32307. CHECKED ADJUSTMENT OF PROXIMITY SENSORS 18GA AND 19GA; IAW AMM. FUNCTIONAL TEST OF SAFETY VALVE IAW AMM, AND EXTENSION AND RETRACTION TEST IAW AMM, ALL CHECKS GOOD. 2L72 4F RTA28NM 20030218000372003021800037 2003 2 18 AWXA200300015 420030106A256560592101 BOTTLE AIRBUS320 A320231 3930325EU ESCAPE SLIDE DISCHARGED A AWXAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION NRNOT REPORTED 1 WP28620AW409997108 052 FLIGHT CREW REPORTED A RED CAUTION LIGHT ON CIDS PANEL. MAINTENANCE PLACED LT OVERWING SLIDE ON MEL 25-60-05, COND. 2 SLIDE BOTTLE PRESSURE INOPERATIVE. SLIDE BOTTLE PRESSURE WAS VERIFIED IN THE GREEN AND AIRCRAFT DEPARTED AS SCHEDULED. UPON RETURN TO PHX MAINTENANCE REMOVED AND REPLACED THE LT OVERWING SLIDE BOTTLE IAW AMM 25-62-46-401, OPERATIONAL CHECK WAS GOOD. **SUPP** VENDOR TEARDOWN OF RESERVOIR ASSEMBLY S/N C0249 CONFIRMED FAILURE OF UNIT. REPLACED 7 EACH O-RING SEALS, BACK UP RING PN 1002-0030-008, SEAT BALL P/N B14246-1, FUSIBLE PLUG PN B13984-3, PULLEY P/N B42013-1, AND CYLINDER P/N 64236-3. 2L72 4F RTA28NM 20030218000392003021800039NM 2003 2 18 AWXA200300018 120030108A3350321430 BATTERY AIRBUSA319 A319132 3930340NM CABIN INOPERATIVE A AWXAO OTHER O OTHER CLCLIMB 1 WP28831AW 1576 DURING CLIMB, THE EMERGENCY EXIT SIGN LOCATED AT OVERHEAD AISLE MID-CABIN POSITION BECAME INOPERATIVE, FOLLOWED BY THE EXIT SIGN AT THE R/H OVER WING EXIT. THE AIRCRAFT CABIN R/H SIDE EMERGENCY ESCAPE PATH LIGHTING WAS ALSO INTERMITTENTLY ILLUMINATING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE R/H MID CABIN EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT 12WL IAW AMM TASK 33-51-38-400-002; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030218000412003021800041GL 2003 2 18 C2XA03CL006 220030107A731423076368 PUMP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENG FUEL READS HIGH A C2XAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2748901 145501 CAE311927 FLIGHT NR 2678, THE CREW REPORTED AT 28000 FT, THE AIRCRAFT BEGAN TO SHAKE AND THE NR 1 ENGINE N1 EXCEEDED 103 PERCENT. THE NR 1 ITT WAS AT LEAST 940 DEGRESS. THE CAPTAIN REDUCED THRUST TO IDLE WITH NO RESPONSE FROM THE ENGINE. THE CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 FUEL PUMP METERING UNIT AND BOTH 1A AND 1B FADEC'S. OPERATIONAL CHECKS WERE GOOD ON THE GROUND.THE AIRCRAFT WAS TEST FLOWN WITH NO DISCREPANCIES. 1A FADEC P/N 23074001 S/N BX160136 1B FADEC P/N 23074001 S/N BX160138 2L72 4T4 FRTT00011ATTE6CH 20030218000672003021800067NM 2003 2 18 AALA20021901 120030102A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21352AA 24033 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR AT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030218000692003021800069NM 2003 2 18 AALA20030015 120030103A3350 TERMINAL BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21380AN 25449 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT FORWARD OF M-2 LAVATORY INOPERATIVE. REPLACED BROKEN TERMINAL AT EMERGENCY EXIT CEILING LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030218000822003021800082NM 2003 2 18 AMTA200300138 120030125A2822609891002 PUMP BOEING757 75723N 1384973NM CENTER TANK MALFUNCTIONED A AMTAK NONE J WARNING INDICATION CRCRUISE 1 GL11525AT 30548 FLT 151 - RT CTR BOOST PUMP LOW PRESSURE LIGHT. EICAS MESSAGE CENTER RT FUEL PUMP DISPLAYED. REMOVED AND REPLACED RT CENTER OVERRIDE PUMP PER M/M CHAP 28-22-03-4. OPS CHECK GOOD, LEAK CHECK GOOD. (M) 2L72 4F RTA2NM 20030218001152003021800115NM 2003 2 18 VNAA0302011 120030213A28002193361 TRANSFER PUMP DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LH FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07432JS20336 3045 ENROUTE, THE CREW NOTICED A FUEL IMBALANCE AND HAD A LEFT HAND FEEDER TANK LOW CAS MESSAGE AND FUEL ASSYMETRY CAS MESSAGE THEN DIVERTED TO BDL. ON FINAL THE MESSAGES CLEARED. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND FUEL JET TRANSFER PUMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030218001562003021800156NM 2003 2 18 HNAA0300009 120030212A2910997305 VALVE DHAV DHC8 DHC8102 2809003NM #2 NACELLE DEFECTIVE A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07908HA4601546015 015 When landing gear selected up, the gear did not retract. The #2 hydraulic ISO valve caution light illuminated, roll spoiler outbd hydraulic caution light and nose gear steering caution light illuminated intermittantly. Nose steering did not work. Cleaned and inspected low level pressure switch on #2 hydraulic reservior. Ground ran aircraft, all systems on #2 hydraulic system, op's checked good.After take off gear selected up, gear went up but stayed unsafe- three red lights. #2 hydraulic ISO annunciator light illuminated and roll spoiler outboard hydraulic. Selected gear down - mains extended but not nose gear. Performed alternate extension. Ferried aircraft to ORF. Replaced #2 rudder ISO valve. O 2H72 4T RTA13NM 20030218001712003021800171NM 2003 2 18 QXEA0300163 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LIGHT PITTING AT STATION 265 IN NR 4 SEAT TRACK. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001812003021800181NM 2003 2 18 QXEA0300173 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 2 SEAT TRACK HAS LIGHT PITTING AT STATION 468. REPAIRED IAW RD 8-53-1342, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001852003021800185NM 2003 2 18 QXEA0300177 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 2 SEAT TRACK HAS LIGHT PITTING AT STATION 438. REPAIRED IAW RD 8-53-1352, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001952003021800195NM 2003 2 18 SWAA030346 120030211A53116545776 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 927, WL 168 AND BL 0. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030218001972003021800197NM 2003 2 18 SWAA030332 120030211A33506574550 LENS BOEING737 7377H4 1384404NM AFT SVC DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 AFT SVC DOOR EMERGENCY EVAC SLIDE SIDE LIGHT LENS DAMAGED. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030218002022003021800202NM 2003 2 18 SWAA030339 120030209A551065C25727 SKIN BOEING737 7373G7 1384595NM RT HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR FWD OF INBD BALANCE BAY. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030218002102003021800210 2003 2 18 SWAA030299 420030208A25656557463 BRACKET BOEING737 7373H4 1384600NM FWD SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 FWD SVC DOOR EMERGENCY EVAC SLIDE ATTACH BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20030218002152003021800215NM 2003 2 18 SWAA030308 120030209A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D AND BS 727E, ABOVE STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030218002192003021800219NM 2003 2 18 SWAA030317 120030208A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED PM CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 2, NR 3 AND NR 4 HINGE HARDWARE AND BUSHINGS PER SWA SI AND MM. 2L72 4F RTA16WE 20030218002302003021800230NM 2003 2 18 SWAA030260 120030131A27506573271 TORQUE TUBE BOEING737 7373H4 1384600NM LT WING T/E BROKEN A SWAAK NONE O OTHER APAPPROACH 1 SW29314SW 23336 DURING APPROACH, RT T/E FLAP POS IND WOULD NOT GO PAST 25 DEG'S. REMOVED AND REPLACED LEFT INBD T/E FLAP TORQUE TUBE PER MM. 2L72 4F RTA16WE 20030218002312003021800231NM 2003 2 18 SWAA030261 120030203A53126546568 WEB BOEING737 7372H4 138448CNM AFT FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED SPECIAL VISIT, FOUND BS 1016 BULKHEAD WEB CRACKED AT 11, 12 AND 1 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA. 2L72 4F A16WE 20030218002332003021800233NM 2003 2 18 SWAA030263 120030203A53116558280 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030218002382003021800238 2003 2 18 SWAA030269 420030203A2565D31354 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29725SW 27857 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030218002472003021800247NM 2003 2 18 SWAA030243 120030130A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED (4 EA) AT ROW NR 11, ROW NR 12, ROW NR 20 AND ROW NR 21. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030218002542003021800254 2003 2 18 SWAA030256 420030201A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030218002552003021800255NM 2003 2 18 SWAA030258 120030202A530065C27314 TIE CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND TIE CLIPS CRACKED (2 EA) AT STR 4L, BS 727B AND BS 807. REMOVED AND REPLACED TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030218002742003021800274SO 2003 2 18 C2XA03SH005 120030218A530014522459003 SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV-DURING C CHECK THE CENTER FLOOR BEAM RAMP ANGLE SUPPORT WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030219000032003021900003CE 2003 2 19 C8F2003F00000 120030203A323050410032 BELLCRANK CESSNA402 402A 207590MCE CONT O520 TSIO520E 17040SO RT MLG CRACKED E C8FAO OTHER O OTHER TXTAXI/GRND HDL 1 WP134576Q 402A0076 275AA8A AFTER TAKE OFF FROM HNL PILOT NOTICED DECREASING MANIFOLD PRESSURE ON RT ENGINE, AND DECIDED TO RETURN TO HNL. DURING LANDING APPROACH PILOT NOTICED AN UNSAFE RT GEAR LIGHT, ATTEMPT WAS MADE TO RECYCLE LANDING GEAR BUT WAS UNSUCCESSFUL. HE THEN TRIED THE EMERGENCY HAND CRANK THAT ALSO FAILED TO CORRECT THE RT MAIN LANDING GEAR UNSAFE PROBLEM. EMERGENCY PROCEDURES WERE CARRIED OUT AND UPON LANDING THE RT MAIN LANDING GEAR COLLAPSED ON ROLL OUT. AC WAS THEN SECURED BY MAINT AND TOWED, WERE IT WAS FOUND THAT THE RT RETRACT BELLCRANK WAS FOUND TO BE CRACKED AND SEPARATED FROM REST OF ASSEMBLY. NOTICED THAT BOLT TO BE SHEARED AS WELL. 1L72 3O3 O A7CE E8CE 20030219000122003021900012SO 2003 2 19 RAQ2003F00000 220030103A852020428 BEARING BOEING75 JONES75 1380105CE CONT R670 W670* 17016SO CRANKCASE FAILED E RAQRO OTHER O OTHER NRNOT REPORTED 1 SW15748BJ493 AR42 6682 REAR MAIN BEARING FAILED IN ENGINE BY THE BEARING CAGES DISINTEGRATE. UPON DISASSEMBLY IT WAS FOUND THAT THE BEARING, ONE IGNITION GEAR, AND THE GENERATOR DRIVE PINION WERE HIGHLY MAGNETIZED. THE ENGINE IS EQUIPPED WITH AN ALTERNATOR IN PLACE OF THE ORIGINAL GENERATOR. WE HAVE SEEN SEVERAL OTHER INSTANCES OF HIGHLY MAGNETIZED PARTS IN THE ACCESSORY CASES OF ENGINES FITTED WITH ALTERNATORS. IS THE ALTERNATOR CAUSING MAGNETISM WITHIN THE BEARING AND CAUSING IT TO ATTRACT ALL FERROUS PARTICLES, THIS LEADING TO EARLY FAILURE. 1Q71 3R3 RNCA743 E162 20030219000222003021900022EU 2003 2 19 YT22003F00001 120030125A6410355A09103601 BEARING SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED A YT2RO OTHER O OTHER NRNOT REPORTED 1 WP01794WC 2122 TAIL ROTOR LAMINATED BEARINGS CRACKED. 1G71 3U3 U H9EU E19EU 20030219000282003021900028NM 2003 2 19 2003UALA00163 120030131A5754114W41101 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLAT #1 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 TRAILING EDGE WEDGE, SLAT #1A, DAMAGED IN TRANSIT. MAJOR REPAIR ACCOMPLISHED. WING SLAT #1A REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030219000302003021900030NM 2003 2 19 2003UALA00171 120030211A5230 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE CUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 FWD CARGO DOOR, AFT LOWER CORNER, FOUND DAMAGE TO DOOR OUTER SKIN. 3-16 BY 1-4 INCH V CUT IN DOOR SKIN. MAJOR REPAIR ACCOMPLISHED. BELENDED OUT DAMAGE BY MANUFACTURING DOUBLER. 2L72 4F4 FRTA2NM E17NE 20030219000342003021900034CE 2003 2 19 CGO2003F00002 120030116A322290140634A CLAMP BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE RT MLG STRUT CHAFED B CGORK NONE O OTHER ININSP/MAINT 1 GL03743TA RK271 INVESTIGATED COMPLAINT OF UNLOCKED GEAR INDICATION AFTER GEAR RETRACTION. FOUND RIGHT MAIN LANDING GEAR NOT FULLY LOCKING IN RETRACTED POSITION DUE TO INTERFERENCE BETWEEN STRUT ASSEMBLY BRAKE LINE CLAMP AND ADJACENT STRUCTURE. LANDING GEAR RETRACT TESTS SATISFACTORY AFTER REPOSITIONING CLAMP. RECENT MAINTENANCE HISTORY NOT SUPPLIED. BE 400A MLG WHEEL WELLS ARE RELATIVELY TIGHT FIT, AND WHENEVER ANY MAINTENANCE IS PERFORMED AROUND STRUT, A RETRACT SYSTEM TEST SHOULD BE PERFORMED BEFORE RETURNING AIRCRAFT TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20030219000412003021900041WP 2003 2 19 MWEA030100 120030214A5320991224319 SHEAR TIE DOUG DC9 DC981 3022081WP STA 1361 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 SHEAR TIE STATION 1361 BETWEEN LONGERON 12 & 13 RIGHT REQUIRES REPLACEMENT DUE TO SKIN REPAIR. -- FABRICATED AND INSTALLED SHEAR TIE AND ANGLE. 2L72 4F A6WE 20030219000422003021900042CE 2003 2 19 CJP2003F00000 120030120A301026190361 GASKET LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP WING HEAT DUCT FAILED E CJPAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM03925DM294 486 FLIGHT CREW AND PASSENGER NOTED BURNING ODOR AND HAZE IN CABIN. AIRCRAFT DIVERTED TO ALTERNATE AIRPORT FOR MAINTENANCE. A LEAK WAS FOUND IN BLEED AIR CROSS OVER DUCT FOR LEFT WING AND STABILIZER HEAT. A GASKET HAD FAILED ON THE CROSSOVER DUCT CONNECTION TO THE CABIN HEAT DUCT. 2L72 4F4 F A10CE E6WE 20030219000512003021900051WP 2003 2 19 MWEA030077 120030217A531299155621 CLIP DOUG DC9 DC981 3022081WP APB CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 REMOVED AFT PRESSURE BULKHEAD ASSEMBLY LOCATED AT AIRCRAFT CENTERLINE OVER VENTRAL DOOR JAMB FRAME STATION 1338 TO FACILITATE OTHER MAINTENANCE. -- FOUND CLIP AND WEB CRACKED AND CLIP BENT LOCATED AND DRILLED AND INSTALLED STIFFENER AND NEW WEB AND INSTALLED CLIP AND FORMER. 2L72 4F A6WE 20030219000552003021900055EU 2003 2 19 R142003F00001 120030113A575325WF217 STRUCTURE HWKSLYDH125 DH125400A 4230140EU LT FLAP FAILED B R14RO OTHER O OTHER NRNOT REPORTED 1 EA17284DB13678 NA715 LEFT FLAP FAILURE 41 INCHES OUTBOARD OF INBOARD END. FLAP WAS IAW HS 125 MSB 27-112-2426, MOD 252426 WHICH STRENGTHENS FLAP FOR LANDING IN HEAVY WATER/ SLUSH CONDITIONS. AIRCRAFT ARRIVED 1/1/2003 WITH HEAVY PRECIP PRIOR TO LANDING. 2L72 4J A3EU 20030219000642003021900064WP 2003 2 19 MWEA030075 120030212A533029525251 DOUBLER DOUG DC9 DC981 3022081WP STA 1287 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 RIGHT FUSELAGE SKIN AT STATION 1287 HAS A GOUGE. -- CUT OUT DAMAGED SECTION FABRICATED AND INSTALLED REPAIR DOUBLER, FABRICATED AND INSTALLED 2 EACH STRAPS AND SHEAR TIE. AND INSTALLED 1 EACH SPECIAL ORDER FASTENERS. 2L72 4F A6WE 20030219000672003021900067WP 2003 2 19 MWEA030088 120030212A53209915558253 FORMER DOUG DC9 DC981 3022081WP STA Z63.5 BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 SECOND FORMER DOWN FROM TOP STATION Z63.5 IS BENT. -- LOCATED AND DRILLED AND INSTALLED NEW FORMER AND TEE. 2L72 4F A6WE 20030219000732003021900073NE 2003 2 19 TSAA0379008 220030125A7200JT8D9A ENGINE BOEING737 737230 1384401NM PWA JT8 JT8D9A 52048NE NR 1 FAILED A TSAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP13821AL48174 23155 P656093B AT CRUISE ALTITUDE, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AND WOULD NOT GO OUT AT REDUCED THRUST SETTING. THE CREW SHUTDOWN THE NR 1 ENGINE AND LANDED AT HNL WITH NO FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED THE NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20030219000772003021900077NM 2003 2 19 SWAA030257 120030201A33506104781 BALLAST BOEING737 7377H4 1384404NM CABIN FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2L72 4F RTA16WE 20030219000822003021900082NM 2003 2 19 SWAA030268 120030203A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SPECIAL VISIT, FOUND 4 EA STRINGER CLIPS CRACKED, BS 685, BS 616, BS 639, STR 4R AND BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030219000872003021900087 2003 2 19 SWAA030304 420030209A2565D31591 SLIDE BOEING737 7373Q8 1384670NM ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030218001832003021800183NM 2003 2 18 QXEA0300175 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 1 SEAT TRACK HAS LIGHT PITTING AT STATION 360. REPAIRED IAW RD 8-53-1342, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001862003021800186NM 2003 2 18 QXEA0300178 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 6 SEAT TRACK HAS SCRATCHES AT STATION 531. REPAIRED IAW RD 8-53-4936, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001902003021800190NM 2003 2 18 QXEA0300182 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 5 SEAT TRACK HAS SCRATCHES AT STATION 470-482. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001942003021800194NM 2003 2 18 SWAA030345 120030212A53116935365 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 19R AND STR 20R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030218001992003021800199NM 2003 2 18 SWAA030336 120030211A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 21L, BS 941 AND BS 986. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030218002042003021800204NM 2003 2 18 SWAA030324 120030209A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030218002052003021800205 2003 2 18 SWAA030326 420030210A2565D31354 SLIDE BOEING737 7377H4 1384404NM FWD SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29427WN 29831 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REMOVED AND REPLACED SLIDE GIRT ASSY PER MM. 2L72 4F RTA16WE 20030218002092003021800209 2003 2 18 SWAA030297 420030208A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030218002142003021800214NM 2003 2 18 SWAA030307 120030208A531365C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030218002202003021800220NM 2003 2 18 SWAA030318 120030207A5315BACB1509 FLOORBEAM BOEING737 7373G7 1384595NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 770 AT LBL 13, BS 860 AT RBL 8, BS 860 AT LBL 3, BS 847 AT LBL 6 AND BS 813 AT LBL 3. REPAIRED FLOORBEAMS PER SWA ER. 2L72 4F RTA16WE 20030218002212003021800221NM 2003 2 18 SWAA030320 120030207A3220R374 RECEPTACLE BOEING737 7373T0 1384582NM E/E COMP FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29684WN 23941 DIVERSION, AFTER DEPARTURE NLG FAILED TO RETRACT, GEAR HANDLE WAS CYCLED, NLG GREEN AND RED LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED RECEPTACLE FOR NOSE GEAR LATCHING RELAY PER MM. 2L72 4F RTA16WE 20030218002222003021800222NE 2003 2 18 SWAA030321 220030206A72306522441 MANIFOLD BOEING737 7372H4 138448CNM JT8 JT8D9A 52048NE NR 2 ENGINE RUPTURED A SWAAAD UNSCHED LANDING RETURN TO BLOCK JM WARNING INDICATION OVER TEMP ININSP/MAINT 1 SW29081SW 22730 707374 AIR TURNBACK, DURING DEPARTURE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. FOUND 13TH STAGE LT MANIFOLD RUPTURED. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 F A16WE E2EA 20030218002342003021800234NM 2003 2 18 SWAA030264 120030203A53136551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5L. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030218002362003021800236NM 2003 2 18 SWAA030266 120030203A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 5R CRACKED AT BS 827+12. REPAIRED STRINGER PER SRM 2L72 4F RTA16WE 20030218002372003021800237 2003 2 18 SWAA030267 420030203A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030219000912003021900091NM 2003 2 19 SWAA030311A 120030207A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030219001032003021900103NM 2003 2 19 SWAA030330 120030210A53126516300 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, WL 235 AND BL 11, LT AND RT. REPAIRED BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20030219001152003021900115NM 2003 2 19 SWAA030341 120030212A253046402015 COFFEEMAKER BOEING737 7373H4 1384600NM AFT GALLEY OVERHEATED A SWAAK NONE MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29347SW 24374 OVERHEAT FUME ODOR AT AFT COFFEE MAKER. FOUND, AFT COFFEE MAKER OVERHEATED AND TRIPPED C/B. REMOVED AND REPLACED COFFEE MAKER PER MM. 2L72 4F RTA16WE 20030219001172003021900117NM 2003 2 19 SWAA030343 120030212A3234A42006028305 SOLENOID BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29619SW 28035 AIR TURNBACK, AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE PAST MID POSITION. REMOVED AND REPLACED LANDING GEAR HANDLE LOCK SOLENOID PER MM. 2L72 4F RTA16WE 20030219001202003021900120NM 2003 2 19 SWAA030348 120030211A32116546113 TRUNNION PIN BOEING737 7373H4 1384600NM LT AND RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030219001222003021900122NM 2003 2 19 SWAA030351 120030212A33506556633 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29738CB 27870 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030219001272003021900127WP 2003 2 19 CALA0300055 120030218A323359370365501 ACTUATOR DOUG DC9 DC982 3022082WP L/H MLG LEAKING A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW09338175741 49371 THE GEAR HORN SOUNDED ON FINAL APPROACH TO IAH AT 1000 FEET. THE QRH PROCEDURE FOR UNSAFE GEAR AND HYD QTY LOSS CHECKLIST WAS COMPLETED DURING A "GO AROUND". A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE L/H MLG ACTUATOR LEAKING DURING A GEAR SWING. THE L/H MLG ACTUATOR WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE R/H MLG DOOR SKIN AND STRUCTURE WERE INSPECTED FOR DAMAGE AND NONE WAS FOUND. THE DOOR BUMPER PAD WAS MISSING. THE BUMPER PAD WAS REPLACED. 2L72 4F A6WE 20030219001282003021900128NM 2003 2 19 CALA0300056 120030206A5330 SKIN BOEING737 737824 13844BZNM STA 460-480 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0926215 28775 INSPECTION FOUND A DENT AND GOUGE IN THE FUSELAGE SKIN BELOW THE FORWARD CARGO DOOR CUTOUT BETWEEN STA 460 AND 480 FROM S26R TO S27R. THE SKIN WAS REPAIRED IAW ECRA 5330-03204. 2L72 4F RTA16WE 20030219001292003021900129NM 2003 2 19 CALA0300057 120030207A5230 SKIN BOEING737 737824 13844BZNM AFT CARGO DR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0926215 28775 INSPECTION FOUND THE AFT CARGO DOOR OUTER SKIN DENTED FORWARD OF THE DOOR HANDLE AT STA 808. THE CUTOUT WAS 3.35" X 7.5" AFTER THE DENTED AREA WAS REMOVED. THE AREA WAS REPAIRED IAW ECRA 5210-01629. 2L72 4F RTA16WE 20030219001322003021900132 2003 2 19 SWAA030357 420030213A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030219001342003021900134NM 2003 2 19 USAA020001A 120030106A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US39448 23984 PIT - FOUND SKIN CRACKED 2 INCHES, STATION 727D AT OVERWING EXIT LIGHT RIGHT SIDE. INSTALLED REPAIR DOUBLER PER TR 53-60-03. (M) 2L72 4F RTA16WE 20030219001462003021900146NM 2003 2 19 USAA030011 120030116A5320 STIFFENER BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US41260 23876 PIT - FOUND STIFFENER CRACKED .5 INCH, RT STIFFENER RBBL 6.15 STATION 663.75 WL 170.4. INSTALLED REPAIR ANGLES PER EA 75661 AND EA 75658. (M) 2L72 4F RTA16WE 20030219001512003021900151NM 2003 2 19 USAABB02016A 120030122A33508731002511REV15 SIGN BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 CLT - FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030219001542003021900154NM 2003 2 19 USAABB03013 120030117A33508731002511REV15 SIGN BOEING757 7572B7 1384964NM CABIN INOPERATIVE A K NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 BDL - FOUND EXIT IDENTIFIERS AT DOORS L3 AND R3 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. 2L72 4F RTA2NM 20030219001552003021900155NM 2003 2 19 USAABB03014 120030118A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19628AU 27806 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS, 1, 4, 6, 13, 18, 23, 26, 29 AND 33 INOPERATIVE OR DIM. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030218002392003021800239NM 2003 2 18 SWAA030270 120030203A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030218002412003021800241NM 2003 2 18 SWAA030236 120030201A3350101114 LENS BOEING737 7375H4 138449DNM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030218002432003021800243NM 2003 2 18 SWAA030239 120030131A3350101073 LENS BOEING737 7373H4 1384600NM FWD CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED C3 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030218002452003021800245NM 2003 2 18 SWAA030241 120030130A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM MID CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A +17, WL 208 AND RBL 44. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20030218002492003021800249NM 2003 2 18 SWAA030246 120030128A53246545785530 WINDOW FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND WINDOW FRAMES CRACKED (2 EA) AT LT WINDOW NR 7 AND RT WINDOW NR 11. REMOVED AND REPLACED WINDOW FRAMES PER SWA EA. 2L72 4F RTA16WE 20030218002512003021800251NM 2003 2 18 SWAA030248 120030202A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 315, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030218002572003021800257 2003 2 18 SWAA030358 420030213A256565C19901 CABLE BOEING737 7373H4 1384600NM AFT SVC DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030218002662003021800266NE 2003 2 18 ALG2003F218A 120030115A64107610105101041 PLUG SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL TAIL ROTOR BLADEDEBONDED B ALGRK NONE O OTHER ININSP/MAINT 1 SW03702AL13065492 760243 DISCOVERED DURING ROUTINE MAINTENANCE INSPECTION. SPAR ELLIPTICAL PLUG 100 PERCENT DEBONDED. NEW PLUG INSTALLED AT MFG O AND R 12-26-00 AT COMPONENT TOTAL TIME 11978.5. 1G72 3U3 U H1NE E1GL 20030218002672003021800267SW 2003 2 18 ALG2003F00022 120030116A2910407076011101 LINE BELL 407 407 1182206SW ALLSN 250C 250C47B GL HYD SYSTEM LEAKING E ALGAK NONE K FLUID LOSS ININSP/MAINT 1 SW03607AL4224 53264 CAE847048 DURING POST FLIGHT. DURING POST FLIGHT PILOT NOTICED EXCESSIVE AMOUNT OF RESIDUAL OIL ON THE LEFT SIDE OF THE FUSELAGE, THE MECHANIC FOUND THE T/R HYDRAULIC RETURN LINE (B) NUT WAS CRACKED, HE REMOVED AND REPLACED THE LINE. AIRCRAFT WAS LEAK CHECKED AND RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20030218002692003021800269SO 2003 2 18 C2XA03IA022 120030212A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712922 145338 BNA- DURING ROUTINE INSPECTION THE MECHANIC NOTED THAT THE FORWARD ORANGE EMERGENCY LIGHT FLOOR PROXIMITY STRIP FAILED TO ILLUMINATE. BNA- MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 EMERGENCY LIGHT INVERTER, IAW EMB 145 MM 33-50-11,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030218002702003021800270EU 2003 2 18 AWXA200300156 120030217A3350 CONNECTOR AIRBUS320 A320231 3930325EU -N/A- BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW0 0 076 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT ROW 26 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPLACED CONNECTOR AT WALL DISCONNECT PER AIRBUS STANDARD PRACTICE SWPM MANUAL. EMERGENCY LIGHTS WERE OPERATIONALLY CHECKED GOOD AFTER REPAIR. 2L72 4F RTA28NM 20030219000012003021900001CE 2003 2 19 2003F00112 120030212A521036420010631 DOOR BEECH 58 58 1152740CE MAIN PAX UNLATCHED G A UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA21707PW5636 TH1106 FORWARD CABIN DOOR OPENED IN FLIGHT WHILE ENROUTE FROM FCI TO CDN. AIRCRAFT LANDED AT RZZ. INSPECTION PERFORMED ON DOOR AT RZZ. FOUND DOOR AND ATTACHING HARDWARE INTACT. NO DEFECTS NOTED. DOOR OPERATIONAL CHECKS GOOD. 1L72 3O 3A16 20030219000042003021900004SO 2003 2 19 DYVA0001 220030130A8520TCM642135 CRANKCASE CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO ENGINE CRACKED A DYVAK NONE O OTHER ININSP/MAINT 1 NM072655B1772 421C0698 265043R DURING ROUTINE INSPECTION. CRACK IN CRACKCASE AT GEAR REDUCTION HOUSING. ENGINE REMOVED FOR REPAIR. CRACK LENGTH 1 INCH. SEEPING OIL. NDT VERIFIED CRACK. 1L72 3O3 O A7CE E7CE 20030219000142003021900014EA 2003 2 19 COMA0360102 120030214A5600NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA L/H BROKEN A COMAO OTHER O OTHER CRCRUISE 1 SO01971CA4971 7145 FLIGHT 5030 PILOTS WINDSHIELD SHATTERED.REPLACED WINDSHIELD. 2L72 4F RTA21EA 20030219000202003021900020EA 2003 2 19 YBN2003F00000 220030204A8520LW13521 BEARING PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA CONNECTING ROD DELAMINATED E YBNAO OTHER O OTHER NRNOT REPORTED 1 GL032197Z3480 447995293 L32277 NR 2 CONNECTING ROD BEARING WAS FOUND TO BE DELAMINATING. THE PROBLEM WAS DISCOVERED DURING A PRELIMINARY INSPECTION DURING AN OVERHAUL. TOTAL TIME IN SERVICE WAS 3480 HOURS. THE BEARINGS IN THE OTHER CONNECTING ROD LOCATIONS APPEARED TO HAVE NORMAL WEAR FOR THE AMOUNT OF HOURS ON THE ENGINE. PROBABLE CAUSE FOR THIS FAILURE IS NOT SURE, THE ENGINE DID NOT LOOK AS THOUGH IT EXPERIENCED OIL STARVATION AT ANY TIME. THE MOST LIKELY CAUSE WOULD BE A MANUFACTURING DEFECT OF SOME KIND. THE ONLY WAY TO PREVENT THIS FROM RECURRING WOULD BE TO IMPROVE THE FACTORYS QUALITY CONTROL PROCESS. 1L72 3O3 O A19S0 E286 20030219000252003021900025NM 2003 2 19 2003UALA00142 120030204A335015AT48 SWITCH BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE A UALAK NONE O OTHER ININSP/MAINT 1 WP29954UA 26739 EMERGENCY EXIT "NOT ARMED" LIGHT DOES NOT ILLUMINATE WHEN SYSTEM IS OFF SUPPLEMENTAL DATA UPDATE REPLACED EMER EXIT LIGHT SWITCH S7. OPS CKECKED NORMAL. 2L72 4F4 FRTA16WE E2GL 20030219000312003021900031NM 2003 2 19 2003UALA00177 120030212A5315 STIFFENER BOEING777 777222 1385219NM PWA PW4077PW4077 NE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29211UA 30217 STA 246 FLOOR BEAM HAD CRACKED STIFFENER AT LBL 26.26 MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER. 2L72 4F4 FRTT0001SE E46NE 20030219000392003021900039WP 2003 2 19 MWEA030095 120030213A5330591142884 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FUSELAGE SKIN IS DENTED AND CRACKED AROUND FORWARD SIDE OF RIGHT THRUST REVERSER BYBASS ACCESS DOOR. -- FABRICATED AND INSTALLED REPAIR DOUBLERS. 2L72 4F A6WE 20030219000432003021900043CE 2003 2 19 FFS2003F00016 120030131A28201183890033 MANIFOLD BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA FUEL SYSTEM BROKEN A FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575Q UC160 WHEN TRANSFERRING FUEL FROM ONE MAIN TANK TO ANOTHER, THERE WAS A SOUND LIKE A HAMMER HITTING THE PIPES. NARROWED IT DOWN TO THE RIGHT MAIN FUEL TANK, FUEL MANIFOLD CHECK VALVE SPRING WAS BROKEN AND THE VALVE WAS CHATTERING, WHEN PRESSURE WAS APPLIED. 2L72 4T4 TRTA24CE E4EA 20030219000452003021900045NM 2003 2 19 HN62003F00000 120030120A2497BMS133ST1C1600 CABLE BOEING757 7572T7 1384914NM RROYCERB211 RB211* 54555NE RT WING CHAFED B HN6RO OTHER O OTHER NRNOT REPORTED 1 NM01513NA53935 23895 NR 2 ENGINE GENERATOR FEEDER CABLES ARE CHAFING ON NR 6 SLAT INBOARD AUXILLARY TRACK. MOUNT PLATE FOR CLAMP IS MISPOSITIONED BELOW AUXILLARY TRACK. THERE ARE 2 POSITIONS FOR THE MOUNT PLATE, IN THE UPPER POSITION THE AUXILLARY TRACK CHAFES THE FEEDER CABLE. MFG HAS REPAIRED THE CABLE AND REPOSITIONED THE CLAMP FOR MAXIMUM CLEARANCE. 2L72 4F4 FRTA2NM A12EU 20030219000472003021900047CE 2003 2 19 KC82003F00000 120030131A7810 CASE LEAR 25 25D 5170514CE GE CJ610 CJ6106 30006NE FORWARD FLANGE WARPED A KC8AO OTHER O OTHER NRNOT REPORTED 1 GL2375CK 256 241322A FOUND EXHAUST CASE FORWARD FLANGE WARPED CAUSING EXHAUST LEAKAGE AND A FALSE FIRE WARNING. REPLACED EXHAUST CASE WITH OVERHAULED CASE SN GGM1158. TESTED FIRE LOOP SYSTEM IAW MFG MM. GROUND RUN AND LEAK CHECKED EXHAUST CASE. ALL WORK PERFORMED IAW SEI186 AND MFG MM. 2L72 4J4 J A10CE 1E16 20030219000492003021900049CE 2003 2 19 MGO2003F00001 120030120A275045A61035011 CONTROL CABLE MTSBSIMU300 MU300 5780602CE PWA JT15 JT15D4 52112NE TE FLAP BROKEN B MGORO OTHER O OTHER NRNOT REPORTED 1 CE09824DW A075SA WHILE INVESTIGATING PILOT REPORT OF SPEED BRAKES. FAILURE TO DEPLOY IN FLIGHT. FOUND LT HAND FORWARD FLAP CABLE CORRODED INTO TWO PIECES INSIDE SWAGED TERMINAL. CABLE SHOWED SLIGHT TO NO VISIBLE INDICATION OF CORROSION ON THE OUTSIDE OF SWAGED TERMINAL, NO REPORT OF ANY FLAP SYSTEM PROBLEMS. 2H72 4F4 FRTA14SW E1NE 20030219000502003021900050WP 2003 2 19 NQ52003F00000 120030129A532025DWG3403180003 SUPPORT BRACKET CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL FUSELAGE CRACKED B NQ5RO OTHER O OTHER NRNOT REPORTED 1 GL2351255 383 501554 APPROX .2500 CRACK DETECTED IN WEB/FLANGE RADIUS OF AFT TEE OF SUPPORT BRACKET ASSEMBLY FOR ATTACHMENT OF MAIN ENTRANCE DOOR ACTUATOR. THIS TEE BRACKET IS ATTACHED TO THE FORWARD FACE OF FUSELAGE BELTFRAME AT FS 176.50, STRINGER L-26 AND IS APPROX 4 INCHES LONG. 2L72 4R4 T 6A6 E282 20030219000652003021900065WP 2003 2 19 MWEA030076 120030212A53129915558513 CLIP DOUG DC9 DC981 3022081WP STA Z34 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 REMOVED AFT PRESSURE BULKHEAD FORMER ASSEMBLY FROM FORWARD SIDE OF AFT OF AFT PRESSURE BULKHEAD AT STATION Z34 TO FACICLITATE OTHER MAINTENACE. -- REMOVED ASSEMBLY AND FORMER DRILLED UP AND INSTALLED NEW CLIP AND INSTALLED FORMER. 2L72 4F A6WE 20030219000702003021900070NM 2003 2 19 SWAA030244 120030201A21216454051 FAN BOEING737 7373H4 1384600NM A/C BAY MALFUNCTIONED A SWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29630WN 27705 DURING FLIGHT A GRINDING NOISE AND BURNING SMELL AT MID CABIN, TURNED RECIRC FAN OFF AND SMELL DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM. 2L72 4F RTA16WE 20030219000792003021900079WP 2003 2 19 MWEA030069 120030217A531259101638785 SPLICE PLATE DOUG DC9 DC981 3022081WP STA 1338 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 NEW AFT PRESSURE BULKHEAD TEE AT STATION 1338 LONGERON 6 RIGHT AND 18 RIGHT REQUIRES NEW SPLICE PLATE AT FACTORY SPLICE LOCATION. -- FABRICATED AND INSATLLED LOWER AND UPPER NEW SPLICE PLATE. 2L72 4F A6WE 20030219000932003021900093NM 2003 2 19 SWAA030311C 120030207A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030219000942003021900094NM 2003 2 19 SWAA030311D 120030207A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030219001012003021900101NM 2003 2 19 SWAA030325 120030210A3350100885 CHARGER BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS AFT CABIN INOP. REMOVED AND REPLACED BATTERY CHARGER BASE PER MM. 2L72 4F RTA16WE 20030219001042003021900104NM 2003 2 19 SWAA030331 120030209A29101062030192 HYDRAULIC LINE BOEING737 7373Q8 1384670NM LT MLG CRACKED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29695SW 23506 AIR TURNBACK, DECLARED EMERGENCY, DURING DEPARTURE LOSS 'A' SYSTEM HYDRAULIC QUANTITY AND PRESSURE. FOUND, LT MLG UPLOCK ACTUATOR LINE CRACKED. REMOVED AND REPLACED UPLOCK ACTUATOR LINE PER MM. 2L72 4F RTA16WE 20030219001052003021900105 2003 2 19 SWAA030333 420030211A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030219001132003021900113NM 2003 2 19 SWAA030334 120030211A532065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 17L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030219001252003021900125NM 2003 2 19 CALA0300051 120030217A5313 STRINGER BOEING737 7373T0 1384582NM STA 323 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND STRINGER 28R AND 29L CORRODED AT STA 323 AT FORWARD SIDE OF E&E DOOR JAMB. THE STRINGER SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030219001612003021900161EU 2003 2 19 USAASA03006 120030118A3350 CONNECTOR AIRBUSA321 A321211 3930370EU CABIN SHORTED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19164UW 1425 CLT - THE AFT EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHT TEST. MAINTENANCE RETERMINATED CONNECTOR 7260VC14A, WHICH WAS SHORTED DUE TO AN UNINSTALLED PROTECTIVE COVER. ALSO, REPLACED EMERGENCY POWER SUPPLY UNIT, AND INSTALLED PROTECTED COVER BACK OVER CONNECTOR 7260VC14A. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030219001622003021900162NM 2003 2 19 USAASB02015A 120030128A335020131A BATTERY PACK BOEING737 737401 1384701NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19418US 23985 PIT - MAINTENANCE REPORTED THE FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030219001682003021900168NM 2003 2 19 UPS03240195 120030214A5310 SUPPORT FITTING BOEING727 72725C 138400HNM MCD LATCH CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C MAIN CARGO DOOR LATCH SUPPORT FITTING @ BS 612-90 FOUND CRACKED DURI NG INSPECTION FITTING REMOVED I.A.W. SRM 51-30-03 FITTING REPLACED I.A.W. EO B727-5310-0437 2L73 4F A3WE 20030219001722003021900172EU 2003 2 19 WRNA200300005 120030214A2710336809101 SWITCH AIRBUS300 A300B4203 3930306EU A WRNAK NONE O OTHER CRCRUISE 1 SO05820SC 154 Flight control servo control lever lock circuit breaker tripsCorrective Action: Removed and replaced low speed aileron green system actuator micr-switch assy. ops checked good. 2L72 4F RTA35EU 20030220000112003022000011NM 2003 2 20 UIEA200300001 120030122A551165B036409 SPAR BOEING747 747243B 1384830NM HORIZONTAL STAB CORRODED E UIEAK NONE O OTHER ININSP/MAINT 1 EA15516MC8396414784 22507 DURING CURRENT C CHECK, FOUND LT STABILIZER REAR SPAR CORRODED AT STABILIZER B/L 372, STA 550. NO ESTABILISHED LEVEL OF CORROSION DECLARED SINCE ITEM DISCOVERED DURING ROUTINE INSPECTION. REMOVED EXISTING SPAR SPLICES LOCATED AT STAB STA. 525 AND 570. REMOVED SPAR SECTION TO EXISTING SPLICES. FABRICATED REPLACEMENT SPAR SECTION, SPLICE STRAP SEGMENTS AND FILLER STRIPS. INSTALLED REPAIR PARTS IAW SRM. 2L74 4F A20WE 20030220000162003022000016EA 2003 2 20 03043663 120030210A7110 COWLING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT ENGINE DEPARTED A VTZAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 EA27663BR 7527 AFTER TAKE OFF, RT ENGINE COWLING DEPARTED THE AIRCRAFT. CREW WAS NOT AWARE OF THE PROBLEM AND FLIGHT CONTINUED ON. AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENTS. THIS EVENT IS STILL UNDER INVESTIGATION. FURTHER INFORMATION WILL BE PROVIDED WHEN MAINTENANCE ACTIONS ARE COMPLETE. (OPEN) (CLOSED) MAINTENANCE PERSONNEL PERFORMED DETAILED INSPECTION OF RT ENGINE COWLINGS, PYLON AND EMPENAGE, NO DEFECTS WERE NOTED. NEW ENGINE COWL WAS INSTALLED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030220000202003022000020EU 2003 2 20 03049311 120030218A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33112UHR WP EMERGENCY LIGHTSLOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27311UE 41029 EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL RESECURED LOOSE CONNECTOR. OPERATIONAL CHECK GOOD AIRCRAFT RELEASED FOR CONTINUED OPERATION. 2L72 4T4 TRTA41NM E4WE 20030220000412003022000041WP 2003 2 20 ABXA030042 120030110A528059149985516 SKIN DOUG DC9 DC941 302207NWP NLG DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23977AX 47513 RT FORWARD NOSE LANDING GEAR DOOR EXTERIOR SKIN WAS CORRODED AROUND AFT DOUBLER. REPLACED RT NOSE LANDING GEAR DOOR IAW DC-9 MM 32-22-01-2. 2L72 4F A6WE 20030220000452003022000045WP 2003 2 20 ABXA030046 120030122A3230 TORQUE TUBE DOUG DC8 DC861 3021952WP RT MLG OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23849AX 45891 GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED WITH RT MLG DOOR SHOWING UNSAFE. CYCLED LANDING GEAR, LIGHTS REMAINED ON. PLACED GEAR HANDLE TO UPLATCH POSITION. LIGHT WENT OUT. EXCESSIVE INBOARD AND OUTBOARD GAPS WERE FOUND ON THE RT MLG TORQUE TUBE. REMOVED THE RT MLG DOOR ROLLER LATCH FOR CLEARNACE ADJUSTMENT AND ADJUSTMENT OF DOOR ROLLER LATCH. RESHIMMED RT MLG TORQUE TUBE. OPS AND LEAK CHECKED GOOD IAW DC-8 MM 32-11-03. 2L74 4F 4A25 20030220000462003022000046WP 2003 2 20 ABXA030047 120030127A3260 PROXIMITY SENSOR DOUG DC9 DC941 302207NWP RT MLG DIRTY A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23954AX 47612 RT GEAR UNSAFE LIGHT CAME ON DURING UPLATCH CHECK AFTER TAKE-OFF. FOLLOWED ABNORMAL PROCEDURE AND RECYCLED GEAR. UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE UP AND RT HYDRAULIC SYSTEM IN 'HIGH', RT GEAR LIGHT REMAINED ILLUMINATED. ON DESCENT AT FL 250, RT GEAR UNSAFE LIGHT WENT OUT AND AUTO SPOILER ACTUATOR CYCLED BACK TO THE ARMED POSITION. CLEANED PROXIMITY SWITCHES AND LUBRICATED MLG AND DOOR UPLATCH MECHANISMS IAW DC-9 MM 12-61-0. PERFORMED GEAR EXTENSION AND RETRACTION TEST SEVERAL TIMES IAW DC-9 MM 32-30-0. NO DEFECTS NOTED. AUTO SPOILER ARM, OPS CHECKED GOOD. 2L72 4F A6WE 20030220000582003022000058NM 2003 2 20 ABXA030059 120030131A7830 SHROUD PWA BOEING767 767231 1385131NM PWA JT9 JT9D7R4D 52054NE RT ENGINE DAMAGED A ABXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23707AX 000040 22570 709643 REVERSER ISOLATION VALVE EICAS MESSAGE AND REVERSER ISOLATION LIGHT ILLUMINATED AFTER LANDING WITH REVERSER LEVERS STOWED. RT ENGINE FAN EXIT DUCT, OUTER SHROUD, FAN STARTORS DAMAGED AND OUTER FAN SHROUD PANELS WERE MISSING. ENGINE AND TRHUST REVERSER CHANGED IAW B767 MM. 2L72 4F4 FRTA1NM E3NE 20030220000592003022000059WP 2003 2 20 ABXA030060 120030130A325047743701 LINK DOUG DC8 DC861 3021952WP NLG STEERING SHEARED A ABXAO OTHER O OTHER NRNOT REPORTED 1 GL23847AX 46031 ON ROLLOUT, NO BRAKING BELOW 15 KNOTS. STICK SHAKER WENT OFF, BLOW AWAY JET INOPERATIVE. SUSPECT GROUND SHIFT FAILURE. FOUND NOSE LANDING GEAR STEERING SHUTOFF VALVE LINK SHEARED. REPLACED LINK ASSEMBLY IAW DC-8 MM 32-21-01. OPS CHECKED GOOD. 2L74 4F 4A25 20030303001092003030300109WP 2003 3 3 ZW0A0302801 120030302A25308201514300D CONTROLLER DOUG DC9 DC982 3022082WP A ZW0AD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE13921TW 49101 AFTER PUSH BACK THERE WAS SMOKE AND SPARKS FROM THE FORWARD GALLEY OVEN. THE AIRCRAFT RETURNED TO THE GATE. A PAPER/FOIL LID WAS TRAPPED BETWEEN THE OVEN AND FOOD CONTAINER AND LODGED AGAINST THE VENT FAN CAUSING THE FAN TO SMOLDER AND CAUSE SMOKE. THE LID WAS REMOVED AND THE OVEN WAS DEFERRED PER MEL. THE OVEN CONTROLLER WAS LATER REPLACED. CHECK-C 3-25-02 STL. --CLOSED-- 2L72 4F A6WE 20030303001122003030300112SW 2003 3 3 HEEA084529 120030214A243230703002 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 MAIN BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030303001132003030300113SW 2003 3 3 HEEA084530 120030214A243230703002 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 MAIN BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030303001202003030300120SW 2003 3 3 HEEA084538 120030214A243239563001 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 33115 MAIN BATTERY WEAK. 1G72 4U H4SW 20030303002032003030300203NM 2003 3 3 CALA0300079 120030228A5347 SEAT TRACK BOEING777 777224 1385225NM BS 1497-1513 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977006 29476 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1497-1513, RBL 74. REPAIRED IAW SRM 53-00-52, REPAIR 3, FIGURE 202. 2L72 4F RTT00001SE 20030303002042003030300204NM 2003 3 3 CALA0300081 120030301A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE OF CAP AND AT FASTENER HOLES AT STA 1006, BL 0 TO RBL 30. THE T-CAP WAS REMOVED AND REPLACED IAW SRM 51-40-04. 2L72 4F RTA16WE 20030303002052003030300205NM 2003 3 3 CALA0300083 120030302A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND FLOORBEAM CORRODED IN AFT GALLEY AREA AT STA 967, LBL 25. REPAIRED IAW ECRA 5320-01726. 2L72 4F RTA16WE 20030303002092003030300209NM 2003 3 3 EIA2003046 120030303A7797BACC45FS14C7S CONNECTOR BOEING747 747212B 1384886NM N1 TACHOMETER DAMAGED A EIAAJ DUMP FUEL O OTHER TOTAKEOFF 1 NM09486EV 20888 DURING TAKE-OFF ROLL, BEFORE TAKE-OFF POWER WAS SET NR 1 ENGINE N1 MAX OUT THEN FAIL, 75,000LBS OF FUEL WAS JETTISON TO GET TO LANDING WEIGHT. REMOVED AND REPLACED N1 TACH CANNON PLUG IAW MM 77-12-00 2L74 4F RTA20WE 20030304000022003030400002 2003 3 4 AC2A084858 420030220A34215040017901 GYRO BELL 206 206L3 1182108SW ATTITUDE DEFECTIVE H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS016533U 51439 ATTITUDE GYRO IS DEFECTIVE. REPLACED 1G71 3U H2SW 20030304000072003030400007SW 2003 3 4 AC2A084863 120030224A6400222012733001 LOCK PLATE BELL 430 430 1182150SW TAIL ROTOR DAMAGED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT1142 49089 LOCK PLATE HAD TO BE REPLACED WHEN TAILROTOR WAS REMOVED FOR PROBLEM OF A WORN, RUSTED TRUNNION, AND CRACKED SPLINE ON TAIL GEARBOX OUTPUT SHAFT. REPLACED LOCKPLATE ASSEMBLY. 1G72 3U RTH9SW 20030304000172003030400017SW 2003 3 4 AC2A084873 120030302A3210430336437101 STRAP BELL 430 430 1182150SW MLG DEBONDED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CT1142 49089 FOUND RUBBER SUPPORT DISBONDED ON MLG DURING INSPECTION. REPLACED STRAP ASSEMBLIES. 1G72 3U RTH9SW 20030304000202003030400020SW 2003 3 4 ALGA084829 120030226A5260212075418105 ACTUATOR BELL 412 412EP 1182205SW STEP DEFECTIVE H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01XAAAR 36255 LINEAR STEP ACTUATOR WILL NOT ACTIVATE. 1G72 4U H4SW 20030304000242003030400024EU 2003 3 4 BAQA084830 120030227A62401179405303 INDICATOR BOLKMS117 BK117B2 5626013EU TRIPLE TACH FLUCTUATES H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS011174U236 7146 TRIPLE TACH NR NEEDLE INTERMITTENTLY FLUCTUATES 20-30 PERCENT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030304000312003030400031EA 2003 3 4 COMA0360125 120030227A7710 ENGINE CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01984CA 7171 FLIGHT 5658 N2 VIB INDICATION DURING T/O.COULD NOT DUPLICATE. VIB INDICATIONS WERE WITHIN LIMITS DURING MAINTENANCE RUNS. 2L72 4F RTA21EA 20030304000332003030400033EA 2003 3 4 COMA0360127 120030228A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01951CA3187 7091 FLIGHT 5861 WHEN GEAR SELECTED UP, ANTI-SKID, PARKING BRAKE WARNINGS, R/H MLG DID NOT RETRACT.REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030219001562003021900156NM 2003 2 19 USAABB03015 120030118A33509221009 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19628AU 27806 BDL - FOUND EXIT IDENTIFIERS AT DOORS R2 AND R4 INOPERATIVE OR DIM. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030219001692003021900169NM 2003 2 19 UPS03440193 120030206A5210 ANGLE BOEING747 747200 1384847NM DOOR #5R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C CRACK REVEALED AT PASSENGER DOOR #5R AT THE DOOR FRAMES FWD BOTTOM CORNER VERTICAL RADIUS, THE CRACK RUNNING UPWARD WITH LENGTH 2.5" LONG APPROX. DOOR FWD ANGLE INSTALLED AS PER SRM 52-10-02 FIG.10 2L74 4F RTA20WE 20030220000142003022000014EU 2003 2 20 03020601 120030206A7710 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE MALFUNCTIONED A UHLAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NE03146SD 146SD DEPARTED PIT ON 100 PERCENT TORQUE, 1000-2000 HAD ERRATIC TORQUE INDICATION OF 80-90 PERCENT. ITT SAME. NG 2-3 PERCENT. PROP RPM 1270-1150. AIRCRAFT LEVELED AT 2000, PULLED BACK 50 PERCENT, NO FLUTUATION, ADVANCED POWER LEVER, ERRACTIC INDICATION CONTINUED, SHUT DOWN ENGINE. TIME FROM SHUT DOWN TO LANDING WAS REPORTED APPROX 7 MINS. 2L72 4T4 TRTA52EU E8NE6 20030220000152003022000015EA 2003 2 20 03036654 120030205A3350110049 BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN FAILED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27654BR 7454 PASSENGER DOOR EMERGENCY LIGHTS FAILED. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY. MAINTENANCE PERSONNEL PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM AND RELEASED AIRCRAFT FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030220000172003022000017EA 2003 2 20 03043706 120030212A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FLOOD LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27706BR 7553 FOWARD CABIN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FOWARD EMERGENCY LIGHT BATTERY. MAINTENANCE PERSONNEL PERFORMED OPERATIONAL CHECK AND RELEASED AIRCRAFT FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030220000212003022000021NM 2003 2 20 03FDEA00012 120030108A5754 SUPPORT DOUG MD11 MD11F 3023600NM RT WING LE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING LEADING EDGE NR 16 SLAT TRACK SUPPORT INBOARD SIDE FOUND CRACKED APPROXIMATELY 1 INCH IN LENGTH. RT WING LEADING EDGE NR 16 SLAT TRACK CRACKED. RIB REMOVED IAW SRM 51-31-01 VOL. II, FABRICATED IAW DWG NR ARB2850 AND INSTALLED IAW SRM 51-31-01 VOL. II. 2L73 4F RTA22WE 20030220000232003022000023EU 2003 2 20 03FDEA00119 120030212A7830 THRUST REVERSER AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE NR2 ENGINE DEPLOYED A FDEAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO25655FE 742 NR 2 ENGINE THRUST REVERSER PRESSURIZED ON TAKEOFF ROLL, REJECTED TAKEOFF AT 70KTS. WHILE DEACTIVATING THE NR 2 ENGINE THRUST REVERSER, WE WERE UNABLE TO LOCK OUT THE SLEEVE DUE TO THE HOLE NOT LINEING UP TO INSTALL BOLTS. DIRECTIONAL PILOT VALVE HAS BEEN ORDERED. ** S/D ** COMING 2L72 4F4 FRTA35EU E13NE 20030220000242003022000024NM 2003 2 20 03FDEA00120 120030212A5315 FLOORBEAM BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 CORROSION ON FLOORBEAM BS 1070, LBL 18, WL 200. ** SD ** COMING 2L73 4F RTA3WE 20030220000272003022000027NM 2003 2 20 03FDEA00123 120030213A5321 FLOORBEAM BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 CORROSION ON FLOORBEAM, BS 950, LBL 50, RBL 25, WL 208. 2L73 4F RTA3WE 20030220000322003022000032NM 2003 2 20 03FDEA00128 120030121A5753ARC050213 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE TE FLAPS LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING OUTBOARD FLAP, INBOARD HINGE (AIRFRAME SIDE) AT ACTUATOR HINGE INBOARD AND OUTBOARD BORE CORRODED. REMOVED AND REPLACED INBOARD FLAP HINGE IAW EA. 1-5750-67563. 2L73 4F4 FRTA22WE E13NE 20030220000332003022000033NM 2003 2 20 03FDEA00129 120030121A5753ARC050311 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING OUTBOARD, FLAP OUTBOARD HINGE, (AIRFRAME SIDE) ACTUATOR HINGE, INBOARD AND OUTBOARD HINGE BORE CORRODED. REMOVED AND REPLACED OUTBOARD FLAP HINGE IAW EA. 1-5750-67564. 2L73 4F4 FRTA22WE E13NE 20030220000342003022000034NM 2003 2 20 03FDEA00130 120030130A5753ARC050214 HINGE DOUG MD11 MD11F 3023600NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO251058 48547 RT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, ACTUATOR HEAD END LUG, CORRODED. COMPLIED WITH EA 1-5750-67563. WING, TRAILING EDGE AND DEVICES LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030220000362003022000036EU 2003 2 20 040 120030116A7830F900HD3100001A3 SKIN AMD AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE731* 01518WP THRUST REVERSER GOUGED E ERYAK NONE O OTHER ININSP/MAINT 1 CE07369BG5978 5978 040 DURING SCHEDULED MAINTENANCE EVENT, FOUND GOUGING AND CHAFING PRESENT ON LT THRUST REVERSER DOOR SKIN. DAMAGE WAS MAPPED AND SENT TO MFG ENGINEERING FOR EVALUATION. MFG ENGINEERING DETERMINED DAMAGE IS NOT ACCEPTABLE, AND GRANTED EXTENSION FOR SERVICE PENDING AVAILABILITY OF SPARE PARTS OR A REPAIR DRAWING. A VISUAL INSPECTION PROGRAM WAS DEVELOPED BY MFG REQUIRING THE AFFECTED SKIN AREA BE INSPECTED EVERY 10 FLIGHTS UNTIL REPLACEMENT & REPAIR WAS ACCOMPLISHED. 2L73 4F4 FRTA46EU E6WE 20030220000402003022000040SW 2003 2 20 20031 120030124A52102724057091 VALVE SWRNGNSA226 SA226TB 8780406SW GARRTTTPE331TPE33110U 01514WP HARTZLHCB4T HCB4TN5 GL PAX DOOR OUT OF ADJUST E STZABA EMER. DESCENT UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 AL0395AC 5613 T381 AT 20,000 FT ALTITUDE, CREW NOTICED THAT THE CABIN ALTITUDE HAD STARTED TO CLIMB AT 2000 FPM. AFTER CHECKING THE PRESSURIZATION CONTROLS, DUMP VALVE SWITCH POSITION, AND THE CABIN DOOR ANNUNCIATOR AND FINDING NO IRREGULARITIES, THE CREW INITIATED A 180 DEG TURN AND ASKED FOR AN IMMEDIATE DECENT. THE CREW WAS CLEARED TO DESCEND DIRECT TO ANC AND LANDED WITHOUT FURTHER INCIDENT. THE CREW ALSO REPORTED THAT ON DECENT THE CABIN WOULD HOLD PRESSURE; HOWEVER THEY EXPERIENCED SEVERAL PRESSURIZATION (BUMPS). MAINTENANCE WAS DISPATCHED TO LOOK AT THE AIRCRAFT AND AFTER TROUBLE SHOOTING THE PROBLEM, THEY ADJUSTED THE DOOR SEAL VALVE. (P/N 27-24057-091) 2L72 4T4 TRTA5SW E4WE 6 CP40EA 20030304000382003030400038SW 2003 3 4 HEEA084572 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MAIN ROTOR BLADE SKIN PEELING OFF TOP MIDDLE SECTION OF BLADE. 1G72 4U H4SW 20030304000542003030400054SW 2003 3 4 HEEA084585 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T A2718 33112 MAIN ROTOR MAST LINK HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030304000562003030400056SW 2003 3 4 HEEA084587 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z4526 36019 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000592003030400059SW 2003 3 4 HEEA084590 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000682003030400068SW 2003 3 4 HEEA084598 120030214A6230 BEARING BELL 412 412 1182202SW LINK WORN E O OTHER O OTHER NRNOT REPORTED 1 SW031202T A1997 33112 HUB AND SLEEVE ASSY LINK HAS A WORN BEARING. REPAIRED. 1G72 4U H4SW 20030304000752003030400075NM 2003 3 4 DL757030087 120030123A5330143N34714 SKIN BOEING757 757232 1384965NM FS 580, S-28L GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 FUSELAGE / SKIN / FS 580 / STRG. 27L-28R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED NEAR FS 580 BETWEEN STRINGERS 27L & 28R. THE GOUGES WERE REMOVED WITH TWO CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384409-14, REV A. 2L72 4F RTA2NM 20030304000782003030400078NM 2003 3 4 DL757030096 120030124A5330146N35317 SKIN BOEING757 757232 1384965NM FS 1540, S-29L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 FUSELAGE / SKIN / FS 1540 / STRG. 29L-30 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1540 BETWEEN STRINGERS 29L & 30. THE DENT WAS REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 384377-14, REV A. 2L72 4F RTA2NM 20030304000842003030400084 2003 3 4 DL76L030133 420030208A3440732591B FAN M732591EF BOEING767 767332 1382001NM AC SYSTEM FAULTY A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27171DN 26 24759 CREW REPORTED STRONG ELEC SMELL AT FIRST COMING FROM THE AREA AROUND THE WX RADAR INDICATOR. LASTED FOR ABOUT 30SEC AND THEN FAINT SMELL. CREW FOUND C/B FOR FWD RACK EXH FAN (H-21 ON P-6) POPPED WITH FWD EQUIP O'HEAT LIGHT. MAD MTC VERIFIED SUPPLY FAN OPERATIONAL AND FWD TO MCO AND PLAC PER MEL 21-58-04B. REPLACED FWD EQUIPT XHAUST FAN. CKS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030304000892003030400089NM 2003 3 4 DLM88030145 120030211A524059615001 PANEL DOUG MD88 MD88 3023688NM FWD SERVICE DOORMISSING A DALAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SO27918DL 49583 ON ARRIVAL FOUND FORWARD AIR CONDITIONING PANEL MISSING - PANEL HAD COME OFF DURING FLIGHT SUSPECT RAMP PERSONNEL FAILED TO LATCH PANEL SECURE AT DOWNLINE STATION - REPLACED SAME 2L72 4F RTA6WE 20030304000902003030400090NM 2003 3 4 DL738030152 120030212A5312141A83718 FRAME BOEING737 737832 13844CFNM R1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27391DA 30560 FUSELAGE / R1 DOOR OPENING / FWD FRAME / LOWER STUB FRAME : CRACK REPAIR THE LOWER STUB FRAME OF THE R1 DOOR OPENING FWD FRAME ASSY WAS FOUND WITH 3 CRACKS AT THE LOWER DOOR STOP FITTING. THE CRACKS WERE CAUSED BY IMPROPER ADJUSTMENT OF THE STOP FITTING. THE CRACKS WERE REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER ER/A 384564-14, REV A. 2L72 4F RTA16WE 20030304001002003030400100 2003 3 4 HEEA084602 420030214A3442 CONNECTOR BELL 412 412 1182202SW WX RADAR IND CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 2713 33073 WEATHER RADAR ANTENNA WILL NOT SWEEP. FOUND UNIT DOES NOT SWEEP. FOUND CORROSION ON CONNECTOR P3001, CLEANED, REPAIRED, BENCH CHECK GOOD. 1G72 4U H4SW 20030305000072003030500007 2003 3 5 HEEA084612 420030214A2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 TRANSCEIVER INOPERATIVE. REPLACED BAD I309 IC CHIP. REPAIRED. ADJUSTED C/N SQUELCH, CARRIER SQUELCH, MIC GAIN, TRANSMIT COMPRESSOR AND SIDETONE. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000102003030500010SW 2003 3 5 HEEA084615 120030214A3210400052007109 BEAM BELL 407 407 1182206SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 AFT CROSSTUBE SLIPPED IN FITTING CAUSING DAMAGE TO FITTING. 1G71 3U O H2SW 20030305000212003030500021NM 2003 3 5 C1HA200383001 120030105A3260 SWITCH BOEING727 7272S7 138407ZNM MLG HANDLE LIGHTOUT OF ADJUST A C1HAO OTHER N FALSE WARNING CLCLIMB 1 GL15683CA 22490 LT MAIN GEAR DOOR LIGHT COMES ON WITH GEAR HANDLE OFF. LIGHT GOES OUT WITH HANDLE UP. ADJUSTED LEFT MAIN GEAR DOOR LIGHT SWITCH. RAN THROUGH SEVERAL TIMES. SYSTEM OPS CHECK NORMAL IN OFF MODE IAW 727 MM 32-12-00. 2L73 4F A3WE 20030305000222003030500022NM 2003 3 5 C1HA200385001 120030123A2612 FIRE DETECTOR BOEING727 7272S7 138407ZNM APU WILL NOT TEST A C1HAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL15685CA 22492 APU FIRE DETECTION SYSTEM WILL NOT TEST. REMOVED AND REPLACED APU FIRE HANDLE. OPS CHECK GOOD. 2L73 4F A3WE 20030305000242003030500024NE 2003 3 5 C1HA200394002 220030107A7200 ENGINE BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 3 STALLED A C1HAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL15294AS 22146 COMPRESSOR STALL NR 3 - 2.0 EPR 80 KT NR 3 ENGINE ICING LIGHT ILLUMINATED BRIEFLY. CHECKED NR 1 DETENT ON REV LEVER AND ADJUSTED ACHIEVE 1.60 EPR AT DETENT, NO STALLS NOTED AT 2 DETENT, AC OK FOR CONTINUED SERVICE IAW M/M CH 76-12-0/78-30-0. 2L73 4F4 F A3WE E2EA 20030305000272003030500027NM 2003 3 5 C1HA200395002 120030113A3397 WIRE BOEING727 727290 138408WNM PATH LIGHTING BROKEN A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15295AS 22147 FWD SECTION OF EMERGENCY PATH LIGHTING DOES NOT ILLUMINATE. FOUND BROKEN WIRE AT ROW 10. REPAIRED AS REQUIRED, OPS NORMAL. 2L73 4F A3WE 20030305000332003030500033NM 2003 3 5 C1HA200397005 120030126A2612 FIRE LOOP BOEING727 727270 138408PNM NR 1 ENGINE WILL NOT TEST A C1HAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL15697CA 23052 NR 1 ENG FIRE TEST DOES NOT TEST IN THE ENG & WW TEST POSITION. TESTS OK IN FW POSITION. REMOVED AND REPLACED FIRE DETECTION LOOP IAW 727 MM 26-11-0, OPS CKS GOOD OK FOR SERVICE. 2L73 4F RTA3WE 20030305000372003030500037SW 2003 3 5 HEEA084619 120030214A3210400052007109 BEAM BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MLG BEAM ASSY HAS CORROSION BEYOND LIMITS. 1G71 3U O H2SW 20030305000392003030500039 2003 3 5 HEEA084621 420030214A2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 VHF TRANCEIVER WILL NOT TRANSMIT. REPLACED BAD Q109 AND Q110 TRANSISTORS. REPAIRED PROBLEM. ALIGNED TRANSMITTER AND ADJUSTED C/N SQUELCH AND CARRIER SQUELCH. REPLACED BAD RF CONNECTOR. REMOVED CORROSION FROM CHASSIS. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000452003030500045 2003 3 5 HEEA084627 420030214A3455066104701 TRANSCEIVER BELL 412 412 1182202SW ADF MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 ADF TRANSCEIVER DOES NOT RECEIVE. REPAIRED. 1G72 4U H4SW 20030305000512003030500051 2003 3 5 HEEA084635 420030214A3451066106902 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 DISPLAY TOO DIM. REPLACED V901 PHOTOCELL, REPAIRED. CLEANED BOARDS AND CONNECTORS. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000552003030500055 2003 3 5 HEEA084639 420030214A3452066107100 TRANSPONDER BELL 412 412 1182202SW COCKPIT WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 TRANSPONDER WEAK AND INTERMITTENT REPORTING. SENT TO HONEYWELL, IN. FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030305000682003030500068EU 2003 3 5 HEEA084651 120030212A6720 BEARING BOLKMS105 BO105S 5626006EU BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 TAIL ROTOR BELLCRANK HAS WORN BEARINGS. REPLACED BEARING 2828P AND EN2015BN06E DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030305000892003030500089NM 2003 3 5 CALA0300088 120030303A5330 SKIN BOEING737 7373T0 1384582NM STA 235.8 NICKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0970330 23460 INSPECTION FOUND A NICK IN L/H FUSELAGE SKIN AT STA 235.8, 17.7 INCHES BELOW WL 207.5. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5330-03218. 2L72 4F RTA16WE 20030305000902003030500090WP 2003 3 5 CALA0300089 120030303A5210 CASTING DOUG DC9 DC982 3022082WP AFT ENTRY DR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 INSPECTION FOUND A 1/2" CRACK IN AFT ENTRY DOOR LEFT LOWER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-0. 2L72 4F A6WE 20030305000912003030500091WP 2003 3 5 CALA0300090 120030303A5311 BELTFRAME DOUG DC9 DC981 3022081WP STA 1446 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1446, LONGERON 6R TO 5L. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F A6WE 20030305000972003030500097SW 2003 3 5 HEEA084712 120030217A6720 SERVO BELL 412 412 1182202SW TAIL ROTOR CONTAMINATED E HEEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW03412SM 33197 IN CRUISE FLIGHT, PILOT NOTED HIGH FREQUENCY VIBRATION IN TAIL ROTOR PEDALS AND UNCOMMANDED MOVEMENT IN T/R PEDALS. FOUND MOISTURE IN TAIL ROTOR SERVO PILOT VALVE AREA AND PILOT VALVE BOLTS STIFF TO ROTATE. DRIED AREA AND FREED BOLTS. TEMPERATURE DURING FLIGHT BELOW FREEZING. 1G72 4U H4SW 20030306000032003030600003 2003 3 6 HEEA084716 420030217A3454071121612 CONTROL UNIT BELL 412 412 1182202SW VOR SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 INTERMITTENTLY LOCKS UP AND WILL NOT CHANGE FREQUENCIES. REPLACED DEFECTIVE TRANSFER SWITCH, DEFECTIVE PHOTOCELL AND FADED LENS. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000252003030600025 2003 3 6 HEEA084738 420030217A2340 SELECTOR KNOB BELL 412 412 1182202SW INTERPHONE BOX STIFF E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 8409977 33113 TRANSMIT SELECTOR HARD TO TURN. FOUND TRANSMIT SELECTOR S1 HARD TO TURN AND SELECTOR KNOB LOOSE. TIGHTENED SELECTOR KNOB AND LUBED TRANSMIT SELECTOR S1. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030220000642003022000064WP 2003 2 20 ABXA030065 120030209A335041B004AD07G3 BATTERY DOUG DC9 DC932F 3022067WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23904AX 47040 DURING PREDEPARTURE CHECK, EMERGENCY LIGHTS ON OVERHEAD PANEL WERE INOPERATIVE. REPLACED THE EMERGENCY POWER SUPPLY BATTERIES. OPS CHECKED GOOD IAW DC-9 MM 33-53-02-4-0001. 2L72 4F A6WE 20030220000662003022000066WP 2003 2 20 ABXA030067 120030211A793141800044 TRANSMITTER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 1 ENG OIL FAILED A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23811AX1848 46113 670977 DURING CLIMBOUT, WHEN NR 1 ENGINE ANTI-ICE WAS TURNED OFF, NR 1 ENGINE COMPRESSOR STALLED ACCOMPANIED BY NR 1 OIL PRESSURE WENT TO 100 PSI AND OIL QUANTITY FLUCTUATED +/-2 GALLONS. SECURED ENGINE. ENGINE WINDMILLED ABOVE 25 PERCENT FOR 45 MINUTES. FOUND NR 1 OIL PRESSURE TRANSMITTER BAD. REPLACED OIL PRESSURE TRANSMITTER IAW DC-8 MM 79-32-01. OIL QUANTITY READ NORMAL. REMAINED STEADY ON ENGINE RUN. REMOVED AND INSPECTED NR 1 ENGINE OIL FILTER, FILTER WAS CLEAN IAW DC-8 MM 79-20-07. PERFORMED ENGINE RUN, CHECKED OPERATION OF PRBC. CHECKED GOOD. TESTED ENGINE ANTI-ICE VALVE UNDER AIRLOAD VALVES. CHECKED GOOD. 2L74 4F4 F 4A25 1E8 20030220000742003022000074NM 2003 2 20 QXEA0300022 120030108A5610 WINDSHIELD BOMBDRDHC8 DHC8401 1390041NM COCKPIT BIRD STRIKE A QXEAO OTHER GHJMULTIPLE FAILURE ELECT. POWER LOSS-50 PC WARNING INDICATION APAPPROACH 1 NM09409QX 4051 FLT 2377 DURING APPROACH, APPROX 2500 FT AGL AND 210 KNOTS ENCOUNTERED MULTIPLE BIRD STRIKES. IMPACT SHATTERED THE LT WINDSHIELD AND THE CAPTAIN WAS INJURED BY THE FLYING GLASS. COPILOT TOOK CONTROL OF THE A/C AND CONTINUED THE APPROACH. A/C LOST ELECTRICAL POWER EXCEPT FOR BATTERIES. APPROACH AND LANDING WAS CONDUCTED ON STANDBY INSTRUMENTS. ENGINE FIRE WARNING LIGHTS ILLUMINATED ON THE GLARESHIELD, BUT NO WARNING TONE AND "T" HANDLES DID NOT ILLUMINATE. ELECTRIC TRIM WAS ALSO INOP. DECLARED AN EMERGENCY AND CFR WAS NOTIFIED. APPROACH AND LANDING WERE UNEVENTFUL. UPON LANDING IT WAS NOTED THAT THE NOSE WHEEL STEERING WAS INOPERATIVE. AIRCRAFT STILL DOWN FOR REPAIRS. 2H72 4T RTA13NM 20030220000782003022000078NM 2003 2 20 QXEA0300075 120030108A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- RIGHT HAND INBOARD SEAT TRACK NR 11 HAS DAMAGED LUGS AT STATION 160.0. REPAIRED IAW DHC-8 400 SRM TASK 51-00-02-250-801 AND HORIZON AIR EA 6-53-169. 2H72 4T RTA13NM 20030220000862003022000086EA 2003 2 20 QXEA0300084 120030114A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09615QX418 10065 ONT-FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220000902003022000090WP 2003 2 20 ABXA030079 120030207A575339145072 FITTING DOUG DC9 DC932 3022066WP RT TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23928AX 47392 RT FLAP INTERIOR FITTING AT INBOARD SIDE OF CENTER HINGE WAS CRACKED IN TWO PLACES BETWEEN RIVETS, BOTH ON UPPER SIDE OF FITTING. REPAIRED FITTING IAW DC-9 SRM 57-09. 2L72 4F A6WE 20030220001002003022000100EU 2003 2 20 QXEA0300095 120030112A5312 ANGLE FOKKERF28 F28MK4000 4990810EU FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09492US 11159 PDX- FORWARD PRESSURE BULKHEAD BOTTOM CONNECTION ANGLE HAS A THREE INCH LONG CRACK IN RADIUS, AFT SIDE OF BULKHEAD FS1550 THROUGH THREE INCHES LEFT OF BL0. REPAIRED IAW FOKKER SRM 53-02-18 AND HORIZON AIR EA 4-53-1578. 2L72 4F RTA20EU 20030220001222003022000122NM 2003 2 20 QXEA0300117 120030123A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR OUT OF POSITION A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09405QX 4047 SEA-ON FLIGHT NUMBER 2312, INFLIGHT AFT CARGO DOOR WARNING LIGHT CAME ON, AIRCRAFT RETURNED TO FIELD. INSPECTED CARGO DOOR. FOUND DOOR HANDLE NOT STOWED "POPPED OUT" CYCLED DOOR AND HANDLE SEVERAL TIMES. DOOR AND HANDLE OPERATE NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001232003022000123EA 2003 2 20 COMA0360108 120030218A52106003804019 SHAFT CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR BENT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01952CA 7092 FLIGHT 5751 CABIN DOOR WARNING.COULD NOT DUPLICATE. REPLACED INNER HANDLE ROD END ROLLER. 2L72 4F RTA21EA 20030220001252003022000125NM 2003 2 20 QXEA0300118 120030123A215078279018 ACM DHAV DHC8 DHC8202 2809007NM A/C BAY MALFUNCTIONED A QXEAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UKUNKNOWN 1 NM09358PH3220 506 IDA-LIGHT HAZE SMOKE CAME IN CABIN AND COCKPIT. LAVATORY SMOKE WARNING WENT OFF. RAN CHECKLIST AND CLEARED SMOKE. ALARM IN LAVATORY TURNED OFF. REMOVED AND REPLACED NR 1 AND NR 2 NL PROBES AND PORT SEALING TUBE PACKINGS. REMOVED AND REPLACED NR 2 ENGINE P2.5 AND P3 PRESSURE VALVE AND AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001362003022000136WP 2003 2 20 MWEA030050 120030203A533059114051 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31207ME 47794 FUSELAGE SKIN CRACKED AT FRAME STATION 180 SHEAR TIE BETWEEN LONGERON 1&2 RIGHT. FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED DOUBLER. 2L72 4F A6WE 20030220001502003022000150NM 2003 2 20 ASAA0140001A 120030102A33508100022601 LIGHT BOEING737 7374Q8 138447QNM CABIN MALFUNCTIONED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01754AS 25095 PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 13-17, DISCONNECTED WIRES. RECONNECTED WIRES, OPS CHECKED NORMAL. (M) 2L72 4F RTA16WE 20031027000992003102700099NM 2003 10 27 ASAA0240244 120030412A533065C32358 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND SKIN DENTED RIGHT SIDE FORWARD OF FORWARD PIT DOOR. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030220001692003022000169CE 2003 2 20 AMWA6 120030117A71201299100471 TRUSS BEECH 1900 1900D 1154162CE RT ENGINE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07106758004 8004 10675 WHILE PERFORMING AN "H" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND A CRACK IN THE INBOARD AND OUTBOARD COWLING SUPPORT BRACKETS. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED IT WITH ANOTHER ENGINE TRUSS. TEARDOWN REPORT REVEALED THAT THERE WAS A CRACK AT THE UPPER SUPPORT BRACKETS. ALSO CHAFED ON SUPPORT BRACKET. THE VENDOR PERFORMED 8000 HR MAG PARTICLE INSPECTION. REPAIRED TRUSS SUPPORT BRACKETS MOUNTS 2 EA BY FABRICATING AND INSTALLING FILLERS AND DOUBLERS ON UPPER COWLING BRACKETS. COMPLIED WITH "H" CHECK INSPECTION. REPAIRED CHAFED AREA ON COWLING BRACKET BY WELDING 2L72 4T RTA24CE 20030220001852003022000185WP 2003 2 20 ARWA20030206 120030216A2910 LINE DOUG DC8 DC862 3021970WP NR 3 HYD SYS LEAKING A ARWAJA DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO198974U 46110 IN FLIGHT ABOUT ONE HOUR OUT OF VTBU AFTER TAKE-OFF AIRCRAFT WAS LOSING HYDRAULIC FLUID. DID IN-FLIGHT TURNBACK, DUMPED FUEL AND LANDED BACK AT VTBU. RAN ALL APPROPIATE CHECK LISTS. FOUND NR 3 ENGINE HYDRAULIC PUMP SUPPLY LINE LEAKING. REMOVED AND REPLACED LINE AND LEAK CHECKED NORMAL IAW MM 20-12-0 AND MM 29-00 & 71-00. 2L74 4F 4A25 20030220001872003022000187NM 2003 2 20 QXEA0300289 120030217A33503017426 SIGN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 MISSING A QXEAK NONE O OTHER UKUNKNOWN 1 NM09407QX 4049 GEG-EXIT SIGN MISSING AT LOWER FORWARD CORNER OF EMERGEMCY EXIT DOOR, FORWARD RIGHT HAND SIDE OF CABIN. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001902003022000190NM 2003 2 20 AWXA200300165 120030203A534065538344 FITTING BOEING737 73733A 1384673NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW0 0 23634 LCQ - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON R/H FORWARD VERTICAL TO FUSELAGE ATTACH FITTING BS 1088. MAINTENANCE REMOVED CORRODED ATTACH FITTING BS 1088; FABRICATED A NEW REPLACEMENT ATTACH FITTING; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 6-8. 2L72 4F RTA16WE 20030221000052003022100005NM 2003 2 21 DHL2003751007 120030221A2611 SMOKE DETECTOR BOEING727 727264 138408MNM A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01751DH 22982 1) WHEN TURNING SMOKE DETECTOR OFF,#2 RED LIGHT ILLUMINATED2) CLEANED AND RESET CANNON PLUG SYS OPS CK GOOD PER MM 20-25-1 2L73 4F A3WE 20030221000062003022100006EA 2003 2 21 QXEA0300123 120030124A261247387202 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA FIRE DETECTION FAILED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09601QX1059 10009 PDX ON FLIGHT 2472- FIRE SYSTEM FAULT STATUS MESSAGE INTERMITTENTLY APPEARS. REMOVED AND REPLACED FIDEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030221000082003022100008EA 2003 2 21 QXEA0300124 120030124A2612474075 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA NR 2 ENGINE FAULTY A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09601QX116 10009 BOI ON FLIGHT 2550- INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 2 ENGINE UPPER, LOWER AND SIDE FIRE DETECTOR RAIL. FIRE DETECTOR SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030221000112003022100011NM 2003 2 21 AWXA200300060 120030109A5320654681282 WEB BOEING737 737300 1384610NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB IN VICINITY OF LT AFT LAVATORY POTABLE WATER AND SINK DRAIN LINES, BS 996, LBL 55, WL 208. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS PER B737-300 SRM 53-60-51, PG. 105, 108, & 112, FIG. 101. REMOVED CORRODED WEB BS 996, LBL 55, WL 208; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13, PG. 1, FIG. 1. 2L72 4F RTA16WE 20030221000212003022100021EU 2003 2 21 AWXA200300069 120030123A3830 LAVATORY AIRBUS320 A320232 3930326EU CABIN INOPERATIVE A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28653AW 1003 EN ROUTE FROM EWR TO PHX ALL FOUR LAVATORIES BECAME INOPERATIVE, DIVERTED TO ORD. SERVICING PERSONNEL SERVICED LAVATORIES AND DRAINED SYSTEM; RESET CIRCUIT BREAKERS FOR LAVATORY VACUUM SYSTEM, AND CLEARED BLOCKAGE FROM FORWARD LAVATORY; OPERATIONAL CHECK OF FORWARD AND AFT LAVATORIES GOOD. FLIGHT CONTINUED TO PHX WITHOUT FURTHER INTERRUPTION. 2L72 4F RTA28NM 20030221000392003022100039NM 2003 2 21 QXEA0300150 120030122A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- REMOVE AND REPLACE SEAT TRACK NR 11 DUE TO CORROSION AT STATION 455.5 WHICH APPEARS TO BE BEYOND BLENDABLE LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-40-00. 2H72 4T RTA13NM 20030221000412003022100041NM 2003 2 21 QXEA0300152 120030120A5220 SKIN DHAV DHC8 DHC8202 2809007NM ESCAPE HATCH GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NUMEROUS GOUGES IN SKIN ON ESCAPE HATCH. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36, 51-20-51 AND 51-20-11. 2H72 4T RTA13NM 20030221000572003022100057NM 2003 2 21 AWXA200300080 120030116A5310654681820 SILL BOEING737 737300 1384610NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND CABIN FLOORBOARD SILL ANGLE BS 639, LBL 56. MAINTENANCE FABRICATED REPAIR PLATES FOR CRACKED CABIN FLOORBOARD SILL ANGLE BS 639, LBL 56; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12, PG. 1-3, 6-7, FIG. 1. 2L72 4F RTA16WE 20030221000622003022100062EU 2003 2 21 AWXA200300082 120030107A5315D53112091200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND RT SIDE OUTBOARD TRACK BEAM EXTENSION OF CABIN FLOORBEAM FRAME 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; CUT OUT DAMAGED SECTION OF FLOORBEAM FR 16; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, PG. 103, FIG. 102. , PG. 203, 205-206, FIG. 201, AND SRM 51-47-00, PG. 2-3, FIG. 1, & TABLES 1 & 2.. 2L72 4F RTA28NM 20030221000652003022100065NE 2003 2 21 MALA030161 220030219A7320 HMU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE A MALAAE UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 GL15411XJ 340B411 ON FLIGHT #2941 GTR-MEM, RH ENGINE SHUTDOWN LEAVING FTR @ 6000 FT. DID NOT RELIGHT. INFLIGHT SHUTDOWN, AIR RETURN TO GTR. NORMAL TAKEOFF, DIALED DOWN CTOT TURNED OFF AUTOCOARSEN AND WENT THROUGH AFTER TO MEMORY ITEMS. CLIMBED TO 2000 FT, LEVELED OFF. ATC INSTRUCTED TO CL TO 6000 FT, SHORTLY THERE AFTER THERE WAD A LOUD BANG FROM RH ENGINE AND LAGE AC YAW. ALL ENGINE PARAMETERS BEGAN ROLLOING BACK, INCLUDING ITT. IGNITION LIGHT CAME ON BUT ENGINE DID NOT RELIGHT. MIKE DONAHUE/ENGINEER, NOTED HMU FAILURE. NO OTHER INFORMATION AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20030221000662003022100066NM 2003 2 21 QXEA0300186 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 9 SEAT TRACK HAS SCRATCHES AT STATION 531. REPAIRED IAW RD 8-53-4472 AND DHC-8 SRM 51-10-00. 2H72 4T RTA13NM 20030221000712003022100071SO 2003 2 21 C2XA03CL045 120030220A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715555 145594 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE #4 EMERGENCY LIGHT BATTERY CHARGER.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030221000722003022100072 2003 2 21 252TR0003 420030211A22004084042911 COUPLER BOEING737 737228 13844AGNM A PIDAK NONE O OTHER CRCRUISE 1 SO05252TR 23001 Yaw damper inop. Removed and replaced yaw damper coupler IAW MM 22-11-141. Ops. check good IAW MM 22-12-01. 2L72 4F RTA16WE 20030221000742003022100074NM 2003 2 21 QXEA0300188 120030126A5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CORROSION AT NUT PLATE HOLES ON TWO FLOOR SUPPORT CHANNELS BELOW COAT CLOSET. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 51-20-16, PAGE 7, PARAGRAPH B(5). 2H72 4T RTA13NM 20030220000602003022000060WP 2003 2 20 ABXA030061 120030129A3231 CONTROL CABLE DOUG DC8 DC861 3021952WP MLG DOOR OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23849AX 45891 GEAR RETRACTION RED GEAR LIGHT STAYED ON. LANDING GEAR RT DOOR LATCHING SELECTOR ON FLT ENGINEER'S PANEL SHOWED RT DOOR. CYCLED GEAR, LIGHTS WENT OUT. ADJUSTED RT MLG DOOR FOLLOW UP MECHANISM AND CABLES 135A & 134A IAW DC-8 MM 32-31-05. CHECKED RT MLG DOOR UPLATCH CLEARANCE AND DOOR DOWN CHECK IAW DC-8 MM 32-17-01 AND 32-31-01-5. OPS CHECKED GOOD IAW DC-8 32-31-05, 32-12-01 AND 32-31-04-5. 2L74 4F 4A25 20030220000612003022000061WP 2003 2 20 ABXA030062 120030207A3230174PH1 EYEBOLT DOUG DC8 DC863F 302198FWP LR MLG WORN A ABXAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 GL23811AX 46113 LT MLG WAS MAKING LOUD NOISE DURING RETRACT. ON SERVICE CHECK, FOUND LT MLG RETRACT CYLINGER EYE BOLT HAD EXCESSIVE PLAY. REWORKED PIN IAW 32-13-0001-001 NEA ON SHOP TRAVELER 5816-01. 2L74 4F 4A25 20030220000692003022000069WP 2003 2 20 ABXA030071 120030124A532099105035 WEB DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23957AX 47759 CUSP WEB CRACKED, LONGERON 18 LT, FS 1021 - 1041. REPLACED CUSP IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030220000792003022000079EA 2003 2 20 QXEA0300076 120030112A2781 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09607QX 10024 DEN ON FLIGHT 2445- INITIAL FLAP SELECTION RESULTED IN SLAT FAIL CAUTION MESSAGE. FOLLOWING CHECKLIST RESULTED IN SLATS WORKING FINE. COMPLIED WITH AMM TASK 27-50-00-710-801-A01. NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220000822003022000082NM 2003 2 20 QXEA0300078 120030112A3010 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09404QX 4046 GEG ON FLIGHT 2357- DE-ICE PRESSURE CAUTION LIGHT IN FLIGHT. ISOLATED SYSTEM AS PER CHECKLIST. ALL BOOT INDICATIONS WERE NORMAL. DE-ICE PRESSURE INDICATED 17 PSI ON NR 1 AND 21 PSI ON NR 2. OPERATIONAL TEST AS PER AMM 30-11-16-710-801 AND 30-11-31-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220000832003022000083NM 2003 2 20 DHL2003745006 120030219A3260 SWITCH BOEING727 727224 1384076NM A DHLAADO UNSCHED LANDING RETURN TO BLOCK OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 1) WHEN GEAR HANDLE WAS PLACED IN OFF POSITION AFTER GEAR RETRACTION, RED DOORS LIGHT AND RT GEAR DOOR LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. DOOR LIGHT OUT. GEAR DOOR LIGHT ON SO PANEL.2) REMOVED AND REPLACED RIGHT MLG DOOR SWITCH. OPS GOOD IAW 727 M/M 32-62-11. 2L73 4F A3WE 20030220000952003022000095NM 2003 2 20 QXEA0300090 120030115A3234574205 SELECTOR VALVE DHAV DHC8 DHC8202 2809007NM LANDING GEAR MALFUNCTIONED A QXEAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 NM09379PH1671 1671 530 PDX ON FLIGHT 2277- WHEN LANDING GEAR SELECTED DOWN FOR LANDING, GEAR DID NOT EXTEND. DID GET RED UNSAFE LIGHTS AND LIGHT IN THE HANDLE. LEVELED OFF AND ADDED POWER TO GO AROUND AND GEAR CAME DOWN APPROXIMATELY 30 SECONDS AFTER ORIGINALLY SELECTED DOWN. GEAR DID NOT RETRACT ON GO AROUND. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220000972003022000097EU 2003 2 20 DHL2003366002 120030219A26103500813 CONTROLLER AIRBUS300 A300B4203 3930306EU A DHLADO RETURN TO BLOCK OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01366DH 249 1) ENGINE AND APU MANIFOLD LIGHTS ILLUMINATED. PERFORMED ABNORMAL PROCEDURES.2) REMOVED AND REPLACED #1 OVERHEAT DETECTION CONTROL UNIT IAW 26-16-00. OPS CHECKED GOOD ON GROUND. 2L72 4F RTA35EU 20030220001072003022000107NM 2003 2 20 QXEA0300102 120030119A3260301450201 PSEU BOMBDRDHC8 DHC8401 1390041NM RT MLG MALFUNCTIONED A QXEAK NONE J WARNING INDICATION UKUNKNOWN 1 NM09411QX2609 4055 PDX-RIGHT HAND AFT GEAR DOORS REMAIN OPEN AFTER GEAR EXTENSION. REMOVED AND REPLACED PROXIMITY SENSING ELECTRONIC UNIT. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001082003022000108NE 2003 2 20 QXEA0300103 220030120A72504124T3P03 TURBINE BLADES GE CG348C1 CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX2468 GEE965279 10019 E965279 PDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT BLADES 1/3 MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRETIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030220001102003022000110EA 2003 2 20 QXEA0300105 120030117A261247359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY FAILED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09614QX1321 1321 10049 SUP PDX ON FLIGHT 2490- INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 3 CARGO SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220001132003022000113EA 2003 2 20 QXEA0300108 120030121A2824P93C13604 CARTRIDGE CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAILED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09604QX2484 10019 BOI-CROSSFLOW PUMP CAUTION. REMOVED AND REPLACED BI-CROSS FLOW PUMP CARTRIDGE. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220001152003022000115EA 2003 2 20 QXEA0300111 120030121A2820D98007606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS UKUNKNOWN 1 NM09609QX2480 10031 SEA-ON FLIGHT NUMBER 2504, FUEL LEAKING FROM BOTTOM OF FUSELAGE ON CENTER LINE BETWEEN MAIN GEAR AND JUST BEHIND TRAILING EDGE OF WING. REMOVED AND REPLACED RIGHT HAND NR 2 ENGINE INLET FUEL PRESSURE SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220001192003022000119EA 2003 2 20 QXEA0300115 120030122A2820D98C07606 SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM MALFUNCTIONED A QXEAK NONE J WARNING INDICATION UKUNKNOWN 1 NM09609QX7 10031 LGB-ON FLIGHT NUMBER 2502, RIGHT FUEL LOW PRESSURE CAUTION MESSAGE. REMOVED AND REPLACED NR 2 ENGINE LOW PRESSURE SWITCH. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030220001292003022000129EA 2003 2 20 QXEA0300122 120030125A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09601QX 10009 BOI- CENTER CHIMNEY IN FORWARD CARGO PIT DAMAGED. REMOVED AND REPLACED CENTER CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030221000752003022100075NM 2003 2 21 QXEA0300189 120030120A5320 ANGLE DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CORROSION ON ANGLE AT OUTBOARD SIDE OF NR 4 SEAT TRACK AT X-222, Y-LT10, Z-100. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 51-20-16, SRM 51-20-36 AND SRM 51-40-11. 2H72 4T RTA13NM 20030221000762003022100076NM 2003 2 21 AWXA200300169 120030128A5532175N2001 PANEL BOEING757 7572S7 1384962NM DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 64" X 32" AREA OF R/H VERTICAL STABILIZER FORWARD LOWER COMPOSITE SKIN PANEL WAS FOUND DELAMINATED AT VERTICAL FIN STA 105 - 175. MAINTENANCE REMOVED R/H VERTICAL STABILIZER FORWARD LOWER COMPOSITE SKIN PANEL AT VERTICAL FIN STA 105 - 175; INSTALLED A REPAIRED VERTICAL STABILIZER FORWARD LOWER COMPOSITE SKIN PANEL IAW DWG 175N2001, & AWA E.R 19-5534-03046-SS2. 2L72 4F RTA2NM 20030221000802003022100080NM 2003 2 21 AWXA200300174 120030129A5315146N5444 FLOOR SUPPORT BOEING757 7572S7 1384962NM -N/A- CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT FRAME BS 1510, LBL 2. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT FRAME BS 1510, LBL 2; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030221000822003022100082NM 2003 2 21 AWXA200300176 120030129A5315146N5444 FLOOR SUPPORT BOEING757 7572S7 1384962NM -N/A- CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT FRAME BS 1510, RBL 2. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT FRAME BS 1510, RBL 2; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030223000072003022300007SO 2003 2 23 C2XA03SH017 120030222A530014525994001 CROSSBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND LEFT HAND FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030223000102003022300010SO 2003 2 23 C2XA03SH010 120030222A530014525422001 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030224000012003022400001GL 2003 2 24 ALGA084074 220030203A7250 BEARING RACE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL TURBINE CORRODED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO FOUND CORROSION PITTING ON POWER TURBINE SHAFT INNER RACE. 1Q71 3R3 U 2A6 E1GL 20030224000022003022400002GL 2003 2 24 ALGA084090 220030205A725023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL TURBINE GOUGED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO FOUND DEEP GOUGES ON SPLINES OF N1 COUPLING ON POWER TURBINE. 1Q71 3R3 U 2A6 E1GL 20030224000042003022400004GL 2003 2 24 ALGA084097 220030207A724023030911 COMBUST CHAMBER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE CRACKED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01408AL1653 53491 CAE847537 CRACKED. EXCESSIVE CORROSION ON ARMPIT AT PATCH AREA, POSSIBLY CAUSED BY BRAZE FILLER MATERIAL. CRACK FOLLOWS WELD SEAM AND EXTENDS INTO PATCH. SCRAPPED PART. HOLDING FOR FINAL DISPOSITION. 1G71 3U3 UO H2SW E1GL 20030224000052003022400005 2003 2 24 ALGA084106 420030210A34201418523122 INDICATOR BELL 412 412EP 1182205SW ADI INCORRECT H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01XAAAR54 36255 INCORRECT INDICATIONS ON ADI- PART TT: 54.20. 1G72 4U H4SW 20030224000072003022400007SW 2003 2 24 ALGA084114 120030211A6420214011801127 ROTOR HEAD BELL 214 214ST 1182106SW TAIL ROTOR WORN H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01392AL6142 28114 TAIL ROTOR HEAD REMOVED DUE TO YOKE FEATHERING, BEARING BORE WORN BEYOND LIMITS. 2G72 4U H10SW 20030224000082003022400008GL 2003 2 24 ALGA084128 220030212A720023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C47B GL ENGINE GOUGED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO CAE847537 FOUND GOUGES ON CROWNS OF SPLINES OF N1 COUPLING, NEAR ADAPTER MATING SURFACE. 1Q71 3R3 U 2A6 E1GL 20030224000092003022400009GL 2003 2 24 ALGA084131 220030213A720023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE GOUGED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO FOUND SPLINES DAMAGED FROM MAUFACTURING PROCESS OF N1 COUPLING. 1Q71 3R3 U 2A6 E1GL 20030224000262003022400026WP 2003 2 24 MWEA030109 120030221A5320591016398 ANGLE DOUG DC9 DC981 3022081WP LONGERON 18 RH CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 SHEAR TIE CRACKED AT LONGERON 18 RIGHT. -- FABRICATED AND INSTALLED REPLACEMENT ANGLE. 2L72 4F A6WE 20030224000362003022400036NE 2003 2 24 HEEA084157 220030212A73200164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE ENGINE LEAKING E O OTHER O OTHER NRNOT REPORTED 1 SW0322342 760096 FUEL CONTROL LEAKING. 1G72 3U3 U H1NE E19EU 20030224000412003022400041 2003 2 24 HEEA084162 420030212A34215040017928 INDICATOR SKRSKYS76 S76A 8143006NE STANDBY ATTITUDEMALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 STANDBY ATTITUDE INDICATOR WILL NOT ERECT. IN SHOP REPAIR. 1G72 3U H1NE 20030224000582003022400058 2003 2 24 HEEA084179 420030212A34217660002113103 GYRO SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 VERTICAL GYRO KICKING IN THE NR 1 PITCH AFCS CHANNEL. 1G72 3U H1NE 20030224000692003022400069WP 2003 2 24 0300281240 120030222A5312 ATTACH ANGLE DOUG DC10 DC1030 3023501WP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01240NW 48319 During "L" check found crack in fuselage bulkhead upper attach angle at BS 2122.8. Repaired per EA 12-194259. 2L73 4F A22WE 20030224000702003022400070EU 2003 2 24 NSVA200300007 120030222A26001734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE TAIL PIPE INTERMITTENT A NSVADC RETURN TO BLOCK ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27239CJ3380 340B239 785311 LGA-On take off roll, RH engine "Tail Pipe Hot" light illuminated. Take off was aborted, aircraft taxied back to gate. MX performed ground run, light did not illuminate, OP's check good. Aircraft returned to service, suspect moisture interfred with operation of sensor. 2L72 4T4 TRTA52EU E8NE 20030224000732003022400073GL 2003 2 24 HEEA084193 220030213A73210164248800 FUEL CONTROL AEROSPAS355 AS355* EU ALLSN 250C 250C* GL ENGINE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03974AE1699 2653 FUEL CONTROL HAS A FUEL LEAK INTO P3 LINE TO SCROLL. 1G72 3U3 U H11EU E4CE 20030224000742003022400074EU 2003 2 24 HEEA084194 120030213A71000292005340 ENGINE AEROSPAS355 AS355* EU ALLSN 250C 250C* GL MAKING METAL E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03973AE1926 3229 ENGINE CHIP LIGHT ILLUMINATED, FOUND NUMEROUS FLAKES AND CHIPS ON ELECTRICAL PLUG AND MO1 MAGNETIC PLUG. 1G72 3U3 U H11EU E4CE 20030224000792003022400079NE 2003 2 24 HEEA084200 120030213A63207635109011105 BEVEL GEAR SKRSKYS76 S76A 8143006NE M/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322342970 A08100268 760096 MAIN ROTOR GEARBOX BEVEL GEAR HAS HEAVY FROSTING AND PITTING - GEAR WAS LOAD TESTED AND ACCEPTED PRIOR BY SIKORSKY PER SO DF 624-0001 ON APRIL 18, 2001. TO BE SENT TO VENDOR. 1G72 3U H1NE 20030224000812003022400081NE 2003 2 24 HEEA084202 120030213A63207635109132102 PINION GEAR SKRSKYS76 S76A 8143006NE M/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322342970 A08100268 760096 MAIN ROTOR GEARBOX PINION GEAR HAS HEAVY FROSTING AND PITTING - GEAR WAS LOAD TESTED AND ACCEPTED PRIOR BY SIKORSKY PER SO # DF 624-0001 ON APRIL 18, 2001. TO BE SENT TO VENDOR. 1G72 3U H1NE 20030224000832003022400083 2003 2 24 HEEA084204 420030213A34578143902240B GPS SKRSKYS76 S76A 8143006NE COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 GPS INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20030224000942003022400094SW 2003 2 24 HEEA084215 120030120A5320407070620125 PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030224000952003022400095SW 2003 2 24 HEEA084216 120030120A5320407070620131 PANEL BELL 407 407 1182206SW CONTROL COLUMN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 CONTROL COLUMN PANEL CRACKED. 1G71 3U O H2SW 20030224001012003022400101EA 2003 2 24 COMA0360109 120030219A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER S AFFECT SYSTEMS APAPPROACH 1 SO01957CA17536 7109 FLIGHT 5575 NLG FAILED TO EXTENDREPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030224001122003022400112WP 2003 2 24 CALA0300061 120030221A5350 CABLE DOUG DC9 DC982 3022082WP TAILCONE FRAYED A CALAK NONE O OTHER ININSP/MAINT 1 SW0972822 49482 THE TAILCONE FAILED TO SEPARATE FROM AIRCRAFT WHEN USING AFT ENTRANCE DOOR TO DEPLOY TAILCONE. FOUND L/H TAILCONE RELEASE CABLE FRAYED IN TWO PLACES WHERE IT PASSES OVER UPPER PULLEY. REPLACED CABLE AND PERFORMED ADJUSTMENT TEST OF TAILCONE SYSTEM IAW MM 53-53-00. 2L72 4F A6WE 20030625000982003062500098NM 2003 6 25 F3LA200300079 120030219A5320 INTERCOSTAL BOEING727 727247 138408FNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03291WA 3501 22109 DURING C-4 CHECK, INSPECTION REPORTED LT. INTERCOSTAL BETWEEN STA. 947.5 AND STA. 967 CORRODED AT APPROXIMATELY LBL 48. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-178 AND SRM 51-30-02. 2L73 4F A3WE 20030224001302003022400130WP 2003 2 24 ZW0A0302601 120030219A3350105606003 HARNESS DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139619V 53566 DURING OVERNIGHT INSPECTION SIX WHITE AND ONE RED EGRESS FLOOR LIGHT INOP ON CABIN FLOOR. REPLACED BROKEN HARNESS 105606-003 CPN 4096971 BETWEEN ROW 24 AND 25 ALSO SEATED BULBS INTO SOCKETS AS REQUIRED. OPS CHEK NORMAL PER MD80 MM33-53-01. CHECK-C MCI 10-30-02. --CLOSED-- 2L72 4F RTA6WE 20030224001332003022400133NM 2003 2 24 AWXA200300182 120030221A3350BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 16 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW0 0 22655 AUS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030224001412003022400141NM 2003 2 24 AWXA200300192 120030216A5320146N5417 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON NUT PLATES OF FLOOR SUPPORT BS 1346 - 1363, RBL 16. MAINTENANCE REMOVED CORRODED SECTION OF FLOOR SUPPORT BS 1346 - 1440, RBL 16; FABRICATED A NEW FLOOR SUPPORT; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 11-12. 2L72 4F RTA2NM 20030224001432003022400143NM 2003 2 24 AWXA200300194 120030216A5320146N5416 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON NUT PLATES OF FLOOR SUPPORT BS 1330, RBL 7. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED AREA ON FLOOR SUPPORT BS 1330, RBL 7; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-2, & 4-6. 2L72 4F RTA2NM 20030224001492003022400149NM 2003 2 24 AWXA200300201 120030206A531369353521 TIE CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 639, STR 1 L/H. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 639, STR 1 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 8, PG. 38, AND SRM 51-40-05, PG. 1-4, FIG. 1 & 2, AND PG. 7, FIG. 4. 2L72 4F RTA16WE 20030224001512003022400151NM 2003 2 24 AWXA200300203 120030217A53126545402582 STIFFENER BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STIFFENER AT R/H AIR CONDITIONING BAY AFT BULKHEAD JUST ABOVE THE TURBO FAN EXHAUST DUCT. MAINTENANCE REMOVED CRACKED STIFFENER AT R/H AIR CONDITIONING BAY AFT BULKHEAD JUST ABOVE THE TURBO FAN EXHAUST DUCT BS 727; FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11. 2L72 4F RTA16WE 20030625001052003062500105NM 2003 6 25 F3LA200300086 120030220A5320 INTERCOSTAL BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA. 927 AND STA. 947.5 ON RT. SIDE OF AIRCRAFT CENTERLINE CORRODED. REMOVED CORROSION AND INTERCOSTAL PER SRM 51-30-02. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 51-10-06. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL AND SHIM PER EA 53-737-198 AND SRM 51-30-02. 2L72 4U RTA16WE 20030225000042003022500004SO 2003 2 25 C2XA03SH026 120030225A530014525480003 BEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-06.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030225000062003022500006SO 2003 2 25 C2XA03SH024 120030225A530014530633003 BEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-22-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030225000082003022500008SW 2003 2 25 HEEA084227 120030120A5210407070620151 PANEL BELL 407 407 1182206SW PAX/CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 CREW/PAX DOOR PANEL CRACKED. 1G71 3U O H2SW 20030225000112003022500011SW 2003 2 25 HEEA084230 120030120A5320407070620155 PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 CRACKED. TO BE SENT TO BELL FOR CREDIT. 1G71 3U O H2SW 20030225000132003022500013SW 2003 2 25 HEEA084232 120030120A5320407070620156 HEADLINER BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 HEADLINER CRACKED. 1G71 3U O H2SW 20030225000182003022500018SW 2003 2 25 HEEA084237 120030120A5210407070620158 PANEL BELL 407 407 1182206SW PAX/CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 PAX/CREW DOOR PANEL CRACKED. 1G71 3U O H2SW 20030225000222003022500022SW 2003 2 25 HEEA084241 120030120A5320407070620179 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030114000562003011400056 2003 1 14 SWAA030003 420030101A256565C19901 CABLE BOEING737 7372H4 138448CNM AFT SVC DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030114000572003011400057NM 2003 1 14 SWAA030004 120030102A551065C25727 SKIN BOEING737 7373H4 1384600NM LT HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB CRACKED ON LOWER SKIN AT STA 125 JUST FWD OF REAR SPAR. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20030306000262003030600026 2003 3 6 HEEA084739 420030217A2340 SWITCH BELL 412 412 1182202SW INTERPHONE BOX DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 8512098 36007 STATIC IN ICS. FOUND SWITCH S1 HAS BLEEDOVER, VOLUME KNOB, SELECTOR KNOB, AND AMP BOARD AR1 BAD. CLEANED SWITCH S1 AND REPLACED VOLUME KNOB AND AMP BOARD AR1. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000292003030600029SW 2003 3 6 HEEA084742 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 STEP ACTUATOR INOPERATIVE. REPAIRED. 1G72 4U H4SW 20030306000392003030600039SW 2003 3 6 HEEA084752 120030218A3210407030112103 FITTING BELL 407 407 1182206SW MLG DAMAGED E O OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 AFT CROSSTUBE SLIPPED IN FITTING, CAUSING DAMAGE TO FITTING, STRAP AND CROSSTUBE. REPLACED FITTING. 1G71 3U O H2SW 20030306000462003030600046SW 2003 3 6 HEEA084760 120030218A3210407030112103 FITTING BELL 407 407 1182206SW MLG CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 FITTING CHAFED. REPLACED FITTING. 1G71 3U O H2SW 20030306000542003030600054SW 2003 3 6 HEEA084769 120030221A3246412050016101 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 SKID SHOE IS WORN. REPAIRED. 1G72 4U H4SW 20030306000722003030600072SW 2003 3 6 HEEA084783 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 STEP ACTUATOR WILL NOT RETRACT. 1G72 4U H4SW 20030306000732003030600073SW 2003 3 6 HEEA084784 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 STEP ACTUATOR WILL NOT COME UP INTERMITTENTLY. 1G72 4U H4SW 20030306000762003030600076SW 2003 3 6 HEEA084787 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 STEP ACTUATOR HAS ERRATIC OPERATION (INTERMITTENTLY). 1G72 4U H4SW 20030306000782003030600078EU 2003 3 6 DHL2003364005 120030306A2610 CONTROLLER AIRBUS300 A300B4203 3930306EU A DHLAKO NONE OTHER O OTHER APAPPROACH 1 SO01364DH 141 1) LEFT BLEED VALVE MANIFOLD FAULT, AND APU MANIFOLD FAULT LIGHTS ILLUMINATED DURING APPROACH WITH WING DE-ICE IN USE. COMPLIED WITH ABNORMAL PROCEDURES AND LIGHTS EXTINGUISHED.2) COULD NOT DUPLICATE DISCREPANCY. REPLACED LEFT CFD CONTROLLER FOR TROUBLESHOOTING IAW M/M 26-16-11. OPS CHECK IS GOOD AT THIS TIME. 2L72 4F RTA35EU 20030306000812003030600081SW 2003 3 6 HEEA084791 120030221A6730212076004101 SERVO BELL 412 412 1182202SW TAIL ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033893N 33010 TAIL ROTOR SERVO LEAKING. REPAIRED. 1G72 4U H4SW 20030306000832003030600083SW 2003 3 6 HEEA084793 120030221A6730212076005105 SERVO BELL 412 412 1182202SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033893L 33006 MAIN ROTOR SERVO HAS EXCESSIVE LEAKING. 1G72 4U H4SW 20030306000892003030600089SW 2003 3 6 HEEA084798 120030221A5260222036044102 STEP BELL 412 412 1182202SW AIR STAIR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 STEP CRACKED. SCRAPPED. 1G72 4U H4SW 20030306001002003030600100SW 2003 3 6 HEEA084807 120030221A6220412010101127 YOKE BELL 412 412 1182202SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 VERY ROUGH VIBRATION IN FLIGHT. WILL NOT TRACK OUT. RADS GEAR CALLS FOR VERY LARGE AMOUNT OF WEIGHT ON THE BLUE SPINDLE. REPAIRED. 1G72 4U H4SW 20030306001042003030600104SW 2003 3 6 HEEA084811 120030221A2510412070820101 SEATBACK CUSHION BELL 412 412 1182202SW CREW SEAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 SEAT BACK CUSHION WORN. REPAIRED. 1G72 4U H4SW 20030306001102003030600110SW 2003 3 6 HEEA084817 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MAIN ROTOR HEAD ROD BEARING WORN BEARING. SCRAPPED. 1G72 4U H4SW 20030306001142003030600114NM 2003 3 6 03063427 120030304A2612SD947022 SMOKE DETECTOR DORNERDO32 DO328300 NM A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27427FJ 3192 During climb, the crew reported a cargo fire indication. An emergency was declared, the fire extinguishers were discharged, the aircraft returned to CVG and landed without incident. Maintenance personnel removed and replaced the baggage compartment smoke detector and both fire extinguisher bottles. The aircraft was returned to service. 2H72 4T RTA55NM 20030306001212003030600121SW 2003 3 6 HEEA084823 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MAIN ROTOR HEAD HAS A WORN ROD BEARING. 1G72 4U H4SW 20030307000012003030700001SO 2003 3 7 C2XA03SH034 120030307A530014522380001 SKIN EMB 145 EMB145LR 3260212SO CARGO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV- DURING C CHECK CORROSION WAS FOUND ON CARGO FLOOR SKIN BETWEEN FRAMES 68 AND 73 AT STRINGERS 21L AND 20R. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030307000032003030700003SO 2003 3 7 C2XA03SH36 120030307A530014534608007 SKIN EMB 145 EMB145LR 3260212SO CARGO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK CORROSION WAS FOUND ON CARGO FLOOR SKIN BETWEEN FRAMES 61 AND 65 AT STRINGERS 21L TO 20R. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EC 5330-01234 AND EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030307000042003030700004SO 2003 3 7 C2XA03SH39 120030307A523014529611003 DOOR FRAME EMB 145 EMB145LR 3260212SO CARGO DOOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV- DURING C CHECK THE AFT EXTERNAL FRAME ON CARGO DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030307000052003030700005SO 2003 3 7 C2XA03SH40 120030307A530014533826003 SKIN EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK CORROSION WAS FOUND ON THE CABIN UNDERFLOOR SKIN BETWEEN FRAMES 50 AND 61. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030307000082003030700008 2003 3 7 HEEA084878 420030227A2312064100900 TRANSCEIVER SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 TRANSCEIVER HAS A SQUELCH PROBLEM. SHOP REPAIR. 1G72 3U H1NE 20030307000122003030700012 2003 3 7 HEEA084882 420030227A34211113034 INDICATOR SKRSKYS76 S76A 8143006NE ADI MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 COPILOT ADI WILL NOT ERECT PROPERLY. SENT TO MASCO FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030307000292003030700029NM 2003 3 7 SWAA030477 120030303A3350W1150B1 WIRE BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D CHECK, FOUND LOOSE CONNECTOR WIRE AT RT OVERWING EXIT LIGHT. REPAIRED WIRE PER WDM. 2L72 4F RTA16WE 20030307000322003030700032NM 2003 3 7 SWAA030480 120030303A53116546548 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO COMPT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND FRAME SHEAR TIE CORRODED AT BS 747, WL 150, RBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030307000342003030700034NM 2003 3 7 SWAA030482 120030303A53116547951 FRAME BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR AFT CUT OUT FRAME CRACKED NEXT TO LOWEST STOP FITTING CASTING. REPAIRED FRAME PER SWA T1-653-044 2L72 4F RTA16WE 20030307000402003030700040 2003 3 7 SWAA030455 420030301A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE ASSY'S OUT OF ADJUST. ADJUSTED SLIDE ASSY'S PER MM. 2L72 4F RTA16WE 20030307000482003030700048NM 2003 3 7 SWAA030466 120030228A53126546568 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED (4 EA) AT 8, 9, 10 AND 11.30 O'CLOCK POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA. 2L72 4F A16WE 20030307000502003030700050NM 2003 3 7 SWAA030468 120030228A52106545871 DOOR FRAME BOEING737 7373T5 1384608NM FWD ENTRY DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT 6TH FROM TOP STOP PIN CASTING ASSY. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030307000562003030700056NM 2003 3 7 SWAA030444 120030227A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED (9 EA) THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030307000592003030700059NM 2003 3 7 SWAA030447 120030226A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT SECOND RADIO ALTIMETER ANTENNA CUTOUT, AT BS 410, LEFT OF BL 0. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030307000632003030700063 2003 3 7 SWAA030413 420030220A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 DURING SCHEDULED BC4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030307000652003030700065NM 2003 3 7 SWAA030416 120030223A335007912 COVER BOEING737 7377H4 1384404NM FWD CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW NR 1. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20030307000722003030700072NM 2003 3 7 SWAA030486 120030304A53306545773 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 767, STRINGER 14R. REPAIRED SKIN PER ERO. 2L72 4F RTA16WE 20030307000742003030700074NM 2003 3 7 SWAA030488 120030304A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 360, BETWEEN STRINGERS 8R AND 9R AND BETWEEN STRINGERS 13L AND 14L, AND BS 440, BETWEEN STRINGERS 8R AND 9R. REPAIRED FRAME SECTIONS PER ER AND SRM. 2L72 4F RTA16WE 20030307000802003030700080NM 2003 3 7 VNAA0303003 120030304A24001060003 BPCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07458PS158898120 3068 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030307000852003030700085WP 2003 3 7 CALA0300100 120030306A5320 WEB DOUG DC9 DC982 3022082WP STA 1338 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 INSPECTION FOUND WEB AT STA 1338 AFT PRESSURE BULKHEAD T-CAP CORRODED. THE CORRODED SECTION OF WEB WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-4, FIGURE 1. 2L72 4F A6WE 20030307000932003030700093NE 2003 3 7 HEEA084895 120030227A62207610600701102 BOLT SKRSKYS76 S76A 8143006NE M/R DAMPER MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 MAIN ROTOR DAMPER BOLT SHANK IS .001 LARGER THAN THE BEARING I.D. THE BOLT HAS TO GO THROUGH. REPLACED BOLT. 1G72 3U H1NE 20030307000952003030700095NE 2003 3 7 HEEA084896 120030227A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 MAIN ROTOR BLADE HAS A HOLE IN THE TIP CAP. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030307000962003030700096NM 2003 3 7 A6WA200330002 120030210A3260870004 PSEU DORNERDO32 DO328100 2996000NM E/E BAY FAILED A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31331MX6209 3074 PSEU SYSTEM FAILURE IN FLIGHT. MULTIPLE INDICATIONS FAIL HYDRAULIC, GEAR, GROUND SPOILER PROXIMITY WOW AND AOA. INSTALLED PSEU. (M) 2H72 4T RTA45NM 20030307001022003030700102NE 2003 3 7 HEEA084901 120030228A6220 BEARING SKRSKYS76 S76A 8143006NE BELLCRANK RATCHETING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792CH 760193 MAIN ROTOR BELLCRANK BEARING RATCHETY. REPLACED BEARINGS. REPAIRED. 1G72 3U H1NE 20030307001152003030700115NM 2003 3 7 AALA20030041 120030109A1420 SPLICE BOEING757 757223 1384957NM CABIN UNSECURE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21628AA 24586 LAX - RIGHT EMERGENCY LIGHTS AT SEATS 1E TO 6E INOPERATIVE. RESECURED WIRE SPLICE AT EMERGENCY EXIT SIGN AT THE L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001182003030700118NE 2003 3 7 HEEA084903 120030228A67103895000907104 BEARING SKRSKYS76 S76A 8143006NE BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792CH 760193 COLLECTIVE TO PITCH BELLCRANK BEARINGS WORN. REPLACED 2 BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030307001202003030700120NM 2003 3 7 AALA20030084 120030118A2750 TRANSMISSION BOEING757 757223 1384957NM T/E FLAP LACK OF LUBE A AALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW21660AM 25294 MIA - FLT 2040 - EN ROUTE DEN-MIA - TRAILING EDGE FLAP DISAGREE WHEN FLAP HANDLE WAS MOVED FROM 15 TO 20 DEGREES. FLAPS STUCK AT 17 DEGREES INITIALLY. FLAPS AT 20 DEGREES FOR LANDING. LANDED MIA WITHOUT INCIDENT. FLAP TRANSMISSION INDICATOR CIRCUIT BREAKER POPPED AT NR 2 FLAP TRANSMISSION, LEFT WING. RESET FLAP TRANSMISSION INDICATOR AND ADVISED TECH SERVICES. FOUND NR 1, 2 AND 5 FLAP TRANSMISSION REQUIRED SERVICING. SERVICED TRANSMISSIONS AND CYCLED FLAPS SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001262003030700126WP 2003 3 7 AALA20030098 120030120A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 TUL - FOUND CORROSION IN LOWER CHANNEL AND LIP OF FRAME. BLENDED OUT CORROSION. TREATED AND PRIMED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-14 PAGE NR 1. (M) 2L72 4F A6WE 20030307001392003030700139NM 2003 3 7 AALA20030110 120030124A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21384AA 26996 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001462003030700146NM 2003 3 7 AALA20030149 120030203A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21393AN 29430 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 40H INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001552003030700155EA 2003 3 7 030466621 120030215A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27662BR 7526 RT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY EXIT LIGHTING BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2L72 4F4 FRTA21EA E15NE 20030307001692003030700169NM 2003 3 7 AALA20030050 120030112A3350 SOCKET BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT SOCKET ON SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001712003030700171NM 2003 3 7 AALA20030052 120030112A3350 SOCKET BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET ON SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001732003030700173NM 2003 3 7 AALA20030054 120030113A3350 LIGHT BOEING767 767323 1385205NM CABIN MALFUNCTIONED A AALAK NONE O OTHER CRCRUISE 1 SW21361AA 24042 LHR - FLT 46 - EN ROUTE ORD-LHR, DURING FLIGHT EMERGENCY EXIT LIGHTS ILLUMINATED FOR 2 MINUTES THEN EXTINGUISHED. LANDED LHR WITHOUT INCIDENT. CYCLED EMERGENCY EXIT LIGHT SWITCH OFF THEN ARMED AND ACCOMPLISHED EMERGENCY EXIT LIGHT TEST, ALL LIGHTS FUNCTION AS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001832003030700183EU 2003 3 7 AALA20030072 120030117A3350 PIN FOKKERF28 F28MK0100 4990807EU CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW211429G 11414 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE STANDBY LIGHTS AT ROW 12 INOPERATIVE. REPLACED PIN ON ROW 12 EMERGENCY EXIT AISLE STANDBY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030307001872003030700187NM 2003 3 7 AALA20030076 120030118A3350 LIGHT BOEING757 757223 1384957NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21685AA 25342 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT FLOOD LIGHT IS DISCONNECTED. RECONNECTED FORWARD GALLEY EMERGENCY EXIT FLOOD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001942003030700194GL 2003 3 7 HEEA084911 220030228A753223073356 POPPET VALVE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL BLEED VALVE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FF40257 RECEIVED FROM STOCK AND FOUND END OF VALVE SURFACE VERY UNEVEN. VALVE WOULD NOT SEAT IN UNIT. 1Q71 3R3 U 2A6 E1GL 20030307001982003030700198 2003 3 7 HEEA084913 420030227A34251113025 INDICATOR BELL 412 412 1182202SW HSI MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 FLIGHT DIRECTOR HUNTS IN ROLL AXIS WHEN COUPLED. 1G72 4U H4SW 20030307001992003030700199NM 2003 3 7 C1HA200381006 120030212A3350 BULB BOEING727 7272S7 138407ZNM A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15681CA 22020 ON A CHECK FOUND R1 LOWER FWD EXIT SIGN INOP.RELAMPED OPS NORMAL. 2L73 4F A3WE 20030307002002003030700200SO 2003 3 7 C2XA03BT033 120030304A3350209 LIGHT EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2716918 145397 BTV---CO2491, DURING SERVICE/ROUTINE FOUND OVERHEAD EMERGENCY LIGHT AT MAIN ENTRANCE DOOR TO BE INOPERATIVE....MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT IAW EMB145 AMM 33-50-06. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20030307002042003030700204NM 2003 3 7 C1HA200397006 120030205A3350 BATTERY PACK BOEING727 727270 138408PNM CABIN DISCHARGED A C1HAK NONE O OTHER CRCRUISE 1 GL15697CA 23052 NR 3 O/H EMERGENCY EXIT LIGHT INOP AT ROW 20 WITH LITE SWITCH ON AND NO SMOKING SWITCH OFF. R&R'D BATTERY PACK IAW MM 33-50-101 LIGHTS OPS CHECK GOOD. 2L73 4F RTA3WE 20030308000022003030800002SO 2003 3 8 RAIA00302048 120030216A304090024252 CONTROLLER EMB 145 EMB145 3260210SO INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03804HK9467 145082 5278-PIT-LEFT WINDSHIELD WIPER INOP. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD CONTROLLED, OPS CK OK. 2L72 4F RTT00011AT 20030308000032003030800003EU 2003 3 8 RAIA00302049 120030218A274145150561 PROBE AEROSPATR42 ATR42300 8680920EU SHORTED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03422TE109693596 106 5464-STL- RIGHT AOA CB POPPED. MAINTENANCE REMOVED AND REPLACED THE RIGHT AOA PROBE, OPS CK OK. 2H72 4T RTA53EU 20030309000012003030900001EU 2003 3 9 RAIA00302059 120030227A3222D56797 AXLE AEROSPATR42 ATR42300 8680920EU BROKEN A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03421TE 102 5555- SBN- RIGHT HAND WHEEL ON NOSE LANDING GEAR WAS DISCOVERED MISSING DURING TAXI FOR PARKING AT STL. THE NLG AXLE BROKE, MAINTENANCE REMOVED AND REPLACED THE NLG AXLE AND INSTALLED NLG WHEEL AND TIRES. 2H72 4T RTA53EU 20030310000022003031000002SO 2003 3 10 C2XA03SH047 120030310A530014527610015 BRACKET EMB 145 EMB145LR 3260212SO CARGO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK CORROSION WAS FOUND ON PULLEY BRACKETS BETWEEN FRAMES 67 TO 68, BETWEEN STRINGERS 21 LEFT AND 20 RIGHT. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030310000032003031000003SO 2003 3 10 C2XA03SH045 120030310A530014528737001 STRINGER EMB 145 EMB145LR 3260212SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 TO 53. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030310000082003031000008 2003 3 10 HEEA084917 420030227A34211113034 INDICATOR BELL 412 412 1182202SW ATTITUDE UNRELIABLE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ATTITUDE INDICATOR UNRELIABLE. DURING GROUND CHECKS UNIT WOULD NOT ERECT. 1G72 4U H4SW 20030310000242003031000024SW 2003 3 10 HEEA084933 120030227A6520204040506003 ADAPTER BELL 412 412 1182202SW T/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03800Y 13761 AFS932 33134 LEAKING OIL FROM PITCH CONTROL SHAFT THROUGH CAVITY. REPAIRED. REPLACED ADAPTER DUE TO WORN AND CAP ASSY 204040502009 DUE TO WORN. 1G72 4U H4SW 20030310000292003031000029SW 2003 3 10 HEEA084938 120030227A7120 BEARING BELL 412 412 1182202SW TRIPOD ASSY GROOVED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ENGINE MOUNT TRIPOD BEARINGS ARE GROOVED. REPAIRED. 1G72 4U H4SW 20030310000332003031000033SW 2003 3 10 HEEA084942 120030227A7120212061108003 BEARING BELL 412 412 1182202SW BIPOD ASSY GROOVED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 BIPOD ASSY BEARINGS GROOVED. SCRAPPED. 1G72 4U H4SW 20030310000402003031000040SW 2003 3 10 HEEA084947 120030227A3213212321103 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 CROSSTUBE DEEP PITS OF CORROSION NEAR MOUNTING FOR STEPS .015 DEEP BEFORE CLEAN WHICH MAKES IT OUT OF LIMITS. SCRAPPED. 1G72 4U H4SW 20030310000422003031000042WP 2003 3 10 0300379871 120030222A261117946081 SEPARATOR DOUG DC9 DC951 3022051WP A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING NRNOT REPORTED 1 GL01780NC 48102 After landing and parking at the gate the right lavatory smoke detector went into alarm. smoke was reported to be visible in the aft cabin. All passengers were evacuated safely and CFR did respond. No source of the smoke was found and no evidence of any type of fire was located. The F/O did discharge a portable fire extinguisher into the lavatory. Maintenance cleaned the extinguisher agent from the lav, replaced the fire bottle and replaced the water separator bags. Aircraft has returned to service. 2L72 4F RTA6WE 20030310000432003031000043NM 2003 3 10 0300386624 120030301A26971W71018R WIRE BOEING747 747251B 1384892NM SHORTED A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01624US 21706 During takeoff the left wing leading edge overheat light illuminated. Aircraft aborted takeoff at 110 knots resulting in 7 blown tires. Passengers were bussed from aircraft to terminal. Repaired shorted and chaffed wires and replaced switch S896. Replaced 7 wheel/tire and brake assemblies. Operational check good. 2L74 4F A20WE 20030310000462003031000046SW 2003 3 10 HEEA084951 120030227A6710214001347005 ACTUATOR BELL 412 412 1182202SW M/R HEAD STICKING E O OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 ACTUATOR STICKING. 1G72 4U H4SW 20030310000512003031000051NE 2003 3 10 HEEA084955 220030227A732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TORQUE OSCILLATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 TORQUE CONTROL UNIT CREATES TORQUE OSCILLATIONS. 1G72 4U4 U H4SW E22EA 20030310000542003031000054 2003 3 10 HEEA084958 420030227A22114025008918 COMPUTER BELL 412 412 1182202SW AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 AFCS COMPUTER NR 1 PITCH MOTORS ALL THE WAY UP IN SAS MODE. 1G72 4U H4SW 20030310000692003031000069SW 2003 3 10 HEEA084973 120030227A3213412050045107 CROSSTUBE BELL 412 412 1182202SW MLG FAILED E O OTHER L NO TEST NRNOT REPORTED 1 SW03223474764 36005 MLG CROSSTUBE FAILED DEFLECTION CHECK. SCRAPPED. 1G72 4U H4SW 20030310000702003031000070SW 2003 3 10 HEEA084974 120030227A3213412050045107 CROSSTUBE BELL 412 412 1182202SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P2214 33012 MLG CROSSTUBE DAMAGED BEYOND LIMITS. SCRAPPED. 1G72 4U H4SW 20030310000712003031000071SW 2003 3 10 HEEA084975 120030227A6710 BEARING BELL 412 412 1182202SW UNIVERSAL WORN E O OTHER O OTHER NRNOT REPORTED 1 SW03107X BT399 33113 COLLECTIVE UNIVERSAL HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030220001302003022000130NM 2003 2 20 F3LA200300023 120030122A1430 CLIP BOEING737 7373M8 1384615NM LT MLG WW CHAFED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED NUT CLIP ON LT MLG WHEEL WELL FAIRING ATTACH BRACKET AT STA 727 CHAFFED THROUGH. REPLACED DAMAGED PART PER SRM 51-40-02, 51-40-06 AND BOEING DRAWING 65-48675. 2L72 4F RTA16WE 20030220001342003022000134WP 2003 2 20 ZW0A0301802 120030205A3350408822101 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139620D 53591 CEILING EMERGENCY LIGHTS WERE INOPERATIVE ROWS 27 TO AFT END OF CABIN, ABOVE AFT FLT ATTEND SEAT, FWD OF RT AFT LAV, AND TWO CEILING LIGHTS ABOVE THE L2 FLIGHT ATTEND POSITION. REPLACED POWER SUPPLY BATTERIES FOR ROW 27 TO AFT DOOR AND FOR FORWARD OF THE RT AFT LAV. REPLACED BULBS FOR OTHER CEILING EMERGENCY LIGHTS. 2L72 4F RTA6WE 20030220001352003022000135EA 2003 2 20 COMA0360106 120030217A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA 3-A DETERIORATED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01420CA8466 7451 FLIGHT 5806 GEAR DISAGREE WARNING AFTER T/O.REPLACED THE 3A HYDRAULIC PUMP. 2L72 4F RTA21EA 20030220001372003022000137WP 2003 2 20 MWEA030051 120030203A575499558281 RIB DOUG DC9 DC932 3022066WP L/E SLAT CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31207ME 47794 LEFT NR 5 SLAT OUTBOARD RIB IS CRACKED AT LOWER AFT CORNER. REMOVED CRACKED RIB AND INSTALLED NEW RIB. 2L72 4F A6WE 20030220001392003022000139NM 2003 2 20 2003F00109 120030114A33501000677 LIGHT BOEING727 727200 138407ENM COCKPIT INOPERATIVE A MYWAK NONE L NO TEST ININSP/MAINT 1 SO19211DB 20766 DURING PREFLIGHT TRANSIT CHECK, FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY IAW MM 33-40-0. (M) 2L73 4F RTA3WE 20030220001402003022000140NM 2003 2 20 2003F00110 120030102A3350900835A BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A MYWAK NONE L NO TEST ININSP/MAINT 1 SO19804MA 22435 DURING PREFLIGHT TRANSIT CHECK FLIGHT TRANSIT RIGHT CENTER OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW MM 33-50-0. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030220001412003022000141CE 2003 2 20 2003F00111 120030117A3260 WARNING SYSTEM BEECH 1900 1900D 1154162CE COCKPIT ACTIVATED A GUUAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO1987552 UE216 FLT 9198 - MIA-TPA - AFTER LANDING, RED LIGHT IN LANDING GEAR HANDLE ILLUMINATED AND LANDING GEAR WARNING HORN WOULD NOT CEASE. RESECURED LANDING GEAR HANDLE LIGHT KNOB. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. (M) 2L72 4T RTA24CE 20030220001462003022000146EA 2003 2 20 A6WA200340011 120030108A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FOUND SUPPORT ANGLES AT FS 484 RIGHT SIDE OF CABIN FLOOR LEVEL ARE CRACKED. CUT AWAY CRACKED FLANGE AND REMOVED INBOARD ANGLE FABRICATED ANGLES. INSTALLED REPAIR IAW WVAC EO 601R-53-37281. (M) 2L72 4F RTA21EA 20030220001472003022000147EA 2003 2 20 A6WA200340021 120030104A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FOUND FLOOR SUPPORT STRUCTURE AT FS 621 CRACKED AT LEFT AND RIGHT SIDES COMPLIED WITH REO 601R-53-61-004 REV B. (M) 2L72 4F RTA21EA 20030220001482003022000148NM 2003 2 20 AMTA200300119 120030120A2612 FIRE WARNING BOEING757 75723N 1384973NM COCKPIT MALFUNCTIONED A AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11519AT 27975 STATUS MESSAGE, CARGO DET AIR. PERFORMED CARGO FIRE TEST, ALL DET GOOD. RECYCLED POWER, STATUS MSG CLEARED. OK FOR FLIGHT. (M) 2L72 4F RTA2NM 20030220001702003022000170NE 2003 2 20 ARWA20030104 220030122A7200 ENGINE LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B40254555NE NR 3 VIBRATION A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO19307GB 193U1131 14613 NR 3 ENGINE VIBRATION DURING CRUISE AT 350 FT LOW POSITION A-B 2.8 CAUTION LIGHT ON. SHUTDOWN ENGINE AT 06:35 Z. REMOVE AND REPLACE ALL NR 3 ENGINE C-1 BLADES IAW MM 72-31-01. REMOVED AND REPLACED VIBRATION MONITOR IAW MM 77-31-00. COMPLETED TRIM BALANCE CHECK OIL FILTER AND CHIP DETECTORS ALL SYSTEM CHECK OK. AFTER TRIM BALANCE AIRBORNE VIBRATION MONITOR (AVM) MAXIMUM AT TAKE OFF WAS 1.3 OPERATIONS NORMAL. 2L73 4F4 F A23WE E12EU 20030220001722003022000172WP 2003 2 20 ARWA20030107 120030130A32322690032B ACTUATOR LKHEED1011 1011385115 5265015WP MLG DOOR FAILED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19307GB 193U1131 AFTER TAKEOFF RED INTRANSIT LIGHT ILLUMINATED. ALSO PERFORMED CHECKLIST, NO CHANGE. RETURNED TO MIAMI. REMOVED AND REPLACED RT TURN LANDING GEAR DOOR LOCK ACTUATOR IAW MM 32-33-08. ADJUSTED ROD ASSEMBLY IAW MM 32-12-05 SYSTEM TESTED NORMAL. 2L73 4F A23WE 20030220001832003022000183WP 2003 2 20 ARWA20030203 120030207A324139241 VALVE DOUG DC8 DC863F 302198FWP ANTI SKID SYS FAILED A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO19784AL 46135 PRIOR TO 80 KTS. ANTI-SKID LIGHT CAME ON. NOTE: REJECTED TAKEOFF AT KMIA. CHECKED ELECTRICAL SYSTEM IAW MM 32-3-0 SMT 1 & 2 FOUND SYSTEM WORKED NORMAL. REMOVED AND REPLACED LAMP CONTROL BOX IAW MM 32-43-7; PENDING OPERATIONAL CONTROL CHECK. ALSO REMOVED AND REPLACED R.A.O. ANTISKID SYSTEM DUAL SERVO VALVE IAW MM 32-43-3. LEAK CHECKED, NO LEAK NOTED. PERFORMED OPS CHECK ANTISKID SYSTEM IAW MM 32-43-0. FOUND ALL NORMAL. PERFORM TAXI AT 70 KTS. NO LIGHT ANTISKID OPERATIONAL NORMAL IAW 32-43-0. 2L74 4F 4A25 20030220001862003022000186WP 2003 2 20 ARWA20030207 120030216A3260 SENSOR DOUG DC8 DC863F 302198FWP MLG MALFUNCTIONED A ARWAO OTHER N FALSE WARNING LDLANDING 1 SO19784AL 46135 WHEN LANDING GEAR SELECTED DOWN, HAD BOTH RED DOORS NOT LATCHED AND GEAR NOT LATCHED LIGHTS WITH NO GREEN LEFT LANDING GEAR LIGHT. REMOVED AND REPLACED LT SENSOR OF MAIN GEAR ALL POSITION & WARNING LIGHTS WORK NORMAL IAW MM 32-60-0. 2L74 4F 4A25 20030221000042003022100004NM 2003 2 21 DHL2003751006 120030220A2611 SMOKE DETECTOR BOEING727 727264 138408MNM A DHLAO OTHER J WARNING INDICATION ININSP/MAINT 1 SO01751DH 22982 1) AT BLOCK-IN IN SAN WHEN MAIN CARGO DECK SMOKE DETECTOR TURNED OFF, #2 SMOKE DETECTOR RED LIGHT ILLUMINATED . NO INDICATION OF SMOKE /FIRE VISIBLE TO CREW. LIGHT STAYS ON WEATHER SMOKE DETECTOR SELECTED ON OR OFF2) CLEANED #2 SMOKE DETECTOR LIGHT SOCKET IAW B-727 M/M 26-17-001.OPS CHECK GOOD. 2L73 4F A3WE 20030221000072003022100007NM 2003 2 21 AWXA200300031 120030112A2824405744 ACTUATOR BOEING737 7373G7 1384595NM SHUTOFF VALVE FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28157AW206804645 23779 ENROUTE FROM MKE TO PHX FUEL IMBALANCE OCCURRED, CROSS FEED VALVE OPEN LIGHT WAS BRIGHT IN BOTH ON AND OFF POSITIONS. DIVERTED TO DEN WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED FUEL SHUT OFF VALVE ACTUATOR ASSEMBLY LOCATED ON CROSS FEED VALVE IAW BMM 28-22-21-4, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN OF FUEL SHUT OFF VALVE ACTUATOR S/N 3269 CONFIRMED FAILURE OF UNIT. UNIT WAS FOUND CORRODED AND CONTAMINATED WITH MOISTURE CAUSING BEARING TO FREEZE. UNIT COMPLETELY OVERHAULED AND FUNCTIONAL TESTED PER OHM 28-20-33. 2L72 4F RTA16WE 20030221000092003022100009 2003 2 21 AWXA200300044 420030114A2565D131516113 SLIDE AIRBUSA319 A319132 3930340NM PAX DOOR DEPLOYED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW125992271 1116 WHILE PARKED AT GATE AT IAD L-1 DOOR PARTIALLY DEPLOYED. L-1 DOOR ARM/DISARM LEVER WOULD NOT MOVE MORE THAN 1/2 AN INCH. DOOR INDICATED DISARMED ON ECAM BUT WAS ACTUALLY STILL ARMED. FLIGHT ATTENDANT OPENED DOOR BELIEVING DOOR WAS DISARMED WHEN SLIDE BEGAN DEPLOYMENT SEQUENCE, FLIGHT ATTENANT HELD THE DOOR CAUSING SLIDE TO ONLY PARTIALLY DEPLOY. MAINTENANCE REMOVED AND REPLACED SLIDE ASSEMBLY IAW AWA T/C R1C25305, WHEN REMOVING SLIDE FOUND DIRT AND DEBRIS IN GIRT BAR AREA. OPERATIONAL CHECK OF ARM/DISARM LEVER IS NOW GOOD. 2L72 4F RTA28NM 20030221000172003022100017NM 2003 2 21 AWXA200300064 120030111A531265163007 BULKHEAD BOEING737 737300 1384610NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT SIDE OF BULKHEAD WEB BS 178, RBL 4.7, WL 198.5, CONFIRMED BY HFEC. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG. 287-288J, FIG. 211. 2L72 4F RTA16WE 20030221000192003022100019NM 2003 2 21 AWXA200300066 120030102A5754654643099 SKIN BOEING737 737300 1384610NM LE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C-14 CHECK THE LT INBOARD FOREFLAP UPPER OUTBOARD END WAS FOUND DELAMINATED. MAINTENANCE REPAIRED DAMAGE TO HONEYCOMB OF LT INBOARD FOREFLAP UPPER OUTBOARD END IAW B737-300 SRM 51-70-10, REP. 9, FIG. 18, PG. 73-77. 2L72 4F RTA16WE 20030221000292003022100029EA 2003 2 21 QXEA0300137 120030114A5320 SPACER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 CKB- RADIO ALTIMETER ANTENNA SPACER HAS SURFACE CORROSION AT STATION 1033.83, BL 2.50 PORT. REPAIRED IAW CRJ SRM 51-21-06. 2L72 4F RTA21EA 20030221000322003022100032EA 2003 2 21 QXEA0300142 120030114A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 CKB- STATION 319 RIGHT HAND AT STRINGER 2R HAS ELONGATED FROM FACTORY. REPAIRED IAW CRJ SRM 51-42-06 AND HORIZON AIR EA R-53-70. 2L72 4F RTA21EA 20030221000352003022100035NM 2003 2 21 QXEA0300146 120030124A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- LEFT HAND WING NR 1 FLAP TRACK UPPER TRACK UNDER SURFACE HAS DIVOTS. REPAIRED IAW DHC-8 RD 8-57-98S AND SRM 51-00-06. 2H72 4T RTA13NM 20030221000382003022100038NM 2003 2 21 QXEA0300149 120030124A5711 SPAR CAP DHAV DHC8 DHC8202 2809007NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- LEFT HAND WING FRONT SPAR, LOWER CAP IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-20-26. 2H72 4T RTA13NM 20030221000402003022100040NM 2003 2 21 QXEA0300151 120030122A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- REMOVE AND REPLACE NR 10 SEAT TRACK DUE TO A PERVIOUS BLEND AND GOUGE WHICH APPEARS TO BE BEYOND BLENDABLE LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11, 51-40-00 AND RD 8-51-102. 2H72 4T RTA13NM 20030221000442003022100044NM 2003 2 21 QXEA0300155 120030121A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- LEFT HAND FIREWALL HAS TWO CRACKS AT INBOARD SIDE NEAR THREE O'CLOCK POSITION NEAR ENGINE EXHAUST PIPE. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-54-806. 2H72 4T RTA13NM 20030221000502003022100050NM 2003 2 21 AWXA200300077 120030126A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 19 CRACKED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28156AW 23778 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS INOPERATIVE. MAINTENANCE FOUND BULB RECEPTACLE CRACKED, REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030221000552003022100055NM 2003 2 21 QXEA0300160 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 1 SEAT TRACK HAS SCRATCHES AT STATION 330. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36, 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20030221000562003022100056NM 2003 2 21 QXEA0300161 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 1 SEAT TRACK HAS LIGHT PITTING CORROSION AT STATION 310. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-16, 51-20-36 AND 8-53-1342. 2H72 4T RTA13NM 20030221000602003022100060NM 2003 2 21 QXEA0300184 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 5 SEAT TRACK HAS SCRATCHES AT STATION 440. REPAIRED IAW RD 8-53-1339, SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030221000852003022100085NM 2003 2 21 AWXA200300180 120030128A5320146N5484 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN STR 29 - 30 RT, BS 1510. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT BS 1510, BETWEEN STR 29 - 30 RT; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030221000902003022100090SW 2003 2 21 AC2A084143 120030130A6420230312001101 LINK BELL 430 430 1182150SW TAIL ROTOR WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CM984 49090 TAIL ROTOR PITCH CONTROL LINKS ARE WORN. REPLACED TAIL ROTOR PITCH CONTROL LINKS. 1G72 3U RTH9SW 20030221000922003022100092SW 2003 2 21 AC2A084145 120030209A3213430036140105 CROSSTUBE BELL 430 430 1182150SW MLG CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH879 49037 CROSSTUBE IS CORRODED. CROSSTUBE WAS REPLACED 1G72 3U RTH9SW 20030114000632003011400063NM 2003 1 14 SWAA030013 120030103A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 751, STR 18R AND STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030114001142003011400114 2003 1 14 SWAA030001 420030101A25651061323469 SLIDE BOEING737 7373A4 1384585NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030114001182003011400118NM 2003 1 14 SWAA030009 120030105A335065C27093 LIGHT BOEING737 7372T4 1384492NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT MID CABIN. SECURED EXIT LIGHT PER MM. 2L72 4F A16WE 20030114001212003011400121NM 2003 1 14 SWAA030023 120030106A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030114001232003011400123NM 2003 1 14 SWAA030031 120030105A53146545866 KEELBEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM LOWER CHORD CORRODED AT BS 500A + 8, STR 28R. REPAIRED KEEL BEAM LOWER CHORD PER SWA EA. 2L72 4F A16WE 20030114001242003011400124 2003 1 14 SWAA030032 420030107A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030114001252003011400125NM 2003 1 14 SWAA030033 120030107A33501000679 LIGHT BOEING737 7372H4 138448CNM COCKPIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT CEILING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F A16WE 20030114001372003011400137 2003 1 14 SWAA030041 420030108A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030114002072003011400207NM 2003 1 14 VNAA0301003 120030105A3350362624 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN INOPERATIVE A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07436JS 3052 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING IN THE GALLEY AREA WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030114002572003011400257EA 2003 1 14 COMA0360025 120030113A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR INOPERATIVE A COMAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO01954CA 7100 FLIGHT 5214 FLOOR EMERGENCY LIGHTS ARE INOP ROW 8 AFT.REPLACED FLOOR LIGHT STRIP. 2L72 4F RTA21EA 20030116002212003011600221EA 2003 1 16 COMA0360027 120030113A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS OUT OF RIG A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01918CA 7018 FLIGHT 5133 FLAPS FAIL MESSAGE DURING TAXI. FOUND THE FLAPS TO BE OUT OF RIG 130TH MECHANICALLY AND ELECTRICALLY. RIGGED FLAPS TO M/M SPECIFICATIONS. 2L72 4F RTA21EA 20030114002642003011400264SO 2003 1 14 C2XA03IA005 120030112A3350487190 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712922 145338 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT FIRST ROW FAILED TO ILLUMINATE. IAH- MAINTENANCE RECONNECTEDA LOOSE CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030115000382003011500038NM 2003 1 15 2003UALA00018 120030103A335058674 INVERTER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29323UA 23955 EMERGENCY ELECTRICAL LIGHTING STRIP BETWEEN ROWS 15 AND 21 INOPERATIVE SUPPLEMENTAL DATA UPDATE INOPERATIVE LIGHT INVERTER. REPLACED AND SYSTEM OPS CK GOOD 2L72 4F4 FRTA16WE E2GL 20030401001012003040100101NM 2003 4 1 DHL2003780001 120030114A2612 FIRE DETECTOR BOEING727 727223 1384074NM APU WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01780DH 22006 APU WILL NOT FIRE TEST. PLACED ON MEL 26-11 CAT-C DMI 11581. REF DMI 11581, APU FIRE WARNING WILL NOT TEST. REMOVED AND REPLACED APU FIRE TEST OPERATING POWER UNIT, AND APU FIRE TEST RELAY, NO HELP IAW BMM 26-15-00. DMI 11581 REMAINS IN EFFECT. 2L73 4F A3WE 20030115000852003011500085NM 2003 1 15 0300016309 120030107A3350 LIGHT BOEING747 747451 1384940NM CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE ON LEFT SIDE FROM ROWS 21-31 AND FROM RIGHT FLIGHT ATTENDANT STATION 2 RIGHT. RELAMPED EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. 2L74 4F RTA20WE 20030221000942003022100094SW 2003 2 21 AC2A084147 120030209A3213430036141105 CROSSTUBE BELL 430 430 1182150SW MLG CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH4024 49037 CROSSTUBE IS CORRODED. CROSSTUBE WAS REPLACED 1G72 3U RTH9SW 20030625000882003062500088NM 2003 6 25 F3LA200300064 120030217A5320 ATTACH ANGLE BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED RT RAM AIR DUCT ANGLE ATTACH POINT FOR CROSS BRACE UNDER WING BLEED AIR DUCT CORRODED AT STA 540, STR 22R. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, FIG 1, SHEET 2, 51-40-3. 2L72 4U RTA16WE 20030625000902003062500090NM 2003 6 25 F3LA200300067 120030218A5320 SUPPORT ANGLE BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED FLOOR/LAVATORY SUPPORT BEAM BETWEEN STA 986.5 AND STA 1006 CORRODED. REMOVED SUPPORT ANGLE AND HAT CHANNEL PER SRM 51-30-02. FOUND CORROSION ON BOTH HAT CHANNEL AND SUPPORT ANGLE OUT OF LIMITS PER SRM 51-30-02. FABRICATED AND INSTALLED REPLACEMENT HAT CHANNEL AND SUPPORT ANGLE PER BOEING DRAWING 65-77457, SRM 51-21-41, 51-30-03 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030625000912003062500091NM 2003 6 25 F3LA200300068 120030218A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, RBL 3, AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE. FABRICATED AND INSTALLED FLOOR SUPPPORT AND SPLICE PER SRM 53-10-3, FIG 11, AND SOPM 20-41-02. 2L72 4U RTA16WE 20030222000012003022200001SO 2003 2 22 C2XA03SH009 120030222A530014522460011 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C CHECK AFT BUTT STRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AFT BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030223000022003022300002SO 2003 2 23 C2XA03SH012 120030222A530014526437001 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030223000042003022300004SO 2003 2 23 C2XA03SH014 120030222A530014522226003 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-01.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030223000052003022300005SO 2003 2 23 C2XA03SH015 120030222A530014525994003 CROSSBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE RIGHT SILL AND RIGHT FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030223000092003022300009SO 2003 2 23 C2XA03SH019 120030222A530014525994003 CROSSBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND SILL AND THE LEFT HAND FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030223000112003022300011SO 2003 2 23 C2XA03SH020 120030222A530014525422003 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE RIGHT HAND SILL AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030223000132003022300013SO 2003 2 23 C2XA03SH022 120030222A530014525991003 STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE LEFT HAND STRAP AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 53-31-19 AND 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030224000102003022400010NE 2003 2 24 ALGA084133 120030217A6520SB8207102 SEAL SKRSKYS76 S76A 8143006NE T/R GEARBOX DEFECTIVE H ALGAO OTHER K FLUID LOSS NRNOT REPORTED 1 FS01PTYAY A12600133 760277 FOUND TAIL ROTOR GEARBOX SEAL DEFECTIVE AND WAS LEAKING. REPLACED SEAL WITH A NEW PART. 1G72 3U H1NE 20030224000112003022400011NE 2003 2 24 ALGA084135 120030219A6520SB8208102 SEAL SKRSKYS76 S76A 8143006NE T/R GEARBOX DEFECTIVE H ALGAO OTHER K FLUID LOSS NRNOT REPORTED 1 FS01518AL A12600111 760134 FOUND TAIL ROTOR GEARBOX SEAL DEFECTIVE AND LEAKING. REPLACED SEAL WITH A NEW PART. 1G72 3U H1NE 20030224000252003022400025EA 2003 2 24 03054627 120030203A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT HAD BEEN BROKEN OF OF THE BULKHEAD. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030224000402003022400040NE 2003 2 24 HEEA084161 120030212A243523081043 STARTER GEN SKRSKYS76 S76A 8143006NE ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X 760050 STARTER GEN INOPERATIVE. 1G72 3U H1NE 20030224000422003022400042 2003 2 24 HEEA084163 420030212A34215040017928 INDICATOR SKRSKYS76 S76A 8143006NE STANDBY ATTITUDEMALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 STANDBY ATTITUDE INDICATOR WILL NOT ERECT. IN SHOP REPAIR. 1G72 3U H1NE 20030224000492003022400049NE 2003 2 24 HEEA084170 120030212A62107615009100048A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH12393 760224 MAIN ROTOR BLADE NICKEL STRIP HAS A CRACK AT THE VERY TIP AND IS STARTING TO PEEL. 1G72 3U H1NE 20030224000642003022400064 2003 2 24 HEEA084185 420030212A2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 CAUSING INTERMITTENT ICS COMMUNICATIONS. FOUND SWITCH S1 NOISY, THREE BULBS IN LIGHT PANEL, VOLUME AND SELECTOR KNOBS BAD. CLEANED SWITCH, REPLACED BULBS AND VOLUME AND SELECTOR KNOBS. BENCH CHECK GOOD. 1G72 3U H1NE 20030224000662003022400066NE 2003 2 24 HEEA084187 120030212A6520B538A3 CHIP DETECTOR SKRSKYS76 S76C 8143008NE T/R GEARBOX SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03276X 760405 CHIP PLUG INTERMITTENTLY SHORTS INTERNALLY. SCRAPPED. 1G72 3U NCH1NE 20030224000752003022400075 2003 2 24 HEEA084195 420030213A3454066107800 RECEIVER SKRSKYS76 S76A 8143006NE VHF NAVIGATION INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 VOR INOPERATIVE. IN SHOP REPAIR. 1G72 3U H1NE 20030224000882003022400088SW 2003 2 24 HEEA084209 120030120A5320407070620111 TRIM PANEL BELL 407 407 1182206SW AFT CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 AFT CABIN TRIM PANEL CRACKED. 1G71 3U O H2SW 20030224000912003022400091SW 2003 2 24 HEEA084212 120030120A5320407070620113 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 PANEL CRACKED. 1G71 3U O H2SW 20030224000932003022400093SW 2003 2 24 HEEA084214 120030120A5320407070620119 TRIM PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 INTERIOR TRIM PANEL CRACKED. 1G71 3U O H2SW 20030224000982003022400098EU 2003 2 24 NSVA200300008 120030222A26001734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE TAIL PIPE OUT OF TOLERANCEA NSVAE ENGINE SHUTDOWN JNMWARNING INDICATION FALSE WARNING OVER TEMP CLCLIMB 1 EA27294CJ 5337 340B294 785443 In route to LGA-Crew notified ARINC of a "Tail Pipe Hot" light that illuminated during flight. Emergency procedures were followed and the engine was subsequently shut down. The aircraft landing was uneventful. MX found no evidence of overheating but did find 2 heat sensors out of tolerance. Heat sensors were removed and replaced, Op's check was good, aircraft returned to service. 2L72 4T4 TRTA52EU E8NE 20030224000992003022400099NM 2003 2 24 F3LA200300078 120030219A5320 INTERCOSTAL BOEING737 7372Y5 1384554NM STA. 957 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT GALLEY FLOOR INTERCOSTAL AT STA. 957, LBL 18.75 THRU LBL 40.5. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 51-30-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SRM 51-30-02. 2L72 4U RTA16WE 20030224001022003022400102EA 2003 2 24 COMA0360110 120030220A2710 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO01986CA 7174 FLIGHT 9458 AILERON MASTER CAUTION, T/O ABORTED.FOUND AILERON TRIM OUT OF THE TAKE OFF RANGE. 2L72 4F RTA21EA 20030224001042003022400104SW 2003 2 24 HEEA084219 120030120A5320407070620139 HEADLINER BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 HEADLINER CRACKED. 1G71 3U O H2SW 20030224001072003022400107SW 2003 2 24 HEEA084222 120030120A5320407070620143 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030224001132003022400113NM 2003 2 24 CALA0300063 120030222A5311 FRAME BOEING737 7373T0 1384582NM STA 793 CORRODED A CALAK NONE K FLUID LOSS ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND BELTFRAME CORRODED AT STA 793. THE CORRODED AREA WAS REMOVED AND A TYPICAL FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20030224001152003022400115NM 2003 2 24 CALA0300065 120030223A5320 STRAP BOEING737 7373T0 1384582NM STA 840-853 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND CORROSION ON AFT LOWER STRAP ON BOTTOM SIDE OF VERTICAL WEB UPPER FLANGE AT STA 840-853, RBL 19. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030115001002003011500100GL 2003 1 15 ALGA082901 220030108A725023064622 NOZZLE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL 2ND STAGE MISMANUFACTURED H ALGAK NONE W INADEQUATE Q C ININSP/MAINT 1 FS01 FOUND NR 1 WHEEL BLADE PATH FINAL MACHINED OVERSIZED. DIM.= 6.275 RETURNED PART. 1Q71 3R3 U 2A6 E1GL 20030115001112003011500111EU 2003 1 15 BAQA082880 120030107A6410365A12002002 BLADE AEROSPSA365 SA365N 8680669EU TAIL ROTOR DAMAGED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM737 6396 TAIL ROTOR BLADE DAMAGED AT ROOT. REPLACED WITH SERVICEABLE BLADE. 1G72 3U H10EU 20030115001152003011500115EU 2003 1 15 BAQA082884 120030107A6410365A12002002 BLADE AEROSPSA365 SA365N 8680669EU TAIL ROTOR DAMAGED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM504 6396 TAIL ROTOR BLADE HAS EXCESSIVE PLAY IN SPOOL. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030115001192003011500119 2003 1 15 BAQA082900 420030108A3416396005241 ENCODER AEROSPSA365 SA365N 8680669EU ALTIMETER INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM5568 6396 ALTIMETER ENCODER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030115001202003011500120NM 2003 1 15 03FDEA00009 120030108A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 OIL CAN DENT IN SKIN AT BS 190, RBL 22, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR IAW SRM 53-30-3. 2L73 4F4 FRTA3WE E2EA 20030115001262003011500126 2003 1 15 BAQA082909 420030109A3421C17027AA01 INDICATOR UROCOPEC135 EC135T1 5620026EU ATTITUDE MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01522ME1546 0144 ATTITUDE INDICATOR FAILED FAR 91-411 CHECK. ALTITUDE OUT OF LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030115001292003011500129EU 2003 1 15 BAQA082953 120030113A2840L281M2008101 PROBE UROCOPEC135 EC135T1 5620026EU FUEL SYSTEM MALFUNCTIONED H BAQAO OTHER N FALSE WARNING NRNOT REPORTED 1 FS01118WS18 0089 FUEL PROBE INITIATES FUEL DEGRADE LIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030115001452003011500145EU 2003 1 15 ERAA082932 120030102A78106879879 TAILPIPE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MISOVERHAULED H ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 FS01134EH 635 EXHAUST COLLECTOR RETURNED FROM OVERHAUL 6-7-02. REMOVED FROM STOCK AND COULD NOT BE USED ON AIRCRAFT DUE TO EXCESSIVE DENTS ON INSIDE OF EXHAUST COLLECTOR. 1G72 3U3 U H3EU E4CE 20030115001882003011500188SW 2003 1 15 ERAA082941 120030106A6230412040366105 MAST BELL 412 412 1182202SW MAIN ROTOR CORRODED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01 12867 MAST ASSY HAS PITTING, CORROSION INSIDE OF MAST POST, FROM 1 1/2 - 3 INCHES FROM TOP OF MAST, LOWER CONE WEAR SLEEVE SOUNDS DEBONDED, EXCESS WEAR, MAST NUT HAS DAMAGED THREADS. OVERHAULED MAST ASSY IAW 412 CR&O. INSTALLED NEW MAST POLE, NEW BEARINGS, NEW LOCK BEARING, NEW NUT, NEW SEAL, ASSEMBLED IAW 412 CR&O, TB 412-96-137, TB412-98-150. COMPLIED WITH TB412-96-134.TB412-98-150. 1G72 4U H4SW 20030115002092003011500209NM 2003 1 15 DL757030015 120030102A5330146N37301 SKIN BOEING757 757232 1384965NM FS 1694, S-14L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27610DL 22817 FUSELAGE / SKIN / FS 1694 / STRG. 13L-15L : DENT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED ABOVE AN EXISTIN REPAIR FOR A SMALL CUTOUT. THE DENT WAS CUTOUT AND THE EXISTING REPAIR REMOVED. THE NEW AND EXISTING CUTOUTS WERE THEN REPAIRED WITH A SINGLE REPAIR DOUBLER/TRIPLER COMBINATION PER ER/A 384264-14, REV A. 2L72 4F RTA2NM 20030115002152003011500215NM 2003 1 15 DL757030051 120030112A3350767 LIGHT BOEING757 757232 1384965NM #1 ENGINE BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27675DL 25980 0 EXTERIOR EMERGENCY LIGHTS OUT AT 2L AND OVER LT WING CA RELAMPED 2L72 4F RTA2NM 20030115002162003011500216EA 2003 1 15 COMA0360028 120030114A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAL ABORTED APPROACH S AFFECT SYSTEMS APAPPROACH 1 SO01466CA 7627 FLIGHT 5161 FLAPS FAIL MESSAGE DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 9-20-01. 2L72 4F RTA21EA 20030116000092003011600009GL 2003 1 16 ERAA082951 220030106A7323252466715H GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE DAMAGED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03292EH11001 562 GOVERNOR REQUIRES REPAIR - BROKEN LOCKWIRE REPAIRED AND FUNCTIONALLY TESTED TO SPECS BY PRECISION ENGINES CORP. 1G72 3U3 U H3EU E4CE 20030116000142003011600014 2003 1 16 HEEA082971 420030107A3416212070238007 INDICATOR SKRSKYS76 S76A 8143006NE ALTIMETER READS HIGH E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031546G 760076 COPILOT ALTIMETER READS 200 FEET HIGH AT 1000 FEET. IN SHOP REPAIR. 1G72 3U H1NE 20030116000172003011600017 2003 1 16 HEEA082974 420030107A34217000466935 INDICATOR SKRSKYS76 S76A 8143006NE ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03764P 760276 COPILOT ATTITUDE INDICATOR TURN NEEDLE PEGGED FULL RIGHT AT ALL TIMES. IN SHOP REPAIR. 1G72 3U H1NE 20030116000232003011600023NE 2003 1 16 HEEA082980 120030107A28207630702904101 CHECK VALVE SKRSKYS76 S76A 8143006NE FUEL DIST DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 NR 1 ENGINE WOULD NOT START IN CROSSFEED AND NR 2 ENGINE WOULD NOT START IN DIRECT FEED. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030116000252003011600025NE 2003 1 16 HEEA082982 120030107A33407655002005101 SEARCH LIGHT SKRSKYS76 S76A 8143006NE EXTERIOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 SEARCH LIGHT WILL NOT STOW FULLY AND CONTINUES TO MOTOR WHEN SET TO SLOW. IN SHOP REPAIR. 1G72 3U H1NE 20030116000292003011600029 2003 1 16 HEEA082986 420030107A2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COMM SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 INTERPHONE BOX MALFUNCTIONED, COULD NOT BALANCE ICS. IN SHOP REPAIR. 1G72 3U H1NE 20030116000362003011600036SW 2003 1 16 HEEA082995 120030106A7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0354641 51184 INTELLISTART COMPUTER LIGHT WON'T STAY OUT. 1G71 3U H2SW 20030116000482003011600048 2003 1 16 HEEA083007 420030106A2562ELT910 ELT BELL 206 206L3 1182108SW CABIN MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 CAUSES ELT TEST LAMP TO REMAIN DIMLY ILLUMINATED AT ALL TIMES. 1G71 3U H2SW 20030116000492003011600049 2003 1 16 HEEA083008 420030106A2562ELT910 ELT BELL 206 206L3 1182108SW CABIN ACTIVATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038592X 51508 ELT HAS AN UNCOMMANDED ACTIVATION FOR UNDETERMINED AMOUNT OF TIME. 1G71 3U H2SW 20030116000522003011600052 2003 1 16 HEEA083011 420030106A2312 CLIP BELL 206 206L3 1182108SW HEADSET BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 HEADSET CLIP BROKEN AT MICROPHONE. SCRAPPED. 1G71 3U H2SW 20030116000582003011600058 2003 1 16 HEEA083017 420030106A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMM SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 MIXER BOX INTERMITTENT. REPAIRED. 1G71 3U H2SW 20030116000592003011600059 2003 1 16 HEEA083018 420030106A2350PHI001L0001201 MIXER BOX BELL 206 206L1 1182107SW COMM SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0327766 45312 FM RADIO RECEIVES WEAK ON PILOT SIDE. REPAIRED. 1G71 3U H2SW 20030116000602003011600060 2003 1 16 HEEA083019 420030106A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMM SYS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 PILOT SIDE SELECTOR KNOB VERY HARD TO TURN. REPAIRED. 1G71 3U H2SW 20030116000662003011600066SW 2003 1 16 HEEA083025 120030106A6520PHI2062003 SEAL BELL 206 206L4 1182110SW T/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW037074W A3564 52033 TAIL ROTOR GEARBOX SEAL LEAKING AND TWO DEEP GROOVES IN SPACER WHERE SEAL RIDES. REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20030116000692003011600069SW 2003 1 16 HEEA083029 120030106A6520PHI206L3957 PITCH LINK BELL 206 206L3 1182108SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 TAIL ROTOR PITCH LINK WORN AT TOP OF LEVERS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116000742003011600074SW 2003 1 16 HEEA083034 120030106A2430SM20ACD200A21 RELAY BELL 206 206L3 1182108SW DC SYSTEM STUCK E O OTHER O OTHER NRNOT REPORTED 1 SW038592X 51508 RELAY CORRODED AND STICKING. 1G71 3U H2SW 20030116000772003011600077SW 2003 1 16 HEEA083037 120030106A2430SM20ACD200A21 RELAY BELL 206 206L3 1182108SW DC SYSTEM STUCK E O OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 STUCK BATTERY RELAY. REPLACED WITH SERVICEABLE RELAY. 1G71 3U H2SW 20030116000782003011600078SW 2003 1 16 HEEA083038 120030106A2430SM20ACD200A21 RELAY BELL 206 206L3 1182108SW DC SYSTEM MALFUNCTIONED E O OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 BATTERY RELAY PRODUCING A WEAK BATTERY. 1G71 3U H2SW 20030116000802003011600080SW 2003 1 16 HEEA083040 120030106A2820S9001EC1 VALVE BELL 206 206L3 1182108SW FUEL SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 FUEL VALVE HAS NO STOPS WHEN ROTATED. 1G71 3U H2SW 20030116000822003011600082 2003 1 16 HEEA083042 420030106A3422060001500 GYRO BELL 206 206L3 1182108SW COCKPIT INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 DIRECTIONAL GYRO HEADING OFF 60 DEGREES IN FLIGHT. 1G71 3U H2SW 20030116000912003011600091CE 2003 1 16 046592 120030109A6123 VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT PROPELLER OUT OF ADJUST A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07139ZV UE139 ON TAXI, THE LEFT PROPELLER FAILED TO FEATHER MANUALLY. THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE FEATHER VALVE. NO PARTS WERE USED. TEARDOWN REPORT WILL NOT BE REQUIRED. 2L72 4T3 TRTA24CE E2NE 20030116000932003011600093SW 2003 1 16 HEEA083049 120030107A6520214040603003 COUPLING BELL 214 214ST 1182106SW T/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N7539 AMD00041 28106 INNER COUPLING AND OUTER COUPLING HAVE PITTING IN TOOTH PROFILE. (CORROSION ON MOUNT LUGS) REPAIRED. 2G72 4U H10SW 20030116000942003011600094 2003 1 16 HEEA083050 420030107A34427007700614 DISPLAY BELL 214 214ST 1182106SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 WEATHER RADAR DISPLAY FAILED IN FLIGHT. 2G72 4U H10SW 20030116001092003011600109GL 2003 1 16 HEEA083060 220030107A726103808808 ELEMENT BELL 206 206L1 1182107SW ALLSN 250C 250C30 03013GL ENGINE OIL MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035007N 45184 ENGINE OIL FILTER WILL NOT FIT IN THE HOUSING. THE HOLE WHERE THE O-RING GOES IS TOO SMALL ON ONE END. SCRAPPED. 1G71 3U3 U H2SW E1GL 20030116001152003011600115SO 2003 1 16 C2XA03CL012 120030114A335020131A BATTERY EMB 145 EMB145 3260210SO CABIN DISCHARGED A C2XAK NONE L NO TEST UKUNKNOWN 1 SW27159737421 2941 145159 CLE FLIGHT#2351 THE CREW REPORTED THE AFT AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030116001192003011600119 2003 1 16 HEEA083068 420030107A2312064101902 TRANSCEIVER BELL 206 206L1 1182107SW VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031076Y 45380 VHF TRANSCEIVER IS DEAD, WILL NOT COME ON. FOUND TRANSMIT POWER OUT AND MODULATION FLUCTUATING. REPLACED Q121 AND Q122 TRANSISTORS AND ALSO BAD DISPLAY LENS. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001202003011600120 2003 1 16 HEEA083069 420030107A2312064101905 TRANSCEIVER BELL 206 206L4 1182110SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0362127 52023 VHF TRAMSCEIVER TRANSMITS SCRATCHY ON ALL FREQUENCIES. FOUND DISPLAY NOT DIMMING PROPERLY. REPLACED V501 PHOTOCELL. REPAIRED PROBLEM. ALSO REPLACED CRACKED FACEPLATE. BENCH CHECK GOOD. 1G71 3U NCH2SW 20030116001232003011600123 2003 1 16 HEEA083072 420030107A2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 VHF TRANSCEIVER SCREEN WENT BLANK AND WOULD NOT TRANSMIT. IN SHOP REPAIR. 1G71 3U H2SW 20030116001272003011600127WP 2003 1 16 MWEA030034 120030116A531199118757 CLIP DOUG DC9 DC932 3022066WP AFT ACCESSORY` CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 RUDDER POWER PACK SUPPORT TO FRAME ATTACH POINT IS CRACKED ON THE FRAME SIDE, RIGHT SIDE OF AFT ACCESSORY. -- REMOVED ATTACH POINT, FABRICATED AND INSTALLED NEW CLIP. 2L72 4F A6WE 20030116001332003011600133 2003 1 16 HEEA083078 420030108A2350066105571 AUDIO PANEL BELL 206 206L4 1182110SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 AUDIO PANEL HAS NO RECEIVER AUDIO. FOUND R103, R104 RESISTORS BAD AND S213 SWITCH INTERMITTENT. REPLACED SAME. REPAIRED. BENCH CHECK GOOD. 1G71 3U NCH2SW 20030116001372003011600137 2003 1 16 HEEA083081 420030108A3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 RADAR ALTIMERTER HAS ERRATIC READINGS. SHOP REPAIR. 1G71 3U H2SW 20030116001382003011600138 2003 1 16 HEEA083082 420030108A3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 RADAR ALTIMETER INDICATOR NEEDLE DISPLAYS 200-300 FEET AFTER LEAVING GROUND. SHOP REPAIR. 1G71 3U H2SW 20030116001402003011600140 2003 1 16 HEEA083084 420030108A3452066106200 TRANSPONDER BELL 206 206L4 1182110SW ATC SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 ATC TRANSPONER HAS NO OUTPUT. CLEANED SLIGHT CORROSION. FOUND WEAK TRANSMIT POWER AND COULD NOT ADJUST PULSE WIDTH. REPLACED CAVITY OSCILLATOR AND R472, ADJUSTED FREQUENCY AND POWER. BENCH CHECK GOOD. 1G71 3U NCH2SW 20030224001172003022400117NM 2003 2 24 CALA0300067 120030223A5320 WEB BOEING737 7373T0 1384582NM AFT CARGO DR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND THE FORWARD I/B CORNER OF WEB CORRODED AT AFT CARGO DOOR LOWER THRESHOLD. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 53-60-15. 2L72 4F RTA16WE 20030224001232003022400123EA 2003 2 24 COMA0360115 120030223A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN CORRODED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01920CA 7022 FLIGHT 5598 FORWARD ORANGE EMERGENCY FLOOR PATH LIGHT IS INOP. CLEANED CORROSION FROM WIRE CONNECTIONS. 2L72 4F RTA21EA 20030625001002003062500100NM 2003 6 25 F3LA200300081 120030219A5320 INTERCOSTAL BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED LT. INTERCOSTAL BETWEEN STA. 967 AND STA. 986.5 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SOPM 20-41-02 2L72 4U RTA16WE 20030625001012003062500101NM 2003 6 25 F3LA200300082 120030219A5320 INTERCOSTAL BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED SHORT INTERCOSTAL AT CENTERLINE BETWEEN STA. 1006 AND STA. 1016 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030224001322003022400132NM 2003 2 24 ZW0A0302604 120030219A3350MS25308302 SWITCH BOEING757 757231 1384950NM CABIN DEFECTIVE A ZW0AK NONE O OTHER LDLANDING 1 CE13719TW 28487 DURING LANDING EMERGENCY EXIT LITES AND EMERGENCY FLOOR TRACK LITES ON AT L3 DOOR AND FLOOR AREA. REMOVED AND REPLACED SWITCH MS25308-302 CPN 5478924. OPS CHK PER 33-51-00. CHECK-C 7-7-02 MCI. --CLOSED-- 2L72 4F RTA2NM 20030224001382003022400138NM 2003 2 24 AWXA200300189 120030128A5320146N872212 WEB BOEING757 7572S7 1384962NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CUSP WEB BS 1701 TO BS 1720, LBL 60. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED CUSP WEB BS 1701 TO BS 1720, LBL 60; FABRICATED A NEW REPLACEMENT CUSP WEB PER DWG 146N8722; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 3 & 10. 2L72 4F RTA2NM 20030224001392003022400139NM 2003 2 24 AWXA200300190 120030127A5320146N5230 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON SURFACE OF FLOOR SUPPORT BS 1660 TO BS 1681, BL 0. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AREA OF FLOOR SUPPORT BS 1660 TO BS 1681, BL 0; FABRICATED REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1 & 6. 2L72 4F RTA2NM 20030224001442003022400144NM 2003 2 24 AWXA200300195 120030216A5320145N5416 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON NUT PLATES OF FLOOR SUPPORT BS 1330, RBL 2. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED AREA ON FLOOR SUPPORT BS 1330, RBL 2; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-2, & 4-6. 2L72 4F RTA2NM 20030225000012003022500001SO 2003 2 25 C2XA03SH029 120030225A530014521699003 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK LEFT HAND BUTT STRAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE CORRSION.MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030225000032003022500003SO 2003 2 25 C2XA03SH027 120030225A530014522460013 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK BUTT STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030225000192003022500019SW 2003 2 25 HEEA084238 120030120A5210407070620158 PANEL BELL 407 407 1182206SW PAX/CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 PAX/CREW DOOR PANEL CRACKED. 1G71 3U O H2SW 20030225000202003022500020SW 2003 2 25 HEEA084239 120030120A5320407070620175 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 CABIN INTERIOR CLOSEOUT PANEL CRACKED. 1G71 3U O H2SW 20030225000252003022500025SW 2003 2 25 HEEA084244 120030120A5320407070620199 TRIM PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 INTERIOR TRIM PANEL CRACKED. 1G71 3U O H2SW 20030225000292003022500029SW 2003 2 25 HEEA084248 120030120A2510407070620207 STRUCTURE BELL 407 407 1182206SW HAT BIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 HAT BIN STRUCTURE CRACKED. 1G71 3U O H2SW 20030225000312003022500031SW 2003 2 25 HEEA084250 120030120A2701407070620209 STRUCTURE BELL 407 407 1182206SW LT COLUMN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 LT COLUMN STRUCTURE CRACKED. 1G71 3U O H2SW 20030225000342003022500034SW 2003 2 25 HEEA084253 120030120A5320407070620213 TRIM PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 INTERIOR TRIM PANEL CRACKED. 1G71 3U O H2SW 20030225000432003022500043SW 2003 2 25 HEEA084262 120030129A6710214001347005 ACTUATOR BELL 412 412 1182202SW FLT CONTROL STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 ROTARY ACTUATOR STICKS INTERMITTENTLY. 1G72 4U H4SW 20030225000442003022500044SW 2003 2 25 HEEA084263 120030129A6710214001347005 ACTUATOR BELL 412 412 1182202SW FLT CONTROL STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 ROTARY ACTUATOR STICKS INTERMITTENTLY. 1G72 4U H4SW 20030225000622003022500062SW 2003 2 25 HEEA084284 120030211A6230 BEARING BELL 206 206L3 1182108SW SWASHPLATE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D GDJG10226 51106 MAIN ROTOR SWASHPLATE PIVOT BEARINGS WORN. REPAIRED. 1G71 3U H2SW 20030225000652003022500065SW 2003 2 25 HEEA084287 120030211A6420 TRUNNION BELL 206 206L1 1182107SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03513EH6262 AFS6342 45421 TAIL ROTOR ASSY TRUNNION SPLINES PITTED. REPAIRED. 1G71 3U H2SW 20030225000662003022500066SW 2003 2 25 HEEA084288 120030211A3212 VALVE BELL 206 206B3 1181506SW FLOAT BOTTLE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322751 0652A 3627 EMERGENCY FLOAT BOTTLE HAS CORROSION ON VALVE. REPLACED FLOAT BOTTLE VALVE BODY. 1G71 3U H2SW 20030225000702003022500070NM 2003 2 25 375PA0011 120030224A3350 CONNECTOR BOEING737 737317 138447PNM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 Forward section emergency exit lights inop. Found emergency light connection at row 3 ABC off. Reconnected and repositioned wiring. Lights ops. chk. normal. 2L72 4F RTA16WE 20030225000712003022500071NM 2003 2 25 371PA0016 120030224A3350 STRIP BOEING737 737306 13844BGNM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 Floor level emergency lights inop. Removed and replaced (3) photo illuminecent floor strips at row 1ABC, 9ABC, 11ABC were shorted. Ops chk. OK. 2L72 4F RTA16NE 20030225000722003022500072SW 2003 2 25 HEEA084293 120030211A6330407310202103 SPRING BELL 407 407 1182206SW GEARBOX MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 MAIN ROTOR GEARBOX MOUNT BEARING WORN; BOOT STRETCHED. 1G71 3U O H2SW 20030225000782003022500078SO 2003 2 25 C2XA03CL048 120030223A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2715973102212313 145159 CLE FLIGHT#2124 THE CREW REPORTED THE AFT AISLE PATH LIGHTING STRIPS #6,#7,#8 WOULD NOT STAY ILLUMINATED.MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001182003032700118SO 2003 3 27 C2XA03CL047 120030222A4950 DUCT EMB 145 EMB145ER 3260211SO APU SHUTOFF VALVSEPARATED A C2XAE ENGINE SHUTDOWN BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW2713929 145009 CLE FLIGHT 2032 THE CREW REPORTED ON TAXI RECEIVED A APU BLEED LEAK INDICATION THEN A SMOKE ODOR WAS NOTICED. THE APU WAS SHUTDOWN. MAINTENANCE INSPECTED AND FOUND THE APU BLEED DUCT SEPARATED DOWN STREAM OF THE APU SHUT-OFF VALVE. THE BLEED DUCT ASSEMBLY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030225000832003022500083SW 2003 2 25 HEEA084297 120030211A6330407310203101 MOUNT BELL 407 407 1182206SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR GEARBOX MOUNT WORN. 1G71 3U O H2SW 20030225000842003022500084SW 2003 2 25 HEEA084298 120030211A6330407310203101 MOUNT BELL 407 407 1182206SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR GEARBOX MOUNT WORN. 1G71 3U O H2SW 20030225000882003022500088SW 2003 2 25 HEEA084302 120030211A6321407340302101 CALIPER BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 ROTOR BRAKE CALIPER WORN AND WEAK. 1G71 3U O H2SW 20030225000892003022500089WP 2003 2 25 ZW0A0302701 120030221A33501315 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13912TW 49183 DURING OVERNITE PS CHECK AFT WALKWAY CTR CHUTE LITE INOP. REPLACED LAMP WITH BULB OPS CHECK PER 33-53-00. CHECK-C STL 11-27-02. --CLOSED-- 2L72 4F A6WE 20030225000932003022500093EU 2003 2 25 03052312 120030221A3350DM21 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU UNSERVICEABLE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27312UE 41025 EMERGENCY TRACK LIGHTING ROWS 3A-4A INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED PROXIMITY LIGHTING ELECTRICAL CONNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTIUED SERVICE. 2L72 4T RTA41NM 20030225000972003022500097EA 2003 2 25 COMA0360120 120030222A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01708CA5332 7235 FLIGHT 5862 GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030225000982003022500098CE 2003 2 25 NSVA200300010 120030212A5100NA SKIN PANEL BEECH 1900 1900C 1154161CE WORN A NSVAK NONE O OTHER UKUNKNOWN 1 EA27119CJ26615 UC19 Detail inspection: Captains partition lug receptacle (in cabin area) elongated and cracked. MX - Removed damaged area and installed doubler repair IAW Field repair FR-CO-00816 REV, dated 02/13/03. 2L72 4T RTA24CE 20030225000992003022500099EU 2003 2 25 AWXA200300205 120030211A5321D537175602400 PANEL AIRBUS320 A320232 3930326EU TORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW0 0 770 MCN - MAJOR REPAIR - DURING C-04 CHECK CORE DAMAGE WAS FOUND ON AFT GALLEY FLOOR PANEL, 2 EACH SCREW INSERTS WERE ALSO FOUND DAMAGED, FR 68 - 70. MAINTENANCE PERFORMED COMPOSITE REPAIR ON AFT GALLEY FLOOR PANEL IAW A320 SRM 53-02-00, PG. 102-105, & 108, FIG. 1, AND PG. 202-207, FIG. 202. 2L72 4F RTA28NM 20030226000082003022600008SW 2003 2 26 HEEA084306 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030226000142003022600014WP 2003 2 26 ABXA030082 120030225A32600080004003 CONTROL BOX DOUG DC9 DC941 302207NWP E & E DEFECTIVE A ABXAO OTHER O OTHER CRCRUISE 1 GL23956AX20 47620 RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR RECYCLED. ABNORMAL COMPLIED WITH FOR RETURN FLIGHT TO ILN. REMOVED AND REPLACED PROX. CONTROL BOX. PERFORMED ADJUSTMENT TEST OF LANDING GEAR POSITION AND WARNING INDICATION SYSTEM IAW DC-9 MM 32-60-00-2. 2L72 4F A6WE 20030226000152003022600015EA 2003 2 26 03057630 120030226A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 Emergency Lighting in passenger compartment inoperative. Maintenance personnel relamped emergency lighting. Operational check good. Aircraft released for continued service 2L72 4F RTA21EA 20030226000212003022600021SW 2003 2 26 HEEA084314 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030226000362003022600036SW 2003 2 26 HEEA084325 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 FUEL CELL PRESSURE SWITCH WILL NOT TURN OFF LIGHT WHEN BOOST PUMP ON. 1G71 3U O H2SW 20030226000382003022600038SW 2003 2 26 HEEA084327 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 FUEL TRANSFER LIGHT WOULD NOT COME ON WHEN RIGHT TRANSFER PUMP IS TURNED OFF. REPLACED FUEL CELL PRESSURE SWITCH. 1G71 3U O H2SW 20030226000502003022600050SW 2003 2 26 HEEA084339 120030211A7933407375004101 INDICATOR BELL 407 407 1182206SW ENGINE OIL TEMP ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 ENGINE OIL TEMP INDICATOR DISPLAYS ERRATIC READINGS. 1G71 3U O H2SW 20030226000512003022600051SW 2003 2 26 HEEA084340 120030211A7933407375004101 INDICATOR BELL 407 407 1182206SW ENGINE OIL TEMP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 ENGINE OIL TEMP INDICATOR CAUSING THE DUAL TACH TO GO INTO TEST MODE AT ANY GIVEN TIME. 1G71 3U O H2SW 20030226000542003022600054SW 2003 2 26 HEEA084343 120030211A6340407375005101 INDICATOR BELL 407 407 1182206SW GEARBOX OIL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 AFTER A FEW MINUTES OF FLIGHT, TEMP SIDE OF GEARBOX OIL TEMP/PRESSURE INDICATOR GOES OUT. 1G71 3U O H2SW 20030226000592003022600059SW 2003 2 26 HEEA084348 120030211A6340407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 DUAL TACH INDICATOR ROTOR INDICATION INTERMITTENTLY DROPS TO ZERO DURING STARTS. 1G71 3U O H2SW 20030226000672003022600067SW 2003 2 26 HEEA084354 120030211A2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL QTY MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 SIGNAL COND UNIT MALFUNCTIONED, LOW LEVEL LIGHT COMES ON. 1G71 3U O H2SW 20030226000712003022600071SW 2003 2 26 HEEA084358 120030211A2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL QTY SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH 53435 SIGNAL COND UNIT GIVES NUMEROUS LOW FUEL LIGHTS AND UNMODIFIED CONDITIONER. 1G71 3U O H2SW 20030227000022003022700002SO 2003 2 27 C2XA03SH032 120030227A270014520739403 BRACKET EMB 145 EMB145ER 3260211SO CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C CHECK THE BRACKET SUPPORTING THE ELEVATOR PULLEYS WAS FOUND CRACKED AND DEFORMED LOCATED IN VERTICAL STABILIZER BY PANEL 325LR. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030227000082003022700008SW 2003 2 27 HEEA084366 120030211A5210407515121 BRACKET BELL 407 407 1182206SW PAX DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 LT PASSENGER DOOR STRUT LOWER BRACKET CRACKED. SCRAPPED. 1G71 3U O H2SW 20030227000312003022700031SW 2003 2 27 HEEA084372 120030211A3030A026 STATIC VENT BELL 407 407 1182206SW PITOT STATIC SYSMALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 RT STATIC VENT HEATING ELEMENT DOES NOT WORK. 1G71 3U O H2SW 20030227000502003022700050SW 2003 2 27 HEEA084379 120030211A6340B47131 CHIP DETECTOR BELL 407 407 1182206SW FREEWHEEL UNIT INTERMITTENT E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03742PH 53461 FREEWHEEL UNIT CHIP DETECTOR CAUSING INTERMITTENT CHIP LIGHTS. 1G71 3U O H2SW 20030227000632003022700063GL 2003 2 27 HEEA084381 220030211A7421CH34187A IGNITER BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 IGNITER PRODUCING A DELAYED LIGHT OFF. SCRAPPED. 1G71 3U3 UO H2SW E4CE 20030227000722003022700072 2003 2 27 HEEA084383 420030211A2312CI197 ANTENNA BELL 407 407 1182206SW VHF COMMS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 VHF COMMUNICATIONS ANTENNA CORRODED. SCRAPPED. 1G71 3U O H2SW 20030227000732003022700073SW 2003 2 27 HEEA084384 120030211A6321D01631 PAD BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 ROTOR BRAKE WEAK, PADS WORN. 1G71 3U O H2SW 20030227000742003022700074GL 2003 2 27 HEEA084385 220030211A7320FCB405AT4 RELAY BELL 407 407 1182206SW ALLSN 250C 250C* GL FADEC MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 RELAY CAUSING A FADEC DEGRADE LIGHT ON START. 1G71 3U3 UO H2SW E4CE 20030227000842003022700084SW 2003 2 27 HEEA084391 120030212A6510PHI40702 SHAFT BELL 407 407 1182206SW T/R BLOWER DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 UNABLE TO BALANCE NR 2 BLOWER ASSY SHAFT. REPAIRED. 1G71 3U O H2SW 20030227000902003022700090SW 2003 2 27 HEEA084396 120030212A6520 SEAL BELL 407 407 1182206SW GEARBOX LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH A1667 53393 GEARBOX INPUT SEAL LEAKING. REPAIRED. 1G71 3U O H2SW 20030227000922003022700092SO 2003 2 27 C2XA03CL056 120030226A27613604401007 ACTUATOR EMB 135 EMB135LR 3260305SO RT WING LEAKING A C2XAB EMER. DESCENT JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW2714522 145383 CLE FLIGHT#2315 THE CREW REPORTED A #1 HYDRAULIC SYSTEM FAILURE IN FLIGHT.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE RIGHT INBOARD SPOILER ACTUATOR LEAKING.THE SPOILER ACTUATOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030227000942003022700094 2003 2 27 HEEA084398 420030212A2340PM212302 SWITCH BELL 407 407 1182206SW CYCLIC STICK STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 ICS/RADIO SWITCH INTERMITTENTLY STICKS IN TRANSMIT POSITION. 1G71 3U O H2SW 20030227000982003022700098NE 2003 2 27 COMA0360121 220030225A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE A COMAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO01984CA 7171 FLIGHT 5048 LEFT ENGINE N2 VIB INDICATION.COULD NOT DUPLICATE. NO VIB INDICATIONS DURING ENGINE RUNS. 2L72 4F4 FRTA21EA E15NE 20030227000992003022700099EA 2003 2 27 COMA0360122 120030225A33506464 CABLE CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR UNRELIABLE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01819CA 7415 FLIGHT 5154 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED POWER STRIP AT ROWS 2 THRU 5. 2L72 4F RTA21EA 20030227001002003022700100SW 2003 2 27 HEEA084404 120030212A2420SM20ACD300A21 CONTACTOR BELL 407 407 1182206SW ELECTRICAL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 NO AUTO RELIGHT AND NO IGNITER ON START. CONTACTOR FAILED. 1G71 3U O H2SW 20030227001012003022700101SW 2003 2 27 HEEA084405 120030212A2420SM20ACD300A21 CONTACTOR BELL 407 407 1182206SW ELECTRICAL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 ENGINE DEGRADE LIGHT. 1G71 3U O H2SW 20030227001142003022700114SW 2003 2 27 HEEA084420 120030212A67001200134A SLEEVE BELL 222 222U 1182140SW BELLCRANK ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 ROUGH BEARINGS. REPLACED BEARINGS DSP4 AND SLEEVES DUE TO WORN. REPAIRED. 1G72 3U H9SW 20030227001202003022700120SW 2003 2 27 HEEA084426 120030213A2510222320823119 SEAT BELT BELL 222 222 1182122SW COCKPIT MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 ON THE SHOULDER RESTRAINT THE LENGTH BETWEEN WHERE THE STRAPS SPLIT AND THE ADJUSTING BUCKLES IS TOO SHORT. REPLACED WITH SERVICEABLE ASSY. 1G72 3U H9SW 20030227001262003022700126 2003 2 27 HEEA084432 420030213A3452066106200 TRANSPONDER BELL 206 206L3 1182108SW VOR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 TRANSPONDER WILL NOT REPLY TO INTERROGATIONS. SHOP REPAIR. 1G71 3U H2SW 20030227001322003022700132SW 2003 2 27 HEEA084438 120030213A6710206001053005 BEARING BELL 206 206L1 1182107SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035014V MW47 45217 CYCLIC CONTROL BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030227001332003022700133SW 2003 2 27 HEEA084439 120030213A6230206010803101 BUSHING BELL 206 206L3 1182108SW M/R IDLER LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR IDLER LINK HAS WORN BUSHINGS. REPLACED 8 BUSHINGS DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030227001342003022700134SW 2003 2 27 HEEA084440 120030213A6230206010803101 BUSHING BELL 206 206L3 1182108SW M/R IDLER LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR IDLER LINK HAS WORN BUSHINGS. REPLACED 8 IDLER LINK BUSHINGS DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030228000012003022800001NM 2003 2 28 751PA0012 120030223A335020131 BATTERY PACK BOEING757 757200 1384950NM CABIN DISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 FOUR EMERGENCY PATH LIGHTS INOP - MAIN CABIN ROW 1-3. REPLACED BATTERY PACK. OPS CHK GOOD PER MM 25-60-00. 2L72 4F RTA2NM 20030228000052003022800005SW 2003 2 28 HEEA084442 120030213A6230206010803101 BUSHING BELL 206 206L3 1182108SW IDLER LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR IDLER LINK HAS WORN BUSHINGS. REPLACED 8 BUSHINGS DUE TO WORN. REPLACED 2 COLLAR SETS, DUE TO CORROSION. REPAIRED. 1G71 3U H2SW 20030228000112003022800011NM 2003 2 28 SWAA030433 120030226A53116516302 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED ( 2 EA ) AT BS 188, STR 17L & STR 17R. R&R FRAMES PER SRM. 2L72 4F RTA16WE 20030228000142003022800014SW 2003 2 28 HEEA084444 120030213A6220206011118001 BEARING BELL 206 206L3 1182108SW M/R HEAD CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y7110 MR052699 51609 GRIP SEAL LEAKING GREASE. REPLACED BEARING 206011118001 DUE TO CORROSION ON ROLLER AND RETAINER 206011129003 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030228000252003022800025NM 2003 2 28 SWAA030385 120030217A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR LOWER HINGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030228000272003022800027NM 2003 2 28 SWAA030387 120030215A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING OTS, FOUND FUSELAGE SKIN CRACKED 2.5 LONG AT BS 311, BELOW STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030228000292003022800029NM 2003 2 28 SWAA030407 120030219A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, ABOVE STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030228000322003022800032EA 2003 2 28 COMA0360123 120030225A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01916CA 7014 FLIGHT 5806 GEAR DISAGREE WARNING.CLEANED AND SERVICED NLG - RETRACTION CHECKS NORMAL. 2L72 4F RTA21EA 20030116001422003011600142 2003 1 16 HEEA083086 420030108A3452066106200 TRANSPONDER BELL 206 206L3 1182108SW ATC SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0392MT 51175 ATC TRANSPONDER CODE TRANSMITTED NOT DISPLAYED. 1G71 3U H2SW 20030116001442003011600144 2003 1 16 HEEA083088 420030108A3444066305401 INDICATOR BELL 206 206L3 1182108SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 RADAR ALTIMETER INDICATOR INOPERATIVE. IN SHOP REPAIR. 1G71 3U H2SW 20030116001452003011600145 2003 1 16 HEEA083089 420030108A3442066305401 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 RADAR ALTIMETER STUCK AT 500 FEET. IN SHOP REPAIR. 1G71 3U H2SW 20030116001462003011600146 2003 1 16 HEEA083090 420030108A3444066305401 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 RADAR ALTIMETER INDICATION INACCURATE ABOVE 450 FEET. 1G71 3U H2SW 20030116001482003011600148 2003 1 16 HEEA083092 420030108A3454069102505 TRANSCEIVER BELL 206 206L3 1182108SW VOR SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251V 51404 VOR TRANSCEIVER INOPERATIVE. CAN HEAR WHEN THE POWER SWITCH IS BEING TURNED ON AND OFF OVER HEADSET. REPLACED DIODE CR413. REPAIRED. ALSO REPLACED BROKEN SWITCH S402. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001572003011600157NM 2003 1 16 2003F00084 120030106A3350 STRIP BOEING737 73783N 13844HINM CABIN LOOSE A AMTAK NONE O OTHER TXTAXI/GRND HDL 1 GL11306TZ 32348 PHOTO LUMINESCENT LIGHT STRIP CAME LOOSE FWD RIGHT SIDE. RESECURED PER MM 33-51-15-960-801. 2L72 4F RTA16WE 20030116001712003011600171SO 2003 1 16 C2XA02SH165 120030103A532014522460013 BUTT STRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV- DURING C-CHECK CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20-23. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116001932003011600193SW 2003 1 16 HEEA083105 120030108A243615891F REGULATOR BELL 206 206B3 1181506SW DC SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 UNABLE TO ADJUST REGULATOR PAST 27 VOLTS. 1G71 3U H2SW 20030116001952003011600195 2003 1 16 HEEA083107 420030108A34571624820 ANTENNA BELL 206 206L3 1182108SW GPS SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331821 51076 ANTENNA SLOW TO COME ON LINE. 1G71 3U H2SW 20030116002022003011600202SW 2003 1 16 HEEA083117 120030108A6710 PAD BELL 206 206L3 1182108SW LT CYCLIC IDLER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 LT CYCLIC IDLER WEAR PAD UNBONDED. REPAIRED. 1G71 3U H2SW 20030116002042003011600204SW 2003 1 16 HEEA083119 120030108A6700 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 ROTORCRAFT FLIGHT CONTROL BELLCRANK HAS WORN BEARINGS. REPAIRED. 1G71 3U H2SW 20030116002062003011600206SW 2003 1 16 HEEA083121 120030108A6700 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 ROTORCRAFT FLIGHT CONTROLS BELLCRANK HAS WORN BEARINGS. SCRAPPED. 1G71 3U H2SW 20030116002112003011600211SW 2003 1 16 HEEA083125 120030108A6420 BEARING BELL 206 206L3 1182108SW PITCH LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 TAIL ROTOR HEAD PITCH CONTROL LINK HAS WORN BEARINGS. REPAIRED. 1G71 3U H2SW 20030116002282003011600228SW 2003 1 16 HEEA083131 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW FLAP STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 MAIN ROTOR FLAP RESTRAINT STICKING IN DOWN POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116002302003011600230SW 2003 1 16 HEEA083132 120030108A6220206011117003 RESTRAINT BELL 206 206B3 1181506SW MAIN ROTOR FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MAIN ROTOR FLAP RESTRAINT STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116002482003011600248SW 2003 1 16 HEEA083134 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MAIN ROTOR FLAP RESTRAINT STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030310000732003031000073SW 2003 3 10 HEEA084977 120030227A6710 BEARING BELL 412 412 1182202SW UNIVERSAL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N BT780 33002 WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030310000782003031000078 2003 3 10 HEEA084982 420030227A22157001484 ACTUATOR BELL 412 412 1182202SW YAW CONTROL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 YAW CONTROL NEEDLE FULL DEFLECTION TO NR 1 SIDE. 1G72 4U H4SW 20030310000882003031000088 2003 3 10 HEEA084992 420030227A3120811B CLOCK BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 DIGITAL CLOCK INOPERATIVE. REPAIRED. 1G72 4U H4SW 20030310000902003031000090 2003 3 10 HEEA084995 420030227A34578143902240B GPS BELL 412 412 1182202SW COCKIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 GPS WILL NOT RECOGNIZE DATA CARD. SENT TO ASM FREEFLIGHT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030310000992003031000099SW 2003 3 10 HEEA085004 120030227A3212D24921115 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 FLOAT BAG ASSY LEAKS. SCRAPPED. 1G72 4U H4SW 20030310001142003031000114 2003 3 10 HEEA085021 420030228A345713824120234 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 GPS LOSES ONBOARD MEMORY WHEN POWER IS TURNED OFF. 1G71 3U H2SW 20030310001152003031000115SW 2003 3 10 HEEA085022 120030228A6230206010440001 BEARING BELL 206 206L3 1182108SW SWASHPLATE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH17539 GDJG10471 51303 SWASHPLATE SUPPORT GROOVED. REPLACED BEARING DUE TO WORN AND SLEEVE SLIDER BEARING 206010459001 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030310001232003031000123EU 2003 3 10 03069324 120030307A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27324UE 41017 During maintenance/inspection emergency light strip inoperative fwd end. Maintenance personnel resecured fwd emergency light connectors. Ops ck'd good. Aircraft returned to service. 2L72 4T RTA41NM 20030310001242003031000124SW 2003 3 10 HEEA085024 120030228A6230206010803101 BUSHING BELL 206 206L3 1182108SW DRIVE LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 WORN BUSHINGS. REPLACED 8 BUSHINGS DUE TO WORN. REPLACED COLLAR SET 206011005101, S/N 2137 DUE TO PITTING ON SPLINES. REPAIRED. 1G71 3U H2SW 20030625001162003062500116WP 2003 6 25 IXXA0300022O 120030305A7603 CONTROL CABLE DOUG DC8 DC871F 302199DWP NR 1 ENGINE OUT OF RIG A IXXAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 SW11820BX826873000 46065 AFTER DEPARTURE FROM GSO WHILE PERFORMING POST HEAVY MAINTENANCE CHECK FLIGHT. COMPRESSOR STALL ON NR 1 ENGINE WAS NOTED WHILE REDUCING POWER SETTING FROM CLIMB TO CRUISE. AS PRECAUTIONARY ACTION NR 1 ENGINE WAS SHUTDOWN. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE INSPECTED FAN EXHAUST AND BOROSCOPED ENGINE IN ACCORDANCE WITH CFM56 MAINTENANCE MANUAL AND ATI JOB CARD 30.07. MAINTENANCE FOUND VARIABLE STATOR VALVE AND VARIABLE BLEED VALVE FEEDBACK CABLE OUT OF RIG. MAINTENANCE RIGGED CABLES IN ACCORDANCE WITH CFM56 MAINTENANCE MANUAL. 2L74 4F RT4A25 20030310001332003031000133NM 2003 3 10 EIA2003038 120030228A5300UNK SKIN PANEL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 LEFT WING WHEEL WELL, UPPER FOWARD RIGHT CORNER, BS 1241, LBL6-LBL175, CORROSION ON OUTER SKIRT CORECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECT AREA, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-68-2 2L74 4F A20WE 20030310001342003031000134NM 2003 3 10 EIA2003039 120030228A5300UNK INTERCOSTAL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 TOP SIDE OF NOSE WHEEL WELL BETWEEN STA 260 & 280, INTERCOSTAL AT RBL20 CRACKED. CORRECTIVE ACTION: REMOVED & REPLACED INTERCOSTAL @ STA 260-280, PER ECRA 481-53-170-2 Rev A 2L74 4F A20WE 20030310001352003031000135NM 2003 3 10 EIA2003007 120030224A5700 SKIN BOEING747 747132 1384882NM FUSELAGE CORRODED A EIAAO OTHER O OTHER ININSP/MAINT 1 NM09481EV 19896 FS 1350 RBL4 TO LBL4 TOP SURFACE OF WING BOX PILLOWING (CORROSION). REMOVED DAMAGE, NDT AREA, FAB'D & INSTALLED REPAIR PARTS PER ECRA 481-53-165-2. 2L74 4F A20WE 20030310001372003031000137NM 2003 3 10 EIA2003010 120030226A530065B2826656 STIFFENER BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 STIFFENER CRACKED AT STA 291, LBL 10 ON TOP OF NOSE WHEEL WELL BO. CORRECTIVE ACION: INSTALLED KIT # 65B28266-5 AND SUB KIT 65B28266-6 PER E.O. 53-747-1138-91 REV C, PER S.B. B747SRM 51-30-02 PGS 1-15 2L74 4F A20WE 20030310001392003031000139NM 2003 3 10 EIA2003012 120030226A5300UNK SKIN PANEL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Improper Fastener on lap Seam at STA. 615 and S-47R on Fuselage below FWD. Lower Cargo Compt. CORRECTIVE ACTION: Removed fastener and existing doubler, cut overlapping skin, requested NDT, fabricated, alondined, primed and installed -1 repair doubler and -2 filler per B-747 SRM, Ch.53-30-03, Fig.17, & SOPM Ch. 20-41-02, Pg. 17-19. Category "B" Repair COI# 53I initiated. 2L74 4F A20WE 20030310001412003031000141NM 2003 3 10 EIA2003040 120030228A5300UNK ANGLE BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 MAIN DECK STA 1168, BBL35R, WL 19.6, CENTER TANK ANGLE HAS CRACK. CORRECTIVE ACTION: REMOVED DAMAGE, NDT AREA, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-172-2 2L74 4F A20WE 20030310001492003031000149NM 2003 3 10 EIA2003017 120030227A5300UNK BELTFRAME BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Cracked frame at STA 1740. Stringer 4 left. CORRECTIVE ACION: Repaired cracked frame at STA 1740 stringer 4 left per ECRA 481-53-173-2 2L74 4F A20WE 20030310001522003031000152NM 2003 3 10 EIA2003020 120030226A5300UNK BELTFRAME BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 R/H STA 1740 between Stringer 12R & 13R frame bent and gouged. CORRECTIVE ACTION: Repaired R/H STA 1740 Frame @ Sringer 12R- 13R per ECRA 481-53-176-2 2L74 4F A20WE 20030310001532003031000153NM 2003 3 10 EIA2003021 120030226A5500UNK SKIN PANEL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Impact damage on R/H bottom of Horizontal Stab at STA 240, 30" from L/E. CORRECTIVE ACTION: Repaired damaged skin and Rib lower chord per B747 SRM 55-10-02, 55-10-03, 51-1002, 51-4--04, & ECRA 481-53-180-2 2L74 4F A20WE 20030310001572003031000157WP 2003 3 10 EIA2003047 120030228A5300UNK SKIN PANEL DOUG DC9 DC933F 302207AWP A EIAAK NONE O OTHER ININSP/MAINT 1 NM09944F 47194 GOUGH AFT OF MAIN CARGO DOOR CORRECTIVE ACTION: CLASS I REPAIR INSTALLED ON L/H FUSELAGE STA 447.5 to STA 457.5, from LONGERON 16L-17L (DOUBLER) PER DC9 SRM 53-04 Pg 60 & DC9 SRM 51-30-5, Pgs 1-30. REPETITIVE INSPECTION REQUIRED PER DC9 SRM 53-04, FIG 12B, SHEET 1, Pg 53. NOTE: F5302 PLUS SKETCH SENT TO EIA ENGINEERING. 2L72 4F A6WE 20030310001602003031000160NM 2003 3 10 EIA2003025 120030228A5300UNK STRAP BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Stringer 46L corroded under frame at B.S. 1700 (AFT PIT). CORECTIVE ACTION: Repaired per ECRA # 481-53-158-2 Rev A. Fab'd Strap (M) per ECRA. Installed per B747 SRM 51-30-02, Pgs 57-58-58B 2L74 4F A20WE 20030310001642003031000164NM 2003 3 10 EIA2003030 120030228A5600UNK WINDOW FRAME BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Fuselage STA 544 Left Side interior window forging corosion. CORRECTIVE ACTION: Repaired per ECRA 481-53-178-2. Reworked forging per B747 SRM 56-20-01, Fig 1, 51-10-02, Pg 7, & SOPM 20-41-02, Pgs 1-15. 2L74 4F A20WE 20030311000022003031100002SW 2003 3 11 HEEA085026 120030228A6220 GRIP SEAL BELL 206 206L1 1182107SW M/R HEAD LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0345RP 8741 HB400 45521 MAIN ROTOR HEAD SLINGING GREASE FROM GRIP SEAL. REPAIRED. 1G71 3U H2SW 20030311000062003031100006SW 2003 3 11 HEEA085030 120030228A5510209001051001 BEARING BELL 206 206L3 1182108SW HORN ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03205FC 51130 HORIZONTAL STAB HORN HAS A WORN BEARING. REPAIRED. 1G71 3U H2SW 20030311000232003031100023SW 2003 3 11 HEEA085044 120030228A2510222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT FRAYED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 SEAT BELT FRAYED AND WORN. REPLACED WITH SERVICEABLE RESTRAINT. 1G71 3U H2SW 20030311000312003031100031GL 2003 3 11 HEEA085048 220030228A7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE STIFF E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 GOVERNOR HAS A STIFF ARM AND UNABLE TO FREE IT. SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030311000372003031100037GL 2003 3 11 HEEA085053 220030228A72506892828 SHIELD BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL NR 1 NOZZLE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 NOZZLE SHIELD CRACKED. IN REPAIR. 1G71 3U3 U H2SW E1GL 20030311000482003031100048SW 2003 3 11 HEEA085063 120030228A6720PHI206L3957 CONTROL ROD BELL 407 407 1182206SW T/R PITCH WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 WORN PITCH CONTROL SHAFT. REPAIRED. 1G71 3U O H2SW 20030311000562003031100056EU 2003 3 11 HEEA085070 120030227A641010531980 BLADE BOLKMS105 BO105S 5626006EU TAIL ROTOR ERODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038199J S826 T/R BLADE HAS PAINT EROSION. 1G72 3U H3EU 20030311000622003031100062EU 2003 3 11 HEEA085078 120030228A6700 BEARING AEROSPAS355 AS355* EU CONTROL TUBE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH 3248 BEARING ON VERTICAL, LONGITUDE CONTROL TUBE RUSTED AND WILL NOT TURN. 1G72 3U H11EU 20030311000642003031100064EU 2003 3 11 HEEA085081 120030228A7931642790041 TRANSMITTER AEROSPAS355 AS355* EU OIL PRESS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03974AE 2653 ENGINE OIL PRESSURE INDICATOR PEGGING OUT AT 10 BARS. REPLACED THE ENGINE OIL PRESSURE TRANSMITTER. 1G72 3U H11EU 20030311000702003031100070NM 2003 3 11 AWXA200300244 120030228A53156545834551 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C-14 CHECK A 3/4 INCH CRACK WAS FOUND ON CHANNEL BETWEEN FLOORBEAMS AT BS 328, LBL 49. MAINTENANCE REMOVED DAMAGED CHANNEL BETWEEN FLOORBEAMS AT BS 328, LBL 49; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11, 38, & 45, FIG. 8 & 12, AND SRM 51-40-05, PG. 4, & 9, FIG. 2 & 4. 2L72 4F RTA16WE 20030228000392003022800039SW 2003 2 28 HEEA084449 120030213A6330 BEARING BELL 206 206L3 1182108SW XMSN RESTRAINT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 LK0808 51520 MAIN ROTOR TRANSMISSION RESTRAINT HAS WORN BEARINGS. SHOP REPAIR. 1G71 3U H2SW 20030228000832003022800083SW 2003 2 28 HEEA084454 120030213A6510 BEARING BELL 206 206L3 1182108SW T/R FAN ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E PHI233 51498 TAIL ROTOR DRIVESHAFT COOLING FAN ASSY HAS WORN BEARINGS. REPAIRED. 1G71 3U H2SW 20030228000962003022800096EU 2003 2 28 MALA030173 120030220A304016581 WINDSHIELD SAAB SF340 340B 7860101EU A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15441XJ 340B441 RH FRONT WINDOW HEAT INOP ON FLIGHT #3034. COULD NOT DEFER DUE TO WEATHER IN BIS. AIR RETURN TO MSP. MAINTENANCE REPLACED RH WINDSHIELD CONTROLLER PN 1658-1 SN/OFF 594, SN/ON 578 PER AMM 30-41-10. OPS CHECK GOOD. 2L72 4T RTA52EU 20030228001022003022800102NM 2003 2 28 DHL2003748002 120030226A7800 TAIL CONE BOEING727 727225 1384077NM A DHLAKO NONE OTHER O OTHER ININSP/MAINT 1 SO01748DH 22440 1) #1 ENGINE TAIL CONE HAS APPROXIMATELY 1" X 1" HOLE.2) TRANSFERRED TO LOG PAGE 338263, ITEM 15M.3) REF. N/R 21A: #1 ENGINE TAIL CONE HAS APPROXIMATELY 1" X 1" HOLE.4) REMOVED #1 ENGINE TAIL CONE. ITEM PLACED ON DEFERRAL PER DHL MEL/CDL 78-30-4, CONTROL #12139. AIRCRAFT LIMITED TO 5 FLIGHT HOURS UNDER THIS REFERENCE. PLACARD INSTALLED.5) RE: DMI #12139 - #1 ENGINE TAIL CONE HAS 1" X 1" HOLE.6) INSTALLED NEW TAIL CONE PER 78-30-0. CLEARS DMI #12139 PLACARD REMOVED. 2L73 4F A3WE 20030228001032003022800103 2003 2 28 HEEA084462 420030213A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 ADI INOPERATIVE. IN SHOP FOR REPAIR. 1G71 3U H2SW 20030228001072003022800107WP 2003 2 28 DHL2003801003 120030227A2820 SEAL DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER K FLUID LOSS NRNOT REPORTED 1 SO01801DH 46033 1) SUBSTANTIAL FUEL LEAK FROM ACCESS PANEL INBOARD OF #1 PYLON.2) FOUND GAMMA SEAL TORN AT #1 MAIN FUEL MANIFOLD INBOARD OF #1 PYLON. REPLACED SEALS AND LEAK CHECKED OK PER M/M 28-20-0. 2L74 4F RT4A25 20030228001162003022800116WP 2003 2 28 MWEA030116 120030227A532199365851 FLOORBOARD DOUG DC9 DC981 3022081WP STA 369 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOORBOARD BETWEEN SEAT TRACKS #1 AND #2 AT STATION 369 IS DENTED. -- REMOVED DAMAGED AREA AND INSTALLED REPAIR. 2L72 4F A6WE 20030228001172003022800117WP 2003 2 28 MWEA030118 120030227A532199365851 FLOORBOARD DOUG DC9 DC981 3022081WP STA 750 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOORBOARD BETWEEN SEAT TRACKS #3 AND #4 AT STATION 750 IS DENTED. -- REPAIRED DENT. 2L72 4F A6WE 20030228001212003022800121WP 2003 2 28 ABXA030092 120030203A5300995823869 FORMER DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 SHEAR TIE AT F.S. 1019, LONGERON 14 - 15 LEFT, CRACKED. REPLACED SHEAR TIE IAW DC-9 SRM. 2L72 4F A6WE 20030228001232003022800123SW 2003 2 28 HEEA084470 120030213A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F233 MAIN BATTERY LOSES ITS CHARGE AFTER SETTING OVERNIGHT. 1G71 3U H2SW 20030409000042003040900004NM 2003 4 9 AWXA200300215 120030219A2420BACC18AE35 CIRCUIT BREAKER BOEING737 7373G7 1384595NM COCKPIT DEFECTIVE A AWXAO OTHER HGSELECT. POWER LOSS-50 PC MULTIPLE FAILURE AFFECT SYSTEMS DEDESCENT 1 WP28322AW 25400 DURING DECENT LOST BOTH IRS, ALL F/O LIGHTS AND INSTRUMENTS, F/O EFIS DISPLAYS, & AUX & PITOT STATIC. MAINT FOUND TRANSFER BUS NR 2 C/B POPPED. INSPECTED WIRING BEHIND P6 & P18 C/B PANELS, & INSIDE AFT NLG WW ACCESS PANELS. INSPECTED J4, J5, & J20 BOXES, & BEHIND P5 PANEL. INSPECTED STANDBY INVERTER & NR 2 FIREWALL CONNECTOR. NO DEFECTS. R & R R4 RELAY & C/B C821 PER SPM. CHECK OF NR 2 TRANSFER BUS, NO SHORTS. RAN ENGS, PRESS A/C TO 3.5 PSI, BUS TRANSFER SYS NORMAL. OPERATED FLAPS IN NORMAL/STANDBY MODES, NO DEFECTS. OPS CHECK OF IRU GOOD, POWER TRANSFER TO BATTERY NORMAL. STALL WARNING COMPUTERS CHECKED GOOD. ANALYSIS OF C/B CONFIRMED FAILURE. ANALYSIS IDENTIFIED CIRCUIT BREAKER WOULD ONLY CARRY 35 AMPS. 2L72 4F RTA16WE 20030302000012003030200001NM 2003 3 2 HNAA0300010 120030227A2611PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8201 2809001NM LAVATORY DEFECTIVE A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07986HA9050 9050 421 Lav smoke detector went off shortly after departure. Captian returned to field, no smoke was detected. Lav smoke detector was replaced proir to this flight for same problem. MEL lav smoke detector, generated EO to pull and collar circuit breaker. Smoke detector replaced 1 MARCH 2003. 2H72 4T RTA13NM 20030303000012003030300001 2003 3 3 HEEA084474 420030214A3452066104100 TRANSPONDER BELL 412 412 1182202SW ATC SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 ATC TRANSPONDER HAS NO POWER OUT. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000022003030300002 2003 3 3 HEEA084475 420030214A3454066107800 RECEIVER BELL 412 412 1182202SW VHF SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 WHEN TUNED TO LOCALIZER, MAX DEFLECTION ON HIS NEEDLE GOES ONLY 1/2 SCALES. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000032003030300003 2003 3 3 HEEA084476 420030214A3416066306401 ENCODER BELL 412 412 1182202SW ALTIMETER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 ALTIMETER ENCODER BOUNCES 80 FT IN CRUISE FLIGHT. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030311001042003031100104 2003 3 11 249TR0013 420030303A2210 LIMIT SWITCH BOEING737 7372K5 138448XNM A PIDAK NONE O OTHER APAPPROACH 1 SO05249TR 22598 Both A & B auto pilots disengage after flaps reach #1 positon during approach. Will not re-engage until selected beyond flaps 5 positon. Replaced flaps up limit switch 5245(?) per MM 27-51-291 ops chk normal per MM 22-11-01. 2L72 4F RTA16WE 20030312000532003031200053WP 2003 3 12 CALA0300114 120030307A5754 SKIN DOUG DC9 DC981 3022081WP FLAP VANE DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 MAINTENANCE FOUND THE L/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED . THE FINAL TRIM OUT AREA MEASURED 4.7" X 5.6". THE SKIN WAS REPAIRED IAW ECRA 5750-03755. 2L72 4F A6WE 20030328000882003032800088NE 2003 3 28 COMA0360142 220030309A73146078T39P04 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01721CA12492 7259 807942 FOUND SMALL PIN HOLE IN RT ENG FUEL PUMP HOUSING, FOUND DURING A LEAK CHECK FOR A NON RELATED ITEM. REPLACED FUEL PUMP. 2L72 4F4 FRTA21EA E15NE 20030312000572003031200057EU 2003 3 12 WRNA200300006 120030307A33404223306 LANDING LIGHT AIRBUS300 A300B4203 3930306EU UNDERSERVICED A WRNAK NONE O OTHER TXTAXI/GRND HDL 1 SO05501TR 53 L/H taxi/take off circuit breaker on pnl #9 trips Corrective Action: Originally MEL assigned MEL 33-46-01 3-7-03 to be cleared by 3-17-03. Closing action: R&R'd L/H taxi light assy, ops check good I/A/W 33-46-12, MEL cleared. Closing date 3-10-03. 2L72 4F RTA35EU 20030312000602003031200060NM 2003 3 12 AWXA200300253 120030303A53206545402581 STIFFENER BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW0 0 24633 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/2" CRACK WAS FOUND ON STIFFENER IN L/H AIR CONDITIONING BAY, INBOARD END JUST ABOVE TURBO FAN, BS 658, LBL 18. MAINTENANCE REMOVED DAMAGED STIFFENER IN L/H AIR CONDITIONING BAY, BS 658, LBL 18; FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11. 2L72 4F RTA16WE 20030312000632003031200063SO 2003 3 12 C2XA03IA025 120030309A33501317 BULB EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713992 145284 IAH- DURING POSTFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT OVERHEAD REAR WAS OUT.IAH- MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BULB, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030312000652003031200065NM 2003 3 12 QXEA0300333 120030307A335010126267 SIGN DHAV DHC8 DHC8202 2809007NM A QXEAK NONE O OTHER UKUNKNOWN 1 NM09350PH 488 PDX- MAIN CABIN DOOR EXIT SIGN BROKE. MAINTENANCE REPLACED THE EXIT SIGN/EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030331001192003033100119NM 2003 3 31 DHL2003727003 120030306A5270 WARNING SYSTEM BOEING727 727228 1384083NM AIRSTAIR DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01727DH 20204 ON CLIMB FROM CVG, THRU 10,000 FT AFT AIRSTAIR AMBER LIGHT ILLUMINATED ON S/O'S PANEL. LIGHT EXTINGUISHED THRU FL 250. NO OTHER INDICATIONS NOTED. INSPECTED AFT AIRSTAIR UP LATCH MECHANISM IN THE OPEN AND CLOSED POSITION. LOCKING MECHANISM LOCKS NORMAL. DEFERRED WARNING LIGHT, PLACARD INSTALLED, IAW MEL 52-6-1 CAT-C DMI 12202. REF DMI 12202. ON CLIMB FROM CVG THRU 10,000 FT AFT AIRSTAIR AMBER LIGHT ILLUMINATED ON S/O PANEL. LIGHT EXTINGUISHED THRU FL 250. NO OTHER INDICATIONS NOTED. VERIFIED AFT AIRSTAIR UP AND LOCKED. DMI 12202 STILL IN EFFECT. 2L73 4F RTA3WE 20030313000262003031300026GL 2003 3 13 ALG2003F00025 220030210A732023072725 FADEC BELL 407 407 1182206SW ALLSN 250C 250C47B GL HMU/ENGINE FAILED A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03477AL3650 1181 53203 CAE847243 DURING FLIGHT, FIVE MILES FROM DESTINATION PLATFORM, ENGINE CHIP LIGHT ILLUMINATED, DURING FINAL APPROACH TO THE PLATFORM APPROXIMATELY 75 TO 100 FEET THE FADEC FAULT, FADEC MANUAL, FADEC FAIL, RESTART FAULT AND AUTO RELIGHT ILLUMINATED WITH FADEC FAIL AUDIO ACTIVATED - LANDING WAS COMPLETED TO THE PLATFORM WITH FADEC IN MANUAL MODE AND MAINTENANCE WAS NOTIFIED. UPON INSPECTION OF THE ENGINE, IT WAS DETERMINED THE ENGINE NEEDS TO BE REPLACED. 1G71 3U3 UO H2SW E1GL 20030313000282003031300028SW 2003 3 13 ALG2003F00027 120030210A6220 CYCLIC CONTROL BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL MAIN ROTOR OUT OF RIG E O OTHER O OTHER APAPPROACH 1 SW03176AL 52146 CAE890494 DURING APPROACH, PILOT WROTE (LANDED INTO WIND AND BACK TAXIED WITH TAILWIND TO PARKING, RAN OUT OF AFT CYCLIC, DID A GO-AROUND AFTER CHECKING TO MAKE SURE NOTHING WAS BLOCKING THE CYCLIC, RETURNED FOR A SLOW, SHALLOW APPROACH, SAME THING HAPPENED AGAIN. VISUALLY CHECKED CYCLIC AND LANDED) UPON LANDING PRELIMINARY INVESTIGATION REVEALED THAT CYCLIC CONTROL WAS OUT OF RIG. 1G71 3U3 UNCH2SW E1GL 20030313000732003031300073NE 2003 3 13 12964 220030304A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE WING MALFUNCTIONED A UHLAEA ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP TOTAKEOFF 1 GL17148SD 340A148 367142 FLT 4474 DEPARTING PIT ON TAKEOFF ROLL, PILOT REPORTED ENGINE ITT PEGGED WITH NO OTHER INDICATIONS NOTED BY CREW. ENGINE SHUTDOWN AND AN EMERGENCY LANDING WAS MADE IN PIT. MAINTENANCE NOTIFIED. 2L72 4T4 TRTA52EU E8NE6 20030313000802003031300080 2003 3 13 B652003F00000 420030210A2210 AUTOPILOT SYS UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE MALFUNCTIONED A B65AO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL13135CR 0164 WHILE ON A IFR TRAINING FLIGHT AIRCRAFT EXPERIENCED UN-COMMANDED ROLL AND PITCH MOVEMENTS WITH NO CAUTION LIGHTS OR MESSAGES. AUTOPILOTS DISENGAGED (REVISION TO FLIGHT MANUAL). NOTE: MAINTENANCE DID NOT FIND A CAUSE FOR THE UNCOMMANDED MOVEMENTS. 1G72 3U3 U H88EU E34NE 20030313000902003031300090CE 2003 3 13 2003F00141 120030313A32601SE33 SWITCH CESSNA310 310J 2074226CE MLG FAILED G O OTHER N FALSE WARNING LDLANDING 1 SW01308J 310J0142 ON APPROACH TO ELP THE PILOT DID NOT HAVE A GREEN LIGHT AFTER SELECTING GEAR DOWN. A FLY BY INDICATED GEAR APPEARED IN NORMAL DOWN POSITION. PILOT LANDED WITHOUT INCIDENT. THE LEFT HAND MICRO SWITCH PN 1SE3-3 FAILED INTERNALLY. REMOVED AND REPLACED SWITCH. 1L72 3O 3A10 20030313000912003031300091EU 2003 3 13 A20203 120030207A2752 SEAL PILATSPC12 PC1245 7090551EU PWA PT6 PT6A66 52043NE TE FLAP ACTUATORLEAKING E WUXAK NONE KW FLUID LOSS INADEQUATE Q C ININSP/MAINT 1 NM11253PC1616 253 FUEL BEGAN LEAKING FROM LEFT WING UPON REMOVAL OF LEFT OUTBOARD FLAP LINEAR ACTUATOR FROM THE WING REAR SPAR. INVESTIGATION REVEALED FLAP ACTUATOR BOX, SEAL PACKING HAD BEGUN LEAKING DUE TO (4 EACH) IMPROPERLY SECURED FASTENERS. THESE FASTENERS ATTACH THE BOX TO THE INSIDE OF THE AFT SPAR. THE TWO FLAP ACTUATOR ATTACHMENT FASTENERS SECURE INTO THIS BOX ASSEMBLY ALONG WITH THE FOUR IMPROPERLY SECURED FASTENERS. REMOVAL OF THE ACTUATOR RELEASED THE BOX ALLOWING FUEL TO ESCAPE THE WING THROUGH THE AFT SPAR. EMERGENCY DEFUELING OF THE AIRCRAFT WAS REQUIRED TO PREVENT ASSOCIATED MAINTENANCE FACILITY HAZARDS. AN AIRCRAFT HISTORICAL RECORDS SEARCH REVEALED NO PREVIOUS MAINTENANCE TO THE AFFECTED BOX ASSEMBLY. 1L71 3T4 TRTA78EU E26NE 20030313001052003031300105SO 2003 3 13 C852003F00000 120030212A321365319004 HOUSING PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA MLG STRUT CRACKED B C85RO OTHER O OTHER NRNOT REPORTED 1 NE014337P9722 288416044 DURING ROUTINE 100 HOUR INSPECTION, STRUT HOUSING WAS FOUND CRACKED IN THE AREA WHERE THE RADIUS IS, FOR THE TORQUE LINK TO PIVOT. WHERE THE EARS COME OFF THE STRUT. IN AREA WHERE RADIUS IS GROUND INTO STRUT HOUSING. 1L71 3O3 O 2A13 E274 20030313001152003031300115CE 2003 3 13 FPI2003F00006 120030206A323398820152 ACTUATOR BEECH 35 E35 1151512CE CONT O520 TSIO520* 17040SO LANDING GEAR CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO153311C16586 D3977 C/W SEB 01-2 INSPECTED ACTUATORS, FOR CRACKS. FOUND CRACKS, REMOVED FROM SERVICE. 1L71 3O3 O A777 E8CE 20030313001252003031300125SO 2003 3 13 HYI2003F00001 220030207A741410357586 DISTRIBUTOR GEAR CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO MAGNETO FAILED E HYIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE01764EA2388 G060017ER 402C0237 816210R ON CLIMB OUT HYDRAULIC PRESSURE LITE REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR WAS EXTENDED FOR LANDING AND WHEN POWER WAS REDUCED THE RIGHT ENGINE LOST POWER. ENGINE WAS SHUTDOWN AND FEATHER, CREW LANDED WITHOUT INCIDENT. MECHANIC FOUND RIGHT ENGINE, BOTH MAGNETO DISTRIBUTOR GEARS HAD FAILED. MECHANIC CHANGED BOTH MAGNETO AND RETURNED AIRCRAFT TO SERVICE. SUGGEST TIME CHANGE OF DISTRIBUTOR GEAR AT MAGNETO HALF LIFE. 1L72 3O3 O A7CE E8CE 20030313001342003031300134 2003 3 13 AALA20030081 420030118A23301302249100 VIDEO UNIT BOEING777 777223 1385213NM CABIN BROKEN A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21762AN 31479 NRT - FLT 129 - EN ROUTE SJC-NRT, NOTED SEAT 2A VIDEO PLAYER SMOKING. MAIN POWER TO VIDEO SYSTEM TURNED OFF. FOUND PERSONAL VIDEO PLAYER HOUR METER CASE BROKEN AT SEAT 2A AND ALL IFE CABLES CHECK GOOD. REPLACED PERSONAL VIDEO PLAYER AT SEAT 2A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030313001382003031300138NM 2003 3 13 AALA20030092 120030122A3350 CONNECTOR BOEING737 737823 13844BZNM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21950AN 30087 MIA - DURING OVERNIGHT MAINTENANCE, L2 DOOR EMERGENCY EXIT LIGHT UNDER EXIT SIGN INOPERATIVE. RECONNECTED L2 DOOR EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030313001712003031300171WP 2003 3 13 AALA20030127 120030131A5310 WINDOW FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21450AA 49476 TUL - FOUND CRACK IN WINDOW FRAME AT STATION 1041 UPPER CORNER RIGHT SIDE. INSTALLED DOUBLER PER 53-10-00. (M) 2L72 4F A6WE 20030313001742003031300174WP 2003 3 13 AALA20030130 120030131A5310 WINDOW FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21450AA 49476 TUL - FOUND CRACK IN WINDOW FRAME AT STATION 1041 UPPER CORNER RIGHT SIDE. INSTALLED DOUBLER PER 53-10-00. (M) 2L72 4F A6WE 20030313001782003031300178EU 2003 3 13 AALA20030134 120030131A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2141063 506 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 27G INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 27G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030313001922003031300192WP 2003 3 13 AALA20030157 120030128A5320 SILL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21274AA 49271 TUL - FOUND BARE METAL AND CORROSION ON DOOR SILL BEAM. INSTALLED DOUBLER PER ESO 80559 DATED 1-27-03. (M) 2L72 4F A6WE 20030313001952003031300195NM 2003 3 13 AALA20030162 120030205A2560P2070003001 FLASHLIGHT BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21339AA 22336 SFO - DURING OVERNIGHT MAINTENANCE, FORWARD CENTER RIGHT FLIGHT ATTENDANT EMERGENCY EXIT FLASHLIGHT INOPERATIVE. REPLACED FORWARD CENTER RIGHT FLIGHT ATTENDANT EMERGENCY EXIT FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030313001962003031300196WP 2003 3 13 AALA20030163 120030205A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21466AA 49596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 7 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313002022003031300202WP 2003 3 13 AALA20030170 120030206A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217517A 49894 DFW - DURING OVERNIGHT MAINTENANCE, AFT REAR FLOOD EMERGENCY EXIT LIGHT INOPERATIVE. SEATED AFT REAR FLOOD EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313002062003031300206WP 2003 3 13 AALA20030174 120030207A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21571AA 49353 DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030313002082003031300208NM 2003 3 13 AALA20030176 120030207A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21383AN 26995 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030313002162003031300216NM 2003 3 13 QXEA0300190 120030121A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - SKIN PROTRUSION AFT OF PANEL 122AR CUTOUT AT STATION 140.000. REPAIRED IAW RD 8-53-2181. 2H72 4T RTA13NM 20030313002182003031300218NM 2003 3 13 QXEA0300192 120030124A5310 STOP FITTING DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - TWO DOOR STOPS CHAFED AT LOWER APERTURE OF CARGO DOOR SILL. REPAIRED IAW RD 8-53-104 PAGE 3. 2H72 4T RTA13NM 20030303000062003030300006SW 2003 3 3 HEEA084479 120030214A7120 BEARING BELL 412 412 1182202SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ENGINE MOUNT HAS A WORN BEARING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000082003030300008SW 2003 3 3 HEEA084481 120030214A5260212075418107 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ACTUATOR STEP WILL NOT ACTUATE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030303000132003030300013NM 2003 3 3 03060428 120030301A33509AR07373302 FRAME DORNERDO32 DO328300 NM LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27428FJ 3193 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW 9 SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL RESECURED EMERGENCY LIGHT STRIP. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030303000172003030300017NE 2003 3 3 HEEA084485 220030214A732132447368 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 1 ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 NR 1 ENGINE FLUTTERS IN MANUAL MODE WHEN THROTTLE ADVANCED. IN SHOP FOR REPAIR. 1G72 4U4 U H4SW E22EA 20030303000192003030300019SW 2003 3 3 HEEA084487 120030214A6320412010182101 BEARING BELL 412 412 1182202SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z2127 36019 MAIN ROTOR GEARBOX HAS A WORN BEARING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000212003030300021SW 2003 3 3 HEEA084488 120030214A6220412010216107 BEARING BELL 412 412 1182202SW PENDULUM ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R1334 36007 MAIN ROTOR PENDULUM ABSORBER HAS A WORN BEARING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000232003030300023SW 2003 3 3 HEEA084491 120030214A3212412050017133 COVER BELL 412 412 1182202SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 WORN. REPLACED WITH SERVICEABLE FLOAT COVER. 1G72 4U H4SW 20030303000282003030300028SW 2003 3 3 HEEA084494 120030214A2510412070810105 SEAT BELL 412 412 1182202SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 COCKPIT SEAT ADJUSTMENT MECHANISM WORN OUT. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000332003030300033SW 2003 3 3 HEEA084497 120030214A6220412310400101 ROD END BEARING BELL 412 412 1182202SW M/R HEAD WORN E O OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MAIN ROTOR ROD END HAS A WORN BEARING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000342003030300034SW 2003 3 3 HEEA084498 120030214A6220412310400101 ROD END BEARING BELL 412 412 1182202SW MAIN ROTOR HEAD WORN E O OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000382003030300038SW 2003 3 3 HEEA084500 120030214A25105017194051028 SEAT BELT BELL 412 412 1182202SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 SEAT BELT WORN. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030303000462003030300046 2003 3 3 HEEA084504 420030214A3442MI5852013 INDICATOR BELL 412 412 1182202SW WX RADAR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 THE WORD "WAIT" APPEARS ON THE WEATHER RADAR SCREEN MOST OF THE OPERATING TIME AND WILL GO OUT. IN SHOP REPAIR. 1G72 4U H4SW 20030303000472003030300047 2003 3 3 HEEA084505 420030214A3421PHI4121017601 INDICATOR BELL 412 412 1182202SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 33115 ATTITUDE INDICATOR FLAG WON'T PULL. IN SHOP REPAIR. 1G72 4U H4SW 20030303000552003030300055SW 2003 3 3 HEEA084510 120030214A30402314M2218 ARM BELL 412 412 1182202SW WINDSHIELD WIPERSTIFF E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 WINDSHIELD WIPER ARM STIFF, SPRING WILL NOT HOLD WIPER ON WINDOW. REPAIRED. 1G72 4U H4SW 20030303000572003030300057NM 2003 3 3 SWAA030389 120030218A32116546113 TRUNNION PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED A2 CHECK, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030313002212003031300221NM 2003 3 13 QXEA0300195 120030125A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING, NR 4 FLAP TRACK, INBOARD LOWER TRACK, LOWER SURFACE PITTED. REPAIRED IAW HORIZON AIR EA 2-57-220. 2H72 4T RTA13NM 20030313002252003031300225NM 2003 3 13 QXEA0300199 120030125A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING, NR 4 FLAP TRACK, OUTBOARD LOWER TRACK, LOWER SURFACE PITTED. REPAIRED IAW HORIZON AIR EA 2-57-220. 2H72 4T RTA13NM 20030313002312003031300231NM 2003 3 13 QXEA0300207 120030113A5730 SKIN BOMBDRDHC8 DHC8401 1390041NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 CKB- RIGHT WING CENTER LEADING EDGE INBOARD BOTTOM CORNER IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-107. 2H72 4T RTA13NM 20030313002322003031300232NM 2003 3 13 QXEA0300208 120030114A7110 CHANNEL BOMBDRDHC8 DHC8401 1390041NM RT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 CKB- CHANNEL IS CRACKED AT AFT END OF RIGHT HAND LOWER COWL. REPAIRED IAW DHC-8 Q400 RD 8/4-71-016. 2H72 4T RTA13NM 20030314000072003031400007 2003 3 14 H9Q2003F00000 420030217A2562E04468 ELT CESSNA150 150L 2071826CE CONT O200 O200* 17020SO CABIN MISOVERHAULED B H9QRK NONE W INADEQUATE Q C ININSP/MAINT 1 NM0911418356 15075405 DURNG THE COURSE OF AN ANNUAL INSPECTION, ACCESS WAS GAINED TO THE ELT FOR TESTING AND BATTERY DATE VERIFICATION. THE FOLLOWING DISCREPANCIES WERE IMMEDIATELY OBVIOUS. THE UNIT HAD BEEN CONNECTED TO THE EXISTING SYSTEMS ANTENNA. THE REMOTE PANEL INDICATOR SWITCH HAD NOT BEEN INSTALLED. 1H71 3O3 O 3A19 E252 20030314000132003031400013NE 2003 3 14 ANCF200300008 220030224A731482550112 PUMP BOEING767 767259 1385136NM PWA 4056 PW4056 NE FUEL SYSTEM FAILED W ANCFD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 SO23985AN 24618 724208CN EICAS MSG RT ENGINE FUEL FILTER DISPLAYED. WIRING CHECK IN CONNECTOR D10996, D4232P, D6238P AND SIGNAL IN BOTH EICAS COMPUTERS WAS PERFORMED IAW WDM 73-34-11 PAG 1 WITH NORMAL RESULTS. IT WAS REPLACED RT FUEL PUMP IAW AMM 73-11-01/401 WITH SATISFACTORY RESULTS. 2L72 4F4 FRTA1NM E24NE 20030314000162003031400016NE 2003 3 14 FE5F200300001 220030212A7314219093 SHAFT DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUEL PUMP WORN W FE5FE ENGINE SHUTDOWN F FLT CONT AFFECTED CRCRUISE 1 WP03 7848 11069 53166 P728163 DURING CRUISE, AT AUTOTHROTTLE MODE, THROTTLE CONTROL LEVER CONTINUED SHIFTING AND LT ENG EPR MAINTAINED 1.68. ALTERD TO MANUAL MODE AND FOUND LT ENG WAS NOT IN COMMAND BUT EPR 1.68 STILL. PILOT DECIDED AIR TURNBACK, AND SHUTDOWN THE ENG FOR LANDING APPROACH. INITIAL INSPECTION REVEALED FUEL PUMP CONTROL SHAFT WORN AT THE END WHICH COUPLED TO FCU. 2L72 4F4 F A6WE E9NE 20030314000172003031400017WP 2003 3 14 MEX2003024 120030204A2530 SOCKET DOUG DC9 DC982 3022082WP NR 2 OVEN BURNED W ASMFA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW23491SH 49150 AIRCRAFT ACCOMPLISHED AN UNSCHEDULED LANDING, SMOKE IN FORWARD GALLEY. DURING CRUISE WAS DETECTED SMOKE IN PASSENGERS CABIN FROM THE UPPER PART OF THE FORWARD GALLEY OVENS A SMOKE WAS INCREASED WHEN THE SYSTEM WAS SHUTOFF. OVEN NR 2 WAS CHECKED BY CONDITION AND WAS DETECTED THAT SOCKET HAD BURNED RESISTANCE, REMAINING OVEN INOPERATIVE IAW MM. THE CIRCUIT BREAKER WAS ASSURED IN OPEN POSITION AND OVEN WAS CANCELLED AND IDENTIFIED WITH AN INOPERATIVE TAG. OVEN WAS CHANGED. 2L72 4F A6WE 20030314000202003031400020 2003 3 14 MEX2003041 420030222A2210 ACCELEROMETER DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE INOPERATIVE W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW231075T 49724 AIRCRAFT RETURNED FROM FLIGHT, AFTER TAKEOFF FLIGHT GUIDANCE COMPUTER WENT OFF. ON BOTH COMPUTERS THERE WERE NO AUTO PILOT AND ATS, PITOT HEAT OFF LIGHT TURN ON AND YAW DAMPER FAILURE LIGHT TURN ON. RESPECT TO PITOT STALL HEATER OFF LIGHT ON, IT WAS DETERMINED THAT THE RELAY (R2-299) WAS OUT OF SERVICE AND IT WAS REPLACED IAW WDM 3 31-02. IN RELATION THE THE OTHER REPORTS, DUAL 3 AXIS ACCELEROMETER WAS REPLACED IAW MM, TESTS CORRECT. ADDITIONALLY THE FLIGHT DATA RECORDER WAS REPLACED IAW MM. IAW OVERWEIGHT LANDING AND IT WAS PERFORMED INSPECTION FOR OVERWEIGHT. ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030314000322003031400032NM 2003 3 14 03FDEA00149 120030221A5730ARB74131 SKIN DOUG MD11 MD11 3023602NM LT WING BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING FWD OF NR 5 SPOILER AREA WING REAR UPPER SPAR CAP FOUND SKIN BULGED. OUTER WING/REAR SPAR TRAILING EDGE LT REAR SPAR UPPER CAP REPAIR CARRIED-OUT AS PER FEDEX EA 1-5720-67571 PART 1. 2L73 4F RTA22WE 20030314000362003031400036NM 2003 3 14 2003740522 120030221A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE MISREPAIRED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT FLOORBEAM AT RBL 12 HAS IMPROPER REPAIR AT STA 950C. REMOVED FLOORBEAM RBL 12 BS 950C FOR REPAIR IAW SRM 51-30-2. FABRICATED NEW FLOORBEAM AND SPLICE DIM OF BEAM 2 INCHES X 57 INCHES AND SPLICE DIM 2 INCHES X 6.5 INCHES IAW SRM 53-10-5 FIG 4. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, INSTALLED REPAIR AND NEW FLOORBEAM IAW SRM 51-30-2 PO 9912219. 2L73 4F RTA3WE 20030314000372003031400037NM 2003 3 14 2003740523 120030221A5320 WEB BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT WEB IS CORRODED AROUND LOWER ROW OF NUTS STR 27R BETWEEN STA 1010 - STA 1030. REMOVED WEB FROM BS 1010 TO 1030 FOR REPAIR IAW SRM 51-30-2, FABRICATED NEM WEB IDIMENSIONS 19 INCHES X 4 INCHES USING 7075-T6 .063 PO 991861 IAW SRM 53-10-2 FIG 5. ALODINED AND PRIMED NEW PIECE IAW SRM 51-10-2 AND INSTALLED NEW WEB IAW 51-30-2. 2L73 4F RTA3WE 20030314000512003031400051WP 2003 3 14 ABXA030095 120030205A5311 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 FRAME AT STA 81, LONGERON 11 LEFT, CRACKED. REPAIRED FRAME IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20030314000632003031400063NM 2003 3 14 CALA0300026 120030129A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914320 23371 INSPECTION FOUND A CRACK IN PRESSURE DECK WEB AT STA 663, LBL 32. THE AREA WAS REPAIRED IAW SRM 53-60-51, FIGURE 203 AND ECRA 5310-04317. 2L72 4F RTA16WE 20030314000662003031400066WP 2003 3 14 CALA0300036 120030211A5230 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0972822 49482 INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD BAGGAGE BIN BACK PAN AT AFT SIDE WALL JUST AT LOWER LATCH BETWEEN THE TWO LOWER STOP PADS. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A. 2L72 4F A6WE 20030303002012003030300201NM 2003 3 3 CALA0300077 120030228A5210 BEAM BOEING737 7373T0 1384582NM L-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND ALL TORQUE BOX MOUNTING HOLES ELONGATED ON L-2 DOOR. REPAIRED IAW ECRA 5210-01658. 2L72 4F RTA16WE 20030303002082003030300208NM 2003 3 3 CALA0300086 120030302A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES OF UPPER CAP AT STA 1006 FROM BL 0 TO RBL 40. REMOVED AND REPLACED T-CAP IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030303002102003030300210NE 2003 3 3 ANCF200300009 220030228A7200 RROYCE BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE W ANCFK NONE X ENGINE FLAMEOUT CRCRUISE 1 SO23321LF 30853 26269 30853 during flight from Bogotá to Aruba at cruise engine experienced low oil press, high oil temperature and flamed the engine out and N3 indication went to zero. Engine with windmilling for 25 minutes aprox. and landed in Aruba.PARTIAL ACTIONS:Initial inspection was performed with Debris found in chip detectors, and as a cause of the problem we suspect an internal damage on radial drive shaft. Now we are replacing the RH engine. 2L72 4F4 FRTA2NM E12EU 20030303002112003030300211SO 2003 3 3 C2XA03IA024 120030226A33507287103507 CONTROL MODULE EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714902 145496 IAH- DURING POST FLIGHT THE CREW NOTED THAT THE "EMERGENCY LIGHT NOT ARMED" CAUTION, AND, EXIT LIGHTS CAME ON EVERY TWO (2) MINUTES FOLLOWING RESET FROM OFF TO ARMED. IAH- MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030304000092003030400009SW 2003 3 4 AC2A084865 120030224A6420222012714001 BEARING RACE BELL 430 430 1182150SW TAIL ROTOR WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT 49089 GROOVES WORN INTO BUSHING. REPLACED WITH NEW BUSHING. 1G72 3U RTH9SW 20030304000142003030400014SW 2003 3 4 AC2A084870 120030224A64201200124A SLEEVE BELL 430 430 1182150SW TAIL ROTOR WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT 49089 SLEEVE IS WORN THRU LINER. REPLACED WITH NEW PART. 1G72 3U RTH9SW 20030304000252003030400025 2003 3 4 BAQA084833 420030227A3120621396231 COMPASS AEROSPAS365 AS365N2 8680815EU COCKPIT CRAZED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME6600 6417 STAND BY COMPASS CRAZING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030304000262003030400026EU 2003 3 4 BAQA084834 120030227A3110 STRUCTURE AEROSPAS365 AS365N2 8680815EU INSTRUMENT PANELBROKEN H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME6600 6417 INSTRUMENT PANEL HARDWARE BROKEN. NR 2 DIM OUT INOP. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030304000282003030400028CE 2003 3 4 NSVA200300016 120030303A520010151411513 DOOR LATCH BEECH BEECH 1900 1900C 1154161CE SEIZED A NSVAK NONE O OTHER TXTAXI/GRND HDL 1 EA27207CJ 561 UC107 LEB-Crew reported door handle stiff with door open or closed and button stuck on handle for airstair door. MX R&R Airstair door latch and lock assembly IAW Beech AMM 52-10-00. Op's check good. 2L72 4T RTA24CE 20030304000402003030400040SW 2003 3 4 HEEA084574 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T8580 33112 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES DUE TO EROSION. 1G72 4U H4SW 20030304000412003030400041SW 2003 3 4 HEEA084575 120030214A6230 BEARING BELL 412 412 1182202SW SWASHPLATE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D11310 RE309 33076 SWASHPLATE GIMBAL BEARINGS WORN. REPAIRED. 1G72 4U H4SW 20030304000422003030400042SW 2003 3 4 HEEA084576 120030214A6230 BUSHING BELL 412 412 1182202SW SWASHPLATE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z RE310 36019 SWASHPLATE LINK BUSHINGS WORN OUT. REPAIRED. 1G72 4U H4SW 20030304000492003030400049EA 2003 3 4 COMA0390003 120030227A5610NP13932110 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA R/H BROKEN A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01354CA781 10064 FLIGHT 5899 CO-PILOTS WINDSHIELD BROKEN DURING TAXI.REPLACED THE CO-PILOTS WINDSHIELD. 2L72 4F RTA21EA 20030304000502003030400050SW 2003 3 4 HEEA084581 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 3274 A2354 33134 MAIN ROTOR MAST LINK HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030304000522003030400052SW 2003 3 4 HEEA084583 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK UNSTAKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S A2612 36002 MAIN ROTOR MAST LINK HAS A BEARING UNSTAKED. SCRAPPED. 1G72 4U H4SW 20030304000532003030400053SW 2003 3 4 HEEA084584 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z1733 A2621 36019 MAIN ROTOR MAST LINK HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030304000552003030400055SW 2003 3 4 HEEA084586 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK UNSTAKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N380 A3015 33002 MAIN ROTOR MAST LINK HAS A BEARING UNSTAKED. REPAIRED. 1G72 4U H4SW 20030304000572003030400057SW 2003 3 4 HEEA084588 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000632003030400063SW 2003 3 4 HEEA084594 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z2816 36019 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000642003030400064SW 2003 3 4 HEEA084595 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R2898 36007 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000702003030400070NM 2003 3 4 DLM88030071 120030117A5342591214186 ANGLE DOUG MD88 MD88 3023688NM FS 1474 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27909DE 53418 FUSELAGE / VERTICAL STAB TO FUSELAGE ATTACH ANGLE : CRACK REPAIR THE LH VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN THE HORIZONTAL FLANGE AT CANT STA 1474. THE CRACK WAS ROUTED OUT OF THE FLANGE AND REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384458-14, REV A. 2L72 4F RTA6WE 20030304000722003030400072NM 2003 3 4 DLM88030076 120030122A2130UNKNOWN VALVE DOUG MD88 MD88 3023688NM AFT FAILED A DALAI CABIN DEPRESSURIZATION S AFFECT SYSTEMS CRCRUISE 1 SO27926DL 49713 AT 350FL THE CABIN PRESS AND CABIN ALT WAS CLBING AT 2K FT/MIN. BOTH PACKS WERE IN AUTO AND WERE NOT RESPONDING. DESCENDING TO 280FL STILL NG. WENT TO MANUAL NO HELP. BOTH PACK PRESS READ ZERO. DESCENDED TO 100FL AND THE CABIN WAS 180FL AND THE O2 MASK DEPLOYED. REPLACED FLOW CONTROL VALVES 2L72 4F RTA6WE 20030304000732003030400073NM 2003 3 4 DL733030082 120030121A53306545800602 SKIN BOEING737 737347 1384647NM FS 280, S-21R DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO273301 23181 FUSELAGE / SKIN / FS 277-290.5 / STRG. 20R-22R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED BY GROUND EQUIPMENT JUST AFT OF THE LAVATORY SERVICE DOOR BETWEEN FS 277 & 290.5 AND BETWEEN STRINGERS 20R & 22R. THE DAMAGE WAS REMOVED WITH A 14.5" X 7" CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384463-14, REV B. 2L72 4F RTA16WE 20030304000762003030400076NM 2003 3 4 DL757030093 120030124A5330146N37805 SKIN BOEING757 757232 1384965NM FS 1717, S-26L LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 FUSELAGE / SKIN / FS 1717 / STRG. 26L : LIGHTNING STRIKE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH A LIGHTNING BURN AT FS 1717 ON THE STRINGER 26L SKIN LAP JOINT. THE DAMAGE WAS REMOVED BY TRIMMING OUT TWO FASTENER LOCATIONS ON THE UPPER SKIN OF THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384395-14, REV A. 2L72 4F RTA2NM 20030304000792003030400079NM 2003 3 4 DL777030099 120030127A2420764939B IDG S281W10120 BOEING777 777232 1385232NM #2 ENGINE INOPERATIVE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27865DA A0676 29737 000 RT IDG TRIPPED OFF SHORTLY AFTER TAKEOFF. ELECT SMELL IN CABIN. TRIED ONE RESET NO HELP. 0634/28JAN/ATL/ 456509 - PASSING 10000 FEET AFTER TAKE OFF ELEC GEN RT LIGHT ILLUM. TRIED 1 RESET PROCEDURE AND REMANED OFF. LANDED WITH 482000 LBS. 02 FWD RT ENG DRIVE GEN. TO MCO AND PLAC PER MEL 24-11-01. RT GENERATOR DISCONNECTED REPLACED RT IDG. OPS CHECK NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2L72 4F RTT00001SE 20030304000802003030400080NM 2003 3 4 DL76L030108 120030129A7110314T401010A ENGINE BOEING767 767332 1382001NM #1 ENGINE DAMAGED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27173DN30650 24800 XXX NBR 1 ENGINE STRUCK BY DEICING BUCKET CREATING 1 FT HOLE IN NOSE COWL. REPLACED NBR 1 ENG INLET COWL PER M/M 71-11-01-4 ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2L72 4F RTA1NM 20030304000832003030400083NM 2003 3 4 DL767030130 120030206A210021T31158 DUCT BOEING767 767232 1385132NM RT A/C BAY RUPTURED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27104DA 22216 LEFT AND RIGHT DUCT LEAK INDICATION IN COCKPIT FOUND FWD CARGO HEAT DUCT AND CROSSOVER MANIFOLD RUPTURED PER IPC 36-11-01-10 2L72 4F RTA1NM 20030304000862003030400086NM 2003 3 4 DLM88030135 120030208A2130 WIRE DOUG MD88 MD88 3023688NM E AND E COMPRT CHAFED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27916DE 53421 CLIMBING THROUGH 14000 FT LOST PRESSURIZATION. FOLLOWING CHECK LIST FOUND BREAKERS U-22 AND W0-22 POPPED. DECENDED TO 10000 FT AND RETURNED TO DFW. FOUND WIRE CHAFING AT PLUG R5-390 REPAIRED SAME 2L72 4F RTA6WE 20030304000922003030400092NM 2003 3 4 DLM88030169 120030221A24207939409501 HARNESS DOUG MD88 MD88 3023688NM APU SHROUD MELTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27927DA 49714 A/C ARRIVED WITH APU GENERATOR INOP ON MCO. DURING TROUB LESHOOTING, WE FOUND TH APU GEN FIREWALL PLUG HAD A L OOSE CONTACT PIN . HARNESS WAS REMOVED AND PLUG WAS OPENED TO DISCOVER A MELTED CONNECTOR AND SHIELDING . HARNESS ASSEMBLY IS TO BE REPLACED ON AEROMEXICO NON ROUTINE CARD. PART # OF HARNESS IS7939409-501 2L72 4F RTA6WE 20030116002582003011600258NM 2003 1 16 ABXA030017 120030106A5320454T2504041 PANEL BOEING767 767281 1385109NM FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE, CORRODED SHEAR PANEL, BETWEEN STA 544-610, LBL 20 - 30 AND CRACKED. CORRODED AND CRACKED SHEAR PANEL. REMOVED AND REPLACED SHEAR PANEL IAW SRM. 2L72 4F RTA1NM 20030116002602003011600260NM 2003 1 16 ABXA030019 120030106A5311143T106013 FRAME BOEING767 767281 1385109NM FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE EXISTING REPAIRS ON UPPER CHORD OF BEAM AT STA 588, BL 45, FOUND DAMAGE. DAMAGED CHORD REMOVED AND NEW FRAME INSTALLED IAW SRM. 2L72 4F RTA1NM 20030116002612003011600261NM 2003 1 16 ABXA030020 120030106A5310140T2102321 SHEAR TIE BOEING767 767281 1385109NM FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE CORRODED SHEAR TIES AT STA 434, BETWEEN LONG 36-37 LEFT AND RIGHT. CORRODED SHEAR TIE REPLACED WITH NEW SHEAR TIE IAW SRM. 2L72 4F RTA1NM 20030116002632003011600263NM 2003 1 16 ABXA030022 120030106A5320451T2504021 PANEL BOEING767 767281 1385109NM FUSELAGE SCRATCHED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE, DEEP SCRATCHES ON SHEAR PANEL BETWEEN STA 610 - 632, LBL 45. DAMAGED SHEAR PANEL REMOVED AND NEW SHEAR PANEL INSTALLED IAW SRM. 2L72 4F RTA1NM 20030116002642003011600264NM 2003 1 16 ABXA030023 120030106A5310140T21020253 SHEAR TIE BOEING767 767281 1385109NM FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE, STA. 742, CORRODED SHEAR TIE, BETWEEN STR 38 - 39 LEFT. CORRODED SHEAR TIE REMOVED, NEW SHEAR TIE INSTALLED IAW SRM. 2L72 4F RTA1NM 20030116002692003011600269WP 2003 1 16 ABXA030032 120030111A3397 GROUND WIRE DOUG DC9 DC933F 302207AWP CABIN LOOSE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 RIGHT OVERHEAD EMERGENCY LIGHT DIM. TIGHTENED GROUND WIRE ON RIGHT OVERHEAD EMERGENCY LIGHT FIXTURE. OPS CHECKED GOOD IAW AMM. 2L72 4F A6WE 20030116002802003011600280SW 2003 1 16 HEEA083140 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR FLAP WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 MAIN ROTOR FLAP RESTRAINT WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030117000012003011700001SW 2003 1 17 HEEA083146 120030108A6220206011139001 ARM BELL 206 206L3 1182108SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR ARM ASSY RUBBER EXPANDED. 1G71 3U H2SW 20030117000042003011700004SW 2003 1 17 HEEA083149 120030108A6420 BOOT BELL 206 206B3 1181506SW T/R HEAD DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 TAIL ROTOR PITCH CONTROL MECHANISM BOOT DETERIORATED. SCRAPPED. 1G71 3U H2SW 20030117000052003011700005SW 2003 1 17 HEEA083150 120030108A6210206015001115 BLADE BELL 206 206L3 1182108SW MAIN ROTOR DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03411282058 51134 MAIN ROTOR BLADE SKIN AT THE TIP ON THE UPPER SIDE IS UNBONDED AND CORRODED. 1G71 3U H2SW 20030117000152003011700015NM 2003 1 17 CALA0300013 120030116A5320 SHEAR TIE BOEING737 7373T0 1384582NM STA 500D CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917321 23372 INSPECTION FOUND SHEAR TIE CORRODED AT STA 500D O/B OF STRINGER 27L. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 203. 2L72 4F RTA16WE 20030117000202003011700020SW 2003 1 17 HEEA083160 120030108A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 TRANSMISSION RESTRAINT WORN. REPAIRED. 1G71 3U H2SW 20030117000312003011700031SW 2003 1 17 HEEA083166 120030108A6330206033506103 RESTRAINT BELL 206 206L4 1182110SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 TRANSMISSION RESTRAINT WORN. REPAIRED. 1G71 3U NCH2SW 20030117000562003011700056SW 2003 1 17 HEEA083175 120030108A6310206040270101 SUPPORT BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 MAIN ROTOR AFT SUPPORT LEAKING. REPAIRED. 1G71 3U H2SW 20030117000592003011700059SW 2003 1 17 HEEA083178 120030108A6510206040328101 SPLINE ADAPTER BELL 206 206B3 1181506SW T/R BLOWER SHAFTWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 BOTH SPLINE ADAPTERS ON TAIL ROTOR BLOWER SHAFT WORN SPLINES. REPAIRED. 1G71 3U H2SW 20030117000742003011700074SW 2003 1 17 HEEA083182 120030108A6520 DOWEL PIN BELL 206 206L3 1182108SW GEARBOX CASE OVERSIZED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 A1309185 OVERSIZE DOWEL PIN INSTALLED IN TAIL ROTOR GEARBOX CASE AND THE EXPOSED PORTION WAS NOT MACHINED DOWN. 1G71 3U H2SW 20030117000782003011700078SW 2003 1 17 HEEA083186 120030108A3212206050248113 FLOAT BELL 206 206L3 1182108SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 EMERGENCY FLOAT BAG LEAKING. 1G71 3U H2SW 20030117000872003011700087NM 2003 1 17 2003UALA00010 120030104A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 807 FRAME CRACK AT RIVET HOLE STR S9-R. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030117000892003011700089NM 2003 1 17 2003UALA00012 120030105A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 827 FRAME CRACKED AT RIVET HOLE AT S9R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030117000922003011700092NM 2003 1 17 2003UALA00016 120030104A5320 PLATE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 STATION 1680 TO 1684, RBL44 TO RBL54.5, AFT DECK PLATE CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20030117000962003011700096NM 2003 1 17 2003UALA00022 120030107A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 867 FRAME CRACKED AT RIVET HOLE NEAR STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030117000972003011700097SW 2003 1 17 HEEA083187 120030108A3212206050248113 FLOAT BELL 206 206L3 1182108SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 EMERGENCY FLOAT BAG LEAKING. 1G71 3U H2SW 20030117000982003011700098SW 2003 1 17 HEEA083188 120030108A3212206050248113 FLOAT BELL 206 206L3 1182108SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 EMERGENCY FLOAT BAG ASSY LEAKING. 1G71 3U H2SW 20030117001032003011700103SW 2003 1 17 HEEA083193 120030108A3213206050288103 CROSSTUBE BELL 206 206B3 1181506SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322751 3627 FOUND AFT CROSSTUBE CORRODED BEYOND LIMITS NEAR AND UNDER SADDLES. SCRAPPED. 1G71 3U H2SW 20030117001052003011700105NM 2003 1 17 UPS03440016 120030106A5210 BEAM BOEING747 747259B 1384804NM 1R DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C NO.1R DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED AND INSTALLED AS PER SRM 52-10-02 FIG.10. 2L74 4F RTA20WE 20030130001502003013000150NM 2003 1 30 F3LA200300001 120030111A335020121 CHARGER BOEING737 7373Q8 1384670NM CABIN SHORTED A F3LAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03319FL 26301 FLIGHT CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT AFTER LANDING IN DEN. FOUND EMERGENCY TRACK LIGHT CHARGER IN FWD GALLEY POSITION M1132 SHORTED AND SMOKING. REPLACED CHARGER AND BATTERY PACK AND CHECKED OKAY. 2L72 4F RTA16WE 20030117001182003011700118SW 2003 1 17 HEEA083198 120030108A7332206061535007 TRANSDUCER BELL 206 206L3 1182108SW ALLSN 250C 250C20B 03013GL FUEL PRESSURE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 TRANSDUCER SHOWING NO FUEL PRESSURE INDICATIION. SCRAPPED. 1G71 3U3 U H2SW E4CE 20030117001192003011700119SW 2003 1 17 HEEA083199 120030108A2821206061634003 VALVE BELL 206 206L3 1182108SW FUEL FILTER LEAKING E O OTHER K FLUID LOSS NRNOT REPORTED 1 SW0321497 51518 FUEL FILTER VALVE LEAKING. SCRAPPED. 1G71 3U H2SW 20030117001212003011700121SW 2003 1 17 HEEA083200 120030108A2821206061634003 VALVE BELL 206 206L3 1182108SW FUEL FILTER LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033116P 51530 FUEL FILTER VALVE LEAKING. SCRAPPED. 1G71 3U H2SW 20030117001302003011700130SW 2003 1 17 HEEA083205 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW MAIN ROTOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F MAIN ROTOR ACTUATOR WILL NOT MAINTAIN FULL ACTUATION IN THE TOP OR BOTTOM STROKE RANGES. 1G71 3U H2SW 20030117001392003011700139SW 2003 1 17 HEEA083209 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 ACTUATOR DOES NOT MOVE. 1G71 3U H2SW 20030117001422003011700142SW 2003 1 17 HEEA083211 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 ACTUATOR INOPERATIVE. 1G71 3U H2SW 20030117001612003011700161SW 2003 1 17 HEEA083215 120030108A2820206063653003 TUBE BELL 206 206L3 1182108SW FUEL SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038589X 51487 TUBE ASSY HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030117001662003011700166EA 2003 1 17 COMA0360031 120030114A2750852D100MD91 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA L/H UNRELIABLE A COMAO OTHER S AFFECT SYSTEMS APAPPROACH 1 SO01918CA16759 7018 FLIGHT 5575 FLAPS FAIL MESSAGE DURING APPROACH.REPLACED THE L/H #1 FLAP ACTUATOR. 2L72 4F RTA21EA 20030117001692003011700169NM 2003 1 17 AWXA200300048 120030103A5320BAC1509100146 FLOOR SUPPORT BOEING737 7373G7 138447JNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 LCQ - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND UNDER NUTPLATE ON AFT CARGO COMPARTMENT FLOOR SUPPORT "L" ANGLE BS 772, RBL 2. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; CUTOUT DAMAGED PORTION OF FLOOR SUPPORT; FABRICATED REPAIR ANGLES PER B737-300 SRM 53-00-53, PG. 201-203; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG. 201-203, FIG. 201 2L72 4F RTA16WE 20030119000022003011900002EU 2003 1 19 RAIA00301011 120030108A3010350A52005009 COMPUTER AEROSPATR72 ATR72202 8680940EU MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03722TE9449 90 220 5602-STL\- CREW REPORTED ANTI-ICE FAULT INDICATION.MAINTENANCDE REMOVED AND REPLACED MULTI FUNCTION COMPUTER, OPS CK OK. 2H72 4T RTA53EU 20030130001572003013000157NM 2003 1 30 F3LA200300006 120030115A5320 STRINGER CLIP BOEING737 7373M8 1384615NM FUSELAGE BROKEN A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED STRINGER CLIP BROKEN AT STA 1006, STR 12L. FABRICATED AND INSTALLED REPLACEMENT STRINGER CLIP PER SRM 51-40-02 AND BOEING DRAWING 6935364. 2L72 4F RTA16WE 20030120000062003012000006EA 2003 1 20 03019653 120030119A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27653FJ 7438 The crew reported that the emergency floor track lighting was inoperative from seat row 5 forward. The aircraft was ferried to ORD for maintenance. Maintenance personnel removed and replaced the forward emergency floor track lighting strip. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030120000112003012000011WP 2003 1 20 MWEA030037 120030120A531199118433 FRAME DOUG DC9 DC932 3022066WP STA 1168 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 CANTED FRAME AT STATION 1168 AT THE 2 O'CLOCK POSITION IS CRACKED. -- LOCATED,DRILLED AND INSTALLED NEW FRAME. 2L72 4F A6WE 20030120000122003012000012WP 2003 1 20 MWEA030038 120030120A5711JO6017321 SPAR DOUG DC9 DC932 3022066WP STA 157 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 LEFT WING STATION XRS 157 AFT SPAR REPAIR. -- FABRICATED AND INSTALLED REPAIR PARTS, FABRICATED AND INSTALLED NEW TEE. 2L72 4F A6WE 20030120000152003012000015EA 2003 1 20 COMA0360033 120030116A2120 ACM CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01818CA 7408 FLIGHT 5587 SMOKE AND BURNING SMELL IN COCKPIT.FOUND TO BE IMPROPERLY APPLIED CLYCOL. RUN APU AND ENGINES TO CLEAR CLYCOL FROM A/C SYSTEM. 2L72 4F RTA21EA 20030120000182003012000018NM 2003 1 20 P5CA0300719 120030119A2720NONE RUDDER BOEING747 74746NF 13848BTNM VERT. STAB MALFUNCTIONED A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23450PA 30808 RUDDER TRAVEL NOT GOING TO LIMITS ON R/H INDICATOR DURING CONTROL CHECK. INSPECTED FWD & AFT RUDDER QUADRANT ASSYS, CABLE SYS., TRIM, CENTERING & FEEL MECHANISM PER MM 27-21-06, 27-21-08 & 27-21-11. ALL OK. PULLED A/C INTO HANGAR. AFTER 30 MIN. SYSTEM OPS CHECKED NORMAL PER MM 27-21-00. SUSPECT POSSIBILITY OF ICE IN AFT QUADRANT AREA DUE TO MOISTURE. 2L74 4F RTA20WE 20030327000882003032700088SO 2003 3 27 C2XA03BT008 120030119A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714573 145638 CREW REPORTED, LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED RIGHTHAND LANDING GEAR PROXIMITY SWITCH IAW EMB145 AMM 32-63-01. OPS CHECKED GOOD. PERFORMED RETRACTION AND EXTENSION OF LANDING GEAR SYSTEM IAW 32-32-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030120000192003012000019SO 2003 1 20 C2XA03BT009 120030118A5610163500112 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT CRACKED A C2XAA UNSCHED LANDING ZO SIGNIFICANT FAILURE REPORTOTHER UKUNKNOWN 1 SW2716981 145 EWR---CO2442, CREW REPORTED, "FIRST OFFICER'S WINDSHIELD (OUTER PANE) SHATTERED IN FLIGHT." MAINTENANCE REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD I/A/W EMB145 AMM #56-10-01. HEAT ELEMENT OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030121000042003012100004NM 2003 1 21 SWAA030081 120030114A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS, BS 520, STRINGER 12R AND BS 515, STRINGER 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030121000102003012100010NM 2003 1 21 SWAA030071 120030112A57536546430121 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND LT WING INBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM. 2L72 4F RTA16WE 20030304001062003030400106NM 2003 3 4 AWXA200300221 120030217A575465C26601180 SLAT BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW0 0 24060 YVR - MAJOR REPAIR - DURING C-11 CHECK 3 EACH 1" CRACKS WERE FOUND ALONG RIVETS ON LOWER EDGE OF THE NO. 6 LEADING EDGE SLAT AT THE INBOARD AUXILIARY TRACK. MAINTENANCE REMOVED EXISTING EXTERNAL DOUBLER; CUTOUT FOUR DAMAGED FASTENER HOLES; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, PG. 216, FIG. 206. 2L72 4F RTA16WE 20030305000112003030500011NM 2003 3 5 2003UALA00202 120030223A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29641UA 25091 EXTERNAL FUSELAGE SKIN GOUGED AT STA 595, STRINGER 1L. BLENDED GOUGE. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F4 FRTA1NM E24NE 20030305000232003030500023NE 2003 3 5 C1HA200394001 220030105A7200 ENGINE BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 3 STALLED A C1HAO OTHER R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 GL15294AS 22146 UPON LANDING NR 3 ENGINE COMPRESSOR STALLED AT 2.0 EPR ANR 90 KTS. RETARDED REVERSER AND ENGINE OPERATED NORMAL. PERFORMED VISUAL INSPECTION OF 1ST STAGE COMPRESSOR & AFT TURBINE IAW P&W JT8 MM REF 72-00-00 PG 122. PERFORMED GROUND ENGINE START/RUN, ALL INDICATIONS NORMAL. 2L73 4F4 F A3WE E2EA 20030305000252003030500025NE 2003 3 5 C1HA200394003 220030109A7200 ENGINE BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 3 STALLED A C1HAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL15294AS 22146 UPON LANDING NR 3 ENGINE COMPRESSOR STALLED AT 85 KTS 1.8 TO 1.85 EPR. RAN ENGINE PER CHECKLIST AT 70 PERCENT N1 15 SECONDS ALL INDICATIONS APPEAR NORMAL. LUBED NR 3 ENG PRESSURE BELLOWS. INSP INLET AND EXHAUST, NO DEFECTS (REF73-00-00). RAN ENGINE AT PWR IN REF TO MM 71-00-00. ALL ENGINE PARAMETERS NORMAL. 2L73 4F4 F A3WE E2EA 20030305000262003030500026NM 2003 3 5 C1HA200395001 120030105A2612 FIRE LOOP BOEING727 727290 138408WNM NR 1 OUT OF POSITION A C1HAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15295AS 22147 NR 1 GROUND LOOP FIRE DETECTION DIMLY FLICKERING ON AND OFF. REPOSITIONED FIRE LOOP, GROUND TESTS NORMAL PER MM 26-11-00. 2L73 4F A3WE 20030305000312003030500031NM 2003 3 5 C1HA200397002 120030115A2612 FIRE LOOP BOEING727 727270 138408PNM NR 1 ENGINE OUT OF POSITION A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15697CA 23052 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT ON FIRE PROTECTION SYSTEM NR 1 ENGINE. FOUND LOOP CONTACTING DRAIN TUBE AND A BRACKET. REPOSITIONED BRACKET AND DRAIN TUBE. NO DEFECTS NOTED, OK FOR SERVICE. 2L73 4F RTA3WE 20030305000352003030500035SW 2003 3 5 HEEA084617 120030214A3210400052007109 BEAM BELL 407 407 1182206SW MLG CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 BEAM ASSY CHAFED FROM LANDING GEAR SHIFTING OVER. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 3U O H2SW 20030305000362003030500036SW 2003 3 5 HEEA084618 120030214A3210400052007109 BEAM BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 BEAM ASSY BOLT HOLES CORRODED AND DAMAGED BEYOND LIMITS. 1G71 3U O H2SW 20030305000462003030500046 2003 3 5 HEEA084628 420030214A3455066104701 TRANSCEIVER BELL 412 412 1182202SW ADF WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 ADF TRANSCEIVER WEAK AND UNRELIABLE. REPAIRED. 1G72 4U H4SW 20030305000492003030500049 2003 3 5 HEEA084631 420030214A3451066106900 INDICATOR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 DISPLAY UNREADABLE. REPLACED DISPLAY CONNECTOR. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000562003030500056NM 2003 3 5 QXEA0300312 120030301A2710A44700009 ACTUATOR DHAV DHC8 DHC8202 2809007NM ZONE 500 FAILED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09357PH12220 504 PDX - FLIGHT 2083 - ON CLIMBOUT, MORE PRESSURE THAN NORMAL WAS REQUIRED TO ROLL THE AIRCRAFT TO THE LEFT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT INBOARD ROLL SPOILER ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030305000592003030500059 2003 3 5 HEEA084641 420030214A3452066107100 TRANSPONDER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 TRANSPONDER WILL NOT COME ON. LOWER CHASSIS CORRODED. CLEANED CORROSION FROM UNIT. REPLACED Q104, Q501, Q502 TRANSISTORS, REPLACED 3 EACH WASHERS AND 3 EACH INSULATORS. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000642003030500064 2003 3 5 HEEA084646 420030214A3452071119208 TRANSPONDER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 TRANSPONDER INOPERATIVE. FOUND HEADER P305, TRANSISTOR Q206, DISPLAY DS103 AND PHOTOCELL V101 BAD. ALSO FOUND CARBON UNDER P305 BETWEEN PINS 12 AND 13. REPLACED HEADER, TRANSISTOR, DISPLAY AND PHOTOCELL AND REMOVED CARBON. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000652003030500065 2003 3 5 HEEA084648 420030212A2350066105571 AUDIO PANEL BOLKMS105 BO105S 5626006EU COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037136H S833 AUDIO PANEL CAUSING STATIC IN PILOTS HEADSET AND VOLUME VARIES. FOUND VOLUME CONTROL R235, LAMPS DS1, DS2, DS5, DS8, PULL KNOB WITH SET SCREWS AND 9 EACH PUSH BUTTONS BAD. REPLACED. BENCH CHECK GOOD. 1G72 3U H3EU 20030305000672003030500067EU 2003 3 5 HEEA084650 120030212A6220 RETAINER BOLKMS105 BO105S 5626006EU MAIN ROTOR HEAD CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW039190Y7080 2180 S669 INTERGRANULAR CORROSION ON GRIP SEAL RETAINER. REPAIRED. 1G72 3U H3EU 20030121000122003012100012NM 2003 1 21 SWAA030073 120030113A3350311500 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS MISSING AT ROW 5 DEF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030121000152003012100015EU 2003 1 21 BAQA082890 120030108A6220 BUSHING AEROSPSA365 SA365N 8680669EU STARFLEX ASSY DEBONDED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01365KY717 M2315 6529 STARFLEX BLUE STAR ARM BUSHING DEBONDED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030121000222003012100022NM 2003 1 21 SWAA030065 120030112A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 296, STR 10L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030121000242003012100024NE 2003 1 21 SWAA030068 220030112A7200JT8D9A ENGINE BOEING737 7372H4 138448CNM JT8 JT8D9A 52048NE LT WING STALLED A SWAAK NONE P NO WARNING INDICATION NRNOT REPORTED 1 SW29102SW 23108 707433 NR 1 ENGINE SUFFERED COMPRESSOR STALL. REMOVED AND REPLACED NR 1 ENGINE, OPS CK GOOD PER MM. 2L72 4F4 F A16WE E2EA 20030121000302003012100030SW 2003 1 21 HEEA083222 120030108A7160206064213103 SCREEN BELL 206 206L3 1182108SW ENGINE INTAKE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 ENGINE INTAKE SCREEN ASSY HAS CORROSION. REPAIRED. 1G71 3U H2SW 20030121000332003012100033SW 2003 1 21 HEEA083225 120030108A5320206064213191 FLOOR SUPPORT BELL 206 206L3 1182108SW FUSELAGE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 FUSELAGE FLOOR SUPPORT HAS CORROSION. REPAIRED. 1G71 3U H2SW 20030121000362003012100036SW 2003 1 21 HEEA083228 120030108A7810206064300005 EXHAUST PIPE BELL 206 206L3 1182108SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 EXHAUST ASSY CRACKED. REPAIRED. 1G71 3U H2SW 20030121000442003012100044SW 2003 1 21 HEEA083237 120030108A2120206070936001 CONTROL ARM BELL 206 206L3 1182108SW AIR DISTRIBUTIONBROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 ACTUATING COPILOTS FRESH AIR VENT KNOB DOES NOT CHANGE AIR FLOW DURING FLIGHT. FLAPPER CONTROL ARM BROKEN. SCRAPPED. 1G71 3U H2SW 20030121000542003012100054SW 2003 1 21 HEEA083256 120030108A7720206075007103 INDICATOR BELL 206 206L3 1182108SW TOT READS HIGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 FOUND INDICATOR READING 20 DEGREES HIGH. REPAIRED. 1G71 3U H2SW 20030121000562003012100056SW 2003 1 21 HEEA083258 120030108A2436206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW DC SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038594X 51531 WHEN RADIO IS KEYED GENERATOR GOES OFF LINE. CHANGED DC VOLTAGE REGULATOR. 1G71 3U H2SW 20030121000572003012100057SW 2003 1 21 HEEA083259 120030108A2436206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW DC SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 GENERATOR KEEPS DROPPING OFF LINE. CHANGED DC VOLTAGE REGULATOR. 1G71 3U H2SW 20030121000582003012100058SW 2003 1 21 HEEA083260 120030108A2436206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW DC SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 GENERATOR KICKS OFF LINE WHEN VHF IS KEYED. CHANGED DC VOLTAGE REGULATOR. 1G71 3U H2SW 20030121000592003012100059SW 2003 1 21 HEEA083261 120030108A7714206075545001 SENSOR BELL 206 206L3 1182108SW ENGINE RPM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 ENGINE OUT CAUTION LIGHT GOES OUT AT 20 PERCENT N1 INSTEAD OF 55 PERCENT AS REQUIRED DURING STARTS. SCRAPPED. 1G71 3U H2SW 20030121000602003012100060SW 2003 1 21 HEEA083262 120030108A7714206075545001 SENSOR BELL 206 206L3 1182108SW ENGINE RPM INTERMITTENT E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW036251X 51552 ENGINE RPM SENSOR HAS AN INTERMITTENT HORN. REPAIRED. 1G71 3U H2SW 20030121000632003012100063SW 2003 1 21 HEEA083265 120030108A7712206075739103 TORQUEMETER BELL 206 206L3 1182108SW COCKPIT UNRELIABLE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 TORQUE METER PRODUCING UNRELIABLE READINGS. REPAIRED. 1G71 3U H2SW 20030305000692003030500069EU 2003 3 5 HEEA084652 120030212A6720 BEARING BOLKMS105 BO105S 5626006EU BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037170D S840 TAIL ROTOR BELLCRANK HAS WORN BEARINGS. REPLACED BEARING 2828P AND EN2015BN06E DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030305000742003030500074 2003 3 5 HEEA084657 420030212A2340A3016W INTERPHONE BOLKMS105 BO105S 5626006EU COMMS NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 INTERPHONE BOX HAS FEEDBACK NOISE ON CHANNEL 2. FOUND SWITCHES S2 THROUGH S11, VOLUME CONTROL R72, VOLUME AND SELECTOR KNOBS BAD. ALSO FOUND CORROSION ON VOLUME AND SELECTOR KNOBS. CLEANED AND REPLACED. REPAIRED. BENCH CHECK GOOD. 1G72 3U H3EU 20030305000752003030500075 2003 3 5 HEEA084658 420030212A2340A3016W INTERPHONE BOLKMS105 BO105S 5626006EU COMMS NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 NOISE WHEN TRANSMITTING ON NR 2 VHF. FOUND COMM 2 TRANSMIT R38 SET TOO LOW AND SWITCH AND SWITCH S1 NOISY. SET COMM AND CLEANED S1. REPAIRED. BENCH CHECK GOOD. 1G72 3U H3EU 20030305000762003030500076EU 2003 3 5 HEEA084659 120030212A3340 MOUNT BOLKMS105 BO105S 5626006EU LANDING LIGHT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 RT PULSE LANDING LIGHT CRACKED MOUNT BRACKET. SCRAPPED. 1G72 3U H3EU 20030305000822003030500082EU 2003 3 5 HEEA084665 120030213A6720350A33200406 SPIDER AEROSPAS355 AS355* EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 TAIL ROTOR SPIDER WORN. 1G72 3U H11EU 20030305000852003030500085EU 2003 3 5 HEEA084668 120030213A3246350A4110161361 SKID AEROSPAS355 AS355* EU MLG CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034000L 2873 RT SKID TUBE CRACKED. 1G72 3U H11EU 20030305000862003030500086EU 2003 3 5 HEEA084669 120030213A7110350A5801091704 COWLING AEROSPAS355 AS355* EU NR 2 ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034000L 2873 COWLING HAS A 12 INCH AREA OF SEPARATION IN THE CURVED AREA OF THE COWL AND 2 EACH 6 INCH AREAS OF SEPARATION NEAR THE COWL LATCHES. TO 1G72 3U H11EU 20030305000942003030500094EU 2003 3 5 HEEA084672 120030213A6730704A34240015 ACCUMULATOR AEROSPAS355 AS355* EU MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 MAIN ROTOR LT LATERAL SERVO ACCUMULATOR AND MAIN ROTOR COLLECTIVE SERVO ACCUMULATOR WILL NOT MAINTAIN PRECHARGE PRESSURE. 1G72 3U H11EU 20030305000962003030500096EU 2003 3 5 HEEA084675 120030213A6720 BEARING BOLKMS105 BO105S 5626006EU CONTROL ROD ASSYWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 TAIL ROTOR PITCH CONTROL LINK BEARINGS WORN. REPLACED WITH SERVICEABLE ASSY. 1G72 3U H3EU 20030306000072003030600007SW 2003 3 6 HEEA084720 120030217A632194501031 BRAKE ASSY BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MAIN ROTOR BRAKE HAS WORN PUCKS. REPAIRED. 1G72 4U H4SW 20030306000082003030600008 2003 3 6 HEEA084721 420030217A23709806020023 CVR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 CVR TEST STAYS ON CONSTANTLY. 1G72 4U H4SW 20030306000142003030600014SW 2003 3 6 HEEA084727 120030217A3246AB412050016102 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 MLG SKID SHOE WORN. REPAIRED. 1G72 4U H4SW 20030306000152003030600015SW 2003 3 6 HEEA084728 120030217A3246AB412050016102 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 MLG SKID SHOE IS WORN. REPAIRED. 1G72 4U H4SW 20030306000162003030600016SW 2003 3 6 HEEA084729 120030217A7931APTE138150G TRANSMITTER BELL 412 412 1182202SW ENG OIL PRESSUREFLUCTUATES E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW032148K 36001 OIL PRESSURE FLUCTUATION. REPAIRED. 1G72 4U H4SW 20030306000182003030600018 2003 3 6 HEEA084731 420030217A2340A3016R MIXER BOX BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 MIXER BOX HAS BLEED OVER. REPLACED BAD S1 SELECTOR SWITCH AND KNOB AND ALSO BAD FACEPLATE. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000272003030600027 2003 3 6 HEEA084740 420030217A2340 SWITCH BELL 412 412 1182202SW INTERPHONE BOX FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 8709132 36007 STATIC IN ICS WHEN VOLUME IS ADJUSTED. REPLACED R72 VOLUME CONTROL AND ALSO BAD S5 AND S9 MONITOR SWITCHES. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000332003030600033SW 2003 3 6 HEEA084746 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 STEP ACTUATOR STUCK. REPAIRED. 1G72 4U H4SW 20030306000362003030600036SW 2003 3 6 HEEA084749 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 LT STEP NOT GOING ALL THE WAY DOWN. REPAIRED ACTUATOR. 1G72 4U H4SW 20030306000372003030600037SW 2003 3 6 HEEA084750 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 LT STEP WILL NOT STOW. REPAIRED ACTUATOR. 1G72 4U H4SW 20030306000402003030600040SW 2003 3 6 HEEA084753 120030218A3210400052015101 STRAP BELL 407 407 1182206SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 STRAP DAMAGED WHEN CROSSTUBE SHIFTED. REPLACED STRAP. 1G71 3U O H2SW 20030306000552003030600055SW 2003 3 6 HEEA084770 120030221A3246412050016101 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 MLG SKID SHOE WELDS WORN. REPAIRED. 1G72 4U H4SW 20030306000612003030600061WP 2003 3 6 MWEA030124 120030305A55225930557501 ELEVATOR DOUG DC9 DC981 3022081WP TRAILING EDGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LEFT ELEVATOR LIGHTNING STRIKE ON THE TRAILING EDGE OF THE ELEVATOR SKIN DIRECTLY FORWARD OF THE ANTI-FLOAT TAB UPPER SURFACE. -- FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER AND BALANCED ELEVATOR. 2L72 4F A6WE 20030306000622003030600062WP 2003 3 6 MWEA030125 120030305A55125922578516 STABILIZER DOUG DC9 DC981 3022081WP HORIZONTAL LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LEFT HORIZONTAL STABILIZER HAS A LIGHTNING STRIKE 6" FORWARD OF THE #4 ELEVATOR HINGE. -- REMOVED DAMAGE WITH DRILL AND INSTALLED SHOVEL RIVETS. 2L72 4F A6WE 20030306000652003030600065SW 2003 3 6 HEEA084776 120030221A7810212061201012 EJECTOR BELL 412 412 1182202SW EXHAUST SYSTEM CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 EXHAUST EJECTOR CRACKED. 1G72 4U H4SW 20030306000692003030600069SW 2003 3 6 HEEA084780 120030221A3340212075139001 LANDING LIGHT BELL 412 412 1182202SW EXTERIOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 LANDING LIGHT STUCK IN ON POSITION. REPAIRED. 1G72 4U H4SW 20030306000702003030600070SW 2003 3 6 HEEA084781 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 STEP ACTUATOR WILL NOT EXTEND. 1G72 4U H4SW 20030306000752003030600075SW 2003 3 6 HEEA084786 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 STEP ACTUATOR WILL NOT RETRACT. 1G72 4U H4SW 20030306000802003030600080SW 2003 3 6 HEEA084790 120030221A6730212076004101 SERVO BELL 412 412 1182202SW TAIL ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 TAIL ROTOR SERVO LEAKING FROM TOP SEAL. REPAIRED. 1G72 4U H4SW 20030306000852003030600085SW 2003 3 6 HEEA084794 120030221A6730212076005111 SERVO BELL 412 412 1182202SW MAIN ROTOR BINDING E O OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 MAIN ROTOR SERVO IS BINDING. REPAIRED. 1G72 4U H4SW 20030306000882003030600088SW 2003 3 6 HEEA084797 120030221A2910212076006007 VALVE BELL 412 412 1182202SW HYD SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 HYDRAULIC PRESSURE READS 30 PSI WHEN NOT RUNNING, REPLACE VALVE. 1G72 4U H4SW 20030306000952003030600095SW 2003 3 6 HEEA084803 120030221A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 STARTER GENERATOR WOULD NOT ROTATE. 1G72 4U H4SW 20030121000672003012100067SW 2003 1 21 HEEA083267 120030108A7712206075739103 TORQUEMETER BELL 206 206L3 1182108SW COCKPIT STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 TORQUEMETER STICKING IN HIGH RANGE. REPAIRED. 1G71 3U H2SW 20030121000762003012100076NM 2003 1 21 DHL2003743002 120030121A3350 BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE ON PREFLIGHT. REMOVED AND REPLACED BATTERY PACK. LIGHT OPS CHECKED GOOD PER M/M 33-50-51. 2L73 4F A3WE 20030121000832003012100083WP 2003 1 21 ABXA030036 120030115A243250112284 POWER SUPPLY DOUG DC8 DC861 3021952WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23853AX174 46037 UPON MOVING AIRCRAFT, FOUND EMERGENCY POWER SUPPLY INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED GOOD IAW DC-8 AMM 24-28-00-0. 2L74 4F 4A25 20030121000842003012100084SW 2003 1 21 HEEA083275 120030108A3213206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 CROSSTUBE HAS CORROSION IN ZONE ONE. SCRAPPED. 1G71 3U H2SW 20030121000922003012100092SW 2003 1 21 HEEA083280 120030108A3246206324008 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 SKID TUBE HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030121000962003012100096SW 2003 1 21 HEEA083284 120030109A2810206362002101 FUEL CAP BELL 206 206L3 1182108SW FUEL STORAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N 51512 FUEL CAP HANDLE WILL NOT STAY CLOSED AND LOCKED. SCRAPPED. 1G71 3U H2SW 20030121001012003012100101SW 2003 1 21 HEEA083287 120030109A7933206375007103 INDICATOR BELL 206 206L3 1182108SW ENG OIL TOT STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 TOT INDICATOR NEEDLE STICKS INTERMITTENTLY. REPAIRED. 1G71 3U H2SW 20030121001062003012100106SW 2003 1 21 HEEA083291 120030109A7720206375007103 INDICATOR BELL 206 206L3 1182108SW TOT FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 TOT INDICATOR FLUCTUATES, SOMETIMES DROPPING TO ZERO. 1G71 3U H2SW 20030121001072003012100107SW 2003 1 21 HEEA083292 120030109A3212212073905001 GAUGE BELL 206 206L3 1182108SW EMERGENCY FLOAT CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 WATER IN FLOAT PRESSURE GAUGE, HARD TO READ. SCRAPPED. 1G71 3U H2SW 20030121001232003012100123SW 2003 1 21 HEEA083300 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT FRAYED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 SEAT BELT FRAYED AT TOP OF SHOULDER HARNESS. 1G71 3U H2SW 20030121001262003012100126SW 2003 1 21 HEEA083302 120030109A2821222366621103 FUEL FILTER BELL 206 206L3 1182108SW ENGINE CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 FUEL FILTER BOWL HAS CHAFE MARK. 1G71 3U H2SW 20030121001292003012100129CE 2003 1 21 GLBA2003005 120030113A21301143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162CE CABIN PRESSURE FAILED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03118GL6615 UE118 RT ENVIRO FAIL ANNUN ILLUM, R&R PRSOV OPS CHECK GOOD 2L72 4T RTA24CE 20030121001302003012100130CE 2003 1 21 GLBA2003007 120030114A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE COCKPIT STUCK A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM0396UX 14485 UE96 ABORTED TAKEOFF, LT TORQUE GAUGE STUCK AT 750 LBS. REMOVED AND REPLACED TORQUE IND. 2L72 4T RTA24CE 20030121001432003012100143SW 2003 1 21 HEEA083309 120030109A750023005667 LINE BELL 206 206L4 1182110SW ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 LINE HAS MECHANICAL DAMAGE. REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20030121001492003012100149SW 2003 1 21 HEEA083312 120030109A243523032048 STARTER GEN BELL 206 206B3 1181506SW ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 STARTER GENERATOR HAS A DEAD SPOT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030121001572003012100157SW 2003 1 21 HEEA083315 120030109A793323034927 WIRE HARNESS BELL 206 206L3 1182108SW TOT INDICATOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 DURING FIRST START, TOT NEEDLE DID NOT WORK. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030121001602003012100160GL 2003 1 21 HEEA083317 220030109A725023062087 CHECK VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL TURBINE OIL DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 CHECK VALVE HAS DAMAGED FITTING THREADS. REPAIRED. 1G71 3U3 U H2SW E1GL 20030121001632003012100163EU 2003 1 21 2003UALA00062 120030115A2900D2901010200400 PIPE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE A UALAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP29423UA 504 FLIGHT DIVERTED DUE TO GREEN HYDRAULIC SYSTEM LOW. SUPPLEMENTAL DATA UPDATE FOUND LINE FROM HYD PRESSURE MODULE #1 ENG LEAKING AT FITTING. THE LINE WAS REPLACED. THE ENGINE PUMP CASE DRAIN AND HYDRAULIC CONTROL UNIT FILTERS WERE ALSO REPLACED PRECAUTIONARY. 2L72 4F4 FRTA28NM E40NE 20030121001642003012100164SW 2003 1 21 HEEA083318 120030109A2435200SGL132Q STARTER GEN BELL 206 206L1 1182107SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032776614776 45312 STARTER GENERATOR WILL NOT STAY ON LINE. 1G71 3U H2SW 20030121001742003012100174WP 2003 1 21 IXXA0300002O 120030103A3260 SOCKET DOUG DC8 DC873F 302199FWP COCKPIT LOOSE A IXXAK NONE N FALSE WARNING CLCLIMB 1 SW11606AL89095818 46044 DURING CLIMB FROM DFW CREW NOTED LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED. THE GEAR WAS CYCLED AND AN UPLATCH CHECK PERFORMED. THE UPLATCH CHECK INDICATED THE GEAR SAFELY STOWED BUT LIGHT REMAINED ILLUMINATED. CREW CONTINUED TO LRD FOR AN UNEVENTFUL LANDING. UPON INSPECTION BY MAINTENANCE, THE INDICATING LIGHT SOCKET WAS FOUND TO BE INSECURE. THE LIGHT SOCKET WAS PROPERLY SECURED PER THE AIRCRAFT MAINTENANCE MANUAL, A SUCCESSFUL OPERATIONAL CHECK PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030121001762003012100176WP 2003 1 21 IXXA0300003O 120030107A3231 UPLOCK DOUG DC8 DC863F 302198FWP LANDING GEAR LACK OF LUBE A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11867BX831202238 46049 AFTER DEPARTURE FROM FWA DURING GEAR RETRACTION DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR AND LIGHT REMAINED ILLUMINATED, APPROX 3 MINUTES LATER LIGHT EXTINGUISHED. CREW PROCEEDED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED LUBED AND TESTED UPLATCH SYSTEM WITH PASSING RESULTS. ALL WORK ACCOMPLISHED PER AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 20030121001842003012100184GL 2003 1 21 HEEA083331 220030109A7321252464431 FUEL CONTROL BELL 206 206B3 1181506SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 FUEL CONTROL PRODUCING HIGH STARTING TEMPS. ADJUST DOWN TO COLD ADJUST UP TO HOT. IN SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030121001852003012100185GL 2003 1 21 HEEA083332 220030109A7323252466715 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 DROOP AND NO ADJUSTMENT LEFT TO ADJUST IT OUT. IN SHOP REPAIR. 1G71 3U3 U H2SW E4CE 20030121001922003012100192SW 2003 1 21 HEEA083337 120030109A243230135002 BATTERY BELL 206 206B3 1181506SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032268V 3605 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121001932003012100193SW 2003 1 21 HEEA083338 120030109A243230135002 BATTERY BELL 206 206B3 1181506SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032268V 3605 MAIN BATTERY TOO WEAK TO START AIRCRAFT. REPLACED BATTERY. 1G71 3U H2SW 20030121001962003012100196SW 2003 1 21 HEEA083340 120030109A243230135002 BATTERY BELL 206 206B3 1181506SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03103PH 3000 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121002062003012100206SW 2003 1 21 HEEA083350 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0381671 51301 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121002142003012100214EU 2003 1 21 MALA030108 120030113A3397 WIRE BAC 146 AVRO146RJ85A1500097EU CABIN EXPOSED A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 FLOOR TRACK LIGHT WIRES EXPOSED ROW 6, LIGHT, COVER ALL BASES. 2H74 4F RTA49EU 20030121002382003012100238SW 2003 1 21 HEEA083359 120030109A6320406340100101 PUMP BELL 206 206L4 1182110SW XMSN OIL LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW037074W 52033 TRANSMISSION OIL PUMP LEAKS. REPAIRED. 1G71 3U NCH2SW 20030121002402003012100240SW 2003 1 21 HEEA083360 120030109A671041001687 LEVER BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TOTAL TRAVEL OF INPUT LEVER WAS UNDER LIMIT OF 0.039 INCH TO 0.046 INCH. ACTUAL TRAVEL WAS 0.037 INCH. 1G71 3U H2SW 20030121002442003012100244EU 2003 1 21 MALA030112 120030118A339774331 WIRE SAAB SF340 340B 7860101EU CABIN BROKEN A MALAK NONE O OTHER NRNOT REPORTED 1 GL15420XJ 340B420 MAINTENANCE FOUND MOST FORWARD FLOOR PROX EMERGENCY LIGHT STRIP, WIRES BROKEN OFF. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP IAW SF340 AMM 33-50-20-4. OPS CHECK GOOD. 2L72 4T RTA52EU 20030121002462003012100246EU 2003 1 21 MALA030113 120030118A5210 TRACK BAC 146 AVRO146RJ85A1500097EU PAX DOOR OBSTRUCTED A MALAK NONE O OTHER NRNOT REPORTED 1 GL15530XJ E2364 PASSENGER DOOR WOULD NOT OPEN FROM OUTSIDE ON FLIGHT 3414. THE LT FWD MAIN CABIN DOOR IS BINDING AND EXTERNAL DIFFICULT TO OPEN FROM BOTH INSIDE AND OUTSIDE. MAINTENANCE REMOVED INNER UPPER DOOR PANEL, INSPECTED, CLEANED AND LUBED. REASSEMBLED DOOR PANEL, OPS CHECK GOOD. FOUND FOREIGN OBJECT IN LOWER SLIDE TRACK. 2H74 4F RTA49EU 20030303002022003030300202NM 2003 3 3 CALA0300078 120030228A5330 SKIN BOEING777 777224 1385225NM STA 1979 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977006 29476 INSPECTION FOUND A DENT IN R/H FUSELAGE SKIN AT STA 1979, S28R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 4, FIGURE 202. 2L72 4F RTT00001SE 20030303002072003030300207NM 2003 3 3 CALA0300085 120030302A5320 CHANNEL BOEING737 7373T0 1384582NM STA 1006-1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND CHANNEL CORRODED ON UPPER SURFACE AND AT NUTPLATES AT STA 1006-1016, LBL 5 TO LBL 9. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02. 2L72 4F RTA16WE 20030304000012003030400001SW 2003 3 4 AC2A084857 120030220A3246430036026101 SKID BELL 430 430 1182150SW MLG CRACKED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CH5443 49037 MLG SKID TUBE IS CRACKED. REPLACED 1G72 3U RTH9SW 20030304000032003030400003SW 2003 3 4 AC2A084859 120030221A6520222042001103 GEARBOX BELL 430 430 1182150SW TAIL ROTOR CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT1142 49089 OUTPUT SHAFT SPLINES ARE RUSTED, WORN AND ONE SPLINE IS CRACKED TOWARDS INBOARD SIDE. THIS IS THE FIRST TIME THE TAIL ROTOR ASSEMBLY WAS REMOVED SINCE RECEIVING THE AIRCRAFT NEW FROM BELL HELICOPTER. REPLACE GEARBOX ASSEMBLY WITH EXCHANGE UNIT. 1G72 3U RTH9SW 20030304000042003030400004SW 2003 3 4 AC2A084860 120030221A6420222012703103 TRUNNION BELL 430 430 1182150SW T/R HEAD CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT1142 49089 SPLINES ON INNER SURFACE ARE RUSTED AND PITTED. THIS TRUNNION WAS ATTACHED TO TAIL GEARBOX SN A782 WHICH ALSO HAD A CRACKED SPLINE. REPLACED TRUNNION ASSEMBLY. 1G72 3U RTH9SW 20030304000052003030400005GL 2003 3 4 AC2A084861 220030221A732323065121 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE DAMAGED H AC2AK NONE O OTHER ININSP/MAINT 1 FS018775 9383 775 831789 POTTING COMPOUND BROKEN ON THE DRIVE SPLINE END. GOVERNOR WAS REPLACED. 1G72 3U3 U H3EU E4CE 20030304000112003030400011SW 2003 3 4 AC2A084867 120030224A64201200134A SLEEVE BELL 430 430 1182150SW BELLCRANK ASSY WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT1142 49089 SLEEVE IS WORN THROUGH THE LINER. REPLACED WITH NEW PART. 1G72 3U RTH9SW 20030304000132003030400013SW 2003 3 4 AC2A084869 120030224A6420312712001 SLEEVE BELL 430 430 1182150SW TAIL ROTOR DELAMINATED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CT 49089 LINER CAME UNBONDED FROM SLEEVE. REPLACED WITH NEW PART. 1G72 3U RTH9SW 20030304000162003030400016NE 2003 3 4 AC2A084872 120030302A53207620103014106 ANGLE SKRSKYS76 S76A 8143006NE FUSELAGE CORRODED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS015401G 760137 COROSION FOUND ON ANGLE DURING INSPECTION. PART WAS REPLACED. 1G72 3U H1NE 20030304000222003030400022EU 2003 3 4 BAQA084705 120030224A6240AWEURO4 SIGNAL COND UNIT UROCOPEC135 EC135T1 5620026EU MAST MOMENT INACCURATE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01522ME158 0144 SIGNAL COND UNIT PRODUCING IRREGULAR READINGS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030324000252003032400025EU 2003 3 24 373PA0007 220030303A7200 ENGINE BOEING737 7373Y0 1384671NM CFMINTCFM56 CFM563B2 13802EU NR 2 MALFUNCTIONED A PIDAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO05373PA 23749 AUTO THROTTLE ON NR 2 ENGINE WILL NOT MAINTAIN POSITION. MOVES FWD & AFT APX.1 INCH WHEN N1 IS STABLE; CLIMB, CRUISE, T/O. PERFORMED BITE CHECK ON CMC AUTO THROTTLE CHECK OF PLA & INFLIGHT FAULTS. SHOWS N1 (BLOOM) FAULT. A/C RELEASED UNDER MEL 22-4, CONT. #0303002. PLACARDS INSTALLED ON AUTO THROTTLE SYSTEM. 3/7/03. REMOVED & REPLACED NR 2 ENGINE MEC IAW 737-300 MM 73-21-01. THIS CLEARS MEL 22-4 CONT. NO. 0303002. 2L72 4F4 FRTA16WE E21EU 20030304000292003030400029EU 2003 3 4 CDBR084854 120030228A2100 BELT AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1D NE AIR CONDITIONINGFAILED H CDBRO OTHER O OTHER NRNOT REPORTED 1 FS01311SJ296 3583 9818 AIR CONDITIONING BELT FAILED CAUSING DAMAGE TO THE HYDRAULIC BELT. 1G72 3U3 U H11EU E19EU 20030304000342003030400034SW 2003 3 4 HEEA084570 120030214A6210412015300109 BLADE BELL 412 412EP 1182205SW MAIN ROTOR OUT OF BALANCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03412PH10825 36140 MAIN ROTOR BLADE NEEDS TO BE REBALANCED ACCORDING TO SPECS. 1G72 4U H4SW 20030314000772003031400077NM 2003 3 14 CALA0300087 120030304A215022064001 ACM BOEING737 737824 13844BZNM RT AC PACK BURNED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW091423112524 28795 FLIGHT ATTENDANT'S REPORTED SMOKE AND A BURNED RUBBER ODOR IN FORWARD CABIN ON LANDING AT EWR. THE SMOKE CLEARED QUICKLY. MAINTENANCE FOUND THE RT ACM AT FAULT. THE RT ACM WAS REMOVED AND REPLACED IAW MM 21-51-04. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20030314000972003031400097 2003 3 14 SWAA030547 420030308A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030314000992003031400099NM 2003 3 14 SWAA030507 120030306A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA 3.5 IN LONG CRACKS AT FUSELAGE SKIN, BS 941 AND BS 972, BELOW STRINGER 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030314001002003031400100NM 2003 3 14 SWAA030508 120030306A53156546804 BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, WL 208, LBL 35 TO RBL 22. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20030314001032003031400103NM 2003 3 14 SWAA030511 120030306A53126516300 WEB BOEING737 7373Q8 1384670NM NOSE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 201, AT LBL 4.75, RBL 4.75, WL 209, AT LBL 4.75 AND WL 234, AT RBL 12. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20030314001082003031400108WP 2003 3 14 AMTA200300196 120030125A5330 DOUBLER LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE FUSELAGE CORRODED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11163AT 1229 AFT FUSELAGE SECT, INTERNAL DOUBLER HAS CORROSION AFT OF C2 DOOR CUT OUT, STA 1625 BETWEEN STR 16, 17. REPAIRED CORROSION DAMAGE IAW EAR. 2L73 4F4 F A23WE A12EU 20030314001102003031400110NM 2003 3 14 BJNA030218 120030227A5313BAC1498117 STRINGER BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM46484 23046 DURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON STRINGER 26 RIGHT, LOCATED AT BS 980. REMOVED THE CORRODED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR SECTION AND STRINGER SPLICE IAW WITH SRM. 2L72 4F4 FRTA16WE E2EA 20030314001112003031400111NM 2003 3 14 BJNA030219 120030227A5414657377482 SKIN BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE NR 2 ENG NACELLECORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM16184 23046 DURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED ON NR 2 ENGINE INBOARD COWLING. CORROSION WAS LOCATED UNDERNEATH THE FIRE SEAL AREA THROUGHOUT THE FORWARD AND AFT SECTION. REMOVED FIRE SEAL FOR ACCESS TO THE CORRODED SECTION OF SKIN. REMOVED THE CORRODED SECTION OF SKIN, FABRICATED AND INSTALLED NEW SECTION OF SKIN IAW SRM. FIRE SEAL WAS THEN REATTACHED TO ENGINE COWLING. 2L72 4F4 FRTA16WE E2EA 20030119000032003011900003SO 2003 1 19 RAIA00301012 120030110A26123601134480220 FIRE LOOP EMB 145 EMB145 3260210SO FALSE INDICATIONA RAIAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 CE03802HK10610 145066 5260-PIT- RIGHT ENGINE FIRE WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE PYLON FIRE DETECTOR LOOP, OPS CK OK. 2L72 4F RTT00011AT 20030119000052003011900005NE 2003 1 19 RAIA00301015 220030116A730031055016 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03564HK6899 41081 75103 5455-CMI- LEFT ENGINE INTEGRATED ENGINE CONTROL FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED THE INLET PRESSURE SENSOR, OPS CK OK. 2L72 4T4 TRTA41NM E18NE 20030130001532003013000153NM 2003 1 30 F3LA200300003 120030114A5310 STRAP BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD DOOR FRAME RADIUS STRAP, STA 794.3, CORRODED AT STR 25R. FOUND RADIUS STRAP OUT OF LIMITS PER SRM 53-16-15, FIG 101. REMOVED AND INSTALLED REPLACEMENT STRAP PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20030130001562003013000156NM 2003 1 30 F3LA200300005 120030115A5311 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FUSELAGE LOWER FRAME CRACKED IN TWO PLACES AT STA 500 BETWEEN STR 27R AND 27L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-70-11. 2L72 4F RTA16WE 20030120000012003012000001NE 2003 1 20 NACA20030068 220030117A8530356993 CYLINDER PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE 2 CRACKED A NACAE ENGINE SHUTDOWN RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET DEDESCENT 1 AL032907F1700 1700 55337 44636 55337 DISCREPANCY: #1 engine precationary shut down for excessive vibration.CORRECTIVE ACTION: Replaced #1 engine #2 cylinder. (Cracked head). 2L74 4R4 R A781 5E8 20030120000022003012000002SO 2003 1 20 C2XA03CL014 120030116A3231MS277891A SWITCH EMB 145 EMB145LR 3260212SO COCKPIT INTERMITTENT A C2XAO OTHER O OTHER CLCLIMB 1 SW2713988 145265 CLE FLIGHT#2301 THE CREW REPORTED THE NOSE GEAR DOORS STAYED OPEN AFTER GEAR RETRACTION.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR EMERGENCY EXTENSION OVERRIDE SWITCH.WIRE SPLICE SP1750 WAS ALSO REPAIRED.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030120000142003012000014EA 2003 1 20 COMA0360032 120030116A2150 ACM CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01472CA 7667 FLIGHT 5732 CLOUDS COMING FROM L/H AIR CODITIONING SYSTEM.COULD NOT DUPLICATE. OPERATED A/C SYSTEM, FOUND NO DEFECTS. 2L72 4F RTA21EA 20030120000172003012000017NM 2003 1 20 QXEA0300099 120030117A243023088002A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09351PH169171023 490 PDX- NO.1 DC GENERATOR CAUTION LIGHT ILLUMINATED. RAN EMERGENCY CHECKLIST, NO OTHER LIGHTS ASSOCIATED WITH PROBLEM. REMOVED AND REPLACED NO.1 STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030130001632003013000163NM 2003 1 30 F3LA200300010 120030117A5320 ATTACH ANGLE BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO DOOR SILL ATTACH ANGLE AT STA 794.5, RBL 24, CORRODED ON FLANGE. FOUND CORROSION OUT OF LIMITS PER SRM 51-60-15, FIG 106, DETAIL VIII. REPLACED ANGLE PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20030121000052003012100005NM 2003 1 21 SWAA030082 120030114A53206548606 SKIN BOEING737 7373H4 1384600NM A/C COMPT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C4 CHECK, FOUND LT/RT EXTERNAL A/C COMPT DOOR CUTOUTS CRACKED AT FWD OUTBD EDGES. REPAIRED SKIN CUTOUTS PER SRM. 2L72 4F RTA16WE 20030121000162003012100016 2003 1 21 SWAA030057 420030110A2565D31354 SLIDE BOEING737 7377H4 1384404NM CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD ENTRY AND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030121000182003012100018NM 2003 1 21 SWAA030061 120030110A575465C26601 SLAT BOEING737 7373Y0 1384671NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C3 CHECK, FOUND NR 6 L/E SLAT T/E SKIN CRACKED AT AFT ROW OF RIVETS. REMOVED AND REPLACED NR 6 L/E SLAT PER MM. 2L72 4F RTA16WE 20030121000202003012100020NM 2003 1 21 SWAA030063 120030111A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29712SW 27846 DURING SCHEDULED SERVICE CHECK, SWA SI 11035-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 4 HINGE ATTACH POINTS PER MM. 2L72 4F RTA16WE 20030121000312003012100031SW 2003 1 21 HEEA083223 120030108A7160206064213103 SCREEN BELL 206 206L3 1182108SW ENGINE INTAKE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 ENGINE INTAKE SCREEN ASSY HAS CORROSION. REPAIRED. 1G71 3U H2SW 20030121000322003012100032SW 2003 1 21 HEEA083224 120030108A7160206064213103 SCREEN BELL 206 206L3 1182108SW ENGINE INTAKE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 ENGINE INTAKE SCREEN ASSY HAS CORROSION. REPAIRED. 1G71 3U H2SW 20030121000392003012100039SW 2003 1 21 HEEA083231 120030108A7603206064713103 POWER LEVER BELL 206 206L3 1182108SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 POWER LEVER WORN. SCRAPPED. 1G71 3U H2SW 20030121000422003012100042SW 2003 1 21 HEEA083234 120030108A7714206070265011 INDICATOR BELL 206 206B3 1181506SW DUAL TACH STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 DUAL TACH TURBINE NEEDLE STICKS. 1G71 3U H2SW 20030121000472003012100047SW 2003 1 21 HEEA083249 120030108A2560206072841111 SEAT BELT BELL 206 206L3 1182108SW COCKPIT FRAYED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 SEAT BELT FRAYED. SCRAPPED. 1G71 3U H2SW 20030121000482003012100048SW 2003 1 21 HEEA083250 120030108A2560206072841111 SEAT BELT BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 RUBBER SHOULDER HARNESS SPACER MISSING. REPAIRED. 1G71 3U H2SW 20030121000502003012100050SW 2003 1 21 HEEA083252 120030108A6510206073913001 BLOWER BELL 206 206L3 1182108SW TAIL ROTOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 TAIL ROTR BLOWER INOPERATIVE. REPAIRED. 1G71 3U H2SW 20030121000662003012100066WP 2003 1 21 IXXA030004O 120030114A7932JT3D3B ENGINE DOUG DC8 DC862 3021970WP #2 ENGINE ASSY DEFECTIVE A IXXAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 SW11799AL605293680 45918 ENROUTE FROM FJDG TO OBBI CREW NOTED #2 OIL QUANTITY DROPPED. CREW ELECTED TO FOLLOW ATI PROCEDURE AND SHUTDOWN THE #2 ENGINE. THE FLIGHT CONTINUED ON TO OBBI FOR AN UNEVENTFUL LANDING.OIL PRESSURE INDICATION ON #2 ENGINE REMAINED IN THE "POSITIVE"RANGE FOR DURATION OF FLIGHT. UPON INSPECTION OF THE #2 ENGINE MAINTENANCE NOTED OIL DISCHARGE THRU TURBINE AND FOREIGN MATERIAL IN OIL STRAINER. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE IAW APPLICABLE AIRFRAME AND ENGINE MANUALS. UPON COMPLETION OF SUCCESFULL ENGINE RUN AND CHECK OUT THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20030121000692003012100069SW 2003 1 21 HEEA083269 120030108A7712206075739103 TORQUEMETER BELL 206 206L3 1182108SW COCKPIT FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 TORQUEMETER NEEDLE FLUCTUATES IN FLIGHT. REPAIRED. 1G71 3U H2SW 20030121000792003012100079WP 2003 1 21 ABXA030033 120030114A3260 STRIKER DOUG DC8 DC861 3021952WP RT MLG WORN A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23843AX 46017 DURING UPLATCH CHECK, THE UNSAFE LIGHT ILLUMINATED WITH THE RIGHT DOOR UNSAFE LIGHT ON FLIGHT ENGINEER'S PANEL. RECYCLED GEAR 3 TIMES WITH NO IMPROVEMENT. RAN THE ALTERNATE UPLATCH CHECK AND A SLIGHT YAW COULD BE FELT. DOOR LIGHT STILL ILLUMINATED. UNTIL FLAPS WERE PLACED TO 25 DEG DOOR CLOSED AND NOT LATCHED/GEAR UNSAFE LIGHT EXTINGUISHED. CONTINUED TO ILN AT NORMAL SPEED AS PER ABNORMAL. FOUND RIGHT MAIN LANDING GEAR DOOR UPLOCK INDICATOR STRIKER WORN. REPLACED RIGHT MAIN LANDING GEAR DOOR UPLOCK INDICATION STRIKER IAW DC-8 MM 32-31-04-4. PERFORMED GEAR EXTENSION AND RETRACTION CYCLE SEVERAL TIMES IAW DC-8 MM 32-30-00-2. NO DISCREPANCIES NOTED, SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 20030121000872003012100087SW 2003 1 21 HEEA083277 120030108A3213206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 CROSSTUBE HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030121000882003012100088WP 2003 1 21 ABXA030038 120030102A523039132492 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 FORWARD LOWER CARGO DOOR NR 2 BEAM FORWARD FITTING CRACKED AT FASTENER. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030121000892003012100089WP 2003 1 21 ABXA030039 120030102A57535919217202 HINGE DOUG DC9 DC931 3022065WP T/E FLAP RUSTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 RUST BLEEDING FROM RIGHT WING CENTER FLAP HINGE INBOARD UPPER ATTACH STUD. REPLACED FORWARD CENTER FLAP HINGE IAW DC-9 MM 57-4-01-2-0001. 2L72 4F A6WE 20030121000902003012100090SW 2003 1 21 HEEA083278 120030108A3210206323202 SUPPORT BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 MLG SUPPORT HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030121000982003012100098SW 2003 1 21 HEEA083286 120030109A3212206369002 FLOAT BELL 206 206L3 1182108SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MLG EMERGENCY FLOAT BAG LEAKS. 1G71 3U H2SW 20030121001042003012100104SW 2003 1 21 HEEA083289 120030109A7720206375007103 INDICATOR BELL 206 206L3 1182108SW TOT STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 TOT INDICATOR STICKS/HANGS AROUND 300 DEGRES DURING ENGINE STARTS. REPAIRED. 1G71 3U H2SW 20030121001052003012100105SW 2003 1 21 HEEA083290 120030109A7720206375007103 INDICATOR BELL 206 206L3 1182108SW TOT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 TOT INDICATOR TEST LIGHT INOPERATIVE. REPAIRED. 1G71 3U H2SW 20030121001132003012100113SW 2003 1 21 HEEA083296 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MISINSTALLED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW036610Y 51419 MOUNTING BRACKET ORIENTATION IS BACKWARD. REEL IS NOT FUNCTIONING PROPERLY (RATCHETY). 1G71 3U H2SW 20030121001202003012100120SO 2003 1 21 LR7A03002 120030117A5311 FRAME LKHEED382 382G 526414USO FS 770 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 472 4606 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB0505 FOUND RH FS 770 FRAME CAP AND WEB CRACKED AT RBL 66, WL 157.REPAIRED CAP IAW SRM SMP 583 51-140-22 AND 51-140-05 AND WEB IAW 51-140-17. NR 0113. 2H74 4T A1SO 20030121001212003012100121SO 2003 1 21 LR7A03003 120030117A574033257062 FITTING LKHEED382 382G 526414USO OWS 28 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 472 4606 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB0521 FOUND RH FLAP TRACK RIB STIFFENER FITTING CRACKED 2.0 IN. IN LOWER FLANGE AT RH OWS 28, FS 598, WL 257.REPLACED FITTING IAW SRM SMP 583 51-70 AND DWG 3325706. NR 0115. 2H74 4T A1SO 20030121001252003012100125SW 2003 1 21 HEEA083301 120030109A2821 WARNING LIGHT BELL 206 206L3 1182108SW FUEL FILTER ACTIVATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 299 51530 FUEL FILTER LIGHT FLICKERED. 1G71 3U H2SW 20030121001392003012100139GL 2003 1 21 HEEA083307 220030109A753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 2716 51527 BLEED VALVE PRODUCING COMPRESSOR STALL. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 U H2SW E1GL 20030121001422003012100142SW 2003 1 21 HEEA083308 120030109A750023005667 LINE BELL 206 206L3 1182108SW PC FILTER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 DURING INSPECTION OF TUBE ASSY, FOUND MECHANICAL DAMAGE TO FLARE AT END OF TUBE CONNECTED TO PC FILTER. FURTHER INSPECTION REVEALED ONE CRACK COMING FROM AREA OF ONE OF THE DAMAGE SIGHTS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030121001622003012100162NM 2003 1 21 2003UALA00060 120030115A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 SHARP DENT FOUND ON SKIN REPAIR DOUBLER BETWEEN BS600 AND 620 AND STR 16L AND 17L; MORE DENTS BETWEEN BS600 AND 660, STR 14L AND 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER SKIN. 2L72 4F4 FRTA2NM E17NE 20030306000962003030600096SW 2003 3 6 HEEA084804 120030221A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 STARTER GENERATOR WENT OFF LINE. 1G72 4U H4SW 20030306000982003030600098 2003 3 6 250TR0006 420030202A2230734SUE23 COMPUTER BOEING737 7372K5 138448XNM A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 Auto throttle would not engage. R&R auto throttle computer. Chks good per MM 22-31-01. 2L72 4F RTA16WE 20030306001012003030600101SW 2003 3 6 HEEA084808 120030221A6320 PLANETARY GEAR BELL 412 412 1182202SW M/R GEARBOX MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 6495 A77 33134 MAIN ROTOR GEARBOX PLANETARY GEAR MAKING METAL. REPAIRED. 1G72 4U H4SW 20030306001072003030600107SW 2003 3 6 HEEA084814 120030221A2510412070820101 SEATBACK CUSHION BELL 412 412 1182202SW CREW SEAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 SEAT BACK CUSHION WORN. REPAIRED. 1G72 4U H4SW 20030306001082003030600108SW 2003 3 6 HEEA084815 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 MAIN ROTOR HEAD ROD BEARING WORN. 1G72 4U H4SW 20030306001132003030600113SW 2003 3 6 HEEA084820 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 MAIN ROTOR HEAD HAS A WORN BEARING. REPAIRED. 1G72 4U H4SW 20030306001192003030600119EU 2003 3 6 03064311 120030305A33503022473 LIGHT JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27311UE 41029 During maintenance it was discovered that the r/h overwing emergency exit light was inoperative. Maintenance personnel removed and replaced the r/h overwing emergency exit light assy. An operational check was satisfactory and the aircraft was returned to service. 2L72 4T RTA41NM 20030307000062003030700006SO 2003 3 7 C2XA03SH41 120030307A530014521725001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV- DURING C CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 22 AND 23. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01089. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE 2L72 4T RTT00011AT 20030307000172003030700017 2003 3 7 SWAA030495 420030305A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 AND L2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29647SW 27717 DURING SCHEDULED C2 CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDES PER MM 2L72 4F RTA16WE 20030307000182003030700018NM 2003 3 7 SWAA030497 120030305A2560P4010021 BATTERY BOEING737 7373H4 1384600NM CABIN WEAK A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACEDFLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20030307000202003030700020NM 2003 3 7 SWAA030499 120030305A53116558280 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 13L TO 14L. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20030307000222003030700022 2003 3 7 SWAA030501 420030305A256565C19901 CABLE BOEING737 7372H4 138448CNM L1 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED SLIDE RELEASE CABLE PER MM. 2L72 4F A16WE 20030307000252003030700025NM 2003 3 7 SWAA030473 120030303A56206545785 FRAME BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW FRAMES CRACKED AT BS 530, STR 12R AND BS 450, STR 5R. REMOVED AND REPLACED BOTH WINDOW FRAMES PER SRM AND SWA AE. 2L72 4F RTA16WE 20030307000262003030700026NM 2003 3 7 SWAA030474 120030303A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 11R CRACKED AT BS 530. REPAIRED STRINGER PER ERO. 2L72 4F RTA16WE 20030307000272003030700027NM 2003 3 7 SWAA030475 120030303A53306545877 STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SPECIAL VISIT, FOUND BEAR STRAP CRACKED AT BS 360, STR 4R. REPAIRED BEAR STRAP PER SRM AND ERO. 2L72 4F RTA16WE 20030307000302003030700030NM 2003 3 7 SWAA030478 120030303A53156546804 BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 208, RBL 1. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20030307000352003030700035NM 2003 3 7 SWAA030450 120030302A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030307000372003030700037 2003 3 7 SWAA030452 420030227A25656557463 BRACKET BOEING737 7375H4 138449DNM FWD CABIN DOORS LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS LOOSE. SECURED ATTACH BRACKETS PER MM. 2L72 4F RTA16WE 20030307000472003030700047NM 2003 3 7 SWAA030465 120030302A53116546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030307000492003030700049NM 2003 3 7 SWAA030467 120030301A552065C27351 HINGE BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR OTBD ATTACH HINGE WORN. REMOVED AND REPLACED LT ELEVATOR ATTACH HINGE PER MM. 2L72 4F RTA16WE 20030307000542003030700054 2003 3 7 SWAA030442 420030227A256565C19901 CABLE BOEING737 7373H4 1384600NM AFT ENTRY DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030307000752003030700075NM 2003 3 7 SWAA030489 120030304A53116546543 FRAME BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, BETWEEN STRINGERS 11R AND 13R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030307000782003030700078NM 2003 3 7 SWAA030492 120030304A5552BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29751SW 29803 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 HINGE ATTACH POINT BOLT BUSHING PER MM. 2L72 4F RTA16WE 20030307000862003030700086NE 2003 3 7 HEEA084886 120030227A2435303001383 BRUSHES SKRSKYS76 S76A 8143006NE STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X282 Y20246 760050 STARTER GENERATOR MOTORING. REPLACED 4 BRUSHES DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030307000892003030700089 2003 3 7 HEEA084890 420030227A34427007700614 INDICATOR SKRSKYS76 S76A 8143006NE WX RADAR SYS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 WEATHER RADAR INTERMITTENTLY SHUTS DOWN AFTER TEN MINUTES. 1G72 3U H1NE 20030307000902003030700090 2003 3 7 HEEA084892 420030227A34427021450601 COMPUTER SKRSKYS76 S76A 8143006NE WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 WEATHER RADAR COMPUTER FAILED IN FLIGHT. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030307001142003030700114EU 2003 3 7 AALA20030032 120030107A2120 SMOKE FOKKERF28 F28MK0100 4990807EU CABIN DETECTED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW211402K 11353 EWR - FLT 867 - EN ROUTE EWR-ORD, SMOKE IN CABIN WITH A ELECTRICAL SMELL. CHECKED GALLEY EQUIPMENT AND LIGHTING. RETURNED EWR AND LANDED WITHOUT INCIDENT. SUSPECT GLYCOL INGESTION FROM APU CAUSE OF SMOKE. RAN ENGINES AND NO SMOKE DETECTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030307001222003030700122WP 2003 3 7 AALA20030094 120030103A5310 WINDOW FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 TUL - FOUND LOWER WINDOW FRAME TAB CRACKED, BOTTOM FORWARD CORNER. INSTALLED REPAIR ANGLE ON BOTTOM FORWARD CORNER OF WINDOW FRAME AT STATION 1155 LEFT PER AARD 53-10-00-25. (M) 2L72 4F A6WE 20030307001282003030700128WP 2003 3 7 AALA20030100 120030120A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21598AA 53288 TUL - FOUND CORROSION AROUND ANTENNA CUTOUT 1 INCH HOLE STATION 380. REMOVED LIGHT CORROSION BY BLENDING PER SRM 51-10-03. (M) 2L72 4F RTA6WE 20030307001382003030700138WP 2003 3 7 AALA20030109 120030125A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21462AA 49592 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTRIP EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED AFT STAIR EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030304000352003030400035EA 2003 3 4 COMA0360128 120030228A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01940CA 7048 FLIGHT 5053 R/H REVERSER UNLOCKED MESSAGE DURING T/O.DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030304000362003030400036SO 2003 3 4 C2XA03CL062 120030303A527014528235401 SWITCH EMB 145 EMB145LR 3260212SO CABIN OUT OF ADJUST A C2XAK NONE J WARNING INDICATION CRCRUISE 1 SW2716981 145208 CLE FLIGHT#2124 THE CREW REPORTED A EMERGENCY EXIT OPEN INDICATION IN FLIGHT ON THE EICAS.THE INDICATION WAS ON THE LEFT SIDE.CABIN PRESSURIZATION WAS MAINTAINED.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND ADJUSTED THE LEFT EMERGENCY EXIT DOOR MICROSWITCH ASSEMBLY.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030304000472003030400047SW 2003 3 4 HEEA084579 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH A1971 33150 MAIN ROTOR MAST LINK HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030304000602003030400060SW 2003 3 4 HEEA084591 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000622003030400062SW 2003 3 4 HEEA084593 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R4058 36007 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000652003030400065SW 2003 3 4 HEEA084596 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030304000662003030400066SW 2003 3 4 HEEA084597 120030214A6230 BEARING BELL 412 412 1182202SW M/R LINK UNSTAKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S A2980 36002 HUB AND SLEEVE ASSY LINK HAS A BEARING UNSTAKED. REPAIRED. 1G72 4U H4SW 20030304000872003030400087NM 2003 3 4 DL73K030140 120030208A5312651630086 BULKHEAD BOEING737 737232 1384475NM FS 178 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27302DL 23047 FUSELAGE / BULKHEAD / FS 178 / WEB AND SIDE CHORDS : CRACK REPAIR THE FS 178 BULKHEAD WEB AND SIDE CHORDS WERE FOUND WITH CRACKS TYPICAL OF BAC S/B 737-53-1173 AND AD 2000-05-29. THE WEB HAD SEVERAL EXISTING REPAIRS INSTALLED. THE WEB WAS REMOVED AND REPLACED, AND THE CRACKED SIDE CHORDS REPLACED PER THE PROCEDURES OF THE BAC S/B AND PER ER/A 384474-14AD. 2L72 4F RTA16WE 20030304000882003030400088NM 2003 3 4 DL72S030141 120030210A3350D334102486 BATTERY PACK BOEING727 727232 1384082NM MID CABIN RT OVHDISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27544DA 22493 RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. 2L73 4F A3WE 20030304000952003030400095NM 2003 3 4 DL757030186 120030221A5330143N37505 SKIN BOEING757 757232 1384965NM FS 1701, S-16L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27652DL 24392 FUSELAGE / SKIN / FS 1701 / STRG. 14L-18L : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH A DENT AND GOUGE AT FS 1701 BETWEEN STRINGERS 14L & 16L. AN EXISTING SRM REPAIR WAS LOCATED IMMEDIATELY BELOW THE DAMAGE. THE DAMAGE WAS REMOVED WITH A CUTOUT AND THE SRM REPAIR REMOVED AND EXISTING CUTOUT INSPECTED. BOTH AREAS WERE COMBINED INTO A SINGLE REPAIR OF 2 ALUMINUM DOUBLERS PER ER/A 384496-14, REV A. 2L72 4F RTA2NM 20030304000982003030400098 2003 3 4 HEEA084600 420030214A3442MI5851345 INDICATOR BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 WEATHER RADAR TEST PATTERN BAD AND OPERATIONAL MODES BROKEN. FOUND ALL GREEN SCREEN, FOUND LOGIC NR 1 BOARD SHORTING OUT AGAINST CHASIS SCREW. RELOCATED SCREW, REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030304001042003030400104EU 2003 3 4 03062306 120030303A33503022471 LIGHT JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27306UE 41020 During preflight inspection, the crew reported that the L/H aft overwing emergency exit light was inoperative. Maintenance personnel removed and replaced the light assembly. An operational check was satisfactory and the aircraft was returned to service. 2L72 4T RTA41NM 20030305000012003030500001 2003 3 5 HEEA084606 420030214A3442MI585200 INDICATOR BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E O OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 WEATHER RADAR WILL NOT PAINT TARGETS/ RF BAND BROKEN. FOUND NO RF TEST BAND AND NO SIGNAL. ADJUSTED LOCAL OSCILLATOR FREQUENCY AND GENERATOR NOISE FILTER. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000042003030500004NE 2003 3 5 HEEA084609 220030214A731402527730006 PUMP BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FUEL SYSTEM LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 FUEL PUMP SEAL LEAKING AT AFCU. POLISHED GEAR SET AND RETESTED UNIT. UNIT TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030305000052003030500005 2003 3 5 HEEA084610 420030214A2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 TRANSCEIVER WEAK. REMOVED CORROSION FROM CHASSIS. ADJUSTED VCO VOLTAGE AND ALIGNED RECEIVER. REPAIRED WEAK RECEIVER. ADJUSTED MIC GAIN, TRANSMIT COMPRESSOR, POWER OUTBACK AND SIDETONE. BENCH CHECK GOOD. 1G72 4U H4SW 20030121001652003012100165SW 2003 1 21 HEEA083319 120030109A2435 SHAFT BELL 206 206L3 1182108SW STARTER GEN SHEARED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 1082 51506 STARTER GENERATOR HAS A SHEARED SHAFT. 1G71 3U H2SW 20030121001682003012100168SW 2003 1 21 HEEA083321 120030109A3212206050248107 FLOAT BELL 206 206B3 1181506SW EMERGENCY FLOAT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032268V 3605 EMERGENCY FLOAT BAG FAILED 6 MONTH INSPECTION (LEAKED). 1G71 3U H2SW 20030121001722003012100172GL 2003 1 21 HEEA083324 220030109A7323 BEARING BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL GOVERNOR DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 20488 51520 N2 RPM INCONSISTENT. GOVERNOR HAD INCONSISTENT OVERSPEED. SPLIT BODIES, CLEANED, AND INSPECTED PARTS. FOUND DEFECTIVE ROLLER BEARINGS ON GOVERNOR LEVER. REPLACED WITH NEW PARTS AND UNIT TESTED SATISFACTORY. 1G71 3U3 U H2SW E1GL 20030121001732003012100173GL 2003 1 21 HEEA083325 220030109A7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 GOVERNOR PRODUCING ERRATIC OPERATION. REPAIRED. 1G71 3U3 U H2SW E1GL 20030121001812003012100181GL 2003 1 21 HEEA083329 220030109A732125490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 N1 HUNG AT 20 PERCENT N1 AND COULD NOT BE INCREASED. SECOND ATTEMPT, START WAS NORMAL. REPAIRED. 1G71 3U3 U H2SW E1GL 20030121001882003012100188SW 2003 1 21 HEEA083334 120030109A28222C271 CARTRIDGE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL FUEL BOOST INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 CARTRIDGE INOPERATIVE. 1G71 3U3 U H2SW E4CE 20030121001942003012100194EU 2003 1 21 MALA030102 120030103A3260 UPLOCK SWITCH SAAB SF340 340B 7860101EU LANDING GEAR ICED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15420XJ 340B420 AFTER TAKEOFF OF FLIGHT 3259, THE LANDING GEAR INTRANSIT LIGHT REMAINED ON. QRH COMPLETED. AIR RETURN TO DTW. MAINTENANCE CLEANED ICE/DEBRIS FROM UPLOCK SWITCH. PERFORMED NUMEROUS GEAR SWINGS IAW MM, ALL CHECKS GOOD. 2L72 4T RTA52EU 20030121002052003012100205SW 2003 1 21 HEEA083349 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0342EA 51542 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121002092003012100209SW 2003 1 21 HEEA083352 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0381671 51301 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121002132003012100213 2003 1 21 HEEA083356 420030109A3442 SWITCH BELL 206 206L3 1182108SW CONTROL HEAD BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038589X 1106 51487 BROKEN TOGGLE SWITCH. FOUND TONE SWITCH S2, VOLUME CONTROL R4/S1, FACEPLATE, VOLUME KNOB AND CHANNEL SELECTOR SWITCH BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030121002152003012100215 2003 1 21 HEEA083357 420030109A3442 SWITCH BELL 206 206L3 1182108SW CONTROL HEAD SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0392MT 1552 51175 ON/OFF TEST SWITCH APPEARS WORN. WIGGLING SWITCH WILL MAKE IT WORK. FOUND CHANNEL KNOB, VOLUME KNOB, SWITCH R4/S1 AND SWITCH S2 BAD. REPLACED. REPAIRED AND BENCH CHECK GOOD. 1G71 3U H2SW 20030121002422003012100242 2003 1 21 MALA030111 420030116A34256226190113 COMPUTER SAAB SF340 340B 7860101EU COCKPIT FAULTY A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15428XJ 340B428 DURING FLIGHT, F/O'S NR 2 EADI GAVE BAD INDICATION. AHARS COMPUTER BAD. AIR RETURN TO MEM. MAINTENANCE REPLACED F/O'S AHRS COMPUTER (AHC-85) WITH SERVICEABLE UNIT IAW SF340 MM 34-21-05-4. OPS CHECKS GOOD IAW AMM 34-21-05. 2L72 4T RTA52EU 20030121002602003012100260NM 2003 1 21 PCAA0301004 120030105A2910 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM LEAKING A PCAAO OTHER K FLUID LOSS DEDESCENT 1 EA13827EX 390 ITH-LGA FLIGHT 3672 CREW REPORTED TOTAL LOSS OF THE NR 2 HYDRAULIC SYSTEM. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND A HYDRAULIC LINE LEAKING UNDER RIGHT NACELLE ACCESS PANEL. LINE WAS REPLACED WITH INTERIM FLEX LINE. ENGINE DRIVEN HYDRAULIC PUMP REPLACED AND UNSCHEDULED INSPECTION OF PUMP PERFORMED. GROUND RUN OF AIRCRAFT PERFORMED, OPERATIONAL AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030121002652003012100265EA 2003 1 21 COMA0360037 120030119A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS DEDESCENT 1 SO01995CA 7229 FLIGHT 5423 FLAPS FAILED AT 9 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2L72 4F RTA21EA 20030121003212003012100321 2003 1 21 HEEA083372 420030109A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 ADI PRECESSES AND WON'T STAY CAGED. REPAIRED. 1G71 3U H2SW 20030307001412003030700141NM 2003 3 7 AALA20030114 120030126A2120 SMOKE BOEING757 757223 1384957NM CABIN DETECTED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21693AA 26973 MIA - FLT 2415 - FLIGHT ATTENDANT REPORTED SMOKE AND BURNING SMELL IN THE VICINITY OF 2L AND R DOORS. LANDED MIA WITHOUT INCIDENT. PERFORMED HIGH POWER RUN-UP, CLOSED AND OPEN AND ISOLATED BLEEDS. NO SMOKE NOTICED OR BURN SMELL OR HOT AIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001422003030700142WP 2003 3 7 AALA20030115 120030124A213121171803 CONTROLLER DOUG DC9 DC982 3022082WP CABIN PRESSURE MALFUNCTIONED A AALAG O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW2190511 49805 DFW - FLT 1035 - EN ROUTE EWR-DFW, CABIN ALTITUDE LIGHT ILLUMINATED AT 35,000 FEET. CABIN PRESSURE WAS CLIMBING. STARTED DESCENT TO LOWER ALTITUDE. TRIED STANDBY. THE MANUAL CONTROL CABIN REACHED 14,000 FEET. MASKS WERE DEPLOYED BY CREW. FINALLY GOT CONTROL OF CABIN WITH MANUAL CONTROLLER. CONTINUED THE FLIGHT WHICH WAS ABOUT 1 HOUR AT 18,000 FEET. IT SEEMED THAT NEITHER OF THE PRIMARY NOR STANDBY AUTO PRESSURIZATION WORKED. BOTH PACKS WORKED. LANDED DFW WITHOUT INCIDENT. REPLACED BOTH NR 1 AND 2 CABIN PRESSURE CONTROLLERS. ACCOMPLISHED ALL REQUIRED LEAK AND OPERATIONS CHECKS. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030307001452003030700145NM 2003 3 7 AALA20030136 120030202A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21669AA 25334 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001472003030700147NM 2003 3 7 AALA20030151 120030125A7722BACC63BR2219PNL CONNECTOR BOEING767 767323 1385205NM COCKPIT LOOSE A AALAK NONE N FALSE WARNING CRCRUISE 1 SW2139356 24037 LEFT EGT INDICATOR EICAS AND STANDBY INDICATOR SLOWLY DROPPED TO 0 6:30 HRS INTO FLIGHT BEGAN WORKING AGAIN 8:00 HRS INTO FLIGHT. CHECKED AND FOUND CP LOOSE. RUN UP NO ANOMALIES NOTED. SYSTEM OK TO CONTINUE. (M) 2L72 4F RTA1NM 20030307001532003030700153EU 2003 3 7 03045308 120030214A3350 SIGN JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27308UE 41023 EMERGENCY EXIT SIGN SEAT 6A INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD 2L72 4T3 TRTA41NM E2WE 20030307001542003030700154EA 2003 3 7 03046662 120030215A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27662BR 7526 EMERGENCY LIGHTING CEILING AISLE LIGHTING, INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030307001572003030700157EA 2003 3 7 03047635 120030216A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27635BR 7295 SERVICE DOOR EMERGENCY EXIT SIDEWALL LIGHT, INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED BULBS. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030307001582003030700158 2003 3 7 HEEA084905 420030228A2200 BEARING SKRSKYS76 S76A 8143006NE ROD END WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 NR 1 YAW ACTUATOR ROD END HAS A WORN BEARING. SCRAPPED DUE TO CORROSION. 1G72 3U H1NE 20030307001612003030700161EA 2003 3 7 03048655 120030217A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27655BR 7457 RIGHT SIDE OVER WING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED OVER WING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2L72 4F4 FRTA21EA E15NE 20030307001642003030700164EA 2003 3 7 COMA0360131 120030303A3010 TERMINAL CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING JN WARNING INDICATION FALSE WARNING CRCRUISE 1 SO01969CA 7141 FLIGHT 5438 ANTI-ICE DUCT WARNING, R/H WING INDICTED.RECONNECTED LOOSE WIRE TERMINAL AT PB8WK. 2L72 4F RTA21EA 20030307001662003030700166EA 2003 3 7 COMA0360132 120030303A27604916405 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAC ABORTED TAKEOFF JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 SO01477CA15262 7670 FLIGHT 5334 SPOILER FAULT STATUS MESSAGE DURING T/O.REPLACED THE SECU. 2L72 4F RTA21EA 20030307001742003030700174NM 2003 3 7 AALA20030062 120030111A2910 B-NUT BOEING757 757223 1384957NM HYD SYSTEM LOOSE A AALAK NONE K FLUID LOSS DEDESCENT 1 SW21688AA 25730 SJU - FLT 633 - LEFT HYDRAULIC SYSTEM FLUID LOSS TO .33. FOUND B-NUT LOOSE ON HYDRAULIC RETURN LINE IN DOG HOUSE AREA FOR NR 1 ENGINE ACCOMPLISHED TORQUE ON B-NUT PER MM. REPLENISHED LEFT HYDRAULIC SYSTEM ACCOMPLISHED LEAK CHECK ON NR 1 ENGINE. NO LEAKS NOTED. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20030307001812003030700181WP 2003 3 7 AALA20030070 120030115A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21400AA 49311 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HEAD STATION 1380 ABOVE LEFT ENGINE STRUT. INSTALLED DOUBLER AT STATION 1380 LEFT SIDE ABOVE ENGINE PYLON PER SRM 53-01-00 PATE 9, 53-30-00-02. (M) 2L72 4F A6WE 20030307001842003030700184WP 2003 3 7 AALA20030073 120030117A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21469AA 49599 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030307001952003030700195NM 2003 3 7 UPS03240256 120030225A5753 PAD BOEING727 727108C 1384039NM #6 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI #6 FLAP TRACK AFT ATTACH POINT LWR PAD ON R/H FALSE SPAR HAVE EVIDEN CE OF CORROSION REMOVED PAD IAW SRM 51-30-02. ON REMOVAL OF CORROAION, CORROSION FOU ND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPLACED PAD IAW SRM 51-30- 02 2L73 4F A3WE 20030121003282003012100328 2003 1 21 HEEA083379 420030109A3421504001790116 INDICATOR BELL 206 206L3 1182108SW HORIZON GYRO PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 HORIZON GYRO PRECESSING. REPAIRED. 1G71 3U H2SW 20030121003292003012100329 2003 1 21 HEEA083380 420030109A34225050031904 INDICATOR BELL 206 206L3 1182108SW DIRECTIONAL GYROMALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 DIRECTIONAL GYRO SPINS IN FLIGHT. 1G71 3U H2SW 20030121003342003012100334GL 2003 1 21 HEEA083386 220030109A72306896888 SCROLL BELL 206 206L1 1182107SW ALLSN 250C 250C* GL COMPRESSOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032759U 45272 COMPRESSOR SCROLL CRACKED AT THE 8 O`CLOCK POSITION. REPLACED SCROLL. 1G71 3U3 U H2SW E4CE 20030121003352003012100335GL 2003 1 21 HEEA083387 220030109A73136899001 FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 ENGINE WOULD NOT LIGHT OFF FOR STARTING. FOUND FUEL FLOW WOULD NOT FLOW THROUGH FUEL NOZZLE. REPAIRED. 1G71 3U3 U H2SW E4CE 20030204002792003020400279NM 2003 2 4 F3LA200300011 120030117A5320 INTERCOSTAL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA 294.5 AND 312, LBL 11, CORRODED. INSTALLED REPLACEMENT PART PER SRM 51-40-2. 2L72 4F RTA16WE 20030122000022003012200002 2003 1 22 HEEA083389 420030109A344280510800001 CONTROL BOX BELL 206 206L3 1182108SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 WEATHER RADAR SYSTEM CONTROL BOX PRODUCING CONSTANT FLICKER ON INDICATOR ANYTIME POWER IS ON. REPAIRED. 1G71 3U H2SW 20030122000032003012200003 2003 1 22 HEEA083390 420030109A344280510800001 CONTROL BOX BELL 206 206L3 1182108SW WX RADAR SYS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 WEATHER RADAR CONTROL BOX IS INTERMITTENTLY INOPERATIVE WITH ERROR CODE 30. REPAIRED. 1G71 3U H2SW 20030122000062003012200006 2003 1 22 HEEA083393 420030109A34578143902240B GPS BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 GPS DATA CARD FAILED ONCE. IN SHOP REPAIR. 1G71 3U H2SW 20030122000072003012200007 2003 1 22 HEEA083394 420030109A34578143902240B GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 GPS MALFUNCTIONED, TROUBLESHOOTING. IN SHOP REPAIR. 1G71 3U H2SW 20030122000092003012200009SW 2003 1 22 HEEA083396 120030109A2820869A6TT CHECK VALVE BELL 206 206L3 1182108SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 POPPET BROKEN IN FUEL SYSTEM CHECK VALVE. SCRAPPED. 1G71 3U H2SW 20030122000142003012200014SW 2003 1 22 HEEA083401 120030109A2432RG222 BATTERY BELL 206 206L1 1182107SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032777D300 45299 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000202003012200020SW 2003 1 22 HEEA083407 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y548 51609 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000212003012200021SW 2003 1 22 HEEA083408 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L349 51529 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000242003012200024SW 2003 1 22 HEEA083411 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS379 51506 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000282003012200028SW 2003 1 22 HEEA083415 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q332 51540 MAIN BATTERY WEAK. 1G71 3U H2SW 20030305000132003030500013NM 2003 3 5 2003UALA00208 120030217A5754114W4220 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 DELAMINATION OF LOWER SKIN ON T/E WEDGE, RIGHT WING. REPAIRED T/E WEDGE, LOWER SKIN, RIGHT WING 2L72 4F4 FRTT0001SE E46NE 20030305000302003030500030NM 2003 3 5 C1HA200397001 120030111A2612 FIRE LOOP BOEING727 727270 138408PNM NR 1 OUT OF POSITION A C1HAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15697CA 23052 FIRE PROTECTION SYSTEM DETECTOR GROUND LIGHT ILLUMINATED ON NR 1. ADJUSTED LOOP AND CLEANED CONNECTOR, OPS CHECKS GOOD. 2L73 4F RTA3WE 20030305000322003030500032NM 2003 3 5 C1HA200397003 120030123A2612 FIRE LOOP BOEING727 727270 138408PNM NR 1 ENGINE MALFUNCTIONED A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15697CA 23052 ENGINE NR 1 FIRE DETECTOR LOOP LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 1 PYLON FIRE LOOP IAW MM 26-14-01, OPS CHECK GOOD. 2L73 4F RTA3WE 20030305000342003030500034SW 2003 3 5 HEEA084616 120030214A3210 BUSHING BELL 407 407 1182206SW MLG BEAM WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033193E 53276 BUSHINGS WORN AND DAMAGED DURING BOLT REMOVAL. SCRAPPED. 1G71 3U O H2SW 20030305000382003030500038SW 2003 3 5 HEEA084620 120030214A3210400052007109 BEAM BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 BEAM ASSY HAS CORROSION BEYOND LIMITS. 1G71 3U O H2SW 20030305000432003030500043 2003 3 5 HEEA084625 420030214A3434066104400 RECEIVER BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 RECEIVER CAUSES MARKER BEACON CIRCUIT BREAKER TO OPEN. REMOVED CORROSION FROM CIRCUIT BOARDS. REPAIRED BURNT FOIL ON POWER SUPPLY BOARD. FOUND UNIT DRAWING EXCESSIVE CURRENT. REPLACED BAD FLEX CABLE AND BAD C209 CAPACITOR. REPAIRED PROBLEM. ADJUSTED HIGH AND LOW SENSE. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000472003030500047 2003 3 5 HEEA084629 420030214A3455066104701 TRANSCEIVER BELL 412 412 1182202SW ADF NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 ADF TRANSCEIVER HAS CONTINUOUS NOISE IN BACKGROUND. REPAIRED. 1G72 4U H4SW 20030305000502003030500050 2003 3 5 HEEA084632 420030214A3451066106901 INDICATOR BELL 412 412 1182202SW INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 DISPLAY IS INOPERATIVE. REPLACED PHOTOCELL, LENS, DISPLAY AND C909 CAPACITOR. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000532003030500053 2003 3 5 HEEA084637 420030214A3452066107100 TRANSPONDER BELL 412 412 1182202SW COCKPIT ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 TRANSPONDER OUTPUT IS ERRATIC ON TEST SET (DIGITS). CLEANED EXCESSIVE CORROSION FROM UNIT. MTL2 TRANSMIT POWER WEAK. ALIGNED RECEIVER AND TRANSMITTER. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000542003030500054 2003 3 5 HEEA084638 420030214A3452066107100 TRANSPONDER BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 TRANSPONDER OUTPUT IS INTERMITTENT. FOUND CORROSION ON Q104, Q501 AND Q502 (ALL TRANSISTORS) AND CHASSIS. CLEANED CORROSION, REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000582003030500058 2003 3 5 HEEA084640 420030214A3452066107100 TRANSPONDER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 TRANSPONDER INOPERATIVE. CLEANED CORROSION FROM UNIT. REPLACED THE INSULATORS AND SPACER ON Q501 TRANSISTOR WHICH WERE DETERIORATED. FOUND MTL AND FREQUENCY OUT OF SPECS. ADJUSTED. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000722003030500072EU 2003 3 5 HEEA084655 120030212A6520112131561 SHAFT BOLKMS105 BO105S 5626006EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037170D S840 TAIL ROTOR SHAFT HAS WORN PLATING. REPAIRED. 1G72 3U H3EU 20030305000782003030500078EU 2003 3 5 HEEA084661 120030213A6230 BEARING AEROSPAS355 AS355* EU M/R SCISSORS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03973AE 3229 MAIN ROTOR SCISSOR LINK HAS WORN BEARINGS. 1G72 3U H11EU 20030305000792003030500079EU 2003 3 5 HEEA084662 120030213A6230350A37112702 BEARING AEROSPAS355 AS355* EU SCISSOR LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03973AE 3229 MAIN ROTOR SCISSOR LINK HAS WORN BEARINGS. 1G72 3U H11EU 20030305000802003030500080EU 2003 3 5 HEEA084663 120030213A3246 CLAMP AEROSPAS355 AS355* EU SKID SHOE BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 DURING TORQUING OF CLAMP ASSY, CLAMP BROKE USING CALIBRATED TORQUE WRENCH. 1G72 3U H11EU 20030305000842003030500084EU 2003 3 5 HEEA084667 120030213A3246350A4110161355 SKID AEROSPAS355 AS355* EU MLG CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034000L 2873 RT SKID TUBE CRACKED. 1G72 3U H11EU 20030307002012003030700201NM 2003 3 7 C1HA200381007 120030212A3350 BULB BOEING727 7272S7 138407ZNM A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15681CA 22020 ON A CHECK FOUND RT OVER WING EXTERIOR EMERGENCY LIGHT MID POSITION INOP.RELAMPED OPS NORMAL. 2L73 4F A3WE 20030307002052003030700205WP 2003 3 7 NACA20030078 120030228A780016121605337943 EXHAUST PIPE PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE CRACKED A NACAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AL03438721095 1095 P32204 44665 P32204 DISCREPANCY: ZONE #1 FIRE WARNING ON #3 ENGINE DURING TAKE OFF ROLL.CORRECTIVE ACTION: REPLACED #10 TO #12 CYLINDER EXHAUST AND #11 TO #13 EXHAUST DUE TO BURN THROUGH. EXHAUST WAS BLOWING ON FIRE DETECTOR. 2L74 4R4 R A781 5E8 20030308000072003030800007SO 2003 3 8 RAIA00302053 120030204A801135059105 STARTER EMB 145 EMB145LR 3260212SO INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03817HK4254 145058 5724-CLT- #1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED #1 ENGINE AIR TURBINE STARTER, OPS CK GOOD. 2L72 4T RTT00011AT 20030310000052003031000005 2003 3 10 HEEA084914 420030227A34221113025 INDICATOR BELL 412 412 1182202SW HSI STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 PILOT HSI YELLOW NEEDLE STICKS. 1G72 4U H4SW 20030310000122003031000012 2003 3 10 HEEA084921 420030227A34571624810 ANTENNA BELL 412 412 1182202SW GPS BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 GPS WILL NOT FIND ITSELF. FOUND ANTENNA BROKEN BEYOND REPAIR. SCRAPPED. 1G72 4U H4SW 20030310000192003031000019SW 2003 3 10 HEEA084928 120030227A6420 BEARING BELL 412 412 1182202SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D7375 A1043 33076 TARGET BLADE BEARING WORN. REPAIRED. 1G72 4U H4SW 20030310000212003031000021SW 2003 3 10 HEEA084930 120030227A5280212030348103 STRUCTURE BELL 412 412 1182202SW NLG DOOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 NLG DOOR STRUCTURE HAS CORROSION. REPAIRED. 1G72 4U H4SW 20030310000272003031000027SW 2003 3 10 HEEA084936 120030227A7120 BEARING BELL 412 412 1182202SW TRIPOD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 ENGINE MOUNT TRIPOD ASSY BEARINGS ARE WORN. SCRAPPED. 1G72 4U H4SW 20030310000382003031000038SW 2003 3 10 HEEA084945 120030227A7120 BEARING BELL 412 412 1182202SW TUBE ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ENGINE MOUNT TUBE ASSY HAS WORN BEARINGS. SCRAPPED. 1G72 4U H4SW 20030310000412003031000041SW 2003 3 10 HEEA084948 120030227A3213212321103 CROSSTUBE BELL 412 412 1182202SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 CROSSTUBE DAMAGED BEYOND LIMITS. SCRAPPED. 1G72 4U H4SW 20030310000492003031000049NE 2003 3 10 HEEA084953 220030227A732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TORQUE SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 TORQUE SPLITS. FOUND PR-PG RESTRICTORS AND SERVO LEVER WORN. REPLACED PARTS. TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030310000532003031000053NE 2003 3 10 HEEA084957 220030227A732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TORQUE SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 TORQUE SPLITS. FOUND LEAKING SERVO VALVES. REPLACED VALVES AND LEVER. TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030310000552003031000055 2003 3 10 HEEA084959 420030227A22114025008918 COMPUTER BELL 412 412 1182202SW AFCS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 AFCS COMPUTER PIN BROKEN ON CONNECTOR "B". 1G72 4U H4SW 20030310000572003031000057 2003 3 10 HEEA084961 420030227A22114025008918 COMPUTER BELL 412 412 1182202SW AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 NR 1 HELIPILOT COMPUTER PITCH HARDOVER. REPAIRED. 1G72 4U H4SW 20030310000582003031000058SW 2003 3 10 HEEA084962 120030227A6220412010216105 BEARING BELL 412 412 1182202SW M/R HEAD ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z8233 36019 MAIN ROTOR HEAD BEARING ROUGH. REPAIRED. 1G72 4U H4SW 20030122000312003012200031SW 2003 1 22 HEEA083418 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671478 51301 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000322003012200032SW 2003 1 22 HEEA083419 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036161A433 51611 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000342003012200034SW 2003 1 22 HEEA083421 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 518 51029 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000362003012200036SW 2003 1 22 HEEA083423 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034282Z379 51499 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000382003012200038 2003 1 22 HEEA083425 420030109A2340AA20030 AMPLIFIER BELL 206 206L1 1182107SW PA SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0320898 45721 PA AMPLIFIER SIREN INOPERATIVE. 1G71 3U H2SW 20030122000402003012200040 2003 1 22 HEEA083427 420030109A2350AMS44 CONTROL MODULE BELL 206 206L3 1182108SW NR 2 COMMS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 COMM NR 2 AUDIO ON RT SIDE IS INTERMITTENT. 1G71 3U H2SW 20030122000412003012200041 2003 1 22 HEEA083428 420030109A2350AMS44 CONTROLLER BELL 206 206L3 1182108SW COMMS SYSTEM WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 RECEPTION WEAK ON ALL STATIONS. BENCH CHECK GOOD. 1G71 3U H2SW 20030122000472003012200047 2003 1 22 HEEA083434 420030109A3423C2300DL4B COMPASS BELL 206 206L3 1182108SW COCKPIT LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 COMPASS LOW ON FLUID. REPLACED. 1G71 3U H2SW 20030122000492003012200049 2003 1 22 HEEA083437 420030109A3140DPUA0101 COMPUTER BELL 206 206L3 1182108SW INTELLASTART PROMALFUNCTIONED E O OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 INTELLASTART PROCESSOR CAUSING INADVERTENT MAINTENANCE LIGHTS TO THE SYSTEM. IN REPAIR. 1G71 3U H2SW 20030122000572003012200057SW 2003 1 22 HEEA083445 120030109A6420LB21010202 BEARING BELL 206 206L3 1182108SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 AFS7751 51074 TAIL ROTOR HEAD BEARING WORN. 1G71 3U H2SW 20030122000592003012200059SW 2003 1 22 HEEA083447 120030109A3297MS24171D1 RELAY BELL 206 206B3 1181506SW MLG INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MLG RELAY INOPERATIVE. SCRAPPED. 1G71 3U H2SW 20030122000612003012200061SW 2003 1 22 HEEA083449 120030109A2497MS24171D1 RELAY BELL 206 206L3 1182108SW MLG STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 MLG RELAY STICKS INTERMITTENTLY. SCRAPPED. 1G71 3U H2SW 20030122000622003012200062SW 2003 1 22 HEEA083450 120030109A2437M450 VOLTMETER BELL 206 206L3 1182108SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671 51301 DIGITAL VOLTMETER NOT WORKING, NO DISPLAY. REPAIRED. 1G71 3U H2SW 20030122000642003012200064SW 2003 1 22 HEEA083452 120030109A3297MS24171D1 RELAY BELL 206 206B3 1181506SW MLG MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MLG RELAY INTERMITTENTLY INOPERATIVE. REPLACED. 1G71 3U H2SW 20030122000672003012200067SW 2003 1 22 HEEA083455 120030109A3212OHSS2061003 COVER BELL 206 206L3 1182108SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 EMERGENCY FLOAT COVER TORN. TO BE SENT TO VENDOR. 1G71 3U H2SW 20030122000702003012200070 2003 1 22 HEEA083458 420030109A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMMS SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 MIXER BOX IS INTERMITTENT AND SCRATCHY. SHOP REPAIR. 1G71 3U H2SW 20030305000882003030500088EU 2003 3 5 HEEA084671 120030213A331055670 LIGHT AEROSPAS355 AS355* EU COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03973AE 3229 CONSOLE LIGHT WON'T DIM. 1G72 3U H11EU 20030305000932003030500093WP 2003 3 5 CALA0300093 120030303A5311 FRAME DOUG DC9 DC982 3022082WP STA 1418 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 INSPECTION FOUND A 3/4" CRACK IN FRAME AT STA 1418, LONGERON 1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 4. 2L72 4F A6WE 20030225000232003022500023SW 2003 2 25 HEEA084242 120030120A5320407070620180 PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030225000282003022500028SW 2003 2 25 HEEA084247 120030120A2510407070620207 STRUCTURE BELL 407 407 1182206SW HAT BIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 HAT BIN STRUCTURE CRACKED. 1G71 3U O H2SW 20030225000302003022500030SW 2003 2 25 HEEA084249 120030120A2510407070620207 STRUCTURE BELL 407 407 1182206SW HAT BIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 HAT BIN STRUCTURE CRACKED. 1G71 3U O H2SW 20030225000332003022500033SW 2003 2 25 HEEA084252 120030120A5320407070620213 TRIM PANEL BELL 407 407 1182206SW INTERIOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 INTERIOR TRIM PANEL CRACKED. 1G71 3U O H2SW 20030225000352003022500035SW 2003 2 25 HEEA084254 120030120A5320407070620217 PANEL BELL 407 407 1182206SW INTERIOR CRACKED E O OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 INTERIOR PANEL CRACKED CRACKED. 1G71 3U O H2SW 20030225000372003022500037SW 2003 2 25 HEEA084256 120030120A2510407070731103 SUPPORT BELL 407 407 1182206SW HEADREST WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 PIN HOLES WORN ON HEADREST CAUSING BINDING. 1G71 3U O H2SW 20030225000402003022500040SW 2003 2 25 HEEA084259 120030120A3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 207 53199 EMERGENCY FLOAT BOTTLE SOLENOID VALVE LEAKS. 1G71 3U O H2SW 20030225000412003022500041SW 2003 2 25 HEEA084260 120030120A3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 211 53398 BOTTLE WILL NOT SERVICE UP FROM EMPTY. LEAKS PASS SEAT ON SOLENOID VALVE. 1G71 3U O H2SW 20030225000452003022500045 2003 2 25 HEEA084264 420030129A34211113034 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 ROLLED OVER IN FLT AND SLOWLY RESET. 1G72 4U H4SW 20030225000492003022500049SW 2003 2 25 HEEA084270 120030129A5246206033111003 DOOR BELL 206 206L3 1182108SW BATTERY UNSECURE E HEEAO OTHER O OTHER LDLANDING 1 SW0341791 51465 BATTERY DOOR OPENED ON APPROACH TO LANDING. DAMAGED BOTH WINDSHIELDS. REPLACED WINDSHIELDS. 1G71 3U H2SW 20030225000502003022500050SW 2003 2 25 HEEA084272 120030211A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T428 28101 MAIN BATTERY WEAK. BATTERY SCRAPPED AT VENDOR 1/17/03. 2G72 4U H10SW 20030225000512003022500051SW 2003 2 25 HEEA084273 120030211A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T604 28101 MAIN BATTERY WEAK. BATTERY SCRAPPED AT VENDOR 1/17/03. 2G72 4U H10SW 20030225000522003022500052SW 2003 2 25 HEEA084274 120030211A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M507 28102 MAIN BATTERY WEAK. BATTERY SCRAPPED AT VENDOR 1/17/03. 2G72 4U H10SW 20030122000792003012200079 2003 1 22 HEEA083471 420030110A3455066104701 TRANSCEIVER BELL 412 412 1182202SW ADF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 ADF TRANSCEIVER INOPERATIVE. IN SHOP REPAIR. 1G72 4U H4SW 20030122000812003012200081 2003 1 22 HEEA083473 420030110A3416066104800 ALTIMETER BELL 412 412 1182202SW COCKPIT UNRELIABLE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ALTIMETER UNRELIABLE. IN SHOP REPAIR. 1G72 4U H4SW 20030122000862003012200086 2003 1 22 HEEA083478 420030110A2312066107800 RECEIVER BELL 412 412 1182202SW GLIDESLOPE WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 VERY WEAK GLIDESLOPE RECEIVER. IN SHOP REPAIR. 1G72 4U H4SW 20030122000892003012200089SW 2003 1 22 HEEA083481 120030110A6230407040011101 MAST BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH4656 53198 MAIN ROTOR MAST HAS DAMAGE IN CONE SEAT AREA. 1G71 3U O H2SW 20030122000912003012200091 2003 1 22 HEEA083483 420030107A2350100005430 HEADSET BOLKMS105 BO105S 5626006EU PAX CABIN DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 PASSENGER HEADSET RT EAR DOES NOT RECEIVE. REPLACED WITH SERVICEABLE HEADSET. 1G72 3U H3EU 20030122000922003012200092EU 2003 1 22 HEEA083484 120030107A6420 BEARING BOLKMS105 BO105S 5626006EU T/R PITCH LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033071K S859 BEARINGS WORN. REPLACED 4 BEARINGS DUE TO WEAR. 1G72 3U H3EU 20030122001132003012200113NM 2003 1 22 DL72S030023 120030104A3350S106 BATTERY BOEING727 727225A 1384077NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO278890Z 21859 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY, CHECKS GOOD. 2L73 4F RTA3WE 20030122001412003012200141EU 2003 1 22 HEEA083501 120030107A6320350A32031000 GEARBOX AEROSPAS355 AS355* EU MAIN ROTOR MAKING METAL E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03971AE1555 3230 CHIP LIGHT ILLUMINATION. METAL FOUND ON LOWER PLUG OF THE MAIN ROTOR GEARBOX. IN SHOP REPAIR. 1G72 3U H11EU 20030122001432003012200143EU 2003 1 22 HEEA083503 120030107A6730SC5083 SERVO AEROSPAS355 AS355* EU MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03974AE1110 2653 SERVO LEAKING FROM OUTPUT SHAFT SEAL. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030314001172003031400117NM 2003 3 14 SWAA030561 120030311A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030314001212003031400121NE 2003 3 14 BTA2003F00000 220030212A7200 ENGINE RKWELLNA265 NA26580 7630108CE GE CF700 CF7002D2 30010NE RIGHT FLAMED OUT E BTAAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 GL23382LS 38051 304368B AIRCRAFT IN FLIGHT AT HIGH ALTITUDE (FL410) AIRCRAFT GOT SLOW (APPROX. 165 KNTS). RIGHT ENGINE FLAMED OUT. ADVISE ATC THAT WE HAD ENGINE PROBLEM AND REQUEST TO GO DOWN TO FL270 TO RESTART ENGINE. DECENDED TO FL270 AND RESTARTED ENGINE. NO OTHER ABNORMALITIES OCCURED DURING BALANCE OF FLIGHT. AFTER AIRCRAFT RETURNED, ENGINE WAS INSPECTED IN INLET, EXHAUST AND ACCESSORY SECTIONS, NO FAULTS FOUND. ENGINE WAS GROUND PERFORMEANCE RAN WITH NO FAULTS FOUND. OK FOR RETURNE TO SERVICE. 2L72 4F4 F A2WE E7EA 20030314001232003031400123CE 2003 3 14 CJP2003F00001 120030120A301026190361 GASKET LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP WING HEAT DUCT FAILED E CJPAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 NM03925DM294 486 FLIGHT CREW AND PASSENGER NOTED BURNING ODOR AND HAZE IN CABIN. AIRCRAFT DIVERTED TO AN ALTERNATE AIRPORT FOR MAINTENANCE. A LEAK WAS FOUND IN BLEED AIR CROSS-OVER DUCT FOR LT WING AND STABILIZER HEAT. A GASKET HAD FAILED ON THE CROSSOVER DUCT CONNECTION TO THE CABIN HEAT DUCT. 2L72 4F4 F A10CE E6WE 20030314001262003031400126CE 2003 3 14 DEL2003F00000 120030202A3610460200 PERISEAL LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP LT PYLON LEAKING E DELAO OTHER O OTHER NRNOT REPORTED 1 CE03273MG 119 LEAKING PERI SEALS (2 EA) IN THE BLEED AIR LINES IN THE LEFT PYLON, CAUSED THE FIRE DETECTION SYSTEM TO ILLUMINATE. 2L72 4F4 F A10CE E6WE 20030314001272003031400127NM 2003 3 14 FX72003F00001 120030215A2730 INDICATOR BOEING727 727224 1384076NM PWA JT8 JT8D17 52049NE ELEV POSITION FAILED A FX7AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19296SC 22449 DURING THE BEFORE TAKEOFF CHECK OF THE ELEVATORS, THE LEFT ELEVATOR POSITION INDICATION FAILED AIRCRAFT RETURNED TO GATE. FLIGHT MECHANIC VERIFIED CORRECT OPERATION OF ELEVATORS IAW MEL 27-10 OF THE DDPG. AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER INCIDENT. 2L73 4F4 F A3WE E2EA 20030314001282003031400128WP 2003 3 14 GTIA030105 120030225A3260 UPLOCK SWITCH DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE RT MLG INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23133NK 48111 RIGHT GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION AND REMAINS ON DURING UPLATCH CHECK AND REMAINDER OF FLIGHT. FOUND WIRE 2G206A24 ON TERMINAL C2 OF RELAY R2-29 (LANDING GEAR LEVER) SHORTED TO GROUND (=240HMS) WITH RT DOWNLOCK SWITCH CP P1-129 DISCONNECTED. REMOVED AND REPLACED RT GEAR UPLIMIT SWITCH. IAW 32-61-00. FOUND PIN (DD) AT CONNECTOR PLUG NR P1-1062 BENT AND SHORTED. REMOVED AND REPLACED PIN (DD) AT PLUG P1-1062 IAWMM 20-50-1. 2L72 4F4 F A6WE E2EA 20030314001462003031400146SO 2003 3 14 N382003F00000 120030224A32331159H202623B ACTUATOR GULSTMG1159 G1159B 3953535SO RROYCESPEY SPEY5118 54523EU NLG CRACKED E N38AO OTHER K FLUID LOSS NRNOT REPORTED 1 EA0595SJ 6650 064 LEAKING ACTUATOR OR LINE CAUSED EXCESSIVE LESS OF COMBINED HYDRAULIC FLUID. FOUND THE END CAP CRACKED APPROXIMATELY .3333 OF THE CAP CIRCUMFERENCE. 2L72 4F4 FRTA12EA E2EU 20030314001542003031400154SO 2003 3 14 RO32003F00000 120030217A2530304316 RIBBON HEATER GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU GALLEY FAILED B RO3RO OTHER O OTHER NRNOT REPORTED 1 CE03460PG 460 DURING AN INSPECTION DISCOVERED MELTED GALLEY DRAIN HEAT TAPE. REMOVED THE DAMAGED HEAT TAPE AND REPLACED. AIRCRAFT WAS INSPECTED FOR PROPER INSTALLATION OF THE EXISTING HEAT TAPE AND MODIFIED AS NECESSARY TO ENSURE PROPER INSTALLATION AND CONTINUED AIRWORTHINESS. 2L72 4F4 F A12EA E2EU 20030314001622003031400162NE 2003 3 14 S2YA03001 220030112A7230 COMPRESSOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE STALLED A S2YAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL13891SK158072 UE89 PCE114171 DURING FLIGHT 1044 MKE-GRB THE CREW REDUCED ENGINE TORQUE TO 2200 LBS. THE FIRST OFFICER OBSERVED FLAME COMING OUT OF FROM THE RIGHT ENGINE. THERE NO INSTRUMENT INDICATION OF ANY ENGINE PROBLEMS. THE CREW SHUT DOWN THE RIGHT ENGINE AS A PRECAUTION, DECLARED AN EMERGENCY AND MEDE AN UNEVENTFUL LANDING IN GRB. MECHANIC INSPECTED THE ENGINE AND FOUND ITS COMPRESSOR WOULD STALL WITH POWER REDUCTION. MECHANIC REPLACED THE COMPRESSOR BLEED VALVE AND SEAT. MECHANIC PERFORMED A BORESCOPE OF THE HOT SECTION AND INSPECTED THE 1ST STAGE COMPRESSOR WITH NO DEFECTS NOTED. THE AIRCRAFT WAS FERRIED BACK TO MKE FOR FURTHER MAINTENANCE. MECHANIC REPLACED THE ENGINE. 2L72 4T4 TRTA24CE E26NE 20030314001682003031400168NM 2003 3 14 USAABB03027 120030302A335086210066 BATTERY BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE ROW 22 DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19604AU 22199 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 22, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2L72 4F4 FRTA2NM A12EU 20030314001692003031400169NM 2003 3 14 USAABB03028 120030301A335096210066 BATTERY BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE ROW 23 DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19628AU 27806 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23, INOPERATIVE. 2L72 4F4 FRTA2NM A12EU 20030314001742003031400174NE 2003 3 14 USAASB03030 220030226A72009325M85G04 ENGINE BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE NR 2 SURGES A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19528AU 24410 AFTER LIFTOFF, CAPTAIN REPORTED THE NR 2 ENGINE RAPIDLY SURGED BACK AND FORTH. APPROXIMATE N1 WAS FROM 77 PERCENT TO 85 PERCENT WITH FUEL FLOW INCREASING TO 8,000 POUNDS AND EGT INCREASING TO 800 DEGREES. CREW PULLED THE NR 2 ENGINE THROTTLE BACK TO IDLE AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND ACCOMPLISHED TAKEOFF POWER CHECK AND ACCEL/DECEL CHECK IAW MM. AIRCRAFT WAS FOUND SAFE FOR MAINTENANCE FERRY FLIGHT TO PIT. ONCE IN PIT, MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSEMBLY. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20030314001782003031400178SW 2003 3 14 WX52003F00000 120030228A3260MS243314 SQUAT SWITCH SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE331* 01514WP LT STRUT INOPERATIVE E WX5AO OTHER O OTHER NRNOT REPORTED 1 SW13158WA5000 TC411 INSUFFICENT FLUID LEVEL INSIDE STRUT HOUSING CREATED (SPONGY) STRUT EXTENSION. DURING RETRACTION WIND LOAD COMPRESSING STRUT GREATER THAN .6250 INCH CLOSING MLG SAFETY SQUAT SWITCH. THUS DISABLING THE RETRACT SEQUENCE, LEAVING THE RIGHT MLG PARTIALLY RETRACTED. SERVICING FLUID AND NITROGEN IN LT STRUT, CURED THE PROBLEM. CHECK STRUT FLUID LEVELS REGULARLY. 2L72 4T3 TRTA8SW E2WE 20030314001822003031400182SO 2003 3 14 000240 120030129A2120 ODOR EMB 145 EMB145 3260210SO COCKPIT DETECTED A CHQAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11260 ON CLIMBOUT AT APPROX 4000CA AND FO NOTICED HOT ODOR. F/A REPORTED CABIN SMOKE; DONNED O2 AND GOOGLES, RECEIVED LAV SMOKE EICAS RETURNED TO SDF. CABIN TEMP REPORTED TO BE WELL ABOVE 100 PERCENT BY FA'S PAX FLOOR BOARDS VERY HOT. ALL OCCURRED AFTER SWITCHING FROM APU BLEED TO ENG BLEEDS. INSPECTED AND FOUND NR 2 PACK TO MALFUNCTIONING PER PACKS OF OF APU AND ENGINE WITH A/I ON AND OFF. WAS UNABLE TO PRODUCE BURNING ODOR OR SMOKE. THERE WAS NO RISE OF CABIN TEMP ALL FLOOR BOARD REMOVED AT CABIN TEMP. 2L72 4F RTT00011AT 20030314001932003031400193NE 2003 3 14 00084 220030228A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE NR 1 FLAMED OUT E HAEAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW05977TW 13 299061 PILOT REPORTED NR 1 ENGINE FLAMEOUT AT FL350, ENGINE RELIT AS N1 DROPPED THROUGH 50 PERCENT, ALL ENGINE INDICATIONS NORMAL, REQUESTED FL310 FOR DURATION OF FLIGHT. ADS MAINTENANCE INSPECTED ENGINE FOUND NO DEFECTS PERFORMED GROUND RUNS, ALL OPS CHECKED NORMAL. 2L72 4F4 F A7EU E7EA 20030314001982003031400198SO 2003 3 14 030002161 120030116A56201159CE2003431 WINDOW GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU CABIN CRACKED B Y3PRK NONE O OTHER ININSP/MAINT 1 SO3596JA 213 OUTER PANE OF CABIN WINDOW WAS FOUND CRACKED .5000 INCHES DURING VISUAL INSPECTION. WINDOW WAS REPLACED. 2L72 4F4 FRTA12EA E2EU 20030314002032003031400203EU 2003 3 14 0300363225 120030304A2150 A/C PACK AIRBUS320 A320211 3930320EU RIGHT ODOR A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL01325US 281 APPROXIMATELY 20 MILES FROM TOUCHDOWN EXPERIENCED A STRONG OIL ODOR IN THE COCKPIT AND CABIN. NO SMOKE WS OBSERVED. FOLLOWED COM PROCEDURES AND LANDED UNEVENTFULLY. INSPECTED ELECTRICAL AND HYDRAULIC COMPARTMENTS, LANDING GEAR WELLS AND FOUND NO EVIDENCE OF SOURCE OF ODOR. ISOLATED ODOR TO RIGHT PACK. APPLIED MEL PROVISIONS FOR INOPERATIVE RIGHT PACK AND RETURNED AIRCRAFT TO SERVICE. AT RON STATION REPLACED RIGHT PACK OZONE CONVERTER AND OPS CHECKED GOOD. CLEARED MEL ITEM. 2L72 4F RTA28NM 20030314002122003031400212NM 2003 3 14 0300426304 120030307A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHTSBROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01664US 23819 DURING LINE CHECK FOUND LEFT SIDE "E" ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RESPLICED WIRE, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030314002132003031400213NM 2003 3 14 0300466312 120030311A3260 PSEU BOEING747 747451 1384940NM NLG FAILED A NWAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL01672US 30267 DURING CLIMB RECEIVED A NOSE "GEAR DISAGREE" AND "GEAR DOOR" EICAS MESSAGE ACCOMPANIED WITH AIRFRAME VIBRATION DURING LANDING GEAR RETRACTION. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE PSEU AND BOTH NOSE WHEEL ASSEMBLIES. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030314002182003031400218EA 2003 3 14 03049669 120030218A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMER EXIT SIGN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 LEFT EMERGENCY EXIT SIGN BULB INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030314002192003031400219EA 2003 3 14 03053655 120030222A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE AFT EMER LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27655BR 7457 AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030314002272003031400227EU 2003 3 14 03064320 120030305A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP EMER TRACK LIGHTLOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27320UE 41043 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE AFT SECTION OF LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20030314002422003031400242EU 2003 3 14 AWXA200300266 120030313A3350ABS0374A24 CABLE AIRBUS320 A320231 3930325EU SEAT ROW 11 R/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW0 0 65 LAS - EEL - DURING INSPECTION THE EMERGENCY PATH LIGHT AT SEAT ROW 11 R/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY PATH LIGHT ASSEMBLY SEAT ROW 11 R/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030316000052003031600005 2003 3 16 RAIA00303062 420030304A3160331EDP12 DISPLAY JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03569HK9150 41088 5540-STL- RIGHT TORQUE INDICATION WENT BLANK. MAINTENANCE REMOVED AND REPLACED ENGINE DISPLAY PANEL, OPS CK OK. 2L72 4T RTA41NM 20030317000052003031700005NM 2003 3 17 03070428 120030311A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAO OTHER L NO TEST TXTAXI/GRND HDL 1 EA27428FJ 3193 DURING TAXI/GROUND HANDLING MAINTENANCE FOUND SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED OPS CHECKED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA55NM 20030317000062003031700006WP 2003 3 17 03FDEA00132 120030214A3230 INDICATOR DOUG DC10 DC1030 3023501WP MLG FALSE ACTIVATIONA FDEAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO25301FE 46800 UPON TAKEOFF FROM ORD, LEFT MAIN GEAR INDICATED UNSAFE ON BOTH PRIMARY AND SECONDARY INDICATIONS AFTER RAISING GEAR HANDLE. RAN CHECK LIST-RECYCLED GEAR DOWN THEN BACK UP- BOTH PRIMARY AND SECONDARY INDICATIONS SHOWED GEAR UP AND LOCKED. CONTINUED TO ANC. UPON APPROACH INTO ANC GEAR EXTENSION WAS NORMAL- GOOD INDICATIONS BOTH PRIMARY AND SECONDARY. ** S/D ** R/R LT MLG RETRACT CYLINDER. 2L73 4F A22WE 20030317000102003031700010NM 2003 3 17 03FDEA00138 120030219A5315 FLOORBEAM BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 CORROSION ON FLOORBEAM LOWER CHORD AROUND NUT PLATE HOLES, BS 1070, RBL 34, WL 200. CORROSION ON 1070 FLOORBEAM WAS OUT OF LIMITS FROM LBL 45 TO RBL 45 WL 200. CUT OUT LWR CHORD AND REPAIRED 1070 FLOORBEAM LOWER CHORD IAW EA 7-5310-68199 AND SRM 53-10-8 FIG 2. 2L73 4F RTA3WE 20030317000112003031700011NM 2003 3 17 03FDEA00141 120030220A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON SHEAR TIE BS 720C NEXT TO STR 26R. REMOVED CORROSION ON SHEAR TIE AT BS 720C NEXT TO STR 26R. FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED FASTENER HOLES IN NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-1, 51-30-2 PART #69-43683-3. 2L73 4F RTA3WE 20030317000232003031700023NM 2003 3 17 03FDEA00156 120030221A5311 FRAME BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 WHILE WORKING CARD FOUND LOWER NOSE FRAME LT SIDE TO BE CORRODED AT BS 296 LBL 20. FOUND LOWER NOSE FRAME LT SIDE TO BE OUT OF LIMITS AT BS 296, LBL 70. REMOVED AND REPLACED LT FRAME IAW SRM 51-20-1, 51-30-7, 51-30-5. 2L73 4F4 F A3WE E2EA 20030317000282003031700028NM 2003 3 17 03FDEA00161 120030218A5712ARB2850506 RIB DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING, FOUND TRACK NR 16 INBOARD STRUCTURAL RIB CRACKED. REMOVED AND REPLACED INBOARD STRUCTURAL RIB IAW SRM 51-31-01 SHT.1 VOL. II. 2L73 4F4 FRTA22WE E13NE 20030317000412003031700041NM 2003 3 17 03FDEA00176 120030225A5310 SHEAR TIE BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 WHILE WORKING N00939, FOUND CRACKED SHEAR TIE AT BS 328, STR 26-27 LEFT. REPAIRED SHEAR TIE BS 328, STR. 26-27 LEFT, IAW SRM 53-10-4 FIG. 15. 2L73 4F4 F A3WE E2EA 20030317000422003031700042NM 2003 3 17 03FDEA00177 120030225A5310 WEB BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON WEB, STA 1174, RBL 18, WL 208. REMOVED CORROSION AT STA 1174. WEB FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-1Q0-1, 51-40-2. 2L73 4F4 F A3WE E2EA 20030317000432003031700043NM 2003 3 17 03FDEA00178 120030226A2150 A/C PACK BOEING727 7272S2F 1384O81NM PWA JT8 JT8D17 52049NE CABIN CONTAMINATED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25208FE 22930 5 MIN. AFTER T/O R/PACK OVERHEAT LIGHT ILLUM'D. PACK COOLING FLAP SELECTOR IN AUTO. PACK TEMP APPROX. 180 DEG. ,SHUT DOWN PACK, TEMP DECREASED. FOLLOWED BY NR 6 MAIN SMOKE CARGO LIGHT AND FIRE WARN GLARESHIELD LIGHTS. HORN ILLUMINATED, FOLLOWED BY NR4 THEN NR5 CARGO SMOKE LIGHTS. DONED O2 MASK, CONTINUED. DEPRESSURIZED A/C, MAIN CARGO DOOR LIGHT ILLUM. BETWEEN 2000 AND 3000 FT. MSL. CLOSED WING AI AND LIGHT EXTINGUISHED SHORTLY THERE AFTER. REMOVED AND REPLACED WATER SEPARATOR (BAG) NO SMOKE OR ODOR. INSPECT MAIN CARGO SMOKE DET SYS. COULD NOT DUPLICATE. FOUND PROBLEM TO BE DEICE FLUID FILLING COMPARTMENT THRU PACKS. AFTER BAG REMOVED AND REPLACED COULD NOT DUP PROBLEM. CHECK MAIN CARGO DOOR AS REQUIRED .2L73 4F4 F A3WE E2EA 20030317000492003031700049NM 2003 3 17 03FDEA00185 120030227A5270 PROXIMITY SWITCHBOEING BOEING727 727233 138408ANM PWA JT8 JT8D NE MAIN CARGO DOOR INOPERATIVE A FDEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO25268FE 0107 21674 INTERMITTENT MAIN CARGO DOOR LIGHT IN FLIGHT, RED CARGO LIGHT BY DOOR OPEN SWITCH, MAX CABIN PRESSURE WAS 6.0 AT 15000 FT. ADJUSTED MAIN CARGO DOOR PROXIMITY SWITCHES IAW FED EX MM 52-34-009-5 STEPS 1E, 5F FUNCTIONAL TESTED GOOD IAW STEP 3E. 2L73 4F4 FRTA3WE E2EA 20030317000562003031700056NM 2003 3 17 SWAA030575 120030312A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND CONNECT DOOR FWD RH. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030225000542003022500054SW 2003 2 25 HEEA084276 120030211A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T238 28101 MAIN BATTERY WEAK. 2G72 4U H10SW 20030225000592003022500059SW 2003 2 25 HEEA084281 120030211A6710206001053005 BEARING BELL 206 206L1 1182107SW BELLCRANK WORN E O OTHER O OTHER NRNOT REPORTED 1 SW035014Y 45219 MAIN ROTOR FLT CONTROL BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS. REPAIRED. 1G71 3U H2SW 20030225000742003022500074NM 2003 2 25 159PL0027 120030224A33501000679 LIGHT BOEING737 737242 1384477NM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05195PL 21186 L2 door ovhd emergency light dim. Removed and replaced emergency exit unit M187 per MM 33-51-0. Ops. chk. good. 2L72 4F A16WE 20030225000752003022500075WP 2003 2 25 DHL2003805003 120030222A2611 BULB DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01805DH 46125 1) #6 AND #8 SMOKE DETECTORS DO NOT TEST.2) SMOKE DETECTORS #6 AND #8 DEFERRED INOPERATIVE PER MEL 26-6-1 DMI #12078.3) REF. DMI #12078 SMOKE DETECTOR #6 AND #8 INOPERATIVE "DO NOT TEST".4) REMOVED AND REPLACED #6 AND #8 SMOKE DETECTOR LIGHT BULBS. OPS CHECKED GOOD PER M/M 26-10-6. CLEARS DMI #12078. 2L74 4F RT4A25 20030225000772003022500077NM 2003 2 25 159PL0028 120030224A3350900835A BATTERY PACK BOEING737 737242 1384477NM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05159PL 21186 Ovhd center aisle emergency light capacity low. Removed and replaced emergency light battery pack on unit M192 per MM 33-51-0. Ops chk. good. 2L72 4F A16WE 20030225000792003022500079SW 2003 2 25 HEEA084294 120030211A6520407310203101 MOUNT BELL 407 407 1182206SW TAIL ROTOR HEAD SEPARATED E O OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 TAIL ROTOR GEARBOX MOUNT SEPARATED BEYOND LIMITS. 1G71 3U O H2SW 20030225000812003022500081SW 2003 2 25 HEEA084295 120030211A6330407310203101 MOUNT BELL 407 407 1182206SW GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 RT REAR MAIN ROTOR GEARBOX MOUNT IS WORN. 1G71 3U O H2SW 20030225000862003022500086SW 2003 2 25 HEEA084300 120030211A6321 PAD BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 322 53207 ROTOR BRAKE CALIPER WORN PADS. REPAIRED. 1G71 3U O H2SW 20030225000912003022500091SW 2003 2 25 HEEA084304 120030211A6510407340339101 BEARING BELL 407 407 1182206SW T/R DRIVESHAFT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 TAIL ROTOR DRIVESHAFT HANGER BEARING GREASE TURNED BLACK. 1G71 3U O H2SW 20030225000942003022500094EA 2003 2 25 COMA0360117 120030222A3010 ELEMENT CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01815CA 7397 FLIGHT 9959 ANTI ICE DUCT WARNING MESSAGE.FOUND DUCT LEAK SENSING ELEMENT POSITIONED TO CLOSE TO BLEED AIR DUCT. REPOSITIONED ELEMENT. 2L72 4F RTA21EA 20030225000952003022500095EA 2003 2 25 COMA0360118 120030223A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01959CA 7116 FLIGHT 5616 CABIN DOOR WARNING DURING FLIGHT.COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR WAS NORMAL. 2L72 4F RTA21EA 20030226000012003022600001 2003 2 26 ALGA084683 420030221A83006893672 PINION GEAR BELL 407 407 1182206SW ENGINE G/B BROKEN H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01477AL1223 CAG47121 53203 FOUND PINION GEARS HAD BROKEN GEAR TEETH CAUSING MASSIVE METAL IN OIL. THIS IS A REOCCURRING EVENT. 1G71 3U O H2SW 20030226000022003022600002 2003 2 26 ALGA084684 420030221A830023066678 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL ACCESSORY G/B SPALLED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01477AL1223 CAG47121 53203 CAE847243 FOUND #3 BEARING SEPARATOR MISSING. BEARING FAILURE CAUSED METAL IN OIL. 1G71 3U3 UO H2SW E1GL 20030226000032003022600003 2003 2 26 ALGA084685 420030221A830023066678 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL ACCESSORY G/B SPALLED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01477AL1223 CAG47121 53203 CAE847243 FOUND NR 4 BEARING SEPARATOR BROKEN IN PIECES. BEARING FAILURE CAUSED METAL IN OIL. 1G71 3U3 UO H2SW E1GL 20030226000112003022600011SW 2003 2 26 HEEA084309 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030317000582003031700058NM 2003 3 17 SWAA030577 120030311A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 520, BETWEEN STR 12R & STR 13R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030317000742003031700074NM 2003 3 17 03FDEA00234 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR30L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000822003031700082NM 2003 3 17 03FDEA00243 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 1R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000932003031700093NM 2003 3 17 03FDEA00254 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 14R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000952003031700095NM 2003 3 17 03FDEA00256 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 16R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000972003031700097NM 2003 3 17 03FDEA00258 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 18R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F RTA22WE 20030317000982003031700098NM 2003 3 17 03FDEA00259 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 19R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F RTA22WE 20030317001112003031700111NM 2003 3 17 03FDEA00270 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 30R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001122003031700112NM 2003 3 17 03FDEA00271 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 31R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001182003031700118NM 2003 3 17 03FDEA00277 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 5R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F RTA22WE 20030317001222003031700122EU 2003 3 17 03FDEA00281 120030220A5280A52810150000J2 STRUCTURE AIRBUS310 A310 EU MLG DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 MLG DOOR, SKIN HAS CORROSION. REMOVED WITHIN LIMITS CORROSION IAW/SRM 51-74-10 ON OUTER SKIN INNER SURFACE. DOOR SKIN OUT OF LIMITS REPAIRED ON E.A.6-5281-6871.RESTORED DOOR IAW/SRM 51-40- 21 PREPPED AND PAINTED IAW/SRM 51-21-50. 2L72 4F RTA35EU 20030317001252003031700125WP 2003 3 17 03FDEA00283 120030307A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 RIGHT WING NR 3 FUEL TANK HAS A CRACKED RIB (APPOX. 5 INCHES LONG) INSIDE TANK PLATE NR 634 AT STATION XORS 402, ALONG LARGE OVAL FLAPPER CHECK VALVE. REMOVED FLIPPER DOOR FOR ACCESS IAW SRM 51-31-01, REMOVED FLIPPER DOOR HINGE IAW SRM 51-35-01, REMOVED STIFFENER IAW SRM.51-31-01. TRIMED CRACK AND CUT-OUT HOLE IAW SRM 51-31-01. FAB DOUBLER IAW SRM 52-20-00 FIG 33. OUT OF 7075-T6FAB DOUBLER ON TRAVELER T2/319454. NDT CRACK AND REINSTALLED DOUBLER IAW SRM 51-31-01. INSTALLED STIFFENER IAW SRM 51-31-01. INSTALLED FLIPPER DOOR HINGE IAW SRM 51-31-01. INSTALLED FLIPPER DOOR IAW SRM 51- 31-01. 2L73 4F A22WE 20030625001282003062500128WP 2003 6 25 03FDEA00285 120030307A2810ARB21762 FITTING DOUG DC10 DC1010 3022110WP WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 N 831 DURING ROUTINE INSPECTION ON W/C 28C1501-02, ON THE LT WING JUST INSIDE TANK PLATE 534 AT, STA. XORS 402 SPAR STATION S-37 FOUND A CRACKED SPAR TO RIB FITTING TO BE WORKED AT MAE, UNDER W/O 13338. REPLACED FITTING IAW SRM ON SNRM N00831, W/O 13338 AT MAE. 2L73 4F A22WE 20030317001282003031700128NM 2003 3 17 03FDEA00288 120030307A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLOOR SUPPORT UNDER NUTPLATE BS 1165-1166, LBL 7, WL 155. REMOVED CORROSION ON FLOOR SUPPORT UNDER NUT PLATE BS 1165-1166, LBL 7, WL 155. AN AREA OF 1 X 2 INCHES. ORIGINAL THICKNESS .063 INCH. REMAINING .050 INCH OUT OF LIMITS PER SRM 53- 10-1. REMOVED FLOOR SUPPORT BS 1166-1155. FABRICATED REPAIR PARTS PER SRM 53-10- 5 & SR 27-53-039. ALODINED & PRIMED PER SRM 51-10-2. INSTALLED PARTS PER SRM 51-30-2. 2L73 4F RTA3WE 20030625001262003062500126NM 2003 6 25 03FDEA00291 120030303A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING O/B FLAP I/B HINGE (FLAP SIDE) O/B LUG HOLE CORRODED. LEFT O/B FLAP- I/B HINGE AFT SUPPORT BORE CORROSION REMOVED AND BUSHING REPAIRED AS PER FEDEX EA 1-5750-68586. 2L73 4F RTA22WE 20030226000182003022600018CE 2003 2 26 GLBA2003024 120030225A5200MS27039116 BOLT BEECH 1900 1900D 1154162CE A GLBAK NONE O OTHER TXTAXI/GRND HDL 1 NM03220GL UE220 CABIN DOOR INNER HANDLE LOOSE, R&R BOLTS OPS CHECK GOOD 2L72 4T RTA24CE 20030226000222003022600022SW 2003 2 26 HEEA084315 120030211A3212407350301101 FLOAT BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 LT FLOAT BAG LOSES PRESSURE. 1G71 3U O H2SW 20030226000262003022600026EU 2003 2 26 MALA030168 120030222A77306222550AM1 ACCELEROMETER BAC 146 AVRO146RJ85A1500097EU A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15508XJ E2318 DURING FLIGHT #3460, #2 ENGINE SHUT DOWN MANUALLY INFLIGHT DUE TO EXCESSIVE VIBRATION INDICATOR. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED ACCELEROMETER PN 62225-50AM1, SN/OFF 11802, SN/ON 10998. IAW AMM 77-32-01 201. 2H74 4F RTA49EU 20030226000302003022600030SW 2003 2 26 HEEA084320 120030211A2842407362005103 SWITCH BELL 407 407 1182206SW FUEL LOW MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 LOW FUEL WARNING LIGHT ON WITH 300 LBS OF FUEL ABOARD. 1G71 3U O H2SW 20030226000322003022600032NM 2003 2 26 2003UALA00184 120030217A5330 BULKHEAD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29368UA 24537 FWD SURFACE OF AFT PRESSURE BULKHEAD BS 1016, SKIN IS WORN AT EDGE APPROXIMATELY THREE THIRTY POSITION OF CUTOUT FOR APU PNEUMATIC BLEED AIR DUCT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030625001102003062500110NM 2003 6 25 F3LA200300092 120030226A5320 WEB BOEING737 7372Y5 1384554NM FUSELAGEW CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED LOWER WEB FROM LAVATORY FLOOR TO FUSELAGE ON LT. SIDE OF FUSELAGE CORRODED AROUND CUTOUTS, STA. 277 TO STA. 294.5. FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-10-01, 51-40-02 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030226000372003022600037SW 2003 2 26 HEEA084326 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 FUEL CELL PRESSURE SWITCH MALFUCTIONED, LIGHT DOES NOT ILLUMINATE. TO BE SENT TO BELL HELICOPTER FOR CREDIT. 1G71 3U O H2SW 20030226000432003022600043SW 2003 2 26 HEEA084332 120030211A7722407375001105 INDICATOR BELL 407 407 1182206SW MGT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 MGT INDICATOR INTERMITTENT, TEMPERATURE DROPS 400 DEGREES THEN BACK TO NORMAL OPERATION. 1G71 3U O H2SW 20030226000462003022600046SW 2003 2 26 HEEA084335 120030211A7714407375002103 INDICATOR BELL 407 407 1182206SW ENGINE NG MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 NG RISES SMOOTHLY AND THEN BEGINS FLUCTUATING. REPLACED NG INDICATOR. 1G71 3U O H2SW 20030226000472003022600047SW 2003 2 26 HEEA084336 120030211A7712407375003107 INDICATOR BELL 407 407 1182206SW ENGINE TORQUE ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 ENGINE TORQUE INDICATOR HAS ERRATIC OPERATION. 1G71 3U O H2SW 20030226000482003022600048SW 2003 2 26 HEEA084337 120030211A7712407375003107 INDICATOR BELL 407 407 1182206SW ENGINE TORQUE FAILED E O OTHER S AFFECT SYSTEMS CRCRUISE 1 SW03447PH 53114 ENGINE TORQUE INDICATOR WENT TO ZERO IN CRUISE FLIGHT. 1G71 3U O H2SW 20030226000522003022600052SW 2003 2 26 HEEA084341 120030211A6340407375005101 INDICATOR BELL 407 407 1182206SW GEARBOX OIL TEMPDAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 MAIN ROTOR GEARBOX OIL TEMP AND PRESSURE INDICATOR BACKLIGHT INOPERATIVE. 1G71 3U O H2SW 20030226000552003022600055SW 2003 2 26 HEEA084344 120030211A6340407375005101 INDICATOR BELL 407 407 1182206SW GEARBOX OIL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 TEMP FLUCTUATING TO FULL SCALE AND BACK WHILE ALSO HAVING SEVERAL SEGMENTS NOT ILLUMINATING. ANNUNCIATOR PANEL TEMP WARNING LIGHT DID NOT ILLUMINATE. 1G71 3U O H2SW 20030226000572003022600057SW 2003 2 26 HEEA084346 120030211A7332407375007105 INDICATOR BELL 407 407 1182206SW FUEL PRESSURE INACCURATE E O OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 FUEL PRESSURE INDICATES PROPERLY BUT LIGHT BARS ABOVE INDICATED PRESSURE OCCASSIONALLY FLICKERS ON DIMLY. 1G71 3U O H2SW 20030226000582003022600058SW 2003 2 26 HEEA084347 120030211A6340407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 DUAL TACH INDICATOR INTERMITTENT FAILED. 1G71 3U O H2SW 20030317001312003031700131NM 2003 3 17 03FDEA00294 120030303A5753 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING O/B FLAP O/B HINGE I/B LUG HOLE (FLAP SIDE) CORRODED. 2L73 4F RTA22WE 20030317001402003031700140NM 2003 3 17 03FDEA00304 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 660 STR 24R. 2L73 4F RTA3WE 20030317001532003031700153WP 2003 3 17 03FDEA00317 120030314A5710ARB1818 RIB DOUG DC10 DC1010 3022110WP NR 6 SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 LT WING NR 6 SLAT OUTBOARD RIB REPAIR AT XOS=889.0, PN ABR 1818. 2L73 4F A22WE 20030317001552003031700155NM 2003 3 17 UPS03240289 120030219A5310 FITTING BOEING727 727108C 1384039NM BS 870 L/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI L/H 870 FITTING HAS 2 CRACKS FWD OF CENT. LINE IN 1ST ROW OF FASTENE RS (HOLES 3 & 4) AND 1 CRACK IN AFT OF BUTT LINE 1ST ROW 3RD FASTENE R FROM TOP FITTING REPLACEMENT CARRIED OUT IAW UPS EO B727-5310-3056 APPENDIX E 2L73 4F A3WE 20030317001632003031700163CE 2003 3 17 048276 120030227A32601143610441 DOWNLOCK SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG FAILED A AMWAO OTHER N FALSE WARNING LDLANDING 1 CE07174YV UE174 UPON LANDING OF FLIGHT 5549 INTO MESSINA NEW YORK, THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR. THE CREW MADE SEVERAL ATTEMPS AND THEN LANDED AT THEIR DESTINATION WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SQUAT SWITCH. NO TEARDOWN REPORT WILL BE AVAILABLE. 2L72 4T3 TRTA24CE E2NE 20030317001672003031700167NM 2003 3 17 AWXA200300279 120030227A5312651758351 ANGLE BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW0 0 24633 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1 3/8" CRACK WAS FOUND ON FORWARD TEE CHORD, AFT SIDE OF BS 178 BULKHEAD WEB, LBL 5.7, WL 184. MAINTENANCE CUTOUT DAMAGED AREA OF FORWARD TEE CHORD, LBL 5.7, WL 184, BS 178; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 4 EACH REPAIR ANGLES, 2 EACH RADIUS BLOCKS, AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG. 221-240, FIG. 205. 2L72 4F RTA16WE 20030317001692003031700169EU 2003 3 17 DHL2003367511 120030222A7110 DOUBLER AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 517513 #1 eng. L/H core cowl aft ctr. inside doubler has depth wear on doubler. Corrective action:Removed worn doubler fabricatednew doubler IAW A300 SRM 54-00-00 primed new doubler IAW A300 SRM 51-40-12,installed new doubler IAW A300SRM 51-40-21. Removed an replaced #1 eng. outboard core cowl IAW A300 mm 71-13-01 2L72 4F4 FRTA35EU E23EA 20030318000072003031800007GL 2003 3 18 ALGA085090 220030305A725023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL TURBINE GOUGED H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO FOUND N1 COUPLING INTERNAL SPLINES CHIPPED/GOUGED AND O.D. RUSTED. 1Q71 3R3 U 2A6 E1GL 20030318000132003031800013EU 2003 3 18 BAQA084837 120030227A6240117945641 INDICATOR BOLKMS117 BK117A3 5626015EU MAST MOMENT WILL NOT TEST H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01932CJ30 7024 MAST MOMENT INDICATOR WILL NOT TEST PROPERLY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030318000202003031800020EU 2003 3 18 BAQA085093 120030305A62401179405303 INDICATOR BOLKMS117 BK117A1 5626010EU TRIPLE TACH INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME383 7243 TRIPLE TACH INDICATOR FOR NR 1 ENGINE NR 2 NEEDLE IS FLUCTUATUING BACK AND FORTH WITH JUST POWER TURN ON. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030318000252003031800025NE 2003 3 18 ERAA085143 120030212A62106117020201067 BLADE SKRSKYS61 S61N 8142104NE MAIN ROTOR LOW H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01562EH8724 61257 VBIM INDICATING LOW PRESSURE . PRESSURE CHECKED AT 2.8 PSI AT 20 DEGREE C. SENT TO CTI FOR REPAIR. INSPECTED PER SRM SA 4045-31E CHAPTER / SECTION 65-10-01 REV 5. PERFORMED 2 DAY CHECK PER SER 50908. REPLACED BIM TRANSDUCER TRANSDUCER AND REINSTALLED BIM; RECHARGED SPAR PER S-61N MM SA4045-80 REV. MARCH 1, 1978 AT TT 8723.6. ALL REPAIRS WERE PERFORMED UTILIZING DESIGNED, PROCESS SPECIFICATION, DRAWINGS, MANUALS OR OTHER MEDIA SUPLIED BY THE MANUFACTURE. PERTINENT DETAILS TO THE INSPECTION, ALTERATION AND REPAIRS ARE ON FILE AT CTI REPAIR STATION. 2G72 4U 1H15 20030318000282003031800028EU 2003 3 18 ERAA085146 120030213A299710545039 WIRE BOLKMS105 BO105S 5626006EU DUAL HYDRAULIC BROKEN A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03124EH2939 S559 GUIDE ASSY HAS BROKEN WIRE. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET AND TESTED & POTTED. INSTALLED NEW FLAT SPRING & SLIDE BLOCK. REPAIRED IAW M BB-BO-105-REM 405. 1G72 3U H3EU 20030318000302003031800030EU 2003 3 18 ERAA085148 120030213A2997 WIRE BOLKMS105 BO105S 5626006EU DUAL HYDRAULIC BROKEN H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01124EH2939 S559 GUIDE ASSY WILL NOT RESET. FOUND BROKEN WIRE. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET AND POTTED AND TESTED. INSTALLED NEW SOCKET AND FLAT SPRING. REPAIRED IAW MBB-BO-105 REM 405. 1G72 3U H3EU 20030318000322003031800032EU 2003 3 18 ERAA085156 120030213A3212D24762102 FLOAT BOLKMS105 BO105S 5626006EU MLG LEAKING H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01298EH1066 S845 FLOAT BAG LEAKS. FLOAT WAS REPAIRED AND C/W ON INSPECTION. TEST BO105 25-60-95 1G72 3U H3EU 20030318000382003031800038SO 2003 3 18 000246 120030314A3240 SHUTOFF VALVE EMB 145 EMB145 3260210SO BRAKE ASSY FAILED A CHQAK NONE J WARNING INDICATION APAPPROACH 1 GL11262 BRAKE OUTBOARD INOPERATIVE MSG ON APP. FOLLOWED POH. NO FIX. DECLARED EMERGENCY FOR LANDING. TRIED BRAKES THEY SEEMED OK. A/C TAXIED TO TERMINAL WITH NO PROBLEMS. RR'D BRAKE CONTROL SHUTOFF VALVE 2L72 4F RTT00011AT 20030226000622003022600062SW 2003 2 26 HEEA084350 120030211A7697407375012101 WIRE HARNESS BELL 407 407 1182206SW FADEC SYS SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 FADEC INTERFACE HARNESS FROM ECU TO FIREWALL OPEN AT PINS 66 & 77 CONNECTOR. 1G71 3U O H2SW 20030226000642003022600064SW 2003 2 26 HEEA084352 120030211A7697407375012101 WIRE HARNESS BELL 407 407 1182206SW FADEC TO ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 SUSPECT CABLE TO BE FAULTY. AIRCRAFT HAD A FADEC FAILURE AND REVERTED TO MANUAL WITH A POSSIBLE TURBINE OVERSPEED. 1G71 3U O H2SW 20030226000692003022600069SW 2003 2 26 HEEA084356 120030211A2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL QTY SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 SIGNAL COND UNIT MALFUNCTIONED, LOW LEVEL LIGHT INOPERATIVE. 1G71 3U O H2SW 20030227000062003022700006SW 2003 2 27 HEEA084363 120030211A6710407375038101 PANEL BELL 407 407 1182206SW COLLECTIVE STICKBROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 START SWITCH LIGHTED PANEL ON COLLECTIVE STICK BROKEN. 1G71 3U O H2SW 20030227000072003022700007SW 2003 2 27 HEEA084364 120030211A6710407375038101 PANEL BELL 407 407 1182206SW COLLECTIVE STICKCRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 LIGHTED PANEL ON COLLECTIVE STICK CRACKED ALONG EDGE AND PIECE IS MISSING. 1G71 3U O H2SW 20030227000352003022700035SW 2003 2 27 HEEA084373 120030211A3340A490ATSDF1428 POWER SUPPLY BELL 407 407 1182206SW ANTI COLLISION FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 ANTI COLLISION LIGHT INOPERATIVE. POWER SUPPLY FAILED. 1G71 3U O H2SW 20030227000812003022700081 2003 2 27 HEEA084387 420030212A3120 LIGHT BELL 407 407 1182206SW CLOCK INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 02048 53323 CLOCK INTERNAL LIGHT INOPERATIVE. 1G71 3U O H2SW 20030227000862003022700086SW 2003 2 27 HEEA084393 120030212A6510 BEARING BELL 407 407 1182206SW BLOWER ASSY VIBRATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH PHI0019 53199 AFT BEARING HAS VIBRATION. REPAIRED. 1G71 3U O H2SW 20030227000882003022700088SW 2003 2 27 HEEA084394 120030212A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 BLOWER ASSY SHAFT SPLINES ARE WORN BEYOND LIMITS. REPAIRED. 1G71 3U O H2SW 20030227000962003022700096SW 2003 2 27 HEEA084402 120030212A2140S9242EC2 SHROUD BELL 407 407 1182206SW HEATER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 EXCESSIVE CRACKING IN LEXAN SHROUD. 1G71 3U O H2SW 20030227001092003022700109SW 2003 2 27 HEEA084415 120030212A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M335 28102 MAIN BATTERY WEAK. 2G72 4U H10SW 20030227001102003022700110SW 2003 2 27 HEEA084416 120030212A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M430 28102 MAIN BATTERY WEAK. 2G72 4U H10SW 20030227001132003022700113SW 2003 2 27 HEEA084419 120030212A6700 BEARING BELL 222 222U 1182140SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 ROUGH BEARINGS. REPLACED BEARING MS276434 AND MS276475 DUE TO WORN. REPAIRED. 1G72 3U H9SW 20030227001212003022700121 2003 2 27 HEEA084427 420030213A34570110005400 GPS BELL 206 206B3 1181506SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03103PH 3000 TAKES MORE THAN 30 MINUTES TO POWER UP. 1G71 3U H2SW 20030227001222003022700122 2003 2 27 HEEA084428 420030213A34570110050400 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 51029 GPS LOSES SIGNAL. 1G71 3U H2SW 20030227001232003022700123 2003 2 27 HEEA084429 420030213A34570110050400 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 51029 GPS CURSOR WILL NOT COME ON IN TCAS MODE. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030227001312003022700131SW 2003 2 27 HEEA084437 120030213A6710206010470101 BEARING BELL 206 206L3 1182108SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038587X 51464 CYCLIC CONTROL BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS DUE TO BEING WORN. REPAIRED. 1G71 3U H2SW 20030227001352003022700135EU 2003 2 27 AWXA200300208 120030226A3350ABS0374A24 CABLE AIRBUS320 A320232 3930326EU SEAT ROW 3 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW0 0 584 PHX - EEL - DURING INSPECTION A BROKEN WIRE WAS FOUND ON EMERGENCY ESCAPE PATH LIGHT SEAT ROW 3 L/H. MAINTENANCE REPAIRED THE BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT SEAT ROW 3 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030228000042003022800004SW 2003 2 28 HEEA084441 120030213A6230206010803101 BUSHING BELL 206 206L3 1182108SW IDLER LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 WORN BUSHINGS. REPLACED 8 BUSHINGS DUE TO BEING WORN. REPAIRED. 1G71 3U H2SW 20030228000192003022800019NM 2003 2 28 SWAA030403 120030218A5330589337 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON CO-PILOT'S UPPER WINDOW POST. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030228000202003022800020NM 2003 2 28 SWAA030388 120030218A5330589337 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON CAPTAINS UPPER WINDOW POST. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030228000212003022800021NM 2003 2 28 SWAA030390 120030217A5710654544555 RIB BOEING737 7373H4 1384600NM RH WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED 1/4D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S2R & S3R. REPAIRED RIB PER SWA EA. 2L72 4F RTA16WE 20030228000282003022800028NM 2003 2 28 SWAA030405 120030220A523065C31308 DOOR FRAME BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492, AT NR 1 STOP FITTING. REPAIRED FRAME PER SWA T1. 2L72 4F RTA16WE 20030228000432003022800043NM 2003 2 28 CALA0300075 120030226A5230 SKIN BOEING737 737824 13844BZNM AFT CARGO DR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912216 28776 A WALKAROUND INSPECTION FOUND THE FORWARD CARGO DOOR DENTED AT STA 474. THE DENT WAS LOCATED 14.5 INCHES FORWARD OF AFT EDGE OF DOOR. THE AREA WAS REPAIRED IAW EA 5231-01039. 2L72 4F RTA16WE 20030228000442003022800044SW 2003 2 28 HEEA084450 120030213A6320357950110932 SHAFT BELL 206 206L3 1182108SW OIL PUMP LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0354641 51184 MAIN ROTOR GEARBOX OIL PUMP IS LEAKING. REPLACED SHAFT 357950110932 DUE TO WEAR ON SEAL RIDE. REPAIRED. 1G71 3U H2SW 20030228000512003022800051SW 2003 2 28 HEEA084452 120030213A6310 SEAL BELL 206 206L3 1182108SW FREEWHEEL UNIT LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW034835 9162 B46286 51131 MAIN ROTOR FREEWHEEL UNIT FORWARD SEAL LEAKING. IN SHOP FOR REPAIR. 1G71 3U H2SW 20030228000542003022800054WP 2003 2 28 MWEA030113 120030227A53205936034502 ANGLE DOUG DC9 DC981 3022081WP STA 993 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 RIGHT WHEEL WELL SUPPORT ANGLE ON LONGERON 20 RIGHT IS CRACKED AT STATION 993. -- FABRICATED AND INSTALLED REPAIR ANGLES, DRILLED AND TRIMMED AND INSTALLED DOUBLERS. 2L72 4F A6WE 20030228000552003022800055WP 2003 2 28 MWEA030119 120030227A531359364369 LONGERON DOUG DC9 DC981 3022081WP STA 1309 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LONGERON 13 CRACKED AT STATION 1309. -- LOCATED, DRILLED AND INSTALLED LONGERON SECTION AND INSTALLED SHOVEL CLIP, LOCATED AND DRILLED REPAIR SPLICE. 2L72 4F A6WE 20030228000722003022800072SW 2003 2 28 HEEA084453 120030213A6310206040270101 SUPPORT BELL 206 206L3 1182108SW FREEWHEEL UNIT LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW034835 51131 FREEWHEEL UNIT SUPPORT GARLOC SEAL LEAKING. REPAIRED. 1G71 3U H2SW 20030228000792003022800079WP 2003 2 28 ASAA0380002 120030103A52605910368 BRACE DOUG DC9 DC983 3022083WP AFT AIRSTAIR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT AIRSTAIR LOWER SECTION RIGHT SIDE BRACE CRACKED. STOP DRILLED CRACK AND INSTALLED ANGLE DOBLER PER SRM 51-30-2, 51-10-2, 51-10-4, AND 52-01. (M) 2L72 4F RTA6WE 20030228000812003022800081WP 2003 2 28 ASAA0380005 120030103A532059360501 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, LONGERON SPLICE CORRODED AT FS 1201. REPLACED DAMAGED SPLICE PER SRM 51-10-2, 51-10-4, AND 53-02. (M) 2L72 4F RTA6WE 20030228000862003022800086WP 2003 2 28 ASAA0380009 120030103A52605910368 BRACE DOUG DC9 DC983 3022083WP AFT AIRSTAIR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT AIRSTAIR LEFT SIDE BRACE CRACKED AT LOWER FORWARD END. STOP DRILLED CRACK AND INSTALLED ANGLE DOUBLER PER SRM 51-10-2, 51-10-4, 51-30-2, AND 52-01. (M) 2L72 4F RTA6WE 20030228000872003022800087WP 2003 2 28 ASAA0380010 120030103A53475936663521 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY TRACK CORRODED/GOUGED AT FS 1130-1322. REPLACED DAMAGED SECTION PER SRM 53-05 AND 51-30-5. (M) 2L72 4F RTA6WE 20030228000912003022800091WP 2003 2 28 ASAA0380013 120030103A52303913249501 ANGLE DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO DOOR VERTICAL ANGLE BEAM IS LOWER PAN AND FASTENERS ARE CORRODED. REPLACED CORRODED PARTS PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20030228000922003022800092SW 2003 2 28 HEEA084456 120030213A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPENSAT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 DROOP COMPENSTATOR ACTUATOR HAS INTERMITTENT OPERATION. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030228000972003022800097SW 2003 2 28 HEEA084459 120030213A6240206076373001 TACH GENERATOR BELL 206 206L3 1182108SW MAIN ROTOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 ROTOR INDICATOR NEEDLE FLUCTUATES AND SOMETIMES FALLS TO ZERO. LOW ROTOR LIGHT INTERMITTENTLY COMES ON. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030228000982003022800098SW 2003 2 28 HEEA084460 120030213A243523081018 STARTER GEN BELL 407 407 1182206SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 STARTER GEN DRAGGING. IN SHOP FOR REPAIR. 1G71 3U O H2SW 20030228001042003022800104WP 2003 2 28 DHL2003805004 120030226A2510 SEAT BELT DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER O OTHER ININSP/MAINT 1 SO01805DH 46125 1) F/O'S SEAT BELT WILL NOT UNLATCH.2) REMOVED AND REPLACED F/O'S LAP SEAT BELT PER M/M 25-11-1. 2L74 4F RT4A25 20030228001112003022800111SW 2003 2 28 HEEA084466 120030213A7740 BATTERY BELL 206 206L3 1182108SW COMPUTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 0552 51552 PROCESSOR HAS A DEAD INTERNAL BATTERY. IN SHOP FOR REPAIR. 1G71 3U H2SW 20030228001142003022800114WP 2003 2 28 MWEA030114 120030227A53473936668507 SUPPORT BRACKET DOUG DC9 DC981 3022081WP STA 332 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FORWARD CARGO COMPARTMENT SUPPORT BRACKET ON FLOOR BEAM STATION 332 AFT SIDE IS CRACKED LOCATED AT CENTER LINE. -- LOCATED, DRILLED AND INSTALLED BRACKET. 2L72 4F A6WE 20030228001222003022800122WP 2003 2 28 ABXA030093 120030203A53203920326501 FITTING DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CRACKED END FITTING STATION 604, LONGERON 28, LEFT. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030228001252003022800125 2003 2 28 HEEA084472 420030214A2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF COMMS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 TRANSCEIVER TRANSMITS DISTORTED. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030228001282003022800128NM 2003 2 28 AWXA200300213 120030227A5610221747541 SEAL AIRBUSA319 A319132 3930340NM ZONE 210 TORN A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28814AW0 0 1281 PHX - DIVERSION - FLT 0251 - ON CLIMB OUT FROM LAS EN ROUTE FOR PHL A NOISE WAS HEARD COMING FROM THE LEFT LOWER CORNER OF THE CAPTAINS WINDSHIELD. NOISE WAS INTERMITTENT AT FIRST, BUT AS DIFFERENTIAL INCREASED THE NOISE INCREASED AND THEN BECAME STEADY. DIVERTED TO PHOENIX WITHOUT FURTHER EVENT. MAINTENANCE REMOVED THE L/H WINDSHIELD AND PERFORMED VISUAL INSPECTION, NO DEFECTS WERE NOTED, REINSTALLED L/H WINDSHIELD IAW AMM 56-11-11-401. INSPECTED THE CAPTAINS L/H SLIDING WINDOW AND FOUND THE FORWARD LOWER CORNER SEAL TORN. REPLACED SEAL ON CAPTAINS L/H SLIDING WINDOW IAW 56-12-11. PRESSURIZATION CHECK WAS GOOD, NO LEAKS NOTED ON FLIGHT DECK WINDOWS. 2L72 4F RTA28NM 20030303000102003030300010SW 2003 3 3 HEEA084483 120030214A243230703002 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 MAIN BATTERY WILL NOT KEEP A CHARGE. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030303000122003030300012EA 2003 3 3 03060673 120030301A3350 BULB CNDAIRCL600 CL6002B19 1900309EA BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27673BR 7599 DURING PREFLIGHT INSPECTION CREW NOTICED THE R/H OVERWING EMERGENCY LAMP INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED OVERWING EMERGENCY LAMP. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030318000442003031800044NE 2003 3 18 105201 220030302A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE RIGHT FLUCTUATES A UHLAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL1719XS 340A019 122 FLIGHT 4556 PIT-FWA, AIRCRAFT WAS TAXIING FOR TAKEOFF WHEN THE CREW NOTICED THE RT ENGINE TORQUE, ITT, FUEL FLOW, AND RPM INDICATIONS WERE FLUCTUATING SEVERELY. AIRCRAFT RETURNED TO GATE AND WAS TAKEN OUT OF SERVICE AT 1628. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030318000452003031800045EU 2003 3 18 115997 120030218A3233L38710SA SWIVEL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE MLG ACTUATOR CRACKED A UHLAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL17158SD6365 6365 158 FLT 4474 IPT-PIT, ON TAKEOFF SELECTED GEAR UP, HYD LIGHT CAME ON WITH MAIN PRESSURE AT ZERO. SECURED PUMP, CONTACTED MAINTENANCE CONTROL AND CONTINUED TO PIT. SELECTED GEAR DOWN ALL INDICATED DOWN AND LOCKED WITH LOSS OF ALL HYDRAULIC FLUID ON QTY INDICATOR. PIT TOWER DECLARED EMERGENCY AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TOWED AIRCRAFT OFF TAXIWAY. VISUAL INSPECTION REVEALED THAT THE RIGHT MAIN GEAR ACTUATOR SWIVEL CRACKED ALLOWING LOSS OF ALL FLUID. MAINTENANCE REPLACED FITTING, SERVICED HYDRAULIC SYSTEM, AIRCRAFT TEST FLOWN WITH NO FURTHER PROBLEMS NOTED. RELEASED FOR SERVICE. 2L72 4T4 TRTA52EU E8NE6 20030318000462003031800046EU 2003 3 18 116001 120030219A5250JEC441091 LATCH SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE COCKPIT DOOR BURRED A UHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL17158SD 158 FLT 4496, PILOT REPORTED THAT DURING TAKEOFF ROLL THE COCKPIT DOOR OPENED. RETURNED TO THE GATE, MAINTENANCE DISPATCHED, FOUND THAT THE LATCH WAS NOT PROPERLY SECURING IN THE HOLE CUTOUT FOR THE LATCH. MAINTENANCE CLEANED THE AREA AROUND THE HOLE AND RECHECKED LATCH ENGAGEMENT, LATCH ENGAGED PROPERLY AND AIRCRAFT WAS RELEASED FOR SERVICE WITHOUT FURTHER INCIDENT. AIRCRAFT HAS BEEN MODIFIED WITH SB 340-25-282, REINFORCED COCKPIT DOOR. 2L72 4T4 TRTA52EU E8NE6 20030318000632003031800063WP 2003 3 18 AALA20030186 120030207A5313 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21417AA 49328 TUL - FOUND STATION 1380 AND STRINGER 14 RT SKIN HAS CRACK EMITTING FROM RIVET HOLE. STOP DRILLED CRACK SPECIFIED BY QA 242, APPLIED DOUBLER PER SRM 53-01 FIG 2 SHT 3. (M) 2L72 4F A6WE 20030318000702003031800070NM 2003 3 18 AMTA200300177 120030204A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 EGRESS LIGHTS JUST FORWARD OF RIGHT NR 2 DOOR 1 RED AND 1 SHITE ARE NOT ON DURING CHECK. REMOVED AND REPLACED BATTERY PACK AT R2 OVERHEAD IAW AMM 33-51-07. LIGHTS CHECK GOOD AT THIS TIME. (M) 2L72 4F RTA2NM 20030318000722003031800072NM 2003 3 18 AMTA200300190 120030108A5400 SHIM BOEING757 75723N 1384973NM NR 1 PYLON DISLODGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 NR 1 PYLON HAS MIGRATING SHIMS ON OUTBOARD LOWER SIDE OF PYLON. REPAIRED PYLON AND REPLACED SHIMS IAW EO 757-54SB-2456. (M) 2L72 4F RTA2NM 20030318000762003031800076NM 2003 3 18 AMTA200300204 120030209A2600 WARNING SYSTEM BOEING757 75733N 1384931NM COCKPIT ACTIVATED A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11556TZ 32590 FLT 645 - STATUS MESSAGE 'R ENG OH LP2" DISPLAYED ON EICAS. (M) 2L72 4F RTA2NM 20030318000822003031800082WP 2003 3 18 ASAA0380019 120030103A532199366403 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD TORN AT FOUR FASTENER HOLES AT FS 886-927. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20030318000832003031800083WP 2003 3 18 ASAA0380020 120030104A573099374822 SKIN DOUG DC9 DC983 3022083WP RT WING LE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE PANEL 1263 SKIN GOUGED AT SCREW HOLES. INSTALLED DOUBLER PER SRM 57-06A. (M) 2L72 4F RTA6WE 20030318000852003031800085WP 2003 3 18 ASAA0380022 120030104A5755 STRUCTURE DOUG DC9 DC983 3022083WP RT SPOILER CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RT OUTBOARD FLIGHT SPOILER IS CHAFED ON TRAILING EDGE UPPER SIDE OUTBOARD OF ACTUATOR MOUNT. REPAIRED DAMAGED AREA PER SRM 51-70-1B. (M) 2L72 4F RTA6WE 20030318000932003031800093WP 2003 3 18 ASAA0380030 120030104A575539615971 ACCESS PANEL DOUG DC9 DC983 3022083WP RT SPOILER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT OUTBOARD FLIGHT SPOILER ACCESS PANEL 1625A IS CRACKED. REPLACED PANEL PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20030318000942003031800094NM 2003 3 18 2003UALA00180 120030216A361033990047U1 CONTROLLER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29522UA 24931 726552 RT ENGINE HIGH STAGE LIGHT ON DURING TAKE OFF ROLL. SUPPLEMENTAL DATA UPDATE ROOT CAUSE: HIGH STAGE CONTROLLER OVER PRESSURE SENSOR & ANTI-ICE SWITCHER CALIBRATION WAS OUT. REPLACED CONTROLLER. 2L72 4F4 FRTA2NM E17NE 20030318000972003031800097NM 2003 3 18 2003UALA00273 120030313A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 LH EXTERNAL FUSELAGE HAS JETWAY DAMAGE (DENTS) AT STA 600 TO 620 BETWEEN STR 16L AND 18L. MAJOR REPAIR ACCOMPLISHED.APPLIED DOUBLER. 2L72 4F4 FRTA2NM E17NE 20030318001002003031800100EA 2003 3 18 COMA0360147 120030315A3230848847 PUMP CNDAIRCL600 CL6002B19 1900309EA 3A MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01960CA14337 7117 FLIGHT 5510 GEAR DISAGREE WHEN GEAR SELECTED DOWN.REPLACED THE #3A ACMP 2L72 4F RTA21EA 20030318001042003031800104EA 2003 3 18 COMA0360149 120030313A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01918CA 7018 FLIGHT 5885 FLAPS FAIL CAUTION DURING TAXI.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030318001052003031800105EA 2003 3 18 COMA0360150 120030313A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS CLCLIMB 1 SO01488CA 7730 FLIGHT 5711 FLAPS FAIL MESSAGE AFTER T/O.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030318001112003031800111NM 2003 3 18 BJNA030210 120030211A5320 FLOOR SUPPORT BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN AFT RIGHT CABIN FLOOR SUPPORT LOCATED AT FS 957. TIMCO REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AND FILLER MADE FROM 7075-T6 .100 MATERIAL. WORK DONE IAW BOEING 737 SRM 51-30-2, AND 51-10-2. (M) 2L72 4F RTA16WE 20030318001692003031800169EA 2003 3 18 COMA0370004 120030315A5312 CNDAIR CNDAIRCL600 CL6002C10 1390015EA A COMAO OTHER O OTHER ININSP/MAINT 1 SO01331CA 10061 F.S. 1098.20 PRESSURE BULKHEAD RIGHT SIDE RBL 34 & 0 RBR 41 BETWEEN STRINGERS 8R AND 9R HAS ONE INCH CRACK ON BULKHEAD.INCORPORATED RIGHT PRESSURE BULKHEAD BOMBARDIER, INC. REO 670-53-61-034 REV A. REMOVED DAMAGED AREA AND INSTALLED FITTING P/N 670-53-61-026-2. 2L72 4F RTA21EA 20030318001872003031800187WP 2003 3 18 IXXA0300025O 120030313A3200 LIGHT DOUG DC8 DC873F 302199FWP ILLUMINATED A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11606AL894021155 46044 DURING FLIGHT, LANDING GEAR DOOR NOT LATCHED LIGHT STAYED ILLUMINATED IN FLIGHT. UPLATCH CHECK OKAY. CREW CYCLED GEAR AND LIGHT FAILED TO EXTINGUISH. INSPECTION IS ON GOING, AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE PERFORMED A GEAR UP ENGAGEMENT FUNCTIONAL TEST IN ACCORDANCE WITH ATI MEL SPECIAL PROCEDURE 32.8, OPERATIONAL CHECK GOOD. MULTIPLE EXTENSIONS AND RETRACTIONS WERE PERFORMED ALONG WITH A GEAR POSITION INDICATING AND WARNING SYSTEM TEST. OPERATIONAL CHECKS WERE GOOD IN ACCORDANCE WITH THE DOUGLAS AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030318001942003031800194NM 2003 3 18 VNAA0303006 120030306A2400 GENERATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LH FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07442JS 3060 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE GENERAOR WAS RESET AND THE FLIGHT WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT. FLIGHT 4103 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030318001962003031800196NE 2003 3 18 VNAA0303012 220030311A7200 CHIP DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE A VNAAO OTHER O OTHER CRCRUISE 1 GL07427JS 3039 ENROUTE, THE CREW RECEIVED A RGB CHIP DETECT BLUE CAS MESSAGE. THE CREW WAS THEN INSTRUCTED TO DIVERT TO PIT AND LANDED WITH NO FURTHER DISCREPENCIES. MAINTENANCE THEN INSPECTED AND FOUND A HAIR LIE PARTICLE AND A FLAKE ON THE RGB CHIP DETECTOR, ALL WITHIN PRESCRIBED LIMITS. MAINTENANCE REPLACED THE FILTERS, CLEANED THE CHIP DETECTORS, AND CANNON PLUGS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030318002002003031800200NM 2003 3 18 UPS03240295 120030308A5710 RIB BOEING727 72725C 138400HNM #4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 INSPECTION TYPE:C&SI L/H WING SUSPECT CRACK AT I/B TRACK RIB ON 4 SLAT CRACK STOP DRILLED IAW SRM 51-10-01. HFEC C/O ON L/H WING AT I/B TR ACK RIB ON NO. 4 SLAT INSP. IAW B727 NDTM PT 6 51-00-00 RESULTS CRAC K CONTAINED BY STOP DRILLED HOLE 2L73 4F A3WE 20030625001172003062500117NM 2003 6 25 UPS03440301 120030317A5320 WEB BOEING747 747200 1384847NM CREW ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: PFLT, 3 INCH CRACK IN WEB AFT FRAME UPPER SIDE, MARKED. REMOVED FRAME WEB AT STA 488 FROM APPROX 5-16 TO 5-22. STARTED FABRICATION OF REPLACEMENT WEB AND TWO SPLICE PLACE IAW SRM 53-10-04. COMPLETED FABRICATING OF WEB & (2) SPLICE PLATES. TREATED, PRIME, PAINTED & STARTED TO INSTALL REF SRM 53-10-4 ON LWR SPLICE PLATE. COMPLETED THE EO FOR SHORT FASTENER EDGE DISTANCE. COMPLETED REPAIR. 2L74 4F RTA20WE 20030318002062003031800206SO 2003 3 18 C2XA03CL069 120030314A2910PV303211 PUMP EMB 145 EMB145ER 3260211SO #2 ENGINE FAILED A C2XAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SW27149392843 145030 CLE FLIGHT#2257 THE CREW REPORTED #2 HYDRAULIC SYSTEM FAILED ON APPROACH INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #2 ENGINE DRIVEN HYDRAULIC PUMP.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030318002132003031800213NM 2003 3 18 030055631 120030314A2530 OVEN BOEING747 747451 1384940NM # 3 GALLEY SMOKE A NWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL01673US 30268 During flight smoke emitted from the #4 oven in the #3 galley. Aircraft continued to destination and landed without incident. Replaced the oven controller, operational check good. 2L74 4F RTA20WE 20030318002202003031800220SO 2003 3 18 RAIA00303060 120030302A323023092900001 UPLOCK EMB 145 EMB145LR 3260212SO INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03820HK9462 145064 5653-STL- NOSE LANDING GEAR WILL NOT RETRACT. TROUBLE SHOOTING FOUND THAT THE GEAR WOULD RETRACT BUT WOULD NOT LOCK IN THE UP POSITION. MAINTENANCE REMOVED AND REPLACED NLG UP-LOCK BOX. 2L72 4T RTT00011AT 20030318002212003031800221SO 2003 3 18 RAIA00303067 120030306A335066367 BULB EMB 145 EMB145LR 3260212SO BURNED OUT A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03817HK 145058 5660-STL- EMERGENCY ESCAPE PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED TRACK BULBS, OPS CK OK. 2L72 4T RTT00011AT 20030318002232003031800223EU 2003 3 18 RAIA00303072 120030313A323054GB CONNECTOR AEROSPATR72 ATR72202 8680940EU SHORTED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03721TE 217 5592-STL - RIGHT MAIN LANDING GEAR SHOWS UNLOCK BUT WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED CONNECTOR 54GB ON RIGHT MLG, OPS CK OK. 2H72 4T RTA53EU 20030318002252003031800225EU 2003 3 18 117111 120030316A32465006227 WHEEL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE SEIZED A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL17121CQ 121 Flt 4497 pit-fwa. during take-off roll at approximately 40-60kts. the crew aborted due to a severe nosewheel shimmy. the a/c returned to the gate without incident. a/c taken out of service @1800. pit mx found the lh nosewheel bearing to be seized. mx removed and replaced both the rh and the lh nosewheels. the a/c was returned to service @1845 on 3-16-03 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030319000032003031900003WP 2003 3 19 GTIA030003 120030114A5330 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23130NK 47604 DTW - FOUND CRACK/PUNCTURE IN SKIN AT STATION NR 1012 LONGERON STATION NR 26R JUST AFT OF CARGO PIT DOOR. REPAIRED CRACK/PUNCTURE IN SKIN AT STATION1012 LONGERON NR 26R JUST AFT OF CARGO PIT DOOR. (M) 2L72 4F A6WE 20030319000042003031900004WP 2003 3 19 GTIA030004 120030114A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810ML 48015 FOUND LEFT CANTED FRAME 1463 HAS A CRACK AT THE 3 O'CLOCK POSITION. REPAIRED CANTED FRAME 1463 IAW MD80 SRM 51-10-4. (M) 2L72 4F A6WE 20030319000052003031900005WP 2003 3 19 GTIA030005 120030109A5553 ATTACH ANGLE DOUG DC9 DC982 3022082WP VERTICAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE CRACKED, APPROXIMATELY 1 INCH. REMOVED LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE. NEW FORMED ANGLE. INSTALLED LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE. (M) 2L72 4F A6WE 20030319000162003031900016 2003 3 19 GTIA030018 420030126A22102589445933 ACTUATOR DOUG DC9 DC983 3022083WP YAW DAMPER FAILED A GTIAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL23815NK 49415 DTW - FOUND FLT 639 - AIR RETURN TO DTW, DUE TO INFLIGHT FLIGHT CONTROL PROBLEM. AIRCRAFT BEGAN AN INCREASING DUTCH ROLL CONDITION AND REQUIRED 5 UNITS OF RIGHT RUDDER TRIM AN 3 UNITS OF RIGHT WING DOWN TRIM TO MAINTAIN STRAIGHT AND LEVEL. AIRCRAFT WAS NOT STABLE AROUND VERTICAL AXIS AND WAS EXHIBITING AN AIRFRAME BUFFET OF UNKNOWN ORIGIN. FOUND YAW DAMPER ACTUATOR FAILED AND JAMMED CAUSING RUDDER TO GO LEFT 4-6 DEGREES. ALSO, FOUND DFGC SWITCH 'B' AND 'C'C CIRCUIT BREAKERS BAD. REMOVED AND REPLACED SWITCH 'B' C/B (B10-368) AND SWITCH 'C' C/B (B10-369). REMOVED AND REPLACED YAW DAMP ACTUATOR PER MD-80 MM 22-14-01. OPS CHECK GOOD. RTS CHECKED GOOD. NO OTHER DISCREPANCIES NOTED. (M) 2L72 4F RTA6WE 20030319000192003031900019WP 2003 3 19 GTIA030021 120030110A3080 WARNING LIGHT DOUG DC9 DC983 3022083WP COCKPIT ILLUMINATED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23808NK 49504 DTW - FLT 1253 - AIRFOIL DE-ICE ON LEFT AND RIGHT ICE PROTECTION LOW LIGHTS STAY ON 90 PERCENT OFF TIME, FLT IDEL LIGHT STAYS ON 100 PERCENT OF THE TIME MAX SUPPLY PRESSURE 7 LBS. BOTH SIDES CABIN PRESSURE FLOW LIGHT COMES ON. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F RTA6WE 20030319000202003031900020 2003 3 19 GTIA030040 420030203A2565 SLIDE DOUG DC9 DC982 3022082WP PAX DOOR DISLODGED A GTIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL23817NK 49141 ORD - FLT 1927 - ON TAKEOFF ROLL L2 SLIDE PACK FELL OFF. REINSTALLED L2 SLIDE PACK PER MM OK FOR SERVICE. (M) 2L72 4F A6WE 20030319000222003031900022WP 2003 3 19 GTIA030042 120030205A3350 SIGN DOUG DC9 DC983 3022083WP GALLEY DETACHED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 DTW - FLT 706 - EMERGENCY EXIT SIGN AT AFT GALLEY FLOOR IS DETACHED. ATTACHED EMERGENCY EXIT SIGN AT AFT GALLEY FLOOR. (M) 2L72 4F RTA6WE 20030319000262003031900026WP 2003 3 19 GTIA030049 120030119A5540 TAB DOUG DC9 DC983 3022083WP RUDDER DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 SW21825NK 53012 FTW - RUDDER CONTROL TAB FLAME SPRAY DETERIORATED IN SEVERAL AREAS, FIXED TAB DELAMINATED AND 4 BONDING STRAPS DETERIORATED AND CORRODED. REPAIRED DELAMINATED FIXED TAB. (M) 2L72 4F RTA6WE 20030319000272003031900027NE 2003 3 19 GTIA030050 220030202A7200 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 LGA - ON WALK AROUND, FOUND RIGHT ENGINE FOD DAMAGE. NR 2 ENGINE NOSE COWL ACOUSTIC LINER DAMAGED. REMOVED AND REPLACED DAMAGED C-1 BLADES. REMOVED AND REPLACED NR 2 ENGINE NOSE COWL. (M) 2L72 4F4 F A6WE E9NE 20030319000282003031900028WP 2003 3 19 GTIA030051 120030113A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - AFT FUSELAGE STATION 1463 LEFT SIDE INBOARD FACE CANTED WEB CRACKED. FABRICATED SPLICE DOUBLER. REMOVED DAMAGED WEB. FABRICATED 13 REPLACEMENT WEB. FABRICATED REPLACEMENT DOUBLER. INSTALLED REPLACEMENT WEB, REPLACEMENT DOUBLER AND SPLICE DOUBLER. (M) 2L72 4F RTA6WE 20030319000302003031900030WP 2003 3 19 GTIA030055 120030212A2120 SMOKE DOUG DC9 DC982 3022082WP CABIN DETECTED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23820NK 49126 RSW - FLT 1504 - AFTER TAKEOFF FLIGHT ATTENDANT IN AFT CABIN REPORT ODOR OF SMOKE. INSPECTED BOTH AFT LAV'S, ABOVE AND AREA AROUND AFT F/A SEAT, OPENED OVERHEAD PANELS AND REINSTALLED, INSPECTED AC SYSTEM AND DUCTING IN TAILCONE AREA WITH ENGINES AND APU AS SUPPLY OF AIR SOURCE, NO DEFECTS NOTED A/C OK FOR SERVICE. (M) 2L72 4F A6WE 20030319000352003031900035WP 2003 3 19 GTIA030060 120030205A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 160-200 LBL 50 HAS CORROSION. DRILLED AND LOCATED NEW PART. (M) 2L72 4F A6WE 20030319000362003031900036WP 2003 3 19 GTIA030061 120030206A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 197 LBL LEFT HAS CORRODED. FABRICATED REPAIR SUPPORT. (M) 2L72 4F A6WE 20030319000372003031900037WP 2003 3 19 GTIA030062 120030206A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 197 LBL 34 HAS CORRODED. FABRICATED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030319000442003031900044WP 2003 3 19 GTIA030069 120030205A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR PANEL FORWARD ENTRY L-1 DETERIORATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030319000482003031900048WP 2003 3 19 GTIA030073 120030205A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR PANEL FORWARD CABIN STATION 200-260 HAS BLUE WATER STAINS AND CRACKED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20030319000492003031900049WP 2003 3 19 GTIA030074 120030204A5321 FLOORBOARD DOUG DC9 DC981 3022081WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FORWARD CABIN FLOORBOARD STATION 160-200 DETERIORATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030319000522003031900052WP 2003 3 19 GTIA030077 120030203A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND AFT PIT STATION 1212 FRAME SECTION RIGHT SIDE CRACK. FABRICATED NEW FRAME SECTION. INSTALLED NEW FRAME SECTION. (M) 2L72 4F A6WE 20030319000552003031900055EU 2003 3 19 03077313 120030318A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27313UE 41026 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT SECTION OF EMERGENCY EXIT LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 4 EMERGENCY EXIT LIGHTING SYSTEM BATTERY PACK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030319000642003031900064NM 2003 3 19 KPVA20032 120030105A335010005511 LIGHT DHAV DHC8 DHC8103 1386005NM PORTABLE LIGHT INOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13808WP 026 HNL - FOUND OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT. OPS CHECK GOOD IAW 8MM 33-52-00 PAGE 201-202 SECTION 2A. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030319000662003031900066NM 2003 3 19 KPVA20036 120030213A3350 BATTERY DHAV DHC8 DHC8103 1386005NM PORTABLE LIGHT WEAK A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13805WP250 353 HNL - PORT EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED PORT EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW DHC-8 MM 33-51-00 PAGE 201-202. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030401001772003040100177WP 2003 4 1 DHL2003806005 120030313A2612 FIRE WARNING DOUG DC8 DC873F 302199FWP NR 3 ENGINE ACTIVATED A DHLAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 SO01806DH 46002 AFTER STARTING ENGINE NR 3, INTERMITTENT FIRE INDICATION, SHUT DOWN ENGINE. INSPECTED ENGINE. FOUND NO PR'S RAN ENGINE PER JRH OPS OK. DEFER NR 3 ENGINE "B" LOOP PRECAUTIONARY ENTER AS DMI #12260 PER MEL REF. 26-2-3. 2L74 4F RT4A25 20030319000712003031900071 2003 3 19 MEX2003005 420030107A3414 INDICATOR DOUG MD88 MD88 3023688NM AIRSPEED FAILED A ASMFCD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW23168PL 53174 FLT 601 - ATL-MEX - ABORTED TAKEOFF DUE TO AIR SPEED INDICATOR FAILURE WITH 80 KNOTS THE LEFT AIR SPEED INDICATOR AND 65 KTS THE RIGHT SIDE. DURING CHECK IT WAS DETECTED A CADC NR 2 FAIL IN CDUS, AIR SPEED INDICATOR FLAG AND FAST/SLOW FUNCTION FAILURE IN RIGHT PFD. CADC NR 2 WAS TESTED IAW MM 34-16-01, ALL CORRECT. PITOT PORT WERE WITH DEBRIS. PITOT LINE WAS CLEANED. (M) 2L72 4F RTA6WE 20030319000742003031900074WP 2003 3 19 MEX2003020 120030102A2780833605 PROXIMITY SWITCH DOUG DC9 DC987 3022087WP SLATS FAILED A ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23205AM 49405 FLT 486 - MEX-SLC - AIRCRAFT RETURNED, WHEN SLAT RETRACTED, THE LIGHTS SLAT DISAGREE CAME ON AND 280 KTS THE OVERSPEED ALARM WAS ACTIVATED. SPEED WAS REDUCED BELOW 280 AND AFTER 3 MINUTES LIGHT WENT OFF. IAW THE INSTRUCTIONS OF SHIFT FOREMAN AIRCRAFT RETURNED TO FLIGHT. IN THE HANGAR, PERFORMED A BITE TO THE PROXIMITY SWITCH AND ELECTRONIC CONTROL PROXIMITY SWITCH WAS REPLACED IAW MM 32-60-04, ALL CORRECT. (M) 2L72 4F RTA6WE 20030319000942003031900094NM 2003 3 19 TSAA0324024 120030211A3150 WARNING LIGHT BOEING737 7372S2C 138448GNM NR 1 CSD FALSE INDICATIONA A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13806AL 21927 AFTER TAKEOFF, THE NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED AND WAS DISCONNECTED IAW THE QRH. THE AIRCRAFT RETURNED TO HNL FOR MAINTENANCE AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED THE NR 1 CSD SERVICING AND FOUND IT PROPERLY SERVICED. THE NR 1 CSD WAS PUT ON MEL AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030319000992003031900099NM 2003 3 19 TSAA0333019 120030131A33501000679 BATTERY PACK BOEING737 7372T4 1384492NM PAX DOOR INOPERATIVE A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13808AL 23445 REPLACED FORWARD PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030319001072003031900107NM 2003 3 19 TSAA0353007 120030204A5330654577655 SKIN BOEING737 7372M6C 1384708NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 REMOVED DAMAGED SKIN AND STRINGERS 26L, 27L, AND 27R BETWEEN BS 908 AND BS 1016. REPLACED SKIN PANEL PER PRODUCTION DRAWINGS 65-45776-55 AND 65-45776-56. INSTALLED PRODUCTION PANEL USING FASTENERS IDENTIFIED IN DRAWINGS. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-79 TYPE III PRIMER. APPLIED A FILLET SEAL OF BMS 5-95 SEALANT AROUND THE EDGES. APPLIED CORROSION INHIBITING COMPOUND TO THE INTERNAL AND EXTERNAL SURFACES OF THE REPAIR AREA. REPAIR COMPLETED IAW ECO 3334 PART 1. (M) 2L72 4F RTA16WE 20030320000072003032000007NM 2003 3 20 USAABB03004 120030107A335086210066 BATTERY BOEING757 7572B7 1384964NM ROW 33 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19631AU 27809 MIA - FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030320000082003032000008NM 2003 3 20 USAABB03005 120030109A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19629AU 27807 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 9, 13, 18, 23 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030320000092003032000009NM 2003 3 20 USAABB03006 120030109A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 26 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19629AU 27807 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030320000112003032000011NM 2003 3 20 USAABB03008 120030112A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19612AU 27124 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 6, 13, 18, 23, 26, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030320000142003032000014NM 2003 3 20 USAABB03018 120030206A33508731002511REV15 LIGHT BOEING757 757225 1384959NM L1 DOOR MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 BDL - FOUND THE EXIT IDENTIFIER EMERGENCY LIGHT AT THE L1 DOOR REMAINING ILLUMINATED ALL THE TIME. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20030320000422003032000042NM 2003 3 20 USAASB03010 120030115A2913887479 PUMP BOEING737 7373B7 1384580NM HYD SYSTEM FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19393US 23315 PHL - FLT 390 - EN ROUTE FROM CLT-DTW, THE 'A' HYDRAULIC SYSTEM ELECTRIC MOTOR DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED WITH THE PUMP CYCLING ON AND OFF. DECISION WAS MADE TO DIVERT TO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE 'A' HYDRAULIC SYSTEM ELECTRIC MOTOR DRIVEN PUMP AND ASSOCIATED FILTERS PER MM 29-15-22. OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030320000492003032000049NM 2003 3 20 USAASB03019 120030206A3260 SENSOR BOEING737 7373B7 1384580NM RT MLG W/W MALFUNCTIONED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19392US 23314 PIT - FLT 1963 - AFTER TAKEOFF, CREW REPORTED LANDING GEAR LEVER WOULD NOT MOVE TO RETRACT GEAR. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ADJUSTED THE GROUND SPOILER BYPASS/GROUND SENSE TELEFLEX CABLE, AS WELL AS, THE S105 AND S106 SAFETY SENSORS. ACCOMPLISHED SATISFACTORY MLG SENSOR TEST PER MM 32-09-01. ACCOMPLISHED SEVERAL GEAR SWINGS. GEAR SWINGS CHECK GOOD. PERFORMED SATISFACTORY TEST FLIGHT FOR LANDING GEAR LEVER OPERATION. REPLACED RIGHT MLG DISAGREEMENT LIGHT SOCKET FOR FAILURE TO ILLUMINATE DURING TEST FLIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030320000502003032000050NM 2003 3 20 USAASB03020 120030206A5240 SEAL BOEING737 7374B7 1384702NM SERVICE DOOR LEAKING A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19785AU 25024 PIT - FLT 1199 - ON CLIMB-OUT, FLIGHT ATTENDANT REPORTED A LOUD AIR LEAK AND NOISE COMING FROM FWD SERVICE DOOR. AT FL110, AS NOISE CONTINUED, CREW DECIDED TO RETURN TO FIELD AT PIT FOR MAINTENANCE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD SERVICE DOOR SEAL LEAKING AROUND THE STOP PADS ON THE DOOR SILL. APPLIED SEALANT AROUND PADS ON DOOR SILL. LEAK CHECK OF DOOR GOOD. 2L72 4F RTA16WE 20030320000542003032000054NM 2003 3 20 USAASB03024 120030211A335020131A BATTERY BOEING737 7373B7 1384580NM AFT CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19527AU 23862 IND - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS, ON SEAT ROWS 16 THROUGH 22, ARE DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATOINAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030320000592003032000059EU 2003 3 20 03078328 120030319A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27328UE 41083 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE WIRING AT THE AFT EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030320000622003032000062NM 2003 3 20 03FDEA00329 120030318A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 GOUGE IN STRINGER 3 RT OB FLANGE STA 520. REMOVED & REPLACED STR 3 RT BS 510 TO BS 530 IAW FED EX EA 7-5310-69439. 2L73 4F RTA3WE 20030320000632003032000063NM 2003 3 20 03FDEA00330 120030318A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 GOUGE IN STRINGER 3 RT OB FLANGESTA 540. REMOVED & REPALCED STRINGER 3 RT BS 530 TO BS 550 I.A.W. FED EX EA 7-5310-69439. 2L73 4F RTA3WE 20030320000652003032000065NM 2003 3 20 03FDEA00332 120030318A5311 FRAME BOEING727 727200 138407ENM BS 1176 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 FRAME IS CRACKED AT WL 208, BS 1176, LBL 16. BS 1176 FRAME CRACKED AT LBL 16, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1, REMOVED BS 1176 FRAME RBL 65 - LBL 65 WL 208, LOCATED AND BACKDRILLED REPLACEMENT FRAME PER SRM 51-30-5 AND 51-30-8, ALODINED, PRIMED AND PAINTED FRAME PER FED EX MM 51-20-151 AND INSTALLED BS 1176 FRAME WL 208 RBL 65 - LBL 65 PER SRM 51-30-2. 2L73 4F RTA3WE 20030320000742003032000074EU 2003 3 20 2003UALA00007 120030102A49904951093 OIL COOLER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE APU LEAKING A UALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29404UA6867 66 450 NOXIOUS ODOR IN CABIN AFTER TAKEOFF. SUBJECT APU OIL LEAK WAS CONFIRMED AT TEST. OIL COOLER WAS LEAKING SEVERELY (APPROX 1/2 QT. / MINUTE) FROM THE INLET SIDE OF THE PRESSURE REGULATOR. FURTHER DISASSEMBLY REVEALED SEVERAL DEEP VERTICAL SCRATCHES EVIDENT AT THE INSIDE DIAMETER THAT INTERFACES WITH THE REGULATOR CAP THAT IS SEALED WITH AN O-RING. THE DAMAGE APPEARS TO HAVE OCCURRED DURING ASSEMBLY OF THE REGULATOR VALVE, SPRING, AND CAP ASSEMBLY. 2L72 4F4 FRTA28NM E40NE 20030320000882003032000088NM 2003 3 20 2003UALA00072 120030117A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29306UA 23667 SECTION OF AIRCRAFT EEL STRIP ADJACENT TO THE MAIN GEAR DOWN LOCK VIEW PORT TORN AND ANOTHER SECTION GLOWS DIM. REPLACED DAMAGED POWER STRIP AROUND VIEW PORT. 2L72 4F4 FRTA16WE E2GL 20030320000922003032000092NM 2003 3 20 2003UALA00078 120030122A2421 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE IDG SHORTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29662UA 27159 SMOKE IN COCKPIT. WHEN SWITCHING OFF UTILITY BUSSES RT GENERATOR TRIPPED. UPON ARRIVAL AT BAQ, REPLACED RT GENERATOR CONTROL UNIT. ALSO FOUND RT ENGINE FIRE DETECTION CIRCUIT BREAKER OPEN ON P11 PANEL, AND HEAT DAMAGED RT ENGINE FIRE DETECT CARD M684. CARD REPLACED, AND CHECKED E AND E BAY FOR POSSIBLE WATER INGRESS. FOUND IDG WIRE W3538-301Y-18 SHORTED TO FIRE LOOP WIRE W3520-505R-16. REPAIRED SHORTED WIRE. 2L72 4F4 FRTA1NM E24NE 20030320000932003032000093NM 2003 3 20 2003UALA00080 120030122A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 847, 15 INCHES AND 20 INCHES, UP FROM AFT PIT DOOR CUTOUT LOWER AFT CORNER, FUSELAGE SKIN GOUGED IN 2 EA PLACES ALONG CUTOUT EDGE. MAJOR REPAIR ACCOMPLISHED. DOUBLER, TRIPLER AND QUADRUPLED MANUFACTURED AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030320000952003032000095NM 2003 3 20 2003UALA00085 120030124A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 DENT IN FUSELAGE AT STATION 322, APPROXIMATELY 24 INCHES BELOW LOWER DOOR SILL OF DOOR 1R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320000962003032000096NM 2003 3 20 2003UALA00086 120030124A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 DENT IN FUSELAGE AT STATION 322, APPROXIMATELY 24 IN BELOW LOWER DOOR SILL OF DOOR 1R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320000972003032000097NM 2003 3 20 2003UALA00088 120030122A3350 BATTERY PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29172UA 24363 ROW 22A-B THRU ROW 26A-B SEAT EELS DIM. REPLACED BATTERY PACK. 2L74 4F4 FRTA20WE E24NE 20030320001012003032000101NM 2003 3 20 2003UALA00092 120030125A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CREASE BEAM WEB AT STATION 827-847 STRINGER 17L HAS CORROSION. ACCOMPLISHED MAJOR REPAIR. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20030320001022003032000102NM 2003 3 20 2003UALA00093 120030125A5320 CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 FRAME AT BODY STATION 807 STRINGER 9L AT SUPPORT RAIL CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030320001032003032000103NM 2003 3 20 2003UALA00094 120030125A5320 ANGLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN BODY STATION 947 THRU 960 RT ZEE ANGLE UPPER SURFACE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE. 2L72 4F4 FRTA16WE E2GL 20030320001052003032000105NM 2003 3 20 2003UALA00096 120030126A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 STATION 767 FRAME CRACKED AT STRINGER 9R AT SUPPORT RAIL ATTACH FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001102003032000110NM 2003 3 20 2003UALA00101 120030127A5320 CHANNEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 AFT CABIN FLOOR MOUNTED HAT CHANNEL WITH L-ANGLE ON UPPER FORWARD WALL MOUNTING HAD CORROSION AT NUT PLATE HOLES STATION 988 13 (RBL OUT TO 43.5) RBL. STR 17R (CABIN FLOOR). MAJOR REPAIR ACCOMPLISHED. CUT TO SIZE NEW SECTION OF HAT CHANNEL EXTRUSION WITH L-ANGLE FLANGE ON UPPER CENTER. 2L72 4F4 FRTA16WE E2GL 20030320001172003032000117NM 2003 3 20 2003UALA00107 120030127A5411 SPAR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29642UA 25092 NR 1 PYLON UPPER SPAR WEB CRACKED AT AFT CUTOUT, AFT OUTBOARD RADIUS. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB W/DOUBLER. 2L72 4F4 FRTA1NM E24NE 20030320001202003032000120NM 2003 3 20 2003UALA00110 120030128A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 BS 178 BULKHEAD WEB CRACKED AT LOWER LT RADAR MOUNT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001282003032000128NM 2003 3 20 2003UALA00119 120030129A278265445516 ACTUATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 LE FLAP INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29318UA 23950 AIRCRAFT RETURNED TO FIELD WHEN FLIGHT CREW WAS UNABLE TO RETRACT THE FLAPS. REPLACED NR 2 LE FLAP ACTUATOR. 2L72 4F4 FRTA16WE E2GL 20030320001372003032000137NM 2003 3 20 2003UALA00128 120030102A5313 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29952UA 26699 FASTENER INSTALLED AT STA 478 BETWEEN STRINGER 2R & STRINGER 3R IS INSTALLED IN A COCKED POSITION AND HAS DENTED SKIN. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030320001442003032000144NM 2003 3 20 2003UALA00137 120030202A3250286W7187003 WIRE HARNESS BOEING777 777222 1385219NM PWA PW4077PW4077 NE NLG STEERING SHORTED A UALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP29775UA29716 26947 MAIN GEAR STEERING INDICATION RECEIVED. MAIN GEAR STEERING POWER CONTROL ACTUATOR LT FAULT. MAIN GEAR STEERING FAULT DUE TO THE LT MAIN GEAR STEERING POWER CONTROL ACTUATOR (PCA) SHOWING NOT LOCKED AT BEGINNING OF TAKE-OFF ROLL. FURTHER TROUBLESHOOTING DISCOVERED A BAD WIRE HARNESS BETWEEN THE PCA AND THE LOWER JUNCTION BOX. THE WIRE HARNESS WAS REPLACED. AIRCRAFT HAS FLOWN SEVERAL FLIGHTS WITH NO FURTHER INCIDENTS. 2L72 4F4 FRTT0001SE E46NE 20030320001452003032000145NM 2003 3 20 2003UALA00138 120030203A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FLOOR INTERCOSTAL AT STATION 1009 TO 1016 LBL 5 TO 9, STRINGER 17L HAD UPPER FLANGE CORRODED TO EXCESS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW VENDER PART [I-CHANNEL ]. 2L72 4F4 FRTA16WE E2GL 20030320001482003032000148NM 2003 3 20 2003UALA00141 120030203A3350 COVER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE EMERGENCY LIGHT MISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP29605UA 21866 EEL LIGHT STRIP FORWARD OF DOOR 2 LEFT IS INOPERATIVE AND COVER IS MISSING. SECURED POWER FEEDER. OPS CHECK OK. INSTALLED NEW LIGHT LENS COVER. 2L72 4F4 FRTA1NM E3NE 20030320001512003032000151EU 2003 3 20 2003UALA00145 120030205A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29412UA 465 FUSELAGE SKIN DAMAGED AT FRAME 61 AT STRINGER 40L & STRINGER 41L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLERS AND DOUBLER. 2L72 4F4 FRTA28NM E40NE 20030320001582003032000158NM 2003 3 20 2003UALA00151 120030205A5320 STIFFENER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29647UA 25284 RIGHT NOSE TUNNEL AT BS 246, RBL 40, FLOORBEAM INTERCOSTAL ATTACH ANGLE STIFFENER IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW STIFFENER. 2L72 4F4 FRTA1NM E24NE 20030320001612003032000161WP 2003 3 20 MWEA030135 120030318A53475957871 SEAT TRACK DOUG DC9 DC932 3022066WP COCKPIT DEFECTIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 FIRST OFFICER SEAT HITS THE HI-LOCS ON SEAT TRACK OUTBOARD OF EXSISTING REPAIR. -- INSTALLED STAINLESS STEEL STRAP ON SEAT TRACK OUTBOARD AND REMOVED AND REPLACED SEAT TRACK. 2L72 4F A6WE 20030303000262003030300026SW 2003 3 3 HEEA084493 120030214A3212412050017135 COVER BELL 412 412 1182202SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 EMERGENCY FLOAT COVER IS WORN. REPLACED WITH SERVICEABLE FLOAT COVER. 1G72 4U H4SW 20030303000492003030300049SW 2003 3 3 HEEA084506 120030214A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 STARTER GENERATOR DRAGGING. 1G72 4U H4SW 20030303000542003030300054SW 2003 3 3 HEEA084509 120030214A30402314M2218 ARM BELL 412 412 1182202SW WINDSHIELD WIPERCORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 WINDSHIELD WIPER ARM CORRODED. SCRAPPED. 1G72 4U H4SW 20030303000592003030300059NM 2003 3 3 SWAA030392 120030218A335065C27093 LIGHT BOEING737 7373Q8 1384670NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED BC1 CHECK, FOUND ONE LIGHT BULB INOP AT EACH CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHT. RELAMPED EACH CABIN DOOR EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030303000602003030300060NE 2003 3 3 HEEA084512 220030214A732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE OSCILLATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 FREE TURBINE GOVERNOR PRODUCING ENGINE OSCILLATION. REPAIRED. 1G72 4U4 U H4SW E22EA 20030303000622003030300062 2003 3 3 SWAA030395 420030219A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29737JW 27869 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030303000682003030300068NM 2003 3 3 SWAA030404 120030219A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 663 AT STR 10R AND BS 706 AT STR 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030303000692003030300069NM 2003 3 3 SWAA030406 120030219A335010126211 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR VERTICAL EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030303000712003030300071NM 2003 3 3 SWAA030423 120030220A2560PH22300L STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROWS 4, 5 & 6 RT. REMOVED AND REPLACED STRIP SECTION PER MM. 2L72 4F RTA16WE 20030303000742003030300074NE 2003 3 3 HEEA084515 220030214A732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K4173 36001 BEEP RANGE KEEPS CHANGING. FOUND GOVERNOR ACTION TO BE A LITTLE SLUGGISH. FOUND FLYWEIGHT PINS COATING TO BE SLIGHTLY WORN AND TEFLON FLYWEIGHT WASHERS ALSO WORN. REPLACED PARTS AND UNIT TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030303000752003030300075NM 2003 3 3 SWAA030426 120030224A32116546113 TRUNNION PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED SERVICE CHECK, SWA SI 11251-32, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030303000772003030300077NM 2003 3 3 SWAA030428 120030225A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29379SW 26586 FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030303000822003030300082NM 2003 3 3 SWAA030437 120030221A335065C34691 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 21 ABC. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030303000852003030300085NE 2003 3 3 HEEA084517 220030214A732325249995 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 LOW SIDE FAILURE. FOUND GOVERNOR RESPONSE SLOW. FOUND ACTION OF FLYWEIGHTS SLOW DUE TO DIRTY AND WORN COATING ON FLYWEIGHT PINS. ALSO FOUND SLIGHT WEAR ON TEFLON TUBE. REPLACED PINS AND TUBE. UNIT TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030303000892003030300089SW 2003 3 3 HEEA084520 120030214A243230126002 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 MAIN BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030303000922003030300092NE 2003 3 3 HEEA084522 220030214A75323039009 BLEED VALVE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 BLEED VALVE FAILED ENGINE HAS HIGH ITT AND N1 SPEED. 1G72 4U4 U H4SW E22EA 20030303000992003030300099SW 2003 3 3 HEEA084525 120030214A243230703001 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 33115 BATTERY HAS LOW VOLTAGE. REPAIRED. 1G72 4U H4SW 20030303001012003030300101SW 2003 3 3 HEEA084526 120030214A243230703002 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 MAIN BATTERY SLOW TO CHARGE. REPAIRED. 1G72 4U H4SW 20030303001042003030300104WP 2003 3 3 0300329614 120030214A5330 SKIN DOUG DC9 DC932 3022066WP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614NW 47128 During "H" check found corrosion on fuselage skin between BS 160-180 L28L-L28R. Repaired per EA 96-194258. 2L72 4F A6WE 20030303001102003030300110SW 2003 3 3 HEEA084528 120030214A2432 CHARGER BELL 412 412 1182202SW BATTERY MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 CHARGING SYSTEM MALFUNCTION RAN BATTERY DOWN. REPAIRED. 1G72 4U H4SW 20030303001152003030300115NE 2003 3 3 HEEA084532 220030214A7321324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 2 ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 DURING FUEL CROSS FEED CHECK THE NR 2 ENGINE FLAMED OUT. FLOW PROBLEMS (INCONSISTENT). THE BYPASS VALVE WAS STUCK. REPLACED VALVE AND SLEEVE. UNIT TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030303001212003030300121SW 2003 3 3 HEEA084539 120030214A243239563001 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 MAIN BATTERY DEAD. 1G72 4U H4SW 20030303001222003030300122 2003 3 3 HEEA084540 420030214A3416 INDICATOR BELL 412 412 1182202SW STDBY ALTIMETER WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0322347 36005 STANDBY ALTIMETER WILL NOT TEST. REPAIRED. 1G72 4U H4SW 20030303001322003030300132SW 2003 3 3 HEEA084556 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 10971 33113 MAIN ROTOR BLADE TIP CAP UNBONDED, FIBERGLASS CRACKED IN SEVERAL AREAS AND TRIM TAB SEPARATED. 1G72 4U H4SW 20030303001352003030300135SW 2003 3 3 HEEA084559 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T10515 33112 MAIN ROTOR BLADE IS TOO HEAVY, WILL NOT FLY, SUSPECT WATER IN THE CORE. 1G72 4U H4SW 20030303001402003030300140SW 2003 3 3 HEEA084564 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033300811334 36004 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS SEVERAL EROSION HOLES. 1G72 4U H4SW 20030303001802003030300180NM 2003 3 3 AALA20030034 120030107A5320 SUPPORT ANGLE BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21673AN 29423 TUL - FOUND GALLEY SUPPORT ANGLE CORRODED RBL 49 INCHES STATION 1715. INSTALLED NEW SERVICEABLE SUPPORT ANGLE PER SRM 51-10-1. (M) 2L72 4F RTA2NM 20030303001812003030300181NM 2003 3 3 AALA20030048 120030110A3350 LIGHT BOEING767 767323 1385205NM COCKPIT DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21383AN 26995 DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT DIM WHEN TESTED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030303001912003030300191WP 2003 3 3 DHL2003804536 120030212A551456541921 RIB DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF. N/R 1430 PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1 . REMOVED UPPER CAP-AFT DAMAGED RIB IAW SRM51-1-21 PG. 1 , FABRICATED UPPER CAP-AFT RIB (7075-T6)IAW ATM 5-19-00 , DWG. 5654192-1. CLEANED, TREATED AND PRIMED IAW SRM51-1-8B. INSTALLED NEW UPPER CAP-AFT RIB ON HORIZ. STAB. STA XE29.000WITH NEW FASTNERS IAW SRM 51-1-21 PG.1 , SRM51-1-20D PG. 9 2L74 4F RT4A25 20030303001972003030300197WP 2003 3 3 DHL2003804542 120030211A571297532974 FORMER DOUG DC8 DC873F 302199FWP WORN A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF. N/R 1727: RH WING L/E OUTBD STUB WING FORMER WORN OUT OF LIMITS XOLDO67.750 (MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 REMOVED WORN FORMER IAW SRM51-1-20DPG. 21 FABRICATED NEW FORMER (7075 "O" .090) IAW ATM5-19-00 & DRAWING 9753297 , PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 13 D.P.S. 7-00-1 REV. BJ PG7 DPS1.05-3 PG 5-11 , CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FORMER ON OUTBD STUB WING STA XOLDO 67.750 IAW SRM 51-1-20D PG 9 2L74 4F RT4A25 20030321001102003032100110NM 2003 3 21 2003UALA00256 120030307A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BURNED OUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 DOOR 4R EMERGENCY SLIDE LIGHT ON OUTSIDE OF FUSELAGE IS INOP. SLIDE LIGHT REPLACED/RELAMPED. 2L72 4F4 FRTA2NM E17NE 20030321001122003032100112WP 2003 3 21 ZW0A0303207 120030318A33500105606003 LAMP DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139403W 53139 THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 6-7. REPLACED THE LAMP AT SEAT 6. CHECK-C 9-11-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030321001132003032100113WP 2003 3 21 ZW0A0303208 120030319A33507732 LAMP DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13974TW 53624 THE AFT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 9-4-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030324000052003032400005EU 2003 3 24 03FDEA00339 120030320A27804907905 CONTROLLER AIRBUS310 A310 EU SLAT/FLAPS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25422FE6993 6993 346 ON CLIMB OUT SIN. GOT "SLATS" LIGHT AND "SLATS" SYS 1 LIGHT ON OVERHEAD. DID PROCEDURE BUT NO CHANGE. RETURN TO SIN RAMP. SFCC 1 BITE SHOW SFCC FAULTED. R & R NR 1 SFCC PER MM 27-51-18-4. OPS CHECKED OK. 2L72 4F RTA35EU 20030324000062003032400006EU 2003 3 24 03FDEA00340 120030320A2750500A000003 SOLENOID VALVE AIRBUS310 A310 EU FLAPS/SLATS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25422FE8496 8496 346 AFTER TAKE OFF AT SIN, RECEIVED FLAPS SYS 1 FAULT. ALSO LOST AIRSPEED HOOK ON CAPT SIDE WITH RED SPEED LIMIT SHOWING. SFCC NR 1 BITE SHOWS FLAP RT WTB. R & R RT WTB SOLENOID VALVE PER MM 27-56-13-4 AND PERFORMED SFCC BITE TEST PER MM 27-51-00 TEST OK. FOR PRECAUTIONARY REPLACED RELAY 31XC. FLAPS OPS CHECKED PER MM 27-54-00-5 CHECKED OK WITH NO SYS FAULT. PERFORMED ADS TEST PER MM 34-18-00-0 ALL TEST OK. A/C OK FOR SERVICE. 2L72 4F RTA35EU 20030402000312003040200031NM 2003 4 2 2003UALA00260 120030310A3260871601 PROXIMITY SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE MLG OUT OF RIG A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29581UA 26701 A/C RECEIVED GEAR DISAGREE INDICATION. GEAR UP LOCK SENSORS S10069 AND S10239 WERE OUT OF RIG. THESE TWO PROXIMITY SENSORS WERE ADJUSTED PER THE AMM. 2L72 4F4 FRTA2NM E17NE 20030324000122003032400012NM 2003 3 24 2003UALA00261 120030309A3350 SIGN BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29609UA 21870 GREEN EMERGENCY LIGHT EXIT SIGNS AT MED 2L AND 2R ARE INOP. REPAIRED DAMAGED SECTION 2L72 4F4 FRTA1NM E3NE 20030324000132003032400013NM 2003 3 24 2003UALA00262 120030306A3250 TILLER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NLG STEERING FAILED A UALAO OTHER O OTHER TXTAXI/GRND HDL 1 WP29109UA 26906 NOSE WHEEL TILLER DID NOT RESPOND TO INPUT. NOSE WHEELS, LEFT WING AND BODY GEAR WENT OFF OF TAXIWAY. REPLACED NOSE GEAR STEERING. METERING VALVE. ADJUSTED NOSE GEAR STEERING CABLES NWS2A & NWS2B TO PROPER TENSION. FOUND TO BE 10LBS. REPLACED BRAKES FOUR POSITIONS LWG. REPLACED TIRES FOUR POSITIONS LWG AND LT & RT NLG. ACCOMPLISHED NOSE GEAR STEERING EXCEEDANCE CHECK AND LANDING GEAR PORTION OF HIGH SIDE LOAD PHASE 1 INSPECTION. 2L74 4F4 FRTA20WE E24NE 20030408000942003040800094NM 2003 4 8 2003UALA00272 120030313A2497 CONTROL PANEL BOEING777 777222 1385219NM GALLEY SHORTED A UALAJA DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29796UA 26931 SPARKS, SMOKE AND ODOR IN CABIN FROM OVERHEAD PANEL IN PAX COMPARTMENT. MECHANICS FOUND MELTED PLASTIC INSIDE BOTH MID-GALLEY WARMING OVENS. MID-GALLEY IS LOCATED JUST FORWARD OF ROW 11. PLASTIC WAS REMOVED FROM WARMING OVENS, OVENS CLEANED AND OP CHECK OK. 2L72 4F RTT0001SE 20030324000382003032400038EU 2003 3 24 40001 120030213A3260D22858000 PROXIMITY SWITCH AMD FALC50FALCON900 2700160EU NLG FAILED E ERYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07369BG6019 040 LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED NOSE GEAR LEFT PROXIMITY SWITCH (3GF). ALL WORK DONE IN ACCORDANCE WITH M/M CHAPTERS 32-300, 32-611, AND 32-303. FUNCTION TEST OK. 2L73 4F RTA46EU 20030324000542003032400054WP 2003 3 24 ABXA030111 120030225A5347 SEAT TRACK DOUG DC9 DC941 302207NWP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23958AX 47760 SEAT TRACK AT BUTT LINE 22 LEFT HAD CORROSION ON UPPER SURFACE OF OUTBOARD LOWER LEG FROM STA. 1034 - 1041 AND LOWER SURFACE OF OUTBOARD UPPER LEG AT STA. 1009. REPLACED TRACK SECTION IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030324000552003032400055WP 2003 3 24 ABXA030114 120030311A57305611350 SKIN DOUG DC8 DC861 3021952WP LT WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE LEFT WING, UPPER PLATING. REPAIRED AREA IAW REA D857-46919. 2L74 4F 4A25 20030324000582003032400058EU 2003 3 24 MALA030206 120030322A8010501113775 STARTER BAC 146 AVRO146RJ85A1500097EU A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15522XJ E2347 AFTER TAKEOFF ON FLIGHT #3533, STARTER OPERATING LIGHT CAME ON DURING DECENT INTO MEMPHIS. LIGHT WENT OFF AND BACK ON. AIR RETURN TO MEMPHIS. MAINTENANCE INSPECTED AND FOUND #3 ENGINE STARTER WIRES BROKEN, INSIDE STARTER. MAINTENANCE REPLACED STARTER PN 501-1-13775, SN/OFF TE2520, SN/ON TE2241. 2H74 4F RTA49EU 20030324000592003032400059WP 2003 3 24 ABXA030117 120030313A2450 RELAY DOUG DC9 DC931 3022065WP ELECTRICAL FAILED A ABXAO OTHER G MULTIPLE FAILURE CRCRUISE 1 GL23924AX 47403 DURING FLIGHT, AUTOPILOT DISCONNECTED, EADI AND EHSI PICTORIAL APPEARED TO HAVE ALL SYMBOLS RAPIDLY SPINNING. SELECTED SG-3, REALIGNED EADI AND EHSI. BUT WHEN CONNECTING AUTOPILOT, AIRCRAFT WOULD RAPIDLY DIVE AND BANK. SERVOS COULD BE HEARD GYRATING AND SERVO INDICATIONS WERE FLUCTUATING. AT PARKING, FOUND EMERGENCY AC BUS FEED CIRCUIT BREAKER OUT. OPS CHECKED AC BUS FEED SYSTEM IAW DC-9 AMM 24-50-00-2. FOUND AC EMERGENCY POWER TRANSFER RELAY R2-47 TO BE INOPERATIVE. REMOVED AND REPLACED RELAY R2-47, ALSO REPLACED AC BUS FEED EMERGENCY CIRCUIT BREAKER FOR PRECAUTION. BOTH UNITS REMOVED AND REPLACED IAW DC-9 24-50-00-2. OPS CHECKED GOOD. 2L72 4F A6WE 20030324000602003032400060WP 2003 3 24 ABXA030118 120030318A53202537717 WEB DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23828AX 45999 CUSP WEB CRACKED AT FS 300 RIGHT ON MOST OUTBOARD TRACK. REPAIRED AREA IAW DC-8 SSRM 51-1-21 AND DWG. K07142. REF: W/O 600166120. 2L74 4F 4A25 20030324000752003032400075CE 2003 3 24 AMWA12 120030214A5411 SPAR CAP BEECH 1900 1900D 1154162CE NACELLE CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0713ZV UE13 UPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP WAS CHAFFING. BLENDED OUT THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030324000762003032400076CE 2003 3 24 AMWA13 120030216A5711 SPAR CAP BEECH 1900 1900D 1154162CE WING CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07218YV UE218 UPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT SPAR CAP WAS CHAFING THE WHEEL WELL. BLENDED THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030324000872003032400087WP 2003 3 24 ARWA20030306 120030312A5311 FRAME DOUG DC8 DC863 302198AWP FUSEAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA 980 BETWEEN L-18 AND L-19 FRAME WITH 1.5 INCH CRACK. 2L74 4F 4A25 20030324000942003032400094EA 2003 3 24 03083634 120030324A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27634BR 7287 During preflight inspection, the crew reported that the r/h exterior emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030324000992003032400099NM 2003 3 24 AWXA200300090 120030110A5414311A145010 DOUBLER BOEING737 737300 1384610NM PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK 2 EACH 5/8 INCHES CRACKS WERE FOUND ON NR 1 PYLON SKIN AND DOUBLER AT THE AFT LOWER CORNER OF PANEL 5724L, NAC STA 254. MAINTENANCE REMOVED EXISTING EXTERNAL DOUBLER AND PERFORMED HFEC INSPECTION VERIFYING CRACK LENGTH; STOP DRILLED CRACK AND RE-ACCOMPLISHED HFEC; REINSTALLED EXISTING EXTERNAL DOUBLER. REPAIR ACCOMPLISHED IAW AWA E.R. 03-5450-03021-SS1. 2L72 4F RTA16WE 20030324001012003032400101NM 2003 3 24 AWXA200300092 120030128A575369737595 STIFFENER BOEING737 737300 1384610NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1 INCH CRACK WAS FOUND ON LT WING INBOARD CANOE FITTING WS 191. MAINTENANCE CUTOUT CRACKED AREA OF LT WING INBOARD CANOE FITTING; FABRICATED A FILLER AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG. 3. 2L72 4F RTA16WE 20030324001082003032400108WP 2003 3 24 MWEA030138 120030321A532199365807 INTERCOSTAL DOUG DC9 DC981 3022081WP STA 788 & 769 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 SUBFLOOR INTERCOSTAL CRACKED IN SEVERAL PLACES BETWEEN FRAME STATION 788 AND 769 CENTERLINE. --FABRICATED AND INSTALLED REPAIR. 2L72 4F A6WE 20030324001232003032400123EA 2003 3 24 03082654 120030323A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 During preflight inspection, the crew reported that the r/h fwd exterior emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030324001242003032400124 2003 3 24 AWXA200300111 420030208A2213 COMPUTER AIRBUSA319 A319132 3930340NM COCKPIT FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28801AW 889 LAS - ABORTED TAKEOFF - FLT 0532 - ON TAKEOFF ROLL IN LAS EN ROUTE FOR RNO AT 85 TO 90 KTS BOTH NAV DISPLAYS AND FLIGHT MANAGEMENT GUIDANCE COMPUTERS (FMGC) TIMED OUT, SCREEN NOT DISPLAYING MAPS. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE RESET FMGC CIRCUIT BREAKERS NR 1 & 2 PER TSM 24-00-00-810-818. REALIGNED AIR DATA INERTIAL REFERENCE UNITS, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030324001272003032400127NM 2003 3 24 UPS03440333 120030304A5310 BRACKET BOEING747 747200 1384847NM STR 25L BS 2231 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C FWD CRACKS WITH THROUGH THICKNESS FOUND AT ONE EACH FASTENER HOLE AT TIE CLIP AT THE I/B CHORD AT STR 25L OF BS 2231. TIE CLIP REPLACED AT BS 2231 STR 25L AREA AS PER SRM 51-10-01 PG.8. 2L74 4F RTA20WE 20030324001322003032400132EA 2003 3 24 COMA0360160 120030320A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA R/H MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01920CA2702 7022 FLIGHT 5242 FLAPS FAIL CAUTION MESSAGE.COULD NOT DUPLICATE - REPLACED THE R/H BPSU FOR TROUBLE SHOOTING. 2L72 4F RTA21EA 20030328000902003032800090EA 2003 3 28 COMA0360161 120030323A2750860D10018ABCD COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01431CA4428 7472 FLIGHT 5002 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20030324001362003032400136WP 2003 3 24 ZW0A0303304 120030321A339701056060035M1 WIRE HARNESS DOUG DC9 DC983 3022083WP CABIN BROKEN A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139402W 53138 THE EMERGENCY FLOOR PATH LIGHTING HAD BROKEN WIRES AT ROW 16. REPLACED LIGHT HARNESS. CHECK-C 9-4-02. --CLOSED-- 2L72 4F RTA6WE 20030325000052003032500005NM 2003 3 25 03FDEA00342 120030321A2612FRFOE2811SX03 CONNECTOR BOEING727 727200 138407ENM NR 2 ENGINE FAILED A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25210FE 22932 ON SHORT FINAL APPROACH TO MEM. NR2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND FIRE BELL SOUNDED. NO INDICATION IN COCKPIT OTHER THAN LIGHT AND BELL. FOUND PIN A AND PIN E OF PLUG D352J SHORTING TOGETHER INTERMITTENTLY. REPLACED D352J IAW MFG STANDARD MAINTENANCE PRACTICES (SMP). CONNECTOR INSTALLED, SECURED, SAFETIED. OPS CHECKED NR2 ENG FIRE DETECTION I/A/W M/M CHAPTER 26-11-001-5 PAGE 1/2 OPS CHECKED NORMAL AT THIS TIME. 2L73 4F RTA3WE 20030325000082003032500008EA 2003 3 25 2003F00155 120030130A3260 WIRE HARNESS CNDAIRCL600 CL6002B16 1900305EA NLG PROX SWITCH SHORTED A UG8AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23241FB 5102 DURING CLIMB, WOW ID FAIL, NOSE GEAR WOULD NOT RETRACT. TROUBLESHOT SYSTEM FOUND THE NOSE GEAR PROXIMITY SWITCH HARNESS TO HAVE A SHORT. REPLACED THE NOSE GEAR PROXIMITY HARNESS IAW THE CHALLENGER CL601 MM CHAPTER 32-20-41. PERFORMED GEAR SWING AND OPERATIONAL CHECK. NO DEFECTS NOTED RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4F RTA21EA 20030325000132003032500013NM 2003 3 25 AWXA200300116 120030126A5312 BULKHEAD BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK 3 EACH .2500 INCH CRACKS WERE FOUND ON 178 FORWARD BULKHEAD, LEFT SIDE, WL 213, LBL 11. MAINTENANCE STOP DRILLED CRACKS, ENLARGED HOLES, AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED DOUBLERS AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 210, PG. 275. INSTALLED FILLET SEAL IAW B737-300 SRM 51-20-05. 2L72 4F4 FRTA16WE E2GL 20030325000182003032500018NM 2003 3 25 AWXA200300128 120030127A5315146N5089 FLOORBEAM BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 MAJOR REPAIR, DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON A MAIN CABIN FLOORBEAM AT BS 1640, BS 0 TO LBL 5. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED EXISTING REPAIR FROM FORWARD SIDE OF FLOORBEAM AND TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR ANGLE, FILLER, AND STRAP; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, FIG. 205, PG. 216-219. 2L72 4F4 FRTA2NM A12EU 20030325000192003032500019NM 2003 3 25 AWXA200300130 120030201A5310146N876935 FRAME BOEING757 7572S7 1384962NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 MAJOR REPAIR - DURING C-09 CHECK A 2 INCH CRACK WAS FOUND ON THE L-4 DOOR AREA CUSP INNER FRAME AT BS 1720, WL 208, LBL 70. MAINTENANCE WELDED CRACK AT THE INNER FRAME BS 1720 IAW AWA E.R. 19-5361-03035-SS2 . CAD PLATING WAS PERFORMED IAW E.O. 19-5361-03035-552, AND SOPM 20-42-10 PAGES 1-11. AREA WAS PRIMED AND PAINTED IAW SRM 51-20-01 PG 1. 2L72 4F RTA2NM 20030325000212003032500021NM 2003 3 25 AWXA200300133 120030210A2560P4010021 BATTERY BOEING737 7373Q8 1384670NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 EMERGENCY EVACUATION - DURING INSPECTION THE AFT GALLEY FLASHLIGHT BATTERY LIFE INDICATOR WAS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE AFT GALLEY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030325000272003032500027NM 2003 3 25 AWXA200300142 120030214A2781 MODULE BOEING737 737277 1384570NM FLAP/SLATS FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28184AW 22651 PHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF AT PHX EN ROUTE FOR TUS RECEIVED AMBER LEADING EDGE FLAP IN TRANSIT LIGHT ON FORWARD PANEL WHILE FLAPS SELECTED TO 2 UNIT; REJECTED TAKEOFF AT 50 KTS. AFTER TAXI OFF RUNWAY AND SITTING ON TAXIWAY, THE IN TRANSIT LIGHT WOULD ILLUMINATE INTERMITTENTLY. MAINTENANCE TROUBLESHOT AND PLACED SYSTEM ON MEL 27-4, COND. 1 "L/E FLAP/SLAT FORWARD PANEL LIGHT INOP". ORDERED M229 MODULE FLAP/SLAT POSITION INDICATING ACCESSORY UNIT. 2L72 4F RTA16WE 20030325000372003032500037EU 2003 3 25 AWXA200300154 120030204A5315D53112698200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM FR 20, RBL 8. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM FR 20, RBL 8; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG. 201, PG. 201-206. 2L72 4F RTA28NM 20030325000402003032500040EU 2003 3 25 AWXA200300159 120030206A5315D53112091200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM 6 INCHES FORWARD OF FR 18, RBL 49. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM FR 18, RBL 49; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG. 201, PG. 201-206. 2L72 4F RTA28NM 20030325000422003032500042NM 2003 3 25 AWXA200300166 120030201A5311651630087 FRAME BOEING737 73733A 1384673NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-18 CHECK A 7/8 INCH CRACK WAS FOUND ON BS 178 RT SIDE FRAME, PASSING THROUGH WL 207 COCKPIT FLOOR AREA.. MAINTENANCE REMOVED DAMAGED RT SIDE FRAME BS 178; FABRICATED A NEW REPLACEMENT FRAME; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1-3. 2L72 4F RTA16WE 20030325000472003032500047NM 2003 3 25 AWXA200300183 120030222A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28812AW 1178 FLIGHT CREW REPORTED THE LT FORWARD GALLEY HAND HELD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030325000482003032500048NM 2003 3 25 AWXA200300187 120030127A5320146N5318 WEB BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 DURING C-09 CHECK, EXFOLIATION CORROSION WAS FOUND ON SEVERAL AREAS OF SHEAR WEB BS 1681 TO BS 1720, RBL 60 TO LBL 60. MAINTENANCE REMOVED DAMAGED SHEAR WEB BS 1681 TO BS 1720, RBL 60 TO LBL 60; FABRICATED A REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-05, PG. 5-7. 2L72 4F RTA2NM 20030325000502003032500050NM 2003 3 25 AWXA200300204 120030223A3010 ANTI-ICE SYSTEM AIRBUSA319 A319132 3930340NM WING INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28818AW 1375 EN ROUTE FROM PIT TO PHX WING ANTI-ICE WENT INOPERATIVE AFTER NR 1 BLEED TRIP, DIVERTED TO CMH. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF WING ANTI-ICE SYSTEM PER AMM 30-11-00-05, ALL CHECKS WERE NORMAL. 2L72 4F RTA28NM 20030325000602003032500060NM 2003 3 25 AWXA200300223 120030301A33971012721 WIRE BOEING737 7373G7 1384595NM SEAT ROW 4 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT WAS HANGING BY WIRE FROM SEAT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030325000622003032500062NM 2003 3 25 AWXA200300225 120030302A33501012881 LIGHT AIRBUSA319 A319132 3930340NM SEAT ROW 3 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28825AW 1527 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030325000682003032500068NM 2003 3 25 AWXA200300232 120030306A2612 WARNING SYSTEM BOEING737 7373S3 1384711NM APU BAY FALSE ACTIVATIONA AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28315AW 23734 DURING CLIMB OUT, APU FIRE LIGHT ILLUMINATED, FOLLOWED QUICK REFERENCE HANDBOOK & DISCHARGED APU FIRE EXTINGUISHER BOTTLE. TURNED BACK & LANDED WITHOUT EVENT. MAINTENANCE INSPECTED APU AREA AND FOUND NO DAMAGE, PLACED APU ON MEL 49-1, COND. 1 "APU INOP". WHEN AIRCRAFT ARRIVED IN PHX MAINTENANCE PERFORMED AN IN DEPTH INSPECTION OF THE APU ASSEMBLY, TAILPIPE, AND SURROUNDING AREA, NO EVIDENCE OF FIRE OR DAMAGE WAS NOTED. REPLACED APU FIRE EXTINGUISHER BOTTLE AND YELLOW DISCHARGE DISK IAW BMM 26-22-11. DURING C-16 CHECK MAINTENANCE REMOVED AND REPLACED THE APU. 2L72 4F RTA16WE 20030325000712003032500071NM 2003 3 25 AWXA200300236 120030309A2560 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28307AW 24634 FLIGHT CREW REPORTED THAT THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030325000742003032500074NM 2003 3 25 AWXA200300240 120030218A5312651630083 FRAME BOEING737 7373S3 1384711NM 178 BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-11 CHECK A 1 INCH CRACK WAS FOUND IN RADIUS OF RT OUTER CHORD OF 178 BULKHEAD AT WL 207. MAINTENANCE CUTOUT DAMAGED SECTION OF RT OUTER FRAME, BULKHEAD 178, WL 207; FABRICATED A NEW SECTION OF FRAME AND SPLICE ANGLES PER SB 737-53A1173, FIG. 61; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5312-03057-KB1. 2L72 4F RTA16WE 20030325000802003032500080EU 2003 3 25 AWXA200300249 120030311A2932501310000 PRESSURE SWITCH AIRBUS320 A320231 3930325EU NR 1 ENGINE FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28622AW 054 ON CLIMB OUT FROM PHX EN ROUTE FOR BDL THE NR 1 ENGINE DRIVEN (GREEN) HYDRAULIC PUMP FAILED. TURNED BACK TO PHX, TOUCHED DOWN AT 144,000 LBS AT LESS THAN 100 FPM. MAINTENANCE TROUBLESHOT AND FOUND GREEN HYDRAULIC SYSTEM PRESSURE SWITCH (1074GK) DEFECTIVE. REMOVED AND REPLACED PRESSURE SWITCH (1074GK) IAW AMM 29-11-17-04. OPERATIONAL CHECK OF GREEN HYDRAULIC SYSTEM WAS GOOD. 2L72 4F RTA28NM 20030325000852003032500085NM 2003 3 25 03FDEA00346 120030323A3020355194310 SENSING ELEMENT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE NR 2 ENGINE DAMAGED A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO25619FE 48770 AFTER DEPARTURE AT TPE TURNED ON ANTI ICE (ENGINE NR 2 A-ICE), WE WERE IN ICING CONDITION, DESCENDED LOWERED AND RETURNED TO TPE. FACT 23MAR03 22:52 TPE R RECEIVED A/C PARTS AT 2110Z, REPLACED SENSING ELEMENTS D1-90 IAW MM 30-22-11-4, AND PERFORMED ANTI-ICE MANIFOLD ADJUSTMENT/TEST IAW MM 30-22-11-5, ALL SYSTEM FUNCTION CHECKED NORMAL. NR 2 ENGINE COWLING CLOSED AND PLATFORM SECURED AND LATCHED. OK FOR SERVICE. 2L73 4F4 FRTA22WE E13NE 20030325000862003032500086NM 2003 3 25 03FDEA00347 120030317A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CABIN SEAT TRACK AT LT X=27.5 STA 420-495 FOUND CORRODED. 2L73 4F4 FRTA22WE E13NE 20030325000882003032500088EU 2003 3 25 03083330 120030324A33501317 LAMP JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030325000912003032500091CE 2003 3 25 049124 120030324A24971293640293 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE CABIN FAILED A AMWAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE07126YV UE126 AFTER TAKE OFF FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 706,WHEN THE LANDING GEAR WAS SELECTED UP, SMOKE WAS DETECTED FROM THE RIGHT HAND CIRCUIT BREAKER PANEL. THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE STOPPED. THE CREW RETURNED TO FARMINGTON NEW MEXICO AND MADE A SAFE LANDING WITH NO FURTHER INCIDENT.THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED THE CIRCUIT BREAKER. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030325000972003032500097NM 2003 3 25 AWXA200300259 120030227A5210 RESERVOIR BOEING757 757225 1384959NM PAX DOOR DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK THE R-1 DOOR EMERGENCY POWER RESERVOIR PRESSURE WAS FOUND DEPLETED. MAINTENANCE SERVICED THE R-1 DOOR EMERGENCY POWER RESERVOIR IAW BMM 12-15-10, PG. 301-308. 2L72 4F RTA2NM 20030305000952003030500095EU 2003 3 5 HEEA084674 120030213A6420 BEARING BOLKMS105 BO105S 5626006EU TAIL ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U 050226 S678 WORN HUB BEARINGS. REPLACED WITH SERVICEABLE ASSY. 1G72 3U H3EU 20030306000042003030600004SW 2003 3 6 HEEA084717 120030217A632194501031 BRAKE ASSY BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 MAIN ROTOR BRAKE WORN, SLOW STOPPING UPON APPLICATION OF BRAKE. FOUND LININGS WORN. REPLACED LININGS. TESTED GOOD. 1G72 4U H4SW 20030306000062003030600006SW 2003 3 6 HEEA084719 120030217A632194501031 BRAKE ASSY BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 MAIN ROTOR BRAKE HAS WORN PUCKS. REPAIRED. 1G72 4U H4SW 20030306000092003030600009 2003 3 6 HEEA084722 420030217A2340AA21400 SIREN BELL 412 412 1182202SW PA SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 AFTER OPERATING FOR 15 MINUTES, SYSTEM QUITS WORKING, AFTER UNIT COOLS DOWN IT WILL WORK AGAIN. 1G72 4U H4SW 20030306000122003030600012SW 2003 3 6 HEEA084725 120030217A3246AB412050015109 SKID BELL 412 412 1182202SW MLG GOUGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 GOUGED NEAR AFT CROSSTUBE SADDLE AND HAS CORROSION IN VARIOUS PLACES. 1G72 4U H4SW 20030306000222003030600022 2003 3 6 HEEA084735 420030217A2340 SWITCH BELL 412 412 1182202SW INTERPHONE BOX DIRTY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 7906036 33150 INTERPHONE BOX IS SCRATCHY. FOUND S1 SELECTOR SWITCH NOISY. CLEANED SWITCH. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000242003030600024 2003 3 6 HEEA084737 420030217A2340 SWITCH BELL 412 412 1182202SW INTERPHONE BOX DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 8106973 33010 HOT MIC IN FM1 MIC SELECT POSITION. REPLACED S1 SELECTOR SWITCH, S6 AND S11 MONITOR SWITCHES, FACEPLATE, VOLUME AND SELECTOR KNOBS, Q9 TRANSISTOR AND C30 CAPACITOR. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000302003030600030SW 2003 3 6 HEEA084743 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 RT STEP WON'T GO UP. REPAIRED ACTUATOR. 1G72 4U H4SW 20030306000312003030600031SW 2003 3 6 HEEA084744 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 RT STEP INTERMITTENTLY WON'T GO UP. REPAIRED ACTUATOR. 1G72 4U H4SW 20030306000412003030600041SW 2003 3 6 HEEA084754 120030218A3210400052015101 STRAP BELL 407 407 1182206SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 RT AFT CROSSTUBE STRAP DAMAGED WHEN CROSSTUBE SHIFTED. REPLACED STRAP. 1G71 3U O H2SW 20030306000452003030600045SW 2003 3 6 HEEA084759 120030218A3210407030112103 FITTING BELL 407 407 1182206SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 FITTING WORN. REPLACED FITTING. 1G71 3U O H2SW 20030306000492003030600049SW 2003 3 6 HEEA084764 120030221A3212412050013115 FLOAT BELL 412 412 1182202SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 EMERGENCY FLOAT DOUBLER AROUND VALVE SEPARATED. 1G72 4U H4SW 20030306000502003030600050SW 2003 3 6 HEEA084765 120030221A3212412050013117 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 EMERGENCY FLOAT BAG LEAKING. 1G72 4U H4SW 20030306000512003030600051SW 2003 3 6 HEEA084766 120030221A3212412050013117 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 EMERGENCY FLOAT BAG LEAKING. 1G72 4U H4SW 20030306000572003030600057SW 2003 3 6 HEEA084772 120030221A3246412050016102 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 MLG SKID SHOE IS WORN. SCRAPPED. 1G72 4U H4SW 20030306000592003030600059SW 2003 3 6 HEEA084774 120030221A3212412050017135 COVER BELL 412 412 1182202SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 EMERGENCY FLOAT COVER IS TORN. 1G72 4U H4SW 20030306000602003030600060WP 2003 3 6 MWEA030123 120030305A275059304961 VANE DOUG DC9 DC981 3022081WP #2 & #3 FLAP DELAMINATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LEFT WING FIXED VANE LOCATED BETWEEN #2 FLAP BRACKET AND #3 FLAP BRACKET HAS AN AREA APPROXIMATELY 4" SQAURE OF DELAMINATION ON UNDERSIDE. -- HOT BOND REPAIRED VANE. 2L72 4F A6WE 20030306000642003030600064SW 2003 3 6 HEEA084775 120030221A7810 BRACKET BELL 412 412 1182202SW EJECTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K A431 36001 EXHAUST EJECTOR BRACKET CRACKED. REPAIRED. 1G72 4U H4SW 20030306000682003030600068SW 2003 3 6 HEEA084779 120030221A7810212061202010 DUCT BELL 412 412 1182202SW EXHAUST SYSTEM CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 CRACKED EXHAUST DUCT RT SIDE FLANGE WELD. REPAIRED. 1G72 4U H4SW 20030306000742003030600074SW 2003 3 6 HEEA084785 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 STEP ACTUATOR WILL NOT EXTEND. 1G72 4U H4SW 20030306000872003030600087SW 2003 3 6 HEEA084796 120030221A6730212076005111 SERVO BELL 412 412 1182202SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW036559Z 36019 MAIN ROTOR SERVO LEAKING FROM THE PILOT VALVE. REPAIRED. 1G72 4U H4SW 20030306000932003030600093SW 2003 3 6 HEEA084801 120030221A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 STARTER GENERATOR DRAGGING DURING START. 1G72 4U H4SW 20030306000972003030600097 2003 3 6 HEEA084805 420030221A2561 CLIP BELL 412 412 1182202SW LIFE VEST BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 CLIP FOR LIFE VEST STRAP BROKEN. 1G72 4U H4SW 20030306001062003030600106SW 2003 3 6 HEEA084813 120030221A2510412070820101 SEATBACK CUSHION BELL 412 412 1182202SW CREW SEAT WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 SEAT BACK CUSHION WEAK. REPAIRED. 1G72 4U H4SW 20030306001092003030600109SW 2003 3 6 HEEA084816 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 MAIN ROTOR HEAD ROD BEARING WORN BEARING. REPAIRED. 1G72 4U H4SW 20030306001112003030600111SW 2003 3 6 HEEA084818 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MAIN ROTOR HEAD HAS A WORN ROD BEARING. REPAIRED. 1G72 4U H4SW 20030306001152003030600115SW 2003 3 6 HEEA084821 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z4187 36019 MAIN ROTOR HEAD HAS A WORN ROD BEARING. 1G72 4U H4SW 20030306001182003030600118EA 2003 3 6 03064665 120030305A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27665BR 7534 During overnight maintenance, it was discovered that the l/h fwd overwing emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light assy. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030307000072003030700007NE 2003 3 7 HEEA084877 120030227A34120401277660 SENSOR SKRSKYS76 S76A 8143006NE OAT WILL NOT TEST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 NR 1 N1 GAUGE DID NOT PASS TACO CHECK, READING WAS LOW FOR OAT. 1G72 3U H1NE 20030307000102003030700010 2003 3 7 HEEA084880 420030227A3452066011560101 TRANSPONDER SKRSKYS76 S76A 8143006NE ALTIMETER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 NOT REPORTING ALTITUDE. REPLACED V101 CAVITY OSCILLATOR, ADJUSTED TO SPECS, REPAIRED. BENCH CHECK GOOD. 1G72 3U H1NE 20030307000142003030700014NE 2003 3 7 HEEA084884 120030227A3213 BEARING SKRSKYS76 S76A 8143006NE DRAG BRACE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792CH PHI117 760193 MLG STRUT DRAG BRACE HAS WORN BEARINGS. REPAIRED. 1G72 3U H1NE 20030307000152003030700015EA 2003 3 7 03066625 120030307A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 During overnight maintenance, it was discovered that the l/h aft exterior emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the light assy. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030307000232003030700023 2003 3 7 SWAA030504 420030305A25656567380 COVER BOEING737 7373H4 1384600NM L2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 AFT ENTRY DOOR EVACUATION SLIDE COVER LOOSE. SECURED SLIDE COVER PER MM. 2L72 4F RTA16WE 20030307000362003030700036NM 2003 3 7 SWAA030451 120030228A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030307000432003030700043NM 2003 3 7 SWAA030459 120030301A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW NR 2 AND ROW NR 22. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20030307000462003030700046 2003 3 7 SWAA030464 420030302A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20030307000552003030700055 2003 3 7 SWAA030443 420030226A256565C19901 CABLE BOEING737 737317 138447PNM AFT ENTRY DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE DAMAGED. REMOVED AND REPLACED SLIDE CABLE PER MM. 2L72 4F RTA16WE 20030307000572003030700057 2003 3 7 SWAA030445 420030226A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29761RR 27875 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030307000602003030700060NM 2003 3 7 SWAA030448 120030226A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030307000662003030700066NM 2003 3 7 SWAA030418 120030220A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 DURING SCHEDULED BC4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030307000732003030700073NM 2003 3 7 SWAA030487 120030304A57556546452 SPOILER BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D CHECK, FOUND NR 5 GROUND SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 5 GROUND SPOILER PER MM. 2L72 4F RTA16WE 20030307000762003030700076 2003 3 7 SWAA030490 420030304A25656557463 BRACKET BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE BIRT BAR ATTACH FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM. 2L72 4F RTA16WE 20030307000792003030700079 2003 3 7 SWAA030494 420030302A25656567380 COVER BOEING737 7373H4 1384600NM L2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 AFT ENTRY DOOR EVACUATION SLIDE COVER LOOSE. SECURED EVACUATION SLIDE COVER PER MM. 2L72 4F RTA16WE 20030307000812003030700081NM 2003 3 7 VNAA0302023 120030225A5200 CONTROL ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DOOR A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07461PS 3075 ENROUTE, THE CREW RECEIVED A MAIN CABIN DOOR RED WARNING PANEL LIGHT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND LANDED AT THE NEAREST SUITABLE AIRPORT, ILM. ON DESCENT INTO ILM, THE INDICATION WENT OUT AT FL 180. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND ADJUSTED THE DOOR CONTROL RODS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030307000832003030700083NM 2003 3 7 CALA0300097 120030214A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 344 BETWEEN LBL 36 AND RBL 12. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. 2L72 4F RTA16WE 20030307000842003030700084NM 2003 3 7 CALA0300099 120030223A5320 STRAP BOEING737 7373T0 1384582NM STA 793 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND R/H FLOOR SUPPORT STRAP CORRODED AT STA 793. THE FLOOR SUPPORT STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030307000882003030700088 2003 3 7 HEEA084889 420030227A3421501122402 GYRO SKRSKYS76 S76A 8143006NE VERTICAL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 NR 1 PITCH AND ROLL ACTUATORS KICKING IN FLIGHT. REPLACED VERT GYRO. 1G72 3U H1NE 20030307000982003030700098NE 2003 3 7 HEEA084899 120030227A32127625101101105 FLOAT SKRSKYS76 S76A 8143006NE NLG FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 NLG EMERGENCY FLOAT DOES NOT HOLD PRESSURE. 1G72 3U H1NE 20030307001102003030700110NM 2003 3 7 AALA20021897 120030102A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21677AN 29427 ORD - FIRST CLASS EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. SECURED LOOSE CONNECTOR UNDER FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001172003030700117NM 2003 3 7 AALA20030059 120030113A3350 PIN BOEING757 757223 1384957NM CONNECTOR NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 12D INOPERATIVE. RESEATED PIN AT EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001212003030700121EU 2003 3 7 AALA20030087 120030121A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW211436A 11426 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AFT ROW 11D MISSING. INSTALLED EMERGENCY EXIT PATH LIGHTING AFT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030307001232003030700123WP 2003 3 7 AALA20030095 120030109A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 TUL - FOUND CUSP INBOARD OF SERVICE DOOR FRAME HAS CORROSION. INSTALLED CUSP DOUBLER INBOARD OF SERVICE DOOR AREA APPROX STATION 160-200 PER AARD 53-20. (M) 2L72 4F A6WE 20030307001242003030700124WP 2003 3 7 AALA20030096 120030114A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 TUL - FOUND CORROSION ON SKIN AND DOUBLER UNDER LOWER AFT CORNER OF AFT LAV PANEL. REPAIRED PER ESO PO559 DATED 1-10-03. (M) 2L72 4F A6WE 20030307001302003030700130WP 2003 3 7 AALA20030102 120030120A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21258AA 49288 TUL - FOUND LEFT CUSP CRACKED. REPAIRED CRACKED CUSP, STOP DRILLED AND DOUBLER PER SRM 53-01 FIG 4. (M) 2L72 4F A6WE 20030307001322003030700132WP 2003 3 7 AALA20030104 120030123A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21497AA 49735 TUL - FOUND CORROSION ON RIGHT CUSP STATION 550. INSTALLED DOUBLER PER AARD 53-00-00-2. (M) 2L72 4F A6WE 20030307001352003030700135WP 2003 3 7 AALA20030107 120030124A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21562AA 49344 DFW - DURING OVERNIGHT MAINTENANCE, AFT CATWALK OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACTS FOR AFT OVERHEAD CATWALK AND RECHARGED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030307001372003030700137NE 2003 3 7 HEEA084904 120030228A6710389500090310 BEARING SKRSKYS76 S76A 8143006NE M/R FLT CONTROLSWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911UK 760275 STIFF BEARING AND MISSING TEFLON. REPLACED 2 BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030307001482003030700148NM 2003 3 7 AALA20030152 120030127A2421GEN5103 IDG BOEING767 767323 1385205NM LT ENGINE FAILED A AALAK NONE J WARNING INDICATION CRCRUISE 1 SW21370AA 25197 MIA - DURING FLIGHT, THE LEFT GEN DRIVE LIGHT FLICKERED. SOON THE LEFT GEN DRIVE LIGHT BEGAN TO FLICKER. THIS CONTINUED FOR A PERIOD AND LEFT DRIVE WAS DISCONNECTED. LEFT IDG VERIFIED INOPERATIVE NO SPARE IDG AT MAD DEFERRED PER MEL 24-01 AUTH 01-455DC-A IDG 1 NAD 2 SERVICED. APU OIL VERIFIED FULL IDG DEC ENTERED ON MIC SHEET. REMOVED AND REPLACED IDG ON LEFT ENGINE, REQUIRES OP AND LEAK CHECK. LEFT IDG OP CHECK GOOD. LEAK CHECK OK. (M) 2L72 4F RTA1NM 20030307001492003030700149NM 2003 3 7 AALA20030154 120030204A3350 LIGHT BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21609AA 27447 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 17D BROKEN. REPLACED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030307001502003030700150NM 2003 3 7 AALA20030159 120030205A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21360AA 24041 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 24B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR ON SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001522003030700152EA 2003 3 7 03029662 120030129A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27662BR 7526 DURING MAINTENANCE INSPECTION, FLOOR EMERGENCY TRACK LIGHTING IN ROWS 2-5 WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY TRACK LIGHTING, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030307001562003030700156EA 2003 3 7 03046662A 120030215A2163 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE A/C BAY DIRTY A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27662BR 7526 DURING CLIMB, THE CREW REPORTED THAT BOTH AIR CONDITIONING PACKS HAD OVER-TEMPED CAUSING SMOKE IN THE CABIN AND COCKPIT. MAINTENANCE PERSONNEL REMOVED, CLEANED AND REINSTALLED THE DUCT TEMPERATURE SENSORS. AN OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEMS WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030307001602003030700160EA 2003 3 7 03048627 120030217A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27627BR 7233 EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED FLOOD LIGHT OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2L72 4F4 FRTA21EA E15NE 20030307001702003030700170NM 2003 3 7 AALA20030051 120030112A3397 WIRE BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE ON SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001752003030700175NM 2003 3 7 AALA20030065 120030114A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21381AN 25450 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT 3B INOPERATIVE. REPAIRED EMERGENCY EXIT PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001762003030700176NM 2003 3 7 AALA20030066 120030114A3397 WIRE BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21381AN 25450 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT 2B INOPERATIVE. REPAIRED EMERGENCY EXIT PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001772003030700177 2003 3 7 HEEA084908 420030228A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 AFCS ACTUATOR KICKING. 1G72 3U H1NE 20030307001792003030700179WP 2003 3 7 AALA20030068 120030116A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21241AA 49254 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN BY SEAT 21F INOPERATIVE. REPLACED UPPER EMERGENCY EXIT SIGN MODULE AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030307001822003030700182EU 2003 3 7 AALA20030071 120030117A3350 CONTACTOR FOKKERF28 F28MK0100 4990807EU LT WING CONTAMINATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW211450A 11459 DFW - DURING OVERNIGHT MAINTENANCE, BOTH OVERWING EMERGENCY EXIT LIGHTS ON LEFT WING BODY FAIRING INOPERATIVE. CLEANED OFF DE-ICE FLUID FROM CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030307001852003030700185NM 2003 3 7 AALA20030074 120030118A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21370AA 25197 SFO - DURING OVERNIGHT MAINTENANCE, LEFT WING SLIDE EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE DURING TEST. SECURED LEFT WING SLIDE EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001892003030700189WP 2003 3 7 AALA20030078 120030118A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21586AA 53249 DFW - DURING OVERNIGHT MAINTENANCE, LOWER OVERWING EMERGENCY EXIT SIGN AT ROW 21 AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030307002032003030700203SO 2003 3 7 C2XA03BT035 120030302A3200 PIN EMB 145 EMB145 3260210SO BENT A C2XAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW2714959 145091 EWR---CO2409, CREW REPORTED, "NOSEWHEEL GEAR DOORS WILL NOT RETRACT, VIBRATE....MAINTENANCE FOUND PIN#31 AT CANNON PLUG P0778 TO BE BENT, REPAIRED PIN #31 IAW EMB145 AMM #20-00-00. PERFORMED GEAR SWING IAW EMB145 AMM #32-30-00, OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030308000042003030800004GL 2003 3 8 RAIA00302050 220030218A7421CH318981 IGNITER EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03808HK 145157 310131 LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED "A" IGNITER AND PLACED ON DEFERRAL THE "B" IGNITER, OPS CK OK. 2L72 4F4 FRTT00011ATTE6CH 20030308000092003030800009EU 2003 3 8 RAIA00302057 120030226A32305004VC CONNECTOR AEROSPATR72 ATR72202 8680940EU DETERIORATED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03723TE 283 5520-STL- LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED CONNECTOR 5004VC, OPS CK OK. 2H72 4T RTA53EU 20030308000102003030800010 2003 3 8 RAIA00302058 420030228A34257003360948 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03571HK1273719 41090 5493-STL- #2 AHRS FAILED. MAINTENANCE REMOVED AND REPLACED #2 AHRS, OPS CK OK. 2L72 4T RTA41NM 20030310000042003031000004SO 2003 3 10 C2XA03SH051 120030310A530013500400019 STRINGER EMB 145 EMB145LR 3260212SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 RIGHT BETWEEN FRAMES 52 TO 53 WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGED AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030310000062003031000006 2003 3 10 HEEA084915 420030227A34221113025 INDICATOR BELL 412 412 1182202SW HSI SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 HSI INDICATOR POPS CIRCUIT BREAKER. 1G72 4U H4SW 20030310000072003031000007 2003 3 10 HEEA084916 420030227A34211113034 INDICATOR BELL 412 412 1182202SW ATTITUDE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 ATTITUDE INDICATOR TURN AND SLIP BALL NOT CENTERED. 1G72 4U H4SW 20030310000092003031000009 2003 3 10 HEEA084918 420030227A34211113034 INDICATOR BELL 412 412 1182202SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 ATTITUDE INDICATOR RT FLAG SLOW TO PULL. 1G72 4U H4SW 20030310000112003031000011 2003 3 10 HEEA084920 420030227A34211113034 INDICATOR BELL 412 412 1182202SW ATTITUDE SPINNING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 ATTITUDE INDICATOR SPINS CONTINOUSLY, WILL NOT STABILIZE. 1G72 4U H4SW 20030310000142003031000014SW 2003 3 10 HEEA084923 120030227A7931209070262101 INDICATOR BELL 412 412 1182202SW ENG OIL PRESS FLUCTUATES E O OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 INDICATOR DISPLAYING FLUCTUATING OIL PRESSURE INDICATIONS. 1G72 4U H4SW 20030310000152003031000015SW 2003 3 10 HEEA084924 120030227A7931209070262101 INDICATOR BELL 412 412 1182202SW ENG OIL PRESSUREREADS HIGH E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW032258F 33073 ENGINE OIL PRESSURE READS HIGH. REPAIRED. 1G72 4U H4SW 20030310000162003031000016SW 2003 3 10 HEEA084925 120030227A7931209070262101 INDICATOR BELL 412 412 1182202SW ENG OIL PRESSUREMALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 HIGH PRESSURE INDICATION. REPAIRED INICATOR. 1G72 4U H4SW 20030310000172003031000017SW 2003 3 10 HEEA084926 120030227A6420 BEARING BELL 412 412 1182202SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 A579 36003 TAIL ROTOR HEAD HAS WORN FEATHERING BEARINGS. REPAIRED. 1G72 4U H4SW 20030310000182003031000018SW 2003 3 10 HEEA084927 120030227A6420 BLADE BELL 412 412 1182202SW T/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S A960 36002 TAIL ROTOR HEAD HAS BLADE DAMAGE. REPAIRED. 1G72 4U H4SW 20030310000222003031000022SW 2003 3 10 HEEA084931 120030227A6520212040003023 GEARBOX BELL 412 412 1182202SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 GEARBOX HAS EXCESSIVE BACKLASH AT FWD COUPLING. REPAIRED. 1G72 4U H4SW 20030310000252003031000025SW 2003 3 10 HEEA084934 120030227A6520212040468001 CASE BELL 412 412 1182202SW T/R GEARBOX DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 RECEIVED HIGH BACKLASH READINGS WHEN GEARBOX WAS REASSEMBLED 0.012, 0.0125 AND 0.0125 INCH. MAXIMUM BACKLASH ALLOWED IS 0.011 INCH. 1G72 4U H4SW 20030310000282003031000028SW 2003 3 10 HEEA084937 120030227A7120 BEARING BELL 412 412 1182202SW TRIPOD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ENGINE MOUNT TRIPOX ASSY BEARINGS WORN. SCRAPPED. 1G72 4U H4SW 20030310000312003031000031SW 2003 3 10 HEEA084940 120030227A7120 BEARING BELL 412 412 1182202SW BIPOD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 BIPOD ASSY BEARINGS WORN. SCRAPPED. 1G72 4U H4SW 20030310000322003031000032SW 2003 3 10 HEEA084941 120030227A7120 BEARING BELL 412 412 1182202SW BIPOD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 BIPOD ASSY BEARINGS WORN. REPAIRED. 1G72 4U H4SW 20030310000372003031000037WP 2003 3 10 DHL2003802002 120030309A2611 LAMP DOUG DC8 DC873 302199CWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01802DH 46076 1) #3, #8, AND #9 MAIN CARGO SMOKE DETECTOR WILL NOT TEST.2) RELAMPED SMOKE DETECTOR #3 AND #8 - OPS CHECKED GOOD. DEFERRED #9 SMOKE DETECTOR PER DC8 MEL 26-6-1. CONTROL #12224 CAT. "C".3) REF. DMI #12224 #9 SMOKE DETECTOR INOPERATIVE.4) REPLACED LAMP ON #9 SMOKE DETECTOR PER M/M 26-10-5. OPS NORMAL. THIS CLEARS DMI #12224. 2L74 4F RT4A25 20030310000442003031000044SW 2003 3 10 HEEA084949 120030227A6220214001347005 ACTUATOR BELL 412 412 1182202SW M/R HEAD BINDING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 ACTUATOR ROTARY LATERAL CYCLIC BINDING. 1G72 4U H4SW 20030310000482003031000048SW 2003 3 10 HEEA084952 120030227A6340214074280107 DETECTOR BELL 412 412 1182202SW RPM LIMIT MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW033893L 33006 RPM LIGHT FLICKERS AT 100 PERCENT. 1G72 4U H4SW 20030310000592003031000059SW 2003 3 10 HEEA084963 120030227A6220412010216105 BEARING BELL 412 412 1182202SW M/R HEAD ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D3285 33076 MAIN ROTOR HEAD BEARING ROUGH. REPAIRED. 1G72 4U H4SW 20030310000632003031000063SW 2003 3 10 HEEA084967 120030227A3213412030437103 CAP BELL 412 412 1182202SW CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 CROSSTUBE CAP RUBBER WORN. REPAIRED. 1G72 4U H4SW 20030310000642003031000064SW 2003 3 10 HEEA084968 120030227A3213412030437103 CAP BELL 412 412 1182202SW MLG CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 CROSSTUBE CAP RUBBER WORN. REPAIRED. 1G72 4U H4SW 20030310000812003031000081 2003 3 10 HEEA084985 420030227A34427021450601 COMPUTER BELL 412 412 1182202SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 WEATHER RADAR SYSTEM SHOWS FAILED ON SCREEN. WON'T PAINT TARGETS. 1G72 4U H4SW 20030310000822003031000082 2003 3 10 HEEA084986 420030227A34427021450601 COMPUTER BELL 412 412 1182202SW WX RADAR SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 WEATHER RADAR RT/ANT RADAR INOPERATIVE. 1G72 4U H4SW 20030310000862003031000086 2003 3 10 HEEA084990 420030227A344580511400003 CONTROL UNIT BELL 412 412 1182202SW COLLISION AVOID INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 AIR COLLISION AVOIDANCE CONTROL UNIT DOESN'T POWER UP INTERMITTENTLY. SENT TO GOODRICH AVIONICS FOR WARRANTY REPAIR. 1G72 4U H4SW 20030310000962003031000096 2003 3 10 HEEA085001 420030227A2300DMC633A ANTENNA BELL 412 412 1182202SW FM COMMS FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032258F 33073 FM COMMS ANTENNA FAILED FUNCTION CHECK. SCRAPPED. 1G72 4U H4SW 20030310001012003031000101 2003 3 10 HEEA085006 420030227A2561PHI10088 COVER BELL 412 412 1182202SW LIFE VEST WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 LIFE VEST COVER HAS WORN VELCRO. 1G72 4U H4SW 20030310001042003031000104 2003 3 10 HEEA085009 420030227A2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 LIFE VEST LEAKS. 1G72 4U H4SW 20030310001052003031000105 2003 3 10 HEEA085010 420030227A2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 LIFE VEST HAS WORN VELCRO AND TORN LIGHT. 1G72 4U H4SW 20030310001092003031000109SW 2003 3 10 HEEA085016 120030227A243239563001 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N 28106 MAIN BATTERY WEAK. TO BE SENT TO VENDOR FOR REPAIR. 2G72 4U H10SW 20030310001122003031000112 2003 3 10 HEEA085019 420030228A34570110050400 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E O OTHER O OTHER NRNOT REPORTED 1 SW038590X 51494 GPS DOES NOT DISPLAY HEADING INFORMATION. 1G71 3U H2SW 20030310001162003031000116SW 2003 3 10 HEEA085023 120030228A6230206010450119FM SWASHPLATE BELL 206 206L3 1182108SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610Y10418 51419 SWASHPLATE WORN. REPLACED SLEEVE SLIDER BEARING 206010459001 DUE TO WORN; PIN 206010408001, S/N TIFS142 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030310001182003031000118NM 2003 3 10 CALA0300102 120030307A5230 SKIN BOEING737 7373T0 1384582NM C-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916310 23361 INSPECTION FOUND A 1/2" CRACK IN C-2 DOOR SKIN AT UPPER CORNER OF THE CUTOUT FOR THE DOOR HANDLE. HANDLE EXCEEDS TRAVEL IN CLOSING DIRECTION ALSO. A DOUBLER WAS INSTALLED IAW SRM 52-00-01. THE DOOR HANDLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030310001202003031000120WP 2003 3 10 CALA0300104 120030307A5330 SKIN DOUG DC9 DC981 3022081WP STA 1338 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND A 0.01" CRACK IN FUSELAGE SKIN AT STA 1338, LONGERON 10R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220. 2L72 4F A6WE 20030310001292003031000129NM 2003 3 10 AWXA200300234 120030307A3350ABS0374A24 CABLE AIRBUSA319 A319132 3930340NM SEAT ROW 14 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW0 0 1088 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030310001312003031000131NM 2003 3 10 EIA2003035 120030227A5300UNK SPLICE BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 FUSELAGE RIGHT SIDE INTERIOR CORROSION ALONG SKIN LONGITUDINAL SPLICE AT STRINGER 19R, FROM STA 1760-2180 CORRECTIVE ACTION: REMOVED DAMAGE, NDT AREA & VISUALLY IINSPECT, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-169-2 Rev A 2L74 4F A20WE 20030310001452003031000145NM 2003 3 10 EIA2003044 120030228A5300UNK STRAP BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 STA 1581.5, THERE ARE TWO MIS-DRILLED HOLES IN HE LAP SKIN AT STRINER 19R. CORRECTIVE ACTION: NDT HOLES, INSTALL FREEZE PLUGS, FAB'D AND INSTALLED REPAIR STRAP PER ECRA 481-53-187-2 Rev A. 2L74 4F A20WE 20030310001542003031000154NM 2003 3 10 EIA2003022 120030227A5315 FLOORBEAM BOEING747 747132 1384882NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 BS 360 AT RBL 68 APPROX 2" UP FROM LOWER CHORD HAS A SHARP DENT WITH CREASED ON FLOOR BEAM WEB. REMOVED DAMAGED AREA PER B747 SRM 51-1-001. FABRICATED REPAIR PARTS: -1 DOUBLER, -2 TRIPLER, -3 FILLER & -4 FILLER PER ECRA 481-53-185-2. ALODINED PER B747 SRM 51-10-01 AND PRIMED PER SOPM 20-44-04. INSTALLED REPAIR PARTS PER B747 SRM 51-30-02 PG. 57-58B & ECRA 481-53-185-2. APPLIED A FILLET SEAL PER SRM 51-10-06. APPLIED AV-8 PER B747 SRM 51-10-02. 2L74 4F RTA20WE 20030310001552003031000155NM 2003 3 10 EIA2003023 120030227A5320 ANGLE BOEING747 747132 1384882NM FUSELAGE GOUGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 INNER CHORD OF UPER DECK FLOORBEAM TO FRAME INTERFACE HAS 2 EA DEEP GOUGES BS 380, RBL 80. REPAIRED ANGLE BS 380 RBL PER ECRA 481-53-186-2 2L74 4F RTA20WE 20030310001582003031000158NM 2003 3 10 EIA2003037 120030227A5300UNK STRINGER BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 AT STATION 1601, ABOUT 3 INCHES ABOVE STRINGER 19R, THERE IS ONE (1) MIS-DRILLED HOLE CORRECTIVE ACTION: NDT HOLE, FAB'D AND INSTALLED REPAIR PARTS PER ECRA 481-53-187-2 Rev A. 2L74 4F A20WE 20030310001622003031000162NM 2003 3 10 EIA2003027 120030228A5300UNK INTERCOSTAL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Top Side of W.W. (Nose) between STA 260-280 Intercostal at LBL 20 cracked. CORRECTIVE ACTION: Removed and Replaced per ECRA 481-53-170-2, B747 51-30-02, Pgs 1-3, & 21-32. Installed per B747 SRM 51-30-02 5-9 & 38-60, plus 51-10-06, Pgs 1-30 2L74 4F A20WE 20030311000082003031100008SW 2003 3 11 HEEA085032 120030228A6510206040346021 HANGER ASSY BELL 206 206L3 1182108SW TAIL ROTOR DRIVECORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 FWD BEARING DUST COVER OFF. BEARING ROUGH. REPLACED FWD HANGER 206040346021 DUE TO CORROSION IN BORES AND AFT HANGER 206040355003 DUE TO CORROSION IN BORES. REPAIRED. 1G71 3U H2SW 20030310000612003031000061SW 2003 3 10 HEEA084965 120030227A6220412010216105 BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MAIN ROTOR HEAD BEARING WORN. REPAIRED. 1G72 4U H4SW 20030401001002003040100100NM 2003 4 1 DHL2003755004 120030306A3260 WARNING LIGHT BOEING727 727225 1384077NM NLG DOOR FALSE ACTIVATIONA DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01755DH 21857 RED DOOR LIGHT ON FRONT PANEL, AND NOSE GEAR DOOR LIGHT ON S/O'S ANNUNCIATOR PANEL ILLUMINATED. VERIFIED NOSE DOORS CLOSED AND FAIRED. TRANSFERRED TO MEL 12203 PER MEL 32-1. PLACARDS INSTALLED. 2L73 4F A3WE 20030310000672003031000067SW 2003 3 10 HEEA084971 120030227A3213412030437103 CAP BELL 412 412 1182202SW MLG CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 MLG CROSSTUBE CAP RUBBER WORN. REPAIRED. 1G72 4U H4SW 20030310000742003031000074 2003 3 10 HEEA084978 420030227A34166221205004 ALTIMETER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 ALTIMETER DH LIGHT IS INOPERATIVE. 1G72 4U H4SW 20030310000762003031000076 2003 3 10 HEEA084980 420030227A22157001484 ACTUATOR BELL 412 412 1182202SW YAW CONTROL STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 ACTUATOR YAW CONTROL STUCK, WILL NOT MOVE. 1G72 4U H4SW 20030310000802003031000080 2003 3 10 HEEA084984 420030227A34427007700614 INDICATOR BELL 412 412 1182202SW WX RADAR SYS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0333008 36004 WEATHER RADAR SYSTEM RANGE MARKING NOT READABLE. 1G72 4U H4SW 20030310000852003031000085 2003 3 10 HEEA084989 420030227A344580511400003 CONTROL UNIT BELL 412 412 1182202SW COLLISION AVOID MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 SKYWATCH WON'T INTERFACE WITH RADAR. SENT TO GOODRICH AVIONICS FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030310000912003031000091 2003 3 10 HEEA084996 420030227A34578143902240B GPS BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 GPS WILL NOT ACQUIRE DATABASE. CLEANED DATA CARD CONNECTOR AND REPLACED ON/OFF VOLUME KNOB. PAINTED FACEPLATE. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030310000942003031000094 2003 3 10 HEEA084999 420030227A34168800T ENCODER BELL 412 412 1182202SW ALTIMETER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 GPS INDICATES EXTERNAL ALTIMETER IN ERROR. REPAIRED. 1G72 4U H4SW 20030310000952003031000095NE 2003 3 10 HEEA085000 220030227A7420CH5339901 LEAD BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE IGNITER CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 IGNITER LEAD CHAFED. 1G72 4U4 U H4SW E22EA 20030310000972003031000097 2003 3 10 HEEA085002 420030227A3452DMNI5062 ANTENNA BELL 412 412 1182202SW ATC TRANSPONDER CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 ANTENNA HAS CORROSION AND TRANSPONDER REPORTED WEAK BY ATC. SCRAPPED. 1G72 4U H4SW 20030310000982003031000098SW 2003 3 10 HEEA085003 120030227A3212D24922113 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 FLOAT BAG ASSY LEAKS. 1G72 4U H4SW 20030310001032003031000103 2003 3 10 HEEA085008 420030227A2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 LIFE VEST LEAKS. 1G72 4U H4SW 20030310001072003031000107 2003 3 10 HEEA085012 420030227A2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN DAMAGED E O OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 LIFE VEST HAS A BROKEN CLIP. 1G72 4U H4SW 20030310001102003031000110SW 2003 3 10 HEEA085017 120030227A7714AG44A TACH GENERATOR BELL 212 212 1181420SW ENGINE CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0327805 31106 TRANSMISSION RPM LIGHT FLASHING AND AUDIO HORN GOING OFF. FOUND TACH GEN FULL OF OIL AND WATER ON SEAL AROUND BACKPLATE. REPLACED WITH SERVICEABLE PART. 1G71 4U H4SW 20030311000092003031100009NM 2003 3 11 HNAA0300012 120030305A2100167301101 APU DHAV DHC8 DHC8201 2809001NM TAIL FOULED A HNAAO OTHER O OTHER TOTAKEOFF 1 EA07983HA12778824 478 After take off and selecting bleeds on, the FO and FA reported smelling an odor followed by the lavatory smoke detector sounding. Selected bleeds off, the odor went away and the smoke detector extinguished. Inspected aircraft bleed system, ran aircraft for 15 minutes with bleeds on. Ran duct temp up above 65 degrees for 15 minutes. No odor noticed or smoke detector went off. Suspect oil in bleed ducts due to previous work on APU. 2H72 4T RTA13NM 20030311000132003031100013SW 2003 3 11 HEEA085034 120030228A3246206053184101 SKID BELL 206 206L3 1182108SW LT MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N 51512 LT SKID TUBE HAS CORROSION BEYOND LIMITS. REPLACED TUBE. 1G71 3U H2SW 20030311000222003031100022SW 2003 3 11 HEEA085043 120030228A3210206323202 SUPPORT BELL 206 206L4 1182110SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 MLG SUPPORT HAS CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE SADDLE. 1G71 3U NCH2SW 20030311000282003031100028SW 2003 3 11 HEEA085045 120030228A300023007827 VALVE BELL 206 206L3 1182108SW ANTI ICE SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 ANTI ICE VALVE INOPERATIVE. REPLACED WITH SERVICEABLE VALVE. 1G71 3U H2SW 20030311000302003031100030GL 2003 3 11 HEEA085047 220030228A7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL DROOP COMPEN FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 13418 51029 GOVERNOR WOULD NOT RESPOND TO DROOP COMPENSATION ADJUSTMENTS. SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030311000382003031100038GL 2003 3 11 HEEA085054 220030228A72506899081 COMBUSTION LINER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 HARD STARTING ON LIGHT OFF, WORN FUEL NOZZLE FERRULE AND LINER CRACKED. IN REPAIR. 1G71 3U3 U H2SW E1GL 20030311000412003031100041SW 2003 3 11 HEEA085057 120030228A3212206050248117 FLOAT BELL 206 206L3 1182108SW MLG FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036160Y 51609 FLOAT BAG ASSY FAILED PRESSURE TEST. 1G71 3U H2SW 20030311000442003031100044EA 2003 3 11 COMA0360140 120030305A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01916CA 7014 FLIGHT 5730 GEAR DISAGREE WARNING, NLG DID NOT RETRACT.ADJUSTED THE NLG CENTERED, PROXIMITY SENSOR GAP. 2L72 4F RTA21EA 20030311000462003031100046 2003 3 11 HEEA085061 420030228A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038592X 51508 NR 1 VHF HAS A BUZZ AND NR 2 VHF HAS A SQUEAL IN THE HEADSET. SHOP REPAIR. 1G71 3U H2SW 20030311000492003031100049SW 2003 3 11 HEEA085064 120030228A2432RG206 BATTERY BELL 206 206B3 1181506SW MAIN MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032275Y14 3626 VOLTAGE DROPS DOWN TO 24 VOLTS AFTER AIRCRAFT SITS FOR ANY EXTENDED PERIOD OF TIME. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030311000532003031100053SW 2003 3 11 HEEA085067 120030228A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610Y356 51419 MAIN BATTERY DEAD. 1G71 3U H2SW 20030311000572003031100057EU 2003 3 11 HEEA085071 120030227A641010531980 BLADE BOLKMS105 BO105S 5626006EU TAIL ROTOR ERODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038199J S826 T/R BLADE HAS PAINT EROSION. 1G72 3U H3EU 20030311000602003031100060EU 2003 3 11 HEEA085076 120030227A3340D3040E LANDING LIGHT BOLKMS105 BO105S 5626006EU EXTERIOR INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 LANDING LIGHT INTERMITTENTLY INOPERATIVE. IN SHOP REPAIR. 1G72 3U H3EU 20030311000612003031100061EU 2003 3 11 HEEA085077 120030228A6510 BEARING BOLKMS105 BO105S 5626006EU T/R DRIVESHAFT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037170D4304 949 S840 TAIL ROTOR DRIVESHAFT HAS A WORN BEARING. REPAIRED. 1G72 3U H3EU 20030311000652003031100065EU 2003 3 11 HEEA085082 120030228A6321704A34130044 HANDLE AEROSPAS355 AS355* EU ROTOR BRAKE STIFF E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 ROTOR BRAKE HANDLE IS STIFF AND HARD TO MOVE. 1G72 3U H11EU 20030311000662003031100066NE 2003 3 11 IO5R084695 220030224A73149A2045 PUMP UROCOPEC135 EC135P2 EU PWA PW206 PW206A NE FUEL SYSTEM INOPERATIVE H IO5RO OTHER O OTHER NRNOT REPORTED 1 FS01552BA713 190 FUEL PUMP INOP REMOVED AND REPLACED. 1G72 3U3 U H88EU E42NE 20030311000682003031100068EU 2003 3 11 IO5R084697 120030224A3110614764031 INDICATOR AEROSPAS355 AS355* EU COCKPIT INOPERATIVE H IO5RO OTHER O OTHER NRNOT REPORTED 1 FS01557CB 3431 N2 INDICATOR INOPERATIVE REMOVED AND REPLACED UNIT 1G72 3U H11EU 20030311000692003031100069SW 2003 3 11 JJWA084103 120030210A243615891F VOLT REGULATOR BELL 206 206B 1181511SW DC SYSTEM DEFECTIVE H JJWAO OTHER O OTHER NRNOT REPORTED 1 FS0125PM 1839 VOLTAGE REGULATOR FAILED ON TAKE OFF, CAUSED BOTH COMM RADIOS TO FAIL WITH SMOKE OBSERVED FROM COLLINS 251 COMM RADIO. REPLACED REGULATOR, SERVICED GILL BATTERY & OVERFLOW BOTTLE, ADJUSTED REG TO 27.5 VDC, BORROWED RADIOS TO USE WHILE COMM ARE REPAIR, NO OTHER DAMAGE FOUND. 1G71 3U H2SW 20030311000712003031100071EU 2003 3 11 AWXA200300246 120030305A5552D5598141100000 FITTING AIRBUS320 A320231 3930325EU ELEVATOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK A 5/16 INCH CRACK WAS FOUND ON THE LT ELEVATOR NR 3 HINGE POINT FITTING AT ELEV STA 2707. MAINTENANCE REMOVED AND REPLACED THE LT ELEVATOR NR 3 HINGE POINT FITTING AT ELEV STA 2707 IAW AMM TASK 55-16-42-000-001, & 55-16-42-400-001. 2L72 4F RTA28NM 20030311000912003031100091EA 2003 3 11 COMA0360137 120030309A2910848847 PUMP CNDAIRCL600 CL6002B19 1900309EA 3A WEAK A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01936CA18310 7043 FLIGHT 5546 GEAR DISAGREE WARNING SELECTED DOWN.REPLACED HYDRAULIC PUMP 3A. 2L72 4F RTA21EA 20030311001072003031100107WP 2003 3 11 MWEA030126 120030305A532199365841 FLOORBOARD DOUG DC9 DC981 3022081WP STA 1147 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOORBOARED BETWEEN SEAT TRACKS #3 AND #4 AT STATION 1147 IS DENTED. -- REPAIRED DENT. 2L72 4F A6WE 20030311001092003031100109NM 2003 3 11 0300446744 120030228A5312 WEB BOEING747 747212F NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01644NW 24177 During "H" check found crack in four frame webs on #1 pylon. Repaired per EA 67-165045. 2L74 4F RTA20WE 20030312000442003031200044CE 2003 3 12 2003F00121 120030206A3210 LANDING GEAR CESSNA402 402B 207590PCE RIGHT COLLAPSED E O OTHER O OTHER LDLANDING 1 GL273796C 402B0803 UPON LANDING, DURING ROLL OUT, THE RT MLG COLLAPSED. THE PILOT WAS INTERVIEWED AND STATED THAT HE HAD ALL THREE GREEN DOWN AND LOCKED INDICATION. UPON INVESTIGATION OF THE LANDING GEAR, ALL DAMAGE WAS LIMITED TO THE RETRACTION/EXTENSION LINKAGE, SPECIFICALLY THE SIDE BRACE BELLCRANK AND WHERE IT ATTACHES TO THE UPPER TRUNNION. NO EVIDENCE OF SIDE LOADING COULD BE FOUND. SINCE THE PILOT STATED THAT HE HAD GEAR SAFE INDICATION, NO CAUSE CAN BE DETERMINED FOR THE GEAR TO UNLOCK AND COLLAPSE. 1L72 3O A7CE 20030312000452003031200045CE 2003 3 12 2003F00123 120030124A2410ALV9510 ALTERNATOR CESSNA310 310R 2074245CE RT ENGINE DISLODGED E H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL27500FS 310R0630 THE PILOT NOTED THAT THE RIGHT HAND ALTERNATOR HAD FALLEN OFF LINE DURING CRUISE FLIGHT. UPON LANDING, MAINTENANCE WAS NOTIFIED AND IT WAS DETERMINED THAT THE ALTERNATOR WAS INOPERATIVE. UPON REMOVAL OF THE ALTERNATOR, IT WAS DISCOVERED THAT THE ALTERNATOR DRIVE GEAR AND THE ALTERNATOR CLUTCH HAD SEVERE DAMAGE. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT THE FORWARD ALTERNATOR DRIVE BEARING HAD FAILED CAUSING THE CLUTCH AND DRIVE GEAR TO MISS ALLIGN. THIS CAUSED SEVERE METAL CONTAMINATION AND THE ENGINE HAD TO BE REPLACED. 1L72 3O 3A10 20030312000462003031200046CE 2003 3 12 2003F00125 120030306A7922639305 VERNATHERM BEECH 58 58 1152740CE CONT O550 IO550C SO ENGINE OIL MALADJUSTMENT E O OTHER W INADEQUATE Q C NRNOT REPORTED 1 NE015565D370 TH1552 815462 OIL TEMP CONTROL VALVE (VERNATHERM) IMPROPERLY ASSEMBLED CREATING CHRONICALLY LOW OIL TEMPERATURES WHICH WERE UNNOTICED IN WARM WEATHER BUT BECAME EVIDENT IN VERY COLD WEATHER. TCM SPEC IS GASKET SURFACE TO BASE OF ADJUSTING NUT TO BE 1.807 +/- .003 INCHES. THIS UNIT FOUND AT ABOUT 1.850 INCH. 1L72 3O3 O 3A16 E3SO 20030312000492003031200049WP 2003 3 12 CALA0300111 120030310A5320 ANGLE DOUG DC9 DC981 3022081WP STA 1338 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND AFT PRESSURE BULKHEAD ANGLE CORRODED AT STA 1338, LONGERON 28R TO 30. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30. 2L72 4F A6WE 20030312000502003031200050NM 2003 3 12 UPS03240271 120030218A2750 CARRIAGE BOEING727 727108C 1384039NM R/H WING WBL203 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C+SI ON REMOVAL OF SEALANT FROM THE INNER BORE OF NO.6 FLAP TRACK CARRIAG E SPINDLE,EXCESSIVE CORROSION IS EVIDENT. NO.6 FLAP TRACK CARRIAGE REPLACED IAW OHM 57-58-02. 2L73 4F A3WE 20030409000052003040900005NM 2003 4 9 AWXA200300238 120030309A521069762242 COVER BOEING737 7373S3 1384711NM L-1 DOOR BROKEN A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28315AW 23734 DURING CLIMB OUT FROM IND EN ROUTE FOR PHX A LOUD SQUEAL DEVELOPED FROM THE FORWARD SIDE OF THE L-1 DOOR, DIVERTED TO CMH FOR REPAIR. MAINTENANCE FOUND THE L-1 DOOR LOWER HINGE COVER PINCHED AROUND DOOR SEAL. REMOVED HINGE COVER, PLACED ON CDL 52-10-1, COND. C-CHECK MAINTENANCE REPLACED L-1 DOOR LOWER HINGE COVER ASSEMBLY IAW BMM 52-11-00, PG. 401, LEAK CHECK WAS GOOD. 2L72 4F RTA16WE 20030312000582003031200058NM 2003 3 12 AWXA200300250 120030310A53302024T363 SKIN BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW0 0 23219 PHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON L/H FUSELAGE BETWEEN BS 500D AND BS 520, BELOW STRINGER 12 L/H. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN; PERFORMED EDDY CURRENT INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG. 202. 2L72 4F RTA16WE 20030312000622003031200062NM 2003 3 12 AWXA200300255 120030307A531569353654 ANGLE BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW0 0 24633 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1" CRACK WAS FOUND ON THE UPPER ANGLE OF INTERCOSTAL AT BS 380 TO BS 400, BL 0. MAINTENANCE REMOVED THE UPPER ANGLE ON INTERCOSTAL FROM BS 380 TO BS 400; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3, & 38, FIG. 8. 2L72 4F RTA16WE 20030310001132003031000113 2003 3 10 HEEA085020 420030228A2300100005430 HEADSET BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 HEADSET MIC BROKEN. REPLACED HEADSET. 1G71 3U H2SW 20030310001222003031000122WP 2003 3 10 CALA0300109 120030309A5330 SKIN DOUG DC9 DC981 3022081WP STA 1338 GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT JACK POINT, STA 1338. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 9. 2L72 4F A6WE 20030310001272003031000127NM 2003 3 10 UPS03240265 120030218A2750 CARRIAGE BOEING727 727108C 1384039NM #5 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI ON REMOVAL OF SEALANT FROM THE INNER BORE OF SPINDLE ON FLAP TRACK C ARRIAGE #5 EXCESSIVE CORROSION IS EVIDENT #5 FLAP TRACK CARRIAGE REPLACED IAW OHM 57-58-02 2L73 4F A3WE 20030310001422003031000142NM 2003 3 10 EIA2003041 120030228A5300UNK FASTENER BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 IMPROPER FASTENER ON LAP SEAM AT BS 755 AND STRINGER 44R, ON R/H SIDE OF FUSELAGE NEXT TO REPAIRED AREA. CORRECTIVE ACTION: REPAIRED IMROPER FASTENER ON LAP SEAM AT BS 755, STRINGER 44R PER ECRA 481-53-179-2 Rev A 2L74 4F A20WE 20030310001432003031000143NM 2003 3 10 EIA2003042 120030228A5300UNK STRINGER BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 AT STA 1416, CENTER OF STRINGER 19R, THERE IS (1) MIS-DRILLED HOLE IN LAP SKIN. CORRECTIVE ACTION: REPAIRED PER ECRA 481-53-187-2, PART 5. INSTALLED STRINGER TEE PER SRM 51-30-02, Pg 5-58. 2L74 4F A20WE 20030310001482003031000148NM 2003 3 10 EIA2003015 120030226A5300UNK SKIN PANEL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 R/H Lower fuselage at STA 400, lower lap skin has evidence of damage and corrosionCORRECTIVE ACTION: Repaired area per ECRA 481-53-182-2 2L74 4F A20WE 20030310001512003031000151NM 2003 3 10 EIA2003019 120030227A5300UNK STRAP BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Lap repairs from STA 1770-1960 at Stringer 12R reguires an additional strap. CORRECTIVE ACTION: Installed external strap per ECRA 481-53-169-2 Rev A 2L74 4F A20WE 20030310001632003031000163NM 2003 3 10 EIA2003028 120030228A5300UNK INTERCOSTAL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Nose W.W. STA 300-320, Intercostal at LBL 10 Cracked. CORRECTIVE ACION: Removed and replaced Intercostal @ STA 300-320 per ECRA 481-53-170-2 & SRM B747 51-10-06, Pgs 1-30 2L74 4F A20WE 20030311000052003031100005SW 2003 3 11 HEEA085029 120030228A6420 BEARING BELL 407 407 1182206SW T/R HEAD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH3732 TR102698 51436 TAIL ROTOR HEAD ASSY HAS WORN FEATHERING BEARINGS. REPAIRED. 1G71 3U O H2SW 20030311000152003031100015SW 2003 3 11 HEEA085036 120030228A2820206063604105 TUBE BELL 206 206L3 1182108SW FUEL DIST CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03205FC 51130 FUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED. 1G71 3U H2SW 20030311000182003031100018SW 2003 3 11 HEEA085039 120030228A2810206064633101 FUEL CELL BELL 206 206L3 1182108SW FUSELAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03205FC 51130 FUEL CELL HAS A LARGE BLISTER INSIDE ON THE LOWER BACK EDGE. 1G71 3U H2SW 20030311000202003031100020SW 2003 3 11 HEEA085041 120030228A2436206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW DC SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 VOLTAGE INTERMITTENTLY SPIKES. SENT VOLTAGE REGULATOR IN FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20030311000252003031100025EU 2003 3 11 YENA200305 120030309A3230EO242A2A0 RELAY AIRBUS320 A320232 3930326EU A YENAO OTHER J WARNING INDICATION LDLANDING 1 EA15527JB 1557 On climb out got L/G LGCIU-1 fault on ECAM, C/B tripped on overhead. reset LGCIU-1 C/B as per MX Control. All ECAM indication went back to normal. At gear down selection into PBI go same LGCIU-1 fault, but no C/B tripped, got C/B tripped rear panel N-R ECAM but on tripped C/B visable. Accomplished manual L/G extension procedure.Removed and Replaced L/G control lever (6GA) per 32-31-11-000. Ops Check normal. T/S lever for continuity at pins D/K had open caused to power to LGCU-1 trouble shoot futher and found no power to relay 48GA which controls the safety valve. Replaced relay and control lever. LGCIU-1 cleared. 2L72 4F RTA28NM 20030311000352003031100035GL 2003 3 11 HEEA085051 220030228A73135233600 FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 FUEL NOZZLE PRODUCING NUMEROUS ABORTED STARTS DUE TO NO LIGHT OFF. SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030311000422003031100042SW 2003 3 11 HEEA085058 120030228A3212OHSS2061001 COVER BELL 206 206L3 1182108SW EMERGENCY FLOAT DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 FLOAT COVER IS TORN AND DETERIORATED. 1G71 3U H2SW 20030311000452003031100045 2003 3 11 HEEA085060 420030228A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW NR 2 VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038592X 51508 NR 2 VHF WILL NOT RECEIVE WHEN ROTARY AND TOGGLE SWITCH ARE SELECTED TOGETHER. SHOP REPAIR. 1G71 3U H2SW 20030312000642003031200064 2003 3 12 QXEA0300336 420030308A3160 CIRCUIT BREAKER CNDAIRCL600 CL6002C10 1390015EA A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09611QX 10041 BIL- ON FLIGHT 2481 (BIL-SEA), JUST AFTER TAKE-OFF, THE CAPTAINS PRIMARY AND MULTIFUNCTION DISPLAYS WENT BLANK. COPILOTS INDICATIONS WERE FINE. RETURNED TO THE FIELD AT BIL AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE L/H DCPC ESS FEED CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20030313000212003031300021NM 2003 3 13 0303001 120030311A3310FA8T5CW LAMP KORRY BOEING737 737230C 1384472NM COCKPIT LOOSE A MJYAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07767TW NSN 20258 SMOKE/ELEC FUMES FROM MASTER CAUTION ANNUNCIATOR PANEL ON CAPTAINS SIDE. STOPPED AFTER 2 MINUTES.FOUND GLARESHIELD FLOURESCENT TUBE NEAR CAPTAINS MASTER CAUTION PANEL DISPLACED FROM SOCKET. THIS ARCED WITH SLIGHT MOVEMENT. CLEANED SOCKET AND TUBE AND RESEATED AND SECURED. OPS CHECKED GOOD. 2L72 4F A16WE 20030313000272003031300027SW 2003 3 13 ALG2003F00026 120030213A2612898426 SENSING ELEMENT BELL 214 214ST 1182106SW NR 1 ENGINE INOPERATIVE E ALGAO OTHER L NO TEST NRNOT REPORTED 1 SW03390AL 28198 DURING RUN-UP CHECKS. NR 1 ENGINE FIRE DETECTION SYSTEM WOULD NOT TEST. 2G72 4U H10SW 20030313000692003031300069NM 2003 3 13 03FDEA00193 120030303A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON 950D FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACES RBL 25, LBL 25, WL 208. REMOVED CORROSION FROM FLOORBEAM BS 950D, RBL 10.5, FOUND OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGED SECTION OF UPPER CHORD BS 950D LBL 37-RBL 37. FABRICATED REPAIR PARTS, INSTALLED IAW SRM 53-10-8 FIG 3, SRM 51-30-2 PG 13 &14. 2L73 4F4 F A3WE E2EA 20030313000702003031300070NM 2003 3 13 03FDEA00194 120030303A5310 CREASE BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION (C55-224-01) ON TOP OF FCD CREASE BEAM BS 325-40 LBL 60. REMOVED CORROSION ON TOP OF CREASE BEAM BS 325-340, OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED CREASE BEAM PER SRM 51-30-2, 51-10-2, 51-30-5. 2L73 4F RTA3WE 20030313001002003031300100CE 2003 3 13 AWK2003F00002 120030212A2140589200541 PUMP BEECH 58 58 1152740CE CONT O550 IO550* SO HEATER INTERMITTENT B AWKRO OTHER O OTHER NRNOT REPORTED 1 WP25658DG264 TH2017 FOUND FUEL PUMP INTERMITTENT. PUMP WOULD WORK ON THE GROUND BUT WHEN THE AIRCRAFT WAS FLOWN THE HEATER WOULD SHUT DOWN AFTER A SHORT TIME. IT FINALLY FAILED ON THE GROUND IMMEDIATELY AFTER THE AIRCRAFT HAD FLOWN. THIS IS THE SECOND AIRCRAFT WE HAVE HAD IN THE PAST WEEK TO HAVE THIS PROBLEM. SAME MODEL AND ONLY 19 SERIAL NUMBERS APART. 1L72 3O3 O 3A16 E3SO 20030313001022003031300102CE 2003 3 13 AZO2003F00000 120030227A521057111454 SKIN CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO CABIN DOOR CRACKED B AZORO OTHER O OTHER NRNOT REPORTED 1 GL133247M 414A0828 A CRACK HAD DEVELOPED IN THE LOWER CABIN DOOR FRAME ASSY AT THE AFT HINGE ATTACH AREA. THE CRACK WAS 2.75 INCHES LONG, RUNNING FORE AND AFT IN THE LOWER RADIUS WHERE THE SKIN AND STRUCTURE ARE RIVETED TOGETHER. THE FRAME ASSY WAS REMOVED AND REPLACED WITH A NEW PART. THE DOOR DOES HAVE THE EXTENDER KIT INSTALLED, BUT THE CRACK DOES NOT APPEAR TO HAVE BEEN CAUSED BY THIS. POSSIBLY A FAILED DOOR CABLE AT A PREVIOUS TIME APPLIED ADDITIONAL STRESS TO THIS AREA. 1L72 3O3 O A7CE E8CE 20030313001042003031300104CE 2003 3 13 BSY2003F00007 120030123A3260JE73 DOWNLOCK SWITCH CESSNA310 310R 2074245CE CONT O520 IO520MB 17032SO MLG BROKEN E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL075215C 310R1515 277901R HAD NO RIGHT GEAR DOWN AND LOCK INDICATION. FOUND DOWN AND LOCK SWITCH ACTUATOR ARM BROKEN, REMOVED AND REPLACED ARM. OPS CHECKED GOOD. 1L72 3O3 O 3A10 E5CE 20030313001112003031300111CE 2003 3 13 EAT2003F00000 120030201A5410 SPAR CESSNA404 404 2075901CE CONT O520 GTSIO520F 17032SO LT NACELLE DAMAGED B EATRK NONE O OTHER ININSP/MAINT 1 GL09167SA 4040639 DURING A REPAIR FOR A EXHAUST BRACKET AND LOWER SKIN REPAIRS ON THE LEFT ENGINE NACELLE HEAT DAMAGE WAS FOUND ON THE LFET FORWARD SPAR BETWEEN WING STA CWS88-10555555. THIS DAMAGE IS MOST LIKELY DUE TO A CRACKED EXHAUST OUTLET OFF THE TURBO DIRECTING HOT EXHAUST GASES AT THE FACTORY HEAT SHIELD. THE FORWARD SPAR HAD A ELECTRICAL CONDUCTIVITY TEST DONE AND THE WEB IACS PERCENT WAS BEYOND LIMITS. A FORWARD WEB SPLICE REPAIR WAS PROVIDED. THIS DAMAGE LIKELY OCCURRED BEFORE THE EXHAUST AD WAS ISSUED, BUT WAS NEVER FOUND DUE TO THE LIMITED ACCESS TO THIS AREA. 1L72 3O3 ORTA25CE E7CE 20030313001142003031300114CE 2003 3 13 FPI2003F00005 120030206A323398820152 ACTUATOR CESSNA210 T210N 2073456CE CONT O520 TSIO520* 17040SO LANDING GEAR CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO156611C16586 21063930 C/W SEB 01-2, INSPECTED ACTUATORS FOR CRACKS, FOUND CRACKS, REMOVED FROM SERVICE. 1H71 3O3 O 3A21 E8CE 20030313001212003031300121SW 2003 3 13 FTU2003F00003 120030214A2917EA1563 REGULATOR GULSTM690TP 695A 7630519SW GARRTTTPE331TPE331* 01514WP LT NACELLE FAILED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE0579PH 16 96029 HYDRAULIC REGULATOR WAS INSTALLED IN THIS AIRCRAFT AS A OVERHAULED, EXCHANGED. THIS UNIT FAILED DURING TAKEOFF, WHICH PREVENTED HYDRAULIC PRESSURE TO BUILD UP TO SYSTEM PRESSURE. UNIT WAS REMOVED AND REPLACED BY THE OWNERS ORIGINAL REGULATOR AFTER IT WAS OVERHAULED BY AN OUTSIDE VENDOR. OPERATIONAL CHECK OF LANDING GEAR PERFORMED, ALL FUNCTIONS NORMAL. FAILED UNIT WAS RETURNED TO VENDOR FOR WARRANTY CONSIDERATION. 1H72 4T3 T 2A4 E2WE 20030313001672003031300167WP 2003 3 13 AALA20030122 120030128A253046700017 COFFEEMAKER DOUG DC9 DC982 3022082WP GALLEY MALFUNCTIONED A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21447AA 49473 DFW - FLT 1607 - ON TAXI OUT DFW, NR 4 FLIGHT ATTENDANT IN REAR OF AIRCRAFT REPORTED A LOUD FLASH/BANK AND SMOKE FROM AFT GALLEY. GALLEY POWER WAS TURNED OFF AND FLIGHT ATTENDANTS REPORTED SMOKE DIMINISHED. ALSO, FLIGHT ATTENDANTS REPORTED A WHITE POWDER COVERING WORK TABLE, NO ABNORMAL INDICATIONS IN COCKPIT. REPLACED COFFEE MAKER AND RAILING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313001682003031300168EU 2003 3 13 AALA20030124 120030131A3350ABS0203B SWITCH AIRBUS300 A300B4605R 3930308EU CABIN FAULTY A AALAO OTHER O OTHER CRCRUISE 1 SW2140064 507 EWR - FLT 882 - EN ROUTE MIA-EWR, DURING CRUISE, EMERGENCY EXIT LIGHTS FLASHING IN FLIGHT. LANDED EWR WITHOUT INCIDENT. REPLACED EMERGENCY EXIT TEST SWITCH AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030313001702003031300170WP 2003 3 13 AALA20030126 120030131A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21450AA 49476 TUL - FOUND CORROSION SEAT TRACK NR 6 STATION 216 TO 219 TOP FORWARD END. REMOVED CORROSION PER SRM 51-10-3, REMOVAL WITH IN MANUAL LIMITS. TREATED AND PRIMED PER 51-10-3. (M) 2L72 4F A6WE 20030313001732003031300173WP 2003 3 13 AALA20030129 120030131A5310 WINDOW FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21450AA 49476 TUL - FOUND STATION 1098 LEFT SIDE WINDOW FRAME CRACKED. REPAIRED PER AARD 53-10-00-25. (M) 2L72 4F A6WE 20030311000512003031100051EA 2003 3 11 COMA0360133 120030306A2910601R752863 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA SYSTEM 1 LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01967CA 7134 FLIGHT 5176 HYDRAULIC SYSTEM #1, LOW WARNING MESSAGE.REPLACED HYDRUALIC LINE TUBE ASSY. 2L72 4F RTA21EA 20030311000522003031100052SW 2003 3 11 HEEA085066 120030228A2432RG222 BATTERY BELL 407 407 1182206SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH320 51436 MAIN BATTERY WEAK. 1G71 3U O H2SW 20030311000542003031100054SW 2003 3 11 HEEA085068 120030228A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS56 51506 MAIN BATTERY, NO VOLTS. 1G71 3U H2SW 20030311000582003031100058EU 2003 3 11 HEEA085073 120030227A2435230331141 BRUSHES BOLKMS117 BK117A1 5626010EU STARTER GEN FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC13530 15712 7152 STARTER-GENERATOR WON'T START. REPLACED 4 EACH BRUSHES DUE TO WORN. REPAIRED. 1G72 3U H13EU 20030311000592003031100059EU 2003 3 11 HEEA085074 120030227A79314011001 INDICATOR BOLKMS105 BO105S 5626006EU TRIPLE OIL PRESSFLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 NR 1 ENGINE OIL PRESSURE INDICATOR FLUCTUATED INTERMITTENTLY IN FLIGHT. 1G72 3U H3EU 20030311000842003031100084EA 2003 3 11 COMA0360135 120030309A2150 ACM CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01941CA 7050 FLIGHT 5892 AFTER T/O - BURNING ODOR IN COCKPIT AND CABIN.INSPECTED AIRCRAFT, NO DEFECTS NOTED, FLIGHT CHECK SATISFACTORY. 2L72 4F RTA21EA 20030311000952003031100095EA 2003 3 11 COMA0360138 120030309A27507805013 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA INST PANEL MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01934CA13706 7042 FLIGHT 5532 FLAPS FAILED AT 20 DEGREES DURING LANDING.REPLACED THE FLAP SELECTOR LEVER. 2L72 4F RTA21EA 20030311001102003031100110WP 2003 3 11 0300459614 120030219A5312 FORMER DOUG DC9 DC932 3022066WP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614NW 47128 During "H" check found crack in outboard end of aft pressure bulkhead horizontal former at Z=34 and X=40. Repaired per EA 96-194267. 2L72 4F A6WE 20030312000392003031200039CE 2003 3 12 0020 120030303A3210508100324 TORQUE KNEE BEECH 90 E90 1152914CE PWA PT6 PT6A60 52043NE RT CRACKED E CIEAK NONE O OTHER ININSP/MAINT 1 NM0363BV 748 LW256 DURING COMPLIANCE OF SB 32-3134 AND AD 2002-01-10, RIGHT LANDING GEAR UPPER TORQUE KNEE WAS FOUND TO BE CRACKED AT PROTRUSION OF CENTER LUG. THIS UNIT HAD BEEN INSPECTED MULTI TIMES PRIOR TO THIS INSPECTION AND PASSED THOSE INSPECTIONS. UNITS EXACT TOTAL TIME AND TOTAL LANDINGS IS UNKNOWN, BUT IS IN EXCESS OF 6000 HOURS AND 6000 LANDINGS. UNIT HAD BEEN INSPECTED 748.4 HOURS AND 953 LANDINGS AND 18 MONTHS PRIOR TO THIS INSPECTION. NOTE: AD 2002-01-10 AND SB 31-3134 HAVE DIFFERENT COMPLIANCE INTERVALS. INDICATES TORQUE KNEES ARE TO BE INSPECTED IAW SB 32-3134, WHICH COULD RESULT IN CONFUSION. EITHER SB OR THE AD SHOULD BE AMENDED TO MAKE THE COMPLIANCE INTERVALS SAME, EITHER BY HOURS OR BY LANDINGS. 1L72 3T4 T 3A20 E4EA 20030312000522003031200052NM 2003 3 12 UPS03240273 120030219A2750 CARRIAGE BOEING727 727108C 1384039NM R/H WING WBL 348CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C+SI NO.7 FLAP TRACK CARRIAGE HAS PITTING COROSION ON BEARING MOUNT HOLE. FLAP TRACK CARRIAGE REPLACED IAW SB 27-112. 2L73 4F A3WE 20030312000562003031200056WP 2003 3 12 ABXA030113 120030303A5700995753613 FLANGE DOUG DC9 DC941 302207NWP LEFT WING SHEARED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23958AX 47760 FLAP INBOARD FIXED VANE CENTER TWO CAM ATTACH FITTINGS ON FLAP LEADING EDGE WERE SHEARED. REPLACED FITTINGS (9957536-13 AND 9957536-7) IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030312000612003031200061NM 2003 3 12 AWXA200300254 120030228A53156545834107 STRAP BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW0 0 24633 MCN - MAJOR REPAIR - DURING C-14 CHECK A 5/16" CRACK WAS FOUND ON STRAP, LOWER SURFACE OF FLOOR BEAM, BS 344, LBL 49. MAINTENANCE REMOVED DAMAGED AREA OF STRAP; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13, PG. 1-3, FIG. 1. 2L72 4F RTA16WE 20030313000792003031300079EU 2003 3 13 136311 120030228A2421 GENERATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE LT ENGINE MALFUNCTIONED A UHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL1735SZ 35 508 FLIGHT 4492 PIT-TTN, APPROXIMATELY 2 MINUTES AFTER STARTING THE LT ENGINE, THE LT DC GENERATOR WENT OFFLINE AND WOULD NOT RESET. A/C RETURNED TO GATE IN PIT. PIT MX INSPECTED LT DC GEN CONNECTIONS AND WIRING. PERFORMED GROUND RUN OF LT ENGINE. OPERATIONAL CHECKS WERE GOOD, COULD NOT DUPLICATE DISCREPANCY. A/C RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030313000852003031300085NE 2003 3 13 M7K2003F00001 220030206A7210430123507 LIMITER SNIAS 350 AS350BA 8680817EU LYC LTS101LTS101600A3 41560NE ENG REDUCT GB FAILED A M7KAO OTHER O OTHER NRNOT REPORTED 1 WP1957717 1479 1334 LE43402CE PILOT REPORTED THAT ON RETURN FLIGHT AT NORMAL CRUISE POWER WITH NO CONTROL INPUT NG AND NR SPEEDS SUDDENLY DROPPED APPROXIMATELY 3 PERCENT AND RAPIDLY RECOVERED WITH A SLIGHT OVERSHOOT BEFORE RETURNING TO STEADY STATE. THIS OCCURRED SEVERAL TIMES OVER A .7 HOUR FLIGHT. REPLACEMENT OF THE OVERSPEED LIMITER CORRECTED THIS DEFECT AS CONFIRMED BY OPERATIONAL CHECK FLIGHTS TO CONFIRM A REPEATABLE DEFECT AND THAT AFTER LIMITER REPLACEMENT DEFECT WAS CORRECTED. 1G71 3U3 UNCH9EU E5NE 20030313001012003031300101CE 2003 3 13 AWK2003F00003 120030212A2140589200541 PUMP BEECH 58 58 1152740CE CONT O550 IO550* SO HEATER INTERMITTENT B AWKRO OTHER O OTHER NRNOT REPORTED 1 WP255096R174 TH1996 TROUBLESHOT HEATER SYSTEM, FOUND INTERMITTENT ELECTRIC FUEL PUMP, HEATER ALSO BACKFIRES PERIODICALLY WHEN STARTING. THIS IS THE SECOND AIRCRAFT WE HAVE HAD IN THE PAST WEEK TO HAVE THIS PROBLEM. SAME MODEL AND ONLY 19 SERIAL NUMBERS APART. 1L72 3O3 O 3A16 E3SO 20030313001102003031300110CE 2003 3 13 DBCA122D1 120030124A32601003810061 UPLOCK SWITCH BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA LT MAIN OUT OF RIG E DBCAO OTHER O OTHER NRNOT REPORTED 1 GL13884PG BB91 AFTER DEPARTING MDW PILOT SELECTED LANDING GEAR UP. LANDING GEAR RETRACTED AND LOCKED BUT (IN TRANSIT) LIGHT IN GEAR HANDLE REMAINED ILLUMINATED. CREW DIVERTED TO MKE. AIRCRAFT WAS PLACED ON JACKS AND LANDING GEAR RETRACTION TEST WAS ACCOMPLISHED. FOUND LEFT HAND MAIN UPLOCK SWITCH OUT OF RIG. ADJUSTED SWITCH. RAN 5 RETRACTION CYCLES. OPERATIONS NORMAL. 1L72 4T4 T A24CE E4EA 20030313001162003031300116SO 2003 3 13 FQA2003F00000 120030213A71608624534 AIR BOX PIPER PA44 PA44180 7104402SO LYC O360 O360A1H 41514EA CARBURETOR CRACKED B FQARO OTHER O OTHER NRNOT REPORTED 1 WP07304PA1053 4496123 L3857336A CARBURETOR HEAT BOX CRACKS WHERE AIR INTAKE AND HEAT INTAKE FLANGE MOUNTS TO BOX. MIXTURE CONTROL BRACKET CRACKED. CARBURETOR HEAT CONTROL CABLE BRACKET CRACKING AT HARDWARE MOUNTING HOLES. POTENTIAL TO CAUSE FOD TO CARBURETOR AND/OR ENGINE IS HIGH. 1L72 3O3 O A19S0 E286 20030313001172003031300117SO 2003 3 13 FQA2003F00001 120030213A78108620376 BAFFLE PIPER PA44 PA44180 7104402SO LYC O360 O360A1H 41514EA NR 4 CYLINDER CRACKED B FQARO OTHER O OTHER NRNOT REPORTED 1 WP07304PA1053 4496123 L3857336A BAFFLE CRACKS UNDER DOUBLER THAT SUPPORTS OIL COOLER. CRACKS START IN BEND RADIUS AND RUN TO RIVETS. THESE CRACKS ARE BETWEEN 1 AND 2 INCHES LONG IN TWO LOCATIONS AND HAVE THE POTENTIAL TO LOOSE ALL OIL COOLER SUPPORT. 1L72 3O3 O A19S0 E286 20030313001222003031300122WP 2003 3 13 FTU2003F00004 220030220A7412103784005B EXCITER GULSTM690TP 690B 7630516SW GARRTTTPE331TPE331* 01514WP LEFT ENGINE FAILED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE05690GS11 11363 EXCITER BOX HAD INTERMITTENT FAILURE AFTER ONLY BEING IN SERVICE FOR 11.3 HOURS. THIS UNIT WAS ORIGINALLY A MFG BLUE LABELED REMANUFACTURED PART. INSTALLED ANOTHER OVERHAULED UNIT, OPS CHECKED SYSTEM, NO PROBLEMS FOUND. THIS UNIT RETURNED TO VENDOR FOR POSSIBLE WARRANTY CONSIDERATION. 1H72 3T3 T 2A4 E2WE 20030313001352003031300135WP 2003 3 13 AALA20030082 120030119A32225963254501 STRUT DOUG DC9 DC982 3022082WP NLG BENT A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21418AA 49329 LGA - FLT 317 - EN ROUTE LGA-ORD, AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE UP IN FLIGHT. UNABLE TO RETRACT LANDING GEAR. RETURNED LGA AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR STRUT PISTON AND SEALS. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313001362003031300136WP 2003 3 13 AALA20030083 120030116A2824 COUPLING DOUG DC9 DC983 3022083WP RT WING DISCONNECTED A AALAE ENGINE SHUTDOWN F FLT CONT AFFECTED CRCRUISE 1 SW21566AA 49348 FSD - FLT 1887 - EN ROUTE ORD-SEA, CENTER TANK AT 12,500 LBS, LT MAIN TANK AT 9,400 LBS AND BOOST PUMPS ON, CROSSFEED CLOSED. THE RT MAIN FUEL QUANTITY WAS DECREASING FROM 9,400 LBS. RT MAIN QUANTITY DECREASED 3,000 LBS IN 30 MIN. AILERON TRIM WAS INCREASING CONFIRMING FUEL IMBALANCE. INSPECTION OF THE RT WING INFLIGHT DID NOT INDICATE LEAK. RT ENGINE WAS SHUT DOWN. LANDED FSD WITHOUT INCIDENT. NO EXTERNAL FUEL LEAKS NOTED. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FOR UNWANTED FUEL TRANSFER RT WING TANK TO CENTER TANK. RECONNECTED GAMMA COUPLING AND SECURED. FILLED RT WING TANK, FOUND NO TRANSFER BACK TO CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030313001372003031300137WP 2003 3 13 AALA20030085 120030120A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217514A 49891 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 30D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313001392003031300139NM 2003 3 13 AALA20030093 120030122A2560P2070003001 FLASHLIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21758AN 32637 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT BY L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT BY L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030313001482003031300148SO 2003 3 13 R2J2003F00003 120030204A57309562306 SKIN PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO WING CRACKED B R2JRK NONE O OTHER ININSP/MAINT 1 EA21113DK5533 347870151 DURING ANNUAL INSPECTION, INSPECTOR FOUND 2 EA .750 INCH CRACKS AT WS 124.6B RIVET. FURTHER INSPECTION FOUND 3 CRACKS IN PN 3743301 RIB AT SOME WS CRACKS EXCEEDED 1 INCH IN LENGTH, ALSO AT THE RIVET HOLES CRACKS REPAIRED IAW APPROVED DATA. CAUSE OF CRACKING, DUE TO AIRCRAFT AGE AND DESIGN. 1L72 3O3 O A7SO E9CE 20030313001632003031300163EU 2003 3 13 AALA20030117 120030127A28411411KID01 INDICATOR AIRBUS300 A300B4605R 3930308EU COCKPIT FAULTY A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2150051 459 BOS - FLT 989 - EN ROUTE BOS-MIA, LEFT OUTER FUEL QUANTITY STARTED DROPPING AFTER TAKEOFF ON ECAM AND FUEL QUANTITY PANEL. RETURNED BOS AND LANDED WITHOUT INCIDENT. REPLACED FUEL QUANTITY INDICATOR. SUMPED LEFT OUTER FUEL TANK. SUMP OF FUEL QUANTITY BITE SHOWED NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030313001652003031300165NM 2003 3 13 AALA20030120 120030128A5312 BULKHEAD BOEING757 757223 1384957NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21664AA 25298 TUL - FOUND MID BULKHEAD OUTBOARD FORWARD HOLE CRACKED. REPAIRED MID BULKHEAD PER ECO 90309 DATED 1/27/2003. (M) 2L72 4F RTA2NM 20030313001882003031300188WP 2003 3 13 AALA20030148 120030202A3350P4010051111 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21442AA 49468 SAN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 21-33 ON SEAT AISLE INOPERATIVE. REPLACED AFT AND MID EMERGENCY EXIT LIGHT BATTERY AND MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313001912003031300191WP 2003 3 13 AALA20030156 120030130A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21226AA 49176 TUL - FOUND SKIN CRACKED STATION 1380 LONGERON 14R. INSTALLED DOUBLER PER SRM 53-01, FIG 2. (M) 2L72 4F A6WE 20030313001972003031300197WP 2003 3 13 AALA20030164 120030205A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21466AA 49596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 24 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313001982003031300198NE 2003 3 13 AALA20030166 220030129A7261 OIL SYSTEM DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 1 ENGINE LEAKING A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21564AA 49346 728204 DFW - FLT 528 - AFTER TAKEOFF, CABIN AND COCKPIT STARTED TO FILL WITH SMOKE. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED NR 1 ENGINE DUE OT OIL LEAK AT 13TH STAGE. ACCOMPLISHED LEAK CHECK. ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA6WE E9NE 20030313001752003031300175EU 2003 3 13 AWXA200300262 120030305A3350E0052R8B3APNE CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 10 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW0 0 099 MCN - EEL - DURING C-02 CHECK THE EMERGENCY LIGHT SIDEWALL CONNECTOR WAS FOUND BROKEN AT SEAT ROW 10 L/H. MAINTENANCE REPLACED THE EMERGENCY LIGHT SIDEWALL CONNECTOR AT SEAT ROW 10 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030313001772003031300177WP 2003 3 13 AALA20030132 120030202A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21403A 49314 MIA - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CEILING EMERGENCY EXIT LIGHT GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313001812003031300181WP 2003 3 13 AALA20030139 120030204A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21588AA 53251 TUL - FOUND LEFT TEMP CONTROL VALVE HAS WORN THROUGH DOUBLER AND INTO STATION 1380 WEB. REMOVED AND REPLACED DOUBLER ON STATION 1380 WEB BY LEFT TEMP CONTROL VALVE IAW AARD 53-40-00-28. (M) 2L72 4F RTA6WE 20030313001822003031300182WP 2003 3 13 AALA20030141 120030204A5312 BULKHEAD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 TUL - FOUND AFT PRESSURE BULKHEAD UPPER RIGHT FS 1338, CRACKED. REMOVED AND REPLACED. (M) 2L72 4F A6WE 20030313001832003031300183WP 2003 3 13 AALA20030142 120030204A5310 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 TUL - FOUND SHEAR TIE CRACKED ABOVE LONGERON 16L STATION 1309. REPLACED SHEAR TIE WITH NEW PART SRM 51-20-00. (M) 2L72 4F A6WE 20030313001852003031300185WP 2003 3 13 AALA20030144 120030131A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21563AA 49345 TUL - FOUND SKIN CRACKED AT CSK RIVET STATION 1380 JUST ABOVE RIGHT PYLON. STOP DRILLED CRACK, INSTALLED DOUBLER FS 1380 ON RIGHT SIDE PER AARD 53-30-00-02 PAGE 1 REV 8/30/02 AND SRM 53-01-00. (M) 2L72 4F RTA6WE 20030313001892003031300189NM 2003 3 13 AALA20030150 120030203A2910AE70577735 HYDRAULIC LINE BOEING767 767223 1385123NM HYD SYSTEM FAILED A AALAK NONE KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21315AA 22317 JFK - FLT 133 - ON DEPARTURE, RIGHT HYDRAULIC SYSTEM WAS LOST AT BOUT 5000 FEET RIGHT HYDRAULIC QUANTITY SHOWED .12 RF HYDRAULIC PRIM PUMP PRESSURE LIGHT ILLUMINATED. RIGHT ENGINE HYDRAULIC PUMP PRESSURE LINE FAILED. REMOVED AND REPLACED PRESSURE LINE. REMOVED AND REPLACED HYDRAULIC PUMP AND CASE DRAIN AND PRESSURE FILTERS LEAK AND OPS CHECK OK. (M) 2L72 4F RTA1NM 20030313001942003031300194NM 2003 3 13 AALA20030161 120030206A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21792AN 30253 MIA - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030313002002003031300200WP 2003 3 13 AALA20030168 120030206A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21297AA 49309 DFW - DURING OVERNIGHT MAINTENANCE, NR 5 EMERGENCY EXIT LIGHT IN TAIL CONE AREA INOPERATIVE. SECURED NR 5 EMERGENCY EXIT AISLE LIGHT BATTERY FOR TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313002032003031300203WP 2003 3 13 AALA20030171 120030206A3000600450 SEAL DOUG DC9 DC982 3022082WP ANTI-ICE SYS DAMAGED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2159523 49915 BNA - FLT 402 - EN ROUTE DFW-PHL, BURNING SMELL REPORTED FROM 24AB. INSPECTED AREA AND FLOOR WAS FOUND TO BE VERY HOT TO TOUCH. DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED ANTI-ICE DUCT SEALS IN SLIP JOINT UNDER FLOOR AREA. LEAK AND GROUND CHECKED GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313002102003031300210NM 2003 3 13 AALA20030178 120030209A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21192AN 32386 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHT AT SEAT 24D INOPERATIVE. TIGHTENED AISLE EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030313002132003031300213WP 2003 3 13 AALA20030181 120030208A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313002142003031300214WP 2003 3 13 AALA20030182 120030208A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21573AA 53092 DFW - FOUND DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT OVER AFT FLIGHT ATTENDANT STATION INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313002152003031300215WP 2003 3 13 AALA20030183 120030209A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21291AA 49303 DFW - FOUND DURING OVERNIGHT MAINTENANCE, AFT CABIN AND FORWARD TAIL CONE SLIDE EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED SLIDE EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030313002222003031300222NM 2003 3 13 QXEA0300196 120030125A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING, NR 4 FLAP TRACK, INBOARD LOWER TRACK, UPPER SURFACE IS PITTED. REPAIRED IAW HORIZON AIR EA 2-57-220. 2H72 4T RTA13NM 20030313002272003031300227NM 2003 3 13 QXEA0300201 120030123A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING, NR 5 FLAP TRACK, OUTBOARD SIDE LOAD SURFACE IS PITTED. REPAIRED IAW HORIZON AIR EA 2-57-221. 2H72 4T RTA13NM 20030313002302003031300230NM 2003 3 13 QXEA0300205 120030116A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 CKB- THERE IS A ONE INCH DENT ON THE RIGHT HAND SIDE SKIN OF STATION X311 ABOVE STRINGER 19. REPAIRED IAW DHC-8 Q400 TASK 53-30-31-992-801, RD 8/4-53-377 AND HORIZON AIR EA 6-53-178. 2H72 4T RTA13NM 20030314000192003031400019NM 2003 3 14 MEX2003031 120030209A2913AS66411LS666 PUMP DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE HYDRAULIC SYS FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 SW23169PL9459 4634 53175 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH ZERO PRESSURE INDICATION. RT ENGINE HYDRAULIC PUMP WAS REPLACED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030314000222003031400022SO 2003 3 14 Z372003F00000 220030123A74144370 MAGNETO PIPER PA28 PA28181 7102807SO CONT O200 O200* 17020SO RT POSITION FAILED B Z37EO OTHER O OTHER NRNOT REPORTED 1 GL094015J 288090034 PILOT REPORTED DEAD MAGNETO IN RT POSITION. REMOVED RT MAGNETO FROM ENGINE. FOUND COIL SHAFT SEVERED AT CAM LIFTER LOBE POSITION. SUSPECT SOME METALLURGICAL DEFECT IN SHAFT. REPLACED MAGNETO WITH NEW. FUNCTIONALLY CHECKED GOOD. 1L71 3O3 O 2A13 E252 20030314000382003031400038NM 2003 3 14 2003740524 120030225A5330 SKIN BOEING727 727200 138407ENM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO0121930 21930 PREVIOUS REPAIR AT BS 1110 STR 22/23L HAS BULGING SKIN AND DISHED FASTENERS. REMOVED PREVIOUS REPAIR AND FOUND SKIN & STRINGERS DAMAGED OUT OF LIMITS IAW SRM 53-10-1 FIG 1 & 53-30-1 FIG 1. CUT OUT DAMAGED SKIN TOTAL DIMENSIONS 20 INCHES X 16.5 INCHES AND FABBED DOUBLER FROM 2024T3 .071 PO 9911586 DIM 20.25 & 20 & .75 AND 2EA FILLERS FROM 2024T3 .063 PO 9911918 DIM 19 .75 X 1 INCH IAW SRM 53-30-3 FIG 3. TWO EACH DAMAGED STRINGERS CUT OUT AND FABBED NEW FROM BAC1498-144 PO 3017135 DIM EA AND 4 EA SPLICES FROM BAC1498-132 PO 3017135 DIM EA IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW 51-10-2 AND INSTALLED IAW SRM 53-10-3 FIG 1 & 53-30-3 FIG 3. 2L73 4F RTA3WE 20030314000402003031400040NE 2003 3 14 ABXA030074 220030218A7200 ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 FAILED A ABXAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL23828AX1059 45999 669403 NR 4 ENGINE SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE, AT 1100Z WINDMILLING, OIL PRESSURE 3 PSI, N2 30 PERCENT. REMOVED AND REPLACED THE NR 4 ENGINE IAW DC-8 MM AND ABX WORK PACK 600166755. 2L74 4F4 F 4A25 1E8 20030314000412003031400041NM 2003 3 14 ABXA030080 120030219A3350 LIGHT BOEING767 767281 1385109NM CABIN INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23785AX 23018 EMERGENCY LIGHT TO RT OF MAIN ENTRY DOOR, INOPERATIVE EMERGENCY LIGHT. REPLAMPED AS REQUIRED. OPS CHECKED GOOD IAW B767 MM. 2L72 4F RTA1NM 20030314000422003031400042WP 2003 3 14 ABXA030081 120030219A2497 WIRE DOUG DC9 DC914 3022034WP NR 1 CIRCUIT BURNED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23925AX 45728 PRIMARY TRIM NR 1 CIRCUIT BREAKER TRIPPED. FOUND WIRES C104C10, C1203C10, C1202C10, C1202B10, C1203B10, C1204B10, C1213A10, C1213B10, C1211B10 BURNED. FOUND WIRE C1205D16 NOT CONNECTED. FOUND RELAY R20-16 BADLY BURNED. REPAIRED ALL WIRING AND REPLACED RELAYS R20-16 AND R20-15 IAW DC-9 WIRING DIAGRAM MANUAL 24-41-01. OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 20030314000462003031400046WP 2003 3 14 ABXA030086 120030131A5542 PANEL DOUG DC9 DC931 3022065WP RUDDER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CRACK FOUND INTERNAL OF RUDDER LOOKING FORWARD LT SIDE THROUGH PANEL NR 6515. REPLACED RUDDER IAWA DC-9 MM 27-20-01-4-0001. 2L72 4F A6WE 20030314000482003031400048WP 2003 3 14 ABXA030088 120030131A5330 DOUBLER DOUG DC9 DC931 3022065WP RT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 DOUBLER AT RIGHT WHEEL WELL UPPER PRESSURE PANEL CRACKED AT STATION 720, RIGHT BUTT LINE 55. REMOVED DOUBLER AND INSTALLED NEW DOUBLER IAW DWG NR 9910155 AND DC-9 SRM 51-30-3. 2L72 4F A6WE 20030314000522003031400052WP 2003 3 14 ABXA030096 120030303A531336483591 LONGERON DOUG DC8 DC863 302198AWP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING LINE OPERATIONS AT ILN, LONGERON 36 WAS FOUND TO HAVE INTERGRANULAR CORROSION IN THE LOWER FLANGE AT STA 1420. REPAIRED LONGERON IAW ABX REA D853-46872MR. 2L74 4F 4A25 20030314000542003031400054WP 2003 3 14 ABXA030098 120030225A5610 WINDOW DOUG DC9 DC931 3022065WP COCKPIT STUCK A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT HOOK FITTING IAW DC-9 MM 56-10-3-5-0002. OPS CHECKED GOOD. 2L72 4F A6WE 20030314000592003031400059WP 2003 3 14 CALA0300012 120030116A5350 CLIP DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0969826 49486 THE FORCE REQUIRED TO PULL EXTERIOR TAIL CONE RELEASE HANDLE FROM ITS RETAINING CLIPS EXCEEDED 35 POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND PULL WAS WITHIN LIMITS AT 25 POUNDS. 2L72 4F A6WE 20030314000612003031400061NM 2003 3 14 CALA0300024 120030122A5320 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0969333 23571 INSPECTION FOUND A CRACK IN THE PRESSURE DECK WEB AT STA 663, LBL 32. THE CRACK WAS ESTIMATED AT BEING .5 - .75 INCH LONG. A REPAIR WAS PERFORMED IAW SRM 53-60-51, FIGURE 203 AND ECRA 5310-04315. 2L72 4F RTA16WE 20030314000712003031400071NM 2003 3 14 CALA0300054 120030218A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND A .5 INCH CRACK IN PRESSURE DECK AT BS 664 - 675, LBL 30 - 35. REPAIRED IAW SRM 53-60-51, PAGE 213-221. 2L72 4F RTA16WE 20030314000742003031400074WP 2003 3 14 CALA0300076 120030228A5347 CARGO TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND AFT BAGGAGE BIN LT TIE DOWN TRACK HOLES CORRODED BETWEEN STA 1231-1271. THE TIE DOWN TRACK WAS REPLACED IAW SRM 53-23-0. 2L72 4F A6WE 20030313002042003031300204WP 2003 3 13 AALA20030172 120030206A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176201 53291 TUL - FOUND CORROSION ON LEFT CUSP MEMBRANE STATION 636 TO 674. CUT OUT CORROSION DAMAGED SPOTS AND REPLACED WITH ONE LARGE CUSP DOUBLER PER SRM 53-01 FIGURE NR 403. (M) 2L72 4F RTA6WE 20030313002052003031300205WP 2003 3 13 AALA20030173 120030206A5320 SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176201 53291 TUL - FOUND CORROSION ON CUSP 'T' AT FORWARD GALLEY SERVICE DOOR, AFT SIDE, STATION 200. REMOVED CORROSION BY BLENDING, TREATED AND PRIMED AREA. INSTALLED DOUBLER PER AARD 53-20-00-14. (M) 2L72 4F RTA6WE 20030313002112003031300211NM 2003 3 13 AALA20030179 120030209A3397 WIRE BOEING757 757223 1384957NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21193AN 32387 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED LIGHT AT SEAT 9D INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRE AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030313002202003031300220NM 2003 3 13 QXEA0300194 120030124A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING, NR 4 FLAP TRACK, OUTBOARD SIDELOAD SURFACE IS PITTED. REPAIRED IAW HORIZON AIR EA 2-57-220. 2H72 4T RTA13NM 20030313002282003031300228NM 2003 3 13 QXEA0300203 120030121A5711 SPAR DHAV DHC8 DHC8202 2809007NM RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - WING LEADING EDGE LOWER SPAR FLANGE AT WS 56 IS CHAFED. REPAIRED IAW RD 8-57-811. 2H72 4T RTA13NM 20030314000012003031400001SO 2003 3 14 C2XA03TY033 120030313A510014522459003 SUPPORT EMB 145 EMB145LR 3260212SO FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716911 145446 TYS DURING A SCHEDULED 1C INSPECTION THE TOP CAP ANGLE BEAM WAS CORRODED.MAINT.REPLACED RAMP ANGLE BEAM FOR TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030116002382003011600238NM 2003 1 16 VNAA0301009 120030109A3150 RACK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE WARNING SYS DEFECTIVE A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE MICROSWITCH RACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030116002422003011600242WP 2003 1 16 ZW0A0300101 120030101A3350408822101 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13954U 49426 THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. 2L72 4F A6WE 20030116002442003011600244WP 2003 1 16 ZW0A0300302 120030106A33502232 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13960TW 49231 AN EMERGENCY CEILING LIGHT AT ROW 11, ROW 27 TO AFT CABIN CEILING LIGHTS, AND BOTH AFT OVERWING EMERGENCY EXIT SIGNS WERE ALL INOPERATIVE. REPLACED THE LAMP AT ROW 11, AND REPLACED THE BATTERY PACK FOR THE AFT CABIN CEILING LIGHTS, AND FOR THE AFT OVERWING EXIT SIGNS. 2L72 4F A6WE 20030116002472003011600247NM 2003 1 16 ZW0A0300503A 120030109A33500105606002 MODULE DOUG MD80 MD83 3023681NM CABIN FAILED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13951TW 53470 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW 19, 21, AND 29. SECURED THE LIGHT SOCKET AT ROW 29, AND REPLACED THE LIGHT MODULE AT ROW 19 AND 21. 2L72 4F RT 20030116002772003011600277SW 2003 1 16 HEEA083138 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 MAIN ROTOR FLAP RESTRAINT STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116002852003011600285SW 2003 1 16 HEEA083144 120030108A6220206011139001 ARM BELL 206 206L3 1182108SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR HEAD RUBBER EXPANDED ON ARMS. 1G71 3U H2SW 20030116002862003011600286SW 2003 1 16 HEEA083145 120030108A6220206011139001 ARM BELL 206 206L3 1182108SW M/R HEAD WORN E O OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR HEAD ARM BEARINGS AND RUBBER WORN. 1G71 3U H2SW 20030116002942003011600294WP 2003 1 16 IXXA0300005O 120030115A3210H141003 SWITCH DOUG DC8 DC873F 302199FWP FAILED A IXXAK NONE J WARNING INDICATION CLCLIMB 1 SW11606AL89143865 46044 AFTER DEPARTURE FROM BFI DURING GEAR RETRACTION CREW NOTED RIGHT HAND MAIN LANDING GEAR DOOR WARNING LIGHT ILLUMINATED. DURING GEAR RECYCLE IT WAS ADDITIONALLY NOTED THAT THE RIGHT HAND MAIN LANDING GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. UPON COMPLETION OF LANDING GEAR RECYCLE ALL INDICATIONS WERE NORMAL. THE CREW PROCEED TO PDX FOR AN UNEVENTFUL LANDING. DURING INSPECTION MAINTENANCE NOTED THE RIGHT HAND MAIN LANDING GEAR DOWNLOCK INDICATING SWITCH HAD FAILED. MAINTENANCE REPLACED THIS SWITCH AND PERFORMED GEAR RETRACT CHECK PER THE AIRPLANE MAINTENANCE MANUAL. ALL OPERATION CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030117000072003011700007SW 2003 1 17 HEEA083152 120030108A3213206030104023 FITTING BELL 206 206L3 1182108SW MLG CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 CROSSTUBE FITTING WORN AND CORRODED. SCRAPPED. 1G71 3U H2SW 20030320001652003032000165NM 2003 3 20 2003UALA00157 120030206A2612 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FIRE LOOP SHORTED A UALABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29662UA 27159 FLIGHT ENCOUNTERED STRONG ODOR, POSSIBLY ELECTRICAL SMOKE, IN COCKPIT. RT GENERATOR TRIPPED APPROX 20 MIN AFTER ODOR; FLIGHT DIVERTED TO DTW. FOUND RT ENGINE FIRE DETECT CARD M684 HEAT DAMAGED. CARD REPLACED; MAINTENANCE FOUND IDG WIRE W3538-301Y-18 (115VAC) SHORTED TO FIRE LOOP WIRE W3520-505R-16 (28VDC), LT SIDE OF ENG BEHIND OIL TANK. INTERIM REPAIR MADE; AFTER MAINT FERRY TO ORD, PERMANENT REPAIR ACCOMPLISHED. 2L72 4F4 FRTA1NM E24NE 20030320001672003032000167 2003 3 20 SWAA030611 420030317A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030320001712003032000171NM 2003 3 20 SWAA030618 120030317A57536546435339 FLAP BOEING737 7373H4 1384600NM LH WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C2 CHECK, FOUND LH OTBD AFT T/E FLAP DELAMINATED AT INBD LOWER SURFACE. R&R LH OTBD T/E FLAP PER MM. 2L72 4F RTA16WE 20030320001742003032000174NM 2003 3 20 SWAA030621 120030318A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ( 8 EA ) AT STR 4R, BS 727D + 19, BS 727E + 1, BS 727E + 13, BS 727E + 14, BS 727E + 15, BS 758, BS 761.5 & BS 777. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030320001762003032000176 2003 3 20 SWAA030592 420030315A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030320001772003032000177 2003 3 20 SWAA030593 420030316A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT SVC DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030122001452003012200145NM 2003 1 22 DL757030017 120030102A5320146N852247 SILL BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27610DL 22817 THE OUTER CHORD OF THE C2 DOOR OPENING WAS FOUND CORRODED. TO REMOVE THE CHORD, THE FS 1440 FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER ENDS REMOVED. A NEW SECTION OF SILL CHORD WAS INSTALLED, AND THE FRAME WEB AND CHORD SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 384242-14, REV A. 2L72 4F RTA2NM 20030122001482003012200148NE 2003 1 22 HEEA083533 220030113A72000292005250 ENGINE SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1D NE NR 2 MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S978 760035 NR 2 ENGINE FAILED CHIP CHECK. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U3 U H1NE E19EU 20030122001862003012200186 2003 1 22 HEEA083545 420030114A34211113034 INDICATOR SKRSKYS76 S76A 8143006NE ATTITUDE PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 ATTITUDE INDICATOR IS SLOW TO ERECT AND PRECESSES. SENT TO SHOP FOR REPAIR. 1G72 3U H1NE 20030122002132003012200213 2003 1 22 DL76G030029 420030106A2330 ENTERTAIN SYS BOEING767 767332 1382001NM CABIN CONTAMINATED A DALAHD DEACTIVATE SYST/CIRCUITSRETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO271604R 30180 ELECTRICAL PLASTIC SMELL REPORTED BY FLIGHT ATTENDANT JUST BEHIND COCKPIT DOOR IN VIDEO CLOSET. DEACTIVATE IFE SYSTEM PER MEL 25-25-02J. REMOVED LOADS OF DUST AND DEBRIS FROM BEHIND IFE COMPONENTS. FOUND DUTY FREE BROCHURES AND SEVERAL SEALS FROM TAPE BOX VMOD LOADED WITH DUST AND LINT. REMOVED ALL. SYSTEM OPS NORMAL AND HAD NO ODORS FROM AREA. MCO AND PLACARD REMOVED. 2L72 4F RTA1NM 20030122002172003012200217 2003 1 22 HEEA083557 420030113A2350100005430 HEADSET BELL 206 206L3 1182108SW COMMS SYSTEM BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 HEADSET HAS MIKE BOOM BROKEN. REPLACED HEADSET. 1G71 3U H2SW 20030122002212003012200221 2003 1 22 DL72S030031 420030106A3497 WIRE BOEING727 727225A 1384077NM COCKPIT OUT OF POSITION A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO278875Z 21293 ESSENTIAL POWER AND ALL FWD PANEL LIGHTS ON WITH A/P WAILER GOING OFF THEN LIGHTS WENT TO FULL ON. CREW THEN SMELLED A BURNING ELECTRICAL SMELL. WINDSHEAR C/BS POPPED. FOUND WIRES TO CAPTS AMBER W/S CAUTION LIGHT TERMINALS 2 AND 4 SWAPPED. REPAIRED WIRING TO BOTH CAPTS WARN AND CAU LIGHTS. RAN WIRING BETWEEN LIGHTS AND COMPUTER, NO FAULTS FOUND. REPLACED W/S COMPUTER PER AMM. W/S TEST NML, LIGHT TEST NORMAL. 2L73 4F RTA3WE 20030122002302003012200230SW 2003 1 22 HEEA083562 120030113A6420 BEARING BELL 206 206L3 1182108SW T/ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 7103 AFS7397 51527 TAIL ROTOR HEAD FEATHERING BEARINGS WORN. REPLACED BEARINGS AND REPAIRED. 1G71 3U H2SW 20030122002582003012200258SW 2003 1 22 HEEA083568 120030113A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW MAIN ROTOR INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 ACTUATOR INTERMITTENTLY WON'T WORK UNLESS YOU TAP ON IT. ALSO HAS BAD CORROSION AT WIRE CONNECTIONS. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030122002632003012200263SW 2003 1 22 HEEA083573 120030113A3040204070907002 MOTOR BELL 412 412 1182202SW WINDSHIELD WIPERLOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 MOTOR LOOSE IN CONVERTER. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030117000132003011700013NM 2003 1 17 ANCF200300002 120030114A213160683218 OUTFLOW VALVE BOEING767 767383 1385214NM CABIN PRESSURE INOPERATIVE W ANCFB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SO23984AN30045542 24357 DURING CLIMB THROUGH 35000 FT, MASTER WARNING AND CABIN ALTITUDE ALARM WERE PRESENTED; EMERGENCY DESCENT WAS STARTED TO 21000 FT. CHECK LIST WAS PERFORMED. DURING MANUAL TEST PROCEDURE IAW AMM 21-31-00 PAGE 507 WAS FOUND THAT OUTFLOW VALVE WAS NOT WORKING WHEN SELECTOR IS IN MANUAL CLIMB AND DESCEND. OUTFLOW VALVE WAS REPLACED IAW AMM 21-31-03 PAGE 201 WITH SATISFACTORY RESULTS. 2L72 4F RTA1NM 20030117000142003011700014WP 2003 1 17 CALA0300011 120030115A5313 LONGERON DOUG DC9 DC982 3022082WP STA 160-170 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0918833 49493 INSPECTION FOUND LONGERON 30 CORRODED IN E&E COMPARTMENT AT STA 160-170. THE CORRODED SECTION OF LONGERON WAS REPLACED IAW SRM 53-02 AND 53-10-01. 2L72 4F A6WE 20030117000232003011700023SW 2003 1 17 HEEA083162 120030108A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 TRANSMISSION RESTRAINT WORN. REPAIRED. 1G71 3U H2SW 20030117000302003011700030SW 2003 1 17 HEEA083165 120030108A6330206033506103 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 TRANSMISSION RESTRAINT WORN. REPAIRED. 1G71 3U H2SW 20030117000532003011700053SW 2003 1 17 HEEA083172 120030108A6330 BUSHING BELL 206 206L3 1182108SW MOUNT ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MAIN ROTOR TRANSMISSION MOUNT BUSHINGS WORN. REPAIRED. 1G71 3U H2SW 20030117000572003011700057SW 2003 1 17 HEEA083176 120030108A6310206040270101 SUPPORT BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 MAIN ROTOR AFT SUPPORT LEAKING. REPAIRED. 1G71 3U H2SW 20030117000582003011700058SW 2003 1 17 HEEA083177 120030108A6310206040270101 SUPPORT BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 MAIN ROTOR AFT SUPPORT LEAKING. REPAIRED. 1G71 3U H2SW 20030117000642003011700064SW 2003 1 17 HEEA083179 120030108A6510206040339101 BEARING BELL 206 206L3 1182108SW T/R DRIVESHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038592X 51508 TAIL ROTOR DRIVE SHAFT FORWARD BEARING ROUGH. REPAIRED. 1G71 3U H2SW 20030117000662003011700066SW 2003 1 17 HEEA083180 120030108A6510206040370105 DRIVE SHAFT BELL 206 206L3 1182108SW TAIL ROTOR ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 TAIL ROTOR DRIVE SHAFT FWD BEARING DUST COVER OFF, GREASE GONE, BEARING ROUGH. REPAIRED. 1G71 3U H2SW 20030117000902003011700090NM 2003 1 17 2003UALA00013 120030105A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 827 FRAME CRACKED AT RIVET HOLE S9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030117000952003011700095NM 2003 1 17 2003UALA00021 120030107A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 887 FRAME CRACKED AT RIVET HOLE NEAR STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030117001002003011700100SW 2003 1 17 HEEA083190 120030108A3212206050248117 FLOAT BELL 206 206L3 1182108SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 FLOAT BAG ASSY LEAKS. 1G71 3U H2SW 20030117001142003011700114SW 2003 1 17 HEEA083196 120030108A3213206053115 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038591X 51495 CROSSTUBE HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030117001342003011700134SW 2003 1 17 HEEA083207 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 ROTOR AND N2 TURBINE WOULD NOT INCREASE OR DECREASE. 1G71 3U H2SW 20030117001512003011700151SW 2003 1 17 HEEA083213 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 RPM NOT STAYING CONSTANT. REPLACED ACTUATOR. 1G71 3U H2SW 20030122002672003012200267NM 2003 1 22 UPS03440043 120030103A5310 SKIN BOEING747 747259B 1384804NM RH BS 1480 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C B/H BS 1480 BULKHEAD NO.11 HOLE CRACK AT FX SKIN RUNNING FWD AND AFT THROUGH THICKNESS. REFER ATTACH SKETCH FOR DETAILS. HOLE REWORKED AS PER RS-53-43-43957 DUE EXCEEDED SB 747-53A2390 REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTION). 2L74 4F RTA20WE 20030122002712003012200271EA 2003 1 22 SWIA200311715 120030114A2530 DOOR CNDAIRCL600 CL6002B19 1900309EA LAV FIRE EXT STUCK A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07589SW 7072 CANNOT GAIN ACCESS TO LAVATORY FIRE EXTINGUISHER BOTTLE, PANEL STUCK. REPLACED DOOR WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 4582073-501 2L72 4F RTA21EA 20030123000112003012300011NM 2003 1 23 2003UALA00025 120030106A5320 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29355UA 24361 CABIN STRINGER CLIP CRACKED BS 270 STRINGER 15R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20030320000762003032000076NM 2003 3 20 2003UALA00027 120030106A3246 BEARING BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE MLG WHEEL FAILED A UALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 WP29615UA 21876 AIRCRAFT LOST NR 4 RIGHT AFT MLG WHEEL. RETURNED TO FIELD. WHEEL LOSS BELIEVED DUE TO BEARING FAILURE. INSPECTION OF RECOVERED PARTS REFLECT LACK OF LUBRICATION OF INBOARD WHEEL BEARING. NR 4R WHEEL AND BRAKE REPLACED. NR 3R MATE REPLACED, REAR AXLE REPLACED. EXTENSION-RETRACTION TEST ACCOMPLISHED CHECKED OKAY. 2L72 4F4 FRTA1NM E3NE 20030320000772003032000077NM 2003 3 20 2003UALA00028 120030106A2410729825G IDG BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR1 GENERATOR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29548UA 25396 NR 1 GENERATOR DRIVE LIGHT ILLUMINATED PRIOR TO ENTERING ETOPS. DISCONNECTED GENERATOR. APU SUPPLIED POWER. LEFT AC INTEGRATED DRIVE GENERATOR (IDG) FAILURE. REPLACED THE LEFT IDG. CARRIER SHAFT FROZEN. REPLACED THE SHAFT AND OVERHAULED THE IDG. 2L72 4F4 FRTA2NM E17NE 20030123000152003012300015NM 2003 1 23 2003UALA00031 120030107A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29951UA 26696 STATION 178 BULKHEAD WEB CRACKED AT RIGHT LOWER RADAR MOUNT INBOARD UPPER SIDE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030123000212003012300021NM 2003 1 23 2003UALA00037 120030108A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 CABIN FRAME STATION 480 FRAME WEB CRACKED AT FASTENER HOLE JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030123000222003012300022NM 2003 1 23 2003UALA00038 120030109A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 BS 440, STRINGER 9L, FUSELAGE FRAME CRACKED JUST ABOVE STR 9L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED FRAME DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030320000792003032000079NE 2003 3 20 2003UALA00045 220030113A72306A7406 BLADE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COMPRESSOR FRACTURED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29404UA1553 1553 450 V10095 COMPRESSOR STALL NR 2 ENGINE. THROTTLED TO IDLE, ENGINE WAS NOT SHUTDOWN. ENGINE TEARDOWN REVEALED C6 BLADE FAILURE RESULTING FROM NICKED C6 VANE. BIRD INGESTION 17 DAYS PRIOR HAD BEEN BORESCOPED WITH NO FINDINGS IN FIRST THREE STAGES. 2L72 4F4 FRTA28NM E40NE 20030123000372003012300037NM 2003 1 23 2003UALA00059 120030115A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29951UA 26696 STATION 178, WL 207, CHORD CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030123000402003012300040NM 2003 1 23 2003UALA00065 120030116A5312 PRESSURE PANEL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29951UA 26696 NOSE LANDING GEAR WHEEL WELL UPPER WEB AND UPPER AFT CHORD ANGLE PUNCTURED AND CRACKED, RBL 24 STA 294. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE. WEB REPAIRED BY INSTALLING DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030123000412003012300041NM 2003 1 23 2003UALA00066 120030116A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 BS 935-990, RBL 54, WL 208, RIGHT CREASE BEAM INBOARD CHORD UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED. DAMAGED SECTION OF CREASE BEAM CHORD REMOVED. REPLACEMENT PART PREPPED AND INSTALLED. DRAIN SCUPPER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030123000632003012300063NM 2003 1 23 P5CA0300723 120030112A5720NONE STIFFENER BOEING747 7472U3B 1384846NM WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CORROSION LEVEL 1 FOUND LEADING EDGE TOP PANEL SUPPORT RIB AT STA. FSS 1336.00, "L" ANGLE STIFFENER TO FRONT SPAR. "L" ANGLE REPAIR CARRIED OUT AS PER SRM 51-30-02. 2L74 4F RTA20WE 20030123000642003012300064NM 2003 1 23 P5CA0300724 120030112A5720NONE STIFFENER BOEING747 7472U3B 1384846NM WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CORROSION LEVEL 1 FOUND R/H WING LEADING EDGE FRONT SPAR "L" STIFFENER AT FSSI 1435 LOWER PORTION. REPAIR CARRIED OUT IAW SRM 51-30-02. 2L74 4F RTA20WE 20030118000042003011800004SO 2003 1 18 C2XA03TY007 120030118A534014521725001 SILL EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 TYS, During a scheduled inspection floor panel support at stringer 15L at frame 18L and 21L was found corroded. Maintenance removed and replaced the floor sill. I/A/W-EMB-135/145-SRM-51-40-02. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2L72 4T RTT00011AT 20030119000042003011900004SO 2003 1 19 RAIA00301013 120030113A2612MS3459KT14S5S CONNECTOR EMB 145 EMB145 3260210SO CORRODED A RAIAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 CE03802HK 145066 5257-SBN-RIGHT ENGINE FIRE WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE PYLON FIRE DETECTOR CANNON PLUG 2L72 4F RTT00011AT 20030119000062003011900006EU 2003 1 19 RAIA00301017 120030116A33503012000 POWERPACK AEROSPATR72 ATR72202 8680940EU DISCHARGED A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03721TE2998 217 MX-STL- AFT RH OH EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY, OPS CK OK. 2H72 4T RTA53EU 20030130001552003013000155NM 2003 1 30 F3LA200300004 120030115A5313 STRINGER BOEING737 7373M8 1384615NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FUSELAGE LOWER STRINGER BETWEEN STA 500 AND 500A AND STR 27R AND 27L CRACKED. REMOVED WORN STRINGER PER SRM 51-40-02, PAGE 3. INSTALLED SERVICEABLE STRINGER PER SRM 51-40-02, PAGE 3 AND 51-10-02, PAGE 12. 2L72 4F RTA16WE 20030120000032003012000003NM 2003 1 20 DHL2003745001 120030118A7933162BL704D INDICATOR BOEING727 727224 1384076NM A DHLAEO ENGINE SHUTDOWN OTHER M OVER TEMP DEDESCENT 1 SO01745DH 20665 1) IN-FLIGHT SHUTDOWN ENGINE #3, OIL TEMPERATURE GAUGE PEGGED ABOVE 165 DEGREE (SUSPECT GAUGE).2) REMOVED AND REPLACED FAULTY OIL TEMPERATURE INDICATOR. OPS CHECKED GOOD. WORK DONE IAW M/M 79-34-0. 2L73 4F A3WE 20030120000052003012000005EU 2003 1 20 MALA030114 120030119A3150005WS00 WEU SAAB SF340 340B 7860101EU A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15417XJ 340B417 DURING FLIGHT #2920, BITE LIGHT ILLUMINATED, ALONG WITH INTERMITTENT LEFT AND RIGHT ENGINE FIRE LIGHTS ON CWP. NO CHIMES ASSOCIATED W/ ENGINE FIRE LIGHTS. ALL ENGINE INDICATION NORMAL. AIR RETURN TO MEM. MAINTENANCE REPLACED WEU PN 005WS00, SN/OFF 1463, SN/ON 1004, PERFORMED ADJUSTMENT TEST-CHECK GOOD. NO DEFECTS NOTED. REF AMM 31-50-05-4. A/C OK FOR CONTINUED SERVICE. 2L72 4T RTA52EU 20030120000102003012000010NM 2003 1 20 0300076628 120030109A5210 FRAME BOEING747 747251B 1384892NM CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01628US 22389 During "H" check found corrosion on LH passenger door frame web. Repaired per EA 66-193831. 2L74 4F A20WE 20030121000012003012100001 2003 1 21 SWAA030078 420030114A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20030121000032003012100003NM 2003 1 21 SWAA030080 120030114A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE. CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 LONG, BS 500D, STRINGER 7R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030121000132003012100013NM 2003 1 21 SWAA030075 120030112A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29729SW 27861 DURING SCHEDULED SERVICE CHECK, (SI 11038-55) FOUND LT ELEVATOR TAB NR 4 ATTACH HINGE BUSHING WORN. REMOVED AND REPLACED NR 4 ATTACH HINGE BUSHING PER MM. 2L72 4F RTA16WE 20030121000142003012100014NM 2003 1 21 SWAA030076 120030112A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29729SW 27861 DURING SCHEDULED SERVICE CHECK, (SI 11038-55) FOUND RT ELEVATOR TAB NR 3 ATTACH HINGE BUSHING WORN. REMOVED AND REPLACED NR 3 ATTACH HINGE BUSHING PER MM. 2L72 4F RTA16WE 20030121000212003012100021NM 2003 1 21 SWAA030064 120030112A5520BACB28AK04 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, FOUND LT ELEVATOR TAB INBD ATTACH POINT WORN. REMOVED AND REPLACED HARDWARE AND BUSHING AT INBD HINGE ATTACH POINT PER MM. 2L72 4F RTA16WE 20030121000232003012100023NM 2003 1 21 SWAA030067 120030111A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, WL 148 AND RBL 10. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030121000252003012100025EU 2003 1 21 BAQA083519 120030116A2840L284M30C1003 SENSOR UROCOPEC135 EC135T1 5620026EU FUEL CELL INACCURATE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01533ME19 132 FUEL SENSOR PRODUCING IMPROPER FUEL READING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030121000262003012100026EU 2003 1 21 BAQA083520 120030116A2842L284M30C1004 PROBE UROCOPEC135 EC135T1 5620026EU FUEL QTY FLUCTUATES H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01533ME19 132 FUEL PROBE GIVING FLUCTUATING QUANTITY READINGS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030325000262003032500026NM 2003 3 25 AWXA200300141 120030214A2420948F4583 GCU BOEING737 7373G7 1384595NM NR 2 GENERATOR FAULTY A AWXAO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC DEDESCENT 1 WP28322AW5565010387 25400 PHX - EMERGENCY LANDING - FLT 0587 - ON DECENT INTO PHX EN ROUTE FROM IND APPROX 30 MINUTES OUT, LOST POWER TO NR 2 TRANSFER BUS, SEVERAL INSTRUMENTS AFFECTED, DECLARED EMERGENCY, LANDED WITHOUT EVENT. MAINT FOUND THE NR 2 TRANSFER BUS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND EXAMINED THE NR 2 GENERATOR CONTROL UNIT (GCU) AND R4 RELAY CONNECTIONS IAW BMM'S 24-24-01, 24-51-41, AND 24-58-21, NO DEFECTS WERE NOTED. REMOVED AND REPLACED THE NO. 2 GCU IAW BMM 24-21-81, PG. 401. PERFORMED ENGINE RUN, NO FAULTS NOTED. VENDOR BENCH TEST OF GCU S/N WF080 CONFIRMED FAILURE OF UNIT FOR FAILING FREQUENCY AND DROPOUT TEST. REPLACED RELAY , RELAY , TRANSISTOR SEMICONDZENER, AND SPACER. UNIT REPAIRED AND TEST IAW. 2L72 4F RTA16WE 20030325000452003032500045NM 2003 3 25 AWXA200300170 120030127A5315146N5089 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOORBEAM IN AND AROUND FASTENER HOLES BS 1640. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOORBEAM BS 1640; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51, PG. 209-213, FIG. 203. 2L72 4F RTA2NM 20030325000752003032500075NM 2003 3 25 AWXA200300241 120030219A5314656212518 KEELBEAM BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-11 CHECK CORROSION WAS FOUND ON RT KEELBEAM AT BS 540. MAINTENANCE TRIMMED OUT DAMAGED SECTION OF RT KEELBEAM AT BS 500C+9 TO BS 541; FABRICATED A NEW SEGMENT OF KEELBEAM, 2 EACH ANGLES, AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5330-03066-TB1. 2L72 4F RTA16WE 20030325000822003032500082NM 2003 3 25 0300586303 120030322A3350 WIRE BOEING747 747451 1384940NM PATH LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01663US 23818 DURING LINE CHECK FOUND LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-61. REPLACED WIRE UNIT AND OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030325000992003032500099NM 2003 3 25 AWXA200300261 120030305A2560 BATTERY BOEING737 7373S3 1384711NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-11 CHECK THE FORWARD OUTBOARD EMERGENCY FLASHLIGHT LED INDICATOR DID NOT FLASH. MAINTENANCE REMOVED AND REPLACED THE FORWARD OUTBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030326000182003032600018SO 2003 3 26 AUS20030103 120030131A2730VARIOUS CONTROL QUADRANT MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL ELEVATOR OUT OF ADJUST W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR AND RUDDER CONTROLS OUT OF LIMIT. RUDDER SYSTEM - LT 27 DEGREES, RT 21 DEGREES (LIMITS 21DEGREES + 1 DEGREE). ELEVATOR SYSTEM - UP 28 DEGREES, DOWN 18 DEGREES (LIMITS UP 30 DEGREES + 1 DEGREE AND DOWN 20 DEGREES + 1 DEGREE). 1H71 3O3 ONC3A23 E286 5 CP920 20030326000242003032600024NM 2003 3 26 AUS20030118 120030205A7500 CLAMP BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE ENGINE BLEED AIRLOOSE W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 3 ENGINE THIRTEENTH STAGE MODULATING VALVE LEAKING FROM REAR DUCT CLAMP. 2L73 4F4 FRTA3WE E2EA 20030326000412003032600041NE 2003 3 26 AUS20030187 220030213A7321 COMPUTER BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUEL CONTROL FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE THRUST MANAGEMENT SYSTEM (TMS) COMPUTER FAULTY. 2H74 4F4 F A49EU E6NE 20030326000492003032600049EU 2003 3 26 AUS20030216 120030221A3620D2475 CONNECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE PNEUMATIC INDICACONTAMINATED W O OTHER N FALSE WARNING DEDESCENT 1 AUS (AUS) LT BLEED AIR LEAK INDICATION. THOROUGH INVESTIGATION FOUND THAT PLUG P2 OF THE LT WING DETECTOR LOOP WAS CONTAMINATED WITHMOISTURE AND CAUSING THE FALSE INDICATION. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20030326000662003032600066NM 2003 3 26 CA030205004 120030126A5610141T480014 WINDSHIELD BOEING767 7673S1 1385211NM GE CF6 CF680C2B6F 30025NE COCKPIT CRACKED W O OTHER O OTHER CLCLIMB 1 CA (CAN) ON CLIMB OUT OF YVR, RT WINSHIELD SHATTERED. ACFT CONTINUED TO YUL. 2L72 4F4 FRTA1NM E13NE 20030327000082003032700008NM 2003 3 27 AWXA200300271 120030315A3350321430 BATTERY AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28820AW 1397 MAINTENANCE FOUND EMERGENCY LIGHTS LEFT ON 2 HOURS AFTER CREW LEFT. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS, ZONES 221, 241, 242, AND 263. FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM WAS GOOD. 2L72 4F RTA28NM 20030327000122003032700012EU 2003 3 27 AWXA200300277 120030301A5320D53480043205 BEAM AIRBUS320 A320231 3930325EU FUSELAGE SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE R-2 DOOR SILL AT INBOARD SIDE OF AFT GIRT BAR ATTACH PLATE, FR 67+16, RBL 50. MAINTENANCE REMOVED EXISTING REPAIR ANGLE; CLEANED CORROSION AND TREATED SURFACE; FABRICATED NEW REPAIR ANGLE; INSTALLED REPAIR PART IAW AWA E.R. 5340-03073-ES1. 2L72 4F RTA28NM 20030327000152003032700015EU 2003 3 27 AWXA200300282 120030301A5315D5347217220390 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM FR 66 - FR 68, RBL 48, Y1292. MAINTENANCE REMOVED CORRODED FLOORBEAM FROM FR 66 TO FR 69; FABRICATED A NEW SECTION OF REPLACEMENT FLOORBEAM AND TWO EACH SPLICES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, PG. 39-41, FIG. 18, SRM 51-44-11, PG. 11-12, TABLES 11 & 12, SRM 51-75-12, PG. 4-5, PARA. C, SRM 51-49-00, PG. 5-6, & 24, TABLE 23, AND 51-76-11, PG. 3-4. 2L72 4F RTA28NM 20030327000302003032700030EU 2003 3 27 AWXA200300302 120030316A5321D5467002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 2723, FR 58, TO BS 2936, FR 62. MAINTENANCE PERFORMED BOND REPAIR ON UPPER SURFACE OF CABIN FLOOR PANEL BS 2723, FR 58, TO BS 2936, FR 62 IAW A320 SRM 53-02-00, PG. 203-207, FIG. 201, PARA. 2. 2L72 4F RTA28NM 20030327000362003032700036NM 2003 3 27 AWXA200300308 120030302A5315146N5458 FLOOR SUPPORT BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT FRAME BS 1480, RBL 12. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOOR SUPPORT FRAME BS 1480, RBL 12; FABRICATED A NEW FLOOR SUPPORT PER DWG 146N5458; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 3. 2L72 4F RTA2NM 20030327000502003032700050NM 2003 3 27 C1HA200381003 120030203A2611 SMOKE DETECTOR BOEING727 7272S7 138407ZNM CARGO BAY WILL NOT TEST A C1HAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL15681CA 22020 AFT CARGO SMOKE DETECTOR 'B' LOOP WILL NOT TEST. REMOVED DUST FROM COOLING FAN ON AFT CARGO SMOKE DETECTOR B LOOP. PERFORMED OPERATIONAL TEST PER M/M 26-23-01. 2L73 4F A3WE 20030327000622003032700062NM 2003 3 27 C1HA200385003 120030203A7722 INDICATOR BOEING727 7272S7 138407ZNM EGT MALFUNCTIONED A C1HAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15685CA 22492 ON TAKE-OFF ROLL NR 3 EGT WAS READING ERRONEOUSLY B/L 500 100 ON TAXI THE GAUGE WANT TO 0. R & R NR 3 EGT INDICATOR PER MM 77-21-51 EGT IND NORMAL OK FOR SERVICE 2L73 4F A3WE 20030327000662003032700066NM 2003 3 27 C1HA200388004 120030214A3150 WARNING LIGHT BOEING727 7272S7 138407ZNM TAIL SKID ILLUMINATED A C1HAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15688CA 22344 TAIL SKID LIGHT ON AFTER DEPARTURE. MEL'D TAIL SKID INDICATION, TAIL SKID OPS NORMAL. 2L73 4F A3WE 20030327000752003032700075NM 2003 3 27 C1HA200396002 120030210A3097 WIRE BOEING727 7272J4 1384006NM ANTI ICE PANEL SHORTED A C1HAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15696CA 22574 LEAVING 15,000 FT SMELLED STRONG ELETRICAL ODOR, STRONG ELECTRICAL BURNING ODOR. F/O NOTICED FIRST. NO SMOKE WAS SEEN. REPOSITIONED WIRE CONTACTING GROUND ON ANTI-ICE PANEL. RAN ALL SYSTEMS ON OVERHEAD PANEL NO SMOKE, ODOR, OR ARCHING NOTED. OK FOR SERVICE 2L73 4F RTA3WE 20030327000782003032700078NM 2003 3 27 C1HA200397007 120030222A3397 CONNECTOR BOEING727 727270 138408PNM EMERGENCY LIGHT LOOSE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15697CA 23052 RT STA 940 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. SECURED LOOSE CONNECTOR AT BATTERY PACK IAW 727 MM 33-50-22. OPS CHECK WAS GOOD. 2L73 4F RTA3WE 20030327000792003032700079NM 2003 3 27 C1HA200397008 120030222A3350 BATTERY BOEING727 727270 138408PNM EMERGENCY LIGHT CORRODED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15697CA 23052 AFT AIRSTAIR EMERGENCY AREA LIGHT IS INOPERATIVE. CLEANED/REMOVED CORROSION FROM BATTERY CONTACTS & OPS CHECK WAS GOOD. REF: 727 MM 33-50-01. 2L73 4F RTA3WE 20030327000842003032700084SO 2003 3 27 C2XA02SH187 120030201A531014521721009 BUTT STRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727523 145389 DURING C-CHECK FOWARD CENTER DIGITAL BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND 16. MAINTENANCE REMOVED DAMAGE SECTION AND PERFORMED A SPLICED REPAIR IAW EMB 135 SRM 53-21-10. 2L72 4F RTT00011AT 20030327001052003032700105SO 2003 3 27 C2XA03CL019 120030121A32343631101007 SELECTOR EMB 145 EMB145LR 3260212SO MLG DEFECTIVE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2713553 145585 IAH FLIGHT 2732 THE CREW REPORTED A LANDING GEAR AURAL WARNING WHEN THE GEAR WAS SELECTED UP. NO WARNING WHEN GEAR WAS DOWN. MAINTENANCE REPLACED THE FLAP SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001072003032700107SO 2003 3 27 C2XA03CL023 120030124A5210 CABLE EMB 135 EMB135ER 3260203SO PAX DOOR OUT OF ADJUST A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2725504 145186 GSP FLIGHT 2129 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE INSPECTED AND RESECURED LOOSE HARDWARE ON INNER HANDLE BOX AND ADJUSTED MAIN CABIN DOOR CABLES. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001132003032700113SO 2003 3 27 C2XA03CL033 120030208A33501317 BULB EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713995 145295 DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 12 OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001152003032700115SO 2003 3 27 C2XA03CL036 120030207A27503631101007 SELECTOR EMB 145 EMB145LR 3260212SO TE FLAPS DEFECTIVE A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2712540 145537 IAH FLIGHT 2584 THE CREW REPORTED A LANDING GEAR WARNING IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR HANDLE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001362003032700136SO 2003 3 27 C2XA03CL076 120030324A33507287580505 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715986 145254 IAH FLIGHT 2906 THE CREW REPORTED ON PREFLIGHT THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001372003032700137SO 2003 3 27 C2XA03IA001 120030101A335066366 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713964 145123 DURING PREFLIGHT THE CREW NOTED THAT THE NR 1 EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327001592003032700159SO 2003 3 27 C2XA03SH006 120030218A532014524131011 NUT PLATE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV- DURING C-CHECK THE PASSENGER DOOR THRESHOLD MOUNTING BRACKETS NUT PLATES WERE FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKETS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001692003032700169SO 2003 3 27 C2XA03SH050 120030310A531014523522017 SHEAR TIE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C-CHECK SHEAR CLIPS WHERE FOUND TO HAVE CORRSION BETWEEN FRAMES 61 TO 66 AT STRINGERS 21 LEFT TO 20 RIGHT. MAINTENANCE REMOVED AND REPLACED AFFECTED SHEAR CLIPS IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001702003032700170SO 2003 3 27 C2XA03SH052 120030316A531014522460013 BUTT STRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 DURING C-CHECK THE CENTER OMEGA BEAM BUTT STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030121000292003012100029SW 2003 1 21 HEEA083221 120030108A7160206064213103 SCREEN BELL 206 206L3 1182108SW ENGINE INTAKE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 ENGINE INTAKE SCREEN ASSY HAS CORROSION. REPAIRED. 1G71 3U H2SW 20030121000352003012100035SW 2003 1 21 HEEA083227 120030108A7160206064213103 SCREEN BELL 206 206L3 1182108SW ENGINE INTAKE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 ENGINE INTAKE SCEEN ASSY HAS CORROSION. REPAIRED. 1G71 3U H2SW 20030121000412003012100041SW 2003 1 21 HEEA083233 120030108A7603206064713103 POWER LEVER BELL 206 206L3 1182108SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 POWER LEVER WORN. SCRAPPED. 1G71 3U H2SW 20030121000432003012100043 2003 1 21 HEEA083235 420030108A3424206070274005 INDICATOR BELL 206 206L3 1182108SW TURN AND BANK INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0392MT 51175 TURN AND BANK INDICATOR INOPERATIVE. 1G71 3U H2SW 20030121000532003012100053SW 2003 1 21 HEEA083255 120030108A3212206073926111 RELIEF VALVE BELL 206 206B3 1181506SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322743 3624 EMERGENCY FLOAT RELIEF VALVE LEAKING. REPAIRED. 1G71 3U H2SW 20030121000552003012100055SW 2003 1 21 HEEA083257 120030108A7933206075187003 INDICATOR BELL 206 206L3 1182108SW ENG OIL & TEMP READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 INDICATOR MALFUNCTIONED, TEMP SIDE READS LOW. 1G71 3U H2SW 20030121000642003012100064SW 2003 1 21 HEEA083266 120030108A7712206075739103 TORQUEMETER BELL 206 206L3 1182108SW COCKPIT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 TORQUEMETER BROKEN. REPAIRED. 1G71 3U H2SW 20030121000682003012100068SW 2003 1 21 HEEA083268 120030108A7712206075739103 TORQUEMETER BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 TORQUEMETER ERRONEOUS READINGS. REPAIRED. 1G71 3U H2SW 20030121000742003012100074SW 2003 1 21 HEEA083271 120030108A6730206076062003 CYLINDER BELL 206 206L1 1182107SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0383MT 12036 45492 MAIN ROTOR CYLINDER LEAKING. REPAIRED. 1G71 3U H2SW 20030121000772003012100077SW 2003 1 21 HEEA083272 120030108A6730206076062003 CYLINDER BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW036748D 51106 MAIN ROTOR CYLINDER LEAKING. REPAIRED. 1G71 3U H2SW 20030121000812003012100081WP 2003 1 21 ABXA030034 120030115A3230 CONTROL CABLE DOUG DC9 DC932 3022066WP MLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23988AX 47084 WITH LANDING GEAR RETRACTED, GEAR DOOR OPEN LIGHT AND RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLING GEAR, HAD NO EFFECT ON THIS CONDITION. FERRIED AIRCRAFT BACK TO ILN UNDER FERRY PERMIT 002-003. REMOVED, CLEANED, LUBRICATED AND REINSTALLED DOOR SEQUENCING CABLE IAW DC-9 MM 32-31-00-4-0001 AND ADJUST TEST IAW DC-9 MM 32-31-00-5-00-01. REPLACED SHEARED RIVETS IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030121000912003012100091SW 2003 1 21 HEEA083279 120030108A3246206324007 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 SKID TUBE HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030121000942003012100094SW 2003 1 21 HEEA083282 120030108A3246206324459 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03319E 51042 SKID TUBE HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030121000952003012100095SW 2003 1 21 HEEA083283 120030109A2810206362002101 FUEL CAP BELL 206 206L3 1182108SW FUEL STORAGE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 FUEL CAP LEVER WORN. SCRAPPED. 1G71 3U H2SW 20030121001082003012100108SW 2003 1 21 HEEA083293 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 SEAT BELT WILL NOT RETRACT. 1G71 3U H2SW 20030327001712003032700171SO 2003 3 27 C2XA03SH053 120030316A5310 BEAM EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 DURING C-CHECK LEFT HAND OMEGA BEAM RAMP ANGLE BETWEEN FRAMES 19 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE SECTION AND PERFORMED AN ANGLE REPAIR IAW EMB 135 SRM 53-21-40. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327001762003032700176SO 2003 3 27 C2XA03TY001 120030109A531514522226003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 DURING A SCHEDULED 2C INSPECTION THE CENTER LAV FLOORBEAM SHOWS SIGNS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE CENTER LAV FLOORBEAM, REMOVED AND REPLACED THE CENTER CARBON FIBER BEAM, PRIMED AND PAINTED THE CENTER LAV FLOORBEAM IAW EMB 135/145 SRM 51-40-02, CPM51-21-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030327001822003032700182SO 2003 3 27 C2XA03TY017 120030131A534714521721 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED INSPECTION THE FORWORD TOP CAP BELOW THE LT SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REPLACED THE RIVETS AND CLEANED CORROSION OFF OF THE TOP CAP IAW-EMB-145-SRM-57-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2L72 4T RTT00011AT 20030327001852003032700185NE 2003 3 27 CA030207008 220030202A7532 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE RIGHT CRACKED W A UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 CA (CAN) DURING CLIMB PILOT NOTICED LARGE FLUCTUATIONS IN RT ENGINE TORQUES APPROX 300-400 LBS AT TAKEOFF CLIMB POWER. THEY ELECTED TO RETURN AND MADE UNEVENTFUL LANDING. DURING INSPECTION BY MAINTENANCE THE GAS GENERATOR SPEED WAS ALSO NOTICED TO BE UNUSUALLY HIGH. THE ENGINE BLEED VALVE WAS REMOVED FOR INSPECTION AND A CRACK WAS THEN NOTICED ON A INTERNAL ENGINE P3 LINE. THE ENGINE WAS REMOVED AND SENT TO REPAIR FACILITY. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030327001872003032700187EU 2003 3 27 CA030210002 120030207A324215907400 BRAKE PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL MLG WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A ROUTINE TIRE CHANGE FOR WEAR, BRAKE UNIT HAD SPLINTERS OF METAL PROTRUDING FROM FRICTION DISC AREA. WEAR INDICATOR ON BRAKE UNIT INDICATED ONLY ABOUT HALF LIFE ON BRAKES. INSPECTION REVEALED BRAKE UNIT WAS NOT WEARING EVENLY THROUGHOUT ALL ROTORS AND STATORS AND DETERIORATED 1 ROTOR TO HALF OF ITS ORIGINAL THICKNESS. OTHER MAIN WHEEL WAS REMOVED AND SAME PROBLEM REVEALED, REPLACEMENT BRAKE UNIT WAS INSTALLED ON BOTH MAINS AND RELEASED FOR RETURN TO SERVICE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030325000112003032500011NM 2003 3 25 AWXA200300113 120030208A3397AW252100111 WIRE BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28322AW 25400 DURING INSPECTION ROW 13 LT ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHTING HARNESS AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20030325000292003032500029NM 2003 3 25 AWXA200300144 120030207A5320654868719 ANGLE BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON THE LT FORWARD, OUTBOARD, WHEEL WELL CUTOUT MOUNTING ANGLE AT THE OUTBOARD END BS 663.75. MAINTENANCE REMOVED THE CRACKED LT FORWARD, OUTBOARD, WHEEL WELL CUTOUT MOUNTING ANGLE BS 663.75; FABRICATED A NEW REPLACEMENT MOUNTING ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10 & 45, FIG. 12. 2L72 4F RTA16WE 20030325000302003032500030EU 2003 3 25 AWXA200300147 120030206A5315D5347218920200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT FLOORBEAM ABOVE FR 68, BS 3257. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOOR BEAM ABOVE FR 68, BS 3257; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11, PG. 1-2. 2L72 4F RTA28NM 20030325000522003032500052NM 2003 3 25 AWXA200300207 120030224A21317612608 CONTROLLER BOEING737 7373S3 1384711NM ZONE 205 FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28316AW131382675 23713 ON CLIMB OUT FROM MKE EN ROUTE FOR PHX, STANDBY PRESSURIZATION FAILED AT 35,000 FT, TURNED BACK AND LANDED AT MKE WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, AND CABIN PRESSURE CONTROL PANEL IAW BMM 21-31-25. CABIN PRESSURIZATION INTEGRITY CHECK, AND CABIN PRESSURE OPERATIONAL CHECK WAS GOOD FOR BOTH UNITS. 2L72 4F RTA16WE 20030325000722003032500072NM 2003 3 25 AWXA200300237 120030306A27204084042911 COUPLER BOEING737 737301 1384611NM ZONE 205 DAMAGED A AWXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP28326AW7180 2386 23258 ON SHORT FINAL, FIRST OFFICER COULDN`T MOVE RUDDER PEDALS IN EITHER DIRECTION; AFTER LANDING, WITH NOSE WHEEL DOWN AND AT LOWER SPEED, BOTH CAPTAIN AND FIRST OFFICER HAD FULL RUDDER MOVEMENT. MAINTENANCE PERFORMED A VISUAL INSPECTION OF RUDDER PEDAL HARDWARE, FORWARD AND AFT RUDDER CONTROL QUADRANTS IAW BMM 27-21-51 & 27-21-61, NO DEFECTS WERE NOTED. PERFORMED CHECK OF RUDDER FEEL AND CENTERING UNIT PER BMM 27-21-81, AND PERFORMED A RUDDER POWER CONTROL UNIT FUNCTIONAL TEST PER BMM 27-21-91, BOTH CHECKS WERE GOOD. PERFORMED TEST OF FLIGHT CONTROL SHUTOFF VALVE AND RUDDER TRIM CONTROL SYSTEM PER BMM 27--09-31 & 27-21-00, BOTH TESTS WERE GOOD. REMOVED AND REPLACED AUXILIARY ACTUATOR IAW T/C R4B27001, OPERATIONAL 2L72 4F RTA16WE 20030325000892003032500089EU 2003 3 25 03084317 120030325A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU ROW 8 INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27317UE 41031 DUTING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHT AT SEAT ROW 8 WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE FLOOR TRACK EMERGENCY LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030325000962003032500096NM 2003 3 25 AWXA200300258 120030227A5210140N28251 POWER CABLE BOEING757 757225 1384959NM L-2 DOOR FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK THE L-2 DOOR EMERGENCY POWER ACTUATION CABLE FAILED TEST, EXCEEDS 1.0 INCH TRAVEL. MAINTENANCE ADJUSTED THE L-2 DOOR EMERGENCY POWER ACTUATION CABLE IAW BMM 52-11-32, PG. 408, PARA. F, STEP 1-4. EMERGENCY POWER ACTUATION TEST WAS GOOD. IAW BMM 52-11-36, PG. 505. 2L72 4F RTA2NM 20030325001012003032500101NM 2003 3 25 AWXA200300264 120030313A335020131A POWER SUPPLY BOEING757 7572S7 1384962NM EMERGENCY LIGHTSDISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28904AW 23566 PHX - EEL - EMERGENCY LIGHTS AT THE L-2 DOOR, AND JUST AFT OF L-2 DOOR REMAIN ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY AT THE L-2 DOOR POSITION, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030326000402003032600040SW 2003 3 26 AUS20030180 120030217A3213OAS5453 YOKE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR YOKE CRACKED ON INNER SURFACE EXTENDING FROM THE FILLER VALVE UPWARDS FOR A LENGTH OF 10MM (0.393IN). FOUNDDURING ULTRASONIC INSPECTION. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20030326000502003032600050SW 2003 3 26 AUS20030217 120030220A24502719115099 PANEL SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C652 NE AC POWER DISTRIBSHORTED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AUS (AUS) RT NON-ESSENTIAL BUS PANEL EMITTING SMOKE ODOR. INSPECTION FOUND A SHORT CIRCUIT CAUSING MELTING OF THE PLASTIC PANEL. SUSPECT SHORT CIRCUIT WAS CAUSED BY CONDENSATION ON THE PANEL DUE TO EXTREME WEATHER CONDITIONS. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20030121001092003012100109SW 2003 1 21 HEEA083294 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 BELTS (SHOULDER HARNESS) WAS SEWN WRONG SIDE OUT. SHOULDER STRAP ADJUSTMENT ARE ON THE INSIDE (WRONG SIDE). 1G71 3U H2SW 20030121001192003012100119SW 2003 1 21 HEEA083299 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 SEAT BELT RESTRAINT TOO SHORT. 1G71 3U H2SW 20030121001282003012100128 2003 1 21 GLBA2003002 420030110A34216224565001 GYRO BEECH 1900 1900D 1154162CE COCKPIT MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03118GL8438 UE118 AMBER ROL INDICATOR OF EADI SEEMED TO BE F/O'S ADF. REMOVED AND REPLACED NR 2 VG, OPS CHECK GOOD. 2L72 4T RTA24CE 20030121001342003012100134WP 2003 1 21 ABXA030040 120030117A3230 UPLOCK DOUG DC8 DC863F 302198FWP NLG MALFUNCTIONED A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23815AX 46097 CREW REPORTED DURING GEAR UPLATCH CHECK, NOSE GEAR SHOWED NOT UP AND LOCKED. GEAR HANDLE WOULD NOT SEAT INTO UPLATCH POSITION. RECYCLED GEAR DOWN AND UP AS PER ABNORMAL PROCEDURES. RED UNSAFE LIGHT REMAINED ON. AFTER SECOND RECYCLE ATTEMPT, UNSAFE LIGHT AND NOSE GEAR LIGHT OFF. SECOND UPLATCH CHECK SATISFACTORY. INSPECTED NOSE GEAR UPLATCH SYSTEM AND CABLES. NO DEFECTS NOTED. RAISED AIRCRAFT AND PERFORMED NOSE GEAR CONTROL VALVE TEST AND UPLATCH CHECK. ALL PERFORMED AS REQUIRED IAW DC-8 MM 32-32-11-2. NO DEFECTS NOTED. LUBRICATED CONTROL VALVE CABLES AS PRECAUTION. 2L74 4F 4A25 20030121001352003012100135GL 2003 1 21 HEEA083305 220030109A753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 BLEED VALVE PRODUCING HIGHER THAN NORMAL TOT. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 U H2SW E1GL 20030121001402003012100140WP 2003 1 21 AT0300002 120030102A3397 GROUND WIRE DOUG DC9 DC932 3022066WP CABIN DAMAGED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15849AT 47484 DURING B-CHECK FOUND AFT EMERGENCY EXIT (OVERWING) IDENTIFIERS DID NOT WORK. FOUND 3 AO RIVNUT GROUND UNDER LEFT AFT OVERWING EXIT, REPAIRED OPS CHECK GOOD. 2L72 4F A6WE 20030121001522003012100152SW 2003 1 21 HEEA083313 120030109A243523032048 STARTER GEN BELL 206 206B3 1181506SW ENGINE FAILED E HEEAO OTHER O OTHER TXTAXI/GRND HDL 1 SW032268V 3605 STARTER GENERATOR FAILED DURING START ATTEMP. ROTATED FAN BY HAND AND TRIED AGAIN AND STARTER ROTATED BUT SENT SPARKS FLYING. 1G71 3U H2SW 20030121001712003012100171 2003 1 21 IXXA0300001O 420030103A3425 INDICATOR DOUG DC8 DC862F 3021972WP COCKPIT MALFUNCTIONED A IXXAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 SW1131CX 758482523 45911 AFTER DEPARTURE FROM BWI CREW NOTICED FIRST OFFICERS HORIZONTAL SITUATION INDICATOR WOULD NOT ROTATE. CREW DIVERTED TO WRI FOR AN UNEVENTFUL LANDING. MAINTENANCE REPLACED INSTRUMENT AMPLIFIER AND FIRST OFFICERS HORIZONTAL SITUATION INDICATOR IAW WITH THE AIRCRAFT MAINTENANCE MANUAL, PERFORMED A SUCCESSFUL OPERATIONAL CHECK AND RETURNED THE AIRCRAFT TO SERVICE. 2L74 4F 4A25 20030121001802003012100180GL 2003 1 21 HEEA083328 220030109A732125490926 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 FUEL CONTROL UNIT PRODUCING HANG STARTS AND AFTER ONE ADJUSTMENT AIRCRAFT FLAMED OUT. START DERICHMENT ADJUSTER JAM NUT LOOSE. ALSO FOUND START DERICHMENT AND START ACCELERATION ADJUSTER ADJUSTED ALL THE WAY TO THE COUNTER CLOCKWISE STOP. RESET BOTH ADJUSTMENTS TO NORMAL SETTINGS AND UNIT TESTED SATISFACTORY. 1G71 3U3 U H2SW E1GL 20030121001872003012100187GL 2003 1 21 HEEA083333 220030109A7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 51029 GOVERNOR HAS ERRATIC OPERATION. ENGINE LOSES RPM. IN SHOP REPAIR. 1G71 3U3 U H2SW E4CE 20030121001912003012100191EU 2003 1 21 MALA030101 120030103A2751522858 INDICATOR SAAB SF340 340B 7860101EU COCKPIT FAILED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15421XJ 340B421 DURING FLIGHT 3296, CREW REPORTED THE FLAP CAUTION LIGHT AND THE GREEN OVERHEAD LIGHT CAME ON. GREEN FLAP LIGHT ON TEST 1 PANEL LIGHTED APPROXIMATELY 5 TIMES INTERMITTENTLY IN LEVEL FLIGHT. FLAPS INDICATED UP WITH NO SPLIT. AIR RETURN TO MSP. MAINTENANCE REPLACED FLAP INDICATOR IAW SAAB AMM 27-51-00-5. OPS CHECK GOOD. 2L72 4T RTA52EU 20030121001982003012100198SW 2003 1 21 HEEA083342 120030109A771432005008 TACH GENERATOR BELL 206 206L3 1182108SW ENGINE MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW033108E 51498 ENGINE OUT LIGHT AND WARNING HORN INTERMITTENT BETWEEN 40 AND 50 PERCENT N1. REPAIRED. 1G71 3U H2SW 20030121002012003012100201SW 2003 1 21 HEEA083345 120030109A243232007001 BATTERY BELL 206 206L4 1182110SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0362127 52023 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U NCH2SW 20030121002022003012100202SW 2003 1 21 HEEA083346 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0381671 51301 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121002112003012100211GL 2003 1 21 HEEA083354 220030109A73143881005 PUMP BELL 206 206L3 1182108SW ALLSN 250B 250B* GL FUEL SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0330KH 51527 DRIVE SEAL LEAK WASHING OUT FUEL CONTROL DRIVE BEARING. REPAIRED. 1G71 3U3 T H2SW E10CE 20030326000532003032600053EA 2003 3 26 CA030130004 120030121A2752852D10011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAP FAILED W A UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CA (CAN) ON DEPARTURE FLAPS FAILED AT 20 DEGREES. DURING TROUBLE SHOOTING IT WAS DISCOVERED THAT THE FOLLOWING ACTUATORS FAILED THE ACTUATOR TORQUE CHECK AS PER MM 27-53-00-750-002, AND WERE REPLACED. 2L72 4F4 FRTA21EA E15NE 20030326000552003032600055CE 2003 3 26 CA030131005 120030124A551407126294 BRACKET CESSNA206 U206C 2073332CE CONT O520 IO520F 17032SO HORIZONTAL STAB CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) HORIZONTAL STABILILZER REAR RT REINFORCEMENT ATTACH BRACKET WAS FOUND CRACKED .250 INCH LONG. 1H71 3O3 O A4CE E5CE 20030326001082003032600108EA 2003 3 26 A6WA200340033 120030307A2910601R7528651 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HYD SYSTEM LEAKING A A6WAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL31409AW 7447 HYD NR 2 LOW PSI CAS MESSAGE. NR 2 HYD FLUID INDICATES ZERO. REMOVED AND REPLACED NR 2 HYD RETURN LINE. REMOVED AND REPLACED NR 2 HYD PSI LINE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP. 2L72 4F4 FRTA21EA E15NE 20030327000092003032700009EU 2003 3 27 AWXA200300272 120030316A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28658AW12865 1110 CMH - EEL - DURING COCKPIT/CABIN GENERAL CHECK THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (11WL) AT L/H OVER WING EXIT LOWER SIDEWALL IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030327000112003032700011EU 2003 3 27 AWXA200300276 120030314A33501012881 LIGHT AIRBUS320 A320231 3930325EU SEAT ROW 19 LT MISSING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND MISSING FROM SEAT ROW 19 L/H. MAINTENANCE INSTALLED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT IAW A320 SRM 51-42-11, AND SRM 51-44-11. OPERATIONAL CHECK WAS GOOD IAW T/C F1C33301. 2L72 4F RTA28NM 20030327000132003032700013NM 2003 3 27 AWXA200300280 120030228A5311651630087 FRAME BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON FRAME AT RT SIDE OF BS 178 BULKHEAD, WL 207, JUST ABOVE FLOOR. MAINTENANCE REMOVED DAMAGED FRAME AT RT SIDE OF BS 178 BULKHEAD, WL 20; FABRICATED A NEW REPLACEMENT FRAME PER B737-300 SRM 51-40-05, FIG. 2, PG. 4; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 2-4, FIG. 205. 2L72 4F RTA16WE 20030327000242003032700024NM 2003 3 27 AWXA200300296 120030320A3350321430 BATTERY AIRBUSA319 A319132 3930340NM ZONE 221 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING INSPECTION THE FORWARD LT EMERGENCY POWER SUPPLY LOAD WAS FOUND INOPERATIVE ON FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT FORWARD LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030327000772003032700077NM 2003 3 27 C1HA200396004 120030212A3397 SWITCH BOEING727 7272J4 1384006NM LIGHT BURNED A C1HAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15696CA 22574 LEAVING 12000 FT SMELLED STRONG ELECTRICAL BURNING ODOR F/O NOTICED FIRST. NO SMOKE WAS SEEN. NOTICED AUTO COOLING DOOR BEGAN TO OPEN. FOUND 2 POSTS AND WIRES TO WING ILLUMINATION LIGHT SWITCH BURNED. R & R SWITCH AND REPLACED WIRES OPS NORMAL. 2L73 4F RTA3WE 20030327000952003032700095SO 2003 3 27 C2XA03BT043 120030318A3350 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHTSDISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 DURING SERVICE/ROUTINE CHECK FOUND AISLE EMERGENCY LIGHT NR 4 INOPERATIVE. RECONNECTED CONNECTOR PLUG TO AISLE EMERGENCY LIGHT IAW ERJ145AMM 33-50-07. OPS CHECK GOOD. 2L72 4F RTT00011AT 20030327001202003032700120SO 2003 3 27 C2XA03CL050 120030224A323414532170401 SELECTOR EMB 145 EMB145ER 3260211SO MLG MALFUNCTIONED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2715941 145035 ROC FLIGHT 2025 THE CREW REPORTED THE LANDING GEAR WOULD NOT FULLY RETRACT AFTER DEPARTURE FORM ROC. THE GEAR WAS RECYCLED AND STILL DID NOT FULLY RETRACT. THE AIRCRAFT RETURNED AND LANDED IN ROC WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED ICE AND SNOW FROM ALL 3 LANDING GEAR AND REMOVED AND REPLACED THE LANDING GEAR SELECTOR HANDLE FOR CAUTIONARY PURPOSES. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001212003032700121SO 2003 3 27 C2XA03CL051 120030226A27503634001021 SHAFT EMB 145 EMB145LR 3260212SO RT TE FLAP BROKEN A C2XAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SW2722909 145459 CLE FLIGHT 2221 THE CREW REPORTED A FLAP FAIL MESSAGE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLEXIBLE SHAFT NR 2 SECTION ON THE RIGHT INBOARD FLAP. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030303001362003030300136SW 2003 3 3 HEEA084560 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K10523 33020 UNABLE TO TRACK OR BALANCE, M/R BLADE APPEARS TO BE HEAVY. 1G72 4U H4SW 20030303001382003030300138SW 2003 3 3 HEEA084562 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K12928 36001 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030303001392003030300139SW 2003 3 3 HEEA084563 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N11746 33002 MAIN ROTOR BLADE EROSION SHIELD ON THE LOWER SIDE AT THE INBOARD END IS PEELING OFF. 1G72 4U H4SW 20030303001412003030300141WP 2003 3 3 ASAA0280003A 120030103A5260593667467 SKIN DOUG DC9 DC983 3022083WP AFT AIRSTAIRS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT AIRSTAIR SKIN CRACKED AND GOUGED ON RIGHT SIDE. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-10-2, 51-10-4, 51-30-2, 52-03 AND 52-60-0. (M) 2L72 4F RTA6WE 20030303001422003030300142WP 2003 3 3 ASAA0280016A 120030103A57535919217512 HINGE DOUG DC9 DC983 3022083WP T/E FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP CENTER HINGE BEARING BOLT HOLES CORRODED. REMOVED CORROSION AND INSTALLED BUSHINGS IN BOLT HOLES PER EA 5750-01756. (M) 2L72 4F RTA6WE 20030303001832003030300183NM 2003 3 3 QXEA0300308 120030228A3230864202 SENSOR DHAV DHC8 DHC8202 2809007NM ZONE 700 INOPERATIVE A QXEAK NONE O OTHER TOTAKEOFF 1 NM09364PH 524 PDX ON FLIGHT 2197- RETURNED TO FIELD DUE TO ON GEAR RETRACT RIGHT MAIN UNSAFE LIGHT REMAINED ON. ALL THREE GEAR DOOR LIGHTS REMAINED ON. RIGHT MAIN AND NOSE GEAR LIGHT WERE OUT. RECYCLED AS PER CHECKLIST WITH THE SAME RESULTS. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT HAND MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030303001842003030300184SW 2003 3 3 HEEA084566 120030214A6210412015300109 BLADE BELL 412 412EP 1182205SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03412PH11922 36140 MAIN ROTOR BLADE OUTBOARD LEADING EDGE ABRASION STRIP HAS SEVERAL EROSION HOLES. ALSO NEEDS TO BE REBALANCED. SENT TO ROTOR BLADES, INC. FOR WARRANTY REPAIR. 1G72 4U H4SW 20030303001892003030300189WP 2003 3 3 2003804501 120030217A531037558421 FITTING DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM : REF. N/R 1557 AFT CARGO COMPT.: FITTING @ STA. 1240.000 WITH .5000 CRACK CORR: REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG. 21 , FABRICATED NEW FITTING AND DOUBLERS (7075.T651) IAW SRM 53-2-0 FIG 2D , CLEANED ,TREATED , AND PRIMEDFITTING AND DOUBLERSIAW SRM51-1-8B , INSTALLED FITTING AND DOUBLERS IAW SRM53-2-0 FIG. 2D , SRM51-1-20D PG.9 2L74 4F RT4A25 20030321001062003032100106NM 2003 3 21 2003UALA00249 120030308A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29953UA 26700 FWD PIT STATION 482 TO 482B STRINGER 25R TO STRINGER 26R IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL SKIN DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030321001092003032100109NM 2003 3 21 2003UALA00255 120030308A5321 FLOOR PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 CABIN PRESSURE DECK FLOOR HAS EXCESS MATERIAL LOSS AT STA 1681, RBL 43 AND RBL 52. MAJOR REPAIR ACCOMPLISHED. DOUBLER APPLIED. 2L72 4F4 FRTA2NM E17NE 20030324000142003032400014NM 2003 3 24 2003UALA00265 120030307A2740 BUSHING BOEING777 777222 1385219NM PWA PW4077PW4077 NE JACKSCREW CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 HORIZONTAL STABILIZER JACKSCREW BUSHING FOUND TO BE DAMAGED/CRACKED. DURING SHOP INSPECTION, JACKSCREW BUSHING FOUND TO BE DAMAGED AND/OR CRACKED WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20030324000162003032400016NM 2003 3 24 2003UALA00267 120030311A2782 ACTUATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LE FLAPS MALFUNCTIONED A UALAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 WP29392UA 24667 AIRCRAFT PREPARED FOR DIVERSION WHEN LEADING EDGE FLAP DID NOT DEPLOY. LEADING EDGE FLAP DEPLOYED ON FINAL APPROACH, AND AIRCRAFT LANDED AT PLANNED DESTINATION. THE NR 1 FLAP ACTUATOR WAS REPLACED. ACTUATOR WAS REMOVED AND SENT TO SHOP FOR REWORK. 2L72 4F4 FRTA16WE E2GL 20030324000182003032400018NM 2003 3 24 2003UALA00269 120030312A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 EXTERNAL FUSELAGE SKIN STA 626 RBL 3 AT VHF ANTENNA HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030324000272003032400027 2003 3 24 GLBA2003035 420030321A3400066030620008 ALTIMETER BEECH 1900 1900D 1154162CE A GLBAD RETURN TO BLOCK I FLT. ATTITUDE INST. CLCLIMB 1 NM03251GL7342 UE251 #1 ALTIMETER RED FLAGGED, R&R ALTIMETER 2L72 4T RTA24CE 20030324000292003032400029NM 2003 3 24 CALA0300136 120030321A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912313 23364 INSPECTION FOUND FLOORBEAM SCREW HOLES CORRODED AT TOP AND BOTTOM OF UPPER CAP AT BS 1006, LBBL 16.5, 20, AND 27.75. REMOVED AND REPLACED T-CAP IAW SRM 51-20-02 AND PERFORMED SPLICE REPAIR IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030324000322003032400032NM 2003 3 24 CALA0300141 120030323A5230 SKIN BOEING737 7373T0 1384582NM AFT CARGO DR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912313 23364 MAINTENANCE NOTED DAMAGE TO THE INNER SKIN AT AN ACCESS PANEL LOCATION DURING REPAIR OF AN AFT CARGO DOOR THAT HAD BEEN REMOVED FROM AIRCRAFT.. THE DAMAGE CONSISTED OF A 1.1" AND 0.5" CRACK AND AN AREA OF DEFORMED SKIN. THE SKIN WAS REPAIRED IAW ECRA 5230-01717. 2L72 4F RTA16WE 20030324000392003032400039EU 2003 3 24 40002 120030306A3260D228580001 PROXIMITY SWITCH AMD FALC50FALCON900 2700160EU NLG OUT OF ADJUST E ERYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07369BG16 16 040 LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. CONFIRMED GEAR DOWN AND LANDED AT DEPARTURE AIRPORT. RAMP AND TAXIWAY WERE SNOW AND SLUSHY. RUNWAY WAS DRY. A FERRY PERMIT WAS OBTAINED TO GO TO MAINTENANCE. AIRCRAFT WAS JACKED UP, SWANG GEAR, WHERE NO DEFECTS WERE NOTED. A CONCURRENT TEST FLIGHT WAS PERFORMED WHERE THE PROBLEM OCCURRED AGAIN. AIRCRAFT CONTINUED TO GARRETT SPRINGFIELD ON THE TEST FLIGHT WHERE THE GEAR WAS AGAIN CONFIRMED DOWN AND LOCKED. LANDED AT GARRETT SPRINGFIELD WHERE THE AIRCRAFT WAS AGAIN JACKED UP, GEAR SWUNG, WHERE MAINTENANCE CAME TO THE DETERMINATION THAT THE NOSE GEAR PROXIMITY SWITCHES NEEDED ADJUSTMENT. AIRCRAFT WAS RETURNED TO SERVICE AFTER SUBSEQUENT SUCESSFUL TEST FLIGHT. 2L73 4F RTA46EU 20030324000452003032400045NE 2003 3 24 ABXA030099 220030304A7200 ENGINE BOEING767 767281 1385109NM GE CF6 CF680A 30025NE NR 2 LEAKING A ABXAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL23789AX1589 23022 580270 RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED EICAS MESSAGE, RIGHT ENGINE OIL PRESSURE WAS ZERO. OIL QUANTITY ZERO. ENGINE SHUT DOWN. N2 RPM WAS NORMAL AFTER SHUT DOWN. REPLACED THE NR 2 OIL SCAVENGE PUMP, NO HELP, OIL CONTINUED TO LEAK. REMOVED AND REPLACED THE NR 2 ENGINE IAW JOB CARD 7010 AND B767 MM. 2L72 4F4 FRTA1NM E13NE 20030324000462003032400046WP 2003 3 24 ABXA030100 120030306A5210 SKIN DOUG DC8 DC861 3021952WP PAX DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 CREW ENTRY DOOR WOULD NOT CLOSE AND LOCK, OR OPEN PROPERLY. REPAIRED AFT UPPER CORNER OF MAIN ENTRY DOOR SKIN IAW DC-8 SRM 52-2-0 AND REA D852-46903. OPS CHECKED GOOD. 2L74 4F 4A25 20030324000492003032400049WP 2003 3 24 ABXA030104 120030220A5220591015931 PAN DOUG DC9 DC931 3022065WP EMERGENCY DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 LEFT FORWARD EMERGENCY DOOR HAD CRACKED PAN AT LOWER AFT FITTING. REPLACED LEFT FORWARD EMERGENCY DOOR IAW DC-9 MM 52-21-00-5-0001. 2L72 4F A6WE 20030324000612003032400061WP 2003 3 24 ABXA030119 120030320A5610 WINDOW DOUG DC9 DC941 302207NWP COCKPIT OUT OF ADJUST A ABXAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23958AX 47760 CAPTAIN'S SIDE WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT WINDOW HOOK IAW DC-9 56-10-03-5-0002. OPS CHECKED GOOD. 2L72 4F A6WE 20030324000622003032400062CE 2003 3 24 ACE030320031 120030303A2822RA5326 DIAPHRAGM BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA FUEL PUMP RUPTURED E YADAK NONE K FLUID LOSS ININSP/MAINT 1 AL0341UE UC41 FUEL WAS FOUND LEAKING FROM NR 1 ENGINE GANG DRAIN - REPLACED LOW PSI FUEL PUMP. DETERMINED THAT DIAPHRAGM WAS RUPTURED 2L72 4T4 TRTA24CE E4EA 20030324000742003032400074SO 2003 3 24 C2XA037 120030322A510014522460015 GUSSET EMB 145 EMB145ER 3260211SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 DURING A SCHEDULED 3C INSPECTION, A GOUGE WAS DISCOVERED ON THE TOP CAP LOCATED IN THE GALLEY AREA, JUST AFT OF THE FWD. DIGITAL. THE AFT GUSSET WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 5170-02. ACFT. WAS RELEASED FOR SERVICE AFTER THE COMPLETION OF THE 3C CHECK. 2L72 4F RTT00011AT 20030324000782003032400078CE 2003 3 24 AMWA7 120030129A71201299100471 TRUSS BEECH 1900 1900D 1154162CE ENGINE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07139ZV5088 5088 UE139 WHILE PERFORMING AN "H" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND A CRACK LOCATED ON THE TRUSS. THE CRACK IS YET TO BE DETERMINED OF THE LOCATION. MAINTENANCE REMOVED AND REPLACED IT WITH ANOTHER ENGINE TRUSS. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20030324000822003032400082WP 2003 3 24 ARWA20030209 120030226A2611100064901 SMOKE DETECTOR DOUG DC8 DC861 3021952WP CARGO BAY FAILED A ARWAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1929UA 46159 ON PRE-FLIGHT, LOWER CARGO SMOKE DETECTOR MAINTENANCE LIGHT ON. ENTERED ON DMI 17527 IAW MEL 26-10-1-1A. REMOVED AND REPLACED LOWER SMOKE DETECTOR UNIT (SDU) FA 16037. OPERATIONAL CHECK IAW STC ST00746LA-D FOUND NORMAL. CLEARED DMI # 17527 AND REMOVED PLACARD. 2L74 4F 4A25 20030324000832003032400083WP 2003 3 24 ARWA20030211 120030227A2612390D AMPLIFIER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 FIRE DETECTFAILED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO19784AL 46135 645355 SHORTLY AFTER TAKEOFF FIRE WARNING ON ENGINE NR 2. REMOVED AND REPLACED NR 2 FIRE DETECTOR AMPLIFIER. OPERATIONAL CHECK NORMAL IAW MM 26-10-0 AND ENGINE RUN UP IAW MM 71-00. 2L74 4F4 F 4A25 1E8 20030324000882003032400088WP 2003 3 24 ARWA20030307 120030312A5311 FRAME DOUG DC8 DC863 302198AWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA. 1280 BETWEEN L-20R AND L-21R FRAME WITH 0.5 INCH CRACK. 2L74 4F 4A25 20030324000892003032400089WP 2003 3 24 ARWA20030308 120030312A5711 SPAR CAP DOUG DC8 DC863 302198AWP LT WING CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; LT WING STA. XRS 22.000 - STA.XRS 74.000 REAR SPAR UPPER CAP FLANGE WITH 8.00 INCH CRACK. 2L74 4F 4A25 20030324000902003032400090WP 2003 3 24 ARWA20030309 120030312A5712 PANEL DOUG DC8 DC863 302198AWP LT MLG WW DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; LT W/W STA 902 STRAP PANEL AND SPLICE FITTING AFT FLANGE BOTH SIDE WITH OUT OF LIMITS CHECK IAW SB 53-61. REPLACED TRAPEZOLDAL FITTING P/N 5750092-505 IAW DC8 REPLACEMENT GUIDE AND DC-8-63 INSTALLATION DRAWING 5750127, DC8 MM MAIN GEAR LINKAGE 32-11-3 AND SERVICE BULLETIN NR 53-61 REV. 3, DATED 05/11/72. BORED TRAP FITTING PER DOUGLAS B/P 5611440 USING TOLL 5611425 SF1 NR 2, INSTALLED (2) P/N 2641877 BUSHINGS PER 5715353. 2L74 4F 4A25 20030324000912003032400091WP 2003 3 24 ARWA20030311 120030318A2910 CONNECTOR LKHEED1011 1011385115 5265015WP HYD SYSTEM LOOSE A ARWAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19307GB 193U1131 SYSTEM "B" RESERVOIR QUANTITY LOW AND DECREASING. SWITCHING PUMP AND ATM OFF STOPPED FLUID LOSS. TIGHTENED CONNECTOR AT "B" SYSTEM ATM PRESSURE SWITCH IAW M/M 29-11-00. OPERATIONAL CHECK ON GROUND NORMAL. 2L73 4F A23WE 20030324000922003032400092WP 2003 3 24 AT0300006 120030308A7500 DUCT DOUG DC9 DC932 3022066WP LT PACK BLOWN A ZZDAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO15831AT 47674 AFT LAVATORY SMOKE DETECTORS WENT OFF APPROXIMATELY F/L 220. AFT FLIGHT ATTENDANT REPORTED HEAVY ELECTRICAL SMELL. MINUTES LATER LEFT AFT LEFT LAV SMOKE DETECTOR WENT OFF. INSPECTED AIRCRAFT FOUND LT PACK OVERHEATED AND DUCT BLOWN OFF ACM. PRESSURIZED A/C TO 4.0 DIFFERENTIAL WITH RIGHT PACK, NO SMELL NOTED. RESECURED LINE IN CABIN BETWEEN RIGHT AND LEFT PACK AND RESECURED INLET DUCT TO LEFT ACM CLAMP. 2L72 4F A6WE 20030324000962003032400096EA 2003 3 24 03083657 120030324A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 During maintenance inspection, the l/h aft overwing emergency exit light was found to be inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030324000982003032400098NM 2003 3 24 AWXA200300089 120030128A351089151114 BOTTLE AIRBUSA319 A319132 3930340NM OXYGEN SYS DISCHARGED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28805AW 1049 FLT 0820 - WHILE EN ROUTE FROM BOS TO PHX CREW OXYGEN WENT TO ZERO, DIVERTED TO ROC. MAINTENANCE REMOVED AND REPLACED THE CREW OXYGEN BOTTLE IAW AWA T/C R2A35301. PERFORMED LEAK CHECK OF ALL CONNECTIONS AT BOTTLE, ALSO CHECK ALL MASKS FOR CORRECT STOWAGE AND LEAKS, NO LEAKS NOTED DURING 2 HOUR PERIOD. 2L72 4F RTA28NM 20030324001032003032400103EU 2003 3 24 AWXA200300094 120030119A3350 BATTERY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28640AW3718823437 448 MCN - EEL - DURING C-07 CHECK THE EMERGENCY LIGHTS FAIL TEST ON CIDS AS REQUIRED ON TASK CARD R1A25301 STEP 7. MAINTENANCE REMOVED AND REPLACED BATTERIES AT EMERGENCY POWER SUPPLY UNITS (11WL) AND (12WL) IAW AMM 33-51-38-04, SUBTASK 33-51-38-020-053, AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-38-04, TASK 33-51-38-000-001; OPERATIONAL TEST GOOD IAW AMM 33-51-38-04, TASK 33-51-38-04, AND TASK 33-51-358-000-001. 2L72 4F RTA28NM 20030314000782003031400078WP 2003 3 14 CALA0300091 120030303A5347 CARGO TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND AFT BAGGAGE BIN RT TIE DOWN TRACK HOLES CORRODED AT STA 1136 - 1155. A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 53-23-00. 2L72 4F A6WE 20030314000922003031400092NM 2003 3 14 SWAA030540 120030307A53116545776 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 927, WL 160, RT. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030314000962003031400096 2003 3 14 SWAA030545 420030308A256565C19901 CABLE BOEING737 7373H4 1384600NM AFT ENTRY DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030314000982003031400098NM 2003 3 14 SWAA030549 120030308A32106582770 FITTING BOEING737 7373H4 1384600NM BOTH LT/RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT/RT MLG FWD OTBD FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG OTBD FITTINGS PER MM. 2L72 4F RTA16WE 20030314001052003031400105NE 2003 3 14 A4J2003F00000 220030218A7200444625 TUBE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE BYPASS DUCT FAILED A A4JAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO35933JK 48159 ON CLIMB OUT FROM FLL (FLIGHT NR 304) ENROUTE, NR 1 ENGINE REQUIRED MORE THROTTLE TO MAINTAIN EQUAL POWER TO NR 2 ENGINE. AT 25,000 FEET, FUEL FLOW ON NR 1 ENGINE WAS 3000 LBS HIGHER THAN NR 2 ENGINE AND AS THE THROTTLES WERE RETARDED NR 1 ENGINE STOPPED PROVIDING POWER. AIRCRAFT DIVERTED FOR MAINTENANCE. AFTER TROUBLESHOOTING, MAINTENANCE FOUND ONE FAILED 6TH STAGE BLEED AIR TRANSFER TUBE AND ONE MISSING 6TH STAGE BLEED AIR TRANSFER TUBE. THE ENGINE WAS REPAIRED AND RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20030314001092003031400109NM 2003 3 14 BJNA030216 120030225A55516547596 FITTING BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE HORIZONTAL STAB CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM46484 23046 DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND IN THE BORES OF THE HORIZONTAL STABILIZER CENTER SECTION FORWARD TERMINAL FITTINGS UPPER AND LOWER AFT LUGS. THE BORES WERE REAMED TO THE MAXIMUM DIAMETER (1.125 INCH) SHOWN IAW SB. AFTER REAMING INSPECTION SHOWED THAT CORROSION WAS STILL PRESENT. REO-L00628 PROVIDED FOR ADDITIONAL REAMING OF THE SUBJECT BORES TO REMOVE THE CORROSION, AND FOR THE FABRICATING AND INSTALLATION OF OVERSIZED BUSHINGS. REPAIR APPROVED, AND 8110-3 ISSUED BY DER RICHARD C SALTIVAN. 2L72 4F4 FRTA16WE E2EA 20030314001122003031400112NM 2003 3 14 BJNA03024 120030205A532069583471 SUPPORT BRACKET BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM46484 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN APU BLEED AIR SUPPORT BRACKET LOCATED IN THE AFT PIT ACCESSORY COMPARTMENT AT STA 1016. REMOVED AND REPLACED THE CORRODED SUPPORT BRACKET IAW SRM. 2L72 4F4 FRTA16WE E2EA 20030314001152003031400115NM 2003 3 14 BJNA03025 120030206A5320 FLOOR SUPPORT BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT ANGLE LOCATED AT BS 285, BL 12L, WL 208.1. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT ANGLE FROM BAC 1510-335 EXTRUSION. DIMENSION OF REPAIR IS APPROXIMATELY 3.3750 INCHES X 30.5000 INCHES. WORK WAS DONE IAW SRM. 2L72 4F4 FRTA16WE E2EA 20030314001312003031400131WP 2003 3 14 GTIA030108 120030207A5330 DOUBLER DOUG DC9 DC981 3022081WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 MID CARGO RADIO ALT ANTENNA DOUBLER CORRODED FS 687-688, STR 30-27L. REMOVED DOUBLER. LOCATED AND DRILLED HOLES ON DOUBLER. INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20030314001362003031400136WP 2003 3 14 GTIA030113 120030207A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE COCKPIT CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 FLIGHT COMPARTMENT STA 138 CORRODED ON WEB UNDER INBOARD CAPTAINS SEAT TRACK. REMOVED DAMAGED AREA OF WEB. FABBED NEW WEB SECTION. FABRICATED SPLICE. INSTALLED SPLICE. INSTALLED NEW WEB SECTION FS 133, FS 160, RBL 4, LBL30. 2L72 4F4 F A6WE E2EA 20030314001382003031400138WP 2003 3 14 GTIA030115 120030302A3350 SIGN DOUG DC9 DC941 302207NWP PWA JT8 JT8D17 52049NE TAILCONE INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23130NK 47604 TAILCONE INTERIOR LUMINESCENT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED TAILCONE INTERION LUMINESCENT EXIT SIGN. OPS CHECK GOOD. 2L72 4F4 F A6WE E2EA 20030314001392003031400139WP 2003 3 14 GTIA030116 120030302A25601001191 FLASHLIGHT DOUG DC9 DC941 302207NWP PWA JT8 JT8D17 52049NE CABIN INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23130NK 47604 FORWARD F/A HANDHELD EMERGENCY LIGHT, INOPERATIVE. REMOVED AND REPLACED FWD HANDHELD EMERGENCY LIGHT. OPS CHECK GOOD. 2L72 4F4 F A6WE E2EA 20030314001442003031400144 2003 3 14 KC82003F00001 420030210A3422 CONNECTOR AMD FALCONFALCON20 2730103EU GE CF700 CF700* 30010NE ADI LOOSE A KC8AO OTHER O OTHER NRNOT REPORTED 1 GL23980R 98 CREW REPORTED (NO PITCH FUNCTION ON CAPTAINS ADI). FOUND CONNECTOR ON THE PILOTS FLIGHT DIRECTOR INDICATOR LOOSE. CLEANED DEBRIS FROM THREADED END OF CONNECTOR AND RESECURED CONNECTOR. MANEUVERED VERTICAL GYRO FROM MOUNTED PLATFORM AND VERIFIED PITCH AND ROLL FUNCTIONS. 2L72 4F4 FRTA7EU E7EA 20030314001452003031400145CE 2003 3 14 MXI2003F00000 120030201A24979224223603 PANEL BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE CIRCUIT BREAKER ARCED E MXIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA21476BJ RK176 ELT PANEL LIGHT AROUND RTU2 (REMOTE TUNING UNIT NR 2) CIRCUIT BREAKER ARCED CAUSING SMOKE IN THE COCKPIT. REPLACED PANEL WITH NEW PANEL. 2H72 4F4 FRTA16SW E25EA 20030121002122003012100212 2003 1 21 HEEA083355 420030109A3442 FACEPLATE BELL 206 206L1 1182107SW CONTROL HEAD DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033905B 612 45598 CONTROL HEAD HAS A BROKEN KNOB. FACEPLATE UNREADABLE. REPLACED BAD FACEPLATE, BAD VOLUME CONTROL AND KNOB, BAD CHANNEL KNOB AND BAD TONE SWITCH. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030121002412003012100241 2003 1 21 HEEA083361 420030109A341344600045800 INDICATOR BELL 206 206L3 1182108SW VERTICAL SPEED ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 VSI INDICATES ERRATIC ALTITUDE CHANGES. 1G71 3U H2SW 20030121002482003012100248GL 2003 1 21 HEEA083365 220030109A731347101 FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X3115 51552 ENGINE FUEL NOZZLE WORN. REPLACED AIR SHROUD DUE TO WORN. 1G71 3U3 U H2SW E4CE 20030121002522003012100252 2003 1 21 CA030107016 420030105A22207273090002 COMPUTER BOEING737 737217 1384464NM PWA JT8 JT8D17 52049NE ELEVATOR FEEL FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA (CAN) MACH TRIM LIGHT CAME ON IN FLIGHT, CREW REPORTED ELEVATOR FEEL INOPERATIVE. AIRCRAFT RETURNED TO DEPARTURE STATION. ELEVATOR FEEL COMPUTER REPLACED AS PER AMM. AND OPERATION CHECKED SERVICEABLE. 2L72 4F4 F A16WE E2EA 20030121002682003012100268NM 2003 1 21 PCAA0301011 120030107A3397 WIRE DHAV DHC8 DHC8102 2809003NM CABIN DAMAGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13835EX 289 DURING ROUTINE MAINTENANCE VISIT 6TH RED FLOOR LEVEL EMERGENCY LIGHT FOUND INOPERATIVE. LEAD WIRE REPAIRED AT ATTACH POINT TO BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030314000142003031400014NM 2003 3 14 ANCF200300010 120030302A21606259469 CONTROLLER BOEING767 767383 1385214NM PACK TEMP MALFUNCTIONED W ANCFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23984AN303888640 24357 DURING FLIGHT APPEARED: "LT PACK INOP IN AUTO AND STANDBY", EICAS MSG "R ENG HPSOV" AND "R ENG BLEED LIGHT". FLIGHT RETURNED TO BOGOTA. LT PACK TEMPERATURE CONTROLLER AND HPSOV CONTROLLER WERE REPLACED IN ACCORDING WITH AMM 21-51-14 PAG 401 AND AMM 36-11-08 PAG401 WITH SATISFACTORY RESULTS 2L72 4F RTA1NM 20030314000182003031400018 2003 3 14 MEX2003029 420030207A2565 SLIDE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE CABIN STUCK W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23802AM 26270 AIRCRAFT RETURNED TO PLATFORM, LEFT AFT SLIDE WAS NOT ARMED. ARMED AND DISARMED MECHANISM OF LEFT AFT SLIDE WAS CHECKED, IT WAS STUCK. BAR WAS REMOVED AND REINSTALLED IAW MM, TESTS CORRECT. 2L72 4F4 FRTA2NM E17NE 20030314000342003031400034NM 2003 3 14 2003740520 120030224A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CABIN FRAME BS 380 CRACKED AT STRINGER 7L. CUT OUT DAMAGED AREA DIM 2 INCH X 1 INCH AND FABBED REPAIR DOUBLER FROM 7075 T6 .071 PO 991208 DIM 8 INCH X 4 INCH IAW SRM 53-10-2 & 53-10-4 FIG 2. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED IAW SRM 53-10-4 FIG 2. 2L73 4F RTA3WE 20030314000432003031400043WP 2003 3 14 ABXA030083 120030225A3260 SENSOR DOUG DC9 DC941 302207NWP MLG DOOR FAILED A ABXAO OTHER P NO WARNING INDICATION LDLANDING 1 GL23964AX 47781 AFTER LANDING GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. AFTER CYCLING GEAR, THE LIGHT REMAINED ON FOR ONE MINUTE, THEN WENT OUT. REMOVED AND REPLACED THE NOSE LANDING GEAR LOCK SENSOR IAW DC-9 MM 32-60-01-2. 2L72 4F A6WE 20030314000452003031400045NM 2003 3 14 ABXA030085 120030221A5310 DOOR FRAME BOEING767 767231 1385131NM MAIN PAX DOOR CONTAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23708AX 22571 EMERGENCY SLIDE WOULD NOT ARM. FOUND DEBRIS IN MAIN ENTRY DOOR JAMB, REMOVED DEBRIS. DOOR CLOSED AND EMERGENCY SLIDE ARMED AS REQUIRED IAW B767 MM. 2L72 4F RTA1NM 20030314000472003031400047WP 2003 3 14 ABXA030087 120030131A5311995774013 FRAME DOUG DC9 DC931 3022065WP LEFT KEEL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 FRAME STATION 622 CRACKED AT LEFT CANTED KEEL. REPAIRED FRAME IAW DC-9 SRM K05159. 2L72 4F A6WE 20030314000492003031400049WP 2003 3 14 ABXA030089 120030131A5330 DOUBLER DOUG DC9 DC931 3022065WP RT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 DOUBLER AT RIGHT WHEEL WELL UPPER PRESSURE PANEL CRACKED AT STATION 76, RIGHT BUTT LINE 55. REMOVED DOUBLER AND INSTALLED NEW DOUBLER IAW DWG NR 9919155 AND DC-9 SRM 51-30-3. 2L72 4F A6WE 20030314000532003031400053WP 2003 3 14 ABXA030097 120030228A3260 DOWNLOCK SWITCH DOUG DC8 DC863F 302198FWP MLG MALFUNCTIONED A ABXAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23819AX 45927 UPON LOWERING LANDING GEAR, LEFT GEAR DOWN LIGHT DID NOT ILLUMINATE AS WELL AS NO RED UNSAFE LIGHT. RAISED GEAR, RED UNSAFE LIGHT ILLUMINATED WITH NO NOT LATCHED LIGHT ILLUMINATED IN ANY POSITION. UPLATCH CHECK NORMAL INDICATION. LOWERED GEAR AGAIN WITH NO ABNORMAL INDICATION. FOUND LEFT MAIN LANDING GEAR DOWN LOCK SWITCH HAD MALFUNCTIONED. REPLACED LEFT MAIN LANDING GEAR DOWNLOCK SWITCH IAW DC-8 MM 32-60-00-2-0001. OPS CHECKED GOOD. 2L74 4F 4A25 20030314000552003031400055WP 2003 3 14 AT0300004 120030222A2133 OUTFLOW VALVE DOUG DC9 DC932 3022066WP CABIN PRESSURE ICED A ZZDAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO15832AT 47451 LOST CABIN PRESSURIZATION AT 20,000 FT IN ICING CONDITIONS. SELECTED MANUAL AND THE VALVE WOULD NOT CLOSE ALL THE WAY. MASKS DROPPED SUSPECT ICING AFTER 30 MINUTE HOLD. OPERATED OUTFLOW VALVE AND PRESSURIZED TO 3 PSI, OPS NORMAL REF MM 21-32. MASK DROPPED CHECK AND REPACK MASK, NO DEFECTS NOTED. 2L72 4F A6WE 20030314000562003031400056NE 2003 3 14 AT0300005 220030221A7200BRR700715A130 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 1 STALLED A ZZDAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO15991AT 55135 LT OIL PRESSURE ZERO AND XXED OUT ON DISPLAY UNIT, COMPRESSOR STALL ENGINE SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE. 2L72 4F4 FTRA6WE E00061EN 20030324001112003032400111WP 2003 3 24 MWEA030141 120030324A5347593056675 SEAT TRACK DOUG DC9 DC981 3022081WP STA 1265 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 # 1&2 SEAT TRACK HAS CORROSION AT FRAME STATION 1265. -- BLENDED SEAT TRACK, LOCATED,DRILLED AND INSTALLED REPAIR. 2L72 4F A6WE 20030324001132003032400113NM 2003 3 24 AWXA200300101 120030202A5300 STRUCTURE BOEING757 7572S7 1384962NM AIRFRAME VIBRATION A AWXAO OTHER E VIBRATION/BUFFET APAPPROACH 1 WP28905AW 23567 LAS - EMERGENCY LANDING - FLT 0048 - ON APPROACH INTO LAS EN ROUTE FROM DCA WITH FLAPS AT 5, LANDING GEAR DOWN, AND SPEED BRAKES ARMED, A VIBRATION DEVELOPED THROUGHOUT THE AIRCRAFT. HYDRAULICS AND ENGINE INDICATIONS APPEARED NORMAL, AND AIRCRAFT CONTROL WAS NOT A PROBLEM, DECLARED AN EMERGENCY, AND LANDED WITHOUT EVENT. MAINTENANCE INSPECTED FUSELAGE AND WINGS FOR LOOSE OR MISSING PANELS; INSPECTED THE FLIGHT CONTROLS, FLAPS, LANDING GEAR, AND LANDING GEAR DOORS; INSPECTED THE TAIL AND HORIZONTAL STABILIZER, ALL CHECKS WERE GOOD. 2L72 4F RTA2NM 20030324001182003032400118NM 2003 3 24 AWXA200300108 120030125A53116546539 FRAME BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK A 2 INCH CRACK WAS FOUND ON 957 FRAME AT CENTER SECTION INTERIOR LT BS 616 OVER WING EXIT. MAINTENANCE TRIMMED OUT CRACK ON CHORD FRAME AT CENTER SECTION INTERIOR LT BS 616; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5311-01143-DD1. 2L72 4F RTA16WE 20030324001252003032400125SO 2003 3 24 C2XA037TY 120030324A510014522460015 GUSSET EMB 145 EMB145ER 3260211SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 DURING A SCHEDULED 3C INSPECTION, A GOUGE WAS FOUND ON THE TOP CAP LOCATED IN THE GALLEY AREA AFT OF THE FWD. DIGITAL. THE AFT GUSSET WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 51-70-02. THE ACFT. WAS RELEASED FOR SERVICE FOLLOING THE COMPLETION OF THE SCHEDULED INSPECTION. 2L72 4F RTT00011AT 20030324001292003032400129NM 2003 3 24 UPS03440337 120030305A5310 LONGERON BOEING747 747200 1384847NM FWD CARGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C FWD CARGO COMP - STA 740 S47R STINGER SPLICE HEAVY CORROSION REVEALE D STRINGER SPLICE REPLACED AS PER SRM 51-10-01 P.8. (DEPTH 0.040", WIDTH 1", LENGTH 2") 2L74 4F RTA20WE 20030324001312003032400131NE 2003 3 24 COMA0360162 220030321A7270 FAN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE A COMAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SO01984CA 7171 FLIGHT 5490 VIB WARNING WHEN T/O THRUST APPLIED.COULD NOT DUPLICATE - INSPECTED ENGINE AND FOUND NO DISCREPANCIES, C/W A FAN TRIM BALANCE AND REDUCED VIB FROM .9 TO .4 2L72 4F4 FRTA21EA E15NE 20030324001332003032400133EA 2003 3 24 COMA0360159 120030320A2710 BELLCRANK CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01915CA 7013 AILERON CONTROLS PARTIALLY JAMMED IN FLIGHT WITH AP TRIM LWD CAUTION.COULD NOT DUPLICATE - DISCREPANCEY ON GROUND - CLEANED AND LUBED AILERON BELLCRANKS AND ADJUSTED WHEEL BIN SPLASH GUARDS I/A/W COMAIR E.O. 27-069 RB. 2L72 4F RTA21EA 20030325000162003032500016NM 2003 3 25 AWXA200300126 120030125A53156546803 FLOORBEAM BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK A .1562 INCH CRACK WAS FOUND EXTENDING BEYOND STOP DRILL HOLE ON FORWARD FACE OF FLOORBEAM AT BS 520. MAINTENANCE CUTOUT MATERIAL FROM FORWARD END OF INTERCOSTAL AND CHANNEL RADIUS FILLER BS 520; FABRICATED A NEW INTERCOSTAL TEE; AND INSTALLED REPAIR PART IAW SB 737-53-1120, AND AWA E.O. 53-14-12, PG. 1-17. 2L72 4F4 FRTA16WE E2GL 20030325000342003032500034EU 2003 3 25 AWXA200300151 120030206A5315D5347209001000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND AT TWO HOLES ON UPPER SURFACE OF FLOORBEAM BETWEEN FR 65 - 66, BS 3101 - 3158. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 65 - 66, BS 3101 - 3158; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11, PG. 1-2. 2L72 4F RTA28NM 20030325000352003032500035EU 2003 3 25 AWXA200300152 120030206A5315D5347209000200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM MOUNT HOLE JUST FORWARD OF FR 66, BS 3155. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM BETWEEN FR 64 - 66, BS 3155; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11, PG. 1-2. 2L72 4F RTA28NM 20030625001222003062500122EU 2003 6 25 AWXA200300219 120030301A2611CG7G0 SMOKE DETECTOR AIRBUS320 A320231 3930325EU ZONE 128 FAULTY A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28633AW42232 082 AIR TURNBACK, AFTER TAKEOFF RECEIVED ECAM MESSAGE TO LAND AS SOON AS POSSIBLE, PULLED UP LAST LEG REPORT THAT INDICATED AVIONIC SMOKE FAULT. RESET CIRCUIT BREAKERS PER MX & CAPTS EMERGENCY AUTHORITY. BROUGHT UP AVIONIC SMOKE CHECKLIST & DECLARED AN EMERGENCY, TURNED BACK TO FLL AND LANDED WITHOUT INCIDENT. MX PERFORMED TROUBLESHOOTING OF AVIONICS CODING & SMOKE DETECTOR SYS. REMOVED & REPLACED SMOKE DETECTOR SENSOR AND SMOKE WARNING RELAY. OPS CHECK WAS GOOD PER AMM TASK 26-15-00-710-001. PART NAME; RELAY, MFG; ALLIED SIGNAL, P/N; E0245-28AO. VENDOR CONFIRMED FAILURE OF SMOKE DETECTOR S/N 1055. NO REASON GIVEN FOR FAILURE. PART DEEMED AS BEYOND ECONOMICAL REPAIR & WAS EXCHANGED WITH UPGRADED M&E. 2L72 4F RTA28NM 20030325000632003032500063EU 2003 3 25 AWXA200300226 220030301A7230 COMPRESSOR BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 1 ENGINE STALLED A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28328AW 23377 720698 DURING TAKEOFF AT BOI EN ROUTE FOR PHX HEARD LOUD POP ON LT SIDE OF AIRCRAFT, SUSPECTED COMPRESSOR STALL AND REJECTED TAKEOFF AT 90 KTS. BOISE MAINTENANCE PERFORMED INSPECTION OF THE NR 1 ENGINE IAW BMM 71-00-00 PG. 248 & 249, ENGINE RUN AT ALL PARAMETERS WAS GOOD. 2L72 4F4 FRTA16WE E21EU 20030325000652003032500065NM 2003 3 25 AWXA200300228 120030303A2121EVT3454H FAN AIRBUSA319 A319132 3930340NM ZONE 128 FAILED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 WP28813AW10429 1350 DURING SHORT APPROACH AT TPA, A LIGHT BURNING ODOR WAS OBSERVED IN FLIGHT DECK AFTER LANDING, RECEIVED ECAM MESSAGE "VENT EXTRACT FAULT". MAINTENANCE DISCOVERED EXTRACT VENT FAN CIRCUIT BREAKER POPPED, ISSUED DPI MEL 21-26-02 , COND. 1 "EXTRACT FAN INOP". WHEN FLIGHT ARRIVED BACK IN PHX MAINTENANCE REMOVED AND REPLACED AVIONICS COOLING FAN (18HQ) IAW AMM TASK 21-26-51-000-001, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN OF AVIONICS COOLING FAN S/N 4203 CONFIRMED FAILURE OF UNIT. INCOMING INSPECTION FOUND FAN WAS SEIZED AND UNABLE TO PERFORM ENTRY TEST. TEARDOWN OF UNIT IDENTIFIED THAT FRONT BEARING CAME APART DAMAGING THE FRONT FLANGE AND SPACER. FAN WAS EXCHANGED BY VENDOR. 2L72 4F RTA28NM 20030325000672003032500067NM 2003 3 25 AWXA200300231 120030305A3397 CONNECTOR BOEING757 757225 1384959NM EMERGENCY LIGHT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28907AW 22691 EMERGENCY LIGHT SEAT HARNESS CONNECTOR BROKEN. CONTACTED MAINTENANCE TO FIND OUT SEAT ROW NUMBER, TECHNICIAN NOT AVAILABLE. 2L72 4F RTA2NM 20030325000812003032500081NM 2003 3 25 AWXA200300251 120030311A2133VFT300B00 OUTFLOW VALVE AIRBUSA319 A319132 3930340NM ZONE 126 MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28807AW13431 1064 AFTER TAKEOFF FROM PIT EN ROUTE FOR PHX RECEIVED ECAM MESSAGE FOR VENT SKIN AIR VALVE FAULT. COMPLIED WITH ECAM INSTRUCTIONS AND DIVERTED TO CMH. MAINTENANCE FOUND AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC) FAULTING 22HQ SKIN/AIR VALVE. VALVE WAS PREVIOUSLY ON MEL AND WAS LOCKED OUT. REMOVED AND REPLACED SKIN/AIR VALVE IAW T/C R2A21301. DURING OPERATIONAL TEST PRESSURE SWITCH 17HQ FAULTED, REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 21-26-11-04. OPERATIONAL TEST OF AEVC SYSTEM WAS GOOD PER T/C F1B21301. PART NAME; SWITCH PRESSURE, MFG; IN LHC GROUPE, P/N 1209-100, LOC; ZONE 121. 2L72 4F RTA28NM 20030314001532003031400153 2003 3 14 PA03004 420030206A2210 CONTROLLER GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE AUTOTHROTTLE SYSMALFUNCTIONED E UG8AO OTHER J WARNING INDICATION CLCLIMB 1 GL23910DC 544 ABNORMAL AUTOTHROTTLE DISENGAGMENT OCCURRED AFTER TAKEOFF. PERFORMED AUTOTHROTTLE OPERATIONAL CHECK IAW MM. NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA12EA E00057EN 20030314001672003031400167NE 2003 3 14 UIEA200300007 220030205A7200 ENGINE BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE NR 3 INOPERATIVE A UIEAEA ENGINE SHUTDOWN UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA15518MC 23476 517545 DURING CLIMB OUT AT APPROXIMATELY 18,800 FT, NR 3 ENGINE HAD THREE LOUD BANGS. WHEN THROTTLE WAS RETARDED BANGS STOPPED. THRUST LEVER REMAINED AT IDLE FOR REMAINDER OF THE FLIGHT. THE ONLY INDICATION NOTICED WAS THAT THE N1 WAS AROUND 76 PERCENT AT ONE POINT. CHANGE ENGINE IAW MM. POWERPLANT REMOVAL/INSTALLATION. 2L74 4F4 F A20WE E23EA 20030314001722003031400172NM 2003 3 14 USAABB03033 120030305A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE ROW 1 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19621AU 27200 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 1, INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F4 FRTA2NM A12EU 20030314001842003031400184SO 2003 3 14 000243 120030130A2761 ACTUATOR EMB 145 EMB145 3260210SO SPEED BRAKE LEAKING A CHQAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11299 HYDRAULIC QUANTITY ON EICAS HYDRAULIC QUANTITY WENT FROM MIDDLE OF GREEN ARC BEFORE TAKEOFF TO MIDDLE OF AMBER DURING FLIGHT. FOUND INBOARD SPEED BRAKE ACUATOR LEAKING. R&R'D SPEED BRAKE SPOILER ACTUATOR. 2L72 4F RTT00011AT 20030314001862003031400186SO 2003 3 14 000245 120030305A4920 APU EMB 145 EMB145 3260210SO APU BAY CONTAMINATED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11280 LAV SMOKE WARNING AND SMOKE IN THE CABIN AND COCKPIT IMMEDIATELY AFTER TAKEOFF DETERMINED TO BE FROM DEICE FLUID IN THE APU FROM DEICING. RAN ALL DEICE FLUID OUT OF APU AND ENGINE AND PACK BLEED SYSTEMS AND OPS CHECK GOOD 2L72 4F RTT00011AT 20030314001902003031400190 2003 3 14 00080 420030225A2300 TRANSMITTER LEAR 24 24E 5170316CE GE CJ610 CJ610* 30006NE NR 1 COMMS INOPERATIVE E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05330TW 330 PILOT REPORTED AIRCRAFT WOULD NOT PRESSURIZE OUT OF 10,000 FT, ALSO COMS HAD STATIC, DIVERT INTO SDF FOR MAINTENANCE. WILL UPDATE REPORT AFTER MAINTENANCE. MAINTENANCE CLEANED SQUAT SWITCHES, JACKED AIRCRAFT AND PERFORMED OPERATIONAL CHECKS, PRESSURIZE CHECKED GOOD ON GROUND, REPLACED NR1 COM TRANSMITTER. OPS CHECKED GOOD, RETURN AIRCRAFT TO SERVICE. 2L72 4J4 J A10CE 1E16 20030314001942003031400194CE 2003 3 14 00085 120030304A2910 LINE LEAR 24 24E 5170316CE GE CJ610 CJ610* 30006NE HYDRAULIC SYS INOPERATIVE E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05330TW 330 PILOT REPORTED AFTER DEPARTURE FROM SHV HYDRULIC PRESSURE DROPPED TO 0 UPON GEAR RETRACTION AND FLAP RETRACTION, AIRCRAFT DIVERTED TO ADS STANDBY PUMP WAS USED TO EXTEND GEAR AND FLAPS FOR NORMAL LANDING. WILL UPDATE THIS REPORT AFTER MAINTENANCE. HYDRULIC (PRESSURE SIDE) HOSE LT SIDE FAILD, PRECAUTIONARY PUMP CHANGE BOTH SIDES AND HOSE REPLACEMENT. OP'S AND LEAK CK GOOD. 2L72 4J4 J A10CE 1E16 20030314002002003031400200SO 2003 3 14 030011693 120030313A5620159SCC10317 WINDOW GULSTMG1159 G1159A 3970109SO CABIN CRACKED B Y3PRK NONE O OTHER ININSP/MAINT 1 SO35477SJ 477 LT NR 3 CABIN WINDOW OUTER PANE IC CRACKED. CRACK IS APPROX 4 INCHES. CRACKED WAS FOUND DURING A FUSELAGE EXTERNAL INSPECTION. 2L72 4F A12EA 20030314002082003031400208WP 2003 3 14 ZW0A0303001 120030308A335041B004AD07G3 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139302B 49528 THE FWD OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 10-1-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030314002112003031400211NM 2003 3 14 0300416314 120030307A3350 LIGHT BOEING747 747451 1384940NM SSEAT 22H INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01674US 30269 DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM LAV DR2R-SEAT 22H. RECONNECTED WIRE, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030314002152003031400215SO 2003 3 14 C2XA03BT037 120030313A4900 APU EMB 145 EMB145 3260210SO TAIL CONE SEIZED A C2XAFO ACTIVATE FIRE EXT. OTHER AY FLAME/FIRE ENGINE STOPPAGE NRNOT REPORTED 1 SW2713968 145138 EWR FLT2578 CREW REPORTED DURING APU START APU FAILED INDICATION WAS INSTRUCTED I HAD A FIRE BLEW EXTINGUISHER BOTTLE. MX FOUND APU SIEZED INSPECTED AND PLACED ON MEL. #49-00-00. ACFT RELEASED FOR SERVICE. SDR REMAINS OPEN. 2L72 4F RTT00011AT 20030314002212003031400221EA 2003 3 14 03054674 120030212A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE DOME EMER LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27674BR 7601 DOME EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030314002242003031400224EA 2003 3 14 03060620BR 120030301A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27620BR 7179 DURING PREFLIGHT INSPECTION LEFT BULKHEAD EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030314002262003031400226EU 2003 3 14 03062311 120030303A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE3312 01514WP CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27311UE 41029 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE LEFT FORWARD AND AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE LAMP SOCKET ON THE FORWARD LIGHT AND REPAIRED AN ELECTRICAL CONNECTION ON THE AFT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E3WE 20030314000602003031400060NM 2003 3 14 CALA0300022 120030202A253072067752 OVEN BOEING737 737524 1384721NM AFT GALLEY INOPERATIVE A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW091962324649 27527 THE AIRCRAFT WAS RETURNED TO LAX AFTER SMOKE WAS REPORTED IN THE AFT GALLEY. THE AIRCRAFT LANDED SAFELY AT LAX WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT GALLEY RIGHT OVEN VERY HOT TO THE TOUCH AND THE COMPARTMENT ABOVE THE OVEN WAS ALSO VERY HOT. MAINTENANCE CONFIRMED THE OVEN WAS AT FAULT. THE OVEN WAS REMOVED AND REPLACED. ALL AFT GALLEY OVENS WERE RUN FOR THIRTY MINUTES WITH NO SMOKE OBSERVED. 2L72 4F RTA16WE 20030314000652003031400065NM 2003 3 14 CALA0300034 120030210A5347 GALLEY TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND GALLEY FLOOR TRACK CORRODED BETWEEN BS 277 - 294 AT RBL 36. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030314000672003031400067NM 2003 3 14 CALA0300045 120030212A3230A42006028305 SOLENOID BOEING737 7373T0 1384582NM MLG CONT LEVER INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0914342 23580 THE CREW WAS UNABLE TO RAISE THE GEAR HANDLE PAST THE OFF POSITION AFTER TAKEOFF. THE GEAR OVERRIDE TRIGGER WAS USED TO RAISE GEAR. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER LOCK SOLENOID IAW MM 32-31-31-024-001, PAGE 401-404. 2L72 4F RTA16WE 20030314000752003031400075NM 2003 3 14 CALA0300080 120030301A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914307 23358 INSPECTION FOUND A 2 INCH CRACK IN PRESSURE DECK AT BS 664, LBL 30. REPAIRED IAW ECRA 5360-01078. 2L72 4F RTA16WE 20030314000892003031400089NM 2003 3 14 SWAA030531 120030310A53306550531 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 270.875 & BS 274, AT STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030314000912003031400091NM 2003 3 14 SWAA030538 120030309A304032315 CONTROLLER BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAK NONE O OTHER UKUNKNOWN 1 SW29310SW 22949 L2 WINDOW ARCING, TURNED OFF WINDOW HEAT, ARCING STOPPED. REMOVED AND REPLACED L2 WINDOW HEAT CONTROLLER AND PWR CHORD PER MM. 2L72 4F RTA16WE 20030314000942003031400094 2003 3 14 SWAA030542 420030308A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030314000952003031400095 2003 3 14 SWAA030543 420030308A2565D31354 SLIDE BOEING737 7377H4 1384404NM FWD SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030314001182003031400118 2003 3 14 SWAA030562 420030311A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH FWD CABIN DOOR SLIDES PER MM. 2L72 4F RTA16WE 20030314001202003031400120NM 2003 3 14 BJNA303217 120030227A5311 FRAME BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM46484 23046 DURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON A FRAME MEMBER LOCATED AT BS787 BETWEEN STRINGERS 22 AND 24 LEFT. 2L72 4F4 FRTA16WE E2EA 20030314001252003031400125CE 2003 3 14 CWQ2003F00001 120030212A21206542072101 DUCT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE DORSAL SCOOP CRACKED B CWQRK NONE O OTHER ININSP/MAINT 1 GL05363QS2919 5600536 DURING ROUTINE INSPECTION, LOOKED INTO DORSAL NACA SCOOPS AND SAW THE LOWER AIR VANE WITH A 3 IN CRACK STARTING FROM CENTER OF (V) CUT TO OUTBOARD EDGE. GAINED ACCESS FROM THE TAILCONE BAGGAGE AREA AND REMOVED CRACKED VANE. REMOVED EA 9309 WHICH SECURES VANE INTO PLACE. ORDERED NEW PART, INSTALLED NEW VANE AND WAS VERY LIBERAL WITH THE EA 9309 IAW MFG STANDARD PRACTICES. UPON REMOVAL NOTICED THAT THE (V) CUT APPEARS TO HAVE BEEN CUT WITH HAND SNIPS AND THERE WAS NO RELIEF HOLE AT BOTTOM OF CUT, ALSO THERE WAS VERY LITTLE EA 9309 SECURING INTO PLACE. UPON FURTHER INSPECTION OF BAD PART NOTICED THAT THE CRACK WAS WORKING TOWARDS THE EDGE WHERE IT MIGHT HAVE COME LOOSE LIKE OTHERS WE HAVE FOUND. (SCR 88915)2L72 4F4 FRTA22CE E25EA 20030314001302003031400130WP 2003 3 14 GTIA030107 120030211A5320 INTERCOSTAL DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 INTERCOSTAL ASSY STA 630 TO 636, RBL 3, CORRODED. DISASSEMBLED INTERCOSTAL ASSY. GUSSET FOUND TO BE OUT OF LIMITS. FABRICATED NEW PART. 2L72 4F4 F A6WE E2EA 20030314001342003031400134WP 2003 3 14 GTIA030111 120030211A5313 LONGERON DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 MAIN CABIN FS 256, STR 17R, CORRODED. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED LONGERON SECTION AND LONGERON SPLICES. INSTALLED LONGERON AND SPLICES. 2L72 4F4 F A6WE E2EA 20030314001372003031400137WP 2003 3 14 GTIA030114 120030228A2820 FITTING DOUG DC9 DC932 3022066WP FUEL MANIFOLD LEAKING A GTIAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL2312536 47113 RIGHT WHEEL WELL AFT FUEL MANIFOLD INBOARD SIDE DRIPPING FUEL. RESECURED LOOSE FITTING AT APU FUEL LINE SHROUD CONNECTION. LEAK CHECK GOOD. 2L72 4F A6WE 20030314001412003031400141EA 2003 3 14 COMA0360144 120030311A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS APAPPROACH 1 SO01956CA 7105 FLIGHT 5103 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030314002312003031400231NM 2003 3 14 UPS03240277 120030218A2750 FLAP TRACK BOEING727 727108C 1384039NM #6 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI #6 FLAP TRACK HAS SUSPECT CRACK FROM HOLE F ON SPOILER SUPPORT BEAM PAD REPLACED #6 FLAP TRACK IAW MM 27-51-31 2L73 4F A3WE 20030314002322003031400232NM 2003 3 14 UPS03240278 120030225A5753 STIFFENER BOEING727 727108C 1384039NM #6 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI #6 FLAP TRACK AFT O/B ATTACH POINT VERTICAL STIFFENER ON R/H FALSE S PAR CRACKED STIFFENER REMOVED IAW SRM 51-30-2. STIFFENER REPLACED IAW SRM 51-30 -02 & DRAWING 65-16216 2L73 4F A3WE 20030314002342003031400234EU 2003 3 14 03069330 120030307A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27330UE 41098 DURING MAINTENANCE/INSPECTION FOUND RT EXTERNAL FWD EMERGENCY LIGHT OUT. MAINTENANCE PERSONNEL INSPECTED FWD RIGHT EXTERNAL EMERGENCY LIGHT, FOUND BOTH BULBS OPERATIONAL. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA41NM 20030314002372003031400237NM 2003 3 14 CALA0300116 120030314A5347 SEAT TRACK BOEING777 777224 1385225NM BS 1500 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0974007 29477 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1500, RBL 88. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-2 AND 51-40-02. 2L72 4F RTT00001SE 20030315000022003031500002EU 2003 3 15 DHL2003367502 120030303A7830 FLANGE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 517321 Item Ref. N/R 0029640:T/R fwd. skin attach cracked on #2 O/B T/R. Corrective action:Cut out damaged area,fabricated repair IAW Timco REO-GO9089. Alodined an primed IAW A300 SRM 51-40-10 an installed IAW A300 SRM 51-30-30. 2L72 4F4 FRTA35EU E23EA 20030316000072003031600007EU 2003 3 16 RAIA00303064 120030305A3060AN60 FUSE JETAIRJETSTMJETSTM4101 1500501EU BLOWN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03559HK 41075 5478-STL- RIGHT PROPELLER HEAT FAIL. MAINTENANCE REMOVED AND REPLACED FUSE, AND SHIMMED BRUSH BLOCK, OPS CK OK. 2L72 4T RTA41NM 20030317000012003031700001NM 2003 3 17 2003F00145 120030131A2931 WARNING LIGHT BOEING737 737* NM HYD SYSTEM ILLUMINATED A UG8AB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 SO19732MA 30618 DURING CRUISE DESCENT TO BGR, ENGINE DRIVEN HYDRAULIC PUMPS AMBER LIGHTS CAME ON. WHEN FLAPS SELECTED, 'A' SYSTEM SHOWED '0' QTY AND '0' PRESSURE. DECLARED AN EMERGENCY AND COMPLETED 'A' SYSTEM FAIL CHECKLIST. AIRCRAFT WAS LANDED AT BGR WITHOUT INCIDENT. (M) 2L72 4F RTA16WE 20030317000022003031700002SO 2003 3 17 2003F00146 120030210A53211159B51417 FLOOR PANEL GULSTMGV GULFSTREAMGV3980116SO APU BAY CHAFED A UG8AK NONE O OTHER ININSP/MAINT 1 GL235101 550 APU COMPARTMENT FLOOR HAS CHAFING MARK .020 INCHES DEEP. CHAF DAMAGE CAUSED BY APU DRAIN HOSE ID TAB RUBBING AGAINST FLOOR. PROVIDED PROPER CLEARANCE. REPAIRED RUB DAMAGE IAW GULFSTREAM REPAIR LETTER DRAWING SE55053001 DATED 2/6/2003. (M) 2L72 4F RTA12EA 20030317000042003031700004NE 2003 3 17 2003F00148 220030131A7250 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE BROKEN A GUUACD ABORTED TAKEOFF RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO1969549 UE194 PS0004 FLT - 9161 - DURNG TAKEOFF, LOUD BANG OCCURRED ON LEFT ENGINE. ABORTED TAKEOFF. SEPARATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT FOUR POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODUEL AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. SUSPECT NR 2 PT BLADE FAILURE. (M) 2L72 4T4 TRTA24CE E26NE 20030317000072003031700007NM 2003 3 17 03FDEA00134 120030215A21307110025 CONTROL PANEL BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE CABIN PRESSURE FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25284FE5467 5467 22621 DURING CLIMB OUT AT MEM, COULD NOT PRESSURIZE, AUTO FAIL, STB. MANUAL NOTHING WORKED, PILOTS WINDOW HAD LOUD WIND NOISE BUT AIR FLOW NOT ENOUGH TO AFFECT PRESSURE, RAN EMERGENCY CHECKLIST AND NOTHING HAPPENED, RETURNED TO FIELD. PRESSURIZED AIRCRAFT TO 3 PSI ON GROUND USING HUFFER WITH BOTH PACKS. NO LEAKS NOTED ON ANY SEALS OR DUCTS. WHILE USING ENG PNUEMATICS THE PACKS WOULD NOT COME ON AND TRIPPING GENERATORS AND HEAVY DRAW ON ELE SYS. FOUND E/E BAY SOAKED, PUT COLD BUSTER IN E/E TO DRY OUT. PERFORMED OPS CHECK ON PNU. SYS CONTROLLER AND CHECK PASSED. REMOVED AND REPLACED CABIN PRESS CONTROL PANEL IAW M/M 21-31-010-4. OPS CHECKED NORMAL. 2L73 4F4 FRTA3WE E2EA 20030317000202003031700020NM 2003 3 17 03FDEA00153 120030221A5330 SKIN BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 DENT IN SKIN BS 460-480 BETWEEN 14.15R 2L73 4F4 F A3WE E2EA 20030317000212003031700021NM 2003 3 17 03FDEA00154 120030221A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON STR 24L AT BS 312. CORROSION ON STR 24 LT AT B.S 312, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. STRINGER 24 LT REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20030317000262003031700026NM 2003 3 17 03FDEA00159 120030220A5730ARB73952 SKIN DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE WING, ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING, TOP SKIN JUST FWD OF FUEL DUMP VALVE PIPE FOUND WITH CORROSION. CENTER OUTER WING, UPPER SKIN CORROSION REWORK CARRIED OUT IAW EA 1-5720-67573. 2L73 4F4 FRTA22WE E13NE 20030317000302003031700030NM 2003 3 17 03FDEA00164 120030220A5750ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END, OUTBOARD FITTING FOUND CORROSION . WING TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD. FLAP OUTBOARD HINGE BRACKET REPAIR CARRIED OUT IAW E.A. 1-5750-67572. 2L73 4F4 FRTA22WE E13NE 20030317000342003031700034NM 2003 3 17 03FDEA00168 120030224A5330 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 344, LBL 3, TO LBL 60. REMOVED CORROSION ON UPPER LOBE OF FLOORBEAM AT 344, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED REPAIR UPPER LOBE IAW SRM 53-10-8, SR 27-53-007, 53-10-1. 2L73 4F4 F A3WE E2EA 20030325000832003032500083NM 2003 3 25 0300596316 120030321A3350 LIGHT BOEING747 747451 1384940NM ROW 9F INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01676NW 33002 DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 9F - DOOR 2L. REPAIRED WIRE AND OPERTATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030625001322003062500132NM 2003 6 25 03FDEA00344 120030313A5753ARC199113 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING OUTBOARD FLAP FOUND OUTBOARD MOST HINGE FITTING HOLE QTY. 02 EACH WITH CORROSION. LT WING OUTBD FLAP, OUTBD MOST HINGE FITTING CORROSION CARRIED OUT REPAIR IAW FEDEX EA 1-5750-67577 2L73 4F RTA22WE 20030325000922003032500092NM 2003 3 25 371PA0019 120030323A3350362624 LIGHT BOEING737 737306 13844BGNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 FORWARD 4 FT. SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. REPLACED FWD 16 FT. POWER STRIP & 2EA. 26 INCH FLEX LAMPS. EMERGENCY PATH LIGHTS OPS OK PER MM 33-51-02. 2L72 4F RTA16NE 20030409000112003040900011NM 2003 4 9 ANCF200300012 120030319A21301942723 HEAT EXCHANGER BOEING767 767383 1385214NM AC PACK CONTAMINATED W ANCFAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SO23984AN 24357 CABIN ALT & CABIN ALT LIGHTS ILLUM, EICAS MESSAGE CABIN ALTITUDE WAS DISPLAYED. UNABLE TO RESTORE CABIN PRESS USING MANUAL MODE, O2 MASKS DEPLOYED. ALSO WAS PRESENTED EICAS MSG FWD CARGO A/C AND FWD CARGO A/C INOP LIGHT ILLUM WHEN THE FLT ARRIVED LT PACK WAS FOUND TRIPPED BY "FWD A/C CARGO FAULT" AND RT PACK DEFICIENT. FOR LT PACK, PACK FLOW AND CARGO A/C CONTROLLER (PFCAC) WAS R & R IAW AMM AND "AUX TEMP CONTROLLER" REPLACED IAW AMM WITH SAT RESULTS. FOR RT PACK, PRIMARY & SECONDARY HEAT EXCHANGERS WERE REPLACED IAW AMM. CONTAMINATION FOUND IN SECONDARY EXCHANGER, IT WAS REPLACED. LOW LIMIT VALVE PACK RT IAW AMM WITH NORMAL RESULTS. ACCOMPLISHED PRESSURIZATION & TEST OF PACKS, PRESSURIZED TO 4 UNITS OF DI2L72 4F RTA1NM 20030326000262003032600026EU 2003 3 26 AUS20030121 120030206A5730HC573H0002000 SKIN BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT LOWER WING SKIN CHAFED ON WATER SCAVENGE PIPE DEBRIS GUARDS. CORROSION WAS ALSO FOUND IN THE SAME AREA BETWEEN FRAME 14 AND FRAME 15. 2H74 4F4 FRTA49EU E6NE 20030326000372003032600037NE 2003 3 26 AUS20030153 220030211A7261 FILTER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE ENGINE DAMAGED W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 AUS (AUS) NR 1 ENGINE OIL FILTER THREAD STRIPPED. PERSONNEL/MAINTENANCE ERROR. 2L73 4F4 FRTA3WE E2EA 20030326000582003032600058 2003 3 26 CA030203003 420030202A3140 DISPLAY BOMBDRBD700 BD7001A10 1390006GL RROYCEBR700 BR700710A22009500NE COCKPIT INTERMITTENT W O OTHER O OTHER CLCLIMB 1 CA (CAN) ON CLIMB OUT, CO-PILOT'S PRIMARY DISPLAYS LOST ALL VIDEO DATA, AND SCREENS HAD A RED X. THIS WAS QUICKLY FOLLOWED BY THE SAME LOSS OF DATA AND RED X ON PILOT'S PRIMARY DISPLAYS. EICAS BEGAN TO FILL UP WITH NUMEROUS AMBER MESSAGES, THEN PILOT'S ANDCO-PILOT'S DISPLAYS RETURNED TO NORMAL AND ALL EICAS MESSAGES WERE GONE. THIS ALL HAPPENED OVER A PERIOD OF ABOUT 20-30 SECONDS. PILOT'S WERE OVERWEIGHT FOR LANDING AND PERFORMED SOME TESTING FOR A PREVIOUS FLIGHT SNAG. APU WAS STARTED AS A PRECAUTION, AND A/C RETURNED TO MONTREAL. THERE WERE NO MORE PROBLEMS UNTIL AFTER ENGINES WERE SHUT DOWN, WITH APU ON LINE. CO-PILOT'S DISPLAYS LOST VIDEO DATA WITH THE RED X AND THERE WERE NUMEROUS AMBER EICAS MESSAGES. 2L72 4F4 FRTT00003NYE00061EN 20030326000762003032600076WP 2003 3 26 03FDEA00349 120030325A2780ARH7024615 CONTROL CABLE DOUG DC10 DC1010 3022110WP LEFT WING SLAT CUT A FDEAO OTHER O OTHER LDLANDING 1 SO2568052 47806 LT WING NR 7 SLAT EXTEND CABLE HAS ALL BUT ONE STRAND CUT AT O/B PULLY. FOUND ON W/C 57SI5502-02 AND TRANSFERRED TO N/R N00275. REMOVED AND REPLACED NR 7 SLAT EXTEND CABLE, TENSIONED LT NR 7 SLAT EXTEND AND RETRACT CABLE AND OP'S CHECK GOOD, ALL IAW M/M 27-80-00-5-2. 2L73 4F A22WE 20030326000822003032600082NM 2003 3 26 2003UALA00277 120030316A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 FUSELAGE FRAME HAD CRACK OUT OF FASTENER HOLE AT STA.827 STR.9L (AIR GRILL SUPPORT) MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030326000842003032600084NM 2003 3 26 2003UALA00279 120030316A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 FUSELAGE FRAME AT STA. 867 STR.9L HAD CRACK OUT OF FASTENER HOLE (AIR GRILL SUPPORT). MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030326000852003032600085NM 2003 3 26 2003UALA00285 120030316A5330 SKIN BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29618UA 21878 A/C DAMAGED BY LOADER AFT OF FWD CARGO DOOR. VARIOUS DENTS AND GOUGES MAJOR REPAIR ACCOMPLISHED WITH DOUBLERS IN AREA FWD OF CARGO DOOR BELOW RT WING LITE. 2L72 4F4 FRTA1NM E3NE 20030326000912003032600091NM 2003 3 26 2003UALA00294 120030218A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BULKHEAD CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 STATION 178 BULKHEAD RH SIDE FRAME CRACKED ABOVE AND BELOW WL 207. MAJOR REPAIR ACCOMPLISHED. SPLICED SIDE FRAME. 2L72 4F4 FRTA16WE E2GL 20030326000932003032600093NM 2003 3 26 2003UALA00296 120030210A5511189W26006 RIB BOEING777 777222 1385219NM PWA PW4077PW4077 NE HORIZONTAL STAB CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 LT O/B HORIZONTAL STABILIZER CLOSE-OUT RIB POST IS DAMAGED/CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACKED RIB POST WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20030326000952003032600095NM 2003 3 26 2003UALA00298 120030318A5320 WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 HORIZONTAL ATTACH WEB BETWEEN FRAMES 188 AND 196 WL 207 CRACKED AT LIGHTNING HOLE AND AT AFT INBOARD CORNER RADIUS CUT OUT AT STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED WEB REPAIR. 2L72 4F4 FRTA16WE E2GL 20030416001962003041600196NM 2003 4 16 AALA20030291 120030306A5320 PLATE BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21624AA 24582 TUL - FOUND DECKPLATE AFT. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-60-51. (M) 2L72 4F RTA2NM 20030314001422003031400142CE 2003 3 14 GUU2003F00006 120030221A2621 CONTACTOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT FIRE BOTTLE DIRTY A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1717541 UE203 DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT FLICKERS. CONTINUED TO DESTINATION. CLEANED CONTACTS AT LEFT FIRE BOTTLE. OPERATIONAL CHECK, OK. 2L72 4T3 TRTA24CE E2NE 20030314001482003031400148NE 2003 3 14 O9I2003F00000 220030201A726130607016 HOUSING ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE73140 29001NE LT ENG SUMP LEAKING B O9IRO OTHER K FLUID LOSS NRNOT REPORTED 1 NM0989HS 1441 089 P113125 PILOT REPORTED OIL ON LEFT ENGINE COWLING AFTER FLIGHT. PERFORMED GROUND RUN OF ENGINE AND FOUND PIN HOLE IN ENGINE DRIVEN OIL SUPPLY PUMP HOUSING. 2L72 4F4 FRTA16NM E1NM 20030314001522003031400152 2003 3 14 PA03003 420030206A2210 CONTROLLER GULSTMGV GULFSTREAMGV3980116SO AUTOTHROTTLE SYSFAILED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL23920DC2719 534 AUTOTHROTTLE 2 NUMEROUS INTERMITTENT FAILURES. FOUND NO FAILURES REPORTED IN MDUA FAULT HISTORY. OPERATIONALLY CHECKED AUTOTHROTTLE SYSTEM CHANNELS 1 AND 2 IAW CMP CODE 223005 SEVERAL TIMES WITH NO FAILURES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA12EA 20030314001552003031400155NE 2003 3 14 S2Y2003F00000 220030121A7260 ENGINE DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT UNDERSERVICED A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13354SK 3126 DURING TAKEOFF, A LEFT HIGH OIL PRESSURE AMBER CAS MESSAGE APPEARED. THE CREW MADE A LOW SPEED ABORTED TAKE OFF. MECHANIC DOWN LOADED THE ENGINE EDU WITH NO FAULTS FOUND. MECHANIC SERVICED THE LEFT ENGINE WITH ONE QUART OF OIL AND RETURN THE AIRCRAFT TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030314001642003031400164NE 2003 3 14 S2YA03003 220030121A7260 ENGINE DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT UNDERSERVICED A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13354SK 3126 DURING TAKEOFF, A LEFT HIGH OIL PRESSURE AMBER CAS MESSAGE APPEARED. THE CREW MADE A LOW SPEED ABORTED TAKE OFF. MECHANIC DOWN LOADED THE ENGINE EDU WITH NO FAULTS FOUND. MECHANIC SERVICE THE LEFT ENGINE WITH ONE QUART OF OIL AND RETURN THE AIRCRAFT TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030314001752003031400175NE 2003 3 14 WRLA200302 220030218A726121S00434 PRESSURE SWITCH DOUG DC10 DC10* WP GE CF6 CF650* 30018NE NR 3 ENGINE INOPERATIVE A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11541SA 46541 NR 3 ENGINE OIL STRAINER CLOG CAME ON AFTER TAKEOFF LIGHT-SHUT DOWN ENGINE. IAW FLIGHT MANUAL PROCEDURES, RETURNED TO DEPARTURE STATION. REMOVED AND REPLACED NR 3 OIL STRAINER PRESSURE SWITCH. PERFORMED ENGINE RUN UP PRESSURE AND TEMPERATURE NORMAL SYSTEM OPS/LEAK CHECK, GOOD. FILTER INSPECTION CLEAN, NO DEFECTS. C/A: REPLACED OIL PRESSURE SWITCH AND FILTER. 2L73 4F4 F A22WE E23EA 20030314001792003031400179CE 2003 3 14 X5C2003F00000 120030131A2821WF334761 FILTER ELEMENT LEAR 24 24 5170302CE GE CF6 CF6* 30020GL MAIN FUEL SYS DIRTY E X5CAK NONE J WARNING INDICATION ININSP/MAINT 1 GL17991TD 24124 DURING SCHEDULED MAINTNANCE, REPLACED MAIN FUEL FILTERS WITH ELEMENTS. EXPERENCED LOW FUEL PRESSURE LIGHT AT HIGH ENGINE POWER SETTINGS WITH JET PUMP OPERATION. LIGHT AT HIGH ENGINE POWER SETTINGS JET PUMP OPERATION. LIGHT WOULD EXTINGUISH WITH STANDBY BOOST PUMP ON AND MOTIVE FLOW VALVE CLOSED. REPLACED FILTERS WITH ELEMENTS. FOUND NO OTHER SYSTEM PROBLEMS WHICH MY HAVE AFFECTED FUEL PRESSURE. AIRCRAFT OPERATION NORMAL PRIOR TO FILTER REPLACEMENT AND AGAIN NORMAL AFTER REMOVAL OF FILTERS AND REPLACEMENT. 2L72 4J4 F A10CE E23EA 20030314001882003031400188NE 2003 3 14 00079 220030220A7200 FUEL NOZZLE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE RT ENGINE MALFUNCTIONED E HAEAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW05221TW 221 304359B PILOT REPORTED, DURING DECENT RT ENGINE FLAMED OUT, ATC NOTIFIED, RESTART OF RT ENGINE PERFORMED, UNEVENTFUL LANDING. DURING TAXI, GROUND CONTROL REPORTED FLAMES SHOOTING OUT OF TAIL PIPE. RT ENGINE, WILL UPDATE THIS SDR AFTER MAINTENANCE. PRECAUTIONARY ENGINE CHANGE PERFORMED. AIRCRAFT RETURNED TO SERVICE. ENGINE SHOP FOUND SECONDARY AND PRIMARY ENGINE FUEL NOZZLES WORKING AT SAME TIME, O/H FUEL NOZZLES. 2L72 4F4 F A7EU E7EA 20030314001922003031400192EU 2003 3 14 00082 120030224A3231 DOOR AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE MLG INOPERATIVE E HAEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW05158TW 158 AIRCRAFT DEPARTED, PILOT REPORTED GEAR DOORS DID NOT FULLY CLOSE, DIVERTED FOR MAINTENANCE. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS SYSTEM CHECKED GOOD. 2L72 4F4 F A7EU E7EA 20030314002022003031400202NM 2003 3 14 0300306314 120030227A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHTSDISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01674US 30269 DURING LINE CHECK FOUND LT (A) ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRE, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030314002062003031400206WP 2003 3 14 0300509953 120030307A5330 SKIN DOUG DC9 DC931 3022065WP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 During "L" check found cracks in fuselage nose skin BS 69.5 fastener holes. Repaired per EA 99-190934. 2L72 4F A6WE 20030314002072003031400207SO 2003 3 14 C2XA03TY035 120030314A53131452G759001 STRINGER EMB 145 EMB145LR 3260212SO GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716911 145446 TYS, During a scheduled inspection a gouge was found at stringer 19R center fuselage IV. Maintenance blended, performed dye-pen inspection, fabricated and installed repair angle and shims. I/A/W-EMB-145-SRM-53-24-02, 51-40-02 and CPM-51-21-06. The repair was satisfactory and aircraft was released to service. 2L72 4T RTT00011AT 20030314002092003031400209WP 2003 3 14 ZW0A0303003 120030310A33508039001 BATTERY DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13982TW 53632 THE TAIL CONE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED BOTH BATTERY PACKS, AT B5-27 AND B5-28. CHECK-C 11-19-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030314002162003031400216EU 2003 3 14 0302251 120030225A2750 LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE FLAP TEST ILLUMINATED A UHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL17340SZ 340A004 02/25/03 FLT 4471 TTN-BED. CREW REPORTED FLAP AND GREEN OVERHEAD TEST LIGHTS ILLUMINATED IN FLIGHT. AIRCRAFT TURNED BACK TO TTN. 2L72 4T4 TRTA52EU E8NE 20030314002222003031400222NM 2003 3 14 03057414 120030226A33508GH00567806 LAMP DORNERDO32 DO328300 NM PWA 306 PW306B NE LAV EMER LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27414FJ 3169 EMERGENCY LIGHT IN LAVORTORY INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED EMERGENCY LIGHT, OPERATIONAL CHECK GOOD AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2H72 4T4 FRTA55NM E35NE 20030314002232003031400223EU 2003 3 14 03058311 120030227A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33112UHR WP CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27311UE 41029 DURING PREFLIGHT INSPECTION THE FLIGHT CREW FOUND EMERGENCY TRACK LIGHTING BETWEEN ROWS 3A AND 4A. MAINTNANCE PERSONNEL PERFORMED OPERATIONAL CHECK OF EMERGENCY TRACK LIGHTING SYSTEM AND FOUND NO DEFECTS. AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4T4 TRTA41NM E4WE 20030314002252003031400225EU 2003 3 14 03061317 120030302A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27317UE 41031 DURING MAINTENANCE INSPECTION, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T3 TRTA41NM E2WE 20030314002292003031400229EU 2003 3 14 03069302 120030309A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU DAMAGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27302UE 41013 DURING INSPECTION/MAINTENANCE MAINTENANCE PERSONNEL FOUD FWD EMERGENCY STRIP LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED WIRES ON EMERGENCY FLOOR TRACK LIGHTS BY PAX DOOR. REMOVED AND REPLACED FUSE IN NR 1 EMERGENCY POWER SUPPLY. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA41NM 20030314002352003031400235SO 2003 3 14 C2XA03SH38 120030307A530014525176007 CLIP EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 20R AND 19R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030314002392003031400239EA 2003 3 14 03069625 120030307A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING MAINTENANCE/INSPECTION, MAINTENANCE PERSONNEL FOUND LT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND RELAMPED LT AFT EXT EMERGENCY LIGHT. OPS CK'D GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030314002402003031400240WP 2003 3 14 IXXA0300020O 120030306A3200 PROXIMITY SWITCH DOUG DC8 DC873F 302199FWP DIRTY A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11606AL893541900 46044 !AFTER DEPARTURE FROM ATL ENROUTE TO MCO. DURING GEAR RETRACTION CREW NOTED MLG "GEAR DOOR NOT LATCHED" LIGHT ILLUMINATED.CREW CYCLED GEAR AND LIGHT FAILED TO EXTINGUSH. **INSPECTION IS ONGOING AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE FOUND RIGHT HAND MAIN LANDING GEAR DOOR SWITCH CANNON PLUG DIRTY. CANNON PLUG WAS REMOVED, CLEANED AND REINSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD. 2L74 4F RT4A25 20030314002412003031400241EU 2003 3 14 WRNA200300008 120030312A3397 WIRE AIRBUS300 A300B4203 3930306EU A WRNAK NONE O OTHER TXTAXI/GRND HDL 1 SO05820SC 154 Taxi and take off R/H supply C/B opens when lights in useCorrective Action: Found Chafed wire, repaired I/A/W standard practices ATA 20, Functional ck good I/A/W ATA 33-46-12. 2L72 4F RTA35EU 20030331001142003033100114EU 2003 3 31 DHL2003367500 120030315A7830 ANGLE AIRBUS300 A300B4203 3930306EU THRUST REVERSER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 THRUST REVERSER FORWARD SKIN ATTACH ANGLE IS CRACKED ON NR 2 I/B T/R. REMOVED FORWARD SKIN,FABRICATED AN INSTALLED REPAIR IAW TIMCO REO-GO9088. ALODINED AN PRIMED IAW A300 SRM 51-40-10. REINSTALLED FWD. SKIN IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20030316000032003031600003SO 2003 3 16 C2XA03SH058 120030316A530014532606015 TRACK EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 SHV DURING C CHECK LEFT UPPER SEAT TRACK NUMBER 3 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED TRACK IAW EMB 135 AMM 53-01-00. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030316000062003031600006EU 2003 3 16 RAIA00303063 120030305A261351228801 OVERHEAT LOOP JETAIRJETSTMJETSTM4101 1500501EU SHORTED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03555HK16087 41072 5634-STL- RIGHT HAND OVERHEAT WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED RIGHT HAND ENGINE OVERHEAT LOOP, OPS CK OK. 2L72 4T RTA41NM 20030317000032003031700003SO 2003 3 17 2003F00147 120030206A56201159CE5000163 WINDOW GULSTMGV GULFSTREAMGV3980116SO CABIN CRACKED A UG8AK NONE O OTHER ININSP/MAINT 1 GL235101 550 NR 4 CABIN WINDOW RIGHT SIDE, HAS CRACKING AT 6:00 POSITION OF OUTER PANEL. KNOWN OCCURRING CONDTION OF G-V CABIN WINDOW OUTER PANE. REPLACED NR 4 CABIN WINDOW RIGHT SIDE. (M) 2L72 4F RTA12EA 20030317000132003031700013NM 2003 3 17 03FDEA00143 120030220A5330 SKIN BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON SKIN AT BS 702, RBL 20, WL 150, BETWEEN STR 26R AND 27R. 2L73 4F4 F A3WE E2EA 20030317000142003031700014NM 2003 3 17 03FDEA00144 120030220A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLANGES OF LONGITUDINAL FLOORBEAM BS 760-848, LBL 25, WL 208. REMOVED DAMAGE LONGITUDINAL BEAM, BS 760-848, LBL 25, WL 208, FABRICATED, ALODINED, PRIMED, AND INSTALLED REPLACEMENT LONGITUDINAL BEAM IAW SRM 51-30-2, 51- 30-5, 53-10-2, 51-10-2, 51-30-2. 2L73 4F RTA3WE 20030317000162003031700016NM 2003 3 17 03FDEA00146 120030220A5754 STRINGER BOEING727 727233 138408ANM NR 1 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 LEFT WING NR 1 SLAT LOWER STRINGER CRACKED. 2L73 4F RTA3WE 20030317000172003031700017NM 2003 3 17 03FDEA00148 120030221A278040174 ACTUATOR BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE LE FLAPS INOPERATIVE A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25215FE 22936 A/C AIR TURNBACK DUE TO NR 6 LEADING EDGE FLAP LIGHT INDICATION, WOULD NOT GO GREEN. ON FRONT PANEL AND S/O STATION. RED TAB PROCEDURES TO NO AVAIL. REMOVED AND REPLACED NR 6 LEADING EDGE FLAP POSITION INDICATING SWITCH IAW M/M 27-82-001-4, OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20030317000182003031700018NM 2003 3 17 03FDEA00150 120030221A5711ARB74131 SPAR CAP DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING FWD OF NR 4 SPOILER AREA REAR UPPER SPAR CAP FOUND RIVET PULLED. SNRM NR 112 : WINGS - OUTER WING / REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIR CARRIED OUT AS PER EA 1-5720-67571, PART 1. 2L73 4F RTA22WE 20030317000192003031700019NM 2003 3 17 03FDEA00151 120030220A2780 ACTUATOR BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE ZONE 600 MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25207FE 22929 AMBER LEADING EDGE FLAPS LIGHT REMAINED ILLUMINATED ON CLIMBOUT AFTER SELECTED FLAPS 2. SECOND OFFICER AUX PANEL SHOWED SLAT 7 AMBER LIGHT ILLUMINATED. QRH PROCEDURES CONDUCTED UNSUCCESSFULLY. FLAPS EXTENDED NORMALLY IN ALL OTHER POSITIONS. REMOVED AND REPLACED NR 7 SLAT ACTUATOR. IAW M/M 27-81-032-4. OPS. AND LEAK CHECKS NORMAL. 2L73 4F4 FRTA3WE E2EA 20030317000252003031700025NM 2003 3 17 03FDEA00158 120030221A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON 950F FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACE FROM LBL 55 TO RBL 55, WL 208. 2L73 4F4 F A3WE E2EA 20030317000332003031700033NM 2003 3 17 03FDEA00167 120030224A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLOORBEAM, UPPER FLANGE AT BS 680 RBL 11, DAMAGED ON REPAIR DOUBLER, NO DAMAGE LIMITS ON REPAIR DOUBLER, REPAIRED FLOORBEAM AT BS 680, WL 208, RBL 11, IAW SRM 53-10-8 FIG 3. 2L73 4F4 F A3WE E2EA 20030317000362003031700036NM 2003 3 17 03FDEA00171 120030224A5710 SUPPORT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING L/E SLAT TRACK, NR 16 RIB SUPPORT, INBOARD SIDE, FOUND WITH CRACK APPROXIMATELY 1 INCH IN LENGTH. 2L73 4F4 FRTA22WE E13NE 20030317000392003031700039NM 2003 3 17 03FDEA00174 120030225A5320 WEB BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE RT WHEEL WELL GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 RT WHEEL WELL HAS GOUGE IN WEB. DAMAGE ON RT WHEEL WELL WEB COMMON TO K-BEAM AREA, BS 872, RBL 5.5, WL 150, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER FROM 7075-T6 .040 INCH, LOT NR 472905. ALODINED, PRIMED, PAINTED, AND INSTALLED IAW 53-10-1, 51-10-1, 51-40-2. 2L73 4F4 F A3WE E2EA 20030317000452003031700045NM 2003 3 17 03FDEA00181 120030226A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLOORBEAM LOWER FRAME AROUND NUT PLATE HOLES, B.S.720, LBL 16 TO LBL 21, W.L. 200 AT PREVIOUS REPAIR. 2L73 4F4 F A3WE E2EA 20030317000462003031700046NM 2003 3 17 03FDEA00182 120030226A5312 PRESSURE PANEL BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE NLG WW GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 GOUGED AREA AT NLW UPPER WEB AT LT PRESSURE PANEL CUT OUT INBOARD SIDE, B.S 242. REMOVED DAMAGE AND REPAIRED IAW SRM 51-40-2. GOUGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. 2L73 4F4 F A3WE E2EA 20030317000472003031700047NM 2003 3 17 03FDEA00183 120030226A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLOORBEAM REPAIR STRAP BS 1130, RBL 30-RBL 36, WL 200. REMOVED CORROSION ON FLOORBEAM REPAIR STRAP BS 1130, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-10-2, 51-10-3, 51-30-2, AND 51-30-5. 2L73 4F4 F A3WE E2EA 20030317000652003031700065SO 2003 3 17 C2XA03BT038 120030314A3246 BEARING EMB 135 EMB135ER 3260203SO SEIZED A C2XAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW2716502 502 EWR ACFT PULLS RIGHT ON T/O. ABORTED T/O AND TAXI BACK TO GATE. ACFT CONTINUED TO PULL RIGHT DURING TAXI. REMOVED AND REPLACED NOSE TIRE/WHEEL ASSYS. FOUND SEIZED BEARING. ALL IAW EMB MM 32-49-05. OPS CHECK GOOD. 2L72 4F RTT00011AT 20030317000682003031700068NM 2003 3 17 03FDEA00202 120030304A2612656020916 FIRE DETECTOR BOEING727 727200 138407ENM NR 2 ENGINE MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25210FE 22932 RETARDED THROTTLES AT 13000 FT AND EXPERIENCED FIRE WARNING BELL, AND LIGHT ON NR 2 TEE HANDLE. NO OTHER ASSOCIATED INDICATIONS. LIGHT WENT OUT SHORTLY AFTER. RETURNED TO GTF AND LIGHT AND HORN CAME ON TWICE MORE DURING RETURN. R/R BOTH SENSING ELEMENTS ON NR 2 ENGINE PER FEDEX 727-200 M/M 26-11-012-4. ALSO R/R'D ENGINE FIRE DETECTION UNIT PER FEDEX 727-200 M/M 26-11-000-4. RAN #2 ENGINE PER FEDEX B727 CHAP.5. SYSTEM OPS CHECKS GOOD ON GROUND. 2L73 4F RTA3WE 20030317000732003031700073NM 2003 3 17 03FDEA00233 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE, NR 29L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000752003031700075NM 2003 3 17 03FDEA00235 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 31L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000762003031700076NM 2003 3 17 03FDEA00236 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 32L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000382003031700038NM 2003 3 17 03FDEA00173 120030225A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION WHILE WORKING CARD N00544 FOUND CORROSION ON FRAME BS 720C, STR-26R. REPAIRED FRAME IAW EA 7-5310-69431. 2L73 4F RTA3WE 20030317000512003031700051NM 2003 3 17 03FDEA00187 120030228A5210 STRUCTURE BOEING727 727200 138407ENM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 COMPLY WITH EO 7-5210-7-2302 EOCN L1, PART 2 DUE TO CRACKS FOUND DURING INSPECTION PER PART 1ON FWD ENTRY DOOR. ALL WORK ACCOMPLISHED IAW FED EX E.O. 7-5210-7-2302 EOCN L1 PART 2 2L73 4F RTA3WE 20030317000522003031700052NM 2003 3 17 03FDEA00188 120030228A5310 FRAME BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON REINFORCEMENT FRAME, BS 1176.9, RBL 45 TO RBL 59, WL 208. REMOVED CORROSION ON REINFORCEMENT FRAME, BS 1176.9 RBL 45-59 WL 208. DETERMINED TO BE OUT OF LIMITS IAW 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20030317000552003031700055NM 2003 3 17 SWAA030573 120030313A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030317000602003031700060NM 2003 3 17 03FDEA00195 120030303A5310 SHEAR TIE BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON SHEAR TIE, BS 720 NEXT TO STR 26R. REMOVED CORROSION ON SHEAR TIE, BS 720 BETWEEN STR 26-27 RIGHT, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED, ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR, ALL WORK ACCOMPLISHED IAW SRM 51-10-3, 51-30-2, 51-30-5, 53-10-4 FIG 11. 2L73 4F4 F A3WE E2EA 20030317000622003031700062NM 2003 3 17 03FDEA00198 120030303A5320 FLOOR SUPPORT BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLOOR SUPPORT UNDER NUT PLATE BS 1165 - 1166, RBL 16, WL 155. REMOVED FLOOR SUPPORT BS 1166-1120, RBL 16, WL 155. FABRICATED REPAIR PARTS IAW SRM 53-10-5 AND SR 27-53-039. ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20030317000632003031700063NM 2003 3 17 03FDEA00200 120030225A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING OUTBOARD HINGE, FLAP SIDE PIVOT HOLE CORRODED AFTER REMOVAL OF BUSHINGS. 2L73 4F4 FRTA22WE E13NE 20030317000672003031700067NM 2003 3 17 PCAA0303055 120030315A335082410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003NM DEFECTIVE A PCAAK NONE O OTHER NRNOT REPORTED 1 EA13845EX 344 ORF-FLIGHT#3555. CREW REPORTED EMERGENCY LIGHTS WILL NOT CYCLE OFF. LIGHTS WORK PROPERLY WITH POWER INTERRPTION. MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL BOX. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030317000692003031700069NM 2003 3 17 03FDEA00204 120030304A3233 ARM BOEING727 727200 138407ENM NLG ACTUATOR BENT A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25234FE 21328 RED "NOSE GEAR" UNSAFE LIGHT REMAINED DIMLY ILLUMINATED AFTER GEAR RETRACTION. COMPLIED WITH RED TAB PROCEDURES AND UPON RECYCLING GEAR, NOSE GEAR LIGHT AGAIN WENT FROM BRIGHT TO DIM AT THE SAME TIME. THE AMBER "NOSE GEAR DOOR" ANNUNICATOR LIGHT EXTINGUISHED ON S/O PANEL. FIVE MINUTES AFTER RECYCLING GEAR, RED LIGHT WENT FROM DIM TO OUT. FOUND THE THE NR 1 THROTTLE CLUTCH PACK HAS A SWITCH ACTUATOR ARM BENT. REMOVED AND REPLACED ACTUATOR ASSY FOR #1 ENG THROTTLE GEAR WARNING IN REF TO 727 MM 31- 26-011 AND OPS CKED IN REF TO 727 MM 31-26-000-5 NO PROBLEMS NOTED. 2L73 4F RTA3WE 20030317000702003031700070EU 2003 3 17 03FDEA00230 120030305A5330 SKIN AIRBUS310 A310203 3930313EU GE CF6 CF680 30025NE ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 RT FUSELAGE, AFT, BETWEEN VERTICAL ATTACHMENT BOLTS CENTER AND AFT OB SIDE HAS CORROSION ON SKIN 1 INCH X 4 INCHES. REMOVED FASTENERS FROM AFFECTED AREA. REMOVED CORROSION IAW A310 SRM 51-22-00 C/W UT THICKNESS INSPECTION IAW NTM 51-10-01/401. FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-19-12. EC INSPECTION REVEALED NO CRACKS. FLAP PEENED THE REWORKED AREA IAW SRM 51-29-00. INSTALLED NEW FASTENERS IAW A310 SRM 51-40-00. RE-PROTECTED AREA IAW A310 SRM 51-23-00. ALL WORK COMPLETED IAW EA 6-5319-68248 DATED 02-13-03 2L72 4F4 FRTA35EU E13NE 20030317000722003031700072NM 2003 3 17 03FDEA00232 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 28L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000792003031700079NM 2003 3 17 03FDEA00240 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 12L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000852003031700085NM 2003 3 17 03FDEA00246 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 4R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000872003031700087NM 2003 3 17 03FDEA00248 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 7R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000882003031700088NM 2003 3 17 03FDEA00249 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 8R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030416002322003041600232WP 2003 4 16 0300749946 120030407A2910 LINE DOUG DC9 DC931 3022065WP HYD SYSTEM LEAKING A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL018926E 45863 ON CLIMB SHORTLY AFTER GEAR RETRACTION THE RIGHT HYDRAULIC PRESSURE BEGAN FLUCTUATING BY FLUID LOSS. THE THE LEFT HYDRAULIC SYSTEM LOST PRESSURE AND LOST FLUID. THE LANDING GEAR WAS LOWERED BY ALTERNATE METHOD. FLIGHT DIVERTED TO IND AND LANDED SAFELY. MAINTENANCE FOUND 3 HYDRAULIC LINES BROKEN/LEAKING AND REPLACED THEM WITH TEMPORARY LINES. ALSO REPLACED BOTH LEFT AND RIGHT ENGINE DRIVED HYDRAULIC PUMPS, ELECTRICAL AUX HYDRAULIC PUMP AND ALL HYDRAULIC SYSTEM FILTERS. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20030416002612003041600261NM 2003 4 16 QXEA0300438 120030405A5420 CHANNEL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 NR 2 NACELLE LOWER DOOR ASSEMBLY DEBRIS DOOR SURROUND STRUCTURE AFT VERTICAL CHANNELS CRACKED AT LOWER ENDS. REPAIRED IAW RD8/4-71-016. 2H72 4T RTA13NM 20030416002752003041600275NM 2003 4 16 QXEA0300444 120030406A3250471525 HARNESS BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09407QX 4049 PDX-NOSE WHEEL STEERING WARNING LIGHT CAME ON 3 TIMES DURING TAXI. STEERING DID NOT WORK. CYCLED STEERING SWITCH PER CHECKLIST. INSPECTED NOSE LANDING GEAR STEERING HARNESS. FOUND THAT WHEN HARNESS SUBJECTED TO VIBRATION, CAUTION LIGHT ILLUMINATED. REPLACED NOSE LANDING GEAR STEERING HARNESS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030416003842003041600384 2003 4 16 YENA200301 420030109A2330 CAPACITOR AIRBUS320 A320232 3930326EU ELECTRICAL BOX FAILED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA15505JB 1173 ELECTRICAL ODOR MID CABIN ON FINAL APPROACH. AREA INSPECTED WITH NO NOTICEABLE DEFECTS. LIVE TV CIRCUIT BREAKER PULLED AND COLLARED AS PERCAUTIONARY. ISSUED MEL 25-22-03 CAT D, ENTIRE LIVETV. PRELIMINARY FINDING: SEAT ELECTRONICS BOX, INTERNAL POWER SUPPLY CAPACITOR C12 APPEARS TO HAVE FAILED. 2L72 4F RTA28NM 20030417000202003041700020EA 2003 4 17 SWIA200311727 120030117A2761270007 PCU CNDAIRCL600 CL6002B19 1900309EA LEFT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07439SW3262 3262 7578 WITH ALL EMHP'S ON, L SPOILERON MESSAGE APPEARS. LEFT SPOILERON IS AMBER ON THE FLIGHT CONTROLS PAGE. INSTALLED SERVICEABLE PCU ON LEFT INBOARD POSITION ON LEFT SPOILERON IAW 27-60-00. OPS CHECKS AND LEAK CHECKS GOOD. 2L72 4F RTA21EA 20030417000652003041700065NM 2003 4 17 UPS03240102 120030121A5754 SEAL BOEING727 72722C 138400FNM NR 6 & SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, NR 6 & 8 LEADING EDGE SLAT CRACK FOUND AT I/B END UNDER PORK CHOP SEAL. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 5. 2L73 4F A3WE 20030417000892003041700089EU 2003 4 17 MALA030118 120030122A3260 UPLOCK SWITCH SAAB SF340 340B 7860101EU MLG LACK OF LUBE A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15364PX 340B262 DURING FLIGHT NR 3113, LANDING GEAR FAILED TO RETRACT. AIR RETURN TO YOW. A/C FERRIED TO DTW. MAINTENANCE JACKED A/C AND PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETRACTION OF LANDING GEAR IAW CHAP 32-30. COULD NOT DUPLICATE DISCREPANCY. INSPECTED GEAR FOUND NO MECHANICAL DEFECTS. CLEANED AND LUBRICATED LT AND RT MLG UPLOCK SWITCHES. ALL CHECKS GOOD IAW CHAP 32. 2L72 4T RTA52EU 20030417001052003041700105EA 2003 4 17 QXEA0300238 120030127A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX- AFT PRESSURE BULKHEAD FEED THROUGH ORIFICE FOR NR 2 HYDRAULIC EDP PRESSURE LINE IS ELONGATED. REPAIRED IAW REO 670-53-61-034 AND 670-53-51-034. 2L72 4F RTA21EA 20030417001822003041700182SO 2003 4 17 SWIA200311773 120030210A5753 BRACKET EMB 120 EMB120ER 3260203SO TE FLAP ROLLER CRACKED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07197SW 120186 INBOARD FLAP FOLLOWER ROLLER BRACKETS CRACKED ON LEFT SIDE. REMOVED AND REPLACED INBOARD FLAP FOLLOWER ROLLER BRACKETS AT BOTH ENDS IAW SRM 51-10-03 AND 51-40-02. PN: 120-22884-001. 2L72 4T RTA31SO 20030417002082003041700208NE 2003 4 17 QXEA0300251 220030212A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX2082 10042 GEE965304 PDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING AND FOUR BLADES HAVE TRAILING EDGE DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030418000032003041800003NM 2003 4 18 P5CA0300767 120030214A5230 BOLT BOEING747 74746NF 13848BTNM ACTUATOR STRIPPED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23453PA 30811 LOWER FWD CARGO DOOR ACTUATOR HAD TWO SUPPORT CARGO DOOR ACTUATORS WITH INSUFFICIENT BOLT THREAD SHOWING AND THE OTHER TWO BOLTS HAD EXCESSIVE THREAD ENGAGEMENT AND BOTTOMED OUT, INDICATING THE ENTIRE ACTUATOR LOAD WAS CARRIED OUT BY ONLY TWO BOLTS. REPOSITIONED AND RE-TORQUE BOLTS IAW AMM 52-34-02. 2L74 4F RTA20WE 20030418000102003041800010NM 2003 4 18 UPS03440179 120030130A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C M/D, R4 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED BELOW STR 24. M/D - R4 DOOR FUSELAGE CUTOUT REVEAL PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 1664 BELOW STR 24. 2L74 4F RTA20WE 20030418000272003041800027NM 2003 4 18 VNAA0302006 120030210A2611 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FIRE FALSE INDICATIONA VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07472PS 3008 THE CREW RECEIVED A LAV FIRE INDICATION, THERE WAS NO LAV FIRE. MAINTENANCE CONTROL DEFERRED THE LAV FIRE EXTINGUISH SYSTEM IN ACCORDANCE WITH MEL 26-4 C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030418000322003041800032NE 2003 4 18 VNAA0302001 220030203A7532311995704 BLEED VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT IBV FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07471PS7665 2434 3007 DURING TAKEOFF, THE RIGHT HAND ENGINE WAS SLOW TO MAKE TORQUE AND THE CREW ABORTED TAKEOFF. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE INTERCOMP BLEED VALVE IN ACCORDANCE DORNIER MAINTENANCE MANUAL 75-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030418000562003041800056NM 2003 4 18 QXEA0300263 120030206A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - X739 Y9.5R SEAT TRACK HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 6-53-193. 2H72 4T RTA13NM 20030418000592003041800059NM 2003 4 18 QXEA0300266 120030206A5320 FLOOR SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - PITTING ON TOP OF FLOOR PANEL SUPPORT TAB AT X39.0 AFT SIDE OF STEP RISER INTO COCKPIT. REPAIRED IAW DHC-8 Q400 SRM 51-21-10, PAGE 201-205 AND HORIZON AIR EA 6-53-195. 2H72 4T RTA13NM 20030418000602003041800060NM 2003 4 18 QXEA0300267 120030207A5315 FLOORBEAM BOMBDRDHC8 DHC8401 1390041NM ZONE 267 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - AFT BAG PIT X783 Y25L ANGLE HAS CHAFE DAMAGE FROM A FLOORBOARD. REPAIRED IAW RD 8/4-53-417, STEPS 4/6 AND DHC-8 Q400 SRM 51-14-00-350-804. 2H72 4T RTA13NM 20030418000672003041800067NM 2003 4 18 QXEA0300277 120030206A5320 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - FORWARD SUPPORT ANGLE UNDER PANEL 262HT HAS CHAFE DAMAGE ON TOP SURFACE. REPAIRED IAW HORIZON AIR EA 6-57-118. 2H72 4T RTA13NM 20030418000722003041800072NM 2003 4 18 QXEA0300282 120030210A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - CHAFING DAMAGE ON PANEL 262FT. REPAIRED IAW HORIZON AIR EA 6-53-196. 2H72 4T RTA13NM 20030418000922003041800092NM 2003 4 18 QXEA0300292 120030217A5270 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DIRTY A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09411QX 4055 SEA- ON FLIGHT NUMBER 2389, REAR BAGGAGE DOOR WARNING LIGHT CAME ON DURING CLIMBOUT. CLEANED AND LUBED. PERFORMED OPERATIONAL CHECK AFT BAGGAGE DOOR LATCH SEVERAL TIMES. NO DEFECTS NOTED. FOUND LATCH OPENED ON SHUTDOWN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030418001092003041800109NM 2003 4 18 F3LA200300070 120030218A5320 CLIP BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED TIE CLIP AND ATTACHING HARDWARE CORRODED AT AFT END OF RT MOP SILL BEHIND R-2 DOOR. REPLACED CLIP HARDWARE PER SRM 51-30-2. NO CORROSION WAS FOUND ON CLIP. CLEANED AREA PER SOPM 20-41-02. 2L72 4U RTA16WE 20030418001122003041800112WP 2003 4 18 UPS03840211 120030206A531336469371 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C3 AFT PIT LONG 34R STA 1420-1440 CORRODED. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20030418001172003041800117NM 2003 4 18 QXEA0300295 120030222A26114462531 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09345PH 476 PDX-ON FLIGHT NUMBER 2009, LAVATORY SMOKE DETECTOR WARNING OCCURRED DURING TAXI-OUT. NO VISIBLE SIGN OF SMOKE OR FUMES. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030418001222003041800122SO 2003 4 18 SWIA200311778 120030209A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07284YV6189 6189 120284 EMERGENCY LIGHTS DO NOT ILLUMINATE ON FLOOR STRIP ROWS 2 TO 6, KNEE LEVEL EXIT SIGNS AT ROW 6 AND OVERHEAD ROW 6. REMOVED AND REPLACED CENTER EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20030418001352003041800135NE 2003 4 18 SWIA200311791 220030217A7200 ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RIGHT OVERSPEED A SWIAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 NM07301YV 120301 AFTER LANDING ROLLOUT AND DURING DECELERATION, HEARD A TRIPLE CHIME WARNING AND THE AURAL WARNING ENGINE CONTROL WHICH STARTED AT ABOUT 90 KTS. AT ABOUT 70 KTS, THE RIGHT ENGINE SURGED SEVERAL TIMES RESULTING IN MODERATE INCREASING YAWING TENDENCIES. POSITIVE AIRCRAFT CONTROL WAS UNCERTAIN AND RIGHT ENGINE WAS SHUT DOWN. FDR DOWNLOAD INDICATES THE RIGHT ENGINE NP REACHED 130 PERCENT NP. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW EMB120 MM 71-00-00. 2L72 4T4 TRTA31SO E20NE 20030416003652003041600365NM 2003 4 16 UPS03240056 120030107A5340 FITTING BOEING727 72721C 138400MNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE: C, CRACK INDICATION IN ONE HOLE BS 870 LT HOLE LOCATED 2ND FASTENER ROW FROM FWD EDGE OF FITTING TOP FASTENER HOLE OF LWR FITTING. REPAIRED IAW UPS EO B727-5310-3057-H. 2L73 4F A3WE 20030416003742003041600374NM 2003 4 16 QXEA0300262 120030107A5410 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - LT ENGINE LOWER NACELLE 412AB BYPASS DOOR APERTURE RIGHT HAND CHANNEL CRACKED AT AFT END RIVET HOLE. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030416003882003041600388SO 2003 4 16 SWIA200311752 120030110A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07294SW 120321 RIGHT SIDEWALL SEAT TRACK NEEDS REPLACED, CORROSION UNDER SCREW HEADS, FORWARD TRACK. FOUND DURING C-CHECK INSPECTION. REPLACED RIGHT SIDEWALL SEAT TRACK IAW EMB120 MM 53-01-04. 2L72 4T RTA31SO 20030416004012003041600401NM 2003 4 16 UPS03240093 120030113A5315 FLOORBEAM BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, SURFACE CORROSION ON FLOORBEAM TOP CAP BS 312 LBL 10 & LBL 24.75. CARRIED OUT REPAIR AT ABOVE LOCATION IAW SRM 53-10-8. 2L73 4F A3WE 20030416004062003041600406 2003 4 16 DL777030063 420030114A2330CBMA21W1S CONNECTOR BOEING777 777232 1385232NM COMMS BURNED A DALAK NONE O OTHER ININSP/MAINT 1 SO27861DA 29952 FOUND BURNED CONNECTOR J2 INPUT TO VDU 7, NEEDS CONNECTOR PART NUMBER DM3134B. REPLACED VDU 7. PULLED C/B AND COLLARED C/B VD3 C-21 ON P110, J2 IS PULLED FROM VDU 7 AND J3 IS PULLED FROM VDU6. 2L72 4F RTT00001SE 20030317000892003031700089NM 2003 3 17 03FDEA00250 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 9R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030121002622003012100262NE 2003 1 21 C8GA2003002R 220030116A7200JT8D15A ENGINE BOEING727 727223 1384074NM PWA JT8 JT8D15A 52051NE BIRD INGESTION A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO15899AA48102 22015 700758 Flight 737 from GDL to MTY. Bird strike on #2 engine after takeoff. Shutdown #2 engine and air turn back to GDL (Guadalajara, Mexico) aircraft landed without incident. Visual inspection revealed damage to the #2 engine fan blades. A special maintenance ferry flight (two engines) was issued from GDL (Guadalajara, Mexico to JAX Jacksonville, Florida. A revision of SDR # C8GA20030002R will be issue to address final corrective maintenance action taken. JANUARY 19, 2003. THE FINAL CORRECTIVE MAINTENANCE ACTION FOR THE #2 ENGINE BIRD STRIKE WAS THE REPLACEMENT OF THE #2 ENGINE IAW CCIA FORM B727-7101B. LEAK, TRIM, AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20030121002632003012100263EA 2003 1 21 COMA0360035 120030116A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01798CA 7348 FLIGHT 5570 CABIN DOOR WARNING AFTER T/O.COULD NOT DUPLCIATE. FOUND NO DEFECTS WITH DOOR OR WARNING SYSTEM. 2L72 4F RTA21EA 20030121002662003012100266EA 2003 1 21 COMA0360038 120030117A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01798CA 7348 FLIGHT 6280 CABIN DOOR WARNING AFTER T/O.COULD NOT DUPLICATE. FOUND NO DEFECTS WITH DOOR OR WARNING SYSTEM. 2L72 4F RTA21EA 20030121002672003012100267NM 2003 1 21 PCAA0301007 120030104A5210 HINGE DHAV DHC8 DHC8102 2809003NM PAX DOOR LACK OF LUBE A PCAAK NONE O OTHER NRNOT REPORTED 1 EA13844EX 339 LGA-FLIGHT 3873 CREW REPORTED PASSENGER DOOR WILL NOT OPEN. MAINTENANCE LUBRICATED DOOR HINGE. DOOR OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030121002732003012100273GL 2003 1 21 HEEA083367 220030109A731347101 FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE DIRTY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X5154 51552 NOZZLE PACKED WITH CARBON. CLEANED AND INSPECTED UNIT. 1G71 3U3 U H2SW E4CE 20030121002762003012100276GL 2003 1 21 HEEA083368 220030109A741249522 EXCITER BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 EXCITER NOT FIRING. REPAIRED. 1G71 3U3 U H2SW E4CE 20030121002772003012100277GL 2003 1 21 HEEA083369 220030109A741249522 EXCITER BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 EXCITER FAILED, NO IGNITION ON START. REPAIRED. 1G71 3U3 U H2SW E4CE 20030121002822003012100282NM 2003 1 21 CALA0300016 120030119A5230 SKIN BOEING777 777224 1385225NM AFT CARGO DR DEFORMED A CALAK NONE O OTHER ININSP/MAINT 1 SW0978005 27581 INSPECTION FOUND AFT CARGO DOOR AFT LOWER CORNER SKIN DEFORMED WITH A CRACK IN SKIN AT RIVET HOLE. THE DOOR SKIN WAS REPAIRED IAW SRM 52-30-01, REPAIR 17. 2L72 4F RTT00001SE 20030121002842003012100284 2003 1 21 HEEA083371 420030109A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 PRECESSES EXCESSIVELY. REPAIRED. 1G71 3U H2SW 20030121003272003012100327 2003 1 21 HEEA083378 420030109A3421504001790116 INDICATOR BELL 206 206L3 1182108SW HORIZON GYRO FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 HORIZON GYRO WILL NOT CAGE. REPAIRED. 1G71 3U H2SW 20030121003312003012100331SW 2003 1 21 HEEA083382 120030109A3213601025015 CLAMP BELL 206 206L3 1182108SW CROSSTUBE BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671 51301 LT OUTBOARD CLAMP ON FWD CROSSTUBE HAS BROKEN T-BOLT. SCRAPPED. 1G71 3U H2SW 20030121003322003012100332SW 2003 1 21 HEEA083383 120030109A3210601029103 SUPPORT BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 SUPPORT CORRODED. SCRAPPED. 1G71 3U H2SW 20030121003332003012100333GL 2003 1 21 HEEA083384 220030109A72506871937 TUBE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENG TO G/BOX CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 REPLACED TUBE ASSY FROM TURBINE PRESSURE CHECK VALVE TO GEARBOX DUE TO B-NUT THREADS FILLED WITH ALUMINUM FROM CHECK VALVE FITTINGS. SCRAPPED. 1G71 3U3 U H2SW E4CE 20030121003382003012100338EA 2003 1 21 COMA0360040 120030120A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO01781CA9637 7312 FLIGHT 5203 R/H EMERGENCY WING LIGHT IS INOP.REPLACED THE #2 EMERGENCY BATTERY. 2L72 4F RTA21EA 20030317000802003031700080NM 2003 3 17 03FDEA00241 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 14L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000832003031700083NM 2003 3 17 03FDEA00244 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 2R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317000922003031700092NM 2003 3 17 03FDEA00253 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 12R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317001062003031700106NM 2003 3 17 03FDEA00266 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 26R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001072003031700107EU 2003 3 17 DHL2003367504 120030223A5210A5211100800201 PLATE AIRBUS300 A300B4203 3930306EU CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R:L1 door upper edge teflon rub strip missing an deterioated. Corrective action:Removed teflon tape IAW A300 SRM 51-30-00. After further evaluation found corrosion on upper plate,out of limits IAW A300 SRM52-10-00,drilled new upper plate IAW A300 SRM 51-30-00 and installed IAW SRM 51-30-00 new teflon tape attached to plate assy. 2L72 4F RTA35EU 20030317001082003031700108NM 2003 3 17 03FDEA00267 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 27R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001142003031700114NM 2003 3 17 03FDEA00273 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 33R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001152003031700115NM 2003 3 17 03FDEA00274 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 34R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001172003031700117NM 2003 3 17 03FDEA00276 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 36R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001272003031700127NM 2003 3 17 03FDEA00287 120030307A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON 950 FLOORBEAM UPPER AND LOWER SURFACE OF UPPER FLANGE AT NUT PLATE HOLE LBL 23 WL 208. REMOVED CORROSION ON BS 950 FLOORBEAM AT LBL 23 WL 208 OUT OF LIMITS IAW SRM 53- 10-1 FIG 5 REMOVED DAMAGED PORTION OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS IAW FED EX EA 7-5310-69433. 2L73 4F RTA3WE 20030317001322003031700132NM 2003 3 17 03FDEA00295 120030311A5310 STRUCTURE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 WHILE WORKING MAIN CARGO CLOSE CARD, FOUND CORROSION EMANATING FROM UNDERNEATH PLASTIC STRIP BS 825, RBL 15, WL 196 2L73 4F RTA3WE 20030317001332003031700133NM 2003 3 17 03FDEA00297 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 500 STR 25L. 2L73 4F RTA3WE 20030317001342003031700134NM 2003 3 17 03FDEA00298 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 500, BETWEEN STR 23R AND 24R. 2L73 4F RTA3WE 20030317001382003031700138NM 2003 3 17 03FDEA00302 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 560, BETWEEN STR 24L AND 25L. 2L73 4F RTA3WE 20030317001412003031700141WP 2003 3 17 03FDEA00305 120030304A5710ARB22161 CAP DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 DURING "C" CHECK, LT WING UPPER CAP AT RIB STATION XORS 402 CRACKED. THE CRACK WAS ALL THE WAY THRU THE CAP AND WAS LOCATED IMMEDIATELY FWD OF STRINGER 15. 2L73 4F A22WE 20030317001422003031700142WP 2003 3 17 03FDEA00306 120030304A5512ALC74392 SKIN DOUG DC10 DC1010 3022110WP HORIZONTAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 DURING "C" CHECK, ON RT HORZ STAB UPPER REAR SKIN PANEL FOUND CRACK ONE INCH LONG. REPAIRED PER IAW DOUGLAS SB 55-18 R1 FIG 2 (REF FEDEX NRC N 381). 2L73 4F A22WE 20030317001452003031700145EU 2003 3 17 DHL2003367506 120030227A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R 0029516:Main cabin floor seat track scallops has gouges at L/side between Sta. 3742 and STA. 3745 Fr. 58. Corrective action:Blended out gouges IAW A300 SRM 53-10-00,alodined IAW A300 SRM 51-40-12,primed IAW A300 SRM 51-40-12,painted IAW A300 SRM 51-40-12. Blended area found within limits IAW A300 SRM 53-10-00,orig. mat. thickness 0.138,mat. removed 0.001 2L72 4F RTA35EU 20030317001522003031700152NM 2003 3 17 03FDEA00316 120030314A26122591153501 BRACKET BOEING727 727200 138407ENM NR 1 ENG NACELLEBROKEN A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING LDLANDING 1 SO25208FE 22930 NR 1 FIRE WARNING LITE AND BELL COMES ON INTERMITTANTLY ABOUT 30 SEC INTERVALS, OCCURRED ON FINAL WITH THRUST LEVER AT IDLE. ENGINE SHUT DOWN ON LANDING. OPENED ENGINE NACELLE TO FACILITATE MAINTENANCE. DISCOVERED ENGINE FIRE DETECTION LOOP BRACKET ASSY TO BE BROKEN NEXT TO THE STARTER AT THE AFT INBOARD SIDE. REMOVED AND REPLACED NR 1 ENGINE SENSING ELEMENT PER MM 26-11-012-4 OK FOR SERVICE. 2L73 4F RTA3WE 20030317001562003031700156NM 2003 3 17 UPS03240290 120030221A5340 SEAT TRACK BOEING727 727108C 1384039NM BS 650-680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI CABIN SEAT TRACK AT STA. 650 TO 680 HAS CORROSION ON O/B FLANGE OF T RACK LBL 45.5. CORROSION REMOVED IAW SRM 53-10-1 OUT OF LIMITS. SEAT TRACK SECTION REMOVED BETWEEN BS 650-740 LBL 45.5 IAW SRM 51-30-2. NEW SECTION OF SEAT TRACK FABRICATED, PROTECTED PRIMED AND FITTED IAW SRM 53-10-5 & 51-30-2 & CPT 2061 2L73 4F A3WE 20030317001582003031700158WP 2003 3 17 03FDEA0163 120030221A3260894601 PROXIMITY SWITCH DOUG DC10 DC1010F 3022111WP GE CF6 CF6* 30020GL MLG INOPERATIVE A FDEAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO25364FE2316 2316 46600 WHEN GEARS WERE LOWERED, ALL 3 GEAR INDICATED UNSAFE ON MAIN GEAR INDICATORS AND CONFIGURATION PAGE. NO ABNORMAL YAW OR NOISE. RECYCLED GEAR AND GOT 3 GOOD DOWN INDICATIONS. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS UNIT IN REF TO MD1 0-10 M/M 31-71-01-2. JACKED AIRCRAFT IAW MD10-10 M/M 07-11-00-2 AND CYCLED GEAR SEVERAL TIMES IAW MD10-10 M/M 32-30-00-5 ALL INDICATIONS NORMAL. 2L73 4F4 F A22WE E23EA 20030317001592003031700159EU 2003 3 17 DHL2003367509 120030226A5230 DOOR FRAME AIRBUS300 A300B4203 3930306EU CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R 0029409:Fwd. cargo door inner frame has corrosion around nutplate at lower end of torque tube area. Outer panal removed for access. Corrective action: Removed corrosion IAW A300 SRM 51-40-11,found to be out of limit. Found to be out of limits IAW A300 SRM 52-30-00. Formed repair angles IAW A300 SRM 51-11-40,located,drilled and trimmed 2 each repair angles IAW A300 SRM 51-40-40 alodined,primed painted an installed angles IAW A300 SRM 51-41-40. 2L72 4F RTA35EU 20030317001622003031700162NM 2003 3 17 159PL0029 120030305A33506013211 BATTERY PACK BOEING737 737242 1384477NM A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05159PL 21186 L2 and R2 emergency exterior light inop. Removed and replaced L2 and R2 emergency light pack M572 per MM 33-52-02. 2L72 4F A16WE 20030317001652003031700165NM 2003 3 17 AWXA200300274 120030226A533065C33756 SKIN BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW0 0 24633 MCN - MAJOR REPAIR - DURING C-14 CHECK 2 EACH CRACKS WERE FOUND COMING FROM FASTENER HOLES AT THE R-1 DOOR CUTOUT, LOWER AFT CORNER BS 323. INTERNAL DOUBLER ALSO FOUND CRACKED AT SAME LOCATIONS. MAINTENANCE REMOVED FASTENERS AND CUTOUT CRACKED SECTION OF SKIN AND INTERNAL DOUBLER; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH REPAIR PLATES AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, PG. 204-208, FIG. 202. 2L72 4F RTA16WE 20030317001682003031700168EU 2003 3 17 DHL2003367510 120030226A5300 DOUBLER AIRBUS300 A300B4203 3930306EU CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R 0029435:AT lower fusl. skin around static drain ports is corroded. Corrective action: Removed existing repair doubler and fab new 2 ea. mat. ID 2024T3 .071 treated and primed and installed it IAW A300 SRM 51-30-30,mat. ID IAW A300 SRM 53-10-10 alodined an primed IAW A300 SRM 51-40-11 and 51-40-12. 2L72 4F RTA35EU 20030317001712003031700171NM 2003 3 17 QXEA0300362 120030314A3260401020101 SENSOR DHAV DHC8 DHC8202 2809007NM ZONE 700 FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09353PH12911 496 BOI - FLIGHT 2204 - ON APPROACH, THE CREW COMPLIED WITH THE EMERGENCY/ABNORMAL CHECKLIST WHEN AFTER LOWERING THE GEAR THEY RECEIVED A NOSE GEAR UNSAFE INDICATION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NOSE LANDING GEAR DRAG STRUT PROXIMITY SENSOR. FUNCTIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030318000052003031800005NM 2003 3 18 SWAA030588 120030314A2560A170033 STRAP BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP PER MM. 2L72 4F RTA16WE 20030318000062003031800006NM 2003 3 18 SWAA030590 120030314A57406545444 RIB BOEING737 7373H4 1384600NM LH WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND LH WING UPPER RIB CHORD CRACKED AT STA 114, STR 2. REPAIRED UPPER RIB CHORD PER BFG ER. 2L72 4F RTA16WE 20030318000142003031800014EU 2003 3 18 BAQA084840 120030227A641011731743 BLADE BOLKMS117 BK117B1 5626012EU TAIL ROTOR ERODED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01213AE1168 7219 TAIL ROTOR BLADE HAS EROSION. 1G72 3U H13EU 20030318000182003031800018EU 2003 3 18 BAQA085091 120030305A28407067863 AMPLIFIER AEROSPAS365 AS365N2 8680815EU NR 1 FUEL INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME6600 6417 NR 1 FUEL AMPLIFIER SYSTEM WILL NOT TEST OR CALIBRATE. DRIVES NEEDLE NEGATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030318000192003031800019 2003 3 18 BAQA085092 420030305A3416375002241 ALTIMETER AEROSPAS365 AS365N2 8680815EU COCKPIT INACCURATE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME950 6417 ALTIMETER INACCURATE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030417000392003041700039EA 2003 4 17 SWIA200311733 120030118A7603 RIVET CNDAIRCL600 CL6002B19 1900309EA THROTTLE ROD CHAFED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 A RIVET ON THE NR 2 ENGINE PUSH-PULL ROD FROM THE THROTTLE GEARBOX TO THE MFC WAS FOUND TO BE RUBBING ON A SCREW ON THE FACE OF THE GEARBOX WHEN THROTTLE MOVED INTO OR OUT OF FUEL SHUTOFF POSITION. RIVET BUCKED TO PROPER DIMENSIONS AND SCREW TIGHTENED. GAP FOUND TO BE AT LEAST .125 INCH AND OPS CHECK GOOD. 2L72 4F RTA21EA 20030417000432003041700043EA 2003 4 17 SWIA200311737 120030119A2913PV304448 PUMP CNDAIRCL600 CL6002B19 1900309EA LT HYD SYSTEM MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07934SW 7722 RECEIVED A HYDRAULIC NR 1 LOW PRESSURE CAUTION MESSAGE CLIMBING THROUGH 14,000 FT. TURNED ON HYDRAULIC 1B AS PER QRH, HYDRAULIC PRESSURE STILL SHOWED ZERO. RETURNED TO PHX. REMOVED AND REPLACED LT ENGINE HYDRAULIC PUMP IAW MM 29-11-01 AND LT HYD PUMP CASE DRAIN LINE. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. NO DEFECTS OR LEAKS NOTED AT THIS TIME. S/N OFF: MX661187. 2L72 4F RTA21EA 20030417000592003041700059NM 2003 4 17 P5CA0300732 120030122A4930 FITTING BOEING747 7472U3B 1384846NM APU FUEL LINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CORROSION LEVEL 1 FOUND ON LINE SHROUD FITTING DURING REMOVAL OF APU FUEL LINE SHROUD FIBERGLASS CLOSE OUT PANEL. NEW SHROUD LINE FITTING INSTALLED & LEAK CHECK CARRIED OUT PER MM 28-25-04. FOUND SATISFACTORY AND NO LEAKS OBSERVED. 2L74 4F RTA20WE 20030417000902003041700090EU 2003 4 17 MALA030138 120030203A5260 ACTUATOR SAAB SF340 340B 7860101EU AIRSTAIR BINDING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15402XJ 340B402 AFTER FLIGHT NR 2906, AIRSTAIRS BINDING ON RT (FORWARD) SIDE DURING EXTENSION AND RETRACTION. MAINTENANCE CLEANED AND LUBRICATED ALL ACTUATORS ON AIR STAIRS, COULD NOT FIND ANY PROBLEMS. OPS CHECK GOOD. 2L72 4T RTA52EU 20030417001292003041700129NM 2003 4 17 UPS03440143 120030208A33503351000002418 LIGHT BOEING747 747123 1384873NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01676UP 20101 FWD MAIN DECK RT STA 340 EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CHECK OK. 2L74 4F A20WE 20030417001652003041700165NE 2003 4 17 QXEA0300245 220030208A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX2406 10033 GEE965288 NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND THREE BROKEN BLADES, ANOTHER WITH MATERIAL MISSING AND SEVERAL OTHERS WITH SMALL NICKS IN TIPS. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER(GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030417001882003041700188EA 2003 4 17 QXEA0300253 120030203A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 PDX- 1.85 INCH CRACK IN AFT PRESSURE BULKHEAD AT NR 2 EDP SUCTION LINE FEED THROUGH. REPAIRED IAW HORIZON AIR EA R-54-64. 2L72 4F RTA21EA 20030417001892003041700189NM 2003 4 17 P5CA300749 120030127A5347 CARGO TRACK BOEING747 747283B 1384867NM FUSELAGE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LOWER LOBE AFT CARGO DISTORTION ON FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1900 - 1920. DAMAGE PORTION FLOOR TRACK REMOVED. NEW PORTION FABRICATED H/F 7178-T65H EXTRU BAC 1580-1688 PER SRM 53-11-25, FIG 7. ANGLE 7075-T6 THS 60-1350 PER SRM 51-40-02. RIVETED PER SRM 51-30-02. 2L74 4F A20WE 20030417002032003041700203WP 2003 4 17 UPS03840169 120030203A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1040-1060 AT L28R SPLICE FITTING IS CRACKED. REMOVED CRACK FITTING. LOCATE NEW FITTING, DRILL EXISTING FASTENER HOLES AND DEBURRED IAW DC8 SRM 51-3-2. REMOVED LOWER FILLET PANEL FOR ACCESS IAW DC8 SRM 51-3-0. INSTALLED NEW FITTING AND LOWER FILLET PANEL IAW DC8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20030418000112003041800011NM 2003 4 18 UPS03440180 120030130A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C M/D, L4 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED AT BS 1664 BELOW STR 24. M/D- L4 DOOR FUSELAGE CUTOUT REVEAL PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 1664 BELOW STR-24. 2L74 4F RTA20WE 20030418000552003041800055WP 2003 4 18 UPS03840194 120030218A2612 BELL ASSY DOUG DC8 DC871F 302199DWP NR 4 FIRE DETCTRWEAK A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE: PFLT, WHEN TESTING FIRE WARNING SYSTEM ON ALL 4 ENG FIRE WARNING BELL IS WEAK, BARELY AUDIBLE. REMOVED AND REPLACED BELL ASSY ENG FIRE WARNING SYSTEM, OPS CHECK PER MMNL 26-10-03. SYSTEM NORMAL. 2L74 4F RT4A25 20030418001152003041800115WP 2003 4 18 UPS03840214 120030211A5330975044829 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, LAP SPLICE BLENDED OUT OF LIMITS L21L/FS 1600. REMOVED DAMAGED SECTION OF CUSP DOUBLER 9750448-29. FAB REPLACEMENT PART, ALODINED, PRIMED & INSTALLED IAW TIMCO REO G09045. FAB FINGER DOUBLER IAW DAC DWG 9750448, ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030418001422003041800142NM 2003 4 18 ZW0A0302704 120030222A335057741 LIGHT BOEING757 7572Q8 1384972NM CABIN DISLODGED A ZW0AO OTHER O OTHER LDLANDING 1 CE13703TW 27620 ON ARRIVAL EMERGENCY STRIP BY MID LAV PULLED UP. REINSTALLED EGRESS LIGHT SYS PN 5774-1 TWA 91-8032. OPS CHECKED NORMAL PER MM33-51-11. CHECK-C MCI 10-12-02. 2L72 4F RTA2NM 20030421000132003042100013WP 2003 4 21 IXXA0300017O 120030221A5270 WARNING LIGHT DOUG DC8 DC873F 302199FWP MLG DOORS ILLUMINATED A IXXAO OTHER N FALSE WARNING CRCRUISE 1 SW11606AL4604428945 46044 AFTER DEPARTURE FROM TOL EN ROUTE TO LAX. DURING UPLATCH CHECK CREW NOTED DOORS NOT LATCHED LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURE AND CYCLED LANDING GEAR. DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED. APPROX 15 MINUTES LATER LIGHT EXTINGUSHED. FLIGHT PROCEEDED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED CHECK OF THIS SYSTEM PER APPLICABLE MANUALS AND WAS UNABLE TO DUPLICATE. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030421000232003042100023 2003 4 21 SWIA200311801 420030216A3414320AS1 INDICATOR EMB 120 EMB120ER 3260203SO AIR SPEED MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07209SW7521 7521 120269 HIGH SPEED AURAL WARNING ON TAKEOFF ROLL AT 70 KNOTS. ABORTED TAKEOFF. REMOVED AND REPLACED CO-PILOTS AIRSPEED INDICATOR. OPS CHECKS GOOD. LEAK CHECK GOOD. 2L72 4T RTA31SO 20030318000222003031800022 2003 3 18 BAQA085107 420030306A342542000332430 INDICATOR UROCOPEC135 EC135T1 5620026EU AHRU INTERMITTENT H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01554ME68 0154 AHRU DOES NOT ALWAYS POWER UP. INTERMITTENT. 1G72 3U H88EU 20030318000262003031800026NE 2003 3 18 ERAA085144 120030213A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE DEBONDED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03575EH 760366 DOUBLER DEBONDING, WORN. SENT TO CTI. INSPECTED PER SA 4047-76-5 REV 11; MODIFIED EXTERNAL DOUBLERS PER RS-017-1; REPLACED ABRASION STRIP PER RS-005N-III; REPAIRED KEVLAR PER PROCEDURE NR 2 AND 18 -1 PLY; REFINISHED PER DRAWING NR 76150-09043; STATIC BALANCE PER RS-005N-VI. 1G72 3U H1NE 20030318000312003031800031EU 2003 3 18 ERAA085151 120030213A2997 WIRE BOLKMS105 BO105C 5626005EU DUAL HYDRAULIC BROKEN H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01 GUIDE ASSY ON DUAL HYD PACK WILL NOT RESET. FOUND BROKEN WIRES. DISASSEMBLED, CLEANED, INSPECTED, ISTALLED NEW SOCKET AND POTTED & INSTALLED NEW FLAT SPRING & TESTED. REPAIRED IAW MBB BO-105 REM 405. 1G72 3U H3EU 20030318000372003031800037EU 2003 3 18 ERAA085164 120030218A65204619002003 GEARBOX BOLKMS105 BO105S 5626006EU TAIL ROTOR MAKING METAL H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01152EH12647 S701 GEARBOX MAKING METAL. GEAR SET SCRAPPED DUE TO MICRO PITTING, OUTPUT BEARINGS SCRAPPED DUE TO MICRO PITTING. REPAIRED IAW REM 304, INSTALLED NEW PINION, BEVEL GEAR, OUTPUT BRGS, ASSEMBLED IAW REM 304, ADJUSTED BACKLASH & DISTANCE AS REQUIRED. COMPLIED WITH ASB BO-105-30-111, SB BO-105-30-109 1G72 3U H3EU 20030318000402003031800040NM 2003 3 18 0300526306 120030314A3397 WIRE BOEING747 747451 1384940NM PATH LIGHTS DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK FOUND UPPER DECK FLOOR PATH EMERGENCY LIGHTS INOP. REPAIRED WIRE AND OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030318000562003031800056EU 2003 3 18 2003F00122 120030224A323010143927M1 SOLENOID VALVE AMD FALC20FALCON 2720302EU MLG STICKS G O OTHER J WARNING INDICATION APAPPROACH 1 EA0150BV 5895 365 ON APPROACH TO SCH WHEN LANDING GEAR EXTENDED THREE GREEN LIGHTS CAME ON WHILE THREE RED LIGHTS STAYED LIT AND GEAR DOORS FAILED TO CLOSE. TROUBLESHOOTING MX DISCOVERED THE LANDING GEAR CONTROL SOLENOID VALVE INTERMITTANTLY STICKING IN THE OPEN POSITION WHEN COLD. THIS PROBLEM WAS DIFFICULT TO DETECT BECAUSE IT ONLY HAPPENED WHEN VALVE BECAME COLD-SOAKED IN FLT. THE NIGHT THE PROBLEM WAS DISCOVERED BY GND MX THE AIR TEMPERATURE WAS -15 F. 2L72 4F A7EU 20030318000622003031800062WP 2003 3 18 AALA20030185 120030209A28223980001 PUMP DOUG DC9 DC982 3022082WP FUEL BOOST FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21456AA 49561 DFW - FLT 1023 - EN ROUTE DFW-BUR - PASSING 7,000 FEET ON CLIMB NOTICED CENTER TANK NOT FEEDING. FOUND FORWARD CENTER FUEL TANK CIRCUIT BREAKER POPPED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CIRCUIT BREAKERS WERE CHECK ON PREFLIGHT AND WERE IN BOTH CAPTAIN AND FIRST OFFICER. CHECKED CENTER PUMPS ON PREFLIGHT AND THE CHECK WAS NORMAL. REPLACED BOTH CENTER AFT AND FORWARD FUEL BOOST PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030318000652003031800065WP 2003 3 18 AALA20031040 120030204A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 TUL - FOUND CRACKED LONGERON 10L AT STATION 1271. INSTALLED DOUBLER SPLICE PER SRM 50-02-00 ON LONGERON 10L. (M) 2L72 4F A6WE 20030318000662003031800066NM 2003 3 18 AMTA200300086 120030114A2120 ODOR BOEING737 73783N 13844HINM CABIN DETECTED A AMTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11330TZ 32616 IN FLIGHT AT FL370 FUMES AND SMOKE IN AFT CABIN. PERFORMED T/S PER FIM 21-00-00-810 (801, 802, 803, 804) FOUND NO EVIDENCE OF HYDRAULIC FLUID, OIL IN PNEUMATIC SYSTEM. NO OVERHEATING OF RECIRCULATION FANS WHILE CHANGING RECIRCULATION FAN FILTERS CHECKED DUCTS FOR EVIDENCE OF FLUID NONE DETECTED. AFTER RUNNING ENGINES FOR 2ND TIME AFTER RECIRCULATION FAN FILTERS WERE CHANGED NO SMOKE OR FUMES DETECTED. OPERATED ALL OVENS, COFFEEMAKERS, CHILLERS AND CHECKED ALL FLORESCENT LIGHTS IN CABIN. FOUND NO EVIDENCE OF SMOKE OR FUMES. PROBLEM COULD NOT BE DUPLICATED ON GROUND OK FOR CONTINUED SERVICE. (M) 2L72 4F RTA16WE 20030318000712003031800071NM 2003 3 18 AMTA200300189 120030108A5412 BULKHEAD BOEING757 75723N 1384973NM NR 1 PYLON GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 NR 1 PYLON STRUT STRUCTURE MID-BULKHEAD FITTING WEB GOUGED. REPAIRED WEB IAW ER/A 757-54R-5041. (M) 2L72 4F RTA2NM 20030318000752003031800075NM 2003 3 18 AMTA200300191 120030101A5400 SHIM BOEING757 75723N 1384973NM NR 2 PYLON DISLODGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 NR 2 PYLON INBOARD AND OUTBOARD SHIMS HAVE EXCESSIVE GAP. COMPLIED WITH EO 757-54SB-2456. (M) 2L72 4F RTA2NM 20030318000772003031800077NM 2003 3 18 AMTA200300205 120030121A3220 LINK BOEING737 73783N 13844HINM NLG LWR TORSION GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11313TZ 32580 NLG LOWER TORSION LINK RIGHT SIDE GOUGED 7 INCHES FROM CENTER OF THE APEX LUGS. REPAIRED LOEWR TORSION LINK IAW ER/A 737-32R-5067. (M) 2L72 4F RTA16WE 20030318000802003031800080WP 2003 3 18 ASAA0380017 120030103A5321993659927 FLOOR PANEL DOUG DC9 DC983 3022083WP CARGO BAY DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL EDGE DAMAGED AT FS 693-730. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030318000922003031800092WP 2003 3 18 ASAA0380029 120030104A575539615971 ACCESS PANEL DOUG DC9 DC983 3022083WP RT SPOILER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT INBOARD FLIGHT SPOILER ACCESS PANEL 1626A IS CRACKED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20030318000992003031800099EA 2003 3 18 COMA0360146 120030315A3110 PANEL CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01934CA 7042 FLIGHT 5605 LOUD CRACKLING SOUND FROM OVERHEAD INSTRUMENT PANEL.COULD NOT DUPLICATE - FOUND NO DEFECTS, PRESSURIZED AIRCRAFT AND NO DEFECTS. 2L72 4F RTA21EA 20030318001072003031800107EA 2003 3 18 ASOA03032 120030125A2910601R7528649 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM CHAFED A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11840AS 7290 FLT 4501 - DURING CLIMB-OUT FROM TUS-DFW, AT APPROXIMATELY 14,000 FEET, THE CREW RECEIVED A NR 1 HYDRAULIC HIGH TEMPERATURE MESSAGE OF 125 DEGREES CELSIUS AND 3,900 PSI. WHILE THE CREW COMPLIED WITH THE QRH PROCEDURES, THE TEMPERATURE CONTINUED TO CLIMB. AT 136 DEGREES CELSIUS, ALL INDICATIONS OF QUANTITY AND PRESSURE IN THE NR 1 SIDE WERE LOST. THE CREW SHUT DOWN THE LEFT ENGINE. DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO TUS, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC SERVICE LINE. ENGINE RUNS, OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030318001102003031800110NM 2003 3 18 BJNA03021 120030203A5330 PANEL BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION, AND BROKEN RIVETS WERE DISCOVERED AROUND AIR CONDITIONING GROUND SERVICE PANEL AT FS 520 STRINGER 29L-28R. TIMCO REMOVED CORRODED SKIN SECTION, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBELR OUT OF 2024 T3. 071 MATERIAL. REPAIR DIMENSIONS APPROXIMATELY 19 INCHES BY 20 INCHES. WORK DONE IAW BOEING 737-200 SRM 53-30-3, FIGURE 28. (M) 2L72 4F RTA16WE 20030318001122003031800112NM 2003 3 18 BJNA030211 120030212A5320 FLOOR SUPPORT BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A CABIN FLOOR SUPPORT ANGLE LOCATED AT BS 277 BL 10L WL 208.1. REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW BOEING 737 SRM 53-10-9 FIGURE 1, 53-10-1 FIGURE 1, AND 51-40-4. (M) 2L72 4F RTA16WE 20030318001152003031800115NM 2003 3 18 BJNA03022 120030203A5330 PANEL BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE FORWARD RIGHT SIDE OF THE FUSELAGE TO WING FILLET PANEL NR 3479R, AFT SUPPORT. REMOVED AND REPLACED THE CORRODED TAPERED SHIMS IAW BOEING 737-200 SRM 51-10-1 PAGE 8. (M) 2L72 4F RTA16WE 20030318001182003031800118NM 2003 3 18 F3LA200300101 120030228A5320 CHANNEL BOEING737 7373Q8 1384670NM STA. 727-787 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR CHANNEL CORRODED BETWEEN STA. 727 AND STA. 787, STR. 25-R TO STR. 26-R. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-60-53, FIG. 204, 51-30-01, FIG. 3, 51-10-02, PARA. 7, AND 51-20-01. 2L72 4F RTA16WE 20030318001212003031800121NM 2003 3 18 BJNA03028 120030211A5347BAC1520792 SEAT TRACK BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE SCALLOPS AND WELLS OF A PASSENGER CABIN SEAT TRACK LOCATED AT BS 344-360 LEFT INBOARD SIDE. REMOVED THE CORRODED SECTION OF SEAT TRACK AND REPLACED WITH A NEW SECTION MADE OUT OF BOEING EXTRUSION P/N BAC1520-792. WORK DONE IAW BOEING 737 SRM 53-10-5 FIGURE 2. (M) 2L72 4F RTA16WE 20030318001232003031800123NM 2003 3 18 GAIA02002OP 120030128A2612 WARNING LIGHT BOEING727 727223 1384074NM NR 2 ENGINE ILLUMINATED A GAIAEC ENGINE SHUTDOWN ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07856AA 20997 FLT 272 - MSP-MCI - AT APPROXIMATELY 200 FEET AGL, THE NR 2 ENGINE HAD A FIRE INDICATION. THE CREW DECLARED AN EMERGENCY AND SHUTDOWN THE NR 2 ENGINE AS PER EMERGENCY PROCEDURES. UPON ENGINE SHUTDOWN, THE FIRE INDICATION EXTINGUISHED. AIRCRAFT PERFORMED AN AIR TURN BACK TO MSP. AN UNEVENTFUL LANDING WAS MADE. (M) 2L73 4F A3WE 20030318001322003031800132NM 2003 3 18 GAIA03004OP 120030205A33501000677 LIGHT BOEING727 727251 138408HNM CABIN INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW07279US 21158 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT AND FORWARD ENTRY EXIT LIGHT WERE DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLIES. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030318001332003031800133NM 2003 3 18 GAIA03005OP 120030205A33501000677 LIGHT BOEING727 727287 1384020NM CABIN WRONG PART A GAIAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07916PG 21690 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE L1 EMERGENCY EXIT LIGHT WOULD NOT TEST. FOUND INCORRECT UNIT INSTALLED. REMOVED AND REPLACED WITH CORRECT PART NR EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20030318001352003031800135NM 2003 3 18 F3LA200300103 120030228A5320 CHANNEL BOEING737 7373Q8 1384670NM STA. 727B - 727CCRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT CHANNEL CRACKED FROM STA. 727B TO 727C, STR. 21-L TO STR. 24-L. FABRICATED AND REPLACED CHANNELS PER SRM 51-20-02, 51-30-01, FIG. 3, 51-10-02, AND 51-20-01. 2L72 4F RTA16WE 20030318001792003031800179EA 2003 3 18 COMA0370005 120030316A5312 CNDAIR CNDAIRCL600 CL6002C10 1390015EA A COMAO OTHER O OTHER ININSP/MAINT 1 SO01331CA 10061 F.S. 1098.20 PRESSURE BULKHEAD RIGHT SIDE RBL34 TO RBR 41 BETWEEN STRINGERS 8R AND 9R. HAS ONE INCH CRACK ON BULKHEAD.INCORPORATED RIGHT PRESSURE BULKHEAD BOMBARDIER, INC. REO 670-53-61-059 REV NC. REMOVED DAMAGED FITTING AND INSTALLED P/N 670-53-61-038-2. 2L72 4F RTA21EA 20030625001152003062500115EU 2003 6 25 IXXA0300024O 220030309A7230 COMPRESSOR DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM562AFR 13802EU NR 1 ENGINE STALLED A IXXAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 SW11820BX 46065 AFTER DEPARTURE FROM GSO DURING CLIMB OUT TO TOL. WHEN POWER REDUCED FROM CLIMB TO CRUISE, CREW NOTED NR 1 ENGINE COMPRESSOR STALL. PRECAUTIONARY ACTION WAS TAKEN AND ENGINE SHUTDOWN FOR REMAINDER OF FLIGHT. CREW MADE AN UNEVENTFUL LANDING IN TOL. 2L74 4F4 FRT4A25 E21EU 20030625001142003062500114WP 2003 6 25 IXXA0300023O 120030310A5610 WINDSHIELD DOUG DC8 DC862 3021970WP COCKPIT CRACKED A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW1141CX 772431108 DURING CLIMB OUT OF WRI COPILOTS WINDSHIELD CRACKED. CREW ELECTED TO RETURN TO WRI AND MADE AN UNEVENTFULL LANDING. 2L74 4F 4A25 20030318001912003031800191NM 2003 3 18 VNAA0303021 120030317A5300 SEAL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RH FAILED A VNAAO OTHER O OTHER CLCLIMB 1 GL07432JS 3045 DURING CLIMB OUT, THE CREW HEARD A THUMPING NOISE FROM THE UPPER RIGHT SIDE OF THE AIRCRAFT AND RETURNED TO DAY. MAINTENANCE INSPECTED AND TRIMMED THE UPPER FUSELAGE FAIRING SEAL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00. FLIGHT 4192 THE LEFT WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030318002022003031800202NM 2003 3 18 UPS03240300 120030223A5730 SKIN BOEING727 727108C 1384039NM BS 856-860 WBL70CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI EVIDENCE OF CORROSION BETWEEN WING CENTER SECTION UPPER SKIN & SKIN UPPER SPLICE @ BS 856 - 860 I/B OF WBL 70.5 RIGHT REPAIR CARRIED OUT IAW SRM 51-10-1, 51-10-2, 51-30-02 & SMRO EO 2003 -008-018 UPS ENGINEERING FILE NO B727-5730-18440-A 2L73 4F A3WE 20030318002052003031800205WP 2003 3 18 ARWA20030310 120030314A2900 HOSE DOUG DC8 DC862 3021970WP A ARWAO OTHER K FLUID LOSS LDLANDING 1 SO198968U 46069 LOG PAGE 506081 & 506082. DISCREPANCY: ON LANDING AT FJDG, AIRCRAFT SUFFERED LOSS OF HYDRAULICS. EMERGENCY AIR BRAKE PRESSURE BOTTLE USED AFTER LANDING. CORRECTIVE ACTION: FOUND BROKEN HOSE IN RIGHT SIDE BOOGIE TRIM CYLINDER. REMOVED AND REPLACED HOSE IAW MM 32-33-0. OPERATIONAL CHECK FOUND NORMAL, NO LEAKS IAW MM 32-33-1. SERVICE HYDRAULIC RESERVOIR IAW MM 12-30-1. EMERGENCY AIR BRAKE BOTTLE SERVICED IAW MM 32-44-2. 2L74 4F 4A25 20030421000252003042100025 2003 4 21 SWIA200311803 420030220A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07439SW 7578 ON ROTATION STALL FAIL MESSAGE DISPLAYED. WOULD NOT CLEAR. INSPECTED STALL PROTECTION SYSTEM AND PERFORMED TESTS. COULD NOT DUPLICATE. SYSTEM OPS CHECKS GOOD. 2L72 4F RTA21EA 20030421000262003042100026EA 2003 4 21 SWIA200311804 120030222A5220 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY EXIT OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07589SW 7072 RIGHT EMERGENCY EXIT IN CABIN WILL NOT REMOVE. RIGHT EMERGENCY EXIT IN CABIN FOUND OUT OF ADJUSTEMENT. ADJUSTED BRACKET AS REQUIRED. 2L72 4F4 FRTA21EA E15NE 20030421000282003042100028NM 2003 4 21 EIA200311 120030226A5330 SKIN BOEING747 747132 1384882NM PWA JT9 JT9D3 52050NE FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 EXTERNAL SKIN REPAIR, AT STATION 1580 STRINGER 35L TO 36L IS NOT IAW SRM. REMOVED EXTERNAL SKIN REPAIR, FABRICATED NEW FILLERS, AND DOUBLER. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-03, PAGE 2A-2F, AND SOPM CH. 20-41-02, PAGE 17-19. CATEGORY (B) REPAIR, COI NR 052 INITIATED. 2L74 4F4 F A20WE E20EA 20030421000322003042100032EU 2003 4 21 MALA030182 120030227A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15454XJ 340B454 COVE LIGHT 11LN WOULD NOT COME ON LINE. MAINTENANCE FOUND POWER SUPPLY 20 LN BAD. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY AND OPS CHECKED GOOD. 2L72 4T RTA52EU 20030421000332003042100033EU 2003 4 21 MALA030181 120030224A3260 BULB SAAB SF340 340B 7860101EU LT MLG INDICATORBURNED OUT A MALAO OTHER P NO WARNING INDICATION LDLANDING 1 GL15414XJ 340B414 DURING FLIGHT 2764 THE MLG DOWN AND LOCK LIGHT (GREEN) DID NOT ILLUMINATE WHEN GEAR WAS LOWERED FOR LANDING. UNABLE TO GET LT MLG INDICATION. PERFORMED QRH PROCEDURES, FINALLY WAS ABLE TO GET INDICATION. MAINTENANCE ADJUSTED TAB ON LEFT GEAR, INDICATION TO BULB. INSTALLED NEW BULB. PERFORMED GEAR SWINGS IAW AMM 32-30-00-5. OPS CHECK GOOD. 2L72 4T RTA52EU 20030421000382003042100038NM 2003 4 21 UPS03440241 120030131A5753 FLAP TRACK BOEING747 747200 1384847NM NR 3 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, LEFT WING - NR 3 FLAP TRACK AFTER END INNER SURFACE I/B WALL AREA FOUND CORROSION (FINDING AFTER PIVOT FITTING REMOVAL). LEFT WING NR 3 FLAP TRACK AFT END INNER SURFACE INBD WALL AREA CORROSION REMOVED AND REPROTECTED REFER CWS SERIAL NR 016250, 016850 TO 16854 FOR WORK DETAILS. REF HX RS 57-53-34971 AND EO B747-5740-18331 -A. BLEND AREA 1.5 X 1.5 INCH, THICKNESS REMAIN 0.124 INCH AND ORIGINAL THICKNESS 0.207 INCH. 2L74 4F RTA20WE 20030421000552003042100055NM 2003 4 21 UPS03640248 120030215A2497BMS1360T2C110 CABLE BOEING767 76734AF 1385212NM ZONE 600 ARCED A IPXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01303UP 27241 INSPECTION TYPE: C, RT WING L/E GENERATOR LEAD HAS ARCING DAMAGE FROM RIB, 4 INCHES O/B OF FUSELAGE, ABOVE PDU. REPAIRED FEEDER CABLES PER SWPM 20-30-13 AND AND 20-10-11. FUNCTIONAL TESTED GOOD. 2L72 4F RTA1NM 20030417000762003041700076NM 2003 4 17 P5CA0300744 120030127A5522 PANEL BOEING747 747283B 1384867NM ELEVATOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 DELAMINATION AND A HOLE FOUND LT ELEVATOR 334JB HONEYCOMB PANEL. REPAIRED BY BONDING FIBERGLASS PLIES PER SRM 51-40-09. 2L74 4F A20WE 20030417000812003041700081WP 2003 4 17 MWEA030053 120030203A532099122433 BULKHEAD DOUG DC9 DC932 3022066WP RT PYLON CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31207ME 47794 STATION 965 RIGHT FORWARD PYLON BULKHEAD HAS A CRACK GOING INBOARD OF LIGHTENING HOLE AT Z = 50.0. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030417001632003041700163WP 2003 4 17 ZW0A0301902 120030209A3350 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13948TW 49575 THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE FROM ROW 18 TO 26, THE EGRESS FLOOR LIGHTS WERE INOPERATIVE IN FIRST CLASS, AND THE LEFT SIDE NUMBER 1 AND RH SIDE NUMBER 1 CABIN DOOR EXIT SIGNS WERE INOPERATIVE. REPLACED THE BATTERIES PN 408822-101 FOR THE CEILING EMERGENCY LIGHTS AND FOR THE EGRESS LIGHTS. REPLACED THE POWER SUPPLY PN 60-0304-51LB FOR THE EXIT SIGNS. CHECK-C 1-21-02 STL. 2L72 4F RTA6WE 20030417001782003041700178SO 2003 4 17 SWIA200311768 120030205A2130 SWITCH EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE CABIN PRESSURE MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07212SW 120286 PRESSURIZATION COULD NOT KEEP CABIN BELOW 12000 FT ON CLIMBOUT WITH APU BLEED. F/A REPORTED SMOKE AND ODOR AT REAR OF CABIN JUST AFTER TURNBACK TO GJT. AT 16-17K AND ABOVE THE MAIN CABIN DOOR PRODUCED AN AIR LEAK. RETURNED TO GJT. REMOVED AND REPLACED RATE/MANUAL DUMP SWITCH. PRESSURE CHECKED AIRCRAFT IAW MM 21-30-00 USING TEST BENCH TO 4 PSID. CHECKED PRESSURIZATION ON GROUND WITH APU ONLY. CHECKED PRESSURIZATION ON GROUND WITH BOTH ENGINES IAW MM 21-30-00. OPS CHECKED ON GROUND GOOD. P/N OFF: MS27788-21P. 2L72 4T4 TRTA31SO E20NE 20030417001962003041700196NM 2003 4 17 P5CA0300761 120030204A5315 FLOORBEAM BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LEVEL 1 CORROSION ON FLOORBEAM AND SEAT TRACK STA 1760-1880 LBLM & RBLM WL 208. 2L74 4F A20WE 20030417001992003041700199WP 2003 4 17 ZW0A0302102 120030212A3350 SIGN DOUG DC9 DC983 3022083WP LT & RT OVERWINGINOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139616G 53563 AT ROW 20 THE LEFT AND RIGHT OVERWING EXIT SIGNS WERE INOPERATIVE, AND SEVERAL EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK, PN 408822-101, FOR THE EXIT SIGNS, AND RESEATED LAMPS IN SOCKET FOR THE EGRESS LIGHTS. CHECK-C7-26-02 STL. 2L72 4F RTA6WE 20030418000132003041800013NM 2003 4 18 UPS03540174 120030215A2560MXP21000 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01455UP 25476 JUMPSEAT SMOKE GOGGLES LENSE CRACKED. REPLACED JUMPSEAT SMOKE GOGGLES. 2L72 4F RTA2NM 20030418000642003041800064NM 2003 4 18 QXEA0300271 120030202A1430 RIVET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - RIVET SHEERED BUCKTAIL, RIGHT HAND VERTICAL U-CHANNEL STATION XN94.330, ON LEFT HAND LOWER COWL. REPAIRED IAW DHC-8 Q400 SRM 51-47-05. 2H72 4T RTA13NM 20030318002172003031800217NM 2003 3 18 AWXA200300290 120030302A532070750071 WEB BOEING757 757225 1384959NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW0 0 22208 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 3/4" CRACK WAS FOUND ON FORWARD CARGO DOOR CUTOUT WEB AT BS 560, BELOW THE NO. 6 DOOR STOP. MAINTENANCE CUTOUT DAMAGED AREA OF FORWARD CARGO DOOR CUTOUT WEB AT BS 560; FABRICATED A NEW SECTION OF WEB; INSTALLED REPAIR PART IAW B737-200 SRM 53-00-07, PG. 205-206, FIG. 202. 2L72 4F RTA2NM 20030318002242003031800224SO 2003 3 18 RAIA00303073 120030313A27300861DT5 VANE EMB 145 EMB145LR 3260212SO INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03818HK636 335 145059 5712-STL- STALL PROTECTION #2 INOP WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE #2 AOA VANE, OPS CK OK. 2L72 4T RTT00011AT 20030319000012003031900001WP 2003 3 19 GTIA030001 120030108A25601001191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FLL - FOUND HAND HELD EMERGENCY LIGHT BY L1 DOOR IS INOPERATIVE. REMOVED AND REPLACED L1 DOOR HAND HELD EMERGENCY LIGHT PER MM 33-50-00, OPS CHECK GOOD. (M) 2L72 4F A6WE 20030319000072003031900007WP 2003 3 19 GTIA030008 120030111A5320 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CABIN FLOOR PANEL AFT AUX TANK DETERIORATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030319000132003031900013 2003 3 19 GTIA030015 420030120A2565 SLIDE DOUG DC9 DC982 3022082WP PAX DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FLL - FLT 9817 - PACK SLIDE FELL OFF L1 WHEN OPENED. REINSTALLED PACK SLIDE ON L1 DOOR. (M) 2L72 4F A6WE 20030319000242003031900024WP 2003 3 19 GTIA030047 120030201A7120K22199SA31 MOUNT DOUG DC9 DC983 3022083WP ENGINE DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 DTW - FOUND FORWARD LOWER ISOLATION MOUNT ALIGNMENT MARKS SHIFTED ON RIGHT ENGINE. REMOVED AND REPLACED FORWARD LOWER ISO MOUNT. (M) 2L72 4F RTA6WE 20030319000312003031900031WP 2003 3 19 GTIA030056 120030213A2612 FIRE LOOP DOUG DC9 DC982 3022082WP NR 2 ENGINE LOOSE A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23821NK 49508 FLT 594 - MCO - NR 2 ENGINE B-LOOP (FIRE WARN) FLICKERS. FOUND LOOSE GROUND WIRE AT P1-828 AND BAD CONNECTOR AT LOWER BURN THROUGH BARRIER P1-865. CORRECTED DISCREPANCIES. CHECKS GOOD. (M) 2L72 4F A6WE 20030319000392003031900039WP 2003 3 19 GTIA030064 120030207A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 160-200 LBL 45 HAS CORROSION. LOCATED AND DRILLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030319000452003031900045WP 2003 3 19 GTIA030070 120030208A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND SUPPORT FS 518-636 HAS CORROSION. FABRICATED SUPPORT. (M) 2L72 4F A6WE 20030319000502003031900050WP 2003 3 19 GTIA030075 120030204A5320 CLIP DOUG DC9 DC981 3022081WP INTERCOSTAL CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND AFT PIT INTERCOSTAL CLIP STATION 1220 HAS SURFACE CORROSION, PANEL CORRODED IN FASTENER HOLES. CLIPS IS OUT OF LIMITS. DRILLED NEW CLIP. (M) 2L72 4F A6WE 20030319000592003031900059NM 2003 3 19 HALA0300008 120030108A2140214T640518 DUCT BOEING767 76733A 1385209NM CARGO HEAT BLOWN A HALAK NONE O OTHER ININSP/MAINT 1 WP13589HA 33422 HNL - FOUND BLOWN AIR SUPPLY DUCT FOR FORWARD CARGO HEAT SYSTEM. REPLACED DUCT ASSEMBLY. (M) 2L72 4F RTA1NM 20030319000632003031900063NM 2003 3 19 KPVA20031 120030103A26113023143 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM CARGO BAY MALFUNCTIONED A KPVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP13806WP 357 FLT 1126 - HNL - BAGGAGE COMPARTMENT SMOKE WARNING ILLUMINATED DURING ENGINE START. NO SMOKE PRESENT AND ALL ELECTRICAL DEVICES VERIFIED OFF (CELL PHONES). REMOVED AND REPLACED NR 2 SMOKE DETECTOR. OPS CHECK GOOD IAW DHC-8 MM 26-12-00 PATE 201. (M) 2H72 4T RTA13NM 20030319000722003031900072NM 2003 3 19 MEX2003007 120030117A2913AS66411LS666 PUMP DOUG MD80 MD83 3023681NM HYD SYSTEM FAILED A ASMFD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23946AS 49658 FLT 945 - MTY-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCES OF LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH ZERO PRESSURE INDICATION. LEFT ENGINE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, ALL CORRECT. (M) 2L72 4F RT 20030319000732003031900073WP 2003 3 19 MEX2003009 120030122A2913AS66411LS666 PUMP DOUG DC9 DC982 3022082WP HYD SYSTEM FAILED A ASMFD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW231003Y 48068 FLT 258 - MEX-CJS - AIRCRAFT RETURNED TO GATE DUE TO LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH CERO PRESSURE INDICATION. LEFT ENGINE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, ALL CORRECT. (M) 2L72 4F A6WE 20030319000762003031900076WP 2003 3 19 MEX2003025 120030204A2910 LINE DOUG DC9 DC983 3022083WP HYD SYSTEM LEAKING A ASMFD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23838AM 49397 FLT 429 - MIA-MEX - AIRCRAFT RETURNED TO GATE DUE TO HYDRAULIC LEAK AT THE NLG STEERING. LINE WAS REPLACED AND WAS INSTALLED HIGH PRESSURE FLEXIBLE HYDRAULIC LINE IAW MM 20-12-0. (M) 2L72 4F RTA6WE 20030418000752003041800075NM 2003 4 18 QXEA0300285 120030204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - NR 2 VHF ANTENNA MOUNT AREA INTERNAL LEFTHAND FORWARD SET OF BRACKETS, FORWARD BRACKET IS CRACKED AT STRINGER 33 AND X80. REPAIRED IAW HORIZON AIR EO/EA 6-53-162A. 2H72 4T RTA13NM 20030418001042003041800104WP 2003 4 18 UPS03840208 120030219A274037048411 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, O/B AFT STRINGER 51 END FT CRACKED AT XRS 74.000 NR 2 MAIN. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. DRILLED LOCATED DEBURRED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. LEAK CHECK TO BE ACCOMPLISHED ON UPS T/C 8000 ITEM 26. 2L74 4F RT4A25 20030418001462003041800146NM 2003 4 18 QXEA0300301 120030224A3350AML51G60GY SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 200 INTERMITTENT A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09360PH 515 PDX- EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANTS POSITION INTERMITTANT. REPLACED FLIGHT ATTENDANT'S EMERGENCY LIGHT SWITCH 3351-S2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421000362003042100036WP 2003 4 21 MWEA030117 120030227A532199365851 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOORBOARD BETWEEN SEAT TRACK NR 1 AND 2 AT STATION 316 IS DENTED. REPAIRED DENT. 2L72 4F A6WE 20030421000782003042100078NM 2003 4 21 DL777030078 120030122A2430 WARNING LIGHT BOEING777 777232 1385232NM BATTERY FALSE INDICATIONA DALAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO27861DA3428 29952 P1307 APU BATTERY AND APU BATTERY OVERHEAT MSG. REPLACED APU BATTERY AND CHARGER. AC ALSO HAD STATUS MSG FOR BATTERY AN CHARGER. INSPECTED FOR DAMAGE, NONE FOUND. 2L72 4F RTT00001SE 20030421000862003042100086NM 2003 4 21 DLM88030118 120030131A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27941DL 49814 THE FUSELAGE SKIN WAS FOUND WITH A .75 INCH CRACK AT FS 1418, JUST OUTBOARD OF THE VERTICAL STAB TO FUSELAGE ATTACH ANGLE AND STRINGER 1L. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH A TITANIUM REPAIR DOUBLER PER ER/A 384509-14, REV A. 2L72 4F RTA6WE 20030421000892003042100089NM 2003 4 21 DL76S030127 120030205A3397 WIRE BOEING767 767332 1382001NM EMERGENCY LIGHT TORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27139DL 25984 A 2R LAV EMERGENCY EXIT RED LIGHT WIRING TORN FROM WALL BY PAX. REPAIRED WIRING AND INSTALLED NEW EMERGENCY EXIT RED LIGHT. 2L72 4F RTA1NM 20030421000932003042100093NM 2003 4 21 DLM88030139 120030209A335060030451 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27913DL 49544 POWER OFF EMERGENCY LIGHTS STAY ON AT L-1, R-1 AND COCKPIT. REPLACED POWER SUPPLY. 2L72 4F RTA6WE 20030421000962003042100096NM 2003 4 21 DLM11030155 120030213A2612 WARNING LIGHT DOUG MD11 MD11 3023602NM LAVATORY ILLUMINATED A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO27804DE 48475 LAV SMOKE MSG ILLUMINATED WITH CORRESPONDING PILOT LIGHT. LIGHT INSPECTED LAV AND TESTED WARNING SYSTEM. 2L73 4F RTA22WE 20030421000972003042100097NM 2003 4 21 DLM11030156 120030213A2530 OVEN DOUG MD11 MD11 3023602NM G5 GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27813DE 48600 GALLEY G5 OVEN HAS BURNING SMELL. REPLACED OVEN. 2L73 4F RTA22WE 20030421001102003042100110NM 2003 4 21 DLM90030205 120030301A3260 UPLOCK TARGET DOUG MD90 MD9030 3023690NM LT MLG DOOR OUT OF ADJUST A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27910DN 53390 AFTER T/O, LT MLG RED WARNING LIGHT REMAINED ILLUMINATED AFTER RETRACTION. FOLLOWED POM PROCEDURES, LIGHT REMAIN ILLUMINATED. ADJUSTED LT GEAR UP AND LOCKED TARGET ON MLG DOOR, SWUNG GEAR. OPS CHECKS GOOD. 2L72 4F RTA6WE 20030421001132003042100113EU 2003 4 21 MALA030185 120030214A302061241 DUCT SAAB SF340 340B 7860101EU LT INTAKE LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15368PX 340B274 DURING FLIGHT 3001, LT ENGINE INTAKE CAUTION LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE PERFORMED CONTINUITY CHECK, FOUND LOWER LT DUCT BAD. REPLACED LOWER LT DUCT P/N 6124-1 SN/OFF 219, SN/ON 100. PERFORMED ENGINE RUN TO OPS CHECK LOWER INLET DUCT. OPS CHECK GOOD. 2L72 4T RTA52EU 20030421001172003042100117EU 2003 4 21 MALA030187 120030304A36209303688100 HOSE SAAB SF340 340B 7860101EU RT BLEED LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15421XJ 340B421 DURING 2920, RT BLEED LEAK LIGHT CAME ON INFLIGHT. AIR RETURN TO MEM. MAINTENANCE FOUND RT WING TO FUSELAGE BLEED HOSE LEAKING. INSTALLED NEW HOSE P/N 9303688-100 TO RT SIDE IAW SAAB AMM 36-11-35-4, OPS CHECK GOOD. 2L72 4T RTA52EU 20030421001302003042100130NM 2003 4 21 VNAA0303001 120030302A2121 FAN DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT A/C PACK FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07434JS 3051 THE CREW REPORTED A LEFT HAND HX FAN FAIL, THEN A LEFT HAND PACK OVERHEAT, AND THEN A LAV SMOKE CAS MESSAGE. THE CREW WITH MAINTENANCE CONTROL MEL'D THE LEFT HAND HX FAN WITH CODE 21-7 C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421001312003042100131NM 2003 4 21 VNAA0302028 120030228A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DOOR FAILED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07429JS 3043 EN ROUTE, THE MAIN CABIN DOOR LIGHT CAME ON, NO PRESSURIZATION WAS LOST. FLIGHT 4295 THEN DIVERTED TO CVG. MAINTENANCE INSPECTED AND CLEANED THE MAIN CABIN DOOR PROXI SWITCH THEN ADJUSTED THE MAIN CABIN DOOR PROXI SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421001352003042100135NM 2003 4 21 VNAA0302024 120030226A3260 INDICATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG MALFUNCTIONED A VNAAL ABORTED APPROACH N FALSE WARNING DEDESCENT 1 GL07433JS 3047 AFTER THE CREW LOWERED THE LANDING GEAR, THE CREW RECEIVED GREEN DOWN AND LOCKED LIGHTS FOR THE MAIN GEAR BUT RED FOR THE NOSE GEAR. THE CAPTAIN CYCLED THE GEAR APPROXIMATELY 5 TIMES AND STILL RECEIVED A RED LIGHT FOR THE NOSE GEAR. THE CREW DECLARED AN EMERGENCY AND WERE ADVISED TO PERFORM A FLY BY WITH THE TOWER. AT 200 FEET, THE CREW RECEIVED A GREEN NOSE GEAR INDICATION AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE WAS DISPATCHED TO PHL TO INSPECT THE AIRCRAFT. MAINTENANCE JACKED THE AIRPLANE AND PERFORMED APPROXIMATELY 30 GEAR RETRACTIONS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00 AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421001672003042100167SW 2003 4 21 2003F00219 120030104A5230 MECHANISM FRCHLDSA227 SA227DC 3377521SW CARGO DOOR OUT OF ADJUST A BSAAO OTHER J WARNING INDICATION CLCLIMB 1 NM05453LA DC852B FLT 2561 - OLF - DURING CLIMB, THE CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHT CAME ON AT CABIN PRESS OF 2 PSID. PASSENGER REPORTED NOISE FROM AFT OF AIRCRAFT. CREW RETURNED TO STATION, LIGHT WENT OUT AS ENGINES WERE SHUT DOWN. DOOR CLOSING PROCEDURES OR DOOR HARD TO CLOSE. CLEANED AND LUBED CLICKS, ADJUSTED LOWER AFT CLICK CLACK AND REINDEXED LINKAGE. (M) 2L72 4T RTA18SW 20030421001852003042100185WP 2003 4 21 ZIAA03002 120030218A5730 SKIN LKHEED188 188A 5262602WP LT WING CORRODED A ZIAAK NONE O OTHER ININSP/MAINT 1 GL03343HA 1053 YIP - FOUND CORROSION ON LEFT WING LOWER SURFACE NR 4 WING PLANK TRAILING EDGE BETWEEN APPROXIMATE LWS 448 AND LWS 533. REMOVED CORRODED SECTION OF NR 4 WING PLANK TRAILING EDGE PER ZANTOP DWG S59-R01. (M) 2L74 4T RT4A22 20030421001912003042100191WP 2003 4 21 GTIA030120 120030303A7120K22199SA31 ISOLATION MOUNT DOUG DC9 DC983 3022083WP NR 2 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL11824NK 53015 DTW - NR 2 ENGINE PYLON FORWARD LOWER BARRY CONTROL MOUNT REQUIRES CHANGING, ISOLATOR MOUNT. REMOVED AND REPLACED FORWARD LOWER ISOLATOR MOUNT. (M) 2L72 4F RTA6WE 20030421001922003042100192NE 2003 4 21 GTIA030121 220030301A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT FAILED A GTIAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL23808NK 49504 718262 ORD - FLT 1442 - SHORTLY AFTER TAKEOFF, THE NR 1 ENGINE LOST OIL PRESSURE AND OIL QUANTITY AT 1000 FEET AGL, APPROX 2 MINUTES AFTER IDENTIFYING AND RUNNING CHECKLISTS NR 1 ENGINE WAS SHUTDOWN NR 1 HAD 0 OIL QTY AT SHUTDOWN AND HAD BEEN AT IDLE POWER FOR MORE THAN 1 MINUTE, OIL PRESSURE WAS AT APPROX ZERO ENGINE WAS AT WINDMILLING SPEED FOR ABOUT 4-5 MINUTES. REMOVED AND REPLACED ENGINE LEFT SIDE IAW SPIRIT AIRLINES TASK CARD 00191. LEAK AND OPS CHECK GOOD. (M) 2L72 4F4 FRTA6WE E9NE 20030421001932003042100193WP 2003 4 21 GTIA030127 120030223A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FWD CABIN DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CABIN STATION 160-148 LBL 8 INCHES FLOOR PANEL, BELOW OBSERVER, SOFT/DAMAGE (15 BY 11). FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20030421001962003042100196WP 2003 4 21 GTIA030133 120030203A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - E/E COMPARTMENT STATION 200 LBL 0 LBL 44, FLOORBEAMS AND SUBFLOOR HAVE WATER, INCLUDING INTERCOSTAL STATION 180-200 LBL 44. UPON FURTHER INVESTIGATION, FOUND CRACK BETWEN 2 RIVET HOLES STATION 200 LBL 21 IN SUBFLOOR WEB. LOCATED AND DRILLED REPAIR FOR CRACK. INSTALLED REPAIR ON WEB. (M) 2L72 4F A6WE 20030417002022003041700202WP 2003 4 17 UPS03840168 120030206A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1160 BETWEEN L33R-34R Z-FITTING IS CRACKED. REMOVED CRACKED FITTING. FABRICATED REPAIR DOUBLER & SHIM IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING REPAIR DOUBLER AND SHIM IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030417002072003041700207NE 2003 4 17 QXEA0300250 220030212A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX2085 10011 GEE965294 PDX - NR1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR MISSING BLADES AND SIX BLADES HAVE TRAILING EDGE DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030418000042003041800004EU 2003 4 18 RAIA00302032 120030202A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK 41040 MX-STL- EMERGENCY PATH LIGHTS INOP. RE-SECURED LOOSE CONNECTOR AT FLOOR LIGHT STRIP, OPS CHECK OK. 2L72 4T RTA41NM 20030418000452003041800045EU 2003 4 18 MALA030139 120030201A526090050 SPRING SAAB SF340 340B 7860101EU AIRSTAIR INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15449XJ 340B449 AIRSTAIRS WOULD NOT UNLOCK TO OPERATE. REPLACED GAS SPRING STAIR ASSY P/N 90050 IAM MM CH 52-60. ALL GOOD AT THIS TIME. 2L72 4T RTA52EU 20030418001102003041800110EU 2003 4 18 YENA200304 120030222A2120 SMOKE AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15516JB 1302 FLT 389 JFK TO FLL PASSING 4000 FT, THE FLT ATTENDANTS CALLED AND INFORMED THE CREW THAT A DEFINITE SMELL OF SMOKE WAS DETECTED IN THE THE AFT AND FWD CABIN. THE STRONGEST ODOR CAME FROM AROUND ROW 10. PERFORMED ENG NR 1 & 2 IDLE ENGINE RUN IAW MM 71-00-0. NO FOREIGN ODORS NOTED THROUGH THE CABIN OR GALLEYS. ALSO CYCLED APU BLEED. CYCLED BOTH NR 1 AND NR 2 PACKS & OPS CHECK PACKS IAW MM 21-51-00, OPS CHECK OK. INSPECTED AND OPERATED ALL COFFEEMAKERS IAW 25-35-00, ALL COFFEEMAKERS CHECK OK. INSPECTED APU & APU AREA INTAKE SYSTEM IAW MM 49-16-00, CHECK OK. NO FOREIGN ODORS NOTED WITH ALL CHECKS OR ABNORMALITIES NOTED IAW MM 05-51-51-11. OVERWEIGHT LANDING INSPECTION CHART ALL VALUES ARE WITH LIMITS. NO 2L72 4F RTA28NM 20030418001142003041800114WP 2003 4 18 UPS03840213 120030221A5711 SPAR DOUG DC8 DC873F 302199FWP LT & RT WINGS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, PERFORM LT WING AND RT WING FWD SPAR INSPECTION OF LWR SPAR CAP PER EO DC8-5 710-14184-C AS REQUIRED. REAMED 1 DISCREPANT HOLE ON L/W TO .3230, PERFORMED HFEC AND NO CRACKS NOTED PER DAC SPM 06-10-01.003. CHECKED SPAR THICKNESS AT .689 & L/E SKIN AT .143. FAB'D BUSHINGS FOR REPAIR IAW DAC DWG 4709980 & SRM 51-1-25. REAMED HOLE TO PRE COIN SIZE AND STRESS COINED PER DPS 3.67-56. INSTALLED BUSHINGS PER SRM 51-1-23. 2L74 4F RT4A25 20030418001442003041800144NE 2003 4 18 XNOA01107 220030225A7230 ENGINE BOEING727 727173C 1384059NM PWA JT8 JT8D7 52053NE NR 2 STALLED A XN0AC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL23704A 19504 ON ROTATION NR 2 ENGINE COMPRESSOR STALLED 3 TIMES. REDUCED POWER, ENGINE STABILIZED. FURTHER ADVANCEMENT OF NR 2 THROTTLE SHOWED ALL PARAMETERS NORMAL. PERFORMED VISUAL INSPECTION AND GROUND OPERATIONAL RUN. ALL ENGINE PARAMETERS WITHIN LIMITS. NO DEFECTS NOTED IAW MM 71-00. BOROSCOPED TURBINE STAGE 1 & 2 BLADES & VANES IAW PRATT & WHITNEY MM 72-50-00. NO DEFECTS NOTED. BOROSCOPED HPC STAGES 6 & 7 IAW PRATT & WHITNEY MM 72-30-00. NO DEFECTS NOTED. INSPECTED CHIP DETECTORS IAW PRATT & WHITNEY MM 72-00-00. NO DEFECTS NOTED. 2L73 4F4 F A3WE E2EA 20030421000412003042100041NM 2003 4 21 UPS03440245 120030128A5314 ANGLE BOEING747 747200 1384847NM LT KEELBEAM BOX CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C FX, KEELBEAM BOX INTERIOR LONGER FRAME FOUND HEAVY CORROSION AT LT SIDE STA 1465 TO STA 1475 LBL 6 TO LBL 8. REPAIRED ANGLE FABRICATED AS PER HX RS R53-49-34970 AND EA 747-53-20123. BLEND OUT 0.079 X 2.4 X 4 INCH. 2L74 4F RTA20WE 20030319000832003031900083CE 2003 3 19 RU3A03002 120030110A32341013841377 LEVER BEECH 300 300BEECH 1152930CE MLG SYSTEM INTERMITTENT A RU3AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2166 FF1 ON 12/31/2002, REPLACED LANDING GEAR CONTROL SWITCH. SWITCH S/N 1669A, WAS INSTALLED AND SYSTEM CYCLED THREE TIMES WITH NO APPARENT PROBLEM. ON 1/09/2003, AIRCRAFT LEFT FOR MAINTENANCE TEST FLIGHT BECAUSE RIGHT ELEVATOR HAD BEEN REMOVED AND REINSTALLED AFTER BALANCE CHECK AFTER HARDWARE REPLACEMENT. ON TAKEOFF RELEASE LEVER FAILED TO RETRACT SO GEAR HANDLE COULD BE RAISED NORMALLY. WHEN CHECKED ON JACKS WITH SQUAT SWITCH DISCONNECTED RELEASE STILL DID NOT OPERATED. REMOVED FROM AIRCRAFT AND TRIED AGAIN ANS WITH JUMPER WIRES UNIT STILL FAILED TO RELEASE SO LEVER COULD BE RAISED. THIS CONTROL SWITCH FAILED ON THE FOURTH TIME IT WAS OPERATED SINCE LAST REPAIR. SWITCH WAS REPLACED AND PROBLEM CORRECTED. (M)2L72 4T A24CE 20030319000922003031900092EU 2003 3 19 SIMA200301202 120030112A3350 LIGHT SAAB SF340 340B 7860101EU ROW 8 INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21396AE 340B396 LBB - FLT 3462 - FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT AT ROW 8 IS INOPERATIVE. AIRCRAFT WAS INSPECTED AND FERRIED TO DFW FOR REPAIR. (M) 2L72 4T RTA52EU 20030319000932003031900093SO 2003 3 19 SIMA200302004 120030116A5610163500111 WINDSHIELD EMB 135 EMB135KL 3260302SO COCKPIT FAILED A SIMAO OTHER O OTHER CRCRUISE 1 SW21814AE 145541 ORD - FLT 4148 - CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT, OUTER PANE ONLY. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030319001002003031900100NM 2003 3 19 TSAA0333020 120030202A335086210066 BATTERY PACK BOEING737 7372T4 1384492NM PAX CABIN INOPERATIVE A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13808AL 23345 REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030319001172003031900117NM 2003 3 19 USAA030014 120030207A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US39017 23992 CLT - FOUND SKIN CRACKED 2.2 INCH, BELOW S23R AT STATION 727D. INSTALLED DOUBLER PER T/R 53-60-03. (M) 2L72 4F RTA16WE 20030319001242003031900124NM 2003 3 19 CH1A200393005 120030314A2822 CONTROL VALVE BOEING727 727212 138407GNM A C1HAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL15293AS 21348 Enroute lost control of #2 fuel tank x-feed valve. Valve appeared to fail in the closed position. 2L73 4F A3WE 20030320000052003032000005NM 2003 3 20 USAABB03002 120030102A33508731002511REV15 LIGHT BOEING757 7572B7 1384964NM L4 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19614AU 27145 MIA - FOUND EXIT IDENTIFIER AT L4 DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030320000062003032000006NM 2003 3 20 USAABB03003 120030105A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19632AU 27810 MIA - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030320000212003032000021EU 2003 3 20 USAASA03001 120030101A5250 DOOR AIRBUS320 A320214 3930316EU COCKPIT STUCK A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19122US 1298 CLT - FLT 654 - EN ROUTE AUA-PHL, WHILE IN FLIGHT, THE COCKPIT DOOR WOULD NOT OPEN. THE CIRCUIT BREAKER CONTROLLING THE COCKPIT DOOR LOCKS WAS PULLED, HOWEVER, THE DOOR STILL REMAINED STUCK CLOSED. A CREW MEMBER THEN TRIED TO EXIT THE COCKPIT THROUGH THE EMERGENCY EGRESS PANEL. THE QUICK RELEASE PINS FOR THE PANEL WERE REMOVED, BUT THE PANEL WOULD NOT RELEASE. THE CREW DECIDED TO DIVERT TO CLT WHERE REPAIRS COULD BE MADE. MAINTENANCE TRIMMED .125 INCH OF MATERIAL FROM ALONG THE LOWER EDGE OF ALL THREE COVER PLATE SLOTS FOR THE LATCH TENONS OF THE COCKPIT DOOR. SYSTEM OPERATIONALLY CHECKS OK. THE EMERGENCY EGRESS PANEL WAS FOUND TO TAKE SOME EFFORT TO GET IT TO RELEASE, HOWEVER, THE PANEL DID RELEASE DURI2L72 4F RTA28NM 20030320000382003032000038NM 2003 3 20 USAASB03004 120030106A2131322684003 CONTROLLER BOEING737 7373B7 1384580NM CABIN PRESSURE FAILED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19374US37456 22953 PWM - FLT 1528 - EN ROUTE FROM PHL TO PWM, AT FL370, CREW REPORTED THE CABIN ALTITUDE GRADUALLY CLIMBED ABOVE 10,000 FEET. NO FAULT INDICATIONS WERE INDICATED ON PRESSURIZATION PANEL. CREW REGAINED CONTROL OF CABIN DURING DESCENT TO FL250 IN MANUAL AC MODE. FLIGHT CONTINUED ONTO PWM AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER (P/N 763810-1). FOUND THE FORWARD OUTFLOW VALVE WOULD NOT PASS OPERATIONAL TEST. REMOVED AND REPLACED FORWARD OUTFLOW VALVE. OPERATIONAL TEST GOOD PER MM 21-31-00. (M) 2L72 4F RTA16WE 20030320000392003032000039NM 2003 3 20 USAASB03007 120030113A3260189929 SENSOR BOEING737 737301 1384611NM RT MLG W/W OUT OF ADJUST A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19353US 23556 PIT - FLT 1228 - AFTER TAKEOFF FROM MKE, CREW WAS UNABLE TO RETRACT THE LANDING GEAR WITH NORMAL GEAR HANDLE MOVEMENT. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND USED THE LANDING GEAR OVERRIDE LEVER TO RAISE THE GEAR. FLIGHT CONTINUED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE S106 AIR/GROUND SENSOR OUT OF ADJUSTMENT. ADJUSTED S106 SENSOR PER MM 32-09-01-825-002. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030402000172003040200017NM 2003 4 2 03FDEA00334 120030313A5347S4929147 CARGO TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 MAIN DECK CARGO BAY DOORWAY FLOOR SEAT TRACK AT LT SIDE STA. 635, 27.5 INCHES FOUND CRACKED. CABIN STA 635, 27.5 INCHES, LT SIDE SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG.1, VOL.I. 2L73 4F RTA22WE 20030320000672003032000067NM 2003 3 20 03FDEA00336 120030319A5270BZ2RW8225551A2 SWITCH BOEING727 727200 138407ENM ZONE 800 FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25480FE 21462 MAIN CARGO DOOR LIGHT CAME ON INFLT . BOTH PACKS TURNED OFF . ALT 6000 FT PSI DIFF. 2.8 . LIGHT WENT OUT ONCE DEPRESS. COMPLIED WITH CHECKLIST RETURN TO MCO . OPERATED MCD OPEN/CLOSED SEVERAL TIMES. CLOSED DOOR AND PRESSURIZED A/C. WAS ABLE TO GET DOOR WARN RED TO COME ON WITH DOOR CLOSED AND BARBER POLE IN LINE. VISUALY INSPECTED AND CHECKED LOCKROD SWITCH AND ALL THE LATCH WARNING SWITCHES. MOST FWD LATCH SWITCH WAS CAUSING THE LIGHT TO COME ON WITH DOOR CLOSED. REPLACED AND ADJ FWD LATCH WARNING SWITCH. OPERATED DOOR OPEN/CLOSE SEVERAL TIMES. OPS CHECK OK. PRESSURIZED TO 3 PSID WITH NO MCD WARNING LIGHT. 2L73 4F RTA3WE 20030320000702003032000070SO 2003 3 20 LR7A03011 120030318A53203431947 STRUT LKHEED382 382G 526414USO FS 858 BROKEN A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 264 4763 DURING SCHEDULED A CHECK INSPECTION PER JOB CARD HA1200 FOUND LH FS 858 STRUT CRACKED AND BROKEN AT LBL 61, WL 190. INSPECTED FOR SECONDARY DAMAGE, NONE NOTED. AIRCRAFT FERRIED UNPRESSURIZED TO EGSC FOR REPAIR.AT EGSC REPAIRED STRUT IAW SRM SMP 583 53-50-25. MARSHALL NR 0001. 2H74 4T A1SO 20030320000852003032000085EU 2003 3 20 2003UALA00067 120030118A5270 TARGET AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMER EXIT DOOR OUT OF ADJUST A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29497UA 1847 CABIN EMERGENCY EXIT RIGHT AFT ECAM ILLUMINATED. ADJUSTED TARGET ON THE RIGHT AFT EMERGENCY EXIT DOOR. 2L72 4F4 FRTA28NM E40NE 20030121003402003012100340NM 2003 1 21 HNAA0300002 120030117A27202379003001 REGULATOR DHAV DHC8 DHC8201 2809001NM TAIL DEFECTIVE A HNAAO OTHER J WARNING INDICATION CRCRUISE 1 EA07966HA8510 8510 452 RUDDER PRESSURE AND FULL RUDDER PRESSURE CAUTION LIGHT ILLUMINATED IN FLIGHT. LIGHTS CAME ON ABOVE 140 KTS REMAINED ILLUMINATED TILL AIRSPEED WENT BELOW 140 KTS ON APROACH TO LAND. REPLACED RUDDER PRESSURE REGULATOR. 2H72 4T RTA13NM 20030122000052003012200005 2003 1 22 HEEA083392 420030109A34578143902240B GPS BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 GPS WILL NOT BOOT UP. 1G71 3U H2SW 20030122000122003012200012SW 2003 1 22 HEEA083399 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 MAIN BATTERY WEAK. SCRAPPED. 1G71 3U H2SW 20030122000272003012200027SW 2003 1 22 HEEA083414 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038593X356 51509 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000302003012200030SW 2003 1 22 HEEA083417 120030109A2432RG222 BATTERY BELL 206 206L4 1182110SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F352 52038 MAIN BATTERY WEAK. 1G71 3U NCH2SW 20030122000522003012200052SW 2003 1 22 HEEA083440 120030109A3212206050248107 FLOAT BELL 206 206B3 1181506SW EMERGENCY FLOAT LEAKING E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032268V 3605 EMERGENCY FLOAT BAG FAILED 10 YEAR INSPECTION AND LEAKED. 1G71 3U H2SW 20030122000582003012200058SW 2003 1 22 HEEA083446 120030109A3297MS24171D1 RELAY BELL 206 206B3 1181506SW MLG INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MLG RELAY INOPERATIVE. SCRAPPED. 1G71 3U H2SW 20030122000692003012200069 2003 1 22 HEEA083457 420030109A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMMS SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 MIXING BOX HAS A LOUD POPPING NOISE ON TRANSMIT AND RECEIVE. SHOP REPAIR. 1G71 3U H2SW 20030122000732003012200073SW 2003 1 22 HEEA083465 120030109A6300 BUSHING BELL 206 206L3 1182108SW DRIVE LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 DRIVE LINK HAS WORN BUSHINGS. REPAIRED. 1G71 3U H2SW 20030122000752003012200075 2003 1 22 HEEA083467 420030109A2330SA340STS SPEAKER BELL 206 206L3 1182108SW PA SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 PA SPEAKER CORRODED. SCRAPPED. 1G71 3U H2SW 20030122000782003012200078 2003 1 22 HEEA083470 420030110A2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 VHF TRANSCEIVER GARBLED. IN SHOP REPAIR. 1G72 4U H4SW 20030122000832003012200083 2003 1 22 HEEA083475 420030110A3452066107100 TRANSPONDER BELL 412 412 1182202SW ATC SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ATC TRANSPONDER WOULD NOT PRODUCE POWER OUT. IN SHOP REPAIR. 1G72 4U H4SW 20030122000852003012200085 2003 1 22 HEEA083477 420030110A2312066107800 RECEIVER BELL 412 412 1182202SW GLIDESLOPE WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 VERY WEAK GLIDESLOPE RECEIVER. IN SHOP REPAIR. 1G72 4U H4SW 20030122000882003012200088SW 2003 1 22 HEEA083480 120030110A2910212076006007 VALVE BELL 412 412 1182202SW HYD SYSTEM MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 HYDRAULIC PRESSURE READS 30 PSI WHEN AIRCRAFT NOT RUNNING. VALVE TO BE SENT TO VENDOR. 1G72 4U H4SW 20030122000952003012200095WP 2003 1 22 ZW0A0300901 120030119A335041B004AD0763 BATTERY DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13982TW 53632 EMERGENCY LIGHTING SYSTEM BATTERIES IN ROW 9 WERE INOPERATIVE. REPLACED FWD BATTERY PACK PER MM33-53-11. OPS CHECKED NORMAL PER MM33-59-00. CHECK-C 11-19-02-STL. --CLOSED-- 2L72 4F RTA6WE 20030122001022003012200102EU 2003 1 22 HEEA083489 120030107A717010593910 PRESSURE SWITCH BOLKMS105 BO105S 5626006EU NR 1 ENGNE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036607K S841 NR 1 ENGINE DIFFERENTIAL PRESSURE SWITCH LIGHT STAYS ON. 1G72 3U H3EU 20030122001202003012200120NM 2003 1 22 DL733030053 120030113A5753654643099 SKIN BOEING737 737347 1384647NM FORE FLAP DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307WA 23440 LEFT INBOARD FORE FLAP DISBONDED. REPAIRED PER ER/A 418180-14. 2L72 4F RTA16WE 20030122001442003012200144NM 2003 1 22 DL757030016 120030102A5315141N51231 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27610DL 22817 THE UPPER CAP OF THE FS 377 FLOORBEAM WAS FOUND CORRODED. THE UPPER CAP WAS TRIMMED OFF AND A NEW SECTION FABRICATED. DURING INSTALLATION OF THE NEW SECTION, SEVERAL ATTACH HOLES COMMON TO THE FS 377 FRAME AT LBL 65 WERE DAMAGED. THE AFFECTED HOLES WERE OVERSIZED, BUSHED, AND REPAIRED WITH AN ALUMINUM DOUBLER. THE REPAIRS WERE ACCOMPLISHED PER ER/A 384265-14, REV A. 2L72 4F RTA2NM 20030122001852003012200185NE 2003 1 22 HEEA083544 220030113A720030176003B ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE OVERHEATED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW032149S14685 36002 ENGINE TEMP WENT ABOVE 1006 DEGREES FOR 15 SEC. AFTER COMPRESSOR STALLED. IN SHOP REPAIR. 1G72 4U4 U H4SW E22EA 20030122001992003012200199GL 2003 1 22 HEEA083547 220030114A7200686404506 CLIP BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 CAE847043 ENGINE INNER CLIP RUSTED. SCRAPPED. 1G71 3U3 UO H2SW E1GL 20030122002022003012200202GL 2003 1 22 HEEA083549 220030114A7200686404606 CLIP BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 CAE847043 ENGINE OUTER CLIP RUSTED. SCRAPPED. 1G71 3U3 UO H2SW E1GL 20030122002042003012200204SW 2003 1 22 HEEA083550 120030113A6520212040452001 SLEEVE BELL 212 212 1181420SW T/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736D 31135 TAIL ROTOR GEARBOX SLEEVE IS CORRODED. 1G71 4U H4SW 20030122002072003012200207SW 2003 1 22 HEEA083552 120030113A6210214015300107 BLADE BELL 214 214ST 1182106SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N4317 28106 THE UPPER GRIP PAD HAS SOME SEPARATION AND THE LOWER EROSION SHIELD HAS SEPARATION ON MAIN ROTOR BLADES. 2G72 4U H10SW 20030122002102003012200210 2003 1 22 HEEA083555 420030113A2312069102435 RECEIVER BELL 206 206L3 1182108SW NAV/COMM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 RECEIVER CHANGES FREQUENCIES BY ITSELF. FOUND VOR/LOC DOESN'T RECEIVE. SWAPPED NAVIGATIONAL RECEIVER BOARD. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G71 3U H2SW 20030122002182003012200218 2003 1 22 HEEA083558 420030113A3422103002201 GYRO BELL 206 206L3 1182108SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03319E 51042 DIRCTIONAL GYRO PRECESSING. REPLACED GYRO. 1G71 3U H2SW 20030122002442003012200244SW 2003 1 22 HEEA083565 120030113A6320 BEARING BELL 206 206L3 1182108SW TRANS RESTRAINT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TRANSMISSON RESTAINT HAS WORN BEARINGS. REPAIRED. 1G71 3U H2SW 20030122002562003012200256SW 2003 1 22 HEEA083567 120030113A6320206033506103 BUSHING BELL 206 206L4 1182110SW XMSN RESTRAINT SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0362127 52023 RUBBER BUSHING SEPARATED ON MAIN ROTOR TRANSMISSION RESTAINT. 1G71 3U NCH2SW 20030122002602003012200260GL 2003 1 22 HEEA083570 220030113A73136899001 FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 ENGINE WOULD NOT START DUE TO FAILED FUEL NOZZLE. IN SHOP REPAIR. 1G71 3U3 U H2SW E4CE 20030122002612003012200261 2003 1 22 HEEA083571 420030113A3416D120P2T ANEROID BELL 206 206L3 1182108SW ALTIMETER FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 BAROMETRIC ANEROID SENDS AN ALTITUDE READING OF 27,600 FEET TO THE SKYWATCH AND THE TRANSPONDER WHILE ON THE GROUND. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030122002622003012200262 2003 1 22 HEEA083572 420030113A3452066106200 TRANSCEIVER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 FIRST TWO DIGITS ARE INCORRECT. FOUND UNIT ONLY HAD ABOUT 8 WATTS OUT AND MTL WEAK. COULD NOT ADJUST POWER OUT. REPLACED BAD V101 CAVITY, BAD L101 COIL, BAD R477 RESISTOR AND BAD PHOTOCELL. FOUND POWER OUT NOW GOOD AND MTL STILL WEAK. ALIGNED PRE SELECTOR AND IF SECTION AND ADJUSTED PULSE WIDTH AND FREQUENCY. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030122002722003012200272SO 2003 1 22 C2XA03CL020 120030120A4900M8324819042 PACKING EMB 135 EMB135ER 3260203SO APU LEAKING A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2727506 145206 FLIGHT#2848 THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WITH THE APU BLEED ON.MAINTENANCE RELEASED THE AIRCRAFT I/A/W MEL 49-00-00.MAINTENANCE INSPECTED AND REPLACED THE PACKING AND TEFLON RETAINER ON THE OUTLET OF THE APU MAIN FUEL SOLENOID VALVE.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030122002732003012200273NM 2003 1 22 AWXA200300054 120030119A3350BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 4 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW0 0 22654 PHX - EEL - DURING INSPECTION A WIRE WAS FOUND PULLED OUT OF SPLICE ON THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H. MAINTENANCE REPAIRED BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030123000182003012300018NM 2003 1 23 2003UALA00034 120030107A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29355UA 24361 AFT PIT RIGHT FRAME STATION 727C DENTED AT RBL 28. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED. 2L72 4F4 FRTA16WE E2GL 20030320000802003032000080NM 2003 3 20 2003UALA00046 120030112A361033990047U1 CONTROLLER BOEING757 757222 1384956NM PWA 2037 PW2037 NE ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29589UA 28707 726591 LEFT ENGINE BLEED PRESSURE REGULATING AND SHUTOFF VALVE FAILURE PRIOR TO ENTERING ETOPS ENVIRONMENT. SUPPLEMENTAL DATA UPDATE HIGH STAGE PILOT CONTROLLER FAILED. REPLACED HIGH STAGE PILOT CONTROLLER. 2L72 4F4 FRTA2NM E17NE 20030320000822003032000082NM 2003 3 20 2003UALA00050 120030111A3397 RELAY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHTSBURNED OUT A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29644UA 25094 FLOOR EMERGENCY LIGHTS ON LEFT SIDE OF COACH CYCLED ON AND OFF THREE TIMES WITH COCKPIT SWITCH IN ARMED POSITION. EMERGENCY LIGHTS ALT TRANSFER RELAY "K868" REQUIRES REPLACEMENT. REPLACED RELAY. 2L72 4F4 FRTA1NM E24NE 20030123000332003012300033NM 2003 1 23 2003UALA00054 120030114A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29951UA 26696 FORWARD NOSE STATION 188 LEFT FRAME OUTBOARD CHORD CRACKED IN RADIUS BELOW STRINGER 17 WEB. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED WEB ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030123000352003012300035NM 2003 1 23 2003UALA00056 120030114A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 STATION 680, CABIN FLOORBEAM UPPER CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. UPPER FLANGE REPAIRED WITH DOUBLER. 2L72 4F4 FRTA2NM E17NE 20030123000362003012300036NM 2003 1 23 2003UALA00057 120030114A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 STATION 660, LBL 46, FLOORBEAM IS CRACKED AT FLOOR SUPPORT ATTACH CLIP. MAJOR REPAIR ACCOMPLISHED AT FLOOR BEAM UPPER CAP. PERFORMED SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20030123000422003012300042NM 2003 1 23 03FDEA000034 120030115A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION ON FLOORBEAM, BS 1030 LBL 9 WL 208. REPAIRED IAW SRM. 2L73 4F4 FRTA3WE E2EA 20030123000552003012300055NM 2003 1 23 CALA0300018 120030122A5320 INTERCOSTAL BOEING737 737524 1384721NM STA 344-360 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914613 27326 INSPECTION FOUND CENTER FLOOR INTERCOSTAL AT CENTERLINE OF AIRCRAFT CRACKED IN TWO PLACES AT STA 344-360. THE CRACKS WERE 1" IN LENGTH. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030123000562003012300056NM 2003 1 23 CALA0300019 120030123A5512 SKIN BOEING737 7373Q8 1384670NM R/H HOR STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914383 26312 INSPECTION FOUND R/H HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED AT 42.5" INBOARD ON LOWER SURFACE. THE GOUGED AREA WAS REPAIRED IAW ECRA 5510-01656. 2L72 4F RTA16WE 20030123000572003012300057NM 2003 1 23 CALA0300020 120030123A5512 SKIN BOEING737 7373Q8 1384670NM HS STA 66.5 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914383 26312 INSPECTION FOUND R/H HORIZONTAL STABILIZER FIXED LEADING EDGE SKIN DENTED AT STA 66.5. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5510-01657. 2L72 4F RTA16WE 20030123000652003012300065NM 2003 1 23 P5CA0300725 120030114A5415321U2731 BRACE BOEING747 7472U3B 1384846NM #1 PYLON GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 NICK/GOUGE FOUND AT SAILBOAT AREA OF PYLON #1 DIAGONAL BRACE - LOCATED APPROX 10:00 O'CLOCK POSITION, 29" FROM FWD END AT ZONE 5. DAMAGED AREA BLEND-OUT CARRIED OUT - FINAL DIMENSION LENGTH 2.0, WIDTH 1.525, DEPTH 0.100. THESE FIGURES ARE WITHIN LIMITS PER BOEING SB 747-54-2198, FIG. 3, PG 42. AREA ROTOR-PEENED ALODINED & REPROTECTED. 2L74 4F RTA20WE 20030325000202003032500020NM 2003 3 25 AWXA200300131 120030127A5320146N5417 FLOOR SUPPORT BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT SCREW HOLE ON THE AFT CARGO COMPARTMENT FLOOR SUPPORT BS 1340, WL 148, RBL 2, STR 29 R/H. MAINTENANCE REMOVED CORRODED SECTION OF FLOOR SUPPORT BS 1340, WL 148, RBL 2, STR 29 RIGHT; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW SRM 51-70-11, PG. 1-7. 2L72 4F4 FRTA2NM A12EU 20030325000232003032500023NM 2003 3 25 AWXA200300138 120030127A5320143N52601 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION AND A .5000 INCH CRACK WAS FOUND ON FLOOR SUPPORT BS 1660 TO BS 1681, RBL 10. MAINTENANCE REMOVED FLOOR SUPPORT ANGLE FROM BS 1660 TO BS 1681, RBL 10; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT ANGLE IAW DWG 143N5260; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 11-12. 2L72 4F RTA2NM 20030325000592003032500059NM 2003 3 25 AWXA200300222 120030214A53106978163 BEAM BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-11 CHECK A 1 INCH CRACK WAS FOUND AT RT STRINGER 18A SHEAR BEAM WEB BS 727 ATTACHMENT. MAINTENANCE REMOVED DAMAGED SHEAR BEAM WEB AT BS 727 ATTACHMENT; FABRICATED A NEW REPLACEMENT SHEAR BEAM WEB PER DWG 65-46877; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030320000862003032000086NM 2003 3 20 2003UALA00069 120030119A5411 SPAR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29646UA 25283 NR 1 PYLON, AFT UPPER SPAR WEB, IS CRACKED AT CORNER OF FEED THROUGH CUT-OUT. MAJOR REPAIR ACCOMPLISHED W/DOUBLER AND STIFFENERS. 2L72 4F4 FRTA1NM E24NE 20030320000872003032000087NM 2003 3 20 2003UALA00071 120030119A2613355604310 OVERHEAT LOOP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT ENGINE SHORTED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29393UA 24668 FLIGHT DIVERTED AS THE RESULT OF A WING BODY OVERHEAT INDICATION ENROUTE. RIGHT WING BODY OVERHEAT DETECTION LIGHT CAME ON SHORTLY AFTER TAKEOFF. LIGHT FLICKERED OFF AND ON AND EVENTUALLY WENT OUT. AFTER APPROXIMATELY 10 MIN, OVERHEAT LIGHT CAME BACK ON. FOUND RIGHT ENGINE STRUT CAVITY OVERHEAT DETECTOR LOOP M488 WITH A HIGH RESISTANCE SHORTED TO GROUND. REPLACED OVERHEAT DETECTOR LOOP M488. 2L72 4F4 FRTA16WE E2GL 20030320000982003032000098NM 2003 3 20 2003UALA00089 120030122A3350 BATTERY PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29172UA 24363 A-ZONE IN SEAT ESCAPE PATH LIGHTING, LT SIDE, IS DIM. REPLACED BATTERY POWER PACK. 2L74 4F4 FRTA20WE E24NE 20030320001152003032000115NM 2003 3 20 DHL2003782003 120030320A3350 BATTERY BOEING727 727227 1384078NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01769AT 21998 1) COCKPIT AND MAIN ENTRY DOOR EMERGENCY LIGHT BATTERY INOPERATIVE. ILLUMINATION DROPS OFF IMMEDIATELY.2) REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES OVER COCKPIT AND MAIN ENTRY DOOR. OPS CHECKED GOOD IAW M/M 33-50. 2L73 4F A3WE 20030320001162003032000116WP 2003 3 20 DHL2003805005 120030319A2611 LAMP DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01805DH 46125 1) CONTROL CABIN #3 SMOKE DETECTOR WILL NOT TEST.2) REPLACED TEST LAMP IN #3 SMOKE DETECTOR. OPS CHECKED OK IAW M/M 26-16-0. 2L74 4F RT4A25 20030320001262003032000126NM 2003 3 20 2003UALA00117 120030129A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FRAME AT STATION 747 STRINGER 9R CRACKED AT RAIL SUPPORT CLIP. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001332003032000133NM 2003 3 20 2003UALA00124 120030131A2740AR6460M2MOD3 SERVO BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE STAB TRIM INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29358UA 24379 AIRCRAFT RETURNED TO FIELD WHEN STABILIZER TRIM LIGHT ILLUMINATED. REPLACED STABILIZER TRIM SERVO. NO FURTHER PROBLEMS NOTED AFTER REPLACEMENT. 2L72 4F4 FRTA16WE E2GL 20030320001342003032000134NM 2003 3 20 2003UALA00125 120030130A3350 INVERTER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29342UA 24246 EMERGENCY EXIT LIGHTING INOPERATIVE FROM ROW 15 TO THE REAR OF AIRCRAFT. REPLACED INVERTER AND POWER CABLE AT ROW 18, EEL LIGHTS OP CHECKED GOOD. 2L72 4F4 FRTA16WE E2GL 20030320001522003032000152NM 2003 3 20 2003UALA00146 120030205A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29952UA 26699 STATION 178 BULKHEAD WEB CRACKED AT WL 199 RBL 5.7 MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001532003032000153NM 2003 3 20 2003UALA00147 120030205A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN BODY STUB FRAME IS CRACKED BS 296 RT WL 257-277. MAJOR REPAIR ACCOMPLISHED. REPLACED STUB FRAME. 2L72 4F4 FRTA16WE E2GL 20030320001552003032000155NM 2003 3 20 2003UALA00149 120030206A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29952UA 26699 STATION 178 BULKHEAD WEB CRACKED AT WL 199 LBL 5.7. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001562003032000156NM 2003 3 20 2003UALA00150 120030206A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 STATION 616 WL 208 LT BODY FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030121003022003012100302EU 2003 1 21 03020316 120030120A33501317 LAMP JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 During preflight inspection, the crew reported that the aft exterior emergency exit light had one of two lamps inoperative. Maintenance personnel secured the forward lamp in the socket of the emergency exit light. The aircraft was returned to service. 2L72 4T RTA41NM 20030121003242003012100324 2003 1 21 HEEA083375 420030109A34215040017901 INDICATOR BELL 206 206L3 1182108SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ATTITUDE INDICATOR INDICATOR TUMBLES AND SPINS. REPAIRED. 1G71 3U H2SW 20030121003262003012100326 2003 1 21 HEEA083377 420030109A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 ADI WOULD NOT ERECT. REPAIRED. 1G71 3U H2SW 20030325000772003032500077NM 2003 3 25 AWXA200300243 120030228A5320654583475 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C-14 CHECK A 3/4 INCH CRACK WAS FOUND ON INTERCOSTAL BS 344, LBL 16. MAINTENANCE REMOVED DAMAGED INTERCOSTAL BS 344, LBL 16; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11, FIG. 12, PG. 15 & 38, FIG. 8, AND SRM 51-40-05, PG. 4, FIG. 2. 2L72 4F RTA16WE 20030326000172003032600017NM 2003 3 26 ANCF200300013 120030323A5270 WARNING LIGHT BOEING767 767259 1385136NM ACCESS DOOR ILLUMINATED W ANCFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO23985AN 24618 DURING T/O ROLL AT 80 KNOTS ACCESS DOORS LIGHT ILLUM STEADY. EICAS MSG E/E ACCESS DOOR DISPLAYED STEADY. T/O WAS REJECTED (90 KNOTS)CORRECTIVE ACTION: E/E ACCESS DOOR INDICATION WAS TRANSFERED TO DMI NO 406 MEL 52-71-1-8 CAT C AND MAINTENANCE PROCEDURE WAS ACCOMPLISHED. BRAKES ASSY WERE CHECKED BY T/O REJECTED AND WERE FOUND IN NORMAL CONDITION IAW AMM 05-51-14 FIG 201. 2L72 4F RTA1NM 20030326000232003032600023EU 2003 3 26 AUS20030115 120030203A3233HTE210014 ACTUATOR BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE MLG FAULTY W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) LANDING GEAR SELECTOR VALVE ACTUATOR SUSPECT FAULTY. 2H74 4F4 F A49EU E6NE 20030326001032003032600103NM 2003 3 26 2003UALA00307 120030320A5320 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 CABIN BODY FRAME STRINGER CLIP IS CRACKED BS685, STR 4R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20030327000012003032700001NM 2003 3 27 0300616306 120030305A2597 WIRE BOEING747 747451 1384940NM GALLEY BROKEN A NWAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NRNOT REPORTED 1 GL01666US 23821 DURING FLIGHT, FIRE FLASHED AT GALLEY 2C AFT COFFEEMAKER WHEN HOT PLATE WAS PULLED OUT. TURNED POWER OFF AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HOT PLATE WIRE BROKEN, REPLACED HOTPLATE. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030327000172003032700017EU 2003 3 27 AWXA200300284 120030301A5320D5347112320000 PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF HORIZONTAL WEB (SHEAR PLATE) FR 69 - FR 70, RBL 49. MAINTENANCE REMOVED CORRODED SHEAR PLATE FR 69 - FR 70, RBL 49; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 8-9. 2L72 4F RTA28NM 20030327000292003032700029EU 2003 3 27 AWXA200300301 120030313A5315D5347209800600 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM WHERE THE LT AFT FLIGHT ATTENDANT SEAT MOUNTS, (OUTBOARD FORWARD MOUNT) FR 66, LBL 35. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM FR 66, LBL 35; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-74-00, PG. 9, STEP 6, SRM 53-00-14, PG. 101, AND SRM 51-72-11, PG. 1 & 2. 2L72 4F RTA28NM 20030327000682003032700068NM 2003 3 27 C1HA200393002 120030201A2611 SMOKE DETECTOR BOEING727 727212 138407GNM LAVATORY INOPERATIVE A C1HAO OTHER L NO TEST NRNOT REPORTED 1 GL15293AS 21348 A/C AFT LAVATORY SMOKE DETECTION INOPERATIVE, OPS CHECK GOOD. COULD NOT DUPLICATE REPORTED PROBLEM. 2L73 4F A3WE 20030327000832003032700083SO 2003 3 27 C2XA02SH183 120030201A531014521700007 BEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727523 145389 DURING C-CHECK LT OMEGA BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A SPLICED REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327000902003032700090SO 2003 3 27 C2XA03BT011 120030120A273062351 STALL WARNING EMB 145 EMB145ER 3260211SO COCKPIT FAULTY A C2XAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW2714930 145011 CREW REPORTED, TAKEOFF CONFIGURATION WARNING ON TAKEOFF ROLL THROUGH 50 KNOTS, WITH AIRCRAFT IN PROPER CONFIGURATION. TAKEOFF ABORTED AND RETURNED TO GATE. MAINTENANCE PERFORMED TAKEOFF CONFIGURATION CHECK TEST IAW EMB145 AMM 31-51-00. OPS CHECKED GOOD. NO FAULTS FOUND AS PER FIM REFERENCE 31-51-00-810-804-A. ON NEXT TAKEOFF ATTEMPT CREW REPORTED, TAKEOFF CONFIGURATION WARNING ON TAKEOFF ROLL THROUGH 60 KNOTS WITH AIRCRAFT IN PROPER CONFIGURATION. MAINTENANCE REMOVED AND REPLACED STICK PUSHER IAW EMB145 AMM 27-36-04. OPS CHECKED GOOD. AIRCRAFT TEST FLOWN SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030327001022003032700102SO 2003 3 27 C2XA03CL015 120030119A326023092900001 UPLOCK EMB 145 EMB145ER 3260211SO NOSE GEAR DEFECTIVE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2715926 145005 CLE FLIGHT 2217 THE CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE NOSE GEAR UPLOCK BOX ASSEMBLY AND BOTH UPLOCK PROXIMITY SENSORS. OPERATIONAL CHECKS WERE GOOD. PROXIMITY SENSOR P/N 8-527-01 AND S/N'S OFF WERE 5105 AND15960. 2L72 4F RTT00011AT 20030327001062003032700106SO 2003 3 27 C2XA03CL022 120030123A3350110049 CHARGER EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714930 145011 DURING ROUTINE MAINTENANCE THE FORWARD RIGHT EMERGENCY EXTERIOR WING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001082003032700108SO 2003 3 27 C2XA03CL024 120030131A3232355022002 CONTROL UNIT EMB 145 EMB145ER 3260211SO COCKPIT FAILED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2715926 145005 CLE FLIGHT 2693 THE CREW REPORTED THE LT MAIN LANDING GEAR REQUIRED 3 CYCLES BEFORE LOCKING IN UP POSITION. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. ALSO REPLACED THE UPLOCK BOX ASSEMBLY ON THE LEFT GEAR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030317001002003031700100NM 2003 3 17 03FDEA00261 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 21R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F RTA22WE 20030317001032003031700103NM 2003 3 17 03FDEA00263 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 23R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030421000482003042100048EA 2003 4 21 SWIA200311809 120030221A3220 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA NLG ILLUMINATED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07591SW 7079 GEAR DISAGREE (NOSE WHEEL WOULD NOT COME UP). RECYCLED 4 TIMES, NO GOOD. RETURNED TO FIELD. SERVICE NOSE STRUT. PERFORMED GEAR SWING 8 TIMES. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20030421000512003042100051CE 2003 4 21 NSVA200300015 120030227A2120 SMOKE BEECH 1900 1900C 1154161CE COCKPIT DETECTED A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27119CJ UC19 DURING IN FLIGHT FUNCTIONAL CHECK-CREW NOTED SMOKE IN COCKPIT AND CABIN DURING CLIMB OUT FROM HEF. CREW TURNED OFF BLEED AND ENVIRON MODE TO OFF. APPROACH AND LANDING WAS UNEVENTFUL. MX PERFORMED COMP WASH, INSPECTED OIL FILTER, RAN ENGINE TO CHECK FOR ANY LEAKS. DURING RUN CHECKED BLEEDS AND HEAT FOR EXCESS OF 10 MIN. COULD NOT DUPLICATE. AIRCRAFT RELEASED. 2L72 4T RTA24CE 20030421000842003042100084NM 2003 4 21 DLM88030109 120030129A54145930645509 PANEL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 NACELLE SEPARATED A DALAO OTHER D INFLIGHT SEPARATION TXTAXI/GRND HDL 1 SO27960DL DL119 49979 718150 SECTION OF ACOUSTIC PANEL SEPARATED FROM INLET COWL OF NR 1 ENGINE. MINOR DAMAGE TO FAN BLADES. REPLACED INLET. 2L72 4F4 FRTA6WE E9NE 20030421000952003042100095NM 2003 4 21 DLM90030150 120030213A243024E508294G01 TRANSFORMER DOUG MD90 MD9030 3023690NM E/E BAY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27912DN 53392 WHILE RELOCATING THE A/C FROM THE PAD TO THE GATE, OPS REPORTED SMOKE/ODOR IN CABIN. DL MTC FOUND THE NR 1 T/R HAD FAILED AND SMOKED. INSULATION ABOVE THE T/R WAS BURNED. REPLACED T/R UNIT. 2L72 4F RTA6WE 20030421002162003042100216EA 2003 4 21 ASOA03110 120030314A493038834491 LINE CNDAIRCL600 CL6002B19 1900309EA APU FUEL SYS CHAFED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11820AS 7188 FLT 4463 - DUIRNG FLIGHT FROM MKE-ATL AND ON THE GROND, A FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN AFTER THE ENGINE WAS STARTED WITH THE BLEEDS ON THE AUXILIARY POWER UNIT OR THE ENGINE. MAINTENANCE REMOVED AND EPLACED A CHAFED FUEL LINE ON THE AUXILIARY POWER UNIT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000012003042200001CE 2003 4 22 2003F00228 120030205A2841 WARNING LIGHT CESSNA750 750 2076810CE WING TANK ACTIVATED A UG8AO OTHER N FALSE WARNING CLCLIMB 1 GL235113 7500013 VENTED FUEL OVERBOARD FROM RIGHT WING. 3240 NR INDICATED YELLOW CAS MESSAGE 'WING TANK OVERFILL RIGHT' ILLUMINATED. AIRCRAFT RATE OF CLIMB WAS 1000 FEET PER MINUTE. PERFORMED WING TANK REFUELING AND TRANSFER SHUTOFF OPERATIONAL CHECKS PER CESNA MM. NO DEFECTS NOTED ALL OPERATIONAL CHECKS ARE GOOD. RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4J RTT00007WI 20030422000032003042200003EU 2003 4 22 USAABA03006 120030218A261237000202 FIRE DETECTOR AIRBUS330 A330323 3930335EU NR 1 ENGINE MALFUNCTIONED A USAAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 EA19673UW13309 0337 PHL - FLT 3 - UPON LANDING AT PHL AND APPLYING REVERSE THRUST, THE CREW RECEIVED A FIRE WARNING ON THE LEFT ENGINE. CREW ACTIVATED BOTH FIRE BOTTLES. WITH ENGINE OUT OF REVERSE, THE FIRE WARNING CEASED. NO EVIDENCE OF ACTUAL FIRE WAS FOUND. MAINTENANCE REPLACED THR NR 1 ENGINE FIRE DETECTION UNIT. (M) 2L72 4F RTA46NM 20030422000092003042200009EU 2003 4 22 USAASA03018 120030220A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU PAX CABIN MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW 0936 DCA - WHEN THE 'NO SMK/PED' SWITCH IS TURNED OFF, THE RIGHT OVERWING EXIT SIGN AND OVERHEAD EMERGENCY LIGHTS FLASH ON AND OFF INTERMITTENTLY. WHEN THE 'NO SMK/PED' SWITCH IS TURNED ON, THE RIGHT EXIT LEFT OVERWING SIGN IS OFF. MAINTENANCE REPLACED THE RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030422000112003042200011EA 2003 4 22 ASOA03063 120030217A493038834491 LINE CNDAIRCL600 CL6002B19 1900309EA APU FUEL SYS LOOSE A ASOAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11915EV 7754 FLT 4628 - DURING TAKEOFF FROM VLV-ATL, A FUEL ODOR OCCURRED PRIMARILY IN THE COCKPIT WITH A SLIGHT ODOR IN THE GALLEY. THE ODOR DISSIPATED DURING FLIGHT AND REAPPEARED DURING LANDIING ROLL OUT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE TIGHTENED A LEAKING FUEL LINE ON THE AUXILIARY POWER UNIT. OPERAIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000132003042200013EA 2003 4 22 ASOA03085 120030301A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11901EV 7616 FLT 4414 - DURING A GROUND INSPECTION AT MGM, THE NR 1 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000162003042200016EA 2003 4 22 ASOA03077 120030222A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11914EV 7752 FLT 4769 - DURNG APPROACH INTO ILM FROM ATL, THE CREW EXPERIENCED A FLAPS FAILURE WHEN SELECTED AT 20 DEGREES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ILM. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT AND RE-RIGGED THE FLAP SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000192003042200019WP 2003 4 22 GTIA030123 120030223A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND MAIN CABIN STATION 1117 TO STATION 1174 FLOOR PANEL DELAMINATING. FABRICATED REPLACEMENT FLOOR PANEL. (M) 2L72 4F RTA6WE 20030327001222003032700122SO 2003 3 27 C2XA03CL052 120030225A21508166011 VALVE EMB 145 EMB145LR 3260212SO NR 2 ENGINE INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2712922 145338 LCH FLIGHT 2218 THE CREW REPORTED NR 2 PACK CREATED SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE NR 2 HIGH STAGE VALVE WOULD NOT OPEN. THE HIGH STAGE BLEED VALVE AND THE PRESSURE SWITCH WERE REPLACED. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001232003032700123SO 2003 3 27 C2XA03CL055 120030226A335066368 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2722971 145149 DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHTING WAS FOUND INOPERATIVE AT ROW 8. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP AT ROW 8. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001262003032700126SO 2003 3 27 C2XA03CL060 120030226A335066367 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST NRNOT REPORTED 1 SW2717928 145007 CLE FLIGHT 2101 THE CREW REPORTED HALF OF THE EMERGENCY AISLE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED NR 2 AND NR 3 EMERGENCY AISLE PATH LIGHT STRIPS. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030122000042003012200004 2003 1 22 HEEA083391 420030109A3457 FACEPLATE BELL 206 206L1 1182107SW GPS SYSTEM MISSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035000K 9016131 45167 GPS FACEPLATE MISSING. 1G71 3U H2SW 20030122000162003012200016SW 2003 1 22 HEEA083403 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610C451 51425 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000182003012200018SW 2003 1 22 HEEA083405 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497513 51518 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000252003012200025SW 2003 1 22 HEEA083412 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH704 51303 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000262003012200026SW 2003 1 22 HEEA083413 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128423 51134 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000372003012200037SW 2003 1 22 HEEA083424 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034282Z227 51499 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000442003012200044SW 2003 1 22 HEEA083431 120030109A3340A490A POWER SUPPLY BELL 206 206L3 1182108SW STROBE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 ANTI COLLISION LIGHT POWER SUPPLY INOPERATIVE. SCRAPPED. 1G71 3U H2SW 20030122000462003012200046 2003 1 22 HEEA083433 420030109A2300CIX100LVHGK374 RECEPTACLE BELL 206 206L3 1182108SW COMMS HEADSET BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 RECEPTACLE FOR HEADSET BROKEN. REPLACED. 1G71 3U H2SW 20030122000482003012200048 2003 1 22 HEEA083436 420030109A3140DPUA0101 COMPUTER BELL 206 206L3 1182108SW INTELLASTART PROFAILED E O OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 QUIT COMMUNICATING DURING DOWNLOAD. IN REPAIR. 1G71 3U H2SW 20030122000502003012200050 2003 1 22 HEEA083438 420030109A3140 BATTERY BELL 206 206L3 1182108SW COMPUTER DISCHARGED E O OTHER O OTHER NRNOT REPORTED 1 SW033116L 0351 51529 INTELLASTART PROCESSOR INTERNAL BATTERY VOLTAGE DROPPED TO .41 VOLTS. 1G71 3U H2SW 20030122000542003012200054 2003 1 22 HEEA083442 420030109A2300H1036 HEADSET BELL 206 206L3 1182108SW COMMS SYSTEM BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 COMMS SYSTEM HEADSET MIC BROKEN. REPLACED HEADSET. 1G71 3U H2SW 20030122000602003012200060SW 2003 1 22 HEEA083448 120030109A3297MS24171D1 RELAY BELL 206 206B3 1181506SW MLG INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MLG RELAY INOPERATIVE. SCRAPPED. 1G71 3U H2SW 20030122000632003012200063SW 2003 1 22 HEEA083451 120030109A1430M45932114A INSERT BELL 206 206B3 1181506SW OIL COOLER PAN DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 ONE THREADED INSERT FOR THE OIL COOLER PAN IS DAMAGED AND CANNOT INSTALL THE BOLT INTO IT. REPAIRED. 1G71 3U H2SW 20030122000712003012200071 2003 1 22 HEEA083459 420030109A2312PHI003000001 AMPLIFIER BELL 206 206L3 1182108SW ICS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 CABIN ICS AMP UNABLE TO ADJUST VOLUME. SHOP REPAIR. 1G71 3U H2SW 20030122000762003012200076SW 2003 1 22 HEEA083468 120030109A2430SM20ACD200A21 RELAY BELL 206 206L3 1182108SW DC SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 RELAY STUD STRIPPED OUT. 1G71 3U H2SW 20030122000772003012200077 2003 1 22 HEEA083469 420030110A2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 VHF TRANSCEIVER GARBLED. IN SHOP REPAIR. 1G72 4U H4SW 20030317001042003031700104NM 2003 3 17 03FDEA00264 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 24R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001092003031700109NM 2003 3 17 03FDEA00268 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 28R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.COMPLIED WITH FEDEX EA 1-5510-67579. 2L73 4F RTA22WE 20030317001192003031700119NM 2003 3 17 03FDEA00278 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 13R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579. 2L73 4F RTA22WE 20030317001202003031700120NM 2003 3 17 03FDEA00279 120030306A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 320 LBL 46. FOUND UPPER LOBE OF FLOOR BEAM AT BS 320 LBL-46 TO BE OUT OF LIMITS. REPAIRED FLOOR BEAM AT BS 320 LBL-46 IAW FED EX E.A. 7-5310-69427A. 2L73 4F RTA3WE 20030317001242003031700124EU 2003 3 17 DHL2003367505 120030226A5101UNK ANGLE AIRBUS300 A300B4203 3930306EU CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R: 0029420:Fwd. pit sub floor area R/H side Sta. 2029 BL55R upper floor support angle upper surface corrosion. Corrective action:Removed fastners IAW A300 SRM 51-30-30,removed corrosion floor support angle IAW A300 SRM 51-40-11. Material thickness .125 material removed .002 found to be within limits IAW A300 SRM 51-10-00. Applied alodine and primer IAW A300 SRM 51-40-11. Reinstalled fastners IAW A300 SRM 51-30-30 2L72 4F RTA35EU 20030317001302003031700130NM 2003 3 17 03FDEA00293 120030310A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 MECHANICAL DAMAGE ON SKIN BS 1066, STR 27R AT EDGE OF FASTENER HOLE. DAMAGE ON SKIN REPAIRED PER SRM 53-03-03 FIG 3. 2L73 4F RTA3WE 20030317001362003031700136NM 2003 3 17 03FDEA00300 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 580 BETWEEN STR 24L AND 25L. 2L73 4F RTA3WE 20030317001462003031700146NM 2003 3 17 03FDEA00309 120030312A2613 CLAMP BOEING727 727200 138407ENM NR 3 ENG NACELLELOOSE A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25220FE 20934 1 HR INTO FLIGHT SELECTED ENGINE THEN WING A/I (FL310 .82M) ALMOST INMEDIATELY ENG 3 STRUT OVERHEAT LIGHT ILLUMINATED. NO CHANGE AFTER QRH PROCEDURES ACCOMPLISHED. NR 3 ENGINE SHUTDOWN AS PER QRH . LIGHT REMAINED ILLUMINATED FOR 5 MORE MINUTES, THEN EXTINGUISHED , NO OTHER PROBLEM NOTED. FOUND CLAMP MISPLACED AT ENGINE NACELLE ANTI-ICE DUCT AT FWD STUD WIND, REINSTALLED CLAMP PROPERLY, CKD OK NOW. 2L73 4F RTA3WE 20030317001472003031700147NM 2003 3 17 03FDEA00310 120030312A5230 SKIN BOEING727 727200 138407ENM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 NR 3 AFT LOWER CARGO DOOR INTERNAL SKIN CRACKED BETWEEN 2 LIGHTNING HOLES 8 INCHES FROM FWD EDGE, 5 INCHES FROM LOWER EDGE. 2L73 4F RTA3WE 20030317001482003031700148EU 2003 3 17 03FDEA00312 120030313A5510A5517860720000 BRACKET AIRBUS310 A310 EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 LT HORZONTAL STABILIZER LEADING EDGE ATTACH APRON IS HEAVILY CORRODED AT AFT UPPER "L" ANGLE. REMOVED AND REPLACED WITH ON SITE FABBRICATED PARTS. 2L72 4F RTA35EU 20030317001502003031700150NM 2003 3 17 03FDEA00314 120030227A5753 FLAP TRACK DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING INBOARD FLAP TRACK ATTACH POINTS 2 EA FOUND WITH CORROSION. 2L73 4F RTA22WE 20030317001512003031700151NM 2003 3 17 03FDEA00315 120030227A5753 FLAP TRACK DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING INBOARD FLAP TRACK AFT ATTACH POINT WITH 1 EA HOLE CORRODED. 2L73 4F RTA22WE 20030317001602003031700160NE 2003 3 17 048029 220030219A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT LEAKING A AMWAC ABORTED TAKEOFF K FLUID LOSS TXTAXI/GRND HDL 1 CE07143YV109 109 UE143 114051 ON FLIGHT 5427 FROM SHREVEPORT LOUISIANA TO NEW ORLEANS LOUISIANA, UPON TAKE OFF ROLL AT 60-70 KIAS, THE TORQUE SURGED TO MAXIMUM. THE LEFT PROP RPM DROPPED TO APPROXIMATELY 1000-1200 RPM. THE TAKE OFF WAS ABORTED. THE CREW RETURNED THE THE GATE WHERE MAINTENANCE DISCOVERED OIL LEAKING OFF THE ENGINE. THERE WAS NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE POWER SECTION WITH ANOTHER ONE. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T4 TRTA24CE E26NE 20030318000042003031800004NM 2003 3 18 SWAA030584 120030314A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030318000122003031800012 2003 3 18 BAQA084698 420030224A3432066304605 CONTROLLER AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL HSI BROKEN H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01941MS 5495 BACK OF CONNECTOR ON HSI IS BROKEN. BROKEN AT TIME OF RECEIVING. 1G72 3U3 U H11EU E4CE 20030327001292003032700129SO 2003 3 27 C2XA03CL066 120030310A32347455501 LEVER EMB 145 EMB145ER 3260211SO MLG INTERMITTENT A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2717507 145215 CLE FLIGHT 2846 THE CREW REPORTED AFTER GEAR RETRACTION RECEIVED A MASTER WARNING AND LANDING GEAR LEVER DISAGREE MESSAGE. THE MESSAGE CLEARED WITHIN 10 SECONDS. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030326001002003032600100NM 2003 3 26 2003UALA00304 120030319A5411 FRAME BOEING777 777222 1385219NM PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29206UA 30212 NR 2 PYLON AFT LOWER INBOARD FRAME CRACKED BELOW PANEL 444 DL. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME. 2L72 4F RTT0001SE 20030327000692003032700069NM 2003 3 27 C1HA200393003 120030214A3260 CONNECTOR BOEING727 727212 138407GNM MLG CONTAMINATED A C1HAO OTHER N FALSE WARNING DEDESCENT 1 GL15293AS 21348 DURING GEAR EXTENSION RT MLG DOOR WAS SLOW TO ILLUMINATE, BUT CAM ON MOMENTARILY AND THEN OUT NORMALLY. NORMAL INDICATION ON PILOT FRONT PANEL FOUND CONNECTOR PLUG CONTANIMATED CLEANUP CONNECTOR PLUG CYCLE DOOR SEVERAL TIMES OPS CHECKED GOOD 2L73 4F A3WE 20030327000722003032700072NE 2003 3 27 C1HA200394005 220030202A7230 COMPRESSOR BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A C1HAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 GL15294AS 22146 DURING TAXI, ENGINE NR 2 EXPERIENCED A COMPRESSOR STALL/ PERFORMED COM 2.72.13. INSPECTED NR 2 ENGINE INLET & EXHAUST PER P&W MM 72-00-00 NO DEFECTS NOTED. OPERATED ENGINE TO 1.85 EPR. ALL PARAMETERS NORMAL. 2L73 4F4 F A3WE E2EA 20030327000732003032700073NM 2003 3 27 C1HA200395006 120030224A3260 ACCESSORY UNIT BOEING727 727290 138408WNM MLG MALFUNCTIONED A C1HAO OTHER N FALSE WARNING DEDESCENT 1 GL15295AS 22147 WHEN EXTENDING LANDING GEAR INTO MSP WE HAD 3 DOWN AND GREEN INITIALLY UNTIL SHORT FINAL, RECEIVED A RED NOSE WHEEL LIGHT AND A HORN CYCLED GEAR. RAN CHECK LIST WITH ONLY 2 MAIN GEAR NORMAL AND ONLY A RED NOSE GEAR LIGHT. R & R LANDING GEAR ASSY UNIT . TEST IS GOOD IAW MM 32-09-121 ALSO JACKED AND CYCLED NOSE GEAR NUMEROUS TIMES SYSTEM OPS CHECKS GOOD OK FOR SERVICE 2L73 4F A3WE 20030327000932003032700093SO 2003 3 27 C2XA03BT040 120030316A3240429513 CONTROL UNIT EMB 145 EMB145ER 3260211SO BRAKE SYSTEM FAILED A C2XAO OTHER J WARNING INDICATION LDLANDING 1 SW2713929 009 EWR "BRK OUTBOARD FAIL" DURING ROLLOUT. REMOVED AND REPLACED BRAKE CONTROL UNIT OPS CHECK IAW EMB145MM 32-41-02 GOOD. 2L72 4F RTT00011AT 20030327000992003032700099SO 2003 3 27 C2XA03CL005 120030102A326023092900001 UPLOCK EMB 145 EMB145 3260210SO NLG DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713956 145078 BNA FLIGHT 3372 THE CREW REPORTED THE NOSE GEAR WOULD NOT STAY RETRACTED AFTER TAKEOFF FROM BNA. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK BOX ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001422003032700142SO 2003 3 27 C2XA03IA009 120030127A325014553688402 SWITCH EMB 145 EMB145LR 3260212SO MLG YOKE STUCK A C2XAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW2714993 145289 ON TAKEOFF ROLL THE CREW NOTED A STEERING INOP MESSAGE. ABORTED THE TAKEOFF. MAINTENANCE CYCLED THE DISCONNECT SWITCH, PERFORMED AN OPERATIONAL CHECK OF THE NOSE WHEEL STEERING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001432003032700143SO 2003 3 27 C2XA03IA010 120030128A27503632001003 DRIVE UNIT EMB 135 EMB135LR 3260305SO TE FLAPS INOPERATIVE A C2XAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW2712530 145533 FLIGHT 2717, AFTER TAKEOFF THE CREW NOTED THAT THE FLAPS FAIL MESSAGE APPEARED AND THE FLAPS DO NOT MOVE. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT, PERFORMED A OPERATIONAL CHECK OF THE FLAPS, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327001882003032700188CE 2003 3 27 CA030210003 120030113A56105111604202 WINDSHIELD CESSNA421 421A 2076012CE CONT O520 GTSIO520D 17032SO MCAULY3AF34C3AF34C92 GL COCKPIT FAILED W BA EMER. DESCENT UNSCHED LANDING DW INFLIGHT SEPARATION INADEQUATE Q C CLCLIMB 1 CA (CAN) WHILE CLIMBING TO FL190, AT APPROXIMATELY FL180 THE COPILOTS WINDSCREEN DEPARTED THE AIRCRAFT RESULTING IN INSTANTANEOUS DECOMPRESSION. OTHER COCKPIT ITEMS ALSO DEPARTED IE, GLARE SHIELD, SUN VISOR DOCUMENTS ETC. AIRCRAFT EMERGENCY DESCENDED TO FL110, RE-ESTABLISHED COMMUNICATION AND LEVEL FLIGHT. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER PROBLEMS. BOTH FRONT WINDSCREENS BEING REPLACED WITH NEW UNITS. OTHER ITEMS BEING INSPECTED AND TESTED PRIOR TO RETURN TO SERVICE. 1L72 3O3 O A7CE E7CE 5 CP22EA 20040223000012004022300001CE 2004 2 23 5300121903 120031218A273155657562 TRIM SYSTEM CESSNA560 560XL 2076702CE ELEVATOR BROKEN E S4WACD ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 WP07613GY713 5605300 AIRCRAFT TOOK EXCESSIVE NOSE DOWN PITCH TRIM ON TAKEOFF AND IN FLIGHT. 2L72 4F RTA22CE 20040223000062004022300006WP 2004 2 23 2003121 120031209A6420NAS561C514 ROLL PIN HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL M/R HUB LOOSE B LS1RO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA13369AW14 0658 470117D CAE830571 PILOT COMPLAINED OF NOISE AND VIBRATION ON SHUT DOWN. INSPECTED MAIN ROTOR HUB, FOUND ROLL PINS ON DROOP STOP FOLLOWER ASSEMBLIES HAD BACKED OUT AND WERE CONTACTING THE LOWER SHOE. THE INTERFERENCE WAS CAUSING THE FOLLOWERS TO BE FROZEN IN PLACE. WHEN THE AIRCRAFT WAS SHUT DOWN AND THE ROTOR BLADES CONTACTED THE ROLLERS. THEY ONLY APPLIED A FORCE TO A FROZEN ITEM. THIS MADE A VERY LOUD NOISE, ALL FOLLOWERS AND BUSHINGS WERE REPLACED AND MFG WAS NOTIFIED. 1G71 3U3 U H3WE E4CE 20040322002042004032200204GL 2004 3 22 ERAA092661 220031126A7200250C20B ENGINE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL MAKING METAL B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03152EH13384 S701 ENGINE MAKING METAL. FOUND GEARS IN GEARBOX BREAKING DOWN. 1G72 3U3 U H3EU E4CE 20040323000362004032300036EU 2004 3 23 BAQA092755 120030908A670041800666100 ACTUATOR AEROSPAS365 AS365N2 8680815EU YAW TRIM ACT INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME7084 6417 YAW KICKS INTERMITTENTLY. REPLACED WITH SERVICEABLE ASSET UNIT. 02/17/2004 1G72 3U RTH10EU 20040324000272004032400027WP 2004 3 24 ASAA0380723 120031111A53219936537505 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FLIGHT COMPARTMENT FLOOR PANEL AT FS 158 HAS CORRODED FASTENERS AND WASHERS. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20030122000802003012200080 2003 1 22 HEEA083472 420030110A3416066104800 ALTIMETER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ALTIMETER INDICATOR INOPERATIVE. IN SHOP REPAIR. 1G72 4U H4SW 20030122000902003012200090SW 2003 1 22 HEEA083482 120030110A6230 SEAL BELL 407 407 1182206SW M/R MAST ASSY LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03493PH1134 BP23 53393 MAST SEAL LEAKS. REPLACED SEAL PN 537855 DUE TO WORN AND PN 406040090103 NUT DUE TO GROOVED SEAL AREA. 1G71 3U O H2SW 20030122000982003012200098EU 2003 1 22 HEEA083486 120030107A6420 BEARING BOLKMS105 BO105S 5626006EU T/R PITCH LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037170D S840 TAIL ROTOR PITCH LINK BEARINGS WORN. REPLACED BEARINGS (2 EA) 113943P AND (2 EA) 116488P. 1G72 3U H3EU 20030122001042003012200104EU 2003 1 22 HEEA083490 120030107A2435230321692 DRIVE SHAFT BOLKMS117 BK117A1 5626010EU STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RZ 18200 7092 STARTER GEN DRIVESHAFT SPLINES WORN. REPLACED DRIVESHAFT. 1G72 3U H13EU 20030122001082003012200108GL 2003 1 22 HEEA083492 220030107A7321252464431 FUEL CONTROL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 1 ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 NR 1 ENGINE SLOW TO ACCELERATE FROM 30 PERCENT THROUGH 50 PERCENT RANGE AND NO ADJUSTMENT LEFT. IN SHOP REPAIR. 1G72 3U3 U H3EU E4CE 20030122001142003012200114EU 2003 1 22 HEEA083496 120030107A3340A413A POWER SUPPLY BOLKMS105 BO105S 5626006EU STROBE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 ANTI COLLISION LIGHT POWER SUPPLY INOPERATIVE. REPLACED WITH SERVICEABLE POWER SUPPLY. 1G72 3U H3EU 20030122001182003012200118NM 2003 1 22 DL733030030 120030106A1430 ROD BOLT BOEING737 7373B7 1384580NM L1 DOOR MISSING A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27951WP 22951 L1 DOOR WOULD NOT OPEN FROM EITHER INSIDE OR OUTSIDE. FOUND LOWER LATCH AND GATE CONTROL ROD BOLT MISSING. INSTALLED CONTROL ROD BOLT. RE- INSTALLED TRIM AND SLIDE, DROPS CKS NORMAL. 2L72 4F RTA16WE 20030122001212003012200121NM 2003 1 22 DL738030050 120030112A256061020 BATTERY BOEING737 737832 13844CFNM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO273764D 30818 FC FLT ATTENDANT EMERG FLASHLIGHT INOP. REPLACED BATTERY. 2L72 4F RTA16WE 20030122001222003012200122NM 2003 1 22 751PA0009 120030119A3350 BULB BOEING757 757200 1384950NM A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 Bulb inop in R1 emergency light. Found bulb loose in socket. Re-installed. Ops chk. good. 2L72 4F RTA2NM 20030122001262003012200126NE 2003 1 22 DL73K030007 220030102A7230 BLADE BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE DAMAGED A DALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO27379DL46482 23606 709195 ON CLIMBOUT FROM BDL PASSING THROUGH FL6000 HEARD AND FELT A LOUD EXPLOSION FROM AREA OF THE FORWARD CARGO NR 2 ENG. DIVERTED TO JFK, THE STALL NOISE WAS AUDIBLE FROM COCKPIT BUT ENGINE INST WERE NORMAL ON BOTH ENGINES. FOUND 5 FAN BLADES CURLED AT TIP. BLENDED ALL BLADES AS REQUIRED, PER AMM 72-00. ALL BLADES ARE WITHIN CONTINUE IN SVC LIMITS EXCEPT FOR 2. THE 2 BLADES ARE WITHIN THE 5 CYC LIMITS. PERFORMED BORESCOPE PER AMM 72-00. CLOSED COWLS. PERFORMED T/O PWR R/U. NO VIBS FELT. ALL OPS. 2L72 4F4 F A16WE E2EA 20030122001312003012200131NM 2003 1 22 751PA0010 120030109A3350GE767 LIGHT BOEING757 757200 1384950NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 BULB INOP IN L1 EMERGENCY LIGHT. REMOVED AND REPLACED LIGHT BULB. OPS CHK. GOOD. 2L72 4F RTA2NM 20030122001422003012200142EU 2003 1 22 HEEA083502 120030107A5350350A54107902 DUCT AEROSPAS355 AS355* EU AIR INLET CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH 3248 AIR INLET DUCT CRACKED. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030122001472003012200147NM 2003 1 22 DL757030033 120030103A5420112N70092 FITTING BOEING757 757232 1384965NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27610DL 22817 DURING ACCOMPLISHMENT OF EO 6-75079-3 OPN 0206, A CRACK WAS FOUND IN THE RIGHT WING UPPER LINK WING FITTING OUTBOARD LUG. REPAIRED PER ER/A 389433-14. BORE OVERSIZED AND OVERSIZED BUSHING INSTALLED. 2L72 4F RTA2NM 20030122001492003012200149 2003 1 22 HEEA083534 420030113A2312064102300 TRANSCEIVER SKRSKYS76 S76A 8143006NE VHF SYSTEM WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 VHF TRANSCIEVER WEAK TO RECEIVE. REMOVED CORROSION FROM CHASSIS. FOUND RECEIVER WEAK AND HAD HIGH PITCH NOISE. REPLACED C368 CAPACITOR. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G72 3U H1NE 20030122001502003012200150NE 2003 1 22 HEEA083535 120030113A64107610105101042 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K5827 760082 TAIL ROTOR BLADE TRAILING EDGE OF PADDLE "A" IS SPLIT OPEN. TO BE SENT TO VENDOR FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20040324000192004032400019WP 2004 3 24 ASAA0380709 120031103A5347593054790 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED, EXFOLIATED, AT FS 220. REPLACED DAMAGED TRACK PER SRM 53-05, 53-20-1 AND 51-30-1. (M) 2L72 4F RTA6WE 20040329000192004032900019WP 2004 3 29 ASAA0380388 120030421A5320593666063 ATTACH ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND AFT CARGO AREA ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE PER SRM. (M) 2L72 4F A6WE 20040329000302004032900030NM 2004 3 29 USAASB03220 120031223A2150 SWITCH BOEING737 737301 1384611NM LT A/C PACK FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19353US 23556 PHL - FLT 579 - AFTER TAKEOFF FROM PHL, EN ROUTE TO IND, RT PACK WOULD NOT PRESSURIZE THE AIRCRAFT. LT PACK WAS ALREADY ON MEL 21-1A. CAPTAIN ELECTED TO RETURN TO FIELD AT PHL. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINTENANCE OPERATIONALLY CHECKED AIR CONDITIONING AND PRESSURIZATION SYSTEMS. NO FAULTS FOUND. R/R LT PACK AIR CYCLE MACHINE 210 DEGREE TURBINE INLET OVERHEAT SWITCH, P/N 1173T12-1, AND THE 250 DEGREE DUCT OVERHEAT SWITCH, P/N 1173T212. OPERATIONAL CHECK GOOD. PERFORMED SINGLE PACK CONFIDENCE CHECK AND HULL LEAK DOWN CHECK. BOTH LEFT AND RIGHT PACKS AND HULL LEAK DOWN CHECK GOOD. NO FAULTS FOUND ON RIGHT PACK. CLEARED MEL 21-1A. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20040329000332004032900033NM 2004 3 29 USAASB03222 120031226A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19425US 23992 CLT - MAINTENANCE REPORTED THE INTERIOR EMERGENCY EXIT MARKER LIGHT AT SEAT ROW 11 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040329000412004032900041WP 2004 3 29 ASAA0380396 120030421A5320993666411 CHANNEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL CENTER POST HAS CORROSION JUST BELOW FLOOR LEVEL AT STRINGER 30L. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040329000452004032900045NM 2004 3 29 ASAA0340319 120030725A534069773083 FITTING BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND LAV ATTACH FITTING CORRODED ON FLOORBEAM AT STATION 947.5 AND WL 208. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040329000502004032900050WP 2004 3 29 ASAA0380381 120030421A53205936597505 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT IN AFT CARGO BAY AT FS 1156 IS CORRODED. REPLACED SUPPORT PER SRM 51-10-4. (M) 2L72 4F A6WE 20040329001332004032900133NE 2004 3 29 CX7A194J0360 220031129A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT MAKING METAL A CX7AO OTHER O OTHER NRNOT REPORTED 1 GL03307CE 340B204 785365 LEFT ENGINE MAKING METAL. 2L72 4T4 TRTA52EU E8NE 20030716000082003071600008WP 2003 7 16 GTIA030453 120030616A3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23826NK 49391 ON TAKEOFF FROM MYR, THE NOSE GEAR RED LIGHT STAYED ON. CYCLED GEAR LIGHT WENT OUT. RESHIMMED NOSE GEAR UP/DOWN AND LOCKED POSITION PROXIMITY SENSOR. SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20030716000102003071600010WP 2003 7 16 GTIA030456 120030512A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND CABIN FS 815 LEFT MID FLOOR PANEL HAS BROKEN INSERT AND MISSING SCREW. FABRICATED NEW PANEL. (M) 2L72 4F A6WE 20030716000562003071600056WP 2003 7 16 GTIA030463 120030519A5330 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT CARGO INNER DOUBLER CORRODED FS 1174 BELOW STRINGER 18L. REMOVED LONGERON 19L. REMOVED DAMAGED AREA. FABRICATED DOUBLER, TRIPLER AND FILLER. INSTALLED FASTENERS IN DOUBLER AND TRIPLER FROM L18L UPPER FLANGE TO L17L STATION 1168 TO 1180. INSTALLED FASTENERS IN DOUBLER AND TRIPLER FROM L18 LOWER FLANGE TO L18L STA 1168 TO 1180. FABRICATED 15 LONGERON SPLICE. INSTALLED L19L FROM STATION 1146-1203 AND LONGERON SPLICE. (M) 2L72 4F A6WE 20030716000962003071600096EU 2003 7 16 HE66087953 120030709A6340 NEEDLE BOLKMS105 BO105LSA1 5626021EU TRIPLE TACH STUCK B HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03202LF 028 2014 TRIPLE TACH NEEDLES WERE STICKING REPLACED TRIPLE TACH 1G72 3U H3AU 20030717000092003071700009GL 2003 7 17 HEEA087986 220030701A75326893483 BELLOWS CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C* GL BLEED VALVE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FF43533 COULD NOT GET BLEED VALVE TO SET VACUUM. INSPECTED AND FOUND BELLOWS CRACKED AT PIPE SOLDERED TO BELLOWS ASSY. TO BE SENT TO VENDOR. 1Q71 3R3 U 2A6 E4CE 20030717000362003071700036SW 2003 7 17 HEEA088011 120030623A5610407030645115 WINDOW BELL 407 407 1182206SW PAX DOOR CRAZED E O OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 LITTER DOOR WINDOW IS CRAZED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000632003071700063SW 2003 7 17 HEEA088056 120030703A5630206201104 WINDOW BELL 206 206L3 1182108SW BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 WINDOW BROKEN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030717000822003071700082SW 2003 7 17 HEEA088074 120030701A2432RG214 BATTERY BELL 214 214ST 1182106SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T213 28101 BATTERY WEAK. 2G72 4U H10SW 20030717000972003071700097NM 2003 7 17 TSAA0353121 120030505A53106573744 SHEAR TIE BOEING737 73725A 1384481NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DAMAGE DISCOVERED ON SHEER TIE BETWEEN STRINGER 14 AND 15L AT BS 360. CUTOUT DAMAGED SECTION OF SHEAR TIE. FABRICATED A REPAIR SHEAR TIE AND RADIUS FILLER. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-4, FIGURE 10. (M) 2L72 4F RTA16WE 20030717000992003071700099NM 2003 7 17 TSAA0333129 120030529A33508610066 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHT DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13823AL 23154 REPLACED FORWARD SERVICE DOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030718000102003071800010NM 2003 7 18 TSAA0353119 120030506A53136573742 STRINGER BOEING737 73725A 1384481NM FUSELAGE DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DENT DISCOVERED AT BS 376 ALONG STRINGER 17L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. (M) 2L72 4F RTA16WE 20030718000272003071800027 2003 7 18 USAASB03076 420030609A2211AR6460M2 SERVO BOEING737 737401 1384701NM STAB TRIM MALFUNCTIONED A USAAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 EA19423US44446 23990 ON CLIMB-OUT FROM CLT, EN ROUTE TO BOS, CAPTAIN LOST HIS AUTO PILOT AND VOR. HE SWITCHED TO THE FIRST OFFICERS AUTO PILOT AND LOST THAT AS WELL. AT THE SAME TIME, SEVERAL INSTRUMETNS WERE GIVING ERRONEOUS DATA ALONG WITH THE MACH TRIM FAIL LIGHT AND SPEED TRIM FAIL LIGHT ILLUMINATING. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMVOED AND REPLACED THE AUTO PILOT STABILIZER TRIM SERVO AND TESTED PER MM 22-11-81. ACCOMPLISHED SATISFACTORY FUNCTINAL CHECK OF AUTO PILOT SYSTEM. VENDOR FOUND MAIN WORN MAGNETIC CLUTCH. REPLACED SAME. NO REPEAT ITEMS. REPORTED AS OF THIS DATE. (M) 2L72 4F RTA16WE 20030718000502003071800050NM 2003 7 18 AUS20030547 120030526A2751 WARNING LIGHT BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU TE FLAP ILLUMINATED W O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 AUS (AUS) FLAP ASSYMETRY PROBLEMS. LIMITED INFORMATION PROVIDED. 2L72 4F4 FRTA16WE E21EU 20030721000092003072100009NM 2003 7 21 AUS20030564 120030612A5330 SKIN BOEING737 737377 NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FORWARD GALLEY DOOR CUTOUT SKIN FORWARD AND AFT UPPER CORNERS CRACKED. THE AFT UPPER CORNER OF THE CUTOUT WAS CRACKED FROM ONEHOLE IN THE BEARSTRAP ONLY. TWO HOLES AT THE FORWARD UPPER CORNER OF THE CUTOUT WERE CRACKED IN THE STUBFRAME ONLY AND ATHIRD HOLE AT THE FORWARD UPPER CORNER WAS CRACKED IN THE BEARSTRAP ONLY. FOUND DURING EDDY CURRENT INSPECTION IAW SB B737-53-1116 (AD/B737/24). 2L72 4F4 FRTA16WE E2GL 20030721000122003072100012NM 2003 7 21 AUS20030568 120030603A5753 SKIN BOEING727 727281 138408NNM PWA JT8 JT8D17 52049NE TE FLAP SEPARATED W O OTHER D INFLIGHT SEPARATION LDLANDING 1 AUS (AUS) LT INBOARD FOREFLAP UPPER SKIN DISBONDED AND SEPARATED. SIZE OF DISBONDED PIECE APPROXIMATELY 355.6MM BY 177.8MM (14IN BY 7IN). SUSPECT CAUSED BY FOREIGN OBJECT LODGED BETWEEN FOREFLAP AND WING UPPER SURFACE. FOD. 2L73 4F4 F A3WE E2EA 20030716001052003071600105 2003 7 16 HEEA087974 420030626A34427007700614 DISPLAY SKRSKYS76 S76A 8143006NE WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 WEATHER RADAR DISPLAY SCREEN DIM AFTER 20 MINUTES. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030717000422003071700042SW 2003 7 17 HEEA088017 120030626A3212407073848101 BOTTLE BELL 407 407 1182206SW FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH 53435 EMERGENCY FLOAT BOTTLE LEAKED DOWN TO ZERO. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000452003071700045SW 2003 7 17 HEEA088020 120030621A5610407539104 WINDOW BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 COCKPIT WINDOW CRAZED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030721001162003072100116NM 2003 7 21 SWAA031482 120030704A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, BETWEEN STR 21R AND 22R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030721001262003072100126 2003 7 21 SWAA031490 420030705A2565D31354 SLIDE BOEING737 7373TO 138447GNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030721001282003072100128NM 2003 7 21 SWAA031492 120030706A575365C2660399 SKIN BOEING737 7373TO 138447GNM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C4 CHECK, FOUND NR 3 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 3 L/E SLAT PER MM. 2L72 4F RTA16WE 20030721001332003072100133 2003 7 21 SWAA031516 420030710A25656557463 BRACKET BOEING737 7373H4 1384600NM ESCAPE SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING BRACKETS CORRODED. REMOVED AND REPLACED GIRT BAR RETAINING BRACKETS PER SRM. 2L72 4F RTA16WE 20030318000152003031800015EU 2003 3 18 BAQA085087 120030304A243523032022 STARTER GEN BOLKMS117 BK117A4 5626017EU DC SYSTEM INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911WS216 7068 DC STARTER GENERATOR HAS SLOW STARTING SPEED. 1G72 3U H13EU 20030318000172003031800017 2003 3 18 BAQA085089 420030305A3421C17027AA01 INDICATOR UROCOPEC135 EC135T1 5620026EU ATTITUDE OUT OF TOLERANCEH BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01575ME1618 0157 ADU FAILS FAR 91.411 CHECK. ALTITUDE OUT OF LIMITS. 1G72 3U H88EU 20030318000242003031800024 2003 3 18 BAQA085117 420030310A34215040017907 INDICATOR BEECH 90 C90 1152913CE PWA PT6 PT6A11 52043NE ATTITUDE INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS0190LF 635 LJ852 ATTUTUDE INDICATOR LEANS TO ONE SIDE. STRAIGHT AND LEVEL. REPLACED WITH SERVICEABLE UNIT. 1L72 3T3 T 3A20 E4EA 20030318000342003031800034SW 2003 3 18 ERAA085158 120030218A6220412010100139 ROTOR HEAD BELL 412 412 1182202SW MAIN ROTOR LOOSE H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01164EH751 33004 SPINDLE & FLEXTURE FITTING IS LOOSE & WORKING. 2 BLADE BOLTS SN A-3115 & A-3155 SCRAPPED FOR CORROSION OR MECHANICAL DAMAGE. PITCH HORN A-176 SCRAPPED FOR MECHANICAL DAMAGE. ALL 4 SPINDLES, NO DEFECTS NOTED. REMOVED SPINDLES. VISUALLY INSPECTED ALL REMOVED PARTS. C/W ERA SPINDLE INSPECTION AND REASSEMBLED IAW BHT-412 CR&O INSTALLING NEW MAST NUT LOCKS, SERVICEABLE PITCH HORN SERVICEABLE BLADE BOLTS AND HARDWARE. 1G72 4U H4SW 20030318000352003031800035SW 2003 3 18 ERAA085159 120030218A6420 BEARING BELL 412 412 1182202SW TAIL ROTOR HEAD WORN H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01164EH3970 HB279 33004 WORN FEATHER BEARINGS. REMOVED T/R BLADES, REMOVED BEARINGS & C/W NDT OF YOKE BORES. INSTALLED 4 EA NEW BEARINGS, INSTALLED BLADES AND MARVEL BALANCED IAW 412 CR&O. 1G72 4U H4SW 20030318000392003031800039NM 2003 3 18 0300516302 120030313A3350 POWER SUPPLY BOEING747 747451 1384940NM CABIN INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOP FROM 1L-2L. REPAIRED WIRES AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030318000412003031800041NM 2003 3 18 03FDEA00179 120030226A3260 SWITCH BOEING727 727173C 1384059NM PWA JT8 JT8D* NE RT GEAR DOOR FAILED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25199FE 19509 RED RT GEAR DOOR LIGHT ILLUMINATED ON LANDING GEAR RETRACTION. CREW CYCLED GEAR IAW QRH, LIGHT REMAINED ILLUMINATED FOR DURATION OF FLIGHT. REMOVED AND REPLACED RT MLG DOOR WARNING SWITCH IAW M/M 32-62-011-4 OPERATIONAL CHECK NORMAL. 2L73 4F4 F A3WE E2EA 20030318000422003031800042EU 2003 3 18 DHL2003367512 120030227A5230 PAN AIRBUS300 A300B4203 3930306EU CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R 0029514:Lwr. fwd. cargo door lwr pan bent. Correctice action:Removed lower door pans to gain access IAW A300 SRM 51-30-30. Cut out cracked "L" angle IAW A300 SRM 51-41-40. Fabricated repairs angles IAW A300 SRM 51-41-40. Formed lower pan IAW A300 SRM 51-26-00 an 51-40-40,located ,drilled,trimmed,alodined,primed,painted and installed repair angles and pan IAW A300 SRM 51-41-40,51-40-12. Reinstalled seal an retainer IAW A300 MM 52-30-18 2L72 4F RTA35EU 20030318000542003031800054SW 2003 3 18 20032 120030228A339783205592 CONNECTOR SWRNGNSA227 SA227AC 8780603SW COCKPIT BURNED E STZAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03505FS1000 475 AC591B ON MEDEVAC FLIGHT FROM BET TO ANC AIRCRAFT ENCOUNTERED TURBULENCE AFTER WHICH THE FLIGHT CREW NOTICED A FAINT BURNING ODOR, ELECTRIC OR RUBBER, AIRCRAFT LANDED AT ANC WITHOUT FURTHER INCIDENT. ALL LIGHTING WAS FOUND TO BE OPERATIVE WITH NO EVIDENCE OF BURNING ODOR. MAINTENANCE INSPECTED COCKPIT INSTRUMENT AND CB PANEL LIGHTING WIRING AND FOUND A BUTT SPLICE POWERING ONE CB PANEL BACKLIGHTING THAT APPEARED CHARRED. SPLICE WAS REPLACED AND THE PANEL TESTED WITH NO OTHER ANOMALIES FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA8SW 20030318000612003031800061WP 2003 3 18 AALA20030137 120030202A2120 ODOR DOUG DC9 DC982 3022082WP CABIN DETECTED A AALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW217536A 49990 DFW - FLT 708 - EN ROUTE DFW-LGA, DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. WHEN POWER REDUCED BELOW 80 PERCENT N1 LIGHT EXTINGUISHED THEN ILLUMINATED AGAIN WHEN POWER ADVANCED ABOVE 80 PERCENT N1. F/A ON REAR JUMP SEAT NOTICED SMELL OF ELECTRICAL OR OIL BURNING ODOR. ODOR DISSIPATED WHEN POWER REDUCED. RETURNED AND LANDED DFW WITHOUT INCIDENT. NO FIRE OR SMOKE PRESENT AFTER LANDING. CLEANED OUT EXCESSIVE HYDRAULIC FLUID IN TAIL COMPARTMENT. REPLACED RIGHT PACK REGULATOR VALVE. TIGHTENED RIGHT FLOW CONTROL SENSE LINE. PERFORMED TAIL COMPARTMENT SENSOR TEST. RAN BOTH ENGINES TO POEWR, ALL INDICATIONS ARE NORMAL NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030318000732003031800073NM 2003 3 18 0300536744 120030228A5412 WEB BOEING747 747212F NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01644NW 24177 During "H" check found cracks in frame webs of #3 pylon rear engine mount bulkhead. Repaired per EA 67-165041. 2L74 4F RTA20WE 20030318000742003031800074NM 2003 3 18 0300546744 120030226A5330 SKIN BOEING747 747212F NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01644NW 24177 During "H" check found cracks in forward upper corner of aft cargo door cutout. Repaired per EA 67-165048. 2L74 4F RTA20WE 20030318000872003031800087WP 2003 3 18 ASAA0380024 120030104A52305910141115 GUIDE DOUG DC9 DC983 3022083WP CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO DOOR FORWARD AND AFT UPLOCK GUIDE ANGLES ARE GOUGED. REPLACED GUIDE ANGLES PER MM 20-30-01. (M) 2L72 4F RTA6WE 20030318000902003031800090WP 2003 3 18 ASAA0380027 120030104A575339195842 FITTING DOUG DC9 DC983 3022083WP RT WING TE FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP VANE NR 6 FITTING IS WORN. REPLACED FITTING PER CMM 27-50-02. (M) 2L72 4F RTA6WE 20030318000912003031800091NM 2003 3 18 F3LA200300099 120030228A5720 CHANNEL BOEING737 7373Q8 1384670NM WBL 73.00 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED LT. WING CHANNEL CRACKED AT WBL 73.00. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-2, PARA 6, AND SRM 51-40-2. 2L72 4F RTA16WE 20030318000952003031800095NM 2003 3 18 2003UALA00254 120030309A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 CABIN FLOOR SUPPORT CORROSION ON UPPER SURFACE, STA 367, RBL 9. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT AT BS 367, STR 9, WL 208. 2L72 4F4 FRTA2NM E17NE 20030328000892003032800089EA 2003 3 28 COMA0360145 120030315A2720601R5122623 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA INSTRUMENT PANELMALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01929CA 7035 FLIGHT 5219 RUDDER TRIM STUCK AT 1/4 RIGHT. REPLACED THE RUDDER TRIM PANEL. 2L72 4F RTA21EA 20030318001142003031800114NM 2003 3 18 BJNA030214 120030217A5320 FLOOR SUPPORT BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT LOCATED IN THE AFT CARGO BAY AT FS 772 LBL 5. REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED NEW REPAIR SECTION IAW BOEING 737 SRM 53-10-5 FIGURE 6. (M) 2L72 4F RTA16WE 20030318001172003031800117NM 2003 3 18 BJNA03026 120030209A5320 FLOOR SUPPORT BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT LOCATED IN THE AFT PIT AT FS 1000 LBL 17. REMOVED THE SUPPORT FITTING, FABRICATED AND INSTALLED NEW REPAIR PART IAW BOEING 737-200 SRM 51-10-2, AND 51-30-2. (M) 2L72 4F RTA16WE 20030318001222003031800122NM 2003 3 18 BJNA03029 120030211A5347BAC1520792 SEAT TRACK BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM46484 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A PASSENGER CABIN SEAT TRACK LOCATED AT BS 360 LEFT OUTBOARD SIDE. REMOVED THE CORRODED SECTION OF SEAT TRACK AND REPLACED WITH A NEW SECTION MADE OUT OF BOEING EXTRUSION P/N BAC 1520-792. WORK DONE IAW BOEING 737 SRM 53-10-5 FIGURE 2, 53-10-01 PAGE 18, AND 51-10-2. (M) 2L72 4F RTA16WE 20030318001312003031800131NM 2003 3 18 GAIA03003OP 120030129A33501000679 SIGN BOEING727 727224 1384076NM CABIN INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW0769740 20668 DURING ROUTINE MAINTENANCE AT PHL, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT WAS INOPERATIVE. FOUND UNIT TO BE LOOSE. RESEATED AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030318001372003031800137NM 2003 3 18 GAIA03008OP 120030214A33501000679 LIGHT BOEING727 727223 1384074NM L1 DOOR INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING ROUTINE MAINTENANCE AT IAH, IT WAS DISCOVERED THAT THE L-1 EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030318001862003031800186EA 2003 3 18 COMA0370006 120030313A5240 SERVICE DOOR CNDAIRCL600 CL6002C10 1390015EA A COMAA UNSCHED LANDING OW OTHER INADEQUATE Q C CLCLIMB 1 SO01340CA 10062 FLIGHT 5936 EXTERNAL POWER PANEL LEFT OPEN.INSPECTED EXTERNAL POWER DOOR FOR DAMAGE, AND SECURED DOOR CLOSED. 2L72 4F RTA21EA 20030318001902003031800190NM 2003 3 18 VNAA0303020 120030317A2400 ALTERNATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RH FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07423JS 3032 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND ALTERNATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. AFTER THE POWER LEVERS WERE PULLED BACK THE ALTERNATOR RESET PRIOR TO EXITING RUNWAY. MAINTENANCE CONTROL HAD THE CREW PERFORM AN AIRCRAFT RUN UP AND THERE WERE NO DISCREPENCIES. FLIGHT 4115 THEN RETURNED TO THE GATE WHERE OUTSTATION MAINTENANCE INSPECTED AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT. FLIGHT 4115 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030318001922003031800192NM 2003 3 18 VNAA0303022 120030317A240020040 ALTERNATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RH FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07423JS156933870 3032 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND ALTERNATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE REPLACED THE RIGHT HAND ALTERNATOR AND THE GARLOCK SEAL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030318001932003031800193 2003 3 18 VNAA0303007 420030306A3100 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LH FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07328JS 3030 AFTER DEPARTING FROM DCA, THE CREW RECEIVED A WEIGHT ON WHEELS CAS MESSAGE AND ASSOCIATED PROXI SYSTEM FAIL CAS MESSAGES. FLIGHT 4031 WAS INSTRUCTED TO DIVERT TO PIT THEN DECIDED TO CONTINUE TO DAY DUE TO RUNWAY CONDITIONS AT PIT. AFTER VERIFYING THE GEAR WAS DOWN AND LOCKED, FLIGHT 4031 LANDED SAFELY AT DAY. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030318001952003031800195NM 2003 3 18 VNAA0303011 120030310A3200 ACCUMULATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE A VNAAO OTHER O OTHER CRCRUISE 1 GL07439JS 3057 ENROUTE, THE CREW RECEIVED A EMERGENCY PARKING BRAKE PRESSURE LOW CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO ITH. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND FOUND THE EMERGENCY ACCUMULATOR PRESSURE LOW. MAINTENANCE THEN SERVICED THE EMERGENCY ACCUMULATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030318001972003031800197NM 2003 3 18 F3LA200300105 120030228A5210 SUPPORT ANGLE BOEING737 7373Q8 1384670NM CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED UPPER FUSELAGE FWD ENTRY DOOR AFT LOWER SIDE, INTERNAL DOOR COVER SUPPORT ANGLE CRACKED AND VERTICAL FLANGE BROKEN. FABRICATED AND INSTALLED ANGLE PER SRM 51-20-02, 51-30-1, FIG. 3, 51-10-09, AND 51-20-01. 2L72 4F RTA16WE 20030318002012003031800201NM 2003 3 18 UPS03240297 120030308A5720 RIB BOEING727 72725C 138400HNM WING TIP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 INSPECTION TYPE:C&SI ON REMOVAL OF WING TIP, INNER RIB FOUND TO BE CRACKED RIB REPLACED IAW SRM 51-20-1 FIG 7 & DRAWING 65-72719 SHEET 6 2L73 4F A3WE 20030318002182003031800218NM 2003 3 18 AWXA200300291 120030228A5315146N5400 INTERCOSTAL BOEING757 757225 1384959NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW0 0 22208 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON INTERCOSTAL WEB UNDER R/H OUTBOARD FLOORBOARD STRINGER, AFT CARGO COMPARTMENT, BS 1300 TO 1320. MAINTENANCE REMOVED CORRODED INTERCOSTAL WEB BS 1300 TO 1320; FABRICATED A NEW INTERCOSTAL WEB PER DWG 146N5400; INSTALLED REPAIR PART IAW B737-200 SRM 51-40-02, PG. 1. 2L72 4F RTA2NM 20030318002192003031800219NM 2003 3 18 AWXA200300292 120030301A5320146N5432 INTERCOSTAL BOEING757 757225 1384959NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW0 0 22208 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON VERTICAL WEB (INTERCOSTAL) TO FUSELAGE SKIN BETWEEN BS 1500 TO 1520, RBL 2. MAINTENANCE REMOVED INTERCOSTAL BS 1500 TO 1520, RBL 2; REMOVED CORRODED LOWER "L" ANGLE FROM INTERCOSTAL; FABRICATED A NEW "L" ANGLE; INSTALLED "L" ANGLE ON TO INTERCOSTAL; REINSTALLED INTERCOSTAL IAW B737-200 SRM 51-40-02, PG. 1. 2L72 4F RTA2NM 20030318002222003031800222EU 2003 3 18 RAIA00303070 120030312A2731C850176 VANE JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03558HK14605 41071 5570-STL- LEFT STALL WARNING ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE AOA VANE, OPS CK OK. 2L72 4T RTA41NM 20030319000062003031900006WP 2003 3 19 GTIA030007 120030115A5315 FLOORBEAM DOUG DC9 DC982 3022082WP CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND PASSENGER CABIN CENTER FLOORBEAM BETWEEN STATION 537 AND 615 BROKEN PLACES. REMOVED PASSENGER CABIN CENTER FLOORBOARD. FABRICATED FLOORBOARD. INSTALLED PASSENGER CABIN CENTER FLOORBOARD. (M) 2L72 4F A6WE 20030319000112003031900011WP 2003 3 19 GTIA030012 120030123A2120 ODOR DOUG DC9 DC982 3022082WP CABIN DETECTED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL23823NK 48020 FLT 1927 - ORD - STRONG ODOR OF BURNING RUBBER OR OIL IN CABIN, JUST FORWARD OF OVERWING EXITS, DURING APPROACH, BEFORE LANDING GEAR WAS LOWERED. INSPECTED CABIN LIGHTING, OPERATED LEFT AND RIGHTS PACKS, NO DEFECTS NOTED. CHECKED C/B'S, NONE TRIPPED. AIRCRAFT OK FOR CONTINUED SERVICE. (M) 2L72 4F A6WE 20030319000142003031900014WP 2003 3 19 GTIA030016 120030122A3297 WIRE DOUG DC9 DC981 3022081WP PROX SWITCH CHAFED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23805NK 48058 SJU - FLT 770 - 'GEAR DOOR OPEN' ANNUNCIATOR LIGHT ILLUMINATED IN CRUISE FLIGHT WITH NORMAL HYDRAULICS PRESSURE FOLLOWED QRH 4-6. GEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. CYCLE MLG DOORS SEVERAL TIMES AND OPS NORMAL. CHECK DOOR WARNING SENSORS FOR PROPER INSTALLATION AND CLEARANCE AND FOUND NORMAL. FOUND CHAFED WIRE ON RIGHT GEAR DOOR PROX SWITCH. REPAIRED WIRE AND CONDUIT. (M) 2L72 4F A6WE 20030319000212003031900021 2003 3 19 GTIA030041 420030202A2565D29984211 SLIDE DOUG MD80 MD83 3023681NM TAIL COMPARTMENTDEPLOYED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 LGA - FLT 9822 - TAILCONE SLIDE DEPLOYED UPON TRIGGERING OF THE AFT ENTRY DOOR. SLIDE REMOVED AND PLACED ON AC. REMOVED AND REPLACED TAILCONE SLIDE. (M) 2L72 4F RT 20030319000322003031900032WP 2003 3 19 GTIA030057 120030217A3230 SCHRADER VALVE DOUG DC9 DC981 3022081WP MLG LEAKING A GTIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23819NK 48016 DTW - FLT 1691 - WHEN LANDING GEAR RAISED AFTER TAKEOFF THE NOSE GEAR LIGHT REMAINED RED. RECYCLED ONCE WITH NO LUCK TRIED ONCE MORE AFTER ABOUT 15 MINUTES TO SEE IF ICE MIGHT HAVE CLEARED, WORKED OK. FOUND NOSE STRUT DOWN TO .5 INCH CHROME, FOUND SCHRADER VALVE LEAKING. SERVICED NOSE STRUT IAW MM 32-21-02. INSTALLED NEW SCHRADER VALVE. LEAK CHECKS GOOD. NO OTHR DEFECTS NOTED. (M) 2L72 4F A6WE 20030319000332003031900033WP 2003 3 19 GTIA030058 120030207A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP CABIN CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT ANGLE STATION 150-160 LBL 12 CORRODED. FABRICATED PART. (M) 2L72 4F A6WE 20030319000342003031900034WP 2003 3 19 GTIA030059 120030206A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FLOOR PANEL STATION 200-260 LBL 20 LBL 44 DETERIORATED. FABRICATED NEW PANEL. (M) 2L72 4F A6WE 20030319000382003031900038WP 2003 3 19 GTIA030063 120030207A5320 WEB DOUG DC9 DC981 3022081WP SUB FLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND SUB FLOOR WEB STATION 160-200 LBL 44-54 HAS CORROSION AND CRACKED. FABRICATED WEB. (M) 2L72 4F A6WE 20030319000402003031900040WP 2003 3 19 GTIA030065 120030209A5321 FLOORBOARD DOUG DC9 DC981 3022081WP CABIN DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - PASSENGER CABIN STATION 1309 TO 1360 FLOORBOARD HAS SOFT/MUSHEY BLUE WATER STAINS AND SEVERAL INSERTS DAMAGE. FABRICATED NEW PASSENGER CABIN FLOORBOARD. (M) 2L72 4F A6WE 20030319000422003031900042WP 2003 3 19 GTIA030067 120030210A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 160 LBL 10 HAS CORROSION. FABRICATED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030319000472003031900047WP 2003 3 19 GTIA030072 120030209A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 218 RBL 10 - LBL 12 HAS CORROSION. FABRICATED NEW SUPPORT. (M) 2L72 4F A6WE 20030319000532003031900053WP 2003 3 19 GTIA030078 120030218A3397 WIRE DOUG DC9 DC981 3022081WP EMERGENCY LIGHT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 MCO - AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE AT EMERGENCY LIGHT TERMINAL END. REPLACED TERMINAL END. EMERGENCY LIGHT GROUND OPS CHECKS GOOD. (M) 2L72 4F A6WE 20030319000542003031900054NM 2003 3 19 0300565512 120030221A5347 SEAT TRACK BOEING757 757251 1384970NM CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01512US 23200 During "H" check found corrosion on seat track at BS 365 RBL 24.75 and RBL 45. Repaired per EA 55-192510. 2L72 4F RTA2NM 20030319000622003031900062NM 2003 3 19 HALA0300029 120030130A2497MS277436 RELAY BOEING767 76733A 1385209NM ELECTRICAL FAILED A HALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 WP13581HA 28141 LAX - BOTH AC AND DC STANDBY POWER LOST AND EICAS MESSAGE STANDBY BUS OFF DISPLAYED. STANDBY POWER BUS OFF LIGHT ILLUMINATED, BOTH INDICATORS SAME WHEN STANDBY POWER MOMENTARILY SELECTED TO BAT. REPLACED K-109 STANDBY POWER RELAY. PERFORMED STANDBY POWER. TEST OPS NORMAL PER MM 24-33-01. (M) 2L72 4F RTA1NM 20030319000792003031900079NE 2003 3 19 MEX2003037 220030215A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8* 52044NE RIGHT FAILED A ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23158PL 49761 FLT 415 - JFK-CUN - AIRCRAFT SUSPENDED TAKEOFF DUE TO LEFT REVERSE UNLOCK LIGHT TURNED ON. IN ORDER TO CHECK AT MORE TENSE, IT WAS SECURED REVERSE WAS OPERATED SEVERAL TIMES, ALL CORRECT. IT WAS CONSIDERED IN CLOSE POSITION IAW MEL 78-1. AFTER TAKEOFF, CAPTAIN REPORTED 3 STALLS IN RIGHT ENGINE AT 22,000 FEET AND RIGHT ENGINE SHUTDOWN PROCEDURE WAS ACCOMPLISHED, RETURNED TO THE AIRPORT. BLEEDS AND RIGHT ENGINE ENTRY WERE INSPECTED, ALL CORRECT, BUT AT TURBINE EXHAUST FOUND SUPPRESSOR OF NOISE, DAMAGED OUT OF LIMITS IAW MM 72-00-00, PAGE 650B, EXCESS OIL BURNED FOR EXHAUST, COWLING ENGINE WAS OPENED, DETECTING BLACK STAINS IN RIGHT ENGINE. AWAITING ENGINE CHANGE. (M) 2L72 4F4 FRTA6WE E2EA 20030319000962003031900096NM 2003 3 19 TSAA0333012 120030124A335086210066 BATTERY PACK BOEING737 7372S2C 138448GNM PAX CABIN INOPERATIVE A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13806AL 21927 REPLACED NR 4 AND NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030319001022003031900102NM 2003 3 19 UPS03240304 120030217A5310 FITTING BOEING727 727108C 1384039NM 940 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI 2 SUSPECT CRACKS ON R/H AFT UPPER 940 FLOORBEAM ATTACH FLANGE CRACKS OUT OF LIMITS FITTING REPLACED IAW UPS EO B727-5310-4501 2L73 4F A3WE 20030319001082003031900108NM 2003 3 19 TSAA0353017 120030204A53306546560 SKIN BOEING737 7372M6C 1384708NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 TRIMMED OUT DAMAGE SKIN AT BS 947.5 ABOVE STRINGER 25L. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIM BY .040 INCH INSURANCE CUT. NDT INSPECTED THE OUTE ROW OF FASTENER HOLES COMMON TO REMOVED EXISTING REPAIR USING .030 NOTCH ROTARY AND SURFACE PROBE INSPECTIONS. FABRICATED A .032 INCH DOUBLER, .050 INCH TRIPLER AND TWO .071 INCH FILLERS FROM 2024-T3 CLAD SHEET. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BVMS 10-79 TYPE III PRIMER. INSTLALED REPAIR PARTS WITH FASTENERS AND HI-LOKS WET WITH BMS 5-95 SEALANT IN TRANSITION FIT HOLES. APPLIED A FILLET SEAL OF BMS 5-95 SEALANT AROUND THE EDGES. APPLIED CORROSOIN INHIBITING COMPOUND TO THE INTERNAL AND EXTERNAL SURFACES OF THE REPAIR AREA. 2L72 4F RTA16WE 20030319001092003031900109NM 2003 3 19 TSAA0353022 120030204A53306546548 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13823AL 23154 TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CUTOUT. ENLARGED TRIMMED AREA BY .040 INCH INSURANCE CUT. FABRICATED A .050 INCH THICK REPAIR PLATE FROM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 USING FASTENERS IDENTIFIED IN TABLE 1. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030319001162003031900116NM 2003 3 19 USAA030013 120030205A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US51460 22954 CLT - FOUND SKIN CRACKED 2 INCHES, LEFT FUSELAGE STATION 727D PLUS 15 AT STRINGER 22L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M) 2L72 4F RTA16WE 20030319001192003031900119NE 2003 3 19 USAABA03003 220030218A7230 BLADE AIRBUS330 A330323 3930335EU RROYCERB211 RB211TRENT77 NE RT ENGINE DAMAGED A USAAA UNSCHED LANDING CEJF.O.D. VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA19671UW 0323 PHL - FLT 196 - DURING INITIAL CLIMB-OUT, CREW NOTED MODERATE VIBRATION FROM THE RIGHT ENGINE. CREW REDUCED THE THRUST TO IDLE. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOND A NINE BLADES DAMAGED BY FOD (ICE INGESTION). (M) 2L72 4F4 FRTA46NM E39NE 20030319001252003031900125NE 2003 3 19 CH1A200383006 220030316A7531 BLEED VALVE BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE A C1HAK NONE E VIBRATION/BUFFET APAPPROACH 1 GL15683CA 22490 Engine #3 had a compressor stall on approach at 1.2 EPR at 4000 ft and 180 KTS 2L73 4F4 F A3WE E2EA 20030320000042003032000004NM 2003 3 20 USAABB03001 120030102A33508731002511REV15 LIGHT BOEING757 7572B7 1384964NM R1 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19611AU 27123 BDL - FOUND EXIT EXIT IDENTIFIER AT DOOR R1 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030320000172003032000017 2003 3 20 USAADUPE 420030128A2565 GIRT BAR AIRBUS320 A320214 3930316EU ESCAPE SLIDE DIRTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19106US 1044 LGA - THE L1 DOOR WAS DIFFICULT TO KEEP IN THE ARMED POSITION. MAINTENANCE CLEANED AND LUBRICATED THE GIRT BAR ASSEMBLY AND LOCKING MECHANISM, AND REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030320000232003032000023EU 2003 3 20 USAASA03014 120030211A3350321430 BATTERY PACK AIRBUS320 A320214 3930316EU PAX CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19101UW 0936 CLT - DURING THE WEEKLY CHECK, THE RIGHT WING BATTERY PACK FOR THE EMERGENCY LIGHTS WAS FOUND FAULTY. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECK OK. (M) 2L72 4F RTA28NM 20030320000372003032000037NM 2003 3 20 USAASB03003 120030105A3397 WIRE BOEING737 7374B7 1384702NM EMERGENCY LIGHT LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19427US 24549 CLT - DURING WEEKLY CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 10 AND 13 INOPERATIVE. MAINTENANCE CONNECTED LOOSE WIRES AT SEAT ROWS 10 AND 13. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030320000412003032000041NM 2003 3 20 USAASB03009 120030115A21337110033 OUTFLOW VALVE BOEING737 7373B7 1384580NM CABIN PRESSURE FAULTY A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19391US 23313 CLT - FLT 879 - AIRCRAFT EXPERIENCED AN AUTO PRESSURIZATION FAILURE WITH CABIN PRESSURE CLIMBING. STANDBY PRESSURIZATION KICKED IN, BUT DID NOT HELP. CAPTAIN SWITCHED TO MANUAL PRESSURIZATION MODE, AND STILL COULD NOT CONTROL CABIN PRESSURE. CAPTAIN ADVISED ATC THAT HE NEEDED TO DESCEND. ATC CLEARED THE FLT TO FL220 BUT CABIN PRESSURE CONTINUED TO CLIMB. AN EMERGENCY WAS DECLARED AND FLT DESCENDED TO FL100 WHERE CREW REGAINED CONTROL OF PRESSURIZATION. FLT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE AFT OUTFLOW VALVE AND REPLACED TERMINAL END ON GROUND WIRE ON AC MOTOR CANNON PLUG. OPERATIONAL CHECK GOOD PER MM 21-31-11. (M)2L72 4F RTA16WE 20030320000472003032000047NM 2003 3 20 USAASB03017 120030202A56105717623116 WINDOW BOEING737 737301 1384611NM COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19353US41958 23556 CLT - FLT 1122 - DURING CRUISE, EN ROUTE FROM PIT TO ATL, THE FIRST OFFICERS SLIDING WINDOW CRACKED. FLGIHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS SLIDING WINDOW PER MM 56-12-11 AND THE WINDOW HEAT CONTROLLER PER MM 30-41-11 AS PRECAUTIONARY. PRESSURIZED AIRCRAFT. LEAK CHECK AND OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20030320000522003032000052NM 2003 3 20 USAASB03022 120030209A278265C3805915 ACTUATOR BOEING737 737301 1384611NM NR 5 SLAT MALFUNCTIONED A USAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA19586US 23931 PIT - FLT 865 - DURING APPROACH, CREW REPORTED THE NR 5 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED WHEN FLAPS/SLATS WERE SET TO 5 UNITS. CREW NOTED AIRCRAFT WANTED TO ROLL RT DURING FLAP/SLAT SET. NR 5 LEADING EDGE SLAT DID NOT RETRACT UNTIL APPROXIMATELY FOUR MINUTES AFTER TRAILING EDGE FLAPS RETRACTED AS PER COCKPIT INDICATION. FLT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 5 LEADING EDGE SLAT ACTUATOR PER MM 27-81-41. OPS CHECK AND LEAK CHECK GOOD. 2L72 4F RTA16WE 20030721001412003072100141NM 2003 7 21 VNAA0307002 120030709A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EXIT DOOR FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07458PS 3068 THE CREW RECEIVED A EMERGENCY EXIT DOOR LIGHT ON THE DOORS PAGE. AS THE FLIGHT DESCENDED THE MESSAGE CLEARED. MAINTENANCE INSPECTED AND RERIGGED THE PROXI SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030721001432003072100143EU 2003 7 21 MALA030331 120030705A302044730501 MODULE SAAB SF340 340B 7860101EU DEICE SYS FAILED A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15451XJ 340B451 DURING FLIGHT 3396, LT INTAKE HEAT INOP. LEFT ENGINE INTAKE WARNING LIGHT ON C/B POPPED. RESET TWO TIMES. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED LT DE-ICE MODULE IAW SF340 AMM CHAPTER 30 SN/ON A00201, SN/OFF A00221 PN/ON & OFF 44730-501. PERFORMED REQUIRED GROUND OPS CHECKS RAN A/C FOR 30 MINUTES, NO FAULTS NOTED. ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20030722000062003072200006NM 2003 7 22 2003F00434 120030307A5310 BEAM BOEING727 727222 1384073NM BULKHEAD CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT AFT PRESSURE BULKHEAD VERTICAL BEAM, BS 1183, RBL 26.9 WL 260. REPAIRED VERTICAL BEAM AFT PRESSURE BULKHEAD, BS 1183, RBL 26.9, WL 260. (M) 2L73 4F A3WE 20030722000112003072200011NM 2003 7 22 2003F00439 120030312A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND TIE FRAME TO FUSELAGE CRACKED AT STATION 680, STRINGER 17L. FABRICATED ANGLE REPAIR. ALODINED, PRIMED AND INSTALLED ANGEL REPAIR ON BS 680, STRINGER 17L, LOWER SILL BEAM TIE FRAME. (M) 2L73 4F A3WE 20030722000122003072200012NM 2003 7 22 2003F00440 120030312A5330 SKIN BOEING727 727222 1384073NM DOOR CUTOUT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN CRACKED. STOPPED DRILLED CRACKS ON RIGHT FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER ON RIGHT FORWARD GALLEY DOOR LOWER AFT, CUTOUT CORNER. (M) 2L73 4F A3WE 20030422000332003042200033EA 2003 4 22 ASOA03078 120030223A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A HANGAR CHECK IN MCN, FRAME 640 BETWEEN STRINGERS 13 AND 14 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED FRAME 640 BETWEEN STRINGERS 13 AND 14 ON THE RIGHT SIDE IAW ASA EO 600-53-0086. (M) 2L72 4F RTA21EA 20030422000352003042200035SO 2003 4 22 ASOA03080 120030225A30103D237606 EJECTOR VALVE EMB 120 EMB120ER 3260203SO DEICE SYS INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11266AS 120188 FLT 4910 - DURING TAKEOFF FROM DFW-ICT, THE NR 1 AND NR 2 LEADING EDGE DE-ICE TIMERS FAILED ON BOTH THE LEFT AND RIGHT OUTBOARD WING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE AFT EJECTOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030422000442003042200044NE 2003 4 22 ASOA03064 220030217A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA PWA JT8 JT8D9A 52048NE LEFT LEAKING A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11846AS 7328 FLT 4250 - DURING CRUISE AT APPROXIMATELY 33,000 FT FROM ATL-PHF, THE CREW RECEIVED AN OIL PRESSURE WARNING MESSAGE ON THE LT ENGINE, ALONG WITH AN OIL PRESSURE DROP TO 15 PSI. THE FAN SPEED VIBRATION GAUGE PRIOR TO THE WARNIGN SHOWED .8 TO .9 AND APPEARED TO SPIKE MOMENTS BEFORE THE THRUST LEVER SHUTOFF. QRH PROCEDURES WERE COMPLIED WITH AND THE CAPTAIN SHUTDOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT DIVERTED TO CLT, LANDING SAFELY. MX FOUND THE LEFT ENGINE OIL TANK EMPTY AND SERVICED IT WITH 6 QUARTS OF OIL. MX SUBSEQUENTLY REMOVED AND REPLACED THE LEFT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E2EA 20030422000502003042200050EA 2003 4 22 ASOA03106 120030313A5346 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING A C-CHECK INSPECTION IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030422000572003042200057WP 2003 4 22 MEX2003080 120030317A278239200485503 ACTUATOR DOUG DC9 DC932 3022066WP LT WING SLAT BROKEN A ASMFK NONE O OTHER ININSP/MAINT 1 SW231003P 48150 DURING EXTERIOR INSPECTION, DETECTED A BREAK IN THE LEFT WING SLATS ACTUATORS ACCESS DOOR, THE FASTENER POINT OF THE UPPER SLAT ACTUATOR WAS BROKEN. BOTH CYLINDERS ACTUATORS WERE REPLACED IAW MM 27-80-5. (M) 2L72 4F A6WE 20030422000682003042200068SO 2003 4 22 SIMA200307001 120030310A2120 ODOR EMB 135 EMB135LR 3260305SO CABIN DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21712AE 145247 CMH - FLT 4576 - AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED STRONG BURNING RUBBER ODOR. PERFORMED PNEUMATIC BLEED CHECK WITH BOTH ENGINES AND APU OPERATING AND RUN UP AT POWER SETTINGS. NO UNUSUAL ODOR WAS NOTED IN THE CABIN OR COCKPIT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030422000862003042200086SO 2003 4 22 SIMA200307906 120030222A532013500469401 STRUCTURE EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION, CROSS MEMBER AT FRAME 22 IS CORRODED. REMOVED AND INSTALLED NEW CROSSMEMBER IAW EMB 135 SRM 51-40-02, 51-40-03. (M) 2L72 4F RTT00011AT 20030422000912003042200091SO 2003 4 22 SIMA200307104 120030216A532114525480003 FLOORBOARD EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, GALLEY FLOORBOARD EXTENSION HAS CORROSION. REMOVED AND INSTALLED FLOORBOARD EXTENSION IAW EMB 135 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M) 2L72 4F RTT00011AT 20030422000992003042200099NM 2003 4 22 USAA030024 120030303A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU58629 22198 CLT - FRAME WEB CRACKED .25 INCH, CARGO CUTOUT FRAME WEB BS 1440 AT NR 6 DOOR STOP FAST. INSTALLED DOUBLER PER EA 86992. (M) 2L72 4F RTA2NM 20030422001232003042200123EU 2003 4 22 USAASA03023 120030313A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19709UW 0997 LGA - THE EMERGENCY LIGHT TEST INDICATED THAT THE LEFT EMERGENCY POWER SUPPLY UNIT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030122001522003012200152NE 2003 1 22 HEEA083538 120030113A63227636209202103 BLOWER SKRSKYS76 S76A 8143006NE GEARBOX COOLER DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 RIVETS LOOSE ON HOUSING. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20030122001622003012200162NE 2003 1 22 HEEA083540 120030113A77147645001076103 INDICATOR SKRSKYS76 S76A 8143006NE TRIPLE TACH STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 TRIPLE TACH NEEDLE STICKS ON PILOT SIDE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030122001682003012200168NE 2003 1 22 DL764030004 220030102A7230 BLADE BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27828MH4651 29699 706261 WORKING MSU TO BORESCOPE THE NR 2 ENGINE DUE TO PARAMETERS SHIFTING (N2 F/F & EGT UP). ATL BORESCOPE TEAM FOUND THE 6TH STAGE HPC HAD BLADE TIPS MISSING AND THE 12TH STAGE HPC HAD BLADES WITH TEARS IN THE MID BLADE AREA. FOUND BOTH AREAS TO BE OUT THE ALLOWABLE MM IN SERVICE DAMAGE LIMITS. ENGINE CHANGE IN PROGRESS. 2L72 4F4 FRTA1NM E13NE 20030122001792003012200179NM 2003 1 22 DL767030043 120030110A2920 MODULE BOEING767 767232 1385132NM RT MLG WW LEAKING A DALAK NONE K FLUID LOSS APAPPROACH 1 SO27113DA 22225 A/C 113 LOST C-SYS HYDRAULIC QUANTITY INFLIGHT. A/C WAS INBOARD TO ATL. FOUND RAT TEST MODULE IN RT W/W LEAKING. REPLACED SAME. 2L72 4F RTA1NM 20030122001962003012200196NM 2003 1 22 HNAA0300004 120030113A3230858601 PSEU DHAV DHC8 DHC8201 2809001NM INOPERATIVE A HNAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA07968HA5140 1353 465 ON GEAR RETRACTION THE LEFT GEAR DOOR CAUTION LIGHT REMAINED ON AND THE LANDING GEAR CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD. REPLACED P.S.E.U. 2H72 4T RTA13NM 20030625000702003062500070EA 2003 6 25 HNAA0300005 120030115A6120V319 SWITCH DHAV DHC8 DHC8311 1386006EA NR 1 ENGINE INOPERATIVE A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07803SA22738 221 AFTER TAKEOFF, NR 1 ENGINE TORQUE AND PROP SPEED BEGAN TO FLUX WITH PROP SPEED AT 900 RPM. AIRCRAFT RETURNED TO FIELD. REPLACED SWITCH 6141-S3. 2H72 4T RTA13NM 20030122002112003012200211NM 2003 1 22 QXEA0300109 120030121A3230471513 HARNESS BOMBDRDHC8 DHC8401 1390041NM ZONE 700 INOPERATIVE A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09403QX3925 4037 PDX-ON FLIGHT NUMBER 2352, AFTER TAKEOFF, GEAR DID NOT RETRACT FOR ALMOST 1-1/2 MIN. GEAR HANDLE WAS UP. ALTERNATE LANDING GEAR RELEASE DOOR WAS CLOSED AND GEAR INHIBIT SWITCH AT NORMAL. REMOVED AND REPLACED WEIGHT ON WHEELS #2 CENTERING HARNESS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030122002192003012200219SW 2003 1 22 HEEA083559 120030113A6230206010450119 SWASHPLATE BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107313000 51519 OUTER RING (206010453009, S/N BFS45) CORRODED; INNER CAP (206010455103) WORN; SLEEVE SLIDER BEARING (206010459001) WORN. REPLACED PARTS AND REPAIRED. 1G71 3U H2SW 20030122002232003012200223SW 2003 1 22 HEEA083561 120030113A6220206011139001 ARM BELL 206 206L1 1182107SW FLAP RESTRAINT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR FLAP RESTRAINT ARM ASSY WORN. 1G71 3U H2SW 20030122002662003012200266NM 2003 1 22 UPS03440042 120030103A5310 FITTING BOEING747 747259B 1384804NM BS 1480 B/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C LH BS 1480 B/H NO.24 HOLE AT OUTER CHORD SPLICE FITTING RUNNING O/B APPROX 5/32" REFER ATTACH SKETCH FOR DETAILS. CRACKED FASTENER HOLE REAMED TO 0.530" AND BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-5310-10732-H WITHIH PLAN 'A' LIMIT CRACK F REE CONFIRMED BY NDT AS PER BTM PART 6 51-00-00 FIG.16 (REF EO B747-5310-1827-A) 2L74 4F RTA20WE 20030122002682003012200268NM 2003 1 22 UPS03440044 120030103A5310 FITTING BOEING747 747259B 1384804NM LH BS 1480 B/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:N/A LH BS 1480 B/H NO.7 HOLE CRACK AT EXTENSION FTG RUNNING AFT UPWARD DIRECTION APPROX 1/16" LONG. REFER ATT SKETCH FOR DETAILS. HOLE REWORKED AS PER RS-53-43-34957 DUE EXCEEDED SB 747-53A2390 REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTIONS). 2L74 4F RTA20WE 20030122002692003012200269NM 2003 1 22 UPS03440046 120030103A5330 SKIN BOEING747 747259B 1384804NM LH BS 1480 B/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C LH BS 1480 B/H NO.11 HOLE CRACK AT FX SKIN RUNNING FWD AD AFT AND THRU THICKNESS. REER ATTACH SKETCH FOR DETAILS. CRACKED FASTENER HOLE REWORK AS PER RS NO.R53-43-34957 DUE TO HOLE DIMENSION EXCEEDED SB REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTIONS). 2L74 4F RTA20WE 20030123000012003012300001NM 2003 1 23 EIA2003002 120030115A21507192387 ACM BOEING747 747273C 1384896NM LEAKING A EIAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09470EV 20653 DURING DESCENT UPPER DECK FILLED WITH LIGHT SMOKE WHEN NR 1 AC PACK SHUTDOWN, SMOKE CLEARED COMPLETELY. 2L74 4F A20WE 20030123000162003012300016NM 2003 1 23 2003UALA00032 120030107A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 CABIN BODY FRAME WEB IS CRACKED BS 400 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2L72 4F4 FRTA16WE E2GL 20030123000192003012300019NM 2003 1 23 2003UALA00035 120030107A2121 BEARING ALIDSG 6454051 BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE RECIRC FAN FAILED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP29952UA 127550 26699 FLIGHT CREW DECLARED AN EMERGENCY WHEN CREW NOTICED ELECTRICAL SMELL IN THE CABIN DURING DESCENT. SUPPLEMENTAL DATA UPDATE THE RECIRCULATION FAN BEARING FAILED, WHICH CAUSED AN ELECTRICAL SMELL IN THE PASSENGER CABIN AND RESULTED IN CIRCUIT BREAKER C884 POPPING. THE RECIRCULATION FAN WAS REPLACED AND SYSTEM OPERATION WAS NORMAL. 2L72 4F4 FRTA16WE E2GL 20030422001262003042200126NM 2003 4 22 UPS03240255 120030221A5752 CASTING BOEING727 727108C 1384039NM LT O/B AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, LT O/B AILERON TAB FIRST & SECOND FROM O/B HINGE CASTINGS HAVE PITTING CORROSION. HINGE CASTINGS REPLACED IAW MM 27-10-19. 2L73 4F A3WE 20030422001362003042200136SO 2003 4 22 RAIA00302045 120030212A3350 SWITCH EMB 145 EMB145ER 3260211SO AIRSTAIR INTERMITTENT A RAIAO OTHER O OTHER CRCRUISE 1 CE03808HK 145157 PIT- EMERGENCY LIGHTS ON STAIRS AND BELOW COCKPIT DOOR FLASH OCCASIONALLY. MAINTENANCE CLEANED SWITCH IN DOOR, OPS CHECK OK. 2L72 4F RTT00011AT 20030422001382003042200138EU 2003 4 22 RAIA00302055 120030225A3230 CONNECTOR AEROSPATR72 ATR72202 8680940EU MLG LOOSE A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03723TE 283 MLI - LANDING GEAR WILL NOT RETRACT. MAINTENANCE RESEATED PIN 10K AT CONNECTOR 14A1 -AA- AT MFC1. OPS CHECK OK. 2H72 4T RTA53EU 20030421000702003042100070EA 2003 4 21 SWIA200311819 120030224A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07403SW 7028 AISLE FLOOR EMERGENCY LIGHT SEGMENT INOP. EMERGENCY EXIT LIGHT, OVERWING (R) SIDE LOWER, INOP. REPAIRED BROKEN WIRE CONNECTOR TO FLOOR SEGMENT OF TRACK LIGHTING. OPS CHECK GOOD. 2L72 4F RTA21EA 20030421001032003042100103NM 2003 4 21 DLM90030174 120030222A2910 VALVE DOUG MD90 MD9030 3023690NM NLG FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27901DA 53381 UNSAFT NOSE GEARUP. RECYCLED GEAR AS PER POM PROCEDURE. ON GEAR UP NOSE GEAR UNSAFE (RED) STAYED ON 35 SECONDS LONGER THAN OTHER GEAR LIGHTS AND THE AIRFLOW NOISE DURING THAT TIME WAS LOUD AND UNUSUAL. JACKED NOSE, RAN GEAR, OPS CHECK GOOD. CHECKED DOWN RIGGING GOOD. SERVICED NOSE STRUT AND REPLACED SHRADER VALVE. CHECKED AIR GAP ON PROX SENSOR FOUND OK. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA6WE 20030421001342003042100134NM 2003 4 21 VNAA0302025 120030226A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AIR DOOR CONTAMINATED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07422JS 3018 AFTER LEVELING OFF, THE CREW RECEIVED A GROUND AIR DOOR PROXI SYSTEM CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RETURNED TO PHL. MAINTENANCE INSPECTED AND FOUND FOREIGN DEBRIS ON THE PROXI SENSOR, THEN REMOVED THE DEBRIS. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421001702003042100170SW 2003 4 21 2003F00222 120030205A7720 PROBE FRCHLDSA227 SA227DC 3377521SW NR 2 ENG TEMP MALFUNCTIONED A BSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM05853LS DC853B BIL - FLT 2565 - NR 2 ENGINE OIL TEMP WAS HIGH DURING CLIMB-OUT. CREW RETUREND TO STATION. INDICATION SYSTEM MALFUNCTION. REPLACED TEMP PROBE DUE TO SUSPECTED OIL INFILTRATION FROM CANNON PLUG SIDE, REPAIRED OIL TEMP BULB CANNON PLUG, AND REPLACED VERNATHERM VALVE. OIL SAMPLE WAS TAKEN, OIL WAS CHECKED FOR BURNING OR BURNED ODOR, NONE WAS NOTED. HALF HOUR GROUND RUN WAS PERFORMED, FOLLOWED BY A TEST FLIGHT. NO FURTHER DISCREPANCIES WERE NOTED. (M) 2L72 4T RTA18SW 20030421001742003042100174WP 2003 4 21 GTIA030125 120030223A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CABIN STATION 160 TO STATION 148 RBL 17 INCHES TO RBL 32 (11 BY 15) FLOOR PANEL SOFT/MUSHY. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20030421001882003042100188NM 2003 4 21 USAABB03043 120030317A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030421002082003042100208NM 2003 4 21 AMTA200300325 120030211A5330 SKIN BOEING757 75723N 1384973NM FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 RIGHT FUSELAGE SKIN DENTED AFT AND BELOW R1 DOOR. REPAIRED FUSELGAE SKIN IAW ER/A 757-53R-5082. (M) 2L72 4F RTA2NM 20030422000102003042200010EU 2003 4 22 USAASA03016 120030216A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU PAX CABIN MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19106US 1044 DCA - DURING THE EMERGENCY LIGHT SYSTEM TEST, RECEIVED 'EPSU INT LOAD FWD LT FAULT' MESSAGE. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030422000612003042200061SO 2003 4 22 SIMA200306204 120030302A3210 LANDING GEAR EMB 145 EMB145LR 3260212SO RIGHT MALFUNCTIONED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21622AE 145108 OMA - FLT 4108 - AFTER TAKEOFF, THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE WHEN GEAR HANDLE WAS SELECTED UP. THE RIGHT MLG DID NOT RETRACT. CREW RETURNED TO OMA WITH NO FURTHER INCIDENTS REPORTED. CFR DID RESPOND. (M) 2L72 4T RTT00011AT 20030422001012003042200101NM 2003 4 22 USAASB03039 120030312A335030043231 LIGHT BOEING737 7373B7 1384580NM CABIN FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU 23594 ATL - MAINTENANCE REPORTED THE AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OP CHECK GOOD. (M) 2L72 4F RTA16WE 20030422001252003042200125NM 2003 4 22 USAABB03041 120030312A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 9 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030422001472003042200147NE 2003 4 22 EIA2003049 220030304A7260UNK LINE BOEING747 747212B 1384886NM PWA JT9 JT9D* NE GEARBOX LEAKING A EIAAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09482EV 20713 662389 NR 2 ENG OIL QTY BEGAN DECREASING FROM 5.0 GAL, OIL PRESS/TEMP NORMAL. LATER NR 2 OIL PRESSURE DROPPED BELOW YELLOW BAND AND OIL PRESSURE LIGHT ILLUMINATED. NR 2 ENGINE WAS SHUTDOWN, WINDMILLING OIL PRESSURE MAINTAINED 20 PSI. INSPECTED AND REPLACED MAIN OIL FILTER IAW MM 72-61-00 AND CHECKED MAIN AND ANGLE GEAR BOX CHIP DETECTORS IAW MM 72-61-00 AL CH OK. FOUND OIL LEAKING FROM ANGLE GEAR BOX ADAPTER SCAVAGE LINE. REPLACED ADAPTER IAW MM 78-21-00. LEAK GOOD. RII C/W. 2L74 4F4 F A20WE E20EA 20030422001522003042200152NE 2003 4 22 HNAA0300013 220030308A7200 ENGINE DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE NR 2 DAMAGED A HNAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA07994HA 459 METAL CHUNK HANGING OUT OF NR 2 ENGINE INTAKE DOOR. FOUND TO BE A PIECE OF THE LOWER COWLING. INSPECTED ENGINE AND COWLING FOR DAMAGE AND WILL FERRIED TO SBY. UPON FURTHER INSPECTION WHEN ARRIVING IN SBY IT WAS DETERMINED THAT THE ENGINE WOULD HAVE TO BE CHANGED. 2H72 4T4 TRTA13NM E20NE 20030422001602003042200160NE 2003 4 22 SH52003F00000 220030214A73216047T74P13 FUEL CONTROL CNDAIRCL600 CL6002A12 1900304EA GE CF34 CF343A 30015NE RT ENGINE INOPERATIVE B SH5RO OTHER O OTHER NRNOT REPORTED 1 NE03500PG 6880 3039 AIRCRAFT WAS HOLDING ON TAXIWAY WITH WINDS OVER 40 KNOTS AND BLOWING SNOW. A/C WAS BEHIND A/C WHICH WAS KICKING UP ADDITIONAL SNOW. PILOT PUT ON THE COWL ANTI-ICE. APPROXIMATELY ONE MINUTE LATER THE RIGHT ENGINE SHUTDOWN UNCOMMANDED, AIRCRAFT RETURNED TO HANGAR. ENGINE WAS BORESCOPED, NO DEFECTS, FUEL WAS TESTED, NO CONTAMINATION. CHECKLIST FOR ENGINE FLAMEOUT WAS PERFORMED WITH NO DEFECTS NOTED. REPLACED MAIN FUEL CONTROL UNIT. PERFORMED ENGINE RUNS, ALL PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (NE03200303671) 2L72 4F4 FRTA21EA E15NE 20030423000112003042300011NM 2003 4 23 EVAS092008 120030227A7920 FILTER BOEING747 74745E 1384947NM GEARBOX CLOGGED W QOCFE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP0316402 27063 DURING CRUISE FOUND NR 3 ENGINE OIL QUANTITY DROP TO ZERO & IN-FLIGHT SHUT DONE ENGINE. PERFORM ENGINE CHANGE. AFTER REMOVE GEARBOX FOUND OIL SCAVENGE FILTER WAS CLOGGED BY OBJECTS. SUSPECT IT IS TEFLON SEAL 2L74 4F RTA20WE 20030423000122003042300012NM 2003 4 23 EVAS092007 120030219A5730 SKIN DOUG MD11 MD11F 3023600NM LT WING GOUGED W QOCFK NONE O OTHER ININSP/MAINT 1 WP0316108 48778 DURING WALK AROUND CHECK FOUND LT WING FIXED LEADING EDGE LOWER SURFACE ACCESS DOOR CUTOUT SKIN GOUGE DAMAGE AT STA SOX463.PER MD-11 SRM 57-10-00 PAGE 58A AND 58B TO REPAIR. 2L73 4F RTA22WE 20030423000302003042300030 2003 4 23 MEX2003125 420030407A344220412220402 INDICATOR DOUG DC9 DC9* WP PWA JT8 JT8D NE RADAR FAILED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW23501AM1010 49188 AIRCRAFT AIR TURNBACK, AFTER TAKE OFF CIRCUIT BREAKER F4 OF WX RADAR UNIT WAS TRIPPEC WITH WX RADAR OUT OF SERVICE INDICATIONS. AT PLATFORM WEATHER RADAR INDICATOR WAS REPLACED IAW MM, TESTS CORRECT. 2L72 4F4 F A6WE E2EA 20030423000332003042300033NM 2003 4 23 S03J27004 120030102A2700 CONTROL CABLE BOEING747 747400 NM GE CF6 CF680C2B2 30025NE RUDDER OUT OF RIG W SAJFO OTHER O OTHER TXTAXI/GRND HDL 1 WP03 30759 B-18701 RUDDER DOES NOT FULL DEFECT TO RT (SHORT OF ABOUT 15-20 PERCENT). RUDDER & RUDDER TRIM SYSTEM RIG CHECK FOUND CONTROL CABLE. TENSION WAS OUT OF LIMIT. PERFORM RUDDER AND RUDDER TRIM CONTROL SYS ADJ IAW AMM 27-21-00. PERFORM RUDDER RATIO GROUND TEST NORMAL. PERFORM RUDDER TRIM SYS TEST NORMAL. ALL CONDITIONS WAS INFORMED BOEING FOR RECOMMENDATION. FURTHER STUDY IS REQUIRED. 2L74 4F4 FRTA20WE E13NE 20030423000382003042300038GL 2003 4 23 AUS20030274 320030228A61103AF32C87 PROPELLER CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 623 (AUS) PROPELLER FAULTY. FOLLOWING FEATHERING CHECK IAW AD/PROP/2 AMDT2IT WAS FOUND THAT TWO BLADES COULD BE ROTATED BACK TO FULL FINE POSITION BY HAND. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20030423000402003042300040WP 2003 4 23 MEX2003131 120030411A3411851AK PITOT TUBE DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE NR 1 FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23803ML 49726 CAPTAIN REPORTED LEFT PITOT SYSTEM OUT OFF SERVICES. PITOT TUBE WAS REPLACED IAW MM, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20030423000622003042300062EU 2003 4 23 BAQA085943 120030410A65401179405303 INDICATOR BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101600A 41560NE TRIPLE TACH INTERMITTENT H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01952CJ6 7052 ROTOR TACH INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 4/10/03 1G72 3U3 U H13EU E5NE 20030423000842003042300084GL 2003 4 23 ALGA085863 220030331A731323008593AL NOZZLE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C* GL ENGINE MISMANUFACTURED E ALGAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 FS01PARTO TROUBLESHOOTING LOW POWER ON TEST CELL. FOUND 1ST STG. NOZZLE MATING SURFACE MEASURING UNDER PRINT DIMENSION. ACTUAL DIM: .610 1Q71 3R3 U 2A6 E4CE 20030423000912003042300091 2003 4 23 BAQA085909 420030404A34217000836907 GYRO AGUSTAA109 A109E 0260119EU ADI MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS017YL 183 11502 ADI HAS ERRATIC COMMAND BARS. ATT BUTTON STICKS. SPEX FILE 00115248. REPLACED WITH SERVICEABLE UNIT. 4/8/03 1G72 3U RTH7EU 20030423001192003042300119 2003 4 23 GLBA2003029 420030305A3416 INDICATOR BEECH 1900 1900D 1154162CE NR 1 ALTIMETER FAILED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03118UX UE118 NR 1 ALTIMETER FLAGGED. PERFORMED PITOT-STATIC CHECK OF SYSTEM, OPS CHECK GOOD. 2L72 4T RTA24CE 20030423001252003042300125NM 2003 4 23 QXEA0300337 120030307A6120 BETA SWITCH DHAV DHC8 DHC8202 2809007NM NR 1 PROPELLER MALFUNCTIONED A QXEAO OTHER O OTHER LDLANDING 1 NM09358PH 506 PROPS SET AT 1050 FOR BRAKING AND POWER LEVELS REDUCED TO FLIGHT IDLE NR 1 ENGINE TORQ STARTED TO SURGE +/- 5 PERCENT FROM 10 PERCENT TORQUE, AND PROP RPM INCREASED. TROUBLESHOOTING NOTED NR 1 ENGINE FAILED OPERATION TEST OF BETA LOCKOUT SYSTEM DUE TO POWER LEVER SWITCH 6141S3 ACTUATING ABOVE FLIGHT IDLE. ADJUSTED 6141S3. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030423001272003042300127NM 2003 4 23 MWEA030131 120030309A5270833703 PROXIMITY SENSOR DOUG MD88 MD88 3023688NM AFT CARGO DOOR MALFUNCTIONED A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31701ME 49760 AFT CARGO DOOR ILLUMINATED OPEN WITH DOOR CLOSED. REMOVED AND REPLACED AFT CARGO DOOR PROXIMITY SENSOR. 2L72 4F RTA6WE 20030421000722003042100072 2003 4 21 XNOA01108 420030304A3414 PITOT TUBE AIRBUS300 A300B4203 3930306EU AIRSPEED IND CLOGGED A XN0AC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL23474AS 219 REJECTED TAKEOFF. NO AIRSPEED INDICATION ON CAPTAINS SIDE. REMOVED DEBRIS FROM CAPT PITOT TUBE. PERFORMED PITOT STATIC CHECK. AIR SPEED IND, OPS CHECKS GOOD IAW 34-11-40 OF A300 MM. 2L72 4F RTA35EU 20030421000942003042100094NM 2003 4 21 DLM88030149 120030212A33408906K1268 SWITCH DOUG MD88 MD88 3023688NM COCKPIT SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27975DL 53243 AT APPROXIMATE TIME OF WING LANDING LIGHT ACTIVATION THERE WAS A FAINT ELEC ODOR AND SMALL AMOUNT OF SMOKE. ODOR AND SMOKE DISSIPATED AFTER SWITCHES TURNED OFF. REPLACED LT WING LANDING LIGHT SWITCH. FOUND SIGN OF ARCING ON ONE OF THE TERMINALS. 2L72 4F RTA6WE 20030422000082003042200008EA 2003 4 22 ASOA03067 120030218A5412601R3701139 FIREWALL CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 FLT 4250 - THE LEFT PYLON FIREWALL AT FRAME STATION 659.75 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT PYLON FIREWALL AT FRAME STATION 659.75 IAW ASA EO 600-54-0010 AND REO 801R-54-51-004. (M) 2L72 4F RTA21EA 20030422000252003042200025WP 2003 4 22 GTIA030135 120030203A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND CORROSION ON CUSP STATION 220-240 LBL 54. REMOVED CUSP STATION 180-230. FABRICATED NEW CUSP FROM STATION 180-230 LEFT. FABRICATED SPLICE FOR NEW CUSP STATION 180. INSTALLED CUSP SPLICE STATION 180. INSTALLED CUSP STATION 180-230. (M) 2L72 4F A6WE 20030422000272003042200027SO 2003 4 22 AQHA0303001 220030312A7414103915 DISTRIBUTOR BLK CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO RT MAGNETO WORN A AQHAK NONE O OTHER ININSP/MAINT 1 WP11414RM 414A0306 822340R MAGNETO WOULD NOT FIRE DURING MAINTENANCE GROUND RUN. FOUND DISTRIBUTOR BLOCK BUSHING WORN EXCESSIVELY. DISTRIBUTOR GEAR, P/N 10-349237, FINGER HITTING ELECTRODES CAUSING METAL GENERATION. THIS MAGNETO IS A FACTORY REBUILT UNIT, DELIVERED ON A FACTORY REBUILT ENGINE. BOTH ARE 117 HOURS TT. ALL OTHER MAGNETOS ON BOTH ENGINES WERE CHECKED SINCE SERIAL NR'S OF ENGINES AND MAGNETOS WERE CLOSE. FOUND SAME DISCREPANCY ON OTHER ENGINE. REF AQHA0303002. (M) 1L72 3O3 O A7CE E8CE 20030422000852003042200085SO 2003 4 22 SIMA200305013 120030125A532014522460013 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 ABI - DURING AN IMBV INSPECTION A LEVEL 2 FINDING WAS FOUND. CORROSION ON SERVICE DOOR AFT SILL. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M) 2L72 4T RTT00011AT 20030422000902003042200090SO 2003 4 22 SIMA200307102 120030216A532014522460013 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION GALLEY CENTER BEAM GUSSET CORRODED. REMOVED AND INSALLED NEW CETNER BEAM GUSSET IAW EMB 135 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M) 2L72 4F RTT00011AT 20030422001112003042200111SO 2003 4 22 SIMA200305014 120030130A532014522226003 GUSSET EMB 145 EMB145LR 3260212SO LAVATORY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 DURING AN IMBV INSPECTION A LEVEL 2 FINDING FOUND LAVATORY CENTER BEAM GUSSET CORRODED. REMOVED AND REPLACED LAVATORY CENTER GUSSET IAW EMB 145 SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030422001152003042200115SO 2003 4 22 SIMA200307910 120030227A532014522461011 GUSSET EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTIN, DIAMOND GUSSET ON RIGHT HAT BEAM AT FRAME 20 HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET IAW EMB 145 SRM 51-40-03. (M) 2L72 4T RTT00011AT 20030422001242003042200124NM 2003 4 22 USAABB03038 120030311A33509221009 BATTERY BOEING757 7572B7 1384964NM EXIT SIGN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 BDL - FOUND R2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030422001292003042200129NM 2003 4 22 UPS03M40261 120030305A5310ADA02333 DOOR FRAME DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP INSPECTION TYPE: 1C, COMPLY WITH D 234863: FWD LOWER CARGO DOOR FRAME CORRODED STA 895 AT LONGERON 41R AND 43R PERM REPAIR AT C-CHECK (REF ATTACHED EO MD11-53 20-17569-A). GAINED ACCESS TO REPAIR AREA CUT OUT DAMAGED AREA AT FS 895 IAW SRM 53-30-00, FABRICATED REPAIR PART FROM 7075-0 .125 R609936 PER SRM 53-30-00. FABRICATED INTERCOSTAL FROM 7075-0 .063 R868206 IAW ADA02662 -26-03. HEAT TREATED TO T6, INSTALLED REPAIR PARTS IAW 51-33-01, 53-30- 02 INSTALLED PANELS REMOVED FOR ACCESS IAW SRM 53-30-00. 2L73 4F RTA22WE 20030422001402003042200140NM 2003 4 22 UPS03240263 120030217A5712 RIB BOEING727 727108C 1384039NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, LEFT WING, L/E CAVITY SUPPORT RIB CORRODED AT FSS 250 ADJACENT TO WIRING P-CLIP. REMOVED RIB IAW SRM 51-30-02, FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01. REPLACED EXTRUDED TEE TO RIB IAW SRM 51-30-02. INSTALLED RIB IAW SRM 51-30-02. 2L73 4F A3WE 20030423000102003042300010GL 2003 4 23 AUS20030266 220030305A72406871486A LINER BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE COMBUSTION LINER FAULTY. THE LINER WAS NOT CLEAN SO IT WOULD HAVE BEEN DIFFICULT TO ASCERTAIN SERVICEABILITY A POSSIBLE CRACKED WELD APPROXIMATELY 75MM (2.95IN) LONG RUNNING FROM THE 6 O'CLOCK TO THE 8 O'CLOCK POSITION. ONE CRACK APPROXIMATELY 25MM (0.984IN) LONG AT THE 7.30 O'CLOCK POSITION. ONE CRACK APPROXIMATELY 65MM (2.55IN) LONG RUNNING FROM THE 8 O'CLOCK TO 9.30 O'CLOCK POSITION AS YOU LOOK AT THE OPEN END OF THE LINER. 1G71 3U3 U H2SW E4CE 20030423000352003042300035NM 2003 4 23 AUS20030287 120030212A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 27R CONTAINED LEVEL 2 EXFOLIATION CORROSION AT BS 480. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423000892003042300089EU 2003 4 23 BAQA085913 120030404A2430GC134223 CIRCUIT CARD AEROSPAS355 AS355F1 8680810EU NR 2 GENERATOR FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TM178 5059 NR 2 GENERATOR DROPS OFF LINE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030423001012003042300101CE 2003 4 23 GLBA2003013 120030124A79311013890235 TRANSDUCER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE OIL PRESSURE FAILED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03118GL17023 UE118 OIL PRESSURE ON NR 1 ENGINE WENT TO 140 PSI, R&R LEFT OIL PRESSURE TRANSDUCER 2L72 4T4 TRTA24CE E26NE 20030123000242003012300024NM 2003 1 23 2003UALA00040 120030110A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 EXTERNAL FUSELAGE SKIN HAS SEVERAL DENTS BS 289-309, STRINGER 21R-24R. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030123000252003012300025NM 2003 1 23 2003UALA00041 120030110A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 500C + 18, STRINGER 16R, CRACKED JUST AFT OF WING LEADING EDGE LIGHT ASSEMBLY. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICED REPAIR. 2L72 4F4 FRTA16WE E2GL 20030123000262003012300026NM 2003 1 23 2003UALA00042 120030110A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 PRESSURE DECK ABOVE LEFT WING WEB WAS CRACKED AT STA 663 LBL 33. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030123000282003012300028WP 2003 1 23 MWEA030043 120030122A79309144169 TRANSMITTER DOUG DC9 DC932 3022066WP ENGINE DEFECTIVE A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31401ME 47133 RIGHT OIL PRESSURE WAS AT ZERO. -- REMOVED AND REPLACED TRANSMITTER AND BUTT SPLICE. 2L72 4F A6WE 20030123000302003012300030NM 2003 1 23 2003UALA00051 120030113A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STRINGER 16L, STATION 500C, SECTION OF STRINGER CUT OUT FOR ACCESS. MAJOR REPAIR ACCOMPLISHED. REPLACEMENT SECTION OF STRINGER FABRICATED AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030123000312003012300031NM 2003 1 23 2003UALA00052 120030113A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 BS 294 THROUGH 342, RBL 52, RIGHT CREASE BEAM ANGLE CORRODED. MAJOR REPAIR ACCOMPLISHED. TRANSFERED HOLES ONTO NEW CREASE BEAM. INSTALLED NEW CREASE BEAM. 2L72 4F4 FRTA16WE E2GL 20030123000432003012300043NM 2003 1 23 03FDEA00024 120030115A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 EXTERIOR FUSELAGE SKIN HAS 2 DENTS, BS 1090, 3 INCHES ABOVE STR 7R. REPAIRED SKIN IAW SRM. 2L73 4F4 FRTA3WE E2EA 20030325000332003032500033EU 2003 3 25 AWXA200300150 120030206A5315D5347217220290 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND AROUND SEVEN FASTENER HOLES ON LT FLOORBEAM BETWEEN FR 66 - 68, BS 3158. MAINTENANCE REMOVED DAMAGED LT FLOORBEAM BETWEEN FR 66 - 68, BS 3158; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11, PG. 1-2. 2L72 4F RTA28NM 20030325000392003032500039EU 2003 3 25 AWXA200300158 120030204A5315D53112091203 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM FR 16, RBL 28. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM FR 16, RBL 28; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG. 201, PG. 201-206. 2L72 4F RTA28NM 20030325000792003032500079EU 2003 3 25 AWXA200300248 120030301A5315D5347209000200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF CABIN FLOORBEAM AT FR 66-4, Y765. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 66-4, Y765; FABRICATED A REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6-7. 2L72 4F RTA28NM 20030326000022003032600002SO 2003 3 26 AUS20030079 220030114A7310 FILTER CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL ENGINE FUEL CONTAMINATED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) ENGINE FUEL FILTER CONTAMINATED WITH WATER. 1H71 3O3 O A4CE E5CE 5 CP21EA 20030326000072003032600007SO 2003 3 26 AUS20030094 120030131A2842 TRANSMITTER MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL FUEL QTY SENSOR SHORTED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AUXILIARY, RT AUXILIARY AND RT MAIN FUEL TRANSMITTERS FAILED. LT MAIN FUEL TRANSMITTER ERRATIC. THE TRANSMITTER EARTH RETURN BRASS PLATES LOCATED ADJACENT TO THE FLOAT SHAFT HAD WORN THROUGH THE LOCATING PEGS RESULTING IN AN OPEN CIRCUIT. 1H71 3O3 ONC3A23 E286 5 CP920 20030326001042003032600104NM 2003 3 26 A6WA200330004 120030301A2497VF0214 CONTROL UNIT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE ELECTRICAL BUSS FAILED A O OTHER O OTHER NRNOT REPORTED 1 GL31340PH405 3064 DURING TROUBLESHOOTING NON ESSENTIAL BUSS 1 FAILURE THERE WAS A LOUD POP FROM 1VE PANEL, AND FIRE OCCURRED ON INSULATION AND SURROUNDING WIRES. REMOVED AND REPLACED 1VE PANEL AND BUS POWER CONTROL UNIT (BPCU). NO FURTHER OCCURRENCES, NO REPEATS. SUSPECT INTERNAL FAILURE TO THE 1VE CONTACTOR AT THE NON-ESSENTIAL BUS 2. (M) 2H72 4T4 TRTA45NM E20NE 20030327000072003032700007NE 2003 3 27 AWXA200300270 220030313A7230 VANE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE COMPRESSOR DAMAGED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28182AW 22649 WHEN PREPARING FOR TAKEOFF AT DFW EN ROUTE FOR PHX WHEN THROTTLES ADVANCED RECEIVED COMPRESSOR VANE FAULT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE RATIO BLEED CONTROL IAW T/C R5M75002, AND LUBRICATED THE 13TH STAGE BLEED VALVE IAW BMM 75-31-0, PG. 602. RAN ENGINES AT TAKEOFF POWER AND PERFORMED BLEED SCHEDULE; SYSTEM CHECK WAS GOOD. VENDOR BENCH TEST OF PRESSURE RATIO BLEED CONTROL S/N 0101 CONFIRMED FAILURE OF UNIT. REPLACED LEVER (P/N 393909), CONNECTOR, VENT, PIN, AND 2 EACH PINS. UNIT TESTED AND RETURNED TO SERVICE IAW CMM 75-31-01, REV. 16. 2L72 4F4 FRTA16WE E2EA 20030327000252003032700025EU 2003 3 27 AWXA200300297 120030320A2560 BATTERY AIRBUS320 A320231 3930325EU FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28620AW 052 FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT R-1 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY AT THE R-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030327000272003032700027NM 2003 3 27 AWXA200300299 120030322A5210 DOOR AIRBUSA319 A319132 3930340NM PAX OUT OF RIG A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28803AW 931 EN ROUTE FROM LAS TO MIA THE FLIGHT DECK DOOR WAS EXTREMELY HARD TO OPEN. DOOR WOULD NOT CLOSE PROPERLY AND THE UPPER & CENTER LATCH WOULD NOT ENGAGE. MAINTENANCE RIGGED THE FLIGHT DECK DOOR IAW AMM 52-51-11, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030327000332003032700033EU 2003 3 27 AWXA200300305 120030316A5321D5367002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 950, FR 24, TO BS 1163, FR 28. MAINTENANCE PERFORMED BOND REPAIR ON UPPER SURFACE OF CABIN FLOOR PANEL BS 950, FR 24, TO BS 1163, FR 28 IAW A320 SRM 53-02-00, PG. 203-207, FIG. 202. 2L72 4F RTA28NM 20030327000342003032700034EU 2003 3 27 AWXA200300306 120030316A5321D5367002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 2136, FR 47, TO BS 2350, FR 51. MAINTENANCE REMOVED DAMAGED FLOOR PANEL BS 2136, FR 47, TO BS 2350, FR 51; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW AWA E.O. 53-22-03. 2L72 4F RTA28NM 20030327000352003032700035EU 2003 3 27 AWXA200300307 120030316A5321D5367005300000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 3158, FR 66, TO BS 3257, FR 68. MAINTENANCE REMOVED DAMAGED FLOOR PANEL BS 3158, FR 66, TO BS 3257, FR 68; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW AWA E.O. 53-22-03. 2L72 4F RTA28NM 20030327000422003032700042NM 2003 3 27 AWXA200300314 120030228A5320146N52407 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON SUPPORT ANGLE ON UNDER SIDE OF SHEAR DECK AT BS 1715, LBL 35-40. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT BS 1715, LBL 35-40; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 146N5240-7. 2L72 4F RTA2NM 20030327000532003032700053NM 2003 3 27 C1HA200382002 120030210A2612 CONNECTOR BOEING727 7272S7 138407ZNM NR 2 ENGINE DISCONNECTED A C1HAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL15682CA 22019 FIRE WARNING TEST FAILED NR 2 ENGINE "B" LOOP. INSPECTED FOUND CONNECTOR PLUG AT ENGINE LOOP DISCONNECTED. RE-CONNECTED OPS CHECK GOOD IN REF TO MM 26-11. 2L73 4F A3WE 20030327000552003032700055NM 2003 3 27 C1HA200382004 120030222A2612 FIRE LOOP BOEING727 7272S7 138407ZNM NR 1 ENGINE OUT OF POSITION A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15682CA 22019 NR 1 GROUND FAULT FIRE DETECTION SYSTEM LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 1 ENGINE FIRE LOOP IAW M/M 26-11-01 GRND OPS. CHECKS GOOD. 2L73 4F A3WE 20030327000572003032700057NM 2003 3 27 C1HA200383003 120030226A2612 FIRE LOOP BOEING727 7272S7 138407ZNM NR 1 ENGINE OUT OF POSITION A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15683CA 22490 IN FLIGHT NR 1 ENGINE FIRE DETECTOR GRND CIRCUIT LIGHT FLICKERED OCCASIONALLY. REPOSITIONED FIRE DETECTION LOOP, LIGHT STAYS OUT NO DEFECTS NOTED 2L73 4F A3WE 20030327000592003032700059NM 2003 3 27 C1HA200383005 120030211A3350 BATTERY BOEING727 7272S7 138407ZNM CABIN INTERMITTENT A C1HAO OTHER O OTHER NRNOT REPORTED 1 GL15683CA 22490 ROW 32 EXIT SIGN WORKS INTERMITTENT. R & R ROW 32 EXIT LIGHT BATTERY CARTRIDGE AND BATTERY POWER SUPPLY IAW MM 33-50-71 GROUND OPS CHECK NORMAL. 2L73 4F A3WE 20030327000672003032700067NM 2003 3 27 C1HA200393001 120030216A2612 CONTROL PANEL BOEING727 727212 138407GNM ENG FIRE DETECT DISLODGED A C1HAO OTHER O OTHER CRCRUISE 1 GL15293AS 21348 ENGINE NR 2 SYSTEM A ENGINE FIRE DETECTION ANNUNCIATION POPPED OUT. UNABLE TO LOCATE. R & R FIRE DETECTION CONTROL PANEL IAW M/M 26-11-0. OPS CHECK GOOD. 2L73 4F A3WE 20030327001092003032700109SO 2003 3 27 C2XA03CL026 120030201A3231 DOOR EMB 145 EMB145LR 3260212SO NLG OUT OF ADJUST A C2XAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW2713903 145479 CLE FLIGHT 2104 THE CREW REPORTED NOSE VIBRATION IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RIGHT NOSE GEAR DOOR OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE RIGHT NOSE GEAR DOOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030327001112003032700111SO 2003 3 27 C2XA03CL030 120030204A2621 CONNECTOR EMB 135 EMB135ER 3260203SO EXTINGUISHER LOOSE A C2XAO OTHER N FALSE WARNING CRCRUISE 1 SW2727512 145274 CLE FLIGHT 2083 THE CREW REPORTED A EXTINGUISHING BOTTLE -B- ENGINE 1/2 MESSAGE INTERMITTENTLY IN FLIGHT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED CANNON PLUG ON EXTINGUISHING BOTTLE -B- AND SECURED LOOSE BACKSHELL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030327001462003032700146SO 2003 3 27 C2XA03IA014 120030202A335066368 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713956 145078 DURING MAINTENANCE THE MECHANIC NOTED THAT THE LAST EMERGENCY LIGHT FLOOR PROXIMITY STRIP FAILED TO ILLUMINATE. MAINTENANCE RELEASED THE AIRCRAFT IWA MEL. MAINTENANCE REMOVED AND REPLACED THE LAST EMERGENCY LIGHT FLOOR PROXIMITY LIGHT STRIP, PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030320001592003032000159EU 2003 3 20 2003UALA00152 120030206A2120 ODOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29439UA 683 RETURNED TO FIELD DUE TO ELECTRICAL ODOR IN COCKPIT. 2L72 4F4 FRTA28NM E40NE 20030320001622003032000162NM 2003 3 20 2003UALA00154 120030206A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 LEFT FUSELAGE WING ROOT FRAME CRACKED AT STATION 540 S22L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030423001162003042300116NM 2003 4 23 KNNA200300001 120030224A5330 SKIN BOEING737 737297 1384480NM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A KNNAK NONE O OTHER ININSP/MAINT 1 WP25147AW54001 22630 AIRCRAFT AT MAINT. BASE FOR "A3" CHECK COMPLIANCE. IN C/W TASK CARD A-07A A 1.8 INCH CRACK WAS FOUND IN EXTERIOR FUSELAGE SKIN AT LT BS 757 BELOW STR 17. A NON-ROUTINE T030446 AND ACO 035313R00 WAS ISSUED TO DOCUMENT SRM REPAIR CH 53-30-3 FIG 25. CRACK IN SKIN AREA WAS REMOVED. A FILLER AND DOUBLER WAS INSTALLED. 2L72 4F4 F A16WE E2EA 20030423001412003042300141EU 2003 4 23 UO22003F00000 120030225A32416000480 CONTROL BOX AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP MLG ANTI SKID MALFUNCTIONED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL1920CF 106 ANTISKID TEST PROBLEM. INTERMITTENTLY, THE RIGHT LIGHT WOULD NOT COME ON DURING TEST. DISCONNECTED THE LT AND RT INPUT CONNECTORS FROM THE ANTISKID CONTROL BOX. ALL INPUTS TO THE BOX WERE CHECKED. NO DEFECTS WERE FOUND. TRIED ANTISKID TEST PUSHBUTTON. WHEN BUTTON IS PRESSED AND RELEASED, THE LT AND RT BRAKE LIGHTS SHOULD ILLUMINATE, THEN GO OUT. TRIED SYSTEM SEVERAL TIMES. THE RT FAILED ONCE. SWAPPED INPUT CONNECTOS ON THE ANTISKID CONTROL BOX AND REPEATED TEST. THE LEFT LIGHT INTERMITTENTLY WOULD NOT COME ON. PROBLEM WAS INSIDE THE ANTISKID CONTROL BOX. (WO 152570) 2L72 4F4 F A33EU E6WE 20030423001452003042300145WP 2003 4 23 ZW0A0303005 120030306A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 AT STA 160 THE FRAME FOOT WAS DAMAGED AT LONGERON 20R TO LONGERON 18R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030423001602003042300160EU 2003 4 23 MALA030199 120030313A3020 MODULE SAAB SF340 340B 7860101EU DEICE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15447XJ 340B447 DURING FLIGHT 2797, LEFT ENGINE INTAKE CAUTION LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE RAN AC LT LIGHT ILLUMINATED AFTER 30 SECONDS. REPLACED DEICE CONTROL MODULE, RAN AC FOR 15/20 MINUTES AND NO FAULTS AT THIS TIME. ALL SYSTEM CHECK NORMAL IAW SF340 MM CHAP 30. 2L72 4T RTA52EU 20030423001622003042300162NM 2003 4 23 PCAA0303056 120030316A3242 BRAKE DHAV DHC8 DHC8102 2809003NM MLG FAILED A PCAAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA13835EX 289 PHL-FLIGHT 3503 CREW REPORTED NORMAL BRAKES FAILED WHEN TAXIING IN WITH ONLY NR 2 ENGINE OPERATING AND STANDBY PUMPS ON. MAINTENANCE BLED ALL BRAKES, TAXIED AIRCRAFT ON NR 1 ENGINE. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030423001652003042300165EU 2003 4 23 MALA030201 120030309A3240189400002 CONTROL CABLE SAAB SF340 340B 7860101EU BRAKE SYSTEM LACK OF LUBE A MALAK NONE O OTHER ININSP/MAINT 1 GL15363PX 340B260 RIGHT BRAKE IS VERY WEAK, LEFT SEEMS OK, CAN'T STOP STRAIGHT. FROM LOG PAGE MM1 1162583 DISC 13 RT BRAKE SEEMS WEAK NOTED NOISED AND RESISTANCE REOM RT BRAKE PEDAL. CAPT SIDE FOUND CAPT RT BRAKE PEDAL TO BE MAKING DRY AND GRAVELY SOUND IN WHEEL WELL. MAINTENANCE REMOVED AND REPLACED RT IB BRAKE CONTROL CABLE PER SF340 AMM 32-42-05-4 P/N 189400-002. OPS AND TAXI CHECK GOOD. REF TO CONT CARDS 069629 AND 069630 FOR WORK DETAIL. 2L72 4T RTA52EU 20030423001682003042300168WP 2003 4 23 ZW0A0303101 120030310A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13901TW 49166 THE OVERHEAD EMERGENCY LIGHT AT SEATS 8 THRU 12 WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 6-28-2002 STL. 2L72 4F A6WE 20030423001872003042300187NM 2003 4 23 VNAA0303008 120030306A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL07439JS1068 840 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 TO 6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030423001942003042300194NM 2003 4 23 UPS03240299 120030214A5310 SUPPORT FITTING BOEING727 727108C 1384039NM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, CRACK FOUND AT CLEAT BETWEEN MCD SUPPORT FITTING AND FRAME AT STA 540 WL 207 CRACK START AT RIVET TO EDGE OF CLEAT .375 INCH. REPAIR CARRIED OUT IAW SRM 51-40-3. 2L73 4F A3WE 20030423002082003042300208NM 2003 4 23 UPS03240308 120030218A5753 ATTACH FITTING BOEING727 727108C 1384039NM NR 7 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, NR 7 FLAP TRACK HAS SURFACE CORROSION ON FWD MOUNT LUG FACES A & D AND IN FWD LUG BOREHOLES. REPAIR CARRIED OUT IAW SRMO EO'S 2002-008-002 & 2003-008-011. UPS ENGINEERING FILE NR 727-57-20093. 2L73 4F A3WE 20030424000072003042400007EA 2003 4 24 SWIA200311831 120030314A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 1 SPOILER MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07924SW 7681 SPOILERON FAULT STATUS MESSAGE ON TAXI OUT. RETURNED TO GATE. REPLACED NR 1 SECU PER CRJ MM 27-61-05. PERFORMED OPS CHECK OF SPOILERONS. OPS CHECK GOOD. S/N OFF 01664. 2L72 4F RTA21EA 20030424000132003042400013NM 2003 4 24 QXEA0300383 120030308A5540 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX- DURING DAILY CHECK FOUND CRACK IN HOLE ON LEFT HAND SIDE OF AFT RUDDER. REPAIRED IAW DHC-8 Q400 RD 8/4-55-075. 2H72 4T RTA13NM 20030424000192003042400019NE 2003 4 24 UPS03540312 220030319A7230 COMPRESSOR BOEING757 75724APF 1384969NM PWA 2037 PW2040 NE LT ENGINE STALLED A IPXAA UNSCHED LANDING AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01418UP 23905 P726519 AT FIRST POWER REDUCTION AFTER TAKEOFF LEFT ENGINE COMPRESS OR STALL OBSERVED. GROUND OBSERVERS NOTED FLAME SMOKE FOR 1 SECOND DURING HOLDING PATTERN, WITH EPR AT 1.25, LEFT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 125 & 165 PSI AND VIB. COMPLIED WITH FIM 71-05-00 EXAMINED MEG CHIP DETECTORS & REPLACED MAIN OIL FILTER, NO DEFECTS NOTED. INLET AND EXHAUST VISUALLY CK OK, EPCS SHOWS NO MSG, OK FOR SERVICE. 2L72 4F4 FRTA2NM E17NE 20030424000262003042400026WP 2003 4 24 UPS03840330 120030320A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: PFLT, ON PREFLIGHT EMERGENCY EXIT LIGHTS INOP, SAME MALFUNCTION ON 3/19/03. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS NORMAL. 2L74 4F RT4A25 20030424000312003042400031WP 2003 4 24 ZW0A0303209 120030318A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13907TW 49165 THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE 20 INCH FLEX ASSEMBLY. CHECK-C 1-30-03 STL. 2L72 4F A6WE 20030320001642003032000164NM 2003 3 20 2003UALA00156 120030205A2420V99167762308 RAM AIR TURB AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE AUX ELECTRICAL FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29848UA 1647 RAT TEST FAILED RPM TEST. REPLACED RAM AIR TURBINE. 2L72 4F4 FRTA28NM E40NE 20030320001662003032000166NM 2003 3 20 2003UALA00160 120030207A2120 SMOKE BOEING757 757222 1384956NM PWA 2037 PW2037 NE LAVATORY DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29540UA 25252 FLASH REPORTED NEAR MID-LAV, THEN SMOKE COMING OUT OF LAV. NO FLAME OR FIRE REPORTED. 2L72 4F4 FRTA2NM E17NE 20030320001682003032000168NM 2003 3 20 SWAA030613 120030318A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, BELOW STR 21L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030320001822003032000182 2003 3 20 SWAA030604 420030316A25656557463 FITTING BOEING737 7373H4 1384600NM FWD SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING LOOSE. R&R FASTENERS PER SRM. 2L72 4F RTA16WE 20030321000022003032100002CE 2003 3 21 048076 120030221A5314 KEEL BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA FUSELAGE GOUGED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07218YV UE218 WHILE DOING AN INSPECTION, MAINTENANCE DISCOVERED THE LT INBOARD MAIN LANDING GEAR KEEL WAS GOUGED. MAINTENANCE REPAIRED THE KEEL. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T3 TRTA24CE E4EA 20030321000032003032100003NM 2003 3 21 SWAA030624 120030314A5311694036723 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030321000052003032100005NM 2003 3 21 SWAA030626 120030319A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 500 + 4 @ STR 10R, BS 500A @ STR 10R & BS 500D + 10 BETWEEN STR 10L & STR 13L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030321000092003032100009EU 2003 3 21 126291 120030320A3250 LINKAGE SAAB SF340 SF340A 7850100EU NLG STEERING LACK OF LUBE A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL17146SD 146SD FLIGHT 4503 LEAVING CRW. WHILE TAKING OFF, FELT THE NOSE WHEEL SHIMMY AT AROUND 70 KNOTS. THE ABORTED THE TAKE OFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE NOSE LANDING GEAR AND STEERING LINKAGE. LUBRICATED NOSE STRUT AND LINKAGE. TAXI CHECKED AIRCRAFT. OPS CHECKED GOOD 2L72 4T RTA52EU 20030321000122003032100012NM 2003 3 21 2003UALA00166 120030212A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 AFT CABIN FUSELAGE STRINGER OUTBOARD SURFACE DENTED APPROXIMATELY BODY STATION 1004 STRINGER 14L. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. 2L72 4F4 FRTA16WE E2GL 20030321000152003032100015NM 2003 3 21 2003UALA00172 120030211A5315 FLOORBEAM BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29211UA 30217 STATION 246 FLOORBEAM WAS CRACKED AT RBL 38.5 AND LBL 38.5. MAJOR REPAIR ACCOMPLISHED. BOTH CRACKS WERE REPAIRED AT 'C' CHECK. 2L72 4F4 FRTT0001SE E46NE 20030321000212003032100021EU 2003 3 21 2003UALA00179 120030215A3397 WIRE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHTSDAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29430UA 568 INTERIOR EMERGENCY LIGHTS WILL NOT TEST, FOUND CIRCUIT BREAKER, H5 POPPED. RESET AND TRIED AGAIN NO HELP CIRCUIT BREAKER POPPED AGAIN. SUPPLEMENTAL DATA UPDATE FOUND WIRE PINCHED BETWEEN SEAT AND SEAT TRACK AT ROW 10. REMOVED DAMAGED WIRE AND SPLICED WIRE. LIGHTS OPERATE NORMALLY AND TEST OK FROM PTP. 2L72 4F4 FRTA28NM E40NE 20030321000252003032100025EU 2003 3 21 128391 120030321A2121 FAN SAAB SF340 SF340A 7850100EU BURNED OUT A UHLAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL1740SZ 40SZ On start up flight 4510 in cle, when aircrew switched on the recirulating fan. After a monment they noticed the fan stopped running and there was smoke in the cabin. The crew shut down the engines. Maintenance pulled up floor boards and found the recirulating fan had failed causing smoke in cabin. 2L72 4T RTA52EU 20030321000382003032100038SO 2003 3 21 C2XA03CL074 120030320A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN DEFECTIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714542 145547 DURING MAINTENANCE THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE.MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY CHARGER.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030321000402003032100040NM 2003 3 21 CALA0300120 120030319A5230 SKIN BOEING737 7373T0 1384582NM C-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712327 23457 INSPECTION FOUND A 5" CRACK IN SKIN AT AFT CARGO DOOR INSIDE INSPECTION HOLE ABOVE HANDLE BOX. A DOUBLER WAS INSTALLED IAW ECRA 5232-01024. 2L72 4F RTA16WE 20030321000442003032100044NM 2003 3 21 CALA0300124 120030320A5330 SKIN BOEING737 7373T0 1384582NM STA 727E CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 1.125" CRACK IN FUSELAGE SKIN AT STA 727E, S24R. A REPAIR WAS INSTALLED IAW ECRA 5330-03229 WITH A PERMANENT REPAIR TO FOLLOW NO LATER THAN 31 MARCH 2003. 2L72 4F RTA16WE 20030321000462003032100046NM 2003 3 21 CALA0300126 120030320A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED ON TOP SURFACE AT NUTPLATE AND LOWER SURFACE AT STA 312, RBL 20 TO RBL 31. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, PAGE 205, 51-40-02, AND 51-20-01. 2L72 4F RTA16WE 20030321000502003032100050NM 2003 3 21 CALA0300130 120030320A5330 SKIN BOEING737 737524 1384721NM STA 400 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716617 27330 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 400 BELOW STRINGER 17L. A REPAIR WAS INSTALLED IAW SRM 53-00-01. 2L72 4F RTA16WE 20030321000522003032100052NM 2003 3 21 CALA0300132 120030320A5347 SEAT TRACK BOEING777 777224 1385225NM BS 1485-1520 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2774007 29477 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1485-1520, RBL 74. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 3, FIGURE 202. 2L72 4F RTT00001SE 20030321000532003032100053WP 2003 3 21 DHL2003805006 120030320A2611 BULB DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01805DH 46125 1) #7 SMOKE DETECTOR WILL NOT TEST.2) REMOVE AND REPLACED BULB. CHECKED GOOD PER 26-00. 2L74 4F RT4A25 20030321000542003032100054EA 2003 3 21 03076646 120030317A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27646BR 7392 During maintenance inspection the L/H fwd overwing emergency exit light was found to be inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030321000592003032100059EA 2003 3 21 COMA0360154 120030317A3230864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS DEDESCENT 1 SO01781CA16273 7312 FLIGHT 5761 GEAR DISAGREE WARNING, NLG FAILED TO EXTEND.REPLACED THE PSEU. 2L72 4F RTA21EA 20030321000602003032100060EA 2003 3 21 COMA0360153 120030316A3230 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01940CA 7048 FLIGHT 5930 GEAR DISAGREE WARNING, NLG FAILED TO RETRACT.ADJUSTED THE NLG "CENTERED" PROXIMITY SENSOR. 2L72 4F RTA21EA 20030321000652003032100065NM 2003 3 21 2003UALA00204 120030219A5754114W41307 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 3 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 DELAMINATED SKIN ON TRAILING EDGE WEDGE, SLAT NR 3, AND SEAL FOAM CORE MISSING SECTION. REPAIRED TRAILING EDGE WEDGE SLAT NR 3. REPLACED SEAL FOAM CORE SECTION. 2L72 4F4 FRTT0001SE E46NE 20030321000682003032100068NM 2003 3 21 2003UALA00207 120030219A5754114W41408 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLAT NR 11 DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 LOWER SKIN DELAMINATED ON TRAILING EDGE WEDGE, SLAT NR 11. REPAIRED TRAILING EDGE WEDGE, SLAT NR 11. 2L72 4F4 FRTT0001SE E46NE 20030321000702003032100070NM 2003 3 21 2003UALA00210 120030225A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29953UA 26700 STATION 178 BULKHEAD UPPER RIGHT ANTENNA MOUNT UPPER OUTBOARD ATTACH POINT HAS CRACK INDICATION. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030321000722003032100072NM 2003 3 21 2003UALA00213 120030226A5310 DOOR FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29953UA 26700 FORWARD GALLEY DOOR FRAME IS CRACKED AT FLOOR STATION 294.5. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030321000942003032100094NM 2003 3 21 UPS03240320 120030305A5310 BRACKET BOEING727 72725C 138400HNM FWD CARDO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 INSPECTION TYPE:C FWD.CARGO DOOR FUSELAGE CUTOUT AFT LWR.DOOR STOP FITTING CRACKED. FABRICATED NEW BRACKET IAW.SRM.51-20-1 REPLACED BRACKET IAW SRM 51-30-2. 2L73 4F A3WE 20030321000982003032100098NM 2003 3 21 2003UALA00240 120030302A5755 RIB BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 SPOILER CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29650UA 25287 NR 2 SPOILER ACTUATOR OUTBOARD SUPPORT RIB CRACKED AT LOWER AFT LEG. MAJOR REPAIR ACCOMPLISHED. REPLACED #2 SPOILER ACTUATOR OUTBOARD HINGE FITTING. 2L72 4F4 FRTA1NM E24NE 20030729000412003072900041NM 2003 7 29 ZW0A0306001 120030713A256069B148551 SPRING BOEING757 7572Q8 1384972NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13707TW 27625 THE EVACUATION SLIDE GIRT BAR LEAF RETENTION SPRING AT THE R1, L2, AND R4 DOOR WERE DEFORMED AND ADJUSTED. THE RETENTION SPRING AT THE L4 DOOR WAS REPLACED ACCOUNT DEFORMED. 2L72 4F RTA2NM 20030729000742003072900074NM 2003 7 29 QXEA200300741 120030615A5420 STRAP DHAV DHC8 DHC8202 2809007NM NACELLE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - THE FORWARD LAND STRAP FOR PANEL 422DT HAS CORROSION FORWARD OF THE FASTENERS. MAINTENANCE BLENDED, MAPPED, CHECKED FOR THICKNESS, AND REPAIRED THE AFFECTED AREA IAW EA 2-54-171. 2H72 4T RTA13NM 20040223000192004022300019 2004 2 23 WVBA2003004 420031224A2200 AUTOPILOT SYS PIPER PA31 PA31350 7103110SO MALFUNCTIONED E WVBAO OTHER O OTHER NRNOT REPORTED 1 AL01 IN THE SUPPLIED DOCUMENTATION FROM S-TEC WE HAVE BEEN ABLE TO FIND ANY INFORMATION ABOUT AUTOPILOT LOSS-IN-TURN AND OTHER CRITICAL LIMITS. THIS SEVERELY HAMPERS OUR ABILITY TO DETERMINE WHETHER OR NOT OUR AUTOPILOT IS OPERATING IN A CORRECT FASHION. 1L72 3O A20SO 20040223000312004022300031CE 2004 2 23 FFK2004F00000 120031111A1430458150031 BOLT BEECH 58 58 1152740CE CONT O520 IO520* 17032SO ROD END FAILED B FFKRO OTHER O OTHER NRNOT REPORTED 1 SO05707RA TH257 UPON LANDING, NOTICED THAT THE RT SIDE IB GEAR DOOR WAS NOT IN THE STOWED POSITION. CAUSE OF FAILURE, THE ROD END THAT CONTROLS MOVEMENT OF THE IB GEAR DOOR HAD EXCESSIVE WEAR CAUSING THE BOLT TO SHEAR AND ALLOWING GEAR DOOR TO SWING FREELY. 1L72 3O3 O 3A16 E5CE 20040223000372004022300037NE 2004 2 23 RAIA00312327 220031229A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RIGHT OUT OF ADJUST A RAIAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 CE03563HK 41079 75083 5364-BWI- RT ENGINE QUIT ON LANDING ROLL. MAINTENANCE ADJUSTED ENGINE DECELERATION SCHEDULE, AND OPS CK OK. 2L72 4T4 TRTA41NM E18NE 20040223000562004022300056CE 2004 2 23 FFK2004F00002 120031117A3230 O-RING BEECH 58 58 1152740CE CONT O520 IO520* 17032SO RETRACT MECH FAILED E FFKRO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0511HW 82 TH271 INSTALLED RETRACT MECHANISM. AFTER 38 HOURS ALL OIL LEAKED OUT, DETERMINED THERE WAS A BAD O-RING REMOVED FOR WARRANTY REPAIR. REINSTALLED SAME RETRACT MECHANISM. AFTER 44 HOURS, BELLCRANK AND DOWN LIMIT ARM GOT BENT (UNKNOWN HOW THIS HAPPENED), WITH ARM BENT IT WAS NOT CONTACTING THE MICROSWITCH TO INDICATE DOWN AND LOCK ALLOWING THE GEAR MOTOR TO CONTINUE TO RUN, OVER EXTENDING THE DOWN LIMITS ON THE GEARBOX AND DAMAGING IT. (SO05200405787) 1L72 3O3 O 3A16 E5CE 20040223000852004022300085NM 2004 2 23 DHL200374267 120031125A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING (C) CHECK; NR 5 SEAT TRACK AT BS 760-850 IS DAMAGED. REMOVED SEAT TRACK AT BS 760-850 FOR REPAIR IS OUT OF LIMITS IAWSRM 51-30-2 AND 51-10-1 FIG.3,FABRICATED NEW SEAT TRACK IAW SAMPLE IAW B727 SRM 51-10-1 DIM.95",USED BAC-1520-841 PO NR 323569 IAW B727 SRM 51-10-2 INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040223001072004022300107NE 2004 2 23 638LJ112403 220031124A7320189111 HYDROMECH UNIT LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE LT ENGINE MALFUNCTIONED G AOQAA UNSCHED LANDING EXJVIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA11638LJ3567 038 PCE305194 DURING CRUISE FLIGHT AT 39,000 FEET, A BANG WAS HEARD FOLLOWED BY LT ENGINE SHUTDOWN AND ILLUMINATION OF BOTH LT ENGINE COMPUTER LIGHTS AND OIL PRESSURE DROP. MFG NOTIFIED. INITIAL EVALUATION REVEALED NO MECHANICAL DAMAGE OR DEFECTS NOTED TO ENGINE ASSY. DOWNLOAD AND INTERROGATION OF EDU INDICATED THE PROBABLE CAUSE TO BE POSSIBLE ELECTRONIC FUEL CONTROL FAILURE. RESTART WAS ATTEMPTED ALTHOUGH UNSUCCESSFUL, AIRCRAFT WAS DIVERTED AND SINGLE ENGINE LANDING WAS ACCOMPLISHED UNEVENTFULLY. (EA11200402145) 2L72 4F4 FRTA10CE E35NE 20040223001212004022300121 2004 2 23 00127 420030107A34215200007 GYRO LEAR 25 25 5170506CE COCKPIT MALFUNCTIONED E HAEAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 SW05147TW 023 PILOT REPORTED AFTER DEPARTING ADS THE CO-PILOTS HIS FLAGGED, RETURN TO ADS FOR MAINTENANCE, HEADING FLAG ON CO-PILOT HIS OPERATES NORMAL ,FOUND BAD CONNECTION AT THE DG REMOVED AND REPLACED DG. OPS CHECK NORMAL. 2L72 4J A10CE 20030321000192003032100019NM 2003 3 21 2003UALA00176 120030213A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29952UA 26699 RIGHT LOWER FUSELAGE SKIN HAS EXCESSIVE MATERIAL LOSS 25 PERCENT, .036 ORIG . 027 AT DEEPEST AREA. STA 450 S25R AND STATION 435 4 IN BELOW LOWER AFT CORNER OF FORWARD CARGO DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHMENT. INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20030321000202003032100020NM 2003 3 21 2003UALA00178 120030217A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29954UA 26739 FUSELAGE SKIN DAMAGED AT STATION 815 STRINGER 18R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030321000222003032100022NM 2003 3 21 03074416 120030315A3350321430 BATTERY DORNERDO32 DO328300 NM A VTZAK NONE O OTHER ININSP/MAINT 1 EA27416FJ 3171 During maintenance inspection the emergency floor track lights at seat rows 4 and 6 were found to be inoperative. Maintenance personnel removed and replaced the emergency battery at position 5LK. An operational check was satisfactory and the aircraft was returned to service. 2H72 4T RTA55NM 20030321000272003032100027NM 2003 3 21 2003UALA00182 120030217A3397 CONNECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 EMERGENCY FLOOR LIGHTING, FLASHING ON AND OFF ON LEFT SIDE OF ECONOMY SECTION BETWEEN ROWS 18-26. FOUND CONNECTOR PLUG LOOSE AND RECONNECTED IT. SYSTEM CHECKED OK. 2L72 4F4 FRTA1NM E24NE 20030321000352003032100035NM 2003 3 21 2003UALA00192 120030219A5321 FLOOR PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29555UA 26647 AFT CABIN FLOOR PLATE CORR0DED AT STA 1680 - 1684, RBL 45 TO RBL 53. RECHECKED FOR EXCESSIVE MATERIAL LOSS AT STA 1681 RBL 49-50 AND RBL 51-53. MAJOR REPAIR ACCOMPLISHED. AFT CABIN FLOOR DECK PLATE CORROSION BLENDED AND REPAIR DOUBLER INSTALLED AT STA 1681. 2L72 4F4 FRTA2NM E17NE 20030321000362003032100036NM 2003 3 21 2003UALA00193 120030221A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29332UA 24193 SKIN IS CREASED NEAR THE FORWARD LAV SERVICE PANEL. 2 CREASES ARE WITHIN LIMITS OF SRM, BUT DAMAGE TO FRAME IS BEYOND LIMITS. MANUFACTURED AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030321000482003032100048NM 2003 3 21 CALA0300128 120030320A5330 SKIN BOEING777 777224 1385225NM BS 676 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2774007 29477 INSPECTION FOUND L/H FUSELAGE SKIN DENTED AT BS 676 BETWEEN S27L AND S28L. REPAIRED IAW SRM 53-00-01, REPAIR 7, FIGURE 202. A DIP WAS INITIATED TO REINSPECT THE REPAIR AT 30,000 FLIGHT CYCLES WITH REPEAT INSPECTION AT 16,000 FLIGHT CYCLES PER SRM 53-00-01, REPAIR 7, TABLE 204. 2L72 4F RTT00001SE 20030321000512003032100051NM 2003 3 21 CALA0300131 120030320A5330 SKIN BOEING737 737524 1384721NM STA 380 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716617 27330 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 380, STRINGER 17L. INSTALLED REPAIR IAW SRM 53-00-01. 2L72 4F RTA16WE 20030320000562003032000056NM 2003 3 20 USAASB03027 120030216A3260189929 UPLOCK SENSOR BOEING737 7373B7 1384580NM RT MLG DIRTY A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19390US 23312 ATL - FLT 1711 - AFTER 15 MINUTES AFTER TAKEOFF FROM CLT, EN ROUTE TO MSY, CAPTAIN REPORTED THE RIGHT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR HAD BEEN RECYCLED THREE TIMES. CREW ALSO NOTED THAT THE AUTOBRAKE DISARM LIGHT REMAINED ILLUMINATED WITH SWITCH IN OFF POSITION. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CLEANED AND CHECKED THE RIGHT MLG UPLOCK PROXIMITY SENSOR PER MM 32-61-21. OPS TEST NORMAL. THE AUTO BRAKE SYSTEM WAS PLACED ON MEL. (M) 2L72 4F RTA16WE 20030320000582003032000058NE 2003 3 20 Y2PA03001 220030106A7230 ENGINE AMD FALCONFALCON20 2730103EU GE CF700 CF7002D 30010NE NR 1 FOD A Y2PAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL23818AA10478 036 NR 1 ENG LOST PWR IN FLT, POST FLT INSPECT REVEALED DAMAGE TO COMPRESS. A/C CRUISING AT INTERMEDIATE (12000 FT) ALTITUDE INBOUND (DESCENDING). CREW HEARD/FELT COMPRESS STALL ON NR 1 ENG, ACCOMPANIED BY EGT RISE AND RPM LOSS. CREW DECLARED EMERGENCY WHILE TROUBLESHOOTING & MADE A NORMAL APPROACH & LANDING AFTER RESTORING (REDUCED THRUST) PWR. MAINT SENT TO EVALUATE ENG. INSPECT OF ENG FOUND FOD TO COMPRESSOR. 1ST STAGE BLADES BENT WITH NO LEADING OR TRAILING EDGE TEARS OR NICKS. LATER STAGES OF COMPRESSOR HAVE BENT & TORN BLADES. ENG U/S AND BEING REPLACED. IT IS SUSPECTED THAT FOD WAS CAUSED BY ICE INGESTED INTO THE COMPRESSOR INLET. UPON COMPLETION OF ENG CHANGE THE A/C WILL BE RETURNED TO SERVICE. 2L72 4F4 FRTA7EU E7EA 20030320000612003032000061EU 2003 3 20 03FDEA00328 120030314A5310 STRUCTURE AIRBUS300 A300B4605R 3930308EU AIRFRAME VIBRATION A FDEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO25661FE 760 ON TAKE OFF, A LOUD THUMP WAS HEARD AND THE AC PULLED LT. GEAR WAS LEFT DOWN & RETURN TO LAND. ON LAND EVERYTHING SEEMED NORMAL AIRCRAFT STEERED STRAIGHT AND WITH NO PULL. NO VIBRATION OF ANY SORT. NO TIRES BLOWN. AC IN WORK FOR FUTHER TROUBLESHOOTING PERFORMED WALK AROUND INSP NO EXT DAMAGE FOUND, MOVED ALL FLT CTRLS NO DAMAGE FOUND. NEEDS MORE TROUBLESHOOTING PERF FLT CONTROL TEST PER AIRBUS 300 MM 27-00-00-5. FND, NO FAULT, NEEDS MORE TROUBLESHOOTING. 2L72 4F RTA35EU 20030402000182003040200018NM 2003 4 2 03FDEA00335 120030308A5712ARB2850505 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING LE CAVITY, FOUND NR 16 TRACK ATTACH FITTING INBOARD SIDE CRACKED. LT WING L/E CAVITY NR 16 TRACK I/B CRACKED FITTING REMOVED AS PER SRM 51- 33-01, VOL. II AND NEW FITTING INSTALLED AS PER SRM 51-31-01, VOL. II. 2L73 4F RTA22WE 20030320000842003032000084 2003 3 20 2003UALA00063 420030116A34144039891903 INDICATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE AIRSPEED FAILED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29525UA 24978 CAPTAINS AIRSPEED INDICATOR FLAGGED. CAPTAIN'S MACH/AIRSPEED INDICATOR FAILED AND WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20030320000892003032000089NM 2003 3 20 2003UALA00073 120030121A5310 ANGLE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 RT CREASE BEAM INBOARD ANGLE CORRODED AT BODY STATION 957. MAJOR REPAIR ACCOMPLISHED. REPLACED RT CREASE BEAM INBOARD ANGLE. 2L72 4F4 FRTA16WE E2GL 20030320000942003032000094NM 2003 3 20 2003UALA00083 120030123A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 FUSELAGE SKIN BLENDED BEYOND LIMITS STATION 227 STRINGER 20R AT EXT POWER PANEL RECPT. MAJOR REPAIR ACCOMPLISHED. SKIN DOUBLER WAS INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030320001072003032000107NM 2003 3 20 2003UALA00098 120030126A5270 WARNING SYSTEM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CARGO DOOR ACTIVATED A UALAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29654UA 25392 FORWARD CARGO DOOR EICAS INDICATION AFTER DEPARTURE. 2L72 4F4 FRTA1NM E24NE 20030320001112003032000111NM 2003 3 20 2003UALA00102 120030127A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FUSELAGE AT STATION 887, FRAME AT STRINGER 9R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001212003032000121NM 2003 3 20 2003UALA00111 120030128A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FLOOR RT CREASE BEAM INNER Z-ANGLE CORRODED FROM STA 270-360. MAJOR REPAIR ACCOMPLISHED. REPLACED Z-ANGLE. 2L72 4F4 FRTA16WE E2GL 20030320001222003032000122NM 2003 3 20 2003UALA00112 120030128A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 FUSELAGE FRAME CRACKED STATION 807 AT STR 9R SUPPORT RAIL CLIP ATTACH FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030320001252003032000125 2003 3 20 2003UALA00115 420030124A2565 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE GIRT BAR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29777UA 26916 LT DOOR 1L AFT GIRT FITTING CRACKED. REPLACED AFT GIRT FITTING. 2L72 4F4 FRTT0001SE E46NE 20030320001272003032000127NM 2003 3 20 2003UALA00118 120030129A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29642UA 25092 L-ANGLE AND CHANNEL CRACKED BETWEEN STA 325 AND 347 AT RBL 42.69. L-ANGLE ATTACHES TO THE FORWARD END OF C-CHANNEL FLOORBOARD SUPPORT AT RBL 42.69 TO THE STA 325, FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW L-ANGLE AND NEW CHANNEL. 2L72 4F4 FRTA1NM E24NE 20030320001302003032000130NM 2003 3 20 2003UALA00121 120030131A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG WW CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 MLG WHEEL WELL PRESSURE PANEL CRACKED AT STA 670 LBL33, OUTBOARD AND AFT OF AILERON TOWER SHAFT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030321000552003032100055EA 2003 3 21 03078635 120030319A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27635BR 7295 DURING MAINTENANCE INSPECTION THE LT FWD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030321000612003032100061EA 2003 3 21 COMA0360152 120030317A3230 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01940CA 7048 FLIGHT 5031 GEAR DISAGREE WARNING - NLG FAILED TO RETRACT.SERVICED THE NLG STRUT, SUSPECT NOT FULLY EXTENDING. 2L72 4F RTA21EA 20030321000622003032100062EU 2003 3 21 DHL2003367513 120030226A5300 SKIN AIRBUS300 A300B4203 3930306EU DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH36183 265 Item Ref. N/R 0029727:External skin at STA. 4925 dented at six oclock position. Corrective action:Removed damaged area IAW A300 SRM 53-10-10 mat. ID IAW A300 SRM 53-10-10 fabbed doubler IAW A300 SRM 53-10-10 alodined an primed filler IAW SRM 51-40-12. Installed IAW A300 SRM 53-10-10. 2L72 4F RTA35EU 20030321000642003032100064NM 2003 3 21 2003UALA00201 120030225A5310 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29956UA 26704 AFT CABIN FLOOR STRUCTURE, INNER CREASE BEAM AT STRINGER 17R BETWEEN STA. 947.5 TO 990 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CREASEBEAM PART. 2L72 4F4 FRTA16WE E2GL 20030321000662003032100066NM 2003 3 21 2003UALA00205 120030219A5754114W41507 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 5 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 TRAILING EDGE WEDGE, SLAT NR 5, DELAMINATED. SEAL FOAM CORE MISSING SECTION. REPAIRED TRAILING EDGE WEDGE, SLAT NR 5. REPLACED SEAL FOAM CORE. 2L72 4F4 FRTT0001SE E46NE 20030321000742003032100074NM 2003 3 21 2003UALA00215 120030223A5754114W416018 SLAT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 9 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 TRAILING EDGE WEDGE, SLAT NR 9, DELAMINATED. REMOVED, REPAIRED AND REINSTALLED SLAT NR 9 WEDGE. 2L72 4F4 FRTT0001SE E46NE 20030321000812003032100081NM 2003 3 21 2003UALA00223 120030227A5313 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29956UA 26704 AFT ENTRY DOOR THRESHOLD CREASE BEAM OUTER CHORD ROUTED OUT BEYOND LIMITS STATION 968 STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2L72 4F4 FRTA16WE E2GL 20030321000832003032100083NM 2003 3 21 2003UALA00226 120030228A5310 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29953UA 26700 STATION 293 THRU 351, RBL 59, FORWARD CABIN RIGHT CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION. 2L72 4F4 FRTA16WE E2GL 20030321000842003032100084NM 2003 3 21 2003UALA00227 120030228A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29956UA 26704 EXTERNAL FUSELAGE HAS 3 EA DENTS BELOW AND ABOVE DOUBLER STA 384 - 390 S17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030321000892003032100089NM 2003 3 21 2003UALA00232 120030228A3350362624 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN SHORTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29301UA 23642 EMERGENCY EXIT FLOOR LIGHTING (EEL) NOT VISIBLE FROM ROW 15 AFT. FOUND AFT GALLEY SHORTING THAT PORTION OUT. REPLACE AND GROUND CHECKS OKAY. 2L72 4F4 FRTA16WE E2GL 20030321000922003032100092NM 2003 3 21 2003UALA00238 120030226A2710113W721234 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE AILERON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA32477 26919 CRACKED AILERON FITTINGS ON A/C. LEFT AILERON INBOARD FITTING - CRACKED HORIZONTAL FLANGE INBOARD AND OUTBOARD SIDES. RIGHT AILERON INBOARD FITTING - CRACKED HORIZONTAL FLANGE INBOARD SIDE. SUPPLEMENTAL DATA UPDATE CRACKED FITTING DISCOVERED DURING NDT INSPECTION CALLED OUT BY ENGINEERING. CRACK LENGTHS 1/16 TO 3/8 INCHES. CAUSE UNDER INVESTIGATION BY BOEING. REPORTED IN BOECOM UAL-OAK-03-00223F. AILERONS HAVE BEEN REMOVED AND WILL BE SENT TO THE SHOP FOR FITTING REPLACEMENTS. 2L72 4F4 FRTT0001SE E46NE 20030321000952003032100095NM 2003 3 21 UPS03240321 120030308A7830 BRACKET BOEING727 72725C 138400HNM NO.3 ENG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 INSPECTION TYPE:C NO.3 ENGINE THRUST REV. FAIRING MID BRACKET CRACKED. REPLACED BRACKET IAW MM 20-80-01. 2L73 4F A3WE 20030321000972003032100097NM 2003 3 21 UPS03440327 120030305A5340 SEAT TRACK BOEING747 747200 1384847NM U/D CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C U/D - SEAT TRACK FOUND HEAVY CORR. CORROSION BLEND OUT 0.048"X1"X2" SEAT TRACK REPAIRED AT U/D BS 570 - BS 710 LBL 47" AS PER SRM 53-10-05 FIG.1A 2L74 4F RTA20WE 20030321001022003032100102NM 2003 3 21 2003UALA00245 120030304A5330 SKIN BOEING777 777222 1385219NM FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 RT FUSELAGE SKIN HAS 2 INCH LONG CRACK, APPROX AT STA 2275 FORWARD OF LE OF HORIZ STAB MOVABLE FAIRING. MAJOR REPAIR ACCOMPLISHED WITH SKIN DOUBLER. 2L72 4F RTT0001SE 20030321001042003032100104NM 2003 3 21 2003UALA00247 120030307A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 FUSELAGE BULKHEAD WEB HAS 2EA CRACKS BS178 RBL6 WL200. ACCOMPLISHED MAJOR REPAIR ACCOMPLISHED. SPLICED WEB REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001322003032000132EU 2003 3 20 2003UALA00123 120030130A2121EVT3454G FAN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY INOPERATIVE A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29449UA 851 VIBRATION FELT UNDER FORWARD GALLEY FLOOR AND FLIGHT DECK AND SMOKE ODOR IN FLIGHT DECK. REPLACED AVIONICS BLOWER FAN (18HQ). 2L72 4F4 FRTA28NM E40NE 20030320001362003032000136NM 2003 3 20 2003UALA00127 120030203A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FLOORBEAM UPPER FLANGE HAD EXCESSIVE CORROSION AT STATION 360 RBL 5 IN TO LBL 18IN STRINGER 17L-17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION OF T-CAP MOUNTED ON AFT SIDE OF VERTICAL WEB WITH 9.5 IN, L-ANGLE SPLICES FWD AND AFT OF EACH CUT, FOUR TOTAL. 2L72 4F4 FRTA16WE E2GL 20030320001412003032000141NM 2003 3 20 2003UALA00133 120030124A5754114N300333 STRUCTURE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 5 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29518UA 24871 TRAILING EDGE WEDGE SLAT NR 5 DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED RIGHT T/E IN SHOP. 2L72 4F4 FRTA2NM E17NE 20030320001422003032000142NM 2003 3 20 2003UALA00134 120030130A5411 SPAR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29642UA 25092 NR 2 PYLON UPPER SPAR WEB AT STA 180 IS CRACKED AT RADIUS OF CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER SPAR WEB WITH DOUBLER AND ANGLE REPAIR. 2L72 4F4 FRTA1NM E24NE 20030320001472003032000147NM 2003 3 20 2003UALA00140 120030203A5320 CHANNEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE INTERCOSTAL CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FLOOR INTERCOSTAL AT STATION 328 TO 344 RBL 51 STRINGER 17R CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERCOSTAL EXTRUSION CHANNEL AND REPLACED WITH NEW VENDER PART. 2L72 4F4 FRTA16WE E2GL 20030320001542003032000154NM 2003 3 20 2003UALA00148 120030205A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FRAME WEB CRACKED AT STATION 616 LT, WL 205. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB SECTION AND SPLICE DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030320001632003032000163EU 2003 3 20 2003UALA00155 120030206A3150 WARNING SYSTEM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29439UA 683 FLIGHTS ABORTED ON TAKEOFF ROLL DUE TO ECAM VENT SKIN VALVE FAULT. 2L72 4F4 FRTA28NM E40NE 20030320001692003032000169NM 2003 3 20 SWAA030615 120030318A53116546543 BELTFRAME BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME CRACKED AT BS 639, RBL 64. R&R BELTFRAME PER SRM. 2L72 4F A16WE 20030320001752003032000175NE 2003 3 20 SWAA030622 220030317A7200CFM56 ENGINE BOEING737 737301 1384611NM CFM56 CFM56* 13802NE LH WING FAILED A SWAAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 SW29659SW 23229 721741 ( IN-FLT SHUTDOWN, DECLARED EMERGENCY )……………………..DURING CLIMB # 1 ENGINE SHUTDOWN, WOULD NOT RESTART. R&R # 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030320001782003032000178 2003 3 20 SWAA030594 420030315A25656557463 FITTING BOEING737 7373H4 1384600NM FWD SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT ATTACH FITTING LOOSE. SECURED AFT ATTACH FITTING PER MM. 2L72 4F RTA16WE 20030320001802003032000180NM 2003 3 20 SWAA030599 120030315A552065C25745 ELEVATOR BOEING737 7373A4 1384585NM TAIL WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C2 CHECK, SWA SI 11139-55, BOTH LH & RH ELEVATORS FAILED FREE PLAY CHECK. R&R BOTH LH & RH ELEVATORS PER MM. 2L72 4F RTA16WE 20030320001812003032000181NM 2003 3 20 SWAA030600 120030315A5520183A8300 HINGE BOEING737 7373H4 1384600NM LH ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, FOUND LH ELEVATOR TAB # 4 HINGE WORN. R&R HARDWARE ON # 4 HINGE PER MM. 2L72 4F RTA16WE 20030320001852003032000185WP 2003 3 20 FE5F200300002 120030313A29007952170565 TUBE DOUG DOUG DC9 DC982 3022082WP LOOSE W FE5FO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP03 15168 NIL 53167 When A/C taxied to the gate position, tower informed smoke is observed from R/H ENG site and then cabin crew reported HYD ordor is smelled in the cabin. Captain shutdown the APU and related symptom disappeared and then L/H HYD QTY indicated 7 QT remained. Mechanics inspected and found one L/H HYD Tube B nut loose. Retighten and running test all symptom is no long observed. 2L72 4F A6WE 20030321000072003032100007NM 2003 3 21 SWAA030628 120030318A53106547978 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEBS CORRODED AT LH BS 825, RH BS'S 442, BS 500 + 8 & BS 880. REPAIRED CREASE BEAM WEBS PER SRM. 2L72 4F RTA16WE 20030321000082003032100008NM 2003 3 21 SWAA030629 120030316A5330589358 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED C3 CHECK, FOUND R-1 COCKPIT WINDOW POST SKIN CRACKED AT UPPER OTBD CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030730000492003073000049WP 2003 7 30 ABXA030272 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 247. REMOVED DAMAGED FRAME SECTION, FABRICATED NEW SECTION AND SPLICES, AND INSTALLED IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-8. 2L74 4F 4A25 20030730001032003073000103SO 2003 7 30 SIMA200313904 120030512A531014525369003 SHEAR TIE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21644AE 145204 ABI - DURING AN IMBV INSPECTION, THE SHEAR TIE AT FRAME 68 AND THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY PERFORMING AN CUT OUT OF THE LOWER PORTION OF THE SHEAR TIE. FABRICATED A REPLACEMENT SPLICE. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/1615 AND STANDARD EMB SRM, SRM 145/1142 REV 21, PRACTICES. (M) 2L72 4T RTT00011AT 20030731000452003073100045EA 2003 7 31 QXEA200300900 120030719A5320 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 PDX- AFT CARGO PIT RIGHT HAND SIDE STRUCTURE AT INTERCOSTAL CRACKED FORWARD OF FEED THROUGH OF NR 2 CASE DRAIN RETURN LINE. REPAIRED IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20030731000562003073100056NM 2003 7 31 QXEA200300875 120030723A2120 ODOR BOMBDRDHC8 DHC8401 1390041NM COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09405QX 4047 YEG-MOMENTARY ELECTRICAL SMELL IN COCKPIT. PERFORMED GENERAL VISUAL INSPECTION OF COCKPIT. OPERATED RECIRC FAN. OPERATED APU BLEED AIR. NO UNUSUAL ODORS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000612003073100061NM 2003 7 31 QXEA200300756 120030622A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG FAULTY A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09405QX521 4047 GTF-ON FLIGHT NUMBER 2324, AFTER TAKEOFF FROM GTF TO HLN, UNABLE TO RETRACT GEAR. THREE GREEN AND 3 RED LIGHTS, NORMAL HYDRAULICS. COMPLIED WITH CHECKLIST, AGAIN ATTEMPTED TO RETRACT GEAR, THREE GREEN & THREE RED LIGHTS ILLUMINATED. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLIGHT FERRIED TO PDX AND REMOVED AND REPLACED NOSE LANDING GEAR WOW NR 2 HARNESS. RIGGED NR 2 NOSE LANDING GEAR HARNESS SENSOR. PERFORMED OPERATIONAL TEST OF NOSE LANDING GEAR EXTENSION/RETRACTION SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000662003073100066NM 2003 7 31 QXEA200300887 120030724A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09374PH23615 528 PSC- FORWARD CABIN OVERHEAD AND FORWARD RIGHT HAND EMERGENCY EXIT SIGNS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT POSITION PS2. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000762003073100076NM 2003 7 31 QXEA200300796 120030617A7110 BRACKET BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - NR 1 LOWER COWL ASSEMBLY VERTICAL WEB UPPER BRACKET CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030731000912003073100091NM 2003 7 31 QXEA200300771 120030623A7110 ANGLE BOMBDRDHC8 DHC8401 1390041NM COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- TOP ANGLE FOR WEB ABOVE CONE FORWARD OF DEBRIS DOOR IS CRACKED. REPAIRED IAW RD8/4-71-016. 2H72 4T RTA13NM 20030731001172003073100117NM 2003 7 31 QXEA200300793 120030624A7110 ACOUSTIC PANEL BOMBDRDHC8 DHC8401 1390041NM LT COWLING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - ACOUSTIC COMPOSITE STRUCTURE AT ENGINE INTAKE AREA IS CHAFED ON OUTBOARD SIDE OF ENGINE INLET OF LEFT HAND LOWER COWL. REPAIRED IAW HORIZON AIR EA 6-71-101. 2H72 4T RTA13NM 20030731001192003073100119NM 2003 7 31 QXEA200300760 120030621A33506138001 BATTERY PACK BOMBDRDHC8 DHC8401 1390041NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09414QX1377 4061 PDX-EMERGENCY LIGHTS ARE INOPERATIVE AT RIGHT HAND FORWARD EXIT DOOR. REMOVED AND REPLACED BATTERY PACKS AND EMERGENCY POWER SUPPLY UNIT FOR RIGHT HAND FORWARD EXIT LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001312003073100131NM 2003 7 31 QXEA200300825 120030711A5711 SPAR BOMBDRDHC8 DHC8401 1390041NM WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - FLANGES ON FORWARD SPAR UNDER PANELS 261CT, 261FT, 261HT AND 261LT ARE CHAFED APPROXIMATELY YW58.00 RIGHT TO YW58.00 LEFT. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030731001382003073100138NM 2003 7 31 QXEA200300912 120030728A2612 FIRE WARNING BOMBDRDHC8 DHC8401 1390041NM COCKPIT FALSE ACTIVATIONA QXEAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 NM09408QX 4050 FCA- ON FLIGHT 2271 NR 2 ENGINE FIRE WARNING ON GROUND. PULLED 'T' HANDLE AFTER ENGINE SHUTDOWN. DID NOT FIRE EXTINGUISHER. THERE WAS NO VISABLE SIGN OF A FIRE. FIRE WARNING WENT OUT AFTER 'T' HANDLE WAS PULLED. INSPECTED ENGINE NACELLE, NO EVIDENCE OF FIRE. TESTED NACELLE FIRE DETECTION SYSTEM IAW Q400 AMM 26-005 TASK 26-11-00-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001402003073100140EA 2003 7 31 QXEA200300901 120030718A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 PDX- FUSELAGE SKIN IS GOUGED AFT OF BAGGAGE BAY DOOR SURROUND INNER EDGE FIVE INCHES ABOVE LOWER FORWARD STOP FITTING. REPAIRED IAW CRJ SRM 53-61-01, 51-12-11 AND 51-25-01. 2L72 4F RTA21EA 20030731001442003073100144EU 2003 7 31 2003F00495 120030515A5512 SKIN AIRBUS320 A320233 3930329EU HORIZ STAB CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE CRACKED AND SEVERAL DENTS. REPAIRED CRACK IAW SRM 55-14-11, FIGURE 205. DENTS WERE REPAIRED PER PER SRM 51-77-11, REV 61. (M) 2L72 4F RTA28NM 20030731001452003073100145WP 2003 7 31 GTIA030501 120030618A5230 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - AFT CARGO DOOR, UPON REMOVAL OF BRACKET FOUND CRACK IN RADIUS OF CARGO DOORS PAN AT LOWER FORWARD CORNER. STOP DRILLED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030731001472003073100147WP 2003 7 31 GTIA030508 120030615A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND AFT PIT STATION 1079 STRINGER 28L-28R FRAME CORRODED. REMOVED CORRODED FORMER ANGLE. FABRICATED REPAIR ANGLES. INSTALLED REPAIR ANGLE AND FRAME ANGLE. (M) 2L72 4F A6WE 20030321001052003032100105NM 2003 3 21 2003UALA00248 120030307A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 BS 188 RT FUSELAGE FRAME CRACKED IN RADIUS ON AFT SIDE AT WL208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030728001022003072800102 2003 7 28 SWAA031585 420030717A2565D31354 SLIDE BOEING737 7373Y0 1384671NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030728001172003072800117NM 2003 7 28 SWAA031541 120030713A53156546804 FLOORBEAM BOEING737 7372T4 1384492NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SPECIAL VISIT, FOUND FLOORBEAM CORRODED AT BS 344, BL 0. REPAIRED FLOORBEAM PER SRM. 2L72 4F A16WE 20030729000422003072900042NM 2003 7 29 ZW0A0306002 120030712A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13719TW 28487 THE EVACUATION SLIDE GIRT BAR LEAF RETENTION SPRINGS WERE REPLACED ACCOUNT DEFORMED AT THE L1, L4, AND R4 DOORS. 2L72 4F RTA2NM 20030729000762003072900076NM 2003 7 29 QXEA200300748 120030615A3150 WARNING HORN BOMBDRDHC8 DHC8401 1390041NM COCKPIT ACTIVATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09403QX 4037 PDX- ON FLIGHT 2309 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED AFTER ADVANCING POWER LEVERS. MAINTENANCE COMPLIED WITH TAKEOFF WARNING HORN IAW S/L DH8-400-SL-27-006-R1 AND FUNCTIONAL TEST IAW TASK 31-52-00-720-801 OF AMM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030729001142003072900114WP 2003 7 29 AMTA200300893 120030529A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 C2 DOOR AFT CUTOUT SURROUND SKIN GOUGED. REPAIRED SKIN IAW ER/A L10-53R-5177. (M) 2L73 4F A23WE 20030729001222003072900122EA 2003 7 29 SWIA200312195 120030716A321316124101 AXLE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07595SW49 49 7292 NOSE LANDING GEAR AXLE ASSY CORRODED. INSTALLED NEW AXLE ASSEMBLY IAW CRJ MM 32-21-15. 2L72 4F RTA21EA 20030730000422003073000042NM 2003 7 30 ABXA030285 120030605A5720113T16476 SUPPORT FITTING BOEING767 767281 1385109NM RT WING DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 RIGHT WING TRAILING EDGE 113T1647-6 PANEL SUPPORT FITTING ASSEMBLY DAMAGED DOUBLE HOLE AND BLENDED AREA STA 1051 RIGHT BUTTLINE 97.4. REPAIRED AREA IAW REA B657-46309MR. 2L72 4F RTA1NM 20030730001182003073000118WP 2003 7 30 AMTA200300897 120030614A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 AFT CABIN FLOORBEAM T-CAP CORRODED. REPAIRED FLOORBEAM T-CAP IAW SRM 53-23-00. (M) 2L73 4F A23WE 20030731000152003073100015NM 2003 7 31 QXEA200300843 120030709A6123 MFC DHAV DHC8 DHC8202 2809007NM NR 1 OUT OF ADJUST A QXEAK NONE O OTHER TOTAKEOFF 1 NM09367PH 511 PDX- ON FLIGHT 2241, AUTOFEATHER DID NOT ARM ON TAKEOFF ROLL PRIOR TO 70 KNOTS. PERFORMED ENGINE RIG IAW MTC 9720022. ADJUSTED NR 1 ENGINE MFC 1/16 OF A TURN COUNTERCLOCKWISE. AUTOFEATHER SYSTEM CHECKS GOOD. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000242003073100024NM 2003 7 31 QXEA200300807 120030712A2751 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09400QX 4030 SEA - FLIGHT 2339 - DURING FLAP RETRACTION AFTER DEPARTURE, THE (FLAP POWER) CAUTION LIGHT ILLUMINATED AS THE FLAP HANDLE WAS PLACED AT ZERO. THE CHECK LIST PROCEDURE WAS ACCOMPLISHED BUT THE LIGHT REMAINED ON. MAINTENANCE INSPECTED THE AIRCRAFT AND INTERROGATED THE CDS AND FOUND NO FAULTS. THE SYSTEM WAS RESET AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000292003073100029NM 2003 7 31 QXEA200300889 120030727A2750C1486561 PDU BOMBDRDHC8 DHC8401 1390041NM T/E FLAP FAILED A QXEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM09411QX3795 3795 4055 PDX- ON FLIGHT 2469 DIVERTED TO PDX FOR FLAPS FAILED TO RETRACT DURING AFTER-TAKEOFF FLOW. FLAP POWER CAUTION LIGHT ILLUMINATED AND RAN CHECKLIST. CAUTION LIGHT WENT OUT BUT CAME BACK ON WHEN ATTEMPTED TO RETRACT FLAPS. NO FLAP MOVEMENT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FLAP DRIVE POWER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000412003073100041EA 2003 7 31 QXEA200300787 120030703A26114462534 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09600QX3798 3798 10005 SEA- ON FLIGHT 2423 SMOKE AFT LAVATORY MESSAGE. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000432003073100043NM 2003 7 31 QXEA200300868 120030722A6123 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM AUTOFEATHER SYS MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09413QX 4060 EUG- ON FLIGHT 2276 ABORTED AUTOFEATHER TEST. CLEARED PEC FAULT IAW AMM TASK 61-20-36-070-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000672003073100067EA 2003 7 31 QXEA200300888 120030724A3620 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT ACTIVATED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09607QX 10024 SEA- ON FLIGHT 2471 RECIEVED "BLEED DUCT" WARNING WHICH STAYED ON FOR 15 SECONDS FOLLOWED BY "RIGHT BLEED DUCT" CAUTION, WHICH WENT AWAY AFTER PERFORMING CHECKLIST AND MANUAL BLEED PROCEDURE. THIS SDR IS WAITING FOR FURTHER INFORMATION. 2L72 4F RTA21EA 20030801000032003080100003WP 2003 8 1 GTIA030519 120030619A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CABIN FLOOR SUPPORT STATION 197 LBL 8 TO LBL 40 CORRODED. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000162003080100016EU 2003 8 1 2003F00497 120030515A5753 COVER AIRBUS320 A320233 3930329EU T/E FLAP FAIRINGBROKEN A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK, 633AR, BROKEN COVER. REPLACED COVER IAW SRM 51-76-00. (M) 2L72 4F RTA28NM 20030801000172003080100017WP 2003 8 1 GTIA030540 120030712A3260833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP NLG INTERMITTENT A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23826NK 49391 ORD - FLT 1442 - NOSE GEAR UNSAFE LIGHT (RED) ON THROUGH CLIMB-OUT AND INTERMITTENT FLASHING IN CRUISE. INITIAL GEAR UP HAD THE LIGHT OUT. QRH PROCEDURES FOLLOWED. LIGHT STILL INTERMITTENT ON. REMOVED AND REPLACED NOSE GEAR UP POSITION (D1-31) PROXIMITY SENSOR. OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20030801000212003080100021WP 2003 8 1 GTIA030551 120030630A5320 ATTACH FITTING DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN FS 864 FLOOR SUPPORT ATTACH FITTING CRACKED BL 0. REMOVED CRACKED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT ATTACH FITTING. INSTALLED FLOOR SUPPORT ATTACH FITTING. (M) 2L72 4F A6WE 20030801000342003080100034EA 2003 8 1 ASOA03286 120030704A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11859AS 7421 FLT 4228 - DURING A GROUND INSPECTION IN MCI, THE RIGHT SIDE EMERGENCY FLOOR LIGHTS AT ROW TWO WERE FOUND TO BE INOPERATIVE. MAITNENANCE RECONNECTED THE RIGHT SIDE EMERGENCY FLOOR LIGHTS AT ROW TWO. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030801000412003080100041WP 2003 8 1 GTIA030527 120030606A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND MID CARGO DOOR CORRODED JAMB BEAM ALL ALONG BOTTOM AT FS 636-693. REMOVED OUT OF LIMIT DOOR BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED NEW BEAM. (M) 2L72 4F A6WE 20030801000432003080100043WP 2003 8 1 GTIA030536 120030628A5522 SKIN DOUG DC9 DC982 3022082WP RT ELEVATOR TORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND RIGHT ELEVATOR INBOARD UPPER LEADING EDGE SKIN TORN. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. INSTALLED SKIN. (M) 2L72 4F A6WE 20030801000482003080100048EU 2003 8 1 2003F00499 120030515A7830 DUCT AIRBUS320 A320233 3930329EU THRUST REVERSER DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 2 ENGINE LEFT THRUST REVERSER COWLING, OUTER SKIN C-DUCT DELAMINATED. C-DUCT REPAIRED IAW SRM V2500 54-30-00, REPAIR NR 4. (M) 2L72 4F RTA28NM 20030801000502003080100050EU 2003 8 1 2003F00501 120030515A7830 DUCT AIRBUS320 A320233 3930329EU THRUST REVERSER CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER C-DUCT, LEFT, WITH CORROSION ON UPSIDE. REPAIRED LEFT THRUST REVERSER IAW RE 2078006, REF CV03-0917-01. (M) 2L72 4F RTA28NM 20030801000552003080100055WP 2003 8 1 GTIA030549 120030629A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOND AFT PIT FLOOR WEB CRACKED AT FS 1271-1309 LONGERON 18R. STOP DRILLED THE TWO ENDS OF THE CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR. (M) 2L72 4F A6WE 20030801000582003080100058EA 2003 8 1 ASOA03285 120030703A5210601R3813211 PUSHROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A ASOAK NONE O OTHER TXTAXI/GRND HDL 1 SO11833AS 7246 FLT 4497 - AFTER LANDING IN DFW, THE MAIN PASSENGER DOOR WOULD NOT OPEN FOR DEPLANING. MAINTENANCE OPENED THE PASSENGER DOOR AND DEPLANING WAS COMPLETED SAFELY. MAINTENANCE ADJUSTED THE PASSENGER DOOR INNER HANDLE PUSH ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030801000622003080100062EU 2003 8 1 2003F00502 120030515A5730 ACCESS PANEL AIRBUS320 A320233 3930329EU LT WING DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK,F OUND LEADING EDGE ROOT WING 192DT ACCESS PANEL DELAMINATED. REPAIR PANEL IAW SRM 51-73-00, PAGES 1 AND 2. (M) 2L72 4F RTA28NM 20030801000672003080100067WP 2003 8 1 GTIA030518 120030619A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CABIN FLOOR SUPPORT LBL 10 STATION 197 TO 256 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000712003080100071EA 2003 8 1 ASOA03291 120030628A5320601R3117121 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE FLOOR SUPPORT INTERCOSTAL AT FS 484, LBL AND RBL 36 AT THE ATTACH FLANGE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT INTERCOSTAL AT FS 484, LBL AND RBL 36 AT THE ATTACH FLANGE IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20030729000712003072900071NE 2003 7 29 QXEA200300678 220030605A7200 ENGINE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 1 AND NR 2 OVERTORQUED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09357PH 504 BOI- ON FLIGHT 2203 OVER TORQUED BOTH NR 1 AND NR 2 ENGINES. ESTIMATE NR 1 TORQUE AT 14490 AND NR 2 TORQUE AT 15090. TORQUES WERE EXCEEDED FOR APPROXIMATLY 2 SECONDS. VERIFIED NR 1 ENGINE TORQUE 13290 AND NR 2 TORQUE 13190, NO ENGINE MAINTENANCE REQUIRED PER MM 05-10-00 PAGE 14. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030729000862003072900086NM 2003 7 29 QXEA200300745 120030611A5753 BUSHING BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA T/E FLAP FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - ENGINEERING REQUEST - GENERAL VISUAL INSPECTION OF BUSHING FOR CONDITION OF LEFT INBOARD FLAP OUTBOARD FITTING OUTBOARD LUG. REF EA 6-57-51 "C" FOR CONTINUATION OF SERVICE. 2H72 4T4 TRTA13NM E00062EN 20030731000742003073100074EA 2003 7 31 QXEA200300861 120030720A2612 FIRE LOOP CNDAIRCL600 CL6002C10 1390015EA LT ENGINE SHORTED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX 10045 PDX- INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. MDC INDICATES LEFT ENGINE FIRE LOOP B SHORT CIRCUIT. REMOVED AND REPLACED LEFT HAND W16 FIRE SENSOR HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000882003073100088NM 2003 7 31 QXEA200300819 120030710A5210 SKIN BOMBDRDHC8 DHC8401 1390041NM PAX DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - MAIN CABIN DOOR HAS GOUGED AREA LOCATED 5.5 INCHES FROM FORWARD EDGE OF DOOR AND 1.3 INCHES DOWN FROM TOP OF DOOR. REPAIRED IAW HORIZON AIR EA 6-52-299. 2H72 4T RTA13NM 20030731000922003073100092NM 2003 7 31 QXEA200300764 120030623A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - AREA OF SKIN NICKS APPROXIMATELY 8 INCHES WIDE BELOW AFT BAGGAGE DOOR CUT-UOT. REPAIRED IAW Q400 SRM 51-25-05, PAGE 208. 2H72 4T RTA13NM 20030731001012003073100101EA 2003 7 31 QXEA200300761 120030623A4990 APU CNDAIRCL600 CL6002C10 1390015EA APU BAY LEAKING A QXEAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM09606QX 10023 BIL - FLIGHT 2481 - CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF THE AFT LAVATORY SMOKE DETECTOR SOUNDED. THE CREW COULD SMELL OIL BUT THE ODOR SOON DISSIPATED AND THE WARNING WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND OIL IN THE MIXING MANIFOLD. MAINTENANCE VERIFIED THAT THE APU WAS LEAKING OIL AND THE APU WAS MEL'D. THE DUCTING WAS CLEANED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731001032003073100103NM 2003 7 31 QXEA200300895 120030725A5240 RETAINER BOMBDRDHC8 DHC8401 1390041NM SERVICE DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX- SEAL RETAINER SCREW AFT LOWER END OF AFT SERVICE DOOR DIMPLED AT SCREW HOLE. REPAIRED IAW HORIZON AIR EA 6-52-302. 2H72 4T RTA13NM 20030731001052003073100105NM 2003 7 31 QXEA200300755 120030620A242131708001A GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 FAILED A QXEAK NONE J WARNING INDICATION UKUNKNOWN 1 NM09366PH10692698 510 SEA- ON FLIGHT 2055 NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED, RAN CHECKLIST WITH NO CHANGE. REMOVED AND REPLACED NR 1 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001082003073100108NM 2003 7 31 QXEA200300798 120030619A7110 CHANNEL BOMBDRDHC8 DHC8401 1390041NM RT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - RIGHT HAND LOWER COWL CRACKED CHANNEL ON RIGHT HAND SIDE AFT OF BYPASS ACTUATOR. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030731001112003073100111NM 2003 7 31 QXEA200300799 120030619A7110 CHANNEL BOMBDRDHC8 DHC8401 1390041NM RT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - RIGHT HAND LOWER COWL OUTBOARD CHANNEL CRACKED ON NR 2 ENGINE. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030731001202003073100120NM 2003 7 31 QXEA200300835 120030709A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - ROCK DENTS ON RIGHT HAND BELLEY, JUST AFT OF NOSE GEAR. REPAIRED IAW Q400 AMM 51-25-31-370-801 AND HORIZON AIR EA 6-53-281. 2H72 4T RTA13NM 20030731001412003073100141EU 2003 7 31 2003F00492 120030515A5753 COVER AIRBUS320 A320233 3930329EU T/E FLAP BROKEN A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK, 632R, BROKEN COVER. REPLACED COVER IAW SRM 51-76-00, REV 60. (M) 2L72 4F RTA28NM 20030801000022003080100002WP 2003 8 1 GTIA030516 120030622A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT STATION 160 TO 200 RBL 48 CORRODED. FLOOR GALLEY MOUNT CORRODED AT STATION 160 RBL 48. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000042003080100004NM 2003 8 1 TSAA0330154 120030625A3020320115 SHUTOFF VALVE BOEING737 7372M6C 1384708NM NR 2 ENGINE DEFECTIVE A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13805AL 21809 FLT 952 - HNL-ITO, NR 2 ENGINE COWL ENGINE ICE LIGHT REMAINS ON IN TRANSITION (BRIGHT BLUE). RETURNED TO HNL FOR UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 2 ENIGNE COWL VALVE. OPS CHECKED GOOD IAW AMM 75-11-0. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030801000232003080100023WP 2003 8 1 2003F00506 120030709A2560AD4002P BATTERY DOUG DC9 DC931 3022065WP FLASHLIGHT DISCHARGED A A4JAK NONE L NO TEST ININSP/MAINT 1 SO35934LK 48157 DURING B-CHECK PIE MAINTENANCE, FOUND FORWARD EMERGENCY LIGHT/FLASHLIGHT AT FORWARD FLIGHT ATTENDANT PANEL INOPERATIVE. REPLACED BATTERIES IN FORWARD EMERGENCY FLASHLIGHT IAW MM 33-53-0, FLASHLIGHT CHECKS NORMAL. (M) 2L72 4F A6WE 20030801000272003080100027WP 2003 8 1 GTIA030541 120030619A5320 STRUCTURE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND MID PIT FS 635 STRINGER 29R DOVE TAIL CORRODED. FABRICATED DOVE TAIL SUPPORT. (M) 2L72 4F A6WE 20030729000772003072900077EA 2003 7 29 QXEA200300739 120030615A2121GG670950227 FAN CNDAIRCL600 CL6002C10 1390015EA CABIN FAULTY A QXEAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UKUNKNOWN 1 NM09606QX4012 10023 SJC-SUP-ON FLIGHT NUMBER 2553, SMELL OF SMOKE FOLLOWED BY A RECIRC FAN FAULT. REMOVED AND REPLACED NR 1 RECIRC FAN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000952003072900095EU 2003 7 29 2003F00475 120030516A7830 SKIN AIRBUS320 A320233 3930329EU THRUST REVERSER DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER SKIN DELAMINATED. REPAIRED NR 1 THRUST REVERSER IAW SRM V2500, 54-30-00, REPAIR NR 22. (M) 2L72 4F RTA28NM 20030729001132003072900113WP 2003 7 29 AMTA200300812 120030505A5330 SKIN PANEL LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 SKIN PANEL AT 20 INCHES RBL 0 TO 24 INCHES RBL 0, FS 983-FS 1212 HAS CORROSION ON SKIN AND FASTENERS. COMPLIED WITH ER/A L10-53R-5178, SKIN SPLICE, FS 983-1209 RBL 16-42.50 (M) 2L73 4F A23WE 20030729001352003072900135SO 2003 7 29 SWIA200312157 120030610A5411 FRAME EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07563SW 120338 REINFORCEMENT FRAME FOR LT HYD PACK FWD FIREWALL, LT SIDE CRACKED AT HYD PRESS LINE FITTING POINT. (DISCOVERED DURING C-CHECK) INSTALLED REPAIR DOUBLER IAW IC 2003-12012138. SEE RII 54-301 & M337. P/N: 120-18896-001 2L72 4T RTA31SO 20030730000352003073000035WP 2003 7 30 ABXA030275 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME STA 237. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-8, 51-1-24, AND 51-3-0. 2L74 4F 4A25 20030730000612003073000061WP 2003 7 30 ABXA030298 120030625A52103925134503 FITTING DOUG DC9 DC932 3022066WP AFT ENTRY DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 AFT ENTRANCE DOOR INTERNAL FITTING CRACKED BEHIND TOP RIGHT DOOR STOP. REPLACED FITTING IAW DC-9 SRM. 2L72 4F A6WE 20030730001062003073000106SO 2003 7 30 SIMA200317605 120030623A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21811AE 145529 ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND SHIMS AND INSTALLED. REPAIR DONE IAW EMB SRM, SRM EMB 145-1142 REV 21, CHAPTER 53-24-02 FIGURE 102. (M) 2L72 4F RTT00011AT 20030730001252003073000125EU 2003 7 30 2003F00488 120030516A5350 ACCESS PANEL AIRBUS320 A320233 3930329EU FUSELAGE DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND RIGHT BELLY FAIRING ACCESS PANEL, 198GB, DELAMINATED STATION 2456. REPAIRED PANEL IAW SRM 51-77-12, PAR 3B, FIGURE 3. (M) 2L72 4F RTA28NM 20030730001462003073000146SO 2003 7 30 SIMA200313907 120030513A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21644AE 145204 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL AND INSTALLED SERVICEABLE SILL IAW EMB-1459 SRM 145/1142, REV 21, 51-20-01/03, 51-40-02/04/06 EMB CPM (CPM-145/1132 REV 8) 51-21-04, 51-21-05, 51-21-06 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030731000202003073100020NM 2003 7 31 QXEA200300836 120030714A3060699009003 CONTROL UNIT BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA PROP DEICE MALFUNCTIONED A QXEAK NONE J WARNING INDICATION CRCRUISE 1 NM09409QX3705 4051 MFR - PROP DEICE CAUTION ILLUMINATED INFLIGHT. PERFORMED CHECKLISH. RESET PROP DEICE CONTROL. CAUTION RE-ILLUMINATED. LANDED IN SEA WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 TMCU. CALIBRATION AND OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20030731000382003073100038NM 2003 7 31 QXEA200300784 120030705A33506138001 BATTERY PACK BOMBDRDHC8 DHC8401 1390041NM CABIN DISCHARGED A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09546DS115 115 4017 SEA- FORWARD EMERGENCY POWER BATTERY PACK LOW. REMOVED AND REPLACED FORWARD EMERGENCY POWER BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000732003073100073NM 2003 7 31 QXEA200300809 120030711A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09345PH 476 PDX- EMERGENCY LIGHT STRIP, THIRD ONE FROM THE AFT OF THE AIRCRAFT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001242003073100124NM 2003 7 31 QXEA200300781 120030629A3397 WIRE BOMBDRDHC8 DHC8401 1390041NM CABIN OUT OF POSITION A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09400QX 4030 SEA- RIGHT HAND AFT EMERGENCY EXIT SIGN INOPERATIVE. FOUND POWER WIRE ON CONNECTOR IN WRONG PIN. REPOSITIONED WIRE TO CORRECT PIN. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001482003073100148WP 2003 7 31 GTIA030511 120030613A5313 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND MID PIT STATION 522-563 STRINGER 30 CORROSION AT FASTENERS. (M) 2L72 4F A6WE 20030801000322003080100032WP 2003 8 1 GTIA030502 120030606A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - AFT CARGO JAMB BEAM CORRODED AT FS 1155-1212 ALL ALONG BOTTOM. REMOVED JAMB BEAM. LOCATED AND DRILLED HOLES NEW JAMB BEAM. INSTALLED NEW JAMB BEAM. (M) 2L72 4F A6WE 20030801000562003080100056EA 2003 8 1 ASOA03293 120030706A5210601R319103 MECHANISM CNDAIRCL600 CL6002B19 1900309EA AFT PAX DOOR OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING HANGAR MAINTENANCE IN MCN, THE AFT PASSENGER DOOR WAS FOUND TO BE HARD TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE AFT PASSENGER DOOR COUNTER BALANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030729001082003072900108EU 2003 7 29 2003F00481 120030523A5280 SKIN AIRBUS320 A320233 3930329EU LT MLG DOOR CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND LEFT MLG WHEEL WELL DOOR INTERIOR SKIN CRACKED AT STATION 17255. REPAIRED DOOR IAW SRM 52-81-14, PAGE 258-264, FIGURE 205. (M) 2L72 4F RTA28NM 20030729001232003072900123SO 2003 7 29 SWIA200312196 120030716A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE CABIN DISCHARGED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07189SW6939 6939 120048 EMERGENCY LIGHTS FRONT 3 ON FLOOR AND FORWARD EXIT SIGN DO NOT ILLUMINATE. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030730000342003073000034WP 2003 7 30 ABXA030274 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME STA 173.8. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-21. 2L74 4F 4A25 20030730000712003073000071WP 2003 7 30 ABXA030261 120030214A5230 MOUNT DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 MAIN CARGO DOOR FRAMES LATCH MOUNT HOLES OVERSIZED. REPAIRED AREA IAW ABX REA D852-46043MR. 2L74 4F 4A25 20030730000842003073000084WP 2003 7 30 ABXA030281 120030710A33505708458503 BATTERY PACK DOUG DC8 DC861 3021952WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23848AX 368 46032 ON PREDEPARTURE CHECK FOUND EMERGENCY LIGHT BATTERY RACK DEAD. REPLACED EMERGENCY LIGHT BATTERY RACK ASSSEMBLY. GROUND OPS CHECKED OK IAW AMM 33-50-02. 2L74 4F 4A25 20030730001412003073000141EU 2003 7 30 USAABA03018 120030312A3350321430 BATTERY AIRBUS330 A330323 3930335EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19676UW 0375 PHL - EMERGENCY LIGHTS AT DOORS, L1, R1, L3, R3 AND R4 FAILED THE CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20030731000112003073100011NM 2003 7 31 QXEA200300910 120030724A5711 SPAR CAP DHAV DHC8 DHC8202 2809007NM LT WING SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- ON LEFT HAND WING FRONT SPAR CAP FOR LEADING EDGE MOUNT, LOWER SPAR CAP HAS 12 AREAS WHERE PRIMER IS SCRATCHED FROM STATION YW214.0 TO YW326.0. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD 8-57-1675. 2H72 4T RTA13NM 20030731000402003073100040NM 2003 7 31 QXEA200300786 120030702A2120 ODOR BOMBDRDHC8 DHC8401 1390041NM CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09400QX 4030 SEA- FLIGHT ATTENDENT REPORTS BURNING ELECTRICAL SMELL IN REAR OF AIRCRAFT ABOUT TIME GEAR CAME DOWN DURING LANDING. PERFORMED VISUAL AND AEROMATIC INSPECTION OF GALLEY AND REAR OF AIRCRAFT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000862003073100086NM 2003 7 31 QXEA200300827 120030714A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - FORWARD FLANGE ON PANEL 262HT CHAFED. REPAIRED IAW RD 8/4-53-521. 2H72 4T RTA13NM 20030731001332003073100133NM 2003 7 31 QXEA200300820 120030714A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - FORWARD FLANGE ON PANEL 262FT IS CHAFED. REPAIRED IAW Q400 RD 8/4-53-521, PAGE 4, STEP 8 AND RD 8/4-52-521, PAGE 5, STEP 11. 2H72 4T RTA13NM 20030731001502003073100150WP 2003 7 31 GTIA030513 120030619A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND RIGHT AFT LAVATORY FLOORBOARD DELAMINATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030801000282003080100028WP 2003 8 1 GTIA030547 120030612A5730 PANEL DOUG DC9 DC982 3022082WP RT WING DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND RIGHT WING UPPER TRAPAZOIDAL PANEL HONEYCOMB COMPOSITE DAMGED AND DELAMINATED AT TWO PLACES 34 INCHES OUTBOARD OF FUSELAGE AND 7 INCHES AFT OF PANELS L/E. REMOVED RIGHT WING UPPER TRAPAZOIDAL PANEL. REPAIRED TWO EACH DELAMINATES. INSTALLED RIGHT WING UPPER TRAPAZOIDAL PANEL. (M) 2L72 4F A6WE 20030801000542003080100054WP 2003 8 1 GTIA030503 120030623A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CABIN STATION 218 TO 236 LBL 44 INCHES TO 54 INCHES CRACK FORWARD SIDE CORNER WEB. REMOVED DAMAGED SECTION OF WEB. FABRICATED REPAIR. INSTALLED REPAIR. (M) 2L72 4F A6WE 20030801000682003080100068NM 2003 8 1 AMTA200300732 120030531A2613 WARNING SYSTEM BOEING757 75723N 1384973NM COCKPIT FALSE INDICATIONA AMTAK NONE N FALSE WARNING ININSP/MAINT 1 GL11528AT 30887 RT TURB OVERHEAT DETECTOR 2 STATUS MESSAGE. TROUBLESHOT PER FIM 26-13-00 FIG 104. NO FAULTS NOTED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030801000772003080100077WP 2003 8 1 GTIA030505 120030624A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CABIN STATION 180 RBL 10 TO 44 INCHES FLOOR SUPPORT CORRODED. LOCATED AND DRILLED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000842003080100084SO 2003 8 1 C2XA03TY095 120030723A532014522184005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713990 145277 TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT. SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE DAMAGED AREA, ALODINED, PRIMED AND FILLED WITH HYSOL 9394, FABRICATED AND INSTALLED A DOUBLER. IAW EMB-GST-1927/02A, THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF THE INSPECTION. 2L72 4T RTT00011AT 20030801000572003080100057WP 2003 8 1 2003F00509 120030709A3350AD4002P BATTERY DOUG DC9 DC931 3022065WP CABIN OUT OF POSITION A A4JAK NONE L NO TEST ININSP/MAINT 1 GL23934LK 48157 DURING B-CHECK, FOUND CEILING EMERGENCY LIGHTS AT ROW 15 THROUGH ROW 10 INOPERATIVE. REPOSITIONED BATTERIES IN EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW MM 33-53-0, SYSTEM CHECKS NORMAL. (M) 2L72 4F A6WE 20030801000652003080100065WP 2003 8 1 GTIA030504 120030623A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CABIN STATION 185 TO 195 LBL 52 INCHES FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. DRILLED AND LOCATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000802003080100080NM 2003 8 1 UPS03440937 120030620A5312 PRESSURE PANEL BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C RT BLG W/W PRESSURE DECK WEB CORRODED CRACK AT FS 1436-1438 RBL 112-114. PRESSURE WEB REPLACED IAW SRM 51-10-01 PG 8 DUE TO COR CRACK 1 INCH X 1 INCH AND THROUGH THE WHOLE THICKNESS EXCEEDED SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F A20WE 20030801000952003080100095EA 2003 8 1 COMA0360310 120030709A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01917CA23162 7017 DURING COMPLIANCE OF TASK NR 002-53-160-610, THREE CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS461.0, BETWEEN LBL9.0 AND RBL9.0. THE CRACKS RANGE FROM 2.5 INCHES TO 3.75 INCHES IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IAW REO NR 610R-53-41-102, REV B, DATED 6-8-2003, AND REO NR 601R-53-41-162, DATED 6-9-2003. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20030801000962003080100096EA 2003 8 1 COMA0360313 120030704A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01912CA12770 7011 FLIGHT 5002 GEAR DISAGREE WARNING WHILE AT GATE. REPLACED THE PSEU. 2L72 4F RTA21EA 20030801001022003080100102EA 2003 8 1 COMA0360337 120030725A2750860D10018ABC ECU CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 SO01934CA9865 7042 FLIGHT 5158 FLAPS FAILED DURING LANDING ROLL. REPLACED THE FECU. 2L72 4F RTA21EA 20030303000582003030300058 2003 3 3 SWAA030391 420030218A2565D31354 SLIDE BOEING737 7373Q8 1384670NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030303000632003030300063NM 2003 3 3 SWAA030399 120030218A32116546113 TRUNNION PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED RON, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED LT AND RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030303000642003030300064NM 2003 3 3 SWAA030400 120030219A32136561740 STRUT BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED RON, FOUND RT MLG UPPER STRUT CYLINDER CORRODED. REMOVED AND REPLACED RT MLG UPPER STRUT CYLINDER PER MM. 2L72 4F RTA16WE 20030303000702003030300070NM 2003 3 3 SWAA030408 120030220A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 EEPLS BROKEN AT OVERWING EXIT. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20030303000802003030300080NE 2003 3 3 HEEA084516 220030214A732325249995 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 TORQUE SPLIT. FOUND GOVERNOR BREAK SLOW TO RESPOND. REPLACED TEFLON TUBE AND ROLLER BEARINGS DUE TO WEAR. UNIT TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030303000832003030300083NM 2003 3 3 SWAA030438 120030225A335065C34691 LENS BOEING737 7373Q8 1384670NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 7 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20030303001022003030300102SW 2003 3 3 HEEA084527 120030214A243230703002 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 MAIN BATTERY IS SLOW TO CHARGE. REPAIRED. 1G72 4U H4SW 20030303001032003030300103NM 2003 3 3 0300316744 120030228A5711 WEB BOEING747 747212F NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01644NW 24177 During "H" check found cracks in two fastener holes #37 & #39 at right and left wing upper mid spar web between MSS 387.99 & 417.20. Repaired per EA 67-165047. 2L74 4F RTA20WE 20030303001142003030300114NE 2003 3 3 HEEA084531 220030214A7532312320301 BLEED VALVE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 BLEED VALVE CAUSES COMPRESSOR STALLS WHEN ROLLING THROTTLE TO FULL OPEN. 1G72 4U4 U H4SW E22EA 20030801001002003080100100EA 2003 8 1 COMA0360340 120030727A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAULTY A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01729CA16620 7265 FLIGHT 5254 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE INSPECTED FLAPS PER AD 98-20-01, NO DEFECTS FOUND - REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20030801001072003080100107EA 2003 8 1 COMA0360327 120030716A2752857D100401 FLEX DRIVE CNDAIRCL600 CL6002B19 1900309EA T/E FLAP BROKEN A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01982CA 7168 FLIGHT 5623 FLAPS FAIL CAUTION. REPLACED THE RT NR 4 FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20030801001102003080100110EA 2003 8 1 COMA0360335 120030727A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01936CA21743 7043 FOUND LOWER LEFT WING PLANK CRACKED AT WS 148.019 DURING EO 57-014. PERFORMED TEMPORARY REPAIR AND DEFERRED PER REO 601R-57-21-138 2L72 4F RTA21EA 20030801001162003080100116WP 2003 8 1 MWEA030275 120030711A324033019500 PRESSURE SWITCH DOUG DC9 DC981 3022081WP BRAKE SYSTEM SHORTED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31813ME 48007 AUTO BRAKE FAIL ANNUNCIATOR LIGHT ILLUMINATED AFTER PARKING BRAKE WAS RELEASED. REMOVED AND REPLACED SOLENOID PRESSURE SWITCH. 2L72 4F A6WE 20030801001192003080100119NM 2003 8 1 MWEA030287 120030720A528059107839 PAN BOEING717 717200 1383700NM MLG DOOR DAMAGED A MWEAO OTHER J WARNING INDICATION CRCRUISE 1 GL31902ME 55166 LANDING GEAR RETRACTION INDICATED GEAR DOOR OPEN ALERT, LEFT MAIN LANDING GEAR RED INDICATION LIGHT CAME ON. HYDRAULIC SERVICE CAP DAMAGED PAN AND JAMB, REPAIRED PAN AND JAMB, PASSED GEAR POSITION INDICATION TEST. 2L72 4F TRA6WE 20030801001222003080100122WP 2003 8 1 MWEA030284 120030718A52203913359547 CABLE DOUG DC9 DC981 3022081WP TAIL CONE MISROUTED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31807ME 48033 TAIL CONE WOULD NOT DEPLOY USING INTERNAL RELEASE HANDLE. FOUND RELEASE CABLE IMPROPERLY ROUTED, REROUTED RELAESE CABLE & RESET FOR TAIL CONE DEPLOYMENT. 2L72 4F A6WE 20030801001322003080100132WP 2003 8 1 MWEA030296 120030728A5753593590622 STIFFENER DOUG DC9 DC982 3022082WP T/E FLAP CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 RIGHT FLAP INTERIOR STRUCTURE INTERNAL ANGLE CORRODED AT STATION XW47.45. FABRICATED AND INSTALLED STIFFENER. 2L72 4F A6WE 20030801001332003080100133WP 2003 8 1 MWEA030297 120030728A5321993659915 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 AFT CARGO COMPARTMENT CENTER FLOORBOARD BETWEEN STATION 1117-1155 IS DAMAGED. FABRICATED ANDINSTALLED FLOORBOARD. 2L72 4F A6WE 20030805000102003080500010CE 2003 8 5 LV02003F00000 120030528A571208220009 RIB CESSNA340 340A 2076405CE CONT O520 TSIO520* 17040SO LT WING BENT B LV0RO OTHER O OTHER NRNOT REPORTED 1 CE0132PT 340A0117 DURING ANNUAL INSPECTION, NOTICED LT ENGINE HUNG LOWER THAN RT. AFTER FURTHER INVESTIGATION, FOUND LT WING RIB (PN 08220009) AT W.S. 63.45 BENT AND DISTORTED. JUST AFT OF FORWARD WING SPAR ALONG WITH OTER MEMBERS IN GEARWELL AREA. SK4148E HAD BEEN PREVIOUSLY C/W. ALSO FOUND HOLES ON TOP OF RIB AND TOP WING SKIN ( EDGED OUT) FROM PREVIOUS REPAIR. WHERE AND WHEN THE REPAIR WAS MADE IS UNKNOWN. BECAUSE OF PREVIOUS REPAIR AND BAD HOLES IN RIB IS PROBABLY THE CAUSE FOR LT ENGINE SAGGING. 1L72 3O3 O 3A25 E8CE 20030805000262003080500026CE 2003 8 5 BSY2003F00012 120030506A33403538013243 SWITCH BEECH 58 58 1152740CE CONT O520 IO520C 17032SO LANDING LIGHT DEFECTIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL074098S TH600 823839R LT LANDING LIGHT SWITCH, WHEN TURNED OFF LIGHT STAYS ON. REMOVED AND REPLACED YET ANOTHER DEFECTIVE SWITCH. 1L72 3O3 O 3A16 E5CE 20030805000272003080500027CE 2003 8 5 BSY2003F00013 120030415A7797 WIRE BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO CONNECTOR BROKEN E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0758WA TH201 827286R RT ENGINE OIL TEMPERATURE, BOUNCING AND OCCASIONALLY PEGS OUT. FOUND BROKEN WIRE AT OIL TEMP PROBE CONNECTOR REPAIRED WIRE OPS CHECK GOOD. 1L72 3O3 O 3A16 E5CE 20030805000382003080500038CE 2003 8 5 DXTA200300037 120030527A2910 O-RING CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL HYD SYSTEM FAILED E DXTAO OTHER K FLUID LOSS LDLANDING 1 GL07975QS 7500175 ON LANDING ROLL, HAD A COMPLETE LOSS OF SYSTEM HYD FLUID AND EMERGENCY BRAKE WAS USED, AIRCRAFT HYDROPLANED BUT STOPPED SAFELY, NO VISIBLE DAMAGE TO AIRCRAFT. REPLACED ORING PLUG, ON "A" HYDRAULIC MANIFOLD, AND OPERATIONALLY TESTED, BLED SYSTEM AND LEAK CHECKED, IAW CE750 M/M CP: 29-10-01. 2L72 4J4 FRTT00007WITE6CH 20030730000962003073000096SO 2003 7 30 SIMA200317401 120030618A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21712AE 145247 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL, INSTALLED NEW CENTER SILL IAW EMB REPAIR STATEMENT IC2003-145/0818 AND STANDARD SRM, SRM 145/1142 REV 22 PRACTICES. (M) 2L72 4F RTT00011AT 20030730001012003073000101WP 2003 7 30 AMTA200300867 120030701A5320 STRUCTURE LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND CRACK IN C2 PIT FLOOR AT FS 1453 CRACK IS 6 INCHES LEFT OF CENTER LINE 1 INCH LONG. PERFORMED INTERIM REPAIR PER ERA L10-53T-2549 REV B. 2L73 4F A23WE 20030730001222003073000122NM 2003 7 30 USAASB03086 120030618A2761 ACTUATOR BOEING737 7373B7 1384580NM NR 3 SPOILER LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19374US 22953 SAV - FLT 486 - DURING CLIMBOUT FROM SAV TO CLT, THE A HYD SYS LOW OIL PRESSURE LIGHT ILLUM. FLT CREW NOTED A LOSS OF A HYD SYS QUANTITY. ELEC HYD PUMPS AND NR 1 ENG DRIVEN HYD PUMP WERE SHUTOFF 40 SECONDS AFTER FIRST INDICATION OF SYS LOSS. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. FLT LANDED WITHOUT INCIDENT. MX FOUND THE NR 3 FLIGHT SPOILER ACTUATOR LEAKING. REPLACED O-RING ON FILTER CHECK VALVE CAP ON ACTUATOR PER MM 27-61-00. R&R NR 1 ENG DRIVEN HYD PUMP (P/N 65075-06) PER MM 29-15-00 DUE TO LOW PRESSURE LIGHT ON AND METAL CONTAMINATION FOUND IN CASE DRAIN FILTER. FLUSHED CASE DRAIN FILTER LINE PER MM 29-15-17. SERVICED HYDRAULIC SYSTEM TO FULL. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M)2L72 4F RTA16WE 20030303001192003030300119SW 2003 3 3 HEEA084537 120030214A243239563001 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 MAIN BATTERY WEAK. 1G72 4U H4SW 20030303001232003030300123SW 2003 3 3 HEEA084541 120030214A243239563001 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 MAIN BATTERY WEAK. 1G72 4U H4SW 20030303001242003030300124SW 2003 3 3 HEEA084542 120030214A243239563001 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 MAIN BATTERY WEAK. 1G72 4U H4SW 20030303001252003030300125SW 2003 3 3 HEEA084543 120030214A243239563001 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MAIN BATTERY WEAK. 1G72 4U H4SW 20030303001282003030300128SW 2003 3 3 HEEA084552 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03330087255 36004 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS EROSION HOLES. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030303001292003030300129SW 2003 3 3 HEEA084553 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K14738 33020 MAIN ROTOR BLADE DAMAGED, UNABLE TO TRACK OR BALANCE. APPEARS TO BE HEAVY. 1G72 4U H4SW 20030303001302003030300130SW 2003 3 3 HEEA084554 120030214A6210412015300109 BLADE BELL 412 412EP 1182205SW MAIN ROTOR OUT OF BALANCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03412PH15977 36140 MAIN ROTOR BLADE NEEDS TO BE BALANCED ACCORDING TO SPECS. 1G72 4U H4SW 20030303001752003030300175WP 2003 3 3 ASAA0280699 120030101A335060030451 POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 PDX - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN FIRST CLASS. REPLACED POWER SUPPLY. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F A6WE 20030303001782003030300178EA 2003 3 3 A6WA200340028 120030129A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA OXYGEN SERVICE OPEN A A6WAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 GL31430AW 7719 AIR RETURN FOR LOUD WHISTLE AND STALL FAIL MESSAGE. INSPECTED AND FOUND OXYGEN SERVICE DOOR OPEN. SECURED DOOR. NO DAMAGE NOTED. OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030303001872003030300187SW 2003 3 3 HEEA084569 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T11603 33112 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES ERODED THROUGH. 1G72 4U H4SW 20030303001882003030300188 2003 3 3 MWEA030121 420030302A34211428300001 GYRO DOUG DC9 DC981 3022081WP NOSE GEAR DEFECTIVE A MWEAA UNSCHED LANDING I FLT. ATTITUDE INST. TOTAKEOFF 1 GL31805ME 48031 HORIZON TILTED 30 DEGREE TO 40 DEGREE TO THE RIGHT. -- REMOVED AND RPLACED #1 MULTIDIRECTIONAL GYRO. 2L72 4F A6WE 20030303001902003030300190WP 2003 3 3 DHL2003804535 120030206A53203754051501N FITTING DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM:REF. N/R 1558 - AFT CARGO COMPT.- "T" BOLT FITTING CRACKED .5000 , STA. 1240 , L32R CORR:REMEVED DAMAGED FITTING IAW SRM51-1-20D PG. 11 . CLEANED .TREATED , AND PRIMED IAW SRM51-1-8B. INSTALLED NEW FITTING WITH NEW FASTNERS IAW SRM51-1-20D PG. 9 2L74 4F RT4A25 20030303001942003030300194WP 2003 3 3 DHL2003804539 120030205A2750 SKIN DOUG DC8 DC873F 302199FWP WORN A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF. N/R 2389 LH INBD FLAP UPPER SKIN CHAFFING WEAR AT STA. XW120.000 (MAJOR REPAIR) CORR.: PERFORMED MAJOR REPAIR IAW SRM57-1-0 PG. 1 SRM 57-7-1 PG. 2 FIG. 1 REMOVED DAMAGED SKIN IAW SRM51-1-21 PG. 1 , CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B FABRICATED NEW SKIN (2024T3.040) IAW SRM57-7-1 PG 2 FIG 1 , SRM51-1-21 PG 1. 2L74 4F RT4A25 20030303001952003030300195WP 2003 3 3 DHL2003804540 120030210A5730 SKIN DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF. N/R 2153 LH WING T/E UPPER SKIN WITH .5000 CRACK AT STA XW90.000 CORR: STOP DRILLED IAW SRM 57-2-0 FIG 2 FABRICATED DOUBLER ( 7075T6.050) IAW SRM 57-2-0 FIG 2 CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B . INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2 , SRM51-1-21 PG. 1 2L74 4F RT4A25 20030321001072003032100107NM 2003 3 21 2003UALA00250 120030309A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 AFT CABIN FLOOR BEAM CORRODED AT STA 986 RBL 7 TO RBL 44. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIR AND SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030321001162003032100116CE 2003 3 21 NSVA20030021 120030320A281079C30 DRAIN VALVE BEECH 1900 1900D 1154162CE BROKEN A NSVAK NONE O OTHER NRNOT REPORTED 1 EA27155CJ UE55 RT wing main fuel tank, outboard of Nacelle, drain valve came apart at insert and started leaking fuel. The drain valve consists of a housing and then an insert (which is the quarter turn drain assembly). These two units are held together with what appears to be a swedged flange. The flange let go and the insert fell out from fuel pressure causing a large fuel leak. The drain valve was replaced and the aircraft was returned to service. 2L72 4T RTA24CE 20030323000012003032300001SO 2003 3 23 C2XA03SH060 120030323A530014521725003 SILL EMB 135 EMB135ER 3260203SO CABINF CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 SHV DURING C CHECK THE RIGHT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED REPAIR ON AFFECTED SILL IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030324000112003032400011NM 2003 3 24 2003UALA00259 120030310A2710 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT AILERON LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29548UA 25396 CENTER HYDRAULIC SYSTEM QUANTITY EICAS MESSAGE. SYSTEM SECURED AT .23. EXCESSIVE HYDRAULIC LEAKAGE FROM LEFT AILERON POWER CONTROL ACTUATOR (PCA). REPLACED SUBJECT ACTUATOR WITH SERVICEABLE UNIT. 2L72 4F4 FRTA2NM E17NE 20030324000192003032400019NM 2003 3 24 2003UALA00270 120030313A5310 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 AFT CABIN FLOOR RT SIDE CREASE BEAM AT STATION 986 MATERIAL REMOVED BEYOND 10 PERCENT LIMIT AT 21 PERCENT MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM ANGLE. 2L72 4F4 FRTA16WE E2GL 20030324000202003032400020NM 2003 3 24 2003UALA00271 120030312A3350 BULB BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHTSBURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29672UA 30027 EXTERIOR EMERGENCY LIGHTS, 2ND AND 4TH ON LEFT SIDE, HAVE BULBS BURNED OUT. RELAMPED BURNED OUT LIGHTS 2L72 4F4 FRTA1NM E24NE 20030324000232003032400023EU 2003 3 24 307031 120030305A29102575F723 LINE BRAERODH125 HS125700A 4230170EU HYD SYSTEM CHAFED E KKYAK NONE K FLUID LOSS ININSP/MAINT 1 NE0381KA 14169961 NA038 DURING A ROUTINE POST FLIGHT INSPECTION, EVIDENCE OF HYD FLUID WAS ON THE AFT EQUIPMENT BAY DRAIN MAST. FURTHER INVESTIGATION REVEALED A HAIRLINE CRACK IN THE NR 2 ENGINE HYD PRESSURE LINE, AS IT EXTENDS INTO THE AFT BAY AREA FROM THE RT PYLON. IT WAS DETERMINED THAT THE LINE WAS CHAFING ON AN ADJACENT HYD ENGINE DRAIN LINE. IT COULD NOT BE DETERMINED (RESEARCH AIRCRAFT RECORDS) IF THE LINE LINE HAD BEEN PREVIOUSLY DISTRUBED, BUT IT WAS OBVIOUS THE LINE HAD BEEN MIS-ROUTED FOR THE CHAFING TO OCCUR. THE TWO AFFECTED LINES WERE REPLACED AND PROPERLY ROUTED, AND PRESSURE CHECKED SATISFACTORY. THE LT ENGINE LINES WERE INSPECTED, AND NO DISCREPANCIES WERE DISCOVERED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A3EU 20030324000242003032400024NM 2003 3 24 371PA0017 120030303A2810 FUEL CELL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE CENTER TANK CONTAMINATED A PIDAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO05371PA 23543 726351 NR 1 ENGINE FLAMED OUT ON CLIMB OUT FROM PUJ. VISUAL INSPECTED NR 1 ENGINE IN FAN & REVERSER AREA, FOUND NO DEFECT. DRAINED MAIN WING & CENTER TANK AND FOUND WATER IN FUEL. A/C REMAINED PARKED FOR 1.5 HOURS AND DRAINED TANK AGAIN. PERFORMED ENGINE RUN PER MM 71-00-42, ENGINE RUN NORMAL. 2L72 4F4 FRTA16NE E2GL 20030324000432003032400043NE 2003 3 24 8627 220030131A8520 BEARING BEECH 18 E18S 1151006CE PWA R985 R985AN14B 52008NE CRANKSHAFT FAILED E VLLAEA ENGINE SHUTDOWN UNSCHED LANDING KEJFLUID LOSS VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL058627A BA283 JP205004 IN CRUISE FLIGHT ENGINE STARTED TO DEVELOP A VIBRATION. ENGINE THEN STARTED TO LOSE OIL PRESSURE. ENGINE WAS SHUT DOWN AIRCRAFT DIVERTED. FOUND OIL LEAKING AT FRONT NOSE CASE AT CRANKSHAFT. SUSPECT FRONT MAIN BEARING FAILURE AND FRONT SEAL FAILURE. SOME METAL FOUND IN SCREEN. 1L72 3R3 R A765 5E1 20030324000472003032400047WP 2003 3 24 ABXA030101 120030219A52105911401 STRUCTURE DOUG DC9 DC931 3022065WP PAX DOOR DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 MAIN ENTRY DOOR FORWARD LOWER CORNER PREVIOUS REPAIR DID NOT CONFORM TO SR09530252-7011. REPAIRED MAIN ENTRY DOOR FORWARD LOWER CORNER IAW REA D953-46800-MR. 2L72 4F A6WE 20030324000502003032400050WP 2003 3 24 ABXA030106 120030305A27803923932502 SUPPORT DOUG DC9 DC941 302207NWP RIGHT WING BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 SLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, NR 1 AND NR 2 SLAT PULLEY BRACKETS BROKEN AND 3 EACH LEADING EDGE RIBS (FORMERS) DAMAGED. THE RIGHT NR 1 SLAT INBOARD IDLER PULLEY SUPPORT UPPER INBOARD ATTACH BOLT LUG WAS BROKEN IN HALF, CORRODED WITHIN THE BOLT HOLE AND CORRODED ON THE BROKEN SURFACE. THE LOWER INBOARD BOLT LUG WAS ALSO BROKEN BUT NOT CORRODED. REPLACED THE IDLER PULLEY SUPPORT IAW DC-9 MM 20-17-2-001. 2L72 4F A6WE 20030324000522003032400052WP 2003 3 24 ABXA030109 120030305A3260 PROXIMITY SWITCH DOUG DC8 DC863F 302198FWP MLG DIRTY A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23811AX 46113 ON CLIMBOUT, GEAR UNSAFE LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. RIGHT GEAR DOOR INDICATED. RECYCLED GEAR TWICE. LIGHT WENT OUT. INSPECTED RIGHT GEAR DOOR AND INDICATING SYSTEM COMPONENTS. NO DEFECTS NOTED. DOOR FAIRED ON GROUND WITH HYDRAULIC PRESSURE AND INDICATED NORMALLY. CLEANED STRIKER AND PROX. SWITCH. FOUND PROX. SWITCH WITH CAKED ON GREASE. 2L74 4F 4A25 20030324000532003032400053WP 2003 3 24 ABXA030110 120030225A531299155839 BULKHEAD DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23958AX 47760 AFT PRESSURE BULKHEAD NR 4 CRACKED AT OUTBOARD END. INSTALLED NEW ANGLE IAW DOUGLAS DWG J060110. 2L72 4F A6WE 20030324000572003032400057 2003 3 24 ABXA030116 420030312A22102588787904 COMPUTER DOUG DC8 DC863 302198AWP E & E BAY DEFECTIVE A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23822AX39 46079 IN CRUISE FLIGHT, FL350, MACH .770, AUTOPILOT ON. RUDDER GAVE UNCOMMANDED INPUT TO LEFT SIDE ON TWO OCCASIONS. RETURNED TO CENTER BY ITSELF, YAW DAMPER ON. REPLACED YAW AXIS COMPUTER. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 22-10-00. 2L74 4F 4A25 20030324000732003032400073CE 2003 3 24 AMWA11 120030212A5411 SPAR CAP BEECH 1900 1900D 1154162CE NACELLE CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07144ZV UE144 UPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP BEHIND INNER FENDER WAS CHAFED BY FUEL PRESSURE SWITCH LINE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED , ALODINED AND PRIMED THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030324000802003032400080CE 2003 3 24 AMWA9 120030212A5711 SPAR CAP BEECH 1900 1900D 1154162CE WING CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07231YV UE231 UPON A SERVICE INSPECTION MAINTENANCE FOUND THE LEFT AND RIGHT LOWER SPAR CAP BEHIND THE NACELLE INNER FEN WAS CHAFED. BLENDED, ALODINED AND PRIMED BOTH OF THE LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JV/0215-03. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030324000852003032400085WP 2003 3 24 ARWA20030303 120030312A5310 DOOR FRAME DOUG DC8 DC863 302198AWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 DURING "C" CHECK THE FOLLOWING WAS FOUND; MAIN CARGO DOOR JAMMED AT AFT SECTION INTERIOR STA 270 BETWEEN L-20L TO L-21L WITH 5 INCH CRACK. REPLACED SIDE BEAN SECTION FROM PRODUCTION SPLICE TO L-21L P/N AE2450-11 IAW DC8 SRM 51-1-21. 2L74 4F 4A25 20030324000862003032400086WP 2003 3 24 ARWA20030305 120030312A5320 WEB DOUG DC8 DC863 302198AWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA. 1180 - STA. 1190 LT CUSP WITH 2 INCH CRACK. 2L74 4F 4A25 20030324001042003032400104NM 2003 3 24 AWXA200300095 120030130A33501012621 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28311AW 24712 TUS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT ON GALLEY FORWARD OF THE L-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON GALLEY FORWARD OF THE L-2 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030324001072003032400107NM 2003 3 24 AWXA200300099 120030131A2761654456113 ACTUATOR BOEING737 737277 1384570NM NR 6 SPOILER WORN A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28183AW5534527666 22650 SLC - AIR TURN BACK - ON CLIMB OUT FROM SLC EN ROUTE FOR PHX FLIGHT ATTENDANT REPORTED AN EXTREMELY LOUD NOISE AND VIBRATION IN FLOOR BOARDS OF AFT CABIN, TURNED BACK TO SLC AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED GROUND INSPECTION OF FUSELAGE INCLUDING ALL SERVICE PANELS AND ACCESS DOORS. INSPECTED RUDDER POWER CONTROL UNITS FOR WEAR AND ABNORMAL CONDITIONS; INSPECTED THE STABILIZER, APU DOOR, AND APU MOUNTS. INSPECTED HELL HOLE AFT OF AFT PRESSURE BULKHEAD, NO DEFECTS WERE NOTED. INSPECTED THE AFT CARGO COMPARTMENT PANELS, THE ENGINE INLET & TURBINE BLADE AREAS, AND THE LANDING GEARS, NO DEFECTS NOTED. INSPECTED THE SLATS AND FLAPS FOR LOOSE FAIRINGS, AND ABNORMAL PLAY, NO DEFECTS FOUND. INSPE2L72 4F RTA16WE 20030324001142003032400114NM 2003 3 24 AWXA200300102 120030112A531165677758 FRAME BOEING737 737300 1384610NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1 1/4 INCH CRACK WAS FOUND ON LOWER INBOARD ANGLE AT BS 616 RT, RBL 60. MAINTENANCE CUTOUT CRACK ON ANGLE AT BS 616 RT, RBL 60; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENING ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5311-01143-DD1. 2L72 4F RTA16WE 20030324001152003032400115NM 2003 3 24 AWXA200300103 120030108A532065566551 REVEAL BOEING737 737300 1384610NM CARGO DOORWAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON THE AFT CARGO COMPARTMENT DOOR OPENING AFT TORQUE BOX WEB COVER. MAINTENANCE REMOVED CRACKED AFT CARGO COMPARTMENT DOOR OPENING AFT TORQUE BOX WEB; FABRICATED A NEW REPLACEMENT TORQUE BOX WEB PER DWG 65-56655, SHT 1; INSTALLED NEW REPLACEMENT WEB IAW B737-300 SRM 51-40-02, PG. 1-6, 38, FIG. 8 AND PG. 42, FIG. 10. 2L72 4F RTA16WE 20030324001162003032400116EU 2003 3 24 AWXA200300106 120030206A2560P4010021 BATTERY AIRBUS320 A320231 3930325EU ZONES 220, 260 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 LAX - EMERGENCY EQUIPMENT - DURING ROUTINE MX INSPECTION MAINTENANCE DISCOVERED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT DISCHARGED/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD FLIGHT ATTENDANT POSITION, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030324001222003032400122WP 2003 3 24 MWEA030142 120030321A216132185831 CONTROL VALVE DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A MWEAA UNSCHED LANDING O OTHER CRCRUISE 1 GL31401ME 47133 RIGHT TEMPERATURE CONTROL NOT WORKING IN MANUAL. -- REMOVED AND REPLACED RIGHT TEMPERATURE CONTROL VALVE. 2L72 4F A6WE 20030324001262003032400126EA 2003 3 24 03082669 120030323A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING MAINTENANCE INSPECTION, THE LT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030325000042003032500004EA 2003 3 25 03083673 120030324A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27673BR 7599 DURING MAINTENANCE INSPECTION, THE AFT CABIN EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL SECURED A CONNECTOR FOR THE AFT EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030325000072003032500007CE 2003 3 25 2003F00154 120030129A335067113101 WARNING LIGHT CESSNA750 750 2076810CE PAX DOOR ILLUMINATED A UG8AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL235115 7500018 CABIN DOOR OPEN AMBER LIGHT FLASHED ON AND OFF WHILE TAXIING IN AT DTW. CLEANED AND LUBRICATED DOOR BAYONETS, CLOSING LATCH AND HANDLE RELEASE MECHANISM. OPERATIONAL CHECK IS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030325000102003032500010NM 2003 3 25 AWXA200300112 120030209A3260 CABLE BOEING737 737277 1384570NM MLG SELECT VALVEOUT OF RIG A AWXAO OTHER N FALSE WARNING DEDESCENT 1 WP28178AW 22645 ON DECENT INTO PHX EN ROUTE FROM AUS AFTER LOWERING LANDING GEAR RECEIVED UNSAFE LANDING GEAR INDICATION, 3 RED OVER 3 GREEN, DECLARED EMERGENCY, LANDED WITHOUT EVENT. MAINTENANCE LUBRICATED THE LANDING GEAR HANDLE AND ADJUSTED CABLE RIG FROM THE LANDING GEAR HANDLE TO THE SELECTOR VALVE IAW BMM 32-31-0, 501. 2L72 4F RTA16WE 20030325000142003032500014EU 2003 3 25 AWXA200300123 120030128A5320D5391167020010 SUPPORT BRACKET AIRBUS320 A320231 3930325EU BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 MCN - MAJOR REPAIR - DURING C-02 CHECK A 1 .7500 INCH CRACK WAS FOUND IN THE FORWARD PIT, ON THE AFT BULKHEAD PANEL NR 131PW SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET ANGLE IAW A320 SRM 51-42-11, PG. 8, 9, & 10 FIG. 2, AND SRM 51-42-11, PG. 21 & 22, FIG. 8. 2L72 4F RTA28NM 20030325000312003032500031EU 2003 3 25 AWXA200300148 120030206A5315D5347217220300 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT FLOORBEAM BETWEEN FR 66 - 67, BS 3231. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM BETWEEN FR 66 - 67, BS 3231; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11, PG. 1-2. 2L72 4F RTA28NM 20030325000322003032500032EU 2003 3 25 AWXA200300149 120030206A5315D5347219020300 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM MOUNT HOLE FR 64 - 65, BS 3O72. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM BETWEEN FR 64 - 66, BS 3072; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11, PG. 1-2. 2L72 4F RTA28NM 20030325000362003032500036EU 2003 3 25 AWXA200300153 120030204A5315D5347218820200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM BETWEEN FR 68 - 69 L/H SIDE, BS 3257 - 3310. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM FR 68 - 69, BS 3257 - 3310; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11, PG. 1-2. 2L72 4F RTA28NM 20030325000412003032500041EU 2003 3 25 AWXA200300160 120030204A5315D53111412200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM FR 16, RBL 8. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM FR 16, RBL 8; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG. 201, PG. 201-206. 2L72 4F RTA28NM 20030325000462003032500046NM 2003 3 25 AWXA200300177 120030129A5320146N5444 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT FRAME AFT CARGO COMPARTMENT, BS 1510, RBL 7. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT FRAME BS 1510, RBL 7; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030325000562003032500056 2003 3 25 AWXA200300217 420030302A34207725005005 INDICATOR BOEING737 737277 1384570NM ADI FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28183AW 22650 ON CLIMB OUT FROM SLC EN ROUTE TO PHX THE CAPTAINS ATTITUDE DIRECTOR INDICATOR (ADI) "ATT" RED FLAG APPEARED, AND "PITCH" AND "ROLL" COMPARATOR LIGHTS ILLUMINATED. SWITCHED TO CAPTAINS ON AUX WITH NO HELP; TURNED BACK TO SLC. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS ADI IAW BMM 34-26-11, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030325000572003032500057NM 2003 3 25 AWXA200300218 120030228A3150 WARNING SYSTEM BOEING737 737375 13844BNNM COCKPIT FALSE ACTIVATIONA AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28336AW 23707 ON TAKEOFF ROLL SLC EN ROUTE FOR PHX REJECTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. DETERMINED STAB TRIM WAS ON AFT EDGE OF GREEN BAND, RESET STAB TRIM AND CONTINUED WITHOUT FURTHER EVENT. 2L72 4F RTA16WE 20030325000692003032500069EU 2003 3 25 AWXA200300233 120030306A3350321454 BATTERY PACK AIRBUS320 A320232 3930326EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28638AW307261457 455 DURING INSPECTION THE EMERGENCY EXIT LIGHTS IN FORWARD GALLEY WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030325000702003032500070 2003 3 25 AWXA200300235 420030307A341746502003030312 ADC AIRBUS320 A320232 3930326EU ZONE 130 MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28653AW14284 1003 ON TAKEOFF ROLL AT PHX EN ROUTE FOR PHL RECEIVED ECAM MESSAGE FOR AUTOFLIGHT, AUTOTHRUST, AND TWO OTHER MESSAGES THAT WE WERE NOT ABLE TO READ DUE TO TIME CONSTRAINT. REJECTED TAKEOFF JUST PRIOR TO 80 KTS. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW T/C R2A34304. RESTORED AIRCRAFT TO CAT IIIB STATUS. VENDOR BENCH TEST CONFIRMED FAILURE OF ADIRU S/N 2016. REPLACED ELECTRONIC SENSOR ASSEMBLY P/N; 465750-03, S/N; 5212, AND LOW VOLTAGE POWER SUPPLY. PERFORMED THERMAL CALIBRATION, TESTED UNIT, AND RETURNED TO SERVICE. 2L72 4F RTA28NM 20030325000842003032500084NM 2003 3 25 03FDEA00345 120030318A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 FORWARD CABIN SEAT TRACK AT STA.487, RIGHT SIDE 27.5 INCHES WITH CORROSION. 2L73 4F4 FRTA22WE E13NE 20030326000102003032600010SO 2003 3 26 AUS20030098 120030131A2710 CONTROL CABLE MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL AILERON WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AILERON CABLES WORN AT FUSELAGE FAIRLEADS. 1H71 3O3 ONC3A23 E286 5 CP920 20030326000292003032600029GL 2003 3 26 AUS20030126 120030115A7120AN523 BOLT EAGLE XTS EAGLEXTS150 05607BZGL CONT O240 IO240A SO MCAULY1A135 1A135BRM GL ENGINE MOUNT SHEARED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BOTTOM RT ENGINE MOUNT BOLT SHEARED. 1H71 3I3 ONCA00005LAE7SO 5 NP842 20030326000342003032600034NM 2003 3 26 AUS20030138 120030211A5312 FRAME BOEING767 767338 1385151NM GE CF6 CF680C2* GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE BULKHEAD OUTER CHORD CRACKED AT STA 1809. FOUND DURING INSPECTION IAW AD/B767/146. 2L72 4F4 FRTA1NM E23EA 20030326000352003032600035NE 2003 3 26 AUS20030151 220030210A726162644715 RELIEF VALVE BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE ENGINE FAULTY W O OTHER EK VIBRATION/BUFFET FLUID LOSS CLCLIMB 1 AUS (AUS) NR 1 ENGINE OIL PRESSURE RELIEF VALVE FAULTY. 2L73 4F4 FRTA3WE E2EA 20030326000602003032600060EU 2003 3 26 CA030203005 120030119A2897 WIRE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BOOST PUMP BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PUMP WAS INSTALLED ON JANURAY 13, 2003. AIRCRAFT WAS RUN FOR 1.5HRS OVER THE 16TH, 17TH, 18TH OF JANUARY.ON THE 19TH THE PILOT NOTED THAT THE NR 2 PUMP WAS OPERATING INTERMITTENTLY. INSPECTION REVEALEDTHAT THE HOLE IN THE COVER FOR THE WIRE WAS OUT BY 180 DEGREES TO THE WIRE ATTACHMENT POINT. THE WIRE WAS CUT BY A CUPPED WASHER ON THE MOTOR SHAFT. WIRE WAS REPAIRED AND THE COVER PUT ON INLINE WITH THE ATTACHMENT POINT.AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 UNCH9EU E19EU 20030326000622003032600062NM 2003 3 26 CA030204010 120030123A533085337034 SKIN BOMBDRDHC8 DHC8400 NM PWC 150 PW150A EA FUSELAGE WRINKLED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) SKIN ASSEMBLIES 85337034 AND 85337055 ARE 'WRINKLED' BETWEEN X819 AND THE REAR PRESSURE BULKHEAD (RPB), BOUNDED BY STRINGERS 22 TO 25 PORT AND STARBOARD. THE TYPICAL 'WRINKLE' OCCURS BETWEEN THE 5TH AND 6TH FASTENER (COUNTING FORWARD ON THE INTERNAL FINGER DOUBLER 85337355) JUST FORWARD OF THE INTERNAL FINGER DOUBLER ENDS, ALONG THE STRINGER LINE.IT APPEARS THAT THERE IS A FITTMENT PROBLEM WITH TAPERED SHIMS (CSP471-040-010-190-065) SHOWN IN SECTION F-F (RHS SKIN ASSY. DRAWING 85337055 SHEET 2 - LT 85337034 SIMILAR). IN-SERVICE REPAIR RD8/4-53-390AND RD8/4-53-0387 ISSUED 2H72 4T4 TRTA13NM E00062EN 20030326000782003032600078NM 2003 3 26 2003UALA00198 120030222A49204500381 TURBINE WHEEL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE APU FAILED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29926UA1096610966 26648 932368 APU HAD AUTO SHUTDOWN EVENT AT DEPARTURE GATE AS THE RESULT OF THE APU TURBINE FAILURE. THERMAL FATIGUE BLADE FAILURE. MINIMAL DUE TO RATE OF INCIDENTS: MTBF IS 2,414,347 HOURS AND 3,380,158 CYCLES. TRENDING WHEEL PERFORMANCE. CONSIDER DEVELOPMENT OF ON-WING INSPECTION METHOD(S) THAT CAN FIND SCALLOP CRACK INDICATIONS. 2L72 4F4 FRTA16WE E2GL 20030326000832003032600083NM 2003 3 26 2003UALA00278 120030316A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 FUSELAGE FRAME AT STRINGER 847 HAD CRACK OUT OF FASTENER HOLE AT STR.9L (AIR GRILL SUPPORT) MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030416002302003041600230SO 2003 4 16 CHQA000247 120030406A3610 CLAMP EMB 145 EMB145LR 3260212SO NR 1 PYLON LEAKING A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11279 145379 LAV SMOKE WARNING (AURAL, VISUAL, EICAS) ON CLIMB OUT. ALSO HAD NR 1 BLEED LEAK WARNING. EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. FIRE DEPT MET WITH AIRCRAFT. NO SMOKE WAS NOTED. UPON INVESTIGATION, FOUND 2 CLAMPS LEAKING IN NR 1 PYLON BY PRECOOLER IAW MM 36-11-04. NO DEFECTS NOTED DURING GROUND RUN. 2L72 4T RTT00011AT 20030416003302003041600330EA 2003 4 16 SWIA200311731 120030102A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW 7518 FS 621 LT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117. ANGLE P/N: 601R-53-61-117-1 REP, ANGLE P/N: 601R-53-61-117-3. 2L72 4F RTA21EA 20030416003532003041600353NM 2003 4 16 UPS03440010 120030104A5320 FLOOR SUPPORT BOEING747 747259B 1384804NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE: C M/D - AFTER FLOOR PANEL REMOVED, FLOOR SUPPORT FOUND CORROSION AT BS 2280-2300 LBL 60. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8. DEPTH 0.035 INCH, WIDTH 1 INCH, LENGTH 3 INCHES. 2L74 4F RTA20WE 20030416003702003041600370NE 2003 4 16 P5CA0300717 220030107A75302605290001 CABLE BOEING747 747300 GL GE CF6 CF650E2 30018NE NR 4 VSV RETURN FAULTY A P5CAO OTHER O OTHER DEDESCENT 1 WP2324837 24837 530277 NR 4 ENGINE COMPRESSOR STALL AT TOP OF DESCENT - EGT 700 DEGREES, N1 20 PERCENT LESS THAN OTHER ENGINES. STALL CLEARED AT 33.0. REPLACED NR 4 ENGINE VSV RETURN CABLE PER MM 75-30-00. BOROSCOPED ENGINE IAW AMM 72-00-00. ENGINE RUN CARRIED OUT AS PER AMM 71-00-00, TEST 4. ALL ENGINE, OPS SATISFACTORY. 2L74 4F4 FRTA20WE E23EA 20030416003922003041600392EA 2003 4 16 SWIA200311708 120030111A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA FLUTTER DAMPER CHAFED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07426SW 7468 FLUTTER DAMPER STATUS MESSAGE IN FLIGHT, AMBER ARC ON L AILERON ON FLIGHT CONTROL SYNOPTIC PAGE. NO CHANGES TO CONTROLLABILITY ON CONTROL FEEL NOTED. FOUND CHAFED WIRE IN MIDDLE WING SECTION LEADING EDGE. REPAIRED WIRE IAW WMM 20-16-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20030417000312003041700031EU 2003 4 17 MALA030124 120030125A7930 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A1 30030NE RIGHT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL1546XJ 340A046 DURING FLIGHT 2747, DTW-CAK RT ENGINE OIL PSI LIGHT ON STEADY, AND OIL PSI GAUGE WAS IN THE YELLOW APPROACHING RED BAND DURING CONVERSATION WITH MAINTENANCE CONTROL. FLIGHT DIVERTED TO CLE. RT ENGINE OIL PSI WARNING LIGHT CAME ON, AND GAUGE PRESSURE WAS DROPPING RAPIDLY, CREW SHUTDOWN ENGINE. MAINTENANCE FOUND OIL LEVEL 4.0 QUARTS LOW, ENGINE CHANGE REQUIRED DUE TO EXCEEDED MM LIMIT FOR OIL LOSS. MAINTENANCE REPORTED MIXING DUCT HEAVILY COKED (ABOUT 1/4 INCH THICK) TAIL PIPE DRY. COULD NOT VERIFY WHERE OIL LOSS OCCURRED ON ENGINE. ENGINE CHANGE IN PROGRESS. 2L72 4T4 TRTA52EU E8NE 20030417000692003041700069 2003 4 17 SWIA200311741 420030127A3417 COMPUTER CNDAIRCL600 CL6002B19 1900309EA NR 1 AIR DATA MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07590SW 7077 OVERSPEED CLACKER WHEN FLAPS EXTENDED FROM 20 DEGREE POSITION THROUGH 30 DEGREE AND 45 DEGREE POSITION. CONTINUED UNTIL FLAPS RETRACTED AFTER LANDING TO THE 20 DEGREE POSITION. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER (ADC 850A) IAW MM 34-13-01. PERFORMED OPERATIONAL CHECK OF AIR DATA COMPUTER WITH PITOT STATIC EQUIPMENT IAW MM 34-11-00. 2L72 4F RTA21EA 20030417000952003041700095NE 2003 4 17 SWIA200311751 220030129A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT FLAMED OUT A SWIAO OTHER XP ENGINE FLAMEOUT NO WARNING INDICATION LDLANDING 1 NM07591SW 7079 RT ENGINE EXPERIENCED FLAME-OUT DURING LANDING ROLLOUT AT PNS. PERFORMED FULL ENGINE RUN WITH CREW. TAKEOFF POWER, THEN REDUCED TO IDLE AND REVERSE POWER UP. CHECKED NORMAL OK FOR CONTINUED SERVICE. PERFORMED INSPECTION AND RUN UP PER MM 76-10-00 AND 71-00-00. 2L72 4F4 FRTA21EA E15NE 20030417001032003041700103WP 2003 4 17 UPS03840138 120030202A5414 PANEL DOUG DC8 DC871F 302199DWP NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 NR 4 PYLON SIDE HAS 3.5 INCH CRACK IN ACCESS PANEL 499E {FIBERGLASS PANEL} 8 INCHES AFT OF L/E OF PANEL VERTICAL CRACK FROM BOTTOM EDGE OF PANEL. PANEL REPAIRED PER REF SRM 51-1-19. 2L74 4F RT4A25 20030417001322003041700132WP 2003 4 17 UPS03840147 120030130A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, FUSELAGE SKIN IS CRACKED AT STA 1734 ABOVE LONG 16L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030417001392003041700139NM 2003 4 17 ZW0A0301804 120030205A3350 BATTERY DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139420D 49824 THE EMERGENCY OVERHEAD LIGHTS WERE INOPERATIVE IN AREA OF ROW 9, AFT AIRSTAIR AREA OVERHEAD, AND 2 OF 3 TAIL CONE LIGHTS. REPLACED BATTERIES FOR ROW 9, PN 408822-101, AND REPLACED ONE SET OF BATTERIES FOR THE OTHER TWO AREAS, PN 408822-101. CHECK-C 11-6-02 STL. 2L72 4F RT 20030417001952003041700195NM 2003 4 17 P5CA0300760 120030204A5315 FLOORBEAM BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LEVEL 1 CORROSION FOUND ON FLOORBEAM STA 2320/LBL 20/WL 208. CORRODED AREA TRIMMED OUT. REINFORCED AREA PER SRM 53-11-25. 2L74 4F A20WE 20030417002052003041700205WP 2003 4 17 UPS03840173 120030203A532057505401 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE:C1 INTERCOSTAL CRACKED ON BOTTOM SIDE AT STA 660 AT LONG 11L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5750540 AND SRM 51-1-20D. 2L74 4F RT4A25 20030417002092003041700209NE 2003 4 17 QXEA0300252 220030212A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX1496 10049 GEE965319 PDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE BROKEN OFF. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. NVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT 1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030418000172003041800017EU 2003 4 18 MALA030157 120030215A3020 THERMISTER SAAB SF340 340B 7860101EU INTAKE HEAT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15447XJ 340B447 DURING FLIGHT NR 3336, LT INTAKE HEAT LIGHT CYCLING. AIR RETURN TO MEM. MAINTENANCE SWAPPED NR 1 AND 2 THERMISTERS TO SPARE THERMISTERS NR 4 AND 5, RAN A/C FOR 40 MINUTES ALL SYSTEMS CHECK NORMAL. 2L72 4T RTA52EU 20030418000182003041800018EU 2003 4 18 MALA030158 120030215A7931 INDICATOR SAAB SF340 340B 7860101EU RT ENG OIL MALFUNCTIONED A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15450XJ 340B450 DURING FLIGHT 2907, RT ENGINE OIL PRESSURE FLUCTUATING. RT ENGINE OIL PRESSURE INDICATING 50 PSI + OR - 5. DURING DESCENT RT ENGINE OIL PRESSURE INDICATED APPROXIMATELY 40 PSI, AT FLIGHT IDLE. ALL OTHER ENGINE PARAMETERS NORMAL INDICATOR BOUNCED APPROXIMATELY 5 PSI. MAINTENANCE UPON INSPECTING ENGINE FOUND QUANTITY TO BE WITHIN LIMITS. RAN ENGINE HAD 35 PSI, SWAPPED INDICATOR WITH LT SIDE, PRESSURE JUMPED TO 50-55 AND STEADY, ALL CHECKS GOOD. 2L72 4T RTA52EU 20030418000522003041800052WP 2003 4 18 UPS03840190 120030208A57403704841501 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED AT XRS 74 INBOARD SIDE. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D. 2L74 4F RT4A25 20030327001472003032700147SO 2003 3 27 C2XA03IA015 120030205A3230355022002MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A C2XAK NONE O OTHER CLCLIMB 1 SW2713988 145265 FLIGHT 2910, GEAR DID NOT RETRACT WHEN HANDLE PLACED IN UP POSITION, THIRD TRY SUCCESSFUL. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT, OPS TEST GOOD. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001502003032700150SO 2003 3 27 C2XA03IA020 120030214A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713990 145277 DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY FLOOR LIGHTING FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001782003032700178SO 2003 3 27 C2XA03TY004 120030115A575114569009406 ATTACH FITTING EMB 145 EMB145ER 3260211SO RT AILERON DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27149408756 145033 DURING A SCHEDULED 3-C INSPECTION THE RT AILERON PCA ATTACH FITTING WAS FOUND DAMAGE AND THE BOLT FROZEN. MAINTENANCE REMOVED AND REPLACED THE RT HAND AILERON PCA ATTACH FITTING, PRIMED AND PAINTED IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030327001802003032700180SO 2003 3 27 C2XA03TY011 120030123A2916 CAP EMB 145 EMB145LR 3260212SO HYD SYSTEM LOOSE A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2715912 145439 DURING A SCHEDULED FLIGHT FROM EWR TO BHM (FLT 2674), THE AIRCRAFT WAS DIVERTED INTO TYS FOR AN EMERGENCY LANDING. THE CREW REPORTED HYD NR 1 LOW LEVEL. MAINTENANCE FOUND THE REFILL CAP LOOSE AND SERVICED THE SYSTEM IAW-EMB-145-AMM-12-13-01. FOUND RETURN FILTER BYPASS INDICATOR POPPED, CHANGED FILTER AND O-RINGS IAW-EMB-145-AMM-29-10-08. THE AIRCRAFT WAS RELEASED FOR TEST FLIGHT. TEST FLIGHT SATISFACTORY, AIRCRAFT RELEASED TO SERVICE. 2L72 4T RTT00011AT 20030327001862003032700186CE 2003 3 27 CA030210001 120030203A30209091009913 TUBE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA ANTI ICE SYS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LT INBOARD ANTI ICE TUBE FOUND CRACKED AT LOWER (COWL) ATTACH POINT .1 INCH FROM ANGLE FITTING. FLEX HOSE ASSY REPLACED WITH NEW PART. NOTE, RECENT INSTALATION IN COMPLIANCE WITH RAYTHEON S/B 71-3142. 1L72 3T4 TRT3A20 E4EA 20030325000872003032500087NM 2003 3 25 AWXA200300256 120030312A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28309AW 24711 FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE AFT GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE EMERGENCY FLASHLIGHT IN AFT GALLEY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030326000092003032600009SO 2003 3 26 AUS20030096 120030131A2840 INDICATOR MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL FUEL SYSTEM INACCURATE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL INDICATING SYSTEM OUT OF CALIBRATION. 1H71 3O3 ONC3A23 E286 5 CP920 20030326000142003032600014SO 2003 3 26 AUS20030102 120030131A2434ALE1013AS BRUSHES MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL DC GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ALTERNATOR CONTAMINATED WITH ENGINE OIL FROM A DETERIORATED CRANKSHAFT SEAL. THE UNIT WAS DISASSEMBLED AND THE FOLLOWING DEFECTS NOTED: THROUGH BOLTS WERE NOT LOCKWIRED, THROUGH BOLT THREAD STRIPPED. DRIVE END BEARING NOISY. BRUSHES WORN TO LIMITS. INTERNAL AND EXTERNAL OIL CONTAMINATION. 1H71 3O3 ONC3A23 E286 5 CP920 20030326000252003032600025EU 2003 3 26 AUS20030120 120030206A5730HC573H0002001 SKIN BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING LOWER SKIN CORRODED BEYOND LIMITS. FOUND DURING X-RAY INSPECTION. 2H74 4F4 FRTA49EU E6NE 20030326000282003032600028NM 2003 3 26 AUS20030125 120030113A28972841200029222 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE FUEL QTY SYS WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL QUANTITY SYSTEM WIRE 284120002922-2 LOCATED UNDER WING ACCESS PANEL 624AT AT WING STN 225 FOUND TO BE CHAFED IN AREA WHERE WIRE ASSEMBLY EXITS ALLOY CONDUIT AND GOES TO FUEL QUANTITY PROBE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030326000382003032600038EU 2003 3 26 AUS20030156 120030209A3260 PLATE BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE MLG MISINSTALLED W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NOSE LANDING GEAR SQUAT SENSOR PLATE FITTED UPSIDE DOWN. A NEWLY OVERHAULED LANDING GEAR HAD JUST BEEN FITTED AND THE SENSOR PLATE HAD BEEN INCORRECTLY FITTED BY THE OVERHAUL FACILITY. PERSONNEL/MAINTENANCE ERROR. 2H74 4F4 F A49EU E6NE 20030326000612003032600061EU 2003 3 26 CA030204009 120030128A2750ABS012130 PROXIMITY SENSOR AIRBUS320 A320212 3930322EU CFMINTCFM56 CFM565A3 NE RT WING LOOSE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN) A/C WAS ON APPROACH WITH CONFIG 1 SELECTED. ATF SPEED, FLAP 2 WAS SELECTED AND FLAPS LOCKED BETWEEN 0 AND 1. SLATS OPERATED NORMALLY. NO EMERGENCY WAS DECLARED. DUE TO ADVERSE WEATHER CONDITIONS AND HIGHER THAN NORMAL LANDING SPEED, 2 LT MAIN WHEELS OVERHEATED AND LOST THEIR THERMAL PLUGS WHILE AT GATE. A CHARTER A/C WAS SENT WITH 2 MAIN WHEELS, AND WHEEL CHANGE EQUIPMENT. MAIN WHEEL WERE REPLACED, AND FLAP SYSTEM VERIFIED FOR PROPER OPERATION. SYSTEM COULD NOT BE FAULTED ON GROUND. A/C RETURNED TO OTTAWA, RIGGING AND FULL SYSTEM INSPECTION TOOK PLACE. RT WING FLAP PROX SENSOR WAS FOUND TO HAVE AN UNLOCKED AT CONNECTOR. BOTH LT AND RT WING PROX SENSORS WERE REPLACED, AND AIRCRAFT RELEASED FOR SERVICE. 2L72 4F4 FRTA28NM E29NE 20030326001092003032600109EA 2003 3 26 A6WA200340034 120030309A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR FALSE INDICATIONA A6WAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL31421ZW 7346 PAX DOOR WARNING AFTER TAKEOFF PLACARDED AND PLACED ON MEL 52-70-011. MAINTENANCE VERIFIED DOOR CLOSED AND LOCKED PROPERLY. 2L72 4F4 FRTA21EA E15NE 20030326001122003032600112EU 2003 3 26 A6WA200360002 120030308A2611473597404 SMOKE DETECTOR BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA CARGO BAY INOPERATIVE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31291UE8199 8199 E2084 DURING INSPECTION FORWARD CARGO BAY B LOOP ON NR 1 DETECTOR FAILED (POSITION 1FW). MAINTENANCE REMOVED AND REPLACED NR 1 SMOKE DETECTOR, OPERATIONAL TEST GOOD. 2H74 4F4 F A49EU E6NE 20030327000312003032700031EU 2003 3 27 AWXA200300303 120030316A5321D5367004800400 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 3158, FR 66, TO BS 3257, FR 68. MAINTENANCE REMOVED DAMAGED FLOOR PANEL BS 3158, FR 66, TO BS 3257, FR 68; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW AWA E.O. 53-22-03. 2L72 4F RTA28NM 20030327000322003032700032EU 2003 3 27 AWXA200300304 120030316A5321D5367004300200 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 3093, FR 64, TO BS 3158, FR 66. MAINTENANCE PERFORMED BOND REPAIR ON UPPER SURFACE OF CABIN FLOOR PANEL BS 3093, FR 64, TO BS 3158, FR 66 IAW A320 SRM 53-02-00, PG. 203-207, FIG. 201, PARA. 2. 2L72 4F RTA28NM 20030327000522003032700052NM 2003 3 27 C1HA200381005 120030201A5270 SWITCH BOEING727 7272S7 138407ZNM MLG DOOR MALFUNCTIONED A C1HAO OTHER N FALSE WARNING CLCLIMB 1 GL15681CA 22020 RT GEAR DOOR LIGHT REMAINED ILLUMINATED. R&R'D GEAR DOOR WARNING SWITCH ON RIGHT HAND GEAR DOOR AS PER M/M 32-62-11 2L73 4F A3WE 20030327000862003032700086SO 2003 3 27 C2XA038TY 120030324A531514522226003 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 DURING A SCHEDULED 3C INSPECTION, A GOUGE WAS DISCOVERED IN THE FLOORBEAM LOCATED JUST AFT OF THE LAV. BULKHEAD, RT SIDE. THE RT FLOORBEAM TOP CAP WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 51-70-02. ACFT. WAS RELEASED FOR SERVICE FOLLOWING THE COMPLETION OF THE SCHEDULED INSPECTION. 2L72 4F RTT00011AT 20030327000962003032700096SO 2003 3 27 C2XA03BT044 120030323A3350110049 BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2715555 145594 CREW REPORTED, EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030327001032003032700103SO 2003 3 27 C2XA03CL016 120030119A3260 CONNECTOR EMB 145 EMB145 3260210SO NLG PROX SENSOR LOOSE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2722971 145149 CLE FLIGHT 2144 THE CREW REPORTED AFTER TAKEOFF RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED THE BACKSHELL AND CLEANED THE CONNECTOR PLUG TO THE NOSE GEAR WEIGHT ON WHEELS PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001252003032700125SO 2003 3 27 C2XA03CL059 120030302A3350BA50933901 CHARGER EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST NRNOT REPORTED 1 SW2712126 145693 CLE FLIGHT 2048 THE CREW REPORTED THE EMERGENCY LIGHT WAS INOPERATIVE ON THE LEFT SIDEWALL. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001652003032700165SO 2003 3 27 C2XA03SH043 120030310A532014522198003 SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK THE CENTER FLOORBEAM SUPPORT COLUMN WAS FOUND TO HAVE CORROSION AT FRAME 60. MAINTENANCE REMOVED AND REPLACED AFFECTED COLUMN IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001672003032700167SO 2003 3 27 C2XA03SH048 120030310A531014524767031 SHEAR TIE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK SHEAR CLIPS WHERE FOUND TO HAVE CORROSION BETWEEN FRAMES 67 TO 69 AT STRINGERS 21 LT TO 20 RT. MAINTENANCE REMOVED AND REPLACED AFFECTED SHEAR CLIPS IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001732003032700173SO 2003 3 27 C2XA03SH057 120030316A5310 THRESHOLD EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 DURING C-CHECK PASSENGER DOOR THRESHOLD U-SHAPE WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED U-SHAPE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327001752003032700175SO 2003 3 27 C2XA03SH37 120030307A5310 BUTT STRAP EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK CORROSION WAS FOUND ON CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001942003032700194SO 2003 3 27 CA030211007 120030203A55114653824 SPAR PIPER PA31T PA31T2 7103127SO PWA PT6 PT6A135 52043NE HORIZONTAL STAB CRACKED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) DURING SCHEDULED 100 HOUR EVENT NR 2 INSPECTION, CRACKS FOUND ON LEFT SIDE STABILIZER SPAR ASSEMBLY AFT BETWEEN RIB STABILIZER LEADING EDGE BL102 AND BL114. 1L72 3T4 TRTA8EA E4EA 20030326000992003032600099NM 2003 3 26 2003UALA00303 120030319A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 MAIN CABIN FLOORBEAM CORRODED ON TOP CAP BS 859.3, LBL 52 AND ENDS AT BS 890. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA AND FABRICATED REPAIR. 2L72 4F4 FRTA1NM E24NE 20030326001012003032600101NM 2003 3 26 2003UALA00305 120030319A5330 SKIN BOEING777 777222 1385219NM FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29206UA 30212 EXTERIOR SKIN IS CREASED AT STA 2115 AFT OF DOOR 4 LT BETWEEN STRINGERS 22 AND 24. MAJOR REPAIR ACCOMPLISHED. EXT DOUBLER INSTALLED. 2L72 4F RTT0001SE 20030326001052003032600105NM 2003 3 26 A6WA200330007 120030313A2910MS287784 O-RING DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HYD LINE TORN A A6WAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL31328MX 3071 HYDRAULIC MAIN QUANTITY LOW CAS ILLUMINATED AFTER GEAR RETRACTION FOLLOWED BY PRIORITY VALVE CLOSED AND STBY PUMP CONTINUES EXTENDED GEAR WITH AUX. FOUND TORN O-RING INBOARD HYDRAULIC LINE TO PILOT VALVE. REMOVED AND REPLACED O-RING, INSPECTED HYD SYSTEM FILTERS FOR DEBRIS. NO DEFECTS NOTED. SERVICED HYD SYSTEM AS REQUIRED NO LEAKS NOTED, OPS CHECK GOOD. 2H72 4T4 TRTA45NM E20NE 20030326001062003032600106EA 2003 3 26 A6WA200340031 120030304A2420 GENERATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 2 FAILED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31403AW 7288 ADG DEPLOYED IN FLIGHT AUTOMATICALLY WHEN GEN 1 WAS MANUALLY SHUT OFF WITH GEN 2 OFF LINE STOWED ADG. SQUIB FIRED. REPLACEMENT NOT AVAILABLE. AUTO DEPLOY FUNCTION PLACED ON MEL. 2L72 4F4 FRTA21EA E15NE 20030327000182003032700018NM 2003 3 27 AWXA200300285 120030301A53306573142 SKIN BOEING737 737277 1384570NM FUSELAGE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 DURING C-18 CHECK 4 SMALL CREASES WERE FOUND IN FUSELAGE SKIN AT BS 450, STR 26-27 RT. MAINTENANCE CUTOUT CREASED SKIN AT BS 450, STR 26-27 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 53-30-3, FIG. 6, PG. 11. 2L72 4F RTA16WE 20030327000412003032700041NM 2003 3 27 AWXA200300313 120030228A5320146N524013 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON SUPPORT ANGLE ON UNDER SIDE OF SHEAR DECK AT BS 1715, RBL 0-5. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT BS 1715, RBL 0-5; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 146N5240-13. 2L72 4F RTA2NM 20030327000512003032700051NM 2003 3 27 C1HA200381004 120030209A2611 FIRE LOOP BOEING727 7272S7 138407ZNM CARGO BAY INOPERATIVE A C1HAO OTHER L NO TEST CRCRUISE 1 GL15681CA 22020 AFT CARGO SMOKE DETECTOR B LOOP INOP. REMOVED & REPLACED AFT CARGO SMOKE DETECTOR "B" LOOP . 2L73 4F A3WE 20030327000642003032700064NM 2003 3 27 C1HA200388002 120030216A3260 BULB BOEING727 7272S7 138407ZNM MLG INDICATOR BURNED OUT A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15688CA 22344 'RIGHT GEAR' GREEN LIGHTS-RIGHT SIDE BURNED OUT. R & R LAMP NOSE GEAR GREEN INDICATOR. OPS NORMAL 2L73 4F A3WE 20030327001352003032700135SO 2003 3 27 C2XA03CL075 120030321A33501317 LAMP EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711535 145518 CLE FLIGHT 2863 THE CREW REPORTED THE AFT CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LAMP IN THE AFT EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001412003032700141SO 2003 3 27 C2XA03IA008 120030125A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716951 145063 DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LAST EMERGENCY LIGHT FLOOR STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001442003032700144SO 2003 3 27 C2XA03IA011 120030129A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A C2XAO OTHER O OTHER CRCRUISE 1 SW2714573 145638 FLIGHT 2856, THE CREW NOTED THAT THE LANDING GEAR DISAGREE APPEARED ON EICAS AFTER TAKEOFF AND THE LANDING GEAR WOULD NOT RETRACT. NOTE, HYDRAULIC QUANTITY AND PRESSURE INDICATION NORMAL. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001452003032700145SO 2003 3 27 C2XA03IA012 120030129A32348271013 LEVER EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A C2XAO OTHER O OTHER CRCRUISE 1 SW2714573 145638 FLIGHT 2856, THE CREW NOTED THAT THE LANDING GEAR LEVER DISAGREE MESSAGE APPEARED ON EICAS AFTER TAKEOFF AND THE LANDING GEAR WOULD NOT RETRACT. NOTE, HYDRAULIC QUANTITY AND PRESSURE INDICATION NORMAL. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001622003032700162SO 2003 3 27 C2XA03SH030 120030227A5315 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV- DURING C-CHECK A RAMP ANGLE WAS FOUND CRACKED ON LEFT HAND FLOORBEAM FOWARD OF FRAME 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED AND ANGLE REPAIR IAW EMB SRM 51-30-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20040324000282004032400028WP 2004 3 24 ASAA0380724 120031111A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURNG 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-180. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040324000312004032400031WP 2004 3 24 ASAA0380710 120031103A5347593054787 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND RIGHT OUTBOARD SEAT TRACK IS CORRODED, EXFOLIATED, AT FS 220. REPLACED DAMAGED TRACK PER SRM 53-05, 53-10-1, AND 51-30-1. (M) 2L72 4F RTA6WE 20040324000182004032400018NM 2004 3 24 ASAA0340344 120031114A5740654544555 ATTACH ANGLE BOEING737 7374Q8 138447QNM RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01755AS 25096 GYR - DURING SI CHECK, RT WING FUEL TANK RIB ATTACH ANGLE CRACKED AT STATION 135.5. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20030321000132003032100013NM 2003 3 21 2003UALA00167 120030212A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 LT STATION 188 FRAME IS CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED MODIFIED FRAME. 2L72 4F4 FRTA16WE E2GL 20030321000162003032100016NM 2003 3 21 2003UALA00173 120030211A5320 STIFFENER BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29211UA 30217 FOUND 3 STIFFENERS CRACKED AT STA 246 FLOORBEAM: LBL 38.5, RBL 7.88, RBL 26.06. MAJOR REPAIR ACCOMPLISHED. STIFFENERS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20030321000182003032100018NM 2003 3 21 PCAA0303058 120030319A291082950010251 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003NM INBOARD RIGHT LEAKING A PCAAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 EA13827EX 390 LGA-ROC FLIGHT#3785. CREW REPORTED LOSS OF #1 HYDRAULIC CONTENTS. RAN LESS THEN ONE MINUTE WITH CONTENTS LOST. CREW DECLARED AN EMERGENCY. FLIGHT LANDED IN BGM WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE FOR FLIGHT SPOILER UNLOADING VALVE FOR SPOILER CLUTCH IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 20-06-03. NO LEAKS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030321000232003032100023EA 2003 3 21 03075655 120030316A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 During maintenance inspection the L/H aft exterior emergency exit light was found to be inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030321000282003032100028NM 2003 3 21 2003UALA00183 120030215A2751 FLAP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE MALFUNCTIONED A UALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP29902UA 25002 AIRCRAFT MADE A LANDING UNDER AMBER ALERT BECAUSE OF A FLAP SYMMETRY PROBLEM. 2L72 4F4 FRTA16WE E2GL 20030321000292003032100029NM 2003 3 21 2003UALA00186 120030222A2611PU90461R2 SMOKE DETECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LAVATORY MALFUNCTIONED A UALAO OTHER N FALSE WARNING CRCRUISE 1 WP29649UA 25286 SMOKE ALARM WENT OFF IN AFT LAV. NO SMOKE OBSERVED AND FLIGHT LANDED UNEVENTFULLY. SUPPLEMENTAL DATA UPDATE THE AFT CENTER LAV SMOKE DETECTOR WAS AT FAULT. THE UNIT WAS REPLACED WITH P/N PU90-461R3 (PCN 563-3542) . THE SYSTEM CHECKED FINE AFTERWARD. 2L72 4F4 FRTA1NM E24NE 20030321000322003032100032NM 2003 3 21 751PA0013 120030320A3397 WIRE BOEING757 757200 1384950NM CABIN DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 TRACK LIGHTING AT L3 DOOR, RED, INOP. REPAIRED WIRE AND RELAMPED. OPS CHK. NORMAL 2L72 4F RTA2NM 20030321000332003032100033NM 2003 3 21 2003UALA00189 120030211A5754114W423012 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 12 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29766UA 26917 DELAMINATED TRAILING EDGE WEDGE SLAT NR 12 BECAME DELAMINATED. REMOVED AND REINSTALLED T/E WEDGE. 2L72 4F4 FRTT0001SE E46NE 20030321000372003032100037NM 2003 3 21 2003UALA00194 120030220A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE DAMAGED DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29555UA 26647 LEFT AT STA 640 SHEARTIE BETWEEN STR 14L AND 15L DAMAGED. MAJOR REPAIR ACCOMPLISHED. SHEAR TIE CLIP REPLACED. 2L72 4F4 FRTA2NM E17NE 20030321000392003032100039WP 2003 3 21 CALA0300119 120030319A5313 LONGERON DOUG DC9 DC982 3022082WP STA 1410 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714840 49580 INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT STA 1410. A REPAIR SECTION AND SPLICE WERE INSTALLED IAW ECRA 5311-01132. 2L72 4F A6WE 20030321000412003032100041NM 2003 3 21 CALA0300121 120030319A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED ON FORWARD AND AFT FLANGES AT STA 344, RBL 12 TO LBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-5, FIGURE 205. 2L72 4F RTA16WE 20030321000422003032100042NM 2003 3 21 CALA0300122 120030320A5330 WINDOW FRAME BOEING777 777224 1385225NM STA 710 GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2774007 29477 INSPECTION FOUND A GOUGE IN L/H PASSENGER WINDOW CUTOUT FRAME AT AFT EDGE, STA 710. REPAIRED IAW ECRA 5330-03227. 2L72 4F RTT00001SE 20030321000492003032100049NM 2003 3 21 CALA0300129 120030320A5230 DOOR FRAME BOEING777 777224 1385225NM FWD CARGO DR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2774007 29477 INSPECTION FOUND A 1" CRACK IN FORWARD CARGO DOOR FRAME UPPER EDGE APPROXIMATELY 21 INCHES FROM FORWARD EDGE. IN ADDITION, THE AREA WAS SCRATCHED AND GOUGED. REPAIRED IAW ECRA 5230-01718. 2L72 4F RTT00001SE 20030321000582003032100058EA 2003 3 21 COMA0360155 120030316A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH S AFFECT SYSTEMS APAPPROACH 1 SO01781CA9605 7312 FLIGHT 5662 GEAR DISAGREE WARNING, "NLG" DID NOT EXTEND.REPALCED THE "MLG" PRIORITY VALVE. 2L72 4F RTA21EA 20030321000712003032100071NM 2003 3 21 2003UALA00211 120030225A3350 BATTERY PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29193UA 26890 PATH LIGHTING ON RIGHT SIDE IN FIRST CLASS WAS FLASHING OFF AND ON. REPLACED BATTERY PACK. 2L74 4F4 FRTA20WE E24NE 20030321000762003032100076NM 2003 3 21 2003UALA00217 120030222A57541114W412014 SLAT BOEING777 777222 1385219NM NR 13 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 TRAILING EDGE WEDGE, SLAT NR 13 DELAMINATED. BULB SEAL FOAM FILLER SECTION MISSING. REMOVED, REPAIRED AND REINSTALLED WEDGE AND REPLACED SECTION OF SEAL CORE. 2L72 4F RTT0001SE 20030321000822003032100082NM 2003 3 21 2003UALA00225 120030217A5313 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29555UA 26647 CABIN CREASE BEAM DENTED AT STA 638, STR 17L, WL 207. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASEBEAM OUTER CHORD FROM STA 630 TO 662 WITH SPLICE AT STA 630. 2L72 4F4 FRTA2NM E17NE 20030321000852003032100085NM 2003 3 21 2003UALA00228 120030228A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29956UA 26704 LEFT STATION 188 FRAME CRACKED IN RAD ON AFT SIDE JUST ABOVE FLOOR LINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR AND EXTERNAL SKIN DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030321000882003032100088NM 2003 3 21 2003UALA00231 120030307A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29953UA 26700 STATION 188 FRAME CRACKED RT SIDE WL 207. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED. SIDE DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030321000902003032100090EU 2003 3 21 2003UALA00233 120030303A2913887673 PUMP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYDRAULIC SYS LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29426UA 510 ECAM WARNING, GREEN HYDRAULIC LOW PRESSURE. NR 1 ENGINE HYDRAULIC PUMP LEAKING. REPLACED PUMP. 2L72 4F4 FRTA28NM E40NE 20030321000912003032100091NM 2003 3 21 2003UALA00234 120030302A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29514UA 24839 EEL STRIP INOPERATIVE, IN FRONT OF AFT LAV. REPLACED EEL STRIP. 2L72 4F4 FRTA2NM E17NE 20030321001032003032100103NM 2003 3 21 2003UALA00246 120030227A5754114W41607 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLAT DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29766UA 26917 T/E WEDGE, SLAT NR 6, DELAMINATED AND IS DENTED. LOWER T/E SPAR IS CRACKED AT BOTH ROLLER RIBS. NEW CORE PANEL INSTALLED. T/E WEDGE AND SPAR REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030729001112003072900111EU 2003 7 29 2003F00484 120030515A5720 ANGLE AIRBUS320 A320233 3930329EU LT WING BROKEN A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND BROKEN ANGLE BEHIND SLAT NR 3 STOP, LEADING EDGE LEFT WING. REPAIRED ANGLE IAW SRM 51-20-00. (M) 2L72 4F RTA28NM 20030729001152003072900115WP 2003 7 29 AMTA200300866 120030701A5320 STRUCTURE LKHEED1011 10113853 5265020WP FUSELAGE DAMAGED A K NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND HOLE IN C1 PIT AT FS 595, 21 INCHES RT OF CENTER LINE, HOLE IS .75 INCH BY .75 INCH. PERFORMED INTERIM REPAIR PER ERA L10-53T-2549 REV B. 2L73 4F A23WE 20030730000162003073000016WP 2003 7 30 ABXA030277 120030610A5311995774011 FRAME DOUG DC9 DC915 3022036WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 FRAME FS 523 WAS CRACKED. REMOVED AND REPLACED FRAME FS 523 LEFT IAW DC-9 SRM. 2L72 4F A6WE 20030730000372003073000037WP 2003 7 30 ABXA030253 120030211A5200 DOOR FRAME DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CENTER LATCH HOOK MOUNT HOLE STA 207.0 HAD CRACK INDICATION. REMOVED DOOR FRAME, FABRICATED NEW FRAME SECTION AND SPLICES, AND INSTALLED IAW ABX REA D852-46041MR, DC-8 SRM 51-1-8 AND 51-1-20D. 2L74 4F 4A25 20030730000392003073000039WP 2003 7 30 ABXA030214 120030528A53115911448509 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 FRAME FS 446 WAS CORRODED LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03. 2L72 4F A6WE 20030730000662003073000066WP 2003 7 30 ABXA030252 120030211A5200 DOOR FRAME DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 UPPER LATCH HOOK MOUNT HOLE AT STA 253.0 HAD CRACK INDICATION. CUT AND REMOVED DOOR FRAME, FABRICATED SPLICES FOR FRAME REPAIR, LOCATED & DRILLED NEW FRAME SECTION AND SPLICES, INSTALLED IAW ABX REA D852-46041MR, DC-8 SRM 51-3-2, 51-1-20D, AND 51-1-21. 2L74 4F 4A25 20030730000722003073000072WP 2003 7 30 ABXA030262 120030223A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE STUB FRAME AT MAIN CARGO DOOR STA 143.5. REMOVED STUB FRAME IAW DC-9 SRM 51-1-21. RECEIVED SERVICEABLE FRAME, LOCATED AND DRILLED FASTENER HOLES IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-24. INSTALLED SERVICEABLE FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-3-0. 2L74 4F 4A25 20030731000012003073100001WP 2003 7 31 03FDEA01158 120030728A5320NCA6044 CAP DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 COMPLY WITH EA 8-5310-70981. FUSELAGE MAINFRAME STA 595 TEE CAP CRACK REPAIR L39 LEFT AND RIGHT P/N NCA6044. CLOSING ACTION ON 07/28/03 COMPLIED WITH EA 8-5310-70981. 2L73 4F A22WE 20030731000032003073100003NM 2003 7 31 03FDEA01103 120030709A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CENTER CARGO DOOR CUT OUT LOWER AFT CORNER FOUND ROLLER TRAY SUPPORT CHORD CRACK. ***** S/D COMING **** 2L73 4F RTA22WE 20030731000462003073100046NM 2003 7 31 QXEA200300873 120030721A2750 FLAP BOMBDRDHC8 DHC8401 1390041NM WING MALFUNCTIONED A QXEAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM09406QX 4048 BOI-ON FLIGHT NUMBER 2364, ON FINAL APPROACH INTO BOI AFTER FLAPS SELECTED 35 DEGREES, AIRCRAFT ROLLED HARD OVER TO RIGHT, NO CAUTION LIGHTS. RESELECTED FLAPS TO 15 DEGREES AIRCRAFT STOPPED ROLL. AFTER LANDING NR 1 STALL FAIL, NR 2 STALL FAIL, PUSHER SYSTEM FAIL LIGHT ILLUMINATED. COMPLIED WITH AIR DATA SYSTEM, NR 1 STALL SYSTEM FAIL & PUSHER SYSTEM FAIL FAULT ISOLATION. NO DEFECTS NOTED. AIRCRAFT STILL UNDER INVESTIGATION. 2H72 4T RTA13NM 20030731000692003073100069EA 2003 7 31 QXEA200300855 120030717A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09612QX 10042 MSO- ON FLIGHT 2429 FIRE SYSTEM FAULT CAUTION MESSAGE. CYCLED SHIPS POWER AND COMPLIED WITH FIRE SYSTEM TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000712003073100071EA 2003 7 31 QXEA200300859 120030717A269747388904 WIRE CNDAIRCL600 CL6002C10 1390015EA LT ENGINE DAMAGED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX3079 3079 10045 PDX- ON FLIGHT 2438 INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. MDC REPORTS LEFT ENGINE FIRE LOOP B FAILED/WIRING, OPEN CIRCUIT. REMOVED AND REPLACED FIRE DETECTION CONTROL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000772003073100077NM 2003 7 31 QXEA200300790 120030624A5520 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - PEEL SHIMS EXTRUDING AT RIGHT HAND FORWARD V-STAB TO H-STAB CONNECTION POINT. REPAIRED IAW Q400 TR 55-011 TASK 55-10-00-400-801. 2H72 4T RTA13NM 20030731000782003073100078NM 2003 7 31 QXEA200300801 120030627A5414 PANEL BOMBDRDHC8 DHC8401 1390041NM NR 2 NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - NR 2 NACELLE TOP AFT PANEL 424AT HAS A SCREW HOLE WITH NO COUNTER SINK REMAINING ON OUTBOARD SIDE AT FLAP TRACK CUTOUT. REPAIRED IAW RD 8/4-54-133, PAGE 4, PARAGRAPH 4 AND HORIZON AIR EA 6-54-258. 2H72 4T RTA13NM 20030731000792003073100079NM 2003 7 31 QXEA200300802 120030624A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - DAMAGE AT STATION X60, OUTBOARD OF STRINGER 29P ON LOWER FUSELAGE EXTERNAL SKIN. REPAIRED IAW RD 8/4-83-629. 2H72 4T RTA13NM 20030731000802003073100080NM 2003 7 31 QXEA200300789 120030626A5410 STRUT BOMBDRDHC8 DHC8401 1390041NM NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - A CIRCULAR GOUGE EXISTS IN THE INBOARD CENTER DIAGONAL STRUT. REPAIRED IAW HORIZON AIR EA 6-54-263. 2H72 4T RTA13NM 20030731000872003073100087NM 2003 7 31 QXEA200300832 120030707A5520 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - H-STAB TO V-STAB FORWARD LEFT HAND CONNECTION POINT SHIMS/SPACERS COMPLETELY EXTRUDED-MISSING. REPAIRED IAW Q400 AMM 55-10-00, TR 55-010, TASK 55-10-00-000-801 AND RD 8/4-55-094. 2H72 4T RTA13NM 20030731000962003073100096NM 2003 7 31 QXEA200300765 120030622A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - IMPACT DAMAGE AT STATION X50, OUTBOARD OF STRINGER 33P, LOWER FUSELAGE EXTERNAL SKIN. REPAIRED IAW HORIZON AIR EA 6-53-259. 2H72 4T RTA13NM 20030731000972003073100097NM 2003 7 31 QXEA200300766 120030621A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - IMPACT DAMAGE AT STATION X2.5 AND STRINGER 28P, LOWER FUSELAGE EXTERNAL SKIN. REPAIRED IAW HORIZON AIR EA 6-53-268. 2H72 4T RTA13NM 20030731001102003073100110NM 2003 7 31 QXEA200300775 120030628A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR UNLATCHED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX 4046 AFTER TAKEOFF REAR BAG DOOR WARNING LIGHT CAME ON. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FOUND REAR CARGO DOOR HANDLE NOT LATCHED. CLEANED AND LUBED HANDLE AND LATCH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT REUTNED TO SERVICE. 2H72 4T RTA13NM 20030731001232003073100123EA 2003 7 31 QXEA200300778 120030625A3610GG670950021 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA BLEED AIR SYS FAILED A QXEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 NM09606QX4063 4063 10023 BOI- ON FLIGHT 2524 "SMOKE AFT LAVATORY" EICAS WARNING OCCURRED WITH SMOKE DETECTOR ALARM ACTIVATION IN LAVATORY. WARNING DISAPPEARED FOLLOWING PULLING CIRCUIT BREAKERS AS PER CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NO.2 HOT AIR SHUTOFF VALVE. OPERATIONAL CHECKS GOOD.APU IS STILL ON MEL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731001322003073100132NM 2003 7 31 QXEA200300818 120030709A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - H-STAB TO V-STAB FORWARD RIGHT HAND CONNECTION POINT SHIMS/SPACERS IS EXTRUDED. REPAIRED IAW DHC-8-S00 T/R 55-011, TASK 55-10-00-400-801 AND RD 8/4-55-094. 2H72 4T RTA13NM 20030731001352003073100135EA 2003 7 31 QXEA200300899 120030723A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX- GOUGE FORWARD EDGE OF MAIN CABIN DOOR APERATURE 18 INCHES UP FROM BOTTOM. REPAIRED IAW HORIZON AIR EA R-53-122. 2L72 4F RTA21EA 20040311000632004031100063WP 2004 3 11 GTIA030506 120030624A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CABIN STATION 200 RBL 10 TO 44 FLOOR SUPPORT CORRODED. FABRICATED, LOCATED AND DRILLED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000012003080100001NM 2003 8 1 AMTA200300796 120030618A2612 FIRE WARNING BOEING757 75723N 1384973NM COCKPIT FALSE ACTIVATIONA AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11523AT 30232 STATUS MSG L ENGINE FIRE LP1 ON IN CRUISE, EXTINGUISHED UPON DESCENT. S/D - CONTINUALLY CHECKED ALL DETECTORS. MESSAGE IS NOT PRESENT ON EICAS. SWAPPED LOOP 1 AND LOOP 2 FIRE DETECTION CARD FILE. LOOP 1 S/N 18837 P/N 6445-01. LOOP 2 S/N 18869 P/N 6445-01. FIRE DETECTION CARD FILE IAW MM 26-10-01-4. OPS NORMAL. (M) 2L72 4F RTA2NM 20030801000132003080100013WP 2003 8 1 GTIA030521 120030619A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CABIN FLOOR SUPPORT RBL 6 STATION 168.75 TO 205 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED SUPPORT. (M) 2L72 4F A6WE 20030801000192003080100019WP 2003 8 1 GTIA030546 120030618A521099155656297 STOP FITTING DOUG DC9 DC982 3022082WP AFT DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND AFT VAULT DOOR LOWER STOPS CORRODED. REMOFED TWO EACH DOOR STOPS. INSTALLED NEW STOPS. (M) 2L72 4F A6WE 20030801000452003080100045WP 2003 8 1 GTIA030545 120030613A5230S2923978516 STOP FITTING DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND MID PIT 8 EACH DOOR STOPPER CORRODED AS MARK. REMOVED AND REPLACED 8 EACH MID PIT DOOR STOPPERS. (M) 2L72 4F A6WE 20030801000472003080100047WP 2003 8 1 GTIA030553 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 16 INCHES TO 25 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000602003080100060NM 2003 8 1 2003F00510 120030619A33500105601003 COVER DOUG MD88 MD88 3023688NM CABIN LOOSE A A4JAK NONE O OTHER ININSP/MAINT 1 SO3511FQ 49759 FLOOR PATH LIGHTING LOOSE. REMOVED AND REPLACED SECTIONS OF FLOOR PATH LIGHTING COVERS THAT WOULD NOT STAY IN PLACE IAW MD-80 MM 33-53-01. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA6WE 20030801000632003080100063EU 2003 8 1 2003F00503 120030515A7110 ACOUSTIC PANEL AIRBUS320 A320233 3930329EU NR 2 ENGINE DETERIORATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 2 ENGINE AIR INTAKE ACOUSTIC PANEL WITH DETERIOATION. REPAIRED ACOUSTIC PANEL IAW SRM V2500, 54-10-00, PAGE 100, SEC11. (M) 2L72 4F RTA28NM 20030801000642003080100064EU 2003 8 1 2003F00504 120030515A5753 TRACK AIRBUS320 A320233 3930329EU T/E FLAP FAIRINGDAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND OUTBOARD FLAP RIGHT FAIRING TRACK 632CB, DAMAGED ON RIGHT SIDE STATION 3059. REPAIRED TRACK IAW SRM 51-77-12, PAGE 10, FIGURE 3. (M) 2L72 4F RTA28NM 20030729000812003072900081NM 2003 7 29 QXEA200300751 120030617A7110 COWLING BOMBDRDHC8 DHC8401 1390041NM NR 1 ENGINE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - LOWER COWL FOR NR 1 ENGINE HAS A CRACK AT THE FORWARD FLAGE FOR UPPER DECK AT THE TOP 90 DEGREE ATTACH LEG. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030326000122003032600012SO 2003 3 26 AUS20030100 120030131A3221AN717 BOLT MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL TAIL GEAR BENT W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL WHEEL FORWARD SPRING ATTACHMENT BOLT BENT. 1H71 3O3 ONC3A23 E286 5 CP920 20030326000222003032600022NM 2003 3 26 AUS20030113 120030130A32131C3976 CHECK VALVE BOEING737 737724 13844BYNM GE CFM56 CFM567B24 NE MLG LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR STRUT SERVICE CHECK VALVE LEAKING. 2L72 4F4 FRTA16WE E00055EN 20030326000452003032600045NM 2003 3 26 AUS20030196 120030105A282260989761 PUMP BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL BOOST FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 02891811 (AUS) NR 2 MAIN FUEL TANK FORWARD BOOST PUMP FAILED RESISTANCE CHECK. FOUND DURING COMPLIANCE WITH AD/B747/173. 2L74 4F4 FRTA20WE E30NE 20030326000482003032600048NE 2003 3 26 AUS20030203 220030218A7260311859701 SEAL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ENGINE LEAKING W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) RT ENGINE DRIVEN HYDRAULIC PUMP DRIVESHAFT OIL SEAL LEAKING. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030326000642003032600064EA 2003 3 26 CA030205001 120030205A5551C2FS4663A BRACKET DHAV DHC2 DHC2MK3 2800107EA PWA PT6 PT6A27 52043EA TAILWHEEL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1305213052 (CAN) DURING CHANGEOVER FROM FLOATS TO WHEELS A CRACK WAS FOUND ON THE TAIL WHEEL ATTACHMENT LUG. THE CRACK WAS ON THE LT FORWARD ATTACH POINT OF THE TAIL WHEEL. THIS BRACKET ALSO ATTACHES THE HORIZONTAL STABILIZER ON THE UPPER PICKUPS. BRACKET WAS REPLACED WITH A NEW UNIT FROM VIKING AIRCRAFT. 1H71 3T4 T A806 E4EA 20030326000682003032600068NM 2003 3 26 CA030205011 120030120A3222 STRUT BOEING737 737217 1384464NM PWA JT8 JT8D17 52049NE NLG OVERSERVICED W A UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER TAKE OFF, NOSE GEAR DID NOT STOW. OLEO DID NOT EXTEND FULLY OR MADE CONTACT WITH SNUBBERS. THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. GEAR WAS CYCLED WAS NORMAL. MAINT FIRST CHECKED NOSE OLEO SERVICING AND DISCOVERED OLEO TO BE OVERSERVICED. THIS CAUSED NITROGEN PRESSURE AND VOLUME TO BE INSUFFICIENT FOR OLEO EXTENSION. FOR THRUST REVERSER ISOLATION LIGHT TO ILLUMINATE, NLG OLEO EXTENSION HAD TO BE LESS THAN 4 INCHES. MAINT PERFORMED A COMPLETE OLEO SERVICING PER MM. A/C WAS JACKED AND OLEO EXTENSION WAS SMOOTH AND COMPLETE AND RETRACTION SYS TESTED SERVICEABLE. INVESTIGATION REVEALED THAT NLG OLEO WAS IMPROPERLY SERVICED DURING HEAVY MAINTENANCE VISIT. 2L72 4F4 F A16WE E2EA 20030326000702003032600070NM 2003 3 26 CA030207001 120030203A291082970410119 TUBE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM CHAFED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) HYDRAULIC LEAK FOUND IN NR 1 WHEEL WELL. LEAK TRACED TO NR 1 AND 2 SYSTEM PRESSURE LINE. LINE LEAKING FROM GOUGE CHAFED BETWEEN 1ST AND 2ND ELBOW FROM TOP OF LINE AT APPROX STA XN 124.00.IPC REF 29-10-00 FIG 15 ITEM 170. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030326000742003032600074CE 2003 3 26 CA030207007 120030206A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE TORQUE FAILED W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CA (CAN) AIRCRAFT TAXIED FOR TAKEOFF AND AT APPROX 45 KNOTSTHE CAPTAIN NOTICED THAT THE R/H TORQUE GAUGE WAS NOT RISING. THEY ABORTED TAKEOFF AND RETURNED TO GATE TO DEPLANE PASSENGERS. MAINTENANCE REPLACED THE R/H TORQUE GAUGE AND GROUND TESTED SYSTEM SERVICABLE. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030326000802003032600080NM 2003 3 26 2003UALA00275 120030315A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 LT CABIN FRAME STA 887 S9R IS STARTING TO CRACK AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030326000812003032600081NM 2003 3 26 2003UALA00276 120030316A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 FUSELAGE FRAME HAD CRACK OUT OF FASTENER HOLE AT STRINGER 9L (SUPPORT FOR AIR GRILL). MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR J-ANGLE. 2L72 4F4 FRTA16WE E2GL 20030326000862003032600086NM 2003 3 26 2003UALA00286 120030316A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY EXIT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29512UA 24809 RIGHT AFT EMERGENCY HATCH HANDLE LIGHT IS INOP RELAMPED. 2L72 4F4 FRTA2NM E17NE 20030326000902003032600090NM 2003 3 26 2003UALA00293 120030218A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BULKHEAD CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 STATION 178 BULKHEAD LT SIDE FRAME CRACKED ABOVE AND BELOW WL 207. MAJOR REPAIR ACCOMPLISHED. SPLICED SIDE FRAME. 2L72 4F4 FRTA16WE E2GL 20030326000922003032600092NM 2003 3 26 2003UALA00295 120030120A5511189W26005 RIB BOEING777 777222 1385219NM PWA PW4077PW4077 NE HORIZONTAL STAB CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29766UA 26917 LT O/B HORIZONTAL STABILIZER CLOSE-OUT RIB POST IS DAMAGED/CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACKED RIB POST WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20030326000962003032600096NM 2003 3 26 2003UALA00299 120030318A5320 WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 BS188 TO 198, WEB AT WL 207 RT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20030326000972003032600097NM 2003 3 26 2003UALA00301 120030319A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 STATION 985, WL 208 STRINGER 17R ON FLOOR CREASE BEAM Z ANGLE IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED Z ANGLE. 2L72 4F4 FRTA16WE E2GL 20030326000982003032600098NM 2003 3 26 2003UALA00302 120030319A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 SEAT TRACK AT STA 1077, RBL 88 HAS CORROSION MAJOR REPAIR ACCOMPLISHED. BLENDED AREA AND REPLACED WITH NEW MATERIAL. 2L72 4F4 FRTA1NM E24NE 20030416002022003041600202 2003 4 16 ABXA030129 420030401A22102588787904 COMPUTER DOUG DC8 DC863F 302198FWP YAW DAMPER DEFECTIVE A ABXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL23828AX2961 45999 RUDDER UNCOMMANDED LT INPUT AT 3,000 FT, 200 KTS, AND 23 DEGREES FLAPS. AUTOPILOT OFF, YAW DAMPER ON. COULD NOT DUPLICATE PROBLEM. REPLACED YAW DAMPER COMPUTER. OPS CHECKED GOOD IAW DC-8 MM 22-10-00. 2L74 4F 4A25 20030416002062003041600206NM 2003 4 16 SWAA030771 120030403A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030416003252003041600325EA 2003 4 16 SWIA200311691 120030101A3030 HEATER CNDAIRCL600 CL6002B19 1900309EA LT AOA PROBE MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07443SW 7638 LT AOA HEAT CAUTION MESSAGE CAME ON IN FLIGHT, WOULD NOT GO OUT. CYCLED POWER AND COULDN'T DUPLICATE PROBLEM. PROBE HEATED OK. 2L72 4F RTA21EA 20030416003322003041600332WP 2003 4 16 UPS03840033 120030102A5320 WEB DOUG DC8 DC871F 302199DWP TORQUE BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE: C2, D-PIT DOOR AFT TORQUE BOX WEB IS CRACKED AND TORN AT HOLES AT STA 1440 LONG 33R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 23. 2L74 4F RT4A25 20030416003592003041600359 2003 4 16 SWIA200311684 420030106A34606229815704 CIRCUIT CARD CNDAIRCL600 CL6002B19 1900309EA NR1 FLT COMPUTERMALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07427SW3394 3394 7497 STAB TRIM/MACH TRIM FAIL MESSAGE AT FL330, WOULD NOT RESET. REMOVED AND REPLACED FCC 4000 NR 1 CARD WITH SERVICEABLE UNIT IAW MM 22-12-14. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20030416003772003041600377NM 2003 4 16 UPS03240124 120030108A5755 HOUSING BOEING727 72722C 138400FNM SPOILER ACTUATORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, .75 INCH CRACK FOUND IN NR 11 SPOILER ACTUATOR SUPPORT FITTING LWR O/B LUG IN UPPER RADIUS. REPLACED NR 11 SPOILER ACTUATOR SUPPORT CASTING IAW DRAWING 65-17315. 2L73 4F A3WE 20030416003872003041600387NM 2003 4 16 UPS03240055 120030110A5521 SPAR BOEING727 72721C 138400MNM ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE: C, DURING REPLACEMENT OF RT O/B RIB FOR ELEVATOR STA 209.5 LWR REAR SPAR FOUND TO BE CRACKED BETWEEN TWO FASTENERS AT O/B EDGE OF SPAR. REPAIRED IAW SRM 55-10-5 FIG 1. 2L73 4F A3WE 20030416004002003041600400NM 2003 4 16 UPS03240126 120030113A5310 SUPPORT BOEING727 72722C 138400FNM TOILET CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C+SI, CORROSION ON TOILET SUPPORT BEAM BETWEEN BS 328 AND 344. INSTALLED NEW SUPPORT BEAM AT ABOVE LOCATION IAW SRM 51-30-2. 2L73 4F A3WE 20030416004102003041600410 2003 4 16 XNOA01101 420030116A3452 TRANSPONDER AIRBUS300 A300B4203 3930306EU ATC MALFUNCTIONED A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL23373PC 218 NR 2 TRANSPONDER REPORTED 7700, 0400, 1410, WITH NO REPORTING. ITEM TRANSFER TO DMI CONTROL 3055 IAW ENA MEL 34-53-02. CAT PLACARDS INSTALLED. 2L72 4F RTA35EU 20030417000662003041700066NM 2003 4 17 UPS03240108 120030115A5753 CARRIAGE BOEING727 72722C 138400FNM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C+SI, NR 3 FLAP CARRIAGE HAS CORROSION AT BASE OF SPINDLE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03 DUE TO CORROSION. 2L73 4F A3WE 20030417000702003041700070SO 2003 4 17 SWIA200311743 120030128A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO RT NACELLE FLAPSLEAKING A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM07292SW 120319 ON SHORT FINAL RECEIVED A FLAP DISAGREE MESSAGE ON THE NACELLE FLAPS AFTER SELECTING FLAPS 45 (ABOUT 125 KTS). THEN LOST RT HYD PRESSURE. REMOVED AND REPLACED LEAKING RIGHT NACELLE FLAP ACTUATOR PER EMB MM 27-50-08. GROUND OPS CHECK AND LEAK CHECK COMPLIED WITH. NO DEFECTS NOTED. 2L72 4T RTA31SO 20030417000772003041700077NM 2003 4 17 P5CA0300745 120030125A5754 SEAL BOEING747 747283B 1384867NM KRUGER FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND WHILE CHECKING FLAP TO PYLON SEAL ON BACK SIDE OF NR 16 KRUEGER FLAP, RT WING, APPROX 4 INCHES INBOARD OF OUTBOARD SEAL. CRACK RUNS FROM LWR EDGE UP 12 INCHES. NR 16 KRUEGER FLAP PANEL REMOVED AND REPLACED IAW MM 27-81-01. 2L74 4F A20WE 20030417001192003041700119EA 2003 4 17 QXEA0300235 120030204A2611 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FALSE ACTIVATIONA QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09601QX 10009 PDX-ON FLIGHT NUMBER 2534, AFTER TAKEOFF, SMOKE AFT LAVATORY WARNING MESSAGE ILLUMINATED WITH NO ASSOCIATED AURAL. WARNING EXTINGUISHED AFTER 15 SECONDS. NO EVIDENCE OF SMOKE/FUMES IN LAVATORY. INSPECTED MDC, NO MESSAGE AND NO HISTORY FOUND. PERFORMED FAULT ISOLATION TASK 26-16-00-810-802. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030417001252003041700125WP 2003 4 17 IXXA0300013O 120030206A3232 CONTROL VALVE DOUG DC8 DC873F 302199FWP MLG DOOR FAILED A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11606AL89229976 46044 AFTER TAKEOFF CREW NOTED DOORS NOT LATCHED LIGHT ILLUMINATED. CREW CYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AFTER APPROX 30 MINUTES LIGHT EXTINGUISHED. AFTER AN UNEVENTFUL LANDING IN BFI MAINTENANCE INSPECTED SYSTEM AND DETERMINED PROBLEM IS INDICATION ONLY. ALL WORK PERFORMED PER APPLICABLE MANUALS. ITEM WAS DEFERRED UNDER MEL AND AIRCRAFT RETURNED TO SERVICE. IN ORDER TO CLEAR THIS MEL ITEM MAINTENANCE REMOVED AND REPLACED THE RT MLG DOOR ACTUATOR CONTROL VALVE. AFTER NUMEROUS OPERATIONAL CHECKS IT WAS DETERMINED THIS ITEM IS CORRECTED. ALL WORK COMPLETED PER APPLICABLE MANUALS, MEL ITEM CLEARED AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20030417002012003041700201WP 2003 4 17 UPS03840167 120030129A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1210 BETWEEN L33R-34R T-BOLT LATCH BACKUP FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2 -0. LOCATED, TRIMMED AND DRILLED UP FITTING 3754930-1 AND REPAIR FITTINGS 5894282-501, 5894282-502, IAW DC8 SRM 53-2-0. INSTALLED FITTING AND REPAIR FITTING IAW DC8 SRM 53-2-0, 51-1-20D. 2L74 4F RT4A25 20030417002042003041700204WP 2003 4 17 UPS03840170 120030206A53403619434503 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, ALC STA 1490 L34R SPLICE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030418000262003041800026NM 2003 4 18 VNAA0302008 120030211A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ROW 1 FAILED A VNAAO OTHER D INFLIGHT SEPARATION TXTAXI/GRND HDL 1 GL07437JS 3055 THE CREW REPORTED THAT THE EMERGENCY TRACK LIGHTING AT SEAT 1 D AND F WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE TRACK LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030418000282003041800028NM 2003 4 18 VNAA0302007 120030210A2612 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FIRE FALSE INDICATIONA VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07434JS 3051 THE CREW RECEIVED A LAV SMOKE CAS MESSAGE, THERE WAS NO LAV FIRE. MAINTENANCE CONTROL DEFERRED THE LAV FIRE EXTINGUISH SYSTEM IN ACCORDANCE WITH MEL 26-3 C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030418000412003041800041WP 2003 4 18 MWEA030062 120030212A53205910130328 STIFFENER DOUG DC9 DC981 3022081WP BULKHEAD DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 AFT PRESSURE BULKHEAD VERTICAL STIFFENER ON AFT SIDE OF AFT PRESSURE BULKHEAD ON RIGHT SIDE IS DAMAGED AT APPROXIMATELY LONGERON 12. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED NEW ANGLE AND REPAIR SPLICE. 2L72 4F A6WE 20030730001242003073000124EU 2003 7 30 2003F00487 120030516A5532 SKIN AIRBUS320 A320233 3930329EU VERTICAL STAB ERODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE WITH EROSION STATION 4869. REPAIRED VERTICAL STABILIZER IAW SRM 55-30-00, PATE 123. (M) 2L72 4F RTA28NM 20040223001012004022300101WP 2004 2 23 MEX2003551 120031215A323239567851 ACTUATOR DOUG DC9 DC9* WP NLG DOOR FAILED W ASMFA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 SW23501AM 49188 AIRCRAFT TURNED BACK, STRONG VIBRATION IN FUSELAGE. ARRIVING IT WAS DETECTED THAT THE LT NLG DOOR WAS OPENED. THE FUSELAGE WAS VISUALLY INSPECTED, ALL CORRECT. AIRCRAFT TAKEN TO HANGAR, BOTH NLG DOOR ACTUATORS WERE REPLACED AND SYSTEM TESTED IAW MM 32-22-01, ALL CORRECT. 2L72 4F A6WE 20040224000492004022400049NM 2004 2 24 ASAA0310119 120030307A57206549539148 ANGLE BOEING737 737298C 1384490NM RT WING CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND RIGHT WING LEADING EDGE ANGLE AT WING STATION 567 CRACKED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040223000182004022300018SO 2004 2 23 FGQ2004F00000 120031219A7500 DUCT LKHEED1329 132925 5263125SO GARRTTTFE731TFE731* 01518WP BLEED AIR CRACKED B FGQRO OTHER O OTHER NRNOT REPORTED 1 SO01701JH8359 5230 FOLLOWING ENGINE REMOVAL, BLEED AIR DUCTS WERE FOUND CRACKED AT SUPPORT BRACKET WELDS, THREE SEPARATE TUBES ASSEMBLIES WERE CRACKED IN A SIMILAR MANNER. PN WERE: JQ3216-1, JPS315-2L, JPS315-2R. 2L74 4F4 F 2A1SO E6WE 20040223000512004022300051SO 2004 2 23 SVU2004F00003 120031227A2621270541 HANDLE EMB 135 EMB135LR 3260305SO COCKPIT BROKEN B SVURO OTHER O OTHER NRNOT REPORTED 1 SW19202CP 145728 HANDLE LIGHT IS INTERMITTENT. (WO 34119) 2L72 4F RTT00011AT 20040223000532004022300053NM 2004 2 23 2003UALA00985 120031226A5230 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29199UA 28717 ON ARRIVAL AT GATE, FOUND DENT IN THE CENTER LOWER EDGE OF AFT CARGO PIT DOOR. MAJOR REPAIR. DOUBLER INSTALLED. 2L74 4F4 FRTA20WE E24NE 20040223000832004022300083WP 2004 2 23 0302229921 120031231A5311 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01943N 47647 DURING (L) CHECK FOUND CRACK IN FUSELAGE FRAME AT BS 76 LBL 17. REPAIRED IAW EA 99-197446. 2L72 4F A6WE 20040223001032004022300103WP 2004 2 23 MEX2003549 120031211A2820600071 ADAPTER DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUEL PANEL LEAKING W ASMFO OTHER K FLUID LOSS NRNOT REPORTED 1 SW23505MD226 217 49149 THE DISPENSER FUEL NOZZLE WAS REMOVED INADEQUATELY AFTER THE FUEL REFILLING SERVICE, THE ADAPTER CHECK VALVE SEAL WAS REMOVED AND A LITTLE FUEL LEAKAGE APPEARED. SUCH SEAL WAS REINSTALLED AND NO LEAKAGES APPEARED AGAIN. THE FUEL FILL ADAPTER WAS REPLACED AND THE SYSTEM WAS TESTED IAW MM 28-20-01. ALL CORRECT. 2L72 4F4 F A6WE E2EA 20040225000482004022500048CE 2004 2 25 BSY2004F00000 120031024A2120 ODOR CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE COCKPIT DETECTED E BSYAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL071026V 208B0319 PCE14195 GOT A STRONG ODOR (ELECTRICAL) IN COCKPIT. HAD MAINTENANCE LOOK AT AIRCRAFT COULD NOT DUPLICATE PROBLEM. 1H71 3T3 T A37CE E4EA 20040225000492004022500049CE 2004 2 25 BSY2004F00001 120030319A33403538013243 SWITCH BEECH 58 58 1152740CE CONT O520 IO520* 17032SO HARTZLHCJ2Y BHCJ2YF2 GL LANDING LIGHT INOPERATIVE E BSYAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL0795BB TH333 299135R 02385 LT LANDING LIGHT SWITCH STUCK IN THE ON POSITION AND SMOKING. REMOVED AND REPLACED SWITCH, OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 5 CP37EA 20040225000562004022500056NM 2004 2 25 IU62004F00000 120031211A323065446924 HOUSING BOEING737 737* NM MLG MODULE CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 59034 3237 HOUSING CRACKED. DESIGN DEFECT, HIGH TIME/ CYCLES. REDESIGN FOR LONGER LIFE. (MECHANIC FXS, JOB NR 182661) 2L72 4F RTA16WE 20040223000502004022300050 2004 2 23 SVU2004F00002 420031231A3130 CONVERTER AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE AFDAU INTERMITTENT B SVURO OTHER O OTHER NRNOT REPORTED 1 SW19262AT 269 262 FDAU FAULT. (WO NR 34225) 2H72 4T4 TRTA53EU E20NE 20040223001752004022300175WP 2004 2 23 ABXA040010 120031129A5340 SKIN DOUG DC8 DC861 3021952WP SERVICE DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 R1 FORWARD SERVICE DOOR, LOWER AFT CORNER HAD A CRACK ON EXTERNAL SKIN. REPAIRED AREA BY FABRICATING REPAIR DOUBLER, FILLERS AND TRIPLERS, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 53-2-0 AND REA D853-48471MR. 2L74 4F 4A25 20040225001532004022500153NM 2004 2 25 DL767031121 120031219A5312 LAP JOINT BOEING767 767232 1385132NM PRESS BULKHEAD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27101DA 22213 DURING INSPECTION OF THE AFT P-DOME AT FS 1582 A CRACK WAS FOUND AT A FASTENER COMMON TO THE STIFFENER 5L WEB LAP JOINT. THE CRACK WAS REMOVED BY TRIMMING OUT THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088021-14AD. 2L72 4F RTA1NM 20040225001602004022500160NM 2004 2 25 DL73S031128 120031223A5330655298863 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 A DENT WAS FOUND ABOVE S19L NEAR THE LWR AFT CORNER OF THE DOOR LOCATED NEAR BS 985. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385887-14. 2L72 4F RTA16WE 20040329000042004032900004EU 2004 3 29 USAASA03138 120031217A3350321431 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19748UW 1311 DCA - THE EMERGENCY LIGHTS TEST FAILED, WITH CIDS MESSAGE 'EPSU BATT FWD L'. MAINTENANCE REPLACED THE FORWARD LEFT POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040329000152004032900015WP 2004 3 29 ASAA0380383 120030421A5347993653557 MOUNT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND GALLEY MOUNT CORRODED. REPLACED MOUNT. (M) 2L72 4F A6WE 20040329000212004032900021WP 2004 3 29 ASAA0380393 120030421A532199366463 RETAINER DOUG DC9 DC982 3022082WP FLOORBOARD CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOORBOARD CENTER STATION 886-946 RETAINER CRACKED AROUND FASTENER. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040329000222004032900022WP 2004 3 29 ASAA0380385 120030421A5320593607111 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND MID CARGO AREA INTERCOSTAL BETWEEN STRINGER L30 AND L29 IS CORRODED. REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F A6WE 20040329000312004032900031NM 2004 3 29 ASAA0340315 120030725A53201509100505 FLOOR SUPPORT BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND UPPER FUSELAGE FLOOR SUPPORT TEE ANGLE CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040329000322004032900032NM 2004 3 29 USAASB03221 120031224A3350210310005 FUSE BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19560AU 23514 DCA- MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHTS ON SEAT ROWS 6, 7, 8, 9 AND 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE IN POWER SUPPLY ABOVE SEAT ROW 10 CEILING. OPERAITONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040329000342004032900034WP 2004 3 29 ASAA0380386 120030421A5347993653473 TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FALSE TRACK CORRODED FROM STATION 160-200. REPLACED FALSE TRACK PER SRM. (M) 2L72 4F A6WE 20030714001332003071400133 2003 7 14 C1HA200394011 420030629A2565 SLIDE BOEING727 727290 138408WNM PAX DOOR DISLODGED A C1HAO OTHER O OTHER NRNOT REPORTED 1 GL15294AS 22146 SLIDE FELL OUT OF R-1 DOOR. 2L73 4F A3WE 20030714001362003071400136NM 2003 7 14 DHL2003751010 120030703A2510 SEAT BELT BOEING727 727264 138408MNM COCKPIT BROKEN A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01751DH 22982 SECOND OBSERVER'S SEAT, THE SEAT BELT STOP BROKEN. REMOVED AND REPLACED SECOND OBSERVER'S SEAT BACK BELT ASSEMBLY IAW B-MM 25-10-71, OPS GOOD. 2L73 4F A3WE 20030714001372003071400137 2003 7 14 DL757030493 420030527A344020414440401 ANTENNA BOEING757 757232 1384965NM WX RADAR SYS FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27604DL 22811 WX RADAR FAIL DISPLAYED ON HSI. WX RADAR TEST DISPLAYS ANT FAIL ON HSI AND ON WX RADAR INDICATOR. DIVERTED TO MCO. REPLACED RADAR ANTENNA AND TRANCEIVER PER MM, OPN TEST NORMAL. 2L72 4F RTA2NM 20030714001412003071400141 2003 7 14 ALGA087895 420030701A830023071895 GEAR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0331211154 CAG95804 760225 CAE890734S FOUND SPALLING ON FWD. GEAR TEETH. REMOVED AND REPLACED WITH NEW PART. 1G72 3U3 U H1NE E1GL 20030418000542003041800054WP 2003 4 18 UPS03840192 120030203A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, RADIOGRAPHIC (X-RAY) INSPECTION DETECTED AN INTERNAL DOUBLER REPAIR BETWEEN THE OUTER SKIN AND INTERNAL DOUBLER OF THE L-2 DOOR UPPER CORNER,THE SKIN HAS A CUTOUT APPROX 1.75 X .90. INTERNAL DOUBLER REPAIR IS CONDITION II, AT STA 1660 LONG 10L. REMOVED PREVIOUS REPAIR DOUBLER, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 18. 2L74 4F RT4A25 20030418000762003041800076NM 2003 4 18 QXEA0300286 120030204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - NR 2 VHF ANTENNA MOUNT AREA INTERNAL RIGHT HAND FORWARD SET OF BRACKETS, FORWARD BRACKET IS CRACKED AT STRINGER 325 AND X80. REPAIRED IAW HORIZON AIR EO/EA 6-53-162A. 2H72 4T RTA13NM 20030418000822003041800082NM 2003 4 18 ZW0A0302403 120030219A3350 BATTERY BOEING757 7572Q8 1384972NM EMERGENCY LIGHT DISCHARGED A ZW0AO OTHER O OTHER CRCRUISE 1 CE13719TW 28487 DURING CRUISE EMERGENCY EXIT LIGHTS AND AISLE STRIP LIGHTS COME ON INTERMITTANTLY WITH COCKPIT EMERGENCY LIGHT SW IN BOTH ARMED AND OFF POSITIONS DUE TO LOW BATTERY. REPLACED BATTERY, OPS CHECKED NORMAL. CHECK-C 7/7/02. 2L72 4F RTA2NM 20030418000832003041800083EA 2003 4 18 QXEA0300215 120030202A2612 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09601QX 10009 PDX- FIRE SYSTEM FAULT STATUS MESSAGE. CLEANED AND INSPECTED AFT COWL FIRE LOOP CONNECTORS. OHMED OUT SAME LOOPS WITH NO DEFECTS NOTED. FIRE SYSTEM TEST COMPLIED WITH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030418000842003041800084EA 2003 4 18 QXEA0300255 120030212A2120 SENSOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09601QX 10009 PDX ON FLIGHT 2494-SUPP-OILY ODOR IN CABIN. COMPLIED WITH VISUAL INSPECTION OF RIGHT HAND ACM AND DUCTING. REMOVED RT PACK DISCHARGE SENSOR AND SAMPLED WITH PACK ON. NO ODOR. REINSTALLED SENSOR. APU BLEED AIR DUCT CLEAN. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030418000852003041800085NE 2003 4 18 MALA030155 220030213A7230 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT STALLED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL15427XJ 340B427 GEE785769 DURING TAKEOFF OF FLIGHT 2781, RT ENGINE COMPRESSION STALLS AT V1 ON TAKEOFF ROTATION. INFLIGHT SHUTDOWN ENGINE. AIR RETURN TO YQT. MAINTENANCE PERFOMRED COLD AND HOT SECTION BOROSCOPE, NO DAMAGE FOUND, LEAK CHECK OF A AXIS GOOD. PERFORMED GPA RUNS FOUND TAKEOFF MAGIN TO BE AT 22,9, DUE TO FDR DOWNLOAD INFO ENGINE REQUIRES CHANGE. FOUND AC TO BE SAFE FOR FERRY FLIGHT FROM YQT-MSP REDUCED PWC TAKEOFF AND ANTI-ICE ON. REPLACED RT ENGINE P/N CT7-9B IAW JOB CARD 7100-301 SN/ON GE-7785670, SN/OFF GE-E785769 REF JOB CARD FOR DETAILS AND OPS CHECK. REPLACED ULB P/N DK120, SN/ON DK5603, SN/OFF DL8379 FDR ULB OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20030418000952003041800095WP 2003 4 18 UPS03840197 120030206A53133646937501 LONGERON DOUG DC8 DC873F 302199FWP L35R STA 1377 DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, AFT PIT LONG 35 RT DENTED STA 1377. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20030418000972003041800097WP 2003 4 18 UPS03840199 120030201A532056449722502U FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, NR 4 ALT TANK STR 59 END FITTING CRACKED STA XW 428 INSIDE PNL 505B. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030418001052003041800105NM 2003 4 18 F3LA200300062 120030214A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP AT STA 1006 CORRODED IN VARIOUS AREAS FROM CENTERLINE EXTENDING TO LEFT SIDE. REPAIRED PER SRM 53-10-9, FIG 7. 2L72 4U RTA16WE 20030418001302003041800130EA 2003 4 18 SWIA200311786 120030214A274270623 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07440SW3211 3211 7589 STAB TRIM CH 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED STAB TRIM ACTUATOR IAW MM 27-42-01. REMOVED AND REPLACED STAB TRIM MCU IAW MM 27-42-05. OPS CHECK GOOD. STAB TRIM ACTUATOR P/N: 8396-3, S/N OFF: 816. 2L72 4F RTA21EA 20030416003552003041600355SO 2003 4 16 SWIA200311692 120030105A5411 FRAME EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07292UX 120292 FOUND CRACKS IN FRAME NR 1 ON RIGHT NACELLE. FOUND DURING ENGINE CHANGE. COMPLIED WITH S/B 120-54-0036, INSTALLED NEW FRAME NR 1. 2L72 4T RTA31SO 20030416003992003041600399NM 2003 4 16 P5CA0300722 120030112A541565B913141 FITTING BOEING747 7472U3B 1384846NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 SIX CRACKS TOTAL FOUND NR 4 REAR ENG MOUNT BATHTUB FITTING: I/B FASTENER HOLE HAS 3 CRACKS - (1) .125 INCH, (1) .1875 INCH & (1) .75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1) .125 INCH, (1) .5 INCH & (1) .75 INCH RADIALLY. CRACKED BATHTUB FITTING REPLACED AS PER SB 747-54-2113-R2. 2L74 4F RTA20WE 20030417000182003041700018EA 2003 4 17 SWIA200311725 120030118A2761270007 PCU CNDAIRCL600 CL6002B19 1900309EA RIGHT SPOILER FAILED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07499SW4529 4529 7398 RIGHT OUTBOARD SPOILER PCU FAILED DURING TAXI OUT. REMOVED AND REPLACED RIGHT O/B PCU. OPS CHECK GOOD IAW 27-60-01. 2L72 4F RTA21EA 20030417000552003041700055EU 2003 4 17 MALA030132 120030120A3530716955 FITTING SAAB SF340 340B 7860101EU OXYGEN LINE DAMAGED A MALAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 GL15438XJ 340B438 AT 17,000 FT OXYGEN CWP CAME ON 02 GAUGE READ 800 PSI, DESCENT WAS INITIATED INTO MEM, AND 02 LEVEL CONTINUED TO DROP. MAINTENANCE REMOVED AND REPLACED TEE FITTING P/N 716955, AND CAPILLARY LINES P/N 803197-12 AND P/N 803197-47, LEAK AND OPS CHECK GOOD. A/C OK FOR CONTINUED SERVICE IAW SF3 AMM 35-11-00. 2L72 4T RTA52EU 20030417000792003041700079NM 2003 4 17 P5CA0300743 120030127A5522 PANEL BOEING747 747283B 1384867NM ELEVATOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 DELAMINATION FOUND LT ELEVATOR 334ML HONEYCOMB PANEL, INBOARD SURFACE. REPAIRED BY BONDING FIBERGLASS PLIES PER SRM 51-40-09. 2L74 4F A20WE 20030417001122003041700112EU 2003 4 17 MALA030143 120030123A5330 SKIN BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 DURING C-CHECK IN CVG, MAINTENANCE FOUND SMALL DENT, LOWER FUSELAGE 2.50 INCHES FORWARD OF FRAME 15, BOTTOM CENTER OF FUSELAGE. MAINTENANCE REPAIRED DAMAGE IAW EOA53104 AND SRM 53-10-12 201. A/C RELEASE DATE 1/30/03. 2H74 4F RTA49EU 20030417001382003041700138WP 2003 4 17 ZW0A0301803 120030205A3350 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139620D 53591 THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 6 TO 15, ROWS 20 THRU 23, ROWS 26 THRU 30, AND MOST AFT POSITION IN TAIL CONE. REPLACED LAMPS PN 7732 FOR ROW 6 TO 15, ROW 20 TO 23, AND ROW 26 THRU 30. REPLACED BATTERIES IN POWER SUPPLY FOR TAIL CONE EMERGENCY LIGHT, PN 408822-101. CHECK-C 10-19-02 STL. 2L72 4F RTA6WE 20030417001412003041700141NM 2003 4 17 ZW0A0301806 120030207A3350 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139420D 49824 THE OVERHEAD EMERGENCY LIGHTS WERE INOEPRATIVE FROM ROW 18 TO 22, EGRESS LIGHT AT ROW 20, AND EGRESS LIGHTS ROW 27 TO AFT CABIN. RESEATED BATTERY PACKS FOR ROW 18 TO 22, REPLACED LAMP PN 7732 FOR ROW 20 EGRESS LIGHT, AND RESEATED PLUG AT ROW 26 FOR AFT CABIN EGRESS LIGHTS. CHECK-C 11-06-02 STL. 2L72 4F RT 20030418000052003041800005EU 2003 4 18 RAIA00302033 120030202A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03574HK 41093 MX-STL- EMERGENCY PATH LIGHTS OUT ROWS 1-3. RE-SECURED CONNECTOR AT FLOOR PATH LIGHTS, OPS CHECK OK. 2L72 4T RTA41NM 20030418000142003041800014WP 2003 4 18 UPS03840172 120030213A3260 CONNECTOR DOUG DC8 DC873F 302199FWP DOWNLOCK SWITCH DAMAGED A IPXAL ABORTED APPROACH N FALSE WARNING LDLANDING 1 SO01807UP 46007 RT MLG DOWNLOCK INDICATION INTERMITTENT. EMERGENCY DECLARED. TWO MINUTES RT MLG IND CAME ON ON ITS OWN. LANDED W/O INCIDENT, GEAR PINNED. REMOVED AND REPLACED RT MAIN LANDING GEAR DOWNLOCK SWITCH CONNECTOR PER MM CHAPTER 20, STANDARD PRACTICES CHECKS NORMAL. 2L74 4F RT4A25 20030418000352003041800035NM 2003 4 18 XNOA01105 120030219A2722 WARNING LIGHT BOEING727 727227 1384078NM RUDDER LOAD ILLUMINATED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL2376753 21249 AFTER PUSHBACK, ENGINES STARTED. FOUND LOWER RUDDER LOAD LIMITED LIGHT ON. TRANSFERRED TO DMI 3159 PER ENA MEL 27-22. CAT C PLACARDS INSTALLED. SP 27-22 APPLY. 2L73 4F A3WE 20030418000362003041800036WP 2003 4 18 MWEA030080 120030217A53204912515523 CLIP DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LONGERON 12 RIGHT CLIP AFT OF STATION 1338 IS DAMAGED. LOCATED AND DRILLED NEW SHOVEL CLIP. 2L72 4F A6WE 20030418001002003041800100WP 2003 4 18 UPS03840203 120030203A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, TRIPLER/DOUBLER REPAIR DOES NOT CONFORM TO THE SRM, AT L-2 DOOR LOWER FORWARD CORNER AT STA 1620 AT LONG 20L. REMOVED PREVIOUS REPAIR, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC8-5310-7975-B. 2L74 4F RT4A25 20030418001012003041800101WP 2003 4 18 UPS03840204 120030203A5320 FITTING DOUG DC8 DC873F 302199FWP CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C-1, LONGERON SPLICE FITTING CRACKED AT LONGERON 12L BETWEEN STA 300-320. REMOVED, FABRICATED AND REPLACED LONGERON SPLICE FITTING IAW SAA SK 811-748, UPS ENGINEERING FILE NUMBER DC8-53-20283, DWG 4613574 SRM 51-1-20D. 2L74 4F RT4A25 20030418001232003041800123EA 2003 4 18 SWIA200311779 120030208A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07590SW 7077 FIRST OFFICER'S STAB TRIM SWITCH IS INOP. REPLACED FIRST OFFICER'S TRIM SWITCH IAW CRJ MM 27-41-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20030418001242003041800124EA 2003 4 18 SWIA200311780 120030209A30307858062 SENSOR CNDAIRCL600 CL6002B19 1900309EA AIR DATA MALFUNCTIONED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07441SW2983 2983 7602 AFTER TAKEOFF, THE FOLLOWING CAUTION MESSAGES WERE DISPLAYED: PITOT BASE HEAT, L AOA HEAT, L STATIC HEAT, AND L PITOT HEAT. RETURNED TO DFW. REMOVED NR 1 ADSHC AND REPLACED IT WITH A SERVICEABLE ONE IAW CL600 30-31-15. OPS CHECK GOOD. 2L72 4F RTA21EA 20030418001312003041800131EA 2003 4 18 SWIA200311787 120030214A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07917SW 7641 FORWARD CEILING EMERGENCY LIGHT INOP. RELAMPED FORWARD EMERGENCY LIGHT BULB. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030418001332003041800133EA 2003 4 18 SWIA200311789 120030214A273170608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07403SW 7028 BOTH STAB TRIM & MACH TRIM DISCONNECT IN FLIGHT, HARD TO RESET. ON LANDING, BOTH STAB AND MACH TRIM DISCONNECTED AGAIN. REMOVED AND REPLACED HSTCU IAW MM 27-41-01. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030418001432003041800143GL 2003 4 18 P5CA0300770 120030224A5753 STRUCTURE BOEING747 747300 GL LT WING TE FLAP DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP2324837 24837 THREE DENTS FOUND 5 INCHES LONG X .0312 INCH DEEP IN LEADING EDGE VARIABLE CONTOUR FLAP NR 7 LT WING - ALLOWABLE DAMAGE A/Y 62.5 THEREFORE THIS MINOR DENT ACCEPTABLE IAW SRM REF 57-50-01. 2) DENT 10 INCHES LONG X .5 INCH DEEP IN BULL NOSE LOCATION VARIABLE CONTOUR FLAP LT WING - REPAIRED CARRIED OUT IAW 57-50-03 & 51-40-00 SECT 2, 3. 3) DENT 7 INCHES X .5 INCH DEEP LEADING EDGE OF KRUEGER FLAP, NR 13 - DENT DRESSED TO CONTOUR AND AREA PROTECTED IAW SRM 57-50-03 & 51-40-01. 2L74 4F RTA20WE 20030418001482003041800148 2003 4 18 MALA030166 420030222A34506226523213 TRANSPONDER SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAK NONE J WARNING INDICATION CRCRUISE 1 GL15441XJ 340B441 DURING FLIGHT 3029, ATC REPORTED BOTH TRANSPONDERS INOPERATIVE ON THREE SEPARATE OCCASIONS, ON FLIGHT FROM GRF-MSP. TRANSPONDER LOCKED UP WITH ACT LIGHT ILLUMINATED. TCAS ALSO SWITCHED TO OFF MODE. ATC REPORTED LOST MODE C AND REGULAR RETURN ONLY WAY TO CLEAR WAS TO RUN TRANSPONDER TEST SWITCHING FROM 1 TO 2, NO EFFECT. MAINTENANCE REMOVED AND REPLACED TRANSPONDER CTL P/N 622-6523-213 SN/OFF 137D SN/ON 12761, REPLACED NR 1 TRANSPONDER P/N 622-9210-004, SN/OFF 5904, SN/ON 6145, TRANSPONDER SYSTEM OPS CHECKS GOOD IAW SF340 MM CHAP 34, FAR 43, APP E, PARA C C/W. 2L72 4T RTA52EU 20030418001522003041800152NM 2003 4 18 QXEA0300294 120030221A3220 BOLT BOMBDRDHC8 DHC8401 1390041NM ZONE 700 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 BOLT CONNECTING INBOARD AND OUTBOARD TOGGLE LINKS TOGETHER IS CHAFING ON FORWARD SIDE OF NOSE LANDING GEAR MECHANISM SUPPORT STRUCTURE. REPAIRED IAW Q400 SRM 51-14-00, PAGES 221-223, SRM 51-25-32, PAGE 201 AND SRM 32-31-00-710-801. 2H72 4T RTA13NM 20030418001542003041800154NM 2003 4 18 QXEA0300303 120030225A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09361PH 516 PDX ON FLIGHT 2193- TRACK LIGHTING ON AISLE FLOOR BY ROW 1 IS COMING UP. REMOVED AND REPLACED FORWARD STRIP OF AISLE EMERGENCY LIGHT TRACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421000072003042100007WP 2003 4 21 UPS03840233 120030130A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, REMOVE STEEL DOUBLER AT UPPER FWD CORNER OF THE L-1 FWD ENTRY DOOR AND REPAIR PER SRM 53-2-0 FIG 15 AT STA 25 LONG 10L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 15. 2L74 4F RT4A25 20030421000182003042100018EA 2003 4 21 QXEA0300299 120030223A352080300013 CONTROL PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09603QX208 10011 PDX - FLIGHT 2493 - SUPP- AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE PASSENGER OXYGEN MASKS DROPPED. OHMED JB10 TO GROUND, OPEN. OHMED AND MEGGERED FROM CPCP TO GROUND, NO SHORT. MEGGED JB10 CP1 PIN 410 TO GROUND, NO SHORT. CHECKED OXYGEN DEPLOY SWITCH WITH OHMETER FROM JB10CP1 PIN 69 TO JB3 PIN A7 FOR INTERMITTENT AND NORMAL OPERATION CHECK GOOD. REMOVED AND REPLACED CONTROL PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040225001722004022500172NM 2004 2 25 DL757031140 120031227A335020131A BATTERY PACK BOEING757 757232 1384965NM EMERGNECY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27604DL 22811 FOUND ON LAYOVER, F/C RIGHT UPPER EMERGENCY LIGHTS AND R1 EXIT LIGHT INOP. REPLACED POWER SUPPLY. 2L72 4F RTA2NM 20040225001232004022500123CE 2004 2 25 M2M2004F00000 120031208A30405419204100 CLAMP LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP WINDSHIELD DIFF LOOSE B M2MRO OTHER O OTHER NRNOT REPORTED 1 GL03 1780 125 A LOOSE CLAMP THAT SECURES HOT AIR LINE TO THE WINDSHIELD DIFFUSER DUCT WAS LOOSE WHICH ALLOWED HOT BLEED AIR BETWEEN THE DUCT AND THE WINDSHIELD. SEVERLY DAMAGING THE WINDSHIELD. 2L72 4F4 F A10CE E6WE 20040225001812004022500181NM 2004 2 25 DL733031150 120031231A27511817389 TRANSMITTER BOEING737 7373B7 1384580NM TE FLAP IND FAILED A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO27947WP 23376 FLAP INDICATORS SPLIT EN ROUTE, LT NEEDLE WENT OFF SCALE. DID A FLAP UP LANDING. REMOVED AND REPLACED FLAP POSITION TRANSMITTER PER M/M. TRANSMITTER (P/N 275701135) (S/N OFF 0497) (S/N ON 4076). 2L72 4F RTA16WE 20040225001822004022500182NM 2004 2 25 DLM90031151 120031231A4900 APU DOUG MD90 MD9030 3023690NM APU BAY FAILED A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO27912DN8524 53392 P1016 APU ELECTRONICS FAILED 45 MIN AFTER T/O. REPLACED APU AND DOOR ASSY. 2L72 4F RTA6WE 20040226000072004022600007WP 2004 2 26 ASAA0380376 120030421A533059360163 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FUSELAGE DENTED AND GOUGED AT FS 1190. INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F A6WE 20040226000202004022600020NM 2004 2 26 ASAA0310395 120030505A335086210144 BATTERY PACK BOEING737 737298C 1384490NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING INSPECTION, FOUND EMERGENCY EXIT LIGHT ON THE BULKHEAD INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040224000552004022400055WP 2004 2 24 ASAA0380262 120030313A33501001101 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS6536820169 53021 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040225000922004022500092NE 2004 2 25 HEEA092087 120031201A2497A1077B RELAY SKRSKYS76 S76A 8143006NE ALLSN 250C 250C* GL NR 2 GENERATOR FAILED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW031546K 760082 NR 2 GENERATOR FAILED IN FLIGHT. (DC CONTROL P/N 51530-006B, S/N 10799B) MAINTENANCE REPLACED NR 2 GENERATOR CONTROL RELAY AND ALSO NR 1 GENERATOR DC CONTROL UNIT. 1G72 3U3 U H1NE E4CE 20040225001562004022500156NM 2004 2 25 DL767031124 120031219A5312 PANEL BOEING767 767232 1385132NM PRESS BULKHEAD GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27101DA 22213 THE GORE PANEL ON THE AFT P-DOME WAS FOUND WITH A GOUGE NEAR STIFFENER 11R. THE GOUGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 087997-14AD. 2L72 4F RTA1NM 20040226000192004022600019WP 2004 2 26 ASAA0380426 120030502A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT NEAR ROW 1. REPLACED TRACK COVERS AND RESECURED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040226000322004022600032NM 2004 2 26 ASAA0310684 120031223A335086210144 BATTERY BOEING737 737290C 138448VNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT THE SMOKE BARRIER INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M) 2L72 4F A16WE 20040225001092004022500109CE 2004 2 25 AKG2004F00001 120031224A561010138402520 WINDSHIELD BEECH 200 B200 1152922CE PWA PT6 PT6A41 52043EA COCKPIT BROKEN B AKGRO OTHER O OTHER NRNOT REPORTED 1 CE05888ZX5299 BB1140 COPILOTS WINDSHIELD INSIDE GLASS SHATTERED IN FLIGHT AIRCRAFT AND WINDSHIELD. 1L72 4T4 T A24CE E4EA 20040226000102004022600010WP 2004 2 26 ASAA0380416 120030429A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS REMAIN ON IN AFT AND TAIL AREA WITH SWITCH OFF. REPLACED ASSOCIATED POWER SUPPLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040227000462004022700046NM 2004 2 27 ASAA0340352 120031208A5310654580722 DOOR FRAME BOEING737 7374Q8 138447QNM R1 DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01756AS 25097 GYR - DURING SI CHECK, FOUND CRACK AT R1 DOOR FRAME AT STATION 291.5. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040227000482004022700048NM 2004 2 27 ASAA0340353 120031208A531565C3394311 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01756AS 25097 GYR - DURING SI CHECK, FOUND CORROSION ON NUTPLATE HOLE ON UPPER T-CAP STATION 344 FROM LBL 20 TO 50. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20030418000582003041800058NM 2003 4 18 QXEA0300265 120030206A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - Y722 Y9.50L SEAT TRACK IS GOUGED. REPAIRED IAW HORIZON AIR EA 6-53-193. 2H72 4T RTA13NM 20030418000632003041800063NM 2003 4 18 QXEA0300270 120030202A5410 CHANNEL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - CRACKED, BOTTOM OF VERTICAL U-CHANNEL AT STATION XN94.330 ON LEFT HAND LOWER COWL. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030418000662003041800066NM 2003 4 18 QXEA0300273 120030203A5413 STRINGER BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - NR 1 NACELLE, CRACK IN OUTBOARD STRINGER OF NACELLE UPPER DECK AT STATION X534. REPAIRED IAW DHC-8 Q400 SRM 51-25-10, PAGES 201-205 AND SRM 51-25-15, PAGES 201-207. 2H72 4T RTA13NM 20030418000682003041800068NM 2003 4 18 QXEA0300278 120030206A5320 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - FORWARD SUPPORT ANGLE UNDER PANEL 262FT HAS CHAFE DAMAGE ON TOP SURFACE. REPAIRED IAW HORIZON AIR EA 6-57-118. 2H72 4T RTA13NM 20030418000792003041800079NM 2003 4 18 PCAA0302044 120030219A3230 SPRING DHAV DHC8 DHC8102 2809003NM MLG WEAK A PCAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA13842EX 341 ROC-LGA - FLIGHT 3905 CREW REPORTED THAT AFTER LANDING GEAR WAS SELECTED DOWN, GEAR HORN SOUNDED, AND NOSE GEAR INDICATED UNSAFE. ALTERNATE EXTENSION INDICATOR SHOWED UNSAFE NOSE GEAR. ALTERNATE EXTENSION PROCEDURE USED, AND NOSE GEAR INDICATED DOWN AND LOCKED. MAINTENANCE FOUND NOSE LOCK SPRINGS TO BE WEAK, BUT STILL USABLE. AIRCRAFT IS CURRENTLY UNDER A STRUCTURAL REPAIR. 2H72 4T RTA13NM 20030418000872003041800087EU 2003 4 18 MALA030163 120030219A7500216118216 BLEED BAND BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 ENGINE BROKEN A MALAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 GL15516XJ E2334 DURING FLIGHT 3477, NR 3 ENGINE WENT TO OVERTEMP. NR 3 ENGINE EXCEEDS NORMAL EGT AT HIGH POWER SETTINGS, ENGINE DISPLAY PANEL NOTED 655 DEGREES FOR 21 SECONDS. MAINTENANCE FOUND NR 3 ENGINE COMPRESSOR BLEED BAND BROKEN. REPLACED NR 3 ENGINE BLEED BAND P/N 2-161-182-16, REF ENGINE MANUAL CHAP 72-00-34. SECURITY CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20030418000932003041800093NM 2003 4 18 UPS03240209 120030219A3350 BATTERY BOEING727 727180C 138406GNM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01920UP 19873 INSPECTION TYPE: C, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES AND OPS CHECKS GOOD IAW M/M 33-50-01. 2L73 4F A3WE 20030418001062003041800106NM 2003 4 18 F3LA200300063 120030217A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAEG CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP CORRODED AT STA 290, RBL 15. FABRICATED AND INSTALLED REPLACEMENT CAP STRIP PER SRM 53-10-2 AND 53-10-9. 2L72 4U RTA16WE 20030418001182003041800118EU 2003 4 18 XNOA01106 120030221A7797 CONNECTOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 PYLON DIRTY A XN0AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL2313974 126 ON TAKEOFF NR 1 ENGINE N1 ERRATIC BETWEEN 93 PERCENT TO 124 PERCENT. CLEANED AND RESEATED CONNECTOR P1 GOOD AT NR 1 PYLON. PERFORMED ENG RUN. OPS CHECKS GOOD. NO DEFECTS NOTED IAW A300 MM 71-00-00. 2L72 4F4 FRTA35EU E23EA 20030418001252003041800125SO 2003 4 18 SWIA200311781 120030218A323412038594001 SELECTOR EMB 120 EMB120ER 3260203SO MLG FAILED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07235SW 120310 UPON GEAR RETRACTION, LEFT MAIN A & B RED LIGHTS WOULD NOT EXTINGUISH AND STAYED ON CONTINUOUSLY UNTIL GEAR PUT DOWN. GEAR EXTENDED NORMALLY. INSPECTED LEFT MLG UPLOCK A & B SENSORS, HARNESS, TARGET PLATES, AND RETRACTION/EXTENSION ACTUATOR. NO DEFECTS FOUND. PERFORMED GEAR SWING SEVERAL CYCLES. OPS CHECKED GOOD. UNABLE TO DUPLICATE DISCREPANCY. REPLACED LDG HANDLE SELECTOR FOR TROUBLESHOOTING. OPS CHECKED ON GEAR SWING. S/N OFF: 120335. 2L72 4T RTA31SO 20030418001342003041800134SO 2003 4 18 SWIA200311790 120030216A2797 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS CONTAMINATED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07214SW 120280 FLAP DISAGREEMENT ON FLAP RETRACTION ON TAKEOFF, OUTBOARD FLAPS. RETURNED TO SLC. INSPECTED OUTBOARD FLAPS CONNECTORS, FOUND GLYCOL IN LEFT OUTBOARD CONNECTOR. CLEANED LEFT OUTBOARD CONNECTOR AND RAN FLAPS 10 CYCLES. OPS CHECK GOOD. NO FAULTS AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 20030418001362003041800136SO 2003 4 18 SWIA200311792 120030207A32331959500007 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM07251YV7231 7231 120251 RIGHT MAIN GEAR WOULD NOT COMPLETELY RETRACT. RED LIGHTS (BOTH) STAYED ON. CYCLED TWICE, WOULD NOT RETRACT. RETURNED TO LAX. REPLACED RIGHT MAIN LANDING GEAR ACTUATOR WITH SERVICEABLE IAW MM 32-32-10. PERFORMED GEAR SWING IAW MM 32-30-00. OPERATIONAL CHECK GOOD. UPDATE: FAT 2/12/2003: RIGHT MAIN GEAR WOULD NOT COMPLETELY RETRACT. RETURNED TO THE FIELD. REMOVED AND REPLACED RIGHT MLG ACTUATOR WITH SERVICEABLE UNIT IAW 32-11-00 AND 32-21-00 AND 32-30-00. OPS CHECK GOOD. NO LEAKS NOTED. 2L72 4T4 TRTA31SO E20NE 20030416003662003041600366NM 2003 4 16 UPS03240117 120030107A5755 STRUCTURE BOEING727 72722C 138400FNM NR 9 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, NDT CARRIED OUT ON SPOILERS, SPOILER NR 9 FOUND TO HAVE CORE DAMAGE. REPAIR CARRIED OUT IAW SRM 51-40-5. 2L73 4F A3WE 20030417000102003041700010SO 2003 4 17 SWIA200311709 120030116A27503472001001 FCU EMB 120 EMB120ER 3260203SO LT FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07229SW7129 7129 120305 LEFT INBOARD FLAP POSITIONS ITSELF TO 45 DEGREES. ASYMMETRY SHOWN IN FLAP (OVERHEAD) WINDOW. INSTALLED SERVICEABLE FLAP CONTROL UNIT. GROUND OPS CHECK GOOD. 2L72 4T RTA31SO 20030417000152003041700015EA 2003 4 17 SWIA200311722 120030121A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07908SW 7540 STAB CH 1 INOP STATUS MESSAGE. WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STABILIZER MOTOR CONTROL UNIT AND TRIM ACTUATOR IAW CRJ MM 27-42-01, 27-42-05. PERFORMED OPS CHECK OF HORIZONTAL STAB TRIM SYSTEM IAW CRJ MM 27-40-00 AND 27-41-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20040227000552004022700055NM 2004 2 27 ASAA0370020 120031229A5247148A63757 DOOR BOEING737 737790 13844CNNM APU BAY PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01618AS 30543 OAK - DURING MAINTENANCE CHECK, FOUND APU COMPARTMENT DOOR DAMAGED ON OUTER SKIN. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040227000782004022700078EU 2004 2 27 BAQA092491 120031231A633041800876800 MOUNT UROCOPEC135 EC135P2 5620027EU GEARBOX DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03584AE48 0288 ACTUATION LIGHT IN THE Y AXIS. HARDCARD ENCLOSED. REPLACED IN SERVICABLE UNIT. 01/30/2004 1G72 3U H88EU 20040301000052004030100005NE 2004 3 1 JYD2004F00004 220031116A7230670802 COMPRESSOR WHEEL SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE ENGINE CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09164AC5978 2937 64034D 672571 2ND STAGE COMPRESSOR DISK (PN 670802, SN H63817) WAS FOUND CRACKED DURING OVERHAUL INSPECTION. COMPRESSOR (SN 672571) WAS REMOVED FROM SERVICE DUE TO REACHING ITS O/H INTERVAL, HAVING A TSO OF 2987.9 HOURS AND A TT OF 5978.0 HOURS. DURING O/H INSPECTION, FIVE CRACKS WERE DETECTED BY EDDY CURRENT INSPECTION. CRACK LOCATIONS DETECTED BY EDDY CURRENT WERE IN THE CENTER RING OF DISK EXTENDING FROM BLADE PIN HOLES AT APPROXIMATELY A 45 DEGREE ANGLE. CRACKS WERE NOT DETECTABLE BY FLUORESCENT PENETRANT INSPECTION, THUS CRACK LENGTHS WERE NOT MEASURABLE. 2G72 4U4 U H4EA E15EA 20040301000092004030100009EU 2004 3 1 KBM2004F00002 120031022A2432160601 BATTERY SNIAS 350 AS350BA 8680817EU MASTER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P497 2347 BATTERY, DEAD. REPLACE WITH SERVICEABLE BATTERY. 1G71 3U NCH9EU 20040301000112004030100011EU 2004 3 1 KBM2004F00008 120031022A6420350A33214501 PITCH LINK SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH1683 2957 P/C LINK OB BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED WITH SERVICEABLE P/C LINK. (K) 1G71 3U3 UNCH9EU E19EU 20040301000132004030100013EU 2004 3 1 KBM2004F00010 120031219A326056337078012 SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE NLG TACH INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 NOSE GEAR TACH SWITCH (INOPERATIVE). REMOVED AND REPLACED WITH SERVICEABLE UNIT. (K) 1G71 3U3 U H9EU E19EU 20040301000332004030100033CE 2004 3 1 CWQ2004F00000 120030513A2120651207212 VANE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA SCOOP CRACKED A CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05376QS 5600276 DURING ROUTINE INSP LOOKED INTO DORSAL NACA SCOOP AND SAW THE UPPER AIR VANE PART NR 651207212 WITH A 2 INCH PIECE MISSING. GAINED ACCESS THROUGH BAGGAGE AREA, REMOVED BROKEN VANE ALSO LOCATED MISSING PART DOWN STREAM PAST ACM AND FRESH AIR CHECK VALVE AND OVERHEAD BLOWER WEDGED IN DUCT WORK ON AFT BULKHEAD. NO DAMAGE WAS NOTICED ON BLOWER FAN OR CHECK VALVE. FIT AND INSTALLED NEW AIR VANE WITH RELIEF HOLE PLACED AT INTERSECTION OF V CUT. IAW 560 SRM WITH LIBERAL AMOUNTS OF EA 9309. REINSTALLED ITEMS REMOVED FOR ACCESS AND LOCATION OF MISSING PART. CLOSED UP BAGGAGE AREA. 2L72 4F4 FRTA22CE E25EA 20040301000342004030100034 2004 3 1 N382004F00000 420030626A22102586686904 COMPUTER GULSTMG1159 G1159A 3970109SO AUTOPILOT SYS INOPERATIVE E N38AO OTHER O OTHER NRNOT REPORTED 1 EA05192FG 192 AUTOPILOT SYSTEM, WHEN AUTOPILOT SELECTED TO ALTITUDE PRESET, A/C DID NOT CAPTURE SELECTED ALTITUDE. FMS HEADING IN ONE DIRECTION AC DID NOT CAPTURE HEADING AS SELECTED. ON APPROACH TO RDG, PILOT WAS UNABLE TO SELECT APP NR ON AUTOPILOT CONTROLLER. REMOVED AND REPLACED A/P PITCH COMPUTER. AC TEST FLOWN SATISFACTORY AND RETURNED TO SERVICE. 2L72 4F A12EA 20040301000442004030100044CE 2004 3 1 SDRO200308 120031205A323399101364 ACTUATOR CESSNA421 421C 2076016CE MLG INOPERATIVE E IBUAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP0784GE 421C1401 LANDING GEAR LOCKED ON ROLL OUT. AIRCRAFT WAS SHUT DOWN. ON INSPECTION, MECHANIC FOUND SWITCH ON RT GEAR ACTUATOR TO BE INOPERATIVE. REPLACED RT GEAR ACTUATOR WITH SERVICEABLE ACTUATOR. PERFORMED MAINTENANCE REQUIREMENTS. GROUND RAN AIRCRAFT AND APPROVED FOR RETURNED TO SERVICE. 1L72 3O A7CE 20040301000602004030100060 2004 3 1 CHI2765 420030915A25620010009 BATTERY NARCO BELL 206 206B 1181511SW ALLSN 250C 250C* GL ELT LEAKING B CHIRK NONE K FLUID LOSS ININSP/MAINT 1 NM09432TV 3286 ELT BATTERY, PILOT DISCOVERED THAT THE BATTERY WAS LEAKING. UPON DISASSEMBLY, IT WAS FOUND TO BE LEAKING AT THE POSITIVE WIRE (RED), WHERE IT GOES INTO THE BATTERY PACK. 1G71 3U3 U H2SW E4CE 20030825000212003082500021WP 2003 8 25 UPS03841096 120030724A551446530252 ATTACH ANGLE DOUG DC8 DC873F 302199FWP HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 RT HORIZONTAL STAB. FRONT SPAR AT STA. XFS322. RIB ATTACH ANGLE IS CRACKED REMOVED, FABRICATED AND REPLACED ATTACH ANGLE I.A.W. DWG.4653025 AND SRM. 51-1-20D. 2L74 4F RT4A25 20030825000302003082500030WP 2003 8 25 UPS03840956 120030707A2560 SMOKE BARRIER DOUG DC8 DC871F 302199DWP COCKPIT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 45914 INSPECTION TYPE:N/A 6 INCH HOLE IN SMOKE CURTAIN LOWER LEFT CORNER NEAR CREW ENTRY DOOR REQ A773119. REPAIRED DAMAGED AREA OF SMOKE CURTAIN LOWER CORNER IAW EO DC8-2550-1872-B. OK FOR SERVICE. 2L74 4F RT4A25 20030825000332003082500033WP 2003 8 25 UPS03840968 120030707A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CKS OK. 2L74 4F RT4A25 20030825000352003082500035NM 2003 8 25 UPS03M40952 120030612A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 INSPECTION TYPE:C AFT CABIN STA 1964 TO 2007 LT MOST OUTER SEAT TRACK FOUND SURFACE CORROSION AS MARKED. CORROSION REMOVED,SEAT TRACK 1964-2007LBL75.25 IAW SRM53-70-00V1R33. FOUND EXCEEDED LIMIT-ORI THK:0.08 AND REMOVED:0.029. AREA TRIMMED OUT IAW SRM53-70-01V1R33,FIG5 STA1964-2007 LT, LBL X=75.25. FILLER AND STRAP FAB AND HOLES PICKED UP IAW SRM53-70-00V1R33. INSTALLED FILLER AND STRAP IAW SRM51-31-01V.2R33. 2L73 4F4 FRTA22WE E24NE 20030825000412003082500041WP 2003 8 25 UPS03840889 120030617A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 RIGHT WING LE. LOWER SKIN IS CRACKED AT SCREWHOLE AT XFS 834 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED DOUBLER I.A.W. DC8-5720-4087-B 2L74 4F RT4A25 20030421000212003042100021EA 2003 4 21 SWIA200311799 120030218A3220 STRUT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG DISCHARGED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07441SW 7602 AFTER SELECTING GEAR UP, TWO RED EICAS MESSAGES NOSE DOOR OPEN, GEAR DISAGREE. AMBER MESSAGE STEERING INOP AND WOW INPUT. SERVICED NOSE STRUT IAW CRJ MM 12-12-32. JACKED AIRCRAFT AND PERFORMED GEAR SWING. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20030421000242003042100024SO 2003 4 21 SWIA200311802 120030217A5610 WINDOW EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07217SW 120286 RIGHT SIDE DV WINDOW CRACKED AT FORWARD BOTTOM CORNER. REMOVED AND REPLACED RIGHT SIDE DV WINDOW. 2L72 4T4 TRTA31SO E20NE 20030421000422003042100042NE 2003 4 21 UPS03640240 220030226A7297 CONNECTOR BOEING767 76734AF 1385212NM GE CF6 CF650C2B 30018NE NR 2 ENGINE DISCONNECTED A IPXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01316UP 27744 INSPECTION TYPE: ETOP, RT ENG OIL PRESS FLUCTUATES BETWEEN 12-45 PSI FOR PAST 5 HR OF FLT OIL TEMP NORMAL (100) OIL QTY STDY (16) AT NORMAL CRUISE WENT INTO RED BETWEEN 1-8 PSI. DIVERTED TO MHT. ENG IND NORMAL ON DESCENT AND APPROACH WHEN THRUST WAS IDLE, NO ENG SHUTDOWN NECESSARY. FOUND C/P OFF OIL PRESS SW. CLEANED AND RECONNECTED. RAN ENG OIL PRESS CK GOOD AS PER 767MM 79-32-00-5. 2L72 4F4 FRTA1NM E23EA 20030421000432003042100043WP 2003 4 21 UPS03840024 120030118A5320 ANGLE DOUG DC8 DC873F 302199FWP RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: A, CORROSION IN RT FWD UPPER CORNER OF RIGHT MLG WHEEL WELL. FERRY TO TCO. REMOVED LITE SURFACE CORROSION, LESS THAN .002 INCH MATERIAL, W/IN LIMITS IAW DC8 SRM 53-2-0. ALODINED IAW DC8 SRM 51-1-8, OK TO PRIME. AFTER FURTHER INSPECTION, FITTING FOUND TO BE CRACKED. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20030421000452003042100045 2003 4 21 SWIA200311806 420030219A22108220044001 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA NR 1 YAW DAMPER INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07591SW3364 3364 7079 NR 1 YAW DAMPER WILL NOT ENGAGE. FERRIED TO SLC. REMOVED AND REPLACED FLIGHT CONTROL PANEL. PERFORMED OPS CHECK OF YAW DAMPERS. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030421000472003042100047EA 2003 4 21 SWIA200311808 120030221A3020 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA 14TH STAGE DUCT FALSE INDICATIONA SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07411SW 7067 SHORTLY AFTER TAKEOFF RED L 14TH STAGE DUCT MESSAGE. MESSAGE WENT OUT WITH AFFECTED THRUST REDUCED TO IDLE. INSPECTED 14TH STAGE LT NAC DUCT AND LOOP. FOUND NO PROBLEMS. CHECKED LOOP CONNECTORS WITH NO PROBLEMS. LEAK CHECKED LT 14TH STAGE NAC DUCT, NO LEAKS. OPERATED SYSTEM. OPS CHECK GOOD. 2L72 4F RTA21EA 20030421000572003042100057 2003 4 21 MWEA030122 420030227A3418 COMPUTER DOUG DC9 DC932 3022066WP STALL WARNING MALFUNCTIONED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31207ME 47794 DURING TAXI, STALL INDICATION FAILURE LIGHT CAME ON. SWAPPED AOA SYSTEM, CHECKS GOOD. MARKED FAULTLY TRANSDUCER ON NR 1 SIDE, NOW IN NR 1 POSITION, RESET NR 2 COMPUTER VANE PIN. 2L72 4F A6WE 20030421000622003042100062 2003 4 21 SWIA200311811 420030217A34206229810016 DISPLAY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ADI MALFUNCTIONED A SWIAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 NM07453SW159 159 7743 FIRST OFFICERS MULTIFUNCTION DISPLAY FAILED IN FLIGHT. REMOVED AND REPLACED FIRST OFFICERS EFD. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030421000642003042100064SO 2003 4 21 SWIA200311813 120030221A243451539014A GCU EMB 120 EMB120ER 3260203SO RT GENERATOR INOPERATIVE A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07212SW4388 3035 120276 AFTER TAKEOFF, RIGHT GEN LOAD RESET DROPPING OFF AND COMING BACK ON WITH A SINGLE CHIME AND ELEC LIGHT ON MAP. DEF RIGHT GEN PER MEL 24-30-1. REMOVED AND REPLACED NR 2 GCU IAW 24-30-02. OPS CHECK GOOD. P/N: 51539-014A, S/N OFF: 96545, S/N ON: 5272. 2L72 4T RTA31SO 20030417001062003041700106WP 2003 4 17 IXXA0300012O 120030204A2913 O-RING DOUG DC8 DC862 3021970WP HYD PUMP LEAKING A IXXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW11728PL830151147 45918 DURING CRUISE CREW NOTED HYD QTY DROPPING ABNORMALLY. CREW COMPLETED ABNORMAL CHECKLIST AND PROCEEDED TOWARDS QPG. WHILE ON FINAL APPROACH, AFTER ADVISING QPG ATC OF ABNORMAL CHECKLIST COMPLETION. QPG ATC DENIED LANDING CLEARANCE. CREW ELECTED TO PROCEED TO ALTERNATE AIRPORT AND MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED NO INDICATION OF ANY HYD LEAK. SYSTEM OPERATIONALLY CHECKED NORMAL. JUST PRIOR TO DEPARTURE MAINTENANCE NOTED STATIC HYD LEAK AT NR 2 ENGINE DRIVEN HYD PUMP OUTPUT AREA. REPLACED O-RINGS AND SYSTEM LEAK CHECKED GOOD. ALL WORK COMPLETED PER APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20030417001732003041700173WP 2003 4 17 UPS03840163 120030130A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, STA 80 LONG 22L EXTERNAL DOUBLER HAS SEVERAL LOOSE CHERRY LOCK RIVETS. REMOVED DOUBLER AND FOUND BLIND FASTENERS UNDER DOUBLER WITH NO PITCH TO REPAIR DOUBLER HOLES, SHEAR TIE DRILLED THRU RADIUS, REMOVED DAMAGED SHEAR TIE, CUT OUT DAMAGED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED SHEAR TIE, DOUBLER, FILLER, AND FINGER DOUBLER IAW DWG 5610088 AND SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030417001932003041700193NM 2003 4 17 P5CA0300757 120030130A7160 DUCT BOEING747 747283B 1384867NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK AND DELAMINATION FOUND ON NR 1 ENG LT -C- DUCT LWR VERTICAL WEB. REPAIRED DUCT AS PER SRM 54-05-009 FIG 5. 2L74 4F A20WE 20030418000062003041800006SO 2003 4 18 RAIA00302037 120030203A3610S2D226 O-RING EMB 145 EMB145 3260210SO BLEED AIR LEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03809HK 145187 PIT- LT BLEED LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING AT LT BLEED LINE COUPLING. 2L72 4F RTT00011AT 20030418000292003041800029NM 2003 4 18 VNAA0302005 120030209A32972276000000 WIRE HARNESS DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG FAILED A VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL07328JS16325 3030 ON APPROACH, CREW LOWERED GEAR AND FAILED TO RECEIVE A GREEN DOWN & LOCKED INDICATION. CREW ABORTED LANDING. CREW MANUALLY LOWERED GEAR, CREW RECEIVED ALL GREEN LIGHTS EXCEPT RIGHT HAND MAIN GEAR. CREW DECLARED AN EMERGENCY, REQUESTED A LOW APPROACH TO SEE IF ATC COULD TELL IF RIGHT HAND MAIN GEAR WAS EXTENDED DOWN. CREW RECEIVED A GREEN DOWN INDICATION FOR RIGHT HAND MAIN GEAR. CONTINUED WITH LOW APPROACH & ATC STATED IT DID LOOK AS THOUGH RIGHT HAND GEAR WAS DOWN. PROCEEDED TO LAND, NO FURTHER INCIDENTS. AIRCRAFT WAS FERRIED TO PIT. MX INSPECTED AND FOUND CODES S12 AND S17 IN THE PSEU. REPLACED RIGHT HAND MAIN LANDING GEAR DETECTING HARNESS. OPS CHECKS WERE PERFORMED, AIRCRAFT RELEASED FOR SERVICE.2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030418000442003041800044WP 2003 4 18 MWEA030107 120030217A53125910130392 BULKHEAD DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 AFT PRESSURE BULKHEAD TEE IS DENTED AND CRACKED BEWEEN LONGERON 9 AND 12 RIGHT AFT OF AFT PRESSURE BULKHEAD STATION 1339. REMOVED AND REPLACED DAMAGED TEE SECTION. 2L72 4F A6WE 20030417001182003041700118NM 2003 4 17 QXEA0300234 120030131A5410 CHANNEL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX-RIGHT HAND LOWER COWL AFT RIGHT HAND VERTICAL U-CHANNEL IS CRACKED. REPAIRED IAW RD8/4-71-016. 2H72 4T RTA13NM 20030417001272003041700127NM 2003 4 17 UPS03240139 120030128A5320 FITTING BOEING727 72725C 138400HNM TAIL SKID BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, LT LOWER TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED LWR TERMINAL FITTING IAW SRM 51-30-02. NEW FITTING INSTALLED IAW DRAWING 65-25992. 2L73 4F A3WE 20030417001342003041700134WP 2003 4 17 UPS03840149 120030201A53403779762U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE:C1 MAIN CABIN FITTING IS CRACKED AT STA 680 FWD SIDE AT LONG 12R. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D. 2L74 4F RT4A25 20030417001362003041700136WP 2003 4 17 UPS03840151 120030131A5310 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, STA 200 FRAME FORMER IS CRACKED ON I/B END BETWEEN LONG 32L AND 33L. REMOVED CRACKED FORMER CLIP, FABRICATED AND INSTALLED FORMER REPAIR CLIP IAW SRM 53-2-0 FIG 2A. 2L74 4F RT4A25 20030417001542003041700154EA 2003 4 17 SWIA200311766 120030131A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAP MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07595SW 7292 FLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF. FLAPS WOULD NOT GO UP OR DOWN. RETURNED TO DFW. INSPECTED CANNON PLUGS AT SELECTOR LEVER. INSPECTED PINS AT FECU. INTERROGATED FECU, NO FAULTS FOUND. RESET SYSTEM. SYSTEM OPS CHECK GOOD IAW CL-600 MM 27-51-00. OPERATED SYSTEM SEVERAL TIMES WITH NO FURTHER DEFECTS NOTED. UPDATE 2/7/03: FLAP FAIL CAUTION MESSAGE ON APPROACH. REMOVED AND REPLACED FECU IAW MM 27-51-10. OPS CHECK GOOD. S/N 369. 2L72 4F4 FRTA21EA E15NE 20030417001582003041700158NE 2003 4 17 MALA030148 220030210A75105056T88P01 VALVE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE BLEED AIR MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15119XJ 340A119 ON FLIGHT 2930 LT AIR VALVE CAME ON INFLIGHT, LIGHT WENT OUT BELOW 92 PERCENT NG. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED LT GARRET VALVE P/N 5056T88P01, SN/ON AEX10142. ALL CHECKS OF LT AIR VALVE SYSTEM ARE GOOD AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20030418000232003041800023NM 2003 4 18 VNAA0302013 120030216A3060 BRUSH BLOCK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT PROP DE-ICE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND PROP DE-ICE FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED, CLEANED, AND REPOSITIONED THE RT BRUSH BLOCK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030418000312003041800031NM 2003 4 18 VNAA0302003 120030205A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER L NO TEST NRNOT REPORTED 1 GL07437JS156092427 3055 THE CREW REPORTED THAT THE FIRST ROW OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030418000472003041800047WP 2003 4 18 UPS03840182 120030210A571037048411 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, LT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD OF XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D. 2L74 4F RT4A25 20030418000802003041800080NE 2003 4 18 ZW0A0302401 220030217A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT MAKING METAL A ZW0AO OTHER J WARNING INDICATION CRCRUISE 1 CE139307R 49663 DURING CRUISE LT ENGINE OIL FILTER CLOGGED, LIGHT ILLUMINATED. THROTTLED BACK TO IDLE REMAINDER OF FLIGHT. EMERGENCY DECLARED TO TOWER AND TO ACFT MAINT. METAL FOUND IN OIL SCREEN. REPLACED NUMBER 1 ENGINE. RUNUP AND TRIMA IAW MM, OPS NORMAL. CHECK-C 10-2-02 MCI. 2L72 4F4 FRTA6WE E9NE 20030418000942003041800094WP 2003 4 18 UPS03840196 120030128A57535751186507 FITTING DOUG DC8 DC873F 302199FWP LT WING TE FLAP CRACKED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, LEFT WING FLAP HINGE SUPPORT FITTING AT STA XF 339 7332 CRACKED AT OUTBOARD SIDE JUST FWD OF FLAP FWD SPAR. REMOVED BASE FITTING, CENTER FITTING, SLIDER PANEL, OUTBOARD TRACK, CLOSURE PANELS AND SPRING PANEL IAW DC8 SRM 51-3-0. LOC AND DRILLED BASE FITTING AND CENTER FITTING IAW DAC DWG 5751174. ALODINED AND PRIMED FITTINGS IAW DC8 SRM 51-1-8. INSTALLED BASE FITTINGS AND CENTER FITTINGS IAW DAC DWG 5751174. RE-INSTALLED PANELS AND OUTBOARD SLIDER TRACK IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030418000992003041800099WP 2003 4 18 UPS03840202 120030211A5711 SPAR DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C3 LT WING FRONT SPAR LOWER CAP XFS 7 HAS A CRACK INDICATION FOUND BY HFEC. STOP DRILLED CRACK, FABBED REPAIR ALODINED AND PRIMED INSTALLED REPAIR. 2L74 4F RT4A25 20030418001262003041800126EA 2003 4 18 SWIA200311782 120030210A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07588SW 7069 BOARDING LIGHT ON PASSENGER DOOR STAIR INOP. REPLACED THE LAMP IN THE LIGHT ASSEMBLY. OPS CHECK GOOD. 2L72 4F RTA21EA 20030418001472003041800147 2003 4 18 MALA030165 420030222A3450 WARNING LIGHT SAAB SF340 340B 7860101EU TRANSPONDER ILLUMINATED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15414XJ 340B414 EN ROUTE TO PLN ON FLIGHT 2765, ATC REPORTED NO TRANSPONDER/MODE C READOUT ON NR 1 & 2 TRANSPONDERS. AIR RETURN TO DTW. MAINTENANCE CYCLED POWER, 1 & 2 TRANSPONDERS. OPS CHECK GOOD IAW SAAB MM CH 34, ALT REPORTING SYSTEM TESTED IAW FAR 43 APPX E PARA C. 2L72 4T RTA52EU 20030418001512003041800151EU 2003 4 18 MALA030171 120030211A5754 STRUCTURE BAC 146 AVRO146RJ85A1500097EU LT WING LE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING LIGHTENING INSPECTION IN CVG, LT WING OUTBOARD SECTION OF LEADING EDGE TOP UPPER SURFACE DEFORMED AND CRACKED. MAINTENANCE REPAIRED LEADING EDGE IAW EO A57048 AND BAE FAX BARA/AVR/6255/03-DC. A/C RELEASE DATE 2/24/03. 2H74 4F RTA49EU 20030418001552003041800155CE 2003 4 18 NSVA200300011 120030222A32601005810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE MLG INOPERATIVE A NSVAO OTHER N FALSE WARNING APAPPROACH 1 EA27031 UC103 FINAL INTO BKW-PILOT REPORTED DURING GEAR EXTENSION, DID NOT GET GREEN LIGHT INDICATION FOR NOSE GEAR DOWN AND LOCKED. CREW RETRACTED GEAR AND PERFORMED A MANUAL EXTENSION IAW WITH CHECKLIST, STILL NO LIGHT FOR NOSE GEAR. CREW DECLARED IN FLIGHT EMERGENCY (IFE). AIRCRAFT LANDING AT BKW WAS UNEVENTFUL. AIRCRAFT WAS ISSUED SFP TO HEF. MX FOUND A FAULTY NOSE LANDING GEAR DOWNLOCK POSITION SWITCH. REMOVED AND REPLACED SWITCH IAW AMM, OP'S CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20030421000052003042100005WP 2003 4 21 UPS03840231 120030213A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, AFTER REMOVAL OF LEAKING FASTENERS FOUND EXTERNAL DOUBLER AND UPPER WING SKIN CRACKED AT FASTENER HOLE AT XRS 22 AT STRINGER 5. REMOVED DOUBLER, OVERSIZED FASTENER HOLE, NDT VERIFIED NO CRACKS AT HOLE, FABRICATED FREEZE PLUG BUSHINGS, DOUBLER AND INSTALLED IAW SAA SK 811-230, DC8-57-20070. 2L74 4F RT4A25 20030421000092003042100009WP 2003 4 21 UPS03840237 120030225A3397 WIRE DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT BROKEN A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01808UP 46008 EMERGENCY LIGHTS DISARMED LIGHT INOP WITH SWITCH DISARMED. REPAIRED BROKEN WIRE AT TERMINAL A2 ON SWITCH S1-327 REF WDM 33-50-01. OPS CHECK GOOD. 2L74 4F RT4A25 20030421000122003042100012NM 2003 4 21 EIA200310 120030226A5320 STIFFENER BOEING747 747132 1384882NM PWA JT9 JT9D3 52050NE NLG WW CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 STIFFENER CRACKED AT STA 291, LBL 10 ON TOP OF NOSE WHEEL WELL BOX. INSTALLED KIT NR 65B282665 AND SUB KIT 65B282666 IAW EO 53-747-1138-91 REV C, IAW SB B747, SRM 51-30-02 PGS 1-15 2L74 4F4 F A20WE E20EA 20030421000202003042100020EA 2003 4 21 SWIA200311797 120030219A2760 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILERS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07589SW 7072 RIGHT FLT SPOILER FAULT STATUS MESSAGE AFTER USING SPOILERS IN FLIGHT. REMOVED AND REPLACED RIGHT FLIGHT SPOILER OUTBOARD PCU PER MM 27-62-01. BLED HYDRAULIC SYSTEM PER 29-10-00, OPERATED SPOILER 10 TIMES. OPS CHECK GOOD. LEAK CHECK GOOD. 2L72 4F RTA21EA 20030421000492003042100049WP 2003 4 21 ZW0A0302802 120030302A3350408822101 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13916TW 49187 THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 13 AND 22 WERE INOPERATIVE. REPLACED BATTERIES IN THE BATTERY PACK. CHECK-C 4-22-02 MCI. 2L72 4F A6WE 20030421000522003042100052NM 2003 4 21 QXEA0300307 120030228A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 OUT OF ADJUST A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09412QX 4059 SEA ON FLIGHT 2365- ON DEPARTURE FROM GEG, LANDING GEAR DID NOT RETRACT FULLY. LT MAIN GEAR INDICATED RED, LT MAIN DOOR INDICATED OPEN, LIGHT WAS ON IN GEAR HANDLE. GEAR CONFIRMED UP BUT GEAR DOOR OPEN CONFIRMED BY FLIGHT ATTENDENT. RAN CHECKLIST AND GEAR RETRACTED NORMALLY. LANDING GEAR INOPERATIVE CAUTION LIGHT DID NOT ILLUMINATE. RIGGED LANDING GEAR UPLOCK PROXIMITY SENSOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421000582003042100058 2003 4 21 MALA030183 420030301A3420 DISPLAY SAAB SF340 340B 7860101EU ADI FAILED A MALAA UNSCHED LANDING P NO WARNING INDICATION NRNOT REPORTED 1 GL15449XJ 340B449 DURING FLIGHT 3085, F/O'S TOP EFIS TUBE WENT BLANK. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 2 EADI P/N 6226342022, SN/OFF 5300, SN/ON 1887. NR 2 EFIS OPS CHECK GOOD IAW SF 340 MM CHAP 34. 2L72 4T RTA52EU 20030421000612003042100061SO 2003 4 21 SWIA200311810 120030217A5753 BRACKET EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAP ROLLER CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07564SW 120339 LT INBOARD FLAP BUTE DOOR INBOARD ROLLER BRACKET CRACKED. REPLACED ROLLER BRACKET ON LEFT INBOARD FLAP BUTE DOOR INBOARD POSITION. 2L72 4T4 TRTA31SO E20NE 20030421000652003042100065SO 2003 4 21 SWIA200311814 120030301A315080055711 WARNING HORN EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07289YV3564 3564 120289 ON TAKEOFF ROLL HAD A TRIPLE CHIME AND AUTO FEATHER AURAL WARNING WITH THE SWITCH IN THE ARMED POSITION AND THE ARMED LIGHT ON. ABORTED TAKEOFF. REMOVED AND REPLACED AURAL WARNING UNIT IAW 31-53-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20030421000712003042100071NM 2003 4 21 PCAA0303047 120030303A2931 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM NR 2 HYD PUMP ILLUMINATED A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13836EX 297 ABE-FLIGHT 3519 CREW REPORTED NR 2 HYDRAULIC PUMP LIGHT ILLUMINATED IN FLIGHT ALONG WITH RUDDER FULL PRESSURE, AND HYDRAULIC RUDDER CAUTION LIGHTS. EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO SIGN OF HYDRAULIC LEAKS. AIRCRAFT WAS GROUND RAN WITH CREW. ALL HYDRAULIC PRESSURE AND QUANTITIES INDICATED NORMAL. BOTH HYDRAULIC SYSTEMS WERE BLED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417000872003041700087NE 2003 4 17 QXEA0300217 220030130A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX2914 10011 GEE965212 PDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT 1 BLADES BROKEN, TWO BLADES CRACKED AND SOME WITH COLLATERAL DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER(ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030417002002003041700200NM 2003 4 17 QXEA0300257 120030213A2760 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 300 ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09374PH 528 SEA ON FLIGHT 2090- DURING STRAIGHT AND LEVEL FLIGHT SPOILER 1 PUSH-OFF LIGHT ILLUMINATED INTERMITTENTLY FOR SEVERAL MINUTES. PUSHED IT OFF AS PER CHECKLIST. REMOVED AND REPLACED MATRIX BLOCK AND PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030418000072003041800007EU 2003 4 18 RAIA00302039 120030204A3297 WIRE AEROSPATR72 ATR72202 8680940EU MLG BROKEN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03723TE 283 UPON GEAR RETRACTION MLG DID NOT RETRACT, NLG DID. MAINTENANCE RE-SEATED RECESSED PIN AND REPAIRED BROKEN WIRE AT NR 1 MULTI FUNCTION CONTROL, OPS CHECK OK. 2H72 4T RTA53EU 20030418000402003041800040WP 2003 4 18 MWEA030061 120030212A531099155964 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FRAME TO LONGERON WEB AT STATION 1380 TO 1401 LONGERON 14 RT IN AFT ACCESSORY HAS TOOLING DAMAGE ON OUTBOARD EDGE. REMOVED WEB, FABRICATED AND INSTALLED REPAIR DOUBLER. INSTALLED WEB AND REMAINING FASTENERS. 2L72 4F A6WE 20030825000462003082500046NM 2003 8 25 UPS03441105 120030718A5320 SUPPORT BEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C NOSE WHEEL WELL COMPARTMENT TUNNEL - AT STA 240 CEILING AREA THE CABIN FLOOR SUPPORT BEAM FWD AND AFT LOWER AREA CORROSION FOUND FROM BL0 - LBL 24. FLOOR SUPPORT BEAM REPAIRED AS IAW SRM 51-40-04 FIG. 1 DUE TO COR BLENDED AREA DEPTH 0.050 INCH, WIDTH 1 INCH AND LENGTH 4 INCHES EXCEEDED SRM 53-10-01 FIG.1 LIMITATION. 2L74 4F A20WE 20030825000992003082500099NM 2003 8 25 03FDEA01174 120030728A5320A5A7114511 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 CTR CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 49L SPLICE FITTING FOUND CRACK. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20030825001032003082500103NM 2003 8 25 03FDEA01314 120030809A5744ARC0503403 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 SNRM N0740 3A L2 FH WING 2FB FLAP 2FB HINGE 28 2FC SIDE 29 CORROSION FOUND ON LOWER ATTACHMENT HOLE12 FB BORE. LT WING O/B FLAP O/B HINGE ( A/C SIDE ) LOWER ATTACHMENT HOLE I/B BORE REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030825001152003082500115NM 2003 8 25 ABXA030193 120030610A5230140T26053 DOOR FRAME BOEING767 767281 1385109NM GE CF6 CF680 30025NE CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 AFT CARGO DOOR BEAM NR 5, CORROSION WAS FOUND ON THE INNER CHORD P/N 140T2605-3 UNDERNEATH PUMP. AFTER CORROSION REMOVED MINIMUM REMAINING THICKNESS WAS 0.082, WHILE ORIGINAL THICKNESS WAS 0.125 INCH. 2L72 4F4 FRTA1NM E13NE 20030825001212003082500121WP 2003 8 25 ABXA030330 120030818A261251114123 ELEMENT DOUG DC8 DC861 3021952WP PWA JT3D JT3D3B 52039NE FIRE LOOP MISSING A ABXAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL23847AX 46031 644651 ENROUTE , NR 3 ENGINE FIRE WARNING CAME ON. ONLY OTHER INDICATION WAS HIGH OIL TEMP. CREW ELECTED TO USE RT WING OB ENGINE FIRE BOTTLE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE NR 3 ENGINE. NO EVIDENCE OF FIRE OR FIRE DAMAGE FOUND. DURING INSPECTION, FOUND NR 3 ENGINE LOWER FIRE SENSING ELEMENT MISSING TAN CENTERING BRACKETS CAUSING CENTER CONNECTOR TO CHAFE AGAINST SHIELD. REPLACED LOWER FIRE SENSING ELEMENT IAW AMM. PERFORMED ADJ/TEST. OPS NORMAL. REMOVED AND INSP. OIL STRAINER. NO DEFECTS FOUND. RAN ENGINE, LEAK CHECKED NORMAL. ALL ENGINE PARAMETERS NORMAL. REPLACED RT WING OB FIRE EXTINGUISHING CONTAINER AND CARTRIDGES IAW AMM. COMPLIED WITH ENGINE FIRE DETECTION JOB CARD 8870501 FOR NR 3 ENGINE. 2L74 4F4 F 4A25 1E8 20030826000042003082600004EU 2003 8 26 03FDEA01353 120030821A3097 WIRE HARNESS AIRBUS310 A310 EU COCKPIT FIRE A FDEAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 SO25446FE 224 EN ROUTE RIGHT SIDE SLIDING WINDOW HEAT POWER CORD CAUGHT FIRE. SWITCH WAS TURNED OFF AND FIRE WAS EXTINGUISHED. LANDED KLCK, INSP HEAT HARNESS WIRE, FOUND BURNED AREA. REMOVED FROM TERMINAL STRIP AND COMPLIED WITH PART 1 OF EA-6-3040-72501. PER MOCC REQUEST, REPLACED WINDOW TEMP CONTROLLER 20DG, PER A310 MM 30-42-11-4. REMOVED AND REPLACED CB'S 4DG, 6DG, AND 8DG REF A310, REF WRI 30-40-6952 FOR REPAIR OF WIRING. COMPLIED WITH EA 6-3040-72501, REMOVAL AND INSTALLATION OF RETRACTABLE WIRING ASSY ON RT SLIDING WINDOW REF A310. OPS CHECK OF RT WINDOW HEAT CHECKS NORMAL REF MM 30-42-00-5. 2L72 4F RTA35EU 20030826000082003082600008WP 2003 8 26 03FDEA01357 120030821A5753ARC0502 HINGE BRACKET DOUG DC10 DC1010 3022110WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 WINGS- OUTBOARD FLAP (RT) INBOARD HINGE BRACKET- ACTUATOR ATTACH HOLE REPAIR P/N ARC0502 ENT BY: 497239 RPT BY: 497239 FACT 19AUG03 13:22 BFM R COMPLIED WITH EA 8-5750-72261, WINGS- OUTBOARD FLAP (RT)- INBOARD HINGE BRACKET- ACTUATOR ATTACH HOLE REPAIR P/N ARCO502 ENT BY: 497191 RPT BY: 497191. 2L73 4F A22WE 20030826000102003082600010NM 2003 8 26 03FDEA01359 120030822A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 DENT IN SKIN BS 380 BETWEEN STR 14L AND STR 15L. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER (EXTERNAL) PER EA 7-5330-70501. 2L73 4F RTA3WE 20030826000142003082600014NM 2003 8 26 03FDEA01362 120030822A5320 STIFFENER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 STIFFENER INSIDE DELTA BEAM AT BS 789, RBL 3, WL 154 IS CORRODED. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2. 2L73 4F RTA3WE 20030826000562003082600056NM 2003 8 26 03FDEA01141 120030725A3260 WARNING LIGHT BOEING727 727200 138407ENM COCKPIT ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25479FE 21461 AFTER LANDING GEAR RETRACTION, RT MLG DOOR LIGHT REMAINED ILLUMINATED (F/O PANEL+S/O PANEL). RECYCLED GEAR PER RED TABS BUT LIGHT REMAINED ILLUMINATED. R/R RT MLG DOOR WARN SWITCH. R/R CONNECTORS D752 & D4660P. 2L73 4F RTA3WE 20030826000762003082600076NM 2003 8 26 CALA0300473 120030821A5330 SKIN BOEING777 777224 1385225NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777012 29860 INSPECTION THE FUSELAGE SKIN DENTED JUST AFT OF R-4 DOOR AT STA 2108-2129, FLOOR LEVEL, BETWEEN S27R AND 28R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 4. A DIP WAS ISSUED TO REINSPECT THE REPAIR WITHIN 30,000 CYCLES, THEN EVERY 16,000 FLIGHT CYCLES. 2L72 4F RTT00001SE 20030826000832003082600083 2003 8 26 YENA200321 420030809A2330 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15506JB 1235 F/A REPORTED BURNING SMELL FROM TV'S ROW 12/14/15/16. TV'S WERE FLICKERING IN ROW 12. POWER REMOVED FROM TV SYSTEM INFLIGHT AS PRECAUTION. PERFORMED MX ACTION IAW JETBLUE INFORMATION NOTICE 2003-T050TR. NO DEFECTS NOTED LIVE TV SYSTEM OPERATIONS NORMAL. OK FOR SERVICE. 2L72 4F RTA28NM 20030826001182003082600118CE 2003 8 26 2003F00372 120030611A323371053101 ROD END DECOTO CESSNA500 500CESSNA 2076602CE RT MLG DEFECTIVE B K NONE O OTHER ININSP/MAINT 1 SO11913RC9723 116 20 5000059 RIGHT MAIN LANDING GEAR ACTUATOR ROD END, ATTACHING TO MLG LEG, FOUND WITH ROD END BEARING EXTENDED TO THE EXTREME AFT POINT OF INSERTION INTO ROD END PLACING RM LG IN DANGER OF COLLAPSE. ROD END ASSEMBLY WAS REPLACED WITH NEW, MFG SUPPLIED UNIT IAW MAINTENANCE MANUAL 32-10-00 OBSERVING PROPER CAMBER AND GEAR RETRACTION OPERATION. 1L72 4F A22CE 20030826001322003082600132NM 2003 8 26 USAABB03123 120030727A493038760355 SENSOR BOEING757 757225 1384959NM APU MALFUNCTIONED A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19603AU 22198 BDA - FLT 1442 - EN ROUTE FROM SXM-PHL, THE LEFT IDG FAILED. CREW STARTED APU AND CONTINUED FLIGHT. APPROXIMATELY 200 NAUTICAL MILES FROM BDA, AND APU FAILED. FLIGHT DIVERTED TO BDA AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE IDG. THE APU FUEL FLOW DIVIDER WAS REPLACED AND DID NOT SOLVE THE PROBLEM. THE P2 SENSOR WAS REPLACED. (M) 2L72 4F RTA2NM 20030826001542003082600154SO 2003 8 26 SIMA200320804 120030720A5330 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21633AE 145148 ABI - REPAIR TO A DENT AND GOUGE IN THE LEFT REAR FUSELAGE SKIN SPANNING THE SIN PANEL SEAM BETWEEN STRINGERS 17L AND 18L, FRAMES 70 AND 71. RECONTOURED THE DENTED SKIN. PERFORMED AN EDDY CURRENT INSPECTION OF THE REWORKED AREA AND OFUND THE SKIN AND SPLICE STRAP HAD CRACKS. COMPLETELY REMOVED CRACKED SECTION OF FUSELAGE SKIN BY PERFORMING A CUTOUT. FABRICATED A SPLICE STRAP AND TWO FUSELAGE SKIN DOUBLERS. REPAIR DONE IAW EMB STATEMENT IC2003-145/2421, IC 2003-145/2445 AND EMB 145 SRM, SRM 145/1142 REV 22, 51-00-01. (M) 2L72 4T RTT00011AT 20030418000612003041800061NM 2003 4 18 QXEA0300268 120030204A5410 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - RIGHT HAND LOWER COWL CONE SUPPORT BRACKET UPPER ANGLE CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030418000652003041800065NM 2003 4 18 QXEA0300272 120030202A5410 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - CRACKED CENTER AFT CONE SUPPORT ANGLE AT STATION XN80.330, ON LEFT HAND LOWER COWL. REPAIRED IAW DHC-8 Q400 SRM 51-42-00, RD 8/4-71-016 AND MM 71-61-01, PAGE 2, PARAGRAPH 4A, SUB TASK 71-61-01-420-001. 2H72 4T RTA13NM 20030418000702003041800070NM 2003 4 18 QXEA0300280 120030212A3213 STRUT BOMBDRDHC8 DHC8401 1390041NM ZONE 700 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - RT MAIN LANDING GEAR DRAG STRUT HAS CHAFE 25 INCHES ABOVE LOWER END. REPAIRED IAW DHC-8 Q400 MM 32-11-11-000-801. 2H72 4T RTA13NM 20030418000742003041800074NM 2003 4 18 QXEA0300284 120030204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - NR 2 VHF ANTENNA MOUNT AREA INTERNAL RIGHT HAND SET OF BRACKETS FORWARD BRACKET IS CRACKED AT 325 AND X86. REPAIRED IAW HORIZON AIR EO/EA 6-51-162A. 2H72 4T RTA13NM 20030418000982003041800098WP 2003 4 18 UPS03840201 120030206A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1000 ABOVE L33R FRAME IS CORRODED. REMOVED FRAME CAP IAW DC8 SRM 51-1-21 & 51-1-20D. LOCATED DRILLED AND DEBURRED NEW FRAME CAP 9755885-7 IAW DC8 SRM 51-1-21 & 51-1-20D. INSTALLED NEW FRAME CAP IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030418001072003041800107WP 2003 4 18 ZW0A0302501 120030218A2120 SMOKE DOUG DC9 DC982 3022082WP CABIN DETECTED A ZW0AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE13924TW 49100 BEFORE LOADING AIRCRAFT, SMOKE IN CABIN. SHUT DOWN PACKS AND APU DUE TO DEICER FLUID IN WATER SEPARATOR BAG. REPLACED WATER SEPARATOR BAGS. ACCOMPLISHED PACK BURN OUT AND COMPLETED MD9-49-06 MD9-21-01 AND MD9-49-04. CHECK-C STL 3-18-02. 2L72 4F A6WE 20030421000042003042100004WP 2003 4 21 UPS03840230 120030208A5720 STRINGER CLIP DOUG DC8 DC873F 302199FWP RIGHT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, RIGHT WING STRINGER CLIP IS CRACKED AT STRINGER 73 AT XRS 50. REMOVED, FABRICATED, AND REPLACED CLIP IAW SAA SK 811-162. 2L74 4F RT4A25 20030421000812003042100081NM 2003 4 21 DLM88030086 120030123A53305911401521 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27932DL 49719 THE FUSELAGE SKIN WAS DENTED AND PUNCTURED NEAR STRINGER 21L BETWEEN FS 110 & 170. THE DAMAGE WAS REMOVED WITH 3 CUTOUTS. TWO SMALL CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER THE MD-88 SRM. THE LARGEST, 16 X 5 INCH, CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 384404-14, REV A. 2L72 4F RTA6WE 20030421000882003042100088NM 2003 4 21 DLM88030123 120030202A492032680 APU DOUG MD88 MD88 3023688NM CONTAMINATED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27955DL13591 49886 P80103 DURING TAXI OUT WITH ONE ENGINE OPERATING AND APU OPERATING, SMOKE BEGAN TO FILL THE CABIN. AFTER BOTH PACKS TURNED OFF, SMOKE BEGAN TO CLEAR. RETURNED TO GATE. FOUND OIL LEAKING FROM APU COMPARTMENT AND DRIPPING IN VICINITY OF APU AIR INTAKE. APU AIR INLET SATURATED WITH OIL. CLEANED INLET, PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20030421000902003042100090NM 2003 4 21 DL76P030128 120030204A335020131A BATTERY PACK BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27140LL 25988 EMERGENCY LIGHTS AT SEATS 1AB THRU 12AB AND 13FG THRU 21FG WILL NOT ILLUMINATE. REPLACED BATTERY PACK M9008, LIGHTS CHECK GOOD. 2L72 4F RTA1NM 20030421000912003042100091NM 2003 4 21 DL76S030132 120030206A5311148T11504 FRAME BOEING767 767332 1382001NM BULKHEAD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27120DL 23279 INSPECTION OF THE FS 1809.5 BULKHEAD OUTER FRAMES PER BAC S/B 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE FWD FRAME AND THE AFT FRAME ON THE RT SIDE NEAR STRINGER 12. THE FWD FRAME WAS REPLACED PER THE S/B. THE AFT FRAME WAS REMOVED AND REPLACED WITH A NEW FRAME PER ER/A 384407-14AD, REV A. 2L72 4F RTA1NM 20030421001012003042100101NM 2003 4 21 DL76P030171 120030220A29107321870018 VALVE BOEING767 767332 1382001NM FLAP/SLAT LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO271402A 25989 C-HYD QTY MESSAGE HYD QUANTITY DOWN TO .43. A/C RETURNED TO CVG. FOUND FLAP/SLAT S/O VLV MODUAL LEAKING IN RT W/W. REPLACED SAME PER M/M. REFILLED HYD SYS, NO RII PER TOPP 40-30-05. 2L72 4F RTA1NM 20030421001092003042100109NM 2003 4 21 DLM88030198 120030225A3350333701850 POWER SUPPLY DOUG MD88 MD88 3023688NM AFT CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27920DL 49644 AFT SECTION EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY. 2L72 4F RTA6WE 20030421001152003042100115EA 2003 4 21 QXEA0300305 120030228A2121 FAN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 PLUGGED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09601QX 10009 FAT - FLT 2530-SUPP, RETURNED TO FIELD. AFT LAV SMOKE DETECTOR LIGHT. NO EMERGENCY DECLARED. NO CURRENT STATUS MESSAGE. INTERROGATED MDC SERVICE MESSAGE HISTORY. FOUND LAVATORY EXTERNAL FAN LOW SPEED MESSAGE. FOUND EXHAUST FAN INLET GRILL PARTLY PLUGGED WITH LINT, CLEANED, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030421001392003042100139NM 2003 4 21 UPS03240254 120030223A5320 STIFFENER BOEING727 727108C 1384039NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, CORROSION ON INTERNAL SIDE OF NLG LT SIDE WALL AT BS 285 (FWD OF VERTICAL STIFFENER) LWR END CORROSION FOUND AT BS 280 & 285 BETWEEN STIFFENER AND SKIN. SKIN CUTOUT MADE AT VERT STIFFENER TO REMOVE CORROSION IAW SRM 51-10-6. DOUBLER FABRICATED IAW SRM 51-40-2. FILLERS FABRICATED IAW SRM 51-40-2. INSTALLED IAW SRM 51-40-2. 2L73 4F A3WE 20030421001772003042100177WP 2003 4 21 GTIA030130 120030220A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND MAIN CABIN FLOOR PANEL STATION 1174 TO STATION 1250, CENTER, HAS SOFT/MUSHY DETERIORATED AND SEVERAL INSERTS CORRODED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030417002102003041700210NM 2003 4 17 QXEA0300259 120030212A5410 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - NR 1 ENGINE LOWER COWL ASSEMBLY CENTER WEB, BOTTOM SUPPORT ANGLE CRACKED ACROSS AFT TWO RIVETS. REPAIRED IAW RD 8/4-71-016 AND Q400 MM 71-61-01. 2H72 4T RTA13NM 20030417002122003041700212NM 2003 4 17 QXEA0300261 120030212A5410 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX -NR 1 ENGINE LOWER COWL ASSEMBLY CENTER WEB UPPER SUPPORT ANGLE CRACKED ACROSS FORWARD TWO RIVETS. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030418000492003041800049WP 2003 4 18 UPS03840184 120030203A5310SAASK8117471 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, STATION 300 TO 320 LONG 13L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SAA SK 811-747 AND SRM 51-1-20D. 2L74 4F RT4A25 20030418000902003041800090NM 2003 4 18 F3LA200300060 120030201A5320 SUPPORT BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON ZEE SUPPORT IN RT SIDE OF AFT CARGO COMPARTMENT, FROM STA 721 TO 767. FABRICATED AND INSTALLED NEW ZEE SUPPORT PER SRM 53-60-53, SRM 51-40-05, SRM 51-40-02, MM 51-21-41 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030418001412003041800141WP 2003 4 18 ZW0A0302703 120030222A3240 BRAKE ASSY DOUG DC9 DC983 3022083WP MLG CONTAMINATED A ZW0AO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE139403W 53139 DURING LANDING ROLL ANOTHER AC REPORTED SMOKE FROM LEFT GEAR AREA. SMOKE QUICKLY DISSIPATED NO EVIDENCE OF HYD FLUID ON GEAR. FIRE DEPT CALLED AS PRECAUTION. NO SYS FAULTED BUT EVIDENCE OF ICE-DEICE FLUID RESTING ON NR 1 BRAKE ASSY AND STRUT. REMOVED ICE. BRAKE OPS WAS NORMAL. CHECK-C STL 9-11-02. 2L72 4F RTA6WE 20030421000192003042100019EA 2003 4 21 SWIA200311796 120030221A27603G5209D LEVER CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07437SW11 11 7564 ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW 27-61-01. OPS CHECK GOOD. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-62-01. OPS AND LEAK CHECK GOOD. P/N OFF: 27000-7, S/N OFF: MAL 4753. 2L72 4F RTA21EA 20030421000372003042100037 2003 4 21 UPS03140247 420030227A2565 BOTTLE AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01130UP 0815 MAIN CABIN DOOR SLIDE LOW PRESSURE DEF M255139. REPLACED MAIN CABIN DOOR SLIDE W/REF TO AMM 25-61-21--401. SATISFACTORY TAG 779646. 2L72 4F RTA35EU 20030421000772003042100077NM 2003 4 21 DLM11030075 120030119A32404305990040 TRANSDUCER DOUG MD11 MD11 3023602NM NR 5 WHEEL FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27802DE 48473 RTO - TIRE PRESSURE LOW PRESSURE LIGHT ON TAKEOFF AFT LEFT TIRE ON CAPTS SIDE INDICATED 54 LBS. AFTER DISCONTINUING TAKEOFF PRESSURE RETURNED TO NORMAL. REPLACED 5 WHEEL TRANSDUCER. 2L73 4F RTA22WE 20030421002072003042100207NM 2003 4 21 AMTA200300323 120030210A5330 SKIN BOEING757 75723N 1384973NM FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FUSELAGE SKIN DENTED AT LEFT CREASE BEAM. REPAIRED DAMAGED AREA PE ER/A 757-53R-5084. (M) 2L72 4F RTA2NM 20030421002132003042100213NM 2003 4 21 AMTA200300371 120030306A5330 SKIN BOEING757 75733N 1384931NM FUSELAGE CANNING A AMTAK NONE O OTHER ININSP/MAINT 1 GL11551TZ 32585 FOUND LEFT FUSELAGE SKIN OIL CANNING AT CREASE BEAM. REPAIRED FUSELAGE SKIN IAW ER/A 757-53R-5098. (M) 2L72 4F RTA2NM 20030422000282003042200028SO 2003 4 22 ASOA03072 120030221A523012023348005 SEAL EMB 120 EMB120ER 3260203SO CARGO DOOR LOOSE A ASOAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SO11639AS 120283 FLT 4955 - DURING CLIMB-OUT FROM DFW-AEX, AT APPROXIMATELY 25,000 FT CABIN PRESSURIZATION STARED TO CLIMB RAPIDLY. THE CREW MADE AN EMERGENCY DESCENT AND LEVELED OFF AT APPROXIMATELY 9,000 FEET. THE AIRCRAFT LANDED SAFELY IN AEX. S/D - MAINTENANCE RE-INSTALLED THE LOOSE CARGO DOOR SEAL INTO ITS RETAINERS. PRESSURIZATION AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030422000342003042200034EU 2003 4 22 ASOA03081 120030225A2120 SMOKE AEROSPATR72 ATR72 EU COCKPIT DETECTED A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11630AS 336 FLT 4121 - DURING CLIMB-OUT FROM ATL-CSG, AT APPROXIMATELY 3,000 FT, THE CREW SMELLED SMOKE WITH NO VISIBLE SIGNS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MX REMOVED, INSPECTED AND RE-INSTALLED THE SMOKE DETECTOR IN THE ELECTRONICS RACK, INCLUDING INSPECTION OF THE DUCTS AND RELAY SHELVES WITH NO DEFECTS NOTED. MAINTENANCE ALSO PERFORMED TWO THIRTY MINUTE ENGINE RUNS WITH NO ELECTRICAL SMOKE MESSAGES OCCURRING ON THE CREW ALERT PANEL. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030422000372003042200037EU 2003 4 22 ASOA03069 120030219A3350 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN MALFUNCTIONED A ASOAO OTHER N FALSE WARNING CRCRUISE 1 SO11530AS 453 DURING FLIGHT FROM ATL-CHA, THE EMERGENCY LIGHTS ILLUMINATED WITH THE SWITCH SELECTED TO THE ARM POSITION. MAINTENANCE RAN THE RIGHT ENGINE WTH THE EMEGENCY LIGHTS OPERATIONING NORMAL. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030422000472003042200047EU 2003 4 22 ASOA03066 120030217A33503012000 BATTERY PACK AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT DISCHARGED A ASOAO OTHER J WARNING INDICATION CRCRUISE 1 SO11530AS 453 FLT 4378 - DURING FLIGHT FROM ABY-ATL, THE FORWARD SECTION OF EMERGENCY LIGHTS ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS NR 2 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030422000562003042200056CE 2003 4 22 2003F00232 120030307A3610C1448732 REGULATOR VALVE CESSNA750 750 2076810CE TAIL BAY MALFUNCTIONED A UG8AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL235115 7500018 ON APPLICATION OF TAKEOFF POWER, AMBER EICAS MESSAGE 'HP DUCT 'O' PRESS R' CAME ON. ABORTED TAKEOFF. RIGHT HIGH PRESSURE REGULATING VALVE FAILED TO REGULATE PROPER BLEED AIR PRESSURE. REPLACED RIGHT HP BLEED AIR REGULATOR VALVE. OPERATION NORMAL. (M) 2L72 4J RTT00007WI 20030422000632003042200063GL 2003 4 22 SIMA200306416 220030305A720023072309 CARBON SEAL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL LT ENGINE WORN A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW21723AE 145288 LGA - FLT 4450 - DURING APPROACH, THE FLIGHT CREW REPORTED FUMES AND SMOKE IN COCKPIT. REPORTED AS A NON-ELECTRICAL SMELL. THE RECIRCULATION FANS WERE TURNED OFF AND MASKS AND GOGGLES WERE PUT ON AS PER CHECKLIST. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE ZERO CARBON SEAL IN THE LT ENGINE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20030422000752003042200075SO 2003 4 22 SIMA200305011 120030125A532014522451011 DOUBLER EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 ABI - DURING IMBV INSPECTION A LEVEL 2 FINDING FOUND. DIAMOND DOUBLER ON RIGHT HAT BEAM AT FRAME 20 CORRODED. INSTALLED NEW DIAMOND DOUBLER IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04, 51-40-06. (M) 2L72 4T RTT00011AT 20030422000822003042200082SO 2003 4 22 SIMA200307908 120030311A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 ABI - DURING AN IMBV INSPECTION, CORROSION ON THE CENTER OMEGA BEAM AT FRAME 20. REMOVED CORRODED AREA BY CUTOUT. FABRICATED AN EXTERNAL U-SHAPE DOUBLER. REPAIRE DONE IAW EMB 145 SRM (145/1142, REV 20) 53-21-10 PARA 5, FIG 204 SHEET 2 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030422000842003042200084SO 2003 4 22 SIMA200203071 120030219A532014521725001 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 ABI - THIS IS A LEVEL TWO FINDING FOUND DURNG AN IMBV INSPECTION GALLEY AREA LEFT SIDE SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-40-06, 51-20-03 AND 51-40-02. (M) 2L72 4F RTT00011AT 20030422000872003042200087SO 2003 4 22 SIMA200307905 120030222A532014521725615 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL IS CORRODED. REMOVED AND INSTALLED SERVICE DOOR SILL IAW EMB 135 SRM 51-40-02, 51-20-03 AND 51-40-06. (M) 2L72 4F RTT00011AT 20030714001662003071400166EU 2003 7 14 BAQA087753 120030625A2121ES730732 FAN BOLKMSBK117 BK117C1 5626025EU BLOWER SEPARATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY102 7544 FAN BLADE DEPARTED FAN HUB. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030714001672003071400167EU 2003 7 14 BAQA087908 120030703A249745023502 MASTER SWITCH UROCOPEC135 EC135T1 5620026EU ELECTRICAL MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03485AE28 0273 WILL NOT TEST EXTERNAL POWER. WILL NOT COME ON. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030716000352003071600035NM 2003 7 16 TSAA0353150 120030522A53106545875 CREASE BEAM BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 FOUND CORROSION DISCOVERED ON LEFT CREASE BEAM BETWEEN BS 307 AND 310. REMOVED AND REPLACED SECTION BETWEEN BS 307 AND BS 310. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2 AND 51-40-3. (M) 2L72 4F RTA16WE 20030716000702003071600070SO 2003 7 16 SIMA200311802 120030424A5330 SKIN EMB 135 EMB135KL 3260302SO FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21802AE 145471 ABI - DURING AN MBV INSPECTION A DENT WAS FOUND BETWEEN FRAME 75 AND 75A AND STRINGERS 10L, 11L. PERFORMED AN EDDY CURRENT INSPECTION OF THE DENT. NO DEFECTS NOTED. REMOVED DAMAGED AREA BY CREATING A 2 INCH BY 3 INCH CUTOUT. PERFORMED ADDITIONAL NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER AND FILLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/1358, IC2003-145/1393 AND STANDARD EMB SRM, SRM 145/1142 REV 21 PRACTICES. (M) 2L72 4F RTT00011AT 20030716000762003071600076CE 2003 7 16 2003F00425 120030617A2720 ACTUATOR CESSNA750 750 2076810CE RUDDER INOPERATIVE A O2GAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NE03610GR 7500163 TAKING OFF FROM CLT, CREW GOT A CYAN FGC FAIL MESSAGE. THE FGC B REVERTED AUTOMATICALLY, IN AN ATTEMPT TO CHANGE FGC SOURCE BACK, GOT THE SAME MESSAGE. LANDED AT GSO. (M) 2L72 4J RTT00007WI 20030717000232003071700023SW 2003 7 17 HEEA088000 120030627A6720407001732101 BELLCRANK BELL 407 407 1182206SW T/R CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 TAIL ROTOR CONTROL BELLCRANK BOLT HOLE WORN (OUT OF ROUND). REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000952003071700095WP 2003 7 17 AMTA200300741 120030430A5330 SKIN LKHEED1011 10113853 5265020WP AC POWER RECP CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 EXTERNAL AC POWER RECEPTACLE CUTOUT DOUBLER CRACKED. REPAIRED INNER DOUBLER IAW ER/A L10-53R-5135. (M) 2L73 4F A23WE 20030721000262003072100026EU 2003 7 21 CA030624002 120030620A5754801B170001 BEARING AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE LE SLAT FAILED W K NONE O OTHER ININSP/MAINT 1 CA 36063 (CAN) AT H 02 CHECK ,FOUND RT SLAT TORQUE TUBE STEADY BEARING FIN 6081CM WITH NO BALL BEARINGS LEFT IN BEARING ASSEMBLY THIS STEADY BEARING IS LOCATED INBOARD OF RIB 13 INBOARD SIDE OF TELESCOPING PNEUMATIC DUCT BRACKET ON RT WING LEADING EDGE REMOVE AND REPLACE AS PER AMM REF,27-84-44-400AC TOTAL TIME 36063, AC CYCLES 16,346 TOTAL COMPONENT TIME 36063 2L72 4F4 FRTA28NM E29NE 20030721000572003072100057WP 2003 7 21 CNMA200300002 120030701A3350EMSE299A BATTERY PACK DOUG DC10 DC1030 3023501WP EMERGENCY LIGHTSNOT SEATED A CNMAO OTHER J WARNING INDICATION CRCRUISE 1 SW07630AX 46596 EXIT LIGHTS AT L-3 AND R-3 DOOR CAME ON IN-FLIGHT AND STAYED ON. 2L73 4F A22WE 20030716001132003071600113NE 2003 7 16 HEEA088043 120030703A24207655009005105 GENERATOR SKRSKYS76 S76A 8143006NE ELECTRICAL INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 GENERATOR INOPERATIVE. 1G72 3U H1NE 20030716001182003071600118 2003 7 16 HEEA088048 420030704A237080510800001 CONTROL BOX SKRSKYS76 S76A 8143006NE WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03776P 760275 SYSTEM DOES NOT COME BACK ON WHEN POWER IS CYCLED FROM CIRCUIT BREAKER OR RADIO MASTER SWITCH. SYSTEM WOULD ONLY COME BACK ON WITH SWITCH ON DISPLAY. TO BE SENT TO VENDOR FOR WARRANTY REPAIR. 1G72 3U H1NE 20030717000072003071700007 2003 7 17 HEEA087984 420030626A3421504001790116 GYRO BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ATTITUDE GYRO WILL NOT ERECT. SHOP REPAIR. 1G72 4U H4SW 20030717000432003071700043SW 2003 7 17 HEEA088018 120030621A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 TAIL ROTOR DISC PACK CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000742003071700074 2003 7 17 HEEA088066 420030705A2350A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 SELECTOR SWITCH WORKS INTERMITTENTLY. SHOP REPAIR. 1G72 4U H4SW 20030717000782003071700078 2003 7 17 HEEA088070 420030625A3457N0002000 GPS BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 GPS UNIT INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030717000842003071700084SW 2003 7 17 HEEA088076 120030707A6420 TRUNNION BELL 206 206L3 1182108SW TAIL ROTOR HEAD MISINSTALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034112812444 A386 51134 TAIL ROTOR TRUNNION INCORRECTLY ASSEMBLED. THERE IS EXCESSIVE END PLAY IN TRUNNION. SHOP REPAIR. 1G71 3U H2SW 20030718000402003071800040NM 2003 7 18 USAASB03088 120030620A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US 23886 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LAST TWO SEAT ROWS, THE AFT RT SERVICE DOOR AND THE RIGHT EMERGENCY EXIT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 6 BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030718000422003071800042WP 2003 7 18 WRLA200314 120030621A36101879009 HEAT EXCHANGER DOUG DC10 DC1030 3023501WP PNEUMATIC SYS LEAKING A WRLAO OTHER J WARNING INDICATION CLCLIMB 1 EA2714075 46922 NR 2 PNEUMATIC MANIFOLD FAILURE LIGHT ILLUMINATED WITH TWO PACKS OFF AND TWO PNEUMATIC SYSTEMS OFF. AGAIN EXECUTE VOL II 01-10-09 EMERGENCY PROCEDURE. FOUND EXCESSIVE HOT AIR LEAKAGE FROM NR 1 AND NR 2 HEAT EXCHANGERS TO BOTH ACM'S CONNECT SLEEVES AND FROM BOTH HEAT EXCHANGERS TO PLENUMS INTERFACE. SECURED NR 2 PACK SLEEVES AND HEAT EXCHANGER TO PLENUMS. LEAK CHECK FOUND GOOD DURING TEST WITH MODERATE PWR ON ALL 3 ENGINE. NO AMC NR 2/3 OR PNEUMATIC SYSTEMS FAULTS NOTED. VISUALLY CHECKED ACCESSIBLE NR 2 MANIFOLD AND NO OBSERVED LEAKS NOTED. DEFERRED NR 1 PACK INOPERATIVE IAW MEL 21-1 ESTABLISHED ON NR 1 ENTERED DMI M21JUU23-44, HEAT EXCHANGER LEAK. AIRCRAT RETURNED TO LGSA FOR REPAIRS. REMOVED AND REPLAC2L73 4F A22WE 20030721001132003072100113GL 2003 7 21 AUS20030618 220030412A7230695687 BLADE BOEING767 767338 1385151NM GE CF6 CF680C2* GL COMPRESSOR SEPARATED W O OTHER DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 AUS 3838 (AUS) RT ENGINE FOURTH STAGE HP COMPRESSOR BLADE MISSING. FOUND DURING BOROSCOPE INSPECTION FOLLOWING ENGINE SURGE. 2L72 4F4 FRTA1NM E23EA 20030721001152003072100115NM 2003 7 21 SWAA031453 120030628A275065503242527 TRANSMISSION BOEING737 7372H4 138448CNM TE FLAPS FAULTY A SWAAO OTHER F FLT CONT AFFECTED LDLANDING 1 SW29082SW 22731 T/E FLAPS WOULD NOT EXTEND PAST 15 DEGREES. REMOVED AND REPLACED NR 7, NR 5 AND NR 4 FLAP TRANSMISSIONS PER MM. 2L72 4F A16WE 20030721001232003072100123NM 2003 7 21 SWAA031487 120030706A53106935365 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030721001272003072100127 2003 7 21 SWAA031491 420030705A25656519901 CABLE BOEING737 7373TO 138447GNM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030721001352003072100135NM 2003 7 21 SWAA031518 120030709A53106545871 DOOR FRAME BOEING737 7373H4 1384600NM SERVICE DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER DOOR STOP. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030722000082003072200008NM 2003 7 22 2003F00436 120030310A5754 RETAINER BOEING727 727222 1384073NM NR 5 SLAT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT NR 5 SLAT, INBOARD HOOK SEAL CUTOUT, OUTBOARD SEAL RETAINER. REMOVED AND REPLACED NR 5 SLAT INBOARD HOOK SEAL, UPPER LEADING EDGE, OUTBOARD SEAL RETAINER TRIM. (M) 2L73 4F A3WE 20030722000182003072200018NM 2003 7 22 2003F00446 120030308A5720 BRACKET BOEING727 727222 1384073NM LT WING CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET, OUTBOARD OF NR 2 SPOILER ACTUATOR. REMOVED AND REPLACED BRACKET ON LEFT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET AT NR 2 SPOILER, OUTBOARD OF ACTUATOR. (M) 2L73 4F A3WE 20030722000192003072200019NM 2003 7 22 2003F00447 120030307A5310 BEAM BOEING727 727222 1384073NM BULKHEAD CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT AFT PRESSURE BULKHEAD VERTICAL BEAM, BS 1183, LBL 26.9, WL 260. STOP DRILLED CRACKS ON AFT PRESSURE BULKHEAD BS 1183, LBL 26.9 VERTICAL BEAM WL 260. LOCATED/DRILLED -UP KIT NR 65C33556-41 REPAIR ANGLE. TREATED AND PRIMED REPAIR ANGLE. INSTLALED KIT NR 65C33556-41 REPAIR ANGLE. (M) 2L73 4F A3WE 20030722000222003072200022NM 2003 7 22 2003F00450 120030124A5514 HINGE PIN BOEING727 727222 1384073NM HORIZONTAL STAB CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND HORIZONTAL STAB, LEFT INNER HINGE PIN, HAS CORROSION ON THREADED END. REMOVED AND REPLACED HORIZONTAL STAB LEFT INNER HINGE PIN. (M) 2L73 4F A3WE 20030722000402003072200040EU 2003 7 22 MALA030326 120030703A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15536XJ E2372 DURING FLIGHT 3478, DURING CRUISE AT 29000 FT THE YELLOW HYD HIGH TEMP LIGHT ILLUMINATED. FOLLOWED THE QRH AND SOME TIME AFTER TURNED OFF THE NR 2 ENG PUMP AC PUMP, AND THE PTU, THE HIGH TEMP ANNUNCIATOR WENT OUT. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED NR 2 EDP IAW RJ85 MM 29-10-17. P/N ON OFF 521449, S/N ON F9717007, S/N OFF GOO1OO70. RAN SYSTEM FOR APPROX 1 HOUR, NO FAULTS NOTED. ALL CHECKS GOOD AT THIS TIME. 2H74 4F RTA49EU 20030722000422003072200042EU 2003 7 22 MALA030328 120030703A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 LEFT CENTER AISLE SEAT TRACK LBL 18.3 FROM STA 297-319 HAS CORROSION. MAINTENANCE COMPLETED SPLICE REPAIR IAW EO S53060. REF 409 NR 192030 FOR FURTHER DETAIL. A/C RELEASE DATE 7/6/03. 2L72 4T RTA52EU 20030722000452003072200045NM 2003 7 22 HNAA0300031 120030713A33506013211X BATTERY DHAV DHC8 DHC8102 2809003NM CABIN DEFECTIVE A HNAAO OTHER O OTHER NRNOT REPORTED 1 EA07931HA28861386 132 THREE EACH EMERGENCY LIGHTS ILLUMINATE WHEN SELECTED OFF AND AIRCRAFT BATTERIES ARE ON. RIGHT EMERGENCY EXIT ROW 1 AND EXIT CENTER AISLE AND CEILING LIGHT FORWARD. REPLACED BATTERY BASE AND POWER SUPPLY. 2H72 4T RTA13NM 20030722000512003072200051NM 2003 7 22 SWAA031509 120030707A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030722000582003072200058GL 2003 7 22 SWAA031498 220030707A7200CFM56 ENGINE BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563B1US GL NR 1 FAILED A SWAAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW29646SW 28331 724703 IN FLIGHT SHUTDOWN, DECLARED EMERGENCY, ONE HOUR INTO FLIGHT NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030722000622003072200062NM 2003 7 22 SWAA031511 120030707A57546573714 SKIN BOEING737 7373H4 1384600NM NR 5 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT CRACKED ON LOWER SKIN AT AFT RIVET ROW. REPAIRED NR 5 L/E SLAT PER SWA EA. 2L72 4F RTA16WE 20030722000732003072200073NM 2003 7 22 SWAA031441 120030627A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGING AT BS 500 + 10, STR 28R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030722000762003072200076EU 2003 7 22 MALA030334 120030620A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15526XJ E2351 DURING C-CHECK INSPECTION IN CVG, NR 2 SEAT RAIL CORRODED BEYOND LIMITS. FLOOR FRAME 20 TO I/B. MAINTENANCE REPLACED SECTION OF RAIL IAW EO A53026. REFER 409 NR 127854 FOR DETAIL. A/C RELEASE DATE 7/1/2003. 2H74 4F RTA49EU 20030722000802003072200080NE 2003 7 22 MALA030340 220030712A7320229333010 HMU BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 1 ENGINE MALFUNCTIONED A MALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL15518XJ E2337 DURING FLIGHT 3541, NR 1 ENGINE OVERSPEED DURING CLIMBOUT FROM TYS ENGINE OVERSPEED LIGHT CAME ON 9 PSI OIL PRESSURE ALL NR 1 GAUGES DROPPED OFF TO WINDMILLING. ENGINE WAS QRH, AND SHUTDOWN. MAINTENANCE REMOVED AND REPLACED HMA P/N 2-293-330-10 S/N ON 3AGU152, S/N OFF 96AGU414C. ALL CHECKS GOOD. ALSO REMOVED AND REPLACED OVERSPEED CONTROLLER ALL CHECKS GOOD SEE BLOW AND JC 7310-502 FOR DETAIL. 2H74 4F4 FRTA49EU E6NE 20030722000842003072200084EU 2003 7 22 MALA030333 120030620A5260 HAND RAIL BAC 146 AVRO146RJ85A1500097EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15526XJ E2351 DURING C-CHECK INSPECTION IN CVG, O/B AIRSTAIR RAIL IS CORRODED BEYOND LIMITS. MAINTENANCE REPLACED RAIL IAW SRM 51-43-00. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-11. DRILLED AND COUNTER SUNK AIRSTAIR RAIL IAW SRM 51-42-00 AND 51-43-00. REFER TO 409 NR 127856 FOR DETAIL. A/C RELEASE DATE 7/1/2003. 2H74 4F RTA49EU 20030722000942003072200094NM 2003 7 22 SWAA031443 120030630A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, BETWEEN STR 2L AND 3R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030722000962003072200096 2003 7 22 SWAA031445 420030629A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030722001052003072200105NM 2003 7 22 SWAA031478 120030702A33501062048 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030722000202003072200020NM 2003 7 22 2003F00448 120030310A5754 PLATE BOEING727 727222 1384073NM NR 6 SLAT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT NR 6 SLAT LOWER BACKSIDE ACTUATOR ROD END ACCESS CUTOUT SUPPORT PLATE. REMOVED DAMAGED PLATE FROM RIGHT WING NR 6 SLATE LOWER BACKSIDE SLAT ACTUATOR ROD END ACCESS CUT OUT. FABRICATED PLATE. TREATED AND PRIMED PART AND AREA. INSTALLED PLATE. (M) 2L73 4F A3WE 20030418001562003041800156EA 2003 4 18 QXEA0300288 120030217A2120 SMOKE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09601QX 10009 BIL-ON FLIGHT NUMBER 2483-SUPP, DURING TAXI OUT, SMOKE AFT LAV WARNING LIGHT CAME ON. SMOKE COULD BE SEEN AND SMELLED IN CABIN. PERFORMED GROUND RUN, NO ODOR NOTED. LAVATORY DETECTOR DID NOT GO OFF. OPERATED RT PACK, NO CAUTION MESSAGE NOTED. COMPLIED WITH OPERATIONAL CHECK OF AIR CONDITION SYSTEM, OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030421000142003042100014EU 2003 4 21 IXXA0300016O 220030220A72613015720330 LUBRICATION UNIT DOUG DC8 DC873F 302199FWP CFMINTCFM56 CFM563C1 13802EU NR 2 ENGINE FAULTY A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11606AL892981670 46044 AFTER DEPARTURE FROM PDX DURING CRUISE EN ROUTE TO EWR CREW NOTED OIL PRESSURE INDICATION FLUCTUATING ON THE NR 2 ENGINE. POWER WAS RETARDED, OIL PRESSURE WARNING ILLUMINATED AND NR 2 ENGINE WAS SHUTDOWN. CREW ELECTED TO CONTINUE TO TOL AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MAINTENANCE FOUND A DEFECTIVE LUBE UNIT. THIS COMPONENT WAS REPLACED AND A GOOD OPERATIONAL CHECK WAS COMPLETED. ALL MAINTENANCE PERFORMED IAW APPLICABLE MANUALS AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20030421000302003042100030NE 2003 4 21 VNAA0302019 220030222A7320 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07439JS 3057 DURING TAKEOFF, THE CREW RECEIVED A LT ENGINE CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE ENGINE CONTROL UNIT CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421000692003042100069EA 2003 4 21 SWIA200311818 120030301A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB FAILED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07499SW3846 3846 7398 STAB CH 1 WILL ENGAGE BUT DISCONNECTS WHEN THE TRIM SWITCH IS ACTIVATED. REMOVED AND REPLACED MOTOR CONTROL AND TRIM ACTUATOR. OPS CHECKED GOOD. P/N: 7062-3, S/N OFF: 138, S/N ON: 777. 2L72 4F RTA21EA 20030421000922003042100092NM 2003 4 21 DL76S030137 120030208A5280113T80002 DOOR BOEING767 767332 1382001NM NR 2 NACELLE DAMAGED A DALAO OTHER D INFLIGHT SEPARATION APAPPROACH 1 SO27128DL 24078 ON APPROACH INTO SJU RT SHOCK STRUT DOOR FELL OFF. DOOR WAS RECOVERED IN A HOUSE CARPORT, NO PERSONAL INJURIES. UPON INSPECTION FOUND TWO HYD BRAKE LINES DAMAGED. ALSO, THE TRUNNION DOOR WAS DAMAGED. REMOVED SAME, REPLACED DOOR. REPAIRED OTHER DAMAGE. 2L72 4F RTA1NM 20030421000982003042100098NM 2003 4 21 DLM88030160 120030217A2420 CSD DOUG MD88 MD88 3023688NM GENERATOR MALFUNCTIONED A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO27972DL 53215 ON TAXI LT GENERATOR TRIPPED AND AC X-TIE LOCKOUT MSG ILLUM. RESET NG. STARTED APU TO PWR THE LT BUS AFTER RESETTING X-TIE. AT 125 KTS RT GENERATOR OFF AND X-TIE MSG RESET GEN, NO HELP. THE RT BUSS WAS DEAD. RT GEN VOLTS AND FREQS ZERO. REPLACED BOTH GENERATORS AND LEFT CSD. ALSO, REPLACED X-TIE RELAY. 2L72 4F RTA6WE 20030421001002003042100100NM 2003 4 21 DLM88030164 120030220A3397 WIRE DOUG MD88 MD88 3023688NM AFT AIRSTAIR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27905DE 53410 AFT CABIN EMERGENCY LIGHTS INOP. REPAIRED WIRING AT AFT AIRSTAIR FWD LIGHT. 2L72 4F RTA6WE 20030421001022003042100102NM 2003 4 21 DL76L030172 120030221A3320 BALLAST BOEING767 767332 1382001NM CABIN ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27182DN 25987 FLIGHT ATTENDANTS SMELLED AN ELECTRICAL ODOR NEAR ROW 21. CHECKED OVERHEAD FOR LIGHT BALLASTS. CHECKED MOVIE PROJECTOR CHECKED SEBS. UNABLE TO SMELL ELECTRICAL ODOR. OK FOR SERVICE. 2L72 4F RTA1NM 20030421001052003042100105NE 2003 4 21 DL76L030179 220030222A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 SURGES A DALAK NONE O OTHER ININSP/MAINT 1 SO27179DN42133 25144 724681 DURING GROUND ENGINE RUN BY MTC, ENGINE SURGED AT ABOUT 1.32 EPR. REPLACING NR 2 ENGINE. 2L72 4F4 FRTA1NM E24NE 20030421001072003042100107NM 2003 4 21 DL76L030195 120030225A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27179DN 25144 ON DEPARTURE FROM ATL CREW SMELLED SMOKE AND RETURNED TO ATL. INSPECTED AIRCRAFT. CHECKED GALLEYS AND RAN ENGINES. UNABLE TO DUPLICATE. 2L72 4F RTA1NM 20030421001112003042100111 2003 4 21 DL76S030209 420030303A2320285T002225 PANEL BOEING767 767332 1382001NM COCKPIT FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27134DL 25123 WHILE AT THE GATE SMOKE AND ODOR STARTED COMING FROM NR 2 COMM PANEL. REPLACED SAME. 2L72 4F RTA1NM 20030421001222003042100122EA 2003 4 21 QXEA0300318 120030227A26124462534 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 INOPERATIVE A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09601QX211 211 10009 SEA ON FLIGHT 2485- MASTER WARNING SMOKE AFT LAVATORY COMES ON INTERMITTENTLY. REMOVED AND REPLACED AFT LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030421001242003042100124NM 2003 4 21 UPS03240253 120030303A5753 STRUCTURE BOEING727 72731C 1384011NM LT TE FLAP GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE: ASV, LEFT O/B TRAILING EDGE FLAP HAS A GOUGE AT LEADING EDGE O/B ATTACH POINT (I/B OF ATTACH POINT). INSTALLED REPAIR DOUBLER PER SRM 57-50-4 FIG 9. REMOVED AND REINSTALLED LEFT O/B TRAILING EDGE AFT FLAP TO FACILITATE REPAIR IAW MM 27-51-12. 2L73 4F A3WE 20030421001282003042100128NM 2003 4 21 VNAA0303005 120030304A3150870004MODB PSEU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AIR DOOR FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07422JS17356465 3018 DURING CLIMBOUT, THE CREW REPORTED A PROXI SYSTEM FAIL FOR THE GROUND AIR DOOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421001642003042100164WP 2003 4 21 2003F00223 220030201A726131080811 LINE FRCHLDSA227 SA227DC 3377521SW GARRTTTPE331TPE33112UHR WP ENGINE OIL CRACKED A BSAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM051119K DC830B FLT 2580 - BIL - DURING DESCENT, CREW OBSERVED THE LEFT ENGINE OIL PRESSURE LIGHT CAME ON, THIS WAS VERIFIED BY LEFT OIL PRESSURE INDICATION LOW, CREW THEN SHUT DOWN LEFT ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. OIL LEAK IN PROP GOVERNOR AREA. REPLACED LINE AND RE-ALIGNED PROP GOVERNOR REVERSE LOCK OUT 90 DEGREE ELBOW FITTING. FOUND END OF LINE TO BE STRESSED FORM THE JAM NUT BEING TIGHTENED AND BENDING THE LINE JUST AFT OF THE B-NUT FERRULE. (M) 2L72 4T4 TRTA18SW E4WE 20030421001692003042100169WP 2003 4 21 2003F00221 220030206A726131080811 LINE FRCHLDSA227 SA227DC 3377521SW GARRTTTPE331TPE33112UHR WP ENGINE OIL LEAKING A BSAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM051119K DC830B MWH - FLT 2569 - LEFT ENGINE OIL PRESSURE LIGHT CAME ON DURING CLIMB AT 18K MSL. CREW VERIFIED READING WITH OIL PRESSUE GAGE, WHICH READ 0 PSI. CREW SHUT DOWN LEFT ENGINE AT THAT TIME. LOST OIL PRESSURE DUE TO OIL LEAK. REMOVED LINE, LOOSENED ALL ATTACHING LINES TO RELIEVE ANY STRESS AT ANY CONNECTION, INSTALLED LINE, AND RETIGHTENED ALL LINES TO PREVENT STRESS AT ANY CONNECTION. GROUND RUN AND LEAK AND OPS CHECK GOOD. (M) 2L72 4T4 TRTA18SW E4WE 20030421001752003042100175WP 2003 4 21 GTIA030126 120030223A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CABIN STATION 160 TO STATION 148 RBL 8 INCHES TO 17 INCHES FLOOR PANEL SOFT/MUSHY INSERTS CORRODED/BROKEN OUT. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20030421001812003042100181NE 2003 4 21 MEX2003063 220030309A7230 BLADE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NR 1 ENGINE DAMAGED A ASMFK NONE O OTHER ININSP/MAINT 1 SW23838AM 49397 FLT 911 - MTY-MEX - DURING MAINTENANCE INSPECTION, DETECTED A FAN BLADE OF ENGINE NR 1 WITH DAMAGE. THE INSPECTOR VERIFIED THE BLADE AND WAS OUT OF LIMITS. THE TECHNICIAN BLENDED THE BLADE IAW MM 72-00-00, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E2EA 20030421001832003042100183NM 2003 4 21 HALA0300105 120030306A27507321855013 CONTROL VALVE BOEING767 767300 1385204NM TE FLAPS DAMAGED A HALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 WP13592HA 33468 FLT 20 - SMF - FLAPS APPEAR TO BE BINDING/CHATTERING BETWEEN FLAP SETTING 20 AND 30. BINDING OCCURS AT THE END OF TRAVEL FOR EACH SETTING AT 20/25/30. EVALUATION FLIGHT REQUIRED. REMOVED AND REPLACED TRAILING EDGE FLAP POWER DRIVE UNIT HYDRAULIC MOTOR CONDITION. REMOVED AND REPLACED TRAILING FLAP PDU CONTROL VALVE MODULE AND BYPASS VALVE MM 27-51-32. LEAK CHECK OF CONTROL VALVE MODULE GOOD. PERFORMED FLAP AND SLAT PRIMARY DRIVE AND POSITION INDICATION SYSTEM TEST PER MM SUBTASK 27-51-00-865-111. CHECKS OK AT THIS TIME. NO OTHER DISCREPANCIES NOTED. EVALUATION FLIGHT CHECK GOOD. FLAP OPERATION NORMAL. (M) 2L72 4F RTA1NM 20030421001942003042100194WP 2003 4 21 GTIA030129 120030221A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FWD CABIN DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CABIN STATION 200-160 FLOOR PANEL SOFT/MUSHY CORRODED INSERTS, 12 BY 40. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030418000212003041800021NM 2003 4 18 PCAA0302042 120030213A3260 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM MLG MALFUNCTIONED A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13849EX 337 LT MAIN GEAR GREEN LIGHT DID NOT ILLUM & LT MAIN RED LIGHT REMAINED ILLUM. ALT EXTENSION LIGHT CHECKED & FOUND GEAR WAS NOT EXTENDED. ALT EXTENSION DOOR CLOSED, & RECEIVED GREEN LIGHT ON GEAR. RE CHECKED ALT GEAR LIGHT & HAD 3 GREEN. MX JACKED ACFT IN HANGAR & RAN GEAR UP & DOWN SEVERAL TIMES. NO FAILURES FOUND. LT SEQUENCE VALVE & SOLENOID VALVE REPLACED. GEAR RAN UP & DOWN, NO FAILURES. OPS & LEAK CHECK GOOD. NR 2 HYD SYS IN NOSE WW BLED. CHECKED NR 1 MAIN LANDING GEAR AUXILIARY & MAIN ACTUATOR LINES FOR SIGNS OF AIR. NO AIR FOUND. PERFORMED PSEU SYS TEST & FOUND FAULT CODE 55. RE RACKED PSEU & PERFORMED SYS TEST TWICE, NO FAULTS. INSPECTED MLG ACTUATOR ASSEMBLIES & LUBED FITTINGS. 2H72 4T RTA13NM 20030418000732003041800073NM 2003 4 18 QXEA0300283 120030210A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - CHAFING DAMAGE ON PANEL 262HT. REPAIRED IAW HORIZON AIR EA 6-53-196. 2H72 4T RTA13NM 20030418001022003041800102WP 2003 4 18 UPS03840205 120030201A532056449721 FITTING DOUG DC8 DC873F 302199FWP STGR 408 #1 ALT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, NR 1 ALT FUEL TANK STR 59 STA 408 END FITTING CRACKED INSIDE PNL 505B. REMOVED CRACKED FITTING PER DC8 SRM 51-1-20D. DRILLED, LOCATED AND DEBURRED NEW END FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20030421000292003042100029NM 2003 4 21 VNAA0302018 120030219A5210 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DOOR FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07431JS 3028 DURING CLIMB OUT FROM DCA, THE CREW RECEIVED A MAIN CABIN DOOR OPEN INDICATION ON THE RED WARNING PANEL. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND LANDED AT THE NEAREST SUITABLE AIRPORT, DCA. MAINTENANCE PRESSURIZED THE AIRCRAFT AND THE MESSAGE FLICKED REPEATEDLY DURING THE INSPECTION. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE AT DAY INSPECTED AND REPLACED THE PASSENGER DOOR LINK ROD IN ACCORDANCE WITH DORNIER SI 328-52-077. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421000352003042100035NE 2003 4 21 MALA030180 220030224A72002003204015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 1 SEIZED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL15526XJ E2351 DURING FLIGHT 3595, NR 1 ENGINE SHUT DOWN JUST AFTER TAKEOFF. NR 1 ENGINE FAILED ON CLIMBOUT, ENGINE VIBRATION LIGHT ILLUMINATED FOR 2 SECONDS. EFT HIT MAX OF ABOUT 718 DEGREES CELSIUS. VAW VERY ERRATIC, OIL INDICATIONS APPEARED NORMAL. N2 AND N1 APPEARED TO WINDMILL IN ON FINAL. FABEC 1 FAULT LIGHT ILLUMINATED. CREW INITIATED THE ENGINE SHUTDOWN. AIR RETURN TO DTW. MAINTENANCE INSPECTED NR 1 ENGINE, FOUND TO BE SIEZED. INSPECTED A/C AND FOUND SAFE FOR ONE TIME FERRY FLIGHT FROM DTW TO MSP. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE IAW MESABA ENGINE CHANGE TASK CARDS. P/N ON/OFF 2-0032-040-15 S/N ON PO7865 S/N OFF PO7799. 2H74 4F4 FRTA49EU E6NE 20030421000542003042100054NM 2003 4 21 UPS03640234 120030224A7100 ENGINE BOEING767 76734AF 1385212NM GE CF6 CF6* 30020GL LEFT STALLED A IPXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01329UP 27755 704902 INSPECTION TYPE: ETOP, SUSPECTED COMPRESSOR STALL LT ENGINE. VIBRATION INCREASED TO 4.4, ALL OTHER PARAMETERS NORMAL. REPLACED LT ENGINE, OPS CHECK NORMAL IAW MAINT FUNCTION TC6002. 2L72 4F4 FRTA1NM E23EA 20030421000762003042100076NM 2003 4 21 DL78K030072 120030117A3610365701065 THERMOSTAT BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 2 ENGINE LEAKING A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO273735D 30381 876655 ON TAKEOFF RIGHT DUCT PRESSURE DROPS TO 10 PSI. REPLACED 450 DEGREE THERMOSTAT. 2L72 4F4 FRTA16WE E00055EN 20030421000832003042100083NE 2003 4 21 DLM88030097 220030127A7320 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 MALFUNCTIONED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27923DL31236 49705 725779 THE ENG ABOUT 8 TO 10 SECA FOR WARM UP, ON T/O ROLL ENG WOULD NOT ACCELERATE PAST IDLE. GAVE THE ENG 6 SECS WITH THROTTLES UP TO RESPOND. ABORTED T/O ROLL AROUND 80 KT. RT ENG, NR 2. PERFORMED CHECK OUT OF RT ENG PER PFHB. OPS CHECK NORMAL. OK FOR SERVICE. 2L72 4F4 FRTA6WE E9NE 20030421001182003042100118NM 2003 4 21 QXEA0300311 120030301A326082450203503 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM ZONE 700 DAMAGED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09412QX2032 4059 SEA-DEPARTING FROM BZN. RETRACTED LANDING GEAR. LT MAIN GEAR UNSAFE AND LT GEAR DOOR LIGHT REMAINED ILLUMINATED. GEAR HANDLE REMAINED ILLUMINATED. CYCLED PER CHECKLIST. ALL LIGHTS WENT OUT. TO INCLUDE RIGHT GEAR UNSAFE AND GEAR DOOR ON INTERMITTENTLY. REMOVED AND REPLACED NR 1 MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR HARNESS. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030826001722003082600172SO 2003 8 26 SWIA200312132 120030621A3350 FUSE EMB 120 EMB120ER 3260203SO CABIN BLOWN A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07189SW 120048 EMERGENCY LIGHTS OUT ON LEFT SIDE OF CABIN FROM ROW 3-6.REMOVED AND REPLACED MID ELBP FUSE. OPS CHECK GOOD. 2L72 4T RTA31SO 20030827000052003082700005EU 2003 8 27 03FDEA00957 120030623A5320F5358970920000 RETAINER AIRBUS300 A300F4605R 3930327EU APU BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 NR 768 APU COMPT DOOR SILL SEAL RETAINERS ARE CRACKED. REMOVED AND REPLACED 4 EA RETAINERS IAW A300-600 SRM 51-40-00. 2L72 4F RTA35EU 20030827000262003082700026NM 2003 8 27 03FDEA00903 120030618A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 N00586 CORROSION (C53-113-01) FWD CARGO STA 720B LBL 2 ON FRAME SHEAR TIE. CORROSION ON FWD CARGO STA 720B, LBL 2, SHEAR TIE WAS FOUND OUT OF LIMITS. REMOVED AND REPAIRED ACTUATOR PANEL AND SPLITER TO ACCESS. REMOVED DAMAGED SHEAR TIE. FABRICATED REPAIR PARTS AND INSTALLED. REINSTALLED REPAIRED ACTUATOR PANEL AND SPLITER IAW SRM 51-30-2, 53-10-4. 2L73 4F RTA3WE 20030827000832003082700083SO 2003 8 27 C2XA03BT074 120030715A261214534610401 SWITCH EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714923 145318 EWR---CO3289, FOUND BAGGAGE FIRE EXTINGUISHER WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED BAGGAGE FIRE TEST SWITCH. OPS. CHECKED SYSTEM GOOD. IAW EMB145 MM NR20-13-04. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030827000932003082700093SO 2003 8 27 C2XA03SH251 120030803A531112010732001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV-DURING C CHECK FRAME 81 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01246. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030827001212003082700121NM 2003 8 27 CALA0300365 120030707A551469731201 HINGE PIN BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717644 28905 INSPECTION FOUND EXTERIOR OF INNER PIN AND BORE OF OUTER HINGE PIN FOR HORIZONTAL STABILIZER CORRODED. THE INNER PIN AND OUTER HINGE PIN ASSEMBLY WERE REMOVED AND REPLACED IAW EA 5550-01315 AND MM 27-41-31. 2L72 4F RTA16WE 20030827001512003082700151NM 2003 8 27 2003UALA00581 120030722A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29381UA 24656 2.75 INCH LONG CRACK FOUND AROUND STATION 887 RT 15 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030827001542003082700154NM 2003 8 27 2003UALA00545 120030708A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 FASTENER HOLES CORRODED AT SEAT TRACK FLANGE BS 830-862, RBL 34 COMMON TO FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030827001722003082700172SO 2003 8 27 C2XA03CL149 120030824A335078241 INVERTER EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714522 145383 CLE FLIGHT NR 2138 THE CREW REPORTED THE NR 2 AND NR 3 EMERGENCY LIGHTS DID NOT WORK. MAINTENANCE REPLACED THE NR 3 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030827001742003082700174SO 2003 8 27 C2XA03CL147 120030817A33503025103 HOUSING EMB 145 EMB145ER 3260211SO EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936 145025 DURING ROUTINE MAINTENANCE THE NR 1 EMERGENCY LIGHT WAS INOPERATIVE ON WING TO FUSELAGE PANEL. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT HOUSING ASSEMBLY IAW 33-51-10.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030827001782003082700178SO 2003 8 27 C2XA03CL138 120030807A3350 SIGN EMB 145 EMB145ER 3260211SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715941 145035 SDF FLIGHT NR 2135 THE CREW REPORTED THE OVERHEAD EMERGENCY LIGHT EXIT SIGN OVER THE EXIT ROW FAILED TO TEST. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030826000072003082600007WP 2003 8 26 03FDEA01356 120030821A78309019M20P06 TRACK DOUG DC10 DC1010 3022110WP THRUST REVERSER GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 COMPLY WITH EA 8-7832-72262 EXHAUST-THRUST REV- GOUGE REPAIR LOWER TEE TRACK P/N 9019M20P06 ENT BY: 497234 RPT BY: 497234 FACT 19AUG03 13:13 BFM R COMPLIED WITH EA 8-7832-72262 EXHAUST- THRUST REV- GOUGE REPAIR LOWER TEE TRACK P/N 9019M20PO6 ENT BY: 497191 RPT BY: 497191. 2L73 4F A22WE 20030826000862003082600086EU 2003 8 26 YENA200309 120030609A5230 DOOR AIRBUS320 A320232 3930326EU CARGO BAY FOD A YENAO OTHER O OTHER CRCRUISE 1 EA15505JB 1173 A/C DIVERTED TO FLL DUE RIGHT AFT DOOR MAKING LOUD HUMMING SOUND LIKE VACUUM. PERFORMED DETAILED VISUAL INSPECTION OF RT AFT DOOR SEAL, NO DAMAGE FOUND. CLEANED SEAL IAW 52-13-00. THE CONDITION REPEATED NEXT FLIGHT. REMOVED FOD FROM BULK CARGO DOOR, INSPECTED R2 DOOR AREA. PERFORMED PRESSURIZATION CHECK ON GROUND. OPS CHECK GOOD IAW MM 21-33-00. NO DEFECT NOTED. 2L72 4F RTA28NM 20030826001032003082600103CE 2003 8 26 CGO2003F00008 120030521A1430MS2001231M BOLT BEECH 36 A36 1151604CE CONT O550 IO550* SO RT WING CRACKED B CGORK NONE O OTHER ININSP/MAINT 1 GL0348GE E3215 BOLT MAGNAFLUX INSP FOR ROUTINE 5-YEAR INSPECTION IAW MM. BOLT RETURNED AS UNAIRWORTHY DUE TO POSSIBLE CRACK INDICATION IN RADIUS UNDER BOLT HEAD. BOLT WAS INSTALLED NEW AT AIRCRAFT MFG IN RIGHT WING LOWER FORWARD POSITION. MAY POSSIBLY BE DUE TO MFG SURFACE DEFECT, WOULD REQUIRE PLATING REMOVAL AND FURTHER ENGINEERING INVESTIGATION TO CONFIRM IF ACTUAL DEFECT PRESENT. REPLACED BOLT WITH NEW RAPID-SUPPLIED BOLT. 1L71 3O3 O 3A15 E3SO 20030826001122003082600112NM 2003 8 26 S03430032 120030609A3040 TERMINAL BOEING747 747400 NM PWA 4056 PW4056 NE WINDSHIELD OVERHEATED W SAJFH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP03 29906 B-18209 DURING FLIGHT FROM LAX TO TPE, LT NR 1 WINDSHIELD WAS NOTICED SMOKE AND SCORCHING SMELL EIGHT HOURS AFTER TAKE-OFF. THE ABNORMALITY DISAPPEARED AFTER SWITCHED OFF LT WINDOW HEAT FUNCTION. CHECK FOUND LT NR 1 WINDSHIELD LOWER BUS BAR HEAT TERMINAL OVERHEATED. ACCORDINGLY, THE TERMINAL WAS REPLACED. AFTER REPLACED THE TERMINAL,THE WINDOW HEAT FUNCTION TEST NORMAL IAW AMM. REPORTED THE SERVICE DIFFICULTY TO MFG, AND WAITING FOR MFG RESPONSE AND RECOMMENDATION. 2L74 4F4 FRTA20WE E24NE 20030421001332003042100133NM 2003 4 21 VNAA0302026 120030227A3060 BRUSH BLOCK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT PROP HEAT FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07426JS 3038 DURING CRUISE, THE RIGHT HAND PROP HEAT FAILED. DUE TO LIGHT SNOW AT THE DESTINATION, FLIGHT 4050 DIVERTED TO DAY. MAINTENANCE INSPECTED AND FOUND THE BRUSHBLOCK TO BE OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE BRUSHBLOCK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421001382003042100138CE 2003 4 21 NSVA200300017 120030303A14301016100195 RIVET BEECH 1900 1900D 1154162CE TORQUE TUBE LOOSE A NSVAK NONE O OTHER ININSP/MAINT 1 EA27155CJ UE55 DURING ACCOMPLISHMENT OF NR 6 DETAILED INSPECTION FOUND THE LT ELEVATOR TORQUE TUBE RIVETS WORKING CAUSING EXCESSIVE PLAY AT ELEVATOR TRAILING EDGE. THE ELEVATOR WAS REMOVED AND THE TORQUE TUBE REPLACED. ELEVATOR REINSTALLED PER ALL MAINTENANCE MANUAL INSTRUCTIONS. 2L72 4T RTA24CE 20030421001662003042100166NM 2003 4 21 BJNA03031 120030301A5320 WEB BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN AFT OVERHEAD WEB LOCATED AT FS 994 LBL 50. REMOVED THE L2 DOOR THRESHOLD DRAIN PAN FOR ACCESS TO CORRODED SECTION OF WEB, CORROSION ALSO EXTENDED TO THE INBOARD CHORD. REMOVED THE CORRODED SECTION OF WEB AND CHORD. FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING 737 SRM 51-10-1 PAGE 8, 51-21-1 FIGURES 3 AND 7, 51-10-2, AND 51-30-2. (M) 2L72 4F RTA16WE 20030421001982003042100198NM 2003 4 21 AMTA200300357 120030316A3397 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 EGRESS LIGHTS BETWEEN ROWS 22-23, INOPERATIVE. SECURED LOOSE CONNECTION AT ROW 22. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030421002112003042100211 2003 4 21 AMTA200300105 420030117A2565 RING BOEING757 75723N 1384973NM ESCAPE SLIDE DETACHED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 FOUND 2L DOOR DIFFICULT TO ARM. REMOVED SURVIVAL KIT D RING FROM GIRT BAR ASSEMBLY AND REATTACHED THE VELCRO END OF THE D-RING TO THE SLIDE THIS IS ITS NORMAL STOWED POSITION. (M) 2L72 4F RTA2NM 20030421002172003042100217EA 2003 4 21 ASOA03109 120030313A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A ASOAO OTHER N FALSE WARNING APAPPROACH 1 SO11847AS 7335 FLT 4708 - DURING APPROACH INTO YUL FROM ATL, THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE CREW COMPLIED WITH QRH PROCEDURES, DECLARED AN EMERGENCY AND REQUESTED EMERGENCY EQUIPMENT. THE AIRCRAFT LANDED SAFELY IN YUL. MAINTENANCE COMPLIED WITH AD 98-20-01, PERFORMED A FLAPS INSPECTION AND RESET THE SYSTEM WITH NO DEFECTS FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000062003042200006EA 2003 4 22 ASOA03112 120030315A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 FLT 4611 - DURING A GROUND INSPECTION IN DFW, THE NR 5 EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 5 EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000142003042200014EA 2003 4 22 ASOA03086 120030301A3350111RJ7001 TAPE CNDAIRCL600 CL6002C10 1390015EA CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11703EV 10038 FLT 4423 - DURING A GROUND INSPECTION AT ATL, THE FLOOR EMERGENCY LIGHT STRIP BY THE GALLEY WAS FOUND TO BE MISSING. MAINTENANCE INSTALLED THE FLOOR EMERGENCY PHOTOLUMINESCENT TAPE BY THE GALLEY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000202003042200020CE 2003 4 22 2003F00231 120030204A27403G5212B TRANSMITTER CESSNA750 750 2076810CE VERTICAL STAB MALFUNCTIONED A UG8AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL235114 7500017 ON PREFLIGHT PRETEST SECONDARY TRIM FAILED SEVERAL TIMES IN THE NOSE UP DIRECTION. MOVEMENT STOPPED AND AMBER CAS 'SEC TRIM FALL' ILLUMINATED. REPLACED FAULTY STABILIZER POSITION TRANSMITTER. RIGGED AND TESTED PER CESSNA MM. OPERATIONAL CHECK IS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030422000362003042200036EU 2003 4 22 ASOA03079 120030224A3397M2275941249 WIRE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY LIGHT ON THE AIRSTAIR DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A CORRODED WIRE ON THE AIRSTAIR DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030422000542003042200054WP 2003 4 22 BMAC030006S 220030215A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP LEFT MALFUNCTIONED A B16AO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NE05538PA 751 BWI - FLT 3103 - PILOT REPORTED LEFT ENGINE PRODUCES FULL POWER WHEN POWER LEVER IS AT STOP. RIGHT POWER LEVER AT STOP PRODUCES 92 PERCENT TORQUE, 530 DEGREES EGT AT 6,000 FEET, TEMP FOR ALT AND TEMP IS 560C. MAINTENANCE FOUND AIRCRAFT FUEL TANKS TO BE CONTAMINATED WITH WATER. REMOVED WATER CONTAMINATION IAW AMM 28-10-00. PERFORMED ENGINE RUNS IAW GMM 71-00-00. CHECKS NORMAL AT THIS TIME. FINAL FIX, REPLACED RIGHT STRAIN GUAGE AND TORQUE SIGNAL CONDITIONER. REPLACED LEFT STRAIN GAUGE, TTL COMPUTER AND BUFFER ASSY, TORQUE SIGNAL. BOTH SIDES TESTED GOOD ON THE GROUND AND GOOD ON APPROX TWO HOUR FLIGHT CHECK. AIRCRAFT RETURNED TO SERVICE ON 2/27/2003. (M) 2L72 4T4 TRTA21EU E4WE 20030422000582003042200058NM 2003 4 22 MEX2003088 120030321A4900 APU BOEING757 757200 1384950NM FAILED A ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23703AM 27203 MEX-ORD - AIRCRAFT RETURNED TO PLATFORM DUE TO AIRCRAFT POWER UNIT FAILED WITHOUT APPARENT CAUSE. PERFORMED BITE PROCEDURE IAW FIM 49-11-00. (M) 2L72 4F RTA2NM 20030422000602003042200060EA 2003 4 22 SIMA200305001 120030215A3230533405 CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA HYDRAULIC BAY INOPERATIVE A SIMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW21505AE 10053 DFW - FLT 3842 - CREW REPORTED WHEN PASSING OVER THE OUTER MARKER, GEAR WAS SELECTED DOWN BUT REMAINED UP AND LOCKED. LANDING GEAR WAS MANUALLY EXTENDED AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE IAW CRJ MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030422000622003042200062SO 2003 4 22 SIMA200304102 120030201A531514522463001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 DURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGE AREA TO COMPLETELY REMOVE THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REPAIR AREA. FABRICATED A U-SHAPED DOUBLER. REPAIR DONE IAW EMB145 SRM (145/1142 REV 20) 53-21-0 FIG 207 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030422000712003042200071SO 2003 4 22 SIMA200302203 120030118A5330 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21653AE 145433 ABI - DURING A MBV INSPECTION, TWO DENTS WERE FOND BETWEEN SKIN JUNCTION 07 AND FRAME 77, STRINGER 18R AND 19R. REMOVED BOTH DENTS WITH SINGLE CUTOUT. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-32-01, TYPE A, FIG 201 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030826001172003082600117EU 2003 8 26 NSVA20030026 120030524A335030718PEGPL LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A NSVAK NONE L NO TEST ININSP/MAINT 1 EA27294CJ 340B294 DURING ROUTINE MAINTENANCE FOUND 3 EMERGENCY PATH LIGHTS INOPERATIVE. MECHANIC REPLACED 3 BULBS OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 20030826001612003082600161EU 2003 8 26 SIMA200321810 120030804A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21375AE 340B375 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSIATED THE APPLICATION OF A REPAIR DOUBLER TO THE UPPER FUSELAGE SKIN BETWEEN FRAME STATIONS 258, 272 AND STRINGERS 1603, 1604 TO COVER TWO DENTS. REMOVED BOTH DENTS BY CREATING A CUTOUT. FBRICATED A DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS005824 PARA 1.3.4 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20030826001652003082600165WP 2003 8 26 MEX2003322 120030703A3241 CONNECTOR DOUG DC9 DC987 3022087WP ANTI-SKID SYS LOOSE A ASMFD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 SW23751RA 49779 MEX-MTY - FLT 920 - AIRCRAFT RETURNED TO PLATFORM, BOTH ANTI-SKID LIGHTS CAME ON. DURING REVISION, DETECTED THE INTERIOR LEFT CONNECTOR VALVE LOOSE. THE WIRING WAS CHECKED AND CONNECTOR WAS CLEANED AND RECONNECTED IAW 32-43-00, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030827000102003082700010NM 2003 8 27 03FDEA00838 120030523A5744ARC0503504 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0750: RT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP-HINGE FWD FITTING FOUND INBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0750: REPAIR CARRIED-OUT IAW CMM 57-44-09 AND EA 1-5740-71708 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030827000122003082700012NM 2003 8 27 03FDEA00835 120030523A5744ARC0502505 HINGE FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0767: LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FWD FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR'S UPPER LT AND RT MOUNT HOLES WITH CORROSION (WING SIDE FITTING). SNRM N0767: REPAIR CARRIED-OUT IAW CMM 57-44-08 AND EA 1-5740-71706 WINGS - LEFT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030827000182003082700018NM 2003 8 27 03FDEA00942 120030621A2780 FLAP BOEING727 727100 1384036NM WINGS MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25185FE 18871 NR 4 LEADING EDGE FLAP WOULD NOT RETRACT WHEN WE MOVED FROM FLAP 5 TO 2 WHILE INFLIGHT. INSTALLED JUMPER CABLE ON NR 4 L/E FLAP. UPON INSP FOUND NR 4 LE FLAP LIGHT ON AT S/O'S. PANEL WHEN NR 4 LE FLAP FULLY RETRACTED. INSTALLED ADAPTER CABLE ON NR 4 LE FLAP INDICATION SWITCH IAW MM CH 27-82-000-1. ALL LEADING EDGE FLAP AND SLATS OPS CK NORM IAW MM 27-81-000-0. REMOVED ADAPTER CABLE FROM NR 4 LEADING EDGE FLAP SWITCH, CLEANED ALL CONNECTIONS, PREFORMED OPS CHECK OF FLAP/SLAT SYSTEM IAW M.M. 27-82-001-4. ALL INDICATIONS NORMAL. 2L73 4F RTA3WE 20030827000452003082700045SW 2003 8 27 ALG2003F00060 120030501A6730206076031021 SERVO BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FLIGHT CINTROL INOPERATIVE A ALGAO OTHER F FLT CONT AFFECTED LDLANDING 1 SW035011F14784 2564 DURING LANDING THE PILOT FELT THE BINDING FORCE FROM THE CYCLIC, UPON LANDING THE PILOT FOUND THE TOP CASTLE NUT OF THE LEFT SERVO FROZEN WHICH PRODUCED BINDING, THE MECHANIC REMOVED THE SERVO BOLT AND NUT, CLEANED AND REINSTALLED. OPS FLIGHT CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 20030827000612003082700061CE 2003 8 27 FOG2003F00000 120030523A32300842102201 BELLCRANK CESSNA310 310P 2074238CE CONT O470 IO470* 17026SO NLG CRACKED E FOGAO OTHER J WARNING INDICATION CLCLIMB 1 SO355811M 310P0111 DURING A SCHEDULED PILOT TRAINING FLIGHT THE GEAR WAS RETRACTED TO UP AND LOCK. A LOUD POP/BANG WAS HEARD AND THE NOSE LANDING GEAR (NLG) INDICATED NO UP AND LOCKED. HOWEVER THE MAIN LANDING GEAR (MLG) WAS UP AND LOCKED. THE MAIN GEAR SYSTEM WAS RECYCLED WITH SAME RESULTS. AIRCRAFT LANDED WITH MLG DOWN AND LOCKED AND NLG NOT DOWN AND LOCKED AFTER INSPECTION THE BELLCRANK IDLER WAS BROKEN. IT SUSPECTED THAT FATIGUE COULD BE THE CAUSE. INSPECTION OF SUSPECTED PART FOR CRACKS. 1L72 3O3 O 3A10 E1CE 20030827000752003082700075CE 2003 8 27 DYV2003F00001 120030605A325059420011 BELLCRANK CESSNA421 421C 2076016CE CONT O520 GTSIO520F 17032SO NLG STEERING CRACKED E DYVAO OTHER O OTHER NRNOT REPORTED 1 NM074119M5552 421C1029 COULD BE OVER STEERING ON TUG MOTOR OR EXCESSIVE USE. 1L72 3O3 O A7CE E7CE 20030827001272003082700127NM 2003 8 27 CALA0300422 120030728A5720 SUPPORT ANGLE BOEING737 7373T0 1384582NM FLAP FAIRING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND A 2 INCHES CRACK IN NR 3 FLAP FAIRING AFT SUPPORT ANGLE THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030827001282003082700128NM 2003 8 27 CALA0300423 120030729A5230 SKIN BOEING737 737524 1384721NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED APPROXIMATELY 37 INCHES FROM FORWARD EDGE AND 31 INCHES FROM TOP EDGE. A REPAIR WAS INSTALLED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030827001332003082700133NM 2003 8 27 CALA0300456 120030809A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND A .5000 INCH CRACK IN CABIN FLOOR SUPPORT BETWEEN BS 380-400, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030827001502003082700150NM 2003 8 27 2003UALA00589 120030723A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29199UA 28717 FORWARD CARGO FLOORBEAM AT STA 640 LBL 40 TOP CHORD BENT. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM CHORD. 2L74 4F4 FRTA20WE E24NE 20030828000172003082800017EU 2003 8 28 CX7A194J0348 120030606A2613173436450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE MALFUNCTIONED A CX7AO OTHER N FALSE WARNING TOTAKEOFF 1 GL03302CE 340B193 LEFT TAILPIPE HOT LIGHT SHORTLY AFTER V1. LIGHT WENT OUT A FEW MINUTES AFTER POWER REDUCTION. 2L72 4T RTA52EU 20030828000202003082800020NE 2003 8 28 0074451 320030313A61117826761 BEARING RACE HAMSTD RFC11M1R5AD EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER CRACKED B EY2RK NONE O OTHER UKUNKNOWN 1 GL03 856553 CRACK IN RACE. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20030722001102003072200110NM 2003 7 22 AWXA200300719 120030608A53206546812158 WEB BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF SHEAR WEB BS 994-1006, RBL 46, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED WEB; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 3-4, 26, 29, 32, 35 & 38 FIG 3-4, 6-7 & 8. 2L72 4F RTA16WE 20030722001222003072200122NM 2003 7 22 AWXA200300739 120030623A53126517582 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 LCQ - MAJOR REPAIR - DURING C-13 CHECK 3 EACH 1 INCH CRACKS WERE FOUND AT TWO FASTENER HOLES ON BS 178 BULKHEAD WEB, LBL 17.1, WL 230. MAINTENANCE CUT OUT CRACKS AT LBL 17.1, WL 230; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1 PG 1-5. 2L72 4F RTA16WE 20030722001232003072200123NM 2003 7 22 AWXA200300740 120030623A53126517582 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 LCQ - MAJOR REPAIR - DURING C-13 CHECK A 1 INCH CRACK WAS FOUND AT FASTENER HOLE ON BS 178 BULKHEAD WEB, RBL 17.1, WL 230. MAINTENANCE CUT OUT CRACK AT RBL 17.1, WL 230; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1 PG 1-5. 2L72 4F RTA16WE 20030723000092003072300009WP 2003 7 23 GTIA030493 120030615A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AFT PIT STATION 1022 STRINGER 28L-29L FRAME CORRODED. CUT OUT DAMAGED AREA. FABRICATED REPAIR. INSTALLED REPAIR. (M) 2L72 4F A6WE 20030723000102003072300010WP 2003 7 23 GTIA030494 120030614A5320 SPLICE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 E/E COMPARTMENT STATION 180 TO STATION 195 CORRODED AT L30 SPLICE. REMOVED CORRODED SPLICE. HOLES LOCATED AND DRILLED. INSTALLED NEW SPLICE. (M) 2L72 4F A6WE 20030723000172003072300017 2003 7 23 2003F00468 420030713A34426225136001 ANTENNA AIRBUS320 A320233 3930329EU WX RADAR SYS INOPERATIVE A RJEFO OTHER O OTHER CLCLIMB 1 SO23451TA 733 AFTER TAKEOFF AT SAL STATION, FLT TA580, PILOT REPORTED THE RADAR WEAK ON AND NON-REAL WX DISPLAYED. THE AIRCRAFT RETURNED TO SAL STATION, WHERE MX TECHNICAN INSPECTED THE OPERATION OF THE RADAR. REPLACEMENT OF THE RADAR ANTENNA AND TEST WERE PERFORMED WITH NORMAL RESULTS, PER AMM 34-41-11. ALSO VISUAL INSPECTION OF THE AIRCRAFT FOR OVERWEIGHT LANDING WAS PERFORMED, THE LOAD REPORT WAS VERIFIED THROUGH AIDS LOAD REPORT (15) PER TASK AMM 05-51-11-200 AND NO FURTHER ACTION WAS REQUIRED. THE A/C WAS RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20030723000212003072300021EA 2003 7 23 2003F00471 120030706A3297 WIRE HARNESS CNDAIRCL600 CL6002B16 1900305EA NLG INOPERATIVE A O2GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE03601BE 5103 TAKING OFF FROM PBI, CREW OBSERVED THAT THE NOSE GEAR DID NOT RETRACT AFTER SELECTING GEAR UP. CREW CYCLED GEAR, RESULTS WERE THE SAME. LANDED AT PBI. (M) 2L72 4F RTA21EA 20030723000282003072300028NM 2003 7 23 UIEA200300024 120030520A5340 FITTING BOEING747 747228F 1384895NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15809MC 20887 DURING C-CHECK AT SIN, FOUND LT NOSE CARGO DOOR PORTAL FRAME CRACKED ON FUSELAGE AT BS 281, WL 312 AND LBL 40, REF SRM 53-10-04 FIG 97. THE NOSE CARGO DOOR PORTAL FRAME CRACK WAS REPAIRED BY MODIFYING SRM 747-53-10-04 FIGURE PER REF TO MATCH THE REPAIR GEOMETRY. THE REASON FOR DEVIATION FROM SRM, IS WHEN INSTALLING THE REPAIR SRM STEEL ANGLE, SHORT EDGE MARGINS WERE ENCOUNTERED AND TWO FASTENER HOLES WERE NOT FOUND ACCORDING TO THE SRM. AT THE TWO MISSING FASTENER HOLES, INSTALLED BACB30NX6K INSTEAD OF THE CALLED FOR BACB30NX8K PER SRM. AT THE SHORT EDGE MARGIN LOCATIONS, IT IS ACCEPTABLE TO INSTALL 5 REPAIR FASTENERS INSTEAD OF 6. THE REPAIR WAS CONFIRMED BY REF B AND C. (M) 2L74 4F A20WE 20030723000312003072300031NM 2003 7 23 UIEA200300025 120030520A5720 FITTING BOEING747 747228F 1384895NM WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15809MC 20887 DURING C-CHECK, FOUND RT KICK FITTING BOLT HOLES POSITION A, B AND K STILL SHOWING CRACK INDICATION AFTER 2ND OVERSIZE REAMING. PERMANENT REPAIR WITH DEVIATION TO REF 'A' SB PER REF 'B', 'C', AND 'D' BY OVERSIZING HOLE 'A', 'B'B AND 'K' THROUGH ALL COMPONENTS IN THE STACKUPS AT EACH LOCATION ON THE RIGHT SIDE SPLICE BEYOND THE LIMITS OF REF 'A' SB TO HOLE DIAMETERS OF 1.00, 1.040 AND .8750 INCH RESPECTIVELY. A SLEEVED BOLT WAS INSTALLED IN HOLE 'B'. 2L74 4F A20WE 20030723000572003072300057EU 2003 7 23 A6WA200360030 120030706A2750 CONNECTOR BAC 146 146200A 1500266EU FLAP COMPUTER DIRTY A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31181US E2042 FLAP FAULT ILLUMINATED DURING FLIGHT. FLAP COMPUTER SHOWS CODE 1 AND 8, RIGHT CONTROL RESOLVER. CLEANED CONNECTORS AT RIGHT RESOLVER. FLAP FAULT CLEARED. OPERATED FLAPS SEVERAL TIMES. OPERATIONAL CHECK GOOD AT THIS TIME. (M) 2H74 4F A49EU 20030723000612003072300061WP 2003 7 23 GTIA030489 120030623A5320 STRUCTURE DOUG DC9 DC982 3022082WP SUB FLOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 SUBFLOOR HAS 1 INCH DIAMETER CRACK AT STATION 150 RBL 30. CUTOUT DAMAGED AREA, FABRICATED DOUBLER REPAIR. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20030723000642003072300064NM 2003 7 23 TSAA0353139 120030505A53306573742 SKIN BOEING737 73725A 1384481NM FUSELAGE DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DISCOVERED A DENT LOCATED AT BS 346, BETWEEN STRINGER 24 AND 25 RIGHT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED A REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. (M) 2L72 4F RTA16WE 20030723000652003072300065NM 2003 7 23 SWAA031462 120030702A53306545766 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN STRAP CRACKED AT BS 360, LOWER AFT CORNER OF PAX WINDOW CUT OUT. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030723000662003072300066NM 2003 7 23 SWAA031463 120030702A53116520722 FRAME BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STRINGER 24R. REPAIRED FRAME PER BFG ER. 2L72 4F A16WE 20030723000762003072300076NM 2003 7 23 AWXA200300793 120030614A53156547690 FLOORBEAM BOEING737 7373Y0 1384671NM CARGO BAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1 INCH CRACK WAS FOUND AT THE INBOARD RADIUS OF AFT CARGO COMPARTMENT FLOORBEAM ZEE ANGLE BS 747, RBL 21, WL 155. MAINTENANCE CUT OUT CRACKED SECTION OF ZEE ANGLE AT BS 747, RBL 21, WL 155; FABRICATED A NEW REPLACEMENT SECTION OF ANGLE AND A SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-53 PG 202 FIG 204 SHEET 1 & 2. 2L72 4F RTA16WE 20030723000782003072300078NM 2003 7 23 AWXA200300795 120030614A532069414372 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP BS 663, STR 9 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP BS 663, STR 9 LT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 3-4. 2L72 4F RTA16WE 20030828000222003082800022NE 2003 8 28 0175156 320030520A61117725367 BEARING HAMSTD SFA13M1ROAD AEROSPATR42 ATR42* 8680900EU PWA PW120 PW124B NE HAMSTD14SF 14SF* NE PROPELLER CORRODED B EY2RK NONE O OTHER UKUNKNOWN 1 GL03 854971 854971 CORROSION ON BEARING BLADE PIN. 2H72 4T4 TRTA53EU E2ONE 6 CP7NE 20030828000462003082800046NM 2003 8 28 XNOA01128 120030508A3260 WARNING SWITCH BOEING727 727227 1384078NM MLG DOOR FAULTY A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL23793A 20774 MLG DOOR LIGHT ILLUMINATED (R GEAR DOOR LT) AFTER T/O. PERFORMED CHECKLIST, LIGHT EXTINGUISHED. REMOVED AND REPLACED RT MAIN GEAR DOOR WARNING SWITCH IAW B727 MM 32-62-11. INSPECTED WIRING. REPLACED C/P PINS. SYSTEM CHECKS GOOD. REFER TO M-12 NR 6494 FOR ORIG SIGN OFF. 2L73 4F A3WE 20030828000492003082800049CE 2003 8 28 113AX62603 120030626A53201144301167 INTERCOSTAL BEECH 1900 1900C 1154161CE FUSELAGE CRACKED E YADAK NONE O OTHER ININSP/MAINT 1 AL03113AX39219 UC41 WHILE C/W STRUCTURAL INSPECTION 53-10-02, FOUND .5 INCH CRACK IN OUTER FLANGE RADIUS OF INTERCOSTAL PN 114-430116-7 AT STATION NR 498.25 AND ADJACENT TO THE CARGO DOOR AFT UPPER GAS STRUT ATTACH BRACKET MOUNTED TO THE DOOR FRAME. 2L72 4T RTA24CE 20030828000502003082800050WP 2003 8 28 ARWA20030803 120030813A2710 O-RING DOUG DC8 DC862 3021970WP RT AILERON WORN A ARWAO OTHER O OTHER DEDESCENT 1 SO198969U 46070 LOG PAGE 110832. DISCREPANCY: AT TOP OF DESCEND LOSS OF HYDRAULIC FLUID AND PRESSURE; COMPLETED ABNORMAL HYDRAULIC LANDING CHECKLIST. REMOVED AND REPLACED RT AILERON POWER ACTUATOR HYDRAULIC O-RINGS TO SWIVEL VALVE IAW DC8 MM 27-14-01. PERFORMED LEAK CHECK, NO LEAKS NOTED. SERVICED HYDRAULIC SYSTEM IAW MM 12-30-1. 2L74 4F 4A25 20030828000732003082800073NM 2003 8 28 DL76L030653 120030715A2530828450407 ODOR BOEING767 767332 1382001NM MID GALLEY DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27171DN 24759 MID GALLEY RT FWD OVEN GIVES OFF BURNING ELECTRICAL PLASTIC SMELL. REMOVED BOTH FWD RIGHT OVENS PERFORMED WIRE INSPECTION IAW S.I. 01-086645-12. NO DEFECTS NOTED REINSTALLED OVENS. OPERATED BOTH OVENS FOR 25 MIN NO BURNING ODORS NOTED. MCC NOTIFIED OK FOR SVC. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030828000772003082800077NM 2003 8 28 DL73S030664 120030718A533065458001000 SKIN BOEING737 737232 1384475NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 FUSELAGE SKIN STA 255, S-23R TO S-24R - CUTOUT: EXISTING TEMPORARY (BLIND FASTENER) SRM REPAIR REMOVED AND PERMANENT SKIN REPAIR INSTALLED IAW DAL ER/A 385263-14. 2L72 4F RTA16WE 20030828000802003082800080 2003 8 28 DL76L030667 420030718A34174040800906 ADC BOEING767 767332 1382001NM COCKPIT FAULTY A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27192DN 28449 F/O ALTIMETER FLUX PLUS/MINUS 200 AT CRUISE, FL290 AND FL330NO FLUX IN ALTN ADC REPLACED RT ADC IAW MM. ADC TEST CHECKS GOOD. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK. 2L72 4F RTA1NM 20030828000832003082800083NM 2003 8 28 DL757030676 120030718A5330146N35317 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27655DL 24395 NEAR THE INTERNAL DOUBLER AND SURROUNDING FUSELAGE SKIN, CORROSION WAS FOUND AT THE RT GTE AIRFONE ANTENNA INSTALLATION ACCESS HOLE, AT STA. 1510 BETWEEN STR 28R AND 29R. REPAIR IAW ER/A 385352-14. 2L72 4F RTA2NM 20030828000842003082800084NM 2003 8 28 DL76G030679 120030720A335020131A BATTERY BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO271611B 30595 DURING L/O FOUND OUTSIDE LT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FWD CABIN BATTERY ASSEMBLY. OPS CKS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030828001052003082800105NM 2003 8 28 MWEA030325 120030822A5310J0602283 DOOR FRAME DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FORWARD PIT LIGHT CORROSION ON LOWER DOOR JAMB AROUND FORWARD DOOR STOP. FABRICATED AND INSTALLED REPAIR AND SPLICE. 2L72 4F RTA6WE 20030828001072003082800107WP 2003 8 28 MWEA030328 120030820A5330592480295 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FUSELAGE SKIN REPAIR ON LEFT SIDE AT STATION 410 JUST ABOVE LONGERON 16 LEFT DOES NOT MEET THE AREO DYNMIC CLEANLINESS. FABRICATED AND INSTALLED DOUBLER AND PLUG AT INTERNAL SKIN. 2L72 4F A6WE 20030828001282003082800128NM 2003 8 28 MWEA030314 120030818A532099365807 INTERCOSTAL DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FLOOR BEAM INTERCOSTAL CRACKED IN SEVERAL PLACES AIRCRAFT CENTERLINE BETWEEN FRAME STATION 769 & 788. FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F RTA6WE 20030827001682003082700168SO 2003 8 27 C2XA03CL154 120030826A3350 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2712567 145623 CLEVELAND FLIGHT 2357 THE CREW REPORTED THE EMERGENCY LIGHT ABOVE THE PASSENGER ENTRY DOOR WAS INOPERATIVE.MAINTENANCE RESECURED THE CONNECTOR AT THE INVERTER OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030827001752003082700175SO 2003 8 27 C2XA03BT082 120030817A3350 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2712567 145623 EWR, GALLEY EMERGENCY LIGHT WILL NOT COME ON. ADJUSTED GALLEY EMERGENCY LIGHT CONNECTION. PERFORMED OPERATIONAL CHECK. OPS CHECK GOOD IAW EMB145 MM 33-50-00. 2L72 4T RTT00011AT 20030827001762003082700176SO 2003 8 27 C2XA03SH286 120030821A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030723000792003072300079NM 2003 7 23 AWXA200300796 120030613A532069414372 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP BS 663, STR 9 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP BS 663, STR 9 RT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 3-4.2. 2L72 4F RTA16WE 20030723000832003072300083NM 2003 7 23 AWXA200300657 120030523A53306545765 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 LT, BS 373. MAINTENANCE CUT OUT CRACKED SKIN AT STR 4 LT, BETWEEN BS 373 AND BS 377; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH DOUBLERS, 2 EACH FILLERS, 2 EACH INTERNAL DOUBLERS, AND A TAPERED FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 PG 353 FIG 228. 2L72 4F RTA16WE 20030723000922003072300092EU 2003 7 23 AWXA200300639 120030518A5321D5367002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU CABIN FLOOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 MCN - MAJOR REPAIR - DURING C-03 CHECK PASSENGER CABIN FLOOR PANEL 251RF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 251RF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D53670022; INSTALLED REPAIR PART IAW T/C R1C25306 AND SRM 53-02-00 PG 233-236 FIG 209. 2L72 4F RTA28NM 20030723001002003072300100NM 2003 7 23 DL73S030497 120030529A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO27317DL 23089 FRAME AND REINFORCEMENT ANGLE CUT AT STA 380 TO REPLACE SECTION OF STR 17L. REPAIRED FORMER PER SRM 53-10-4 FIG 9. REPAIRED REINFORCEMENT ANGLE PER SRM 51-40-3, OK PER LIA ENGINEERING. 2L72 4F RTA16WE 20030723001022003072300102NE 2003 7 23 8939 220030611A7261 CARBON SEAL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A1 30030NE RT ENGINE FAILED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL17149 353 FLT 4467 ON T/O ROLL AT 100 KIAS RT ENG OIL PRESS WARNING INDICATOR ILLUM WITH TRIPLE CHIME. CAPT ABORTED T/O AND RETURNED TO GATE. 2L72 4T4 TRTA52EU E8NE 20030723001082003072300108NM 2003 7 23 AWXA200300688 120030611A3350100865 BATTERY BOEING737 73733A 1384673NM FUSELAGE DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 DURING INSPECTION THE EMERGENCY EXIT LIGHTS IN AFT CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY IN AFT CABIN, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030721001202003072100120NM 2003 7 21 SWAA031484 120030702A53106546525 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 12L AND STR 13L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030722000142003072200014NM 2003 7 22 2003F00442 120030307A5700 ATTACH ANGLE BOEING727 727222 1384073NM BULKHEAD CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT NLG WHEEL WELL AFT BULKHEAD CENTER TOP RIGHT STIFFENER BRACKET. REMOVED CRACK ANGLE. FABRICATED ANGLE. TREATED AND PRIMED. INSTALLED ANGLE AT NOSE LANDING GEAR WHEEL WELL AFT BULKHEAD CENTER RIGHT TOP. (M) 2L73 4F A3WE 20030722000672003072200067NM 2003 7 22 SWAA031456 120030701A57536546435274 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C2 CHECK, FOUND RT OUTBD AFT T/E FLAP DELAMINATED AT INBD END LOWER SURFACE. REMOVED AND REPLACED RT OUTBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030722000952003072200095NM 2003 7 22 SWAA031444 120030630A256010C801 LATCH BOEING737 7373H4 1384600NM ESCAPE COVER INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 CAPT'S ESCAPE ROPE COVER LATCH INOP. REMOVED AND REPLACED ROPE COVER LATCH PER MM. 2L72 4F RTA16WE 20030722001082003072200108EU 2003 7 22 AWXA200300717 120030619A351089151114 BOTTLE AIRBUS320 A320231 3930325EU OXYGEN SYS DISCHARGED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28633AW 082 IND - DIVERSION - FLT 0687 - EN ROUTE FROM PHX TO EWR CREW OXYGEN INDICATED ZERO PSI. ONE-HOUR PRIOR OXYGEN INDICATED 1300 PSI, PRIOR TO DEPARTING PHX CREW OXYGEN WAS AT 1425 PSI. MASKS WERE NOT USED, DIVERTED TO IND. MAINTENANCE REMOVED AND REPLACED THE CREW OXYGEN BOTTLE SERVICED TO 1760 PSI, LEAK CHECK WAS GOOD. OXYGEN BOTTLE REMOVED NEVER DROPPED BELOW 120 PSI. INSPECTED MASKS AND OXYGEN LINES ON FLIGHT DECK, NO LEAKS NOTED. 2L72 4F RTA28NM 20030722001122003072200112NM 2003 7 22 SWAA031469 120030703A5230AND10141 DOOR FRAME BOEING737 7373G7 1384595NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR AFT FRAME T-CHORD CRACKED AT NR 3 STOP FITTING. REM0VED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20030722001172003072200117NM 2003 7 22 SWAA031425 120030628A3350BR2013 LIGHT BOEING737 7373H4 1384600NM MID CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 EEPLS STRIP MISSING BETWEEN ROW NR 18 AND ROW NR 20. INSTALLED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20030723000492003072300049EA 2003 7 23 A6WA200340101 120030703A2613 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LT ENG OVRHT FALSE INDICATIONA A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31409AW 7447 BLEED AIR DUCT MASTER WARNING ILLUMINATED ON TAKEOFF REMAINS ON EVEN AFTER LEFT ENGINE SHUTDOWN PER QRH COMPLIED WITH 14TH STAGE DUCT LEAK CHECK. NO LEAKS. OHMED OVERHEAT ELEMENTS. ALL CHECK GOOD. COMPLIED WITH CHECK FLIGHT, NO DEFECTS NOTED. (M) 2L72 4F RTA21EA 20030723000742003072300074NM 2003 7 23 AWXA200300791 120030617A575565C25242 SKIN BOEING737 7373G7 1384595NM SPOILER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - MINOR REPAIR - DURING C-13 CHECK 2 EACH 1 INCH CRACKS WERE FOUND ON NR 9 SPOILER SKIN AROUND FORWARD HINGE POINT. MAINTENANCE 2 EACH FORWARD HINGE SKINS; FABRICATED NEW HINGE SKINS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-31-01 PG 7. 2L72 4F RTA16WE 20030827001852003082700185SO 2003 8 27 C2XA03IA079 120030805A335078241 INVERTER EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727962 145110 CLT DURING PREFLIGHT INSPECTION THE CREW FOUND CABIN EMERGENCY LIGHTS TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER AND OPERATIONALLY CHECKED THE LIGHTING SYSTEM. THE SYSTEM TESTED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030828000052003082800005CE 2003 8 28 51552 120030612A3230 FLEX LINE BEECH 1900 1900D 1154162CE LANDING GEAR DEFECTIVE A AMWAO OTHER O OTHER APAPPROACH 1 CE0726YV UE26 WHILE ON APPROACH ON FLIGHT 5578 INTO PITTSBURGH PENNSYLVANIA, THE GEAR WAS SELECTED DOWN BY NORMAL EXTENSION. WHEN FAILED, THE EMERGENCY EXTENSION WAS PERFORMED WITH GEAR DOWN AND LOCKED. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLEX LINE. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030828000522003082800052NM 2003 8 28 P5CA0300892 120030706A274035EN234 SWITCH BOEING747 747341 13848AMNM HORIZ STAB MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23355MC 23395 RETURNED TO BLOCKS - TAKEOFF WARING HORN SOUNDED WHEN THROTTLES ADVANCED - UNABLE TO SELECT APL NOSE DOWN ON STAB TRIM GREEN BAND SELECTOR (TRIM 3.5). REPLACED STAB SWITCH S334. 2L74 4F RTA20WE 20030828000562003082800056NE 2003 8 28 P5CA0300899 220030709A7200JT9D7J ENGINE BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE NR 4 MALFUNCTIONED A P5CAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 WP23524UP 21446 662533 AT FL 39.0 NR 4 ENGINE WOULD NOT MAINTAIN POWER AND SLOW RESPOND. ENGINE REPLACED FOR COMPANY CONVENIENCE 2L74 4F4 FRTA20WE E20EA 20030828000762003082800076NM 2003 8 28 DLM90030660 120030717A3222 SEAL DOUG MD90 MD9030 3023690NM NLG STRUT LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27905DA 53385 NOSE GEAR INDICATION SHOWED IT DID NOT RETRACT AFTER TAKEOFF. THERE WAS THE ASSOCIATED NOISE WITH AN EXTENDED NOSE GEAR. THE HANDLE WAS LOWERED ALL GEAR DOWN/LOCKED. A NORMAL LANDING WAS PERFORMED. FOUND NOSE STRUT SERVICING VALVE SEAL LEAKING,STRUT WAS FLAT. REPLACED VALVE ASSEMBLY, LEAK CHECKS GOOD IAW MM. 2L72 4F RTA6WE 20030828001262003082800126 2003 8 28 MWEA030316 420030818A3418R2168 RELAY DOUG DC9 DC932 3022066WP COCKPIT FAILED A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31207ME 47794 AFTER ROTATION STICK SHAKERS AND STALL INDICATION LIGHT CAME ON. REMOVED AND REPLACED RIGHT RELAY. 2L72 4F A6WE 20030828001362003082800136NM 2003 8 28 MEX2003284 120030711A5280 DOOR DOUG MD88 MD88 3023688NM NLG OUT OF ADJUST A ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23161PL 49764 FLT 490 - MID-MEX - AIRCRAFT ARRIVED WITH CAPTAIN REPORT 'NOSE LANDING GEAR LEFT DOOR OUT OF LIMITS MEASURED 38MM WITH 7MM OUT OF LIMIT'. THE NOSE LANDING GEAR LEFT DOOR WAS ADJUSTED IAW MM 32-22-01, ALL CORRECT. (M) 2L72 4F RTA6WE 20030828001382003082800138EA 2003 8 28 ASOA03354 120030803A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG DOOR MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11844AS 7317 FLT 4460 - DURING CLIMB-OUT FROM DFW-LEX, AT APPROXIMATELY 27,000 FEET THE CREW RECEIVED A NOSE DOOR OPEN WARNING MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE MESSAGE EXTINGUISHED WHEN THE GEAR WAS DOWN AND LOCKED. THE AIRCRAFT DIVERTED TO XNA, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT NOSE DOOR PROXIMITY SENSOR. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030828001432003082800143NM 2003 8 28 BJNA030701 120030723A3244247F621 TIRE BOEING737 737282 13844ATNM NLG SEPARATED A BJNAA UNSCHED LANDING O OTHER TOTAKEOFF 1 WP11233TM 23043 ON TAKEOFF ROLL HEARD LOUD BANG JUST BEFORE ROTATION. INSPECTION FOUND NR 2 NOSE TIRE HAD THROWN TREAD. (M) 2L72 4F RTA16WE 20030828001612003082800161NM 2003 8 28 USAASB03131 120030807A3397 WIRE BOEING737 7373B7 1384580NM CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19518AU 23704 ORD - MAINTENANCE REPORTED THE EMERGENCY LIGHT ASSEMBLY ON SEAT ROW 10, LEFT SIDE, WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 10, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030828001692003082800169EU 2003 8 28 USAASA0345 120030520A2560D5211044000700RDGIRT BAR AIRBUSA319 A319112 3930323EU CABIN DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US 1038 BOS - THE RIGHT FORWARD SERVICE DOOR GIRT BAR WOULD NOT LATCH. MAINTENANCE REMOVED AND REPAIRED THE GIRT BAR TELESCOPING MECHANISM. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030828001902003082800190NM 2003 8 28 CALA0300446 120030806A212165771 COOLING FAN BOEING737 737524 1384721NM E/E BAY FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714604 27317 AN OBJECTIONABLE ODOR WAS DETECTED BY FLIGHT ATTENDANT AND PASSENGERS JUST PRIOR TO DESCENT INTO COS. NO SIGN OF SMOKE WAS DETECTED IN CABIN OR COCKPIT. ALL ELECTRICAL SYSTEMS AND FLUID LEVELS CHECKED NORMAL. THE AIRCRAFT LANDED AT COS WITHOUT INCIDENT. MAINTENANCE FOUND THE EQUIPMENT COOLING FAN FAILED AND THE CIRCUIT BREAKER WAS POPPED. THE FAN WAS TEMPORARILY PLACARD INOPERATIVE FOR FUTURE REPLACEMENT. 2L72 4F RTA16WE 20030828001942003082800194NM 2003 8 28 CALA0300466 120030813A5754 SKIN BOEING737 7373T0 1384582NM L/E SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND NR 1 SLAT LOWER L/E SKIN CRACKED AT O/B TRACK. THERE WERE FOUR CRACKS MEASURING FROM .125 TO .25 INCH IN LENGTH. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20030829000122003082900012WP 2003 8 29 MEX2003231 120030617A71605930645511 NOSE COWL DOUG DC9 DC987 3022087WP RT ENGINE DENTED W ASMFK NONE O OTHER ININSP/MAINT 1 SW231075T 49724 DURING TRANSIT CHECK WAS DETECTED NOSE COWLING ENGINE RIGHT WITH DENT OUT OF LIMITS OF APPROXIMATELY 2.0 OF DIAMETER. DURING OVERNIGHT SERVICE NOSE COWLING WAS REPLACED IAW MM, ALL CORRECT. 2L72 4F RTA6WE 20030829000162003082900016NM 2003 8 29 CALA0300461 120030810A5321 FLOOR PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND A 4 INCH CRACK IN PILOT'S LT SIDE FLOOR PANEL. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030829000272003082900027NM 2003 8 29 CALA0300485 120030824A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED AT STA 227-350. A NEW Z-ANGLE WAS INSTALLED IAW SRM 53-10-15. 2L72 4F RTA16WE 20030723001112003072300111NM 2003 7 23 AWXA200300691 120030517A575369353323 FAILSAFE BOEING737 73733A 1384673NM TE FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 LCQ - FLIGHT CONTROL - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND ON RT WING OUTBOARD FLAP, INBOARD FLAP TRACK, AT WBL 254. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FILLER WELDED STOP DRILL HOLE; GRINDED WELD BEAD FLUSH; PERFORMED CLOSE VISUAL INSPECTION TO VERIFY NO CRACKS EXIST; CLEANED AND PRIMED AREA. REPAIR WAS PERFORMED IAW AWA ER 03-5750-03147-SS1. 2L72 4F RTA16WE 20030723001232003072300123NM 2003 7 23 AWXA200300609 120030513A5311654654019 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND ON LT FUSELAGE FRAME AT BS 639. MAINTENANCE REMOVED DAMAGED SECTION OF LT FUSELAGE FRAME AT BS 639; FABRICATED SPLICE REPAIR AND NEW SECTION PER S/B 737-53-1061, INSTALLED REPAIR PARTS IAW ER 15-5300-03142-TB1. 2L72 4F RTA16WE 20030724000132003072400013NM 2003 7 24 DL73S030594 120030626A3350 CHARGER BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27317DL 23089 AFTER LANDING FWD EMERGENCY LIGHT COVER FELL ON FLOOR. REINSTALLED COVER AND LIGHT DOES NOT OPS OK. CHANGED EMERGENCY LIGHT BATTERY PACK, NO HELP. CHANGED BATTERY CHARGER, OPS CHECK OK. 2L72 4F RTA16WE 20030724000262003072400026NM 2003 7 24 AWXA200300668 120030519A5712654544555 RIB BOEING737 73733A 1384673NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT WING RIB AT WBL 135.5. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING RIB AT WBL 135.5; FABRICATED A NEW SECTION OF AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW ER 03-5723-03149-TB1. 2L72 4F RTA16WE 20030724000282003072400028NM 2003 7 24 DL76L030529 120030608A3320190611 BALLAST BOEING767 767332 1382001NM CABIN LIGHTS OVERHEATED A DALAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27183DN 27110 APPROX 3 HRS INTO FLT F/A REPORTED STRONG ODOR IN AFT GALLEY. ODOR WAS STRONGEST IN VICINITY OF CAPT SIDE LAVATORY/ AISLE AIR VENTS. ODOR WAS ELECTRICAL IN NATURE AND DISSIPATED AFTER 10 MIN. FOUND CEILING LIGHT BALLAST AT 41A, B OVERHEAD INOP AND WITH STRONG ODOR. REPLACED BALLAST AT 41 A, B. CHECKS GOOD NO MORE ODOR, 2L72 4F RTA1NM 20030724000332003072400033NM 2003 7 24 EIA2003092 120030706A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 EMERGENCY LIGHT ASSY IN UPPER DECK DOME LIGHT INOP. DMI OPEN. 2L74 4F A20WE 20030724000362003072400036NM 2003 7 24 DL764030536 120030611A3397 WIRE BOEING767 767432ER 1385134NM EMERGENCY LIGHT LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27829MH 29700 SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP FROM ROW 22AB TO 25AB. FOUND EMERGENCY LIGHT WIRE UNPLUGGED UNDER SEAT 22B. RECONNECTED SAME, OPS CKS GOOD. 2L72 4F RTA1NM 20030724000382003072400038EU 2003 7 24 AWXA200300626 120030501A5330D5323133520201 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON CORNER FITTING AT AFT LOWER CORNER OF FORWARD CARGO DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED CORNER FITTING AT AFT LOWER CORNER OF FORWARD CARGO DOOR CUTOUT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2-7 PG 7-22 & FIG 9-18 PG 23-36. 2L72 4F RTA28NM 20030724000392003072400039NM 2003 7 24 DL757030538 120030611A323027N20881 SHUTTLE VALVE BOEING757 757232 1384965NM MLG FAILED A DALAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO27613DL 22820 GEAR WOULD NOT RAISE AFTER T/O. FOLLOWED ABNORMAL PROCEDURE USING LOCK OVERRIDE AND GEAR RAISED NORMALLY. REPLACED TRUCK SHUTTLE VALVE PER M/M. 2L72 4F RTA2NM 20030724000412003072400041NM 2003 7 24 DL757030540 120030612A5330143N36911 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27614DL 22821 FUSELAGE / FS 680 AND STR 26L - REPAIR OF LIGHTNING STRIKE: DAL ER/A 385076-14 PROVIDES INSTRUCTIONS TO TRIM OUT THE DAMAGED SKIN AND INSTALL AN EXTERNAL DOUBLER AND STRUCTURAL FILLER. THE FUSELAGE SKIN IS M/F 2024-T3 CLAD ALUMINUM WITH A LOCAL THICKNESS OF 0.056 INCH AND 0.042 INCH IN THE TRIMMED AREA. 2L72 4F RTA2NM 20030422000932003042200093SO 2003 4 22 SIMA200307915 120030315A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 ABI - DURING A IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED NEW SILL IAW EMB-145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-40-06, 51-40-02, 51-20-03, EMB 145 CPM 51-21-04, THROUGHT 51-21-06. (M) 2L72 4F RTT00011AT 20030422001142003042200114SO 2003 4 22 SIMA200307909 120030227A532014521725615 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, SERVICE DOOR AFT SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SERVICE DOOR AFT SILL IAW EMB SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030422001172003042200117NM 2003 4 22 USAASB03034 120030302A21337110033 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN PRESSURE MALFUNCTIONED A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19341US 23510 PHL - FLT 419 - EN ROUTE FROM MHT TO CLT, AT FL 350, THE CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN ALTITUDE WENT TO 11,500 FEET. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES AND SWITCHED TO STANDBY PRESSURIZATION WITH NO HELP. CREW THEN ACCOMPLISHED A RAPID DESCENT AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE FOUND THE FORWARD OUTFLOW VALVE STUCK OPEN. REPLACED FORWARD OUTFLOW VALVE (P/N 32-2684-003). OPERAITONAL CHECK REVEALED THE FORWARD OUTFLOW VALVE CLOSED ONCE AND REMAINED CLOSED. FOUND THE AFT OUTFLOW VALVE 'CLOSED' SIGNAL STUCK. REPLACED AFT OUTFLOW VALVE PER MM 21-31-00. OPERATIONAL CHECK GOOD. (2L72 4F RTA16WE 20030422001222003042200122EU 2003 4 22 USAASA03020 120030228A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19738US 1254 CLT - AN 'INT LOAD EMERG L' FAULT WAS GENERATED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030422001272003042200127NM 2003 4 22 UPS03240258 120030214A5312 PRESSURE PANEL BOEING727 727108C 1384039NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, AIR LEAK COMING FROM WHAT APPEARS TO BE CRACK IN PRESSURE WEB IN NOSE W/W LEFT SIDE MIDWAY ON LT SIDE WALL. CRACKED AREA CUT OUT IAW SRM 51-40-2. DOUBLER & FILLER FABRICATED IAW SRM 51-40-2. HFEC C/O ON CUTOUT ON THE ABOVE AREA IAW NDTM 51-00-00 PT 6. - NDF. REPAIR PARTS INSTALLED IAW SRM 51-40-2. 2L73 4F A3WE 20030829000332003082900033NM 2003 8 29 CALA0300497 120030826A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND UPPER AND LOWER SURFACE OF FLOOR SUPPORT CORRODED BETWEEN STA 967 AND 986.5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030829000452003082900045NM 2003 8 29 DHL2003745016 120030719A5280 DOOR BOEING727 727224 1384076NM RIGHT OUT OF ADJUST A DHLAO OTHER JE WARNING INDICATION VIBRATION/BUFFET CRCRUISE 1 SO01745DH 20665 RED DOORS LIGHT ON FORWARD PANEL CAME ON DURING CRUISE. PERFORMED ABNORMAL PROCEDURE AND LIGHT WENT OUT. RUMBLE IN CRUISE. DURING TROUBLESHOOTING FOUND RIGHT-HAND SHOCK STRUT DOOR OUT OF ADJUSTMENT. ADJUSTED RIGHT-HAND SHOCK STRUT DOOR ROD ASSEMBLY IAW B-727 M/M 32-22-12 FIGURE 501 SECTION A-A. OPS CHECKED GOOD IAW B-727 M/M 32-33-0. 2L73 4F A3WE 20030829000492003082900049EU 2003 8 29 DHL2003363004 120030716A3260BED2011 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU RT MLG FAULTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01363DH 85 RT MAIN GEAR GREEN DOWN LIGHT ON FORWARD PANEL REMAINED ON AFTER T/O WITH GEAR HANDLE IN THE UP POSITION. THE ANTI-SKID OFF LIGHT ON THE MASTER WARNING PANEL WAS ALSO ILLUMINATED. AFTER A SHORT TIME THE LIGHTS FLICKERED AND THEN REMAINED OFF. NR 2 SYSTEM WAS SELECTED AND ALL LIGHTS WERE OUT ON S/O'S PANEL. VERIFIED CONNECTOR CLEAN AT 66GB PROXIMITY DETECTOR. LANDING GEAR WARNING SYSTEM OPS CHECKED GOOD PER M/M 32-61-00. VERIFIED WIRING FROM 54GB PROXIMITY BOX TO 66GB SYSTEM 1 SENSOR & ASSOCIATED GROUND WIRE PER WDG 32-61-11 & -14. WIRING CHECKED GOOD. REMOVED AND REPLACED PROXIMITY DETECTOR MODULE UNIT PER M/M 32-61-12 & OPS CHECKED GOOD. 2L72 4F RTA35EU 20030829000822003082900082NE 2003 8 29 P5CA0300925 220030822A7230 COMPRESSOR BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE STALLED A P5CAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23923FT 22769 702370 ENGINE COMPRESSOR STALL ON DESCENT. REMOVED AND REPLACED NR 3 ENG, REF PAC ENG CHANGE WORK CARDS 7100-002. 2L74 4F4 FRTA20WE E3NE 20030829000922003082900092WP 2003 8 29 P8UF200300001 120030709A3610AAM72411 DUCT DOUG DC10 DC1030F 3023504WP BLEED AIR SYS LEAKING W P8UFBGFAEMER. DESCENT O2 MASK DEPLOYED ACTIVATE FIRE EXT. UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO23831LA 46936 MANIFOLD FAIL LIGHT ON NR 2. SMOKE DETECT CABIN CARGO NR 8, 9, 10 LIGHT ON. SMOKE DETECT AFT CARGO NR 1, 2, 3 AND HEAT DET AND AFT CARGO FIRE LIGHT ON. PRESENCE OF SMOKE IN ALL CARGO MAIN UPPER & COCKPIT. 2L73 4F RTA22WE 20030828000322003082800032SO 2003 8 28 6203N50KC 120030602A27101159CSM5510627 BALANCE WEIGHT GULSTM GULSTMGV GULFSTREAMGV3980116SO LT AILERON DETACHED E KKYAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NE0350KC 480 480 659 659 ON DESCENT, EXPERIENCED DIFFICULTY IN TURNING ACFT LATERALLY TO RIGHT. PILOTS WERE ABLE TO CONTROL ACFT AND MAKE A NORMAL LANDING. INITIAL INVESTIGATION BY PILOTS REVEALED A LOUD CLUNK WHEN LEFT AILERON WAS MOVED PHYSICALLY. T/R WAS ABLE TO VERIFY THAT AILERON'S MASS BALANCE WEIGHT HAD BECOME UNATTACHED {LOSS OF ATTACHING HARDWARE}. MECHANICS DISPATCHED TO MAKE REPAIRS AS WELL AS OPERATOR'S MECHANIC TO OVERSEE REPAIRS. ACFT'S FLIGHT CONTROLS WERE FURTHER INSPECTED, & NO ABNOMALIES DISCOVERED. ACFT WAS LATER FLOWN TO MANUFACTURER'S MAINTENANCE FACILITY FOR FURTHER INVESTIGATION. MANUFACTURER ISSUED A MAINTENANCE & OPERATIONS LETTER GV-MOL-03-0034 DESCRIBES OCCURRENCE, NO OTHER ACFT HAVE BEEN AFFECTED. 2L72 4F RTA12EA 20030828000372003082800037SW 2003 8 28 505060503 120030604A32440283353 TIRE SWRNGNSA227 SA227AC 8780603SW MLG BLOWN E STZAC ABORTED TAKEOFF G MULTIPLE FAILURE TOTAKEOFF 1 AL03505FS629 22 AC591B UNCONTAINED NR 2 MAIN LANDING GEAR TIRE FAILURE ON TAKEOFF ROLL. FURTHER EXAMINATION REVEALED FAILURE OF TORQUE LINK ATTACH POINT ON LOWER YOKE OF MAIN GEAR STRUT. LOWER STRUT ASSEMBLY ROTATED 360 DEG. CLOCKWISE WRAPPING BRAKE LINES AROUND LOWER STRUT. NO DAMAGE TO AIRCRAFT. INSUFFICIENT DATA EXISTS AT THIS TIME TO DETERMINE IF THE LOWER TORQUE LINK ATTACH POINT FAILURE PRECEDED THE TIRE FAILURE OR WAS A RESULT OF THE TIRE FAILURE. 2L72 4T RTA8SW 20030828000552003082800055NM 2003 8 28 P5CA0300897 120030711A27016604291 PLATE BOEING747 747341 13848AMNM CONTROL COLUMN DEFECTIVE A P5CAO OTHER O OTHER CRCRUISE 1 WP23355MC 23395 DURING FLT CNTRL CK, FELT A THUMP AND CLICK IN LEFT TURN - FORE AND AFT MOVEMENTS. REMOVED CAPT CONTROL COLUMN -REMOVED AND REPLACED PLATE ASSY - REINSTALLED COLUMN AND TESTED NRML IAW AMM 27-31-04/05. 2L74 4F RTA20WE 20030828000652003082800065NE 2003 8 28 P5CA03000316 220030817A723069B482277 COMPRESSOR BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE STALLED A P5CAK NONE R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23923FT 22769 702370 NR 3 ENG COMPRESSOR STALLED AT FL 330 FUEL TEMP PEGGED AT OFF SCALE HOT AND OIL TEMP WENT TO 150 DRGS. PREFORMED 8TH STAGE BLEED CHECK VALVE. CHECKED P/R LINE ON T12 SENSOR, CHECKED FUEL HEAT VALVE, CHECKED NR 3 MAIN TANK SUMP DRAIN CHECKED FUEL / OIL COOLER TEMP BULB, ALL CHECKED OK REPLACED FUEL HEATER TIMER AND LOCKED OUT PYLON VALVE AND DEFERRED. 2L74 4F4 FRTA20WE E3NE 20030828001062003082800106 2003 8 28 MWEA030271 420030707A2565113317 SLIDE DOUG DC9 DC981 3022081WP R1 DOOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 FORWARD GALLEY DOOR SLIDE WAS KNOCKED OFF DOOR. CAGE AROUND THE GAUGE WAS DAMAGED. REMOVED AND REPLACED FORWARD GALLEY DOOR SLIDE. 2L72 4F A6WE 20030828001482003082800148NM 2003 8 28 HALA0300700 120030808A5755 SUPPORT FITTING BOEING717 717200 1383700NM LT SPOILER CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13475HA 55121 HNL - FOUND LEFT WING INBOARD SPOILER HAS A CRACK ON THE OUTBOARD SPOILER ACTUATOR SUPPORT FITTING. REPAIR IN WORK. (M) 2L72 4F TRA6WE 20030828001562003082800156NM 2003 8 28 USAABB03115 120030709A521080330035 BOTTLE BOEING757 757225 1384959NM L1 DOOR DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU 22199 BWI - FOUND THE L1 DOOR ASSIST BOTTLE EMPTY DURING A WEEKLY CHECK. MAINTENANCE REPLACED THE BOTTLE. (M) 2L72 4F RTA2NM 20030828001572003082800157EU 2003 8 28 USAASA03085 120030804A2121EVT3454H FAN AIRBUSA319 A319112 3930323EU E/E BAY OVERHEATED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19768US 1389 CMH - FLT 42 - EN ROUTE DEN-PHL, WHILE IN CRUISE FLIGHT, CREW RECEIVED ECAM WARNING, 'AVIONICS SMOKE'. THE CREW ALSO REPORTED NOISES COMING FROM THE AVIONICS BAY. THE FLIGHT DIVERTED TO RIC AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS BLOWER FAN AND AEVC FILTER. SYSTEM TEST OK. (M) 2L72 4F RTA28NM 20030828001972003082800197NM 2003 8 28 CALA0300476 120030821A5342 ANGLE BOEING737 737524 1384721NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714645 28906 INSPECTION FOUND LT VERTICAL STABILIZER PANEL ATTACH ANGLE GOUGED AT STA 1065-1085 JUST BELOW VERTICAL STAB ON LT SIDE JUST FORWARD OF RUDDER. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW ECRA 55380-01013. 2L72 4F RTA16WE 20030829000362003082900036NM 2003 8 29 CALA0300500 120030827A5753 STIFFENER BOEING737 7373T0 1384582NM FLAP TRACK GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND RT WING NR 6 FLAP TRACK FAIRING I/B STIFFENER GOUGED. THE STIFFENER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030829000562003082900056NM 2003 8 29 DHL2003726011 120030722A3234 CONTROL HANDLE BOEING727 727228 1384083NM COCKPIT DIRTY A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01726DH 20409 WHEN GEAR WAS CYCLED DOWN, ALL 3 GREEN AND ALL 3 RED GEAR LIGHTS STAYED ON. DOORS LIGHT OUT. SECONDARY INDICATIONS CONFIRMED ALL GEAR DOWN. FOUND GEAR HANDLE SLIGHTLY STICKY ON SLIDE FUNCTION. CLEANED AND LUBRICATED HANDLE. CYCLED 3 TIMES ALL NORMAL PER M/M 32-00. 2L73 4F RTA3WE 20030829001002003082900100 2003 8 29 3144032703 420030327A3416150201182 ALTIMETER SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP075226R27 3144 22090 ALTITIUDE INDICATOR INOP. 1G71 3U3 U H9EU E19EU 20030829001362003082900136NM 2003 8 29 SWAA031864 120030819A21506937319148 MODULE BOEING737 7375H4 138449DNM COCKPIT DIRTY A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29522SW 26564 AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. FOUND, P5-10 AIR COND MODULE SOILED. REMOVED AND REPLACED AIR COND MODULE PER MM. 2L72 4F RTA16WE 20030829001382003082900138NM 2003 8 29 SWAA031832 120030816A3350101073 LENS BOEING737 7373H4 1384600NM ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030829001512003082900151 2003 8 29 SWAA031845 420030814A2565D31354 SLIDE BOEING737 7372T4 1384492NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20030829001582003082900158NM 2003 8 29 SWAA031822 120030814A25606557463 ATTACH FITTING BOEING737 7373H4 1384600NM FWD ENTRY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FWD AND AFT GIRT BAR ATTACHMENT FITTINGS CORRODED. REMOVED AND REPLACED ATTACHMENT FITTINGS PER MM. 2L72 4F RTA16WE 20030829001642003082900164NM 2003 8 29 SWAA031829 120030813A3260FCA410 RELAY BOEING737 7373Q8 1384670NM COCKPIT FAULTY A SWAAK NONE J WARNING INDICATION CRCRUISE 1 SW29663SW 23256 INTERMITTENT NLG UNSAFE LIGHT WITH HANDLE IN OFF OR UP, WITH GEAR EXTENDED ALL LIGHTS NORMAL. REMOVED AND REPLACED R-374 RELAY, M1214 AND M1215 LOGIC CARDS PER MM. 2L72 4F RTA16WE 20030829001682003082900168NM 2003 8 29 SWAA031817 120030811A551265C45727 SKIN BOEING737 7373H4 1384600NM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED CHECK, FOUND LT HORIZ STAB SKIN CRACKED AT STA 157.10 JUST FWD OF REAR SPAR. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001702003082900170NM 2003 8 29 SWAA031787 120030807A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030829001822003082900182NM 2003 8 29 SWAA031793 120030811A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R AT BS'S 400, 500A, 827 AND 887. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030829001952003082900195EA 2003 8 29 ASOA03348 120030801A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11889AS 7538 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE MAIN PASSENGER DOOR WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE MAIN PASENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030829001982003082900198NM 2003 8 29 USAA030105 120030626A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 CLT - FOUND FRAME CRACKED 1 INCH BY 2 INCH BY .080 INCH, BS 580 BETWEEN S24L AND S25L. FABRICATED AND INSTALLED REPAIR DOUBLER AND TIE CLIPS PER EA 87259, SRM 53-00-07. (M) 2L72 4F RTA2NM 20030829001992003082900199NM 2003 8 29 USAA030106 120030626A5240 WEB BOEING757 757225 1384959NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 CLT - FOUND WEB CRACKED .200 INCH, UPPER HINGE CUTOUT WEB L4 DOOR. FABRICATED DOUBLER, TRIMMED OUT DAMAGE, INSTALLED REPAIR PER EA 87189. (M) 2L72 4F RTA2NM 20030829002012003082900201NM 2003 8 29 USAA030135 120030709A5320 ANGLE BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 PIT - FOUND Z-ANGLE WITH 3 AREAS OF CORROSION, RIGHT CREASE BEAM INNER CHORD Z-STATION 947.5-986.5 PLUS 8 INCHES, 3 INCH BY 2 INCH, 2 INCHES BY 2 INCHES, 4 INCHES BY 2 INCHES. REPLACED Z-ANGLE PER SRM 53-60-15. (M) 2L72 4F RTA16WE 20030902000332003090200033SO 2003 9 2 FFS2003F00019 120030502A28202319517 LINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT WING FUEL LEAKING E FFSAO OTHER O OTHER NRNOT REPORTED 1 AL013536B21559 317952205 PILOT REPORTED LT FUEL BOOST PUMP CIRCUIT BREAKER POPPED IN FLIGHT. UPON INSPECTION OF FUEL PUMP IN LT WING ROOT, IT WAS APPARENT THERE HAD BEEN A BRIEF FIRE IN THE AREA. PLASTIC SPIRAL WRAP AROUND FUEL LINE HAD SHRUNK AND MELTED. PNEUMATIC LINE TH LT WING DE-ICE BOOT WAS MELTED. AREA WAS COVERED WITH SOOT. WIRE TO LOW-PRESSURE BOOST PUMP HAD CHAFFED AGAINST THE FUEL LINE TO BOOST PUMP WARNING PRESSURE SWITCH. THE WIRE ARCED A HOLE IN THE FUEL LINE CREATING A FUEL LEAK AND FIRE. WHEN CIRCUIT BREAKER POPPED, BOOST PUMP FAILED AND REMOVED PRESSURE FROM LEAKING LINE. 1L72 3O3 O A20SO E14EA 20030422000722003042200072SW 2003 4 22 2003F00233 120030206A792031080811 LINE FRCHLDSA227 SA227DC 3377521SW LT ENGINE CRACKED A I7WAK NONE J WARNING INDICATION ININSP/MAINT 1 NM051119K DC830B MWH - FLT 2569 - LEFT ENGINE OIL PRESSURE LIGHT CAME ON DURING CLIMB AT 18K MSL. CREW VERIFIED READING WITH OIL PRESSURE GAGE, WHICH READ 0 PSI. CREW SHUT DOWN LEFT ENGINE AT THAT TIME. LOST OIL PRESSURE DUE TO OIL LEAK. REMOVED LINE, LOOSENED ALL ATTACHING LINES TO RELIEVE ANY STRESS AT ANY CONNECTION, INSTALLED LINE, AND RETIGHTENED ALL LINES TO PREVENT STRESS AT ANY CONNECTION. GROUND RUN AND LEAK AND OPS CHECK GOOD. (M) 2L72 4T RTA18SW 20030422000812003042200081SO 2003 4 22 SIMA200307916 120030314A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVIVCE DOOR SILL AND INSTALLED NEW SILL IAW EMB SRM, SRM EMB145/1142 REV 20, CHAPTERS 51-40-02, 51-20-03, AND 51-40-06. (M) 2L72 4F RTT00011AT 20030422000882003042200088SO 2003 4 22 SIMA200307911 120030227A532014521725013 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, SERVICE DOR FORWARD SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030422001002003042200100NM 2003 4 22 USAA030025 120030306A5330 SKIN BOEING757 757225 1384959NM FUSELAGE DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU 22198 CLT - FOUND SKIN DISBONDED 6 INCH DIAMETER AREA, 77 INCHES FORWARD OF STATION 2005.2 AT LBL 14. METAL BOND REPAIR PER EA 87080. (M) 2L72 4F RTA2NM 20030422001052003042200105SO 2003 4 22 SIMA200307907 120030221A532114525381003 DOUBLER EMB 135 EMB135LR 3260305SO CARGO FLOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, LEFT CARGO FLOOR DOUBLER FROM STATION 65 TO 68 CORRODED. REMOVED AND INSTALLED CARGO FLOOR DOUBLER FROM STATION 65 TO 68 IAW EMB SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030422001082003042200108EA 2003 4 22 2003F00235 120030326A56106003303025 WINDSHIELD CNDAIRCL600 CL6002B16 1900305EA COCKPIT CRACKED A PI1MO OTHER O OTHER CRCRUISE 1 EA2787 5190 DURING CRUISE AT FL330, PILOTS WINDSHIELD, OUTER PLY, POPPED AND THEN CRACKED IMMEDIATELY FROM TOP TO BOTTOM ORIGINATING FROM CENTER. (M) 2L72 4F RTA21EA 20030422001202003042200120NM 2003 4 22 USAABB03039 120030311A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030422001282003042200128WP 2003 4 22 UPS03840260 120030306A5610 WINDOW DOUG DC8 DC871F 302199DWP COCKPIT LEAKING A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01755UP 46055 INSPECTION TYPE:N/A, F/O CLEAR VIEW WINDOW STILL SQUEALING AT CRUISE AIR SPEEDS AND THE WINDOW IS VERY DIFFICULT TO OPEN. PRESSURIZED A/C TO 8 PSI DIFF, NO SQUEAL NOTED. SEALED EYEBROW WINDOW WITH AERODYNAMIC SEALENT. LUBED F/O CLEARVIEW WINDOW & WINDOW OPERATES SMOOTHLY. 2L74 4F RT4A25 20030422001342003042200134SO 2003 4 22 SWIA200311824 120030304A3350 LIGHT EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE CABIN INOPERATIVE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07268UE 120207 FLOOR LEVEL EMERGENCY LIGHTS FORWARD OF ROW THREE INOP. REPLACED A BAD FUSE. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030422001422003042200142NM 2003 4 22 UPS03440252 120030304A5414 SKIN BOEING747 747200 1384847NM NR 4 ENG PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01528UP 24071 INSPECTION TYPE:ASV NR 4 ENGINE PYLON CRACKED ON I/B SIDE. CRACK IN NR 4 ENG PYLON INBD SIDE AFT OF SLOT SEAL COMING FROM TOP SIDE OF PREVIOUS DOUBLER. REMOVED EXISTING DOUBLER FROM A/C 75705 03/04/03, REPAIRED PER EO B747-5430-18401-A. NEW DOUBLER REPAIR INSTALLED. 2L74 4F RTA20WE 20030418001572003041800157NM 2003 4 18 UPS03440227 120030204A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C FX - LOWER FUSELAGE INTERIOR STRUCTURE ATT STRINGER FOUND HEAVY CORROSION AT STA 2340 TO STA 2360 STR 50R. STRINGER CUT OFF AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-0 2. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. TIE CLIP REPLACED AS PER SRM 51-10-01 PAGE 8. CORROSION BLEND OUT 0.060 X 1 X 2 INCH. 2L74 4F RTA20WE 20030421000012003042100001NM 2003 4 21 UPS03440228 120030204A5711 FITTING BOEING747 747200 1384847NM WING REAR SPAR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, RIGHT BS 1241 WING REAR SPAR KICK FITTING, HOLE D-CORROSION CRACK FOUND APPROX 0.040 INCH RUNNING I/B FWD SURFACE. D-HOLE REWORKED AS PER EO B747-5710-12138 AND EO B747-5710-18343A RS 57-12-34973. 2L74 4F RTA20WE 20030421000032003042100003NM 2003 4 21 UPS03440235 120030224A3350 MODULE BOEING747 747200 1384847NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01523UP 22381 EMERGENCY LIGHTS UNARMED ANNUNCIATOR INOPERATIVE. RELAMPED, NO HELP. REPLACED EMERGENCY LIGHT MODULE ASSY, OPS CHECK OK. 2L74 4F RTA20WE 20030421000082003042100008WP 2003 4 21 UPS03840236 120030224A33506012235 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01803UP 46073 ON PREFLIGHT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC8 MM 33-50-01. EMERGENCY EXITS OPS CK NORMAL. 2L74 4F RT4A25 20030421000672003042100067EA 2003 4 21 SWIA200311816 120030302A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB FAILED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07587SW3227 3227 7062 STAB TRIM CH 1 AND MACH TRIM MESSAGES WOULD NOT RE-ENGAGE. RETURNED TO FIELD. REPLACED MCU. REMOVED AND REPLACED HSTA WITH SERVICEABLE UNIT IAW MM 27-24-01. OPS CHECK GOOD AT THIS TIME. MCU P/N: 7062-3, S/N OFF: 597. 2L72 4F RTA21EA 20030421001042003042100104SW 2003 4 21 CA030404003 120030403A2913PV30448A CASE BELL 205 205A1 1181414SW LYC T53 T53* 41549NE HYD PUMP CRACKED W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN) NOTICED SMALL AMOUNT OF HYDRAULIC FLUID ON HYDRAULIC PUMP CASE. THOUGHT IT WAS LOOSE BUT WAS NOT. REMOVED LINE ATTACHED TO IT AND FOUND SMALL CRACK. 1G71 4U4 U H1SW E1EA 20030421001842003042100184NM 2003 4 21 BJNA030302 120030312A3350362624 LIGHT BOEING737 737282 13844ATNM PAX CABIN BROKEN A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM 23043 EMERGENCY FLOOR LIGHTING STRIP BROKEN AT SEAT 15D. INSTALLED LIGHT STRIP AS REQUIRED, OPS CHECK GOOD, IAW AMM 33-51-07. (M) 2L72 4F RTA16WE 20030421001862003042100186NM 2003 4 21 AMTA200300096 120030116A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 EGRESS LIGHT INOPERATIVE AT ROW 5. RECONNECTED WIRES AS REQUIRED. OPS CHECK NORMAL. 2L72 4F RTA2NM 20030421002002003042100200CE 2003 4 21 2003F00227 120030301A5210671132249 BEARING CESSNA750 750 2076810CE PAX DOOR SEIZED A UG8AK NONE O OTHER ININSP/MAINT 1 GL235116 7500019 MAIN CABIN DOOR IS HARD TO OPEN FROM THE INSIDE. REPLACED AFT CABLE ASSEMBLY, SPRING PIVOT BEARINGS ANDLONG SHAFT. RIGGED THE DOOR PER CESSNA MM. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030421002102003042100210NM 2003 4 21 AMTA200300333 120030308A3297 WIRE BOEING757 75723N 1384973NM MLG LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11524AT 30233 AFTER GEAR RETRACT EICAS MESSAGE LANDING GEAR MONITOR RETURNED. FOUND WIRE W3054-AD 'BLUE' OF PROX SENSOR NOSE GEAR SYSTEM NR 2 BACKED OUT TERMINAL BLOCK TB25. RESECURED WIRE IN TERMINAL BLOCK, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030421002142003042100214NM 2003 4 21 AMTA200300365 120030315A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11522AT 29330 FOUND TWO EGRESS LIGHTS OUT IN FRONT OF RIGHT AFT LAV DOOR. REPLACED LT SOCKETS AND HARNESS. EGRESS LIGHT CHECKED GOOD. (M) 2L72 4F RTA2NM 20030422000292003042200029NM 2003 4 22 AMTA200300344 120030310A3350 POWER SUPPLY BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11516AT 27972 EMERGENCY LIGHT AT SEAT 26 ABC IS OUT. REMOVED AND REPLACED FUSE TO PIN 16 ON THE MID AFT EMERGENCY POWER SUPPLY AS REQUIRED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030422000312003042200031EA 2003 4 22 ASOA03083 120030227A3350OL3071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 FLT 4415 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMPS BY THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422001452003042200145EU 2003 4 22 NSVA200300019 120030307A324613889 BEARING SAAB SF340 340B 7860101EU MLG WHEEL DESTROYED A NSVAK NONE O OTHER TXTAXI/GRND HDL 1 EA27242CJ NOV982481 340B242 FLIGHT CREW FELT NOSE WHEEL SHIMMY DURING LANDING AND TAXI AT PVD. MAINTENANCE WAS DISPATCHED TO AIRCRAFT AND REMOVED THE NOSE WHEELS AND FOUND THE LT INBOARD WHEEL BEARING FROZEN TO THE NLG AXLE FROM LACK OF LUBRICATION. MAINTENANCE REMOVED AND REPLACED THE AXLE AND BOTH WHEEL ASSEMBLIES AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTA52EU 20030422001552003042200155EU 2003 4 22 MALA030193 120030223A3010HTE2500761 VALVE BAC 146 AVRO146RJ85A1500097EU DEICE SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15505XJ E2313 DURING FLIGHT 3651, WHILE HOLDING AT 240 SO. OF STL LT OUTER DEICE VALVE C/B TRIPPED PART WAY THROUGH CYCLE. AIR RETURN TO MEM. MAINTENANCE SWAPPED VALVES P/N HTE250076-1 HH11 AND HH5 C/B MX3 AND F26 P/N MS3320-3. OPS CHECK GOOD. SWAPPED, PERFORMED IAW AMM CHAP 30. 2H74 4F RTA49EU 20030422001642003042200164WP 2003 4 22 UPS03840270 120030310A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW M/M 33-50-01. 2L74 4F RT4A25 20030423000062003042300006NE 2003 4 23 AUS20030256 120030304A63207635109600044 GEARBOX SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE MAIN ROTOR CONTAMINATED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS 2704 (AUS) MAIN TRANSMISSION CHIP DETECTORS CONTAINED A SMALL AMOUNT OFFERROUS PARTICLES. THE PARTICLES WERE WITHIN LIMITS AS PER THEMAINTENANCE MANUAL. AFTER CHANGING THE OIL AND OIL FILTER A FURTHER CHECK FOUND NO EVIDENCE OF METAL PARTICLES AND THEAIRCRAFT WAS RETURNED TO SERVICE WITH AN INCREASED INSPECTION REGIME ON THE CHIP DETECTORS. 1G72 3U3 UNCH1NE E19EU 20030423000182003042300018NM 2003 4 23 AUS20030301 120030212A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 29L CONTAINED LEVEL 2 CORROSION ON THE OUTBOARD LEG ON THE FORWARD AND AFT SIDES OF FRAME 950E. FOUND DURING CPCPINSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423000202003042300020NM 2003 4 23 AUS20030303 120030212A5330 PANEL BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AFT CARGO DOOR THRESHOLD PANEL CONTAINED LEVEL 2 CORROSION ANDREQUIRED REPLACEMENT DUE TO BEING WORN BEYOND LIMITS. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423000222003042300022NM 2003 4 23 AUS20030298 120030212A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE MAIN, LCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 27L CONTAINED LEVEL 2 CORROSION IN AREA LOCATED BETWEEN BS 1070 TO BS 1090. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423000342003042300034NM 2003 4 23 AUS20030286 120030212A5311 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME LOWER FLANGE CONTAINED LEVEL 2 CORROSION AT BS 660 BETWEEN STRINGER 26R AND STRINGER 27R. FOUND DURING CPCPINSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423000392003042300039NE 2003 4 23 UIAFAA9201 220030208A72611779MK2 SCAVENGE PUMP DOUG MD90 MD9030 3023690NM IAE V2525 V2525D5 NE ENGINE OIL BROKEN Z O OTHER J WARNING INDICATION CRCRUISE 1 TW0017916 53539 RT GEN OFF SHOW ON EOAP DURING THE FIGHT FROM MACAU TO SHANGHAI, AFTER LANDING LINE MAINTENANCE PERSONNEL REPORTED RT GEN BEARING FAIL WAS SHOWN ON EPCU AND HE CLAIMED THAT SERIOUS DAMAGE WAS FOUND ON VSCF GEN INCLUDING; EXTRUSION OF 3 ELECTRIC PLUGS BACKSHELLS, BROKEN PORTION OF DRIVE GEAR OF GEN WAS STUCK INTO THE ENGINE GEARBOX. AFTER REPLACED NR 4 BEARING SCAVENGE VALVE AND REPLACED CARBON SEAL ,THE A/C BACK NORMAL. 2L72 4F4 FRTA6WE A40NE 20030423000992003042300099NE 2003 4 23 GLBA2003009 320030117A6111 BEARING BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE PROPELLER BLADE FAILED A GLBAO OTHER O OTHER NRNOT REPORTED 1 NM03201GL4222 UE201 REPLACED PROP DUE OVERHAUL FOUND NR 2 BLADE BEARING HAD FAILED. REMOVED AND REPLACED PROP. 2L72 4T RTA24CE 5 CP10NE 20030423001052003042300105NE 2003 4 23 S4WA5226R 220030120A7200 ENGINE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE LEAKING E S4WAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP075226R1803 3144 22043 THE ENGINE WAS EXPERIENCING UNUSUALLY HIGH OIL CONSUMPTION. THERE WAS NOT AN OBVIOUS LEAK AND AFTER CONSULTING WITH MANUFACTURER, THEY SUGGESTED WE REMOVE AND SEND IN FOR THEM TO REPAIR. APPARENTLY THEY KNOW OF AN INTERNAL LEAK CAUSING THE HIGH CONSUMPTION. OIL USAGE WAS APPROXIMATELY 1.0 QT PER FIVE HOURS 1G71 3U3 U H9EU E00054EN 20030423001102003042300110NM 2003 4 23 F3LA200300072 120030218A5320 PANEL BOEING737 7372Y5 1384554NM FUSELAGE PUNCTURED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED SMALL PUNCTURE IN TRANSITION PANEL BETWEEN STA. 767 AND 794. REPAIRED PANEL PER SRM 53-10-13 AND SOPM 20-4-02. 2L72 4U RTA16WE 20030423001152003042300115EU 2003 4 23 U30A200300002 120030109A2760321000M03 COMPUTER AIRBUS320 A320212 3930322EU ZONE 211 INTERMITTENT A U30AK NONE O OTHER ININSP/MAINT 1 EA17265AV 427 DURING INSPECTION AFTER FLT 314 AT BWI, INTERROGATED CFDS & FOUND MESSAGE: "SEC 1 OR INPUT OF CAPT ROLL CTL SSTU 4CE1". CAATS RECOMMENDS REPLACEMENT OF SEC NR 1 (SPOILER AND ELEVATOR COMPUTER). REPLACED SEC NR 1 I/A/W AMM 27-94-34-000-001. PERFORMED OPS CK WITH NO DEFECT. THIS SDR AMMENDED ON 2/25/2003 TO DOCUMENT ADDITIONAL MAINTENANCE ACTIVITY. THE # 1 SEC (P/N B372BAM0508, MFG BY THALES, S/N 5894 DID NOT CORRECT ORIGINAL DISCEPANCY. DUE TO REPEAT CFDS MESSAGE "SEC 1 OR INPUT OF CAPT ROLL CTL SSTU 4CE1", THE SSTU (SIDE STICK TRANSDUCER UNIT) 4CE1 WAS REPLACED I/A/W AMM TASK 27-92-41-000-002 AND OPERATIONALLY CHECKED I/A/W AMM 27-92-41-710-001. THE SSTU REPLACEMENT TOOK PLACE AT TAT 33661.8 AND TAC 13328 ON2L72 4F RTA28NM 20030423001232003042300123WP 2003 4 23 UPS03840275 120030311A5270H206B SWITCH DOUG DC8 DC871F 302199DWP MLG DOOR INOPERATIVE A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01748UP 45948 DOORS NOT LATCHED LIGHT ILLUMINATED REMAINED ON AFTER GEAR RETRACTION (LEFT GEAR DOOR). RECYCLED GEAR, BROUGHT FLAPS TO 10 DEG, LIGHT EXTINGUISHED. BROUGHT FLAPS UP, RESUMED NORMAL FLIGHT. CHECKS OK ON GROUND. REMOVED AND REPLACED LEFT ALT GEAR DOOR SWITCH. PRECAUTIONARY INSP GEAR AND DOOR UPLATCHES. COULD NOT DUPLICATE SWITCH WAS CHANGED PRECAUTIONARY. 2L74 4F RT4A25 20030421000822003042100082NM 2003 4 21 DL777030091 120030125A2150 A/C PACK BOEING777 777232 1385232NM LEFT ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27861DA 29952 STRONG FUMES FROM LEFT PACK ON CLIMBOUT BELOW 12,000 AND ON DESCENT 12,000 TO LANDING FUMES SMELLED LIKE OIL OR ENG EXHAUST ODOR ISOLATED TO FLIGHT DECK AREA ONLY. NO ODOR NOTED IN CABIN. BOTH ENGINES NEEDED NO OIL SERVICING. BOTH OIL QTY OK, FWD LT PACK TO MCO/PLAC PER MEL 21-51-01. LEFT PACK INOP. 2L72 4F RTT00001SE 20030421001212003042100121NM 2003 4 21 QXEA0300317 120030303A315035138505004 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09411QX4047 4047 4055 GEG ON FLIGHT 2304- SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT ON MASTER WARNING PANEL ONLY. REMOVED AND REPLACED WARNING PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030327001402003032700140GL 2003 3 27 C2XA03IA006 220030124A732023074001 FADEC EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL E/E BAY INOPERATIVE A C2XAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW2716951 145063 CAE311671 ON TAKEOFF ROLL THE CREW NOTED LOW N1 ON ENGINE NR 1. THE CREW ABORTED TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE NR 1B FADEC, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20030327001492003032700149SO 2003 3 27 C2XA03IA019 120030212A3350MS3476L106S CONNECTOR EMB 145 EMB145LR 3260212SO CABIN DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715555 145594 DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTING FAILED TO ILLUMINATE. MAINTENANCE RESECURED THE EMERGENCY LIGHTS CONNECTOR PLUG, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001552003032700155SO 2003 3 27 C2XA03IA029 120030315A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715555 145594 DURING SCHEDULED MAINTENANCE THE EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE DIM. MAINTENANCE REMOVED AND REPLACED THE NR 3 LIGHT BATTERY PACK. THE SYSTEM OPERATIONALLY TESTED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001562003032700156SO 2003 3 27 C2XA03IA030 120030315A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715555 145594 DURING SCHEDULED MAINTENANCE THE EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE DIM. MAINTENANCE REMOVED AND REPLACED THE NR 4 LIGHT BATTERY PACK. THE SYSTEM OPERATIONALLY TESTED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001602003032700160SO 2003 3 27 C2XA03SH007 120030218A531014521725615 BEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 DURING C-CHECK THE RIGHT DIGITAL BEAM AFT OF SERVICE DOOR WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 22 TO 23. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327001892003032700189EA 2003 3 27 CA030211001 120030204A5751C6WA110137 RIB DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA RT WING AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACKED RIB FLANGE OUTBOARD MOST RIB WING STATION 376.20. 1H72 3T4 TRTA9EA E4EA 20030902000432003090200043NE 2003 9 2 ALG2003F00058 120030403A2612 LIGHT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL FIRE HANDLE INOPERATIVE A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03741SW 760070 DURING START, THE NR 2 ENGINE FIRE DETECTION (T) HANDLE LIGHT WOULD NOT ILLUMINATE. THE MECHANIC REPAIRED THE WIRE IAW MM. OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20030828001332003082800133 2003 8 28 MWEA030331 420030826A34205223120005 AMPLIFIER DOUG DC9 DC932 3022066WP COCKPIT INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31302ME 47102 CAPTAIN'S ATTITUDE INICATOR SHOWS GYRO FLAG DURING ANY ATTITUDE CHANGE. REMOVED AND REPLACED NR 1 INSTRUMENT AMPLIFIER. 2L72 4F A6WE 20030829000052003082900005 2003 8 29 52532 420030713A3418 SWITCH BEECH 1900 1900D 1154162CE STALL WARNING OUT OF ADJUST A AMWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07231YV UE231 ON FLIGHT 9415 FROM PANAMA CITY FLORIDA TO PENSACOLA FLORIDA, AFTER TAKEOFF FROM PANAMA CITY FLORIDA, THE STALL WARNING WENT OFF AND WOULD NOT SILENCE. THE AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE RE-ADJUSTED THE SWITCHES. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030829000072003082900007WP 2003 8 29 ARWA20030511 120030527A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT FUSELAGE INNER SKIN WITH CORROSION BETWEEN STATION 1660 AND STATION 1680, BETWEEN L-24R AND L-25R. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, REMOVED DAMAGED AREA AND FABRICATED PARTS IAW REPAIR ORDER AROW-031RO-7, REV IR, AND DRAWING AIPSAC-N784AL-06/03, REV IR, SHEET A.1 TO A.5, DATED 05/08/03. TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW REPAIR ORDER AROW-031RO-7, REV IR AND DRARWING AIPSAC-N784AL-06/03, REV IR, SHEET A.1 TO A.5, DATED 05/08/03. ISSUED FAA FORM 8110-3. 2L74 4F 4A25 20030829000302003082900030NM 2003 8 29 CALA0300488 120030824A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND WEB AT RT LAV WATER SUPPLY LINE FITTING AFT OF STA 1006 CORRODED. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-60-15. 2L72 4F RTA16WE 20030722000742003072200074NM 2003 7 22 SWAA031502 120030702A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 11R AND STR 12R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030722000922003072200092EA 2003 7 22 COMA0360323 120030715A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01962CA 7123 FLIGHT 5698 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030718000462003071800046WP 2003 7 18 AMTA200300743 120030409A5310 FITTING LKHEED1011 10113853 5265020WP CARGO DOOR FRAMEGOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 C-1A DOOR LOWER AFT LATCH ATTACH FITTING GOUGED. REPLACED FITTING IAW MM 52-35-01 AND 52-35-05. (M) 2L73 4F A23WE 20030721001182003072100118NM 2003 7 21 VNAA0306015 120030627A3300 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07423JS 3032 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT WORKING AT SEAT 9A. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR PATH LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030722000072003072200007NM 2003 7 22 2003F00435 120030310A5754 BRACKET BOEING727 727222 1384073NM NR 6 SLAT ACT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT NR 6 SLATE ACTUATOR SUPPORT BRACKET. ACCOMPLISHED AN HFEC INSPECTION ON RIGHT WING NR 6 SLAT ACTUATOR OUTBOARD MOUNT BRACKET. NO CRACKS NOTED. (M) 2L73 4F A3WE 20030722000212003072200021NM 2003 7 22 2003F00449 120030310A5754 RETAINER BOEING727 727222 1384073NM NR 5 SLAT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT RIGHT WING NR 5 SLAT OUTBOARD SEAL RETAINER. REMOVED AND REPLACED RIGHT WING NR 5 SLAT, OUTBOARD HOOK SEAL, UPPER LEADING EDGE WING, OUTBOARD SEAL RETAINER TRIM. (M) 2L73 4F A3WE 20030722000522003072200052NM 2003 7 22 SWAA031510 120030708A335065C34691 LIGHT BOEING737 7373H4 1384600NM ROW 23 INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED A1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 23 DEF. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030722000862003072200086EU 2003 7 22 AWXA200300786 120030611A5347D5347217220000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF SEAT TRACK EXTRUSION AT FR 67, Y1321. MAINTENANCE REMOVED DAMAGED SEAT TRACK EXTRUSION BETWEEN AT FR 67, Y1321; FABRICATED A NEW REPLACEMENT SEAT TRACK EXTRUSION; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 39-41, FIG 18. 2L72 4F RTA28NM 20030722000972003072200097 2003 7 22 SWAA031446 420030628A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030722001012003072200101 2003 7 22 SWAA031474 420030704A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29415WN 0015 29836 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030722001092003072200109NM 2003 7 22 AWXA200300718 120030611A5312651630086 FRAME BOEING737 7373Y0 1384671NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A 2 INCH CRACK WAS FOUND ON BS 178 BULKHEAD LT SIDE FRAME AT AFT SIDE OF CENTER RADIUS WL 207. MAINTENANCE REMOVED LT SIDE FRAME AT BS 178, WL 207; FABRICATED A NEW REPLACEMENT SIDE FRAME, INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 3 & 4. 2L72 4F RTA16WE 20030722001152003072200115 2003 7 22 SWAA031423 420030627A2565D31354 SLIDE BOEING737 7372H4 138448CNM FWD PAX DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29061SW 21970 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F A16WE 20030722001322003072200132NM 2003 7 22 AWXA200300659 120030516A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 1.0, WL 192. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT LBL 1.0, WL 192 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08 PG 213. 2L72 4F RTA16WE 20030723000042003072300004NM 2003 7 23 USAA030101 120030620A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 FOUND INTERCOSTAL CRACKED .5 INCH, STATION 420 OBL INTERCOSTAL TOP RADIUS. REPLACED INTERCOSTAL PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20030723000082003072300008WP 2003 7 23 GTIA030492 120030620A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FOUND CABIN FLOORBOARD STATION 617-674 STIFFENER DELAMINATED FROM BOTTOM. RESEALED DISBONDED STRIPS. (M) 2L72 4F A6WE 20030723000192003072300019NM 2003 7 23 2003F00470 120030520A5533 BEARING BOEING727 727222 1384073NM VERTICAL STAB CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077639U 19912 AT C-CHECK, FOUND RIGHT FIN UPPER STABILIZER HINGE FITTING BEARING CRACKED AND BOTH RETAINERS CORRODED AT BS 1586. REMOVED AND REPLACED RIGHT STABILIZER HINGE BEARING ASSEMBLY. (M) 2L73 4F A3WE 20030723000242003072300024 2003 7 23 UIEA200300030 420030627A34212591201921 COMPUTER BOEING747 7472F6B 1384807NM COMPASS MALFUNCTIONED A UIEAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15535MC 21833 AIR TURNBACK, AT APPROXIMATELY 80-85 KNOTS ON TAKEOFF ROLL, HEADING FLAG ON CAPTAIN'S HSI AND FO'S RMI WITH FILGHT DIRECTOR WARNING LIGHT ON CAPTAINS SIDE. FLAG REMAINED IN FIEW ENTIRE FLIGHT. APPROXIMATELY 5 DEGREES DIFFERENCE IN NR 1 COMPASS VS NR 2 COMPASS AIRCRAFT RRETURNED TO AMS, 24,000 KGS OF FUEL DUMPED. FOUND WIRE SHORTED TO GROUND W153-1F263-22. REPLACED WIRE FROM D1166P TO TX214H26 AND REPLACED COMPAS COUPLER IAW MM 34-12-00 SATISFACTORY. ALSO, REPLACED INU NR 1 AND NR 3 ACC MM 34-41-03 P/N 7886580-011. REPLACED CIWS COMPUTER ACC MM 34-44-01 P/N 777-1826-004. REPLACED CAPTAINS HSI ACC MM 34-41-06 P/N 2592639-901. ALL OPERATIONAL CHECKS SATISFACTORY. (M) 2L74 4F A20WE 20030723000332003072300033EU 2003 7 23 2003F00472 120030623A3250200490001 CONTROL UNIT FOKKERF27 F27MK600 4990706EU NLG STEERING INTERMITTENT A COEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM13703FE 10420 NOSE WHEEL INTRANSIT LIGHT REMAINED ON AFTER TAKEOFF WITH LANDING GEAR SELECTOR UP. THE PRESSURE FAIL LIGHT DID NOT ILLUMINATE. NOSE WHEEL STEERING WAS THEN SWITCHED OFF AND THE LANDING GEAR WAS EXTENDED WITH SIX GREEN INDICATED, HOWEVER THE TILLER REMAINED UNCENTERED. THE CREW DECLARED AN EMERGENCY AND TURNED BACK TO CWA. ABOUT SEVEN MINUTES AFTER LOWERING THE GEAR, THE TILLER RETURNED TO THE CENTERED POSITION. THE AIRCRAFT LANDED IN CWA WITHOUT FURTHER INCIDENT. AFTER FULL STOP, NOSE WHEEL STEERING WAS TURNED ON AND WORKED FINE. MAINTENANCE JACKED THE AIRCRAFT, INSPECTED AND LUBED ALL NOSE GEAR SWITCHES AND COMPONENTS, MADE REPEATED FUNCTIONAL TESTS OF THE NOSE GEAR STEERING. COULD NOT DUPLICATE. (M)2H72 4T A817 20030723000422003072300042EU 2003 7 23 USAASA03071 120030627A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19104UW 0863 THE EMERGENCY LIGHTS SYSTEM TEST FAILED. MAINTENANCE REPLACED THE FORWARD AND AFT POWER SUPPLY UNITS, 10WL AND 13WL. (M) 2L72 4F RTA28NM 20030723000442003072300044NM 2003 7 23 TSAA0353134 120030505A5310 SHEAR TIE BOEING737 73725A 1384481NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DAMAGED SHEAR TIE DISCOVERED AT BD 908 BETWEEN STRINGERS 14 AND 15 LEFT. CUTOUT DAMAGED SECTION. FABRICATED NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-04, FIGURE 10. (M) 2L72 4F RTA16WE 20030723000462003072300046NM 2003 7 23 TSAA0353136 120030505A5313 STRINGER BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 CORROSION DISCOVERED AT BS 967, LBL 7, AND WL 171. CUTOUT DAMAGED PORTION OF THE STRINGER. FABRICATED NEW STRINGER SECTION, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3. (M) 2L72 4F RTA16WE 20030723000582003072300058WP 2003 7 23 GTIA030483 120030624A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 EMERGENCY LIGHT BELOW COALESCER UNITS IS INOPERATIVE. REPAIR WIRE. OPS CHECK NORMAL. (M) 2L72 4F A6WE 20030723000622003072300062WP 2003 7 23 GTIA030490 120030620A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP CABIN DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 CABIN FLOORBOARD DELAMINATED AND NUMEROUS INSERTS CORRODED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20030723001092003072300109NM 2003 7 23 AWXA200300689 120030611A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 18 DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 LAS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030723001102003072300110NM 2003 7 23 AWXA200300690 120030611A3397BMS13311122 WIRE BOEING737 73733A 1384673NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 PHX - EEL - DURING INSPECTION THE EMERGENCY PATH LIGHTING DID NOT ILLUMINATE AT L1 & R1 DOORS, AND SEAT ROWS 1-4. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHTING POWER SUPPLY AND REPAIRED A BROKEN WIRE AT POWER SUPPLY CONNECTOR. OPERATIONAL CHECK WAS GOOD. PART NAME; POWER SUPPLY, MFG; RADIANT ILLUM, P/N 100865. 2L72 4F RTA16WE 20030723001132003072300113NM 2003 7 23 DHL2003727006 120030703A26111000649 SMOKE DETECTOR BOEING727 727228 1384083NM CARGO BAY WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01727DH 20204 NR 2 LEFT MAIN CARGO SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED NR 2 LEFT SMOKE DETECTOR IAW BMM CHAPTER 26-17-01, OPS CHECKED GOOD. 2L73 4F RTA3WE 20030723001152003072300115NM 2003 7 23 DL76S030503 120030602A5330NA SKIN BOEING767 767332 1382001NM STA STR3L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27124DE 23438 MECHANIC FOUND 2 INCH CRACK IN FUSELAGE SKIN RT SIDE STA 1654.5 STR 3R. ALSO, FOUND STRINGER 3R AND 3L CRACKED AT SAME LOCATION. REPAIRED CRACK. 2L72 4F RTA1NM 20030723001212003072300121NM 2003 7 23 DL757030512 120030603A5330146N31712 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27633DL 23614 FUSELAGE SKIN WAS FOUND WITH 2 LIGHTNING STRIKES IN THE CROWN SKIN AREA. ONE STRIKE WAS AT FS 1540 AND STRINGER 6R AND THE OTHER STRIKE WAS AT FS 1560 AND STRINGER 5R. THE LIGHTNING STRIKES WERE REMOVED WITH SMALL CUTOUTS. EACH CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385182-14, REV A. 2L72 4F RTA2NM 20030721001242003072100124NM 2003 7 21 SWAA031488 120030705A53146545866 KEELBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 650 AND BS 663. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20030722000042003072200004NM 2003 7 22 2003F00432 120030308A5320655617522 PLATE BOEING727 727222 1384073NM CARGO DOOR CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT C-2 DOOR SCUFF PLATE. REMOVED, REPAIRED AND REINSTALLED SCUFF PLATE ON C-2 DOOR, LOWER CUTOUT. (M) 2L73 4F A3WE 20030722000682003072200068NM 2003 7 22 SWAA031457 120030702A53156584176 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 706, LBL 57. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030722000982003072200098NM 2003 7 22 SWAA031447 120030627A532065C27314 STRINGER CLIP BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F A16WE 20030722001192003072200119NM 2003 7 22 SWAA031470 120030703A53146545866 KEELBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM CORRODED AT BS 520-540. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20030722001252003072200125NM 2003 7 22 AWXA200300742 120030621A5414D54530052201 SKIN AIRBUSA319 A319132 3930340NM RT PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28820AW 1397 MCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054; INSTALLED REPAIR PART IAW A319 SRM 54-50-00 PG 106 FIG 104. 2L72 4F RTA28NM 20030723000112003072300011WP 2003 7 23 GTIA030495 120030612A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - AFT PIT STATION 1287-1309 STRINGER 18R FLOOR PANEL CRACKED. TRIMMED OUT DAMAGED AREA. LOCATED AND DRILLED DOUBLER/FILLERS. INSTALLED DOUBLER/FILLERS. (M) 2L72 4F A6WE 20030723000402003072300040 2003 7 23 MEX2003248 420030625A34228221088001 DISPLAY DOUG DC9 DC982 3022082WP COCKPIT FAILED A ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23EIBTX 49660 AIRCRAFT ARRIVED WITH CAPTAIN REPORT THAT DURING CRUISE THE LT EHSI LOST ALL NAV INFORMATION. THE EHSI INDICATOR WAS REPLACED IAW MM 34-22-03, ALL TESTS CORRECT. (M) 2L72 4F A6WE 20030723000482003072300048EA 2003 7 23 A6WA200340100 120030703A2613 WIRE CNDAIRCL600 CL6002B19 1900309EA OVERHEAT SYS OUT OF POSITION A A6WAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL31408AW 7568 BLEED AIR DUCT MASTER WARNING WOULD COME ON INTERMITTENTLY AND REPEATEDLY IN FILGHT 31,000 FEET. COMPLIED WITH QRH MSS EXTINGUISHING 55 PERCENT N1 LEFT ENGINE. STRAIGHTENED WIRE AT 14TH STAGE BLEED AIR DUCT AND TIGHTENED CLAMP AT AIR SWITCH. RAN ENGINE, OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA21EA 20030723000542003072300054WP 2003 7 23 GTIA030482 120030615A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP CARGO BAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AFT PIT STATION 1117-1155 STRINGER 18L FLOOR WEB CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030723000602003072300060WP 2003 7 23 GTIA030485 120030620A2420 GENERATOR DOUG DC9 DC982 3022082WP LEFT FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 SELECTED EMERGENCY POWER AFTER LEFT GEN FAIL. CAPTAINS ATTITUDE FLAGS IN VIEW AND UNPOWERED EMER AC AND EMG DC ANNUNCIATOR LIGHTS REMAINED OUT AND ALL INDICATIONS WERE BUSSES POURED FOR EMERGENCY AC AND DC. PERFORMED OPS CHECKS ON EMERGENCY POWER SYSTEM, NO DEFECTS NOTED. (M) 2L72 4F A6WE 20030723001222003072300122NM 2003 7 23 DLM88030513 120030604A5321024201934 FLOOR PANEL DOUG MD88 MD88 3023688NM C5 CARGO PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27911DL 49542 ON ARRIVAL IAD FOUND HOLE IN FLOOR OF NR 5 BAG BIN. REPAIRED PER DRD 5305D. 2L72 4F RTA6WE 20030723001252003072300125NM 2003 7 23 AWXA200300622 120030529A3350BACC18Z5R CIRCUIT BREAKER BOEING737 737277 1384570NM COCKPIT INTERMITTENT A AWXAH DEACTIVATE SYST/CIRCUITS S AFFECT SYSTEMS CRCRUISE 1 WP28189AW 22656 EN ROUTE FROM AUS TO PHX THE EMERGENCY EXIT LIGHTS CAME ON WITH THE SWITCH IN ARMED POSITION, TURNED SWITCH OFF TO CONSERVE BATTERIES. MAINTENANCE TROUBLESHOT AND FOUND THE EMERGENCY EXIT LIGHT POWER CIRCUIT BREAKER (C250) WAS INTERMITTENT. REMOVED AND REPLACED CIRCUIT BREAKER, OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. 2L72 4F RTA16WE 20030724000032003072400003NM 2003 7 24 DL733030519 120030605A53306545775594 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27951WP 22951 THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK AT FS 727D JUST ABOVE STRINGER 23R RUNNING ALONG THE BONDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A 4 X 1 INCH CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385208-14, REV B. 2L72 4F RTA16WE 20030724000042003072400004NM 2003 7 24 DL73S030520 120030606A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 THE FUSELAGE SKIN AT FS 750 WAS FOUND WITH A 2 INCH CRACK RUNNING ALONG THE EDGE OF THE BONDED DOUBLER AT STRINGER 18R. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385222-14. 2L72 4F RTA16WE 20030724000072003072400007NM 2003 7 24 DL76P030523 120030606A2121 FAN BOEING767 767332 1382001NM CABIN INOPERATIVE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27140LL 25988 AT CRUISE, SUDDEN ODOR IN COCKPIT THAT SMELLS LIKE FAULTY LIGHT BALLAST AND SEEMS TO BE STRONGEST NEAR/UNDER GLARESHIELD. TURNED OFF ALL LIGHTS. MAINTENANCE NEEDS TO CHECK ODOR IN CARGO AND E/E. OPERATED BALLAST FOR ALL COCKPIT LIGHTING PER FLIGHT CREW ODOR CAME FIRST FOLLOWED BY FWD EXHAUST FAN STATUS. C/B PULLED & COLLARED FWD TO MCO & PLACARD. 2L72 4F RTA1NM 20030724000092003072400009 2003 7 24 DLM88030526 420030607A2565D29985103 SLIDE DOUG MD88 MD88 3023688NM L2 DOOR UNSERVICEABLE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27985DL 53312 L2 SLIDE FEEL OUT OF DOOR WHEN DOOR WAS OPENED. FOUND SLIDE STILL ARMED INFLATED WHILE HANGING BUT DID NOT OPEN. REPLACED SLIDE PER MM. 2L72 4F RTA6WE 20030724000102003072400010NM 2003 7 24 DL738030527 120030607A3350S283E6032 CHARGER BOEING737 737832 13844CFNM ROW 16 UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO273765 30819 ON CHECK FOUND EMERGENCY LIGHTS ON ROWS 16 - 18 INOP. REPLACED EMERGENCY LIGHTS BATTERY CHARGER. ALL LIGHTS OPERATE OK. 2L72 4F RTA16WE 20030724000122003072400012EA 2003 7 24 COMA0360317 120030706A274070608 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO01924CA12320 7026 FLIGHT 5489 DURING T/O, STAB TRIM FLUCTUATED FULL VP AND DOWN. REPLACED THE HSTCU. 2L72 4F RTA21EA 20030724000162003072400016 2003 7 24 AWXA200300679 420030609A2565D30665105 SLIDE AIRBUS320 A320231 3930325EU R-2 DOOR LEAKING A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW347156309 091 FLIGHT CREW REPORTED R-2 DOOR SLIDE PRESSURE INDICATOR NOT IN THE GREEN AREA. MAINTENANCE REMOVED AND REPLACED R-2 DOOR SLIDE IAW T/C R1C25304, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030724000172003072400017EU 2003 7 24 AWXA200300680 120030607A261346619 THERMOCOUPLE AIRBUS320 A320231 3930325EU NR 2 BRAKE FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28626AW 65 ON TAKEOFF ROLL AT LAS EN ROUTE FOR PDX NR 2 BRAKE TRIGGERED HOT BRAKE ECAM MESSAGE, REJECTED TAKEOFF AT 85 KTS. NR 2 BRAKE INDICATED 580 CELSIUS MAXIMUM TEMPERATURE. MAINTENANCE PLACED SYSTEM ON MEL 32-47-01, COND 1 NR 2 BRAKE TEMP MONITORING UNIT INOP AND COMPLIED WITH MEL TASK PROCEDURE 05-51-16-700-001. WHEN AIRCRAFT ARRIVED BACK IN LAS MAINTENANCE REMOVED AND REPLACED THE NR 2 BRAKE TEMPERATURE SENSOR IAW AMM 32-47-15-401. PERFORMED BRAKE SYSTEM TEMPERATURE ADJUSTMENT TEST IAW AMM 32-47-00-501 AND ALTERNATE BRAKE & ANTI SKID SERVICING IAW AMM 32-43-00-301, SYSTEM OPERATES NORMALLY. 2L72 4F RTA28NM 20030724000182003072400018EU 2003 7 24 AWXA200300681 120030607A2133VFT210A1 VALVE AIRBUS320 A320232 3930326EU ZONE 127 DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28642AW2781920552 584 ON CLIMBOUT OF PHX EN ROUTE FOR SAN RECEIVED SKIN AIR VALVE FAULT, AMBER XX'S ON INLET VALVE. VALVE WOULD NOT CLOSE AFTER FOLLOWING ECAM PROCEDURE. TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE COMPLIED WITH MEL PROCEDURE 21-26-05 COND. 1 DEACTIVATING THE SKIN AIR INLET VALVE IN THE CLOSED POSITION. ON 06/11/2003 IN PHX MAINTENANCE REMOVED AND REPLACED THE SKIN AIR INLET VALVE IAW AMM 21-26-52, PG. 401, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAILURE OF SKIN AIR INLET VALVE S/N 2173. FAILED FUNCTIONAL TEST FOR HIGH RESISTANCE, FOUND A BAD MOTOR, WORN SEALS, AND A BAD PIN. REPLACED MOTOR, PLUG, 4 EACH PINS 3 EACH PACKINGS. 2L72 4F RTA28NM 20030724000202003072400020NM 2003 7 24 AWXA200300683 120030515A53306545800219 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A .375 INCH CRACK WAS FOUND AT FASTENER HOLE ON FUSELAGE SKIN, LOWER FORWARD CORNER OF R-1 DOOR CUTOUT BS 294.5. MAINTENANCE REMOVED FASTENER AT LOWER FORWARD CORNER OF R-1 DOOR CUTOUT BS 294.5; PERFORMED NDT INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED A DOUBLER; AND INSTALLED REPAIR PART IAW SB 737-53-1074, AND ER 15-5313-03148-ES3. 2L72 4F RTA16WE 20030724000312003072400031NM 2003 7 24 DL76L030532 120030610A33200581416 BALLAST BOEING767 767332 1382001NM CABIN LIGHTS ODOR A DALAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27177DN 25122 ELECTRICAL ODOR NOTICED BY F/AS BETWEEN ROWS 20 AND 30. ALL OVERHEAD LIGHTS WERE TURNED OFF AND ODOR DISAPPEARED. TURNED ALL OVERHEAD LIGHTS ON FOR 1.5 HRS. UNABLE TO DETECT ODOR. SUSPECT INDIRECT CEILING LIGHTS BALLAST ABOVE SEATS 20-21AB. REPLACED SAME. OPS CHECK NORMAL. 2L72 4F RTA1NM 20030724000472003072400047NM 2003 7 24 DL76S030547 120030613A33500201991005 LENS BOEING767 767332 1382001NM EMERGENCY LIGHT BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27122DL 23436 ONE WHITE EMERGENCY LIGHT IS BROKEN ON SEAT 2B. REPLACED LENS AND SHROUD. 2L72 4F RTA1NM 20030724000592003072400059NM 2003 7 24 AWXA200300714 120030617A5610NP1653116 WINDSHIELD AIRBUSA319 A319132 3930340NM COCKPIT CRACKED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28809AW13841 1111 AT CRUISE ALTITUDE EN ROUTE FROM BOS TO PHX THE FIRST OFFICERS WINDSHIELD CRACKED, DIVERTED TO CMH AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM 56-11-11-401. CENTRAL FAULT DISPLAY SYSTEM TEST OF WINDOW HEAT CONTROLLER NR 2 WAS GOOD, WINDOW HEAT NORMAL. VENDOR CONFIRMED FAILURE OF F/O WINDSHIELD S/N 99172H1464, FAILURE ANALYSIS WAS NOT ACCOMPLISHED. WINDOW WAS SCRAPPED AT VENDOR. 2L72 4F RTA28NM 20030724000632003072400063NM 2003 7 24 AWXA200300772 120030702A3397BACC18Z5R CIRCUIT BREAKER BOEING737 737277 1384570NM EMERGENCY LIGHT WEAK A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 EN ROUTE FROM AUS TO PHX ALL EMERGENCY EXIT LIGHTS ILLUMINATED. EMERGENCY EXIT LIGHT WAS SWITCHED OFF TO CONSERVE BATTERY ENERGY. MAINTENANCE FOUND A WEAK EMERGENCY LIGHT SYSTEM CONTROL CIRCUIT BREAKER (5 AMP) ON THE P-18 PANEL. REMOVED AND REPLACED 5 AMP CIRCUIT BREAKER ON THE P-18 PANEL. EMERGENCY LIGHT CHECK WAS GOOD. 2L72 4F RTA16WE 20030724000702003072400070EU 2003 7 24 AWXA200300767 120030610A5313D5348004720400 STRINGER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 30 RT 3 INCHES AFT OF FR 65 IN A 6 X 3 INCH AREA. MAINTENANCE REMOVED DAMAGED AREA OF STRINGER 30 RT 3 INCHES AFT OF FR 65; FABRICATED A NEW SECTION OF STRINGER PER DWG 18D53480047 AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-0013 PG 201-210 FIG 201. 2L72 4F RTA28NM 20030724000712003072400071EU 2003 7 24 AWXA200300768 120030611A5320D5347112420000 PLATE AIRBUS320 A320231 3930325EU FLOOR WEB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK TWO AREAS OF EXFOLIATION CORROSION WERE FOUND ON LOWER SURFACE OF FLOOR WEB (SHEAR PLATE) AT FR 70, Y-1193. MAINTENANCE REMOVED CORRODED SHEAR PLATE AT FR 70, Y-1193; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-12. 2L72 4F RTA28NM 20030724000762003072400076NM 2003 7 24 AWXA200300699 120030613A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 23 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030721001192003072100119NM 2003 7 21 SWAA031483 120030705A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29784SW 29810 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (7 EA) AT ROWS NR 1, 3, 5, 19, 20, 22 AND 23. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030721001342003072100134NM 2003 7 21 SWAA031517 120030709A573065C26714 SKIN BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C2 CHECK, FOUND LT WING SKIN CRACKED AT INBD FIXED L/E JUST OUTBD OF KRUGER FLAP. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030722000642003072200064NM 2003 7 22 SWAA031513 120030707A2761251A12403 ACTUATOR BOEING737 7377H4 1384404NM SPOILER FAULTY A SWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW29729SW 27861 ABORTED TAKEOFF, WITH POWER LEVERS FWD, TAKEOFF WARNING HORN SOUNDED WITH SPEED BRAKES EXTENDED AND LIGHT ILLUMINATED. REMOVED AND REPLACED NR 9 SPOILER ACTUATOR AND SPEED BRAKE EXTEND LIGHT SWITCH PER MM. 2L72 4F RTA16WE 20030722000902003072200090NM 2003 7 22 AWXA200300789 120030708A3242 MONITOR AIRBUS AIRBUSA319 A319132 3930340NM LT MLG BRAKE MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28660AW 3654 1234 ON TAKEOFF ROLL AT LAS EN ROUTE FOR LAX THE LT OUTBOARD BRAKE INDICATOR SPIKED TO 610 DEGREES CELSIUS, AND THE LT INBOARD TO 330 DEGREES CELSIUS. REJECTED TAKEOFF UNDER 60 KTS. MAINTENANCE REMOVED AND REPLACED THE LT BRAKE TEMPERATURE MONITOR IAW AMM 32-47-18, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST OF BRAKE TEMPERATURE MONITOR S/N 3654 (CHANGED TO S/N T0117) CONFIRMED FAILURE OF UNIT. TEARDOWN OF UNIT REVEALED 2 EACH CONNECTORS DEFECTIVE. REMOVED AND REPLACED CONNECTORS (P/N'S 16N8B3ASNL & A1001427) IAW CMM 32-47-18 & 18A, REV 08 & 03. 2L72 4F RTA28NM 20030722001062003072200106NM 2003 7 22 SWAA031479 120030702A57536546435 SKIN BOEING737 7373H4 1384600NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED C4 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE INBD END. REMOVED AND REPLACED LT OUTBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030722001132003072200113NM 2003 7 22 SWAA031435 120030629A33506104781 BATTERY PACK BOEING737 7373Y0 1384671NM CABIN FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 OVERWING EMERGENCY EXIT LIGHTS ILLUMINATE INTERMITTANTLY. REMOVED AND REPLACED OVERWING BATTERY PACKS (2 EA). 2L72 4F RTA16WE 20030722001182003072200118NM 2003 7 22 SWAA031426 120030626A3350AD20131A BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT IN FWD CABIN INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030722001202003072200120NM 2003 7 22 SWAA031471 120030703A53106545871 DOOR FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT NR 4 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030722001292003072200129NM 2003 7 22 AWXA200300654 120030324A53306545765 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 LT BS 387. MAINTENANCE CUTOUT CRACKED SKIN AT STR 4 LT, BS 387; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, A FILLER, 2 EACH INTERNAL DOUBLERS, AND A TAPERED FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 PG 355 FIG 228. 2L72 4F RTA16WE 20030723000722003072300072NM 2003 7 23 VNAA0306016 120030629A2420230GC02Y02 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT GENERATOR FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07432JS1107122 3045 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030723000942003072300094NM 2003 7 23 VNAA0306014 120030625A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07470PS167731226 3006 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030724000112003072400011EA 2003 7 24 COMA0360316 120030707A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01927CA 7031 DURING FLIGHT 5122, L REV UNLOCKED CAUTION MESSAGE APPEARED IN FLIGHT. AIRCRAFT PERFORMED UNSCHEDULED LANDING AT CKB AND DEFERRED LEFT T/R IAW MEL 78-30-01. 2L72 4F RTA21EA 20030724000212003072400021NM 2003 7 24 AWXA200300684 120030514A53304577665 SKIN BOEING737 737277 1384570NM KEELBEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK CORROSION WAS FOUND ON LOWER FUSELAGE SKIN AT BS 727-727A AND LT KEEL BEAM. MAINTENANCE REMOVED EXISTING DOUBLER & TRIPLER AND TRIMMED OUT CORRODED SKIN; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPLACEMENT DOUBLER & TRIPLER, AND 4 EACH FILLERS; AND INSTALLED REPAIR PARTS IAW ER 15-5361-03154-SS3. 2L72 4F RTA16WE 20030724000222003072400022NM 2003 7 24 AWXA200300685 120030514A531050794577 DOOR FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A .25 INCH CRACK WAS FOUND ON FRAME OF R-1 DOOR AT UPPER HINGE CUTOUT. MAINTENANCE PERFORMED A HFEC INSPECTION TO VERIFY END OF CRACK; STOP DRILLED CRACK IAW B737-200 SRM 52-00-2 FIG 7 PG 32. 2L72 4F RTA16WE 20030327001952003032700195CE 2003 3 27 CA030211008 120030107A3233CJ0701 ACTUATOR CESSNA310 T310Q 2074244CE CONT O520 TSIO520B 17040SO MCAULY3AF32C3AF32C87 GL MLG FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CJ0701 ACTUATOR TAB IS A SMALL METAL TAB THAT FITS ON PORT GEAR DOWN SWITCH. TAB FAILED DUE TO METAL FATIGUE CAUSING INTERMITTENT GEAR SAFE LIGHT ON PORT SIDE. 1L72 3O3 O 3A10 E8CE 5 CP22EA 20030325000432003032500043EU 2003 3 25 AWXA200300167 120030219A27303945128102 COMPUTER AIRBUS320 A320231 3930325EU ELAC FAULTY A AWXAH DEACTIVATE SYST/CIRCUITS JFSWARNING INDICATION FLT CONT AFFECTED AFFECT SYSTEMS DEDESCENT 1 WP28626AW4800 1691 65 ON DECENT RECEIVED AN ELEV/AIL COMP (ELAC) NR 2 FAULT, RESET ELAC NR 2. AFTER LEVELING OFF AT 11,000 FT, 250 KTS, WITH A/P ON, A/C DID AN UNCOMMANDED PITCH DOWN, WITH ELAC AIL SERVO FAULT. MINUTES PRIOR TO PITCH DOWN RECEIVED ELAC NR 2 PITCH FAULT. DISCONNECTED A/P AND LANDED W/O EVENT. MAINT R & R ELAC NR 2 COMP, SYS TEST GOOD. PRIOR TO TAKEOFF RECEIVED F/CTL ELAC NR 2 FAULT, AND F/CTL AIL SERVO FAULT. MAINT GROUND SCAN OF ELECTRICAL FLT CONTROL SYS 2, NO FAULTS NOTED. PERFORMED SIDE STICK TRANSDUCER CHECK, CHECKED GOOD. PERFORMED HISTORY CHECK OF ELAC COMP INSTALLED PREVIOUS FLT AND FOUND IT HAD BEEN REPLACED TWICE IN 60 DAYS, NO CORRECTIVE ACTIONS PRIOR TO RETURNING UNIT TO SERVICE. R & R ELAC NR 2 COMP. 2L72 4F RTA28NM 20030325000552003032500055NE 2003 3 25 AWXA200300214 220030227A7200 ENGINE BOEING737 737277 1384570NM PWA JT8 JT8D* NE NR 2 MALFUNCTIONED A AWXAC ABORTED TAKEOFF EP VIBRATION/BUFFET NO WARNING INDICATION TOTAKEOFF 1 WP28183AW 22650 P708359B ON TAKEOFF ROLL AT SLC EN ROUTE FOR PHX FELT STRONG VIBRATION FROM RT SIDE OF AIRCRAFT AND IN RT THRUST LEVER. ALL ENGINE INDICATIONS WERE NORMAL AT THIS POINT WITH NO WARNING INDICATIONS. REJECTED TAKEOFF AT 130 KTS INDICATED AIRSPEED. AS POWER WAS PULLED TO IDLE THE NR 2 ENGINE DECELERATED FASTER THAN NR 1. SHUTDOWN NR 2 ENGINE AND TAXIED TO GATE USING NR 1 ENGINE. MAINTENANCE FOUND DAMAGE TO THE NR 2 ENGINE LOW PRESSURE TURBINE SECTION. REMOVED AND REPLACED NR 2 ENGINE IAW T/C R5M71003, AND R5M78002. STATIC RIG ACCOMPLISHED IAW T/C F5M76001, AND TRIM RUN PERFORMED IAW T/C F5M71002. 2L72 4F4 FRTA16WE E2EA 20030325000932003032500093NM 2003 3 25 375PA0013 120030323A3350 CONNECTOR BOEING737 737317 138447PNM EMERGENCY LIGHT DISCONNECTED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 EMERGENCY EXIT LIGHTS INOP (4 OF THEM HALFWAY DOWN AISLE). FOUND 2 LIGHTS WITH BOTH CONNECTORS DISCONNECTED. REPLACED CONNECTORS AND OPS CHK GOOD PER MM 33-51-02. 2L72 4F RTA16WE 20030325000942003032500094NM 2003 3 25 377PA0011 120030321A335058782 LIGHT BOEING737 7373L9 1384470NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05377PA 23718 ROW 1-4 LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED EMERGENCY FLOOR PATH STRIP ELEMENT IAW MM 33-50-00. TESTS OK. 2L72 4F RTA16WE 20030326000042003032600004NM 2003 3 26 AUS20030089 120030128A2760 CABLE BOEING737 737400 138449ANM CFMINTCFM56 CFM563C 13802EU DRAG CONTROL DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) GROUND SPOILER INTERLOCK VALVE TELEFLEX CABLE DISTORTED DUE TOCABLE BOTTOMING OUT ON VALVE DURING STRUT COMPRESSION. CABLE OUTER CASING WIRES BROKEN. 2L72 4F4 FRTA16WE E21EU 20030326000362003032600036NE 2003 3 26 AUS20030152 220030212A7261F42C11925 HOSE BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE ENGINE OIL PRESSLEAKING W O OTHER EK VIBRATION/BUFFET FLUID LOSS DEDESCENT 1 AUS (AUS) NR 2 ENGINE OIL PRESSURE TRANSMITTER SUPPLY LINE HOSE LEAKING. 2L73 4F4 FRTA3WE E2EA 20030326000432003032600043EU 2003 3 26 AUS20030194 120030214A3110 PANEL BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE INSTRUMENT MISINSTALLED W O OTHER W INADEQUATE Q C TOTAKEOFF 1 AUS (AUS) CAPTAINS INSTRUMENT PANEL DISLODGED AND MOVED REARWARDS DURING TAKEOFF. INVESTIGATION FOUND THAT THE PANEL HAD NOT BEEN CORRECTLY SECURED FOLLOWING MAINTENANCE. PERSONNEL/MAINTENANCE ERROR. 2H74 4F4 F A49EU E6NE 20030326000572003032600057 2003 3 26 CA030131007 420030131A3197 WIRE CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA INSTRUMENT PANELCHAFED W O OTHER L NO TEST CRCRUISE 1 CA (CAN) CREW REPORTED INSTRUMENT PANEL LIGHTS WOULD OPERATE INTERMITTANTLY IN FLIGHT. CONDITION ONLY SEEMED TO OCCUR WHEN PILOT OPERATED THROTTLE CONTROL. MAINTENANCE INVESTIGATING DEFECT DETERMINED THE AIRCRAFT WIRING BUNDLE BEHIND THE PANEL WAS POSITIONED IN SUCH A WAY THAT IT RESTED ON THE TOP OF THROTTLE CONTROL IN AREA WHERE THREADS ARE CUT FOR RETAINING NUT. ONE OF THE WIRES IN THE BUNDLE (FOR THE PANEL LIGHTS) HAD CHAFED THROUGH AND WAS AFFECTED BY THE HAND PRESSURE WHICH ANGLED THE THROTTLE CONTROL JUST ENOUGH TO INITIATE FAULTY CONDITION. WIRING WAS REPAIRED AND WIRE BUNDLE WAS REPOSITIONED AND SECURED. THE LIGHTING CIRCUIT WAS THEN TESTED AS SAT. AIRCRAFT TOTAL TIME WAS 3958.2 HOURS 1H71 3O3 ONT3A12 1E10 20030326001102003032600110EA 2003 3 26 A6WA200340035 120030309A2497 RELAY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 1 BUSS FAILED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31422AW 7341 AC ESSENTIAL BUSS CAUTION MESSAGE. THE AC ESSENTIAL BUSS WOULD NOT ACCEPT POWER FROM EITHER AC BUSS 1 OR AC BUSS 2. T/S IAW FIM 24-20-00. FOUND RELAY K1XD BAD. REMOVED AND REPLACED RELAY K1XD. PN V210D090BC, IAW MM. OPS CHECK GOOD IAW MM. 2L72 4F4 FRTA21EA E15NE 20030326001142003032600114NM 2003 3 26 AMTA200300155 120030129A3350 LIGHT BOEING757 75728A 1384976NM EMERGENCY EXIT BROKEN A AMTAK NONE O OTHER ININSP/MAINT 1 GL11521AT 24368 EMERGENCY EXIT LIGHT AT 2R DOOR BROKEN. REMOVED AND INSTALLED EMERGENCY EXIT LAMP ASSEMBLY AS REQUIRED PER MM CHAPTER 33, OPS CHECK GOOD, OK FOR SERVICE. (M) 2L72 4F RTA2NM 20030327000102003032700010NM 2003 3 27 AWXA200300273 120030316A2560P4010021 BATTERY BOEING737 737277 1384570NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28182AW 22649 FLIGHT CREW REPORTED THAT THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030327000232003032700023EU 2003 3 27 AWXA200300294 120030319A3510MF100511 OXYGEN MASK AIRBUS320 A320232 3930326EU COCKPIT LT SIDE LEAKING A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28654AW141928160 1050 ON CLIMB OUT OF PHX EN ROUTE FOR BOS CREW OXYGEN WENT FROM 1110 PSI TO 420 PSI. TURNED BACK TO PHX FOR REPAIR. MAINTENANCE TROUBLESHOT CREW OXYGEN SYSTEM PER LEAK TEST T/C F8M35301 AND FOUND THE SWEDGES LEAKING ON THE LINES INSIDE BOTH THE CAPTAINS AND LT OBSERVERS OXYGEN MASK BOXES. REMOVED AND REPLACED BOTH MASKS AND BOTH MASK BOXES IAW R1B35301. REACCOMPLISHED LEAK TEST, NO LEAKS WERE NOTED, OXYGEN LEVEL HOLDING STEADY AT 1680 PSI. 2L72 4F RTA28NM 20030327000432003032700043NM 2003 3 27 AWXA200300315 120030228A5320146N5240 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON SUPPORT ANGLE ON UNDER SIDE OF SHEAR DECK AT BS 1715, RBL 20-25. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT BS 1715, RBL 20-25; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 146N5240-11. 2L72 4F RTA2NM 20030327000472003032700047CE 2003 3 27 BSY2003F00009 120030216A213126140629 MODULE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP CABIN PRESSURE INOPERATIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0725AN 35A259 74724 LOST PRESSURIZATION AT 35,000 FT, RETURNED TO (NEW) REMOVED AND REPLACED PRESURIZATION MODULE OPS CHECKED GOOD. 2L72 4F4 F A10CE E6WE 20030421000222003042100022EA 2003 4 21 SWIA200311800 120030224A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07928SW876 876 7701 JUST PRIOR TO TOUCHDOWN RECEIVED A FLAPS FAIL CAUTION MESSAGE. FLIGHT CONTROL PAGE SHOWED FLAPS SET AT 45. FLAPS WOULD NO RETRACT AFTER LANDING. REMOVED AND REPLACED LEFT BPSU. OPS CHECK GOOD. 2L72 4F RTA21EA 20030421000732003042100073NM 2003 4 21 PCAA0303048 120030303A2910 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM NR 1 HYD ISO VALFALSE INDICATIONA PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13979HA 373 PIT-FLIGHT 3890 CREW REPORTED NR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT AND PARTIAL LOSS OF HYDRAULIC FLUID. HYDRAULIC FLUID OBSERVED ON NR 2 ENGINE. MAINTENANCE SERVICED NR 1 AND NR 2 HYDRAULIC RESERVOIRS AND INSPECTED AREA. FLUID WAS FOUND TO BE GLYCOL. CREW GROUND RAN AIRCRAFT. NO LEAKS WERE NOTED. FLAP WELLS, WHEEL WELLS AND CENTER WING AREA WERE INSPECTED. NO LEAKS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421000792003042100079NM 2003 4 21 DL78K030084 120030123A2750285A12001 FSEU BOEING737 737832 13844CFNM E & E BAY FAILED A DALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO273734B 30776 FLAPS STUCK AT 25 DEG ON FINAL WOULD NOT RAISE OR LOWER. T/S PER FIM FAULTS 27-52260 LEG 0 FAULTS 27-53280 LEG2 - 17 CHECKS EXC VOLTAGE INPUT VAC. REPLACED FSEU CHECKS NORMAL. PER AMM FSEU CHECKS NORMAL. RAN FLAPS PER AMM, ALL CHECKS NORMAL. FLAP LOAD RELIEF AND T/E SKEW CHECKS NORMAL PER AMM. 2L72 4F RTA16WE 20030421001722003042100172NM 2003 4 21 KPVA200313 120030307A771230005000034 SIGNAL COND UNIT DHAV DHC8 DHC8103 1386005NM NR 1 ENG TORQUE MALFUNCTIONED A KPVAO OTHER N FALSE WARNING CLCLIMB 1 WP13805WP 353 HNL - FLT 1550 - DURING AND AFTER TAKEOFF, AUTO FEATHER DE-SELECTED BUT ARM LIGHT STILL ILLUMINATED. WHEN POWER REDUCED BELOW 80 PERCENT ARM LIGHT OUT, ABOVE 80 PERCENT ARMED LIGHT ON AGAIN. REMOVED AND REPLACED NR 1 ENGINE TORQUE SIGNAL CONDITION UNIT IAW PW MM CHAPTER 72-01-10 PAGE 414-419/420. OPS CHECK GOOD IAW FEATHER TEST, OPS MANUAL, SECTION NORMAL PAGE 8. (M) 2H72 4T RTA13NM 20030421001782003042100178WP 2003 4 21 GTIA030131 120030220A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND MAIN CABIN FLOOR PANEL STATION 1155 TO STATION 1250 HAS SOFT/MUSHY DETERIORATED SEVERAL INSERTS. FABRICATED FLOOR PANEL. (M) 2L72 4F RTA6WE 20030421001802003042100180WP 2003 4 21 MEX2003058 120030306A2913AS66411LS666 PUMP DOUG DC9 DC987 3022087WP HYD SYSTEM FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23204AM 49404 FLT 413 - MIA-MEX - AIRCRAFT RETURNED TO PLATFORM, LT HYDRAULIC PUMP FAIL. BREAKERS WERE VERIFIED AND CONNECTORS WERE CLEANED. HYD PUMP WAS REPLACED AND TESTS WERE PERFORMED IAW MM 29-10-05, ALL CORRECT. (M) 2L72 4F RTA6WE 20030421002122003042100212NM 2003 4 21 AMTA200300265 120030224A3350 SIGN BOEING737 73783N 13844HINM CABIN DETACHED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11325TZ 32884 'EXIT' SIGN AT 2L DOOR FELL OFF AFTER TAKEOFF. REINSTALLED EXIT SIGN AT 2L DOOR, ORIGINAL SIGN, NO DEFECTS NOTED. OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030422000772003042200077SO 2003 4 22 SIMA200305015 120030125A532014521725001 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 ABI - DURING AN IMBV INSPECTION A LEVEL 2 FINDING WAS FOUND. CORROSION ON LEFT SILL BETWEEN FRAME 19 AND 23. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-02, 51-40-06. (M) 2L72 4T RTT00011AT 20030422001432003042200143NM 2003 4 22 UPS03440259 120030306A7100JT9D7AH COMPRESSOR BOEING747 747121 1384871NM PWA JT9 JT9D7AH 52054NE NR 3 ENGINE STALLED A IPXAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01682UP 20349 AIR TURNBACK NR 3 ENG COMPRESSOR STALL IN CLIMB AT FL190 PAX REPORTED GLOW IN N1 SECTION. EGT RISING, ENG SHUTDOWN. REMOVED AND REPLACED NR ENGINE S/N OFF P685985CN, INSTALLED S/N P662942 PER TC 5000, 5001, 5016 & MM 71-00-00 OPS & LEAK CHECK GOOD. OK FOR CONTINUED SERVICE. 2L74 4F4 F A20WE E20EA 20030423000372003042300037NM 2003 4 23 AUS20030271 120030212A5320 ANGLE BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) VERTICAL ANGLE LOCATED IN THE AVIONICS COMPARTMENT BILGE AT STA 368 LBL 15 CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01. 2L73 4F4 FRTA3WE E2EA 20030423000472003042300047EU 2003 4 23 BAQA085902 120030403A73317440823 METER AEROSPAS365 AS365N2 8680815EU FUEL FLOW FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME6673 6417 COULD NOT SET TOTAL. FLOW WOULD NOT REGISTER. REPLACED WITH SERVICABLE UNIT. 4/11/03 1G72 3U RTH10EU 20030423000612003042300061 2003 4 23 BAQA085898 420030402A3442071015190101 DISPLAY AGUSTAA109 A109E 0260119EU WX RADAR SYS MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109DU 11503 S/N 5782 JUST CAME BACK FROM REPAIR. UNIT STILL TILTS TO FULL UP POSITION AND STAYS THERE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH7EU 20030423000772003042300077GL 2003 4 23 ALGA085823 220030325A725023051646 SHAFT CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C* GL TURBINE CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01 ON INSTALLATION INSPECTION FOUND PART HAD HEAVY PITTING ON INNERWALL OF SHAFT, ALSO DEEP GROOVES AT INNER SHAFT MATING SURFACE. RETURNED PART FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E4CE 20030423000972003042300097WP 2003 4 23 U2RB010103 120030103A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 76557551 46088 DURING COMPLIANCE WITH A/D 2000-20-08 AND REMOVAL OF TEMPORARY EXTERNAL REPAIR AT LEFT FRONT PAX ENTRANCE DOOR UPPER FORWARD CORNER, VISUALLY DETECTED ONE ADDITIONAL FUSELAGE SKIN CRACK TERMINATING AT RIVET FASTENER 3 FASTENERS UP FROM PREVIOUS CRACK REPAIRED BY CUTOUT AND FILLER METHOD. EXTENDED CUTOUT AND FILLER IN FUSELAGE SKIN"REPAIR ZONE"TO REMOVE SKIN CRACK.INSTALLED PREVENTATIVE REPAIR I/A/W DAC S/B 53-075 & SERVICE REWORK DRAWING SR08530021. 2L74 4F 4A25 20030423001112003042300111 2003 4 23 GLBA2003020 420030221A34216229681001 DISPLAY BEECH 1900 1900D 1154162CE NR EADI INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03204GL877 UE204 NR 2 EADI SCREEN FAILED, REPLACED EADI OPS CHECKED SYSTEM SATISFACTORY 2L72 4T RTA24CE 20030327000482003032700048CE 2003 3 27 BSY2003F00010 120030205A3230 MOTOR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MLG INOPERATIVE E BSYAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL076160X 310R1305 277585R GEAR WOULD NOT COME UP. CYCLED GEAR SEVERAL TIMES COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLACED GEAR MOTOR AS A PRECAUTIONARY MEASURE. OPS CHECK GOOD. 1L72 3O3 O 3A10 E5CE 20030327000612003032700061NM 2003 3 27 C1HA200384003 120030224A3260 CONNECTOR BOEING727 7272S7 138407ZNM MLG LOOSE A C1HAO OTHER N FALSE WARNING CLCLIMB 1 GL15684CA 22491 RED GEAR DOORS LIGHT AND R. GEAR DOOR LIGHT ON ENGINEER PANEL ILLUMINATED AFTER T/O WITH GEAR HANDLE OFF. LIGHTS OUT WHEN GEAR HANDLE PLACED IN UP POSITION. INSPECTED RT MLG DOOR SWITCH AND FOUND CONNECTOR PLUG LOOSE & DIRTY. CLEANED CONNECTOR PLUG AND RE-INSTALLED. INSTALLED GEAR PINS AND OPERATED DOORS PER 727 MM 32-12-00. DOOR LIGHTS OPERATED NORMALLY WITH GEAR HANDLE IN "UP/DOWN POSITIONS" 2L73 4F A3WE 20030327001192003032700119SO 2003 3 27 C2XA03CL049 120030222A3260 WARNING SYSTEM EMB 145 EMB145ER 3260211SO MLG FALSE INDICATIONA C2XAO OTHER N FALSE WARNING APAPPROACH 1 SW2714930 145011 CLE FLIGHT 2201 THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE DURING APPROACH INTO SDF. THE LANDING GEAR WAS RECYCLED AND THE MESSAGE WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED MULTIPLE GEAR OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030327001302003032700130SO 2003 3 27 C2XA03CL067 120030307A3350375921 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715941 145035 CLE FLIGHT 2123 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON MID CABIN WALL WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001322003032700132SO 2003 3 27 C2XA03CL070 120030314A3260 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO MLG FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714938 145029 CLE FLIGHT#2268 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS.MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR NR 2 PROXIMITY SWITCH AND THE LANDING GEAR ELECTRONIC UNIT.OPERATIONAL CHECKS WERE GOOD.PROXIMITY SWITCH P/N 8-527-01 S/N A27260 2L72 4F RTT00011AT 20030327001522003032700152SO 2003 3 27 C2XA03IA026 120030309A2530 COFFEEMAKER EMB 145 EMB145LR 3260212SO GALLEY ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2712922 145338 FLIGHT 2466 PASSENGER REPORTED POSSIBLE BURNING ODOR POSSIBLY CAME FROM GALLEY. ODOR WENT AWAY AFTER TURNING OFF COFFEEMAKERS. SERVICED COFFEEMAKERS WITH H2O, VERIFIED NORMAL OPERATION OF COFFEEMAKERS IAW CMM 25-30-40, NO BURNING ODOR NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001532003032700153SO 2003 3 27 C2XA03IA027 120030315A335020131A LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716911 145446 FLT 2380 - DURING POSTFLIGHT INSPECTION THE AFT EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED THE SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20030327001832003032700183SO 2003 3 27 C2XA03TY018 120030131A532014521721009 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD FLOOR SUPPORT DIGITAL PLATE AFT OF THE COCKPIT DOOR. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PLATE IAW-EMB-145-SRM-57-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2L72 4T RTT00011AT 20030327000042003032700004NM 2003 3 27 AWXA200300267 120030313A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28812AW 1178 FLIGHT CREW REPORTED THE AFT RT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT HAS A LOW BATTERY. MAINTENANCE REMOVED AND REPLACED THE AFT RT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030327000212003032700021NM 2003 3 27 AWXA200300289 120030227A5320146N5318 STRUCTURE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR DECK AT BS 1715, RBL 23 TO 31. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS REQUIRED REPAIR; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 53-60-51, PG. 204-208. 2L72 4F RTA2NM 20030327000712003032700071NM 2003 3 27 C1HA200394004 120030224A3260 ACCESSORY UNIT BOEING727 727290 138408WNM MLG MALFUNCTIONED A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15294AS 22146 FWD NOSE GEAR WARNING LIGHT ON RETRACTION WOULD NOT EXTINGUISH. REMOVED AND REPLACED LANDING GEAR ACC UNIT REF 32-09-121. 2L73 4F A3WE 20030327001282003032700128SO 2003 3 27 C2XA03CL065 120030223A3232355022002MOD3 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A C2XAO OTHER J WARNING INDICATION APAPPROACH 1 SW2729906 145472 DAY FLIGHT 2450 THE CREW REPORTED ON FINAL APPROACH INTO DAYTON PRIOR TO GEAR DOWN RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030327001342003032700134SO 2003 3 27 C2XA03CL072 120030318A3230355022002MOD2 CONTROL UNIT EMB 145 EMB145ER 3260211SO MLG ERRATIC A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW2716944 145045 CLE FLIGHT 2367 THE CREW REPORTED A LANDING GEAR AIR/GROUND CAUTION MESSAGE ON DESCENT. THE SOLENOID SWITCH IN THE GEAR HANDLE CYCLING WITH THE GEAR DOWN.THE MESSAGE CLEARED ON ROLLOUT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030327001642003032700164SO 2003 3 27 C2XA03SH042 120030310A531014534535001 SHEAR TIE EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK SHEAR CLIPS WHERE FOUND TO HAVE CORROSION BETWEEN FRAMES 56 TO 60 AND STRINGERS 21 LEFT AND 20 RIGHT. MAINTENANCE REMOVED AND REPLACED AFFECTED SHEAR CLIPS IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20040324000292004032400029WP 2004 3 24 ASAA0380705 120031103A5310991960433 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND SHEAR TIE IS CORRODED AT FS 1231 IN AFT CARGO BAY. REPLACED SHEAR TIE PER SRM 51-10-2, 3 AND 4. (M) 2L72 4F RTA6WE 20040324000102004032400010NM 2004 3 24 ASAA0340343 120031114A552465C313077 FITTING BOEING737 7374Q8 138447QNM LT ELEVATOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01755AS 25096 GYR - DURING SI CHECK, FOUND LEFT ELEVATOR HINGE FITTING WORN AT STAB STA 213.43. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040324000132004032400013WP 2004 3 24 ASAA0380708 120031103A53305936667501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS CORRODED UNDER DRAIN HOLE COVER AT FS 1293. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-04 AND 51-30-5. (M) 2L72 4F RTA6WE 20040324000322004032400032WP 2004 3 24 ASAA0380688 120031020A53305936021505 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN DENTED AT FS 1263. INSTALLED REPAIR DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040329000232004032900023NM 2004 3 29 ASAA0340317 120030725A53201496337 SUPPORT ANGLE BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND SUPPORT ANGLE AT FS 767-807 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040329000262004032900026NM 2004 3 29 USAA030268 120031208A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 CLT - FOUND SKIN CRACKED .75 INCH AND .5 INCH, BS 727D-727E S23L. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040329000372004032900037WP 2004 3 29 ASAA0380384 120030421A53475952421503 MOUNT DOUG DC9 DC982 3022082WP GALLEY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND GALLEY MOUNT CORRODED. REPLACED MOUNT. (M) 2L72 4F A6WE 20040329000382004032900038WP 2004 3 29 ASAA0380382 120030421A5320993653531 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 218. REPLACED SUPPORT PER SRM 51-10-3 AND 4. (M) 2L72 4F A6WE 20040325000992004032500099NE 2004 3 25 BAQA093003 220030531A74129550176020 IGNITER BOX BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG 7506 18013 IGNITOR BOX NOT FIRING. IGNITOR BOX IS ORIGINAL EQUIPMENT. REPLACED WITH SERVICABLE UNIT. 02/27/2004 1G72 3U3 UNCH13EU E19EU 20040329000242004032900024NM 2004 3 29 ASAA0340318 120030725A5320654587545 SUPPORT ANGLE BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND SIDE WALL SUPPORT ANGLE AT FS 328 TO 340 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040329000422004032900042NM 2004 3 29 ASAA0240298 120030514A53206547690 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01778AS 25110 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY LEFT SIDEWALL SUPPORT AT BS 440 IS DAMAGED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030714001592003071400159 2003 7 14 ALGA087940 420030629A2210214074305105 AMPLIFIER BELL 214 214ST 1182106SW WILL NOT TEST B ALGAO OTHER L NO TEST NRNOT REPORTED 1 SW03390AL 28198 NR 2 ELEVATOR WILL NOT TEST AND ALSO KICKS OFF. 2G72 4U H10SW 20030714001642003071400164SW 2003 7 14 ALGA087947 120030704A8011214060056109 STARTER BELL 214 214ST 1182106SW ENGINE BROKEN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03390AL 28198 REPAIR DUE TO THE STARTER WOULD NOT ENGAGE. 2G72 4U H10SW 20030716000062003071600006WP 2003 7 16 GTIA030451 120030531A7120K22199SA31 ISOLATOR DOUG DC9 DC983 3022083WP NR 1 PYLON OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FLL - NR 1 ENGINE/PYLON, FORWARD LOWER ISOLATOR ALIGNMENT MARKS ARE OFF BY .25 INCH. REMOVED AND REPLACED NR 1 ENGNE LOWER FORWARD ISOLATOR. (M) 2L72 4F RTA6WE 20030716000222003071600022NM 2003 7 16 2003F00414 120030313A5320 FAIRING BOEING727 727222 1384073NM LEFT A/C BAY CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON LEFT AIR CONDITIONING BAY FAIRING BELOW TAXI LIGHT. CUT OUT CRACKED SECTION AND INSTALLED DOUBLER AT LEFT AIR CONDITIONING BAY FAIRING BELOW TAXI LIGHT. (M) 2L73 4F A3WE 20030716000312003071600031NM 2003 7 16 USAABB03099 120030621A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19631AU 27809 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 9, 18, 23, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030716000822003071600082NE 2003 7 16 A6WA200340098 220030616A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 MALFUNCTIONED A A6WAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL31445AW 7804 NR 2 ENGINE ONLY PRODUCED 50 PERCENT POWER. ABORTED TAKEOFF AT 60 KNOTS. ALMOST NO BREAKING USED, MAX 2 PERFORMED POWER ASSURANCE CHECK IAW AMM 71-00-00-710-804. PERFORMED CHECKS WITHIN LIMITS. COULD NOT DUPLICATE PROBLEM. (M) 2L72 4F4 FRTA21EA E15NE 20030716000902003071600090 2003 7 16 USAASA03053 420030524A2565 SLIDE AIRBUSA319 A319112 3930323EU PAX DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US 1038 THE LEFT AFT ENTRY DOOR SLIDE WAS FOUND TO BE UNRAVELING. MAINTENANCE REPLACED THE LEFT AFT ENTRY DOOR SLIDE OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030716001112003071600111NE 2003 7 16 HEEA088041 120030704A24207655009005104 GCU SKRSKYS76 S76A 8143006NE AC GENERATOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 GCU HAS SLIGHT DELAY TO COME ON LINE. 1G72 3U H1NE 20030717000152003071700015SW 2003 7 17 HEEA087992 120030619A3212206050247131 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 TORN VELCRO ON END CAP. REPLACED COVER. 1G71 3U O H2SW 20030717000332003071700033SW 2003 7 17 HEEA088010 120030623A5630407030635102 WINDOW BELL 407 407 1182206SW CREW DOOR CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 CREW DOOR WINDOW CRAZED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000602003071700060 2003 7 17 HEEA088053 420030703A3422066304607 INDICATOR KI525A BELL 206 206L3 1182108SW HSI INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 93698 51527 HSI HAS INTERMITTENT OPERATION. SHOP REPAIR. 1G71 3U H2SW 20030718000182003071800018NM 2003 7 18 TSAA0353132 120030506A531365516989 STRINGER BOEING737 73725A 1384481NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 CRACK DISCOVERED ON STRINGER 4 LEFT, LOCATED AT BS 907. CUTOUT DAMGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DIRLLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-2. (M) 2L72 4F RTA16WE 20030718000262003071800026WP 2003 7 18 GTIA030477 120030514A5755 PANEL DOUG DC9 DC981 3022081WP SPOILER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 RIGHT INBOARD SPOILER PANEL DELAMINATED. REPAIRED RIGHT INBOARD SPOILER PANEL. (M) 2L72 4F A6WE 20030718000492003071800049NM 2003 7 18 AUS20030546 120030528A3232 ACTUATOR BOEING747 747438 NM RROYCERB211 RB211524* NE MLG DOOR OUT OF POSITION W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) MAIN BODY GEAR DOOR FAILED TO RETRACT. INVESTIGATION FOUND THE BODY GEAR DOOR ALTERNATE EXTENSION ACTUATORS WERE OUT OF POSITION. 2L74 4F4 FRTA20WE E12EU 20030721000012003072100001NM 2003 7 21 AUS20030557 120030528A243523088002A STARTER GEN DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE ENGINE FAULTY W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 AUS 1293 (AUS) NR 1 STARTER-GENERATOR SUSPECT FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030716000802003071600080 2003 7 16 USAASA03061 420030612A2565 SLIDE AIRBUSA321 A321211 3930370EU PAX DOOR MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19175US 1496 THE DIRECTIONAL GUIDANCE LIGHTS DID NOT WORK DURING OPERATIONAL TEST OF AFT RIGHT SERVICE DOOR ESCAPE SLIDE. MAINTENANCE REPLACED THE AFT RIGHT SERVICE DOOR ESCAPE SLIDE. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030716000942003071600094EU 2003 7 16 USAASA03057 120030531A54103380730100 PANEL AIRBUSA319 A319112 3930323EU LT ENGINE INLET LOOSE A USAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA19745UW 1289 EN ROUTE SFO-PIT, ON TAKEOFF, A LOUD AIR NOISE FROM LEFT SIDE OF AIRCRAFT WAS HEARD, FOLLOWED BY FIVE COMPRESSOR STALLS. NO IRREGULAR ENGINE INDICATIONS WERE NOTED. CREW FOLLOWED THE QUICK REFERENCE HANDBOOK PROCEDURES. BOTH ENGINES REMAINED IN OPERATION THROUGH OUT THE FLIGHT. FLIGHT RETURNED TO SFO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SEVERAL MID-ACOUSTICAL PANELS DAMAGED, BLOCKING BYPASS DUCT AIRFLOW, DURING WALK AROUND INSPECTION. ALSO, FOUND SEVERAL OUTLET GUIDE VANE DOUBLERS DAMAGED. REPLACED FOUR MID-ACOUSTICAL PANELS, POSITIONS 0100, 0300, 0500, AND 1100. ALSO, REPLACED OUTLET GUIDE VANE DOUBLERS IN POSITIONS 1200 AND 0200. ENGINE OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030729001202003072900120SO 2003 7 29 SWIA200312193 120030715A3350 LIGHT EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07568SW 120343 FLOOR TRACK LIGHTING AT SEAT 7A INOPERATIVE. REPLACED DEFECTIVE FLOOR TRACK LIGHT AT 7A IAW MM 33-50-00. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030729001212003072900121SO 2003 7 29 SWIA200312194 120030716A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE CABIN DISCHARGED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07217SW6828 6828 120286 AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD IAW 33-50-02. 2L72 4T4 TRTA31SO E20NE 20030729001362003072900136NM 2003 7 29 UPS03240949 120030606A5330 SKIN BOEING727 727185C 138406NNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C SUSPECT CORROSION BS 605 STR 4R LFEC + HFEC CARRIED OUT, NDF. VISUAL INSPECTION SHOWS CORROSION AT STR 4 BS 521-BS740. DAMAGE REMOVED IAW SRM 53 30 03. REPAIR PARTS FABRICATED IAW SRM 53 30 03. REPAIR INSTALLED IAW SRM 53 30 03. REPAIR CARRIED OUT IAW EO B727 5330 0509. 2L73 4F A3WE 20030730001082003073000108SO 2003 7 30 SIMA200317603 120030623A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21811AE 145529 ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R CHAFED AT FRAME 53. BLENDED THE CAHFED AREA AND PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS AND INSTALLED. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-24-02 FIGURE 201. RESTORED SURFACE FINISH TO THE REPAIR AREA. (M) 2L72 4F RTT00011AT 20030423001172003042300117CE 2003 4 23 GLBA2003019 120030221A3000 SWITCH BEECH 1900 1900D 1154162CE ANTI-ICE SYS OUT OF ADJUST A GLBAO OTHER J WARNING INDICATION CRCRUISE 1 NM03153GL UE153 RIGHT ANTI-ICE ANNUNCIATOR ILLUMINATED. ADJUSTED RT ICE VANE SENSE SWITCHES, OPS CK GOOD. 2L72 4T RTA24CE 20030423001222003042300122SO 2003 4 23 GLBA2003030 120030307A3260 WARNING LIGHT EMB 120 EMB120ER 3260203SO MLG ILLUMINATED A GLBAO OTHER N FALSE WARNING CLCLIMB 1 NM03299UX 120299 LANDING LT GREEN A LIGHT ILLUM AFTER RETRACTION. SWING GEAR 10 TIMES, CND INSP PROX SENSORS GAP, NO DEFECTS. 2L72 4T RTA31SO 20030423001262003042300126NM 2003 4 23 QXEA0300334 120030309A30104D205401 TIMER DHAV DHC8 DHC8202 2809007NM ZONE 200 ERRATIC A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09357PH12258 504 WING DE-ICE BOOT SEGMENTS INFLATED FOR 15 SECONDS EACH, IN FAST MODE WITH NORMAL DWELL TIME. TOTAL TIME 1:54 SLOW MODE TIME 58 SECONDS TO CYCLE THROUGH. REPLACED AIRFRAME DE-ICE SYSTEM TIMER. FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421000752003042100075NM 2003 4 21 DL777030065 120030115A2150 ACM BOEING777 777232 1385232NM LT PACK BAY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27860DA 29951 FUMES IN COCKPIT ON CLIMB AND DESCENT WENT AWAY WHEN LT PACK SWITCHED OFF. SNAPSHOTS SHOWED LT PACK O/P TEMP HIGH WITH TBV IN SAME POSITION AS RT DISCONNECTED AND OPENED LT TBV ODOR DISAPPEARED. SUSPECT LT ACM FWD TO MCO AND PLACED PER MEL 21-52-01. UPDATE: REACTIVATED TURBINE BYPASS VALVE AND RAN LT PACK F HOURS AT DIFFERENT TEMP SETTINGS, NO FUMES OR ODORS. PACK INDICATIONS NORMAL, C/W LT PACK TEMP CONTROL PASS MCO AND PLACARD REMOVED. 2L72 4F RTT00001SE 20030421001162003042100116NM 2003 4 21 QXEA0300313 120030301A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 OUT OF ADJUST A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09409QX4051 4051 SEA - FLIGHT 2293 - THE RIGHT MAIN GEAR DOOR WAS SLOW TO CLOSE, TAKING APPROXIMATELY 30-45 SECONDS. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE PROXIMITY SENSORS. OPERATIONAL CHECKS OF THE LANDING GEAR WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421001192003042100119NM 2003 4 21 QXEA0300314 120030302A3150 WARNING HORN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FALSE ACTIVATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09400QX 4030 PDX-ON FLIGHT NUMBER 2292, ABORTED TAKEOFF FOR TAKEOFF WARNING HORN. PERFORMED FUNCTIONAL TEST OF TAKEOFF WARNING SYSTEM. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421002182003042100218EU 2003 4 21 BMAC03005S 120030215A7712 SIGNAL COND UNIT BAG JETSTMJETSTM3101 1500215EU ENGINE TORQUE MALFUNCTIONED A B16AA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NE05538PA 751 FLT 3157 - BWI - PILOT REPORTED AT 12,000 FT WITH POWER LEVERS AGAINST STOPS COULD ONLY GET 80 PERCENT TORQUE AND 630 EGT POWER LEVER AGAINST STOPS, SRL AND TTL ON, ENGINE ANTI-ICE ON. PILOT PERFORMED AIR TURN BACK TO BWI. THE MECHANIC PLACED BOTH LEFT AND RIGHT SRL SYSTEMS ON MEL. FINAL FIX, REPLACED RIGHT STRAIN GAUGE AND TORQUE SIGNAL CONDITIONER. REPLACED LEFT STRAIN GAUGE, TTL COMPUTER AND BUFFER ASSY TORQUE SIGNAL. BOTH SIDES TESTED GOOD ON THE GROUND AND GOOD ON APPROX TWO HOUR FLIGHT CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 20030422000922003042200092SO 2003 4 22 SIMA200307006 120030307A532014521725615 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 ABI - DURING A IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA OF THE CENTER SILL AND PERFORMED AN NDT INSPECTION. FABRICATED A DOUBLER, REPAIR DONE IAW EMB SRM (SRM 145/1142 REV 20) CHAPTER 51-21-02 AND EMB REPAIR STATEMENT 1C2003-145/0771. (M) 2L72 4F RTT00011AT 20030422001322003042200132NE 2003 4 22 SWIA200311822 220030221A7321 WARNING LIGHT EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT ENGINE ILLUMINATED A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07196SW 120151 EEC LEFT FAILURE ON TAKEOFF ROLL. ABORTED TAKEOFF. RAN VARIOUS EEC-RELATED TESTS, COULD NOT DUPLICATE DISCREPANCY. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED LEFT ENGINE. 2L72 4T4 TRTA31SO E20NE 20030422001462003042200146NM 2003 4 22 EIA2003009 120030226A532065B282665 INTERCOSTAL BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 INTERCOSTAL CRACKED AT STA 291 LBL 20 ON TOP TOP OF NOSE WHEEL WELL BOX. C/A: K/H SIDE INSTALLED KIT NR 65B28266-5 AND SUB KIT NR 65B28266-6 EO 53-747-1138-91 REV C, IAW SB NR 747-53A-2293 REV 8 AND DRWG 3 62460005. 2L74 4F A20WE 20030423000232003042300023NM 2003 4 23 AUS20030299 120030212A5320 INTERCOSTAL BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INTERCOSTAL IN AFT CARGO AREA CONTAINED LEVEL 2 CORROSION BETWEEN BS1070 TO BS1090 AND STRINGER 30. FOUND DURING CPCP INSPECTIONIAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423000432003042300043EU 2003 4 23 BAQA085226 120030321A28221176415103 PUMP BOLKMS117 BK117A3 5626015EU FUEL PUMP INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH2448 7030 BOOSTER PUMP INOPERABLE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030423000952003042300095NM 2003 4 23 AWXA200300379 120030402A5210 CONTROL CABLE BOEING757 757225 1384959NM PAX DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - EMERGENCY EVACUATION SYSTEM - DURING C-08 CHECK THE L-1 DOOR FAILED EMERGENCY POWER ACTUATION TEST FOR TRAVEL OF ACTUATION CABLE. MAINTENANCE ADJUSTED THE L-1 DOOR EMERGENCY POWER ACTUATION CABLE IAW BMM 52-11-32 PG 404 & 408, CABLE TRAVEL CHECKED GOOD IAW T/C F1C52605. 2L72 4F RTA2NM 20030423001442003042300144WP 2003 4 23 ZW0A0303004 120030306A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 SKIN AT STA 181 ABOVE LONGERON 20R WAS DENTED. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030423001512003042300151WP 2003 4 23 ZW0A0303011 120030306A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 LONGERON 20R AT STA 160 TO 154 WAS DAMAGED. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030730001202003073000120WP 2003 7 30 MEX2003207 120030406A21331036361 RELIEF VALVE DOUG DC9 DC987 3022087WP CABIN PRESSURE FAILED A ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW231075T 49724 FLT 926 - MEX-CUU - AIRCRAFT AIR TURNBACK AS A CONSEQUENCE OF DURING CRUISE AT 35,000 FEET, STRONG NOISE WAS HEARD, THE FLOW LIGHT CAME ON. PRESSURIZATION VALVE WAS CLOSED AND CABIN ALTITUDE WAS 7,600 FEET. PRESSURIZATION TEST WAS ACCOMPLISHED, NO LEAKS WERE FOUND AND RELIEF VALVES WERE CHECKED FOR PROPER OPERATION. DURING OVERNIGHT SERVICE, THE RELIEF VALVES WERE REPLACED IAW MM 21-32-07, ALL TESTS OK. (M) 2L72 4F RTA6WE 20030730001282003073000128SO 2003 7 30 SIMA200314803 120030515A531514525381003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21644AE 145204 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 24 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT A 1.1250 BY 1.5625 SECTION OF DAMAGE OMEGA BEAM. FABRICATED ONE FILLER, EXTERNAL ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 21, CHAPTER 53-21-10 FIG 202. (M) 2L72 4T RTT00011AT 20030730001422003073000142NM 2003 7 30 USAABB03094 120030618A3397 WIRE BOEING767 767201 1385125NM CABIN CUT A USAAK NONE L NO TEST ININSP/MAINT 1 EA19645US 23897 CDG - FOUND RIGHT AISLE EMERGENCY LIGHT BETWEEN ENVOY CLASS AND COACH INOPERATIVE. WIRE WAS CUT/DISCONNECTED. MAINTENANCE SPLICED THE WIRE. (M) 2L72 4F RTA1NM 20030731000162003073100016EA 2003 7 31 QXEA200300891 120030726A3620 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT ACTIVATED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09606QX 10023 SMF- ON FLIGHT 2492 SMF TO SEA, DIVERTED TO PDX DUE TO ON GROUND (LEFT BLEED DUCT) WARNING MESSAGE CAME ON. BOTH PACKS SHUTDOWN. AFTER 10 SECONDS THE WARNING WENT OUT, FOLLOWED BY (LEFT BLEED DUCT) CAUTION MESSAGE. THE MANUAL BLEED PROCEDURES PRODUCED NO RESULTS. AIRCRAFT LANDED WITHOUT INCIDENT. RAN BLEED LEAK DETECTION TEST ON BOTH CHANNELS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000582003073100058EA 2003 7 31 QXEA200300877 120030724A2710 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT ACTIVATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09614QX 10049 PDX-ON FLIGHT NUMBER 2437, CONFIG AILERON WARNING MESSAGE APPEARED. ABORTED TAKEOFF AND MESSAGE DISAPPEARED AFTER 1-2 SECONDS. MDC HAS NO REPORTS FOR AILERON TRIM SYSTEM. PERFORMED FAULT CONFIRM OF AILERON TRIM SYSTEM. OPERATIONAL TEST OF AILERON SYSTEM GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000642003073100064NM 2003 7 31 QXEA200300885 120030724A3620 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09411QX 4055 SUN- ON FLIGHT 2344 NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST. TURNED BLEED OFF AND LIGHT EXTINGUISHED. BLEED REMAINED OFF. CLEARED ECU FAULT BY RESETTING NACELLE DUCT LOCK OVERTEMPERATURE SWITCH CANNON PLUG. PERFORMED GROUND RUN WITH NR 2 BLEED ON FOR 10 MINUTES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000682003073100068NM 2003 7 31 QXEA200300853 120030719A1430 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM FUSELAGE BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX- ON NO.3 VHF ANTENNA FOUND FORWARD RIGHT HAND AND MIDDLE LEFT HAND NUT PLATES ARE BROKEN. REPAIRED IAW Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030731000952003073100095NM 2003 7 31 QXEA200300763 120030621A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - LEFT HAND OUTBOARD FLAP HAS CHAFE 19 INCHES UP TRAILING EDGE, 6 INCHES IN FROM INBOARD FLAP. REPAIED IAW RD 8/4-57-0132. 2H72 4T RTA13NM 20030731001072003073100107NM 2003 7 31 QXEA200300865 120030720A3350 CONNECTOR DHAV DHC8 DHC8202 2809007NM CABIN DIRTY A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09350PH 488 PDX- EMERGENCY LIGHTING IS INOPERATIVE ON FLOOR STRIP AT SEAT ROWS 1 AND 2. CLEANED CONNECTOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030801000072003080100007WP 2003 8 1 GTIA030525 120030620A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - AFT CARGO COMPARTMENTS AT STATIN 1218, LONGERON 18R, SUB FLOOR WEB IS CORRODED. SUB FLOOR WEB. DRILLED AND LOCATED SPLICE AND ODUBLER. INSTALLED WEB SPLICE/DOUBLER. (M) 2L72 4F A6WE 20030801000862003080100086SO 2003 8 1 C2XA03SH217 120030710A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 SHV-DURING C CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PEROFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030805000252003080500025CE 2003 8 5 BSY2003F00011 120030506A3230583800901 MOTOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MLG INOPERATIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL073703Q TH1189 823784R GEAR WOULD NOT EXTEND, HAND CRANKED GEAR DOWN. REMOVED AND REPLACED GEAR MOTOR OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 20030730001312003073000131NM 2003 7 30 USAASB03081 120030612A21307110025 CONTROL PANEL BOEING737 7373B7 1384580NM COCKPIT FAULTY A USAAGBH O2 MASK DEPLOYED EMER. DESCENT DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 EA19518AU45839 23704 CLT - FLT 1254 - MCI TO CLT, AT FL350, CAPTAIN REPORTED A PRESSURIZATION PROBLEM, AS CABIN ALTITUDE INCREASED. CABIN ALTITUDE EXCEEDED 14,000 FT, THE OXYGEN MASKS AUTO DEPLOYED. AN EMERGENCY DESCENT TO FL100 WAS ACCOMPLISHED. THE FLT CONTINUED ONTO CLT, AT THIS LEVEL, AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT SYS AND FOUND THE AFT OUTFLOW VALVE AND GASKET LEAKING. REPLACED VALVE (P/N 711003-3) AND GASKET PER MM 21-31-11 AND MM 21-31-12. OPS CHECK GOOD. FOUND AFT CARGO DOOR LOWER CORNERS LEAKING EXCESSIVELY. REPAIRED DOOR SILL MATING SURFACES. LEAK CHECK GOOD. ACCOMPLISHED HULL LEAK RATE CHECK AND REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL PER MM TASK 21-31-00. OPERATIONAL TEST GOOD. (M) 2L72 4F RTA16WE 20030731000122003073100012EA 2003 7 31 QXEA200300812 120030702A5730 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX - RIGHT WING INBOARD LEADING EDGE PANEL 622AR HAS CHAFE FROM CONTACT WITH SLAT LOWER EDGE, AT APPROXIMATELY WS108. REPAIRED IAW EA R-57-40. 2L72 4F4 FRTA21EA E15NE 20030731000352003073100035NM 2003 7 31 QXEA200300911 120030724A5711 SPAR CAP DHAV DHC8 DHC8202 2809007NM RT WING GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- RIGHT HAND WING FRONT SPAR UPPER CAP, UPPER SURFACE HAS MINOR GOUGES/SCRATCHES INTO BASE METAL BETWEEN STATIONS YW315 AND YW387. REPAIRED IAW DHC-8 RD 8-57-1675 AND 8-57-1119. 2H72 4T RTA13NM 20030731000622003073100062EA 2003 7 31 QXEA200300753 120030619A4920WE38007703 APU CNDAIRCL600 CL6002C10 1390015EA APU BAY ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09609QX4218 10031 BOI-SUP-ON FLIGHT NUMBER 2424, BURNING OIL SMELL DETECTED DURING CLIMB. OIL SMELL DISSIPATED AFTER APU SHUTDOWN. VISUALLY INSPECTED APU EXHUAST & INTAKE. NO DEFECTS NOTED. GROUND RAN APU. SLIGHT OIL SMELL WHEN FIRST STARTED. REMOVED ND REPLACED APU. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000632003073100063EA 2003 7 31 QXEA200300847 120030720A3620 LOOP CNDAIRCL600 CL6002C10 1390015EA A/C BAY OUT OF POSITION A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09606QX 10023 SEA- ON FLIGHT 2512 LEFT BLEED DUCT WARNING MESSAGE FOLLOWED BY LEFT BLEED DUCT CAUTION MESSAGE. SYSTEM AUTO SHUTDOWN. PER CHECKLIST RESTARTED IN MANUAL. FOUND BLEED LOOP TOUCHING LOOSE SHROUD IN AFT EQUIPMENT BAY. RESECURED SHROUD AND ADJUSTED BLEED LOOP TO PROPER CLEARANCE. NO PARTS REPLACED. OPERATIONAL CHEKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000892003073100089NM 2003 7 31 QXEA200300830 120030714A5410 SUPPORT FITTING BOMBDRDHC8 DHC8401 1390041NM NACELLE LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - LOWER INBOARD ENGINE SUPPORT FITTING IN NACELLE IS PULLED LOOSE FROM LOWER BOX STRUCTURE OF NACELLE. REPAIRED IAW Q400 SRM 51-25-15, PAGE 205-G-1-4 AND SRM 51-40-15, PAGE 203. 2H72 4T RTA13NM 20030801000442003080100044SO 2003 8 1 SIMA200317607 120030620A1430MS20470E65 RIVET EMB 135 EMB135KL 3260302SO FUSELAGE LIGHTNING STRIKEA SIMAK NONE O OTHER ININSP/MAINT 1 SW21811AE 145529 ABI - DURING A LIGHTNING STRIKE INSPECTION ONE RIVET AT STRINGER 6R, 2 INCHES FORWARD OF FRAME 34 WAS FOUND DAMAGED. REMOVED DAMAGED RIVET AND PERFORMED A CIRCULAR CUTOUT .6 INCHES IN DIAMETER. FABRICATED A REPAIR PLUG, REPAIR DOUBLER. REPAIR DONE IAW BME IC2003-145/1685 AND IC2003-145/1688 AND STANDARD SRM PRACTICES. EDGE SEALED AND RESTORED SURFACE PROTECTION. (M) 2L72 4F RTT00011AT 20030801000462003080100046WP 2003 8 1 GTIA030548 120030703A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 160 LBL 54 INCHES SUB FLOOR WEB ELONGATED HOLES/CRACKED. REMOVED SUB FLOOR WEB FS 160-200. FABRICATED NEW SUB FLOOR WEB. INSTALLED NEW SUB FLOOR WEB. (M) 2L72 4F A6WE 20030801000522003080100052WP 2003 8 1 GTIA030514 120030617A5313 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - MID PIT STATION 769-775 STRINGER 30 CORRODED AND FASTENERS CORRODED. (M) 2L72 4F A6WE 20030801000812003080100081NM 2003 8 1 UPS03440938 120030620A5312 PRESSURE PANEL BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C RT BLG W/W PRESSURE DECK SKIN CORRODED AT FS 1391 - 1395 RBL 116-120 . FS 1385- FS 1395 PRESSURE DECK WEB REPAIRED IAW SRM 53-10-07 FIG 2. 2L74 4F A20WE 20030801001122003080100112EA 2003 8 1 COMA0360324 120030718A5330601R3114627 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01918CA23579 7018 DURING COMPLIANCE OF TASK NR 002-53-160-610, 2 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL 9.0 AND RBL 9.0. THE CRACKS RANGE FROM 2.875 INCHES TO 3.125 INCHES IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IAW BOMBARDIER REO #610-53-41-102, REV B, DATED 6-8-2003, AND REO#601R-53-41-162, DATED 6-9-2003. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20030805000232003080500023CE 2003 8 5 MYN2003F00000 120030405A2820IS1523 DIODE MTSBSIMU2 MU2B60 5780460CE FUEL TRANSFER FAILED B MYNRO OTHER O OTHER NRNOT REPORTED 1 GL11322TA5000 760SA DIODE CR 406 SHORTED, ALLOWING POWER FROM LT FUEL TRANSFER CIRCUIT TO FEED BACK TO THE RT FUEL TRANSFER CIRCUIT. WHEN LT TP FUEL SHUT OFF VALVE WAS COMMANDED ON AND RT TIP FUEL SHUTOFF VALVE COMMANDED OFF. THE RT TP FUEL SHUT OFF VALVE HAD POWER ON PINS A AND B TELLING IT TO OPEN AND CLOSE AT THE SAME TIME, WHICH CAUSED VALVE FAILURE. 1H72 3T RTA10SW 20030805000332003080500033SW 2003 8 5 505060103 120030601A79312719153003 TRANSDUCER SWRNGNSA227 SA227AC 8780603SW OIL PRESSURE INDFAILED E STZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AL05505FS AC591B OIL PRESSURE GAUGE PEGGED OUT SCALE HIGH, ALL OTHER INDICATIONS NORMAL, AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE REMOVED AND REPLACED OIL PRESSURE TRANSDUCER WITH SERVICABLE UNIT. OPERATIONAL CHECKS SATISFACTORY. 2L72 4T RTA8SW 20030805000602003080500060EA 2003 8 5 ASOA03267 120030618A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11843AS 7310 DURING A GROUND INSPECTION IN MGM, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030805000652003080500065NM 2003 8 5 AALA20030663 120030613A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21795AN 30257 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD RIGHT LOWER FORWARD FACING EMERGENCY EXIT PATH LIGHTING IN THE G3 GALLEY CARTS STORAGE WALL IS BROKEN. REPLACED FORWARD RGHT LOWER FORWARD FACING EMERGENCY EXIT PATH LIGHT ASSEMBLY ON THE G3 GALLEY CARTS STORAGE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030805000782003080500078EA 2003 8 5 ASOA03306 120030701A53116013600123 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE FRAME SECTOR AT FS 640 ON THE RIGHT SIDE BELOW STRINGER 9R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME SECTOR AT FS 640 ON THE RIGHT SIDE BELOW STRINGER 9R IAW ASA EO 600-53-0075. (M) 2L72 4F RTA21EA 20030805000802003080500080EU 2003 8 5 ASOA03275 120030624A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURING A HANGAR INSPECTIN IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030805000812003080500081NM 2003 8 5 AALA20030660 120030613A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21795AN 30257 DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 40C INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030805000932003080500093EA 2003 8 5 ASOA03281 120030702A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 DURING HANGAR MAINTENANCE IN BTR, THE LOWER EMERGENCY LIGHT AT THE PASSENGER DOOR ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOWER EMERGENCY LIGHT LAMP AT THE PASSENGER DOOR ENTRANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030805000952003080500095EA 2003 8 5 ASOA03297 120030707A5330601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030805001042003080500104EU 2003 8 5 ASOA03253 120030605A3397EO1173110 TERMINAL AEROSPATR72 ATR72 EU CABIN LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11640AS 405 DURING AN A-CHECK IN MCN, AN EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE WHEN THE AFT BUTTON SWITCH WAS PUSHED. MAINTENANCE REPAIRED THE TERMINAL ON THE AFT EMERGENCY EXIT BUTTON SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030805001052003080500105EA 2003 8 5 ASOA03277 120030627A3000GG670800144 DUCT CNDAIRCL600 CL6002C10 1390015EA WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11717EV 10088 DURING GROUND INSPECTION IN DFW, THE RT INBOARD SLAT TELESCOPIC DUCT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SLAT TELESCOPIC DUCT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030805001112003080500111SO 2003 8 5 SIMA200319003 120030707A27513633501003 SENSOR EMB 135 EMB135KL 3260302SO LEFT FLAP INOPERATIVE A SIMAO OTHER O OTHER DEDESCENT 1 SW21804AE 145487 DURING DESCENT CREW REPORTED THE FLAPS FAILED TO DEPLOY. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP VELOCITY SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030806000112003080600011EU 2003 8 6 BAQA088099 120030715A28229A2045 PUMP UROCOPEC135 EC135T1 5620026EU FUEL SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH2249 0131 FUEL PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030806000122003080600012SW 2003 8 6 ALGA088105 120030715A632023076252 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03587AL405 CAG47258 53248 CAE847158 REMOVED GEAR FOR EXCESSIVE SPALLING ON GEAR TEETH. REMOVED FOR WARRANTY CREDIT. 1G71 3U3 UO H2SW E1GL 20030806000202003080600020NE 2003 8 6 BAQA088146 220030718A723070BM025020 COMPRESSOR AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1D NE ENGINE WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 1931 6036 MODULE 2 DUE CHANGE FOR WEAR AT BLEED AIR DUCT. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H10EU E19EU 20030806000302003080600030 2003 8 6 BAQA088272 420030731A3421C17027AA01 INDICATOR UROCOPEC135 EC135T1 5620026EU COCKPIT OUT OF LIMITS B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME1822 132 ALTITUDE OUT OF LIMITS PER FAR 91-411. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030806000492003080600049SO 2003 8 6 C2XA03SH239 120030730A5411145766631622 STRUCTURE EMB 145 EMB145LR 3260212SO RT WING COWL CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 SHV DURING C-CHECK, THE RIGHT HAND LOWER COWLING AFT EDGE MEMBER WAS FOUND TO HAVE CHAFING MARKS. MAINTENANCE REMOVED AND REPLACED AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806000502003080600050NM 2003 8 6 AWXA200300845 120030726A3320325030 BALLAST AIRBUSA319 A319132 3930340NM SEAT ROW 16 LT OVERHEATED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28820AW 1397 ON CLIMBOUT FROM SAN EN ROUTE FOR LAS AT 20,000 FT, FLT ATTENDANT REPORTED A STRONG ELECTRICAL BURNING ODOR IN MID TO AFT CABIN, DIVERTED TO LAX. MAINTENANCE FOUND CABIN LIGHTING BALLAST AT SEAT ROW 16 LT EXTREMELY HOT. REMOVED AND REPLACED BALLAST, PERFORMED ENGINE RUN OPERATING BOTH A/C PACKS, INSPECTED ALL LIGHTING AND ELECTRICAL BOXES, NO BURNING ODOR NOTED. OPERATIONAL TEST OF LIGHT BALLAST SEAT ROW 16 LT WAS GOOD. 2L72 4F RTA28NM 20030806000572003080600057SO 2003 8 6 C2XA03CL121 120030708A3397 WIRE EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714945 145049 THE CREW REPORTED FLOOR EMERGENCY LIGHTS BURNED OUT IN TWO SECTIONS. MAINTENANCE RESECURED LOOSE WIRE ON EMERGENCY LIGHT STRIP. 2L72 4F RTT00011AT 20030806000592003080600059NE 2003 8 6 AWXA200300866 220030729A73145008735G PUMP AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 ENGINE DEFECTIVE A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28634AW380078391 091 ON TAKEOFF, RECEIVED ECAM WARNING FOR NR 1 ENG COMPRESSOR VANE FAULT ALONG WITH N1/N2 OVERSPEED, REJECTED TAKEOFF AT 60 KTS, RETURNED TO BLOCK. MX R & R NR 1 ENG VSV ACTUATOR, FAULT STILL PRESENT DURING ENG RUN. R & R NR 1 ENG FUEL METERING UNIT. REPLACED LOW/HIGH PRESSURE FUEL PUMP. PERFORMED IDLE LEAK TEST, HIGH POWER ASSURANCE RUN AND ELECTRONIC ENG CONTROL/FULL AUTHORITY DIGITAL ENG CONTROL TEST. ALL TESTS GOOD, NO FAULTS NOTED. VENDOR FUNCTIONAL TEST OF VSV ACT COULD NOT CONFIRM REASON FOR REMOVAL, UNIT OPERATED NORM ON RIG, TESTED & RETURNED TO SERVICE IAW CMM. VENDORS FUNCTIONAL TEST OF FMU, NO FAULT FOUND. UNIT OPERATED NORM ON RIG. VENDOR DID CONFIRM FAILURE OF LOW/HIGH PRESS FUEL PUMP. 2L72 4F4 FRTA28NM E311NE 20030806000662003080600066SO 2003 8 6 C2XA03TY096 120030727A534714532606011 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 TYS- DURING A SCHEDULED 3C INSPECTION THE FOLLOWING SEAT TRACKS WERE FOUND CORRODED (RW1 THRU RW3 AND LW1 THRU LW2). MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EC 5340-01048 AND EMB 145 AMM53-01-06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030731001132003073100113NM 2003 7 31 QXEA200300791 120030627A5330 PAINT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - FOUR SCRATCHES IN PAINT ON FUSELAGE, APPROXIMATELY 1-2 INCHES LONG. THREE GO DOWN TO BARE METAL. REPAIRED IAW RD 8/4-53-505, STEPS 1 AND 2. 2H72 4T RTA13NM 20030731001272003073100127NM 2003 7 31 QXEA200300884 120030726A5260 ARM BOMBDRDHC8 DHC8401 1390041NM AFT AIRSTAIR OUT OF POSITION A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09402QX 4032 ON FLIGHT 2353 AFT AIRSTAIR WILL NOT DEPLOY. FOUND ROLLER ARM FELL OUT OF TRACK ON AFT AIRSTAIRS. REINSTALLED ARM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030423001572003042300157NM 2003 4 23 UPS03M40285 120030215A53131D11047150T615 LONGERON DOUG MD11 MD11F 3023600NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP INSPECTION TYPE: C, CABIN INTERIOR FOUND LONGERON SPICE L-24L BETWEEN STA 5-113 & STA 15 41 WITH CRACK AS MARKED. CRACKED LONGERON SPLICE L-24 BETWEEN STA 5-113 TO 1541. REMOVED PER SRM 51-33-01 VOL 2 REV 32. NEW STRINGER SPLICE FABRICATED AS DWG A5A7 112 AND PROTECTED PER SRM 51-21-01 VOL 2 REV 32. FAB LONGERON SPLICE, INSTALLED AS PER SRM 51-33-01 VOL 2 REV 32. 2L73 4F RTA22WE 20030423001672003042300167EU 2003 4 23 MALA030203 120030305A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15428XJ 340B428 DURING 4Y/2Y INSPECTION IN CWA, FOUND FRAME TOP FLANGE AT STA 294 DAMAGED AT RBL 18. MAINTENANCE COMPLETED REPAIR IAW EO S53108. A/C RELEASE DATE 3/9/03. REF TO 409 176255 FOR DETAIL. 2L72 4T RTA52EU 20030423001702003042300170NM 2003 4 23 F3LA200300096 120030228A5311 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED FWD PRESSURE BULKHEAD SIDE FRAME AT LOWER FUSELAGE, STA. 178, WL 207, LBL 28, CRACKED. REPLACED FRAME PER BOEING SERVICE BULLETIN 737-53A1173, REV. 3, SECTION III, PART XI, POINT I, FIGURES 71 AND 72. 2L72 4F RTA16WE 20030423001752003042300175NM 2003 4 23 P5CA0300781 120030316A2751 FLAP BOEING747 7472U3B 1384846NM TE FLAPS FAILED A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23923FT 22769 OUTBOUND FLAPS FAILED TO EXTEND PRIOR TO TAXI. FLAPS WERE CYCLED ELECTRICALLY & THEN WITH HYDRAULICS. OPS CHECK WAS SATISFACTORY. UNABLE TO DETERMINE THE CAUSE AT THE TIME. 2L74 4F RTA20WE 20030423001832003042300183NM 2003 4 23 QXEA0300363 120030311A2120 SMOKE BOMBDRDHC8 DHC8401 1390041NM COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09402QX 4032 PDX FLIGHT 2373 SMOKE IN CABIN FROM APU. MAINTENANCE RAN APU FOR THREE HOURS, NO SMOKE OR ODOR. COULD NOT DUPLICATE PROBLEM. NO PARTS REPLACED. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030423001862003042300186NM 2003 4 23 VNAA0303014 120030312A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL07470PS17545104 3006 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030423002042003042300204NM 2003 4 23 UPS03240302 120030218A5753 FLAP TRACK BOEING727 727108C 1384039NM NR 5 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, NR 5 FLAP TRACK HAS CORROSION ON MOUNT HOLES C, E, F & CORROSION ON MOUNT PADS A & B. REFER TO SMRO EO 2003-008-008 & UPS EO B727-5742-0651-K FOR DETAILED SIGNOFF & RECTIFICATION. UPS ENGINEERING FILE B727-540-18418-B. 2L73 4F A3WE 20030423002092003042300209NM 2003 4 23 UPS03240309 120030218A5753 FLAP TRACK BOEING727 727108C 1384039NM NR 3 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&S, NR 3 FLAP TRACK HAS SURFACE CORROSION IN THE FOLLOWING AREAS, INSIDE HOLE D, INSIDE HOLE E, INSIDE HOLE F, INSIDE HOLE G & FLAP AFT PAD (B). REPAIR CARRIED OUT IAW SRMO EO 2003-008-006 & 2003-008-012 UPS ENGINEERING FILE NR 727-57-20094. 2L73 4F A3WE 20030424000032003042400003NM 2003 4 24 QXEA0300366 120030318A323054C546349 VALVE DHAV DHC8 DHC8202 2809007NM ZONE 700 MALFUNCTIONED A QXEAL ABORTED APPROACH O OTHER APAPPROACH 1 NM09353PH 496 SEA ON FLIGHT 2051- ON APPROACH NOSE GEAR DID NOT EXTEND. CREW MISSED APPROACH AND PERFORMED ALTERNATE GEAR EXTENSION. NR 1 NOSE GEAR THEN IDICATED GREEN. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE LANDING GEAR SOLENOID SEQUENCE VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424000102003042400010EA 2003 4 24 SWIA200311834 120030316A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB FAILED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07439SW3593 3593 7578 LOST STAB AND MACH TRIM EN ROUTE. REENGAGED AS PER QRH. AFTER 10 MINUTES, THE PROBLEM OCCURRED AGAIN. REENGAGED AND SLOWED TO 250 KIAS. MAINTENANCE DIAGNOSTIC COMPUTER INDICATED HSTCU FAILED. REMOVED AND REPLACED HSTCU IAW 27-41-01. 2L72 4F RTA21EA 20030424000122003042400012EA 2003 4 24 QXEA0300377 120030314A2840D98C07606 SENSOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09607QX 10024 YEG ON FLIGHT 2371- LEFT FUEL LOW PRESSURE CAUTION. REMOVED AND REPLACED ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030424000162003042400016NM 2003 4 24 UPS03240322 120030308A5753 RIB BOEING727 72725C 138400HNM NR 4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 INSPECTION TYPE:C, LEFT WING, SUSPECT CRACK AT I/B TRACK RIB ON NR 4 SLAT. CRACK STOP DRILLED IAW SRM 51-10-01. 2L73 4F A3WE 20030424000202003042400020WP 2003 4 24 UPS03840313 120030302A5754 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2 LEFT WING L/E LOWER RIBS ARE CRACKED AT FASTENER END AT XFS 616.25 AND XFS 622.5 FWD OF PANEL OPENING. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATED CRACKS. FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030424000442003042400044NM 2003 4 24 QXEA0300346 120030309A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CHAFING ON PANEL ATTACH FLANGES, PANEL 262FT, ENTIRE FORWARD EDGE OF PANEL FLANGE. REPAIRED IAW HORIZON AIR EA 6-57-122 AND RD 8/4-57-143. 2H72 4T RTA13NM 20030424000482003042400048NM 2003 4 24 QXEA0300323 120030227A5410 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - SUPPORT BRACKET CRACKED AT LOWER AND UPPER ANGLE OF LEFT HAND LOWER COWL, ABOVE BYPASS DOOR. REPAIRED IAW Q400 MM TASK 71-61-06-400-801. 2H72 4T RTA13NM 20030424000492003042400049NM 2003 4 24 QXEA0300324 120030227A5410 HINGE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - LEFT HAND LOWER COWL, BYPASS DOOR HINGE HAS APPROXIMATELY .030 RADIAL PLAY. REPAIRED IAW RD 8/4-71-016 AND Q400 MM TASK 71-61-01-400-801. 2H72 4T RTA13NM 20040223000162004022300016NM 2004 2 23 Y1R2004F00000 120031212A7921UA52627624 OIL COOLER BOEING727 727223 1384074NM PWA JT8 JT8D15A 52051NE CSD NR 3 ENG CRACKED B Y1RRO OTHER K FLUID LOSS NRNOT REPORTED 1 WP01289MT 244 22467 CRACK DEVELOPED ON RT SEAM OP OIL COOLER, UNIT WAS REPAIRED AND ACCUMULATED 31.5 HOURS TSR. CRACKED AGAIN IN WELD AREA OF RT SEAM OF CSD OIL COOLER. (WP01200405240) 2L73 4F4 F A3WE E2EA 20040223000482004022300048NM 2004 2 23 SVU2004F00000 120031230A2750 CABLE AMD FALC50FALCON2000 2730170NM TE FLAP XMTER BINDING B SVURO OTHER O OTHER NRNOT REPORTED 1 SW19202FX412 970 002 CABLE BINDING AND CAUSES FLAP ASYMMETRY. 2K73 4F RTA50NM 20040223000582004022300058EA 2004 2 23 SVU2004F00004 120031216A2740 TRANSFORMER CNDAIRCL604 CL604 1900301EA GE CF34 CF34* NE HCU DEFECTIVE B SVURO OTHER O OTHER NRNOT REPORTED 1 SW19322FX3718 256 5434 CHANNEL NR 1 DISENGAGES DURING FLIGHT. (WO NR 34166) 2L72 4F4 FRTA21EA E15NE 20040223000752004022300075SO 2004 2 23 SWIA200312748 120031214A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07229SW 120305 CABIN CENTER FLOORBEAM FLOORBOARD SUPPORT HAS CORROSION (AFT OF MUFFLER ASSY). (DISCOVERED DURING C-CHECK INSPECTION)REPLACED CENTER BEAM BUTT STRAPS, 2 EACH, 1 FORWARD AND 1 AFT OF LAVATORY IAW 120 SRM 51-10-02 PG 3 SEC 3. 2L72 4T4 TRTA31SO E20NE 20040223000932004022300093NM 2004 2 23 F3LA200300191 120031231A278265C3805823 ACTUATOR BOEING737 73736N 1384408NM NR 3 SLAT INOPERATIVE A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED NR 3 SLAT ACTUATOR FAILED LOCK PIN TEST. REPLACED NR 3 SLAT ACTUATOR IAW MM 27-81-41 AND ACCOMPLISHED LE SLAT ACTUATOR LOCK PIN TEST AND LE SLAT ALTERNATE SYSTEM TESTS IAW TASK CARD 5-2710 AND MM 27-81-00. 2L72 4F RTA16WE 20040223000942004022300094NE 2004 2 23 PNSA031213 220031225A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 1 ENGINE FOD A PNSAA UNSCHED LANDING C F.O.D. CLCLIMB 1 AL03675PA 340B206 785539 WHILE AC WAS BEING RELOCATED AFTER MAINTENANCE, A/C WAS ON TAKEOFF IN NR 1 ENGINE SUFFERED FOD AND SUBSEQUENT COMPRESSOR STALL. ENGINE WAS SHUT DOWN AND AN UNEVENTFUL LANDING WAS MADE. A BLUE SHOP TO WELL WAS LOCATED IN THE ENGINE INLET COVERING AT LEAST TWO INLET GUIDE VANES. ENGINE WAS REMOVED FOR INSPECTION AND REPAIR. 2L72 4T4 TRTA52EU E8NE 20040223000992004022300099EA 2004 2 23 SVU2004F00006 120031219A2741 EXTRACTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HSTCU BROKEN B SVURO OTHER O OTHER NRNOT REPORTED 1 SW19967CA6986 204 7134 CHANNEL (A) INTERMITTENT FAILURE. (WO NR 00033982) 2L72 4F4 FRTA21EA E15NE 20040223001772004022300177WP 2004 2 23 ABXA040020 120031223A531099577397 SHEAR TIE DOUG DC9 DC932 3022066WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 SHEAR TIE CRACKED AT FS 947 BETWEEN LONGERON 15 AND 16 RT. REMOVED AND REPLACED SHEARTIE IAW DC-9 SRM. 2L72 4F A6WE 20040223001862004022300186WP 2004 2 23 ABXA040025 120031229A533059114187 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 SKIN AT FS 610 BETWEEN LONGERON 28 LT AND LONGERON 28 RT WAS SEVERLY CORRODED, EXFOLIATED AND BULGED. CUT OUT CORROSION AREA OF SKIN, INSTALLED REPAIR DOUBLER / FILLER IAW SRM 53-01. 2L72 4F A6WE 20040223001332004022300133EU 2004 2 23 MALA030608 120031229A1430 FASTENER SAAB SF340 340B 7860101EU GALLEY CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4Y/2Y INSPECTION, FWD LT GALLEY LOCK DOWN POINT HAS CORRODED FASTENERS, 8 EACH. MECHANIC REMOVED AND REPLACED CORRODED FASTENERS AND FLOOR SUPPORTS IAW SAAB 340 SRM 51-40-21, 51-40-40, 51-20-20, 51-20-42 AND 51-20-43. A/C RELEASE DATE 01/09/04. REFER TO NR 1196389 FOR ADDITIONAL DETAIL. 2L72 4T RTA52EU 20040224000532004022400053WP 2004 2 24 ASAA0380276 120030330A33970105603 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01961AS 53075 SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING AT ROW 27-30 WAS FOUND TO BE INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040224000752004022400075WP 2004 2 24 GKZR200479905 120031104A574456466014 SUPPORT FITTING DOUG DC8 DC862 3021970WP RT AILERON CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 RIGHT O/B AILERON NR 7 SUPPORT HINGE FITTING HAS A CRACK AT LWR O/B BOLT HOLE. REMOVED RIGHT O/B AILERON IAW DC8 MM 27-11-2. REMOVED AND REPLACED RIGHT O/B AILERON HINGE SUPPORT FITTING IAW DC8 DRAWING 5619462. REINSTALLED RIGHT O/B AILERON IAW DC8 MM 27-11-2. 2L74 4F 4A25 20040224000782004022400078WP 2004 2 24 GKZR200479906 120031105A574456466011 SUPPORT FITTING DOUG DC8 DC862 3021970WP LT AILERON CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 LEFT O/B AILERON NR 7 SUPPORT FITTING CRACKED. REMOVED LEFT AILERON IAW DC8 MM 27-11-2, REMOVED AND REPLACED LEFT O/B AILERON O/B ATTACHMENT BRACKET IAW DC8 DRAWING 5619462. REINSTALLED AILERON IAW DC8 MM 27-11-2. 2L74 4F 4A25 20040223000272004022300027WP 2004 2 23 G1F2004F00000 220031208A7320XA9511E0033 PUMP BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE731* 01518WP FUEL SYSTEM CORRODED B G1FRO OTHER O OTHER NRNOT REPORTED 1 GL13466AE NA0466 THIS UNIT WAS SUPPLIED BY THE CUSTOMER FOR REPLACEMENT OF A FAILED TKS METERING PUMP IN THE AIRCRAFT. PRIOR TO INSTALLATION, UNIT WAS INSPECTED BY TECHNICIANS. LINE FITTINGS WHERE FOUND TO BE INSTALLED INCORRECTLY. FURTHER INSPECTION UPON DISASSEMBLY FOUND THE PUMP WITH INTERNAL CORROSION AND A SWELLED FILTER ELEMENT. PUMP ASSEMBLY APPEARS TO BE CONTAMINATED BY UNKNOWN FLUID. ADDITIONAL INSPECTION FOUND THE PUMP MOTOR INOPERATIVE. UNIT WAS OVERHAULED TO CORRECT THE CORROSION AND FILTER DAMAGE. DEFECTIVE PUMP WAS NOT INSTALLED AND NO CONTAMINATION OCCURRED TO THE AIRCRAFT. A REPLACEMENT METERING PUMP WAS PROCURED FROM A DIFFERENT VENDOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20030801000392003080100039WP 2003 8 1 GTIA030538 120030630A5755 MOUNT BRACKET DOUG DC9 DC982 3022082WP RT SPOILER CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - RIGHT WING INBOARD SPOILER TORSION BAR INBOARD MOUNT BRACKET CRACKED. REMOVED AND REPLACED RIGHT WING INBOARD SPOILER TORSION BAR INBOARD MOUNT BRACKET. (M) 2L72 4F A6WE 20030801000422003080100042WP 2003 8 1 GTIA030528 120030606A5230 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD CARGO DOOR PAN AND STRAPS CORRODED AND SOME AREAS FORWARD AND AFT EXFOLIATED AT FS 370-427 ALL ALONG BOTTOM. FORMED NEW DOUBLERS. LOCATED AND DRILLED DOOR PAN. INSTALLED FORWARD CARGO PIT DOOR PAN. INSTALLED 4 EACH REPAIR DOUBLERS. (M) 2L72 4F A6WE 20030801001082003080100108EA 2003 8 1 COMA0360328 120030717A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01958CA 7111 FLIGHT 5368 EMERGENCY FLOOR PATH LIGHTING IS INOP. RECONNECTED POWER STRIP AT ROW 6. 2L72 4F RTA21EA 20030801001242003080100124WP 2003 8 1 MWEA030270 120030630A2120 DUCT DOUG DC9 DC932 3022066WP A/C BAY LOOSE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31401ME 47133 FLIGHT ATTENDANT REPORTED A LOUD NOISE COMING FORM TAIL COMPARTMENT. FOUND ORANGE DUCT LOOSE AT TURBINE EXHAUST, RECONNECTED AND CLAMPED THE SAME. 2L72 4F A6WE 20030805000722003080500072SO 2003 8 5 SIMA200319002 120030708A550014534370415 ELEVATOR EMB 135 EMB135LR 3260305SO TAIL DAMAGED A SIMACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW21726AE 145314 CLT - FLT 4430 - DURNG TAKEOFF ROLL AT ABOUT 60 KNTS CREW NOTED YOKES BEING SLAMMED TOWARDS THEM. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. DURING POST FLIGHT NOTED LEFT ELEVATOR TRIM STUCK DOWN IN THE 90 DEGREE POSITION. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR ASSEMBLY IAW EMB MM. GORUND FUNCTINAL CHECK WAS GOOD AND A FUNCTIONAL CHECK FLIGHT WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE.(M) 2L72 4F RTT00011AT 20030805000752003080500075EA 2003 8 5 ASOA03301 120030710A3350MS220735 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSTRIPPED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY LIGHTS REMAINED ON WHEN IN THE ARMED POSITION. MAINTENANCE RESET THE CIRCUIT BREAKER TO THE EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030805000902003080500090EU 2003 8 5 ASOA03302 120030710A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 FLT 4164 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030805001082003080500108EA 2003 8 5 ASOA03273 120030611A5330601R310621 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING HANGAR MAINTENANCE IN CKB, THE FUSELAGE SKIN AT FS 310 BETWEEN STRINGERS 16L AND 17L WAS FOUND TO BE DENTED BEYOND LIMITS. MAINTENANCE REPAIRED THE FUSELAGE SKIN AT FS 310 BETWEEN STRINGERS 16L TO 17L IAW ASA EO 600-53-0097. (M) 2L72 4F RTA21EA 20030805001122003080500112EA 2003 8 5 ASOA03276 120030624A270013740002 SWITCH CNDAIRCL600 CL6002C10 1390015EA COCKPIT INOPERATIVE A ASOAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO11709EV 10068 DUIRNG CRUISE, LEVELING AT 37,000 FT THE CREW RECEIVED STABILIZER, MACH AND PITCH TRIM MESSAGES. UNABLE TO GET STABILIZER CHANNELS ONE OR TWO TO RE-ENGAGE. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM ENGAGE SWITCH. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030806000782003080600078NM 2003 8 6 AWXA200300873 120030712A53126517583136 STIFFENER BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C14 CHECK A .5 INCH CRACK WAS FOUND INBOARD SIDE BS 178 BULKHEAD VERTICAL TEE AT CENTER RADIUS LBL 5.7, WL 183-184. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL TEE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 5 EACH REPAIR ANGLES, 2 EACH STRAPS, 6 EACH FILLERS, AND A STIFFENER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG 205, PG 221-240. 2L72 4F RTA16WE 20030806000962003080600096SO 2003 8 6 C2XA03TY119 120030801A534714532606013 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION, SEAT TRACK LF4 WAS FOUND CORRODED. MAINTENANCE REMOVED THE TRACK, CLEANED THE CORROSION AND REINSTALLED IAW EC5340-01048. 2L72 4F RTT00011AT 20030806001062003080600106SO 2003 8 6 C2XA03TY104 120030802A532014522459003 ANGLE EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IN THE GALLEY IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030806001172003080600117SO 2003 8 6 C2XA03TY089 120030710A323023092900001 UPLOCK EMB 145 EMB145ER 3260211SO MLG FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW271594811297 145056 AIRCRAFT DIVERTED INTO TYS (FLIGHT WAS SCHEDULED FROM ALANTA TO CLEVLAND) BECAUSE NOSE GEAR WOULD NOT COME UP. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UPLOCK BOX IAW EMB-145-MM-32-33-07, OPERATIONAL CHECKED GOOD. AIRCRAFT WAS RELEASED TO SERVICE WITH NO FURTHER FAULTS. 2L72 4F RTT00011AT 20030806001182003080600118SO 2003 8 6 C2XA03TY099 120030725A5522 SKIN EMB 145 EMB145ER 3260211SO ELEVATOR SPLIT A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW27139295438 5438 041 145009 ON GROUND WITH GUSTLOCK ENGAGED, AIRCRAFT EXPERIENCED WINDS GUSTING 54+KTS. GUSTLOCK DISENGAGED. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE LEFT ELEVATORS UPPER SKIN DAMAGED. MAINTENANCE REPAIRED THE DAMAGE AND BALANCED ELEVATORS IAW EC5520-0026 AND AMM-51-60-00. TEST FLIGHTED GOOD. 2L72 4F RTT00011AT 20030806001312003080600131SO 2003 8 6 C2XA03SH259 120030804A532014522459001 RAMP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 SHV- DURING C-CHECK, THE SUPPORT RAMP BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030724000562003072400056NM 2003 7 24 DL76L030552 120030609A80108113901 START VALVE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27171DN 24759 724639 DIVERTED TO SNN DUE TO LEFT ENGINE START VALVE LIGHT ILLUMINATED IN FLIGHT. REPLACED LT ENGING START VALVE. OPS CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20030724000772003072400077NM 2003 7 24 AWXA200300700 120030615A2751 WARNING HORN AIRBUSA319 A319132 3930340NM TE FLAPS ACTIVATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28806AW 1056 ON TAKEOFF ROLL AT SNA EN ROUTE FOR LAS AT 70 KTS TAKEOFF CONFIGURATION WARNING SOUNDED, REJECTED TAKEOFF. RECONFIGURED FLAP HANDLE AND TOOK OFF WITHOUT FURTHER EVENT. 2L72 4F RTA28NM 20030724000812003072400081EU 2003 7 24 AWXA200300800 120030628A5415D54630462200 ATTACH ANGLE AIRBUS320 A320231 3930325EU ZONE 480 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 MCN - MAJOR REPAIR - DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON RT PYLON UPPER ATTACH ANGLE AT SCREW HOLE FORWARD OF RIB 8. MAINTENANCE CUT OUT DAMAGE ON RT PYLON ATTACH ANGLE FORWARD OF RIB 8; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A320 SRM 54-52-12 PG 215-220 FIG 2. 2L72 4F RTA28NM 20030725000092003072500009NM 2003 7 25 AWXA200300755 120030617A5320652998504 SUPPORT ANGLE BOEING737 7373G7 138447JNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-13 CHECK CORROSION WAS FOUND ON L-1 DOORWAY THRESHOLD SUPPORTS BS 312, STR 18 LT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED 2 EACH L-1 DOORWAY THRESHOLD SUPPORT ANGLES BS 312, STR 18 LT; FABRICATED 2 EACH NEW REPLACEMENT THRESHOLD SUPPORT ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-30-01, FIG 7. 2L72 4F RTA16WE 20030725000192003072500019NM 2003 7 25 03FDEA00827 120030530A3260656021132 ACCESSORY UNIT BOEING727 727200 138407ENM E&E COMPARTMENT FALSE INDICATIONA FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25496FE 21670 DURING T/O GEAR RETRACTION, RED "RIGHT GEAR" LIGHT REMAINED ILLUMINATED. FOLLOWED RED TAB PROCEDURES BUT LIGHT REMAINED ON. NO OTHER LIGHTS OR INDICATIONS OBSERVED. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND OPS CHECKED GOOD IAW M/M 32-09-122-5. RECHECKED R/H UP LOCK SENSOR. OPS CHECKED GOOD IAW M/M 32-61-081- 4 A/C OK FOR SERVICE. 2L73 4F RTA3WE 20030725000232003072500023EU 2003 7 25 RAIA00305133 120030507A33507012210 BULB AEROSPATR72 ATR72202 8680940EU EMERGENCY LIGHT BURNED OUT A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03721TE 217 EMERGENCY LIGHT INOP ON STEP. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. 2H72 4T RTA53EU 20030731000272003073100027EA 2003 7 31 QXEA200300857 120030717A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT FALSE INDICATIONA QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX 10045 EUG- FIRE SYSTEM FAULT STATUS MESSAGE. CYCLED CB FIREX A&B PER PMM 4-1-0 AND PERFORMED FIRE SYSTEM TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000322003073100032EA 2003 7 31 QXEA200300867 120030721A2160 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING UKUNKNOWN 1 NM09607QX 10024 BOI- ON FLIGHT 2457 RIGHT PACK TEMPERATURE CAUTION LIGHT. RETURNED TO FIELD. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH LRU TEST ACSC, NO FAULTS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000752003073100075EA 2003 7 31 QXEA200300806 120030709A4920WE38007703 APU CNDAIRCL600 CL6002C10 1390015EA APU BAY MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09602QX3893 10010 PDX-SUP-WHILE AIRCRAFT WAS SITTING AT GATE WITH APU RUNNING CABIN FILLED WITH SMOKE.AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED APU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000902003073100090NM 2003 7 31 QXEA200300834 120030709A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - RIGHT HAND FUSELAGE HAS THREE DENTS JUST BEHIND ICE SHIELD AT STRINGER 175 AND STRINGER 185. REPAIRED IAW HORIZON AIR EA 6-53-2801. 2H72 4T RTA13NM 20030731001092003073100109EA 2003 7 31 QXEA200300898 120030723A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX- SCRAPE BELOW FORWARD SERVICE DOOR FORWARD SIDE 10 INCHES BELOW DOOR APERATURE. REPAIRED IAW CRJ-700 SRM 51-12-00, 53-21-01, 51-25-16 AND 51-20-06. 2L72 4F RTA21EA 20030801000082003080100008WP 2003 8 1 GTIA030526 120030617A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND MID PIT STATION 750 STRINGER 29R-28R CORROSION ON SKIN. CUT SKIN TO FOM SIZE OF SKIN CUTOUT IS 7.5 INCHES BY 11 INCHES. CORROSION REMOVAL WITHIN ALLOWABLE LIMITS. FABRICATED REPAIR PARTS 1 EACH FILLER, 1 EACH DOUBLER, 2 EACH FINGER DOUBLER. INSTALLED FINGER DOUBLER, FILLER, AND REPAIR DOUBLER. (M) 2L72 4F A6WE 20030801000742003080100074EU 2003 8 1 ASOA03288 120030704A33507012210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11531AS 454 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LGIHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030801001042003080100104EA 2003 8 1 COMA0360330 120030719A7710 SWITCH CNDAIRCL600 CL6002B19 1900309EA RT ENGINE FLUCTUATES A COMAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO01492CA 7763 FLIGHT 5772 RT ENGINE N1,N2,ITT,F/F, AND OIL PRESSURE FLUCTUATING - AIRCRAFT OSCILLATED UP AND DOWN. DEFERRED THE ENGINE SPEED SWITCHES IAW MEL. 2L72 4F RTA21EA 20030801001252003080100125NM 2003 8 1 MWEA030290 120030727A291366180 PUMP BOEING717 717200 1383700NM HYD SYSTEM LEAKING A MWEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31906ME 55170 LEFT HYDRAULIC QUANITY ALERT LOW. REMOVED AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP AND FILTER ELEMENTS, ALSO RETORQUED LOOSE B-NUT. 2L72 4F TRA6WE 20030806001322003080600132SO 2003 8 6 C2XA03SH206 120030701A532014525422001 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE LEFT HAND SILL BETWEEN FRAMES 61 AND 65 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030806001442003080600144NM 2003 8 6 AWXA200300850 120030711A5311654653949 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A .25 INCH CRACK WAS FOUND ON FRAME AT BS 616, LBL 65, WL 200. MAINTENANCE CUT OUT CRACK ON FRAME AT BS 616, LBL 65, WL 200; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20030806001652003080600165 2003 8 6 AWXA200300838 420030722A34601714970501 COMPUTER BOEING737 7373G7 1384595NM FLT MANAGEMENT MALFUNCTIONED A AWXAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 WP28157AW6192 23779 ON DEPARTURE, EN ROUTE. THE FLIGHT MANAGEMENT COMPUTER (FMC) FAILED. NAV FLAGS INDICATED ON CAPTAINS & FIRST OFFICERS RMI IN BOTH NAV IN VOR MODE, AND HEADING FLAG ON CAPTAINS HSI. TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FMC IAW BMM 34-62-21, T/C A1B34067, & T/C AIB34060. ALSO PERFORMED AN INTERFACE TEST OF LT IRU. VENDOR COULD NOT VERIFY REASON FOR REMOVAL. UNIT PASSED DIAGNOSTIC INTERFACE TEST, DOWNLOAD OF OFP & NDB SOFTWARE VERIFIED PROPER OPERATION. MODULES, CHASSIS, AND BACKPLANE WERE INSPECTED AND UNIT WAS TESTED EXTENSIVELY WITH NO FAULT FOUND. 2L72 4F RTA16WE 20030806001702003080600170EU 2003 8 6 AWXA200300871 120030802A5220 DOOR AIRBUS320 A320232 3930326EU EMERGENCY EXIT OBSTRUCTED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28619AW 527 ON TAKEOFF AT IAD EN ROUTE FOR PHX RECEIVED DOOR WARNING INDICATION LT OVERWING EXIT, REJECTED TAKEOFF AT 79 KTS. MAINTENANCE FOUND THE COVER OVER THE LT OVERWING EMERGENCY EXIT LOOSE AND WEDGED IN DOOR, RESECURED COVER AND WARNING INDICATION EXTINGUISHED. 2L72 4F RTA28NM 20030807000072003080700007EA 2003 8 7 ASOA03259 120030614A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11880AS 7606 DURING A GROUND INSPECTION IN MGM, THE AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OVERHEAD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030801000792003080100079NM 2003 8 1 UPS03440936 120030617A5320HXC108663 ANGLE BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C FX - AIR CONDITIONING BAY PANEL SUPPORT LOWER SURFACE FLOATING NUT AREA FOUND SURFACE CORROSION AT STA 1220 TO STA 1235 RBL 57 I/B SIDE. PANEL SUPPORT REPAIRED AT FX BODY FAIRING SUPPORT LOWER BS 1220-1235 RBL 57 I/B SIDE AS IAW SRM 51-40-04 FIG 1. 2L74 4F A20WE 20030801000852003080100085SO 2003 8 1 C2XA03SH225 120030717A33977287580501 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 SHV-DURING C CHECK THE NUMBER 3 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030801001112003080100111EA 2003 8 1 COMA0360332 120030722A3234750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01819CA7709 7415 FLIGHT 5312 GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20030805000732003080500073EU 2003 8 5 USAASA03076 120030708A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19723UW 1109 AN EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POEWR SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030806000622003080600062EU 2003 8 6 AWXA200300857 120030728A3397ABS0374A24 CABLE AIRBUS320 A320231 3930325EU SEAT ROW 22 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT WAS FOUND INOPERATIVE. RELAMP, NO HELP. MAINTENANCE REPAIRED A BROKEN WIRE AT SIDE WALL DISCONNECT FOR SEAT ROW 22 LT EMERGENCY ESCAPE PATH LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030806000692003080600069NM 2003 8 6 AWXA200300851 120030711A49106566212 SHROUD BOEING737 7373G7 1384595NM APU CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A .375 INCH CRACK WAS FOUND ON APU UPPER SHROUD AT RT FORWARD CORNER. MAINTENANCE PERFORMED A WELD REPAIR ON UPPER APU SHROUD IAW AWA ER 03-4913-00110-DL1; DYE PENETRANT INSPECTION OF WELD VERIFIED NO CRACKS EXIST. 2L72 4F RTA16WE 20030806000902003080600090SO 2003 8 6 C2XA03TY108 120030801A534714532606003 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK LW3 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030806001422003080600142SO 2003 8 6 C2XA03BT076 120030725A27413621001009MOD1 CONTROL MODULE EMB 145 EMB145ER 3260211SO EMPENNAGE FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149373489 3489 145026 CREW REPORTED, AFTER TAKEOFF PITCH TRIM SYSTEM NR 1 AND NR 2 INOPERATIVE. RETURNED FOR LANDING BACK IN NEWARK. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT (HSCU) IAW EMB145 AMM 27-40-01. OPS CHECKED PITCH TRIM SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030806001552003080600155SO 2003 8 6 C2XA03SH215 120030702A531014525480003 BEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 SHV- DURING C-CHECK, THE CARGO DOOR LOWER STRUCTURE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030807000062003080700006NM 2003 8 7 USAASB03103 120030706A2780189929 SWITCH BOEING737 737301 1384611NM NR 2 LE FLAP FAILED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19590US 23935 ON CLIMB-OUT FROM PHL, EN ROUTE TO ATL, CREW REPORTED THE LT WING INBOARD LEADING EDGE FLAP WOULD NOT RETRACT. CREW RECYCLED FLAPS TWICE WITH NO SUCCESS. FLIGHT RETURNED TO FIELD TO PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 LEADING EDGE FLAP S170 RETRACT SWITCH PER MM 27-81-11-004. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040223001322004022300132NM 2004 2 23 DHL2003753502 120030106A5312 PRESSURE PANEL BOEING727 727223 1384074NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING "C" CHECK, NOSE SECTION LOWER LOBE INTERIOR PRESSURE WEB AT BS 294. PREVIOUS CRACK REPAIR DO NOT MEET SRM. REMOVED PREVIOUS REPAIR AT NOSE SECTION LOWER LOBE INTERIOR PRESSURE WEB, BS 294 IAW B-727, SRM 51-30-2. CUT OUT DAMAGED IAW B727 SRM 51-40-2, REPAIR DOUBLER AND FILLER MAT. USED 7075-T6, .071, PO NR 9012380, DIMENSIONS AREA DOUBLER 5 INCHES X 4 3/4 INCHES AND FILLER 3 INCHES X 2 INCHES IAW B-727 SRM 51-40-2. ACCOMPLISHED MAT. HFEC AROUND CUT OUT HICA IAW PART 6, 51-00-00 FIG. 6. NO CRACKS TREATED, ALODINED, AND PRIMED IAW B-727 SRM 51-10-2 INSTALLED DOUBLER AND FILLER REPAIR IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040223001672004022300167SO 2004 2 23 QRX2004F00001 120031205A783094HEN102RA SWITCH GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE THRUST REVERSER FAILED B QRXRO OTHER O OTHER ININSP/MAINT 1 SW0584GV 2334 584 SWITCH FAILED. FOUND THE SWITCH HOUSING FULL OF WATER. THIS SWITCH IS LOCATED ON THE TOP SIDE OF THE ENGINE NACELLE. IT APPEARS TO HAVE WATER MIGRATING THROUGH THE SWITCH PLUNGER INTO THE HOUSING. THIS COULD COME FROM BEING PARKED IN THE RAIN OR AIRCRAFT BEING WASHED. 2L72 4F4 FRTA12EA E00057EN 20040224000502004022400050NM 2004 2 24 ASAA0310252 120030327A531165549581 FRAME BOEING737 737298C 1384490NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FRAME AT BS 500B, STRINGER 23L CHAFED AND DENTED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040224001002004022400100WP 2004 2 24 GKZR200479909 120031115A5330 SKIN DOUG DC8 DC862 3021970WP FUSELAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 RIGHT AFT FUS BETWEEN STA 1540 & 1551 HAS CORROSION UNDER PAINT. STARTED REMOVING CORROSION FOUND SMALL POCKET OF INTERGRANULAR, CUT DAMAGED AREA OUT, FABRICATED FILLER & DOUBLER IAW DC8 SRM 53-02-01, TREATED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FILLER & DOUBLER IAW DC8 SRM 53-02-01. 2L74 4F 4A25 20040225001632004022500163NM 2004 2 25 DL73S031131 120031224A5510 ATTACH FITTING BOEING737 737232 1384475NM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 CORROSION WAS NOTED DURING INSPECTION OF THE HORIZ STAB ATTACH LUGS PER 03-069697-03 AND 03-053025-03AD. THE RIGHT SIDE OUTBOARD HORIZ STAB REAR SPAR UPPER ATTACH LUG WAS BEYOND PUBLISHED ALLOWABLE LIMITS. CORROSION WAS REMOVED AND LUG REWORKED PER ERA 385985-14AD. 2L72 4F RTA16WE 20040223001852004022300185NM 2004 2 23 UPS04M41715 120031227A1430 FASTENER DOUG MD11 MD11F 3023600NM NR 2 NOSE COWL LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01253UP INSPECTION TYPE: 1C, NR 2 ENGINE NOSE COWL HAS LOOSE FASTENERS. MODIFIED BULKHEAD WEB TO ALLOW ACCESS TO LOOSE RIVETS BY ENLARGING ORIGINAL ACCESS HOLES AND ADDING 6 NEW ACCESS HOLES AND ADDED DOUBLERS AND ACCESS PANELS TO ALL HOLES IAW SAA SK 253-532 AND UPS ENGINEERING FILE MD11-71-20001. 2L73 4F RTA22WE 20040224000742004022400074WP 2004 2 24 GKZR200479904 120031101A5730 SKIN DOUG DC8 DC862 3021970WP RT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 RIGHT WING UPPER SURFACE FROM WING ROOT TO STA 624 HAS NUMEROUS LOCATIONS OF EXFOLIATION RUNS FROM FRONT SPAR TO AFT SPAR. REMOVED CORROSION IAW DC8 SRM 51-1-8, NDT VERIFIED ALL WITHIN LIMITS. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FASTENERS IAW DC8 SRM 51-1-20. 2L74 4F 4A25 20040225001102004022500110SO 2004 2 25 T042004F00000 120030826A214027D48 FAN BLADE PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA HEATER FAILED E T04AO OTHER O OTHER NRNOT REPORTED 1 AL0327663 580 19997785 317852094 FAN BLADE BROKE (1 OF 4 PADDLES). VIBRATION CAUSED WIRE CONNECTOR TO FAIL. FURTHER DAMAGE AVOIDED. 1L72 3O3 O A20SO E14EA 20040225001542004022500154NM 2004 2 25 DL767031122 120031219A531214872610100 PANEL BOEING767 767232 1385132NM PRESS BULKHEAD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27101DA 22213 INSPECTION OF THE AFT P-DOME GORE PANELS PER AD 88-19-03 REVEALED A CRACK AT A FASTENER LOCATION COMMON TO THE STIFFENER 13R LAP JOINT. THE CRACK WAS REMOVED WITH A CUTOUT TO THE GORE PANEL AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088005-14AD. 2L72 4F RTA1NM 20040225001802004022500180 2004 2 25 DL76G031149 420031230A256520131A BATTERY BOEING767 767324 1385203NM ESCAPE SLIDE DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27394DL 27394 ON PDC FOUND LEFT SLIDE AND RIGHT SPOILER SQUIBS NOT TESTING IN COCKPIT. REPLACED BATTERY PACK AT 22G, CHECKS NORMAL. 2L72 4F RTA1NM 20040226000042004022600004NM 2004 2 26 ASAA0380294 120030406A3397 CONNECTOR GULTON DOUG MD80 MD83 3023681NM EMERGENCY LIGHT UNSECURE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01981AS 53472 SJC - DURING PREFLIGHT, FOUND PORTION OF EMERGENCY TRACK LIGHTS INOPERATIVE. SECURED EMERGENCY TRACK LIGHT CONNECTOR. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RT 20040226000052004022600005WP 2004 2 26 ASAA0380295 120030406A3397 WIRE GULTON DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 PDX - DURING PREFLIGHT, FOUND FIRST CLASS SECTION OF EMERGENCY TRACK LIGHTS INOPERATIVE. REPAIRED EMERGENCY TRACK LIGHT WIRING. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20040226000062004022600006WP 2004 2 26 ASAA0380305 120030411A33970105603 WIRE GULTON DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 SEA PREFLIGHT CHECK, FIRST FOUR FEET OF EMERGENCY TRACK LIGHTING INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040226000172004022600017NM 2004 2 26 ASAA0370007 120030408A5320146A75032 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01607AS 29751 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT RAIL. REPLACED FLOOR SUPPORT RAIL PER SRM. (M) 2L72 4F RTA16WE 20040226000242004022600024NM 2004 2 26 ASAA0240166 120030322A534065C1612938 CHANNEL BOEING737 7374Q8 138447QNM RADAR MOUNT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND RADAR MOUNT SHELF CHANNEL IS CRACKED AT BS 204. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040226000272004022600027NM 2004 2 26 ASAA0310686 120031226A335086210144 BATTERY PACK BOEING737 7372X6C 1384552NM EXIT SIGN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND THE EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY PACK, THEN EXIT IDENTIFIER TESTED NORMAL. (M) 2L72 4F RTA16WE 20040224000572004022400057WP 2004 2 24 ASAA0380266 120030317A335060030451 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01967AS 49103 OAK - DURING LINE CHECK, FOUND THAT OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS CABIN ILLUMINATE WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040224000882004022400088WP 2004 2 24 GKZR200471C01 120031113A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 45961 FINGER DOUBLER ON PRESSURE WEB STA 188 TO 208 RBL 28 HAS CORROSION AND RIVET HEADS SHEARED. REMOVED CORROSION, CUT OUT DAMAGED AREA, FABRICATED FILLER, FINGER DOUBLER 2 EACH AND PLATE IAW DC8 SRM 53-2-0. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ALL REPAIR PARTS IAW DC8 SRM 51-1-21. 2L74 4F 4A25 20040225001572004022500157NE 2004 2 25 DL76K031125 220031222A7200CF680C2B6F ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 MAKING METAL A DALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27174DZ15403 29693 706101 ON CLIMBOUT 22,000 LEFT ENGINE COMPRESSOR STALL APPROX 5-6 TIMES. MOMENTARY FUEL ODOR IN CABIN. BOROSCOPE INSPECTION NR 1 ENGINE HPC, COMBUSTION CHAMBER, AND HPT NO DAMAGE FOUND, WENT FOR ENGINE RUN UNABLE TO COMPLETE DUE EGT IDLE 800 DEG. AFTER RUN FOUND METAL IN TAILPIPE. ENGINE TO BE REPLACED. 2L72 4F4 FRTA1NM E13NE 20040225001712004022500171NM 2004 2 25 DL73S031139 120031227A29106546858110 LINE BOEING737 737232 1384475NM NR 2 ENG HYD SYSCHAFED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27312DL 23084 717150 A SYSTEM HYDRAULIC FAILURE ON FINAL, PRESSURE AND QUANTITY WENT TO ZERO. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE CHAFED THROUGH. REPLACED LINE. 2L72 4F RTA16WE 20040226000032004022600003WP 2004 2 26 ASAA0380302 120030407A3397 WIRE GULTON DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01974AS 53450 PDX - PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040226000302004022600030NM 2004 2 26 ASAA0240146 120030318A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM FS 727D CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE FLANGE AT STATION 727D STRINGER 26-27R. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040225001752004022500175NM 2004 2 25 DL76L031144 120031228A30307705401 RELAY BOEING767 767332 1382001NM E/E FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27180DN 25985 UPON ROTATION FROM CVG, CAPT PITOT EICAS ILLUMINATED ALONG WITH ASSOCIATED DISAGREE LIGHT ON OVERHEAD PANEL. CYCLING C/B DID NOT HELP. ALL INDICATIONS NORMAL DURING START UP AND TAXI. DIVERT TO JFK. REPLACED K241 RELAY. OPS CHECK OK. 2L72 4F RTA1NM 20040226000402004022600040NM 2004 2 26 ASAA0240150 120030318A573065C2631175 SKIN BOEING737 7374Q8 138447QNM LT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND LEFT WING INBOARD EXHAUST GATE UPPER SKIN IS CHAFED ON FORWARD OUTBOARD EDGE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040227000222004022700022NM 2004 2 27 ASAA0340362 120031217A55126573783 SKIN BOEING737 737490 1384715NM STAB LE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01713AS 30161 OAK - DURING C-CHECK, FOUND DENT IN RIGHT STABILIZER LEADING EDGE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040227000442004022700044NM 2004 2 27 ASAA0340355 120031208A5414311A145017 SKIN BOEING737 7374Q8 138447QNM PYLONS CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01756AS 25097 GYR - DURING SI CHECK, FOUND NR 1 AND 2 PYLON INBOARD AND OUTBOARD STRUT SKINS CHAFING DAMAGE. REPAIRED IAW EA. 2L72 4F RTA16WE 20040227000792004022700079EU 2004 2 27 BAQA091475 120031210A56101172429702 WINDOW BOLKMS117 BK117B1 5626012EU COCKPIT CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME1995 7235 COCKPIT WINDOW IS CRACKED. REPLACED WITH SERVICABLE UNIT. 02/02/2004 1G72 3U H13EU 20040301000082004030100008EU 2004 3 1 KBM2004F00001 120031022A2842647510033 PROBE SNIAS 350 AS350BA 8680817EU FUEL GAUGE STICKS E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 FUEL GAUGE STICKS AT 20 PERCENT EVEN WHEN 65 GALLONS ADDED. REMOVED FUEL PROBE, BENCH TESTED, INSPECTED, FOUND GOOD. 1G71 3U NCH9EU 20040301000162004030100016EU 2004 3 1 KBM2004F00013 120031126A6510 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R DRIVESHAFT WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH1166 2884 TAIL DRIVE SHAFT NR 5 BEARING, WORN. REMOVED AND REPLACED WITH NEW. (K) 1G71 3U3 U H9EU E19EU 20040301000322004030100032EU 2004 3 1 PG92004F00011 120031020A33407051A4334017 LIGHT UROCOPEC130 EC130B4 8680989EU ANTI COLLISION FAILED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19135PH270 3695 ANTI COLLISION LIGHT FAILED WITH 270 HOURS. (RMA NR R045380) (K) 1G72 3U H9EU 20030805000192003080500019SO 2003 8 5 JUF2003F00000 120030519A32136531904 STRUT PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA MLG FAILED D JUFSO OTHER O OTHER LDLANDING 1 SO158258A11315 288116020 UPON TOUCH DOWN FOR LANDING, THE UPPER TORQUE LINK ATTACHMENT, ON THE LEFT MAIN LANDING GEAR BROKE AT THE CYLINDER ASSEMBLY, CAUSING THE OLEO PISTON TO FALL OUT OF THE CYLINDER. THE ATTACHMENT POINT APPEARED TO BE CRACKED PRIOR TO THE FLIGHT. RECOMMEND THAT DURING REGULAR INSPECTIONS, THE AREA BETWEEN THE (EARS) THE UPPER TORQUE LINK ATTACH POINT, BE CLEANED AND INSPECTED FOR CRACKS. 1L71 3O3 O 2A13 E274 20030805000222003080500022CE 2003 8 5 BKE2003F00000 120030522A29105407002340 TUBE LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE RT WHEEL WELL CHAFED E BKEAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP01502RP1961 199 DURING A ROUTINE INSPECTION, FOUND HYDRAULIC FLUID THAT APPEARED TO HAVE BEEN SPRAYED INTO THE RT WHEEL WELL. UPON INVESTIGATION FOUND THE UPLOCK ACTUATOR TUBE ASSY. NR 2 (PN 5407002340) HAD CHAFED THROUGH BY RUBBING ON A RIB ON THE AIRFRAME. THIS TUBE PASSES FIVE RIBS IN THIS AREA AND IS NOT SUPPORTED BY ANY CLAMPS IN ITS APPROX 21 INCH SPAM INSPECTION OF THE LT WHEEL WELL REVEALED THAT THE UPLOCK LINE WAS ROUTED BENEATH THE RIGS BUT STILL HAS POTENTIAL TO CONTACT THE RIBS AND CHAFE. NEED A PROCEDURE TO CLAMP THIS LINE TO PREVENT CHAFING. 2L72 4F4 FRTA10CE E35NE 20030805000572003080500057EA 2003 8 5 ASOA03252 120030604A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11845AS 7324 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FS 718 FORWARD SIDE BETWEEN STRINGERS 10 AND 12 WERE FOUND TO BE CRACKED BYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT FS 718 FORWARD SIDE BETWEEN STRINGERS 10 AND 12 IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20030805000582003080500058EA 2003 8 5 ASOA03251 120030604A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11845AS 7324 DURING A C-CHECK IN MCN, THE LT AND RT AFT DOUBLERS AT FS 718 BETWEEN STRINGERS 10 AND 12 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT AFT DOUBLERS AT FS 718 BETWEEN STRINGERS 10 AND 12 IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20030805000882003080500088EA 2003 8 5 ASOA03279 120030701A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11859AS 7421 DURING AN A-CHECK IN BTR, THE LEFT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EMERGENCY EXIT LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030805001062003080500106SO 2003 8 5 SIMA200319709 120030710A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21814AE 145541 ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE SHIMS. REPAIR DONE IAW EMB SRM EMB 145/1142 REV 21, CHAPTER 53-241-02 FIGURE 201. (M) 2L72 4F RTT00011AT 20030805001132003080500113SO 2003 8 5 SIMA200319706 120030710A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21814AE 145541 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGED SECTION OF LEFT OMEGA BEAM CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, EMB 145/1142 REV 22, CHAPTER 53-21-10 FIG 201, SHEET 1 AND CPM 51-61-00. (M) 2L72 4F RTT00011AT 20030806000042003080600004CE 2003 8 6 BAQA088143 120030718A213010246426 COMPUTER BEECH 100 100BEECH 1152916CE PRESSURIZATION MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 879 B144 UNABLE TO MAINTAIN ALTITUDE SETTINGS. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20030806000142003080600014SW 2003 8 6 ALGA088260 120030731A29135001908 COUPLING BELL 206 206B3 1181506SW HYD PUMP BROKEN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035011F 99100396 2564 HYD. PUMP REMOVED DUE TO ROTOR TACH. COUPLING NOT ENGAGED. FOUND COUPLING THREADED BUSHING HAD SEPARATED FROM COUPLING.REPLACED FAILED PARTS WITH NEW PARTS. SUBMITTED BY: PRESTON BARZARE 1G71 3U H2SW 20030806000292003080600029GL 2003 8 6 ALGA088266 220030801A725023031478 BEARING BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL NR 8 GALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03272M 647 CAT90102 45365 CAE890171 FOUND THE NR 8 BEARING GALLED ON INNER RACE. REMOVED AND REPLACED WITH SERVICABLE PART. 1G71 3U3 U H2SW E1GL 20030806000342003080600034NM 2003 8 6 AWXA200300823 120030706A5320D53470477208 PROFILE AIRBUSA319 A319132 3930340NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT PROFILE BETWEEN FR 54 AND FR 55, RBL 711.2. MAINTENANCE CUT OUT DAMAGED SECTION OF PROFILE BETWEEN FR 54 AND FR 55, RBL 711.2; FABRICATED A REPAIR SPLICE AND NEW SECTION OF PROFILE; INSTALLED REPAIR PART IAW AWA ER 26-5320-03154-SS1. 2L72 4F RTA28NM 20030806000352003080600035SO 2003 8 6 C2XA03CL136 120030805A3260CR0105 DIODE EMB 145 EMB145LR 3260212SO MLG WARNING SYS FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2715912 145439 THE CREW REPORTED A AUDIBLE LANDING GEAR WARNING WITH GEAR UP AND FLAPS UP DURING CLIMB AND LEVEL CRUISE. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR DOWNLOCK AURAL WARNING DIODE (CR0105). OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030806000382003080600038SO 2003 8 6 C2XA03CL133 120030804A3350 LIGHT EMB 145 EMB145ER 3260211SO EMERGENCY MALFUNCTIONED A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2716944 145045 THE CREW REPORTED THE EXIT LIGHT BY THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESET POWER. PERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030806000482003080600048SO 2003 8 6 C2XA03SH224 120030717A33977287580501 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT EXPOSED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 DURING C-CHECK, THE NUMBER 4 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A EXPOSED WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806000512003080600051NM 2003 8 6 AWXA200300846 120030727A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 13 LT MISSING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - EEL - DURING INSPECTION MAINTENENACE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT MISSING. INSTALLED A NEW EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030807000402003080700040EA 2003 8 7 COMA0360346 120030731A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01810CA 7370 FLIGHT 5132 LT EXTERIOR EMERGENCY LIGHT IS INOP. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20030807000612003080700061SO 2003 8 7 C2XA03SH262 120030805A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, THE NUMBER ONE EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY CHARGER IAW EMB 145 AMM 3350-50. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030421001232003042100123NM 2003 4 21 UPS03240251 120030304A3230 TORQUE TUBE BOEING727 72730C 1384009NM RT MLG LOOSE A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01919UP 19012 INSPECTION TYPE:N/A ATB-AFTER T/O, LG RAISED AND RIGHT MAIN GEAR STAYED DOWN. RED GEAR LIGHT AND DOORS LIGHT REMAINED ON. GEAR CAME DOWN NORMALLY. REPLACED 6 EA SHEARED RIVETS ON UPLOCK TORQUE TUBE, OPS CHECKS GOOD PER MM 32-30-00. 2L73 4F A3WE 20030421001252003042100125WP 2003 4 21 MWEA030128 120030223A3244 BOLT DOUG DC9 DC981 3022081WP LT MLG WHEEL SHEARED A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31804ME 48030 NR 1 MAIN WHEEL ASSY THROUGH BOLT SHEARED OFF. REPLACED NR 1 WHEEL AND TIRE ASSEMBLY. 2L72 4F A6WE 20030421001372003042100137NM 2003 4 21 VNAA0302021 120030224A3240S4340200001 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BRAKE FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07460PS17697 3061 EN ROUTE, THE CREW RECEIVED A EMERGENCY PARKING BRAKE CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030422000262003042200026 2003 4 22 TSAA0334040 420030305A3414 INDICATOR BOEING737 7372S2C 138448GNM AIRSPEED FAILED A O OTHER J WARNING INDICATION CRCRUISE 1 WP13806AL 21927 FIRST OFFICERS AIRSPEED INDICATOR FAILED IN FLIGHT. THE AIRCRAFT RETURNED HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED FOD FROM THE FIRST OFFICERS PITOT TUBE. THE PITOT/STATIC SYSTEM WAS TESTED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030422000392003042200039EA 2003 4 22 ASOA03073 120030222A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING A GROUND INSPECTION AT MGM, THE NR 3 OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 OVERHEAD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422000422003042200042EA 2003 4 22 ASOA03068 120030219A3350BM1000600 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING A HANGAR INSPECTION IN MCN, THE EXTERIOR EMERGENCY LIGHT AT THE AIRSTAIR DOOR WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY AT THE AIRSTAR DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422001632003042200163 2003 4 22 UPS03840269 420030311A2565 SLIDE DOUG DC8 DC873F 302199FWP CABIN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 LOOK AT ESCAPE SLIDE CONTAINER PARTIALLY OPEN. REPACKED AND RESECURED ESCAPE SLIDE AS REQ, A/C OK TO CONTINUE. 2L74 4F RT4A25 20030423000282003042300028EU 2003 4 23 AUS20030234 120030226A27223545H7 ACTUATOR BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE RUDDER FAULTY W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 AUS (AUS) RUDDER ACTUATOR SUSPECT FAULTY. ACTUATOR ADJUSTMENT/TEST CARRIED OUT IAW AMM 27-21-34 PAGE 501 AND ELECTRICAL CONNECTORS CLEANED.NIL FURTHER FAULTS. 2H74 4F4 F A49EU E6NE 20030423001282003042300128CE 2003 4 23 DXTA200300005 120030309A5610 WINDSHIELD CESSNA750 750 2076810CE ALLSN AE300 AE3007A GL COCKPIT CRACKED E DXTAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07987QS 7500087 DURING FLIGHT AT 31,000 FT THE RIGHT WINDSHIELD CRACKED. 2L72 4J4 FRTT00007WITE6CH 20030423001302003042300130EU 2003 4 23 MALA030194 120030312A242031342001 GENERATOR SAAB SF340 340B 7860101EU AC SYSTEM FAILED A MALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 GL15410XJ 340B410 DURING CLIMBOUT ON FLIGHT 3205, RT AC GEN FAILED IN FLIGHT IN ICING CONDITIONS. AIR RETURN TO MSP. MAINTENANCE FOUND RT AC GEN HAD INTERNAL FAILURE, ALSO TOOK OUT AC GCU. REPLACED GENERATOR P/N 31342-001, SN/OFF 219, SN/ON 1353. IAW TASK CARD 242102, REPLACED RT AC GCU P/N 51634-002, SN/OFF 98012, SN/ON 97016, IAW SAAB AMM 24-21-10. ALL CHECKS GOOD. 2L72 4T RTA52EU 20030423001332003042300133CE 2003 4 23 GLBA2003011 120030120A28201143890425 PUMP BEECH 1900 1900D 1154162CE LP FUEL FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03184UX14233 UE184 RIGHT FUEL LOW PRESS LIGHT ILLUM. REMOVED AND REPLACED LP FUEL PUMP, OPS CHECK GOOD. 2L72 4T RTA24CE 20030423001582003042300158NM 2003 4 23 UPS03M40286 120030215A53131D11047150T615 LONGERON DOUG MD11 MD11F 3023600NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP INSPECTION TYPE: C, CABIN INTERIOR FOUND LONGERON SPICE L-18L BETWEEN STA 5-113 & STA 15 41 WITH CRACK AS MARKED. REMOVED CRACKED LONGERON SPICE L-18 BETWEEN STA 5-113 TO 1541 AS PER SRM 51-33-01 VOL 2 REV 32. NEW STRINGER SPLICE FAB AS PER DWG A5A7112, FAB LONGERON SPLICE, INSTALLED AS PER SRM 51-33-01 VOL 2 REV 32. 2L73 4F RTA22WE 20030423001762003042300176WP 2003 4 23 MWEA030133 120030317A56105912290506 WINDSHIELD DOUG DC9 DC932 3022066WP COCKPIT FAILED A MWEAA UNSCHED LANDING O OTHER CRCRUISE 1 GL31207ME 47794 FIRST OFFICER'S WINDSHIELD SHATTERED AT ALTITUDE (OUTER PANE). REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD. 2L72 4F A6WE 20030423001802003042300180NM 2003 4 23 VNAA0303023 120030317A2434 GENERATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE DC SYSTEM FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07458PS 3068 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE CONTROL THEN HAD OUTSTATION MAINTENANCE CHECK THE LEADS, CLEAN THE CANNON PLUG, AND RESEAT THE DC GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. THE CREW THEN PERFORMED AN AIRCRAFT RUN UP AND THERE WERE NO DEFECTS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030423001812003042300181NM 2003 4 23 VNAA0303016 120030313A5210 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR FAILED A VNAAO OTHER O OTHER CRCRUISE 1 GL07429JS 3043 DURING CRUISE, THE CREW RECEIVED A MAIN CABIN DOOR OPEN INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE DOOR LINK ROD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030423001912003042300191NM 2003 4 23 UPS03240293 120030225A3270 FITTING BOEING727 727108C 1384039NM TAILSKID TRUNN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, DURING REMOVAL OF UPPER AIRSTAIR THREADS IT WAS NOTED THAT THE TAILSKID ACTUATOR FITTING (RT SIDE) WAS CRACKED (TRUNNION FITTING). TAILSKID TRUNNION FITTING REMOVED & REPLACED IAW SRM 51-10-01 & DRG 65-25992. 2L73 4F A3WE 20030423001932003042300193NM 2003 4 23 UPS03240298 120030228A5315 FLOORBEAM BOEING727 727108C 1384039NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 950 LBL 50. REPAIR CARRIED OUT IAW SRM EO 2003-008-022. UPS ENGINEERING FILE 7 27-53-20100. 2L73 4F A3WE 20030423001992003042300199NM 2003 4 23 PCAA0303057 120030317A2120 ODOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE CABIN DETECTED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13839EX203427116 226 121354 LGA-FLIGHT 3920 CREW REPORTED WITH POWER LEVERS AT FLIGHT IDLE BLEED AIR SMELLS OILY AND MAKES EYES BURN. MAINTENANCE CHECKED BOTH OIL LEVELS AND FOUND THEM TO BE PROPERLY SERVICED. AIRCRAFT GROUND RAN WITH BOTH BLEEDS ON FOR 20 MINUTES. OPERATIONAL CHECK WAS GOOD ON THE GROUND. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP ON 18 MARCH 2003, RIGHT ENGINE ASSEMBLY SERIAL NUMBER 121354 WAS REPLACED DUE TO A HISTORY OF ODOR IN BLEED AND OIL CONSUMPTION. 2H72 4T4 TRTA13NM E20NE 20030424000082003042400008SO 2003 4 24 SWIA200311832 120030317A3297 WIRE HARNESS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE MLG DAMAGED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07209SW 120269 AFTER TAKEOFF AND GEAR RETRACTION, RECEIVED GEAR INDICATIONS, LOUD NOISE AND VIBRATION FROM THE NOSE THAT INCREASED WITH AIRSPEED. RETURNED TO LAX. PERFORMED GEAR RETRACTION. FOUND THAT GEAR DOORS WOULD NOT CLOSE DUE TO A FAULTY NOSE GEAR A-HARNESS. REMOVED AND REPLACED LT MLG DOWNLOCK B-HARNESS AND NLG A & B HARNESS. PERFORMED NUMEROUS GEAR RETRACTION AND EXTENSION CYCLES. OPS CHECKED GOOD. 2L72 4T4 TRTA31SO E20NE 20030424000112003042400011EA 2003 4 24 QXEA0300367 120030316A7120 MOUNT CNDAIRCL600 CL6002C10 1390015EA ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX- NR 1 ENGINE MAIN ENGINE MOUNT ON ENGINE HAS AREA OF DAMAGE ON THE TOP SIDE OF THE MAIN ENGINE MOUNT THAT WILL NOT ALLOW THRUST FITTING BEARING TO ENGAGE MOUNT. REPAIRED IAW CRJ SRM 71-20-01 AND 70-42-00. OPERATIOANL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030424000242003042400024WP 2003 4 24 UPS03840317 120030304A551037014272N FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, RT STAB I/B LEADING EDGE ANGLE FITTING IS CRACKED AT XRS 0. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20030424000252003042400025WP 2003 4 24 UPS03840318 120030302A5730 SKIN DOUG DC8 DC873F 302199FWP LEFT WING LE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 766.25 TO XFS 772.5. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20030424000352003042400035WP 2003 4 24 ZW0A0303202 120030317A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13922TW 48013 THE OVERHEAD EMERGENCY LIGHTS AT THE LEFT SIDE NUMBER 2 CABIN DOOR AND JUST BEHIND THE DOOR, AND THE LEFT AND RIGHT EMERGENCY LAMPS IN TAIL AREA, WERE INOPERATIVE. RESEATED THE BATTERIES IN THE BATTERY PACK FOR L2 DOOR LIGHTS, AND REPLACED THE LAMPS P/N 1315 IN THE TAIL AREA. CHECK-C 6-6-02 STL. 2L72 4F A6WE 20030424000372003042400037NM 2003 4 24 QXEA0300339 120030308A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - PANEL 261FT IS LIGHTLY CHAFED THROUGH PAINT ON TRAILING EDGE. REPAIRED IAW RD 8/4-53-457 AND DHC-8 SRM 51-21-10. 2H72 4T RTA13NM 20030424000432003042400043NM 2003 4 24 QXEA0300345 120030305A5240 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - AFT SERVICE DOOR AFT CENTER GUIDE BRACKET IS GOUGED. REPAIRED IAW HORIZON AIR EA 6-52-247. 2H72 4T RTA13NM 20040223000042004022300004CE 2004 2 23 TCM2004F00000 120031208A561066004047 WINDSHIELD LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP COCKPIT DAMAGED E TCMAK NONE O OTHER ININSP/MAINT 1 GL03610JR1780 125 WINDSHIELD FOUND DAMAGED UNDER WINDSHIELD HEAT DIFFUSER SHIELD. HOT BLEED AIR WAS ESCAPING THROUGH A LOOSE DUCT AND PRESSURIZING AREA BETWEEN SHIELD AND AIRCRAFT SKIN. AIR EVENTUALLY FOUND A PATH THROUGH SHIELD GASKET AND SKIN AND BEGAN TO ESCAPE UNDER SHIELD AND ACROSS WINDSHIELD. THIS ALLOWED HOT AIR TO BYPASS TEMPERATURE SENSORS AND BE DIRECTED DIRECTLY ONTO PLASTIC WINDSHIELD. 2L72 4F4 F A10CE E6WE 20040223000342004022300034NM 2004 2 23 AWXA200400019 120031227A5320654583311 WEB BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 DURING C-17 CHECK A 1.1875 INCH CRACK WAS FOUND ON FLIGHT COMPARTMENT FLOOR WEB AT FRAME CUTOUT BS 196, LBL 65, WL 207. MAINTENANCE REMOVED CRACKED WEB AT BS 196, LBL 65, WL 207; FABRICATED A NEW REPLACEMENT WEB IAW DWG 65-45833; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 8. 2L72 4F RTA16WE 20040223000362004022300036EU 2004 2 23 RAIA00312326 120031228A2930 HYDRAULIC SYSTEM JETAIRJETSTMJETSTM4101 1500501EU DISCHARGED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03566HK 41084 5559-STL- HYDRAULIC CONTENTS GAUGE READS .5000 EMPTY. MAINTENANCE SERVICED HYDRAULIC RESERVOIR AND CHECKED FOR LEAKS WITH NONE NOTED. 2L72 4T RTA41NM 20030806000522003080600052NM 2003 8 6 AWXA200300847 120030710A53126545409245 PRESSURE PANEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A .75 INCH CRACK WAS FOUND ON PRESSURE WEB AT BS 664, LBL 34. MAINTENANCE CUT OUT DAMAGE ON PRESSURE WEB AT BS 664, LBL 34; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENER, DOUBLER AND 3 EACH FILLERS PER B737-300 SRM 53-60-51, PG 215, FIG 203 & PG 4, FIG 1; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG 3 & 38. 2L72 4F RTA16WE 20030806000612003080600061NM 2003 8 6 AWXA200300852 120030712A5320654659222 FLOOR SUPPORT BOEING737 7373G7 1384595NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT AND NUT PLATES AT BS 770, RBL 8. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL FROM BS 770 TO BS 774; FABRICATED A NEW SECTION OF CHANNEL AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG 10-11. 2L72 4F RTA16WE 20030731000652003073100065NM 2003 7 31 QXEA200300886 120030725A2434 GENERATOR BOMBDRDHC8 DHC8401 1390041NM NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09412QX 4059 GTF- ON FLIGHT 2323 NR 1 DC GENERATOR FAILED INFLIGHT. RESET PER CHECKLIST WITH NO FURTHER DEFECTS. REMOVED AND REPLACED DC STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000722003073100072NM 2003 7 31 QXEA200300896 120030725A5240 RETAINER BOMBDRDHC8 DHC8401 1390041NM SERVICE DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX- SEAL RETAINER SCREW FORWARD LOWER END OF AFT SERVICE DOOR IS DIMPLED AT SCREW HOLE. REPAIRED IAW HORIZON AIR EA 6-52-302. 2H72 4T RTA13NM 20030731001062003073100106EA 2003 7 31 QXEA200300788 120030630A2150 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT ACTIVATED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09603QX 10011 PDX-ON FLIGHT NUMBER 2553, LEFT HAND PACK CAUTION MESSAGE. PACK SELECTED OFF (CHECKLIST), STATUS MESSAGE LEFT PACK OFF VERIFIED. CAUTION MESSAGE OUT. MDC READS "FLOW CONTROL VALVE MPE11, NO CONTROL/POS DISAGREE" IN FAULT HX. COMPLIED WITH FIM. PERFORMED OPERATIONAL TEST NORMAL WITH NO CURRENT FAULTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731001342003073100134NM 2003 7 31 QXEA200300893 120030725A27423994001011 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM PITCH TRIM MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09403QX5317 5317 4037 PDX- ON FLIGHT 2315 SEA TO EUG, DIVERTED TO PDX DUE TO ON CLIMBOUT OF SEA AT 6,000 FEET ACCELERATING TO 240 KTS, "PITCH TRIM" CAUTION LIGHT ILLUMINATED. NO OTHER CAUTION LIGHTS ILLUMINATED. ELEVATOR TRIM POINTER WENT TO FULL NU AND ELEVATOR TRIM WAS INOPERATIVE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PITCH TRIM ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001372003073100137NM 2003 7 31 QXEA200300890 120030726A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR OUT OF POSITION A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX 4046 ON FLIGHT 2302 RETURNED TO FIELD DUE TO FORWARD BAGGAGE DOOR WARNING ILLUMINATED ON CLIMBOUT OF 19,000 FT. FOUND CARGO DOOR HANDLE NOT FLUSH. CYCLED DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030801000052003080100005WP 2003 8 1 GTIA030523 120030618A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND CABIN FLOOR SUPPORT CORRODED FS 160-190 LBL 7 INCHES. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030801000312003080100031WP 2003 8 1 GTIA030499 120030628A2133 SEAL DOUG DC9 DC981 3022081WP OUTFLOW VALVE LEAKING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23805NK 48058 DTW - FLT 599 - OUTFLOW VALVE SEAL WAS LEAKING HAD TO REMOVE OUTFLOW VALVE AND RESEAL THEN WAIT FOR CURE TIME. ALSO, HAD LATE ARRIVING PARTS. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F A6WE 20030801000492003080100049EU 2003 8 1 2003F00500 120030515A7830 DUCT AIRBUS320 A320233 3930329EU THRUST REVERSER CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER C-DUCT, RIGHT, WITH CORROSION ON UPSIDE. REPAIRED RIGHT THRUST REVERSER IAW ENGINEER REPORT 2078002, REF, CV03-0799. (M) 2L72 4F RTA28NM 20030801001052003080100105EA 2003 8 1 COMA0360331 120030718A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01821CA7078 7420 FLIGHT 5037 GEAR DISAGREE WARNING, NLG DID NOT EXTEND. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20030805000042003080500004WP 2003 8 5 03FDEA00741 120030516A3230 SLEEVE DOUG DC10 DC1010 3022110WP MLG BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 LT MLG TRUCK BEAM OUTBOARD PIVOT BORE SLEEVE IS BROKEN AS VIEWED IN FWD AND AFT OUTBOARD BEAM ASSY. BORES. 05/29/03 A.M.M. 32-12-01-2 - SHOWS WASHER BETWEEN FLANGE BUSHINGS, WASHER AND MATING SURFACE AS BUSHING IS WHAT APPEAR TO BE A CHANK ON BUSHING. NO CRACK CONDITION EXIST. 2L73 4F A22WE 20030805000892003080500089EA 2003 8 5 ASOA03296 120030707A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING A C-CHECK IN MCN, THE AFT PRESSURE BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT PRESSURE BULKHEAD LOWER LEFT AND RT SIDE FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20030805001172003080500117 2003 8 5 BAQA088235 420030729A342240205773 GYRO BOLKMS117 BK117A3 5626015EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911BK295 7099 SLOW TO SLAVE TO HEADING. SPEX FILE ; 128575 REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030806000552003080600055SO 2003 8 6 C2XA03SH216 120030710A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806000732003080600073SO 2003 8 6 C2XA03SH232 120030726A541014576631622 STIFFENER EMB 145 EMB145LR 3260212SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, THE NUMBER 2 LOWER COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040301000482004030100048CE 2004 3 1 CWQ2004F00001 120030513A21206512072101 DUCT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE CRACKED B CWQRK NONE O OTHER ININSP/MAINT 1 GL05373QS 5600373 DURING ROUTINE INSPECTION LOOKED INTO DORSAL NACA SCOOP AND SAW THE LOWER AIR VANE WITH A 1.5 INCH CRACK STARTING FROM THE CENTER OF THE (V) CUT TOWARD THE OB EDGE. GAINED ACCESS FROM THE TAILCONE BAGGAGE AREA AND REMOVED CRACKED VANE. UPON REMOVAL NOTICED THAT THERE WAS NO RELIEF HOLE WAS INSTALLED AT INTERSECTION OF (V) NOTCH WHICH ALSO APPEARS TO HAVE BEEN CUT WITH HAND SNIPS. RECEIVED NEW PART AND INSTALLED WITH A RELIEF HOLE AT (V) INTERSECTION. REINSTALLED ITEMS REMOVED FOR ACCESS AND CLOSED UP BAGGAGE AREA. 2L72 4F4 FRTA22CE E25EA 20040301000542004030100054GL 2004 3 1 HP62004F00000 220030921A7314 SEAL HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL FUEL PUMP LEAKING B HP6RO OTHER K FLUID LOSS NRNOT REPORTED 1 NM01511SB3132 1090592D FUEL PUMP FOUND LEAKING. HAD TO BLEED THE FUEL SYSTEM BEFORE FACT WHEN NO MAINTENANCE HAD BEEN ACCOMPLISHED TO THE FUEL SYSTEM AT THAT POINT IT WAS DISCOVERED THAT THE FUEL PUMP SEAL WAS LEAKING. SUSPECT THAT WAS WHY THE SYSTEM NEEDED TO BE PULLED AFTER HAVING SAT SEVERAL DAYS. REMOVED PUMP. 1G71 3U3 U H3WE E4CE 20040301000612004030100061CE 2004 3 1 800LL082303 120030822A2750 FLAP RAYTHNDH125 HAWKER800 7450004CE WINGS INOPERATIVE E AOQAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 EA11800LL 258079 UPON APPROACH, FLAPS WOULD NOT EXTEND FOR LANDING. SYSTEM WAS INSPECTED AND OPERATION CHECKS WERE ACCOMPLISHED. NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. NO FLAPS LANDING ACCOMPLISHED IAW FLIGHT MANUAL. (EA11200305003) 2L72 4F RTA3EU 20030825000322003082500032WP 2003 8 25 UPS03840967 120030708A3350 BATTERY DOUG DC8 DC873F 302199FWP COCKPIT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT IAW MM 33-50-01. SYSTEM OPS CHECKS GOOD ON GROUND. 2L74 4F RT4A25 20030825000392003082500039WP 2003 8 25 UPS03840887 120030617A5730576957210 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 PRODUCTION SPLICE DOUBLER CRACKED AT XFS 710 ON RH WING LE. REMOVED,FABRICATED AND REPLACED DOUBLER I.A.W. DWG. 5769572,AND SRM. 51-1-21 2L74 4F RT4A25 20030825000402003082500040WP 2003 8 25 UPS03840888 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 RIGHT WING OB. LE. LOWER RIB IS CRACKED AT XFS 728 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030825000792003082500079NM 2003 8 25 EIA2003109 120030808A5711 SPAR BOEING747 747SR46 1384816NM LT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 LT WING STA 1440 EXFOLIATION CORROSION ON THE LOWER CHORD OF THE FWD SPAR, LEADING EDGE CAVITY. REPAIRED LT WING LEADING EDGE LOWER CHORD AT WS 1440 BY REMOVING CORROSION, NDT AREA FABRICATED AND INSTALLED REPAIR PER ECRA 477-57-096-2 REV A. 2L74 4F RTA20WE 20030825001372003082500137SO 2003 8 25 C2XA03CL145 120030811A323122250100003 SOLENOID VALVE EMB 145 EMB145 3260210SO NLG DOOR FAULTY A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2741104 145646 IAH FLIGHT NR 7631, THE CREW REPORTED THE NOSE GEAR DOOR WAS STUCK OPEN AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030825001572003082500157NM 2003 8 25 AMTA200300987 120030801A3350D71702001 POWER SUPPLY BOEING737 73783N 13844HINM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11313TZ 32580 RIGHT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE, ALSO EXTERIOR EMERGENCY LIGHT FORWARD OF LIGHT POWER SUPPLY AS PER AMM 33-51-06. (M) 2L72 4F RTA16WE 20030825001712003082500171WP 2003 8 25 DHL2003873564 120030702A5347S4889036 SEAT TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 ITEM REF.: N/R 0827.: MAIN CARGO COMPT. NR 6 TRACK LUG WORN STA.1470.000-STA.1590.000. REMOVED DAMAGED TRACK IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW TRACK IAW SRM 51-3-0 PG.1. 2L74 4F4 FRT4A25 E2GL 20030826000032003082600003NM 2003 8 26 03FDEA01382 120030807A5744ARC0503503 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING OUTBOARD FLAP OUTBOARD HINGE BRACKET (WING SIDE) LOWER OUTBOARD HOLE FOUND CORROSION. LT WING OUTBD FLAP OUTBD HINGE BRACKET (WING SIDE) LOWER OUTBD HOLE REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-71796, WINGS- LT AND RT OUTBOARD FLAP- OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030826000132003082600013NM 2003 8 26 03FDEA1361 120030822A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 SIX PREVIOUSLY PLUGGED HOLES IN SKIN AT BS 400 BETWEEN STR 14 - 15 LT ADJACENT TO EXISTING FASTENERS. 2L73 4F RTA3WE 20030826000612003082600061CE 2003 8 26 5300040403 120030404A216099125182 CONTROL VALVE CESSNA560 560XL 2076702CE CABIN TEMP FAILED E S4WAK NONE O OTHER CRCRUISE 1 WP07613GY241 5605300 NO CONTROL OF CABIN TEMPERATURE AVAILABLE. 2L72 4F RTA22CE 20030826000752003082600075NM 2003 8 26 CALA0300471 120030814A5512 SKIN BOEING737 7373T0 1384582NM HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 MAINTENANCE FOUND A SMALL CRACK IN THE LT HORIZONTAL STABILIZER LOWER SKIN JUST FORWARD OF THE REAR SPAR FORWARD FLANGE, STAB STA 152. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5510-01692. A DIP WAS ISSUED TO PERFORM A DETAILED VISUAL INSPECTION OF THE INTERIM REPAIR AT INTERVALS NOT TO EXCEED 3,000 FLIGHT HOURS AND TO PERFORM A PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 15,000 FLIGHT HOURS. 2L72 4F RTA16WE 20030826000932003082600093NM 2003 8 26 C8GA20030017 120030603A275118157014 TRANSMITTER BOEING727 727223 1384074NM T/E FLAP DEFECTIVE A C8GAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO15899AA 22015 FLT 001 FROM MIA TO PTO. ON ROTATION, STICK SHAKER ACTIVATED. UNABLE TO STOP STICK SHAKER IN FLIGHT, FUEL WAS DUMP AND THE FLIGHT RETURNED TO MIA. AIRCRAFT LANDED IN MIA WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE LEFT HAND INBOARD FLAP POSITION TRANSMITTER WAS REPLACED. GROUND OPERATIONAL CHECKS NORMAL IN ALL SETTINGS IAW MM 27-52-1. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030806000842003080600084NM 2003 8 6 03207451 120030726A33508GH00247308 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27451FJ 3205 DURING MAINTENANCE INSPECTION 2 CEILING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CEILING EMERGENCY LAMPS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030806000892003080600089SO 2003 8 6 C2XA03TY107 120030801A534714530659003 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION, SEAT TRACK LF3 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030806000932003080600093SO 2003 8 6 C2XA03TY109 120030801A534714530659001 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION, SEAT TRACK LF2 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030806000952003080600095SO 2003 8 6 C2XA03TY090 120030718A552414537536002 FITTING EMB 145 EMB145 3260210SO ELEVATOR LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 A/C 962 WAS FERRIED TO TYS AFTER A PRELIMIARY INSPECTION FOUND A/C SATISFACTORY FOR A FERRY FLIGHT. MAINTENANCE REMOVED AND REPLACED THE RT ELEVATOR TRAILING EDGE FITTING; CUT OUT THE DAMAGED AREA AND FAB A DOUBLER, FILLER AND INSTALLED; ALODINED PRIMED AND PAINTED REPAIR DOUBLER AND FILLER IAW IC2003-145/2448 AND 51-40-02, AS WELL AS 135/145 CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. PERFORMED A LIGHTNING STRIKE INSPECTION, ALL SERVICEABLE. 2L72 4F RTT00011AT 20030806000992003080600099SO 2003 8 6 C2XA03TY113 120030801A534714532606017 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK LF6 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030806001012003080600101SO 2003 8 6 C2XA03CL120 120030707A33507137215501 SIGN EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936 145025 CLE FLIGHT 2327, THE CREW REPORTED THE EMERGENCY LIGHTS ABOVE 3B WOULD NOT COME ON. MAINTENANCE REPLACED THE EMERGENCY EXIT LOCATOR SIGN. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030806001072003080600107SO 2003 8 6 C2XA03SH260 120030804A531014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE CENTER BUTTSTRAP AT FRAME 19 WAS FOUND TO BE CORRODED AND BENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001102003080600110SO 2003 8 6 C2XA03TY116 120030801A534714532606017 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION, SEAT TRACK LW6 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030806001142003080600114SO 2003 8 6 C2XA03SH258 120030803A531514530633003 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 FROM FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001192003080600119SO 2003 8 6 C2XA03SH255 120030803A5311145337302 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001242003080600124SO 2003 8 6 C2XA03SH257 120030803A531514523186001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE LT FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001452003080600145NM 2003 8 6 AWXA200300853 120030722A5320694147315 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK 1 INCH CRACK WAS FOUND ON INTERCOSTAL BETWEEN BS 400 AND BS 420, STR 26 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL BETWEEN BS 400 AND BS 420; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-41473; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3, AND SRM 51-40-04 PG 6, FIG 2. 2L72 4F RTA16WE 20030806001482003080600148SO 2003 8 6 C2XA03SH210 120030701A531014522460013 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE CENTER BUTTSTRAP BETWEEN FRAMES 16 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030806001512003080600151SO 2003 8 6 C2XA03SH209 120030701A531014521699003 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE LT HAND BUTTSTRAP BETWEEN FRAMES 16 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030806001612003080600161SO 2003 8 6 C2XA03SH229 120030718A532014522459001 ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 145477 DURING C-CHECK, THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040223000542004022300054NM 2004 2 23 2003UALA00986 120031226A3350 LENS AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT MISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP29844UA 1581 FIRST CLASS CLOSET EEL LIGHT IS MISSING LENS ASSY. REPLACED LIGHT ASSY. 2L72 4F4 FRTA28NM E40NE 20040223000632004022300063NM 2004 2 23 DHL200374258 120031125A575465172769 RIB BOEING727 727225 1384077NM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING "C" CHECK, NR 4 SLAT HAS SEVERAL CRACKS IN RIB IB SIDE OF THE ACTUATOR, VIEWED THRU THE ACCESS HOLE. CA: REMOVED DAMAGED RIB AND INSTALLED NEW, PN 65-17276-9 PO NR 3348104 IAW 727 SRM 51-30-2, REMOVED AND REPLACED THE NR 4 SLAT FOR STRUCTURAL ACCESS IAW B727 MM 27-81-11. 2L73 4F A3WE 20040223000652004022300065WP 2004 2 23 UPS04841687 120031230A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, RT WING LE UPPER RIB IS CRACKED AT XFS 316.5 STOP DRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20040223000822004022300082WP 2004 2 23 54284 220031229A7230310166812 PLENUM SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE3311U 01514WP ENGINE CRACKED B EATAK NONE O OTHER ININSP/MAINT 1 GL2526932 1283 AC660 P44531 PLENUM CRACKED AT IGNITER BOSS WELD. 2L72 4T3 TRTA8SW E3WE 20040223001062004022300106NM 2004 2 23 2004F00010 120031031A5753654792328 SPAR BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE RT WING TE FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 NM01379SW 1903 26586 CRACKED AT OB AFT FLAP TRACK ATTACH HOLES. 2L72 4F4 FRTA16WE E2GL 20040223001412004022300141NM 2004 2 23 2003UALA00863 120031114A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMPENNAGE DAMAGED A UALAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 WP29178UA57335 24385 TAIL STRIKE ON TAKEOFF. AT BEGINNING OF FLIGHT, AT LIFTOFF, EMPENNAGE WAS SCRAPPED ON RUNWAY BETWEEN STATIONS 2635-2734. APU BATT ACCESS DOOR AND APU CLAMSHELL DOORS WERE REPLACED. ALL OTHER FRAME/SKIN DAMAGE BETWEEN NOTED STATIONS REPAIRED. AREA STRUCTURAL INSPECTIONS ACCOMPLISHED WITH NO FURTHER FINDINGS. 2L74 4F4 FRTA20WE E24NE 20040223000522004022300052NM 2004 2 23 2003UALA00984 120031229A5310 TORQUE BOX BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO BAY CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29180UA 25224 FWD CARGO PIT AFT TORQUE BOX CRACKED AT CENTER LINE GUIDE STA. 860. INSTALLED WEB SECTION AND ACCOMPLISHED SPLICE REPAIR. 2L74 4F4 FRTA20WE E24NE 20040223000672004022300067WP 2004 2 23 UPS04841689 120031229A5730576960035 DOUBLER DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. 5769600 AND SRM. 51-1-21,51-1-20D,57-3-0 FIG. 2D. 2L74 4F RT4A25 20040223001482004022300148CE 2004 2 23 TZR2004F00000 120031223A8120 BEARING CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C* GL TURBOCHARGER FAILED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05408TE81 BI048213 4010269 290804R 842170 AFTER INSTALLATION OF RT ENGINE, WHILE PERFORMING ENGINE FUEL SET-UP AND ADJUSTMENT OF MANIFOLD PRESSURE, THERE WAS A DECREASE IN MANIFOLD PRESSURE AND A NOTICEABLE NOISE AND VIBRATION FROM THE RT ENGINE. UPON FURTHER INVESTIGATION IT WAS NOTED THAT THE TURBOCHARGER MAIN BEARING SEAL HAD FAILED CAUSING BEARING FAILURE. 1L72 3O3 O A7CE E8CE 5 CP22EA 20040223001732004022300173WP 2004 2 23 ABXA040019 120031223A5310995773911 SHEAR TIE DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 SHEARTIE CRACKED AT FS 947, BETWEEN LONGERON 15 LT AND 16 LT. REMOVED AND REPLACED SHEAR TIE IAW SRM. 2L72 4F A6WE 20040223001742004022300174WP 2004 2 23 ABXA040016 120031222A5314392409291 KEELBEAM DOUG DC9 DC932 3022066WP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 KEELBEAM LONGERON 30 END CAP WAS CRACKED, LT SIDE FS 604. REPLACED KEELBEAM END CAP IAW DC-9 SRM. 2L72 4F A6WE 20040223001872004022300187WP 2004 2 23 ABXA040026 120031230A5320D0489837 WEB DOUG DC9 DC933F 302207AWP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 CUSP WEB CRACKED AT FS 310 ABOVE LONGERON 20 LT. REPAIRED AREA IAW SRM 53-01. 2L72 4F A6WE 20040223001882004022300188WP 2004 2 23 ABXA040024 120031226A2740591096233 JACKSCREW DOUG DC9 DC933F 302207AWP HORIZONTAL STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 JACKSCREW THREADS HAD AREAS WHICH WERE PITTED. REMOVED AND REPLACED HORIZONTAL JACKSCREW IAW DC-9 MM 27-40-01. 2L72 4F A6WE 20040223001642004022300164CE 2004 2 23 S492004F00001 120031213A275051155382 BRACKET CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO FLAP BELLCRANK BROKEN E S49AO OTHER J WARNING INDICATION APAPPROACH 1 SW13442BK9284 402C0332 PIC ON APPROACH TO LAND, EXTENDED 10 DEGREES OF FLAPS. AIRCRAFT IMMEDIATELY ROLLED RT APPROXIMATELY 30 DEGREES. PILOT RETRACTED FLAPS AND LANDED WITHOUT INCIDENT WITH NO FLAPS EXTENDED. POST FLIGHT INSPECTION REVEALED RT FLAP BELLCRANK BRACKET BROKEN. 1L72 3O3 O A7CE E8CE 20030807000112003080700011NM 2003 8 7 UIEA200300039 120030624A2810 SKIN BOEING747 7472D3B 1384805NM CENTER TANK CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15506MC 21252 DURING C-CHECK, CENTER TANK UPPER SKIN FOUND CORRODED AT BS 1060, RBL 106-122 UNDER FLOORBEAM LOWER CHORD. PERMANENT REPAIR PER REF, CORROSION WAS REMOVED BY BLENDING. BLENDED AREA WAS SHOP PEENED, REFINISHED AND BMS 5-95 SEALANT WAS USED TO FILL THE BLENDED AREA TO PREVENT MOISTURE ACCUMULATION. NO REINFORCEMENT WAS REQUIRED. (M) 2L74 4F RTA20WE 20030807000132003080700013NM 2003 8 7 USAA030114 120030615A5314 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 FOUND LT KEEL BEAM WITH EXFOLIATION CORROSION 3 INCHES LONG BY 1 INCH WIDE, FS 500 C PLUS 18 INCHES. CORROSION LEVEL 2, TASK NR C53-208-01. INSTALLED KIT NR 65C28106-1 AND 65C28106-16 PER EO 5302V112 REV A. (M) 2L72 4F RTA16WE 20030807000152003080700015NM 2003 8 7 USAA030122 120030617A5312 PRESSURE PANEL BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 FOUND TWO CRACKS IN WEB 1 INCH EACH, PRESSURE WEB AT STATION 665 RBL 40. DOUBLERS AND FILLERS INSTALLED AT CUTOUT OF WEB PER TYP REP 53-60-04. (M) 2L72 4F RTA16WE 20030805000612003080500061EA 2003 8 5 ASOA03274 120030623A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 FLT 4340 - DURING GROUND INSPECTION IN ATL, THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT LAMP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030806000632003080600063SO 2003 8 6 C2XA03SH230 120030726A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE T-REINFORCEMENT ON STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001292003080600129NM 2003 8 6 AWXA200300828 120030714A531369353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500C, STR 27 LT. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 500C, STR 27 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3-4, FIG 8. 2L72 4F RTA16WE 20030807000022003080700002EA 2003 8 7 ASOA03295 120030706A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING A C-CHECK IN MCN, THE RIGHT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT FRAME FS 718 BETWEEN STRINGERS 10 TO 11 IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20030807000182003080700018NM 2003 8 7 UIEA200300035 120030603A531265B17004 BULKHEAD BOEING747 7472D3B 1384805NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15506MC 21252 DURING C-CHECK, FOUND CRACKS AT LT AND RT SIDES OF STATION 140, FORWARD PRESSURE BULKHEAD WEB, WL 205-227 AND WL 250-258. THE REPAIR TRIMS OUT THE CRACKS, HFEC INSPECTS THE TRIM. INSTALLED REPAIR DOUBLERS ON THE AFT SIDE PER REF AND MOD DOUBLERS ON THE FORWARD SIDE PER REF. FASTENER HOLES ARE HFEC INSPECTED. (M) 2L74 4F RTA20WE 20030807000292003080700029NM 2003 8 7 USAABB03112 120030716A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU 22198 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030807000432003080700043NM 2003 8 7 C1HA200393011 120030708A3350900835A BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15293AS 21348 AFT SECTION OF FLOOR TRACK EMERGENCY ESCAPE LIGHTING INOP. 2L73 4F A3WE 20030807000532003080700053EU 2003 8 7 03212324 120030731A3397DBP213 CONNECTOR BAG JETSTMJETSTM4112 EU EMERGENCY LIGHT BROKEN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27324UE 41017 DURING MAINTENANCE INSPECTION THE CONNECTOR ON THE MIDDLE EMERGENCY TRACK LIGHTING SECTION WAS FOUND BROKEN. 1L72 4T RTA196 20030807000572003080700057SO 2003 8 7 C2XA03SH261 120030805A335066364 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, THE NUMBER ONE EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030807000642003080700064EA 2003 8 7 03216689 120030804A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27689BR 7737 DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULBS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030807000782003080700078EU 2003 8 7 03207309 120030726A33506047051 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27309UE 41022 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY TRACK LIGHTING FORWARD OF ROW 3A INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK AND REPAIRED TRACK LIGHTING WIRING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030807000852003080700085EU 2003 8 7 03217324 120030805A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27324UE 41017 DURING MAINTENANCE INSPECTION THE AFT SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL RESECURED THE CONNECTOR ON THE AFT SECTION OF EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030826001242003082600124WP 2003 8 26 03FDEA00985 120030627A5320 CLIP DOUG DC10 DC1030 3023501WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 N 1137 AFT FUSELAGE ZONE 312. FS 2140 AFT CANT BULKHEAD TOP FUSELAGE FRAME CLIP ANGLE SKIN ATTACHMENT SUPPORT HAS 2 INCH CRACK ON LT SIDE. REMOVED FRAME CLIP IAW SRM 51-35-01. FAB NEW CLIP ON MAE TRAVLER T2/343533. INSTALLED NEW CLIP IAW SRM 51-35-01 AND 51-33-01. 2L73 4F A22WE 20030826001342003082600134SO 2003 8 26 SIMA200321601 120030729A7830 WARNING SYSTEM EMB 145 EMB145LR 3260212SO COCKPIT ACTIVATED A SIMAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SW21645AE 145212 ORD - FLT 4202 - DURING APPROACH CREW REPORTED AN E1 REV FAIL INDICATION FOLLOWED BY ENGINE ONE STARTING TO SPOOL UP AND DOWN. CREW COMPLIED WITH AOM PROCEDURES AND SHUT DOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY IN ORD WITH NO OTHER INCIDENTS NOTED. (M) 2L72 4T RTT00011AT 20030826001372003082600137EA 2003 8 26 ASOA03264 120030618A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11835AS 7258 FLT 4681 - DURING A GROUND INSPECTION IN ATL, THE RIGHT SIDE FLOOR EMERENCY LIGHT STRIPS FROM THE SERVICE DOOR TO ROW EIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE FLOOR EMERGENCY LIGHT STRIPS FROM THE SERVICE DOOR TO ROW EIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030826001632003082600163WP 2003 8 26 MEX20030321 120030703A7830 THRUST REVERSER DOUG DC9 DC987 3022087WP RT ENGINE MALFUNCTIONED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW231075T 49724 FLT 605 - DFW-MEX - AIRCRAFT RETURN TO PLATFORM, DURING TAXI THE RIGHT ENGINE REVERSE UNLOCKED INDICATOR LIGH TON. DURING REVISION THE LIGHT WAS OFF AND REVERSE WAS OPERATED THREE TIMES, ALL CORRECT. THE REVERSE WAS DEFERRED UNDER MEL 78-1. AT MEX, SWITCH REVERSE LATCH WAS CLEANED AND CHECKED IAW MM 78-32-03 AND 78-30-06 RESPECTIVELY, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030827000782003082700078SO 2003 8 27 C2XA03SH250 120030803A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV-DURING C CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030827000792003082700079SO 2003 8 27 C2XA03CL119 120030706A335078241 INVERTER EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2715941 145035 CLE FLIGHT NR 2243, THE CREW REPORTED THE EMERGENCY LIGHTS ABOVE THE GALLEY AREA AND COCKPIT ENTRANCE DID NOT WORK. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030827000812003082700081SO 2003 8 27 C2XA03BT078 120030808A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO NLG FAULTY A C2XAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW2716987 145261 EWR---CO2320, CREW REPORTED, (AIR/GROUND SENSOR FAILED. LANDING GEAR WOULD NOT RETRACT.) RETURNED TO EWR, MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH (WOW) IAW EMB145 MM NR 32-63-02. OPS. CHECKED AND GEAR SWING GOOD. IAW EMB145 MM NR 32-30-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030827000822003082700082SO 2003 8 27 C2XA03BT069 120030708A335078241 INVERTER EMB 145 EMB145 3260210SO ALLSN AE3007AE3007C GL CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713965 145125 BTV---CO2316, DURING SERVICE/ROUTINE CHECK FOUND EMERGENCY LIGHT AISLE PATH LIGHTING FROM SEAT ROW 11 THROUGH 19 INOPERATIVE. REMOVED AND REPLACED AC/DC INVERTER IAW AMM NR 33-50-11. OPS. CHECKED LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030827000842003082700084SO 2003 8 27 C2XA03IA075 120030803A2120 SMOKE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN DETECTED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2721129 145703 IAH- FLIGHT 2719, THE CREW NOTED SMOKE IN THE CABIN DURING CLIMB, DID AN AIR RETURN, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE INSPECTED THE AIRCRAFT, AND, PERFORMED A OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030827000872003082700087SO 2003 8 27 C2XA03SH226 120030717A33977287580503 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 SHV-DURING C CHECK THE NUMBER 6 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030827001012003082700101NM 2003 8 27 CALA0300397 120030719A5320 SUPPORT BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND RT AFT LAV WALL SUPPORT HAT SECTION CORRODED. THE WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-00. 2L72 4F4 FRTA16WE E2GL 20030827001532003082700153NM 2003 8 27 2003UALA00567 120030716A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29663UA 27160 MAIN CABIN SEATTRACK AT STA 654+14 RBL 89 IS CORRODED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION WITH SPLICE DOUBLERS. 2L72 4F4 FRTA1NM E24NE 20030827001772003082700177 2003 8 27 C2XA03CL140 420030807A31407013348940 DAU EMB 135 EMB135ER 3260203SO NR 1 FAULTY A C2XAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW2719503 145176 CLE FLIGHT NR 2802 THE CREW REPORTED THE NR 1 ENGINE SHOWED NO FUEL FLOW WHILE ENGINE NR 1 WAS RUNNING. MAINTENANCE INSPECTED AND REPLACED THE NR 1 DAU. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030826000022003082600002NM 2003 8 26 03FDEA01381 120030808A5753ARC70561 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING OUTBOARD FLAP VANE NR 4 FITTING FWD HOLE FOUND CORROSION. LT WING OUTBD FLAP VANE NR 4 FITTING FWD HOLE CARRIED OUT REPAIR AS PER EA 1-5750-71794 (WINGS - RT AND LT OUTBOARD FLAP - NR 4 FITTING SUPPORT VANE TO TRACK CORROSION). 2L73 4F RTA22WE 20030826000902003082600090EU 2003 8 26 YENA200320 120030807A3250 SENSOR AIRBUS320 A320232 3930326EU NLG STEERING MALFUNCTIONED A YENAK NONE J WARNING INDICATION CLCLIMB 1 EA15561JB 1927 NOSE WHEEL STEERING FAULT AFTER GEAR RETRACTION. RESET BOTH FEED BACK SENSORS AT NOSE WHEEL STEERING. PERFORMED OPERATIONS CHECK IAW MM 32-51-00-710-001. NO FAULT NOTICED DURING OPS CHECK OF SYSTEM. WORKING NORMAL. 2L72 4F RTA28NM 20030807000902003080700090CE 2003 8 7 GLBA2003113 120030803A3260H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03211GL UE211 GEAR INTRANSIT LIGHT DID NOT EXTINGUISH. REMOVED AND REPLACED RT MLG UPLOCK SWITCH. 2L72 4T RTA24CE 20030807000942003080700094NE 2003 8 7 EIA2003093 220030710A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 1 STALLED A EIAAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 NM09486EV 20888 685635 AT CRUISE ALTITUDE FL 320 NOTICED NR 1 ENG EPR DROP TO .25 LOWER THAN THE OTHERS. ALL OTHER READINGS AND INDICATIONS WERE NORMAL. WHEN ADJUSTING THRUST LEVER, ENGINE COMPRESSOR STALLED MULTIPLE TIMES, SHUT DOWN ENGINE. AFTER SHUTDOWN OIL PRESS 29 PSI, N1 29.9 AND N2 27.8. STATUS OF THIS SDR IS OPEN UNTIL COMPLETION OF INVESTIGATION. 2L74 4F4 F A20WE E20EA 20030807000952003080700095CE 2003 8 7 GLBA2003102 120030707A3230 RELAY BEECH 1900 1900D 1154162CE MLG FAILED A GLBAO OTHER O OTHER APAPPROACH 1 NM03169GL UE169 LANDING GEAR HAD TO BE MANUALLY EXTENDED. REPLACED K3 RELAY, OPS CHECK GOOD. 2L72 4T RTA24CE 20030807000982003080700098NM 2003 8 7 EIA2003095 120030724A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 UPPER DECK FLOORBEAM HAS MISSING FASTENERS AND WEB IS TORN AND GOUGED AT BS 440 RBL 32. FABRICATED REPAIR PER ECRA 485-53-145-2. 2L74 4F A20WE 20030807001052003080700105NM 2003 8 7 EIA2003102 120030725A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 FRAME CRACKED, INTERIOR FUSELAGE STA 300L, BELOW S-25L, OUTBOARD NEAR SKIN. REMOVED AND REPLACED FUSELAGE FRAME AT FS 300L, STR 23-41, PER SB 747-53-2272, PER -B-DRAWINGS 141U1021 AND 65B1708 & ECRA 485-53-152-2. 2L74 4F A20WE 20030807001062003080700106NM 2003 8 7 EIA2003103 120030725A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE BULGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 BODY STATION 780 IN AREA OF STRINGER 46R, SKIN BULGE. REPAIR WORK ACCOMPLISHED ON ECRA 485-53-143-2 & ECRA 485-53-160-2. 2L74 4F A20WE 20030807001112003080700111 2003 8 7 HNAA0300035 420030722A3400101741011 CONTROL UNIT DHAV DHC8 DHC8201 2809001NM COCKPIT DEFECTIVE A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA07985HA19779186 479 WHILE IN RANGE, UNS FAILED AND WAS FOLLWED BY SMOKE ALL AROUND UNIT. THE UNIT RE-ILLUMINATED AND WOULD NOT RESPOND TO OFF SWITCH. F/D FAILED, NAV AND A/P IND LIGHTS FLASHED ALONG WITH RADAR. CAPTAINS ADI BECAME ERRONEOUS. REMOVED UNS UNIT TO INSPECT FOR POSSIBLE ELECTRICAL FIRE OR SMOKE DAMAGE. CONFIRMED UNS-1C UNIT IS BAD, PERFORMED OPERATIONAL CHECKS OF OTHER SYSTEMS. 2H72 4T RTA13NM 20030812000092003081200009NE 2003 8 12 HEEA088409 120030712A31507655001001103 PANEL SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 COCKPIT CAUTION PANEL LAMPS WILL NOT LIGHT UP WHEN FAULTS OCCUR. SHOP REPAIR. 1G72 3U H1NE 20030812000122003081200012GL 2003 8 12 HEEA088416 220030724A74219550175400 IGNITER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X 760050 IGNITER INSULATOR CRACKED. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U3 U H1NE E1GL 20030812000142003081200014NE 2003 8 12 HEEA088425 120030724A2110ES611001 MOTOR SKRSKYS76 S76A 8143006NE COMPRESSOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ1919 760231 AIR CONDITIONER DOES NOT COOL. REPLACED COMPRESSOR MOTOR WITH A SERVICEABLE MOTOR - BRUSHES BURNED. 1G72 3U H1NE 20030812000152003081200015NE 2003 8 12 HEEA088426 120030730A32977655202010105 WIRE HARNESS SKRSKYS76 S76A 8143006NE MLG DOOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X 760050 GEAR DOOR EXPLOSIVE LINK CABLE ASSEMBLY BROKEN. SCRAPPED. 1G72 3U H1NE 20030812000252003081200025SW 2003 8 12 HEEA088446 120030723A6410206011809109 PITCH HORN CLARK 1000 1000CLARK 2230102SW T/R ASSY CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03266P 707 52271 FRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE. 1Q71 3R 2A6 20030812000402003081200040EU 2003 8 12 BAQA088209 120030728A7714L771M10C1002 INDICATOR UROCOPEC135 EC135P1 8680990EU ENGINE N1 INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME2651 0009 ENGINE N1 INDICATOR HAS INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030829000722003082900072EA 2003 8 29 MAS2003F00000 120030305A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WINGS MALFUNCTIONED A MASAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 SW0727314 7314 FLT 6231. GDL-PHX. MECH CONTROL NR 189906. PIC DECLARED AN EMERGENCY FOR LANDING. FLAP FAIL AT 30 DEGREES. CW FLAPS FAIL MAINTENANCE PROCEDURE PART A (MTC-27-50-001). FLAPS RESET OK. PART B (MTC 27-50-002) DUE NLT 1100MST 03/08/03. 03/07/03. MECHANIC PERFORMED BART B. NO DEFECTS NOTED. (SW07200303663) 2L72 4F4 FRTA21EA E15NE 20030829001022003082900102 2003 8 29 3144031403 420030314A3416150201182 LIGHT SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE ALTIMETER INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP075226R1897 3144 22090 ALTIMETER LIGHTING INOP. 1G71 3U3 U H9EU E00054EN 20040224000712004022400071WP 2004 2 24 GKZR200479901 120031102A54145753014501 PANEL DOUG DC8 DC862 3021970WP NR 4 PYLON CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 NR 4 INBOARD PYLON PLANK CRACKED ABOUT 30 SCREWS AFT FROM L/E BOTTOM ROW. REMOVED NR 4 ENGINE PYLON I/B PLANK PANEL FOR REPAIRS, FABRICATED REPAIR IAW DC-8 SRM 54-2-2, INSTALLED REPAIR IAW DC-8 SRM 54-2-2. REINSTALLED NR 4 ENGINE PYLON PLANK IAW DC-8 SRM 54-2-2. 2L74 4F 4A25 20040224000732004022400073WP 2004 2 24 GKZR200479903 120031211A53135750198501 LONGERON DOUG DC8 DC862 3021970WP FUSELAGE CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 LEFT L24 HAS ABOUT 1.25 INCH CRACK AFT OF THE FWD MAIN ATTACH BOLT. REMOVED AND REPLACED LT L24 AT STA 903 TO 960 IAW DC8 SRM 51-1-21 & 51-3-0. TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8. TORQUED FWD MAIN ATTACH BOLT IAW DRW 5750553. 2L74 4F 4A25 20040224000862004022400086WP 2004 2 24 GKZR200479908 120031115A5330 FINGER DOUBLER DOUG DC8 DC862 3021970WP FUSELAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 RIGHT AFT FUSELAGE BETWEEN STA 1540 & 1551 FROM L22R TO L25R PREVIOUS REPAIR HAS 2 RIVETS BLOWN OUT & CORROSION. REMOVED & FABRICATED DOUBLER & FINGER DOUBLER IAW DC8 SRM 53-02-01. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER & FINGER DOUBLER IAW DC8 SRM 53-02-01. 2L74 4F 4A25 20040224000272004022400027EA 2004 2 24 A6WA200340205 120031222A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM INOPERATIVE A A6WAO OTHER J WARNING INDICATION CLCLIMB 1 GL31406AW10923 7402 AFTER TAKEOFF GOT (GEAR DISAGREE) WARNING LIGHT, COMPLIED WITH QRH ALSO HAD STEERING INOP CAUTION MESSAGE. MESSAGE RESET. REPLACED HYDRAULIC PUMP 3A, GEAR SWINGS CHECKED GOOD. (M) 2L72 4F RTA21EA 20040225001292004022500129WP 2004 2 25 AAL2004F00000 120030929A5347 SEAT TRACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21484AA 49677 CORROSION ON NR 1 SEAT TRACK AT STA 1278. INSTALLED PLUG AT STA 1278, NR 1 SEAT TRACK IAW SRM AND TREATED AND PRIMED. 2L72 4F4 F A6WE E2EA 20040225001552004022500155NM 2004 2 25 DL73S031123 120031222A53306545866688 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 CRACK DAMAGE WAS NOTED ON THE KEEL BEAM LOWER SKIN PANEL. SKIN PANEL WAS REPLACED PER ERA 385927-14. 2L72 4F RTA16WE 20040225001592004022500159NM 2004 2 25 DL73S031127 120031223A5311654654925 FRAME BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 A DENT WAS FOUND IN THE INNER CHORD OF THE BS 767 FRAME JUST ABOVE S24L. DENT WAS REMOVED AND REPAIRED PER ERA 385960-14. 2L72 4F RTA16WE 20040225001672004022500167NM 2004 2 25 DLM88031135 120031225A3350RPS1S CHARGER DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27910DL 49541 EMERGENCY LIGHTS INOP IN AFT CABIN. REPLACED POWER SUPPLY, BATTERY AND LIGHT ASSY L2-845. EMERGENCY LIGHTS SELF TEST GOOD. 2L72 4F RTA6WE 20040225001682004022500168NM 2004 2 25 DL75K031136 120031225A3397BACS53B1EA1 GROUND STUD BOEING757 757232 1384965NM EMERGENCY LIGHT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27685DA 27588 GROUND STUD GD00510 LOOSE RENDERING EMERGENCY LIGHT POWER SUPPLY M732 INOPERATIVE. REPLACED GC00510 PER WSPM 20-20-10. 2L72 4F RTA2NM 20040223001492004022300149CE 2004 2 23 XGN2004F00000 120031212A143050452013 BOLT CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO NOSE FORK BROKEN E XGNAO OTHER O OTHER NRNOT REPORTED 1 SW053378Q16174 402B0334 THE NOSE GEAR WOULD NOT RETRACT AFTER DEPARTURE. AIRCRAFT LANDED WITHOUT PROBLEMS. FOUND THE NOSE GEAR RETRACT FORK BOLT BROKEN. THE BOLT SEPARATED AT THE LAST THREAD BEFORE WHERE THE SHANK STARTS. THE BELLCRANK THAT THE BOLT SCREWS INTO WAS ALSO DAMAGED AND WAS REPLACED AT THE SAME TIME. (PN 0842104-3) SUGGEST THESE BOLTS BE REMOVED AND INSPECTED WITH NDT INSPECTION PROCEDURE. PROBABLE CAUSE, METAL FATIGUE. (SW05200403502) 1L72 3O3 O A7CE E8CE 20040223001602004022300160WP 2004 2 23 EAT2004F00000 220031231A7230310166812 PLENUM SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE3311U 01514WP IGNITER AREA CRACKED B EATRO OTHER O OTHER NRNOT REPORTED 1 GL0926932 1283 AC660 A CRACK IN THE PLENUM NEAR THE IGNITER BOSS. THE CRACK WAS RIGHT ALONG THE WELD AROUND THE IGNITER BOSS. MOST LIKELY THE IGNITER WAS AT SOME POINT MAY HAVE BEEN OVERTORQUED CAUSING STRESS TO THE PLENUM. 2L72 4T3 TRTA8SW E3WE 20040225001662004022500166NM 2004 2 25 DLM88031134 120031225A7500759702325 DUCT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27984DL 53311 718127 NR 1 ENGINE, INBOARD SIDE 8TH STAGE ENGINE ANTI ICE DUCT IS BROKEN. REPLACED DUCT. 2L72 4F4 FRTA6WE E9NE 20040225001742004022500174NM 2004 2 25 DL76K031143 120031228A2121211002939 FAN BOEING767 767332 1382001NM RIGHT ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27173DZ 29692 DISTINCT HOT ODOR OCCURRED 3 SEPARATE TIMES DURING FLIGHT. FWD RT RECIRCULATION FAN TO MCO/PLAC PER MEL 21-25-01A. REPLACED RT RECIRCULATION FAN PER M/M, REMOVED MCO/PLAC. 2L72 4F RTA1NM 20040225001792004022500179NM 2004 2 25 DL738031148 120031230A302032156183 ANTI-ICE VALVE BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 2 ENGINE FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27388DA 30375 875510 NR 2 ENG COWL ANTI-ICE LIGHT ILLUMINATED DURING T/O ROLL. ABORTED AT 50 KTS N1 89 PERCENT. REPLACED NR 2 AIV, OPS CHECKS OK. 2L72 4F4 FRTA16WE E00055EN 20040226000022004022600002WP 2004 2 26 ASAA0380378 120030421A5312 BULKHEAD DOUG DC9 DC982 3022082WP CRACKED CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND AFT PRESSURE BULKHEAD FORWARD FACE IS CRACKED AT OP MOST RIVETS. REPLACED WEB AT BL 0 PER SRM 51-30-5. (M) 2L72 4F A6WE 20030829001042003082900104 2003 8 29 3144022703 420030227A3424A593002 INDICATOR SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT DEFECTIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP075226R1864 3144 22090 TURN SLIP INDICATOR LOST TURN FUNCTION. 1G71 3U3 U H9EU E00054EN 20030829001102003082900110NM 2003 8 29 SWAA031878 120030821A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 PLUS 3, BELOW STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030902000562003090200056EU 2003 9 2 VY1L103169 120030112A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED L VY1LO OTHER O OTHER NRNOT REPORTED 1 SW19453NW6019 2475 TAIL ROTOR BEARING CRACKED BEYOND LIMITS. 1G71 3U3 U H9EU E19EU 20030902000612003090200061EA 2003 9 2 2003F00388 220030623A7314 DIAPHRAGM LYC PIPER PA32 PA32300 7103212SO LYC O540 IO540K1G5 41532EA HARTZLHCC2Y HCC2YK1 GL ENG FUEL PUMP TORN E LABAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL0554KA 2100 2100 327840197 L833948A CH32896B AIRCRAFT EXPERIENCED ERRATIC FUEL FLOW AND SURGING ON CLIMB-OUT. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. UPON TROUBLESHOOTING BY MAINT DEPT THE UPPER DIAPHRAGM ON ENG DRIVEN PUMP WAS FOUND TORN. THIS WAS EVIDENTLY ALLOWING AIR INTO THE FUEL SYSTEM. REMOVED AND REPLACED PUMP. 1L71 3O3 O A3SO 1E4 5 CP920 20030902000662003090200066CE 2003 9 2 000100 120030625A3260 UPLOCK SWITCH LEAR 24 24D 5170311CE MLG INOPERATIVE E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05324TW 24D324 PILOT REPORTED GEAR WOULD NOT RETRACT AFTER DEPARTING YIP, CREW RETURNED TO YIP WITH GEAR DOWN AND LOCKED INDICATION. MAINTENANCE CLEANED LUBED AND ADJUSTED ALL UPLOCK SWITCHES IAW M/M AIRCRAFT RETURNED TO SERVICE. 2L72 4J A10CE 20030902000682003090200068SO 2003 9 2 PNSA030602 120030622A3243 LINE PIPER PA32 PA32301 7103207SO LYC O540 IO540* 41532EA HYD SYSTEM LEAKING E PNSAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL038212H 328006046 DURING CRUISE SMELLED A BURNING ODOR AND SLIGHT SMOKE IN COCKPIT WITH CABIN HEAT TURNED ON. OPENED COCKPIT VENTS AND SMOKE WENT AWAY, RETURNED TO CDB AIRPORT WHERE MAINTENANCE FOUND HYDRAULIC LINE FOR BRAKE RES. LEAKING ONTO HEAT DUCT, REPLACED LINE AND GROUND RUNUP NORMAL. 1L71 3O3 O A3SO 1E4 20030902000892003090200089SO 2003 9 2 SWIA200312142 120030619A3230 PIN EMB 120 EMB120ER 3260203SO MLG CONTROL DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07250YV 120250 DURING LANDING GEAR RETRACTION, LEFT MAIN FORWARD GEAR DOORS WOULD NOT CLOSE AFTER GEAR RETRACTED. CLOSED AFTER GEAR WAS DOWN. REPAIRED AND REPLACED PIN ON P1067 LANDING GEAR CONTROL. PERFORMED SEVERAL GEAR SWINGS. OPS CHECK GOOD. 2L72 4T RTA31SO 20030902000932003090200093SO 2003 9 2 SWIA200312146 120030627A5753 ROLLER EMB 120 EMB120ER 3260203SO TE FLAPS DAMAGED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07268UE 120207 AFTER TAKEOFF, FLAPS WOULD NOT RETRACT TO FULL UP POSITION. QRH PROCEDURE FOLLOWED BUT WITH NO RESULT. DISAGREEMENT OBSERVED. REPLACED ROLLER AND BRACKET ON LT OUTBOARD FLAP GAP FAIRING. 2L72 4T RTA31SO 20030902000992003090200099CE 2003 9 2 BSY2003F00015 120030605A26122440723503915 FIRE LOOP LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP TAILPIPE LWR ENDINOPERATIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0756JA 342 P74236 LEFT ENGINE HAD A FIRE LIGHT COME ON IN FLIGHT, SHUT ENGINE DOWN, BLEW BOTH FIRE BOTTLES AND RETURNED TO AIRPORT. INSPECTED ENGINE FOR FIRE, NONE NOTED. REMOVED ENGINE TAILCONE AND CHECKED FOR EXHAUST LEAKS NONE FOUND. REMOVED AND REPLACED LOWER MIDDLE AND AFT ENGINE TAIL PIPE FIRE LOOPS AS PRECAUTIONARY MEASURES. TEST FLIGHT TO FOLLOW. 2L72 4F4 F A10CE E6WE 20030902001072003090200107EU 2003 9 2 COE2003F00001 120030527A261251271107 FIRE DETECTOR FOKKERF27 F2760 4990616EU RT ENGINE FALSE INDICATIONA COEAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM13719FE 10467 IN FLIGHT, THE FIRE WARNING LIGHT AND BELL CAME ON FOR RIGHT ENGINE. ENGINE WAS SHUT DOWN PRECAUTIONARY AND BOTH FIRE BOTTLES WERE DISCHARGED. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. FIRE WARNING WAS DETERMINED TO BE A FALSE INDICATION. REMOVED AND REPLACED THE OIL BREATHER TUBE FIRE WIRE AND CLEANED CONTACTS AT COUPLINGS. REPLACED FIRE BOTTLES AND SQUIBBS. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTEXPA2H72 20030902001342003090200134 2003 9 2 2003F00395 420030702A2312VC207 CONTROL HEAD SWRNGNSA227 SA227AC 8780603SW COMMS DIRTY E HKGAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW17691AX 200 AC691 ON FINAL THE PILOT REPORTS THAT HE OBSERVED AND SMELLED AN ELECTRICAL ODOR IN THE COCKPIT AREA. FOLLOWING LANDING, THE AIRCRAFT WAS GROUNDED, AND AN INSPECTION WAS CONDUCTED. MAINTENANCE DETERMINED THE PROBLEM TO BE ASSOCIATED WITH THE NR 2 COM TUNER HEAD. THE UNIT WAS REMOVED AND REPLACED WITH A SERVICABLE PART. INSPECTION OF THE UNIT REVEALED MINOR ARCHING HAD OCCURED, HOWEVER MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM. POSIBLE DIRT AND DEBRIS MAY HAVE CONTRIBUITED TO THE PROBLEM.THIS COMPONENT HAS BEEN SHIPPED TO A VENDOR FOR FURTHER INSPECTION. AS A PRECAUTION, ALL INSTRUMENTS IN THE AREA WERE CLEANED AND INSPECTED. ALL NAV AND COM CONTROL HEADS WERE REPLACED. 2L72 4T RTA8SW 20030902001482003090200148EA 2003 9 2 SWIA200312160 120030702A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07587SW 7062 FLAPS FAIL MESSAGE AT FLAPS 45 DEGREES.REMOVED AND REPLACED RT BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD, PN OFF 855D100-7 SN OFF 238. 2L72 4F RTA21EA 20030902001582003090200158CE 2003 9 2 GVR2003F00004 120030617A2520551900939 SEAT CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE CABIN CRACKED B GVRRO OTHER O OTHER NRNOT REPORTED 1 CE05490CC 5500490 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. 1L72 4F4 F A22CE E1NE 20030902001732003090200173NM 2003 9 2 PCAA0307081 120030710A5210 DOOR DHAV DHC8 DHC8102 2809003NM PASSENGER DOOR OUT OF ADJUST A PCAAK NONE O OTHER TXTAXI/GRND HDL 1 EA13825EX 388 PHL-FLIGHT NR 3556. CREW REPORTED THAT FLIGHT ATTENDANT COULD NOT OPEN THE PASSENGER DOOR. MAINTENANCE ADJUSTED THE PASSENGER DOOR IAW MFG DASH 8 MAINTENANCE MANUAL 52-10-00. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030902001782003090200178 2003 9 2 03FDEA01091 420030711A2210B415ABM1 CONTROLLER AIRBUS300 A300B4605R 3930308EU AUTOFLIGHT SYS FAILED A FDEAO OTHER G MULTIPLE FAILURE APAPPROACH 1 SO25670FE 777 CWF CLOSER DURING CATIII APPROACH WITH A NORMAL GLIDE SLOPE AND SINK RATE A RAPID COUNTDOWN (50,40,30,ECT) OCCURED AND THE AIRCRAFT FLARED EARLY FOLLOWED BY A PUSHOVER AND SUBSEQUENT FIRM LANDING. REMOVED AND REPLACED TCC IAW AMM 22-36-34-4 AND RADIO ALT. (ON NR S00026) IAW AMM 22-36-42-4. PERFORMED AFS/LAND TEST IAW AMM 22-40-00 AND TEST OF THE RAD. ALT. SYSTEM IAW AMM 34-42-00-5, OP'S CHECK GOOD. PERFORMED PRECAUTIONARY INSPECTION, IAW CUSTOMER REQUEST, FOR FIRM LANDING VIA AMM REF 05-11-00 PG 5 THRU 62 PHASE ONE. WITH NO DEFECTS EXCEPT TIRE WEAR. 2L72 4F RTA35EU 20030902001892003090200189NM 2003 9 2 03FDEA00977 120030623A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 FLOOR SEAT TRACK AT STA 635 LH X=47.5 CRACKED. FLOOR TRACK AT STA 635 LH X=47.5 CARRIED OUT REPAIR IAW SRM 53- 70-00 VOL.I. 2L73 4F RTA22WE 20030902001962003090200196NM 2003 9 2 03FDEA01088 120030710A2840 DISPLAY DOUG MD11 MD11 3023602NM FUEL SYSTEM INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25601FE 48401 CLIMBING THRU 18,000 FT BOTH "TIP LOW" (1 AND 3) LEVEL ONE ALERTS CAME ON SHORTLY AFTER FUEL SYSTEM SELF CORRECTED. UPON REACHING CRUISE FL 370 NOTICED FUEL DECREASING AT AN ABNORMAL RATE. ONE MINUTE LATER "FUEL QTY/USED CHK" LEVEL 2 ALERT CAME ON. AT THAT TIME TOTAL FUEL WAS 10,000 #S BELOW PLANNED WITH FUEL STILL DECREASING (ALL TANKS EQUALLY). ENROUTE KOAK TO KSEA DIVERTED TO KSMF. FUEL SYSTEM INDICATED WE HAD LOST 12,000#S. AFTER LANDING AT KSMF. "MEL 28-01-01-02: TANK NO. 2_ FUEL TANK SYN OPTIC QTY DISPLAY- INOP. 2L73 4F RTA22WE 20030903000222003090300022NM 2003 9 3 03FDEA01098 120030715A2610 CONTROL BOX BOEING727 727200 138407ENM FIRE & OVERHEAT MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25278FE 22345 GOT LOWER BODY OVERHEAT LIGHT ON CLIMBOUT UPON DESCENT, LIGHT EXTINGUISHED WITH THROTTLE REDUCTION. T/S IAW 26-14-000-1, FOUND AFT STAIR LT LOOP RUBBING AGAINST STREAMER OF A/C. REPOSITIONED SAME, RERACKED FIRE AND OVERHEAT CONTROL BOX. RAN ENGINES AT GATE AND CHECKED FOR LEAKS, NONE FOUND. RAN A/C AT TAKEOFF POWER FOR 3 MINUTES, LIGHT FOR LOWER AFT BODY DID NOT COME ON. OK TO CONTINUE. 2L73 4F RTA3WE 20030828001452003082800145EA 2003 8 28 2003F00522 120030513A7830TY214810A ISOLATION VALVE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER MALFUNCTIONED A FDKAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07501MJ 10047 FRL - FLT 6721 - PHD-FAT, ABORTED TAKEOFF, NR 1 ENGINE REV UNSAFE MSG ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE, MAINTENANCE TROUBLESHOT AND APPLIED MEL 78-30-01 AND RETURNED AIRCRAFT TO SERVICE. MAINTENANCE REPLACED THE ISOLATION CONTROL VALVE. (M) 2L72 4F RTA21EA 20030828001472003082800147NM 2003 8 28 HALA0300695 120030729A5755 FITTING BOEING717 717200 1383700NM LT SPOILER CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13476HA 55118 DURING ACCOMPLISHMENT OF M1-57-01, FOUND LEFT OUTBOARD SPOILER ACTUATOR, INBOARD FITTING CRACKED. REMOVED OUTBOARD SPOILER PANEL AND SPOILER ACTUATOR PER AMM 27-60-01 AND 27-67-05. SPOILER IDLER REMOVED PER AMM, 7-29-03/5718 PER AMM 27-60-01-4 COMPLETED STEPS D THRU J ON SPOILER INSTALLATION SUBTASK 27-60-01-430-003. COMPLETED STEPS K THRU R AMM SUBTASK 27-60-01-430-003 OF SPOILER ACCOMPLISHED MM 27-60-01-430-003 (SUBTASK) F1S-F2 ACCOMPLISHED MM TASK 27-60-01-820-801 3A-G1. ACCOMPLISHED MM TASK 27-60-01-720-801 2A-01D2. COMPLETED SPOILER INSTALLATION PER MM 27-60-01-5. (M) 2L72 4F TRA6WE 20030828001762003082800176NM 2003 8 28 SWAA031871 120030819A3350101073 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING IN AFT CABIN. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030829000062003082900006CE 2003 8 29 52753 120030719A2701 BRACKET BEECH 1900 1900D 1154162CE COCKPIT OUT OF POSITION A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07174YV UE174 ON FLIGHT 5541 FROM LATROBE PENNSYLVANIA TO PITTSBURGH PENNSYLVANIA, AFTER TAXI OUT THE RIGHT AILERON TRAVEL HAS A CATCH AND A NOISE. THE CREW RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED THE COVERING IN THE COCKPIT OVER THE CONTROL CABLES WERE NOT SECURED. MAINTENANCE DISPATCHED FOR REPAIR. MAINTENANCE REPOSITIONED THE BRACKET AND RESECURED THE YOKE BOOT. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030829000082003082900008WP 2003 8 29 ARWA20030512 120030527A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR SURFACE WITH CORROSION, STATION 510, L-35R. REPAIRED FUSELAGE LOWER SKIN AT FUSELAGE STA 510 AND L-35R IAW AVITAS ENGINEERING REPAIR ORDER AROW-031RO-5, PAGE 1 & 2, DATED 05/01/03 AND REPAIR DRAWING AIPSAC-N784AL-05/03, REV IR, SHEETS A.1 TO A.5, DATED 05/01/03. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. 2L74 4F 4A25 20030829000422003082900042EA 2003 8 29 COMA0360367 120030818A53116013600121 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA10366 7306 CRACKS NOTED IN THE FLANGE RADIUS OF FRAMES AT FS 640 BELOW STRINGER 9. LT AND RT SIDE REPAIRED IAW REO 601R-53-61-487. 2L72 4F RTA21EA 20030829000432003082900043EA 2003 8 29 COMA0360377 120030818A5730601R100461 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01932CA22101 7038 DURING COMPLIANCE OF SERVICE BULLETIN S/B A601R-57-031, A CRACK WAS FOUND IN THE LEFT WING LOWER PLANK IN THE AREA OF THE REAR SPAR AT WS 148.019. THE PLANK WAS REPAIRED PER BOMBARDIER REO 601R-57-21-351. 2L72 4F RTA21EA 20030829000542003082900054WP 2003 8 29 DHL2003873528 120030628A5522 PLATE DOUG DC8 DC873F 302199FWP LT ELEVATOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT ELEVATOR L\E PLATING WITH INTERIM REPAIR AT STA XE.74.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-4-1 FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW PLATING IAW SRM 55-4-1 FIG 1. CLEANED, TREATED AND PRIMED PLATING INNER SIDE IAW SRM 51-1-8B. INSTALLED NEW PLATING WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. REFER TO N\R 2156 FOR REBALANCING. 2L74 4F RT4A25 20030829000612003082900061EU 2003 8 29 DHL2003362012 120030711A261224402534 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 1 ENGINE FAULTY A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01362DH 84 ENGINE NR 1 FIRE DETECTION LOOP-A LIGHT ILLUMINATED IN FLIGHT. ABNORMAL PROCEDURE COMPLETED. REMOVED AND REPLACED NR 1 ENGINE PYLON SECTIONS OF LOOP WITH SERVICEABLE UNITS IAW A300 M/M 26-12-12. 2L72 4F RTA35EU 20030829000682003082900068WP 2003 8 29 03FDEA01204 120030803A78303113M59P0001A RING DOUG DC10 DC1030 3023501WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 EXHAUST- THRUST REVERSER-REPAIR OF TR OUTER RING P/N 3113M59P001A. FACT 02AUG03 01:10 BFM R COMPLIED WITH EA 8-7832-70994 EXHAUST- THRUST REVERSER- REPAIR OF T/R OUTER ENG P/N 3113M59P001A AT MAE. 2L73 4F A22WE 20030829000712003082900071SO 2003 8 29 LR7A03049 120030716A24212CM353C1H GENERATOR LKHEED382 382G 526414USO NR 1 ENGINE FAILED A LR7AE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 AL03402LC698 4698 EN ROUTE OJAF/ETAR AT FL140, NR 1 GENERATOR OUT LIGHT WITH BEARING FAIL LIGHT CAME ON. SHUTDOWN NR 1 ENGINE IAW QRH. REMOVED AND REPLACED NR 1 ENGINE DRIVEN GENERATOR IAW SMP 581 24-20. OPS CHECK NORMAL. 2H74 4T A1SO 20030829001322003082900132NM 2003 8 29 SWAA031860 120030819A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (3 EA) BS 360 AT STR 4L, BS 360 AT STR 10L AND BS 908 AT STR 4R. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030829002072003082900207 2003 8 29 USAASB03117 420030720A23304976500001 VIDEO MONITOR BOEING737 7373B7 1384580NM CABIN ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19522AU 23857 CLT - FLT 1009 - AFTER TAKEOFF FROM CLT, AT APPROXIMATELY 7,000 FEET, THE FLIGHT ATTENDANT REPORTED TO THE FLIGHT CREW A STRONG ELECTRICAL ODOR IN THE MID AND AFT CABIN. NO SMOKE WAS NOTED. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIEDL AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. ODOR WAS GONE BY THE TIME AIRCRAFT REACHED THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 3 VIDEO MONITOR. OPERATIONAL CHECK GOOD. REMOVED MONITOR WAS REPORTED TO SMELL OF HOT CIRCUITRY. (M) 2L72 4F RTA16WE 20030829002082003082900208NM 2003 8 29 USAA030133 120030727A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US52921 22956 PIT - FOUND SKIN CRACKED .5 INCH, RIGHT AFT DOOR LOWER HINGE CUTOUT FORWARD LOWER CORNER. INSTALLED DOUBLER AND TRIPLER PER SRM 53-60-01 AND EA 76713. (M) 2L72 4F RTA16WE 20030902001032003090200103EU 2003 9 2 U30A200300019 120030630A3350321430 BATTERY PACK AIRBUS320 A320212 3930322EU ZONE 263 DISCHARGED A U30AK NONE L NO TEST ININSP/MAINT 1 EA17265AV 427 DURING DAILY CHECK, AFTER FLT 329 IN BWI, MAINTENANCE PERSONNEL DISCOVERED THAT ROWS 21, 25 & 27 ON LT SIDE OF AIRCRAFT AND THE L2 & R2 (LT AND RT REAR DOORS) EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN TESTED. THE EPSU (EMERGENCY POWER SUPPLY UNIT) BATTERY PACK AT THE L2 DOOR WAS REPLACED AND TESTED I/A/W AMM 33-51-38-401. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA28NM 20030902001742003090200174NM 2003 9 2 372PA0033 120030709A3350 LIGHT BOEING737 737306 13844BGNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 EMERGENCY FLOOR PATH LIGHTS INOPERATIVE, ROW 20 AFT. REPLACED TERMINAL BLOCK. CHECKS OK. 2L72 4F4 FRTA16NE E2GL 20030903000052003090300005WP 2003 9 3 DHL2003803009 120030711A2510 SEAT DOUG DC8 DC873 302199CWP GE CFM56 CFM56* 13802NE COCKPIT BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH 46123 SO'S SEAT LATERAL ADJUST HANDLE BROKE. REMOVED AND REPLACED SO'S SEAT IAW M/M 25-11-3. OPS CK NORMAL. 2L74 4F4 FRT4A25 E2GL 20030903000342003090300034CE 2003 9 3 HI12003F00000 120030617A5350R821486 CHANNEL CESSNA208 208B 2073701CE FAIRING DAMAGED B HI1RO OTHER O OTHER NRNOT REPORTED 1 NE05919FE 208B0019 DAMAGE TO FUSELAGE DUE TO CHAFE FROM LOWER WING STRUT FAIRING. DAMAGE FOUND ON AIRCRAFT. RECOMMEND P/M OF RUBBER CHANNEL IN THE IPC BE ADDED TO PAGE 57-10-04. 1H71 3T A37CE 20030903000452003090300045NE 2003 9 3 52531 220030713A7250PT6A67DGG GAS GENERATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE ENGINE FAILED A AMWAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE07135YV9555 9555 UE135 ON FLIGHT 702 FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO, TAKEOFF WAS NORMAL. AS THEY DID THE INITIAL CLIMBOUT, THE CREW RECEIVED A LOW OIL PRESSURE INDICATION (ANNUNCIATOR). THE LEFT ENGINE OIL PRESSURE GAUGE INDICATED A RAPID AND CONTINUOUS DROP IN OIL PRESSURE. THE CREW INITIATED A LT ENGINE SHUTDOWN AND DECLARED AN EMERGENCY PROCEDURES CHECKLIST. THE CREW IMMEDIATELY RETURNED TO FARMINGTON NEW MEXICO AND THE PASSENGERS WERE DEPLANED. MAINTENANCE REMOVED AND REPLACED THE LEFT GAS GENERATOR. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T4 TRTA24CE E26NE 20030903000472003090300047NM 2003 9 3 DHL2003743011 120030715A2612 DETECTOR BOEING727 727225 1384077NM PWA JT8 JT8D* NE NR 3 ENGINE INTERMITTENT A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01743DH 22438 NR 3 ENGINE DETECTOR CIRCUIT GROUND LIGHT CAME ON. INSPECTED NR 3 ENGINE DETECTOR AND FOUND NO DEFECTS IAW M/M 26-11-00. 2L73 4F4 F A3WE E2EA 20030903000732003090300073 2003 9 3 133131 420030514A34216226342022 DISPLAY SAAB SF340 SF340A 7850100EU FAILED A UHLAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL17148SD 340A148 FLIGHT 4477 PIT-IPT. DURING FLIGHT THE RT EHSI SCREEN WENT BLANK. A/C RETURNED TO PIT FOR REPAIR 2L72 4T RTA52EU 20030903000802003090300080EA 2003 9 3 SWIA200312179 120030711A2750855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07587SW4051 4051 7062 FLAPS FAIL MESSAGE WHEN SELECTING FLAPS FROM 0-8 DEGREES. LANDED AT FLAPS 8 DEGREES.REPLACED LT AND RT BPSU'S IAW MM 27-51-10. OPS CHECKS GOOD AT THIS TIME. LT P/N: 855D100-5 S/N OFF: 230 2L72 4F RTA21EA 20030903000852003090300085 2003 9 3 MEX2003273 420030707A3443232963 ANTENNA BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE WAVE GUIDE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23805AM 26272 AIRCRAFT ARRIVED WITH CAPTAIN REPORT RADAR OUT OF SERVICE. DURING REVISION WAS DETECTED WAVE GUIDE WITH DAMAGE. AIRCRAFT WAS SENT TO THE HANGAR, AND THE WAVE GUIDE WAS REPLACED IAW 34-40-01. ADDITIONALLY AS A PREVENTIVE ACTION ANTENNA RADAR WAS REPLACED, ALL TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20030903001062003090300106EU 2003 9 3 USAASA03068 120030621A3242 BRAKE AIRBUS320 A320214 3930316EU MLG MALFUNCTIONED A K NONE O OTHER LDLANDING 1 EA19105UW 0868 FLL - FLT 1623 - EN ROUTE CLT-FLL, DURING LANDING IN FLL, ALL FOUR MAIN TIRES BLEW OUT DUE TO LOCKED UP BRAKES. SUBSEQUENT INVESTIGATION FOUND THAT THE PARKING BRAKES WERE LEFT ON FOR LANDING. (M) 2L72 4F RTA28NM 20030903001072003090300107 2003 9 3 USAASA03086 420030806A2565C37103103 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE O OTHER ININSP/MAINT 1 EA19751UW 1317 BOS - THE AFT RIGHT EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030903001142003090300114EA 2003 9 3 2003F00526 120030513A7830TY214810A ISOLATION VALVE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER FAULTY A FDKAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07501MJ 10047 FRL - FLT 6721 - PHX-FAT - ABORTED TAKEOFF, NR 1 ENGINE REV UNSAFE MSG ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE, WERE MAINTENANCE TROUBLESHOT AND APPLIED MEL 78-30-01 AND RETURNED A/C TO SERVICE. MAINTENANCE REPLACED THE ISLOATION CONTROL VALVE. (M) 2L72 4F RTA21EA 20030829001272003082900127NM 2003 8 29 SWAA031855 120030818A256065C16820 LATCH BOEING737 7373H4 1384600NM FWD ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMRGENCY EVAC SLIDE GIRT ASSY LATCH LOOSE. SECURED LATCH PER MM. 2L72 4F RTA16WE 20030829001292003082900129NM 2003 8 29 SWAA031857 120030819A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 616,WL 206 AND RBL 66. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20030829001372003082900137 2003 8 29 SWAA031831 420030802A2565D31354 SLIDE BOEING737 7375H4 138449DNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030829001452003082900145NM 2003 8 29 SWAA031839 120030813A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 760 AT STR 19R, BS 932 AT STR 23R AND BS 940 AT STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001532003082900153NM 2003 8 29 SWAA031847 120030816A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND BS 1016 BULKHEAD WEB CORRODED BETWEEN STR 24L AND STR 24R ON FWD SIDE. REPAIRED BULKHEAD WEB PER SRM AND SWA ACO. 2L72 4F RTA16WE 20030829001672003082900167NM 2003 8 29 SWAA031816 120030811A335007912 COVER BOEING737 7375H4 138449DNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER MISSING AT ROW NR 12. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20030829001732003082900173NM 2003 8 29 SWAA031810 120030812A3350101073 LENS BOEING737 7377H4 1384404NM FWD ENTRY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29753SW 29848 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030829001772003082900177 2003 8 29 SWAA031814 420030811A256565C19901 CABLE BOEING737 7373H4 1384600NM AFT ENTRY DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030902001272003090200127NM 2003 9 2 AWXA200300781 120030625A53156545834107 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A .3125 INCH CRACK WAS FOUND THE LOWER SURFACE OF TRANSVERSE FLOOR BEAM AT BS 344, LBL 46. MAINTENANCE REPAIRED CRACKED STRAP ON LOWER SURFACE PER BOEING SRM 53-10-51 PAGE 213-219 FIG. 204. 2L72 4F RTA16WE 20030902001632003090200163CE 2003 9 2 S1F2003F00000 120030618A812046P22250 TURBOCHARGER CESSNA206 T206H 2073303CE LYC O540 TIO540AJ1A EA ENGINE DAMAGED B S1FRO OTHER O OTHER NRNOT REPORTED 1 SO335224A64 T20608385 L1124961A ON TAKEOFF TOWER REPORTED SMOKE FROM ENGINE TAILPIPE. MECHANIC FOUND TURBOCHARGER BEARING VERY LOOSE AND INTAKE BLADES ON TURBO BROKEN. INSTALLED NEW TURBOCHARGER. 1H71 3O3 ORTA4CE E14EA 20030902001872003090200187NM 2003 9 2 03FDEA00975 120030623A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 FLOOR SEAT TRACK AT STA 635 LH X=8.5 CRACKED. CORRECTIVE ACTION SNRM N0163 : CABIN - FLOOR TRACK AREA AT BS 625 TO BS 745 LT X=8.5 CARRIED OUT SEAT TRACK REPAIR IAW SRM 53-70-00 VOL.I 2L73 4F RTA22WE 20030903000312003090300031EU 2003 9 3 PG9R103183 120030320A7931704A37642042 PRESSURE SWITCH SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ENGINE OIL FAILED A PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19911KR5668 2094 ENGINE OIL PRESSURE SWITCH FAILED WITH ONLY 221.1 HOURS. 1G71 3U3 UNCH9EU E19EU 20030903000922003090300092WP 2003 9 3 MEX2003277 120030708A5260 SENSOR DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE AIRSTAIR DOOR MALFUNCTIONED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW231075T 49724 AIRCRAFT AIR TURN BACK, DURING FLIGHT THE LIGHT FWD STAIRWAY DOOR COME ON. THE FWD STAIRWAY DOOR SENSOR WAS CHECKED IAW 52-61-00, AND BITE WAS PERFORMED TO PRESSURIZATION CONTROLLERS IAW 21-32-03, ALL TESTS CORRECT. 2L72 4F4 FRTA6WE E2EA 20030903000962003090300096WP 2003 9 3 MEX2003288 120030714A301012911211 SWITCH DOUG DC9 DC982 3022082WP ANTI-ICE SYS MALFUNCTIONED A ASMFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW23491SH 49150 FLT 215 - HMO-GDL - AIRCRAFT ARRIVED WITH CAPTAIN REPORT 'L ICE PROTECT TEMP HI' LIGHTS TURN ON. DURING TRANSIT CHECK THE THERMOSTAT AND ANTICIPATOR WERE REPLACED IAW MM 36-10-00. AIRCRAFT WAS DISPATCHED AND AIR TURN BACK AS A CONSEQUENCE OF 'L ICE PROTECT TEMP HI' LIGHTS TURN O. THE HI TMEP SENSOR AND ELECTRONIC THERMAL SW WERE SWAPPED. ADDITIONALLY, THE ANTICIPATOR WAS ADJUSTED AND ENGINES WERE STARTED IT AT 1.8 EPR IAW MM 30-10-06/08, 71-00-00, ALL TESTS CORRECT. (M) 2L72 4F A6WE 20030903001112003090300111WP 2003 9 3 0301249614 120030707A272037723745503 SHUTOFF VALVE DOUG DC9 DC932 3022066WP TAIL AREA CRACKED A NWAAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 GL01614NW 47128 RIGHT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO DURING TAXI OUT. FUMES ENTERED THE CABIN BUT CREW WAS ABLE TO CLEAR THE AIR.CREW STATED THAT THE RED EMERGENCY WARNING LIGHT DID NOT ILLUMINATE. AIRCRAFT WAS TOWED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RUDDER POWER SHUTOFF VALVE CRACKED AND REPLACED IT. ALSO REPLACED THE NBR 2 ENGINE DRIVEN AND ELECTRICAL HYDRAULIC PUMPS AND ASSOCIATED FILTERS AS A PRECAUTION. COALESCER BAGS WERE ALSO REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030903001162003090300116NM 2003 9 3 KPVA200333 120030726A3234574205A SELECTOR VALVE DHAV DHC8 DHC8103 1386005NM LANDING GEAR FAULTY A KPVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13807WP 023 MKK - FLT 1242 - DURING TAKEOFF, GEAR CAME UP AND DOOR LIGHTS ALL OUT, THEN MAIN AMBER DOOR LIGHTS CAME ON. CYCLED GEAR DOWN, ALL LIGHTS OUT. WITH GEAR UP, RIGHT MAIN DOOR LIGHT STAYED ON. PUT GEAR DOWN, LIGHTS OUT. DISPATCH INSTRUCTED FLIGHT CREW TO RETURN TO MKK. SENT MAINTENANCE CREW TO MKK TO T/S, AIRCRAFT FERRIED BACK TO HNL FOR FURTHER MAINTENANCE. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE, RETRACTION CHECK, ON GROUND, CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. ALL WORK PERFORMED IAW APPROVED MANUFACTURERS MAINTENANCE MANUALS. (M) 2H72 4T RTA13NM 20030903001182003090300118WP 2003 9 3 GTIA030604 120030802A3150 WARNING SYSTEM DOUG DC9 DC983 3022083WP COCKPIT MALFUNCTIONED A GTIAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL23824NK 53015 LGA - FLT 313 - TOO LOW GEAR WARNING FROM GPS SHORT FINAL, DID GO AROUND. RETRACTED GEAR. NO FURTHER WARNING ON SUBSEQUENT LANDING. PERFORMED FUNTIONAL TEST SEVERAL TIMES COULD NOT GET THE SYSTEM TO FAIL. (M) 2L72 4F RTA6WE 20030903001282003090300128NE 2003 9 3 2003F00529 220030711A7200 ENGINE CVAC 240 240* 2422601WP PWA R2800 R2800* 52026NE LEFT MALFUNCTIONED A I5HAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL23156PA 324 P32466 WHILE EN ROUTE TO CVG FROM PIT, IN CRUISE CONFIGURATION, THE CREW FELT A SHUDDER IN THE LEFT ENGINE. FIFTEEN MINUTES LATER FELT ANOTHER SHUDDER AND AGAIN ONE MINUTE LATER WITH A LARGE TORQUE SWING AND OIL QUANTITY DROP. THE OIL LOSS WAS FASTER THAN THE CAPACITY OF THE OIL TRANSFER PUMP TO HANDLE. THE CREW FEATHERED THE LEFT ENGIEN AND DIVERTED TO LCK MX BASE. LANDED UNEVENTFULLY AT LCK. AN EXAM OF THE OIL FILTER HAS REVEALED A LARGE AMOUNT OF FERROUS METAL. THE LEFT ENGINE WILL BE REMOVED AND REPLACED. (M) 2L72 4R4 R A793 5E8 20030903001372003090300137NM 2003 9 3 GAIA03048OP 120030722A3260669482725 CIRCUIT BOARD BOEING727 727223 1384074NM E/E BAY LOOSE A GAIAK NONE N FALSE WARNING APAPPROACH 1 SW076833 20186 FLT 864 - FWA-EWR, ON APPROACH THE FILGHT CREW NOTICED THAT THE NOSE GEAR DOWN AND LOCKED GREEN LGIHT DID NOT ILLUMINATE ON GEAR EXTENSION. AN UNEVENTFUL LANDING WAS MADE IN EWR. RESECURED THE CIRCUIT BOARD CARD IN THE MASTER LIGHT DIMMING CONTROL UNIT. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030903001392003090300139WP 2003 9 3 2003F00540 120030405A53475R095301157003 SEAT TRACK DOUG DC9 DC987 3022087WP FUSELAGE CORRODED A WXOAK NONE O OTHER ININSP/MAINT 1 WP17948MA 49778 FOUND CABIN FLOOR SEAT TRACK HAS CORROSION FS 200-221 LBL 44. REMOVED CORRODED SECTION. FABRICATED AND INSTALLED REPAIR MEMBER IAW DC9 MD80 SRM 53-05 FIG 4F. (M) 2L72 4F RTA6WE 20030903001452003090300145SO 2003 9 3 RAIA00307191 120030714A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03801HK 145053 EXIT LIGHT AT RT OVERWING EMERGENCY EXIT INOP. RE-SECURED CONNECTOR AT EXIT LIGHT. 2L72 4F RTT00011AT 20030903001502003090300150NM 2003 9 3 VNAA0308014 120030821A3412012JG1AG02 PROBE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07441JS20494 3059 DURING FLIGHT, THE CREW RECEIVED A TAT HEAT FAIL CAS MESSAGE AND RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE TAT PROBE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030903001662003090300166NM 2003 9 3 DHL2003747009 120030730A5210 SNUBBER BOEING727 727224 1384076NM PAX DOOR OUT OF ADJUST A DHLAK NONE O OTHER LDLANDING 1 SO01747DH 22253 ON TOUCHDOWN FORWARD ENTRY DOOR HANDLE POPPED OPEN. ADJUSTED ENTRY DOOR SNUBBERS, OPS CHECKED GOOD IAW 52-11-0. 2L73 4F A3WE 20030903001682003090300168WP 2003 9 3 DHL2003873578 120030628A5244 PLATE DOUG DC8 DC873F 302199FWP ACCESS DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 AFT ACCY COMPT NR 13 ACCESS DOOR EXTERNAL PLATING CRACKED 0.500 NEXT TO HANDLE AT STA 660.000, L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1, SRM 52-8-1 FIG 1 PG 2. REMOVED FASTENERS AND CRACKED EXTERNAL PLATING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW PLATING IAW SRM 51-1-8B. INSTALLED NEW PLATING ON NR 13 ACCESS DOOR AT STA 660.000, L-36 IAW SRM 51-1-15 PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030903001822003090300182WP 2003 9 3 AALA20030814 120030730A499038761864 PRESSURE SWITCH DOUG DC9 DC982 3022082WP APU FAULTY A AALAK NONE O OTHER CLCLIMB 1 SW21558AA 53088 STL - FLT 1677 - STL-PHX - APU SHUT DOWN AT 3000 FT, RETURNED STL AND LANDED WITHOUT INCIDENT. REPLACED OIL FILTER AND OIL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030903001912003090300191NM 2003 9 3 USAASB0301A 120030711A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 PIT - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030903001932003090300193NM 2003 9 3 AALA20030789 120030723A3350 GUARD BOEING777 777223 1385213NM CABIN OUT OF ADJUST A AALAK NONE L NO TEST ININSP/MAINT 1 SW21798AN 30797 LGW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT SWITCH COVER SPRING DETACHED FROM SWITCH ASSEMBLY CAUSING EMERGENCY LIGHTS TO GO TO OFF POSITION WHEN CLOSED. ADJUSTED EMERGENCY LIGHT SWITCH GUARD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030903002132003090300213NM 2003 9 3 QXEA200301004 120030818A33508250977001 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A QXEAK NONE O OTHER UKUNKNOWN 1 NM09359PH 514 PDX- SEVERAL EMERGENCY LIGHTS NOT ILLUMINATED. REMOVED AND REPLACED FORWARD EMERGENCY FLOOR LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903002222003090300222EA 2003 9 3 QXEA200301044 120030828A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT ACTIVATED A QXEAK NONE J WARNING INDICATION UKUNKNOWN 1 NM09613QX 10045 SEA- ON FLIGHT 2465 FIRE SYSTEM FAULT. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030903002282003090300228EA 2003 9 3 03224706 120030812A2613356024310 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE UNRELIABLE A VTZABE EMER. DESCENT ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 EA27706BR 7553 873113 DURING DESCENT CREW RECEIVED A 14TH STAGE WARNING MESSAGE AND SHUT DOWN THE LEFT ENGINE AS A PRECAUTION EMERGENCY WAS DECLARED FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT ENGINE PYLON 14TH STAGE OVERHEAT DETECTION LOOP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030826000992003082600099SW 2003 8 26 TU32003F00007 120030513A6220206011149105 YOKE BELL 206 206L3 1182108SW ALLSN 250B 250B17 03012GL MAIN ROTOR BRINELLED B TU3RK NONE O OTHER ININSP/MAINT 1 WP07112TV836 HB938 51123 DURING A 100 HOUR INSPECTION THE MAIN ROTOR HUB WAS BEING LUBRICATED. THE PITCH CONTROL LINKS WERE DISCONNECTED AND RATCHETING WAS FELT WHEN THE BLADES WERE ROTATED. THE HUB WAS REMOVED AND DISASSEMBLED. THE MAIN ROTOR YOKE HAD SEVERE BRINNELLING ON EACH SPINDLE. THE WAS NO INDICATION OF THE SEALS LEAKING AND THE PROPER AMOUNT OF GREASE WAS STILL INTACT THIS YOKE WAS PUT INTO SERVICE MAY 18, 2000 NEW. ALTHOUGH PROBABLE CAUSE IS UNDETERMINED, IT IS POSSIBLE THE METAL HARDNESS OF THE SPINDLES IS NOT ADEQUATE. 1G71 3U3 T H2SW E10CE 20030826001232003082600123EU 2003 8 26 03FDEA00986 120030627A2450 CIRCUIT BREAKER AIRBUS310 A310 EU ELECTRICAL SYS POPPED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25446FE 224 PDIS 446 24-50 0006790 27JUN03 RDU CLOSE R LOST AC BUS 2 DURING TAKE OFF ROLL AT ABOUT 40 KTS. FACT 27JUN03 11:53 RDU R FOUND 202XP BUS BAR BREAKER POPPED AND NR 2 GE HYD PUMP C/B POPPED , RESET SAME BOTH GREEN PUMPS OPERATE NORMAL, NR 2 AC BUS FAULT CLEARED , OK FOR SERVICE. 2L72 4F RTA35EU 20030826001412003082600141EA 2003 8 26 SIMA200307002 120030308A3234533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG INOPERATIVE A SIMAO OTHER O OTHER LDLANDING 1 SW21507AE 10059 DFW - FLT 9800 - DURING APPROACH, THE LANDING GEAR WOULD NOT EXTEND WHEN GEAR WAS SELECTED DOWN. CREW WAS ABLE TO EXTNED LANDING GEAR AFTER USING LANDING GEAR MANUAL RELEASE AS PER CHECKLIST IN ABNORMAL SECTION VOL 1. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE IAW CRJ MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030827000242003082700024NM 2003 8 27 03FDEA00905 120030618A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 N00801 FRAME AT BS 640, LBL 3, WL 155 IS CRACKED ON UPPER FLANGE IN RADIUS. CUTOUT CRACKED PORTION OF FRAME IN AREA OF 2.2 INCHES X 1.8 INCHES. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ON FRAME BS 640, LBL 3, W/L 155 IAW SRM 51-40-3 FIG 1 AND 51-30-2 STEPS 4 AND 7. 2L73 4F RTA3WE 20030827000352003082700035SO 2003 8 27 J792003F00001 220030606A8510641250 SEAL BEECH 58 58 1152740CE CONT O550 IO550C SO ENGINE LEAKING A J79RK NONE K FLUID LOSS ININSP/MAINT 1 GL1395KM 497 TH1315 810484R DURING ANNUAL 100 HOUR INSPECTION, FOUND LEFT ENGINE CRANKSHAFT SEAL LEAKING. REPLACED WITH NEW PN 641250. LEAK CHECK, OK. SUSPECT LEAK CAUSED BY WEAK SEALANT AND TSMOH. 1L72 3O3 O 3A16 E3SO 20030827000712003082700071SO 2003 8 27 CY42003F00001 220030331A8530FRCN712ACA CYLINDER HEAD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE SEPARATED A CY4RO OTHER O OTHER NRNOT REPORTED 1 AL0373047233 20700556 280019R CYLINDER HEAD SEPARATED FROM THE BARREL. 1H71 3O3 O A16CE E5CE 20030827001022003082700102NM 2003 8 27 CALA0300398 120030719A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714342 23580 INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE DECK AT BS 663, LBL 31. THE CRACKED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-60-51. 2L72 4F4 FRTA16WE E2GL 20030827001042003082700104NM 2003 8 27 CALA0300400 120030720A5240 ANGLE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE R1 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20030827001062003082700106NM 2003 8 27 CALA0300419 120030727A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND AFT BAGGAGE BIN AFT FLOOR SUPPORT CORRODED AT STA 947.5. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030827001162003082700116NM 2003 8 27 CALA0300414 120030725A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND STRINGER 27R CORRODED AT STA 1016, LBL 26. THE STRINGER WAS REMOVED AND A NEW STRINGER SECTION WAS INSTALLED IAW SRM 53-60-03. 2L72 4F RTA16WE 20030827001302003082700130NM 2003 8 27 CALA0300402 120030721A5330 BEAR STRAP BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A 2 INCH CRACK IN SKIN AND SILL PLATE SUPPORT STRUCTURE(BEAR STRAP/SKIN) AT FORWARD END OF FORWARD CARGO PIT OPENING, STA 450, STRINGER 25R. REPAIRED AREA IAW ECRA 5330-03272. 2L72 4F RTA16WE 20030827001602003082700160NM 2003 8 27 2003UALA00616 120030812A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29176UA 24383 AFT CARGO COMPARTMENT FLOOR FRAME STA 1580 RBL 47-57, UPPER T-CHORD BENT. 2L74 4F4 FRTA20WE E24NE 20030827001812003082700181SO 2003 8 27 C2XA03TY137 120030820A531514526437001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED 2C INSPECTION THE RT LAV FLOORBEAM WAS CORRODED. MAINT R&R THE RT FLOORBEAM SEAL IAW EMB135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030828000112003082800011WP 2003 8 28 ARWA20030313 120030315A5312 BULKHEAD DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, THE FOLLOWING WAS FOUND, RADOME BULKHEAD WEB LOWER SECTION WITH CRACKS, STA 44. CUT OUT DAMAGED AREA, FABRICATED STRAP AND FILLER IAW DC8 SRM 53-2-0, PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW DC8 SRM 53-2-0. 2L74 4F 4A25 20030828000132003082800013WP 2003 8 28 ARWA20030315 120030315A5320 STIFFENER DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR W/W STA 857 AND XCW51 PRESSURE BULKHEAD STIFFENER UPPER SECTION ANGLE WITH CRACK. DRILLED A STOP HOLE AT END OF CRACK IAW DC8 SRM 53-2-0, FABRICATED REINFORCEMENT IAW DC8 SRM 53-2-0, PRIMED REINFORCEMENT IAW DC8 SRM 51-1-8 AND INSTALLED REINFORCEMENT IAW DC8 SRM 51-1-21. 2L74 4F 4A25 20030828000192003082800019WP 2003 8 28 0379001 220030626A7261 WARNING SYSTEM AMD FALC2020F5 2730105EU GARRTTTFE731TFE7315BR WP COCKPIT ACTIVATED E ERYAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07892SB 379 98159 NR 1 (LT) ENGINE N2 INDICATOR AD OIL PRESSURE FLUCTUATED, THEN LOW PRESSURE LIGHT ILLUMINATED. SHUT NR 1 (LT) ENGINE DOWN AND RETURNED TO BASE (KFOB). FOUND AFTER TEARDOWN NR 4 BEARING FAILURE. END OF REPORT. 2L72 4F4 FRTA7EU E6WE 20030828000482003082800048EU 2003 8 28 XNOA01134 120030617A3097 WIRE AIRBUS300 A300B4203 3930306EU COCKPIT BURNED A XN0AD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23371PC 157 STRONG ELECTRICAL OVERHEAT SMELL IN COCKPIT. NO SMOKE OR MWP INDICATIONS. DURING TROUBLESHOOTING OF ELECTRICAL SMELL FOUND F/O'S LATERAL WINDOW HEAT WIRING BURNT. NO OTHER DEFECTS NOTED IAW CHAPT 30-00. 2L72 4F RTA35EU 20030828000532003082800053NE 2003 8 28 P5CA0300895 220030703A7320R4101 ACTUATOR BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE MALFUNCTIONED A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23923FT 22769 702193 NR 2 ENGINE FAILED TO START (NO FUEL) AFTER SECOND ATTEMPT. PRESSURE CHECKED FUEL PUMP IAW MM 71-00-00. REMOVED FUEL CONDITION ACTUATOR CHECKED SHAFT. REINSTALLED FUEL CONDITION ACTUATOR ENG RUN/ OPS CK 2L74 4F4 FRTA20WE E3NE 20030828000542003082800054NM 2003 8 28 P5CA0300896 120030603A8010713723 COUPLING BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE SHEARED A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23922FT 22768 702269 NR N2 INDICATION ON NR 3 ENGINE, DURING START - ENGINE DID NOT START PYLON AND START VALVE LIGHTS SHOW AIR PRESS TO STARTER BUT NO ROTATION. REMOVED AND REPLACED PNUEMATIC STARTER ALSO COUPLING WAS SHEARED. 2L74 4F4 FRTA20WE E3NE 20030828000692003082800069NM 2003 8 28 DL738030628 120030711A7110 SHROUD BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO273754A5850 29626 888486 ON L/O FOUND SMALL PIECE OF ABRADABLE SHROUD ON NR 1 ENGINE DAMAGED LOCATED 11 OCLOCK POSITION AS VIEWED FROM FRONT 1 OCLOCK AS VIEWED FROM AFT - REPAIRED SAME 2L72 4F4 FRTA16WE E00055EN 20030828000722003082800072NM 2003 8 28 DL76S030648 120030712A5753113T12121 SUPPORT BEAM BOEING767 767332 1382001NM T/E FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27119DL 23278 WING / LT / INBD FLAP / INBD SUPPORT BEAM / SUPPORT NR 4 : FLAP ATTACH HOLE CORROSION THE LT INBD FLAP INBD SUPPORT BEAM WAS FOUND WITH CORROSION IN THE AFT INBD AND AFT OUTBD ATTACH LUG HOLES. THE HOLES WERE REAMED TO REMOVE CORROSION, HFEC INSPECTED, OVERSIZED, AND ALUMINUM BUSHINGS INSTALLED TO RESTORE THE AREA. THE REPAIR WAS ACCOMPLISHED IAW ER/A 385379-14. 2L72 4F RTA1NM 20030828000862003082800086NM 2003 8 28 DL76S030684 120030722A5753113T122622 BEAM BOEING767 767332 1382001NM T/E FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27128DL 24078 DURING REPLACEMENT OF BOLTS IAW AD 2003-11-16, CORROSION WAS FOUND IN THE BORES OF THE RH WING INBOARD FLAP, OUTBOARD ATTACH FITTING. 3 OF THE 4 AFT ATTACH LOCATIONS WERE CORRODED IN THE 9-10 BEAM ASSEMBLY. THE HOLES WERE OVERSIZED TO REMOVE THE CORROSION, FREEZE PLUGGED, AND THE MODIFICATION CONTINUED WITHOUT DEVIATION. BOEING APPROVED THE SUBJECT REPAIR VIA 8110-3 FORM. 2L72 4F RTA1NM 20030828000872003082800087NM 2003 8 28 DL76G030696 120030725A5411311T21112 SPAR BOEING767 7673P6 1385105NM GE CF6 CF680 30025NE NR 1 NACELLE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27154DL 25241 PYLON, NR 1 FWD UPPER SPAR WEB, POWER FEEDER CABLE CUTOUT CRACKS. TWO CRACKS WERE FOUND IN THE UPPER SPAR WEB FROM THE POWER FEEDER CUTOUT TO THE NUTPLATE ATTACH HOLES. ERA INSTALLED REPAIR DOUBLER AND FILLER PER S/B 767-54-0090._ERA 385462-14 REVISION ORIGINAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F4 FRTA1NM E13NE 20030828000932003082800093NM 2003 8 28 DLM88030686 120030722A32225920602511N1 STRUT DOUG MD88 MD88 3023688NM NLG LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27912DL 49543 ON TAKEOFF NOSE LANDING GEAR REMAINED EXTENDED, RED NOSE GEAR LIGHT ON. CA:REPLACING NOSE GEAR STRUT ASSY. REPLACED NOSE GEAR INNER CYLINDER AND PACKINGS. 2L72 4F RTA6WE 20030828001002003082800100WP 2003 8 28 MWEA030330 120030825A361012J82350 CLAMP DOUG DC9 DC981 3022081WP A/C BAY LEAKING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31814ME 48010 TAIL COMPARTMENT TEMPERATURE LIGHT CAME ON. REMOVED AND REPLACED AUGMENTATION VALVE OUTBOARD DUCT CLAMPS. 2L72 4F A6WE 20030828001012003082800101WP 2003 8 28 MWEA030306 120030810A3241 BRAKE DOUG DC9 DC982 3022082WP AUTO BRAKES MALFUNCTIONED A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31809ME 48071 THE AUTO-BRAKE SYSTEM WOULD NOT ARM. PERFORMED AUTO BRAKE SYSTEM CONTROL UNIT SELF-TEST AND AIRCRAFT SYSTEM CHECK-OUT. NO DEFECTS NOTED. 2L72 4F A6WE 20030828001032003082800103NM 2003 8 28 MWEA030322 120030821A532299365357 SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 NR 2 GALLEY FORWARD INBOARD SUPPORT CORRODED AT STATION 218 10 INCHES RIGHT OF AIRCRAFT CENTER LINE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F RTA6WE 20030828001112003082800111NM 2003 8 28 MWEA030323 120030821A5347593056627 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 MODERATE CORROSION ON NR 6 SEAT TRACK AT FRAME STATION 1293. FABRICATED AND INSTALLED PLUG. 2L72 4F RTA6WE 20030828001182003082800118WP 2003 8 28 MWEA030292 120030728A523059101419 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 CARGO DOOR HAS A CRACK ON THE INNER PAN AFT FLANGE BY THE LATCH. FABRICATED AND INSTALLED REPAIR. 2L72 4F A6WE 20030828001222003082800122WP 2003 8 28 MWEA030304 120030802A21701808492 COALESCER BAG DOUG DC9 DC981 3022081WP A/C BAY DIRTY A MWEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31812ME 48006 FLIGHT ATTENDANT REPORTED A ELECTRICAL SMELL. VERIFIED AN EXTREMELY LARGE AMOUNT OF INSECT CARCASSES COVERING THE ENTIRE AIRCRAFT REMOVED, FOUND COALESCER BAGS DIRTY, CLEANED. RAN BOTH ENGINES THROUGH ALL POWER PHASES WITH AND WITHOUT AIR CONDITIOING, NO ABNORMALITIES. THE STRANGE SMELL WAS NOT REPLICATED AT ANYTIME.OK FOR SERVICE. 2L72 4F A6WE 20030828001242003082800124 2003 8 28 MWEA030303 420030801A34189650041027 COMPUTER DOUG DC9 DC932 3022066WP COCKPIT MALFUNCTIONED A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31207ME 47794 STALL INDICATION FAILURE ANNUCIATOR COMES OFF AND ON. REMOVED AND REPLACED STALL WARNING COMPUTER. 2L72 4F A6WE 20030827001692003082700169SO 2003 8 27 C2XA03SH295 120030827A531014522480003 DOOR FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE CARGO DOOR CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030827001822003082700182SO 2003 8 27 C2XA03TY138 120030820A255014526333401 TRIM PANEL EMB 145 EMB145LR 3260212SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED 2C INSPECTIONTHE AREA UNDER THE BAGGAGE DOOR LOWER TRIM PIECE SHOWS SIGNS OF CORROSION. MAINT R&R THE CARGO DOORWAY LOWER BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030827001832003082700183SO 2003 8 27 C2XA03IA084 120030815A3260D3899926FA98SN CONNECTOR EMB 145 EMB145LR 3260212SO LT MLG DAMAGED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2715910 145455 EWR - FLT NR 2685 - CREW REPORTED THAT DURING CLIMB THE LANDING GEAR WOULD NOT RETRACT WITH AN AIR/GRD FAIL MESSAGE. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT MAIN LANDING WEIGHT ON WHEELS CONNECTOR TO BE DAMAGED. THE AFFECTED CONNECTOR WAS REMOVED AND REPLACED, THE GEAR OPERATIONALLY CHECKED, AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030828000062003082800006CE 2003 8 28 51894 120030624A7603 CONTROL ROD BEECH 1900 1900D 1154162CE RIGHT OUT OF POSITION A AMWAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE073199Q UE213 ON FLIGHT 5445 FROM PANAMA CITY FLORIDA TO TAMPA FLORIDA, DURING TAKEOFF ROLL THE RIGHT POWER LEVER WAS STUCK. THE AIRCRAFT DID NOT MAKE TAKEOFF TORQUE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REPOSITIONED THE CONTROL ROD. NO PARTS WERE USED. THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030828000162003082800016NM 2003 8 28 C8GA20030018 120030620A5754 BEARING BOEING727 727223 1384074NM L/E SLAT SEIZED A C8GAJA DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO15899AA 22015 FLT 231 FROM MIA TO PTY. AFTER TAKEOFF, NR 2 SLAT DID NOT RETRACT. CYCLED SYSTEM TWICE STILLS NO RETRACTION. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NR 2 LEADING EDGE SLAT ACTUATOR WAS REPLACED. PERFORMED TEST FLIGHT AND WAS UNSUCCESSFUL. UPON FURTHER INSPECTION, FOUND THE FORWARD ROLLER TRACK BEARING SEIZED INBOARD AND OUTBOARD. REPLACED AND LUBED NR 2 SLAT BEARINGS AND NR 2 SLAT. ALL OPERATIONAL WORK CHECKS NORMAL IAW MM 27-81-11 AND 27-81-32. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030828000402003082800040WP 2003 8 28 FRISBY03002 120030416A291041022021 HOUSING DOUG DC9 DC987 3022087WP HYD SYSTEM CRACKED B UFHRK NONE K FLUID LOSS APAPPROACH 1 SO05OELMK9532 707 49411 DURING APPROACH, HYD PRESSURE OF BOTH HYD SYSTEMS DECREASED TO 0 PSI. UNEVENTFUL LANDING. BOTH SYSTEMS HAD BEEN SELECTED TO HIGH, AUXILIARY PUMP & PTU. DUE TO LANDING WITH OPEN LANDING GEAR DOORS, DOOR BUMPERS & DOOR STRUCTURE DAMAGED. AFTER LANDING, PTU WAS SELECTED OFF, HYD PRESSURE RECOVERED. WHEN PTU WAS SELECTED TO ON, HYD PRESSURE DECREASED AGAIN. INSPECTION OF PTU, P/N 4100310-6, S/N 707C, REVEALED DRAIN PORT HOUSING, P/N 4102202-1, CRACKED. PTU HAD ACCUMULATED 9,532 HRS & 6,724 CYCLES. AUSTRIAN AIRLINES/SR TECH ACCOMPLISHED FAILURE INVESTIGATION, FORWARDED FAILED DRAIN PORT HOUSING TO FRISBY AEROSPACE FOR ANALYSIS. PTU & DRAIN PORT HOUSING SUBJECT OF PREVIOUS S/B 4100310-29-0031 (AD 94-22-03). 2L72 4F RTA6WE 20030828000412003082800041NM 2003 8 28 XNOA01131 120030607A5610 WINDOW BOEING727 727227 1384078NM R1 CRACKED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL2379754 21363 R-1 WINDOW CRACKED. REMOVED AND REPLACED R-1 WINDOW AS REQ IAW 727 MM 56-11-11. 2L73 4F A3WE 20030828000742003082800074NM 2003 8 28 DL777030654 120030715A2520 ODOR BOEING777 777232 1385232NM CABIN DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27862DA 29734 IR-0515/16JUL/CDG/ 534841 - AT 11000 ON DESCENT FLIGHT ATTENDANTS REPORTED THE ODOR OF SMOKE /HEAT IN THE AREA OF 2 R. IT LASTED FOR APPROX 1 MINUTE. ENGINE HEAT WAS ON AT THE TIME AND WE WERE PENETRATING A RAIN SHOWER. CA-INSPECTION OF DOOR 2 R AREA PERFORMED WITH LIGHTS ON AND A/C ON. FOUND NO EVIDENCE OF ELECTRICAL BURN OR A/C OVERHEAT. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTT00001SE 20030828000782003082800078NM 2003 8 28 DL73S030665 120030718A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 FUSELAGE SKIN STA 663, S2R TO S1 - MISALIGNMENT: DURING INSPECTION OF THE FS 663 FRAME, MTC FOUND CRACKS IN THE FRAME AT S2R AND S1R. THESE WERE WITHIN THE AREA ADDRESSED BY B737-200 SRM 53-10-4, FIG 14. DURING INSTALLATION OF SRM FRAME REPAIR, SKIN ATTACH FASTENERS NEEDED TO BE RELOCATED THROUGH THE SKIN. THEY WERE CUTOUT IN THE SKIN AND DOUBLER, AND AN EXTERNAL DOUBLER AND TRIPLER WERE INSTALLED IAW DAL ER/A 385226-14. 2L72 4F RTA16WE 20030828000912003082800091NM 2003 8 28 DL76G030606 120030703A7920 TUBE BOEING767 767324 1385203NM GE CF6 CF680 30025NE NR 2 ENGINE LOOSE A DALAE ENGINE SHUTDOWN K FLUID LOSS TOTAKEOFF 1 SO27394DL14157 27394 ON DEPARTURE, RIGHT ENGINE OIL PRESSURE AND QTY WENT TO ZERO. FOUND SHROUD B-NUT ON NBR 6 BEARING SCAV SUPPLY TUBE LOOSE - SECURED SAME - LIMITS FOR LOSS OF OIL PSI NOT EXCEEDED IAW PIREP AND MTC OBSERVANCE - C/W REQD INSPN IAW AMM 72-00-00- LK AND OPS CK GD ETOPS CATEGORY 'B': DIVERSION OR TURNBACK. 2L72 4F4 FRTA1NM E13NE 20030828001042003082800104NM 2003 8 28 MWEA030324 120030822A5320993061225 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CORROSION FOUND JUST AFT OF FRAME STATION 1060 OUTBOARD OF RIGHT SEAT TRACK. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030828001152003082800115WP 2003 8 28 MWEA030279 120030715A5313592480289 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LONGERON 16 LEFT IS CRACKED ON BACK SIDE OF HAT SECTION AT STATION 313. FABRICATED AND INSTALLED NEW LONGERON. 2L72 4F A6WE 20030828001162003082800116WP 2003 8 28 MWEA030280 120030715A533059102285 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 TWO CRACKS IN FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERON 3&4 RIGHT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F A6WE 20030828001312003082800131WP 2003 8 28 MWEA030299 120030729A5310SRO95200089 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 MID CARGO LOWER DOOR JAMB HAS LIGHT CORROSION ON REPAIR DOUBLER AROUND SCREW HOLES AT STATION 644-685. FABRICATED AND INSTALLED NEW REPAIR DOUBLER. 2L72 4F A6WE 20040224000832004022400083WP 2004 2 24 GKZR200479907 120031108A5321 FLOOR PANEL DOUG DC8 DC862 3021970WP FUSELAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 AFT PASS AREA AT STA 1480 FLOOR PANEL SUPPORT CORRODED UNDER FLOOR PLANK. FABRICATED DOUBLER FROM .063 7075T6 IAW DC8 SRM 53-2-3, TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 53-2-3. 2L74 4F 4A25 20040226000142004022600014WP 2004 2 26 ASAA0380427 120030506A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT MALFUNCTIONED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SAN - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS REMAINED ON WITH POWER SWITCH OFF. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040225001642004022500164NM 2004 2 25 DL73S031132 120031224A5730655212156 SKIN BOEING737 737232 1384475NM RT WING DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 DAMAGE FOUND ON LOWER SKIN PANEL OF RIGHT WING AT STA 525 NEAR OUTBOARD TIP. REPAIRED PER ERA 426849-14. 2L72 4F RTA16WE 20040226000122004022600012WP 2004 2 26 ASAA0380415 120030428A3350 WIRE GULTON DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTORS AND REPLACED A COUPLE OF DAMAGED WIRE SEGMENTS. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040226000182004022600018NM 2004 2 26 ASAA0370008 120030408A5320146A75036 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01607AS 29751 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT RAIL. REPLACED FLOOR SUPPORT RAIL PER SRM. (M) 2L72 4F RTA16WE 20040226000252004022600025NM 2004 2 26 ASAA0240164 120030322A532069434961 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 847-867. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030716001002003071600100NE 2003 7 16 HEEA087969 120030619A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 EXTERNAL DOUBLER HAS A CRACK ACROSS THE SCREW HOLE AND THE LOWER INTERNAL DOUBLER SEPERATED. 1G72 3U H1NE 20030717000462003071700046SW 2003 7 17 HEEA088022 120030626A5630407706301105 WINDOW BELL 407 407 1182206SW PAX DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 LT AFT DOOR WINDOW CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000812003071700081SW 2003 7 17 HEEA088073 120030708A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L625 51529 DROPS DOWN TO 12 VOLTS DURING STARTS. NO AMPERAGE POWER. CAUSES AIRCRAFT TO HAVE SLUGGISH STARTS. SHOP REPAIR. 1G71 3U H2SW 20030718000212003071800021WP 2003 7 18 GTIA030473 120030613A3397 TERMINAL DOUG DC9 DC981 3022081WP EMERGENCY LIGHTSSHORTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND OVERHEAD EMERGENCY LIGHT AT SEAT 31 SHORTED. TROUBLESHOT EMERGENCY LIGHTS AND FOUND LOOSE TERMINAL AT LIGHT FIXTURE. TIGHTENED LOOSE TERMINAL. (M) 2L72 4F A6WE 20030721001142003072100114EU 2003 7 21 AUS20030619 220030615A7200 THROTTLE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU ENGINE FAULTY W O OTHER E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) NR 1 ENGINE AUTO-THROTTLE DISENGAGED AND SUBSEQUENTLY RE-ENGAGED. ENGINE PARAMETERS FLUCTUATED FROM 70 PERCENT N1 TO APPROXIMATELY 107 PERCENT N1 WITH WARNING LIGHT ILLUMINATION. 2L72 4F4 FRTA16WE E21EU 20030721001172003072100117NM 2003 7 21 SWAA031434 120030629A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C, ABOVE STR 15L. REPAIRED SKIN AT PAE DURING D-CHECK PER BFG ER. 2L72 4F RTA16WE 20030721001252003072100125NM 2003 7 21 SWAA031489 120030706A575465C26601180 SKIN BOEING737 7373TO 138447GNM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM. 2L72 4F RTA16WE 20030721001312003072100131 2003 7 21 SWAA031514 420030709A256565C19901 CABLE BOEING737 7372H4 138448CNM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030721001382003072100138 2003 7 21 SWAA031451 420030630A2565D31354 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030903002292003090300229EA 2003 9 3 03225629 120030813A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27629BR 7251 DURING MAINTENANCE INSPECTION THE RT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030902001212003090200121NE 2003 9 2 52223 220030703A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT DAMAGED A AMWAEC ENGINE SHUTDOWN ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE07159YV UE159 ON FLIGHT 6848, ON POWER UP FOR TAKEOFF THE LT ENGINE BEGAN TO SHAKE AND MAKE NOISES. THE CREW SHUT THE ENGINE DOWN AND RETURNED TO GATE WITH NO FURTHER INCIDENT. UPON RETURN TO GATE, MAINTENANCE INSPECTED THE LEFT ENGINE. THE PROP WOULD NOT TURN AND DAMAGE WAS FOUND ON EXHAUST STACKS FROM EXITING PARTS. THERE WAS NO INDICATION OF FIRE OR FLUID LEAKAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. MORE INFORMAITON WILL BE AVAILABLE AT A LATER DATE. 2L72 4T4 TRTA24CE E26NE 20030903000372003090300037NM 2003 9 3 03FDEA01003 120030627A5510NLC6725 STABILIZER DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT HORIZONTAL STABILIZER NR 36 BARREL NUT BORE FOUND WITH CORROSION ON BEARING, SIDEWALL AND BOTTOM SURFACE. BOTTOM SURFACE BLEND OUT CORROSION UP TO MAXIMUM LIMIT CORROSION STILL PRESENT. CORROSION ON LT HORIZONTAL STABILIZER NR 36 BARREL NUT BORE REMOVED AND REPAIR CARRIED OUT IAW EA 1-5510-69391. 2L73 4F RTA22WE 20030903000482003090300048WP 2003 9 3 0301289916 120030623A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01949N 47566 DURING (L) CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 BETWEEN LBL 16 TO 22. REPAIRED IAW EA 99-191008. 2L72 4F A6WE 20030903000882003090300088EA 2003 9 3 A6WA200340121 120030815A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 FOUND LEFT FS 625 STRINGER 14 OBLIQUE ANGLE, P/N 601-35012-51, IS CRACKED APPROX 2 INCHES. (M) 2L72 4F RTA21EA 20030903002332003090300233EA 2003 9 3 03210656 120030729A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27656BR 7485 DURING MAINTENANCE INSPECTION THE LT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030903002462003090300246EU 2003 9 3 03231330 120030819A335016011011 HOUSING JETAIRJETSTMJETSTM4101 1500501EU CABIN FAULTY A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 DURING MAINTENANCE INSPECTION THE LT FWD EMERGENCY LIGHT WAS FOUND INTERMITENTLY WORKING. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT HOUSING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AN AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. DCN#146389-1 2L72 4T RTA41NM 20030903002572003090300257SO 2003 9 3 C2XA03IA087 120030830A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712567 145623 IAH- DURING SERVICE CHECK THE MECHNIC NOTED THAT THE GALLEY EMERGENCY EXIT LIGHT WOULDN'T ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030903002612003090300261SO 2003 9 3 C2XA03SH310 120030829A711014576010001 RIB EMB 145 EMB145ER 3260211SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE AFT RIB ON THE UPPER RIGHT COWLING WAS FOUND TO BE CHAFFED AT THE CENTER LINE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030903002632003090300263SO 2003 9 3 C2XA03SH309 120030829A532014521721009 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AT FR 15-17. MAINTENANCE REMOVED DAMAGED SECTION AND REPLACED FORWARD DIGITAL BUTTSTRAP AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030904000042003090400004EA 2003 9 4 SWIA200312153 120030625A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 589 LBL 42 TRANSVERSE BEAM ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601R-35011-11 2L72 4F RTA21EA 20030904000082003090400008NE 2003 9 4 UPS03440947 220030707A7200JT97Q ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7Q 52054NE NR 3 FAILED A IPXAE ENGINE SHUTDOWN XRJENGINE FLAMEOUT PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO01526UP 21937 NR 3 ENGINE SHUTDOWN 56 MIN. AFTER TAKEOFF, ICE LIGHT CAME ON,FUEL HEAT APPLIED AND ICING LIGHT STAYED ON.OIL TEMP INCREASED TO 140 DEGREES AFTER 5 MINUTES EPR,N1 AND N2 ROLLED BACK AND ENG. DID NOT RESPOND. ENGINE SHUTDOWN . FOUND METAL IN TAILPIPE AND FUEL PUMP CRACKED. REMOVED AND REPLACED ENGINE. 2L74 4F4 F A20WE E3NE 20030904000112003090400011EU 2003 9 4 AWXA200300775 120030704A3251C2473600001 SERVO VALVE AIRBUS320 A320231 3930325EU NLG STEERING FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28622AW7736 7728 054 ON TAKEOFF PILOT REPORTED A NOSE WHEEL STEERING FAULT. AIRCRAFT PROCEEDED AFTER WHICH AN UNEVENTFUL LANDING OCCURED. AIRCRAFT TAXIED TO GATE UNDER ITS OWN POWER. MECHANIC PERFORMED BSCU BITE CHECKS THAT IDENTIFIED FAULT CODE 4E. REMOVED AND REPLACED THE NOSE LANDING GEAR SERVO CONTROL VALVE IAW AMM 32-51-51-04. OPERATIONAL AND LEAK CHECK WERE GOOD. VENDOR BENCH TEST OF NOSE LANDING GEAR SERVO CONTROL VALVE S/N M075 COULD NOT CONFIRM REASON FOR REMOVAL (NFF). UNIT WAS TESTED, INSPECTED, AND RETURNED TO SERVICE IAW CMM 32-57-01. 2L72 4F RTA28NM 20030904000152003090400015WP 2003 9 4 ARWA20030702 120030707A5330 SKIN DOUG DC8 DC862 3021970WP MLG DOOR CUTOUT CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198974U 46110 NR 34M. DURING "A" CHECK NON-ROUTINE INSPECTION, THE FOLLOWING WAS FOUND- NLG WW LT SIDE, STA. 208 L-33L CORNER WITH .2500 INCH CRACK. TRIMMED OUT CRACK ON EDGE OF NOSE SKIN AT NOSE LANDING GEAR DOOR LEFT AFT CORNER AND FABRICATED FILLER FROM 707STG.O50 AND DOUBLER FROM 707STG-063 IAW AVITAS ENGINEERING REPAIR ORDER AROW-033RO-1, INITIAL RELEASE, DATED 07/08/03, PAGE 1 TO 2, AND REPAIR SKETCH AIPSAC-N8974U-01/03, SHEET 1 TO 4, DATED 07/02/03. PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW AVITAS ENGINEERING REPAIR ORDER AROW-033RO-1, AND REPAIR SKETCH AIPSAC-N8974U-01/03. ISSUED FAA FORM 8110-3 DATED 07/08/03. 2L74 4F 4A25 20030904000162003090400016CE 2003 9 4 DXTA200300063 120030707A3297 WIRE CESSNA500 560CESSNA 2076750CE A/S TRANSDUCER BROKEN E DXTAO OTHER N FALSE WARNING LDLANDING 1 GL07336QS 5600336 BRAKES FAILED UPON TOUCHDOWN DEPLOYED EMERGENCY BRAKING SYSTEM. BLED BRAKE SYSTEM, TROUBLESHOT TO BROKEN WIRES ON THE ANTI-SKID TRANSDUCER. REPAIRED WIRING, PERFORMED OPERATIONAL CHECK AND TAXI CHECK OF THE BRAKE SYSTEM, CHECKED GOOD. ALL WORK DONE IAW CESSNA CE 560 MM CHAPTER 32-42-00 AND CHAPTER 32-40-01 OF THE CE560 WIRING DIAGRAM MM. 2L72 4F RTA22CE 20030904000302003090400030EA 2003 9 4 SWIA200312328 120030817A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 DISCOVERED DURING C-CHECK, FS 280 LT FLOORBEAM LBL 9.0 OB ATTACH ANGLE CRACKED. ANGLE REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-57 2L72 4F RTA21EA 20030904000422003090400042EA 2003 9 4 SWIA200312279 120030710A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.0, LBL 38.0. DISCOVERED DURING C-CHECK, REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV ''A''. ANGLE P/N: 601R-53-61-117-1 2L72 4F RTA21EA 20030904000452003090400045EA 2003 9 4 SWIA200312330 120030817A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 PAX DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK. PAX DOOR OUTER HANDLE REPLACED IAW CRJ MM 52-11-03-000-802 AND 52-11-03-400-802. 2L72 4F RTA21EA 20030904000532003090400053EA 2003 9 4 SWIA200312259 120030809A2760 ECU CNDAIRCL600 CL6002B19 1900309EA NR 1 FAULTY A SWIAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM07433SW 7550 OUTBOARD GROUND SPOILER STATUS MESSAGE. REPLACED SECU NR 1. OPS CHECKS GOOD IAW CRJ MM 27-61-05. 2L72 4F RTA21EA 20030904000592003090400059EA 2003 9 4 SWIA200312340 120030825A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FS 280 RT FLOORBEAM RBL 9.0 INBD AND OB ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00. P/N: 601R31113-58 2L72 4F RTA21EA 20030904000622003090400062EA 2003 9 4 SWIA200312302 120030822A2751601R930301 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER N FALSE WARNING UKUNKNOWN 1 NM07587SW 7062 WITH FLAPS SELECTED AT 20, LEFT FLAP PANEL INDICATES 20 DEGREES, RIGHT SIDE INDICATES 18 DEGREES. WITH FLAPS SELECTED AT 30, LEFT SIDE INDICATES 30 DEGREES AND RIGHT SIDE INDICATES 28 DEGREES. ALL OTHER FLAP SELECTOR POSITIONS INDICATE NORMAL. REMOVED AND REPLACED RIGHT SIDE FLAP TRANSMITTER. OPERATIONAL CHECK IS OK IAW MM 27-55-00. PN OFF: 601R93030-1 2L72 4F RTA21EA 20030904000642003090400064 2003 9 4 SWIA200312304 420030822A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER O OTHER UKUNKNOWN 1 NM07234SW7346 7346 120308 CAPT REPORTS A/P WILL NOT CAPTURE ALTITUDE AS GIVEN ON THE ALT ALERTER. REPLACED ELEVATOR SVO65 SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030904000682003090400068EA 2003 9 4 SWIA200312246 120030809A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07939SW 7742 RETURN TO GATE WITH LEFT SPOILER ON STATUS MESSAGE. REMOVED AND REPLACED LEFT OUTBOARD SPOILER ON PCU WITH SERVICEABLE UNIT. OPS AND LEAK CHECK GOOD IAW CRJ MM 27-62-01. 2L72 4F RTA21EA 20030904000772003090400077NM 2003 9 4 QXEA200300959 120030807A5210D5D592395926 SPRING DHAV DHC8 DHC8202 2809007NM PAX DOOR DEFECTIVE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09359PH1415 1415 514 PDX- ON FLIGHT 2223 MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. REMOVED AND REPLACED BOTH GAS SPRINGS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903000492003090300049NE 2003 9 3 C1HA200381015 220030710A7261 SCAVENGE PUMP BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 ENGINE FAILED A C1HAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 GL15681CA 22020 DURING TAXI OUT TOWER ADVISED NR 2 ENGINE SMOKING EXCESSIVLY ALSO NOTED NR 2 OIL QTY DECREASING BELOW 1 GAL-FOUND NR 6 SCAVAGE PUMP BAD. REMOVED AND REPLACED ENGINE. 2L73 4F4 F A3WE E2EA 20030903001252003090300125EA 2003 9 3 2003F00532 120030805A57302113C1 SKIN CNDAIRCL600 CL6002B16 1900305EA RT WING LIGHTNING STRIKEA O2GAK NONE O OTHER ININSP/MAINT 1 NE03601VH 5043 DURING A POST FLIGHT INSPECTION, FOUND EVIDENCE OF AN APPARENT LIGHTNING STRIKE ON THE TRAILING EDGE OF RIGHT WING TIP, BELOW THE WINGLET. AS PER REO 601-57-20-036, ALUMINUM TAPE APPLIED TO DAMAGED AREA. AIRCRAFT TO BE REPOSITION FROM PBI TO AGS FOR FURTHER EVALUATION. (M) 2L72 4F RTA21EA 20030903001342003090300134CE 2003 9 3 ESE2003F0000A 120030411A2731505244749 TUBE BEECH 90 C90A 1152911CE ELEVATOR TRIM SHEARED B ESERO OTHER O OTHER NRNOT REPORTED 1 SO1195PC LJ1109 THE RT ELEVATOR TRIM CONTROL ROD CLEVIS, BOLT AND BUSHING SEIZED DUE TO CORROSION AND LACK OF LUBRICATION CAUSING THE CONTROL ROD THREADED ROD TO SHEAR. 1L72 3T RT3A20 20030903002432003090300243EA 2003 9 3 03238623 120030826A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27623BR 7192 DURING MAINTENANCE INSPECTION THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTIUED SERVICE 2L72 4F RTA21EA 20030904000092003090400009NE 2003 9 4 DXTA200300059 220030706A7261 SOLENOID BRAERO1000 HAWKER1000 7450005EU PWA 305 PW305B 52128NE LT ENGINE FAILED E DXTAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 GL07546QS 259046 PCE305064 AFTER STARTED TAXIING, HEARD POPPING NOISE FROM LT ENGINE, ITT RAPIDLY CLIMBED TO 710 DEGREES OIL 1 LOW PRESSURE CAME ON, SHUTDOWN THE LEFT ENGINE. REMOVED & REPLACED THE 3 O’CLOCK AND 9 O’CLOCK 2.8, 2.5 BOV’S AND BOV SOLENOID IAW RAYTHEON HAWKER 1000 AMM CHAP 75-30-00. PERFORMED FUEL SAMPLE AND INSPECTED FUEL FILTER, ALL CHECKED GOOD. ACCOMPLISHED ENGINE RUN, OPS CHECKED GOOD IAW PWC 305 MM CHAPTER 71-00-00. 2L72 4F4 FRTA3EU E35NE 20030904000672003090400067NE 2003 9 4 SWIA200312261 220030817A73203035659 HMU EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE NR 2 ENGINE MALFUNCTIONED A SWIAO OTHER Y ENGINE STOPPAGE TXTAXI/GRND HDL 1 NM0715732 120195 ON TAXI OUT, RT EEC LIGHT ON RESET AND WOULD NOT RESET. TWO MINUTES LATER, RIGHT GEN CAME OFF LINE. CONSULTED QRH, WOULD NOT RESET. ONE MINUTE LATER, NR 2 ENGINE FAILED, WOULD NOT FEATHER. ACTIVATED ELEC FEATHER. REMOVED AND REPLACED HMU FUEL CONTROL AND FUEL PUMP WITH SERVICEABLE UNIT IAW MM 73-13-00 AND 73-21-00. OPS AND LEAK CHECK GOOD. SN OFF M80569PN OFF 3117095-01 SN OFF 2137 2L72 4T4 TRTA31SO E20NE 20030904000902003090400090NM 2003 9 4 QXEA200300996 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GROOVED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 9 SEAT TRACK HAS A GROOVE IN THE LOWER SURFACE AT STATION X543.000. REPAIRED IAW DHC-8 RD 8-53-4936. 2H72 4T RTA13NM 20030904000922003090400092NM 2003 9 4 QXEA200300998 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GROOVED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 6 SEAT TRACK HAS A GROOVE IN THE LOWER TRACK SURFACE AT STATION 533.04. REPAIRED IAW DHC-8 RD 8-53-4936. 2H72 4T RTA13NM 20030904001032003090400103NM 2003 9 4 QXEA200301049 120030829A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09345PH 476 PDX- EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT SEAT ROW 7 AND 8. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904001102003090400110NM 2003 9 4 QXEA200301038 120030826A5210 ROLLER BOMBDRDHC8 DHC8401 1390041NM PAX DOOR LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09406QX 4048 PDX- AFT PASSENGER DOOR IS DIFFICULT TO OPERATE. CLEANED AND LUBRICATED DOOR SEAL AND ROLLERS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904001262003090400126NM 2003 9 4 DL733030611 120030703A3350 LIGHT BOEING737 737347 1384647NM CABIN INOPERATIVE A DALAK NONE O OTHER CRCRUISE 1 SO27303WA 23183 EMERGENCY LIGHTS INOP AT SEAT 2B OVERHEAD, AT 10D AND 14D. REPLACED OVERHEAD LIGHT ASSY AT 2B AND RELAMPED SEAT LIGHTS AT 10D & 14D CHECKS GOOD. 2L72 4F RTA16WE 20030904001312003090400131NM 2003 9 4 DL757030617 120030706A3350 LIGHT BOEING757 757232 1384965NM EXTERIOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27697DL 30318 ON LAYOVER CHECK FOUND 1R EMERGENCY DOOR OUTSIDE LIGHT INOP. RELAMPED SAME CHECKS OK. 2L72 4F RTA2NM 20030904001362003090400136 2003 9 4 DL733030626 420030710A3441HG1050AD05 IRU BOEING737 737347 1384647NM LEFT FAULTY A DALAK NONE I FLT. ATTITUDE INST. CRCRUISE 1 SO27312WA 23598 LOST LEFT IRU IN FLIGHT. UNABLE TO GET HEADING IN ATT. BOTH AUTOPILOTS INOP. REPLACED LEFT INERTIAL REFERENCE UNIT PER M/M. 2L72 4F RTA16WE 20030904001372003090400137NM 2003 9 4 DLM11030627 120030711A3411340701301 PITOT TUBE DOUG MD11 MD11 3023602NM PITOT/STATIC SYSDEFECTIVE A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27815DE 48624 MULTIPILE ERRONEOUS AIR DATA IND ON CAPT SIDE SW TO F/O CADC. CAPT PITOT PROBE BLOCKED BLOW OUT LINE BETWEEN ADC TO PROBE. REPLACED CAPT PITOT PROBE AND CADC LEAK CHECK AND OPS CHECKS OK 2L73 4F RTA22WE 20030904001492003090400149WP 2003 9 4 DHL2003873548 120030630A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 INTERIM REPAIR ON RT HORZ STAB INBD L/E AT STA XFS 178.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17. CLEANED, TREATED AND PRIMED INNER SIDE OF DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17, SRM 51-1-15 PG 1, SRM 51-1-21 PG 1. REFER TO JC BX3H55072 FOR RT HORZ STAB INBD L/E REMOVAL/INSTALLATION. 2L74 4F RT4A25 20030904001512003090400151WP 2003 9 4 DHL2003873570 120030627A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 A 0.500 INCH CRACK IN FWD UPPER CORNER SKIN OF D-CARGO DOOR JAMB AT STA 1400.000 L25R TO L26R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 21 PG 149-150. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG 21 PG 149-150. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER, DOUBLER AND TRIPLER IAW SRM 53-2-0 PG 149-150. CLEANED, TREATED AND PRIMED FILLER, DOUBLER AND TRIPLER IAW SRM 51-1-8B. INSTALLED FILLER, DOUBLER AND TRIPLER IAW SRM 53-2-0 PG 21, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1 (PRC). 2L74 4F RT4A25 20030904001732003090400173NE 2003 9 4 AALA20030779 220030716A73143843017 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RT ENGINE DEFECTIVE A AALAA UNSCHED LANDING KX FLUID LOSS ENGINE FLAMEOUT CLCLIMB 1 SW217528A 49920 ORD - FLT 1771 - EN ROUTE ORD-ELP, AFTER TAKEOFF PASSING 4000 FEET IN RIGHT TURN,RIGHT ENGINE FLAMED OUT. ACCOMPLISHED RESTART NORMALLY. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FUEL PUMP AND CONTROL PER MM. LEAK CHECKS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030904001852003090400185NE 2003 9 4 AALA20030649 220030610A732176960612 FUEL CONTROL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT ENGINE MALFUNCTIONED A AALAA UNSCHED LANDING JX WARNING INDICATION ENGINE FLAMEOUT CLCLIMB 1 SW21575AM 53152 LAX - FLT 237 - EN ROUTE LAX-SJD, DURING CLIMB-OUT, LEFT START VALVE OPEN LIGHT ILLUMINATED. CREW PREPARED TO SHUT DOWN ENGINE WHEN LEFT ENGINE FLAMED OUT. RETURNED LAX AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL CONTROL AND ENGINE FUEL PUMP. ACCOMPLISHED ENGINE RUN AND POWER ASSURANCE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030904001932003090400193WP 2003 9 4 AALA20030723 120030705A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21475AA 49650 SFO - EMERGENCY LIGHTS GO DIM AND THEN OFF IN FIVE SECONDS AT ROWS 22, 24, AND 26. RESEATED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904001952003090400195WP 2003 9 4 AALA20030677 120030622A3241392492 CONTROL VALVE DOUG DC9 DC982 3022082WP ANTI-SKID SYS LEAKING A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21218AA 49168 BOS - FLT 1201 - EN ROUTE BOS-DFW, DURING CLIMB-OUT, RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. RIGHT HYDRAULIC SYSTEM HAD TOTAL LOSS OF FLUID, UNABLE TO RETRACT LANDING GEAR. RETURNED BOS AND LANDED WITHOUT INCIDENT. REPLACED ANTI-SKID CONTROL VALVE. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP AND ELECT HYDRAULIC PUMP AS PRECAUTIONARY. REPLACED RIGHT ENGINE AND RIGHT HYDRAULIC SYSTEM FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904001962003090400196NM 2003 9 4 C1HA200394015 120030717A3350 LIGHT BOEING727 727290 138408WNM CABIN INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15294AS 22146 RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. 2L73 4F A3WE 20030905000252003090500025SO 2003 9 5 LR7A03070 120030725A5320 ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND RT MLG FS 528 VERTICAL BEAM ANGLE CRACKED AT RBL 71, WL 225. REPAIRED IAW SRM SMP 583 51-140-23. NR 2132. 2H74 4T A1SO 20030905000272003090500027SO 2003 9 5 LR7A03072 120030725A5320 ANGLE LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL FS 597 CHINE ANGLE CORRODED AT LBL 61, WL 143. REPAIRED IAW SRM SMP 583 53-40-27. NR 2151. 2H74 4T A1SO 20030903001732003090300173NM 2003 9 3 UIEA200300043 120030802A2751 TRANSMITTER BOEING747 7472D7B 1384803NM T/E FLAP LOOSE A UIEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15527MC 22471 TLV - ACCEPTANCE FLIGHT FROM C-CHECK AIR TURNBACK, AFTER TAKEOFF DURING FLAP RETRACTION INBOARD FLAPS STOPPED AT 19 DEGREES INDICATES FLAP ASYMMETRY. AIRCRAFT RETURNED TO TLV. NO FUEL DUMPED. FOUND RIGHT OUTBOARD FLAP TRANSMITTER LOOSE. TIGHTENED TRANSMITTER LOOSE. TIGHTENED TRANSMITTER AND ADJUSTED THE SYSTEM PER MM 27-50-00. CHECKED ALL SYSTEMS ON GROUND PER MM 27-58-00. FOUND OK. (M) 2L74 4F RTA20WE 20030903001752003090300175NM 2003 9 3 2003F00545 120030628A57546548422267 SKIN BOEING737 7372L9 1384497NM L/E SLAT DELAMINATED A KNNAK NONE O OTHER ININSP/MAINT 1 WP25465AT 21528 MSY-BNA - DURING POST REPOSITIONING FLIGHT INSPECTION, FLIGHT CREW OBSERVED UPPER SKIN DELAMINATION OF THE TRAILING EDGE NR 2 L/E SLAT, P/N 65-46422-267. A FOUR INCH SECTION OF THE UPPER SKIN HAD DELAMINATED THE ENTIRE LENGTH OF THE LE SLAT AND DEPARTED THE AIRCRAFT. DETAILED INSPECTION SHOWS NO FURTHER OR HIDDEN DAMAGE WITH THE WING OR ANY ASSOCIATED COMPONENTS. INSPECTION REVEALED THAT THE NR 3 LE SLAT WAS ALSO SPONGY AND BEGINNING TO DELAMINATE IN THE SAME AREA. INSPECTIONS OF NR 1, NR 4, NR 5 AND NR 6 SHOWED NO REJECTABLE DISCREPANCIES, P/N NR 3 LE SLAT 65-46423-9065. (M) 2L72 4F RTA16WE 20030903001892003090300189WP 2003 9 3 AALA20030733 120030709A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21471AA 49601 DFW - EMERGENCY LIGHT AT AFT GALLEY FLOOR JUST FORWARD OF DOOR IS INOPERATIVE. REPLACED BATTERY AND CHARGER MODULE. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030903002502003090300250EA 2003 9 3 03236659 120030824A3350364911 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27659BR 7509 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING IN ROW 1C WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY TRACK LIGHT AT ROW 1C. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030904000172003090400017WP 2003 9 4 ARWA20030703 120030708A2134 LINE DOUG DC8 DC863 302198AWP CABIN PRESSURE BROKEN A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19345JW 46042 ON CLIMB OUT HEARD LOUD NOISE AND CABIN CLIMBED, UNABLE TO MAINTAIN CABIN PRESSURE. ENTERED ON DMI NR 17926 IAW MEL 21-65 CAT "C" PLACARD INSTALLED. FOUND VENTURI SENSING LINE BROKEN. REMOVED AND REPLACED SENSING LINE IAW STC ST466CH; PERFORMED OPERATIONAL CHECK ON GROUND FOUND NORMAL IAW STC ST466CH. CLEARED DMI 17926. 2L74 4F 4A25 20030904000582003090400058EA 2003 9 4 SWIA200312339 120030825A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FS 280 LT FLOORBEAM LBL 9.0 OB ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00. REF. RII 53-401. P/N: 601R31113-57 2L72 4F RTA21EA 20030904000892003090400089NM 2003 9 4 QXEA200300995 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GROOVED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 4 SEAT TRACK HAS A GROOVE IN THE LOWER SURFACE AT STATION X531.00. REPAIRED IAW DHC-8 RD 8-53-4936. 2H72 4T RTA13NM 20030904001202003090400120EA 2003 9 4 COMA0360372 120030815A2760 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO01514CA 7809 FLIGHT 5060 FLIGHT SPOILER AND GROUND SPOILER FAULT MESSAGE. COULD NOT DUPLICATE. RESET SPOILER SYSTEM, OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20030904001322003090400132NM 2003 9 4 DL73S030618 120030707A3620 SENSE LINE BOEING737 737247 138448DNM LT ENGINE LOOSE A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27379DL 23606 A/C WOULD NOT PRESSURIZE DURING CLIMBOUT. POM PROCEDURE WERE FOLLOWED AS WELL AS MULTIPLE BLEED CONFIGURATIONS WERE TRIED INCLUDING USING APU BLEED AND STBY AND MANUAL AC/DC MODES ON CONTROLLER. MAIN AND FWD OUTFLOW VLVS WERE CLOSED. SECURED LOOSE SENSE LINE TO LEFT ENGINE BLEED. 2L72 4F A16WE 20030904001392003090400139NM 2003 9 4 AWXA200300784 120030613A5320654681812 WEB BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF CABIN FLOOR PANEL SIDE RAIL (SHEAR WEB) AT BS 618, RBL 64 WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF SHEAR WEB BS 600 TO BS 626, RBL 64; FABRICATED NEW REPLACEMENT SECTION OF SHEAR WEB AND 2 EACH SPLICES; INSTALLED REPAIR PARTS IAW ER 03-5322-03182-TB1. 2L72 4F RTA16WE 20030904001632003090400163WP 2003 9 4 DHL2003873580 120030704A53204753360502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT FITTING CRACKED 2.000 INCH STA 822.500 - STA 826.000, L-22L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030905000032003090500003SO 2003 9 5 LR7A03050 120030725A5320 BRACE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5315 FOUND RH AFT FUSELAGE FS 968 BRACE CRACKED AT RBL 20, WL 280. REPLACED BRACE IAW SRM SMP 583 51-60 AND 51-70. NR 2004. 2H74 4T A1SO 20030905000312003090500031SO 2003 9 5 LR7A03075 120030725A5320 CAP LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL FS 597 BEAM CAP CORRODED AT LBL 62, WL 150. REPAIRED IAW LAC MEA 382-53-03-056. NR 2150. 2H74 4T A1SO 20030905001082003090500108NM 2003 9 5 DL76L030634 120030711A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27179DN 25144 DURING ETOPS LAYOVER CHECK FOUND SEAT MOUNTED EMERGENCY LIGHT; SEATS21-30 LT AND RT SIDES INOP. FOUND POWER SUPPLY M9009, CONNECTOR D9047, POWER SUPPLY INOP. REMOVED AND REPLACED POWER SUPPLY. CHECKS GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030828001422003082800142NM 2003 8 28 BJNA030700 120030714A3350GE1691 LIGHT BOEING737 737282 13844ATNM CABIN INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT LOCATED BY THE LEFT AFT ENTRY DOOR EXTERIOR WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB IAW BOEING MM 33-51-0, SYSTEM NOW CHECKS NORMALLY. (M) 2L72 4F RTA16WE 20030828001512003082800151NE 2003 8 28 UIEA200300032 220030711A7200 ENGINE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 3 MALFUNCTIONED A UIEAJEA DUMP FUEL ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP TOTAKEOFF 1 EA15508MC 21644 455167 DURING TAKEOFF NR 3 ENGINE HAD EXCEEDANCE OF PEAK TEMPERTURE OF 994 DEGREES FOR A 91 SECOND DURATION. THRUST LEVER WAS RELATIVE TO THE SAME POSITION AS OTHERS. TAKEOFF N1 WAS 113.5 DUE TO EXCEEDING 990 DEGREES THE ENGNE WAS SHUT DOWN. APPROXIMATELY 23,000 KGS OF FUEL DUMPED EN ROUTE TO AMS. EGT OVERTEMP ALREADY ON DMI N03-029. PERFORMED VISUAL INSPECTION IAW MM 72-00-00 PAGE 680 FV. OPENED ENGINE COWLS AND VISUALLY INSPECTED COOLING DUCT ETC. ALL SATISFACTORY. ENGINE TO BE REPLACED AT JFK 7/12/03. REMOVED AND REPLACED NR 3 ENGINE PER ATLAS FORM 01-AA-45 AND ACCOMPLISHED ENGINE RUNS PER MM 71-00-00, TEST 1, 3, 8 AND 4. NIL LEAKS NOTED. (M) 2L74 4F4 F A20WE E23EA 20030828001582003082800158EU 2003 8 28 USAASA03087 120030809A3350321431 BATTERY AIRBUS320 A320214 3930316EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19102UW 0844 PHL - THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND DISCHARGED. MAINTENANCE REPLACED THE BATTERY ON THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030828001632003082800163NM 2003 8 28 USAASA03134 120030809A335020131A BATTERY PACK BOEING737 737301 1384611NM CABIN DISCHARGED A K NONE O OTHER ININSP/MAINT 1 EA19577US 23742 MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AROUND SEAT ROW 10ABC EXTINGUISHED AFTER 45 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE M1134 BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030828001712003082800171NM 2003 8 28 SWAA031866 120030819A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 312, BELOW 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030828001832003082800183NM 2003 8 28 CALA0300493 120030825A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 500D BETWEEN S26L AND S27L, LOWER AREA. THE CORRODED AREA WAS CUT OUT AND FILLER, DOUBLER AND A SHIM WERE INSTALLED IAW SRM 53-00-07, FIGURE 203 AND 204. 2L72 4F RTA16WE 20030828001852003082800185NM 2003 8 28 CALA0300495 120030825A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030829000102003082900010WP 2003 8 29 ARWA20030708 120030722A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPARTMENT STATION 1520, RBL 32 FLOORBEAM UPPER FLANGE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM UPPER AFT FLANGE AT STATION 1520 RBL 32 IAW AVITAS ENGINEERING ORDER AROW-034RO-1, PAGES 1 TO 2, INITAL RELEASED, DATED 07/23/03, AND REPAIR SKETCH AIPSAC-N802BN-001/03, SHEETS 1 TO 5, DATED 07/23/03 AND APPROVED BY FAA 8110-3 FORM, DATED 07/23/03 NRC 158M, ENGINEERING ASSISTANCE EA 1013, DATED 07/22/03. 2L74 4F 4A25 20030829000182003082900018NM 2003 8 29 CALA0300481 120030822A5514 BUSHING BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714645 28906 INSPECTION FOUND RT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR LOWER FORWARD LUG PITTED AT BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW CMM 55-10-06. 2L72 4F RTA16WE 20030829000192003082900019NM 2003 8 29 CALA0300452 120030807A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FLOORBEAM CORRODED AT BS 986.5, RT SIDE. A T-CAP WAS INSTALLED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030829000212003082900021NM 2003 8 29 CALA0300454 120030808A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FLOORBEAM NUT PLATE HOLE CORRODED AT FS 967, LBL 28. A REPAIR STRAP WAS INSTALLED IAW SRM 51-21-3. 2L72 4F RTA16WE 20030829000232003082900023NM 2003 8 29 CALA0300451 120030807A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND RT CABIN FLOOR Z-ANGLE CORRODED AT STA 947.5-1006. THE Z-ANGLE WAS REPLACED IAW SRM 51-00-02. 2L72 4F RTA16WE 20030829000342003082900034NM 2003 8 29 CALA0300498 120030826A5320 BRACKET BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND CORROSION ON CORNER BRACKET O/B OF DOOR CUTOUT RT AFT CORNER FWD ACC COMPT, STA 219. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030829000482003082900048WP 2003 8 29 DHL2003803012 120030719A2611327 LAMP DOUG DC8 DC873 302199CWP SMOKE DETECTOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01803DH 46123 DURING PREFLIGHT, DISCOVERED NR 14 SMOKE DETECTOR INOPERATIVE. MAYBE DEFERRED IAW MEL 26-6 DMI 13597 PLACARD INSTALLED. REF DMI 13597. DURING PREFLIGHT DISCOVERED NR 14 SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED BOTH BEACON AND TEST LAMP ON NR 14 SMOKE DETECTOR. CHECKED OPS OK IAW SMM 26-15-0. DMI 13597 CLEARED. 2L74 4F RT4A25 20030829000512003082900051WP 2003 8 29 DHL2003873535 120030628A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL CRACKED (1.000), STA 640 RBL 11. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030829000992003082900099 2003 8 29 2904070703 420030707A3425066304600 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT DEFECTIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP07894NA104 2904 9456 HSI WILL NOT SAVE TO GPS. 1G71 3U3 U H9EU E19EU 20030828000512003082800051 2003 8 28 P5CA0300913 420030817A344220414440404 DRIVE SYSTEM BOEING747 747341 13848AMNM NR 1 & 2 RADAR INOPERATIVE A P5CAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP23354MC 23394 NR 1 AND NR 2 RADAR ANT FAULT WX RADAR INOPERATIVE. REMOVED AND REPLACED WX RADAR ANTENNA DRIVE IAW MM 34-43-03. OPS CK AND FUCTION TEST SAT IS IAW MM 34-43-00. 2L74 4F RTA20WE 20030828001102003082800110NM 2003 8 28 MWEA030321 120030821A5320993023836 WEB DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 GALLEY SUB FLOOR IS CRACKED AT STATION 218 OUTBOARD OF NR 5 SEAT TRACK. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F RTA6WE 20030828001202003082800120WP 2003 8 28 MWEA030294 120030728A5730993681110 SKIN DOUG DC9 DC982 3022082WP RT WING CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 RIGHT WING APPEARS TO BE BURNT OR CORRODED NEAR NR 3 STATIC WICK ON LOWER WING SURFACE. FABRICATED AND INSTALLED NEW SKIN AND DOUBLER. 2L72 4F A6WE 20030828001992003082800199NM 2003 8 28 CALA0300478 120030822A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AND SHIM MISSING AT STA 540 BETWEEN LEFT I/B AND O/B SEAT TRACK. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030829000282003082900028NM 2003 8 29 CALA0300486 120030824A5720 CHANNEL BOEING737 7373T0 1384582NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND THE LT WING T/E NR 3 FLAP TRACK FAIRING AFT END U-CHANNEL CRACKED IN TWO PLACES UNDER THE TRACK. THE CRACKS WERE .25 INCH LONG. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030829000412003082900041EA 2003 8 29 COMA0360374 120030818A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO01982CA16949 7168 FLIGHT 5587 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20030829000832003082900083 2003 8 29 P5CA0300926 420030822A25657A124825 SLIDE BOEING747 747249F 1384849NM COCKPIT DEPLOYED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FLT DECK LT ESCAPE SLIDE DEPLOYED INADVERTENTLY. REPLACED SLIDE ASSY, REPLACED SLIDE GAS GENERATOR BOTTLE AND REPLACED DOOR (SLIDE) ASSIST BOTTLE. 2L74 4F A20WE 20030829000882003082900088 2003 8 29 P5CA0300906 420030803A3460 CDU BOEING747 7472U3B 1384846NM COCKPIT MALFUNCTIONED A P5CAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 WP23923FT 22769 NR 1 INS DISPLAY WENT BLANK AFTER PUSH BACK WARNING LIGHT CAME ON AND ADI TUMBLED. SWAPPED NR 1 CDU AND NR 3 CDU OPERATIONAL CHECK NORMAL PER MM 34-41-02. 2L74 4F RTA20WE 20030829001052003082900105 2003 8 29 SWAA031873 420030821A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030829001072003082900107NM 2003 8 29 SWAA031875 120030821A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787 PLUS 5, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030829001092003082900109NM 2003 8 29 SWAA031877 120030820A57536546434370 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C3 CHECK, FOUND RT INBD T/E FOREFLAP DELAMINATED AT LOWER OUTBD CORNER. REMOVED AND REPLACED RT INBD T/E FOREFLAP PER MM. 2L72 4F RTA16WE 20030829001142003082900114 2003 8 29 SWAA031802 420030810A256565C19901 CABLE BOEING737 7373H4 1384600NM SERVICE DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030829001202003082900120NM 2003 8 29 SWAA031805C 120030811A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030829001352003082900135NM 2003 8 29 SWAA031863 120030818A2781189929 PROXIMITY SENSOR BOEING737 7373H4 1384600NM L/E FLAP FAULTY A SWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29320SW 23341 AIR TURNBACK, NR 2 L/E FLAP AMBER LIGHT AND L/E FLAP TRANSIT LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. REMOVED AND REPLACED UP PROXIMITY SENSOR PER MM. 2L72 4F RTA16WE 20030905001322003090500132NM 2003 9 5 DL76S030649 120030712A5744113T122633 SUPPORT BEAM BOEING767 767332 1382001NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27119DL 23278 WING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : FWD FLAP ATTACH HOLE CORROSION, THE 2 FWD FLAP ATTACH HOLES ON THE OUTBD SUPPORT BEAM NR 3 SUPPORT FOR THE INBD FLAP LOCATION WERE FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES, HFEC INSPECTING, OVERSIZING FOR AN INSURANCE CUT, AND INSTALLING ALUMINUM BUSHINGS TO RESTORE THE PROPER HOLE SIZE. THE REPAIR WAS ACCOMPLISHED PER ER/A 385394-14. 2L72 4F RTA1NM 20030905001392003090500139NM 2003 9 5 DL757030651 120030714A3350 FUSE BOEING757 757232 1384965NM POWER SUPPLY BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27688DL 27587 ON L/O CHECK FOUND FOUND FIRST CLASS EMERGENCY LIGHTS INOP. REPLACED FUSES IN POWER SUPPLY CHECKS OK. 2L72 4F RTA2NM 20030905001422003090500142NM 2003 9 5 DLM88030652 120030715A2910 B-NUT DOUG MD88 MD88 3023688NM HYD SYSTEM LOOSE A DALAD RETURN TO BLOCK KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27989DL 53341 DURING TAXI OUT SMOKE/FUMES ENTERED CABIN. DISAPPEARED WHEN APU WAS SHUT DOWN. FOUND "B' NUT LOOSE ON HYD LINE TO LT THRUST REVERSE MODULE. HYD FLUID LEAKED INTO 48 SECTION AND OVERBOARD. DUCT BURNOUT IN PROGRESS. 2L72 4F RTA6WE 20030905001562003090500156NM 2003 9 5 DLM88030668 120030718A21208981501 DUCT DOUG MD88 MD88 3023688NM A/C BAY RUPTURED A DALAFA ACTIVATE FIRE EXT. UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27960DL 49979 AFTER TAKE OFF LEFT PNEUMATIC SUPPLY DUCT RUPTURED, CAUSING A TAIL COMPARTMENT TEMP HIGH CONDITION, THERMALLY DISCHARGING BOTH FIRE BOTTLES. COCKPIT INDICATING TAIL COMP TEMP HIGH AND BOTH AGENT LOW LIGHTS. AIRCRAFT PERFORMED AIR TURN BACK TO ATL. REPLACED DUCT AND BOTTLES 2L72 4F RTA6WE 20030905001612003090500161NM 2003 9 5 USAA030144 120030627A5320 CHANNEL BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US40808 23986 PIT - FOUND CHANNEL CORRODED 4 INCHES BY 6 INCHES, AFT CARGO Z-CHANNEL STATION 727D TO 867 JUST ABOVE STRINGER 24L. NEW CHANNEL SPLICED IN PER TYPICAL REPAIR 53-40-01 AND SRM 51-70-11, SRM 53-60-53. (M) 2L72 4F RTA16WE 20030905001662003090500166EU 2003 9 5 USAASA03091 120030725A2560C37103103 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE O OTHER ININSP/MAINT 1 EA19748UW 1311 PHL - FOUND AN INCORRECT RELEASE CABLE ON THE FORWARD LEFT ESCAPE SLIDE DURING INSPECTION. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20030905001682003090500168NM 2003 9 5 USAA030151 120030805A5330 SKIN BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU35713 27148 CLT - FOUND SKIN CRACKED 1 INCH, AFT LT FS 1787 BETWEEN STRINGER 16L AND STRINGER 17L, BELOW HORIZ STAB. INSTALLED REPAIR PER EA 94570, SRM 53-80-70 FIG 1, AND SRM 51-70-12. (M) 2L72 4F RTA2NM 20030905001692003090500169NM 2003 9 5 USAA030150 120030814A5311 FRAME BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU35769 27148 CLT - FOUND FRAME CORRODED FS 1640 RBL 5 - LBL 5. BLENDED OUT CORROSION PER SRM 51-00. (M) 2L72 4F RTA2NM 20030905001702003090500170WP 2003 9 5 AALA20030590 120030519A2150 B-NUT DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW217533A 49987 ORD - FLT 1990 - EN ROUTE ORD-BOS, AFTER TAKEOFF WHITE ACRID SMOKE ENTERED CABIN AND COCKPIT. BOTH AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHTS ILLUMINATED. ABNORMAL PROCEDURE WERE FOLLOWED AND UNABLE TO EXTINGUISH LIGHTS. RETURNED ORD, SMOKE DISSIPATED WHILE ON FINAL, AND LANDED WITHOUT INCIDENT. UPON LANDING ORD, BOTH TEMPERATURE HIGH LIGHTS EXTINGUISHED. TIGHTENED B-NUTS ON LEFT AND RIGHT AUXILIARY VALVE SENSE LINES. ALSO, REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905001782003090500178WP 2003 9 5 AALA20030561 120030512A2120 CLAMP DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW21579AA 53156 ELP - FLT 1168 - EN ROUTE ELP-DFW, SHORTLY AFTER TAKEOFF, THE TAIL COMPARTMENT TEMPERATUTE HIGH LIGHT ILLUMINATED. EXECUTED RED BOX ITEMS AND AIR INTERRUPTED. LANDED ELP WITHOUT INCIDENT. ACCOMPLISHED INSPECTION OF DUCTING AND SECURITY OF CLAMPS IN THE TAIL COMPARTMENT. REINSTALLED AIR CONDITIONING MACHINE CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905001842003090500184EA 2003 9 5 ASOA03371 120030814A5210HSP115P0941400 PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BENT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 FLT 4160 - DURING A GROUND INSPECTION IN ATL, THE CREW REPORTED THE PASSENGER DOOR INSIDE HANDLE WOULD NOT LIFT AND THE DOOR WAS DIFFICULT TO OPEN SOMETIMES. MAINTENANCE STRAIGHTENED THE OUTER HANDLE PIN ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030905001872003090500187NM 2003 9 5 USAA030138 120030814A5330654576599 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US49220 23315 PIT - FOUND SKIN CRACKED .125 INCH BY .25 INCH CRACKING AT RIVET HEADS, APPROX 40, AND DISONDING, LEFT SIDE STATION 360-540 STRINGER 10 LEFT. REMOVED SKIN PANEL STATION 360-540, INSTALLED 3 SECTIONS WITH 2 SPLICE AT STATION 420 AND 480 PER EA 76610. (M) 2L72 4F RTA16WE 20030905001902003090500190NM 2003 9 5 USAA030142 120030804A5320 ANGLE BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US47187 23237 PIT - FOUND L-ANGLE CORRODED 2 INCHES BY 2 INCHES, UNDER POTTING COMPOUNT, STATION 727 FORWARD BULKHEAD AFT FACE IN AFT CARGO. FABRICATED AND INSTALLED NEW STRINGER END FITTINGS AND STRAP PER EA 76684 AND SRM 53-00-01. (M) 2L72 4F RTA16WE 20030905001952003090500195NM 2003 9 5 USAA030136 120030813A5210 SKIN BOEING737 737401 1384701NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 PIT - FOUND INNER SKIN CRACKED APPROX 1 INCH, AFT EDGE OF INNER SKIN OF MAIN ENTRY DOOR. TRIMMED OUT CRACKS AND INSTALLED DOUBLER AND FILLER PER EA 76156. (M) 2L72 4F RTA16WE 20030905002022003090500202SO 2003 9 5 C2XA03CL159 120030902A33501010861 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2713989 145271 CLE FLIGHT NR 2004 THE CREW REPORTED THE EMERGENCY LIGHT NEAR THE GALLEY DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN AT THE GALLEY DOOR.OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030829001402003082900140NM 2003 8 29 SWAA031834 120030815A4920GTCP85129H APU BOEING737 7375H4 138449DNM APU BAY MALFUNCTIONED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29506SW 24183 AIR TURNBACK, SMOKE REPORTED IN CABIN. REMOVED AND REPLACED APU AND WATER SEPARATOR BAGS PER MM. 2L72 4F RTA16WE 20030829001522003082900152NM 2003 8 29 SWAA031846 120030816A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 747 AT STR 22L, BS 747 AT STR 24L, BS 727E AT STR 24L AND BS 907 AT STR 23L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030829001562003082900156NM 2003 8 29 SWAA031820 120030813A5751654645424 AILERON BOEING737 7372H4 138448CNM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED PM CHECK, FOUND RT AILERON DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT AILERON PER MM. 2L72 4F A16WE 20030829001662003082900166NM 2003 8 29 SWAA031830 120030813A275065C16951 ROLLER BOEING737 7372H4 138448CNM T/E FLAP WORN A SWAAK NONE E VIBRATION/BUFFET NRNOT REPORTED 1 SW29074SW 22674 AIRCRAFT VIBRATION FELT WHEN FLAPS ARE IN TRANSIT. REMOVED AND REPLACED RT MID FLAP DEFLECTOR ROLLER ASSY PER MM. 2L72 4F A16WE 20030829001762003082900176 2003 8 29 SWAA031813 420030811A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030829001812003082900181NM 2003 8 29 SWAA031792 120030811A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR 8L AND STR 9L, BS'S 480, 767 AND 867. REPAIRED FRAMES PER BFG ER. 2L72 4F RTA16WE 20030829001842003082900184NM 2003 8 29 SWAA031795 120030808A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (5 EA) AT STR 4L, BS'S 409, 488, 470, 692 AND BS 697. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001892003082900189NM 2003 8 29 SWAA031800 120030811A33502330127 BATTERY PACK BOEING737 7372H4 138448CNM COCKPIT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED PM CHECK, FOUND FLIGHT DECK EXIT DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM. 2L72 4F A16WE 20030829001942003082900194WP 2003 8 29 GTIA030621 120030725A5520 TIP CAP DOUG DC9 DC983 3022083WP RT ELEVATOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND RIGHT ELEVATOR OUTBOARD AFT EDGE TIP, METAL CRACKED. REMOVED RIGHT ELEVATOR, OUTBOARD AFT EDGE TIP. LOCATED AND DRILLED NEW END TIP. INSTALLED NEW END TIP ON RIGHT, OUTBOARD AFT EDGE ELEVATOR. (M) 2L72 4F RTA6WE 20030829002122003082900212EU 2003 8 29 ASOA03345 120030729A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU CABIN DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030902000502003090200050EA 2003 9 2 UIAFAA9204 120030620A710030005000056 TSCU DHAV DHC8 DHC8311 1386006EA NR 1 ENGINE MALFUNCTIONED Z C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 TW00152257811 405 DURING T/O AUTOFEATHER NO ARM ,CHK FND TSCU FAULT, IAW PWC 72-01-00 REPLACED TSCU AND IAW AMM 71-00-00 ENG RUNING AUTOFEATHER SYSTEM FUNCTION TEST NORMAL. 2H72 4T RTA13NM 20030828001462003082800146EA 2003 8 28 2003F00523 120030717A27303C2200 TRANSDUCER CNDAIRCL600 CL6002C10 1390015EA RT ELEVATOR MALFUNCTIONED A FDKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07511MJ 10104 FRL 6717 - PHX-FAT - RETURNED TO FIELD FOR AN ELEVATOR SPLIT EICAS MSG IN FLIGHT. MAINTENANCE TROUBLESHOT AND FOUND RTVD BAD. THE RVDT WAS CHANGED AND PERFORMED OPS CHECK. AIRCRAFT CURRENTLY IN SERVICE. (M) 2L72 4F RTA21EA 20030828001782003082800178 2003 8 28 SWAA031848 420030818A256563550101 SLIDE BOEING737 7377H4 1384404NM ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29727SW 27859 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030829000172003082900017NM 2003 8 29 CALA0300462 120030810A5414 SKIN BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND A 0.40 INCH CRACK IN PYLON CUTOUT FOR PANEL NR 5727, NR 1 ENGINE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5430-01230. 2L72 4F RTA16WE 20030829000252003082900025NM 2003 8 29 CALA0300483 120030822A5320 SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND FORWARD LAV WALL SUPPORT CORRODED AT STA 307, LBL 13 TO 15. THE WALL SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030829000602003082900060WP 2003 8 29 DHL2003801085 120030713A3231 UPLOCK DOUG DC8 DC873F 302199FWP RT GEAR DOOR LACK OF LUBE A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 AFTER GEAR RETRACTION GEAR DOOR NOT LATCHED LIGHT STAYED ILLUMINATED. WHEN PUTTING THE GEAR HANDLE IN UP LATCH CHECK POSITION LIGHT WENT OUT. VISUALLY INSPECTED RIGHT GEAR DOOR AND UP LATCH MECHANISM. NO DEFECTS NOTED. LUBED UP LATCH MECHANISM PER M/M 32-31-4. 2L74 4F RT4A25 20030903002652003090300265SO 2003 9 3 C2XA03IA077 120030806A242451545002 GCU EMB 135 EMB135LR 3260305SO NR 4 FAULTY A C2XAK NONE G MULTIPLE FAILURE APAPPROACH 1 SW27245175300 4249 145332 IAH - FLT NR 3325 - UPON APPROACH TO IAH THE CREW REPORTED THAT GENERATOR NUMBERS 1, 2, 3, AND APU SHOWING VOLTS BUT NO AMPS AND THAT GENERATOR 4 WENT OFF LINE AT 1500FT. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 4 GENERATOR CONTROL UNIT TO FAULT AND CAUSE THE OTHER GENERATORS TO DROP OFF LINE. MAINTENANCE REPLACED THE AFFECTED GENERATOR CONTROL UNIT, OPERATIONALLY TESTED THE SYSTEM GOOD, AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030904000572003090400057 2003 9 4 SWIA200312251 420030809A22156225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR RATCHETING A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07213SW6955 6955 120277 YOKE RATCHETS WHEN MOVED FORWARD AND AFT, REPLACED ELEVATOR SERVO MOTOR WITH SERVICEABLE UNIT IAW EMB MM 27-00-03. SYSTEM OPS CHECKS GOOD. 2L72 4T RTA31SO 20030904000812003090400081NM 2003 9 4 QXEA200300985 120030817A3150 LIMIT SWITCH DHAV DHC8 DHC8202 2809007NM WARNING SYS OUT OF ADJUST A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09357PH 504 PDX- ON FLIGHT 2033 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN WENT OFF DURING TAKEOFF WITH ALL SETTINGS CORRECT. ADJUSTED LIMIT SWITCH 3151-S3. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904000932003090400093NM 2003 9 4 QXEA200300999 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 1 SEAT TRACK AT STATION X376.100 HAS TOP SURFACE CORROISON. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20030904001562003090400156WP 2003 9 4 DHL2003873583 120030628A5245 SKIN DOUG DC8 DC873F 302199FWP A/C BAY DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LWR FUSELAGE EXTERIOR AIR COND COMPT DOOR NR 12 SKIN WITH 0.250 INCH CRACK (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1, SRM 52-8-1 FIG 1 PG 2. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN IAW SRM 52-8-1 FIG 1 PG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20030904001812003090400181WP 2003 9 4 AALA20030657 120030611A2120 DUCT DOUG DC9 DC982 3022082WP A/C BAY OUT OF POSITION A AALAK NONE MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW21579AA 53156 DFW - FLT 1058 - EN ROUTE DURING TAKEOFF AT 800 FT MASTER WARNING LIGHT AND TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. WHEN THROTTLES WERE REDUCED TO LEVEL OFF AT 3,000 FT LIGHT EXTINGUISHED APPROXIMATELY 1 MINUTE LATER. WHILE ACCOMPLISHING EMERGENCY CHECKLIST AND POWER WAS INCREASED TO CLIMB TO 4,000 FT LIGHT RE-ILLUMINATED. DURING VECTORS AROUND THE PATTERN TO LAND AT DFW AND AS POWER WAS REDUCED ON GLIDESLOPE THE LIGHT AGAIN EXTINGUISHED. LANDED DFW WITHOUT FURTHER INCIDENT. REINSTALLED AND SECURED LEFT PACK COMPRESSOR INLET DUCT. CONTINUE ENGINE RUN WITH NO OTHER LEAKS FOUND IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905000182003090500018SO 2003 9 5 LR7A03065 120030725A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND LH FS 597 'L' BRACKET CRACKED AT LBL 18, WL 283. REPLACED BRACKET IAW SRM SMP 583 51-60 AND 51-70. NR 2110. 2H74 4T A1SO 20030905000242003090500024SO 2003 9 5 LR7A03069 120030725A53203305036 FITTING LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND FS 627 FITTING CORRODED AT LONGERON ATTACH, LBL 20, WL 270. REPLACED FITTING IAW SRM SMP 583 51-10 PG 4. NR 2120. 2H74 4T A1SO 20030905000332003090500033SO 2003 9 5 C2XA03SH316 120030905A532014521699003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 19 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030905001442003090500144NM 2003 9 5 DL738030656 120030716A3350D71702030 CHARGER BOEING737 737832 13844CFNM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO273754A 29626 FOUND EMERGENCY LIGHTS INOP ROWS 10-15. FOUND EMERGENCY LIGHTS BATTERY CHARGER BAD AT ROW 11 LOWER SIDEWALL. RPLD CHARGER, CKS GOOD. 2L72 4F RTA16WE 20030905001622003090500162NM 2003 9 5 USAA030143 120030807A5311 FRAME BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US40913 23987 PIT - FOUND FRAME CRACKED .5 INCH, FS 400 S8R AND S9R AT PSU SUPPORT BRACKET. INSTALLED DOUBLER PER SRM 53-10-20A. (M) 2L72 4F RTA16WE 20030905001922003090500192NM 2003 9 5 USAA030139 120030716A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US37758 24552 PIT - FOUND FRAME CRACKED APPROX 1 INCH, CRACKED THROUGH 2 FASTENERS, FRAME 601, LEFT SIDE JUST BELOW CABIN FLOOR. DAMAGE CUT OUT, FILLER AND DOUBLER INSTALLED PER EA 76450. (M) 2L72 4F RTA16WE 20030905002002003090500200NM 2003 9 5 USAA030146 120030727A5414 SKIN BOEING737 737401 1384701NM LT NACELLE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US41222 23886 PIT - FOUND SKIN CRACKED 1 INCH, NACELLE STRUT SKIN CRACK AROUND PANEL 57271, LEFT PYLON. DOUBLER INSTALLED PER TR 54-30-07 AND EA 56543B. (M) 2L72 4F RTA16WE 20030905002092003090500209SO 2003 9 5 C2XA03SH307 120030829A711014576631622 STIFFENER EMB 145 EMB145ER 3260211SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030905002102003090500210SO 2003 9 5 C2XA03SH297 120030827A532013500322001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE LEFT HAND SILL BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030722000022003072200002NM 2003 7 22 2003F00430 120030310A5720 ANGLE BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND STRUCTURE CRACKED, NOSE WHEEL WELL AT BS 294.5, LBL 12 RT, WL 177. STOP DRILLED CRACKS. FABRICATED FORMED ANGLE REPAIRS AND STRAPS. TREATED, PRIMED AND INSTALLED ANGLES AND STRAPS IN NOSE WHEEL WELL RIGHT SUPPORT AT STATION 294.5. (M) 2L73 4F A3WE 20030722000172003072200017NM 2003 7 22 2003F00445 120030307A5312 PRESSURE PANEL BOEING727 727222 1384073NM RT MLG WW CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT RIGHT WHEEL WELL FORWARD PRESSUER WEB, RBL 870, OUTBOARD LOWER END OF 850 FRAME. STOP DRILLED CRACK ON RIGHT WHEEL WELL FORWARD PRESSURE WEB RBL 870, OUTBOARD LOWER END OF 870 FITTING. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED REPAIR. (M) 2L73 4F A3WE 20030722000242003072200024NM 2003 7 22 2003F00452 120030124A551469144106 HINGE PIN BOEING727 727222 1384073NM HORIZONTAL STAB CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND HORIZONTAL STAB, RIGHT OUTER HINGE PIN IS GALLED AND PITTED. REMOVED AND REPLACED HORIZONTAL STAB RIGHT OUTER HINGE PIN. (M) 2L73 4F A3WE 20030722000272003072200027NE 2003 7 22 2003F00455 220030415A7230 COMPRESSOR BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 2 ENGINE STALLED A RYNAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 CE077645U 20039 FROM 31,000 FEET, ON DESCENT INTO BWI, NR 2 ENGINE COMPRESSOR STALL. ALL ENGINE READINGS APPEARED NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE. OPERATIONAL AND LEAK CHECKED NORMAL. (M) 2L73 4F4 F A3WE E2EA 20030722000282003072200028NM 2003 7 22 2003F00456 120030123A5347 SEAT TRACK BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CRACKED SEAT TRACK AT STATION 948C, LBL 25. REPLACED SEAT TRACK AT STATION 950B TO 950D. (M) 2L73 4F A3WE 20030722000312003072200031NM 2003 7 22 2003F00459 120030125A5712 RIB BOEING727 727222 1384073NM LEFT WING CHAFED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CHAFED RIB, LEFT WING LEADING EDGE, STATION 407.90. REMOVED CHAFED RIB LEFT WING LEADING EDGE STATION 407.90. FABRICATED NEW RIB. TREATED AND PRIMED. INSTALLED FABRICATED RIB. (M) 2L73 4F A3WE 20030722000322003072200032NM 2003 7 22 2003F00460 120030125A5754 STRUCTURE BOEING727 727222 1384073NM RT KRUEGER FLAP CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND RIGHT WING LEADING EDGE NR 4 KRUEGER FLAP BULLNOSE WITH AREAS OF CORROSION ON INBOARD SIDE WS 130.7. (M) 2L73 4F A3WE 20030722000332003072200033NM 2003 7 22 2003F00461 120030123A5315 FLOORBEAM BOEING727 727222 1384073NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CORROSION ON FLOORBEAM, STATION 328 RBL 10, UNDERNEATH NUTPLATE. REMOVED CORROSION. MATERIAL LOSS OTU OF LIMITS. FABRICATED ONE EACH END CAP AND 4 ANGLES. TREATED, PRIMED AND INSTALLED REPAIRED PARTS. (M) 2L73 4F A3WE 20030722000342003072200034NM 2003 7 22 2003F00462 120030123A5754 STRUCTURE BOEING727 727222 1384073NM RT NR 6 SLAT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CRACK ON UPPER TRAILINGE EDGE, NR 6 SLAT WS 629. TRIMMED OUT DAMAGED AREA OF TRAILING EDGE. FOUND TO BE WITHIN LIMITS. ALODINED BARE METAL AT NR 6 SLAT TRAILING EDGE WL 629. (M) 2L73 4F A3WE 20030722000372003072200037NM 2003 7 22 2003F00465 120030123A5315 FLOORBEAM BOEING727 727222 1384073NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CORROSION, FORWARD CARGO PIT, MAIN FLOORBEAM, LOWER FLANGE AT STATION 575, RBL 0, BENEATH NUTPLATE. CUTOUT DAMAGED AREA. FABRICATED ANGLE REPAIR AND FILLER. TREATED AND PRIMED. INSTALLED FABRICATED ANGLE ON FORWARD CARGO PIT, MAIN FLOORBEAM LOWER FLANGE AT STATION 575, RBL 0. (M) 2L73 4F A3WE 20030722000392003072200039NM 2003 7 22 2003F00467 120030123A5754 STRUCTURE BOEING727 727222 1384073NM KRUEGER FLAP CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CRACK ON NR 4 KRUEGER FLAP, INBOARD EDGE. (M) 2L73 4F A3WE 20030722000442003072200044NM 2003 7 22 SWAA031495 120030703A57516568269 FRAME BOEING737 7372H4 138448CNM RT WING CRACKED A SWAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW29095SW 23054 AIRCRAFT REQUIRES EXCESSIVE LEFT AILERON TO FLY STRAIGHT. FOUND NR 7 CANOE FAIRING A FRAME CRACKED. REMOVED AND REPLACED A FRAME PER MM. 2L72 4F A16WE 20030722000462003072200046 2003 7 22 SWAA031504 420030708A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 0076A 33715 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030722000552003072200055EA 2003 7 22 COMA0360318 120030709A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01818CA7837 7408 FLIGHT 5318 GEAR DISAGREE WARNING DURING GEAR EXTENSION. REPLACED HYDRAULIC PUMP 3A. 2L72 4F RTA21EA 20030722000572003072200057NM 2003 7 22 SWAA031497 120030708A533065458001133 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER FWD CORNER OF AIRSTAIR CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030829000702003082900070WP 2003 8 29 IXXA0300047O 120030710A5330 PLUG DOUG DC8 DC871F 302199DWP FUSELAGE LOOSE A IXXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW11828BX81006868 45993 AFTER TAKEOFF FROM KMCO AND GEAR RETRACTION, THERE WAS A VIBRATION ASSOCIATED WITH NOISE COMING FROM THE NOSE WHEEL WELL AREA. GEAR WAS CYCLED AND NOISE AND VIBRATION CONTINUED. CREW DECIDED TO RETURN AND LAND AT KMCO. MAINTENANCE FOUND NOSE CURTAIN LOOSE AND RESECURED. INSPECTED AND FOUND WINDOW PLUG LOOSE. MAINTENANCE RESECURED PLUG IN ACCORDANCE WITH ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030829000782003082900078CE 2003 8 29 1850301 120030702A5220 HANDLE BEECH 1900 1900C 1154161CE EMERGENCY EXIT OUT OF ADJUST A NSVAK NONE O OTHER ININSP/MAINT 1 EA27207CJ UC107 EMERGENCY EXIT LOOSE IN LOCKED POSITION. ADJUSTED EXIT DOOR HANDLE TENSION. 2L72 4T RTA24CE 20030829001082003082900108NM 2003 8 29 SWAA031876 120030820A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030829001152003082900115 2003 8 29 SWAA031803 420030811A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030829002062003082900206NM 2003 8 29 USAABB03108 120030704A2424 GCU BOEING757 7572B7 1384964NM LEFT FAILED A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19632AU 27810 PIT - FLT 21 - EN ROUTE, WITH THE LEFT GENERATOR ON MEL FOR RIGHT GENERATOR NOT PICKING UP THE LEFT GENERATOR LOAD, AND APU OPERATING, THE APU PERFORMED AN AUTO SHUTDOWN. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHR INCIDENT. MAINTENANCE REPLACED THE LEFT GCU, AND SUBSEQUENTLY (O6JUL03), REPLACED THE STANDBY POWER MODULE AND RIGHT GENERATOR BUS TIE BREAKER. A BITE WAS PERFORMED ON THE APU WITH NO FAULTS FOUND. (M) 2L72 4F RTA2NM 20030902000602003090200060EU 2003 9 2 R7MR34599 120030119A6210350A11001001 BLADE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR DELAMINATED E R7MRO OTHER O OTHER NRNOT REPORTED 1 NM073593X7160 1814 1081 SKIN DELAMINATION, 3 FT FROM ROOT (MAY QUALIFY FOR BLADE EXCHANGE). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20030902000712003090200071NE 2003 9 2 ARWA20030603 220030611A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D* 52039NE NR 2 FAILED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO198969U600415072 46070 671379 PRECAUTIONARY SHUTDOWN NR 2 ENGINE; TIME 0030. OIL PRESSURE -0 OIL TEMP 145. ENGINE WINDMILLED 3 1/2 HOURS, ZERO OIL PRESSURE. ALL ABNORMAL PROCEDURES FOLLOWED. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARDS 72-000-30-02-01, 77-000-00-03-1 & 77-000-02-1; AND ACCOMPLISHED R/B 17029 IAW MSG-3 MAINTENANCE PROGRAM. PERFORMED ENGINE TRIMMING AND TEST, FOUND WITHIN LIMITS IAW MM 71-00 AND IAW CARD DC8UN-003. 2L74 4F4 F 4A25 1E8 20030902000842003090200084 2003 9 2 EOO2003F00001 420030613A2562 ANTENNA LEAD HUGHES369 369D 4470706WP ALLSN 250C 250C* GL ELT DISCONNECTED B EOORO OTHER O OTHER NRNOT REPORTED 1 AL03511SB 1090592D FOUND ELT ANTENNA LEAD STOWED AND TERMINATED IN THE WIRE BUNDLE AND NOT HOOKED UP TO THE ELT ANTENNA. DURING A CONFORMITY INSPECTION OF A LEASED AIRCRAFT THE ELT ANTENNA LEAD WAS FOUND TO BE, NOT ONLY DISCONNECTED, BUT TERMINATED WITH HEATSHRINK AND STOWED IN THE ADJACENT WIRE BUNDLE TOT HE ELT ANTENNA. RECONNECTED ELT ANTENNA. 1G71 3U3 U H3WE E4CE 20030902000922003090200092EA 2003 9 2 SWIA200312145 120030627A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07720SW 7297 CH 1 STAB TRIM DOES NOT TEST. STAB AND MACH TRIM DISENGAGE WITH NO MOVEMENT OF TRIM. REMOVED AND REPLACED MOTOR CONTROL UNIT & HORIZONTAL STAB ACTUATOR. OPS CHECKS GOOD IAW MM 27-40-00. ACT P/N: 8396-3, S/N ON: 569, S/N OFF: 494. 2L72 4F RTA21EA 20030902000962003090200096WP 2003 9 2 ARWA20030602 120030610A793141800141 TRANSMITTER DOUG DC8 DC863F 302198FWP OIL PRESSURE INOPERATIVE A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO19441J 45988 AFTER BRAKE RELEASE, WHILE SETTING MAX POWER, NUMBER ONE ENGINE OIL PRESSURE ROSE TO 60 PSI. REMOVED AND REPLACED PRESSURE TRANSMITTER IAW MM 79-32-1. ACCOMPLISHED ENGINE RUN UP IAW ARROW AIR J/C 72-000-30-02 2L74 4F 4A25 20030902001332003090200133WP 2003 9 2 IXXA0300046O 120030708A5320 COUPLING DOUG DC8 DC871F 302199DWP DUCT SEPARATED A IXXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW11828BX81002865 45993 AFTER TAKE OFF FROM KPHL TO KTOL, DURING GEAR RETRACTION A NOISE AND VIBRATION OCCURRED. WHEN GEAR WAS LOWERED NOISE AND VIBRATION DISSIPATED SLIGHTLY. GEAR WAS CYCLED AND NO CHANGE OCCURRED. MAINTENANCE FOUND DUCT SEPERATED AT COUPLING. RESECURED DUCT, RESECURED CANVAS CURTAIN IN NOSE WHEEL WELL, IAW MM. INSPECTION OF NOSE WHEEL FRICTION BRAKES FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030902001462003090200146SO 2003 9 2 SWIA200312158 120030704A275012064207615 SWITCH EMB 120 EMB120ER 3260203SO FLAP SELECTOR INOPERATIVE A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07293SW 120320 UPON SELECTING FLAPS, 25 GOT A (CONTROL FAULT). PERFORMED QRH, CLEARED FAULT. SELECTED FLAPS 25 SECOND TIME, ALSO GOT A CONTROL FAULT. SELECTED RESET, CLEARED FAULT AND LANDED. REPLACED FLAP SELECTOR. RERACKED FCU COMPUTER. CLEARED ALL FAULTS. OPS CHECKED GOOD. SN OFF 120025R. 2L72 4T RTA31SO 20030902001512003090200151SO 2003 9 2 SWIA200312163 120030703A27503075001017 CONTROL UNIT EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07189SW2409 2409 120048 ON TAXI OUT, GOT FLAP CONTROL FAULT WITH FLASHING NAC LIGHTS. COULD NOT CLEAR ''CONTROL FAULT''. VISUAL INSPECTION FOUND RT NACELLE APPROX. .2500 - .5000 INCH DOWN - ALL OTHER FLAP SEGMENTS UP. COULD NOT DUPLICATE SQUAWK. REPLACED FCU FOR TROUBLESHOOTING. OPS CHECK GOOD . 2L72 4T4 TRTA31SO E20NE 20030902001532003090200153SO 2003 9 2 SWIA200312165 120030627A3350 FUSE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE EMERGENCY LIGHT BLOWN A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07197SW 120186 FORWARD SECTION OF EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. REPLACED BLOWN FUSE. OPS CHECK GOOD. P/N: 1AFUSE 2L72 4T4 TRTA31SO E20NE 20030902001792003090200179NM 2003 9 2 03FDEA01087 120030710A3244 TIRE DOUG MD11 MD11 3023602NM MLG INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25620FE 48791 AFTER GEAR RETRACTION DURING CLIMB OUT OF NRT, GOT LVL 1 TIRE PRESS LO ALERT AND OBSERVED NR 1 MAIN LANDING GEAR LOOSING PRESSURE UNTILL TIRE FAIL ALERT ILLUMINATED. DIVERED TO TPE AND LANDING UNEVENTFULY WITY O PSI IN NR 1 MAIN LANDING GEAR. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRE ASSY IAW MM 32-41-01-4. TIRE PRESSURE SERVICED AND LEAK CHECK PASSED. INSP GEAR STRUT, BRAKE ASSY, AND OTHER TIRE ASSY, ALL CONDITIONS NORMAL. OK FOR CONTINUE SERVICE. 2L73 4F RTA22WE 20030722000602003072200060NM 2003 7 22 SWAA031500 120030704A32201061226 BRACKET BOEING737 7372H4 138448CNM NLG LOOSE A SWAAO OTHER N FALSE WARNING APAPPROACH 1 SW29090SW 22905 AFTER GEAR EXTENSION, NLG RED UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED GEAR ALL LIGHTS OPERATED NORMAL. FOUND, LOCK LINE SENSOR TARGET BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F A16WE 20030722000632003072200063NM 2003 7 22 SWAA031512 120030708A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030722000652003072200065 2003 7 22 SWAA031454 420030702A2565D31354 SLIDE BOEING737 7373H4 1384600NM PAX DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030722000692003072200069NM 2003 7 22 SWAA031458 120030702A57536546435277 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED C4 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED AT INBD END LOWER SURFACE. REMOVED AND REPLACED LT OUTBD AFT T/E FLAP PER MM 2L72 4F RTA16WE 20030722000712003072200071 2003 7 22 SWAA031460 420030701A25656557463 GIRT BAR BOEING737 7377H4 1384404NM ESCAPE SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29783SW 29809 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED HOOK FASTENERS PER SRM. 2L72 4F RTA16WE 20030722000792003072200079EU 2003 7 22 MALA030336 120030712A1430 BOLT SAAB SF340 340B 7860101EU MLG BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15366PX 340B267 RT SEPARATION BOLT (ON MAIN LANDING GEAR) BROKE. MAINTENANCE REPAIRED WIRING AT CONNECTOR GB602-20 AND WIRE GB604-20 IAW SAAB WM 20-20-35. REFER LOG PAGE 177372 FOR DETAIL. 2L72 4T RTA52EU 20030722000832003072200083EU 2003 7 22 MALA030332 120030619A5530 ANGLE BAC 146 AVRO146RJ85A1500097EU VERTICAL STAB CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15526XJ E2351 DURING C-CHECK INSPECTION IN CVG, LT VERTICAL STABILIZER TO FUSELAGE CLOSING ANGLE CRACKED. MAINTENANCE REPAIRED PER EO A55027. REFER TO 409 127862 FOR DETAIL. A/C RELEASE DATE 7/1/2003. 2H74 4F RTA49EU 20030722000912003072200091EU 2003 7 22 AWXA200300790 120030628A5411D5453003220000 RIB AIRBUS320 A320231 3930325EU NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 DURING C-03 CHECK A .125 INCH CRACK WAS FOUND ON NR 1 PYLON RIB, 4TH LOWER RIB FROM UPPER DRAIN LINE CLEARANCE HOLE, OUTBOARD EDGE IN AFT FIXED FAIRING. MAINTENANCE REMOVED CRACKED RIB; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-12 & 21-22, FIG 2, 3 & 8. 2L72 4F RTA28NM 20030722000992003072200099NM 2003 7 22 SWAA031448 120030630A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED RON, FOUND OVERHEAD BIN BULL MOSE EMERGENCY EXIT LIGHT SOCKET DAMAGED AT ROW 18 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030722001032003072200103NM 2003 7 22 SWAA031476 120030702A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 13R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030718000122003071800012NM 2003 7 18 TSAA0333130 120030529A33508610066 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHTSINOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13823AL 23154 REPLACED FORWARD CONTROL MODULE EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030718000362003071800036NM 2003 7 18 USAABB03102 120030626A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030718000782003071800078NM 2003 7 18 CA030627008 120030618A8097BACC45FN12C3S CONNECTOR BOEING727 727231 1384079NM PWA JT8 JT8D9A 52048NE STARTER SHORTED W E ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 CA (CAN) ON DESCENT THROUGH 3,000 FT, IT WAS OBSERVED THAT THE NR 2 ENGINE START VALVE OPEN LIGHT WAS FLICKERING AND THEN REMAINED STEADY. NR 2 ENGINE IN FLT SHUTDOWN WAS CARRIED OUT AND AIRCRAFT LANDED WITHOUT INCIDENT. DURING INVESTIGATION, IT WAS OBSERVED THAT THE CONNECTOR WAS SHORTED. THE CONNECTOR WAS REPLACED WITH WIRING IAW WDM 80-11-01. NR 2 ENGINE START VALVE WAS REPLACED AS A PRECAUTION IAW MM 80-11-11. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L73 4F4 F A3WE E2EA 20030718000792003071800079NM 2003 7 18 CA030627012 120030610A2910BACH8B04NN0157 LINE BOEING727 727223 1384074NM PWA JT8 JT8D15A 52051NE HYD SYSTEM RUPTURED W D RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) DURING TAXI, CREW APPLIED THE BRAKES AND OBSERVED LOSS OF 'B' SYSTEM HYDRAULIC PRESSURE AND HYD BRAKE PRESSURE. AIRCRAFT STOPPED AND MAINTENANCE TOWED AIRCRAFT BACK TO MAINTENANCE FACILITY. MAINTENANCE OBSERVED LEAKAGE FROM THE RT ELEVATOR PCU. THE AREA WAS INSPECTED AND FOUND THE HYDRAULIC FLEX LINE HAD RUPTURED. A SERVICEABLE LINE WAS INSTALLED AND CHECKED SERVICEABLE IAW MM 20-10-12. NO FURTHER PROBLEM DURING SUBSEQUENT FLIGHT. 2L73 4F4 F A3WE E2EA 20030718000852003071800085WP 2003 7 18 CA030704001 120030703A29101515762419 LINE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE HYD SYSTEM RUPTURED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB-OUT, A COMPLETE (RAPID) LOSS OFB HYD SYS OCCUR. THE AIRCRAFT RETURNED TO THE STATION WITH NO FURTHER PROBLEM. DURING INVESTIGATION THE (B PRESSURE LINE) TO THE FILTER MODULE, LOCATED IN THE HYDRAULIC SERVICE CENTER WAS FOUND RUPTURED. THE HYDRAULIC LINE WAS REPAIRED IAW MM AND THE AIRCRAFT WAS RETURN TO SERVICE. 2L73 4F4 F A23WE E12EU 20030722000772003072200077EU 2003 7 22 MALA030338 120030711A799715EDP1 WIRE SAAB SF340 340B 7860101EU OIL PRESS IND BROKEN A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15434XJ 340B434 DURING FLIGHT 3096, LT PROP OIL PRESSURE PEGGED AT 200 PSI. AIR RETURN TO MSP. MAINTENANCE REPAIRED BROKEN GROUND WIRE AT 15 EDP1. OPS CHECK GOOD LT PROP OIL PRESSURE. REFER TO LOG PG 109053 FOR DETAIL. 2L72 4T RTA52EU 20030722001142003072200114NM 2003 7 22 SWAA031503 120030702A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS CRACKED (2 EA) AT BS 395 AT STR 16L AND BS 364 AT STR 15L. REPAIRED STRINGERS PER SRM. 2L72 4F RTA16WE 20030722001262003072200126EU 2003 7 22 AWXA200300743 120030611A5315D5347217220000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND IN TWO PLACES ON UPPER SURFACE OF FLOORBEAM BETWEEN FR 67-78, Y-1193. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM Y-1193 BETWEEN FR 66-68; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20030722001342003072200134NM 2003 7 22 AWXA200300661 120030516A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 6.5, WL 222-233.5. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT RBL 6.5, WL 222-233.5 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08 PG 267 FIG 209. 2L72 4F RTA16WE 20030723000062003072300006NM 2003 7 23 MEX2003242 120030620A3222 STRUT DOUG MD80 MD83 3023681NM NLG LEAKING A ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23861LF 49826 DURING TRANSIT CHECK WAS DETECTED AN HYDRAULIC LEAK AT NOSE LANDING GEAR STRUT. THE NOSE LANDING GEAR STRUT WAS SERVICED WITH HYDRUALIC FLUID AND NITROGEN IAW MM 32-00-01, ALL TEST CORRECT. DURING OVERNIGHT SERVICE NOSE LANDING GEAR PISTON WAS REPLACED IAW MM 32-21-02 AND NOSE LANDING GEAR STRUT WAS SERVIED WITH HYDRAULIC FLUID AND NITROGEN, ALL CORRECT. (M) 2L72 4F RT 20030723000132003072300013EU 2003 7 23 RU3A03010 120030621A243523080005 STARTER GEN BRAERODH125 BAE125800A 1500285EU NR 2 ENGINE FAILED A RU3AAE UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 SW2194 258129 AT FL330 AND APPROX 1.5 HOURS INTO THE FLIGHT THE CREW BEGAN TO NOTICE AN AIRCRAFT VIBRATION. THE AIRCREW ISOLATED THE VIBRATION TO THE NR 2 ENGINE. THE VIBRATION BECAME EXCESSIVE AND THE CREW ELECTED TO PLACE THE NR 2 ENGINE IN IDLE POWER AND DIVERTED TO ANOTHER AIRPORT. AT 20 DME FROM THE AIRPORT THE AIRCREW ELECTED TO SHUT THE NR 2 ENGINE DOWN DUE TO THE VIBRATION INCREASING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED. INVESTIGATION REVEALED THE STARTER-GENERATOR HAD FAILED. STARTER-GENERATOR WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA3EU 20030723000142003072300014 2003 7 23 KPVA200331 420030703A2210MS390166105L RELAY DHAV DHC8 DHC8103 1386005NM AUTOFEATHER FAILED A KPVAO OTHER J WARNING INDICATION CLCLIMB 1 WP13808WP 026 DURING CLIMB-OUT, 'AFTER T/O' CHECKLIST, WHEN AUTO-FEATHER DESELECTED ARM LIGHT REMAINED ILLUMINATED. COMPLETED A NORMAL APPOACH AND LANDING, TAXIED TO TERMINAL. MAINTENANCE T/S SYSTEM BY SWAPPING THE NR 1 AND NR 2 TSCU'S, DID NOT SOLVE PROBLEM REPLACED THE ARM CONTROL RELAY (6121-KS). SYSTEM WAS OPERATIONALLY CHECKED SATISFACTORILY, AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 20030723000182003072300018NM 2003 7 23 2003F00469 120030525A5230655720515 RETAINER BOEING727 727222 1384073NM DOOR SEAL DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077639U 19912 AT C-CHECK, FOUND C2 DOOR PRESSURE SEAL RETAINER AT TOP CENTER OF DOOR DAMAGED. REMOVED AND REPLACED C2 DOOR PRESSURE SEAL RETAINER AT TOP CENTER OF DOOR. (M) 2L73 4F A3WE 20030723000342003072300034WP 2003 7 23 MEX2003246 120030624A5753 FAIRING DOUG DC9 DC987 3022087WP RT WING DAMAGED A ASMFK NONE O OTHER ININSP/MAINT 1 SW23751RA 49779 AFTER MAKING HIS ROUTINE CHECK-UP TO BE IN POOR CONDTIONS, RIGHT WING NR 4 INBOARD FLAP ACCESS FAIRING, CANOE, DEEP SCRATCHES, PAINT CHIPPED, HAD A SMALL AIR BUBBLE ON THE SURFACE AND IN NUMEROUS PLACES THE WAS CHIPPED OFF. IN ATTENTION TO THE REPORTS THE FAIRING AND RADOME WERE REPAIRED IAW SRM 51-10-3B AND THE ACTUATOR FLAP WAS REWORKED IAW 53-10-01, ALL CORRECT. (M) 2L72 4F RTA6WE 20030723000672003072300067NM 2003 7 23 SWAA031464 120030702A3350D1494 CONNECTOR BOEING737 7372H4 138448CNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EVACUATION LIGHT INOP. RESEATED EMERGENCY LIGHT BATTERY ASSY CONNECTOR D1494. OPS CK GOOD. 2L72 4F A16WE 20030723000692003072300069NM 2003 7 23 SWAA031466 120030703A55526959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEV TAB NR 1 HINGE ATTACH BUSHING PER MM AND SI. 2L72 4F RTA16WE 20030723000812003072300081NM 2003 7 23 AWXA200300798 120030706A53206548687 ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK 1 INCH CRACK WAS FOUND ON LT WHEEL WELL FORWARD CUTOUT FAIRING SUPPORT ANGLE BS 679. MAINTENANCE CUT OUT DAMAGED AREA OF FAIRING SUPPORT ANGLE AT BS 679; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12 PG 1-7 FIG 1. 2L72 4F RTA16WE 20030723000872003072300087 2003 7 23 DL757030496 420030528A3440 ANTENNA BOEING757 757232 1384965NM WX RADAR SYS MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27637DL 23760 RADAR INDICATOR PAINTS AND TESTS ONLY 30 DEG LEFT OF CENTER /C TRY INDICATOR AND T/R NO HELP. REPLACED ANTENNA, OPS CHECKS GOOD. 2L72 4F RTA2NM 20030723000892003072300089NM 2003 7 23 AWXA200300636 120030514A5330507945164 SKIN BOEING737 737277 1384570NM DOOR FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND AT L-1 DOOR ON THE AFT EDGE OF THE CENTER DOOR STOP ACCESS HOLE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 51-40-2, FIG 1. 2L72 4F RTA16WE 20030723000932003072300093EU 2003 7 23 AWXA200300640 120030518A5321D5367002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 MCN - MAJOR REPAIR - DURING C-03 CHECK PASSENGER CABIN FLOOR PANEL 251LF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 251LF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D53670022; INSTALLED REPAIR PART IAW T/C R1C25306 AND SRM 53-02-00 PG 233-236 FIG 209. 2L72 4F RTA28NM 20030723001012003072300101 2003 7 23 AWXA200300585 420030526A341746502003030312 ADC AIRBUSA319 A319132 3930340NM E/E BAY DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28812AW7852 40 1178 ON CLIMBOUT, EN ROUTE WHLE SELECTING FLAPS UP THE CAPTAINS PRIMARY FLIGHT DISPLAY INDICATED A BROKEN POLE OF 230 KTS, AND THE OVERSPEED WARNING HORN WOULD GIVE A CONTINUOUS ALARM IF THE AIRSPEED EXCEEDED 230 KTS. TURNED BACK TO RDU AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW AWA T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDOR EVALUATION TEST OF ADIRU S/N 2891 WAS NFF, TEST CONDUCTED IAW CMM TP1011, REV 22. 2L72 4F RTA28NM 20030723001052003072300105NM 2003 7 23 DL76L030500 120030530A5753 RIB BOEING767 767332 1382001NM LT WING TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27178DN 25143 LT INBOARD AFT FLAP TRAILING EDGE WEDGE LEADING EDGE RIBS WERE FOUND WITH OVERSIZED HOLES. HOLES REPAIRED PER ER/A 423104-14 (NORDAM EWO'S E0043938 AND E0043943). 2L72 4F RTA1NM 20030723001122003072300112 2003 7 23 SWAA031473 420030703A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030723001162003072300116NE 2003 7 23 DL73K030504 220030602A7200 ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15 52051NE NR 1 MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27311DL48119 23083 709119 ENG FUEL FLOWS WERE 1500 SPLIT AFTER TAKEOFF. TRIED ENG ANTIICE ON AND MISMATCH ON THROTTLES REVERSED. EPR ON LEFT ENG 1.40 AND ON RIGHT ENG WAS 1.77. AFTER CONSULTATION WITH MAINTENANCE COORDINATOR AND DISPATCH, DIVERTED TO MCO. DUPLICATED ITEM ON R/U. REPLACED NR 1 ENG NOSE DOME. LEAK CHECK NBR 1 PT2 LINE, RAN ENGS 1 AND 2 PER PFHB. ALL CHECKS NORMAL. 2L72 4F4 FRTA16WE E2EA 20030722000052003072200005NM 2003 7 22 2003F00433 120030309A5522 SKIN BOEING727 727222 1384073NM RT ELEVATOR BURNED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND STATIC DISCHARGE BURN, RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. CUT OUT DAMAGED AREA ON RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. FABRICATED DOUBLERS AND FILLER. TREATED AND PRIMED PARTS. INSTALLED REPAIR PARTS. (M) 2L73 4F A3WE 20030722000722003072200072NM 2003 7 22 SWAA031461 120030701A56105593543129 WINDOW BOEING737 7372T4 1384492NM COCKPIT CRACKED A SWAAO OTHER O OTHER CRCRUISE 1 SW29702ML 22054 CAPT'S NR 1 WINDOW ARCING AND CRACKED. REMOVED AND REPLACED NR 1 WINDOW PER MM. 2L72 4F A16WE 20030722000882003072200088EU 2003 7 22 AWXA200300788 120030617A5315D5347217220000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT FR 66, Y1292. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7 & 29-30. 2L72 4F RTA28NM 20030723000592003072300059 2003 7 23 GTIA030484 420030623A2565 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 R1 SLIDE PACK BROKEN. RESECURED LANYARD ON R1 DOOR SLIDE PACK. NO DEFECTS NOTED AT THIS TIME. (M) 2L72 4F RTA6WE 20030723000822003072300082NM 2003 7 23 AWXA200300655 120030523A53306545765 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH .25 INCH CRACKS WERE FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 RT, BS 500B+1, BS 500B+2, AND BS 500B+15. MAINTENANCE CUTOUT AND REMOVED CRACKED SKIN AT STR 4 RT, BETWEEN BS 500A+18 & BS 500B+4, AND BS 500B+13 & BS 500B+16; PERFORMED A HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH DOUBLERS, 2 EACH FILLERS, 2 EACH INTERNAL DOUBLERS, AND A TAPERED FILLER; INSTALLED REPAIR PARTS BS 500A+18 - BS 500B+17 IAW B737-300 SRM 53-00-01PG 362, FIG 228. 2L72 4F RTA16WE 20030723000962003072300096NM 2003 7 23 AWXA200300771 120030702A3350362624 LAMP BOEING737 7373U3 13844CCNM SEAT ROW 7 MISSING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 28740 DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT STRIP AT SEAT ROW 7 WAS FOUND MISSING. MAINTENANCE INSTALLED A NEW REPLACEMENT EMERGENCY ESCAPE PATH LIGHT STRIP AT SEAT ROW 7 IAW BMM 33-51-81, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030723001172003072300117NM 2003 7 23 DL73S030505 120030530A5311652072270 FRAME BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 THE SUBJECT DOOR FRAME WAS FOUND CRACKED AT THE INTERSECTION OF FS 440 AND STR 24R. THE FRAME WAS ORIGINALLY 0.071 INCH 7075-T6 CLAD. THE CRACK WAS TRIMMED OUT, STEEL REPAIR ANGLES WERE INSTALLED, AND TWO DOOR STOP FITTINGS WERE MODIFIED TO ALLOW FOR THE INSTALLATION OF THE REPAIR PARTS PER DAL ER/A 385003-14. 2L72 4F RTA16WE 20030723001282003072300128EU 2003 7 23 AWXA200300625 120030502A5320D5397490500000 PROFILE AIRBUS320 A320231 3930325EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT CENTER FLOOR PROFILE STR 38 LT TO STR 38 RT, FR-50. MAINTENANCE REMOVED CENTER FLOOR PROFILE FROM STR 38 LT TO STR 38 RT, FR-50; FABRICATED A NEW REPLACEMENT CENTER FLOOR PROFILE; INSTALLED REPAIR PART IAW AWA ER 26-5341-03142-TB5. 2L72 4F RTA28NM 20030723001322003072300132EU 2003 7 23 AWXA200300695 120030612A3397D43636 SPLICE AIRBUS320 A320231 3930325EU SEAT ROW 9 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED SPLICES ON WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030723001332003072300133NM 2003 7 23 DL738030514 120030604A5610 SEAL BOEING737 737832 13844CFNM WINDSCREEN LEAKING A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27382DA 30345 RETURN TO DFW DUE TO COCKPIT WINDSCREEN DRAIN LINE CAUGHT IN F/O SLIDING WINDOW. EXTREMELY LOUD COCKPIT NOISE ABOVE 18K FT. REPOSITIONED SAME. 2L72 4F RTA16WE 20030724000232003072400023NM 2003 7 24 AWXA200300686 120030514A5753657193086 SKIN BOEING737 737277 1384570NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK THE RT OUTBOARD HINGED FLAP TRAILING EDGE WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGE AND PERFORMED COMPOSITE REPAIR IAW BAC5514-589/5101 AND DWG 65-71930. 2L72 4F RTA16WE 20030724000252003072400025NM 2003 7 24 AWXA200300667 120030518A575465C26602217 SKIN BOEING737 73733A 1384673NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT FASTENER HOLES ON NR 2 SLAT LOWER LEADING EDGE. MAINTENANCE CUTOUT DAMAGED AREA NR 2 SLAT LOWER LEADING EDGE; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 PG 216-219 FIG 206. 2L72 4F RTA16WE 20030724000272003072400027NM 2003 7 24 DL738030528 120030607A2613106200817 SENSOR BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 2 ENGINE WORN A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO273761R 29628 888497 RIGHT ENGINE BLEED TRIP OFF. T/S PER FIM 36-10-TASK-801. HOOKED UP AIR SOURCE PER FIM. NO LEAKS NOTED. RECONNECTED MUSCLE LINE AT TEE. REPLACED HIGH PRESSURE BLEED 390 TEMP SENSOR AND 490 TEMP SWITCH PER M/M. PERFORMED PNEUMATIC CHECK OUT PER PFHB. OP CKS GOOD. RAN ENGINE AT 80 P/C FOR 5 MINUTES. NO BLEED TRIP. 2L72 4F4 FRTA16WE E00055EN 20030724000302003072400030NM 2003 7 24 DL73S030531 120030609A5753 SKIN BOEING737 737232 1384475NM LT WING TE FLAP DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 LT OUTBOARD AFT FLAP T/E WEDGE DISBONDED. T/E WEDGE REPAIRED PER ER/A 423067-14. 2L72 4F RTA16WE 20030724000682003072400068NM 2003 7 24 AWXA200300765 120030629A2120213N110310 DUCT BOEING757 7572S7 1384962NM ZONE 126 BLOWN A AWXAGBA O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 WP28904AW 23566 ON CLIMBOUT AT FL 190 HEARD A LOUD BANG AND FELT AIRCRAFT SHUDDER. CHECKED PRESSURIZATION AND FOUND OUTFLOW VALVE WAS IN FULL CLOSED POSITION, CABIN PRESSURE WAS CLIMBING. MANUALLY DEPLOYED OXYGEN MASKS & MADE EMERGENCY DESCENT. DECLARED EMERGENCY & TURNED BACK TO PHX. MX FOUND A BLOWN DUCT IN RT A/C PACK BAY, REMOVED & REPLACED DUCT ASSEMBLY IN RT PACK BAY, LEAK CHECK WAS GOOD. THE CHECK VALVE THAT PREVENTS REVERSE AIRFLOW FROM THE MIX MANIFOLD ALSO FAILED, FLAPPER DISK WAS TORN OFF HINGES & FOUND WEDGED IN DUCTING. REMOVED & REPLACED CHECK VALVE ASSEMBLY, OPERATIONAL CHECK GOOD. REPLACED ALL OXYGEN MASKS & GENERATORS. 2L72 4F RTA2NM 20030724000742003072400074NM 2003 7 24 AWXA200300696 120030614A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM ZONE 900 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28831AW 1576 FLIGHT CREW REPORTED THAT THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030724000792003072400079EA 2003 7 24 JBXA03014 120030702A300011513361 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYS FAILED A JBXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05261BD 7137 UPON DEPARTURE FROM CHS ANTI-ICE DUCT MESSAGE ALERTED WHEN WING ANTI-ICE SELECTED DIVERTED INTO RDU. REMOVED AND REPLACED WING ANTI-ICE CONTROL UNIT IAW AMM 30-12-19 AFTER FOLLOWING CL-65 FIM 30-10-00 PG 108, OPS CHECK GOOD. 2L72 4F RTA21EA 20030724000992003072400099NM 2003 7 24 AWXA200300757 120030629A3320059341 BALLAST BOEING737 7373G7 1384595NM CABIN LIGHTS ODOR A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28302AW 24009 PRIOR TO PUSHBACK FLIGHT ATTENDANT REPORTED AN ELECTRICAL BURNING ODOR AND PASSENGER CABIN LIGHTS INOPERATIVE ABOVE SEAT ROW 12 LT. MAINTENANCE FOUND SIDEWALL LIGHT BALLAST AT SEAT ROW 12 LT INOPERATIVE, DEACTIVATED AND SECURED BALLAST AND ISSUED MEL 33-2, C-1, CABIN LIGHT INOP. MAINTENANCE. REPLACED THE LIGHT BALLAST AT SEAT ROW 12 L/H, OPERATIONAL CHECK OF SIDEWALL LIGHTS AT LH SEAT ROW 12 WAS GOOD. 2L72 4F RTA16WE 20030724001042003072400104NM 2003 7 24 DL733030563 120030619A53126545658578 BULKHEAD BOEING737 737347 1384647NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311WA 23597 CORROSION WAS FOUND ON THE FWD SIDE OF THE AFT PRESSURE BULKHEAD. THE DAMAGE IS TO THE WEB AND STIFFENER AT THE BOTTOM OF THE BULKHEAD AT BL 0 AND STA 1016. DAL ER/A 385133-14AD PROVIDES INSTRUCTIONS TO REPAIR THE WEB AND STIFFENER PER BOEING SB 737-53A1075, AS MANDATED BY AD 2002-10-11. 2L72 4F RTA16WE 20030724001062003072400106NM 2003 7 24 DLM88030566 120030621A5280 DOOR DOUG MD88 MD88 3023688NM NLG LIGHTNING STRIKEA DALAO OTHER O OTHER APAPPROACH 1 SO27958DL 49977 SUSPECT AIRCRAFT STRUCK BY LIGHTNING ON APPROACH. FOUND CORNER OF RIGHT NOSE GEAR FLYING DOOR WITH EVIDENCE OF LIGHTNING STRIKE. BURNISHED AREA PER SRM, OK FOR SERVICE. 2L72 4F RTA6WE 20030724001102003072400110NM 2003 7 24 DLM88030570 120030621A2781 SENSOR DOUG MD88 MD88 3023688NM LEFT WING STICKING A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27981DL 53268 AFTER TAKEOFF WHEN SLATS WERE RETRACTED, THE DISAGREEMENT LIGHT REMAINED ON. ALL OTHER INDICATIONS AND POSITIONS NORMAL. T/S AND FOUND SENSOR D32 ON LEFT WING STICKING. LUBRICATED SAME, OPS CHECK NORMAL PER M/M. 2L72 4F RTA6WE 20040227000532004022700053NM 2004 2 27 ASAA0490001 120031207A1430512GU3K10 SCREW BOEING737 737990 NM MLG MISSING A ASAAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 NM01315AS 30019 SEA - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION. LEVER WOULD NOT RETURN TO THE DOWN POSITION, WHEN ATTEMPTED TO MOVE BY CREW. 6 GREEN LANDING GEAR INDICATOR LIGHTS AND 3 RED LIGHTS ILLUMINATED THEN ACCOMPANIED THIS. RETURNED TO SEA AND LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR CONTROL LEVER MODULE. FOUND 3 SCREWS AND WASHERS THAT SECURED TELEFLEX CABLE ASSEMBLY TO REAR OF CONTROL LEVER MODULE MISSING. INSTALLED MISSING HARDWARE, OPS CHECKED SYSTEM, OPS CHECKED GOOD. APPEARS SCREWS WERE NOT INSTALLED ORIGINALLY DURING AIRCRAFT ASSEMBLY. (M) 2L74 4F RTA16WE 20040301000282004030100028EU 2004 3 1 PG92004F00006 120031117A7160 STRUCTURE UROCOPEC130 EC130B4 8680989EU AIR INTAKE CRACKED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19131GC489 M265790 3691 AIR INTAKE ASSEMBLY CRACKED. (RMA NR R045785) (K) 1G72 3U H9EU 20040301000452004030100045NE 2004 3 1 EGR2004F00000 220030205A7230JBS2211 COMPRESSOR SKRSKYS76 S76B 8143007NE PWA PT6 PT6A36 52043NE PULLEY SHAFT CRACKED E EGRAO OTHER O OTHER NRNOT REPORTED 1 EA17549G 760448 COMPRESSOR PULLEY SHAFT CRACK AT WOODRUFF KEY. 1G72 4U4 T H1NE E4EA 20040301000462004030100046EU 2004 3 1 EGR2004F00001 120030802A6210365A11005007 BLADE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1C 60030NE MAIN ROTOR FAILED E EGRAO OTHER O OTHER NRNOT REPORTED 1 EA17798LL3019 6102 MAIN ROTOR BLADE FAILED. CONTINUITY TEST BETWEEN LEADING EDGE AND GROUND STRAP BOLT. 1G72 3U3 U H10EU E19EU 20030825000172003082500017NM 2003 8 25 UPS03440979 120030711A3350 LIGHT BOEING747 747123 1384873NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:N/A MAIN DECK CARGO AREA HAS AFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY EXIT LIGHT ASSY OPS CKS OK AS IAW MM 33-51-07. 2L74 4F A20WE 20030825000512003082500051NM 2003 8 25 UPS03641134 120030820A3230 LANDING GEAR BOEING767 76734AF 1385212NM NLG NOISY A IPXAO OTHER O OTHER CRCRUISE 1 SO01308UP 27761 INSPECTION TYPE:N/A INC SDF - NOSE GEAR NOISE ON RETRACTION. CREW DELARED AN EMERGENCY ON ARRIVAL AT SDF. INSPECTED NOSE WHEEL AREA FOR ANY SIGN OF DEFECT, NONE FOUND. LUBED NOSE GEAR STRUT AND DOORS. RETRACTED SEVERAL TIMES, NO DEFECTS NOTED. 2L72 4F RTA1NM 20030825000592003082500059WP 2003 8 25 UPS03841139 120030821A2150 ACM DOUG DC8 DC873F 302199FWP A/C BAY DEFECTIVE A IPXAB EMER. DESCENT O OTHER DEDESCENT 1 SO01868UP 45968 INSPECTION TYPE:N/A WILL NOT MAINTAIN PRESSURIZATION. EMERGENCY DELARED AND REQUESTED IMMEDIATE DESCENT PER EVENT REPORT. FOUND LEFT ACM TEMP UNCONTROLLABLE. R/R'D LEFT ACM PER 21-55-01-4 OPS CHECKS GOOD. 2L74 4F RT4A25 20030825000632003082500063NM 2003 8 25 UPS03441074 120030810A3350900835A BATTERY BOEING747 747212B 1384886NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE:A CK CREW SERVICE DOOR EMERGENCY LIGHTS INOP. FOUND BATTERY DEAD. REPLACED BATTERY PACK ASSY. 2L74 4F A20WE 20030825000832003082500083NM 2003 8 25 03FDEA01224 120030722A5315 FLOORBEAM BOEING727 7272S2F 1384O81NM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 BS 740 FLOORBEAM UPPER CHORD CHAFED ALONG AFT EDGE LBL 44 RBL 44 WL 208. R/R FLOORBEAM. 2L73 4F A3WE 20030825000902003082500090WP 2003 8 25 03FDEA01243 120030810A3610 BRACKET DOUG DC10 DC1030 3023501WP NR 3 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 233 ENG HP TURBINE COOLING PNEUMATIC DUCT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW AMM 70-00-00-2. 2L73 4F A22WE 20030825001072003082500107NM 2003 8 25 234TR0009 120030725A272065C370539 PCU BOEING737 737228 13844AGNM RUDDER MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 YAW DAMPER REPORTED WILL NOT STAY ENGAGED. SHOWS FAULT HISTORY MESSAGE 22-21003. REPLACED RUDDER POWER CONTROL UNIT PER MM 27-21-91 AND PERFORMED ADJUSTMENT AND TEST PER MM 27-21-91. YAW DAMPER CHECKS NORMAL PER MM 22-12. 2L72 4F RTA16WE 20030825001332003082500133SO 2003 8 25 C2XA03IA076 120030804A335020131A BATTERY PACK EMB 145 EMB145 3260210SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. IAH- MAINTENANCE RESECURED THE NR 2 BATTERY PACK, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030825001342003082500134SO 2003 8 25 C2XA03SH288 120030824A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED OMEGA BEAM IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030826000052003082600005WP 2003 8 26 03FDEA01354 120030821A5753ANB7170 SUPPORT DOUG DC10 DC1010 3022110WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 RIGHT INBOARD FLAP-INBOARD FLAP SUPPORT OVERSIZED HOLE REPAIR P/N 7170, COMPLY WITH EA 8-5750-72263 ENT BY: 497234 RPT BY: 497234 FACT 21AUG03 15:14 BFM R COMPLIED WITH EA 8-5750-72263 ENT BY: 497191 RPT BY: 497191. 2L73 4F A22WE 20030826000162003082600016NM 2003 8 26 03FDEA01289 120030806A5744ARC0502404 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) FOUND CORROSION ON PIVOT HOLE AT BORE AND SPOT FACES. RIGHT WING OUTBOARD FLAP INBOARD HINGE (A/C SIDE) PIVOT HOLE BORE AND SPOT FACES (FWD & AFT FACES) REPAIR AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030826000782003082600078NM 2003 8 26 CALA0300475 120030821A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND FLOOR SUPPORT CORRODED JUST AFT OF STA 947.5, LBL 30 TO LBL 40. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030826001022003082600102SO 2003 8 26 CTU2003F00006 120030523A2510 SUPPORT BRACKET MAULE M7 M7260C 5470112SO LYC O540 IO540* 41532EA PILOT SEAT BROKEN B CTURK NONE O OTHER ININSP/MAINT 1 GL215500E1055 30026C WHILE INSPECTING THE AIR DURING AN ANNUAL INSPECTION THE TECHNICIAN FOUND THE PILOT SEAT SUPPORT BRACKET TO BE CRACKED, WHICH ALLOWED THE SEAT STOP BRACKET TO MOVE AWAY FROM THE LOCKING POSITION WHEN A PERSON IS IN THE PILOTS SEAT. THIS ALLOWED THE SEAT STOP TO BE IN A POSITION IN WHICH IT DID NOT ALLOW A POSITIVE SEAT LOCKING FUNCTION. IF THE SEAT WAS IN ANY POSITION OTHER THAN FULL AFT IT COULD WITHOUT WARNING MOVE TO THE FULL AFT POSITION WHICH COULD PUT THE PILOT IN A POSITION NOT TO HAVE FULL CONTROL OF THE AIRCRAFT. 1H71 3O3 ONC3A23 1E4 20030826001272003082600127WP 2003 8 26 03FDEA00982 120030627A5753 BUSHING DOUG DC10 DC1030 3023501WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 NR S-20 COMPLY WITH EA 8-5750-70945, FOR LT INBD FLAP OUTBD HINGE SUPPORT. ON 06/24/03. RECEVIED BUSHINGS IAW MAE TRAVELERS T2/343779@T2/343901.INSTALLED BUSHINGS IAW CMM 57-52-01. COMPLIED WITH EA 8-5750-70954. 2L73 4F A22WE 20030826001582003082600158WP 2003 8 26 WX030010 120030725A3350 COVER DOUG DC9 DC983 3022083WP CABIN LOOSE A WXOAK NONE O OTHER ININSP/MAINT 1 WP17860GA 49786 DURING ACCOMPLISHMENT OF A SERVICE CHECK IN LAS, MAINTENANCE FOUND EMERGENCY TRACK FLOOR LIGHTS COVER LOOSE AT ROW 25 THE COVER WAS RE-SECURED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20030826001602003082600160WP 2003 8 26 WX030009 120030723A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WXOAK NONE L NO TEST ININSP/MAINT 1 WP17860GA 49786 DURING ACCOMPLISHMENT OF SERVICE CHECK IN FAT, MAINTENANCE FOUND EMERGENCY TRACK FLOOR LIGHTS DAMAGED AT ROW 2, EMERGENCY FLOOR TRACK LIGHT AT ROW 12 BURNED OUT, AND FLOOR TRACK AT ROW 24 LOOSE. THE FLOOR TRACK LIGHTING AT ROW 24 WAS REPLACED AS REQUIRED. THE LAMPS WRE REPLACED AT ROW 12. THE FLOOR TRACK WAS SECURED AT ROW 24 AS REQUIRED. OPS CHECKS WERE SATISFACTORILY PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20030827000012003082700001NM 2003 8 27 03FDEA00995 120030628A534053FX14281 FITTING BOEING727 727200 138407ENM MAIN CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25463FE 22551 MDIS 463 53-10 0005658 24JUN03 BFM CLOSE R COMPLY WITH EA NR 7-5310-70960, FUSELAGE - MAIN CARGO DOOR ACTUATOR FITTING GOUGE REPAIR P/N 53FX1428-1. FACT 27JUN03 13:57 BFM R COMPLIED WITH EA NR 7-5310-70960,FUSELAGE-MAIN CARGO DOOR ACTUATOR FITTING GOUGE REPAIR P/N 53FX1428-1. 2L73 4F RTA3WE 20030827000042003082700004EU 2003 8 27 03FDEA00958 120030623A5320A5381293220100 FLOOR SUPPORT AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 NR 378 MCD FLOORBOARD SUPPORT FRAME 46 CRACKED RBL 35. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20030827000082003082700008NM 2003 8 27 03FDEA00840 120030523A5744ARC0503503 HINGE FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0769: LT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FWD FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR'S UPPER LUG MOUNT HOLES, LT AND RT WITH BORE SURFACE CORROSION (WING SIDE FITTING). SNRM N0769: REPAIR CARRIED-OUT AS PER CMM 57-44-09 AND FEDEX EA 1-5740-71707 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030827000192003082700019WP 2003 8 27 03FDEA00943 120030621A5753ARC2761 BRACKET DOUG DC10 DC1030 3023501WP T/E FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 NR S 22 LT INBD FLAP BRACKET ASSY, GOUGED COMPLY WITH E.A.8-5750-70945. CLOSING ACTION ON 06/20/03. COMPLIED WITH E.A.8-5750-70945.WINGS-LT INBD FLAP-BRACKET ASSY GOUGE REPAIR P/N ARC2761. 2L73 4F A22WE 20030827000592003082700059SO 2003 8 27 RKW2003F00000 220030606A7414M3984 CONDENSER SLICK CESSNA206 TU206F 2073353CE CONT O520 TSIO520C 17040SO MAGNETO SHORTED E RKWAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM111953U828 U20602306 178573R FLYING OVER MOUNTAINS, ENGINE BEGAN TO RUN ROUGH. DIVERTED, RIGHT MAGNETO CONDENSER FOUND TOTALLY SHORTED. ON RUN UP AFTER MAINTENANCE, LEFT MAGNETO RAN ROUGH, ENGINE NEARLY DIED FROM 1700 RPM. CHANGED OUT LEFT MAGNETO CONDENSER. OPS CHECKED GOOD. (MAG CHECK BEFORE 1.3 HOUR FLIGHT WAS GOOD). 1H71 3O3 O A4CE E8CE 20030827000772003082700077SO 2003 8 27 C2XA03CL142 120030809A2730 ELEVATOR EMB 145 EMB145LR 3260212SO FLIGHT CONTROL MALFUNCTIONED A C2XAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW2713903* 145479 GRR FLIGHT NR 2584 THE CREW REPORTED ON SHORT FINAL APPROXIMATELY 500' ABOVE GROUND THE ELEVATORS COULD NOT BE MOVED FORWARD OR AFT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT IAW EMBRAER IC 2003-145/2694A. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS REPORTED. AIRCRAFT RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030827000802003082700080SO 2003 8 27 C2XA03TY091 120030723A531514526437001 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27129467512 145052 TYS, DURING A SCHEDULED INSPECTION THE RIGHT CENTER FLOORBEAM WAS FOUND CORRODED UNDER THE AFT WALL COMPOSIT FLOOR SUPPORT. MAINTENANCE REMOVED AND REPLACED THE CENTER LAV FLOORBEAM CAP. I/A/W-EMB-145-SRM-51-40-02, THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF THE INSPECTION. 2L72 4F RTT00011AT 20030827000912003082700091SO 2003 8 27 C2XA03CL123 120030711A3350744437 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715973 145159 CLE FLIGHT NR 3389 THE CREW REPORTED THE LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030827000952003082700095SO 2003 8 27 C2XA03SH271 120030817A531514521721005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV DURING C CHECK FOWARD DIGITAL WAS FOUND TO HAVE CORROSION DOWN THE CENTER LINE BETWEEN FRAMES 15 AND 18. MAINTENANCE REPAIRED AFFECTED DIGITAL IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030827000972003082700097SO 2003 8 27 C2XA03BT079 120030809A3350220131A BATTERY EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714945 145049 EWR---CO2573, CREW REPORTED DURING PREFLIGHT, EMERGENCY LIGHTS WERE INOPERATIVE......MAINTENANCE REMOVED AND REPLACED BATTERY AND REPAIRED BROKEN WIRE. (IAW EMB145 MM NR 33-50-01) OPS.CHECKED SYSTEM GOOD. 2L72 4F RTT00011AT 20030827001392003082700139NM 2003 8 27 2003UALA00553 120030714A3350 BATTERY PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29178UA 24385 RT UPPER DECK EMERGENCY BATTERY PACK NO TEST. REPLACED BATTERY PACK. 2L74 4F4 FRTA20WE E24NE 20030827001662003082700166 2003 8 27 MALA030366 420030802A34426227337001 TRANSCEIVER SAAB SF340 340B 7860101EU WEATHER RADAR FAULTY A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15410XJ 340B410 DURING FLIGHT NR 3252 WEATHER RADAR WOULD NOT PAINT KNOWN WEATHER. AIR RETURN TO MEM. MAINTENANCE SET SECTOR KNOB TO RADAR RANGE AND PERFORMED WEATHER RADAR CONTROL PANEL OPS CHECK. IAW SF340 AMM 34-42-00-2 CND DISC. OK FOR SERVICE. REPLACED WX RADAR R/T WXT-250B PN OFF/ON 622-7337-001, SN/OFF 4483 SN/ON 4722. OP TEST GOOD IAW AMM 34-42-00-2 2L72 4T RTA52EU 20030827001862003082700186SO 2003 8 27 C2XA03TY128 120030818A53151452246013 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED THE CORRODED AREA AND ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 51-40-02 AND 53-21-10, ALSO CPM 51-21-04,05,06. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030827001882003082700188SO 2003 8 27 C2XA03CL152 120030825A3350110049 CHARGER EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716944 145045 DURING ROUTINE CHECK MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT SIDE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY BATTERY AND BATTERY CHARGER. OPERATIONAL CHECKS GOOD. 2L72 4F RTT00011AT 20030826000092003082600009NM 2003 8 26 03FDEA01358 120030822A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 EMPENNAGE SKIN GOUGED, STA 1348, 12 INCHES ABOVE LEFT AFT AIRSTAIR CORNER. REMOVED DAMAGE AT SKIN AT BS 1348. FOUND TO BE OUT OF LIMITS. FABRICATED THE REPAIR DOUBLER, AND INSTALLED THE REPAIR PART IAW SRM 54-30-3. 2L73 4F RTA3WE 20030826000882003082600088EU 2003 8 26 YENA200308 120030609A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15505JB 1173 SMELLED ODOR DESENDING THROUGH FL300; F/A CONFIRMED. SWITCHED OVER TO APU BLEED AT LOWER ALT, F/A CONTINUED TO SMELL & FELT SICK. CREW DID NOT SMELL ANYMORE. F/A NR 2 USED PORTABLE OXYGEN BOTTLE. ON ARRIVAL CHECKED NR 1 & 2 ENGINE INLET & EXHAUST AREA, CHECKED NR 1 & 2 PACK INLETS & EXHAUST AREA, CHECK APU INLET & EXHAUST AREA. ALL CHECK CLEAN & NO LEAKS DETECTED. REMOVED AND REPLACED NR 1 PACK'S OZONE FILTER PER 21-51-41-401. FILTER CHECKED CLEAN (REINSTALLED SAME FILTER). GAIN ACCESS TO RECIRCULATION FILTER PER 21-21-41, CK'D GOOD. CHECK LAV AND GALLEY FILTER, CHECK CLEAN. RAN PACKS FOR 2 HRS, SYSTEM CHECKED NORMAL. NO ODOR DETECTED. REMOVED AND REPLACED FWD / LT POB PER 35-11-41. LEAK CHECK GOO2L72 4F RTA28NM 20030826000952003082600095 2003 8 26 T2B2003F00000 420030516A6122 ROLL PIN PIPER PA60 PA60600 7106001NM LYC O540 TIO540* 41532EA PROP GOVERNOR MISSING E T2BAO OTHER O OTHER APAPPROACH 1 SW0590609 600320118 L1196548A ON APPROACH, PILOT LOST CONTROL OF PROPELLER. PROPELLER WOULD NOT CHANGE PITCH OR FEATHER. PILOT LANDED WITHOUT INCIDENT. ENGINE AND PROPELLER EXPERIENCED OVER SPEED BY 25 PERCENT. ENGINE PROPELLER REMOVED FOR TEARDOWN INSPECTION PROPELLER REMOVED FROM SERVICES DUE TO AMOUNT OF OVER SPEED. TEARDOWN INSPECTION OF GOVERNOR REVEALED THAT A ROLL PIN REQUIRED BETWEEN SPOOL EXTENSION (PN A-3167) AND SPOOL (PN B3166) TO BE MISSING NO PIECES FOUND IN GOVERNOR. 1M72 3O3 ORTA17WE E14EA 20030826001682003082600168SO 2003 8 26 SWIA200312111 120030617A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO CABIN DISCHARGED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07212SW6046 6046 120276 EMERGENCY LIGHTS ''EXIT'' SIGNS ROW 6 ILLUMINATE ONLY VERY BRIEFLY THEN EXTINGUISH. REMOVED AND REPLACED ROW 6 BATTERY PACK. OPS CHECK GOOD ON EMERGENCY LIGHTS. 2L72 4T RTA31SO 20030827000032003082700003EU 2003 8 27 03FDEA00959 120030623A5420A5461139220600 PANEL AIRBUS300 A300B4605R 3930308EU GE CF6 CF680 30025NE NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 NR 593 NE 2 PYLON PRECOOLER PANEL 423 BL CRACKED LT AND RT FWD CORNERS OF SEAL BACKUP PLATE. REMOVED AND REPLACED CRACKED WEB IAW SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20030827000072003082700007NM 2003 8 27 03FDEA00853 120030602A5514ALC8103 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0938 - RT HORZ STAB BARREL NUT BORE NR 35 CORROSION BLEND OUT, OUT OF LIMIT. CORRECTIVE ACTION: SNRM N0938: RH HORIZONTAL STABILIZER BARREL NUT BORE NR 35 CORROSION BLEND OUT AREA CARRIED-OUT REPAIR AS IAW EA 1-5510-71716 - STABILIZER - HORIZONTAL STABILIZER - REWORK OF HOLE 35R, REFERENCE EO 1-5510-7-5000. 2L73 4F RTA22WE 20030827001102003082700110NM 2003 8 27 CALA0300410 120030724A55536938716501 BUSHING BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE VERTICAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT I/B FORWARD AND AFT AND RT I/B AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE IAW DRAWING NR 65-46872. 2L72 4F4 FRTA16WE E2GL 20030827001122003082700112NM 2003 8 27 CALA0300361 120030703A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT STA 1006 BETWEEN RBL 24 AND RBL 32 AND RBL 27 INTERCOSTAL BS 1006-1016. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 202, PAGE 207-211. 2L72 4F RTA16WE 20030827001142003082700114NM 2003 8 27 CALA0300363 120030706A5320 ANGLE BOEING757 757224 1384958NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717122 27564 INSPECTION FOUND ANGLES CRACKED IN LT AND RT MLG WHEEL WELLS AT BS 1097 AT LOWER CORNER OF CENTER CUTOUT. THE CRACKS WERE 0.2 INCH AND 0.5 INCH LONG. THE ANGLES WERE REPAIRED IAW ECRA 5352-01025. 2L72 4F RTA2NM 20030827001292003082700129NM 2003 8 27 CALA0300401 120030721A335020131A BATTERY PACK BOEING737 7373T0 1384582NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2747332 23570 THE EMERGENCY EXIT LIGHTS AT ROWS 21-25 AND THE LEFT, CENTER, AND RIGHT AFT EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REMOVED AND REPLACED M9101 EMERGENCY LIGHT BATTERY PACK PER MM 33-51-51. 2L72 4F RTA16WE 20030827001352003082700135NM 2003 8 27 2003UALA00544 120030708A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 CABIN FLOOR AT BS 852, RBL 56, TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030827001372003082700137NM 2003 8 27 2003UALA00524 120030627A3350M1137 CHARGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29351UA 24319 AFT SECTION EMERGENCY EXITING LIGHTS (EEL) INOPERATIVE. REPLACED AFT BATTERY CHARGER, BATTERY PACK AND AFT EEL STRIP 24 FT CABLE. OPS OK. 2L72 4F4 FRTA16WE E2GL 20030827001412003082700141NM 2003 8 27 2003UALA00555 120030714A5610 WINDOW BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT UNSECURE A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29548UA 25396 FIRST OFFICER'S WINDOW SQUEAL ON FLIGHT DECK DURING CLIMB. ATTEMPTED TO OPEN AND CLOSE DURING CLIMBOUT. DISCOVERED A LOOSE SEAL COMING OUT OF TRACK WHICH PREVENTED THE WINDOW FROM CLOSING PROPERLY. SEAL WAS REINSTALLED IN TRACK AND WINDOW OPERATED NORMALLY. 2L72 4F4 FRTA2NM E17NE 20030827001462003082700146NM 2003 8 27 2003UALA00539 120030706A7930 WARNING SYSTEM BOEING777 777222 1385219NM PWA PW4077PW4077 NE COCKPIT ACTIVATED A UALAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29774UA 26936 LOST LEFT OIL QUANTITY AND PRESSURE. ENGINE SHUTDOWN. THE MAIN GEARBOX IDLER SHAFT BEARING FAILED AT ITS INNER RACE. CONFIGURATION WAS POST SB PW4G-112-72-149. THIS SB WAS INTRODUCED TO PREVENT SPINNING OF THE SPUR GEAR ON THE OUTER RACE. FAILURE OF THE INNER RACE ALLOWED THE REMAINDER OF THE BEARING AND SPUR GEAR TO SPIN ON THE IDLER SHAFT. THEREFORE, DRIVE TORQUE TO THE DE-OILER WAS LOST. THIS RESULTED IN OIL EXITING THE ENGINE THROUGH THE OVERBOARD BREATHER PORT. 2L72 4F4 FRTT0001SE E46NE 20030827001482003082700148 2003 8 27 2003UALA00543 420030703A2565 O-RING BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE SLIDE BOTTLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29951UA 26696 UPON ARRIVAL FOUND BOTTLE PRESSURE ON SLIDE AT DOOR 1R BELOW THE GREEN BAND. LEAKING O-RING BETWEEN RESERVOIR AND VALVE/REGULATOR CAUSED REDUCED BOTTLE PRESSURE. REPLACED SLIDE BOTTLE, INSPECTED/TESTED REMOVED BOTTLE TO DETERMINE CAUSE, THEN OVERHAULED VALVE INCLUDING REPLACEMENT OF DEFECTIVE O-RING. 2L72 4F4 FRTA16WE E2GL 20030827001622003082700162EA 2003 8 27 QXEA200300936 120030715A5751 AILERON CNDAIRCL600 CL6002C10 1390015EA LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 PDX- LEFT AILERON BOTTOM FORWARD HAS CHAFE 12 INCHES FROM INBOARD EDGE. REPAIRED IAW CRJ SRM 51-20-06, 51-25-01 AND 51-21-11. 2L72 4F RTA21EA 20030828000092003082800009WP 2003 8 28 ARWA20030320 120030315A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK THE FOLLOWING WAS FOUND; FS 1606 AFT PRESSURE BULKHEAD TEE CAP WITH 8 INCH CRACK BTW L-9L AND L12L. CUT LONGERONS 11L, 12L AND 13L AND REMOVED SPLICES (OPEN), CUT DAMAGED AREA OF FRAME IAW DC8 SRM 53-2-0, PREPARED NEW FRAME SEGMENT IAW BOEING ATM. TREATED AND PRIMED REPAIR AREA AND PARTS IAW DC8 SRM 51-1-8, INSTALLED FRAME SEGMENT AND REINSTALLED SPLICES (4 EACH) IAW DC8 SRM 53-2-0, FABRICATED LONG SPLICES (3 EACH) IAW DC8 SRM 53-2-2, TREATED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED LONG SEGMENT AND SPLICES IAW SRM 53-2-0. 2L74 4F 4A25 20030902001822003090200182 2003 9 2 03FDEA01092 420030711A3454959960714901 ALTERNATOR AIRBUS300 A300F4605R 3930327EU COCKPIT FAILED A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25670FE 777 PDIS 670 34-54 0005194 10JUL03 CWF CLOSER GPWS TERRAIN PULL-UP" OCCURED ON FINAL WITH GEAR AND FLAPS 40 FACT, 11JUL03, 12:46 CWFU REMOVED AND REPLACED RADIO ALT NR 2 IAW A300-600 AMM 34-42-33-4 OPS CHECK GOOD IAW A300-600 AMM 34-71-00-5 AND 34-42-00-5. EGPWS SYSTEM CHECKS GOOD IAW A300-600 AMM 34-48-00-5. 2L72 4F RTA35EU 20030903000212003090300021EU 2003 9 3 03FDEA01097 120030714A5315 FLOORBEAM AIRBUS300 A300B4605R 3930308EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25659FE 757 FLOORBEAM CRACKED ON BEAM 27 FWD LOWER CARGO PIT 17 INCHES OF CENTRLINE. REPAIRED FLOORBEAM IAW A300-600 IAW ENG DISPO PAGE 2 AND 3. FAB 2 EA ANGLES IAW SRM 53-10-15,HFEC INSPECT IAW SRM 51-10-08. PENETRANT INSPECTION IAW SRM 51-90-00,PART ID PMS 01-06-08. ALODINE AND PRIME IAW SRM 51-21-10,SEALED PARTS SRM 51-76-10. TOPCOATED GREY IAW SRM 51-23-00. 2L72 4F RTA35EU 20030903000292003090300029EU 2003 9 3 PG9R103181 120030515A6321350A32501000 BRAKE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ROTOR BRAKE WARPED A PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19453NW165 2475 UNIT WAS INSTALLED ON MGB ASSY, SN M2518. ROTOR BRAKE ASSY, SN M1546 OF UNIT 350A32001100, SNM2518. ROTOR BRAKE WARPED. (REF; AEC WO NR 79881 4/7/03) 1G71 3U3 U H9EU E19EU 20030724000492003072400049NM 2003 7 24 DL76G030549 120030615A2781321001258 PROXIMITY SENSOR BOEING767 767332 1382001NM LE FLAPS FAULTY A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO271612T 30575 EN ROUTE TO LGW SLAT ASSY LIGHT ILLUMINATED AND FLAP POSITION INDICATOR BEGAN BOUNCING BETWEEN 0 AND .5 DEGREE. A/C HAS EXTENSIVE HISTORY OF THIS PROBLEM. A/C DIVERTED TO JFK AS A PRECAUTION. FAULTS 276285 CARD 10 CARD AND SW PREV REPLACED. REPLACED PS BITE CK OK. INSPECTED CONNECTOR P4434J FOUND SILVER PINS INSTALLED. PINS FREE AND CLEAR OF CORROSION AND CLEAN. REINSTALLED CONNECTOR. 2L72 4F RTA1NM 20030724000542003072400054 2003 7 24 SWAA031440 420030629A25656557463 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED C3 CHECK, FOUND LOOSE RIVETS AT FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER HOOK. REMOVED AND REPLACED RETAINER HOOK RIVETS PER SRM. 2L72 4F RTA16WE 20030724000692003072400069NM 2003 7 24 AWXA200300766 120030629A3520785801 ACTUATOR BOEING757 7572S7 1384962NM ZONE 200 DEFECTIVE A AWXAB EMER. DESCENT O OTHER DEDESCENT 1 WP28904AW 23566 DURING EMERGENCY DESCENT AFTER MANUAL DEPLOYMENT OF OXYGEN MASKS, SEVERAL MASKS FAILED TO DEPLOY. FLIGHT ATTENDANT MANUALLY DEPLOYED MASKS AT SEAT ROW 2, 4 & 12 AND LAVATORIES A & C. MAINTENANCE REPLACED SOLENOIDS (ACTUATORS) AT SEAT ROWS 2, 4 & 12 AND LAVATORIES A & C; PERFORMED OXYGEN MASK DEPLOYMENT TEST IAW BMM 35-21-00 PG 501 AND T/C F1C35601. 2L72 4F RTA2NM 20030724000752003072400075 2003 7 24 AWXA200300697 420030614A2565D30665105 SLIDE AIRBUS320 A320231 3930325EU R-2 DOOR TORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW411483702 064 DURING C-04 CHECK FOUND THE R-2 DOOR SLIDE LACING TORN. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR SLIDE IAW T/C R1C25304MT-82. 2L72 4F RTA28NM 20030724000782003072400078NM 2003 7 24 AWXA200300701 120030615A2612PPA120100 SMOKE DETECTOR AIRBUSA319 A319132 3930340NM LAVATORY DEFECTIVE A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP28823AW8007 1463 AT CRUISE RECEIVED CARGO SMOKE DETECTOR ECAM FAULT. F/A CHECKED LAV`S FOR SMOKE, SMELLED BURNING PLASTIC IN FWD LAV, BUT NO SMOKE WAS PRESENT. DIVERTED TO ABQ. MX FOUND LOWER ECAM HAD INFO SDCU NR 2 INOP, MESSAGE CLEARED. TROUBLESHOT SYSTEM USING TSM 26-17-00-810-802 (SDCU SINGLE CHANNEL FAULT): NO DEFECTS NOTED. INSPECTED FWD LAV O2 CONTAINER, FIRE BOTTLE, TEMP STRIP, HOT WATER HEATER, AND LIGHTS, FOUND NO SIGNS OF FIRE OR MELTED PLASTIC. MX FERRIED BACK TO PHX, AND A FUP WAS WRITTEN TO REPLACE ALL CARGO & LAV SMOKE DETECTORS. REPLACED 3 EACH LAVATORY SMOKE DETECTORS IAW 26-17-00, & 6 EACH CARGO SMOKE DETECTORS. 2L72 4F RTA28NM 20030724000902003072400090EU 2003 7 24 AWXA200300729 120030607A5210FE1740011 CYLINDER DAMPER AIRBUS320 A320231 3930325EU R-2 DOOR INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW4019 052 DURING C-04 CHECK THE R-2 DOOR DAMPER CYLINDER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR DAMPER CYLINDER IAW AMM SUBTASK 52-13-14-020-050. VENDOR TEARDOWN OF R-2 DOOR DAMPER CYLINDER S/N 215 FOUND UNIT HEAVILY CONTAMINATED DUE TO LEAKAGE AT FRONT AND REAR CUPS, AND ALSO HAD DETERIORATED SEALS ON THE PERCUSSION & BOTTLE ASSEMBLIES. UNIT OVERHAULED PER CMM 52-11-03, AND S/B FE174-52-1, 2, 3R1 WAS ACCOMPLISHED. 2L72 4F RTA28NM 20030724000912003072400091EU 2003 7 24 AWXA200300730 120030624A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU POS 4, ZONE 263 DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW1987710153 543 DURING 8-DAY CHECK THE EMERGENCY LIGHT SYSTEM FAILED TEST AT PROGRAM AND TEST PANEL. PRODUCED THE FOLLOWING CODES IN ADDITION TO SYSTEM NOT OK LIGHT: 115VAC R, 115VAC L, AFT L, EMER R, EMER L, & AFT L. MAINTENANCE REMOVED AND REPLACED 3 EACH EMERGENCY POWER SUPPLY UNITS (LT OVERWING 11WL, RT OVERWING 12WL, & AFT 13WL), OPERATIONAL CHECK WAS GOOD PER T/C F1C33301. PART NAME; ESPU (11WL), MFG; DIEHL GMBH, P/N; 3214-54, S/N; 493, LOC; POS 2 ZONE 241, TT; 34520, TC; 16142, TSR 10281. PART NAME; ESPU (12WL), MFG; DIEHL GMBH, P/N; 3214-54, S/N; 6583, LOC; POS 3 ZONE 242, TT; 19571, TC; 12872, TSR 10992. 2L72 4F RTA28NM 20030724000932003072400093EU 2003 7 24 AWXA200300732 120030623A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 221 DEFECTIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28670AW24 2029 FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS AT L-1 & R-1 DOOR ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK OF EXIT LIGHTS WAS GOOD. 2L72 4F RTA28NM 20030724000962003072400096NM 2003 7 24 DL757030561 120030618A5410311N31551 FITTING BOEING757 757232 1384965NM NR 1 PYLON CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 DURING THE ACCOMPLISHMENT OF SIP MODIFICATION, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LT DOUBLER OF THE MID SPAR INSTALLATION. REPAIRED PER: ER/A 385115-14AD. 2L72 4F RTA2NM 20030724001012003072400101NM 2003 7 24 AWXA200300759 120030625A5320657374183 STIFFENER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A .1875 INCH CRACK WAS FOUND ON VERTICAL STIFFENER AT FORWARD SIDE OF FLOORBEAM BS 328, BL 0, WL 208. MAINTENANCE REMOVED CRACKED VERTICAL STIFFENER AT FORWARD SIDE OF FLOORBEAM BS 328, BL 0; FABRICATED A NEW REPLACEMENT VERTICAL STIFFENER PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 10-11 & 45, FIG 12. 2L72 4F RTA16WE 20030724001032003072400103EU 2003 7 24 AWXA200300761 120030611A5320D5348002043700 WEB AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 MCN - MAJOR REPAIR - DURING C-04 CHECK A 6 INCH CRACK WAS FOUND ON FLOOR WEB BETWEEN FR 68-69, Y-1270. MAINTENANCE REMOVED DAMAGED FLOOR WEB BETWEEN FR 68-69, Y-1270; FABRICATED A NEW REPLACEMENT FLOOR WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-12 FIG 2. 2L72 4F RTA28NM 20030724001292003072400129NM 2003 7 24 DLM88030577 120030623A3260 SENSOR DOUG MD88 MD88 3023688NM NLG MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27904DL 49535 RED NOSE GEAR LIGHT ON AFTER HANDLE PLACED UP POSITION. REPLACED NOSE GEAR UP SENSOR. 2L72 4F RTA6WE 20030722000012003072200001NM 2003 7 22 2003F00429 120030312A5330 SKIN BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT LOWER FORWARD CORNER SKIN CRACKED. STOP DRILLED CRACK ON RIGHT FORWARD GALLEY DOOR CUTOUT, FORWARD, LOWER CORNER SKIN. FABRICATED DOUBLER AND TRIPLER. TREATED, PRIMED AND INSTALLED DOUBLER AND TRIPLER ON FORWARD GALLEY DOOR CUTOUT, FORWARD LOWER CORNER. (M) 2L73 4F A3WE 20030722000932003072200093NM 2003 7 22 AWXA200300725 120030614A5320654529624 SPLICE BOEING737 7373Y0 1384671NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK CORROSION WAS FOUND ON CARGO FLOOR PANEL ATTACH ANGLE (SPLICE STRAP) AT BS 860, RBL 18.5, WL 166. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED CORRODED SPLICE STRAP AT BS 860, RBL 18.5, WL 166; FABRICATED A NEW REPLACEMENT SPLICE STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 2-3 & 38 FIG 8. 2L72 4F RTA16WE 20030723000152003072300015NM 2003 7 23 TSAA0353138 120030505A5330 SKIN BOEING737 73725A 1384481NM FUSELAGE DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DISCOVERED A 15 INCH GOUGE WITH A DENT LOCATED AT BS 981 THROUGH BS 996, 4 INCHES ABOVE STRINGER 4 LT. CUTOUT GOUGE AND DENTED PORTION OF THE SKIN. FABRICATED DOUBLER AND TRIPLER, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48. 2L72 4F RTA16WE 20030723000222003072300022NM 2003 7 23 KPVA200329 120030621A33506104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A KPVAK NONE O OTHER ININSP/MAINT 1 WP13805WP 353 EMERGENCY LIGHTS INOPERATIVE, PS2. REMOVED AND REPLACED POWER SUPPLY PS2 IAW DHC MM 33-51-00 PAGE 201-22 SECT 1A. OPS CHECK GOOD IAW DHC MM 33-51-00 PAGE 201-202 SECT 2A. (M) 2H72 4T RTA13NM 20030723000292003072300029NM 2003 7 23 USAABB03105 120030627A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030723000362003072300036 2003 7 23 UIEA200300029 420030625A34232591201921 COUPLER BOEING747 7472F6B 1384807NM COMPASS FAILED A UIEAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15535MC 21833 DURING TAKEOFF ROLL, HEADING FLAG ON CAPTAIN'S HSI AND FO'S RMI. AIRCRAFT DIVERTED TO AMS, 23,000 KGS OF FUEL DUMPED. INSTALLED TEMP SPAR WIRE FROM D2206P TO DB105, WING TIP TO WIG DISC, AND REPLACED BOTH COMPASS COUPLER NR 1 AND FO'S RMI IAW MM 34-12-00, RMI P/N 2594661-801. (M) 2L74 4F A20WE 20030723000522003072300052WP 2003 7 23 GTIA030475 120030513A5753 SKIN DOUG DC9 DC981 3022081WP TE FLAPS CHAFED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 LEFT WING INBOARD FLAP, OUTBOARD VANE BARE METAL AT LOWER SURFACE AND CHAFED ON FIXED TRAILING EDGE. DISCOVERED CRACK ON BOTTOM SIDE OF VANE. ON REMOVAL OF RUBSTRIPS, FOUND SKIN DELAMINATION. REPAIRED DELAMS UNDER RUBSTRIPS. (M) 2L72 4F A6WE 20030723001042003072300104NM 2003 7 23 DL76L030499 120030529A3350 BULB BOEING767 767332 1382001NM LT AND RT WING INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO271201P 28458 EXTERIOR EMERGENCY EXIT LIGHTS, 1 BULB INOP, 1 LT AND 2 RT OVERWING EXIT LIGHTS. RELAMPED, OPS CHECK NORMAL. 2L72 4F RTA1NM 20030724000062003072400006NM 2003 7 24 DLM88030522 120030606A2611SAAU308C SMOKE DETECTOR DOUG MD88 MD88 3023688NM LAVATORY MALFUNCTIONED A DALAO OTHER N FALSE WARNING LDLANDING 1 SO27947DL 49878 AFT LEFT LAV SMOKE DETECTOR CHIRPING. REPLACED SAME. 2L72 4F RTA6WE 20030724000152003072400015NM 2003 7 24 AWXA200300666 120030519A5313BAC1498157 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT BOTH SIDES OF LIGHT HOUSING ON STRINGER 16 LT, BS 500C&D. MAINTENANCE CUTOUT DAMAGE AT BOTH SIDES OF LIGHT HOUSING ON STRINGER 16 LT, BS 500C&D; FABRICATED A REPAIR CHANNEL, 2 EACH SPLICE ANGLES, AND 4 EACH SHIMS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 PG 201 FIG 201. 2L72 4F RTA16WE 20030724000422003072400042NM 2003 7 24 DL738030541 120030612A3244B737800NLG TIRE BOEING737 737832 13844CFNM NLG SEPARATED A DALAB EMER. DESCENT C F.O.D. CLCLIMB 1 SO27380DA 30266 RT NOSE TIRE RECAP SEPARATED ON T/O FROM COS. ON ARRIVAL IN ATL FOUND RECAP SEPARATED, TIRE PRESSURE GOOD 195 PSI. UPON FURTHER INSPECTION FOUND NR 2 ENG FOD DAMAGE, RT NLG DOOR FWD HINGE BROKEN, NLG W/W FWD BULKHEAD RT LOWER CORNER DENTED. REPAIRED DAMAGE, REPLACED WHEEL ASSY. 2L72 4F RTA16WE 20030724000662003072400066EU 2003 7 24 AWXA200300763 120030612A5320D5347048120050 PROFILE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON RT PROFILE IN AFT CARGO COMPARTMENT AT FR 51+17, STR 37 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF PROFILE AT FR 51+17, STR 37 RT; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE, A DOUBLER, AND SPLICE; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1. 2L72 4F RTA28NM 20030724001112003072400111NM 2003 7 24 DL757030571 120030622A256061020 BATTERY BOEING757 757232 1384965NM L1 ENTRY DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27628DL 22918 EMERGENCY FLASHLIGHT RED LED DOES NOT BLINK AT L1 MED. REPLACED BATTERY, OPS NORMAL. REINSTALLED STRAP. 2L72 4F RTA2NM 20030725000012003072500001NE 2003 7 25 DL757030580 220030623A7320 TAILPIPE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE FIRE A DALAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 SO27633DL40667 716553 23614 716553 DURING NR 2 ENGINE START DURING/AFTER PUSHBACK FROM GATE, TAILPIPE FIRE OCCURRED. FIRE SELF-EXTINGUSHED ON ENGINE START. NO COCKPIT WARNINGS WERE NOTED BY THE FLIGHT CREW. HOWEVER PASSENGERS PANICKED AND DEPARTED THE AIRCRAFT THRU EMERGENCY EXITS. ALL SLIDES PERFORMED AS DESIGNED. REPLACED EEC PER AMM DUE TO FAULT CODE. 2L72 4F4 FRTA2NM E17NE 20030725000072003072500007NM 2003 7 25 AWXA200300753 120030627A532069353521 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 RT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 616, STR 2 RT IAW B737-300 SRM 51-40-02 PG 3-4 & 38 FIG 8. 2L72 4F RTA16WE 20030725000182003072500018NM 2003 7 25 XNOA01123 120030530A3260 WARNING LIGHT BOEING727 727227 1384078NM MLG ILLUMINATED A XN0AO OTHER J WARNING INDICATION CLCLIMB 1 GL2376753 21249 AFTER GEAR RETRACTION ALL 3 RED GEAR UNSAFE LIGHTS ILLUMINATED WITH GEAR LEVER IN GEAR UP POSITION. ALSO TAIL SKID LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. ALL LIGHT EXTINGUISHED. CONTINUED TO KRDU. 2L73 4F A3WE 20030725000252003072500025EU 2003 7 25 RAIA00305135 120030507A3397 WIRE AEROSPATR42 ATR42300 8680920EU EMERGENCY LIGHT BROKEN A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03421TE 102 5621-STL- EMERGENCY LIGHT OUT ON STAIRS. REPAIRED BROKEN WIRE AT STAIR EMERGENCY LIGHT. 2H72 4T RTA53EU 20030728000042003072800004NM 2003 7 28 SWAA031563 120030714A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 6, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030728000092003072800009NM 2003 7 28 VNAA0307003 120030715A36200132ADK SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BLEED AIR SYS FAILED A VNAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07459PS20851 3070 DURING CRUISE FLIGHT THE FLIGHT CREW EXPERIENCED STATIC ON BOTH VHF RADIOS AND A FAILING LEFT HIGH PRESSURE BLEED VALVE. AFTER CONFERING WITH MAINTENANCE CONTROL THE CREW DIVERTED TO DAYTON. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED BOTH SPEAKER VOLUMES FOR THE VHF RADIOS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 23-00-00 AND REPLACED THE LEFT HIGH PRESSURE BLEED TEMPERATURE SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-21. FUNCTIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030728000172003072800017NM 2003 7 28 SWAA031532 120030711A27316545166 ROD END BOEING737 7377H4 1384404NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 DURING SCHEDULED C4 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB ROD END HARDWARE PER MM. 2L72 4F RTA16WE 20030728000192003072800019NM 2003 7 28 SWAA031534 120030711A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727D + 6, FROM RBL 3 TO LBL 12. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030728000202003072800020NE 2003 7 28 SWAA031535 220030712A7200CFM56 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 1 MALFUNCTIONED A SWAAK NONE Y ENGINE STOPPAGE LDLANDING 1 SW29313SW 23335 724528 NR 1 ENGINE QUIT ON LANDING ROLLOUT AFTER COMING OUT OF REVERSER THRUST. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030728000302003072800030NM 2003 7 28 SWAA031578 120030717A3350604222 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29713SW 27847 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030728000702003072800070NM 2003 7 28 SWAA031529 120030711A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728000812003072800081 2003 7 28 SWAA031581 420030717A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030728000862003072800086 2003 7 28 SWAA031640 420030723A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29747SA 29799 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030723000852003072300085NM 2003 7 23 AWXA200300665 120030519A5313BAC1498139 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD SIDE OF STRINGER END AT BS 500C, STR 16 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER AT BS 500C, STR 16 RT; FABRICATED A REPAIR CHANNEL AND 2 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 PG 201 FIG 201. 2L72 4F RTA16WE 20030723000902003072300090NM 2003 7 23 AWXA200300637 120030514A53116545871515 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON R-1 DOOR FRAME AT AFT NR 4 STOP FITTING CUTOUT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC TO VERIFY CRACK WAS CONTAINED, ALODINED AND PRIMED IAW B737-200 SRM 51-10-2 PG 7. 2L72 4F RTA16WE 20030723000982003072300098EA 2003 7 23 COMA0360321 120030714A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01973CA 7146 FLIGHT 5007 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL. 2L72 4F RTA21EA 20040114000342004011400034NE 2004 1 14 AWXA200300698 220030614A7530 ACTUATOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE VARI STATOR VANELOOSE A AWXAEA ENGINE SHUTDOWN UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 WP28624AW 55 V0084 TEARDOWN REPORT OF ENG IDENTIFIED HIGH INTERNAL LEAKAGE AT VSV ACT ALONG WITH SLOW PISTON VELOCITY. TEARDOWN REVEALED THAT CONTROL SERVO VALVE & SEAL WERE WORN BEYOND LIMITS & CAUSED INTERNAL LEAKAGE AT VSV ACT. FAILURE MODE & EFFECTS ANALYSIS CONSIDER THIS A MAJOR FAILURE & WOULD RESULT IN CSV TO M 2L72 4F4 FRTA28NM E311NE 20030828000152003082800015WP 2003 8 28 ARWA20030317 120030315A5347 CARGO TRACK DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA 740, RBL 45, TRACK WITH CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3, CUT AWAY DAMAGED SECTION OF TRACK AND FABRICATED SPLICES IAW DC8 SRM 53-2-3, PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW DC8 SRM 53-2-3. 2L74 4F 4A25 20030828000262003082800026EU 2003 8 28 00099 120030619A2730 ELEVATOR AMD FALC20FALCON 2720302EU FLIGHT CONTROLS MALFUNCTIONED E HAEAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW05204TW 204 PILOT REPORTED ELEVATOR FELT SOFT ON TAKEOFF AND ABORTED. MAINTENANCE INSPECTED ELEVATOR AND CONTROLS WITH HYDRAULICS ON/OFF PER THE FALCON M/M FOUND TO BE WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A7EU 20030828000312003082800031WP 2003 8 28 IXXA0300040O 120030604A7931 PRESSURE SWITCH DOUG DC8 DC862 3021970WP NR 1 ENGINE SHORTED A IXXAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SW11799AL727461470 45922335 ON CLIMB FROM KTOL TO KNGU, NR 1 OIL PRESSURE LIGHT CAME ON WITH NORMAL PRESSURE INDICATION. CREW PERFORMED ABNORMAL CHECKLIST. AIRCRAFT LANDED AT KNGU WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL PRESSURE SWITCH IN ACCORDANCE WITH THE DOUGLAS AIRCRAFT MAINTENANCE MANUEL. OIL FILTER INSPECTED OK. RAN NR 1 ENGINE PER ATI ENGINE RUN HANDBOOK. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20030828000442003082800044NM 2003 8 28 XNOA01126 120030430A3260 WARNING SWITCH BOEING727 727227 1384078NM RT MLG DOOR OUT OF ADJUST A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL23793A 20774 AFTER T/O KMDT WITH GEAR UP AND HANDLE IN OFF POSITION, RED RIGHT MAIN DOOR LIGHT ILLUMINATED. ALL CHECKLISTS COMPLETED. RED DOOR LIGHT WENT OUT. ADJUSTED RT MLG DOOR WARNING SWITCH. OPS CHECK OK PER B727 MM 32-62-11. 2L73 4F A3WE 20030828000602003082800060NM 2003 8 28 P5CA03009023 120030819A5420 STRUCTURE BOEING747 747200 1384847NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 NR 4 PYLON SLOT CUT OUT HAS APPROX .5000 INCH CRACK AT THE IB UPPER AFT CORNER. CORRECTIVE ACTION TAKEN: CRACK TRIMMED IAW SECT 3 OF 54-2034. NO CRACK VISIBLE AFTER TRIM OUT. EXTERNAL DOUBLER INSTALLED ON THE INBND SIDE OF PYLON IAW SB 54-2034. 2L74 4F RTA20WE 20030828000622003082800062NM 2003 8 28 P5CA03000918 120030819A575365B02093202 SKIN BOEING747 747200 1384847NM T/E FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 RT INBND MID FLAP - DELAMINATION AT MID UPPER FLT PNL. CORRECTIVE ACTION: PANEL NR 65B02093-202 INTERNAL DISBONDED SKIN REMOVED AND NEW SKIN BONDED IN PLACE SRM 51-40-05. 2L74 4F RTA20WE 20030828000642003082800064NE 2003 8 28 P5CA0300911 220030811A7200 ENGINE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 3 POWER LOSS A P5CAK NONE R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23923FT 22769 702370 NR 3 ENG STALL CONDITION AFTER DESCENT FROM FL 330. PERFORMED FULL NR 3 ENG INSP. SUMPED ALL FUEL TANKS. CHECKED AND INSPECTED EVBC SCREEN. CHECKED FCU LINES FOR SECURITY AND NO LEAKAGE. PERFORMED ENG RUN ALL PARAMETERS IND NORMAL TO, OK TO CONTINUE SRVC. IAW MM 71-00-00 & 73-00-00 2L74 4F4 FRTA20WE E3NE 20030828000752003082800075NE 2003 8 28 DL76L030659 220030717A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 SURGES A DALAK NONE A FLAME/FIRE CLCLIMB 1 SO27199DN18865 28456 727830 NBR 1 ENGINE SURGED DURING CLIMB AT FL230. FLAMES REPORTED BY PAXS AND F/A. ENGINE RECOVERED AND NORMAL INDICATIONS. ENGINE CHANGE IN PROGRESS. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2L72 4F4 FRTA1NM E24NE 20030828000792003082800079NM 2003 8 28 DL73S030666 120030718A53126546547212 PRESSURE PANEL BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 FUSELAGE STA 727 BLKHD, MLG WW, UPPER CHORD - REPAIR: A 0.5 INCH CRACK WAS PREVIOUSLY REPAIRED IN TEH UPPER CHORD OF THE SUBJECT BULKHEAD NEAR BL 0. THE CRACK WAS IN THE UPPER FLANGE OF THE COMPRESSION CHORD AND RAN THROUGH A FASTENER HOLE. DURING THE CURRENT HMV, THE TIME LIMITED REPAIR WAS REMOVED AND, DUE TO ADDITIONAL DAMAGE FOUND, THE COMPRESSION CHORD, THE UPPER CHORD, THE COMPRESSION STRAP AND THE LT FLOOR WEB WERE TRIMMED OUT AND A REPAIR ANGLE, WEB DOUBLER AND SPLICE STRAP WERE INSTALLED IAW DAL ER/A 368710-14. 2L72 4F RTA16WE 20030828000952003082800095NM 2003 8 28 DL73S030688 120030720A5342 ATTACH FITTING BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 DURING ACCOMPLISHMENT OF INSPECTIONS IAW SB 737-55-1028 (DAL EO 3-85220-3), CORROSION WAS FOUND ON FIVE (5) VERT STABILIZER CLEVIS LUGS AND THREE (3) VERT STABILILZER ATTACH LUGS. THE BORES WERE OVERSIZED AND THE LUG FACES MACHINED TO REMOVE CORROSION. O/S BUSHINGS WERE INSTALLED IAW SB 737-55-1028. ER/A 385290-14 WAS ISSUED TO ADDRESS THESE 8 LUGS THAT WERE MACHINED BEYOND THE SERVICE BULLETIN LIMITS. 2L72 4F RTA16WE 20030828000972003082800097NM 2003 8 28 DLM88030622 120030709A26136712152180 SENSOR DOUG MD88 MD88 3023688NM A/C BAY FAULTY A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27948DL 49879 IR: TAIL COMPARTMENT TEMP HI LIGHT CAME ON AT 400 FT. REPLACED TAIL TEMP HI SENSOR. RAN ENGINES TO TAKEOFF POWER. ALL INDICATIONS NORMAL. 2L72 4F RTA6WE 20030828001142003082800114WP 2003 8 28 MWEA030278 120030715A533059102285 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 3 CRACKS IN FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERON 3L AND LONGERON 5L. FABRICATED AND INSTALLED DOUBLER AND FILLERS. 2L72 4F A6WE 20030827001872003082700187SO 2003 8 27 C2XA03TY131 120030818A532014521725013 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD SERVICE DOOR SILL. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB GST NR 1907/20A AND EMB CPM 51-21-04, 05, 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030827001892003082700189SO 2003 8 27 C2XA03SH283 120030821A532014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 58 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030828000082003082800008WP 2003 8 28 ARWA20030319 120030315A5310 DOOR FRAME DOUG DC8 DC862F 3021972WP FUSELAGE DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT DOOR JAMB UPPER WEB BROKEN STA 360, L-6L. CUT OUT DAMAGED AREA IAW DC8 SRM 53-2-0, FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-0, PRIMED FILLER AND DOUBLER IAW DC8 SRM 51-1-8 AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-0. 2L74 4F 4A25 20030724000882003072400088EU 2003 7 24 AWXA200300727 120030623A332032507010 BALLAST AIRBUS320 A320231 3930325EU SEAT ROW 21 FAULTY A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28626AW 65 FLIGHT ATTENDANT REPORTED A BURNING RUBBER ODOR ABOVE SEAT ROW 20. MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST UNIT ABOVE SEAT ROW 21 RT IAW AMM 33-21-11; OPERATIONAL CHECK WAS GOOD, NO ODOR NOTED. 2L72 4F RTA28NM 20030725000032003072500003NM 2003 7 25 DL73K030582 120030624A2560MV10 MEGAPHONE BOEING737 737232 1384475NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27327DL 23099 ON PREFLIGHT FWD MEGAPHONE INOP. REPLACED MEGAPHONE. 2L72 4F RTA16WE 20030728000182003072800018NM 2003 7 28 SWAA031533 120030711A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, FROM LBL 3 TO LBL 12. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030728000612003072800061NM 2003 7 28 SWAA031636 120030722A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 8L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030728000802003072800080NM 2003 7 28 SWAA031580 120030715A53116545819139 FRAME BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED C3 CHECK, FOUND T-CHORD CRACKED AT TOP NOSE WHEEL WELL FWD CENTER BEAM AT BS 230. REMOVED AND REPLACED T-CHORD AND WEB PER SRM. 2L72 4F A16WE 20030728000902003072800090NM 2003 7 28 SWAA031614 120030720A57536546435227 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED C3 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED ON INBD EDGE. REMOVED AND REPLACED LT OUTBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030728000932003072800093NM 2003 7 28 SWAA031574 120030717A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (3 EA) AT BS 500D AT STR 4R, BS 500B AT STR 9L AT BS 727C AT STR 7L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030728000992003072800099NM 2003 7 28 SWAA031620 120030721A53306545800 BEAR STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SPECIAL VISIT, FOUND BEAR STRAP CRACKED AT BS 360, ABOVE STR 14R. REPAIRED BEAR STRAP PER SRM. 2L72 4F RTA16WE 20030728001042003072800104NM 2003 7 28 SWAA031587 120030716A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728001072003072800107NM 2003 7 28 SWAA031624 120030721A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND BOTH LT AND RT OUTBD FRAMES CRACKED AT BS 188, WL 207. REMOVED AND REPLACED BOTH LT AND RT FRAMES PER SRM. 2L72 4F RTA16WE 20030728001262003072800126NM 2003 7 28 SWAA031430 120030627A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728001352003072800135NM 2003 7 28 A6WA200300844 120030628A2121731376 COOLING FAN BOEING757 75723N 1384973NM E/E BAY MALFUNCTIONED A AMTAK NONE J WARNING INDICATION UKUNKNOWN 1 GL11516AT 27972 FLT 102 - EQUIPMENT COOLING OVERHEAT LEGEND ILLUMINATED WITH 'EQ CLG GAN' STATUS MESSAGE. WORKS OK IN ALT MODE. REMOVED AND REPLACED FAN AND FILTER. REF AMM 21-58-06-04 AND 21-58-07-4. (M) 2L72 4F RTA2NM 20030728001362003072800136NM 2003 7 28 AMTA200300850 120030630A3397 WIRE BOEING757 75723N 1384973NM CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11525AT 30548 EMERGENCY EGRESS LIGHTS OUT INOPERATIVE AT ROW 15 TO 21. RECONNECTED EGRESS WIRE AT ROW 15, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030729000072003072900007EA 2003 7 29 03199626 120030718A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27626BR 7225 DURING MAINTENANCE INSPECTION, AN EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030729000132003072900013EA 2003 7 29 03202703 120030721A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27703BR 7467 DURING MAINTENANCE INSPECTION, AN EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030729000142003072900014EA 2003 7 29 03188663 120030707A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27663BR 7527 DURING MAINTENANCE INSPECTION, AN INTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000162003072900016NM 2003 7 29 03199451 120030718A33508GH00567806 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27451FJ 3205 DURING MAINTENANCE INSPECTION, THE LAV EMERGENCY LAMP WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAV EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030729000312003072900031EA 2003 7 29 03163636 120030721A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27636BR 7307 DURING MAINTENANCE INSPECTION A SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A SECTION OF EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000322003072900032EA 2003 7 29 03198644 120030717A33503071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27644BR 7379 DURING MAINTENANCE INSPECTION, 2 EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LAMPS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000332003072900033EA 2003 7 29 03192641 120030711A2910 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA COCKPIT TRIPPED A VTZAB EMER. DESCENT F FLT CONT AFFECTED DEDESCENT 1 EA27641BR 7349 DURING DESCENT, THE FLIGHT CREW RECEIVED STAB AND MACH TRIM MSGS, AFTER LEVELING OFF THEY RECEIVED AP NOSE UP TRIM AND AP PITCH TRIM MSGS WITH NO SYSTEM CIRCUIT BREAKERS NOTICEBLY TRIPPED. CREW WAS UNABLE TO MAINTAIN ALTITUDE WITH AUTOPILOT ENGAGED, EMERGENCY WAS DECLARED AND AUTOPILOT WAS DISENGAGED. FLIGHT LANDED WITHOUT INCIDENT MAINTENANCE PERSONNEL DISCOVERED NR 1 HYDRAULIC SYSTEM CIRCUIT BREAKER TRIPPED. FUNCTIONAL AND OPERATIONAL CHECK OF THE STAB AND MACH TRIM SYSTEMS WERE PERFORMED WITH SATISFACTORY RESULTS AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000442003072900044NM 2003 7 29 ZW0A0305706 120030701A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13716TW 28484 THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS WERE ADJUSTED ACCOUNT DEFORMED AT THE L1, R1, L2, R2, L4, AND R4 CABIN DOORS. 2L72 4F RTA2NM 20030729000472003072900047NM 2003 7 29 ZW0A0305703 120030703A256069B148551 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13708TW 28480 THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRING WAS ADJUSTED ACCOUNT DEFORMED AT THE L1, R1, L2, R2, L4, AND R4 CABIN DOORS. 2L72 4F RTA2NM 20030729000522003072900052NM 2003 7 29 ZW0A0306101 120030722A256069B148553 SPRING BOEING757 7572Q8 1384972NM GIRT BAR BROKEN A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13713TW 28173 DURING CHECK-C THE EVACUATION SLIDE GIRT BAR LEAF RETENTION SPRING WAS FOUND BROKEN AND REPLACED AT THE L1 AND R1 CABIN DOORS. THE SPRINGS WERE FOUND DEFORMED AND REPLACED AT THE L2, R2, L4 AND R4 CABIN DOORS. 2L72 4F RTA2NM 20030729000542003072900054NM 2003 7 29 QXEA200300814 120030712A5542 SKIN BOMBDRDHC8 DHC8401 1390041NM RUDDER DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - TRAILING RUDDER HAS DAMAGE NINE RIBS DOWN FROM TOP OF TRAILING RUDDER. REPAIRED IAW SRM 51-25-05 AND EA 6-55-46. 2H72 4T RTA13NM 20030729000592003072900059EA 2003 7 29 QXEA200300849 120030718A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA PAX DOOR JAMMED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09603QX 10011 SMF- ON FLIGHT 2493 MAIN CABIN DOOR JAMMED. OPERATED DOOR SEVERAL TIMES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000602003072900060NM 2003 7 29 QXEA200300850 120030718A1430 BOLT BOMBDRDHC8 DHC8401 1390041NM LT MLG DOOR LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 BOI- ON FLIGHT 2364 DURING LINE CHECK, PULLING ALTERNATE RELEASE HANDLE, LEFT MAIN LANDING GEAR DOORS WOULD NOT OPEN. INSPECTED LINKAGE, PIVOT ASSMEBLIES, AND VALVES. SECURED LOOSE BOLT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030729000662003072900066NM 2003 7 29 QXEA200300829 120030709A5320 WEB BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - SUB FLOOR SKIN IS PULLED UP AT NUTPLATE UNDER AFT CARGO FLOOR PANEL 144AZ, INBOARD OF SEAT TRACK STATION X727. REPAIRED IAW HORIZON AIR EA 6-53-283. 2H72 4T4 TRTA13NM E00062EN 20030729000682003072900068EA 2003 7 29 QXEA200300810 120030702A5754 SEALANT CNDAIRCL600 CL6002C10 1390015EA L/E SLAT CHIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX - SEALANT CHIPPED AND POSSIBLE CORROSION ON FASTENER ON RIGHT LEADING EDGE UNDER SLAT. REPAIRED IAW EA R57-29 AND CRJ SRM 51-25-01. 2L72 4F RTA21EA 20030723001302003072300130EU 2003 7 23 AWXA200300693 120030429A5320D53911609200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MINOR REPAIR - DURING C-04 CHECK A .4375 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 28, LBL 28. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT AT FR 28, LBL 28; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND SPLICE REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1. 2L72 4F RTA28NM 20030724000082003072400008NM 2003 7 24 DLM88030525 120030606A3260 SWITCH DOUG MD88 MD88 3023688NM MLG INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27906DL 49537 NOSE WHEEL UNSAFE INDICATION AFTER TAKEOFF. FOLLOWED APPROPRIATE CHECKLIST STILL HAD UNSAFE INDICATION. NLG IND VISUAL INSPECTION CONFIRMED GEAR DOWN. RETURNED FOR LANDING. FOUND PROX SENSOR D1-32 INOP. REPLACED AND SWUNG GEAR. CHECKS OK PER M/M. 2L72 4F RTA6WE 20030724000142003072400014EU 2003 7 24 DHL2003366520 120030629A21701879421 COALESCER BAG AIRBUS300 A300B4203 3930306EU AIR DIST CLOGGED A DHLAO OTHER J WARNING INDICATION DEDESCENT 1 SO01366DH36541 249 CABIN SMOKE DETECTOR LIGHT R2 ILLUMINATED WITH SMOKE LIGHT ON MWP DURING STALL CHECKS WITH ODOR, THEN LIGHT WENT OUT AFTER 1 MINUTE. RAN SMOKE CHECKLIST MAIN CARGO DECK ISOLATION VALVE WENT AMBER & RT ISOLATION LIGHT WENT CROSSLINE. REMOVED AND REPLACED RT AND LT COALESCER BAGS PER A300 DHL MM 21-51-16. PERFORMED GROUND IDLE ENG RUNS HAD NO SMOKE SMELL OR INDICATING PER A300 DHL MM 21-00-00 PO 407168.1. 2L72 4F RTA35EU 20030724000572003072400057NM 2003 7 24 AWXA200300712 120030618A2560P2070001101 FLASHLIGHT BOEING757 7572G7 1384963NM L-2 DOOR DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 EMERGENCY EQUIPMENT - DURING 4-DAY CHECK FOUND THE EMERGENCY FLASHLIGHT AT L2 DOOR STATION INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT AT L2 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030724000802003072400080EU 2003 7 24 AWXA200300799 120030628A5415D54630462200 ATTACH ANGLE AIRBUS320 A320231 3930325EU LT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7. MAINTENANCE CUT OUT DAMAGE ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A320 SRM 54-52-12, PG 216-218. 2L72 4F RTA28NM 20030724000872003072400087NM 2003 7 24 DL757030557 120030618A5742012N88883 FITTING BOEING757 757232 1384965NM NR 1 NACELLE MISMANUFACTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 PYLON LEFT WING, PYLON BACKUP FITTING, NR 2 HOLE THE FACTORY HOLE ON THE FITTING DID NOT LINE UP WITH THE EXISTING HOLE IN THE WING. OPENED UP HOLE TO INSTALL BUSHING TO ALLOW INSTALLATION OF THE NEW FITTING. REINSTALLED THE ORIGINAL FASTENER TYPE. ER/A 385153-14AD 2L72 4F RTA2NM 20030724001022003072400102NM 2003 7 24 AWXA200300760 120030618A53206547973101 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 LCQ - MAJOR REPAIR - DURING C-13 CHECK 3 EACH .5 INCH CRACKS WERE FOUND ON WEB AT FLOOR LINE BELOW LT OVERWING EXIT CUTOUT BS 597, STR 17 LT. MAINTENANCE REMOVED CRACKED WEB BELOW LT OVERWING EXIT CUTOUT BS 616-639; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-47973; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-04 PG 1. 2L72 4F RTA16WE 20030724001122003072400112NM 2003 7 24 DL76G030572 120030622A2530 ODOR BOEING767 767332 1382001NM BUN WARMER DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271608 30573 MID GALLEY BUN WARMER OVERHEATED WITH STRONG ELECTRICAL SMELL. INSPECTED BUN WARMER, FOUND VERY HOT TO TOUCH, PULLED AND SECURED C/B AND FORWARD TO MCO AND PLACARD PER MEL 25-20-01B. 2L72 4F RTA1NM 20030724001212003072400121NM 2003 7 24 AWXA200300677 120030524A53306545765 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK 7 EACH .25 INCH CRACKS WERE FOUND ON FUSELAGE INTERIOR SKIN AT FASTENER HOLES ON LOWER ROW LAP SEAM STR 4 LT, BETWEEN BS 500B+9 AND BS 500B+19. UPON BOEING REQUEST TO EXTEND THE INSPECTION 1 EACH ADDITIONAL CRACK INDICATION WAS DETECTED AT BS 500A+13. MAINTENANCE TRIMMED OUT CRACKS ON SKIN AT STR 4 LT, BETWEEN BS 500A+13 AND BS 500B+19; FABRICATED A REPAIR DOUBLER, TRIPLER, 2 EACH FILLERS, AND 4 EACH INTERNAL DOUBLERS; INSTALLED REPAIR PARTS FROM BS 500A+10 TO 500C+2 IAW ER 03-5300-03155-TB2. 2L72 4F RTA16WE 20030725000082003072500008NM 2003 7 25 AWXA200300754 120030627A532069353521 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 1 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 616, STR 1 LT IAW B737-300 SRM 51-40-02, PG 3-4 & 38 FIG 8. 2L72 4F RTA16WE 20030725000112003072500011 2003 7 25 DL75K030585 420030625A2564D806627 LATCH BOEING757 757232 1384965NM RAFT BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO276714Q 30485 FLIGHT ATTENDANT REPORTS FWD OVERHEAD RAFT COMPARTMENT LATCH BROKEN. FOUND LIFE RAFT SLOWLY DEPLOYING IN ITS COMPARTMENT. REPLACED SAME. REPAIRED DOOR. 2L72 4F RTA2NM 20030725000282003072500028EU 2003 7 25 RAIA00305140 120030513A3150 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03565HK 41082 GOT TAKEOFF CONFIGURATION WARNING DURING TAKEOFF. MAINTENANCE OPERATIONAL CHECKED CONFIGURATION WARNING WITH NO DEFECTS NOTED. 2L72 4T RTA41NM 20030728000062003072800006NM 2003 7 28 SWAA031551 120030713A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030728001192003072800119NM 2003 7 28 DL757030593 120030625A2910271N67011066 HYDRAULIC LINE BOEING757 757232 1384965NM VERTICAL STAB CRACKED A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO27601DL 22808 SLOW HYD LEAKING LEFT SYSTEM OVER 3 HRS QTY WENT FROM NORMAL TO 0.24 AT LANDING. FOUND SYS 1 RUDDER RET LINE LEAKING IN VERT FIN 2 BAYS ABOVE STAB COMPARTMENT REPLACED WITH APPROVED FLEX LINE LEAK, OPS CHECK NORMAL. 2L72 4F RTA2NM 20030728001322003072800132NM 2003 7 28 AMTA200300898 120030707A26125816 FIRE DETECTOR BOEING757 75733N 1384931NM APU BAY FAULTY A AMTAK NONE N FALSE WARNING ININSP/MAINT 1 GL11559TZ 32593 EICAS STATUS MESSAGE 'APU FIRE LP2' DISPLAYED. REMOVED AND REPLACED UPPER DETECTOR ASSEMBLY PER MM 26-15-02. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030728001372003072800137WP 2003 7 28 AMTA200300811 120030504A5311 FRAME LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 FS 943 MESC FORWARD CUTOUT LOWER PART OF FORMER CORROSION. AREA WAS REPAIRED PER SRM 51-50-02 ON M12A 106843 ITEM 6 AND REPAIRED INTERNAL BONDED DOUBLER PER ERA L10-53R-5190. (M) 2L73 4F A23WE 20030729000122003072900012EA 2003 7 29 03185634 120030704A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27634BR 7287 DURING MAINTENANCE INSPECTION, THE FORWARD LEFT AND RIGHT EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000382003072900038NM 2003 7 29 ZW0A0305802 120030706A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13725TW 30338 THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS AT THE L4 DOOR WERE ADJUSTED ACCOUNT DEFORMED. 2L72 4F RTA2NM 20030729000432003072900043WP 2003 7 29 ZW0A0305701 120030703A335058222 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13948TW 49575 THE AFT EGRESS TRACK LIGHTING WOULD NOT ILLUMINATE. REPLACED THE BATERY PACK AND SECURED CONNECTOR ON THE TRACK LIGHTING. 2L72 4F RTA6WE 20030828000142003082800014WP 2003 8 28 ARWA20030316 120030315A5312 PRESSURE PANEL DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W UPPER SURFACE WITH 0.750 INCH CRACK, STA 934. DRILLED A STOP HOLE AT END OF CRACK IAW DC8 SRM 53-2-0, FABRICATED DOUBLER IAW DC8 SRM 53-2-0, PRIMED DOUBLER IAW DC8 SRM 51-1-8 AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21. 2L74 4F 4A25 20030828000282003082800028NE 2003 8 28 00095 220030601A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT X ENGINE FLAMEOUT CLCLIMB 1 SW05237TW 24D237 251457 PILOT REPORTED WHILE CLIMBING FROM 410 TO 430 THE LT ENGINE FLAMED-OUT. DESCEND TO RELIGHT ALTITUDE, RELIGHT AND CLIMB BACK TO 410 FOR THE REST OF FLIGHT. WILL UPDATE AFTER MAINTENANCE. NO DEFECTS NOTED. RESTRICTED AIRCRAFT TO FL410. 2L72 4J4 J A10CE 1E16 20030828000302003082800030GL 2003 8 28 IXXA0300041O 220030521A7230 STATOR VANE DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563B1US GL NR 3 ENGINE OUT OF RIG A IXXAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 SW11825BX83965915 45978 692276 EN ROUTE TO KRFD FROM IAH NR 3 ENGINE COMPRESSER STALLED ON DECELERATION OF DESCENT. ON LEVEL OFF, ENGINE STALLED AGAIN WHEN POWER WAS APPLIED. IT WAS DECIDED TO FLY DIRECT TO TOL. POWER NOT ADJUSTED UNTIL NR 3 ENGINE WAS SHUTDOWN ON FINAL APPROACH TO TOL. MAINTENANCE PERFORMED BORESCOPE INSPECTION, AND NO DEFECTS WERE NOTED. UPON FURTHER INSPECTION VSV AND VBV WERE FOUND OUT OF RIG. MAINTENANCE RE-RIGGED VSV AND VBV IN ACCORDANCE WITH APPLICABLE MANUELS. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20030828000382003082800038EU 2003 8 28 U30A200300016 120030613A2730B372BAM0509 COMPUTER AIRBUS320 A320214 3930316EU NR 1 FAULTY A U30AK NONE J WARNING INDICATION CRCRUISE 1 EA17261AV4820 4820 1615 DURING CRUISE ON FLT 299 NAS-EWR, THE NR 1 SEC (SPOILER & ELEVATOR COMPUTER) FAULT CAME ON. ECAM COMPLETED AND FAULT CLEARED. FIVE MINUTES LATER, SEC NR 1 FAULT AGAIN. COMPLETED ECAM NR 1 SEC OFF FOR THE REST OF FLT. ON GROUND IN EWR; REPLACED NR 1 SEC IAW AMM TASK 27-94-34-401 AND OPS CK'D OK IAW 27-94-00-501. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030828000452003082800045NM 2003 8 28 XNOA01127 120030503A3297 WIRE BOEING727 727227 1384078NM GEAR DOOR DAMAGED A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL23793A 20774 DEPARTING MCO RT GEAR DOOR LIGHT ILLUMINATED. PERFORMED CHECKLIST, LIGHT EXTINGUISHED. REPAIRED WIRING AT RT DOOR SWITCH CONNECTOR. CHECKS GOOD ON GROUND MM 32-62-11. 2L73 4F A3WE 20030828000472003082800047NM 2003 8 28 XNOA01129 120030520A3260 SWITCH BOEING727 727227 1384078NM LANDING GEAR DIRTY A XN0AO OTHER P NO WARNING INDICATION TXTAXI/GRND HDL 1 GL23793A 20774 GEAR DOOR LIGHT ON F/E PANEL DOES NOT ILLUMINATE WITH GEAR TRANSITION. CLEANED CANNON PLUG ON RIGHT GEAR DOOR SWITCH. OPS CHECKS GOOD IAW MM 32-12-1 B727. 2L73 4F A3WE 20030828000902003082800090NM 2003 8 28 DL75A030629 120030712A5297 WIRE BOEING757 757212 1384951NM PWA 2037 PW2037 NE CARGO DOOR BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27751AT 23125 IRR: FWD AND AFT CARGO DOORS INOPERATIVE. FOUND BURNT WIRE BEHIND AFT CARGO DOOR SWITCH. REPLACED SAME. REPLACED K101 AND PSEU. SLACK IN WIRES ENOUGH WHEN CUT BACK TO REINSTALL ON NEW SWITCH. K101 AND PSEU DAMAGED WHEN WIRE SHORTED OUT. 2L72 4F4 FRTA2NM E17NE 20030828000942003082800094NM 2003 8 28 DL767030687 120030722A3350BPS73 CHARGER BOEING767 767232 1385132NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27103DA 22215 MID LEFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER, OPS GOOD. 2L72 4F RTA1NM 20030828001082003082800108WP 2003 8 28 MWEA030307 120030813A7711795325 CATCHER DOUG DC9 DC981 3022081WP ENGINE PLUGGED A MWEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL31806ME 48032 ADDING POWER FOR TAKE-OFF THE ENGINE PRESSURE RATIO WAS AT 1.80. UNPLUGGED TRAP ASSY- CONDENSATION LEAK CHECK GOOD. 2L72 4F A6WE 20030828001212003082800121WP 2003 8 28 MWEA030295 120030728A5313592480215 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LONGERON 17 LEFT IS CRACKED UNDER HAT SECTION AT STATION 294. FABRICATED AND INSTALLED LONGERON. 2L72 4F A6WE 20030828001272003082800127NM 2003 8 28 MWEA030313 120030818A5320993061223 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 SEVERAL AREAS OF CORROSION FROM STATION 1155-1212 RIGHT SIDE OUTBOARD OF OUTER SEAT TRACK. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030828001412003082800141EA 2003 8 28 ASOA03351 120030803A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11917EV 7769 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP AT THE BRACKET ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE MAIN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030828001492003082800149NM 2003 8 28 HALA0300696 120030804A5755 BRACKET BOEING717 717200 1383700NM RT SPOILER CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13478HA 55123 HNL - RIGHT OUTBOARD SPOILER BRACKET CRACKED. REPAIRS IN WORK. (M) 2L72 4F TRA6WE 20030828001622003082800162NM 2003 8 28 USAASB03132 120030806A33501012721 LIGHT BOEING737 7373B7 1384580NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19511AU 23594 PHL - FOUND EMERGENCY PATH LIGHT INOPERATIVE AT ROW 15. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA16WE 20030828001672003082800167 2003 8 28 USAABA03028 420030810A3460C12858CA01 COMPUTER AIRBUS330 A330323 3930335EU COCKPIT MALFUNCTIONED A USAAO OTHER O OTHER CRCRUISE 1 EA19675US9468 0370 PHL - FLT 11 - EN ROUTE, CREW RECEIVED INDICATIONS THAT BOTH FMGEC'S HAD LOST DATA. CREW MANUALLY ENTERED WAYPOINTS AND ROUTE DATA WAS UPLINKED. SYSTEM PERFORMED NORMALLY THROUGHOUT THE REMAINDER OF THE FLIGHT. MAINTENANCE REPLACED BOTH FMGEC'S. (M) 2L72 4F RTA46NM 20030828001722003082800172NM 2003 8 28 SWAA031867 120030819A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED C2 CHECK, FOUND SEVERAL BULBS INOP IN BOTH AFT ENTRY AND MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS. RELAMPED EXIT LIGHTS PER MM. 2L72 4F A16WE 20030828001812003082800181NM 2003 8 28 SWAA031851 120030818A57536546435282 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER DEDESCENT 1 SW29330SW 23694 RT OUTBD AFT T/E FLAP PREVIOUS REPAIR CAME APART. REMOVED AND REPLACED RT OUTBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030828001862003082800186NM 2003 8 28 CALA0300496 120030826A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND STRINGER 27L CORRODED AT STA 996. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20030828001932003082800193NM 2003 8 28 CALA0300465 120030813A5542 PANEL BOEING737 7373T0 1384582NM RUDDER GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND RUDDER HINGE COVER PANELS NR 9559 AND 9555 GOUGED. NEW PANELS WERE INSTALLED IAW SRM 51-10-02 AND BOEING DRAWING 65C25973. 2L72 4F RTA16WE 20030829000202003082900020NM 2003 8 29 CALA0300453 120030807A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FLOORBEAM CORRODED AT BS 986.5 LT SIDE, AFT OF WATER TANK. A T-CAP WAS INSTALLED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030829000292003082900029NM 2003 8 29 CALA0300487 120030824A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND FLOOR SUPPORTS CORRODED FROM STA 947.5 TO 967 AT RBL 7 AND RBL 46. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-40-02 AND ECRA 5310-03585. 2L72 4F RTA16WE 20030829000352003082900035WP 2003 8 29 CALA0300499 120030826A3222 STRUT DOUG DC9 DC982 3022082WP NLG LOW A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714839 49635 THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM LAS. RECYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG SHOCK STRUT INFLATION LOW. THE SHOCK STRUT WAS SERVICED IAW MM 32-31-02. NO LEAKS WERE NOTED. THE NLG WAS SWUNG AND ALL OPERATION AND INDICATIONS WERE GOOD. 2L72 4F A6WE 20030829000442003082900044EA 2003 8 29 COMA0360376 120030819A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNSECURE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01929CA 7035 FLIGHT 5221 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. FOUND OUTER HANDLE OPEN - OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS NOTED. 2L72 4F RTA21EA 20030829000472003082900047NM 2003 8 29 DHL2003727007 120030715A2510 MECHANISM BOEING727 727228 1384083NM PILOT SEAT OUT OF ADJUST A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01727DH 20204 RIGHT SIDE OF CAPTAIN'S SEAT BACK WILL NOT SECURELY LOCK INTO PLACE (SLIPPING OUT OF LOCK). ADJUSTED CAPTAIN'S SEAT BACK ADJUSTMENT MECHANISM IAW B727 M/M 25-10. OPS CHECKED OK. 2L73 4F RTA3WE 20030829000552003082900055WP 2003 8 29 DHL2003873523 120030624A5730 PLATE DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING OUTBD L/E PLATING CORRODED, XFS 710.000 - XFS 741.500 (UPPER SURFACE) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION FROM RT WING OUTBD L/E UPPER PLATING (STA XFS 710.000 - 741.500) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 57-2-1 PG 11-12. CUT OUT CORRODED AREA IAW SRM 57-2-1 FIG 38, FABRICATED FILLER & DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED TREATED & PRIMED INNER FACE OF FILLER & DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER & DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38 SRM 51-1-21 PG 1, SRM 51-1-15 PG 1 REFER TO N/R 0823 FOR RT. WING OUTBD L/E REMOVAL / REINSTALLATION. 2L74 4F RT4A25 20030829000632003082900063WP 2003 8 29 DHL2003806012 120030714A3350 BATTERY DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01806DH 46002 EMERGENCY LIGHTS BATTERY IS WEAK DURING PRE-FLIGHT. CHARGED EMERGENCY LIGHTS BATTERY IAW DC-8 M/M 33-50-1. LIGHTS CHECKED GOOD ON TEST. 2L74 4F RT4A25 20030829000902003082900090NM 2003 8 29 P5CA0300914 120030816A731276602 VALVE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE MALFUNCTIONED A P5CAK NONE R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23923FT 22769 702280 PRIOR TO DESCENT APPLIED FUEL HEAT TO NR 3 ENG, FUEL HEAT DID COME DOWN AND PEGGED HOT ENG STALL ON DESCENT. PERFORMED A PRECAUTIONARY ENG SHUT DOWN AT 1600 FT ACCORDING TO PROCEDURE. 2L74 4F4 FRTA20WE E3NE 20030829000932003082900093NM 2003 8 29 PCAA0307087 120030728A3350 CONTROL PANEL DHAV DHC8 DHC8102 2809003NM CABIN FAULTY A PCAAK NONE O OTHER NRNOT REPORTED 1 EA13814EX 318 ALB-FLIGHT 3583. CREW REPORTED THAT THE EMERGENCY LIGHTS WERE FLICKERING ON AND OFF DURING FLIGHT. MAINTENANCE REPLACED THE FLIGHT ATTENDANTS SWITCH PANEL. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030829000972003082900097EU 2003 8 29 2904061103 120030611A3340122024102 LIGHT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE EXTERIOR INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP074027Q3331 2904 9456 PULSLITE INOP. 1G71 3U3 U H9EU E19EU 20030828000232003082800023EU 2003 8 28 F3LA200300121 220030618A73218062495 MEC BOEING737 73736E 138443ANM CFMINTCFM56 CFM563B2 13802EU NR 1 ENGINE MALFUNCTIONED A F3LAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM03315FL 2750 25159 727254 AFTER DEPARTURE NR 1 ENG BEGAN TO ROLL BACK THUR RECOVERY & CONTINUED TO FLUCTUATE. FUEL FLOW & ENG FLUCTUATIONS CONTINUED UNTIL LANDING WITH AT LEAST 2 ROLL BACKS TO IDLE. DECLARED AN EMERGENCY & DIVERTED. ACFT LANDED W/O INCIDENT. REPLACED NR 1 ENG FUEL PUMP, MEC, PMC & N2 ALTERNATOR. ENG OPS & LEAK CHECK GOOD. ALL PARAMETERS WITHIN LIMITS. PERFORMED A/T PLA SYNCHRO ADJ/TEST & A/T BITE TEST, NO FAULTS FOUND. PULLED MAGNETIC CHIP DETECTORS, NO DEFECTS NOTED. CHECKED CIT SENSOR TUBING & SENSOR, NO DEFECTS NOTED. PERFORMED OVERWEIGHT LANDING INSPECTION, NO DEFECTS NOTED. PERFORMED TEST FLIGHT. NO DISCREPANCIES NOTED. PERFORMED POST TEST FLIGHT WALKAROUND. NO DISCREPANCIES NOTED. 2L72 4F4 FRTA16WE E21EU 20030801001212003080100121WP 2003 8 1 MWEA030272 120030708A2612P1831 CONNECTOR DOUG DC9 DC932 3022066WP LT ENGINE FAULTY A MWEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL31209ME 47730 LEFT ENGINE LOOP A FIRE INDICATION CAME ON. REMOVED AND REPLACED BOTH FIRE EXTINGUISHER BOTTLE,1 EACH SQUIBS,LEFT ENGINE B AND REPLACED FAULTY CONNECTORS, 2L72 4F A6WE 20030801001292003080100129WP 2003 8 1 MWEA030277 120030715A523039260461 FITTING DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD CARGO DOOR INTERIOR FITTING CRACKED INBOARD OF AFT HINGE. FABRICATED AND INSTALLED FITTINGS. 2L72 4F A6WE 20030730000992003073000099WP 2003 7 30 AMTA200300891 120030513A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FUSELAGE DISTORTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 C2 BILGE FLOORBEAM WEB DISTORTED AT LIGHTENING HOLE EDGE. REPAIRED WEB IAW SRM 51-50-01. (M) 2L73 4F A23WE 20030730001072003073000107EU 2003 7 30 USAABA03019 120030624A3350321430 BATTERY AIRBUS330 A330323 3930335EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19678US 0388 PHL - DURING EPSU CAPACITY CHECK, FOUND THREE EPSU'S DISCREPANT. MAINTENANCE REPLACED THE BATTERIES IN EPSU LOCATIONS 11WL, 18WL AND 13WL. (M) 2L72 4F RTA46NM 20030731001042003073100104NM 2003 7 31 QXEA200300776 120030627A242111522183 GENERATOR BOMBDRDHC8 DHC8401 1390041NM NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09403QX1294 4037 SEA-ON FLIGHT NUMBER 2331, THE NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. AFTER CHECK LIST WAS RAN, THE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED NR 1 AC GENERATOR. PERFORMED OPERATIONAL TEST, OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030801000302003080100030EU 2003 8 1 2003F00498 120030515A7110 ACOUSTIC PANEL AIRBUS320 A320233 3930329EU NR 1 ENGINE DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK FOUND NR 1 ENGINE AIR INTAKE ACOUSTIC PANEL DENTED. REPAIRED ACOUSTIC PANEL IAW SRM 54-10-00, PAGE 110, SEC 11. (M) 2L72 4F RTA28NM 20030801000402003080100040WP 2003 8 1 GTIA030535 120030628A5320 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND MID CARGO FORWARD BULKHEAD LOWER SUPPORT HAS CORROSION UPPER LOWER SURFACES FROM STRINGER 27L-27R. REMOVED LOWER SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW SUPPORT. (M) 2L72 4F A6WE 20030801000992003080100099EA 2003 8 1 COMA0360315 120030705A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01811CA 7380 FLIGHT 5218 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F RTA21EA 20030801001172003080100117WP 2003 8 1 MWEA030285 120030722A523059101419 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 AFT CARGO DOOR PAN CRACKED, LOCATED AT FORWARD TORQUE TUBE LATCH LOBE AREA. FABRICATED AND INSTALLED REPAIR. 2L72 4F A6WE 20030805000082003080500008CE 2003 8 5 N6P2003F00000 120030514A3220AN517A BOLT CESSNA340 340A 2076405CE CONT O520 TSIO520* 17040SO NLG SCISSORS BROKEN E N6PAO OTHER O OTHER NRNOT REPORTED 1 EA13340AB4785 340A0471 DURING REPAIR OF THE TAXI LIGHT WIRES, WHILE REMOVEING THE NUT FROMT HE BOLT ATTACHING AN ADEL CLAMP WHICH HOLES THE WIRE HARNESS TO THE NOSE GEAR SISSORS, AT THE SCISSORS PIVOT POINT, THE BOLT BROKE IN HALF DURING REMOVAL. LOG BOOK RESEARCH INDICATES PREVIOUS DAMAGE TO NOSE GEAR DUE TO RETRACTION WITH A FLAT STRUT (6/12/98 AT 4364.8 HOURS), AND FORK BOLT PN 5045211-2 WAS CHANGED BUT THE BOLT THAT FAILED WAS NOT. SUGGEST THAT BOLTS ASSOCIATED WITH LANDING GEAR RETRACTION AND EXTENSION BE REPLACED WHENEVER THEY MAY HAVE BEEN SUBJECTED TO ABNORMAL FORCES. 1L72 3O3 O 3A25 E8CE 20030805000622003080500062EU 2003 8 5 SIMA200315301 120030531A2120460250 SEAL SAAB SF340 340B 7860101EU RT ENGINE LEAKING A SIMAE ENGINE SHUTDOWN D INFLIGHT SEPARATION CLCLIMB 1 SW21382AE 340B382 NR 2 RIGHT ENGINE BLEED LEAK LIGHT CAME ON IN FLIGHT. THEN THE ENGINE WAS SHUTDOWN IAW EPC/DOM. EMERGENCY WAS DECLARED BY CREW. RAI RIGHT WING FLAP COVE PERI-SEALS IAW SAAB 340 W/C 47223. OPS CHECK GOOD. (M) 2L72 4T RTA52EU 20030805000702003080500070SO 2003 8 5 ASOA03268 120030619A339703091022 CONNECTOR EMB 120 EMB120 3260201SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11239AS 120057 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHTS IN THE FLOOR AND FORWARD CABIN PANEL WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY LIGHTS IN THE FLOOR AND FORWARD CABIN PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030805000792003080500079EU 2003 8 5 USAASA03080 120030714A3350 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 THE EMERGENCY FLOOR LIGHTS AT SET 18D STAYED ON. MAINTENANCE REPLACED THE RECEIVER ASSEMBLY AND BATTERY. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030805000842003080500084EA 2003 8 5 ASOA03294 120030706A5300 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DUIRNG A C-CHECK IN MCN, THE LEFT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 12 IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20030805000852003080500085EU 2003 8 5 ASOA03278 120030630A5330 DOUBLER AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD PASSENGER/CREW DOOR FIRST STEP DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR ON THE FORWARD PASSENGER/CREW DOOR FIRST STEP DOUBLER IAW ASA EO 72-52-0073. THIS MRR WILL REMAIN OPEN PENDING THE PERMANENT REPAIR WHICH IS TO BE ACCOMPLISHED NO LATER THAN THE NEXT SCHEDULED 'A' CHECK PER SRM 52-11-00. (M) 2H72 4T RTA53EU 20030905002152003090500215SO 2003 9 5 C2XA03SH245 120030731A532014521725015 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV DURING C CHECK SERVICE DOOR AFT SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED SECTION IAW EMB 145 SRM 53-21-10 AND CONTINENTAL EXPRESS EC 5320-01089. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905002242003090500224SO 2003 9 5 C2XA03SH291 120030827A532014521725013 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE RIGHT HAND SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030904001162003090400116NM 2003 9 4 QXEA200300981 120030812A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX- DURING LIGHTNING STRIKE INSPECTION FOUND A BURN MARK .0625 IN DIAMETER ON A RIVET ON RIGHT HAND STRINGER 3 AND 14.5 INCHES FROM STATION X19.850 JOINT. REPAIRED IAW Q400 SRM 51-25-05. 2H72 4T RTA13NM 20030904001382003090400138NM 2003 9 4 DL76G030631 120030712A3320191311 BALLAST BOEING767 767332 1382001NM LAVATORY DEFECTIVE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271604R 30180 AFT RT LAV HAS ACRID SMELL BUT NO VISABLE SMOKE OR HAZE. INSPECTED TRASH CAN, ALL OK. HOT WATER HEATER PWR SWITCH AND LAV LIGHTS TURNED OFF. REPLACED LIGHT BULBS. SUSPECT BAD BALLAST IN RT AFT LAV. WD TO MCO AND PLAC 38-30-01B. PULLED FUSE IN BALLAST ASSY. TURNED ON WATER HEATER-NO ACRID SMELL NOTED FROM AREA. REPLACED OVERHEAD FOUR LIGHT BALLST. INSPECTED WIRING IN OVERHEAD AREA, NO SMELL OR SIGNS OF ARCING/BURNING NOTED. LEFT LIGHTS AND WATER HEATER ON FOR EXTENDED PERIOD OF TIME, ALL CKS OK. MCO AND PLAC RMVD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2L72 4F RTA1NM 20030904001662003090400166WP 2003 9 4 DHL2003873521 120030617A534774529523 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT NR 5 TRACK PLUG LUG WORN AT STA 954.000. REMOVED AND REPLACED PLUG ON MAIN CARGO COMPT NR 5 TRACK AT STA 954.000 IAW SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20030904001672003090400167WP 2003 9 4 DHL2003873571 120030628A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FUSELAGE EXTERIOR REPLACE INTERIM DOUBLER BY A CLASS I REPAIR BETWEEN STA 480.000 - 500.000 L-21R TO L-23R. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 PG 99/108. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7 PG 99/108. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER AND SHIM IAW SRM 53-2-1 FIG 7 99/108. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER AND SHIM IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER AND SHIM WITH NEW FASTENERS IAW SRM 53-2-1 FIG 7 PG 99/108, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030904001752003090400175WP 2003 9 4 AALA20030608 120030527A2120 CLAMP DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW21490AA 49683 LAS - FLT 870 - EN ROUTE LAS-DFW, ON TAKEOFF ABOUT TWO MINUTES INTO FLIGHT THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED, ACCOMPLISHED PROCEDURES AND LIGHT EXTINGUISHED, LIGHT THEN ILLUMINATED ABOUT 30 SECONDS LATER AND FLIGHT ABORTED, RETURNED AND LANDED LAS WITHOUT INCIDENT. READJUSTED THE INBOARD LEFT PRIMARY HEAT EXCHANGER CLAMP, PERFORMED LEAK CHECK WITH THE APU AND THEN WITH BOTH ENGINES AT IDLE. REVEALED NO LEAKS, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905000192003090500019SO 2003 9 5 LR7A03066 120030725A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND RT BRACKET ATTACHMENT FOR PRESSURIZED FAIRING CRACKED FS 597-617, RBL 18, WL 283. REPLACED BRACKET IAW SRM SMP 583 51-60 AND 51-70. NR 2111. 2H74 4T A1SO 20030905001542003090500154NM 2003 9 5 DL757030662 120030716A3350 BATTERY PACK BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27677DL 25982 F/C FLOOR EPATH LIGHTS INOP, REPLACED BATTERY PACK. 2L72 4F RTA2NM 20030812000432003081200043GL 2003 8 12 HEEA088387 220030719A73200164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE SURGES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 FUEL CONTROL SURGING. TO BE SENT TO VENDOR. 1G72 3U3 U H1NE E1GL 20030812000492003081200049SW 2003 8 12 HEEA088447 120030723A6410206011809109 PITCH HORN CLARK 1000 1000CLARK 2230102SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03266P 707 52271 FRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE. 1Q71 3R 2A6 20030806000402003080600040SO 2003 8 6 C2XA03TY094 120030723A532014522184006 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713990 145277 DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE DAMAGED AREA, ALODINED, PRIMED AND FILLED WITH HYSOL 9394, FABRICATED AND INSTALLED A DOUBLER IAW-EMB-GST-1927/02A. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2L72 4T RTT00011AT 20030806000602003080600060NM 2003 8 6 AWXA200300849 120030712A532065476902 PANEL BOEING737 7373G7 1384595NM CARGO BAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A CRACK WAS FOUND ON AFT CARGO COMPARTMENT LT TRANSITION PANEL AT BS 747, LBL 22, WL 160. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT -ZEE- BETWEEN BS 747 AND BS 787; FABRICATED A NEW SECTION OF REPLACEMENT -ZEE-, AND 2 EACH SPLICE -ZEE'S-; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-53, PG 208-209, FIG 204. 2L72 4F RTA16WE 20030806001132003080600113SO 2003 8 6 C2XA03SH219 120030711A541014576056607 STIFFENER EMB 145 EMB145LR 3260212SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 DURING C-CHECK, THE LEFT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001532003080600153SO 2003 8 6 C2XA03IA070 120030630A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717560 145605 THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE INVERTER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001692003080600169NM 2003 8 6 AWXA200300870 120030802A21206549571 DUCT BOEING737 7373S3 1384711NM ZONE 222 LEAKING A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28316AW 23713 APPROX 3 MIN AFTER DEPARTURE THE RT WING TO BODY OVERHEAT LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURES AND LIGHT EXTINGUISHED APPROX 2 MIN LATER. DURING TAXI & TAKEOFF PACK WAS IN AUTO POSITION, AND AFTER TAKEOFF POSITIONED PACK TO HIGH WITH OVERHEAT CONDITION OCCURING APPROX 1 MIN LATER. ACFT TURNED BACK & LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT OVERHEAT SYSTEM PER TSM 26-18-00. CHECKED LOOP RESISTANCE FROM M237 COMPARTMENT OVERHEAT CONTROL UNIT THROUGH PINS: 10-11 (8.4 OHMS), PINS 4-12 (11.4 OHMS), PINS 2-8 (5.9 OHMS), PINS 2-29 (6 OHMS), & PINS 13-27 (10.3 OHMS), ALL PIN RESISTANCE WAS WITHIN TOLERANCE. REMOVED AND REPLACED RT RAM AIR OUTLET DUCT IAW BMM 21-51-21, LEAK AND OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20030807000322003080700032NM 2003 8 7 USAA030124 120030717A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 FOUND SKIN CORRODED 2 INCHES BY 1 INCH, STATION 500C PLUS 17 INCHES AT S-27R. CORROSION LEVEL 1, TASK NR C53-208-01. REMOVED RIVETS, BLENDED CORROSION, TREATED, PRIMED, PAINTED PER SRM 53-00-01 AND 53-30-01. (M) 2L72 4F RTA16WE 20030807000482003080700048EA 2003 8 7 COMA0360347 120030730A3230555405 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01978CA20723 7158 FLIGHT 5772 GEAR DISAGREE WARNING. NLG DID NOT EXTEND. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20030807000522003080700052EA 2003 8 7 03214673 120030802A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27673BR 7599 DURING MAINTENANCE INSPECTION THE RT AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030807001032003080700103NM 2003 8 7 EIA2003100 120030725A5310 STRUCTURE BOEING747 747212B 1384886NM RT MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 RT WING GEAR WELL, STA 1307, RBL 115, CORROSION ON AFT SIDE OF WEB STIFFENER. REMOVED AND REPLACED STIFFENER AS PER B747 SRM 51-30-02, PGS 5-9, 38, 57, 58B. 2L74 4F A20WE 20030812000362003081200036NE 2003 8 12 HEEA088402 120030802A62207610608000050 DAMPENER SKRSKYS76 S76A 8143006NE MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03792P 760193 MAIN ROTOR DAMPENER LEAKING. SHOP REPAIR. 1G72 3U H1NE 20030812000372003081200037EU 2003 8 12 KBMA088329 120030713A6340614764021 INDICATOR AEROSPAS355 AS355* EU COCKPIT READS LOW B KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 N/R GAGE READS APPROXIMATELY 6-10 RPM LOW AT FLIGHT IDLE, N2 POINTER ACCURATE. INSTALLED REPAIRED TACH INDICATOR. 1G72 3U H11EU 20030812000832003081200083EU 2003 8 12 HEEA088658 120030730A561004011651990 WINDOW AEROSPAS355 AS355* EU COCKPIT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03973AE 3229 THE RAILS FOR THE SLIDING VENT WINDOW ARE CRACKED. 1G72 3U H11EU 20030813000012003081300001EU 2003 8 13 HEEA088638 120030729A243230248001 BATTERY BOLKMS105 BO105S 5626006EU MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0350293 S677 BATTERY OUT LIGHTS CAME ON. SHOP REPAIR. 1G72 3U H3EU 20030813000122003081300012 2003 8 13 HEEA088597 420030804A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610C 51425 PILOT MIC SWITCH IS WORN OUT. CAUSES LOUD POPPING NOISES WHEN CHANGE FROM ONE POSITION TO ANOTHER. SHOP REPAIR. 1G71 3U H2SW 20030813000132003081300013SW 2003 8 13 HEEA088598 120030801A5260PHI101741 STEP BELL 412 412 1182202SW FUSELAGE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 RT STEP ASSY WOULD NOT STOW. SHOP REPAIR. 1G72 4U H4SW 20030813000202003081300020SW 2003 8 13 HEEA088602 120030806A6510212040600005 HANGER ASSY BELL 412 412 1182202SW TAIL ROTOR DAMAGED E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW032149S 36002 HUMS, READINGS WERE HIGH. REPLACED PART. 1G72 4U H4SW 20030813000252003081300025NE 2003 8 13 HEEA088567 220030805A7532312320301 BLEED VALVE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE COMPRESSOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 ENGINE COMPRESSOR BLEED VALVE FAILED TO REMAIN CLOSED AT HIGH ENG OUTPUT CAUSING COMPRESSOR SURGES. REPLACED. 1G72 4U4 U H4SW E22EA 20030813000272003081300027SW 2003 8 13 HEEA088569 120030805A6230 SEAL BELL 407 407 1182206SW SWASHPLATE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03 TI75 SWASHPLATE UPPER GREASE SEAL PERMITTING GREASE BY. 1G71 3U O H2SW 20030813000392003081300039 2003 8 13 RAIA00305153 420030530A3425HG2010AC02 INDICATOR EMB 145 EMB145LR 3260212SO AHRS FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03813HK7335 145044 F/O'S AHRS FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 AHRU. 2L72 4T RTT00011AT 20030813000402003081300040CE 2003 8 13 DXTA200300039 120030601A3020 TUBE CESSNA560 560XL 2076702CE ANTI-ICE SYSTEM LEAKING E DXTAO OTHER N FALSE WARNING CLCLIMB 1 GL07690QS2619 5605090 LT ENGINE FIRE WARNING LIGHT ILLUMINATED ON CLIMBOUT AT 14,000 FT. TROUBLESHOT FIRE DETECTION SYSTEM. PERFORMED FIRE LOOP CONTINUITY RESISTANCE CHECK IAW CE-560 XL MAINTENANCE MANUAL CHAPTER 26-1-0. PERFORMED HIGH POWER RUNS ON LT ENGINE FOUND ANTI-ICE PLUMBING LEAKING AT TOP OF ENGINE AT UNION CLAMPS. 2L72 4F RTA22CE 20030813000522003081300052NM 2003 8 13 2003UALA00469 120030604A7930 WARNING LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 1 ENG OIL ILLUMINATED A UALAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29778UA 26940 777023 RETURN TO FIELD AFTER RECEIVING LOW OIL QUANTITY INDICATION FOLLOWED BY LOW OIL PRESSURE INDICATION ON NR 1 ENGINE. NR 3 BEARING EXTERNAL SCAVENGE LINE FAILED (LR04) LEAKAGE WAS DUE TO CRACKING OF THE INTERNAL PTFE (POLYTETRAFLUOROETHYLENE) LINER. THIS LEAD TO OIL PRESSURE BUILDUP UNDER THE FIRESLEEVE, WHICH EVENTUALLY BURST. NO EVIDENCE WAS FOUND OF DAMAGE TO THE WIRE BRAID. (CORROSION, KINKS, ETC.) 2L72 4F4 FRTT0001SE E46NE 20030813000542003081300054NM 2003 8 13 2003UALA00476 120030605A5320 WEB BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE DOOR SILL CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 AFT CARGO PIT AT BS 1329-1351, LOWER DOOR SILL LOWER WEB IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. INSTALLED WEB AND SPLICE REPAIR. 2L72 4F4 FRTA1NM E3NE 20030813000562003081300056NM 2003 8 13 2003UALA00478 120030605A5350 SKIN BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE TAIL CONE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 FUSELAGE TAILCONE SKIN AT STA 1848, LBL 24 PUNCTURED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA1NM E3NE 20030813000702003081300070SO 2003 8 13 SWIA200312082 120030609A2797 WIRE EMB 120 EMB120ER 3260203SO FLAP ACT HARNESSBROKEN A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07293SW 120320 FLAPS CONTROL FAULTED INFLIGHT. OUTBOARD PAIR ON ANNUNCIATOR FLASHING. TROUBLESHOT FLAP SYSTEM. FOUND BROKEN WIRES IN HARNESS AT LEFT OUTBOARD FLAP ACTUATOR. REPAIRED BROKEN WIRES IAW WM 20-21-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030813000732003081300073EA 2003 8 13 SWIA200312087 120030528A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 NR 1 FLOOR TRACK LIGHTING INOP. DISCOVERED DURING C-CHECK. 2L72 4F RTA21EA 20030813000752003081300075EU 2003 8 13 UPS03140849 120030613A3242 FUSIBLE PLUG AIRBUSA300 A300F4622R 3930360EU NR 5 BRAKE OVERTEMP A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01125UP 0809 NR 5 BRAKE OVERTEMP CAUSING NR 5 TIRE FUSE PLUG TO BLOW. *** OPEN *** 2L72 4F RTA35EU 20030813000802003081300080NM 2003 8 13 2003UALA00454 120030530A2121 BEARING BOEING757 757222 1384956NM PWA 2037 PW2037 NE BLOWER FAILED A UALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 WP29590UA AFM975 28708 EICAS STATUS MESSAGE FWD CARGO DET AIR DISPLAYED. NR 1 LOWER CARGO SMOKE DETECTION SYSTEM BLOWER MOTOR ASSY FAILED. SHOP FINDINGS REVEALED REAR ROTOR BEARING WILL NOT ROTATE. REAR ROTOR BEARING FAILURE. 2L72 4F4 FRTA2NM E17NE 20030813000892003081300089NM 2003 8 13 2003UALA00489 120030610A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE MLG WW CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29670UA 29240 LEFT NOSE TUNNEL AT STA 246 STIFFENER AT LBL 40 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20030813000922003081300092NM 2003 8 13 2003UALA00497 120030613A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29198UA 28716 TWO EACH DENTS TOP FLOORBEAM BS 540 RBL 12. MAJOR REPAIR ACCOMPLISHED. REPLACED TOP T-CAP. 2L74 4F4 FRTA20WE E24NE 20030806001042003080600104SO 2003 8 6 C2XA03SH241 120030731A531514522459001 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV- DURING C-CHECK, THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001262003080600126NM 2003 8 6 AWXA200300825 120030711A5320654583471 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A 2 INCH CRACK WAS FOUND ON TIE STRAP AT BS 343, RBL 41, WL 200. MAINTENANCE STOP DRILLED CRACK ON TIE STRAP AT BS 343, RBL 41, WL 200; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51, PG 213 & 219, FIG 204. 2L72 4F RTA16WE 20030807000082003080700008EU 2003 8 7 ASOA03258 120030614A5753S57512248200000 BRACKET AEROSPATR72 ATR72212 8680945EU LT CANOE FAIRINGCRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING A GROUND INSPECTION IN MGM, THE LEFT OUTBOARD FLAP CANOE FAIRING SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP CANOE FAIRING SUPPORT BRACKET. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030807000212003080700021NM 2003 8 7 USAA030113 120030615A53126546568529 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 FOUND WEB CORRODED, 12 INCHES BY 6 INCHES, AFT PRESS BULKHEAD STATION 1016 LBL 4 INCHES-RBL 4 INCHS. MODIFIED PART NR INSTALLED, KIT NR 65C28106-1 AND 65C28106-16 PER EO 5302V112, REV A. (M) 2L72 4F RTA16WE 20030807000302003080700030NM 2003 8 7 USAABB03111 120030714A3397 CONNECTOR BOEING767 7672B7 1385107NM RT OVERWING INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 CDG - FOUND FLOOR PROXIMITY EMERGENCY LIGHTING INOPERATIVE FROM ROW 7 TO THE OVERWING EXIT ON THE RT SIDE. MAINTENANCE FOUND A DISCONNECTION AT THE OVERWING AREA AND RECONNECTED. (M) 2L72 4F RTA1NM 20030807000832003080700083NM 2003 8 7 QXEA200300926 120030729A2150 ODOR DHAV DHC8 DHC8202 2809007NM ZONE 200 DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09357PH 504 AIR CONDITIONER SYSTEM PUTS OUT PUTRID ODOR FOR 2-3 MINUTES AFTER ENGINE START THROUGHOUT AIRCRAFT. DISAPPEARS AFTER THIS PERIOD. RETURNS ON FINAL APPROACH AT LOW POWER SETTINGS. ECS OPERATED FOR 20 MINUTES TO PURGE BAD ODOR. RAN AIRCRAFT AT LOWER POWER SETTINGS WITH NO ODOR NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030812000352003081200035EU 2003 8 12 BAQA088261 120030801A2842647571012 TRANSMITTER AEROSPAS355 AS355F1 8680810EU FUEL LEVEL FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035797X 5182 INSTALLED UNIT AND FAILED ON FIRST FLIGHT OF .2 HOURS. GAGE FELL TO BELOW ZERO. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030812000602003081200060 2003 8 12 HEEA088510 420030711A3424214075244001 GYRO BELL 412 412 1182202SW RATE OF TURN MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 RATE TURN NEEDLE DISPLACED 1/2 STEP TO RIGHT. 1G72 4U H4SW 20030813001162003081300116WP 2003 8 13 AALA20030743 120030713A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21553AA 53083 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001352003081300135NM 2003 8 13 SWAA031748 120030805A3350BR2013 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 EEPLS LOOSE AT ROW NR 7. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030813001362003081300136 2003 8 13 SWAA031749 420030805A2565D31354 SLIDE BOEING737 7377H4 1384404NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030813001532003081300153NM 2003 8 13 SWAA031663 120030724A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 207, RBL 14 AND WL 203, RBL7. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030813001562003081300156NM 2003 8 13 SWAA031666 120030725A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 874, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030813001632003081300163NM 2003 8 13 SWAA031673 120030727A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR LOWER FWD CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030813001682003081300168NM 2003 8 13 SWAA031678 120030728A53116516309 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030813002002003081300200 2003 8 13 SWAA031648 420030723A2565D31354 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030813002052003081300205 2003 8 13 SWAA031653 420030724A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030813002072003081300207NM 2003 8 13 SWAA031655 120030724A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) BELOW STR 4L, BS 661, BS 648 AND BS 667. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000042003081400004 2003 8 14 SWAA031716 420030801A2565D31354 INDICATOR BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030814000132003081400013NM 2003 8 14 SWAA031725 120030801A53306545765 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (15 EA) AT STR 4L, BS'S 500D, 571, 602, 625, 626, 628, 630, 631, 632, 647, 649, 653, 658, 669 AND 706. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000302003081400030 2003 8 14 SWAA031701 420030729A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030814000372003081400037NM 2003 8 14 SWAA031741 120030805A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030814000512003081400051EU 2003 8 14 2003UALA00590 120030726A2910 TRANSFORMER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE BLUE HYD SYS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29426UA 510 RETURN TO FIELD DUE TO LOSS OF BLUE HYDRAULIC PRESSURE. REPLACED CURRENT TRANSFORMER. 2706GJ 2L72 4F4 FRTA28NM E40NE 20030814000802003081400080EA 2003 8 14 SWIA200312085 120030528A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 FS 280 RBL 9.0 FLOORBEAM I/B AND O/B ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. P/N: 601R31113-58. 2L72 4F4 FRTA21EA E15NE 20030814000852003081400085WP 2003 8 14 UPS03840942 120030625A53104611067N FITTING DOUG DC8 DC873F 302199FWP A/C COMPARTMENT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, AFTER REMOVING CRACKED LONGERON END FITTING AT STATION 8 LONG 33L FOUND LONG 33L AND END FITTING AT STATION 70 FWD SIDE CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING AND REMOVED, FABRICATED AND REPLACED LONGERON 33 IAW DWG 4611067 AND DWG 3642838 AND SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20030814000862003081400086NM 2003 8 14 2003UALA00547 120030708A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 CABIN FLOORBEAM BS 286, RBL 88 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030807000252003080700025NM 2003 8 7 USAASB03093 120030627A274191238071 RELAY BOEING737 7374B7 1384702NM STAB TRIM FAILED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19437US 24559 ON CLIMB-OUT FROM CLT, EN ROUTE TO PNS, CREW REPORTED A RUNAWAY STABILIZER TRIM CONDITION AS AIRCRAFT BEGAN TO TRIM NOSE UP. CREW TRIMMED AIRCRAFT FOR NOSE DOWN BUT ONCE THE TRIM BUTTON WAS RELEASED, THE AIRCRAFT BEGAN TO TRIM FOR NOSE UP AGAIN. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE R64 STABILIZER TRIM CONTROL RELAY PER MM. PERFORMED OPS TEST OF HORIZONTAL STABILIZER TRIM SYSTEM PER MM 27-41-00. OPS TEST GOOD. (M) 2L72 4F RTA16WE 20030807000552003080700055NM 2003 8 7 03210413 120030729A3397 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27413FJ 3168 DURING INSPECTION THE CREW REPORTED THE EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL FOUND A LOOSE CONNECTOR ON THE EMERGENCY TRACK LIGHTING AND RESECURED THE CONNECTOR. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030807000992003080700099NM 2003 8 7 EIA2003096 120030724A5730 DOUBLER BOEING747 747212B 1384886NM WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CRACK ON DOUBLER OF 1241 WEB APPROX LBL 80 ABOVE LOWER CHORD. REMOVED AND REPLACED DOUBLER PER B747 SRM 57-30-2 AND ECRA 485-53-151-2. 2L74 4F A20WE 20030812000102003081200010 2003 8 12 HEEA088414 420030715A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 2303 760166 AFCS ACTUATOR INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030812000282003081200028EU 2003 8 12 KBMA088326 120030714A6410355A09103601 BEARING AEROSPAS355 AS355* EU T/R BLADE CRACKED B KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 TAIL ROTOR BLADE HALF SHELL BEARINGS HAVE CRACKS. REPLACED WITH NEW 4 EACH HALF SHELL BEARING KIT. 1G72 3U H11EU 20030812000552003081200055SW 2003 8 12 HEEA088483 120030717A3212206030104023 FITTING BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 FITTING MISSING RUBBER PADS AND CORRODED. SCRAPPED. 1G71 3U H2SW 20030812000682003081200068NE 2003 8 12 HEEA088560 220030713A753223005366 BLEED VALVE BELL 206 206L3 1182108SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 HIGH TOT. SHOP REPAIR. 1G71 3U4 U H2SW E22EA 20030812000752003081200075SW 2003 8 12 HEEA088603 120030806A2910212076015001 CHECK VALVE BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 CHECK VALVE SEEPING FROM WEEP HOLE. SHOP REPAIR. 1G72 4U H4SW 20030812000802003081200080EU 2003 8 12 HEEA088639 120030704A243230248001 BATTERY BOLKMS105 BO105S 5626006EU MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MASTER BATTERY DISCHARGED, SHOP REPAIR. 1G72 3U H3EU 20030805000982003080500098CE 2003 8 5 2003F00511 120030620A800035059184 STARTER CESSNA750 750 2076810CE RT ENGINE FAILED A GMCME ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL235116 7500019 RIGHT ENGINE REPORTED AS SMOKING BY TOWER AND OTHER AIRCRAFT DURING TAXI OUT. RIGHT ENGIEN STARTER FAILED TO DISENGAGE AFTER START. STARTER WAS REPLACED, SERVICED AND OPERATIONALLY CHECKED. RIGHT ENGINE STARTER CHECK GOOD PER CESSNA CITATION X MM AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030805001022003080500102SO 2003 8 5 SIMA200319710 120030708A532014525480003 SILL EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21649PP 145234 DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTER 51-40-02 AND CPM 51-21-04, 51-21-05, 51-21-06, 51-61-00. (M) 2L72 4T RTT00011AT 20030805001092003080500109SO 2003 8 5 ASOA03283 120030703A3397MS22759 WIRE EMB 120 EMB120RT 3260202SO CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11240AS 120060 DURING HANGAR MAINTENANCE IN MCN, THE EXIT SIGN AT SEAT ONE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE EXIT SIGN AT SEAT ONE OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030805001102003080500110EU 2003 8 5 USAASA03075 120030708A2611PAI283000 SMOKE DETECTOR AIRBUSA321 A321211 3930370EU PAX CABIN FAULTY A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19186US 1701 BWI - FLT 197 - EN ROUTE PHL-SFO, WHILE CLIMBING THROUGH FL280, RECEIVED ECAM MESSAGE 'SMOKE LAV CRG DETECT FAULT', ACCOMPANIED BY A DISTINCT SMOKE ODOR IN THE FORWARD CABIN AND COCKPIT. THE FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE ODOR. THE FORWARD LAVATORY SMOKE DETECTOR WAS REPLACED THE FIX THE DETECTOR FAULT. ALL TESTS WERE NORMAL. (M) 2L72 4F RTA28NM 20030806000212003080600021SW 2003 8 6 ALGA088160 120030721A623023068295 GEAR BELL 407 407 1182206SW ALLSN 250C 250C30S 03013GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03507AL288 CAG90759 53103 CAE890824S HEAVY SPALLING ON GEAR TEETH DUE TO IMPROPER MESHING OF GEAR TEETH. REMOVED AND REPLACED. 1G71 3U3 UO H2SW E1GL 20030806000312003080600031 2003 8 6 ALGA088227 420030605A3416214175278101 INDICATOR BELL 412 412EP 1182205SW ALTIMETER MALFUNCTIONED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBDZ 36278 PILOTS ALTIMETER DOES NOT COMFORM WITH DIGITAL READ OUT. DMR #719722 RO #38175 1G72 4U H4SW 20030806000442003080600044SO 2003 8 6 C2XA03TY103 120030802A531514521713003 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 TYS DURING A SCHEDULED 3C INSPECTION THE CENTER FLOORBEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030806000452003080600045SO 2003 8 6 C2XA03TY092 120030723A534714532605003 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713990 145277 DURING A SCHEDULED INSPECTION THE ROW 2, CABIN SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145-AMM-53-01-06. 2L72 4T RTT00011AT 20030806000532003080600053NM 2003 8 6 AWXA200300848 120030714A5320652072619 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A .375 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT RT TRANSITION ZEE CHANNEL JUST FORWARD OF THE CARGO DOOR AT BS 436, RBL 23.5, WL 156. MAINTENANCE REMOVED DAMAGED -ZEE- CHANNEL FROM BS 420 TO BS 440; FABRICATED A NEW REPLACEMENT ZEE CHANNEL PER DWG 65-20726; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG 3-4, 10-11, & 38, FIG 8. 2L72 4F RTA16WE 20030806000582003080600058EU 2003 8 6 03207317 120030726A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27317UE 41031 DURING MAINTENANCE INSPECTION THE OUTSIDE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OUTSIDE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030731000942003073100094NM 2003 7 31 QXEA200300768 120030621A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - DAMAGE TO SKIN AT STATION X 8.0, 15 INCHES BELOW BAGGAGE DOOR CUT-OUT. REPAIRED IAW HORIZON AIR EA 6-53-110. 2H72 4T RTA13NM 20030731001122003073100112NM 2003 7 31 QXEA200300800 120030624A7110 STIFFENER BOMBDRDHC8 DHC8401 1390041NM RT COWLING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - THE OIL COOLER SHROUD HAS CHAFED A MILLED STIFFENER ON THE UPPER DECK OF THE RIGHT HAND LOWER COWL. REPAIRED IAW HORIZON AIE EA 6-71-100. 2H72 4T RTA13NM 20030731001252003073100125NM 2003 7 31 QXEA200300871 120030721A2161T87277 CONTROL VALVE DHAV DHC8 DHC8202 2809007NM A/C BAY MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09356PH108504021 502 SEA-ON FLIGHT NUMBER 2101, FLIGHT ATTENDANT SAYS CABIN VERY WARM. AIR FROM VENTS SMELLED LIKE OLD GYM SOCKS FOR FIRST 10 MINUTES OF FLIGHT. REMOVED AND REPLACED PACK TEMP CONTROL VALVE. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001362003073100136NM 2003 7 31 QXEA200300883 120030723A2810 FUEL SYS DHAV DHC8 DHC8202 2809007NM LT WING LEAKING A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09346PH 477 LWS- FUEL LEAKING UNDERNEATH LEFT LEADING EDGE OUTBOARD OF ENGINE NACELLE. LEAK IS THREE FEET OUTBOARD OF LANDING LIGHT ASSEMBLY. THIS LEAK IS CLASSIFED AS A SEEP, NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030801000612003080100061EU 2003 8 1 ASOA03287 120030704A3397MS2275941249 WIRE AEROSPATR72 ATR72 EU CABIN BROKEN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11642AS 395 FLT 4534 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030812000922003081200092EU 2003 8 12 HEEA088632 120030720A32131178429302 SLEEVE BOLKMS117 BK117A1 5626010EU MLG DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC 7152 MLG SLEEVE RUBBER DETERIORATING. SCRAPPED. 1G72 3U H13EU 20030813000142003081300014SW 2003 8 13 HEEA088599 120030713A6520PHI2062003 SEAL BELL 206 206L3 1182108SW T/R HOUSING LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03141BH 51303 TAIL ROTOR HOUSING SEAL LEAKING. SHOP REPAIR. 1G71 3U H2SW 20030813000242003081300024NE 2003 8 13 HEEA088563 220030713A732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FREE TURBINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 LOW SIDE FAILURE. SHOP REPAIR. 1G72 4U4 U H4SW E22EA 20030813000552003081300055NM 2003 8 13 2003UALA00477 120030605A5313 STRINGER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 AFT CARGO STRINGER 34R AT STA 1337 HAS HEAVY CORROSION ON SIDE. MAJOR REPAIRED ACCOMPLISHED. INSTALLED SPLICE REPAIR. 2L72 4F4 FRTA1NM E3NE 20030813000832003081300083NM 2003 8 13 2003UALA00482 120030606A5313 STRINGER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 STRINGER 36L IS GOUGED FROM BS 303 TO 325. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR. 2L72 4F4 FRTA1NM E24NE 20030813001002003081300100EA 2003 8 13 SWIA200312104 120030610A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 FOUND A .75 INCH CRACK ON FUSELAGE FRAME FS 640.00 AT STRINGER 9. DISCOVERED DURING B001 INSPECTION. COMPLIED WITH EA RJ208-53 IAW REO 601R-53-61-557. 2L72 4F RTA21EA 20030813001522003081300152NM 2003 8 13 SWAA031662 120030725A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030813001832003081300183NM 2003 8 13 SWAA031693 120030728A29107321124002 MODULE BOEING737 7373H4 1384600NM HYD SYSTEM LEAKING A SWAAO OTHER O OTHER DEDESCENT 1 SW29368SW 26579 STRONG ODOR IN CABIN. REMOVED AND REPLACED HYD A AND B SYSTEM RESEVOIR PRESS MODULE, AND SYSTEM BLEED VALVE PER MM. 2L72 4F RTA16WE 20030813001882003081300188NM 2003 8 13 SWAA031556 120030715A57546573714 SKIN BOEING737 7372T4 1384492NM NR 3 L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SPECIAL VISIT, FOUND NR 3 L/E SLAT SKIN CRACKED AT L/E, OUTBD OF ACTUATOR. REPAIRED NR 3 L/E SLAT PER SRM. 2L72 4F A16WE 20030814000482003081400048NM 2003 8 14 UPS03441053 120030718A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FRAME FOUND SURFACE CORR AT STA 1050, RBL 22 - 25 AND RBL 50 - 60 AS MARK. FX - BODY FAIRING SUPPORT FRAME STA 1050 RBL 22 - 25 SURFACE CORROSION AREA CORROSION CLEANED AS PER SRM 51-10-01 AND REPROTECTED AS PER SRM 51-10-02 AND BODY FAIRING SUPPORT STA 1050 RBL 50 - 60 AREA REPAIRED AS PER SRM 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 WORK DETAIL REFER ATTACH CWS. 2L74 4F A20WE 20030814000932003081400093NM 2003 8 14 CALA0300445 120030807A5311 BELTFRAME BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME AT STA 807 BETWEEN S27L AND S27R. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-07. 2L72 4F RTA16WE 20030814001022003081400102 2003 8 14 SWIA200312238 420030802A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STICK SHAKER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07954SW 7815 STICK SHAKER ABOUT 1000 FT AT VFTO IN STABLE CLIMB TWO TIMES ABOUT 1 SECOND EACH OCCURRENCE. REMOVED AND REPLACED STALL COMPUTER IAW CRJ MM. OPS CHECK GOOD. P/N: 39-951-002-08 S/N OFF: 208. 2L72 4F RTA21EA 20030814001072003081400107EU 2003 8 14 RAIA00306063 120030612A210032145882 VALVE AEROSPATR42 ATR42300 8680920EU NR 1 PACK INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03426TE2686416851 228 LT PACK FAULT INDICATION. MAINTENANCE DEFERRED NR 1 BLEED SYS PER MEL; SUBSEQUENTLY CLEARING DEFERRAL BY REMOVING AND REPLACING THE NR 1 PACK VALVE. 2H72 4T RTA53EU 20030814001182003081400118NM 2003 8 14 UPS03M40944 120030603A5347S49291477075T6 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 INSPECTION TYPE: C, CORROSION ON SEAT TRACK & FLANGE AT STA 840-860 LBL 27.5. CORROSION ON SEAT TRACK STA 840-860 LBL 27.5, BLENDED OUT AS PER SRM 51-21-01V2R33.ORI-0.090 THK & REMOVED 0.050 FOUND EXCEEDED LIMIT AS PER SRM 53-70-00V1R33. SEAT TRACK LBL 27.5 STA 830-869 TRIMMED & SMOOTHED OUT AS PER SRM 53-70-00V1R33. FAB SPICE & REWORKED SEAT TRACK LBL 27. 5 STA 830-869 & INSTALLED AS PER SRM 51-31-01V2R33. 2L73 4F RTA22WE 20030814001242003081400124WP 2003 8 14 UPS03841042 120030724A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, UPPER MAIN DECK AT BALLMAT AREA STA 140 BL 0 SEAT TRACK SCALLOP WORN. SEAT TRACK SCALLOP OUT OF LIMITS (MAS .500 INCH, ACT .750 INCH) IAW DC8 SRM 53-2-3. REMOVED SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK IAW DC8 SRM 51-3-2, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030814001312003081400131WP 2003 8 14 0301209855 120030527A5330 DOUBLER DOUG DC9 DC951 3022051WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING L-CHECK FOUND CORRODED AND CRACKED DOUBLER ON THE LOWER AFT EDGE OF FUSELAGE PLATE AROUND VENT AT BS 1136 LONGERON 22L. REPAIRED PER EA 98-190987. 2L72 4F RTA6WE 20030814001342003081400134EU 2003 8 14 2003UALA00585 120030722A3610 WARNING SYSTEM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29430UA 568 RETURNED TO FIELD DUE TO NR 2 BLEED INOPERATIVE ECAM MESSAGE. AIRCRAFT RETURNED DUE TO NON-ICING RESTRICTIONS, NR 2 PRV REPLACED. 2L72 4F4 FRTA28NM E40NE 20030814001372003081400137NM 2003 8 14 AALA20030471 120030418A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21678AN 29428 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 1E-6E AND 25D-31D INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR BETWEEN SEATS 1E-6E AND 25D-31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030814001382003081400138NM 2003 8 14 AALA20030315 120030314A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING AT ROWS 4-6 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTING STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030814001432003081400143WP 2003 8 14 GTIA030577 120030708A5320 STRUCTURE DOUG DC9 DC982 3022082WP SUBFLOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND SUBFLOOR AT STATION 210 RBL 24 CRACKED. REMOVED SUBFLOOR. INSTALLED SUBFLOOR. (M) 2L72 4F A6WE 20030725000272003072500027EU 2003 7 25 RAIA00305139 120030512A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03552HK 41057 EMERGENCY EXIT LIGHT BEHIND ROW 10 INOP. RE-SECURED CONNECTOR ON LIGHT ASSEMBLY. 2L72 4T RTA41NM 20030725000302003072500030 2003 7 25 RAIA00305143 420030518A31607011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 CE03559HK8667 41075 CAPTAIN'S SYMBOL GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 SYMBOL GENERATOR. 2L72 4T RTA41NM 20030725000382003072500038EU 2003 7 25 RAIA00305141 120030514A3297 WIRE JETAIRJETSTMJETSTM4101 1500501EU MLG BROKEN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03573HK 41092 LANDING GEAR SELECTOR WILL NOT MOVE TO THE UP POSITION MAINTENANCE REPAIRED BROKEN WIRE NR GA17N. 2L72 4T RTA41NM 20030725000412003072500041NM 2003 7 25 03FDEA00795 120030428A5753ARC0535501 FLAP TRACK DOUG MD11 MD11 3023602NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP INBOARD TRACK (ON WING)FOUND WITH CHAFING MARKS. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD FLAP TRACK REPAIRED AS PER EA 1-5750-69241. 2L73 4F RTA22WE 20030725000462003072500046EU 2003 7 25 03FDEA00843 120030602A5347 SEAT TRACK AIRBUS310 A310 EU CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25410FE 356 FLOOR DAMAGED ON UPPER DECK AT POSITION 6R.DAMAGE CAUSED BY BALLAST PALLET HITTING LOCK DAMAGING FLOOR. NO RESTRICTION FLOOR DAMAGE ON UPPER DECK..REF E.A 6-5321-71244, OK FOR SCV TEMPORARY REPAIR ACCOMPLISHED PER E.A. 6-5321-71244. 0FACT 02JUN03 18:06 CWF U REPAIRED DAMAGED FLOOR STRUCTURE BY REPLACING THE BROKEN SEAT TRACK ADAPTER AND THE BROKEN FLOOR PANEL IAW EA 6-5321-71244 PART 2 2L72 4F RTA35EU 20030725000472003072500047EU 2003 7 25 03FDEA00842 120030602A7714636004502 INDICATOR AIRBUS310 A310 EU ENGINE INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25422FE794 794 346 ON TAKEOFF, N1 ON NR 1 ENG WENT TO 0, TAKEOFF WAS REJECTED AT 95KTS. AFTER REJECT ALL BRAKES WERE HOT AFTER REJECT TO 365DEG, N1 ON #1 MAY HAVE BEEN COMPRESSOR STALL FROM WATER ON RUNWAY. R & R NR 1 N1 INDICATOR PER MM 77-11-21-4. CLEANED AND PROPERLY SECURED ELECT. CONNECTOR OF N1 TACH PER SMP. RAN ENG. PER A310JRH,ALL PARAMETERS, NORMAL. 2L72 4F RTA35EU 20030728000102003072800010NM 2003 7 28 SWAA031629 120030721A323365448105 ACTUATOR BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAK NONE J WARNING INDICATION CLCLIMB 1 SW29320SW 23341 DURING CLIMB-OUT RT MLG EXTENDED. CYCLED LANDING GEAR DOWN THEN UP. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20030728000142003072800014NM 2003 7 28 SWAA031598 120030720A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 689, STR 4R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728000272003072800027NM 2003 7 28 SWAA031544 120030714A3350D71701100 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29700GS 27835 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY EEPLS LIGHTS EXTINGUISHED AFTER 1 MINUTE. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030728000422003072800042NM 2003 7 28 SWAA031536 120030713A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030728000542003072800054 2003 7 28 SWAA031611 420030720A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29758SW 27873 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030801000692003080100069WP 2003 8 1 GTIA030531 120030612A5730 PAINT DOUG DC9 DC982 3022082WP LT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND LEFT WING UPPER TRAILING EDGE TRAP PANEL PAINT CRACKED THROUGH OUT TOP COAT AND VISABLE TO COMPOSITE MATERIAL. REPAIRED DAMAGED AREAS. (M) 2L72 4F A6WE 20030801001032003080100103EA 2003 8 1 COMA0360338 120030724A2730 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ELEVATOR STICKING A COMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01983CA 7169 FLIGHT 5050 ELEVATOR CONTROL STICKING TWICE DURING APPROACH. COULD NOT DUPLICATE. INSPECTED ELEVATOR CONTROL SYSTEM AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20030801001152003080100115 2003 8 1 COMA0360333 420030722A31706229820009 DCU CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01489CA82 7755 FLIGHT 5818 DISPLAY COOL CAUTION MESSAGE. REPLACED THE NR 2 DCU. 2L72 4F RTA21EA 20030805000742003080500074EU 2003 8 5 USAASA03078 120030713A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19755US 1331 DURING THE WEEKLY CHECK, THE EMERGENCY LIGHTS TEST FAILED WITH AN 'EPSU BATTERY R' MESSAGE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY, AND PERFORMED THE EMEGENCY LIGHTS TEST. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030805000832003080500083EU 2003 8 5 ASOA03263 120030617A5330 DOUBLER AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING AN A-CHECK IN MCN, THE FORWARD PASSENGER/CREW DOOR FIRST STEP DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR OF THE FORWARD PASSENGER/CREW DOOR FIRST STEP DOUBLER IAW ASA EO 72-52-0072. (M) 2H72 4T RTA53EU 20030805001032003080500103SO 2003 8 5 ASOA03254 120030605A3397M22759209 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT CHAFED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11268AS 120202 DURING A GROUND INSPECTION IN DFW, THE LT AND RT AFT EXTERNAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A CHAFED WIRE ON THE RIGHT AFT EXTERNAL EMERGENCY LIGHT. REMOVED AND REPLACED THE RIGHT AFT EMERGENCY LIGHT ASSEMBLY. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030806000282003080600028NE 2003 8 6 BAQA088188 220030723A72000319007030 ENGINE UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03533ME2163 132 EXCESSIVE OIL DRAINING FROM TAILPIPE AT SHUT DOWN. ENGINE LOG BOOK ENCLOSED. 7/30/03 1G72 3U3 U H88EU E19EU 20030806000642003080600064SO 2003 8 6 C2XA03SH233 120030726A532013500322001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV-DURING C-CHECK, THE LEFT HAND SILL BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806000762003080600076SO 2003 8 6 C2XA03SH220 120030711A541014576057622 STIFFENER EMB 145 EMB145LR 3260212SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 DURING C-CHECK, THE RIGHT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806000802003080600080EU 2003 8 6 AWXA200300807 120030627A5350D5331032300820 PANEL AIRBUS320 A320231 3930325EU FAIRING DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 DURING C-03 CHECK THE LOWER CENTER BELLY FAIRING (191BB) WAS FOUND DELAMINATED ALONG THE FORWARD LOWER EDGE AT THE RT AFT OUTBOARD CORNER, FR 34. MAINTENANCE REMOVED AND REPLACED THE LOWER CENTER BELLY FAIRING (191BB) IAW A320 AMM SUBTASK 53-35-13-020-052-AO & 53-35-13-420-051-AO. 2L72 4F RTA28NM 20030806000822003080600082NM 2003 8 6 AWXA200300809 120030709A5315D5347217220340 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y-1292, BETWEEN FR67 AND FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOORBEAM Y-1292, BETWEEN FR67 AND FR 68; INSTALLED A NEW REPLACEMENT FLOORBEAM IAW SRM 51-42-11, PG 6-7. 2L72 4F RTA28NM 20030806000852003080600085SO 2003 8 6 C2XA03CL130 120030729A335074441 LIGHT EMB 135 EMB135ER 3260203SO GALLEY INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2725504 145186 CLE FLIGHT 2239, THE CREW REPORTED THE EMERGENCY LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REPLACED THE GALLEY EMERGENCY LIGHT, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030806000942003080600094SO 2003 8 6 C2XA03TY088 120030704A533014520556001 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 TYS- DURING A SERVICE ROUTINE THE FUSELAGE JUST AFT OF THE SERVICE DOOR DAMAGE WAS FOUND BETWEEN FR 24 AND 25 AND STR 12 AND 13 RT. MAINTENANCE INSTALLED FILLER AND PATCH IAW EC 2003-145/2279 AND 135/145 SRM CHAPTER 51. ALL WORK WAS ACCOMPLISHED AND WAS REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030806001032003080600103SO 2003 8 6 C2XA03SH240 120030731A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO DOORWAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, THE CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001112003080600111SO 2003 8 6 C2XA03TY117 120030801A534714530659007 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION, SEAT TRACK RW4 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030806001152003080600115SO 2003 8 6 C2XA03SH242 120030731A531014522460009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO HAVE CORRSION AND TOOLING MARKS BETWEEN FRAMES 18-23. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001282003080600128NM 2003 8 6 AWXA200300827 120030711A5311654653932 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A 1 INCH CRACK WAS FOUND ON FRAME INNER CHORD AT BS 616, RBL 45, WL 200. MAINTENANCE CUT OUT CRACK ON FRAME INNER CHORD AT BS 616, RBL 45, WL 200; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENING ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20030806001542003080600154SO 2003 8 6 C2XA03SH212 120030702A531014529150001 CROSSBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030806001602003080600160SO 2003 8 6 C2XA03SH247 120030801A491012010732001 FRAME EMB 145 EMB145LR 3260212SO APU FIREWALL GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, THE APU FIREWALL FRAME 81 WAS FOUND GOUGED AT BOTTOM CENTER. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR ON AFFECTED FRAME IAW CONTINENTAL EXPRESS EC 5310-01246. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001622003080600162NE 2003 8 6 AWXA200300805 220030716A732079830018050 EEC AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28645AW34782384 238 DURING TAKEOFF AT PHX EN ROUTE FOR DEN THE CREW PUSHED POWER UP FOR TAKEOFF AND THE NR 2 ENGINE DID NOT RESPOND, POWER REMAINED AT IDLE, REJECTED TAKEOFF. FLIGHT CREW NOTED THAT THE NR 1 ENGINE DID RESPOND NORMALLY. APPROXIMATELY 5 MINUTES LATER; RECEIVED ECAM MESSAGE NR 2 ENGINE EPR MODE FAULT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ELECTRONIC ENGINE CONTROL UNIT (EEC) PER AWA T/C R5M73002. OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST OF EEC S/N 2005-0011 CONFIRMED FAILURE OF UNIT FOR FAILING DISCRETE DRIVER OUTPUT TEST AND OVER CURRENT PROTECTION TEST. TEARDOWN REVEALED THE FLAME SHIELDS AND PB PORT SCREEN WERE DAMAGED BEYOND REPAIR. REPLACED FLAME SHIELDS (P/N'S 809426-1, 808144-1, & 8082L72 4F4 FRTA28NM E311NE 20030807000012003080700001EA 2003 8 7 ASOA03262 120030611A521060031535 STRIKER CNDAIRCL600 CL6002B19 1900309EA DOOR SEAL DENTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING HANGAR MAINTENANCE IN CKB, THE PASSENGER DOOR SEAL STRIKER AT FS 310 AND FS 349 BETWEEN STRINGERS 15L AND 16L WAS FOUND TO BE DENTED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR SEAL STRIKER AT FS 310 AND FS 349 BETWEEN STRINGERS 15L AND 16L IAW REO 601R-52-11-008, REV B. (M) 2L72 4F RTA21EA 20030807000092003080700009EA 2003 8 7 ASOA03257 120030611A531560035031563 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING HANGAR MAINTENANCE IN CKB, THE LT AND RT FLOORBEAM ANGLE AT FS 621, WL 73, RBL AND LBL 39 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FLOORBEAM ANGLE AT FS 621, WL 73, RBL AND LBL 39 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20030807000192003080700019NM 2003 8 7 USAA030111 120030706A5314 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 FOUND LT KEELBEAM CORRODED LOWER CHORD INBOARD SURFACE STATION 727, 1.5 INCHE LONG .050 INCH - .070 INCH DEEP. KEELBEAM INSTALLED WITH SPLICE AT STATION 540 PER TYPICAL REPAIR 53-60-09. (M) 2L72 4F RTA16WE 20030805000712003080500071EA 2003 8 5 ASOA03269 120030611A5320601R31171 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING HANGAR MAINTENANCE IN CKB, THE FLOOR SUPPORT INTERCOSTAL AT THE ATTACH FLANGE, FS 484 AT RBL AND LBL 36, AND THE ANGLE AT LBL 27, WL 73 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT INTERCOSTALS AT THE ATTCH FLANGE, FS 484 AT RBL AND LBL 36, AND THE ANGLE AT LBL 27, WL 73 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20030805000872003080500087EA 2003 8 5 ASOA03303 120030713A53306013600129 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE FRAME DOUBLER AT FS 640 BETWEEN STRINGERS 9 AND 12 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPLACED THE FRAME DOUBLER AT FS 640 BETWEEN STRINGERS 9 AND 12 ON THE LEFT SIDE IAW ASA EO 600-53-0075. (M) 2L72 4F RTA21EA 20030806000192003080600019 2003 8 6 I05R088310 420030721A3120B1894522282A CLOCK SNIAS 350 AS350* EU COCKPIT INTERMITTENT E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 3560 CLOCK IS INTERMITTENT, REPLACED PART 1G71 3U H9EU 20030806000372003080600037SO 2003 8 6 C2XA03CL134 120030804A3350110049 POWER SUPPLY EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716944 145045 DURING ROUTINE MAINTENANCE BOTH OVERWING EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 POWER SUPPLY AND THE RIGHT OVERWING LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030806001302003080600130NM 2003 8 6 AWXA200300856 120030714A5312651758245 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, RBL 17.1, WL 183. MAINTENANCE CUT OUT DAMAGED SECTION OF BULKHEAD WEB, RBL 17.1, WL 183; FABRICATED A DOUBLER AND NEW SECTION OF WEB; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG 10-11. 2L72 4F RTA16WE 20030806001492003080600149SO 2003 8 6 C2XA03IA069 120030629A3397487191 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716559 145603 DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT SIGN AT THE FRONT GALLEY WAS INOP. MAINTENANCE RESECURED THE CONNECTOR AT THE LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001662003080600166NM 2003 8 6 AWXA200300839 120030706A5320D53470477208 PROFILE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT PROFILE BETWEEN FR-52 AND FR 56, LBL 711.2. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT PROFILE BETWEEN FR-52 AND FR 56, LBL 711.2; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND REPAIR SPLICE; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1. 2L72 4F RTA28NM 20030728000602003072800060 2003 7 28 SWAA031635 420030722A256565C19901 CABLE BOEING737 7372H4 138448CNM ENTRY DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030728000672003072800067NM 2003 7 28 SWAA031539 120030712A3350101114 LENS BOEING737 7377H4 1384404NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29783SW 29809 RT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. REINSTALLED LENS PER MM. 2L72 4F RTA16WE 20030728000712003072800071NM 2003 7 28 SWAA031522 120030711A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 21L, BS 967 AND BS 973. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728000742003072800074NM 2003 7 28 SWAA031548 120030714A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030728000792003072800079 2003 7 28 SWAA031569 420030716A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030723000472003072300047NM 2003 7 23 TSAA0351142 120030505A5320 ANGLE BOEING737 73725A 1384481NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DISCOVERED A CRACKED ATTACHMENT ANGLE LOCATED AT BS 289, WL 239. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2. (M) 2L72 4F RTA16WE 20030723000562003072300056NM 2003 7 23 TSAA0353141 120030505A5320 STRINGER CLIP BOEING737 73725A 1384481NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DISCOVERED A DAMAGED STRINGER CLIP LOCATED AT BS 380, STRINGER 2 RIGHT. REMOVED AND REPLACED DAMAGED CLIP. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-2, FIGURE 1. (M) 2L72 4F RTA16WE 20030723001072003072300107NM 2003 7 23 DL733030502 120030531A53306545775594 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO273301 23181 THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST ABOVE STRINGER 24R AND A 2 INCH CRACK JUST BELOW STRINGER 24R. THE CRACKS RAN ALONG THE BONDED WAFFLE DOUBLER MILL LINE. THERE WAS AN EXISTING EXTERNAL DOUBLER REPAIR IN THE AREA FOR SIMILAR PREVIOUS CRACKING. THE AREA OF SKIN BETWEEN FS 720D & 747 AND BETWEEN STRINGERS 20R & 25R WAS CUT TO REMOVE DAMAGE AND DOUBLER. A NEW SECTION OF SKIN WAS SPLICED. 2L72 4F RTA16WE 20030723001142003072300114NM 2003 7 23 AWXA200300663 120030518A53116546526 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON OUTBOARD FLANGE OF FRAME AT BS 400, STR 14 RT. MAINTENANCE CUTOUT CRACK ON OUTBOARD FLANGE OF FRAME AT BS 400, STR 14 RT, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A SHEAR TIE AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07 PG 213-215, FIG 205. 2L72 4F RTA16WE 20030724000342003072400034NM 2003 7 24 DLM88030534 120030611A53305920323249 SKIN DOUG MD88 MD88 3023688NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27981DL 53268 LIGHTNING STRIKES OCCURRED TO MULTIPLE FASTENER LOCATIONS THROUGH THE FUSELAGE SKIN AND POTABLE WATER SERVICE DOOR SURROUND DOUBLER. A CUTOUT MEASURING 3.7 INCH (FWD-AFT) X 3.8 INCH (UP-DOWN) WAS MADE WITH THE LOWER EDGE BEING 3 INCH FROM THE UPPER EDGE OF THE POTABLE WATER SERVICE PANEL CUTOUT. THE SKIN IS 0.050 INCH 2024-T3 CLAD SHEET. THE SURROUND DOUBLER IS 0.063 INCH 7075-T6 CLAD SHEET. DAL ER/A 379042-14 INSTALLS A 0.063 INCH 2024-T3 CLAD DOUBLER AND 0.071 INCH 7075-T6 CLAD TRIPLER SIMILAR TO MD80 SRM 53-04, F12B, EXCEPT FINGER DOUBLERS WERE OMITTED. 2L72 4F RTA6WE 20030724000532003072400053 2003 7 24 SWAA031439 420030629A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29712SW 0283 27846 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030724000642003072400064NM 2003 7 24 AWXA200300773 120030702A27512061141 INDICATOR BOEING737 7373S3 1384711NM TE FLAPS FALSE INDICATIONA AWXAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP28312AW110241843 24060 ON DESCENT INTO BUR EN ROUTE FROM PHX TRAILING EDGE FLAPS LOCKED OUT BETWEEN 1 AND 2 DEGREES. RUNWAY TO SHORT AT BUR, DIVERTED TO LAX WITH LONGER RUNWAY. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR, OPERATIONAL CHECK WAS GOOD IAW BMM 27-58-41 PG 401-404. 2L72 4F RTA16WE 20030724000852003072400085NM 2003 7 24 DLM88030556 120030617A33500201984001 LIGHT DOUG MD88 MD88 3023688NM L2 DOOR BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27908DE 53417 L2 GALLEY DOOR EXIT LIGHT IDENTIFIER BASE BROKEN. REPLACED L2 GALLEY EXIT DOOR EMERGENCY LIGHT BASE. EMERGENCY LIGHT, CHECKS OK. 2L72 4F RTA6WE 20030725000042003072500004NM 2003 7 25 DL76S030583 120030624A3350 BULB BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27134DL 25123 CREW REPORTS L1 DOOR EMERGENCY LIGHT INOPERATIVE IN THRESHOLD UPPER FWD CORNER. RELAMPED, TESTED IAW M/M. 2L72 4F RTA1NM 20030728000212003072800021 2003 7 28 SWAA031525 420030711A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030728000282003072800028NM 2003 7 28 SWAA031564 120030714A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030806001672003080600167SO 2003 8 6 C2XA03TY118 120030801A534714532606015 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION, SEAT TRACK LF5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030807000172003080700017NM 2003 8 7 UIEA200300036 120030624A5315 FLOORBEAM BOEING747 7472D3B 1384805NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15506MC 21252 DURING C-CHECK, MAIN DECK FLOORBEAM WEB AND BEAM FOUND CRAKCED AT BS 320 AND APPROXIMATE AT RBL 40. FLOORBEAM AND WEB REPAIR CARRIED OUT PE IAI REPAIR SCHEME AND 8110-3. REPAIR AREA BS 320, RBL 38 TO BE VISUAL INSPECTED, AT THE FOLLOWING INTERVAL, 1500 HOURS OR 200 CYCLES, WHICH EVER COMES FIRST. ATLAS AIR MCI NR A139 ISSUED FOR THE REINSPECTION. (M) 2L74 4F RTA20WE 20030807000232003080700023NM 2003 8 7 USAA030128 120030624A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US 24552 FOUND FLOORBEAM CORRODED SEVERAL 1 INCH AREAS, BS 986, LBBL 45 TO RBBL 35. CORROSION LEVEL 1, TASK NR C53-107-02. INSTALLED NEW-T-CAP PER TYPICAL REP 53-60-01. (M) 2L72 4F RTA16WE 20030807000242003080700024NM 2003 8 7 USAABB03113 120030716A335020121 CHARGER BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 FOUND FORWARD RIGHT FLOOR LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2L72 4F RTA1NM 20030807000372003080700037NM 2003 8 7 C1HA200381013 120030603A2751 WARNING HORN BOEING727 7272S7 138407ZNM COCKPIT MALFUNCTIONED A C1HAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15681CA 22020 AFTER CLEARED FOR TAKEOFF WHILE PERFORMING 1.4 EPR TAKEOFF WARNING HORN SOUNDED. AFTER RETURNING TO GATE FLAPS AND SPEED BRAKE HANDLE CYCLED, NO TROUBLE FOUND. 2L73 4F A3WE 20030807000462003080700046NM 2003 8 7 C1HA200394014 120030711A2697 WIRE BOEING727 727290 138408WNM OVERHEAT LIGHT DAMAGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 LOWER AFTER BODY OVERHEAT LIGHT CAME ON DURING TAXI BACK TO GATE. REPAIRED DAMAGED WIRE ABOVE ROW 3DEF W298-122-16+ W298-012-16 IAW WIRING PRACTICES CH 20. REMOVED AND REPLACED FIRE AND OVERHEAT ACCY UNIT, OPS CHECK NORMAL IAW MM 26-14-11. 2L73 4F A3WE 20030807000742003080700074SO 2003 8 7 C2XA03SH236 120030728A541014576057021 STIFFENER EMB 145 EMB145LR 3260212SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE NUMBER 1 UPPER ENGINE COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030807000792003080700079EA 2003 8 7 03209668 120030728A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27668BR 7544 DURING MAINTENANCE INSPECTION THE FLOOR EMERGENCY LIGHTING AT THE SERVICE DOOR WAS DISCOVERED INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FLOOR EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030807000802003080700080NM 2003 8 7 03209411 120030728A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27411FJ 3166 DURING INSPECTION THE CREW REPORTED THE LAST ONE THIRD EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND COULD NOT DUPLICATE THE FAULT. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030807000892003080700089 2003 8 7 GLBA2003109 420030721A34226226136002 GYRO BEECH 1900 1900D 1154162CE COCKPIT FROZEN A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 NM03240GL11387 UE240 NR 1 DG FROZE. REMOVED AND REPLACED NR 1 DG. 2L72 4T RTA24CE 20030807000962003080700096CE 2003 8 7 GLBA2003103 120030707A2120 SCREEN BEECH 1900 1900D 1154162CE CABIN PRESSURE DIRTY A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03226GL UE226 CABIN WILL NOT PRESSURIZE. CLEANED PRESSURE CONTROLLER INLET SCREEN, OPS CHECK GOOD. 2L72 4T RTA24CE 20030807001012003080700101NM 2003 8 7 EIA2003098 120030724A5330 DOUBLER BOEING747 747212B 1384886NM FUSELAGE CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 LT LOWER FUSELAGE EXTERNAL CHAFING MARKS ON REPAIR DOUBLER AT STA 980 STR 44L. REMOVED AND REPLACED DOUBLER PER B747 SRM 553-30-03. 2L74 4F A20WE 20030807001082003080700108CE 2003 8 7 GLBA2003104 120030710A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE TORQUE FAILED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03153GL5809 UE153 NR 1 TORQUE INDICATOR FAILED. REMOVED AND REPLACED NR 1 TORQUE IND. 2L72 4T RTA24CE 20030807001102003080700110EA 2003 8 7 HNAA0300037 120030729A32338300101 ACTUATOR DHAV DHC8 DHC8311 1386006EA NLG SLOW A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07342EN18104 395 AFTER TAKEOFF, CREW RECEIVED A NOSE GEAR UNSAFE INDICATION FOR 5 - 10 SECONDS AFTER THE MAIN GEAR LIGHTS EXTINGUISHED. REPLACED NOSE LANDING GEAR RETRACTION ACTUATOR. 2H72 4T RTA13NM 20030807001162003080700116 2003 8 7 BAQA087761 420030625A3442071137800 SENSOR BOLKMS117 BK117A3 5626015EU RADAR INACCURATE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LC 7027 INDICATING ERRONEOUSLY AND COLORED BARS. REPLACED. 7/22/03 1G72 3U H13EU 20030807001202003080700120SW 2003 8 7 ALGA088137 120030709A6340407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH STUCK B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03507AL 53103 DUAL TACH STUCK AT 120 PERCENT. 1G71 3U O H2SW 20030728000292003072800029NM 2003 7 28 SWAA031577 120030717A52306547952 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR OUTER SKIN CRACKED AT UPPER AFT CORNER OF HANDLE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728000912003072800091 2003 7 28 SWAA031622 420030722A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT CABIN DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS ARE OUT OF VIEW. REPOSITIONED BOTH AFT CABIN DOOR SLIDES PER MM. 2L72 4F A16WE 20030728000952003072800095NM 2003 7 28 SWAA031616 120030720A53126545409 PRESSURE PANEL BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, RBL 43. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20030728001002003072800100 2003 7 28 SWAA031583 420030720A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29754SW 29849 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030728001112003072800111NM 2003 7 28 SWAA031582 120030717A7711658536911 SENSE LINE BOEING737 7372H4 138448CNM NR 1 ENGINE FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING UKUNKNOWN 1 SW29096SW 23055 AIR TURNBACK, NR 1 ENGINE EPR HIGH INDICATIONS AT ALTITUDE. REMOVED AND REPLACED NR 1 ENGINE EPR PT2 SENSING LINE AT ENGINE NOSE DOME PER MM. 2L72 4F A16WE 20030728001122003072800112 2003 7 28 SWAA031570 420030714A2565D31354 SLIDE BOEING737 737301 1384611NM ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030728001232003072800123NM 2003 7 28 SWAA031481 120030705A335007912 COVER BOEING737 7375H4 138449DNM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED PM CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 3. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030728001242003072800124NM 2003 7 28 SWAA031429 120030626A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29751SW 29803 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (12 EA) THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030728001302003072800130WP 2003 7 28 AMTA200300896 120030608A5210 DOUBLER LKHEED1011 10113853 5265020WP L1 DOOR BENT A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 L1 DOOR UPPER FORWARD CORNER REPAIR DOUBLER BENT. REPAIRED DOOR SKIN IAW ER/A L10-52R-5185. (M) 2L73 4F A23WE 20030728001392003072800139NM 2003 7 28 03FDEA01043 120030704A5510NLC6725 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 SNRM N0883 : LT HORIZONTAL STABILIZER NR 10 BORE CORROSION EXCEEDED LIMIT AFTER REWORK. CORROSION REMOVED AND REPAIR CARRIED OUT IAW EA NR 1-5510-69392. 2L73 4F RTA22WE 20030729000042003072900004NM 2003 7 29 03196426 120030715A2450230GC02Y04 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE COCKPIT FAULTY A VTZAK NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA27426FJ 3190 DURING CRUISE, THE CREW REPORTED A TOTAL GENERATOR FAILURE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE 1VE PANEL. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030729000212003072900021EA 2003 7 29 03193637 120030712A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27637BR 7308 DURING PREFLIGHT INSPECTION THE CREW REPORTED THE L/H OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED THE OVERWING EMERGENCY LAMP. A SATISFACTORY OPERTIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000252003072900025EA 2003 7 29 03193650 120030712A33503071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27650BR 7418 DURING OVERNIGHT MAINTENANCE THE FORWARD EMERGENCY LIGHT WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED THE FOWARD EMERGENCY LAMP. A SATISFACTORY OPERTIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000272003072900027EA 2003 7 29 03195636 120030714A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27636BR 7307 DURING OVERNIGHT MAINTENANCE THE RT OVERWING EMERGENCY EXIT LIGHT WAS DISCOVERED INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED THE OVERWING EMERGENCY LAMP. A SATISFACTORY OPERTIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000402003072900040NM 2003 7 29 ZW0A0305804 120030702A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13727TW 30340 THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS AT THE L1, R1, L2, R2, L4, AND R4 DOORS WERE ADJUSTED ACCOUNT DEFORMED. 2L72 4F RTA2NM 20030807001212003080700121SW 2003 8 7 ALGA088159 120030721A6420406312100101 BEARING BELL 407 407 1182206SW TAIL ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03404AL288 53479 FOUND 4 EA. BEARINGS WORN EXCESSIVELY. REMOVED AND REPLACED. 1G71 3U O H2SW 20030812000032003081200003NE 2003 8 12 HEEA088385 220030804A73200164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE TMECA ARRIUSARRIUS1A NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 FUEL CONTROL PRODUCING HARD START. TO BE SENT TO VENDOR. 1G72 3U3 U H1NE E34NE 20030812000042003081200004 2003 8 12 HEEA088393 420030730A3455071121004 CONTROL BOX SKRSKYS76 S76A 8143006NE ADF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 ADF SYSTEM CONTROL BOX INOPERATIVE. IN SHOP REPAIR. 1G72 3U H1NE 20030812000052003081200005NE 2003 8 12 HEEA088401 120030805A62207610608000050 DAMPENER SKRSKYS76 S76A 8143006NE MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03763P 760166 MAIN ROTOR DAMPENER LEAKING. SHOP REPAIR. 1G72 3U H1NE 20030812000232003081200023SW 2003 8 12 HEEA088444 120030729A2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL TRANS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TROUBLESHOOTING FUEL TRANSFER LIGHT STAYING ON TOO LONG. REPLACED SIGNAL COND. UNIT. 1G72 4U H4SW 20030903000322003090300032WP 2003 9 3 EOO2003F00002 120030612A2560369H30251 FITTING HUGHES369 369D 4470706WP SHOULDER HARNESSWORN A EOORO OTHER O OTHER NRNOT REPORTED 1 AL03511SB 1090592D DURING A CONFORMITY INSPECTION ON A LEASE AIRCRAFT, METAL SET WAS FOUND ON THE REAR SEAT SHOULDER HARNESS FITTINGS, REMOVAL OF THE METAL SET REVEALED EXTENSIVE WEAR ON ONE FITTING AND MINOR WEAR ON THE OTHER. SEE MDN SOR NR 300198 - TSN 11596.9. 1G71 3U H3WE 20030828001342003082800134NE 2003 8 28 A102003F00000 220030403A72301277M97G02 ROTOR BOEING737 737317 138447PNM GE CFM56 CFM56* 13802NE NR 1 ENGINE DAMAGED A A10BK NONE O OTHER ININSP/MAINT 1 SO15253DV 23800 721787 WHILE PERFORMING BORESCOPE OF NUMBER ONE ENGINE FOUND HPC 6TH STAGE ROTOR TO BE DAMAGE BY FOD AND OUT OF LIMITS. 2L72 4F4 FRTA16WE E2GL 20030828001542003082800154EU 2003 8 28 USAASA03047 120030311A25609Y52262591 DOUBLER AIRBUS320 A320214 3930316EU CABIN DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19119US 1268 BOS - THE TELESCOPING PORTION OF THE GIRT BAR ASSEMBLY WAS FOUND TO COLLAPSE WITHOUT PULLING ON THE TRIGGER. ADDITIONALLY, THE DOUBLER WAS FOUND BEYOND LIMITS. MAINTENANCE REPLACED THE DOUBLER. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030828001602003082800160EU 2003 8 28 USAABA03027 120030804A335032146210 POWER SUPPLY AIRBUS330 A330323 3930335EU CABIN FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 PHL - EPSU AT DOOR R3 FAILED CHECK. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA46NM 20030828001652003082800165 2003 8 28 USAABA03029 420030810A3460C12858CA01 COMPUTER AIRBUS330 A330323 3930335EU COCKPIT MALFUNCTIONED A USAAO OTHER O OTHER CRCRUISE 1 EA19675US 0370 PHL - FLT 11 - EN ROUTE, CREW RECEIVED INDICATIONS THAT BOTH FMGEC'S HAD LOST DATA. CREW MANUALLY ENTERED WAYPOINTS AND ROUTE DATA WAS UPLINKED. SYSTEM PERFORMED NORMALLY THROUGHOUT THE REMAINDER OF THE FLIGHT. MAINTENANCE REPLACED BOTH FMGEC'S. (M) 2L72 4F RTA46NM 20030829000022003082900002CE 2003 8 29 52055 120030629A3240 BRAKE ASSY BEECH 1900 1900D 1154162CE RT MLG CONTAMINATED A AMWAK NONE O OTHER UKUNKNOWN 1 CE07133YV UE133 THE RIGHT BRAKES GO FLAT WHEN PRESSURE WAS APPLIED. MAINTENANCE BLED THE BRAKES. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030829000112003082900011 2003 8 29 MEX2003237 420030618A34134067241862 INDICATOR BOEING757 7572Q8 1384972NM COCKPIT FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23804AM 26271 AIRCRAFT RETURN TO PLATFORM DUE TO TCAS NR 1 BLOCKED WITH INDICATION IN DISPLAY. THE INDICATOR VSI/TRA DISPLAY WAS REPLACED IAW 34-22-06, ALL TEST CORRECT. 2L72 4F RTA2NM 20030829000382003082900038NM 2003 8 29 CALA0300491 120030825A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND CORROSION AROUND NUT CLIP HOLES ON LT AFT LAV WALL SUPPORT HAT CHANNEL. THE WALL SUPPORT HAT CHANNEL WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030829000402003082900040EA 2003 8 29 COMA0360375 120030818A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS MALFUNCTIONED A COMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO01977CA 7157 FLIGHT 5808 FLAPS FAILED AT 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030829000642003082900064NM 2003 8 29 DHL2003721007 120030715A498065379457 DUCT SEAL BOEING727 727228 1384083NM APU LEAKING A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01721DH 19545 WHEEL WELL ALARM ACTIVATED. FOUND APU UPPER EXHAUST SEAL LEAKING INTO WHEEL WELL. NO WHEEL WELL ALARM AFTER APU SHUTDOWN. NO OTHER INDICATIONS NOTED PER B-727 M/M 26-12-00. SEE ITEM 2M BELOW. APU UPPER EXHAUST DUCT LEAKING INTO RT WHEEL WELL. ITEM DEFERRED PER DHL MEL 49-1 CAT-C CONTROL 13541. NOTE: NO APU OPERATION PLACARDS INSTALLED. REF DMI 13541 MEL 49-1 APU UPPER EXHAUST DUCT LEAKING IN WHEEL WELL. REMOVED AND REPLACED APU EXHAUST DUCT SEALS. LEAK CHECKED GOOD IAW B727 M/M 49-80-53. THIS CLEARS DMI 13541. ALL PLACARDS REMOVED. 2L73 4F RTA3WE 20030729000622003072900062EA 2003 7 29 QXEA200300842 120030708A2820D98C09602 PRESSURE SWITCH CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS UKUNKNOWN 1 NM09607QX2082 2082 10024 SEA- ON FLIGHT 2471 FUEL LEAKING FROM CENTER TANK AREA. REMOVED AND REPLACED LEFT BOOSTER PUMP PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000632003072900063NM 2003 7 29 QXEA200300869 120030723A6123 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE NACELLE OUT OF ADJUST A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09364PH 524 PDX- ON FLIGHT 2092 ABORTED TAKEOFF DUE TO AUTOFEATHER FAILED TO ARM. RESET AUTOFEATHER ARMING POINTS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030724000402003072400040NM 2003 7 24 DL73K030539 120030612A53126546568553 STRAP BOEING737 737247 138448DNM FUSELAGE BUCKLED A DALAK NONE O OTHER ININSP/MAINT 1 SO27381DL 23608 FS 1016 PRESSURE BULKHEAD / OUTER CIRCUMFERENTIAL TEAR STRAP / STR5L TO 7L - BUCKLING: THE SUBJECT STRAP WAS FOUND BUCKLED BETWEEN FASTENERS FROM THE BULKHEAD WEB SPLICE AT S-7L TO APPROXIMATELY S-6L. THERE IS NO BUCKLING OR OIL CANNING OF THE BULKHEAD WEB. THE TEAR STRAP IS M/F 0.025 INCH CLAD 2024-T3 SHEET. DAL ER/.A 385240-14 INSTRUCTS TO CUTOUT THE DAMAGED TEAR STRAP, VISUALLY INSPECT THE SURROUNDING AREA, HFEC INSPECT FASTENERS IN THE AREA, AND INSTALL A REPLACEMENT SECTION OF TEAR STRAP FROM 0.032 INCH 2024-T3 CLAD SHEET. 2L72 4F A16WE 20030724000482003072400048NM 2003 7 24 DL733030548 120030613A2130215001003 VALVE BOEING737 737301 1384611NM CABIN PRESSURE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27948WP 23259 AT 33000 FT WARNING HORN SOUNDED AND COCKPIT LOST PRESURIZATION. CABIN ALT CLIMBED TO 12500 AND AUTO FAIL LIGHT ILLUMINATED ON CABIN PRESSURIZATION CONTROLLER. RAN PRESSURIZATION CONTROLLER CHECK, PRESSURIZED ACFT CHECKED ENGINE PNEUMATICS ALL CHECKED GOOD. WHILE CHECKING PACK SYSTEM FOUND LT PACK CONTROL VALVE WILL NOT SHUT OFF. REPLACED VALVE SYSTEM CHECKS GOOD. 2L72 4F RTA16WE 20030724000622003072400062EA 2003 7 24 03190675 120030709A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27675BR 7635 DURING MAINTENANCE INSPECTION, AN INTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030724000732003072400073NM 2003 7 24 AWXA200300555 120030517A27511812996 INDICATOR BOEING737 7373G7 1384595NM TE FLAPS FROZEN A AWXAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 WP28322AW3962 25400 ON APPROACH INTO SAN EN ROUTE FROM PHX TRAILING EDGE FLAPS FROZE IN POSITION -10-, WOULD NOT MOVE UP OR DOWN. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR IAW AWA T/C R1B27001, OPERATIONAL CHECK WAS GOOD. **SUPP** VENDOR BENCH TEST OF FLAP INDICATOR WAS NO FAULT FOUND, UNIT WAS TESTED/INSPECTED IAW CMM 27-50-07 AND RETURNED TO SERVICE. 2L72 4F RTA16WE 20030724000822003072400082NM 2003 7 24 DL733030553 120030617A25304160001 COFFEEMAKER BOEING737 7373B7 1384580NM FWD GALLEY LEAKING A DALAH DEACTIVATE SYST/CIRCUITS K FLUID LOSS CRCRUISE 1 SO27951WP 22951 ELEC ODOR COMING FROM FWD GALLEY COFFEEMAKER UNIT WAS TURNED OFF AND CB'S OPENED ODOR WENT AWAY. REMOVED COFFEEMAKER FOR INSPECTION FOUND WATER LEAK AT WATER SUPPLY TO HEATING TANK SECURED B-NUT DRIED ENTIRE DISPENSER CAVITY REINSTALLED BREWED TWICE THROUGH CYCLE NO ODORS DETECTED ALL WIRE CONNECTIONS AND RELATED ELECTRICAL COMPONENTS TO DISPENSER APPEAR NORMAL, OK FOR SERVICE. THIS OCCURRED IN FLIGHT. 2L72 4F RTA16WE 20030725000362003072500036SO 2003 7 25 RAIA00305148 120030521A243051545002A GCU EMB 145 EMB145 3260210SO NR 4 GENERATOR FAULTY A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03807HK5981 145119 GENERATOR NR 4 FELL OFF LINE. MAINTENANCE REMOVED AND REPLACED NR 4 GENERATOR CONTROL UNIT. 2L72 4F RTT00011AT 20030725000392003072500039 2003 7 25 RAIA00305037 420030509A34207003360948 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU NR 2 AHRS UNRELIABLE A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03550HK146322845 41039 FO PITCH ERROR INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS INDICATOR. 2L72 4T RTA41NM 20030725000452003072500045EU 2003 7 25 CX7A194J0347 120030602A2613173436450 DETECTOR SAAB SF340 340B 7860101EU LT ENG TAILPIPE MALFUNCTIONED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03302CE 340B193 LT TAIL PIPE HOT ILLUMINATED DURING T/O EXECUTED CHECKLIST. LIGHT EXTINGUISHED. RETURN TO AIRPORT 2L72 4T RTA52EU 20030728000412003072800041NM 2003 7 28 SWAA031526 120030710A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS COVERS BROKEN AT ROW NR 1. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030728000582003072800058 2003 7 28 SWAA031633 420030723A256563551101 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030729000152003072900015EA 2003 7 29 03200500 120030719A3350321473 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27500FJ 3197 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING IN ROWS 4 THRU 6 WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A POWER SUPPLY. AN SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000512003072900051NM 2003 7 29 ZW0A0305704 120030626A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13711ZX 28481 THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS WERE ADJUSTED ACCOUNT DEFORMED AT THE L1, L2, AND R4 DOORS. THE SPRING WAS REPLACED ACCOUNT BENT AT THE R1 DOOR. 2L72 4F RTA2NM 20030729000722003072900072EA 2003 7 29 QXEA200300726 120030612A2840 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM09612QX 10042 SJC-ON FLIGHT NUMBER 2456, TRANSFER PUMP CAUTION LIGHT ON TAXI OUT. RESET FUEL SYSTEM CONTROL CIRCUIT BREAKERS. NO FURTHER CAUTION OR FAULT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000782003072900078NE 2003 7 29 QXEA200300747 220030617A7321 CONNECTOR DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 1 ENGINE DIRTY A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09357PH 504 SEA-ON FLIGHT NUMBER 2124, NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. ECU MODE SELECTOR CYCLED PER EMERGENCY CHECKLIST. INSPECTED AND CLEANED CANNON PLUGS ON NR 1 ENGINE ECU. PERFORMED RESET OF BETA LOCKOUT SYSTEM. LIGHT EXTINGUSHING. PERFORMED POWER ASSURANCE TEST OF NR 1 ENGINE. NO DEFECTS NOTED. NO LIGHT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030729000892003072900089WP 2003 7 29 ABXA030287 120030718A3260 UPLOCK SWITCH DOUG DC9 DC941 302207NWP PWA JT8 JT8D* NE RT MLG FAILED A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23951AX 47616 RT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. ALL INDICATIONS WERE NORMAL. REPLACED RIGHT GEAR UPLOCK SWITCH IAW MM 32-60-01-2. ALSO FOUND CANNON PLUG P1-1150 VERY CORRODED, REPLACED PLUG. OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20030729000922003072900092NE 2003 7 29 MEX2003219 220030609A7321 FUEL CONTROL DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE NR 1 ENGINE CONTAMINATED A ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23881LF 53051 FLT 162 - MEX-CUL - AIRCRAFT RETURNED TO GATE, DURING TAKEOFF POWER, NR 1 ENGINE HAD A DELAY 15 OF SECONDS TO REACH 1.4 EPR. FCU WATER TRAMP WAS DRAINED AND CLEANED IAW MM 71-00-00, ALL CORRECT. (M) 2L72 4F4 FRT E9NE 20030729000972003072900097EU 2003 7 29 2003F00477 120030515A5350 SKIN AIRBUS320 A320233 3930329EU REAR CONE DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND DENT ON REAR CONE SKIN FS 82, STATION 38035. REPAIRED DENT IAW SRM 53-51-11 FIGURE 203 PAGE 217-218. (M) 2L72 4F RTA28NM 20030729001022003072900102NM 2003 7 29 USAA030097 120030605A5512 SKIN BOEING737 737401 1384701NM HORIZ STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US40316 23988 PIT - FOUND SKIN CRACKED 1.5 INCH, RIGHT HORIZONTAL STAB LOWER SKIN APPROX STATION 115. DAMAGE CUTOUT AND EXTERNAL SKIN DOUBLER INSTALLED PER SRM 55-10-01 FIG 204. (M) 2L72 4F RTA16WE 20030729001062003072900106NM 2003 7 29 USAASB03084 120030616A2120 ODOR BOEING737 7373B7 1384580NM COCKPIT DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19387US 22959 PIT - FLT 398 - MCI TO PIT, CREW REPORTED AN ELEC BURNING SMELL IN COCKPIT FROM CAPTAINS CENTER WINDSHIELD AIR VENT. CREW CYCLED EQUIPMENT COOLING FAN AND RECIRCULATION FAN WITH NO HELP. FLT LANDED IN PIT WITHOUT INCIDENT. MX PULLED OUT CAPTAINS SIDE OF INSTRUMENT PNL, NO SIGNS OF ARCING OR BURNING FOUND. NO ODORS DETECTED WITH WINDOW HEAT OPERATION. ACCOMPLISHED A VISUAL CHECK OF THE FWD AND AFT E/E BAY AND FOUND NO ODORS OR SIGNS OF BURNING. CHECKED GLARESHIELD, MASTER CAUTION AND WARNING AND SIX PACK CONNECTION LEFT SIDE ONLY, CHECKED GOOD. CHECKED AIR/GROUND MODE, NO ODOR FOUND. DROPPED CENTER SECTION OF OVERHEAD PANEL AND INSPECTED ALL AREAS, NO SIGNS OF ARCING OR ODOR FOUND. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030729001102003072900110EU 2003 7 29 2003F00483 120030515A7110 COWLING AIRBUS320 A320233 3930329EU NR 2 ENGINE PUNCTURED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK FOUND NR 2 ENGINE INTAKE UP WITH TWO PUNCTURES AT THE 7 AND 2 O'CLOCK POSITIONS. REPAIRED AIR INTAKE COWL IAW EM 71-11-11-300-015. (M) 2L72 4F RTA28NM 20030729001372003072900137NM 2003 7 29 UPS03440934 120030621A532065B1107935 SPLICE BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C FX - STA 255 S39L STRINGER SPLICE FOUND CRACKED. FX - STA 249 - STA 260 S39L STRINGER SPLICE REPLACED IAW SRM 51-10-01 P.8 2L74 4F A20WE 20030729001382003072900138NM 2003 7 29 UPS03440935 120030621A5320 FLOOR SUPPORT BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: C FX - STA 240 LBL 28, M/D FLOOR SUPPORT BEAM WEB FOUND CRACKED AS MARKED. FX - STA 240 M/D FLOOR SUPPORT BEAM WEB REPAIRED IAW SRM 53-10-07 FIG 11 JUST BETWEEN LBL 18 INCHES TO LBL 38 INCHES. 2L74 4F A20WE 20030729001412003072900141NE 2003 7 29 ABXA030234 220030613A7250 BLADE DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE LT ENGINE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23969AX515 47464 666710 TURBINE DAMAGE (T-1) ON NR 1 ENGINE. BLADE TIP MISSING. REPLACED THE NR 1 ENGINE IAW DC-9 MM. 2L72 4F4 F A6WE E2EA 20030729001472003072900147WP 2003 7 29 ABXA030288 120030721A3097 WIRE DOUG DC9 DC932 3022066WP COCKPIT DAMAGED A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23902AX 47426 DURING TAXI, WHEN FIRST OFFICER PERFORMED TAXI CHECK LIST, THERE WAS A POPPING SOUND AND SPARKS EMITTING FROM THE OVERHEAD ON THE CAPTAIN'S SIDE. REPLACED LEFT WINDSHIELD ANTI-ICE TEMPERATURE SENSOR WIRING IAW DC-9 MM 20-50-01-2. OPS CHECKED GOOD. 2L72 4F A6WE 20030730000032003073000003WP 2003 7 30 ABXA030200 120030415A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23843AX 46017 RIGHT AFT SERVICE DOOR UPPER AFT CORNER HAD CRACK INDICATION. CUT OUT CRACK IAW REA D853-46692MR. FABRICATED REPAIR IAW REA D853-46692MR. INSTALLED REPAIR IAW REA D853-46692MR, DC-8 SRM 51-1-21, 51-1-20D, AND 51-1-11. 2L74 4F 4A25 20030730000132003073000013WP 2003 7 30 ABXA030210 120030525A533059114065 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 FOSELAGE SKIN AT UPPER AFT MAIN ENTRY DOOR STOP CRACKED. REPAIRED AREA IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030730000242003073000024 2003 7 30 P5CA0300903 420030720A3441 INU BOEING747 747283B 1384867NM NR 2 MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23921FT 21575 NR 2 INU HAD RED WARNING LIGHT CODE 02-50-42 (NR 3 WAS ALREADY DEFERRED). RE-RACKED NR 2 INU, PERFORMED REALIGNMENT & RESET FAULT CODES AS PER WC M3400-002. 2L74 4F A20WE 20030730000292003073000029WP 2003 7 30 ABXA030265 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 187. CUT AND NEW SECTION SPLICED IN IAW ABX REA D852-46043MR. 2L74 4F 4A25 20030829000732003082900073NE 2003 8 29 NACA20030093 220030716A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 4 ENGINE FAILED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F861 861 44636 33553 NR 4 ENGINE WOULD NOT TAKE A LEAN. DOUBLE SHORTED SECONDARY. REPLACED NR 4 ENGINE NR 16 CYLINDER. 2L74 4R4 R 6A3 5E8 20030829000772003082900077NE 2003 8 29 NACA20030098 220030728A7322PR58E5 CARBURETOR DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 1 ENGINE FAULTY A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03993303200 3200 43576 P31669 NR 1 ENGINE LEANS ITSELF OUT DURING FLIGHT AND ALL CLIMB CONFIGURATIONS. REPLACED NR 1 ENGINE CARBURETOR. CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20030829000852003082900085NM 2003 8 29 P5CA0300907 120030810A361073836219 VALVE BOEING747 747283B 1384867NM NR 3 PYLON MALFUNCTIONED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23921FT 21575 NR 3 ENG PYLON VLV WOULD NOT OPEN. REMOVED AND REPLACED PYLON VLV IAW 36-11-00, LEAK CHECK OK. 2L74 4F A20WE 20030829000982003082900098NE 2003 8 29 2904071503 220030715A75329550164960 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE DEFECTIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP07894NA15 2904 9456 BLEED AIR VALVE FLAG NOT GOING OFF. 1G71 3U3 U H9EU E19EU 20030829001162003082900116NM 2003 8 29 SWAA031804 120030811A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR 8L AND STR 9L, BS'S 400, 827 AND 907. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030829001242003082900124NM 2003 8 29 SWAA031809 120030809A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C3 CHECK, FOUND AFT PRESS BULKHEAD CRACKED AT BS 1016, BETWEEN STR 4L AND STR 7L AT THE Y CHORD. REPAIRED AFT PRESS BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20030829001262003082900126 2003 8 29 SWAA031854 420030819A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030829002092003082900209NM 2003 8 29 USAA030134 120030725A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US52921 22956 PIT - FOUND SKIN CRACKED 1 INCH, LEFT AFT DOOR LOWER HINGE CUTOUT FORWARD LOWER CORNER. FABRICATED PARTS AND INSTALLED FILLRE AND DOUBLER PER SRM 53-60-01 AND SRM 51-40-03. (M) 2L72 4F RTA16WE 20030902000442003090200044SW 2003 9 2 ALG2003F00061 120030501A6340407362013101 PRESSURE SWITCH BELL BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUEL TRANSFER FAILED A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03627AL A500 53284 UPON TAXING OUT, THE TRANSMISSION CHIP LIGHT ILLUMINATED. THE PILOT RETURNED TO THE PAD AND LANDED AS SOON AS POSSIBLE. ON SHUT DOWN WHILE TURNING OFF FUEL BOOST PUMP CIRCUIT BREAKER SWITCHES, THE LEFT TRANSFER PUMP LIGHT DID NOT ILLUMINATE. THE MECHANIC REMOVED AND REPLACED LT FUEL TRANSFER PRESSURE SWITCH ALSO THE MECHANIC FOUND A SMALL METAL PARTICLE ON LOWER TRANS CHIP PLUG, HE CLEANED THE PLUG, REMOVED AND REPLACED TRANS OIL AND FILTER, COMPLIED WITH PENALTY RUN AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20030902001242003090200124NM 2003 9 2 AWXA200300778 120030607A5330654577070 SKIN BOEING737 7373Y0 1384671NM ZONE 200 - FUSELDENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK, DENTS FOUND ON CROWN SKIN FROM BS 540 TO BS 727, STRINGER 4L TO 4R. MAINTENANCE REMOVED AND REPLACED CROWN SKIN FROM BS 540 TO BS 727, STR 4 L/H TO STR 4 R/H PER B737-300 SRM 51-40-02 PG. 3 & 4. ADDITIONALLY AWA E.R. 03-5100-01187-JS1C WAS UTILIZED FOR REPAIR OF THE AFFECTED AREA. 2L72 4F RTA16WE 20030903000042003090300004WP 2003 9 3 DHL2003803008 120030710A2510 SEAT DOUG DC8 DC873 302199CWP COCKPIT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH 46123 F/O SEAT SLIDES FORE AND AFT EASILY BUT DIFFICULT TO LOCK IN PLACE. REPLACED F/O SEAT ASSY IAW MM 25-11-1. OPS CHKS GOOD 2L74 4F RT4A25 20030903000712003090300071EU 2003 9 3 197121 120030715A7603 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE COCKPIT ILLUMINATED A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17146SD 146SD ON 07/15/03, AT APPROX 1240 UTC, AIRCRAFT N146SD HAD TAKEN OFF ON FLT 4465 PIT-TOL. WHEN THE CREW RETRACTED THE LANDING GEAR, THE FLIGHT IDLE OPEN LIGHT ILLUMINATED. THE AIRCRAFT HAD RETURNED BACK TO PIT. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030903000822003090300082NE 2003 9 3 GJQ2003F00000 220030616A725030606901 BLADE AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE73140 29001NE ROTOR ASSY BROKEN B GJQRO OTHER O OTHER NRNOT REPORTED 1 NM0126WP 991 312 P115294 PILOT REPORTED ENGINE NR 2 N1 VIBRATION HEARD/ FELT VIBRATION BEGINNING DESCENT. VIBRATION INDICATOR (N1) AT 10 - 20 PERCENT THROUGHOUT DESCENT- AS HIGH AS 40 - 50 PERCENT ON OCCASION. INSPECTION REVEALED OUTER 1.2500 INCH LENGTH SEGMENT OF LPT3 TURBINE BLADE MISSING. REMOVED AND REPLACED ENGINE ASSEMBLY. REMOVED ENGINE. 2L73 4F4 F A46EU E1NM 20030903000842003090300084WP 2003 9 3 MEX2003271 120030707A7820 SUPPRESSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE EXHAUST CONE DAMAGED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23583MD 49659 AIRCRAFT AIR TURN BACK DUE TO ENGINE 2 FAILURE DURING INITIAL CLIMB, REACHING 660 DEGREE C OF EGT EMERGENCY PROCEDURE WAS PERFORMED. DURING REVISION THE EXHAUST CONE, SUPPRESSOR AND TURBINE FAN WITH DAMAGE. ENGINE NR 2 WAS REPLACED IAW MM, OPERATIONAL TEST WAS ACCOMPLISHED IAW MPCM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030903000932003090300093WP 2003 9 3 MEX2003227 120030616A243201128 RELAY DOUG DC9 DC982 3022082WP BATTERY CHARGER FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW231003X 48067 DURING TRANSIT CHECK WAS DETECTED CIRCUIT BREAKER BATTERY CHARGER WITHOUT INDICATION. THE BATTERY CHARGER, BATTERIES AND RELAY R2-56 WERE REPLACED, TESTS PERFORMED IAW 24-30-01, ALL CORRECT. 2L72 4F A6WE 20030903000942003090300094NM 2003 9 3 AALA20030598 120030525A2913PV32402F PUMP BOEING757 757223 1384957NM LT ENGINE LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21647AM 24605 DFW - FLT 2478 - EN ROUTE LAS-MIA, 1 HR AND 8 MIN INTO FLT LT HYD PUMP PRESSURE EICAS MESSAGE DISPLAYED. FOLLOWED QRH PROCEDURE AND SECURED LT ENGINE HYD PUMP. 40 MIN LATER, A BUZZING SCOURING SENSATION AND SOUND APPEARED. A MIN LATER RECEIVED A CALL FROM NR 1 FLT ATTENDANT ABOUT A SIMILAR SOUND FROM THE WING AREA. RAISED GEAR HANDLE TO CHK FOR POSSIBLE GEAR DOOR MISRIG,NO HELP. GEAR HANDLE PLACED TO OFF, 2 MINUTES LATER LT HYD FLUID STARTED TO DECREASE. WENT TO BELOW RF LEVEL AT .50 AND SECURED THE LT ELEC PUMP. FLUID LOSS CONTINUED TO 0.00 AND FLUCTUATED BETWEEN THERE AND .09. DIVERTED TO DFW, LANDED WITHOUT INCIDENT. REPLACED LT ENG DRIVE PUMP, LEAK AND OPS CHK GOOD. SYS GRND CHKED NORMAL. (M) 2L72 4F RTA2NM 20030903000952003090300095NM 2003 9 3 AALA20030647 120030608A2421GEN5103 IDG BOEING767 767323 1385205NM RT ENGINE FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21360AA 24041 RIGHT GENERATOR DRIVE INOPERATIVE, EICAS MESSAGE ACCOMPLISHED DISCONNECT PROCEDURE. SERVICED RIGHT IDG TO FULL RECONNECTED IDG RAN ENGINE FOR SEVERAL MIN, OPS CHECKS GOOD. DUE TO PREVIOUS REPORT THAT RT IDG FAILED DUE TO LOW OIL QTY. REPLACED THE IDG. REPLACED IDG PER MM. SERVICED WITH OIL. OPS CHECK AND LEAK CHECK DUE ON ENGINE RUN UP. OPS NORMAL AND LEAK CHECK OK. (M) 2L72 4F RTA1NM 20030903000992003090300099WP 2003 9 3 MEX2003286 120030713A2450B1740 CIRCUIT BREAKER DOUG DC9 DC983 3022083WP ELECTRICAL SYS FAILED A ASMFA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SW23838AM 49397 FLT 133 - TIJ-BJX - AIR TURNBACK AS A RESULT OF BREAKERS J23 FORWARD LT FUEL TANK PUMP, J21 AFT CENTER FUEL TANK PUMP, J8 AND J9 RECIRCULATION FAN WERE BOUNCED IN FLT. RESET THE BREAKERS, ALL CORRECT. LT AND RT AC BUS PHASES VOLTAGE WERE CHECKED, ALL CORRECT. ENGINES WERE TESTED WITH CROSSFEED FUEL SUPPLY, ALL CORRECT. AGAIN AIRCRAFT AIR TURN BACK AS A RESULT OF THE SAME REPORT. DURING REVISIT BREAKER B1-740 PHASE C OF RIGHT BAR A/C WAS WITH DAMAGE. THE BREAKER B1-740 AND FAN CABIN RECIRCULATION WERE REPLACED IAW MM 21-20-12, ALL TEST CORRECT. DURING PUSH BACK STARTER VALVE OF ENGINE NR 1 DID NOT OPEN. AFTER THIS CHECK LEFT ENGINE STARTING WAS CORRECT. AIRCRAFT WAS SENT FERRY TO MEX. (M) 2L72 4F RTA6WE 20030903001012003090300101WP 2003 9 3 MEX2003287 120030713A7920 TUBE DOUG DC9 DC987 3022087WP OIL SYSTEM CLOGGED A ASMFO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW23205AM 49405 FLT 440 - GDL-MTY - AIRCRAFT RETURN TO PLATFORM, DURING TAXIING THE CLOGGING LIGHT OIL ENGINE NR 2 ON. THE RESTRICTORS LP5 AND LP6 WERE CLEANED, BOTH ENDS LP5 AND LP6 TUBES WERE SERVICED WITH AIR PRESSURE TO REMOVE ANY CONTAMINATION AND THE DIFFERENTIAL PRESSURE SWITCH CONNECTOR PINS WERE VERIFIED FOR CONDITION. AFTER THIS CHECK RIGHT ENGNE STARTING WAS CORRECT IAW MM 71-00-01. (M) 2L72 4F RTA6WE 20030903001032003090300103NM 2003 9 3 USAABB03126 120030728A4920380029815 APU BOEING757 7572B7 1384964NM APU BAY MALFUNCTIONED A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19631AU 27809 PIT - FLT 44 - PILOT NOTED BURNED OIL SMELL FROM AIR CONDITIONING SYSTEM. MAINTENANCE RAN AND ISOLATED BOTH PACKS. A SLIGHT ODOR WAS NOTED. PACKS WERE RUN AT FULL HOT AND THE ODOR DISSIPATED. ON A FOLLOWING FLIGHT, THE ODOR RETURNED. MAINTENANCE REPLACED THE APU. (M) 2L72 4F RTA2NM 20030903001192003090300119WP 2003 9 3 GTIA030614 120030728A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND CABIN STRINGER 18R WEB CRACKED FS 1264. STOP DRILLED CRACK. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20030903001242003090300124NE 2003 9 3 2003F00534 220030803A7200 ENGINE AIRBUS320 A320233 3930329EU IAE V2524 V2524A5 NE NR 2 MAKING METAL A RJEFO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO23455TA 874 V10404 SAL - FLT 531 - FLIGHT CREW REPORTED ENGINE NR 2 N1 VIBRATION WHILE ARRIVING AT SAL STATION. TECHNICIANS PERFORMED INSPECTION OF ENGINE NR 2, AND FOUND SOME METALLIC DEBRIS AT THE EXHAUST AREA AND THE FAN BLADES COULD NOT BE TURNED BY HAND. ENGINE NR 2 ENGINE WAS REPLACED AND TESTED AS PER AMM 71-00-20. ALL RESULTS WERE SATISFACTORY AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F4 FRTA28NM E40NE 20030829001212003082900121NM 2003 8 29 SWAA031806 120030811A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030829001492003082900149NM 2003 8 29 SWAA031843 120030816A53306545767 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, ABOVE STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001572003082900157NM 2003 8 29 SWAA031821 120030813A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 1011, STRINGER 7L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030829001592003082900159NM 2003 8 29 SWAA031824 120030813A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS 500B AND BS 500C. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001652003082900165NM 2003 8 29 SWAA031823 120030813A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM. 2L72 4F RTA16WE 20030829001792003082900179NM 2003 8 29 SWAA031790 120030809A5753114A111012 WEB BOEING737 7377H4 1384404NM T/E FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED C3 CHECK, FOUND NR 4 L/E FLAP CRACKED AT OUTER WEB. REMOVED AND REPLACED NR 4 L/E FLAP PER MM. 2L72 4F RTA16WE 20030829001912003082900191WP 2003 8 29 GTIA030618 120030725A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND CABIN FLOOR PANEL STATION 579-617 DELAMINATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030902001382003090200138NE 2003 9 2 C1HA200385004 220030620A73207436024 FUEL CONTROL BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 1 ENGINE MALFUNCTIONED A C1HAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL15685CA 22492 NR 1 ENGINE NOT MAKING TAKE-OFF POWER. NR 1 2.07 EPR NR 2 AND NR 3 AT 2.15 EPR ALL OTHER INDICATIONS REFLECT SAME POWER DIFFERENCE. NR 1 SLIGHTLY LOWER N1, N2, EGT. ABORTED TAKEOFF IAW AOM -SMAC PROCEDURES 4.51.28 2L73 4F4 F A3WE E2EA 20030828000632003082800063NM 2003 8 28 P5CA0300921 120030819A5753 PANEL BOEING747 747200 1384847NM T/E FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 LEFT INBOARD MID FLAP DELAMINATION AT OUTBOARD UPPER FLT PANEL. CORRECTIVE ACTION TAKEN: DELAMINATION PANEL -REPAIRED- SRM 51-40-05. 2L74 4F RTA20WE 20030828000672003082800067NM 2003 8 28 DL76L030613 120030706A2530828450407 OVEN BOEING767 767332 1382001NM FWD GALLEY MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27177DN 25122 GALLEY FIRST CLASS CENTER OVEN OVERHEATS WHEN COOKING HAS A ELECTRICAL ODOR. OVEN INOP. PULLED AND SECURED C/B FWD TO MCO AND PLACARD IAW MEL 25-20-01I. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2L72 4F RTA1NM 20030828000982003082800098NM 2003 8 28 DL73S030630 120030712A2520 INSULATION BOEING737 737232 1384475NM PWA JT8 JT8D1 52044NE CARGO BAY OUT OF POSITION A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27329DL30782 23101 P50180 SMOKE SMELL IN AFT CABIN. FOUND INSULATION TOUCHING APU BLEED DUCT CAUSING SMELL. REPOSITIONED INSUL. FWD APU AIR TO MCO AND PLAC AS PRECAUTION. 2L72 4F4 FRTA16WE E2EA 20030828001442003082800144NE 2003 8 28 BJNA030801 220030813A7261 BEARING BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE NR 1 SCAV PUMP FAILED A EA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CRCRUISE 1 WP11344TM 23044 688356 AT FL 310, NR 1 ENGINE OIL PRESSURE NOTICED DROPPING, OIL QUANTITY WENT TO HALF GALLON, AND OIL TEMPERATURE ROSE TO THE YELLOW BAND. ENGINE WAS SHUTDOWN, LOW OIL PRESSURE LIGHT CAME ON AND THE ENGINE WIND-MILLED ABOUT 23 MINUTES AT 5-8 PSI OIL PRESSURE. DISASSEMBLY INSPECTION REVEALED THE DRIVE SHAFT BEARING IN THE 4 1/2 AND 5 SCAVENGE PUMP FAILED RESULTING IN OIL CONTAMINATION. (M) 2L72 4F4 FRTA16WE E2EA 20030828001552003082800155NM 2003 8 28 USAA030126 120030717A5330 SKIN BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 CLT - FOUND SKIN CORRODED 1 INCH BY 4 INCH AREA, AFT CARGO INT STRUCT STATION 1400 BETWEEN STRINGER 26L AND 27L. INSTALLED DOUBLER PER EA 87349. CORROSION LEVEL 1, TASK NR C53-155, 156, 163, 164, 165, 166-02. (M) 2L72 4F RTA2NM 20030829000532003082900053WP 2003 8 29 DHL2003873547 120030628A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 VERTICAL STABILIZER L/E EXTERNAL SKIN SHOWS INTERIM REPAIR AT ZFS 110.700. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AEA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17. CLEANED, TREATED AND PRIMED DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED DOUBLER ON L/E EXTERNAL SKIN AT ZFS.110.700 IAW SRM 55-2-1 FIG 4 PG 17, SRM 51-1-21 PG 1. FOR REMOVAL AND REINSTALLATION SEE JC BX3B55076. 2L74 4F RT4A25 20030829000672003082900067NM 2003 8 29 03FDEA01096 120030713A5101 STRUCTURE BOEING727 727200 138407ENM FUSELAGE NOISY A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25283FE 22350 PASSING 10K MSL, EXTREMELY LOUD SQUEAL APPEARED IN COCKPIT. PRESSURIZATION NORMAL. CLIMBED TO 14K AND SQUEAL REMAINED ON. NOISE WENT OUT PASSING 10K MSL IN DESCENT. SHUT OFF ALL RADIOS & COULD NOT ISOLATE PROBLEM. PRESSURIZED A/C TO 8.5 PSI NO SQUEAL OR HISS NOTED FROM ANYWHERE, IN REFERENCE TO B-727-200 M/M 05-51-101-2, ALSO COMPLIED WITH AIRFRAME DECAY CHECK IAW B-727-200 M/M 05-51-101-2 NO DEFECTS NOTED. INSPECTED AND CLEANED BOTH COCKPIT SLIDING WINDOWS AND FRAMES, NO DEFECTS NOTED. OPENED WINDOWS AND CHECKED SEALS FOR INTEGRITY, NO FAULTS FOUND. OPENED AVIONICS DOOR UNDER COCKPIT AND CHECKED, NO DEFECTS FOUND. PRESSURIZED A/C AGAIN TO 8 PSI, NO SQUEAL OR ANY ABNORMAL SOUNDS. 2L73 4F RTA3WE 20030829000812003082900081NM 2003 8 29 P5CA0300924 120030824A291060B0025435 HYDRAULIC LINE BOEING747 7472U3B 1384846NM HYD SYSTEM RUPTURED A P5CAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23922FT 22768 NR 1 HYDRAULIC SYS QUANITITY AND PRESSURE DROPPED TO ZERO AT STARTUP. SWAPPED PRESSURE LINE FROM NR 2 TO NR 1. CAPPED NR 2 ADP LINE FITTINGS. PERFORMED LEAK CHECKS, OPERATIONAL CHECK PER 29-11-00. SYS OPERATIONAL CHECK AND LEAK CHECK NORMAL. 2L74 4F RTA20WE 20030829000862003082900086NM 2003 8 29 P5CA0300908 120030807A2751 CONNECTOR BOEING747 747283B 1384867NM T/E FLAP DIRTY A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23921FT 21575 FLAP POS INDICATOR. CLEANED FLAP POS CONNECTOR, OPS CHECK FLAPS PER MM 27-51-00. CHECK OK. 2L74 4F A20WE 20030829001032003082900103EU 2003 8 29 2904062403 120030624A3340122024102 LIGHT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE EXTERIOR INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP074027Q4 2904 9456 PULSLITE INOP. 1G71 3U3 U H9EU E19EU 20030829001302003082900130NM 2003 8 29 SWAA031858 120030818A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 882 AT STR 25R AND BS 885 AT STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001332003082900133NM 2003 8 29 SWAA031861 120030819A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED (2 EA) STR 11R, BS'S 385 AND 425. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030829001422003082900142NM 2003 8 29 SWAA031836 120030815A339707912 WIRE BOEING737 7372H4 138448CNM CABIN EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS WIRES EXPOSED AT ROW'S NR 4 AND NR 8. INSTALLED EEPLS COVERS PER MM. 2L72 4F A16WE 20030829001502003082900150NM 2003 8 29 SWAA031844 120030816A33506104789 LIGHT BOEING737 7372H4 138448CNM EXTERIOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F A16WE 20030829001542003082900154 2003 8 29 SWAA031818 420030812A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030829001722003082900172NM 2003 8 29 SWAA031789 120030809A5753114A11011 SKIN BOEING737 7377H4 1384404NM T/E FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED C3 CHECK, FOUND NR 1 L/E FLAP CRACKED (2 EA) ON OUTER SKIN. REMOVED AND REPLACED NR 1 L/E FLAP PER MM. 2L72 4F RTA16WE 20030829001742003082900174NM 2003 8 29 SWAA031811 120030812A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030829001802003082900180NE 2003 8 29 SWAA031791 220030809A7200JT8D9A ENGINE BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE NR 1 FAILED A SWAAA UNSCHED LANDING EJYVIBRATION/BUFFET WARNING INDICATION ENGINE STOPPAGE CLCLIMB 1 SW29722WN 22698 687777 IN FLIGHT SHUTDOWN, AIR TURN BACK, NR 1 ENGINE FAILED ON CLIMB-OUT WITH STRONG VIBRATION AND ZERO OIL QUANTITY INDICATION. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 F A16WE E2EA 20030829001862003082900186NM 2003 8 29 SWAA031797 120030808A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (12 EA) AT STR 4R, BS'S 380, 410, 420, 430, 460, 500, 500B, 500C, 500C + 10, 500D, 520 AND 530. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001872003082900187NM 2003 8 29 SWAA031798 120030811A3397BR2013 WIRE BOEING737 7377H4 1384404NM CABIN EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 EEPLS WIRES EXPOSED AT ROW NR 23. SECURED WIRES PER MM. 2L72 4F RTA16WE 20030829001922003082900192WP 2003 8 29 2003F00524 120030725A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND CABIN FLOOR PANEL STATION 579-617 DELAMINATED. (M) 2L72 4F RTA6WE 20030829002032003082900203NM 2003 8 29 USAA030132 120030725A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US50148 23314 CLT - FOUND SKIN CRACKED 2 INCHES, S23L AND BS 727E. INSTALLED DOUBLER PER EA 94536. (M) 2L72 4F RTA16WE 20030829002052003082900205NM 2003 8 29 USAABB03068 120030506A2613 CONNECTOR BOEING767 7672B7 1385107NM LT WING DEFECTIVE A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19651US 24764 PHL - FLT 192 - EN ROUTE CLT-FRA, NEAR BOS, CREW RECEIVED THE EICAS MESSAGE 'L STRUT DCT LEAK' AND THE ASSOCIATED LIGHT. THE CREW CLOSED THE LEFT BLEED SWITCH WITH NO EFFECT ON THE PROBLEM. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE M691 DUCT LEAK AND WHEEL WELL OVERHEAT CARD. ENGINE WS RUN TO TAKEOFF POEWR WITH BLEEDS ON. NO FAULTS WERE NOTED. ON A SUBSEQUENT FLIGHT, THE EICAS MESSAGE REOCCURRED. MAINTENANCE REPLACED THE STRUT NACELLE CONNECTOR. (M) 2L72 4F RTA1NM 20030829002102003082900210 2003 8 29 USAABB03069 420030306A2565 LIGHT BOEING767 7672B7 1385107NM EVAC SLIDE INOPERATIVE A K NONE L NO TEST ININSP/MAINT 1 EA19655US 25257 PHL - DURING AN ANNUAL SLIDE DEPLOYMENT CHECK, THE R1 DOOR SLIDE WAS DEPLOYED AND INFLATED NORMALLY. HOWEVER, NONE OF THE LIGHTS OPERATED. THE SLIDE WAS REPLACED. THE SHOP CONCLUDED THAT THE SLIDE FUNCTIONED PROPERLY, BUT THAT THE BATTERY WAS DEAD. (M) 2L72 4F RTA1NM 20030902000342003090200034EU 2003 9 2 S9H2003F00000 120030427A2913704A336900004 BELT SNIAS 350 AS350BA 8680817EU HYD PUMP FAILED E S9HAO OTHER O OTHER NRNOT REPORTED 1 WP19356NT229 2280 AIRCRAFT EXPERIENCED HYD FAILURE SHORTLY AFTER DEPARTURE. PILOT RETURNED TO BASE AND LANDED. UPON INVESTIGATING THE CAUSE OF THE FAILURE, HYDRAULIC AND AIR CONDITIONING COMPRESSOR BELTS WERE DISCOVERED MISSING AND REMNANTS OF BOTH BELTS WERE FOUND ON THE TRANSMISSION DECK. UNABLE TO DETERMINE WHAT CAUSED BELTS TO FAIL. REPLACED BELT, INSPECTED COUPLING, PUMP. GROUND RUN SYSTEMS, CHECK GOOD 1G71 3U NCH9EU 20030902000352003090200035NE 2003 9 2 ARWA20030601 220030610A7200 ENGINE LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B40254555NE NR 3 VIBRATION A ARWAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SO19308GB540936105 193U1133 14637 ABORTED TAKE OFF AT 130 KTS 470,000 LBS DUE TO NR 3 ENGINE VIBRATION WARNING AT 2.8 UNITS. BRAKES OK, TIRES OK. RETURNED TO RAMP. LUBED FAN BLADES, PERFORMED INSPECTION IAW L1011 MM 71-91-00. ALL PARAMETTERS WITHIN LIMITS ON RUN UP NR 3 ENGINE. 2L73 4F4 F A23WE E12EU 20030902000452003090200045SW 2003 9 2 ALG2003F00062 120030501A62302060103605 LINK BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL MAIN ROTOR PC INOPERATIVE A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03351AL 51431 ON POST FLIGHT, THE PILOT FOUND MAIN ROTOR PC LINK SN TY3241 JAM NUT LOOSE, THE MECHANIC REMOVED AND REPLACED THE PC LINK AND HE COMPLIED WITH TRACK AND BALANE AND AUTO ROTATION CHECK. 1G71 3U3 U H2SW E1GL 20030828001392003082800139EA 2003 8 28 ASOA03353 120030803A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20030828001522003082800152 2003 8 28 USAASA03083 420030727A2565C37103101 CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE O OTHER ININSP/MAINT 1 EA19754UW 1328 BOS - FOUND AN INCORRECT RELEASE CABLE ON THE FORWARD LEFT ESCAPE SLIDE DURING INSPECTION. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. S/D - THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20030828001872003082800187 2003 8 28 CALA0300458 420030810A2565D31354418 SLIDE BOEING737 7373T0 1384582NM L2 DOOR UNSERVICEABLE A CALAK NONE O OTHER ININSP/MAINT 1 SW271430747930 23358 INSPECTION FOUND THE L-2 DOOR EMERGENCY SLIDE PRESSURE LOW. THE EMERGENCY ESCAPE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35. 2L72 4F RTA16WE 20030829000262003082900026NM 2003 8 29 CALA0300484 120030823A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A 1 INCH CRACK IN CEILING WEB OF LT WHEEL WELL AT BS 663, LBL 32. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, FIGURE 203. 2L72 4F RTA16WE 20030829000762003082900076WP 2003 8 29 NACA20030091 120030703A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CRACKED A NACAK NONE O OTHER ININSP/MAINT 1 AL0343872 44665 CRACK IN FUSELAGE SKIN AT LEFT HAND SIDE AT STATION 415 & 417. REPAIRED CRACK PER NAC DRAWING NAC2003-08 DATED 07/03/2003 AND FAA APPROVED 8110-3 DATED 07/03/2003. 2L74 4R 6A3 20030829001062003082900106NM 2003 8 29 SWAA031874 120030821A33506104789 BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED RON, FOUND BOTH AFT CABIN DOORS OVERHEAD EMERGENCY EXIT LIGHTS BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030829001132003082900113NM 2003 8 29 SWAA031801 120030811A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727D + 4 AT STR 19R AND BS 944 AT STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030902000582003090200058EU 2003 9 2 R7MR34649 120030205A5532350A1400201901 STRUCTURE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE VERTICAL STAB CRACKED E R7MRO OTHER O OTHER NRNOT REPORTED 1 NM07392LG 3252 RT CRACK, THREE WORKING RIVETS. SUSPECT IMPROPERLY SHIMMED AT FACTORY INSTALLATION. NO SHIMS FOUND AT REMOVAL OF FIN. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20030902000592003090200059EU 2003 9 2 R7MR34600 120030119A6210350A11001001 BLADE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR CRACKED E R7MRO OTHER O OTHER NRNOT REPORTED 1 NM073593X6510 1539 1081 SKIN DELAMINATION AND CRACK, 3 FT FROM ROOT (MAY QUALIFY FOR BLADE EXCHANGE). REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20030902001002003090200100CE 2003 9 2 CJP2003F00003 120030619A3241393091 ANTI-SKID SYS LEAR 25 25D 5170514CE RT GEAR WELL OUT OF TOLERANCEE CJPAO OTHER O OTHER NRNOT REPORTED 1 NM03727CS 243 25D313 FLIGHT CREW REPORTED DISPROPORTIONED BRAKE (EFFECTIVENESS) ON LANDING, AT LOW SPEED. REMOVED AND REPLACED ANTI-SKID PRESSURE CONTROL VALVE WITH SERVICEABLE VALVE. TEST TAXI WAS PERFORMED BY SAME FLIGHT CREW AND BRAKES OPERATION WAS NORMAL. 2L72 4J A10CE 20030902001102003090200110EU 2003 9 2 CX7A194J0350 120030701A33506510348 SIGN SAAB SF340 340B 7860101EU EMERGENCY LIGHT ODOR A CX7AO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL03311CE 340B214 F/A REPORTED ELECTRICAL SMOKE ODOR FROM EMERGENCY EXIT SIGN IN ROW 8C 2L72 4T RTA52EU 20030902001132003090200113NM 2003 9 2 P5CA0300893 120030706A2700 AILERON BOEING747 74746NF 13848BTNM MALFUNCTIONED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23451PA 30809 AFTER ENG START CREW REPORTED AILERON INDICATION PROBLEMS DURING FLT CNTRL CHECK. CONFIRMED W/ VISUAL OPERATION THAT THE CONTROL SURFACES LOOKED NORMAL, DEFERRED IAW MEL 27-18-1 2L74 4F RTA20WE 20030902001152003090200115NM 2003 9 2 XNOA01136 120030701A3210 ACCESSORY UNIT BOEING727 727227 1384078NM MLG MALFUNCTIONED A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23793A 20774 AT 1.4 EPR STALL WARNING ACTIVATED CONTINUOUSLY. BOTH WINDSHEAR CAUTION LIGHTS ILLUMINATED. OIL COOLER CSD WOULD NOT STAY IN GRD OFF MODE; WENT BACK TO NORMAL POSITION. REJECTED TAKEOFF. WENT TO RAMP. R&R'D LANDING GEAR ACCESSORY UNIT. ALL SYSTEMS. OPS CHECK GOOD IAW B727 32-09-121. NO DEFECTS NOTED. 2L73 4F A3WE 20030902001292003090200129NM 2003 9 2 AWXA200300783 120030607A33971703661 SOCKET BOEING737 7373Y0 1384671NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 INSPECTION, MAINTENANCE DISCOVERED NUMEROUS SEAT MOUNTED EPLS CONNECTORS AND SPLICES DAMAGED. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EPLS HARNESS IAW BSWPM 20-42-01 PAGES 1-4. OPERATIONAL CHECK OF THE SYSTEM WAS GOOD IAW AWA TASKCARD NR A1C33006. 2L72 4F RTA16WE 20030902001362003090200136NM 2003 9 2 03FDEA00940 120030618A5753ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LT-O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT POINT BUSHING FOUND LOOSE. CORRECTIVE ACTION: SNRM N0712 - LHW- O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT POINT BUSHING REPLACED AS PER FEDEX EA 1-5750-69372, TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030902001452003090200145WP 2003 9 2 0301259884 120030707A324495608597 TIRE DOUG DC9 DC951 3022051WP MLG SEPARATED A NWAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL01677MC 47756 DURING TAKEOFF, THE NR 4 TIRE EXPERIENCED COMPLETE TREAD SEPARATION. DEBRIS FROM THIS FAILED TIRE DAMAGED THE NR 2 ENGINE CAUSING A LOSS OF OIL PRESSURE REQUIRING POWER REDUCTION TO IDLE BY FLIGHT CREW. FLIGHT RETURNED TO MCI AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NBR 3 AND NBR 4 TIRE AND NBR 2 ENGINE. 2L72 4F RTA6WE 20030902001472003090200147EA 2003 9 2 SWIA200312159 120030701A3241428853 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ANTI-SKID SYS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07426SW6832 6832 7468 INFLIGHT (ANTISKID INBD ANTISKID OUTBOARD) YELLOW MESSAGES ILLUMINATED - QRH COMPLIED WITH - MESSAGES WOULD NOT EXTINGUISH. BOTH LEFT SIDE MAIN LANDING GEAR TIRES FAILED ON LANDING. FOUND LEFT AND RIGHT ANTISKID CB'S POPPED. RESET CB'S AS REQUIRED IAW MM 32-44-00. OUTBOARD CHECKS GOOD, IB CHECKS BAD. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IAW 32-44-06. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030902001752003090200175WP 2003 9 2 NACA20030092 120030703A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CRACKED A NACAK NONE O OTHER ININSP/MAINT 1 AL0343872 44665 CRACK IN FUSELAGE SKIN ON RIGHT HAND SIDE AT STATION 415 & 417. REPAIRED CRACK PER NAC DRAWING NAC2003-07, DATED 07/03/2003 AND FAA APPROVED 8110-3 DATED 07/03/2003. 2L74 4R 6A3 20030902001802003090200180WP 2003 9 2 03FDEA01086 120030710A5350 RIB DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 TAILCONE , LT SIDE- INTERNAL RIB IS CRACKED, FWD END AT NR 2 RIB: 24 INCHES BELOW MAINT PLATFORM. ACCOMPLISHED AT MAE UNDER W/O NO.13414. FABRICATED REPAIR AND INSTALLED REPAIR IAW/SRM 53-00-01 FIG 10 REPAIR PARTS FABRICATED ON MAE TRAVELLER NO. T2/347292 2L73 4F A22WE 20030903000742003090300074WP 2003 9 3 ARWA20030707 120030714A3260 PROXIMITY SWITCH DOUG DC8 DC862F 3021972WP MLG DIRTY A ARWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19791AL 46150 GEAR NOT LATCHED LIGHT CAME ON IN FLIGHT AND STAYED ON ALL THE TIME. LUBED UPLATCHED MAIN & NOSE GEAR MECHANISM IAW MM 12-81-1; CLEANED ALL PROXIMITY SWITCHES IAW MM 20-50-1. OPERATIONAL CHECK FOUND NORMAL IAW MM 32-30-0. SEVERAL GEAR SWING PERFORMED. 2L74 4F 4A25 20030903001402003090300140NE 2003 9 3 AWXA20030021A 220030227A7250 TURBINE BLADES BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE ENGINE FRACTURED A AWXAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 WP28183AW 22650 P708359B SLC - ABORTED TAKEOFF - FLT 0220 - ON TAKEOFF ROLL AT SLC EN ROUTE FOR PHX FELT STRONG VIBRATION FROM R/H SIDE OF AIRCRAFT AND IN R/H THRUST LEVER. ALL ENGINE INDICATIONS WERE NORMAL AT THIS POINT WITH NO WARNING INDICATIONS. REJECTED TAKEOFF AT 130 KTS INDICATED AIRSPEED. AS POWER WAS PULLED TO IDLE THE NO. 2 ENGINE DECELERATED FASTER THAN NO. 1. SHUTDOWN NO.2 ENGINE AND TAXIED TO GATE USING NO. 1 ENGINE. MAINTENANCE FOUND DAMAGE TO THE NO. 2 ENGINE LOW PRESSURE TURBINE SECTION. **SUPP** REMOVED AND REPLACED NO. 2 ENGINE IAW T/C R5M71003, AND R5M78002. STATIC RIG ACCOMPLISHED IAW T/C F5M76001, AND TRIM RUN PERFORMED IAW T/C F5M71002. **SUPP** TEARDOWN FINDINGS OF ENGINE S/N P708359 ATTRIBUTE ENGINE FAILURE TO 2L72 4F4 FRTA16WE E2EA 20030903001482003090300148NM 2003 9 3 VNAA0308008 120030813A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07328JS 3030 THE CREW REPORTED THAT THE LAV SMOKE DETECTOR WAS INOP. MAINTENANCE THEN DEFERRED THE LAV SMOKE DETECTOR, 26-3 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030903001522003090300152NM 2003 9 3 VNAA0308012 120030820A3240AC69965 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BRAKE SYS FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07431JS152006203 3028 EN ROUTE, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR LOW CAS MESSAGE. UPON ARRIVAL, MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030903001562003090300156NE 2003 9 3 183921 220030726A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NACELLE OVERTORQUED A UHLAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL17123XS N123XS DURING TAKEOFF ROLL FLT 4515 PIT TO TTN EXPERIENCED A MAX TRQ OF 60 PERCENT NG. CAPTIAN ABORTED TAKEOFF AND RETURNED TO GATE. 2L72 4T4 TRTA52EU E8NE6 20030903001572003090300157NM 2003 9 3 XNOA01140 120030724A2933 PIN BOEING727 727227 1384078NM HYD INDICATOR BACKED OUT A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23793A 20774 HYD FLUID QTY INDICATOR CIRCUIT BREAKER TRIPPED. RETURNED TO RAMP. FOUND PUSHBACK PIN ON A SYS HYD TANK QUANTITY IND. RESEATED PUSHBACK PIN PER B727 MM 20-11-80. 2L73 4F A3WE 20030903001592003090300159EU 2003 9 3 175051 120030722A7600 WARNING SYSTEM SAAB SF340 SF340A 7850100EU COCKPIT ACTIVATED A UHLAD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 FLIGHT 4558 FROM FWA TO PIT, SHORTLY AFTER TAKEOFF AIRCREW NOTICED THAT THE FLIGHT IDLE STOP OPEN LIGHT WAS ILLUMINATED. AIRCRAFT RETURNED TO FWA. 2L72 4T RTA52EU 20030903001622003090300162CE 2003 9 3 ACE071903 120030719A2612 FIRE LOOP BEECH 1900 1900C 1154161CE RT ENGINE DEFECTIVE E YADAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 AL03112AX UC45 RIGHT ENGINE FIRE LIGHT CAME ON IN FLIGHT REQUIRING ENGINE SHUTDOWN. PILOT REPORTED THAT WARNING DISCONTINUED 15 MINUETS AFTER ENGINE SHUTDOWN. SYSTEM OPS CHECKED GOOD ON GROUND AFTER LANDING. MAINTENANCE INSPECTED WARNING SYSTEM AND REPLACED FORWARD LOOP DUE TO A TIGHT BEND IN THE LOOP, REPLACED THE AFT LOOP DUE LOW RESISTANCE AND REPAIRED A CHAFE AREA ON THE WIRING HARNESS. 2L72 4T RTA24CE 20030903001632003090300163EA 2003 9 3 SWIA200312219 120030726A3244 TIRE CNDAIRCL600 CL6002B19 1900309EA RT MLG SEPARATED A SWIAO OTHER S AFFECT SYSTEMS LDLANDING 1 NM07431SW 7536 RIGHT INBOARD FLAP DAMAGED FROM THE NR 3 MLG TIRE TREAD CAME APART. REMOVED AND REPLACED RIGHT INBOARD FLAP WITH SERVICEABLE FLAP IAW CRJ MM 27-54-01. REMOVED AND REPLACED NR 3 WHEEL ASSY IAW CRJ MM 32-41-01. TIRE PRESSURE GOOD. S/N OFF: 4004. 2L72 4F RTA21EA 20030903001642003090300164EU 2003 9 3 DHL2003364011 120030715A3350 LIGHT AIRBUS300 A300B4203 3930306EU CABIN OUT OF POSITION A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01364DH 141 EXIT LIGHT FELL ON FLOOR. REPLACED IAW 33-51-13. 2L72 4F RTA35EU 20030903001672003090300167WP 2003 9 3 DHL2003873606 120030705A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 A-BELLY DOOR INTERIM REPAIR ON LOWER OUTER SKIN FS 280.000 - 340.000. PERFORMED MAJOR IAW EODHL-030633, ED-3459. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN SEGMENT IAW EODHL-030633, ED-3459. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED NEW SKIN SEGMENT AND DOUBLER SPLICE IAW EODHL-030633, ED-3459. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN SEGMENT AND DOUBLER SPLICE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED SKIN SEGMENT AND DOUBLER SPLICE WITH NEW FASTENERS IAW EODHL-030633, ED-3459, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030903001862003090300186WP 2003 9 3 AALA20030731 120030709A2120 BOOT DOUG DC9 DC983 3022083WP A/C BAY OUT OF POSITION A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21961TW 53611 LAS - FLT 1306 - EN ROUTE LAS-STL, AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON. DECLARED EMERGENCY AND RETURNED TO LAS WITHOUT FURTHER INCIDENT. REINSTALLED DISLOCATED BOOT AND CLAMP IN BETWEEN AIR CYCLE MACHINE AND HEAT EXCHANGER ON LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030903001902003090300190NM 2003 9 3 AALA20030806 120030726A2520M18101001002 SEAT BOEING777 777223 1385213NM CABIN FAULTY A AALAK NONE O OTHER ININSP/MAINT 1 SW21792AN 30253 DFW - REPLACED SEAT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030903002152003090300215NM 2003 9 3 QXEA200300925 120030729A5210 STOP DHAV DHC8 DHC8202 2809007NM DOOR DEFECTIVE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09346PH 477 SEA- ON FLIGHT 2116 UNABLE TO OPEN DOOR. DOOR HANDLE JAMMED BY DETENT PANEL. REMOVED AND REPLACED STOP UNDER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030902001902003090200190NM 2003 9 2 03FDEA00992 120030626A5510ALC8100 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STABILIZER, LT UPPER AFT PLANK BARREL NUT BORE NR 34L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LT HOR STAB UPPER AFT PLANK BARREL NUT NR 34L BORE REPAIR CARRIED OUT IAW EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030902001942003090200194SO 2003 9 2 GLBA2003105 120030711A315012034428505 PANEL EMB 120 EMB120ER 3260203SO STALL WARNING INOPERATIVE A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM0396ZK 7244 120096 STALL WARNING SOUNDS CONSTANTLY, REMOVED AND REPLACED STALL WARNING PANEL. 2L72 4T RTA31SO 20030903000012003090300001NM 2003 9 3 DHL2003748009 120030709A26121014A POWER SUPPLY BOEING727 727225 1384077NM APU FIRE DETECT MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01748DH 22440 APU FIRE DETECTION TEST WILL NOT TEST. "DEFERRED APU PER MEL 49-1; CAT. "C"; ASSIGNED DMI 13486; PLACARD INSTALLED. TROUBLESHOOTING SYSTEM, CHECKED TEST SWITCH FOR CONTINUITY BETWEEN PINS 2 & 3; CHECKED GOOD. VERIFIED THAT SENSOR/ RESPONDER IS HEATING UP WITH TEST SWITCH DEPRESSED, HOT TO THE TOUCH. RESET ALL CIRCUIT BREAKERS IN SYSTEM. SWAPPED FIRE TEST RELAYS WITH KNOWN GOOD ONE; NO HELP RETURNED TO ORIGIN. CLEANED CONNECTOR TO FLASHER FIRE BELL RELAY. CHECKED FOR CONTINUITY AT PINS 4 & 6 ON FIRE DETECTION POWER UNIT; NO CONTINUITY AT PINS 4 & 6 ON POWER UNIT; SUSPECT BAD POWER UNIT ORDERED ON REQ. 300082358; P/N 1014A FIRE/OVERHEAT POWER UNIT. ALSO GOING TO ORDER APU ALARM CUTOUT RELAY AS PRECAUTIONARY.) 2L73 4F A3WE 20030903000062003090300006WP 2003 9 3 DHL2003803010 120030712A2510 SEAT DOUG DC8 DC873 302199CWP COCKPIT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH 46123 F/O SEAT DOES NOT ADJUST VERTICALLY WITH LEVER. REPLACED F/O SEAT ASSY IAW MM 25-11-0. OPS CHECK GOOD. 2L74 4F RT4A25 20030903000232003090300023 2003 9 3 MEX2003268 420030507A2312107C80021 MICROPHONE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE VHF COMM SYS FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23216AM33245 49586 AIRCRAFT RETURNED TO PLATFORM, BOTH VHF COM WERE OUT OF SERVICE. MICROPHONES WERE SWAPPED AND THEY WERE OPERATING IN A CORRECT WAY. DURING OVERNIGHT SERVICE THE MICROPHONE OF OBSERVERS SIDE WAS REPLACED IAW MM 23-50-00, ALL TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20030903000252003090300025 2003 9 3 MEX2003261 420030703A3460 FMC BOEING757 7572Q8 1384972NM COCKPIT INOPERATIVE W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23301AM 30045 DURING TRANSIT CHECK WAS DETECTED BOTH INTERNAL SYSTEM OUT SERVICE IN ANY SELECTION. THE BOTH FMC COMPUTER SYSTEM WERE DEFERRED IAW MEL. FMC COMPUTERS WERE REPROGRAMMED IAW MM 34-21-00, ALL TESTS CORRECT. 2L72 4F RTA2NM 20030903000272003090300027WP 2003 9 3 MEX2003258 120030630A2897 WIRE DOUG DC9 DC987 3022087WP FUEL PANEL FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23803ML32 32 49726 DURING FUELING SERVICE, WAS DETECTED THE REFUELING CONTROL PANEL OUT OF SERVICE. DURING REVISION WAS DETECTED THE BREAKER E-5 OF PANEL P-11 DAMAGED. THE REFUELING CONTROL PANEL WAS DEFERRED IAW MEL 28-41-6. THE REFUELING CONTROL PANEL WIRING WAS REPAIRED IAW WDM 28-21-22 AND FUEL QUANTITY INDICATOR WAS REPLACED IAW MM 28-41-06, ALL CORRECT. 2L72 4F RTA6WE 20030828001732003082800173NM 2003 8 28 SWAA031868 120030819A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 500C AT STR 10R, BS 500C AT STR 5L, BS 500D AT STR 8L AND BS 727B AT STR 7R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030828001922003082800192NM 2003 8 28 CALA0300448 120030805A5730 PANEL BOEING757 757224 1384958NM LT WING DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712116 27558 INSPECTION FOUND LT WING L/E PANEL DELAMINATED ON UPPER SURFACE AT FSS 410. THE AREA WAS REPAIRED IAW EA 5731-01010, REV D, OP 4. 2L72 4F RTA2NM 20030829000132003082900013SO 2003 8 29 MG3478109 120030618A32421159SCL5043 BRAKE ASSY GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE MLG BROKEN B BTVRK NONE O OTHER ININSP/MAINT 1 GL23910DC2717 544 DURING INSPECTION OF THE MAIN LANDING GEAR BRAKES, DRIVE ROTOR CLIPS FOUND THE NR 3 AND NR 4 BRAKE ASSEMBLIES TO HAVE FOUR CLIPS EACH BROKEN OFF. REPLACED BOTH BRAKE ASSEMBLIES WITH OVERHAULED UNITS. THIS IS A KNOWN CONDITION AND TROUBLESHOOTING IS ON GOING. 2L72 4F4 FRTA12EA E00057EN 20030829000652003082900065CE 2003 8 29 EPD2003F00000 120030616A33106854705 LIGHT LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP COCKPIT SHORTED B EPDRO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM13354EF 35A378 ON 6/16/03, IN FLIGHT, CREW REPORTED SMOKE IN FLIGHT DECK. FOUND FLUORESCENT TUBE UNDER GLARESHIELD, INOPERATIVE (SHORTED) AND INSULATION BURNED. AIRCRAFT WAS RETURNED TO BASE WHERE LAMP WAS REPLACED. 2L72 4F4 F A10CE E6WE 20030829000952003082900095NM 2003 8 29 S2YA03009 120030307A2460230GC02Y04 CONTROL PANEL DORNERDO32 DO328300 NM COCKPIT FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13355SK 2399 3124 DURING FLIGHT 2074, THE LEFT DC GENERATOR FELL OFF LINE. THE CREW MADE AN AIR TURNBACK, MECHANIC SWAPPED THE GENERATORS AND OPS CHECK THE SYSTEM. NO DEFECTS NOTED MECHANIC RETURNED THE AIRCRAFT TO SERVICE. ON 03/09/03 THE LEFT DC GENERATOR FAILED IN FLIGHT. MECHANIC REPLACED THE DC POWER CONTROL UNIT (1VE PANEL) AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DEFECTS. 2H72 4T RTA55NM 20030829001012003082900101 2003 8 29 31440227031 420030227A34215040017901 GYRO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP075226R1864 3144 22090 GYRO INOP. 1G71 3U3 U H9EU E00054EN 20030829001192003082900119NM 2003 8 29 SWAA031805B 120030811A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030829002132003082900213EA 2003 8 29 ASOA03344 120030728A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11828AS 7213 DURING A C-CHECK IN MCN, THE FLOORBEAMS AT FS 349 ON THE RIGHT INBOARD AND OUTBOARD SIDES WRE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOORBEAMS AT FS 349 ON THE RIGHT INBOARD AND OUTBOARD SIDES IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20030730000442003073000044WP 2003 7 30 ABXA030254 120030316A5200 STRUCTURE DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CENTER LATCH HOOK MOUNT HOLE AT STA 203.5 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR. 2L74 4F 4A25 20030730000472003073000047WP 2003 7 30 ABXA030250 120030305A5730 SKIN DOUG DC8 DC863F 302198FWP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 HOLE NR 2 ON RIGHT WING AT XFS 515, SHOWED CRACK INDICATION IN SKIN DURING INSPECTION. REPAIRED AREA IAW ABX REA D857-46040MR. 2L74 4F 4A25 20030730000522003073000052WP 2003 7 30 ABXA030266 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CUT AND SPLICE MAIN CARGO DOOR AT FRAME STA 213.5. CUT AND NEW SECTION SPLICED IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-8, 51-1-20D, AND 51-3-0. 2L74 4F 4A25 20030730000532003073000053WP 2003 7 30 ABXA030295 120030624A522059131951 PAN DOUG DC9 DC932 3022066WP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 LEFT AFT OVERWING EMERGENCY EXIT DOOR PAN WAS CRACKED AT 2ND FITTING FROM BOTTOM, AFT EDGE. REPAIRED FITTING IAW DC-9 SRM. 2L72 4F A6WE 20030730000602003073000060WP 2003 7 30 ABXA030291 120030704A57403923255501 SUPPORT FITTING DOUG DC9 DC941 302207NWP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 LEFT INBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1, 51-30-2, AND 51-30-5. 2L72 4F A6WE 20030728000152003072800015NM 2003 7 28 SWAA031599 120030718A531069353656 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND STR 14L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030728000352003072800035NM 2003 7 28 SWAA031600 120030718A53106546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 827, WL 148 AT LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030728000372003072800037NM 2003 7 28 SWAA031579 120030717A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 697 AT BS 717. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728000482003072800048NM 2003 7 28 SWAA031605 120030720A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030814001572003081400157WP 2003 8 14 GTIA030575 120030702A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND FORWARD CABIN STATION 236 RIGHT SIDE L18R HAS CORROSION ON SUB FLOOR WEB. REMOVED DAMAGED SECTION. FABRICATED WEB SECTION AND SPLICE. INSTALLED WEB AND SPLICE. (M) 2L72 4F A6WE 20030814001642003081400164WP 2003 8 14 GTIA030579 120030701A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND MAIN CABIN STATION 256 TO STATION 313 RBL 22 TO RBL 45 FLOORBOARD HAS CORROSION AND PUNCTURE HOLES AT BACKSIDE R5. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030815000012003081500001WP 2003 8 15 GTIA030571 120030630A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND CORROSION AT R1 DOOR AFT LOWER CORNER AT FS 195-210 18R. REMOVED CORRODED CUSP AT R1 DOOR STATION 164 TO FS 230. FABRICATED NEW CUSP. FABRICATED CUSP SPLICE. INSTALLED NEW CUSP AND SPLICE. (M) 2L72 4F A6WE 20030815000172003081500017SW 2003 8 15 HEEA088553 120030802A7722212075067113 INDICATOR BELL 412 412 1182202SW ITT STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 STICKS AT ZERO DURING START. SHOP REPAIR. 1G72 4U H4SW 20030815000262003081500026SW 2003 8 15 HEEA088539 120030805A6230406010410121 RING BELL 407 407 1182206SW SWASHPLATE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 INNER RING OF SWASHPLATE DAMAGED. 1G71 3U O H2SW 20030815000272003081500027SW 2003 8 15 HEEA088540 120030805A1430HL36PB612 FASTENER BELL 407 407 1182206SW MISMARKED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 PAPERWORK SHOWS CORRECT P/N, PART IS NOT CORRECT. 1G71 3U O H2SW 20030815000292003081500029SW 2003 8 15 HEEA088546 120030719A2510206072219101 SEAT BELL 206 206L3 1182108SW COCKPIT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 SEAT BOTTOM TORN. IN REPAIR. 1G71 3U H2SW 20030903002162003090300216NM 2003 9 3 QXEA200300927 120030730A36103045593 VALVE DHAV DHC8 DHC8202 2809007NM BLEED AIR SYS MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09368PH 512 BOI- ON FLIGHT 2196 AFTER ENGINE START AND THE BLEEDS TURNED ON, AIRCRAFT FILLED WITH SMOKE. REMOVED AND REPLACED NR 2 ENGINE P2.5/P3 SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903002182003090300218NM 2003 9 3 QXEA200300988 120030810A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 4 SEAT TRACK HAS CORROSION ALONG RIVETS FOR ALUMINUM TRAY AT STATIONS X215.500 TO X222.00. REPAIRED IAW DHC-8 RD 8-55-1002, SRM 53-40-11, 51-20-16 AND 51-20-36. 2H72 4T RTA13NM 20030903002202003090300220NM 2003 9 3 QXEA200300991 120030811A5230 DOOR FRAME DHAV DHC8 DHC8202 2809007NM CARGO DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- CARGO DOOR EDGE FRAME FOR TOP OF DOOR AT FORWARD CORNER IS DAMAGED ON INSIDE RADIUS. REPAIRED IAW DHC-8 SRM 51-20-11, 51-00-04, 51-20-36, AND 51-20-16. 2H72 4T RTA13NM 20030903002302003090300230EA 2003 9 3 03224633 120030812A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27633BR 7274 DURING MAINTENANCE INSPECTION THE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030902001042003090200104NM 2003 9 2 ANCF200300019 120030628A3250S4916689AS04012 CABLE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE NLG STEERING BROKEN W ANCFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO23632CT 49632 WHILE TURNING TO POSITION ON THE RUNWAY FOR TAKE OFF,THE NOSE WHEEL STEERING SYSTEM BROKE DOWN. LOOSING ALL CONTROL. C/A: ACCOMPLISHED REPLACE OF THE SYSTEM DIRECTIONAL CABLES,WAS VERIFICATED RIGGING OF SYSTEM IAW AMM 32-50-00 PAG 201-205 TEST ON GROUND SATISFACTORY AND LEFT OUTBOARD REFLECTOR WAS REPLACED WATER AMM 32-20-01 2L72 4F4 FRT E9NE 20030902001162003090200116EU 2003 9 2 XNOA01137 120030701A2910 B-NUT AIRBUS300 A300B4203 3930306EU MLG DRG BRCE CYLLOOSE A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23473AS 203 LOST GREEN HYD FLUID AND PRESSURE. MOTOR DUMPED FUEL TO MAX LANDING AND RETURNED TO SJU. ACTION TAKEN: TIGHTENED LOOSE AND LEAKING B-NUT ON LEFT MLG DRAG BRACE CYLINDER. LEAK CHECK GOOD AND SERVICED GREEN HYD IAW A300 MM 12-12-29. 2L72 4F RTA35EU 20030902001172003090200117EU 2003 9 2 XNOA01138 120030707A3150 WARNING LIGHT AIRBUS300 A300B4203 3930306EU CONFIGURATION ILLUMINATED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23371PC 157 CONFIGURATION LIGHT ON FSPI ON. CLEANED AND INSPECTED PINS, RESECURED. OPS CHECK NORMAL IAW MM 27-84-00. 2L72 4F RTA35EU 20030903000122003090300012CE 2003 9 3 071403 120030710A32332327100VAR ACTUATOR LEAR 25 25D 5170514CE MLG INOPERATIVE E ESUAO OTHER J WARNING INDICATION LDLANDING 1 CE039QM 286 AIRCRAFT UPON LANDING DID NOT HAVE A LEFT GREEN LIGHT DOWN AND LOCKED. AFTER THE AIRCRAFT LANDED, MAINTENANCE DETERMINED THAT THE LEFT ACTUATOR WAS THE PROBLEM, THE PART WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4J A10CE 20030903000192003090300019NM 2003 9 3 03FDEA01093 120030711A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 N00177 LIGHTNING STRIKE BS 350 BETWEEN STR 2L AND STR 3L. FOUND LIGHTNING STRIKE DAMAGE TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW SRM 53-30-3 AT BS 350 BETWEEN STR 2L AND 3L. 2L73 4F4 FRTA3WE E2EA 20030903000792003090300079EA 2003 9 3 SWIA200312178 120030710A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07426SW 7468 LT FLIGHT SPOILER INDICATES FAULT AFTER PERFORMING THE FIRST FLIGHT OF THE DAY TEST. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILER PCU. OPS AND LEAK CHECKS GOOD IAW MM 27-62-01. S/N OFF: 3957 2L72 4F RTA21EA 20030903001042003090300104 2003 9 3 USAABB03114 420030714A2565D30656126 SLIDE BOEING757 7572B7 1384964NM L4 DOOR MALFUNCTIONED A K NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 MBJ - CLEANER INADVERTENTLY DEPLOYED THE L4 DOOR SLIDE. THE SLIDE PARTIALLY DEPLOYED. MAINTENANCE REPLACED THE SLIDE. THE SLIDE SHOP VERIFIED THE SATISFACTORY CONDITON OF THE SLIDE. IT IS BELIEVED THAT THE DEPLOYMENT SEQUENCE WAS INHIBITED BY THE INITIATOR, THEREBY PREVENTING THE COMPLET DEPLOYMENT OF THE SLIDE. (M) 2L72 4F RTA2NM 20030903001232003090300123SO 2003 9 3 2003F00530 120030602A27101159CSM5510627 BALANCE WEIGHT GULSTMGV GULFSTREAMGV3980116SO LT AILERON DETACHED A KKYAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NE0350KC 659 ON DESCENT AT YIP, WITH TWO PAX ONBOARD, PILOTS EXPERIENCED DIFFICULTY IN TURNING A/C LATERALLY TO THE RT. PILOTS WERE ABLE TO CONTROL A/C AND MAKE A NORMAL LANDING. THE LOCAL AREA TECH REP FOR THE AIRFRAME MANUFACTURER WAS ABLE TO VERIFY THAT THE AILERON'S MASS BALANCE WEIGHT HAD BECOME UNATTACHED, LOSS OF ATTACHING HARDWARE. MX WAS DISPATCHED TO MAKE REPAIRS AS WELL AS THE OPERATORS MECHANIC TO OVERSEE THE REPAIRS. THE A/C'S FLT CONTROLS WERE FURTHER INSP, AND NO ABNOMALIES WERE DISCOVERED. THE A/C WAS LATER FLOWN TO THE MANUFACTURER'S MX FACILITY FOR FURTHER INVESTIGATION. THE MANUFACTURER HAS ISSUED A MX AND OPS LETTER GV-MOL-03-0034 WHICH DISCRIBES THIS OCCURENCE. (M) 2L72 4F RTA12EA 20030903001362003090300136EU 2003 9 3 2003F00533 120030802A3222 SEAL AIRBUS320 A320233 3930329EU NLG STRUT DAMAGED A RJEFK NONE K FLUID LOSS ININSP/MAINT 1 SO23EITAA V10445 SFO - FLT 562 - DURING GROUND CHECK, MAINTENANCE TECHS FOUND THE NOSE LANDING GEAR STRUT WITH FLUID LEAKAGE. TECHS PERFORMED REPLACEMENT OF THE NOSE LANDING GEAR STRUT SEALS AS PER AMM 32-21-13. OPS TEST OF THE NOSE LANDING GEAR RETRACTION AND EXTENSION WAS PERFORMED AS PER AMM 32-31-00. ALL RESULTS WERE SATISFACTORY AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20030903001472003090300147NM 2003 9 3 VNAA0308015 120030822A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY DIRTY A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07458PS 3068 THE CREW RECEIVED A LAV SMOKE CAS MESSAGE AND DIVERTED TO CMH. MAINTENANCE INSPECTED AND BLEW OUT THE LAV SMOKE DETECTOR WITH NITROGEN AND CLEANED THE CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030903001982003090300198NE 2003 9 3 AALA20030738 220030709A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RIGHT FLAMED OUT A AALABA EMER. DESCENT UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SW21461AA 49566 718435 SMF - FLT 1842 - EN ROUTE SMF-DFW, AFTER DEPARTURE, THE FLIGHT CREW REPORTED THE RIGHT ENGINE HAD A FLAME OUT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SMF WITHOUT FURTHER INCIDENT. REPLACED RIGHT ENGINE USING MAINTENANCE CHECK MANUAL CARD 71-91-99. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030815000342003081500034 2003 8 15 HEEA088520 420030802A3451066106902 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 COPILOT DME DISPLAY LIGHTS FLICKER. IN SHOP REPAIR. 1G72 4U H4SW 20030820002262003082000226NM 2003 8 20 USAASB03100 120030704A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 PIT - PILOT REPORTED THE EMERGENCY EXIT LIGHTS CONTINUALLY FLASH ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT EMERGENCY LGIHT BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030820002322003082000232EA 2003 8 20 ASOA03336 120030725A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11861AS 7445 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE BRACKETS AT FS 621, ON THE LEFT AND RIGHT SIDES, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20030821000012003082100001NM 2003 8 21 USAASB03112 120030717A274050556011 CHAIN BOEING737 7374B7 1384702NM STAB SEIZED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA19428US 24550 EN ROUTE FROM CLT TO PNS, FLIGHT CREW HEARD A CLUNKING SOUND WHEN ATTEMPTING TO USE STABILIZER TRIM. AFTER A FEW MORE ATTEMPTS TO USE THE NORMAL STABILIZER TRIM, IT FROZE UP AT FL280. MANUAL TRIM WAS UTILIZED, AND IT WAS DECIDED THAT A LONGER RUNWAY WOULD BE NEEDED FOR A 15 DEGREE FLAPS LANDING. CREW DECLARED AN EMERGENCY AND DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE STABILIZER CONTROL CABLE DRUM CHAIN TENSION HIGH. ADJUSTED TENSION PER MM 27-41-41-824. CLEANED AND LUBRICATED CHAIN. OPERATED SMOOTHLY AT THIS TIME. (M) 2L72 4F RTA16WE 20030821000702003082100070NM 2003 8 21 03FDEA00921 120030617A2752ARC198414 ACTUATOR DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING- O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR I/B BORE FOUND CORROSION. RIGHT WING- O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR I/B BORE REPAIRED AS PER FEDEX EA 1-5750-69375, TITLE: WINGS- TRAILING EDGE FLAP- RIGHT HAND OUTBOARD FLAP- INBOARD SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000802003082100080NM 2003 8 21 03FDEA00933 120030620A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT HORIZONTAL STAB UPPER CENTER PLANK 24L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. 2L73 4F RTA22WE 20030821001432003082100143NM 2003 8 21 03FDEA00885 120030616A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 FUSELAGE SKIN HAS A DENT, STRINGER 6L, BS 720C. REPAIR DENTED SKIN PER SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20030821002672003082100267WP 2003 8 21 GTIA030584 120030715A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - MAIN CABIN LEFT SIDE STATION 1174 TO 1250 SUB-FLOOR PANEL (PHENOLIC) HAS DISBONDED AT LOWER HATS SECTION AND CRACKS AT FORWARD EDGE. REPAIRED LOWER HAT SECTIONS AND CRACKS ON SUB FLOOR PANEL STATION 1174 TO 1250. (M) 2L72 4F A6WE 20030822000742003082200074NM 2003 8 22 CALA0300434 120030625A5330 SKIN BOEING737 737824 13844BZNM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 THE FUSELAGE SKIN SUSTAINED DAMAGE BELOW L-2 DOOR AT BS 958 BETWEEN S22L AND S23L. THE DAMAGE WAS REPAIRED IAW ECRA 5330-03261. A DIP WAS ISSUED TO ACCOMPLISH AN EXTERNAL DETAIL VISUAL INSPECTION OF THE FILLER AND DOUBLER LOOKING FOR CRACKS AND LOOSE OR MISSING FASTENERS. INITIAL INSPECTION THRESHOLD IS 56,000 TOTAL AIRFRAME CYCLES WITH REPEAT INSPECTION EVERY 12,000 CYCLES. 2L72 4F RTA16WE 20030822000842003082200084NM 2003 8 22 CALA0300385 120030710A256069B148553 SPRING BOEING757 757224 1384958NM GIRT BAR BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2712125 28967 A LEAF SPRING FOR L-2 DOOR GIRT BAR WAS FOUND BROKEN DURING PERFORMANCE OF FCD 2560-02033, B757-200/-300 GIRT BAR - INSPECT FOR PRESENCE AND CONDITION WHILE AT LAX. THE BROKEN SPRING PERMITS THE POSSIBILITY THAT THE SLIDE MIGHT NOT PERFORM ITS INTENDED FUNCTION WHEN OPERATED. THE LEAF SPRING WAS REPLACED. 2L72 4F RTA2NM 20030822000882003082200088NM 2003 8 22 CALA0300388 120030714A5210 GATE BOEING737 737524 1384721NM L-1 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711641 28902 INSPECTION FOUND CORROSION AND GOUGES ON EXTERIOR OF L-1 DOOR LOWER GATE. THE LOWER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030822000892003082200089NM 2003 8 22 03224430 120030812A3350DOLN1081M3D4NC RELAY DORNERDO32 DO328300 NM CABIN FAILED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27430FJ 3209 DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE 9LK RELAY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030822001362003082200136NM 2003 8 22 03022 120030806A2612 FIRE LOOP BOEING747 747146 1384905NM PWA JT9 JT9D7 52054NE NR 2 ENGINE SHORTED A KCSAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23702CK 20332 662517 SHUT DOWN NR 2 ENGINE AT 1640Z DUE TO HIGH NACELLE TEMP 8+ ON THE SCALE INDICATOR LOOP -A-. WINDMILL OIL PRESSURE 23 FOR 2 HOURS 16 MINUTES. NO RESTART ATTEMPTS WERE MADE. 2L74 4F4 FRTA20WE E20EA 20030822001382003082200138NM 2003 8 22 CALA0300442 120030806A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 316-322, LBL 45. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030822001502003082200150NM 2003 8 22 C1HA200383007 120030817A3350900835A BATTERY PACK BOEING727 7272S7 138407ZNM CABIN DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW 727 MM 33-50-22, ALL OPS NORMAL. 2L73 4F A3WE 20030903002042003090300204NM 2003 9 3 QXEA200301034 120030825A5512 VORTEX GEN DHAV DHC8 DHC8202 2809007NM HORIZ STAB LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- HORIZONTAL STABILIZER LEFT INBOARD VORTEX GENERATOR IS LOOSE AND SEPERATING FROM THE BOTTOM OF THE STABILIZER. REPAIRED IAW DHC-8 SRM 55-10-10 AND TASK 55-10-10-000-801. 2H72 4T RTA13NM 20030903002062003090300206NM 2003 9 3 QXEA200300968 120030810A30104100S00501 VALVE BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09406QX927 927 4048 SEA- ON FLIGHT 2384 DEICE PRESSURE CAUTION LIGHT ILLUMINATED AFTER SELECTING DEICE BOOTS TO SLOW. ACCOMPLISHED DEICE PRESSURE CHECKLIST. INBOARD BOOT OF HORIZONTAL STABILIZER SHOWS NOT INFLATING. DEICE PRESSURE FOR BOTH SIDES SHOWED NO DROP. BOOT DID NOT WORK IN MANUAL AS WELL. REMOVED AND REPLACED DISTRIBUTION VALVE. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903002412003090300241EA 2003 9 3 03238671 120030826A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA CABIN DEFECTIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27671BR 7572 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND TO BE DIM. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 4 INVERTER. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030903002682003090300268SO 2003 9 3 C2XA03TY140 120030828A532014522460015 GUSSET EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 TYS DURING A SCHEDULED 2C INSPECTION THE AFT GUSSET WAS FOUND WITH SEVERAL AREAS THAT WAS CORRODED. MAINT R&R THE AFT GUSSET IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030904000022003090400002CE 2003 9 4 DXTA200300046 120030611A3240 BRAKE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG FAILED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07330QS 5600329 ON TAXI IN DEPRESSED BRAKE AND AIRCRAFT WOULD NOT STOP FOR 2-3 SECOND . WITH BRAKE PEDALS DEPRESSED AIRCRAFT CONTINUED TO ROLL FOR SHORT DISTANCE. ITEM IS UNDER INVESTIGATION. INSPECTED BRAKE RESEVIOR, ACUMULATOR, MASTER CYLINDERS AND BREAK ASSY'S ALL CHECKED NORMAL. CHECKED FOR LEAKS AND CONDITION, ALL WERE GOOD- BLED BRAKES AND CARRIED OUT TAXI CHECK ON AND STATIC BRAKE TOE CHECK WITH N1=60 PERCENT ALL WERE GOOD- ALL WORK DONE I.A.W. CE-560 MM CHAP 32-42-01. 2L72 4F4 FRTA22CE E25EA 20030904000062003090400006EA 2003 9 4 SWIA200312155 120030625A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-51 2L72 4F RTA21EA 20030904000132003090400013EU 2003 9 4 AWXA200300777 120030705A2913887673 PUMP AIRBUS320 A320232 3930326EU HYD SYS FAULTY A AWXAO OTHER J WARNING INDICATION CLCLIMB 1 WP28658AW1399213992 1110 PHX - EMERGENCY LANDING - FLT 0614 - AFTER TAKEOFF PHX EN ROUTE FOR ATL, PILOT REPORTED THAT A GREEN RESERVOIR OVERHEAT ECAM MESSAGE APPEARED. PILOT FOLLOWED ECAM DIRECTIONS, HOWEVER WAS UNABLE TO RESTORE GREEN SYSTEM PRESSURE. MAINTENANCE REMOVED AND REPLACED NO. 1 ENGINE GREEN SYSTEM ENGINE DRIVEN HYDRAULIC PUMP PER AMM 29-11-51-401. OPERATIONAL AND LEAK CHECK WAS FOUND TO BE GOOD. VENDOR TEARDOWN OF HYDRAULIC PUMP S/N MX611108 COULD NOT VERIFY REASON FOR REMOVAL. THERE WERE NO INDICATIONS THAT PUMP CAUSED HYDRAULIC SYSTEM FAILURE. UNIT WAS FOUND TO HAVE WORN SEALS, AND ALSO REQUIRED LAPPING OF PISTONS, WEAR PLATE, AND CYLINDER BLOCK DUE TO NORMAL SCORING, ALL CLEARANCES WERE WITHIN LIMITS. 2L72 4F RTA28NM 20030904000292003090400029SO 2003 9 4 C2XA03SH272 120030817A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV DURING C CHECK APU FIRE WALL AT LEFT HAND SIDE HAS A CRACK ALONG THE BOTTOM PORTION OF SUPPORT FLANGE AT 10 O'CLOCK POSITION. MAINTENANCE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030904000312003090400031SO 2003 9 4 SWIA200312217 120030725A5420 MOUNT BRACKET EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07585SW 120353 RIGHT HYD PACK LOWER MOUNT BRACKET HAS 2 CRACKS, ONE APPROX 3 INCHES AND ONE APPROX 1.5 INCHES. DISCOVERED DURING E003 INSPECTION. REPLACED RIGHT HYD PACK LOWER MOUNT BRACKET WITH SERVICEABLE PART IAW SRM 51-40-00. 2L72 4T RTA31SO 20030904000332003090400033EA 2003 9 4 SWIA200312273 120030817A2711 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA AILERON DIRTY A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07437SW 7564 AILERON TRIM IS FROZEN IN POSITION, WOULD NOT MOVE AFTER LANDING. CLEANED AILERON TRIM SWITCH. RESET CB CBP2F7. OPERATED AILERON TRIM. OPS CHECK GOOD. 2L72 4F RTA21EA 20030904000362003090400036 2003 9 4 SWIA200312274 420030819A22156225734002 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07268UE7669 7669 120207 DURING FLIGHT CONTROL COLUMNS BEGIN TO OSCILLATE FOLLOWED BY AUTOPILOT FAIL ON MAP AND AP ON FCP. HAPPENED ON BOTH CAPT AND FO SIDE. REPLACED PITCH DATA RELAYS K0312 & K0256 (CAPT'S SIDE). REPLACED AILERON SERVO AND AP TRANSFER BOX. AP AND AP TRANSFER OPS CHECKS GOOD. P/N 622-5734-002, S/N 5847, S/N ON 5851, P/N 120-39864-001 S/N 120207, P/N ON 120-49625-001, S/N ON 120341. 2L72 4T4 TRTA31SO E20NE 20030904000492003090400049 2003 9 4 SWIA200312255 420030809A341845150340 SENSOR CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAILED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07426SW7124 7124 7468 AFTER T/O, GOT A STALL FAIL MSG. CAPT SLOW SPD CUE CLIMBED TO 200 KTS AND CONTINUED TO 280 KTS AS A/C ACCEL TO 290 KTS. THIS CONDITION CONTINUED UNTIL DESCENT. FOUND AOA FAILED IN MDC. REMOVED AND REPLACED LEFT AOA SENSOR IAW CL600 MM 27-35-05. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030904000502003090400050EA 2003 9 4 SWIA200312256 120030808A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07411SW 7067 DURING GLD FFOD WHEN (MAN ARM) IS SELECTED OR FLT SPOILERS EXTENDED THE (FLT SPOILERS FAULT) STATUS MSG IS DISPLAYED. RESET CB'S IAW, FAULT MSG. STILL CAME ON. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILER PCU W/SERVICEABLE UNIT IAW MM 27-62-01. OPS CHECK GOOD . P/N: 27000-7 2L72 4F RTA21EA 20030904000562003090400056EA 2003 9 4 SWIA200312248 120030811A2760 SWITCH CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07423SW 7456 GROUND SPOILER DEPLOY MSG DURING TO ROLL AT 70 KIAS ACCOMPANIED BY CONFIG SPLRS WARNING MESSAGE. ABORTED TAKEOFF. REPLACED AUTO/MANUAL/GROUND LIFT DUMPING SWITCH. SYSTEM CHECKS OK. P/N: MS27789-21A 2L72 4F RTA21EA 20030904000652003090400065EA 2003 9 4 SWIA200312305 120030819A274270623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07412SW3090 3090 7101 STAB TRIM CH 2 INOPERATIVE, WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL UNIT AND REMOVED AND REPLACED FO'S DISCONNECT SWITCH IAW 27-40-00. P/N: 8396-3 S/N OFF: 806 2L72 4F RTA21EA 20030822001802003082200180WP 2003 8 22 UPS03841076 120030812A8011 OIL CAP DOUG DC8 DC873F 302199FWP NR 3 ENG STARTERUNSECURE A IPXAEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO01805UP 46117 INSPECTION TYPE:N/A NR 3 ENGINE SLOW TO RESPOND TO THROTTLE INPUT DURING BOOST TO START NR 2 ENGINE. APPROX 10 MIN INTO FLT OIL QTY DECREASED TO 4 QTS. ENGINE SHUTDOWN ACCOM AT 2 QTS, IAW CHECKLIST. WINDMILL TIME OF APPROX 40 MIN WITH 2-5 PSI. FOUND NR 3 STARTER SERVICING CAP OFF CAUSING STARTER TO FAIL AND OIL TO VENT OVERBOARD. STARTER REMOVED AND REPLACED IAW MM 80-10-01. SERVICED ENG OIL, OPS CHECKS GOOD IAW MM 71-00-00. 2L74 4F RT4A25 20030825000012003082500001NM 2003 8 25 UPS03441128 120030723A531165B07935194 FRAME BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RT TUNNEL TORQUE BOX STA 340 IN BETWEEN STR 42 AND STA 43 CHORD FOUND CORRODED. THE CORD REPLACED IAW SRM 51-10-01 P8. (CORROSION REMOVED - BLEND OUT DEPTH 0.050 WIDTH 1 INCH LENGTH 1 INCH OUT OF SRM 53-10-01 FIG 1 LIMITS. 2L74 4F A20WE 20030825000152003082500015WP 2003 8 25 UPS03840977 120030710A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 RT FWD FUSELAGE SKIN (EXTERNAL DOUBLER) IS CRACKED AT LOWER AFT CORNER OF RH AFT HEAT EXCHANGER OPENING AT STA -12 AT LONG. 27R CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED FILLER AND DOUBLER IAW UPS EO DC8-5330-4732 2L74 4F RT4A25 20030825000192003082500019WP 2003 8 25 UPS03841090 120030726A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C2 STATION 1750 LONGERON 15R IS CRACKED. CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 53-2-2 FIG. 12 2L74 4F RT4A25 20030825000222003082500022WP 2003 8 25 UPS03841107 120030805A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 LEFT UPPER CUSP IS CRACKED AT STA. 1180 LONG.21L NDT VERIFIED CRACKED AREA, CUTOUT DAMAGE BETWEEN STA. 1170 TO 1190, FABRICATED AND INSTALLED REPAIR DOUBLER AND SPLICES I.A.W. SRM. 53-2-5 FIG. 15 2L74 4F RT4A25 20030825000262003082500026WP 2003 8 25 UPS03840908 120030606A5313 LONGERON DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3 AFT PIT FS 1350, LONGERON 35L IS CRACKED. REMOVED CRACKED LONG 35L FS 1270 TO 1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 3 5L FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0. 2L74 4F4 FRT4A25 1E8 20030825000272003082500027WP 2003 8 25 UPS03840910 120030626A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: PFLT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01. OPS CKS GOOD, OK FOR SERVICE. 2L74 4F RT4A25 20030825000282003082500028NM 2003 8 25 UPS03M40909 120030326A5751S2929242 SUPPORT DOUG MD11 MD11F 3023600NM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP 48572 INSPECTION TYPE: RT WING FWD INBOARD AILERON FOUND CORROSION AT PANEL SUPPORT FROM ST A XW=291 TO XW=373 AS MARK. CORROSION ON PANEL SUPPORT RT WING STA XW291 TO XW373 REMOVED AND PROTECTED IAW SRM 51-21-01 VOLIIREV32. FOUND OUT OF LIMIT IAW SRM 57-00-0 1 VOLIREV 32.OUT OF LIMIT AREA AT PANEL SUPPORT TRIMMED IAW EN1005-0 3. TEE CAP AND REPAIR ANGLES FABRICATED IAW EN1005-03. TEE CAP AND REPAIR ANGLES AND TEE ANGLE INSTALLED IAW EN1005-03. 2L73 4F RTA22WE 20030825000542003082500054WP 2003 8 25 UPS03841125 120030819A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:N/A EMERGENCY LIGHTING WILL NOT WORK. REMOVED & REPLACED EMERGENCY BATTERY PACK OPS CK GOOD PER MM 33-50-01-2 P/N ON AND OFF SAME 60-1223-5. S/N ON 219 & OFF FTL070. 2L74 4F RT4A25 20030825000562003082500056NM 2003 8 25 UPS03M41133 120030818A2910 HYDRAULIC SYSTEM DOUG MD11 MD11F 3023600NM LEFT FAILED A IPXAK NONE J WARNING INDICATION CRCRUISE 1 SO01252UP LT HYD SYS FAILED. (RT HYD CNTRL C/B POPPED) PER A/C STATUS IN IMPACTS THIS OCCURED IN CRUISE. R&R HYD SYS CONTROLLER PER 29-08-01 OP TEST DUE FOR REPLACEMENT OF CONTROLLER (A/P NO. ILLEGIBLE) RAN ENGS AND TESTED PUMPS & HSC PER 29-11-20 & 29-11-21 NO FAULTS. PUMP OPS NORMAL.R&R RELAY R2-5414 & ENG 2R HYD PUMP BYPASS SOLENOID. R&R C/B R&R DEPRESSURIZATION VALVE NR 2 PER 29-11-21. RAN ENGS TESTED HYD PUMPS PER 29-11-20 CHECKS OK 2L73 4F RTA22WE 20030821001642003082100164NM 2003 8 21 03FDEA01028 120030702A2781859803 PSEU DOUG MD11 MD11 3023602NM L/E SLAT MALFUNCTIONED A FDEAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25619FE 48770 ON CLIMBOUT OF FRA, RECEIVED A SLAT DISAGREE ALERT WHEN SLATS RETRACTED WITH A STRONG ROLL TO RIGHT. RED TABS COMPLIED WITH AND SLATS EXTENDED A/S 270 KIAS. SLATS EXTENDED FINE WITH NO CONTROL PROBLEMS. DUMPED FUEL AND DIVERTED TO PARIS. T/S AS PER FIM 31-71-07-00. REMOVED AND REPLACED PROX SENSOR DI-14 AS PER AMM 27-84-03-4. REMOVED AND REPLACED PSEU AS PER AMM 31-71-01-2. PERFORMED OPS/TEST 27-84-00. ALL TESTS ARE OK. 2L73 4F RTA22WE 20030821002232003082100223EU 2003 8 21 RAIA00306180 120030630A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN NOT SEATED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03550HK 41039 5479-STL- ONE STRIP OF EMERGENCY PATH LIGHTS INOP. RESEATED LIGHT STRIP CONNECTOR. 2L72 4T RTA41NM 20030821002332003082100233 2003 8 21 250TR0021 420030719A34252591092904 INDICATOR BOEING737 7372K5 138448XNM COCKPIT FAULTY A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 ADI ATTITUDE FLAG STICKS WHEN TEST SWITCH ACTUATED ON FIRST OFFICER'S SIDE. REPLACED FIRST OFFICER'S INDICATOR AND OPS CHECKED OK PER MM 34-22-0. 2L72 4F RTA16WE 20030821002522003082100252WP 2003 8 21 03FDEA01336 120030818A2150ACM70191 DUCT DOUG DC10 DC1010 3022110WP NR 3 A/C PACK DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 AIR CONDITIONING- NR 3 AC PACK EXHAUST DUCT REPAIR P/N ACM7019. FACT 18AUG03 22:55 BFM R COMPLIED WITH EA 8-2150-72259 AIR CONDITIONING NR 3 AC PACK EXHAUST DUCT REPAIR P/N ACM7019 AT MAE. 2L73 4F A22WE 20030821002662003082100266WP 2003 8 21 GTIA030593 120030721A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - LEFT FLOOR PANEL, FS 886, SKIN CRACKED WITH MATERIAL MISSING AND EDGE FILLER DAMAGED AROUND PERIPHERY. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030904000702003090400070NM 2003 9 4 QXEA200301052 120030901A2120 SMOKE DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09364PH 524 PIH- ON FLIGHT 2187 AFTER ENGINE START WHEN BLEEDS WERE SELECTED ON FLIGHT ATTENDANT NOTICED BLUE/GRAY SMOKE COMING FROM FLOOR VENTS. SMOKE STOPPED AFTER A MINUTE OR TWO. GROUND RAN NR 1 AND NR 2 ENGINES WITH BLEEDS ON. NO NOTICABLE SMOKE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904000752003090400075NM 2003 9 4 QXEA200301047 120030901A2422DH103024600C INVERTER DHAV DHC8 DHC8202 2809007NM ELECTRICAL SYS FAILED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09354PH 498 SEA- ON FLIGHT 2240 FISH OIL SMELL IN FLIGHT DECK. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904000792003090400079NM 2003 9 4 QXEA200300983 120030816A5420 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM NR 2 NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX- NR 2 NACELLE UPPER HEAT SHIELD RIGHT FORWARD SUPPORT BRACKET IS CRACKED AT RADIUS. REPAIRED IAW HORIZON AIR EA 8-54-273 AND Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030904000852003090400085NM 2003 9 4 QXEA200300993 120030812A1430 BOLT DHAV DHC8 DHC8202 2809007NM GUST LOCK LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- ELEVATOR GUST LOCK JO-BOLTS CONNECTING THE ARM ASSEMBLY TO THE BUMPER STEP ASSEMBLY IS LOOSE. REPAIRED IAW DHC-8 RD 8-55-112 AND SRM 27-70-11. 2H72 4T RTA13NM 20030903000622003090300062 2003 9 3 HYI2003F00006 420030708A3197CM358950 MASTER SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LT SWITCH PANEL BURNED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE011376G999 402C0271 UPON CLIMBOUT, PILOT SMELLED SMOKE, FOUND SMOKE COMING FROM AVIONICS MASTER SWITCH. PILOT NOTIFIED TOWER BEFORE SHUTTING DOWN AVIONICS SWITCH, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20030903001512003090300151NM 2003 9 3 VNAA0308013 120030820A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN INOPERATIVE A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07437JS 3055 THE CREW REPORTED THAT THE AFT EMERGENCY FLOOR LIGHT STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030903002142003090300214NM 2003 9 3 QXEA200300918 120030720A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX-NR 2 DME HAS CORROSION ON SKIN WHEN ANTENNA IS REMOVED. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16 AND 51-00-06. 2H72 4T RTA13NM 20030903002472003090300247EA 2003 9 3 03232621 120030820A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27621BR 7186 DURING MAINTENANCE THE FWD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULBS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICEDCN#147776 2L72 4F RTA21EA 20030903002512003090300251SO 2003 9 3 C2XA03BT086 120030830A36208166243 SENSOR EMB 145 EMB145LR 3260212SO NR 1 FAULTY A C2XAO OTHER BN SMOKE/FUMES/ODORS/SPARKS FALSE WARNING UKUNKNOWN 1 SW2729906 145472 EWR---CO2452, CREW REPORTED, WHEN ENTERING ICING CONDITIONS NR 1 BLEED TEMPERATURE INDICATOR TRAVELS FROM BOTTOM OF WHITE TO TOP OF THE RED ARC FOLLOWED BY BURNING SMELL IN COCKPIT. REMOVED AND REPLACED NR 1 FAN AIR PRECOOLER SENSOR. OPS CHECKED GOOD IAW EMB145 AMM 36-11-06. 2L72 4T RTT00011AT 20030904000102003090400010NE 2003 9 4 DXTA200300061 220030706A7200 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT INOPERATIVE E DXTAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 GL07396QS 5600396 PCEJCO584 AFTER ENGINE START HEARD LOUD POP WITH LEFT GENERATOR COMMING OFF LINE AND FOLLOWED BY ENGINE FLAMMING OUT. PERFORMED RIGGING ON LT ENGINE AFT THROTTLE CABLE TO FCU IAW CESSNA 560 MAINTENANCE MANUAL CHAPTER 76-11-00 AND PRATT WHITNEY JT15D MAINTENANCE MANUAL CHAPTER 71-00-00. PERFORMED ENGINE RUN OPERATIONAL CHECKS SATISFACTORY. 2L72 4F4 FRTA22CE E25EA 20030904000942003090400094NM 2003 9 4 QXEA200301000 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 1 SEAT TRACK HAS TOP SURFACE CORROSION AT STATION X342.250. REPAIRED IAW DHC-8 RD 8-53-1342 AND SRM 51-00-06. 2H72 4T RTA13NM 20030904001022003090400102NM 2003 9 4 QXEA200301046 120030831A2120 SMOKE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09364PH 524 AG0069 SEA- ON FLIGHT 2075 ON ENGINE START WHEN BLEEDS SELECTED ON, LIGHT SMOKE WAS OBSERVED ON FLIGHT DECK AND CABIN. ALL SMOKE CLEARED AFTER A FEW MINUTES, ALL OTHER INDICATIONS ARE NORMAL. GROUND RAN NR 1 AND NR 2 ENGINE BLEEDS. NO SMOKE NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030904001082003090400108NM 2003 9 4 QXEA200301006 120030820A5230 MECHANISM BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR LACK OF LUBE A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09408QX 4050 PDX- ON FLIGHT 2308 RETURNED TO FIELD DUE TO BAGGAGE DOOR INDICATED OPEN. AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED AND LUBED LOCK MECHANISM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904001152003090400115EA 2003 9 4 QXEA200300962 120030810A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09613QX 10045 BOI- ON FLIGHT 2523 FIRE SYSTEM FAULT STATUS MESSAGE. COMPLIED WITH FIDEEX SYSTEM OPERATIONAL TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030904001292003090400129NM 2003 9 4 DLM90030614 120030706A242128B5278 GENERATOR DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 2 ENGINE CRACKED A DALAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO27907DA 53387 020046 ON TAKEOFF ROLL PILOT ABORTED TAKEOFF WHEN HE GOT A RT GEN OVERHEAT MESSAGE AND A RT GEN FILTER MESSAGE. REPLACED VSCF FOR CRACKED HOUSING 2L72 4F4 FRTA6WE E40NE 20030821002782003082100278NM 2003 8 21 USAASB03107 120030713A335020121 CHARGER BOEING737 7374B7 1384702NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19784AU 25023 PHL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LGIHTS AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030822000222003082200022NM 2003 8 22 03FDEA01041 120030704A5514NLC6725 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT HORIZONTAL STABILIZER NR 2 BORE CORROSION EXCEEDED LIMIT AFTER REWORKED. CORROSION ON LEFT HORIZONTAL STABILIZER NR 2 BORE REMOVED AND REPAIRED CARRIED OUT AS PER EA 1-5510-69394 (TITLE : STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL - BORE 2 LEFT). 2L73 4F RTA22WE 20030822000552003082200055WP 2003 8 22 03FDEA01233 120030810A5753ARC0154 HINGE DOUG DC10 DC1030 3023501WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 WINGS-R 2FH INBOARD FLAP 2C HINGE ASSY ATTACH LUG REWORKED ENT BY 3A 39017C RPT BY 3A39017. FACT 10AUG03 21 3A10 BFM COMPLIED WITH EA 8-5740-70995A WINGS-R 2FH INBOARD FLAP 2C HINGE ASSY ATTACH LUG REWORK MAE BY 3A DC40999V RPT BY 3A 40999V. 2L73 4F A22WE 20030822000712003082200071NM 2003 8 22 2003UALA00517 120030620A3350M1137 CHARGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29321UA 23953 FLIGHT CREW REPORTED THAT THE EMERGENCY ASILE LIGHTS ABOVE ROW 19 AND 20, AND THE DOOR 2R FLOOR LEVEL LIGHT ARE INOPERATIVE. *SUPPLEMENTAL DATA UPDATE* REPLACED M1137 BATTERY CHARGER ASSY. 2L72 4F4 FRTA16WE E2GL 20030822001552003082200155EA 2003 8 22 QXEA200300945 120030802A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX- FORWARD CARGO BAY CHIMNEY HAS DAMAGE IN WEBBING. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20030822001592003082200159NM 2003 8 22 UPS03441115 120030717A5312141U11073 PRESSURE PANEL BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C NLG W/W BOX STRUCTURE LT BS 320 VERTICAL BEAM WEB FOUND APPROX .125 INCH CRACK AT LOWER STAND OFF HOLE BETWEEN 1ST AND 2ND STAND OFF HOLE (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20030822001732003082200173WP 2003 8 22 UPS03841087 120030724A53134772397U1 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 STA 1766 LONG 17L AND END FITTING ARE CRACKED REMOVED, FABRICATED AND REPLACED LONGERON SECTION, AND REPLACED END FITTING IAW DWG 5649327, 4772397 AND SRM 51-1-20D. 2L74 4F RT4A25 20030825000582003082500058NM 2003 8 25 UPS03441140 120030821A242465B000106 GCU BOEING747 747123 1384873NM E/E BAY MALFUNCTIONED A IPXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO01672UP 20324 INSPECTION TYPE:N/A DURING SHUTDOWN ON ENG 2 & 3 DURING TAXI IN BTB NR 2 OPENED. WHEN CLOSURE ATTEMPTED THE KW OUTPUT ON GEN 4 SPIKED TO 60+ KW AND BTB REOPENED. ALSO SMELLED SLIGHT ODOR OF ELECTRICAL SMELL/BURN. REMOVED AND REPLACED NR 2 GCU. 2L74 4F A20WE 20030825000662003082500066NM 2003 8 25 UPS03541002 120030725A3510 OXYGEN MASK BOEING757 75724APF 1384969NM COCKPIT OUT OF ADJUST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01447UP 27736 INSPECTION TYPE:P/C, F/O O2 MASK DOES NOT TEST. ADJUSTED F/O O2 MASK, F/O OXYGEN BOTTLE TEST GOOD IAW MM 35-11-5. 2L72 4F RTA2NM 20030825000672003082500067NM 2003 8 25 UPS03541003 120030725A3510 OXYGEN MASK BOEING757 75724APF 1384969NM COCKPIT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01447UP 27736 INSPECTION TYPE:P/C LEFT JUMPSEAT O2 MASK DOES NOT TEST. REMOVED & RE-INSTALLED O2 MASK LEFT JUMPSEAT PER 35-11-51-4 & PERFORMED ADJ & TEST PER 35-11-5. 2L72 4F RTA2NM 20030825000692003082500069WP 2003 8 25 UPS03841001 120030726A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A IPXAK NONE O OTHER TOTAKEOFF 1 SO01804UP 46004 INSPECTION TYPE:N/A CAPTS SEAT SLIDES AFT ON TAKEOFF ROLL. INSTALLED NEW BOTH AFT SEAT TRACKS REF EO DC8-5340-0741E SRM 53-2-3 FIG 11, REMOVED AND REPLACED CAPT SEAT PER DC8 MM 25-11-01. OPS CHECK GOOD. 2L74 4F RT4A25 20030825000802003082500080EA 2003 8 25 COMA0370022 120030802A274070744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA HORIZ STAB MALFUNCTIONED A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO01390CA185 10106 FLIGHT 5743 STAB TRIM AND MACH TRIM WARNINGS AUTO PILOT AND PITCH TRIM WARNING. REPLACED THE MCU. 2L72 4F RTA21EA 20030825000872003082500087NM 2003 8 25 CALA0300439 120030805A5347 SEAT TRACK BOEING777 777224 1385225NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776010 29480 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1496-1580, LBL 75. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 3, FIGURE 202. 2L72 4F RTT00001SE 20030825001292003082500129SO 2003 8 25 C2XA03SH275 120030817A711014576608003 SKIN EMB 145 EMB145LR 3260212SO RT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV DURING C CHECK THE RIGHT HAND LOWER COWLING WAS FOUND TO HAVE A GOUGE MARK AT FRAME 8 ON MOST OUTBOARD STRINGER. MAINTENANCE REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030825001422003082500142WP 2003 8 25 GTIA030611 120030728A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN DISCONNECTED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23804NK 49104 FOUND L2 DOOR AND AFT ENTRY DOOR EMERGENCY EXIT SIGNS ARE INOPERATIVE. FOUND BATTERY PACK CONNECTOR DISCONNECTED. CONNECTED CANNON PLUG TO BATTERY PACK. (M) 2L72 4F A6WE 20030825001642003082500164WP 2003 8 25 GTIA030603 120030725A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND RIGHT COCKPIT FLOOR PANELS TWO NO FILL AND DELAMINATED. FABRICATED TWO NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030825001652003082500165SO 2003 8 25 C2XA03BT071 120030710A26123601133500230 FIRE DETECTOR EMB 145 EMB145ER 3260211SO NR 1 ENGINE FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2713929 145009 GRR/EWR---CO2355, CREW REPORTED, ( NR 1 ENGINE FIRE INDICATION IN CRUISE FLIGHT, DIVERTED)....MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION CONTROL MODULE (PN: 902061 SN: 236) IAW EMB145 AMM NR 26-11-03. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTOR (PN: 3601-133-500/230C-9.0M SN: 228082) IAW EMB145 AMM NR 26-11-01. OPERATIONAL TEST OF NR 1 ENGINE FIRE DETECTION SYSTEM GOOD IAW EMB145 AMM NR 26-10-00. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030825001672003082500167SO 2003 8 25 C2XA03BT070 120030706A3320 LIGHT EMB 145 EMB145 3260210SO LAVATORY INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2713956 145078 EWR---CO2233, CREW REPORTED, "AFT CABIN HAS SMOKE ODOR WITH APU BLEED ON AND BOTH PACKS ON GROUND AND BURNING SMELL FROM AIRCRAFT CABIN AND INSIDE LAV ON GROUND WITH APU BLEED AND BOTH PACKS ON.......TROUBLESHOOTING PERFORMED, INSPECTED CABIN AND LAV AREAS AND REMOVED AND REPLACED SINK LIGHT ASSEMBLY REFERENCE EMB145 MM 33-28-03, REMOVED AND REPLACED CONNECTOR J8488. OPS. CHECKED OF LAV LIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030825001752003082500175NM 2003 8 25 03FDEA01313 120030809A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 SNRM N0739 3A L2 FH WING 2FB FLAP 2FB HINGE 28 2FC SIDE 29 CORROSION FOUND ON FORWARD ATTACHMENT HOLE I2 FB BORE. ** S/D ** COMING 2L73 4F RTA22WE 20030826000012003082600001NM 2003 8 26 03FDEA01380 120030808A5753ARC70571 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING OUTBOARD FLAP VANE NR 5 FITTING (MOST OUTBOARD) FWD AND AFT HOLE FOUND CORROSION. 2L73 4F RTA22WE 20030822000192003082200019NM 2003 8 22 03FDEA00808 120030523A5753ARC198414 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP - HINGE AFT FITTING FOUND OUTBOARD ACTUATOR BORE WITH MINOR CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69346 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030822001042003082200104SO 2003 8 22 RAIA00307184 120030706A3350 CONNECTOR EMB 145 EMB145 3260210SO CABIN LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03803HK 145077 MX-PIT- EMERGENCY PATH LIGHT INOP ROW 12. RE-SECURED CONNECTOR TO PATH LIGHT TRACK. 2L72 4F RTT00011AT 20030822001772003082200177NM 2003 8 22 UPS03441078 120030718A532065B0432629 ATTACH ANGLE BOEING747 747123 1384873NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D- BS 1780 STR 22R-23R FRAME ATT ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-10-01 P 8. 2L74 4F4 F A20WE E20EA 20030826000152003082600015NM 2003 8 26 03FDEA01287 120030806A5744ARC0502 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) LOWER INBOARD ATTACH HOLE CORRODED AT BORE AND FWD / AFT FACE. RIGHT OUTBOARD FLAP INBOARDD HINGE (A/C SIDE) LOWER INBOARD ATTACH HOLE BORE AND FWD & AFT FACE (SURFACE) REPAIRED AS PER CMM 57-44-08 & DWG ARC0502. 2L73 4F RTA22WE 20030826000212003082600021NM 2003 8 26 03FDEA01367 120030806A5744ARC0502506 HINGE BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) ACTUATOR HOLE FOUND CORROSION. RT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR HOLE REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-71797, TITLE - WINGS - LT AND RT O/B FLAP - I/B HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030826000232003082600023NM 2003 8 26 03FDEA01223 120030807A5311 FRAME BOEING727 7272S2F 1384O81NM FUSELAGE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 FWD CARGO BAY 680 FRAME BENT AT RBL 35 BETWEEN STR 24R+25R. 2L73 4F A3WE 20030826000252003082600025NM 2003 8 26 03FDEA01371 120030806A5744ARC0503504 HINGE BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE BRACKET (WING SIDE) BARREL NUT BOLT HOLE FOUND CORROSION. RT WING OUTBD FLAP OUTBD HINGE BRACKET (WING SIDE) BARREL NUT BOLT HOLES REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-71796, TITLE - WINGS - LT AND RT O/B FLAP - O/B HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030826000262003082600026NM 2003 8 26 03FDEA01372 120030806A5753ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE FOUND CORROSION. LT WING OUTBD FLAP OUTBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-71800: WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20030826000282003082600028NM 2003 8 26 03FDEA01374 120030806A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING OUTBOARD FLAP INBOARD HINGE BRACKET (FLAP SIDE) OUTBOARD PIVOT HOLE FOUND CORROSION. LT WING OUTBD FLAP INBD HINGE BRACKET (FLAP SIDE) OUTBD PIVOT HOLE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71799, TITLE - WINGS - LEFT AND RIGHT O/B FLAP - I/B HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20030826000462003082600046NM 2003 8 26 03FDEA01190 120030725A5744ARC050213 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. LEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69406, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030904001442003090400144WP 2003 9 4 DHL2003873590 120030710A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FWD CARGO COMPT RT TUNNEL LONGERON 26R CORRODED BETWEEN STA180.000 AND STA 200.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 PG 1-3 FIG 10-11. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON L-26R. FOUND OUT OF LIMITS. CUT OUT CORRODED AREA, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND SPLICE FITTING IAW SRM 53-2-2 PG 1-3 FIG 10-11. PERFORMED LIQUID PENETRANT INSPECTION IAW DC8 NDT SPM PART 08-00-02106. CLEANED, TREATED AND PRIMED FILLER SPLICE FITTING IAW SRM 51-1-8. INSTALLED FILLER AND SPLICE FITTING ON L-26R WITH NEW FASTENERS IAW SRM 53-2-2 PG 1-3, FIG 10-11, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20030904001522003090400152WP 2003 9 4 DHL2003873518 120030617A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT OUTER WING INBD L/E UPPER PART PLATING SHOWS CORROSION IN MANY POINTS BETWEEN XFS 560 AND XFS 710 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED INTERIM REPAIR. REMOVED CORROSION FROM INBD L/E UPPER PART PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11, 12. CUT OUT CORRODED AREA IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLERS AND DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER PART IAW SRM 51-1-8B. INSTALLED FILLERS AND DOUBLER ON LT OUTER WING INBD L/E UPPER PART PLATING IAW SRM 57-2-1 FIG 38, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030904001532003090400153WP 2003 9 4 DHL2003873508 120030610A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING CTR L/E FORMER CRACKED 0.250 AT STA XFS 379. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT XFS 379 IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCEMENT ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED REINFORCEMENT ANGLE IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE WITH NEW FASTENERS ON CENTER L/E FORMER (LT WING) IAW SRM 57-2-0 PG 9,10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030904001542003090400154WP 2003 9 4 DHL2003873584 120030629A532047516252 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT FITTING CRACKED 3.000, STA.680.000 L-11L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING AT STA 680.000 L-11L IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030904001782003090400178WP 2003 9 4 AALA20030797 120030728A2751 TRANSFORMER DOUG DC9 DC982 3022082WP T/E FLAP MALFUNCTIONED A AALAO OTHER N FALSE WARNING CLCLIMB 1 SW21587AA 53250 FLT 385 - DFW-SJC - ON CLIMB-OUT, FLAP INDICATION SPLIT. LEFT 0 DEGREES, RIGHT 8 DEGREES WITH NO ABNORMAL FLIGHT CONDITIONS. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED RT INST XFMR CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND REPLACED T1-20 TRANSFORMER AS A PRECAUTIONARY MEASURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904001892003090400189WP 2003 9 4 AALA20030794 120030724A2120C38C37 CLAMP DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21228AA 49178 FLT 528 - DFW-ATL - TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON 3 TIMES DURING CLIMB-OUT. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED CLAMPS THAT SECURE THE EIRHG TRIM AIR VALVE TO BE LOOSE. RESECURED THE ASSOCIATED V-BAND CLAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904002002003090400200NM 2003 9 4 C1HA200396015 120030828A3260 SWITCH BOEING727 7272J4 1384006NM NLG CONTAMINATED A C1HAK NONE N FALSE WARNING UKUNKNOWN 1 GL15696CA 22574 BOTH RED (NOSE GEAR) DISAGREEMENT LIGHT AND GREEN (NOSE GEAR) DOWN/LOCKED LIGHT ILLUMINATED. NOSE GEAR LOCK AND POS SWITCHES ADJUSTMENT TEST DONE AFTER FOUND SW CONTAMINATED AND SAME CLEANED. IND NORMAL.MM 32-61-71. 2L73 4F RTA3WE 20030904002022003090400202NM 2003 9 4 DHL2003747008 120030626A3260106122615 DOWNLOCK SENSOR BOEING727 727224 1384076NM RT MLG FAULTY A DHLAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01747DH 22253 WHEN LANDING GEAR LOWERED, RIGHT GEAR RED LIGHT ILLUMINATED WITH RIGHT GEAR GREEN LIGHT OUT. SECONDARY MAIN GEAR POSITION INDICATOR GREEN LIGHTS BOTH ON. COMPLETED ABNORMAL PROCEDURES PER AOM 6.2.69. REPLACED RIGHT GEAR DOWN LOCK SENSOR. OPS NORMAL IAW MM 32-32-0. OK FOR SERVICE. 2L73 4F A3WE 20030905000042003090500004SO 2003 9 5 LR7A03051 120030725A5312 WEB LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5315 FOUND RH FS 924 BULKHEAD LOWER WEB CRACKED APPROX 2.0 IN. AT RBL 65, WL 200. REPLACED WEB IAW SRM SMP 583 51-60 AND 51-70. NR 2008. 2H74 4T A1SO 20030905000112003090500011SO 2003 9 5 LR7A03058 120030725A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT CARGO DOOR FS 1023 SKIN DENTED AT RBL 20. REPAIRED IAW SRM SMP 583 51-140-12. NR 2101. 2H74 4T A1SO 20030905000152003090500015SO 2003 9 5 LR7A03062 120030725A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT CARGO DOOR FS 990 SKIN DENTED AT BL 0. REPAIRED IAW SRM SMP 583 51-140-12. NR 2105. 2H74 4T A1SO 20030905000172003090500017SO 2003 9 5 LR7A03064 120030725A53203759441R CHANNEL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND RH FS 617 SPLICE FITTING (CHANNEL) CRACKED AT RBL 20, WL 283. REPLACED CHANNEL IAW SRM SMP 583 51-10 PG 4. NR 2109. 2H74 4T A1SO 20030905000202003090500020SO 2003 9 5 LR7A03067 120030725A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND RT FS 597 'L' BRACKET CRACKED AT RBL 22, WL 285. REPLACED BRACKET IAW SRM SMP 583 51-60 AND 51-70. NR 2112. 2H74 4T A1SO 20030905000342003090500034SO 2003 9 5 C2XA03TY145 120030904A532014521725613 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030905000352003090500035SO 2003 9 5 C2XA03CL150 120030823A3350145C338296B CONTROL MODULE EMB 145 EMB145LR 3260212SO CABIN DEFECTIVE A C2XAK NONE J WARNING INDICATION UKUNKNOWN 1 SW2711544 145557 IAH FLT NR 2849 THE CREW REPORTED THE EMERGENCY LIGHTS INDICATE "NOT ARMED" ON EICAS WHEN THEY ARE ACTUALLY IN ARMED POSITION (INTERMITENTLY). MAINTENANCE REMOVED AND REPLACED LIGHTING CONTROL MODULE. OPERATIONAL CHECKS GOOD 2L72 4T RTT00011AT 20030905000372003090500037SO 2003 9 5 C2XA03IA081 120030808A27403621001009 CONTROL UNIT EMB 145 EMB145LR 3260212SO HORIZ STAB FAULTY A C2XAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW2713914 145430 IAH - FLT 2546 - CREW REPORTED THAT THE PITCH TRIM 1 AND 2 FAIL MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU). THE AIRCRAFT WAS OPERATIONALLY TESTED AND APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905000422003090500042SO 2003 9 5 C2XA03SH304 120030828A533014535010003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE FUSELAGE SKIN BETWEEN FRAMES 67 AND 71 STRINGERS 15R AND 20L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN IAW EC 5330-01065. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905000462003090500046SO 2003 9 5 C2XA03SH267 120030811A531014525480003 DOOR FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV-DURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM BETWEEN FRAMES 65 AND 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030903001772003090300177 2003 9 3 AALA20030787 420030723A3442 TRANSCEIVER BOEING777 777223 1385213NM WEATHER RADAR FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21754AN 30262 WEATHER RADAR INOPERATIVE, CALLED DISPATCH TECH AND DISCUSSED SOLUTIONS. CYCLED E6 AND E/6 CIRCUIT BREAKER, NO HELP. STATUS WXR SYSTEM DISPLAYED. FOUND RIGHT WXR FAIL EXISTS FAULTS. REPLACED RT WXR TRANSCEIVER (P/N TRA7133), OPS CHECKS NORMAL. (M) 2L72 4F RTT00001SE 20030903001922003090300192NM 2003 9 3 AALA20030599 120030527A2520 RECEPTACLE BOEING777 777223 1385213NM CABIN CONTAMINATED A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21777AN 29585 FLT 153 - EN ROUTE ORD-NRT, POWER CORD PLUGGED INTO POWER PORT AT SEAT 3H BEGAN SMOKING. CORD UNPLUGGED AND STOPPED SMOKING. POWER PORT POWER WAS SHUTOFF. LANDED NRT WITHOUT INCIDENT. POWER PORT AT 3H FOUND TO BE WET, DRIED BY CLOTH. RE-ESTABLISHED POWER OT PORTS. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030903002252003090300225EA 2003 9 3 QXEA200300965 120030810A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 PDX- LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA R-53-100B AND REO 670-53-11-011. 2L72 4F RTA21EA 20030904000202003090400020EU 2003 9 4 DHL2003362011 120030708A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 1 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01362DH 84 ENGINE NR 1 FIRE DETECT LOOP (A) FAULT LIGHT ILLUMINATED IN FLIGHT. ABNORMAL PROCEDURE COMPLETED. UNABLE TO DUPLICATE CONDITION ON GROUND. REPOSITIONED LOOP 23WD. CLEANED ALL CONNECTORS. GROUND CHECKED NORMAL IAW M/M 26-12-00. 2L72 4F RTA35EU 20030904000412003090400041EA 2003 9 4 SWIA200312278 120030710A53206013501252 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 AFT FUSELAGE, CLIP CRACKED AT FS 625.0; STR 14R. DISCOVERED DURING C-CHECK, CLIP REPLACED IAW CRJ SRM 51-42-06. P/N: 601-35012-52 2L72 4F RTA21EA 20030904002062003090400206SO 2003 9 4 SWIA200312181 120030713A27223081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER FAULTY A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07226SW7912 7912 120296 ON CLIMBOUT, RIGHT RUDDER TRAVEL RESTRICTED PAST FIRST 20 DEGREES. PER QRH, TURNED BLUE RUDDER SYSTEM SWITCH OFF, PROBLEM CEASED. RETURNED TO FIELD UNEVENTFULLY.INSTALLED SERVICEABLE ACTUATOR IAW EMB120 MM 27-22-02. OPS AND LEAK CHECKS GOOD. 2L72 4T RTA31SO 20030905000072003090500007SO 2003 9 5 LR7A03054 120030725A5230 WEB LKHEED382 382G 526414USO CARGO DOOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5212 FOUND AFT CARGO DOOR FS 869 BULKHEAD WEB CRACKED AT LBL 6, WL 195. REPAIRED IAW SRM SMP 583-51-140-17. NR 2025. 2H74 4T A1SO 20030905000102003090500010SO 2003 9 5 LR7A03057 120030725A5312 PRESSURE PANEL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND LMLG FS 517 WEB CRACKED AT LBL 61, WL 160 APPROX 1.5 IN. REPAIRED IAW LAC MEA 382-53-03-057. NR 2092. 2H74 4T A1SO 20030905000162003090500016SO 2003 9 5 LR7A03063 120030725A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND LH BRACKET ATTACHMENT FOR PRESSURIZED FAIRING CRACKED FS 597-617, LBL 18, WL 283. REPLACED BRACKET IAW SRM SMP 583 51-60 AND 51-70. NR 2107. 2H74 4T A1SO 20030905001012003090500101SO 2003 9 5 C2XA03SH305 120030828A532014522459003 ANGLE EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030905001042003090500104SO 2003 9 5 C2XA03BT080 120030812A3350110049 BATTERY PACK EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713929 145009 EWR---CO2024, CREW REPORTED, EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS IAW EMB145 MM 33-50-04. OPS CHECKED GOOD. EMERGENCY LIGHT BATTERY PACK S/N REMOVED: [1]72619 [2]68594 [3] 68911 [4] 68902). AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030905001162003090500116NM 2003 9 5 DL767030640 120030713A2597 WIRE HARNESS BOEING767 767232 1385132NM CABIN CHAFED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27101DA 22213 FOUND LEFT AFT CHILLER WIRE HARNESS BURNT THROUGH DUE CHAFFING ON CHILLER RACK FRAME. SECURED HARNESS ASSY AND PULLED C/B'S. VERIFIED NO POWER TO HARNESS ASSY. WILL NEED WIRE HARNESS W284 REF IPC 25-33-02-01. ALSO WILL NEED DISCONNECT D2650DPN 014206555. TMC NOTIFIED FOR POSSIBLE ENGINEERING REROUTING/REPAIR OF HARNESS. FWD TO MCO. 2L72 4F RTA1NM 20030905001172003090500117NM 2003 9 5 DL76L030642 120030714A5753 SKIN 015T141585 BOEING767 767332 1382001NM T/E FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27178DN DL6 25143 LT WING INBOARD AFT FLAP WAS FOUND WITH NUMEROUS DISBONDS. RESKINNED IAW ER/A 423259-14. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F RTA1NM 20030905001602003090500160NM 2003 9 5 DL73S030674 120030718A531565C345379 FLOORBEAM BOEING737 737232 1384475NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 DURING ACCOMPLISHMENT OF EO 03-062982-03AD, MTC ADDED ADDITIONAL FASTENER HOLES THROUGH THE UPPER CAP AND SPLICE ANGLES OF THE CENTER WING BOX FLOORBEAMS FROM BS 650 TO 675 AT BL 0.07. REPAIR PER ER/A 385423-14AD. 2L72 4F RTA16WE 20030905001632003090500163NM 2003 9 5 USAASB03139 120030814A33209781 BALLAST BOEING737 7374B7 1384702NM CABIN FAILED A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 EA19436US 24558 CLT - FLT 828 - EN ROUTE FROM IAH-CLT, CAPTAIN REPORTED A STRONG ELECTRICAL ODOR IN THE MID CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE 'CABIN SERVICE LT O/H LIGHTING' CIRCUIT BREAKER POPPED. CIRCUIT BREAKER WOULD NOT RESET. SUSPECT OVERHEAD LIGHTING BALLAST SHORTED. RELEASED AIRCRAFT ON MEL 33-2. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD LIGHTING BALLAST AT SET ROW 20, LEFT SIDE. OPERATIONAL CHECK GOOD. CLEARED MEL 33-2. (M) 2L72 4F RTA16WE 20030905001742003090500174EA 2003 9 5 ASOA03372 120030815A52102R5206B MOTOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 FLT 4792 - DURING A GROUND INSPECTION IN ORD, THE PASSENGER DOOR WAS BINDING WHEN OPENED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR POWER ASSIST MOTOR, AND CLEANED DEBRIS FROM THE RETRACT MECHANISM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030905001762003090500176EA 2003 9 5 ASOA03374 120030815A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20030905001812003090500181EA 2003 9 5 ASOA03367 120030809A5320MM67075562005 SUPPORT BRACKET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11719EV 10099 DURING HANGAR MAINTENANCE IN MCN, THE LEFT HYDRAULIC FIREWALL SHUT OFF VALVE SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT HYDRAULIC FIREWALL SHUTOFF VALVE SUPPORT BRACKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030905001932003090500193WP 2003 9 5 AALA20030456 120030413A216060714811 SENSOR DOUG DC9 DC982 3022082WP A/C BAY DEFECTIVE A AALAO OTHER N FALSE WARNING CLCLIMB 1 SW21295AA 49307 DFW - FLT 1698 - EN ROUTE DFW-IAD, ON CLIMB-OUT AT 24,000 FEET, TAIL COMPARTMENT TAIL HIGH LIGHT ILLUMINATED. FOLLOWED CHECKLIST AND LIGHT EXTINGUISHED. LIGHT ILLUMINATED AGAIN WHEN POER ADVANCED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED HIGH AND LOW TEMPERATURE SENSORS FOR LEFT BLEED AIR LEFT AIR CONDITIONING PACKS. RAN PACKS ON APU AIR, ENGINE BLEED AIR ON BOTH. CHECKED FOR PNEUMATIC AIR LEAKS NONE FOUND. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905001992003090500199WP 2003 9 5 AALA20030559 120030511A2120 CLAMP DOUG DC9 DC983 3022083WP A/C BAY DEFECTIVE A AALAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW21438AA 49456 DFW - FLT 1035 - EN ROUTE DFW-AUS - MASTER WARNING AND ASSOCIATED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. DID IMMEDIATE ACTION ITEMS AND LIGHT EXTINGUISHED WHEN AIR CONDITIONING SUPPLY SWITCHES MOVED TO HIGH PRESSURE BLEED OFF. RETURNED AND LANDED DFW WITHOUT INCIDENT. INSTALLED NEW HEAT EXCHANGER CLAMP. LEAK CHECKED GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030905002062003090500206SO 2003 9 5 C2XA03SH300 120030827A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030903002342003090300234EU 2003 9 3 03240318 120030828A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27318UE 41041 DURING MAINTENANCE INSPECTION THE FORWARD EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4T RTA41NM 20030903002362003090300236EA 2003 9 3 03233649 120030821A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27649BR 7414 DURING MAINTENANCE THE LT FWD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULBS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICEDCN#148250 2L72 4F RTA21EA 20030903002602003090300260SO 2003 9 3 C2XA03SH314 120030901A531014525480003 DOOR FRAME EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030903002642003090300264SO 2003 9 3 C2XA03SH312 120030830A711014576518001 STRINGER EMB 145 EMB145ER 3260211SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK NR 1 LOWER COWLING, OUTBOARD STRINGER WAS FOUND TO CHAFFED NEAR AFT RIB. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030903002662003090300266SO 2003 9 3 C2XA03TY133 120030818A553014540881001 HOUSING EMB 145 EMB145LR 3260212SO VERTICAL STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND VERTICAL STAB SPHERICAL BEARING HOUSING. MAINTENANCE CLEANED AND REPAIRED THE HOUSING IAW EXPRESS JET EC 5510-01061 AND EMB MM 51-50-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030903002672003090300267SO 2003 9 3 C2XA03SH306 120030828A532014522460013 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030904001002003090400100EA 2003 9 4 QXEA200301012 120030817A2425 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09607QX 10024 SEA- ON FLIGHT 2502 GENERATOR 2 OFF MESSAGE. PERFORMED CHECKLIST. RESET AUTO-MESSAGE DID NOT PRESIST. CYCLED ON AND OFF. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030904001602003090400160WP 2003 9 4 DHL2003873612 120030706A5313S1616757 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FUSELAGE TAIL SECTION L-17L CRACKED 2.000, STA 1771 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON ON FUSELAGE TAIL SECTION, STA 1771 IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030902000722003090200072EU 2003 9 2 XNOA01135 120030624A3244 TIRE AIRBUS300 A300B4203 3930306EU MLG FAILED A XN0AA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 GL23473AS 203 AFTER T/O TOWER SAID LT MLG TRAILING SMOKE-NO ABNORMAL INDS ON BRAKE TEMP GUAGES. THEN TWR ADVISED THEY FOUND TIRE DEBRIS ON RWY-HAD NOT RETRACTED GEAR AS PRECAUTION. PHONE PATCH WITH CO. THEY REQUESTED US TO RETURN TO CLT. JETTISONED 15000 KILOS OF FUEL. REMOVED & REPLACED NR 5 & 6 MLG TIRES IAW A300 MM 12-37-32. NO OTHER DEFECTS NOTED. 2L72 4F RTA35EU 20030902001052003090200105SO 2003 9 2 CHQA000413 120030701A3040 WASHER EMB 145 EMB145 3260210SO HEAT CONTROLLER MISSING A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11294 SMOKE VAPOR OR TOXIC/NOXIOUS FUMES IN COCKPIT AND/OR CABIN. RETURNED TO FIELD IN IND TO "HOT CHARRED" ODOR IN COCKPIT. MTX DETERMINED SOURCE OF ODOR TO BE A MISSING WASHER ON THE LEFT WINDSHIELD HEAT CONTROLLER. WHEN THE W/S HEAT WAS CYCLING ON, THE ABSCENCE OF THE METAL WASHER CAUSED THE SURROUNDING PLASTIC TO HEAT UP AND MELT LEADING TO THE ODOR DESCRIBED. 2L72 4F RTT00011AT 20030902001062003090200106EU 2003 9 2 YT2R110913 120030322A64103551409105601 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED E YT2RO OTHER O OTHER NRNOT REPORTED 1 WP01211FN 2174 TAIL ROTOR LAMINATES, PART REMOVED, DUE TO CRACKING. 1G71 3U3 U H9EU E19EU 20030902001832003090200183NM 2003 9 2 03FDEA00941 120030619A5511ALC8100 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 SNRM N0824 - HOR STAB LT UPPER SPAR CAP NR 36L BARREL NUT BORE CORROSION FOUND BEYOND EO 1-5510-7-5000 B PT1 LIMITATION. CORRECTIVE ACTION: SNRM N0824 - HOR STAB LH UPPER SPAR CAP NR 36L BARREL NUT BORE REPAIR CARRIED OUT EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT REWORK/REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030724001162003072400116NM 2003 7 24 AWXA200300672 120030519A5712654544555 RIB BOEING737 73733A 1384673NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT WING AFT RIB, WBL 135.5. MAINTENANCE CUT OUT CRACKED LT WING AFT RIB AT WBL 135.5; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF RIB AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW AWA ER 03-5723-03149-TB1. 2L72 4F RTA16WE 20030724001192003072400119NM 2003 7 24 AWXA200300675 120030506A532069165096 ANGLE BOEING737 737330 13844BJNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK .125 INCH CRACK WAS FOUND ON LOWER ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED LOWER ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-16509; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 10 & 11. 2L72 4F RTA16WE 20030724001222003072400122NM 2003 7 24 AWXA200300678 120030507A53206546877103 WEB BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON SHEAR BEAM WEB OF STR 18A LT, AFT OF BS 706 FRAME TRUNNION BEAM SUPPORT FITTING IN FORWARD OUTBOARD CORNER. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR ANGLE PER DWG 65C29228; INSTALLED REPAIR PARTS IAW EO 53-14-09. 2L72 4F RTA16WE 20030724001252003072400125NE 2003 7 24 AWXA200300736 220030625A75301685MK7 ACTUATOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE FAULTY A AWXAO OTHER MYJOVER TEMP ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 WP28645AW33369191 238 V0066 AT CRUISE FL 360, NR 2 ENG COMPRESSOR VANE ECAM MSG, AT FL 290 NR 2 ENG STALLED. SHUTDOWN ENG, EMERGENCY EQUIP TO STANDBY. LANDED, TAXIED TO GATE. REPORT INDICATED NR 2 ENG OVERTEMP 663'C APPX 7 SEC. MX INSPECTED INTERMEDIATE PRESSURE CHECK VALVE, FAULT ISOLATION TEST OF FULL AUTHORITY DIGITAL ENG CONTL CHANNELS 1 & 2, NO DEFECTS. PERFORMED BORESCOPE INSP OF HOT SECTION & HPC, NO DEFECTS. PERFORMED WINDMILLING INSP, NO DEFECTS. COMPLIED WITH BURNER PRESSURE SENSE LINE LEAK CHECK. R&R 10TH STAGE HPT AIR CONTROL VALVE. PERFORMED HPC BLEED VALVE FUNCTIONAL TEST, FOUND VALVE FAULTY, R&R HPC BLEED VALVE SOLENOID. REPLACED VSV ACTUATOR. PERFORMED POWER ASSURANCE RUN & ACCEL/DECEL, ALL NORMAL. 2L72 4F4 FRTA28NM E311NE 20030724001282003072400128NM 2003 7 24 DL757030576 120030620A5330143N31211 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 THE FUSELAGE SKIN SUFFERED A LIGHTNING BURN AT FS 724 AND STRINGER 1. THE DAMAGE WAS REMOVED WITH A CUTOUT THROUGH THE SKIN AND UNDERLYING DOUBLER. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385154-14, REV A. 2L72 4F RTA2NM 20030724001302003072400130NM 2003 7 24 DL757030578 120030620A5330143N33203 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 THE FUSELAGE SKIN WAS FOUND WITH A DENT AND GOUGE NEAR AN EXISTING SKIN DOUBLER REPAIR BETWEEN FS 600 & 620 AND BETWEEN STRINGERS 16L & 17L. THE DAMAGE AND THE EXSITING DOUBLER REPAIR WERE REMOVED WITH A SINGLE 22 X 8.8 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385158-14, REV A. 2L72 4F RTA2NM 20030721001212003072100121 2003 7 21 SWAA031485 420030707A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030722000482003072200048 2003 7 22 SWAA031506 420030707A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20030722000852003072200085EU 2003 7 22 AWXA200300785 120030611A5320D5348002069601 WEB AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK A 4.75 INCH CRACK WAS FOUND ON FLOOR WEB BETWEEN FR 68-69, Y1270. MAINTENANCE REMOVED DAMAGED FLOOR WEB BETWEEN FR 68-69, Y1270; FABRICATED A NEW REPLACEMENT FLOOR WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 21-22, FIG 8. 2L72 4F RTA28NM 20030723000232003072300023NM 2003 7 23 KPVA200330 120030701A3230XD4N RELAY DHAV DHC8 DHC8103 1386005NM MLG FAILED A KPVAO OTHER J WARNING INDICATION CLCLIMB 1 WP13807WP 023 'LDG GEAR INOP' CAUTION LIGHT ON AFTER GEAR SELECTED UP ON TAKEOFF. PERFORMED GEAR EXTENSION AND RETRACTINO CHECK NUMEROUS TIMES. COULD OT DUPLICATE DISCREPANCY. AS PRECAUTIONARY MEASURE, REMOVED AND REPLACED RELAYS 3261-K4, 3261-K5, 3261-K6 AND 3261-K7 IAW SB 8-32-7, PAR N, PAGE 10, DHC 8 WIRING DIAGRAME 32-30-00, PATE 9. SWING GEAR,OPS CHECK GOOD IAW DHC 8 MM 32-30-00 PATE 204-206. POST MAINTENANCE CHECK FLIGHT SATISFACTORY, NO CAUTION LIGHTS. (M) 2H72 4T RTA13NM 20030723000552003072300055NM 2003 7 23 TSAA0353140 120030505A5310 SHEAR TIE BOEING737 73725A 1384481NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DISCOVERED A DAMAGED SHEAR TIE LOCATED AT BS 360, BETWEEN STRINGER 14 AND 15 RIGHT. CUTOUT DENTED PORTION. FABRICATED A NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-4, FIGURE 10. (M) 2L72 4F RTA16WE 20030723001192003072300119NM 2003 7 23 DL73S030508 120030530A53116546541504 FRAME BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 MTC FOUND CRACKS IN THE FRAME AT S6L, 3L, 2L, 1, 2R, AND 3R EXTENDING FROM THE STRINGER PASS THRU CUTOUTS. THE CRACKS WERE CUTOUT AND A REPAIR SIMILAR TO B737-200 SRM 53-10-04, F14, WAS INSTALLED TO EXTEND FROM O/B OF STR 6L TO O/B OF STR 4R. FUSELAGE SKIN WAS CUT AT EACH STRINGER/FRAME INTERSECTION AND STRINGERS 6L THRU 4R WERE CUT AND SRM STYLE REPAIRS WERE INSTALLED TO PROVIDE ACCESS FOR INSTALLATION OF FRAME REPAIR PER DAL ER/A 384937-14. 2L72 4F RTA16WE 20030723001202003072300120NM 2003 7 23 DLM90030511 120030604A2420 GENERATOR 1B1895 DOUG MD90 MD9030 3023690NM LEFT INOPERATIVE A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO27914DN 085C0132 53394 SHORTLY AFTER T/O L GEN OFF MSG AND L AC POWER FAULT MSG APPEARED ON OAP. ISOLATED LT GEN PER CHECKLIST AND RETURNED TO SLC SENCE APU WAS ALSO INOP. STATUS MSG SHOWED L ELEC SYSTEM FAIL. REPLACED LEFT GEN CONVERTER RAN ENG GEN OPS NORMAL OK FOR SVC. 2L72 4F RTA6WE 20030724000442003072400044EU 2003 7 24 AWXA200300627 120030521A5320D5347047400390 PROFILE AIRBUS320 A320231 3930325EU PAX DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 MCN - MINOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON PROFILE AT STR 38 RT, JUST FORWARD OF FRAME 48. MAINTENANCE REMOVED DAMAGED PROFILE AT STR 38 RT, JUST FORWARD OF FRAME 48; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2-7 PG 7-22 & FIG 9-18 PG 23-36. 2L72 4F RTA28NM 20030724000502003072400050NM 2003 7 24 DL764030551 120030616A3350PAC5026 POWER SUPPLY BOEING767 767432ER 1385134NM SEAT 36G INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27827MH 29698 EMERGENCY LIGHTS AT SEATS 31-41 FG INOP. REPLACED EMERGENCY LIGHTS POWER SUPPLY LOCATED AT 36G AND OPS CHECK OK. PART BORROWED FROM AMERICAN AIRLINES. 2L72 4F RTA1NM 20030724000832003072400083NM 2003 7 24 DL73S030554 120030616A7500 DUCT BOEING737 737247 138448DNM PWA JT8 JT8D15 52051NE NR 2 ENGINE DAMAGED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27379DL47518 709195 23606 709195 NR 2 ENGINE OVERHEAT LIGHT ILLUM SHORTLY AFTER T/O EGT APPROX 620 FULL T/O POWER SETTING. RETARDED THROTTLE, LIGHT WENT OUT APPROACHING IDLE. REPLACED FLEX DUCT AND TWO LOWER FIRE LOOPS. 2L72 4F4 F A16WE E2EA 20030724001082003072400108NM 2003 7 24 DL733030568 120030621A3350 BULB BOEING737 737347 1384647NM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27303WA 23183 ON L/O FOUND EMERGENCY OVERHEAD PATH LIGHTING AT SEATS 23ABC AND 17D INOP. RELAMPED SAME, OPS CHECK NORMAL. 2L72 4F RTA16WE 20030724001232003072400123NM 2003 7 24 AWXA200300750 120030614A531565479601 FLOORBEAM BOEING737 7373Y0 1384671NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM AT BS 847 TO BS 865, RBL 21, WL 166. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM Z-ANGLE FROM BS 847 TO BS 865; FABRICATED A NEW REPLACEMENT FLOORBEAM Z-ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 2-5, 10-1 & 3 FIG 8. 2L72 4F RTA16WE 20030725000162003072500016NM 2003 7 25 DLM88030592 120030627A5754 SKIN 5922500510 DOUG MD88 MD88 3023688NM LT WING SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27901DE DL9 53378 NR 1 SLAT OUTER SKIN ASSEMBLY, XFS 155 TO XFS 168 REPAIR OF DAMAGE TO OUTER SKIN. REPAIRED PER ER/A 418073-14. 2L72 4F RTA6WE 20030725000212003072500021SO 2003 7 25 RAIA00304130 120030428A4950 O-RING EMB 145 EMB145 3260210SO BLEED SYSTEM LEAKING A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03809HK 145187 5286 DTW DURING TAKE-OFF NR 1 BLEED LEAK LIGHT CAME ON. MAINTENANCE DEFERRED PER MEL 49-52-2, SUBSEQUENTLY CLEARING DMI BY REPLACING O-RING IN LEFT BLEED LINE. 2L72 4F RTT00011AT 20030725000342003072500034EU 2003 7 25 RAIA00305145 120030519A33507012210 BULB AEROSPATR42 ATR42300 8680920EU EMERGENCY LIGHT BURNED OUT A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE 119 EMERGENCY EXIT LIGHT INOP ON STAIRS. REMOVED AND REPLACED LIGHT BULB. 2H72 4T RTA53EU 20030725000432003072500043WP 2003 7 25 NACA20030086 120030528A8200190255 REGULATOR DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 4 ENGINE MALFUNCTIONED A NACAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 AL031377K288 288 44596 P34219 NR 4 ENGINE WOULD NOT ENRICH AFTER WATER WAS SHUT OFF. REPLACED ADI REGULATOR, OPS CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20030725000482003072500048NM 2003 7 25 03FDEA00817 120030527A5310 CHANNEL BOEING727 727200 138407ENM LT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION LT WHEEL WELL BS 927-932 LBL 65 WL 188 STR 18A SHELF. REMOVED AND REPLACE SILL CHANNEL BS 870-936, WL 188, LBL 65 AT STR 18A PER SRM 51- 30-2, 51-30-5. 2L73 4F RTA3WE 20030728000032003072800003NM 2003 7 28 SWAA031576 120030717A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030728000112003072800011NM 2003 7 28 SWAA031630 120030721A32306544915 VALVE BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAK NONE J WARNING INDICATION TOTAKEOFF 1 SW29320SW 23341 AFTER TAKEOFF GEAR RETRACTED NORMALLY, WHEN GEAR HANDLE PLACED FROM UP TO OFF, RT MLG EXTENDED (BOTH RED AND GREEN LIGHTS) RETRACTED GEAR AGAIN, GEAR RETRACTED NORMALLY. REMOVED AND REPLACED RT MLG PRIORITY MODULAR VALVE PER MM. 2L72 4F RTA16WE 20030728000242003072800024 2003 7 28 SWAA031519 420030711A256561620468 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030728000312003072800031NM 2003 7 28 SWAA031591 120030717A3350BR2013 STRIP BOEING737 7375H4 138449DNM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS STRIP CRACKED AT ROW NR 2. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20030728000362003072800036NM 2003 7 28 SWAA031595 120030718A32601061226 SENSOR BOEING737 7373H4 1384600NM NLG FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SW29606SW 27926 AIR TURNBACK, DECLARED EMERGENCY, NOSE LANDING GEAR INDICATED UNSAFE. REMOVED AND REPLACED NOSE GEAR S846 LOCK SENSOR PER MM. 2L72 4F RTA16WE 20030728000452003072800045NM 2003 7 28 SWAA031602 120030720A2560P2070021 BATTERY BOEING737 7373Q8 1384670NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED A2 CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT STRAP BROKEN AND STATUS LIGHT ON STEADY. REMOVED AND REPLACED STRAP AND BATTERY PER MM. 2L72 4F RTA16WE 20030728000572003072800057 2003 7 28 SWAA031632 420030723A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29747SA 29799 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030728000592003072800059NM 2003 7 28 SWAA031634 120030723A335065C27093 RETAINER BOEING737 7373Q8 1384670NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS HOLDER CRACKED. REMOVED AND REPLACED LENS HOLDER PER MM. 2L72 4F RTA16WE 20030728000732003072800073NM 2003 7 28 SWAA031547 120030714A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 727E AND BS 7827D. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030722001372003072200137NM 2003 7 22 SWAA031436 120030629A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 20L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20030724000462003072400046NM 2003 7 24 DLM88030546 120030613A3260 SENSOR DOUG MD88 MD88 3023688NM NLG UNSERVICEABLE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27955DL 49886 AFTER TAKEOFF, NOSE GEAR LIGHT REMAINED RED WITH GEAR HANDLE UP. GEAR LOWERED NORMALLY PER POM PROCEDURES. ADJUSTED NOSE GEAR UP POSITION SENSOR. 2L72 4F RTA6WE 20030724000972003072400097EA 2003 7 24 COMA0360308 120030702A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01957CA 7109 FLIGHT 5562 RECEIVED A RIGHT THRUST REVERSER UNLOCK CAUTION DURING TAKEOFF ROLL, ABORTED AND RETURNED TO THE GATE. DEFERRED THE RIGHT THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20030725000332003072500033EU 2003 7 25 RAIA00305147 120030520A3397 CONNECTOR AEROSPATR72 ATR72202 8680940EU EMERGENCY LIGHT DIRTY A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03723TE 283 EMERGENCY LIGHT ON STEPS INOP. CLEANED CONNECTOR AT STEP LIGHTING. 2H72 4T RTA53EU 20030728000082003072800008NM 2003 7 28 SWAA031531 120030711A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030728000232003072800023GL 2003 7 28 SWAA031553 220030713A7530301792702 ACTUATOR BOEING737 7375H4 138449DNM CFMINTCFM56 CFM563B1US GL NR 2 ENGINE FAULTY A SWAABA EMER. DESCENT UNSCHED LANDING JM WARNING INDICATION OVER TEMP TOTAKEOFF 1 SW29503SW 24180 DIVERSION, NR 2 ENGINE EGT EXCEEDANCE. FOUND, VBV MASTER ACTUATOR STUCK IN OPEN POSITION. REMOVED AND REPLACED VBV MASTER ACTUATOR AND VBV MOTOR PER MM. 2L72 4F4 FRTA16WE E2GL 20030728000252003072800025 2003 7 28 SWAA031520 420030711A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030728001082003072800108NM 2003 7 28 SWAA031625 120030721A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030728001102003072800110NM 2003 7 28 SWAA031627 120030722A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030904001992003090400199NM 2003 9 4 C1HA200375001 120030823A5753 FLAP BOEING727 727225 1384077NM LT WING DELAMINATED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15675MG 21450 LEFT OUTBOARD FORE FLAP DELAMINATED ON OUTBOARD END, UNDER SIDE. 2L73 4F A3WE 20030905002132003090500213SO 2003 9 5 C2XA03TY132 120030818A532014522460015 GUSSET EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030905002182003090500218SO 2003 9 5 C2XA03CL139 120030807A2560P2070005120 CHARGER EMB 145 EMB145ER 3260211SO CABIN FAULTY A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2712934 145019 CLE FLIGHT NR 2158 THE CREW REPORTED A BURNING ODOR COMING FROM THE FORWARD CABIN FLASHLIGHT CHARGING BRACKET. MAINTENANCE INSPECTED AND REPLACED THE FORWARD F/A FLASHLIGHT BASE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030905002272003090500227SO 2003 9 5 C2XA03TY122 120030811A534714532605015 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION SEAT TRACK RW3 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030904000862003090400086NM 2003 9 4 QXEA200300987 120030810A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 7 SEAT TRACK HAS NUMEROUS AREAS OF PITTING CORROSION FROM STATIONS X215.500 TO X234.500. REPAIRED IAW DHC-8 RD 8-53-1102, SRM 51-40-00 AND 51-20-16. 2H72 4T RTA13NM 20030904000872003090400087NM 2003 9 4 QXEA200301013 120030822A2612 CONNECTOR DHAV DHC8 DHC8202 2809007NM FIRE LOOP DIRTY A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09352PH 494 PDX- NR 2 CHANNEL B FIRE DETECTION LOOP WILL NOT TEST. CLEANED BOTH CONNECTOR PLUGS ON B LOOP HARNESS IN NACELLE AND AT CONTROLLER IN CLOSET. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904001232003090400123NM 2003 9 4 DL757030608 120030703A5330143N31711 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27686DA 27589 FUSELAGE SKIN FS 840 STRG 9L-10L, LIGHTNING STRIKE REPAIR, AN EXISTING TEMPORARY DOULBER FOR A LIGHTNING STRIKE DAMAGE WAS REMOVED FROM THE FUSELAGE SKIN AT FS 840 BETWEEN STRINGERS 9L & 10L. THE DAMAGE CUTOUT WAS INSPECTED AND OVERSIZED AND THE EXISTING REPAIR FASTENER HOLES INSPECTED AND OVERSIZED. THE AREA WAS REPAIRED WITH AND EXPANDED ALUMINUM REPAIR DOUBLER PER ER/A 385299-14. 2L72 4F RTA2NM 20030904001462003090400146CE 2003 9 4 DXTA200300041 120030603A2697 GROUND WIRE CESSNA560 560XL 2076702CE LT ENGINE DAMAGED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07690QS 5605090 LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMB THRU FL260 WITH ENGINE/WING ANTI-ICE ON. REDUCED POWER TO 72 PERCENT ON EFFECTED ENGINE AND LIGHT EXTINGUISHED. REMOVED AND REPLACED LT ENGINE FIRE LOOP WITH A NEW PART IAW CESSNA 560XL MAINTENANCE MANUAL CHAPTER 26-11-01. PERFORMED ENGINE RUN AND LT FIRE DETECT ILLUMINATED AFTER 3 MIN AT POWER. CHECKED ENGINE FOR BLEED AIR LEAKS, NONE NOTED. PROCEEDED TO TROUBLESHOOT LT ENGINE FIRE DETECT SYSTEM AND FOUND A BAD GROUND FROM RESISTER R2019 TO GND BLOCK XZ004 PIN B. REPAIRED GND AND CHECKED RESISTANCE ON RESISTORS RZ018 AND RZ019 BOTH CHECKED AT 99.9 OHMS. RUN LT ENGINE AT VARIOUS POWER SETTINGS FOUR 15 MIN, NO DEFECTS NOTED. 2L72 4F RTA22CE 20030904001822003090400182WP 2003 9 4 AALA20030665 120030615A2150 A/C PACK DOUG DC9 DC983 3022083WP A/C BAY OVERHEATED A AALAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21972TW 53622 DTW - FLT 1055 - EN ROUTE DTW-STL, CABIN FILLED WITH SMOKE DURING CLIMB THROUGH 28,000 FEET. FLIGHT ATTENDANT HEARD SEVERAL BOOMS RIGHT BEFORE SMOKE BEGAN. RIGHT PACK TURNED OFF AND SMOKE CLEARED. RETURNED AND LANDED DTW WITHOUT INCIDENT. DETERMINED SMOKE WAS FROM A PACK OVERHEAT. RAN ENGINES AND PACKS FOR BLEED SHIFT AND OVERHEAT. INSPECTED PACKS AND DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030904001902003090400190WP 2003 9 4 AALA20030721 120030707A3397 WIRE HARNESS DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21562AA 49344 DFW - SEAT MOUNTED EMERGENCY LIGHT AT 32A INOPERATIVE. REPLACED HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030905001712003090500171WP 2003 9 5 AALA20030486 120030422A2150 A/C PACK DOUG DC9 DC982 3022082WP A/C BAY DIRTY A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21245AA 49257 ORD - FLT 386 - EN ROUTE ORD-LGA, A THICK HAZE/SMOKE IN CABIN AND COCKPIT WAS NOTED. PASSENGERS COMPLAINED ABOUT BEING ILL FROM SMOKE, RAN CHECKLIST. RETURNED ORD AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN OUT, TEST NORMAL DURING CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905002212003090500221SO 2003 9 5 C2XA03CL141 120030808A3260 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO LANDING GEAR MALFUNCTIONED A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW2713929 145009 CLE FLIGHT NR 2227 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER RETRACTION UNTIL ABOUT 300AGL. THE GEAR DID NOT RETRACT. MAINTENANCE INSPECTED AND COULD NOT FIND ANY DEFECTS. ALL 5 WEIGHT ON WHELLS PROXIMITY SWITCHES WERE REPLACED FOR PRECAUTIONARY REASONS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030908001202003090800120EA 2003 9 8 SWIA200312129 120030615A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52. 2L72 4F4 FRTA21EA E15NE 20030908001222003090800122SO 2003 9 8 SWIA200312202 120030714A5753 FLAP TRACK EMB 120 EMB120ER 3260203SO T/E FLAP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07218SW 120287 RIGHT OUTBOARD FLAP, OUTBOARD FLAP TRACK ON WING, IS CRACKED AT BOTTOM AFT RADIUS. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED RIGHT OUTBOARD FLAP OUTBOARD AFT TRACK IAW EMB 120 MM 57-53-04. PN ON 120-33047-004. 2L72 4T RTA31SO 20030908001232003090800123EA 2003 9 8 SWIA200312203 120030719A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07438SW4663 4663 7574 STAB TRIM AND MACH TRIM WILL NOT ENGAGE ON GROUND. REMOVED AND REPLACED HSTA & MCU IAW MM 27-40-00. OPS CHECK OK.MCU P/N: 7062-3 S/N OFF: 829. 2L72 4F RTA21EA 20030728001252003072800125WP 2003 7 28 DHL2003807012 120030708A21612275020 INDICATOR DOUG DC8 DC873F 302199FWP TEMP CONTROL FAULTY A DHLAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01807DH 45990 LEFT PACK OPERATES NORMALLY, BUT INTERMITTENTLY BEGINS TO OVER TEMP RAPIDLY WITH A CORRESPONDING BURNING SMELL NOTICED IN THE COCKPIT. PACK EVENTUALLY HAD TO BE SHUT DOWN. REMOVED AND REPLACED LEFT PACK MIX VALVE INDICATOR. OPS CHECKED GOOD PER 21-61-0. 2L74 4F RT4A25 20030728001282003072800128NM 2003 7 28 SWAA031432 120030629A27823820001001 ACTUATOR BOEING737 7377H4 1384404NM L/E FLAP FAILED A SWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29756SA 27872 AIR TURNBACK, DECLARED EMERGENCY, L/E DEVICES WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 L/E FLAP ACTUATOR PER MM. 2L72 4F RTA16WE 20030728001342003072800134EA 2003 7 28 REXA03003 120030630A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FAULTY A REXAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SO258673D 7673 CARGO SMOKE WARNING ON APPROACH, FIRE EXTINGUISHERS ACTIVATED. FOUND NR 1 CARGO SMOKE DETECTOR FAILED. REMOVED AND REPLACED DETECTOR, BOTTLES, AND SQUIBS. (M) 2L72 4F RTA21EA 20030729000012003072900001EA 2003 7 29 03188669 120030707A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING MAINTENANCE INSPECTION, AN INTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000062003072900006EA 2003 7 29 03199625 120030718A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27625BR 7214 DURING MAINTENANCE INSPECTION, THE FWD RT WING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030729000102003072900010EA 2003 7 29 03188653 120030707A324250105201 BRAKE ASSY CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A VTZAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA27653BR 7438 DURING TAKE-OFF ROLL, THE CREW REPORTED THAT HE HAD NO DIRECTIONAL CONTROL, THAT THE AIRCRAFT TURNED TO THE LEFT WITH FULL RIGHT PEDAL. THE TAKE-OFF WAS REJECTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 2 MLG BRAKE ASSY. 2L72 4F RTA21EA 20030729000282003072900028NE 2003 7 29 03193698 220030712A72506047T63P04 CARBON SEAL GE CF34B CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE LEAKING A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27698BR279 873761 7799 873761 DURING CRUISE CREW REPORTED SMOKE IN THE FLIGHT DECK AND CABIN. MAINTENANCE PERSONNEL PERFORMED A BORESCOPE INSPECTION AND FOUND NO DISCREPANCIES, DURING AN EXTERNAL VISUAL INSPECTION OF THE TURBINE SECTION THE NR 1 CARBON SEAL WAS FOUND TO BE LEAKING AND WAS REPLACED. A SATISFACTORY ENGINE RUN AND LEAK CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F4 FRTA21EA E15NE 20030729000352003072900035NM 2003 7 29 03195428 120030714A21505729C000002 A/C PACK DORNERDO32 DO328300 NM A/C BAY MALFUNCTIONED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27428FJ 3193 DURING CRUISE THE FLIGHT CREW REPORTED SMOKE IN THE COCKPIT. EMERGENCY WAS DECLARED FLIGHT. FLIGHT WAS DIVERTED TO RIC. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE PERSONNEL PERFORMED OPS CHECK LT PACK FOUND LT ENVIRONMENTAL CONTROL UNIT BAD UNIT WAS REMOVED AND REPLACED A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030729000392003072900039NM 2003 7 29 ZW0A0305803 120030702A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13726TW 30339 THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS AT THE R2 DOOR WERE ADJUSTED ACCOUNT DEFORMED. 2L72 4F RTA2NM 20030729000552003072900055EA 2003 7 29 QXEA200300839 120030630A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX - INSTALLATION OF DOUBLER FOR RE-INFORCEMENT OF THE LEFT SIDE REAR PRESSURE BULKHEAD WHERE EDP LINES PASS THROUGH. REPAIRED IAW REO 670-53-61-034 AND REO 29-08-B, ITEM 4 PAGE 9. 2L72 4F4 FRTA21EA E15NE 20030729000582003072900058NM 2003 7 29 QXEA200300845 120030719A243523088002A STARTER GEN DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A QXEAK NONE J WARNING INDICATION CRCRUISE 1 NM09358PH725 506 BOI-SUP-ON FLIGHT 2206 NR 2 DC GENERATOR CAUTION LIGHT ON ENROUTE. AS PER ABNORMAL CHECKLIST RESET WITH NO CHANGE. REMOVED AND REPLACED NR 2 DC STARTER GENERATOR. OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030729000692003072900069NM 2003 7 29 QXEA200300816 120030702A5541 RIB BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA RUDDER DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - TRAILING RUDDER HAS DAMAGE NINE RIBS DOWN FROM TOP OF TRAILING RUDDER. REPAIRED IAW HORIZON AIR EA 6-55-46. 2H72 4T4 TRTA13NM E00062EN 20030724001172003072400117NM 2003 7 24 AWXA200300673 120030506A5320692655552 ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK .1875 INCH CRACK WAS FOUND ON ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-26555; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 10 & 11. 2L72 4F RTA16WE 20030728000462003072800046 2003 7 28 SWAA031603 420030720A2565D31354 CLIP BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE RETAINING CLIP OUT OF ADJUST. ADJUSTED RETAINING CLIP PER MM. 2L72 4F RTA16WE 20030728000552003072800055NM 2003 7 28 SWAA031612 120030721A33506104789 BATTERY BOEING737 7372T4 1384492NM CARGO BAY DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED PM CHECK, FOUND AFT CABIN DOORS AND BOTH OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030908001442003090800144 2003 9 8 SWIA200312214 420030722A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAULTY A SWIAO OTHER N FALSE WARNING UKUNKNOWN 1 NM07589SW 7072 WINDSHEAR FAIL STATUS MSG ON EICAS FOLLOWED BY A TCAS FAIL. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW MM 27-35-1. OPS CHECK GOOD. SN OFF 149. 2L72 4F RTA21EA 20030908001462003090800146EA 2003 9 8 SWIA200312215 120030723A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07589SW6748 6748 7072 HSTCU CHANNEL 2 INOP.REMOVED AND REPLACED HSTCU. OPS CHECK GOOD. 2L72 4F RTA21EA 20030908001522003090800152 2003 9 8 SWIA200312227 420030803A2210 PIN EMB 120 EMB120ER 3260203SO AUTOPILOT SYS BACKED OUT A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07268UE 120207 AUTOPILOT DISCONNECTED IN FLIGHT WITH 'AUTOPILOT FAIL' ON MAP AND 'AP' ON AUTOPILOT CONTROL PANEL. WHEN AP DISCONNECTED, A/C FELT OUT OF TRIM IN ROLL. DISCONNECT OCCURED WITH FO FLYING. MEL 22-11-1A. FOUND PIN 12 AT J2 OF NR 2 AUTO PILOT COMPUTER RACK RECESSED. REPAIRED PIN NR 2 AUTOPILOT. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20030812000382003081200038EU 2003 8 12 BAQA088263 120030731A2842647511011 TRANSMITTER AEROSPAS355 AS355F1 8680810EU FUEL QTY READS LOW B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035797X4953 5182 FUEL QUANTITY FLUCTUATES BETWEEN FULL AND LESS THAN 20 PERCENT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030812000522003081200052SW 2003 8 12 HEEA088467 120030608A2435 COVER BELL 206 206L3 1182108SW STARTER GEN DENTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206LS8237 2047 51070 FOUND FAN COVER DENTED IN AND FAN BLADE BROKEN OFF. OVERHAULED BY ACCESSORY SHOP AND REPLACED DEFECTIVE PARTS AND RETURNED TO SERVICE. 1G71 3U H2SW 20030812000662003081200066SW 2003 8 12 HEEA088550 120030707A6710212001035101 FORCE GRADIENT BELL 412 412 1182202SW FLT CONTROLS WILL NOT TEST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 FORCE GRADIENT WILL NOT TEST BEFORE AND AFTERY CYCLE. SHOP REPAIR. 1G72 4U H4SW 20030812000702003081200070 2003 8 12 HEEA088572 420030731A34214020936903 GYRO BELL 412 412 1182202SW 3-AXIS IND INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 COPILOT RMI DROPS OFF LINE INTERMITTENTLY. SHOP REPAIR. 1G72 4U H4SW 20030805000942003080500094EA 2003 8 5 ASOA03280 120030701A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11904EV 7628 DURING A GROUND INSPECTION IN ATL, THE EXTERIOR RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR RIGHT FORWARD OVERWING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030806000082003080600008 2003 8 6 BAQA088141 420030624A34104027170904 INDICATOR BEECH 100 100BEECH 1152916CE HSI INACCURATE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03777GS33 B241 COURSE POINTER IS 5 DEGREES OFF. UNIT WAS JUST INSTALLED IN MAY AS AN EXCHANGE. PART ONLY LASTED 32.6 HOURS SPEX FILE: 00125687 REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20030806000472003080600047SO 2003 8 6 C2XA03SH222 120030717A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 DURING C-CHECK, THE LT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806000922003080600092SO 2003 8 6 C2XA03TY111 120030801A534714530658001 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION, SEAT TRACK RF1 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030806001412003080600141SO 2003 8 6 C2XA03CL124 120030714A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711565 145621 THE CREW REPORTED THE FIRST ROW OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE RESECURED WIRE, OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030806001642003080600164EU 2003 8 6 AWXA200300837 120030717A3240A25461103 SELECTOR AIRBUS320 A320232 3930326EU HYD SYSTEM BYPASSING A AWXAO OTHER OSJOTHER AFFECT SYSTEMS WARNING INDICATION TXTAXI/GRND HDL 1 WP28642AW28196 584 NORMAL AND PARKING BRAKES FAILED AT GATE. NORMAL BRAKES WERE APPLIED TO STOP AIRCRAFT, PARKING BRAKE WAS SET & STARTED TO SHUTDOWN NR 2 ENG WHEN AIRCRAFT STARTED TO ROLL. NORMAL BRAKES REAPPLIED & PARKING BRAKE RESET, AIRCRAFT STOPPED THEN STARTED TO ROLL AGAIN. NORMAL BRAKES APPLIED WITH NO EFFECT, RECYCLED PARKING BRAKE WHILE FIRST OFFICER SHUTDOWN NR 1 ENG. AIRCRAFT WAS CHOCKED AND STOPPED ROLLING. MAINTENANCE TROUBLESHOT THE BRAKE SYSTEM AND FOUND GREEN HYDRAULIC SYSTEM MIGRATING TO YELLOW HYDRAULIC SYSTEM. DURING T/S FOUND THERE WAS NO BRAKE PRESSURE WITH THE NR 1 ENG AND ONLY THE GREEN HYD SYS BEING USED. REMOVED AND REPLACED AUTOMATIC SELECTOR VALVE, OPERATIONAL AND LEAK CHECKS WERE GOOD. 2L72 4F RTA28NM 20030807000122003080700012NM 2003 8 7 USAASB03098 120030702A2710316X7X19MILW8342CONTROL CABLE BOEING737 7373B7 1384580NM AILERONS BROKEN A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19383US 22956 ON CLIMB-OUT FROM ATL, EN ROUTE TO CLT, CREW REPORTED THE AIRCRAFT REQUIRED EXCESSIVE AILERON TRIM. CREW NEEDED ALMOST FULL LEFT AILERON CONTROL WHEEL DEFLECTION TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT AILERON CONTROL CABLE ABSB 4 BROKEN IN RIGHT MAIN LANDING GEAR WHEEL WELL. ALSO, FOUND RIGHT AILERON CONTROL CABLE ABSA 4 FRAYED. REMOVED AND REPLCED BOTH CABLES PER JOB PROCEDUE CARD J3-10-27200 AND ACCOMPLISHED SATISFACTORY ADJUSTMENT/TEST. (M) 2L72 4F RTA16WE 20030807000492003080700049EA 2003 8 7 COMA0360345 120030803A2750860D10018ABCD COMPUTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS LDLANDING 1 SO01979CA491 7159 FLIGHT 5158 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20030728000632003072800063NM 2003 7 28 VNAA0307004 120030718A3240AC69965 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BRAKE SYSTEM FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07439JS3539 3057 DURING CLIMBOUT THE FLIGHT CREW RECEIVED AN EICAS MESSAGE FOR LOW EMERGENCY PARKING BRAKE ACCUMULATOR PRESSURE. AFTER CONFERRING WITH MAINTENANCE THE FLIGHT CREW RETURNED TO THE FIELD. THE LANDING WAS MADE WITHOUT INCIDENT. MAINTENANCE REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-43-02. FUNCTIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030728000722003072800072NM 2003 7 28 SWAA031546 120030713A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030728000872003072800087NM 2003 7 28 SWAA031641 120030723A2121215201 GASPER FAN BOEING737 7375H4 138449DNM E/E BAY FAILED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29525SW 26567 ELECTRICAL SMELL THROUGHOUT CABIN. FOUND GASPER FAN CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20030728000982003072800098NM 2003 7 28 SWAA031619 120030721A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030729000092003072900009EA 2003 7 29 03186701 120030705A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27701BR 7448 DURING MAINTENANCE INSPECTION, A SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED FOUR EMERGENCY FLOOR TRACK LIGHT STRIPS AND AN INVERTER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030729000752003072900075NM 2003 7 29 QXEA200300738 120030616A5270 PROXIMITY SWITCH BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR STUCK A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09546DS 4017 SUP - PDX - FLIGHT 2388 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE CREW RECEIVED A FORWARD BAGGAGE DOOR WARNING AND ALSO NOTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FORWARD PROXIMITY SWITCH STUCK. THE SWITCH WAS CLEANED AND LUBED, AND THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20030729000832003072900083EA 2003 7 29 QXEA200300742 120030613A1430 SCREW CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE TCAS ANTENNA UNSECURE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - LOWER TCAS ANTENNA FORWARD RIGHT HAND NUTPLATE SCREW SPINS. REPAIRED IAW TR 34-0051, TASK 34-43-07-400-801-A01, PARAGRAPH A THROUGH D. 2L72 4F4 FRTA21EA E15NE 20030729000902003072900090WP 2003 7 29 ABXA030282 120030712A32302643040 CABLE DOUG DC8 DC863 302198AWP LANDING GEAR BROKEN A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23815AX 46097 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. GOT (MAIN GEAR SPOILERS INOP) LIGHT. PERFORMED ABNORMALS, GEAR RETRACTED. ALL OTHER INDICATIONS NORMAL. PRESSURIZATION OK. - REPLACED ANTI-RETRACTION CABLE IAW DC8 MM 32-31-00-2-0003. TESTED AND OPS CHECKED GOOD DURING GEAR SWING IAW MM 32-31-00-2-0003. 2L74 4F 4A25 20030729000992003072900099NM 2003 7 29 2003F00479 120030605A21216056751 COOLING FAN BOEING727 727222 1384073NM CABIN MALFUNCTIONED A RYNAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE077645U 20039 AFTER 'BLOCK-IN', THERE WAS SMOKE IN THE COCKPIT. (M) 2L73 4F A3WE 20030729001092003072900109EU 2003 7 29 2003F00482 120030516A5350 FAIRING AIRBUS320 A320233 3930329EU FUSELAGE DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND BELLY FAIRING 197EB DELAMINATED. REPAIRED FAIRING IAW SRM S3-4S-12, PAGE 220 FIGURE 205. (M) 2L72 4F RTA28NM 20030729001162003072900116WP 2003 7 29 AMTA200300865 120030701A5320 STRUCTURE LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND PUNCTURE AND CRACK IN C1 PIT AT FS 594, 9 INCHES RT OF CENTER LINE. CRACK IS 4.5 INCHES LONG PUNCTURE IS .75 INCH BY .5 INCH. PERFORMED INTERIM REPAIR PER ERA L10-53T-2549 REV B. 2L73 4F A23WE 20030729001242003072900124EA 2003 7 29 SWIA200312197 120030717A2710 SEAL CNDAIRCL600 CL6002B19 1900309EA RT AILERON TORN A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07413SW 7102 RIGHT AILERON IS UP INFLIGHT, REQUIRES 5 PERCENT LEFT RUDDER TRIM TO CENTER SLIP/SKID INDICATOR FOR STRAIGHT AND LEVEL FLIGHT. FOUND SEAL UNDER AILERON RT SIDE TO BE TORN. REPLACED TORN SEAL. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030729001252003072900125NE 2003 7 29 SWIA200312198 220030716A7200CF34 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT MALFUNCTIONED A SWIAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 NM07592SW4744 4744 7279 LEFT ENGINE FAILED ON DESCENT. JUST PRIOR TO FAILURE, ''L MAIN EJECTOR'' AND ''L SCAV EJECTOR'' MSG DISPLAYED ON EICAS. REMOVED AND REPLACED LEFT POWER PLANT IAW CRJ MM 72-00-00. OPS AND LEAK CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20030729001302003072900130EA 2003 7 29 SWIA200312185 120030604A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 193 ELECTRICAL BAY FLOOR RT CRACKED. (DISCOVERED DURING C-CHECK)REPAIRED DAMAGED FLOOR IAW CRJ REO 601R-53-11-245 REV. ''NC''. 2L72 4F4 FRTA21EA E15NE 20030729001322003072900132EA 2003 7 29 SWIA200312187 120030604A5320 STIFFENER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 559 BULKHEAD VERTICAL POST RBL 9.0 INBOARD LOWER FLANGE CRACKED. (DISCOVERED DURING C-CHECK)REPAIRED POST IAW CRJ REO 601R-53-41-057 REV ''NC''. 2L72 4F4 FRTA21EA E15NE 20030807001092003080700109NM 2003 8 7 HNAA0300038 120030807A531185330073 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07975HA 176 DURING 40K INSPECTION FRAME LEG WAS FOUND WITH CORROSION AT STATION X510 AND BETWEEN STR 32S AND STR 31S. A NEW FRAME WAS SPLICED IN AS PER EO 8-53-03-0782. 2H72 4T RTA13NM 20030812000212003081200021NE 2003 8 12 HEEA088368 120030606A6230SB5200103 BEARING SKRSKYS76 S76A 8143006NE ROTATING SCISSORWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X A18500505 760050 ROTATING SCISSOR HAS WORN BEARINGS. REPLACED 4 EACH BEARINGS SB5200103 DUE TO BEING WORN. REPAIRED. 1G72 3U H1NE 20030812000332003081200033 2003 8 12 HEEA088397 420030718A23126221879001 TRANSCEIVER SKRSKYS76 S76A 8143006NE VHF DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 VHF TRANCEIVER FREQUENCY OFF. SHOP REPAIR. 1G72 3U H1NE 20030812000582003081200058SW 2003 8 12 HEEA088500 120030715A2841 INDICATOR BELL 412 412 1182202SW FUEL QTY MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 FUEL QTY INDICATOR, NEEDLE DROPS INTERMITTENTLY. 1G72 4U H4SW 20030812000792003081200079EU 2003 8 12 HEEA088629 120030721A760011204300106 SUPPORT BOLKMS117 BK117A1 5626010EU ENG CONTROLS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC 7152 CARDAN JOINT WORN CAUSING EXCESSSIVE WEAR ON INSIDE OF BASE SUPPORT. SCRAPPED. 1G72 3U H13EU 20030812000862003081200086SW 2003 8 12 HEEA088624 120030806A2820206063653001 TUBE BELL 206 206L3 1182108SW FUEL SYSTEM TWISTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 TUBE TWISTED AND WILL NOT SEAL IN CELL. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20030812000872003081200087EU 2003 8 12 HEEA088625 120030512A670010541310 BELLCRANK BOLKMS105 BO105S 5626006EU FLT CONTROLS ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03133AE S800 BELLCRANK ROUGH BEARINGS. REPLACED BEARING (2 EACH) LN9089-20E1 DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030812000942003081200094EU 2003 8 12 HEEA088640 120030709A5230350A25110602 LOCK AEROSPAS355 AS355* EU CARGO DOOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03732AE 2873 CARGO DOOR LOCK WILL NOT LOCK. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030813000152003081300015SW 2003 8 13 HEEA088600 120030723A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X319 51412 MASTER BATTERY DROPS TO 22 VOLT OVERNIGHT. SHOP REPAIR. 1G71 3U H2SW 20030813000322003081300032SW 2003 8 13 HEEA088576 120030729A6220 BEARING BELL 412 412 1182202SW PENDULUM ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L PHI702 33006 PENDULUM ASSY HAS ROUGHNESS IN BEARINGS. SHOP REPAIR. 1G72 4U H4SW 20030813000412003081300041NM 2003 8 13 2003UALA00455 120030601A3350 SOCKET BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29398UA 24673 NR 1 RIGHT HAND DOOR EXTERNAL FUSELAGE EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED SLIDE LIGHT SOCKET ASSY. 2L72 4F4 FRTA16WE E2GL 20030813000602003081300060NM 2003 8 13 UPS03440832 120030519A5320 WEB BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - STA 560 TO 580 STR 23R ATT WEB FOUND CORROSION CRACK. SUPPORT WEB REPLACED AS PER SRM 51-10-01. 2L74 4F RTA20WE 20030813000652003081300065NM 2003 8 13 UPS03440837 120030518A5320 FLOOR SUPPORT BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, BULK CARGO STA 1920-1980 LBL 45 FLOOR SUPPORT UPPER AND LWR SURFACE CORRODED. BULK CARGO STA 1920-1950 LBL 45 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 DUE TO BLEND OUT (1.25 INCH X 3 INCH X 0.019 INCH) EXCEEDED SRM 53-10-01 FIG 1 LIMITATION. BS 1950 TO BS 1980 LBL 45 FLOOR SUPPORT CORROSION REMOVED WITHIN SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F RTA20WE 20030813000712003081300071EA 2003 8 13 SWIA200312083 120030608A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07590SW5051 5051 7077 STAB TRIM CHANNEL 2 WILL NOT REMAIN ENGAGED DURING TEST. REMOVED AND REPLACED HSTA AND MCU WITH A SERVICEABLE UNITS. OPS CHECK GOOD AT THIS TIME. P/N ON 7062-3 OFF 814. 2L72 4F RTA21EA 20030813000782003081300078NM 2003 8 13 UPS03M40847 120030611A5210 BOTTLE DOUG MD11 MD11F 3023600NM PAX DOOR DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01253UP FOUND L1 ENTRY DOOR EMERGENCY EXIT BOTTLE DISCHARGED / DOOR OPEN. SERVICED L1 DOOR EMERGENCY BOTTLE PER MM 12/25/04, P301. OPS CHECKED GOOD. 2L73 4F RTA22WE 20030729001332003072900133EA 2003 7 29 SWIA200312188 120030604A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 664 STR 9L FIREWALL SHUTOFF VALVE INTERCOSTAL SUPPORT AND ANGLE CRACKED. (DISCOVERED DURING C-CHECK) REPAIR INTERCOSTAL AND ANGLE FABRICATED AND INSTALLED IAW CRJ SRM 51-31-00. 2L72 4F RTA21EA 20030730000252003073000025WP 2003 7 30 ABXA030213 120030528A5320991050313 WEB DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 RIGHT CUSP WEB JUST FORWARD OF FS 1041 CRACKED. REPAIRED CRACK IN CUSP IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030730000302003073000030WP 2003 7 30 ABXA030267 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE STUB FRAME IN MAIN CARGO DOOR STA 217. REMOVED, FABRICATED AND INSTALLED NEW FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-3-0. 2L74 4F 4A25 20030730000322003073000032WP 2003 7 30 ABXA030269 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 227. CUT AND REMOVED DOOR FRAME, INSTALLED SPLICED SECTION IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-20. 2L74 4F 4A25 20030807000622003080700062SO 2003 8 7 C2XA03CL131 120030801A33503025103 LIGHT EMB 145 EMB145ER 3260211SO FUSELAGE INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716944 145045 DURING ROUTINE MAINTENANCE THE LT OVERWING EMERGENCY LIGHT DID NOT ILLUMINATE DURING TESTING. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030807000762003080700076SO 2003 8 7 C2XA03CL126 120030725A27403621001009MOD1 CONTROL UNIT EMB 145 EMB145ER 3260211SO HORIZONTAL STAB INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149373488 145026 EWR FLIGHT 2403, THE CREW REPORTED THE PITCH TRIM 1/2 WAS INOPERATIVE. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030807000862003080700086EU 2003 8 7 03217301 120030805A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27301UE 41012 DURING MAINTENANCE INSPECTION THE LT OVERWING LIGHT ASSEMBLY WAS DISCOVERED LOOSE. MAINTENANCE PERSONNEL RESECURED THE OVERWING LIGHT ASSEMBLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030807000872003080700087 2003 8 7 QXEA200300870 420030719A3140 CIRCUIT BREAKER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TRIPPED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09612QX 10042 ADG DEPLOY AUTO CB (2N6) OPENED PER PROXIMITY SYSTEM CHANNEL MESSAGE CHECKLIST AND SHUTDOWN APU. CLOSED ADG DEPLOY AUTO CB. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030807000912003080700091 2003 8 7 GLBA2003111 420030802A34006226137201 RECEIVER BEECH 1900 1900D 1154162CE COCKPIT INCORRECT A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03253GL14819 UE253 NAV NEEDLE SHOWED 15 DEG ERROR BETWEEN EACH OTHER. REMOVED AND REPLACED NR 2 NAV RECEIVER. 2L72 4T RTA24CE 20030807000932003080700093NM 2003 8 7 EIA2003105 120030725A5311 FRAME BOEING747 747212B 1384886NM BULKHEAD CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 BS 1000 BULKHEAD FRAME CRACKED AT S-38L. CRACK VERIFIED WITH HFEC S/N J032592, CAL DUE 4-21-04. CRACK LENGTH APPROXIMATELY .75 INCH. REPAIRED PER ECRA 485-53-157-2. 2L74 4F A20WE 20030807001142003080700114SW 2003 8 7 ALGA088162 120030721A6320E6893672 PINION GEAR BELL 407 407 1182206SW ALLSN 250C 250C30S 03013GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03507AL723 CAG90759 53103 CAE890824S HEAVY SPALLING ON GEAR TEETH,DUE TO IMPROPER MESHING OF GEAR TEETH. 1G71 3U3 UO H2SW E1GL 20030807001182003080700118SW 2003 8 7 ALGA088196 120030724A6320206040032101 BEARING BELL 206 206B3 1181506SW GEARBOX FAILED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03168H BKW10006 3453 TRANSMISSION DISASSEMBLED FOR 4500HR. OVERHAUL ,FOUND BEARING BREAKING DOWN DURING NORMAL INSPECTION PROCEDURE. 1G71 3U H2SW 20030812000162003081200016 2003 8 12 HEEA088435 420030722A34427001840903 TRANSCEIVER SKRSKYS76 S76A 8143006NE WX RADAR SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 WEATHER RADAR TRANSCEIVER INOPERATIVE. 1G72 3U H1NE 20030812000262003081200026 2003 8 12 HEEA088377 420030718A34427001840903 TRANSCEIVER SKRSKYS76 S76A 8143006NE WX RADAR SYS INTERFERENCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 WEATHER RADAR TRANSCEIVER, TROUBLESHOOTING INTERFERENCE. REPAIRED. 1G72 3U H1NE 20030812000292003081200029EU 2003 8 12 KBMA088328 120030719A2150MS2524430 CIRCUIT BREAKER AEROSPAS355 AS355* EU AIR CONDITIONER FAILED B KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 12295 2300 AIRCRAFT AIR CONDITIONER BLOWS HOT AIR 20 MIN AFTER TAKE OFF. REPLACED 3D AMP C/B FOR COMP WITH SERVICEABLE 3DAMP CB REMOVED FROM SPARE CONTROL BOX . 1G72 3U H11EU 20030812000312003081200031 2003 8 12 HEEA088395 420030711A34424000038 CONTROL HEAD SKRSKYS76 S76A 8143006NE WX RADAR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 WX RADAR CONTROL HEAD VOLUME CONTROL KNOB SLIPS AND ROUGH WHEN ADJUSTING VOLUME. SHOP REPAIR. 1G72 3U H1NE 20030812000412003081200041 2003 8 12 HEEA088370 420030709A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 AFCS ACTUATOR HAS INTERMITTENT KICK AND FREEZES IN CENTER. 1G72 3U H1NE 20030812000482003081200048 2003 8 12 HEEA088439 420030709A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 WORN AND CORRODED. REPLACED CLUTCH WASHER A7683361 DUE TO WORN; ROD END BEARING MS21151-8C DUE TO ROUGH; POTENTIOMETER (2 EA) A768343-3 DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030812000572003081200057SW 2003 8 12 HEEA088494 120030718A5230212513101 GAS CYLINDER BELL 412 412 1182202SW CARGO DOOR WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 GAS CYLINDER WEAK. SCRAPPED. 1G72 4U H4SW 20030812000692003081200069SW 2003 8 12 HEEA088566 120030730A28222C271 CARTRIDGE BELL 206 206L3 1182108SW FUEL SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 CARTRIDGE QUIT WORKING. MAKES A GROWLING NOISE BUT WILL NOT PRODUCE PRESSURE. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030805000562003080500056NE 2003 8 5 ASOA03300 220030709A7200 ENGINE AEROSPATR72 ATR72 EU PWA PW120 PW127 NE RIGHT MALFUNCTIONED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11641AS 387 DURING FINAL APPROACH FROM MGM-ATL, WHEN THE CREW PULLED THE POWER LEVERS BACK TO IDEL, THE FLIGHT ATTENDANTS NOTICED A STRONG SMOKE ODOR AND HAZE IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRT E20NE 20030805000642003080500064NM 2003 8 5 AALA20030659 120030613A3397 WIRE BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21794AN 30256 DURING OVERNIGHT MAINTENANCE, LEFT FORWARD FIRST CLASS GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT FORWARD FIRST CLASS GALLEY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030805000762003080500076EA 2003 8 5 ASOA03304 120030713A5310601350061 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE LEFT AND RIGHT ENGINE SUPPORT BEAM LOWER WEB AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT ENGINE SUPPORT BEAM LOWER WEB AT BL 36.20 IAW ASA EO 600-53-0073. (M) 2L72 4F RTA21EA 20030805000912003080500091EU 2003 8 5 USAASA03079 120030715A2120 ODOR AIRBUSA321 A321211 3930370EU CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19180US 1525 DURNG DESCENT, THE CABIN CREW IN THE AFT CABIN NOTIFIED THE FLIGHT CREW OF AN ELECTRICAL SMOKE ODOR. SHORTLY AFTERWARDS, THE COCKPIT CREW NOTICED THE SAME ODOR. THE COCKPIT CREW FOLLOWED CHECKLIST PROCEDURES AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN BOTH PACKS WITH BLEED SOURCES FROM BOTH ENGINES AND THE APU. POWERED THE CABIN, GALLEY'S AND LAVATORIES WITH A/C POWER. CHECKED THE AVIONICS COOLING SYSTEM. NO FAULTS WERE FOUND. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030806000432003080600043NM 2003 8 6 AWXA200300861 120030720A532065468232 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK .5 INCH CRACK WAS FOUND AT SCREW HOLE ON STRAP ATTACHED TO WEB AT BS 1032, BL 0 - LBL 30, WL 208. MAINTENANCE REMOVED CRACKED AT BS 1032, FROM BL 0 TO LBL 30; FABRICATED A NEW REPLACEMENT SECTION OF STRAPS; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 5 & PG 42, FIG 10. 2L72 4F RTA16WE 20030806000652003080600065SO 2003 8 6 C2XA03SH234 120030726A532014521725001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV-DURING C-CHECK, THE LEFT HAND SILL BETWEEN FRAMES 19 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806000712003080600071NM 2003 8 6 AWXA200300855 120030712A53206546592 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT AND NUT PLATES BS 770, RBL 3, WL 155. MAINTENANCE REMOVED DAMAGE SECTION OF FLOOR SUPPORT AT BS 770, RBL 3, WL 155; FABRICATED A CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG 201, FIG 201, SHT 1 & 2. 2L72 4F RTA16WE 20030807000332003080700033NM 2003 8 7 USAA030125 120030708A5314 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 FOUND KEELBEAM CORRODED 1 INCH BY 3 INCH AREA, FS 727 LEFT KEELBEAM. CORROSION LEVEL 1, TASK NR C53-208-01. REPLACED LEFT KEELBEAM PER TYP REPAIR 53-60-09. (M) 2L72 4F RTA16WE 20030807000362003080700036NM 2003 8 7 UIEA200300037 120030624A5330 SKIN BOEING747 7472D3B 1384805NM FUSELAGE CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15506MC 21252 DURING C-CHECK, AS PER XEO 53-06/04/03 FOUND AFT BELLY SKIN WITH CORROSION AND DENTS UNDER PREVIOUS REPAIR AT THE FOLLOWING STATIONS 2200-2240 STRINGER 45R-48L AND STATION 1977-2008 STRINGER 45R-48L REPAIR CARRIED OUT PER BOEING TELEX SEP-SIN-03-00036H AND 8110-3. (M) 2L74 4F RTA20WE 20030807000692003080700069EU 2003 8 7 AWXA200300840 120030724A2120 ODOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE CABIN DETECTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28631AW 077 AFTER TAKEOFF FROM LAS EN ROUTE FOR PDX NOTICED AIRCRAFT VIBRATION, CLIMBING THROUGH FL 180 NR 2 ENGINE VIBRATION AT 2.2, VIBRATION BECAME STRONGER AND AFT CABIN FLIGHT ATTENDANT REPORTED A BURNING ODOR COMING FROM AFT GALLEY AREA. ODOR BECAME STRONGER AS FLIGHT CONTINUED, DIVERTED TO RENO. MAINTENANCE PERFORMED AN ENGINE RUN, NR 2 ENGINE AT 1.265 EPR WITH A N1 VIBRATION PEAK OF 2.3, WITHIN LIMITS. INSPECTED TAIL SURFACES AND WING TO BODY FAIRINGS, NO DAMAGE NOTED. RAN A/C PACKS WITH APU BLEED, AND OPERATED AND INSPECTED ALL GALLEY EQUIPMENT, NO BURNING ODOR NOTED. 2L72 4F4 FRTA28NM E311NE 20030813000912003081300091NM 2003 8 13 2003UALA00496 120030613A5347 SEAT TRACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29189UA 26878 SEAT TRACK CRACKED BS 619 RBL 45 OUTBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. REPLACED TRACK. 2L74 4F4 FRTA20WE E24NE 20030813000952003081300095NM 2003 8 13 0301136739 120030614A272019642122 COMPUTER BOEING747 747251F 1384898NM YAW DAMPER FAILED A NWAAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CLCLIMB 1 GL01639US5241437560 23887 DURING CLIMB THE LOWER RUDDER WAS DISPLACED 5 UNITS LEFT OF CENTER AND THE AIRCRAFT YAWED LEFT. RUDDER DISPLACEMENT WENT TO ZERO AT FL 270 AND NO FURTHER MALFUNCTIONS WERE EXPERIENCED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LOWER YAW DAMPER COMPUTER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030806001252003080600125SO 2003 8 6 C2XA03TY101 120030725A5513KSC27072OV BEARING EMB 145 EMB145ER 3260211SO HORIZONTAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713929 145009 THE LEFT AND RIGHT HORIZ STAB SPHERICAL BEARINGS FAILED WEAR CHECK. MAINTENANCE REPAIRED THE LEFT AND RIGHT VERTICAL STAB SPHERICAL BEARING HOUSINGS AND INSTALLED BOTH SPHERICAL BEARINGS IAW EC5510-01059 AND EMB-IC2003-145/2529. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4F RTT00011AT 20030806001342003080600134NM 2003 8 6 AWXA200300875 120030802A352011708004 OXYGEN GEN BOEING737 7373G7 1384595NM SEAT ROW 5 RT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK THE OXYGEN GENERATOR AT PSU SEAT ROW 5 RT WAS FOUND WITH A BLACK BAND. REMOVED AND REPLACED OXYGEN GENERATOR AT PSU SEAT ROW 5 RT IAW T/C R1C350004. 2L72 4F RTA16WE 20030806001402003080600140SO 2003 8 6 C2XA03SH214 120030702A541014576631621 STIFFENER EMB 145 EMB145 3260210SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL STIFFENER WAS FOUND TO GOUGED AT FRAME 71L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030806001522003080600152SO 2003 8 6 C2XA03SH207 120030701A532014521725001 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE LT HAND SILL BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030807000102003080700010EA 2003 8 7 ASOA03261 120030611A5330601R31062 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING HANGAR MAINTENANCE IN CKB, THE FUSELAGE SKIN AT FS 310 BETWEEN STRINGER 15L AND 16L WAS FOUND TO BE DENTED BEYOND LIMITS. MAINTENANCE REPAIRED THE FUSELAGE SKIN AT FS 310 BETWEEN STRINGERS 15L AND 16L IAW REO 601R-52-11-008 REV B REPAIR A. (M) 2L72 4F RTA21EA 20030807000702003080700070NM 2003 8 7 AWXA200300841 120030725A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 DURING INSPECTION A 1.5 INCH CRACK WAS FOUND ON SKIN AT BS 520, STR 12 RT. MAINTENANCE REMOVED DAMAGED AND FABRICATED A REPAIR DOUBLER OUT 2024T3.071. PLACED ON MCK, PERMANENT REPAIR REQUIRED NO LATER THAN 20,000 FLIGHTS. 2L72 4F RTA16WE 20030807000722003080700072NM 2003 8 7 AWXA200300843 120030713A572065C3024217 CLIP BOEING737 7373G7 1384595NM LT WING PANEL CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A .5 INCH CRACK WAS FOUND ON LT WING LOWER TRAILING EDGE PANEL CLIP, OUTBOARD OF THE NR 3 FLAP TRACK FAIRING WS 210. REMOVED DAMAGED PANEL CLIP ON LT WING LOWER TRAILING EDGE WS 210; FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 PG 4, FIG 2 & SRM 51-40-02 PG 17. 2L72 4F RTA16WE 20030812000542003081200054SW 2003 8 12 HEEA088479 120030703A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801120 51074 MASTER BATTERY DEAD. 1G71 3U H2SW 20030812000712003081200071SW 2003 8 12 HEEA088579 120030804A6230 BEARING BELL 412 412 1182202SW LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L A2190 33006 LINK ASSY BEARINGS WORN. SHOP REPAIR. 1G72 4U H4SW 20030812000762003081200076SW 2003 8 12 HEEA088609 120030806A3213212321103 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 CROSSTUBE CORRODED BEYOND LIMITS IN ZONE C-3. SCRAPPED. 1G72 4U H4SW 20030813000982003081300098EA 2003 8 13 SWIA200312102 120030612A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07916SW 7634 LEFT REAR AFT EMERGENCY LIGHT (EXTERIOR) INOP. REPLACED BAD BULB ON LEFT REAR AFT EMERGENCY LIGHT OVERWING. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030813001052003081300105WP 2003 8 13 AALA20030703 120030630A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21473AA 49648 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LAVATORY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED FORWARD LAVATORY EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001102003081300110EU 2003 8 13 USAABA03023 120030422A24974206513 WIRE HARNESS AIRBUS330 A330323 3930335EU LT ENGINE CHAFED A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19671UW 0323 LGW - FLT 893 - EN ROUTE FRA-PHL, AT APPROXIMATELY 55 N, 020 W, THE LEFT IDG FAULTED AND WOULD NOT RESET. THE CREW ALSO COLD NOT GET THE APU STARTED. THE FLIGHT DIVERTED TO LGW. EN ROUTE TO LGW, THE APU WAS STARTED. FLIGHT LANDED AT LGW WITH NO FURTHER INCIDENT. MAINTENANCE SWAPPED THE APU AND LEFT IDG GCU'S. AN ENGINE RUN WAS PERFORMED AND THE LEFT GENERATOR OPERATED NORMALLY, AS DID THE APU GENERATOR. THE FLIGHT DEPARTED LGW WTH THE APU RUNNING. EN ROUTE, THE LEFT IDG FAULTED AGAIN. THE FLIGHT CONTINUED AND LANDED IN PHL WITHOUT FURTHER INCIDENT. THE FINAL FIX FOR THE APU WAS TO REPLACED THE FUEL FLOW DIVIDER. THE FINAL FIX FOR THE IDG WAS REPLACING THE IDG WIRING HARNESS, ON WHICH THE WIRE TO PIN N2L72 4F RTA46NM 20030826001152003082600115NM 2003 8 26 S02453034 120030506A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJFO OTHER O OTHER TXTAXI/GRND HDL 1 WP03 28710 B-18202 FUSELAGE SKIN REPAIR COMMON TO BS 741,S-25L,S-26L. REPAIR IAW EO 744-53-00-003. 2L74 4F4 FRTA20WE E24NE 20030826001282003082600128NM 2003 8 26 03FDEA01000 120030629A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25463FE 22551 MDIS 463 53-30 0005661 26JUN03 BFM CLOSE R COMPLY WITH EA NR 7-5330-70964 FUSELAGE-SKIN-PRE-EXISTING ELONGATED HOLES UNDER MCD HINGE (AD 2002-16-19).. FACT 29JUN03 17:38 BFM U COMPLIED WITH EA NR 7-5330-70964 FUSELAGE-SKIN-PRE-EXISTING ELONGATED HOLES UNDER MCD HINGE (AD2002-16-19 ). CLOSED ON 06/29/2003 2L73 4F RTA3WE 20030827000022003082700002EU 2003 8 27 03FDEA00994 120030628A5320 CROSSBEAM AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 MDIS 658 53-10 0006641 24JUN03 BFM CLOSE R COMPLY WITH E.A. 6-5310-70959 FUSELAGE-MAINFRAME-REWORK OF MAIN DECK CROSSBEAM DAMAGE. FACT 28JUN03 14:23 BFM U COMPLIED WITH EA6-5310-70959 FUSELAGE-MAINFRAME- REWORK OF MAIN DECK CROSSBEAM DAMAGE. 2L72 4F4 FRTA35EU E13NE 20030827000152003082700015NM 2003 8 27 03FDEA00955 120030623A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 N00459 CRACKED FRAME SHEAR TIE AT STA 500 ABOVE STR 18 LT. ** SD ** COMING 2L73 4F RTA3WE 20030827000422003082700042CE 2003 8 27 51904 120030624A7797 LEAD BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE BUSS BAR LOOSE A AMWAD RETURN TO BLOCK O OTHER CRCRUISE 1 CE07173YV UE173 ON FLIGHT 5517, DURING THE FLIGHT THE RIGHT ENGINE ITT WENT TO 1000 DEGREES CELSIUS THEN WENT BACK TO NORMAL. SHORTLY THERE AFTER THE ITT AGAIN WENT TO 1000 DEGREES CELSIUS AND STAYED THERE. THE CREW REDUCED POWER ON THE RIGHT ENGINE AND RETURNED TO AIRPORT WITH NO FURTHER INCIDENT. MAINTENANCE FROUND THE LOOSE ELECTRICAL LEAD ON T3 BUS BAR. THE CORRECTIVE ACTION WAS THAT MAINTENANCE TIGHTENED THE NUT AT T5 BLOCK. NO PARTS WERE USED. THEREFORE, NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T4 TRTA24CE E26NE 20030822001492003082200149NM 2003 8 22 C1HA200383008 120030817A3350900835A BATTERY PACK BOEING727 7272S7 138407ZNM CABIN DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW 727 MM 33-50-22, ALL OPS NORMAL. 2L73 4F A3WE 20030822001642003082200164WP 2003 8 22 UPS03841020 120030708A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 COMPLY WITH PERMANENT REPAIR IAW EO DC8-5330-14974-A AT L-1 FWD UPPER CORNER STA 25 AT LONG 10L. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 15. 2L74 4F RT4A25 20030822001822003082200182NM 2003 8 22 UPS03M41084 120030506A5711 SPAR CAP DOUG MD11 MD11F 3023600NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 INSPECTION TYPE:C LT WING REAR SPAR AT XORS 772.500 UPPER SURFACE FOUND CORROSION AS MARKED. CORR REMOVED AND REPROTECTED AT REAR SPAR UPP CAP AFT LEG FROM STA XORS 772 TO STA XORS 799 IAW SRM 51-21-01 REV 32 VOL II, MATERIAL REMOVED 0.009, ORG THK 0.266, LEAVE THE BLEND OUT AREA AS 'AS IS' PER EN1013-03 AND UPS REPAIR/ALTERNATION AUTO, ENGINEERING FILE NO. : MD11-57-20009. 2. HFEC INSP ON REWORK AREA FOUND NO CRACK EVIDENT. 2L73 4F RTA22WE 20030822001832003082200183 2003 8 22 UPS03141127 420030818A2565 BATTERY AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01120UP 0805 INSPECTION TYPE:N/A ESCAPE SLIDE FAILED BATT LOAD TEST. TC 256120-02-1-L-200. REMOVED AND REPLACED IAW A300 AMM 25-61-21. 2L72 4F RTA35EU 20030825000612003082500061NM 2003 8 25 UPS03241060 120030722A5210509326 HINGE FITTING BOEING727 72725C 138400HNM ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C, DURING NDT OF ALL FASTENER HOLES COMMON TO SKIN CHANGE AT FWD ENTRY DOORWAY, CRACK FOUND IN FWD ENTRY DOOR UPPER HINGE LOWER FITTING. FITTING REPLACED IAW DRG 65-17684. 2L73 4F A3WE 20030825000962003082500096WP 2003 8 25 03FDEA01268 120030812A5320 ANGLE DOUG DC10 DC1030 3023501WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 REMOVED AND REPLACED 3EA ANGLES IAW 2F SRM 51-31-01 STA 1361. CLOSED 08 2F122 2003 ON FEDEX N 2FR N00327 AND N0112 10 UNDER MAE 2FO NR 3423. 2L73 4F A22WE 20030825000972003082500097NM 2003 8 25 VNAA0308001 120030801A2611SD9422AOAO SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAULTY A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07436JS199717 3052 THE CREW RECEIVED A LAV SMOKE CAS MESSAGE AND CALLED MAINTENANCE. MAINTENANCE DEFERRED THE LAV SMOKE DETECTOR WITH THE CREW. UPON ARRIVAL AT PIT, MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR FLIGHT. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030825001082003082500108EA 2003 8 25 03229642 120030817A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27642BR 7536 DURING MAINTENANCE INSPECTION THE EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EXTERIOR EMERGENCY LAMPS. A SATISFACTORY OPERATIONAL CEHCK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030825001532003082500153NM 2003 8 25 AMTA200300969 120030728A2150 WARNING SYSTEM BOEING737 73783N 13844HINM COCKPIT MALFUNCTIONED A AMTAD RETURN TO BLOCK J WARNING INDICATION ININSP/MAINT 1 GL11303TZ 28648 RIGHT PACK LIGHT ILLUMINATED ALONG WITH CONT CABIN AND FORWARD CABIN LIGHTS. PERFORMED FIM 21-62-00-810-848, AND PACK/ZONE TEMP CONTROLLER BITE IAW 21-62-00-810-801. NO DEFECTS NOTED. (M) 2L72 4F RTA16WE 20030825001592003082500159WP 2003 8 25 GTIA030602 120030725A5320 PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 256 LEFT SIDE INBOARD WEB PANEL, PHENOLIC, HAS DISBONDED AT HAT SECTION. BONDED LEFT SIDE INBOARD WEB PANEL AT HAT SECTION EDGE. (M) 2L72 4F RTA6WE 20030826000392003082600039NM 2003 8 26 03FDEA01338 120030819A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 DENT IN SKIN BS 268 BETWEEN STR 16-17L. DENT IN SKIN AT BS 268 BETWEEN STR 16-17L WAS OUT OF LIMITS. AREA WAS REPAIRED PER SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20030826000412003082600041NM 2003 8 26 03FDEA01195 120030730A5720ANB7445 SHIM DOUG MD11 MD11 3023602NM LT WING OUT OF POSITION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT WING ROOT- STRINGER NR 1 SHIM FOUND MIGRATED 0.3 INCH DOWN. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION. 2L73 4F RTA22WE 20030826000472003082600047NM 2003 8 26 03FDEA01219 120030807A5311 FRAME BOEING727 727200 138407ENM FUSELAGE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 FWD CARGO BAY 680 FRAME BENT AT RBL 35 BETWEEN STR 24R & 25R. FRAME AT BS 680, RBL 35 BETWEEN STR 24 & 25 RT OUT OF LIMITS. REPAIRED FRAME IAW FEDEX EA 7-5310-72507, SRM 53-10-1 & 51-40-3 FIG 1. 2L73 4F RTA3WE 20030826000512003082600051NM 2003 8 26 03FDEA01216 120030725A5744ARC0155504 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE CORRODED. RIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE REPAIRED AS PER FEDEX AE 1-5750-71880, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES- RT INBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030826000532003082600053WP 2003 8 26 03FDEA01144 120030725A5347FX601096418 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 MAIN CARGO DECK SEAT TRACK RBL 48 STA 1341 TO 1361 HAS CORROSION AROUND FASTENERS. CLOSING ACTION ON 07/16/03 REMOVED AND REPLACED SEAT TRACK AT RBL 48 STA 1341 TO 1361. PARTS FAB ON TRAVELER T2/348647, T2/348645, T2/348646. PARTS INSTALLED IAW SRM 53-70-00 AND M/M 53- 21-08-2. 2L73 4F A22WE 20030826000802003082600080EU 2003 8 26 YENA200319 120030802A3234114079017 SELECTOR VALVE AIRBUS320 A320232 3930326EU LANDING GEAR FAILED A YENAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA15519JB10026 1398 ON GO-AROUND MANEUVER, LANDING GEAR WOULD NOT RETRACT. GOT A (LANDING GEAR NOT UPLOCKED) ECAM FOLLOWED BY L/G DOOR NOT CLOSED ECAM - WE PUT L/G HANDLE BACK DOWN - GEAR ALREADY DOWN". AIRCRAFT FLEW BACK TO JFK UNDER MEL 32-31-00 WITHOUT PASSENGER. L/D DOOR SELECTOR VALVE WAS REPLACED BUT DID NOT CORRECT THE PROBLEM. THE PROBLEM WAS CORRECTED UPON REPLACING THE L/G SELECTOR VALVE. 2L72 4F RTA28NM 20030826000912003082600091EU 2003 8 26 YENA200318 120030729A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A YENAK NONE O OTHER UKUNKNOWN 1 EA15565JB7882 175 2031 OVERHEAD EMERGENCY EXIT AT AFT GALLEY THRESHOLD INOP. REMOVED AND REPLACED EMERGENCY POWER UNIT FIN NO 13WL PER AMM 33-51-38. OPS CHECK GOOD OK TO CONTINUE SERVICE. 2L72 4F RTA28NM 20030826001552003082600155NM 2003 8 26 MEX2003315 120030311A783059380541 LINKAGE DOUG MD80 MD83 3023681NM THRUST REVERSER BROKEN A ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23831LF 53050 FLT 225 - GDL-MEX - THE RIGHT ENGINE THRUST REVERSER WAS REMOVED DUE TO INDICATION OF RIGHT ENGINE UNLOCK CAME ON AFTER TAKEOFF. AFTER THE THRUST REVERSER ASSEMBLY WAS RECEIVED AT THE SHOP, A DETAILED INSPECTION WAS PERFORMED. DOWN RIGHT OVER CENTER LINK ASSEMBLY WAS FOUND BROKEN (P/N 5938053-1) FOR THE OBSERVED EVIDENCES OF THE BLOCKAGE OF THE CARRIER, P/N 5933054-1, PROBABLY LED TO THE FOLDING OF ROD GUIDES AND BREAKING OF THE OVER CENTER LINK, RESULTING AT THE SAME TIME MISALIGNMENT OF BOTH DOORS AT THE CLOSING POSITION AND DAMAGED ON THE NOZZLE OUTSIDE SKIN. THE REVERSER SENT OUT OF SERVICE TO AN EXTERNAL SHOP IN EXCHANGE, INCLUDED IN A PROGRAM OF EXCHANGE OF PARTS. (M) 2L72 4F RT 20030827000512003082700051NM 2003 8 27 ANCF200300017 120030622A793121SN04104E PRESSURE SWITCH BOEING757 757200 1384950NM LT ENGINE MALFUNCTIONED W ANCFA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO23262CT 26246 PILOT REPORT: DURING FLIGHT MESSAGE (L OIL FILTER) DISPLAYED. OIL PRESS AND VIBRATION WERE NORMAL. ENGINE WAS NOT SHUTDOWN. FLIGHT RETURNED. FIM 792100 PAGE 103 WAS PERFORMED; REPLACED SCAVENGE AND PRESSURE FILTER ELEMENT IAW AMM 79-21-08/07/ 401, MAGNETIC CHIP DETECTORS WERE INSPECTED AND WERE FOUND IN NORMAL CONDITIONS, SCAVENGE FILTER DIFERENCIAL PRESSURE SWITCH WAS REPLACED IAW AMM 793502/402 AND CHAFING WAS ELIMINATED IAW WDM 71-51-11/19/ 79-35-11 WITH SATISFACTORY RESULTS. 2L72 4F RTA2NM 20030827000942003082700094SO 2003 8 27 C2XA03CL128 120030727A323023092500401 UPLOCK EMB 145 EMB145ER 3260211SO NLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714938 145029 CLE FLIGHT NR 2001 THE CREW REPORTED THE NOSE WHEEL DID NOT RETRACT AFTER TAKEOFF. THE GEAR WAS RECYCLED AND IT STILL DID NOT RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR UPLOCK BOX ASSEMBLY.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030827000962003082700096SO 2003 8 27 CX2A03SH276 120030817A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK CENTER OMEGA BEAM WAS IDENTIFIED AS CORRODED AT FR 19-22. MAINTENANCE REMOVED AMD REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030827000992003082700099NM 2003 8 27 CALA0300426 120030730A5347 SEAT TRACK BOEING777 777224 1385225NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776010 29480 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1510, LBL 85. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02, PAGE 10 AND SRM 51-40-02. 2L72 4F RTT00001SE 20030827001132003082700113NM 2003 8 27 CALA0300362 120030703A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND A GOUGE IN STRINGER AT STA 1120, RT, IN APU COMPARTMENT. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030827001222003082700122NM 2003 8 27 CALA0300366 120030707A5347 SEAT TRACK BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717122 27564 INSPECTION FOUND FLOOR SEAT TRACK CORRODED AT CABIN FORWARD FLOOR STRUCTURE, STA 377, LBL 24.78. THE SEAT TRACK WAS REMOVED AND REPLACED IAW BOEING DRAWING 141N5130. 2L72 4F RTA2NM 20030827001242003082700124NM 2003 8 27 CALA0300368 120030708A3397BR963512024 WIRE HARNESS BOEING757 757224 1384958NM RROYCERB211 RB211* 54555NE CABIN DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717122 27564 INSPECTION FOUND FLOOR PROXIMITY LIGHT WIRE HARNESS DAMAGED IN SEVERAL PLACES BETWEEN ROWS 26-35. THE WIRE HARNESS WAS REPLACED IAW DRAWING ACM BR2013-P-757CO/-1/-2/-3. 2L72 4F4 FRTA2NM A12EU 20030813001222003081300122NM 2003 8 13 USAA030117 120030717A5542 SKIN BOEING737 737301 1384611NM RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND RUDDER WITH SKIN DAMAGE, 24 INCH OVAL ONE LAYER DAMAGE, LEFT SIDE OF RUDDER 107 INCH FROM BOTTOM 12 INCHES FROM TRAILING EDGE. WET LAY UP REPAIR PER SRM 51-70-17 AND EA 76292. (M) 2L72 4F RTA16WE 20030813001282003081300128WP 2003 8 13 AALA20030697 120030626A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21575AM 53152 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAIL CONE AREA INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT CONNECTOR ON BOTTOM CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001412003081300141NM 2003 8 13 SWAA031754 120030805A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 16L, BS 277 AND BS 520. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030813001442003081300144NM 2003 8 13 SWAA031757 120030805A53116546543 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030813001622003081300162 2003 8 13 SWAA031672 420030727A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030813001672003081300167NM 2003 8 13 SWAA031677 120030728A3350207377 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 EEPLS LENS MISSING AT ROW NR 13. REPLACED LENS PER MM. 2L72 4F RTA16WE 20030813001712003081300171NM 2003 8 13 SWAA031681 120030728A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED C2 CHECK, FOUND RT OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED RT OUTBD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20030813001742003081300174NM 2003 8 13 SWAA031684 120030726A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LENS BROKEN. REPAIRED LENS AND REINSTALLED PER MM. 2L72 4F RTA16WE 20030813001772003081300177NM 2003 8 13 SWAA031687 120030728A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 19R, BS 410 AND BS 735. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030813001782003081300178NM 2003 8 13 SWAA031688 120030729A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 440 AT STR 8R, BS 520 AT STR 8L, BS 597 AT STR 11L AND BS 706 AT STR 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030813001892003081300189 2003 8 13 SWAA031557 420030715A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030814000112003081400011NM 2003 8 14 SWAA031723 120030801A33506104789 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EXTERIOR AND RT AFT LOWER EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030814000142003081400014NM 2003 8 14 SWAA031726 120030801A53306545765 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 4R, BS'S 597, 727B, 685 AND 706. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000442003081400044NM 2003 8 14 SWAA031773 120030807A53306545776 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000502003081400050NM 2003 8 14 UPS03441055 120030718A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FRAME FOUND SURFACE CORROSION AT STA 920 FROM RBL 20 - 50. CORROSION BLEND OUT 0.056 X 1 X 1.5 INCH. BODY FAIRING SUPPORT FRAME REPAIRED AS PER SRM 53-50-04 FIG 2 AT STA 920 FROM RBL 0 - RBL 30 AREA. BODY FAIRING SUPPORT CORROSION AREA STA 920 RBL 30 - RBL 50 CORROSION CLEANED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02 WITHIN SRM 53-50-01 FIG 5 LIMIT. 2L74 4F A20WE 20030812000022003081200002NE 2003 8 12 HEEA088376 120030712A771454487129110 INDICATOR SKRSKYS76 S76A 8143006NE NR 1 ENGINE N1 WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03792P 760193 NR 1 N1 INDICATOR WON'T PASS TACH CHECK. SENT TO HELICOPTER SUPPORT, INC. FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030812000082003081200008NE 2003 8 12 HEEA088408 120030728A67207640009506041 BELLCRANK SKRSKYS76 S76A 8143006NE T/R CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 TAIL ROTOR BELLCRANK HAS A WORN BEARING. SHOP REPAIR. 1G72 3U H1NE 20030812000242003081200024 2003 8 12 HEEA088445 420030729A3417214175421101 ADC BELL 214 214ST 1182106SW COCKPIT MALFUNCTIONED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03 AIR DATA COMPUTER FAILED 4. STAYS ON CONSTANTLY. 2G72 4U H10SW 20030812000392003081200039EU 2003 8 12 BAQA088343 120030710A6230 BEARING BOLKMS117 BK117A1 5626010EU CONTROL ROD WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1784 7243 PBH SHIP. BEARINGS WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030812000812003081200081EU 2003 8 12 HEEA088646 120030720A6340614764021 INDICATOR AEROSPAS355 AS355* EU ROTOR TACH STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03732AE 2873 ROTOR NEEDLE STAYS AT ZERO WHEN STARTING AIRCRAFT AND WILL ONLY GO TO 100 RPM AT 100 PERCENT FLAT PITCH. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030812000822003081200082NE 2003 8 12 HEEA088651 220030723A74219550175400 IGNITER AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1D1 NE ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 ENGINE RIGHT SIDE IGNITER WORN. TO BE SENT TO VENDOR. 1G72 3U3 U H11EU E19EU 20030812000852003081200085SW 2003 8 12 HEEA088622 120030606A6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 33115 WORN BEARINGS. REPLACED LINK ASSY (2 EA) 212-010-711-003 DUE TO WORN BEARINGS; LINK ASSY (2 EA) 212-011-710-001 DUE TO WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030813000022003081300002EU 2003 8 13 HEEA088647 120030709A6340614764021 INDICATOR AEROSPAS355 AS355* EU ROTOR TACH READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03732AE 2873 3 PERCENT SPLIT IN FLIGHT ROTOR INDICATOR INDICATES LOW. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030813000052003081300005 2003 8 13 HEEA088592 420030731A2350A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 INTERPHONE INTERMITTENT ON COMM CHANNEL. SHOP REPAIR. 1G72 4U H4SW 20030813000062003081300006 2003 8 13 HEEA088593 420030724A2350A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 INTERPHONE PAINT MISSING FROM FACE PLATE. SHOP REPAIR. 1G72 4U H4SW 20030813000192003081300019 2003 8 13 HEEA088589 420030728A34217000788175 INDICATOR BELL 430 430 1182150SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03430XM 49073 TAKES 10 MINUTES TO CAGE. SHOWS 3 DEGREES LT BANK. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U RTH9SW 20030813000212003081300021SW 2003 8 13 HEEA088616 120030730A2910212076015001 CHECK VALVE BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 HYD SYSTEM CHECK VALVE LEAKING. 1G72 4U H4SW 20030813000232003081300023SW 2003 8 13 HEEA088562 120030721A243523081018 STARTER GEN BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032249Z18624 45753 FIRST START AFTER INSTALLATION GENERATOR WOULD NOT COME ON LINE. SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030813000302003081300030SW 2003 8 13 HEEA088574 120030721A6220412010100193FM ROTOR HEAD BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 MAIN ROTOR WILL NOT TRACK, SUSPECT RED AND ORANGE. SHOP REPAIR. 1G72 4U H4SW 20030813000442003081300044NM 2003 8 13 2003UALA00458 120030602A5313 STRINGER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 AFT CARGO PIT AT BS 1081-1087, STRINGER 37L IS CORRODED AT END FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SECTION AND SPLICE. 2L72 4F4 FRTA1NM E3NE 20030814000552003081400055NM 2003 8 14 UPS03M40954 120030604A5754 RIB DOUG MD11 MD11F 3023600NM NR 16 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 INSPECTION TYPE: C, LT NR 08 SLAT FOUND NR 16 SLAT AT X0S98 WITH I/B RIB CRACK AS MARKED. CRACKED SUPPORT LT NR 8 SLAT XOS98 REMOVED IAW SRM 51-35-01V2.R33. INSTALLED NEW SUPPORT RIB PER SRM 51-35-01 & 51-33-01V.2.R33. 2L73 4F RTA22WE 20030814000692003081400069SO 2003 8 14 SWIA200312116 120030522A5411 FRAME EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 RIGHT ENGINE FRAME 1 CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME 1 IAW SERVICE BULLETIN 120-54-0036. 2L72 4T RTA31SO 20030814000702003081400070SO 2003 8 14 SWIA200312117 120030522A5415 BRACKET EMB 120 EMB120ER 3260203SO HYDRAULIC PUMP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 RT ELECTRIC HYDRAULIC PUMP ATTACH BRACKET CRACKED. FOUND DURING C-CHECK INSPECTION. NEW BRACKET INSTALLED IAW SRM 120 51-10-02. 2L72 4T RTA31SO 20030814000822003081400082EA 2003 8 14 SWIA200312088 120030528A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 FS 521.0 LBL 36 FLOOR SUPPORT ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE AREA IAW CRJ REO 601R-53-61-117 REV A. 2L72 4F4 FRTA21EA E15NE 20030814000892003081400089SO 2003 8 14 SWIA200312169 120030707A5411 FRAME EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07188SW 120039 RT ENGINE FRAME 1 CRACKED. DISCOVERED DURING C-CHECK. REMOVED & REPLACED FRAME 1 PER SB 120-54-0036 WITH NEW P/N 120-0351-004. 2L72 4T RTA31SO 20030807000632003080700063NM 2003 8 7 03216425 120030804A3397 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27425FJ 3189 DURING MAINTENANCE INSPECTION A FORWARD SECTION OF THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL DISCOVERED A LOOSE CONNECTOR AND RECONNECTED IT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030807000652003080700065EU 2003 8 7 03213311 120030801A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27311UE 41029 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE FROM ROW 2-4A. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY BATTERY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030807000822003080700082EA 2003 8 7 03207676 120030726A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27676BR 7644 DURING MAINTENANCE INSPECTION THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030807000972003080700097NM 2003 8 7 EIA2003094 120030724A5230 STRUCTURE BOEING747 747212B 1384886NM CARGO DOOR CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 BULK PIT DOOR INTERIOR CRACKED AT 2ND FROM BOTTOM STOP ON LOWER FWD SIDE IN LOWER RADIUS. REMOVED AND REPLACED FRAME SECTION PER B747 SRM 51-30-02. 2L74 4F A20WE 20030807001172003080700117EU 2003 8 7 BAQA087950 120030711A2435524031 STARTER GEN AEROSPAS365 AS365N2 8680815EU ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME355 6417 STARTER GENERATOR INOPERATIVE. 1G72 3U RTH10EU 20030812000012003081200001NE 2003 8 12 HEEA088366 120030712A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH8145 760224 PRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OF TAIL ROTOR BLADE. 1G72 3U H1NE 20030812000502003081200050SW 2003 8 12 HEEA088451 120030717A3340099799100 SEARCH LIGHT BELL 206 206L1 1182107SW EXTERIOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035019F 45244 SEARCH LIGHT WILL NOT MOVE PROPERLY. 1G71 3U H2SW 20030812000672003081200067SW 2003 8 12 HEEA088554 120030802A7722212075067113 INDICATOR BELL 412 412 1182202SW ITT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 STICKS AT ZERO DURING START. SHOP REPAIR. 1G72 4U H4SW 20030812000722003081200072SW 2003 8 12 HEEA088583 120030712A3213412030437103 CAP BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 MLG CAP HAS WORN RUBBER. SHOP REPAIR. 1G72 4U H4SW 20030813000072003081300007SW 2003 8 13 HEEA088595 120030727A3340G62504 SEARCH LIGHT BELL 412 412 1182202SW EXTERIOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 BULB RETAINER SCREW BROKEN AND STUCK IN UNIT, BULB HOUSING LOOSE. SHOP REPAIR. 1G72 4U H4SW 20030827001652003082700165EU 2003 8 27 MALA030359 120030704A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING C-CHECK INSPECTION IN CVG, NR 3 SEAT RAIL FROM FRAME 18 TO 6 INCHES AFT OF FRAME 20 IS CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED IAW EO NR A53026. REFER TO 409 NR 128125, TASK CARD NR 0893A FOR DETAIL. A/C RELEASE DATE 7/25/03. 2H74 4F RTA49EU 20030909001882003090900188SW 2003 9 9 HEEA088938 120030109A5610407030115125A WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 WINDSHIELD CRAZED. 1G71 3U O H2SW 20030909001972003090900197SW 2003 9 9 ALGA088832 120030822A5320407030740116 SUPPORT BELL 407 407 1182206SW FUSELAGE CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03409AL 53494 CHAFED AND CRACKED AT DZUS RECEPTICALS.INSTALLED DOUBLERS AT RECEPTICAL LOCATIONS,AND CHAFE TAPE ALONG LENGTH OF SUPPORT. 1G71 3U O H2SW 20030909002112003090900211EU 2003 9 9 BAQA088794 120030819A771230802014 INDICATOR BOLKMS117 BK117A1 5626010EU TORQUE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03300CP2702 7249 TORQUE INDICATOR INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030909002212003090900221NM 2003 9 9 DHL2003782009 120030826A5250 MECHANISM BOEING727 727227 1384078NM COCKPIT DOOR DIRTY A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01769AT 21998 COCKPIT DOOR LATCH INOPERATIVE. FOUND COCKPIT DOOR PLUNGER MECHANISM STUCK WITH DUST AND DIRT DEBRIS. CLEANED AND LUBRICATED MECHANISM. OPS CHECKED GOOD. REF M/M 52-50-01 A/C OK FOR SERVICE. 2L73 4F A3WE 20030909002222003090900222EU 2003 9 9 DHL2003368010 120030827A2750 FLAP AIRBUS300 A300B4203 3930306EU WINGS MALFUNCTIONED A DHLAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SO01368DH 207 WHEN FLAPS WERE SELECTED, NO RESPONSE. ABNORMAL PROCEDURE (SLAT/FLAP ASYMMETRY OR JAM) WAS PERFORMED. PERFORMED SYSTEM OPS CHECK IAW M/M 27-51-00. OPS CHECK WAS GOOD. ALSO PERFORMED OPS WITH ELECTRIC PUMPS AND ENGINE DRIVEN PUMPS. OPERATION WAS NORMAL. 2L72 4F RTA35EU 20030910000162003091000016WP 2003 9 10 DHL2003604547 120030502A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING INBD L/E INNER LOWER DOUBLER CRACKED 2.500 AT XFS 598.500. REMOVED CRACKED INNER LOWER DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW INNER LOWER DOUBLER IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 26. CLEANED, TREATED AND PRIMED AREA AND NEW INNER LOWER DOUBLER IAW SRM 51-1-8B. INSTALLED NEW INNER LOWER DOUBLER ON RT OUTER WING INBD L/E AT XFS 598.500 IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000192003091000019WP 2003 9 10 DHL2003604551 120030513A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CENTER L/E FORMER CRACKED 0.500 AT XFS 354.000. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030910000642003091000064WP 2003 9 10 ABXA030338 120030804A531099577397 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 CRACKED SHEAR TIE FS 1021 JUST BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030910000912003091000091NM 2003 9 10 MWEA030308 120030813A216111508801 CONTROLLER BOEING717 717200 1383700NM A/C SYSTEM FAILED A MWEAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 GL31902ME 55166 RIGHT AIR CONDITION PACK OVERHEAT ALERT CAME ON. REMOVED AND REPLACED CABIN TEMPERATURE CONTROLLER. 2L72 4F TRA6WE 20030910001172003091000117NM 2003 9 10 DHL2003750006 120030718A3350 COVER BOEING727 7272M7 138407SNM PWA JT8 JT8D NE EMERGENCY LIGHT BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 EMERGENCY EXIT LIGHT COVER OVER CREW DOOR IS BROKEN. REMOVED AND REPLACED LIGHT COVER OVER CREW DOOR. WORK DONE IAW M/M 33-50-0. 2L73 4F4 F A3WE E2EA 20030910001212003091000121NM 2003 9 10 MWEA030338 120030827A5347593054767 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 SEAT TRACK NR 3 HAS VARIOUS AREAS OF CORROSION FROM STATION 1164-1250. AT STATION 1180 THE CORRSION IS VERY DEEP MOST LIKELY BEYOND LIMITS. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2L72 4F RTA6WE 20030910001352003091000135WP 2003 9 10 ARWA20030805 120030823A2130801813 SWITCH LKHEED1011 1011385115 5265015WP AIR DISTRIBUTIONUNSERVICEABLE A ARWAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO19308GB 193U1133 AVIONIC AIR, FWD AND MID LIGHT COMING ON IN FLIGHT. AIRCRAFT GOING INTO GROUND MODE WITH AIRCRAFT DEPRESSURIZING. FUEL DUMP, AND RETURN TO MIA FOR LANDING WITHOUT INCIDENT. REMOVED AND REPLACED LT AND RT GROUND. SAFETY SENSORS IAW CURRENT MFG. MANUAL CHAPTER 32. OPERATIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L73 4F A23WE 20030910001362003091000136NM 2003 9 10 03FDEA01320 120030815A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 GRAVEL DAMAGE ON FUSELAGE BELLY SKIN, BS 1050-1060 BETWEEN STR 26R AND 28R. REMOVED DAMAGED SKIN AT BS 1050-1060 BETWEEN STR 26 RT AND 28 RT AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3 & EA 7-5330-70493. 2L73 4F RTA3WE 20030910001402003091000140NM 2003 9 10 MWEA030350 120030827A5320593054497 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CORROSION FOUND AT STATION 1155 BETWEEN SEAT TRACK 2&3 ON FLOOR SUPPORT AROUND SCREW HOLES. FABRICATED AND INSTALLED NEW SUPPORT. 2L72 4F RTA6WE 20030813000472003081300047NM 2003 8 13 2003UALA00461 120030601A3350 BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29523UA 24932 AFT CABIN EEL LIGHTS BETWEEN ROW 23 AND 31 INOPERATIVE WITH TEST SWITCH AND MASTER SWITCH IN COCKPIT. REPLACED POWER SUPPLY BATTERY PACK. 2L72 4F4 FRTA2NM E17NE 20030813000762003081300076NM 2003 8 13 UPS03240846 120030611A2910 SWIVEL BOEING727 72725C 138400HNM HYD SYSTEM FAILED A IPXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO01951UP 19850 A-SYSTEM HYDRAULIC LOSS AFTER T/O DURING FLAP RETRACTION. AIR TURN BACK TO SDF. ALL CKLISTS ACCOMPLISHED. FOUND NR 4 SLAT ACTUATOR SWIVEL SPRING RETAINER BLOWOUT AND O-RINGS CAUSING MASSIVE LEAKAGE. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM 27-81-01. OPS CKS GOOD. 2L73 4F A3WE 20030813000822003081300082NM 2003 8 13 2003UALA00474 120030606A5321 FLOOR PANEL BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29198UA 28716 FWD PIT STA 720 FLOOR WEB CRACKED AT RBL 12 INCHES. CRACK LOCATED APPROX 8 INCHES BELOW T-CHORD OF FRAME & IS APPROXIMATELY 1 INCH LONG. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FILLER AND DOUBLER. 2L74 4F4 FRTA20WE E24NE 20030813000862003081300086NM 2003 8 13 2003UALA00485 120030606A5270 DOOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE E/E BAY OPEN A UALAA UNSCHED LANDING JW WARNING INDICATION INADEQUATE Q C CLCLIMB 1 WP29838UA 1477 ECAM WARNING AFTER TAKEOFF. AFT AVIONICS COMPARTMENT DOOR OPEN. RETURN TO FIELD. LUBRICATED AFT AVIONIC COMPARMENT DOOR PROXIMITY SWITCH 2L72 4F4 FRTA28NM E40NE 20030806000862003080600086NM 2003 8 6 AWXA200300810 120030709A5320D5347112420100 PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR PLATE Y-1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SHEAR PLATE Y-1292, BETWEEN FR 69 AND FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW SRM 51-42-11 PG 8-10 FIG 2. 2L72 4F RTA28NM 20030806001052003080600105SO 2003 8 6 C2XA03SH248 120030801A532014522178005 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV- DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001212003080600121SO 2003 8 6 C2XA03SH243 120030731A491014547494403 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, A CRACK WAS FOUND AT THE APU FIREWALL BY RT UPPER MOUNT. MAINTENANCE REMOVED DAMAGED AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001362003080600136SO 2003 8 6 C2XA03IA072 120030710A32347455501 CONTROL LEVER EMB 145 EMB145LR 3260212SO COCKPIT INTERMITTENT A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2716561 145610 THE CREW NOTED THAT THE LANDING GEAR WOULD NOT RAISE. THE PILOT BUMPED THE HANDLE AND THE GEAR CAME UP. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001582003080600158NM 2003 8 6 AWXA200300830 120030718A5415D546341520020500ANGLE AIRBUSA319 A319132 3930340NM NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28821AW 1406 DURING B-02 CHECK A .75 INCH CRACK WAS FOUND ON PANEL ATTACH ANGLE AT OUTBOARD SIDE OF NR 1 PYLON, RIB 8. MAINTENANCE CUT OUT DAMAGE ON ATTACH ANGLE AT OUTBOARD SIDE OF NR 1 PYLON, RIB 8; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A319 SRM 54-52-12, PG 215-220, FIG 203. 2L72 4F RTA28NM 20030806001632003080600163SO 2003 8 6 C2XA03TY087 120030704A532014523131011 SILL EMB 145 EMB145 3260210SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712957 145080 DURING A SCHEDULE 3-C INSPECTION, THE PAX DOOR CENTER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR CENTER SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030807000442003080700044EA 2003 8 7 03215701 120030803A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27701BR 7448 DURING MAINTENANCE INSPECTION, THE LT AND RT OVERWING EMERGENCY LAMPS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030812000062003081200006NE 2003 8 12 HEEA088406 120030724A62107615009043054 TIP CAP SKRSKYS76 S76C 8143008NE M/R BLADE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 MAIN ROTOR BLADE TIP CAP CRACKED. TO BE SENT TO VENDOR. 1G72 3U NCH1NE 20030812000452003081200045NE 2003 8 12 HEEA088410 120030718A33407655002005104 SEARCH LIGHT SKRSKYS76 S76A 8143006NE EXTERIOR INTERFERENCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 SEARCH LIGHT PRODUCING INTERFERENCE. SHOP REPAIR. 1G72 3U H1NE 20030813001022003081300102EA 2003 8 13 SWIA200312106 120030611A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07431SW 7536 1ST OVERHEAD EMERGENCY LIGHT IN CABIN INOP. REMOVED AND REPLACED THE LAMP. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030813001042003081300104WP 2003 8 13 AALA20030707 120030603A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21242AA 49255 DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY TAIL HANDLE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT STAIRWAY TAIL HANDLE EMERGENCY EXIT LIGHTS SPLICES. SYSTEM GROUND CHCKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001092003081300109NM 2003 8 13 AALA20030746 120030714A3397 WIRE HARNESS BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21360AA 24041 SFO - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT SEAT HARNESS PLUG AT SEAT 35. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030813001192003081300119WP 2003 8 13 AALA20030777 120030716A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21472AA 49647 DFW - DURING OVERNIGHT MAINTENANCE, BOTH EMERGENCY EXIT CEILING LIGHTS INBOARD OF AFT GALLEY DOOR INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001212003081300121NM 2003 8 13 USAA030118 120030711A5720 ANGLE BOEING737 737301 1384611NM NR 5 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND ANGLE HAS .375 INCH CRACK, NR 5 LE SLAT ACTUATOR ATTACH FITTING ANGLE. FABRICATED REPAIR ANGLE FROM 17-7 PH PER EA 76202. (M) 2L72 4F RTA16WE 20030813001512003081300151NM 2003 8 13 SWAA031661 120030724A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGERS CRACKED (3 EA) AT BS 380 AT STR 8L, BS 400 AT STR 8L AND BS 706 AT STR 11R. REPAIRED STRINGERS PER SRM. 2L72 4F RTA16WE 20030813001662003081300166 2003 8 13 SWAA031676 420030728A2565D31354 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030813001752003081300175NM 2003 8 13 SWAA031685 120030729A3350BR2013 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED PM CHECK, FOUND EEPLS COVER MISSING AT ROW NR 20. REMOVED AND REPLACED EEPLS LIGHT ASSY AT ROW NR 20 PER MM. 2L72 4F RTA16WE 20030813001922003081300192NM 2003 8 13 SWAA031560 120030715A53116546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, WL 148 AND RBL 9. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030813002022003081300202NM 2003 8 13 SWAA031650 120030721A531169353656 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030813002122003081300212 2003 8 13 SWAA031709 420030730A2565D31354 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030813002132003081300213NM 2003 8 13 SWAA031710 120030729A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) BS 727C AT STR 5R AND BS 727D AT STR 2R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030814000022003081400002NM 2003 8 14 SWAA031714 120030731A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 EEPLS COMING LOOSE IN CABIN. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030814000072003081400007NM 2003 8 14 SWAA031719 120030801A32601061226 UPLOCK SENSOR BOEING737 7373H4 1384600NM LT MLG FAULTY A SWAAO OTHER N FALSE WARNING CLCLIMB 1 SW29649SW 27719 LT MLG UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION, RECYCLED GEAR ALL GEAR LIGHTS NORMAL. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20030814000202003081400020 2003 8 14 SWAA031732 420030802A2565 GIRT BAR BOEING737 7377H4 1384404NM AFT SERVICE DOOROUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29430WN 33659 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030814000232003081400023NM 2003 8 14 SWAA031735 120030803A3230BACC18Z23R CIRCUIT BREAKER BOEING737 7373H4 1384600NM COCKPIT TRIPPED A SWAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SW29648SW 27718 DIVERSION, LANDING GEAR WOULD NOT RETRACT. FOUND, LANDING GEAR LEVER LATCH CIRCUIT BREAKER TRIPPED, RESET CIRCUIT BREAKER AND CYCLED GEAR PER MM. OPS CHECKED GOOD PER MM. 2L72 4F RTA16WE 20030814000312003081400031NM 2003 8 14 SWAA031702 120030730A3350BR2013 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29729SW 27861 DURING SCHEDULED CHECK, FOUND EEPLS INOP AT ROW NR 18. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20030814000332003081400033NM 2003 8 14 SWAA031704 120030730A273065C35943 BEARING BOEING737 7373H4 1384600NM BOTH ELEVATORS WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR INPUT ARM BEARINGS PER MM. 2L72 4F RTA16WE 20030910001432003091000143NM 2003 9 10 MWEA030335 120030827A532199366511 FLOOR PANEL DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CENTER CABIN FLOOR PANEL FRAME STATION 541-579 HAS SEVERAL INSERTS PULLING THROUGH, TOP LAYER IS PEELING OFF BOARD AND IS MISSING EDGE FILLER. REMOVED AND REPLACED INSERTS AND REPLACED EDGE FILLER AND INSTALLED COMPOSITE REPAIR DOUBLER. 2L72 4F RTA6WE 20030910001482003091000148NE 2003 9 10 MEX2003382 220030817A7321 FUEL CONTROL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LT ENGINE MALFUNCTIONED A ASMFD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW23160PL 49763 FLT 432 - GDL-MEX - AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE DIDN'T REACH THE ACCLERATION PARAMETERS REQUIRED FOR TAKEOFF. AIRCRAFT WAS SENT TO GDL HANGAR. THE MOISTURE TRAP FUEL CONTROL WAS SERVICED AND TRIM WAS PERFORMED IAW MM 73-20-03 AND 71-00-00, RESPECTIVELY. THE OPERATIONAL TEST WAS PERFORMED IAW MPCM 71-00-01, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20030910001492003091000149NM 2003 9 10 USAASB03126 120030802A21337110033 OUTFLOW VALVE BOEING737 7373B7 1384580NM CABIN PRESSURE LEAKING A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19397US 23319 DTW - FLT 390 - EN ROUTE FROM CLT TO DTW, AT FL350, A/C LOST PRESSURIZATION. CABIN CLIMBED TO 11,000 FT WITH CABIN ALTITUDE WARNING HORN SOUNDING. CREW ACCOM QRH PROCEDURES AND RAPID DESCENT TO 10,000 FEET. FLT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MX PERFORMED SINGLE PACK CONFIDENCE CHECK. R&R AFT OUTFLOW VALVE, ALL HEAT EXCHANGERS, DELTA P MODULE, LT ACM, FWD CARGO DOOR SEAL AND FWD RADIO ALTIMERTER ANTENNA GASKET. RIGGED FORWARD SVC DOOR AND ACCOM TEMP REPAIR TO A THREE INCH CRACK IN FUSELAGE AT STA 520R, STRINGER 12. OPS AND LEAK CHECKED ALL WORK PERFORMED. ACCOMPLISHED SATISFACTORY TEST FLIGHT FOR PRESSURIZATION SYSTEM. (M) 2L72 4F RTA16WE 20030910001632003091000163EA 2003 9 10 ASOA03357 120030805A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11872AS 7542 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS ONE TO FIVE WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS ONE TO FIVE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030910001712003091000171SO 2003 9 10 SIMA200321808 120030731A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND AT FRAME 53. BLENDED THE CHAFE AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2577 AND EMB SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02 FIGURE 201. (M) 2L72 4F RTT00011AT 20030910001832003091000183SO 2003 9 10 SIMA200322505 120030809A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21819AE 145566 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUTOUT OF THE CORRODED SECTION OF THE OMEGA BEAM. FABRICATED A REPAIR DOUBLER, FILLER TWO SHIMS AND A REPAIR PLATE. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 53-21-10, FIGURE 201. (M) 2L72 4F RTT00011AT 20030910002002003091000200WP 2003 9 10 AALA20030875 120030515A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21964TW 53614 MCI - FOUND CORROSION ON CARGO FLOOR SUPPORT AT STATION 1212, 6 INCHES RBL TO 10 INCHES LBL TOP SIDE AND BOTTOM SIDE. REPLACED WITH NEW MPN 5936597-509, RIVETS WERE INSTALLED PER SRM 51-30-02. (M) 2L72 4F RTA6WE 20030910002072003091000207EU 2003 9 10 MALA030382 120030817A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15407XJ 340B407 CABIN CENTER SEAT AISLE TRACK BL 0 HAS CORROSION OUT OF LIMITS. PERFORMED REPAIR BY INSTALLING NEW SEAT TRACK ASSEMBLY AT BL 0 BETWEEN STA 297-354 IAW EO NR S53060. REFER TO LOG PAGE NR 177362 FOR DETAIL. 2L72 4T RTA52EU 20030910002112003091000211EU 2003 9 10 MALA030351 120030725A2612 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY MALFUNCTIONED A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15402XJ 340B402 DURING TAKEOFF ON FLIGHT NR 3342, AVIONIC SMOKE DETECTION LIGHT ILLUMINATED. ABORTED TAKEOFF. AVIONICS SMOKE LIGHT ILLUMINATED ON TAKEOFF, PERFORMED HIGH SPEED ABORT AND USED MAX BRAKING. MECHANIC SIGN OFF: PERFORMED REJECTED TAKEOFF INSPECTION IAW SAAB AMM 05-50-00. ALL CHECKS GOOD. DEFERRED AVIONICS SMOKE LIGHT IAW 26-13-3B ENTERED INTO DMR AND MXC NOTIFIED. MAINTENANCE REPLACED DETECTOR. 2L72 4T RTA52EU 20030911000022003091100002NM 2003 9 11 03FDEA01186 120030725A5753ARC050311 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. LT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-71807. 2L73 4F RTA22WE 20030911000032003091100003 2003 9 11 DHL2003873011 420030809A2214 INDICATOR DOUG DC8 DC873F 302199FWP TRIM INOPERATIVE A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01873SJ 46091 SMOKE IN COCKPIT COMING FRON HYD PITCH TRIM AREA. CHECKED AREA FOUND LONGITUDINAL TRIM INDICATOR LIGHT PLATE BAD, ISOLATED WIRES AND DEFERRED LIGHT PLATE. SEE ITEM 7M PAGE 279774. LONGITUDINAL TRIM INDICATOR LIGHT PLATE IS INOPERATIVE. ITEM TRANSFERRED TO DMI 13789 BY MEL 33-1. PLACARD INSTALLED. REFER TO DMI 13789 LONGITUDINAL TRIM INDICATOR LIGHT PLATE IS INOPERATIVE. PART NOT IN STOCK. DMI REMAINS OPEN 2L74 4F RT4A25 20030911000052003091100005NM 2003 9 11 03FDEA01253 120030812A5311 FRAME BOEING727 727200 138407ENM FUSELAGE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 FWD CARGO BAY 680 FRAME BENT AT RBL 35 BETWEEN STR 24R 26 25R. FRAME AT BS 680, RBL 35 BETWEEN STR 24 & 25 RT OUT OF LIMITS. REPAIRED FRAME IAW FED EX EA 7-5310-72507, SRM 53-10-1 & 51-40-3 FIG 1. 2L73 4F RTA3WE 20030911000092003091100009WP 2003 9 11 03FDEA01229 120030808A3610 MANIFOLD DOUG DC10 DC1010 3022110WP PNEU SYS FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25550FE 46521 ABOUT 1 50 2FO FLT AT FL370 LEVEL 3 23 MANIFOLD FAIL OCCURRED. SECURED 232 ENG TO IDLE PER LIST WITH 232 BLEED OFF DIVERTED KDEN. AACN RELEASED FOR SERVICE PER MEL 2 FCDL 36-23-01-02 CATEGORY 3 AC EXPIRATION 3A 18AUG 03 FACT: CHECKED ELEMENTS_D1-50, D1-29 AND D1-27 ALL CHECKED NORMAL. FOUND D1-28 SHORTED TO GROUND PER MD10 WDM 36-23-02 AND CHAP 20 STANDARD MAINTENANCE PRACTICES. REPLACED ELEMENT D1-28 SYSTEM GND TEST NORMAL PER M/M 36-26 2 MANIFOLD FAIL CHECKED OK ON RUN. 2L73 4F A22WE 20030911000152003091100015NM 2003 9 11 03FDEA01309 120030808A5753ARC0503403 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING - O/B T/E FLAP, O/B FWD FLAP HINGE FITTING FOUND HYD ACTUATOR'S INBOARD MOUNT HOLE SPOT FACES WITH CORROSION. LT WING O/B FLAP, O/B FWD HINGE FITTING HYD ACTUATOR INBOARD MOUNT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030909002562003090900256WP 2003 9 9 AMTA200301053 120030811A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND LOWER LEFT FUSELAGE BELLY SKIN GOUGED. REPAIRED AREA IAW ER/A L10-53R-5274. (M) 2L73 4F A23WE 20030910000282003091000028EU 2003 9 10 BAQA088186 120030709A6220365A3118100451 STARFLEX AEROSPSA365 SA365N 8680669EU MAIN ROTOR DEBONDED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM484 6396 STAR ARM BUSHING DEBONDED. REPLACED WITH SERVICEABLE UNIT. THIS PART WAS SENT TO AEC DIRECTLY FROM OUR SITE IN ROCHESTER, IN W/O A MMIR. 1G72 3U H10EU 20030910000382003091000038SW 2003 9 10 HEEA088218 120030717A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 STEP ACTUATOR OPERATION INTERMITTENT. 1G72 4U H4SW 20030910001242003091000124NM 2003 9 10 MWEA030340 120030827A534759305475 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 SEAT TRACK NR 4 HAS MANY AREAS OF CORROSION STATION 200-258. FABRICATED AND INSTALLED SEAT TRACK AND SPLICE ASSEMBLY. 2L72 4F RTA6WE 20030910001952003091000195NM 2003 9 10 USAASB03129 120030805A523010608211 SEAL BOEING737 7373B7 1384580NM CARGO DOOR LOOSE A USAAO OTHER O OTHER CRCRUISE 1 EA19375US 22954 MSY - FLT 997 - APPROXIMATELY ONE HOUR INTO FLIGHT, PRESSURIZATION WAS LOST. CREW SELECTED TO STANDBY. CABIN ALTITUDE CONTINUED TO CLIMB AT APPROXIMATELY 100 FEET PER MINUTE TO 9000 FEET. FLIGHT DESCENDED TO FL 250 WHERE CABIN ALTITUDE STABILIZED AT 8000 FEET. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND ABOUT 18 INCH OF THE FORWARD CARGO DOOR SEAL IN THE LOWER AFT CORNER OUT OF THE TRACK. THE SEAL WAS SECURED. (M) 2L72 4F RTA16WE 20030910002222003091000222EU 2003 9 10 MALA030393 120030828A3320 SOCKET BAC 146 AVRO146RJ85A1500097EU CABIN BURNED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15533XJ E2367 DURING FLIGHT NR 3532, ELECTRICAL SMOKE SMELL IN ROWS 8 & 9. MAINTENANCE REPLACED BURNT SOCKET OVERHEAD LIGHTING AT ROW 8, INSPECTED WIRING, NO FURTHER DAMAGED NOTED, ALL WORK PERFORMED IAW CHP 33. 2H74 4F RTA49EU 20030911000182003091100018NM 2003 9 11 03FDEA01312 120030809A5753ARC0503404 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT WING O/B FLAP O/B HINGE ( A/C SIDE ) CORROSION FOUND ON UPPER ATTACHMENT HOLE I/B BORE. RT WING O/B FLAP O/B HINGE ( A/C SIDE ) UPPER ATTACHMENT I/B HOLE BORE REPAIERD AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030911000222003091100022NM 2003 9 11 03FDEA01099 120030706A5710 PIVOT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LT INBD FLAP,OUTBOARD HINGE (FLAP SIDE ) INBD AND OUTBOARD PIVOT BORES CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. 2 AND FEDEX EA - 1-5750-71842 WINGS - TRAILING EDGE FLAPS - INBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKET CORROSION REPAIRED. 2L73 4F RTA22WE 20030911000232003091100023NM 2003 9 11 03FDEA01100 120030708A5753 PIVOT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LT INBD FLAP OUTBD HINGE (FLAP SIDE ) OUTBD PIVOT BORE CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. 2 AND FEDEX EA - 1-5750-71842 WINGS - TRAILING EDGE FLAPS - INBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKET CORROSION REPAIRED. 2L73 4F RTA22WE 20030911000352003091100035NM 2003 9 11 03FDEA01255 120030812A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 CORROSION AFT CARGO BAY FLOORBEAM LOWER FLANGE HAS CORROSION AT FASTENER HOLES BS 1070 WL 200 2C LBL 40 TO RBL 53. BLENDED DAMAGE. COMPLIED WITH EA 7-5310-72306. REPAIRED 1070 FLOORBEAM AT BS 1070 WL 200, LBL 40 TO RBL 40. 2L73 4F RTA3WE 20030911000382003091100038EA 2003 9 11 SWIA200312319 120030801A5315 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. (DISCOVERED DURING C-CHECK) ANGLE REPAIRED IAW CRJ REO 601R5361117 REV. ''A''. REF. RII 53-401. 2L72 4F4 FRTA21EA E15NE 20030911000512003091100051CE 2003 9 11 DXTA200300073 120030721A2821 FILTER RAYTHNDH125 HAWKER800XP 7150012CE FUEL SYSTEM DAMAGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07872QS 258472 NR 1 ENG FUEL LIGHT CAME ON DURING TAKE OFF ROLL (LIGHT CAME ON AT 50 KIAS), LIGHT EXTINGUISHED WHEN POWER REDUCED. - REMOVED NR 1 AND 2 ENG FUEL FILTERS PER HONEYWELL TFE731 MM CH 73-21-02. RAN NR 1 AND 2 ENG TOT/O POWER, NO DEFECTS NOTED. 2L72 4F RTA3EU 20030911000572003091100057NM 2003 9 11 2003UALA00608 120030805A5330 SKIN BOEING747 747422 1384935NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29197UA 26901 SKIN DENTED AT STA 760 APROX. 3 INCHES ABOVE STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER REPAIR. 2L74 4F4 FRTA20WE E46NE 20030911000832003091100083WP 2003 9 11 DHL2003873536 120030624A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAING CARGO COMPT NR 2 TRACK LUG WORN, STA 1590.000 - 1680.000. REMOVED NR 2 TRACK DAMAGED SEGMENT IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT WITH NEW FASTENERS IAW SRM 51-3-0 PG 1. 2L74 4F4 FRT4A25 E2GL 20030911000982003091100098WP 2003 9 11 DHL2003873507 120030611A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OUTBD L/E FORMER CRACKED 0.250 AT XFS 882.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED REINFORCING ANGLE IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9,10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001152003091100115NM 2003 9 11 03FDEA01293 120030806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBD FLAP OUTBD HINGE ( A/C SIDE ) PIVOT HOLE CORRODED AT BORE AND SPOT FACES. RT WING OUTBD FLAP OUTBD HINGE ( A/C SIDE ) PIVOT HOLE BORE AND SPOT FACES ( FWD & AFT FACE ) REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030911001342003091100134CE 2003 9 11 MTNA20034 120030812A7331 GAUGE CESSNA208 208B 2073701CE FUEL FLOW FLUCTUATES A MTNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO33715FX 208B0440 DURING CLIMB OUT FROM PKB TO HTS THE PILOT NOTICED THE FUEL FLOW GAUGE FLUCTUATING. HE CHECKED THE PAR AND FOUND THE SAME INDICATION. THE PILOT ELECTED TO TURN BACK TO PKB AND LANDED WITH OUT INCIDENT. 1H71 3T A37CE 20030911001812003091100181NM 2003 9 11 DHL2003754013 120030726A2613 CONNECTOR BOEING727 727223 1384074NM OVERHEAT SENSOR DIRTY A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 LOWER AFT BODY OVERHEAT WILL NOT TEST. CLEANED AND RE-SEALED CONNECTOR PLUG ON LOWER AFT BODY OVERHEAT SENSOR, TESTED UNIT IAW M/M 26-14-01, OPS CHECKED NORMAL. 2L73 4F A3WE 20030911001862003091100186WP 2003 9 11 AALA20030332 120030304A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND FRAME CRACKED AT STATION 1174 AND LONGERON 6L AT BIN ATTACH POINTS TWO EACH. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-30. (M) 2L72 4F A6WE 20030911002052003091100205WP 2003 9 11 AALA20030326 120030311A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21567AM 53293 TUL - FOUND STATION 1309, L18R JUST BELOW RIGHT ENGINE PYLON HAS GOUGE, DENT AND SCRATCH APPROX 6 INCHES LONG, APPEARS PREVIOUSLY WORKED. BLENDED AND INSTALLED TWO ROWS DOBLER PER 53-04-38. (M) 2L72 4F RTA6WE 20030911002092003091100209WP 2003 9 11 AALA20030329 120030311A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21567AM 53293 TUL - FOUND CORROSION BOTTOM NR 3 SEAT TRACK STATION 1177-1178. REMOVED CORRODED SECTION OF TRACK, SPLICED IN NEW SECTION FROM STATION 1174-1309 PER SRM 53-05 FIG 4F. (M) 2L72 4F RTA6WE 20030909002732003090900273SO 2003 9 9 RAIA00307194 120030718A27403621001007 CONTROL UNIT EMB 145 EMB145 3260210SO HORIZ STAB INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03809HK5914 145187 5324-RIC- PITCH TRIM NR 2 FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT. 2L72 4F RTT00011AT 20030910000012003091000001EU 2003 9 10 BAQA088802 120030820A28221176415103 PUMP BOLKMS117 BK117A3 5626015EU FUEL BOOST INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03932CJ2110 7024 BOOSTER PUMP WOULD NOT PUMP. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030910000132003091000013EU 2003 9 10 BAQA088164 120030721A6340L771M40C1003 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE TACH ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH147 0131 ROTOR INDICATOR ERRATIC. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030910000892003091000089GL 2003 9 10 AWXA200300868 220030730A72301663M24P01 BLADE BOEING737 73733A 1384673NM CFMINTCFM56 CFM563B1US GL NR 2 COMPRESSOR DAMAGED A AWXAO OTHER C F.O.D. NRNOT REPORTED 1 WP28174AW 23633 721850 FORIEGN OBJECT DAMAGE WAS FOUND ON THE NR 2 ENGINE FAN BLADES. MAINTENANCE PERFORMED A FOD INSPECTION OF THE NO. 2 ENGINE IAW T/C I8M05030, AND BORESCOPED THE HIGH PRESSURE TURBINE (HTP) IAW T/C I5M72017, NO DAMAGE WAS NOTED TO HPT. REMOVED AND REPLACED ALL FAN BLADES ON THE NO. 2 ENGINE IAW AMM 72-31-02. NR 2 ENGINE VIBRATION BEYOND LIMITS, REMOVED AND REPLACED ENGINE IAW T/C R5M71001, F8M71001, AND F8M75001, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20030910000922003091000092WP 2003 9 10 MWEA030309 120030814A2751ST12AF TRANSMITTER DOUG DC9 DC932 3022066WP T/E FLAP FAULTY A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31207ME 47794 STALL INDICATION FAILURE LIGHT CAME. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER. PERFORMED ADJUSTMENT TEST OF STALL SYSTEM CHECKED GOOD. 2L72 4F A6WE 20030910001022003091000102NM 2003 9 10 MWEA030355 120030902A5347593054734 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 LIGHT CORROSION ON NUMBER 6 SEAT TRACK STATION 755. FABRICATED INSTALLED REPAIR SEAT TRACK. 2L72 4F RTA6WE 20030910001602003091000160EA 2003 9 10 ASOA03361 120030807A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030910001662003091000166SO 2003 9 10 SIMA200321806 120030718A532014522460013 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 ABI - THIS LEVEL TWO ITEM FOUND DURING AN IMBV INSPECTION, THE CENTER BEAM WEB EXTENSION CORRODED AT FRAMES 22-23. REMOVED CORRODED CENTER BEAM WEB EXTENSION AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 51-20-03, 51-40-06, 51-40-02. (M) 2L72 4F RTT00011AT 20030910001972003091000197NE 2003 9 10 MEX2003375 220030819A7230500050101J DISK DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED A ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23946AS 49658 FLT 907 - MTY-MEX - DURING OVERNIGHT CHECK, DETECTED RIGHT ENGINE DAMAGED FOR FOD, WITH 2 BLADES OUT OF LIMITS IN THE FIRST STAGE COMPRESSOR. THE BOROSCOPIC INSPECTION WAS PERFORMED AND THE C1 DISK WAS REPLACED IAW MM 72-00-33, ALL CORRECT. THE RIGHT ENGINE WAS STARTED IAW MM 71-00-00, ALL TESTS CORRECT. (M) 2L72 4F4 FRT E9NE 20030911000362003091100036NM 2003 9 11 03FDEA01256 120030812A5310 DOOR FRAME BOEING727 727200 138407ENM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 WHILE WORKING CARD N00281 2C FOUND CRACK ON 2FH LWR CORNER WEB OF ENTRY DOOR. 2L73 4F RTA3WE 20030814000342003081400034NM 2003 8 14 UPS03241062 120030717A1430 FASTENER BOEING727 72725C 138400HNM SPAR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, FOLLOWING HFEC INSPECTION AROUND FASTENER HOLES IN O/B FLANGES OF VERTICAL FIN FRONT SPAR FORGING, 2 CRACKS FOUND COMING FROM FASTENER HOLES ON LEFT SIDE. CRACKS STOP DRILLED IAW DRG 65-81528. REFERENCE SMRO EO 2003-041-001 FOR REWORK. REFERENCE UPS EO B727-5530-19081. 2L73 4F A3WE 20030814000532003081400053NM 2003 8 14 2003UALA00592 120030724A335020131 BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 EMERGENCY ELECTRICAL LIGHTING (EEL) INOPERATIVE FROM ROW 15 TO AFT OF AIRPLANE. REPLACED POWER SUPPLY AT STA 755. 2L72 4F4 FRTA16WE E2GL 20030814000672003081400067EA 2003 8 14 SWIA200312225 120030725A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 REINFORCEMENT ANGLE AND FRAME ON RIGHT SIDE OF FS 640.00 BETWEEN STR 9 AND STR 12 IS CRACKED NEAR TOP OF BOX BEAM. DISCOVERED DURING A CHECK INSPECTION. REPLACED RIGHT QUARTER FRAME AT FS 640 WITH SERVICEABLE UNIT IAW SRM 51-42-06 AND 51-42-20. 2L72 4F RTA21EA 20030814000762003081400076NM 2003 8 14 CALA0300376 120030630A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 MAINTENANCE FOUND THE INNER CHORD ON THE LT FRAME AT STA 616 CRACKED. THE AREA WAS REPAIRED IAW ECRA 5311-01154. 2L72 4F RTA16WE 20030814000902003081400090SO 2003 8 14 SWIA200312170 120030624A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07583SW 120351 EMERGENCY EXIT ROW 6C LIGHT OUT. INSTALLED SERVICEABLE BULB AT 6C EMERGENCY EXIT OVERHEAD LIGHT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030807000342003080700034EU 2003 8 7 USAABA03021 120030621A2430 GCU AIRBUS330 A330323 3930335EU NR 2 GENERATOR FAILED A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19675US 0370 EN ROUTE FROM FRA TO PHL, CREW RECEIVED THE ECAM WARNING 'E'EC GEN 2 FAULT.' THE GENERATOR WOULD NOT RESET. CREW ATTEMPTED TO START THE APU. THE APU WOULD NOT START AT FL360 OR FL300. APU FINALLY DID START AT 14,000 FT. MAINTENANCE REPLACED THE GCU, BUT FINAL FIX WAS TO REPLACE THE IDG. AFTER EXTENSIVE T/S, THE APU WAS REPLACED. (M) 2L72 4F RTA46NM 20030807000452003080700045EA 2003 8 7 COMA0360342 120030725A79106087T04P05 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT ENGINE CLOGGED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01807CA5953 7364 807655 FLIGHT 5655 LT ENGINE OIL PRESSURE WARNING. SCAVANGE LUBE PUMP INLET SCREENS CLOGGED. REPLACED LUBE PUMP. 2L72 4F4 FRTA21EA E15NE 20030812000172003081200017NE 2003 8 12 HEEA088436 120030725A62107615009100053 BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR UNBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 13945 760193 MAIN ROTOR BLADE NICKEL ABRASION STRIP IS UNBONDED ON THE INBOARD END. 1G72 3U H1NE 20030812000632003081200063NE 2003 8 12 HEEA088523 220030719A7412103815504 EXCITER BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 EXCITER CORRODED. TO BE SENT TO VENDOR. 1G72 4U4 U H4SW E22EA 20030902001882003090200188NM 2003 9 2 03FDEA00976 120030623A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 FLOOR SEAT TRACK AT STA 635 LH X=27.5 CRACKED. DAMAGED FLOOR TRACK AREA FROM BS625 TO BS 665 LH X=27.5 CARRIED OUT SEAT TRACK REPAIR IAW SRM 53-70-00 VOL. I. 2L73 4F RTA22WE 20030903000242003090300024WP 2003 9 3 MEX2003263 120030407A3260833605 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP MLG FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23583MD1068110681 49659 AIRCRAFT ARRIVED WITH CAPTAIN REPORT THAT DURING FINAL APPROACH THE NOSE LANDING GEAR LIGHT TURNED RED AND NOSE LANDING GEAR ALARM CAME ON. AFTER MISSED APPROACH AND A NOSE LANDING GEAR CYCLE, THE GREEN LIGHTS COME ON. AIRCRAFT WAS SENT TO THE HANGAR FOR ITS REVISION AND DURING OVERNIGHT SERVICE THE PROXIMITY SWITCH AND SENSOR D1-32 WERE REPLACED IAW MM, ALL TEST CORRECT. 2L72 4F RTA6WE 20030903000502003090300050EA 2003 9 3 SWIA200312171 120030706A2613 SWITCH CNDAIRCL600 CL6002B19 1900309EA FIRE PANEL INOPERATIVE A SWIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM07925SW 7682 ''CARGO BOTTLE LOW MSG'' DURING FLIGHT. FOLLOWED QRH AND LANDED AT NEAREST SUITABLE AIRPORT. REMOVED AND CLEANED SWITCHES ON FIRE PANEL. SYSTEM CHECKS GOOD. 2L72 4F RTA21EA 20030903000572003090300057WP 2003 9 3 03FDEA01104 120030716A1430 BOLT DOUG DC10 DC1030 3023501WP EXHAUST NOZZLE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 NR 1 ENGINE EXHAUST NOZZLE HAS LOOSE AND MISSING HARDWARE AROUND THE ATTACH POINT TO CASE. CLOSING ACTION ON 06/16/03. ON N/R S00104. REPLACED LOOSE AND MISSING BOLT'S AND TORQUED IAW M/M 78-11-02-2. 2L73 4F A22WE 20030903000762003090300076EU 2003 9 3 MALA030341 120030712A2930HE832731 SWITCH BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15531XJ E2365 DURING FLIGHT 3554, CREW REPORTED GREEN HYDRAULIC HIGH TEMP LIGHT INFLIGHT TO CVG. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED GREEN SYSTEM TEMPERATURE SWITCH PN HE83273-1, SN/ON 1304TW, OFF/1358TW. IAW S9-33-11-201. RAN ENGINES AT OR ABOVE 72 PERCENT- N1, NO HI TEMP. CYCLED ROLL SPOILERS AND AIR BRAKE STILL NO HI-TEMP LIGHT AFTER 25 MINUTES. ALL SYSTEMS CHECK GOOD. OK FOR SERVICE. 2H74 4F RTA49EU 20030903000782003090300078EA 2003 9 3 SWIA200312177 120030710A7910 CHECK VALVE CNDAIRCL600 CL6002B19 1900309EA RT ENG OIL MALFUNCTIONED A SWIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM07457SW 7773 RT ENGINE OIL DROPPED TO 30 PSI AND ENG OIL LOW PRESSURE WARNING ILLUMINATED. DIVERTED TO JAN. REMOVE AND REPLACE OIL REPLENISHMENT SYSTEM CHECK VALVE IAW CL 600 79-12-13. OPS AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20030911000462003091100046WP 2003 9 11 DHL2003873569 120030704A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OB L/E PLATING CORRODED BETWEEN STA XFS.710.000 AND XW.761.000. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED SKIN SEGMENT IAW. PERFORMED NDT INSPECTION IAW DC8 NDTSPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA, FABRICATED TWO REPAIR DOUBLERS, A SHIM AND A REPAIR TRIPPLER, ED-3478. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLERS AND TRIPLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLERS AND TRIPLER AND SHIM ON LT WING OB L/E SURFACE (BETWEEN STA. XFS.710.000 - XW.761.000) USING NEW FASTENERS. 2L74 4F RT4A25 20030911000482003091100048WP 2003 9 11 DHL2003873562 120030703A575346495971 FITTING DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FITTING IN LT OUTBD FLAP WELL CRACKED 1.500 AT STA XFS.434.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030911000492003091100049NE 2003 9 11 AWXA200301001 220030828A7397 PIN BOEING757 757225 1384959NM RROYCERB211 RB211535* NE CONNECTOR DAMAGED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28913AW11441 22207 ON TAKEOFF, NR 2 ENG DID NOT MAKE REQ POWER (EPR 1.61), ONLY REACHED EPR 1.41, ALL OTHER INDS NORM, REJECTED TAKEOFF AT 100 KTS. MAINT CHECKED THROTTLE WITH PART POWER PINS INSTALLED, BOTH THROTTLES WERE IN ALIGNMENT. RAN ENG WITH RT ELC SYS ON & LT ELC OFF, (INOP LIGHT ON STEADY), LINED UP N1 AT 85.9 WITH NR 2 THROTTLE 4 KNOBS FORWARD, ALL ENG PARAMETERS MATCH, BUT NR 2 EPR LIMITED AT 1.43, TURNED RT ELC OFF, RESULTS SAME. COMPLIED WITH P1 TEST, LEAK LESS THAN .5 AT 392 KTS. REPLACED NR 2 ENG EEC & RAN ENG, NR 2 ENG MADE TAKEOFF POWER BUT "INOP" LIGHT CAME ON WITH RT EEC MSG, CLEARED ON ENG SHUTDOWN. MAINT SWAPPED LT & RT EEC'S, BITE CHECK OF RT ENG IND NO FAULTS. FOUND PIN 4 AT (D1384) DEDICATED STATOR GEN BA2L72 4F4 FRTA2NM E12EU 20030911000802003091100080WP 2003 9 11 DHL2003873511 120030617A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING OB L/E FORMER CRACKED 0.250 AT XFS.822.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT XFS.822.500 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RT OUTER WING L/E WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001592003091100159WP 2003 9 11 AALA20030324 120030306A5320 SILL DOUG DC9 DC982 3022082WP CARGO DOOR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21459AA 49564 AFT CARGO DOOR SILL DAMAGED FS 1160. INSTALLED REPAIR PER AARD 53-10-00-3 CONDITOIN IV AND EOS 80559. (M) 2L72 4F A6WE 20030911001692003091100169WP 2003 9 11 UPS03841040 120030708A5315 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, FLOORBEAM CORRODED AT STA 980 LBL 58 MAIN CABIN. REMOVED CORROSION, OUT OF LIMITS IAW DC8 SRM 53-2-0, 51-1-8; CUT OUT DAMAGE IAW DC8 SRM 53-2-0. FABBED FILLER, ANGLE, SHIM FOR WEB IAW DC8 SRM 53-2-0 FIG 1B&G; ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED F ILLER, SHIM, 2 EA ANGLES AND WEB STIFFENER IAW DC8 SRM 53-2-0 FIG 1B &G, 51-1-24, 51-1-20D. FAB & INSTALLED ANGLE SPLICES IAW DC8 SRM 53-2-0. 2L74 4F RT4A25 20030911001832003091100183NM 2003 9 11 DHL2003753005 120030802A3350 BATTERY BOEING727 727223 1384074NM CABIN DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01753DH 22468 EMERGENCY EXIT SIGN OVER THE CREW DOOR BATTERIES ARE DEAD. REMOVED AND REPLACED EMERGENCY EXIT SIGN BATTERIES IAW B727 M/M 33-50-1. OPERATIONAL CHECK SERVICEABLE. 2L73 4F A3WE 20030911001842003091100184EU 2003 9 11 DHL2003365011 120030805A3350312101 POWER SUPPLY AIRBUS300 A300B4203 3930306EU CABIN DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01365DH 149 L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGE SUPPLY UNIT, OPS CHECKED OK IAW 33-51-00. 2L72 4F RTA35EU 20030911001982003091100198EU 2003 9 11 AALA20020439 120030403A5320 RIB AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 TUL - FOUND RIGHT RIB CRACKED AT UPPER AREA END AND MARKED FRAME 13A AND FRAME 14. REPAIRED PER AARD 53-10-00 AND PER DRAWING 12R53610650 AND ESO 30595 DATED 4-2-2002. (M) 2L72 4F RTA35EU 20030911002182003091100218EU 2003 9 11 DHL2003363005 120030814A25605MA21251 SMOKE BARRIER AIRBUS300 A300B4203 3930306EU CABIN TORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 SMOKE BARRIER TORN AWAY IN 4 PLACES FROM MOUNTING ANGLE. REPLACED SMOKE CURTAIN IAW M/M 25-58-00. OPS GOOD. 2L72 4F RTA35EU 20030911002232003091100223NM 2003 9 11 DHL2003784004 120030819A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01767AT 22001 ENGINE DETECTION CIRCUIT GROUND NR 3 LIGHT ILLUMINATED ON P6-3. TRANSFERRED NR 3 ENGINE FIRE WARNING GROUND FAULT DETECTOR SYSTEM TO DMI NR 13879, MEL REF 26-9 CAT "C". DMI EXPIRES IN 10 CONSECUTIVE CALENDAR DAYS. PLACARD INSTALLED. REPOSITIONED LOOP, SYSTEM OPS CHECKED GOOD PER M/M 26-11-001. THIS CLEARS DMI. PLACARD REMOVED. 2L73 4F A3WE 20030912000502003091200050WP 2003 9 12 DHL2003604538 120030430A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING INBD L/E FORMER CRACKED 0.250 STA XFS 691.250. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D PG 9-10, SRM 51-1-20D, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000632003091200063NM 2003 9 12 DHL2003752005 120030828A3610BACH7D0161DL FLEX LINE BOEING727 727223 1384074NM NR 1 ENGINE LEAKING A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01752DH 22466 ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF AT MAX THRUST. THRUST REDUCTION TO CLIMB LIGHT EXTINGUISHED. PERFORMED ABNORMAL PROCEDURE OVERHEAT LIGHT REMAIN EXTINGUISHED. REMOVED AND REPLACED 13TH STAGE FLEX LINE P/N: BACH7D0161DL IAW B727 M/M 20-10-12. OPS CHECKED NORMAL IAW JRH CHAPTER 7.5. 2L73 4F A3WE 20030912000692003091200069WP 2003 9 12 DHL2003604786 120030616A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT ACCESSORY COMPT L-30R CORRODED BETWEEN STA 1640.000 AND STA 1660.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 8. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION FROM L-30R (STA 1640.000 - 1660.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT LONGERON DAMAGED SEGMENT IAW SRM 53-2-2 FIG 8. FABRICATED STRAPS IAW SRM 53-2-2 FIG 8. CLEANED, TREATED, PRIMED AREA, STRAPS AND NEW LONGERON SEGMENT IAW SRM 51-1-8B. INSTALLED NEW LONGERON AND STRAPS WITH NEW FASTENERS IAW SRM 53-2-2 FIG 8, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030910000882003091000088EU 2003 9 10 DHL2003365013 120030805A3260141FL0D3 DOWNLOCK SWITCH AIRBUS300 A300B4203 3930306EU NLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING APAPPROACH 1 SO01365DH 149 NO GREEN NOSE LIGHT ON S/O PANEL FOR LANDING GEAR. GPWS TOO LOW GEAR FORWARD GEAR INDICATIONS NORMAL. REMOVED AND REPLACED SYSTEM 2 NLG DOWNLOCK MICROSWITCH 79GB PER M/M 32-00-00 AND OPS CHECKED GOOD PER M/M 32-61-00. 2L72 4F RTA35EU 20030903000862003090300086 2003 9 3 MEX2003275 420030708A3417HG280D80 ADC DOUG MD88 MD88 3023688NM COCKPIT FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23160PL 49763 DURING TRANSIT CHECK WAS DETECTED CADC NR 1 IS OUT OF SERVICE WITH DATE BUS FAILED MESSAGE. CADC NR 1 WAS REPLACED IAW MM 34-16-01, BUT CADC NR 2 WAS OUT OF SERVICE, CADC NR 2 WAS REPLACED IAW MM 34-16-01, ALL TESTS CORRECT. 2L72 4F RTA6WE 20030903001092003090300109WP 2003 9 3 2003F00536 120030405A5320 FLOOR SUPPORT DOUG DC9 DC987 3022087WP FUSELAGE CORRODED A WXOAK NONE O OTHER ININSP/MAINT 1 WP17948MA 49778 FOUND CABIN FLOOR SUPPORT HAS CORROSION FS 254 LBL 14. REMOVED CORRODED FLOOR SUPPORT. FABRICATED AND INSTALLED REPAIR FLOOR SUPPORT IAW MD-80 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2 AND 51-30-8. (M) 2L72 4F RTA6WE 20030903001132003090300113EA 2003 9 3 2003F00525 120030609A32406007300 SENSOR CNDAIRCL600 CL6002C10 1390015EA NR 2 BRAKE MALFUNCTIONED A FDKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07507MJ 10077 ASH - FLT 6717 - PHX-FAT - AIRCRAFT RETURNED TO FIELD WITH NR 2 BRAKE TEMP WARNING MESSAGE. MAINTENANCE APPLIED MEL 32-46-01. AIRCRAFT CONTINUED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BRAKE TEMP SENSOR. (M) 2L72 4F RTA21EA 20030829001232003082900123NM 2003 8 29 SWAA031808 120030811A531265826711 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND MAIN W/W FWD PRESS BULKHEAD CRACKED AT BS 663, WL 200 AND LBL 33. REPAIRED BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20030829001252003082900125 2003 8 29 SWAA031853 420030819A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030829001392003082900139 2003 8 29 SWAA031833 420030816A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 FWD ENTRY DOOR EMERGENCY EXIT EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030829001472003082900147NM 2003 8 29 SWAA031841 120030813A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR UPPER FWD CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030829001552003082900155 2003 8 29 SWAA031819 420030804A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030829001612003082900161NM 2003 8 29 SWAA031826 120030813A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM CARGO BAY DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030829001712003082900171NM 2003 8 29 SWAA031788 120030807A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED C4 CHECK, FOUND CENTER KEEL BEAM CRACKED (3 EA) AT LOWER SKIN PANEL BETWEEN W/W'S. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20030829001932003082900193WP 2003 8 29 GTIA030619 120030726A5321 STIFFENER DOUG DC9 DC983 3022083WP FLOOR PANEL SEPARATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND CABIN FLOOR PANEL RIGHT OUTBOARD STATION 541-620 STIFFENER SEPARATED FROM PANEL. REBONDED STIFFENER. (M) 2L72 4F RTA6WE 20030902000622003090200062NE 2003 9 2 156060303 220030603A8500 ENGINE CVAC 340 340CVAC 242270AWP PWA R2800 R2800CB3 52026NE NR 2 MALFUNCTIONED A JRAAO OTHER O OTHER NRNOT REPORTED 1 GL11156JR 200 P35171 REJECTED TAKEOFF DUE TO BACKFIRING OF THE NUMBER TWO ENGINE. 2L72 4R4 R 6A6 5E8 20030902001402003090200140WP 2003 9 2 DHL2003803007 120030709A2510 SEAT DOUG DC8 DC873 302199CWP COCKPIT INOPERATIVE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01803DH 46123 SECOND OFFICER'S SEAT WILL NOT LOCK UP OR DOWN. LUBED SECOND OFFICER'S SEAT VERTICAL ADJUSTMENT IAW 25-11-6. OPS CHECK WAS GOOD. 2L74 4F RT4A25 20030902001542003090200154NE 2003 9 2 52413 220030709A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT MALFUNCTIONED A AMWAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE07242YV UE242 ON FLIGHT 5496, THE AIRCRAFT UPON REACHING CRUISE ALTITUDE NOTED LT ENGINE TORQUE HAD INCREASED ABOVE LIMITATIONS (4500 TO 4600 LBS FOR ABOUT 10 SECONDS). THE CREW THEN EXECUTED A PRECAUTIONARY SHUT OFF OF LEFT ENGINE AND RETURNED TO FIELD. THEY LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE DISCOVERED THE LEFT ENGINE WAS OVER TORQUED IN FLIGHT. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T4 TRTA24CE E26NE 20030902001602003090200160SO 2003 9 2 349811 120030602A57511159CSM5510631 BLOCK GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE LT AILERON SEPARATED B BTVRO OTHER O OTHER NRNOT REPORTED 1 GL2350KC 480 659 TUNGSTEN BLOCK (BALLAST WEIGHT) AT OUTBOARD END OF LT AILERON FOUND SEPARATED FROM MAIN COUNTER WEIGHT. BLOCK SLID FORWARD AGAINST WING REAR BEAM AND WAS RESTRICTING AILERON DOWNWARD MOVEMENT. PROBABLE CAUSE: LOOSE AND MISSING HARDWARE. ONE SCREW AND TWO NUTS FOUND RESTING ON LOWER REAR WING BEAM. 2L72 4F4 FRTA12EA E00057EN 20030910001132003091000113NM 2003 9 10 MWEA030358 120030902A5347593054765 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 SEAT TRACK NR 5 IS CORRODED AT STATION 237-256. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2L72 4F RTA6WE 20030910001202003091000120WP 2003 9 10 MWEA030367 120030909A5330591142739 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CANNING A MWEAK NONE O OTHER ININSP/MAINT 1 GL31216ME 47740 STATION 959 LONGERON 18 RIGHT & LONGERON 16 RIGHT EVIDENCE OF OIL CANNING UNDER RIGHT PYLON. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20030910001502003091000150EA 2003 9 10 A6WA200340125 120030822A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASMFK NONE O OTHER ININSP/MAINT 1 SW23407AW 7424 THE LEFT AND RIGHT CARGO FLOOR SUPPORT STRUCTURE IS CRACKED AT AFT PRESSURE BULKHEAD FS 621, WL 73.5 AND LBL 40 AND RBL 40. REPAIR IAW REO 601R-53-611-117 REV A. (M) 2L72 4F RTA21EA 20030911001612003091100161CE 2003 9 11 DXTA200300062 120030705A7897 WIRE CESSNA500 560CESSNA 2076750CE FUSELAGE BROKEN E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07302QS 5600402 LEFT THRUST REVERSER UNLOCK LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. BLED BRAKE SYSTEM, TROUBLESHOT TO BROKEN WIRES ON THE ANTI-SKID TRANSDUCER. REPAIRED WIRING, PERFORMED OPERATIONAL CHECK AND TAXI CHECK OF THE BRAKE SYSTEM, CHECKED GOOD. ALL WORK DONE IAW CESSNA CE 560 MM CHAPTER 32-42-00 AND CHAPTER 32-40-01 OF THE CE560 WIRING DIAGRAM MM. 2L72 4F RTA22CE 20030911001782003091100178WP 2003 9 11 DHL2003873616 120030706A57535751183506 FITTING DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT IB FLAP FITTING CRACKED 4.000 AT STA XW.97.000. PERFORMED MAJOR REPAIR IAW S/B DC8-27-249, SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030911002302003091100230WP 2003 9 11 DHL2003604531 120030508A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING CTR L/E FORMER LOWER PORTION CRACKED 1.000, STA XS.466.651. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RT WING CTR L/E FORMER LWR PART (XS.466.651) IAW SRM 51-1-20D PG 9 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911002392003091100239WP 2003 9 11 DHL2003604530 120030508A5320 FRAME DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 UPPER CARGO DOOR FORMER INNER SKIN CRACKED 1.000 AT STA 220.000, L-6,L-7L. REMOVED DAMAGED AREA FROM MAIN CARGO DOOR FORMER INNER SKIN AND FABRICATED FILLER AND DOUBLER IAW SRM 53-2-0 FIG 1D. CLEANED, TREATED AND FABRICATED AREA IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030912000612003091200061WP 2003 9 12 DHL2003604665 120030509A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBD FLAP UPPER PLATING SHOWS INTERIM REPAIR BETWEEN STA XW 91.000 AND XW 75.500. PERFORMED MAJOR REPAIR IAW EO DHL 030506, ED 3280. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EO DHL 030506, ED 3280. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN SEGMENT, A SPLICE STRAP IAW EO DHL 030506, ED 3280. CLEANED, TREATED AND PRIMED NEW SKIN SEGMENT INTERIOR SURFACE AND SPLICE STRAP IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SEGMENT AND SPLICE STRAP ON LT WING INBD FLAP UPPER PLATING (STA XW 91.000 TI XW 75.500) USING NEW FASTENERS IAW EO DHL 030506, ED 3280 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000832003091200083NM 2003 9 12 AWXA200300822 120030709A5320D5323028120140 ANGLE AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MINOR REPAIR - DURING C-04 CHECK .5000 INCH CRACK WAS FOUND ON FUSELAGE RT SIDE ANGLE AT BS 1323, FR 34, STR 32 RT. MAINTENANCE REMOVED RT SIDE ANGLE AT BS 1323, FR 34, STR 32 RT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 7-22, FIG 2-8, PG 23-39, FIG 9-17. 2L72 4F RTA28NM 20030912000892003091200089NM 2003 9 12 AWXA200300858 120030713A53206546812169 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 976, RBL 17, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT FROM BS 976 TO BS 977; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51, PG 105-100, FIG 101, AND SRM 51-40-02, PG 10-11, & 44-45, FIG 12. 2L72 4F RTA16WE 20030912001422003091200142NM 2003 9 12 AWXA200300900 120030731A53206546817 SUPPORT ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON CUSP WEB SUPPORT ANGLE BS 380-290, STR 17 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED WEB SUPPORT ANGLE FROM BS 380-290, STR 17 RT; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12, FIG 1, PG 1-7. 2L72 4F RTA16WE 20030912001462003091200146NM 2003 9 12 AWXA200300903 120030725A53206546592 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 770, LBL 10. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF FLOOR SUPPORT BS 770, LBL 10; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-70-53, FIG 201, PG. 1. 2L72 4F RTA16WE 20030912001572003091200157EU 2003 9 12 AWXA200300909 120030811A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28631AW10574 077 LAS - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT WAS NOT ILLUMINATED AT CENTER AISLE OVERWING EXITS. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030912001632003091200163NM 2003 9 12 AWXA200300915 120030812A3397 WIRE BOEING737 7373Y0 1384671NM CABIN SHORTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28331AW 23747 LAS - EEL - DURING INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM SEAT ROW 19 BACK. MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT WIRE GOING TO SEAT ROW 19 LT SHORTED AGAINST THE SEAT FRAME, REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030912001652003091200165NM 2003 9 12 AWXA200300917 120030811A3520785801 ACTUATOR BOEING737 7373G7 1384595NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28158AW 23780 LCQ - EMERGENCY EQUIPMENT - DURING C-17 CHECK THE O2 DOOR LOCATED AT PASSENGER SERVICE UNIT (PSU) 23 RT FAILED TO OPEN DURING PASSENGER OXYGEN SYSTEM CHECK. MAINTENANCE REMOVED AND REPLACED THE ACTUATOR SOLENOID AT PSU 23 RT IAW BMM 35-22-21, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030912001672003091200167EU 2003 9 12 AWXA200300919 120030803A5320D5348004320501 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON MAIN CABIN FLOOR SILL FR 66, RBL 60, JUST FORWARD OF R2 DOOR FORWARD GIRT BAR HOLD DOWN FITTING. MAINTENANCE REMOVED FLOOR SILL FR 66, RBL 60; FABRICATED A NEW REPLACEMENT FLOOR SILL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-10, & 12, FIG 2 & 3, AND PG 28-31, FIG 12 & 13. 2L72 4F RTA28NM 20030902001912003090200191NM 2003 9 2 03FDEA01019 120030624A5753NRC6055507 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 SNRM N0344 : LH WING - INBOARD T/E MAIN FLAP HAS CHAFING MARK AT L/E SKIN APPROX. 3 INCHES FROM INBOARD EDGE. CHAFING MARK SMOOTHENED AND FOUND OUT OF LIMIT IAW SRM 57-00-01 VOL.I AND REPAIR CARRIED OUT AT LH WING INBOARD TRAILING EDGE MAIN FLAP LEADING EDGE SKIN IAW SRM 57-00-01 FIG.7 VOL.I 2L73 4F RTA22WE 20030903000082003090300008NM 2003 9 3 DHL2003750005 120030712A5270 PIN BOEING727 7272M7 138407SNM PWA JT8 JT8D NE CARGO DOOR LATCHINOPERATIVE A DHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01750DH 21951 MAIN CARGO DOOR RED LIGHT ILLUMINATED ON FLIGHT, ACCOMPANIED BY LATCH LOCK PINS NOT ENGAGED AMBER LIGHT ON MCD CONTROL PANEL.(FL 370, WITH 6.3 CABIN ALTITUDE AND 8.4PSI DIFF.) EXECUTED EMERGENCY CHECK LIST IAW AOM 5.2.6 AT 2 PSI DIFF ON DESCENT/DEPRESSURIZATION, BOTH LIGHTS WENT, CLEANED AND LUBRICATED LATCH PIN MECHANISM CLEANED AND LUBRICATED LATCH PIN SWITCHES AND CLEANED LATCH PIN SWITCH CONNECTOR PINS AND SOCKETS CARGO DOOR INSPECTION CHECK ACCOMPLISHED IAW MM 52-34-0 DOOR CYCLED SEVERAL TIMES COULD NOT FAULT AT THIS TIME. 2L73 4F4 F A3WE E2EA 20030903000282003090300028NM 2003 9 3 PCAA0307083 120030712A212082110848005 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RT WING SEVERED A PCAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA13812EX 312 FLT NR 3544. CREW REPORTED UNKNOWN FUMES IN CABIN NEAR AISLE 2. MAINT INSPECTED AIRCRAFT OVERHEAD LIGHTING AND UNDER FLOOR NEAR AHARS UNIT. OVERHEAD LIGHTING WAS SUSPECT. LIGHT BULBS ABOVE ROWS 2 AND 3 LT AND RT SIDE WERE REPLACED. BOTH ENGINES WERE GROUND RAN WITH BLEEDS ON. PRESENCE OF ODORS OR FUMES COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 13 JULY 2003 YUL-FLIGHT 3539 CREW REPORTED AN UNKNOWN ODOR IN THE CABIN. MAINT REMOVED RIGHT FUSELAGE BLEED LINE PANELS FOR INSPECTION AND REMOVED BLEED LINE SHROUD. A SEVERED BLEED PIPE WAS FOUND. BLEED PIPE ON RT FRONT SPAR REPLACED. A/C GROUND RAN. OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. NO ODORS FOUND. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030903000912003090300091EA 2003 9 3 A6WA200340113 120030717A1430 FASTENER CNDAIRCL600 CL6002B19 1900309EA T/E FLAP LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LEFT INBOARD FLAP VANE HAS A PROTRUSION THAT IS CHAFING THE FLAP STUB WING STRUCTURE. PERFORMED A MAJOR REPAIR TO THE LEFT FLAP VANE BY REPLACEMENT OF LOOSE FASTENERS. WORK ACCOMPLISHED IAW WEST VIRGINIA AIR CENTER EO 601R-57-4131. (M) 2L72 4F RTA21EA 20030903001082003090300108NM 2003 9 3 USAASB03130 120030807A335020131A BATTERY PACK BOEING737 7374B7 1384702NM CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US 24548 TPA - MAINTENANCE REPORTED THE AFT RIGHT EXTERIOR EMERGENCY LIGHT WAS ILLUMINATED WHILE THE AIRCRAFT WAS SITTING AT THE GATE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030903001542003090300154EU 2003 9 3 199681 120030725A2770 SWITCH SAAB SF340 SF340A 7850100EU FLT CONTROLS LACK OF LUBE A UHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL17340SZ 340A004 FLT 4466 ON TAKEOFF FROM TTN-PIT ABORTED T/O DUE TO GUST LOCK WARNING LIGHT ILLUM. AC RETURNED TO GATE. MAINTENANCE INSPECTED AC FOUND STICKY THROTTLE QUADRANT SWITCH. LUBED SWITCH, OPS CHECK GOOD. AC RETURNED TO SERVICE. 2L72 4T RTA52EU 20030903001842003090300184NE 2003 9 3 AALA20030805 220030727A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RIGHT MALFUNCTIONED A AALAC ABORTED TAKEOFF RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET TOTAKEOFF 1 SW21575AM 53152 709930 FLT 1237 - MCO-STL, UPON TAKEOFF, RIGHT ENGINE COMPRESSOR STALLS AND VIBRATIONS. RETURNED MCO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030903001882003090300188WP 2003 9 3 AALA20030728 120030708A3260 SWITCH DOUG DC9 DC982 3022082WP NLG OUT OF ADJUST A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW21456AA 49561 ORD - FLT 2034 - EN ROUTE ORD-BOS - AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. THEN THE CABIN PRESSURE DUMPED, RECEIVED STALL INDICATION FAILURE AND AUTO SPOILER DO NOT USE LIGHTS ON. RETURNED TO ORD WITHOUT FURTHER INCIDENT. FOUND NOSE GEAR OLEO SWITCHES OUT OF ADJUSTMENT. ADJUSTED SWITCH CABLE AND CABLE TENSION. ACCOMPLISHED LANDING GEAR FUNCTIONAL CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030903002012003090300201NM 2003 9 3 QXEA200301031 120030825A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- DENT IN EMPENNAGE BOTTOM SKIN 7 INCHES AFT OF STATION X730 AND ONE INCH TO THE RIGHT OF STRINGER 33. REPAIRED IAW DHC-8 SRM 53-10-11, 51-00-06, 51-00-04, 51-20-16, 51-20-36 AND RD'S 8-53-4941 AND 8-53-2181. 2H72 4T RTA13NM 20030903002072003090300207 2003 9 3 QXEA200300969 420030812A6122697072003 GOVERNOR BOMBDRDHC8 DHC8401 1390041NM NR 2 MALFUNCTIONED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09401QX4547 4547 4031 GEG- NR 2 PROP SLOW TO COME OUT OF FEATHER. REMOVED AND REPLACED OVERSPEED GOVERNER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903002092003090300209EA 2003 9 3 QXEA200300973 120030812A5230 DOOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY NOT CLOSED A QXEAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 NM09603QX 10011 BOI- ON FLIGHT 2524 RETURNED TO FIELD DUE TO FORWARD CARGO DOOR WARNING. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND FORWARD CARGO DOOR NOT TOTALLY STOWED. STOWED HANDLE AND LIGHT WENT OUT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030903002172003090300217NM 2003 9 3 QXEA200301036 120030825A3240 LINE DHAV DHC8 DHC8202 2809007NM MLG LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09375PH 529 IDA- ON FLIGHT 2204, DURING SHUTDOWN AT THE GATE MASSIVE FLUID LEAK ON NR 1 ENGINE NACELLE. NR 1 HYDRUALIC QUANTITY ZERO AND PARK BRAKE PRESSURE ZERO. FOUND NR 1 LOWER BRAKE LINE LEAKING. REMOVED AND REPLACED BRAKE LINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903002192003090300219NM 2003 9 3 QXEA200300990 120030811A5230 DOOR FRAME DHAV DHC8 DHC8202 2809007NM CARGO DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- CARGO DOOR UPPER AFT CORNER INSIDE VERTICAL FRAME AT CONNECTION TO FIRST CROSS FRAME HAS A DRILL GOUGE WITH A CRACK. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-16 AND 51-20-36. 2H72 4T RTA13NM 20030903002242003090300224EA 2003 9 3 QXEA200300960 120030808A4970 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM09607QX 10024 SEA- ON FLIGHT 2454 'APU PUMP FAIL' AND 'APU ECU FAIL' CAUTION MESSAGES AFTER APU WAS SHUT DOWN AS PART OF AFTER START CHECKLIST. OPERATED APU IAW CRJ AMM 49-10-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030903002312003090300231EA 2003 9 3 03206641 120030725A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27641BR 7349 DURING MAINTENANCE INSPECTION THE LT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030912001822003091200182NM 2003 9 12 AALA20030870 120030815A2520 SEAT BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21378AN 25447 FOUND SEATS 33C, E, G, HAVE COME OFF BRACKET AND ARE LOOSE. SECURED SEAT 33C, E, G IAW AA MM 25-25-01-2. (M) 2L72 4F RTA1NM 20030924000722003092400072NM 2003 9 24 2003UALA00629 120030816A5753 STRUCTURE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE TE FLAP BULGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29377UA 24642 BIRD STRIKE ON RT WING OUTBOARD FLAP, TRAILING EDGE FLAP AT OUTBOARD END CAUSING APPROX 6 INCHES BY 2 INCHES DENT IN FLAP AND BULGE OF APPROX 4 INCHES LONG INBOARD TO OUTBOARD 1-8 INCH HIGH ON TOP OF FLAP SAME AREA. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030925000202003092500020 2003 9 25 AALA20030760 420030709A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21637AM 24595 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000282003092500028 2003 9 25 AALA20030762 420030710A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21640A 24598 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST OT CHECK GIRT BAR SPRINGS TO EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000442003092500044 2003 9 25 AALA20030768 420030709A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21181AN 29591 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS NEEDING REPLACED. REPLACED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000732003092500073NM 2003 9 25 AALA20030892 120030823A3150COM5115 COMPUTER BOEING767 767323 1385205NM E/E COMPT ERRATIC A AALAK NONE O OTHER ININSP/MAINT 1 SW21377AN 25446 LEFT EICAS COMPUTER STATUS MESSGE TURNING SELECTOR TO LEFT BOTH SCREENS BLANK. LEFT EICAS COMPUTER WORKING NORMAL ON ARRIVAL. LEFT EICAS COMPUTER CHECKED SECURE, LEFT EICAS COMPUTER C/B CYCLED STATUS MESSAGE SELF ERASED EICAS TEST CARRIED OUT PASSED NIL FAULTS. (M) 2L72 4F RTA1NM 20030925000812003092500081 2003 9 25 GTIA030625 420030807A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 SLIDE PACK ON R1 DOOR IS LOOSE. RESET SLIDE PACK AS REQUIRED ON R1 DOOR. (M) 2L72 4F A6WE 20030926000202003092600020CE 2003 9 26 JIKA20030001 120030718A2752 DRIVE SHAFT BEECH 99 C99 1154006CE ACTUATOR CRACKED E JIKAO OTHER O OTHER NRNOT REPORTED 1 WP0162989 AFA3309 U183 AFTER NR ONE FLAP REMOVAL, THE NR ONE FLAP ACTUATOR WAS INSPECTED AND AN EIGHT INCH CRACK WAS FOUND RUNNING LATERAL ON THE FLAP ACTUATOR DRIVE SHAFT. 1L72 3T A14CE 20030926000362003092600036NM 2003 9 26 03FDEA01390 120030826A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 CORROSION ON FRAME STA 950E BETWEEN STR 28L & 29L. REPAIRED FRAME BS 950E, STR 28L-29L IAW SRM 53-10-4 FIG 13 AND EA 7-5310-54947. 2L73 4F RTA3WE 20030926001082003092600108NM 2003 9 26 2003UALA00641 120030822A5347 SEAT TRACK BOEING747 747422 1384935NM PWA 4090 PW4090 52119NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29197UA 26901 SEAT TRACK SCALLOPS GOUGED ON SEAT TRACK - RBL 77 STA 1000-1022. MAJOR REPAIR ACCOMPLISHED. SEAT TRACK SECTION WAS REPLACED FROM STA 1000 TO 1082. INSTALLED REPAIR SPLICE AT STA 1022. 2L74 4F4 FRTA20WE E46NE 20030926001332003092600133NM 2003 9 26 C8GA20030022 120030830A3260189929 PROXIMITY SWITCH BOEING727 727223 1384074NM MLG DEFECTIVE A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15287SC 21345 FLT 738 FROM TOL TO MMIO. AFTER TAKEOFF, GEAR LEVEL WOULD NOT MOVE TO UP POSITION. WARNING HORN WAS SOUNDING AND BOTH PACKS TRIPPED OFF AND AUTO PRESSURIZATION INOPERATIVE. PERFORMED CCIA AOM ABNORMAL PROCEDURE 06-1, AIR TURNBACK AND LANDED IN TOL WITHOUT INCIDENT. AIRCRAFT CONTROL HANDLE LOCK SYSTEM WAS CHECKED AND REPLACED THE AIR SENSOR PROXIMITY SWITCH. OPERATIONAL SYSTEM CHECKS GOOD IAW MM 32-31-11 AND 32-09-221. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030926001372003092600137CE 2003 9 26 DXTA200300096 120030819A783021681 SWITCH CESSNA500 560CESSNA 2076750CE THRUST REVERSER MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07344QS 5600344 RT THRUST REVERSER UNLOCK LIGHT ILLUMINATED BELOW 70K ON TAKEOFF ROLL. TAKEOFF ABORTED W/O INCIDENT, T/R DID NOT DEPLOY, LIGHT WOULD NOT CLEAR BY PUSHING T/R PADDLE DOWN. LIGHT DID CLEAR BY CYCLING RIGHT T/R. REMOVED AND REPLACED RIGHT TR OUTBOARD STOW SWITCH AS PER CESSNA 560 COMPONENT MM CHAPTER 78-30-09. OPS CHECKED GOOD. 2L72 4F RTA22CE 20030926001652003092600165NM 2003 9 26 CALA0300510 120030903A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND CORROSION ON FRAME AT STA 793 BETWEEN S26R AND S25R IN AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030929000052003092900005EA 2003 9 29 COMA0360396 120030830A783022850231101 BLOCKER DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE THRUST REVERSER BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01716CA 7250 807248 FLIGHT 5675 RT THRUST REVERSER BLOCKER DOOR AT 4 O'CLOCK POSITON FOUND BROKEN IN HALF. REMOVED BROKEN BLOCKER DOOR AND INSTALLED A SERVICEABLE ONE. 2L72 4F4 FRTA21EA E15NE 20030929000342003092900034NM 2003 9 29 03FDEA01431 120030829A5712 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING L/E CAVITY, NR 16 RIB CRACKED. LT WING- L/E CAVITY, NR 16 RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20030929000542003092900054 2003 9 29 DHL2003780012 420030903A34165223698003 ALTIMETER BOEING727 727223 1384074NM COCKPIT FAILED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01780DH 22006 GPWS AND WINDSHEAR INOPERATIVE LIGHT ILLUMINATED INTERMITTENTLY. FOUND RADIO ALTIMETER RT FAILED. TRANSFERRED TO DMI LOG NR14023 IAW MEL 34-28-2B CAT. (A) ITEM 2 FLT DAY. PLACARDS INSTALLED. FAINT ODOR OF BURNED RUBBER WAS DETECTED IN COCKPIT. FOUND RADIO ALTIMETER RT FAILED. COLLARED BREAKER DMI CONTROL NR1 4023. REF. DMI NR1 4023. FAINT ODOR OF BURNED RUBBER WAS DETECTED IN COCKPIT. REMOVED AND REPLACED RADIO ALTIMETER IAW B-M/M 34-48-21. OPS CHECKED GOOD. THIS CLEARS DMI NR 14023. PLACARD REMOVED. 2L73 4F A3WE 20030929000562003092900056EU 2003 9 29 DHL2003364013 120030904A3210C230056 DAMPER AIRBUS300 A300B4203 3930306EU LEFT INOPERATIVE A DHLAO OTHER O OTHER CLCLIMB 1 SO01364DH 141 ON TAKEOFF THE LANDING GEAR LEVER WOULD NOT RETRACT PAST THE OFF POSITION. PERFORMED ABNORMAL PROCEDURE AND LEVER WOULD STILL NOT RETRACT PAST OFF. FOUND DAMPER RED INDICATOR POPPED. REMOVED AND REPLACED LT PITCH DAMPER IAW M/M 32-11-15. 2L72 4F RTA35EU 20030929000692003092900069NM 2003 9 29 QXEA200301054 120030831A33501161361 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 600 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 RT UNDERWING EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS TEST. REMOVED AND REPLACED EMERGENCY EXIT DOOR BETA LIGHT. 2H72 4T RTA13NM 20030929000722003092900072EA 2003 9 29 QXEA200301057 120030901A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 PDX- FORWARD CARGO PIT HAS TWO DAMAGED SMOKE DETECTOR SCREENS. REMOVED AND REPLACED CHIMNEYS. 2L72 4F RTA21EA 20030929000812003092900081NM 2003 9 29 CALA0300511 120030903A5330 SKIN BOEING737 737524 1384721NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714609 27322 INSPECTION FOUND FUSELAGE SKIN REPAIR PLATE GOUGED AT STA 980 UNDER L-2 DOOR. THE REPAIR PLATE WAS REMOVED AND A NEW REPAIR PLATE WAS INSTALLED IAW SRM 53-00-01, PAGE 204-206. 2L72 4F RTA16WE 20030929000872003092900087NM 2003 9 29 UPS03241167 120030903A335038931002 BATTERY BOEING727 72722C 138400FNM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 FWD ENTRY DOOR EMERGENCY LIGHT DOES NOT TEST. REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-67, OPS CK GOOD. P/N ON 38931-002. 2L73 4F A3WE 20030929000992003092900099 2003 9 29 MALA030399 420030830A2250 LIGHT SAAB SF340 340B 7860101EU CABIN LOOSE A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 PILOT REPORTED FLOOR LIGHTING COMING LOOSE. RESECURED FLOOR LIGHTS. 2L72 4T RTA52EU 20030929001052003092900105NM 2003 9 29 AWXA200301020 120030812A5315654541025 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK 2 EACH 1.25 INCH CRACKS WERE FOUND ON PASSENGER CABIN FLOORBEAM AT BS 674, RBL 45. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 674, RBL 45; FABRICATED A REPAIR EXTRUSION AND 3 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-04 FIG 1 PG 1. 2L72 4F RTA16WE 20030929001172003092900117 2003 9 29 RAIA00308232 420030831A3425HG2010AC02 DISPLAY EMB 145 EMB145LR 3260212SO NR 2 AHRS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK431 145044 F/OS AHRS FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS. 2L72 4T RTT00011AT 20030929001292003092900129NM 2003 9 29 03FDEA01454 120030906A5610 SEAL DOUG MD11 MD11 3023602NM WINDOW DEFORMED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25610FE 48603 DURING CLIMB FROM RJBB, A VERY LOUD NOISE OCCURRED AT THE CAPTAINS WINDOW. NOISE WAS SO LOUD THAT AN INFLT RETURN WAS NECESSARY. UPON DESCENT, NOISE CEASED AT 4.4 DIFFERENTIAL PRESSURE. RETURN WAS NECESSARY DUE TO SAFETY OF FLIGHT DUE TO DIFFICULTY IN COMMUNICATION. INSPECTED SLIDING WINDOW SEAL ON CAPT SIDE AND FOUND SEAL DEFORMED AT FWD LWR CORNER. REMOVED AND REPLACED SEAL MPN ABA7805-1 IAW MM 56-12-01-8. LEAK AND NOISE CHECK OK WITH DP 6.0 OF CABIN PRESSURE APPLIED IAW MM 21-00-00-2. 2L73 4F RTA22WE 20030930000012003093000001NE 2003 9 30 C1HA200382009 220030906A7200 ENGINE BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 MALFUNCTIONED A C1HAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL15682CA 22019 666314 NR 2 ENG WAS FLUC EPR+- 4 N1, N2 EGT AND FUEL FLOW ALL WERE FLUCT. PRIOR TO SHUTDOWN NR 2 ENG FUEL HEAT ICING LIGHT STROBING EVEN WITH FUEL HEAT ON. ENG SHUT DOWN DURING FINAL CLIMB TO 37000 WHEN ENG SHUT DOWN ENG OIL CLIMBED TO 140 C ENG WINDMILLED FOR 37 MIN 09 SEC FOR FINAL 2 MIN AND 30 SEC OIL PSI DROPPED BELOW 10 PSI BUT NEVER BELOW 5 PSI. REMOVED AND REPLACED NR 2 ENG IAW CA TASK CARD 7102, CW ENG TRIM, LEAK CHECK OK FOR SERVICE. 2L73 4F4 F A3WE E2EA 20030930000052003093000005NM 2003 9 30 F3LA200300125 120030830A5320 WEB BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT DOOR SILL WEB CORRODED. REPLACED SILL WEB IAW MFG DRAWING 65-20726 AND SRM 51-40-02. 2L72 4F RTA16WE 20030930000112003093000011NM 2003 9 30 AWXA200301030 120030907A3260 CIRCUIT BREAKER BOEING737 737277 1384570NM MLG INDICATOR INOPERATIVE A AWXAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 WP28182AW 22649 ON APPROACH INTO PHX EN ROUTE FROM BUR AFTER LANDING GEAR EXTENSION THERE WAS NO LANDING GEAR DOWN AND LOCKED OR UNSAFE GEAR INDICATIONS, ABORTED APPROACH. FOUND CIRCUIT BREAKER (SECT5) EXTENDED, AFTER DISCUSSION WITH MAINTENANCE CONTROL, CIRCUIT BREAKER WAS RESET AND SYSTEM WAS RESTORED, LANDED WITHOUT FURTHER EVENT. MAINTENANCE JACKED THE AIRCRAFT AND RETRACTED THE LANDING GEAR 3 TIMES; ALL INDICATIONS WERE NORMAL, COULD NOT DUPLICATE PROBLEM. 2L72 4F RTA16WE 20030930000142003093000014NM 2003 9 30 QXEA200301067 120030903A2120 SMOKE DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09364PH 524 ON FLT 2110 FLIGHT ATTENDANT REPORTED SMOKE IN CABIN AFTER ENGINE START. CLEARED AFTER A COUPLE OF MINUTES. TEST TEMPERATURE CONTROL SYSTEM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930000192003093000019 2003 9 30 BAQA089234 420030919A34447000839901 INDICATOR AGUSTAA109 A109E 0260119EU RADAR ALTIMETER MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA031UW 2046 11034 OFF FLAG DOES NOT PULL. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH7EU 20030930000212003093000021SO 2003 9 30 CHQA000419 120030907A2120 SMOKE EMB 145 EMB145 3260210SO CABIN DETECTED A CHQAGB O2 MASK DEPLOYED EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11836 FLYING SHORT FINAL FOR RUNWAY 35 INTO MCO. RECIEVED A CALL STATING - SMOKE IN THE CABIN. NO INDICATIONS ON EICAS BUT COULD DETECT A BURNING SCENT ON THE FLIGHT DECK. DECLARED AN EMERGENCY, TURNED OFF RECIRCS, DEPLOYED PILOT O2 MASK, LANDED UNEVENTFULLY, TURNED OFF THE PACKS AND WAITED FOR CFR AT THE END OF THE RUNWAY ON THE LAST TAXIWAY. SMOKE IMMEDIATELY DISSIPATED. RAN THE AFTER LANDING CHECKLIST, WHILE CFR EXAMINED THE EXTERIOR OF THE PLANE. NO SIGN OF FIRE INTERIOR OR EXTERIOR. WAS ESCORTED BY CFR TO GATE. 2L72 4F RTT00011AT 20030930000322003093000032EU 2003 9 30 MALA030385 120030820A49204501690A LABYRINTH SEAL BAC 146 AVRO146RJ85A1500097EU APU FAILED A MALAK NONE O OTHER TXTAXI/GRND HDL 1 GL15524XJ E2349 DURING TAXI ON FLIGHT 3504, BAD ODOR FROM PACKS. MAINTENANCE FOUND APU INOPERATIVE DUE TO LABYRINTH SEAL BAD. FROM LP 1216605 REMOVED AND REPLACED APU P/N 4501690A S/N OFF SP-E9875 49 S/N ON SP-E977516 PER TASK CARD APU CHANGE ALL CHECKS GOOD REMOVED. FROM DMR MXC NOTIFIED 2H74 4F RTA49EU 20030930000592003093000059NM 2003 9 30 P5CA0300938 120030907A3610 DUCT BOEING747 7472U3B 1384846NM RT WING LOOSE A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23923FT 22769 RT WING L/E OVERHEAT LIGHT CAME ON TAXI OUT. REMAINED ON WHEN ISOLATED. FOUND LOOSE DUCT LEADING TO NR 3 LEADING EDGE FLAP MOTOR. TIGHTENED AS REQUIRED SYS LEAK CK GOOD IAW MM 27-81-00 PG 207. 2L74 4F RTA20WE 20030925000552003092500055WP 2003 9 25 GTIA030667 120030828A3350 SIGN DOUG DC9 DC983 3022083WP G4 GALLEY MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 SAFETY GLO 'EXIT SIGN' LOCATED AT G4 GALLEY IS MISSING. RE-INSTALLED SAFETY GLO 'EXIT' SIGN LOCATED AT G-4 GALLEY. (M) 2L72 4F RTA6WE 20030926000152003092600015WP 2003 9 26 ABXA030334 120030801A552049198891 ATTACH FITTING DOUG DC9 DC941 302207NWP LT ELEVATOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 LT ELEVATOR WAS CORRODED ON UPPER SURFACE AT OUTBOARD BALANCE HORN ATTACH FITTING. REPLACED LT ELEVATOR ATTACH FITTING CLIP. 2L72 4F A6WE 20030926000292003092600029 2003 9 26 AWXA200300992 420030817A256560592101 RESERVOIR AIRBUS320 A320231 3930325EU ESCAPE SLIDE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW9798 67 DURING C-03 CHECK THE LT OVER WING ESCAPE SLIDE RESERVOIR INFLATION CABLE CONNECTOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE RESERVOIR ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030926000302003092600030NM 2003 9 26 CALA0300502 120030828A5347 GALLEY TRACK BOEING737 7373T0 1384582NM NR 3 GALLEY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND NR 3 GALLEY I/B AFT MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030926000552003092600055EA 2003 9 26 COMA0360383 120030822A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01729CA13611 7265 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F4 FRTA21EA E15NE 20030926000562003092600056EA 2003 9 26 COMA0360384 120030824A2750 CONTROL QUADRANT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01477CA 7670 FLAPS FAILED AT 30 DEGREES DURING APPROACH. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD98-20-01. 2L72 4F RTA21EA 20030926000632003092600063EU 2003 9 26 AWXA200300994 120030827A33501012887 LIGHT AIRBUS320 A320232 3930326EU SEAT ROW 1 LT BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28662AW 1274 FLIGHT CREW REPORTED THE EMERGENCY LIGHT COVER MISSING AT SEAT ROW 1 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 1 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030926001172003092600117NM 2003 9 26 AT0300024 120030831A2450762904C CONTROL UNIT BOEING717 717200 1383700NM LEFT IDG INOPERATIVE A ZZDAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO15955AT 55139 IMMEDIATELY AFTER TAKE OFF, SMOKE (ELECTRICAL) AND FUMES FROM FLOOR VENTS IN BUSINESS CLASS. LOST LEFT DC BUSS. FOUND LEFT HAND PCDU TO BE FAULT. REMOVED AND REPLACED LEFT HAND PCDU AND LEFT IDG. 2L72 4F TRA6WE 20030926001302003092600130NM 2003 9 26 UPS03241155 120030814A5310 STRUCTURE BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 INSPECTION TYPE:C, CRACK INDICATION FOUND AT BS 910 AFT SIDE OF REINFORCING BEAD RBL 52. REPAIRED IAW EO B727-5310-0088 APPDX C. 2L73 4F A3WE 20030929000492003092900049NM 2003 9 29 03FDEA01409 120030902A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING I/B FLAP I/B DRIVE ARM ATTACHMENT BORE (FLAP SIDE) CORRODED. 2L73 4F RTA22WE 20030929000712003092900071NM 2003 9 29 QXEA200301056 120030831A33501161361 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 LT UNDERWING EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS TEST. REMOVED AND REPLACED LT UNDERWING EMERGENCY EXIT DOOR BETA LIGHT. 2H72 4T RTA13NM 20030929000842003092900084NM 2003 9 29 DHL2003726012 120030903A7720JT8D7B ENGINE BOEING727 727228 1384083NM PWA JT8 JT8D7B 52053NE NR 2 FAILED A DHLAEC ENGINE SHUTDOWN ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 SO01726DH 20409 649465 DURING T/O FROM ATL, ENGINE NR 2 EGT CLIMBED TO 620 C WITH EPR SET AT 1.95, N1 = 94 PERCENT, REDUCED THRUST TO 1.72 EPR, N1 = 89.5, EGT = 580 C, N2 = 92.8, FF = 6800, PERFORMED EGT OVER TEMPERATURE ABNORMAL PROCEDURE IAW 727 A.O.M. SHUTDOWN NR 2 ENGINE. ENGINE NR 2 EGT WAS AT 620 C FOR APPROX. 8-10 SECONDS. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY IAW DHL B727 MTM 71.2. OK FOR SERVICE . 2L73 4F4 FRTA3WE E2EA 20030903002322003090300232EA 2003 9 3 03239626 120030827A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27626BR 7225 DURING PREFLIGHT INSPECTION THE CREW DISCOVERED THE CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT AS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030902001222003090200122CE 2003 9 2 52268 120030705A3260 INDICATOR BEECH 1900 1900D 1154162CE MLG INOPERATIVE A AMWAO OTHER O OTHER LDLANDING 1 CE07146ZV UE146 UPON ARRIVAL, ON FLIGHT 700, THE LANDING GEAR HANDLE DOWN, NO GREEN INICATORS ON. THE RIGHT MAIN MANUAL EXTENSION WAS PERFORMED. FLYBY TOWER CONFIRMED GEAR APPEARED DOWN. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GEAR DOWN INDICATOR. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20030903000102003090300010NM 2003 9 3 SCNA03004 120030714A3350 LIGHT BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15806SY 28215 EXTERIOR EMERGENCY LIGHT BEHIND LT GEAR ON FUSELAGE INOPERATIVE. RELAMPED THE EMERGENCY LIGHT. OPS CHECKED GOOD 2L72 4F RTA16WE 20030903000612003090300061SW 2003 9 3 CYX2003F00001 120030627A7931222375077119 TRANSDUCER BELL 407 407 1182206SW OIL PRESS INACCURATE B CYXRO OTHER O OTHER NRNOT REPORTED 1 CE01407LG1359 53143 PILOT STARTED HELICOPTER AND NOTICED HIGH MAIN TRANSMISSION OIL PRESSURE. HELICOPTER SHUT DOWN. WITH ROTOR STOPPED TRANS OIL PRESSURE STILL READ 40-50 PSI. OIL PRESSURE TRANSDUCER WAS CHANGED AND OIL PRESSURE WAS BACK TO NORMAL. 1G71 3U O H2SW 20030903000682003090300068CE 2003 9 3 GLBA2003107 120030716A2841 ANNUNCIATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA FUEL QTY ILLUMINATED A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03261GL UE261 FUEL QTY ANNUNCIATOR ILLUMINATED, PREFORMED OPERATIONAL RUN-UP OF A/C CND TEST OF SYSTEM OK. 2L72 4T3 TRTA24CE E2NE 20030903001382003090300138WP 2003 9 3 2003F00539 120030410A5321 FLOOR PANEL DOUG DC9 DC987 3022087WP FUSELAGE BROKEN A WXOAK NONE O OTHER ININSP/MAINT 1 WP17948MA 49778 FOUND CABIN FLOOR PANEL LBL 22-44 FS 802-889 IS BROKEN. FABRICATED AND INSTALLED REPAIR FLOOR PANEL IAW MD80 SRM 53-05 PAGE 122A THROUGH 127. (M) 2L72 4F RTA6WE 20030903001762003090300176EU 2003 9 3 2003F00546 120030627A3230C247300016 UPLOCK AIRBUS320 A320232 3930326EU NLG BROKEN A RYNAO OTHER J WARNING INDICATION CLCLIMB 1 CE07DALAE 659 AFTER TAKEOFF FROM SAN ANTONIO, RETRACTED GEAR. RECEIVED 'LANDING GEAR NO UPLOCKED WITH RED 'UNLOCK' INDICATION ON LANDING GEAR ANNUNCIATOR. REVIEWED COCKPIT PROCEDURE MANUAL AND ACCOMPLISHED ECAM ACTIONS. AFTER UNSUCCESSFUL UPLOCK, GEAR WAS DOWNLOCKED AND AIRCRAFT RETURNED TO SAN ANTONIO WITHOUT INCIDENT. REMOVED AND REPLACED UPLOCK ASSEMBLY FOR NOSE LANDING EAR, 'GEAR NOT LOCKED. OPERATIONAL AND LEAK CHECK NORMAL. (M) 2L72 4F RTA28NM 20030903002402003090300240NM 2003 9 3 03236500 120030824A3350321431 BATTERY DORNERDO32 DO328300 NM CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27500FJ 3197 DURING MAINTENANCE INSPECTION THE EMERGENCY BATTERIES WERE FOUND DISCHARGED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY BATTERIES. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030903002592003090300259SO 2003 9 3 C2XA03TY143 120030830A531014525480003 DOOR FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED 2C INSPECTION THE AREA UNDER THE BAGGAGE DOOR LOWER TRIM WAS CORRODED. MAINT R&R THE CARGO DOORWAY LOWER BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030903002702003090300270SO 2003 9 3 C2XA03SH281 120030821A531514522226003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 58 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030903002742003090300274SO 2003 9 3 C2XA03SH269 120030817A532014521725017 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV- DURING C CHECK THE SERVICE DOOR FOWARD SILL WAS FOUND TO HAVE CORROSION AT SCREW HOLES. MAINTENANCE REPAIRED AFFECTED SILL IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030904000192003090400019EU 2003 9 4 DXTA200300064 120030707A2120 ODOR HAWKERBAE125BAE125700B 7450007EU CABIN DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07503QS 259003 1.5 HOURS INTO FLIGHT, DESCENDING OUT OF FL 410, CREW SMELLED A STRONG ODOR SIMILAR TO THE BURNING OF ELECTRICAL INSULATION. INSPECTED AIRCRTAFT INTERIOR AND COCKPIT AREA, COULD NOT FIND SOURCE OF ODOR, ACCOMPLISHED OPERATIONAL CHECK FLIGHT COULD NOT DUPLICATE WRITE UP. 2L72 4F RTA3EU 20030904000252003090400025SO 2003 9 4 C2XA03IA089 120030903A326023092900401 UPLOCK EMB 145 EMB145 3260210SO LT MLG INOPERATIVE A C2XAK NONE N FALSE WARNING ININSP/MAINT 1 SW2727962 145110 IAH- MAINTENANCE NOTED THAT THE LANDING GEAR INDICATION DISAGREES WITH THE LEVER. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030904000262003090400026SO 2003 9 4 C2XA03CL156 120030830A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN MALFUNCTIONED A C2XAK NONE O OTHER UKUNKNOWN 1 SW2714945 145049 CLE FLIGHT NR 2115 THE CREW REPORTED TWO EMERGENCY AISLE LIGHTS OUT OF SERVICE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST OF AISLE PATH EMERGENCY LIGHTS OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030904000272003090400027SO 2003 9 4 C2XA03BT089 120030824A3397 WIRE EMB 145 EMB145 3260210SO CABIN LOOSE A C2XAK NONE L NO TEST NRNOT REPORTED 1 SW2715973 145159 EWR LOG SQUAWK EMERGENCY EXIT SIGN ROW 12 LEFT SIDE BURNED OUT. RESECURED SPLICE FOR EMERGENCY EXIT SIGN AT ROW 12 LEFT HAND IAW EMB145 MM 33-50-00. OPS CHECK GOOD. 2L72 4F RTT00011AT 20030904000372003090400037SO 2003 9 4 SWIA200312275 120030819A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07268UE5560 3251 120207 ON THE GROUND FLAP AND ADVANCED SWS ON MAP ILLUMINATED WITH CONTROL FAULT ON FLAP PANEL AND SECOND NAC BAR FLASHING. REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030904000402003090400040EA 2003 9 4 SWIA200312277 120030710A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 MID FUSELAGE, PULLEY INTERCOSTAL OB FLANGE IS CRACKED; FS 484.0, LBL 36.0. DISCOVERED DURING C-CHECK, CUT OUT DAMAGE IAW CRJ REO 601R-53-41-059 ''A''. REPAIRED ANGLE IAW CRJ REO 601R-53-41-059 ''A'' & RII 53-401. 2L72 4F RTA21EA 20030904000442003090400044EA 2003 9 4 SWIA200312329 120030817A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 FS 280 RT FLOORBEAM RBL 9.0 INBD AND OB ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-58 2L72 4F RTA21EA 20030904000602003090400060EA 2003 9 4 SWIA200312341 120030826A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FS 484 LT INTERCOSTAL OB FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRJ REO 601-53-41-059 REV. ''A'' (RII 53-401). 2L72 4F RTA21EA 20030904000712003090400071NM 2003 9 4 QXEA200301050 120030831A2120 ODOR BOMBDRDHC8 DHC8401 1390041NM CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09403QX 4037 SEA- ON FLIGHT 2349 BOTH FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL SMELL JUST AFT OF MID CABIN. INSPECTED AIRCRAFT FOR ELECTRICAL SMELL WITH CABIN CLOSED AND PRESSURE OFF, NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904000802003090400080NM 2003 9 4 QXEA200300984 120030816A5420 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM NR 2 NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX- NR 2 NACELLE UPPER HEAT SHIELD LEFT FORWARD SUPPORT BRACKET IS CRACKED AT RADIUS. REPAIRED IAW HORIZON AIR EA 6-54-273 AND Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030904000822003090400082NM 2003 9 4 QXEA200300978 120030812A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX-DURING LIGHTNING STRIKE INSPECTION FOUND A BURN MARK AT ONE OF THE RIVETS ON STRINGER 4 STATION X19350 JOINT. REPAIRED IAW Q400 SRM 51-25-05, PG 208. 2H72 4T RTA13NM 20030904000832003090400083NM 2003 9 4 QXEA200300986 120030811A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM RT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- RIGHT MAIN LANDING GEAR WHEEL BAY FORWARD AT TWO OCLOCK FIREWALL IS CRACKED. REPAIRED IAW DHC-8 RD 8-54-109 AND SRM 51-00-06. 2H72 4T RTA13NM 20030904000842003090400084NM 2003 9 4 QXEA200300989 120030811A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- LEFT WING NR 4 FLAP TRACK HAS PITTING ON INBOARD SIDE OF TRACK, FORWARD END OF RAIL. REPAIRED IAW HORIZON AIR EA 2-57-2277 AND DHC-8 SRM 51-00-08. 2H72 4T RTA13NM 20030903000522003090300052EU 2003 9 3 U30A200300020 120030710A2611 SMOKE DETECTOR AIRBUS320 A320214 3930316EU LAVATORY MALFUNCTIONED A U30AO OTHER N FALSE WARNING CRCRUISE 1 EA17260AV 1564 DURING CRUISE ON FLT 123 MDPC-KPHL THE MASTER WARNING FOR "LAV SMOKE" TRIGGERED BY HAIRSPRAY. NO ACTUAL SMOKE PRESENT. ON FLT 100, MMUN-KPHL, (LATER SAME DAY,TAT 4642.8, 1748 CYC.) DURING CRUISE "LAV SMOKE" WARNING WAS TRIGGERED BY AIR FRESHENER USED BY CABIN CREW. ON 7/12/03 ON FLT 133, MYNN-KPHL,(TAT 4664.1, 1755 CYC.) DURING CRUISE "LAV SMOKE" WARNING WAS TRIGGERED BY AIR FRESHENER USED BY CABIN CREW (AGAIN). IN ALL CASES NO SMOKE WAS PRESENT. FURTHERMORE, IN ALL CASES THE SYSTEM WAS TESTED I/A/W AMM 26-17-00-501 WITH NO FAULTS FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE QUALITY CONTROL DEPT. HAS NOTIFIED THE OPERATIONS DEPT. NOT TO USE THESE PRODUCTS IN THE LAVATORIES DURING FLIGHT. 2L72 4F RTA28NM 20030903000672003090300067 2003 9 3 IXXA0300048O 420030714A3422 GYRO DOUG DC8 DC862 3021970WP COCKPIT FAILED A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW1131CX 76460487 45911318 AFTER TAKEOFF FROM WSAP NR 1 COMPASS PRECESSING 8-10 DEGREES IN APPROX. 1 1/2 MINUTES. CREW RETURNED TO WSAP AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WILL PROVIDE MORE INFORMATION AS IS BECOMES AVAILABLE. MAINTENANCE REMOVED AND REPLACED NR 1 DIRECTIONAL AND VERTICAL GYRO PER ALL APPLICABLE MANUALS. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20030903000892003090300089NE 2003 9 3 MEX2003276 220030708A75311074741 REGULATOR BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE PILOT PRESS FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23703AM 27203 AIRCRAFT AIR TURN BACK DUE TO (RT ENGINE BLEED OFF) AND (RT PACK OFF) MESSAGES AT 310 FT, LOOSING CABIN PRESSURE AND APPEARING MESSAGE OF CABIN ALTITUDE WITH AUDIBLE ALARM. AIRCRAFT WAS SENT TO THE HANGAR. PILOT PRESSURE REGULATOR AND TEMPERATURE SENSOR OF ENGINE 2 AND ALL OXYGEN CYLINDER WERE REPLACED IAW MM RESPECTIVELY, ALL TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20030903001432003090300143WP 2003 9 3 GTIA030616 120030725A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND CABIN FLOOR PANEL RIGHT STATION 886-927 DELAMINATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030903001532003090300153NM 2003 9 3 VNAA0308011 120030820A2611 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY DIRTY A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07458PS 3068 EN ROUTE, THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. UPON ARRIVAL, MAINTENANCE INSPECTED AND CLEANED THE LAV DETECTOR CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030903001552003090300155EU 2003 9 3 161281 120030725A2770 SWITCH SAAB SF340 SF340A 7850100EU FLT CONTROLS LACK OF LUBE A UHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL17340SZ 340A004 FLT 4466 ON TAKEOFF FROM TTN-PIT ABORTED T/O DUE TO GUST LOCK WARNING LIGHT ILLUM. AC RETURNED TO GATE. MAINTENANCE INSPECTED AC FOUND STICKY THROTTLE QUADRANT SWITCH. LUBED SWITCH, OPS CHECK GOOD. AC RETURNED TO SERVICE. 2L72 4T RTA52EU 20030903001702003090300170NM 2003 9 3 2003F00542 120030627A2910106056340 HYDRAULIC LINE BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE HYD SYSTEM DAMAGED A MYWAK NONE K FLUID LOSS TOTAKEOFF 1 SO19803MA 22434 687682 ON TAKEOFF, OUT OF SDF AT GEAR ROTATION LOST SYS 'A' HYD FLUID, SHUT PUMPS OFF ACCOMPLISHED ABNORMAL CHECKLIST. REMOVED AND REPLACED HOSE ASSEMBLY NR 2 ENGINE P/N 10-60563-40, NO METAL FOUND IN CASE DRAIN FILTERS OR SUPPLY FILTERS REPLACED NR 1 AND NR 2 HYDRAULIC PUMPS. PERFORMED OPS AND LEAK TEST RETURNING AIRCRAFT TO SERVICE. (M) 2L73 4F4 F A3WE E2EA 20030903002002003090300200NM 2003 9 3 QXEA200301030 120030820A5711 SPAR DHAV DHC8 DHC8202 2809007NM RT WING GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- GOUGE IN RADIUS OF RIGHT FORWARD SPAR TOP FLANGE TO SKIN JOINT FROM YW318.0 TO YW327.0. REPARIED IAW DHC-8 SRM 51-00-06 AND RD 8-57-1675. 2H72 4T RTA13NM 20030903002022003090300202NM 2003 9 3 QXEA200301032 120030823A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM LT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- FIREWALL FOR LEFT NACELLE IS CRACKED AT THE 10 O'CLOCK POSITION OF THE EXHAUST APERTURE ABOVE THE NUT PLATE HOLE. REPAIRED IAW DHC-8 SRM 51-40-11, 51-00-06 AND RD 8-54-651. 2H72 4T RTA13NM 20030903002102003090300210NM 2003 9 3 QXEA200300966 120030810A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM CABIN OUT OF ADJUST A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09405QX 4047 SEA- ON FLIGHT 2363 AFT PASSENGER DOOR IS INOPERATIVE. SEQUENCED DOOR TO CLOSE PROPERLY. NO PARTS REPLACE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903002122003090300212EA 2003 9 3 QXEA200300972 120030812A2550 PULLEY BRACKET CNDAIRCL600 CL6002C10 1390015EA CARGO BAY CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX- AFT CARGO DOOR AFT PULLEY BRACKET ON CARGO BAY NET SUPPORT BRACKET IS CHAFED. REPAIRED IAW HORIZON AIR EA R-53-124. 2L72 4F RTA21EA 20030903002452003090300245EA 2003 9 3 03231705 120030819A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27705BR 7470 DURING MAINTENANCE INSPECTION THE NR 4 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030904000512003090400051 2003 9 4 SWIA200312257 420030808A34183995100207A STALL WARNING CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING UKUNKNOWN 1 NM07954SW 7815 STALL FAIL CAUTION MSG ON INTERMITTENTLY. REPLACED STALL PROTECTION UNIT WITH SERVICEABLE UNIT. ALL CHECKS GOOD. PN: 39-951-002-08 SN OFF: 1055 2L72 4F RTA21EA 20030904000962003090400096NM 2003 9 4 QXEA200301002 120030812A5753 DOUBLER DHAV DHC8 DHC8202 2809007NM T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- LEFT OUTBOARD FLAP TOP INBOARD EDGE HAS A DEEP CUT IN FLAP ON PREVIOUS REPAIR. REPAIRED IAW DHC-8 RD 8-57-1549, 8-57-1734 AND SRM 51-20-26. 2H72 4T RTA13NM 20030904001042003090400104NM 2003 9 4 QXEA200301042 120030820A5720 BRACKET DHAV DHC8 DHC8202 2809007NM LT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- LEFT HAND UPPER BRACKET ON LEFT HAND WING STATION YW139.00 IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20030904001072003090400107NM 2003 9 4 QXEA200300980 120030813A5522 SKIN BOMBDRDHC8 DHC8401 1390041NM RT ELEVATOR PIN HOLE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX-DURING LIGHNING STRIKE INSPECTION FOUND RIGHT ELEVATOR HAS PIN HOLE LOCATED AT ELEVATOR RIGHT EDGE AND TRAILING EDGE OF ELEVATOR. REPAIRED IAW RD8/4-55-061. 2H72 4T RTA13NM 20030904001482003090400148WP 2003 9 4 DHL2003873582 120030630A532047505211 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT FITTING CRACKED 4.000 STA.902.000, L-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030904001502003090400150WP 2003 9 4 DHL2003873556 120030630A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 VERTICAL STAB L/E EXTERNAL PLATING SHOWS INTERIM REPAIR AT ZFS.96.000 RT SIDE (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4, PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17. PERFORMED HEAT TREATMENT IAW DPS 1.05-3, SRM 51-1-4 PG 1-3, SRM 51-1-1 PG 13, 17. CLEANED, TREATED AND PRIMED DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED DOUBLER ON VERTICAL STAB L/E AT ZFS 96.00 WITH NEW FASTENERS IAW SRM 55-2-1 FIG 4 PG 17, SRM 51-1-15 PG 1, SRM 51-1-21 PG 1. FOR REMOVAL AND REINSTALLATION SEE JC BX3B55076. 2L74 4F RT4A25 20030904001572003090400157WP 2003 9 4 DHL2003873586 120030629A532037797621 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT SPLICE FITTING CRACKED 3.000, STA 680.000, L-5L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH FASTENERS IAW SRM 51-1-20D PG 9, PLI-WASHERS IAW SRM 51-1-23 FIG 48. 2L74 4F RT4A25 20030904001652003090400165WP 2003 9 4 DHL2003873600 120030705A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING INBD L/E LOWER PLATING SHOWS CORROSION AND 2EA CRACKS 0.44 EACH ONE (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT CORRODED AND CRACKED AREA SEGMENT IAW EODHL 030608, ED-3453. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01.001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER AND FILLER IAW EODHL-030608, ED-3444. CLEANED, TREATED AND PRIMED FABRICATED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLER IAW EO DHL 030608, ED-3453. 2L74 4F RT4A25 20030904001702003090400170WP 2003 9 4 AALA20030782 120030717A3260833703 SENSOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW217518A 49895 DFW-ORD - DURING CRUISE, NOSE INDICATOR LIGHT/RED/CAME ON AND OFF SEVERAL TIMES. FOLLOWED QRH PROCEDURES. FLEW REST OF FLIGHT WITH LANDING GEAR DOWN. USED EMERGENCY GEAR EXTENSION HANDLE AS PER QRH. GOT 3 GREEN LIGHTS WITH HANDLE DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED D1-32 AND D1-32 SENSORS. PERFORMED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904001722003090400172WP 2003 9 4 AALA20030546 120030508A3350BAT5014 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21585AA 53248 DFW - DURING OVERNIGHT MAINTENANCE, DISCOVERED EMERGENCY EXIT CEILING LIGHTS FROM ROW 7 TO 10 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AY STA50. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904001802003090400180WP 2003 9 4 AALA20030690 120030624A2910 B-NUT DOUG DC9 DC982 3022082WP RT MLG LOOSE A AALAO OTHER K FLUID LOSS CRCRUISE 1 SW21442AA 49468 IAD - FLT 1088 - EN ROUTE BNA-LGA, LOST RIGHT HYDRAULIC PRESSURE IN FLIGHT, USED ALTERNATE GEAR EXTENSION. LANDED IAD WITHOUT INCIDENT. SECURED RIGHT WHEEL WELL HYDRAULIC B-NUTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904001862003090400186NE 2003 9 4 AALA20030624 220030601A73143843017 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT ENGINE MALFUNCTIONED A AALAK NONE Y ENGINE STOPPAGE CLCLIMB 1 SW21427AA 49339 DFW - FLT 1325 - EN ROUTE, AUS-DFW, LEFT ENGINE FAILED DURING CLIMB-OUT PASSING 11,000 FEET. NO OTHER INDICATIONS OF DAMAGE, INSTRUMENTS OR VISUAL. RESTARTED LEFT ENGINE OPERATION NORMAL FOR REMAINDER OF FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL PUMP AND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030904001982003090400198NM 2003 9 4 C1HA200392003 120030715A3397 WIRE BOEING727 727212 138407GNM CABIN BROKEN A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15292AS 21458 MID CABIN EMERGENCY PATH FLOOR LIGHTING INOPERATIVE. FOUND BROKEN WIRE AT ROW 21. 2L73 4F A3WE 20030904002032003090400203CE 2003 9 4 DXTA200300045 120030609A26131173T421 SENSOR CESSNA500 560CESSNA 2076750CE OVERHEAT SYS FAULTY E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07393QS 5600393 SHORTLY AFTER T/O EMER PRESS LIGHT ILLUMINATED AND EMERGENCY PRESSURIZATION ACTIVATED W/SYSTEM IN NORMAL POSITION. AIRCRAFT RETURNED AFTER TAKEOFF AND LANDED OVERWEIGHT. COPILOTS WINDSHIED HAS DISTORTION LOCATED ON BOTTOM 3RD OF WINDSHIELD. REMOVED AND REPLACED DUCT OVERHEAT SENSOR P/N1173T42-1 AND DUCT TEMPERATURE SENSOR P/N9912069-14 IAW CESSNA WIRING MANUAL CHAPTER 20-10-04. 2L72 4F RTA22CE 20030904002052003090400205WP 2003 9 4 MWEA030265 120030623A5330591140885 SKIN DOUG DC9 DC981 3022081WP FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LIGHTING STRIKE STATION 332. REPAIRED SKIN 2L72 4F A6WE 20030905000052003090500005SO 2003 9 5 LR7A03052 120030725A5320 ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL FS 527 CHINE ANGLE, CRACKED JUST BELOW SHELF BRACKET APPROX 1.5 IN. AT LBL 61, WL 143. REPAIRED IAW SRM SMP 583 53-40-27. NR 2014. 2H74 4T A1SO 20030905000122003090500012SO 2003 9 5 LR7A03059 120030725A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT CARGO DOOR FS 913 SKIN DENTED AT BL 0. REPAIRED IAW SRM SMP 583 51-140-12. NR 2102. 2H74 4T A1SO 20030905000132003090500013SO 2003 9 5 LR7A03060 120030725A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT CARGO DOOR FS 935 SKIN DENTED AT LBL 10. REPAIRED IAW SRM SMP 583 51-140-12. NR 2103. 2H74 4T A1SO 20030905000392003090500039SO 2003 9 5 C2XA03SH315 120030905A531514521700007 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 19 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EC 5320-01099. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030905000402003090500040SO 2003 9 5 C2XA03SH317 120030905A531514523186001 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030905000412003090500041SO 2003 9 5 C2XA03SH265 120030811A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV-DURING C CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND REPAIRED THE AFFECTED STRINGER IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905000482003090500048SO 2003 9 5 C2XA03SH284 120030821A711014576631622 STIFFENER EMB 145 EMB145LR 3260212SO RT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE RIGHT HAND LOWER COWLING AFT INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030903001792003090300179WP 2003 9 3 AALA20030727 120030708A2120 CLAMP DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21226AA 49176 LAS - FLT 1560 - EN ROUTE LAS-DFW, SHORTLY AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO LAS WITHOUT FURTHER INCIDENT. FOUND CLAMP BETWEEN AIR CYCLE MACHINE AND HEAT EXCHANGER LEAKING HOT AIR. CLEANED FLANGES AND REINSTALLED CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030903001802003090300180WP 2003 9 3 AALA20030816 120030730A3260 TARGET DOUG DC9 DC983 3022083WP NLG OUT OF ADJUST A AALAA UNSCHED LANDING N FALSE WARNING UKUNKNOWN 1 SW21567AM 53293 LAX - FLT 642 - BUR-DFW, RED NOSE GEAR LIGHT REMAINED ON AFTER LANDING GEAR HANDLE RAISED UP. NO GEAR FAILED TO RETRACT. MAINS OK. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR TARGETS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030903002232003090300223NM 2003 9 3 QXEA200300937 120030722A1430 BOLT DHAV DHC8 DHC8202 2809007NM GUST LOCK LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- GUST LOCK BUMPER STOP ASSEMBLY MOUNTING PLATES ON LEFT HAND AND RIGHT HAND SIDES HAVE LOOSE MOUNTING JO BOLTS. REPAIRED IAW DHC-8 RD 8-55-112. 2H72 4T RTA13NM 20030903002552003090300255SO 2003 9 3 C2XA03BT088 120030815A3260 CONNECTOR EMB 145 EMB145LR 3260212SO LANDING GEAR FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2715910 145455 EWR---CO2685, CREW REPORTED, LANDING GEAR SENSOR LIGHT IN FLIGHT COULD NOT GET GEAR UP. MAINTENANCE REMOVED AND REPLACED CONNECTOR P1192, ADJUSTED PROXIMITY SWITCH POSITION AND PERFORMED GEAR RETRACTION TEST IAW EMB145 MM 32-61-50 AND 32-30-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030903002562003090300256SO 2003 9 3 C2XA03CL157 120030829A3350 SIGN EMB 135 EMB135LR 3260305SO CABIN MALFUNCTIONED A C2XAK NONE O OTHER UKUNKNOWN 1 SW2728518 145334 CLE FLIGHT NR 2130 THE CREW REPORTED THE PAX DOOR EMERGENCY EXIT SIGN OVER THE FLIGHT ATTENDANTS SEAT INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST OF EXIT SIGN.OPERATIONAL TESTS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030904000012003090400001CE 2003 9 4 GLBA001 120030901A7700 TACH GENERATOR BEECH 1900 1900D 1154162CE NR 1 PROPELLER LOOSE A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM0396UX UE96 NR 1 PROP RPM 1450 IDLE AT 600, TIGHTENED NR 1 N2 TACH GEN. 2L72 4T RTA24CE 20030904000212003090400021NE 2003 9 4 03FDEA01085 220030710A7261 SCAVENGE PUMP BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 2 ENGINE INOPERATIVE A FDEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25258FE 20940 NR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO OIL QUANTITY SLOWLY DECREASING TO ZERO. AS OIL QUANTITY DROPPED TO ZERO OIL PRESSURE DROPPED BELOW 40 PSI AND OIL TEMP WAS INCREASING. R & R NR 2 ENG OIL PUMP IAW PRATT & WHITNEY, ENGINE MANUAL 72-00-61. RAN ENGINE AND PERFORMED LEAK CHECK. 2L73 4F4 FRTA3WE E2EA 20030904000692003090400069 2003 9 4 SWIA200312249 420030808A2210 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS FAULTY A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07916SW 7634 YD2 INOPERATIVE, CAME ON DURING TAXI OUT, WAS UNABLE TO RE-ENGAGE. INSTALLED SERVICEABLE YAW DAMPER CONTROL PANEL. OPS CHECK GOOD. 2L72 4F RTA21EA 20030905000382003090500038SO 2003 9 5 C2XA03IA080 120030808A21214611028900 GASPER FAN EMB 145 EMB145 3260210SO CABIN FAULTY A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2711107 145654 FLIGHT 3499 FROM RDU TO IAH, CREW REPORTED THAT THERE WAS A BURNING SMELL IN THE COCKPIT. THE CREW ELECTED TO DIVERT AND LANDED AT HSV WITHOUT FURTHER INCIDENT. THE FAN WAS DEFFERED UNDER MEL 21-23-03. THE MEL WAS CLEARED ON 8/8/2003 IN EWR WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED FAN. THE SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030905001102003090500110NM 2003 9 5 DL76G030637 120030712A2510 ODOR BOEING767 7673P6 1385105NM CABIN DETECTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27153DL 24985 0913 13 JUL GRU 2509601- THERE WAS A MILD ELECTRICAL SMELL AROUND SEATS 11C, 12C WHICH STOPPED WHEN THOSE OVERHEAD PANEL READING LIGHTS WERE TURNED OFF ATL MCC/MC/0236Z. INSPECTED READING LIGHT PANELS AND AREA AROUND MENTIONED SEATS NOTHING ABNORMAL FOUND. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030905001192003090500119NE 2003 9 5 DL73S030643 220030714A7200JT8D15AHK ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 BIRD INGESTION A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27304DL47615 23076 709154 IRREG: ON T/O DETECTED SMELL IN COCKPIT AND CABIN. RETURN TO CVG. FOUND EVIDENCE OF BIRD STRIKE NR 1 ENG. INSP ENG AND ENG BLEED DUCTS. PERFORMED DUCT BURNOUT AND REPLD. WATER SEPARATOR BAGS. 2L72 4F4 FRTA16WE E2EA 20030905001232003090500123NM 2003 9 5 DL764030645 120030714A3350D71701100 BATTERY PACK BOEING767 767432ER 1385134NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27827MH 29698 OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 36FG AISLE. REPLACED BATTERY PACK, CHECKS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030905001502003090500150NM 2003 9 5 DL73S030658 120030716A5551 ATTACH FITTING BOEING737 737232 1384475NM HORIZ STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 HORIZ STAB LT, RT, AND CENTER SECTIONS ATTACH FITTINGS :LUG CORROSION, INSPECTION OF THE HORIZONTAL STABILIZER ATTACH LUGS ON THE LT, RT, AND CENTER SECTIONS OF THE STAB PER BAC S/B 737-55- 1055, CORROSION WAS FOUND IN SEVERAL OF THE LUG BORES AND ON THE LUG FACES. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES AND SPOTFACING THE LUG FACES. THE LUGS WERE RESTORED WITH OVERSIZED BUSHINGS. THE REPAIR WAS ACCOMPLISHED PER ER/A 385250-14AD. 2L72 4F RTA16WE 20030905001512003090500151NM 2003 9 5 DL757030661 120030716A2611SAAU308C SMOKE DETECTOR BOEING757 757232 1384965NM LAVATORY INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27629DL 22919 FWD LAV SMOKE DETECTOR INOP, REPLACED SAME 2L72 4F RTA2NM 20030905001572003090500157NM 2003 9 5 DL76G030669 120030719A2510 ODOR BOEING767 767332 1382001NM COCKPIT DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO271603 29695 ON DECENT BELOW 5,000 FT SMELLED AN ELECTRICAL ODOR COMING FROM THE GLARESHIELD LASTED APPROX 5 MIN'S. INSP AREA AROUND AND UNDER GLARESHIELD. NO DEFECTS NOTED. ODOR NOTED. ALL CHKS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030905001732003090500173EU 2003 9 5 A6WA200360032 120030819A2120 SMOKE BAC 146 146200A 1500266EU COCKPIT DETECTED A A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31290UE E2080 ON TAXI, CABIN AND COCKPIT FILLED WITH SMOKE. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURES PER SUP 96-31. CABIN TEMP CONTROL OPS NORMAL, OK FOR SERVICE. (M) 2H74 4F A49EU 20030905001862003090500186NM 2003 9 5 USAA030140 120030804A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US47187 23237 PIT - FOUND CHORD CORRODED 8 INCHES BY 2 INCHES, BS 1016 BETWEEN STRINGERS 26L AND 26R. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-00-01 AND BOEING DWG 65C28106. CORROSION LEVEL 2, TASK NR C53-208-01. (M) 2L72 4F RTA16WE 20030905002042003090500204SO 2003 9 5 C2XA03SH302 120030827A531514523186001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905002052003090500205SO 2003 9 5 C2XA03SH293 120030827A532014521725615 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE RIGHT HAND SILL BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030903002542003090300254SO 2003 9 3 C2XA03BT087 120030902A3397 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713908 145465 EWR---CO2248, DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REPAIRED BROKEN WIRE IAW EMB145 MM 20-21-00. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20030903002582003090300258SO 2003 9 3 C2XA03TY144 120030830A532014521721009 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 TYS DURING A SCHEDULED 2C INSPECTION THE FWD DIGITAL BUTTSTRAP WAS CORRODED. MAINT REMOVED THE FWD DIGITAL, FAB A DOUBLER AND INSTALL A NEW FWD DOUBLER, ALLODINED, PRIMED AND PAINTED. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030903002692003090300269SO 2003 9 3 C2XA03SH279 120030818A321014571033005 CAP EMB 145 EMB145LR 3260212SO MLG GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK AFT LOWER MAIN LANDING GEAR BEARING CAP WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED AFT LOWER MAIN LANDING GEAR BEARING CAP IN ACCORDANCE WITH EMB 145 AMM 32-10-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2L72 4T RTT00011AT 20030903002712003090300271SO 2003 9 3 C2XA03SH277 120030817A531314529485003 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK STR 19L WAS IDENTIFIED AS GOUGED FR 52-53. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB 145 SRM 53-24-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030904000952003090400095NM 2003 9 4 QXEA200301001 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 1 SEAT TRACK HAS TOP SURFACE CORROSION AT STATION X405.737. REPAIRED IAW DHC-8 RD 8-53-1342 AND SRM 51-00-06. 2H72 4T RTA13NM 20030904001012003090400101EA 2003 9 4 QXEA200301014 120030823A5210 HINGE CNDAIRCL600 CL6002C10 1390015EA PAX DOOR LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09606QX 10023 BOI- ON FLIGHT 2456 UNABLE TO OPEN MAIN CABIN DOOR FROM EXTERNAL HANDLE. CLEANED AND LUBED HINGE AND PINS. NO PARTS REPLACED. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030904001192003090400119EA 2003 9 4 COMA0360371 120030812A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01457CA4131 7612 FLIGHT 5875 STAB TRIM, MACH TRIM AND AUTO PILOT TRIM CAUTION MESSAGES. REPLACED THE HSTCU. 2L72 4F RTA21EA 20030904001252003090400125NM 2003 9 4 DL76G030610 120030703A7334731703265 PRESSURE SWITCH BOEING767 7673P6 1385105NM GE CF6 CF680C2B6 30025NE NR 2 ENGINE FAULTY A DALAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SO27152DL 24984 695689 DURING TAKEOFF AND CLIMB GOT A R ENG FUEL FILTER MESSAGE. MESSAGE GOES OUT BELOW 88 PERCENT N1. RETURNED TO JFK AFTER DUMPING FUEL. LANDED BELOW MAX LDG WEIGHT. FOUND DIFF PRESS SWITCH AT FAULT REPLACED SAME R/U AND LEAK CK OK. MAIN FUEL FILTER CLEAN. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2L72 4F4 FRTA1NM E13NE 20030904001332003090400133NM 2003 9 4 DL73S030623 120030710A532065479564 SILL BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 FUSELAGE C-2 DOOR UPPER SILL FS 818 WEB CORROSION. DURING INSPECTION OF A TIME LIMITED REPAIR TO THE C-2 DOORWAY UPPER SILL WEB, CRACKING OF THE WEB WAS NOTED AS WELL AS A SHORT ED FASTENER IN THE SILL OUTER CHORD. THE WEB WAS REPAIRED WITH A DOUBLER AND THE CHORD WITH AN EXTRUDED ANGLE PER ER/A 381103-14AD, REV C. THE REPAIR IS CENTERED APPROX ATSTA 818. 2L72 4F RTA16WE 20030904001772003090400177WP 2003 9 4 AALA20030718 120030704A3222 SCHRADER VALVE DOUG DC9 DC983 3022083WP NLG LEAKING A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21567AM 53293 LAX - FLT 2430 - EN ROUTE LAX-DFW, AFTER TAKEOFF, UNABLE OT RETRACT NOSE GEAR. RETURNED TO LAX WITHOUT FURTHER INCIDENT. FOUND NOSE GEAR SCHRADER VALVE LEAKING. REPLACED VALVE AND SERVICED NOSE GEAR. ACCOMPLISHED NOSE GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030904001972003090400197NM 2003 9 4 C1HA200385005 120030715A2611 HOUSING BOEING727 7272S7 138407ZNM SMOKE DETECTOR BROKEN A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 FORWARD LAV SMOKE DETECTOR HOUSING IS BROKEN. 2L73 4F A3WE 20030904002012003090400201NM 2003 9 4 C1HA200396016 120030828A3397 WIRE BOEING727 7272J4 1384006NM NLG WW CHAFED A C1HAK NONE N FALSE WARNING CLCLIMB 1 GL15696CA 22574 RED (NOSE GEAR) DISAGREEMENT LIGHT REMAINED ILLUMINATED AFTER RETRACTION IN MDJ. LIGHT EXTINGUISHED WHEN GEAR LEVER WAS PLACED TO OFF FOUND CHAFFED WIRE COMING FROM LOCK SWITCH, WIRE WAS RUBBING ON AFT WALL OF WHEEL WELL, REPAIRED AND SECURED WIRE. SYS CHECK GOOD IAW MM 32-61-71 2L73 4F RTA3WE 20030905001642003090500164WP 2003 9 5 AALA20030582 120030516A2140 HEATER DOUG DC9 DC982 3022082WP CARGO BAY MALFUNCTIONED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21510AM 49804 AUS - FLT 1171 - EN ROUTE HSV-DFW, ENCOUNTERED SMOKE IN FIRST CLASS CABIN AT 33,000 FEET. ACCOMPLISHED CABN FIRE/SMOKE CHECKLIST. DIVERTED AUS AND LANDED WITHOUT INCIDENT. REPLACED FORWARD CARGO COMPARTMENT HEATER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905001652003090500165EU 2003 9 5 USAASA03089 120030727A2560C37103101 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE O OTHER ININSP/MAINT 1 EA19749US 1313 CLT - THE FORWARD RIGHT EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20030905001752003090500175EA 2003 9 5 ASOA03373 120030815A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11824AS 7203 FLT 4629 - DURING A GROUND INSPECTION IN ATL, THE CREW FOUND THE EMERGENCY FLOOR LIGHTS AT ROWS 3 AND 4 C/D TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROWS 3/4 C/D. OPERATIONAL CHECKS GOOD. AIRCRAT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030905002072003090500207SO 2003 9 5 C2XA03CL155 120030826A335078812 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712922 145338 DURING ROUTINE MAINTENANCE THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10-11 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030904000972003090400097NM 2003 9 4 QXEA200301003 120030812A5311 FRAME DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- CORROSION ON BOTTOM FLANGE OF FRAME X545 INBOARD OF STRINGER 31R BELOW NR 9 SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-20-11, 51-00-06, 51-40-11 AND 51-20-56. 2H72 4T RTA13NM 20030904001172003090400117NM 2003 9 4 QXEA200301040 120030827A3040 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09412QX 4059 BOI- 'SUP' ON FLIGHT 2303 WINDSHIELD HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT. PERFORMED EMERGENCY CHECKLIST. SELECTED WARM-UP. WINDSHIELD HEAT CAUTION LIGHT REMAINED ILLUMINATED. WINDSHIELD CONTROL CAUTION LIGHT ILLUMINATED FOR 3 SECONDS AND WENT OUT. COMPLIED WITH TEST OF PILOT AND CO-PILOT WINDSHIELD ANTI-ICE SYSTEM IAW 30-41-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030904001352003090400135NM 2003 9 4 DL73K030625 120030710A335020131A POWER SUPPLY BOEING737 737247 138448DNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27375DL 23602 LEFT OVER WING DOOR EXIT SIGN INOP DURING TEST. REPLACED POWER SUPPLY 2L72 4F A16WE 20030904001432003090400143WP 2003 9 4 DHL2003873579 120030704A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OTBD FLAP LOWER FWD PLATING SHOWS CRACK (1.000 ) AND DENT BETWEEN STA XF.322.000 AND XF.355.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030620, ED-3451. REMOVED FASTENERS. TRIMMED OUT AND REMOVED THE DAMAGED SKIN SEGMENT IAW EODHL-030620, ED-3451. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGMENT AND TWO SPLICE STRAPS IAW EODHL-030620, ED-3451. CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT INTERIOR SURFACE AND SPLICE STRAPS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE NEW SKIN SEGMENT AND SPLICE STRAPS ON LT WING OTBD FLAP LOWER FWD. SURFACE (BETWEEN STA XF.322.000 AND XF.355.000) USING NEW FASTENERS. 2L74 4F RT4A25 20030904001642003090400164WP 2003 9 4 DHL2003873614 120030703A532037797621 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT END FITTING CRACKED 2.000 STA 680.000 L-4R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVE CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IN M/C COMPT STA 680.000 L-4R IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030904001842003090400184WP 2003 9 4 AALA20030641 120030608A2711 TRIM TAB DOUG DC9 DC982 3022082WP RT AILERON DEFECTIVE A AALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW21420AA 49332 TUL - FLT 2328 - IN CRUISE AT 33,000 MACH .75 AIRCRAFT ROLLED RAPIDLY LEFT WITH AUTOPILOT ENGAGED. AUTOPILOT DISCONNECTED AND FIRST OFFICER GRABBED YOKE TO PREVENT AIRCRAFT FROM ROLLING INVERTED. DECLARED EMERGENCY AND LANDED AT TUL WITHOUT FURTHER INCIDENT. REQUIRED ABOUT 45 DEGREE RIGHT YOKE ANGLE TO KEEP AIRCRAFT LEVEL. REPLACED AILERON TRIM SPIRAL PLATE, RECLOCKED AND CENTERED. RECLOCKED RUDDER TRIM SPIRAL PLATE AND SET TRIM KNOB AND RUDDER AND TAB TO NEUTRAL. ALL SEGMENTS AT RIG NORMAL CHECKED NULL OF YAW DAMP ACTUATOR. REPLACED RIGHT AILERON TRIM TAB AND RIGGED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905000432003090500043SO 2003 9 5 C2XA03SH266 120030811A532014529150001 CROSSBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV-DURING C CHECK THE CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905000492003090500049SO 2003 9 5 C2XA03SH287 120030821A711014576057622 STIFFENER EMB 145 EMB145LR 3260212SO RT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE RIGHT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905001032003090500103SO 2003 9 5 C2XA03IA078 120030731A335020131A BATTERY EMB 145 EMB145 3260210SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 CLE - DURING PREFLIGHT INSPECTION THE CREW NOTICED THAT THE FORWARD 3 STRIPS OF FLOOR PROXIMITY LIGHTING DID NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 BATTERY TO BE LOOSE IN THE BATTERY CHARGER. THE BATTERY WAS RE-SECURED AND THE LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. 2L72 4F RTT00011AT 20030905001672003090500167EU 2003 9 5 USAASA03090 120030825A2560C37103101 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE O OTHER ININSP/MAINT 1 EA19748UW 1311 PHL - FOUND AN INCORRECT RELEASE CABLE ON THE FORWARD RIGHT ESCAPE SLIDE DURING INSPECTION. MAITNENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20030905001802003090500180EA 2003 9 5 ASOA03368 120030810A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11876AS 7576 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR LOWER STEP IAW SRM 51-73-00. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030905002332003090500233SO 2003 9 5 C2XA03CL146 120030818A3260852701 PROXIMITY SWITCH EMB 135 EMB135ER 3260203SO NLG DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2719503 145176 CVG FLIGHT NR 2645 THE CREW REPORTED AFTER GEAR RETRACTION THE NOSE GEAR DOOR REMAINED OPENED. THE GEAR WAS RECYCLED AND ON THE 2ND RETRACTION THE MAIN GEAR REMAINED DOWN WITH LANDING GEAR LEVER DISAGREE. THE AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030908001212003090800121EA 2003 9 8 SWIA200312130 120030615A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. DAMAGED AREA REPAIRED IAW CRJ 601R-53-61-117 REV 'A'. P/N: 601R-53-61-117-3 2L72 4F4 FRTA21EA E15NE 20030908001302003090800130EA 2003 9 8 SWIA200312209 120030722A27604916406 ECU CNDAIRCL600 CL6002B19 1900309EA NR 1 FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07453SW 7743 ON DEPARTURE FROM MEM WE RECEIVED FLIGHT SPOILER FAULT & OUTBOARD GROUND SPOILER FAULT MESSAGES. MDC INDICATED BOTH CHANNELS OF SECU ONE AT FAULT. REMOVED AND REPLACED SECU NR 1 IAW MM 27-61-05. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20030908001372003090800137SO 2003 9 8 SWIA200312210 120030722A2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203SO HYD SYSTEM BROKEN A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM07584SW 120352 LOST ALL GREEN SYSTEM HYDRAULIC PRESSURE AND FLUID ENROUTE FROM CDC TO SLC. REPLACED BROKEN HYDRAULIC LINE AT LEFT RESERVOIR FOR ENGINE DRIVEN HYDRAULIC PUMP. FLUSHED SYSTEM & REPLACED ENGINE DRIVEN HYDRAULIC PUMP IAW 29-10-00. OPS AND LEAK CHECKS GOOD. 2L72 4T RTA31SO 20030908001532003090800153SO 2003 9 8 SWIA200312228 120030804A275012064207613 CONTROL HANDLE EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM07268UE 120207 CONTROL FAULT ON NACELLE FLAPS. REPLACED FLAP CONTROL HANDLE. OPS CHECK GOOD. SN OFF: 200513-308 2L72 4T RTA31SO 20030908001542003090800154EA 2003 9 8 SWIA200312229 120030801A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07594SW5525 4056 7285 STAB CHANNEL 2 HSTCU WOULD NOT ENGAGE DURING PREFLIGHT. CLEANED PINS & RE-RACKED CONTROL UNIT. PERFORMED OPS CHECK. REMOVED AND REPLACED HORIZONTAL STABILIZER MOTOR CONTROL UNIT WITH A SERVICEABLE UNIT IAW MM 27-42-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20030908001572003090800157EA 2003 9 8 SWIA200312232 120030802A274170609 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07594SW 7285 STAB TRIM CH2/ MACH TRIM MESSAGE ON TAXI OUT. REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT IAW MM 27-41-01. REMOVED AND REPLACED COPILOTS STAB TRIM SWITCH WITH A SERVICEABLE UNIT IAW MM 27-41-05. NR 2 PN 309-4334 2L72 4F RTA21EA 20030908001582003090800158EA 2003 9 8 SWIA200312233 120030804A27604916406 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07411SW3826 3826 7067 INFLIGHT SLIGHT ROLLING MOTION (UNCOMMANDED) LEFT ACCOMPANIED BY FLIGHT SPOILERS FAULT STATUS MESSAGE. LEFT INBD GRND SPOILER BOXED IN WHITE. REMOVED AND REPLACED NR 2 SECU IAW CRJ MM 27-61-00 & 21-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20030908001632003090800163EA 2003 9 8 SWIA200312237 120030801A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07926SW 7687 STAB TRIM NR 2 KICKED OFF LINE AND WOULD NOT REENGAGE. REMOVED AND REPLACED HSTCU. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030908001752003090800175EA 2003 9 8 SWIA200312245 120030624A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 LT CABIN SIDE SEAT RAIL BETWEEN FS 444 AND 495 CORRODED. DISCOVERED DURING C-CHECK, DAMAGED SEAT RAIL REMOVED AND REPLACED PER CRJ AMM CH 20-21-00. P/N: 601R38312-115 2L72 4F RTA21EA 20030908001952003090800195EA 2003 9 8 SWIA200312281 120030719A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 280 PILOT'S BULKHEAD RT VERTICAL ANGLE RBL 12 CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ REO 601R-53-11-034 REV 'A'. P/N: 600-34017-724 2L72 4F RTA21EA 20030908001992003090800199EA 2003 9 8 SWIA200312285 120030719A5411 RIB CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 LT PYLON HAS CRACK IN RIB AT FS 605.00. DISCOVERED DURING C-CHECK, REPLACED RIB IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20030908002022003090800202EA 2003 9 8 SWIA200312288 120030719A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 RT LWR WING PLANK WS 148 CRACKED. DISCOVERED DURING C-CHECK, REPAIRED DAMAGED AREA IAW CRJ REO 601R-57-21-130 REV 'D'. 2L72 4F RTA21EA 20030905001362003090500136NM 2003 9 5 DL76S030650 120030712A5744113T22551 SUPPORT BEAM BOEING767 767332 1382001NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27119DL 23278 WING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : CORROSION IN AFT ATTACH HOLE BORES. THE AFT 4 ATTACH HOLES FOR THE OUTBD SUPPORT BEAM AT THE INBD FLAP ATTACH LOCATION WERE FOUND CORRODED. THE HOLES WERE REAMED TO REMOVE CORROSION, HFEC INSPECTED, OVERSIZED FOR AND INSURANCE CUT, AND BUSHED WITH ALUMINUM BUSHINGS TO RESTORE ORIGINAL HOLE SIZE. THE REPAIR WAS ACCOMPLISHED PER ER/A 385378-14. 2L72 4F RTA1NM 20030905002322003090500232GL 2003 9 5 C2XA03CL148 220030822A720023070401 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 FAILED A C2XAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW27129227540 83 145338 CAE311160 CLE FLIGHT NR 2962 THE CREW REPORTED THE NR 2 ENGINE FALIED ON CLIMBOUT FROM BTV. THE AIRCRAFT DIVERTED INTO SYR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT RELEASED FOR SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20030908001962003090800196EA 2003 9 8 SWIA200312282 120030719A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 280 RT FLOORBEAM RBL 9.0 ATTACH ANGLES IB & OB CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLES IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20030908002072003090800207EA 2003 9 8 SWIA200312293 120030719A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 CARGO PIT HAS FLOORBEAM WITH BUCKLED WEB & CRACKED AT FS 589.0 - FS 605.0; LBL 27 INBOARD SIDE. DISCOVERED DURING C-CHECK, REPAIRED IAW CRJ SRM 51-24-36. 2L72 4F RTA21EA 20030908002392003090800239EU 2003 9 8 MALA030346 120030723A29104204002 PTU BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15507XJ E2316 DURING FLIGHT NR 3482, NR 3 ENGINE HYDRAULIC TEMP LIGHT CAME ON. FOLLOWED QRH AND MX PROCEDURES, AFTER COOLING AND APX 50 MILES OUT FROM LANDING TURNED PUMP BACK UNDER DIRECTION OF MXC-DID NOT ILLUMINATE. AIR RETURN TO MEM. MAINTENANCE REPLACED PTU IAW AMM 29-20-17 PN 4204002 SN/ON LW85, SN/OFF OH75 AND REPLACED AIRBRAKE SERVO VALVE AS A PRECAUTIONARY MEASURE IAW AMM 27-63-14, PN P458A0101-02 SN/ON DAW 51-98 SN/OFF DAW49-98 RAN GREEN SYSTEM HYDRUALIC NO HIGH TEMP INDICATION NOTED.SEE 409 NR 181762 AND CONTINUATION NR 040003,040004,040000,039971 AND 039693 FOR FURTHER DETAIL. 2H74 4F RTA49EU 20030908002492003090800249NM 2003 9 8 VNAA0308018 120030826A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DISCHARGED A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07434JS1671532 3051 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030908002562003090800256CE 2003 9 8 AMWA20 120030818A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV UE163 WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB, STA 39.289 AND STAB 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL REPAIR MANUAL P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20030908002652003090800265SO 2003 9 8 SWIA200312357 120030822A4950 SWITCH EMB 120 EMB120ER 3260203SO APU MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM07235SW 120310 USING APU BLEEDS, SMOKE ENTERED THE CABIN. SMOKE WENT AWAY WHEN BOTH PACKS WERE TURNED OFF. REMOVED AND REPLACED APU BLEED SWITCH. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030908002722003090800272 2003 9 8 SWIA200312363 420030826A34256226190204 COMPUTER EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER O OTHER DEDESCENT 1 NM07268UE5771 3011 120207 DURING CLIMB AND DESCENT FLIGHT DIRECTOR V-BARS BECAME ERRATIC AND AP FOLLOWED ERRATIC MOVEMENTS. BOTH WORKED NORMALLY DURING CRUISE. REPLACED CAPTAIN'S AHRS COMPUTER AND REPAIRED WIRING TO NR 2 DPU FAN CONNECTOR. BOTH AUTOPILOTS AND FLIGHT DIRECTOR SYSTEMS OPERATE NORMALLY PER MM 22-11-00. 2L72 4T RTA31SO 20030908002792003090800279CE 2003 9 8 AMWA26 120030724A5320114430002140 CLIP BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07131YV UE131 DURING ABC CHECK, A RIGHT HAND CLIP WAS FOUND CRACKED. REPLACED CLIP IN ACCORDANCE WITH BEECH SRM 53-90-23. NO TEAR DOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030812000972003081200097EU 2003 8 12 HEEA088643 120030728A62304619307020 BUSHING BOLKMS105 BO105S 5626006EU MAIN ROTOR MISMARKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 WHEN BUSHING WAS REMOVED FROM PACKAGE, FOUND THAT IT IS ACTUALLY BUSHING P/N 4619-307-026. TO BE SENT TO VENDOR FOR CREDIT. 1G72 3U H3EU 20030812000982003081200098EU 2003 8 12 HEEA088657 120030731A3246117501031 SKID BOLKMS117 BK117A1 5626010EU MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC 7152 SKID TUBE HAS CORROSION BEYOND LIMITS. SCRAPPED. 1G72 3U H13EU 20030813000092003081300009EU 2003 8 13 HEEA088653 120030725A7714DL41239 INDICATOR BOLKMS105 BO105S 5626006EU ENG TACH HUNG UP E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033071K S859 HANGS AT 50 PERCENT DURING STARTS. PLUG CONNECTION FELL OFF DURING REMOVAL. SHOP REPAIR. 1G72 3U H3EU 20030813000792003081300079 2003 8 13 UPS03140850 420030613A2565 LIGHT AIRBUS300 A300B4622R 3930312EU EVACUATION SLIDEINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01134UP 0818 REF M26073 EVAC SLIDE WARNING LIGHT INOP. PERFORMED TEST P/N ASPCU TEST OK, WARNING LIGHT RESET OK THIS CLEARS M260973. 2L72 4F RTA35EU 20030813000932003081300093EU 2003 8 13 UPS03140845 120030606A2597 WIRE AIRBUS300 A300B4622R 3930312EU SLIDE IND LIGHT BROKEN A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01134UP 0818 BROKEN WIRE ON EMERGENCY SLIDE INDICATOR LIGHT ASSY ON CREW DOOR. DEFERRED M260973. PERFORMED TEST P/N ASPCU TEST OK, WARNING LIGHT RESET, OK THIS CLEARS M260973. 2L72 4F RTA35EU 20030813001132003081300113WP 2003 8 13 GTIA030560 120030718A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN OBSTRUCTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 GTIA - CLO PATH LIGHTING OBSCURED, EXIT ROW 21. CLEANED GLO PATH LIGHTING PAD. (M) 2L72 4F RTA6WE 20030813001182003081300118NM 2003 8 13 USAA030121 120030709A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US48813 23232 CLT - FOUND SKIN CRACKED 3.125 INCH, BETWEEN 727E AND 747, STRINGER 23L AND 24L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M) 2L72 4F RTA16WE 20030813001482003081300148NM 2003 8 13 SWAA031761 120030805A2910BACH8C04EE0230B LINE BOEING737 7373H4 1384600NM HYD SYSTEM SPLIT A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29385SW 26600 AIR TURNBACK, DECLARED EMERGENCY, A-HYD SYSTEM FAILURE ON GEAR RETRACTION. FOUND LT MLG ACTUATOR HYD UP LINE SPLIT, REMOVED AND REPLACED HYD UP LINE AND ALL 'A' HYD SYSTEM FILTERS PER MM. 2L72 4F RTA16WE 20030813001502003081300150NM 2003 8 13 SWAA031660 120030725A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030813001592003081300159NM 2003 8 13 SWAA031669 120030725A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29421LV 32452 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S NR 1, 17 AND 21. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20030813001932003081300193NM 2003 8 13 SWAA031561 120030714A53106547978 CREASE BEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CORRODED AT BS 638, BS 907 AND BS 946. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20030814000102003081400010NM 2003 8 14 SWAA031722 120030801A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030814000172003081400017 2003 8 14 SWAA031729 420030802A256565C19901 CABLE BOEING737 7373H4 1384600NM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030814000462003081400046 2003 8 14 234TR0007 420030725A3450 INDICATOR BOEING737 737228 13844AGNM HSI MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 FIRST OFFICER'S HSI - VOR FROM, ILS VALID, VOR VALID, FLAG ERRONEOUS. REPLACED HSI. ALL FUNCTIONS OPERATE NORMAL. 2L72 4F RTA16WE 20030814001042003081400104EU 2003 8 14 RAIA00306160 120030608A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03571HK 41090 EMERGENCY LIGHTS INOP AT 2A. REINSTALLED CONNECTOR AT EMERGENCY LIGHT. 2L72 4T RTA41NM 20030814001152003081400115WP 2003 8 14 UPS03840943 120030618A53404612650N FITTING DOUG DC8 DC873F 302199FWP AC COMPARTMENT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 A/C BAY STA 8 LONG 33L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4612650 AND SRM 51-1-20D. 2L74 4F RT4A25 20030814001402003081400140NM 2003 8 14 AALA20030552 120030510A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21617AM 24525 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030814001462003081400146WP 2003 8 14 GTIA030570 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200 56 INCHES LBL L1 DOOR THRESHOLD. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030814001492003081400149NM 2003 8 14 AALA20030259 120030301A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING FROM 4E-6E INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030814001602003081400160NM 2003 8 14 AALA20030470 120030418A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21643AA 24601 DURING OVERNIGHT MAINTENANCE, AFT FACING CLASS DIVIDER EMERGENCY EXIT SIGN INOPERATIVE. CONNECTED EMERGENCY EXIT SIGN QUICK DISCONNECT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000282003081500028SW 2003 8 15 HEEA088545 120030806A6320 SEAL BELL 206 206L3 1182108SW PUMP LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0330KH BH268 51527 SEAL LEAKING. IN REPAIR. 1G71 3U H2SW 20030821000132003082100013NM 2003 8 21 USAABB03116 120030724A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU 22192 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMLBY. (M) 2L72 4F RTA2NM 20030821000552003082100055NM 2003 8 21 03FDEA01053 120030702A5753 BUSHING DOUG MD11 MD11 3023602NM TE FLAP HINGE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD ACTUATOR LUG BUSHING FOUND LOOSE. RT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD ACTUATOR LUG LOOSE BUSHING REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000662003082100066NM 2003 8 21 03FDEA00925 120030616A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING- O/B FLAP I/B HINGE ACTUATOR I/B BORE FOUND CORROSION. LEFT WING- TRAILING EDGE FLAP- OUTBOARD TRAILING EDGE FLAP- SUPPORT BRACKETS- CORROSION REMOVAL AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69373. 2L73 4F RTA22WE 20030821001822003082100182WP 2003 8 21 03FDEA01271 120030812A1430716584 BOLT DOUG DC10 DC1010 3022110WP NR 3 PYLON LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO2510060 46970 NR 3 ENG UPPER PYLON HAS NUMEROUS 1/4 BOLT LOOSE ON LT, RT, FWD AND AFT SIDE OF FWD AND AFT THRUST LINK FITTING (MARKED WITH RED). REPLACED (24) LOOSE BOLTS AND TORQUED REMAINING FASTENERS REF SRM 51-31-01 AND M/M 20-50-02-2. HFEC INSPECTED AROUND NEW BOLTS, NO INDICATIONS. 2L73 4F A22WE 20030813000182003081300018 2003 8 13 HEEA088606 420030715A2350AA34300 INTERPHONE BELL 206 206L3 1182108SW COCKPIT DISTORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 INTERPHONE HAS IT`S MODULATION DISTORTED. 1G71 3U H2SW 20030813000372003081300037EU 2003 8 13 RAIA00306154 120030602A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSLOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03561HK 41077 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RESECURED CONNECTOR. 2L72 4T RTA41NM 20030813000872003081300087NM 2003 8 13 2003UALA00486 120030608A5270 PROXIMITY SENSOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CARGO DOOR DIRTY A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29849UA 1649 FWD CARGO MESSAGE DISPLAYED ON UPPER ECAM SCREEN. CLEANED CARGO DOOR PROXIMITY SENSOR. 2L72 4F4 FRTA28NM E40NE 20030813001252003081300125NM 2003 8 13 AALA20030734 120030709A2420 RELAY BOEING767 767323 1385205NM ELECTRICAL FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21396AN 29603 LAX - FLT 217 - EN ROUTE ORD-OGG, THREE HOURS INTO FLIGHT, RECEIVED LEADING EDGE SLAT ASYMMETRY EICAS CAUTION AND STANDBY BUS OFF CONDTIONS. DC STANDBY CIRCUIT BREAKER POPPED. EMERGENCY DECLARED AND LANDED AT LAX WITHOUT FURTHER INCIDENT. REPLACED DC STANDBY CIRCUIT BREAKER AND K109 RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030813001472003081300147NM 2003 8 13 SWAA031760 120030804A274069763511 BUSHING BOEING737 7373H4 1384600NM STAB TRIM WHEEL WORN A SWAAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW29621SW 28037 EXCESSIVE VIBRATION IN STAB TRIM WHEEL WHEN TRIM IS APPLIED. REMOVED AND REPLACED RT OUTBD STAB TRIM WHEEL BUSHING PER MM. 2L72 4F RTA16WE 20030813001692003081300169NM 2003 8 13 SWAA031679 120030728A53116546529 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKRD (2 EA) AT BS 500, WL 148 AT RBL 8 AND BS 827, WL 148 AT RBL 3. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030814000912003081400091NM 2003 8 14 2003UALA00558 120030715A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 CABIN STA 776-796, LBL 56, SHORT SEAT TRACK IS GOUGED AT CROWN. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SEAT TRACK. 2L72 4F4 FRTA1NM E24NE 20030814000992003081400099SO 2003 8 14 RAIA00306157 120030606A323023092900001 UPLOCK EMB 145 EMB145 3260210SO MLG BROKEN A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03805HK9422 145096 NOSE GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED NLG UPLOCK BOX. 2L72 4F RTT00011AT 20030814001012003081400101NM 2003 8 14 UPS03441056 120030718A5320 SUPPORT BOEING747 747123 1384873NM FAIRING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FOUND SURFACE CORR AT STA 920 FROM LBL 30 - RBL 20. BODY FRG SUPPORTT COR REMOVED AT LBL 25 TO LBL 30 AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 WITHIN SRM 53-50-01 FIG 5 LIMITATION, BL 0 TO LBL 26 SUPPORT REPAIRED AS PER SRM 53-50-04 FIG 2 DUE TO EXCEEDED LIMITATION AS PER SRM 53-50-01 FIG 5 AFTER COR BLEND OUT 0.050 X 1 X 1 INCH BL 0 TO RBL 20 SUPPORTT REPAIRED REF NRC 5856 DETAIL. 2L74 4F A20WE 20030814001062003081400106SO 2003 8 14 RAIA00306162 120030610A7830TY203802A ACTUATOR EMB 145 EMB145 3260210SO THRUST REVERSER FAULTY A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03806HK9494 145112 EICAS MSG ENG REV DISAGREEMENT. MAINTENANCE PLACED NR 2 TR ON DMI PER MEL; SUBSEQUENTLY CLEARED DMI REMOVING BY REPLACING THE PRIMARY DOOR LOCK ACTUATOR. 2L72 4F RTT00011AT 20030814001092003081400109GL 2003 8 14 RAIA00306165 220030615A753223074337 BLEED VALVE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE FALSE INDICATIONA RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03817HK 145058 311092 EICAS MESSAGE ENGINE 1 NO MARGIN. MAINTENANCE PERFORMED THRUST ASSURANCE CHECKS AND DEFERRED THE ATTCS SYSTEM PER MEL; SUBSEQUENTLY CLEARED DEFERRAL BY REMOVING AND REPLACING THE NR 1 ACCELERATION BLEED VALVE. 2L72 4T4 FRTT00011ATTE6CH 20030814001112003081400111CE 2003 8 14 DXTA200300055 120030627A2120 ACM CESSNA750 750 2076810CE CABIN COOLING SEIZED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07983QS 7500083 AT TEB DURING GROUND OPS OF APU NORMAL APU BLEED SELECTED WITH NORMAL APU EGT TEMPS, ISOLATION VALVE OPEN, PILOTS NOTED GRINDING NOISE. ACM SEIZED CAUSING CABIN TO FILL WITH SMOKE. REMOVED SEIZED FORWARD ACM AND INSTALLED OVERHAULED UNIT, OPS & LEAK CHECK GOOD ALL WORK PERFORMED IAW CE750 MM CHAPTER 21-51-00. 2L72 4J RTT00007WI 20030814001222003081400122WP 2003 8 14 UPS03841037 120030706A5520 INTERCOSTAL DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C2 LT HORIZONTAL STAB INBOARD L/E T-ANGLE AT STA XFS 60 IS CRACKED. REMOVED LT HORZ STAB T-ANGLE. DRILLED AND LOCATED NEW ANGLE IAW DC8 SRM 51-1-24. INSTALLED ANGLE IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030814001452003081400145WP 2003 8 14 GTIA030569 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 44 INCHES RBL TO 15 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030814001472003081400147NM 2003 8 14 AALA20030354 120030319A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21619AA 24577 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD COACH EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHEKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030821002552003082100255NM 2003 8 21 USAABB03124 120030727A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19621AU 27200 CLT - FOUND SEAT 18 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20030822000422003082200042NM 2003 8 22 2003UALA00475 120030605A492038269612 BEARING BOEING777 777222 1385219NM PWA PW4077PW4077 NE APU MISREPAIRED A UALAH DEACTIVATE SYST/CIRCUITS BW SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C CRCRUISE 1 WP29211UA 30217 OIL ODOR IN FLIGHT DECK AREA. SMOKE AND ODOR IN MAIN CABIN WITH LOWER RECIRCULATING FAN OFF. *SUPPLEMENTAL DATA UPDATE* MAINTENANCE CONFIRMED THE SMELL WAS COMING FROM APU. APU WAS REPLACED AND THE SHOP DISASSEMBLED THE LOAD COMPRESSOR MODULE TO FIND THE ROOT CAUSE OF THE PROBLEM. THE SHOP FOUND IMPROPER REPAIR OF THE LOAD COMPRESSOR REAR BEARING CARRIER. THE BUFFERED AIR PASSAGE WAS BLOCKED TO THE REAR LOAD COMPRESSOR KNIFE EDGES BY FLAME SPRAY. 2L72 4F4 FRTT0001SE E46NE 20030822001222003082200122NM 2003 8 22 SCNA03006 120030728A3350D71702001 POWER SUPPLY BOEING737 7378Q8 13844BXNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15806SY 28215 EMERGENCY LIGHTS AT 17ABC OFF IN OVERHEAD & SEATS (17 THROUGH 23). REMOVED AND REPLACED POWER SUPPLY & BATTERY PACK AT 21 ABC & CKS GOOD. 2L72 4F RTA16WE 20030822001342003082200134NM 2003 8 22 QXEA200300939 120030803A3040 SMOKE DHAV DHC8 DHC8202 2809007NM COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09369PH 513 BOI- ON FLIGHT 2217 NOTICE STRONG BURNING ODOR ON FLIGHT DECK WITH WINDSHIELD HEAT IN WARM UP AND NORMAL. BEFORE GOING TO OFF, NOTICED LITE SMOKE FROM WIRES ON CAPTAIN'S SIDE WINDSHIELD. BOTH WINDSHIELDS FELT COOL TO THE TOUCH IN FLIGHT. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030822001372003082200137NM 2003 8 22 CALA0300441 120030506A5320 STIFFENER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INSPECTION FOUND AFT PRESSURE BULKHEAD SIDE, TWO EACH CENTER CHANNEL STIFFENERS CORRODED ON BOTH SIDES AT STA 1016. A STIFFENER REPAIR WAS INSTALLED IAW DRAWING 65C28106-1. 2L72 4F RTA16WE 20030822001692003082200169WP 2003 8 22 UPS03841025 120030726A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 172.5 TO XFS 178. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-0 FIG 2, 51-1-21 FIG 33. 2L74 4F RT4A25 20030822001712003082200171WP 2003 8 22 UPS03841027 120030725A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 260 AT LBL 60. CUT OUT DAMAGE AND INSTALLED SEAT TRACK PLUG IAW SRM 53-2-3 FIG 6D. 2L74 4F RT4A25 20030825000102003082500010NM 2003 8 25 UPS03240964 120030606A5330 SKIN BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C SUSPECT CRACK AT MID GALLEY DOOR UPPER HINGE CUT OUT REPAIR CARRIED OUT IAW SRM 51-10-2. SKIN REPAIR CARRIED OUT IAW SMRO EO 2003-038-004 UPS ENGINEERING FILE NO. B727-5330-18961. 2L73 4F A3WE 20030825000182003082500018WP 2003 8 25 UPS03841089 120030724A53134772397U1 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 STATION 1766 LONG. 17R LONGERON AND END FITTING ARE CRACKED. REMOVED,FABRICATED AND INSTALLED LONGERON SECTION,AND REPLACED END FITTING IAW DWG 5649327,4772397 AND SRM. 51-1-20D 2L74 4F RT4A25 20030825000232003082500023 2003 8 25 UPS03M41018 420030731A2565 SLIDE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE R1 DOOR DEPLOYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP 48768 R1 DOOR SLIDE DEPLOYED. DEFERRED IAW MEL 52-10-3-2. DOOR IS INOPERATIVE, M263900 ASSIGNED. PLACARD INSTALLED. 2L73 4F4 FRTA22WE E13NE 20030825000292003082500029NM 2003 8 25 UPS03440961 120030618A5330 SKIN BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C FX - LOWER FUSELAGE EXTERNAL SKIN FOUND BULGE - AT STA 2182 TO STA 2184 STRG 44R RT SIDE. FX STRINGER REPAIRED AT BS 2180 - 2210 STR 41R AS IAW SRM 53-10-03 FIG 1 AND FX EXTERNAL SKIN REPAIRED AT BS 2180 - 2184 STR 44R AS IAW SRM 53-30-03 FIG 47 DUE TO SKIN BLENDED OUT AREA 0.042 INCH X 2 INCH LENGTH X 1 WIDTH AND STRINGER CORROSION CRACK ABOUT .7500 INCH LONG WHICH ARE EXCEEDED SRM 53-30-01 FIG 1 AND 53-10-01 FIG 1 LIMITATION RESP. 2L74 4F A20WE 20030825000372003082500037WP 2003 8 25 UPS03840885 120030622A5730 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 LEFT WING CENTER LE. LOWER SKIN IS CRACKED AT FASTENER HOLES AT XOLDI 6.225 STOP DRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX. C 2L74 4F4 FRT4A25 E2GL 20030825000432003082500043WP 2003 8 25 UPS03841086 120030725A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 LEFT AFT HEAT EXCHANGER EXTERNAL FUSELAGE SKIN LOWER AFT CORNER IS CRACKED STA. -12 AT LONG. 27L CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. E.O. DC8-5330-4732 2L74 4F RT4A25 20030825000482003082500048WP 2003 8 25 UPS03841108 120030726A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 MAIN CABIN LONGERON 5R IS CORRODED BEYOND LIMITS AT STA. 1745. CUTOUT DAMAGED AREA,FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM. 53-2-2 FIG. 12 2L74 4F RT4A25 20030825000572003082500057EU 2003 8 25 UPS03141141 120030815A5330 SKIN AIRBUSA300 A300F4622R 3930360EU FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01139UP 0805 INSPECTION TYPE:C1 DENT ON FUSELAGE, FWD OF TAIL STAND FITTING WITHIN LIMITS REINSPECTED DENTS FOUND TO BE OUT OF LIMITS, INSTALLED REPAIR IAW A3 00 SRM 53-40-12. FABBED DOUBLER IAW A300 SRM 53-10-12. ALODINED AND PRIMED DOUBLER IAW A300 SRM 51-21-10 2L72 4F RTA35EU 20030929001022003092900102NE 2003 9 29 0301689961 220030903A7314 SHAFT DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE FUEL PUMP FAILED A NWAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL01924RW RW3372 47185 696561 SHORTLY AFTER TAKEOFF AT APPROX. 700 FT. ENGINE NR 1 FLAMED OUT. FLIGHT CREW RETURNED AC TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE FUEL PUMP INPUT SHAFT FAILED. MAINTENANCE REPLACED THE FUEL PUMP AND FUEL CONTROL. 2L72 4F4 F A6WE E2EA 20030929001302003092900130NM 2003 9 29 03FDEA01452 120030904A3610 CLAMP BOEING727 727200 138407ENM ZONE 400 LEAKING A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 SO25207FE 22929 ON CLIMBOUT, FROM MEM NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH. LIGHT EXTINGUISHED. FOUND CLAMP BETWEEN SHUTOFF VALVE AND PRECOOLER LEAKING. REMOVED AND REPOSITIONED CLAMP IAW SMP PERFORMED ENGINE IAW JRH. LEAK CK. GOOD. RE-INSTALL LOWER STUB PANEL. IAW SMP. 2L73 4F RTA3WE 20030930000302003093000030NE 2003 9 30 MALA030397 320030829A61408542M2 COMPUTER SAAB SF340 SF340A 7850100EU ROTOL R389 R3894123F26 NE AUTOCOARSEN MALFUNCTIONED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15110XJ 504 340A110 AUTOCOURSEN LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED AUTOCOURSEN COMPUTER. P/N ON AND OFF 8542M2, SN/ON 504, S/N OFF 215 2L72 4T RTA52EU 6 CP30NE 20030930000372003093000037NM 2003 9 30 2003UALA00654 120030831A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 AFT CARGO COMPT AT STA. 1580, RBL 48 INCH FLOORBEAM CRACKED BELOW UPPER T-CHORD. MAJOR REPAIR ACCOMPLISHED. WEB REPAIRED AND DOUBLER INSTALLED. 2L74 4F4 FRTA20WE E24NE 20030930000682003093000068EU 2003 9 30 MALA030405 120030805A5330 SKIN SAAB SF340 SF340A 7850100EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15106XJ 340A106 DURING 4K CHECK IN CWA, LT FUSELAGE HAS SEVERAL DENTS ABOVE WINDOW DOUBLER REINFORCEMENT FROM STA 340-353. COMPLETED REPAIR ON LH FUSELAGE IAW EO S53009. A/C RELEASE DATE 8/11/03. REFER TO 409 192555 FOR DETAIL. 2L72 4T RTA52EU 20030930000902003093000090WP 2003 9 30 ABXA030349 120030815A5312995821225 PRESSURE PANEL DOUG DC9 DC932F 3022067WP LT WHEEL WELL CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 PRESSURE PANEL DOUBLER WAS BULGING LEFT BUTT LINE 8 TO LEFT BUTT LINE 16, FS 756. REPLACED LOWER T-ANGLE OF FLOORBEAM FS 756, BUTT LINE 56 RIGHT TO BUTT LINE 54 IAW DC-9 SRM 51-30-2, 51-30-5 AND REA D953-48132. 2L72 4F A6WE 20030930000912003093000091WP 2003 9 30 ABXA030350 120030818A53209922042506 FLOOR SUPPORT DOUG DC9 DC932F 3022067WP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 RIGHT FLOOR SUPPORT STRUT END FITTING STA 313 CRACKED AT LONGERON 23 RIGHT. REPLACED FLOOR SUPPORT STRUT IAW DC-9 SRM. 2L72 4F A6WE 20030930001032003093000103NM 2003 9 30 PCAA0309106 120030904A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT LOOSE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13842EX 341 DURING ROUTINE MAINTENANCE VISIT THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. AFTER INSPECTION A BROKEN WIRE WAS DISCOVERED. WIRE WAS RESECURED, AND THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930001292003093000129EU 2003 9 30 DHL2003365014 120030908A3240 SERVO VALVE AIRBUS300 A300B4203 3930306EU RT MLG INOPERATIVE A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01365DH 149 RT REAR MAIN TIRE NR 8 BLOWN ON TAXI OUT ROLLED EMERGENCY EQUIPMENT AND MAINTENANCE TO VERIFY OKAY TO TAXI BACK TO BLOCKS. TROUBLESHOT FOUND NR 8 TIRE MAINTAINING PROPER PRESSURE. ALSO FOUND A PORTION OF THE TIRE RECAP PEELED OFF. REPLACED TIRE IAW MM 12-37-32. DEACTIVATED NR 8 BRAKE IAW CVG MX REQUEST IAW MEL NR 32-42-09 DMI NR 14074. REFERENCE DMI NR 14074 NR 8 BRAKE DEACTIVATED IAW MX CONTROL REQUEST DUE TO BRAKE DRAGGING REACTIVATED NR 8 BRAKE. REPLACED NR 8 BRAKE GREEN SERVO VALVE ANTISKID IAW M/M 32-42-48 OPS CHECKED NORMAL. THIS CLEARS DMI NR 14074. 2L72 4F RTA35EU 20030930001312003093000131EU 2003 9 30 DHL2003367007 120030909A3350 BATTERY PACK AIRBUS300 A300B4203 3930306EU EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01367DH 265 LT L1 DOOR EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERY PACK 44WL IAW M/M 33-51-11. OK FOR SERVICE. 2L72 4F RTA35EU 20030930001332003093000133WP 2003 9 30 ARWA20030901 120030903A323056165545503 CYLINDER DOUG DC8 DC863F 302198FWP MLG BROKEN A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19441J 45688 AFTER TAKE-OFF, WHEN GEAR WAS RETRACTED; NOT LATCHED AND DOORS NOT LATCHED. LIGHT REMAINED ILLUMINATED. PERFORMED LANDING GEAR SYSTEM ABNORMAL CHECK LIST AND RETURNED TO MNMG. FOUND RT GEAR BOGIE TRIM CYLINDER BROKEN AT FORWARD ATTACH POINT; REMOVED AND REPLACED RT BOGIE TRIM CYLINDER IAW MM 32-33-1. LEAK CHECKED; NO LEAKS NOTED. ACCOMPLISHED PER ALTERNATE METHOD IAW MM 32-33-1. ALSO FOUND RT GEAR DOOR LATCH ASSEMBLY WITH ARMS BROKEN; REMOVED AND REPLACED ARMS IAW MM 32-12-1 & MM 20-10-1. DOOR OPERATIONAL CHECK NORMAL IAW MM 32-12-1. 2L74 4F 4A25 20031001000142003100100014WP 2003 10 1 ARWA20030904 120030905A5420 ANGLE DOUG DC8 DC861 3021952WP NR 3 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1929UA 46159 DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YIP NR 227 RT SIDE ANGLE WITH CRACK. 2L74 4F 4A25 20031001000192003100100019NM 2003 10 1 QXEA200301080 120030828A5753 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CHAFE ON INBOARD END OF RT OUTBOARD FLAP. REPAIRED IAW DHC-8 SRM 51-20-26 AND RD 8-57-1022. 2H72 4T RTA13NM 20031001000242003100100024EA 2003 10 1 103901 120030904A2120600950679 DUCT CNDAIRCL600 CL6001A11 1900302EA AFT A/C DISCONNECTED E ERYAO OTHER J WARNING INDICATION CRCRUISE 1 CE07895CC6758 1039 DETECTED A RISE IN CABIN ALTITUDE THAT WAS NOT CONSIDERED NORMAL. MADE A PRECAUTIONARY DESCENT AND PERFORMED THE CABIN PRESSURE LOW CHECKLIST. LANDED AIRCRAFT AT INTENDED DESTINATION WITHOUT INCIDENT. FOUND A/C DISTRIBUTION DUCT FORWARD OF APU DISCONNECTED. RECONNECTED DUCT. 2L72 4F RTA21EA 20031001000292003100100029 2003 10 1 CALA0300519 420030910A2565D31393110 SLIDE BOEING757 757224 1384958NM CABIN OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW271712816397 27567 THE RT OFF WING SLIDE SYSTEM FAILED DURING FUNCTION TEST WHILE AIRCRAFT WAS IN (C) CHECK AT LTN. THE DOOR AND SLIDE CARRIER FAILED TO DEPLOY DURING FUNCTION TEST AS PRESCRIBED BY CO WORK CARD 19-2560-1-7602(MPD-25-65-00-05B, MRB-25-020. THE LOCK FITTING, CONTROL ROD PIN, CARRIER LOCK ASSEMBLY, DOOR LATCHES AND STUDS WERE ADJUSTED AND LUBRICATED IAW MM 25-65-00. A FUNCTIONAL TEST WAS PERFORMED WITH SUCCESS. 2L72 4F RTA2NM 20030821001202003082100120NM 2003 8 21 03FDEA00872 120030613A3260 WARNING SYSTEM BOEING727 727200 138407ENM COCKPIT ACTIVATED A FDEAK NONE J WARNING INDICATION CLCLIMB 1 SO25270FE 22035 AFTER TAKEOFF AND PLACING THE GEAR LEVER TO UP RECEIVED A RED DOORS LIGHT. RECYCLED GEAR AND LIGHT WENT OUT. UNABLE TO DETERMINE WHICH DOOR CAUSED RED LIGHT TO ILLUMINATE. NO MENTION OF AMBER LIGHT ON S/O ANNUN PANEL. PERFORMED ADJ/TEST PER AMM 32-62-011-5. OPS CHECKS NORMAL. 2L73 4F RTA3WE 20030821002182003082100218NM 2003 8 21 03FDEA00811 120030522A5753ARC29531 RIB DOUG MD11 MD11 3023602NM T/E FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LEFT WING - INBOARD TRAILING EDGE FLAP, NR 2 VANE TRACK CUTOUT FOUND RIB STRUCTURE WITH CHAFING MARK NEAR ROLLER AREA. WORK CARRIED OUT IN ACCORDANCE WITH FEDEX EA 1-5750-69350 - WINGS - LEFT INBOARD FLAP NUMBER 2 FLAP VANE TRACK RIB WORN LUG - REPAIR. 2L73 4F RTA22WE 20030821002432003082100243NM 2003 8 21 2003UALA00471 120030605A352021654 CONTROL UNIT BOEING747 747451 1384940NM PWA 4056 PW4056 NE PAX O2 SYSTEM OVERHEATED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29105UA 132 26473 PASSENGER EMERGENCY OXYGEN SYSTEM PROBLEM. PASSENGER OXYGEN QUANTITY AT 800 PSI AND DECREASING. *SUPPLEMENTAL DATA UPDATE* A VOLTAGE AVERAGING UNIT INTERNALLY OVERHEATED AND BURNED THE CIRCUIT BOARD, CAUSING FAILURE OF THE PASSENGER INDICATION SYSTEM. THE UNIT WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 20030821002502003082100250NM 2003 8 21 03FDEA01351 120030821A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CORROSION (C53-224-03(1/2) AT BS 344, LBL 40, WL 208, ON TOP OF FLOORBEAM. REMOVED CORROSION BS 344, WL 208, LBL 40. FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM UPPER CHORD BS 344, BL 0 TO LBL 70 & INSTALLED REPAIR. ALL IAW SRM 53-10-1 & 53-10-8, FIG 9. 2L73 4F RTA3WE 20030821002692003082100269NM 2003 8 21 USAASB03124 120030731A335020131A BATTERY PACK BOEING737 7374B7 1384702NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19426US 24548 PIT - MAINTENANCE FOUND A SECTION OF SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030821002762003082100276NM 2003 8 21 USAASB03105 120030711A33503114981 REFLECTOR BOEING737 7373B7 1384580NM EXTERIOR CORRODED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19531AU 24478 ORD - MAINTENANCE REPORTED THE AFT ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE FOUND THE REFLECTOR ASSEMBLY CORRODED. INSTALLED NEW REFLECTOR ASSEMBLY AND BULB, P/N 1619. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030822000512003082200051NM 2003 8 22 2003UALA00564 120030716A5753 FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE T/E FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 LEFT INBOARD FLAP, INBOARD FITTING FOR AFT FLAP ATTACH POINT CRACKED ON INBOARD SIDE OF FITTING. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING. 2L72 4F4 FRTA1NM E24NE 20030822000642003082200064NM 2003 8 22 UPS03441100 120030723A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C FWD CARGO COMPT - LT STA 740 - STA 820 STRINGER 44 FOUND CRACKED (3 LOCATION). FWD CARGO COMPT - LT STA 740 - STA 820 STR 44L REPAIRED PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20030822001182003082200118 2003 8 22 RAIA00307183 420030706A34177000700959 ADC AEROSPATR42 ATR42300 8680920EU E/E BAY FAULTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03421TE224 102 5500-STL- F/O'S ALTIMETER SHOWS OFF FLAG AT 5000 FT. MAINTENANCE REMOVED AND REPLACED AIR DATA COMPUTER. 2H72 4T RTA53EU 20030822001572003082200157NM 2003 8 22 QXEA200300947 120030731A5330 PAINT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX- FUSELAGE SKIN HAS A SCRATCH BELOW RIGHT HAND AFT SERVICE DOOR. REPAIRED IAW Q400 RD 8/4-53-0677 AND HORIZON AIR EA 6-53-288. 2H72 4T RTA13NM 20030822001632003082200163EU 2003 8 22 UPS03141028 120030802A5270 SWITCH AIRBUS300 A300B4622R 3930312EU PAX DOOR FAULTY A IPXAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO01148UP 831 INSPECTION TYPE:N/A AIR TURNBACK DUE TO CABIN DOOR INDICATING OPEN IN FLIGHT AT FL230 AND 60 NM FROM MCI. FOLLOWED CHECKLIST AND RETURNED TO MCI. C/W FWD PASSENGER DOOR ADJUSTMENT TEST IAW A300 AMM 52-10-11-5 UP TO FUNCTIONAL TEST. DIMENSIONS ARE WITHIN AMM LIMITS. REMOVED AND REPLACED BOTH DOOR WARNING SWITCHES WITH REF TO MM 52-10-11-5. NO DEFECTS. 2L72 4F RTA35EU 20030825000642003082500064NM 2003 8 25 UPS03241069 120030717A57536521632 SKIN BOEING727 72725C 138400HNM T/E FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C 2 AREAS OF DELAM FOUND DURING SURFACE CORROSION REMOVAL ON LEFT I/B MIDFLAP AFT UPPER SKIN. NOTE THAT DURING REPAIR 2 AREAS OF DISBOND OCCURRED ON LOWER SURFACE. REPAIRS CARRIED OUT IAW SRM 51-40-20. 2L73 4F A3WE 20030825000842003082500084NM 2003 8 25 03FDEA01343 120030819A5320 STRUCTURE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 BS 1225 RBL 20 WL 185 STRUCTURE UNDER AIRSTAIR ACTUATOR MOUNT IS CRACKED. REMOVED, DRILLED UP & INSTALLED REPLACEMENT "L" ANGLE SUPPORT BS 1265, WL 185, RBL 20-45 IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20030825000882003082500088NM 2003 8 25 CALA0300440 120030806A5514 BUSHING BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FORWARD LUG CORRODED AROUND BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW SRM 55-10-10. 2L72 4F RTA16WE 20030825000892003082500089NM 2003 8 25 03FDEA01244 120030808A5753 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING INBOARD FLAP SIDE LOAD FITTING FOUND CRACKED. LT WING INBOARD FLAP SIDE LOAD FITTING REMOVED AND REPLACED AS PER MM 20-50-02 AND OPERATIONAL CHECK REFER WORK CARD NO: E1-5750-7-5003A PT1, INSPECT AND REFURBISH INBOARD TRAILING EDGE FLAP & VANE ASSEMBLY. 2L73 4F RTA22WE 20030825001002003082500100EA 2003 8 25 COMA0360365 120030809A497038760016 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA APU MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01446CA 7546 FLIGHT 5711 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE LOW OIL PRESSURE SWITCH. 2L72 4F RTA21EA 20030825001052003082500105EU 2003 8 25 03226302 120030814A3350FU248 FUSE JETAIRJETSTMJETSTM4101 1500501EU BATTERY PACK BLOWN A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27302UE 41013 DURING MAINTENANCE INSPECTION THE LEFT AFT EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A FUSE FROM THE NR 4 EMERGENCY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030825001172003082500117WP 2003 8 25 ABXA030232 120030603A54209915500029 ANGLE DOUG DC9 DC933F 302207AWP PWA JT8 JT8D* NE LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 TWO ANGLES CRACKED (UPPER AND LOWER) IN LEFT PYLON, UNDER PANEL 8111. REPLACED ANGLES IAW SRM 51-30-2 AND 51-30-1. 2L72 4F4 F A6WE E2EA 20030825001182003082500118WP 2003 8 25 ABXA030329 120030818A32600080004003 CONTROL BOX DOUG DC9 DC941 302207NWP LANDING GEAR FAULTY A ABXAB EMER. DESCENT N FALSE WARNING APAPPROACH 1 GL23958AX67 47760 UPON GEAR EXTENSION FOR LANDING, THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. COMPLIED WITH ABNORMAL PROCEDURES AND LANDED WITH THE LIGHT ILLUMINATED. REPLACED THE MAIN LANDING GEAR PROXIMITY SWITCH CONTROL BOX IAW DC9 MM. 32-60-03-2-0201. 2L72 4F A6WE 20030825001262003082500126GL 2003 8 25 C2XA03IA083 220030813A727023060117 MANIFOLD EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 1 ENGINE DISLODGED A C2XAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SW27171151835 145666 CAE312306 IAH - AFTER ROTATION THE CREW REPORTED THAT THE NR 1 ENGINE EXCEEDED ALLOWABLE TEMPERATURE LIMITS. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 ENGINE AND FOUND THAT THE UPPER BYPASS DUCT PANEL AND MANIFOLD ASSEMBLY HAD PULLED LOOSE FROM THE OUTER BYPASS DUCT. THE NR 1 ENGINE WAS REMOVED AND REPLACED, OPERATIONALLY TESTED AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030825001362003082500136SO 2003 8 25 C2XA03TY135 120030820A339766367 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED 2C INSPECTION THE NR 4 PROXIMITY LIGHTING STRIP WIRE WAS FOUND BROKEN. MAINT REPAIRED THE BROKEN WIRE AND OPS CHECK GOOD IAW EMB 145 AMM 33-50-00. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030825001382003082500138NM 2003 8 25 AMTA200300968 120030728A2560 STRIP BOEING737 73783N 13844HINM CABIN DETACHED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11314TZ 30640 EMERGENCY FLOOR LIGHTING STRIP DETACHED FROM FLOOR BY AFT LAVATORY. REMOVED AND REPLACED AFT LEFT PHOTOLUMINESCENT STRIP PER MM 33-51-15. (M) 2L72 4F RTA16WE 20030825001392003082500139NE 2003 8 25 AMTA200300997 220030802A7260 SEAL BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE LEAKING A AMTAO OTHER K FLUID LOSS CRCRUISE 1 GL11552TZ 32586 31804 LEFT ENGINE OIL QUANTITY DECREASING APPROX 1 QUART PER 15 MIN IN CRUISE ARRIVED SFO 9 QUARTS TOTAL. REPLACED TOWER SHAFT UPPER SEALS PER MM 72-62-01-04. LEAK CHECK NR 1 ENGINE, OPS CHECK NORMAL. (M) 2L72 4F4 FRTA2NM E12EU 20030825001402003082500140WP 2003 8 25 GTIA030612 120030723A5753 MOUNT DOUG DC9 DC982 3022082WP T/E FLAP CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - LEFT INBOARD FLAP VANE RIGHT AFT MOUNT CORRODED. LEFT INBOARD FLAP VANE HAS .75 INCH DIAMETER DENT IN LEADING EDGE VERTICAL CRACK THROUGH CENTER OF DEN. DUE TO INTERNAL DAMAGE FROM CORROSION IN ATTACH FITTINGS UNIT EXCHANGE. INSTALLED LEFT INBOARD FLAP VANE. (M) 2L72 4F A6WE 20030825001432003082500143WP 2003 8 25 GTIA030608 120030628A5522 SKIN DOUG DC9 DC982 3022082WP ELEVATOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND RIGHT ELEVATOR ALL UNPAINTED UPPER AND LOWER SKIN HAS LEFT SURFACE CORROSION. ELEVATOR SKINS FOUND TO BE OUT OF LIMITS. ELEVATOR REPLACED WITH NEW ELEVATOR. (M) 2L72 4F A6WE 20030825001492003082500149NM 2003 8 25 AALA20030671 120030615A2120 ODOR BOEING777 777223 1385213NM CABIN DETECTED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21771AN 29579 YQX - FLT 98 - UNIDENTIFIED STRONG ELECTRICAL ODOR IN AREA OF 3HJ UNABLE TO LOCATE SOURCE. LANDED AT NEAREST AIRPORT. REMOVED F/C CEILING PANEL AND INSPECTED. REMOVED FORWARD CARGO SIDEWALL PANELS AND INSPECTED. INSPECTED ALL AVIONICS RACKS IN /E/ COMPARTMENT. INSPECTED EVERY F/C SEAT FOR BURNED WIRES OR COMPONENTS, RAN BOTH ENGINES AND SUPPLIED ELECTRICAL POWER FROM EACH IDG TO ALL GALLEYS. IFE SYSTEM AND POWER BUSES. AIRCRAFT OPERATES WITH NO ABNORMAL ODORS OR SYSTEM FAULTS DURING INSPECTION. SUSPECT SEAT 4D VIDEO POWER SUPPLY FAULTY. REQUEST FURTHER INFORMATION FROM CREW. AIRCRAFT IN SAFE CONDITION FOR FLIGHT. (M) 2L72 4F RTT00001SE 20030825001542003082500154NM 2003 8 25 AMTA200300984 120030731A2613 OVERHEAT LOOP BOEING757 75733N 1384931NM RT ENGINE OUT OF ADJUST A AMTAK NONE J WARNING INDICATION CRCRUISE 1 GL11561TZ 33526 RIGHT ENGINE OVERHEAT LOOP 2 INOPERATIVE, STATUS MESSAGE. VERIFIED SECURITY OF ALL RELATED CONNECTORS. PERFORMED ADJ/TEST OF OVERHEAT SYSTEM. SYSTEM CHECKS NORMAL PER MM 26-11-00-05. (M) 2L72 4F RTA2NM 20030825001562003082500156EA 2003 8 25 ASOA03271 120030621A5260601R3198059 SUPPORT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 FLT 4571 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STAIR SUPPORT PANEL ASSEMLBY WAS FOUND TO BE BROKEN BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STAIR SUPPORT PANEL ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030825001582003082500158 2003 8 25 AMTA200300986 420030801A2565 SLIDE BOEING737 73783N 13844HINM DOOR UNSECURE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11307TZ 28653 FLT 645 - ESCAPE SLIDE PACK IS HANGING LOOSE IN DOOR. RESECURED VELCRO STRIPS TO SLIDE BACKING PAN PER M/M 25-66-01, OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030825001722003082500172WP 2003 8 25 DHL2003873594 120030704A5730 PLATE DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 N/R 1450.: RT. OUT WING OB EXTEND L/E LWR PLATING SHOWS CORR BTWN STA. XFS.710.000, XFS.722.500. PERFORMED MJR REPAIR IAW EODHL, ED-3445. RMD FASTENERS IAW SRM. REMOVED CORR IAW SRM. FOUND OUT OF LIMITS IAW SRM. TRIMMED OUT DAMAGED AREA IAW EODHL, ED-3445. PERFORMED NDT INSP IAW NDT SPM PART 6-10-01-001. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. FAB A REPAIR EXT DBLR , FILLER IAW EODHL-030606, ED-3445. CLEANED, TREATED, PRIMED REPAIR EXT DOUBLER INT SURFACE, FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTLD FILLER AND DBLR ON RT OUTER WING OB. EXTENDED L/E LWR PLATING USING NEW FASTENERS IAW EODHL-030606, ED-3445, SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. 2L74 4F RT4A25 20031001000302003100100030NE 2003 10 1 CALA0300520 220030909A7230 FAN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE SEIZED A CALAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 SW2714335 23573 721691 THE NR 2 ENGINE GAVE OFF A LOUD BANG FOLLOWED BY VIBRATION AND THE ENGINE SPOOLED DOWN TO IDLE. THE ENGINE NEVER DID SHUTDOWN. CREW WAS UNABLE TO GET POWER ABOVE IDLE. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ENGINE FAN SEIZED. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. INVESTIGATION REVEALED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO FAILURE OF NR 4 BEARING. 2L72 4F4 FRTA16WE E2GL 20031001000352003100100035WP 2003 10 1 UPS03841177 120030806A53473657504501 SEAT TRACK DOUG DC8 DC873F 302199FWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, OBSERVER SEAT TRACK FWD AND AFT IS CORRODED AT MOUNTING POINTS REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 51-3-0 2L74 4F RT4A25 20031001000392003100100039WP 2003 10 1 UPS03841182 120030807A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, MAIN CABIN LT SIDE AT STA 1140 FWD SIDE 4 INCH ABOVE CUSP FRAME HAS CORROSION. REMOVED CORROSION, AREA IS OUT OF LIMITS IAW DC8 SRM 53-2-0, FABRICATED REPAIR IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, AND INSTALLED REPAIR IAW DC8 SRM 51-1-21. REPLACED FITTING P/N 46 40162 PO 420224.3, LOCATED DRILLED AND DEBURRED FITTING IAW DC8 SRM 51-3-2 AND INSTALLED FITTING IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030926000832003092600083NM 2003 9 26 AWXA200301000 120030828A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28818AW 1375 FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030926001522003092600152NM 2003 9 26 AWXA200300971 120030821A71602607MK2 ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE NR 2 ENGINE MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28814AW8287 1281 ON TAKEOFF ROLL AT SMF EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306, OPERATIONAL AND LEAK CHECK WERE GOOD PER T/C F5M71312. FUEL LACQUER BUILDUP DEGRADED UNIT PERFORMANCE SUFFICIENTLY ENOUGH TO PLAY AN INSTRUMENTAL PART IN REPORTED FAILURE MESSAGE. 2L72 4F4 FRTA28NM E311NE 20030926001642003092600164NM 2003 9 26 CALA0300509 120030903A5410 ANGLE BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030929000162003092900016EA 2003 9 29 COMA0370028 120030901A5320 SEALANT CNDAIRCL600 CL6002C10 1390015EA DOOR AREA MISSING A COMABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01391CA336 10108 FLIGHT 5717 CABIN DOOR MAKING LOUD NOISE, FA AND PASSENGER SAID THEY SMELLED SOMETHING BURNING. COULD NOT DUPLICATE - FOUND VERY SMALL AREA OF DOOR FRAME THAT WAS MISSING SEALANT. FILLED HOLE WITH SEALANT. 2L72 4F RTA21EA 20030929000262003092900026NM 2003 9 29 03FDEA01417 120030901A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD BORE FOUND CORRODED. RHW O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD CORRODED BORE REPAIRED AS PER EA 1-5750-73297. 2L73 4F RTA22WE 20030929000382003092900038NM 2003 9 29 03FDEA01425 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RIGHT WING I/B FLAP VANE O/B TEE FITTING I/B AND O/B FACE FOUND WITH SURFACE CORROSION. SURFACE CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG I/B AND O/B FACE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490. 2L73 4F RTA22WE 20030929001192003092900119EU 2003 9 29 RAIA00309234 120030901A3697 WIRE AEROSPATR72 ATR72202 8680940EU NR 1 ENGINE BROKEN A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03723TE 283 BLEED FAULT NR 1 ENGINE. MAINTENANCE REPAIRED BROKEN WIRE AT CONNECTOR 404VC. 2H72 4T RTA53EU 20030930001062003093000106NM 2003 9 30 03FDEA01494 120030902A5753 HINGE DOUG MD11 MD11 3023602NM LEFT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG I/B SIDE SURFACE CORRODED. 2L73 4F RTA22WE 20030930001102003093000110NM 2003 9 30 03FDEA01490 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) ACTUATOR MOUNT O/B LUG CORRODED. 2L73 4F RTA22WE 20031001000072003100100007NM 2003 10 1 QXEA200301075 120030827A5347 CHANNEL DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 11 SEAT TRACK BOTTOM OF CHANNEL IS LIGHTLY CORRODED ALONG LT AND RT EDGES FORWARD OF STATION X510.0. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031001000512003100100051WP 2003 10 1 UPS03841197 120030816A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, CABIN SEAT TRACK CORRODED STA 822 RBL 48 REMOVED AND REPLACED SEAT TRACK IAW UPS EO DC8-5320-8309. MATERIAL VERIFICATION IS P/N 4755395-2400, NR 00633513, NR 00633514,NR 00633527, 00 633528, PO NR 0841577 2L74 4F RT4A25 20031001000532003100100053NM 2003 10 1 CALA0300568 120030929A3397 WIRE BOEING737 7373T0 1384582NM BATTERY PACK BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2717309 23360 INSPECTION FOUND EMERGENCY AISLE LIGHTS AT ROW S 12-20 INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT STA 378 EMERGENCY LIGHT BATTERY PACK. THE BROKEN WIRE WAS REPLACED IAW CHAPTER 20 STANDARD WIRING PRACTICES MANUAL AND WDM 33-50-00. 2L72 4F RTA16WE 20031001000602003100100060WP 2003 10 1 03FDEA00658 120030430A2612 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP CARGO BAY INOPERATIVE A FDEAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25392FE 46626 LOWER AFT CARGO FIRE INDICATION, BOTTLE DISCHARGED, LANDED TUL WITHOUT INCIDENT. 1L EMERGENCY SLIDE DEPLOYED. ACN RELEASED FOR SERVICE PER MEL/CDL: 26-17-01-02-B "MEL 26-17-01-02-B: ALL LWR CENTER/AFT CARGO COMPT SMOKE DETECTORS - INOP. CENTER/AFT CARGO COMPT MUST REMAIN EMPTY." ALSO SEE AMLS 26-20-5060 ,52-10-5059 , AND 26-20-5061. 01MAY03 MEM MX R/R'D NR 4 SMOKE DETECTOR WITH KNOWN GOOD UNIT. OPS OK I.A.W. AMM 26-14-01-5. 2L73 4F A22WE 20031001000632003100100063NM 2003 10 1 03FDEA00449 120030415A5312 BULKHEAD BOEING727 727200 138407ENM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 CRACK IN LEFT WHEEL WELL STATION 870 BULKHEAD SKIN WEB. ** S/D ** REPAIRED CRACK IAW FEDEX EA 7-5310-69465 2L73 4F RTA3WE 20031001000652003100100065NM 2003 10 1 2003UALA00703 120030920A3350 LIGHT BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29620UA 21880 EMERGENCY EXIT LIGHTS-FLOOR LIGHT DAMAGED DOOR 2R. FOUND EEL TRACK COVER OFF FWD OF DOOR 2R. SECURED COVER AND OPS CHECKED EMERGENCY LIGHTS. OPS CHECKED NORMAL. 2L72 4F4 FRTA1NM E3NE 20031001000712003100100071NM 2003 10 1 2003UALA00709 120030921A3232 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE MLG OOOR FAILED A UALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP29559UA 26657 RIGHT MAIN GEAR DOOR FOUND FULL OPEN UPON GATE ARRIVAL. FAILED MLG DOOR RETRACT ACTUATOR. ACTUATOR WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20031001000872003100100087SW 2003 10 1 2003F00585 120030607A2497 WIRE FRCHLDSA227 SA227DC 3377521SW GARRTTTPE331TPE33112UA 01514WP BLEED SWITCH BROKEN A BSAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM05453LA DC852B ON DESCENT TO THE STATION, HOT AIR AND SMOKE STARTED COMING OUT OF THE RIGHT BLEED, WITH THE RIGHT BLEED SHUTOFF AND DEFERRED. CREW FOLLOWED PROCEDURES AND LANDED AT THE NEXT STATION, WHICH WAS THE CLOSEST. THE FLOW CONTROL VALVE WAS RECEIVING AN UNCOMMANDED OPEN SIGNAL, THE ENVIRONMENTAL AIR DUCTING GOT HOT, WHICH CAUSED SMOKE. FOND INTERMITTENT FAILURE DUE TO BROKEN WIRE ON A DIODE ON THE BLEED SWITCH. THE DIODE WIRE HAD BROKEN AT THE CRIMP CONNECTOR, WHICH WOULD OPEN AND CLOSE THE CIRCUIT, CAUSING AN UNCOMMANDED BLEED VALVE OPENING. THE DEFERRED RIGHT ACM WAS ALSO REPLACED AT THIS TIME. (M) 2L72 4T4 TRTA18SW E4WE 20031001001002003100100100NM 2003 10 1 AMTA200301134 120030824A5415 ATTACH FITTING BOEING757 75733N 1384931NM NR 1 PYLON DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11555TZ 32589 NR 1 PYLON UPPER LINK ATTACH FITTING TO MID-BULKHEAD SHIMS MIGRATING. COMPLIED WITH ER/A 757-54R-5285. (M) 2L72 4F RTA2NM 20031001001062003100100106EA 2003 10 1 COMA0360440 120030929A261324403615 ELEMENT CNDAIRCL600 CL6002B19 1900309EA RT MLG FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01819CA 7415 FLIGHT 5444 MLG BAY OVERHEAT WARNING. REPLACED THE RT MLG OVERHEAT SENSE ELEMENT. 2L72 4F RTA21EA 20031001001162003100100116NM 2003 10 1 USAA030185 120030908A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US49351 23556 FOUND SKIN CRACKED .750 INCH, FUSELAGE SKIN FS 727D AT S23R. INSTALLED DOUBLER PER EA 94676. (M) 2L72 4F RTA16WE 20031001001192003100100119NM 2003 10 1 USAA030182 120030820A5311 FRAME BOEING737 737401 1384701NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US40788 23984 PIT - FOUND FRAME WITH FOUR GOUGES .25 INCH BY .5 INCH .019 DEEP, FRAME AT STATION 294.5 BETWEEN STRINGER 4L AND 3L AT SPLICE. REMOVED SPLICE DOUBLERS AND CUTOUT DAMAGE. INSTALLED FILLER AND REPAIR DOUBLERS PER SRM 53-00-07. (M) 2L72 4F RTA16WE 20031001001272003100100127NM 2003 10 1 QXEA200301085 120030827A5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 AFT FLOOR SUPPORT FOR PANEL 144AZ TOP SIDE IS CORRODED AT STATION Y21L. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16 AND 51-20-36. 2H72 4T RTA13NM 20031001001292003100100129WP 2003 10 1 UPS03841200 120030827A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, STATION 1240 LONG. 30R IS CRACKED REMOVED LONGERON SECTION STATION 1230-1250,FABRICATED AND INSTALLED REPLACEMENT SECTION I.A.W. SRM. 53-4-1 FIG.4,53-2-2 FIG. 10. 2L74 4F RT4A25 20031001001312003100100131NE 2003 10 1 UIEA200300055 220030911A7200 ENGINE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 1 STALLED A UIEAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA15508MC 21644 517510 DOV/RMS DIVERSION TO JFK, IN CRUISE AT FL350 NR 1 ENGINE BEGAN TO SHUDDER/STALL WITH DROP OF N1 ONLY. PULLED THRUST LEVER BACK. IT THEN DID IT AGAIN AND CONTINUED TO DO IT. SHUT DOWN ENGINE IAW QRH. DIVERTED TO JFK. NO FUEL DUMPED. REMOVED AND REPLACED NR 1 ENGINE PER ATLAS AIR TASK CARD 01-AA-45. ACCOMPLISHED GROUND RUN UP TESTES 3, 4 AND 8 PER MM 71-00-00. OPS AND LEAK CHECK NORMAL. NO DEFECTS NOTED. CLOSED AND SECURED ALL PANELS, COWLINGS AND FAIRINGS. ENGINE S/N ON 517265. (M) 2L74 4F4 F A20WE E23EA 20031002000032003100200003WP 2003 10 2 GTIA030682 120030909A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FLIGHT COMPARTMENT STATION 120-160 RIGHT SIDE FLOOR PANEL HAS CRACK/DAMAGED. REPAIRED CRACK AND DAMAGE ON FLOOR PANEL. (M) 2L72 4F A6WE 20031002000142003100200014WP 2003 10 2 AMTA200301097 120030827A5210 MECHANISM LKHEED1011 10113853 5265020WP DOOR ELECTRICAL INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 R1 DOOR INOPERATIVE ELECTRICALLY. (M) 2L73 4F A23WE 20031002000202003100200020EA 2003 10 2 A6WA200340136 120030911A2612 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA FIRE DETECTOR INTERMITTENT A A6WAO OTHER N FALSE WARNING CRCRUISE 1 GL31448AW 7814 INTERMITTENT RT ENGINE FIRE FAIL CAS INDICATION INFLIGHT AT ONE TIME FOR 3 SECONDS ENGINE FIRE CAS MESSAGE. REMOVED AND REPLACED FIRE DETECTION CONTROLLER. (M) 2L72 4F RTA21EA 20031002000222003100200022EU 2003 10 2 A6WA200360036 120030906A5311 FRAME BAC 146 146200A 1500266EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 FOUND CORROSION ON FRAME 18 MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060003. (M) 2H74 4F A49EU 20031002000322003100200032EU 2003 10 2 A6WA200360037 120030908A5310 DOOR FRAME BAC 146 146200A 1500266EU FUSELAGE GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 AFT CARGO DOOR OUTSIDE DOOR SURROUND GOUGED AT TOP AFT RADIUS MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060004. (M) 2H74 4F A49EU 20031002000432003100200043NM 2003 10 2 USAA030177 120030827A5553 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US40788 23984 FOUND FITTING WITH CORROSION AND PITTING .5 INCH, 5-7 O'CLOCK, VERT STAB AFT OUTBOARD LUG FORWARD CLEVIS BETWEEN CLEVIS AND T-FITTING. REMOVED AND REPLACED BUSHING/OVERSIZE PER EA 76801. CORROSION LEVEL 1, TASK NR C55-706-11. (M) 2L72 4F RTA16WE 20030929000472003092900047NM 2003 9 29 03FDEA01407 120030903A5410 STIFFENER BOEING727 727200 138407ENM LT NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 AFT STIFFNER IS CHAFED AT NR 6 LT NACELLE, ATTACH POSITION ABOVE NR 2 ENGINE BS 1456. REMOVED AFT STIFFENER, FABRICATED, DRILLED, ALODINED, PRIMED AND RE-INSTALLED RIBS AND STIFFENER AT BS 1456 AND 1459 AT NR 6 LT COWL ATTACH POSITION ABOVE NR 2 ENGINE. 2L73 4F RTA3WE 20030929000612003092900061 2003 9 29 GLBA2003126 420030827A2397 WIRE BEECH 1900 1900D 1154162CE CAPT PHONE JACK BROKEN A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03201GL UE201 CABIN SIDE HEADSET GETS A LOT OF STATIC AND CUTS IN AND OUT, REPAIRED WIRING UNDER ENTRY FLOORBOARD BETWEEN CAPT'S PHONE JACK TO OBSERVE, PHONE JACK. OPS CK GOOD. 2L72 4T RTA24CE 20030929000632003092900063 2003 9 29 251TR0004 420030806A221065C370537 PCU BOEING737 737228 13844AGNM RUDDER MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 YAW DAMPER WILL NOT COUPLE. REPLACED RUDDER PCU PER MM 27-21-91. OPS CHECKS OK PER MM 27-21-91. 2L72 4F RTA16WE 20030929001042003092900104NM 2003 9 29 AWXA200301019 120030815A575469619221 FRAME BOEING737 737277 1384570NM LT WING LE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1.75 INCH CRACK WAS FOUND ON LT WING LEADING EDGE FORMER AT WS 222.7, JUST INBOARD OF NR 1 PYLON. MAINTENANCE CUT OUT DAMAGE ON LT WING LEADING EDGE FORMER AT WS 222.7 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-40-03 FIG 1 PG 1-6. 2L72 4F RTA16WE 20030929001332003092900133NE 2003 9 29 GLBA2003127 320030901A6140 TACH GENERATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA HARTZLHCE4A HCE4A3A NE NR 1 PROPELLER MALFUNCTIONED A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM0396UX UE96 NR 1 PROP RPM 1450 IDLE AT 600, TIGHTENED NR 1 N2 TACH GEN. 2L72 4T3 TRTA24CE E2NE 5 CP10NE 20030930000332003093000033NM 2003 9 30 2003UALA00630 120030816A3260806002 SQUAT SWITCH BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG FAILED A UALABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29364UA 24533 MULTIPLE SYSTEM FAILURES IN FLIGHT, LOSS OF CABIN PRESSURE. PASSENGER OXYGEN MASKS DEPLOYED. GROUND SENSING SQUAT SWITCH M990 FAILED. REPLACED M990 AND PERFORMED OPERATIONAL CHECK OF ALL FAILED SYSTEMS. COULD NOT DUPLICATE IN GROUND OR FLIGHT MODE. 2L72 4F4 FRTA16WE E2GL 20030930000412003093000041NM 2003 9 30 2003UALA00660 120030830A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 CABIN FLOORBEAM CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FLOOR BEAM UPPER 'T' CAP. 2L72 4F4 FRTA16WE E2GL 20031001000112003100100011NM 2003 10 1 QXEA200301079 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 10 SEAT TRACK HAS A PIT OF CORROISON .25 INCH IN CENTER OF CHANNEL FOUR INCHES FORWARD OF STATION X370. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-1342. 2H72 4T RTA13NM 20031001000662003100100066NE 2003 10 1 2003UALA00704 220030919A7261MS21902J4 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29395UA 24670 LANDED OKC UNDER AMBER ALERT DUE TO NR 2 ENGINE LOW OIL QUANTITY INDICATION. FOUND ENGINE OIL PRESSURE TUBE UNION FITTING AT TRANSFER GEARBOX CRACKED. REPLACED UNION FITTING . ELBOW/UNION FITTINGS AND BRACKETS ON THE ENGINE LEFT SIDE BETWEEN THE TRANSFER GEARBOX HOUSING AND OIL PRESSURE TRANSMITTER, MAY BE DAMAGED IF THE SHIPPING STAND ENGINE SUPPORT SHAFT, DROPS ONTO THE TUBING DURING ENGINE CHANGE. 2L72 4F4 FRTA16WE E2GL 20031002000522003100200052WP 2003 10 2 UPS03841208 120030827A53403750330527 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, LONG. 32L SPLICE FITTING IS CRACKED AT STA. 610. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG. 3750330,AND SRM. 51-1-20D. 2L74 4F RT4A25 20031002000572003100200057WP 2003 10 2 UPS03841215 120030827A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, LONGERON 28R IS CORRODED BEYOND LIMITS AT SPLICE FITTING AT STA. 450. REMOVED,FABRICATED AND REPLACED LONGERON SECTIONS BETWEEN STA.430 AND 470,AND REPLACED LONGERON SPLICES I.A.W. SRM. 53-2-2 FIG.8. 2L74 4F RT4A25 20031002000622003100200062NM 2003 10 2 QXEA200301088 120030831A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 FIREWALL HAS A CRACK ALONG INBOARD SIDE OF EXHAUST APERTURE UNDER INBOARD CLIP. REPAIRED IAW HORIZON AIR EA 2-54-180. 2H72 4T RTA13NM 20031002000752003100200075SO 2003 10 2 C2XA03TY152 120030910A321014571035409 CAP EMB 135 EMB135ER 3260203SO LEFT MLG CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE LT MLG BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031002000782003100200078 2003 10 2 250TR0023 420030910A22114038891916 COMPUTER BOEING737 7372K5 138448XNM FLT CNTRL INOPERATIVE A PIDAO OTHER J WARNING INDICATION CRCRUISE 1 SO05250TR 22597 FIRST OFFICER'S FLIGHT DIRECTOR FLAG IN VIEW DURING FLIGHT. REPLACED NR 1 AND NR 2 FLIGHT CONTROL COMPUTER IAW MM 22-11-331. 2L72 4F RTA16WE 20031002000792003100200079EU 2003 10 2 XNOA01152 120030905A2711 SERVO AIRBUS300 A300B4203 3930306EU FLT CONTROL LEAKING A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23474AS 219 LOST BLUE HYD QTY ON TAXI OUT. REMOVED AND REPLACED BLUE HYD FILTER AND HOUSING BLUE FLIGHT CONTROL SERVO SYS. LEAK AND OPS CHECK GOOD IAW A300 MM 27-14-00. 2L72 4F RTA35EU 20031002000842003100200084NM 2003 10 2 CALA0300522 120030910A5320 STRAP BOEING777 777224 1385225NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778013 29861 INSPECTION FOUND A .1875 INCH CRACK AT FASTENER HOLE IN LT SIDE AFT LOWER LONGERON STRAP AT BS 2273, LBL 64, WL 217. THE LONGERON STRAP WAS LOCATED AT LT HORIZONTAL STABILIZER LOWER SEAL FAIRING. THE LONGERON STRAP WAS REPAIRED IAW ECRA 5310-04370. 2L72 4F RTT00001SE 20031002000962003100200096NM 2003 10 2 C1HA200386012 120030909A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 CORROSION ON SEAT TRACK BS 1130 LBL 25. 2L73 4F A3WE 20031002001052003100200105EU 2003 10 2 00110 120030909A2130 LINE AMD FALC20FALCONE 2720305EU CABIN PRESSURE BROKEN E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05285TW 285 PILOT REPORTED CABIN ALTITUDE INDICATING HIGH, CYCLED PRESSURIZATION VALVES, RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE, REPAIRED BROKEN PRESSURIZATION LINE IAW / FALCON MM. RETURN AIRCRAFT TO SERVICE. 2L72 4F A7EU 20031002001062003100200106SO 2003 10 2 C2XA03CL162 120030910A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711565 145621 CLE FLIGHT 2058 THE CREW REPORTED 2 EMERGENCY AISLE PATH LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20031002001172003100200117NM 2003 10 2 QXEA200301101 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 5 SEAT TRACK HAS LIGHT CHAFING DAMAGE FROM SEAT PEG MOVEMENT ON Z LUGS IN BOTTOM OF CHANNEL RIGHT SIDE AFT OF STATION X445. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-467. 2H72 4T RTA13NM 20031002001182003100200118NM 2003 10 2 QXEA200301102 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 6 SEAT TRACK CENTER CHANNEL BOTTOM HAS A CHAFED AREA WITH LIGHT PITTING FOUR INCHES FROM AFT END. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1339. 2H72 4T RTA13NM 20031002001202003100200120NM 2003 10 2 QXEA200301104 120030826A5320 PAN DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CARGO COMPARTMENT FLOOR PAN IS CORRODED ON BOTTOM SIDE AROUND FORWARD ROW OF NUTPLATES FOR PANEL 144HZ. REPAIRED IAW DHC-8 SRM 51-20-16, 53-00-16, 51-20-36, 51-40-11, 51-40-00 AND 51-20-51. 2H72 4T RTA13NM 20031002001242003100200124NM 2003 10 2 QXEA200301108 120030826A5512 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 EMPENNAGE LEFT HAND SIDE UPPER SKIN IS AN ABRASION ONE INCH LONG FORWARD OF FRAME NR 1 OUTBOARD OF STRINGER 5. REPAIRED IAW DHC-8 SRM 51-20-16. 2H72 4T RTA13NM 20031002001262003100200126EU 2003 10 2 AWXA200301037 120030910A3350321430 BATTERY AIRBUS320 A320231 3930325EU GE CFM56 CFM56* 13802NE ZONE 242 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING INSPECTION THE RT OVER WING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E2GL 20031002001322003100200132CE 2003 10 2 ACE091103 120030911A2822 PUMP BEECH 1900 1900C 1154161CE PWA PT6 PT6A60 52043NE FUEL SYSTEM LEAKING E YADAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 AL03114AX1246 UC36 PILOT NOTICED FUEL LEAKING FROM ENGINE DRAIN ON PRE-FLIGHT. MAINTENANCE REPLACED THE DEFECTIVE PUMP. 2L72 4T4 TRTA24CE E4EA 20031002001332003100200133NM 2003 10 2 PCAA0309108 120030910A33506104789 BATTERY PACK DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EMERGENCY LIGHT DEFECTIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13815EX 321 DURING ROUTINE MAINTENANCE VISIT LEFT FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. AFTER TROUBLESHOOTING SYSTEM IT WAS DISCOVERED THAT THE EMERGERGENCY LIGHT BATTERY IN POSITION 100 WAS DEFECTIVE. EMERGENCY LIGHT BATTERY WAS REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031002001342003100200134NM 2003 10 2 G6OA 120030911A3210ANB720321M BRACKET DOUG MD11 MD11F 3023600NM MLG BROKEN A G6OAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 EA27703GC 48411 LEFT MAIN LANDING GEAR UPLOCK INDICATION BOTH SYNOPTIC AND GEAR LIGHTS SHOWED UNSAFE. 2L73 4F RTA22WE 20030930000812003093000081WP 2003 9 30 ABXA030354 120030818A532099100785 STRUCTURE DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 LEVEL II CORROSION ON SUBFLOOR AT RIGHT BUTT LINE 44 F.S. 180 SHACKLE BOX. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20031001000082003100100008NM 2003 10 1 QXEA200301076 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR11 SEAT TRACK BOTTOM OF CHANNEL IS CORRODED ONE INCH FORWARD OF STATION X488. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031001000342003100100034WP 2003 10 1 UPS03841176 120030807A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, STA 25 S21L CUSP CRACKED APPROX. 3 INCHES IN LENGTH. FABRICATED NEW CUSP WEB, MATERIAL ID .063 2024-T3, PO 415380.3, ALODIINED, PRIMED, INSTALLED NEW CUSP CHORD WEB AND PARTS REMVOED TO FOM IAW DAC DWG 5597646, DC8 SRM 51-1-8, 51-1-21, 51-3-0, 51-1-24A, AND 51-1-20D. 2L74 4F RT4A25 20031002000022003100200002NM 2003 10 2 GTIA030676 120030915A2170 COALESCER BAG DOUG MD80 MD83 3023681NM AIR CONDITIONINGODOR A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23822NK 49392 CABIN AIR SMELLS LIKE BURNT OIL WHEN MIX VALVES MOVE TOWARD MID RANGE WARM OR HOT. REMOVED AND REPLACED AIR CONTIONING COALESCER BAGS. INSPECTED ACM OIL LEVEL CK GOOD. RAN PACKS, NO ABNORMAL ODORS NOTD, OK FOR SERVICE. (M) 2L72 4F RT 20031002000192003100200019SW 2003 10 2 2003F00591 120030525A2400ANL225 CURRENT LIMITER FRCHLDSA227 SA227DC 3377521SW COCKPIT FAILED A BSAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM05850LS DC850B FLT 6016 - BOI - DURING CLIMB-OUT, THE CREW COULD NOTICED A BURNING ODOR. THE CO-PILOT SAW SMOKE COMING FROM THE ELECTRICAL BOX LOCATED BEHIND THE CAPTAINS SEAT. THE CREW FOLLOWED EMERGENCY PROCEDURES AND RETURNED TO STATION WTH NO FURTHER INCIDENT. FAILED CURRENT LIMITER. REPLACD LEFT ESS BUSS CURRENT LIMITER, SYSTEM OPS CHECK GOOD. (M) 2L72 4T RTA18SW 20031002000412003100200041 2003 10 2 UIEA200300054 420030901A25657A1323111 SLIDE BOEING747 747300 GL CABIN MISINSTALLED A UIEAK NONE O OTHER ININSP/MAINT 1 EA1524837 24837 DURING FC02 CHECK AT AMS, AN INSPECTION OF LEFT U/D TYPE 'A' DOOR THE TECHICIAN NOTICED THAT THE SLIDE DEPLOYMENT HOOK WOULD NOT ENGATE THE SLIDE DEPLOYMENT LINK. THE FIRST OBSERVATION WAS THAT THE SLIDE OUTER COVER (INBOARD SIDE) WAS NOT FLUSH WITH THE DOOR THRESHOLD. NON-ROUTINE 02UM5001 WAS RAISED. UPON REVIEW OF THE MM FOR SLIDE INSTALLATION (25-68-07) IT IS BELIEVED THAT THE LAST INSTALLATION WAS ACCOMPLISHED IN CORRECTLY. SLIDE AND PLATFORM ASSEMBLY WAS REMOVED AND CHECKED. SLIDE WAS SENT TO THE SHOP FOR EVALUATION. THE PLATFORM ASSEMBLY WAS REINSTALLED AND A NEW SLIDE INSTALLED. THERE WERE NO ABNORMAL FINDING ON THE SLIDE IN THE SHOP. SLIDE REMOVED. (M) 2L74 4F RTA20WE 20031002001382003100200138EU 2003 10 2 YENA200323 120030907A2120 SMOKE AIRBUS320 A320232 3930326EU COCKPIT DETECTED A YENAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 EA15566JB 2042 DURING CRUISE AT FL 350 SMOKE WAS NOTICED IN FLT DECK FROM CENTER CONSOLE, EMERGENCY PROCEDURE PERFORMED, SMOKE WAS EVACUATED. NO OTHER SMOKE WAS NOTED. RETURNED TO JFK. EXTENSIVE TROUBLESHOOTING FAILED TO PINPOINT THE SOURCE OF THE SMOKE. ALL TESTS AND GROUND POWER RUN WAS NORMAL. TEST FLIGHT WAS CONDUCTED AND NO DISCREPANY WAS NOTED. MULTIPLE COMPONETS (2 RMPS, 3 ACPS, 1 LAPTOP STATIC INVERTER, COCKPIT SEB FOR CSS)WERE REPLACED AS A PRECAUTION. AIRCRAFT RELEASED FOR FLIGHT WITH FAA AND MAINTENACE PERSONNEL ON BOARD FOR FURTHER OBSERVANCE. NO DISCREPANCIES NOTED. 2L72 4F RTA28NM 20031002001402003100200140NM 2003 10 2 CALA0300524 120030912A3350B21506 FUSE BOEING737 737524 1384721NM POWER SUPPLY BLOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2762631 27535 INSPECTION FOUND EMERGENCY LIGHTING ON FIRST CLASS SEATS INOPERATIVE. REPLACED PICOFUSES IN POWER SUPPLY FOR LIGHT. 2L72 4F RTA16WE 20031002001452003100200145NM 2003 10 2 F3LA200300131 120030912A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOORBEAM CAP STRIP FROM LT TO RT SIDE OF AIRCRAFT AT STA. 986.5. REMOVED DAMAGED SECTION OF FLOOR SUPPORT BEAM AND REPAIRED IAW SRM 53-00-51, FIG. 202. 2L72 4F RTA16WE 20031002001502003100200150NM 2003 10 2 03FDEA01472 120030909A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 DENT ON SKIN BS 359 BETWEEN STR 19-20 LT. REPAIR PER ER 03-3244 AND EA 7-5330-72319. 2L73 4F RTA3WE 20031002001612003100200161SO 2003 10 2 SWIA200312381 120030906A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07187SW6557 4938 120037 ON APPROACH INTO SLC WE SELECTED FLAPS 15 AND GOT THE ''CONTROL FAULT'' WITH THE ''FLAP'' AND ''ADVANCED SWS'' ON THE MAP. QRH PROCEDURE CORRECTED PROBLEM.REMOVED AND REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031002001742003100200174NM 2003 10 2 252TR0011 120030912A33501000679 LIGHT BOEING737 737228 13844AGNM CABIN INOPERATIVE A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05252TR 23001 RT AFT SERVICE DOOR EMERGENCY EXIT LIGHT DOES NOT HOLD CHARGE. REPLACED EMERGENCY EXIT LIGHT AT RT AFT SERVICE DOOR POSITION. OPS CHECKS OK. 2L72 4F RTA16WE 20030905001962003090500196NM 2003 9 5 USAA030149 120030724A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US40465 23988 CLT - FOUND SKIN CRACKED .5 INCH, FS 500C BELOW S26L. FABRICATED REPAIR PARTS PER EA 94532. (M) 2L72 4F RTA16WE 20030905001982003090500198NE 2003 9 5 AALA20030611 220030526A7510 DUCT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT ENGINE DAMAGED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21207AA 49158 LAX - FLT 1716 - EN ROUTE LAX-AUS, INTERMITTENT FIRE WARNING OF LEFT ENGINE AFTER TAKEOFF WITH LEFT ENGINE IN LOOP A ONLY. RETURNED LAX AND LANDED WITHOUT INCIDENT. CHECK OF LEFT ENGINE FIRE DETECTION LOOP A WORKS NORMAL. REPLACED LEFT ENGIEN RIGHT IGV ANTI-ICE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030905002232003090500223SO 2003 9 5 C2XA03BT085 120030827A3350110049 POWER SUPPLY EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2714925 145004 EWR LOG BOOK SQUAWK AISLE PATH LIGHTING STRIPS SEGMENTS 2 AND 3 INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY POWER SUPPLY IAW EMB145 MM 33-50-04. OPS CHECK GOOD. 2L72 4F RTT00011AT 20030908001552003090800155EA 2003 9 8 SWIA200312230 120030801A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07405SW 7029 FLIGHT SPOILER FAULT MESSAGE DURING TAXI. RESET BREAKERS, FAULT DID NOT CLEAR. REMOVED AND REPLACED RIGHT OUTBOARD FLIGHT SPOILER PCU. OPS CHECK GOOD IAW 27-62-01. SN OFF: MAL 0278 2L72 4F RTA21EA 20030908001732003090800173EA 2003 9 8 SWIA200312243 120030805A2761270007 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA SPOILER FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07438SW 7574 SPOILERON FAULT RIGHT SIDE WHITE MESSAGE WON'T EXTINGUISH.REMOVED AND REPLACED RIGHT INBOARD SPOILERON ACTUATOR PER CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. S/N OFF: 4775 2L72 4F RTA21EA 20030908001912003090800191EA 2003 9 8 SWIA200312268 120030814A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM07587SW 7062 A STRONG BURNING SMELL OCCURRED IN COCKPIT (ELECTRICAL), LASTED FOR APPROX 2 MINS. INSPECTED AFT EQUIPMENT BAY, CARGO BAY AND COCKPIT FOR ANY SIGNS OF SOURCE. OPERATED LT & RT PACKS IAW MM 21-00-00 AT MULTIPLE TEMPERATURES FOR ANY SMOKE. NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20030905001062003090500106NM 2003 9 5 DL777030632 120030712A3620S210W1101124 SENSOR BOEING777 777232 1385232NM BLEED AIR SYS FAULTY A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27877DA 29739 CREW REPORTS BLEED OFF ENG L MESSAGE RESET AND TRIPPED AGAIN APPROX 40 MINUTES LATER. A/C RETURNING TO ATL FOUND MAINT MESSAGE 36-10500. MANIFOLD DUAL TEMP SENSOR LEFT FAILED. REPLACED SAME PER M/M. RAN ENGINE TO POWER AND ALS PERFORMED ENGINE BLEED AIR OPERATIONAL TEST PER M/M. NO MESSAGES. OPS CK GOOD. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK. 2L72 4F RTT00001SE 20030908001802003090800180EA 2003 9 8 SWIA200312253 120030807A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB DIRTY A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07448SW 7678 (STAB TRIM) AND (MACH TRIM) CAUTION MESSAGES ILLUMINATED. COULD NOT CORRECT/RE-ENGAGE TRIM SYSTEMS. RETURN TO FIELD. CYCLED CB'S 3A5, 4A1, 2F5, 2B8. CLEANED SWITCHES (DISCONNECT), CLEARED HSTCU OF FAULTS. OPS CHECKS GOOD AT THIS TIME. 2L72 4F RTA21EA 20030908002102003090800210 2003 9 8 SWIA200312296 420030819A2210 SWITCH EMB 120 EMB120ER 3260203SO AUTOPILOT SYS DEFECTIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07579SW 120347 AUTOPILOT WILL NOT TEST. AMBER 'R' ON PEDISTAL PANEL. REPLACED FIRST OFFICER'S AP DISCONNECT SWITCH AS REQUIRED. SYSTEM OPS CHECK GOOD IAW 22-10-00. 2L72 4T RTA31SO 20030908002422003090800242NE 2003 9 8 MALA030355 220030728A7200 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 GL15535XJ E2371 DURING FLIGHT NR 3527, NR 2 ENGINE LOW OIL PRESSURE LIGHT. NR 2 ENGINE SHUTDOWN. OIL QUANTITY READ ZERO. OIL PRESSURE 40 PSI, AT 80 PERCENT N2, OIL TEMP 160 C. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE PN 2-003-040-015, SN/OFF PO7894, SN/ON P07665 IAW MAL 7100-502. REFER JOB CARDS FOR DETAILS. 2H74 4F4 FRTA49EU E6NE 20030908002432003090800243 2003 9 8 SWIA200312350 420030823A2210DL2233M11 DAMPENER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07587SW 7062 YAW DAMPNER NR 1 FAILED ON PUSHBACK/WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPNER WITH A SERVICEABLE UNIT IAW CL600 AMM 22-22-01. OPS CHECK GOOD. S/N OFF: 2762. 2L72 4F4 FRTA21EA E15NE 20030908002442003090800244EA 2003 9 8 SWIA200312351 120030828A2750854D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07587SW 7062 FLAPS FAIL CAUTION MSG ON APPROACH WHEN SELECTED FROM 30 TO 45 DEGREES. FLAPS FAILED RIGHT AT 30 INDICATED BOTH SIDES. REMOVED AND REPLACED LEFT BPSU WITH SERVICEABLE UNIT IAW MM 27-51-10. OPS CHECKS GOOD. S/N OFF: 1577B. 2L72 4F RTA21EA 20030908002572003090800257CE 2003 9 8 AMWA22 120030818A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07178YV UE178 WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20030908002772003090800277EA 2003 9 8 SWIA200312375 120030902A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07912SW 7595 INFLIGHT STAB AND MACH TRIM CAUTION. REPLACED F/O'S STAB TRIM DISCONNECT SWITCH IAW CRJ MM 27-00-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20030908002822003090800282CE 2003 9 8 AMWA29 120030818A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV UE163 WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20030908003022003090800302NM 2003 9 8 SWAA031921 120030827A53106558280 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED, BS 360, BETWEEN STRINGERS 13R AND 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030908003072003090800307NM 2003 9 8 SWAA031885 120030822A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) STR 25L, BS 775 AND BS 895. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030908003092003090800309NM 2003 9 8 SWAA031887 120030822A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED RON, FOUND EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030825001762003082500176NM 2003 8 25 03FDEA01189 120030727A5744ARC050312 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 SNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. CORRECTIVE ACTION: SNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS IAW EA 1-5750-71806, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030821002892003082100289EU 2003 8 21 YENA200313 120030710A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A YENAK NONE L NO TEST TXTAXI/GRND HDL 1 EA15565JB186 2031 AFT EMERGENCY EXIT LIGHTS AT L2 R2 AND OVERHEAD POSITIONS INOP. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT. OPS CHECK IAW 33-51-00 OK. 2L72 4F RTA28NM 20030822000302003082200030NM 2003 8 22 03FDEA01042 120030704A5514NLC6725 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT HORIZONTAL STABILIZER NR 4 BORE CORROSION EXCEEDED LIMIT AFTER REWORKED. CORROSION ON LEFT HORIZONTAL STABILIZER NR 4 BORE REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-69395, TITLE: STABILIZERS- HORIZONTAL STABILIZER BARREL NUT BORES- CORROSION REMOVAL- BORE 4 LEFT. 2L73 4F RTA22WE 20030730000362003073000036WP 2003 7 30 ABXA030276 120030224A5711 SPAR DOUG DC8 DC863F 302198FWP RT WING DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 RIGHT FORWARD LOWER SPAR HAD EXISTING CUTOUT THAT EXCEEDED THE LIMITS OF THE SERVICE REWORK DRAWING SR-8570012. FABRICATED FILLER IAW ABX REA D857-46655MR. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-21. 2L74 4F 4A25 20030730000562003073000056WP 2003 7 30 ABXA030308 120030722A3230 SPRING DOUG DC8 DC863 302198AWP LT MLG WORN A ABXAO OTHER J WARNING INDICATION CRCRUISE 1 GL23811AX 46113 THE GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY ACCOMPANIED WITH LEFT DOOR NOT LATCHED LIGHT AT FLIGHT ENGINEER'S PANEL. PERFORMED ABNORMAL CHECK, UNSAFE LIGHT WOULD NOT REMAIN ILLUMINATED LONG ENOUGHT TO DETERMINE WHICH SWITCH MAY BE MALFUNCTIONING. REPLACED DOOR CONTROL VALVE SPRING. INSPECTED UPLATCH AREA, NO DEFECTS FOUND. INDICATION SYSTEM OPS CHECKED GOOD IAW DC8 MM 32-30-00-2. 2L74 4F 4A25 20030730000592003073000059WP 2003 7 30 ABXA030303 120030618A522059131951 PAN DOUG DC9 DC941 302207NWP EMERGENCY EXIT DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 RIGHT AFT EMERGENCY OVERWING DOOR HAD FIBERGLASS REPAIR ON DOOR PAN UPPER FORWARD CORNER OF DOOR. REPAIRED AREA IAW DC-9 SRM 52-51 AND SSRM K07390. 2L72 4F A6WE 20030725000022003072500002NE 2003 7 25 DL76G030581 220030624A7200CF680C2B6F ENGINE BOEING767 767324 1385203NM GE CF6 CF680C2B6F 30025NE NR 2 FAILED A DALAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO27394DL123828141 27394 704234 ON TAKEOFF ROLL, ABORTED AT 100 KTS DUE TO NR 2 ENG FAILURE. FLAMES REPORTED COMING FROM THE FRONT AND REAR OF THE ENG. ENG EXPERIENCED A COMPRESSOR STALL. ENGINE CHANGE IN WORK IN BOM. 2L72 4F4 FRTA1NM E13NE 20030725000132003072500013NM 2003 7 25 DL76L030587 120030620A2780 CONTROL UNIT BOEING767 767332 1382001NM SLATS MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27197DN 28454 LEADING EDGE SLAT ASSY EICAS ON SLAT RETRACTION. AIR RETURN TO ATL. REPLACED S301 PER M/M. ACFT RETURNED TO ETOPS STATUS AFTER VERIFICATION FLIGHT. L/E SLATS OPERATED NORMAL. 2L72 4F RTA1NM 20030728000522003072800052NM 2003 7 28 SWAA031609 120030721A55106551524 FITTING BOEING737 7373A4 1384585NM HORIZ STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB HINGE FITTING LOWER AND UPPER LUGS CORRODED. REPAIRED LUGS PER SRM. 2L72 4F RTA16WE 20030728000852003072800085 2003 7 28 SWAA031639 420030723A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030729000082003072900008EA 2003 7 29 03203626 120030722A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27626BR 7225 DURING MAINTENANCE INSPECTION, MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LAMPS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE, 2 EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. 2L72 4F RTA21EA 20030729000362003072900036NM 2003 7 29 03194428 120030713A3350 LIGHT DORNERDO32 DO328300 NM CABIN INTERMITTENT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27428FJ 3193 DURING MAINTENANCE INPSECTION PERSONNEL DISCOVERED THE THE FWD EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND COULD NOT DUPLICATE THE FAULT. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030729000982003072900098EU 2003 7 29 2003F00478 120030515A7830 DUCT AIRBUS320 A320233 3930329EU THRUST REVERSER DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 2 ENGINE RIGHT THRUST REVERSER COWLING OUTER SIDING C-DUCT DELAMINATED. REPAIRED DAMAGE IAW SRM V2500, PAGE 201-206, FIGURE 201. (M) 2L72 4F RTA28NM 20030729001042003072900104NM 2003 7 29 USAA030096 120030430A5311 BELTFRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND BELTFRAME CRACKED .75 INCH LONG, AT RIVET FOR LOWER OVERHEAD BIN, BETWEEN S8L AND S9L, FS 440. PER TYPICAL REPAIR PER 53-10-20A. (M) 2L72 4F RTA16WE 20030729001442003072900144WP 2003 7 29 ABXA030292 120030624A274059109625 JACKSCREW DOUG DC9 DC932 3022066WP HORIZ STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 HORIZONTAL STABILIZER JACKSCREW HAD 4 EA PITTED THREADS. REPLACED JACKSCREW IAW DC-9 MM 27-40-01-4-0001. 2L72 4F A6WE 20030730000402003073000040WP 2003 7 30 ABXA030286 120030707A5610 WINDOW DOUG DC9 DC941 302207NWP COCKPIT UNSECURE A ABXAI CABIN DEPRESSURIZATION O OTHER CRCRUISE 1 GL23969AX 47464 EN ROUTE, CREW REPORTED LOUD AIR NOISE IN COCKPIT. NOISE WAS SO LOUD CREW COULD NOT HEAR. DESCENDED TO 10K AND CONTINUED UNPRESSURIZED. RESECURED AND RESEALED CAPTAIN'S EYEBROW WINDOW IAW DC-9 AMM. PRESSURIZED TO 4 PSID AND NO LEAKS NOTED. 2L72 4F A6WE 20030730000682003073000068WP 2003 7 30 ABXA030259 120030312A5200 DOOR FRAME DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 UPPER LATCH HOOK MOUNT HOLE AT STA 163.5 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR. 2L74 4F 4A25 20030730000692003073000069WP 2003 7 30 ABXA030270 120030315A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 233.5. CUT AND REMOVED DOOR FRAME, AND SPLICED IN NEW SECTION IAW ABX REA D852-46041MR AND DC-8 SRM 51-1-20D. 2L74 4F 4A25 20030730000852003073000085WP 2003 7 30 ABXA030300 120030625A531159135961 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 FRAME 1059 CRACKED AT LONGERON 16 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030730000872003073000087WP 2003 7 30 ABXA030306 120030619A541559132626 ATTACH ANGLE DOUG DC9 DC941 302207NWP RT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 RIGHT PYLON LEADING EDGE INBOARD ATTACH MOUNT HAD CRACKED REPAIR ANGLES. REMOVED, FABRICATED NEW ANGLE AND INSTALLED IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20030730000882003073000088WP 2003 7 30 ABXA030297 120030624A53155910347445 FLOORBEAM DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 FLOORBEAM FS 945, LEFT BUTTLINE 30 WAS CORRODED. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030730000892003073000089WP 2003 7 30 ABXA030304 120030618A522059131951 PAN DOUG DC9 DC941 302207NWP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 RIGHT AFT EMERGENCY OVERWING EXIT DOOR PAN CRACKED AT AFT UPPER JAMB SUPPORT FITTING. REPAIRED AREA IAW DC-9 SRM 52-51 AND SSRM K07390. 2L72 4F A6WE 20030730000922003073000092WP 2003 7 30 ABXA030309 120030721A5320566440111 ANGLE DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX 45927 CORROSION ON FORWARD EDGE OF ANGLES AT UPPER OUTBOARD CORNER OF RIGHT WHEEL WELL. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-21, 51-3-0 AND ABX JOB CARD 8078002. 2L74 4F 4A25 20030730001002003073000100WP 2003 7 30 AMTA200300888 120030529A5310 SHEAR TIE LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 C1 BILGE SHEAR TIE CRACKED. REPAIRED SHEAR TIE IAW SRM 53-12-00. (M) 2L73 4F A23WE 20030730001042003073000104SO 2003 7 30 SIMA200317606 120030623A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21811AE 145529 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGE SECTION ON LEFT OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND SHIMS AND INSTALLED. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 22 CHAPTER 53-21-10 FIG 201 SHEET A AND CPM 51-61-00. RESTORED SURFACE FINISH AND APPLIED CORROSION INHIBITING COMPOUND. (M) 2L72 4F RTT00011AT 20030730001052003073000105SO 2003 7 30 SIMA200317608 120030623A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21712AE 145247 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM LOEW FLANGE AND WEB WERE FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 20 AND 22. BLENDED THE DAMGE AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED A REINFORCEMENT DOUBLER, INSTALLED. REPAIR DONE IAW EMB STATEMENT IC2003-145/2088, EMB SRM, SRM EMB 145/1142 REV 22, 53-21-10 PARA 9, FIG 208 AND STANDARD SRM PRACTICES. RESTORED ORIGINAL SURFACE FINISH AND APPLIED CORROSION INHIBITING COMPOUND TO THE REPAIR AREA. (M) 2L72 4F RTT00011AT 20030730001112003073000111WP 2003 7 30 AMTA200300895 120030523A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 L2 DOOR CUTOUT SKIN LOWER AFT CORNER CRACKED .75 INCH. REPAIRED SKIN IAW EO L10-53AD-0659D. (M) 2L73 4F A23WE 20030730001122003073000112WP 2003 7 30 AMTA200300905 120030520A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 LEFT FUSELAGE SKIN INTERIM REPAIR REQUIRES PERMANENT REPAIR. REPAIRED FUSELAGE SKIN IAW ER/A L10-53R-4759. (M) 2L73 4F A23WE 20030730001142003073000114WP 2003 7 30 AMTA200300902 120030517A5712 RIB LKHEED1011 10113853 5265020WP RT WING DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 RIGHT WING RIB UPPER CAP TEMPORARY REPAIR REQUIRES PERMANENT REPAIR. REPAIRED RIB UPPER CAP IAW ER/A L10-57R-4383A. (M) 2L73 4F A23WE 20030730001292003073000129 2003 7 30 MEX2003206 420030406A34212587335113 GYRO DOUG MD80 MD83 3023681NM COCKPIT FAILED A ASMFK NONE L NO TEST ININSP/MAINT 1 SW23881LF 53051 FLT 259 - CJS-MEX - DURING TRANSIT CHECK WAS DETECTED, GYRO NR 2 WITH ATT FLAG AND CYLINDER DEFACED. THE C/B OF VERTICAL GYRO NR 2 WAS RESET WITH NEGATIVES RESULTS. THE VERTICAL GYRO WAS REPLACED IAW MM 34-23-01, ALL TESTS OK. (M) 2L72 4F RT 20030730001432003073000143NM 2003 7 30 USAABB03101 120030620A3350232T41052 LIGHT BOEING767 7672B7 1385107NM COCKPIT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19655US 25257 PHL - FOUND THE COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA1NM 20030730001472003073000147NE 2003 7 30 2003F00491 220030515A7220 LINER AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE NR 2 ENGINE ERODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK FOUND NR 2 ENGINE AIR INTAKE ATTRITION LINING WITH EROSION. REPAIRED ATTRITION LINING IAW EM 72-32-85 PAGE 6, FIGURE 72-32-85-990-016. (M) 2L72 4F4 FRTA28NM E40NE 20030731000022003073100002NM 2003 7 31 03FDEA01071 120030707A5514NLC6725 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT HORIZONTAL STABILIZER NR 2 BORE CORROSION EXCEEDED CONDITION 3. CORROSION ON RT HORIZONTAL STABILIZER NR 2 BORE REMOVED AND REPAIR CARRIED OUT IAW EA NR 1-5510-71832. 2L73 4F RTA22WE 20030731000142003073100014EA 2003 7 31 QXEA200300863 120030719A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT FALSE INDICATIONA QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09612QX 10042 ON FLIGHT 2494 FIRE SYSTEM FAULT AMBER. CYCLED SHIPS POWER AND FIRE SYSTEM FAULT CLEARED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000192003073100019NM 2003 7 31 QXEA200300854 120030716A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX- DENT IN FUSELAGE EIGHT FEET BACK OF ESCAPE HATCH 12 O'CLOCK POSITION ON THE RIGHT HAND SIDE. REPAIRED IAW DHC-8 RD 8-53-2181. 2H72 4T RTA13NM 20030731000212003073100021EA 2003 7 31 QXEA200300914 120030726A7120 YOKE CNDAIRCL600 CL6002C10 1390015EA RT ENGINE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX- RIGHT HAND ENGINE YOKE HAS GOUGE ON FORWARD CENTER. REPAIRED IAW HORIZON AIR EA R-71-51 AND REO 670-71-21-004. 2L72 4F RTA21EA 20030731000342003073100034NM 2003 7 31 QXEA200300904 120030719A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- LEFT HAND OUTBOARD NR 1 SEAT TRACK HAS LIGHT SURFACE CORROSION AT STATION X333.30. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36 AND RD 8-53-1342. 2H72 4T RTA13NM 20030731000492003073100049NM 2003 7 31 QXEA200300881 120030722A5210 STOP DHAV DHC8 DHC8202 2809007NM PAX DOOR MISSING A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09364PH 524 PDX-GROUND CREW REPORTED EXTERNAL MAIN CABIN DOOR HANDLE RECESSED TOO FAR IN, AND UNABLE TO OPEN. REPLACED MISSING BUMPER AND BUSHING STOP ASSY. CYCLED DOOR AND HANDLE ASSEMBLY WITH NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000502003073100050EA 2003 7 31 QXEA200300872 120030723A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX-DAMAGE FOUND AROUND EXTERNAL AIR CONDITIONING AND HEATING HOOKUP POINT. REPAIRED IAW HORIZON AIR EA R-53-123 AND REO 670-53-61-077. 2L72 4F RTA21EA 20030731000532003073100053NM 2003 7 31 QXEA20030871 120030721A2160T87277 CONTROL VALVE DHAV DHC8 DHC8202 2809007NM A/C BAY MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09356PH108504021 502 SEA-ON FLIGHT NUMBER 2101, FLIGHT ATTENDANT SAYS CABIN VERY WARM. AIR FROM VENTS SMELLED LIKE OLD GYM SOCKS FOR FIRST 10 MINUTES OF FLIGHT. REMOVED AND REPLACED PACK TEMP CONTROL VALVE. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030911000242003091100024NM 2003 9 11 03FDEA01101 120030709A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LT WING OUTBD FLAP OUTBD HINGE ( A/C SIDE ) LOWER OUTBD ATTACH POINT ( TO AFT SPAR ) HOLE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71841 WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKETS LOWER OUTBOARD ATTACHMENT BORE COMMON TO THE REAR SPAR LOWER CAP. 2L73 4F RTA22WE 20030911000562003091100056NM 2003 9 11 2003UALA00587 120030721A5754 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29770UA 26925 TRAILING EDGE WEDGE DELAMINATED, SLAT NR 6. MAJOR REPAIR ACCOMPLISHED. REMOVED , REPAIRED AND REINSTALLED TRAILING EDGE WEDGE. 2L72 4F4 FRTT0001SE E46NE 20030911000642003091100064NM 2003 9 11 03FDEA01154 120030728A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 ELONGATED FASTENER HOLE AT B/S 1070, 1050, 1110, LBL-22, WL-152. REPAIRED FRAME AT B.S. 1070, 1050, 1110, LBL 22 (WL 152) IAW SRM 51-40-3 AND EA 7-5310-54911. 2L73 4F RTA3WE 20030911000682003091100068WP 2003 9 11 DHL2003873512 120030617A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING IB L/E FORMER CRACKED 0.250 AT STA XFS.578.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITHE NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911000772003091100077WP 2003 9 11 DHL2003873538 120030627A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OUTBOARD L/E FORMER CRACKED 0.250 AT STA XFS.741.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001262003091100126NM 2003 9 11 03FDEA01214 120030729A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND WITH CORROSION IN HOLE. LT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71810. 2L73 4F RTA22WE 20030908003142003090800314NM 2003 9 8 SWAA031892 120030824A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CRACKED AT BS 947, STRINGER 26R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030908003302003090800330NM 2003 9 8 SWAA031906 120030826A53116516309 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, BETWEEN STR 14L AND STR 15L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030905002282003090500228SO 2003 9 5 C2XA03TY123 120030811A534714530659005 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF4 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030908002952003090800295NM 2003 9 8 SWAA031913 120030827A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SPECIAL VISIT, FOUND 2 EA STRINGER SPLICES CRACKED, BS 540, STR 10R, AND BS 908, STR 4. REMOVED AND REPLACED BOTH STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030908002982003090800298NM 2003 9 8 SWAA031916 120030826A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 907, LBL 3 TO RBL 3. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030908003352003090800335NM 2003 9 8 SWAA031911 120030826A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 10L, BS 727B PLUS 14 AND BS 727D PLUS 12. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030908003392003090800339NM 2003 9 8 SWAA031923 120030827A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 EEPLS RED LIGHTS MISSING AT OVERWING EXITS. INSTALLED EEPLS LIGHT BULB AND LENSES PER MM. 2L72 4F A16WE 20030909000282003090900028EA 2003 9 9 SWIA200312322 120030808A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 FS 280 RT FLOORBEAM ATTACH ANGLE I/B & O/B CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R-31113-58 2L72 4F RTA21EA 20030909000422003090900042SO 2003 9 9 C2XA03SH319 120030908A33501317 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715948 145056 SHV- DURING C CHECK EMEREGENCY LIGHT ON PANEL 243 ALC FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BULB. RETESTED AFFECTED EMERGENCY LIGHT AND OPERATED GOOD IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030909000582003090900058NM 2003 9 9 VNAA0308023 120030829A2611SD9422AOAO SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY MALFUNCTIONED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07423JS1997713 3032 THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030909000882003090900088EA 2003 9 9 SWIA200312312 120030820A27604916405 ECU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07438SW3285 3285 7574 RT SPOILERS FAULT MESSAGE DURING TAXI OUT. REMOVED AND REPLACED RIGHT SECU. OPS CHECKS GOOD IAW 27-62-01. 2L72 4F4 FRTA21EA E15NE 20030909001092003090900109CE 2003 9 9 53163 120030801A3260327 LIGHT BEECH 1900 1900D 1154162CE COCKPIT INOPERATIVE A AMWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE0726YV UE26 DURING FLIGHT 2511 FROM DALLAS/FORT WORTH TEXAS TO ELDORADO ARKANSAS, THE CREW RETRACTED THE LANDING GEAR, THE RED INTRANSIT GEAR HANDLE LIGHTS DID NOT ILLUMINATE. PRESSED THE GEAR HANDLE LIGHT TEST SWITCH AND THE LIGHTS STILL DID NOT ILLUMINATE. CONTACTED MAINTENANCE, WAS ADVISED TO RETURN TO DALLAS/FORT WORTH. THE CREW THEN NOTIFIED AIR TRAFFIC CONTROL AND DECLARED AND EMERGENCY. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HANDLE LAMP. NO TEARDOWN WILL BE REQUIRED DUE TO THE FACT THAT THE PART IS A NON REPAIRABLE PART. 2L72 4T RTA24CE 20030909001162003090900116EU 2003 9 9 U30A200300022 120030728A2611 SMOKE DETECTOR AIRBUS320 A320212 3930322EU LAVATORY MALFUNCTIONED A U30AK NONE N FALSE WARNING ININSP/MAINT 1 EA17265AV 427 ON GROUND AFTER FLT 326 BWI-PUJ, LAV-D SHOWS SMOKE DETECTOR FAULT. DEFERRED LAV-D PER MEL 26-17-01. ON RETURN TO BWI (7/28/03) AFTER FLT 327, BWI MAINTENANCE OPERATIONALLY TESTED THE SMOKE DETECTOR SYSTEM IAW AMM 26-17-00-501, WITH NO FAULTS FOUND. THIS CLEARED THE MEL AND THE AIRCRAFT WAS RETURNED TO SERVICE. ADDITIONAL WIRE TOUBLESHOOTING OF THE SMOKE DETECTOR SYSTEM PER SRTC 26-03-005 WAS ACCOMPLISHED WITH NO FAULTS FOUND. 2L72 4F RTA28NM 20030909001222003090900122CE 2003 9 9 S2YA03007 120030211A52601294000371 SEAL BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA AIRSTAIRS BLEW OUT A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL13118SK UE108 DURING FLIGHT 1403, THE AIRSTAIR DOOR SEAL BLEW OUT IN FLIGHT. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT AND REPLACED DOOR SEAL AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T3 TRTA24CE E2NE 20030908002732003090800273NE 2003 9 8 SWIA200312364 220030824A73214147T69P01 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT ENGINE MALFUNCTIONED A SWIAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 NM07499SW2556 2556 7398 ON FINAL APPROACH TO SLC, HAD LEFT ENGINE OIL PRESSURE MESSAGE ON EICAS. SHUT DOWN THE LEFT ENGINE PER THE QRH AND CONTINUED IN TO SLC. INSTALLED LEFT FUEL CONTROL PER RII 73-401. 2L72 4F4 FRTA21EA E15NE 20030908002832003090800283CE 2003 9 8 AMWA30 120030818A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV UE163 WHILE PERFORMING INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM MANUAL P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20030908003212003090800321 2003 9 8 SWAA031899 420030825A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030908003252003090800325NE 2003 9 8 SWAA031903 220030824A7200CFM56 ENGINE BOEING737 7375H4 138449DNM GE CFM56 CFM563B1 13802NE NR 2 OVERTEMP A SWAAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW29503SW 24180 858187 ABORTED TAKEOFF, NR 2 ENGINE EGT EXCEEDED TAKEOFF LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030908003332003090800333 2003 9 8 SWAA031909 420030825A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030909000212003090900021EA 2003 9 9 SWIA200312332 120030823A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913SW 7597 FS 280 LT FLOORBEAM LBL 9.0 INBD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: S6144-13 2L72 4F RTA21EA 20030909000932003090900093EA 2003 9 9 SWIA200312315 120030801A5320601R3111357 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 FS 280 O/B LEFT FLOORBEAM ATTACH ANGLE LBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401. P/N: 601R31113-57. 2L72 4F4 FRTA21EA E15NE 20030909000972003090900097WP 2003 9 9 DHL2003873602 120030710A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING EXTENDED L/E I/B VANE HOLES ELONGATED AT STA XS.247 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-0306029, ED-3468. REMOVED FASTENERS, TRIMMED OUT THE ELONGATED HOLES SKIN AREA, PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR EXTERNAL DOUBLER (7075-T6 AL0.071), AN INTERNAL DOUBLER AND A FILLER. CLEANED, TREATED AND PRIMED THE REPAIR EXTERNAL DOUBLER INTERIOR SURFACE FILLER AND INTERNAL DOUBLER. APPLIED PRC SEALANT ON FAYING SURFACE. INSTALLED EXTERNAL DOUBLER, INTERNAL DOUBLER AND FILLER ON RT WING EXTENDED L/E I/B VANE AT STA 247 USING NEW FASTENERS. 2L74 4F RT4A25 20030909001142003090900114 2003 9 9 ARWA20030701 420030702A22112588787904 COMPUTER DOUG DC8 DC862 3021970WP AUTOPILOT SYS MALFUNCTIONED A ARWAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO198968U 46069 LOG PAGE 504844. RUDDER KICKING AFTER TAKEOFF AND OSCILATING. FOUND YAW CHANNEL COMPUTER; REMOVED AND REPLACED YAW CHANNEL COMPUTER AND PERFORMED OPERATIONAL CHECK SYSTEM IAW MM 22-10-37 CHECKED GOOD. CHECKED AND PERFORMED RUDDER OPERATIONAL CHECK IAW MM 27-20-0; CHECKED GOOD. 2L74 4F 4A25 20030909001322003090900132EA 2003 9 9 SWIA200312349 120030830A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07447SW57 57 7677 FLAP FAIL ON TAXI IN. REMOVED AND REPLACED BPSU ON LEFT SIDE PER CRJ MM 27-51-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20030909001372003090900137NM 2003 9 9 S2YA03008 120030303A5610001A561A0000201 WINDSHIELD DORNERDO32 DO328300 NM PWA 306 PW306B NE COCKPIT CRACKED A S2YAA UNSCHED LANDING O OTHER CRCRUISE 1 GL13356SK1913 3163 DURING FLIGHT 2265, THE F/O FORWARD WINDSHIELD INNER PANE SHATTERED THE CREW MADE AN AIR TURNBACK. MECHANIC REPLACED THE WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030909001392003090900139EA 2003 9 9 SWIA200312366 120030826A2751 POTENTIOMETER CNDAIRCL600 CL6002B19 1900309EA T/E FLAP DEFECTIVE A SWIAO OTHER N FALSE WARNING UKUNKNOWN 1 NM07588SW 7069 LEFT FLAP POSITION ON EICAS INTERMITTENTLY FLICKERS 1-3 DEGREES LOWER THAN RIGHT FLAP POSITION - BELOW 8 DEGREE SETTINGS. REPLACED POTENTIOMETER IN LEFT FLAP POSITION TRANSMITTER IAW CMM 27-55-01 & MM 27-55-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20030909001412003090900141EA 2003 9 9 SWIA200312368 120030817A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB FAILED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07907SW2181 2181 7511 HORIZONTAL STAB TRIM FAILS CHANNEL 2 ON PREFLIGHT TEST. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT. OPS CHECK GOOD IAW RII 27-415. MOTOR CONTROL UNIT PN: 7062-3 SN OFF: 961 SN ON: 218. 2L72 4F RTA21EA 20030909001582003090900158SW 2003 9 9 ALGA088882 120030826A6240407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH STUCK B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03557AL 53243 DUAL TACH NP NEEDLE STUCK AT 16 PERCENT. 1G71 3U O H2SW 20030909001622003090900162EA 2003 9 9 SWIA200312309 120030822A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB CHAFED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07929SW 7703 STAB TRIM CH 1 STATUS MSG ILLUMINATED INFLIGHT. COMPLIED WITH QRH PROCEDURE, WOULD NOT RESET. REPAIRED CHAFED WIRE CD75C22 AT P0268. STAB TRIM SYSTEM OPERATIONAL CHECKS GOOD IAW AMM 27-40-00. 2L72 4F RTA21EA 20030909001712003090900171 2003 9 9 BAQA088676 420030813A3420H140CWM INDICATOR AEROSPSA365 SA365N 8680669EU ADI FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 6425 UNIT WAS SLOW TO ERECT AND LANE 2 PITCH ROLL WAS INOPERATIVE. WOULD NOT RUN AUTOPILOT LANE 2 PITCH ROLL. 1G72 3U H10EU 20030909001902003090900190SW 2003 9 9 HEEA088939 120030109A5610407030115123A WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 WINDSHIELD CRAZED. 1G71 3U O H2SW 20030909001952003090900195SW 2003 9 9 HEEA088943 120030704A5610407030115125A WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 WINDSHIELD CRAZED. 1G71 3U O H2SW 20030909001982003090900198NE 2003 9 9 IXXA0300050O 220030725A7200JT3D3B ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 4 LEAKING A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW11799AL729482671 45922335 644407 DURING FLIGHT FROM GOOY TO EDDS NR 4 ENGINE HAD A LOW OIL PRESSURE, LOW OIL QUANTITY AND HIGH TEMPERTURE WARNING. THE ENGINE WAS SHUT DOWN AND THE CREW RETURNED AIRCRAFT TO GOOY. MAINTENANCE INSPECTION IS ON GOING. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED NR 4 ENGINE IN ACCORDANCE WITH ALL APPLICABLE MANUALS. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20030909001992003090900199SW 2003 9 9 HEEA088947 120030826A5330212030268007 PANEL BELL 412 412 1182202SW FUSELAGE MISMANUFACTURED E O OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 PANEL MISMANUFACTURED. WHEN WE STARTED TO DRILL FASTENER HOLES INTO TRIMMED PANEL AT AFT CENTER EDGE, PANEL SEPERATED AND A CLEAR HARD SUBSTANCE CAME OUT OF PANEL. PANEL REPAIRED BY ACI. 1G72 4U H4SW 20030909002012003090900201SW 2003 9 9 HEEA088948 120030829A5302206030433103A SUPPORT BRACKET CLARK 1000 1000CLARK 2230102SW TAILBOOM MISMANUFACTURED E O OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 BRACKET MISMANUFACTURED. BRACKET DOES NOT FIT INTO LOCATOR ARM OF FIXTURE. BRACKET VERTICAL FLANGES ARE BOWED OUT ALONG RADIUS OF BRACKET. THE DIMENSIONS OF THE BRACKET ARE 1.828 AT THE LT AND RT SIDES; AND 1.910 AT THE CENTER OF THE BRACKET. THIS .082 BULGE AT THE CENTER DOES NOT ALLOW THE BRACKET TO FIT INTO OUR FIXTURE LOCATOR ARMS. 1Q71 3R 2A6 20030909002192003090900219WP 2003 9 9 ABXA030333 120030801A57539957578503 SKIN DOUG DC9 DC941 302207NWP T/E FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 BULGE IN SKIN, CUPPED FASTENERS FLAP UNDER SURFACE NR 2 EXPANSION JOINT. REPLACED UPPER AND LOWER FLAP SEGMENT SKIN. 2L72 4F A6WE 20030909002232003090900223WP 2003 9 9 DHL2003604710 120030616A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 D-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR IN IT (MAJOR REPAIR). PERFORMED MAJOR REAPAIR IAW SRM 52-1-0 PG 1, SRM 52-4-1 PG 5, DHL-CVG-00079H. REMOVED D-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SKIN IAW SRM 52-1-0 PG 1, SRM 52-4-1 PG 5, DHL-CVG-00079H. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030909002432003090900243EA 2003 9 9 ASOA03378 120030816A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE FLOOR STRINGER AT FS 349 AFT OF THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOOR STRINGER AT FS 349 AFT OF THE PASSENGER DOOR IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20030909002472003090900247EA 2003 9 9 ASOA03377 120030816A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SEAT TRACKS AT FS 349 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT SEAT TRACKS AT FS 349 IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20030909002482003090900248EA 2003 9 9 ASOA03387 120030818A5320KMM67080001001 SUPPORT BRACKET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11713EV 10081 DURNG A HANGAR CHECK IN BTR, THE LEFT ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE DUCT SUPPORT BRACKETS AFT THE PRESSURE BULKHEAD AT FS 1098.2 IAW ASA EO 700-36-0003B. (M) 2L72 4F RTA21EA 20030909002522003090900252WP 2003 9 9 AMTA200300958 120030721A3350 TRACK LKHEED1011 10113853 5265020WP CABIN CONTAMINATED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11163AT 1229 EGRESS LIGHTS INOPERATIVE AT THE FORWARD GALLEY, EXIT SIGNS AT THE R1 DOOR AND THE FLOOR LIGHTS BETWEEN THE R1 DOOR AND THE R2 DOOR. REMOVED FLUID FROM TRACK AND REMOVED AND REPLACED CABLE IAW AMM 33-50-01. OPS CHECK GOOD. (M) 2L73 4F A23WE 20030909002532003090900253WP 2003 9 9 AMTA200301013 120030730A5320 TRIPLER LKHEED1011 10113853 5265020WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 INSIDE SURFACE OF L3 INTERIOR DOOR OPENING SURROUND TRIPLER CORRODED. REPAIRED TRIPLER IAW ER/A L10-53R-5245. (M) 2L73 4F A23WE 20030909002542003090900254WP 2003 9 9 AMTA200301015 120030723A5512 SKIN LKHEED1011 10113853 5265020WP HORIZ STAB DELAMINATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN DELAMINATED. REPAIRED SURFACE OF SKIN PANEL IAW SRM 51-50-06. (M) 2L73 4F A23WE 20030909002592003090900259NM 2003 9 9 AMTA200301064 120030816A2820285N0200203 PRESSURE SWITCH BOEING757 75733N 1384931NM FUEL SYSTEM FAULTY A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11561TZ 33526 EICAS MESSAGE 'CTR L FUEL PUMP'. TROUBLESHOT PER FIM 28-22-00 FIG 105. REMOVED AND REPLACED LEFT OVERRIDE PUMP PSI SWITCH. OPS AND LEAK CHECK GOOD PER MM 28-42-01-4. (M) 2L72 4F RTA2NM 20030909002602003090900260WP 2003 9 9 AMTA200301017 120030731A5210 SKIN LKHEED1011 10113853 5265020WP PAX DOOR BENT A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 FOUND LEFT P4A DOOR SKIN UPPER AFT CORNER BENT. REPAIRED DOOR SKIN IAW ER/A L10-52R-5255. (M) 2L73 4F A23WE 20030911001892003091100189WP 2003 9 11 AALA20030337 120030305A5534 ANGLE DOUG DC9 DC982 3022082WP VERTICAL STAB CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND LEFT AND RIGHT VERTICAL STABILIZER L/E FAIRING TO FUSELAGE ATTACH ANGLES CRACKED BEYOND STOP DRILLS. REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES PER AARD 55-30-00-7. (M) 2L72 4F A6WE 20030911002062003091100206WP 2003 9 11 AALA20030327 120030317A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE LIGHTNING STRIKEA AALAK NONE O OTHER ININSP/MAINT 1 SW21567AM 53293 TUL - FOUND TWO LIGHTNING STRIKES, FS 599 AND 603. REMOVED DAMAGED AREA OF SKIN AND INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M) 2L72 4F RTA6WE 20030911002172003091100217NM 2003 9 11 DHL2003784003 120030814A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01767AT 22001 ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON P6-3 CIRCUIT BREAKER PANEL. CONFIRMED, NR 3ENGINE GROUND LIGHT DEFERRED IAW DHL B727 MEL 26-9, CONTROL NR 13827, CAT C. PLACARD INSTALLED. REF DMI 13827 ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT IS ILLUMINATED ON P6-3 CIRCUIT BREAKER PANEL. FOUND FIRE LOOP CONTACTING A CLAMP IN STUB WING. REPOSITIONED LOOP AND PERFORMED OP CK IAW B727 MM 26-11-01. OP CK GOOD. THIS CLEARS DMI 13827. PLACARDS REMOVED. 2L73 4F A3WE 20030912000052003091200005CE 2003 9 12 DXTA200300088 120030817A2130 COALESCER BAG CESSNA500 560CESSNA 2076750CE CABIN CONTAMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07393QS 5600393 DIVERTED BACK INTO CMH WHEN EMERGENCY PRESSURIZATION LIGHT CAME ON AFTER TAKEOFF, EMERGENCY PRESSURIZATION CHECK LIST FOLLOWED. - FOUND WATER SEPARATOR COALESCER WATER SOAKED, REMOVED DRIED OUT AND RE-INSTALLED COALESCER, LEAK CHECK GOOD IAW CESSNA 560 MM CHAPTER 21-70-00. 2L72 4F RTA22CE 20030912000392003091200039WP 2003 9 12 DHL2003604702 120030530A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 INTERIM REPAIR ON AFT LWR CORNER OF FWD SERVICE DOOR JAMB. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 14, SHEET 2, TR 53-127, DWG 5750776, DWG SR08530021. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA AND FABRICATED FILLER AND 2 DOUBLERS IAW SRM 53-2-0 FIG 14, SHEET 2, TR 53-127, DWG 5750776, DWG SR08530021. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLERS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 14, SHEET 2, TR 53-127, DWG 5750776, DWG SR08530021, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000852003091200085NM 2003 9 12 AWXA200300833 120030709A5315D5311282600101 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM (DUMMY RAIL) Y503, FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM Y503 FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 29-30. 2L72 4F RTA28NM 20030912001772003091200177WP 2003 9 12 AALA20030869 120030818A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217543A 53025 DFW - FOUND R1 EXIT SIGN EMERGENCY LIGHT INOPERATIVE. SPLICED WIRE FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030915000362003091500036EU 2003 9 15 BAQA089104 120030911A6330L633M2010104 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135QC17 0281 GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030915000472003091500047SW 2003 9 15 HEEA088927 120030822A6700204001364101S CONTROL STICK BELL 412 412 1182202SW COCKPIT MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 CONTROL STICK BOLT HOLE FOR ELBOW IS MISALIGNED. BOLT WILL NOT GO THROUGH. 1G72 4U H4SW 20030915000552003091500055GL 2003 9 15 ALGA088970 220030905A731347105 FUEL NOZZLE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO NEW PART CAUSED FUEL NOZZLE TO STREAK ON FINAL TEST AFTER INSTALLATION. REMOVED AND REPLACED. 1Q71 3R3 U 2A6 E1GL 20030915000702003091500070SW 2003 9 15 ALGA089009 120030905A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03436AL60 53069 DURING TRACKING PROCEDURE, TRIM TAB FAILED TO REMAIN AT SET POSITION. SHORTLY AFTER SETTING TAB TO REQUIRED POSITION,TAB WOULD RETURN TO +5 DEGREE SETTING. BLADE WILL BE SENT O.O.H FOR WARRANTY REPAIR PER B.H.T.I. P.S.E. 1G71 3U O H2SW 20030915000712003091500071EU 2003 9 15 BAQA088838 120030825A7712642519032 TRANSMITTER AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20F 03013GL TORQUE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA039UC 5500 TORQUE TRANSMITTER IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H11EU E4CE 20030915000742003091500074EU 2003 9 15 BAQA088184 120030901A240045023501 MASTER BOX UROCOPEC135 EC135T1 5620026EU ELECTRICAL MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03554ME33 0154 NR 2 ENGINE NO START "BUS TIE OPEN" CAUTION ON CAD. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030915000842003091500084GL 2003 9 15 ALGA089062 220030909A7313E23062061 NOZZLE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE MISMANUFACTURED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO OMEGA RING GROOVE MEASURED AT .021 INCH BELOW SERVICABLE LIMIT OF .100 RETURNED PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20030915001122003091500112NM 2003 9 15 S03453046 120030626A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJFO OTHER O OTHER NRNOT REPORTED 1 WP037119A 29219 FUSELAGE SKIN IMPACK DAMAGE BETWEEN BS 700 AND BS 720, S-46R, S-47R REPAIRED IAW EO 744-53-00-0008 2L74 4F4 FRTA20WE E24NE 20030916000042003091600004NM 2003 9 16 EVAS092017 120030815A2697 WIRE DOUG MD11 MD11F 3023600NM SMOKE DETECTOR LOOSE W QOCFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP0316102 48543 DURING TAIPEI TO BOM CARGO FLIGHT,SYSTEM REPORT (MAIN DECK CABIN SMOKE) WARNING MESSAGE, CHECK THIS AREA NO SMOKE CAN BE FOUND, BUT ACCORDING TO COMPANY PROCEDURE, CAPTAIN DECIDE TO DIVERT AIRPLANE. AFTER REPLACE 3L SMOKE DETECTOR AND PERFORM DETAIL CHECK WIRING, FOUND THE DETECTOR'S GROUND WIRE LOOSEN, RETIGHT THE WIRE AND PERFORM. SYSTEM CONDITION BACK TO NORMAL. 2L73 4F RTA22WE 20030916000172003091600017NM 2003 9 16 EVAS092018 120030905A5210 DOOR BOEING747 74745E 1384947NM MAIN DECK DAMAGED W QOCFO OTHER O OTHER NRNOT REPORTED 1 WP0316403 27141 DURING CARGO LOADING, THE MAIN DECK CARGO DAMAGED BY THE LATCH/HOOK ACTUATOR. AIRCRAFT REPAIR PER SRM 52-00-01 FIGURE 204. THE REPAIR DOUBLER MADE FROM 0.125, 2024-T3 CLAD ALUMINUM SHEET, LOCATED ON MAIN DECK SIDE CARGO DOOR EXTERNAL SKIN (P/N:65B17701-1) AT STATION 1910. 2L74 4F RTA20WE 20030916000242003091600024NM 2003 9 16 HNAA0300033 120030714A3260858601 SQUAT SWITCH DHAV DHC8 DHC8201 2809001NM LT MLG FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07996HA11524 497 ON CLIMB OUT WHEN GEAR WAS RETRACTED, LT MLG DOORS REMAINED OPEN. CREW CYCLED THE GEAR AND LT MLG DID NOT EXTEND. CREW RETRACTED THE GEAR AND ALL DOORS CLOSED. ON APPROACH CREW PERFORMED AN ALTERNATE GEAR EXTENSION. MAINTENANCE FOUND THE LEFT MLG OUTBOARD WOW SENSOR OUT OF ADJUSTMENT AND A FAULT CODE 58 IN THE PSEU BITE MEMORY. ADJUSTED THE WOW SENSOR AND REPLACED THE PSEU. 2H72 4T RTA13NM 20030916000292003091600029NM 2003 9 16 371PA0029 120030715A3350 LAMP BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 R2 EMERGENCY EXIT LIGHT INOP. RELAMPED R2 EMERGENCY EXIT LIGHT. OPS. CHECK OK. 2L72 4F RTA16NE 20030916000382003091600038NM 2003 9 16 03FDEA00978 120030623A2780ARB2850506 SUPPORT FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT WING L/E SLAT NR 16 IB TRACK FITTING CRACKED. REMOVED AND REPLACED RIB AT RT WING LEADING EDGE INBOARD SLAT TRACK NR 16 SUPPORT IAW SRM 51-31-01 VOL. II AND DRAWING NO. ARB2850. 2L73 4F RTA22WE 20030916000732003091600073CE 2003 9 16 BSY2003F00017 120030613A32332317100121EN18 DOWNLOCK SWITCH LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE7312 01518WP ACTUATOR INOPERATIVE A BSYAO OTHER O OTHER NRNOT REPORTED 1 GL078040A 048 GOING INTO ALT, HAD NO NOSE GEAR DOWN AND LOCK INDICATION, LANDED, NO PROBLEM. REMOVED AND REPLACED NOSE GEAR ACTUATOR AND DOWNLOCK SWITCH. OPS CHECK GOOD. 2L72 4F4 F A10CE E6WE 20030912000412003091200041NM 2003 9 12 SROM200300044 120030722A5330 SKIN BOEING737 737205 1384456NM FUSELAGE CRACKED I SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA330977007 23466 DURING RON INSPECTION FOUND FUSELAGE CRACK APROXIMATELY 2 INCHES LONG AND TWO INCHES ABOVE FWD WING TO BODY FAIRING APROXIMATE STA 520, BETWEEN STRS 15 L AND 16L. INSTALLED REPAIR DOUBLER IAW B 737 SRM 53-30-3, FIG 48, DETAIL 10. 2L72 4F RTA16WE 20030912000512003091200051WP 2003 9 12 DHL2003604537 120030430A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING INBD L/E FORMER CRACKED 0.250) STA XFS 566.250. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000772003091200077NM 2003 9 12 AWXA200300815 120030721A53132024T3063 STRINGER BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 PHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON STRINGER 23 LT AT BS 727E. MAINTENANCE REMOVED EXISTING DOUBLER AND REMOVED DAMAGED SECTION OF STRINGER 23 LT AT BS 727E; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR IAW B737-300 SRM 53-00-01, FIG 202. 2L72 4F RTA16WE 20030912000902003091200090NM 2003 9 12 AWXA200300859 120030712A5320654529623 TEE FITTING BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR TEE SPLICE AND NUT PLATES BS 770, LBL 21 TO RBL 21. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CARGO COMPARTMENT FLOOR TEE SPLICE BS 770, LBL 21 TO RBL 21; FABRICATED A NEW REPLACEMENT SECTION OF TEE SPLICE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 6-9. 2L72 4F RTA16WE 20030912001192003091200119NM 2003 9 12 AWXA200300886 120030725A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 770, RBL 10. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF AFT CARGO COMPARTMENT FLOORBEAM AT BS 770, RBL 10; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-53, FIG 201, PG 1. 2L72 4F RTA16WE 20030912001212003091200121NM 2003 9 12 AWXA200300888 120030730A5210507945178 WEB BOEING737 7373G7 1384595NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK 2 EACH .5 INCH CRACKS WERE FOUND ON L1 DOOR INNER CENTER WEB. MAINTENANCE BLENDED OUT CRACKS AT EDGE OF L1 DOOR INNER CENTER WEB; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 52-00-01, FIG 203, PG 205. 2L72 4F RTA16WE 20030912001272003091200127NM 2003 9 12 AWXA200300894 120030714A5320654654039 ATTACH ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK A .25 INCH CRACK WAS FOUND AT UPPER EDGE OF ATTACH ANGLE, JUST BELOW FLOOR AT BS 639, LBL 46. MAINTENANCE REMOVED ATTACH ANGLE FROM FLOORBEAM AT BS 639, LBL 46; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 65-46540; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1, SECT 7, & PG 45, FIG 12, SHT 2. 2L72 4F RTA16WE 20030912001522003091200152NM 2003 9 12 AWXA200300905 120030725A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR BEAM AT BS 858, RBL 5. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT FLOOR BEAM BS 858, RBL 5; FABRICATED 2 EACH REPAIR ANGLES AND AN EXTRUSION; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-70-53, FIG 201. 2L72 4F RTA16WE 20030912001582003091200158NM 2003 9 12 AWXA200300910 120030722A552365C2638415A SKIN BOEING737 7373G7 1384595NM ELEVATOR TAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MINOR REPAIR - DURING C-17 CHECK A CRACK WAS FOUND ON THE LT ELEVATOR TAB LOWER SKIN AT THE INBOARD HINGE CUTOUT. MAINTENANCE REPAIRED LT ELEVATOR TAB BY BLENDING OUT THE CRACK AT THE INBOARD HINGE CUTOUT IAW SRM 55-20-01. 2L72 4F RTA16WE 20030912001732003091200173WP 2003 9 12 AALA20030865 120030815A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21567AM 53293 DEN - AFT EMERGENCY BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030915000492003091500049SW 2003 9 15 HEEA088929 120030826A6220206011132113A GRIP BELL 206 206L3 1182108SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FOUND RETAINER BORE PITTING DUE TO INSUFFICIENT AMOUNT OF PROSEAL AT TIME OF GRIP ASSEMBLY. 1G71 3U H2SW 20030915000722003091500072EU 2003 9 15 BAQA088156 120030721A240045023501 MASTER BOX UROCOPEC135 EC135T1 5620026EU ELECTRICAL FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME1210 132 WILL NOT START AIRCRAFT. CODE (6) WHEN TESTED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030916000122003091600012NM 2003 9 16 MEX2003303 120030721A21301305027 CONTROL PANEL BOEING757 757200 1384950NM COCKPIT BROKEN W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23703AM 27203 AIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORT THAT DURING LANDING ALTIMETER SELECTION WAS STUCK AT 3200 AND ALTITUDE SELECT WAS BROKEN. REPORT WAS DEFFERED IAW MEL DURING TRANSIT CHECK, PANEL SELECTOR CABIN PRESSURE WAS REPLACED IAW 21-31-01, ALL TESTS CORRECT. 2L72 4F RTA2NM 20030916000212003091600021 2003 9 16 MEX2003394 420030826A34254055900906 SYMBOL GENERATOR DOUG MD88 MD88 3023688NM EFIS FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23162PL 49765 AIRCRAFT REJECTED TAKEOFF DUE TO BOTH EFIS AND PFD DISPLAYS BEING LOOSE. BOTH CADC WERE REPLACED IAW MM 34-16-01, ALL TESTS CORRECT. 2L72 4F RTA6WE 20030916000542003091600054CE 2003 9 16 RCO2003F00000 120030606A2421F424R ALTERNATOR CESSNA210 T210M 2073451CE CONT O520 TSIO520R 17040SO FAN BROKEN B RC0RO OTHER O OTHER NRNOT REPORTED 1 SW17732XE 21061850 WHILE INSTALLING A 135 AMP ALTERNATOR KIT UNDER A STC FROM MFG, IT LOOKED LIKE THE COOLING FAN PN 8-4 HAD A SMALL CRACK IN IT. THIS PULLEY IS A ONE-PIECE CAST ASSEMBLY MADE OF ALUMINUM. WHEN THE ALTERANTOR WAS REMOVED FOR CLOSER INSP, THE PULLEY WAS FOUND TO BE COMPLETELY BROKEN IN HALF. THIS VERY POOR CASTING; THE REPLACEMENT WE RECEIVED WAS FULL OF CASTING FLAWS. IF THIS PART HAD COME APART IN FLIGHT OR WHILE A MAINT TECH WAS WORKING ON THE A/C SERIOUS HARM COULD HAVE HAPPENED. WHILE WORKING IN THIS AREA, CARE SHOULD BE USED NOT TO CHIP THIS FAN. ONE TIME INSP, AT THE LEAST SHOULD BE DONE TO THIS PART. THE MFG SHOULD LOOK INTO A BETTER WAY TO MAKE THIS COOLING FAN RATHER THAN CASTING. 1H71 3O3 O 3A21 E8CE 20030916000782003091600078WP 2003 9 16 GTIA030632 120030724A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND CABIN FLOOR PANEL STATION 1003-1072 IS CRACKED AND DISBONDED. STOP DRILLED CRACK. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20030916000832003091600083WP 2003 9 16 GTIA030660 120030827A3260833703 UPLOCK SENSOR DOUG DC9 DC983 3022083WP NLG WW MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION DEDESCENT 1 GL23826NK 49391 ON DESCENT, BETWEEN 10,000 FT - 7000 FT, AFTER NORMAL POWER NOSE GEAR RED UNSAFE LIGHT ON, FOLLOWED QRH. ALL OTHER INDICATION NORMAL, BELIEVED TO BE A MICROSWITCH MALFUNCTION. REMOVED AND REPLACED NOSE GEAR UPLOCK SENSOR. OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20030916000902003091600090WP 2003 9 16 GTIA030658 120030824A5754 RIB DOUG DC9 DC983 3022083WP LE SLAT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FOUND SMALL CRACK ON INTERNAL RIB OF NR 1 L/E SLAT ON LT WING. REMOVED AND REPLACED NR 1 SLAT ON LEFT WING. (M) 2L72 4F RTA6WE 20030916001062003091600106WP 2003 9 16 GTIA030641 120030805A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND CABIN FLOOR PANEL DEBONDED 'HAT' CHANNEL FS 1117-1174. REBONDED HAT CHANNEL. (M) 2L72 4F RTA6WE 20030916001192003091600119WP 2003 9 16 AALA20030882 120030821A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21276AA 49273 ORD - EMERGENCY EXIT LIGHTS ON SEATS FLASH INTERMITTENTLY IN FLIGHT. REPLACED TRACK LIGHTING BATTERY PACKS AT OVERHEAD PANEL ABOVE AFT SERVICE DOOR AND BOTH BATTERY PACKS AT OVERHEAD PANEL ABOVE SEAT 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030916001222003091600122NM 2003 9 16 UIEA200300047 120030822A3097 WIRE BOEING747 74747UF 1384949NM WINDOW HEAT BURNED A UIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19498MC 29259 CAPTAINS WINDOW HEAT TURNED OFF IN FIGHT DUE TO SMOKING WIRE. STATUS MESSAGE 'WINDOW HEAT 1L.' LEFT L1 WINDOW CONTROL SENSOR TERMINAL FITTING TIGHTENED AND CLEANED. FUNCTION, OPS AND CMC TESTS PASSED. NO FAULT FOUND PER MM 30-41-00. (M) 2L74 4F RT1384945 20030822001782003082200178NM 2003 8 22 UPS03441079 120030723A5311HXB149952FT FRAME BOEING747 747123 1384873NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C FESC-LT STA 410 LBL 8- LBL 16 WEB FOUND CRACKED. FESC LT STA 410 LBL 8- LBL 16 FRAME WEB CRACK TRIMMED OFF IAW SRM 51-10-01 AND REPROTECTED IAW SRM 51-10-02. 2L74 4F4 F A20WE E20EA 20030826000272003082600027NM 2003 8 26 03FDEA01373 120030806A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LT WING OUTBOARD FLAP INBOARD HINGE BRACKET (FLAP SIDE) INBOARD PIVOT HOLE FOUND CORROSION. LT WING OUTBD FLAP INBD HINGE BRACKET (FLAP SIDE) INBD PIVOT HOLE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71799, WINGS- LT AND RT OUTBOARD FLAP- INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20030826000332003082600033NM 2003 8 26 VNAA0307009 120030730A7600 HEATER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ENGINE CONTROL OUT OF POSITION A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07429JS 3043 WHILE CREW WAS DOING CHECKLIST AND CHECKING FLIGHT CONTROLS. AILERONS FELT LIKE THEY WERE HANGING UP. MAINTENANCE INSPECTED AND FOUND ENGINE CONDITION LEVER CABLE HEATER RUBBING ON AILERON CABLE. MAINTENANCE REPOSITIONED HEATER AND FOUND NO DAMAGE TO THE CABLE OR THE HEATER. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030826000342003082600034EU 2003 8 26 03FDEA01203 120030803A2170 COALESCER BAG AIRBUS310 A310 EU A/C BAY DIRTY A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25414FE 400 GTF-RNO SMELLED STRONG ODOR IN THE COCKPIT, WORSE AS FLT PROGRESSED. SMELL NOT NOTICEABLE IN CUR OR LAV AREA. NO SMOKE WARN OR ECAM. FACT 03AUG03 07:39 BOI R INSP MDC & CAB & AVIS COMPT NO SMOKE, DETECTED A SLIGHT JET EXHAUST TYPE ODOR IN MDC AREA. REMOVED & INSPECTED COALESCER BAGS FOUND THEM TO HAVE SAME ODOR. REPLACED BOTH BAGS, PERFORMED AIR COOLING SYS CONTAMINATION CK, RAN BOTH ENGS TO PWR & APU NO ODORS. SUSPECT EXTERNAL FUME INGESTION. ALL MAINT IAW A310 TSM 21-20-00 FIG 210 M/M 21-51-16-3, 21-51-00-3. 2L72 4F RTA35EU 20030826000522003082600052WP 2003 8 26 03FDEA01145 120030725A5347FX601096418 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 MAIN CARGO DECK SEAT TRACK LBL 48 STA 1441 TO 1541 HAS 7 EACH GOUGED AREAS. CLOSING ACTION ON 07/16/03 BLENDED OUT AREAS AND FOUND OUT OF LIMITS IAW SRM 53-70-00. REMOVED DAMAGED TRACK AND INSTALLED NEW TRACK IAW SRM 53-70-00. PARTS FAB ON TRAVELERS T2/348607, T2/348609, T2/348608. 2L73 4F A22WE 20030826000682003082600068 2003 8 26 3144043003 420030430A3424A593002 INDICATOR SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP075226R147 3144 22090 T/ SLIP IND INOP. 1G71 3U3 U H9EU E00054EN 20030826001252003082600125WP 2003 8 26 03FDEA00984 120030627A5753 BUSHING DOUG DC10 DC1030 3023501WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 NR S 21 COMPLY WITH EA 8-5750-70954, FOR RT INBD FLAP OUTBD SUPPORT. RECEIVED BUSHINGS IAW MAE TRAVELERS T2/343953 @ T2/343780. INSTALLED BUSHINGS IAW CMM 57-44-09.COMPLIED WITH EA 8-5750-70954 FOR RT INBD FLAP OUTBD HINGE SUPPORT. 2L73 4F A22WE 20030826001312003082600131NM 2003 8 26 03FDEA00996 120030628A533053FX130179 TRIPLER BOEING727 727200 138407ENM FUSELAGE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25463FE 22551 MDIS 463 53-30 0005660 25JUN03 BFM CLOSER COMPLY WITH EA 7-5330-70962; MAIN CARGO DOOR TRIPLER WEAR. FACT 27JUN03 13:59 BFM R COMPLIED WITH EA NR 7-5330-70962, FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR, P/N 53FX1301-7/-9. 2L73 4F RTA3WE 20030826001352003082600135SO 2003 8 26 SIMA200321002 120030725A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21713AE 145249 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT THE DAMAGED AREA OF LEFT OMEGA BEAM AND PERFORMED NDT INSPECTION. FABRICATED AN EXTERNAL DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-10, FIG 201. (M) 2L72 4F RTT00011AT 20030826001442003082600144EU 2003 8 26 SIMA200320807 120030722A55127255150521 SKIN SAAB SF340 340B 7860101EU HORIZ STAB DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21375AE 340B375 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN. INSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS 3079, REV 41, 51-40-22, 23, 40, 51-20-40, 41-43. (M) 2L72 4T RTA52EU 20030826001452003082600145WP 2003 8 26 MEX2003297 120030703A362012911021 THERMOSTAT DOUG DC9 DC987 3022087WP BLEED AIR SYS FAILED A ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23216AM 49586 FLT 523 - MEX-VER - AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF 'L ICE PROTECT TEMP HI AND R AIR CON TEMP HI' LIGHTS. THE ELECTRONIC THERMAL LEFT SW WAS REPLACED IAW MM 21-31-4. DURING OVERNIGHT SERVICE THE ANTICIPATOR AND THERMOSTAT RIGHT SIDE AND ELECTRONIC THERMAL LEFT SW WERE REPLACED IAW MM 36-10-06/07 AND 21-31-4, IN TWO MODE TESTS WERE PERFORMED IAW MM 36-10-00, ALL CORRECT. (M) 2L72 4F RTA6WE 20030826001482003082600148NE 2003 8 26 MEX2003325 220030703A7250 TURBINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE DAMAGED A ASMFA UNSCHED LANDING M OVER TEMP TOTAKEOFF 1 SW23802AM 26270 MEX-TIJ - FLT 176 - AIRTURN BACK, DURING TAKEOFF RIGHT ENGINE HAD 600 DEGREES CELSIUS REDUCING THRUST TO MAINTAIN TEMPERATURE ON LIMITS. DURING EHM ANALYSIS WAS DETECTED R EGT YELLOW MESSAGE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING REVISION DETECTED MISING VANE ON 2ND STAGE AND DAMAGES IN HPTV 2 AND L/E BLADE OF HPT 2 OUT OF LIMITS. THE ENGINE WAS REPLACED IAW MM 71-00-02 AND ENGINE WAS TESTED IAW MM 71-00-00, ALL CORRECT. (M) 2L72 4F4 FRTA2NM E17NE 20030826001492003082600149WP 2003 8 26 MEX2003330 120030108A3241392491 CONTROL VALVE DOUG DC9 DC987 3022087WP ANTI-SKID SYS FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23751RA 49779 FLT 464 - CUL-HMO - AIRCRAFT RETURNED TO PLATFORM, DURING TAXI ANTI-SKID LIGHTS CAME ON. DURING REVISION, DETECTED FAILURE OF DUAL PRESS CONTROL VALVE. THE DUAL PRESSURE CONTROL VALVE AT LEFT INTERIOR SIDE WAS REPLACED IAW MM 32-43-02, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030826001572003082600157WP 2003 8 26 WX030012 120030730A3350 COVER DOUG DC9 DC983 3022083WP CABIN LOOSE A WXOAK NONE O OTHER ININSP/MAINT 1 WP17860GA 49786 DURING ACCOMPLISHMENT OF A SERVICE CHECK IN FAT, MAINTENANCE FOUND EMERGENCY TRACK FLOOR LIGHTS COVER NOT SECURED. THE COVERS WERE RE-SECURED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20030826001742003082600174SO 2003 8 26 SWIA200312134 120030619A3397 WIRE EMB 120 EMB120ER 3260203SO CABIN DAMAGED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07209SW 120269 EMERGENCY LIGHT OVERHEAD BIN DOOR ROW 9 B & C INOP. REPAIRED WIRE TO EMERGENCY LIGHT AT 9BC. OPS CHECK GOOD. 2L72 4T RTA31SO 20030827000172003082700017NM 2003 8 27 03FDEA00953 120030623A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 N00460 CRACKED FRAME SHEAR TIE STA 580 ABOVE 18L ** SD ** COMING 2L73 4F RTA3WE 20030827000252003082700025NM 2003 8 27 03FDEA00904 120030618A5320 STIFFENER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 N00606 CORROSION (C53-132-02-1) ON UPR SURFACE HORIZONTAL FLANGE BS 744, LBL 8, WL 159 ABOVE DELTA BEAM FWD OF PANEL 3209L IN AIR CONDITIONING BEAY. REMOVED CORROSION AREA 3 INCHES X 1 INCH X .021 INCH FROM ORIGINAL .100 INCH FOUND OUT OF LIMITS IAW SRM 53-10-1. REPLACED STIFFENER ON UPPER SURFACE HORIZONTAL FLANGE BS 744, LBL 10 TO RBL 10, WL 159 ABOVE DELTA BEAM IAW SRM 51-10-1 AND 51-30-02, 51-30-04 AND 51-30- 5. 2L73 4F RTA3WE 20030827000442003082700044SO 2003 8 27 J792003F00000 220030603A854025102 SEAL BEECH 58 58 1152740CE CONT O520 IO520* 17032SO RT ENGINE WORN B J79RK NONE K FLUID LOSS ININSP/MAINT 1 GL1395KM 497 TH1315 DURING 100 HOUR INSPECTION, FOUND RT ENGINE PNEUMATIC PUMP COUPLING OILY. FURTHER INVESTIGATION REVEALED DRIVE SHAFT ADAPTER SEAL LEAKING OIL INTO PUMP COUPLING AND INTO PUMP. REPLACED SEAL (PN 25102) AND PRESSURE PUMP (442CW-12). SYSTEM OPS CHECK OK. RECOMMEND INSPECTING THIS AREA ANYTIME ACCESS IS AVAILABLE. 1L72 3O3 O 3A16 E5CE 20030822001312003082200131WP 2003 8 22 0301379970 120030727A217039706221 VALVE DOUG DC9 DC931 3022065WP A/C BAY FAULTY A NWAAB EMER. DESCENT O OTHER CRCRUISE 1 GL019334 47247 CABIN PRESSURE FLUCTUATED AT CRUISE POWER WITH ICE PROTECTION ACTIVATED. CABIN CLIMBED IN AUTO MODE AND CREW ATTEMPTED TO STOP CABIN CLIMB IN MANUAL MODE. RED CABIN PRESS LIGHT ILLUMINATED SO CREW INITIATED A RAPID DESCENT AND FOLLOWED RED-BORDER CHECK LIST. FLIGHT CONTINUED TO DESTINATION IN MANUAL MODE. LANDING AT PHL WAS WITHOUT INCIDENT. MAINTENANCE COULD NOT FIND ANY PRESSURE LEAKS OR SYSTEM FAULTS. EXCESSIVE AMOUNT OF WATER WAS FOUND IN RIGHT WATER SEPARATOR. REPLACED WATER SEPARATOR AND TEMPERATURE CONTROL VALVE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030822001412003082200141NM 2003 8 22 C1HA200381016 120030805A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON TOP OF FS 1030 FLOORBEAM BETWEEN LBL 22 AND RBL 22. 2L73 4F A3WE 20030822001432003082200143NM 2003 8 22 C1HA200381018 120030806A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON FLOORBEAM FS 344 LBL 58 RBL 58. 2L73 4F A3WE 20030822001482003082200148NM 2003 8 22 C1HA200381023 120030806A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON SEAT TRACK FS 1000 / 1050 LBL 24. 2L73 4F A3WE 20030822001852003082200185NM 2003 8 22 UPS03441122 120030718A5311141U1009343 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D- BS 380 STR 25L FRAME CRACKED. FRAME REPLACED AS PER SB747-53-2272 DWG 624U0003 FROM S23L TO S44L AT BS380. 2L74 4F A20WE 20030825000952003082500095NM 2003 8 25 CALA0300436 120030804A5230 DOOR FRAME BOEING777 777224 1385225NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776010 29480 INSPECTION FOUND AFT CARGO DOOR INTERNAL DOOR UPPER FRAME DENTED. THE FRAME WAS REPAIRED IAW ECRA 5230-01729. 2L72 4F RTT00001SE 20030825001042003082500104NM 2003 8 25 0301495506 120030805A29133508806 PUMP BOEING757 757251 1384970NM LT ENGINE FAILED A NWAAH DEACTIVATE SYST/CIRCUITS K FLUID LOSS CRCRUISE 1 GL01506US733912254 23195 ONE HOUR AND 20 MINUTES INTO FLIGHT AT FL370, THE LEFT ENGINE HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND TURNED OFF PUMP. FIFTEEN MINUTES WITH PUMP OFF THE OVERHEAT LIGHT EXTINGUISHED. FIFTEEN ADDITIONAL MINUTES, THE RESERVOIR LIGHT ILLUMINATED. TURNED OFF ALL LEFT PUMPS PER COM PROCEDURES WITH +3 REMAINING. FLUID QUANTITY CONTINUED TO DEMINISH UNTIL REACHING ZERO. A YELLOW EMERGENCY WAS CALLED AND AIRCRAFT MADE AN UNEVENTFUL LANDING. WHILE SERVICING THE LEFT HYDRAULIC SYSTEM, HYDRAULIC FLUID WAS LEAKING FROM THE LEFT ENGINE EDP DRAIN. REMOVED AND REPLACED THE EDP. 2L72 4F RTA2NM 20030825001462003082500146NM 2003 8 25 AMTA200300979 120030730A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11527AT 30886 EMERGENCY EGRESS TRACK LIGHTING FLOOR SECTION FROM 2FED-5FED, OPS GOOD. (M) 2L72 4F RTA2NM 20030825001632003082500163EA 2003 8 25 ASOA03270 120030611A533060033010 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING HANGAR MAINTENANCE IN CKB, THE FUSELAGE SKIN AT FS 235 ON THE RIGHT SIDE OF THE AFT NOSE GEAR CUT OUT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FUSELAGE SKIN AT FS 235 ON THE RIGHT SIDE OF THE AFT NOSE GEAR DOOR CUTOUT IAW ASA EO 600-53-0104 AND WVAC EO 601R-53-4109A. (M) 2L72 4F RTA21EA 20030825001702003082500170WP 2003 8 25 DHL2003873593 120030404A53209754022502 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 ITEM REF: N/R 1684: FWD CARGO COMPT FLOOR BEAM CUSP EXTRUSION FITTING SHOWS 1 CRACK IN IT (STA.340.000 RBL-49) (MAJOR REPAIR). CORR: PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON FWD. CARGO COMPT (STA.340.000, RBL-49) IAW SRM 51-1-20D PG.9. 2L74 4F4 FRT4A25 E2GL 20030826000112003082600011NM 2003 8 26 03FDEA01288 120030806A5744ARC0502404 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) FOUND CORROSION ON UPPER OUTBOARD ATTACH HOLE FWD FACE. RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) UPPER OUTBOARD ATTACH HOLE FWD FACE REMOVED AND REPAIRED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030826000432003082600043NM 2003 8 26 03FDEA01193 120030730A5720ANB7445 SHIM DOUG MD11 MD11 3023602NM LT WING OUT OF POSITION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT WING ROOT- UPPER SURFACE- STRINGER NR 4 SHIM FOUND MIGRATED 0.6 INCH DOWN AND 0.4 INCH FWD. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION. 2L73 4F RTA22WE 20030826000492003082600049NM 2003 8 26 03FDEA01218 120030803A5712 RIB DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING NR 16 SLAT TRACK INBOARD RIB FOUND CRACK APPROX 0.5 INCH IN LENGTH. RT WING NR 16 SLAT TRACK INBOARD RIB REMOVED AND NEW RIB INSTALLED AS PER SRM 51-35-01 VOL. II AND SRM 51-33-01 VOL.II. 2L73 4F RTA22WE 20030826000552003082600055WP 2003 8 26 03FDEA01142 120030725A5753ARC2177 SUPPORT DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 WINGS- LEFT OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM ARC2177. CLOSING ACTION ON 07/22/03. COMPLIED WITH EA 8-5740-70985. WINGS- LEFT OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM. 2L73 4F A22WE 20030826000892003082600089EU 2003 8 26 YENA200312 120030622A3350321430 BATTERY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15503JB 1123 DURING WEEKLY CHECK FOUND AFT EPSU BATTERY FAILING TEST. REPLACED LEFT AFT BATTERY PER AMM; TEST OK. 2L72 4F RTA28NM 20030826001202003082600120WP 2003 8 26 NACA20030088 120030529A5711 SPAR DOUG DC6 DC6 3021702WP LT WING CORRODED A NACAK NONE O OTHER ININSP/MAINT 1 AL032907F 44636 DISCREPANCY: REAR SPAR CORRODED L351 TO 399 UPPER AND LOWER CAPS AND WEB. SPLICED IN NEW SECTION OF AFT SPAR WEB FROM LT WING STA. 361 TO STA. 393 IAW O/H MANUAL 13-10 FIG. 13-4. 2L74 4R A781 20030826001692003082600169SO 2003 8 26 SWIA200312112 120030614A5753 CHANNEL EMB 120 EMB120ER 3260203SO T/E FLAP CRACKED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07214SW 120280 AFTER DEPARTURE THE FLAPS WOULD NOT RETRACT PAST APPROXIMATELY 10 DEGREES. RECEIVED FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING APPROXIMATELY 10 DEGREES. FOUND THE LEFT OUTBOARD FLAP LOWER CHANNEL CRACKED AT INBOARD END [ROLLER BRACKET ATTACH POINT]. REMOVED CHANNEL AND REPAIRED IAW 51-70-02. REINSTALLED CHANNEL, RAN FLAPS. OPS CHECK GOOD. 2L72 4T RTA31SO 20030827000222003082700022NM 2003 8 27 03FDEA00907 120030618A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 N00368 970 FRAME DENTED AT S25L. REPAIRED FRAME AT BS 970 STR 25L IAW SRM 51-40-3, FIG 1, BS 970 FRAME DENT AT STR 25L OUT OF LIMITS IAW SRM 53-10-1. 2L73 4F RTA3WE 20030827000472003082700047SW 2003 8 27 HEEA0029620 120030216A7920209062010001 VALVE BELL 412 412 1182202SW PWA PT6 PT6* 52043EA ENGINE OIL LEAKING A HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032149S 36002 VALVE, LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 4U3 T H4SW E2NE 20030827000522003082700052NM 2003 8 27 ANCF200300018 120030622A5240580801034 PIN BOEING767 767383 1385214NM SERVICE DOOR BENT W ANCFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23984AN 24357 PILOT REPORT: DURING FLIGHT WAS PRESENTED ENTRY DOORS LIGHT ILLUMINATED STEADY AND EICAS MSG. RT AFT ENTRY DOOR DISPLAYED STEADY. LOCK PIN ENGAGED. FLIGHT RETURNED. AFT ENTRY SERVICE DOOR LATCH PIN WAS FOUND BENT AND IT WAS REPLACED IAW AMM 521115 PAGE 401 TO 406 WITH SATISFACTORY RESULTS. 2L72 4F RTA1NM 20030827000662003082700066NE 2003 8 27 JUL2003F00000 220030528A73133014795 ADAPTER CESSNA208 208 2073702CE PWA PT6 PT6A114 52043NE FUEL NOZZLE DEFECTIVE B JULRK NONE O OTHER ININSP/MAINT 1 SW01276MA395 20800276 UPON REMOVAL OF FUEL NOZZLES FOR CLEANING, FOUND ROLL PIN IN SECONDARY HOLE. NOTIFIED MFG OF CONDITION. 1H71 3T3 TNTA37CE E4EA 20030827000882003082700088SO 2003 8 27 C2XA03CL129 120030727A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714945 145049 EWR FLIGHT NR 2568 THE CREW REPORTED THE AISLE PATH LIGHTING WAS INOPERATIVE STARTING FROM ROW 8. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030827000922003082700092SO 2003 8 27 C2XA03SH252 120030803A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV-DURING C CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20030827001002003082700100NM 2003 8 27 CALA0300396 120030719A5315 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714342 23580 INSPECTION FOUND FLOORBEAM CORRODED AT L-2 DOOR AFT GIRT BAR ATTACH POINT, STA 986. A REPAIR WAS ACCOMPLISHED ON UPPER CHORD OF FLOORBEAM IAW ECRA 5310-03851. 2L72 4F4 FRTA16WE E2GL 20030827001182003082700118NM 2003 8 27 CALA0300463 120030811A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND LT CHANNEL CORRODED ON FORWARD SIDE OF AFT PRESSURE BULKHEAD AT LOWER END, STA 1016, BL 0. THE CHANNEL WAS REPAIRED IAW EA 5310-04045 AND DRAWING 65C28106-1. 2L72 4F RTA16WE 20030827001262003082700126NM 2003 8 27 CALA0300421 120030728A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND RT LOWER AFT END OF KEEL BEAM ANGLE HOLES ELONGATED FROM PANEL HARDWARE. INSTALLED REPAIR STRAPS AND FILLERS IAW ECRA 5311-01160. 2L72 4F RTA16WE 20030827001452003082700145NM 2003 8 27 2003UALA00538 120030703A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 MAIN CABIN BS 1043, RBL 90, SEAT TRACK CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS 2L72 4F4 FRTA1NM E24NE 20030827001472003082700147NE 2003 8 27 2003UALA00541 220030703A7230 COMPRESSOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 ENGINE STALLED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CRCRUISE 1 WP29179UA 25158 NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND N1 ROLLBACK. ENGINE EXPERIENCED A SURGE AT HIGH EPR NOT AT TAKEOFF ( NO GROUP 3). EICAS MESSAGE SVA FAIL. REMOVED ENGINE SENT TO TEST CELL AND FOUND SVA BINDING. CHANGED SVA. 2L74 4F4 FRTA20WE E24NE 20030827001522003082700152NM 2003 8 27 2003UALA00582 120030720A2432 BATTERY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE MASTER DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29657UA 27112 MAIN BATTERY CHARGER STATUS MESSAGE. MAIN BATTERY REPLACED. SHOP REPORTS THE BATTERY WAS COMPLETELY DISCHARGED. BATTERY WAS PROCESSED THROUGH THE OVERHAUL CYCLE AND PASSED ITS ACCEPTANCE TEST. 2L72 4F4 FRTA1NM E24NE 20030827001672003082700167EU 2003 8 27 MALA030365 120030801A2910 B-NUT SAAB SF340 340B 7860101EU MLG LOOSE A MALAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL15366PX 340B267 DURING APPROACH ON FLIGHT NR 3268, ON SHORT FINAL WITH GEAR AND FLAPS DOWN, HYDRAULIC CAUTION LIGHT ILLUMINATED. WENT AROUND BUT GEAR AND FLAPS REMAINED DOWN. HYDRAULIC QUANTITY AND MAIN PRESSURE INDICATED ZERO. LOST HYDRAULIC AND PRESSURE. GEAR WAS SELECTED DOWN ALREADY BEFORE QUANTITY STARTED GOING DOWN. MAINTENANCE FOUND HYDRAULIC FLUID COMING FROM THE GEARWELL. FOUND B-NUT LOOSE ON RETRACTION ACTUATOR ON AFT LINE. MAINTENANCE RETORQUED LINE. FLUID STOPPED. SERVICED HYDRAULIC IAW SF340 AMM 29-10-29 PERFORMED LEAK AND OPS CHECK ON RETRACTION ACTUATOR . OPS CHECK GOOD. NO LEAKS AT THIS TIME. 2L72 4T RTA52EU 20030909000702003090900070 2003 9 9 SWIA200312356 420030823A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07157326906 6906 120195 F/O AUTOPILOT CAPTURES 400 FT HIGH. INSTALLED SERVICEABLE APP-65 AUTOPILOT CONTROL PANEL. OPS CHECK GOOD. PN: 622-6684-006, SN ON: 2297, SN OFF: 1715. 2L72 4T RTA31SO 20030909001212003090900121SW 2003 9 9 ALGA088782 120030818A5320407030740115S SUPPORT BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL6498 53240 SUPPORT CRACKED AT DZUS RECEPTICALES. PROBABLE CAUSE IS ASB407-02-54. REC. DOUBLERS AT RECEPTICALE AREAS. 1G71 3U3 UO H2SW E1GL 20030909001732003090900173EU 2003 9 9 BAQA088264 120030822A62401179405303 INDICATOR BOLKMS117 BK117B1 5626012EU TRIPLE TACH INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE13 7219 TRIPLE TACH NR 1 NEEDLE IS INOPERATIVE. THIS UNIT LASTED FOR 5 DAYS (11.2) HOURS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030909001912003090900191SW 2003 9 9 HEEA088940 120030821A5610407030115123A WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 WINDSHIELD CRAZED. 1G71 3U O H2SW 20030909002572003090900257WP 2003 9 9 AMTA200301018 120030802A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 FUSELAGE BELLY SKIN INTERIM REPAIR REQUIRES PERMANENT DISPOSITION. REMOVED INTERIM REPAIR AND REPAIRED SKIN IAW ER/A L10-53R-52 38. (M) 2L73 4F A23WE 20030909002702003090900270EU 2003 9 9 RAIA00308219 120030821A772231055017 SENSOR JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE DEFECTIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03561HK277 41077 5595-FWA- LEFT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE INLET TEMP SENSOR. 2L72 4T RTA41NM 20030910000222003091000022 2003 9 10 XG3R088170 420030721A3120B1894522282A CLOCK UROCOPEC130 EC130B4 EU COCKPIT INTERMITTENT B XG3RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 3560 CLOCK IS INTERMITTENT. REPLACED CLOCK. 1G72 3U H9EU 20030910000402003091000040SW 2003 9 10 HEEA088222 120030722A77203030083A COMPENSATOR BELL 412 412 1182202SW NR 2 ITT FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 NR 2 ITT FLUCTUATING. MAINTENANCE REPLACED THE TRIM COMPENSATOR. 1G72 4U H4SW 20030910000412003091000041EA 2003 9 10 HEEA088223 220030715A732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6 PT6* 52043EA FREE TURBINE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0321498 36003 DURING FLIGHT HAD NR 1 ENGINE LOW SIDE GOVERNOR FAILURE. MAINTENANCE LEAK CHECKED ALL LINES AND REPLACED GOVERNOR. ALSO CHECKED LINES FOR CONTAMINATION. 1G72 4U3 T H4SW E2NE 20030910000942003091000094 2003 9 10 MWEA030361 420030903A31604059051931 CIRCUIT BREAKER BOEING717 717200 1383700NM COCKPIT TRIPPED A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31905ME 55169 CAPTAIN'S NUMBER ONE MULTIFUNCTION CONTROL DISPLAY UNIT WENT BLANK. RESET BREAKERS OPERATES NORMAL, RETURN TO SERVICE. 2L72 4F TRA6WE 20030910001002003091000100WP 2003 9 10 MWEA030311 120030817A2780R2159 RELAY DOUG DC9 DC932 3022066WP L/E SLAT FAILED A MWEAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 GL31207ME 47794 SLAT EXTEND LIGHT INOPERATIVE. REMOVED AND REPLACED RELAY. 2L72 4F A6WE 20030910001042003091000104WP 2003 9 10 MWEA030282 120030718A53305910228507 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 FUSELAGE SKIN AT STATION 1164 ON RIGHT SIDE OF AFT OF LOUVER HAS DAMAGE TO THE INTERNAL SIDE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20030910001152003091000115NM 2003 9 10 03FDEA01306 120030807A5753ARC0502403 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING - O/B FLAP I/B HINGE FITTING ( WING SIDE ) LOWER PIVOT ATTACHMENT BORE HOLE FOUND CORROSION. LT WING O/B FLAP I/B HINGE FITTING (WING SIDE) LOWER PIVOT ATTACHMENT HOLE BORE REPAIRED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030910001252003091000125NM 2003 9 10 MWEA030341 120030827A5347593054744 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 NR 6 SEAT TRACK REQUIRE'S REMOVAL OF FILLER STRIP, CLEANING AND A DETAILED INSPECTION OF STATION 215-256. CLEANED SEAT TRACK, FABRICATED AND INSTALLLED REPAIR PART IN SEAT TRACK SPLICE SECTION. 2L72 4F RTA6WE 20030910001382003091000138NM 2003 9 10 MWEA030348 120030827A53205930961533 THRESHOLD DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FLOOR THRESHOLD SUPPORT LOCATED JUST INBOARD OF THE AFT SERVICE DOOR IS CRACKED. REPAIRED FLOOR THRESHOLD. 2L72 4F RTA6WE 20030910001582003091000158EA 2003 9 10 ASOA03363 120030807A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11908EV 7654 DURING A GROUND INSPECTION IN DFW, THE RIGHT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030910001752003091000175SO 2003 9 10 SIMA200321809 120030730A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 22, CHAPTER 53-21-10 FIG 201, SHEET 3 CPM 51-61-00 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030910001802003091000180SO 2003 9 10 SIMA200321803 120030804A5610163500112 WINDSHIELD EMB 135 EMB135KL 3260302SO COCKPIT CRACKED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21821AE 145577 RIC - FLT 4128 - DURING CLIMB AT ABOUT 10,000 FEET, CREW NOTED FIRST OFFICER WINDSHIELD ARCING SHORTLY AFTER HEAT WAS SELECTED OFF THE WINDSHIELD STARTED TO SHATTER. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO FURTHER PROBLEMS REPORTED. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030910001812003091000181SO 2003 9 10 SIMA200322502 120030809A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21819AE 145566 ABI - DURING AN MBN INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED ARE AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE, SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20030910001882003091000188EU 2003 9 10 SIMA200322306 120030806A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21375AE 340B375 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE APPLICATION OF A REPAIR DOUBLER TO THE UPPER FUSELAGE SKIN AFT OF FRAME STATION 439 AND BETWEEN STRINGERS 1602 AND 1603. REMOVED DENT BY CREATING A CUTOUT. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB STATEMENT 340SDS005824 AMENDENT 2 PARA 1.3.4 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20030910002082003091000208EU 2003 9 10 MALA030396 120030831A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 DURING 4Y/2Y CHECK IN CWA, FUSELAGE HAS DENTS AT STA 317, WL77, WL73, STA 341, WL85,25, STA 339-365 AND SL1618-SL1622. REPAIRED. INSTALLED DOUBLER AT STA 339-365 AND SL1618-1622. 2L72 4T RTA52EU 20030910002102003091000210EU 2003 9 10 MALA030361 120030709A2910 HYDRAULIC LINE BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING C-CHECK INSPECTION IN CVG, MAIN HYDRAULIC PIPE PN HC291H0310-000 CHAFED BEYOND LIMITS FOR NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED MAIN HYDRAULIC PIPE PN HC291H0310-000 IAW AMM 20-09-12 LEAK CHECK GOOD. REFER TO 409 NR 128404 FOR DETAIL. A/C RELEASE DATE 7/25/2003. 2H74 4F RTA49EU 20030910002122003091000212NE 2003 9 10 MALA030353 220030727A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1568XJ 340A068 AFTER TAKEOFF ON FLIGHT NR 2724, RT ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE APPROXIMATELY 10-20 RETURNED FOR LANDING AT ALO DID NOT SHUT ENGINE DOWN. AIR RETURN TO ALO. MAINTENANCE INSPECTED OIL LEVEL, FOUND TO NEED 3.5 QTS OF OIL RAN A/C AT CRUISE POWER FOR 30 MNUTES IN CHECKED OIL LEVEL AGAIN, AND WAS 3/5 QTS LOW. A/C WAS PARKED NO FERRY. MAINTENANCE REMOVED AND REPLACED RT ENGINE PN ON/OFF CT7-5A2, SN/ON GE-E367387, SN/OFF GE-E367283 IAW J/C 7100-301 FOR OPS AND LEAK CHECK GOOD. 2L72 4T4 TRTA52EU E8NE6 20030910002152003091000215EU 2003 9 10 MALA030364 120030728A3350 LIGHT BAC 146 AVRO146RJ85A1500097EU CABIN BROKEN A MALAK NONE O OTHER NRNOT REPORTED 1 GL15508XJ E2318 EMERGENCY EXIT LIGHT BY FORWARD PAX DOOR, BROKEN OFF. MAINTENANCE RESECURED EMERGENCY EXIT LIGHT BY FORWARD RT PAX DOOR. OK FOR SERVICE. 2H74 4F RTA49EU 20030911000102003091100010NM 2003 9 11 03FDEA01168 120030726A5753ARC41251 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT WING- O/B FLAP STOP BOLT SUPPORT ISLAND FOUND CRACKED. LT OUTBD FLAP STOP BOLT SUPPORT ISLAND REPAIRED AS PER FEDEX EA 1- 5750-69259 - WINGS - TRAILING EDGE FLAPS - LT OUTBOARD FLAP SECONDARY UP STOP REPAIR. 2L73 4F RTA22WE 20030911000112003091100011NM 2003 9 11 03FDEA01161 120030722A5730ARC74132 SKIN DOUG MD11 MD11 3023602NM ZONE 600 BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE. RT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE REPAIRED AS PER FEDEX EA 1-5720-69399 - WINGS - OUTER WING - RH REAR SPAR/TRAILING EDGE CORROSION REWORK. 2L73 4F RTA22WE 20030911000142003091100014CE 2003 9 11 DXTA200300102 120030824A3230 VALVE CESSNA650 650 2076802CE MLG STUCK E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07710QS 6507100 AFTER TAKE OFF, DURING GEAR RETRACTION THE LANDING GEAR "UNLOCK" ANNUNCIATOR REMAINED ILLUMINATED, CYCLES GEAR SEVERAL TIMES LIGHT REMAINED ON, DIVERTED INTO BFI AND LANDED SAFELY. TROUBLESHOT AND FOUND RETRACT PRESSURE RELEASE VALVE STUCK. RESEATED VALVE AND ACTUATED 50 TIMES LEFT AND RIGHT NO FURTHER STICKING OR BINDING NOTED. PERFORMED 15 NORMAL GEAR CYCLES AND 5 EMERGENCY EXTENSIONS ALL CHECKED GOOD, SERVICED RESERVOIR TO FULL AND GEAR BOTTLE TO 2000 PSI REFERENCE CESSNA 650 MM CHAPTER 12-11. PERFORMED 3 MORE NORMAL GEAR CYCLES, BLED SYSTEM ALL CHECKS GOOD. 2L72 4F A9NM 20030909001642003090900164EU 2003 9 9 BAQA088841 120030825A28221176415103 PUMP BOLKMS117 BK117A3 5626015EU FUEL BOOST INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LG459 7032 BOOST PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030909001652003090900165EU 2003 9 9 BAQA088853 120030826A6240L771M40C1005 INDICATOR UROCOPEC135 EC135P1 8680990EU TRIPLE TACH INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH335 0179 TRIPLE TACH BOTH N2 INDICATIONS FALL OFF LINE INTERMITTENTLY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030909002422003090900242NM 2003 9 9 AMTA200301069 120030818A2421727792K IDG BOEING757 75733N 1384931NM NR 1 ENGINE FAILED A AMTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL11551TZ 32585 EICAS MSG LT GEN OFF DISPLAYED, LT GEN OFF LIGHT ILLUMINATED, GEN SWT RESET DID NOT CORRECT CONDITION. REMOVED AND REPLACED NR 1 ENGINE IDG PER MM 24-11-01-4. PERFORMED IDLE LEAK TEST PER AMM 71-00-00/501. RAN ENGINE NO LEAKS NOTED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030910000252003091000025WP 2003 9 10 DHL2003604529 120030429A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT HORZ STAB L/E OUTER PLATING DENTED, STA XFS 241.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4. CUT OUT DAMAGED AREA OF LT HORZ STAB L/E OUTER PLATING IAW SRM 55-2-1 FIG 4. FABRICATED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000512003091000051EU 2003 9 10 HEEA088919 120030623A6230407040038105 MAST BOLKMS105 BO105S 5626006EU MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 WEAR SLEEVE IS DEBONDED. 1G72 3U H3EU 20030910000602003091000060WP 2003 9 10 DHL2003604555 120030530A57305611013501 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED AT STA XRS 219.000. REMOVED AND REPLACED LT WING T/E LWR PANEL AT STA XFS 219.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030910000992003091000099NE 2003 9 10 AWXA200300804 220030714A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 OVERHEATED A AWXAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP28657AW 1003 DURING TAKEOFF AT LAS EN ROUTE FOR SEA, AT TAKEOFF POWER NR 1 ENGINE TEMPERATURE REACHED APPROXIMATELY 620 DEGREE'S FOR LESS THAN 2 SECONDS. FLIGHT CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE INLET AND EXHAUST SYSTEM WITH NO FINDINGS PER AMM TASK 71-00-00-710-014. NO ADDITIONAL INSPECTIONS REQUIRED DUE TO ENGINE DID NOT REACH THE 635 DEGREE THRESHOLD. 2L72 4F4 FRTA28NM E40NE 20030910001302003091000130NM 2003 9 10 DHL2003782006 120030722A2611 SMOKE DETECTOR BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE CARGO BAY FALSE INDICATIONA DHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01769AT 21998 NR 6 MAIN CARGO SMOKE DETECTOR ILLUMINATED AT FL 310. PERFORMED EMERGENCY CHECKLIST. LANDED AT MDT. REMOVED AND REPLACED NR 6 MAIN CARGO COMPARTMENT SMOKE DETECTOR. OPS CHECKED GOOD IAW AMM 26-17-0. 2L73 4F4 F A3WE E2EA 20030910001792003091000179EA 2003 9 10 ASOA03355 120030803A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11856AS 7404 FLT 4680 - DURING CRUISE FROM ROA-ATL, WHILE LEVELING OFF AT 23,000 FEET A STRONG FUEL SMELL OCCURRED IN THE COCKPIT AND THEN DISAPPEARED WITHIN APPROXIMATELY FIVE MINUTES AFTER SWITCHING THE BLEEDS TO THE AUXILIARY POWER UNIT. THE AICRAFT LANDED SAFELY IN ATL. MAINTENANCE RAN EACH ENGINE BLEED INDEPENDENTLY WITH THE PACK AND AUXILIARY POWER UNIT SEPARATELY. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030911000042003091100004NM 2003 9 11 03FDEA01254 120030812A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 BS 740 FLOORBEAM UPR CHORD CHAFED ALONG AFT EDGE LBL 44 -RBL 44 WL 208 . BLENDED DAMAGE PER EA 7-5310-72307. 2L73 4F RTA3WE 20030911000302003091100030NM 2003 9 11 03FDEA01200 120030730A5511ALC81312 SPAR CAP DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 HORIZONTAL STAB RT AFT SPAR CAP NR 36R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STABILIZER AFT SPAR CAP NR 36R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69404 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 36 RIGHT HAND SIDE. 2L73 4F RTA22WE 20030911000312003091100031 2003 9 11 373PA0020 420030818A2220 COMPUTER BOEING737 7373Y0 1384671NM MACH TRIM FAILED A PIDAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO05373PA 23749 SPEED TRIM FAIL AND MACH TRIM FAIL ON OVERHEAD PANEL. ENGINES RUNNING, READY FOR TAXI. DEFERRED PER MEL 22-1 AND 22-5-1. 8/18/2003: REPLACED FLIGHT CONTROL COMPUTER IAW MM 22-11-33. FCC BITE TEST GOOD. SPEED TRIM AND MACH TRIM OPS CHECKS NORMAL. 2L72 4F RTA16WE 20030911000442003091100044NM 2003 9 11 DHL2003741006 120030718A2611302842 SMOKE DETECTOR BOEING727 7272Q9 138448MNM CARGO BAY FAULTY A DHLAO OTHER N FALSE WARNING DEDESCENT 1 SO01741DH 21931 CARGO SMOKE LIGHT ILLUMINATED DURING DESCENT. CYCLED SWITCH OFF THEN ON AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 6 CARGO SMOKE DETECTOR IAW M/M 26-16-01. OPS CHECKED NORMAL. 2L73 4F RTA3WE 20030911000552003091100055WP 2003 9 11 DHL2003873561 120030703A5753S124328612000 TEE FITTING DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT OUTBOARD FLAP LOWER PART INBOARD TEE ANGLE CRACKED 1.500 AT XFS.164.000. REMOVED CRACKED TEE ANGLE IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 581-1-8B. INSTALLED NEW TEE ANGLE ON LT OUTBOARD FLAP LOWER PART, AT XFS.164.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030911000592003091100059WP 2003 9 11 DHL2003873563 120030630A572046143901 CLIP DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 NR 2 MAIN TANK SHOWS CLIP ATTACHING STRINGER 9 TO WING UPPER SKIN CRACKED (STA. 22.000, S-9L). REMOVED CRACKED CLIP IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CLIP IN NR 2 MAIN TANK (LT WING), STA 22.000, S-9L IAW SRM 51-1-20D PG9. REFER TO NR 2088 FOR LEAK CHECK 2L74 4F RT4A25 20030911000602003091100060NE 2003 9 11 2003UALA00610 220030803A7230 COMPRESSOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29659UA 27114 ABORTED TAKEOFF DUE TO NR 1 ENGINE COMPRESSOR STALL. AIRCRAFT SURGED ON TAKE OFF AT EPR ABOVE 1.25. SURGE CHECKS FOUND NO DISCREPANCY. EVENT CLASSIFIED AS A GROUP 3 SURGE DUE TO TIP CLEARANCES IN THE HPC. 2L72 4F4 FRTA1NM E24NE 20030911000712003091100071WP 2003 9 11 DHL2003873573 120030701A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING OTBD FLAP LOWER AFT PLATING SHOWS DENTS DAMAGE, CUT OUT AND TERIM REPAIR BETWEEN STA XF.415.000 AMD XW.408.000 (MAJOR REPAIR) PERFORMED MAJOR REPAIR IAW EODHL-030616, ED-3430. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-030616, ED-3430. CLEANED, TREATED AND PRIMED THE NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED THE NEW SKIN PANEL ON RT WING OTBD FLAP LWR AFT PLATING (STA. XF.415.000 - XW.408.000) USING NEW FASTENERS IAW EODHL-030616, ED-3430, SRM 51-1-21 PG 1, SRM 51-1-21A PG 3. 2L74 4F RT4A25 20030911000762003091100076WP 2003 9 11 DHL2003873527 120030621A5311 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FWD CARGO COMPT FRAME DOUBLER CORRODED STA 160.000 L26R. REMOVED FASTENERS AND DOUBLER IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1F. HEAT TREATED IAW SRM 51-1-1 PG 11. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F4 FRT4A25 E2GL 20030911000812003091100081WP 2003 9 11 DHL2003873544 120030624A5347S4889036 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT NR 2 TRACK LUG WORN,( STA.1570.000-STA.1590.000) REMOVED NR 2 TRACK DAMAGED SECTION IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT WITH NEW FASTENERS IAW SRM 51-3-0 PG 1. 2L74 4F4 FRT4A25 E2GL 20030911000862003091100086WP 2003 9 11 DHL2003873540 120030627A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OTBD L/E FORMER CRACKED AT XFS.735.000. REMOVED FASTENTERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT XFS.735.000 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON LT OTBD L/E FORMER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911000892003091100089WP 2003 9 11 DHL2003873558 120030626A5522 SKIN DOUG DC8 DC873F 302199FWP LT ELEVATOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT ELEVATOR UPPER SKIN IB SECTION HAS INTERIM REPAIR AND CORROSION FROM STA XAR.0.000 TO XE.132.000. REMOVED FASTENERS AND THE DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL. CLEANED,TREATED AND PRIMED THE NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED NEW SKIN PANEL ON LT ELEVATOR UPPER SKIN IB SECTION USING NEW FASTENERS IAW EODHL-030611, ED3460, SRM 51-1-21 PG 1. SEE N/R 2156 FOR REBALANCING. SEE J/C BX3H55074 FOR ELEVATOR REMOVAL AND REINSTALLATION. 2L74 4F RT4A25 20030911000942003091100094WP 2003 9 11 DHL2003873501 120030612A534736575031 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ 46091 FLIGHT COMPT F/E FWD SEAT TRACK SHOWS HOLES ELONGATED. REMOVED AND REPLACED F/E FWD SEAT TRACK (FLIGHT COMPT) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030911001142003091100114WP 2003 9 11 DHL2003873503 120030612A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING CENTER LE FORMER CRACKED 0.250 AT XFS 297.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9,10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001182003091100118WP 2003 9 11 DHL2003873543 120030624A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FWD CARGO CMPT PRESSURE BULKHEAD INTERCOSTAL CRACKED (1.000) STA 640.000 RBL 41. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001402003091100140CE 2003 9 11 DXTA200300071 120030718A3150 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE NR 1 ENGINE ILLUMINATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07872QS 258472 NR 1 ENGINE FUEL LIGHT CAME ON WHEN TAKEOFF POWER APPLIED, LIGHT EXTINGUISHED WHEN POWER REDUCED AT APPROX. 20 KNOTS. ABORTED TAKEOFF. - INSPECTED LT ENGINE FUEL FILTER FOR BLOCKAGE / FOD, NONE WAS FOUND. REINSTALLED FILTER IAW 731 MM CH. 73-21-02. RAN ENGINE COULD NOT DUPLICATE, NO DISCREPANCIES NOTED. 2L72 4F RTA3EU 20030911001442003091100144WP 2003 9 11 DHL2003873619 120030618A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT NR 5 TRACK PLUG LUG WORN AT STA 1315.000. REMOVED DAMAGED PLUG AND CHANNEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG CHANNEL TO TRACK NR 5 AT STA 1315.000 IAW SRM 51-3-0 PG 1. 2L74 4F4 FRT4A25 E2GL 20030911001502003091100150WP 2003 9 11 AALA20030330 120030311A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21567AM 53293 FOUND RIGHT CUSP WEB CRACKED AT STATION 788-800 AND STATION 804. INTALLED NEW CUSP WEB FROM STATION 788-807 RIGHT PER SRM 53-05-00. (M) 2L72 4F RTA6WE 20030911001742003091100174WP 2003 9 11 DHL2003873599 120030707A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 NLG W/W AFT JAMB SKIN CRACKED .250 AT STA FS.8.000 L33R. PERFORMED MAJOR REPAIR IAW EODHL-030623, ED-3439. REMOVED EXISTING REPAIR DBLR, FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030623, ED-3439. PERFORMED NDT INSP IAW NDT SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FAB A REPAIR DBLR A FILLER IAW EODHL-030623, ED-3439. CLEANED, TREATED, PRIMED REPAIR DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11. INSTALL FILLER AND DBLR ON NLG W/W AFT JAMB SKIN (STA. FS 8.000, L-33R) USING NEW FASTENERS IAW EODHL 030623, ED-3439, SRM 51-1-21 AND SRM 51-1-20D. 2L74 4F RT4A25 20030911001792003091100179NM 2003 9 11 DHL2003782007 120030722A2611774001 SMOKE DETECTOR BOEING727 727227 1384078NM CARGO BAY MALFUNCTIONED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01782DH 21998 NR 6 MAIN CARGO SMOKE DETECTOR ILLUMINATED AT FL 310, PREFORMED EMERGENCY CHEK LIST AND LANDED AT MDT. REMOVED AND REPLACED NR 6 MAIN CARGO COMPARTMENT SMOKE DETECTOR, OPS CHK GOOD IAW M/M 26-17-0. 2L73 4F A3WE 20030911001922003091100192WP 2003 9 11 AALA20030342 120030225A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND CORROSION ON SEAT TRACK NR 1. BLENDED AND ROUTED OUT CORROSION AND TREATED AND PRIMED INSTALLED PLUG REPAIR PER 53-05-00 AND AARD 53-20-00-10 AND POINTED. (M) 2L72 4F A6WE 20030911002082003091100208WP 2003 9 11 AALA20030344 120030305A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE BULGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND MINOR BULGE APPROX .25 INCH DIAMETER 2 FEET FORWARD OF GROUND ELECT PANEL, FS 82. DYE CHECKED REPAIRED BULGE WITH DOUBLER PER SRM 53-04-00 FIG 38 SHEET 20. (M) 2L72 4F A6WE 20030910001332003091000133NM 2003 9 10 03FDEA01326 120030815A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 KEEL BEAM (STR 29R OUTBD FLANGE) IS CORRODED BEYOND LIMITS. REPAIRED RT KEEL BEAM OUTBD FLANGE AT BS 950F-970 PER SR 27-53-023A. 2L73 4F RTA3WE 20030910001422003091000142NM 2003 9 10 MWEA030332 120030827A523059101419 PAN DOUG MD88 MD88 3023688NM CARGO DOOR GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FORWARD PIT DOOR AFT EDGE OF INNER DOOR PAN GOUGED NEAR AFT LATCH. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030911000392003091100039NM 2003 9 11 UPS03641142 120030822A5712114T25032 RIB BOEING767 76734AF 1385212NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01323UP 27749 INSPECTION TYPE:C3 NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IS CRACKED ON FORWARD FLANGE. REPAIRED NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IAW GOODRICH ER NR 03-3162 2L72 4F RTA1NM 20030911000502003091100050WP 2003 9 11 DHL2003873560 120030703A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING OUTB L/E UPPER SKIN CORRODED AT STA XFS.90.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG.38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-3-0 PG 1. REMOVED CORROSION FROM UPPER SURFACE OF RH WING OUTBD L/E SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. CUT OUT CORRODED AREA IAW SRM 57-2-1 FIG 38. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS FOR RT WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20030911000652003091100065WP 2003 9 11 UPS03841103 120030812A5230 DOOR DOUG DC8 DC871F 302199DWP MAIN CARGO OUT OF ADJUST A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01750UP 45950 ON CLIMB THRU 26,000 THE MAIN CARGO DOOR SYSTEM "A" LIGHT ILLUM. THE SENSORS MUNE ON ACARS POPPED UP INDICATING MAIN CARGO DOOR OPEN. ABOU T 20 SECONDS LATER TWO BANGS WITH ACCOMPANING YAW. A/C PRESS STARTED T O CLIMB. SLOWED A/C AND STARTED DESCENT. ON FINAL APPROACH ALL THE IN DICATOR LIGHTS WENT OUT. REMOVED AND REPLACED 51-256 DOOR SWITCH IAW UPS DC8 M.M. 32-70-00. PRESSURIZED A/C UP TO 8.2 PSI IAW UPS DC8 M.M. 21-10-00. MCD "A" SYS LIGHT DID NOT ILLUMINATE AND OPS CHECKED GOOD IAW UPS DC8 M.M. 52-70-00. N/R 632638 2L74 4F RT4A25 20030911001002003091100100WP 2003 9 11 DHL2003873526 120030617A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING CTR LE UPPER PLATING CORRODED, XS.466.651 - XS.442.115. PERFORMED MAJOR REPAIR IAW SRM 567-1-0 PG 1, SRM 57-3-30 PG 14, FIG 5. REMOVED CORROSION FROM CTR LE UPPER PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. REMOVED CORRODED PLATING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW PLATING IAW SRM 57-3-3 PG 14, FIG 5. CLEANED, TREATED AND PRIMED NEW PLATING INNER PART IAW SRM 51-1-8B. INSTALLED NEW PLATING ON LT WING CTR LE XFS.422.000 - XW.408.000 IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. FOR REMOVAL AND REINSTALLATION OF CTR LE SEE N/R 0903 2L74 4F RT4A25 20030911001312003091100131WP 2003 9 11 UPS03841033 120030705A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, AFT ACCESSORY COMPT AT STA 1650 LT SIDE L23L IS CRACK AND CORROSION. REMOVED EXT REPAIR DOUBLER, FASTENERS AND DAMAGED LONG 23L FROM 1610 TO 1690. LOCATED & DRILLED NEW SPLICE & NEW LONGERON SECTION IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON SECTION, SPLICE AND EXT DOUBLER IAW DC8 SRM 51-1-21 & 51-1-20D. FAB FLOORBOARD SPLICE AND INSTALLED IAW DC8 SRM 53-2-3 & 51-3-0. 2L74 4F RT4A25 20030911001452003091100145WP 2003 9 11 DHL2003873620 120030701A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT NR 6 TRACK LUGS WORN AT STA 1306.000. CUT OUT NR 6 TRACK DAMAGED AREA IAW SRM 53-2-3 PG 17-18, SRM 51-3-0 PG 1. CLEANED,TREATED, AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG AND CHANNEL IAW SRM 53-2-3 PG 17-18, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030911001752003091100175WP 2003 9 11 DHL2003873605 120030704A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FUSELAGE EXTERIOR NOSE SECTION SKIN LAP JOINT BROKEN .250 STA. -165.000, L-1. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1D SHEET 3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 FIG 1D SHEET 3. FABRICATED FILLER AND DOUBLER IAW SRM 53-2-0 FIG 1D, SHEET 3. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 53-2-0 FIG 1D SHEET , SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911002142003091100214NM 2003 9 11 DHL2003754014 120030806A33501000679 BATTERY BOEING727 727223 1384074NM COCKPIT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. INSTALLED SERVICEABLE BATTERIES IN BOTH COCKPIT AND CREW DOOR EMERGENCY EXIT SIGNS. OPS CHECKED GOOD. WORK DONE IAW B-727 M/M 33-50-71. 2L73 4F A3WE 20030911002192003091100219EU 2003 9 11 DHL2003364012 120030814A2560 SMOKE BARRIER AIRBUS300 A300B4203 3930306EU CABIN DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 SMOKE BARRIER HAS 1 SMALL HOLE AND (L) FRAYED AREAS ON BOTTOM BY RAIL REPAIRED HOLE AND FRAY AREA AS REQUIRED IAW SMR REPORT NR 92-33-024 PARA 4.1.1.9.2.2 2L72 4F RTA35EU 20030911002372003091100237WP 2003 9 11 DHL2003604568 120030523A5514 ANGLE DOUG DC8 DC873F 302199FWP HORIZ STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT HORIZ STAB INNER ANGLE CRACKED 1.000 AT XFS.30.500. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE IAW SRM 55-1-0 PG 1. PERFORMED HEAT TREATMENT TO NEW ANGLE IAW SRM 51-1-1 PG 11,13. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030912000062003091200006 2003 9 12 2003UALA00606 420030801A3442066500080407 TRANSCEIVER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE WX RADAR SYS FAILED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29353UA 24321 AIRCRAFT DIVERTED ENROUTE WHEN WEATHER RADAR FAILED. TRANSCEIVER FAILED. REMOVED AND REPLACED TRANSCEIVER. FAILURE WAS CONFIRMED IN THE SHOP AS AN ANTENNA DRIVE FAILURE. 2L72 4F4 FRTA16WE E2GL 20030912000072003091200007NE 2003 9 12 DXTA200300093 220030818A7200PW305B ENGINE BRAERO1000 BAE1251000A 1500104EU PWA 305 PW305B 52128NE NR 2 FAILED E DXTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL07533QS5599 259033 PCE305010 ON SHORT FINAL WITH A REDUCTION IN POWER NR 2 ENG FAILED AND MASTER CAUTION ILLUMINATED. OIL PRESSURE CAUTION LIGHT CAME ON NOTICED OIL PRESSURE GAUGE READ 10 PSI, ENGINE SHUTDOWN UNCOMMANDED. - REMOVED RT THROTTLE RDVT AND INSTALLED A NEW RDVT AND RIGGED IAW HAWKER 1000 MM CHAPTER 76-10-00 USING THRUST LEVER TEST SET. ACCOMPLISHED SATISFACTORY ENGINE OPERATIONAL GROUND CHECK IAW HAWKER 1000 MM CHAPTER 71-00-00. 2L72 4F4 FRTA3EU E35NE 20030912000682003091200068WP 2003 9 12 DHL2003604783 120030614A5320 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT ACCY COMPT END FITTING CRACKED 1.500, STA 1640.000 - STA 1660.000, L-30R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 43A SHEET 2. REMOVED CRACKED END FITTING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW END FITTING IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 43A. PERFORMED HEAT TREATMENT TO NEW END FITTING IAW SRM 51-1-1, SRM 51-1-4, DPS 1.05-3, DPS 7.00-1. PERFORMED LIQUID PENETRANT INSPECTION IAW NDT SPM PART 08-00-02/06. CLEANED, TREATED AND PRIMED NEW END FITTING IAW SRM 51-1-8B. INSTALLED NEW END FITTING WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000732003091200073WP 2003 9 12 DHL2003604696 120030714A53203750257U1 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD CARGO COMPT SPLICE FITTING CRACKED 2.000 STA 440.000 - 460.000, L-31L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030912000782003091200078NM 2003 9 12 AWXA200300816 120030721A53302024T3063 SKIN BOEING737 73733A 1384673NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 PHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 520, BETWEEN STRINGER 12-13 LT. MAINTENANCE CUT OUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01 FIG 202. 2L72 4F4 FRTA16WE E2GL 20030912000802003091200080NM 2003 9 12 AWXA200300817 120030709A5320D5347112420000 PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR PLATE Y1292, BETWEEN FR 69-70. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SHEAR PLATE Y1292, BETWEEN FR 69-70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 8-10, 12, 21-22, & A24-A27. 2L72 4F RTA28NM 20030910001062003091000106NM 2003 9 10 MWEA030315 120030818A5320993061223 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 AREA OF CORROSION FROM FRAME STATION 1098-1174 OUTBAORD OF NR 6 SEAT TRACK ON SUBFLOOR. 2L72 4F RTA6WE 20030910001282003091000128NM 2003 9 10 MWEA030343 120030827A5347593054744 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CORROSION ON NR 6 SEAT TRACK OUTBOARD FLANGE AT FRAME STATION 484. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2L72 4F RTA6WE 20030910001342003091000134NM 2003 9 10 03FDEA01291 120030806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBOARD FLAP INBOARD HINGE 28 2FC SIDE 29 LOWER OUTBOARD ATTACH HOLE CORRODED AT BORE AND FORWARD 2FAFT FACES. RH OUTBD FLAP INBD HINGE (A/C SIDE) LOWER OUTBD ATTACH HOLE CORRODED AT BORE AND FWD / AFT FACES. RT OUTBD FLAP INBD HINGE ( A/C SIDE ) LOWER OUTBD ATTACH HOLE BORE AND FWD / AFT FACES ( SURFACE ) REPAIRED AS PER CMM 57-44-08 AND DWG ARC0502. 2L73 4F RTA22WE 20030910002032003091000203EU 2003 9 10 MALA030380 120030813A3150 WARNING SYSTEM SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15369PX 340B295 CONFING CWP LIGHT ILLUMINATED DURING TAKEOFF ROLL OF FLIGHT NR 3342. ALL ENGINE INDICATIONS NORMAL. FLAP (0) CONDITION LEVERS MAX, ALL TRIMS IN GREEN ARC, AIRSPEED APPROXIMATELY 110 KNOTS. ABORTED TAKEOFF MININAL BRAKING APPLIED. MAINTENANCE PERFORMED REJECTED TAKE OFF INSPECTION IAW MM SECTION 05-50-00-6 NO DISC NOTED. PERFORMED TEST FLIGHT BY FLIGHT CREW UNABLE TO DUPLICATE CONFIG WARNING CAS. 2L72 4T RTA52EU 20030910002182003091000218EU 2003 9 10 MALA030358 120030704A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING C-CHECK INSPECTION IN CVG, NR 2 SEAT RAIL FROM FRAME 18 TO 20 IS CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED IAW EO NR A53026. REFER 409 NR 128124, TASK CARD NR 0893A FOR DETAIL. A/C RELEASE DATE 7/25/03. 2H74 4F RTA49EU 20030911000402003091100040NM 2003 9 11 DHL2003743012 120030716A2612 DETECTOR BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FIRE WARNING MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01743DH 22438 NR 3 ENGINE DETECTOR CIRCUIT GROUND FAULT LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. DEFERRED IAW MEL 26-9. DMI NR 13565 PLACARD INSTALLED. NR 3 ENGINE DETECTOR CIRCUIT GROUND FAULT LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. DMI NR 13565 REF. ISOLATED DETECTOR ON GEAR BOX AREA. OPS CHECKED GOOD M/M 26-11. THIS CLEARS DMI NR 13565. PLACARD REMOVED. 2L73 4F4 F A3WE E2EA 20030911000742003091100074WP 2003 9 11 DHL2003873546 120030629A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLOT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT INBD WING L/E SLOT SKIN CORRODED, XS.220.000 - XS.250.089. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT CORRODED AREA IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS ON L/E SLOT SKIN, XS.220.000 - XS.250.089 IAW SRM 57-2-1 FIG 38, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030911001322003091100132WP 2003 9 11 DHL2003873551 120030628A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 VERTICAL STAB L/E EXTERNAL SKIN SHOWS INTERIM REPAIR AT ZFS142.250. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17. CLEANED, TREATED AND PRIMED DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED DOUBLER ON L/E EXTERNAL SKIN (VERTICAL STAB.) AT ZFS.142.250 IAW SRM 55-2-1 FIG 4 PG 17, SRM 51-1-21 PG 1. FOR REMOVAL AND REINSTALLATION SEE JC BX3B55076 2L74 4F RT4A25 20030911001382003091100138WP 2003 9 11 DHL2003873596 120030704A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING INBD FLAP UPPER AFT PLATING HAS INTERIM REPAIR AND DENT BETWEEN STA XW.2.000 - XW.91.000. PERFORMED MAJOR REPAIR IAW EODHL-030617, ED-3443. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-030617, ED-3443. CLEANED, TREATED AND PRIMED THE NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON RT WING INBD FLAP UPPER AFT SURFACE (STA.XW.2.000 CANT - XW.91.000) USING NEW FASTENERS IAW EODHL-030617, ED3443 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001462003091100146NM 2003 9 11 2003UALA00613 120030805A335060243 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29340UA 24244 EEL LIGHTS FROM ROW 15 AFT INOPERATIVE REPLACED LAMP FEEDER AND TWO LAMPS. 2L72 4F4 FRTA16WE E2GL 20030911001652003091100165CE 2003 9 11 DXTA200300076 120030801A2120 ODOR CESSNA560 560XL 2076702CE CABIN DETECTED E DXTAO OTHER O OTHER DEDESCENT 1 GL07639QS 5605139 UPON DESCENT STRONG EXHAUST SMELL OF JET FUMES, APU WAS NOT RUNNING AT THE TIME, AND ENVIRONMENTAL SOURCES SHOWED 50 DEGREES. INSPECTED BOTH ENGINE INLETS AND TAILPIPES FOR TRACES OF OIL, NONE FOUND. OPENED LOWER COWLS AND RAN BOTH ENGINES INDIVIDUALLY FOR SEVERAL MINUTES, NO EXTERNAL FUEL OR OIL LEAKAGE WAS OBSERVED, NO UNUSUAL ODORS WERE DETECTED INSIDE THE CABIN COMING FROM THE AIR DISTRIBUTION SYSTEM. OPENED THE WATER SEPARATOR TO CHECK FOR SIGNS OF OIL, NONE FOUND. ALL APPEARS TO BE NORMAL AT THIS TIME. 2L72 4F RTA22CE 20030911001672003091100167WP 2003 9 11 UPS03841029 120030722A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C2, RT WING UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 195 TO XFS 220.190. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO DC8-5720-7767-A AND SRM 57-3-3 FIG 3. 2L74 4F RT4A25 20030911001702003091100170WP 2003 9 11 UPS03841041 120030708A5315 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, MAIN CABIN STA 920 LBL 49 FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. ORIG .340 INCH REMAINING .120 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLES, SHIM FOR ANGLES AND SHIM FOR BLENDED OUT DAMAGE IAW REO G09354. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES AND SHIMS IAW REO G09354 AND SRM DC8 51-3-0. 2L74 4F RT4A25 20030911002022003091100202WP 2003 9 11 AALA20030877 120030515A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21964TW 53614 MCI - FOUND CORROSION ON CARGO FLOOR SUPPORT AT STATION 1155 10 INCHES RBL TOPSIDE AND LOWER SIDE. CORRODED FLOOR SUPPORT WAS REPLACED WITH NEW MPH 5936660-63, PART WAS PRIMED, PAINTED WHITE AND HI-LOCKS WERE INSTALLED PER SRM 51-31-05. (M) 2L72 4F RTA6WE 20030815000082003081500008NM 2003 8 15 AALA20030374 120030327A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21184AN 29594 SJU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT 9D THROUGH 11D INOPERATIVE. INSTALLED AND SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000182003081500018NE 2003 8 15 HEEA088650 220030717A74219550175400 IGNITER SNIAS 350 AS350* EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 ENGINE IGNITER WORN BEYOND LIMITS. TO BE SENT TO VENDOR. 1G71 3U3 U H9EU E19EU 20030815000202003081500020EU 2003 8 15 HEEA088660 120030807A641011731743 BLADE BOLKMS105 BO105S 5626006EU TAIL ROTOR PEELING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TAIL ROTOR BLADE PAINT PEELING. 1G72 3U H3EU 20030815000232003081500023SW 2003 8 15 HEEA088530 120030713A6330 BEARING BELL 206 206L3 1182108SW GEARBOX MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA LK3518 51542 MAIN ROTOR GEARBOX MOUNT HAS WORN BEARINGS. IN SHOP REPAIR. 1G71 3U H2SW 20030820002442003082000244EA 2003 8 20 ASOA03310 120030715A53306013600130 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE DOUBLER IN THE RADIUS AT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPLACED THE DOUBLER IN THE RADIUS AT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 IAW ASA EO 600-53-0075. (M) 2L72 4F RTA21EA 20030821000222003082100022NM 2003 8 21 USAABB03118 120030723A33508731002511REV15 SIGN BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19621AU 27200 CLT - FOUND R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030821000282003082100028NM 2003 8 21 03FDEA00961 120030616A5753ARC0502 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING- O/B FLAP I/B HINGE LOWER O/B STUD BORE AFT SURFACE FOUND CORROSION. AFT SURFACE OF O/B STUD BORE REPAIRED AS PER CMM 57-44-08. WITHIN ALLOWABLE LIMIT AS PER CMM 57-44-08 AT LEFT WING O/B FLAP I/B HINGE. 2L73 4F RTA22WE 20030821000292003082100029EU 2003 8 21 03FDEA00913 120030619A5315 FLOORBEAM AIRBUS300 A300B4605R 3930308EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE 742 FWD CARGO -CROSS BEAM AT FRAME 28 IS CRACKED APPROX 1 INCH LONG 18 INCHES RIGHT OF CENTER. REPAIRED IAW SRM 53-10-15 FIGURE 208 SHEET 3. 2L72 4F RTA35EU 20030821000682003082100068NM 2003 8 21 03FDEA00917 120030617A5313AGA720213 STRINGER DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 AFT CARGO COMPT STRINGER SPLICE BRACKET AT STA 1951 STRINGER 51LT FOUND CRACKED. AFT CARGO COMPARTMENT STA 1951 STRINGER 51LT CRACKED CLIP REMOVED AND NEW CLIP FABRICATED PER DRAWING AGA 3092, SRM 51-35-01 VOL II, SRM 51-33-01 VOL II AND REFER TO FEDEX EA 1-5310-71724, FUSELAGE- MAINFRAME- TRACKING OF B TYPE REPAIR ON FRAME. 2L73 4F RTA22WE 20030821001242003082100124NM 2003 8 21 03FDEA00875 120030614A5610 WINDSHIELD DOUG MD11 MD11 3023602NM COCKPIT CRACKED A FDEAA UNSCHED LANDING O OTHER CRCRUISE 1 SO25595FE 48553 CAPT'S WINDSHIELD CRACKED. 2L73 4F RTA22WE 20030821001762003082100176NM 2003 8 21 03FDEA01319 120030815A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 CORROSION (C53-224-02) ON FLOORBEAM AT BS 480, RBL 3 - RBL 10, WL 207.9 ON LOWER SIDE OF TOP FLANGE. CORROSION OUT OF LIMITS. REPLACED FLOORBEAM UPPER CHORD BS 480, LBL 38 - RBL 65, WL 207.9 IAW FED EX EA 7-5310-72538. 2L73 4F RTA3WE 20030821002882003082100288EU 2003 8 21 YENA200315 120030715A335010335140004 BATTERY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A YENAK NONE L NO TEST DEDESCENT 1 EA15565JB221 2031 EMERGENCY EXIT SIGNS AT AFT INOPERATIVE. REMOVED AND REPLACED BATTERY IN EPSU FIN NR 13W IAW AMM 33-51-38, OPS. CHECK OK. 2L72 4F RTA28NM 20030822001392003082200139NM 2003 8 22 CALA0300443 120030806A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 334, LBL 45. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030822001402003082200140NM 2003 8 22 CALA0300444 120030806A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO COMPARTMENT FORWARD BULKHEAD PANEL SUPPORT LOWER SECTION ANGLE APPROXIMATELY 8 INCHES ABOVE CARGO FLOOR SURFACE. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20030822001422003082200142NM 2003 8 22 C1HA200381017 120030805A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON SEAT TRACK LBL 24 IN NUMEROUS LOCATIONS BETWEEN FS 958 AND FS 1130. 2L73 4F A3WE 20030911002032003091100203NM 2003 9 11 AALA20030863 120030806A5414 SKIN BOEING767 767323 1385205NM NR 2 PYLON CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2139365 24046 AFW - FOUND NR 2 ENGINE INBOARD SIDE PYLON TORQUE BOX AREA FOUND CRACK EXTENDING FROM ACCESS HOLE AFT. DAMAGED SKIN AREA REMOVED REPAIRED PER SRM REPAIR 54-52-01-2. (M) 2L72 4F RTA1NM 20030911002262003091100226NM 2003 9 11 DHL2003746012 120030821A3350 LIGHT BOEING727 727224 1384076NM CABIN MALFUNCTIONED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01746DH 22252 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY REMAINS ILLUMINATED WITH EMERGENCY EXIT LIGHT OFF OR ARMED. FOUND THE NO SMOKING LIGHT SWITCH IN THE ON POSITION. TURNED SWITCH OFF, LIGHTS EXTINGUISHED PER M/M 33-50-06. 2L73 4F A3WE 20030912000372003091200037WP 2003 9 12 DHL2003604532 120030430A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING OTBD L/E FORMER CRACKED 0.250 STA XFS 59.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, 51-2-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000762003091200076NM 2003 9 12 AWXA200300814 120030718A2497D95401005000AC WIRE HARNESS AIRBUSA319 A319132 3930340NM ELECTRICAL SYS ARCED A AWXAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 WP28819AW 1395 FLT 0002 -AT CRUISE RECEIVED MASTER CAUTION AND ECAM MSG FOR BLUE HYD SYS LOW PRESS, NOSE WHEEL STEERING (NWS), AVIONICS VENT FAULT, PRIMARY FLT DISPLAY (PFD), NAV DISPLAY (ND), FREQ CNTRL UNIT (FCU), GEN NR 1, BTRY NR 2, CABIN LIGHTS. DECLARED EMER AND DIVERTED, MAINT FOUND AVIONICS VENT BLWR FAN CB (AD10) TRIPPED, RESET, PERFORMED AMM TASK 21-26-00-71-001, AVIONICS EQUIP VENT TEST WAS GOOD. UPON ENGINE START THE CAPT PFD, ND, AND FCU CYCLED ON THEN OFF SEVERAL TIMES, AND ECAM MSG RETURNED FOR BLUE HYD SYS LOW PRESS AND NWS; MEL 24-20-01, COND. 2, "NR 1 IDG INOP". MAINT FOUND IDG FEEDER CBL PIN "C" WITH ARC DAMAGE. REMOVED AND REPLACED IDG FEEDER CABLES (400VCI) IAW 24-21-43, PG. 401, OPS CHECK WAS GOOD. 2L72 4F RTA28NM 20030912001062003091200106NM 2003 9 12 AWXA200300864 120030712A5320654659221 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT BS 859, RBL 3, WL 158. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT CHANNEL FROM BS 857 TO BS 861, RBL 3 TO RBL 4; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG 201-203, FIG 201. 2L72 4F RTA16WE 20030912001142003091200114NM 2003 9 12 AWXA200300881 120030723A553165C27446 RIB BOEING737 7373G7 1384595NM VERTICAL STAB CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK THE FORWARD VERTICAL STABILIZER LT AND RT RIB ASSEMBLIES HAVE CHAFED AREAS AT BS 1006. MAINTENANCE REMOVED VERTICAL STABILIZER LT AND RT RIB ASSEMBLIES; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG 1, PG 1-5. 2L72 4F RTA16WE 20030912001162003091200116NM 2003 9 12 AWXA200300884 120030806A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 PHX - EEL - EMERGENCY ESCAPE PATH LIGHT BROKEN SEAT ROW 23 LT. MAINTENANCE REMOVED AND REPLACED ESCAPE PATH LIGHT ASSEMBLY AND REPAIRED BROKEN WIRE AT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030912001242003091200124NM 2003 9 12 AWXA200300891 120030724A5310693535214 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .375 INCH CRACK WAS FOUND ON SHEAR TIE AT BS 727A, STR 10 RT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 727A, STR 10 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1-4. 2L72 4F RTA16WE 20030912001262003091200126EU 2003 9 12 AWXA200300893 120030807A2560P4010021 BATTERY AIRBUS320 A320231 3930325EU FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28620AW 052 PHX - EEL - EMERGENCY FLASHLIGHT AT AFT NR 3 FLIGHT ATTENDANT STATION IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY AT THE AFT NR 3 FLIGHT ATTENDANT STATION, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030912001352003091200135NM 2003 9 12 AWXA200300897 120030711A5311651630087 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK A .5000 INCH CRACK WAS FOUND ON BS 178 BULKHEAD RT SIDE CHORD JUST ABOVE WL 207. MAINTENANCE REMOVED BS 178 BULKHEAD RT SIDE CHORD AT WL 207; FABRICATED A NEW REPLACEMENT SIDE CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8, PG 3, 10, & 38. 2L72 4F RTA16WE 20030924000832003092400083NM 2003 9 24 QXEA200301021 120030814A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 DENT IN LT SIDE OF FUSELAGE JUST AFT OF ICE SHIELD AT STATION X333.000. DENT IN FIVE INCHES FROM WINDOW OPENING. REPAIRED IAW DHC-8 RD 8-53-5384, SRM 51-00-05 AND HORIZON AIR EA 2-53-466. 2H72 4T RTA13NM 20030924001432003092400143 2003 9 24 AALA20030633 420030603A22102VA3925G1 ACTUATOR AIRBUS300 A300B4605R 3930308EU YAW DAMPER MALFUNCTIONED A AALAK NONE O OTHER ININSP/MAINT 1 SW2114065 508 WHEN YAW DAMP NR 1 IS ENGAGED, RUDDER MOVES RAPIDLY TO THE LT AND REMAINS IN THAT POSITION UNTIL ITS DISARM/DISENGAGED. REPLACED YAW DAMP NR 1 ACTUATOR AND LEAK, OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA35EU 20030925000072003092500007NM 2003 9 25 USAABB03137 120030817A33509221009 BATTERY BOEING757 7572B7 1384964NM L1 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 FOUND L1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030925000632003092500063WP 2003 9 25 AALA20030897 120030824A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21487AA 49680 DURING OVERNIGHT MAINTENANCE, WHEN BATTERY MASTER WAS PLACED IN OFF POSITION OR EMERGENCY LIGHT SWITCH WAS PLACED IN THE ARM POSTION THE COCKPIT, FORWARD ENTRY, SERVICE ENTRY AND STATION 213 EMERGENCY LIGHTS CAME ON. REPLACED BATTEYR PACK AT B5 23. SYSTEM GROUND CHECKED NORMAL OPERAITON. (M) 2L72 4F A6WE 20030925000842003092500084WP 2003 9 25 I5HA0358004 120030904A7933232N90 SENSOR CVAC 580 580 2422806WP RT ENG OIL TEMP MALFUNCTIONED A I5HAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL23581PA 29 DURING CLIMB-OUT, RT OIL TEMP ROSE TO APPROX 95 DEGREES CENT. ABLE TO CONTROL TEMP MANUALLY AT 85 DEGREES. OIL TEMP REMAINED IN 80 TO 85 RANGE UNTIL DESCENT. DURING DESCENT, OIL TEMP BEGAN CLIMBING & WAS NOT CONTROLLABLE IN MANUAL OR AUTOMATIC MODE. AT 95 DEGREES & CLIMBING, ELECTED A PRECAUTIONARY ENG SHUTDOWN. OIL PRESS NORMAL DURING HIGH OIL TEMP CONDITIONS. ENG RESTARTED ON GRND FOR TROUBLESHOOTING. ENG OIL TEMP STARTED CLIMING & WAS NOT CONTROLLABLE IN MANUAL OR AUTOMATIC MODES EVEN THOUGH OIL COOLER DOOR & INDUCER VALVE OPERATING NORMALLY. NO CHANGE IN OIL PRESSURE. R & R OIL TEMP SENSOR, ASSOCIATED CONNECTOR & OIL COOLER. GROUND RUN SUCCESSFUL & AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RT 20030926000282003092600028NM 2003 9 26 AWXA200300991 120030821A5320654147314 INTERCOSTAL BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 3 INCH CRACK WAS FOUND ON UPPER FLANGE OF INTERCOSTAL (BAFFLE) AT BS 440-460, OUTBOARD OF STR 26 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL FROM BS 440 TO BS 460; FABRICATED A NEW REPLACEMENT INTERCOASTAL PER DWG 65-41473; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-30-02, PG. 1, FIG. 7. 2L72 4F RTA16WE 20030926000472003092600047NM 2003 9 26 0301636642 120030826A3350 BATTERY PACK BOEING747 747212B 1384886NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01642NW 21942 DURING LINE CHECK, FOUND 'B' ZONE LEFT FLOOR PATH EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030926000522003092600052EA 2003 9 26 COMA0360380 120030826A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILER ILLUMINATED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01491CA 7756 FLIGHT 5831 FLIGHT SPOILER AND GROUND SPOILER FAULT MESSAGE. RESET SYSTEM, OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA21EA 20030926000712003092600071 2003 9 26 MTNA20035 420030825A8300601011141 CLAMP FOKKERF27 F27MK500 4990629EU GEARBOX OIL LOOSE A MTNAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO33709FE 10375 ON DESCENT INTO KIN THE LT GEARBOX OIL LIGHT CAME ON. THE EMERGENCY CHECK LIST WAS ACCOMPLISHED AND THE ENGINE SHUT DOWN. AN EMERGENCY WAS DECLARED WITH ATC. THE AIRCRAFT LANDED WITH OUT ANY OTHER INCIDENT. MAINTENANCE TROUBLESHOT THE PROBLEM AND FOUND A CLAMP LOOSE ON THE COMPRESSOR. THE MECHANIC REMOVED, INSPECTED AND REINSTALLED THE COMPRESSOR. THE SYSTEM CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T A817 20030926000762003092600076NM 2003 9 26 03FDEA01388 120030826A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 FWD CARGO BAY, DENT IN FRAME, BS 500, AT STR 24L. REMOVED, REPLACED AND INSTALLED FRAME SECTION BS 500 AT STR 21L TO STR 25L. ALL WORK DONE IAW SRM 51-30-5, SRM 51-30-2, SRM 51-10-2 AND MM 51-20-151-7 PG 1. 2L73 4F RTA3WE 20030926001112003092600111NM 2003 9 26 2003UALA00644 120030821A5320 FLOOR SUPPORT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 MAIN CABIN RT SIDE STA 330 RBL 60 FLOOR SUPPORT CORROSION BLEND OUT BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED, INSTALLED FLOOR SUPPORT. 2L72 4F4 FRTA16WE E2GL 20030926001562003092600156NM 2003 9 26 HNAA0300042 120030830A3397 WIRE DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHTSBROKEN A HNAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA07966HA 452 CREW REPORTED FLOOR EMERGENCY LIGHTS AT ROWS 5 AND 6 WERE INOPERATIVE REPAIRED BROKEN WIRE GOING TO EMERGENCY LIGHTS. 2H72 4T RTA13NM 20030929000482003092900048NM 2003 9 29 03FDEA01408 120030903A3260UNK SWITCH BOEING727 727100 1384036NM NLG FALSE INDICATIONA FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25107FE 19202 NOSE GEAR DID NOT INDICATE SAFE AFTER PLACING LANDING GEAR HANDLE DOWN. CYCLED LANDING GEAR LEVER. NOSE GEAR INDICATED SAFE AFTER APPROX 10 - 15 SEC. RED UNSAFE WAS NOT ILLUMINATED. REMOVED AND REPLACED SWITCHES S93 AND S96 IAW M/M 32-61-021-4. OPS CK GOOD. 2L73 4F RTA3WE 20030929000732003092900073NM 2003 9 29 03FDEA01439 120030904A3260656021123 ACCESSORY UNIT BOEING727 727200 138407ENM E&E BAY FALSE ACTIVATIONA FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25216FE 22937 DURING CONFIGURATION TO LAND AFTER PLACING LANDING GEAR LEVER DOWN ALL LIGHTS REMAINED ILLUMINATED ON GEAR ANNUNCIATOR PANEL, REDS AND GREENS. RECYCLED GEAR IAW QRH AND AGAIN ALL LIGHTS REMAINED ILLUMINATED. RECYCLED AGAIN AND GOT A SAFE 3 GREEN INDICATION AND LANDED UNEVENTFULLY. TROUBLESHOT PER MM 32-61-001-1, NEEDS LANDING GEAR ACCESSORY UNIT P/N 65-60211-23 NIS GTF/LINE. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER FEDEX 727-200 M/M 32-09-121-4. PERFORMED TEST OF LANDING GEAR ACCESSORY UNIT PER FEDEX 727-200 M/M 32-09-122-5. TEST CHECKS GOOD. 2L73 4F RTA3WE 20030929000752003092900075NM 2003 9 29 03FDEA01444 120030830A5754 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER BORE FOUND CORRODED. 2L73 4F RTA22WE 20030929000782003092900078NM 2003 9 29 03FDEA01449 120030901A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING I/B FLAP O/B HINGE (FLAP SIDE) LOWER O/B BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE) LOWER O/B BORE (PIVOT HOLE) CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-72651 TITLE : WINGS - TRAILING EDGE DEVICES - RT I/B FLAP O/B AFT HINGE PIVOT BORE CORROSION. 2L73 4F RTA22WE 20030929000822003092900082NM 2003 9 29 CALA0300512 120030903A3397BR963180 WIRE HARNESS BOEING737 737524 1384721NM ROW 12ABC BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2714609 27322 INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 12ABC DUE TO A BROKEN WIRE. THE EMERGENCY ESCAPE PATH LIGHTING WIRE HARNESS WAS REPLACED. OPERATION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS RESTORED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-81. 2L72 4F RTA16WE 20030929000862003092900086WP 2003 9 29 0301679997 120030903A2120 DUCT DOUG DC9 DC931 3022065WP LT HEAT EXCHANGESEPARATED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL018933E 47142 AIRCRAFT LOST CABIN PRESSURIZATION AT FL 290 AND THE CABIN STARTED DESCENDING AT 1000 FPM. CREW VERIFIED THE OUTFLOW VALVE WAS FULLY CLOSED AND NOTED THAT BOTH ENGINE AND AIRFOIL ANTI-ICE WERE ON. DUCT PRESSURES AND TEMPERATURES WERE NORMAL. COM PROCEDURES FOR EMERGENCY DESCENT COMPLIED WITH AND CABIN PRESSURE CONTROL WAS REGAINED AT 14,000 FEET. CABIN O2 MASKS DID NOT DEPLOY. FLIGHT DIVERTED TO TYS AND AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED A BITE OF THE PRESS CONTROLLER AND NO CODES WERE DISPLAYED. A DUCT FROM THE LEFT PACK CONTROL VALVE AND HEAT EXCHANGER WAS FOUND TO BE SEPARATED AND WAS REPLACED WITH NEW PERI-SEALS. LEAK CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030929000902003092900090WP 2003 9 29 UPS03841159 120030825A5754 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, RT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030929000942003092900094WP 2003 9 29 UPS03841163 120030825A5511 RIB DOUG DC8 DC873F 302199FWP RT STAB LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, RT HORIZONTAL STAB. LEADING EDGE RIB IS CRACKED AT XFS 116.25 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATED CRACK,FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2 2L74 4F RT4A25 20030929000962003092900096WP 2003 9 29 UPS03841165 120030826A55104651609 FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, LT HORIZONTAL STAB O/B TIP INTERNAL REAR SPAR ANGLE FITTING IS CRACKED AT XE 312.5 REMOVED,FABRICATED AND REPLACED FITTING I.A.W. DWG. 5640789 AND SRM 51-1-20D,51-3-0,AND DWG. 4651609 2L74 4F RT4A25 20030929001062003092900106NM 2003 9 29 AWXA200301021 120030812A53156545410391 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK .875 INCH CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM AT BS 644, LBL 45. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 694, LBL 45; FABRICATED A FILLER AND 3 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-04 FIG 1 PG 1. 2L72 4F RTA16WE 20030929001082003092900108NM 2003 9 29 AWXA200301024 120030815A5753657192666 SKIN BOEING737 737277 1384570NM RT WING TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 MCN - MAJOR REPAIR - DURING C-16 CHECK THE RT OUTBOARD HINGED FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED ALONG EDGE. MAINTENANCE PERFORMED HONEYCOMB REPAIR ON TRAILING EDGE WEDGE OF RT OUTBOARD HINGED FLAP IAW B737-200 SRM 51-40-20 FIG 10 PG 40-41. 2L72 4F RTA16WE 20030929001112003092900111EA 2003 9 29 QXEA200301059 120030905A5210 STRUT CNDAIRCL600 CL6002C10 1390015EA ZONE 800 OUT OF ADJUST A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09606QX 10023 ON FLIGHT 2528 MAIN CABIN DOOR WILL NOT OPEN. ADJUSTED COUNTER BALANCE FORWARD GAS STRUT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030929001232003092900123NM 2003 9 29 HNAA0300046 120030908A533085530199 SKIN DHAV DHC8 DHC8102 2809003NM FUSELAGE DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07906HA4876848768 9 DURING C CHECK, CONTACT FROM PERSONNEL LIFT CAUSED GOUGE AND DENT. 2H72 4T RTA13NM 20030929001272003092900127WP 2003 9 29 03FDEA01456 120030907A2750ARB0393501 BOLT DOUG MD10 MD1010F WP ZONE 500 INACCURATE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 WINGS-RIBS AND BULKHEADS-LT OUTBOARD FLAP HINGE STUD BOLT SUBSTITUTION. COMPLIED WITH E.A.8-5710-72287. WINGS-RIBS AND BKHDS- FLAP HINGE STUD BOLT SUBSTITUTION. 2L73 4F RTA22WE 20030929001282003092900128WP 2003 9 29 03FDEA01455 120030907A2750ARC2177 ARM DOUG MD10 MD1010F WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 WINGS-OUTBOARD FLAP REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177. COMPLIED WITH E.A. 8-5740-72289. WINGS-OUTBD FLAPS REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177. 2L73 4F RTA22WE 20030929001392003092900139EU 2003 9 29 IXXA0300057O 220030903A72009026M70G01 ENGINE DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C 13802EU NR 3 FLAMED OUT A IXXAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SW11828BX3502062 45993 AFTER LEVEL OFF AT CRUISE ALTITUDE FROM KTOL NR3 ENGINE FLAMED OUT. CREW COMPLIED WITH CFM-56 FLAME OUT/INFLIGHT START CHECKLIST AND HAD A SUCCESSFUL RESTART WITH NO FURTHER PROBLEMS NOTED. AIRCRAFT RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ONGOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE PERFORMED FLAMEOUT INSPECTION IAW CFM MM 71-00-00. THEY REMOVED AND REPLACED FUEL FILTER IAW CFM MM 73. ENGINE WAS RUN AT TAKEOFF POWER IAW ATI ERH 70.01 TABLE 91.01.4 SUMPED TANK AND NO DEFECTS NOTED. OPERATIONAL CHECK GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20030929001442003092900144NM 2003 9 29 QXEA200301062 120030904A215078279018 ACM DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09364PH9528 36 524 ON FLIGHT 2115 SMOKE IN COCKPIT AND CABIN AFTER NO.2 BLEED SELECTED ON. REMOVED AND REPLACED ACM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930000042003093000004EA 2003 9 30 QXEA200301064 120030907A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 FORWARD CARGO BAY CHIMNEY ABOVE DOOR HAS A TORN SCREEN. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20030930000082003093000008EU 2003 9 30 AWXA200301027 120030907A2910 HYDRAULIC SYSTEM AIRBUS320 A320231 3930325EU YELLOW LOW A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28620AW 052 AIR TURN BACK-FLT 0459-AFTER T/O, EN ROUTE, RECD ECAM YELLOW AND GREEN HYD SYS LOW PRESS IND, TURNED BACK AND LANDED. MAINT PWR UP YELLOW, GREEN HYD SYS, NO ECAM WARNING PRESENT, FOUND QTY LEVELS OF BOTH SYS LOW, BUT ABOVE MIN GAUGE LEVEL (GAUGE AND ECAM QTY LEVELS MATCH). REPORT IND YELLOW AND GREEN ENG DRIVEN PUMPS (EDP) WERE SELECTED TO OFF AFTER LOW PRESS IND WERE DISPLAYED. INSP ENG NR 1 (GREEN) AND ENG NR 2 (YELLOW) HYD HIGH PRESS BYPASS IND PINS, HYD CTRL UNIT BYPASS IND PIN, AND EDP BYPASS IND PINS, NO PINS WERE EXTENDED. CKD GREEN, YELLOW, AND BLUE HYD SYS HEAD PRESS, ALL READ (76 PSI) WITHIN LIMITS. SERVICED YELLOW AND GREEN SYS HYDR AND PERFORMED ENG RUN, QTY AND PRES WERE CORRECT. NO LEAKS NOTED.2L72 4F RTA28NM 20030930000162003093000016NM 2003 9 30 QXEA200301069 120030906A3150 WARNING SYSTEM DHAV DHC8 DHC8202 2809007NM ZONE 300 ACTIVATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09361PH 516 ON FLIGHT 2041 ABORTED TAKEOFF DUE TO TAKEOFF WARNING AT 85 KNOTS. THE WARNING STOPPED BRIEFLY, BUT AT 90 KNOTS TAKEOFF WARNING SOUNDED AGAIN. RIGGED ELEVATOR TRIM TAKEOFF WARNING SWITCH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930000382003093000038NM 2003 9 30 2003UALA00655 120030829A5330 DOUBLER BOEING777 777222 1385219NM PWA 4052 PW4052 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29795UA 26927 DOUBLER DAMAGE AT BS 660 STRINGER 25 L. MAJOR REPAIR ACCOMPLISHED. DOUBLER WAS REPAIRED. 2L72 4F4 FRTT0001SE E24NE 20030930000452003093000045NM 2003 9 30 2003UALA00664 120030903A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 CARGO DOOR DENTED ABOVE HANDLE ASSY. MAJOR REPAIR ACCOMPLISHED. FABRICATED EXTERNAL DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20030930000472003093000047EU 2003 9 30 2003UALA00666 120030902A3350 SWITCH AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29467UA 1359 WITH NO SMOKING SWITCH IN THE ON POSITION, EMERGENGY EXIT SIGNS WERE ILLUMINATED DURING TAXI & FOR THE FIRST 30 MIN OF FLIGHT. FLIGHT ATTENDANT CALLED TO REPORT THAT ALL EMERGENCY EXIT SIGNS EXTINGUISHED AT SAME TIME WITH NO CHANGE IN COCKPIT SWITCH POSITION. 2L72 4F4 FRTA28NM E40NE 20030925000492003092500049NM 2003 9 25 AALA20030843 120030808A21503966081 VALVE BOEING737 737823 13844BZNM LT A/C PACK MALFUNCTIONED A AALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21926AN 29527 ON TAKEOFF AIRCRAFT WAS UNABLE TO PRESSURIZE AND HAD A LOUD PACK NOISE FROM LT PACK. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REPACKED SURGE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030925000892003092500089 2003 9 25 00109 420030103A3197 WIRE AMD FALC20FALCON 2720302EU GLARE SHIELD SHORTED E HAEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW05158TW 158 PILOT REPORTED SMOKE COMING FROM CENTER PANEL AREA ABOVE ANNUCIATOR. REQUESTED DECENT TO NEAREST AIRPORT LANDED ATL WITH NO FURTHER PROBLEM. WILL UPDATE THIS SDR AFTER MAINTENANCE. MAINTENACE FOUND WIRE IN PILOTS GLARE SHEILD LT ASSY SHORTED AND BURNED. REPLACED FLOURESCENT TUBES AND CONNECTOR TO CO-PILOTS LIGHT ASSEMBLY. 2L72 4F A7EU 20030925000912003092500091NM 2003 9 25 03FDEA01559 120030918A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON LOWER STRUCTURE BS 1010 FLOORBEAM, LBL 43-LBL 2. BLENDED CORROSION DAMAGE ON LOWER STRUCTURE BS 1010 FLOORBEAM LBL 43-LBL 2 PER SRM 51-10-1. DAMAGE AT BS 1010, LBL 4-LBL 14, WL 200 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 AND 53-10-6. ALL OTHER BLEND AREAS WERE FOUND TO BE IN LIMITS PER SRM 53-10- 1. REPAIRED DAMAGE LOWER STRUCTURE BS 1010, LBL 4 - LBL 14, WL 200 PER SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 20030925000972003092500097CE 2003 9 25 DXTA200300120 120030919A3260 LAMP CESSNA500 560CESSNA 2076750CE ANNUNCIATOR INOPERATIVE E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07308QS 5600277 DURING APPROACH, SELECTED GEAR DOWN AND THE LEFT MAIN GEAR LIGHT DID NOT SHOW DOWN AND LOCKED. MANUAL (T-HANDLE) GEAR EXTENSION PULLED TO BLOW GEARS DOWN, LANDING UNEVENTFUL. - REPLACED 4 LAMPS IN ANNUNCIATOR PANEL, SWUNG GEARS SEVERAL TIMES, SERVICED NITROGEN, AND HYDRAULIC SYSTEM, ALL SYSTEMS TEST GOOD IAW CE 560 MM CHAPTER 32-00. 2L72 4F RTA22CE 20030926000062003092600006NM 2003 9 26 QXEA200301026 120030826A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 7 SEAT TRACK HAS A COM LOCK LUG CORRODED ON AFT EDGE OF INBOARD SIDE THREE INCHES AFT OF FRAME X201. REPAIRED IAW DHC-8 SRM 51-40-11, AND RD'S 8-53-4698, 8-53-1102 AND 8-53-4473. 2H72 4T RTA13NM 20030926000482003092600048NM 2003 9 26 0301646308 120030827A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01668US 24223 DURING LINE CHECK, FOUND LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM THE DOOR TO ROW 12. RECONNECTED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030926000932003092600093NM 2003 9 26 03FDEA01368 120030806A5753ARC0503504 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RT WING OUTBD FLAP OUTBD HINGE BRACKET (WING SIDE) LOWER OUTBD STUD HOLE FOUND CORROSION. RT WING OUTBD FLAP OUTBD HINGE BRACKET (WING SIDE) LOWER OUTBD STUD HOLE REPAIR CARRIED IAW FEDEX EA 1-5740-71796, WINGS- LT AND RT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030926001052003092600105EU 2003 9 26 DHL2003368011 120030830A2750 LINKAGE AIRBUS300 A300B4203 3930306EU TE FLAPS DISCONNECTED A DHLAL ABORTED APPROACH O OTHER APAPPROACH 1 SO01368DH 207 ON APPROACH WITH SLATS 16 FLAPS 8, FLAPS DIDN'T OPERATE NORMALLY. PERFORMED ABNORMAL. FOUND DEFLECTOR MECH LINKAGE DISCONNECTED. RESECURED IAW M/M 27-51-65. OPS CHECKED GOOD ON GROUND. 2L72 4F RTA35EU 20030926001382003092600138EA 2003 9 26 A6WA200340126 120030825A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31407AW 7424 FS 625 AT STR 14R, FUSELAGE TO HORIZONTAL INTERCOSTAL CONNECTING CLEAT HAS A CRACK AT THE FORWARD RADIUS. REPLACED CLEAT WITH PN S6144-4 IAW EO 601R-53-4181. NEW BRACKET (CLEAT) INSTALLED REF CRJ SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20030926001542003092600154WP 2003 9 26 ARWA20030806 120030821A5310 DOOR FRAME DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45688 DURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER WITH CRACKS OF 0.625 & 0.437 INCH. REPAIRED THE AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER IAW SRM 53-2-0 FIG 18, SHEETS 1, 5, 6, 7 & 8, TEMPORARY REVISION 53-134 & TEMPORARY REVISION 53-158, DATED 01/23/02 & 12/20/02 RESPECTIVELY EA 1020, DATED 08/21/03. 2L74 4F 4A25 20030929000772003092900077NM 2003 9 29 03FDEA01446 120030901A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING O/B FLAP I/B HINGE (A/C SIDE) I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. 2L73 4F RTA22WE 20030929001072003092900107NM 2003 9 29 AWXA200301022 120030813A53156546803504 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .5 INCH CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM AT BS 520, LBL 24. MAINTENANCE STOP DRILLED CRACK ON FLOORBEAM AT BS 520, LBL 24 AND PERFORMED HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW AWA ER 15-5311-03241-ES2. 2L72 4F RTA16WE 20030929001122003092900112EA 2003 9 29 QXEA200301060 120030904A5210 COUNTERBALANCE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 OUT OF ADJUST A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09606QX 10023 ON FLIGHT 2482 MAIN CABIN DOOR WILL NOT OPEN. ADJUSTED MAIN CABIN DOOR AFT COUNTERBALANCE. NO PARTS REPLACE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030929001412003092900141NM 2003 9 29 DHL2003748501 120030822A5347 SEAT TRACK BOEING727 727225 1384077NM ZONE 900 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 DURING C CHECK AT MFG, N/R 691F1-1601-005 MAIN PASSENGER CABIN SEAT TRACK L/H O/B STA. 688 STA. 738 CORROSION FOUND AT ATTACHING SCREWS, HOLES CRACKED OUT, TOOL MARKING IN CENTER OF TRACK. REMOVED FAB. AND INSTALLED NEW SEAT TRACK P/N 60-6549 7178 T 6511 P.O. NR 0341745 FROM STA. 688 TO STA. 740 I.A.W. B-727 SRM 51-30-02, 51-30-8, 51-10-8, SEAT TRACK MACHINED ON TRAVELER 691T9-5001. 2L73 4F A3WE 20030929001432003092900143NM 2003 9 29 QXEA200301058 120030903A3150522942 INDICATOR DHAV DHC8 DHC8202 2809007NM ZONE 300 FAILED A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09357PH3118013112 504 ON FLIGHT 2228 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN AT 10 KNOTS. DID NOT RECIEVE WITH CONFIGUATION TEST. REMOVED AND REPLACED FLAP POSITION INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930000222003093000022NM 2003 9 30 F3LA200300126 120030906A5330 SKIN AIRBUSA319 A319111 3930336NM FUSELAGE DENTED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03903FR 1560 DURING WALKAROUND, MAINTENANCE FOUND TWO SMALL DENTS AFT AND EVEN WITH FORWARD ENTRY DOOR, APPROXIMATELY 3 FT. AFT OF DOOR AT STA. 950, STR. 22L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW EA A9-53R-10127 AND SRM 53-00-11. 2L72 4F RTA28NM 20030930000252003093000025WP 2003 9 30 03FDEA01465 120030909A5753ARC050211 HINGE BRACKET DOUG MD10 MD1010F WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 LT OUTBOARD FLAP INBOARD HINGE BRACKET, CORROSION REPAIR (P/N ARC0502-11) LT O/B FLAP I/B HINGE BRACKET CORROSION REPAIR,P/N ARC,0502-11 CLOSED ON 09/09/2003 FEDEX N/R S00031. 2L73 4F RTA22WE 20030930000712003093000071NM 2003 9 30 DHL2003748502 120030820A5753 FLAP TRACK BOEING727 727225 1384077NM RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 DURING C-CHECK AT PEMCO IN DOTHAN, ALABAMA N/R 691F1-1442-005, RT WING LOWER TRAILING EDGE AT O/B FLAP TRACK FWD END-CORROSION ON SKIN I/B OF TRACK. REMOVED RT O/B FLAP O/B TRACK FAIRING, REPAIRED AREA PER EA PD 27-57-01. RE-INSTALLED O/B FLAP O/B TRACK FAIRING IAW B-727 M/M 20-81-01. 2L73 4F A3WE 20030930000722003093000072NM 2003 9 30 0301706301 120030904A3350 LIGHT BOEING747 747451 1384940NM CABIN INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01661US 23719 DURING LINE CHECK FOUND ZONE "C" RIGHT FLOOR PATH EMERGENCY LIGHTS INOP. INSTALLED NEW LIGHT ASSEMBLY AT 29H. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030930000952003093000095EU 2003 9 30 AWXA200301032 120030906A5320D5323022620100 PLATE AIRBUS320 A320232 3930326EU FAIRING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON RT FUSELAGE UNDER BELLY BODY FAIRING CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CRACKED CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 8-9, FIG. 2 AND 3, AND PG. 22, FIG. 8. 2L72 4F RTA28NM 20030930001162003093000116NM 2003 9 30 03FDEA01484 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT POINT O/B LUG HOLE CORRODED. 2L73 4F RTA22WE 20030930001212003093000121NM 2003 9 30 03FDEA01479 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG HOLE CORRODED. 2L73 4F RTA22WE 20030930001232003093000123NM 2003 9 30 03FDEA01477 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B ACTUATOR LUG HOLE CORRODED. 2L73 4F RTA22WE 20030930001242003093000124NM 2003 9 30 03FDEA01476 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) O/B ACTUATOR LUG HOLE CORRODED. 2L73 4F RTA22WE 20031001000012003100100001NM 2003 10 1 0301716303 120030817A3260 CONTROL PANEL BOEING747 747451 1384940NM COCKPIT INOPERATIVE A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01663US 23818 DURING TAKEOFF, RECEIVED (SMOKE DR5 REST) MESSAGE ACCOMPANIED WITH AN EICAS AND MASTER CAUTION. AIRCRAFT ABORTED TAKEOFF AT 75 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. REPLACED THE P24 PANEL AND 4 CREW REST SMOKE DETECTORS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031001000272003100100027NM 2003 10 1 CALA0300517 120030909A5210 SKIN BOEING777 777224 1385225NM R-4 DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778013 29861 MAINTENANCE DISCOVERED A DENT IN THE R-4 DOOR LOWER AFT CORNER SKIN AFTER AIRCRAFT ARRIVED IN LGW. THE DENT WAS WITHIN LIMITS AND DEFERRED. THE DOOR SKIN WAS REPAIRED IAW SRM 52-10-01, REPAIR 8 WHILE AIRCRAFT WAS IN A 4C CHECK AT HKG. 2L72 4F RTT00001SE 20031001000322003100100032WP 2003 10 1 UPS03841174 120030819A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, CORROSION AT FASTENER HOLES FOR SEAT TRACK/FLOORBEAM STA 781 LBL 50. REMOVED FASTERNERS IAW DC8 SRM 51-3-0. CUT SEAT TRACK STA 781 TO 845 LT IAW UPS EO DC8 5320-8309. FABBED SPLICE CHANNEL IAW UPS EO DC8- 5320-8309 LOCATED & DRILLED SEAT TRACK & 4 SPLICES IAW UPS EO DC8-53 20-8309. ALODINED & PRIMED IAW DC8 SRM 51-1-8 INSTALLED SEAT TRACK A ND 2 SPLICES CHANNEL & 4 SPLICES IAW DC8 SRM 51-1-20D & 51-3-0. 2L74 4F RT4A25 20031001000332003100100033WP 2003 10 1 UPS03841175 120030806A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, MAP OUT L1 UPPER FWD EXTERNAL DOUBLER FOR ENGINEERING MAPPED OUT DOUBLER, TRIPLER SIZE AND FASTENER PATTERN AND CHECKED THICKNESS .063 AND .080. CUT OUT CRACK IN SKIN IAW DC8 SRM 53-2-0 FIG 15TR 53-155.FABBED -17 DBLR -15 TPLR AND FILLER IAW DC8 SRM 5-1-20D AND 53 -2-0 TR53-155. DRILLED NEW SPLICE P/N 5597646-99 TO FIT IAW DC8 SRM 5 1-1-24. INSTALL SPLICES IAW DC8 SRM 51-1-21 & 51-3-0. 2L74 4F RT4A25 20031001000402003100100040WP 2003 10 1 UPS03841184 120030808A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, CORROSION ON FRAME FS 1340 S36L. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIG THICK 0.080, LOSS .020 REM. MATERIAL .060, FOUND OUT OF LIMITS IAW DC8 SRM 53-4-1, 51-2-0, & 53-2-0.FAB BED ANGLE REPAIR (7075-0, 0.080, PO 312487.0) IAW DC8 T/R NR 53-110; HEAT TREAT TO 7075-T6. DRILLED IAW DC8 SRM 51-1-20D ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20031001000442003100100044WP 2003 10 1 UPS03841189 120030810A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, CORROSION ON FLOORBEAM UNDERSIDE AT STA 1680 LBL 43 REMOVED CORROSION IAW DC8 SRM 51-1-8. MATERIAL REMAINING 0.00 FROM .125 FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR ANGLE AND FILLER IAW DC8 SRM 53-2-0 FIG 1B AND TR 53-124. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 FIG 1B AND TR 53-124. 2L74 4F RT4A25 20030926000742003092600074NM 2003 9 26 03FDEA01397 120030828A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 A/C BAY LT SIDE, ABOVE PANEL 3355L, CORROSION ON TORQUE BOX LWR FLANGE NUT CLIPS FOUND DAMAGE TO LOWER FLANGE TO BE .066 MATERIAL LOSS ORIGINAL THICKNESS .125. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED CHORD. DRILLED UP NEW CHORD. ALODINED, PRIMED & INSTALLED LOWER CHORD FOR TORQUE BOX IN A/C BAY LT SIDE. WORK DONE PER SRM 53-10-1, 51-10-3, 51-30-2, 51-30-5, WORK DONE FROM BS 740-870, LBL 10, WL 145. 2L73 4F RTA3WE 20030926000842003092600084EU 2003 9 26 AWXA200301002 120030822A5321D53671615002 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW 543 DURING C-05 CHECK CABIN FLOOR PANEL 241EF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGE FLOOR PANE 241EF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 15-D53671615; INSTALLED NEW PANEL IAW T/C R1C25306. 2L72 4F RTA28NM 20030926001322003092600132WP 2003 9 26 DHL2003802012 120030830A5280 DOOR DOUG DC8 DC873 302199CWP RT MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH 46076 RT MAIN GEAR DOOR HAS .2500 INCH CRACK PROPAGATING FROM RIVET B.S. 875.125 20 INCH OUT FROM INBOARD HINGE. STOPPED DRILLED CRACK, INSTALLED A DOUBLER REPAIR IAW SRM 52-2-3. 2L74 4F RT4A25 20030929000112003092900011NM 2003 9 29 AWXA200301011 120030815A575365521411 SKIN BOEING737 737277 1384570NM TE FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 - DURING C-16 CHECK A 0.080 INCH CRACK WAS FOUND ON EDGE OF RT INBOARD HINGED FLAP UPPER SKIN AT WBL 180.75. MAINTENANCE TRIMMED OUT CRACK ON RT INBOARD HINGED FLAP UPPER SKIN AT WBL 180.75 IAW B737-200 SRM 57-50-01 PG 1 FIG 3, SHEETS 2-4. 2L72 4F RTA16WE 20030929000452003092900045NM 2003 9 29 03FDEA01405 120030903A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 CORROSION ON 740 FRAME COMMON TO DELTA BOX RBL 7 THRU LBL 7 WL 156 REMOVED CORROSION ON 740 FRAME COMMON TO DELTA BOX RBL 7 TO LBL 7, WL 156. CORROSION BLEND-OUT OUT OF LIMITS IAW SRM 53-10-1 FIG 1. ORIGINAL THICKNESS .112 MATERIAL REMAINING = .052. REMOVED CHORD AND REPLACED IAW SRM 51-30-2. AIR DISTRIBUTION DUCTS REMOVED FOR ACCESS LEAK CHECKED GOOD IAW FED EX MM 36-00- 000-5 IAW EA 7-5330-54955. 2L73 4F RTA3WE 20030929000522003092900052NM 2003 9 29 03FDEA01420 120030901A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD BORE FOUND CORRODED. RT WING O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD CORRODED BORE REPAIRED AS PER EA 1-5750-73297. 2L73 4F RTA22WE 20030929001312003092900131NM 2003 9 29 HNAA0300044 120030824A335082410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DEFECTIVE A HNAAO OTHER O OTHER CRCRUISE 1 EA07975HA3657536575 176 EMERGENCY LIGHTS COMES ON AND REMAINS ON IN FLIGHT. REPLACED EMERGENCY LIGHT CONTROL BOX. 2H72 4T RTA13NM 20030930000762003093000076NM 2003 9 30 AUC2003F00001 120030730A3244 TIRE LKHEEDP3A P3A 5260103NM MLG FAILED B AUCRO OTHER O OTHER NRNOT REPORTED 1 WP25900AU28 151391 WHEEL ASSEMBLY WITH RECAPPED TIRES INSTALLED ON AIRCRAFT. THESE TIRES INSTALLED FOR A TOTAL OF 10 DAY AND OPERATED FOR A TOTAL OF 28 FLIGHT HOURS. UPON TAKE OFF ONE OF THE NOSE WHEELS LOST THE CENTER PORTION OF THE TIRE TREAD. THE FLIGHT CREW EXPERIENCED AN VIBRATION ON TAKE OFF AND ELECTED TO RETURN TO BASE. THE MADE A SAFE LANDING. THE PAIR OF TIRES WERE CHANGED AND THEY INSPECTED THE AIRCRAFT AND NO DAMAGE WAS FOUND. WHEN THE TIRES RETURN TO MAINTENANCE, BOTH TIRES WERE CHECKED FOR PROPER INFLATION, NO LOSS OF PRESSURE FOUND. 2L74 4T RTA32NM 20030930000792003093000079WP 2003 9 30 ABXA030352 120030818A53209922042505AX FLOOR SUPPORT DOUG DC9 DC932F 3022067WP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 LEFT FLOOR SUPPORT STRUT TO FRAME ATTACH BRACKET CRACKED AT STA. 275, BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED LEFT FLOOR SUPPORT STRAP TO FRAME ATTACH BRACKET IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 20030930000932003093000093SO 2003 9 30 LR7A03076 120030907A55513734901L FITTING LKHEED382 382G 526414USO HORIZONTAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 667 4698 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB2703 FOUND LT HORIZONTAL STAB TIP LOOSE DUE TO OUTBOARD ELEVATOR HINGE FITTING LOWER LUG CRACKED AT HSS 296L, FS 1095, WL 277. REPLACED FITTING IAW DWG 373490. NR 0017. 2H74 4T A1SO 20030930001002003093000100NE 2003 9 30 QXEA200301111 220030905A7200 ENGINE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 2 LEAKING A QXEAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 NM09364PH11501897 524 PCEAG0096 ON FLIGHT 2148 SMOKE IN COCKPIT AND CABIN AFTER ENGINE START. REMOVED AND REPLACED NR 2 ENGINE FOR INTERNAL OIL LEAK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030930001052003093000105EA 2003 9 30 03253630 120030909A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR DURING MAINTENANCE INSPECTION, THE FLOOR TRACK EMERGENCY LIGHTING WAS DIM. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FWD LIGHT POWER STRIP, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20030930001072003093000107NM 2003 9 30 03FDEA01493 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG O/B SIDE SURFACE CORRODED. 2L73 4F RTA22WE 20030930001082003093000108NM 2003 9 30 03FDEA01492 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT O/B LUG CORRODED. 2L73 4F RTA22WE 20030930001252003093000125NM 2003 9 30 03FDEA01475 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG O/B SIDE SURFACE CORRODED. 2L73 4F RTA22WE 20030930001262003093000126NM 2003 9 30 03FDEA01474 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG HOLE CORRODED. 2L73 4F RTA22WE 20031001000492003100100049WP 2003 10 1 UPS03841194 120030812A5313564932743 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, AFT FUSELAGE TAIL SECTION AT FS 1766-1780 L17L IS CRACKED. REMOVED L17LT TO FOM. LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20031001000572003100100057NM 2003 10 1 P5CA0300956 120030922A5753 SKIN BOEING747 7472U3B 1384846NM TE FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 RT OUTBOARD MID FLAP COVE PNL DELAMINATED / CRACKED - 24 INCH LONG - WBL 660. REPAIRED DAMAGE AREA 2L74 4F RTA20WE 20031001000682003100100068NM 2003 10 1 2003UALA00706 120030919A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29529UA 25019 FRAME DAMAGED AT FUSELAGE STA.1681 AT WL210. 2L72 4F4 FRTA2NM E17NE 20031001000762003100100076NM 2003 10 1 2003UALA00714 120030924A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29369UA 24538 CABIN FLOORBEAM IS CRACKED IN THE RADIUS AT STA 927 RBL 45. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031001000902003100100090SW 2003 10 1 2003F00587 120030407A5200H29497 GATE FRCHLDSA227 SA227DC 3377521SW PAX DOOR OUT OF RIG A BSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM05453LA DC852B CARGO DOOR WARNING LIGHT CAME ON AT 14,000 MSL, CREW RETURNED TO STATION, LIGHTS WENT OUT AT 400 FEET AGL. SUSPECT DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, OR DOOR CLICK CLACK OR SWITCH RIGGING. RELOCATED AIRCRAFT TO MX BASE ON AND SFP AFTER INITIAL INSPECTION, THEN REPLACED TOP FRONT CLICK CLACK AND RIGGED REAR BOTTOM CLICK CLACK. PERFORMED FLIGHT CHECK FLIGHT AFTER WORK TO VERIFY OPERATION. NO DEFECTS NOTED. (M) 2L72 4T RTA18SW 20031001000972003100100097WP 2003 10 1 AMTA200301128 120030901A5210 MECHANISM LKHEED1011 1011385115 5265015WP ELEC DOOR CLOSE INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 193B1230 R3 PASSENGER DOOR DOES NOT CLOSE ELECTRICALLY. MANUALLY CLOSED, DOOR WARNING LIGHT OFF. (M) 2L73 4F A23WE 20031001001132003100100113NM 2003 10 1 UIEA200300048 120030816A531165B01718503 FRAME BOEING747 747271C 1384869NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 DURING C-CHECK AT AMS, FOUND CRACK IN STATION 500 FRAME WEB OUTER FLANGE BETWEEN RT STRINGERS S-10 AND S10A. TRIM CRACK AND SURFACE HFEC INSPECT TRIM LINE TO INSURE CRACK FREE CONDITION. INSTALLED TWO FILLERS, A REPAIR ANGLE, AND A REPAIR DOUBLER PER REF A OPEN HOLE HFEC INSPECT FASTENER HOLES COMMON TO REPAIR PARTS TO INSURE CRACK FREE CONDITION. CONTINUED INSPECTIONS ARE REQUIRED PER REF C SB 747-53A2265. REINSPECT AT REPEAT INTERVALS NOT TO EXCEED 3,000 FLIGHT CYCLES UNTIL THE AIRPLANE ACCUMULATES 20,000 FLIGHT CYCLES. THE REPAIR HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE TO PARAGRAHP B OF AD 91-11-01 AND HAS BEEN FOUND TO MEET THE TYPE CERT BASIS OF THIS AIRPLANE AS REQUIRED. (M) 2L74 4F A20WE 20031001001172003100100117NM 2003 10 1 USAA030164 120030731A5340 FITTING BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US40913 23987 FOUND FITTING CORRODED .125 INCH AREA, 2 INCHES AROUND FITTING, BOTH SIDES, BS 685 LT MLG SIDE STRUT FITTING. REMOVED BUSHINGS, MACHINED FACES AND BORE OF LUG AND INSTALLED NEW BUSHINGS PER EA 76728. (M) 2L72 4F RTA16WE 20031001001212003100100121NM 2003 10 1 USAA030187 120030908A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU 23514 CLT - FOUND SKIN CRACKED 2.5 INCHES, FUSELAGE SKIN JUST BELOW S19R AT FS 760. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20031001001282003100100128WP 2003 10 1 UPS03841199 120030826A5320 WEB DOUG DC8 DC873F 302199FWP SUBFLOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, FLIGHT DECK SUBFLOOR FS 133 LBL36 INDICATION OF HIDDEN CORROSION (MISSING AND FITTED REIVET HEADS) REMOVED COVER PANEL TO FOM. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED FILLER DOUBLER AND FINGER DOUBLERS IAW DAC DWG SR08530026. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FILLER, DOUBLERS, FINGER DOUBLERS AND ALL PARTS REMOVED TO FOM IAW DC8 SRM 51-1-21, 51-1-20D, MM 21 -56-05 STEP 3B 1-13, DAC DWG SR08530026, AND SRM 51-3-0. 2L74 4F RT4A25 20031002000082003100200008NM 2003 10 2 USAA030172 120030822A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19587US49297 23932 FOUND SKIN CRACKED 2.25 INCH, S23R 4 INCHES AFT 727D. INSTALLED DOUBLER PER EA 94640, SRM 737-300 AND 53-00-01. (M) 2L72 4F RTA16WE 20031002000102003100200010WP 2003 10 2 AMTA200301086 120030811A5320 STIFFENER LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER AFT OF STRINGER 33, CORRODED AT FRAME ATTACH POINT. INSTALLED FASTENERS AND REPAIR PARTS PER SRM 53-11-00 FIG 8 59. EDGE SEALED PER SRM 51-25-00. (M) 2L73 4F A23WE 20031002000112003100200011WP 2003 10 2 AMTA200301101 120030811A5313 STRINGER LKHEED1011 10113851 5265010WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND STRINGER CORRODED NEAR APB. REMOVED CORRODED STRINGER SECTION AND REPAIRED IAW SRM 53-13-00. (M) 2L73 4F A23WE 20031002000152003100200015WP 2003 10 2 AMTA200301126 120030902A52101281T10033 ACTUATOR LKHEED1011 10113853 5265020WP PAX DOOR INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 R-1 DOOR IS INOPERATIVE ELECTRICALLY. REMOVED AND REPLACED R-1 DOOR ELECT ACTUATOR IAW 52-12-01, OPS CHECKED OK. (M) 2L73 4F A23WE 20031002000272003100200027WP 2003 10 2 GTIA030668 120030812A5754 SKIN DOUG DC9 DC983 3022083WP LT WING SLAT LIGHTNING STRIKEA GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 LT WING NR 5 SLAT HAS LIGHTNING STRIKE AT INBOARD END ON TOP OF SLAT. AFTER FURTHER EVALUATION LIGHTNING STRIKE WAS FOUND TO BE CORROSION. CUT OUT DAMAGED SKIN. FABRICATED REPAIR SKIN AND DOUBLERS. INSTALLED REPAIR SKIN AND DOUBLERS. (M) 2L72 4F RTA6WE 20031002000342003100200034NM 2003 10 2 UIEA200300049 120030816A572065B145282 SPLICE BOEING747 747271C 1384869NM RT WING DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 DURING C-CHECK, AT AMS WHILE PERFORMING SB 747-53A 2309 KLM ACCIDENTALLY DAMAGED THE AFT INBOARD FASTENE HOLE OF THE OUTBOARD FLANGE OF THE LOWER SPLICE PLATE. REPAIR HOLE H IN THE LOWER SPLICE PLATE ON THE RT WING WAS OVERSIZED TO 1.0030 INCHES. AL-N1-BR BUSHING WAS INSTALLED. (M) 2L74 4F A20WE 20031002000382003100200038WP 2003 10 2 GTIA030669 120030827A3350 SIGN DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 EXIT IDENTIFIER AT RIGHT FORWARD OVERWING EXIT INOPERATIVE. REPAIRED BROKEN WIRE BEHIND LIGHT ASSEMBLY AT THE RIGHT FORWARD OVERWING EXIT. (M) 2L72 4F RTA6WE 20031002000392003100200039NM 2003 10 2 USAA030178 120030828A5553 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US40788 23984 FOUND FITTING CORRODED 2.5 INCHES AROUND, VERT STAB AFT RT OUTBOARD LUG AFT CLEVIS AND T-FITTING. REMOVED AND REPLACED BUSHING/OVERSIZE PER EA 76801. CORROSION LEVEL 1, STAK NR C55-706-11. (M) 2L72 4F RTA16WE 20031002000452003100200045WP 2003 10 2 UPS03841201 120030827A5311 FRAME DOUG DC8 DC873F 302199FWP AC BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, BELT FRAME IC CRACKED AT STA. 55 LONG. 24L TO 25L CUTOUT DAMAGE, FABRICATED AND INSTALLED FILLER AND ANGLE DOUBLER I.A.W. SRM. 53-2-0 FIG. 2. 2L74 4F RT4A25 20030929000502003092900050NM 2003 9 29 03FDEA01438 120030904A3260 POSITION SWITCH BOEING727 727200 138407ENM NLG INOPERATIVE A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25479FE 21461 NOSE GEAR UNSAFE LIGHT CAME ON AND FLICKERED DURING T/O ROLL WITH A STEADY GREEN. NOSE GEAR DOWN AND LOCKED LIGHT DOORS LIGHT AND S/O NOSE GEAR DOOR LIGHT REMAINED OFF ALL LIGHTS WENT OUT NORMALLY DURING GEAR RETRACTION. OKAY ON LANDING. REMOVED NOSE GEAR POSITION SWITCH C/P FOR TROUBLESHOOTING. REMOVED AND REPLACED NOSE GEAR POSITION SWITCH AS A PRECAUTION IAW 727-200 M/M 32-61-071-4 STEPS 2A-B- AND C(3). AIRCRAFT STILL REQUIRES JACK AND GEAR SWING IAW STEP 2C(4). JACKED ACFT AND C/W 727-200 M/M 32-61-071-4 STEP 2C-(4) AND (5). CYCLED GEAR SEVERAL TIMES ALL INDICATIONS NORMAL. NO DEFECTS NOTED AT THIS TIME. 2L73 4F RTA3WE 20030929000932003092900093WP 2003 9 29 UPS03841162 120030827A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, STA. 1720 AND 1740 LONG. 15R IS CRACKED AT FRAME ATTACH BOLTS. REMOVED DAMAGED LONGERON SECTION STA. 1720-1760, FABRICATED AND INSTALLED SECTION IAW SRM. 53-2-2 FIG. 10. 2L74 4F RT4A25 20030929001102003092900110NM 2003 9 29 F3LA200300124 120030904A5320 PANEL BOEING737 73736Q 1384409NM COCKPIT MISINSTALLED A F3LAC ABORTED TAKEOFF WF INADEQUATE Q C FLT CONT AFFECTED TOTAKEOFF 1 NM03305FA 253 28662 ABORTED TAKEOFF. DURING TAKEOFF ROLL, FLIGHT CREW REPORTED AIRCRAFT WOULD NOT STEER TO LT. TAKEOFF REJECTED AT APPROXIMATELY 60 KNOTS. FOUND LOWER SIDEWALL PANEL IN FLIGHT DECK, RT SIDE BETWEEN STA 178 AND 254, IMPROPERLY INSTALLED AND INTERFERRING WITH FIRST OFFICER'S RT RUDDER PEDAL. REINSTALLED PANEL PROPERLY PER MM 25-11-21. RUDDER PEDALS MOVED FREELY THROUGH FULL TRAVEL WITH NO INTERFERENCE. PERFORMED HIGH ENERGY STOP CONDITIONAL INSPECTION. NO DISCREPANCIES FOUND. 2L72 4F RTA16WE 20030930000102003093000010NM 2003 9 30 AWXA200301029 120030811A5753654643090 FLAP BOEING737 737277 1384570NM RT WING TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK THE UPPER SURFACE OF THE RT INBOARD FORE-FLAP WAS FOUND DISBONDING 33 INCH TO 37 INCH FROM THE OUTBOARD END. MAINTENANCE PERFORMED HONEYCOMB CORE REPAIR ON RT INBOARD FORE-FLAP IAW B737-200 SRM 51-40-20, REPAIR NR 9, FIG. 18, PG. 63-67. 2L72 4F RTA16WE 20030930000442003093000044NM 2003 9 30 2003UALA00663 120030903A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 AFT PIT STA 1580 FLOORBEAM AT RBL48 FLOOR LINE DENTED 2.8IN BY 0.90IN BY 0.260 DEEP. MAJOR REPAIR ACCOMPLISHED. FABRICATED A NESTED ANGLE REPAIR. INSTALLED WITH SHIMS AND FILLERS, SEALED AND PAINTED. 2L74 4F4 FRTA20WE E24NE 20030930000772003093000077WP 2003 9 30 ABXA030358 120030818A533059114213 SKIN DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 CORROSION BETWEEN LONGERON 26 LT AND SKIN BETWEEN STA. 775 AND 813. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20030930000862003093000086WP 2003 9 30 ABXA030356 120030818A532059217181 FLOOR SUPPORT DOUG DC9 DC932F 3022067WP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 CABIN FLOOR SUPPORT FITTING FS 434 LONGERON 18 LEFT CRACKED AT UPPER HORIZONTAL FLANGE BETWEEN FASTENERS AND HAD LEVEL I CORROSION ON AFT SIDE. REPLACED FITTING AND REPAIRED AREA IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 20031001000092003100100009NM 2003 10 1 QXEA200301077 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 11 SEAT TRACK IS CORRODED IN BOTTOM OF CHANNEL AND ON TOPS OF LT AND RT RAILS FROM AFT OF STATION X467. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031001000162003100100016WP 2003 10 1 ARWA20030906 120030906A5411 SPAR CAP DOUG DC8 DC861 3021952WP NR 2 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1929UA 46159 DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON LT CENTER SPAR CAP WITH CRACK STA YIP 235. 2L74 4F 4A25 20031001000882003100100088NM 2003 10 1 USAABB03135 120030815A33508731002511REV15 LIGHT BOEING757 7572B7 1384964NM L4 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU 27244 FOUND L4 DOOR EXIT IDENTIFIER LIGHT INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER LIGHT ASSEMBLY AT L4 DOOR. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20031001001072003100100107WP 2003 10 1 G6OA070 120030612A2140542100001 CONTROL PANEL DOUG DC10 DC1030F 3023504WP COCKPIT BURNED A G6OAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27607GC 46978 WHILE IN FLT, PITOT INOP LIGHT CAME ON. SWITCH WAS ROTATED TO ALL POSITIONS AND ALL HEATERS WERE WORKING. SHORTLY THERE AFTER SMOKE STARTED COMING OUT FROM BEHIND THE METER SEL AND HEAT CONTROL PANEL. SWITCH WAS IMMEDIATLY TURNED OFF AND A/C RETURNED TO MIA. 2L73 4F RTA22WE 20031002000562003100200056WP 2003 10 2 UPS03841213 120030827A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP COCKPIT SUBFLOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, COCKPIT SUBFLOOR INTERCOSTAL UPPER FLANGE IS CRACKED AT STA.-21 LBL 12. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 53-2-0 FIG. 1B. 2L74 4F RT4A25 20031002000612003100200061NM 2003 10 2 QXEA200301087 120030830A5712 RIB DHAV DHC8 DHC8202 2809007NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 RT HAND WING RIB IS CHAFED BY FUEL LINE AT STATION YW207 LOWER SURFACE OF UPPER RIB MEMBER 4 INCHES AFT OF PANEL 624AT CUTOUT. REPAIRED IAW DHC-8 SRM 51-00-06, 57-20-00 AND RD 8-57-2664. 2H72 4T RTA13NM 20031002000772003100200077NM 2003 10 2 PCAA0309107 120030909A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13832EX 280 DURING A ROUTINE MAINTENANCE VISIT SEVERAL EMERGENCY FLOOR EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. A BROKEN WIRE WAS DISCOVERED AT THE MID-CABIN FLOOR AREA. WIRING WAS SPLICE REPAIRED, AND SEVERAL BULBS WERE REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031002000822003100200082NM 2003 10 2 MWEA030368 120030911A53305936434501 DOUBLER DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FUSELAGE DENT ON LT AT STATION 313-332 AND LONGERON 24 LEFT AND 25 LEFT. FABRICATED AND INSTALLED TITANIUM FINGER DOUBLER AND UPPER SKIN PLUG OUT. 2L72 4F RTA6WE 20031002000972003100200097NM 2003 10 2 C1HA200386013 120030910A5320 SUPPORT BOEING727 7272S7 138407ZNM LAV WALL CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 CORROSION IN SEVERAL AREAS OF LT AFT LAV INBOARD WALL SUPPORT AT BS 1138/1164. 2L73 4F A3WE 20031002001092003100200109NM 2003 10 2 QXEA200301094 120030828A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 SEAT TRACK NR 4 LEFT SIDE HAS 8 AREAS OF DEEP PITTING CORROSION ON OUTBOARD FLANGE AROUND RIVET HOLES AT STATIONS X205.000 THROUGH X220.000. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-4473. 2H72 4T RTA13NM 20031002001162003100200116SO 2003 10 2 C2XA03IA093 120030906A49004800102 SWITCH EMB 145 EMB145LR 3260212SO APU INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714902 145496 WHILE TRYING TO START THE APU THE CREW NOTED A STRONG FUEL ODOR AFTER TGE APU WAS STARTED. NOTE: IT IS DIFFICULT TO START THE APU, HAVE TO HOLD SWITCH UNTIL APU IS AT 100 PERCENT. MAINTENANCE REMOVED AND REPLACED THE APU EXTINGUISHER SWITCH, PERFORMED A OPERATIONAL CHECK, NO FUMES NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031002001192003100200119NM 2003 10 2 QXEA200301103 120030826A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CARGO COMPARTMENT FLOOR PAN HAS A CORRODED NUTPLATE ON BOTTOM SIDE ALONG AFT ROW OF 144.HZ APERTURE. REPAIRED IAW DHC-8 SRM 51-20-16, 53-00-16, 51-20-36, 51-40-00 AND 51-20-51. 2H72 4T RTA13NM 20031002001362003100200136NM 2003 10 2 372PA0035 120030909A3350362624 LIGHT BOEING737 737306 13844BGNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 EMERGENCY FLOOR PATH LIGHTS OUT FROM ROW 6 FWD TO FRONT. REPLACED 5 EA. LUMI STRIPS. OPS CHECKS GOOD IAW MM 33-51-02. 2L72 4F RTA16NE 20031002001432003100200143NM 2003 10 2 CALA0300527 120030912A3350 CONNECTOR BOEING737 737524 1384721NM EMERGENCY LIGHT LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW2762631 27535 INSPECTION FOUND EMERGENCY LIGHT ABOVE LT OVERWING EXIT INOPERATIVE. MAINTENANCE FOUND DISCONNECT ON LT OVERWING EXIT LIGHT ASSEMBLY L-7 AND L-751 WITH LOOSE CONNECTOR D2976 AND LOOSE GROUND GD 1912-DC. RECONNECTED AND OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20031002001472003100200147NM 2003 10 2 03FDEA01470 120030909A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 MAIN CARGO DOOR STUB FRAME IS CRACKED AT O/B FLANGE THRU FASTENER HOLE 49 INCHES AFT OF FWD FRAME, 3 INCHES BELOW UPPER FRAME. REMOVED AND REPLACED PER SRM 51-30-2. 2L73 4F RTA3WE 20031002001682003100200168CE 2003 10 2 GMZ2003F00000 120030811A2121903840311 BLOWER BEECH 90 C90A 1152911CE PWA PT6 PT6A60 52043NE COCKPIT FAILED B GMZRO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0172TG 2001 LJ1252 BLOWER MOTOR WEARS OUT CAUSING BLOWER MOTOR TO START SMOKING FILLING THE AIRCRAFT WITH SMOKE. WHEN THE BLOWER MOTOR IS REMOVED AND INSPECTED. IT IS FOUND THAT THE BRUSHES ARE WORN OUT. RECOMMEND BLOWER ASSEMBLY BE CHANGED EVERY 1000 HOURS. IT WAS ALSO FOUND THAT WHEN THE BLOWER ASSEMBLY WEARS OUT NEITHER THE CIRCUIT BREAKER OR CURRENT LIMITER POPS. 1L72 3T4 TRT3A20 E4EA 20031002001762003100200176WP 2003 10 2 UPS03841220 120030912A3397 WIRE DOUG DC8 DC873 302199CWP BATTERY PACK LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS NOT PERATING PROPERLY. RESET CONNECTOR ON EMERGENCY LIGHT BATTERY PACK, OPS CK NORMAL. 2L74 4F RT4A25 20030930000822003093000082WP 2003 9 30 ABXA030355 120030818A53209910078679 DOUBLER DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 LEVEL II CORROSION BUTT LINE '0' F.S. 180 AT SHACKLE BOX. REPLACED SUBFLOOR DOUBLER WITH NEW FABRICATED DOUBLER AND INSTALLED IAW DC-9 SRM 53-01, 53-10-4, 53-10-3, 51-30-1, AND 51-30-2. 2L72 4F A6WE 20030930000892003093000089WP 2003 9 30 ABXA030360 120030821A53209910078215 STRUCTURE DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 COCKPIT SUBFLOOR HAD AREAS OF LEVEL II CORROSION, STA 160 RPL 32 TO 54. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20031001000182003100100018WP 2003 10 1 ARWA20030908 120030908A5411 SPAR CAP DOUG DC8 DC861 3021952WP NR 4 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1929UA 46159 DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON LT LOWER SPAR CAP WITH CRACK STA YOP 251 BY ACCESS DOOR NR 411. 2L74 4F 4A25 20031001000222003100100022NM 2003 10 1 QXEA200301083 120030827A5330 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 AFT FLOOR SUPPORT FOR PANEL 144CZ IS CORRODED AT STATION Y27R. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16, 51-40-00 AND 51-20-36. 2H72 4T RTA13NM 20031001000702003100100070NM 2003 10 1 2003UALA00708 120030921A7921 OIL COOLER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 1 ENGINE FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29615UA 21876 DIVERTED TO SYR DUE TO NR 1 ENGINE OIL PRESSURE INDICATION. REPLACED OIL COOLER. SHOP TEST CONFIRMED OIL COOLER MATRIX LEAKING INTERNALLY, ALLOWING FUEL TO CONTAMINATE THE ENGINE OIL SYSTEM. 2L72 4F4 FRTA1NM E3NE 20031001001042003100100104WP 2003 10 1 AMTA200301094 120030806A5320 STIFFENER LKHEED1011 10113851 5265010WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 ON APB RIGHT RADIAL STIFFENER IN C3 CARGO COMP AT STRINGER 25 CORROSION AROUND DRAIN HOLE. REPAIRED APB RT RADIAL STIFFENER AT STRINGER 25 IAW SRM 53-11-00. SEE M12A'S AND 156 FORMS FOR OTHER WORK ACCOMPLISHED AND PARTS FABRICATION. (M) 2L73 4F A23WE 20031001001262003100100126NM 2003 10 1 03FDEA01523 120030831A5730 SKIN DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING - UPPER SURFACE, STA 118 TO 162, FWD AREA BETWEEN FRONT AND REAR AREA, NUMEROUS PLACES FOUND CORRODED. LT WING UPPER SURFACE, NUMEROUS CORRODED PLACES AT FORWARD AREA BETWEEN FRONT AND REAR AREA STA 118 TO 162 BLENDED OUT AS PER SRM 51-21-01 VOL 2 WITH MATERIAL REMOVED : 0.035" FROM ORIGINAL THICKNESS = 0.170" AND FOUND WITHIN LIMIT AS PER EA 1-5750-73296 WITH TITLE : WINGS - WING STRUCTURE - LT UPPER WING SKIN CORROSION REPAIR. 2L73 4F RTA22WE 20031001001322003100100132WP 2003 10 1 GTIA030680 120030914A2612892809040001 CONTROL UNIT DOUG DC9 DC982 3022082WP LT FIRE LOOP MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23812NK 48021 LT ENGINE LOOP 'A' LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE. REMOVED AND REPLACED CONTROL UNIT. OPS CHECK NORMAL. (M) 2L72 4F A6WE 20031002000172003100200017NM 2003 10 2 GAIA03107OP 120030910A33501000679 LIGHT BOEING727 727224 1384076NM PAX DOOR INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW0769740 20668 DURING ROUTINE MAINTENANCE AT DEN, IT WAS DISCOVERED THAT THE MAIN ENTRY EMREGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031002000422003100200042WP 2003 10 2 GTIA030670 120030905A25304110001131 COFFEEMAKER DOUG DC9 DC983 3022083WP GALLEY ODOR A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 RUBBER BURNING ODOR IN AFT GALLEY. TURNED GALLEY POWER OFF SMELL WENT AWAY. FOUND NR 1 COFFEEMAKER WOULD NOT ACCEPT WATER BUT HEATED OK. REMOVED AND REPLACED NR 1 C/M IN AFT GALLEY. OPS CHECK NORMAL AND NO ODORS. (M) 2L72 4F RTA6WE 20031002000632003100200063NM 2003 10 2 QXEA200301089 120030827A5530 BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CONNECTION BRACKET IS CRACKED AT LEFT HAND STABILIZER STATION 716.00 AFT OF FRAME 4 AND STRINGER 4L. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-55-199. 2H72 4T RTA13NM 20031002001282003100200128NM 2003 10 2 AWXA200301039 120030827A532069165096 ANGLE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE FUSELAGEW CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .5 INCH CRACK WAS FOUND ON WEB ANGLE JUST AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 216. MAINTENANCE REMOVED CRACKED WEB ANGLE BS 348.20; FABRICATED A NEW REPLACEMENT WEB ANGLE IAW DWG 69-16509; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 39, FIG. 11. 2L72 4F4 FRTA16WE E2EA 20031002001662003100200166 2003 10 2 SWIA200312386 420030831A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM0716731 120190 SYSTEM ONE ON STALL WARNING TEST FAILS STICK PUSHER TEST, CAPTAINS. REMOVED AND REPLACED STALL WARNING COMPUTER IAW 27-00-00. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031003000032003100300003NM 2003 10 3 AALA20030741 120030707A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21656AA 24614 DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 18D INOPERATIVE. RECONNECTED EMERGENCY EXIT ILGHT WIRE AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000202003100300020WP 2003 10 3 AALA20030903 120030825A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY SIGN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21241AA 49254 RIGHT NR 2 EMERGENCY EXIT SIGN INOPERATIVE FOR NR 2 DOOR. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031003000512003100300051NM 2003 10 3 QXEA200301114 120030910A2910 LINE DHAV DHC8 DHC8202 2809007NM ZONE 200 RUPTURED A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09363PH 520 ON FLIGHT 2060 SEA TO YVR AIRCRAFT RETURNED TO FIELD DUE TO: AFTER GEAR RETRACTION NR 1 ENGINE HYDRAULIC PUMP CAUTION WARNING LIGHT ILLUMINATED. AT THE SAME TIME QUANTITY AND PRESSURE WENT TO ZERO. THE SYSTEM WAS WITHOUT PRESSURE FOR 25 MINUTES. WHEN STANDBY PUMPS WERE SELECTED GOT PRESSURE BACK. AIRCRAFT LANDED SAFELY. PRESSURE LINE WAS FOUND RUPTURED. REMOVED AND REPLACED PRESSURE LINE FROM EDP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031003000772003100300077NM 2003 10 3 03FDEA01528 120030830A5753ARC198414 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP INBD HINGE (FLAP SIDE) LOWER OUTBOARD ATTACHMENT BORE FOUND CORRODED. 2L73 4F RTA22WE 20031003000832003100300083SO 2003 10 3 RAIA00309236 120030904A7830 SWITCH EMB 145 EMB145 3260210SO THRUST REVERSER DIRTY A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03805HK 145096 THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE CLEANED BOTH STOW SWITCHES. 2L72 4F RTT00011AT 20031003000842003100300084SO 2003 10 3 RAIA00309237 120030908A25105041314011028 SHOULDER BELT EMB 145 EMB145 3260210SO COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03809HK 145187 FIRST OFFICERS SHOULDER HARNESS WILL NOT RETRACT OR EXTEND. MAINTENANCE REMOVED AND REPLACED SHOULDER HARNESS. 2L72 4F RTT00011AT 20031006000082003100600008WP 2003 10 6 MWEA030371 120030911A27617274555 CIRCUIT BREAKER DOUG DC9 DC981 3022081WP SPOILER TRIPPED A MWEAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL31805ME 48031 GROUND SPOILER CIRCUIT BREAKER POPPED. FOUND VOLTAGE DROP. RIGHT SPOILER CONTROL VALVE FAULTY. REMOVED AND REPLACED CONTROL VALVE. UNABLE TO DUPLICATE CIRCUIT BREAKER POPPING. REMOVED AND REPLACED SPOILER CONTROL CIRCUIT BREAKER. 2L72 4F A6WE 20031006000352003100600035NM 2003 10 6 QXEA200301121 120030911A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 FUSELAGE SKIN IS DENTED 5 INCHES LONG BY 2.4 INCHES WIDE BY .200 INCH DEEP, BELOW PILOTS WINDSHIELD FSX122.000 AND WLZ137.000. REPAIRED IAW Q400 TASK 51-00-02-250-801 AND RD 8/4-53-697. 2H72 4T RTA13NM 20031006000502003100600050EU 2003 10 6 DHL2003368012 120030916A3234 LEVER AIRBUS300 A300B4203 3930306EU MLG INOPERATIVE A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01368DH 207 LANDING GEAR LEVER LOCK AND WARNING SYSTEM NR 1 INOPERATIVE. AFTER T/O UNABLE TO RAISE THE GEAR, CREW PERFORMED ABNORMAL PROCEDURE AND SYSTEM NR 2 IS WORKING NORMALLY. CLEANED CONNECTORS 82GB, 83GB, 84GB, AND 85GB (MLG ELECTRICAL CONNECTORS). PERFORMED OPERATIONAL CHECK OF MLG SYSTEM NR 1 & 2 WARNING SYSTEM WITH NO DEFECTS NOTED. OPS CHECKED GOOD IAW M/M 32-30-00. 2L72 4F RTA35EU 20031006000602003100600060CE 2003 10 6 AMWA34 120030907A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV UE163 RIB AT CSS 54.026 CRACKED AT STRG. 101-640000-47 STRG. P/N 101-640000-42 RT SIDE AND STRG 101-640000-43 STRG P/N 101-640000-39 STRG P/N 10164000041 5 EA CRACKS ON THIS RIB) 2L72 4T RTA24CE 20031001000462003100100046WP 2003 10 1 UPS03841191 120030811A522038884061 FITTING DOUG DC8 DC873F 302199FWP EMERGENCY EXIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, RT FORWARD TYPE 1 DOOR HAS CORROSION INSIDE OF FASTENER HOLE AT AFT LOWER CORNER. REMOVED FITTING IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW DC8 SRM 51 -1-8. MATERIAL LOSS TO 0.00 FROM .185, FOUND BEYOND LIMITS IAW DC8 SRM 52 -2-0 AND DAC DWG 3888406. LOCATED AND DRILLED NEW FITTING P/N 388406 -1 IAW DC8 SRM 51-3-2. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AN D 51-3-0 2L74 4F RT4A25 20031001000732003100100073NE 2003 10 1 2003UALA00711 220030923A7261 OIL SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 ENGINE OVERHEATED A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29549UA 25397 717982 RETURNED TO FIELD DUE TO HIGH OIL TEMPERATURE NR 2 ENGINE. FUEL OIL HEAT EXCHANGER AND VALVE WERE REPLACED AND PROBLEM SEEMED FIXED. NO DISCREPANCIES FOR NEARLY FOUR WEEKS. THEN LOW OIL QUANTITY AND INCREASING OIL TEMPERATURE HIT AGAIN. NO. 5 BEARING PRESSURE AND SCAVENGE TUBES REPLACED WITH NO EFFECT. ROOT CAUSE FINALLY FOUND AS THE RETAINING STUDS ON THE GEARBOX SCAVENGE PUMP FAILED AND ONE HELICOIL STRIPPED. COA WRITTEN TO INCORPORATE FIX. COA ACCOMPLISHED ON THIS ENGINE AND NO FURTHER DISCREPANCIES FOUND. 2L72 4F4 FRTA2NM E17NE 20031001001092003100100109WP 2003 10 1 G6OA071 120030722A1430NAS6208160 BOLT DOUG DC10 DC1030F 3023504WP WORN A G6OAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27605GC 47925 AIRCRAFT PERFORMED AN AIR RETURN SAFELY DUE TO UNABLE TO PRESSURIZE AFTER TAKE OFF. DURING TROUBLESHOOTINGFOUND GROUND SENSE ROD LOOSE. R/R UPPER BOLT PER MM 32-21-01 2L73 4F RTA22WE 20031001001182003100100118NM 2003 10 1 USAA030174 120030822A5315 FLOORBEAM BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US 23984 FOUND BEAM CORRODED .5 INCH BY 4 INCHES, FLOORBEAM 986.5 RBL 15 AND RBL 29. UPPER FLANGE REPAIR PER TYPICAL REP 53-60-01 REV A. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2L72 4F RTA16WE 20031001001252003100100125NM 2003 10 1 03FDEA01588 120030919A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OUTBOARD FLAP HINGE (FLAP SIDE) FOUND CORRODED ON INBD AND OUTBOARD ACTUATOR LUG BORES AND SPOT FACES. RT OUTBD FLAP HINGE (FLAP SIDE) INBOARD AND OUTBOARD ACTUATOR LUG BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT AS PER EA 1-5750-72684 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031002000182003100200018NM 2003 10 2 GAIA03108OP 120030912A3240211473 BRAKE ASSY BOEING727 727225 1384077NM RT MLG DRAGGING A GAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07936PG 22441 FLT 372 - LAX-PHX-FWA, DURING TAXI TO DEPARTURE, THE FLIGHT CREW NOTICED THE NR 3 BRAKE DRAGGING. REMOVED AND REPLACED THE NR 3 BRAKE AND THE NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031002000252003100200025WP 2003 10 2 GTIA030678 120030914A3260833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP NLG INOPERATIVE A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23826NK 49391 MYR - FLT 382 - NOSE GEAR RED LIGHT FLICKERS IN FLIGHT PUMPS ON HIGH GOES OUT. R & R NOSE GEAR UP PROXIMITY SENSOR D1-31. SYSTEM OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20031002001222003100200122NM 2003 10 2 QXEA200301106 120030827A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 LEFT SIDE FUSELAGE SKIN INTERIOR SURFACE IS NICKED .2500 INCH LONG AND 6 INCHES AFT OF FRAME X253.4 ABOVE STRINGER 22. REPAIRED IAW DHC-8 SRM 51-20-11, 51-00-06, 51-00-04 AND RD 8-53-7513. 2H72 4T RTA13NM 20031002001712003100200171WP 2003 10 2 WVE2003F00012 220030808A720030728692 SPLINE ADAPTER LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP ALTERNATOR CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09419FX 125 P116242 DURING 600 HOUR INSPECTION OF THE ALTERNATOR SPLINE ADAPTOR, IT WAS FOUND TO BE CRACKED. (EA09200301366) 2L72 4F4 FRTT00008WIE6WE 20031003000222003100300022NM 2003 10 3 AALA20030815 120030730A3350 CONTROL PANEL BOEING757 757223 1384957NM EMERGENCY LIGHT DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 DURING OVERNIGHT MAINTENANCE, 'UNARMED LIGHT' ON EMERGENCY LIGHT PANEL DOES NOT ILLUMINATE IN THE 'OFF' POSITION. REPLACED EMERGENCY LIGHT PANEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000452003100300045NM 2003 10 3 AWXA200301049 120030814A5330654576988 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1.250 CRACK WAS FOUND ON FUSELAGE EXTERNAL SKIN FROM FASTENER HOLE AT AFT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 450, BL 0 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER, 2 EACH FILLERS, AND SPACER RING; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5312-03248-SH1. 2L72 4F RTA16WE 20031003000552003100300055SO 2003 10 3 C2XA03TY159 120030911A531514521699003 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM TOP CAP WAS FOUND TO BE CORRODED UNDER SEAT TRACK LF1. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02 AND M.M. 53-01-06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030822001652003082200165WP 2003 8 22 UPS03841021 120030721A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 RIGHT L/E LOWER RIB IS CRACKED AT XFS 347.750. REMOVED EXISTING REPAIR ANGLE, NDT VERIFIED CRACK IS TERMINATED AT STOPDRILL, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030822001672003082200167WP 2003 8 22 UPS03841023 120030726A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 MAIN CABIN LONGERON 16L IS CRACKED AT STA 1750. REMOVED LONGERON SECTION STATION 1742 TO 1765, FABRICATED AND INSTALLED LONGERON SECTION, SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 11. 2L74 4F RT4A25 20030822001762003082200176NM 2003 8 22 UPS03441077 120030724A532065B0424325 TIE CLIP BOEING747 747123 1384873NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D STA 1901 STR 23R TIE CLIP FOUND CRACKED. M/D STA 1901 STR 23R TIE CLIP REPLACED IAW SRM 51-10-01 P8. 2L74 4F4 F A20WE E20EA 20030822001792003082200179NM 2003 8 22 UPS03441080 120030725A531065B048418 SHEAR TIE BOEING747 747123 1384873NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D: BS 1820 FRAME SHEAR TIE FOUND CRACKED AT LOWER RIVET HOLE AS MARKED BETWEEN S22R AND S23R. M/D- BS 1820 FRAME SHEAR TIE BETWEEN S22R - S23R REPLACED IAW SRM 51-10-01 P.8 2L74 4F4 F A20WE E20EA 20030822001842003082200184NM 2003 8 22 UPS03241123 120030819A3350 BATTERY BOEING727 72751C 1384015NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01904UP 18946 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BOTH NOT WORKING. REMOVED AND REPLACED BATTERIES. OPS CK GOOD. 2L73 4F A3WE 20030825000062003082500006NM 2003 8 25 UPS03M41011 120030514A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 INSPECTION TYPE C :CABIN SEAT TRACK AT STA 1321 TO STA 1341 LBL 27.5 FOUND CORROSION. CORROSION REMOVED AT STA 1321 TO STA 1341 LBL 27.5 SEAT TRACK AT CAB IN FOUND EXCEED LIMIT IAW SRM 53-70-00 VOL I FIG 3 REV 32. CORRODED AREA TRIMMED OFF IAW SRM 53-70-00 VOL I REV 32 FIG 1. NEW SEAT TRACK REWORKED AND INSTALLED IAW SRM 53-70-00 VOL I FIG 1 REV 3 2 2L73 4F RTA22WE 20030825000092003082500009NM 2003 8 25 UPS03240962 120030606A5313 STRINGER BOEING727 727185C 138406NNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C SUSPECTED CORROSION AT BS 1180 STR. 20R REPAIR CARRIED OUT IAW SRM 51-10-06, SRM 53-30-01 & 53-30-02. NEW STRINGER ENDS INSTALLED, FASTENERS INSTALLED IAW SRM 51-30-02. LAP REFASTENED IAW UPS EO. 2L73 4F A3WE 20030825000122003082500012NM 2003 8 25 UPS03240966 120030607A5320 STIFFENER BOEING727 727185C 138406NNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C CORROSION ON LT 870 MID SECTION ATTACHMENT TO BULKHEAD STIFFENER REPAIR CARRIED OUT IAW SRMO EO 2003-038-006 SRM 51-30-02, UPS EO B72 7-5310-3056 AND DRAWING 65C23231 UPS ENG. FILE NO. 727-53-20118 2L73 4F A3WE 20030825000132003082500013NM 2003 8 25 UPS03440960 120030619A5330 SKIN BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C FX - FUSELAGE EXTERIOR SKIN CORROSION CRACKED AT RIVET HOLE AREA AT STA 2200, S40R - S42R AS MARKED. FX EXTERIOR SKIN REPAIRED AT BS 2200 STR 40R - STR 42R IAW SRM 53-30-03 FIG 1 DUE TO CORROSION CRACKED AREA TRIMMED 2.75 INCHES X 3 INCHES. 2L74 4F A20WE 20030825000142003082500014WP 2003 8 25 UPS03840976 120030626A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 STA. 1260-1280 LONG. 36 IS CRACKED, CUTOUT DAMAGED SECTION,FABRICATED AND INSTALLED LONGERON SECTION, STRAPS,CHANNELS AND DOUBLERS IAW UPS ENGINEERING FILE NUMBER DC8-53-20339 DATED 07/13/03,AND SAA SK 807-542 REV. IR DATED 06/27/03 2L74 4F RT4A25 20030825000162003082500016WP 2003 8 25 UPS03840978 120030617A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 LT WHEEL WELL AFT BULKHEAD LOWER SIDE OF CANTED WEB IS CORRODED BEYOND LIMITS STA 980-992 BETWEEN LONG 28L AND 31L CUTOUT CORRODED AREA ON BULKHEAD AND SKIN FABRICATED AND INSTALLED DOUBLER,FILLER,FINGER DOUBLERS,SKIN SEGMENT AND CANTED FRAME IAW DWG 5646444,AND EO DC8-5320-18960-A DATED 07/08/03,DC8-5330-18949- B DATED 07/08/03,SAA SK 807-683 REV. IR DATED 06/27/03 2L74 4F RT4A25 20030825000252003082500025WP 2003 8 25 UPS03840907 120030605A5330 SKIN DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C3 LOWER FUSELAGE CENTER SECTION AT FS 1350 LONGERON 34L FUSELAGE SKIN IS CRACKED. REMOVED 2 EA EXISTING REPAIR DOUBLERS, TRIMMED OUT CRACK FS 1350 LONG 34L FABBED REPAIR DOUBLER COMBINING 2 EA EXISTING REPAIR DOUBLERS, FABBED SKIN FILLERS AND FINGER DOUBLER ALL IAW DC8 SRM 53-2-1 FIG 7 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER, S KIN FILLERS AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7. 2L74 4F4 FRT4A25 1E8 20030825000422003082500042WP 2003 8 25 UPS03840890 120030617A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 RIGHT WING OB. LE. LOWER SKIN IS CRACKED AT XFS 628 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. DC8-5720-4087-B 2L74 4F RT4A25 20030825000452003082500045NM 2003 8 25 UPS03441097 120030718A541265B9031077 BULKHEAD BOEING747 747123 1384873NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C NR 1 PYLON REAR MOUNT BULKHEAD CRACK FOUND AT I/B FWD WEB EDGE NAS 221. NR 1 PYLON REAR MOUNT BULKHEAD REPAIRED IAW HX RS R54-53-35042 AND UPS ENGINEERING FILE NUMBER 747-54-20038. 2L74 4F A20WE 20030825000502003082500050NM 2003 8 25 UPS03441131 120030726A5712112U804065 RIB BOEING747 747123 1384873NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C LT WING NR 2 NACELLE RIB POST 4EA ATT HOLES FOUND CRACK INDICATIONS AT FRONT SPAR WEB. NR 2 NACELLE RIB REPLACED AS PER EO B747-5720-11421-F AND LH FRONT SPAR WEB REPLACED AS PER EO B747-5720-11421-F 2L74 4F A20WE 20030821001132003082100113NM 2003 8 21 03FDEA00880 120030616A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 CORROSION (C53-113-01) FWD CARGO STA 640, RBL 4 - LBL 4 OF FRAME SHEAR TIE. 2L73 4F RTA3WE 20030821001792003082100179NM 2003 8 21 03FDEA01274 120030806A5753 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 SNRM N0478: RT INBOARD FLAP HINGE (FLAP SIDE), PIVOT HOLES CORRODED AT INBOARD AND OUTBOARD BORES. 2L73 4F RTA22WE 20030821001802003082100180NM 2003 8 21 03FDEA01273 120030813A5753 RIB DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBOARD FLAP NOSE RIB SUPPORT ISLAND FOUND 01 CRACK AT OUTBOARD SIDE APPROX .1875 INCH LONG. RT OUTBD FLAP NOSE RIB DAMAGED SUPPORT ISLAND CARRIED OUT REPAIR IAW FEDEX EA 1-5750-63119, TITLE- WINGS- TRAILING EDGE FLAPS- OUTBOARD TRAILING EDGE FLAP- SECONDARY UP STOP- REPAIR. 2L73 4F RTA22WE 20030822000262003082200026NM 2003 8 22 03FDEA01095 120030711A5270 SWITCH BOEING727 727200 138407ENM CARGO DOOR DEFECTIVE A FDEAIA CABIN DEPRESSURIZATION UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25270FE 22035 MAIN CARGO DOOR LIGHT ILLUMINATED INFLIGHT AFTER T/O PSI DIFFERENTIAL WAS 1 PSID PACKS OFF, AIRCRAFT DEPRESS MAIN CARGO DOOR LIGHT WENT OUT. AIR TURNBACK, MAIN CARGO DOOR LIGHT WAS INTERMITTENT ON TAXI BACK TO GATE. ADJUSTED THE LOCK SWITCHES PER EO (.040" GAP..7EA) SWITCH S9038 IS DEFECTIVE, GOT HOT TO THE TOUCH AND IT'S END IS DENTED IN FROM THE TARGET HITTING IT. INSTALLED SWITCH S9038 IAW 727-200WDM52-71-01. MADE ADJUSTMENT WITH REFERENCE TO EO 7-5230-7-2347, LOCKWIRED SAME, TEST OF MAIN CARGO DOOR WARNING SYSTEM MADE WITH REFERENCE TO 727-200 AMM 52-70-009-5, NORMAL INDICATIONS WERE OBSERVED THROUGH NUMEROUS ATTEMPTS. 2L73 4F RTA3WE 20030822000282003082200028NM 2003 8 22 03FDEA01083 120030710A52436556235159 DOOR BOEING727 727200 138407ENM HYD SERVICE MISSING A FDEAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 SO25220FE 20934 HYDRAULIC SERVICE AREA ACCESS PANEL MISSING FROM A/C. REPLACED DOOR IAW SMP. OK FOR SERVICE. 2L73 4F RTA3WE 20030822000312003082200031NM 2003 8 22 03FDEA01044 120030705A5514ALC81071 FITTING DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT HORIZONTAL STABILIZER NR 26 BORE CORROSION EXCEEDED LIMIT. LEFT HORIZONTAL STABILIZER NR 26 FITTING FABRICATED IAW FEDEX EA 1-5510- 71836, STABILIZERS- HORIZONTAL STABILIZER BARREL NUT BORES- CORROSION REMOVAL- BORE 26 LEFT- FITTING ALC8107-1- FABRICATION AND INSTALLED AS PER SRM 51-33-01VOL II. 2L73 4F RTA22WE 20030822000392003082200039EU 2003 8 22 2003UALA00473 120030605A3610ABS073764 SEAL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE A/C BAY DEFECTIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29445UA 826 RETURN TO FIELD DUE TO ECAM RIGHT WING LEAK. WITH NR 1 BLEED SYSTEM ALREADY DEFERRED INOPERATIVE, AIRCRAFT EXPERIENCED LOSS OF BLEED SYSTEM NR 2 DUE TO RIGHT WING AIR LEAK. REPLACED SEALS AND COUPLING AT RIGHT PACK HEAT EXCHANGER. SUBSEQUENT MAINTENANCE INCLUDED REPLACEMENT OF DEFECTIVE SEALS AFT OF THE NR 2 ENGINE PRECOOLER. 2L72 4F4 FRTA28NM E40NE 20030822000532003082200053NM 2003 8 22 UPS03441059 120030718A2520 REVEAL BOEING747 747123 1384873NM CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT BS 2231 BETWEEN 15R AND 16R STRINGER AREA UPPER REVEAL FOUND CRACKED. REVEAL PANEL REPAIRED AS PER SRM 53-10-04 FIG 91. 2L74 4F A20WE 20030822001742003082200174WP 2003 8 22 UPS03841094 120030723A55425644210505 SKIN DOUG DC8 DC873F 302199FWP RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 SKIN CRACKED LT SIDE OF RUDDER AT BASE AT ZR 61. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER AND BALANCED RUDDER IAW SRM 55-2-0 FIG 2 AND 51-4-6. 2L74 4F RT4A25 20030822001752003082200175EU 2003 8 22 UPS03141088 120030812A3350 POWER SUPPLY AIRBUSA300 A300F4622R 3930360EU CABIN INTERMITTENT A IPXAK NONE O OTHER NRNOT REPORTED 1 SO01152UP 0834 INSPECTION TYPE: N/A WITH OVERHEAD EMERGENCY EXIT LIGHT SWITCH IN THE ARMED POSITION. ALL EXIT LIGHTS CAME ON INTERMITTENTLY IN FLIGHT. REPLACED EPSU P33-51-14, OPS CHECK OK 2L72 4F RTA35EU 20030825000652003082500065NM 2003 8 25 UPS03241070 120030714A5755 PANEL BOEING727 72725C 138400HNM NR 3 SPOILER DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C NR 3 SPOILER PANEL LOWER SURFACE DISBOND AT ACTUATOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-40-05. 2L73 4F A3WE 20030825000732003082500073WP 2003 8 25 0301439153 120030731A291659137045504 RESERVOIR DOUG DC9 DC914 3022034WP HYD SYSTEM DEFECTIVE A NWAAH DEACTIVATE SYST/CIRCUITS K FLUID LOSS CRCRUISE 1 GL018912E 45829 WHILE AT CRUISE, THE RIGHT HYDRAULIC PRESSURE LOW ANNUNCIATOR LIGHT ILLUMINATED. THE RIGHT HYDRAULIC PRESSURE AND HYDRAULIC QUANTITY INDICATORS WENT TO ZERO. COMPLIED WITH COM PROCEDURES AND LANDED WITH LANDING GEAR DOORS OPEN. MAINTENANCE FOUND THE RIGHT HYDRAULIC SYSTEM RESERVOIR AND ACCUMULATOR BAD AND REPLACED THEM ALONG WITH THE NR 2 ENGINE DRIVEN PUMP. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030825000752003082500075NM 2003 8 25 C1HA200381026 120030810A5320 INTERCOSTAL BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON INTERCOSTAL BS 305 RBL 40. 2L73 4F A3WE 20030825001012003082500101NM 2003 8 25 03FDEA01316 120030815A3234 LATCH BOEING727 727200 138407ENM COCKPIT STUCK A FDEAK NONE O OTHER CLCLIMB 1 SO25206FE 22928 AFTER T/O FROM KGEG F2 F/O COULD NOT RAISE THE LANDING GEAR LEVER BEYOND THE OFF POSITION. FOLLOWED RED TABS LANDING GEAR LEVER LATCH FAILED TO RELEASE. CHECKLIST, CHECK 2F RESET P6- 3 LANDING GEAR 2 LEVER LATCH 2 FLIGHT CB. LANDING GEAR THEN RETRACTED. 2L73 4F RTA3WE 20030825001202003082500120 2003 8 25 ABXA030326 420030812A344259100913 RADOME DOUG DC9 DC941 302207NWP NOSE OUT OF TOLERANCEA ABXAA UNSCHED LANDING O OTHER CLCLIMB 1 GL23964AX 47781 RADAR PAINTS STREAK OF GROUND RETURNS AT 60 DEGREES RIGHT OF NOSE ON COUNTER CLOCKWISE SWEEP. SOUNDS LIKE RADAR HITS DOME ON CLOCKWISE SWEEP. FOUND RADAR DRIVE PLATE BINDING AGAINST RADOME STATIC DISCHARGE STRIP PLASTIC NUT PLATES. REPLACED THE RADOME ASSEMBLY. 2L72 4F A6WE 20030825001232003082500123NE 2003 8 25 AWXA200300812 220030718A7532658385 BLEED VALVE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 1 ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28182AW 22649 DEN - ABORTED TAKEOFF - FLT 0640 - DURING TAKEOFF ROLL AT DEN EN ROUTE FOR PHX, A LOUD "BANG" CAME FROM THE NR 1 ENGINE, REJECTED TAKEOFF, SUSPECT COMPRESSOR STALL. MAINTENANCE PERFORMED A BORESCOPE INSPECTION IAW T/C I5M72008, NO DAMAGE NOTED. REMOVED AND REPLACED THE PRESSURE RATIO BLEED CONTROL IAW T/C R5M75002. LUBRICATED BLEED VALVES IAW BMM 75-31-0, AND PERFORMED A HIGH POWER ENGINE RUN, SYSTEM OPERATES NORMALLY. VENDOR FUNCTIONAL TEST OF PRESSURE RATIO BLEED CONTROL S/N 6159383 COULD NOT CONFIRM REASON FOR REMOVAL, NO FAULT FOUND. TESTED IAW CMM 75-31-01 AND RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20030825001352003082500135SO 2003 8 25 C2XA03TY134 120030820A339766367 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED 2C INSPECTION THE NR 5 PROXIMITY LIGHTING STRIP HAD A BROKEN WIRE. MAINTENANCE REPAIRED THE BROKEN WIRE AND OPS CHECKED GOOD IAW EMB 145 AMM 33-50-00. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030825001412003082500141WP 2003 8 25 GTIA030606 120030630A2752 FITTING DOUG DC9 DC982 3022082WP T/E FLAP CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND LEFT INBOARD FLAP INBOARD ACTUATOR ATTACH FITTING CRACKED AT MLG TRAP FITTING. REMOVED CRACKED FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20030825001502003082500150 2003 8 25 AALA20030673 420030616A3416 ALTIMETER BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAK NONE J WARNING INDICATION CRCRUISE 1 SW21354AA 24035 DFW - FLT 946 - CAPTAINS ALT INOPERATIVE. REPLACED CAPTAINS ALT IND, ACCOMPLISHED REQUIRED INSTALLATION TEST . GROUND CHECKS GOOD. (M) 2L72 4F RTA1NM 20030825001522003082500152NM 2003 8 25 AALA20030692 120030616A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21369AA 25196 AFW - FOUND CORROSION ON BEAM RBL 11.06 STATION 798 OUT OF SRM LIMITS. REMOVED CORROSION PER SRM. DYE PENETRANT CHECKED AREA AFTER BLENDING FOR CRACKS, ROTO-PEENED AREA, APPLIED ALODINE AND TWO COATS OF PRIMER. FILLED BLENDED AREA WITH BMS 5-95. (M) 2L72 4F RTA1NM 20030825001602003082500160WP 2003 8 25 GTIA030601 120030725A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 160 LEFT OUTBOARD FLOOR PANEL HAS SOFT/MUSHEY CORRODED AT INSERTS. REFAB FORWARD CABIN FLOOR PANEL. (M) 2L72 4F RTA6WE 20030825001622003082500162WP 2003 8 25 GTIA030599 120030725A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND FORWARD CABIN STATION 200-260 LEFT SIDE FLOOR PANEL HAS CRACK/DAMAGED AND CORRODED AT INSERTS. FORMED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030825001662003082500166SO 2003 8 25 C2XA03BT073 120030721A32201170A330001 COLLAR EMB 145 EMB145ER 3260211SO NLG DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27169441128811288 145045 BTV---CO 2943, DURING 2A INSPECTION FOUND DENT/CRACK DAMAGE TO NOSE LANDING GEAR COLLAR . DURING REMOVAL PROCESS FOR REPLACEMENT OF THE DAMAGED COLLAR, INSPECTED AND FOUND SLIDING TUBE ASSEMBLY DAMAGED AND INNER BORE OF NOSE LANDING GEAR DAMAGED (DEEPLY SCORED) CAUSED BY LOCKING BOLT SHEARED ON TOP OF THE STRUT BARREL. REMOVED AND REPLACED NOSE LANDING GEAR ASSEMBLY IAW EMB145 AMM NR 32-20-01 WITH SERVICEABLE UNIT, OPS. CHECKED AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030825001682003082500168WP 2003 8 25 DHL2003873513 120030617A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 ITEM REF.: N/R 1815.: LT WING INBD. L/E FORMER CRACKED 0.250 AT STA. XFS.678.750. CORR.: REMOVED FASTENERS IAW SRM 51-1-21 PG.1. STOP DRILLED CRACK IAW SRM 57-2-0 PG.9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG.9-10, SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030821002912003082100291EU 2003 8 21 03206327 120030725A33506047051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27327UE 41080 DURING INSPECTION THE CREW REPORTED THE EMERGENCY TRACK LIGHTING BETWEEN ROW 3A AND 4A WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK AND REPLACED TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4T RTA41NM 20030822000272003082200027NM 2003 8 22 03FDEA01210 120030729A5753ARC70551 TEE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71878, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RIGHT OUTBOARD FLAP NR 2, 3, 4 AND 5 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20030822000572003082200057NM 2003 8 22 03FDEA01171 120030726A5320A5A7114517 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 CTR CARGO RT TUNNEL STA 5-123 LONGERON 38 SPLICE FITTING FOUND CRACK. CTR CARGO RT TUNNEL STA 5-123 LONGERON 38 SPLICE FITTING FABRICATED AS PER DWG A5A7114 & INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20030822000662003082200066NM 2003 8 22 03FDEA01008 120030630A2913 PUMP DOUG MD11 MD11 3023602NM HYD SYSTEM FAILED A FDEAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO25619FE 48770 HYD PUMP 1R OFF DISPLAYED DURING CRUISE AT FL280. PUMP 1R FAULT LIGHT ON HYD OVERHEADD ILLUMINATED. HYD SYS 1 TEMP INDICATED 94 DEG C. SUBSEQUENTLY HYD 1 OFF ALERT AND NR 2 AUTOPILOT DISCONNECT. RETURNED TO RPLB. TEMP DECREASED TO 79 DEG C, WHEN ON APPROACH. SLATS EXTENDED, BOTH PUMPS ON, NORMAL FLAP AND GEAR EXTENSION. NO A/P WITH LOWER YAW DAMP INOP. FACT: REMOVED AND REPLACED 1L AND 1R EDP AND CASE DRAIN FILTERS. FLUSHED HYD SYSTEM. OP/LEAK CHECKS GOOD ON ENGINE RUN. 2L73 4F RTA22WE 20030822000912003082200091NM 2003 8 22 03FDEA01055 120030702A5753ARC199114 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT WING OUTBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT LUG BUSHING FOUND LOOSE. RT WING OUTBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT LUG LOOSE. BUSHING REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030822001352003082200135EA 2003 8 22 QXEA200300942 120030731A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 BOI- CENTER CHIMNEY DAMAGED. REMOVED AND REPLACED DAMAGED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030822001542003082200154NM 2003 8 22 QXEA200300944 120030803A1430 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM EXTERIOR LIGHT STRIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX- RED ANTI-COLLISION LIGHT HAS TWO NUT PLATES STRIPPED OUT. REPAIRED IAW Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030822001612003082200161NM 2003 8 22 UPS03441117 120030723A5313BAC14981457075 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C FWD CARGO COMPT- LT STA 780 - STA 800 STRINGER 47L FOUND CORROSION. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 DUE TO CORROSION CRACK LENTH WAS 1-45 INCH LENGTH WHICH EXCEEDED SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F A20WE 20030822001622003082200162NM 2003 8 22 UPS03441121 120030814A3350 LIGHT BOEING747 747123 1384873NM CABIN FAULTY A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:N/A EMERGENCY LIGHT AT OVERHEAD AT UPPER DECK SLIDE COMES ON AND GOES OFF APPROX 5 SEC AFTER SWITCH TURNED ON. REMOVED AND REPLACED EMERGENCY LIGHT PER MM REF 33 51 07. OPS CHECK NORMAL. 2L74 4F A20WE 20030826000172003082600017NM 2003 8 26 03FDEA01363 120030807A5730ARB73952 SKIN DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING UPPER SURFACE AT OUTBOARD OF OUTBOARD AILERON FOUND WITH MINOR CORROSION. RT WING UPPER SURFACE AT OUTBD OF OUTBD AILERON MINOR CORROSION REMOVED AS PER FEDEX EA 1-5710-71785 - WINGS - WING STRUCTURE - RT UPPER SURFACE CORROSION. 2L73 4F RTA22WE 20030826000292003082600029NM 2003 8 26 03FDEA01375 120030806A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RT WING OUTBOARD FLAP INBOARD HINGE BRACKET(FLAP SIDE) INBOARD PIVOT HOLE FOUND CORROSION. RT WING OUTBD FLAP INBD HINGE BRACKET (FLAP SIDE) INBOARD PIVOT HOLE REPAIR CARRIED OUT PER FEDEX EA 1-5750-71799, WINGS- LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20030826000312003082600031NM 2003 8 26 03FDEA01377 120030808A5753ARC70561 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING OUTBOARD FLAP VANE NR 4 FITTING FWD HOLE FOUND CORROSION. RT WING OUTBD FLAP VANE NR 4 FITTING FWD HOLE CARRIED OUT REPAIR AS PER EA 1-5750-71794 (WINGS - RIGHT AND LEFT OUTBOARD FLAP - NR 4 FITTING SUPPORT VANE TO TRACK CORROSION). 2L73 4F RTA22WE 20030826000322003082600032NM 2003 8 26 03FDEA01378 120030808A5753ARC70541 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LT WING OUTBOARD FLAP VANE NR 2 FITTING FWD HOLE FOUND CORROSION. LT WING OUTBD FLAP VANE NR 2 FITTING FWD HOLE CARRIED OUT REPAIR AS PER EA 1-5750-71793 (WING - LEFT OUTBOARD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK CORROSION). 2L73 4F RTA22WE 20030826000362003082600036NM 2003 8 26 03FDEA01341 120030819A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 AFT AIRSTAIR, HAS A GOUGE ON THE EXTERNAL SKIN, 40 INCHES FROM THE LOWER END. EVALUATED GOUGE ON AFT AIRSTAIR EXTERNAL SKIN 40 INCHES FROM LOWER END. FOUND GOUGE TO BE .012 INCHES DEEP. ORIGINAL THICKNESS IS .040. FOUND TO BE OUT OF LIMITS PER SRM 52-00-2. REMOVED DAMAGE IN AN AREA OF 2.25 X 4.25 INCHES. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 52-10-2. 2L73 4F RTA3WE 20030826000382003082600038NM 2003 8 26 03FDEA01339 120030819A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 DENT IN SKIN AT EDGE OF MAIN CARGO DOOR CUTOUT BS 620 ABOVE STR 17L. REWORKED DENT IN SKIN AT EDGE OF MAIN CARGO DOOR CUTOUT, BS 620, ABOVE STR 17L PER EA 7-5330-70490. 2L73 4F RTA3WE 20030826000402003082600040NM 2003 8 26 03FDEA01337 120030819A5312 PRESSURE PANEL BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 NOSE LANDING GEAR FWD RT PRESSURE ACCESS PANEL SKIN CUTOUT IS GOUGED. REPAIRED FWD RT PRESSURE ACCESS PANEL SKIN AT NOSE LANDING GEAR. ALL WORK DONE IAW SRM 51-40-2. 2L73 4F RTA3WE 20030826000442003082600044NM 2003 8 26 03FDEA01192 120030730A5720ANB7445 SHIM DOUG MD11 MD11 3023602NM RT WING OUT OF POSITION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT WING ROOT UPPER SURFACE- STRINGER NR 1 SHIM FOUND SEPARATED INTO 2 VISIBLE PIECES AND EACH WITH MIGRATION OF: (1) 0.7 INCH FWD AND 0.5 INCH DOWN AND (2) 0.6 INCH DOWN. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION. 2L73 4F RTA22WE 20030826000482003082600048NM 2003 8 26 03FDEA01165 120030723A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT WING- O/B FLAP (FLAP SIDE) I/B HINGE O/B PIVOT HOLE CORRODED. RIGHT WING- O/B FLAP (FLAP SIDE) I/B HINGE O/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RIGHT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030826000542003082600054WP 2003 8 26 03FDEA01143 120030725A5753FXARC2744502 FLAP DOUG DC10 DC1010 3022110WP RT WING DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 RIGHT INBOARD FLAP T/E DELAMINATED AS MARKED. CLOSING ACTION ON 07/20/03 REMOVED 4 EACH SECTIONS OF TRAILING EDGE IAW M/M 51-31-01. FABRICATED 4 EACH SECTIONS OF T/E ON TRAVELERS T2/347267, T2/347290, T2/347288. FABRICATED Z-ANGLE ON TRAVELER T2/347381. INSTALLED FOUR EACH SECTIONS OF T/E AND Z-ANGLE IAW SRM 57-20-00, PAINTED AREA IAW SRM 51-21-02. 2L73 4F A22WE 20030826000622003082600062CE 2003 8 26 5300051903 120030519A216099125182 CONTROL VALVE CESSNA560 560XL 2076702CE CABIN TEMP FAILED E S4WAK NONE O OTHER CRCRUISE 1 WP07613GY347 5605300 NO CONTROL OF COCKPIT TEMPERATURE. 2L72 4F RTA22CE 20030826000632003082600063 2003 8 26 2904050703 420030507A23129710831 TRANSCEIVER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP074027Q3252 2904 9456 TECHNOSONIC TFM-500 RADIO WILL NOT POWER UP. 1G71 3U3 U H9EU E00054EN 20031003000672003100300067SO 2003 10 3 C2XA03TY163 120030913A532014521721005 STRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719503 145176 TYS DURING A SCHEDULED 2C INSPECTION THE FWD DIGITAL IN GALLEY WAS FOUND CORRODED. MAINT. R/R THE FWD DIGITAL,ALLODINED,PRIMED AND PAINTED IAW EMB 135/145 SRM 53-21-10 AND EMB 135/145 CPM51-21-04,05,06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031006000022003100600002SO 2003 10 6 C2XA03CL164 120030911A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714933 145018 CLE FLIGHT NR 2278 THE CREW REPORTED THE EMERGENCY EXIT SIGN BEHIND THE F/A SEAT WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031006000192003100600019EU 2003 10 6 MALA030411 120030812A5260 TRACK BAC 146 AVRO146RJ85A1500097EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK INSPECTION IN CVG, IB AIRSTAIR RAIL CORROSION. MAINTENANCE REMOVED AND REPLACED RAIL. REFER TO 409 NR 190256 FOR DETAIL, A/C RELEASE DATE 9/2/03. 2H74 4F RTA49EU 20031006000382003100600038NM 2003 10 6 QXEA200301124 120030913A5720 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 L-ANGLES ATTACHING RT HAND WING INBOARD FLAP WELL (U) CHANNELS NR 2, NR 6 AND NR 7 TO AFT SPAR ARE CRACKED. REPAIRED IAW EA 6-57-166 AND 6-57-167. 2H72 4T RTA13NM 20031006000412003100600041NM 2003 10 6 QXEA200301126 120030911A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 NUMEROUS DENTS AFT OF ICE SHIELD RT SIDE X281.0 - X301.0 BETWEEN STRINGERS 17S AND 20S. REPAIRED IAW Q400 RD 8/4-53-658 AND EA 6-53-253. 2H72 4T RTA13NM 20031006000442003100600044SO 2003 10 6 CHQA000420 120030913A3260 PROXIMITY SENSOR EMB 145 EMB145 3260210SO MLG CRACKED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11272 AFTER TAKEOFF GEAR WOULD NOT RETRACT. EICAS MESSAGE LANDING GEAR AIR/GRND FAIL. RAN QRH CHECKLIST, CONTACT DISPATCH AND MTX AND RETURNED TO MCO FOR LANDING. NO EMERGENCY WAS DECLARED, BUT EMERGENCY EQUIPMENT WAS DISPATCHED. FOUND LF AFT (WOW) PROXIMITY SENSOR FACE CRACKED. REMOVED AND REPLACED PROXIMITY SENSOR, PERFORMED GEAR SWING OPS CHECK GOOD. 2L72 4F RTT00011AT 20031006000722003100600072CE 2003 10 6 AMWA46 120030907A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07159YV UE159 RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-46 (1EA CRACK ON THIS RIB) 2L72 4T RTA24CE 20031006000772003100600077CE 2003 10 6 AMWA50 120030903A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07132YV UE132 WHILE PERFORMING AN INSP IN THE VERT. STAB., THE RIB FLANGE AT CANTED STAB. STA 54.026 WAS FOUND CRACKED IN 3 PLACES ON THE RT SIDE NEAR THE FWD, CENTER AND AFT STRG AND 2 PLACES ON THE LT. REPAIRED CRACKS TO THE RIB FLANGE IN ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031006000842003100600084WP 2003 10 6 ARWA20030910 120030915A5410 STRUCTURE DOUG DC8 DC863F 302198FWP NR 1 PYLON BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON EDGE BROKEN, AFT OF LT FORWARD MOUNT. 2L74 4F 4A25 20031006000892003100600089SO 2003 10 6 C2XA03CL166 120030831A3234MS2106024 RELAY EMB 145 EMB145XR SO MLG HANDLE DEFECTIVE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2716112 145660 CLE FLIGHT NR 3239, THE CREW REPORTED THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION WITHOUT DEPRESSING THE RELEASE BUTTON ON THE GEAR HANDLE CONTROL BOX. MAINTENANCE INSPECTED AND REPLACED AIR/GROUND RELAY KOO24. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20031006000982003100600098CE 2003 10 6 DXTA200300094 120030819A2710 BUNGEE CYLINDER CESSNA750 750 2076810CE LT PCU ACTUATOR OUT OF ADJUST E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07942QS 7500024 AILERON CONTROL BINDING WORSE TO THE RIGHT, TAKES EXCESSIVE RIGHT WING DOWN TRIM AT HIGH SPEEDS. - ADJUSTED LT PCU ACTUATOR INPUT BUNGEE TO ELIMINATE FORCE FIGHT CONDITION. PERFORMED ADJUSTMENT IAW MFG 750 MM CHAPTER 27-10-00, OPS CHECKED GOOD. 2L72 4J RTT00007WI 20031006000992003100600099 2003 10 6 DXTA200300103 420030822A34607011702929 CONTROLLER CESSNA750 750 2076810CE FLT CONTROL FAILED E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07933QS739 7500133 DURING DESCENT AT APPROX 13000 FT, (FGC A FAIL) MESSAGE ON EICAS, FOLLOWED SHORTLY AFTER BY SMOKE ODOR AND (TRIM SW FAIL L) ON EICAS. EVENT BUTTON WAS CYCLED. TROUBLESHOT AND FOUND THE F/O’S FLIGHT GUIDANCE CONTROLLER GC-810 FAILED. REMOVED AND REPLACED F/O CONTROLLER AND OPS CHECKED GOOD IAW CE750 CHAPTER 22-10-03 AND 22-10-00. 2L72 4J RTT00007WI 20031006001012003100600101NM 2003 10 6 2003UALA00648 120030821A5751113W721213 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE LT AILERON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29771UA30719 26932 I/B & O/B ACTUATOR FITTINGS CRACKED. LEFT AILERON WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20031006001062003100600106NM 2003 10 6 2003UALA00674 120030909A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29368UA 24537 STATION 927 AT RBL45 INCH, FLOORBEAM HAS A CRACK IN THE WEB AND A CRACK IN THE RADIUS OF THE T-CAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND STRAP REPAIRS. 2L72 4F4 FRTA16WE E2GL 20031006001082003100600108NM 2003 10 6 2003UALA00676 120030909A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29372UA 24637 DENTED FUSELAGE SKIN AT BS 388-393, STR 5L TO STR 7L, 11 INCHES LONG AND 1 INCH WIDE. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031006001152003100600115NM 2003 10 6 HOC2003F00019 120030826A5330 SKIN BOEING727 727224 1384076NM FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0779749 22451 DURING (C) CHECK, CORROSION WAS NOTED ON FUSELAGE INTERIOR SKIN AT STA 660-680, LBL-1. 2L73 4F A3WE 20031006001162003100600116EA 2003 10 6 HNAA0300049 120030915A2520 SEAT BELT DHAV DHC8 DHC8311 1386006EA CABIN LOOSE A HNAAO OTHER O OTHER NRNOT REPORTED 1 EA07327EN 261 SEAT BELT AT 10D CAME LOOSE, INSTALLED SEAT BELT HARDWARE, OPS CHECK GOOD. 2H72 4T RTA13NM 20031006001312003100600131 2003 10 6 SWAA032025 420030911A2565 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031006001352003100600135 2003 10 6 SWAA032029 420030910A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031006001462003100600146NM 2003 10 6 SWAA032012 120030909A53306545776 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR HINGE CUTOUT UPPER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031006001522003100600152GL 2003 10 6 SWAA032018 220030909A7320CFM563B1 ENGINE BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563B1US GL NR 2 FAILED A SWAACD ABORTED TAKEOFF RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW29357SW 26594 723136 ABORTED TAKEOFF, NR 2 ENGINE WOULD NOT ACCELERATE ON TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20031006001752003100600175NM 2003 10 6 03FDEA01649 120030926A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION BS 1130, WL 201, LBL 38 - BL 0, IN AND AROUND NUTPLATE HOLES. REPAIRED BS 1130 FLOORBEAM LOWER CHORD, W.L 201, LBL 65 TO RBL 65. CORROSION ON FLOOR BEAM WAS FOUND TO BE OUT OF LIMITS. LOWER CHORD OF 1130 FLOOR BEAM WAS REMOVED AND REPLACED PER FED EX EA 7-5310-54974. 2L73 4F RTA3WE 20031002000602003100200060WP 2003 10 2 UPS03841218 120030827A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT STA 1766 AT RBL 26 AND 36. CUTOUT DAMAGED AREAS AT RBL 26 AND 36,NDT VERIFIED NO CRACKS AT CUTOUTS, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRO8530007. 2L74 4F RT4A25 20031002000802003100200080 2003 10 2 0301731232 420030910A2200 AUTOTHROTTLE SYS DOUG DC10 DC1030 3023501WP GE CF6 CF650C 30018GL COCKPIT MALFUNCTIONED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01232NW 46961 517441 DURING TAKE-OFF ROLL THE CREW OBSERVED THE NR 1 ENGINE EXCEED LIMITS FOR N1, N2 AND EGT. THE NR 3 ENGINE ALSO EXCEEDED THE N2 LIMIT. THE TAKE-OFF WAS ABORTED AT 115KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 1 AND 3 ENGINES PER THE AMM WITH NO DEFECTS NOTED. THE AUTOTHROTTLE SYSTEM WAS PLACED ON MEL22-7 AS A PRECAUTION. 2L73 4F4 F A22WE A23EA 20031002000932003100200093NM 2003 10 2 C1HA200386009 120030909A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 SEAT TRACK GOUGED AND SCRATCHED AT BS 344 RBL 50. 2L73 4F A3WE 20031002001012003100200101NE 2003 10 2 GLBA2003130 220030910A7250 TURBINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67A 52043NE RT ENGINE FAILED A GLBAC ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 NM03228GL16400 UE228 PS0014 RT ENGINE POWER TURBINE FAILED AT 1000 LBS TORQUE. REMOVED AND REPLACED RT ENGINE ASSY. 2L72 4T4 TRTA24CE E26NE 20031002001022003100200102SO 2003 10 2 C2XA03TY156 120030910A532014534612001 SILL EMB 135 EMB135ER 3260203SO FUSELAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE MAIN DOOR SILL SKIN, MAINTENANCE REMOVED AND REPLACED THE SILL I/A/W-EMB-135-AMM-53-21-00. 2L72 4F RTT00011AT 20031002001252003100200125NM 2003 10 2 AWXA200301036 120030910A2560P4010021 BATTERY BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28324AW 23261 FLIGHT CREW REPORTED THE AFT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20031002001312003100200131NM 2003 10 2 AWXA200301042 120030812A53156545410555 FLOORBEAM BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .5625 INCH CRACK WAS FOUND ON FLOORBEAM REPAIR BS 677, RBL 24. MAINTENANCE REMOVED REPAIR ANGLE AND 2 EACH DOUBLERS; FABRICATED A NEW REPLACEMENT REPAIR CHANNEL AND 3 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5715-03240-ES2. 2L72 4F4 FRTA16WE E2EA 20031002001372003100200137CE 2003 10 2 DXTA200300113 120030912A5310 WINDOW POST CESSNA750 750 2076810CE COCKPIT CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07943QS 7500043 WHILE PERFORMING MAINTENANCE NEAR PILOT'S SIDE WINDOW, NOTICED WINDSHIELD CENTER POST HAS CHAFE DAMAGE, FURTHER EVALUATION SHOWED DAMAGE MEASURED APPROX. .375 INCH LONG BY .100 INCH WIDE AND APPROX. .028 DEEP. THE THICKNESS OF THE POST IS .062 INCH. - ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20030908002092003090800209 2003 9 8 SWIA200312295 420030822A3418 CONNECTOR EMB 120 EMB120ER 3260203SO STALL WARNING DIRTY A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07579SW 120347 STALL TEST FAILS TEST, NO PUSHER. CLEANED CANNON PLUG ON 'G' SWITCH AND OPS CHECKS GOOD. 2L72 4T RTA31SO 20030908003102003090800310NM 2003 9 8 SWAA031888 120030823A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030909000462003090900046EA 2003 9 9 SWIA200312325 120030808A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. ANGLE REPLACED IAW CRJ SRM 51-40-11. P/N: 601-35012-51 2L72 4F RTA21EA 20031105000082003110500008NM 2003 11 5 03FDEA01844 120031031A2740 BRAKE BOEING727 727200 138407ENM HORIZ STAB OUT OF ADJUST A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-2740-72134 FLIGHT CONTROLS - HORIZONTAL STAB BRAKE CONTROL, ADJUST NUMBER OF REQUIRED WASHERS. CLOSING ACTION ON 10/31/03 ON N/R S00027. COMPLIED WITH EA 7-2740-72134. 2L73 4F RTA3WE 20030909001382003090900138CE 2003 9 9 S2YA03011 120030312A32601143610441 DOWNLOCK SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT MLG FAILED A S2YAO OTHER N FALSE WARNING APAPPROACH 1 GL13831SK UE83 DURING APPROACH OF FLIGHT 1019, THE CREW DID NOT ACHIEVE A DOWN AND LOCKED INDICATION FOR THE RT MAIN GEAR. THE CREW MANUALLY EXTENDED THE GEAR. THE CREW STILL DID NOT GET THREE GREEN BUT THE IN-TRANSIT LIGHT EXTINGUISHED. THE CREW DID NOT DECLARE AN EMERGENCY AND MADE AN UNEVENTFUL LANDING. MECHANIC REPLACED THE RT MAIN LANDING GEAR DOWNLOCK SWITCH AND OPS CHECK THE SYSTEM WITH NO FURTHER DEFECTS NOTED. 2L72 4T3 TRTA24CE E2NE 20030909001742003090900174SW 2003 9 9 HEEA088925 120030728A5610407030115125A WINDSHIELD BELL 407 407 1182206SW COCKPIT SCRATCHED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 WINDSHIELD SCRATCHED. 1G71 3U O H2SW 20030909001852003090900185EU 2003 9 9 KBMA088811 120030710A2121050173 BLOWER MOTOR AEROSPAS355 AS355* EU A/C BAY INOPERATIVE B KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 A/C INOPERATIVE CIRCUIT BREAKER POPS REMOVED AND REPLACE WITH NEW MOTOR 1G72 3U H11EU 20030909002102003090900210 2003 9 9 BAQA088788 420030819A3442790010003 RADAR UROCOPEC135 EC135T1 5620026EU COCKPIT INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME248 0143 RADAR UNIT INTERMITTENT OPERATION. SPIKES. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030909002322003090900232WP 2003 9 9 ABXA030319 120030801A3230 PIVOT ASSY DOUG DC9 DC941 302207NWP RT MLG LACK OF LUBE A ABXAO OTHER O OTHER CRCRUISE 1 GL23951AX 47616 RIGHT MAIN LANDING GEAR CAME OUT ON UPLATCH CHECK. RECYCLED LANDING GEAR AND RECEIVED NORMAL INDICATION. FOUND UPLOCK PIVOT BOLT BOUND UP TO HOOK AND STRUCTURE IMPEDING MOVEMENT OF HOOK. PULLED, CLEANED AND LUBRICATED PIVOT BOLT AND BOSS. INSTALLED REMOTE HYDRAULIC PUMP TO UPLATCH ACTUATOR AND VERIFIED OPS OF ACTUATOR. PERFORMED GEAR SWING AND LEAK CHECK OF LINES. OPS CHECKED GOOD. 2L72 4F A6WE 20030909002342003090900234WP 2003 9 9 ABXA030314 120030716A57539957578506 SKIN DOUG DC9 DC933F 302207AWP T/E FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 LEVEL II CORROSION, BULGING SKIN, CUPPED AND BROKEN FASTENERS FLAP LOWER SURFACE AT NR 3 EXPANSION JOINT. REPLACED LOWER SKIN ON RIGHT LOWER NR 3 FLAP SEGMENT IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030909002442003090900244EA 2003 9 9 ASOA03379 120030816A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE ANGLE AT FS 640 AND BL 45 BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ANGLE AT FS 640 AND BL45 BETWEEN STRINGERS 9 AND 12 IAW ASA EO 600-53-0081B. (M) 2L72 4F RTA21EA 20030909002742003090900274SO 2003 9 9 RAIA00307195 120030720A7830 THRUST REVERSER EMB 145 EMB145LR 3260212SO NR 2 ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03815HK 145048 5693-STL-ENGINE NR 2 THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE DEFERRED NR 2 T/R IAW MEL. SUBSEQUENTLY CHECKING THE T/R SYSTEM WITH NO DEFECTS NOTED CLEARING THE DMI. 2L72 4T RTT00011AT 20031003000112003100300011NM 2003 10 3 AALA20030932 120030902A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21693AA 26973 EMERGENCY LIGHTS WERE VERY DIM IN THE FIRST CLASS CABIN. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000332003100300033NM 2003 10 3 AALA20030915 120030901A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21653A 24611 SEAT MOUNT EMERGENCY LIGHT INOPERATIVE AT 6E. BATTERY PACK FAILED DUAL FEED CHECK. SECURED LOOSE SEAT CONNECTOR AT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000362003100300036EU 2003 10 3 AALA20030645 120030609A3397 WIRE FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211467A 11499 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM SEATS 8D FORWARD INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031003000542003100300054SO 2003 10 3 C2XA03TY158 120030911A532014590070004 SILL EMB 135 EMB135ER 3260203SO FUSELAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE SERVICE DOOR FORWARD SILL AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 53-00-04, 51-40-02, 51-30-01 AND CPM 51-21-04, 05. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031003000602003100300060SO 2003 10 3 C2XA03SH323 120030913A542014576631621 STIFFENER EMB 145 EMB145LR 3260212SO NR 1 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE NUMBER 1 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031003000682003100300068SO 2003 10 3 C2XA03SH329 120030914A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031003000692003100300069SO 2003 10 3 C2XA03SH330 120030914A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031003000792003100300079NM 2003 10 3 03FDEA01526 120030902A5753ARC0503504 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP OUTBOARD HINGE (A/C SIDE) INBOARD ACTUATOR ATTACH BORE FOUND CORRODED. 2L73 4F RTA22WE 20031003000802003100300080NM 2003 10 3 03FDEA01525 120030829A5753ARC0503504 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP OUTBOARD HINGE (A/C SIDE) SIDE ATTACHMENT BORE FOUND CORRODED. 2L73 4F RTA22WE 20031003000882003100300088NM 2003 10 3 F3LA200300133 120030912A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED MIDDLE INTERCOSTAL BETWEEN FLOORBEAMS AT STA. 1006 - 986.5 CORRODED. FABRICATED AND INSTALLED INTERCOSTAL IAW EA B3-53R-10114 AND SRM 51-40-02. 2L72 4F RTA16WE 20031003000932003100300093NM 2003 10 3 F3LA200300134 120030913A5511 FRAME BOEING737 73736E 138443ANM HORIZONTAL STAB CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED LT HORIZONTAL STABILIZER FRAME CRACKED WHERE ELEVATOR ATTACH MECHANISM ATTACHES TO HORIZONTAL STABILIZER. FABRICATED AND INSTALLED REPLACEMENT CHORD IAW SRM 51-40-2. 2L72 4F RTA16WE 20031003000972003100300097NM 2003 10 3 AT0300026 120030913A33506011779 BATTERY PACK BOEING717 717200 1383700NM EXTERIOR UNSERVICEABLE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15945AT 55008 EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FUSELAGE EMERGENCY LIGHTS. OPS CHECK GOOD B717 AMM 33-51. 2L72 4F TRA6WE 20031006000122003100600012EU 2003 10 6 MALA030408 120030908A33971013073 WIRE BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT BROKEN A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15517XJ E2335 DURING BOARDING ON FLIGHT 3445, PASSENGER KICKED FLOOR TRACK LIGHTING (BY ACCIDENT). SOME WIRING BROKE. UNLOADED PASSENGERS AND MARINTENANCE REPAIRED. MAINTENANCE REPLACED 2 EMERGENCY LIGHT ASSEMBLIES P/N 10-1307-3 LOCATION LE67 AND LE68 OPS CHECK GOOD. A/C GOOD FOR CONT SERVICE. 2H74 4F RTA49EU 20031006000142003100600014EU 2003 10 6 MALA030413 120030812A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK IN CVG, NR 3 SEAT RAIL CORROSION. MAINTENANCE REPAIRED PER EO A 53026, REFER TO 409 190259 FOR DETAIL. A/C RELEASE DATE WAS 8/2/03. 2H74 4F RTA49EU 20031006000182003100600018EU 2003 10 6 MALA030418 120030909A3350 LIGHT SAAB SF340 340B 7860101EU CABIN LOOSE A MALAK NONE O OTHER NRNOT REPORTED 1 GL15423XJ 340B423 DURING FLIGHT NR 3028, EMERGENCY FLOOR LIGHTING LOOSE AROUND ROW 5 AND 6. MAINTENANCE REMOVED AND REPLACED ADHESIVE AND REINSTALLED FLOOR TRACK LIGHTS AT SEATS 5-6A SEC AND OPS CHECKS GOOD. 2L72 4T RTA52EU 20031006000232003100600023NM 2003 10 6 QXEA200301118 120030905A5510 SHIM BOMBDRDHC8 DHC8401 1390041NM ZONE 300 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 HORIZONTAL STABILIZER RT HAND FORWARD ATTACH FITTING HAS EXTRUDED SHIMS. REPAIRED IAW Q400 SRM 51-00-02 AND TASK 55-10-00-400-801. 2H72 4T RTA13NM 20031006000342003100600034NM 2003 10 6 AWXA200301060 120030914A5754655331615 PANEL BOEING737 737277 1384570NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK .1875 INCH CRACK WAS FOUND ON CLOSE OUT PANEL BELOW NR 2 SLAT INBOARD MAIN TRACK AT WBL 355. MAINTENANCE REMOVED CRACKED NR 2 SLAT CLOSE OUT PANEL AT WBL 355; FABRICATED A NEW REPLACEMENT PANEL IAW DWG 69-53316; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 1, DETAIL 1, FIG. 007. 2L72 4F RTA16WE 20031006000532003100600053NM 2003 10 6 MEX2003408 120030831A2797 WIRE BOEING757 7572Q8 1384972NM BCPU LOOSE W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23804AM 26271 AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF (WARN ELEX/ SLAT FLAP ELEC STATUS) MESSAGE IN EICAS. DURING REVISION WAS DETECTED BCPU POPPED DUE TO LOOSE OF WIRE NUMBER 5 TB 5001. THE BCPU C/B 6-14 WAS RESETED AND FSEU POWER OPERATED IN A NORMAL WAY TEST PERFORMED IAW MM, ALL TESTS CORRECT. 2L72 4F RTA2NM 20031006000582003100600058CE 2003 10 6 AMWA32 120030907A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07182YV UE182 RIB AT CS 54.026 CRACKED AT STRG. P/N 101-640000-46 STRG P/N 101-640000-47 ON RT SIDE AND STRG P/N 101-640000-39 LT SIDE (3EA CRACKS ON THIS RIB). 2L72 4T RTA24CE 20030826000712003082600071EU 2003 8 26 36020820 120030820A6410355A12005004 BLADE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR DEBONDED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07820NA953 3602 22342 TRIM TAB DISBONDED ON RED TAIL ROTOR BLADE. RESULTING IN APPROXIMATELY 1.25 INCH LONG SEPARATION. 1G71 3U3 U H9EU E00054EN 20030826000772003082600077NM 2003 8 26 CALA0300474 120030821A5330 SKIN BOEING777 777224 1385225NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777012 29860 INSPECTION FOUND THE FUSELAGE EXTERNAL SKIN DENTED AT BS 680 BETWEEN S27L AND S28L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 4, FIGURE 202. A DIP WAS ISSUED TO REINSPECT THE REPAIR WITHIN 30,000 FLIGHT CYCLES, THEN EVERY 16,000 FLIGHT CYCLES. 2L72 4F RTT00001SE 20030826000822003082600082EU 2003 8 26 YENA200317 120030722A25203042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN CONTAMINATED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15520JB8825 1446 LIVETV ROW: 10 DEF SMOKED AND SHORTED OUT. TURNED SYSTEM OFF. NO FURTHER PROBLEM. TRANSFERRED TO MEL 25-22-03. LATER UPON ARRIVAL AT JFK, REMOVED AND REPLACED SEB AT SEAT 10 DEF. IT WAS REPORTED THAT PASSENGER SPILLED LARGE AMOUNT OF LIQUID ON SEAT. CONFIRMED SEB WAS CONTIMINATED. 2L72 4F RTA28NM 20030826000982003082600098NM 2003 8 26 03FDEA00841 120030601A5340 HINGE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25245FE 22016 MDIS 245 53-30 0005255 27MAY03 BFM CLOSE R COMPLY WITH E.A. NR 7-5330-70910 FUSELAGE - MAIN CARGO-RE WORK OF ATTACHMENT HOLE (AD 2002-16-19). FACT 30 MAY 03 15:18 BFM R COMPLIED WITH E.A. 7-5330-70910 - FUSELAGE - MAIN CARGO - REWORK OF HINGE ATTACHMENT HOLE (AD2002-16-19). 2L73 4F RTA3WE 20030826001162003082600116NM 2003 8 26 S03453035 120030506A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJFO OTHER O OTHER TXTAXI/GRND HDL 1 WP03 28710 B-18202 FUSELAGE SKIN REPAIR COMMON TO BS 500,S-46R. REPAIR IAW EO 744-53-00-0004. 2L74 4F4 FRTA20WE E24NE 20030826001192003082600119NM 2003 8 26 XNOA01133 120030612A3260 CONNECTOR BOEING727 727227 1384078NM RT MLG DOOR DIRTY A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL2376753 21249 ON DEPART FROM BOS RT MAIN GEAR DOOR LIGHT. RECYCLE GEAR. DOOR LIGHT OUT. ACTION TAKEN: CLEANED AND RESEATED RT MAIN GEAR DOOR SWITCH CONNECTOR PLUG. CYCLED THROUGH SEVERAL TIMES. OPS CHECK NORMAL IAW ENA MM 32-12-1. 2L73 4F A3WE 20030826001332003082600133NM 2003 8 26 USAASB03127 120030803A335020121 CHARGER BOEING737 737301 1384611NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19592US 23937 PIT - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. ALSO, REPAIRED A PUSHED BACK CONNECTOR PIN. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030826001402003082600140NM 2003 8 26 UIEA200300042 120030801A3610 SEAL BOEING747 747243B 1384830NM LT MLG WW WORN A UIEAA UNSCHED LANDING O OTHER CRCRUISE 1 EA15518MC 23476 DFW/ANC AIR TURNBACK, AT FL 31 CABIN ALT WENT TO 10 WITH DIFFERENTIAL AT 6.8 AND UNABLE TO PREVENT CABIN FROM CLIMBING 50-100 FPM. AIRCRAFT DESCENDED TO FL 29.0 THEN FL 25.0. MAX DIFFERENTIAL THAT COULD BE HELD WAS 6.5 AND CABIN CONTINUED TO CLIMB 50-100 FPM. BOTH OUTFLOW VALVES WERE FULLY CLOSED IN BOTH AUTO AND MANUAL. NO FUEL DUMPED. FOUND SUBSTANTIAL AIR LEAK LEFT WHEEL WELL PNEUMATIC DUCT AT 2 CLAMPS. REPLACED SEALS AT BOTH CLAMPS IAW MM 36-11-01. PRESSURIZED SYSTEM AND OPS NORMAL. AS PRECAUTION CHECKED A/C FOR LEAKS DURING PRESSURIZATION. NONE FOUND. ALL CHECKS NORMAL. (M) 2L74 4F A20WE 20030826001512003082600151SO 2003 8 26 SIMA200321003 120030725A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21713AE 145249 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 51-20-03, 51-40-02, 51-40-06 AND 51-20-01. (M) 2L72 4F RTT00011AT 20030826001642003082600164WP 2003 8 26 MEX2003327 120030703A3241392492 CONTROL VALVE DOUG DC9 DC987 3022087WP ANTI-SKID SYS FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23751RA 49779 FLT 263 - REX-MEX - RETURNED TO PLATFORM. DURING TAXI, ANTI-SKID LIGHTS CAME ON, BREAKERS WERE RESEATED IN-CORRECTLY. DURING REVISION ON CONNECTOR, DETECTED FAILURE OF DUAL PRESS CONTROL VALVE. THE CONNECTOR WAS CLEANED IAW 32-43-02, ALL TESTS CORRECT. DURING OVERNIGHT SERVICE, THE DUAL PRESSURE CONTROL VALVE AT LEFT EXTERIOR SIDE WAS REPLACED IAW 32-43-02, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030826001752003082600175EA 2003 8 26 SWIA200312135 120030623A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA CABIN FAILED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07407SW 7034 ONE SECTION OF THE FLOOR EMERGENCY LIGHTS IS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING INVERTER NR 3. OPS CHECK GOOD. 2L72 4F RTA21EA 20030826001792003082600179EU 2003 8 26 VY1L103201 120030127A771253526 TORQUEMETER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT LEAKING L VY1LO OTHER K FLUID LOSS NRNOT REPORTED 1 SW19911KR5733 2094 TORQUEMETER TRANSMITTER LEAKS. 1G71 3U3 UNCH9EU E19EU 20030827000112003082700011NM 2003 8 27 03FDEA00837 120030523A5744ARC0502506 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0746: RT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP-HINGE FWD FITTING FOUND INBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0746: REPAIR CARRIED-OUT AS PER CMM 57-44-08 AND FEDEX EA 1-5740-68424 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030827000132003082700013NM 2003 8 27 03FDEA00831 120030526A5753ARC198414 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0875: RT WING - OUTBOARD TRAILING EDGE FLAP, AFT OUTBOARD FLAP-HINGE ASSEMBLY FOUND PIVOT MOUNT, OUTBOARD HOLE WITH BUSHING LOOSE. SNRM N0875 - LOOSE BUSHINGS AT PIVOT MOUNT OUTBOARD HOLE REPLACED WITH OVERSIZED BUSHING AS PER FEDEX EA 1-5750-69255 - WINGS - RT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030827000212003082700021NM 2003 8 27 03FDEA00908 120030618A5311 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 N00369 990 FRAME GOUGED BETWEEN S25L - S26L. REPAIRED FRAME AT BS 990 BETWEEN STR 25L - STR 26L PER SRM 51-40-3 FIG 1, BS 990 FRAME GOUGE OUT OF LIMITS IAW SRM 53-10-1 AT STR 25L - STR 26L. 2L73 4F RTA3WE 20030822001462003082200146NM 2003 8 22 C1HA200381021 120030806A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON SEAT TRACK FS 344 / 360 LBL 24. 2L73 4F A3WE 20030822001472003082200147NM 2003 8 22 C1HA200381022 120030806A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON SEAT TRACK FS 344 / 360 LBL 44. 2L73 4F A3WE 20030822001512003082200151NM 2003 8 22 QXEA200300940 120030802A3230XD4N RELAY DHAV DHC8 DHC8202 2809007NM LANDING GEAR FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09351PH 490 SEA- ON FLIGHT 2175 EN ROUTE TO SEA GOT LANDING GEAR INOPERATIVE CAUTION LIGHT. USED ALTERNATE EXTENSION 1 UPON LANDING. GEAR INOPERATIVE LIGHT EXITING, NOSE WHEEL STEERING LIGHT CAME ON AND LOST STEERING. REMOVED AND REPLACED RELAY 3261-K14. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030822001532003082200153NM 2003 8 22 QXEA200300943 120030801A5320 STRUCTURE DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX- SCRATCH IN AIRFRAME BELOW RIGHT HAND EMERGENCY EXIT BETWEEN STATION X366-355. REPAIRED IAW DHC-8 RD 8-53-7489 AND HORIZON AIR EA 2-53-462. 2H72 4T RTA13NM 20030825000052003082500005WP 2003 8 25 UPS03840941 120030618A53204611067N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 A/C BAY FORWARD BULKHEAD STA 8 LONG 33L END FITTING IS CRACKED REMOVED,FABRICATED AND REPLACED FITTING IAW DWG 4611067 AND SRM 51-1-20D. 2L74 4F RT4A25 20030825000242003082500024WP 2003 8 25 UPS03840906 120030604A5313 LONGERON DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C3 MAIN CABIN AT FS 1660, LONGERON 11R IS CRACKED. REMOVED OLD LONG 11RT TO FOM , LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONG 11RT IAW DC8 SRM 51-1-21. 2L74 4F4 FRT4A25 1E8 20030825000602003082500060EU 2003 8 25 UPS03141073 120030806A33503245410 POWER SUPPLY AIRBUS300 A300B4622R 3930312EU CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01127UP 0812 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS STAY ON IN THE ARMED POSITION THROUGH FLIGHT. REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT PER M/M 33-51-14-4, SYSTEM TEST OK P/N 324-54-10, S/N OFF 2804, S/N ON 3215. 2L72 4F RTA35EU 20030825000762003082500076NM 2003 8 25 EIA2003107 120030726A2611FR2121 SMOKE DETECTOR BOEING747 747132 1384882NM CARGO BAY MALFUNCTIONED A EIAAO OTHER N FALSE WARNING CRCRUISE 1 NM09481EV 19896 NR 4 MAIN CARGO DECK SMOKE DETECTOR WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALL FIVE (5) TIMES AN EXAMINATION OF UPPER DECK DISCLOSED NO FIRE. 2L74 4F A20WE 20030825001062003082500106 2003 8 25 234TR0008 420030725A2297 WIRE BOEING737 737228 13844AGNM AUTOPILOT SYS BROKEN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 B-AUTO PILOT FAILED LRU INTERFACE -MCP TEST 73.6 (HDG SYNC). REPAIRED BROKEN WIRE AT CONNECTOR D994 ON E1-2 SHELF. OPERATES NORMAL. 2L72 4F RTA16WE 20030825001272003082500127SO 2003 8 25 C2XA03SH270 120030817A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV DURING C CHECK LEFT OMEGA BEAM AT CARBON FIBER CROSSBEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030825001482003082500148NM 2003 8 25 AMTA200301009 120030805A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11527AT 30886 EGRESS LIGHTS NOT LIGHTED FROM SEAT 4 DEF, FORWARD. REMOVED AND REPLACED EGRESS LIGHT ASSEMBLY PER AMM 33-51-11-3. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030826000182003082600018NM 2003 8 26 03FDEA01364 120030814A5753ARC199114 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE INBOARD & OUTBOARD BUSHING FOUND LOOSE. RT WING OUTBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT HOLE INBOARD & OUTBOARD BUSHING REMOVED AND REPLACED AS PER FEDEX EA 1-5750-71800, TITLE - WINGS - LT AND RT O/B FLAP - O/B HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20030826000452003082600045NM 2003 8 26 03FDEA01191 120030728A5514ALC8103502 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-1-5000 LIMITATIONS. RIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69402 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 35 RIGHT HAND SIDE. 2L73 4F RTA22WE 20030826001302003082600130NM 2003 8 26 03FDEA00997 120030628A533053FX130179 TRIPLER BOEING727 727100 1384036NM FUSELAGE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 MDIS 166 53-30 0004746 26JUN03 BFM CLOSER COMPLY WITH EA NR 7-5330-70966 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR (AD 2002-16-19). FACT 27JUN03 14:10 BFM R COMPLIED WITH EA NR 7-5330-70966, FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR (AD2002-16-19). 2L73 4F RTA3WE 20030826001422003082600142SO 2003 8 26 SIMA200320806 120030721A322114524475001 BEARING COVER EMB 135 EMB135LR 3260305SO NLG CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21713AE 145249 ABI - THIS IS A LEVEL TWO ITEM FOUND DURING AND IMBV INSPECTION, THE LEFT AND RIGHT LOWER NOSE LANDING GEAR TRUNNION BEARING CAPS PITTED. REMOGED AND INSTALLED SERVICEABLE CAPS ON NLG IAW EMB 135 AMM 32-20-01. (M) 2L72 4F RTT00011AT 20031003000732003100300073NM 2003 10 3 03FDEA01532 120030902A5753ARC0502506 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP INBOARD HINGE (A/C SIDE) ACTUATOR OUTBD ATTACH BORE, FOUND CORRODED. 2L73 4F RTA22WE 20031006001192003100600119NM 2003 10 6 HNAA0300051 120030908A3350 POWER SUPPLY DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT INOPERATIVE A HNAAK NONE O OTHER NRNOT REPORTED 1 EA07988HA 426 TWO EMERGENCY FLOOR LEVEL LIGHTS AT 1D ARE INOPERATIVE. RESEATED ALL FOUR POWER PACKS IN CABIN OVERHEAD, OPS CHECK GOOD. 2H72 4T RTA13NM 20031006001332003100600133 2003 10 6 SWAA032027 420030910A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH FITTINGS LOOSE. SECURED ATTACH FITTINGS PER MM. 2L72 4F RTA16WE 20031006001822003100600182NM 2003 10 6 03FDEA01644 120030926A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON BEAM BS 269, LBL 3, WL 208. REMOVED CORROSION IN A 3.0 X 3.0 AREA, .050 MATERIAL LOSS FROM AN ORIGINAL THICKNESS OF .125 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG. 1. REMOVED FE'S SEAT TRACK AT BS 268, REMOVED 4EA FLOOR SUPPORTS AT BS 266-276, LBL 3,RBL 3,RBL 14, AND BS 260-276, LBL 8, WL 208. REMOVED BEAM UPPER CHORD, FABRICATED CHORD FROM P/N 65-17588-66, ALOODINED, PRIMED, RESTORED SURFACE FINISH, INSTALLED REPLACEMENT CHORD AT BS 269, LBL 8-RBL 21, WL 208. REINSTALLED FLOOR SUPPORTS, INSTALLED FASTENERS IN FLOOR WEB REMOVED FOR BEAM REMOVAL, REINSTALLED F.E.'S SEAT TRACK. ALL WORK DONE PER SRM 51-30-2, 51-10-2, 51-30-5. 2L73 4F RTA3WE 20031006001842003100600184NM 2003 10 6 03FDEA01674 120031001A532065453132 STRINGER CLIP BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A FDEAO OTHER O OTHER ININSP/MAINT 1 SO25469FE 21581 CRACK IN STRINGER CLIP AT BS 950C STRINGER 7 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, 7RH IAW SRM 51-30-2 & 51-30-5 2L73 4F4 FRTA3WE E2EA 20031006001862003100600186NM 2003 10 6 03FDEA01676 120031001A5320654531313 STRINGER CLIP BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 STRINGER CLIP CRACKED AT BS 950C, STRINGER 9 LT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 9 LT IAW SRM 51-30-2 2L73 4F4 FRTA3WE E2EA 20031006001892003100600189NM 2003 10 6 03FDEA01679 120031001A532065453132 STRINGER CLIP BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CRACK IN STRINGER CLIP AT BS 950C, STRINGER 4 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 4 RT IAW SRM 51-30-2 & 51-30-5 2L73 4F4 FRTA3WE E2EA 20031006001912003100600191NM 2003 10 6 03FDEA01662 120031001A5230 FRAME BOEING727 727200 138407ENM MAIN CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 MAIN CARGO DOOR FWD SIDE FRAME GOUGED 52 INCHES FROM LOWER CORNER. GOUGE IN MAIN CARGO DOOR FWD FRAME 52 INCHES ABOVE LOWER CORNER FOUND TO BE OUT OF LIMITS IAW SRM 52-00-1. REPAIRED IAW FED EX EA 7-5230-70516. 2L73 4F RTA3WE 20031006001932003100600193NM 2003 10 6 03FDEA01586 120030919A5712ARC41252 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OUTBOARD FLAP FWD RIB SUPPORT ISLAND FOUND ONE CRACK APPROX 3/16 IN LENGTH AT OUTBOARD SIDE. RT OUTBOARD FLAP FWD RIB SUPPORT ISLAND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71897. 2L73 4F RTA22WE 20031007000172003100700017NM 2003 10 7 AALA20030967 120030906A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 26G. BATTERY PACK FAILED DUAL FEED CHECK. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031007000602003100700060NM 2003 10 7 SWAA031974 120030904A532065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031007000662003100700066NE 2003 10 7 SWAA031980 220030902A7250JT8D9A TURBINE BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 2 ENGINE FAILED A SWAAC ABORTED TAKEOFF ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW29090SW 22905 707364 ABORTED TAKEOFF, UPON ADVANCING THROTTLES NR 2 ENG STARTED VIBRATING. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 F A16WE E2EA 20031007000782003100700078 2003 10 7 SWAA031952 420030830A2565D31354 SLIDE BOEING737 7377H4 1384404NM CABIN SVC DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 DURING SCHEDULED C4 CHECK, FOUND BOTH RT CABIN SVC DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20031007000902003100700090NM 2003 10 7 SWAA031988 120030904A5520BACB28AMO7 BUSHING BOEING737 7373G7 1384595NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C4 CHECK, SWA SI 11138-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER MM. 2L72 4F RTA16WE 20031007000912003100700091NM 2003 10 7 SWAA031989 120030904A53306545765 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 575, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031007000972003100700097NM 2003 10 7 SWAA031995 120030907A3350100885 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29716SW 27850 DURING SCHEDULED PM CHECK, FOUND AFT CABIN EEPLS EXTINGUISHED AFTER SEVERAL SECONDS. REMOVED AND REPLACED AFT CABIN EEPLS BATTERY PER MM. 2L72 4F RTA16WE 20031007000982003100700098NM 2003 10 7 SWAA031996 120030906A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C2 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20031007001012003100700101NM 2003 10 7 SWAA031999 120030908A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 827, STR 20L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20031007001022003100700102NM 2003 10 7 SWAA032000 120030908A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 984, STR 25R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20031007001142003100700114NM 2003 10 7 03244430 120030901A3397 TERMINAL BLOCK DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27430FJ 3209 DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT SWITCH IN THE COCKPIT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL FOUND A LOOSE TERMINAL BLOCK CONNECTION AT 41VPND AND RECONNECTED IT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031007001152003100700115SO 2003 10 7 C2XA03CL167 120030915A3350 LIGHT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2714959 145091 FLIGHT NR 2448 THE CREW REPORTED 2 ADJACENT EXIT ROW LIGHTS WERE INOPERATIVE IN MIDDLE OF CABIN. MAINTENANCE INSPECTED AND RESET EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031007001182003100700118CE 2003 10 7 DXTA200300117 120030915A2821 FILTER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL SYSTEM CLOGGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07908QS 7500108 CAE330233 FUEL FILTER BYPASS L CAS MESSAGE CAME ON ABOUT 5 SECONDS AFTER TAKEOFF POWER APPLIED. TAKEOFF ABORTED. INSTALLED NEW FUEL FILTER & RESET BYPASS INDICATOR IAW AE3007C MM CHAPTER 73-30-00, LEAK AND OPS CHECKED GOOD. 2L72 4J4 FRTT00007WITE6CH 20031007001232003100700123NM 2003 10 7 03250425 120030907A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27425FJ 3189 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20031008000012003100800001WP 2003 10 8 MWEA030376 120030916A5310SRO95200089 SPACER DOUG DC9 DC981 3022081WP CARGO DOORWAY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 AFT CARGO DOOR LOWER JAMB HAS LIGHT CORROSION ALONG THE ENTIRE LENGTH AROUND AND INSIDE SCREW HOLES. FABRICATED AND INSTALLED JAMB SPACER. 2L72 4F A6WE 20031008000072003100800007NM 2003 10 8 03252411 120030909A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27411FJ 3166 DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTING WAS FOUND INTERMITTENTLY OPERATING. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031003000132003100300013NM 2003 10 3 AALA20030615 120030529A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21191AN 32385 DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. CLEANED EXTERIOR EMERGENCY EXIT LIGHT SOCKET AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000182003100300018EU 2003 10 3 ASOA03423 120030908A5260S5217642500400 STEP AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SO11532AS 458 DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE BRACKET HOLDING THE TOP STEP WAS CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031003000532003100300053EA 2003 10 3 QXEA200301116 120030908A2820 O-RING CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09602QX 10010 FUEL LEAKING FROM UNDERWING CENTER AREA DURING REFUELING. REMOVED AND REPLACED BOTH O-RINGS AT COUPLING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031003000622003100300062SO 2003 10 3 C2XA03SH325 120030913A532014521721005 STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE FORWARD STRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031003001002003100300100NM 2003 10 3 UPS03241224 120030914A3350 LIGHT BOEING727 72725C 138400HNM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 EXIT EMERGENCY LIGHT INOP R/R MAIN EXIT EMERGENCY LIGHT ASSY. OPS CKS OK. 2L73 4F A3WE 20031006000642003100600064CE 2003 10 6 AMWA38 120030907A553111464000069 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127ZV UE127 RIB AT CS 24.973 CRACKED AT STRG P/N 101-640000-39 LT SIDE (1EA CRACK ON THIS RIB). 2L72 4T RTA24CE 20031001000472003100100047WP 2003 10 1 UPS03841192 120030811A52203884062 FITTING DOUG DC8 DC873F 302199FWP EMERGENCY EXIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, RT AFT TYPE 1 DOOR HAS A CRACKED FITTING BELOW THE MOST FORWARD LOWER DOOR STOP AT AFT FRAME OF THE FORWARD WEB SECTION REMOVED RT AFT TYPE 1 DOOR. REMOVED FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20031001000782003100100078NM 2003 10 1 2003UALA00716 120030924A3220 WHEEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NLG SEPARATED A UALAO OTHER O OTHER LDLANDING 1 WP29337UA 24241 ON LANDING DCA, NOSE LANDING GEAR COLLAPSED. UPON ROTATION IN ORD, THE NOSE WHEEL ASSEMBLIES DEPARTED THE AXLE. AIRCRAFT LANDED ON THE AXLE IN DCA. CAUSE OF FAILURE WAS THE REPAIR SHAFT, UAL P/N 3F13178-2. IT WAS DETERMINED THAT THE REPAIR SHAFT THREADS WERE NOT MANUFACTURED PER THE UA DRAWING. THIS EVENT IS CURRENTLY SUBJECT TO NTSB INVESTIGATION NO. DCA03SA057. ALL UAL 737 AIRCRAFT NLG AXLES WERE INSPECTED FOR SIMILAR REPAIRS. SEVEN AIRCRAFT HAD THE REPAIR SHAFT REMOVED AND INSPECTED. ANY DISCREPANT SHAFTS WERE REPLACED. 2L72 4F4 FRTA16WE E2GL 20031001000842003100100084EU 2003 10 1 03273312 120030930A3350S34C12ST6S0S0 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27312UE 41025 DURING INSPECTION THE EMERGENCY TRACK LIGHTING AT ROW 8 WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031002000402003100200040WP 2003 10 2 GTIA030681 120030909A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FOUND PAX CABIN, STATION 864 TO 886 LT SIDE INBOARD PANEL HAS CRACK/DAMAGED AT CORNERS. FABRICATED PANEL. (M) 2L72 4F A6WE 20031002000492003100200049WP 2003 10 2 UPS03841205 120030826A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, RT PRIMARY HEAT EXCHANGER CUTOUT HAS A CRACK ON SKIN AT LOWER AFT CORNER STATION -12 AT LONG. 27R. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-5330-4732-D APPX. A. 2L74 4F RT4A25 20031002000762003100200076SO 2003 10 2 C2XA03TY153 120030910A321014571035405 BEARING CAP EMB 135 EMB135ER 3260203SO RT MLG CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031002001072003100200107NM 2003 10 2 G60A072 120030911A3210ANB720321M BRACKET DOUG MD11 MD11F 3023600NM MLG BROKEN A G6OAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 EA27703GC 48411 LEFT MAIN LANDING GEAR UPLOCK INDICATION BOTH SYNOPTIC AND GEAR LIGHTS SHOWED UNSAFE. 2L73 4F RTA22WE 20031002001512003100200151NM 2003 10 2 03FDEA01521 120030912A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON STRAP LOWER SURFACE OF UPPER FLANGE OF BS 950 FLOORBEAM RBL 45 WL 208. 2L73 4F RTA3WE 20031002001562003100200156NM 2003 10 2 T192003F00000 120030825A291551091 PRESSURE SWITCH ISRAEL1125 1125 NM GARRTTTFE731TFE731* 01518WP HYD SYSTEM FAILED E T19AO OTHER O OTHER NRNOT REPORTED 1 WP19225AL 075 THE RT ENGINE HYD PRESSURE SWITCH LOCATED IN THE AFT EQUIPMENT BAY FAILED AND LEAKED HYDRAULIC FLUID EXTERNALLY. THIS CAUSED A FAILURE OF THE PRIMARY HYDRAULIC SYSTEM. THE SWITCH IS A KNOWN PROBLEM AND HAS BEEN REPLACED WITH AN IMPROVED STYLE KIT BY SB 1125-29-188. BOTH ENGINE DRIVEN HYDRAULIC PUMPS WERE REPLACED, THE HYDRAULIC SYSTEM WAS FLUSHED AND ALL THE FILTERS WERE REPLACED. INCORPORATION OF SB 1125-29-188 WILL PREVENT RECURENCE. 2L72 4F4 FRTA16NM E6WE 20031003000562003100300056SO 2003 10 3 C2XA03TY160 120030911A532014522459003 ANGLE EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 TYS DUEING A SCHEDULED INSPECTION THE LEFT HAND FORWARD RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031006000042003100600004NE 2003 10 6 COMA0360407 220030905A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT FAILED A COMAA UNSCHED LANDING MXJOVER TEMP ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO01739CA11771 7273 807520 FLIGHT 9486 RT ENGINE OVER TEMP AND AUTO SHUT DOWN. REPLACED RT ENGINE. 2L72 4F4 FRTA21EA E15NE 20031006000162003100600016EU 2003 10 6 MALA030416 120030815A5711 SPAR BAC 146 AVRO146RJ85A1500097EU LT WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK IN CVG, LT WING FALSE SPAR CRACKED BETWEEN RIBS NR 5 AND 6. MAINTENANCE REPAIRED IAW BAE FAX: BARA/AVR/6475/03-MK. A/C RELEASE DATE 9/2/03. REFER TO 409 NR 190364 FOR DETAIL. 2H74 4F RTA49EU 20031006000562003100600056WP 2003 10 6 IXXA0300058O 120030916A3260 UPLOCK DOUG DC8 DC871F 302199DWP MLG INOPERATIVE A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11828BX811831046 45993 AFTER TAKEOFF FROM KTOL TO KBNA UPLATCH CHECK POSITION OF GEAR HANDLE DURING CLIMBOUT THE (LANDING GEAR UNSAFE) LIGHT CAME ON. CYCLED GEAR DOWN AND BACK UP TWICE BEFORE GETTING A SATISFACTORY UPLATCH CHECK. AN INSPECTION IS ONGOING. AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. 2L74 4F RT4A25 20031006000572003100600057CE 2003 10 6 AMWA31 120030907A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07182YV UE182 RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-39, 1EA CRACK AT THIS RIB. 2L72 4T RTA24CE 20030826001472003082600147 2003 8 26 MEX2003296 420030718A3400 INDICATOR DOUG DC9 DC987 3022087WP COCKPIT MALFUNCTIONED A ASMFA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SW23751RA 49779 FLT 419 - IAH-MEX - AIRTURN BACK, LOST NAVIGATION INSTRUMENTS INDICATIONS. REFUEL WAS PERFORMED AND AIRCRAFT TAKEOFF WITHIN PROBLEMS. DURING OVERNIGHT SERVICE, ALL CORRECT. (M) 2L72 4F RTA6WE 20030826001672003082600167EA 2003 8 26 SWIA200312110 120030620A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07903SW 7425 CENTER ROW MID EMERGENCY LIGHT INOP. RE-LAMPED CENTER ROW MID EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030827000482003082700048SW 2003 8 27 LS12003F00000 120030606A5302205030800101 SKIN BELL 204 UH1H 1181407SW LYC T53 T53* 41549NE TAILBOOM CRACKED A LS1RK NONE O OTHER ININSP/MAINT 1 EA1351AG 7120178 LE20507X THE TAILBOOM FIRST 2 UPPER SKINS HAD NUMEROUS CRACKS. UNDER NORMAL OPERATIONS THESE CRACKS WOULD NEVER MATERIALIZE. THE AIRCRAFT HAS BEEN DOING LIFTING WORK. MUCH MORE THAN NORMAL OPERATIONS. THIS LOADS AND UNLOADS THE TAILBOOM NUMEROUS TIMES. THE RESULTING CRACKS ARE DUE TO THE FATIGUE ON THE SKIN. RECOMEND THICKER SKIN OR A DIFFERENT TYPE ALUMINUM. (2003-6-1) 1G71 4U4 U EXPA1G71E1EA 20030827000502003082700050SW 2003 8 27 ALG2003F00059 120030511A6510VNMK47498 BEARING BELL 206 206L1 1182107SW ALLSN 250C 250C* GL T/R DRIVESHAFT BINDING A ALGAK NONE O OTHER ININSP/MAINT 1 SW035734M17439876 45449 DURING DAILY SERVICE CHECK WHEN MAIN ROTOR BLADES WERE BEING ROTATED TO BE SECURED. BINDING/ RATCHETING NOISE WAS HEARD WHEN MAIN ROTOR BLADES WERE ROTED. FURTHER INVESTIGATION REVEALED THAT NOISE WAS COMING FROM NR4 TAIL ROTOR DRIVESHAFT BEARING. BEARING DID NOT LOOK OVERHEATED. 1G71 3U3 U H2SW E4CE 20030827000542003082700054NM 2003 8 27 F3LA200300122 120030622A21317638101 CONTROLLER BOEING737 73736E 138443ANM CABIN PRESSURE INOPERATIVE A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03314FL 210 25256 AIR TURN BACK. FLIGHT CREW REPORTED ALTITUDE WARNING HORN SOUNDED WHILE CLIMBING THROUGH 23,000 FT. STARTED DESCENT TO 10,000 FT. COMPLETED CHECKLIST AT 10,000 FT. IN MANUAL MODE AND AIRCRAFT STARTED PRESSURIZING. DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. ON THE GROUND, THE AIRCRAFT PRESSURIZED TO 2,000 FT. HAD TO OPEN THE OUTFLOW VALVE USING THE MANUAL MODE TO DEPRESSURIZE AIRCRAFT. PERFORMED TROUBLESHOOTING OF THE CABIN PRESSURE SYSTEM IAW MM 21-31-00, PAGES 501-522. AUTO SYSTEM BAROMETRIC CORRECTION FAILED STEPS 2.4.G, ALL OTHER SYSTEMS (STANDBY, MANUAL) OPERATED NORMALLY. REPLACED CABIN PRESSURE CONTROLLER AND TESTED THE SYSTEM IAW MM 21-31-00. SYSTEM CHECKED NORMAL IN ALL MODES. 2L72 4F RTA16WE 20030827000762003082700076NM 2003 8 27 SWAA031881 120030821A552365C26384 BEARING BOEING737 7377H4 1384404NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED PM CHECK, SWA SI 11038-55,FOUND LT ELEVATOR TAB HINGE BEARINGS WORN AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPLACED HINGE BEARINGS AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2L72 4F RTA16WE 20030827001072003082700107NE 2003 8 27 CALA0300468 220030815A7250 BLADE BOEING757 757224 1384958NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE FAILED A CALAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW2719130 28970 31308 THE NR 1 ENGINE BEGAN TO VIBRATE WHILE ENROUTE. THE VIBRATION GAGE WAS AMBER AT 5.2. THE ENGINE WAS BROUGHT TO IDLE AND THE VIBRATION DECREASED INITIALLY THEN WENT BACK UP TO 5.3. THE CREW SHUT THE ENGINE DOWN AND DIVERTED, WHERE THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. METAL WAS FOUND IN THE NR 1 ENGINE EXHAUST. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ENGINEERING INVESTIGATION REVEALED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO THE FAILURE OF AN INTERMEDIATE PRESSURE TURBINE BLADE. 2L72 4F4 FRTA2NM E12EU 20030827001192003082700119NM 2003 8 27 CALA0300464 120030811A5730 SKIN BOEING737 7373T0 1384582NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 4 SLAT ACTUATOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-41-01. 2L72 4F RTA16WE 20030827001202003082700120NM 2003 8 27 CALA0300364 120030707A3230 CIRCUIT BREAKER BOEING737 7373T0 1384582NM LANDING GEAR TRIPPED A CALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2717316 23367 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM OKC. THE GEAR HANDLE WOULD NOT GO PAST THE OFF POSITION. CREW ATTEMPTED TO USE OVERRIDE WITH NO SUCCESS. THE AIRCRAFT WAS RETURNED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LATCH AND PRESS WARNING CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET AND A GEAR SWING CHECKED GOOD. 2L72 4F RTA16WE 20030827001382003082700138EU 2003 8 27 2003UALA00551 120030710A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29419UA 487 LIGHTNING STRIKE DAMAGE AT FRAME 24, 3 INCHES BELOW STRINGER 36L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SOLID FASTENER. 2L72 4F4 FRTA28NM E40NE 20030827001432003082700143NM 2003 8 27 2003UALA00536 120030703A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 MAIN CABIN STATION 246 FLOORBEAM IS CORRODED AT RBL 78- T-CAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS . 2L72 4F4 FRTA1NM E24NE 20030827001492003082700149NM 2003 8 27 2003UALA00580 120030721A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29526UA 24994 LT EXTERNAL FUSELAGE SKIN HAS 4 EA DENTS AT STATION 600-620 AND BETWEEN STR 15-17. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20030909000232003090900023EA 2003 9 9 SWIA200312334 120030824A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913SW 7597 FS 484 LT INTERCOSTAL OUTBOARD FLANGE CRACKED LBL 36. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRT REO 601R-53-41-059 REV. 'A'. 2L72 4F RTA21EA 20030909001522003090900152 2003 9 9 ALGA088898 420030828A83006898642 GEARSHAFT CLARK 1000 1000CLARK 2230102SW GEARBOX CORRODED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO GEARSHAFT HAS CORROSION ON SURFACE OF GEAR. 1Q71 3R 2A6 20030909002402003090900240NE 2003 9 9 ABX030320 220030801A7200CF680A ENGINE BOEING767 767281 1385109NM GE CF6 CF680A 30025NE LEFT MALFUNCTIONED A ABXAA UNSCHED LANDING EY VIBRATION/BUFFET ENGINE STOPPAGE CRCRUISE 1 GL23785AX370434432 23018 580239 LT ENGINE OIL PRESSURE AND QUANTITY LOSS WITH 5.1 VIBRATION THAT COULD BE FELT THROUGH THE AIRCRAFT AND THE ENGINE SHUT DOWN. REPLACED ENGINE IAW WORK PACK 600178060. 2L72 4F4 FRTA1NM E13NE 20031006000072003100600007EA 2003 10 6 COMA0370029 120030907A3250530133 TILLER CNDAIRCL600 CL6002C10 1390015EA NLG STEERING MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01317CA2386 10055 FLIGHT 454 NOSE WHEEL STEERING FAIL CAUTION MESSAGE. REPLACED THE TILLER. 2L72 4F RTA21EA 20031006000172003100600017EU 2003 10 6 MALA030417 120030816A5711 SPAR BAC 146 AVRO146RJ85A1500097EU RT WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK IN CVG, RT WING FALSE SPAR CRACK BETWEEN RIB NR 5 AND 6. MAINTENANCE REPAIRED IAW BAE/FAX:BARA/AVR/6476/03-MK. A/C RELEASE DATE 9/2/03. REFER TO 409 NR 190372 FOR DETAIL. 2H74 4F RTA49EU 20031006000332003100600033NM 2003 10 6 AWXA200301059 120030814A5754656710836 DOOR BOEING737 737277 1384570NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK .1250 INCH CRACK WAS FOUND ON NR 4 SLAT ACTUATOR CLOSE OUT DOOR, WBL 279.25. MAINTENANCE REMOVED CRACKED NR 4 SLAT ACTUATOR CLOSE OUT DOOR; FABRICATED A NEW REPLACEMENT DOOR; INSTALLED REPAIR PART IAW BMM 20--050-011-2, FIG. 203. 2L72 4F RTA16WE 20031006000492003100600049WP 2003 10 6 UO22003F00002 220030904A723030733931 IMPELLER LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE731* 01518WP HP COMPRESSOR FAILED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19575WW5766 043 P74223 HP IMPELLER FAILED, CAUSING DAMAGE TO ENGINE. 2L72 4F4 F A10CE E6WE 20031006000862003100600086SO 2003 10 6 C2XA03CL165 120030916A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715941 145035 DURING ROURINE MAINTENANCE THE NR 5 EMERGENCY LIGHT INVERTER WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 5 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031006000872003100600087EU 2003 10 6 PNSA030802 120030812A7603 LEVER SAAB SF340 340B 7860101EU RT CONDITION OUT OF RIG A PNSAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 AL03590MA 340B181 CTOT INOPERATIVE ON TAKEOFF ROLL. PILOT ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND RT CONDITION LEVER RIGGING OUT OF RIG. CONDITION LEVER WAS IN TORQUE MOTOR LOCKOUT WHILE INDICATING HIGH RPM POSITION. 2L72 4T RTA52EU 20031006000912003100600091NM 2003 10 6 0301753142 120030912A49901319A APU AIRBUSA319 A319114 3930350NM LEAKING A NWAAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01342NB3729 3729 01746 DURING CLIMB AND CRUISE, FLIGHT ATTENDANT REPORTED AN ODOR IN THE CABIN. EVENTUALLY COCKPIT CREW ALSO NOTICED THE ODOR. FLIGHT CONTINUED TO DESTINATION AND AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND AN APU OIL LEAK. REPLACED THE APU, PACK BURNOUT PERFORMED, AND OZONE CONVERTERS AND RECIRCULATION FILTERS WERE REPLACED. 2L72 4F RTA28NM 20031006001972003100600197NM 2003 10 6 03FDEA01585 120030908A5712 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OUTBD FLAP FWD RIB SUPPORT ISLAND FOUND ONE CRACK APPROX 3/16 IN LENGTH AT OUTBOARD SIDE. LT OUTBOARD FLAP FWD RIB SUPPORT ISLAND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71897. 2L73 4F RTA22WE 20031007000262003100700026EA 2003 10 7 ASOA03403 120030825A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 DURING A C-CHECK IN MCN, THE RIGHT SIDE FS 718 FRAME SKIN BELOW THE DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT SIDE FS 718 FRAME SKIN BELOW THE DOUBLER IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20031007000442003100700044 2003 10 7 AALA20030188 420030205A25655A33073 SLIDE BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21944AN 29535 DURING OVERNIGHT MAINTENANCE WHILE ACCOMPLISHING PATTERN CARD SLIDE DID NOT INFLAT DURING AUTOMATIC FUNCTION. PULLED MANUAL INFLATION HANDLE AND SLIDE STILL DID NOT INFLATE. MOVING INFLATION BOTTLE SLIDE INFLATED. REPLACED SLIDE AND INFLATION BOTTLE. SYSTEM GROUND CHEKCED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20031007000742003100700074NM 2003 10 7 SWAA031948 120030828A53116935365 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20031007000802003100700080NM 2003 10 7 SWAA031954 120030830A3350 POWER SUPPLY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY AND POWER SUPPLY PER MM. 2L72 4F RTA16WE 20031007000942003100700094 2003 10 7 SWAA031992 420030906A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031008000122003100800012NM 2003 10 8 03FDEA01550 120030916A5320A5A7116507 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CENTER CARGO PIT HAS A POSSIBLE CRACK AT STR 47R STA 1540 UNDER PANEL 183CF JUST AFT OF TRANSVERSE SPLICE. 2L73 4F RTA22WE 20031008000142003100800014NM 2003 10 8 03FDEA01544 120030916A3230656021132 ACCESSORY UNIT BOEING727 727200 138407ENM E&E BAY FALSE INDICATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25478FE 21395 LANDING GEAR LEVER LATCH FAILED TO RELEASE DURING GEAR RETRACTION. THE QRH PROCEDURE ON PAGES 2-6-2-12 /13 COMPLIED WITH. LANDING GEAR FAILED TEST NR 1 OF THE PROCEDURE. WHEN THE FLAPS WERE RETRACTED FROM 5 TO 2 DEGREES. AN INTERMITTENT HORN SOUNDED. AN EMERGENCY WAS DECLARED AND UNEVENTFUL LANDING WAS MADE ON RWY 27 AT MEM. R & R MLG ACCESORY UNIT IAW 727-200 AMM 32-09-121-5. JACKED A/C, RETRACTED AND EXTENDED GEAR SEVERAL TIMES, NO DEFECTS NOTED. R & R MLG CONTROL LEVER LOCK SOLENOID PER M/M 32-31-016-4.STILL REQUIRES OPS CK. COMPLETED OPS TEST OF LEVER LOCK SOLENOID AND ALSO RAN GROUND OPS TEST OF LDG GEAR ELECTRONIC MODULE. 2L73 4F RTA3WE 20030910000432003091000043 2003 9 10 I05R088213 420030628A220043800100030 GYRO UROCOPEC135 EC135P1 8680990EU TAIL BOOM MALFUNCTIONED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05552BA 190 AIRCRAFT HAD A PROBLEM WITH THE GYRO CAUTION LIGHT. REPLACED PART. 1G72 3U O H88EU 20030910000752003091000075NM 2003 9 10 DHL2003749008 120030802A2920 HYDRAULIC LINE BOEING727 727200 138407ENM HYD SYSTEM LEAKING A DHLAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO01749DH 22013 HYDRAULIC SYSTEM-B FAILED EN ROUTE MTY-CVG. LOST ALL B-SYSTEM HYDRAULIC QUANTITY. ALL ABNORMAL PROCEDURES/CHECKLIST ACCOMPLISHED PER M/M 29-00-00. REMOVED AND REPLACED B-SYSTEM HOSE ASSEMBLIES TO AND FROM NR 2 HYDRAULIC PUMP. SERVICED HYDRAULICS. OPS AND LEAK CHECKED GOOD. 2L73 4F RTA3WE 20030910000862003091000086WP 2003 9 10 DHL2003604643 120030527A5754 SKIN DOUG DC8 DC873F 302199FWP SLOT VANE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT INBOARD SLOT VANE OUTER PLATING SHOWS ELONGATED HOLES AT STA XS 247.000. PERFORMED MAJOR REPAIR. REMOVED FASTERNERS FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR EXTERNAL DOUBLER AN INTERNAL DOUBLER AND A FILLER IAW EODHL-030561, ED-3291. CLEANED, TREATED AND PRIMED EXTERNAL DOUBLER INTERIOR SURFACE, FILLER AND INTERNAL DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED EXTERNAL DOUBLER, INTERNAL DOUBLER AND FILLER ON RT WING INBOARD SLOT VANE OUTER PLATING, STA XS 247.000 USING NEW FASTENERS IAW EODHL-030561, ED-3291 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000902003091000090NE 2003 9 10 2003UALA00552 220030711A7261ST201014 ADAPTER BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 1 ENGINE CRACKED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29769UA 26921 777053 RETURN TO FIELD DUE TO NR 1 ENGINE OIL TEMP. INDICATED OVER TEMP. THE TUBE-TO-BOSS ADAPTER, WHICH SECURES THE 12TH STAGE AIR COOLING LINE FROM THE NR 3 BEARING BUFFER AIR COOLER WAS FOUND CRACKED. THIS FAILURE RESULTED IN LOSS OF 12TH STAGE COOLING AIR FROM THE BUFFER AIR COOLER TO THE NO. 3 BEARING COMPARTMENT. THIS IS A "FIRST-OF-KIND" FAILURE. 2L72 4F4 FRTT0001SE E46NE 20030910001092003091000109NE 2003 9 10 MWEA030318 220030818A73217436024 FUEL CONTROL DOUG DC9 DC914 3022034WP PWA JT8 JT8D7B 52053NE ENGINE MALFUNCTIONED A MWEAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 GL31700ME 45696 CREW OBSERVED THE N2 SLOWLY DROP TO 40 PERCENT. REMOVED AND REPLACED ROD END AND PERFORMED ENGINE TRIM ALL PARAMETERS NORMAL. ALSO REPLACED FUEL CONTROL. 2L72 4F4 F A6WE E2EA 20030910001102003091000110NM 2003 9 10 MWEA030357 120030902A53205930544133 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CABIN FLOOR SUPPORT AT STATION 256 BETWEEN SEAT TRACK 3 AND 4. FABRICATED AND INSTALLED NEW SUPPORT. 2L72 4F RTA6WE 20030910001142003091000114WP 2003 9 10 MWEA030351 120030828A32600080004003 PROXIMITY SWITCH DOUG DC9 DC932 3022066WP LT MLG FAULTY A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31202ME 47672 RED LEFT GEAR UNSAFE LIGHT CAME ON ALONG WITH HORN. REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX. 2L72 4F A6WE 20030910001372003091000137NM 2003 9 10 MWEA030347 120030827A524039361901 ATTACH FITTING DOUG MD88 MD88 3023688NM SERVICE DOOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FORWARD GALLEY SERVICE DOOR AFT GIRT BAR LATCH ATTACH FITTINGS IS CORRODED. FABRICATED AND INSTALLED NEW FITTINGS. 2L72 4F RTA6WE 20030910001412003091000141WP 2003 9 10 MWEA030362 120030904A2913AS66411LS666 PUMP DOUG DC9 DC981 3022081WP ENGINE FAILED A MWEAO OTHER J WARNING INDICATION CLCLIMB 1 GL31812ME 48006 HYDRAULIC PRESSURE LOW ANNUCIATOR LIGHT ILLUMINATED. REMOVED AND REPLACED HYDRAULIC PUMP. 2L72 4F A6WE 20030910001542003091000154WP 2003 9 10 GTIA030610 120030629A7830 ACCOUSTIC LINER DOUG DC9 DC982 3022082WP THRUST REVERSER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND NR 2 ENGINE THRUST REVERSER INNER ACCOUSTIC CORE MISSING/DELAMINATED AND 1 PIN WELD LOOSE. REPAIRED DAMAGED AREA. (M) 2L72 4F A6WE 20030910001552003091000155EA 2003 9 10 A6WA200340123 120030813A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A A6WAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL31416AW 7603 STAB TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PER QRH. MACH TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PRE QRH. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW 27-41-01, GROUND OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030910001572003091000157EA 2003 9 10 ASOA03364 120030808A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11844AS 7317 FLT 4784 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP AT ROW TWO WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW TWO. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030910001642003091000164EA 2003 9 10 ASOA03358 120030805A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11837AS 7271 FLT 4732 - DURING HANGAR MAINTENANCE IN BTR, THE RIGHT SIDE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030910001652003091000165EA 2003 9 10 ASOA03356 120030804A32347179015 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A ASOAK NONE J WARNING INDICATION APAPPROACH 1 SO11853AS1294 7374 FLT 4531 - DURING APPROACH INTO ATL FROM FAY, AFTER EXTENDING THE LANDING GEAR, THE CREW RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. THE CREW COMPLIED WITH QRH PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE GEAR HANDLE ASSEMBLY AND PERFORMED TEN GEAR SWINGS WITHOUT ANY DEFECTS NOTED. OPS CHECKS GOOD. AIRCRAFT OK SERVICE. (M) 2L72 4F RTA21EA 20030910001682003091000168SO 2003 9 10 SIMA200321805 120030729A532014521713005 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21713AE 145249 ABI - DURING AN IMBV INSPECTION, THE GALLE FLOOR CENTER BEAM WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER BEAM AND INSTALLED NEW BEAM. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-20-01,03, 51-40-02,04. RESTORED SURFACE AND APPLIED CORROSION PREVENTIVE. (M) 2L72 4F RTT00011AT 20030910001722003091000172SO 2003 9 10 SIMA200321807 120030719A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21815AE 145545 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED NUT PLATE FROM ATTACHED AREA. COMPLETELY REMOVED CORROSION BY BLENDING. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREA WITH NO DEFECTS NOTED. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2423B, AND STANDARD EMB 140 SRM, SRM 145/1142 REV 22. (M) 2L72 4F RTT00011AT 20030910001742003091000174SO 2003 9 10 SIMA200322503 120030808A532014521725615 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND CLEANED THE REPAIR AREA. INSTALLED NEW SILL IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-20-03, 51-40-06 AND 51-40-02. (M) 2L72 4F RTT00011AT 20030910001772003091000177EU 2003 9 10 SIMA200322304 120030810A335066362 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21901AE 340B401 CLL - FLT 3280 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT ROW 8 TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030910001862003091000186SO 2003 9 10 SIMA200320802 120030722A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 ABI - DURING AN IMBV INSPECTION, CORROSION FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. COMPLETELY REMOVED CORROSION BY CREATIN A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND A PLATE. REPAIR DONE IAW EMB 145 SRM, 145-1142 REV 22, 53-21-10 PARA 2 FIG 201 SHEET 1, AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030910001912003091000191NE 2003 9 10 MEX2003386 220030823A7200 ENGINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RIGHT MALFUNCTIONED A ASMFD RETURN TO BLOCK Y ENGINE STOPPAGE TXTAXI/GRND HDL 1 SW23301AM 30045 FLT 494 - MID-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER RIGHT ENGINE STARTED, IT SHUT DOWN. RIGHT ENGINE AND EICAS MESSAGES WERE CHECKED IAW 72-00-00 AND RIGHT ENGINE WAS RESTARTED, ALL CORRECT. DURING OVERNIGHT SERVICE, RIGHT ENGINE WAS STARTED AT DIFFERENT POWER SETTINGS IAW MM 71-00-01, ALL TESTS CORRECT. (M) 2L72 4F4 FRTA2NM E17NE 20030910001922003091000192CE 2003 9 10 2003F00550 120030716A5511 SPAR BEECH 1900 1900D 1154162CE HORIZ STAB CRACKED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1969547 UE189 AT SCHEDULED EMPANNAGE ZONAL INSPECTION, FOUR CRACKS FOUND RADIATING FROM PASSAGE HOLE IN FORWARD WEB OF THE HORIZONTAL STABILIZER FORWARD SPAR. REMOVED SECTION OF CRACKED SKIN. FABRICATED AND INSTALLED SHIM AND DOUBLER IAW FAA APPROVED DATA CONTAINED IN DER 8110-3, REPORT NR 030715. (M) 2L72 4T RTA24CE 20030910002012003091000201EU 2003 9 10 MALA030368 120030803A7603M83726282001P RELAY SAAB SF340 340B 7860101EU E/E BAY FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15364PX 340B262 DURING FLIGHT NR 3117, F1 STOOP OPEN LIGHT ILLUMINATED JUST AFTER TAKEOFF FROM MEM. AIR RETURN TO MEM. NO OTHER ABNORMALITIES. MAINTENANCE REMOVED AND REPLACED RELAY AT RDI POSITION 82KA PN M83726-28-2001P NSN IAW AMM 76-10-60-1 FIG 101 OPS CHECK DONE AMM 76-10-60 AND IAW JOB CARD #76-10-60. OPS CHECK GOOD. 2L72 4T RTA52EU 20030910002092003091000209EU 2003 9 10 MALA030350 120030729A3520 HOSE SAAB SF340 340B 7860101EU PAX O2 BOTTLE BROKEN A MALAK NONE O OTHER ININSP/MAINT 1 GL15402XJ 340B402 DURING PREFLIGHT INSPECTION OF FLIGHT NR 2994, PAX O2 BOTTLE HOSE BROKEN. MAINTENANCE CUT END AND REATTACHED TO O2 BOTTLE. 2L72 4T RTA52EU 20030910002132003091000213EU 2003 9 10 MALA030348 120030724A2910 HYDRAULIC LINE SAAB SF340 SF340A 7850100EU HYD SYSTEM BURST A MALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL1599XJ 340A099 ON TAKEOFF OF FLIGHT NR 3257, HYDRAULIC CAUTION LIGHT ILLUMINATED. A NOISE SIMILIAR TO A POP OCCURED AND THE HYDRAULIC CAUTION LIGHT ILLUMINATED. MAIN ACCUMLATOR WENT TO ZERO AND HYD QTY WAS DECREASING ONLY LT MAIN RETRACTED QRH WAS COMPLETED AND HYDRAULIC PUMP WAS TURNED OFF. HYDRAULIC QUANTITY STABILIZED, BUT MAIN REMAINED AT ZERO. DECLARED AN EMERGENCY. MAINTENANCE FOUND UPPER LINE ON NLG ACTUATOR BURST AND LEAKING. INSTALLED NEW LINE AND REPLACED LT AND RT SEPARATION BOLTS. SERVICED HYDRAULIC SUPPLY AND CLEANED NLG BAY AS REQUIRED. SEE 409 NR 168226 FOR DETAILS. ALL FUNCTIONAL CHECKS GOOD. 2L72 4T RTA52EU 20030910002242003091000224EU 2003 9 10 MALA030392 120030728A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 DURING C-CHECK IN CVG, NR 4 SEAT RAIL AT FRAME 20A HAS CORROSION ON UPPER SURFACE. MAINTENANCE REPAIRED IAW EO NR A53026. A/C RELEASE DATE 8/11/03. REFER TO 409 NR 128569 FOR DETAIL. 2H74 4F RTA49EU 20030910002252003091000225EU 2003 9 10 MALA030394 120030828A5220 SEAL SAAB SF340 340B 7860101EU EMERGENCY EXIT LOOSE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15423XJ 340B423 RT FORWARD EMERGENCY DOOR SEAL IS LOOSE. RESECURED SEAL. 2L72 4T RTA52EU 20030911000082003091100008NM 2003 9 11 03FDEA01290 120030806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 SNRM N0456 3A RT OB FLAP IB HINGE 28 2FC SIDE 29 BOTH IB AND OB UPPER ATTACH HOLES CORRODED AT BORES. RT WING OUTBOARD FLAP INBD HINGE ( A/C SIDE ) BOTH INBOARD AND OUTBOARD UPPER ATTACHED HOLES BORES REPAIRED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030911000162003091100016NM 2003 9 11 03FDEA01310 120030808A5753ARC0502403 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING - O/B FLAP, I/B FWD HINGE FITTING HAS SURFACE CORROSION ON SPOT FACES OF THE PIVOT BEARING MOUNT HOLE. LT WING O/B FLAP, I/B FWD HINGE FITTING PIVOT BEARING MOUNT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030909002122003090900212WP 2003 9 9 ABXA030339 120030804A5320D0489841 WEB DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 RIGHT CUSP WEB CRACKED JUST FORWARD OF FS 1041 BULKHEAD. REPAIRED RIGHT CUSP WEB JUST FORWARD OF FS 1041 IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030910000492003091000049WP 2003 9 10 DHL2003604544 120030502A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING CENTER L/E FORMER CRACKED 1.000, AT XFS 416.500 (UPPER PART). STOP DRILLED CRACK AT XFS 416.500 AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910001052003091000105NM 2003 9 10 MWEA030312 120030817A3240DC62105LJ35N SENSOR DOUG MD88 MD88 3023688NM MLG BRAKE FAULTY A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31601ME 49762 BRAKE TEMPERURE CLIMBED TO 250 DEGREES. REMOVED AND REPLACED BRAKE SENSOR. 2L72 4F RTA6WE 20030910001072003091000107WP 2003 9 10 MWEA030363 120030906A2797D553H24 WIRE DOUG DC9 DC932 3022066WP RUDDER BROKEN A MWEAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 GL31302ME 47102 RUDDER TRAVEL UNRESTRICTED LIGHT NOT ON. FOUND WIRE BROKEN NEAR RUDDER, REPAIRED WIRE. 2L72 4F A6WE 20030910001112003091000111NM 2003 9 10 MWEA030359 120030902A533059360461 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 RIGHT WING FILLET PANEL LOWER CHAFE STRIP AREA BLENDED OUT OF LIMITS AT FRAME STATION 806. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030910001122003091000112NM 2003 9 10 MWEA030360 120030902A533059360461 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 RIGHT WING FILLET PANEL LOWER CHAFE STRIP AREA BLENDED OUT OF LIMITS AT FRAME STATION 769 AND 778. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030910001182003091000118WP 2003 9 10 MWEA030365 120030909A5330591287060 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CANNING A MWEAK NONE O OTHER ININSP/MAINT 1 GL31216ME 47740 EVIDENCE OF OIL CANNING RIGHT SIDE OF FUSELAGE UNDER PYLON STATION 1006 LONGERON 8 RIGHT AND LONGERON 17 RIGHT. FABRICATED AND INSTALLED REPAIR SPLICE AND DOUBLER. 2L72 4F A6WE 20030910001192003091000119WP 2003 9 10 MWEA030366 120030909A5330591142739 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CANNING A MWEAK NONE O OTHER ININSP/MAINT 1 GL31216ME 47740 EVIDENCE OF OIL CANNING ON RIGHT SIDE OF FUSELAGE UNDER PYLON STATION 988 LONGERON 17,18 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20030910002192003091000219EU 2003 9 10 MALA030363 120030731A7931IPTE1191000200 TRANSDUCER SAAB SF340 340B 7860101EU LT ENGINE LEAKING A MALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15370PX 340B300 DURING FLIGHT CREW NOTED LT ENGINE OIL PRESSURE CONTINUALLY DROPPING INFLIGHT. RED WARNING LIGHT WAS ON. SHUTDOWN ENGINE AND DIVERTED TO SDF. MAINTENANCE FOUND OIL LEAKING FROM LT ENGINE TRANSDUCER REFER TO 409 NR 181832 FOR DETAIL. MAINTENANCE REPLACED RT OIL PRESS TRANSDUCER PN IPTE119-1000-200D1 SN/ON 67338-114, SN/OFF 55471-1-552 AMM REF 79-30-05-4. 2L72 4T RTA52EU 20030910002202003091000220EU 2003 9 10 MALA030389 120030728A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 DURING C CHECK INSPECTION IN CVG, MAINTENANCE FOUND FLOOR FRAME 18 BETWEEN NR 3 & NR 4 SEATRAILS WITH CORROSION. REPAIRED IAW EO NR A53126. A/C RELEASE DATE 8/11. REFER TO 409 NR 128559 FOR DETAIL. 2H74 4F RTA49EU 20030911000322003091100032WP 2003 9 11 DHL2003803015 120030819A3350 BATTERY DOUG DC8 DC873 302199CWP EMERGENCY LIGHT INOPERATIVE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01803DH 46123 EMERGENCY LIGHTS BATTERY CHARGER CIRCUIT BREAKER WILL NOT RESET. REMOVED AND REPLACED EMERGENCY BATTERY LIGHT BATTERY AND RELAY UNIT IAW M/M 33-50-1 OPS CHECKED SERVICEABLE. 2L74 4F RT4A25 20030911000342003091100034NM 2003 9 11 03FDEA01258 120030812A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAO OTHER O OTHER ININSP/MAINT 1 SO25215FE 22936 CORROSION ON LOWER FLANGE OF FLOORBEAM BS 720 LBL 46 TO RBL 46 WL 200. REMOVED CORROSION ON BS 720 FLOORBEAM LOWER CHORD LBL 46 TO RBL 46, WL 200. ALL AREAS WITHIN LIMITS EXCEPT AT LBL 5 AND THIS AREA WAS REPAIRED PER FED EX EA 7- 5310-72309. 2L73 4F RTA3WE 20030911000452003091100045WP 2003 9 11 DHL2003873533 120030623A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 ITEM REF N/R 0621: NOSE SECTION RT TUNNEL FRAME AT STA -32.000 WITH 2.000 CRACK IN IT.(MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED DAMAGED FRAME IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FRAME IAW SRM 53-2-0 FIG 2. HEAT TREATED IAW SRM 51-1-1 PG 11. CLEANED, TREATED AND PRIMED FRAME IAW SRM 51-1-8B. INSTALLED FRAME WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911000522003091100052WP 2003 9 11 DHL2003873557 120030626A5522 SKIN PANEL DOUG DC8 DC873F 302199FWP LT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT ELEVATOR UPPER PLATING HAS DENTS AND CORROSION FROM STA XE.246.000 TO XH.285.000. PERFORMED REPAIR REMOVED FASTENERS AND THE DAMAGED SKIN PANEL. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-030607, ED-3432. CLEANED, TREATED AND PRIMED THE NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON LT ELEVATOR UPPER SURFACE (STA. XE.246.000 XH-285.000) USING NEW FASTENERS. SEE N/R 2156 FOR REBALANCING. SEE JC BX3H55074 FOR LT ELEVATOR REMOVAL AND REINSTALLATION 2L74 4F RT4A25 20030911000542003091100054CE 2003 9 11 DXTA200300066 120030714A3260 BULB CESSNA500 560CESSNA 2076750CE MLG INDICATOR INOPERATIVE E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07372QS 5600372 RT MAIN LANDING GEAR INDICATOR LIGHT IS INOPERATIVE, BLEW THE GEAR DOWN PER THE CHECKLIST. THREE GREEN LIGHTS NOW APPEAR ON AND TEST CORRECTLY AFTER LANDING. - REPLACED GEAR POSITION INDICATING BULBS PER CESSNA 560 MM CHAPTER 33-13-10, PERFORMED GEAR RETRACTION AND EXTENSION TESTS PER CESSNA 560 MM CHAPTER 32-30-00 FOUND NORMAL. SERVICED BOTTLE WITH NITROGEN PER CESSNA 560 MM CHAPTER 12-10-00. 2L72 4F RTA22CE 20030911000632003091100063NM 2003 9 11 03FDEA01155 120030728A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 DAMAGED FASTENER HOLES ON FRAME AT BS 1110, LBL 22, WL 152. CUT OUT MATERIAL FROM FRAME THAT HAD DAMAGED FASTENERS HOLES AT BS 1110, LBL 22, WL 152. FABRICATED REPAIR FROM HFAB53-FR-011, AND INSTALLED ALL IAW SRM 53-10-1, 51- 40-3, 51-30-5, 51-30-2, AND 51-10-2, FED-EX E.A. 7-5310-54912. 2L73 4F RTA3WE 20030911000692003091100069WP 2003 9 11 DHL2003873514 120030617A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING IB L/E FORMER CRACKED 0.250 AT STA XFS.603.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10, AND INSTALLED NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031006000702003100600070CE 2003 10 6 AMWA44 120030902A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07176YV UE176 RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-46, STRG 101-640000-42 ON RT SIDE AND STRG P/N 101-640000-41, STRG P/N 101-640000-37 (4EA CRACKS TOTAL ON THIS RIB) 2L72 4T RTA24CE 20031006000732003100600073CE 2003 10 6 AMWA47 120030904A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07166YV UE166 2 CRACKS FOUND ON RIB NR 1 ON LT SIDE AT STRINGER INTERSECTION STRINGER P/N 101-64000-37 AND 1 ON RH SIDE AT STRG P/N 101-640000-46. CRACKS LOCATED AT THE END RIVET ON JOGGLE OVER STRINGER BOTH LOCATIONS 2L72 4T RTA24CE 20031006000792003100600079CE 2003 10 6 AMWA52 120030903A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07167YV UE167 WHILE PERFORMING INSP IN THE VERT. STAB., THE RIB FLNAGE AT CANTED STAB. STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RT SIDE NEAR THE FWD, CENTER, AND AFT STRG. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03 2L72 4T RTA24CE 20031006000952003100600095CE 2003 10 6 DXTA200300089 120030817A2720EM40706 ACTUATOR CESSNA750 750 2076810CE RUDDER LIMITER MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07946QS926 7500195 DURING FLIGHT FROM VNY TO HPN THE RUDDER LIMIT FAIL "A" WARNING LIGHT ILLUMINATED. ACCOMPLISHED AIR TURN BACK TO VNY AND LANDED OVERWEIGHT. REMOVED AND REPLACED UPPER RUDDER LIMITER ACTUATOR WITH A REPAIRED UNIT. OPS CHECKED GOOD, WORK DONE IAW CESSNA 750 MM CHAPTER 27-23-00. 2L72 4J RTT00007WI 20031006000972003100600097CE 2003 10 6 DXTA200300108 120030902A521066113598 PUSHROD CESSNA560 560XL 2076702CE PWA 545 PW545A NE PAX DOOR CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07627QS 5605227 DURING ROUTINE INSPECTION FOUND MAIN ENTRY DOOR PUSHROD (OPENING/CLOSING) RUBBING AGAINST THE CUTOUT IN THE DOOR STRUCTURE. ADJUSTED PUSHROD TO PREVENT CHAFING, PERFORMED BLEND OUT REPAIR TO CABIN DOOR FORMER IAW MFG REPAIR DEFINITION REPORT NR S-560XL-5227/01RD. 2L72 4F4 FRTA22CE E00059EN 20031006001002003100600100GL 2003 10 6 00067538 320030821A6110D50172 LATCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MCAULY5JFR C5JFR36C1104GL PROPELLER CRACKED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 960663 CRACK ON PROPELLER LATCH PAWL. 2L72 4T3 TRTA41NM E2WE 5 CP15NE 20031006001032003100600103NM 2003 10 6 2003UALA00671 120030908A5330 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29772UA 26930 LT EXTERNAL FUSELAGE SKIN AT STATION 835, BETWEEN STR 25L AND 26L DENTED AND CRACKED. MAJOR REPAIR ACCOMPLISHED. FLUSH REPAIR. 2L72 4F4 FRTT0001SE E46NE 20031006001092003100600109NM 2003 10 6 2003UALA00677 120030909A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29368UA 24537 AFT CARGO DOOR AFT EDGE OF CUTOUT IS DAMAGED APROX 16 INCH FROM LWR EDGE, WORN ON INSIDE AND CUT BACK ON OUTSIDE. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031006001122003100600112NM 2003 10 6 2003UALA00680 120030909A2150 RHEOSTAT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE TEMP SELECTOR INOPERATIVE A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29932UA 26658 LT PACK TEMP SELECTOR RHEOSTAT HAS SMOKE COMING OUT OF IT. CONTROL CABIN (LEFT PACK) TEMPERATURE SELECTOR RHEOSTAT FAILED. REPLACED RHEOSTAT. 2L72 4F4 FRTA16WE E2GL 20031006001132003100600113NM 2003 10 6 2003UALA00683 120030909A5414 SKIN BOEING777 777222 1385219NM NR 2 NACELLE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29228UA 30556 NR 2 NACELLE HAS A LARGE HOLE IN THE UPPER SKIN AT TWELVE O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND LIP SPLICE. 2L72 4F RTT0001SE 20031006001342003100600134NM 2003 10 6 SWAA032028 120030910A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, ABOVE STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031006001432003100600143NM 2003 10 6 SWAA032009 120030905A3350BR2013 WIRE BOEING737 7377H4 1384404NM EMERGENCY LIGHT EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 EEPLS WIRES EXPOSED AT ROW NR 8. SECURED WIRES PER MM. 2L72 4F RTA16WE 20031006001512003100600151NE 2003 10 6 SWAA032017 220030909A7200JT8D9 ENGINE BOEING737 7372T4 1384492NM PWA JT8 JT8D9 52048NE NR 2 LEAKING A SWAAK NONE K FLUID LOSS ININSP/MAINT 1 SW29702ML 22054 687808 NR 2 ENGINE FUEL LEAKING FROM ENGINE CASE DIRECTLY UNDER P/D VALVE. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 F A16WE E2EA 20031006001772003100600177NM 2003 10 6 03FDEA01640 120030926A5320 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION AFT CARGO BAY ON STRINGER CLIP BS 1050, RBL 14, WL 163. REMOVED CORROSION FROMS TR CLIP. ORIGINAL THICKNESS .040. AREA REMOVED 1 X 1 X .010 INCH. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR. CLIP AT BS 1050, RBL 14, WL 163. IAW SRM 51-30-2, 51-30-5, 53-10-1. 2L73 4F RTA3WE 20031006001782003100600178NE 2003 10 6 ARWA20030914 220030921A7532 BLEED VALVE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 1 ENGINE STUCK A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19441J 45688 UNABLE TO OBTAIN MAX POWER INDICATION WITH NR 1 TROTTLE AT IT'S FULL FORWARD STOP POSITION. FOUND NR 1 ENGINE SURGE BLEED VALVE STUCK OPEN; REMOVED AND REPLACED NR 1 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3; OPERATIONAL CHECK NORMAL IAW MM 71-00. 2L74 4F4 F 4A25 1E8 20031002001352003100200135 2003 10 2 250TR0024 420030910A2230P84000003 SWITCH BOEING737 7372K5 138448XNM AUTOTHROTTLE DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 AUTO THROTTLE WILL NOT ENGAGE. REPLACED BOTH AUTO THROTTLE DISCONNECT SWITCHES. OPS CHECKS OK PER MM 22-31-01. 2L72 4F RTA16WE 20031002001422003100200142NM 2003 10 2 CALA0300526 120030912A5230 SKIN BOEING737 737524 1384721NM C-2 DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716646 28907 INSPECTION FOUND C-2 DOOR OUTER SKIN DENTED ABOVE HANDLE. THE DOOR SKIN WAS REPAIRED IAW SRM 52-00-01. 2L72 4F RTA16WE 20031002001572003100200157EA 2003 10 2 SWIA200312377 120030909A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 COCKPIT/ESCAPE HATCH WILL NOT OPEN FROM OUTSIDE HANDLE. (DISCOVERED DURING ROUTINE INSPECTION) REMOVED AND REPLACED COCKPIT ESCAPE HATCH OUTER HANDLE DUE TO CORROSION IAW MM 52-22-03. OPS CHECK GOOD . 2L72 4F RTA21EA 20031002001752003100200175NM 2003 10 2 UPS03441219 120030907A5210 SKIN BOEING747 747SR46 1384816NM FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: SPV, COMPLY WITH D266098 L1 DOOR OUTER AFT SKIN IS CRACKED AT APPROX STA 472 AT APPROX WATER LINE 210. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-10-02 FIG 9, 51-10-02, 51-30-08. 2L74 4F RTA20WE 20031002001812003100200181WP 2003 10 2 15HA03580005 120030918A323024085571018 LEVER CVAC 580 580 2422806WP NLG CRACKED A I5HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23585P 163 AFTER TAKEOFF FROM PIT, EN ROUTE TO MIDDLETOWN, THE PILOT OBSERVED A LANDING GEAR 'UNSAFE' LIGHT AFTER GEAR RETRACTION. THE PILOT LOWERED THE GEAR AND PROCEEDED, GEAR DOWN, TO THE COLUMBUS MAINTENANCE FACILITY. THE LANDING GEAR 'UNSAFE' LIGHT WAS EXTINGUISHED WITH THE GEAR DOWN. DURING AN INSPECTION OF THE LANDING GEAR, A BROKEN NOSE LANDING GEAR DOWN LOCK RETRACT LEVER WAS DISCOVERED. THE LEVER WAS REMOVED AND REPLACED AND A LANDING GEAR RETRACTION WAS PERFORMED SUCCESSFULLY WITH THE AIRCRAFT ON JACKS. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RT 20031003000052003100300005NM 2003 10 3 AALA20030977 120030908A335002101991008 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A K NONE L NO TEST ININSP/MAINT 1 SW21612AA 24488 FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 17D BATTERY PACK FAILED DUAL FEED CHECK. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000062003100300006EU 2003 10 3 AALA20030747 120030714A3397 WIRE FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW211455K 11467 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHT WIRE PULLED FROM LIGHT FIXTURE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND SECURED WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031003000312003100300031EA 2003 10 3 ASOA03425 120030908A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031003000592003100300059SO 2003 10 3 C2XA03SH322 120030913A531514521718003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE RAMP ANGLE ON THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031003001022003100300102WP 2003 10 3 UPS03841222 120030827A53409754022504N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, FLOORBEAM FITTING IS CRACKED AT STA. 340 RBL. 58 REMOVED AND REPLACED FITTING IAW DWG. 9754022,AND SRM. 51-1-20D 2L74 4F RT4A25 20031006000362003100600036NM 2003 10 6 QXEA200301122 120030910A5720 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM RT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 AUXILARY STRUCTURE AT WING STATION YW389 IS DAMAGED BY OUTBOARD RT SPOILER ACTUATOR LOWER SURFACE. REPAIRED IAW Q400 SRM 51-42-05-330-801, 51-42-05 AND HORIZON AIR EA 6-51-15. 2H72 4T RTA13NM 20031006000552003100600055 2003 10 6 MEX2003413 420030907A3441HG1103BA01 IRU DOUG MD88 MD88 3023688NM POS 1 FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23161PL 49764 AIRCRAFT RETURNED TO PLATFORM DURING ENGINE STARTING THE IRS NUMBER 1 BATTERY LIGHT CAME ON AND THE ND AND PDF LT INFORMATION DISAPPEARED. THE IRS NR 1 AND BATTERY INERTIAL WERE REPLACED IAW MM, ALL TESTS CORRECT. 2L72 4F RTA6WE 20031006000932003100600093NM 2003 10 6 CALA0300529 120030905A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND CORROSION ALONG THE ENTIRE UPPER SECTION OF FLOORBEAM AT STA 967. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT AND A REPAIR SECTION WAS INSTALLED IAW ECRA 5311-01142. 2L72 4F RTA16WE 20031006001212003100600121NM 2003 10 6 EIA2003112 120030829A5310 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 SHEAR TIE L-ANGLE AT BS 2220 HAS HEAVY CORROSION ON BOTTOM LOWER FLANGE STR. 37L TO 41L. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR IAW B747 SRM 51-40-03 FIG 1, 51-10-01, 51-10-02, 51-30-02 AND BSOPM 20-41-2. 2L74 4F A20WE 20031006001382003100600138NM 2003 10 6 SWAA032032 120030910A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C3 CHECK, FOUND STRINGER CRACKED AT BS 947, STR 24R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20031006001602003100600160 2003 10 6 SWAA031963 420030903A2565 INDICATOR BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 FWD SERVICE DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030911000702003091100070WP 2003 9 11 DHL2003873515 120030616A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING CENTER L/E FORMER CRACKED 0.250 AT XFS.404.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS.404.000 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RT CENTER L/E FORMER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-0, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911000872003091100087WP 2003 9 11 DHL2003873531 120030628A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING IB L\E PLATING CORRODED, XFS.591.250 - XFS.685.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION FROM RT WING IB L\E PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. CUT OUT CORRODED PLATING IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED INNER SIDE OF FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FOR RT WING INBD L/E REMOVAL/INSTALLATION. 2L74 4F RT4A25 20030911000962003091100096WP 2003 9 11 DHL2003873505 120030614A5511 FRAME DOUG DC8 DC873F 302199FWP HORIZ STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT HORIZONTAL STAB L/E INNER FORMER CRACKED 0.500 AT XFS 60.000 (UPPER/LOWER PART). REMOVED FASTENERS IAW SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 55-2-0 PG 7,8. FABRICATED REINFORCING ANGLE IAW SRM 55-2-0 PG 7,8. CLEANED,TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 55-2-0 PG 7,8 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030911001052003091100105WP 2003 9 11 MWEA030317 120030818A3297 WIRE DOUG DC9 DC932 3022066WP MLG CONNECTOR OPEN A MWEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL31301ME 47190 UNABLE TO GET A GREEN DOWN LIGHT. FOUND OPEN WIRES IN RIGHT GEAR DOWN CONNECTOR, ALL ASSOCIATED WIRES WERE REPLACED. 2L72 4F A6WE 20030911001062003091100106WP 2003 9 11 UPS03841031 120030704A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, FRAME CORRODED AT STA 1420 AT L25R ABOVE D-PIT DOOR OPENING. REMOVED CORROSION IAW DC8 SRM 51-1-8. AREA OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED FRAME REPAIR DOUBLER IAW UPS EO DC8-5310-11728. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030911001092003091100109WP 2003 9 11 DHL2003873524 120030621A5542 SKIN PANEL DOUG DC8 DC873F 302199FWP RUDDER DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RUDDER LT PLATING DEFLECTED BETWEEN STA ZR.150.000 AND ZR.178.000. PERFORMED MAJOR REPAIR IAW EODHL-030601, ED-3422. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030601, ED-3422. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-0303601, ED-3422. CLEANED, TREATED AND PRIMED NEW SKIN PANEL IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON RUDDER LT PLATING BETWEEN STA ZR.150.000 - ZR.178.000 USING NEW FASTENERS IAW EODHL-030601, ED-3422 AND SRM 51-1-21 PG 1. SEE N/R 2141 FOR REBALANCING. 2L74 4F RT4A25 20030911001242003091100124NM 2003 9 11 03FDEA01295 120030806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBD FLAP OUTBOARD HINGE ( A/C SIDE ) LOWER INBOARD ATTACH HOLE CORRODED AT BORE AND FWD / AFT FACES. RT WING OUTBOARD FLAP OUTBOARD HINGE ( A/C SIDE ) LOWER INBOARD ATTACHMENT HOLE BORE AND FWD / AFT FACES REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030911001292003091100129NM 2003 9 11 03FDEA01199 120030729A5512ALC81072 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 HORIZONTAL STAB RT UPPER CENTER PLANK NR 26R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STABILIZER RT UPPER CTR PLANK NR 26R FITTING REMOVED & REPLACED AS PER FEDEX EA 1-5510-69397 - STABILIZERS - HORIZONTAL STABILIZER - FITTING ALC8107-2 FABRICATION. 2L73 4F RTA22WE 20030911001352003091100135NM 2003 9 11 03FDEA01323 120030815A5310 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 CORROSION ON FRAME AT STA 1010, STR 29R TO 29L, WL 138. BLENDED OUT CORROSION ON FRAME AT STA 1010, STR 29R TO 29L, WL 138. FOUND OUT OF LIMITS I.A.W. BOEING 727 SRM 53-10-1. REPAIRED BLEND OUTS PER BOEING 727 SRM 53-10-4, FIG 15, BOEING 727 SRM 51-10-6. 2L73 4F RTA3WE 20030911001472003091100147WP 2003 9 11 03FDEA01198 120030801A5720 ANGLE DOUG DC10 DC1030 3023501WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 N 651 RT WING L/E, CRACKED ANGLE AT XORS 317 CLOSING ACTION ON 07/30-03. REMOVED ANGLE IAW SRM 51-31-01.FAB NEW ANGLE IAW DPS 3.69. TREATED AND PRIMED IAW SRM 51-21-01, WITH 2024-T3 BATCH 545293, SERVICE ORDER 6016327.INSTALLED ANGLE IAW SRM 51-31-01. 2L73 4F A22WE 20030911001482003091100148WP 2003 9 11 DHL2003873589 120030630A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLOT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT OUTR WING CTR L/E SLOT LWR OUTR PLATING ELONG HOLES AROUND STA XFS.526.000. PERFORMED MJR REPAIR IAW EODHL-030613, ED-3456. REMOVED FASTNR IAW SRM 51-1-21 PG 1. BLENDED OUT ELONG HOLES SKIN AREA IAW EODHL-030613, ED-346. PERFORMED NDT INSP IAW NDT SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FAB A REPAIR DBLR IAW EODHL-030613, ED-3456. CLEANED, TREATED, PRIMED REPAIR DBLR INTR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALNT ON FAYING SURFACES IAW SRM 51-1-11. INSTALL DBLR ON LT OUTER WING CTR L/E SLOT LWR OUTR PLATING (AROUND STA. XFS.526.000) USING NEW FASTENERS IAW EODHL-030613, ED-3456, SRM 51-1-21 , SRM 51-1-20D. 2L74 4F RT4A25 20030911001492003091100149NE 2003 9 11 MEX2003387 220030823A7200 SHUTOFF VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803AM 26268 DURING PUSH BACK AND LEFT ENGINE STARTING, ENGINE VALVE LIGHTS TURNED ON, SPAR VALVE DID NOT GO OFF AND N2 WAS BETWEEN 25 PERCENT AND 30 PERCENT WITHOUT EGT INCREMENTATION. THE SPAR VALVE AND FUEL SHUTOFF VALVE WERE RESET IAW MM 73-10-01, ALL TEST CORRECT. DURING OVERNIGHT SERVICE THE LT ENGINE SHUTOFF VALVE AND APU SHUTOFF VALVE ACTUATORS WERE SWAPPED IAW MM 28-25-11, ALL CORRECT. (M) 2L72 4F4 FRTA2NM E17NE 20030911001552003091100155WP 2003 9 11 AALA20030340 120030311A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 FOUND DEEP STATIC DISCHARGE STATION 615 L21R. INSTALLED LONGERON SPLICE AND EXTERNAL PATCH TO DAMAGED AREA PER SRM 53-02-00- FIG 8. (M) 2L72 4F A6WE 20030911001622003091100162CE 2003 9 11 DXTA200300074 120030729A3241 BLEED VALVE CESSNA500 560CESSNA 2076750CE ANTI SKID SYS INOPERATIVE E DXTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07319QS 5600519 POWER BRAKE LOW PRESS LIGHT AND ANTI SKID INOP. LIGHT ILLUMINATED DURING TAXI, LIGHTS STAYED ILLUMINATED AFTER CESSNA EMERGENCY CHECK LIST COMPLETED. - TROUBLESHOT ANTI-SKID SYSTEM AND FOUND BLEED VALVE INOP, INSTALLED BLEED VALVE ASSY IAW MM 32-42-06. OPS AND LEAK CHECKED GOOD. 2L72 4F RTA22CE 20030911001642003091100164NM 2003 9 11 UPS03241013 120030731A2612 INDICATOR BOEING727 72751C 1384015NM CARGO FIRE MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION DEDESCENT 1 SO01902UP 18898 FIRE INDICATION IN LWR FWD PIT. CREW CLOSED BELL TESTED SYSTEM & FIRE INDICATION RETURNED. CREW DECLARED EMERGENCY & SHOT FIRE BOTTLE. A/C LANDED WITHOUT FURTHER INCIDENT. CFR CONFRIMED NO FIRE. PERFORMED LOWER CARGO COMPT SMOKE DETECTION SYSTEM ADJUSTMENT & TEST FOUND MX & SYS OK LIGHTS ILLUM DETECTOR F1717=ODB TESTED LOWER CARGO SMOKE DETECTION SYSTEM, NO FAULTS NOTED, OPS CHECK GOOD PER MM 26-18-00 THIS CLEARS MEL 26-19-1-2, PLACARD REMOVED. 2L73 4F A3WE 20030911001722003091100172WP 2003 9 11 DHL2003873609 120030707A532097540241 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FWD CARGO COMPT FLOORBEAM TO DOOR JAMB FITTING SHOWS 3.500 CRACK. (STA.280.000, RBL-45) PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031006001812003100600181NM 2003 10 6 03FDEA01645 120030926A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION GOUGE IN UPPER SURFACE OF FLOOR BEAM B/S 328, LBL 33, WL 208. REPAIRED IAW SRM 53-10-8. 2L73 4F RTA3WE 20031006001952003100600195NM 2003 10 6 03FDEA01589 120030908A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OUTBD FLAP OUTBD HINGE (FLAP SIDE) FOUND CORROSION ON INBD AND OUTBOARD PIVOT BORES AND SPOT FACES. RT OUTBOARD FLAP OUTBD HINGE (FLAP SIDE) INBD AND OUTBD PIVOT BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-72684. 2L73 4F RTA22WE 20031007000042003100700004NM 2003 10 7 AALA20030736 120030703A5330 SKIN BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21358AA 24039 FOUND FUSELAGE SKIN HAS SMALL CRACK INDICATION IN FASTENER HOLE, RIGHT SIDE, AREA 1 AT STATIN 1809.5, LOWER FORWARD FASTENER HAD CRACK INDICATION ON THE FUSELAGE SKIN ONLY. OVERSIZE THE HOLE IN THE SKIN ONLY TO 2ND OVERSIZE .341 INCH AND VERIFY CRACK IS REMVOED. REAMED SKIN ONLY FOR FREEZE PLUG. INSTALLED FREEZE PLUG PER SRM 767 51-20-01, INSTALLED FASTENERS AS REQUIRED. WORK ACCOMPLISHED IAW MRB 767-2506. FABRICATE AND INSTALL A RETAINER OVER THE FREEZE PLUG PER SRM 767/REQUIREMENTS. (M) 2L72 4F RTA1NM 20031007000052003100700005NM 2003 10 7 AALA20030803 120030728A2910 O-RING BOEING767 767223 1385123NM HYD SYSTEM LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21322AA 22323 CENTER HYDRAULIC QUANTITY LOSS INDICATION. AIRCRAFT DIVERTED AND LANDED ORD WITHOUT INCIDENT. REPLACED O-RING ON HEX NUT FOR FILTER SCREEN ON NR 10 SPOILER. SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031007000092003100700009NM 2003 10 7 AALA20030469 120030418A3350 LIGHT BOEING757 757223 1384957NM EXIT SIGN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 DURING OVERNIGHT MAINTENANCE, LT AFT EMERGENCY EXIT HATCH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT HATCH LIGHT ASSEMBLY. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000102003100700010NM 2003 10 7 AALA20030792 120030724A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT MISINSTALLED A AALAK NONE LW NO TEST INADEQUATE Q C ININSP/MAINT 1 SW21620AA 24578 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT 16D TO 23D INOPERATIVE. FOUND WIRE CROSSED AT SEAT 16D. RESPLICED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000112003100700011NM 2003 10 7 AALA20030682 120030623A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 4-6 INOPERATIVE. PLUGGED IN EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 4-6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000132003100700013NM 2003 10 7 AALA20030625 120030531A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21181AN 29591 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS UNDER EXIT MARKER AFT RIGHT LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP UNDER EXIT MARKER AFT RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000272003100700027EA 2003 10 7 ASOA03406 120030831A52102R5206B MOTOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ASSIST MOTOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031007000282003100700028NE 2003 10 7 ASOA03407 220030831A72614138T09P01 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE LEAKING A ASOAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11851AS 7360 DURING CLIMB-OUT FROM DFW-SAT, AT APPROX 19,000 FT THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW REDUCED THE RIGHT ENGINE TO IDLE. THE OIL PRESSURE CONTINUED TO FLUCTUATE BETWEEN 40 TO 45 PSI AND SHORTLY AFTERWARDS FLUCTUATED INTO THE RED RANTE. THE CREW FOLLOWED QRH PROCEDURES AND SHUT DOWN THE RT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN SAT. MAINTENANCE REMOVED AND REPLACED THE INTEGRATED DRIVE GENERATOR CARBON SEAL ASSY ON THE RIGHT ENGINE, THEN PERFORMED AN OIL CONSUMPTION CHECK. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20031007000322003100700032EU 2003 10 7 ASOA03401 120030828A3397M2275941249 WIRE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING AN 'A' CHECK IN MCN, THE AIRSTAIR DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE AIRSTAIR DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031007000612003100700061NM 2003 10 7 SWAA031975 120030904A53206551698 SPLICE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031007000642003100700064NM 2003 10 7 SWAA031978 120030903A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031007000712003100700071 2003 10 7 SWAA031945 420030830A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20031007000772003100700077NM 2003 10 7 SWAA031951 120030831A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B + 16, STR 17R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031007000792003100700079NM 2003 10 7 SWAA031953 120030829A335007912 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29790SW 30604 DURING SCHEDULED C4 CHECK, FOUND EEPLS LENS MISSING IN FWD CABIN. INSTALLED EEPLS LENS PER MM. 2L72 4F RTA16WE 20031007001032003100700103 2003 10 7 SWAA032001 420030907A2565D31354 INDICATOR BOEING737 7372H4 138448CNM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031007001042003100700104NM 2003 10 7 SWAA032002 120030908A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 20L. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20031007001122003100700112EA 2003 10 7 03243677 120030831A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27677BR 7652 DURING MAINTENANCE INSPECTION THE RIGHT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031007001202003100700120EA 2003 10 7 03246677 120030903A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27677BR 7652 DURING MAINTENANCE INSPECTION THE LEFT HAND EMERGENCY EXTERIOR EMERGENCY LAMP WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EXTERIOR EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031007001222003100700122EA 2003 10 7 03247411 120030904A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27411FJ 3166 DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL RE-ATTACHED THE EMERGENCY TRACK LIGHTING AND PERFORMED A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031008000042003100800004NM 2003 10 8 03251500 120030908A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27500FJ 3197 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031008000082003100800008EA 2003 10 8 03252630 120030909A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FAULTY A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING PREFLIGHT INSPECTION THE EMERGENCY TRACK LIGHTING WAS NOTED AS BEING DIM. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FOWARD TRACK LIGHTING STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031003000282003100300028EU 2003 10 3 AALA20030537 120030507A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211405J 11356 DURING OVERNIGHT MAINTENANCE, AFT CEILING EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED AFT CEILING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031003000502003100300050NM 2003 10 3 QXEA200301113 120030909A2913570347 PUMP DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09359PH8809 8809 514 ON FLIGHT 2154 EUG TO SEA AICRAFT DIVERTED TO PDX DUE TO NR 2 HYDRAULIC PUMP CAUTION ILLUMINATED AFTER TAKEOFF AND REMAINED ILLUMINATED UNTIL LANDING IN PDX. GEAR AND ASSOCIATED DOORS REMAINED EXTENDED FOR FLIGHT. ASSOCIATED NR 2 HYDRAULIC QUANTITY AND PRESSURE WENT IMMEDIATLY TO ZERO AFTER GEAR HANDLE WAS RETRACTED. ENGINE OPERATED WITH ZERO PRESSURE AND QUANTITY FOR APPROXIMATELY 55 MINUTES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031003000522003100300052NM 2003 10 3 QXEA200301115 120030909A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 EMERGENCY TRACK LIGHTING AT ROWS 5 AND 6 ARE BROKEN ON THE INBOARD SIDE. REMOVED AND REPLACED EMERGENCY LIGHTING. 2H72 4T RTA13NM 20031006000392003100600039NM 2003 10 6 QXEA200301117 120030911A2612 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM APU ILLUMINATED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09409QX 4051 ON FLIGHT 2364 FIRE DETECTION PANEL APU FAULT LIGHT. RESET APU INDICATOR CIRCUIT BREAKER. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031006001202003100600120SO 2003 10 6 LR7A03077 120030916A24203S2060DR113A1 VOLT REGULATOR LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL NR 1 ENGINE OVERHEATED A LR7AHEA DEACTIVATE SYST/CIRCUITSENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL03402LC 4698 DURING CLIMB OUT FROM ETAR CREW DETECTED ELECTRICAL OVERHEAT ODOR IN COCKPIT. FOUND NR 1 ENGINE GENERATOR VOLTAGE REGULATOR SMOKING. FIELD TRIPPED GENERATOR, NO EFFECT. ISOLATED THE LEFT AC BUS, NO EFFECT. SHUTDOWN NR 1 ENGINE AND SMOKE STOPPED. RETURNED TO ETAR. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION IAW HN51130, NO DEFECTS NOTED. REPLACED NR 1 VOLTAGE REGULATOR AND NR 1 GENERATOR IAW SMP 581 24-20. ENGINE RUN OPS CHECK NORMAL. 2H74 4T4 T A1SO E282 20031006001222003100600122NM 2003 10 6 EIA2003117 120030910A2613 WARNING LIGHT BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE COCKPIT INTERMITTENT A EIAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09480EV 20348 DURING CLIMB RT WING OVERHEAT LIGHT FLICKER DIM TO BRIGHT, STAYED ON THE FLICKER, DID SAME THROUGHOUT PROCEDURE (FULL) ABNORMAL LIGHT WENT OUT AND STOPPED FLICKERING ON DECENT. UNABLE TO DUPLICATE FAULT ON GRD. CHECKED WING AND PYLON DUCTS FOR AIRLEAKS, NONE FOUND. CHECKED WIRES AND SWITCHES FOR DAMAGE, NONE FOUND, PERFORM OPS CKS IAW MM 26-18-00 ALSO CHKD THERMAL ANT-ICE SYSTEM IAW MM 30-11-00. 2L74 4F4 F A20WE E20EA 20031006001372003100600137NM 2003 10 6 SWAA032031 120030910A57536546431279 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND LT OUTBD TE FORE FLAP DELAMINATED AT T/E. REMOVED AND REPLACED LT OUTBD T/E FORE FLAP PER MM. 2L72 4F RTA16WE 20030911001802003091100180NM 2003 9 11 DHL2003742012 120030726A2612 FIRE DETECTOR BOEING727 727225 1384077NM NR 4 WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01742DH 21290 NR 4 FIRE DETECTOR WON'T TEST. REMOVED AND REPLACED SMOKE DETECTOR IAW 26-17-0. OPS CHECKED GOOD. 2L73 4F A3WE 20030911002112003091100211NM 2003 9 11 QXEA200300961 120030809A2497 WIRE DHAV DHC8 DHC8202 2809007NM ELECTRICAL SYS CHAFED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09352PH 494 LWS- ON FLIGHT 2165 AFTER LANDING NR 2 AC GENERATOR CAUTION LIGHT CAME ON. RAN CHECKLIST ON GROUND AND TURNED NR 2 AC GENERATOR OFF AND THEN BACK ON. THERE WAS NO CHANGE. INSPECTED WIRING IN NR 2 AC GENERATOR BOX AND FOUND CB 2421 CB4 POPPED AND A CHAFED WIRE. REPAIRED WIRE IAW AMM 20-45-07. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030910000952003091000095NM 2003 9 10 03FDEA01187 120030725A5710ARC050214 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. RT WING O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69405 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030910000972003091000097NM 2003 9 10 MWEA030353 120030902A532059124921 PAN DOUG MD88 MD88 3023688NM FUSELAGE GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FORWARD GALLEY SERVICE DOOR PAN GOUGED IN BOTTOM SECTION OF PAN. FABRICATED AND INSTALLED NEW PAN SECTION AND ANGLE. 2L72 4F RTA6WE 20030910001452003091000145NM 2003 9 10 MWEA030337 120030827A534759305661 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 AFT CABIN NR 2 SEAT TRACK HAS CORROSION AT VARIOUS LOCATIONS FROM STATION 1250-1309. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2L72 4F RTA6WE 20030910001522003091000152EU 2003 9 10 SIMA200322501 120030809A2121EVCTA465A FAN SAAB SF340 340B 7860101EU CABIN FAILED A SIMAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW21380AE 340B380 ACT - FLT 3263 - AFTER LANDING WITH AIRCRAFT PARKED AT GATE CREW RECEIVED A RECIRC LIGHT WITH AN ELECTRICAL SMELL AND SMOKE. FIRE DEPARTMENT WAS CALLED BUT NO EVIDENCE OF FIRE WAS FOUND. MAINTENANCE FOUND THE RIGHT RECIRCULATION FAN TO BE THE CAUSE. RECIRC FAN WAS PUT ON MEL. MAINTENANCE REMOVED AND REPLACED THE RIGHT RECIRCULATION FAN IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030910001962003091000196WP 2003 9 10 MEX2003384 120030822A3610 CLAMP DOUG DC9 DC982 3022082WP BLEED AIR SYS DEFECTIVE A ASMFO OTHER J WARNING INDICATION CLCLIMB 1 SW23501AM 49188 FLT 266 - MEX-REX - AIRCRAFT ARRIVED WITH CAPTAIN REORTING THAT AFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON. THE AUGMENTATION VALVE AND REGULATOR VALVE DUCTS CLAMPS WERE REPLACED IAW MM 36-10-00 AND TEMPERATURE SENSORS WERE CLEANED IAW MM 36-20-02. DURING OVERNIGHT SERVICE, BOTH AIR CONDITIONING PACKAGES AND PNEUMATICK DUCTS WERE CHECKED FOR LEAKS IAW MM 21-00-00 AND MM 36-00-00, ALL CORRECT. (M) 2L72 4F A6WE 20030910002042003091000204EU 2003 9 10 MALA030383 120030817A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15407XJ 340B407 LT CENTER AISLE SEAT TRACK LBL 18.3 FEW SECTION HAS CORROSION OUT OF LIMITS. MAINTENANCE COMPLETED REPAIR IAW EO NR S53060 FROM STA 297 TO STA 349. REFER TO 409 NR 177361 FOR DETAIL. 2L72 4T RTA52EU 20030911000662003091100066WP 2003 9 11 DHL2003873553 120030629A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 INTERIM REPAIR ON RT HORIZONTAL STABILIZER INBOARD LE (STA.XFS.85.000-110.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17. CLEANED, TREATED AND PRIMED INNER SIDE OF DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-1 FIG 4 PG 17, SRM 51-1-15 PG 1, SRM 51-1-21 PG 1. REFER TO JC BX3H55072 FOR RT HORZ STAB LE REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20030911000752003091100075WP 2003 9 11 DHL2003873541 120030628A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL CRACKED (1.000), STA 640.000 LBL 11. REMOVED FASTENTERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENTERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F4 FRT4A25 E2GL 20030911001102003091100110NM 2003 9 11 CALA0300420 120030727A253072067002 OVEN BOEING757 757224 1384958NM F/C GALLEY INOPERATIVE A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2718119 27561 THE FIRST CLASS GALLEY OVEN #204 BEGAN TO PRODUCE AN ELECTRICAL ODOR WHILE IN ROUTE TO ANC. THE OVEN SHUTDOWN AUTOMATICALLY AND WOULD NOT RESET. THE FLIGHT CONTINUED TO ANC WITHOUT FURTHER INCIDENT. THE OVEN WAS PLACARDED INOPERATIVE. THE OVEN WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD. THE PLACARD WAS REMOVED. 2L72 4F RTA2NM 20030911001172003091100117WP 2003 9 11 DHL2003873537 120030627A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OB L/E FORMER CRACKED 0.250 AT XFS.772.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT XFS.772.000 IAW SRM 57-2-0 PG 9,10. FABRICATED DOUBLER ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON LT OB L/E FORMER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001192003091100119WP 2003 9 11 DHL2003873550 120030630A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 INTERIM REPAIR ON RT HORIZ STAB OB L/E AT XFS.180.000. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4, PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17. CLEANED, TREATED AND PRIMED DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED DOUBLER ON RT HORIZ STAB OB L/E AT XFS.180.000 IAW SRM 55-2-1 FIG 4 PG 17, SRM 51-1-15 PG 1, SRM 51-1-21 PG 1. FOR REMOVAL/REINSTALLATION OF L/E SEE JC BX3455072. 2L74 4F RT4A25 20030911001432003091100143CE 2003 9 11 DXTA200300091 120030815A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG FAILED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07330QS 5600329 COPILOT'S BRAKE FAILED ON TAXI, PILOT'S BRAKES PULSATING DURING SLOW TAXI. - PERFORMED BRAKE BLEED PROCEDURE IAW CE560 MM CHAPTER 32-42-01 LEAK CHECK GOOD. FUNCTIONAL TEST GOOD. 2L72 4F RTA22CE 20030911001542003091100154WP 2003 9 11 DHL2003873592 120030705A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT OUTER WING IB EXTENDED LE LOWER PLATING CRACKED 1.000, AROUND STA. XFS.597.500 PERFORMED MAJOR REPAIR IAW EODHL-030625, ED-3457. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030625, ED3457. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER AND A FILLER. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER ON LT OUTER WING EXTENDED LE LOWER PLATING SURFACE (AROUND STA XFS.597.500) USING NEW FASTENERS FOR LE REMOVAL/INSTALLATION. 2L74 4F RT4A25 20031008000202003100800020EU 2003 10 8 03258330 120030915A3350 SIGN JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY EXIT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 DURING MAINTENANCE INSPECTION, THE FOWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4T RTA41NM 20031008000232003100800023CE 2003 10 8 GLBA2003133 120030916A77121303890023 TRANSMITTER BEECH 1900 1900D 1154162CE ENGINE TORQUE MALFUNCTIONED A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03195GL3805 UE195 NR 1 ENG WILL NOT MAKE TAKE OFF POWER, R&R NR 1 TORQUE TRANSMITTER 2L72 4T RTA24CE 20031008000242003100800024NM 2003 10 8 HOC2003F00021 120030826A5330 SKIN BOEING727 727224 1384076NM FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0779749 22451 DURING A (C) CHECK, CORROSION WAS NOTED ON FUSELAGE BILDGE INTERIOR SKIN AND N/PS UNDER SUPPORT FRAME AT STA 660-680, LBL13.5. 2L73 4F A3WE 20031008000272003100800027EA 2003 10 8 COMA0360411 120030915A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01914CA 7012 FLIGHT 5530 FLAPS FAIL MESSAGE DURING TAXI. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031008000352003100800035EA 2003 10 8 QXEA200301129 120030913A7830 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 400 DIRTY A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09600QX 10005 ON FLIGHT 2452 ABORTED TAKEOFF DUE TO LEFT THRUST REVERSER UNSAFE CAUTION MESSAGE. CLEANED HYDRAULIC FLUID RESIDUE FROM NR 1 ICV CONNECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031008000542003100800054WP 2003 10 8 UPS03841157 120030825A5511 RIB DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, LEFT HORIZONTAL STAB. LE. RIB IS CRACKED AT XFS 47.5 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2 2L74 4F RT4A25 20031008000642003100800064NM 2003 10 8 USAA030199 120030815A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US47187 23237 FOUND STRINGER CRACKED .75 INCH ON 18A SHELF IN L/RL WHEEL WELL. REPAIRED PER EA 65576. (M) 2L72 4F RTA16WE 20031008000672003100800067EU 2003 10 8 SIMA200326502 120030910A55127255150522 SKIN SAAB SF340 340B 7860101EU RT HORIZ STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21903AE 340B282 AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT ON THE RIGHT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM (72LKS 3079, REV 41) 51-40-21, 22, 40, 51-20-40, 41, 43. (M) 2L72 4T RTA52EU 20031008000682003100800068WP 2003 10 8 AALA20030851 120030811A2450 CHAIN DOUG DC9 DC982 3022082WP ELEC OUTLET MISINSTALLED A AALAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21210AA 49161 EN ROUTE AUX OUTLET COVER IN AFT GALLEY ARCING. AIRCRAFT LANDED DFW WITHOUT INCIDENT. FOUND OUTLET COVER CHAIN MAKING CONTACT WITH OUTLET. CHAIN WAS DISLODGED FROM THE PRONGS ON THE UTILITY CAP. CHAIN WAS RETURNED TO ITS PROPERLY INSTALLED POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031009000042003100900004NM 2003 10 9 USAA030196 120030916A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US53110 22956 FOUND SKIN CRACKED 2.75 INCHES, LEFT FUSELAGE STATION 970 AT STRINGER 21L. INSTALLED DOUBLER SRM 53-00-01, FIG 202. (M) 2L72 4F RTA16WE 20031009000052003100900005NM 2003 10 9 USAA030197 120030731A5500 BALANCE ARM BOEING737 737401 1384701NM RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US40913 23987 FOUND RUDDER BALANCE ARM HAS HOLE 1.25 INCH BY .75 INCH, UPPER SURFACE. ROUTED OUT DAMAGE AND INSTALLED DOUBELR PER EA 76691. (M) 2L72 4F RTA16WE 20031009000062003100900006NM 2003 10 9 AALA20030799 120030725A2751215016001 INDICATOR BOEING767 767223 1385123NM COCKPIT FAULTY A AALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW21329AA 22329 UPON DEPARTURE FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FAULTY FLAP/SLAT INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031009000152003100900015NM 2003 10 9 USAASB03144 120030822A3260 WARNING LIGHT BOEING737 737301 1384611NM MLG ILLUMINATED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19590US 23935 AFTER DEPARTURE FROM MCI AND GEAR RETRACTION, CREW REPORTED VIA ACARS THAT THE NOSE GEAR RED LIGHT ILLUMINATED WITH THE MAIN GEAR INDICATION NORMAL. PER QUICK REF HANDBOOK PROCEDURES, CREW EXTENDED THE LANDING GEAR AND RECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS AND NO RED LIGHTS. FLIGHT RETURNED TO FIELD AT MCI AND LANDED WITHOUT FURTHER INCIDENT. (M) 2L72 4F RTA16WE 20031009000232003100900023SO 2003 10 9 SIMA200323001 120030813A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21625AE 145115 MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTING STRIP BETWEEN SEAT 12A AND 13A INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT ROW 12 AND 13. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031009000362003100900036SO 2003 10 9 SIMA200320801 120030724A3350MS277891A SWITCH EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21649PP 145234 CREW REPORTED AN EMERGENCY LIGHT NO ARMED MESSAGE ON EICAS WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031006001612003100600161 2003 10 6 SWAA031964 420030901A2565D31591478 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SERVICE CHECK, FWD SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20031006001762003100600176NM 2003 10 6 03FDEA01535 120030907A5510ALC81312 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 REFERENCE EO 1-5510-7-5000: HORIZONTAL STABILIZER LT UPPER END CAP NR 36L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION AFTER REWORK. HORIZONTAL STAB LT UPPER END CAP 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-73294 STABLIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 36 LEFT HAND SIDE. 2L73 4F RTA22WE 20031006001872003100600187NM 2003 10 6 03FDEA01677 120031001A532065453132 STRINGER CLIP BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CRACK IN STRINGER CLIP AT BS 950D, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950D, STRINGER 6 RT IAW SRM 51-30-2. 2L73 4F4 FRTA3WE E2EA 20031007000072003100700007WP 2003 10 7 GTIA030685 120030921A3240 CONNECTOR DOUG DC9 DC983 3022083WP LT MLG ASSY DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 BRAKES CAVITIATE ONLY AT SLOW SPEEDS. INSPECTED BRAKES, FOUND NR 1 BRAKE AFT CONNECTOR DISCONNECTED AND NR 2 BRAKE FWD CONNECTORS DISCONNECTED, RESECURED CONNECTORS. REMOVED AND REPLACED NR 1 BRAKE AFT CONNECTOR, LEAK CHECKS GOOD AT THIS TIME. (M) 2L72 4F RTA6WE 20031007000512003100700051NM 2003 10 7 AALA20030675 120030620A2120 ODOR BOEING757 757223 1384957NM CABIN DETECTED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21657AM 24615 FLIGHT ATTENDANT AT MID CABIN NOTICED AN ELECTRICAL ODOR AT 1,200 FT DECLARED EMERGENCY AND LANDED AT FJK. FLIGHT ATTENDANT REPORTED THAT THE ODOR WAS WORSE AT HIGHER POWER SETTING (CLIMB). RAN BOTH ENGINES WITH AND WITHOUT PACKS AT TAKEOFF POWER. NO ABNORMAL ODORS NOTED AIRCRAFT OK FOR SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000562003100700056NM 2003 10 7 03FDEA01671 120031001A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON LOWER FLANGE OF FLOORBEAM STA 720, WL 201, RBL 18. REMOVED 1 X 1 X .031 CORROSION ON LOWER FLANGE OF FLOORBEAM BS 720, WL 201, RBL 18. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED PER SRM 53-10-1, 53-10-8, 51-30-2, 51-10-2 2L73 4F4 FRTA3WE E2EA 20031007000702003100700070NM 2003 10 7 SWAA031944 120030830A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29727SW 27859 DURING SCHEDULED C3 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20031007000872003100700087NM 2003 10 7 SWAA031985 120030905A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031008000302003100800030NM 2003 10 8 HOC2003F00025 120030826A5313 STRINGER BOEING727 727224 1384076NM FUSELAGE CORRODED B HOCRK NONE O OTHER ININSP/MAINT 1 WP0779749 22451 DURING A C-CHECK, CORROSION WAS NOTED ON STRINGER 30 AT STA 1148-1166. 2L73 4F A3WE 20031008000312003100800031NM 2003 10 8 VNAA0309008 120030911A3150 WARNING SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07471PS 3007 THE CREW REPORTED A PUSHER FAIL CASS MESSAGE. MAINTENANCE CYCLED IAC C/B. OPERATIONAL CHECK WAS PERFORMED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 22-00-00 AND AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031008000382003100800038NM 2003 10 8 QXEA200301131 120030914A3397 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DISCONNECTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX- LEFT HAND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT IS INOPERATIVE. FOUND CONNECTOR AT LIGHT ASSEMBLY TO BE DISCONNECTED. RECONNECTED CANNON PLUG. NO PARTS REPLACED. 2H72 4T RTA13NM 20031008000462003100800046NM 2003 10 8 P5CA0300943 120030915A3260387 BULB BOEING747 747341 13848AMNM CAUTION PANEL SHORTED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23355MC 23395 ON PUSHBACK THE INDICATOR AND DIGITAL DISPLAY CIRCUIT BREAKER POPPED AND WOULD NOT RESET. REPEAT CAME BACK TO BLOCKS. FOUND SHORTED BULB ON CAPT'S CAUTION PANEL GEAR PER NOT CENTERED LIGHT, RELAMPED OPS CK GOOD PER 33-10-00 GROUND OPS GOOD PER 33-10-00. GROUND OPS BODY GEAR PER 32-60-00, NO FAULTS. 2L74 4F RTA20WE 20031008000472003100800047 2003 10 8 P5CA0300942 420030914A3197 WIRE BOEING747 747341 13848AMNM ELECTRICAL POWERGROUNDED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23355MC 23395 INDICATOR AND DIGITAL DISPLAY CIRCUIT BREAKER ON PG PANEL POPPED AND WOULD NOT RESET. PILOTS INDICATION LIGHTS WENT OUT. FOUND PWR WIRE GROUNDED TO CASE ON CAPT'S PNL CNTRL DIMMER SWITCH. REPOSITION WIRES AND OPERATION CK GOOD PER MM 33-11-11. 2L74 4F RTA20WE 20031008000492003100800049 2003 10 8 VNAA0309009 420030914A31407013348937 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT FAILED A VNAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07426JS5735 357 3038 THE CREW REPORTED A LT PUSHER FAIL CASS MESSAGE. AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED LT DATA ACQUISION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND AIRCRAFT WAS RELEASED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031008000522003100800052NM 2003 10 8 UPS03441234 120030905A5347BAC15201566 CARGO TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 554 RBL 46 TIE DOWN TRACK LT FLANGE CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.045 X 1 X 3 EXCEED SRM 53-10-01 FIG 1 LIMITS , FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 6. CIC APPLIED IAW EO M-5100-2780-E 2L74 4F A20WE 20030911001712003091100171WP 2003 9 11 DHL2003873613 120030706A532037739062 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT FITTING CRACKED 2.000 AT STA 702.000, RBL 23. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F4 FRT4A25 E2GL 20030911001912003091100191WP 2003 9 11 AALA20030341 120030310A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND MID CARGO DOOR BEAM CORRODED BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-01-00. (M) 2L72 4F A6WE 20030911001952003091100195WP 2003 9 11 AALA20030435 120030226A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW219615W 53562 MCI - FOUND FLOOR TRACK AT LBL 23, FS 1166 HAS CORROSION GALLEY NR 3. REMOVED DAMAGED CHAIR TRACK FROM STATION 1088-1220, AND INSTALLED NEW CHAIR TRACK AND SPLICE PER SRM 53-05-00. (M) 2L72 4F RTA6WE 20030911002042003091100204WP 2003 9 11 AALA20030339 120030311A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE BENT A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND FRAME IN FORWARD CARGO LOWER LEG BENT, SIDE OF FRAME DEFORMED AND RADIUS FROM DENT IN FUSELAGE. REMOVED AND REPLACED FRAME IN FWD CARGO PER SRM 51-10-04. (M) 2L72 4F A6WE 20030911002152003091100215NM 2003 9 11 DHL2003754016 120030809A3240 BRAKE BOEING727 727223 1384074NM RIGHT MALFUNCTIONED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01754DH 22008 BRAKES WERE LOCKED WHEN TRYING TO TAXI OUT OF CLT. RIGHT BRAKE ACTIVATED ON CONTROL CHECK WITH THE RUDDER PEDALS. UNABLE TO DUPLICATE ON GROUND. PERFORMED VISUAL CHECK OF ALL BRAKES, JACKED AND ROTATED ALL TIRES. NO DEFECTS NOTED IAW MM 32-41-00. 2L73 4F A3WE 20030911002162003091100216NM 2003 9 11 DHL2003784002 120030813A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE FAULTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01767AT 22001 NR 3 ENGINE FIRE DETECTOR CIRCUIT GRD ANNUNCIATOR ON P6-3 ILLUMINATED AFTER TO FROM KDAL DEFERED IAW DHL MIL 26-9, CONTROL NR 13813, PLACARD INSTALLED, BY 35840 REF DMI NR 13813 (NR 3 ENGINE FIRE DTECTOR CIRCUIT GRD ANNUNCIATOR ON P6 -3 ILLUMINATED) REMOVED AND REPLACED FIRE LOOP ON NR 3 ENGINE IAW B-MM 26-11-2 OP'S GOOD IAW B-MM 26- 11-01. THIS CLEARS DMI NR 13813 PLACARDS REMOVED. 2L73 4F A3WE 20030911002202003091100220EU 2003 9 11 DHL2003368008 120030815A3241 BRAKE AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAO OTHER O OTHER APAPPROACH 1 SO01368DH 207 AUTO BRAKES WOULD NOT ENGAGE ON APPROACH. DEFERRED AUTO BRAKES IAW MEL 32-42-07. ASSIGNED CONTROL NR 13838. PLACARD INSTALLED. REF CI 13838 AUTOBRAKES WOULD NOT ENGAGE ON APPROACH. PERFORMED OPS CHECK OF AUTOBRAKE SYS IAW 32-42-00. SYS CKS OK. DMI 13838 CLEARED. 2L72 4F RTA35EU 20030911002252003091100225NM 2003 9 11 DHL2003745017 120030820A3260 WARNING SWITCH BOEING727 727224 1384076NM RT MLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER DEPARTURE RIGHT GEAR DOOR LIGHT AND DOOR LIGHT ILLUMINATED, PERFORMED ABNORMAL PROCEDURE AND LIGHT EXTINGUISHED WITH GEAR HANDLE IN THE UP POSITION. ADJUSTED RIGHT MAIN LANDING GEAR WARNING SWITCH (DOOR), OPS CHECKED NORMAL IAW M/M 32-12-0, 32-62-11, AND 32-32-0. REMOVED AND STORED GEAR PINS (3EA) IAW M/M 32-00-11. 2L73 4F A3WE 20030911002312003091100231WP 2003 9 11 DHL2003604581 120030522A5321 FLOOR PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT, CORROSION ON FLOOR PANEL SKIN STA 1160.000 TRACK NR 6. REMOVED CORROSION IAW SRM 51-1-8 PG 17,18 FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED DOUBLER IAW SRM 53-2-3 FIG 10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911002342003091100234WP 2003 9 11 DHL2003604609 120030603A53205711283501N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT CARGO COMPT CLIP RETAINER FITTING CORRODED, STA 1380.000 - STA.1400.000 LBL 8. REMOVED CORRODED FITTING IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON AFT CARGO COMPT CLIP RETAINER FITTING STA 1380.000 - STA.1400.000, LBL 8 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-21 PG 2. 2L74 4F RT4A25 20030911002382003091100238WP 2003 9 11 DHL2003604528 120030502A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING INDB L/E INTERNAL DOUBLER CRACKED .500, STA XFS.572.500. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 & SRM 57-3-3 FIG 6. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED INTERNAL DOUBLER IAW SRM 57-3-3 FIG 6. FABRICATED NEW INTERNAL DOUBLER, A SHIM IAW SRM 57-3-3 FIG 6. CLEANED, TREATED AND PRIMED INTERNAL DOUBLER AND SHIM INNER SURFACE IAW SRM 51-1-8B. INSTALLED INTERNAL DOUBLER AND SHIM WITH NEW FASTENERS IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 6 & SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911002412003091100241WP 2003 9 11 DHL2003604607 120030609A57535652287505 SKIN DOUG DC8 DC873F 302199FWP FLAP VANE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING NR 1 VANE FLAP INTERNAL SKIN DELAMIATED. REMOVED AND REPLACED NR 1 VANE FLAP ON LT WING IAW MM 27-51-14 PG 201, 202. FOR OPS CHECK SEE N/R. 2L74 4F RT4A25 20030911002442003091100244WP 2003 9 11 DHL2003604577 120030506A5755 SKIN DOUG DC8 DC873F 302199FWP RT SPOILER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING NR 4 SPOILER EXTERNAL SKIN DELAMINATED. CUT OUT DAMAGED AREA IAW SRM 57-2-3 PG 14 PARAGRAPH 6B. FABRICATED PLUG AND DOUBLER IAW SRM 51-1-9 PG 4 PARAGRAPH 4. CLEANED IAW SRM 51-1-9 PG 1, PARAGRAPH 1. BONDED AND CURED IAW SRM 51-1-9 PG 2, PARAGRAPH 2. FOR REMOVAL AND INSTALLATION SEE N/R 2642. 2L74 4F RT4A25 20030912000402003091200040WP 2003 9 12 DHL2003604715 120030606A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 UPPER FUSELAGE EXTERIOR SKIN WITH 0.750 CRACK AT STA 1751.000 BETWEEN L-14L AND L-17L. PERFORMED MAJOR REPAIR IAW EODHL-030546, ED-3298. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW EODHL-030546, ED-3298. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED 2 EA FILLERS AND DOUBLER IAW EODHL-030546, ED-3298. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLERS AND DOUBLER WITH NEW FASTENERS IAW EODHL-030546, ED-3298, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000582003091200058WP 2003 9 12 DHL2003604600 120030611A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT RUDDER INTERNAL SKIN CORRODED, STA ZR 150.000 - ZR 178.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED DAMAGED SKIN PANEL IAW EODHL-030533, ED-3354. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL IAW EODHL-030533, ED-3354. CLEANED, TREATED AND PRIMED NEW SKIN PANEL IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON LT RUDDER INTERNAL SURFACE STA ZR 150.000 TO ZR 178.000 WITH NEW FASTENERS IAW EODHL-030533, ED-3354, SRM 51-1-21 PG 1. SEE N/R 4051 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20030912000642003091200064WP 2003 9 12 DHL2003604706 120030527A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING OTBD L/E SHOWS CORROSION AT STA XW 761.000. REMOVED FASTENERS, REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT THE DAMAGED SKIN AREA IAW EODHL-030547, ED-3313. PERFORMED NDT INSPECTION, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER, A FILLER IAW EODHL-030547, ED-3313. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLER ON LT OUTER WING OTBD L/E (STA XW 761.000) USING NEW FASTENERS IAW EODHL-030547, ED-3313, SRM 51-1-21 PG 1-2. 2L74 4F RT4A25 20031008000572003100800057WP 2003 10 8 UPS03841229 120030914A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE:N/A EMERGENCY LIGHTING SWITCH LEFT IN ARMED POS. BATTERY PACK DEAD. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK. NOW OPS OK. 2L74 4F RT4A25 20031008000582003100800058WP 2003 10 8 UPS03841230 120030915A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CK GOOD IAW MM CH 33. 2L74 4F RT4A25 20031008000622003100800062NM 2003 10 8 USAA030200 120030806A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US 23237 FOUND STRINGER CRACKED .75 INCH, ON 18A SHELF IN R/RL WHEEL WELL. REPAIRED PER EA 65576. (M) 2L72 4F RTA16WE 20031009000012003100900001NM 2003 10 9 AALA20030689 120030530A5320 PLATE BOEING767 767223 1385123NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21324AA 22325 DURING REMOVAL OF H-11 BOLTS THROUGHT THE SPLICE PLATE PER SB 767-57A0046, TWO HOLES WERE FOUND CORRODED AND REQUIRED OVERSIZING THE HOLES WERE COMMON TO THE HORIZONTAL FLANGES OF THE CENTER WING SPAR CHORD AND THE OUTBOARD WING SPAR CHORD. REMOVED HOLE BORE CORROSION DAMAGE BY REAMING THE OUTBOARD HOLE TO THE SECOND OVERSIZE AND THE INBOARD HOLE TO THE NEXT FULL DIAMETER.875 INCH. HFEC INSPECTION BOTH HOLES TO ENSURE A CORROSION AND CRACK FREE CONDITION. REFINISH RE-WORKED AREA PER SRM AND INSTALL A BACB300S14RK .875 INCH AND BACB3OUS12KY, 2ND OVERSIZE .75 INCH BOLTS IN THE APPLICABLE HOLE INSTEAD OF THE NOMINAL BACB3OUS12K .75 INCH BOLTS SEAL THE FASTENERS PER SB 767-57A0046. (M) 2L72 4F RTA1NM 20031009000352003100900035SO 2003 10 9 SIMA200320811 120030727A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21642AE 145193 DURING PRE-FLIGHT, THE CREW NOTED EMERGENCY EXIT LIGHTS AT ROW 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AC/DC INVERTER IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031009000372003100900037SO 2003 10 9 SIMA200326507 120030916A531514525381003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21610AE 145073 DURING AN MBV INSPECTION, THE CENTER FLOORBEAM FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED CORROSION BY BLENDING. FABRICATED A REINFORCEMENT PLATE FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3007 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031009000392003100900039EU 2003 10 9 SIMA200325308 120030909A2910HP14081004 VALVE SAAB SF340 340B 7860101EU HYD BAY INOPERATIVE A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21370AM 340B370 DURING TAKEOFF AT ABOUT 110 KNOTS THE AIRCRAFT VEERED HARD TO THE LEFT. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETUREND TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE POWER BRAKE CONTROL VALVE IAW SAAB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20031014000672003101400067NM 2003 10 14 SWAA032207 120031004A5320BAC1503 STIFFENER BOEING737 7373Y0 1384671NM LT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED RON, FOUND VERTICAL STIFFENER CRACKED AT LT W/W FWD BULKHEAD, BS 663 AND LBL 6.15. REPAIRED VERTICAL STIFFENER PER SWA EA. 2L72 4F RTA16WE 20031014000992003101400099 2003 10 14 SWAA032144 420030923A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031014001012003101400101NM 2003 10 14 SWAA032142 120030924A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 823, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001052003101400105NM 2003 10 14 SWAA032138 120030920A53126546568 BULKHEAD BOEING737 7377H4 1384404NM FUSELAGE CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29725SW 27857 DURING SCHEDULED C4 CHECK, FOUND AFT PRESS BULKHEAD OIL CANNED AT BS 1016, STR 1L. REPAIRED BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20031014001202003101400120NM 2003 10 14 SWAA032172 120030928A53406557463 ATTACH FITTING BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE BOTH FWD AND AFT GIRT BAR ATTACHMENT FITTINGS LOOSE. SECURED ATTACHMENT FITTINGS PER SRM. 2L72 4F RTA16WE 20031014001262003101400126NM 2003 10 14 SWAA032166 120030927A2560PH22300L STRIP BOEING737 7373H4 1384600NM AFT CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DAMAGED LT AFT CABIN. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20031014001282003101400128NM 2003 10 14 SWAA032164 120030927A2910A5118G0194CTR LINE BOEING737 7373TO 138447GNM NR 1 PYLON CRACKED A SWAAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW29697SW 23838 DECLARED EMERGENCY, ENGINE NR 1 'A' HYD LOW PRESS LIGHT ILLUMINATED AND PUMP WAS TURNED OFF. FOUND 'A' SYSTEM PRESS LINE IN PYLON CRACKED. REMOVED AND REPLACED HYD LINE PER MM. 2L72 4F RTA16WE 20031014001302003101400130NM 2003 10 14 SWAA032162 120030927A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 792, LBL 8. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20031014000232003101400023CE 2003 10 14 N382003F00002 120030825A2612 WARNING LIGHT LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP LT ENG FIRE FALSE ACTIVATIONE N38AO OTHER N FALSE WARNING NRNOT REPORTED 1 EA05630SJ 344 LT ENGINE FIRE LIGHT CAME ON FOR A FEW SECONDS. AFTER REDUCTION OF POWER, LIGHT EXTINGUISHED. NO OTHER INDICATIONS OF A FIRE. INSPECTED FIRE HARNESS LOOPS WITH NO DEFECTS NOTED. COMPLIED WITH FIRE LOOP RESISTANCE CHECKS IAW MFG MM AND FOUND WITHIN LIMITS. FIRE LOOP TEST, OK. AIRCRAFT GROUND RUN AND COULD NOT DUPLICATE. REPLACED HP SECTION OF MOD VALVE CRUSH GASKET DUE TO MINOR AIR LEAK. THIS WAS NOT BELIEVED TO CAUSE THE PROBLEM. 2L72 4F4 F A10CE E6WE 20031014000242003101400024CE 2003 10 14 E812003F00000 120030902A3510174060 OXYGEN MASK BEECH 200 200BEECH 1152920CE PWA PT6 PT6* 52043EA COCKPIT WRONG PART E E81RK NONE W INADEQUATE Q C ININSP/MAINT 1 GL03355TW BB521 DURING SCHEDULED PHASE CHECK, NOTED NON-STANDARD CREW OXYGEN MASKS INSTALLED. PN PILOTS MASK DID NOT SHOW ON EQUIPMENT LIST OR BE 200 IPC. CONTACTED MFG TECH SUPPORT, INSTALLED MASK ASSY NOT LISTED AS A VALID CROSS REFERENCE FOR APPROVED MASK ASSY. NO TSO MARKINGS NOTED ON MASK ASSEMBLY. NO VERIFIABLE RECORDS TO INDICATE WHEN INSTALLED IN AIRCRAFT OR SUPPORTING DOCUMENTATION. TECH AND REPAIR STATIONS NEED TO VERIFY INSTALLED OXYGEN MASKS ARE VALID FOR THAT AIRCRAFT, AS WELL AS IN SERVICEABLE CONDITION. OPERATORS ASSUME ONE MASK IS THE SAME AS ANOTHER, WHEN FLOW RATES, AIRFRAME COMPATABILITY, MAY RENDER IT UNSUITABLE FOR THAT INSTALLATION. REPLACED MASK ASSEMBLY. 1L72 4T3 T A24CE E2NE 20031014000612003101400061NM 2003 10 14 SWAA032191 120031002A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4 D CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031014000652003101400065NM 2003 10 14 SWAA032187 120031001A52306547952 SKIN BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT UPPER AFT CORNER. REPAIRED DOOR SKIN PER SWA EA. 2L72 4F RTA16WE 20031014000772003101400077NM 2003 10 14 SWAA032197 120031003A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 2550 27929 DURING SCHEDULED SERVICE CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON OUTBD END. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20031014000942003101400094NM 2003 10 14 SWAA032149 120030924A27816544651 ACTUATOR BOEING737 7377H4 1384404NM LT/RT WING L/E FAULTY A SWAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29783SW 29809 T/E FLAPS WOULD NOT RETRACT ON T/O AND NR 6 L/E SLAT STUCK. REMOVED AND REPLACED ALL L/E SLAT ACTUATORS PER MM. 2L72 4F RTA16WE 20031014000972003101400097NM 2003 10 14 SWAA032146 120030924A53116546529 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BS 460, ABOVE STR 14L AND BS 400 BETWEEN STR 14R AND STR 13R. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20031014001082003101400108NM 2003 10 14 SWAA032135 120030923A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 847 AT STR 16L AND BS 945 AT STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001322003101400132NM 2003 10 14 SWAA032160 120030925A3350100885 BATTERY BOEING737 7372H4 138448CNM FWD CABIN WEAK A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED C1 CHECK, FOUND EEPLS DIM IN FWD CABIN. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2L72 4F A16WE 20031014001782003101400178NM 2003 10 14 SWAA032100 120030921A26126566207 FIRE DETECTOR BOEING737 7373H4 1384600NM APU FALSE INDICATIONA SWAAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SW29331SW 23695 DECLARED EMERGENCY, APU FIRE WARN LIGHT INDICATION. FIRE EXTINGUISHER BOTTLE DISCHARGED. C/W APU COMPT INSPECTION, NO EVIDENCE OF FIRE. REMOVED AND REPLACED APU TAILPIPE FIRE DETECTOR AND HARNESS. OPS CK GOOD PER MM. 2L72 4F RTA16WE 20031014001812003101400181 2003 10 14 SWAA032097 420030919A256565C16820 CLIP BOEING737 7377H4 1384404NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR CLIP ATTACH RIVET SHEARED. REPAIRED GIRT BAR CLIP PER SRM. 2L72 4F RTA16WE 20031014001822003101400182NM 2003 10 14 SWAA032096 120030919A53156545410 FLOORBEAM BOEING737 7373A4 1384585NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED 1/4D CHECK, FOUND CENTER FLOORBEAM CRACKED AT BS 663.75, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20031014001842003101400184NM 2003 10 14 SWAA032094 120030919A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C3 CHECK, FOUND .5 INCH LONG CRACK AT FUSELAGE SKIN, LOWER FWD CORNER OF AFT ENTRY DOOR CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001992003101400199EU 2003 10 14 BAQA089651 120031008A56101172429702 WINDOW BOLKMS117 BK117A1 5626010EU COCKPIT CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME6375 7243 RT SLIDING WINDOW HANDLE CRACKED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031014002112003101400211CE 2003 10 14 BAQA089689 120031009A78301266021 ACTUATOR LEAR 35 35A 5170602CE THRUST REVERSER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0330DK 345 ACTUATOR INOPERATIVE. WOULD NOT OPERATE THRUST REVERSERS IN OR OUT. REPLACED WITH SERVICEABLE UNIT. 2L72 4F A10CE 20031014001952003101400195NM 2003 10 14 SWAA032102 120030920A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG AT BS 894, STRINGER 25R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031014002042003101400204EU 2003 10 14 BAQA089616 120031008A2913704A34310019 PUMP AEROSPAS365 AS365N2 8680815EU HYD SYSTEM MAKING METAL B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME7126 6417 HYDRAULIC PUMP MAKING METAL. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20031015000032003101500003WP 2003 10 15 DHL2003802014 120031006A2697 CONNECTOR DOUG DC8 DC873 302199CWP FIRE LOOP SHORTED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01802DH 46076 NR 2 ENGINE SHORT CIRCUIT (FIRE LOOP "A") DETECTION CAME ON INTERMITTENTLY, ONCE SHORTLY AFTER TAKE-OFF, ONCE AT 3 HOURS. TRANSFERRED TO DMI LOG IAW MEL. PLACARD INSTALLED. NR 2 ENGINE SHORT CIRCUIT FIRE LOOP "A" DETECTION COME ON. INSPECTED NR 2 ENGINE FIRE LOOP AND PERFORMED ADJ./TEST OF NR 2 ENGINE FIRE LOOP PER MM. NO DEFECTS NOTED. DMI REMAINS OPEN FOR FURTHER TROUBLESHOOTING DUE TO HISTORY. TROUBLESHOT, FOUND FIREWALL FEED THRU CONNECTOR IN ENGINE SECTION DIRTY. CLEANED & TESTED SYSTEM PER MM. NO HELP. CONTINUED TROUBLESHOOTING, WITH LOOP "A" DISCONNECTED IN FAN COWL & CORE SECTION. FOUND SHORT BETWEEN PINS 1 & 3, AND 2 & 3 ON AIRCRAFT SIDE, 2L74 4F RT4A25 20031015000162003101500016 2003 10 15 USAASA03100 420030830A2565C37103103 RELEASE CABLE AIRBUSA319 A319112 3930323EU GIRT BAR WRONG PART A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19756US 1340 THE AFT RIGHT EMERGENCY ESCAPE SLIDE WAS FOND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20031015000172003101500017NM 2003 10 15 DHL2003749516 120030920A5720 STIFFENER BOEING727 727200 138407ENM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C CHECK, DISCREPANCY AS FOLLOWS N/R 64533 W.B.L. 70 LT. WING LE VERT. STIFFENER BOTTOM END CRACKED. REMOVED LEFT LT WING PANEL. REMOVED FASTENER FOR ACCESS BOTTOM SIDE OF VERTICAL STIFFENER. STOP DRILL CRACK BOTTOM END OF VERTICAL STIFFENER. ACCOMPLISHED N.D.T. MARKED END OF CRACK PER N.D.T. NDT ACCOMPLISHED AROUND STOP HOLE NO CRACK BEYOND STOP HOLE IAW PART T6-51-00 FIG. 4. 6) FABRICATED ANGLE REPAIR NDT USED 7075 T6 .063 P.O.NR 9912495 DIM. 5.5 INCH X 2.5 INCH IAW B-727 SRM 51-40-3 FIG 1. ALODINED AND PRIMED I.A.W. B727 SRM 51-10-2. 8) INSTALLED ANGLE REPAIR I.A.W. B-727 SRM 51-30-2. LEAK CHECK GOOD IAW B-727 M.M. 28-11-0. 2L73 4F RTA3WE 20031015000252003101500025EA 2003 10 15 ASOA03414 120030904A3350BF50390901 COVER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11875AS 7559 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN COVER AT ROW 11 A/B WAS FOUND MISSING. MAINTENANCE LOCATED THE MISSING EMERGENCY EXIT SIGN COVER AND RE-INSTALLED IT AT ROW 11 A/B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000272003101500027EA 2003 10 15 ASOA03435 120030912A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP LEADING FROM THE CLOSET TO THE MAIN DOOR AREA OPERATED INTERMITTENTLY. MAINTENANCE CLEANED THE CONNECTORS TO THE EMERGENCY FLOOR LIGHT STRIP LEADING FROM THE CLOSET TO THE GALLEY AREA. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000452003101500045WP 2003 10 15 MEX2003442 120030922A215020495054 COOLING TURBINE DOUG DC9 DC982 3022082WP LEFT FAILED A ASMFBA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23505MD 49149 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, AT FL290 LIGHT FLOW CAME ON AND THE CABIN PRESSURE STARTED TO CLIMB OF 1500 FT/MIN, UNABLE TO CONTROL IT IN MANUAL AND AT 9500 FEET CABIN LIGHT CAME ON AND EMERGENCY DESCENT WAS DONE, PROCEEDING TO LANDING AT DCO. AT DGO, THE TURBINE ASSEMBLY COOLING AND PRESSURIZATION VALVE OF LEFT AIR CONDITIONING PACKAGE WERE REPLACED IAW MM 21-51-01 AND 36-10-08 RESPECTIVELY. DURING OVERNIGHT SERVICE PRESSURIZATINO AND ANTI-ICE SYSTEM WERE TESTED IAW MM 21-32-00 AND 30-10-00, ALL CORRECT. (M) 2L72 4F A6WE 20031015000682003101500068NM 2003 10 15 USAASB03140 120030820A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU 23856 MAINTENANCE REPORTED THE FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A WEAK EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031020000962003102000096SO 2003 10 20 C2XA03SH368 120031003A711014576599003 STRUCTURE EMB 145 EMB145 3260210SO RT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 SHV- DURING C-CHECK THE RIGHT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031020001162003102000116NE 2003 10 20 COMA0360446 220031002A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAA UNSCHED LANDING EY VIBRATION/BUFFET ENGINE STOPPAGE CRCRUISE 1 SO01805CA9252 7354 807599 FLIGHT 5685 LEFT ENGINE VIBRATION FOLLOWED BY ENGINE FAILURE. REPLACED ENGINE. 2L72 4F4 FRTA21EA E15NE 20031020001292003102000129SO 2003 10 20 RAIA00309252 120030913A49204501968D APU EMB 145 EMB145 3260210SO APU BAY MALFUNCTIONED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03804HK9663 2085 145082 5283-PIT- SMOKE IN CABIN. MAINTENANCE PLACED APU ON DEFERRAL PER MEL. SUBSEQUENTLY CLEARING THE DMI BY REMOVING AND REPLACING THE APU. 2L72 4F RTT00011AT 20031020001402003102000140EU 2003 10 20 MALA030440 120030926A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU NR 3 ENGINE FAILED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15513XJ E2329 DURING FLIGHT 3626, GREEN HYDRAULIC TEMP ILLUMINATED INFLIGHT, FOLLOWED QRH AND LIGHT EXTINGUISHED. DECLARED AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED NR 3 EDP P/N 521449, S/N ON F9818779, S/N OFF F9932847 AMM 29-10-17. OPS AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20031020001482003102000148NM 2003 10 20 DLM88030798 120030830A33506011773 POWER SUPPLY DOUG MD88 MD88 3023688NM CARGO BAY DEFECTIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27909DE 53418 FLOOR LEVEL EMERGENCY EXIT LIGHTS WILL NOT COME ON WHEN SELECTED FROM THE COCKPIT. OPS NORMAL FROM FLIGHT ATTENDANT PANEL. FOUND VOLTAGE BEING INDUCED ON TB 53-18 BLOCK 2. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY. SYSTEM OPS NORMAL. 2L72 4F RTA6WE 20031014001552003101400155 2003 10 14 SWAA032072 420030916A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031014001582003101400158 2003 10 14 SWAA032069 420030916A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031014002032003101400203 2003 10 14 BAQA089760 420031009A2210L673M20A1005 ACTUATOR UROCOPEC135 EC135T1 5620026EU MAIN ROTOR WILL NOT TEST B BAQAK NONE L NO TEST NRNOT REPORTED 1 EA03554ME2073 0154 WOULD NOT TEST AUTOPILOT. THIS UNIT CAUSED A FAILURE IN THE PREFLIGHT TEST OF THE AUTOPILOT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031015000232003101500023EA 2003 10 15 ASOA03432 120030910A541422850081141 PANEL CNDAIRCL600 CL6002B19 1900309EA LT NACELLE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11862AS 7476 DURING A GROUND INSPECTION IN DFW, THE LT ENGINE COWL ON THE UNDERSIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT NOSE COWL PANEL ON THE LEFT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031020000972003102000097EU 2003 10 20 AWXA200301122 120031002A25304110001147 COFFEEMAKER AIRBUS320 A320231 3930325EU GALLEY MALFUNCTIONED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28645AW8949 6479 238 EN ROUTE, REPORTED STRONG ELECTRICAL BURNING ODOR IN CABIN & COCKPIT. MX INSPECTED WIRING IN MAIN FWD GALLEY AREA BEHIND C/B PANEL, NR 1 & 2 OVENS, COFFEEMAKERS, NO SIGNS OF CHAFING OR BURNING. FOUND BURNT FOOD IN OVENS, DISCOVERED NR 1 COFFEEMAKER BASE UNIT HAD SOME BURNT PINS. MX REMOVED & REPLACED NR 1 & 2 OVENS, NR 1 & 2 COFFEEMAKERS, AND REPLACED NR 1 COFFEEMAKER BASE UNIT. OPS CHECKS GOOD. TEARDOWN REPORT OF COFFEE MAKER COULD NOT VERIFY REASON FOR REMOVAL. VENDOR REPLACED BOTH UPPER AND LOWER SPRINGS, FLOAT TIP, WATER LEVEL SENSOR, PROBE, RELAY, AND LOWER PC BOARD PER CMM 25-30-09, REV. 5. 2L72 4F RTA28NM 20031020001012003102000101WP 2003 10 20 ABXA030376 120030917A532049125151 CAP DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 CRACK IN LONGERON 16 LEFT END CAP AT FS 994. REPLACED END CAP IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20031020001552003102000155NM 2003 10 20 DL733030784 120030826A3260189929 SENSOR BOEING737 737347 1384647NM RT MLG WW OUT OF TOLERANCEA DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27305WA 23346 AFTER TAKEOFF GEAR WOULD NOT RETRACT NORMALLY, HAD TO USE OVERRIDE TO RAISE HANDLE. ONCE GEAR WAS UP AND FLAPS WERE RETRACTED TAKEOFF WARNING HORN SOUNDED UNTIL FLAPS WERE LOWERED AGAIN. AIRCRAFT RETURNED TO SFO. SFO LINE MTC T/S TAKEOFF WARNING SYSTEM, FOUND MAIN LANDING GEAR SAFETY SENSOR S106 BAD. REPLACED SAME, TAKEOFF WARNING SYSTEM NOW CHECKS OK. 2L72 4F RTA16WE 20031020001732003102000173NM 2003 10 20 DLM88030809 120030820A3260387 LIGHT DOUG MD88 MD88 3023688NM COCKPIT INOPERATIVE A DALAO OTHER N FALSE WARNING DEDESCENT 1 SO27976DL 53257 RIGHT MAIN GEAR BULB BURNT OUT. RELAMPED RIGHT MAIN GEAR BULBS PER MM, CHECKS OK. 2L72 4F RTA6WE 20031020001892003102000189 2003 10 20 DL73S030815 420030905A3417HG480B42 ADC BOEING737 737247 138448DNM E/E BAY FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27375DL 23602 AFTER LIFTOFF F/O ALT AND AIRSPEED FAILED. CONTACTED ATL MTC RTN TO CVG. REPLACED NR 2 DADC. 2L72 4F A16WE 20031020002092003102000209WP 2003 10 20 0301889921 120031003A215020495055 ACM DOUG DC9 DC932 3022066WP A/C BAY FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01943N 47647 SHORTLY AFTER TAKEOFF, THE RIGHT AIR CONDITIONING PACK AIR FLOW STOPPED. THE LEAD FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO BIL AND MADE AN EMERGENCY OVERWEIGHT LANDING WITHOUT ANY FURTHER INCIDENT. NO COMMENTS ABOUT COM OR ATTEMPTED CORRECTIVE ACTIONS OR IF SMOKE HAD CLEARED PRIOR TO LANDING. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE, ANTI-ICE VALVE, AND BOTH WATER SEPARATOR BAGS. ACCOMPLISHED BURN OUT PROCEDURES. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20031020002222003102000222NM 2003 10 20 UPS03241337 120030924A5330 SKIN BOEING727 72751C 1384015NM FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 INSPECTION TYPE:SP LT FUSELAGE SKIN JUST AFT OF MAIN CARGO DOOR AT SKIN LAP HAS A LIGHTNING STRIKE AT STA 620 BETWEEN STRINGER 13L AND 14L. BLENDED OUT LIGHTNING STRIKE AREA FOUND CRACKED. CUT OUT DAMAGE, NDT CUTOUT AREA NO CRACKS NOTED AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW UPS EO B727-5330-19302-A AND SAA SK 903-275. 2L73 4F A3WE 20031020002462003102000246NM 2003 10 20 DL75K030825 120030908A3350 CONNECTOR BOEING757 757232 1384965NM CABIN LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27695DA 29727 RED EMERGENCY LIGHT ON LAV FWD OF SEAT ROW 9 INOP. SECURED CONNECTION. 2L72 4F RTA2NM 20031020002672003102000267EU 2003 10 20 03264303 120030921A3350 CONTACTOR JETAIRJETSTMJETSTM4101 1500501EU LIGHT ASSY DIRTY A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27303UE 41015 DURING INSPECTION THE FORWARD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE CONTACTS ON THE LIGHT ASSEMBLIES. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031020002702003102000270EA 2003 10 20 03257639 120030914A55206002113443 PANEL CNDAIRCL600 CL6002B19 1900309EA ELEVATOR DAMAGED A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27639BR 7313 DURING GROUND OPERATION CREW REPORTED BINDING IN ELEVATOR CONTROL. MAINTENANCE PERSONNEL DETERMINED BINDING TO BE CAUSED BY DAMAGED ELEVATOR VISOR. VISOR WAS REMOVED AND REPLACED. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002742003102000274EU 2003 10 20 03263327 120030920A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN MALFUNCTIONED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27327UE 41080 DURING INSPECTION THE EMERGENCY LIGHT NEAR THE PAX DOOR WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK AND FOUND NO DEFECTS WITH THE EMERGENCY LIGHTING SYSTEM. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031020002842003102000284NM 2003 10 20 VNAA0309010 120030917A3240AC69965 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PARK BRAKE FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07422JS10698458 3018 THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARK BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030912000672003091200067WP 2003 9 12 DHL2003604743 120030515A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LWR FUSELAGE SKIN WITH TWO DENTS BETWEEN STA 25.000 AND 45.000, L-24L - L-25L. PERFORMED MAJOR REPAIR IAW EODHL-030513, ED-3285. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. BLENDED OUT DAMAGED AREA IAW EODHL-030513, ED-3285. PERFORMED EDDY CURRENT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED (4) FINGER DOUBLERS AND DOUBLER IAW EODHL-030513, ED-3285. CLEANED, TREATED AND PRIMED AREA AND FINGER DOUBLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FINGER DOUBLERS AND DOUBLER WITH NEW FASTENERS IAW EODHL-030513, ED-3285, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000822003091200082NM 2003 9 12 AWXA200300819 120030709A5320D5323022620000 PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MINOR REPAIR - DURING C-04 CHECK .25 INCH CRACK WAS FOUND ON CLOSING PLATE AT LT SIDE PANEL BS 1323, FR 34, STR 32 LT. MAINTENANCE REMOVED AND REPLACED CLOSING PLATE AT LT SIDE PANEL BS 1323, FR 34, STR 32 LT IAW A319 SRM 51-42-11, PG 28-32, FIG 12 AND 13. 2L72 4F RTA28NM 20030912000862003091200086NM 2003 9 12 AWXA200300834 120030706A5320D53476461000 PROFILE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT PROFILE BETWEEN FR 59-62, RBL 711.2. MAINTENANCE REMOVED CORRODED PROFILE BETWEEN FR 59-62, RBL 711.2; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND REPAIR SPLICE; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1. 2L72 4F RTA28NM 20030910001762003091000176SO 2003 9 10 SIMA200322507 120030809A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21819AE 145566 ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 53-24-02. (M) 2L72 4F RTT00011AT 20030910001852003091000185SO 2003 9 10 SIMA200322508 120030810A532014521713005 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 ABI - DURING AN IMBV INSPECTION, THE GALLEY AREA CENTER HAT BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING HAT BEAM AND INSTALLED NEW HAT BEAM IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20030910002212003091000221EU 2003 9 10 MALA030390 120030728A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 DURING C CHECK IN CVG, FOUND NR 1 SEATRAIL CORRODED BEYOND LIMITS FROM FRAME 20 FORWARD. MAINTENANCE REPAIRED IAW EO NR A53026. A/C RELEASE DATE 8/11/03. REFER TO 409 NR 128567 FOR DETAIL. 2H74 4F RTA49EU 20030910002262003091000226EU 2003 9 10 MALA030395 120030830A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15448XJ 340B448 DURING WALKAROUND FOUND FLOOR TRACK LIGHTING 426N, 436N, 446N INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY 20LN, PN 3301-51 SN/OFF 21987, SN/ON 2134 IAW SF340 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTA52EU 20030911000422003091100042EA 2003 9 11 SWIA200312320 120030801A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 FS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. (DISCOVERED DURING C-CHECK) REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV. ''A'', RII 53-401.P/N: 601R-53-61-117-2 & P/N: 601R-53-61-117-4 2L72 4F4 FRTA21EA E15NE 20030911000472003091100047WP 2003 9 11 DHL2003873549 120030630A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 INTERIM REPAIR ON RIGHT HORZ STAB INBOARD L/E (STA.XFS.53.750-78.250) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17. CLEANED, TREATED AND PRIMED INNER FACE OF DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17, SRM 51-1-15 PG 1, SRM 51-1-21 PG 1. REFER TO JC BX3H55072 FOR RT HORZ STAB LE REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20030911000912003091100091WP 2003 9 11 DHL2003873517 120030619A573056110111 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING T/E PANEL SHOWS INNER SKIN DELAMINATED 4.000, (XW0.000-XW97.000). REMOVED AND REPLACED LT WING T/E PANEL (XW0.000-XW97.000) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030911001032003091100103NE 2003 9 11 DXTA200300092 220030816A7200 ENGINE BRAERO1000 HAWKER1000 7450005EU PWA 305 PW305B 52128NE LEFT MALFUNCTIONED E DXTAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 GL07551QS 259051 PCECB0001 LEFT ENGINE SHUTDOWN ON LANDING ROLL OUT, DURING ATTEMPTED START, ITT ROSE TO 680 DEG C, N2 APPROX 30 PERCENT, START ABORTED. TROUBLESHOT ENGINE USING PW305 MM, ATTEMPTED START FOUND ENGINE HUNG STARTED, SUMPED FUEL FOR CONTAMINATION FOUND NONE. REMOVED AND REPLACE P3 SOLENOID VALVE, RAN ENGINE, OPS CHECKED GOOD. 2L72 4F4 FRTA3EU E35NE 20030911001392003091100139WP 2003 9 11 DHL2003873585 120030628A532047505211 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT FITTING CRACKED 5.000 STA 857.000 L1. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030911001942003091100194WP 2003 9 11 AALA2003434 120030226A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW219615W 53562 MCI - FOUND LEFT SIDE, INBOARD SET TRACK, INBOARD SIDE AT FS 1157 HAS EVIDENCE OF CORROSION. REMOVED DAMAGED CHAIR TRACK FROM STATION 1088-1220 AND INSTALLED NEW CHAIR TRACK AND SPLICE PER SRM 53-05-00. (M) 2L72 4F RTA6WE 20030911002292003091100229WP 2003 9 11 DHL2003604563 120030514A5753 FLAP DOUG DC8 DC873F 302199FWP RT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING OB FLAP T/E DENTED FROM STA XF 304.000 - XF 310.000. REMOVED DAMAGED T/E IAW SRM 51-1-21A PG. 4, FABRICATED NEW T/E IAW SRM 57-1-0 PG 7,SRM 57-7-1 FIG 4. CLEANED, TREATED AND PRIMED AREA AND T/E LOWER SURFACE IAW SRM 51-1-8B. INSTALLED NEW T/E IAW SRM 51-1-21A PG 3. 2L74 4F RT4A25 20030912000662003091200066WP 2003 9 12 DHL2003604777 120030624A532047732951N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT DOOR FRAME LOWER INTERNAL SKIN FITTING 2.00 CRACKED AT STA 255.000, L-21L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030912000872003091200087NM 2003 9 12 AWXA200300835 120030709A5315D5311281400200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, BETWEEN FR 16-18. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT DAMAGED AREA OF FLOORBEAM Y1292, BETWEEN FR 16-17; FABRICATED 2 EACH FILLERS AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-14, PG 205-206, FIG 201, & SRM 51-11-14, PG 203-208, FIG 201. 2L72 4F RTA28NM 20030912001082003091200108EU 2003 9 12 AWXA200300867 120030723A5414D5463080900100 FAIRING AIRBUS320 A320231 3930325EU NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28644AW 317 MCN - MINOR REPAIR - DURING C-01 CHECK A 8.5 INCH CRACK WAS FOUND AT THE AFT END OF THE NR 1 PYLON INBOARD UPPER FAIRING WELDED ASSEMBLY, NAC STA 5369-6077, BETWEEN RIBS 7 & 8. MAINTENANCE REMOVED AND REPLACED WELDED ASSEMBLY INBOARD SIDE OF NR 1 PYLON IAW AMM SUBTASK 54-57-22-020-050-0A2. 2L72 4F RTA28NM 20030912001092003091200109NM 2003 9 12 AWXA200300876 120030805A33501012721 LIGHT BOEING737 737301 1384611NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 LAS - EEL - DURING 8 DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030912001112003091200111EU 2003 9 12 AWXA200300878 120030722A2560P4010021 BATTERY AIRBUS320 A320231 3930325EU FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28644AW 317 MCN - EMERGENCY EQUIPMENT - DURING C-01 CHECK ALL 4 EMERGENCY FLASHLIGHTS UNDER FLIGHT ATTENDANTS SEATS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL 4 EMERGENCY FLASHLIGHT BATTERY PACKS, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20030912001322003091200132NM 2003 9 12 AWXA200300896 120030712A53126516300511 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK A .75 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 5, WL 226-227. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD WEB AT RBL 5, WL 226-227; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, FIG 209, PG 265-274. 2L72 4F RTA16WE 20030912001382003091200138NM 2003 9 12 AWXA200300898 120030712A53126516300511 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK A .7500 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 7-7.5, WL 226. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD WEB AT RBL 7-7.5, WL 226; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW SRM 53-10-08, FIG 209, PG 265-274. 2L72 4F RTA16WE 20030912001542003091200154NM 2003 9 12 AWXA200300907 120030730A53476546592 CARGO TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR TRACK TIE DOWN AT BS 787, RBL 15. MAINTENANCE CUTOUT DAMAGED SECTION FLOOR TRACK TIE DOWN AT BS 787, RBL 15; FABRICATED 2 EACH REPAIR ANGLES, AN EXTRUSION, AND A STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12, FIG 1, PG 1. 2L72 4F RTA16WE 20030912001682003091200168WP 2003 9 12 AALA20030679 120030622A3350 CONTACTOR DOUG DC9 DC983 3022083WP CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21963TW 53613 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS FROM SEAT ROW 18 THROUGH 21 INOPERATIVE. CLEANED CEILING EMERGENCY EXIT LIGHTS BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030924001022003092400102NM 2003 9 24 03FDEA01286 120030811A5753ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING O/B T/E FLAP O/B AFT HINGE ASSY FOUND PIVOT BEARING MOUNT HOLE I/B BORE SURFACE CORRODED. ( FLAP SIDE ). LT WING O/B T/E FLAP O/B AFT HINGE ASSY (FLAP SIDE) PIVOT BEARING MOUNT HOLE I/B BORE SURFACE REPAIRED AS PER FEDEX EA 1-5750-63180. 2L73 4F RTA22WE 20030924001142003092400114SO 2003 9 24 BSY2003F00019 120030708A3260 DOWNLOCK PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MLG INOPERATIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0735871 318052123 L861761A HAD NO GEAR DOWN INDICATION ON RIGHT GEAR, DID A TOWER FLY BY, CYCLED GEAR THEN WAS OK. CLEANED DOWN AND LOCK. HOOKS CYCLED GEAR COULD NOT DUPLICATE. 1L72 3O3 O A20SO E14EA 20030925000182003092500018EU 2003 9 25 AALA20030784 120030721A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2114077 612 TUL - FOUND CORROSION ON END OF SEAT TRACK R LEFT AT FRAME 31, FORWARD SIDE OF LAVATORY MODULE L. INSTALLED NEW SEAT TRACK PER SRM 51-72-10. (M) 2L72 4F RTA35EU 20030926000132003092600013WP 2003 9 26 UPS03841145 120030826A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP COCKPIT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 EMERGENCY LIGHTS BATTERY PACK LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2L74 4F RT4A25 20030926000692003092600069EU 2003 9 26 226050303A 120030503A5532 SKIN PILATSPC12 PC1245 7090551EU VERTICAL STAB CRACKED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07308NA 226 3 INCH CRACK FOUND ON LEFT SIDE OF VERTICAL STAB. CRACK LOCATED APPROXIAMATELY 1INCH FROM AFT CORNER OF VERTICAL STABILIZER GOING FORWARD. 1L71 3T RTA78EU 20030926000992003092600099CE 2003 9 26 255031 120030901A2701 YOKE BEECH 1900 1900D 1154162CE COCKPIT EXCESS PLAY A NSVAD RETURN TO BLOCK F FLT CONT AFFECTED CLCLIMB 1 EA27136MJ UE36 EXCESSIVE PLAY IN ALL QUADRANTS IN CAPTAINS YOKE BOTH PITCH AND ROLL AXIS. 2L72 4T RTA24CE 20030926001152003092600115NM 2003 9 26 2003UALA00651 120030827A5712 RIB BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29177UA 24384 LT WING TRAILING EDGE WBL 445.94 RIB 65B08150-99 HAS A CRACK IN THE VERTICAL FLANGE BETWEEN 2 FASTENERS. DAMAGE CAN BE VIEWED FROM OUTBOARD END OF INBOARD FLAP WELL BELOW 65B07818 MIDFLAP DEFLECTOR RAMP. 2L74 4F4 FRTA20WE E24NE 20031021000272003102100027WP 2003 10 21 GTIA030689 120030907A5320 ANGLE DOUG DC9 DC982 3022082WP FS 826 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND CRACKED ANGLE AT FS 826 40 INCHES LBL ON TOP CTR FUEL TANK. STOP DRILLED CRACK. FORMED NEW ANGLE. INSTALLED ANGLES. (M) 2L72 4F A6WE 20031021000302003102100030 2003 10 21 USAABA03035 420030921A2565 SLIDE AIRBUS330 A330323 3930335EU R4 DOOR DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 PHL - A TEST OF THE EMERGENCY LIGHTS INDICATED A FAULT FROM THE R4 DOOR EPSU. MAINTENANCE REPLACED THE R4 DOOR SLIDE. (M) 2L72 4F RTA46NM 20031020001682003102000168 2003 10 20 DL73S030794 420030829A3417HG480B42 ADC BOEING737 737247 138448DNM E/E BAY FAILED A DALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO27382DL 23609 ON T/O LOST BOTH CAPT AND F/O AIRSPEED AND ALTIMETER. CAPTS FROZE, NO FLAGS. F/O HAD FLAGS IN VIEW. FOUND HOSES OFF NR 1 ADC. RECONNECTED HOSES, BOTH WERE SECURE. PERFORMED TEST ON ADC CHECKS OK. F/O ADC HAD FAILED. REPLACED SAME, TEST OK. 2L72 4F A16WE 20031020001942003102000194NM 2003 10 20 DLM11030818 120030906A3320 LIGHT DOUG MD11 MD11 3023602NM CABIN INOPERATIVE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27801DE 48472 IN FLIGHT READING (SNAKE) LIGHT AT 3 HJ WENT OUT. PAX NOTED ELECTRICAL SMELL, IFE SYSTEM DEACTIVATED. ON ARRIVAL RELAMPED SNAKE LIGHT, ALL CHECKS GOOD. 2L73 4F RTA22WE 20031020002082003102000208NM 2003 10 20 DLM90030821 120030908A215020495072 ACM DOUG MD90 MD9030 3023690NM A/C BAY SEIZED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27909DA 53389 AFTER T/O SMOKE REPORTED IN AFT CABIN. FOUND RT ACM FROZEN. REPLACED ACM AND COALESCER. 2L72 4F RTA6WE 20031020002412003102000241WP 2003 10 20 UPS03841345 120030922A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK IS WORN BEYOND LIMITS BETWEEN STA 340 TO 418 AT RBL 25. REMOVED, FABRICATED AND REPLACED SEAT TRACK BETWEEN STA 390-450 IAW SRM 53-2-3 FIG 8A. 2L74 4F RT4A25 20031020002432003102000243NM 2003 10 20 DLM88030822 120030908A3260 LIGHT DOUG MD88 MD88 3023688NM COCKPIT INOPERATIVE A DALAK NONE N FALSE WARNING LDLANDING 1 SO27951DL 49882 ON APPROACH, DID NOT GET GREEN NOSE GEAR SAFE LIGHT ON GEAR EXTENSION. INDICATOR PIN NORMAL. RELAMPED NOSE GEAR INDICATOR LIGHT. 2L72 4F RTA6WE 20031021000422003102100042NM 2003 10 21 USAABB03182 120030930A335020121 CHARGER BOEING767 767201 1385125NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 SNN - FOUND L1 AND R1 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE SWAPPED THE M738 POWER SUPPLY (CHARGER) WITH THE DEFECTIVE M1208 POWER SUPPLY. MAINTENANCE IN PHL REPLACED THE POWER SUPPLY. (M) 2L72 4F RTA1NM 20031021000432003102100043NM 2003 10 21 USAABB03179 120030928A2560 RELAY BOEING767 767201 1385125NM R2 DOOR FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19646US 23898 PHL - THE RIGHT OVERWING SLIDE FAILED SQUIB TEST 1. MAINTENANCE REPLACED THE K3 RELAY. (M) 2L72 4F RTA1NM 20031021000442003102100044NM 2003 10 21 USAA030190 120030729A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 CLT - FOUND SKIN CRACKED 6 INCHES, UPPER FORWARD CORNER OF L1 DOOR CUTOUT, STATION 340L, BETWEEN STRINGER 7/8. FABRICATED A SPLICE DOUBLER AND INSTALLED PER EA 94596 AND 94535. (M) 2L72 4F RTA2NM 20031021000642003102100064NM 2003 10 21 HALA0300786 120030912A28225006003C HOUSING BOEING767 76733A 1385209NM BOOST PUMP DAMAGED A HALAK NONE O OTHER ININSP/MAINT 1 WP13583HA 25531 PAE - RIGHT WING MAIN TANK BOOST PUMPS SHOWS EVIDENCE OF ARCING BETWEEN PUMP HOUSING AND SHUTOFF SLEEVES. REPAIR IN WORK. (M) 2L72 4F RTA1NM 20031021000652003102100065NM 2003 10 21 HALA0300785 120030912A28225006003C HOUSING BOEING767 76733A 1385209NM BOOST PUMP DAMAGED A HALAK NONE O OTHER ININSP/MAINT 1 WP13583HA 25531 PAE - LEFT WING MAIN TANK FUEL BOOST PUMPS SHOWS EVIDENCE OF ARCING BETWEEN PUMP HOUSING AND SHUTOFF SLEEVES. REPAIRS IN WORK. (M) 2L72 4F RTA1NM 20031021000942003102100094NM 2003 10 21 AALA20030995 120030911A33500202365001 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21789AN 30252 LHR - TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT FIRST CLASS GALLEY CLOSET. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20031021001162003102100116EU 2003 10 21 A6WA200360040 120030927A5753 SKIN BAC 146 146200A 1500266EU T/E FLAP DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 DAMAGED RIGHT OUTBOARD FLAP TAB BOTTOM SKIN BETWEEN RIBS 21-22. REPAIR IAW BAE FAX BARA/AVR/6530/03-DC. (M) 2H74 4F A49EU 20031021001192003102100119WP 2003 10 21 GTIA030711 120030914A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND SKIN CREASE AT FS 418 BETWEEN LONGERONS 16R AND 18R REQUIRES REPAIR. CUT OUT DAMAGED AREA FS 418 L16R TO 18R. FABRICATED FILLER, FINGER DOUBLER, DOUBLER. FABRICATED 3 STRAPS. INSTALLED FINGER DOUBLER, DOUBLER, FILLER AND STRAPS. (M) 2L72 4F A6WE 20031021001262003102100126NM 2003 10 21 AALA20030947 120030903A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21357AA 24038 DFW - EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 17H. BATTERY PACK FAILED DUAL FEED CHECK. CONNECTED SEAT WIRING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030926001192003092600119EA 2003 9 26 A6WA200340118 120030804A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT FAILED A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31410AW 7490 ON TAXI, CABIN BEGAN TO FILL WITH SMOKE. PLACED RT PACK ON MEL. RT PACK MAKING LOUD GRINDING NOISE AND EXCESSIVE VIBRATION. RAN RIGHT ENGINE, CHECKED NR 2 BLEED AND APU BLEED ON NR 1 PACK. NO SMOKE NOTED. REMOVED AND REPLACED AIR CYCLE MACHINE IAW AMM. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030929000032003092900003EA 2003 9 29 COMA0350394 120030902A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA23585 7027 DURING COMPLIANCE OF TASK NR 002-53-160-610, 4 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL9.0 AND RBL9.0. THE CRACKS RANGE FROM 2.5 INCHES TO 3.250 INCHES IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IAW MFG REO NR 601R-53-41-102, REV B., DATED 6-8-2003, AND REO NR 601R-53-41-162, DATED 6-9-2003. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20030929000552003092900055EU 2003 9 29 DHL2003367006 120030903A5270 SWITCH AIRBUS300 A300B4203 3930306EU CARGO DOOR INOPERATIVE A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01367DH 265 DURING CLIMB OUT, THE AFT CARGO DOOR LIGHT ON THE S/O PANEL ILLUMINATED. THE (DOORS) LIGHT ON THE MASTER WARNING PANEL DID NOT ILLUMINATE AND NO CHIME WAS HEARD. THE DOORS TESTED CORRECTLY. PERFORMED EMERGENCY CHECK LIST. PRESSURIZATION NORMAL. RIGGED BULK PIT DOOR WARNING SWITCH AND CHECKED IAW M/M 52-71-11. SYSTEM OK FOR CONTINUED SERVICE. 2L72 4F RTA35EU 20030929000592003092900059CE 2003 9 29 ENHA200320807 120030904A2750262228112 BELLCRANK CESSNA208 208B 2073701CE ZONE 600 MISMANUFACTURED E ENHAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL031276P 208B0852 FLAP BELLCRANK INSPECTION FOUND MISSING WELDS AT MATING PORTIONS OF THE ASSEMBLY. BELLCRANK COULD BE SUBJECT TO CATASTROPHIC FAILURE. INSPECTION PROMPTED BY AL FSDO LETTER DATED 8/15/03. SUBJECT BELLCRANK REPLACED WITH P/N 2622311-7 OF NEW DESIGN. 1H71 3T A37CE 20030929000662003092900066NM 2003 9 29 AWXA200301016 120030813A57546546424 SKIN BOEING737 737277 1384570NM KRUEGER FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .75 INCH CRACK WAS FOUND ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205. MAINTENANCE BLENDED OUT CRACK ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A EXTERNAL REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 15-5742-03242-ES2. 2L72 4F RTA16WE 20030929000742003092900074NM 2003 9 29 03FDEA01440 120030829A5754 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE CORROSION REMOVED AND REPLACED AS PER EA 1-5750-72654 . 2L73 4F RTA22WE 20030929000912003092900091WP 2003 9 29 UPS03841160 120030825A5754 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, RT WING L/E LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030929000952003092900095WP 2003 9 29 UPS03841164 120030828A5544 WEB DOUG DC8 DC873F 302199FWP RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, WEB IN RUDDER LE AT FORWARD SPAR IS CRACKED AT XR 160 REMOVED WEB SECTION,FABRICATED AND INSTALLED REPLACEMENT WEB SECTION IAW SRM. 55-2-4 FIG. 1 2L74 4F RT4A25 20030929001242003092900124WP 2003 9 29 03FDEA01459 120030907A7110 CASE DOUG MD10 MD1010F WP GE CF6 CF66D 30020GL ZONE 400 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 451426 GOUGES IN EXTERIOR OF NR 2 FAN FRAME CASE. COMPLIED WITH E.A. 8-7220-72285 ENGINES-DISPOSITION OF GOUGES IN EXTERIOR OF NR 2 ENGINE FAN FRAME CASE. 2L73 4F4 FRTA22WE E23EA 20030929001262003092900126WP 2003 9 29 03FDEA01457 120030907A78309690M05G30S2 WEB DOUG MD10 MD1010F WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 EXHAUST SYSTEM THRUST REVERSER SUPPORT WEB CRACK REPAIR. COMPLIED WITH E.A.8-7830-72281. EXHAUST SYSTEM THRUST REVERSER SUPPORT ASSY WEB CRACK REPAIR. 2L73 4F RTA22WE 20030929001342003092900134NM 2003 9 29 CALA0300514 120030905A5753 FITTING BOEING737 7373T0 1384582NM I/B T/E PANEL CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A .5 INCH CRACK IN LT WING UPPER AFT INBOARD T/E PANEL OUTBOARD SUPPORT FITTING. A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030929001372003092900137WP 2003 9 29 UPS03841170 120030723A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C2, RADIOGRAPHIC (X-RAY) INSPECTION REVEALED A CRACK ON THE R-2 DOOR UPPER AFT CORNER APPROX. .375 INCH IN LENGTH,STA. 1660 LONG. 11R CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER I.A.W. SRM. 53-2-0 FIG. 16 2L74 4F4 FRT4A25 E2GL 20030729001012003072900101NM 2003 7 29 USAA030093 120030528A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19504AU48519 23379 CLT - FOUND SKIN CRACKED 1.25 INCH, STATION 727D PLUS 7 INCHES ABOVE S-24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20030729001032003072900103NM 2003 7 29 MEX2003220 120030609A2910340545 BYPASS VALVE BOEING757 7572Q8 1384972NM L/E SLAT LEAKING A ASMFD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23806AM 26273 FLT 494 - MID-MEX - AIRCRAFT RETURN TO GATE, HYDRAULIC LEAK AT LEFT COMPARTMENT RESERVOIR AND DURING ENGINES STARTING THE 'LIGHT RUDDER PCU' EICAS STATUS MESSAGE TURN ON. THE LEFT SLATS BYPASS VALVE WAS REPLACED IAW MM, TASK CARD 27-81-09-024-001 AND 27-81-09-424-016) FIM PROCEDURE WAS ACCOMPLISHED AND MESSAGE WAS ERASED IW FIM 31-4-00. THE SLATS SYTEM WAS CHECKED IAW MM 27-80-01, ALL TESTS CORRECT. (M) 2L72 4F RTA2NM 20030729001172003072900117WP 2003 7 29 2003F00485 120030618A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WXOAK NONE L NO TEST TXTAXI/GRND HDL 1 WP17860GA 49786 DURING A TURN IN LAS, THE FLIGHT CREW REPORTED EMERGENCY TRACK LIGHTING WIRES EXPOSED, SEVERAL LIGHTS INOPERATIVE ON RIGHT SIDE MID CABIN. EMERGENCY MAINTENANCE WAS CALLED OUT. UNABLE TO GET THE PROBLEM RESOLVED. A MECHANIC WAS DISPATCHED FROM FAT WITH PARTS. THE MECHANIC RE-LAMPED 11 OF 12 POSITIONS ON FLOOR TRACK LIGHTS ROW 23 THROUGH 30. ALL LIGHTS, OPS CHECKED GOOD. THE WIRE BUNDLES WERE SECURED UNDER THE FLOOR TRACK LIGHTING COVER. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20030729001272003072900127EA 2003 7 29 SWIA200312200 120030718A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT SPOILERON MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07435SW5026 5026 7555 ON TAXI OUT, GOT ''R SPOILERON'' AND ''SPOILERON FAULT'' MSGS. REMOVED AND REPLACED RIGHT SPOILERON INBOARD PCU IAW 27-62-01. LEAK AND OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030729001392003072900139NE 2003 7 29 P5CA0300894 220030703A7320R41013 CONNECTOR BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE DIRTY A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23923FT 22769 702193 NR 2 ENG WILL NOT START. NO FUEL FLOW. NR 2 ENG FUEL CONDITION ACTUATOR PLUG CLEANED AND RESECURED. ACTUATOR EXERCISED. ENG START SATIS. SUSPECT WIRING TO FUEL CONDITION ACTUATOR. 2L74 4F4 FRTA20WE E3NE 20030730000052003073000005WP 2003 7 30 ABXA030201 120030421A5311 FRAME DOUG DC8 DC861 3021952WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23843AX 46017 AFT CARGO STATION 1240, LONGERON 36 FRAME CORRODED. REPAIRED STATION 1240, LONGERON 36 IAW REA D853-46706. INSTALLED INTERCOSTAL, SHEAR TIE, GILLINER ATTACH ANGLE AND GUSSETTS IAW DC-8 SRM 51-1-20D. 2L74 4F 4A25 20030730000262003073000026WP 2003 7 30 ABXA030264 120030322A5230 FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE STUB FRAME IN MAIN CARGO DOOR AT STA 183.5. REMOVED STUB FRAME, LOCATED AND DRILLED, AND INSTALLED STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-24. 2L74 4F 4A25 20030730000282003073000028NM 2003 7 30 P5CA0300901 120030716A8012 START VALVE BOEING747 74746NF 13848BTNM GE CF6 CF680 30025NE NR 2 ENGINE MALFUNCTIONED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23450PA 30808 706199 ENG NR 2 WOULD NOT START EICAS MESSAGE -ENG NR 2 START VLV-. DEFERRED NR 2 ENG PER DDG START VLV REQUIRED MANUAL START. 2L74 4F4 FRTA20WE E13NE 20030730000382003073000038 2003 7 30 P5CA0300890 420030618A344220414440404 ANTENNA BOEING747 747341 13848AMNM WEATHER RADAR FAULTY A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23354MC 23394 RADAR SYS 1 & 2 ANT FAULT ON BOTH SCREENS INTERMITENT IN BOTH TEST & WX MODE, RETURNED TO GATE. WEATHER RADAR FAIL. REPLACED WEATHER RADAR ANTENNA. UNKNOWN WEATHER RADAR FAILED TO PAINT WEATHER. 2L74 4F RTA20WE 20030730000452003073000045WP 2003 7 30 ABXA030255 120030316A5200 DOOR FRAME DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 UPPER LATCH HOOK MOUNT HOLE AT STA 196.5 HAD CRACK INDICATION. REMOVED DAMAGED FRAME, LOCATED, DRILLED, AND DEBURRED NEW FRAME, INSTALLED IAW ABX REA D852-46041MR AND DC-8 SRM 51-1-21 AND 51-1-8. 2L74 4F 4A25 20030730000462003073000046WP 2003 7 30 ABXA030256 120030211A5200 MOUNT DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 UPPER LATCH HOOK MOUNT HOLE AT STA 193 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR. 2L74 4F 4A25 20030730000512003073000051WP 2003 7 30 ABXA030260 120030312A5200 DOOR FRAME DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 UPPER LATCH HOOK MOUNT HOLE AT STA 153.0 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR. 2L74 4F 4A25 20030725000122003072500012NM 2003 7 25 DL76S030586 120030616A7120 LINK BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27127DL43993 24077 580356 A/C LOG E302036 ITEM 007 DETAILS REPLACEMENT OF AFT MOUNT O/B TANGENTAL LINK DUE TO CRACK THROUGH ONE SIDE OF LINK EVEN WITH CENTERLINE OF BEARING. CRACK WAS FOUND BY MTC ON WALK AROUND AND REPLACED. NO OPERATIONAL PROBLEMS WERE NOTED BEFORE OR AFTER REPLACMENT. REPLACED CRACKED LINK ON O/B AFT MOUNT NR 1 ENG PER MM. 2L72 4F4 FRTA1NM E13NE 20030728000052003072800005NM 2003 7 28 SWAA031571 120030714A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 500D AT STR 7R AND BS 420 AT STR 4R. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030728000132003072800013NM 2003 7 28 SWAA031597 120030720A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (6 EA) AT STR 4L, BS'S 591, 592, 644, 698, 702 AND 590. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728000322003072800032NM 2003 7 28 SWAA031592 120030718A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, 2, 3, 7, 17, 20, 22 AND 23. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030728000492003072800049 2003 7 28 SWAA031606 420030719A2565D31354 SLIDE BOEING737 7375H4 138449DNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030728000532003072800053NM 2003 7 28 SWAA031610 120030717A2612 FIRE WARNING BOEING737 7373H4 1384600NM COCKPIT MALFUNCTIONED A SWAABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29614SW 28033 AIR TURNBACK, DECLARED EMERGENCY, FWD CARGO FIRE DETECTION LIGHT ILLUMINATED, DISCHARGED BOTTLES. REMOVED AND REPLACED FOLLOWING, NR 1 AND NR 2 FIRE BOTTLES, CONTROL CABIN FIRE DETECTION PANEL, CARGO FIRE SYSTEM METERING VALVE, FIRE DETECTORS NR 1, NR 2, NR 3 AND NR 4 AND DIVERTER VALVE PER MM. AWAITING ENGINEERING INVESTIGATION TO DETERMINE ACTUAL CAUSE. 2L72 4F RTA16WE 20030728000762003072800076NM 2003 7 28 SWAA031566 120030716A53156545410 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, WL 208 AND LBL 17 TO RBL 12. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20030728000832003072800083 2003 7 28 SWAA031573 420030717A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030728001052003072800105NM 2003 7 28 SWAA031588 120030718A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728001202003072800120NM 2003 7 28 SWAA031543 120030712A3230M991 CIRCUIT CARD BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29335SW 23939 AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED M991 CARDS ON E-11 LANDING GEAR LOGIC SHELF. 2L72 4F RTA16WE 20030729000652003072900065NM 2003 7 29 QXEA200300824 120030711A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - PANEL 261CT CHAFED FORWARD AND AFT FLANGES. REPAIRED IAW Q400 RD 8/4-53-521, PAGE 4, STEPS 4 THROUGH 7 AND RD 8/4-53-521, PAGE 4, STEP 8. 2H72 4T4 TRTA13NM E00062EN 20030729000882003072900088NM 2003 7 29 QXEA200300754 120030619A3620 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM COCKPIT ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09404QX 4046 BZN-ON FLIGHT NUMBER 2350, NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED EN ROUTE AT 25, 00 FEET. NR 2 BLEED SEL OFF PER CHECKLIST. LIGHT REMAINED ON FOR TWO MINUTES AFTER TOUCHDOWN. COMPLIED WITH OPERATIONAL CHECK OF ECS SYSTEM. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030730000942003073000094WP 2003 7 30 ABXA030310 120030719A5310 DOOR FRAME DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX 45927 L2 DOOR, UPPER AFT CORNER OF DOOR CUTOUT CRACKED. REMOVED AND REPLACED DOUBLER, TRIPLER AND FILLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21 AND 51-1-11. 2L74 4F 4A25 20030730001232003073000123NM 2003 7 30 MEX2003222 120030612A8011784750A3 SHAFT BOEING757 7572Q8 1384972NM NR 1 STARTER BROKEN A ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23301AM 30045 FLT 402 - MEX-JFK - AIRCRAFT RETURN TO PLATFORM, ENGINE NR 1 DID NOT START. DURING REVISION, THE STARTER SHAFT WAS BROKEN. THE STARTER WAS REPLACED IAW MM 80-11-01, ALL TESTS CORRECT. (M) 2L72 4F RTA2NM 20030730001272003073000127EU 2003 7 30 SIMA200318101 120030627A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21901AE 340B401 ILE - FLT 3594 - CREW REPORTED THE FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO DFW FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030730001342003073000134EU 2003 7 30 SIMA200317601 120030624A3350 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21263AE 340B263 DFW - FLT 3491 - CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED THE POWER PACKS AND RECHARGED ON THE BENCH. POWER PACKS WERE REINSTALLED AND AN OPERATIONAL CHECK WAS COMPLIED WITH AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030730001382003073000138SO 2003 7 30 SIMA200314703 120030524A3610 CLAMP EMB 145 EMB145 3260210SO BLEED AIR SYS LOOSE A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21611AE 145074 CLE - FLT 4383 - DURING APPROACH, THE CREW RECEIVED A BLEED ONE LEAK WARNIGN IN ICING CONDITIONS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED SAFELY IN CLE WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE INSPECTED ALL BLEED LINES AND RESECURED LOOSE CLAMPS AND COUPLINGS IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030730001402003073000140SO 2003 7 30 SIMA200316008 120030531A5330 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21648AE 145225 ABI - DURING AN INSPECTION, A DENT WAS DISCOVERED BETWEEN FRAMES 64 AND 65 AND BETWEEN STRINGERS 19L AND 21L. RECONTURED DENT AND PERFORMED AN NDT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/1817. (M) 2L72 4T RTT00011AT 20030731000132003073100013EA 2003 7 31 QXEA200300860 120030717A26114735972 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX 10045 PDX- ON FLIGHT 2439 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731000182003073100018NM 2003 7 31 QXEA200300817 120030709A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA HORIZ STAB MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - HORIZONTAL STABILIZER TO VERTICAL STABILIZER FORWARD LEFT CONNECTION POINT SHIMS/SPACERS COMPLETELY EXTRUDED/MISSING. REPAIRED IAW SRM 51-23-00 AND RD 8/4-55-094. 2H72 4T4 TRTA13NM E00062EN 20030731000232003073100023NM 2003 7 31 QXEA200300913 120030725A2611 FIRE WARNING DHAV DHC8 DHC8202 2809007NM COCKPIT ACTIVATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09349PH 486 EAT- ON FLIGHT 2134 ENROUTE SEA TO EAT MASTER WARNING AND CHECK FIRE DETECTION ILLUMINATED. DURING EMERGENCY CHECKLIST SELECTED LOOP A ONLY BECAUSE LOOP B WAS ILLUMINATED. MASTER WARNING AND CHECK FIRE DETECTION WENT OUT. REMOVED AND REPLACED SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000312003073100031EU 2003 7 31 QXEA200300866 120030721A33506008905 BATTERY FOKKERF28 F28MK4000 4990810EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09497US* 2 11173 PDX- LEFT HAND AND RIGHT HAND AFT EVACUATION LIGHTS ARE INOPERATIVE. REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20030731000362003073100036NM 2003 7 31 QXEA200300782 120030702A5540 STRUCTURE DHAV DHC8 DHC8202 2809007NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- CRACK IN UPPER AFT SECTION OF FORE LEFT HAND RUDDER. REPAIRED IAW RD 8-55-335. 2H72 4T RTA13NM 20030731000372003073100037NM 2003 7 31 QXEA200300783 120030701A3010 BOOT BOMBDRDHC8 DHC8401 1390041NM LT WING CUT A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09412QX 4059 SEA- ON FLIGHT 2372 DURING CRUISE WITH ICE DETECTED TURNED ON BOTH BOOTS AND GOT "DEICE PRESSURE" CAUTION. RAN CHECKLIST. PRESSURE ON BOTH SIDES IS OKAY. NR 1 OUTER BOOT WILL NOT INFLATE AND NR 2 OUTER BOOT WILL NOT DEFLATE. FOUND TWO CUTS ON LEFT HAND OUTBOARD LEADING EDGE DEICE BOOT. REPAIRED IAW DHC-8 Q400 MM 30-11-00. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000542003073100054NM 2003 7 31 QXEA200300848 120030718A323311300105 ACTUATOR DHAV DHC8 DHC8202 2809007NM MLG MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09362PH217015926 518 PDT- ON FLIGHT 2096 ON DEPARTURE FROM PSC, PUT GEAR UP AND HEARD A ROUGH UNUSUAL SOUND AND HYDRAULIC SOUND WAS LONGER THAN NORMAL. RIGHT GEAR DOOR LIGHT AND RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. MAINTENANCE INSPECTED AIRCRAFT AND REPLACED THE UPLOCK ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030911000612003091100061NE 2003 9 11 2003UALA00611 220030804A7200 ENGINE BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 SHUTDOWN A UALAE ENGINE SHUTDOWN RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP29116UA 26908 717696 SHUT DOWN NR 2 ENGINE. REMOVED ENGINE AND FOUND A FAILURE OF THE ANGLE GEARBOX. THE FAILURE OF THE ANGLE GEARBOX CAUSED FAILURES IN THE MAIN GEARBOX CAUSING THE LOSS OF N2 AND OIL PRESSURE. 2L74 4F4 FRTA20WE E24NE 20030911000852003091100085WP 2003 9 11 DHL2003873534 120030627A5514 ANGLE DOUG DC8 DC873F 302199FWP HORIZ STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT HORIZONTAL STABILIZER INNER ANGLE CRACKED AT XFS.47.500. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW ANGLE IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE ON RT HORIZONTAL STABILIZER AT XFS.47.500 IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001232003091100123WP 2003 9 11 DHL2003873554 120030627A5751 SKIN DOUG DC8 DC873F 302199FWP RT AILERON DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OTBD. AILERON 0.750 DENTED ON UPPER PLATING AT ZA.651.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 2X PG 30-31. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG 2X PG 30-31. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED REPAIR DOUBLER AND FAIRING PLATE IAW SRM 57-2-1 FIG 2X PG 30-31. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERNAL PART AND FAIRING PLATE IAW SRM 51-1-8B. INSTALLED REPAIR DOUBLER AND FAIRING PLATE ON RT OTBD AILERON AT ZA.651.000 WITH NEW FASTENERS AND BONDED IAW SRM 57-2-1 FIG 2X PG 30-31, SRM 51-1-9 PARAGRAPH 3, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001302003091100130WP 2003 9 11 UPS03841032 120030705A5310 SHEAR TIE DOUG DC8 DC871F 302199DWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, AFT PIT STA 1200 STR 33L SHEAR TIE FITTING CORRODED. REMOVED CORRODED FITTING IAW DC8 SRM 51-1-20D. LOCATE AND DRILLED NEW FITTING AND FABRICATED SPLICE ANGLES IAW DC8 SRM 53-2-0 FIG 2D. ALODINE AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED 2 FITTING AND SPLICE ANGLES IAW DC8 SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20030911001682003091100168WP 2003 9 11 UPS03841039 120030707A53403755822U505 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, FWD PIT FS 272 AND L25L Z-FITTING CORRODED. REMOVED FITTING, FABBED SPLICE ANGLES 2 EA IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED AND DRILLED HOLES ON NEW FITTING IAW DC8 SRM 53-2-0, INSTALLED NEW FITTING AND SPLICE ANGLES IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030911002222003091100222NM 2003 9 11 DHL2003782008 120030816A5250 HANDLE BOEING727 727227 1384078NM COCKPIT DOOR BROKEN A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01769AT 21998 COCKPIT DOOR HANDLE IS BROKEN, DOOR DOESN'T FULLY SHUT. RE-SECURED HANDLE, OPS CHECKED GOOD IAW BMM CHAPTER 52-00. 2L73 4F A3WE 20030911002362003091100236WP 2003 9 11 DHL2003604566 120030513A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CENTER L/E FORMER CRACKED 0.500 AT XFS 304.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9,10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030912000032003091200003NM 2003 9 12 03FDEA01318 120030807A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING - O/B FLAP O/B HINGE FITTING ( WING SIDE ) FWD ATTACHMENT O/B HOLE SPOT FACE FOUND CORROSION. LT WING O/B FLAP, O/B HINGE FITTING ( WING SIDE ) FWD ATTACHMENT O/B HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030912000432003091200043WP 2003 9 12 DHL2003604732 120030604A53203755856502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT FITTING CORRODED AT STA 1280.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, ATM PO201389, DWG 3755856. REMOVED CORRODED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW FITTING IAW DWG 3755856. PERFORMED LIQUID PENETRANT INSPECTION TO NEW FITTING IAW DC8 NDT SPM PART 08-00-02/06. CLEANED, TREATED AND PRIMED NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030912000532003091200053WP 2003 9 12 DHL2003604606 120030520A5754 DOUBLER DOUG DC8 DC873F 302199FWP L/E SLOT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING CTR EXTENDED L/E SLOT INNER DOUBLER CRACKED 0.630 AT STA XFS 526.000. PERFORMED MAJOR REPAIR IAW EODHL-030532, ED-3350. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED THE CRACK END 0.250 DIA IAW EODHL-030532, ED-3350. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER IAW EODHL-030532, ED-3350. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON RT OUTER WING CTR EXTENDED L/E SLOT, STA 526.000 USING NEW FASTENERS IAW EODHL-030532, ED-3350, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912001072003091200107NM 2003 9 12 AWXA200300865 120030713A532065C326772 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF SHEAR WEB BS 986 TO 997, LBL 35-44, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB BS 986 TO 997, LBL 35-44; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1-11, & 38, FIG 8. 2L72 4F RTA16WE 20030912001392003091200139EU 2003 9 12 AWXA200300883 120030806A3350321430 BATTERY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28626AW 65 LAX - EEL - SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE AT MID CABIN. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT MID CABIN EMERGENCY POWER SUPPLY UNIT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030912001752003091200175WP 2003 9 12 AALA20030867 120030815A3350 RELAY DOUG DC9 DC982 3022082WP CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114551 53033 DFW - DURING OVERWING EMERGENCY LIGHTS INOPERATIVE FROM FLIGHT ATTENDANT SWITCH. REPLACED RELAY R2 271. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030915000382003091500038EU 2003 9 15 BAQA088890 120030905A2140JBS8803 HEATER UROCOPEC135 EC135T1 5620026EU CABIN MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME20 132 HEAT COMES ON INTERMITTENTLY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030915000462003091500046SW 2003 9 15 HEEA088926 120030822A6700204001364101S CONTROL STICK BELL 412 412 1182202SW COCKPIT MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 STICK BOLT HOLE FOR ELBOW IS MISALIGNED. BOLT WILL NOT GO THROUGH. 1G72 4U H4SW 20030915000982003091500098SW 2003 9 15 BAQA089106 120030905A6330206033554101 LINK BELL 206 206L1 1182107SW GEARBOX MOUNT DELAMINATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035744Y 45465 LINK IS DELAMINATED BEYOND LIMITS. OIL SOAKED. REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20030916000192003091600019WP 2003 9 16 ANCF200300021 120030814A2131 CONTROLLER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN PRESSURE MALFUNCTIONED W ANCFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23190AN 53190 T/O WAS PERFORMED ACCORDING TO OPTION NR 1 OF MEL 21-1 (RT PACK INOPERATIVE) AT 100FT WE SWITCHED LT A/C SYSTEM SWITCH TO AUTO & IT DIDN´T PRESSURIZE AIRCRAFT, SUPPLY PRESSURE DROPS TO ZERO CHECK LIST WAS PERFORMED & WAS UNSUCCESFULL THE WE SWITCHED THE PRESSURE CONTROL SYSTEM FROM AUTO 2 TO AUTO 1 AND THE FAULT REMAINED AT 10.000IN RNG VOR DURING APROACH THE LT PACK STARTER TO WORK. ACCOMPLISHED TROUBLESHOOTING REF AMM 21-20-00 PAG 121 PARAG. 3 - 4 FOR FLOW CONTROL VALVE DEFECTIVE SO WAS INSPECTED FLOW CONTROL VALVE FILTER. IT WAS FOUND CLOGGED.THEREBY WAS CLEANED AND WAS SWAPPED WITH THE RT FLOW CONTROL VALVE REF AMM 21-31-02. 2L72 4F4 FRTA6WE E9NE 20030916000272003091600027 2003 9 16 252TR0006 420030705A22202590650901 COUPLER BOEING737 737228 13844AGNM PWA JT8 JT8D NE MACH TRIM INTERMITTENT A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05252TR 23001 MACH TRIM IS INTERMITTENT. PLACED ON MEL 22-5. 7/15/2003; REMOVED AND REPLACED MACH TRIM COUPLER IAW MM 22-21-0 AND CLEARED MEL. 2L72 4F4 FRTA16WE E2EA 20030916000352003091600035CE 2003 9 16 DXTA20030072 120030721A2120 ODOR CESSNA500 560CESSNA 2076750CE CABIN DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07333QS 5600333 OILY ODOR ON TAKEOFF AND DESCENT AND AT ALTITUDE OF 15,000 FT. - ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20030916000362003091600036NM 2003 9 16 C1HA200394017 120030717A3150 WARNING HORN BOEING727 727290 138408WNM COCKPIT FALSE ACTIVATIONA C1HAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15294AS 22146 DURING TAKE-OFF, WHEN POWER ADVANCED PAST 1.4 EPR THE T/O WARNING SOUNDED - ALL SETTINGS NORMAL TRIM IN GREEN FLAPS 15 DEG SPEED BRAKE FORWARD - ACCOMPLISHED SYSTEM TEST NO TROUBLE FOUND. 2L73 4F A3WE 20030916000522003091600052NE 2003 9 16 52767 220030720A7532 BLEED VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE INOPERATIVE A AMWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE07144ZV UE144 DURING TAKE OFF ON FLIGHT 5578, THE POWER ADDED TO THE RT ENGINE WOULD NOT DEVELOP MORE THAN 1000 FT LBS TORQUE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BLEED VALVE AND THE PROP GOVERNOR. STILL AWAITING MORE INFORMATION TO COME. 2L72 4T4 TRTA24CE E26NE 20030912000482003091200048WP 2003 9 12 DHL2003604712 120030607A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 C-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR AND DENTS AT SEVERAL SPOTS. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1, SRM 52-4-1 FIG 2, BOEING MESSAGE DHL-CVG-0079H. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN IAW SRM 52-1-0 PG 1, SRM 52-4-1 FIG 2, BOEING MESSAGE DHL-CVG-0079H. CLEANED, TREATED AND PRIMED NEW SKIN IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 21. 2L74 4F RT4A25 20030912000572003091200057WP 2003 9 12 DHL2003604535 120030502A5720 SPLICE PLATE DOUG DC8 DC873F 302199FWP LT WING BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING OTBD L/E FORMER SPLICE PLATE BROKEN AT XFS 710.000. REMOVED SPLICE PLATE IAW SRM 51-1-21 PG 1. FABRICATE NEW SPLICE PLATE IAW SRM 57-1-0 PG 2, SRM 57-3-0 FIG 20. CLEANED, TREATED AND PRIMED AREA AND NEW SPLICE PLATE IAW SRM 51-1-8B. INSTALLED NEW SPLICE PLATE IAW SRM 57-1-0 PG 1, SRM 57-3-0 FIG 20, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912001102003091200110NM 2003 9 12 AWXA200300877 120030805A5754 ROLLER BOEING737 737277 1384570NM L/E SLAT OUT OF ADJUST A AWXAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 WP28188AW 22655 LAX - FLIGHT CONTROL - FLT 0102 - ON TAKEOFF AT LAS EN ROUTE FOR LAX AT FLAP 1 THE AIRCRAFT HAD TENDENCY TO ROLL RIGHT, 20 DEGREES LEFT AILERON NEEDED TO HOLD WINGS LEVEL. AFTER FLAPS WERE RETRACTED ROLL TO THE RIGHT STOPPED. ON APPROCH INTO LAX AT FLAP 1 AND SPEED BRAKES OUT NO ROLL WAS PRESENT. WHEN SPEED BRAKES WERE RETRACTED ROLL RETURNED, THE MORE FLAPS WERE EXTENDED THE LESS ROLL WAS NOTICED. MAINTENANCE INSPECTED THE LEADING EDGE FLAPS/SLATS, SPOILERS, TRAILING EDGE FLAPS, AND ACTUATING MECHANISMS FOR SECURITY AND PROPER ALIGNMENT. FOUND NR 4 SLAT OUT OF ALIGNMENT WHEN SLATS EXTENDED; ADJUSTED DETENT ROLLER ARMS ON NR 4 SLAT IAW BMM 27-81-21; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030912001472003091200147NM 2003 9 12 AWXA200300904 120030725A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR BEAM AT BS 858, RBL 15. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT FLOOR BEAM BS 858, RBL 15; FABRICATED 2 EACH REPAIR ANGLES AND AN EXTRUSION; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-70-53, FIG 201. 2L72 4F RTA16WE 20030912001622003091200162EU 2003 9 12 AWXA200300914 120030802A5320D5391379020002 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE BUCKLED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 MCN - MINOR REPAIR - DURING C-04 CHECK FOUND THE FORWARD CARGO COMPARTMENT CENTER FLOOR PROFILE BUCKLED AT FR 28, BETWEEN STR 43 LT & 43 RT. MAINTENANCE REMOVED CENTER FLOOR PROFILE BETWEEN STR 43 LT & 43 RT AT FR 28; FABRICATED A NEW REPLACEMENT CENTER FLOOR PROFILE; INSTALLED REPAIR PART IAW 51-42-11, PG 8-9, & 22, FIG 8, & SRM 51-44-11, PG 1 & 4, FIG 1. 2L72 4F RTA28NM 20030915000592003091500059 2003 9 15 BAQA089010 420030905A34215040017926 GYRO BOLKMS117 BK117B2 5626013EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KC 7168 INTERNAL LIGHTING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030915000962003091500096 2003 9 15 BAQA088915 420030910A34215040017926 INDICATOR BOLKMS117 BK117A1 5626010EU ATTITUDE DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03300CP893 7249 ATTITUDE INDICATOR WILL NOT CAGE. PARTS LOOSE INSIDE. MOTOR NOISY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030916000312003091600031NM 2003 9 16 03FDEA01072 120030709A5510NLC6725 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT HORIZONTAL STABILIZER NR 36 BORE CORROSION EXCEEDED CONDITION "3". CORROSION ON RT HORIZONTAL STABILIZER NR 36 BORE REMOVED AND REPAIR CARRIED-OUT IAW EA 1-5510-71838 (STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL BORE 36 RIGHT). 2L73 4F RTA22WE 20030916000772003091600077WP 2003 9 16 GTIA030643 120030808A7120K22199SA32 ISOLATION MOUNT DOUG DC9 DC983 3022083WP NR 2 ENGINE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FTW - FOUND NR 2 ENGINE AFT VIBRATION ISOLATOR INNER RESILIENT ELEMENT HAS .5 INCH AREA OF LOOSE AND UNRAVELING STRANDS. REMOVED NR 2 ENGINE AFT VIBRATION ISOLATOR. INSTALLED NR 2 ENGINE AFT VIBRATION ISOLATOR. (M) 2L72 4F RTA6WE 20030916000802003091600080WP 2003 9 16 GTIA030635 120030722A5310 DOOR FRAME DOUG DC9 DC983 3022083WP AFT CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND AFT CARGO DOOR JAMB BEAM CORRODED AND RUNS UNDER THRESHOLD PANEL FS 1155-1212. FABRICATED 1 DOUBLER. INSTALLED 1 DOUBLER. (M) 2L72 4F RTA6WE 20030916001112003091600111WP 2003 9 16 AALA20030685 120030623A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217539A 49993 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROWS 24-26 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY FOR ROWS 24-26. SYTSEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030916001122003091600112EU 2003 9 16 AALA20020440 120030408A5246A2150407 HINGE AIRBUS300 A300B4605R 3930308EU FUEL PANEL BROKEN A AALAK NONE J WARNING INDICATION ININSP/MAINT 1 SW2140064 507 EN ROUTE MIA-SDQ - ON ARRIVAL DURNG WALK AROUND DETECTED FUELING PANEL DOOR CRACK ON AFT LOWER SECTION. REPLACED DOOR PARTS,(HINGE P/N A2150407, LATCH P/N ASNA2386). SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030916001162003091600116EU 2003 9 16 AALA20030884 120030821A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211473K 11515 LT OVERWING EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS IN LIGHT ASSY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030916001302003091600130WP 2003 9 16 GTIA030633 120030715A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 TEMP REPAIR INSTALLED AT FS 230 BETWEEN L16 AND 17. REMOVED EXISTING SKIN REPAIR. FORMED NEW SKIN SECTION. INSTALLED NEW SKIN SECTION. (M) 2L72 4F RTA6WE 20030916001472003091600147WP 2003 9 16 ARWA20030508 120030527A5313 FITTING DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE RT MLG WW CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 N/R 421. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR WHEEL WELL STATION 879, L-24R FITTING WITH CORROSION AND 3 INCH CRACK. REMOVED AND REPLACED FITTING OF R/H MAIN LANDING GEAR WHEEL WELL STA 879, L-24R IAW SRM 51-1-20D AND SRM 53-1-0. 2L74 4F4 F 4A25 1E8 20030916001552003091600155NM 2003 9 16 373PA0017 120030723A335020131A BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 SEVERAL OVERHEAD BIN EMERGENCY LIGHTS IN AFT SECTION OF AIRCRAFT WILL NOT COME ON. REPLACED BATTERY FOR AFT SECTION EMERGENCY LIGHTS. OPS CHECKS NORMAL IAW MM 25-60. 2L72 4F RTA16WE 20030916001572003091600157NM 2003 9 16 PCAA0307085 120030724A33501013079 LIGHT DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13846EX 326 DURING A ROUTINE MAINTENANCE VISIT 2 AFT FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. LIGHT ASSEMBLY PART NUMBER 10-1307-9 WAS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030917000352003091700035EA 2003 9 17 COW2003F00001 220030529A7320RSA7AA1 SERVO SCWZER269 269D 8059501EA LYC O360 HIO360* 41514EA ENGINE FUEL INOPERATIVE D C0WMO OTHER O OTHER NRNOT REPORTED 1 GL23103WP1 S1573 ON INITIAL TEST FLIGHT, AFTER INSTALLING ENGINE RECEIVED FROM OVERHAULER, ENGINE HAD UNUSUALLY HIGH CYLINDER HEAD TEMPERATURES AND RAN ROUGH. REMOVED AND REPLACED FUEL SERVEO (PRECISION AIRMOTIVE) WITH SERVICEABLE UNIT AND ENGINE POWER AND TEMPS FOUND NORMAL. FUEL SERVO THAT WAS REMOVED WAS OVERHAULED BY MFG. 1G71 3U3 O0 4H12 1E10 20030917000402003091700040EU 2003 9 17 0301393207 120030728A2910 LINE AIRBUS320 A320211 3930320EU RT WHEEL WELL LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01307US 106 THIRTY MINUTES INTO FLIGHT, LOST ALL HYDRAULIC FLUID IN YELLOW SYSTEM. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED LEAKING PARKING BRAKE LINE IN RIGHT WHEEL WELL. OPERATIONAL CHECK GOOD AND NO EVIDENCE OF LEAKAGE IN YELLOW SYSTEM. 2L72 4F RTA28NM 20030929001382003092900138 2003 9 29 0301696718 420030904A2210 COMPUTER BOEING747 747251F 1384898NM YAW DAMPER INOPERATIVE A NWAAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CLCLIMB 1 GL01618US 21122 DURING CLIMB THE LOWER YAW DAMPER LIGHT ILLUMINATED BRIEFLY AND THE AIRCRAFT WAS DIFFICULT TO CONTROL IN HEADING. SLOWED AIRCRAFT TO 270 KNOTS AND TURNED OFF LOWER YAW DAMPER BUT AIRCRAFT WAS STILL DIFFICULT TO CONTROL IN HEADING. AIRCRAFT DECLARED AN EMERGENCY DUMPED 20,000 LBS OF FUEL AND RETURNED TO JFK AND AFTER LANDING EIGHT TIRE FUSES BLEW. REPLACED UPPER AND LOWER RUDDER POWER CONTROL UNITS BOTH YAW DAMPER COMPUTERS AND EIGHT TIRE ASSEMBLIES. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20031021001292003102100129NM 2003 10 21 AALA20030948 120030903A335002011991008 SOCKET BOEING757 757223 1384957NM CABIN DEFECTIVE A K NONE L NO TEST ININSP/MAINT 1 SW21642AA 24600 EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 26DEF. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021001402003102100140NM 2003 10 21 AALA20030564 120030514A3350 CONNECTOR BOEING757 757223 1384957NM CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21646AA 24604 ATL - DURING OVERNIGHT MAINTENANCE, INTERIOR OVERWING EMERGENCY EXIT LIGHT AND AISLE LIGHT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONNECTOR AND REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021001952003102100195NE 2003 10 21 AALA20031028 220030918A7320 REGULATOR FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY65015 54557NE NR 2 ENGINE FAILED A AALAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 SW211409B 11367 ORD - FLT 1988 - AIRCRAFT EN ROUTE XNA TO ORD, THROTTLE STUCK IN THE CRUISE POWER SETTING. EMERGENCY DECLARED AND SHUTDOWN NR 2 ENGINE PRIOR TO LANDING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE FUEL FLOW REGULATOR. LEAK AND SYSTEM GROUND CHECKED NORMAL. (M) 2L72 4F4 FRT E25NE 20031021002022003102100202NM 2003 10 21 AALA20030498 120030426A3350P4010051112 CHARGER BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21183AN 29593 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM ROW 16 AFT INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002032003102100203NM 2003 10 21 AALA20030620 120030601A3350P2010031302 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21183AN 29593 LAX - DURING OVERNIGHT CHECK, RIGHT AFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002072003102100207NM 2003 10 21 AALA20030505 120030428A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21699AN 27051 MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT PATH LIGHTING AT SEAT 4E INOPERATIVE. SECURED EMERGENCY EXIT PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002322003102100232SO 2003 10 21 SIMA200326805 120030920A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 ABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 22, CHAPTER 53-24-02 AND EMB IC2003-145/3093A. (M) 2L72 4F RTT00011AT 20031021002332003102100233SO 2003 10 21 C2XA03SH334 120030920A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031021002352003102100235EU 2003 10 21 RAIA00309242 120030915A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03574HK 41093 MX-STL- FRONT HALF OF FLOOR EMERGENCY LIGHTS OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2L72 4T RTA41NM 20031021002372003102100237WP 2003 10 21 GTIA030687 120030924A2560 SMOKE GOGGLES DOUG DC9 DC983 3022083WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL31814NK 49619 DTW - FIRST OFFICERS SMOKE GOGGLES CRACKED. REPLACED FIRST OFFICERS SMOKE GOGGLES. (M) 2L72 4F RTA6WE 20031021002382003102100238SO 2003 10 21 C2XA03SH335 120030920A532013500079001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK THE LT SILL BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031021002512003102100251WP 2003 10 21 GTIA030698 120030904A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND SEAT TRACKS LEFT INBOARD FROM STATION 1079-1174, STATION 1212-1250, STATION 1271-1309, CORRODED. REMOVED SEAT TRACK FROM STATION 1079 TO 1309. FABRICATED NEW TRACK. INSTALLED NEW TRACK. DRILLED AND LOCATED NEW SPLICES STATION1070, 1130 AND 1220 AND INSTALLED SPLICES. (M) 2L72 4F A6WE 20031021002642003102100264NM 2003 10 21 03FDEA01593 120030919A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 FUSELAGE SKIN DENTED AT APPROX STA 1130 STR 18R. 2L73 4F RTA3WE 20031021002732003102100273EU 2003 10 21 2750301 120030912A3350 BULB SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A NSVAK NONE O OTHER ININSP/MAINT 1 EA27252CJ 340B252 EMERGENCY LIGHT OUT AT SEAT 11F, REMOVED AND REPLACED BULB, OPS CHECKED GOOD. 2L72 4T RTA52EU 20031021002972003102100297 2003 10 21 GLBA2003135 420030919A61228210410 GOVERNOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE PROPELLER MALFUNCTIONED A GLBAO OTHER O OTHER NRNOT REPORTED 1 NM03255GL17 UE255 RT PROP STARTS TO FEATHER WHEN POWER LEVER IS BROUGHT BACK, REMOVED AND REPLACED PROP GOV. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030930000242003093000024WP 2003 9 30 03FDEA01466 120030909A5753ARC0503 HINGE BRACKET DOUG MD10 MD1010F WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 RT OUTBOARD FLAP- OB HINGE BRACKET CORROSION REPAIR (P/N ARC0503) COMPLIED WITH EA 8-5750-72274_WINGS RT O/B FLAP-O/B HINGE BRACKET CORROSION REPAIR P/N ARC, 0503 CLOSED ON 09/09/2003 FEDEX NR S00018 2L73 4F RTA22WE 20030930000262003093000026NM 2003 9 30 03FDEA01464 120030906A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200, CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 MAIN DECK CARGO COMPT. FLOOR TRACK AT STA 635, X = 27.5 FOUND CRACKED APPROX. 3 INCHES LONG. 2L73 4F RTA22WE 20030930000312003093000031EU 2003 9 30 MALA030384 120030820A33507239050512 CONNECTOR SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15435XJ 340B435 DURING PREFLIGHT FROM LOG PAGE 1179023 EMERGENCY LIGHTS ARMED AND GENERATOR OR EXTERNAL POWER ON-LINE. EMERGENCY LIGHTS CWP ILLUMINATES AND CABIN EMERGENCY LIGHTS FLICKER ON AND OFF. SLIGHT OZONE SMELL NOTED BY CREW, COULD NOT REPEAT. MAINTENANCE FOUND PIN C ON 20LN, 21LN, AND FOUND 28VDC AT PIN C ON 23LN, & 24LN DISC 20: REPLACED EMERGENCY OVERHEAD PANEL PN 7239050-512. OPS CHECK GOOD. 2L72 4T RTA52EU 20030930000422003093000042NM 2003 9 30 2003UALA00661 120030829A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29303UA 23644 FUSELAGE SKIN DENTED. STA 318 AT STR 24R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE SKIN AT LAP JOINT. FABRICATED DOUBLER AND FILLERS. 2L72 4F4 FRTA16WE E2GL 20030930000512003093000051EU 2003 9 30 MALA030387 120030823A5520 RETAINER SAAB SF340 340B 7860101EU BEARING FAILED A MALAO OTHER O OTHER DEDESCENT 1 GL15360PX 340B220 DURING DESCENT INTO MSP ON FLIGHT 2915, ELEVATOR FLUTTER INFLIGHT. SLOWED TO 180 KNOTS AND IT STOPPED, SPEED BACK TO 185 AND IT STARTED AGAIN WITH FLAPS 15, FLUTTERED AGAIN AT 165 KNOTS. SAME INDICATION WITH AP ON OR OFF. TRIMS APREARED NORMAL. MAINTENANCE FOUND LT ELEVATOR TRIM TAB INBOARD BEARING RETAINER BROKEN CAUSING TRIM TAB TO BE LOOSE/FLUTTERING. REMOVED LT ELEVATOR TRIM TAB AND REMOVED AND REPLACED BEARING AND RETAINER IAW AMM 20-41-00-2. REINSTALLED LT ELEVATOR TRIM TAB IAW AMM 27-32-25-4, PERFORMED ELEVATOR TRIM TAB ELECTRICAL FUNCTION TEST IAW AMM 27-32-00-5. TEST GOOD, SECURITY CHECK GOOD. 2L72 4T RTA52EU 20030925000922003092500092NM 2003 9 25 03FDEA01450 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING I/B FLAP O/B HINGE PIVOT I/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71784. 2L73 4F RTA22WE 20030925000932003092500093NM 2003 9 25 2003UALA00682 120030805A5751113W72121 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE AILERON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29772UA31818 26930 LT & RT AILERON INBD AND OUTBOARD PCU FITTINGS CRACKED. LT AND RIGHT AILERONS WERE REPLACED. 2L72 4F4 FRTT0001SE E46NE 20030925000982003092500098EU 2003 9 25 DXTA200300119 120030917A3097 WIRE BRAERO1000 HAWKER1000 7450005EU WINDSHIELD HEAT BURNED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07552QS 259052 DURING FLIGHT FROM PHL TO 3J7 CREW NOTICED A STRONG BURNING ODOR IN COCKPIT AND CABIN, DIVERTED TO GSP AND LANDED SAFELY. - INSPECTED COCKPIT AND FOUND THE LT WINDSHIELD A SCREEN WIRES TO STATIC FILTER CHAFED AND BURNED. 2L72 4F RTA3EU 20030926000232003092600023CE 2003 9 26 53738 120030818A5531 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07UE178 UE178 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STABILIZER, THE RIB FLANGES AT CANTED STAB STA. 39.289 AND STAB STA. 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IAW STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03 2L72 4T RTA24CE 20030926000342003092600034NM 2003 9 26 03FDEA01393 120030808A5753ARC70541 SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBD FLAP VANE NR 2 ( FROM INBD) TEE FITTING ATTACH HOLE CORRODED. CORROSION AT THE FITTING ATTACH HOLE RT OUTBD FLAP VANE NR 2 REMOVED AS PER FEDEX EA 1-5750-63189, WINGS: RT OUTBOARD VANE-TEE FITTING REWORK. 2L73 4F RTA22WE 20030929000602003092900060EA 2003 9 29 COMA0360403 120030828A712060135006 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 CRACK ON ENGINE SUPPORT BEAM LOWER WEB AT FWD I/B CORNER OF LT ACCESS PANEL. REPAIRED IAW REO 601R-53-61-366. 2L72 4F RTA21EA 20030929000642003092900064EU 2003 9 29 AWXA200301014 120030818A5414D54530052200 SKIN AIRBUS320 A320231 3930325EU NR 1 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-03 CHECK CORROSION WAS FOUND ON NR 1 PYLON TRAILING EDGE FAIRING INBOARD SKIN, PYLON STA 8370 TO 9278. MAINTENANCE REMOVED CORROSION ON NR 1 PYLON TRAILING EDGE FAIRING INBOARD SKIN AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN PYLON STA 8370 TO 9278; UPON FURTHER INSPECTION FOUND CRACKED LOWER RIB; REMOVED CRACKED RIB; FABRICATED NEW REPLACEMENT SKIN AND LOWER RIB; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 PG 7-12, FIG 2. 2L72 4F RTA28NM 20030930000802003093000080WP 2003 9 30 ABXA030353 120030818A53209922042505 FLOOR SUPPORT DOUG DC9 DC932F 3022067WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 LEFT FLOOR SUPPORT STRUT TO FRAME ATTACH FITTING CRACKED STA. 237 BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED SUPPORT IAW DC-9 SRM. 2L72 4F A6WE 20030930000832003093000083WP 2003 9 30 ABXA030346 120030814A532099100649 STRUCTURE DOUG DC9 DC932F 3022067WP RT WHEEL WELL CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 RIGHT WHEEL WELL UPPER AFT CORNER STA. 756, BUTT LINE '0' - BUTT LINE '4', CORROSION ON KEEL ANGLE AND BULGES UNDER RETAINER. REPAIRED AREA IAW REA D953-48136MR. REMOVED PREVIOUS REPAIR FROM AFT UPPER KEEL ANGLE, REPAIRED IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030930001022003093000102NM 2003 9 30 PCAA0309105 120030905A291082920010307 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM BROKEN A PCAAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA13979HA 373 WHILE ON DEICING PAD CREW REPORTED THAT A HYDRAULIC LINE WAS LEAKING IN THE CABIN AT SEATS 5DF AND 6DF. EMERGENCY WAS DECLARED. FLIGHT ATTENDANT AND ONE PASSENGER WERE TAKEN TO HOSPITAL DUE TO AFFECT OF HYDRAULIC FLUID IN THE CABIN. MAINTENANCE REPLACED A HYDRAULIC LINE FOR THE NOSE LANDING GEAR SYSTEM. ALSO REPLACED WERE AFFECTED INNER CABIN WINDOWS, CARPETING, AND PASSENGER SERVICE UNITS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930001042003093000104SO 2003 9 30 C2XA03SH320 120030909A21508152403 ACM EMB 145 EMB145ER 3260211SO SEIZED A C2XABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27159483917 3802 145056 DURING FLIGHT CREW DETECTED SMOKE IN CABIN AND COCKPIT. CREW INITIATED EMERGENCY PROCEDURES AND PERFORMED EMERGENCY DESCENT. AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND NUMBER ONE AIRCYCLE MACHINE SEIZED. MAINTENANCE REMOVED AND REPLACED NUMBER ONE AIRCYCLE MACHINE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030930001122003093000112WP 2003 9 30 ABXA030361 120030906A2120 ODOR DOUG DC9 DC941 302207NWP COCKPIT DETECTED A ABXAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL23954AX 47612 A FAINT BURNING ODOR DETECTED ON DESCENT. INSPECTED ELECTRONIC COMPARTMENT, ENGINE CONTROL UNITS FOR LOOSE CONNECTOR AND ACCESSORIES FOR SECURITY. NO DEFECTS NOTED. 2L72 4F A6WE 20030930001132003093000113NM 2003 9 30 03FDEA01488 120030907A5754 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB CRACKED. RT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. 2 & SRM 51-35-01 VOL. 2 2L73 4F RTA22WE 20030930001172003093000117NM 2003 9 30 03FDEA01483 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG HOLE CORRODED. 2L73 4F RTA22WE 20030930001182003093000118NM 2003 9 30 03FDEA01482 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) ACTUATOR MOUNT O/B LUG HOLE CORRODED. 2L73 4F RTA22WE 20030930001302003093000130NM 2003 9 30 F3LA200300128 120030909A5320654659258 CHANNEL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT APPROX. STA. 727C, RBBL 3. REPLACED DAMAGED FLOOR SUPPORT CHANNEL FROM STA. 727 - 847, RBBL 3, IAW SRM 53-60-53, 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20031001000042003100100004NM 2003 10 1 QXEA200301072 120030830A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 FUSELAGE SKIN UNDER ATC ANTENNA HAS CORROSION AND PITTING AT STATION X257.7. REPAIRED IAW DHC-8 SRM 51-00-06, 51-00-04 AND HORIZON AIR EA 2-53-481. 2H72 4T RTA13NM 20031001000122003100100012WP 2003 10 1 ARWA20030902 120030905A5420 WEB DOUG DC8 DC861 3021952WP NR 1 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1929UA 46159 NR 188. DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 1 PYLON BETWEEN STATION YOP NR 226 AND STATION YOP NR 243 UPPER WEB DOUBLER WITH CRACKS. CORRECTIVE ACTION: 2L74 4F 4A25 20031001000132003100100013WP 2003 10 1 ARWA20030903 120030905A5415 FITTING DOUG DC8 DC861 3021952WP NR 3 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1929UA 46159 DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON UPPER SECTION, FRONT SPAR AND FOOT STOOL SPLICE FITTING WITH 3 INCH CRACK. 2L74 4F 4A25 20031001000372003100100037WP 2003 10 1 UPS03841180 120030807A53404758514502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, AFT CARGO PIT AT FS 1140-1150 BETWEEN L32R-L33R INTERCOSTAL ATTACK F ITTING IS CRACKED VERIFIED CRACK IAW DYE PENETRANT TEST IAW DPS 4.707.1. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. REC'D, LOCATED, AND DRILLED NEW FIT TING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20031001000412003100100041WP 2003 10 1 UPS03841186 120030808A53403779498502 FITTING DOUG DC8 DC873F 302199FWP FUSELAEG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, CABIN STA 857, L19R FITTING BEHIND INTERCOSTAL CRACKED. REMOVED FITTING FROM STA 857, L19R FOR REPLACEMENT, RECEIVED SUPPORT FITTING P/N 3779498-502. LOCATED AND DRILLED IAW DC8 SRM 51-3-2. IN STALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20031001000452003100100045WP 2003 10 1 UPS03841190 120030811A522038884062 FITTING DOUG DC8 DC873F 302199FWP EMERGENCY EXIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, RT FWD TYPE 1 DOOR HAS A CRACKED FITTING BELOW THE MOST FORWARD LOWER ST OP FITTING AT AFT FRAME OF THE FORWARD WEB SECTION REMOVED FITTING RT EMERGENCY EXIT DOOR LOWER CORNER. REMOVED RT EMERGENCY EXIT DOOR. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2 INSTALLED FITTING IAW DC8 SRM 51-1-20D, 51-1-21, 51-3-0. 2L74 4F RT4A25 20030926001142003092600114NM 2003 9 26 2003UALA00647 120030824A3350 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT SHORTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29370UA 24539 FLOOR ESCAPE PATH LIGHTING INOP ROW 17 AND BACK. REPAIRED SHORTED LIGHT STRIP. 2L72 4F4 FRTA16WE E2GL 20030929000352003092900035NM 2003 9 29 03FDEA01430 120030902A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING O/B FLAP O/B HINGE (A/C SIDE) O/B ACTUATOR ATTACH BORE FOUND CORRODED. 2L73 4F RTA22WE 20030929000532003092900053NM 2003 9 29 PCAA0309104 120030903A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13831EX 160 DURING ROUTINE MAINTENANCE VISIT, AN EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 9DF. A WIRE WAS FOUND BROKEN AT THE LIGHT ASSEMBLY. A NEW FLOOR LIGHT ASSEMBLY WAS RESPLICED INTO WIRING. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031021002982003102100298NE 2003 10 21 DHL2003809002 220031008A73218063211 MEC DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 3 ENGINE MALFUNCTIONED A DHLAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SO01604AL 46047 NR 3 ENG FAILED 3-5 MIN AFT SETTING CRUISE THRUST (0938Z) ENG LOST POWER SLOWLY. PERFORMED ENG FAILURE CHECKLIST ATTEMP RESTART, NO FUEL FLOW, OR EGT INDICATION, BOOST PUMP 21 PSI. ENG WINDMILL TIME 1 HR 22 MIN. OIL PRESS DROPPED TO 0 AFT APPROX 10-15 MIN AFT ENG FAILURE. FOUND 4 EA BOLTS ON BOOST PUMP FEED LINE LOOSE. PERFORMED PRESSURE CHECK ON FUEL LINE FROM IN TANK BOOST PUMP TO NASH PUMP ON NR 3 ENG. NO DEFECTS FOUND. RETIGHTENED BOLTS ON BOOST PUMP. BOROSCOPE INSPECTION OF NR 3 ENG BOOSTER, HPC 3, 5, & 9, COMBUSTOR HPT & LPT. REINSTALLED ALL REMOVED PLUGS. REMOVED & REPLACED NR 3 ENG MEC, OPS AND LEAK CHECKED. RIGGED NR 3 ENG MEC, VSV AND VBV. NO LEAKS. PARAMETERS WITHIN LIMITS. 2L74 4F4 FRT4A25 E2GL 20031021003032003102100303NM 2003 10 21 MWEA030379 120030922A5347593056675 SEAT TRACK DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 AFT CABIN NR 3 SEAT TRACK HAS CORROSION FROM STATION 1304-1309. BLENDED CORROSION AND REMOVED AND REPLACED SEAT TRACK. 2L72 4F4 FRTA6WE E2EA 20031022000042003102200004NM 2003 10 22 MWEA030384 120030922A532099365347 SUPPORT DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 PASSENGER DOOR SILL PAN SUPPORT CORRODED AT STATION 157-200. FABRICATED AND INSTALLED SUPPORT . 2L72 4F4 FRTA6WE E2EA 20031022000062003102200006NM 2003 10 22 MWEA030386 120030922A5347993061223 SEAT TRACK DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 AREA OF CORROSION BETWEEN STATION 1117-1136 OUTBOARD OF RT OUTER SEAT TRACK. REMOVED CORROSION FABRICATED AND INSTALLED WEB SECTION. 2L72 4F4 FRTA6WE E2EA 20031022000192003102200019EU 2003 10 22 AWXA200301069 120030908A5315D53472090004 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF Y1292 FLOORBEAM BETWEEN FR 65-66. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRODED Y1292 FLOORBEAM BETWEEN FR 65-66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00, PG 5-6 TABLE 1. 2L72 4F RTA28NM 20031022000202003102200020EU 2003 10 22 AWXA200301070 120030908A5347D53472209245 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF Y1292 SEAT TRACK AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED Y1292 SEAT TRACK FR 64-66; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-49-00, PG 5-6 TABLE 1. 2L72 4F RTA28NM 20031022000232003102200023EU 2003 10 22 AWXA200301073 120030907A5321D5361060500100 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF R-1 DOOR SILL FLOOR PANEL (222FF), AT INBOARD AFT CORNER FR 20. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL ASSEMBLY IAW T/C C1D25306. 2L72 4F RTA28NM 20031022000352003102200035NM 2003 10 22 P5CA0300944 120030921A74109238M66P08 EXCITER BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 4 ENGINE INOPERATIVE A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23355MC 23395 530439 NR 4 ENG START NO INGITION. REPLACED NR 4 ENG NR 1 EXCITER BOX: DEFERRED NR 4 ENG NR 2 IGNITION SYS. 2L74 4F4 FRTA20WE E23EA 20031022000472003102200047NM 2003 10 22 QXEA200301149 120030912A5410 SHROUD BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX- NR 2 NACELLE RT HAND SIDE, NACELLE TO FLAP SHROUD DIAPHRAGM IS CRACKED AT STATION XN200.06. REPAIRED IAW Q400 SRM 51-40-10, 51-42-05. 2H72 4T4 TRTA13NM E00062EN 20031022000582003102200058NM 2003 10 22 QXEA200301159 120030917A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 LOWER FUSELAGE SKIN EXTERIOR IS NICKED BETWEEN LEFT HAND STRINGERS 32 AND 33 11.5 INCH AFT OF X32.4. REPAIRED IAW Q400 SRM 51-26-10, 51-00-04, 51-00-02, 51-25-05-370-801 AND RD 8/4-53-666. 2H72 4T4 TRTA13NM E00062EN 20031022000732003102200073NM 2003 10 22 03FDEA01549 120030916A5320A5A7114521 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 POSSIBLE CRACKS AT STRINGER SPLICE 39R STA 1540 AT TRANSVERSE SPLICE RT TUNNEL. CTR CARGO STA 1540 STR 39R STRINGER CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG N5A6774 AND SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20031022000752003102200075NM 2003 10 22 03FDEA01442 120030830A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING- O/B FLAP I/B HINGE (FLAP SIDE) UPPER ATTACHMENT BORE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) UPPER ATTACHMENT BORE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71894. WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031022000762003102200076NM 2003 10 22 03FDEA01441 120030830A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 O/B FLAP I/B HINGE (FLAP SIDE) LOWER ATTACHMENT BORE FOUND CORRODED. O/B FLAP I/B HINGE (FLAP SIDE) LOWER ATTACHMENT I/B & O/B BORES. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71894. WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031022000832003102200083 2003 10 22 UPS03641380 420031008A3446 INDICATOR BOEING767 767300 1385204NM GE CF6 CF680 30025NE CAPT'S IVSI/TCASINOPERATIVE A IPXAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 SO01331UP 27757 INSPECTION TYPE: ETOP DIVERSION, CAPTIANS VERTICAL SPEED FLAG IN VIEW ALT AIR DATA DOESN'T CORRECT. (TCAS FLAG IN VSI ALSO IN VIEW) REPLACED CAPTAIN'S VSI PER MM 34-22-06-4 & 34-45-00-5. OPS CHK NORMAL. 2L72 4F4 FRTA1NM E13NE 20031022000972003102200097CE 2003 10 22 9903N76CK 120030910A243530B3749 STARTER GEN LEAR 25 25 5170506CE LEFT ENGINE VIBRATION E KC8AO OTHER O OTHER NRNOT REPORTED 1 GL2376CK 25020 AIRCRAFT DEVELOPED VIBRATION. REPLACED LT STARTER GENERATOR WITH SERVICEABLE REPAIRED UNIT, GROUND OPERATIONAL CHECK GOOD. NO RECOMMENDATION FOR PREVENTION. 2L72 4J A10CE 20031022001022003102200102CE 2003 10 22 DXTA200300125 120030922A7603 BELLCRANK CESSNA560 560XL 2076702CE PWA 545 PW545A NE THROTTLE LINKAGEMISINSTALLED E DXTAK NONE RJ PARTIAL RPM/PWR LOSS WARNING INDICATION ININSP/MAINT 1 GL07690QS 5605090 DURING ENGINE RUN FOR POST INSTALLATION OF MFG SB 560XL7603R1 (THROTTLE CUT OFF IMPROVEMENT) FOUND ENGINES FAILED TO STAY IN FLIGHT IDLE, WHEN POWER IS REDUCED TO IDLE, ENGINES WOULD GO TO CUT OFF, INSPECTED THROTTLE LINKAGE AND FOUND THE BELLCRANK ASSEMBLIES PN 66610381 AND -6 WERE INSTALLED IN OPPOSITE POSITIONS, REMOVED THE BELLCRANKS AND FOUND NO PART NUMBER STAMPED ON BELLCRANKS. RE POSITIONED BELLCRANKS, RE-RIGGED THE THROTTLE AND PERFORMED ENGINE RUN, AL CHECKED GOOD IAW MFG MM CH 72-11-00 AND CESSNA SB 560XL-76-03R1. 2L72 4F4 FRTA22CE E00059EN 20031021002762003102100276NM 2003 10 21 QXEA200301147 120030914A5210 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA PAX DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 MAIN CABIN DOOR OUTER SHELL HAS A SMALL DENT AT UPPER FORWARD CORNER. REPAIRED IAW Q400 SRM 51-20-10, 51-25-05 AND RD 8/4-53-666. 2H72 4T4 TRTA13NM E00062EN 20031022000282003102200028NM 2003 10 22 AWXA200301078 120030921A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 23 LT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031022000792003102200079WP 2003 10 22 ABXA030366 120030908A53203643758503AX FITTING DOUG DC9 DC9* WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 FITTING IN RT WHEEL WELL DAMAGED (CRACKED). FABRICATED NEW PART REF: ST-9300-01 AND PARTS FABRICATION RECORD WO 600179300 AND IAW SRM. 2L72 4F A6WE 20031022000862003102200086 2003 10 22 AWXA200301198 420031009A3417250062725 GEAR HONEYWELL BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE AIRSPEED IND WORN A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28907AW 85100937 22691 ON TAKEOFF ROLL, THE CAPTS AIRSPEED IND FAILED. VMO AIRSPEED MACH FLAGS IN VIEW, & AIRSPEED POINTER OFF SCALE & INOP IND VIEW, REJECTED TAKEOFF BELOW 100 KTS. MAINT PERFORMED A BITE TEST OF LT ADC IAW BMM. R & INSP CONNECTOR TO CAPTS AIRSPEED IND, NO DEFECTS NOTED, OPS CHECK GOOD. A FOLLOW-UP WRITTEN TO REPLACE MACH SPEED IND. MAINT R & R CAPTS AIRSPEED IND IAW BMM, OPS CHECK WAS GOOD. FUNCTIONAL TEST OF MACH SPEED IND CONFIRMED FAILURE OF UNIT FOR FAILING SLEW RATE TEST. TEARDOWN REVEALED A BROKEN TORSION SPRING & AIR SPEED COUNTER, ALSO FOUND RESOLVER & AIR SPEED BACK GEARS WORN OUT. REPLACED DAMAGED PARTS, CLEANED CONTAMINATION FROM GEAR TRAIN AND BEZEL GLASS, CALIBRATED, AND PERFORMED FUNCTIONAL TEST. 2L72 4F4 FRTA2NM A12EU 20031022001172003102200117NM 2003 10 22 F3LA200300144 120030923A5320 STRIP BOEING737 73736E 138443ANM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED CAP STRIP BETWEEN STA. 344 AND 360, RBL 12 TO 24, CRACKED. FABRICATED AND INSTALLED REPLACEMENT CAP STRIP IAW SOPM 51-40-02 AND DRAWING 65C33971. 2L72 4F4 FRTA16WE E2GL 20031022001212003102200121NM 2003 10 22 QXEA200301171 120030921A2810 POPPET VALVE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09374PH 528 PDX- ON FLIGHT 2136 SMALL FUEL LEAK NEAR HINGE POINT OF REFUELING DOOR. FOUND POPPET VALVE UNDER FUEL CAP NOT SEATED CORRECTLY. RESEATED VALVE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031022001392003102200139EU 2003 10 22 AWXA200301081 120030917A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 221 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHT SYSTEM, FAULTS WERE FOUND AT TEST PANEL. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031023000012003102300001NM 2003 10 23 CALA0300552 120030922A7120310A20343 LINK ASSY BOEING737 737824 13844BZNM GE CFM56 CFM56* 13802NE NR 1 ENGINE MISINSTALLED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 876105 A MAINTENANCE TECHNICIAN NOTICED THE FIRE SEALS THAT SADDLE THE PYLON WERE NOT ALIGNED PROPERLY ON THE NR 1 ENGINE WHILE THE AIRCRAFT WAS IN ROUTINE MAINTENANCE AT IAH. FURTHER INVESTIGATION FOUND THAT THE AFT ENGINE MOUNT CENTER LINK ASSEMBLY HAD BEEN INSTALLED BACKWARDS. THIS ENGINE HAD NOT BEEN REMOVED SINCE INSTALLED AT THE MANUFACTURER. THE SIGNIFICANCE OF THIS FINDING IS THAT THE AIRWORTHINESS DIRECTIVE(REFERENCE AD 2003-03-01) WAS EXPLICIT IN INSTRUCTING INSPECTIONS OF THE AFT CENTER LINK ON ENGINES THAT HAD BEEN REMOVED/INSTALLED SINCE DELIVERY FROM THE MANFACTURER. THE NR 1 ENGINE WAS REMOVED AND REPLACED IAW WORK CARD 29-7100-1-9800. 2L72 4F4 FRTA16WE E2GL 20031023000042003102300004EA 2003 10 23 JBXA03017 120030923A2710 AILERON CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF341A NE LEFT FROZEN A JBXAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 SO05652ML 7036 FLIGHT 5119 FROM PWM TO DCA PILOT REPORTED LT AILERON WAS FROZEN. PERFORMED DISCONNECT. ON DESCENT PILOTS RECONNECTED AND NO FURTHER PROBLEMS WERE REPORTED. PROBABILITY OF ICE ON CONTROL SURFACE OR CABLES. AIRCRAFT LANDED UNEVENTFULLY. MX PREFORMED FUNCTIONAL TEST OF AILERON SYSTEM. PERFORMED FUNCTIONAL FLIGHT TEST TO RDU. NO DEFECTS NOTED. IAW CRJ AMM 27-11-00 2L72 4F4 FRTA21EA E15NE 20031023000192003102300019SO 2003 10 23 C2XA03BT095 120030922A32347455501 LEVER EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SW27155553167 145594 CREW REPORTED, "ON DEPARTURE, DURING GEAR RETRACTION RECEIVED LANDING GEAR DISAGREEMENT MESSAGE AND LANDING GEAR DID NOT RETRACT. (AIR RETURNED TO EWR)"....MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM NR 32-32-02. OPS. AND GEAR (RETRACTION CHECK) SWING GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20031023000352003102300035WP 2003 10 23 UPS03841244 120030825A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, WHILE ACCOMPLISHING WORK TASK AND REMOVAL OF SHUTTER BOX ON NR 687218. FOUND LOWER AFT SKIN CUT OUT CRACKED. C/W EO DC-8-5330-4732D, HFEC IAW NDBDM 06-10-01.0001, NO CRACKS AROUND CUT OUT,FABBED FILLER AND DOUBLER FROM 2024T3 .100 TREATED AND PRIMED PARTS AND SKIN, INSTALLED COUNTERSINK WASHERS IAW EO DC8 5330-4732D,INSTALLED REPAIR PARTS IAW EO DC8-5330-4732D. 2L74 4F4 FRT4A25 E2GL 20031023000372003102300037WP 2003 10 23 UPS03841259 120030923A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. OPS CHECK GOOD IAW MM 33-50. 2L74 4F4 FRT4A25 E2GL 20031023000442003102300044EU 2003 10 23 AWXA200301092 120030913A5320D5347112420000 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON SHEAR PLATE BETWEEN FR 69-70, LBL 49. MAINTENANCE REMOVED CORRODED SHEAR PLATE BETWEEN FR 69-70, LBL 49; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-44-11, PG. 24-25, AND A24-A26, FIG. 9, & 61. 2L72 4F RTA28NM 20031023000452003102300045EU 2003 10 23 AWXA200301093 120030914A5321D5367175300800 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK FOUND FLOOR PANEL 74L DELAMINATED. MAINTENANCE REMOVED FLOOR PANEL 74L; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG D536-71753; INSTALLED NEW PANEL IAW A320 SRM 53-02-00, PG. 231, 233-236, FIG. 9. 2L72 4F RTA28NM 20031023000522003102300052EA 2003 10 23 SWIA200312442 120030921A2740 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07464SW 7827 STAB CH 1 WILL NOT RE-ENGAGE/RUNNING EITHER TRIM DISENGAGED CH. 2. REMOVED AND REPLACED HSTA IAW MM CH 27-42-01. OPS CHECK GOOD. PN OFF: 601R92305-3 SN OFF: 1095 2L72 4F RTA21EA 20031023000562003102300056EA 2003 10 23 SWIA200312446 120030920A2750860D10018 ECU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07445SW3078 3078 7651 ''FLAPS FAIL'' CAUTION DURING CRUISE FLIGHT. NO FLAP LANDING IAW QRH. REMOVED AND REPLACED FECU IAW CL 600 MM 27-51-05. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031023000602003102300060EA 2003 10 23 QXEA200301177 220030921A7200 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA NR 1 OVERHEATED A QXEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 NM09409QX 4051 ON FLIGHT 2289 AIRCRAFT RETURNED TO FIELD DUE TO, ON INITIAL CLIMB ITT OBSERVED AT 848 DEGREES WITH RED NEEDLE ON NR 1 ENGINE. FIELD ELEVATION 4453, TEMPERATURE 0 DEGREES AND ALTIMETER 30.12. AIRCRAFT LANDED SAFELY. INTEROGATED CDS AND FOUND NR 1 ENGINE ITT 855.4 FOR 24 SECONDS. THIS IS WITHIN LIMITS IAW Q400 AMM 05-11-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20031023000682003102300068SO 2003 10 23 C2XA03SH352 120030924A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 -DURING C CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031023000692003102300069SO 2003 10 23 C2XA03SH353 120030924A541214526850403 FIREWALL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 SHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO CRACKED AT THE TOP VERTICAL REINFORCEMENT. MAINTENACE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH AND DOUBLER REPIAR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031027000162003102700016NE 2003 10 27 COMA0360426 220030921A7200CF343A1 POWERPLANT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT FAILED A COMAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO01937CA11090 7044 807539 FLIGHT 5014 AT APPROXIMATELY 80 KTS DURING T/O ROLL THE RT ENGINE SPIKED TO 998 DEGREES C, WITH RAPID RPM DECREASE, ABORTED T/O AND RETURNED TO THE GATE. REPLAED THE RT ENGINE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20031027000252003102700025EU 2003 10 27 AWXA200301101 120030913A5411D5463046220200 ANGLE AIRBUS320 A320232 3930326EU NR 2 NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK A 1.0625 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON INBOARD ANGLE AT RIB 7. MAINTENANCE CUTOUT CRACK ON NR 2 ENGINE PYLON INBOARD ANGLE AT RIB 7; FABRICATED A REPAIR SPLICE, FILLER AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 54-52-12, PG. 217-220, AND 223-224, FIG. 204. 2L72 4F RTA28NM 20031027000312003102700031EU 2003 10 27 AWXA200301107 120030922A5411D5453003420200 RIB AIRBUS320 A320232 3930326EU NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK A .25 INCH CRACK WAS FOUND ON NR 1 ENGINE PYLON AFT FIXED FAIRING RIB 13. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PYLON AFT FIXED FAIRING RIB IAW A320 SRM 51-42-11 PG 21-22 FIG 8, AND SRM 51-42-11 PG 7-12 FIG 2 & 3. 2L72 4F RTA28NM 20031027000362003102700036NM 2003 10 27 CALA0300555 120030925A5330 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND TWO DENTS IN AFT FUSELAGE SKIN FROM STA 934-943 BETWEEN S23L AND S24L. A REPAIR WAS INSTALLED IAW SRM 53-00-01. 2L72 4F4 FRTA16WE E2GL 20031027000472003102700047NM 2003 10 27 03FDEA01632 120030924A2613 OVERHEAT LOOP BOEING727 727200 138407ENM KEELBEAM INOPERATIVE A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25492FE 21530 LOWER AFT BODY OVERHEAT LIGHT ON IN CRUISE FLIGHT (35,000) OVERHEAT SELECTOR SWITCH UTILIZED = KEELBEAM LIGHT STAYED ON. COMPLETED QRH PROCEDURE. RIGHT PACK AND NR 3 BLEED CLOSED. LIGHT EXTINGUISHED. REMOVED AND REPLACED KEELBEAM LOOP PER MM 26-14-001-2. OPS CK NORMAL, NO LEAKS NOTED IN AREA. PART- KEEL BEAM LOOP P/N 35548-4-255. 2L73 4F RTA3WE 20031021002242003102100224EU 2003 10 21 F3LA200300136 120030915A335032146210 POWER SUPPLY AIRBUSA318 A318111 EU EMERGENCY LIGHT INOPERATIVE A F3LAO OTHER O OTHER NRNOT REPORTED 1 NM03803FR 2017 FLIGHT CREW REPORTED SEAT BELT/NO SMOKING LIGHTS AND FWD GALLEY EXIT SIGNS INOPERATIVE. REPLACED EPSU IAW MM 33-51-13-04. 2L72 4F RT 20031021002452003102100245SO 2003 10 21 C2XA03SH340 120030921A531514521700003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 SHV-DURING C CHECK THE LEFT FLOORBEAM BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031022000432003102200043EA 2003 10 22 SWIA200312425 120030916A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07441SW4610 4610 7602 AFTER TAKEOFF PHX, FLAPS FAIL CAUTION MSG. 0 DEGREES FLAP LANDING SLC IAW QRH. REMOVED AND REPLACED FECU IAW MM 27-50-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20031022000452003102200045SO 2003 10 22 SWIA200312427 120030917A492038003762 APU EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LEAKING A SWIAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07190SW8181 8181 120050 CAPT REPORTS SMOKE IN COCKPIT FROM AIR CONDITIONING SYSTEM. BOTH LT AND RT AIR CONDITIONING PACKS ARE COVERED IN OIL. APU BLEED SYSTEM IS PUTTING OIL INTO PACKS. REMOVED AND REPLACED THE APU IAW RII 49-301. OPS AND LEAK CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20031022000522003102200052NM 2003 10 22 QXEA200301154 120030911A5410 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 NR 1 ENGINE LOWER COWL BYPASS DOOR APERTURE LEFT SIDE SUPPORT ANGLE IS CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103. 2H72 4T4 TRTA13NM E00062EN 20031022000662003102200066NM 2003 10 22 QXEA200301167 120030918A5541 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 300 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 FORE RUDDER HAS A DENT 4 INCHES FROM LOWER CENTER HINGE. REPAIRED IAW Q400 SRM 51-25-05-370-801, RD 8/4-55-126 AND HORIZON AIR EA 6-55-54. 2H72 4T4 TRTA13NM E00062EN 20031022001342003102200134 2003 10 22 2003UALA00691 420030917A3454 INDICATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE VOR SYSTEM FAILED A UALAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 WP29399UA 24674 ON CLIMBOUT FROM GEG PREVIOUS WRITEUPS RETURNS CAPT LOST VOR WITH LOC DISPLAY ON EADI & VOR DISPLAY ON EHSI. FMC POS INIT PG DID NOT SHOW GW, FUEL OR ZFW. THEN ON DESCENT BACK INTO GEG THE NR 2 VOR FAILED WITH FLAG ON RDDMI BUT NO FLAGS ON ADI-HSI. NR 1 ILS INOP BUT NR 2 OK. DAA NR 1 (MR41922-224) WAS REMOVED. HOWEVER BOTH SHOP AND HONEYWELL TESTING FOUND NO FAULTS. TWO NR 2 VOR RECEIVERS WERE REPLACED, WITH THE MOST RECENT REPLACEMENT OCCURING ON 5 OCTOBER. 2L72 4F4 FRTA16WE E2GL 20031022001512003102200151SO 2003 10 22 SWIA200312436 120030921A27503472001001 FCU EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07233SW6846 6846 120307 FLAP CONTROL FAULT INDICATION OCCURED WHEN GOING FROM 25 TO 45 DEGREE FLAP COULD NOT RESET. REPLACED FCU WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031023000082003102300008NM 2003 10 23 03FDEA01447 120030901A5730APB74471 SKIN DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 MAIN DECK- CTR AUX TANK UPPER SKIN EXTERIOR SURFACE FOUND CORRODED AT STA 1239, LBL 24. MAIN DECK STA 1239 LBL 24 CTR AUX TANK UPPER SKIN CORROSION REPAIRED AS PER SRM 57-00-01 VOL 1 AND EA 1-5720-72606 FUSELAGE. MAINFRAME - UPPER CTR WING SKIN CORROSION REPAIR. 2L73 4F RTA22WE 20031023000112003102300011NM 2003 10 23 03FDEA01496 120030902A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING - I/B FLAP O/B HINGE PIVOT O/B LUG I/B SIDE SURFACE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71783. WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20031023000132003102300013NM 2003 10 23 03FDEA01546 120030902A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING - I/B FLAP O/B HINGE PIVOT O/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71783, TITLE - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20031023000312003102300031NM 2003 10 23 UPS03441255 120030912A5313BAC1498143 STRINGER BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, BELOW FLOOR BILGE AREA STRINGER FOUND CORROSION CRACKED AT STA 2020 STRG 46R. CORROSION CRACKED STRINGER TRIMMED OFF IAW SRM 51-10-01 AND PERFORMED STRINGER REPAIRED IAW SRM 53-10-03 FIG 1 AT BTN STA 1980 AND STA 2030 AN AREA PAINT TOUCHED UP IAW MM 51-24-11. 2L74 4F4 F A20WE E20EA 20031023000542003102300054EA 2003 10 23 SWIA200312444 120030922A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07907SW6077 6077 7511 AFTER TAKEOFF, UPON GEAR RETRACTION, EICAS WARNINGS ''NOSE DOOR OPEN'' AND ''GEAR DISAGREE'' ILLUMINATED. RETURNED TO LAX. REMOVED AND REPLACED NLG SELECTOR VALVE AND REPLACED PROX SENSOR. SWUNG GEAR, ALL CHECKS GOOD. NO LEAKS NOTED IAW MM 32-33-00. 2L72 4F4 FRTA21EA E15NE 20031027000082003102700008WP 2003 10 27 MWEA030394 120030925A533059102285 SKIN DOUG DC9 DC981 3022081WP PWA JT8 JT8D NE FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1.25 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 RT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20031027000852003102700085NM 2003 10 27 2003UALA00689 120030915A2121 FAN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE AVIONICS SEIZED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29848UA 1647 FLIGHT DIVERTED DUE TO SMOKE IN COCKPIT. AVIONICS EXTRACT FAN (18HQ) FOUND SEIZED. REPLACED FAN. 2L72 4F4 FRTA28NM E40NE 20031027000932003102700093NM 2003 10 27 ASAA02402AA 120030330A5100BAC1496377 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT FROM BS 727E PLUS 14, 835 IS CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027000962003102700096NM 2003 10 27 ASAA02401DD 120030330A53006548240 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CHAFED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND SKIN HAS AREAS OF CHAFING DAMAGE AT THE LEFT AFT LOWER SLIDE SEAL AT BS 1154. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030929000572003092900057CE 2003 9 29 GLBA2003124 120030823A526012940003359 DOOR BEECH 1900 1900D 1154162CE AIRSTAIR OPEN A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03192GL UE192 CABIN DOOR OPENED IN FLIGHT. REMOVED AND REPLACED AIRSTAIR DOOR RIG, CK AND LEAK CHECK GOOD. 2L72 4T RTA24CE 20030929001152003092900115EU 2003 9 29 RAIA00308228 120030822A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT UNSECURE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK 41040 ESCAPE PATH LIGHTS INOPERATIVE. SECURED CONNECTOR AT PATH LIGHT STRIP. 2L72 4T RTA41NM 20030930000022003093000002NM 2003 9 30 C1HA200385007 120030906A276165C163001 ACTUATOR BOEING727 7272S7 138407ZNM SPOILER LEAKING A C1HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15685CA 22492 HYD SYS A QUANTITY GUAGE WENT TO 0.4 GAL RAN CHECK LISTS. FOR SYS LOSS CALLED DISPATCH DIVERTED TO DAL. DECLARED EMERGENCY. NO LOSS OF SYS PRESSURE END. REMOVED AND REPLACED NR 14 SPOILER ACTUATOR IAW MM 27-61-81. AND SERVICED HYD SYST TO FULL IAW MM 12-20-00. ADJ/ TEST + LK CHECKS GOOD. 2L73 4F A3WE 20030930000122003093000012NM 2003 9 30 QXEA200301065 120030905A5411 STRINGER DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 MIDDLE STRINGER ON UPPER DECK OF NR 2 ENGINE COWL IS CHAFED. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20030930000362003093000036NM 2003 9 30 2003UALA00653 120030830A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29177UA 24384 FLOORBEAM BENT AT STA 760 AND RBL 42.50. INSTALLED NESTED ANGLE EXTRUSION REPAIR USING FILLER AND WEB. 2L74 4F4 FRTA20WE E24NE 20030930000972003093000097NM 2003 9 30 AWXA200301034 120030905A5320693535214 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK A .5625 INCH CRACK WAS FOUND ON STRINGER CLIP AT BS 621, STR 2 R/H. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 621, STR 2 R/H; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7. 2L72 4F RTA16WE 20031001000522003100100052WP 2003 10 1 UPS03841198 120030825A53403751193503 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, AFT ACCY COMPT. FS 1660 FLOORBEAM END FITTING AT RBL 48 IS CRACKED. HFEC IAW DC8 NDT SPM 06-10-01.001 NOTED TO BE CRACKED. RECEIVED, LOCATE D, AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0 REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20031001000582003100100058WP 2003 10 1 MWEA030399 120030928A2913AS66411LS666 PUMP DOUG DC9 DC982 3022082WP LT ENG HYD SYS INOPERATIVE A MWEAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL31809ME 48071 LEFT HYDRAULIC SYSTEM PRESSURE INICATED ZERO. REMOVED AND REPLACED LT ENGINE HYDRAULIC PUMP. 2L72 4F A6WE 20031001000722003100100072NM 2003 10 1 2003UALA00710 120030922A5610 WINDSHIELD AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT CRACKED A UALAO OTHER O OTHER CRCRUISE 1 WP29812UA 850 CAPTAIN'S WINDSHIELD IS CRACKED. WATER INGRESSION AND HEAT SENSOR ARCING DUE TO HUMP SEAL FAILURE. WINDSHIELD REPLACED. 2L72 4F4 FRTA28NM E40NE 20031001000752003100100075NM 2003 10 1 2003UALA00713 120030905A2430 INDICATOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE DC FAIL LIGHT INOPERATIVE A UALAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 WP29946UA 26687 BOTH DC FAIL LIGHTS INOPERATIVE. DIVERTED TO BOI DUE TO ELECTRICAL PROBLEMS. FOUND GENERATOR CONTROL CIRCUIT BREAKER OUT. REPLACED RELAY R41. 2L72 4F4 FRTA16WE E2GL 20031001000812003100100081NM 2003 10 1 2003UALA00720 120030925A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29369UA 24538 STA 805 FUSE FRAME HAS CORROSION ON THE AFT SIDE, JUST ABOVE AND FWD OF THE CARGO DOOR THRESHOLD. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031001000862003100100086EA 2003 10 1 COMA0360441 120030929A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01779CA10716 7306 FLIGHT 5770 MLG INDICATED UNSAFE AFTER RETRACTION. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20031001000912003100100091EA 2003 10 1 COMA0360438 120030929A5210601R3862427 VENT CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR BROKEN A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01912CA 7011 FLIGHT 5170 AIRCRAFT WILL NOT PRESSURIZE. REPLACED THE CABIN DOOR VENT VALVE. 2L72 4F RTA21EA 20031001000932003100100093SW 2003 10 1 2003F00588 120030407A5270 WARNING LIGHT FRCHLDSA227 SA227DC 3377521SW PAX DOOR ILLUMINATED A BSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM05453LA DC852B CARGO DOOR WARNING LIGHT CAME ON AT 14,000 MSL, CREW RETURNED TO STATION, LIGHTS WENT OUT AT 400 FEET AGL. SUSPECT DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, OR DOOR CLICK CLACK OR SWITCH RIGGING. CHECKED RODS FOR EXTENSION, FOUND NO PROBLEMS, LUBED SWITCHES AND CLICK CLACKS, DOOR WAS OPENED AND CLOSED, DOOR OPS CHECK GOOD. (M) 2L72 4T RTA18SW 20031001001022003100100102WP 2003 10 1 AMTA200301099 120030812A5311 FRAME LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND BULKHEAD FRAME, CORRODED BETWEEN STRINGER 33 AND STRINGER 39 AT FS 1809 APB. FRAME WAS REPAIRED PER SRM 53-11-00 FIG 848 REF M-12 1342M-12A 10591 ITEMS 5 AND 6 AT FS 1809 FROM STRINGER 40 TO BETWEEN STRINGER 24 AND 25, REF M-12A FOR OTHER SIGN-OFFS. (M) 2L73 4F A23WE 20031001001032003100100103NM 2003 10 1 USAABB03136 120030815A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19631AU 27809 FOUND FLOOR MOUNTED EMERGENCY LIGHT AT SEAT ROW 26 WITH A WEAK BATTERY. MAINTENANCE REPLACED THE BATTERY AT SEAT ROW 26 EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20031001001082003100100108EA 2003 10 1 COMA0370031 120030928A5610NP1393225 WINDOW CNDAIRCL600 CL6002C10 1390015EA CRACKED A COMAO OTHER O OTHER DEDESCENT 1 SO01625CA113 10113 FLIGHT 5043 PILOTS SIDE WINDOW CRACKED. REPLACED SIDE WINDOW. 2L72 4F RTA21EA 20031002000062003100200006NM 2003 10 2 USAA030170 120030821A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US48878 23318 FOUND SKIN CRACKED 3 INCHES, .5 INCH BELOW STRINGER S12L, FORWARD OF FS 520. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201 AND 202. (M) 2L72 4F RTA16WE 20031002000122003100200012WP 2003 10 2 AMTA200301135 120030802A5314 KEELBEAM LKHEED1011 10113851 5265010WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 TOP PORTION OF LOWER FLANGES OF BOTH KEELBEAMS CORRODED. AREA WAS REPAIRED PER E/R L10-53R-5281. (M) 2L73 4F A23WE 20031002000162003100200016NM 2003 10 2 GAIA03081OP 120030917A33501000679 LIGHT BOEING727 7272J0 138407ENM COCKPIT MALFUNCTIONED A GAIAO OTHER O OTHER CRCRUISE 1 SW07281KH 21105 DURING CRUISE, THE CREW NOTICED THE COCKPIT EMERGENCY EXIT LIGHT CAME ON WITH THE SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040504000232004050400023EA 2004 5 4 A6WA200340137 120030918A5350601R53841031 TAIL CONE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31441ZW 7777 DAMAGE TO TAIL CONE, RESULTING IN DELAMINATION OF INNER AND OUTER SKINS AND CORE DAMAGE. REPAIR, FABRICATED SKIN PLIES TWO EACH AND EXTRA PLY ONE EACH FOR EACH DAMAGED SKIN FROM KEVLAR 49 STYLE 281 FABRICATED PREPEG CMS532-01. EXTRA PLY TO EXTEND .5 INCHES PAST THE OUTER SCARF LINE. FABRICATE CORE PLUG FROM CMS599-01, .050 INCHES THICK. (M) 2L72 4F RTA21EA 20031002000212003100200021WP 2003 10 2 AMTA200301137 120030806A5310 THRESHOLD LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 C-2 CARGO THRESHOLD AFT TOP BEAM/TRACK CRACKED AT FASTENER HOLE WERE FLOOR PANEL AND THRESHOLD MEET. REMOVED AND REPLACED C-2 CARGO THRESHOLD AFT TOP BEAM WITH SERVICEABLE UNIT AS PER SRM 51-40-01. (M) 2L73 4F A23WE 20030929001402003092900140 2003 9 29 801DM0012 420030905A256569B148551 SPRING BOEING757 757200 1384950NM GIRT BAR FAILED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05801DM 26240 L1, R1, L4, AND R4 GIRT BAR LEAF SPRINGS FAILED INSPECTION LIMITS PRESCRIBED IN MM-7200-03-00917 AND PACE MAINTENANCE ORDER NO. B-757-52-21003. REPLACED L1, R1, L4, AND R4 GIRT BAR LEAF SPRINGS AND OPS CHECKED IAW CMM 25-66-14 AND MM 25-66-10. 2L72 4F RTA2NM 20030930000172003093000017NM 2003 9 30 QXEA200301070 120030908A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 EMERGENCY TRACK LIGHT BROKEN WITH EXPOSED WIRES ON RIGHT HAND SIDE OF ROW 1. REMOVED AND REPLACED EMERGENCY TRACK LIGHT ASSEMBLY. 2H72 4T RTA13NM 20030930000182003093000018SO 2003 9 30 ACE090503 220030905A8500 ENGINE CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO VIBRATION E YADAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 AL0375941 20700656 291451R PILOT REPORTED ENGINE SHAKING DURING CLIMBOUT, RETURNED FOR AN UNEVENTFUL LANDING. MAINTENANCE COULD NOT DUPLICATE. INSPECTED FUEL, IGNITION, AND MECHANICAL SYSTEMS, NO DISCREPANCIES NOTED. 1H71 3O3 O A16CE E5CE 20030930000482003093000048NM 2003 9 30 2003UALA00667 120030904A2432 BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE MASTER DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29549UA 25397 MAIN BATTERY CHARGER STATUS MESSAGE. REPLACED MAIN BATTERY. SHOP FINDINGS: FAULT WAS CONFIRMED, ONE BAD CELL WAS FOUND IN THE BATTERY. 2L72 4F4 FRTA2NM E17NE 20030930000492003093000049NE 2003 9 30 2003UALA00668 220030904A7200 ENGINE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 SURGES A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 WP29653UA 25391 ENGINE 2 SURGE DETECTED. ENGINE SURGE IN FLIGHT AT TOP OF DECENT. EPR BELOW 1.25. SURGE CHECKS ACCOMPLISHED SHOWED NO IRREGULARITIES. NO CAUSE FOUND. 2L72 4F4 FRTA1NM E24NE 20030930000882003093000088WP 2003 9 30 ABXA030359 120030819A5312991015517 PRESSURE PANEL DOUG DC9 DC932F 3022067WP LT WHEEL WELL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 PRESSURE PANEL LEFT WHEEL WELL AT FS 718 LEFT BUTT LINE 36 APPROXIMATELY, CRACKED. REPAIRED RPESSURE PANEL IAW REA D953-48107. 2L72 4F A6WE 20031001000832003100100083SO 2003 10 1 LR7A03080 120030929A335044910 LIGHT LKHEED382 382G 526414USO CABIN CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 4 5025 DURING SCHEDULED A-1 INSPECTION PER JOB CARD HA1201 FOUND CREW ENTRANCE EMERGENCY EXIT LIGHT DIM DURING TEST. REPLACED EMERGENCY EXIT LIGHT ASSY DUE CORRODED. LP 12613, ITEM M2. 2H74 4T A1SO 20031001000952003100100095WP 2003 10 1 AMTA200301125 120030903A5330 SKIN LKHEED1011 10113851 5265010WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 AFT FUSELAGE SKIN CORRODED. REPAIRED DAMAGED AREA PER ER/A L10-53R-5272. (M) 2L73 4F A23WE 20031001000992003100100099 2003 10 1 AMTA200301131 420030904A2565D30170535 SLIDE LKHEED1011 10113853 5265020WP CABIN MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 R-1 DOOR WOULD NOT ARM BEFORE FLIGHT. REMOVED AND REPLACED R-1 DOOR SLIDE PER M-11-25-36. OPS CHECK GOOD. (M) 2L73 4F A23WE 20031001001112003100100111EA 2003 10 1 03272674 120030929A335059465 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27674BR 7601 DURING INSPECTION THE FIRST SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY TRACK LIGHTING STRIP. A SATISFACTORY OPERATIONAL CHECK WAS AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20031002000302003100200030WP 2003 10 2 GTIA030675 120030907A5320 WEB DOUG DC9 DC982 3022082WP CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FOUND RIGHT CABIN WEB HAS 1 CRACK AND SEVERAL DEEP TOOL MARKS FS 1002-1022 RBL 48. CUT OUT DAMAGE AREA. FABRICATED REPAIRED DOUBLER. INSTALLED REPAIRED DOUBLER. (M) 2L72 4F A6WE 20031002000332003100200033NE 2003 10 2 AALA20030963 220030904A7200 ENGINE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY65015 54557NE NR 2 BIRD INGESTION A AALAEA ENGINE SHUTDOWN UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SW211450A 11459 17598 SHORTLY AFTER TAKEOFF, AIRCRAFT HIT A FLOCK OF BIRDS. ENGINE NR 2 FAILED. FOLLOWED CHECKLIST, SHUTDOWN NR 2 ENGINE, AIRCRAFT HAD SEVERE VIBRATION. COMPLIED WITH PROCEDURE TO PULL FIRE HANDLE AND DISCHARGE FIRE BOTTLE. LANDED AT JFK APPROX 79,000 LBS WEIGHT WITHIN NORMAL LIMITS FOR LANDING. ENGINE FAILRUE WAS UNCONTAINED, DEVELOPING A 4 BY 8 INCH HOLE IN COWLING. INTERIM REPAIRS MAD TO PREPARE FOR FERRY FLIGHT FOR ADDITIONAL MAINTENANCE INCLUDING ENGINE CHANGE. SYTEM GROUND AND LEAK CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRT E25NE 20031002000542003100200054WP 2003 10 2 UPS03841210 120030826A5340DC853B003501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, 2 EACH CRACKED SEAT TRACK FITTINGS ,B-PIT CEILING STA. 420,RBL 24. REMOVED DAMAGED SEAT TRACK SECTION BETWEEN STA. 300 TO 490 RBL 24-31 FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM. 53-2-3 FIG. 8A,AND REPLACED FITTINGS IAW SRM. 53-2-3 FIG. 8A. 2L74 4F RT4A25 20031002000592003100200059WP 2003 10 2 UPS03841217 120030827A5313 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, AFT SIDE STATION 70 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONGERON 29L AND 30L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED ANGLE REPAIR AND DOUBLERS I.A.W. SRM. 53-2-5 FIG. 8C-2. 2L74 4F RT4A25 20031002000642003100200064NM 2003 10 2 QXEA200301090 120030830A5410 STRUCTURE DHAV DHC8 DHC8202 2809007NM NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 TOP OUTBOARD FASTENER HOLE FOR REFUEL/DEFUEL SHUTTOFF VAVLE IS CRACKED. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-54-1839. 2H72 4T RTA13NM 20031002000722003100200072SO 2003 10 2 C2XA03TY149 120030910A532014522461011 PLATE EMB 135 EMB135ER 3260203SO GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE GALLEY RIGHT HAND AFT CROSS BEAM PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CROSS BEAM PLATE IAW EMB SRM 51-10-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031002000742003100200074SO 2003 10 2 C2XA03TY151 120030910A531513500469403 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE FLOORBEAM AT FRAME 22 RT, WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 22 IAW EMB SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031002000862003100200086NM 2003 10 2 C1HA200386002 120030908A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 CORROSION ON FLOORBEAM UPPER CHORD AT BS 344. 2L73 4F A3WE 20031002000872003100200087NM 2003 10 2 C1HA200386003 120030908A5754 WEDGE BOEING727 7272S7 138407ZNM NR 7 SLAT GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 NR 7 SLAT TRAILING EDGE WEDGE GOUGED. 2L73 4F A3WE 20031002000922003100200092NM 2003 10 2 C1HA200386008 120030909A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 CORROSION AROUND SEAT TRACK FASTENERS AT BS 420-480 RBL 50. 2L73 4F A3WE 20031002000942003100200094NM 2003 10 2 C1HA200386010 120030909A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 LITE CORROSION ON SEAT TRACK BS 990-1030 LBL 22. 2L73 4F A3WE 20031002000982003100200098NM 2003 10 2 C1HA200386014 120030910A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 AFT CABIN SEAT TRACK IS CORRODED AT BS 1034 LBL 25 2L73 4F A3WE 20031002000992003100200099SO 2003 10 2 C2XA03TY154 120030910A2840 CONNECTOR EMB 145 EMB145XR SO DAU DIRTY A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2721144 145741 FLIGHT 2658, IAH TO PIT, AIRCRAFT DIVERTED INTO TYS FOR A FUEL IMBALANCE. WING TANK NR 1 FUEL QTY INDICATION WAS MEL'ED IN IAH PRIOR TO FLIGHT DEPARTURE, UPON LANDING IN TYS, MAINTENANCE CHECKED THE FUEL QTY. WITH UNDER WING STICKS AND FOUND THE SPLIT TO BE WITHIN TOLERANCE. THE FLIGHT CONTINUED ON, LATER THAT NIGHT MECHANICS CLEARED THE MEL IN EWR BY CLEANING THE NR 1 DAU CONNECTOR. THE AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4F RT 20031027001002003102700100NM 2003 10 27 ASAA02402GG 120030412A5320656571035 ANTENNA BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND CORROSION ON ANTENNA STRUCTURE AFT CARGO BAY AT BS 727D. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001082003102700108NM 2003 10 27 ASAA02402OO 120030331A532069434562 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND FLOOR SUPPORT STRAP IS CORRODED AT BS 792. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028000142003102800014NM 2003 10 28 UPS03241270 120030924A5330 SKIN BOEING727 72751C 1384015NM AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 INSPECTION TYPE: SPV, LIGHTNING STRIKE AND AREA OF CORROSION 15 INCHES ABOVE NR 1 PYLON AT TR SECTION ON EXTERIOR FUSELAGE AT STA 1283 LONG 9L-10L. BLENDED OUT CORROSION AND LIGHTNING STRIKE, FOUND A CRACK AT BLEND OUT AREA, CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLERSAND DOUBLER IAW SRM 53-30-3 FIG 14. 2L73 4F A3WE 20031028000152003102800015NM 2003 10 28 UPS03441267 120030904A5510BACB30US6K22 BOLT BOEING747 747121 1384871NM EMPENNAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, HORIZONTAL STAB BOX INTERIOR RT BL 43.5 WEB UPPER CORNER 2 EACH MOUNTING SCREW BROKEN. HORIZONTAL STAB BOX INTERIOR RT BL 43-5 WEB UPPER CORNER UPPER BOLT HOLE OVERSIZED AND BOLT REINSTALLED IAW SB 747-55A2050 R1 LWR BOLT REPLACED PER MM 20-51-01. 2L74 4F A20WE 20031028000192003102800019NM 2003 10 28 UPS03441272 120030905A575365B078435 RIB BOEING747 747121 1384871NM TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 3 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 3 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS R57-41-35067 & UPS CONTINUE EO B747-5740-19269-A RAISED. 2L74 4F A20WE 20031028000232003102800023NM 2003 10 28 CALA0300564 120030926A5210 GATE BOEING737 7373T0 1384582NM PAX DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND CORROSION ON INTERIOR OF R-1 DOOR LOWER GATE. THE GATE WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20031028000252003102800025NM 2003 10 28 CALA0300566 120030927A3233273A12011 ACTUATOR BOEING737 737824 13844BZNM NLG INOPERATIVE A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW271222115484 28930 THE NLG WOULD NOT EXTEND WHEN GEAR WAS LOWERED ON APPROACH TO AUS. A GO AROUND WAS PERFORMED AND THE TOWER CONFIRMED THAT THE GEAR WAS STILL UP. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE NOSE GEAR EXTENDED. THE AIRCRAFT LANDED AT AUS WITHOUT INCIDENT. EXTENSIVE TROUBLESHOOTING BY MAINTENANCE FOUND THE NLG LOCK ACTUATOR AT FAULT. THE LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-21. A GEAR SWING WAS PERFORMED SEVERAL TIMES AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20031022000102003102200010NM 2003 10 22 F3LA200300140 120030920A5320 FLOOR SUPPORT BOEING737 73736E 138443ANM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT AT STA. 951, RBL 26-46, CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AND COVER PLATE IAW SRM 51-10-02, 51-20-01, AND EA B3-53R-10148. 2L72 4F4 FRTA16WE E2GL 20031022000402003102200040EA 2003 10 22 SWIA200312422 120030914A2711 SWITCH CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07943SW 7762 AILERON TRIM SWITCH STICKS INTERMITTENTLY. REMOVED AND REPLACED AILERON/RUD TRIM PANEL. OPS CHECK GOOD IAW CRJ MM 27-00-00. 2L72 4F RTA21EA 20031022000682003102200068SO 2003 10 22 C2XA03IA096 120030919A3397W192855720 WIRE EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714920 145380 THE CREW NOTED THAT THE EMERGENCY LIGHTS POP THE CIRCUIT BREAKER WHEN SELECTED ON DURING POST-FLIGHT. STL- MAINTENANCE RESECURED WIRE TO THE EMERGENCY LIGHT BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031022001092003102200109NM 2003 10 22 F3LA200300142 120030923A5347 SEAT TRACK BOEING737 73736E 138443ANM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK AT STA. 328 TO STA. 360, RBL 24, CORRODED. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-40-02, MFG DRAWING 65C34624 AND SOPM 20-41-02. 2L72 4F4 FRTA16WE E2GL 20031022001522003102200152 2003 10 22 SWIA200312437 420030912A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE AUTO PILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07213SW8771 8771 120277 FO'S HDG BUG SLEWS ITSELF CLOCKWISE INTERMITTENTLY. SEEMS TO ONLY DO IT WITH AP SELECTOR TO FO'S SIDE WITH OR WITHOUT AP ENGAGED. REMOVED AND REPLACED FO'S AUTOPILOT COMPUTER IAW EMB MM 22-10-00. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031022001602003102200160SO 2003 10 22 C2XA03SH347 120030924A542014576631622 STIFFENER EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL NR 2 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK MAINTENANCE FOUND THE NR 2 ENGINE UPPER COWLING AFT STIFFENER TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031023000592003102300059NM 2003 10 23 QXEA200301176 120030919A5330 SKIN DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 ON FLIGHT 2040 DENT IN LT HAND FUSELAGE SKIN PANEL STATION X23.00 BETWEEN STRINGERS 23P AND 24P. REMOVED AND REPLACED RIVET IAW EA 2-53-455D. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031023000702003102300070EA 2003 10 23 COMA0360423 120030923A21320945 DUCT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN CRACKED A COMAD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 SO01988CA 7204 FLIGHT 5838 DURING CLIMB THE CABIN ALTITUDE INCREASED IN AUTO MODE FOLLOWED BY A RUMBLING NOISE, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE RIGHT 10TH FUSELAGE DUCT. 2L72 4F4 FRTA21EA E15NE 20030908001652003090800165SO 2003 9 8 SWIA200312239 120030804A3350 SIGN EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07229SW 120305 MAIN ENTRYWAY EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. REPLACED EMERGENCY EXIT SIGN WITH A SERVICEABLE UNIT AT PAX DOOR . OPS TEST GOOD. 2L72 4T RTA31SO 20030908001682003090800168EA 2003 9 8 SWIA200312240 120030731A27507455001 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07460SW 7803 AFTER LANDING FLAPS FAILED WITH A 'FLAPS FAIL' CAUTION ON ED1. REMOVED AND REPLACED FLAP CONTROL HANDLE IAW MM 27-51-01 OPS CHECK GOOD. 2L72 4F RTA21EA 20030908001762003090800176SO 2003 9 8 SWIA200312247 120030811A3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO LANDING GEAR FAULTY A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07196SW 120151 ON APPROACH, GEAR WOULD NOT EXTEND. RAN THE LDG GEAR EXTENSION BY ELECTRICAL OVERRIDE WITHOUT SUCCESS. RAN LDG GEAR EXTENSION BY FREEFALL AND ALL GREEN A & B LIGHTS ILLUMINATED. REPLACED LEFT 'A' PROXIMITY SENSOR IAW 32-61-01. LANDING GEAR OPS CHECKS GOOD. P/N: 922AA2Y-A6Y2722A S/N ON: LOT 008343 2L72 4T RTA31SO 20030908001842003090800184SO 2003 9 8 SWIA200312263 120030816A275012064207615 CONTROL HANDLE EMB 120 EMB120ER 3260203SO COCKPIT FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07584SW4028 4028 120352 CREW REPORTS MULTIPLE FLAP FAILURES WITH CONTROL FAULTS.REMOVED AND REPLACED FLAP HANDLE IAW MM 27-50-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030908001862003090800186SO 2003 9 8 SWIA200312264 120030811A5753 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO T/E FLAP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07218SW 120287 LEFT OUTBOARD FLAP, INBOARD ROLLER SUPPORT BRACKET IS CRACKED. DISCOVERED DURING LINE INSPECTION, INSTALLED SERVICEABLE BRACKET AND OPERATED FLAPS. OPS CHECKS GOOD. P/N: 120-21940-001 2L72 4T RTA31SO 20030908001982003090800198EA 2003 9 8 SWIA200312284 120030719A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PILOT'S BULKHEAD AFT FLOOR ANGLE RBL 11.0 CRACKED. DISCOVERED DURING C-CHECK, REPAIRED ANGLE IAW CRJ REO 601R-53-11-137 REV 'NC'. 2L72 4F RTA21EA 20030908002002003090800200EA 2003 9 8 SWIA200312286 120030719A5411 RIB CNDAIRCL600 CL6002B19 1900309EA RT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 RT PYLON RIB FS 605 CRACKED. DISCOVERED DURING C-CHECK, REPLACED RIB IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20030908002052003090800205EA 2003 9 8 SWIA200312291 120030719A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-52 2L72 4F RTA21EA 20030905001592003090500159NE 2003 9 5 DL76P030673 220030718A7321 EEC BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE DEFECTIVE A DALAK NONE E VIBRATION/BUFFET DEDESCENT 1 SO27140LL24118 25988 727745 ON DESCENT INTO FLL RT ENGINE SURGED. EGT WENT INTO YELLOW. BOROSCOPE PER FIM 71005-00 ALL OK. EEC AND PT2 PROBE REPLCD C/W ALL INSP PER FIM 71-05-00. ENGINE RUN PER PFHB 6-7-4-14 AND T/O PWR CHECK ALL OK. 2L72 4F4 FRTA1NM E24NE 20030905001972003090500197NM 2003 9 5 USAASB03138 120030813A56105893543129 WINDSHIELD BOEING737 7374B7 1384702NM COCKPIT CRACKED A USAAHBA DEACTIVATE SYST/CIRCUITSEMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19442US 24841 BWI - FLT 242 - EN ROUTE FROM CLT-EWR, AT FL330, THE CAPTAIN'S L1 WINDSHIELD BEGAN ARCING. C REW TURNED OFF THE WINDOW HEAT TO THIS WINDOW, THEN THE WINDSHIELD BEGAN CRACKING IN SEVERAL PLACES. CREW DONNED THEIR OXYGEN MASKS AND REQUESTED A PRIORITY DESCENT OT 14,000 FEET FOR OPERATIONAL ABNORMALITIES. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS L1 WINDSHIELD AND TE WINDOW HEAT CONTROLLER, P/N 83000-05602. OPS CHECK AND LEAK GOOD. (M) 2L72 4F RTA16WE 20030905002202003090500220SO 2003 9 5 C2XA03TY127 120030811A5347145332605017 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION SEAT TRACK RW4 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030905002222003090500222SO 2003 9 5 C2XA03SH298 120030827A531514521713005 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 20 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030905002302003090500230SO 2003 9 5 C2XA03TY125 120030811A534714530659007 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF5 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030905002372003090500237WP 2003 9 5 DHL2003873615 120030705A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT OUTER STUB WING OUTER PLATING UPPER SURFACE SHOWS CORROSION BETWEEN STA XFS 526 AND XW.485 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED FASTENERS, TRIMMED OUT DAMAGED SKIN AREA IAW EODHL-030630, ED-3461. PERFORMED NDT INSPECTION IAW DC8 NDTSPM 6-10-01-001. CLEANED, TREATED AND PRIMED AREA, FABRICATED A REPAIR DOUBLER AND TWO FILLERS. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES, INSTALLED FILLER AND DOUBLER ON LT OUTER STUB WING OUTER PLATING UPPER SURFACE (BETWEEN STA XFS.526 AND XW.485) USING NEW FASTENERS. 2L74 4F RT4A25 20030908001882003090800188SO 2003 9 8 SWIA200312265 120030810A3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO LT MLG MALFUNCTIONED A SWIAO OTHER N FALSE WARNING DEDESCENT 1 NM07188SW 120039 LANDING GEAR WOULD NOT EXTEND NORMALLY, GEAR EXTENDED USING ELECTRICAL OVERRIDE PROCEDURE.FOUND LEFT MAIN GEAR 'A' DOWN LOCK PROX SENSOR INOP. REPLACED MAIN "A" HARNESS IAW EMB120 MM 32-61-01. OPS CHECK GOOD. P/N: 120-22623-501 2L72 4T RTA31SO 20031023000712003102300071EA 2003 10 23 COMA0360424 120030923A213131197688 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE AVIONICS BAY FAULTY A COMAO OTHER O OTHER CRCRUISE 1 SO01988CA6500 7204 FLIGHT 5834 DURING CRUISE FLIGHT THE AUTO PRESSURIZATION MODE FAILED CAUSING CABIN ALTITUDE INCREASE. REPLACED THE PRESSURIZATION CONTROLLER NR 2. 2L72 4F4 FRTA21EA E15NE 20031023000822003102300082NM 2003 10 23 F3LA200300146 120030924A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT LBL 25, BETWEEN STA 967 AND 947.5, CORRODED. REPLACED INTERCOSTAL PER SRM 51-40-02. 2L72 4F RTA16WE 20031027000392003102700039NM 2003 10 27 CALA0300558 120030925A5320 STRAP BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND STRESS WEB UPPER STRAP CORRODED AT STA 1006-1022, RBL 28. THE CORRODED STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031027000622003102700062NM 2003 10 27 UPS03441262 120030904A533065B044888 SKIN BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LOWER FUSELAGE EXTERNAL SKIN EDGE FOUND CRACKED AT STA 1480 RT SIDE STR 41 TO 42 RT. LOWER FUSELAGE EXTERNAL SKIN REPAIRED AS IAW RS NR R-53-61-35068 JUST AT STA 1480 RT SIDE STR 41R TO STR 42R AND REF UPS ENGINEERING FILE NR 747-53-20154. 2L74 4F4 F A20WE E20EA 20031027000722003102700072EU 2003 10 27 MALA030431 120030918A5414 SKIN SAAB SF340 340B 7860101EU RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 DURING 4K INSPECTION IN CWA, RT NACELLE OUTBOARD SKIN PANEL NS 203 IS CRACKED. MAINTENANCE ACCOMPLISHED REPAIR IAW SAAB REPAIR STATEMENT 340SDS006007, EO S54068. A/C RELEASE DATE 9/25/03. REFER TO 409 NR 193407 FOR DETAIL. 2L72 4T RTA52EU 20031027000872003102700087CE 2003 10 27 DXTA200300131 120030929A2131 CONTROLLER CESSNA750 750 2076810CE CABIN TEMP FAILED E DXTAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 GL07900QS2971 7500123 WHILE CLIMBING THROUGH FL330 THE COCKPIT TEMP CIRCUIT BREAKER POPPED, COCKPIT AIR-CONDITIONING PAC WOULD NOT STOP BLOWING HOT AIR. EICAS WARNING “DU-HOT” ILLUMINATED, AFTER LOSING DU 1 & 2 ELECTED TO DIVERT INTO LBL. DURING DESCENT INTO LBL STARTED LOSING DU 4 & 5, EMERGENCY DECLARED. - CHECKED CIRCUIT BREAKER AND WIRING, ALL CHECKED GOOD, RAN AIRCRAFT WITH APU AND BOTH ENGINES ALL CHECKED GOOD. REPLACED TEMP CONTROLLER AND SENSOR AS PRECAUTIONARY, OPS CHECKED GOOD IAW CESSNA 750 MM CHAPTER 21-00 2L72 4J RTT00007WI 20031028000212003102800021NM 2003 10 28 CALA0300562 120030926A5330 SKIN BOEING777 777224 1385225NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777014 29862 INSPECTION FOUND A .375 INCH CRACK IN FUSELAGE SKIN AT STA 575 BETWEEN S42L AND S43L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 2. 2L72 4F RTT00001SE 20031028000562003102800056NM 2003 10 28 QXEA200301190 120030927A2810 CAP DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 400 LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09350PH 488 FUEL DRIPPING FROM NR 2 NACELLE, IMMEDIATELY FORWARD OF RE-FUEL PANEL. REMOVED AND REPLACED DUST CAP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031028000612003102800061SO 2003 10 28 C2XA03SH356 120030930A531014526437001 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE RT BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031028000682003102800068 2003 10 28 219PA0010 420030925A22102588812901 COMPUTER BOEING737 737222 1384473NM ROLL CHANNEL MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05219PA 19956 ROLL CHANNEL WILL NOT ENGAGE ON AUTO PILOT AND HEADING SELECT WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED GOOD PER MM 22-11-0. 2L72 4F A16WE 20031028000702003102800070EA 2003 10 28 HNAA030052 120030926A26123601881000390 FIRE LOOP DHAV DHC8 DHC8311 1386006EA NR 1 ENGINE FALSE INDICATIONA HNAAO OTHER N FALSE WARNING CRCRUISE 1 EA07284BC 336 WARNING LIGHT, AND NR 1 ENGINE A-LOOP LIGHT ILLUMINATED. SELECTED B-LOOP AND FAULT A-LOOP WENT OUT, ALL ENGINES INDICATIONS NORMAL. 2H72 4T RTA13NM 20031028000742003102800074NM 2003 10 28 2003UALA00697 120030918A2710113W72124 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE RT & LT AILERONSCRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA32068 26947 RT AND LT AILERON PCU, IB FITTINGS CRACKED ON INBOARD SIDE. BOEING HAS RELEASED SB 777-57-0047 TO REPLACE AILERON FITTINGS WITH IMPROVED PART. AILERONS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20031028000772003102800077CE 2003 10 28 54574 120030920A5270 SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ACCESS DOOR OUT OF ADJUST A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07182YV UE182 MASTER WARNING ILLUM WITH A CABIN DOOR ANNUNCIATOR. TAKEOFF WAS ABORTER AFT RETURNED TO GATE. ADJUSTED CABIN DOOR ANNUNCIATOR LIGHT SWITCH. 2L72 4T3 TRTA24CE E2NE 20031028000822003102800082NM 2003 10 28 2003UALA00768 120031010A213190221570210 CONTROLLER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN PRESSURE FAILED A UALABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29810UA 843 RETURN TO FIELD DUE TO A PRESSURIZATION PROBLEM. CFDS REPORTED NO FAULTY SYSTEMS OR COMPONENTS. GROUND TESTING OF CABIN PRESSURE CONTROL, FMGC, AND ADIRS SYSTEMS REVEALED NO SYSTEM FAULTS. REPLACED CPC 2 AS PRECAUTIONARY MEASURE AS THIS WAS CPC IN CONTROL AT TIME OF EVENT. 2L72 4F4 FRTA28NM E40NE 20031028000862003102800086NM 2003 10 28 DHL2003747011 120031011A3350 LIGHT BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01747DH 22253 ENTRY EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-00. OPS CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20031028000912003102800091NM 2003 10 28 ASAA0240DDD 120030403A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND SHEAR TIE CORRODED AT BS 727D. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028000972003102800097NM 2003 10 28 03FDEA01602 120030908A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OB FLAP, FOUND CORROSION ON IB HINGE (FLAP SIDE) IB AND OB PIVOT HOLES BORES AND SPOT FACES. LT OB FLAP IB HINGE (FLAP SIDE) IB AND OB PIVOT HOLES BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT IAW EA NR 1-5750-72698 WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - LT OB FLAP/ IB SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031028000982003102800098NM 2003 10 28 03FDEA01600 120030908A5753ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FOUND CORROSION ON OUTBOARD PIVOT HOLE BORE AREA. LT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORROSION AREAS REPAIR CARRIED OUT AS PER EA 1-5750-72685 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031028001042003102800104EU 2003 10 28 KBM2003F00001 120030823A6230 BUSHING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE SWASHPLATE DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 MAIN ROTOR SWASHPLACE UPPER ROTATING SCISSOR BLOCK (1) EA BUSHING IS DEBONDED. REPAIRED DEBONDED BUSHING. 1G71 3U3 UNCH9EU E19EU 20031028001282003102800128EA 2003 10 28 ASOA03492 120031006A5260 HINGE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE UPPER STEP HINGE ON THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE UPPER STEP HINGE ON THE PASSENGER DOOR IAW ASA EO 600-53-0052A. (M) 2L72 4F RTA21EA 20031028001292003102800129EA 2003 10 28 ASOA03479 120031004A5210H341433 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11881AS 7445 FLT 4853 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR OTUER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031022001352003102200135NM 2003 10 22 2003UALA00692 120030917A5330 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29772UA 26930 SKIN AT STA 624 BETWEEN STRINGERS 46L AND 47L, UNDER LOWER FUSELAGE ANTENNA BASE HAS 2 EA OVERSIZED AND ELONGATED HOLES. MAJOR REPAIR. REPAIRED BELLY SKIN AND INSTALLED NEW INNER DOUBLER. 2L72 4F4 FRTT0001SE E46NE 20031022001532003102200153SO 2003 10 22 SWIA200312438 120030917A27106225735004 MOUNT EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE SERVO MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07213SW3114 3103 120277 AILERON SYSTEM HAS BUMP. MOVEMENT NOT SMOOTH. INSTALLED SERVICEABLE MOUNT, CAPSTAN AND SERVO MOTOR FOR AILERON CONTROL IAW 27-20-00. P/N 622-5734-002 S/N OFF 6176. 2L72 4T4 TRTA31SO E20NE 20031023000202003102300020NM 2003 10 23 ABXA030369 120030924A5510182T01302 SPLICE BOEING767 767281 1385109NM GE CF6 CF680 30025NE HORIZONTAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23775AX 22790 CRACK INDICATION ON RT UPPER INBOARD HORIZONTAL STABILIZER PIVOT FITTING DURING X-RAY. REMOVED AND REPLACED PLATE IAW REA B655-48039-MR. 2L72 4F4 FRTA1NM E13NE 20031023000322003102300032NM 2003 10 23 UPS03441256 120030907A53107075T60063IN SHEAR TIE BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C AFT CARGO COMPT - BELOW FLOOR SUPPORT FRAME LOWER SHEAR TIE PLATE FOUND CRACKED AT STA 1880 LT SIDE STR 43 LT. DEFECT SHEAR TIE TRIMMED OUT IAW SRM 51-10-01 AND PERFORMED SHEAR TIE REPAIRED IAW SRM 53-10-04 FIG 41 AN AREA PAINT TOUCHED UP. 2L74 4F4 F A20WE E20EA 20031027000202003102700020EU 2003 10 27 AWXA200301096 120030913A5315D5347209001000 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON Y1292 FLOORBEAM AFT SIDE OF FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y1292 FLOORBEAM FROM FR 64 TO FR 67; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, PG. 28, FIG. 12. 2L72 4F4 FRTA28NM E311NE 20031027000422003102700042NM 2003 10 27 CALA0300561 120030922A5512 PANEL BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716646 28907 INSPECTION FOUND CRACKS ON THE LOWER SIDE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL. THE CRACKS WERE CONFINED TO THE BONDED INTERNAL DOUBLER AT ONE FASTENER HOLE, 5.2 INCHES OB OF THE STA 188 RIB. THE AREA WAS REPAIRED IAW ECRA 5510-01695. 2L72 4F4 FRTA16WE E2GL 20031027001212003102700121EA 2003 10 27 QXEA200301182 120030923A7120 MOUNT CNDAIRCL600 CL6002C10 1390015EA ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 ENGINE THRUST FITTING MOUNT PLATE DROPPED FROM PYLON HAS BURS ON EDGE. REPAIRED IAW HORIZON AIR EA R-71-65. 2L72 4F RTA21EA 20031027001322003102700132NE 2003 10 27 RAIA00309247 220030923A7261TPE33114HR ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RIGHT CONTAMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03567HK13991 41085 76107 RIGHT ENGINE OIL CONTAMINATION INDICATION. MAINTENANCE REMOVED AND REPLACED ENGINE. 2L72 4T4 TRTA41NM E18NE 20031112000702003111200070NM 2003 11 12 ASAA0240CCC 120030314A531065465497 FAILSAFE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON FAILSAFE AT BS 767 STRINGER 27L-27R AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028000922003102800092NM 2003 10 28 ASAA0240EEE 120030401A53306545778 SKIN BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND FUSELAGE EXTERIOR SKIN IS GOUGED AT BS 919-928. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001222003102800122SO 2003 10 28 SIMA200324603 120030824A531014522460013 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21718AE 145275 ABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED CUT OUT OF THE DAMAGED AREA. FABRICATED REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 53-21-10 PARA 5 FIG 204 SHEET 2. (M) 2L72 4F RTT00011AT 20031028001342003102800134NM 2003 10 28 GAIA03082 120030910A5347 SEAT TRACK BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW096806 19481 DURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 360 TO BS 344, RBL 25.5. REF FASI N/R 50402, FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 140 INCHES REPAIRED IAW B727 SRM 53-10-5, FIGURE 7 AND 53-10-2, FIGURE 7. (M) 2L73 4F A3WE 20031028001362003102800136NM 2003 10 28 GAIA03100 120030910A5320 FLOOR SUPPORT BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FLOOR SUPPORT ANGLE LBL 61 BS 1090 UPPER CHORD CORRODED. REF FASI N/R 53253, REPLACED UPPER CHORD PER B727 SRM 53-10-2 FIG 5 AND 51-30-2. (M) 2L73 4F A3WE 20031028001792003102800179NM 2003 10 28 ASAA0340075 120030227A5311 FRAME BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND GOUGE ON FRAME AT BS 727D RBL 14 AND W165. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001812003102800181NM 2003 10 28 ASAA0340077 120030227A531165C32351 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 500E LBL 5, RBL 5 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001852003102800185NM 2003 10 28 ASAA0340098 120030301A532069653622 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND UPPER FLANGE OF INTERCOSTAL AT BS 867-877 WL 156 AND RBL 23 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000072003102900007NM 2003 10 29 ASAA0340106 120030301A5320654795711 STRAP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON THRESHOLD STRAP AT BS 847-860 RBL 20 AND WL 155. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000122003102900012 2003 10 29 ASAA0380535 420030709A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 PREFLIGHT CHECK, FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND INOPERATIVE, DISCONNECTED. 'RESET' RECONNECTED LANYARD. (M) 2L72 4F A6WE 20031029000132003102900013NM 2003 10 29 ASAA0340109 120030301A510065479576 BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON THRESHOLD BEAM FROM BS 795-846 RBL 21 AND WL 153. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000232003102900023NM 2003 10 29 ASAA0340079 120030227A531165C22908 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON FRAME BS 500B LBL5 RBL 5 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000262003102900026NM 2003 10 29 ASAA0340082 120030227A5320654769020 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 867 TO BS 487 RBL 21 AND WL 152. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000312003102900031EA 2003 10 29 ASOA03472 120031001A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING HANGAR MAINTENANCE IN BTR, THE EXTERIOR FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR FORWARD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031029000352003102900035EU 2003 10 29 USAASA03108 120030904A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19720US 1089 PHL - THE LEFT EMERGENCY EXIT LIGHT AT THE OVERWING POSTION WAS FOUND INOPERATIVE DURING TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031029000412003102900041EU 2003 10 29 USAASA03097 120030820A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW 1040 DURING TEST OF EMERGENCY LIGHTS, RECEIVED 'EPSU UNIT FWD L' MESSAGE ON THE FLIGHT ATTENDANT PANEL. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031029000442003102900044NM 2003 10 29 ASAA0310403 120030506A5320 WEB BOEING737 737290C 138448VNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND E/E DOOR RISER PANEL WEB AT BS 323.7-351.2, STRINGER 27R CHAFED. REPLACED WEB PER SRM. (M) 2L72 4F A16WE 20030908001892003090800189EA 2003 9 8 SWIA200312266 120030811A2750860D10018 ECU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07590SW 7077 AFTER LANDING IN SLC, WHEN FLAP SELECTED UP, 'FLAP FAIL' MSG AND FLAPS FAILED TO RETRACT. REMOVED AND REPLACED THE FECU WITH A SERVICEABLE UNIT IAW AMM 27-51-5. SYSTEM CHECKS GOOD. SN OFF 658. 2L72 4F RTA21EA 20030908002062003090800206EA 2003 9 8 SWIA200312292 120030719A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 LT FIRE WALL SHUTOFF VALVE FS 665 ANGLE CRACKED. DISCOVERED DURING C-CHECK, REPAIRED ANGLE IAW CRJ SRM 51-40-11. P/N: S6144-13 2L72 4F RTA21EA 20030908002482003090800248EA 2003 9 8 SWIA200312355 120030827A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07435SW 7555 SPOILERON FAULT STATUS MSG ON TAXI OUT. REPLACED LEFT I/B FLT SPOILERON PCU IAW 27-60-00 & NR 1 SECU. OPS AND LEAKS CHECKS GOOD IAW 27-60-00. S/N OFF: 5587. SECU P/N: 49-164-20 S/N OFF: 01664 S/N ON: 03079. 2L72 4F RTA21EA 20030908002742003090800274EA 2003 9 8 SWIA200312365 120030825A3260 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07588SW 7069 ON TAKEOFF, GEAR DISAGREE AND NOSE DOOR WARNING MSGS. INSPECTED NOSE LANDING GEAR AND ALL PROXIMITY SENSORS FOR CLEARANCE AS WELL AS SECURITY, AND WIRES. FOUND NO DISCREPANCIES. SWUNG GEAR APPROX 25+ TIMES WITH NO FAULTS IAW CL600 MM 32-61-05. OPS CHECKS GOOD AT THIS TIME. 2L72 4F RTA21EA 20030908002752003090800275 2003 9 8 SWIA200312373 420030828A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07268UE7138 4554 120207 F/O'S A/P - F/D INTERMITTENTLY DISCONNECTED INFLIGHT WITH ASSOCIATE A/P FAILED. REPLACED NR 2 A/P COMPUTER. INSTALLED NEW PINS/SOCKETS ON PITCH TRANSFER RELAYS K0311, K0310, K0312 AND K0256. INSTALLED NEW RELAY SOCKETS FOR RELAYS K0310 AND K0312 AND REPLACED AUTOPILOT DISCONNECT RELAYS K0462 AND K0463. BOTH AUTOPILOT SYSTEMS OPS CHECK GOOD IAW MM 22-10-00. OPS CHECKED GOOD ON GROUND. 2L72 4T4 TRTA31SO E20NE 20030908002802003090800280CE 2003 9 8 AMWA27 120030724A1430 RIVET BEECH 1900 1900D 1154162CE FUSELAGE LOOSE A AMWAK NONE O OTHER ININSP/MAINT 1 CE07131YV UE131 WHILE PERFORMING AN ABC STRUCTURAL INSPECTION, TWO RIVETS WERE FOUND TO BE LOOSE ON THE RIGHT SIDE OF THE FUSELAGE AT APPROXIMATELY FS 220.75, STRINGER 5R. REPAIR ACCOMPLISHED. NO TEAR DOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030908002812003090800281CE 2003 9 8 AMWA28 120030818A553111464000069 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV UE163 WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH SRM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20030908002852003090800285NM 2003 9 8 SWAA031934 120030828A53106546532 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND BS 480, FUSELAGE SHEAR TIE CORRODED AT STR 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030908003032003090800303NM 2003 9 8 SWAA031922 120030827A53306545877 BEAR STRAP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED SPECIAL VISIT, FOUND BS 360 BEAR STRAP CRACKED AT STRINGER 4R. REPAIRED BEAR STRAP PER SRM. 2L72 4F RTA16WE 20030908003042003090800304NM 2003 9 8 SWAA031882 120030820A575465C26602223 SKIN BOEING737 7375H4 138449DNM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON OUTBD UPPER SURFACE. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20030908003122003090800312NM 2003 9 8 SWAA031890 120030824A335065C27093 LENS BOEING737 7373Y0 1384671NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 FWD ENTRY DOOR EMERGENCY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030908003192003090800319 2003 9 8 SWAA031897 420030825A2565BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 EEPLS INOP AT OVERWING EMERGENCY EXIT. REPAIRED EEPLS PER MM. 2L72 4F A16WE 20030908003202003090800320NM 2003 9 8 SWAA031898 120030825A53306545767118 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (4 EA) BS 500D, BETWEEN STR 15R AND STR 16R, BS 395 ABOVE STR 15L, BS 773 AT STR 19L AND BS 805 AT STR 19L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030908003262003090800326NM 2003 9 8 SWAA031929 120030828A532065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND 4 EA STRINGER CLIPS CRACKED, BS 500D, STRINGERS 8R AND 7R, BS 500C, STRINGERS 8R AND 7R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030908003282003090800328NM 2003 9 8 SWAA031904 120030826A3350311500 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED RON, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW NR 3 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030908003322003090800332NM 2003 9 8 SWAA031908 120030826A57546573714 SKIN BOEING737 7373H4 1384600NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND NR 4 L/E SLAT DELAMINATED ON UPPER SURFACE OUTBD END. REPAIRED NR 4 L/E SLAT PER SRM. 2L72 4F RTA16WE 20030908003382003090800338NM 2003 9 8 SWAA031932 120030828A3350BR2013 TRACK BOEING737 7372T4 1384492NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C4 CHECK, FOUND SEVERAL EELPS TRACKS LOOSE. SECURED EEPLS TRACKS PER MM. 2L72 4F A16WE 20030908003422003090800342NM 2003 9 8 SWAA031926 120030827A55236959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED C2 CHECK, (SI 11138-55), LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE ATTACH BUSHING/HARDWARE. 2L72 4F RTA16WE 20030908001502003090800150SO 2003 9 8 SWIA200312220 120030726A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN BROKEN A SWIAK NONE O OTHER TXTAXI/GRND HDL 1 NM07569SW 120344 EXIT ROW LIGHT BELOW DOOR AT SEAT 6A BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY AT SEAT 6A. OPS CHECK GOOD. PN: 10-1301-15 2L72 4T RTA31SO 20030908001972003090800197EA 2003 9 8 SWIA200312283 120030719A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 484 LT INTERCOSTAL OB FLANGE LBL 36 AND IB CLIP LBL 27 CRACKED. DISCOVERED DURING C-CHECK, INTERCOSTALS REPAIRED IAW CRJ REO 601R-53-41-059 REV 'A'. 2L72 4F RTA21EA 20030908002582003090800258CE 2003 9 8 AMWA21 120030813A53121144100266 BULKHEAD BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07139ZV UE139 WHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SHELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FWD PRESSURE BULKHEAD AT FS 84 BELOW THE SHELF. THE CRACK RUNS LATERALY 4 INCHES, ON RT LOWER WEB, UNDERNEATH STIFFENER P/N 114-410026-55. 2L72 4T RTA24CE 20030908002622003090800262CE 2003 9 8 AMWA24 120030818A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07178YV UE178 WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20030908003342003090800334 2003 9 8 SWAA031910 420030825A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED C1 CHECK, FOUND BOTH CABIN SVC DOORS EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH SLIDES PER MM. 2L72 4F RTA16WE 20030909000522003090900052EA 2003 9 9 SWIA200312327 120030808A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 CARGO FLOOR SILL PLATE CRACKED AT FS 576.00, LBL 36, WL 73.50. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-690 REV. ''A''. 2L72 4F RTA21EA 20030909000782003090900078SO 2003 9 9 SWIA200312300 120030818A275012064207615 CONTROL HANDLE EMB 120 EMB120ER 3260203SO COCKPIT FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07301YV2899 2899 120301 ON TAXI OUT, FLAPS CONTROL FAULT 3 TIMES. COULD NOT GET FLAPS TO GO TO 15 DEGREES. REMOVED AND REPLACED FLAP HANDLE WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030909000982003090900098WP 2003 9 9 DHL2003873576 120030706A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT INNER WING CTR EXTENDED L/E OUTER PLATING CORRODED ON SEVERAL AREAS, AROUND XW.257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA IAW EODHL-030624, ED-3448. PERFORMED NDT INSPECTION IAW DC8 NDT SPM 6-10-01-001. CLEANED, TREATED AND PRIMED, FABRICATED A REPAIR DOUBLER AND 4 FILLERS. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLERS AND DOUBLER ON RT INNER WING CTR EXTENDED L/E OUTER PLATING, (AROUND STA XW.257.500) USING NEW FASTENERS. 2L74 4F RT4A25 20030909001052003090900105CE 2003 9 9 53305 120030806A2913 POWERPACK BEECH 1900 1900D 1154162CE HYD SYSTEM FAILED A AMWAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CE07144ZV UE144 WHILE ON APPROACH INTO PITTSBURGH PENNSYLVANIA ON FLIGHT 5557 THE CREW SELECTED THE LANDING GEAR DOWN AND THE GEAR DID NOT GO DOWN. THE LANDING GEAR CIRCUIT BREAKER POPPED. THE CREW INFORMED AIR TRAFFIC CONTROL OF MISSED APPROACH AND PROCEEDED FOR A HOLD. TRIED TO RECYCLE THE GEAR AND IT WOULD NOT RECYCLE. THE CREW PERFORMED A MANUAL GEAR EXTENSION PER THE ABNORMAL PROCEDURES CHECKLIST AND ACHIEVED THREE GREEN LIGHTS. AS A PRECAUTION DID A TOWER FLYBY AND REQUESTED EMERGENCY PERSONNEL TO STANDBY. A NORMAL LANDING. MAINTENANCE REMOVED AND REPLACED THE POWER PACK. STILL AWAITING MORE INFORMATION. 2L72 4T RTA24CE 20030909001202003090900120EA 2003 9 9 SWIA200312316 120030801A5320601R3111358 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 FS 280 I/B AND O/B RIGHT FLOORBEAM ATTACH ANGLES RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. ANGLED REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-58 2L72 4F4 FRTA21EA E15NE 20030909001232003090900123SW 2003 9 9 ALGA088783 120030818A5320206064902035S CHANNEL BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL6498 53240 CHANNEL CRACKED LOWER EDGE AND MIDDLE DZUS RECEPTICALES AREA. PROBABLE CAUSE IS ASB407-02-54. REC. DOUBLERS AT RECEPTICALE AREAS. 1G71 3U3 UO H2SW E1GL 20030908002452003090800245 2003 9 8 SWIA200312352 420030826A34178220372154 ADC CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07906SW 7028 STALL TEST WILL NOT TEST PROPERLY. REMOVED AND REPLACED NR 1 ADC. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031029000492003102900049NM 2003 10 29 ASAA0310398 120030506A53107075T6050 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND WEB SHEAR TIE AT BS 277, STRINGER 27L CORRODED. REPLACED SHEAR TIE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031029000592003102900059NM 2003 10 29 ASAA0310500 120030602A53306545778 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 923-925, STRINGER 19R CRACKED. REMOVED DAMAGED SECTION OF SKIN AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031029000622003102900062NM 2003 10 29 ASAA0240220 120030401A532065C2730892 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND AFT CARGO SIDE WALL SUPPORT IS DENTED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000652003102900065NM 2003 10 29 ASAA0340069 120030227A531065C32395 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727F BETWEEN STRINGER 25R AND 26R. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000802003102900080NM 2003 10 29 ASAA0310499 120030602A5347BAC15201430 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 420-500B, RIGHT BUTTOCK LINE 62 CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20031029000922003102900092EU 2003 10 29 KBM2003F00007 120030709A21500600180500847 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE AIR CONDITIONINGBROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH148 2337 AIR CONDITIONING BELT BROKEN. INSPECTED REPLACED A/C BELT AND 7 INCH MOTOR.(K) 1G71 3U3 UNCH9EU E19EU 20031110000512003111000051SO 2003 11 10 RAIA00310270 120031020A3240429513 CONTROL UNIT EMB 145 EMB145 3260210SO BRAKE SYSTEM MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03803HK8204 145077 5295-STL- BRAKE INBOARD INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT. 2L72 4F RTT00011AT 20031110000562003111000056 2003 11 10 P5CA0300979 420031109A341719039254 ADC BOEING747 747200 1384847NM E/E BAY FAILED A P5CAA UNSCHED LANDING O OTHER CRCRUISE 1 WP23524UP 21446 NR 2 CADC FAILED EN ROUTE (AIRTURN BACK). REMOVED AND REPLACED NR 2 CADC, TEST OK PER MM 34-12-00. 2L74 4F RTA20WE 20031110000662003111000066SO 2003 11 10 C2XA03SH443 120031110A711014576058005 STRUCTURE EMB 145 EMB145LR 3260212SO LT COWLING DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE LEFT UPPER COWLING INBOARD EDGE MEMBER WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110000782003111000078NM 2003 11 10 PCAA0311136 120031106A323282970018013 ACTUATOR DHAV DHC8 DHC8102 2809003NM LT GEAR DOOR MALFUNCTIONED A PCAAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA13839EX13590 226 AIRCRAFT 839EX, FLIGHT NR 3698, ROCHESTER, HAD TO PERFORM A SECOND GEAR SWING DUE TO AN AMBER LEFT GEAR DOOR LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. CREW PERFORMED GEAR SWING AND THE LIGHT EXTINGUISHED ON SECOND ATTEMPT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FORWARD GEAR DOOR ACTUATOR AND ALL OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD, AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031110001632003111000163 2003 11 10 SWAA032265 420031015A2565D31591 SLIDE BOEING737 7375H4 138449DNM L1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED RON, FOUND L1 DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031110001682003111000168EU 2003 11 10 MALA030485 120031031A3260 CONNECTOR SAAB SF340 340B 7860101EU RT MLG DISCONNECTED A MALAO OTHER P NO WARNING INDICATION DEDESCENT 1 GL15364PX 340B262 DURING FLIGHT NR 2990, RT MAIN GEAR GREEN LIGHT NOT ILLUMINATING DURING EXTENSION. AFTER SELECTING GEAR HANDLE DOWN RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE. COMPLETED QRH WITH GEAR HANDLE DOWN TRANSIT LIGHT WAS OUT. NO FLIGHT IDLE LIGHT, PULLED OVERRIDE. MAINTENANCE FOUND RT DOWNLOCK CONNECTOR DISCONNECTED. CLEANED AND INSPECTED CONNECTOR PINS AND FOUND TO BE SERVICEABLE. REINSTALLED CONNECTOR AND PERFORMED GEAR SWINGS IAW SF3 AMM 32-30-00-5. RESET FLIGHT IDLE STOP AS REQUIRED. ALL OPS CHECKS WERE GOOD. 2L72 4T RTA52EU 20031110001752003111000175EA 2003 11 10 03293654 120031020A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE OUT OF LIMITS A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 DURING HEAVY INSPECTION A REPAIR TO THE FUSELAGE SKIN WAS MADE AT FS 625-640 AND STRINGER 20-21 ON THE LEFT HAND SIDE. REPAIRED WITH DOUBLER, HI LITE, AND COLLAR. 2L72 4F4 FRTA21EA E15NE 20031110001772003111000177WP 2003 11 10 GTIA030728 120030911A5320 EXPANSION JOINT DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - MAIN CABIN FLOOR PANEL CENTER STATION 886 TO STATION 946, EXPANSION JOINT CRACKED. REMOVED EXPANSION JOINT. FABRICATED EXPANSION JOINT. INSTALLED EXPANSION JOINT. (M) 2L72 4F A6WE 20031110001812003111000181NM 2003 11 10 SWAA032252 120031009A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031110001852003111000185NM 2003 11 10 SWAA032256 120031011A53206545409 WEB BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND BOTH LT/RT FLOOR WEBS CRACKED BETWEEN BS 188 AND BS 196, STR 17. REMOVED AND REPLACED FLOOR WEBS PER SRM. 2L72 4F RTA16WE 20031110001872003111000187NM 2003 11 10 SWAA032232 120031010A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 EEPLS SECTION MISSING AT ROW 15. INSTALLED EEPLS SECTION PER MM. 2L72 4F A16WE 20031110001902003111000190NM 2003 11 10 SWAA032235 120031009A53126546568 BULKHEAD BOEING737 7377H4 1384404NM FUSELAGE ACTIVATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29761RR 27875 DURING SCHEDULED C4 CHECK, FOUND AFT PRESS BULKHEAD BS 1016 OIL CANNED AT STR 16. REPAIRED BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20031110001982003111000198NM 2003 11 10 SWAA032243 120031012A53306552988 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 935-BS 971, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031118000252003111800025NM 2003 11 18 AWXA200301140 120030906A5312 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK A 1.1 INCH CRACK WAS FOUND ON WEB, AFT SIDE OF BS 178 BULKHEAD AT INBOARD SIDE LBL 5.7, WL 189. MAINTENANCE REMOVED EXISTING DOUBLER ON BS 178 BULKHEAD WEB AT INBOARD SIDE LBL 5.7, WL 189; FABRICATED A NEW REPLACEMENT DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG 211, FIG 203. 2L72 4F RTA16WE 20031118000292003111800029NM 2003 11 18 AWXA200301144 120030906A5753BACB30NR6K7 BOLT BOEING737 7373Q8 1384670NM ZONE 500 - LEFT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK CORROSION WAS FOUND ON LT WING INBOARD MID FLAP OUTBOARD CARRIAGE ASSEMBLY BOLTS. MAINTENANCE REMOVED AND REPLACED LT WING INBOARD MID FLAP OUTBOARD CARRIAGE ASSEMBLY BOLTS IAW BMM 20-50-11. 2L72 4F RTA16WE 20031118000352003111800035EU 2003 11 18 AWXA200301150 120030924A5321D5367009924400 FLOOR PANEL AIRBUS320 A320232 3930326EU CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON FLOOR PANEL TIE STRAP (CONNECTING PLATE) FROM Y765 TO Y254 AT FR 24. MAINTENANCE REMOVED CORRODED CONNECTING PLATE FROM Y765 TO Y254 AT FR 24, FABRICATED AND INSTALLED A NEW REPLACEMENT CONNECTING PLATE PER DWG D53670099. 2L72 4F RTA28NM 20031118000472003111800047EU 2003 11 18 AWXA200301162 120030924A5315D53472172201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y1292 FLOORBEAM BETWEEN FORWARD SIDE OF FR 67 TO FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1292 FLOORBEAM FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 23-28 & 39-41, FIG 9-12 & 18. 2L72 4F RTA28NM 20031118000602003111800060EU 2003 11 18 AWXA200301175 120030925A5414D54530052200201 SKIN PANEL AIRBUS320 A320232 3930326EU NR 2 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN. MAINTENANCE REMOVED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-11, FIG 2, 3. 2L72 4F RTA28NM 20031118000652003111800065NM 2003 11 18 03FDEA01629 120030924A5315BAC1518347 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON BS 1130 FLOORBEAM LOWER SECTION LBL 2 - LBL 40 WL 200. REPAIRED FLOORBEAM BS 1130 LOWER CHORD, LBL 65 TO RBL 65 PER FED EX EA 7-5310- 55008. 2L73 4F RTA3WE 20031118000772003111800077 2003 11 18 P5CA0300961 420031007A3433 AUTOLAND SYS BOEING747 747236B 1384804NM COCKPIT MALFUNCTIONED A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23924FT 21730 LOUD SIDE TONE IN F/O INTERPHONE. RERACKED NR 2 LRRA - TRANSCEIVER IAW MM 34-42-00, OPS CHECK OK. NOISE DISAPPEARED. 2L74 4F A20WE 20031118000792003111800079WP 2003 11 18 200391 120030902A78306870992R COMBUST CHAMBER HUGHES369 369E 4470707WP ALLSN 250C 250C20B 03013GL NR 1 ENGINE CRACKED B LS1RO OTHER O OTHER NRNOT REPORTED 1 EA138330P 0330E CAE833998 4 INCH CRACK IN OUTER COMBUSTION CAN AT REINFORCED (ARM PIT) INLET ELBOW. THE CRACK CAUSED A LOSE AND DISRUPTION OF AIRFLOW. THIS AIRFLOW LOSS CAUSED THE NR 1 TURBINE NOZZLE TO OVERHEAT AND BURN IN ONE SPOT. 1G71 3U3 U H3WE E4CE 20031118000932003111800093SO 2003 11 18 SWIA200312482 120031004A3232 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE MLG DOOR MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07566SW 120341 LEFT MAIN LANDING GEAR WOULD NOT RETRACT ON DEPARTURE.ADJUSTED LEFT MAIN LANDING GEAR INBOARD DOOR ACTUATOR. OPS CHECKS GOOD.. 2L72 4T4 TRTA31SO E20NE 20031118000982003111800098NE 2003 11 18 QXEA200301224 220031007A7200 ENGINE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE NR 1 FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09354PH 498 ON FLIGHT 2117 FLIGHT ATTENDENT REPORTED SMOKE IN CABIN. REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031118001042003111800104NM 2003 11 18 AWXA200301180 120030911A5350149N7664 SUPPORT ANGLE BOEING757 7572S7 1384962NM WING TO BODY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK A .75 INCH CRACK WAS FOUND ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 21 RT. MAINTENANCE CUT OUT DAMAGE ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 21 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-71, PG 203 FIG 202. 2L72 4F RTA2NM 20030908002682003090800268SO 2003 9 8 SWIA200312359 120030826A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07296SW75 75 120325 WHEN RETRACTING FLAPS ON CLIMBOUT, RECEIVED A CONTROL FAULT AND THE OVERHEAD PAIR OF FLAP BARS FLASHING. RESET VIA QRH PROCEDURE; WORKED FINE REST OF FLIGHT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030908002902003090800290NM 2003 9 8 SWAA031939 120030828A53306552988 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG AT BS 927, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030909000222003090900022EA 2003 9 9 SWIA200312333 120030823A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913SW 7597 FS 280 RT FLOORBEAM RBL 9.0 INBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601R-31113-58. 2L72 4F RTA21EA 20030909001312003090900131EA 2003 9 9 SWIA200312348 120030828A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07441SW4463 4463 7602 STAB CH2 HSTA C/B POPPED WHEN POWERING A/C UP. WOULD NOT RESET. REMOVED AND REPLACED HSTC MOTOR CONTROL UNIT AND ACTUATOR IAW 27-42-01. OPS CHECKS GOOD. MCU P/N: 7062-3 S/N OFF: 113. 2L72 4F RTA21EA 20030909001332003090900133CE 2003 9 9 S2YA03020 120030602A2720LMD500P RELAY BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RUDDER FAILED A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1392SK UE92 BEFORE TAKEOFF OF FLIGHT 1226, THE RUDDER BOOST ACTIVATED. THE CREW ABORTED THE TAKEOFF. THE SYSTEM WAS PUT ON MEL AND THE FLIGHT CONTINUED. ON 6/16 THE MECHANIC CLEARED THE MEL BY REPLACING A RELAY AND REPAIRING SOME CHAFED WIRES TO THAT RELAY. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. 2L72 4T3 TRTA24CE E2NE 20030909001432003090900143SO 2003 9 9 SWIA200312370 120030902A3244314461 TIRE EMB 120 EMB120ER 3260203SO MLG BLOWN A SWIAO OTHER O OTHER LDLANDING 1 NM07220SW 120288 ALL 4 MAIN TIRES BLEW ON LANDING. REMOVED AND REPLACED ALL 4 MLG WHEEL ASSY'S PER MM 32-44-02 AND C/W ST12-311. P/N: 3-1446-1, NR 1 S/N ON: 0966, S/N OFF: 1789, NR 2 S/N ON: 0618, NR 3 S/N ON: 0627 S/N OFF: 1101, NR 4 S/N ON: 0005, S/N OFF: 1729. 2L72 4T RTA31SO 20030909001472003090900147 2003 9 9 BAQA088843 420030823A34570110028010 GPS BEECH 100 100BEECH 1152916CE COCKPIT FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03777GS B241 FAILED RIGHT OUT OF BOX. ORDERED REPLACEMENT ON 8/25/2003. REPLACEMENT UNIT HAD NOT BEEN RECEIVED AT TIME OF CORE RETURN. 1L72 3T A14CE 20030909001492003090900149SW 2003 9 9 AGQA088876 120030812A7920RG17350D PUMP BELL 204 UH1H 1181407SW LYC T53 T5313A 41549NE ENGINE OIL BROKEN B AGQAK NONE O OTHER ININSP/MAINT 1 EA1353AG 7221588 PUMP PRODUCING FLUXUATING OIL PRESSURE 1G71 4U4 U EXPA1G71E17EA 20030909001542003090900154NM 2003 9 9 S2YA03023 120030624A3000 SEAL DORNERDO32 DO328300 NM ICE/RAIN PROTECTLOOSE A S2YAA UNSCHED LANDING O OTHER CRCRUISE 1 GL13354SK 3126 DURING FLIGHT 2015, THE CREW AND PASSENGERS NOTICED A LOUD BANGING SOUND OUTSIDE THE AIRCRAFT. THERE WERE NO COCKPIT INDICATIONS. THE CREW SLOWED THE AIRCRAFT BUT THERE WERE NO CHANGE IN THE SOUND. THE CREW DIVERTED. OUTSTATION MECHANIC FOUND A FOUR INCH PIECE OF WEATHER STRIPPING THE BE SOURCE OF THE NOISE. THE STRIP WAS REMOVED AND PUT ON MCO. THE AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER DISCREPANCIES. 2H72 4T RTA55NM 20030909001662003090900166EU 2003 9 9 BAQA088822 120030815A62401179405303 INDICATOR BOLKMS117 BK117B1 5626012EU TRIPLE TACH MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE484 7219 TRIPLE TACH N2 WILL NOT GO ABOVE 100 PERCENT (LAGS BEHIND). REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030909001672003090900167SO 2003 9 9 SWIA200312310 120030822A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07223SW7385 7381 120291 OUTBOARD FLAPS CONTROL FAULT FOR ABOUT 30 SECONDS WHEN RETRACTING FROM 15 DEGREES. REPLACED FCU WITH SERVICEABLE UNIT. SYSTEM OPS CHECKS OKAY. 2L72 4T RTA31SO 20030909001862003090900186EU 2003 9 9 BAQA088825 120030822A2422SPS1307 INVERTER AEROSPSA365 SA365N 8680669EU AC SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 6036 INVERTER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030909002182003090900218EU 2003 9 9 BAQA088668 120030812A65204639003007 TRANSMISSION BOLKMS117 BK117A4 5626017EU TAIL ROTOR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA039024Z2987 7134 TAIL ROTOR TRANSMISSION HAS BLACK PASTY RESIDUE ON CHIP PLUG WITH 3 SLIVERS OF FERROUS METAL APPROXIAMATELY 1/4 INCH LONG EACH. 1G72 3U H13EU 20030909002262003090900226WP 2003 9 9 DHL2003604681 120030616A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT MLG W/W SPOILER AND AILERON ACTUATING MECH SUPPORT Z-FORMER CORRODED AT STA 857.000, LBL-54. REMOVED CORROSION ON FORMER IAW SRM 51-1-8 PG 17, 18. FOUND OUT LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED Z-FORMER IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FORMER IAW SRM 53-2-0 PG 1-2. CLEANED, TREATED AND PRIMED NEW FORMER IAW SRM 51-1-8B. INSTALLED NEW FORMER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030909002282003090900228NM 2003 9 9 DHL2003745018 120030821A5210 HANDLE BOEING727 727224 1384076NM PAX DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01745DH 20665 DURING LANDING ROLLOUT FORWARD ENTRY LIGHT ILLUMINATED AND STAYED ON. DOOR HANDLE WAS SLIGHTLY AJAR. ADJUSTED FORWARD ENTRY DOOR IAW B-M/M 52-11-01. NO DEFECTS NOTED. 2L73 4F A3WE 20030909002302003090900230WP 2003 9 9 DHL2003604573 120030606A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OTBD SKIN SEGMENT FLAP PLATING CRACKED 2.00, XW 160.000 - XW 169.000. CUT OUT DAMAGED AREA AND FABRICATED SPLICE AND NEW SKIN SEGMENT IAW SRM 57-2-0 FIG 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED SPLICE AND NEW SKIN SEGMENT IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030909002362003090900236WP 2003 9 9 ABXA030316 120030717A5347591076913 SEAT TRACK DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 SEAT TRACK RIGHT BUTT LINE 34 LOWER INBOARD LEG WAS CORRODED. REPLACED SECTION OF TRACK STA 917 - 931 LEFT BUTT LINE 34 IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20030909002392003090900239WP 2003 9 9 ABXA030336 120030801A5210995576311 WEB DOUG DC9 DC941 302207NWP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 MAIN ENTRY DOOR INTERIOR WEB JUST FORWARD OF DOOR HANDLE WAS CRACKED. REPLACED WEB IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030909002492003090900249EA 2003 9 9 A6WA20030124 120030820A2910 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A A6WAA UNSCHED LANDING K FLUID LOSS TOTAKEOFF 1 GL31401AW 7280 ON TAKEOFF, NR 2 HYDRAULIC SYSTEM QUANTITY DECREASED TO 0 PERCENT, NR 2 EDP, RAN 11 MINUTES AT 0 PERCENT RETURNED TO LNK. REMOVED AND REPLACED NR 2 SYSTEM HYD FILL LINE. (M) 2L72 4F RTA21EA 20030908002352003090800235NE 2003 9 8 MALA030343 220030719A7200200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER CRCRUISE 1 GL15532XJ E2366 DURING CRUISE ON FLIGHT NR 3421 OIL QUANTITY DROPPED TO ZERO OIL TEMP ROSE TO 180 DEGREES AND OIL PSI 110. SHUTDOWN ENGINE AS PRECAUTION. A/C DIVERTED TO GFK. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE PN ON/OFF 2-003-040-15, SN/ON P07860 SN/OFF P07877 IAW J/C 71-00-502.OPS AND LEAK CHECK GOOD. 2H74 4F4 FRTA49EU E6NE 20030908002942003090800294 2003 9 8 SWAA031943 420030831A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. SECURED SLIDE INTO CONTAINER PER MM. 2L72 4F RTA16WE 20030908002962003090800296 2003 9 8 SWAA031914 420030827A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER AS DOOR WAS OPENED. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030909001682003090900168EU 2003 9 9 BAQA088805 120030821A28221176415103 PUMP BOLKMS117 BK117A4 5626017EU FUEL BOOST INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911WJ813 7050 FUEL BOOST PUMP HAS INTERMITTENT FAIL LIGHT. VERY NOISY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030909001822003090900182SW 2003 9 9 ALGA088799 120030819A6220407310101101 BEARING BELL 407 407 1182206SW M/R HUB ASSY SEPARATED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03457AL4167 LK7 53151 FOUND TOTAL SEPARATION OF ELASTROMER. REPLACED SHEAR BEARING. 1G71 3U O H2SW 20030909001892003090900189WP 2003 9 9 IXXA0300052O 120030729A2520 CURTAIN DOUG DC8 DC871F 302199DWP NLG WW UNSECURE A IXXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW11828BX81049912 45993 AFTER TAKEOFF FROM KBDL AND AFTER GEAR RETRACTION, THERE WAS A VIBRATING NOISE COMING FROM NOSE WHEEL WELL. CREW RETURNED TO KBDL AND LANDED WITHOUT INCIDENT. DURING INSPECTION OF THE NOSE GEAR AREA MAINTENANCE FOUND NOSE WHEEL CURTAIN UNSNAPPED. MAINTENANCE INSPECTED THE NOSE GEAR WHEEL ASSEMBLY FOR EXCESSIVE PLAY, NONE WAS FOUND. THE CURTAIN WAS SECURED IN ACCORDANCE WITH ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030909002172003090900217WP 2003 9 9 ABXA030332 120030801A57539957578509 SKIN DOUG DC9 DC941 302207NWP T/E FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 BULGE IN SKIN, CUPPED FASTENERS, FLAP LOWER SURFACE AT NR 3 EXPANSION JOINT. REPLACED LOWER SKIN IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030909002582003090900258EU 2003 9 9 2003F00548 120030812A612089548119 PITCH CONTROL BAG JETSTMJETSTM3101 1500215EU LT ENGINE LEAKING A B16AE ENGINE SHUTDOWN KE FLUID LOSS VIBRATION/BUFFET CRCRUISE 1 NE05529PA 771 FLT 3525 - BGR - OIL CAP LIGHT CAME ON DURING FLIGHT. LESS THAN 50 PSI ON LEFT ENGINE, FOLLOWED BY 10 PERCENT LOSS OF TORQUE AND SLIGHT VIBRATION. INITIATED ENGINE SHUT DOWN. FOUND OIL LEAKING FROM FITTING ON PPC. REMOVED AND REPLACED LEFT PPC IAW GARRETT MM 72-10-02. LEAK CHECK AND OPS CHECKED GOOD. (M) 2L72 4T RTA21EU 20030909002752003090900275NE 2003 9 9 RAIA00307196 220030721A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LEFT POWER LOSS A RAIAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 CE03567HK 41085 75073 5466-MEM- ON TAXI OUT LEFT ENGINE SPOOLED DOWN, MAINTENANCE PERFORMED OPS CK IAW MAINTENANCE MANUAL WITH NO DEFECTS NOTED. 2L72 4T4 TRTA41NM E18NE 20030909002772003090900277SO 2003 9 9 RAIA00307198 120030726A783053990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER DEFECTIVE A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03815HK132 145048 5700-STL- RIGHT ENGINE T/R DISAGREE. MAINTENANCE DEFERRED IAW MEL, SUBSEQUENTLY CLEARING THE DMI BY REPLACING THE NR 2 OB STOW SWITCH. 2L72 4T RTT00011AT 20030909002812003090900281EA 2003 9 9 QXEA200300950 120030802A261247388904 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA FIRE WARNING MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX186 186 10045 SBA- ON FLIGHT 2453 FIRE SYSTEM FAULT STATUS MESSAGE ON. FIRE SYSTEM DOES TEST OKAY. REMOVED AND REPLACED FIDEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030909002852003090900285NM 2003 9 9 QXEA200300954 120030804A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM AFT PAX DOOR MALFUNCTIONED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09411QX 4055 GEG- ON FLIGHT 2354 AFT PASSENGER STAIRS WILL NOT DEPLOY. DEPLOYED AIRSTAIRS AND RETRACTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030909002872003090900287 2003 9 9 QXEA200300957 420030807A3442MI5853505 TRANSCEIVER DHAV DHC8 DHC8202 2809007NM WEATHER RADAR FAILED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09345PH9459 652 476 PSC- ON FLIGHT 2115 RETURNED TO FIELD DUE TO WEATHER RADAR INOPERTIVE. WHEN WX/C SELECTED, SCREEN FLASHES AND THEN GOES BLANK. REMOVED AND REPLACED WEATHER RADAR R/T. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030910000202003091000020WP 2003 9 10 DHL2003604552 120030502A5522 SKIN DOUG DC8 DC873F 302199FWP LT ELEVATOR CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT ELEVATOR L/E UPPER EXTERNAL SKIN DEFLECTED AT XE.55.06 (OIL CANNING). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-4-1 FIG 1. REMOVED DEFLECTED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN IAW SRM 55-1-0 PG 1, SRM 55-4-1 FIG 1. CLEANED, TREATED AND PRIMED AREA AND SKIN INNER PART IAW SRM 51-1-8B. INSTALLED NEW SKIN IAW SRM 51-1-21 PG 1. FOR WEIGHT AND BALANCE SEE N/R 4038. 2L74 4F RT4A25 20031002001082003100200108NM 2003 10 2 QXEA200301093 120030830A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CRACK ON FIREWALL OF NR 1 NACELLE INBOARD SIDE. REPAIRED IAW DHC-8 RD 8-54-1840 AND HORIZON AIR EA 2-54-180. 2H72 4T RTA13NM 20031002001102003100200110NM 2003 10 2 QXEA200301095 120030826A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 6 SEAT TRACK AFT TWO LUGS HAS LIGHT SURFACE CORROSION ON INSIDE OF BORE. REPAIRED IAW DHC-8 SRM 51-20-16 AND EA 2-53-468. 2H72 4T RTA13NM 20031002001122003100200112NM 2003 10 2 QXEA200301097 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 2 SEAT TRACK IS CORRODED BELOW RIGHT HAND LUG ONE INCH FORWARD OF STATION X488.5. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031002001292003100200129NM 2003 10 2 AWXA200301040 120030828A532069265552 ANGLE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .1875 INCH CRACK WAS FOUND ON ATTACH ANGLE AFT OF L-1 DOOR CUTOUT BS 348.20, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED A NEW REPLACEMENT ATTACH ANGLE IAW DWG 69-26555; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 39, FIG. 11. 2L72 4F4 FRTA16WE E2EA 20031002001542003100200154NM 2003 10 2 03FDEA01517 120030911A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 AFT CARGO FRAME DENTED BS 950F AT STR 23L. 2L73 4F RTA3WE 20031002001552003100200155NM 2003 10 2 03FDEA01500 120030911A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON FLOORBEAM UPPER CHORD, STA 340, RBL 4 WL 208. 2L73 4F RTA3WE 20031002001582003100200158EA 2003 10 2 SWIA200312378 120030905A322016050105 STRUT CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07588SW 7069 ON CLIMBOUT, WHEN LANDING GEAR LEVER WAS SELECTED UP, THE NOSE GEAR DID NOT RETRACT. COMPLIED WITH QRH AND RECYCLED GEAR, STILL NO NOSE GEAR RETRACTION. RETURN TO FIELD. REMOVED AND REPLACED NOSE LANDING GEAR AND DRAG BRACE ASSY IAW MM 32-21-01. SN OFF: DCL88/95 2L72 4F RTA21EA 20031002001592003100200159EA 2003 10 2 SWIA200312379 120030907A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07903SW 7425 STAB TRIM CHANNEL 1 INOPERATIVE. REMOVED AND REPLACED FO'S STAB TRIM DISCONNECT SWITCH AND STAB TRIM PANEL IAW CRJ MM 27-41-15. OPS CHECKS GOOD. PANEL PN: 601R51707-9 SWITCH PN: 996-0013 2L72 4F RTA21EA 20031002001622003100200162SO 2003 10 2 SWIA200312382 120030902A5753 BRACKET EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE FLAP ROLLER CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RT INBOARD FLAP ROLLER BRACKET IS CRACKED. REPLACED RT INBOARD FLAP OUTBOARD GAP PANEL ROLLER BRACKET. CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20031002001642003100200164EA 2003 10 2 SWIA200312384 120030905A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07590SW4460 4460 7077 ''FLAPS FAIL'' CAUTION MESSAGE IN FLIGHT WITH FLAPS 0. (OCCURED ON DESCENT WITHOUT FLAP HANDLE BEING MOVED.)REMOVED AND REPLACED LEFT BPSU, REF MM 27-51-10. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031002001652003100200165 2003 10 2 SWIA200312385 420030902A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07295SW 120322 CAPTAIN SIDE AUTOPILOT INOP - WILL NOT MAINTAIN ALT OR PITCH IN CLIMB. REPLACED ELEVATOR AUTOPILOT SERVO. OPERATES NORMALLY PER MM 22-11-00. 2L72 4T RTA31SO 20031001000212003100100021NM 2003 10 1 QXEA200301082 120030826A5542 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 300 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 THREE DENTS ON RIGHT SIDE OF RUDDER TRAILING, FOUR TO SEVEN INCHES FROM TOP AFT OF FORWARD SPAR. REPAIRED IAW DHC-8 SRM 55-40-16, 51-20-16, 51-20-36 AND 51-20-26. 2H72 4T RTA13NM 20031118001092003111800109NM 2003 11 18 AWXA200301185 120030912A5321144N533017 FLOOR PANEL BOEING757 7572S7 1384962NM FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK CABIN FLOOR PANEL L-1 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1. 2L72 4F RTA2NM 20031118001192003111800119NM 2003 11 18 AWXA200301195 120030912A5321144N533013 FLOOR PANEL BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK CABIN FLOOR PANEL K-3 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 146N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1. 2L72 4F4 FRTA2NM A12EU 20031119000062003111900006WP 2003 11 19 ABXA030385 120031008A251056410321 SEAT DOUG DC8 DC863 302198AWP COCKPIT DEFECTIVE A ABXAO OTHER O OTHER CLCLIMB 1 GL23817AX94 45928 FLIGHT ENGENEERS SEAT FELL DURING TAKE OFF AND INITIAL CLIMB. VERTICAL HOLD INOPERATIVE WITH SEAT POSITIONED FORWARD AT A 45 DEGREE ANGLE. SEAT NOT SAFE FOR FLIGHT. MAINTENANCE REPLACED FLIGHT ENGINEER'S SEAT ASSEMBLY AS REQUIRED IAW DC-8 AMM. OPS CHECKED GOOD. 2L74 4F 4A25 20031119000082003111900008WP 2003 11 19 BBC2003F00000 220030915A7261 HOUSING BEECH 100 B100 1152919CE GARRTTTPE331TPE3316252B 01514WP OIL PUMP CRACKED E BBCAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA03264PA271 02140500101 BE86 P27175 AUGUST 22, 2003 ENGINE LOST OIL PRESSURE INFLIGHT, PILOT COMMANDED SHUTDOWN, AIRCRAFT LANDED. SUBSEQUENT TEARDOWN OF GEARBOX REVEALED CRACKED OIL PUMP HOUSING. PUMP HOUSINGS ARE NOT STRONG ENOUGH DESIGN OR ALLOY. 1L72 4T4 T A14CE E2WE 20031119000102003111900010NM 2003 11 19 UPS03241369 120030915A5754 RIB BOEING727 7271A7C 13840X2NM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 INSPECTION TYPE:C NR 6 SLAT IB TRACK IB FLAP RIB CRACK AT FWD CORNER NR 6 FLAT IB TRACK REMOVED IAW OHM 57-51-51 REPAIR CARRIED OUT IAW SRM 51-40-3. NR 6 SLAT IB TRACK INSTALLED IAW OHM 57-51-51. FUNCTION TEST CARRIED OUT IAW MM 27-81-00. OPS. OK 2L73 4F A3WE 20031119000152003111900015WP 2003 11 19 UPS03841372 120030920A5712 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 653.75, STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2 2L74 4F4 FRT4A25 E2GL 20031119000182003111900018WP 2003 11 19 UPS03841376 120030924A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE MAIN CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, SEAT TRACK CORRODED BEYOND LIMITS AT STA. 1188 AT RBL 60. REMOVED SEAT TRACK SECTION BETWEEN STA. 1070 TO 1210, FABRICATED AND INSTALLED REPLACEMENT SECTION I.A.W. SRM. 53-2-3 FIG. 14 2L74 4F4 FRT4A25 E2GL 20031119000232003111900023NE 2003 11 19 00116 220031007A7200 ENGINE LEAR 24 24 5170302CE GE CJ610 CJ6104 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05222TW 24161 240372 PILOT REPORTED LT ENGINE FLAMMED OUT WHILE CLIMBING FROM FL420 TO FL430, DECENT TO RELIGHT ALTITUDE, RELIGHT NORMAL AND CONTINUED TO DESTINATION. WILL UPDATE AFTER MAINTENANCE.NO DEFECTS NOTED. 2L72 4J4 J A10CE 1E16 20031119000722003111900072WP 2003 11 19 ABXA030391 120030923A533059122851 DOUBLER DOUG DC9 DC932F 3022067WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 WINDOW INTERIOR DOUBLER CRACKED FORWARD LOWER CORNER, F.S. 579 RIGHT. REPAIRED DOUBLER IAW DC-9 SRM AND DWG K05159. 2L72 4F A6WE 20031119000822003111900082NM 2003 11 19 QXEA200301265 120031010A3060 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 400 ILLUMINATED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09401QX 4031 ON FLIGHT 2374 PROP DE-ICE CAUTION LIGHT ILLUMINATED AFTER PROPS BROUGHT OUT OF FEATHER. RAN CHECKLIST, NO HELP. COMPLIED WITH DHC-84 SL-31-001 R11. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031119000962003111900096EU 2003 11 19 AWXA200301216 120030924A5320D5347047720600 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LT PROFILE BETWEEN FR 57 AND FR 58. MAINTENANCE REMOVED DAMAGED LT PROFILE BETWEEN FR 56 AND FR 58; INSTALLED NEW REPLACEMENT PROFILE IAW A320 SRM 51-42-11, PG. 21-22, FIG. 8, PG. 8-10, FIG. 2, AND PG. 12, FIG. 3. 2L72 4F RTA28NM 20031110002012003111000201 2003 11 10 SWAA032227 420031007A2565 SLIDE BOEING737 7377AD 1384502NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20031119001062003111900106NM 2003 11 19 CALA0300593 120031013A5420 CHANNEL BOEING737 737524 1384721NM LT PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714653 28914 INSPECTION FOUND A 1INCH CRACK IN LT PYLON RT SIDE VERTICAL CHANNEL THAT FORWARD END PANEL NR 5843R AND AFT END OF PANEL NR 5842R ATTACHES TO. A NEW SPLICE PLATE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20031119001092003111900109NM 2003 11 19 C1HA200397013 120031013A3350 BATTERY PACK BOEING727 727270 138408PNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 MID CABIN FLOOR EMERGENCY PATH LIGHTING INOP. REMOVED AND REPLACED FORWARD FLOOR POWER SUPPLY AND BATTERY PACK IAW 727 MM 33-50-23. FLOOR EMERGENCY PATH LIGHTING OPS. CHECKS NORMAL. 2L73 4F RTA3WE 20031119001132003111900113EU 2003 11 19 2003UALA00741 120031003A5520 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ELEVATOR CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29402UA 439 INDICATIONS OF WATER INGRESS WERE FOUND IN 4 AREAS. ALL AREAS WERE APPROX 2.5 X 2 INCHES AND WERE APPROX 3 INCHES FROM THE TRAILING EDGE. THE FIRST AREA WAS ON THE LT UPPER SURFACE 102 INCHES FROM THE INBOARD EDGE. THE OTHER 3 AREAS WERE ON THE LT LOWER SURFACE. 2L72 4F4 FRTA28NM E40NE 20031119001192003111900119NM 2003 11 19 2003UALA00748 120031006A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 STRINGER DENTED AT STATION 1600, STRINGER 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031119001292003111900129NM 2003 11 19 2003UALA00761 120031005A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 FUSELAGE SKIN GOUGED AT STA 737 STR 1L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031119001362003111900136CE 2003 11 19 16082 120031010A2133 OUTFLOW VALVE CESSNA500 550 2076604CE CABIN PRESSURE FAILED E ESUAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03120JP 5500468 THE AIRCRAFT, AFTER DEPARTURE FROM SUS, WAS UNABLE TO PRESSURIZE THE CABIN. THE AIRCRAFT RETURNED TO SUS. OBTAINED A FERRY PERMIT TO RETURN TO AFJ. THE PROBLEM COULD NOT BE DUPLICATED. THE OUTFLOW VALVE AND SQUAT SWITCH WAS CHECKED. 1L72 4F A22CE 20031119001382003111900138WP 2003 11 19 MWEA030418 120031013A53215930563505 FLOORBOARD DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE CABIN GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 CABIN FLOORBOARD LEFT SIDE BETWEEN STATION 1250-1309 HAS A GOUGE IN THE CENTER AREA. REPAIRED FLOORBOARD. 2L72 4F4 F A6WE E2EA 20031120000042003112000004SO 2003 11 20 SWIA200312489 120030904A5414 CLIP EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07218SW 120287 RIGHT NACELLE FLAP WELL, OUTBOARD SKIN SUPPORT CLIP IS CRACKED OUT OF LIMITS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT CLIP OUTBOARD IN RIGHT NACELLE FLAP WELL PER SRM 51-40-02. 2L72 4T RTA31SO 20031120000072003112000007 2003 11 20 SWIA200312492 420031009A22166225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07566SW8049 8049 120341 ELECTRIC TRIM FAILED ON BOTH SIDES. INSTALLED A SERVICEABLE SERVO IAW 27-00-06 AND OPS CHECK GOOD. P/N ON 622-5734-002, S/N ON 7105 OFF 5806. 2L72 4T RTA31SO 20031120000092003112000009NM 2003 11 20 QXEA200301236 120030927A5320 STRUCTURE DHAV DHC8 DHC8202 2809007NM ZONE 700 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 LEFT HAND MAIN LANDING GEAR WHEEL WELL OUTBOARD TIRE BUBBLE HAS POSSIBLE CRACK IN RADIUS AT FORWARD INBOARD CORNER. REPAIRED IAW DHC-8 SRM 51-00-06 AND 51-40-11. 2H72 4T RTA13NM 20031120000182003112000018NM 2003 11 20 AWXA200301227 120030922A532065C10592156 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT UPPER AFT LEG BS 963, RBL 40, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 963, RBL 40, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51, PG 111, FIG 101. 2L72 4F RTA16WE 20031120000212003112000021NM 2003 11 20 AWXA200301230 120030925A5312651630016 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD VERTICAL WEB AT LIGHTENING HOLE RBL 17, WL 184. MAINTENANCE CUT OUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB AT RBL 17, WL 184; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED REPAIR DOUBLER AND NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG 288L-288Z, FIG 212. 2L72 4F RTA16WE 20031120000522003112000052EA 2003 11 20 SWIA200312500 120031013A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07405SW5934 5934 7029 SPOILERONS FAULT MESSAGE AND FLIGHT SPOILERS FAULT - LEFT SPOILERON MESSAGE. REMOVED AND REPLACED NR 1 AND NR 2 SECU IAW 27-61-05. OPS CHECKS GOOD IAW 27-64-00. P/N OFF: 49-164-06, S/N OFF: 01397, S/N ON: 01455. 2L72 4F RTA21EA 20031120000612003112000061NM 2003 11 20 QXEA200301250 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 9 SEAT TRACK TOP FLANGE IS NICKED 9 INCHES FORWARD OF STATION X545.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-784. 2H72 4T RTA13NM 20031120000782003112000078NE 2003 11 20 NACA20030115 220031014A8530356993 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 18 GALLED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL0343872610 610 533294 55337 NR 1 ENGINE SHUT DOWN DUE TO DOUBLE SHORTED SECONDARY NR 18 CYLINDER. REPLACED NR 18 CYLINDER. OP CHECKED GOOD. 2L74 4R4 R A781 5E8 20031120000822003112000082EU 2003 11 20 MALA030457 120031010A5311 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN CWA, FOUND FRAME AT STA 225 CORRODED. COMPLETED REPAIR IAW EO NR 53182. A/C RELEASE DATE 10/12/2003. REF 409 NR 195723 FOR ADDITIONAL DETAIL. 2L72 4T4 TRTA52EU E8NE 20031120000842003112000084EU 2003 11 20 MALA030453 120031010A5220 WIRE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE SAFETY WIRE BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15420XJ 340B420 SAFETY WIRE IS BROKEN ON RIGHT FRONT EMERGENCY EXIT. MSP MAINTENANCE RE-SAFTIED RT FWD EMERGENCY EXIT COVER AS REQUIRED. 2L72 4T4 TRTA52EU E8NE 20031120001032003112000103EU 2003 11 20 03286309 120031013A5220 HANDLE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY EXIT LACK OF LUBE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27309UE 41022 DURING INSPECTION THE LT EMERGENCY EXIT HATCH HANDLE WAS FOUND STICKING. MAINTENANCE PERSONNEL LUBRICATED THE EMERGENCY HATCH HANDLE. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031120001042003112000104NM 2003 11 20 CALA0300594 120031014A5754 SKIN BOEING737 7373T0 1384582NM NR 6 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A .7500 INCH CRACK IN NR 6 SLAT LOWER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20031120001052003112000105NM 2003 11 20 CALA0300596 120031007A5330 DOUBLER BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733608 27321 INSPECTION FOUND THE EXTERNAL POWER DOOR CUTOUT SKIN DOUBLER CRACKED AT THE FORWARD LOWER CORNER. THE SKIN DOUBLER WAS REPAIRED IAW ECRA 5330-03290. IN ORDER TO VERIFY CRACK REMOVAL IN THE DOUBLER, THE II-SECTION(EXTRUSION) REQUIRED REMOVAL. THE II-SECTION AND THE SKIN DOUBLER WERE DAMAGED DURING REMOVAL REQUIRING TRIM OF THE SKIN DOUBLER AND REMOVAL OF THE II-SECTION UPPER FLANGE. THE II-SECTION AND ASSOCIATED SKIN DOUBLER WERE REPAIRED IAW ECRA 5330-03289. 2L72 4F RTA16WE 20031120001182003112000118NM 2003 11 20 SWAA032456 120031106A53116546546 BELTFRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FWD LEG OF BELTFRAME BS 727D RBL 4. REPAIRED PER SRM. 2L72 4F RTA16WE 20031120001252003112000125NM 2003 11 20 AWXA200301450 120031111A53206554862504 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL BETWEEN BS 1016 TO BS 1040, LBL 7 TO LBL 15, WL 208.1. MAINTENANCE REMOVED CRACKED INTERCOSTAL BETWEEN BS 1016 TO BS 1040, LBL 7 TO LBL 15; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-54862; INSTALLED REPAIR PART IAW SRM 51-40-02 FIG 3, 8 & 12. 2L72 4F RTA16WE 20031120001302003112000130NM 2003 11 20 AWXA200301455 120031104A531069353509 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT SHEAR TIE AT BS 500A, STR 28 LT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 500A, STR 28 LT; INSTALLED NEW REPLACEMENT SHEAR TIE IAW SRM 51-40-02 FIG 4 PG 38. 2L72 4F RTA16WE 20031120001332003112000133NM 2003 11 20 AWXA200301458 120031029A575365C2630934 STIFFENER BOEING737 7373G7 1384595NM NR 6 TE FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 DURING C-13 CHECK A .375 INCH CRACK WAS FOUND NR 6 FLAP TRACK INNER STIFFENER AT WBL 191. MAINTENANCE REMOVED DAMAGED STIFFENER AT WBL 191; FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20031121000072003112100007CE 2003 11 21 AMWA77 120031104A5230129400035131 RISER BEECH BEECH 1900 1900D 1154162CE AIRSTAIR DOOR CRACKED A AMWAO OTHER O OTHER ININSP/MAINT 1 CE07127YV UE127 WHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE CARGO DOOR UPPER AFT GAS SPRING ASSEMBLY BRACKET WORKING RIVETS. 2L72 4T RTA24CE 20031121000142003112100014NM 2003 11 21 SWAA032464 120031106A3350A170033 STRAP BOEING737 7373Y0 1384671NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C2 CHECK, FOUND FWD OB EMERGENCY LIGHT LOWER STRAP BROKEN. REMOVED AND REPLACED STRAP PER MM. 2L72 4F RTA16WE 20031121000202003112100020NM 2003 11 21 SWAA032483 120031109A53126516300 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT BS 178 BULKHEAD WEB LBL 7, WL 213 AND LBL 5, WL 213. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20031121000212003112100021NM 2003 11 21 AWXA200301461 120031112A5240 PANEL BOEING757 7572S7 1384962NM GOUND POWER LOOSE A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28905AW 23567 ON TAKEOFF ROLL AT LAS EN ROUTE FOR JFK THE TOWER ADVISED FLIGHT CREW A PANEL WAS OPEN, TAKEOFF WAS REJECTED AT LOW SPEED. TAXIED BACK TO RAMP AND MAINTENANCE SECURED THE FORWARD GROUND POWER PANEL. TAXIED BACK TO RUNWAY, DEPARTED WITHOUT FURTHER EVENT. 2L72 4F RTA2NM 20031121000252003112100025NE 2003 11 21 VNAA0311002 220031110A73208110994L28 HMU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ENGINE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07423JS3968 3032 DURING TAKEOFF, THE AIRCRAFT FAILED TO PRODUCE TAKEOFF TORQUE AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE HYDROMECHANICAL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031121000292003112100029CE 2003 11 21 DXTA200300162 120031116A7830 CONTROL LEVER CESSNA500 560CESSNA 2076750CE THRUST REVERSER LOOSE E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07326QS 5600526 RIGHT HAND THRUST REVERSER LEVER VERY LOOSE, DEPLOYED BY ITSELF DURING TAXI. INSPECTED ENGINE CONTROL AND THRUST REVERSER LEVER SPRING PLUNGER LOOSE, TIGHTEN RT THRUST REVERSER LEVER SPRING PLUNGER IAW CE560 MAINTENANCE MANUAL CHAPTER 78-31-00, OPS CHECK GOOD. 2L72 4F RTA22CE 20031121000332003112100033WP 2003 11 21 ABXA030445 120031118A561059124261 WINDOW DOUG DC9 DC941 302207NWP COCKPIT STIFF A ABXAO OTHER O OTHER NRNOT REPORTED 1 GL23952AX 47615 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. MAINTENANCE OPS CHECKED WINDOW ON GROUND. OPS CHECKED GOOD IAW DC9 MM 56-10-03. 2L72 4F A6WE 20031121000352003112100035WP 2003 11 21 IXXA0300072O 120031108A36009799086 PRECOOLER DOUG DC8 DC871F 302199DWP ENGINE CRACKED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11822BX868364 45813 DURING CLIMB FROM KGSO TO KTOL NR 2 ENGINE PNEUMATIC SYSTEM OVERHEATS WITH LOW OR HIGH STAGE BLEED WITH CLIMB POWER SET AND LT PACK AT MIN FLOW. CREW RETURNED TO KGSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 PRECOOLER CONTROL VALVE PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20031121000372003112100037NM 2003 11 21 SWAA032484 120031109A53116516301 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME T-CHORD CRACKED AT BS 188, WL 207, RT SIDE. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040113001802004011300180WP 2004 1 13 WRLA200322 120031111A3233AGR73765517 ACTUATOR DOUG DC10 DC1030 3023501WP RT MLG FAILED A WRLAO OTHER J WARNING INDICATION CLCLIMB 1 SO11526MD 46998 AFTER TAKEOFF WHEN PUT GEAR HANDLE UP RIGHT LANDING GEAR RED UNSAFE LIGHT PILOT AND F/E PANEL ON SAME AS PREVIOUS 001 LOG PAGE 213293 ACCOMPLISHED ABNORMAL PROCEDURE 2602.83 NO HELP. WHEN PUT GEAR DOWN RIGHT GEAR DOWN RIGHT GEAR RED LIGHTS PILOT AND F/E PANEL WENT FROM RED TO GREEN IMMEDIATELY. REMOVED AND REPLACED THE RIGHT CYLINDER. OPS CHECKED OK. SWING GEAR. LANDING GEARS POSITION INDICATIONS NORMAL FOLLOWED PROCEDURES IAW MM 32-33-01. REMOVED AND REPLACED RIGHT MLG ACTUATOR. (M) 2L73 4F A22WE 20040113001882004011300188NM 2004 1 13 TSAA0334197 120031207A3411 PITOT LINE BOEING737 737282C 13844AUNM AIRSPEED OBSTRUCTED A TSAAC ABORTED TAKEOFF CN F.O.D. FALSE WARNING TOTAKEOFF 1 WP13826AL 23051 FLT 220 - HNL-OGG - F/O AIRSPEED AT 70 KTS, CAPTAINS AIRSPEED AT 100KTS. ABORTED T/O AND RETURNED TO GATE. INSPECTED F/O PITOT SYSTEM. FLUSHED OUT DEBRIS FROM SYSTEM. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040113001912004011300191WP 2004 1 13 AALA20031187 120031026A351011900301 PBE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217526A 49918 RDU - DURING OVERNIGHT MAINTENANCE, FOUND FLIGHT ATTENDANT PROTECTIVE BREATHING EQUIPMENT INOPERATIVE. REPLACED PROTECTIVE BREATHING EQUIPMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040114000332004011400033NM 2004 1 14 HNAA0300082 120031219A1430 FASTENER DHAV DHC8 DHC8301 1386003NM CONTROL YOKE LOOSE A HNAAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 EA07337HA 284 CAPT CONTROL YOKE HAS SOME FORE & AFT PLAY IN PITCH MOTION. INSPECTED NR 1 PITCH CONTROL LEVER FOR DAMAGE, NONE FOUND. TIGHTENED 3 UNSAFETIED FASTENERS & INSPECTED SAFETIED FASTENERS FOR SECURITY, OK FOR SERVICE. INSPECTED & EVALUATED PITCH CONTROL LEVERS IAW FCD 8-27-03-0278. 2H72 4T RTA13NM 20040114000422004011400042NM 2004 1 14 DL75K030954 120031026A3350BACC45FT22A55P CONNECTOR BOEING757 757232 1384965NM CABIN NOT SEATED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27650DL 24390 DURING L/O CHECK FOUND EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANT PNL 1L DOOR INOP. ALSO LIGHTS WOULD COME ON WHEN COCKPIT SWITCH TURNED OFF. RESEATED CONNECTOR D40882P LOC OVERHEAD AT SEAT 1A. OPS NORMAL FROM BOTH FLIGHT ATTENDANT PNL AND COCKPIT. 2L72 4F RTA2NM 20040114000462004011400046NM 2004 1 14 DL757030960 120031027A352080300004 OXYGEN GEN BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27690DL 27585 DURING MAINTENANCE NOTICED O2 GENERATOR TEMP BAND WAS BLACK AND PIN WAS OUT OF GENERATOR SAFETY, SEAT 27 ABC OVERHEAD. REPLACED GENERATOR PER AMM, MASKS WERE NOT DEPLOYED. 2L72 4F RTA2NM 20040114000472004011400047NM 2004 1 14 DL757030961 120031027A261230903852 CARTRIDGE BOEING757 757232 1384965NM CARGO BAY WILL NOT TEST A DALAK NONE L NO TEST ININSP/MAINT 1 SO27622DL 22912 FWD CARGO SQUIB LIGHT WILL NOT TEST ON TEST NR 1. REMOVED AND REPLACED FWD CARGO SQUIB CARTRIDGE PER MM. PERFORMED SQUIB TEST. CHECKS OK ON TEST 1 AND 2. 2L72 4F RTA2NM 20040114000972004011400097NM 2004 1 14 03FDEA01987 120031126A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB RIGHT UPPER FWD SPAR NR 1R BARREL NUT BORE FOUND CORROSION EXCEEDED EO LIMITATION. HOR STAB RT UPPER FWD SPAR 1R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR 1- 5510-7-5000. 2L73 4F RTA22WE 20040114001302004011400130NM 2004 1 14 2003UALA00872 120031118A2121731376A FAN BOEING757 757222 1384956NM PWA 2037 PW2037 NE AIR DISTRIBUTIONBROKEN A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29543UA45000 25698 ELECTRICAL BURNING ODOR IN FORWARD CABIN AND FLIGHT DECK. THE EQUIPMENT COOLING FAN HAD A WORN SHAFT AND EXHIBITED SHAFT END PLAY, ALLOWING THE BLADES TO CONTACT THE HOUSING. THIS WAS THE ORIGINAL FAN INSTALLED. FAN REPLACED 2L72 4F4 FRTA2NM E17NE 20040115000422004011500042EU 2004 1 15 XNOA1169 120031205A7797 WIRE HARNESS AIRBUS300 A300B4203 3930306EU EGT INDICATOR DAMAGED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23373PC 218 NR 1 ENGINE EGT INDICATION ERRATIC. R&R NR 1 ENGINE EGT HARNESS PER A-300 AMM 77-21-01. OPS CK NORMAL. (CLOSED) 2L72 4F RTA35EU 20040115001132004011500113NM 2004 1 15 03FDEA02086 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 03 EA LOCK BOLT COLLARS CRACKED. RH CENTER SECTION OF NR 3 BANJO FITTING AJC7053-503 AFT FACE FLANGE 3 CRACKED LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND INSTALLED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II. 2L73 4F RTA22WE 20040115001252004011500125NM 2004 1 15 03FDEA02102 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL2 AND REPLACED AS PER SRM51-33-01VOL2 2L73 4F RTA22WE 20040115001292004011500129NM 2004 1 15 03FDEA02107 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 3 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363AL. LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 3 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040115001322004011500132NM 2004 1 15 DL73S031097 120031216A5330 DOUBLER BOEING737 737232 1384475NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 FOUND ON W-2 LETTER CK, STRINGER 22RT CUT AT STA 957, 977, 996 FOR OUTFLOW VALVE DOUBLER REPLACEMENT. REPAIR PER SRM 53-10-3 FIG 1. 2L72 4F RTA16WE 20040115001462004011500146NM 2004 1 15 03FDEA02151 120031209A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 FWD CARGO STA 520 STR 23L FRAME IS DENTED. REMOVED DAMAGE ON FRAME BS 520, STR 23L. FABRICATED FRAME DOUBLER FOR CUT OUT. ALODINED, PRIMED & INSTALLED IAW SRM 51-40-3 AND EA 7-5310-70600. 2L73 4F RTA3WE 20040115001652004011500165NM 2004 1 15 DL75K031120 120031221A3350 PIN BPS73 BOEING757 757232 1384965NM POWER SUPPLY BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO276704Z 0174 30396 ON L/O, FOUND EMERGENCY EXIT LIGHT ABOVE EMERGENCY EXIT DOOR AT 16A INOP. FOUND PIN BROKEN ON POWER SUPPLY. REMOVED AND REPLACED SAME, OPS OK. 2L72 4F RTA2NM 20040115001682004011500168SO 2004 1 15 RAIAOO312311 120031211A3260852701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO LEFT & RIGHT MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03804HK2090 145082 RIC- AIR GROUND FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED LEFT FORWARD AND RIGHT AFT PROX SWITCHES. 2L72 4F RTT00011AT 20040115001732004011500173NM 2004 1 15 USAASB3208 120031125A2910654468111 MODULE BOEING737 7373B7 1384580NM HYD SYSTEM FAILED A USAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA19514AU 23700 ON CLIMB-OUT, EN ROUTE, CREW RECEIVED A LEADING EDGE SLAT TRANSITION LIGHT. CREW COULD NOT RETRACT THE LEADING EDGE SLATS. TRAILING EDGE DEVICES WERE NORMAL. CREW ELECTED TO RETURNED TO FIELD WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE STANDBY HYDRAULIC SYSTEM MODULE IAW MM 29-15-81. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20040115001832004011500183NM 2004 1 15 DHL200342539 120031124A2782 MOUNT BRACKET BOEING727 727225 1384077NM KRUEGER FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, N/R60109 NR 6 KRUEGER FLAP INBD ACT MOUNT CRACKED 2 EA PLACES. REMOVED SUPPORT BRACKETS IAW B727 SRM 51-30-02. FABRICATED AT 2 EA SUPPORT BRACKETS IAW B727 SRM 57-20-02. ALODINED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED SUPPORTS IAW B727 SRM 51-30-02. OPS CHECK GOOD IAW B727 MM 27-81-00. 2L73 4F A3WE 20040115001852004011500185 2004 1 15 AWXA200301648 420031231A34426225137601 RADAR AIRBUS320 A320232 3930326EU RADOME BIRD STRIKE A AWXAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 WP28649AW21975 803 ORD - AIR TURNBACK - FLT 0010 - SHORTLY AFTER TAKEOFF AT ORD EN ROUTE FOR PHX A BIRD STRUCK THE AIRCRAFT, LOST WEATHER RADAR AND HAD A LOT OF NOISE COMING FROM AREA. TURNED BACK TO ORD AND LANDED WITHOUT EVENT. MAINTENANCE FOUND DAMAGE TO RADOME AND WEATHER RADAR, REMOVED AND REPLACED THE RADOME IAW AMM 53-15-11, AND REPLACED WEATHER RADAR ANTENNA & DRIVE ASSEMBLY IAW AMM34-41-00, OPERATIONAL CHECK OF RADAR SYSTEM WAS GOOD. PART NAME; RADOME, MFG; AIRBUS, P/N; D5311047700007, S/N; NT1016, TT; 21964, TC; 8516. PART NAME; DRIVE, ANTENNA MOUNT, MFG; ROCKWELL COLLINS, P/N; 622-5136-001, S/N; 1752, TT; 38556, TC; 17676. 2L72 4F RTA28NM 20040116000022004011600002NM 2004 1 16 03FDEA02169 120031211A5330 SKIN BOEING727 727200 138407ENM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 N00325 BULGE IN LOWER FUSELAGE SKIN BETWEEN FASTENERS BS 704 STR 28L LBL 6. CUT OUT STR 28L BETWEEN B/S 700-720. FOUND SPLICE PIECE TO BE OUT OF LIMITS (CORRODED). SKIN WAS NOT AFFECTED BY CORROSION. DRILLED UP NEW STR SPLICE SECTION FROM BAC1498-144 LOT 478915. ALODINED AND PRIMED SECTION AND INSTALLED. ALL IAW SRM 53-10-1, 51-30-2, 53-10-3 AND 51-40-2. 2L73 4F RTA3WE 20040116000052004011600005NM 2004 1 16 03FDEA02172 120031211A5230 DOOR FRAME BOEING727 727200 138407ENM CARGO DOORWAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 FWD CARGO BAY, LWR DOOR CUTOUT THRESHOLD FRAME TOP FLANGE HAS 4 DAMAGED NUT PLATE HOLES. REPAIRED FLOOR BOARD BS 950F-1030, RBL 45-65, WL 208 BY REPLACING MISSING INSERTS PER FED EX DWG SRZ-25-005 REV E. 2L73 4F RTA3WE 20040127001652004012700165NM 2004 1 27 ASAA0310173 120030320A524765509041 FRAME BOEING737 737298C 1384490NM APU DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND APU DOOR LATCH CUT OUT FRAME AT BS 1121, WATER LINE 230 GOUGED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20040127002432004012700243NM 2004 1 27 ASAA0310213 120030325A5320 ANGLE BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND RIGHT WHEELWELL AFT OUTBOARD WALL FORWARD ATTACH ANGLE AT BS 706, STRINGER 24R GOUGED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040128000152004012800015EU 2004 1 28 BAQA092329 120031229A6220 BEARING BOLKMS117 BK117A1 5626010EU ROD END WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1360 7243 MAIN ROTOR ROD END HAS BEARINGS WORN. REPLACED WITH SERVICABLE UNIT. 1G72 3U H13EU 20040128000242004012800024SO 2004 1 28 RAIA00312320 120031217A3080CM6180 BULB EMB 145 EMB145 3260210SO INDICATOR INOPERATIVE A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03827HK STL- WING ANTI-ICE INOP INDICATION. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. 2L72 4F RTT00011AT 20040128000332004012800033SO 2004 1 28 C2XA03CL214 120031227A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713988 145265 CLE FLIGHT 3230 THE CREW REPORTED THE EMERGENCY OVERHEAD AISLE WING EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE OVERHEAD EMERGENCY EXIT LAMP. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040128000382004012800038WP 2004 1 28 DHL2003809009 120031227A5210 DOOR DOUG DC8 DC873F 302199FWP MAIN PAX LACK OF LUBE A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01604AL 46047 MAIN CABIN DOOR HARD TO CLOSE. LUBED MAIN CABIN DOOR MECHANISM. OPS CHECKED GOOD PER 52-11-1. 2L74 4F RT4A25 20040128000422004012800042WP 2004 1 28 ABXA030488 120031215A53205956879501 WEB DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 WEB CRACKED FS 200 LONGERON 8 LEFT. REPAIRED AREA IAW REA-D953-48739. 2L72 4F A6WE 20040128000442004012800044WP 2004 1 28 ABXA030490 120031212A5415591326227 ATTACH ANGLE DOUG DC9 DC941 302207NWP AFT FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 NR 1 ENGINE UPPER PYLON ATTACH ANGLE WAS CRACKED AT STA 1114. REPAIRED AREA IAW DC-9 SRM 54-04. 2L72 4F A6WE 20031015000012003101500001NM 2003 10 15 2003UALA00690 120030914A2913 SHAFT BOEING757 757222 1384956NM PWA 2037 PW2037 NE HYD PUMP SHEARED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29539UA 25223 LOSS OF LEFT HYDRAULIC SYSTEM. LOST ALL HYDRAULIC FLUID ON LEFT SIDE. THE CAUSE OF THIS FAILURE WAS A SHEARED SHAFT, WHICH CAUSED THE PUMP TO SEIZE AND CRACK THE CASE. THE PUMP WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20031015000022003101500002NM 2003 10 15 2003UALA00739 120031003A5754 SKIN BOEING777 777222 1385219NM NR 4 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29217UA 30550 NR 4 SLAT OUTBOARD ON THE LOWER SURFACE OF TR EDGE DELAMINATED 1.7 INCH CHORDWISE BY .7 INCH SPAN WISE. MAJOR REPAIR ACCOMPLISHED. INJECTED STRUCTURAL ADHESIVE INTO DELAMINATED AREA. 2L72 4F RTT0001SE 20031015000302003101500030EA 2003 10 15 ASOA03428 120030909A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20031015000392003101500039EU 2003 10 15 ASOA03445 120030905A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK AT FS 39 TO FS 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK AT FS 39 TO FS 41 IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20031015000432003101500043EA 2003 10 15 ASOA03442 120030915A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN AIR DIRTY A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11849AS 7347 DURING APPROACH INTO ATL FROM TLH, THE CREW NOTICED AN UNUSUAL ODOR IN THE CABIN WHEN SWITCHING FROM THE ENGINE BLEEDS TO THE AUXILIARY POWER UNIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT AND LEFT COALESCER BAGS ON THE WATER SEPARATOR ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000492003101500049WP 2003 10 15 ASOA03450 120030917A5210 HINGE DOUG DC9 DC982 3022082WP PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821US 49138 DURING A C-CHEC IN MCN, THE TOP HINGE SEGMENT ON THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP HINGE SEGMENT ON THE PASSENGER DOOR TOP STEP IAW SRM 51-00. (M) 2L72 4F A6WE 20031016000042003101600004EU 2003 10 16 YENA200327 120031011A5240FE240221001 DIAPHRAGM RATIER AIRBUS320 A320232 3930326EU DOOR DAMPER PUNCTURED A YENAK NONE O OTHER ININSP/MAINT 1 EA15505JB 1972 1173 AFT SEVICE DOOR DAMPER AND EMMERGENCY OPERATION CYLINDER PUNCTURED DIAPHRAM IN PERCUSSION MECHANISM. REPLACED DIAPHRAM IAW AMM 52-10-00, OPERATIONAL CHECK PER 52-10-00 GOOD. 2L72 4F RTA28NM 20031020000582003102000058 2003 10 20 RAIA00310259 420031009A23507012100811 RMU JETAIRJETSTMJETSTM4101 1500501EU LEFT FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03574HK2138 41093 5452-STL- LEFT RADIO MANAGEMENT UNIT FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 RMU. 2L72 4T RTA41NM 20031020000602003102000060SO 2003 10 20 C2XA03SH381 120031011A532014521725015 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031020000992003102000099WP 2003 10 20 ABXA030377 120030917A5310SR095302527 STOP FITTING DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 MAIN ENTRY DOOR AFT UPPER DOOR STOP A3, HAD CRACK FROM STOP HOLE TOWARDS DOOR OPENING APPROXIMATELY .1875 INCH LONG. REPAIRED AREA IAW DC-9 SRM AND EA 53100131-001. 2L72 4F A6WE 20031020001342003102000134SO 2003 10 20 RAIA00309254 120030905A3610 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS WORN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK 145044 5663-STL=- ENGINE NR 2 BLEED LEAK MESSAGE. MAINTENANCE PLACED ON DEFERRAL PER MEL. SUBSEQUENTLY CLEARING DMI BY REPLACING O-RING AT BLEED COUPLING IN CARGO BAY. 2L72 4T RTT00011AT 20031020001452003102000145NM 2003 10 20 DL757030796 120030830A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27670DN 25331 FLIGHT ATTENDANT REPORTED SMELL OF FUMES AROUND ROW 24 ON APPROACH AND TAXI. ENGINE BLEEDS ON WITH BOTH PACKS ON WHEN SMELL REPORTED. RAN ENGS FOR 5 MINS WITH BLEEDS OPEN AND PACKS ON, NO ODORS DETECTED. 2L72 4F RTA2NM 20031020001492003102000149NM 2003 10 20 DL75K030799 120030831A3350 LIGHT BOEING757 757232 1384965NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO276701 30187 DURING T/C SERVICE FOUND MID LAV RT SIDE EMERGENCY LIGHT INOP. RELAMPED SAME, OPS OK. 2L72 4F RTA2NM 20031014001572003101400157NM 2003 10 14 SWAA032070 120030916A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO COMP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, WL 208 AND LBL 46. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20031015000212003101500021SO 2003 10 15 ASOA03434 120030911A2150 A/C PACK EMB 120 EMB120ER 3260203SO ACM BAY FAILED A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO11246AS 120100 DURING A SCHEDULED TEST FLIGHT, WHILE IN CRUISE THE SMOKE DETECTOR SOUNDED WITH SMOKE OCCURRING IN THE CABIN. THE PACK SUBSEQUENTLY FAILED AND THE SMOKE DISSIPATED. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE RAN THE AUXILIARY POWER UNIT, PERFORMED ENGINE GROUND RUNS AND INSPECTED THE PACKS. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20031015000572003101500057NM 2003 10 15 USAASB03172 120030924A335020121 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU 23381 BDL - FOUND EMERGENCY EXIT SIGN OVER AFT LEFT DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER. (M) 2L72 4F RTA16WE 20031020001432003102000143EU 2003 10 20 MALA030443 120031002A3297ATG130902 WIRE HARNESS SAAB SF340 340B 7860101EU LT MLG FAULTY A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15450XJ 340B450 LOW ENERGY ABORT ON FLIGHT 2794 DUE TO LEFT MAIN LANDING GEAR LIGHT EXTINGUISHING ON TAKEOFF ROLL. MAINTENANCE REPLACED LT DOWNLOCK ACTUATOR HARNESS. REF SAAB AMM CH 32-61-05-2 PN ATG130902. PERFORMED GEAR SWINGS, ALL CHECKS GOOD. 2L72 4T RTA52EU 20031020001542003102000154NM 2003 10 20 DL73S030805 120030902A3350BPS73 POWER SUPPLY BOEING737 737232 1384475NM CABIN DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 DURING LAYOVER CHECK FOUND EMERGENCY ESCAPE PATH LIGHTING FROM ROW 11 THRU AFT CABIN BLINKING ON AND OFF WHEN THE SWITCH WAS OFF. REPLACED POWER SUPPLY (M9013) AND BATTERY PACK. ALL OPS NORMAL. 2L72 4F RTA16WE 20031020001622003102000162NM 2003 10 20 DL73S030788 120030827A7997 WIRE BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE OIL SYSTEM SHORTED A DALAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO27374DL47902 23521 709179 NR 2 ENG SHUTDOWN INFLT DUE TO OIL TEMP PEGGED HIGH. FOUND TO BE INDICATION PROBLEM (SHORTED WIRE). REPAIRED WIRE. 2L72 4F4 F A16WE E2EA 20031020001652003102000165NM 2003 10 20 DL76G030791 120030828A2121732591B FAN BOEING767 767332 1382001NM CARGO BAY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271603 29695 DIVERTED TO TER DUE TO SMOKE AND ELECTRICAL ODOR IN THE COCKPIT. TURNED EQUIPMENT COOLING TO OVERRIDE AND SMOKE DISSIPATED. MTC FOUND EQUIPMENT COOLING EXHAUST FAN C/B TRIPPED. TRIED ONE, RESET AND TRIPPED AGAIN. REPLACED EXHAUST FAN. FOUND FAN WITH SUSPECT BAD BEARINGS. RAN ENGINES, IFE, PACK AND CHECKED BATTERY CHARGING SYSTEM. ALL CHECKS GOOD. 2L72 4F RTA1NM 20031020001902003102000190WP 2003 10 20 UPS03841360 120030919A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 728.75 AND XFS 735. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATE CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20031020001922003102000192NM 2003 10 20 DL73G030817 120030906A33970201875003 WIRE HARNESS BOEING737 73735B 13844BMNM CABIN DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27223DZ 23972 EMERGENCY LIGHTING AT ROW 5DEF INOP. REPLACED E-PATH SEAT CABLE ASSY PER AMM. E-PATH LIGHTING CHECKS GOOD. 2L72 4F RTA16WE 20031020002252003102000225WP 2003 10 20 UPS03841339 120030922A53203779762U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 LONGERON END FITTING IS CRACKED AT STA 680 LONG 2R. REMOVED AND REPLACED END FITTING IAW DWG 3779762, AND SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20031020002602003102000260NM 2003 10 20 03264425 120030921A3222 STRUT DORNERDO32 DO328300 NM NLG OVERSERVICED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27425FJ 3189 DURING CLIMB THE CREW NOTED A PROXY FAIL CAS MESSAGE. FLIGHT RETURNED TO FIELD AS A PRECAUTION AND AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE PERSONNEL FOUND NOSE STRUT OVERSERVICED AND DESERVICED TO PROPER LEVEL. AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031020002682003102000268EA 2003 10 20 03265628 120030922A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27628BR 7240 DURING INSPECTION THE 2ND CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002792003102000279EU 2003 10 20 03268303 120030925A33508GS00599705 SIGN JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27303UE 41015 DURING INSPECTION THE RT EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031020002802003102000280EA 2003 10 20 03271663 120030928A3350OL3071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27663BR 7527 DURING INSPECTION SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED SEVERAL FILAMENTS IN THE EMERGENCY LIGHTING SYSTEM. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002952003102000295NM 2003 10 20 2003UALA00724 120030929A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29651UA 25389 SKIN DENTED AT STATION 1241 STRINGER 39L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA1NM E24NE 20031020002242003102000224WP 2003 10 20 UPS03841334 120031003A3260 WARNING SYSTEM DOUG DC8 DC873F 302199FWP COCKPIT MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801UP 46101 INSPECTION TYPE:N/A DURING CLIMBOUT THRU FL150, OBSERVED RED GEAR NOT LATCHED LIGHT ON. PERFORMED ABNORMAL CHECKLIST. AFTER CYCLING GEAR ALL INDICATIONS NORMAL. JACKED A/C PER MM 07-11-00-2, PERFORMED UPLATCH CK PER MM 32-31-03-2, 32-31-04-6. PERFORMED LDG CK POS WARNING CK PER MM 32-60-00-2. ALL CK'D NORMALLY DURING MANY CYCLES F/O LOG GEAR EXT & RETRACTION. 2L74 4F RT4A25 20031020002352003102000235WP 2003 10 20 UPS03841342 120030919A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 597.5. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A. 2L74 4F RT4A25 20031020002692003102000269EU 2003 10 20 03269308 120030926A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN DIRTY A VTZAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA27308UE 41023 DURING INSPECTION A SPARK WAS NOTED BY CREW ON BOARD. MAINTENANCE PERSONNEL CLEANED THE 1LF2 CONNECTOR AND REINSTALLED THE CONNECTOR. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031020002722003102000272EU 2003 10 20 03266319 120030923A1430MS1656230 ROLL PIN JETAIRJETSTMJETSTM4101 1500501EU COCKPIT BROKEN A VTZAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA27319UE 41042 DURING TAXI/GROUND HANDLING THE CREW ATTEMPTED TO ENGAGE THE PARKING BRAKE. CREW RETURNED TO GATE UNEVENTFULLY AND PASSENGERS WERE DEPLANED NORMALLY. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE PARKING BRAKE HANDLE ROLL PIN. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031020003112003102000311NM 2003 10 20 2003UALA00702 120030919A5230 DOOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29180UA 25224 AFT CARGO PIT CONTAINER DOOR DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20031020003122003102000312NE 2003 10 20 T48R384Y 220030925A7261318195 BEARING PWA BOEING737 737 UTILSYSNM PWA JT8 JT8D17A 52049NE SCAVENGE PUMP FAILED B T48RK NONE O OTHER UKUNKNOWN 1 GL09 F685 688356 BEARING IN 4 1/2 AND 5 SCAVAGE PUMP FAILED RESULTING IN OIL CONTAMINATION. 2L72 4F4 FRTA16WE E2EA 20031021000522003102100052EU 2003 10 21 A6WA200360043 120030924A5313 STRINGER BAC 146 146200A 1500266EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 FOUND STRINGER 33 RIGHT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101 AVMAX NON-ROUTINE 2289 FOR REPAIR. REPAIRED STRINGER IAW BAE SRM 53-00-12 FIG 207. (M) 2H74 4F A49EU 20031021000562003102100056 2003 10 21 USAASA03106 420030804A2565 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19752US 1319 BOS - THE AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20031021000772003102100077SO 2003 10 21 SIMA200326503 120030909A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21820AE 145576 ABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02 FIGURE 201. (M) 2L72 4F RTT00011AT 20031021001202003102100120WP 2003 10 21 GTIA030712 120030909A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND DELAMINATED AND MISSING INSERT, MISSING EDGE FILLER FLOORBOARD MAIN CABIN STATION 1022-1117. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031021001312003102100131NM 2003 10 21 AALA20030949 120030903A3350S283TD143 BATTERY PACK BOEING767 767223 1385123NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21305AA 22311 DFW - EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 28. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031021001362003102100136NM 2003 10 21 AALA20030945 120030903A3350S283TD143 BATTERY PACK BOEING767 767323 1385205NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21363AA 24044 SFO - EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 21H. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED LIGHT ASSEMBLY BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031021001492003102100149NM 2003 10 21 AALA20030566 120030514A3350 SOCKET BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21688AA 25730 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATHWAY LIGHTING AT SEAT 22DEF INOPERATIVE. SECURED EMERGENCY EXIT PATHWAY LIGHT SOCKET AT 22DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021001962003102100196NM 2003 10 21 AALA20031001 120030914A3350 CONNECTOR BOEING757 757223 1384957NM CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21696AN 26976 MIA - TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 19D. RESEATED CONNECTOR TO THE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002042003102100204NM 2003 10 21 AALA20030619 120030621A3397 WIRE BOEING757 757223 1384957NM COCKPIT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21658AA 24616 LAX - DURING OVERNIGHT MAINTENANCE, ALL CABIN EMERGENCY EXIT LIGHTS REMAIN ON EVEN THOUGH THE EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION. SECURED WIRE ON EMERGENCY LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002002003102100200NM 2003 10 21 AALA20030609 120030526A3350 CONNECTOR BOEING757 757223 1384957NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21195AN 32389 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3EF INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002272003102100227SO 2003 10 21 SIMA200325302 120030902A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21717AE 145272 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED THE DAMAGED SECTION OF THE LEFT OMEGA BEAM, THE CUTOUT OF THE FLANGED AREA WAS EXTENDED BEYOND THAT OF THE WEB TO EMCOMPASS THE REPAIR SHIMS. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2917, PRINCIPLES CONTAINED IN THE EMB SRM, SRM EMB 145/1142 REV 22, CHAPTERS 53-21-10 FIG 202, SHEET 1 AND STANDARD SRM AND CPM PRACTICES. (M) 2L72 4F RTT00011AT 20031021002412003102100241WP 2003 10 21 GTIA030692 120030903A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND SEAT TRACKS RIGHT OUTBOARD BETWEEN STATION 927-1003, STATION 1022-1098, STATION 1098-1155, STATION 1174-1250, STATION 1271-1309 CORRODED. REMOVED SEAT TRACK RIGHT OUTBOARD STATION 927-1309. FABRICATED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK. (M) 2L72 4F A6WE 20031021002472003102100247SO 2003 10 21 C2XA03SH341 120030921A532014522178005 THRESHOLD EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SEVICE. 2L72 4T4 FRTT00011ATTE6CH 20031021002522003102100252WP 2003 10 21 GTIA030699 120030904A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND MAIN CABIN FLOORBAORD FS 1117 BETWEEN RIGHT INBOARD AND MIDDLE SEAT TRACKS HAS CORROSION ON LOWER SIDE AND HOLE PUNCTURE. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031021002572003102100257NE 2003 10 21 USAABA03032 220030912A75306764B030000 REGULATOR VALVE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19673UW 0337 PHL - FLT 2 - EN ROUTE PHL-FCO, THE RIGHT ENGINE HIGH PRESSURE BLEED BECAME INOPERATIVE. AT VARIOUS POWER LEVELS AND ALTITUDES THE BLEED SYSTEM RETURNED TO NORMAL. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE PRV. (M) 2L72 4F4 FRTA46NM 20031021002592003102100259WP 2003 10 21 03FDEA01596 120030919A2910 LINE DOUG DC10 DC1030F 3023504WP MAIN HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25301FE 46800 HYD SYSTEM NR 1 FAILED. NOTE: DUE TO LOSS OF HYD FLUID. FOUND HYD LINES CHAFED TOGETHER JUST AFT OF 1-3 REVERSIBLE MOTOR PUMP IN CENTER W/W CHANGED LINE, LEAK CHECK OK. 2L73 4F RTA22WE 20031021002812003102100281NM 2003 10 21 CALA0300539 120030919A5414 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230. 2L72 4F4 FRTA16WE E2GL 20031022000012003102200001NM 2003 10 22 MWEA030381 120030922A5347593054770 SEAT TRACK DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 MODERATE CORROSION ON NR 6 SEAT TRACK STATION 722. REMOVED CORROSION, REMOVED AND REPLACED SEAT TRACK. 2L72 4F4 FRTA6WE E2EA 20031022000182003102200018EU 2003 10 22 AWXA200301068 120030908A5315D5347209800000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF Y924 FLOORBEAM AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED Y924 DUMMY RAIL AT FR 66; INSTALLED NEW REPLACEMENT RAIL IAW A320 SRM 51-24-00 PG 1-6, AND SRM 51-42-11 PG 1-7. 2L72 4F RTA28NM 20031022000222003102200022EU 2003 10 22 AWXA200301072 120030909A5315D53472189200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF Y1292 FLOORBEAM 3 INCHES FORWARD OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED Y1292 FLOORBEAM FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-00-14 PG 101-106 FIG 102. 2L72 4F RTA28NM 20031022000292003102200029NM 2003 10 22 AWXA200301079 120030920A3150 WARNING HORN BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE COCKPIT ACTIVATED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28309AW 24711 ON TAKEOFF AT PHX EN ROUTE FOR OAK WHEN POWER LEVERS WERE ADVANCED THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF THRUST NEVER ACHIEVED, REJECTED TAKEOFF 10-20 KTS. TAXIED OFF RUNWAY AND CHECKED SETTINGS, EVERYTHING APPEARED NORMAL. RESET SPEED BRAKE LEVER IN DOWN DETENT, SUBSEQUENT TAKEOFF NORMAL. 2L72 4F4 FRTA16WE E2GL 20031022000322003102200032NM 2003 10 22 C1HA200393014 120030922A3350 BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15293AS 21348 L-1 DOOR EMERGENCY EXIT SIGN/LIGHT BATTERY PACK IS INOPERATIVE. REMOVED AND REPLACED L-1 DOOR EMERGENCY EXIT/SIGN LIGHT BATTERY PACK IAW 727 MM 33-50-71. OPS CHECK WAS GOOD. 2L73 4F A3WE 20031022000332003102200033NM 2003 10 22 UPS03241247 120030919A575465162251 DOUBLER BOEING727 72722C 138400FNM RROYCEDART DART* NE KRUEGER FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 FOUND CORROSION ON NR 3 KRUEGER FLAP EXTENDING UNDER DOUBLER REPAIR R&R REQUIRED. REMOVED AND REPLACED NR 3 KRUEGER FLAP IAW MM 27-81-01. 2L73 4F4 T A3WE 20031022000342003102200034NM 2003 10 22 UPS03441246 120030904A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, ONE EACH FASTENER HOLE FOUND CRACK AT BS 1830 STR 4R APPROX 0.020 INCH LONG RUNNING TOWARD AFT. CRACKED PORTION AT TOP SKIN WERE TRIMMED OFF IAW SRM 51-10-01 AND 51-10-02 NDT INSP THE CUT-EDGE NO DEFECTS AND PERFORMED A EXT PATCH REPAIRED AT AFFECT AREA IAW SRM 53-30-03 FIG 17 AN AREA PAINT TOUCHED UP IAW MM51-24-11. 2L74 4F A20WE 20031022000372003102200037SO 2003 10 22 SWIA200312419 120030916A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07224SW5931 5931 120294 EMERGENCY LIGHTING INOPERATIVE, ROW 9 AND AFT. REMOVED AND REPLACED AFT ELBP IAW EMB120 MM 33-50-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20031022000502003102200050NM 2003 10 22 QXEA200301152 120030911A5341 FLANGE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 WING TO FUSELAGE FAIRING FORWARD APERTURE FLANGE IS CHAFED AT PANEL 262AT. REPAIRED IAW Q400 SRM 51-00-02 AND RD 8/4-53-451. 2H72 4T4 TRTA13NM E00062EN 20031022000512003102200051NM 2003 10 22 QXEA200301153 120030916A5410 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 NR 1 ENGINE LOWER COWL BYPASS DOOR APERTURE RIGHT SIDE SUPPORT ANGLE IS CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103. 2H72 4T4 TRTA13NM E00062EN 20031022000542003102200054NM 2003 10 22 QXEA200301156 120030915A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX- RIGHT FUESLAGE SKIN IS NICKED 3 INCHES AFT OF X712.3 JOINT ALONG STRINGER 22 AFT OF RIGHT SERVICE DOOR. REPAIRED IAW Q400 SRM 51-26-10, 51-00-02, 51-00-04 AND RD 8/7-53-666. 2H72 4T4 TRTA13NM E00062EN 20031022000572003102200057NM 2003 10 22 QXEA200301158 120030916A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 TWO NICKS 1 INCH APART IN LOWER FORWARD FUSELAGE SKIN BETWEEN LEFT STRINGERS 26 & 27 AT X38.4 LOWER FORWARD FUSELAGE EXTERIOR. REPAIRED IAW Q400 SRM 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801 AND RD 8/4-53-716. 2H72 4T4 TRTA13NM E00062EN 20031022000592003102200059NM 2003 10 22 QXEA200301160 120030917A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 LOWER FORWARD FUELAGE EXTERIOR SKIN IS NICKED BETWEEN LT STRINGERS 32 AND 33, 6 INCHES AFT OF X32.4. REPAIRED IAW Q400 SRM 51-26-10, 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801, RD 8/4-53-717 AND HORIZON AIR EA 6-53-295. 2H72 4T4 TRTA13NM E00062EN 20031022000782003102200078SO 2003 10 22 CHQA000422 120030922A3230 CONTROL UNIT EMB 145 EMB145 3260210SO CONT C85 C85* 17008SO MLG MALFUNCTIONED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11272 LANDING GEAR WOULD NOT RETRACT, LG A/G FAIL EICAS MESSAGE. REMOVED AND REPLACED LGEU. 2L72 4F3 ORTT00011ATE233 20031022000802003102200080WP 2003 10 22 ABXA030365 120030908A53203643758501AX FITTING DOUG DC9 DC9* WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 FITTING IN RIGHT WHEEL WELL DAMAGED (CRACKED). FABRICATED NEW PART REF: ST-9300-01 AND PARTS FABRICATION RECORD WO 600179300 AND IAW SRM. 2L72 4F A6WE 20031022000842003102200084NM 2003 10 22 03FDEA01764 120031017A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25493FE 21531 CORROSION FOUND ON AIRCRAFT SKIN, UNDER STRINGER 28 LT AT BS 950E, 950E+9, AND 950F+6. FOUND SKIN TO BE OUT OF LIMITS AT 950E, 950E 9 AND 950F 6. CUT OUT CORRODED SKIN AND REPAIRED PER 727 SRM 53-30-3 FIG 3 2L73 4F RTA3WE 20031022000902003102200090NM 2003 10 22 03FDEA01738 120031015A5330 LAP JOINT BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 CHAFING ON LAP JOINT SKIN STR19R, BS720D PLUS 10 INCHES. BLENDED OUT LAP JOINT SKIN STR 19R, BS 720D 10, 2 X 2 X .022 FROM ORIGINAL OF .060. FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 CUT OUT DAMAGE FROM LAP AND REPAIRED PER SRM 53-30-3, 2L73 4F RTA3WE 20031022000942003102200094WP 2003 10 22 DM42003F00000 120030916A27425914405501 NUT DOUG DC9 DC915F 3022037WP H/S ACTUATOR CRACKED B DM4RO OTHER O OTHER NRNOT REPORTED 1 SO19785TW DAC027 47015 SUBJECT HORIZONTAL STABILIZER ACTUATOR: RECEIVED WITH A CRACKED NUT WITH METAL PARTICLES ON SCREW SECTION AD 200-15-15. 2L72 4F A6WE 20031022000952003102200095WP 2003 10 22 MWEA030390 120030923A2730 ANNUNCIATOR DOUG DC9 DC982 3022082WP COCKPIT BURNED OUT A MWEAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 GL31810ME 48072 ELEVATOR POWER ON ANNUNCIATOR WILL NOT LIGHT UP. RELAMPED, OPERATIONS CHECK GOOD. 2L72 4F A6WE 20031021002942003102100294NM 2003 10 21 CALA0300551 120030922A3350D71701100 BATTERY PACK BOEING777 777224 1385225NM CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2727015 28678 ALL EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK. FIFTEEN BATTERY PACKS WERE REMOVED AND REPLACED IAW MM 33-51-06-960-802. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00001SE 20031022000242003102200024EU 2003 10 22 AWXA200301074 120030908A5414D54530052200201 SKIN AIRBUS320 A320232 3930326EU NR 1 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK THE NR 1 PYLON AFT FIXED FAIRING SKIN WAS FOUND PITTED. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED AFT FIXED FAIRING SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-13, & A23-A25 FIG 2-4, & 60-61. 2L72 4F RTA28NM 20031022000632003102200063NM 2003 10 22 QXEA200301164 120030917A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 NICK IN LOWER FORWARD FUSELAGE SKIN BETWEEN RT STRINGERS 32 AND 33, 7 INCHES AFT OF X1.0. REPAIRED IAW Q400 SRM 51-26-10, 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801, RD 8/4-53-719 AND HORIZON AIR EA 6-53-296. 2H72 4T4 TRTA13NM E00062EN 20031022000932003102200093CE 2003 10 22 DXTA200300133 120031002A3230 LANDING GEAR CESSNA500 560CESSNA 2076750CE MAIN STUCK E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07311QS 5600311 ON TAKE OFF FROM EWR GEAR WAS STUCK IN DOWN POSITION ACCOMPLISHED AIR TURN BACK TO EWR. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20031022001012003102200101NE 2003 10 22 MEX2003420 220030911A7412103538754 EXCITER DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE NR 1 FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23946AS 49658 AIRCRAFT RETURNED TO PLATFORM DURING ENGINE NUMBER ONE STARTING, IT DID NOT HAD IGNITION. EXCITER IGNITION BOX WAS REPLACED IAW MM 74-10-01, ALL CORRECT. 2L72 4F4 FRT E9NE 20031022001192003102200119NM 2003 10 22 QXEA200301170 120030921A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 800 INOPERATIVE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09414QX 4061 ON FLIGHT 2395 AFT AIRSTAIR WILL NOT SLIDE OUT. CLEANED AND LUBED AFT AIRSTAIR SLINDING ASSEMBLY. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20031022001292003102200129NM 2003 10 22 2003UALA00669 120030830A2410106123311 OIL COOLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LEFT MALFUNCTIONED A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29379UA 24654 ON TAKEOFF AND CLIMBOUT 3000 FT MASTER CAUTION LOW OIL PRESS FLICKERING (LT) GEN HIGH OIL TEMP RAN PROCEDURE- DISCONNECTED CSD RETURN TO ORD. THE LEFT CSD WAS RECENTLY REPLACED PRIOR TO THIS EVENT. HOWEVER, DURING THE REPLACEMENT OF THE CSD, THE OIL COOLER WAS NOT REPLACED. THE OIL COOLER WAS SUSPECT AS THE CAUSE OF THIS EVENT AND WAS REPLACED ON 06SEP IN ORD. 2L72 4F4 FRTA16WE E2GL 20031022001372003102200137NM 2003 10 22 2003UALA00696 120030917A3350 LIGHT BOEING777 777222 1385219NM CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29792UA 26934 RT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT AND RT SIDE FLOOR EMERGENCY LIGHT IN AFT GALLEY INOP. RELAMPED. 2L72 4F RTT0001SE 20031022001412003102200141EU 2003 10 22 AWXA200301083 120030914A5414D54530052200201 SKIN AIRBUS320 A320232 3930326EU NR 2 ENG PYLON ERODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK THE NR 2 ENGINE PYLON AFT FAIRING INBOARD SKIN WAS FOUND ERODED AT THE LOWER SECTION. MAINTENANCE REMOVED ERODED INBOARD SKIN ON THE NR 2 ENGINE PYLON; FABRICATED A NEW SECTION OF REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 8-13, AND A25, FIG. 2-4, AND 61. 2L72 4F RTA28NM 20031022001432003102200143NM 2003 10 22 AWXA200301085 120030923A3243NSA82018 PACKING AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE ZONE 190 RUPTURED A AWXAO OTHER KSJFLUID LOSS AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 WP28825AW 1527 PHX - FLIGHT CONTROL - FLT 0261 - EN ROUTE FROM YYZ TO PHX RECEIVED ECAM (YELLOW) NR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE INDICATION. LANDED AT PHX WITHOUT INCIDENT, EMERGENCY EQUIPMENT CALLED TO STANDBY AS PRECAUTION. MAINTENANCE DISCOVERED A BLOWN SEAL AT PORT (E) OF AUTOMATIC BRAKE SELECTOR VALVE (2576GM). REPLACED SEAL IAW AMM 32-42-13, AND PERFORMED OPERATIONAL CHECK OF NORMAL AND ALTERNATE BRAKES PER AMM 32-43-00, LEAK AND OPERATIONAL CHECK WERE GOOD. 2L72 4F4 FRTA28NM E311NE 20031022001492003102200149EA 2003 10 22 SWIA200312434 120030922A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 FS 621 RT FLOOR SUPPORT ANGLE CRACK. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401.PN: 601R-53-61-117-2 2L72 4F4 FRTA21EA E15NE 20031023000092003102300009NM 2003 10 23 03FDEA01451 120030902A5753ARC2512503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING - I/B FLAP O/B HINGE PIVOT LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71784, TITLE - WINGS - LEFT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20030908002842003090800284NM 2003 9 8 SWAA031933 120030828A53116546560 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND BS 947, FUSELAGE FRAME CORRODED AT WL 210, RBL 45. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030908002922003090800292NM 2003 9 8 SWAA031941 120030831A2923887477 PUMP BOEING737 7375H4 138449DNM HYD SYSTEM FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29527SW 26569 AIR TURN BACK, HYD B-SYS PUMP LOW PRESS INDICATION LIGHT ILLUMINATED. REMOVED AND REPLACED HYD B-SYS PUMP PER MM. 2L72 4F RTA16WE 20030908003012003090800301NM 2003 9 8 SWAA031920 120030827A53306550570 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CUTOUT CRACK AT AFT ENTRY DOOR UPPER AFT CORNER. REPAIRED SKIN PER SRM AND SWA EA. 2L72 4F RTA16WE 20030908003112003090800311NM 2003 9 8 SWAA031889 120030823A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 759 AT STR 23L AT BS 773 AT STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030908003222003090800322NM 2003 9 8 SWAA031900 120030825A3350BR2013 STRIP BOEING737 7373A4 1384585NM CABIN DETERIORATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED A2 CHECK, FOUND EEPLS DETERIORATED AT ROW'S NR 7, NR 8 AND NR 9. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20030908003372003090800337NM 2003 9 8 SWAA031931 120030829A3350610478 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. CHARGED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20030905002082003090500208SO 2003 9 5 C2XA03TY142 120030828A531513500469401 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 TYS DURING A SCHEDULED 2C INSPECTION THE FLOORBEAM AT FR 22 RT SIDE WAS FOUND CORRODED IN SEVERAL AREAS. MAINT R&R THE FLOOR BEAM AT FR 22 IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030905002262003090500226SO 2003 9 5 C2XA03TY121 120030811A534714530659001 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF2 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. 2L72 4T RTT00011AT 20031001000422003100100042WP 2003 10 1 UPS03841187 120030827A5310 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, MIDSHIP ACCESSORY COMPARTMENT RT SIDE AT STA 670 L28R IS CRACKED. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS IAW DC8 SRM 53-2 -0(ORIG-.062 AND REMAINING-.017). FABRICATED REPAIR ANGLE IAW DC8 SRM T R53-122. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE IAWDC8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20031001000802003100100080NM 2003 10 1 2003UALA00719 120030731A5754114W426012 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 9 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29771UA 26932 T/E WEDGE DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE AND FASTENER HOLES. 2L72 4F4 FRTT0001SE E46NE 20031001001302003100100130WP 2003 10 1 GTIA030673 120030906A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FOUND AMIN CABIN FS 525 AND FS 446 WEB IS CRACKED AT LBL 54. TRIMMED OUT DAMAGE. FABRICATED TWO REPAIRED DOUBLERS AND FILLER. INSTALLED TWO REPAIRED DOUBLERS AND FILLER. (M) 2L72 4F A6WE 20031002000052003100200005NM 2003 10 2 USAA030184 120030828A5553AMS4640 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US40788 23984 FOUND FITTING CORODED 1 INCH BETWEEN LAYERS, VERT STAB RT AFT OUTBOARD ATTACH POINT BETWEEN T-FITTING AND CLEVIS. OVERSIZED PART, REMOVED AND REPLACED BUSHING PER SRM 55-30-90 AND EA 76801. CORROSION LEVEL 1, TASK NR C55-706-11. (M) 2L72 4F RTA16WE 20031002000132003100200013SW 2003 10 2 2003F00590 120030408A5270 SWITCH FRCHLDSA227 SA227DC 3377521SW CARGO DOOR OUT OF RIG A BSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM05853LS DC853B CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB-OUT AT 11,500 FEET MSL. CREW FOLLOWED CHECKLIST PROCEDURES AND RETURNED TO STATION. SUSPECT DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, OR DOOR CLICK CLACK OR SWITCH RIGGING. DOOR WAS OPENED AND RECLOSED. FLIGHT CONTINUED WITH NO FURTHER PROBLEM. AIRCRAFT WAS REINSPECTED BY MAINTENANCE UPON RETURN TO MAIN BASE. NO DEFECTS WERE NOTED. (M) 2L72 4T RTA18SW 20031002001802003100200180EU 2003 10 2 AALA20030658 120030615A3350 CONNECTOR FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211470K 11506 DURING OVERNIGHT MAINTENANCE, RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. INSTALLED PIN IN CONNECTOR FOR RIGHT AFT OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031003000042003100300004NE 2003 10 3 AALA20030965 220030907A7200 ENGINE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 1 AND 2 BIRD INGESTION A AALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW2177080 626 695169 AT 130 KNOTS ON TAKEOFF, THE NR 1 ENGINE BLACK AND WHITE STRIPE NEEDLE FAILED TO ZERO. TAKEOFF CONTROL THEN ENGINE TRIM FAULT LIGHT ILLUMINATED WITH THE TRIM OF NR 1 ENGINE PARAMETERS FLUCTUATED CONSISTENE WITH AN ENGINE PROBLEM. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. NO OVERWEIGHT LANDING. EVIDENCE OF BIRD STRIKE ON THE NR 1 AND 2 ENGINES. UPON FURTHER INVESTIGATION WITH CARDS 05-92-15 BIRD STRIKE CARDS, IT WAS DETERMINED THAT THE BLOOD SPLATTER ALL OVER THE NOSE COWL WAS DUE TO INSECTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA35EU E13NE 20031003000152003100300015NM 2003 10 3 AALA20030918 120030830A3397 TERMINAL BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 EMERGENCY LIGHTS INOPERATIVE ON FORWARD SIDE OF AFT LEFT DOOR. BATTERY PACK FAILED DUAL FEED CHECK. TIGHTENED LOOSE NR 1 TERMINAL AT LIGHT FIXTURE L396. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031003000412003100300041NM 2003 10 3 AWXA200301045 120030909A54106552263231 GUSSET BOEING737 737277 1384570NM NR 1 NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .1250 INCH CRACK WAS FOUND AT FASTENER HOLE ON NR 1 ENGINE FIXED FAIRING COVER PLATE (GUSSET) AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED GUSSET ON NR 1 ENGINE FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT GUSSET IAW DWG 65-52263; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 1. 2L72 4F RTA16WE 20031003000432003100300043NM 2003 10 3 AWXA200301047 120030903A53206545402244 ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .3125 INCH CRACK WAS FOUND AT FASTENER HOLE ON L ANGLE AT BS 663 IN LT AFT AIR CONDITIONING BAY ABOVE TURBO FAN. MAINTENANCE REMOVED CRACKED HORIZONTAL (L) ANGLE AT BS 663; FABRICATED A NEW REPLACEMENT (L) ANGLE IAW DWG 65-45402; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 1 FIG. 011. 2L72 4F RTA16WE 20031003000492003100300049EA 2003 10 3 QXEA200301112 220030909A7320304768305 VALVE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 MALFUNCTIONED A QXEAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NM09405QX4183 4183 4047 AF0118 ON FLIGHT 2355 RECIEVED NR 2 FADEC LIGHT IN FLIGHT. SHUTDOWN NR 2 ENGINE IAW CHECKLIST. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 ENGINE P-2-2 BLEED VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20031003000612003100300061SO 2003 10 3 C2XA03SH324 120030913A542014576631622 STIFFENER EMB 145 EMB145LR 3260212SO NR 2 NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE NUMBER 2 LOWER COWLING AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031003000632003100300063SO 2003 10 3 C2XA03SH326 120030913A532014522460015 STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE AFT DIGITAL STRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031003000762003100300076NM 2003 10 3 03FDEA01529 120030906A5753ARC198414 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) INBOARD PIVOT ATTACHMENT BORE BUSHING FOUND LOOSE. 2L73 4F RTA22WE 20031003000942003100300094NM 2003 10 3 C1HA200395067 120030913A3610 DUCT BOEING727 727290 138408WNM NR 3 ENGINE LEAKING A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15295CA 22147 ON TAKEOFF A RIGHT A/C PACK TRIP, FOLLOWED BY A RIGHT DUCT OVERHEAT, ABOUT A MINUTE LATER WITH AN ENG 3 STRUT OVERHEAT ILLUMINATING ABOUT 30 SEC LATER. COMPLIED COM PROCEDURE 2.36.9 WHICH CAUSED THE STRUT OVERHEAT LIGHT TO GO OUT AND ISOLATED THE LEAK ON REMOVED STUB WING PANELS ENG NR 3. FOUND 3 EACH DUCTS LEAKING, 2 ON PRE-COOLER AND 1 ON 13TH STAGE MODULATING VALVE. NO CRACKS FOUND. TIGHTENED CLAMPS ON LEAKING DUCTS, RAN ENGINE. TURNED OFF NR 2/APU BLEEDS, OPENED NR 1 AND NR 3 BLEEDS, TURNED ON BOTH. 2L73 4F A3WE 20040128000852004012800085NM 2004 1 28 AWXA200301628 120031207A5320654681233 STRAP BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT LAVATORY MAIN DECK STIFFENER STRAP BS 1016 TO BS 1025, LBL 17. MAINTENANCE REMOVED CORRODED STIFFENER STRAP BS 1016 TO BS 1025, LBL 17; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 9, PG 1 & 39-41. 2L72 4F RTA16WE 20040128001332004012800133SO 2004 1 28 C2XA03CL219 120031230A3350BA50933901 CHARGER EMB 145 EMB145XR SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714116 145672 SAT FLIGHT 2877 THE CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. THE PROBLEM REOCCURED ON FLIGHT 2877. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGING TRAY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20040128001752004012800175SO 2004 1 28 C2XA03IA116 120031228A33501317 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712957 145080 CLE FLIGHT 2390, PILOT REPORTED THAT THE COCKPIT ENTRANCE EMERGENCY LIGHT OPERATES INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB AND OPERATIONALLY TESTED THE LIGHT ASSEMBLY. 2L72 4F RTT00011AT 20040129000322004012900032EU 2004 1 29 MALA030577 120031225A3020 LINE BAC 146 AVRO146RJ85A1500097EU NR 4 ENGINE CONTAMINATED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15536XJ E2372 INTAKE LOW PRESSURE LIGHTS ILLUMINATED ON NR 3 AND NR 4 ENGINES ON TAKEOFF OF FLIGHT 3589. ABORTED TAKEOFF. MAINTENANCE PERFORMED TROUBLESHOOTING OF NR 4 ENGINE INTAKE LOW PRESSURE LIGHT IAW MM 30 FOUND NR 4 ENGINE PRESS REF LINE CONTAMINATED. REMOVED, CLEANED AND REINSTALLED LINE IAW MM. PERFORMED OPS CHECKS IAW MM, ALL CHECKS GOOD. 2H74 4F RTA49EU 20040129001002004012900100NM 2004 1 29 DHL2003742535 120031205A3210651986311 STIFFENER BOEING727 727225 1384077NM MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPON REMOVAL LT HAND NOSE LG TRUNNION THE VERTICAL STIFFENERS SUPPORT FWD & AFT (2 EA) FOUND CRACKED NDT CONFIRMED. DRILLED UP NEW PARTS P/N 65-19863-11 PO3348189 & P/N 65-19863-9 PO3348189 USING EXISTING FASTENER HOLES IAW B727 SRM 51-30-05 & 51-30-06. ALODINE, PRIMED AND PAINTED PARTS IAW B727 SRM 51-10-02 AND INSTALLED VERTICAL STIFFENERS IAW B727 SRM 51-30-02. 2L73 4F A3WE 20040129001022004012900102NM 2004 1 29 DHL2003742537 120031120A5343 SUPPORT FITTING BOEING727 727225 1384077NM MLG DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, LT MLG SUPPORT FITTING RETAINER BOLT LUGS ELONGATED. ACCOMPLISHED REPAIR TO LT MLG SUPPORT FITTING IAW B727 S/B 57-0153 REV 4, LEAK CHECK GOOD. 2L73 4F A3WE 20040129001082004012900108SO 2004 1 29 DHL200374246 120031202A5751 SKIN PIPER PA18 PA18150 7101828SO AILERONS SEPARATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742 188146 DURING A C-CHECK, LT WING OUTBOARD AILERON HAS THREE LOOSE RIVETS IN UPPER SKIN. REMOVED OLD SKIN FOR LT WING O/B AILERON IAW B727 SRM 51-30-2, FABRICATED NEW SKIN O/B AILERON FROM MAT 2024-T3 .020 PO900355 DIM 121 X 15.25 INCH AND DOUBLER SKIN FROM MAT 2024-T3 .020 PO 900355 DIM 121 X 15.25 INCH IAW B727 SRM 57-50-2. NEW SKIN DOUBLER CLEANED, TREATED, PRIMED, PREPPED AND BONDED IAW B727 SRM 51-40-5. INSTALLED NEW SKIN FROM O/B AILERON IAW B727 SRM 51-30-2. 1H71 3O 1A2 20040129001162004012900116WP 2004 1 29 0302219935 120031227A5315 FLOORBEAM DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011332U 47404 DURING M-CHECK FOUND CORROSION ON FLOORBEAM WEB AT BS 996 RBL 50. REPAIRED PER EA 99-197352. 2L72 4F A6WE 20040129001222004012900122NM 2004 1 29 DHL2003742554 120031124A5730 SKIN BOEING727 727225 1384077NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, RT WING UPPER L/E SKIN WS 460 HAS CRACKS FROM RIVET ROW HOLES 3 PLACES. REMOVED FUELING RECEPTACLE MANIFOLD IAW B-727 MM 28-21-11. CUT OUT DAMAGED AREA, FABRICATED FILLER DIM 5.5 X 2.5 INCH FROM 2024 T3 .040 PO 900414 AND DOUBLER DIM 8 X 7 INCH FROM 2024 T3 .050 PO 900414 IAW B-727 SRM 57-30-4. TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED FILLER AND DOUBLER ON RT WING UPPER SKIN WS 460 IAW B-727 SRM 51-30-2. LEAK CHECK GOOD IAW B-727 MM 28-21-0. 2L73 4F A3WE 20040129001412004012900141NM 2004 1 29 AWXA200400016 120031227A532165458332 FLOOR PANEL BOEING737 7373B7 1384580NM CRACKED CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 .3125 INCH CRACK WAS FOUND ON WEB UNDER FLIGHT COMPARTMENT FLOOR AT BS 196, RBL 65, WL 207. MAINTENANCE CRACKED WEB AT BS 196, RBL 65, WL 207; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45833; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040129001752004012900175NM 2004 1 29 DHL200374263 120031123A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM, LBL 50 - RBL 50, WL 208, AS VIEWED FROM NWW DOGHOUSE AREA. REMOVED 9G BULKHEAD, AND SHEAR WEB FOR ACCESS IAW B727 SRM 51-30-2 AND MM 53-20-11, REMOVED DAMAGED UPPER CHORD BS 344 AND FABED NEW FROM BAC1505-29222 PO 3348139 DIM 11.75 FT LONG IAW 727 SRM 51-20-1 & 53-10-2 FIG 7. NEW CHORD TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2. REINSTALLED SHEAR WEB, FLOORBOARDS AND 9G BULKHEAD IAW 727 SRM 51-30-2 & MM 53-20-11. 2L73 4F A3WE 20040129001882004012900188NM 2004 1 29 F3LA200300189 120031231A5320 SILL BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03304FL 3318 27633 DURING C-7 CHECK, INSPECTION REPORTED R2 DOOR FRAME MOP SILL CORRODED FROM STA 947.5 TO 1000, STR 17R. REPLACED MOP SILL PER SRM 51-40-02 AND 53-60-15. 2L72 4F RTA16WE 20040130000032004013000003NM 2004 1 30 SWAA032834 120031230A3350101114 LENS BOEING737 7373H4 1384600NM OVERWING EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 RT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20040130000042004013000004NM 2004 1 30 SWAA032835 120031230A53116552874 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR UPPER HINGE BOX FRAME ASSY BROKEN. REPAIRED UPPER HINGE BOX FRAME ASSY PER SRM. 2L72 4F RTA16WE 20040130000052004013000005NM 2004 1 30 SWAA032836 120031230A52106545871 FRAME BOEING737 737301 1384611NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER FRAME WEB CRACKED AT FWD STOP FITTING. REMOVED AND REPLACED L1 DOOR ASSY PER MM. 2L72 4F RTA16WE 20040130000062004013000006NM 2004 1 30 SWAA032837 120031230A533065C35777 BEAR STRAP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 847, WL 148, RBL10. REPAIRED STRAP PER BFG ER. 2L72 4F RTA16WE 20040204000222004020400022EU 2004 2 4 03FDEA01802 120031025A5420 FITTING AIRBUS300 A300B4605R 3930308EU GE CF6 CF680 30025NE NR 1 ENGINE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25660FE 759 BFM CLOSER NR S 10 COMPLY WITH EA NR 6-5450-73844 PYLONS/NACELLES-NR 1 ENGINE PYLON FWD MOUNT CORROSION REPAIR. FACT 25OCT03 16:43 BFM U COMPLIED WITH EA NR 6-5450-73844- PYLONS/NACELLES - NR 1ENGINE PYLON FWD MOUNT CORROSION REPAIR. CLOSED ON 10/25/03. 2L72 4F4 FRTA35EU E13NE 20040204000382004020400038NM 2004 2 4 AWXA200301257 120030924A339714803180 CONNECTOR BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - EEL - DURING C-17 CHECK SEVERAL EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTORS WERE FOUND DAMAGED BETWEEN BS 370 TO BS 920 L/H SIDE. MAINTENANCE REMOVED AND REPLACED DAMAGED EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTORS AND SPLICES BETWEEN BS 370 TO BS 920 L/H SIDE IAW SWPM 20-42-01 & SWPM 20-30-12, OPERATIONAL CHECK WAS GOOD. PART NAME; SOCKET, MFG; HS ELECTRONICS, P/N 60-617-1 PART NAME; SPLICE, MFG; HS ELECTRONICS, P/N D436-37 2L72 4F4 FRTA16WE E2GL 20040204000682004020400068EU 2004 2 4 03FDEA01728 120031014A5270 WARNING LIGHT AIRBUS300 A300B4622 3930401EU CARGO DOOR FALSE ACTIVATIONA FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25716FD 358 JUST STARTING T/O ROLL GOT ECAM-AFT CARGO DOOR NOT CLOSED. REJECTED T/O LESS THAN 60 KNOTS. RIGHT ECAM SHOWED AFT CARGO DOOR CLOSED. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-30-03, CATEGORY: C EXPIRATION: 24OCT03 (MEL 52-30-03: AFT CARGO DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE) INOP. AFT CARGO DOOR VISUALLY CHECKED, CLOSED AND LOCKED. FACT 15OCT03 17:07 IAH R CHECKED DOOR OPS, CLEANED DOOR RELEASE HANDLE LATCH CAM ASSY, OPERATED DOOR SEVERAL TIMES AND OPERATION NORMAL, INDICATION SYSTEM CHECKS OK. ENT BY: 097974 2L72 4F RTA35EU 20040204000772004020400077EU 2004 2 4 U30A200300036 120031018A5220 WARNING LIGHT AIRBUS320 A320212 3930322EU GE CFM56 CFM56* 13802NE EMEGENCY EXIT FALSE ACTIVATIONA U30AO OTHER N FALSE WARNING CRCRUISE 1 EA17265AV 427 DURING CRUISE ON FLT 143 PUJ-BWI, THE LT AFT EMERGENCY WINDOW EXIT SHOWED ARMED ON ECAM (ABOVE FL 250). NO CHANGE IN CABIN ALTITUDE. ON GROUND, MAINTENANCE VERIFIED THAT THE PROX SENSOR AT THE LT AFT EMERGENCY EXIT HATCH ACCESS COVER TO BE OPERATIONAL IAW AMM 52-70-00-040-007. INDICATION OK AT THIS TIME. NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E2GL 20040204000782004020400078NM 2004 2 4 2003UALA00771 120031011A3350 GUARD BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGNECY LIGHT LOOSE A UALAO OTHER O OTHER APAPPROACH 1 WP29122UA 29168 EMERGENCY LIGHTS ON WITH SWITCHES IN NORMAL POSITION DURING ARRIVAL. SECURED EMERGENCY LIGHTS SWITCH GUARD AT DOOR 1L. 2L74 4F4 FRTA20WE E24NE 20040204000922004020400092EA 2004 2 4 SWIA200312508 120031012A5210 SHAFT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HANDLE ROLLER BENT A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07432SW 7548 ON ARRIVAL TO DFW, RECEIVED PAX DOOR OUT HANDLE CAUTION MESSAGE. MESSAGE INTERMITTENT, THEN ON CONTINUOUSLY TO LANDING. DOOR HARD TO OPEN. FOUND INNER DOOR HANDLE ROLLER SHAFT BENT. REMOVED AND REPLACED INNER DOOR HANDLE ROLLER ASSY WITH SERVICEABLE ONE IAW CL600 MM 52-10-00. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040204001002004020400100NM 2004 2 4 AWXA200301280 120031003A53476546815 SEAT TRACK BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK CORROSION WAS FOUND ON SEAT TRACK BS 887 TO BS 947, LBL 45. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF SEAT TRACK BS 887 TO BS 947, LBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK, 2 EACH SPLICES AND RADIUS FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-52, FIG. 204. 2L72 4F4 FRTA16WE E2GL 20040204001112004020400111EA 2004 2 4 JBXA03019 120031022A2613 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE COCKPIT FALSE ACTIVATIONA JBXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO05592ML 7036 FLIGHT 5156 FROM DCA TO JAX DEVERTED TO RDU AT 5156 FOR A LT 14TH STAGE DUCT WARNING. INSPECTED SYSTEM NO DEFECTS FOUND. RAN AC COULD NOT DUPLICATE. IAW CRJ AMM 26-10-07. AC RELEASED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040204001152004020400115NM 2004 2 4 QXEA200301311 120031023A5270 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 800 FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09413QX 4060 PIH-ON FLIGHT NUMBER 2288, AFTER TAKEOFF CREW RECEIVED AN AFT BAGGAGE DOOR WARNING. NO LOSS OF PRESSURE. FLIGHT CONTINUED ON TO PIH AND LANDED WITHOUT INCIDENT. NO CFR. INSPECTED DOOR CLOSE SENSOR, NO DEFECTS NOTED. CLEANED DOOR CLOSED SENSOR SPRING. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040204001162004020400116EU 2004 2 4 00119 120031022A3260 DOWNLOCK SWITCH AMD FALC20FALCON 2720302EU MLG OUT OF ADJUST E HAEAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 SW05240TW 40 PILOT REPORTED LT MAIN INDICATOR LIGHT OFF, RAN EMERGENCY PROCEEDURES, LANDING UNEVENTFUL AT LEX, LT GEAR INSPECTED AND FOUND SAVE FOR FERRY FLIGHT FROM LEX TO SDF, AT SDF MAINTENANCE FOUND LT MAIN DOWN LOCK SWITCH OUT OF AJUSTMENT, RIGGED SWITCH AND OPS GOOD. 2L72 4F A7EU 20040204001272004020400127NM 2004 2 4 EIA2003121 120031003A5311 SPAR BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 CORROSION ON REAR SPAR WEB TO THE INBOARD SIDE AND UNDER THE LT BULKHEAD FITTING AT BS 1241 UPPER PORTION APPROXIMATELY FASTENER NR 32 AREA DOWN. REMOVED CORROSION ON REAR SPAR WEB UNDER THE LT BULKHEAD FITTING AT BS 1241, IAW EO NR 57-747-1544-99 REV A 2L74 4F A20WE 20040204001292004020400129NM 2004 2 4 EIA2003118 120030930A5313 STRINGER BOEING747 747212B 1384886NM FUSLEAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 AFT CARGO COMPT. BS 1790 TO 1800 STR. 51R STRINGER HAS LIGHT SURFACE CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW B747 SRM 53--10-01 PG2-3. REMOVED AND REPLACED DAMAGED STRINGER FROM STA. 1740-1810 AND REPAIRED IAW B747 SRM 53-10-03 FIG 8 PGS. 33-40, 51-10-02 AND BSOPM 20-41-02 PAGES 7-8. 2L74 4F A20WE 20040204001312004020400131NM 2004 2 4 EIA2003115 120030725A3350S1356B37 LIGHT BOEING747 747212B 1384886NM CABIN MALFUNCTIONED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09485EV 20712 DURING GROUND TEST FOLLOWING FLIGHT EVALUATION. EMERGENCY CEILING LIGHT AFT UPPER DECK ILLUMINATES FOR ABOUT 3 SECONDS BEFORE GOING OUT: REMOVED AND REPLACED LIGHT UNIT IAW MM 747-33-51-00 2L74 4F A20WE 20040204001322004020400132NM 2004 2 4 EIA2003125 120030921A3320S1356B37 LIGHT BOEING747 747132 1384882NM UPPER DECK UNSERVICEABLE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 DOME LIGHT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-07. 2L74 4F A20WE 20040204001332004020400133CE 2004 2 4 DXTA200300146 120031024A3260 BULB CESSNA500 560CESSNA 2076750CE MLG INDICATOR INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07335QS 5600335 DURING APPROACH AT TEB LT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED, EXTENDED GEAR WITH PNEUMATIC BLOW DOWN SYSTEM. REMOVED 4 INOPERATIVE LIGHT BULBS AND INSTALLED 4 NEW BULBS IAW CE560 MM CHAPTER 33-13-01. BLED GEAR HYDRAULIC SYSTEM, PERFORMED OPS CHECK IAW CE-560 MM CHAPTER 32-01-00. OPS CHECKED GOOD. 2L72 4F RTA22CE 20040204001412004020400141NM 2004 2 4 EIA2003144 120031020A5330 LAP JOINT BOEING747 747212B 1384886NM PWA JT9 JT9D* NE FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 UPON REMOVAL OF A/C DUCTS, CHAFFING WAS FOUND ON UPPER AND LOWER SKINS AND ON NUMEROUS FASTENERS AT STA. 980 STRINGER 39 LAP JOINT. REPAIRED DAMAGE ON UPPER AND LOWER SKINS AND FASTENERS AT STA. 980 STRINGER 39L, LAP JOINT IAW B747 SRM 53-30-03 FIG 13 AND B747 SRM 53-10-03, FIG 1. 2L74 4F4 F A20WE E20EA 20040204001482004020400148NM 2004 2 4 EIA2003141 120031020A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 FUSELAGE BELLY SKIN CRACKING AT THE AFT EDGE OF THE EQUIPMENT COOLING OUTLET BETWEEN STRINGER 44L AND 45L AT BS 580 ( APPROX) CRACK IS BOTH FORWARD AND AFT OF COUNTER SUNK RIVET FASTNER. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR IAW ECRA 482-53-189-2 AND SB 747-53-2386 2L74 4F A20WE 20040204001572004020400157NM 2004 2 4 EIA2003130 120031020A5711 SPAR BOEING747 747212B 1384886NM RT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 RT WING UPPERCHORD OF FIX TRAILING EDGE PANEL SUPPORT BEAM SPAR APPROX WBL 235.2-445 CORRODED. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-57-184-2 2L74 4F A20WE 20040204001632004020400163WP 2004 2 4 IXXA0300070O 120031029A2133 BEARING DOUG DC8 DC862 3021970WP PWA JT3D JT3D* 52039NE OUTFLOW VALVE LACK OF LUBE A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11728PL847912923 45918 DURING CLIMB FROM FJDG CREW LOST CABIN PRESSURIZATION. CREW RETURNED TO FJDG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED OUTFLOW VALVE. THEY LUBED MECHANICAL ARMS AND BEARINGS. OPERATIONAL CHECK GOOD BOTH IN AUTO AND MANUAL PER ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20040204001682004020400168EU 2004 2 4 XNOA1162 120031023A2910 LINE AIRBUS300 A300B4203 3930306EU GREEN HYD SYSTEMLEAKING A XN0AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23474AS 219 IN FLIGHT LOST GREEN HYD SYS. LOST GREEN HYD QTY ASSOCIATED WITH LEVEL LOW LT. MANUAL GEAR EXTENDED. FOUND PINHOLE IN LT GEAR OVER-CENTER LINK FLEX LINE, GREEN HYD SYS, REMOVED AND REPLACED FLEX LINE IAW A300 AMM 20-23-11 BLEED OUT HYD SYS, REPLENISHED AS REQUIRED. NO LEAKS NOTED. OP'S CK GOOD. RESTORED LANDING GEAR EXT SYS TO NORM CONFIGURATION IAW A300 AMM 32-30-00. (STATUS: ORIG/CLOSED) 2L72 4F RTA35EU 20040204001792004020400179CE 2004 2 4 55657 120031029A3240 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG WEAK A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07133YV UE133 CREW REPORTED BRAKES ON RT SIDE FELT SPONGY. MAINT. BLEED BRAKES AND FOUND NO LEAKS. OPS CK NORMAL 2L72 4T3 TRTA24CE E2NE 20040204001832004020400183NM 2004 2 4 PCAA0311135 120031102A5320 SILL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE FUSELAGE GOUGED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13828EX 392 WHILE IN ROUTINE MAINTENANCE, IT WAS DISCOVEERED THE BAG DOOR HANDLE HAD GOUGED THE UPPER BAG DOOR SILL ON AIRFRAME IN TWO PLACES. MAINTENANCE REPAIRED UPPER SILL IAW CAS AAL150 REPAIR DRAWING AND PERFORMED EDDY CURRENT INSPECTION, NO FLAWS DETECTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040204001922004020400192NM 2004 2 4 03FDEA01881 120031105A3260 DOWNLOCK SENSOR BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE NLG DIRTY A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25484FE 21466 ON APPROACH, WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR, LEFT GEAR AND RIGHT GEAR ALL INDICATED (GREEN) DOWN AND LOCKED, AND THE RIGHT GEAR ALSO INDICATED (RED) GEAR UNSAFE. RECYCLED THE GEAR TO UP THEN DOWN, AND INDICATION WAS NORMAL. T/S DOWNLOCK SENSOR. PER 727 M/M 32-61-091-4. ALL INDICATIONS NORMAL. CLEANED SENSOR AND TARGET. LUBED UP LOCK PER 727 M/M 12-21-001-2. 2L73 4F4 FRTA3WE E2EA 20040204001962004020400196 2004 2 4 SWIA200312570 420031031A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07578SW 120346 STALL WARNING LIGHT WOULD NOT EXTINGUISH ON THE MAP. REMOVED AND REPLACED STALL WARNING PANEL WITH A SERVICEABLE PANEL IAW AMM 27-00-00. OPS CHECK GOOD. P/N: 120-34428-505 2L72 4T4 TRTA31SO E20NE 20040204002012004020400201 2004 2 4 SWIA200312575 420031103A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07295UX6582 6582 120295 WITH YAW ENGAGED AND RUDDER IN TRIM, THEN ENGAGED AUTO PILOT AND AIRPLANE YAWED AND BALL JUST WENT .5 SCALE TO LT, HAPPENED ON BOTH SIDES. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL IAW MM 22-10-04. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040210000042004021000004EA 2004 2 10 COMA0360521 120031127A2741 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MACH TRIM ACTIVATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01496CA 7791 FLIGHT 6858) AFTER TAKE OFF AND DURING CLIMB RECEIVED A (STAB TRIM) AND (MACH TRIM) CAUTION, SYSTEM WOULD NOT RESET, AIRCRAFT RETURNED TO DEPARTING CITY (DSM). INTERROGATED HSTCU, NO FAULT CODES FOUND, CLEANED THE STAB TRIM PANEL AND PERFORMED AN OPERATIONAL CHECK, SYSTEM OPERATED NORMAL. 2L72 4F RTA21EA 20040210000872004021000087EU 2004 2 10 USAA030298 120031122A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH AREA, FS 57 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210000982004021000098EU 2004 2 10 USAA030294 120031122A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .150 SQUARE INCH, FRAME 58 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040212000182004021200018CE 2004 2 12 AMWA87 120031126A553110164000025 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07138YV UE138 DURING THE D-6 INSPECTION THERE WAS TWO CRACKS FOUND ON THE RIB ON RT SIDE AT STRINGER. CRACK LOCATED AT END OF RIVET ON JOGGLE OVER STRINGER. RIB NR 3 FROM TOP. REPAIRED CRACKS IAW BMM. P/N 101-640000-25, 39.289 2L72 4T RTA24CE 20040212000482004021200048SO 2004 2 12 ENHA2003P3101 120031207A2140 ENGINE PIPER PA31 PA31350 7103110SO LEFT CONTAMINATED E ENHAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL0378GA 318352030 DURING TAKE-OFF ROLL AND INITIAL CLIMB PASSENGERS NOTIFIED PIC OF SMOKE/HAZE IN THE CABIN. THE PILOT DECLARED AN EMERGENCY AND RETURNED FOR LANDING. THE AIRCRAFT HAD BEEN DEICED PRIOR TO DEPARTURE. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT DEICE FLUID HAD BEEN SPRAYED SUCH THAT IT WAS ALLOWED TO ENTER THE AUX HEATER MUFF AIR INLETS. THIS AIRCRAFT IS EQUIPPED WITH STC NR SA240CH AUXILLARY HEATING INSTALLED ON LEFT ENGINE. CAUSE OF SMOKE/HAZE DETERMINED TO BE INGESTION OF DEICE FLUID IN AUX HEATER INLETS. FURTHER OPERATION OF HEATING SYS AFTER CLEARING DEICE RESIDUE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 1L72 3O A20SO 20031003000952003100300095NM 2003 10 3 C1HA200385008 120030912A2910 HYDRAULIC LINE BOEING727 7272S7 138407ZNM NR 2 SYSTEM RUPTURED A C1HAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL15685CA 22492 ON DESCENT HAD HYD A ENG 1 PUMP LOW PRES LITE ON A QUANTITY -0- RAN PRECEDURE 2.29.2- AFTER A PUMP AND FLUID SHUT OFF TURNED OFF, QUANTITY CAME UP TO 1.5 GAL. FLT ATTENDANT REPORTED GRINDING NOISE FROM ENG 1 WHEN QTY INDICATED 1.5- PUMPS AND SHUTOFFS WERE TURNED ON AND QTY IMMEDIATLY WENT DOWN TO ZERO- PUMPS AND SHUTOFFS TURNED BACK OFF FOR REMAINDER OF FLT. QUANTITY SHOWED 1.5 GAL AGAIN. INSP AND FOUND NR 1 ENG PUMP OK . FURTHER INSP FOUND NR 2 HYD HI PRESSURE LINE RUPTURED. REMOVED AND REPLACED LINE IAW MM 29-00-00 PG 3. LEAK CHECK GOOD. (REMOVED AND REPLACED PRESSURE AND K STRAINS FILTERS IAW MM 29-11-41 PG 202 AND 29-11-60 PG 301) 2L73 4F A3WE 20031003001012003100300101WP 2003 10 3 UPS03841221 120030827A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT LBL 26 AND 36, 67 ABOVE CABIN FLOOR CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLERS AND FILLERS I.A.W. DWG. SRO08530007 2L74 4F RT4A25 20031006000102003100600010EU 2003 10 6 MALA030406 120030905A5610 WINDSHIELD SAAB SF340 340B 7860101EU COCKPIT BIRD STRIKE A MALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL15363PX 340B260 DURING FLIGHT 3107, BIRD STRIKE TO CAPTAINS FWD WINDSCREEN. AIR RETURN TO DTW. MAINTENANCE INSPECTED A/C AND ENGINE VERIFIED BIRD STRIKE ON CAPT WINDSCREEN CLEANED, NO FURTHER DAMAGE NOTED. ALL WORK DONE IAW GMM ALL CHECKS GOOD. 2L72 4T RTA52EU 20031006000262003100600026NM 2003 10 6 QXEA200301120 120030909A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 DENTS IN LT HAND FUSELAGE SKIN BETWEEN X281.0 - X301.0 AND STRINGERS 10P AND 11P. REPAIRED IAW Q400 SRM 51-00-02, 51-18-00, RD 8/4-53-659 AND EA 6-53-202. 2H72 4T RTA13NM 20031006000272003100600027NM 2003 10 6 AWXA200301052 120030813A5330 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .5625 INCHES CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN OF L-1 DOOR CUTOUT AT FASTENER HOLE LOWER AFT CORNER. MAINTENANCE CUTOUT CRACK ON SKIN OF L-1 DOOR CUTOUT LOWER AFT CORNER AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; 2L72 4F RTA16WE 20031006000282003100600028NM 2003 10 6 AWXA200301054 120030912A2560P4010021 BATTERY BOEING757 757225 1384959NM ZONE 900 - LAV DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28913AW 22207 FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20031006000312003100600031NM 2003 10 6 AWXA200301057 120030913A2421803689 GARLOCK SEAL BOEING BOEING737 737277 1384570NM CSD FAILED A AWXAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 WP28178AW 14890 22645 ON CLIMB OUT OF PHX EN ROUTE FOR BOI THE NR 1 GENERATOR TEMPERATURE WENT INTO THE YELLOW FOLLOWED BY A GENERATOR HIGH TEMPERATURE LIGHT, ATTEMPT APU START WITH NO SUCCESS. FOLLOWED QUICK REFERENCE HANDBOOK AND DISCONNECTED THE NR 1 GENERATOR, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 CONSTANT SPEED DRIVE IAW T/C R5M24003, AND REPLACED GARLOC SEAL IAW BMM 72-61-00, PG. 5, STEP 5B. OPERATIONAL AND LEAK CHECKS WERE GOOD. VENDORS FUNCTIONAL CHECK OF CSD S/N 14890 CONFIRMED FAILURE OF UNIT. UNIT WAS FOUND LEAKING FROM INPUT CARBON SEAL DUE A WORN INPUT BEARING AND SEAL RETAINER, LOSS OF OIL CAUSED HIGH TEMPERATURE INDICATION. UNIT WAS OVERHAULED. 2L72 4F RTA16WE 20031006000522003100600052NE 2003 10 6 MEX2003407 220030902A7200 ENGINE BOEING757 757200 1384950NM PWA 2037 PW2037 NE NR 1 AND 2 MALFUNCTIONED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23703AM 27203 AIRCRAFT RETURN TO PLATFORM DURING ENGINES STARTING, THEY DID NOT STABILIZE IN LOW RPM AND THEY WERE SHUT DOWN. DURING REVISION NO ERROR EICAS MESSAGES WERE DETECTED AND PNEUMATIC PRESSURE OF APU WAS CORRECT. BOTH ENGINES WERE STARTED IAW MM, ALL TESTS CORRECT. DURING OVERNIGHT SERVICE, BOTH ENGINES WERE STARTED WITH IGNITION SYSTEMS 1 AND 2 IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20031006000622003100600062CE 2003 10 6 AMWA36 120030907A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 RIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 STRG P/N 101-640000-46 LT SIDE (3EA CRACKS ON THIS RIB) 2L72 4T RTA24CE 20031001001052003100100105NM 2003 10 1 USAABB03141 120030815A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19631AU 27809 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031001001142003100100114NM 2003 10 1 USAA030186 120030908A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 FOUND SKIN CRACKED 1.250 INCH, FUSELAGE SKIN FS 727E JUST ABOVE S23L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20031002000352003100200035 2003 10 2 GTIA030677 420030913A2565 SLIDE DOUG DC9 DC982 3022082WP L-2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 MCO - FLT 1304 - L-2 SLIDE FELL OFF DOOR. RE-INSTALLED L-2 SLIDE ON TO DOOR. (M) 2L72 4F A6WE 20031002000442003100200044WP 2003 10 2 WRLA200317 120030807A77208901224 SENSOR DOUG DC10 DC1030 3023501WP NR 1 ENGINE INOPERATIVE A WRLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27352WL 47838 ON TAKEOFF RUN ABOVE 80 KNOTS THE ENGINE FAIL LIGHT CAME ON TAKEOFF REJECTED AT 95 KNOTS. TROUBLE SHOOT PER TAFI 71-00-00 TO BAD CIT SENSOR REMOVED AND REPLACED SENSOR PER MM 73-20-02. OPERATION CHECK GOOD DURING ENGINE GROUND RUN ON NR 1 ENGINE ALL PARAMETERS NORMAL. REPLACED CIT SENSOR. (M) 2L73 4F A22WE 20031002000882003100200088NM 2003 10 2 C1HA200386004 120030908A5754 WEDGE BOEING727 7272S7 138407ZNM NR 3 SLAT GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 NR 3 SLAT TRAILING EDGE WEDGE GOUGED. 2L73 4F A3WE 20031002001142003100200114NM 2003 10 2 QXEA200301099 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- NR 2 SEAT TRACK IS CORRODED BELOW LEFT LUG IN CHANNEL, 11 INCHES AFT OF STATION X488. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20040212000512004021200051 2004 2 12 DYV2003F00003 420031201A6122DCFS290DT6 GOVERNOR CESSNA421 421C 2076016CE CONT O520 GTSIO520F 17032SO PROPELLER FAILED E DYVAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM074119M 420 421C1029 AFTER TAKEOFF THE POWER WAS REDUCED TO CLIMB POWER. AT THE PROPELLER RPM REDUCTION FROM 2235 TO 1900, THE PROPELLER WENT DIRECTLY INTO FEATHER. A SAFE PRECAUTIONARY LANDING. UPON INVESTIGATION ALL ENGINE FUNCTIONS WERE FOUND NORMAL EXCEPT THAT THE POSITION. WHEN THE GOVERNOR WS CHANGED, THE PROP UNFEATHERED AND ALL ENGINE AND PROPELLER FUNCTIONS WERE THEN FOUND TO BE NORMAL. THE REMOVED GOVERNOR DRIVE SHAFT COULD NOT BE TURNED BY HAND. IT HAS BEEN SENT TO O/H FACILITY TO DETERMINE THE INTERNAL FAILURE. SUPPLEMENTAL REPORT WILL BE ADDED WHEN INFORMATION BECOMES AVAILABLE. 1L72 3O3 O A7CE E7CE 20040212000572004021200057EU 2004 2 12 KBM2003F00099 120031105A6220126891P BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ROD END DAMAGED B KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 UPPER AND LOWER BEARING HAS DAMAGE, WORN AND HAS EXCESSIVE PLAY ON BEARING. REPLACED WITH NEW ROD END BEARINGS. 1G71 3U3 U H9EU E19EU 20040212000622004021200062CE 2004 2 12 GLBA20030513 120031203A1430 FASTENER BEECH 1900 1900D 1154162CE EMERGENCY EXIT CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03192GL UE192 SEVERAL CHERRY MAX RIVET HEADS CRACKED AROUND EMERGENCY EXIT DOOR INNER FRAME SKIN, REMOVED AND REPLACED CRACKED RIVETS STATION R4C 273.75, 288.00, 327.63, 348.25 USED RIVETS PN CR3243-5 AND -3. 2L72 4T RTA24CE 20040212000732004021200073NE 2004 2 12 MDR03015 120030606A6320SB3401103 BEARING SKRSKYS64 S64E 8142604NE M/R GEARBOX DISINTEGRATED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09FP201 A6032 64019 ROLLER BRG FAILED. MGB, SN A6-032, REMOVED FOR MAKING METAL, INDICATED BY MGB CHIP LIGHT. INSP IN SHOP INDICATEDRATCHETING NOISE COMING FROM RT INPUT ASSY WHEN ROTATED. LG AMOUNT OF METALS WERE FOUND IN MGB SUMP. WHILE REMOVING RT 1ST STG PRIMARY INPUT ASSY, ROLLER BRGS FROM SB3401-103 ROLLER BRG CONE WERE FOUND IN WEB AREA OF INTERMEDIATE HSG. REMOVAL OF RT INTERMEDIATE INPUT ASSY SHOWED EXCESSIVE AMOUNTS OF FERROUS METAL ON 2ND STG INPUT HSG. REMOVAL AND TEARDOWN INSP OF 2ND STG INPUT ASSY REVEALED ROLLER BRG CONE FAILED DURING OPERATION. DURING FAILURE,CAGE TO BRG CONE DISINTEGRATED EXCEPT FOR BOTTOM EDGE AS INSTALLED. NUMEROUS ROLLERS WERE MISSING, SOME WERE IN CHUNKS. 2G72 4U H4EA 20040212000922004021200092NM 2004 2 12 F3LA200300169 120031211A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND FLOORBOARD HOLE ON INTERCOSTAL AT STA. 950, LBL 46, WL 208. FABRICATED AND REPLACED INTERCOSTAL PER SRM 53-60-51, FIG. 1, SRM 51-40-02, AND EA B3-53R-10228. 2L72 4F RTA16WE 20040212000942004021200094NM 2004 2 12 EIA2003164 120031201A335051356B37 BATTERY BOEING747 747212B 1384886NM PWA JT9 JT9D* NE EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 OVERHEAD EMERGENCY LIGHT AT STA 2130 IS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSY IAW BMM 33-35-01 OPS CKD GOOD. 2L74 4F4 F A20WE E20EA 20040212001002004021200100NE 2004 2 12 PCAA0310125 220031018A7320 CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EEC DIRTY A PCAAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 EA13846EX 326 WHILE ON TAKEOFF ROLL IN DCA, FLIGHT NR 3516 HAD NR 2 ENGINE CONTROL MANUAL LIGHT COME ON, PROPS DROPPING TO 650 RPM. CONNECTOR ON ELECTRONIC ENGINE CONTROL AND TORQUE SIGNAL CONDITION UNIT WERE CLEANED AND AIRCRAFT WAS GROUND RUN AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040212001072004021200107NM 2004 2 12 DHL2003754020 120031212A3150 WARNING HORN BOEING727 727223 1384074NM COCKPIT ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01754DH 22008 RTO PERFORMED DUE TO TAKEOFF WARNING HORN SOUNDING. TRIM WAS IN THE GREEN, ADJUSTED SLIGHTLY AND PERFORMED NORMAL TAKEOFF. A/S AT TIME OF RTO WAS OK. THE EPR WAS APPROXIMATELY 1.5. NOTED BY MECHANIC. 2L73 4F A3WE 20040212001082004021200108NM 2004 2 12 757BJ0003 120031211A335020131A BATTERY PACK BOEING757 757236 1384971NM EMERGENCY LIGHT DISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05757BJ 22176 R4 DOOR EMERGENCY EXIT LIGHT BATTERY PACK WILL NOT HOLD CHARGE. REPLACED BATTERY PACK IAW MM 33-51-07. OPS CHECK NORMAL. 2L72 4F RTA2NM 20040212001222004021200122SW 2004 2 12 KBM2003F00107 120031119A256011010214 SEAT BELT BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL COCKPIT FRAYED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 PILOT OUTBOARD SEATBELT FRAYED. INSTALLED REPAIRED SEATBELT ASSY. 1G71 3U3 U H2SW E4CE 20040212001242004021200124WP 2004 2 12 ABXA030475 120031213A3231 ARM DOUG DC8 DC863F 302198FWP MLG DOOR WORN A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23811AX 46113 RED GEAR UNSAFE LIGHT CAME ON AFTER GEAR RETRACTION WITH RT GEAR DOOR LIGHT ON FLIGHT ENGINEER'S PANEL. RECYCLED GEAR, ALL INDICATIONS NORMAL. MAINTENANCE FOUND DOOR ROLLER OUT OF ADJUSTMENT AND AFT ARM WORN. REPLACED ARM, ADJUSTED MAIN GEAR DOOR UPLATCH MECHANISM IAW MM 32-31-04-4. PERFORMED ADJUSTMENT TEST IAW MM 32-31-04-5. 2L74 4F 4A25 20040212001272004021200127EU 2004 2 12 009521 120031216A2611 WARNING LIGHT SAAB SF340 SF340A 7850100EU CARGO SMOKE ILLUMINATED A UHLAFBA ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL17340C 340C FLT 4555 FWA TO PIT HAD A CARGO SMOKE INDICATION, CREW ACTIVATED CARGO FIRE SUPPRESSION SYSTEM AND BLEW BOTTLE, DECLARED EMERGENCY AND DIVERTED TO CAK. NO INCIDENT. 2L72 4T RTA52EU 20040212001352004021200135NM 2004 2 12 PCAA0312150 120031215A323311300107 ACTUATOR DHAV DHC8 DHC8102 2809003NM MLG FAULTY A PCAAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 EA13834EX19885 285 FLIGHT NR 3897 DEPARTING ISLIP HAD TO RETURN TO FIELD WHEN DURING INITIAL CLIMB FOLLOWING GEAR RETRACTION, IT WAS NOTICED THAT THE RT MAIN GEAR UNSAFE LIGHT WAS ILLUMINATED AND A GRINDING NOISE WAS PRESENT. GEAR WAS SELECTED DOWN AND THREE GREENS WERE OBTAINED. ALL HYDRAULIC INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO FIELD. NO EMERGENCY DECLARED. MAINTENANCE FOUND THE UPLOCK ACTUATOR ON THE RT SIDE AT FAULT AND REMOVED AND REPLACED SAME. OPERATIONAL CHECKS AND LEAK CHECKS ALL GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040212001412004021200141NM 2004 2 12 DHL2003742521 120031124A5710 DOUBLER BOEING727 727225 1384077NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, RT WING L/E STA 130 INT FRAME DOUBLER TO UPPER SURF IS CRACKED ABOVE FASTENER. REMOVED DAMAGED AREA IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM MAT ID 7075 T6 .050 PO 90096 DIM 10 X 1.75 INCH IAW B-727 SRM 51-40-4 FIG 1. TREATED PRIMED IAW B-727 SRM 51-10-2. INSTALLED NEW DOUBLER ON RT WING L/E STA 130 INT FRAME UPPER SURFACE IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040212001432004021200143CE 2004 2 12 ENHA20032002B 120031217A54121019100383 BULKHEAD BEECH 200 200BEECH 1152920CE RT NACELLE CRACKED E ENHAK NONE O OTHER ININSP/MAINT 1 AL0390PB 12272 BB125 RT NACELLE WAS WEARING AND CRACKING WITH RT AFT LOWER COWL. REPLACED BULKHEAD 1L72 4T A24CE 20031002001482003100200148NM 2003 10 2 03FDEA01469 120030909A531065198616 STRUCTURE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CORROSION ON STRUCTURE IN NLG BAY AT BS 284 RBL 18 INSIDE TORQUE BOX O/B OF STRUT DOOR FWD HINGE. REMOVED AND REPLACED PER SRM 51-30-2. 2L73 4F RTA3WE 20031002001632003100200163 2003 10 2 SWIA200312383 420030908A2210 SWITCH EMB 120 EMB120ER 3260203SO AUTOPILOT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07234SW 120308 FO AUTOPILOT WILL NOT ENGAGE.REPLACED FO AP DISCONNECT SWITCH. SYSTEM OPS CHECK GOOD IAW 22-10-00. 2L72 4T RTA31SO 20031003000172003100300017NM 2003 10 3 AALA20030913 120030824A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21357AA 24038 FOUND EXTERNAL EMERGENCY EXIT LIGHTS LEFT OVERWING, ALL THREE ARE INOPERATIVE. ALSO, 1L EXT EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED M736 AND OPS CHECKED OK. (M) 2L72 4F RTA1NM 20031003000252003100300025NM 2003 10 3 AALA20030778 120030716A3350 BALLAST BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21632AA 24590 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDEWALL LIGHT ABOVE RIGHT AFT EMERGENCY EXIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BALLAST AT SEAT 17ABC SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000272003100300027NM 2003 10 3 AALA20030474 120030419A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21609AA 27447 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 17 INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT ASSEMBLY AT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000572003100300057SO 2003 10 3 C2XA03TY161 120030911A531514521721009 FLOORBEAM EMB 135 EMB135ER 3260203SO GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE RT HAND FORWARD DIGITAL UNDER THE GALLEY WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04,05AND 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031003000722003100300072NM 2003 10 3 03FDEA01533 120030901A5753ARC0502506 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RTWING OUTBOARD FLAP INBOARD HINGE (A/C SIDE) INBD ACTUATOR ATTACH BORE FOUND CORRODED. 2L73 4F RTA22WE 20031003000752003100300075NM 2003 10 3 03FDEA01530 120030830A5753ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) LOWER INBOARD ATTACHMENT BORE FOUND CORRODED. 2L73 4F RTA22WE 20031006000652003100600065CE 2003 10 6 AMWA39 120030907A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127ZV UE127 RIB 69.184 CS CRACKED AT STRG P/N 101-640000-45 (1EA CRACK ON THIS RIB) LT SIDE. 2L72 4T RTA24CE 20031006000682003100600068CE 2003 10 6 AMWA42 120030902A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07176YV UE176 RIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 FIRST STRG FWD OF AFT SPAR RT SIDE OF VERTICAL STABILIZER. 2L72 4T RTA24CE 20031006000742003100600074CE 2003 10 6 AMWA48 120030904A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07166YV UE166 6 CRACKS FOUND ON THIS RIB LOCATED AT END RIVET OF RIB AREA THAT IS JOGGLED OVER STRG. STRG INTERSECTION LH P/N 101-640000-37, LT 101-640000-39, LH P/N101-640000-45 THEN RH P/N 101-640000-38, RH P/N 101-640000-46, RH P/N 101-640000-42. 2L72 4T RTA24CE 20031006000762003100600076CE 2003 10 6 AMWA49 120030903A5320114430002180 ANGLE BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07132YV UE132 DURING AN ABCD STRUCTURAL INSPECTION, THE RT FUSELAGE CLOSING ANGLE WAS FOUND CRACKED 2.4 INCHES. THE CRACK WAS REPAIRED IN ACCORDANCE TO THE BEECH SRM 53-90-23 AND RAYTHEON AIRCRAFT COMPANY FIELD REPAIR FR-CO-00934 2L72 4T RTA24CE 20031006000812003100600081CE 2003 10 6 AMWA54 120030903A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07167YV UE167 WHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLNAGE AT CANTED STAB. STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE LT SIDE AT THE CENTER STRG,. REPAIRED CRACK TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-91, 51-70-03 2L72 4T RTA24CE 20031006001142003100600114NM 2003 10 6 HOC2003F00018 120030826A5313 STRINGER BOEING727 727224 1384076NM FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0779749 22451 DURING A (C) CHECK, CORROSION WAS NOTED ON STRINGER 22R AT STATION 1166-1183. 2L73 4F A3WE 20031006001182003100600118NM 2003 10 6 HNAA0300050 120030915A5270 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM PAX DOOR ILLUMINATED A HNAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA07908HA 015 PAX DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. DIVERTED INTO CAE. VERIFICATION OF NORMAL OPERATION OF PASSENGER ENTRY DOOR IAW MEL 52-2. CLT MAINTENANCE CERIFIED NORMAL OPERATION CHECK GOOD. 2H72 4T RTA13NM 20030905002352003090500235WP 2003 9 5 DHL2003873610 120030704A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING FUEL TANK I/B EXTENDED L/E OUTER PLATING CORRODED BTW STA XFS 207 AND XFS189 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN SEGMENT. PERFORMED NDT INSPECITION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER AND A FILLER IAW EODHL-030614, ED-3353. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER ON LT WING FUEL TANK EXTENDED L/E OUTER PLATING ( STA XFS 207 - 189) USING NEW FASTENRES IAW EODHL-030614, ED-3353, SRM 51-1-21 PG 1. SEE N/R 2088 FOR FUEL LEAK CK. 2L74 4F RT4A25 20030908001902003090800190SO 2003 9 8 SWIA200312267 120030815A243523080013 STARTER GEN EMB 120 EMB120ER 3260203SO APU MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07196SW6030 333 120151 APU GEN WENT OFF LINE ON TAXI, SMELT SMOKE THROUGHOUT CABIN. REMOVED AND REPLACED APU STARTER/GEN. OPS CHECK GOOD IAW 24-35-00. 2L72 4T RTA31SO 20030908001942003090800194EA 2003 9 8 SWIA200312271 120030817A2752865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07411SW 7067 FLAPS HALF SPEED MESSAGE. REPLACED FLAP PDU WITH SERVICEABLE UNIT IAW MM 27-52-01. OPS CHECK GOOD. S/N OFF: 161. 2L72 4F RTA21EA 20030908002992003090800299NM 2003 9 8 SWAA031917 120030826A53116546549 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 767, STR 13R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030908003172003090800317NM 2003 9 8 SWAA031895 120030823A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 18. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20030909000262003090900026EA 2003 9 9 SWIA200312337 120030823A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913SW 7597 FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. ANGLE REPAIR CARRIED OUT IAW CRJ REO 601R-53-61-117 AND RII 53-401. P/N: 601R-53-61-117-3 2L72 4F RTA21EA 20030909000342003090900034SO 2003 9 9 C2XA03BT090 120030906A3350110049 BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712567 145623 EWR---CO 2342, DURING PREFLIGHT CREW REPORTED THAE THE EMERGENCY PATH LIGHTING FORWARD STRIP STRIP WAS INOPERATIVE, MAINTENANACE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD. IAW EMB145AMM 33-50-04. 2L72 4T RTT00011AT 20030909000352003090900035SO 2003 9 9 C2XA03IA088 120030901A3230355022002MOD3 CONTROL UNIT EMB 145 EMB145XR SO COCKPIT MALFUNCTIONED A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2726141 145733 IAH- ON CLIMB THE CREW NOTED THAT THE LANDING GEAR AURAL WARNING ACTIVATED WHEN THE GEAR RETRACTED. THE CREW DID AN AIR RETURN TO IAH, AND, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, AND, THE AIRCRAFT WAS APROVED FOR RETURN TO SERVICE. 2L72 4F RT 20030909000372003090900037SO 2003 9 9 C2XA03CL160 120030904A3350375921 SIGN EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2714937 145026 CLE FLIGHT NR 2015. THE CREW REPORTED THAT THE FORWARD MID CABIN CEILING OVER WING EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD MID CABIN OVER WING EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030909000382003090900038SO 2003 9 9 C2XA03TY146 120030906A5330 SKIN EMB 145 EMB145 3260210SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS AIRCRAFT FERRIED FROM BNA, A LARGE DENT WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF THE SERVICE DOOR WITH A DEEP SCRATCH, MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A DOUBLER AND FILLER, ALLIDINED, INSTALLED PATCH, PRIMED AND PAINTED I/A/W-EMB-135/145-SRM-51-60-02, 53-21-01 AND CMP-51-21-06, PRESSURIZED GOOD I/A/W-EMB-145-AMM-21-31-00 2L72 4F RTT00011AT 20030909000392003090900039SO 2003 9 9 C2XA03IA091 120030813A33501317 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714516 145323 IAH-DURING PREFLIGHT THE CREW NOTED THAT THE ROW 9 OVERHEAD EMERGENCY LIGHTS FAILED TO ILLUMINATE ABOVE SEATS 9A, AND, 9B. IAH- MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS IN THE EXIT LIGHT, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030909000552003090900055NM 2003 9 9 VNAA0308022 120030829A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DISCHARGED A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07460PS3461 3061 THE CREW REPORTED THAT THE FIRST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030909000622003090900062NM 2003 9 9 VNAA0308021 120030828A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN INOPERATIVE A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07437JS 3055 THE CREW REPORTED THAT THE LAST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030909001002003090900100 2003 9 9 53566 420030815A61228210410 GOVERNOR BEECH 1900 1900D 1154162CE LT ENGINE FAILED A AMWAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 CE07144ZV3136 3136 UE144 AFTER TAKEOFF ON FLIGHT 5549 FROM PITTSBURGH PENSYLVANIA, THE LEFT PROP RPM ONLY SHOWED 1500 RPMS. THE CREW RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROP GOVERNOR. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20030909001252003090900125CE 2003 9 9 S2YA03010 120030310A284211838900447 PROBE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT WING FAULTY A S2YAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL1379SK 1474 UE79 DURING TAKEOFF ROLL OF FLIGHT 1050, THE CREW NOTICED A FUEL QUANTITY ANNUCIATOR ILLUMINATED. THE CREW RETURNED TO GATE AND MEL-ED THE SYSTEM. ON 3/14/03 MECHANIC CLEARED THE MEL BY REPLACING A FUEL PROBE. MECHANIC RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DISCREPANCIES. 2L72 4T3 TRTA24CE E2NE 20040212001442004021200144NM 2004 2 12 200300287 120031217A335020131A BATTERY PACK BOEING737 737 UTILSYSNM EMERGENCY LIGHT DISCHARGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07363CE 27456 L1 AND R1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. 2L72 4F RTA16WE 20040212001702004021200170NM 2004 2 12 2003UALA00973 120031218A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STA 400 STRINGER 16 R HAS CRACKED SHEAR TIE. ALSO STA 420 STR 9L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040212001722004021200172NM 2004 2 12 2003UALA00975 120031218A5320 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 FWD CARGO LOWER AFT WEB CRACKED PIECE MISSING. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB PIECE. 2L72 4F4 FRTA16WE E2GL 20040329000162004032900016WP 2004 3 29 ASAA0380391 120030421A5753 SKIN DOUG DC9 DC982 3022082WP TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT OUTBOARD FLAP TRAILING EDGE CREASED. REPAIRED FLAP TRAILING EDGE PER SRM. (M) 2L72 4F A6WE 20040329000172004032900017WP 2004 3 29 ASAA0380394 120030421A532199517883 FLOORBOARD DOUG DC9 DC982 3022082WP FUSLEAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURNG 30K CHECK, FOUND FLOORBOARD STATION 811 RBL 22-43 LOWER SKIN CORNER GOUGED. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040329000462004032900046NM 2004 3 29 ASAA0340321 120030725A53206545855538 ANGLE BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND CHINE ANGLE AT STATION 947 TO 992 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040401000232004040100023WP 2004 4 1 ASAA0380273 120030322A335001056603 LIGHT DOUG DC9 DC983 3022083WP ROW 6 INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01958AS 53024 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE FORWARD OF ROW 6. REPLACED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040401000302004040100030WP 2004 4 1 ASAA0380397 120030421A5420593803829 STIFFENER DOUG DC9 DC982 3022082WP NR 1 NACELLE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND NR 1 ENGINE NOSE COWL TWO STIFFENERS CRACKED AFT SIDE OF FORWARD BULKHEAD AT 6 O'CLOCK POSITION. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040401000442004040100044NM 2004 4 1 AALA20031159 120031020A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21623AA 24581 BOS - MAINTENANCE OBSERVED SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE FROM ROWS 16 TO 23. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401001402004040100140EU 2004 4 1 TRB2004F00000 120031206A3220D226981722 SHOCK ABSORBER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW124B NE NLG CRACKED A TRBAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO21270AT16910 270 DURING PARKING, THE AIRCRAFT A LOUD NOISE CAME FROM THE NOSE GEAR. INSPECTION REVEALED THAT THE NOSE GEAR AXLE WAS CRACKED. REMOVED AND REPLACED NOSE LANDING GEAR SHOCK ABSORBER. 2H72 4T4 TRTA53EU E2ONE 20040407000372004040700037NM 2004 4 7 TSAA0357216 120031117A57306545403 PANEL BOEING737 737230 1384401NM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 BLENDED OUT THE CORROSION TO A 20:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. REMOVED FASTENERS IN REPAIR AREA. FLAT PEEN BLENDOUT AREA. ALODINED AND TWO COATS BMS 10-20 TYPE II PRIMER TO BLEND AND SPOT FACE AREAS. INSTALLED 1/32 INCH OVERSIZE PROTRUDING TENSION HEAD HI-LOCKS WET WITH BMS 5026 TYPE II IN COLD WORKED TRANSITION FIT HOLES. REPAIR COMPLETED IAW ECO 3397. AIRCRAFT RETURNED TO SERVICE. CENTER FUEL TANK LOWER PANEL P/N 6545403, BS 638.60 AT STRINGER 4C WAS REPAIRED.(M) 2L72 4F RTA16WE 20031112000292003111200029NM 2003 11 12 03FDEA01722 120031008A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING OB FLAP OB HINGE FITTING (FLAP SIDE) IB ACTUATOR ATTACHMENT LUG HOLE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - I/B ACTUATOR ATTACHMENT LUG HOLE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - I/B ACTUATOR ATTACHMENT LUG HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 LT AND RT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031112000662003111200066NM 2003 11 12 CALA0300629 120031108A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A 0.55 INCH CRACK IN STRINGER 16R AT BS 504. REPAIRED IAW ECRA 5310-03262. 2L72 4F RTA16WE 20031112000992003111200099EU 2003 11 12 BAQA090604 120031028A77141179405603 INDICATOR BOLKMS117 BK117B1 5626012EU N1 FLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME6453 7235 N1 INDICATOR FLUCTUATES. REPLACED WITH SERVICEABLE ASSET. 1G72 3U H13EU 20031112001022003111200102EU 2003 11 12 AWXA200301381 120031109A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28627AW378254626 66 PHX - EEL - DURING INSPECTION THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) FAILED SELF TEST (INTERNAL LOAD FAULT). MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031006001282003100600128 2003 10 6 SWAA032022 420030911A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20031006001532003100600153 2003 10 6 SWAA032019 420030910A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2L72 4F A16WE 20031006001582003100600158 2003 10 6 SWAA031961 420030903A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20031006001622003100600162NM 2003 10 6 SWAA031965 120030901A335020131A BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20031006001632003100600163 2003 10 6 SWAA031966 420030904A2565D31354 SLIDE BOEING737 7375H4 138449DNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031006001642003100600164NM 2003 10 6 SWAA031967 120030831A335065C2709 LIGHT BOEING737 7377H4 1384404NM PAX DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29711HK 27845 DURING SCHEDULED A CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20031006001702003100600170NM 2003 10 6 SWAA031973 120030903A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B + 4, STR 14L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031006001722003100600172WP 2003 10 6 03FDEA01655 120030929A5312 CAP DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25308FE 48297 COMPLY WITH EA 8-5710-72305. WINGS-MAIN FRAME-GOUGE REPAIR XORS 562.390 (LT) FLAP BULKHEAD LWR CAP. CLOSING ACTION ON 09/26/03. ON N/R S00015. COMPLIED WITH EA 8-5710-72305.WINGS, MAIN FRAME, GOUGE REPAIR STA XORS 562.390. 2L73 4F4 F A22WE E23EA 20031006001742003100600174NM 2003 10 6 03FDEA01650 120030926A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION / GOUGE ON FLOORBEAM BS 277, LBL 14 - LBL 10, WL 208. REPAIRED FLOORBEAM BS 277, LBL 10-14 PER EA 7-5310-54991. 2L73 4F RTA3WE 20031003000462003100300046NM 2003 10 3 AWXA200301050 120030820A339714803180 CONNECTOR BOEING737 737277 1384570NM EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK NUMEROUS CONNECTORS AND SPLICES WERE FOUND DAMAGED ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS LT SIDE OF AIRCRAFT. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS LT SIDE OF AIRCRAFT IAW SWPM 20-42-01, PG. 1-4, AND 20-30-12, STEP 1-8. OPERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33006. PART NAME; SPLICE, MFG; BOEING, P/N; D436-36 & -37. 2L72 4F RTA16WE 20031003000822003100300082NM 2003 10 3 03FDEA01522 120030912A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON FLOORBEAM BS 328 LBL 18 TO LBL 30 WL 208. 2L73 4F RTA3WE 20031003000852003100300085SO 2003 10 3 RAIA00309238 120030911A32501170A180001 POTENTIOMETER EMB 145 EMB145 3260210SO NLG STEERING INTERMITTENT A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03802HK114032827 145066 AIRCRAFT WILL NOT STEER PROPERLY. MAINTENANCE REMOVED AND REPLACED NWS FEED BACK POT. 2L72 4F RTT00011AT 20031006000292003100600029 2003 10 6 AWXA200301055 420030910A2213 CONTROL PANEL BOEING737 7373S3 1384711NM AUTOPILOT FAILED A AWXAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 WP28312AW 24060 DURING CRUISE EN ROUTE FROM PHX TO MSY AT 33000 FT AUTOPILOT DISCONNECTED DUE TO MODE CONTROL PANEL (MCP) FAILURE, FLIGHT DIRECTORS AND AUTOPILOT INOPERATIVE. ONLY WINDOW WORKING ON MCP WAS THE FIRST OFFICERS COARSE SELECTOR, FLIGHT INSTRUMENTS AND RADIO MAGNETIC INDICATOR WORKING FINE. DECLARED EMERGENCY AS PRECAUTION, AND ABANDONED APPROACH INTO MSY DUE TO WIND SHEAR, DIVERTED TO IAH. MAINTENANCE INSPECTED THE MCP AND CHECKED CONNECTIONS IAW BMM 22-11-34, PANEL FULLY OPERATIVE, COULD NOT DUPLICATE. 2L72 4F RTA16WE 20031006000632003100600063CE 2003 10 6 AMWA37 120030907A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-45 STRG P/N 101-640000-39 (2EA CRACKS ON THIS RIB) 2L72 4T RTA24CE 20031006001362003100600136NM 2003 10 6 SWAA032030 120030909A5753654643489 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND LT INBOARD AFT T/E FLAP DELAMINATED AT LOWER INBD CORNER. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20031006001832003100600183NM 2003 10 6 03FDEA01642 120030926A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 EXTERNAL FUSELAGE SKIN CRACKED BS 685 JUST BELOW STR 26 RT. EXTERNAL FUSELAGE SKIN DAMAGE B.S. 685 BELOW STR 26 RT REPAIRED PER EA 7-5330- 70519. 2L73 4F RTA3WE 20031007000192003100700019NM 2003 10 7 AALA20030729 120030613A5320 PLATE BOEING767 767223 1385123NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21329AA 22329 DURING INSPECTION OF THE H11 BOLTS THROUGH THE SPLICE PLATE PER BOEING S/B 767-57A0064, 'C' HOLE WAS FOUND TO BE CORRODED. REQUIRED OVERSIZING. THE HOLE WAS COMMON TO THE HORIZ FLANTES OF THE OUTBOARD WING SPAR CHORD. REAMED CORRODED 'C' HOLE TO 0.781 INCH DIAMETER. INSTALLED A 2ND OVERSIZE. (M) 2L72 4F RTA1NM 20031007000552003100700055NM 2003 10 7 03FDEA01670 120031001A5320651627910 FLOOR SUPPORT BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON LONGITUDINAL BEAM AT STA 760 TO 850 LBL 29 WL 208. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208, AND INSTALLED NEW LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208. ALL WORK DONE PER SRM 51-30-2 2L73 4F4 FRTA3WE E2EA 20031007000622003100700062NM 2003 10 7 SWAA031976 120030904A532065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 440 AT STR 7R, BS 500C AT STR 3R, BS 500C AT STR 2R AND BS 520 AT STR 16C. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20031007000632003100700063NM 2003 10 7 SWAA031977 120030904A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 727D + 10 AND BS 887 + 4, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031007000682003100700068NM 2003 10 7 SWAA031982 120030904A32301N3311B DIODE BOEING737 7372H4 138448CNM P6 PANEL FAULTY A SWAAB EMER. DESCENT P NO WARNING INDICATION APAPPROACH 1 SW29086SW 22827 DECLARED EMERGENCY, LANDING GEAR WOULD NOT ILLUMINATED DOWN AND LOCKED WITH GEAR LEVER IN DOWN POSITION, RECYCLED GEAR NO CHANGE. REMOVED AND REPLACED M208 DIODE AND ADJUSTED GEAR EXTENSION CABLE PER MM. 2L72 4F A16WE 20031007000732003100700073NM 2003 10 7 SWAA031947 120030828A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031007000992003100700099NM 2003 10 7 SWAA031997 120030907A53126545409 BULKHEAD BOEING737 7373H4 1384600NM LT MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD BEADED WEB CRACKED AT BS 664, LBL 31. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20031007001002003100700100NM 2003 10 7 SWAA031998 120030905A53206554698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 25L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031007001072003100700107 2003 10 7 SWAA032005 420030904A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20031008000022003100800002NM 2003 10 8 03252406 120030909A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27406FJ 3156 DURING MAINTENANCE INSPECTION THE THIRD SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031008000062003100800006EA 2003 10 8 03251648 120030908A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27648BR 7406 DURING MAINTENANCE INSPECTION THE LT HAND EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031003000192003100300019WP 2003 10 3 AALA20030904 120030826A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21585AA 53248 AFT LEFT SERVICE DOOR INTERIOR EMERGENCY EXIT SIGN LIGHT FORWARD OF THE DOOR IS INOPERATIVE. REPLACED BATTERY PACK AB5 4 IN LEFT GALLEY CEILING NEAR LEFT SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031003000212003100300021NM 2003 10 3 AALA20030834 120030804A2913S270T2017 PUMP BOEING757 757223 1384957NM HYD SYSTEM LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21650AA 24608 EN ROUTE DIVERTED TO ORD DUE TO CENTER SYSETM HYD QUANTITY LOSS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 CENTER SYSTEM ELECTRIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000242003100300024NM 2003 10 3 AALA20030921 120030830A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHTSLOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21391AA 27451 FOUND EMERGENCY LIGHTS INOPERATIVE AT SEAT 24B. RECONNECTED CONNECTOR AT SEAT 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031112001172003111200117WP 2003 11 12 ABXA030429 120031027A523059101419 PAN DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 FORWARD LOWER CARGO DOOR OUTER PAN HAD CRACK INDICATION AROUND HI-LOK AT AFT LOWER STOP. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM. 2L72 4F A6WE 20031112001232003111200123CE 2003 11 12 BAQA089501 120031004A27501005240741 GEARBOX BEECH 100 100BEECH 1152916CE PWA PT6 PT6A27 52043EA FLAP DRIVE MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 2 B144 GEARBOX BINDING. REPLACED WITH SERVICEABLE UNIT. 1L72 3T4 T A14CE E4EA 20031113000282003111300028 2003 11 13 BAQA090581 420031006A3452066011410101 TRANSPONDER UROCOPEC135 EC135P1 8680990EU ATC SYSTEM INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH556 0179 SQUAKS 1200 INTERMITTENT. NO INPUT. THIS IS THE ORIGINAL UNIT INSTALLED ON 0179/137MH (NEW AIRCRAFT). PART HAS LASTED ONLY 555.9 HOURS. DID NOT RECEIVE AIRCRAFT UNTIL 3/18/03. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20031113000302003111300030NE 2003 11 13 BAQA090586 220031022A7321430121106 FUEL CONTROL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ENGINE MALFUNCTIONED B BAQAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 EA03911BK684 7099 ENGINE FLAME-OUT DURING OVERSPEED CHECKS. REPLACED WITH SERVICEABLE UNIT. 11/3/03 1G72 3U3 U H13EU E5NE 20030909002802003090900280EA 2003 9 9 QXEA200300949 120030802A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX 10045 SFO- ON FLIGHT 2434 FIRE SYSTEM FAULT STATUS MESSAGE DISPLAYED. CLEARED FAULT IAW SIM 26-10-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030910000102003091000010WP 2003 9 10 DHL2003604565 120030507A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING INBD FLAP UPPER PLATING HAS INTERIM REPAIR FROM XW 104.000 TO XW 115.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PLATING IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING IAW SRM 51-1-8B. INSTALLED NEW PLATING WITH NEW FASTENERS IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000122003091000012WP 2003 9 10 DHL2003604564 120030603A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL CRACKED 1.000, L-27R STA 70.000. REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-20-D PG 21, SRM 51-1-21 PG 1. FABRICATED NEW INTERCOSTAL IAW SR5M 53-2-0 PG 1, 2. CLEANED, TREATED AND PRIMED AREA AND NEW INTERCOSTAL IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000342003091000034NE 2003 9 10 HEEA088214 120030706A261261423473205 FIRE DETECTOR SKRSKYS76 S76A 8143006NE LEFT MALFUNCTIONED E HEEAO OTHER N FALSE WARNING CRCRUISE 1 SW03278X 760440 IN CRUISE FLIGHT THE NR 1 ENGINE FIRE LIGHT ILLUMINATED AND THE FIRE HORN SOUNDED. NO OTHER INDICATIONS NOTED. REPLACED LT FLAME DETECTOR. 1G72 3U H1NE 20030910000442003091000044WP 2003 9 10 ABXA030324 120030721A52303926046503 STOP FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 UPPER AFT DOOR STOP FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20030910000482003091000048WP 2003 9 10 DHL2003604757 120030709A5713 STRINGER DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING NR 1 ALT TANK, S-59 CRACKED 1.500 (LOWER), NEAR XRS 463.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-2 FIG 3D, 3E, 3F. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED SPLICES (02 EA), CLIPS (02) AND SPACERS (04 EA) IAW SRM 57-2-2 FIG 3D, 3E, 3F. APPLIED TANK COATING MATERIAL TO AREA AND SPLICES AND CLIPS SPACERS IAW SRM 51-1-12 PG 12. INSTALLED SPLICES, CLIPS, SPACERS WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. FOR LEAK CHECK SEE NR 3824. 2L74 4F RT4A25 20030910000662003091000066NM 2003 9 10 DHL2003747010 120030827A3350 LIGHT BOEING727 727224 1384076NM CABIN MALFUNCTIONED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01747DH 22253 EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR ILLUMINATED. EMERGENCY EXIT LIGHT NOT ILLUMINATED PER 33-50-01 PAGE 7. THE 2-28V BULBS ILLUMINATED WITH NO SMOKING SWITCH IN ON POSITION. TURNED SWITCH OFF LIGHTS EXTINGUISHED. 2L73 4F A3WE 20030910000722003091000072WP 2003 9 10 DHL2003604787 120030625A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FUSELAGE EXTERIOR SKIN SHOWS DENTS (03 EA), FS 255.000, L-24L TO L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030516, ED-3357. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. BLENDED OUT DENTS IAW EODHL-030516, ED-3357. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICTED INTERNAL DOUBLER IAW EODHL-030516, ED-3357. CLEANED, TREATED AND PRIMED REPAIR AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED INTERNAL DOUBLER WITH NEW FASTENERS IAW EODHL-030516, ED-33547, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000802003091000080WP 2003 9 10 DHL2003604735 120030527A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT ACCY COMPT FLOORBEAM CORRODED, STA 1640.000, LBL-5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1G, TR 53-124. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND STRAP AND REPAIR ANGLE IAW SRM 53-2-0 FIG 16, TR 53-124. INSTALLED FILLER AND STRAP AND REPAIR ANGLE IAW SRM 53-2-0 FIG 1G, SRM 51-1-20D. 2L74 4F RT4A25 20031027000632003102700063NM 2003 10 27 UPS03441265 120030903A541165B9031077 FRAME BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, NR 1 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD FRAME WEB. DETAILS PLS REFER ATTACHED FIGURE. FRAME WEBS REPLACED AND REPAIRED AS IAW RS NR R-54-53-35064 INSPECTIONS TO CONTINUE PER UPS EO B747-5410-13908 ( UPS ENGINEERING FILE NR 747-54 -20040) RAISED. 2L74 4F4 F A20WE E20EA 20031027000732003102700073EU 2003 10 27 MALA030429 120030918A5347 SEAT TRACK SAAB SF340 340B 7860101EU GE CT7TP CT79C 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 DURING 4K-CHECK IN CWA, LT FORWARD SEAT TRACK LBL 18.3 WEB HAS CORROSION. MAINTENANCE COMPLETED REPAIR IAW EO S53077 FROM STA 299-311.75. A/C RELEASE DATE 9/25/03. 2L72 4T4 TRTA52EU E8NE 20030909001262003090900126NM 2003 9 9 S2YA03013 120030404A2760 SPOILER DORNERDO32 DO328300 NM LT WING MALFUNCTIONED A S2YAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 GL13355SK 3124 DURING TAKEOFF OF FLIGHT 2183, AFTER CREW POWERED UP THE GROUND SPOILERS DEPLOYED. THE TAKEOFF WAS ABORTED. THE CREW CONSULTED WITH MECHANIC AND PERFORMED THE GROUND SPOILERS DEPLOYING AGAIN, THE CREW ABORTED THE TAKEOFF AGAIN. MECHANIC INSPECTED THE SYSTEM AND FOUND THE LEFT I/B SPOILER. 2H72 4T RTA55NM 20030908001772003090800177EA 2003 9 8 SWIA200312250 120030810A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07437SW5074 5074 7564 STAB CH 1 INOP STATUS MESSAGE OCCURRED; WAS RESETTABLE, BUT REOCCURRED. STAB TRIM CAUTION AND MACH TRIM CAUTION ALSO OCCURRED AFTER RESETTING CHANNEL 1; ALSO RESETTABLE.REMOVED AND REPLACED HSTA AND MCU IAW CRJ MM 27-42-01. OPS CHECK GOOD. P/N: 7062-3 S/N OFF: 736 S/N ON: 1004 2L72 4F RTA21EA 20030908002312003090800231SO 2003 9 8 SWIA200312297 120030822A3097 WIRE EMB 120 EMB120ER 3260203SO PROP DE-ICE SYS LOOSE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07296SW 120325 LEFT PROP HEAT FAILED IN CRUISE WITH SUBSEQUENT SMELL OF ELECTRONICS FAILURE ALTERNATED BETWEEN LEFT 'PROP HEAT' AND 'MONITOR' WITH SMELL BECOMING STRONGER. PROP HEAT WAS TURNED OFF AND CONTINUES FOR APPROX 30 SECONDS TO INDICATE INOP. INSPECTED LEFT PROP DEICE SYSTEM. FOUND LOOSE WIRES ON RELAYS K0063 AND K0065. TIGHTENED WIRES AS NEEDED. OPERATED PROP DEICE SYTEM FOR 20 MINUTES. NO DEFECTS NOTED. OPS CHECK OK AT THIS TIME. 2L72 4T RTA31SO 20030908003002003090800300NM 2003 9 8 SWAA031918 120030827A57146545410 BEAM BOEING737 7373Q8 1384670NM CENTER WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL BEAM CRACKED, BS 663, BL 0. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20030908003232003090800323NM 2003 9 8 SWAA031901 120030825A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29726SW 27858 DURING SCHEDULED A CHECK, FOUND EEPLS INOP AT ROW NR 20 THROUGH ROW NR 25. REPAIRED EEPLS PER MM. 2L72 4F RTA16WE 20030909000272003090900027EA 2003 9 9 SWIA200312338 120030823A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913SW 7597 FS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK. ANGLE REPAIR CARRIED OUT IAW CRJ REO 601R-53-61-117. P/N: 601R53-61-117-2 2L72 4F RTA21EA 20030909000292003090900029EA 2003 9 9 SWIA200312323 120030808A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 FS 484 LT INTERCOSTAL I/B & O/B FLANGES LBL 27 + LBL 36 CRACKED. DISCOVERED DURING C-CHECK. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. ''A''. P/N: S6144-14 2L72 4F RTA21EA 20030909000542003090900054NM 2003 9 9 VNAA0308025 120030830A3397 WIRE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN BROKEN A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07427JS 3039 THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REAIRED A BROKEN WIRE IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030909000732003090900073NE 2003 9 9 SWIA200312298 220030821A7320 CONTROL ARM EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT ENGINE LOOSE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07393SW 120330 LEFT ENGINE DID NOT SHUTDOWN IN FUEL CUT OFF (1ST ATTEMPT). FOUND FUEL CUTOFF SERRATED ARM ON THE HMU TO PCU LOOSE. RETORQUED, SAFETIED AND RAN LT AND RT ENGINES. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030909000862003090900086CE 2003 9 9 53866 120030826A32301143640681 PRINTED CKT BOAR BEECH 1900 1900D 1154162CE LANDING GEAR FAULTY A AMWAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CE07176YV1822418224 UE176 UPON APPROACH TO VPS LANDING GEAR WOULD NOT EXTEND. A SECOND ATTEMP WAS MADE WITH THE SAME THING NO DOWN AND LOCKED INDICATION FLY BY OF TOWER AT VPS. CONFIRMED GEAR WAS NOT DOWN. GEAR WAS THEN PUMPED DOWN AND LOCKED CONFIRMED BY GEAR DOWN AND LOCK INDICATION AIRCRAFT. THEN OVER FLEW VPS TO PFN AND LANDED SAFELY AT THE MAINT BASE. MAINT REPLACED GEAR PRINTED CIRCUIT BOARD. OPS CHECK NORMAL. 2L72 4T RTA24CE 20030909000922003090900092 2003 9 9 SWIA200312314 420030822A221212049625001 CONTROLLER EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07295SW 120322 AFTER AUTOPILOT IS ENGAGED, ALL PARTS OF AUTOPILOT SYSTEM WORK PROPERLY EXCEPT THE AUTOPILOT WILL NOT CHANGE THE PITCH OF THE AIRPLANE. REPLACED TRANSFER BOX IAW 22-10-1. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20030909001122003090900112CE 2003 9 9 53080 120030730A2750 FLAP BEECH 1900 1900D 1154162CE WINGS MALFUNCTIONED A AMWAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE07165YV UE165 AFTER TAKEOFF FROM PANAMA CITY FLORIDA ON FLIGHT 5445, THE FLAPS WERE SELECTED UP, STAY AT 17 DEGREES. THE CREW DECIDED TO RETURN TO PANAMA CITY FLORIDA WITH NO FURTHER INCIDENT. THE FLAPS WERE RETRACTED TO ZERO AND MEL'D. THE AIRCRAFT WAS RETURNED TO SERVICE. STILL AWAITING MORE INFORMATION. 2L72 4T RTA24CE 20030909001282003090900128 2003 9 9 SWIA200312346 420030831A22156225734002 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07295SW2800 2800 120322 ENGAGING EITHER YAW DAMPER CAUSES UNCOMMANDED RUDDER DEFLECTION. REMOVED AND REPLACED RUDDER SERVO MOTOR WITH NEW SERVO MOTOR IAW 22-10-09. OPS CHECK GOOD AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 20030909001292003090900129SO 2003 9 9 SWIA200312347 120030831A5753 FLAP TRACK EMB 120 EMB120ER 3260203SO T/E FLAP LACK OF LUBE A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07295SW 120322 FLAP DISAGREEMENT ON CLIMBOUT FROM GEG. FLAPS STUCK BETWEEN 0-15 DEGREES. FLAPS CAME DOWN TO 25 DEGREES OK, BUT WOULD NOT GO UP UNTIL ON THE GROUND. CLEANED AND LUBED TRACKS AND ROLLERS, CYCLED FLAPS SEVERAL TIMES. NO FAULTS NOTED, FLAPS OPS CHECK NORMAL. 2L72 4T RTA31SO 20030909001302003090900130WP 2003 9 9 ARWA20030705 120030710A32312714425 SPRING DOUG DC8 DC863F 302198FWP RT MLG DOOR BROKEN A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19784AL 46135 LOG PAGE 102010. AFTER TAKEOFF, DOORS NOT LATCHED LIGHT ILLUMINATED. FOUND BROKEN SPRING AT RT MAIN LANDING GEAR DOOR CONTROL VALVE MECHANISM. REPLACED SPRING IAW MM 32-32-7, PERFORMED GEAR SWING IAW MM 32-30-0; FOUND NORMAL SYSTEM. 2L74 4F 4A25 20031027000952003102700095NM 2003 10 27 ASAA02402CC 120030330A532065479573 THRESHOLD BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND AFT CARGO DOOR CUTOUT THRESHOLD WEB IS CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001222003102700122NM 2003 10 27 QXEA200301183 120030924A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 SEAT TRACK NR 8 HAS PITTING CORROSION AT STATION 496. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T4 TRTA13NM E20NE 20031028000282003102800028SO 2003 10 28 C2XA03TY169 120030929A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713995 145295 DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PLATE IAW-EMB-135/145-SRM-53-21-10 AND CMP-51-21-04, 05, 06. 2L72 4T RTT00011AT 20031029000112003102900011 2003 10 29 ASAA0380549 420030804A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 PDX PREFLIGHT CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20031029000292003102900029NM 2003 10 29 ASAA0340115 120030305A532065C30940 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT ANGLE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000512003102900051NM 2003 10 29 ASAA0310433 120030512A5347BAC15201331 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND SEAT TRACK AT BS 400-480, BUTTOCK LINE 0 HAS A BROKEN LUG. REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20031029000972003102900097EU 2003 10 29 KBM2003F00011 120030710A2822 PUMP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE NR 1 BOOST LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 NO NR 1 BOOST PUMP LEAKING (1 DROP IAW SECOND). DEFUELED, REMOVED AND REPLACED GASKET (PN 350A55-1103-22). ORINGS (PN 81811050) REFUELED AIRCRAFT. OPS CHECK GOOD.(K) 1G71 3U3 U H9EU E19EU 20031029001332003102900133EU 2003 10 29 KBM2003F00028 120030904A6720XEMRE8RSA8 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ROD END LOOSE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 PITCH CHANGE LINK UPPER ROD END HAS EXCESSIVE RADIAL PLAY. REPLACED ROD END BEARING WITH NEW. 1G71 3U3 UNCH9EU E19EU 20031030000482003103000048NM 2003 10 30 UPS03441311 120030901A5330 PANEL BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D BS 1241 LBL 75-79 BELOW FLOOR CANTED BULKHEAD CLOSEOUT PANEL CUTOUT CORRODED. CORROSION BLEND OUT 0.050 X 1 X 3 INCH. CLOSEOUT PANEL CUTOUT REPAIRED AS PER SRM 53-10-07 FIG 6. 2L74 4F A20WE 20031030000502003103000050NM 2003 10 30 UPS03441313 120030901A5310 PANEL BOEING747 747121 1384871NM FUSELAGE BULGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D BS 1241-1244, RBL 8 - 11 BELOW FLOOR CANTED BULKHEAD APU FUEL LINE CLOSEOUT PANEL FWD RT CORNER BULGE UP AND RIVET SHEARED. CORROSION BLEND OUT 0.035 X 1.5 X 4 INCH. EXISTING DOUBLER REMOVED AND NEW EXTENDED DOUBLER REPAIR AS PER RS R53-48-35075 AND ENGINEERING FILE NUMBER 747-53-20156. 2L74 4F A20WE 20031030000642003103000064WP 2003 10 30 UPS03841308 120030922A5311 FRAME DOUG DC8 DC873F 302199FWP AFT CABIN CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 STATION 1708 CANTED FRAME AT LONG 20R IS CHAFED BEYOND LIMITS. BLENDED OUT CHAFED AREA, AREA OF BLENDOUT BEYOND LIMITS IAW SRM 53-2-0 FIG 1F, FABRICATED AND INSTALLED ANGLE DOUBLER IAW DC8-5310-11728-A. 2L74 4F RT4A25 20031030000732003103000073EU 2003 10 30 WRNA200300013 120031001A361014J63550 CLAMP AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE ENGINE LOOSE A WRNAHJA DEACTIVATE SYST/CIRCUITSDUMP FUEL UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO05501TR 53 517468 NR 1 ENG NACELLE TEMP READ 300+ ON CLIMB OUT. TEMP. REACTED TO THROTTLE MOVEMENT. DUMPED APPROX. 30K LBS. RETURNED TO FIELD, LANDING NORMAL. MAINTENANCE FOUND IP CHECK VALVE CLAMP OFF DUCT. REINSTALLED CLAMP IAW PROCESS MATERIAL SPEC. MANUAL 01-05-42. ENGINE RUN UP LEAK AND OP'S CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20031030000812003103000081EU 2003 10 30 AWXA200301119 120030926A5320D534800432050100SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON THE R-2 DOOR SILL BEAM AT FR 66 Y1732. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR SILL BEAM FR 66 Y1732 IAW A320 SRM 51-42-11 PGS. 8-10, 12, 23-28 FIG. 9,10,11,12,23. 2L72 4F RTA28NM 20031030000822003103000082EU 2003 10 30 AWXA200301120 120030927A5345D535853070000100BRACKET AIRBUS320 A320232 3930326EU APU DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK THE RT APU DOOR HOLD OPEN HANDLE STAY PIN BRACKET WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED RT APU DOOR HOLD OPEN STAY PIN BRACKET IAW AWA E.R. 26-5358-03270-ES-1. 2L72 4F RTA28NM 20031030000892003103000089SO 2003 10 30 C2XA03SH366 120031002A541014576631621 STRUCTURE EMB 145 EMB145 3260210SO LT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C-CHECK THE LT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO CHAFED THRU. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031030000912003103000091WP 2003 10 30 ABXA030370 120030925A2897 WIRE DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE LT BOOST PUMP BURNED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 LEFT AFT BOOST PUMP AND RADIO RACK COOLING VALVE WIRES CHARRED AT STATION 237 (P1-1061L). REPAIRED WIRES HV-Q 13A20B, HV-Q 12A20C, H 211A24 IAW W.D. MANUAL 28-21-00 AND 21-21-00. LEFT AFT BOOST PUMP AND RADIO RACK COOLING VALVE. OPS CHECK GOOD. 2L72 4F4 F A6WE E2EA 20031030000982003103000098NM 2003 10 30 0301446624 120030806A5315 FLOORBEAM BOEING747 747251B 1384892NM PWA JT9 JT9D* NE FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING "L" CHECK FOUND CRACKS IN THE FLOORBEAM WEB, UPPER SECTION AND FRAME WEB AT BS 340 LT. THERE WERE CRACKS IN THE FLOORBEAM UPPER SECTION AT BS 340 RT. ALSO CRACKS WERE FOUND IN THE FLOORBEAM WEB, UPPER SECTION AND THE FRAME WEB AT BS 360 RT. REPAIRED IAW EA 66-165085. 2L74 4F4 F A20WE E20EA 20031031000032003103100003EA 2003 10 31 SWIA200312461 120030925A5752 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE AILERON DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07944SW 7764 AILERON TRIM WILL NOT MOVE RIGHT WING DOWN DIRECTION. WILL MOVE LEFT WING DOWN. REPLACED TRIM PANEL. OPS CHECK GOOD IAW MM 27-00-00. PN: 601R51226-23SW 2L72 4F4 FRTA21EA E15NE 20031031000052003103100005SO 2003 10 31 SWIA200312463 120030923A3320 LIGHT EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE GALLEY FAILED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07295SW 120322 LIGHT TO LEFT OF PHONE IN GALLEY BURNED OUT IN FLIGHT. AFTER, WE NOTICED AN ACRID SMELL IN COCKPIT AND CABIN. AFTER ABOUT 10 MINUTES, SMELL CAME BACK AND LIGHTS ON GALLEY PANEL FLICKERED.REPLACED AFT GALLEY LIGHT BALLAST. OPS CHECKS OKAY. 2L72 4T4 TRTA31SO E20NE 20031031000062003103100006EA 2003 10 31 SWIA200312464 120030927A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07405SW 7029 FLIGHT SPOILER FAULT STATUS MSG ON TAXI RESET CB'S 1N8, 1F3, 2N8, 2F3, 4A2, 4A3, 4A4, 4A5 IAW MX CONTROL. MESSAGE WENT AWAY. REMOVED AND REPLACED NR 1 SECU IAW MM 27-61-05. OPS CHECKS GOOD. S/N OFF 0273 2L72 4F4 FRTA21EA E15NE 20031031000122003103100012SO 2003 10 31 HYI2003F00016 220030827A741410357586 DISTRIBUTOR GEARCONT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO LT MAGNETO FAILED E HYIAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 NE01120PC634 I200011ER 402C0079 823344 ON CLIMB OUT, PILOT REPORTED RIGHT ENGINE RUNNING ROUGH, RETURNED W/O INCIDENT. MECHANIC FOUND RT ENGINE/ LEFT MAGNETO DIST GEAR FAILED. REMOVED AND REPLACED MAGNETO AND RETURNED A/C TO SERVICE. 1L72 3O3 O A7CE E8CE 20031028000412003102800041EA 2003 10 28 SWIA200312454 120030903A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07916SW 7634 PAX DOOR OUTER HANDLE IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE REMOVED AND REPLACED. P/N: 601R31763-1. 2L72 4F RTA21EA 20031028000622003102800062SO 2003 10 28 C2XA03SH357 120030930A532014521725001 SILL EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE LEFT SILL BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031028000872003102800087NM 2003 10 28 DHL2003741010 120031018A33501000679 LIGHT BOEING727 7272Q9 138448MNM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01741DH 21931 CREW ENTRY DOOR GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED GALLEY EMERGENCY LIGHT PER M/M 33-50-01. OPS CHECKED GOOD. 2L73 4F RTA3WE 20031029000272003102900027NM 2003 10 29 ASAA0310522 120030815A3350 BATTERY PACK BOEING737 737298C 1384490NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 DURING INSPECTION, FOUND EMERGENCY FLOOR PATH LIGHTS AT PALLETS 1-6, 2-1, AND 3-1 INOPERATIVE. REPLACED FORWARD TRANSMITTER P/N 87320304, AND BATTERY PACKS P/N 883200312, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20031029000542003102900054 2003 10 29 ASAA0380512 420030627A25653961896501 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A K NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 PREFLIGHT CHECK, FORWARD RIGHT SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20031029000612003102900061NM 2003 10 29 ASAA0240219 120030401A532065C2730892 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 PAE - DURING C-CHECK, FOUND CORROSION ON SIDE WALL SUPPORT. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000852003102900085NM 2003 10 29 AMTA200301197 120030918A2162 WARNING LIGHT BOEING737 73783N 13844HINM LT PACK ILLUMINATED A AMTAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL11315TZ 28245 LT PACK LIGHT COMES ON DURING MASTER CAUTION RECALL. PERFORMED BITE TEST ON LEFT PACK TEMP ZONE CONT. OP CHECK GOOD, AS PER FIM 21-62-00-810. (M) 2L72 4F RTA16WE 20031030000412003103000041NM 2003 10 30 UPS03441299 120030905A5712 RIB BOEING747 747121 1384871NM NR 2 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 2 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 6 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). BOLT HOLES NR 2 TO NR 6 AND NR 8 REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000432003103000043NM 2003 10 30 UPS03441301 120030905A5712 RIB BOEING747 747121 1384871NM NR 1 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 1 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20030909001352003090900135NE 2003 9 9 ARWA20030706 220030711A7230 COMPRESSOR LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B40254555NE NR 3 ENGINE DAMAGED A ARWAEJ ENGINE SHUTDOWN DUMP FUEL EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO19308GB547566768 193U1133 14637 LOG PAGE 23902 NR 3 ENGINE VIBRATION 4 UNITS BOTH A & B CHANNELS IN NORMAL POSITION NR 3 ENGINE SHUTDOWN AT 1340 Z. INSPECTED NR 3 ENGINE; FOUND METAL ON EXHAUST TAIL PIPE; BOROSCOPED ENGINE, FOUND DISCREPANCIES ON HIGH PRESSURE COMPRESSOR OUT OF LIMITS AND REJECTED ENGINE S/N 14637 IAW RB211 MM 72-00-00. REMOVED AND REPLACED NR 3 ENGINE IAW L-1011 MM VOLUME 1, FORM L-1011-7104A AND OPERATIONAL CHECK FORM L-1011-7102B FOUND NORMAL. BOROSCOPED, NO DISCREPANCIES FOUND IAW FORM L-1011-7200 FOR ENGINE NR 3, S/N 14611. 2L73 4F4 F A23WE E12EU 20030909001402003090900140EA 2003 9 9 SWIA200312367 120030828A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07590SW 7077 FLAPS FAIL CAUTION DURING INITIAL DESCENT INTO SLC. NO FLAP LANDING. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10. OPS CHECK GOOD. P/N: 955D100-9, S/N OFF: 206B. 2L72 4F RTA21EA 20030909001502003090900150SW 2003 9 9 ALGA088877 120030826A7120230511106 SUPPORT BELL 407 407 1182206SW ALLSN 250C 250C47B GL COMPRESSOR DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03647AL 53357 CAE847389 COMPRESSOR SUPPORT LEAKING INTERNALLY ON PRESSURE CHECK TEST. RETURNED PART TO VENDOR FOR WARRANTY CREDIT. 1G71 3U3 UO H2SW E1GL 20030909001922003090900192SW 2003 9 9 HEEA088941 120030821A5610407030115125A WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 WINDSHIELD CRAZED. 1G71 3U O H2SW 20030909001942003090900194WP 2003 9 9 IXXA0300051O 120030729A2120PS1317 VALVE DOUG DC8 DC862 3021970WP A/C BAY DAMAGED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW1131CX 76597623 45911311 ON CLIMBOUT FROM PHIK THE LEFT PACK DUCT TEMPERATURE WENT TO 80 DEGREES. CREW TURNED OFF PACK AND THE TEMPERATURE WENT UP. CREW RETURNED TO PHIK AND LANDED WITH OUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT AIR MIX VALVE IN ACCORDANCE WITH ALL APPLICABLE MANUALS. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 20030909002022003090900202NM 2003 9 9 PCAA0307086 120030727A3320BV0330012150 SOCKET DHAV DHC8 DHC8102 2809003NM CABIN MELTED A PCAAK NONE MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13810EX 308 BUF-FLIGHT 3597 CREW REPORTED A BURNING SMELL IN THE CABIN, PROMINENT AROUND SEATS 4DF & 5DF. MAINTENANCE FOUND THE PLUNGER ABOVE 4DF OVERHEAD LIGHT WAS MELTED. PLUNGER AND SOCKET ASSEMBLY WERE REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030909002062003090900206EU 2003 9 9 HEEA088946 120030815A6210117151341 BLADE BOLKMS117 BK117A1 5626010EU MAIN ROTOR DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 OPEN IN BONDING BETWEEN ROOT AND VIBRATION ABSORBER. 1G72 3U H13EU 20030909002072003090900207SW 2003 9 9 ALGA088833 120030822A5320206064902036 CHANNEL BELL 407 407 1182206SW FUSELAGE CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03409AL 53494 CHANNEL CRACKED AT LOWER. AND MIDDLE DZUS RECEPTICALS.PROBABLE CAUSE IS ASB 407-02-54. 1G71 3U O H2SW 20030909002242003090900224WP 2003 9 9 DHL2003604662 120030606A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT HORZ STAB L/E HAS INTERIM REPAIR & SEVERAL DENTS BETWEEN STA XFS 47.500 AND XFS 91.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030505, ED 3270. REMOVED FASTENERS & EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER & A FILLER IAW EO DHL 030505, ED 3270. CLEANED, TREATED & PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER & DOUBLER ON LT HORZ STAB L/E STA XFS 47.500 AND XFS 91.250, USING NEW FASTENERS IAW EO DHL 030505, ED 3270, SRM 51-1-21 PG 1 SRM 51-1-21A PG 4-3. 2L74 4F RT4A25 20030909002272003090900227WP 2003 9 9 DHL2003604580 120030603A5753 TEE FITTING DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTBD FLAP TEE ANGLE 2.000 CRACKED (FLAP JOINT AREA) STA XF 165.000. REMOVED DAMAGED TEE ANGLE IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TEE ANGLE IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030909002332003090900233WP 2003 9 9 ABXA030313 120030715A532039172861 ATTACH FITTING DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 FLOORBEAM TO KEEL ATTACH FITTING CRACKED AFT SIDE AT FS 718. REPLACED FITTING IAW REA D953-47908. 2L72 4F A6WE 20030909002452003090900245EA 2003 9 9 ASOA03375 120030816A5320601R311719 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE INTERCOSTAL BRACKET AT FS 484 AND LBL 27 AND RBL/LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INTERCOSTAL BRACKET AT FS 484 AND LBL 27, RBL/LBL 36 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030909002632003090900263NE 2003 9 9 RAIA00308221 220030822A731431057809 PUMP JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE LT ENGINE DEFECTIVE A RAIAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE03561HK13858277 41077 5619-STL- LEFT ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE REMOVED AND REPLACED NR 1 FUEL PUMP. 2L72 4T4 TRTA41NM E18NE 20030909002642003090900264EU 2003 9 9 RAIA00308222 120030825A2432407817 BATTERY JETAIRJETSTMJETSTM4101 1500501EU RIGHT OVERHEATED A RAIAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 CE03573HK13294145 41092 5568-STL- RIGHT BATTERY HIGH TEMP LIGHTS. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN BATTERY. 2L72 4T RTA41NM 20030909002652003090900265EU 2003 9 9 RAIA00308223 120030827A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK 41040 MX-STL- ESCAPE PATH LIGHT OUT AFT CABIN. SECURED ELECTRICAL CONNECTOR AT PATH LIGHTS. 2L72 4T RTA41NM 20031030000592003103000059NM 2003 10 30 UPS03441322 120030903A5720 ANGLE BOEING747 747121 1384871NM NLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, FX NOSE TUNNEL RT WW SIDEWALL ATTACH ANGLE CORRODED AT STA 380. CORROSION BLEND OUT 0.040 X 1.25 X 4 INCH. BS 380 RT VERT ANGLE REPAIRED AS PER RS R53-18-35076 AND UPS EO B747-5310-19273-A FOR REPEAT DETAIL EXTERNAL VISUAL INSPECTION. 2L74 4F A20WE 20031030000792003103000079NM 2003 10 30 QXEA200301197 120030927A5320 WEB DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 WEB BETWEEN FRAMES 333.3 AND 312.35 ARE BROKEN AT AFT INBOARD END OF LEFT FUSELAGE. REPAIRED IAW DHC-8 RD 8-53-7555 AND EA 2-56-484. 2H72 4T4 TRTA13NM E20NE 20031030000802003103000080EU 2003 10 30 AWXA200301114 120030925A5420D54530052200201 FAIRING AIRBUS320 A320232 3930326EU AFT PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON IB SIDE OF AFT PYLON FIXED FAIRING AT RIB 11 TO RIB 16. MAINTENANCE REMOVED AND REPLACED AFT FAIRING FIXED SKIN AT RT PYLON RIB 11-16 IAW A320 SRM 51-42-11 FIG. 8 PAGES 21 AND 22 AND SRM 54-54-11 FIG.1 PAGES 1-3 AND 51-42-11 FIG.2-3 PAGES 7-12. 2L72 4F RTA28NM 20031030000952003103000095NM 2003 10 30 03FDEA01672 120031001A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 EXTERNAL SKIN CHAFED BS 720D 13 INCHES, STR 19R ** SD ** COMING 2L73 4F4 FRTA3WE E2EA 20031031000232003103100023SO 2003 10 31 C2XA03IA101 120030926A2913PV303211 PUMP EMB 145 EMB145 3260210SO NR 2 ENGINE LEAKING A C2XAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW2712957 145080 FLIGHT 2680, DURING DESCENT THE CREW NOTED THAT HYD. 2 LOW QTY MES ON EICAS, LOSS OF FLUID IN FLIGHT, DECLAIRED EMERGENCY, AND, PERFORMED EMERGENCY DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. PERFORMED A LEAK CHECK, AND, A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031031000252003103100025SO 2003 10 31 C2XA03SH369 120031003A531014521721009 BUTTSTRAP EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 SHV-DURING C CHECK THE FWD DIGITAL BUTTSTRAP AT FR 14 TO FR 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031031000282003103100028NM 2003 10 31 03FDEA01666 120031001A5310 STRUCTURE BOEING727 727200 138407ENM NLG WW GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 NLG WHEEL WELL HAS NUMEROUS GOUGES AROUND RT AFT PRESSURE PANEL CUTOUT. REPAIRED AS PER SRM 51-40-2. 2L73 4F RTA3WE 20031031000502003103100050EA 2003 10 31 COMA0360442 120030930A30205399001 VALVE CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYS FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01810CA1 7370 FLIGHT 5814 RIGHT COWL ANTI ICE CAUTION MESSAGE. REPLACED THE ANTI ICE VALVE. 2L72 4F RTA21EA 20031031000612003103100061NM 2003 10 31 QXEA200301211 120031002A5412 ANGLE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 NR 1 ENGINE FIREWALL ANGLE IS CRACKED AT BOTH ENDS JUST BELOW AFT TOP HEAT SHIELD. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20031031000682003103100068NM 2003 10 31 DL757030833 120030912A3397BV031120333 TERMINAL BOEING757 757232 1384965NM CABIN BURNED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27633DL 23614 RETURN TO GATE, F/A REPORT FAINT ELECTRICAL SMELL IN AFT LAV. LOCATED ELECTRICAL SMELL FROM ROW 44 RT SIDE CEILING LIGHTS FLUORESCENT LIGHT ASSY AFT END TERMINAL BURNT. PULLED C/B-7 IN P37 PANEL AND DEACTIVATED RT CEILING LIGHTS. FWD TO MCO AND PLAC PER 33-21-01. NO ELECTRICAL SMELL FROM AFT LAV. 2L72 4F RTA2NM 20031031000702003103100070NM 2003 10 31 DLM88030835 120030914A3260387 BULB DOUG MD88 MD88 3023688NM LTGEAR IND BURNED OUT A DALAL ABORTED APPROACH P NO WARNING INDICATION LDLANDING 1 SO27931DL 49718 A/C DID FLY BY TO CONFIRM GEAR DOWN LOG BOOK WRITE UP WAS: BULB BURNED OUT IN LT MAIN GEAR INDICATOR. RELAMPED INDICATOR. 2L72 4F RTA6WE 20031031000722003103100072NM 2003 10 31 DL757030838 120030912A5330146N330511 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27658DL 24420 THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS BELOW THE C2 DOOR CUTOUT AT FS 1396 BETWEEN STRINGERS 27R & 29R. THE DENTS WERE REMOVED WITH 2 CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER REPAIR PER ER/A 385618-14, REV A. 2L72 4F RTA2NM 20031031000742003103100074NM 2003 10 31 DL757030840 120030912A5330146N351111 SKIN BOEING757 757232 1384965NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27660DL 24422 THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 1335 BETWEEN STRINGERS 29L & 30. THE GOUGE WAS REMOVED WITH A CUTOUT TO THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385637-14, REV A. 2L72 4F RTA2NM 20031031000772003103100077NM 2003 10 31 DL757030843 120030912A5330143N34719 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27658DL 24420 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 500 AND STRINGER 28L. THE CORROSION WAS REMOVED WITH A 4.5 X 3.3 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385647-14, REV A. 2L72 4F RTA2NM 20031031000832003103100083NM 2003 10 31 DL733030850 120030916A532065458331 INTERCOSTAL BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312WA 23598 MODIFICATION OF THE FS 178 BULKHEAD REVEALED A CRACK IN THE LBL & RBL 28 COCKPIT FLOOR INTERCOSTAL WEB AND CHORD AT WL 107. THE CRACKED CHORD AND WEB WERE REMOVED AT BOTH LOCATIONS AND PARTS INSTALLED PER ER/A 385678-14AD. 2L72 4F RTA16WE 20031103000072003110300007GL 2003 11 3 DL764030859 220030921A7530 SHUTOFF VALVE BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 1 ENGINE FAILED A DALAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO27842MH 29715 706253 ON TAKEOFF ROLL L ENG BLEED OFF CAUTION LIGHT ILLUMINATED. FOLLOWED BY L PACK OFF LIGHT. ALSO LT BLEED HPSOV STATUS MESSAGE. REPLACED PRESSURE REGULATOR VALVE. 2L72 4F4 FRTA1NM E23EA 20031103000172003110300017NM 2003 11 3 DL76G030871 120030924A2910272T3100485 LINE BOEING767 767332 1382001NM LEFT PYLON CHAFED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO271604R 30180 FLIGHT DIVERTED TO LGW WITH LOSS OF LEFT HYDRAULIC FLUID. FOUND HYD PIPE IN LEFT PYLON CHAFED THROUGH DUE TO PYLON LATCH OPENING IN FLIGHT AND CHAFING ON PIPE. THE LINE IS DETAILED IN IPC 29-11-27-02 ITEM 116 RESERVOIR RETURN LINE FROM HEAT EXCHANGER. TIME LIMITED REPAIR WITH FLEX LINE. ALSO FOUND LEFT EDP LEAKING AT BLEED POINT. EDP REPLACED. 2L72 4F RTA1NM 20031103000262003110300026NM 2003 11 3 DLM11030881 120030927A2520 MODULE DOUG MD11 MD11 3023602NM CREW REST LOOSE A DALAO OTHER O OTHER CRCRUISE 1 SO27804DE 48475 COULD NOT STOW CREW REST MODULE, L1 DOOR BLOCKED. FOUND LOOSE SCREW ON TRACK ASSY CAUSING INTERFERENCE WITH TRACK. TIGHTENED SAME. CREW REST MODULE OPEN/CLOSE AND LOCK/UNLOCK FUNCTIONS CHECKS OKAY. 2L73 4F RTA22WE 20031103000312003110300031NM 2003 11 3 DL757030889 120030930A335020131A BATTERY BOEING757 757232 1384965NM EMERGENCY LIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27618DL 22908 ON LAYOVER FOUND FIRST THREE ROWS IN FIRST CLASS MISSING OVERHEAD EMERGENCY LIGHTS. REMOVED AND REPLACED PWR SUPPLY BATTERY, SYSTEM CHECKS NORMAL. 2L72 4F RTA2NM 20031103000412003110300041NM 2003 11 3 DL73S030899 120031003A8012 DUCT BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE DAMAGED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27302DL43088 23047 709178 RT ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB, WENT OUT WITH THROTTLE AT IDLE. FOUND DAMAGED STARTER DUCT. REPLACED SAME. 2L72 4F4 FRTA16WE E2EA 20031103000492003110300049WP 2003 11 3 03FDEA01694 120031003A5753ARB3897501 STUD DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 LT WING OB FLAP IB 4 EACH FITTINGS ATTACH STUDS HAVE PITTING CORROSION AND FLAT THREATS. CLOSING ACTION ON 10/03/03.ON N/R N01201. REMOVED AND REPLACED LT FLAP MOUNT STUDS HINGES IAW M/M 57-41-01-2. ENCAPSULATED (2) BOTTOM MOUNT STUDS IAW M/M 57-41- 01-2, AND E.A 8-5750-72304. 2L73 4F A22WE 20031103000612003110300061NM 2003 11 3 03FDEA01683 120031002A5713 STRINGER BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 N01203 LT WING STA 656.5, STRINGER 12 UPPER TAB CRACKED (VENT BOX) REPAIRED IAW EA 7-5710-55011. 2L73 4F RTA3WE 20031103000762003110300076EU 2003 11 3 DHL2003364014 120031004A3242C200601004 BRAKE AIRBUS300 A300B4203 3930306EU MLG DAMAGED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01364DH 141 UNCOMMANDED BRAKE APPLICATION DURING TAXI AFTER LANDING. FOUND NR 3 BRAKE DAMAGED, REPLACED NR 3 BRAKE ASSEMBLY IAW M/M 32-42-27. OPS AND LEAK CHECKED GOOD. 2L72 4F RTA35EU 20031103000832003110300083NE 2003 11 3 ALG2003F00075 120030729A7921763080790106 OIL COOLER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 2 ENGINE MALFUNCTIONED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03709AL 760278 SHORTLY AFTER TAKE OFF, DURING CLIMB OUT NR 2 ENGINE OIL TEMP EXCEDED REDLINE. AIRCRAFT RETURNED TO CREOLE, TEMPERATURE REACHED 115 DEGREES FOR 10 MINUTES, THE MECHANIC CHECKED CHIP PLUGS AND REPLACED THE ENGINE OIL, THERMOSTAT AND OIL COOLER AND HE CHECKED THE ENGINE INTERNAL OIL FILTER. 1G72 3U3 U H1NE E1GL 20031103000852003110300085SW 2003 11 3 ALG2003F00077 120030729A243523081014 STARTER GEN BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE FAILED E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW035756N 45546 CAE860301 AFTER TAKE OFF ENGINE BEGAN SURGING, AIRCRAFT WAS YAWING LEFT AND RIGHT, TORQUE WAS FLUCTUATING +/- 30 PERCENT. THROTTLE CONFIRMED OPEN, ENGINE BEEPED TO MAXIMUM N2 AND NR WOULD NOT GO ABOVE 94 PERCENT UPON LANDING THE MECHANIC REMOVED AND REPLACED THE GOVERNOR AND STARTER GENERATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E1GL 20031028001352003102800135EA 2003 10 28 ASOA03489 120031006A5210601R3807413 ANCHOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11885AS 7521 DURING A HANGAR INSPECTION IN MCN, THE FORWARD ADN AFT ANCHORS ON THE PASSENGER DOOR WERE FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR CRACK AND REPLACE ANCHORS WITHIN 100 FLIGHT HOURS PER REO 601R-52-11-272. (M) 2L72 4F RTA21EA 20031028001442003102800144NM 2003 10 28 GAIA03098 120030910A5521 RIB BOEING727 727223 1384074NM RT ELEVATOR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND RIGHT ELEVATOR SUPPORT RIB STATION 17.2 CRACKED. REF FASI N/R 53208, REPLACED ELEVATOR SUPPORT RIB PER S/B 727-55A0091. (M) 2L73 4F A3WE 20031028001492003102800149NM 2003 10 28 GAIA03083 120030910A5347 SEAT TRACK BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 344 TO BS 360, RBL 45.5. REF FASI N/R 50403. FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 14 INCHES REPAIRED IAW B727 SRM 53-10-05, FIGURE 7 AND 53-10-2, FIGURE 7. (M) 2L73 4F A3WE 20031028001502003102800150NM 2003 10 28 GAIA03084 120030910A5311 FRAME BOEING727 727223 1384074NM BS CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND FUSELAGE FRAME AT BS 950D CRACKED, ABOVE STRINGER 22R. REF FASI N/R 50407, FABRICATED REPAIR DOUBLER FROM 7075-T6, .080, DIMENSIONS 9 INCHES BY 3 INCHES. REPAIRED IAW S-727 SRM 51-40-3, FIGURE 1. (M) 2L73 4F A3WE 20031028001522003102800152NM 2003 10 28 GAIA03088 120030910A5311 FRAME BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 560 CRACKED BELOW STRINGER 16RT. REF FASI N/R 53131 CUTOUT DAMAGE, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F A3WE 20030908002872003090800287NM 2003 9 8 SWAA031936 120030828A53126545409 PRESSURE PANEL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 30. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20030908003272003090800327 2003 9 8 SWAA031930 420030828A2565D31354 SLIDE BOEING737 7375H4 138449DNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030908003312003090800331NM 2003 9 8 SWAA031907 120030826A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 907, WL 162 AND RBL 3. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030908003402003090800340NM 2003 9 8 SWAA031924 120030828A573065C25204 SKIN BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED 1/2D CHECK, FOUND LT WING UPPER SKIN CRACKED AT WBL 181. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030909000602003090900060NM 2003 9 9 VNAA0308024 120030829A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DISCHARGED A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07436JS12425704 3052 THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT 9A WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030909001362003090900136NE 2003 9 9 S2YA03005 220030207A7261 GARLOCK SEAL BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE LEAKING A S2YAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL1392SK UE92 PCE114207 AFTER TAKEOFF ON FLIGHT 1167, A LEFT ENGINE OIL PRESSURE FLUCTUATION BETWEEN 70 AND 90. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT, SERVICED THE LEFT ENGINE WITH 4 QUARTS OF OIL AND RETURNED THE AIRCRAFT TO SERVICE. MECHANIC INSPECTED THE AIRCRAFT ON 2/14/03 AND REPLACED THE LEFT GARLOC SEAL. 2L72 4T4 TRTA24CE E26NE 20030909001722003090900172EU 2003 9 9 BAQA088896 120030822A62401179405303 INDICATOR BOLKMS117 BK117B1 5626012EU TRIPLE TACH INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE13 7219 TRIPLE TACH NR 1 NEEDLE IS INOPERATIVE. THIS UNIT LASTED FOR 5 DAYS (11.2) HOURS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030909002142003090900214WP 2003 9 9 ABXA030340 120030811A53203957174505 FITTING DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 FS 1152 LEFT SIDE OF AFT VENTRAL STAIR CUTOUT FRAME FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030909002292003090900229WP 2003 9 9 DHL2003604572 120030513A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING INBD L/E FORMER CRACKED 0.250 AT XFS 597.500. STOP DRILLED CRACK AT XFS 597.500 AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030909002612003090900261WP 2003 9 9 2003F00549 220030813A7210310703411 TORQUE RING BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP NR 1 ENGINE FAILED A B16AA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 NE05538PA 751 FLT 3525 - BGR - PILOT REPORTED AFTER TAKEOFF, NR 1 ENGINE TORQUE GAUGE BEGAN TO FLUCTUATE FROM 120 PERCENT OT 0 PERCENT. ENGINE BEGAN TO TTL DUE TO TORQUE READING. TTL WAS TURNED OFF AND ENGINE CONTINUED AND STABILIZED. THEN TORQUE GAUGE DROPPED TO 0 PERCENT AND STAYED THERE. REMOVED AND REPLACED NR 1 ENGINE TORQUE RING ASSEMBLY WITH SERVICEABLE UNIT IAW GARRETT MM 72-10-12. SET SIGNAL CONDITIONER TO CURRENT DSC SHEET. (M) 2L72 4T4 TRTA21EU E4WE 20030909002672003090900267GL 2003 9 9 RAIA00308225 220030828A7532 BLEED VALVE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE DIRTY A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03811HK 145256 5251-PIT- ENGINE NR 1 ATTCS INOPERATIVE-NO MARGIN. MAINTENANCE CLEANED NR 1 COMPRESSOR ACCELERATION BLEED VALVE. 2L72 4T4 FRTT00011ATTE6CH 20030909002692003090900269EU 2003 9 9 RAIA00308227 120030829A3397 WIRE AEROSPATR42 ATR42300 8680920EU CABIN BROKEN A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE 119 MX-STL- EMERGENCY LIGHT AT CABIN STEPS INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY. 2H72 4T RTA53EU 20030909002712003090900271EU 2003 9 9 RAIA00307192 120030716A21501718D000 ACM JETAIRJETSTMJETSTM4101 1500501EU A/C BAY SEIZED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03566HK1313212453 41084 5645-STL- UNABLE TO COOL AIRCRAFT IN AUTO OR MANUAL. MAINTENANCE REMOVED AND REPLACED NR 2 ECS COLD AIR UNIT. 2L72 4T RTA41NM 20030909002722003090900272EU 2003 9 9 RAIA00307193 120030718A3610K11752 SEAL JETAIRJETSTMJETSTM4101 1500501EU BLEED AIR SYS BLOWN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03569HK 41088 5641-STL- LEFT DUCT FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED THE LEFT DUCT GAMMA SEAL. 2L72 4T RTA41NM 20030909002792003090900279EA 2003 9 9 QXEA200300948 120030802A7830 RELAY CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER FAILED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09602QX 10010 PDX- ON FLIGHT 2431 ABORTED TAKEOFF DUE TO RIGHT REVERSE CAUTION MESSAGE APPEARED DURING POWER APPLICATION FOR TAKEOFF. MESSAGE WENT AWAY WHEN THRUST LEVERS RETRACTED TOWARDS IDLE. FOUND FAULT GROUND RELAY AK30 RELAY CLOSED. GROUND RAN AIRCRAFT AND PERFORMED OPERATIONAL TEST OF THRUST REVERSER. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031003000712003100300071NM 2003 10 3 03FDEA01536 120030904A5753ARC2512504 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBD PIVOT LUG INBD AND OUTBD SURFACE FOUND CORRODED. 2L73 4F RTA22WE 20031003000992003100300099NM 2003 10 3 MWEA030369 120030911A2910AE712811503 HYDRAULIC LINE BOEING717 717200 1383700NM ENGINE INOPERATIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31908ME 55172 HYRAULIC RIGHT AND LEFT LOW ALERT APPEARED. REMOVED AND REPLACED PRESSURE LINE AT HYDRAULIC PUMP. 2L72 4F TRA6WE 20031006000062003100600006EA 2003 10 6 COMA0360410 120030907A1220 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE OVERSERVICED A COMAA UNSCHED LANDING WMJINADEQUATE Q C OVER TEMP WARNING INDICATION CLCLIMB 1 SO01965CA 7131 FLIGHT 5244 RT ENGINE, HIGH OIL TEMP. FOUND OIL SYSTEM OVERSERVICED - DRAINED OIL TO NORMAL LEVEL. 2L72 4F RTA21EA 20031006000882003100600088GL 2003 10 6 CHQA000421 220030914A7200AE3007A1P ENGINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 SHUTDOWN A CHQAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL11278 DURING CLIMB WITH NORMAL INDICATIONS ON OIL LEVELS, TEMPS, AND PRESSURES THE RIGHT NR 2 ENGINE SHUTDOWN AS WE CLIMBED THROUGH 26,000 FT. AN EMERGENCY WAS DECLARED AND DIVERTED TO DFW. ENGINE WAS CHANGED ON SEPTEMBER 15. 2L72 4F4 FRTT00011ATTE6CH 20031006001102003100600110NM 2003 10 6 2003UALA00678 120030909A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29368UA 24537 STA. 927 AT RBL45 INCH FLOORBEAM HAS A CRACK IN THE WEB AND A CRACK IN THE RADIUS OF THE T CAP. MAJOR REPAIR ACCOMPLISHED, INSTALLED ANGLES AND STRAPS. 2L72 4F4 FRTA16WE E2GL 20031006001262003100600126EU 2003 10 6 RAIA00309240 120030912A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSBROKEN A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03552HK 41057 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT PATH LIGHTS. 2L72 4T RTA41NM 20031006001492003100600149NM 2003 10 6 SWAA032015 120030908A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 482B AND BS 520, STR 10L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031006001502003100600150NM 2003 10 6 SWAA032016 120030908A27106939429 SPRING BOEING737 7373H4 1384600NM AILERON FEEL WORN A SWAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW29333SW 23697 AILERONS SLUGGISH WHEN TURNING FROM EITHER DIRECTION. REMOVED AND REPLACED AILERON FEEL AND CENTERING MECHANISM SPRINGS PER MM. 2L72 4F RTA16WE 20031007000462003100700046EA 2003 10 7 A6WA200340135 120030908A282069254517 SOLENOID VALVE CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM LEAKING A A6WAK NONE K FLUID LOSS ININSP/MAINT 1 GL31436AW 7734 SUSPECT FUEL LEAK AT APU BAY. INSPECTED AND FOUND NO FUEL LEAKS SUSPECT APU FUEL SOLENOID VALVE NOT FULLY CLOSING. REMOVED AND REPLACED FUEL SOLENOID VALVE. OPS AND LEAK CHECK GOOD. (M) 2L72 4F RTA21EA 20031007000492003100700049NM 2003 10 7 AALA20030492 120030422A2530 OVEN BOEING757 757223 1384957NM GALLEY INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21671AA 25336 FLIGHT ATTENDANTS REPORTED SMOKE AND A BURNING SMELL FROM FORWARD GALLEY OVEN. RETURNED AND LANDED JFK WITHOUT INCIDENT. REMOVED DEBRIS FROM FIRT CLASS OVEN. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000842003100700084 2003 10 7 SWAA031958 420030830A2565D31354 SLIDE BOEING737 737301 1384611NM AFT ENTRY DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20031007000892003100700089NM 2003 10 7 SWAA031987 120030905A533065558788 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR CUTOUT FWD UPPER CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031008000112003100800011NM 2003 10 8 03FDEA01552 120030916A5320A5A7116503 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CENTER CARGO PIT HAS A POSSIBLE CRACK AT STA 5-115 STRINGER SPLICE 45L FLOOR AREA. 2L73 4F RTA22WE 20031008000162003100800016NM 2003 10 8 03FDEA01542 120030916A5320AFA7125501 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CENTER CARGO BAY, UPON REMOVAL OF STRINGER SPLICE 48R STA 1541 REF CARD NUMBER N0697 FOUND SUPPORTING BRACKET CRACKED. 2L73 4F RTA22WE 20031008000292003100800029NM 2003 10 8 HOC2003F00024 120030826A5311 FRAME BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0779749 22451 DURING A C-CHECK CORROSION WAS NOTED ON SUPPORT FRAME STA 920-920A AT BLO-LBL-1. 2L73 4F4 F A3WE E2EA 20031008000422003100800042NM 2003 10 8 QXEA200301132 120030913A5542 SKIN BOMBDRDHC8 DHC8401 1390041NM RUDDER DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 DENT IN SKIN OF FORE RUDDER TRAILING EDGE AFT OF LOWER HING, LEFT SIDE. REPAIRED IAW HORIZON AIR EA 6-27-140. 2H72 4T RTA13NM 20031008000512003100800051NM 2003 10 8 UPS03441233 120030905A5315AND101362006 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 400 FLOORBEAM UPPER SECTION UPPER FACE BTN RBL 0 / RBL 37 CORRODED. CORROSION REMOVED IAW SRM 51-10-01 CORROSION BLEND OUT 0.050 INCH X 1 INCH X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FOR BS400 RBL 0" REPAIR REFER SRM 53-10-07 FIG 8. CIC APPLIED IAW EO M5100-2780-E. AND BS400 RBL 37 CORROSION BLEND OUT 0.005 X 1 X 1 WITHIN SRM 53-10-01 FIG 1 LIMITS. 2L74 4F A20WE 20031008000562003100800056WP 2003 10 8 UPS03841227 120030916A2910 LINE DOUG DC8 DC871F 302199DWP HYD SYSTEM LEAKING A IPXAB EMER. DESCENT K FLUID LOSS LDLANDING 1 SO01744UP 45944 EMERGENCY LANDING FOR LOSS OF HYD QTY. REMOVED AND REPLACED BOGIE TRIM CYLINDER FLEX LINE, LT GEAR SERVICED HYD FLUID & OPERA TED ALL SYSTEMS CHECKS GOOD NO LEAKS. 2L74 4F RT4A25 20031009000022003100900002NM 2003 10 9 AALA20030853 120030804A5330 SKIN BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21384AA 26996 FOUND FUSELAGE SKIN HAS SMALL CRACK INDICATION IN FASTENER HOLE. FIRST OVERSIZE ON FASTENER HOLE. FASTENER HOLE OUTER SKIN ONLY HAS BEEN OVERSIZED TO .3075 INCHES TO REMOVED CRACK INDICATION. REAM OUTER SKIN ONLY FOR FREEZE PLUG .063 PLUS/MINUS .006 INCH PAST .3075 INCHES. INSTALL FREEZ PLUG PER 767 SRM 51-20-07 AND RETAIN PLUG PER SRM REQUIREMENTS. INSTALL FASTENER AS REQUIRED. (M) 2L72 4F RTA1NM 20031009000092003100900009NM 2003 10 9 USAA030192 120030913A5330 SKIN BOEING737 7373B7 1384580NM FS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US 22955 FOUND SKIN CRACKED .5 INCH, AFT ENTRY DOOR LOWER HINGE CUTOUT AT STATION 947.5, S-14L. DOUBLERS INSTALLED PER EA 76982 AND SRM 53-60-01, FIG 1, FIG 207. (M) 2L72 4F RTA16WE 20031009000122003100900012NM 2003 10 9 AALA20030802 120030708A5311 FRAME BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21359AA 24040 FOUND FRAME WEB AT STATION 1562 BL 0 HAD CORROSION BLENDED FROM SIDE. REQUEST ENGINE APPROVAL TO CONTINUE AS IS. ALODINED 2 COATS OF PRIMER. BLEND OUT CORROSION AND VERIFY CORROSION HAS BEEN COMPLETELY REMVOED. REFINISH BLENDED AREA WITH ALODINE AND TWO COATS BMS 10-11 PRIMER. (M) 2L72 4F RTA1NM 20031009000172003100900017NM 2003 10 9 USAASB03142 120030821A324140817 BEARING BOEING737 737301 1384611NM ANTI SKID XDUCERWORN A USAAO OTHER O OTHER LDLANDING 1 EA19592US 23937 UPON TOUCHDOWN AT ORF, FROM PHL, THE NR 2 MAIN LANDING GEAR TIRE BLEW. THE AIRCRAFT WAS OPERATING WITH MEL'S ON THE ANIT-SKID AND AUTO BRAKE SYSTEM. AIRCRAFT HAD TO BE TOWED INTO THE GATE FROM THE TAXIWAY. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND NO DAMAGE TO AIRCRAFT STRUCTURE. FOUND NR 2 ANTI-SKID TRANSDUCER BEARINGS BAD. REMOVED AND REPLACED NR 2 ANTI-SKID TRANSDUCER. OPS CHECK AND BITE CHECK GOOD PER MM 32-42-00. CLEARED MEL'S FOR ANTI-SKID AND AUTO BRAKE SYSTEM. ALSO, REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY, P/N 2-1474-7) AND BOTH NR 1 AND NR 2 MLG TIRE/WHEEL ASSEMBLIES, P/N 65-58256-275. SPIN CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20031009000182003100900018NM 2003 10 9 USAA030195 120030915A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US 23879 FOUND SKIN CRACKED 2 INCHES, FS 944 AT STRINGER 25L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202 IAW EA 77014. (M) 2L72 4F RTA16WE 20031009000222003100900022SO 2003 10 9 SIMA200323603 120030817A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21649PP 145234 CREW REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT STRIP IS INOPERATIVE. LIGHT STRIP PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE INVERTOR ASSEMBLY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031009000292003100900029 2003 10 9 SIMA200314805 420030527A34178221310003 DCU CNDAIRCL600 CL6002C10 1390015EA AVIONIC BAY INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21500AE 10025 CREW REPORTED A RUDDER LIMITER CAUTION AFTER TAKEOFF FOLLOWED BY PROXIMITY SYSTEM CHANNEL AND STEERING INOPERATIVE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND DCU1 FAULTED IN THROUGH THE MAINTENANCE DATA COMPUTER HISTORY. REMOVED AND REPLACED DCU1 IAW CRJ MM. OPS CEHCK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20031009000312003100900031SO 2003 10 9 SIMA200325103 120030908A3350 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21853AE 145742 CREW REPORTED THE LAST THREE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS TO BE INOPERATIVE. (M) 2L72 4F RTT00011AT 20031009000332003100900033SO 2003 10 9 SIMA200323602 120030820A3350744437 SIGN EMB 135 EMB135LR 3260305SO EMERGENCY EXIT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21707EB 145195 DURING PREFLIGHT CREW REPORTED THE LEFT WING EXIT SIGN DID NOT WORK. AIRCRAFT WAS INSPECTED AND FERRIED TO LGA FOR CORRECTIVE ACTION. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031014000062003101400006EU 2003 10 14 BAQA089601 120030819A212119A2772 BLOWER BOLKMS117 BK117A1 5626010EU VENT FAN INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 BLOWER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031014000202003101400020NM 2003 10 14 UPS03541240 120030906A5330 SKIN BOEING757 75724APF 1384969NM FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01449UP 27738 INSPECTION TYPE: C1, FUSELAGE SKIN HAS 3 LIGHTNING STRIKES AT BS 1736 TO BS 1739 BETWEEN STR 23L AND 24L. REPAIRED PER ER 03-3472 DATED 09/15/03. 2L72 4F RTA2NM 20031014000302003101400030CE 2003 10 14 AMWA56 120030910A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB. CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE073199Q UE3199Q 2 CRACKS FOUND IN THE RIB. IN JOGGLED SECTION OVER STRNG AT LAST RIVET. CRACKS LOCATED AT STRNG P/N 101-640000-37 AND 10-640000-46. 2L72 4T RTA24CE 20031014000922003101400092 2003 10 14 SWAA032210 420031004A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031014001032003101400103NM 2003 10 14 SWAA032140 120030923A27813818001005 ACTUATOR BOEING737 7377H4 1384404NM NR 5 LE SLAT FAULTY A SWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29776WN 30591 AIR TURN BACK, ON FLAP RETRACTION L/E LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED NR 5 L/E SLAT ACTUATOR PER MM. 2L72 4F RTA16WE 20031014001362003101400136NM 2003 10 14 SWAA032156 120030926A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 895, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031014001402003101400140NM 2003 10 14 SWAA032053 120030913A53116546569 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 22R AND STR 23R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031014001882003101400188 2003 10 14 SWAA032109 420030920A256565C19901 CABLE BOEING737 7373Q8 1384670NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED SLIDE RELEASE CABLE PER MM. 2L72 4F RTA16WE 20031014001902003101400190NM 2003 10 14 SWAA032107 120030920A55206959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 AND NR 2 HINGE ATTACH HARDWARE PER MM. 2L72 4F RTA16WE 20031014001972003101400197CE 2003 10 14 BAQA089635 120031007A2422PC17 INVERTER BEECH 100 100BEECH 1152916CE INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G B144 INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20031014001982003101400198EU 2003 10 14 BAQA089497 120031007A32402058000001 BRAKE ASSY AEROSPAS365 AS365N2 8680815EU MLG WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 BRAKE ASSY WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20031014002012003101400201EU 2003 10 14 BAQA089690 120030925A2435524031 STARTER GEN AEROSPAS365 AS365N2 8680815EU ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME58 6417 STARTER GEN INOPERATIVE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20031014002072003101400207EU 2003 10 14 BAQA088356 120031002A2822P94C16606 PUMP AEROSPSA365 SA365N 8680669EU FUEL BOOST INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM398 6396 BOOST PUMP INOPERATIVE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20031014002132003101400213CE 2003 10 14 BAQA089577 120031004A2752505212233 ACTUATOR BEECH 100 100BEECH 1152916CE TE FLAPS WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G B144 ACTUATOR WORN. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20031015000242003101500024EU 2003 10 15 ASOA03418 120030905A3230S3238006120100 SUPPORT BRACKET AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING HANGAR MAINTENANCE IN MCN, THE LT MAIN LANDING GEAR TOP LT AFT UPLOCK SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR TOP LEFT AFT UPLOCK SUPPORT BRACKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031015000312003101500031EA 2003 10 15 ASOA03438 120030913A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11904EV 7628 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT PRESSUER BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT AFT PERSSURE BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20031015000402003101500040EU 2003 10 15 ASOA03443 120030903A5320 BRACKET AEROSPATR72 ATR72212 8680945EU TAIL CONE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING A C-CHECK IN BNA, THE TAIL CONE MOUNTING BRACKETS AND SEAL RETAINERS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TAIL CONE MOUNTING BRACKETS AND SEAL RETAINERS IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20031015000412003101500041EU 2003 10 15 ASOA03447 120030916A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031015000462003101500046EA 2003 10 15 ASOA03448 120030916A5300 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 IAW ASA EO 600-53-0122. (M) 2L72 4F RTA21EA 20031020000632003102000063NM 2003 10 20 VNAA0310004 120031004A3020 LINE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT ENGINE FAILED A VNAAO OTHER N FALSE WARNING CLCLIMB 1 GL07426JS 3038 DURING FLIGHT, THE CREW RECEIVED A RIGHT HAND ENGINE INTAKE DE-ICE FAIL INDICATION AND RETURNED TO PHL. MAINTENANCE INSPECTED AND REPLACED THE INTAKE LINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031020001502003102000150NM 2003 10 20 DL777030800 120030831A2597 WIRE HARNESS BOEING777 777232 1385232NM CABIN DAMAGED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27864DA 29736 SEAT 44D EXPOSED SPARKING WIRES LEADING TO INSEAT TV MONITOR FWD TO MCO MEL 25-25-02J ENTIRE IFE INOP. ALSO DISCONNECTED C/P J1 AND J2 AT AVU UNDERSEAT 44D. REPLACED MONITOR HARNESS. CHECKS GOOD. 2L72 4F RTT00001SE 20031014001222003101400122 2003 10 14 SWAA032170 420030927A2565 GIRT BAR BOEING737 7377H4 1384404NM SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031014001532003101400153NM 2003 10 14 SWAA032074 120030917A53116546529 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500D, BETWEEN STR 28R AND STR 28L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031014001612003101400161 2003 10 14 SWAA032066 420030917A2565 INDICATOR BOEING737 7372H4 138448CNM SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031014001632003101400163NM 2003 10 14 SWAA032091 120030918A53206551698 SPLICE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360. STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031015000082003101500008NM 2003 10 15 USAASB03162 120030909A335020121 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU 23595 MAINTENANCE REPORTED THE LEFT OVERWING EMERGENCY IDENTIFIER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK, P/N 2013-1A, AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031015000522003101500052EA 2003 10 15 ASOA03427 120030909A3010GG670800144 DUCT CNDAIRCL600 CL6002C10 1390015EA WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11713EV 10081 DURING A GROUND INSPECTION IN DFW, THE RIGHT INBOARD LEADING EDGE SLAT DE-ICE TUBE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SLAT TELESCOPIC DUCT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000552003101500055EA 2003 10 15 ASOA03415 120030904A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11880AS 7606 DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52-00. (M) 2L72 4F RTA21EA 20031015000592003101500059NM 2003 10 15 USAASB03160 120030906A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 CLT - MAINTENANCE REPORTED THE AFT RIGHT CABIN EMERGENCY LIGHTS EXTINGUISHED PREMATURELY DURING OPS TEST OF EMERGENCY LIGHT SYSTEM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M1137 PER MM 33-51-51. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031020001522003102000152NM 2003 10 20 DL777030803 120030902A33500201804001 LENS BOEING777 777232 1385232NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27862DA 29734 SEAT MOUNTED ESCAPE PATH LIGHTING LEN(S) MISSING AT SEATS 52G & 32G RESPECTIVELY (2 WHITE). REPLACED MISSING LIGHT LENS AT SEATS 52G & 32G. LIGHTS OPS CHECK OK. 2L72 4F RTT00001SE 20031020001692003102000169NE 2003 10 20 DLM90030795 220030830A7250V2528D5 ENGINE DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 1 FIRE A DALAK NONE A FLAME/FIRE TXTAXI/GRND HDL 1 SO27914DN21511 020024 53394 020024 RAMP AND FLEET SERVICE REPORT NR 1 ENG TAIL PIPE FIRE ON SHUTDOWN. REF ERA087224-14 NO COKING FOUND IN NR 5 BEARING SCAV TUBE ENG, LEAK AND OPS NORM PER PFHB. 2L72 4F4 FRTA6WE E40NE 20031020001842003102000184NM 2003 10 20 DL757030814 120030905A3040012N87716 ANTI-ICE SYSTEM BOEING757 757232 1384965NM COCKPIT MALFUNCTIONED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27677DL 25982 AT APPROX 1000 FT ABOVE YVR RIGHT SIDE WINDOW HEAT WENT INOP, HEARD ARCING AND SMELLED ELECTRICAL SMELL. MTC IN YVR DEACTIVATED R2 WINDOW HEAT PER MEL 30-41-01B. C/B PULLED AND COLLARED. 2L72 4F RTA2NM 20031020001882003102000188SO 2003 10 20 C2XA03SH372 120031007A711014576631622 STIFFENER EMB 135 EMB135ER 3260203SO NR 2 COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 SHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031020002182003102000218WP 2003 10 20 UPS03841366 120030924A53203755843U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 STATION 1184 BATHTUB FITTING IS CRACKED BETWEEN LONG 35R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20031020002582003102000258EA 2003 10 20 03282669 120031009A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002712003102000271NM 2003 10 20 03263425 120030920A32607144003 PSEU DORNERDO32 DO328300 NM LANDING GEAR FAULTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27425FJ 3189 DURING CLIMB THE CREW NOTED A PROXY FAIL AND NLG WOW CAS MESSAGE. EMERGENCY WAS DECLARED AS A PRECAUTION AND AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE PSEU PROXIMITY BOX. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031020002732003102000273EU 2003 10 20 03262330 120030919A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27330UE 41098 DURING INSPECTION THE LT EXT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL FOUND A LOOSE WIRE ON THE EMERGENCY LIGHT HOUSING AND TIGHTENED WIRE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031020002782003102000278EA 2003 10 20 03268671 120030925A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27671BR 7572 DURING INSPECTION THE AFT CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002852003102000285NM 2003 10 20 VNAA0309014 120030921A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DISCHARGED A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07429JS167921030 3043 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 6 AND 9 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031020003032003102000303NM 2003 10 20 2003UALA00729 120030930A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29307UA 23668 AFT SECTION OF EMERGENCY EEL LIGHT SYSTEM IS INOP. REPLACED AFT SECTION OF RIBBON & AFT EEL GALLEY LIGHT. 2L72 4F4 FRTA16WE E2GL 20031020003062003102000306NM 2003 10 20 2003UALA00732 120031001A5230 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 AFT BULK CARGO DOOR SKIN BETWEEN STR 26L AND 27L DOOR SKIN DENTED 3 INCHES FROM EDGE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA1NM E24NE 20031020003092003102000309NM 2003 10 20 2003UALA00700 120030919A5420 STIFFENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 3 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29180UA 25224 NR 3 PYLON AFT BULKHEAD STIFFENER CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STIFFENER. 2L74 4F4 FRTA20WE E24NE 20031020001712003102000171NE 2003 10 20 DL75K030806 220030902A7200 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 BIRD STRIKE A DALAK NONE E VIBRATION/BUFFET TOTAKEOFF 1 SO276705Y 30397 716383 DURING T/O ROLL IN PBI SUSTAINED BIRD STRIKE. SUSPECT INJECTION BY RIGHT ENGINE. AUDIBLE NOISE DIFFERENCE ON RIGHT ENGINE. VIB MONITOR N, 1.0 IN CLIMB ON RIGHT ENGINE. PERFORMED BIRD STRIKE INSPECTION AND REPLACED BLADES AS NECESSARY. 2L72 4F4 FRTA2NM E17NE 20031020002442003102000244NM 2003 10 20 DL76S030823 120030908A335020131A BATTERY PACK BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27126DL 24076 ON LAYOVER FOUND LT OVERHEAD EMERGENCY LIGHT OUT. REPLACED BATTERY PACK. 2L72 4F RTA1NM 20031020002772003102000277EA 2003 10 20 03268628 120030925A324450105711 TIRE CNDAIRCL600 CL6002B19 1900309EA MLG SEPARATED A VTZAO OTHER O OTHER LDLANDING 1 EA27628BR 7240 DURING LANDING THE NR 3 MAIN TIRE HAD TREAD SEPARATION. NO EMERGENCY DECLARED AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT PASSENGERS WERE DEPLANED NORMALLY. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 3 MAIN TIRE. 2L72 4F RTA21EA 20031021000312003102100031NE 2003 10 21 USAABA03034 220030917A75306764B040000 REGULATOR VALVE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT ENGINE MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19670UW16712 0315 PHL - FLT 894 - EN ROUTE PHL-FRA, THE CREW RECEIVED THE ECAM WARNING 'AIR ENG 2 BLEED FAULT.' DUE TO PARTS AVAILABILITY IN FRA AND IMPENDING WEATHER FROM HURRICANE ISABEL, THE DECISION WAS MADE TO RETURN TO PHL. THE FLIGHT LANDED WITHOUR FURTHER INCIDENT. MAINTENANCE REPLACED THE PRV. (M) 2L72 4F4 FRTA46NM 20031021000452003102100045EU 2003 10 21 USAASA03114 120030919A2611CDGU2000000 SMOKE DETECTOR AIRBUSA319 A319112 3930323EU E/E BAY FAULTY A USAAK NONE N FALSE WARNING CRCRUISE 1 EA19756US 1340 LGA - FLT 2127 - EN ROUTE BOS-LGA, CREW RECEIVED 'AVNCS SMOKE' ECAM MESSAGE DURING FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS COMPARTMENT SMOKE DETECTOR. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031021000602003102100060EA 2003 10 21 A6WA200340138 120030910A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31432AW 7257 STRONG BURNING SULFUR ODOR IN FLIGHT. COMPLIED WITH PACK BURN OUT PROCEDURE. NO SMELLS OR DEFECTS NOTED AT THIS TIME. INSPECTED AVIONICS AND APU BAY, NO DEFECTS NOTED. AIRCRAFT OK FOR CONTINUED SERVICE. (M) 2L72 4F RTA21EA 20031021000712003102100071 2003 10 21 REXA03005 420030923A22108220044001 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A REXAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO258694A 7694 ON FINAL APPROACH, A LARGE POPPING NOISE CAME FROM THE FCP PANEL. SHORTLY AFTER IT STARTED TO VENT SMOKE BETWEEN NAV AND ALT BUTTON. CREW DECLARED EMERGENCY, FOLLOWED QRH PROCEDURES, LANDED NO FURTHER INCIDENT. REMOVED AND REPLACED FCP IAW AMM 22-11-07. COMPLIED WITH ALL FUNCTIONAL CHECKS IAW 22-11-07, OPS CHECK GOOD. OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030910000082003091000008EU 2003 9 10 I05R088840 120030812A33006485000 LIGHT SNIAS 350 AS350* EU ANTI COLLISION INOPERATIVE E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 500 3560 ANTI COLLISION LIGHT INOPERATIVE REPLACED ANTICOLLISION LIGHT WITH S/N 553 OUT OF AIRFLITE STOCK ORDERED NEW PART FOR AIRFLITE STOCK UNDER WARRANTY. 1G71 3U H9EU 20030910000112003091000011EU 2003 9 10 BAQA088161 120030721A282157188 FUEL FILTER AEROSPAS365 AS365N2 8680815EU WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 MECHANIC ADVISED IT NEEDED CHANGED, DUE TO A LOT OF WEAR TO IT. MECHANIC SCRAPPED AT SITE. 1G72 3U RTH10EU 20030910000172003091000017WP 2003 9 10 DHL2003604548 120030526A5730BIT0109917 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED AT XRS 436.000. REMOVED AND REPLACED UPPER PANEL ON LT WING T/E AT XRS 436.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030910000262003091000026EU 2003 9 10 HE66088176 120030703A63204649005005 SEAL UROCOPEC135 EC135T1 5620026EU GEARBOX LEAKING B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03135CR980 0164 LEAKING HYDRAULIC DRIVE SEAL NOT ALLOWED TO CHANGE SEAL, MUST CHANGE ENTIRE GEARBOX. 1G72 3U H88EU 20030910000352003091000035WP 2003 9 10 ABXA030322 120030804A275257726925011 ACTUATOR DOUG DC8 DC863 302198AWP T/E FLAP BROKEN A ABXAK NONE F FLT CONT AFFECTED APAPPROACH 1 GL23817AX5910 45928 DURING FLAP EXTENTION ON FINAL APPROACH AT APPROXIMATELY 5 DEGREES FLAPS, THE RIGHT AND LEFT FLAP INDICATORS SPLIT APPROXIMATELY 5-8 DEGREES WITH AN AIRCRAFT ROLL. FURTHER EXTENTION, EVENED OUT. FOUND LEFT MID WING FLAP ACTUATOR AND LINK BROKEN. REPLACED FLAP ACTUATOR IAW DC8 MM 27-51-09-4-0001. 2L74 4F 4A25 20030910000522003091000052WP 2003 9 10 DHL2003604545 120030519A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL 46047 FWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL 1.000 AT L-31L, STA 70.000. STOP DRILLED CRACK AT L-31L, STA 70.000 AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000552003091000055SW 2003 9 10 HEEA088922 120030821A6220206011149105 YOKE BELL 206 206L3 1182108SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 BEARING JOURNAL WAS FOUND TO HAVE MISHANDLING MARKS AND PITTED AS MARKED ON YOKE. 1G71 3U H2SW 20030910000622003091000062NM 2003 9 10 DHL2003741007 120030827A3260 SWITCH BOEING727 7272Q9 138448MNM RT MLG DIRTY A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01741DH 21931 THE RIGHT MAIN GEAR DOOR WENT DOWN WITH GEAR HANDLE ON THE OFF POSITION. ABNORMAL PROCEDURE COMPLETED, THE DOOR WENT BACK UP WITH HANDLE ON UP POSITION. TROUBLESHOT RIGHT MAIN LANDING GEAR DOOR IAW M/M 32-61-01. CLEANED DOOR SWITCH IAW WPM 20-60-01. TESTED INDICATION AND WARNING IAW M/M 32-61-01. SYSTEM OPS CHECKED GOOD. OK TO CONTINUE. 2L73 4F RTA3WE 20030910000692003091000069WP 2003 9 10 DHL2003604793 120030624A5347S4889185 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA -55.000 - STA 310.000. REMOVED NR 2 TRACK WITH WORN LUGS IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW NR 2 TRACK ON MAIN CARGO COMPT STA -55.000 - STA 310.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030910000842003091000084WP 2003 9 10 DHL2003604567 120030529A5240 SKIN DOUG DC8 DC873F 302199FWP SERVICE DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD SERVICE DOOR UPPER AFT PART INNER SKIN CRACKED 1.000. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 52-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000852003091000085WP 2003 9 10 DHL2003604561 120030513A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CENTER L/E FORMER CRACKED 0.500 AT XFS 366.500. STOP DRILLED CRACK AT XFS 366.500 AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031027001342003102700134NM 2003 10 27 03029 120030926A2612 WARNING LIGHT BOEING747 747123 1384873NM PWA JT9 JT9D* NE NR 4 ENGINE ILLUMINATED A KCSAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23673UP 20325 662590 NR 4 ENGINE FIRE, AFTER SETTING CLIMB THRUST, NR 4 ENGINE FIRE LIGHT LIT AND BELL SOUNDED. CONFIRMED BOTH NR 4 NACELLE TEMP. INDICATORS PEGGED OUT HIGH. ACCOMPLISHED ENGINE FIRE SEVERE DAMAGE CHECKLIST WITH FIRE INDICATION OUT AFTER ONE BOTTLE. APPROXIMATELY 5 MIN. LATER FIRE LIGHT AND BELL SOUNDED AGAIN; DISCHARGED SECOND BOTTLE AND RETURNED TO OBBI. 2L74 4F4 F A20WE E20EA 20031028000542003102800054WP 2003 10 28 NACA20030112 120030916A2612N88A92 FIRE WARNING DOUG DC6 DC6A 3021706WP PWA R2800 R2800* 52026NE TAIL HEATER FALSE ACTIVATIONA NACAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 AL03993304733 4733 43576 TAIL HEATER FIRE WARNING INTERMITTENTLY CAME ON AFTER HEATER CHECK. GROUND OPS CHECKED ANTI-ICE HEATER SYSTEM PER NAC DC-6 OPS MANUAL CH.14-20 SECT. C, CHECKED GOOD. INSPECTED HEATER FOR VISUAL DISTRESS, NONE NOTED. 2L74 4R4 R 6A3 5E8 20031029000022003102900002NM 2003 10 29 ASAA0340101 120030301A531065C32395 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSON ON SHEAR TIE BS 727F LBL 4 AND WL 158. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000332003102900033EU 2003 10 29 USAASA03118 120030925A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19755US 1331 DCA - THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT WAS FOUND INOPERATIVE DURING TESTING. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031023000282003102300028NM 2003 10 23 UPS03441250 120030907A532065B38600208 CLIP BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D, BS 820 STR 6L FRAME ATT TIE CLIP CRACKED. M/D BS 820 STR 6L FRAME ATT TIE CLIP REPLACED AS PER SRM 51-10-01 P.8. 2L74 4F4 F A20WE E20EA 20031023000332003102300033NM 2003 10 23 UPS03441257 120030907A53107075T60063IN SHEAR TIE BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, AFT CARGO COMPT- BELOW FLOOR SUPPORT FRAME LOWER SHEAR TIE PLATE FOUND CRACKED AT STA 1880 LT SIDE STR 44 LT. SHEAR TIE REPAIRED IAW SRM 53-10-04, FIG 41 AT AFT CARGO COMPT STA 1880, BETWEEN S44L. 2L74 4F4 F A20WE E20EA 20031023000382003102300038NM 2003 10 23 AWXA200301086 120030922A3397BMS13311122 WIRE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE SEAT ROW 13 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2EA 20031023000502003102300050 2003 10 23 SWIA200312440 420030919A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE STALL WARNING MALFUNCTIONED A SWIAO OTHER PF NO WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07936SW 7726 STALL TEST FAILED. INSTALLED SERVICEABLE STALL PROTECTION COMPUTER IAW MM 27-34-00. PN: 3995100208 SN OFF: 955 2L72 4F4 FRTA21EA E15NE 20031023000662003102300066SO 2003 10 23 C2XA03SH350 120030924A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 DURING C CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031023000772003102300077NM 2003 10 23 P5CA0300951 120030923A272169050008 CONTROL QUADRANT BOEING747 7472U3B 1384846NM PWA JT9 JT9D* NE RUDDER FAULTY A P5CAO OTHER J WARNING INDICATION CLCLIMB 1 WP23923FT 22769 RUDDER RADIO LIGHT CAME ON WHEN FLAPS MOVING 5 TO 1 AT 220KNTS. REMOVED AND REPLACED RUDDER UPPER CONTROL IAW 27-21-13 LEAK CHECK GOOD. 2L74 4F4 FRTA20WE E20EA 20031023000802003102300080NM 2003 10 23 P5CA0300954 120030924A7714 ENGINE BOEING747 747430 1384942NM GE CF6 CF650E2 30018NE NR 1 MALFUNCTIONED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23354MC 23394 517365 ON START UP NO (N1) INDICATION ON NR 1 ENG RESET C/13 NO HELP. DEFERRED NR 1 ENG (N1) IAW MEL 77-1-2. 2L74 4F4 FRTA20WE E23EA 20031027000022003102700002NM 2003 10 27 DHL2003782011 120030925A3260 WARNING LIGHT BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE MLG FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01769AT 21998 IN FLIGHT, RED LT GEAR ANNUNCIATOR ILLUMINATED. HYDRAULIC SYSTEM (A) NORMAL AND NO INDICATION ON S/O'S ANNUNCIATOR PANEL. AFTER 5 MINUTES THE RED LEFT GEAR ANNUNCIATOR LIGHT EXTINGUISHED. ALL INDICATIONS NORMAL. PERFORMED OPERATIONAL CHECK OF LANDING GEAR ON GROUND IAW B727 MM 32-61-01. NO DEFECTS NOTED ON GROUND. 2L73 4F4 F A3WE E2EA 20031027000182003102700018EA 2003 10 27 COMA0360428 120030924A335059465 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DEFECTIVE A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01710CA 7241 FLIGHT 5601 DURING INSPECTION FOUND THE FLOOR EMERGENCY LIGHTING INOPERATIVE AT ROWS 8 THROUGH 13. REPLACED SECTION OF THE FLOOR EMERGENCY LIGHTING STRIP. 2L72 4F4 FRTA21EA E15NE 20031027000212003102700021EU 2003 10 27 AWXA200301097 120030913A5315D5347219320000 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON Y765 FLOORBEAM FR 67-69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y765 FLOOR BEAM FROM FR 67 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PARTS IAW A320 SRM 51-49-00, PG. 5-6, TABLE 1. 2L72 4F4 FRTA28NM E311NE 20031027000232003102700023EU 2003 10 27 AWXA200301099 120030913A5347D5347209800000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON LT DUMMY RAIL AFT OF FR 66 AT FLIGHT ATTENDANT SEAT ATTACH HOLE. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED LT DUMMY RAIL AFT OF FR 66; RECEIVED NEW REPLACEMENT DUMMY RAIL; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, PG. 35-36, 39-41, FIG. 18. 2L72 4F RTA28NM 20031027000242003102700024EU 2003 10 27 AWXA200301100 120030913A5315D5347219220000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON MAIN CABIN FLOORBEAM Y765 BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED MAIN CABIN FLOORBEAM Y765 BETWEEN FR 67 AND FR 68; RECEIVED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, PG. 28, 39-40, FIG. 12. 2L72 4F RTA28NM 20031027000262003102700026EU 2003 10 27 AWXA200301102 120030913A5315D5347207500100 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON MAIN CABIN FLOORBEAM Y1732 BETWEEN FR 65 AND FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED MAIN CABIN FLOORBEAM Y1732 BETWEEN FR 65 AND FR 66; RECEIVED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, PG. 8-28, 39-41, FIG. 18. 2L72 4F RTA28NM 20031027000352003102700035 2003 10 27 219PA0009 420030918A2210 COMPUTER BOEING737 737222 1384473NM AUTOPILOT MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05219PA 19956 AUTO PILOT AILERON WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED NORMAL PER MM 22-11-0. 2L72 4F A16WE 20031027000372003102700037NM 2003 10 27 CALA0300556 120030925A5320 PAN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE LAVATORY FLOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND CORROSION ON LT AFT LAV FLOOR PAN AT DUMP CHUTE, STA 1006, LBL 10. A NEW LAV PAN WAS INSTALLED IAW SRM 51-20-07 AND 51-10-02. 2L72 4F4 FRTA16WE E2GL 20031021002282003102100228 2003 10 21 C2XA03TY164 420030919A31309804700042 FLIGHT RECORDER EMB 145 EMB145XR SO COCKPIT FAULTY A C2XAAF UNSCHED LANDING ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27111211751 1751 145683 THE CREW RECIEVED A BAGGAGE SMOKE INDICATION AT FL270, THE FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT DIVERTED TO ATL. THE AIRCRAFT WAS INSPECTED AND DEEMED SAFE FOR A FERRY FLIGHT TO TYS. MAINTENANCE FOUND THE SSDFDR TO BE FAULTY AND WAS REPLACED IAW EMB M.M. 31-31-01, ALL OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB M.M. 31-31-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RT 20031021002312003102100231SO 2003 10 21 C2XA03SH333 120030920A532014521721009 STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 SHV-DURING C CHECK THE FORWARD DIGITAL STRAP BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031021002392003102100239SO 2003 10 21 C2XA03SH336 120030920A532014522460015 STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 SHV-DURING C CHECK THE AFT DIGITAL STRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01079. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031021002822003102100282NM 2003 10 21 CALA0300540 120030919A5330 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND FUSELAGE SKIN WORN TO BARE METAL BELOW FORWARD END OF DORSAL FIN AT STA 867-907. THE WORN AREA OF SKIN WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 201. 2L72 4F4 FRTA16WE E2GL 20031022000152003102200015NM 2003 10 22 C1HA200395069 120030919A3260 UPLOCK BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE MLG WORN A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15295AS 22147 DURING TAKEOFF ROLL RED DOORS LIGHT ON FORWARD PANEL ILLUMINATED, LT GEAR DOOR LIGHT (AMBER) ON ENGINEERS PANEL ILLUMINATED TAKE OFF WAS ABORTED AT 80 KTS. VERY LIGHT BRAKING WAS USED WITH 9000 FEET OF RUNWAY REMAINING FOUND LT MLG UPLOCK ASSY HAD 2 BOLTS WITH EXCESSIVE WEAR IN SHAFT. REMOVED AND REPLACED LT MLG UPLOCK ASSY IAW MM 32-32-51, JACKED A/C IAW MM 07-11-00. PERFORMED GEARSWING. GEAR TESTED NORMAL. ALSO PERFORMED MANUAL EXTENSION ALL GOOD IAW MM 32-32-51. 2L73 4F4 F A3WE E2EA 20031022000462003102200046SO 2003 10 22 SWIA200312428 120030920A27503471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07296SW7986 6389 120325 FLAP'S FAULT COULD NOT BE CLEARED (IT WOULDN'T GO TO ''M'' MODE). REPLACED FLAP ANNUNICIATOR. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031022001002003102200100CE 2003 10 22 BSY2003F00024 120030903A61239696001175 TUBE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YF2 GL PROP GOV BROKEN E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL07140S TH1155 299231R ED4588B LEFT ENGINE LOST OIL PRESSURE, PILOT FEATHERED ENGINE AND SHUT IT DOWN. FOUND UNFEATHERING LINE BROKEN AT FLAIR AT PROP GOV. REMOVED AND REPLACE LINE. OPS CHECKS GOOD. SERVICES WITH OIL GROUND RAN FOR 1 HR. REMOVED FILTER NOTHING FOUND IN FILTER. OK FOR SERVICE. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20031022001152003102200115NM 2003 10 22 F3LA200300143 120030923A5320 SUPPORT BOEING737 73736E 138443ANM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RT. ZEE SUPPORT IN AFT CARGO COMPARTMENT FROM STA. 767 TO STA. 797.2. REPLACED ZEE SUPPORT IAW SRM 51-40-02, 53-60-53 AND DRAWING 69-43477. 2L72 4F4 FRTA16WE E2GL 20031022001482003102200148EA 2003 10 22 SWIA200312433 120030922A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 FS 484 RT INTERCOSTAL IB ANGLE RBL 27 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION). ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV ''A''. 2L72 4F4 FRTA21EA E15NE 20031023000272003102300027NM 2003 10 23 UPS03441249 120030907A532065B386001034 CLIP BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, AFT CARGO COMPT. RT STA 1780 STR STR 35 TIE CLIP FOUND CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 PG8. 2L74 4F4 F A20WE E20EA 20031023000292003102300029NM 2003 10 23 UPS03441253 120030906A531065B04406730 DOOR FRAME BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE ESCAPE DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D, RT NR 4 DOOR FORWARD FRAME MOST UPPER DOOR FITTING AREA FOUND CRACK. FORWARD FRAME CRACKED AREA REPAIRED IAW RS NR R52-11-35065 AND UPS AUTH NR 747-52-20006. 2L74 4F4 F A20WE E20EA 20031023000302003102300030NM 2003 10 23 UPS03441254 120030915A5320BACR15BB6D7C WEB BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, BS 1480 STR 41 RT ATT WEB FOUND CRACKED (BODY FAIRING LOCATIONS) DAMAGED SECTION TRIMMED OUT AND PERFORMED EXT PATCH REPAIRED IAW SRM 51-40-02 FIG 1. 2L74 4F4 F A20WE E20EA 20031023000422003102300042EU 2003 10 23 AWXA200301090 120030913A5320D5348002069701 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK A 1 INCH CRACK WAS FOUND ON FLOOR SHEAR PLATE BETWEEN FR 68-69, AT LBL 49. MAINTENANCE REMOVED CRACKED SHEAR PLATE FR 68-69, LBL 49; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW 51-44-11, PG. 3-10, 12, AND A24-A25, FIG. 2, 3, 61 & 62. 2L72 4F RTA28NM 20031021000782003102100078SO 2003 10 21 SIMA200324607 120030815A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21716AE 145264 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL IAW EMB SRM, SRM EMB-145/1142 REV 22, CHAPTERST 51-40-02, 51-20-01, 51-20-03, 51-40-06 AND AMERICAN EAGLE AIRLINES INC ETN NR EB-51-009. (M) 2L72 4F RTT00011AT 20031021000952003102100095SO 2003 10 21 SIMA200324609 120030819A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21818AE 145561 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142, REV 22, CHAPTER 53-21-10, FIG 201 SHEET 1, CPM 51-61-00 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031021001102003102100110NM 2003 10 21 USAASB03166 120030913A2120 ODOR BOEING737 737401 1384701NM COCKPIT DETECTED A USAAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19417US 23984 ORF - FLT 1162 - DURING CRUISE, EN ROUTE PHL TO ORF, REPORTED AN ODOR OF BURNING ELEC WIRES OR ELEC COMPONENTS. ODOR WAS STRONGEST ON CAPT'S SIDE OF FLT DECK. NO SMOKE AND ODOR WAS NOT IN CABIN. CREW PUT ON MASKS FOR ABOUT 3-4 MIN. A COUPLE OF MINS LATER, ODOR BEGAN TO DISSIPATE AND THE SMELL RANGED FROM CHEMICAL TO ELECTRICAL TO PLASTIC. SOURCE COULD NOT BE DETERMINED. FLT LANDED IN ORF WITHOUT INCIDENT. DURING THE TIME OF THE ODOR, FLT ATTENDANT REPORTED A PAX IN THE FWD LAV. MX CHECKED BOTH SIDES OF CB PNLS FOR TRIPPED OR BURNED CB`S. CHECKED INSTRUMENT PNL, OVERHEAD PNL AND CONSOLE. CHCKD RECIRC FANS AND EQUIP COOLING FANS FOR PROPER OPS. ALL CHK NORMAL. COULD NOT FIND SOURCE OF ELECTRICAL ODOR. (M) 2L72 4F RTA16WE 20031021001132003102100113 2003 10 21 USAASA03116 420030921A2565 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19746UW 1297 BOS - THE AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031021001182003102100118WP 2003 10 21 GTIA030710 120030904A5320 CLIP DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND FORWARD PIT FS 237 INTERCOSTAL CLIP CRACKED STRINGER 27R. REMOVED INTERCOSTAL CLIP. FABRICATED NEW INTERCOSTAL CLIP. INSTALLED NEW FORWARD PIT INTERCOSTAL CLIP. (M) 2L72 4F A6WE 20031021001332003102100133NM 2003 10 21 AALA20031023 120030918A3350D71702001 CHARGER BOEING777 777223 1385213NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21757AN 32636 MIA - DURNG OVERNIGHT MAINTENANCE, EMERGNCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT THE FIRST CLASS GALLEY EXIT SIGN LOCATION. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20031021001522003102100152NM 2003 10 21 AALA20030562 120030403A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21645AA 24603 MIA - DURING OVERNIGHT MAINTENANCE, LEFT SIDE PASSENGER FORWARD DOOR SLIDE LIGHT INOPERATIVE. REPLACED LEFT SIDE PASSENGER FORWARD DOOR SLIDE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002082003102100208NM 2003 10 21 AALA20031024 120030918A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21672AA 25337 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROWS 24 THROUGH 34. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002152003102100215NM 2003 10 21 AALA20030953 120030903A33503015643 LIGHT BOEING767 767323 1385205NM EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21348AN 33087 SFO - FLT 1994 - EMERGENCY EXIT LIGHTS INOPERATIVE AT LEFT FUSELAGE. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031021002262003102100226SO 2003 10 21 SIMA200325307 120030908A27103631101005 SELECTOR EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A SIMAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 SW21628AE 145124 EVV - FLT 4010 - DURING APPROACH CREW REPORTED A FLAP FAIL MESSAGE. AFTER SELECTING FLAPS TO 45 DEGREES FLAPS STUCK AT 38 DEGREES EVEN WITH FLAP HANDLE AT 0 DEGREES. PERFORMED GO AROUND DURING WHICH AIRSPEED INCREASED TO APPROX 180KTS. PERFORMED FLAP FAIL PROCEDURE AS PER AOM AND LANDED UNEVENTFULLY. MAINTENANCE COMPLIED WITH AN EXCEEDING FLAP/DOWN SPEED CONDITION INSPECTION AND FLAP MECHANICAL LINE GENERAL VISUAL INSPECTION WITH NO DEFECTS NOTED. THE FLAP SELECTOR LEVER WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CEHCK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031021002442003102100244SO 2003 10 21 C2XA03SH339 120030921A531514521700003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK THE LT FLOORBEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031021002492003102100249WP 2003 10 21 GTIA030697 120030903A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND RIGHT INBOARD SEAT TRACK NUMEROUS AREAS OF CORROSION, GOUGES AND BARE METAL FROM STATION 210-207. (M) 2L72 4F A6WE 20031021002532003102100253SO 2003 10 21 C2XA03SH342 120030922A532014521725013 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK THE RT SILL BETWEEN FRAMES 19 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031021002602003102100260WP 2003 10 21 03FDEA01595 120030919A3610 CONTROLLER DOUG DC10 DC1030 3023501WP PNEUMATIC SYS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25317FE 46835 APPROXIMATELY 2.45 HRS INTO FLIGHT, LEVEL AT 33,000 FT EXPERIENCED NR 3 MANIFOLD FAILURE LIGHT. ACCOMPLISHED RED TABS LIGHT WENT OUT. DIVERTED TO INDY. REMAINDER OF FLIGHT UNEVENTFUL. REMOVED AND REPLACED MANIFOLD FAIL CONTROLLER PER DC-10 M/M 36-23-01-2, NO DEFECTS NOTED. PREMATURE REMOVAL/INSTALLATION OFF MFG 35008-2, POS ONL SRL B214, TAG 940710, ON MFG 35008-2 SRL B306, TAG 495125. 2L73 4F A22WE 20031021002612003102100261NM 2003 10 21 03FDEA01594 120030919A2613 ELEMENT BOEING727 727200 138407ENM AFT AIRSTAIR GROUNDED A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 SO25285FE 22622 LOWER AFT BODY HEAT LIGHT ILLUMINATED, FOLLOWED RED TAB PROCEDURES AND LIGHT EXTINGUISHED. LIGHT ILLUMINATED DURING CLIMB EPR AT 205. PER RED TAB ISOLATION PRODEDURE FAULT OCCURRED IN NR 3 ENG - RH PACK PNEU DUCTING. INSPECTED AFT AIRSTAIR AREA O/H LOOP AND FOUND LOOP TOUCHING IN TWO PLACES. REPOSITIONED AS NECESSARY. RAN ENGINE TO 2.00 EPR AND FAULT DID NOT RE-OCCUR. FOR PRECAUTION CHECKED INTEGRITY AND OPERATION OF RH PNEU SYSTEM PER JRH 7- 19. CKS OK. CHECKED AFT CARGO COMPT AND KEEL BEAM AREA FOR WARM AREA'S CKS OK. DUCT PNEUMATIC PRESS ALL CKS OK. PERFORMED TROUBLESHOOTING CK PER MM 26-14- 000-1 AND OPS CK AS PER MM 26-14-000-5. CKS NORMAL. 2L73 4F RTA3WE 20031021002632003102100263NM 2003 10 21 03FDEA01592 120030919A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 AFT FRAME DOOR CUTOUT, AFT FRAME CRACKED, LOWER CORNER, BS 990, RBL 26. 2L73 4F RTA3WE 20031021002682003102100268NM 2003 10 21 03FDEA01579 120030918A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 LWR SURFACE, FWD SIDE OF TOP FLANGE OF FLOOR BEAM BS 440, LBL 35, WL 208 HAS TOOLING DAMAGE. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 20031021002702003102100270NM 2003 10 21 03FDEA01576 120030918A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 FUSELAGE SKIN EXTERNAL REPAIR DOUBLER HAS CHAFE DAMAGE, BS 720D 10 INCHES AT STR 19L. FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 5. 2L73 4F RTA3WE 20031021002722003102100272NM 2003 10 21 03FDEA01574 120030918A532065233312 STRINGER CLIP BOEING727 727200 138407ENM 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 BS 440, STR 7 LT STR CLIP CRACKED. REMOVED DAMAGED STR CLIP AT BS 440 STR 7L DRILLED NEW STR CLIP AND INSTALLED IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20031021002912003102100291NM 2003 10 21 CALA0300549 120030921A5312 STIFFENER BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED BELOW FLOOR ON LEFT HAND SIDE AT BL 0. REPAIRED STIFFENER IAW SRM 53-80-08 AND DRAWING PL NR 65C28106. 2L72 4F4 FRTA16WE E2GL 20031021003042003102100304NM 2003 10 21 MWEA030380 120030922A5347593056675 SEAT TRACK DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 AFT CABIN NR 3 SEAT TRACK HAS CORROSION FROM STATION 1250-1283. BLENDED CORROSION, REMOVED AND REPLACED SEAT TRACK. 2L72 4F4 FRTA6WE E2EA 20031022000022003102200002NM 2003 10 22 MWEA030382 120030922A5347593054770 SEAT TRACK DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 HEAVY CORROSION ON SEAT TRACK NR 6 AT FRAME STATION 788. REMOVED CORROSION, REMOVED AND REPLACED SEAT TRACK. 2L72 4F4 FRTA6WE E2EA 20031022000052003102200005NM 2003 10 22 MWEA030385 120030922A32304920206503 BOLT DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE MLG CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 NOSE LANDING GEAR DRAG LINK KNEE HINE BOLT IS CORRODED. REMOVED AND REPLACED KNEE HINE. 2L72 4F4 FRTA6WE E2EA 20031022000082003102200008NM 2003 10 22 QXEA200301169 120030918A6120782490A50 PCU DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 SURGES A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09357PH4725 504 AFTER ROTATION NR 2 ENGINE STARTED TO SURGE. PROP RPM'S WERE AROUND 960 TORQUE FLUCTUATED + OR - 30 PERCENT. STARTED TO RUN THE ENGINE FAILURE CHECKLIST. RETURNED TO FIELD UNEVENTFULLY. REMOVED AND REPLACED NR 2 PROPELLER CONTROL UNIT. NO SURGES NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031022000442003102200044 2003 10 22 SWIA200312426 420030918A22106226190204 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE AUTOPILOT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07215SW6215 4547 120281 CAPTAINS AUTOPILOT PITCH IS ERRATIC IN LEVEL FLIGHT PITCH CHANGED +/- 2 DEGREES. REPLACED CAPT AHC 85. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031022000612003102200061NM 2003 10 22 QXEA200301162 120030916A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 LOWER FORWARD FUSELAGE SKIN IS NICKED AT RIGHT STRINGER 31, 9 INCHES FORWARD OF X19.7. REPAIRED IAW Q400 SRM 51-26-10, 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801 AND RD 8/4-53-666. 2H72 4T4 TRTA13NM E00062EN 20031022000672003102200067SO 2003 10 22 C2XA03IA097 120030917A335066368 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713978 145180 THE CREW NOTED DURING PREFLIGHT THE EMERGENCY FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. BNA- MAINTENANCE PLACED FLOOR LIGHTING ON DMIDO TO PARTS NOT IN STOCK.THE AIRCRAFT WAS RETURNED TO SERVICE. IAH- MAINTENANCE REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE AFTER THE DMI WAS CLEARED. 2L72 4T4 FRTT00011ATTE6CH 20031022000742003102200074NM 2003 10 22 03FDEA01547 120030916A5320A5A7114519 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 POSSIBLE CRACK AT LONGERON SPLICE AT TRANSVERSE SPLICE STA 1540 RT TUNNEL. CTR CARGO STA 1540 LONG 37R CRACK LONGERON SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG N5A6774 AND SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20031022000822003102200082 2003 10 22 UPS03141375 420031008A2565 WARNING SYSTEM AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01124UP 0808 WHEN TRYING TO ARM THE ESCAPE SLIDE HAD TO CYCLE THE ARMING LEVER 2 OR 3 TIMES IN ORDER TO GET THE SLIDE ARMED INDICATION ON THE ECAMS. SYSTEM TEST OK PER 52-73-14-4. THIS CLEARS M267914. 2L72 4F RTA35EU 20031022000882003102200088NM 2003 10 22 UIE2003F00001 120031001A2780 WARNING SYSTEM BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE TE FLAPS MALFUNCTIONED A UIEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA15524MC 21784 DURING TAKEOFF AT APPROXIMATELY 75 KNOTS, PILOTS LEADING EDGE FLAP INDICATED UNSAFE WITH F/E LT WING PANEL LEADING EDGE FLAP INDICATORS ALSO INDICATING UNSAFE. NO WARNING HORN WAS HEARD AT ANY TIME DURING TAKEOFF. VISUALLY AND MANUALLY CHECKED ALL LEFT WING PDU`S AND CONNECTORS. OPERATIONALLY CHECKED FLAPS IN PRIMARY AND ALTERNATE MODES IAW MM 27-81-03. ALL INDICATIONS AND FUNCTIONS NORMAL. 2L74 4F4 FRTA20WE E23EA 20031022000892003102200089NM 2003 10 22 03FDEA01739 120031015A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25493FE 21531 CORROSION (C53-113-01(2) ON EXTERNAL SKIN BS 1054 AT STR 28L. COMING CUT OUT & REMOVED DAMAGED SKIN B/S 1054. FABRICATED & INSTALLED REPAIR IAW SRM 53- 30-3 FIG 3. (STR 28L). 2L73 4F RTA3WE 20031022001102003102200110EU 2003 10 22 XNOA01155 120030920A8011 STARTER AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE FAILED A XN0AO OTHER L NO TEST TXTAXI/GRND HDL 1 GL23371PC 157 517443 NR 1 ENGINE NO N-2 DURING START, NO ENG ROTATION, START VALVE OPEN. REMOVED AND REPLACED NR 1 ENG STARTER, GROUND CHECK OK IAW A300 AMM 80-13-01. STATUS: (SUPP/CLOSED) 2L72 4F4 FRTA35EU E23EA 20031021002112003102100211SO 2003 10 21 SIMA200324610 120030821A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21818AE 145561 ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED TWO REPAIR DOUBLERS, FOUR SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2777. (M) 2L72 4F RTT00011AT 20031021002132003102100213SO 2003 10 21 SIMA200324402 120030828A49304504205D FADEC EMB 145 EMB145LR 3260212SO APU MALFUNCTIONED A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21615AE 145087 MQT - FLT 4331 - DURING APU START THE APU HUNG AT 25 PERCENT GROUND CREW NOTICED FIRE AT APU. MAINTENANCE FOUND THE PROBLEM TO BE THE FADEC. THE FADEC WAS REMOVED AND REPLACED IAW EMB MM ALONG WITH A WIRING HARNESS AND FUEL DRAIN LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031021002832003102100283NM 2003 10 21 CALA0300541 120030919A5753 SKIN BOEING757 757224 1384958NM RROYCERB211 RB211* 54555NE RT I/B FLAP CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717128 27567 INSPECTION FOUND RT I/B MAIN FLAP SKIN PANEL CORRODED ON LOWER SURFACE. REPAIRED SKIN IAW ECRA 5750-03811. 2L72 4F4 FRTA2NM A12EU 20031022000072003102200007WP 2003 10 22 ABXA030367 120030902A534339164091N FITTING DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE LT MLG WW CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23985AX 47522 SLANT PANEL OUTBOARD ATTACH ANGLE WAS EXFOLIATED. REPLACED DAMAGED FITTING WITH NEW FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F4 F A6WE E2EA 20031022000312003102200031NM 2003 10 22 C1HA200393013 120030922A3350 BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15293AS 21348 L-2 AND R-2 SLIDE EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK FOR AFT SLIDE LIGHTS IAW 727 MM 33-50-51. OPS CHECK WAS GOOD. 2L73 4F A3WE 20031022000392003102200039EA 2003 10 22 SWIA200312421 120030824A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07442SW 7609 PAX DOOR HANDLE CRACKED. (DISCOVERED DURING C-CHECK) PAX DOOR OUTER HANDLE REMOVED AND REPLACED IAW CRJ AMM 52-11-03-000-802. 2L72 4F RTA21EA 20031022000992003102200099WP 2003 10 22 BSY2003F00023 220030903A7200 ENGINE LEAR 35 35A 5170602CE GARRTTTFE731TFE7312 01518WP LEFT MALFUNCTIONED E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0781FR 081 P74402 AFTER DEPARTING CMH, LT ENGINE OIL PRESSURE ROLLED BACK TO 18 PSI AND STAYED THERE. SHUT ENGINE DOWN, JETTISON FUEL AND LANDED BACK IN CMH. RESTARTED ENGINE, OIL PRESSURE RETURNED TO NORMAL. RESTARTED SEVERAL TIMES, ALL OK. FLEW TO HOME BASE, NO PROBLEMS. 2L72 4F4 F A10CE E6WE 20031022001132003102200113EU 2003 10 22 XNOA01156 120030922A2612 ELEMENT AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE MALFUNCTIONED A XN0AFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23371PC 157 517443 DURING CLIMB NR 1 ENG (B LOOP) LT ILLUM WITH LOOPS LT ILLUM ON MWP. CHECKLIST CARRIED OUT AND ENG FIRE WARNING REMAINED ON AFTER POSITIVE TEST OF (LOOP A). ENG FIRE CHECKLIST CARRIED OUT AND FIRE IND CEASED AFTER LEFT FIRE BOTTLE DISCHARGED. INSP NR 1 ENG NO LEAKS FOUND. FOUND NR 1 ENG B-LOOP CORE INSULATION ELEMENT IS LOW AROUND 27 & ALSO A-LOOP CORE ELEMENT ABOUT 58. REPLACED CORE FIRE SENSEING ELEMENT IAW A300 AMM 26-12-12 GRN CK NORMAL.R&R NR 1 ENG NR 1 FIRE BOTTLE & DISCHARGE CARTIDGE IAW A300 AMM 26-21-11 & 13 GRD CK NORMAL. (STATUS:SUPP/CLOSED) 2L72 4F4 FRTA35EU E23EA 20031022001142003102200114EU 2003 10 22 JGV2003F00002 120030910A2810 FUEL TANK ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE7312B WP CENTER WING LEAKING B JGVRO OTHER K FLUID LOSS NRNOT REPORTED 1 CE09302TS1394 108 FUEL LEAKING INTO CABIN FROM CENTRAL TANK LOWER. INSUFFICIENT AMOUNT OF SEALANT APPLIED TO INTERIOR TANK AND EXTERIOR PORTION OF FUEL TANK. FUEL FLOWING OUT OF CABIN DRAIN. INSULATION IN LEAKING AREA SOAKED WITH FUEL. (CE09200304095) 2L72 4F4 FRTA16NM E6WE 20031022001182003102200118 2003 10 22 C2XA03CL169 420030918A3431S672002 ANTENNA EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL RADIO ALTIMETER FAULTY A C2XAK NONE J WARNING INDICATION CRCRUISE 1 SW2713956 145078 CLE FLIGHT NR 2068 THE CREW REPORTED A LANDING GEAR WARNING AT 10,000 FT. MAINTENANCE INSPECTED AND REPLACED BOTH NR 2 RADIO ALTIMETER ANTENNAS. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031022001242003102200124NM 2003 10 22 QXEA200301174 120030922A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM ZONE 800 UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX 4046 IDA- ON FLIGHT 2289 AIRCRAFT RETURNED TO FIELD DUE TO FORWARD BAGGAGE DOOR WARNING IN FLIGHT AT FL 200 AT -5.0 PSID. AIRCRAFT MAINTAINED PRESSURIZATION, DEPRESSED MANUALLY IAW EMERGENCY PROCEDURES. AIRCRAFT LANDED SAFELY. OBSERVED HANDLE POPPED OUT UPON GROUND INSPECTION. VISUALLY INSPECTED DOOR AND HANDLE MECHANISM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031022001282003102200128NM 2003 10 22 2003UALA00441 120030522A2421745329 IDG BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE RIGHT DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29673UA 29241 RIGHT IDG DRIVE LIGHT ILLUMINATED. REMOVED AND REPLACED THE IDG. SHOP FINDINGS, THE RING WHICH HOLDS THE BALANCE WEIGHTS BROKE CAUSING SIGNIFICANT INTERNAL DAMAGE. 2L72 4F4 FRTA1NM E24NE 20031022001552003102200155 2003 10 22 RAIA00309245 420030920A34257011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP FLT DIRECTOR MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03558HK146781498 41071 FLIGHT DIRECTOR BARS ARE TILTED, LEFT SIDE. MAINTENANCE REMOVED AND REPLACED SYMBOL GENERATOR. 2L72 4T3 TRTA41NM E2WE 20031023000022003102300002NM 2003 10 23 CALA0300553 120030923A5320 PAN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE RT AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND RT AFT LAV FLOOR PAN CORRODED AT SERVICE WATER FITTING. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031023000102003102300010NM 2003 10 23 03FDEA01495 120030902A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING - I/B FLAP O/B HINGE PIVOT I/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71783, TITLE - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20031023000402003102300040NM 2003 10 23 AWXA200301088 120030904A5751 WEB BOEING737 7373Q8 1384670NM AILERON CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK THE LT WING INBOARD AILERON ATTACH HINGE SUPPORT WEB WAS FOUND CHAFED. MAINTENANCE CUTOUT CHAFED AREA OF LT WING INBOARD AILERON ATTACH HINGE SUPPORT WEB; FABRICATED A SPLICE REPAIR; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13, PG. 1-5, FIG. 1. 2L72 4F RTA16WE 20031023000552003102300055SO 2003 10 23 SWIA200312445 120030921A5420 STRUCTURE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07584SW 120352 LT ENGINE NACELLE DECK CRACKED BY ENGINE DRIVEN HYD LINE. (DISCOVERED DURING E005 INSPECTION) REPAIRED LEFT ENGINE NACELLE DECK CRACK IAW IC 2003-120/3178 2A AND SRM 51-40-00. 2L72 4T4 TRTA31SO E20NE 20031023000632003102300063NM 2003 10 23 QXEA200301180 120030922A3260 SENSOR BOMBDRDHC8 DHC8401 1390041NM MLG MALFUNCTIONED A QXEAO OTHER N FALSE WARNING DEDESCENT 1 NM09402QX 4032 ON FLIGHT 2323 DURING DESCENT AT 245 KIAS, ALL AMBER GEAR DOOR LIGHTS AND BOTH MAIN RED UNSAFE LIGHTS FLASHED INTERMITTENTLY AS AIRCRAFT ENCOUNTER LIGHT TURBULENCE. LIGHT IN GEAR HANDLE ALSO ILLUMINATED. COCKPIT NOISE LEVEL INDICATED THAT THE DOORS DID OPEN TO SOME DESCENT. FLIGHT ATTENDANTS CONFIRMED THAT IT SOUNDED AS IF THE GEAR WAS COMING DOWN. AMBER GEAR LIGHTS OCCASIONALLY CAME ON (WITH NO RED UNSAFE) AND OFF UNTIL GEAR WAS EXTENDED FOR LANDING. GEAR EXTENDED NORMALLY. AIRCRAFT LANDED SAFELY. UPON INSPECTION OF AIRCRAFT FOUND RGUPLK/RGDRCL SENSORS NEAR GAP ARE TOO LARGE. RIGGED RGUPLK/RGDRCL SENSORS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031023000642003102300064SO 2003 10 23 C2XA03SH348 120030924A531514529150001 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 SHV-DURING C CHECK MAINTENANCE FOUND THE FLOORBEAM AT FR 20 TO BE CORRODED. MAINTENANCE REMOVED AFFECTED PART AND REPLACED IT WITH A NEW CROSS BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031023000672003102300067SO 2003 10 23 C2XA03SH351 120030924A532014521725015 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 SHV-DURING C CHECK THE AFT SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031023000782003102300078NM 2003 10 23 P5CA0300952 120030922A272160130011 ACTUATOR BOEING747 7472U3B 1384846NM PWA JT9 JT9D* NE RUDDER DEFECTIVE A P5CAO OTHER J WARNING INDICATION CLCLIMB 1 WP23923FT 22769 RUDDER RATIO LIGHT CAME ON AFTER FLAPS UP. REPLACED UPPER RUDDER RATIO CHANGER ACTUATOR AND ADJUSTED UPPER RUDDER IAW MM 27-21-12 AND 27-21-00. 2L74 4F4 FRTA20WE E20EA 20031027000042003102700004SO 2003 10 27 LR7A03079 120030923A5230 WEB LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 1911 4698 AFTER LOADING CARGO RAMP LOCKS WOULD NOT ENGAGE. FOUND PN 33035471 RAMP LATCH ACTUATOR FITTING BROKEN AND WEB CRACKED AT FS 791, BL 0, WL 173. SECURED RAMP AND FERRIED AIRCRAFT UNPRESSURIZED TO EGSC FOR REPAIR. AT EGSC REPLACED FITTING AND REPAIRED WEB IAW SRM SMP 583 51-140-17. WC 02/06/01 AND NR 0001. 2H74 4T A1SO 20031027000092003102700009WP 2003 10 27 MWEA030395 120030925A53305911423501 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31209ME 47730 FUSELAGE SKIN HAS A DENT AT STATION 967, 2 INCHES ABOVE LONGERON 27 LEFT. FABRICATED AND INSTALLED DOUBLER AND FILLERS. 2L72 4F4 F A6WE E2EA 20031027000222003102700022EU 2003 10 27 AWXA200301098 120030913A5320D53480020697 WEB AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK A 1INCH CRACK WAS FOUND ON WEB BETWEEN FR 68 AND FR 69 AT RBL 49, FLOOR LEVEL. MAINTENANCE REMOVED CRACKED WEB BETWEEN FR 68 AND FR 69 AT RBL 49; FABRICATED A NEW REPLACEMENT WEB IAW DWG 18D53480020; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, PG. 21-25. 2L72 4F RTA28NM 20031027000282003102700028EU 2003 10 27 AWXA200301104 120030813A5315D5347209000500 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON Y1292 FLOORBEAM AFT OF FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y1292 FLOORBEAM AFT OF FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PARTS IAW A320 SRM 51-49-00, PG. 5-6. 2L72 4F RTA28NM 20031027000452003102700045NM 2003 10 27 03FDEA01637 120030925A2780 INDICATOR BOEING727 727200 138407ENM NR 6 L/E FLAP FALSE INDICATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25496FE 21670 AFTER TAKEOFF NR 6 LED FAILED TO RETRACT, COMPLIED WITH QRH AND RETURNED TO MEM. JUMPER INSTALLED ON NR 6 KRUEGER FLAP. DETERMINED TO BE INDICATION PROBLEM, CYCLED FLAPS SEVERAL TIMES- INDICATIONS NORMAL, REF MM27-82-000-1. REMOVED JUMPER FROM NR 6 KRUEGER FLAP AND CONNECTED C/P CYCLED FLAPS PER MM 27-82-001-4, OPS CK NORMAL. 2L73 4F RTA3WE 20031027000492003102700049NM 2003 10 27 03FDEA01612 120030924A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION (C53-111-01, 3) ON FLOORBEAM BS 1070, LBL 39-42. 2L73 4F RTA3WE 20031027000512003102700051NM 2003 10 27 03FDEA01614 120030924A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 EXTERNAL FUSELAGE SKIN CREASED BS 189 LBL 9-12 LWR HALF. 2L73 4F RTA3WE 20031028001612003102800161NM 2003 10 28 GAIA03093 120030910A5315 FLOORBEAM BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM UPPER 'T' CAP CORRODED RBL 45.5 BS 765 TO 848. REF FASI N/R 53136 REPLACED DAMAGED 'T' CAP P/N 65-16279-10 PER B-727 SRM 51-30-5, AND 51-30-2. (M) 2L73 4F A3WE 20031028001692003102800169NM 2003 10 28 ASAA0340116 120030305A53206553844 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR TO SIDEWALL SUPPORT AT BS 727 TO BS 767. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001742003102800174EU 2003 10 28 USAASA03095 120030818A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19756US 1340 DCA - DURING THE EMERGENCY LIGHTS TEST, RECEIVED 'EPSU BATTERY EMER R, MESSAGE ON THE FLIGHT ATTENDANT PANEL SCREEN. MAINTENANCE REPLACED BATTERY FROM MID-CABIN RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031028001762003102800176EU 2003 10 28 USAASA03102 120030830A3350 LIGHT AIRBUSA319 A319112 3930323EU ESCAPE SLIDE FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19766US 1378 CLT - THE LEFT MAIN ENTRANCE DOOR SLIDE EMERGENCY LIGHTS FAILED DURING TEST. MAINTENANCE REPLACED THE LEFT FORWARD DOOR SLIDE. EMERGENCY LIGHTS PASSED TEST. OK FOR SERVICE. THE REPAIR SHOP FOUND NO FAULTS WITH THE SLIDE LIGHTS. SLIDE RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 20031028001802003102800180NM 2003 10 28 ASAA0340076 120030227A5320654529623 STRAP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR SUPPORT STRAP AT BS 772 LBL 21 AND RBL 21. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000792003102900079NM 2003 10 29 AMTA200301226 120030924A2751 TRANSMITTER BOEING757 75733N 1384931NM TE FLAPS MALFUNCTIONED A AMTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL11554TZ 32588 ON TAKEOFF, THE TRAILING EDGE ASSYMETRY LIGHT CAME ON. WHEN FLAPS WERE MOVED FROM 20 DEGREES TO 5 DEGREES THE LEFT T/E FLAP INDICATOR MOVED TO 15 DEGREES PLUS THE RT T/E IND REMAINED AT 20 DEGREES. REMOVED AND REPLACED RIGHT OUTBOARD T/E FLAP POSITION TRANSMITTER IAW 27-58-03-4. PERFORMED TEST OF TRANSMITTER IAW APPROPRIATE SUBTASKS. SYSTEM TEST GOOD. (M) 2L72 4F RTA2NM 20031029000912003102900091NM 2003 10 29 ASAA0240214 120030401A5320654795711 STRAP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND AFT CARGO DOOR WAY STRAP CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031030000072003103000007NE 2003 10 30 092503 220030925A8520 ROD BEARING DOUG DC3 DC3C 3021457WP PWA R1830 R183090D 52020NE RT ENGINE FAILED E VLLAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL0536AP 5879 977 13439 CP355054 AT CLIMB POWER 10 MINUTES OUT OF GSO ENROUTE TO BIV RT ENGINE OIL TEMP. WENT TO 100 C, OIL PRESSURE DROPPED TO 40 PSI. AIRCRAFT RETURNED TO GSO. SUSPECTED MASTER ROD BEARING FAILURE. METAL FOUND IN OIL SCREEN AND OIL TANK. 2L72 4R4 R A669 5E4 20031030000122003103000012NE 2003 10 30 092703 220030929A8500R183090D ENGINE DOUG DC3 DC3C 3021457WP PWA R1830 R183090D 52020NE RIGHT FAILED E VLLAEA ENGINE SHUTDOWN UNSCHED LANDING EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 GL05932H 7288 1183 34368 319903 AT CRUISE POWER FOR 3 HOURS ENROUTE FROM LRD-GMU, RT ENGINE STARTED RUNNING ROUGH AND BLOWING OIL OUT OF THE CRANKCASE BREATHER. AIRCRAFT DIVERTED TO LFT. SUSPECT CYLINDER AND SCAVENGE PUMP FAILURE. 2L72 4R4 R A669 5E4 20031030000222003103000022NM 2003 10 30 UPS03441280 120030905A5712 RIB BOEING747 747121 1384871NM NR 21 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 21 V/C FLAP O/B LINKAGE O/B RIB NR 3 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 3 TO NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000552003103000055NM 2003 10 30 UPS03441318 120030903A5410 WEB BOEING747 747121 1384871NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, SEVERAL CRACKS WERE FOUND AT NR 3 PYLON REAR MOUNT BULKHEAD FORWARD AND AFT FRAME WEB, DETAILS PLEASE REER ATTACHED FIGURE. FRAME WEBS REPLACED AND REPAIRED AS PER RS R54-53-35063 INSPECTIONS TO CONTINUE PER UPS EO B747-5410-13908 AND UPS ENGINEERING FILE NR 747-54-20040. 2L74 4F A20WE 20031031000042003103100004EA 2003 10 31 SWIA200312462 120030926A3220 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07595SW 7292 NOSE GEAR DID NOT RETRACT W/FOLLOWING MESSAGE: NOSE DOOR OPEN, GEAR DISAGREE, WOW INPUT, WOW OUTPUT, STEER INOPERATIVE. RETURNED TO CYVR. REMOVED AND REPLACED THE NLG LOWER BEARING TEE SEAL IAW MM 32-21-20. OPS AND LEAKS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031031000272003103100027NM 2003 10 31 03FDEA01660 120031001A2612774001 SMOKE DETECTOR BOEING727 727200 138407ENM CARGO BAY FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25215FE1429014290 22936 NR 5 CARGO SMOKE ALARM SOUNDED, CLIMBING THROUGH 1500 AGL SILENCED ALARM SOUNDED 3 MORE TIMES PRIOR TO LANDING. INSPECTED A/C UPON ARRIVAL. NO EVIDENCE OF CARGO SMOKE. CARGO SMOKE TEST GOOD. FOR PRECAUTION REPLACE NR 5 CARGO SMOKE DETECTOR AND CHECKED GOOD IAW MM 26-16-011-4. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20031031000712003103100071NM 2003 10 31 DL757030837 120030912A5330141N34318 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27658DL 24420 THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS BETWEEN FS 385 & 392 NEAR STRINGER 18R. THE DENTS WERE REMOVED WITH LOCAL SKIN CUTOUTS. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER/TRIPLER REPAIR PER ER/A 385655-14,REV B. 2L72 4F RTA2NM 20031031000792003103100079NM 2003 10 31 DL76L030845 120030916A3320 LIGHT BOEING767 767332 1382001NM AFT GALLEY SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO271200K 28457 ON TAKEOFF OVERHEAD AFT GALLEY LIGHT SHORTED, HAD AN AUDIBLE POP, PUFF OF SMOKE, AND SPARK FROM LIGHT. REMOVED POWER FROM THAT AREA OF GALLEY. NO FURTHER PROBLEMS. INSPECTED LIGHT AT LT SIDE OF AFT GALLEY. F/A REPORTED AREA. LIGHT AND COFFEEMAKERS FUNCTION NORMAL. FOUND NO SHORTED WIRES OR BURN MARKS OR SMELL. OK FOR SERVICE. 2L72 4F RTA1NM 20031103000242003110300024NM 2003 11 3 DLM88030878 120030925A71102190060501 BARREL DOUG MD88 MD88 3023688NM INLET COWL DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27901DL 49532 THE INNER ACCOUSTIC BARREL ASSEMBLY WAS FOUND WITH DAMAGE TO THE UPPER AND LOWER BACKSHEETS AND INNER WIRE MESH. NOTE - TAIL NUMBER PICKED AT RANDOM, BARREL IS A SHOP SPARE. BARREL ASSEMBLY WAS REWORKED PER ERA 423517-14, REV A. 2L72 4F RTA6WE 20031103000472003110300047NM 2003 11 3 03FDEA01699 120031003A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 FWD CARGO SIDE FRAME DENTED STA 660 RBL 35 WL 160 ** SD ** COMING 2L73 4F RTA3WE 20031103000902003110300090GL 2003 11 3 ALG2003F00082 220030828A732323065124 GOVERNOR BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE MALFUNCTIONED E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION HOHOVERING 1 SW031078N165271773 45389 CAE860266 UPON COMING TO A HOVER. NR 2 DROPPED TO 92 PERCENT AND TOOK UP TO 15 SECONDS TO RECOVER AT HIGH TORQUE SETTING (ABOVE 80 PERCENT) N2, WOULD NOT DROOP AT LOW TORQUE SETTING. MAINTENANCE CHANGED GOVERNOR, LINER ACTUATOR, AND CHECKED NR2 RIGGING, CHECKED GOOD. 1G71 3U3 U H2SW E1GL 20031103001012003110300101NM 2003 11 3 AWXA200301125 120031003A3397BMS13311122 WIRE BOEING737 7373S3 1384711NM SEAT ROW 9 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DFW - EEL - DURING INSPECTION DISCOVERED A BAD CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT. ISSUED MEL 33-19, COND. 1 (FLOOR PROXIMITY LIGHT INOP). WHEN AIRCRAFT RETURNED TO PHX MAINTENANCE RE-TERMINATED CONNECTOR AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031103001062003110300106NM 2003 11 3 AWXA200301130 120030908A53306545871523A SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK A .3750 INCH CRACK WAS FOUND ON OUTER SKIN OF R-1 DOOR UPPER HINGE CUTOUT. MAINTENANCE ROUTED OUT CRACK ON OUTER SKIN OF R-1 DOOR UPPER HINGE CUTOUT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA E.R. 03-5241-03254-ES1. 2L72 4F RTA16WE 20031103001132003110300113EU 2003 11 3 AWXA200301109 120030926A5315D534721220000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS ON A CABIN FLOORBEAM BETWEEN STA. 67 AND 68 ON Y1200. MAINTENANCE REMOVED AND REPLACED FLOORBEAM I.A.W. A320 SRM 51-42-11 PAGES 39-41 FIGURE 18 AND SRM 51-42-11 PAGE 28 FIG 12. 2L72 4F RTA28NM 20031103001142003110300114EU 2003 11 3 AWXA200301110 120030926A5315D5347218820200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS ON A CABIN FLOORBEAM BETWEEN STA. 68 AND 69 ON Y1200. MAINTENANCE REMOVED AND REPLACED FLOORBEAM I.A.W. A320 SRM 51-42-11 PAGES 39-41 FIGURE 18 AND SRM 51-42-11 PAGE 28 FIG 12. 2L72 4F RTA28NM 20031103001152003110300115EU 2003 11 3 AWXA200301111 120030926A7830D5461014100100 PROFILE AIRBUS320 A320232 3930326EU THRUST REVERSER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK A CRACK WAS FOUND ON THE LEFT THRUST REVERSER PROFILE. MAINTENANCE REMOVED AND REPLACED LEFT INBOARD THRUST REVERSER PROFILE IAW A320 SRM 51-42-11 PAGES 6-7. ADDITIONALLY WORK WAS PERFORMED IAW 51-49-00 PAGS 1-12, AMM SUBTASK 54-57-22-020-51, AND 54-57-22-400-003. 2L72 4F RTA28NM 20031103001162003110300116EU 2003 11 3 AWXA200301112 120030926A5315D53480043202 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON Y1732 FLOORBEAM AT FRAME 68 STA. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REPAIRED AFFECTED AREA AT FRAME 68 Y1732 IAW A320 SRM 53-41-14 FIG.201 PAGE 203-213. 2L72 4F RTA28NM 20031103001322003110300132NM 2003 11 3 03FDEA01730 120031008A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE HOLE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031103001332003110300133NM 2003 11 3 03FDEA01751 120031009A5753 FITTING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE RT WING O/B FLAP I/B HINGE FITTING (WING SIDE)- I/B ACTUATOR ATTACH HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71748, WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F4 FRTA22WE E13NE 20031103001342003110300134NM 2003 11 3 03FDEA01806 120031027A5343BAC1505100360 SUPPORT BEAM BOEING727 727200 138407ENM NLG CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25493FE 21531 CORROSION AROUND NOSE GEAR SUPPORT BEAM PANEL ATTACHMENT FLANGE CORROSION ON TEE CHORD FLANGE AT NOSE GEAR SUPPORT BEAM PANEL ATTACHMENT FLANGE FOUND TO BE OUT OF LIMITS. REMOVED TEE CHORD AND SENT OUT FOR FABRICATION. INSTALLED NEW TEE CHORD IN PLACE OF CORRODED TEE CHORD PER 727 SRM 51-30-2, 51-30-5, 51-20-4, FED EX M/M 51-20-151-7, SRM 51-10-1, 51-10-2. 2L73 4F RTA3WE 20031103001442003110300144 2003 11 3 IXXA0300068O 420031028A2310 RADIO DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE NR 1 & 2 HF FAILED A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11822BX87377366 45813 DURING CLIMB NR 1 AND NR 2 HF WOULD NOT TRANSMIT. CREW RETURNED AIRCRAFT AND LANDED AT FJDG WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED.MAINTENANCE PERFORMED PRESSURE CHECK OF CABIN SENSING LINE FOR ANTENNA COUPLER PER ALL APPLICABLE MANUALS. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20031105000032003110500003SO 2003 11 5 C2XA03SH384 120031011A532014522459003 SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 SHV-DURING C-CHECK THE LT AND RT GALLEY RAMP SUPPORTS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED PARTS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031029001082003102900108EU 2003 10 29 MALA030434 120030926A3020 CONNECTOR SAAB SF340 SF340A 7850100EU THERMISTER DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1527XJ 340A027 DURING CLIMBOUT ON FLIGHT NR 2742, LT INTAKE HEAT LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE MOVED LT SHOE BOX THERMISTER CONNECTOR FROM NR 4 TO NR 2 20 MIN OPS CHECKS GOOD IAW AMM 30-00-00. 2L72 4T RTA52EU 20031030000282003103000028NM 2003 10 30 UPS03441286 120030905A5712 RIB BOEING747 747121 1384871NM NR 19 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 19 V/C FLAP I/B LINKAGE O/B RIB NR 4 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 4 TO NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000382003103000038NM 2003 10 30 UPS03441296 120030906A5712 RIB BOEING747 747121 1384871NM NR 7 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 7 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 4 AND NR 6 ROTARY A ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 4 AND NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030001052003103000105NM 2003 10 30 03FDEA01539 120030908A5740NRC6066 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OUTBOARD FLAP VANE NR 4 FITTING FROM INBOARD FOUND FORWARD HOLE CORRODED. LT OUTBOARD FLAP VANE NR 4 FITTING INBOARD FORWARD HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-72700, TITLE - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP NR 2 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20031030001152003103000115NM 2003 10 30 03FDEA01625 120030924A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 AFT CARGO BAY, FRAME DENTED BS 1050 STR 26R. *S/D* DAMAGE ON FRAME AT BS 1050, STR 26R (DENT) FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 1050, STR 26R IAW SRM 51-40-3 AND EA 7-5310-54986. 2L73 4F RTA3WE 20031103000212003110300021NM 2003 11 3 DL73S030875 120030923A5330654577647 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334DL 23105 TWO DENTS WERE FOUND BELOW THE C2 DOOR CUTOUT IN THE FUSELAGE SKIN. THE DENTS WERE REMOVED WITH A 7.75 X 2.6 INCH CUTOUT AND A 9.7 X 3.4 INCH CUTOUT. THE CUTOUTS WERE REPAIRED SEPARATELY WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385609-14. 2L72 4F RTA16WE 20031103000442003110300044NM 2003 11 3 DL75K030902 120031005A332019811 BALLAST BOEING757 757232 1384965NM CABIN LIGHTS ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27644DL 23998 REPORT OF SMOKE IN THE AREA ABOVE WINDOW AT ROW 22 ON CAPTS SIDE. FLIGHT ATTENDANTS TURNED OFF SIDEWALL LIGHTS AND ODOR DISSIPATED QUICKLY MCC 0114Z JNP. FOUND WINDOW LIGHT BALLAST BAD AT SEAT 21A REPLACED SAME WINDOW NOW OP CK GOOD. NO SIGN OF BURNING, SMELL CONTAINED ENTIRELY WITHIN BALLAST. 2L72 4F RTA2NM 20031103000552003110300055NM 2003 11 3 03FDEA01689 120031002A5311 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 BS 1150 FRAME GOUGED AT LBL 13 & LBL 15 WL 163 IN RADIUS. REPAIRED FRAME FAIL SAFE BS 1150, LBL 13 & 15, WL 163. ALL IAW SRM 51-40-3. 2L73 4F RTA3WE 20031105000122003110500012NM 2003 11 5 03FDEA01840 120031031A5311 FRAME BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25124FE 19360 AFT CARGO BAY FRAME DENTED AT BS 1030 STR 26R. CUT OUT DAMAGED FRAME SECTION IN 1 X 2 INCH AREA. FABRICATED REPAIR PARTS, ALODINED, PRIMED, PAINTED AND INSTALLED ALL PER SRM 51-40-3. 2L73 4F RTA3WE 20031105000142003110500014NM 2003 11 5 03FDEA01838 120031030A2782 MOTOR BOEING727 727200 138407ENM L/E FLAP FAILED A FDEAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO25217FE 22938 ALT FLAPS EXT SYSTEM DOES NOT EXTEND LED'S. FLAPS APPEAR TO WORK OK BUT DIDN'T GO BEYOND 2. TROUBLESHOT ALT FLAP SYS. REPLACED L/E MOTOR PUMP ASSY. REPLACED L/E FLAP AND SLAT SELECTOR VALVE. REPAIRED L/E STANDBY DRIVE SHUT OFF VALVE GROUND WIRES AT GD846. ALL WORK DONE IAW FEDEX WDM 27-51-01 FEDEX MM 27-81-091-4, FEDEX MM 27-81- 041-4 SWPM 20-30-11, 20-10-12. FUNCTIONAL TESTED GOOD. RII INSP COMPLIED WITH ENT BY: 59992V RPT BY: 59992V. 2L73 4F RTA3WE 20031105000352003110500035NM 2003 11 5 AWXA200301300 120031002A532065C320747 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF INTERCOSTAL BS 999 TO BS 1006, RBL 34, WL 208. MAINTENANCE REMOVED CORRODED INTERCOSTAL BS 999 TO BS 1006, RBL 34, WL 208; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12, PARA 7D2. 2L72 4F RTA16WE 20031105000372003110500037SO 2003 11 5 C2XA03SH420 120031028A3397 WIRE EMB EMB 145 EMB145 3260210SO CABIN DAMAGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 SHV-DURING C-CHECK THE AFT AISLE EMERGENCY PROXIMITY LIGHT STRIP WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED THE LIGHT STRIP WIRING IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031105000392003110500039WP 2003 11 5 ABXA030401 120031008A5210991556525 CHANNEL DOUG DC9 DC931 3022065WP BULKHEAD DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 AFT PRESSURE BULKHEAD DOOR CRACKED AT UPPER HINGE. REPAIRED DOOR IAW DC-9 SRM 52-05. 2L72 4F A6WE 20031105000552003110500055NM 2003 11 5 SWAA032308 120031020A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, WL 208, RBL 59. REPAIRED FLOORBEAM UPPER CHORD PER SRM. 2L72 4F RTA16WE 20031105000772003110500077NM 2003 11 5 03FDEA01834 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE INBOARD ACTUATOR LUG BORE FOUND CORROSION. 2L73 4F RTA22WE 20031105000812003110500081EU 2003 11 5 03FDEA01830 120031029A5320 CROSSBEAM AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25661FE 760 CROSSBEAM AT FR29 HAS 1 INCH CRACK BETWEEN RT SEAT TRACKS R1 & R2. REPAIRED CROSSBEAM AS PER A300-600 SRM 53-10-15 FIG 206. 2L72 4F RTA35EU 20031105000822003110500082NM 2003 11 5 03FDEA01810 120031021A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP OUTBOARD FWD HINGE OUTBOARD ACTUATOR LUG BORE FOUND CORRODED. 2L73 4F RTA22WE 20031105000832003110500083CE 2003 11 5 55504 120031023A2612 FIRE WARNING BEECH 1900 1900D 1154162CE CCOKPIT ACTIVATED A AMWAFD ACTIVATE FIRE EXT. RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE07133YV UE133 DURING TAXI TO RUNWAY FOR TAKEOFF CREW OBSERVED THE ILLUMINATION OF THE RT ENG FIRE HANDLE. CREW ACCOMPLISHED THE EMERGENCY PROCEDURES FOR ENG FIRE. SECURED THE ENG AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENG FIRE BOTTLE/SQUIB P/N 30100023, S/N 29392A1. 2L72 4T RTA24CE 20031106000082003110600008NM 2003 11 6 AWXA200301356 120031014A5315146N5444 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK A .5625 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM BS 1600, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1545 TO BS 1640, LBL 2; FABRICATED A REPAIR CHANNEL; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11 PG 1-6 FIG 1. 2L72 4F RTA2NM 20031106000132003110600013NM 2003 11 6 AWXA200301359 120031014A5315146N5447 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1502-1517, RBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1502 TO BS 1517, RBL 2; FABRICATED A REPAIR ANGLE & FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1. 2L72 4F RTA2NM 20031106000542003110600054NM 2003 11 6 03FDEA01814 120031022A5744 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE FITTING (WING SIDE), ACTUATOR ATTACHMENT LUG OUTBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20031106000722003110600072NM 2003 11 6 03FDEA01822 120031029A5330 SKIN BOEING727 727200 138407ENM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 OUTER EXTERIOR SKIN HAS BULGE AT STA 1050 STR 28L. REMOVED CORROSION ON SKIN STA 1050 STR 28L, FOUND OUT OF LIMITS PER SRM 53-30-01. REPAIRED STRINGER PER SRM 53-10-03 FIG. 1. 2L73 4F RTA3WE 20031106000762003110600076 2003 11 6 SWIA200312524 420031017A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07250YV98 98 120250 DURING FLIGHT, THE CAPTAIN'S FLIGHT DIRECTOR COMMAND BARS DEVIATED FROM LEVEL TO +/- 5 DEGREES. NOSE DOWN PITCH, FOLLOWED BY AN AUTOPILOT FAILURE MAP INDICATION. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW EMB-120 MM 22-10-02. OPS CHECK NORMAL. 2L72 4T RTA31SO 20031106000852003110600085WP 2003 11 6 UPS03841516 120031023A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED 2 PLACES AT STA 1766 AT LBL 26 AND LBL 35, 65 .5 INCH ABOVE FLOOR LEVEL. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRM 53-2-5 FIG 14A AND DWG SRO8530007. 2L74 4F RT4A25 20031106001062003110600106EA 2003 11 6 COMA0360475 120031030A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01816CA 7398 FLIGHT 5897 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031106001142003110600114EA 2003 11 6 SWIA200312527 120031021A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07595SW5622 5622 7292 DURING DESCENT WITH FLIGHT SPOILERS DEPLOYED, STATUS MESSAGE FLT SPOILER FAULT APPEARED. REPLACED OUTBOARD RIGHT FLIGHT SPOILER PCU PER MM 27-62-01. SYS OPS CHECK AND LEAK CHECK OKAY. 2L72 4F RTA21EA 20031103000202003110300020 2003 11 3 DL757030874 420030925A3410347080006 INDICATOR BOEING757 757232 1384965NM COCKPIT MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27625DL 22915 IR/ IVSI C/B POPPED OUT, ACCOMPANYING BURNING ODOR FROM IVSI. FOUND IVSI IND C/B POPPED F/O`S SIDE. INSTALLED NEW IVSI IND. OPS OK. F/O`S IND CAUSE OF BURNING ODOR . 2L72 4F RTA2NM 20031103000562003110300056NM 2003 11 3 03FDEA01688 120031002A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON FUSELAGE INNER SKIN BETWEEN STR 28L - STR 27L, STA 720D TO 720E. INSTALLED REPAIR IAW SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20031103000862003110300086NE 2003 11 3 ALG2003F00078 120030701A2612 CONNECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL FIRE TEE HANDLE CONTAMINATED E ALGAO OTHER L NO TEST NRNOT REPORTED 1 SW03376AL 760002 CAE890262S DURING THE PRESTART CHECKS. THE FIRE T HANDLE FOR THE NR 1 ENGINE WOULD NOT TEST. WATER FOUND IN SYSTEM CONNECTORS, CONNECTORS DRIED AND REINSTALLED, SYSTEM CHECKED GOOD. 1G72 3U3 U H1NE E1GL 20031105000452003110500045NM 2003 11 5 SWAA032302 120031019A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20031105000562003110500056 2003 11 5 SWAA032309 420031020A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF POSITION AND RELEASE CABLE MISROUTED. REPOSITIONED SLIDE ASSY AND REROUTED CABLE PER MM. 2L72 4F RTA16WE 20031105000842003110500084CE 2003 11 5 55495 120031023A3230 LANDING GEAR BEECH 1900 1900D 1154162CE NLG & MLG MALFUNCTIONED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE073YV UE3 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. GEAR DOWN AND LOCKED. PERFORMED OPERATIONAL CHECK OF LANDING GEAR, OP CHECKED GOOD. 2L72 4T RTA24CE 20031106000552003110600055NM 2003 11 6 03FDEA01815 120031022A5710 STOP FITTING DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT OUTBOARD. FLAP SECONDARY UP STOP REPAIR. 2L73 4F RTA22WE 20031106000602003110600060NM 2003 11 6 03FDEA01819 120031028A3260 CONNECTOR BOEING727 727200 138407ENM NLG LOOSE A FDEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO25203FE 22925 ON FINAL FOR LANDING WITH FLAPS 30 AND GEAR DOWN THE NOSEWHEEL GREEN DOWN AND LOCKED ILLUMINATED INTERMITTENTLY CAUSING THE GEAR WARNING HORN TO GIVE A STEADY AURAL WARNING. A GO-AROUND WAS ACCOMPLISHED AND QRH CHECK LIST WAS RUN. AFTER RECYCLING, HAD 3 GREEN DOWN AND LOCKED INDICATIONS WITH THE NOSE WHEEL ALIGNMENT STRIP SHOWING DOWN AND LOCKED. NO FURTHER WARNINGS AFTER RECYCLING GEAR. INSP NOSE GEAR LOCK INDICATING SWITCHES, FOUND SWITCH D-298 CONNECTOR LOOSE. TIGHTENED CONNECTOR PLUG AND PERFORMED TEST PER 727-200 AMM 32-61-071-5, OPS CHECK GOOD. 2L73 4F RTA3WE 20031106000842003110600084WP 2003 11 6 UPS03841515 120031028A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 FINGER DOUBLERS ARE CORRODED BEYOND LIMITS BETWEEN STA 900 TO 980 AT LBL 67. REMOVED, FABRICATED AND REPLACED FINGER DOUBLERS IAW DWG 5645332 AND SRM 51-1-21. 2L74 4F RT4A25 20031106001272003110600127 2003 11 6 SWAA032269 420031015A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031106001582003110600158NM 2003 11 6 03FDEA01846 120031101A323269163395 SUPPORT FITTING BOEING727 727200 138407ENM NLG DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-3220-73848 LANDING GEAR - NLG - ELONGATED HOLES IN 69-16339-5 SUPPORT FITTING. COMPLIED WITH EA 7-3220-73848 LANDING GEAR - NLG - ELONGATED HOLES IN 69-16339-5 SUPPORT FITTING, AT MAE. 2L73 4F RTA3WE 20031106001642003110600164NM 2003 11 6 03FDEA01852 120031021A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), HINGE LUG INBOARD HOLE FOUND CORRODED. 2L73 4F RTA22WE 20031106001712003110600171NM 2003 11 6 QXEA200301387 120031028A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX- INVERTED DENT AT STATION X463.0 BETWEEN STRINGERS 30 AND 31. REPAIRED IAW DHC-8 SRM 51-00-06, 51-00-05 RD 8-53-7604 AND HORIZON AIR EA 2-53-498. 2H72 4T RTA13NM 20031106001802003110600180 2003 11 6 03FDEA01829 420031029A2216 TRANSDUCER DOUG DC10 DC1010 3022110WP AUTOPILOT SYS OUT OF ADJUST A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO2568053 47807 AIRCRAFT RESPONDED AS IN PREVIOUS WRITE-UPS AT LEVEL OFF FL330, PORPOISING /- 500 IN ALT HOLD, SAME RESULT AP 1 OR 2. DISCONNECTED THE AP AND SLOWED 20 KNOTS, AIRPLANE WAS DIFFICULT TO CONTROL, VSI /- 1000 FPM AND ALTITUDE /- 200 FT. DESCENDED TO FL 290, NO IMPROVEMENT. DIVERTED TO SLC. WHEN HYD PRESSURE APPLIED CHECKED ELEVATORS FOR MOVEMENT BY PHYSICALLY TRYING TO MOVE ELEVATOR SURFACES. NO MOVEMENT WAS NOTICED. CHECKED AUTO PITCH TRIM LVDT NULLS. FOUND CHANNEL A NULL TO BE 574 MVAC, JAM NUT WAS LOOSE ON THE LVDT. FOUND CHANNEL-B NULL TO BE 175 MVAC. ADJUSTED AUTO PITCH TRIM LVDT'S NULL. OPS CHECKED AUTO PITCH TRIM SYSTEM PER MM 22-22-00-5, SYSTEM TESTED NORMAL. 2L73 4F A22WE 20031106001912003110600191NM 2003 11 6 SWAA032279 120031016A3350BR2013 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, 3, 5, 12, 15, 20 AND 23. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20031106001932003110600193NE 2003 11 6 SWAA032281 220031016A7200JT8D9A ENGINE BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE NR 1 FAILED A SWAAA UNSCHED LANDING Y ENGINE STOPPAGE TOTAKEOFF 1 SW29721WN 22697 707429 IN FLIGHT SHUT DOWN, DECLARED EMERGENCY, AIR TURN BACK, NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 F A16WE E2EA 20031106002072003110600207NM 2003 11 6 2003F00597 120031006A3350RPS1B CHARGER BOEING727 727200 138407ENM CABIN FAILED A P9RAK NONE O OTHER ININSP/MAINT 1 SO11288SC 20765 BATTERY CHARGER FOR L1 EMERGENCY EXIT LIGHTING NOT CHARGING. REMOVED AND REPLACED CHARGER UNIT PER MM 33-50-51. (M) 2L73 4F RTA3WE 20031106002112003110600211NM 2003 11 6 ASAA0310515 120030603A53136552928516 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 26L AT FUSELAGE STATION 767-768.5 CRACKED. REMOVED DAMAGED AREA AND REPAIRED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20031106002152003110600215NM 2003 11 6 ASAA0310474 120030517A532065516983 SPLICE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND STRINGER SPLICE AT FUSELAGE STATION 907, STRINGER 22L-23L CORRODED. REPLACED STRINGER SPLICE PER SRM. (M) 2L72 4F A16WE 20031106002202003110600220NM 2003 11 6 ASAA0310442 120030514A5311 FRAME BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE FRAME AT BODY STATION 500, STRINGER 23R-25R DENTED. CUT OUT DAMAGED SECTION AND REPAIRED FRAME PER SRM. (M) 2L72 4F A16WE 20031103001032003110300103EU 2003 11 3 AWXA200301127 120031004A5610NP1653116 WINDSHIELD AIRBUS320 A320231 3930325EU COCKPIT CRACKED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28633AW13229 082 CMH - AIR TURN BACK - FLT 0747 - AFTER TAKEOFF FROM CMH EN ROUTE FOR LAS THE FIRST OFFICERS WINDSHIELD CRACKED, TURNED BACK TO CMH. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM 56-11-11, BITE TEST OF WINDOW HEAT COMPUTER WAS GOOD. VENDOR DID NOT PERFORM FAILURE ANALYSIS OF WINDSHIELD. 2L72 4F RTA28NM 20031103001222003110300122NM 2003 11 3 03FDEA01735 120031008A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B HINGE HOLE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B HINGE HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 LT AND RT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031027000522003102700052NM 2003 10 27 03FDEA01615 120030924A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON BS 1070 FLOORBEAM LBL 45 - RBL 50. 2L73 4F4 FRTA3WE E2EA 20031021002342003102100234WP 2003 10 21 GTIA030706 120030910A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND BROKEN INSERT, EDGE DELAMINATED CABIN FLOORBOARD STATION 542-617. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20031021002772003102100277NM 2003 10 21 PCAA0309113 120030919A3397 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EMERGENCY LIGHT DISCONNECTED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13827EX 390 DURING ROUTINE MAINTENANCE VISIT, THE EMERGENCY LIGHT ABOVE THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. EMERGENCY LIGHT WAS FOUND TO BE DISCONNECTED. EMERGENCY LIGHT WAS RECONNECTED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETUNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031021002842003102100284NM 2003 10 21 CALA0300542 120030920A5330 SKIN BOEING757 757224 1384958NM RROYCERB211 RB211* 54555NE FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717128 27567 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT BS 730, STRINGER 16L. THE SKIN WAS REPAIRED IAW ECRA 5330-03281. 2L72 4F4 FRTA2NM A12EU 20031021002862003102100286NM 2003 10 21 CALA0300544 120030920A5311 FRAME BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND A .7500 INCH CRACK IN LT FRAME AT STA 616 JUST BELOW MAIN DECK FLOOR. A REPAIR WAS INSTALLED IAW ECRA 5311-01158. 2L72 4F4 FRTA16WE E2GL 20031021002882003102100288NM 2003 10 21 CALA0300546 120030920A5330 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717345 23583 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AFT OF EQUIPMENT COOLING EXHAUST DUCT AT STA 373. A REPAIR WAS INSTALLED IAW 5330-02894. 2L72 4F4 FRTA16WE E2GL 20031021002902003102100290NM 2003 10 21 CALA0300548 120030921A5312 BULKHEAD BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT STA 1016 JUST LEFT OF BL 0. REPAIRED WEB IAW SRM 53-80-08 AND BOEING DRAWING 65C28106. 2L72 4F4 FRTA16WE E2GL 20031021002932003102100293NM 2003 10 21 CALA0300550 120030921A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND A .2500 INCH CRACK IN FLOOR SUPPORT ANGLE AT STA 500D-520, BL 0. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031022000422003102200042EA 2003 10 22 SWIA200312424 120030918A2760270003 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SPOILERONS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07406SW1006810068 7030 SPOILERON FAULT STATUS MESSAGE. REMOVED AND REPLACED LEFT OUTBOARD SPOILERON PCU IAW 27-62-01. OPS AND LEAK CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031022000912003102200091NM 2003 10 22 03FDEA01737 120031014A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 CHAFING ON LAP JOINT SKIN STR 19L B/S 720D PLUS 10 INCHS. BLENDED CHAFFE FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA AND REPAIRED. PER SRM 53-30-3 FIG 14. 2L73 4F RTA3WE 20030910000302003091000030WP 2003 9 10 DHL2003604591 120030625A5754 PANEL DOUG DC8 DC873F 302199FWP L/E SLOT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTBOARD SLOT UPPER CENTER DOOR WITH 0.500 CRACK IN IT. REMOVED AND REPLACED RT OUTBOARD SLOT UPPER CENTER DOOR IAW MM 27-80-2 PG 201-204. REFER TO NR 0531 FOR OPS CHECK. 2L74 4F RT4A25 20030910000312003091000031EU 2003 9 10 BAQA088189 120030721A673031026010 SERVO AEROSPAS355 AS355F2 8680812EU MAIN ROTOR LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03942MS6359 5498 MAIN ROTOR SERVO LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030910000332003091000033WP 2003 9 10 DHL2003604652 120030510A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD FLAP LOWER SKIN SHOWS INTERIM REPAIR BETWEEN STA XF 415.000 AND XW 408.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030502, ED-3379. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. REMOVED DAMAGED SKIN PANEL IAW EODHL-030502, ED-3279. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-030502, ED-3279. CLEANED, TREATED AND PRIMED NEW SKIN INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON LT WING OUTBOARD FLAP LWR SURFACE WITH NEW FASTENERS IAW EODHL030502, ED-3279, SRM 51-1-21 PG 1, SRM 51-1-21A PG 3. 2L74 4F RT4A25 20030910000452003091000045EU 2003 9 10 BAQA088910 120030821A2841647571012 INDICATOR AEROSPAS355 AS355F1 8680810EU RT FUEL QTY FLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035797X25 5182 RIGHT FUEL GUAGE FLUCTUATES IN FLIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030910000462003091000046WP 2003 9 10 DHL2003604668 120030529A5522 SKIN DOUG DC8 DC873F 302199FWP LT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT ELEVATOR UPPER EXTERNAL SKIN HAS SEVERAL DENTS FROM STA XE 132.000 TO XE 246.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030501, ED 3277. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EO DHL 030501, ED 3277. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN IAW EO DHL 030501, ED 3277. CLEANED, TREATED AND PRIMED NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN AND FASTENERS ON LT ELEVATOR UPPER EXTERNAL SURFACE IAW EO DHL 030501, ED 3277, SRM 51-1-21 PG 1, SRM 51-1-21A PG 3. SEE NR 4038 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20031103001262003110300126NM 2003 11 3 03FDEA01752 120031009A5753ARC0502506 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE FITTING (WING SIDE)- O/B ACTUATOR ATTACH HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71748, WINGS - RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031103001362003110300136EA 2003 11 3 SWIA200312476 120031002A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 280 RT FLOORBEAM RBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-58 2L72 4F4 FRTA21EA E15NE 20031105000272003110500027NM 2003 11 5 AWXA200301352 120031014A5320146N5469 WEB BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FORMER WEB AT LOWER PORTION OF WEB WHERE ATTACHED TO SKIN BS 1500 TO BS 1520. MAINTENANCE REMOVED DAMAGED FORMER WEB FROM BS 1500 TO BS 1520; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 1, PARA B1-A. 2L72 4F RTA2NM 20031105000292003110500029NM 2003 11 5 AWXA200301354 120031014A5315146N5446 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATES HOLES OF AFT CARGO COMPARTMENT FLOORBEAM BS 1624 TO BS 1638, RBL 14. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CAP AT BS 1624 TO BS 1638, RBL 14; FABRICATED REPAIR ANGLES AND NEW REPLACEMENT SECTION OF UPPER CAP; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 1-6. 2L72 4F RTA2NM 20031105000612003110500061NM 2003 11 5 03FDEA01858 120031103A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 FORWARD LOWER CARGO FRAME IS DENTED AT STA 580 STR 24L. REMOVED DAMAGE AT FRAME IN AREA OF 1 X 3 INCHES AT BS 580, STR 24L. FABRICATE THE DOUBLER MADE FROM 7075-T6 0.063 AND INSTALLED THE REPAIR DOUBLER IAW SRM 51-40-3. 2L73 4F RTA3WE 20031105000642003110500064WP 2003 11 5 UPS03841503 120031023A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 LONGERON 33L CORRODED BEYOND LIMITS BETWEEN STA 330-390. REMOVED, FABRICATED AND REPLACED LONGERON SECTION STA 330-390 IAW SRM 51-1-20D AND DRAWING 9754913. 2L74 4F RT4A25 20031105000662003110500066WP 2003 11 5 UPS03841505 120031022A53203641126501 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 MAIN CABIN FLOORBEAM TO CENTER WING BOX ATTACH FITTING IS CRACKED, STA 781, RBL48. REMOVED FITTING IAW SRM 51-3-0 AND SRM 51-1-20D AT STA 781, RBL 48, INSTALLED NEW FITTING AT STA 781 RBL 48 IAW SRM 51-1-20D, 51-3-0, AND 51-1-11. 2L74 4F RT4A25 20031105000692003110500069NM 2003 11 5 SWAA032284 120031016A5330654589015 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED BELOW AIR STAIR CUT OUT AT BS 340, STR 21R. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20031105000732003110500073NM 2003 11 5 SWAA032288 120031019A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 380, LBL 20. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031106000052003110600005NM 2003 11 6 AWXA200301355 120031014A5315146N5444 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT NUT PLATES ON LOWER SIDE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1500 TO BS 1540, LBL 9. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1500 TO BS 1540, LBL 9; FABRICATED A REPAIR ANGLE AND CHANNEL; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 1-6 FIG 1. 2L72 4F RTA2NM 20031106001052003110600105SO 2003 11 6 C2XA03SH404 120031022A532014530633003 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 23 AND 29 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031106002302003110600230NM 2003 11 6 ASAA0310477 120030519A531565671406 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE LONGITUDINAL BEAM AT FUSELAGE STATION 685, RIGHT BUTTOCK LINE 43 CORRODED. REPAIRED BEAM PER SRM. (M) 2L72 4F A16WE 20031106002422003110600242NM 2003 11 6 GTIA030013 120030121A716059306451 LINER DOUG MD80 MD83 3023681NM NR 2 NOSE COWL DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 MCO - NR 2 ENGINE NOSE COWL LINER DAMAGED. REMOVED AND REPLACED NR 2 ENGINE NOSE COWL AS REQ. (M) 2L72 4F RT 20031107000292003110700029NM 2003 11 7 QXEA200301393 120031103A242111522184 GENERATOR BOMBDRDHC8 DHC8401 1390041NM NR 2 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09546DS161 4017 SEA- ON FLIGHT NUMBER 2323, AFTER LANDING, NR 2 AC GENERATOR CAUTION LIGHT CAME ON. RESET PER CHECKLIST, WOULD NOT COME BACK ONLINE. REMOVED AND REPLACED NR 2 AC GENERATOR. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031107000362003110700036SO 2003 11 7 C2XA03TY188 120031104A531514522461011 DOUBLER EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND GALLEY FLOORBEAM DOUBLER AT FRAME 20 AND 22. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW EMB SRM 51-30-01, 51-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030910000572003091000057SW 2003 9 10 HEEA088924 120030728A5610407030115123A WINDSHIELD BELL 407 407 1182206SW COCKPIT SCRATCHED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 WINDSHIELD SCRATCHED. 1G71 3U O H2SW 20030910000632003091000063NM 2003 9 10 DHL2003754015 120030809A3242 BRAKE BOEING727 727223 1384074NM RT MLG CONTAMINATED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01754DH 22008 RIGHT BRAKES ARE DRAGGING DURING TAXI AND LANDING, WITH OR WITHOUT ANTI-SKID ON. BLEED BRAKES, OPS CHECK GOOD IAW B-727 MM 32410, REF N/R 34729. 2L73 4F A3WE 20030910000812003091000081WP 2003 9 10 DHL2003604557 120030530A57305611013502 PANEL DOUG DC8 DC873F 302199FWP RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED BETWEEN STA XRS 162.000 AND XF 219.000. REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XRS 162.000 - XF 219.000) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030910000822003091000082WP 2003 9 10 DHL2003604559 120030503A5720 ATTACH ANGLE DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD STUB WING ATTACHING ANGLE CRACKED 1.000 AT XS 520.168. REMOVED CRACKED ATTACHING ANGLE ON LT WING OUTBOARD STUB WING AT XS 520.168 IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED NEW ANGLE AND AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 57-2-0 PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031027001042003102700104NM 2003 10 27 ASAA02402KK 120030412A532014902785 STANCHION BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND E-1 RACK LEFT FORWARD STANCHION CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028000222003102800022NM 2003 10 28 CALA0300563 120030926A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND A .5 INCH CRACK IN UPPER HINGE SKIN CUTOUT ON R-1 DOOR. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW ECRA 5241-01013. 2L72 4F RTA16WE 20031028000272003102800027SO 2003 10 28 C2XA03TY168 120030929A532014524119007 SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713995 145295 DURING A SCHEDULED INSPECTION THE PAX DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD IAW-EMB-145-AMM-20-10-01 AND CMP-51-14-02, 04, 05 AND 06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLETION OF THE INSPECTION. 2L72 4T RTT00011AT 20031028000902003102800090NM 2003 10 28 UPS03441455 120031020A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 CRACK JUST AFT OF NLG CUTOUT. CRACK VERIFIED BY EDDY CURRENT READING. REMOVED CRACKED AREA OF SKIN VERIFIED CRACK REMOVED W/T EDDY CURRENT. REPAIRED IAW SRM 53-30-3 2L74 4F A20WE 20031029000042003102900004NM 2003 10 29 ASAA0340104 120030301A5320 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND RT AC BAY RAM AIR INLET PLENUM ANGLE CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000192003102900019NM 2003 10 29 ASAA0340113 120030305A532069434771 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029001032003102900103NE 2003 10 29 MALA030435 220030926A7510216118218 BLEED BAND BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 ENGINE BROKEN A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15509XJ E2321 DURING CLIMBOUT ON FLIGHT NR 3446, NR 2 ENGINE EGT HIGH AND NR 1 12 PERCENT LOW IN CLIMB. AIR RETURN TO MEM. MAINTENANCE FOUND NR2 ENGINE BLEED BAND BROKEN. REMOVED AND REPLACED NR 2 ENG. BLEED BAND IAW ALLIED SIGNAL MM CHAP 72-00-34.OPS CHECKS GOOD.P/N ON AND OFF 2-161-182 -18,S/N ON 032463712277 2H74 4F4 FRTA49EU E6NE 20031029001042003102900104 2003 10 29 MALA030438 420030906A3440 COMPUTER BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE TCAS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15523XJ E2348 DURING RON OUTBOUND FROM MSP, TCAS FAILED. WE RECEIVED ERRONEOUS TCAS TRAFFIC ADVISORIES (TA) AND RESOLUTION ADVISORIES(RA) AT VARIOUS ALTS. SWITCHED TO NR 1 AND WE STILL RECEIVED SOME ERRONEOUS WARNINGS (LESS FREQUENT) AIR RETURN TO MSP. MAINTENANCE REPLACED TCAS COMPUTER TESTED SYSTEM IAW FUNCTIONAL CHECK 34-44-00 P 5 01 ALL OPS NORMAL. 2H74 4F4 FRTA49EU E6NE 20031029001072003102900107EU 2003 10 29 MALA030433 120030924A5330 SKIN SAAB SF340 SF340A 7850100EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL1599XJ 340A099 DURING 4Y/2Y INSPECTION IN CWA, LT FUSELAGE HAS DENT AT STA 560 BETWEEN STRINGER SL1516 & SL1517 6 INCH X 1INCH CREASE, MAINTENANCE REPAIRED DENT IAW EO NR S53035. REFER TO 409 NR 177009, LOG PAGE NR 1222281, FOR DETAIL. 2L72 4T RTA52EU 20031029001232003102900123EU 2003 10 29 KBM2003F00018 120030821A6710123645P BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE M/R PITCH LINK LOOSE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 MAIN ROTOR PC LINK LOWER ROD END BEARING LAS EXCESSIVE PLAY. REPLACED WITH SERVICEABLE ROD END BEARING.(K) 1G71 3U3 UNCH9EU E19EU 20031029001262003102900126EU 2003 10 29 KBM2003F00021 120030811A6710 SWITCH SNIAS 350 AS350BA 8680817EU CYCLIC STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 CYCLIC TRIGGER SWITCH IS STICKING. REPLACED WITH NEW SWITCH.(K) 1G71 3U NCH9EU 20031029001292003102900129EU 2003 10 29 KBM2003F00024 120030726A6720350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH762 1864 LAMINATE BEARINGS HAVE MULTIPLE CUTS. REPLACED WITH NEW LAMINATE BEARING KIT. 1G71 3U3 UNCH9EU E19EU 20031030000162003103000016NM 2003 10 30 UPS03441274 120030908A532069B027098 ANGLE BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, BULK CARGO BAY BS 1920 FRAME ATT WEB ANGLE CRACKED AT STR 40L. ANGLE REPLACED IAW SRM 51-10-01 PG.8 2L74 4F4 F A20WE E20EA 20031030000192003103000019NM 2003 10 30 UPS03441277 120030906A5712 RIB BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR6 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 6 V/C FLAP IB UNKAGE OB RIB NR 4 AND NR 5 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM IB CLOCKWISE). NR 4 AND NR 5 BOLT HOLES REPAIRED IAW RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F4 F A20WE E20EA 20031030000202003103000020NM 2003 10 30 UPS03441278 120030906A5712 RIB BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 5 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C LT WING NR 5 V/C FLAP IB LINKAGE OB RIB NR 1, NR 2 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM IB CLOCKWISE). NR 1, NR 2 AND NR 8 BOLT HOLES REPAIRED IAW RS 57-41-35066 AND REFER EO B747574019269A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F4 F A20WE E20EA 20031030000242003103000024NM 2003 10 30 UPS03441282 120030905A5712 RIB BOEING747 747121 1384871NM NR 20 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING - NR 20 V/C FLAP O/B LINKAGE I/B RIB NR 8 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 8 BOLT HOLE REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000332003103000033NM 2003 10 30 UPS03441291 120030905A5712 RIB BOEING747 747121 1384871NM NR 9 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 9 V/C FLAP O/B UNKAGE O/B RIB NR 8 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 8 BOLT HOLE REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000402003103000040NM 2003 10 30 UPS03441298 120030906A5712 RIB BOEING747 747121 1384871NM NR 3 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 3 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 5 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 5 AND NR 8 BOLT HOLES REPAIRED AS PER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000522003103000052NM 2003 10 30 UPS03441315 120030903A5320 ANGLE BOEING747 747121 1384871NM NLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, FX NOSE TUNNEL LT WW SIDEWALL ATTACH ANGLE CORRODED AT STA 380. CORROSION BLEND OUT 0.040 X 1 X 4 INCH. THE ANGLE REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20031030000572003103000057NM 2003 10 30 UPS03441320 120030901A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D BS 1239-1241 RBL 35-38 BELOW FLOOR WING CENTER SECTION UPPER SKIN UPPER FACE CORRODED. CORROSION BLEND OUT 0.056 X 3 X 4 INCH. REPAIR PARTS INSTALLED AS PER RS NR R57-14-35078 AND UPS ENGINEERING FILE NR 747-57-20047. 2L74 4F A20WE 20031030000602003103000060NM 2003 10 30 UPS03441323 120030911A5320 WEB BOEING747 747121 1384871NM NLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, NLG W/W BAY RT STA 380 VERTICAL LOWER END ATTACH WEB AREA CORRODED. CORROSION BLEND OUT 0.40 X 1.25 X 4 INCH. NLG WW RT BS 380 VERT STRUCTURE & LOWER END ATTACH WEB REPAIRED AS PER RS R53-18-35076 DEFER THE NEW CRACK REPAIR UNTIL NEXT C-CHECK, REPEAT DETAIL EXTERNAL VISUAL INSPECTION AT 1500 FLIGHT. CYCLES INTERVALS UNTIL NEXT C-CHECK, BUT NOT TO EXCEED 3000 FLIGHT CYCLES. UPS EO B747-5310-19273-A RAISED. 2L74 4F A20WE 20031030000772003103000077NM 2003 10 30 QXEA200301195 120030926A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 LEFT HAND WING FLAP TRACK NR 4 INBOARD SIDE A SHOWS SIGNS OF MINOR PITTING ON AFT END. REPAIRED IAW DHC-8 RD 8-57-988 AND HORIZON AIR EA 2-57-236. 2H72 4T RTA13NM 20031030000842003103000084NM 2003 10 30 QXEA200301199 120030927A5552 BOLT DHAV DHC8 DHC8202 2809007NM ZONE 300 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 LT AND RT ELEVATOR GUSTLOCK PLATES HAVE LOOSE JO-BOLTS. REPAIRED IAW DHC-8 RD 8-55-112. 2H72 4T RTA13NM 20031030000862003103000086NM 2003 10 30 QXEA200301201 120030926A5330 SKIN DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 DENT/SCRAPE ON LEFT FUSELAGE 14 INCHES FORWARD AND 7 INCHES BELOW CARGO DOOR THRESHOLD. REPAIRED IAW DHC-8 SRM 51-20-11, 51-00-06, 51-20-16 AND 51-20-26. 2H72 4T4 TRTA13NM E20NE 20031030001002003103000100CE 2003 10 30 HYI2003F00014 120030829A2810CM3758E310B000S LINE CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO RT ENG FUEL PUMPLOOSE E HYIAE ENGINE SHUTDOWN KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NE012714M4755 402C0211 828571 ON CLIMB OUT, AFTER FIRST POWER REDUCTION, RIGHT ENGINE COST POWER, ATTEMPTED AUX FUEL PUMP, CROSSFEED, NO HELP. SECURED ENGINE AND FEATHERED PROP. RETURNED W/O INCIDENT. MECHANIC FOUND MAIN FUEL LINE TO ENGINE PUMP LOOSE. TIGHTENED LINE, RETURNED A/C TO SERVICE. 1L72 3O3 O A7CE E8CE 20031030001032003103000103SO 2003 10 30 CHQA000423 120030926A3040 HEATER EMB 145 EMB145 3260210SO WINDSHIELD SMOKE A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11262 ODOR NOTED IN COCKPIT FOLLOWED BY VISIBLE TRAIL OF WHITE SMOKE EMANATING FROM JUNCTION OF F/O WINDSHIELD AND GLARESHIELD. EMERGENCY DECLARED, QRH MEMORY ITEMS ACCOMPLISHED FOR SMOKE/FUMES AND IMMEDIATE DIVERSION TO NEAREST AIRPORT(CLE). SMOKE DISSIPATED AFTER WINDSHIELD HEAT SELECTED OFF. REMOVED AND REPLACED F/O'S WINDSHIELD IAW EMB 145 MM 56-10-01, OPS CHECK GOOD P/N 163500-112 OFF S/N 3954DE ON S/N 8758. 2L72 4F RTT00011AT 20031030001122003103000112NM 2003 10 30 03FDEA01599 120030908A5753ARC050214 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) INBOARD AND UPPER ACTUATOR ATTACH LUGS FOUND CORRODED AT BORES AND SPOT FITTING. RT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) INBOARD AND UPPER ACTUATOR ATTACH LUGS BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT AS PER FEDEX EA 1- 5750-72704, TITLE - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP. INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031031000112003103100011SO 2003 10 31 SWIA200312469 120030910A5210 BRACKET EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07297SW 120327 PAX DOOR AFT SIDE FRAME 5 HAS A L BRACKET CRACKED. (DISCOVERED DURING C-CHECK)PERFORMED PATCH REPAIR IAW 120 SRM 52-10-02 FIG. 203 AND CARD RII 52-301. 2L72 4T4 TRTA31SO E20NE 20031031000152003103100015NM 2003 10 31 DHL2003741009 120031002A5250 SCREW BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE COCKPIT DOOR LOOSE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01741DH 21931 COCKPIT DOOR IS DIFFICULT TO OPEN AND CLOSE. TIGHTENED SCREWS ON DOOR FRAME AND DOOR. OPS CHECKED GOOD IAW 20-80-1 AND 52-50-1. 2L73 4F4 FRTA3WE E2EA 20031031000212003103100021WP 2003 10 31 MWEA030403 120030929A2611CGAB140000 SMOKE DETECTOR DOUG DC9 DC981 3022081WP FWD CARGO PIT FAILED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 FORWARD ANNUNCIATOR FAIL LIGHTS ILLUMINATED ON OVERHEAD CARGO DETECTION SUPPRESSION PANEL. REMOVED AND REPLACED FORWARD CARGO PIT ANNUNCIATOR SMOKE DETECTOR. 2L72 4F A6WE 20031028000422003102800042EA 2003 10 28 SWIA200312455 120030903A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07916SW 7634 FS 484 RT INTERCOSTAL O/B FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. DAMAGED FLANGE REPAIRED IAW CRJ REO 601R-53-41-059 REV A AND RII 53-401. 2L72 4F RTA21EA 20031028000462003102800046EA 2003 10 28 03270667 120030927A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27667BR 7535 DURING INSPECTION THE AFT OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031028000532003102800053SO 2003 10 28 C2XA03IA100 120030928A32347455501 CONTROL LEVER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2718556 145595 AFTER DEPARTURE THE CREW NOTED THAT THE LANDING GEAR DID NOT RETRACT, AND, RETURNED TO DAL, AND, LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE PINNED LANDING GEAR,AND, SIGNED FERRY FLIGHT RELEASE. THE AIRCRAFT FLEW FROM DAL TO IAH FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER REF. EMB 145 MM 32-32-02, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031028000712003102800071EA 2003 10 28 HNAA0300052 120030926A26123601881000390 FIRE LOOP DHAV DHC8 DHC8311 1386006EA NR 1 ENGINE FALSE INDICATIONA HNAAO OTHER N FALSE WARNING CRCRUISE 1 EA07284BC 336 WARNING LIGHT, AND NR 1 ENGINE A-LOOP LIGHT ILLUMINATED. SELECTED B-LOOP AND FAULT A-LOOP WENT OUT, ALL ENGINES INDICATION NORMAL. 2H72 4T RTA13NM 20031028000732003102800073NM 2003 10 28 2003UALA00695 120030918A2612 FIRE WARNING BOEING777 777222 1385219NM PWA PW4077PW4077 NE CARGO BAY ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29768UA 26919 RETURNED TO ORD DUE TO AFT CARGO FIRE INDICATION. 2L72 4F4 FRTT0001SE E46NE 20031028000782003102800078NM 2003 10 28 2003UALA00774 120031012A3350 LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29948UA 26691 EEL LIGHTS INOP AT SEATS 15ABC. REPLACED EEL LAMPS. 2L72 4F4 FRTA16WE E2GL 20031028000892003102800089NM 2003 10 28 UPS03241453 120031021A2611 WARNING LIGHT BOEING727 72730C 1384009NM SMOKE DETECTION ILLUMINATED A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01918UP 19008 INSPECTION TYPE:N/A LOWER CARGO MX LIGHT ILLUMINATED INFLIGHT, MAINT. CODES DISPLAYED; A3398. SYSTEM TEST NORMAL PER MM 26-18-00. TESTED SEVERAL TIMES DURING LAYOVER PERIOD WITH NO DEFECTS NOTED AT THIS TIME DI 268782 CLOSED 2L73 4F A3WE 20031029000282003102900028NM 2003 10 29 ASAA0340329 120030818A33978100022608 WIRE BOEING737 737490 1384715NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT MID CABIN INOPERATIVE. REPAIRED WIRE ADN OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20031029001092003102900109CE 2003 10 29 DXTA200300126 120030925A281099145053 VALVE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL WING TANK MALFUNCTIONED E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07998QS1089 7500198 WHILE IN LEVEL CRUISE FLIGHT AT 29,000 FT THE (WING TANK O'FULL L-R) AMBER CAS MESSAGE ILLUMINATED. BOTH WING TANKS OBSERVED TO BE DUMPING FUEL FOR 2 MINUTES. - TROUBLESHOT AND FOUND BOTH WING VENT VALVES INOP. REMOVED AND REPLACED LEFT AND RIGHT WING VENT VALVES, OPS CHECK AND LEAK CHECK GOOD. WORK PERFORMED I.A.W. 750 M.M. CHAPTER 28-10-04. 2L72 4J4 FRTT00007WITE6CH 20031029001222003102900122EU 2003 10 29 KBM2003F00017 120030821A6720 BUSHING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 BALL END BEARING IS WORN BEYOND LIMITS. REPLACED WITH NEW BUSHING 350A27191200, WASHER 350A27-1911-20, BEARING EN282B506E. BOLT 22731BCD60017M AND NUT ASNA0045T-060BEL.(K) 1G71 3U3 UNCH9EU E19EU 20031029001312003102900131NE 2003 10 29 KBM2003F00026 220030917A721002352376000 CHIP DETECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE FAILED E KBMAO OTHER L NO TEST NRNOT REPORTED 1 WP19313LV4947 3296 9590 CHIP DETECTOR WILL NOT PASS OPS CHECKS. REPLACED WITH NEW CHIP DETECTOR.(K) 1G71 3U3 U H9EU E19EU 20031027000542003102700054 2003 10 27 0301809927 420030918A256513621228 SLIDE DOUG DC9 DC931 3022065WP TAILCONE MALFUNCTIONED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018920E 45835 PER MAINTENANCE CONTROL ORDER 4721, AN OPERATIONAL CHECK OF THE TAIL CONE DEPLOYMENT WAS PERFORMED. FOUND SLIDE PACK DEPLOY STRAP DID NOT SNAP ON THE SLIDE ASSEMBLY AS DESIGNED. SLIDE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20031027000702003102700070CE 2003 10 27 8483504 120030926A2720 BOLT RAYTHN BEECH 1900 1900D 1154162CE CONTROL HORN LOOSE A JJBAK NONE O OTHER ININSP/MAINT 1 EA01848CA3027 672 UE387 DURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE. 2L72 4T RTA24CE 20031027000922003102700092NE 2003 10 27 MALA030447 220031006A7220CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT MALFUNCTIONED A MALAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 GL15457XJ 340B457 GEE785758 DURING FLIGHT, LT ENGINE SHUTDOWN DUE TO CHIP LIGHT ON AND OIL PRESSURE LOSS. LT ENGINE CHIP LIGHT LITE UP AT 16000 FT. FOLLOWED QRH & REDUCED POWER. ENGINE PARAMETERS NORMAL FOR 10 MINS THEN A SUDDEN POP AND A/C SHOOK TO THE LT. ITT SUDDENLY RISED FOLLOWED QRH SHUT DOWN ENGINE AND COMPLETED SINGLE ENGINE LANDING. MAINTENANCE C/W TASK CARD 7910-303- VERIFIED LT ENGINE REQUIRES REPLACEMENT DUE TO EXCESSIVE UNALLOWABLE MATERIAL IN CHIP DETECTOR. REPLACED LT ENGINE IAW MAL TASK CARD 7100-301. A/C OK FOR RETURN TO SERVICE. UPDATED INFORMATION THE LAB REPORT FOR THE CHIP DETECTOR DEBRIS CAME BACK AS A MAJOR AMOUNT OF 1.2 PERCENT CHROMIUM, 3.2 NICKEL STEEL SUCH AS AISI 9310 (AMS 6260 OR 6265) MEASURING IN SIZE F2L72 4T4 TRTA52EU E8NE 20031027001202003102700120EU 2003 10 27 PA03004BB 120030123A7160 BULKHEAD BRAERODH125 HS125700A 4230170EU RT INLET COWL CRACKED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL2348FB 9630 257129 THE RIGHT ENGINE COWL AFT BULKHEAD IS CRACKED AT THE 12 OCLOCK POSITION. PROBABLE CAUSE IS VIBRATION. 2L72 4F A3EU 20031027001262003102700126NM 2003 10 27 QXEA200301187 120030924A3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM COCKPIT ILLUMINATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09367PH 511 ON FLIGHT 2057 ABORTED TAKEOFF DUE TO NR 2 ENGINE MANUAL CAUTION LIGHT AFTER ADVANCED POWER LEVERS FORWARD OF FLIGHT IDLE GATE FOR TAKEOFF. COMPLIED WITH BETA LOCKOUT PROCEDURE IAW FSM 02-14. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. CLOSED 2H72 4T RTA13NM 20031027001412003102700141SO 2003 10 27 C2XA03BT096 120030927A3350110049 LIGHT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 DURING ROUTINE INSPECTION MAINTENANCE FOUND THE LEFT AND THE RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 AMM NR 33-50-04. OPS. CHECKED SYSTEM GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031028000102003102800010EU 2003 10 28 155541 120030929A7710522948 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE COCKPIT FAILED A UHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL17149SZ 340A149 470 FLIGHT NR 4586 FROM PIT TO IPT. AFTER 15 MINUTES OF FLIGHT. THE LT SIDE TORQUE INDICATOR WENT TO ZERO WITH NO ENGINE ABNORMALITIES. AIRCRAFT RETURNED TO PIT SAFELY. MAINTENANCE TO AIRCRAFT REMOVED AND REPLACED TORQUE INDICATOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE6 20031028000122003102800012WP 2003 10 28 0301829612 120030927A215020495054 COOLING TURBINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE LEFT FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01612NW 47436 IMMEDIATELY AFTER TAKEOFF, SMOKE WAS REPORTED IN THE CABIN AREA AND LAV SMOKE DETECTORS WERE IN ALARM. CREW COMPLIED WITH COM, DONNED OXYGEN MASKS, & RETURNED TO AN UNEVENTFUL LANDING AT GFK. SMOKE HAD DISSIPATED BEFORE LANDING & THERE WAS NO EVIDENCE OF ANY FIRE. MAINTENANCE FOUND THE LT ACM DUMPING OIL & CAUSING SMOKE IN CABIN. THE LT ACM WAS MEL'D & BOTH WATER SEPARATOR BAGS WERE REPLACED. A/C RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20031028000172003102800017NM 2003 10 28 UPS03441269 120030927A3260 MODULE BOEING747 747123 1384873NM MLG LIGHTS INOPERATIVE A IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01672UP 20324 ATB ON RETRACTION OF GEAR AFTER TAKEOFF THE RED GEAR AND DOOR OPEN LIGHTS WOULD NOT EXTINGUISH. THE RED GEAR LIGHT REMAINS ILLUM AND GEAR DOOR OPEN LIGHT ILLUM. BASED ON SOUND AND FEEL AT LEAST ONE DOOR AND OR GEAR WOULD NOT RETRACT. ACCOMPLISHED GEAR RETRACTION ABLE TO DUPLICATE PRIMARY DISPLAY RED WARNING LIGHT GEAR, TROUBLESHOOT LOGIC MODULE BOX FOUND CARD FILE PRIMARY CARD A-13 PER MM 32-61-16. RETRACTED GEAR SEVERAL TIMES, OPS CHECKED GOOD. 2L74 4F A20WE 20031028000292003102800029EA 2003 10 28 COMA0360432 120030925A261223410400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LEFT ENGINE FALSE INDICATIONA COMAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO01991CA 7216 FLT 5051 LT ENGINE FIRE WARNING DURING TAXI. REPLACED THE LT ENGINE FIRE LOOP-B. 2L72 4F RTA21EA 20031021002462003102100246WP 2003 10 21 GTIA030695 120030905A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND L1 DOOR AT DOOR CUTOUT AFT WEB CRACKED TWO PLACES. CUT OUT DAMAGED AREA. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20031022000122003102200012NM 2003 10 22 MWEA030387 120030922A5320993653519 FLOOR SUPPORT DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CORROSION ON CABIN FLOOR SUPPORT AT STATION 200-209 12 INCHES LEFT OF AIRCRAFT CENTER LINE. REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20031022000252003102200025EU 2003 10 22 AWXA200301075 120030914A5414D54530052202203 SKIN AIRBUS320 A320232 3930326EU NR 2 PYLON ERODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK THE LOWER SECTION OF THE NR 2 PYLON AFT FAIRING OUTBOARD SKIN WAS FOUND ERODED. MAINTENANCE REMOVED ERODED AFT FAIRING SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-13, & A24-A25 FIG 2-4, & 61. 2L72 4F RTA28NM 20031022000482003102200048NM 2003 10 22 QXEA200301150 120030911A5341 FLANGE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 WING TO FUSELAGE FAIRING FORWARD APERTURE FLANGE IS CHAFED ON PANEL 262HT. REPAIRED IAW Q400 RD 8/4-53-451 AND SRM 51-00-02. 2H72 4T4 TRTA13NM E00062EN 20031022000642003102200064NM 2003 10 22 QXEA200301165 120030916A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 LOWER FUSELAGE SKIN HAS A NICK BELOW THE RIGHT FORWARD EMERGENCY EXIT, 10 INCHES AFT OF X71.2, BELOW RIGHT HAND STRINGER 28. REPAIRED IAW Q400 SRM 51-26-10, 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801 AND RD 8/4-53-505. 2H72 4T4 TRTA13NM E00062EN 20031022000702003102200070SO 2003 10 22 C2XA03IA098 120030920A33501317 BULB EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711526 145410 THE CREW NOTED THAT THE EMERGENCY LIGHT WAS INOPERATIVE IN THE CABIN DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031022000812003102200081 2003 10 22 HYI2003F00011 420030903A2210STEC55X COMPUTER CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO AUTO PILOT FAILED E HYIAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NE012714M 402C0211 5 MINUTES INTO CLIMB, CREW REPORTED SMOKE FROM AVIONICS RACK, RETURNED W/O INCIDENT. MECHANIC FOUND A/P PITCH SERVO HARNESS SHORTED, CAUSING A/P COMPUTER TO FAIL INTERNALLY, (TRANSISTORS OVERHEATED AND BURNED) REPAIRED SHORTED HARNESS. REPAIRED A/P COMPUTER, RETURNED MECHANIC TO SERVICE. (NE01200306064) 1L72 3O3 O A7CE E8CE 20031022001202003102200120NM 2003 10 22 P5CA0300946 120030920A78301960003501 SKIN BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE THRUST REVERSER DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 689185 ON MX PREFLIGHT, ON NR 3 ENG INSIDE REVERSER AREA FOUND DELAMINATION. PERFORMED REPAIR WITHIN 10 CYC - COI 921-150 ISSUED. 2L74 4F4 F A20WE E3NE 20031022001332003102200133NE 2003 10 22 2003UALA00688 220030912A7200 ENGINE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 SURGES A UALAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 WP29653UA 25391 NR 2 ENGINE, SURGE. ENGINE SURGE IN FLIGHT AT TOP OF DECENT. EPR BELOW 1.25. ENGINE REMOVED TO PERFORM SURGE CHECKS AND TEST-21. PERFORMED EXTERNAL CHECKS AND FOUND NO DISCREPANCIES. 2L72 4F4 FRTA1NM E24NE 20031023000532003102300053EA 2003 10 23 SWIA200312443 120030922A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07408SW2635 2635 7055 AFTER TAKE-OFF AND AFTER GEAR WAS SELECTED UP, RECEIVED ''NOSE DOOR OPEN'' MESSAGE. WAS UNABLE TO GET LIGHT OUT AND WE RETURNED TO FIELD. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW CRJ MM 32-22-20. OPS AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20031023000622003102300062NM 2003 10 23 QXEA200301179 120030922A243251539008C GCU DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE DC SYSTEM FAILED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09351PH243737724 490 ON FLIGHT 2228 FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS ON CONTINUOUSLY DURING START UP WHILE POWER LEVERS IN DISC AND CONDITION LEVERS IN FEATHER. EMERGENCY LIGHTS EXITING WHEN PROPS BROUGHT OUT OF FEATHER. REMOVED AND REPLACED NR 1 DC GCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031027000582003102700058EA 2003 10 27 COMA0360431 120030925A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01526CA 7824 FLIGHT 5217 DURING TAKE OFF RECEIVED A SPOILER CONFIGURATION CAUTION MESSAGE AT 85KTS, AIRCRAFT RETURNED TO THE GATE. PERFORMED FUNCTIONAL CHECK OF SPOILER CONTROL SYSTEM, NO DEFECTS NOTED. 2L72 4F RTA21EA 20031027000652003102700065WP 2003 10 27 UPS03841223 120030915A5753 FITTING DOUG DC8 DC871F 302199DWP LT WING TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 LT INBOARD FLAP HINGE CRACKED (MARKED) LT WING STA 98. DEFERRED PER FERRY PERMIT 9020. REMOVED STA 98 BASED FTG & ATTACHING STRUCTURE. LOCATED & DRILLED NEW 5751182-505 BASE FTG IAW DAC DWG 5751172. INSTALLED BASE FTG IAW DAC DWG 5751172. INSTALLED CLOSURE PANELS & ATTACHING STRUCTURE IAW DC8 SRM 51-3-0. CHECK FLAP IAW DC8 MM 27-51-04. OPS CHECK GOOD. 2L74 4F RT4A25 20031027001372003102700137NM 2003 10 27 03FDEA01620 120030924A5310 STRINGER CLIP BOEING727 727200 138407ENM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 BS 440 STR 6 LT STR CLIP CRACKED. REMOVED DAMAGED STR CLIP AT BS 440, STR 6L. DRILLED NEW STR CLIP AND INSTALLED IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20031028000052003102800005WP 2003 10 28 03FDEA01656 120030929A5753ARC2761 FLAP TRACK DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25308FE 48297 IB FLAP TRACK AND DRIVE SUPPORT BORE HAS CORROSION. COMPLIED WITH EA 8-5750-72297. RT WING IB FLAP TRACK AND DRIVE SUPPORT BORE CORROSION. 2L73 4F4 F A22WE E23EA 20031028000302003102800030EA 2003 10 28 COMA0360433 120030926A2930 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01951CA 7091 FLT 5235 NR 1 HYD SYSTEM LOW PRESSURE WARNING. COULD NOT DUPLICATE. SYSTEM PRESSURE INDICATION NORMAL. 2L72 4F RTA21EA 20031028000312003102800031EA 2003 10 28 COMA0360434 120030927A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01477CA 7670 FLT 5275 FLAPS FAIL CAUTION MESSAGE WHEN SELECTED TO 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031028000352003102800035NM 2003 10 28 03266452 120030923A26127153552 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE FIRE WARNING INACCURATE A VTZAB EMER. DESCENT N FALSE WARNING DEDESCENT 1 EA27452FJ 3214 DURING APPROACH CREW RECEIVED A RT ENGINE FIRE INDICATION. CREW PERFORMED AN INFLIGHT SHUTDOWN AND INDICATION EXTINGUISHED. EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. PASSENGERS DEPLANED NORMALLY AT GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED FIRE EXTINGUISHING PANEL ENG AND INNERCORE FIRE WIRE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2H72 4T4 FRTA55NM E35NE 20031028000382003102800038NM 2003 10 28 MWEA030397 120030926A2460 BUSS TIE BOEING717 717200 1383700NM ENGINE FALSE INDICATIONA MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31902ME 55166 BUSS TIE RIGHT LOCKOUT. PERFORMED FAULT ISOLATION MANUAL PROCEDURES OPERATION CHECK GOOD, NO FAULTS AT THIS TIME. 2L72 4F TRA6WE 20031028000482003102800048EA 2003 10 28 03271629 120030928A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27629BR 7251 DURING INSPECTION A SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A SECTION OF EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031030000232003103000023NM 2003 10 30 UPS03441281 120030905A5712 RIB BOEING747 747121 1384871NM NR 26 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 26 V/C FLAP O/B LINKAGE I/B RIB NR 1 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000262003103000026NM 2003 10 30 UPS03441284 120030905A5712 RIB BOEING747 747121 1384871NM NR 19 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING - NR 19 V/C FLAP O/B LINKAGE O/B RIB NR 1, NR 6 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1, NR 6 AND NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000492003103000049NM 2003 10 30 UPS03441312 120030905A5712 RIB BOEING747 747121 1384871NM NR 4 V/C FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING - NR 4 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 4 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS NR R57-41-35067 AND AS PER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031031000102003103100010SO 2003 10 31 SWIA200312468 120030928A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07295SW6149 6149 120322 VARIOUS EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER ELBP IAW MM 33-50-00. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031031000262003103100026NM 2003 10 31 234TR0012 120030929A33501000677 LIGHT BOEING737 737228 13844AGNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05234TR 23004 EMERGENCY LIGHT ABOVE R1 DOOR INOP. REPLACED LIGHT ASSEMBLY. OPS CHECKS OK. 2L72 4F RTA16WE 20031031000302003103100030NM 2003 10 31 03FDEA01684 120031002A5713 STRINGER BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 LT WING STR 10 UPPER CRACKED AT TAB WING STA 656.50 ** SD ** COMING 2L73 4F RTA3WE 20031031000322003103100032NM 2003 10 31 MWEA030404 120031001A2751ST12BH TRANSMITTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE LT TE FLAP CORRODED A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31601ME 49762 LT FLAP INDICATION BEGAN SCROLLING UP AND DOWN FULL RANGE. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER AND CONNECTOR. 2L72 4F4 FRTA6WE E2EA 20031031000342003103100034WP 2003 10 31 4516610012003 220031001A7200 ENGINE LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP RIGHT MALFUNCTIONED E J7SAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW05430FX 166 P116326 RIGHT ENGINE QUIT IN-FLIGHT AT FL370. WAS PRECEEDED BY A RT ENGINE CHIP DETECTOR CAS MESSAGE, VERY HIGH OIL PRESSURE AND HIGH OIL TEMP. EMERGENCY DELARED AND UNSCHEDULED LANDING MADE WITHOUT INCIDENT. ENGINE CHANGE HAS BEEN PERFORMED AND ENGINE SENT TO SERVICE CENTER FOR TEARDOWN AND INVESTIGATION. 2L72 4F4 FRTT00008WIE6WE 20031031000422003103100042NM 2003 10 31 UPS03441333 120030906A5712 RIB BOEING747 747121 1384871NM NR 4 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 4 V/C FLAP OB LINKAGE IB RIB NR 1 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION. LT WING - NR 4 VC FLAP OB LINKAGE IB RIB ASSY REPLACED IAW SRM 51-10-01 P8 DUE ACTUATOR MOUNTING HOLES CORROSION REMOVAL EXCEED SRM 57-20-03 FIG 6 LIMIT. 2L74 4F A20WE 20031031000592003103100059NE 2003 10 31 QXEA200301209 220030930A7220 FAN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE ZONE 400 VIBRATION A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 NM09604QX 10019 965280 ON FLIGHT 2528 AIRCRAFT RETURNED TO FIELD DUE TO, LEFT ENGINE FAN VIBRATION 1.6 AFTER TAKEOFF, INCREASED TO 2.2 DURING CLIMB AT 25K, REDUCED TO AS LOW AS 1.6 WHEN POWER WAS AT IDLE. DEFINITE AIRFRAME VIBRATION FELT AND INCREASE CABIN NOISE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND LUBED NR 1 ENGINE FAN BLADES AND REINSTALLED BLADES AND SPINNER IAW CRJ TASK 72-21-02-400-801. 2L72 4F4 FRTA21EA E15NE 20031031000652003103100065NM 2003 10 31 DL777030830 120030910A2530 SEAT BOEING777 777232 1385232NM CABIN MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS M OVER TEMP CRCRUISE 1 SO27864DA 29736 SEAT 44D HEAT BUILD UP ON BOARD MECHANIC (DELTA) DISCONNECTED ELECTRONICS AT SEAT. REACTIVATED SEAT 44D. CHECKED ALL LIGHTS FANS/WATER/HEATERS IN AREA, NO SMOKE OR ODOR NOTICED SEAT 44D. NO EVIDENCE OF SMOKE OR OVERHEAT. DISCONNECTED AND STOWED 44D SEAT CONNECTIONS AND FWD IFES TO MCO/PLAC PRECAUTUONARY. MEL REF 25-25-02JC/BS PULLED/SECURED PER MEL ON P110/210 PANELS. 2L72 4F RTT00001SE 20031031000752003103100075NM 2003 10 31 DL757030841 120030912A5330146N37506 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27660DL 24422 THE FUSELAGE SKIN WAS FOUND WITH A DEEP DENT AT FS 1690 BETWEEN STRINGERS 18R & 19R. THE DENT WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385638-14, REV A. 2L72 4F RTA2NM 20031031000842003103100084NM 2003 10 31 DL76S030851 120030917A4990 APU BOEING767 767332 1382001NM APU BAY LEAKING A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27132DN17416 24981 62248 ODOR OF HOT AIR CONDITIONING, SMOKE DETECTORS ALL OVER AIRCRAFT WENT OFF. DESCENDED FROM 410 TO 310 AND SMOKE/ODOR DISSIPATED. ALL SMOKE DETECTORS DISABLED. UPON ENTERING A/C ODOR OF BURNED OIL. INSPECTED ENGS, APU AND PACK BAY AREAS AND ALL NORMAL. SUSPECT RESIDUAL OIL IN DUCTS FROM APU OIL LEAK. REF LOG E729128 ITEM OO1. PERFORMED REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEMS PER M/M 21-00-21. NO ODOR PRESENT FROM APU AIR SOURCE. RAN PACKS FROM ENGINES, NO ODOR PRESENT. BURN ODOR GONE AND NO SMOKE EVER PRESENT. CHECKS NORMAL. ENABLED ALL SMOKE DETECTORS. CHECKS NORMAL. 2L72 4F RTA1NM 20031103000062003110300006NM 2003 11 3 DL76G030858 120030920A2530 OVEN BOEING767 7673P6 1385105NM GALLEY BURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27154DL 25241 F/A REPORTS AFT GALLEY OVEN SMELLS BURNED AND HAS SCORCHED MARKS. THE 02 OVEN NR 4 SMELLS BURNED. REMOVED AND REPLACED OVEN. CHECKS GOOD MCO/PLACARD REMOVED. 2L72 4F RTA1NM 20031103000142003110300014NM 2003 11 3 DL757030866 120030923A2910 B-NUT BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENG HYD LOOSE A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27677DL 25982 728791 LT HYDRAULIC SYSTEM QUANTITY/PRESSURE LOSS. LT HYD QTY 1 GALLON REMAINING. FOUND LT ENG EDP HYD PRESS LINE B-NUT LOOSE AT FIREWALL FITTING. TIGHTENED SAME. CHECKED CASE/PRESSURE FILTER MODULE POP-OUT OK. SERVICED HYD QTY OPS CHECK AND LEAK CHECK GOOD. HYD PRESS NORMAL. 2L72 4F4 FRTA2NM E17NE 20031028000492003102800049NE 2003 10 28 AWXA200301108 220030926A7321FFG022AC GOVERNOR BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE FUEL FLOW FAULTY A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28913AW37078915 22207 DURING TAKEOFF, PILOT REPORTED THAT THE NR 1 ENGINE WOULD NOT MAKE T/O POWER. MAINT R&R NR 1 ENGINE FUEL FLOW GOVERNOR & PERFORMED T/O POWER TEST NR 13 IAW BMM. OPERATIONAL CHECK GOOD. EVALUATION OF FUEL FLOW GOVERNOR CONFIRMED FAILURE OF UNIT. ROTARY FACE SEALS & DRIVE SHAFT SLEEVE SEAL FOUND WORN BEYOND LIMITS, & TORQUE MOTOR SPRING FOUND BROKEN. R&R 2 EACH SEALS, SLEEVE SEAL, & TORQUE MOTOR SPRING UNIT REPAIRED AND TESTED IAW CMM 73-21-02, REV. 5. 2L72 4F4 FRTA2NM A12EU 20031028000522003102800052NM 2003 10 28 QXEA200301188 120030926A3350 SWITCH DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 WILL NOT TEST A QXEAO OTHER L NO TEST NRNOT REPORTED 1 NM09352PH 494 ON FLIGHT 2249 FLIGHT ATTENDENT EMERGENCY LIGHT TEST SWITCH IS INOPERATIVE. COMPLIED WITH EMERGENCY LIGHTS SYSTEM ADJUSTMENT/TEST IAW DHC-8 MM 33-51-00, SWITCH OPERATED NORMALLY. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031028000662003102800066SO 2003 10 28 C2XA03SH360 120030930A532014521725615 SILL EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE AFT SERVICE DOOR SILL AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031028000952003102800095NM 2003 10 28 03FDEA01639 120030926A750065266897 DUCT BOEING727 727100 1384036NM NR 3 ENGINE LOOSE A FDEAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO25168FE 18865 ON CLIMBOUT NR 3 GENERATOR BREAKER TRIPPED. OBSERVED GENERATOR DRIVE OIL TEMP PEGGED ON THE HIGH SIDE. COMPLIED WITH CSD HIGH OIL TEMP PROCEDURE AND CSD FAILED TO DISCONNECT. TEMP REMAINED HIGH THRU THE FLIGHT. FOUND CSD EJECTOR LINE LOOSE AT VALVE AND HOT AIR BLOWING ON ENGINE ELEC HARNESS, 7 WIRES SEVERED AND NUMEROUS OTHERS DAMAGED. CSD INJECTOR TUBE IS ALSO DAMAGED. NR 3 ENGINE HARNESS REMOVED AND NEW HARNESS BEING INSTALLED IAW SMP. CSD OIL COOLER INJECTOR TUBE REPLACED PER SMP RAN NR 3 ENG PER JRH. ALL SYSTEMS OPS CK GOOD. 2L73 4F RTA3WE 20031028000992003102800099NM 2003 10 28 03FDEA01601 120030908A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OUTBOARD FLAP - FOUND CORROSION ON INBOARD HINGE (FLAP SIDE) INBOARD AND OUTBOARD ACTUATOR LUGS BORES AND SPOT FACES. LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) INBOARD AND OUTBOARD ACTUATOR LUG BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT AS PER EA 1-5750-72698. WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031028001012003102800101NM 2003 10 28 03FDEA01569 120030918A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON SHEAR TIE BETWEEN STR 26L AND 27L, BS 1050. REMOVED AND REPLACED SHEAR TIE. 2L73 4F RTA3WE 20031028001092003102800109NE 2003 10 28 KMB2003F00000 220030813A7261ADA6848P BOWL SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE OIL FILTER WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 OIL FILTER BOWL WRENCH FITTING IS ROUNDED, WORN OUT. REPLACED WITH SERVICEABLE BOWL. 1G71 3U3 UNCH9EU E19EU 20031028001112003102800111NE 2003 10 28 AT0300028 220030927A7200JT8D9A ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE NR 2 UNSERVICEABLE A ZZDAEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO15836AT 47397 LOW OIL PRESSURE AND LOSS OF QUANTITY DURING CLIMB OUT AT 16,000 AND 300 KNOTS. REMOVE AND REPLACED THE NR 2 ENGINE 2L72 4F4 F A6WE E2EA 20031028001202003102800120SO 2003 10 28 SIMA200324605 120030813A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED NEW SILL IAW EMB 135 SRM, SRM 145/1142 REV 22, 51-40-02, 06, 51-20-03 EMB 145 CPM 51-21-04, 51-21-05. (M) 2L72 4F RTT00011AT 20031028001232003102800123EA 2003 10 28 A6WA200340141 120030924A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 GEN UNDERSERVICED A A6WAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 GL31422AW 7341 DURNG TAKEOFF, IDG 1 MESSAGE FOLLOWED BY GEN 1 MESSAGE. SERVICED IDG NR 1 WITH OIL IAW AMM 12-13-24. (M) 2L72 4F RTA21EA 20031028001252003102800125NM 2003 10 28 AALA20030407 120030404A3260MS250112 SWITCH BOEING737 737823 13844BZNM MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21958AN 30091 SFO - FLT 1608 - ENR OUTE SFO-ORD, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. RETURNED SFO AND LANDED WITHOUT INCIDENT. REPLACED MANUAL SYSTEM ACCESS DOOR SWITCH AND ACTUATOR. ACCOMPLISHED GEAR SWING. GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20031022001322003102200132NE 2003 10 22 2003UALA00687 220030912A7230 ACTUATOR BOEING747 747422 1384935NM PWA 4090 PW4090 52119NE NR 3 ENG VSV FAILED A UALAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 WP29197UA 26901 TOP OF DESCENT, NR 3 ENGINE SHUT DOWN. THE CAUSE OF THE IFSD WAS THE FAILURE OF THE STATOR VANE ACTUATOR. THE ACTUATOR EXPERIENCED A DUAL CHANNEL TRACK CHECK FAULT AND DID NOT GO TO THE COMMANDED POSITION. THE STATOR VANE ACTUATOR WAS CHANGED AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E46NE 20031027000062003102700006WP 2003 10 27 MWEA030392 120030925A53305911408507 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31209ME 47730 FUSELAGE SKIN HAS A DENT AT STATION 388 AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED FILLER AND DOUBLER. 2L72 4F4 F A6WE E2EA 20031027000442003102700044NM 2003 10 27 03FDEA01638 120030926A2780UNK SWITCH BOEING727 727200 138407ENM NR 6 L/E FLAP FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25496FE 21670 AFTER T/O NR 6 LED FAILED TO RETRACT. COMPLIED WITH QRH AND RETURNED TO MEM. REPEAT WRITEUP, NO DIRECTIONAL PROBLEMS. DURING CREW DEBRIEF, INDICATION WAS FOR NR 6 LEADING EDGE SLAT, NOT KRUEGER FLAP. AFTER TRANSLOAD, CYCLED FLAPS SEVERALTIMES AND FINALLY DUPLICATED PROBLEM WITH NR 6 SLAT AMBER {INTRANSIT} LIGHT ON BOTH FWD AND AFT PANELS. LEFT FLAPS EXTENDED FOR MORE T/S REF 727 MM 27-82-001-4. DURING T/S OPERATED L/E FLAPS AND SLATS APPROX 30 CYCLES. THE NR 6 FLAP IS THE ONLY LED THAT FAILED INDICATION, ABOUT 8 TIMES OUT OF TEN IT FAILED. AT NO TIME DID THE NR 6 SLAT FAIL INDICATION. INSTALLED FLAP POSITION SWITCH PER BOEING MM 27-82-0001-4. SYSTEM OPS CK OK. 2L73 4F RTA3WE 20031027001432003102700143WP 2003 10 27 DHL2003802013 120030926A2612 FIRE LOOP DOUG DC8 DC873 302199CWP GE CFM56 CFM56* 13802NE NR 2 ENGINE SHORTED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01802DH 46076 NR 2 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED ON LOOP (A). LOOP (B) OPS CHECKED NORMAL. CLEANED CONNECTOR ON NR 2 ENGINE SYSTEM OPS CHECK GOOD IAW DC8 M/M 26-10-0. 2L74 4F4 FRT4A25 E2GL 20031103000162003110300016NM 2003 11 3 DL777030868 120030924A2530 CHILLER BOEING777 777232 1385232NM AFT GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27877DA 29739 DURING FLT ELECTRICAL ODOR IN CHILLERS ON THE RT SIDE OF AFT GALLEY. CHILLERS TURNED OFF AND ODOR DISSIPATED. NOTE THE AFT GALLEY HEATER WAS TURNED ON PRIOR TO THE ODOR BEING NOTICED/REPLACED A3 RT AFT CHILLER. 2L72 4F RTT00001SE 20031103000222003110300022NM 2003 11 3 DL733030876 120030925A53306545768 SKIN BOEING737 737347 1384647NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312WA 23598 FUSELAGE/SKIN/FS430-460, S23R TO S27R - DENTS AND WEAR. THE SUBJECT DAMAGE IS CUT OUT FROM THE FUSELAGE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLER, TRIPLER AND STRUCTURAL FILLER IN ACCORDANCE WITH ER/A 385699-14. DAMAGE DUE TO CONTACT WITH GROUND EQUIPMENT. 2L72 4F RTA16WE 20031103000462003110300046WP 2003 11 3 03FDEA01702 120031004A7830901M81P06 PANEL DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 COMPLY WITH E.A.8-7830-73199. EXHUST SYSTEM-THURST REVERSER-FWD CRACK REPAIR. CLOSING ACTION ON 10/04/03.ON N/R S00017. COMPLIED WITH E.A.8-7830-73199.EXHAUST SYSTEM-THRUST REVERSER-FWD CLOSEOUT REPAIR. 2L73 4F A22WE 20031103000582003110300058NM 2003 11 3 03FDEA01686 120031002A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 STRINGER CLIP CRACKED AT BS 950C STRINGER 4 LT. REMOVED AND REPLACED STRINGER CLIP AT BS 950C STRINGER 4 LT IAW SRM 51-30-2 AND 51- 30-5. 2L73 4F RTA3WE 20031103000742003110300074NM 2003 11 3 GK42003F00000 120030818A3350 CHARGER DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE EMERGENCY LIGHT MALFUNCTIONED A GK4YO OTHER O OTHER NRNOT REPORTED 1 WP03614FE 48528 CREW REPORT ON AML: BEFORE START GOT (BATT CHARGER INOP) AND (EMER PWR TST FAIL) ALERTS. TROUBLESHOOTING IAW F/M 24-30-03-00 CARRIED OUT. BOTH MAIN REPLACED IAW AMM 24-32-02 IAW MMDC AD. BATTERY CHARGER REPLACED IAW AMM 24-34-03. EPCU REMOVED AND REPLACED IAW AMM 24-32-6. EMERGENCY INVERTER RCCB B1-134 REMOVED AND REPLACED IAW AMM54-50-1. CLEANED AND INSPECTED TERMINALS AT S4-1 SHUNT. REMOVED AND REPLACED BATTERY CHARGER RELAY R2-24 IAW SMP. CARRIED OUT EMERGNCY PWR TEST AND BATTERY TES IAW AMM 24-34-03. ALL OPS NORMAL. AIRCRAFT RELEASED TO SERVICE. 2L73 4F4 FRTA22WE E13NE 20031103000752003110300075EU 2003 11 3 DU22003F00000 120030916A771231017263 TORQUE SENSOR BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP ENGINE FAILED C DU2RO OTHER YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 SW05903EH 605 P42014C THE ENGINE SHUT DOWN ON FINAL APPROACH. IT WILL NOT BE KNOWN UNTIL THE ENGINE IS APART ON WHAT EXACTLY FAILED. IT IS SUSPECTED THAT THE TORQUE SENSOR FAILED. THE FAILURE OF THIS UNIT CAUSED THE ACCESSORY DRIVE FOR THE ENGINE DRIVEN FUEL PUMP TO STOP ROTATION, LOOSING FUEL TO THE ENGINE. THE OCCURANCE WAS ON SEPT 16, 2003. 2L72 4T4 TRTA21EU E4WE 20031103000782003110300078NE 2003 11 3 ALG2003F00072 120030909A3260 SQUAT SWITCH SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG MALFUNCTIONED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03917QS 760217 CAE890809S DURING TAKE OFF PHASE, THE LANDING GEAR WOULD NOT RETRACT, RETURNED TO ARA FOR MAINTENANCE. MAINTENANCE ADJUSTED WEIGHT ON WHEEL SWITCH IAW S76 MM. 1G72 3U3 U H1NE E1GL 20031028001392003102800139NM 2003 10 28 GAIA03103 120030910A5347 SEAT TRACK BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2, FOUND MAIN CABIN SEAT TRACK CORRODED BS 360 BL0. ERF FASI N/R 53268, REPLACED SEAT TRACK BS 344-480 BL 0 PER B727 SRM 53-10-5 FIG 7. (M) 2L73 4F A3WE 20031028001432003102800143NM 2003 10 28 GAIA03097 120030910A5720 STIFFENER BOEING727 727223 1384074NM LT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND LEFT WING REAR SPAR VERTICAL STIFFENER CRACKED AT WS 556. REF FASI N/R 53206, REPLACED STIFFENER PER B727 SRM 51-30-2. (M) 2L73 4F A3WE 20031028001472003102800147EA 2003 10 28 ASOA03490 120031006A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE ATTACH ANGLE UNDER THE RIGHT FORWARD FLOOR PANEL INBOARD OF THE SERVICE DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ATTACH ANGLE UNDER THE RIGHT FORWARD FLOOR PANEL INBOARD OF THE SERVICE DOOR IAW SRM 51-00. (M) 2L72 4F RTA21EA 20031028001512003102800151NM 2003 10 28 GAIA03085 120030910A5753 FLAP TRACK BOEING727 727223 1384074NM TE FLAPS CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND NR 5 FLAP TRACK SPACER BLOCK CRACKED AT WBL 124. REF FASI N/R 50408, INSTALLED OVERSIZE FASTENERS IAW S/B 727-57-136 REV 1, FIGURE 2. (M) 2L73 4F A3WE 20031028001532003102800153NM 2003 10 28 GAIA03089 120030910A5311 FRAME BOEING727 727223 1384074NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 580 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53132 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F A3WE 20031028001592003102800159NM 2003 10 28 GAIA03106 120030910A5311 FRAME BOEING727 727223 1384074NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 950E HAS A DENT BY STRINGER 25L. REF FASI N/R 53292. FABRICATED DOUBLER REPAIR FROM 7075-T6, .080, DIMENSIONS 17.75 INCH BY 2.5 INCHES REPAIRED IAW B727 SRM 51-10-2. (M) 2L73 4F A3WE 20031028001622003102800162NM 2003 10 28 GAIA03094 120030910A5315 FLOORBEAM BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURNG B-2 CHECK, FOUND MAIN CABIN FLOORBEAM ANGLE CORRODED LBL 60 BS 848. REF FASI N/R 53138 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-1 FIG 1. (M) 2L73 4F A3WE 20031028001672003102800167EU 2003 10 28 ASOA03458 120030924A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11640AS 405 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031028001862003102800186NM 2003 10 28 ASAA0340094 120030228A531065C25008 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE AT BS 727B RBL 1 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000222003102900022NM 2003 10 29 ASAA0340070 120030227A53206916500 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 727A-B AND RBL 3 WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000302003102900030EA 2003 10 29 ASOA03459 120030926A52106003188715 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND DIFFICULT TO CLOSE AND SECURE FROM THE INSIDE. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE AND RE-SEATED THE BEARING ON THE LOWER RIGHT ROLLER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031029000462003102900046NM 2003 10 29 ASAA0310405 120030506A5330655965819 DOUBLER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC- DURING C-CHECK, FOUND DOUBLER AT BODY STATION 947, LEFT BUTTOCK LINE 45.5 CORRODED. REMOVED CORROSION AND REPLACED DOUBLER PER SRM. (M) 2L72 4F A16WE 20031029001302003102900130NE 2003 10 29 KBM2003F00025 220030917A73100301037060 PIPE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE FUEL SYSTEM CHAFED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 5690 2300 PIPE CHAFED DUE TO CONTACT WITH BLEED VALVE WASH KIT. REPLACED PIPE WITH SERVICEABLE ITEM.(K) 1G71 3U3 UNCH9EU E19EU 20031022001462003102200146EA 2003 10 22 SWIA200312431 120030922A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INBOARD AND OUTBOARD ANGLES AT FS 280 RT RBL 9.0 FLOORBEAM REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-58 2L72 4F4 FRTA21EA E15NE 20031022001562003102200156EU 2003 10 22 RAIA00309244 120030914A243523095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP RT ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03554HK435 41067 5567-SPI- RIGHT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED STARTER GENERATOR. 2L72 4T3 TRTA41NM E2WE 20031023000392003102300039 2003 10 23 AWXA200301087 420030923A256560592101 RESERVOIR AIRBUSA319 A319132 3930340NM RT OVERWING LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW5518 1291 1178 DURING INSPECTION THE RT OVER WING EMERGENCY EVACUATION SLIDE BOTTLE WAS FOUND TO HAVE LOW PRESSURE. MAINTENANCE REMOVED AND REPLACED THE RT OVER WING EMERGENCY EVACUATION SLIDE BOTTLE IAW AMM 25-62-46-000-001, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN OF R/H OVER WING EMERGENCY EVACUATION SLIDE BOTTLE S/N 4733 CONFIRMED FAILURE OF UNIT. UNIT WAS FOUND TO HAVE LOW PRESSURE DUE TO A LEAK, REPAIRED LEAK AND PERFORMED LEAK CHECK. MAINTENANCE ACCOMPLISHED IAW CMM 25-65-17, REV. 8. 2L72 4F RTA28NM 20031023000432003102300043EU 2003 10 23 AWXA200301091 120030915A3230D57251041 NUT AIRBUS320 A320232 3930326EU MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON THE RT MAIN LANDING GEAR FORWARD PINTLE BEARING RETAINING NUT THREADS. MAINTENANCE REMOVED AND REPLACED THE RT MAIN LANDING GEAR FORWARD PINTLE BEARING RETAINING NUT IAW A320 SRM 57-26-13, PG. 201-202, & 222-230, FIG. 203. 2L72 4F RTA28NM 20031023000722003102300072EA 2003 10 23 COMA0360425 120030923A5240601R313613 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SERVICE DOOR TORN A COMAD RETURN TO BLOCK O OTHER CLCLIMB 1 SO01934CA 7042 FLIGHT 5920 HIGH PITCH NOISE FROM SERVICE DOOR DURING CLIMB, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE SERVICE DOOR SEAL. 2L72 4F4 FRTA21EA E15NE 20031027000342003102700034NM 2003 10 27 PCAA0309116 120030924A2611 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE CARGO SMOKE FALSE INDICATIONA PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13814EX 318 CREW REPORTED THAT THE SMOKE WARNING LIGHT HAD ILLUMINATED INTERMITTENTLY IN FLIGHT. CHECK LIST WAS COMPLETED, AND NO SMOKE WAS FOUND IN THE CARGO COMPARTMENT. IT WAS SUSPECT THAT THERE WAS INTERFERENCE FROM A HEARING AID IN SEAT 8A. MAINTENANCE INSPECTED THE CARGO SMOKE DETECTORS. NO VISUAL DAMAGE WAS FOUND. CARGO SMOKE TEST PERFORMED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031027000782003102700078EU 2003 10 27 MALA030428 120030909A2720 PEDAL SAAB SF340 340B 7860101EU RUDDER FROZEN A MALAH DEACTIVATE SYST/CIRCUITS O OTHER APAPPROACH 1 GL15365PX 340B265 DURING APPROACH ON FLIGHT 2906, RUDDER PEDALS CONTROL ALMOST COMPLETELY UNMOVABLE (FELT AS IF GUST LOCK WAS ENGAGED). FLT CONTROLS FREE AND FULL ON GROUND W/ GUST LOCK DISENGAGED YAW DAMPER AP OFF. INSPECTED RUDDER & ATTACHMENTS FOR CONDITION AND SECURITY, ALL CHECKS GOOD. MAINTENANCE COULD NOT DUPLICATE. FROM LOG PAGE 1212595, COMPLETED FUNCTIONAL AND SYSTEM SELF TEST IAW 27-21-45 AMM OF RUD LIM SYS. CHECK GOOD. INSPECTED RUDDER PEDALS, TAIL COMPARTMENT RUDDER CONTROL AND RUDDER ASSY. NO DEFECTS NOTED. COMPLETED OPERATIONAL CHECKS OF RUDDER GUST LOCK AND YAW DAMPER/AUTOPILOT CONTROL IAW SF 340 MM. ALL CHECKS GOOD AT THIS TIME. MXC NOTIFIED. REMOVED FROM DMR. 2L72 4T RTA52EU 20031027000832003102700083WP 2003 10 27 DHL2003873013 120031017A5280 DOOR DOUG DC8 DC873F 302199FWP MLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01873SJ 46091 LANDING GEAR DOOR UNLATCHED LIGHT WITH GEAR UP ON. COMPLETED ABNORMAL PROCEDURE LIGHT REMAINED ON. COMPLIED WITH RESTRICTIONS IN ABNORMAL PROCEDURE. MAY BE INOPERATIVE PER MEL 32-16-2 DMI 14484 PLACARD INSTALLED. REF. DMI 14484 LANDING GEAR DOOR UNLATCHED LIGHT WITH GEAR UP REMAINED ON. CHECKED TARGET STOPS, FOUND LEFT-HAND OUT OF ALIGNMENT. ADJUSTED IAW 32-60-0,OPS CHECKS NORMAL. THIS CLEARS DMI 14484 PLACARD REMOVED. 2L74 4F RT4A25 20031027000862003102700086NM 2003 10 27 2003UALA00693 120030917A2460 CIRCUIT BREAKER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A UALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 WP29335UA 24230 LANDED MCI UNDER AMBER ALERT DUE TO ELECTRICAL AND PRESSURIZATION PROBLEMS. FOUND NR 1 TRANSFER NORMAL CIRCUIT BREAKER POPPED. COULD NOT DUPLICATE PROBLEM ON THE GROUND DURING TROUBLESHOOTING. REPLACED CIRCUIT BREAKERS C819, C826, C806, AND NR 1 TRANSFER UNIT. BASED ON PREVIOUS HISTORY THE NR 1 TRANSFER NORMAL CIRCUIT BREAKER (C819) IS SUSPECT AS THE CAUSE OF THE PROBLEM. 2L72 4F4 FRTA16WE E2GL 20031027000892003102700089CE 2003 10 27 DXTA200300128 120030928A21207756024 HEAT EXCHANGER CESSNA500 560CESSNA 2076750CE CABIN COOLING DIRTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07320QS 5600321 DURING ENROUTE FROM PHL TO ACK, NOTICED A BURNING ELECTRICAL ODOR FOLLOWED BY THE EMERGENCY PRESSURIZATION LIGHT. ACCOMPLISHED AIR TURN BACK TO PHL CLEANED LINTS AND DEBRIS FROM 3RD HEAT EXCHANGER COOLING FINS, RAN AIRCRAFT WITH NO ABNORMAL INDICATIONS FROM THE AIR-CONDITIONING SYSTEM (HOT AND COLD, NORMAL AND MANUAL). ALL WORK PERFORMED IAW CE560 MM CHAPTER 21-11-00, 21-31-04 AND 21-51-00. 2L72 4F RTA22CE 20031028000502003102800050EA 2003 10 28 03271667 120030928A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27667BR 7535 DURING INSPECTION THE EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED A SATISFACTORY OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031028001242003102800124EU 2003 10 28 A6WA200360039 120030922A5330 SKIN BAC 146 146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 RIGHT FUSELAGE SKIN AT FRAME 32 ABOVE STRINGER 19 HAS A .0250 INCH CRACK ORIGINATING AT FASTENER. REPAIR I/P. (M) 2H74 4F A49EU 20031028001332003102800133NM 2003 10 28 GAIA03104 120030910A5311 FRAME BOEING727 727223 1384074NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND AFT CARGO FRAME DENTED BS 1070 AT STRINGER 25 RT. REF FASI N/R 53281, DOUBLER REPAIR IAW B727 SRM 53-10-2 FIG 5. (M) 2L73 4F A3WE 20031028001422003102800142NM 2003 10 28 GAIA03095 120030910A5315 FLOORBEAM BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM BS 480 CORRODED AT LBL 30 AND CRACKED AT LBL 59. REF FASI N/R 53187, CUT OUT DAMAGED AREA, INSTALLED REPAIR PER B727 SRM 53-10-8 FIG 1. (M) 2L73 4F A3WE 20031028001602003102800160NM 2003 10 28 GAIA03092 120030910A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN STRINGER 15 RT CRACKED AT AFT SIDE OF BS 720B. REF FASI N/R 53135, ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M) 2L73 4F A3WE 20031028001832003102800183NM 2003 10 28 ASAA0340103 120030301A5310 SHEAR TIE BOEING737 7374Q8 138447QNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 767 RBL 13 AND WL 160. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000052003102900005EA 2003 10 29 ASOA03474 120031002A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 DURING A C-CHECK IN MCN, THE FLOOR EMERGENCY FLOOR LIGHT NEAR THE FLIGHT ATTENDANTS STATION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY FLOOR LIGHT LAMP NEAR THE FLIGHT ATTENDANTS STATION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031029000212003102900021WP 2003 10 29 ASAA0380572 120030831A335060020451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01954AS 49387 SEA LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS FOUND INOPERATIVE AT THREE LOCATIONS. REPLACED ASSOCIATED BATTERIES. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20031029000392003102900039EU 2003 10 29 USAASA03101 120030830A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19756US 1340 THE AFT LT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE BATTERY ON THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031029000402003102900040EU 2003 10 29 USAASA03098 120030825A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19717UW 1069 AN AFT EMERGENCY POWER SUPPLY UNIT WAS FOUND BAD DURING TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. (M) 2L72 4F RTA28NM 20031029000562003102900056NM 2003 10 29 ASAA0240215 120030401A532065479573 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND AFT CARGO DOR WAY THRESHOLD WEB IS CORRODED AT CORNER NUT PLATES. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000582003102900058NM 2003 10 29 AMTA200301174 120030916A2842 INDICATOR BOEING757 75723N 1384973NM COCKPIT INACCURATE A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11517AT 27973 TOTAL FUEL DIFFERS FROM CAPTAIN. TOTAL FUEL DIFFERS FROM CAPTAIN AND F/O CALCULATED FUEL QUANITY FUEL QTY ERROR, PROG 2/2. ALT MESSAGE. (M) 2L72 4F RTA2NM 20031029000602003102900060NM 2003 10 29 ASAA0240222 120030401A532065C2614311 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 PAE - DURING C-CHECK, FOUND WX RADAR SHELF CHANNEL CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000632003102900063NM 2003 10 29 ASAA0340092 120030228A53106546552 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE BS 827 LBL 2 AND WL 158. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000682003102900068WP 2003 10 29 ASAA0380533 120030709A56105912290506 WINDOW DOUG DC9 DC982 3022082WP COCKPIT STIFF A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 PREFLIGHT CHECK, RIGHT SLIDING CLEARVIEW WINDOW IS HARD TO OPEN. ADJUSTED (RE-RIGGED) WINDOW. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20031107000612003110700061NM 2003 11 7 03303424 120031030A3150327410 WARNING SYSTEM DORNERDO32 DO328300 NM COCKPIT INOPERATIVE A VTZAO OTHER P NO WARNING INDICATION UKUNKNOWN 1 EA27424FJ 3185 MASTER WARNING SYSTEM IDENTIFIED AS INOPERATIVE. THE RED WARNING PANEL WAS REPLACED. 2H72 4T RTA55NM 20031107000712003110700071 2003 11 7 03309643 420031105A22136229815704 CIRCUIT CARD CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS FAULTY A VTZAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 EA27643BR 7363 DURING FLIGHT THE AIRCRAFT EXPERIENCED EXCESSIVE YAW WITH NO YAW DAMPER FAIL INDICATIONS. THE NR 2 FCC CARD WAS REPLACED. 2L72 4F RTA21EA 20031107001002003110700100WP 2003 11 7 MWEA030437 120031031A3350079123 LIGHT DOUG DC9 DC932 3022066WP CABIN LOOSE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31209ME 47730 EMERGENCY EXIT LIGHT FOR SERVICE DOOR AFT SIDE HAS COME LOOSE FROM TOP SIDE. REMOVED AND REPLACED EEPLS EXIT LIGHT FOR SERVICE DOOR. 2L72 4F A6WE 20031107001082003110700108EU 2003 11 7 AALA20030667 120030615A3397 WIRE HARNESS AIRBUS300 A300B4605R 3930308EU CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114061 471 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23G INOPERATIVE. REPLACED SEAT HARNESS AT SEATS 23G AND 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031107001142003110700114EA 2003 11 7 ASOA03477 120031003A5260601R3177351 STEP CNDAIRCL600 CL6002B19 1900309EA PAX STAIRS CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 DURING A C-CHECK IN MCN, THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031105000202003110500020EA 2003 11 5 COMA0370040 120031019A27011205722 BEARING CNDAIRCL600 CL6002C10 1390015EA CONTROL YOKE STICKING A COMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01390CA788 10106 FLIGHT 9463, DURING SMALL BANK TURNS, STICKING CAN BE FELT IN AILERONS. REPLACED THE CONTROL WHEEL BEARINGS IN COPILOTS CONTROL YOKE. 2L72 4F RTA21EA 20031105000382003110500038WP 2003 11 5 ABXA030397 120031007A522059131951 PAN DOUG DC9 DC931 3022065WP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 LEFT AFT OVERWING DOOR HAD CRACKED DOOR PAN AT STOP NR 6. REPAIRED AREA IAW DC-9 SRM 52-05. 2L72 4F A6WE 20031105000482003110500048NM 2003 11 5 CALA0300612 120031031A532065C807351 CHANNEL BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914654 28915 R2 DOOR JAMB Z-CHANNEL CORRODED AT STA 992.8. REMOVED AND REPLACED CORRODED Z-ANGLE AT R2 DOOR PER SRM 51-40-02. 2L72 4F RTA16WE 20031105000522003110500052NM 2003 11 5 SWAA032305 120031020A3350101114 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER LENS LOOSE. SECURED LENS COVER PER MM. 2L72 4F RTA16WE 20031105000782003110500078NM 2003 11 5 03FDEA01833 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE INBOARD PIVOT LUG BORE OUTBOARD SURFACE FOUND CORROSION. 2L73 4F RTA22WE 20031106000382003110600038SO 2003 11 6 C2XA03SH406 120031022A532014522460013 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031106000682003110600068NM 2003 11 6 SWAA032298 120031018A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C1 CHECK, FOUND PRESS BULKHEAD CRACKED AT BS 1016, STR 6L AT THE Y-CHORD ATTACH AREA. REPAIRED BULKHEAD PER SRM. 2L72 4F RTA16WE 20031106000702003110600070NM 2003 11 6 SWAA032300 120031019A2121215201 GASPER FAN BOEING737 7373H4 1384600NM E/E BAY MALFUNCTIONED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29369SW 26580 F/A'S REPORTED SMELL OF ELECTRICAL SMOKE IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20031106000732003110600073NM 2003 11 6 03FDEA01823 120031029A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-111-01, 3) LWR CHORD OF FLOORBEAM BS 1110, RBL 38, WL 201. *S/D* REMOVED CORROSION AREA 1.5 X 3 X .029 INCH DEEP FROM ORIGINAL .150 FOUND OUT OF LIMITS PER SRM 53-10-1 FIG 4. REPAIRED LWR CHORD OF FLOORBEAM BS 1110 RBL 38 WL 201 PER SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 20031106001722003110600172NM 2003 11 6 03FDEA01866 120031103A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION WHILE WORKING CARD N01362, FOUND CORROSION ON FLOORBEAM STA 312 RBL 14 WL 208. 2L73 4F RTA3WE 20031106001982003110600198NM 2003 11 6 ASAA0310519 120030723A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 8-11 INOPERATIVE. REPLACED BATTERY PACKS, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20031106002222003110600222NM 2003 11 6 ASAA0310459 120030515A53206548866505 SPLICE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE KEEL BEAM SPLICE ANGLES AT FUSELAGE STATION 727-727A, RIGHT BUTTOCK LINE 6 CORRODED. REPLACED SPLICE ANGLES PER SRM. (M) 2L72 4F A16WE 20031107001422003110700142NM 2003 11 7 ASAA0310488 120030526A5330654576939 SKIN PANEL BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE INNER SKIN PANEL AT FUSELAGE STATION 492, STRINGER 27R-28R CORRODED. REPAIRED SKIN PANEL PER EA. (M) 2L72 4F A16WE 20031107001582003110700158NM 2003 11 7 AALA20031048 120030920A2530 COFFEEMAKER BOEING767 767323 1385205NM AFT GALLEY DIRTY A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21390AA 27450 LGW - FLT 134 - EN ROUTE STL-LGW, CREW REPORTED SMOKE IN AFT GALLEY. PULLED CIRCUIT BREAKER AND SMOKE DISSIPATED. FOUND DEBRIS ON COFFEE MAKER NR 6. REMOVED DEBRIS NO SMOKE. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031107001592003110700159NM 2003 11 7 AALA20031045 120030920A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21696AN 26976 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT DOOR L4. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031110000412003111000041 2003 11 10 COMA0360486 420031105A31406229820008 DCU CNDAIRCL600 CL6002B19 1900309EA E/E BAY FAULTY A COMAD RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01477CA7855 7670 FLIGHT 5458 REJECTED TAKEOFF DUE TO A RUDDER CONFIGURATION WARNING, AIRCRAFT RETURNED TO THE GATE. REPLACED THE NR 2 DCU. 2L72 4F RTA21EA 20031110000432003111000043SO 2003 11 10 C2XA03TY195 120031008A531514521700001 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 TYS DURING A SCHEDULED 3C INSPECTION THE LT OMEGA BEAM WAS FOUND CORRODED. MAINT REMOVED CORRODED AREA, FABRICATED A NEW DOUBLER AND INSTALLED FILLER, SHIMS, PLATE AND DOUBLER. ALODINED, PRIMED AND REPAINTED WORK AREA. REINSTALLED RAMP ANGLE. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-21-04; 51-40-02 AND EMB 135/145 CPM51-21-04/05/06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031110000492003111000049EU 2003 11 10 RAIA00310272 120031027A3060306015 BRUSH BLOCK JETAIRJETSTMJETSTM4101 1500501EU LT PROPELLER WORN A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03553HK 41066 5371-BWI- LEFT PROP HEAT FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 PROP DEICE BRUSH BLOCK. 2L72 4T RTA41NM 20031110000522003111000052EU 2003 11 10 RAIA00311278 120031102A33506134031 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK 41040 MX-STL- EXIT LIGHT OUT ON LAV DOOR. REMOVED AND REPLACED POWER SUPPLY. 2L72 4T RTA41NM 20031110000532003111000053SO 2003 11 10 C2XA03SH435 120031109A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031106001182003110600118NM 2003 11 6 SWAA032266 120031016A33506104789 BATTERY PACK BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 EEPLS INOP AT ROW 16. REMOVED AND REPLACED BATTERY PACK. 2L72 4F A16WE 20031106001342003110600134NM 2003 11 6 SWAA032272 120031016A53106558280 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031106001922003110600192NE 2003 11 6 SWAA032280 220031014A7200CFM56 ENGINE BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE NR 1 FAILED A SWAAA UNSCHED LANDING Y ENGINE STOPPAGE TOTAKEOFF 1 SW29709SW 27843 875195 ENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURN BACK, NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20031107001262003110700126SO 2003 11 7 SIMA200327911 120031005A531514521713005 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 ABI - DURING AN IMBV INSPECTION, THE GALLEY HAT BEAM AT FRAME 22 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED AN NDT INSPECTION. CLEANED, TREATED AND APPLIED EPOXY PRIMER TO BLENDED AREA. FABRICATED A DOUBLER REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-10 FIGURE 207. (M) 2L72 4F RTT00011AT 20031107001402003110700140NM 2003 11 7 ASAA0310437 120030512A53206559658 INTERCOSTAL BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND INTERCOSTAL AT BODY STATION 947-967, LEFT BUTTOCK LINE 45, LEFT BUTTOCK LINE 55 CORRODED. REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F A16WE 20031027000902003102700090NE 2003 10 27 UPS03841454 220031021A7261 ENGINE DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE NR 1 LEAKING A IPXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01866UP 45966 INSPECTION TYPE: C1, ENG 1 BEGAN RAPIDLY LOSING OIL QUANITY PASSING FL 250. THE OIL PRES SURE ALSO DROPPED TO 35 PSI. THE CREW COMPLETED THE INFLIGHT ENGINE SHUTDOWN CHECK LIST. DECLARED AN EMERGENCY AND RETURNED TO SAT FOR AN UNEVENTFUL LANDING. FOUND STARTER FILL PLUG LOOSE (DISCONNECTED), SERVICED STARTER AND ENGINE OIL CKD ENG CHIP DETECTORS, NO DEFECTS NOTED. DETECTORS WERE CLEAN RAN ENGINE AT IDLE NO LEAKS NOTED. RAN ENG AT T/O POWER 3 TIMES FOR 2 MINS EACH, OIL QUANTITY REMAINED STABLE & OIL PRESSURE GOOD. REMOVED AND REPLACED ENG STARTER (PRECAUTIONARY). 2L74 4F4 FRT4A25 E2GL 20031027000912003102700091NM 2003 10 27 AWXA200301095 120030923A2910 LINE BOEING737 737277 1384570NM HYD SYSTEM LEAKING A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28184AW 22651 DURING DECENT INTO DFW EN ROUTE FROM PHX (A) SYSTEM HYDRAULIC QUANTITY INDICATOR BEGAN SHOWING LOSS OF FLUID. FLUID LEVEL DROPPED TO APPROX .7500 OF A GAL REMAINING. EMERGENCY EQUIPMENT CALLED OUT AS A PRECAUTION. MAINTENANCE FOUND THE NOSE LANDING GEAR ACTUATOR (UP-LINE) LEAKING, REPLACED HYDRAULIC LINE IAW BMM 20-10-52, OPERATIONAL AND LEAK CHECK WAS GOOD. 2L72 4F RTA16WE 20031027000972003102700097NM 2003 10 27 ASAA02402EE 120030407A510065458595 DOOR BOEING737 7374Q8 138447QNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND AFT GALLEY SERVICE DOOR UPPER AFT INNER CORNER CHAFED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001022003102700102NM 2003 10 27 ASAA02402II 120030412A532065C1612935 STANCHION BOEING737 7374Q8 138447QNM WX RADAR RACK CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND CRACK IN WEATHER RADAR SHELF. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001062003102700106NM 2003 10 27 ASAA02401MM 120030329A5311 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND CORRODED FRAME AT BS 500B. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001122003102700112NM 2003 10 27 ASAA02402QQ 120030407A5320654961688 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001162003102700116NM 2003 10 27 ASAA02402SS 120030331A572065508211071 SUPPORT BRACKET BOEING737 7374Q8 138447QNM RT WING WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND RT WING TRAILING EDGE LOWER SURFACE PANEL SUPPORT BRACKET WORN AT NR 5 SPOILER OUTBOARD ACTUATOR. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001182003102700118NM 2003 10 27 ASAA02402UU 120030401A531465C32953 KEELBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND LEFT KEELBEAM IS CORRODED AT FUSELAGE DRAIN. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027001242003102700124NM 2003 10 27 QXEA200301185 120030924A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 4 FLAP TRACK RIGHT WING OUTBOARD FORWARD MAIN ROLLER TRACK SURFACE IS PITTED. REPAIRED IAW EA 2-57-234. 2H72 4T4 TRTA13NM E20NE 20031027001352003102700135 2003 10 27 SWAA032093 420030919A2565 INDICATOR BOEING737 7372H4 138448CNM SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20031028000072003102800007 2003 10 28 03FDEA01653 420030927A22104059001908 COMPUTER DOUG MD11 MD11 3023602NM FLT CONTROL INOPERATIVE A FDEAJA DUMP FUEL UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO25578FE3624 3624 48458 IMMEDIATELY AFTER TAKEOFF, FUEL AND MISC CUE ALERTS CAME ON. (FUEL ALERT, LEVEL 1 (TANK 3 FWD PUMP OFF). MISC CUE ALERT, LEVEL 1 (NO AUTOLAND). ADDITIONALLY, PFD AUTOPILOT BOX WENT AMBER, WITH (AP OFF) DISPLAYED. NEITHER AP WOULD ENGAGE AT 500 FT AGL, AFTER CYCLING THE SWITCH (AUTOFLIGHT BUTTON). REFERRED TO QRH AND HAND FLEW THE AIRCRAFT AS MAINTENANCE WAS CONSULTED. RETURNED TO PANC AFTER FUEL DUMP (50 K LBS). LANDING UNEVENTFUL. REMOVED AND REPLACED FCC NR 2 IAW MM 22-01-03 AFS RTS ACCOMPLISHED IAW MM 22-01-10-5. 2L73 4F RTA22WE 20031028000082003102800008NM 2003 10 28 03FDEA01652 120030926A5200ABM7063501 DOOR DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE RAM AIR SEPARATED A FDEAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO25589FE3915939159 48491 MODERATE SOUNDING BANG AT CRUISE ALT 33,000 FT APPEARED TO BE AROUND FUSELAGE AREA BELOW CAPT. SEAT. NO ABNORMAL ENG/HYD/AIR INDICATIONS. A/C INSPECTED FOR POSSIBLE BIRD STRIKE. THIS WAS NOT A BIRD STRIKE NR 1 RAM AIR SCOOP DOOR CAME OFF IN FLIGHT DOOR ON ORDER. FACT REMOVED AND REPLACED NR 2 RAM AIR INLET DOOR ASSY IAW AMM 21-55-01-41 AND 21-62-14-5 1. OP CHECKS AND LEAK CHECKS GOOD. 2L73 4F4 FRTA22WE E13NE 20031028000092003102800009NM 2003 10 28 C1HA200393015 120030929A3350 BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 FWD CABIN EMERGENCY EXIT OVER HEAD SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACK , OPS CHECK NORMAL 2L73 4F A3WE 20031028000132003102800013NM 2003 10 28 C1HA200394018 120030926A3234 SWITCH BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE MLG SELECTOR MALFUNCTIONED A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15294AS 22146 ON DEPARTURE RETRACTED THE GEAR AND HAD THREE RED GEAR LIGHTS ILLUMINATED AT REMAINED ILLUMINATED. CLEANED GEAR HANDLE POSITION POSITION SWITCH S92 IAW B727MM32-60-0 OPS CK GOOD IAW B727MM32-60-0. 2L73 4F4 F A3WE E2EA 20031028000162003102800016NM 2003 10 28 UPS03441268 120030905A53107075T60071IN DOOR FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D- R1 DOOR AFT UPPER STOP FITTING AREA DOOR FRAME FOUND CRACK. M/D - R1 DOOR AFT UPPER STOP FITTING AREA DOOR FRAME REPAIRED AS PER RS R52-11-35073 AND UPS ENGINEERING FILE 747-52-20007. 2L74 4F A20WE 20031107001502003110700150WP 2003 11 7 GTIA030741 120030904A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW- FORWARD PIT CEILING WEB CORRODED/CRACKED RBL 57 INCHES STATION 294-313. CUT OUT DAMAGE. FABRICATED WEB AND DOUBLER. INSTALLED WEB AND DOUBLER. (M) 2L72 4F A6WE 20031107001562003110700156NM 2003 11 7 ASAA0310464 120030515A5315BAC1518431 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 480, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 45.5 CORRODED. REMOVED DAMAGE AND REPAIRED PER EA. (M) 2L72 4F A16WE 20031110000652003111000065SO 2003 11 10 C2XA03SH442 120031110A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110000732003111000073CE 2003 11 10 AMWA70 120031105A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE23 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED AT FWD CENTER STRINGER INTERSECTION. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031110000752003111000075CE 2003 11 10 AMWA72 120031105A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07165YV UE165 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED ONCE ON THE RIGHT SIDE. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031110001182003111000118 2003 11 10 03289317 420031016A22117010680938 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AUTOPILOT SYS FAULTY A VTZAK NONE O OTHER NRNOT REPORTED 1 EA27317UE 41031 THE ELECTRIC ELEVATOR TRIM WAS IDENTIFIED AS BEING INOPERATIVE AND THE AUTOPILOT SYSTEM WAS DISENGAGED TO IN ABLE MANUAL TRIM VIA THE TURN WHEEL. THE FCC CARD IN THE AUTOPILOT COMPUTER WAS REPLACED. 2L72 4T RTA41NM 20031110001402003111000140NM 2003 11 10 C8GA20030024 120031011A3230 ACCESS PANEL BOEING727 7272A1 138407FNM EXTERNAL POWER OPEN A C8GAA UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CLCLIMB 1 SO15287SC 21345 FLT 738 FROM TOL TO MMIO. DURING CLIMB OUT THROUGH FL270 A NOISE VIBRATION COMING FROM OUTSIDE RIGHT COCKPIT CAUSING AIRCRAFT TO GIVE ABNORMAL CRUISE READING. NOISE INCREASE WITH AIRSPEED INCREASE, NOSE GEAR LIGHT INDICATED CORRECTLY AT THIS TIME. HOWEVER, NOSE GEAR LIGHT WOULD NOT TEST WHEN THE NOSE GEAR WAS IN THE UP POSITION. A PHONE PATCH WAS MADE TO COMPANY TO REQUEST DIVERSION TO BRO AND THE ATC WAS NOTIFIED OF THE PLAN. THE AIRCRAFT DID A FLY BY AND THE TOWER CONFIRMED THE GEAR DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. UPON LANDING AND INSPECTING THE AIRCRAFT, THE AIRCRAFT VIBRATION WAS DUE TO THE EXTERNAL POWER ACCESS DOOR WAS FOUND TO BE OPEN. DURING FURTHER TROUBLESHOOTING OF THE LANDING GEAR RETRACT2L73 4F A3WE 20031110001502003111000150NM 2003 11 10 AWXA200301349 120031013A5315146N5447 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON NUT PLATES LOWER SIDE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1470, RBL 20. MAINTENANCE REMOVED DAMAGED FLOORBEAM FROM BS 1440 TO BS 1500, RBL 20; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11 PG 1-7. 2L72 4F RTA2NM 20031110001542003111000154NM 2003 11 10 C1HA200381031 120031026A2612 FIRE LOOP BOEING727 7272S7 138407ZNM NR 3 ENGINE OUT OF POSITION A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15681CA 22020 NR 3 GROUND FAULT ILLUMINATED IN FLT. COMP WITH COM PROCEDURE INSPECTED AND RESCHEDULED PER MEL 26-9, CAT-C, C/N C05473. MC NOTIFIED, PLACARDS INSTALLED. (ITEM RESOLVE UNDER MDDR: C05473). REPOSITION NR 3 ENG FIRE LOOP IAW B727 MM REF 26-11. OK FOR SERVICE, THIS CLEARS MEL 26-9 C/N C05473. MX CONTROL NOTIFIED PLACARDS. 2L73 4F A3WE 20031110001592003111000159NM 2003 11 10 UPS03241532 120031015A5753 SUPPORT BRACKET BOEING727 72731C 1384011NM T/E FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE:C RT WING I/B MID FLAP GUIDE ROLLER SUPPORT BRACKET CRACKED AT UPPER CHORD REAR SPAR JUST O/B OF NR 6 FLAP TRANSMISSION. ROLLER SUPPORT REPLACED IAW SRM 51-30-02 AND BOEING DRG 65-16201. 2L73 4F A3WE 20031110001602003111000160NM 2003 11 10 SWAA032262 120031015A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031110001712003111000171NM 2003 11 10 03FDEA01873 120031105A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 FWD LWR CARGO FRAME IS DENTED AT STA 660 STR 22L. FWD LOWER CARGO FRAME IS DENTED AT STR 22L AT BS 660. FOUND TO BE OUT OF LIMITS PER SRM5 3-10-1. REPAIRED DAMAGE FRAME PER SRM 51-40-3. 2L73 4F RTA3WE 20031110001842003111000184NM 2003 11 10 SWAA032255 120031014A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031110001922003111000192NM 2003 11 10 SWAA032237 120031011A53116516301 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND RT FUSELAGE FRAME CRACKED AT BS 188, WL 207, RBL 30. REMOVED AND REPLACED FRAME ASSY PER SRM. 2L72 4F RTA16WE 20031110002082003111000208EU 2003 11 10 AALA20030472 120030418A3397 WIRE AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170054 461 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 15G INOPERATIVE. SECURED EMERGENCY EXIT SEAT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031110002162003111000216WP 2003 11 10 AALA20031047 120030920A3350 CONNECTOR DOUG DC9 DC983 3022083WP CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219619V 53566 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROW 12DEF. RECONNECTED CONNECTOR AT SEAT 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031112000232003111200023SO 2003 11 12 C2XA03SH445 120031112A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV-DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031112000322003111200032SO 2003 11 12 SWIA200312579 120031015A5420 BRACKET EMB 120 EMB120ER 3260203SO RT HYD BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07566SW 120341 RIGHT HYD BAY CROSS BRACKET CRACKED AT INBOARD SIDE OUT OF LIMITS. DISCOVERED DURING C-CHECK. REMOVED AND REPLACED RIGHT HYD BAY CROSS BRACKET IAW SRM 51-10-02 & 51-40-00. 2L72 4T RTA31SO 20031112000352003111200035WP 2003 11 12 ABXA030436 120031110A2161 CONTROLLER DOUG DC9 DC932 3022066WP A/C BAY MALFUNCTIONED A ABXAI CABIN DEPRESSURIZATION O OTHER CLCLIMB 1 GL23903AX 47427 AFTER TAKEOFF 3000 FT, BOTH AUTO TEMP CONTROLLERS WERE SELECTED FULL HOT. ABOUT 14000 FT, AIRFLOW STOPPED & CABIN CLIMBED UNCONTROLLABLY AT 1400 FT FPM. LEFT PRESSURE GAUGE INDICATED '0' PSI, RIGHT GAUGE INDICATED '30' PSI, LEFT AND RIGHT DUCTS TEMPS PEGGED HOT. AFTER 15 MINUTES AIRFLOW REGAINED TO LEFT PACK, RIGHT PACK REMAINED INOP THOUGH PRESSURE OF '30' PSI WAS INDICATED. DUE TO EN ROUTE PACK PROBLEMS, FLT 129 RESTRICTED TO 10,000 FT INTO ILN. REMOVED & REPLACED 2 DUCT COUPLERS BELOW & FORWARD OF RIGHT AC PACK. LEAK CHECKED GOOD. REMOVED AND REPLACED LEFT PACK CONTROLLER IAW DC-9 MM 21-60-00. OPS CHECKED GOOD. PRESSURIZED CABIN TO 7 PSID, LEFT AND RIGHT AC DUCTS LEAK CHECKED GOOD DURING PRESSURIZATION.2L72 4F A6WE 20031107000222003110700022WP 2003 11 7 MWEA030441 120031103A14309936719219 SETSCREW DOUG DC9 DC981 3022081WP NOSE WEIGHT STRIPPED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 LEFT TOP SET SCREW IS STRIPPED FOR NOSE WEIGHT ATTACHMENT POINT AT FRAME STATION 218. REMOVED AND REPLACED NEW SET SCREWS. 2L72 4F A6WE 20031107000262003110700026EA 2003 11 7 03295670 120031022A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27670BR 7561 DURING INSPECTION DAMAGE TO THE PRESSURE BULKHEAD AT FS 621. 2L72 4F RTA21EA 20031107000392003110700039EA 2003 11 7 03306670 120031102A3246501598 WHEEL CNDAIRCL600 CL6002B19 1900309EA NLG DEFECTIVE A VTZAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA27670BR 7561 DURING CLIMB ON FLT 7245 CREW NOTED A VIOLENT NOSE WHEEL SHAKE AND BANGING IN THE WHEEL WELL. CREW DECLARED EMERGENCY AND RETURNED TO GATE WHERE PASSENGERS WERE DEPLANED NORMALLY. THE NOSE WHEELS WERE REPLACED. 2L72 4F RTA21EA 20031107001212003110700121NE 2003 11 7 SIMA200328202 220031007A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 MALFUNCTIONED A SIMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW21392AE 340B392 GEE785645 ILE - FLT 3412 - CREW ABORTED TAKEOFF DUE TO LOUD BANG COMING FROM THE NR 2 ENGINE ACCOMPANIED WITH DIRECTIONAL CONTROL PROBLEM. AFTER STOP ON RUNWAY OIL PRESSURE LIGHT CAME ON AND ITT WENT TO 1215 DEGREES. AFTER DEPLANING, THE RIGHT PROPELLER WAS FOUND TO BE SEIZED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW SAAB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. THE FDR RIGHT MAIN BATTERY, AND RIGHT ENGINE FIRE BOTTLE WERE ALSO REPLACED. (M) 2L72 4T4 TRTA52EU E8NE 20031107001242003110700124EA 2003 11 7 REXA03008 120031017A2697PU90421R3 WIRE CNDAIRCL600 CL6002B19 1900309EA SMOKE DETECTOR LOOSE A REXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO258423C 7423 LAVATORY SMOKE WARNING. FLIGHT ATTENDANT VERIFIED NO SMOKE, CREW ELECTED TO RETURN TO AIRPORT. UNEVENTFUL LANDING. MAINTENANCE FOUND LOOSE WIRE ON LAV SMOKE DETECTOR CANNON PLUG. SYSTEM DEFERRED PER MEL 26-16-01 CAT C. (M) 2L72 4F RTA21EA 20031107001302003110700130SO 2003 11 7 SIMA200327901 120031004A2510 LOCKPIN EMB 145 EMB145LR 3260212SO COCKPIT LACK OF LUBE A SIMAO OTHER O OTHER TOTAKEOFF 1 SW21623AE 145109 CMH - FLT 4394 - DURING TAKEOFF, BOTH CAPTAIN AND FIRST OFFICER SEATS SLIDE OFF POSITION. CREW WAS UNABLE TO SET LOCK PIN. MAINTENANCE PERFORMED INSPECTION OF CAPTAINS AND FIRST OFFICERS SEAT LOCKING PIN AND SEAT TRACKS. SEAT TRACKS AND LOCKING PINS WERE CLEANED AND LUBED. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031107001392003110700139WP 2003 11 7 MEX2003448 120030926A7830221CH54RB SWITCH DOUG DC9 DC987 3022087WP THRUST REVERSER DEFECTIVE A ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW231075T 49724 FLT 306 - ACA-MEX - AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE REVERSE UNLOCKED LIGHT TURNED ON. REVERSE MECHANISM AND ACTUATOR WERE LUBRICATED AND REVERSE WAS OPERATED THREE TIMES NON REPRODUCING THE FAIL. FURTHER, AIRCRAFT RETURN TO PLATFORM AGAIN WITH THE SAME REPORT BUT WITHOUT LIGHT INDICATION. IT WAS CHECKED NON REPRODUCING THE FAIL. REVERSE WAS DEACTIVATED AND STOWED AND REPORT WAS DEFERRED IAW MEL 78-03. DURING OVERNIGHT SERVICE SWITCHES S1-47 AND S1-450 WERE REPLACED IAW MM 78-32-03, TESTS CORRECT. (M) 2L72 4F RTA6WE 20031107001602003110700160EU 2003 11 7 AALA20030464 120030417A2560 FLASHLIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2125071 514 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031107001652003110700165NM 2003 11 7 AALA20031043 120030921A33508200008731 SIGN BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21383AN 26995 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT DOOR R1. REPLACED EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031112000042003111200004NM 2003 11 12 2003UALA00813 120031028A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 STR 7R IS CRACKED AT STA 500B AND 500C. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STRINGER FROM STA 500 PLUS 10 INCHES TO STA 500C PLUS 10 INCHES. SPLICED IN SECTION OF STRINGER. 2L72 4F4 FRTA16WE E2GL 20031112000432003111200043NM 2003 11 12 DHL2003782013 120031106A1430 STUD BOEING727 727227 1384078NM OIL FILTER COVERSTRIPPED A DHLAED ENGINE SHUTDOWN RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01769AT 21998 AFTER ENGINE START NR 3 OIL PRESSURE LIGHT CAME ON, AND CONFIRMED BY LOW OIL PRESSURE GAUGE. ENGINE SHUT DOWN OIL QUANTITY DECREASED TO ZERO. FOUND STUD ON OIL FILTER COVER IN GEARBOX STRIPPED. REMOVED STUD AND INSTALLED HELICAL COIL INSERT PER P&W M/M 70-00-00. REINSTALLED OIL FILTER. GROUND RAN ENGINE, NO LEAKS NOTED. 2L73 4F A3WE 20031112000452003111200045SO 2003 11 12 SWIA200312580 120031015A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07566SW 120341 RIGHT FRAME 9 CLIP UNDER DV WINDOW CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FRAME 9 RIGHT SIDE PER SERVICE BULLETIN 120-53-007 REV 00 DATED 21 JUL 99. 2L72 4T RTA31SO 20031112000772003111200077NM 2003 11 12 AWXA200301400 120031025A5414311A102311 SKIN BOEING737 7373G7 1384595NM LT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1.125 INCH CRACK WAS FOUND IN LT PYLON ACCESS PANEL LANDING (5727L), NAC STA 220. MAINTENANCE PERFORMED HFEC INSPECTION TO IDENTIFY CRACK LENGTH; STOP DRILLED CRACK IN LT PYLON ACCESS PANEL LANDING; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 03-5433-01037-DL1. 2L72 4F RTA16WE 20031112000912003111200091NM 2003 11 12 C1HA200394025 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 480-690, RBL 24 HAS BARE METAL & CORROSION AS MARKED. 2L73 4F A3WE 20031112000942003111200094NM 2003 11 12 C1HA200394028 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 689 - 741, LBL 24.75 HAS AREAS OF CORROSION AND WORN AREAS. 2L73 4F A3WE 20031112001042003111200104NM 2003 11 12 AWXA200301383 120031109A4920 APU AIRBUSA319 A319132 3930340NM APU BAY MALFUNCTIONED A AWXAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP28814AW 1281 NR 1 GENERATOR INOPERATIVE AND ON (MEL), APU AUTO SHUTDOWN AT 330 FT, ATTEMPTED 1 RESTART, NO LUCK, DIVERTED & LANDED WITHOUT FURTHER EVENT. MAINT R & R NR 1 IDG, OPS CHK GOOD. MAINT FOUND APU BEARINGS GRINDING & DAMAGE TO BLADES, R & R APU, OPS CHECK GOOD. INCOMING TEST & VISUAL INSPECT OF IDG COULD NOT VERIFY REASON FOR REMOVAL, UNIT DISASSEMBLED & INSPECTED, NO DISCREP NOTED, REPLACED SPEED SENSOR. CONFIRMED FAILURE OF APU TURBINE SECTION DAMAGE. PRIMARY CAUSE OF DAMAGE DUE TO TURBINE WHEEL SHAFT SEPARATION; THIS CAUSED SECONDARY DAMAGE TO LOAD COMP & COMP IMPELLERS. INLET GUIDE VANES, COMP DIFFUSERS, & TURBINE NOZZLE DAMAGED BY CONTACT WITH CENTER SHAFT. UNIT REPAIRED, TESTED, & RETURNED TO SERVICE. 2L72 4F RTA28NM 20031112001072003111200107EU 2003 11 12 BAQA090156 120030716A6410360A33104011 BLADE AEROSPSA365 SA365N 8680669EU TAIL ROTOR NICKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 3866 6036 NICKS IN BLADE, AND OUT OF LIMITS. COPY OF TAIL ROTOR HEAD ASSEMBY ENCLOSED. 1G72 3U H10EU 20031113000022003111300002EA 2003 11 13 HEEA090148 220030930A7200312295201 ENGINE BELL 412 412 1182202SW PWA PT6 PT6* 52043EA NR 1 MALFUNCTIONED E HEEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW03412SM1928 33197 IN FLIGHT NR 1 ENGINE ITT WENT TO 970 DEGREES, NR 2 ENGINE TORQUE DROPPED TO ZERO. APPEARED TO BE NR 1 ENGINE GOVERNOR HIGH SIDE FAILURE. RETURNED NR 1 ENGINE THROTTLE TO IDLE, SWITCHED NR 1 ENGINE THROTTLE TO MANUAL AND FLEW TO NEAREST AIRPORT IN MANUAL THROTTLE. MAINTENANCE REPLACED NR 1 ENGINE ASSY INCLUDING FUEL MANAGEMENT SYSTEM. 1G72 4U3 T H4SW E2NE 20031113000082003111300008NE 2003 11 13 BAQA090338 220031020A73140319928670 PUMP AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE FUEL SYSTEM MALFUNCTIONED B BAQAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 EA037YL 436 11502 NR 1 ENGINE SLOW TO START. REPLACED PUMP. 1G72 3U3 URTH7EU E42NE 20031113000122003111300012 2003 11 13 BAQA090303 420031027A34214021541671 INDICATOR BOLKMS117 BK117B2 5626013EU COCKPIT OSCILLATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KC6044 7168 ARTIFICIAL HORIZON OSCILLATING YAW MOTION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20031113000192003111300019 2003 11 13 BAQA090300 420031027A3454069102525 DISPLAY BOLKMS117 BK117B1 5626012EU VOR SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME6466 7235 VOR TRANSCEIVER DISPLAY INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031113000202003111300020 2003 11 13 BAQA089756 420031010A3410C19252PC08 DISPLAY UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE FLT MONITOR INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME2115 0157 FCDM INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 10/15/03 1G72 3U3 U H88EU E34NE 20031113000232003111300023SW 2003 11 13 BAQA090021 120031017A6330 BEARING BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL ISOLATION MOUNT WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03870SF LK0263 23018 ISOLATION MOUNT BEARING OUT OF LIMITS. 1G72 3U3 UNCH9SW E1GL 20031107001512003110700151WP 2003 11 7 AMTA200301278 120030807A5743 SUPPORT LKHEED1011 10113851 5265010WP RT WING DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 SW21188AT 193C1078 INTERIM REPAIR OF CORROSION TO RIGHT MLG TRUNNION LOWER SUPPORT FLANGE REQUIRES PERMANENT REPAIR. APPLIED PERMANENT REPAIR TO BLENDOUTS PER ER/A L10-57R-4741. (M) 2L73 4F A23WE 20031110000772003111000077CE 2003 11 10 AMWA74 120031102A1430 BOLT BEECH 1900 1900D 1154162CE RUDDER LOOSE A AMWAK NONE O OTHER ININSP/MAINT 1 CE073199Q N3199Q DURING A NR 6 DETAIL, IT WAS FOUND THAT THE FOUR BOLTS SECURING THE RUDDER TORQUE TUBE TO THE RUDDER AT THE LOWER ATTACH POINT FLANGE WERE LOOSE. CAUSING PLAY IN THE RUDDER CONTROL SYS AFTER REPLACING THE 4 BOLTS AND PERFORMING RUNNING TORQUE TESTS ON THE FASTENERS. SERVICED ACFT WITHOUT FURTHER INCIDENTS. 2L72 4T RTA24CE 20031110001302003111000130NM 2003 11 10 AWXA200301347 120031007A533065458001134 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND IN FUSELAGE SKIN OF R-1 DOOR LOWER HINGE CUTOUT AT EDGE OF FIRST LAYER CUTOUT OF BONDED DOUBLER. MAINTENANCE BLENDED OUT CRACKS ON R-1 DOOR LOWER HINGE CUTOUT BONDED DOUBLER; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01 FIG 208. 2L72 4F RTA16WE 20031022000172003102200017EU 2003 10 22 AWXA200301067 120030915A5730D5744357220000 SKIN AIRBUS320 A320232 3930326EU LT WING LE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK A .5 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN AT NR 3 SLAT AFT INBOARD EDGE UP STOP PAD, RIB 15. MAINTENANCE REMOVED UP STOP PAD AND BLENDED OUT CRACK ON LT WING LEADING EDGE SKIN RIB 15; FABRICATED A REPAIR DOUBLER AND NEW REPLACEMENT UP STOP PAD; INSTALLED REPAIR PARTS IAW AWA ER 26-5721-00006-JS2. 2L72 4F RTA28NM 20031022000272003102200027NM 2003 10 22 AWXA200301077 120030920A2560P4010021 BATTERY BOEING737 737277 1384570NM ZONE 900 - LAVATDISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE AFT GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN AFT GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031022000412003102200041EA 2003 10 22 SWIA200312423 120030918A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA H/S MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07947SW 7786 STAB CH 2 WILL NOT ENGAGE. INSTALLED SERVICEABLE HORIZONTAL STABILIZER MOTOR CONTROL UNIT IAW CRJ MM 27-42-05. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031022000492003102200049NM 2003 10 22 QXEA200301151 120030911A5341 FLANGE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 WING TO FUSELAGE FAIRING FORWARD APERTURE FLANGE IS CHAFED AT PANEL 262FT. REPAIRED IAW Q400 SRM 51-00-02 AND RD 8/4-53-451. 2H72 4T4 TRTA13NM E00062EN 20031022000692003102200069SO 2003 10 22 C2XA03IA099 120030921A3350 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2719554 145587 THE CREW NOTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE RESET THE ELECTRICAL POWER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031022000722003102200072SO 2003 10 22 C2XA03TY166 120030922A531514521700007 FLOORBEAM EMB 135 EMB135ER 3260203SO ALLSN AE3007AE3007C GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719503 145176 DURING A SCHEDULED 2C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED. MAINT. REMOVED AND FAB. A NEW FLOORBEAM. CLEANED SURFACE CORROSION,PRIMED,PAINTED AND INSTALL THA NEW FAB. PART IAW EMB 135/145 SRM 51-10-03 AND CPM 51-21-03,05,06. ALL WORK WAS ACCOMPLISHED AND WILL BE EL. UPON COMPLETION OF ALL WORK. 2L72 4F4 FRTT00011ATTE6CH 20031022001222003102200122NM 2003 10 22 QXEA200301172 120030919A2430 CONNECTOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09359PH 514 ON FLIGHT 2114 NR 2 DC GENERATOR HOT ILLUMINATED. AFTER CHECKLIST WAS COMPLETED, LIGHT WENT OUT, THEN REILLUMINATED WITH NR 2 DC GENERATOR OFF, THEN WENT OUT. REMOVED AND REPLACED CONNECTOR 2431-P14. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031022001302003102200130NM 2003 10 22 2003UALA00685 120030914A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29304UA 23665 FUSELAGE SKIN DENTED AT STA 365 BETWEEN STRINGER 18L AND 19L. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031022001582003102200158SO 2003 10 22 C2XA03SH345 120030924A541114576603013 RIB EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL NR 1 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 SHV-DURING C CHECK A NR 1 ENGINE LOWER COWLING INBOARD RIB 8 INCHES FORWARD OF AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031023000032003102300003NM 2003 10 23 CALA0300554 120030923A5320 SUPPORT BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE RT AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND RT AFT LAV WALL SUPPORT CORRODED AT STA 994, RBL 14 TO RBL 38. THE SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031028000322003102800032EA 2003 10 28 COMA0360435 120030927A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01986CA 7174 FLT 5077 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE, LUBED DOOR HANDLE. 2L72 4F RTA21EA 20031028000342003102800034EA 2003 10 28 COMA0360437 120030927A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ACTIVATED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01986CA 7174 FLIGHT 5765 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED DOOR WARNING SYSTEM IAW MEL. 2L72 4F RTA21EA 20031028000432003102800043SO 2003 10 28 SWIA200312456 120030928A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07268UE3574 3574 120207 RECEIVED FLAP CONTROL FAULT MULTIPLE TIMES EN ROUTE. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB120 MM 27-50-00. OPS AND LEAK CHECKS GOOD. S/N OFF: 0214 2L72 4T RTA31SO 20031028000452003102800045 2003 10 28 SWIA200312458 420030926A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE STALL WARNING MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07567SW 120342 NUMBER ONE STALL WARNING SYSTEM TEST DOES NOT CLEAR THE STALL WARNING ANNUNCIATION FROM THE MAP. REMOVED AND REPLACED STALL WARNING TEST PANEL. OPS CHECK GOOD IAW 27-00-00. 2L72 4T4 TRTA31SO E20NE 20031028000472003102800047NM 2003 10 28 03271416 120030928A3350321430 BATTERY DORNERDO32 DO328300 NM PWA 306 PW306B NE EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27416FJ 3171 DURING INSPECTION THE FIRST SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE 6LK EMERGENCY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T4 FRTA55NM E35NE 20031028000582003102800058SO 2003 10 28 C2XA03TY170 120030929A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713995 145295 DURING A SCHEDULED 2C INSPECTION THE RAMP ANGLE IN GALLEY SHOWED SIGNS OF BEING CORRODED. MAINT. REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T4 FRTT00011ATTE6CH 20031028000632003102800063SO 2003 10 28 C2XA03SH358 120030930A531014522226003 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031028000652003102800065SO 2003 10 28 C2XA03SH359 120030930A531014522226003 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE LEFT BUTTSTRAP BETWEEN FRAMES 65 AND 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031028000812003102800081EU 2003 10 28 2003UALA00754 120031006A561006282 WINDSHIELD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LEFT CRACKED A UALAO OTHER O OTHER CRCRUISE 1 WP29473UA8185 1469 AT FL370, .80 MACH, HEARD LOUD POP AND NOTED CAPT'S FWD WINDSCREEN HAD CRACKED MORE THAN .750 INCH OF OUTER PANEL SURFACE AREA. ALSO NOTED 7-8 INCH BURN MARK AT LOWER LEFT. BUS BAR ARCED CAUSING CRACK. WINDSHIELD WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20031028000832003102800083NM 2003 10 28 2003UALA00769 120031010A21339024157042 VALVE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN PRESSURE MALFUNCTIONED A UALABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29810UA 843 FLIGHT DIVERTED DUE TO A PRESSURIZATION PROBLEM. FLIGHT CREW NOTED CABIN PRESSURE ALTITUDE INCREASING DURING CRUISE, F/A'S NOTED RUMBLING IN AFT GALLEY AREA. REPLACED BOTH SAFETY VALVES. 2L72 4F4 FRTA28NM E40NE 20031028000932003102800093NM 2003 10 28 ASAA0240FFF 120030403A531165C32396 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 727 BETWEEN BL 26 AND 27 RT. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001002003102800100NM 2003 10 28 03FDEA01605 120030912A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OB FLAP IB HINGE (FLAP SIDE) FOUND CORROSION ON IB AND OB ACTUATOR LUG BORES AND SPOT FACES. RT OB FLAP IB HINGE (FLAP SIDE) IB AND OB ACTUATOR LUG BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT IAW EA NR 1-5750-72686 : WINGS,TRAILING EDGE AND TRAILING EDGE DEVICES - RT OB FLAP / IB SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031028001022003102800102EU 2003 10 28 IXXA0300060O 220030925A73218062479 MEC DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM562AFR 13802EU NR 4 ENGINE FAULTY A IXXAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW11820BX 9211 46065 692211 IN CRUISE AT 17,000 FT NR 4 ENGINE FLAMED OUT, 7,000 LBS INDICATED ON FUEL GAUGE. ALL CROSSFEEDS CLOSED. ENGINE RE-LIT AFTER COMPLETION OF CFM56 FLAMEOUT/INFLIGHT RESTART CHECK LIST. AN INSPECTION IS ON GOING. AS THE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE PERFORMED TROUBLESHOOTING PER CFM MM 71-00-00 FAULT 51 LEAD TO MEC CHANGE. MAINTENANCE REMOVED AND REPLACED MEC PER CFM 73-21-10. OPERATIONAL AND CHECK LEAK GOOD IN ACCORDANCE WITH ALL APPLICABLE MANUALS. ALL ENGINE PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20031028001032003102800103EA 2003 10 28 03273684 120030930A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27684BR 7708 DURING INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031028001062003102800106NE 2003 10 28 KBM2003F00003 220030813A73235529 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE GOVERNOR CONTROLLOOSE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 GOVERNOR CONTROL CABLE END BALL BEARING HAS EXCESSIVE PLAY. REPLACED WITH NEW END BALL BEARING. 1G71 3U3 UNCH9EU E19EU 20031028001072003102800107EU 2003 10 28 KBM2003F00004 120030813A6220126892P BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ROD END LOOSE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 ROD END BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED WITH SV ROD END. 1G71 3U3 UNCH9EU E19EU 20031028001082003102800108CE 2003 10 28 JIKA 120030918A533011443000227 SKIN BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE FUSELAGE CORRODED E JIKAK NONE O OTHER ININSP/MAINT 1 WP013170128678 UB2 DURING MAINTENANCE FOR A PRESSURIZATION SQUAWK FOUND THE LOWER BELLY SKIN AT FUSELAGE STATION 258.25 HAD A CRACK EMINATING FROM A RIVET HEAD AND THE SKIN AROUND THE RIVET WAS BULGED OUT. UPON FURTHER INSPECTION UNDER THE FLOOR BOARDS FOUND HEAVY CORROSION ON THE SKIN IN THE ARE OF STRINGERS 14 AND 15. AFTER REMOVING THE CORRODED SECTION FO SKIN FOUND STRINGER 14 AND 15 WERE NOT CORRODED, BUT THE FILLER BETWEEN THE SKIN AND THE STRINGER WAS SEVERLY CORRODED AND NEEDED TO BE REPLACED. WORKING WITH ENGINEERING ON AN APPROVED REPAIR. 2L72 4T4 TRTA24CE E4EA 20031028001122003102800112EU 2003 10 28 KBM2003F00006 120030724A792147750 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE OIL COOLER NOISY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 LOUD NOISE, SQUEAKING IN FLIGHT. REMOVED AND REPLACED OIL COOLER MOTOR. 1G71 3U3 UNCH9EU E19EU 20031022001252003102200125EA 2003 10 22 COMA0360421 120030921A2710CLREF2768 CONTROL QUADRANT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG BAY CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA23679 7027 FLIGHT 5845 DURING TAXI CHECK, AILERON SYSTEM FAILED TEST, BINDING NOTICED IN THE AILERON SYSTEM. REPLACED THE RIGHT AILERON QUADRANT. 2L72 4F4 FRTA21EA E15NE 20031022001272003102200127NM 2003 10 22 C1HA200395070 120030920A275065219458 POWER UNIT BOEING727 727290 138408WNM TE FLAPS FAILED A C1HAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL15295CA 22147 DURING FLAP RETRACTION INBOARD TRAILING EDGE FLAPS STAYED AT 5 DEG OUTBOARDS WENT TO 2 DEG RAN SPLIT FLAP PROCEDURE AND FLAPS WOULD RETRACT FROM 5 DEG WITH ALTERNATE FLAPS. AS PER CHECK LIST. RETURNED TO HRL. FOUND ROLLER ON LT IB FLAP CARRIAGE OB TRUCK IB DEAD WEIGHT ROLLER MISSING. REPLACED BOLT AND BEARING ASSY IAW MM 2751. ALSO FOUND IB FLAP POWER UNIT ASSY INTERMITTENTLY LOCKING UP. REMOVED AND REPLACED POWER UNIT ASSY IAW MM 27-51-61 FLAPS OPS CHECK GOOD. 2L73 4F A3WE 20031023000232003102300023SO 2003 10 23 C2XA03CL170 120030923A33503025103 LIGHT EMB 145 EMB145LR 3260212SO RROYCEDART DART* NE LT OVERWING INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712569 145630 DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 TRTT00011AT 20031023000512003102300051 2003 10 23 SWIA200312441 420030922A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE STICK SHAKER BROKEN A SWIAO OTHER LF NO TEST FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07910SW 7566 STALL SHAKER WILL NOT FUNCTION DURING TEST. REPAIRED BROKEN WIRES ON BOTH STICK SHAKERS. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20031027000112003102700011CE 2003 10 27 HYI2003F00012 120030818A3150CM358950 MASTER SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LT SWITCH PANEL BURNED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE012611X693 402C0072 CLIMBING THROUGH 1000 FEET, CREW NOTICED SMOKE COMING FROM AVIONICS MASTER SWITCH, TURNED OFF SWITCH, TURNED ON ALTERNATE AVIONICS SWITCH, LANDED WITHOUT INCIDENT. MECHANIC REMOVED OLD, REPLACED SWITCH. 1L72 3O3 O A7CE E8CE 20031027000302003102700030EU 2003 10 27 AWXA200301106 120030913A5315D5347217220300 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON Y1292 FLOORBEAM FR 66-68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED Y1292 FLOORBEAM FROM FR 66-68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00 PG 5-6. 2L72 4F RTA28NM 20031027000332003102700033NM 2003 10 27 PCAA0309115 120030924A3350 SOCKET DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13849EX 337 DURING A ROUTINE MAINTENANCE VISIT THE EMERGENCY LIGHT AT SEAT 8DF WAS FOUND BROKEN. EMERGENCY LIGHT SOCKET WAS REPAIRED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031027000462003102700046NM 2003 10 27 03FDEA01633 120030925A261265249203 POWER SUPPLY BOEING727 727100 1384036NM FIRE DETECTION FAILED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25193FE 19142 ON CLIMBOUT PASSING ABOUT 3,000 FT FIRE WARNING BELL SOUNDED WITH NO ASSOCIATED LIGHTS. ALL SYSTEM INDICATIONS WERE IN THE GREEN. ALL ENGINE INST INDICATED NORMAL. LOWER CARGO SMOKE, CARGO SMOKE AND ENG AND WHEEL WELL FIRE DETECTIONS SYSTEM ALL TESTED WITH GOOD RESULTS. ON GROUND THE APU FIRE WARNING TEST WAS GOOD. REMOVED AND REPLACED ALL 3 FIRE & OVERHEAT DETECTION POWER UNITS, PER STANDARD PRACTICES. REMOVED AND REPLACED FIRE DETECTION CONTROL BOX PER 20-10-017-2, SYSTEM TEST NORMAL AMM 26-11-000-0. ALSO FOUND SEVERE CORROSION AT THE R-421 BLOCKING RECT CONN D4858, CLEANED. ALSO REMOVED AND REPLACED NAME-FIRE & OVERHEAT DETECTION POWER UNITS P/N 1011C. 2L73 4F RTA3WE 20031027000762003102700076NE 2003 10 27 MALA030426 220030913A75106068T56P01 VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ANTI ICE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15453XJ 340B453 DURING FLIGHT 3160, AT 16,000 FT, ENGAGED THE RT ENGINE ANTI ICE SWITCH. THE RT AIR VALVE ILLUMINATED QRH REF. RECYCLED TO NO AVAIL, ALSO MANEUVERED RT POWER THEN CYCLED SWITCH NO CHANGE. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RT ANTI ICE VALVE PER SAAB MM 72-00-00. P/N ON/OFF 6068T56P01, S/N ON GRTB9690, S/N OFF GRTB3641. 2L72 4T4 TRTA52EU E8NE 20031027000882003102700088CE 2003 10 27 DXTA200300127 120030926A3230 BOLT CESSNA750 750 2076810CE NLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07931QS 7500064 CLIMBING THROUGH FL360 THE NLG ATTEMPTED TO EXTEND & RETRACT ITSELF REPEATEDLY. GEAR UNSAFE RED LIGHT CAME ON & OFF EACH TIME, BLEW GEAR DOWN PNEUMATICALLY ON APPROACH. PERFORMED VISUAL INSPECTION TO EMERGENCY GEAR EXTENSION SYSTEM IAW CE 750 MM FOR A ONE TIME FERRY FLIGHT TO ICT FOR INVESTIGATION, AIRCRAFT HAS NUMEROUS WRITE UPS ON THIS DISCREPANCY. TROUBLE SHOT UN-COMMANDED NOSE GEAR EXTENSION & FOUND UP-LOCK HOOD BOLT CORRODED, BEARINGS WORN & SPRING WEAK, THIS COMBINATION WAS NOT ALLOWING THE UP-LOCK ACTUATOR TO BE FULLY EXTENDED. INSTALLED NEW BOLT P/N NAS464P5-37, INSTALLED 2 NEW BEARINGS P/N M81934/2-05C008, INSTALLED NEW SPRING P/N 5527401-3 IAW CESSNA 750 MM CHAPTER 32-30-05. ADJUSTED NOSE GEAR UP-LO2L72 4J RTT00007WI 20031028000032003102800003 2003 10 28 U30A20030034 420030917A2565D30665105 SLIDE AIRBUS320 A320212 3930322EU ZONE 842 MALFUNCTIONED A U30AK NONE L NO TEST ININSP/MAINT 1 EA17265AV2709 2709 427 AIRCRAFT IN C CHECK AT YWG. DURING AN INTENTIONAL DEPLOYMENT OF THE R2 PAX/CREW DOOR SLIDE/RAFT, THE SLIDE/RAFT FAILED TO DEPLOY PROPERLY. THE DISCHARGE RIPCORD HAD TO BE PULLED MANUALLY. ONCE THE RIPCORD WAS MANUALLY PULLED, THE SLIDE/RAFT INFLATED IN NORMAL TIME. AWAITING TEAR DOWN REPORT FROM VENDOR. 2L72 4F RTA28NM 20031028000552003102800055NM 2003 10 28 QXEA200301189 120030927A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09349PH1312413124 486 ON FLIGHT 2052 SMOKE WARNING LIGHT CAME ON IN FLIGHT THREE TIMES FOR 45 SENCONDS, THEN WENT OUT. NO OTHER INDICATIONS OF SMOKE IN COCKPIT OR CABIN. REMOVED AND REPLACED NR 2 SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCARFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031028001142003102800114EA 2003 10 28 ASOA03482 120031004A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20031028001192003102800119SO 2003 10 28 SIMA200324604 120030825A5330 SKIN EMB 135 EMB135LR 3260305SO UFSELAGE CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21718AE 145275 ABI - DURING AN IMBV INSPECTION, A CRACK WAS DISCOVERED ON THE LEFT FUSELAGE SKIN BETWEEN FRAMES 48 AND 49 AT THE OVERWING PANEL AFT UPPER ATTACH POIT. PERFORMED CUT OUT OF THE DAMAGE AREA. FABRICATED A FILLER, REPAIR DOUBELR. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 22, CHAPTERS 53-23-12, 51-40-04 AND 51-40-06. (M) 2L72 4F RTT00011AT 20031028001302003102800130EA 2003 10 28 ASOA03475 120031002A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA AIRSTAIR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031028001382003102800138NM 2003 10 28 GAIA03102 120030910A5347 SEAT TRACK BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED BS 360, LBL 25.5. REF FASI N/R 53267, REPLACED SEAT TRACK LBL 25.5 BS 344 TO 480 PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 7. (M) 2L73 4F A3WE 20031028001722003102800172EA 2003 10 28 ASOA03457 120030924A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11875AS 7559 FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031028001772003102800177EU 2003 10 28 ASOA03460 120030927A7712311649902 TORQUE SENSOR AEROSPATR72 ATR72212 8680945EU LEFT ENGINE INTERMITTENT A ASOAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO11531AS 454 DURING CRUISE FROM ATL-GPT - AT APPROXIMATELY 16,000 FEET THE CREW NOTICED AN ENGINE PITCH CHANGE ACCOMAPNIED BY A YAW, ALONG WITH THE LEFT ENGINE TORQUE DROPPING TO APPROXIMATELY TWENTY PERCENT AND THEN RETURNING TO NORMAL. THE CREW REDUCED THE POWER LEVERS TO APPROXIMATELY SIXTY PERCENT TORQUE WITH THE FLUCTUATION PATTERN CONTINUING PLUS OR MINUS THIRTY PERCENT, AT WHICH TIME THE CREW MOVED THE POWER LEVERS TO FLIGHT IDLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MGM, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 TORQUE SENSOR ON THE LEFT ENGINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031029000012003102900001WP 2003 10 29 ASAA0380571 120030831A33501001191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS396922186 49387 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20031029000092003102900009NM 2003 10 29 ASAA0340108 120030301A532065479577 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND WEB AT BS 847-867 WL 16 AN RBL 18 HAS CORROSION DAMAGE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000102003102900010NM 2003 10 29 ASAA0340328 120030818A3350 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 13 INOPERATIVE. REPAIRED WIRE AND OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20031029000242003102900024NM 2003 10 29 ASAA0340080 120030227A531165C22902 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON FRAME BS 500C RBL 5 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000362003102900036EU 2003 10 29 USAASA03104 120030901A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19716UW 1055 PHL - THE EMERGENCY LIGHT SYSTEM FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE RIGHT, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031029000502003102900050NM 2003 10 29 ASAA0340316 120030725A56202238883 SUPPORT BOEING737 737400 138449ANM FLOORBOARD CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 DURING C-CHECK, FOUND FLOORBOARD SUPPORT STRAP AT STA 767 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000552003102900055NM 2003 10 29 ASAA0310434 120030512A54136941209801 LONGERON BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND NR 2 ENGINE FAIRING LONGERON AT NACELLE STATION 99.25 HAS A HOLE. REPLACED LONGERON PER SRM. (M) 2L72 4F A16WE 20031029000832003102900083NM 2003 10 29 AMTA200301196 120030918A49708TJ99GGE1 TRANSMITTER BOEING757 75733N 1384931NM APU OIL QTY MALFUNCTIONED A AMTAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL11560TZ 33525 APU OIL QUANTITY FLUCTUATES BETWEEN FULL AND 0.5. REMOVED AND REPLACED APU OIL QUANTITY TRANSMITTER IAW MM 49-94-04-2, OPS CHECK NORMAL, NO LEAKS NOTED. (M) 2L72 4F RTA2NM 20031029000882003102900088NM 2003 10 29 USAABB03175 120030923A3350 CONNECTOR BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU 27244 PHL - FOUND THE EXTERIOR EMEREGNCY ILGHTS AT THE R1 AND R4 DOORS INOPERATIVE. MAINTENANCE REPAIRED THE ELECTRICAL CONNECTIONS AT THE R1 AND R4 DOOR LIGHT ASSEMBLIES. (M) 2L72 4F RTA2NM 20031029000932003102900093NE 2003 10 29 KBM2003F00008 220030712A75329550164960 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH2400 2884 BLEED VALVE DOES NOT CLOSE, FLAG CONTINOUS TO SHOW. REPLACED BLEED VALVE WITH SERVICEABLE UNIT. 1G71 3U3 U H9EU E19EU 20031029000992003102900099EA 2003 10 29 COMA0370032 120030927A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01378CA1253 10097 F S 1098.20 BULKHEAD BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPARIED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING I/A/W MFG REO 670-53-61-034 REV B. 2L72 4F4 FRTA21EA E15NE 20031110000472003111000047 2003 11 10 RAIA00310277 420031031A31407013348940 DAU EMB 145 EMB145LR 3260212SO NR 1 INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03815HK7687 145048 5729-STL- DAU NR 1 FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 1 DAU. 2L72 4T RTT00011AT 20031110000542003111000054SO 2003 11 10 C2XA03SH436 120031109A532014529150007 CROSSBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110001472003111000147NM 2003 11 10 03FDEA01748 120031015A5510 BARREL NUT DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 HORIZONTAL STAB RT NR 1 BORE FOUND BEARING, SIDEWALL AND BOTTOM WITH CORROSION. BLEND OUT CORROSION FOUND EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000. 2L73 4F4 FRTA22WE E13NE 20031110001792003111000179NM 2003 11 10 SWAA032250 120031013A2560PL2230LH00 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 DURING SCHEDULED C3 CHECK, FOUND 4 EA SECTIONS OF PHOTOLUMINESCENT EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20031110001932003111000193NM 2003 11 10 SWAA032238 120031012A53306545766 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED SVC CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG BETWEEN BS 517-BS 519, JUST BELOW STR 12R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031110002112003111000211NM 2003 11 10 AALA20031037 120030920A2611 SENSOR BOEING757 757223 1384957NM CARGO BAY FAILED A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21172AJ 32400 LAX - FLT 276 - AIRCRAFT EN ROUTE LAX-MIA WHEN AFT CARGO SMOKE DETECTOR INDICATED A FIRE. RETUNED IMMEDIATELY TO LAX FOR A LANDING WITHOUT INCIDENT. AIRCRAFT WAS OVERWEIGHT. PERFORMED OVERWEIGHT INSPECTION. REPLACED FAILED WARNING SYSTEM SENSOR IN THE AFT CARGO. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031110002122003111000212NM 2003 11 10 AALA20031095 120031001A335002019241004 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21390AA 27450 ORD - OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROW 20C. REPLACED EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031110002132003111000213NM 2003 11 10 AALA20031080 120030926A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21674AN 29424 MIA - OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 20D. REINSTALLED LOOSE CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031112000492003111200049WP 2003 11 12 MWEA030432 120031023A801138334221 STARTER DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE ENGINE INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31806ME 48032 NO HIGH-PRESSURE COMPRESSOR SHAFT SPEED ROTATION WHEN STARTING RT ENGINE, START VALVE OPEN LIGHT DID NOT COME ON. REMOVED AND REPLACED ENGINE STARTER. 2L72 4F4 F A6WE E2EA 20031112001092003111200109EU 2003 11 12 BAQA090678 120031104A33101179203103 CONTROL UNIT BOLKMS117 BK117A1 5626010EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 FEEDBACK IN HEADSET WHEN ADJUSTING LIGHTS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030728001152003072800115NM 2003 7 28 SWAA031530 120030712A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 619, STR 4L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030729000492003072900049WP 2003 7 29 ZW0A0305601 120030704A7930 PRESSURE SWITCH DOUG DC9 DC982 3022082WP RT ENGINE FAULTY A ZW0AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE13912TW 49183 DURING CLIMB FAILURE OF FILTER CLOG LIGHT OF RIGHT ENGINE ILLUMINATED. MADE UNSCHEDULED LANDING AT IAD AT IDLG AND DID NOT SHUT DOWN ENGINE. REMOVED OIL FILTER FOR INSPECTION NTF. INSTALLED NEW FILTER CPN 5790859. RAN ENGINE CLOG LIGHT ILLUMINATED. CHANGED RIGHT ENGINE OIL FILTER CLOG PRESSURE SWITCH CPN SW13004. LEAK CHECK OK. 2L72 4F A6WE 20030729000822003072900082NM 2003 7 29 QXEA200300746 120030611A5510 SHIM BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - SHIMS UNDER FORWARD RIGHT HAND MOUNT FOR HORIZONTAL STABILIZER HAVE EXTRUDED OUT. REPAIRED IAW TR 55-011, TASK 55-10-00-400-801, PAGE 6. 2H72 4T4 TRTA13NM E00062EN 20030729000842003072900084EA 2003 7 29 QXEA200300743 120030614A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - RIGHT HAND WING BOTTOM TRAILING EDGE CHAFED. REPAIRED IAW MFG EA R-57-38 AND REO 670-57-51-012. 2L72 4F4 FRTA21EA E15NE 20030729000912003072900091NM 2003 7 29 USAA030092 120030606A5420035403 STRUCTURE BOEING737 737301 1384611NM NACELLE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19586US11546 23931 PIT - BEARING BORE REPAIR, SINGLE LUGE MOUNT BEARING BORE OF CROSSBEAM. INSTALLED OVERSIZED BEARING. (M) 2L72 4F RTA16WE 20030729001072003072900107WP 2003 7 29 MEX2003225 120030614A7722 THERMOCOUPLE DOUG DC9 DC987 3022087WP NR 1 ENGINE DAMAGED A ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW231075T 49724 FLT 101 - HMO-CUL - AIRCRAFT RETURNED TO GATE DUE TO ENGINE NR 1 DID NOT HAVE EGT INDICATION. DURING REVISION FOUR, THERMOCOUPLE PROBES WERE DAMAGED. DURING OVERNIGHT SERVICE SUCH THERMOCOUPLE PROBES WERE REPLACED AND TESTED IAW MM 77-21-00, ALL CORRECT. (M) 2L72 4F RTA6WE 20030729001282003072900128SO 2003 7 29 SWIA200312183 120030713A3397 WIRE EMB 120 EMB120ER 3260203SO CABIN BROKEN A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07564SW 120339 OVERHEAD EMERGENCY LIGHT GOING ON/OFF INTERMITTENTLY WHILE FA TESTED SWITCH. REPAIRED BROKEN WIRE TO ROW 9 OVERHEAD BIN EMERGENCY LIGHT. OPS CHECKED GOOD. 2L72 4T RTA31SO 20030729001312003072900131EA 2003 7 29 SWIA200312186 120030604A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS193 ELECTRICAL BAY FLOOR LT CRACKED. (DISCOVERED DURING C-CHECK) REPAIRED DAMAGED FLOOR IAW CRJ REO 601R-53-11-081 REV. ''NC''. 2L72 4F4 FRTA21EA E15NE 20030729001422003072900142WP 2003 7 29 ABXA030289 120030702A57553923259501N SUPPORT BRACKET DOUG DC9 DC941 302207NWP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 LEFT OUTBOARD SPOILER TORSION BAR OUTBOARD SUPPORT BRACKET CRACKED AT UPPER END. REPLACED SUPPORT BRACKET FOR LEFT OUTBOARD SPOILER TORSION BAR IAW DC-9 SRM. 2L72 4F A6WE 20030730000112003073000011WP 2003 7 30 ABXA030209 120030524A5230591014161 SKIN DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 FORWARD LOWER CARGO DOOR EXTERIOR SKIN CRACKED ON LEADING EDGE. BLENDED CRACK IAW DC-9 SRM 52-01 AND REA D952-47410. 2L72 4F A6WE 20030730000642003073000064WP 2003 7 30 ABXA030283 120030711A25105641032 SEAT DOUG DC8 DC863 302198AWP COCKPIT LACK OF LUBE A ABXAK NONE O OTHER CRCRUISE 1 GL23817AX248 45928 FLIGHT ENGINEER'S SEAT FELL VERTICALLY, WOULD NOT STAY IN SELECTED VERTICAL POSITION IN TURBULENCE. CLEANED AND LUBRICATED FLIGHT ENGINEER'S VERTICAL ADJUST ON SEAT. OPS CHECKED GOOD IAW DC8 MM 25-00-00. 2L74 4F 4A25 20030730000652003073000065NM 2003 7 30 ABXA030279 120030617A335020131A BATTERY PACK BOEING767 767281 1385109NM CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23767AX 22785 DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT SPARE BATTERY PACK INOP. REPLACED EMERGENCY LIGHT SPARE BATTERY IAW 33-51-00-5. OPS CHECKED GOOD. 2L72 4F RTA1NM 20030730000932003073000093WP 2003 7 30 ABXA030311 120030719A5730 SKIN DOUG DC8 DC863F 302198FWP CENTER WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX 45927 MAIN CARGO COMPARTMENT CORROSION ON CENTER WING UPPER SKIN AND DOUBLER FROM FS 760 - 855, LEFT BUTTLINE 3 - 23. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND BUSHINGS, ALODINED, PRIMED, INSTALLED AND LEAK CHECKED IAW REA D857-47555MR AND REA D857-47547MR, REV A. 2L74 4F 4A25 20030730001092003073000109SO 2003 7 30 SIMA200316901 120030610A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21645AE 145212 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142 REV 21, CHAPTER 51-40-02 AND CPM 51-21-04/06 AND 51-61-00. (M) 2L72 4T RTT00011AT 20030730001172003073000117WP 2003 7 30 AMTA200300900 120030601A5712 RIB LKHEED1011 10113853 5265020WP LT WING DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 LEFT WING RIB UPPER CAP TEMPORARY REPAIR REQUIRES PERMANENT REPAIR. REPAIRED RIB UPPER CAP IAW ER/A L10-57R-4383A. (M) 2L73 4F A23WE 20030730001192003073000119WP 2003 7 30 MEX2003223 120030612A324151130 SWITCH DOUG DC9 DC987 3022087WP ANTI-SKID SYS FAILED A ASMFO OTHER J WARNING INDICATION UKUNKNOWN 1 SW23755RA 49727 FLT 426 - MEX-IAH - AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF LIGHTS ANTI-SKID COME ON. DURING REVISION, THE SWITCH S1-130 WAS OUT OF SERVICE. THE SWITCH S1-130 WAS REPLACED IAW WDM 32-41-00 AND LIGHTS ANTI-SKID COME OFF. THE CONTROL BOX WAS TESTED IAW MM 32-43-00, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030730001302003073000130NM 2003 7 30 USAASB03091 120030624A3260806007 CIRCUIT CARD BOEING737 7374B7 1384702NM E/E BAY FAULTY A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19441US 24812 CLT - FLT 255 - ON APPROACH TO CLT, AT APPROX 5,000 FEET, THE CREW DID NOT RECEIVE A GREEN LIGHT FOR THE RIGHT MAIN LANDING GEAR UPON GEAR EXTENSION. CAPTAIN ABORTED APPROACH AND HAD A DEAD HEAD FIRST OFFICER VISUALLY CHECK FOR GEAR EXTENSION. IT WAS DETERMINED THAT THE GEAR WAS DOWN. FLIGHT LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE CHECKED THE INTEGRITY OF THE RIGHT MLG DOWNLOCK SENSOR S73. SENSOR CHECKS GOOD. FOUND D4574 CONTAMINATED. CLEANED D4574. PERFORMED INDICATION CHECK PER MM TASK 32-61-31-714-017. INDICATION CHECKS GOOD. REMOVED AND REPLACED M981 LOGIC CARD PER MM TASK 32-09-20-844-019. INDICATION CHECKS GOOD. (M) 2L72 4F RTA16WE 20030730001452003073000145SO 2003 7 30 SIMA200313905 120030514A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21646AE 145213 ABI - DURING AN IMBV INSPECTION, STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATION OF CRACKS NOTED. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145-1142, REV 21, CHAPTER 53-24-02 FIGURE 201. (M) 2L72 4T RTT00011AT 20030731000052003073100005NM 2003 7 31 QXEA200300902 120030719A5720 MOUNT BRACKET DHAV DHC8 DHC8202 2809007NM WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- NUTPLATE MOUNT BRACKET FOR LEADING EDGE 611AR UPPER OUTBOARD NEXT TO NACELLE ON THE SPAR IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20030731000082003073100008NM 2003 7 31 QXEA200300907 120030719A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- RIGHT HAND INBOARD NR 8 SEAT TRACK HAS A GOUGE IN CENTER OF TRACK AT STATION X440.500. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36, 51-00-06 AND RD 8-53-1339. 2H72 4T RTA13NM 20030731000102003073100010NM 2003 7 31 QXEA200300909 120030723A3222 STRUT DHAV DHC8 DHC8202 2809007NM NLG GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- NOSE LANDING GEAR SHOCK STRUT GOUGED .006 INCHES DEEP AND ONE INCH LONG ON FORWARD SIDE FOUR INCHES BELOW PIVOT POINT ON TRAILING ARM. REPAIRED IAW DHC-8 RD 8-32-289. 2H72 4T RTA13NM 20030731000172003073100017EA 2003 7 31 QXEA200300852 120030718A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 PDX- CHIMNEY SCREEN IS TORN IN FORWARD CARGO BAY. REMOVED AND REPLACED FORWARD CARGO BAY CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031110001112003111000111SO 2003 11 10 SWIA200312538 120031018A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO CABIN DISCHARGED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07197SW90 90 120186 CENTER EMERGENCY LIGHTS ARE INOP. REPLACED CENTER ELBP WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20031110001422003111000142NE 2003 11 10 IXXA0300063O 220031021A7297 WIRE HARNESS DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 2 ENGINE FAILED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11603AL914232423 46003 693494 UPON CLIMBOUT FROM KLRD CREW NOTED NR 2 ENGINE EXHAUST GAS TEMP (EGT) CLIMBING ABNORMALLY. AS A PRECAUTIONARY MEASURE CREW ELECTED TO RETURN TO KLRD AND MADE AN UNEVENTFUL LANDING. MAINTENANCE IS INVESTIGATING. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE TROUBLE SHOT IAW CGM MM 71-00-00. NO DEFECTS WERE NOTED. EGT SYSTEM WAS INSPECTED WITH NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED EGT HARNESS AND 2 THERMOCOULPES PER ALL APPLICABLE MANUALS. MAINTENANCE ALSO REMOVED AND REPLACED CIT SENSOR PER ALL APPLICABLE MANUALS. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20031110001742003111000174NM 2003 11 10 03FDEA01726 120031014A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 HORZ STAB RT NR 17 BORE FOUND BEARING, SIDEWALL AND BOTTOM WITH CORROSION. REAMED BORE UP TO MAX SB LIMIT CORROSION STILL EXIST ON SIDEWALL. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20031110002062003111000206NM 2003 11 10 SWAA032224 120031007A2560PH22300L STRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN, ROW NR 1 ABC TO ROW NR 8 ABC, ROW NR 1 DEF TO NR 6 DEF AND ROW NR 8 DEF TO ROW NR 11 DEF. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20031110002072003111000207EU 2003 11 10 AALA20031057 120030923A3397 WIRE FOKKERF28 F28MK0100 4990807EU CABIN MISWIRED A AALAK NONE L NO TEST ININSP/MAINT 1 SW211430D 11415 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROWS 4 THROUGH 13. CORRECTED POLARITY ON WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031118000322003111800032NM 2003 11 18 AWXA200301147 120030906A53206546579 WEB BOEING737 7373Q8 1384670NM APU BAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON LT APU COMPARTMENT WEB CUTOUT. MAINTENANCE ROUTED OUT CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13, FIG 1. 2L72 4F RTA16WE 20031118000342003111800034NM 2003 11 18 AWXA200301149 120030906A575369431206 ATTACH FITTING BOEING737 7373Q8 1384670NM ZONE 600 - RIGHTCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT WING INBOARD MID FLAP INBOARD CARRIAGE ASSEMBLY SPINDLE ATTACH FITTING. MAINTENANCE REMOVED AND REPLACED RT WING INBOARD MID FLAP INBOARD CARRIAGE ASSEMBLY SPINDLE ATTACH FITTING IAW BMM 57-53-22 PG 527. 2L72 4F RTA16WE 20031118000522003111800052EU 2003 11 18 AWXA200301167 120030925A5350D5323028120040 ANGLE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON WING TO BODY FAIRING VERTICAL ATTACH ANGLE, AFT OF FR 34 LT, BELOW LOWER FASTENER HOLE. MAINTENANCE REMOVED AND REPLACED VERTICAL ATTACH ANGLE AT FR 34 LT IAW A320 SRM 51-42-11 PG 21-22, FIG 8. 2L72 4F RTA28NM 20031118000532003111800053EU 2003 11 18 AWXA200301168 120030922A5347D5311278220200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FORWARD END OF RT OUTBOARD PASSENGER SEAT TRACK AT Y1292, FR 12 TO FR 24. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF SEAT TRACK Y1292 FROM FR 12 TO FR 24; RECEIVED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 23-28, FIG 9-12. 2L72 4F RTA28NM 20031118000582003111800058EU 2003 11 18 AWXA200301173 120030925A5321D5367202200000 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL 151DF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL; FABRICATED A NEW REPLACEMENT PANEL IAW A320 SRM 53-02-00, PG 231-236, FIG 209. 2L72 4F RTA28NM 20031118000682003111800068CE 2003 11 18 CHQA000424 220031002A7200 ENGINE EMB 145 EMB145 3260210SO CONT IO360 IO360* 17025CE NR 2 MALFUNCTIONED A CHQAO OTHER J WARNING INDICATION CRCRUISE 1 GL11262 P3370217 DURING CLIMB OUT OF LGA HIGH ITT WAS NOTED ON NR 2 ENGINE. AT MAX CLIMB THRUST ITT WAS AMBER AND RISING ABOVE 290. WE PULLED POWER BACK 7 PERCENT N1 LOWER THAN NR 1 ENGIN FOR REST OF FLIGHT ITT ON NR 2 ENGINE RAN AT 880-890 DEGREES WHEN N1 WAS PULLED BACK 7 PERCENT LESS THAN NR 1 ENGINE. THEN E2 FIRE DETECT FAIL MESSAGE ON EICAS ON CLIMBOUT OF LGA. REMOVED AND REPLACED NR 2 ENGINE. 2L72 4F3 ORTT00011ATE1CE 20031118000802003111800080SW 2003 11 18 BDJ2003F00000 120030929A57115147R SPAR BBAVIA7 7AC 2110102SW CONT A65 A65* 17003SO RT WING CRACKED E BDJAO OTHER O OTHER NRNOT REPORTED 1 GL272205E4437 7AC5776 OWNER REQUESTED AN INSPECTION IAW AD 2000-25-02R1, WOOD SPAR INSPECTION. INSPECTION REVEALED ADDITION INSPECTION. HOLES WERE NOT ADDED IAW LS406, REV A, RT REAR SPAR HAD AN OPEN CRACK AT THE BUTT INTO THE SPAR ATTACH PLATE BOLT HOLE, SPAR SEPARATING AT THE LAMINATIONS SEVERAL PLACES THE FULL LENGTH OF THE SPAR. .5 INCH X .1875 INCH X .2500 INCH DEEP GOUGE IN LOWER PART OF THE SPAR, WHERE SCREWS THAT WERE TOO LONG INSTALLING THE WING ROOT FAIRING. NAILS MISSING ON SOME RIBS. LAST INSPECTION, AUG/03. LAST SPAR VARNISH DATED NOV 1977. 1H71 3O3 O A759 E205 20031118000882003111800088NM 2003 11 18 C1HA200394021 120031009A3350 BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT DISCHARGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 EMERGENCY LIGHT EXIT OVER LEFT OVERWING EXITS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-00, OPS CHECK GOOD. 2L73 4F A3WE 20031118001032003111800103NM 2003 11 18 AWXA200301179 120030909A5350149N7664 SUPPORT ANGLE BOEING757 7572S7 1384962NM WING TO BODY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 1.25 INCH CRACK WAS FOUND ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 25 RT. MAINTENANCE CUT OUT DAMAGE ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 25 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-71, PG 203 FIG 202. 2L72 4F RTA2NM 20031118001102003111800110NM 2003 11 18 AWXA200301186 120030912A5321144N533014 FLOOR PANEL BOEING757 7572S7 1384962NM CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL K-2 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1. 2L72 4F RTA2NM 20030731000592003073100059NM 2003 7 31 QXEA200300878 120030721A2120 DUCT DHAV DHC8 DHC8202 2809007NM EMERGENCY AIR TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 SEA-FOUND TORN DUCT HOSE ON EMERGENCY AIR SUPPLY LOCATED ABOVE AIRCRAFT CONDENSOR. REMOVED AND REPLACED EMERGENCY AIR SUPPLY DUCT HOSE. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030911000582003091100058NE 2003 9 11 2003UALA00609 220030803A7261 CARBON SEAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE ENGINE FAILED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29590UA 28708 SMOKE AND FUMES IN FLIGHT DECK AND CABIN. ENGINE DISASSEMBLY VERIFIED A BAD NR 2&3 CARBON SEAL. WHEN THIS CARBON SEAL LEAKS, PRESSURE BUILDS UP IN THE NR 1&3 AFT COMPARTMENT. EXCESSIVE PRESSURE ALLOWS OIL TO SEEP PAST AND THOSE SEALS AND ALLOWING BURNING OIL TO ENTER THE BLEED SYSTEM, WHICH FEEDS AIR TO THE CABIN. THE NR 2&3 CARBON SEAL IS A KNOWN PROBLEM THAT IS SYSTEMIC TO THE FLEET. ENGINES MODIFIED WITH A NEW DESIGN NR 2&3 CARBON SEAL WILL ELIMINATE THIS FAILURE MODE. 2L72 4F4 FRTA2NM E17NE 20030911000732003091100073WP 2003 9 11 DHL2003873566 120030701A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT ELEV LWR PLATING OB SEC SHOW CORROSION, DENTS ON SEVERAL SPOTS FROM STA XE.246.000 - XH 285.000. PERFORMED MAJOR REPAIR IAW EODHL-030604, ED-3424. REMOVED FASTERNERS, DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS. CLEANED, TREATED, PRIMED AREA. FAB A NEW SKIN PANEL IAW EODHL-030605, ED-3424. CLEANED, TREATED AND PRIMED NEW SKIN PANEL INTER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-1. INSTALLED NEW SKIN PANEL ON RT ELEV LWR SURFACE OB SECTION (STA. XE.246.000 - XH.285.000) USING NEW FASTENERS IAW EODHL-030605, ED-3424, SRM 51-1-21. FOR RT ELEV REMOVAL, INSTALL SEE N/R 2157 FOR REBALANCING. 2L74 4F RT4A25 20030911000842003091100084WP 2003 9 11 DHL2003873574 120030701A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING OB FLAP UPPER FWD PLATING SHOWS INTERIM REPAIR BETWEEN STA XF.210.000 AND XF.213.000. PERFORMED MAJOR REPAIR IAW EODHL-030612, ED-3442. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EODHL-030612, ED-3442. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FAB NEW SKIN SEGMENT AND SPLICE STRAP IAW EODHL-030612, ED-3442, CLEANED, TREATED AND PRIMED NEW SKIN SEG INTERIOR SURFACE, SPLICE STRAP IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED NEW SKIN SEG AND SPLICE STRAP ON RT WING OB FLAP UPPER FWD PLATING (STA. XF.210.000 - XF.213.000) USING NEW FASTENERS IAW EODHL-030612, ED-3442, SRN 51-1-21. 2L74 4F RT4A25 20030911001112003091100111WP 2003 9 11 DHL2003873525 120030623A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 INTERIM REPAIR ON FWD UPPER PLATING OF RT IB FLAP BETWEEN STA XW.104.000 AND XW.109.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED FWD UPPER PLATING OF RT IB FLAP WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 1. CLEANED, TREATED AND PRIMED INNER FACE OF NEW PLATING IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030911001162003091100116WP 2003 9 11 DHL2003873504 120030612A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING CENTER L/E FORMER CRACKED 0.250 AT XFS 354.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9,10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001532003091100153WP 2003 9 11 AALA20030334 120030227A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 FOUND FOUR DEEPLY BLENDED AREAS BETWEEN STATION 918 AND 930 BETWEEN LONGERONS 3R AND 4R. INSTALLED DOUBLER USING RIVETS AND HI-LOCKS PER SRM 53-04-00 FIG 38. (M) 2L72 4F A6WE 20030911001572003091100157WP 2003 9 11 AALA20030322 120030304A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21459AA 49564 FOUND STATION 255-254 LAVATORY FLOOR SUPPORT BETWEEN LAVATORY TRACK 2 AND 3 CORRODED TOP SIDE AT NUT PLATE. REMOVED FLOOR SUPPORT STATION 254, MANUFACTURED NEW SUPPORT PIECE PER AARD 51-00-00-01. (M) 2L72 4F A6WE 20030911001632003091100163CE 2003 9 11 DXTA200300075 120030729A2432 MOTOR CESSNA500 560CESSNA 2076750CE A/C BAY BURNED E DXTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07328QS 5600428 GROUND CREW OBSERVED SMOKE FROM BATTERY COMPARTMENT. GPU CONNECTED WITH AIR CONDITIONER RUNNING, STRONG SMOKE ODOR IN BATTERY COMPARTMENT. FOUND A/C MOTOR HAD INTERNAL FAILURE (BURNED) REPLACED A/C MOTOR AND SYSTEM OPS CHECKED GOOD. 2L72 4F RTA22CE 20030912000382003091200038WP 2003 9 12 DHL2003604687 120030529A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 INTERIM REPAIR ON FWD LWR CORNER OF AFT PASSENGER DOOR JAMB. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18, SHEET 2, TR 53-135, DWG 5750776, DWG SR08530021. REMOVED INTERIM REPAIR AND EXISTING DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED (2) DOUBLERS IAW SRM 53-2-0 FIG 18 SHEET 2 TR 53-135, DWG 5750776, DWG SR08530021. CLEANED, TREATED, AND PRIMED EXISTING FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 53-2-0 FIG 18, (SHEET 2) TR 53-135, DWG 5750776, DWG SR080530021, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912001122003091200112NM 2003 9 12 AWXA200300879 120030805A252065535944 REVEAL BOEING737 7373G7 1384595NM DOOR FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MINOR REPAIR - DURING C-14 CHECK A .25 INCH CRACK WAS FOUND ON R-1 DOOR UPPER REVEAL DEPRESSOR AT AFT SIDE. MAINTENANCE REMOVED AND REPLACED R-1 DOOR UPPER REVEAL DEPRESSOR IAW B737-300 SRM 51-40-02, PG. 3-4, & 38. 2L72 4F RTA16WE 20030915000422003091500042EU 2003 9 15 I05R089182 120030828A733076228310 INDICATOR UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE FUEL SYSTEM INACCURATE E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 565 3560 FUEL INDICATOR GIVEING ERRONEOUS READINGS, REPLACED PART. 1G72 3U3 U H9EU E00054EN 20030915000612003091500061GL 2003 9 15 ALGA089015 220030905A725023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO N1 COUPLING FOUND TO HAVE INTERNAL SPLINES DAMAGED ON INSPECTION. RETURNED PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20030915000622003091500062GL 2003 9 15 ALGA089016 220030905A725023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE GALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO N1 COUPLING FOUND TO HAVE SPLINES GALLED ON INSPECTION. RETURNED PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20030915000642003091500064SW 2003 9 15 HEEA088950 120030902A2420222375060119 VOLT REGULATOR CLARK 1000 1000CLARK 2230102SW NR 1 GENERATOR INOPERATIVE B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO NR 1 GENERATOR VOLT REGULATOR IS INOPERATIVE. 1Q71 3R 2A6 20030915000862003091500086SW 2003 9 15 ALGA089068 120030909A6510327211 DISC PACK BELL 206 206L1 1182107SW TAIL ROTOR BROKEN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031075W 45377 FOUND 3 CRACKED AND BROKEN DISC. IN THIS ONE PACK. CORROSION PITTING ON ASSY. 1G71 3U H2SW 20030915000882003091500088NE 2003 9 15 BAQA089069 220030729A73130319307840X INJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE FUEL SYSTEM CLOGGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH2015 0131 INJECTOR IS CLOGGED. REPLACED WITH SERVICEABLE UNITS. 9/9/03 1G72 3U3 U H88EU E19EU 20030916000062003091600006NM 2003 9 16 ANCF200300020 120030723A5242 ACCESS DOOR BOEING767 767259 1385136NM E/E BAY OUT OF RIG W ANCFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO23985AN 24618 DURING TAKE OFF ACCESS DOOR LIGHT ILLUMINATED AND EICAS MSG E/E ACCESS DOOR DISPLAYED; TAKE OFF WAS REJECTED AND WHEN LEAVING THE RUNWAY THE MESSAGE WAS NO LONGER DISPLAYED. C/A: MAINTENANCE PEOPLE CHECKED THE DOOR IAW SECURITY AND CONDITION AND WAS FOUND IN NORMAL CONDITION. E/E ACCESS DOOR WAS VERIFIED BY ADJUST AND PROXIMITY SENSORS RIGGING WAS PERFORMED IAW AMM 527100 / 501 WITH SATISFACTORY RESULTS. 2L72 4F RTA1NM 20030916000092003091600009WP 2003 9 16 MEX2003344 120030807A7933699151 STRAINER DOUG DC9 DC987 3022087WP LT ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23754RA 49641 AIRCRAFT RETURN TO PLATFORM DU TO FILTER OBSTRUCTED LT ENGINE LIGHT CAME ON. THE FILTER AND ALARM WERE REPLACED AND ALARM WAS CHECKED IAW MM 79-35-00/01 AND 71-00-01 RESPECTIVELY, ALL TESTS CORRECT. 2L72 4F RTA6WE 20030916000112003091600011NM 2003 9 16 MEX2003343 120030805A3244 TIRE DOUG MD88 MD88 3023688NM MLG FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL6369 6369 53175 AIRCRAFT RETURNED TO PLATFORM, DURING TAXI WHEEL ASSEMBLY NR 4 PRESSURE OUT, THE WHEEL ASSY OF MLG POSITION 4 WAS REPLACED IAW MM 32-40-01, ALL CORRECT. 2L72 4F RTA6WE 20030916000142003091600014NM 2003 9 16 S03453042 120030602A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJFO OTHER O OTHER NRNOT REPORTED 1 WP03 29219 FUSELAGE SKIN IMPACT DAMAGE AT BS 180, S-46R. REPAIRE PER EO 744-53-00-0005 R1 2L74 4F4 FRTA20WE E24NE 20030916000342003091600034NE 2003 9 16 52743 220030719A7532 BLEED VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE FAILED A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07144ZV UE144 ON FLIGHT 5561, THE CREW WAS TAXING OUT WHEN THEY NOTICED THE RT ENGINE WOULD ONLY MAKE 1000 FT LBS TORQUE ON TAKE OFF. THE TAKE OFF WAS ABORTED AND THE AIRCRAFT RETURNED TO GATE WITHOUT ANY FURUTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED THE BLEED VALVE. STILL AWAITING MORE INFORMATION. 2L72 4T4 TRTA24CE E26NE 20030916000392003091600039NM 2003 9 16 03FDEA00980 120030624A5753ARC41252 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT WING OB FLAP IB UP STOP NOSE SUPPORT RIB ISLAND FOUND CRACKED. REMOVED AND REPLACED RT WING OUTBOARD FLAP INBOARD UP STOP NOSE SUPPORT RIB AS IAW SRM 51-31-01 VOL. II. COMPLIED WITH EA 1-5750-71834 - WINGS - TRAILING EDGE FLAPS - OB TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR. 2L73 4F RTA22WE 20030916000442003091600044WP 2003 9 16 GTIA030053 120030209A3297 WIRE DOUG DC9 DC941 302207NWP MLG SENSOR BROKEN A GTIAO OTHER N FALSE WARNING LDLANDING 1 GL23131NK 47605 DURING LANDING GEAR RETRACTION (RT GEAR UNSAFE) LT REMAINED ILLUMINATED. C/W QRH PROC. UPLATCH CHECKS GOOD WITH GEAR EXTENDED FOR LANDING, ALL INDICATIONS NORMAL. FLT 262. FOUND BROKEN WIRE AT RT GER UP LOCK SENSOR, CONNECTOR NR P1-1150. REPINNED IAW STD PCTS 20-50-00. REMOVED AND REPLACED UPLOCK SENSOR AS PRECAUTION. 2L72 4F A6WE 20030916000482003091600048NM 2003 9 16 03FDEA01126 120030723A5270 LIGHT BOEING727 727200 138407ENM AIRSTAIR DOOR ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25484FE 21466 AFT AIRSTAIR LIGHT (AMBER) ILLUMINATED ON DEPARTURE WHILE PASSING 5000 FT -SLAT CLIMB POWER. REMAINED ON AT ALL POWER SETTINGS FOR REMAINDER OF FLIGHT. LIGHT EXTINGUISHED AT TOUCHDOWN. 2L73 4F RTA3WE 20030911002212003091100221EU 2003 9 11 DHL2003368009 120030815A523094FS494295133 SHEAR PIN AIRBUS300 A300B4203 3930306EU CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01368DH 207 MAIN CARGO DOOR WILL NOT LATCH CLOSED. REPLACED SHEAR PIN ON MAIN CARGO DOOR LATCH IAW M/M 52-36-11. OPS CKS GOOD. PIN P/N 94FS494295-133 2L72 4F RTA35EU 20030911002322003091100232WP 2003 9 11 DHL2003604583 120030610A2820 ACCESS PANEL DOUG DC8 DC873F 302199FWP FUEL TANK CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 89636 RT C/W AUX TANK, PERFORM ANTI-CORROSION TREATMENT TO RT UPPER ACCESS DOOR NR 5056. REMOVED CORROSION ON 5056 RT UPPER ACCESS DOOR IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 57-2-1 FIG 43. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ON RT UPPER ACCESS DOOR NR 5056 (RT C/W AUX TANK) IAW SRM 51-1-21 PG 1. SEE N/R 3824 FOR FUEL LEAK CHECK. 2L74 4F RT4A25 20030912000622003091200062WP 2003 9 12 DHL2003604677 120030606A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT HORIZ STAB L/E OUTER SKIN DENTED FROM STA XFS 91.250 - XFS 116.250. PERFORMED MAJOR REPAIR IAW EODHL-030515, ED-3270. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030515, ED-3270. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER, A FILLER IAW EODHL-030515, ED-3270. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER ON LT HORZ STAB L/E OUTER SKIN FROM STA XFS 91.250 TO XFS 116.250 USING NEW FASTENERS IAW EODHL-030515, ED-3270, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000702003091200070WP 2003 9 12 DHL2003604736 120030602A532037540322N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT FITTING CRACKED AT STA 1170.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 51-1-20D PG 9, 21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030912001552003091200155NM 2003 9 12 AWXA200300737 120030626A3150 WARNING SYSTEM BOEING737 7373G7 1384595NM COCKPIT MALFUNCTIONED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28309AW 24711 GEG - ABORTED TAKEOFF - FLT 0301 - ON TAKEOFF ROLL AT GEG EN ROUTE FOR PHX TAKEOFF CONFIGURATION HORN SOUNDED, REJECTED TAKEOFF BELOW 80 KNOTS, TAKEOFF THRUST NOT SET. RECONFIGURED TAKEOFF FLAP HANDLE, SPEED BRAKES, AND STAB TRIM; DEPARTED WITHOUT FURTHER EVENT. 2L72 4F RTA16WE 20030912001832003091200183EU 2003 9 12 AALA20030871 120030818A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211434A 11419 DFW - TWO FLOOR TRACK LIGHT BULBS IN FIRST CLASS INOPERATIVE FOR EMERGENCY PATH LIGHTING. REPLACED SECTION OF TRACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030915000752003091500075EU 2003 9 15 BAQA088792 120030902A6340IPT20RT1100080G TRANSMITTER BOLKMS117 BK117B1 5626012EU GEARBOX OIL FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 PRESSURE TRANSMITTER GIVING NO INDICATION TO GUAGE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030916000462003091600046WP 2003 9 16 JRA2003F00000 120030227A291034000831001581 LINE CVAC 640 640340D 2422814WP RROYCEDART DART54210 54522EU HYD SYS LEAKING A JRAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL11587CA 463 AFTER MOVING THE LANDING GEAR HANDLE (DOWN) AND SELECTING FLAPS (DOWN); THE HYDRAULIC PRESSURE GAUGE READ ZERO PSI. NO FLUID WAS VISIBLE IN THE HYDRAULIC RESERVOIR SIGHT TUBE. WITH BYPASS VALVE SELECTOR (UP) BRAKES OPERATED. HYDRAULIC LINE WAS REPAIRED. 2L72 4T4 TRTA793 E5EU 20030916000792003091600079WP 2003 9 16 GTIA030634 120030813A3260 PROXIMITY SWITCH DOUG DC9 DC981 3022081WP MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23810NK 48015 NOSE GEAR UNSAFE LIGHT ILLUMINATED ON CLIMB-OUT PASSING 20,000 FT THROUGH 23,000 FT THE LIGHT WENT OUT AFTER THAT AND REMAINED OUT. ALL OTHER NORMAL INDICATIONS. IT JUST FLICKERED ON AND OFF. FOUND AIR GAP ON NOSE DOWN LOCK PROXIMITY SWITCH OUT OF LIMITS. ADJUSTED AIR GAP TO WITHIN LIMITS. PERFORMED GEAR RETRACTION CHECK ON NOSE GEAR. OPS CHECKED GOOD. PROXIMITY BOX BITE CHECKED GOOD. NO OTHER DISCREPANCIES NOTED. (M) 2L72 4F A6WE 20030916000852003091600085WP 2003 9 16 GTIA030663 120030811A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FOUND FORWARD PIT FRAME AT FS 465 LONGERON 30 CORRODED OUT OF LIMITS. FABRICATED REPAIR ANGLE, FILLER AND DOUBLER. INSTALLED REPAIR ANGLE, FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20030916000872003091600087WP 2003 9 16 GTIA030665 120030808A5410 ATTACH ANGLE DOUG DC9 DC983 3022083WP RT NACELLE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FTW - FOUND RT ENGINE UPPER PYLON ATTACH ANGLE CRACKED AT CANT 1500. CUT OUT DAMAGED CRACK. FABRICATED ANGLE DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER REPAIR. (M) 2L72 4F RTA6WE 20030916000972003091600097NE 2003 9 16 2003F00555 220030824A7321 FUEL CONTROL BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE NR 1 ENGINE CONTAMINATED A PCSAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO17794AJ 21243 657040 AFTER DEPARTURE FROM KMIA, NR 1 ENGINE RPM BEGAN TO INCREASE AND DECREASE DURING CLIMB OUT. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAITNENANCE INSPECTED NR 1 ENGINE INLET AND EXHAUST IAW CHAPTER 71-00. NO DAMAGE FOUND, INSPECTED FCU AND FOUND WATER IN MOISTURE TRAP. MAINTENANCE CLEANED AND LUBE BELOW IAW MM CHAPTER 73-21-01. PERFORMED RUN UP IAW MM CHAPTER 71-00, OPS CHECK GOOD. AIRCRAFT RETURNED BACK SERVICE. (M) 2L73 4F4 F A3WE E2EA 20030916001022003091600102EU 2003 9 16 ASOA03383 120030722A5320 SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING A C-CHECK, PASSENGER DOOR STEP SUPPORT FRAME AT THE CENTER OUTBOARD NUT PLATE ON THE FIRST AND FOURTH STEPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR STEP SUPPORT FRAME AT THE CENTER OUTBOARD NUT PLATE ON THE FIRST AND FOURTH STEPS IAW SRM 51-25-01. (M) 2H72 4T RT 20030916001092003091600109NE 2003 9 16 AALA20030885 220030820A7261 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RIGHT LEAKING A AALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW21972TW 53622 717857 EN ROUTE LAX-BNA, CREW SHUT DOWN RIGHT ENGINE DUE TO ENGINE OIL QUANTITY PRESSURE LOSS AND COMPRESSOR STALLS. CREW DECLARED EMERGENCY. AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA6WE E9NE 20030916001142003091600114 2003 9 16 AALA20030873 420030817A3160EARLM8504413 MONITOR FOKKERF28 F28MK0100 4990807EU RUDDER DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW211449D 11458 EN ROUTE ORD-EWR, RECEIVED RUDDER 1 AND RUDDER 2 WARNINGS ON CLIMB-OUT. RETURNED TO ORD WITHOUT FURTHER INCIDENT. ACCOMPLISHED BITE CHECK OF AFCAS. SUSPECT RUDDER LIMITER MONITOR UNIT DEFECTIVE. REPLACED RCMU. ACCOMPLISHED STICKING SWITHC TEST AND TEST 40. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030916001172003091600117NM 2003 9 16 AALA20030889 120030822A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21603AA 27054 EMERGENCY PATH LIGHTS AT SEATS 20 AND 24 ARE INOPERATIVE. FOUND GROUND AT LEFT SEAT ROW 24. CHECKED WIRES AND REPLACED BULBS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030916001232003091600123NM 2003 9 16 UIEA200300053 120030828A36103206257 RELIEF VALVE BOEING747 747212B 1384886NM NR 4 ENGINE FAILED A UIEAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA15808MC 21048 LIM-MIA - DURING CLIMB AT FL250, NR 4 NACELLE TEMP WENT OT 8.0 WITH A FIRE BELL AND LIGHT IN NR 4 FIRE SWITCH. WHEN NR 4 THRUST LEVER WAS RETARDED TO IDLE, THE FIRE LIGHT WENT OUT AND THE NACELLE TEMP RETURNED TO NORMAL 2.0. CLOSED NR 4 BLEED VALVE AND ADVANCED THROTTLE. NACELLE REMAINED NORMAL. REMOVED AND REPLACED PRESSURE RELIEF VALVE PER MM 36-11-03. LEAK CHECK OK. REMOVED AND REPLACED REGULATING VALVE, P/N 878806-1, PER MM 36-11-19. LEAK CHECK OK. (M) 2L74 4F A20WE 20030916001252003091600125NM 2003 9 16 AALA20030509 120030429A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21906AN 29508 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT SIGN MOUNTED LIGHTS AT ROWS 9-11L INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030916001282003091600128WP 2003 9 16 AALA20030684 120030623A33500201720004 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2114551 53033 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH FORWARD RED LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SEAT PATH LIGHT. SYSTEM GORUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030916001312003091600131WP 2003 9 16 GTIA030636 120030727A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FWD LAVATORY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND FORWARD LAVATORY INBOARD ASSEMBLY HAS FLOORBOARD CORROSION AND IS DISBONDED. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. REMOVED CORRODED PARTS FROM FLOORBOARD. (M) 2L72 4F RTA6WE 20031029000732003102900073NM 2003 10 29 ASAA0340097 120030228A53106546596 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE BS 727B RBL 11 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000782003102900078NM 2003 10 29 USAA030179 120030825A5314 KEELBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US 22959 FOUND KEELBEAM CORRODED 2 INCHES BY 4 INCHES LONG, RT KEELBEAM STATION 520 AT STRINGER 28 RT. REPLACED WTH FORWARD SECTION OF NEW KEEL BEAM AND SPLICE ANGLES AT STATION S40R PER TYP REP 53-60-09. (M) 2L72 4F RTA16WE 20031029000812003102900081NM 2003 10 29 USAA030180 120030902A5320655163911 ANGLE BOEING737 7373B7 1384580NM MLG DOOR SEAL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 FOUND SEAL ANGLE CRACKED 10.5 INCHES, LEFT GEARWELL, TIRE O/D AT FILLET FAIRING. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20031029000862003102900086NM 2003 10 29 ASAA0240217 120030401A5320654652850 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT NUT PLATES. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000892003102900089NM 2003 10 29 USAABB03177 120030927A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19632AU 27810 CLT - FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031029001002003102900100EU 2003 10 29 YENA200325 120030925A3260 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU MLG MALFUNCTIONED A YENAO OTHER J WARNING INDICATION APAPPROACH 1 EA15503JB 1123 LANDING GEAR MALFUNCTIONED ON FIRST ATTEMPT. SECOND ATTEMPT LANDING GEAR FUNCTIONED PROPERLY. UPON LANDING ECAM L/G SYS DISAREE. CHECKED LGCIU 1 AND 2 FOR LAST LEG HISTORY. FOUND RT DOOR PROX FAULT ON LGCIU NR 2. CHECKED SENSOR 34GA REF TSM TASK 32-31-00-810-816 STEP 3. FAULT NOT CONFIRMED. BITE CHECKED LGCIU 1AND 2 OPERATES NORMALLY. OK FOR FURTHER SERVICE. 2L72 4F RTA28NM 20031110000392003111000039GL 2003 11 10 C2XA03TY192 220031107A7200AE3007A13 ENGINE EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 SW27275126313 6313 145274 CAE311435 AIRCRAFT AIR-RETURNED TO CLE, EMERGENCY DECLARED, THE LEFT ENGINE FAILED IN FLIGHT, ITT SPIKED AT 1100 DEG C, WITH A LOUD BANG. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE, OPS AND LEAK CHECKED GOOD IAW EMB135-MM-71-00-00 AND TASK CARD 6271001. AIRCRAFT RELEASED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031110000482003111000048SO 2003 11 10 RAIA00311279 120031102A2730 CONTROL COLUMN EMB 145 EMB145LR 3260212SO COCKPIT VIBRATION A RAIAA UNSCHED LANDING FE FLT CONT AFFECTED VIBRATION/BUFFET CLCLIMB 1 CE03824HK 145498 5686-STL- FLIGHT CREW REPORTED HIGH FREQUENCY VIBRATION IN ELEVATOR CONTROLS. MAINTENANCE INSPECTED ELEVATOR CONTROL SYSTEM AND PERFORMED ENGINE GROUND RUN, NO DEFECTS NOTED. 2L72 4T RTT00011AT 20031110000792003111000079EA 2003 11 10 COMA0360476 120031028A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE UNSECURE A COMAO OTHER W INADEQUATE Q C CLCLIMB 1 SO01458CA 7613 FLIGHT 5494 AIRCRAFT WOULD NOT PRESSURIZE. FOUND AVIONICS COOLING OVERBOARD SOV ON DEFERRED MAINT LIST TO BE INCORRECTLY SECURED. 2L72 4F RTA21EA 20031110001062003111000106EA 2003 11 10 SWIA200312536 120031023A2722 ROD END CNDAIRCL600 CL6002B19 1900309EA RUDDER ACTUATOR EXCESS PLAY A SWIAO OTHER FE FLT CONT AFFECTED VIBRATION/BUFFET CLCLIMB 1 NM07720SW 7297 RUDDER PEDAL VIBRATION FELT IN LEFT AND RIGHT INPUTS DURING CLIMB TO FL200 AND IN ROUGH AIR. ALSO FELT IN SMOOTH AIR BELOW FL200. FOUND NR 1 RUDDER ACTUATOR ROD END WITH EXCESSIVE PLAY. REPLACED NR 1 ACTUATOR ROD END BOLT AND BUSHING IAW MM 27-24-01. OPS CHECKS GOOD AT THIS TIME. 2L72 4F RTA21EA 20031110001162003111000116NM 2003 11 10 C1HA200392005 120031023A3610652244143 DUCT BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE NR 2 ENGINE DAMAGED A C1HAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15292AS 21458 INFLIGHT NR 2 ENG FIRE LT, BELL ON HIGH EGT AND OIL TEMP CHECKLIST SHUTDOWN NR 2 ENG RETURN. DUMP FUEL, NR 2 ENG THROTTLE FELT STIFF, POSSIBLY BINDING. FUEL CUTOFF LEVER DIFFICULT TO MOVE. PERFORMED VISUAL INOP OF INLET, EXHAUST FOUND 13TH STAGE BLEED SADDLE DUCT SPLIT OPEN APPROX 4 INCHES. REMOVED & REPLACED 13TH STG BLEED SADDLE DUCT (AC REQUIRES ENG RUN, LEAK CHECK. PERFORMED VISUAL INSP OF NR 2 ENG THROTTLE CROSS SHAFT AND ALL THROTTLE RODS FOR SAFETY AND SECURITY. LUBRICATED CROSS SHAFT AND ASSOCIATED CONNECTIONS, CHECKED FUEL CUTOFF LEVER FOR SAFETY, SECURITY, LUBRICATED SHAFT BRGS OPERATED THROTTLES, CUTOFF LEVER APPROX 20 TIMES. ALL OPS NORMAL. RAN ENGINE, RECHECKED, NO DEFECTS NOTED. 2L73 4F4 F A3WE E2EA 20031110001582003111000158WP 2003 11 10 DHL2003873014 120031029A326027749431 STRIKER DOUG DC8 DC873F 302199FWP RT MLG DOOR DAMAGED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01873SJ 46091 DOOR UNLATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION PERFORMED ABNORMAL PROCEDURES TO NO AVAIL. LIGHT EVENTUALLY WENT OUT ON ITS OWN. REMOVED AND REPLACED RIGHT MAIN DOOR STRIKER, FOR INDICATION SYSTEM, STRIKER MOD REMOVED FROM 803DH, OPS CHECKED GOOD, PER 32-60-0 P/N: 2774943-1 PART NR OFF. 2L74 4F RT4A25 20031110001722003111000172NM 2003 11 10 03FDEA01725 120031013A5510ALC81071 FITTING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 HORIZONTAL STAB LT NR 26L BORE FOUND BEARING, SIDE WALL & BOTTOM WITH CORROSION. REAMED BORE FOUND CORROSION EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000. 2L73 4F4 FRTA22WE E13NE 20031110001832003111000183NM 2003 11 10 SWAA032254 120031014A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 574, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031110002002003111000200NM 2003 11 10 SWAA032245 120031013A2710654476121 PCU BOEING737 7373H4 1384600NM MLG WW LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW29357SW 26594 DIVERSION, DECLARED EMERGENCY HYD 'A' SYS QTY IND DECREASED AND 'A' SYS ENG DRIVEN PUMP LOW PRESS LIGHT ILLUMINATED. FOUND HYD FLUID LEAK AT 'A' SYS AILERON PCU. REMOVED AND REPLACED SAME PER MM. 2L72 4F RTA16WE 20030916001362003091600136NE 2003 9 16 GTIA030656 220030826A7230854021 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE NR 2 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 NR 2 ENGINE 1ST STAGE FAN BLADE IS MANGLED BEYOND BLENDABLE LIMITS. REMOVED AND REPLACED TWO C-1 BLADES IAW MD-80 A/C MM REV 76 REV 76 SECTION 72-33-21. COMPLIED WITH TEST 6 AND 1 PER SECTION 72-00-00 PER TIMCO ENGINE CENTER CERT T48R384Y. (M) 2L72 4F4 F A6WE E9NE 20030916001392003091600139CE 2003 9 16 2003F00552 120030726A361033099740183 HOSE BEECH 1900 1900D 1154162CE LEFT ENGINE LEAKING A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO1787551 UE206 UNIDENTIFIABLE ODOR IN THE CABIN WHEN BLEEDS ARE ON. REMOVED AND REPLACED LEFT ENGINE FUEL PURGE PNEUMATIC HOSE. LEAK CHECK GOOD. (M) 2L72 4T RTA24CE 20030916001412003091600141NM 2003 9 16 NACA20030095 120030721A278210605595 ACTUATOR BOEING727 727100 1384036NM NR 2 SLAT FALSE INDICATIONA NACAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AL03930FT 34 19387 NR 2 SLAT LIGHT ON IN FLT WITH FLAPS IN UP POSITION. REPLACED SLAT ACTUATOR. 2L73 4F RTA3WE 20030916001452003091600145WP 2003 9 16 ARWA20030506 120030527A5312 BULKHEAD DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19789AL 46135 DURING (C) CHECK INSPECTION THE FOLLOWING WAS FOUND; STATION 1766 AFT PRESSURE BULKHEAD, L-3R UUPER EAP WITH 2 INCH CRACK. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR PART IAW REPAIR ORDER AROW-031RO-2, PAGE 1 TO 2, DATED 05/01/03 AND REPAIR DRAWING NUMBER AIPSAC-N784AL-02/03, SHEET 1 TO 5, REV.IR, DATED 05/01/03. TREATED AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-8 AND INSTALLED REPAIR PARTS IAW REPAIR ORDER AROW-031RO-2, PAGE 1 AND 2, DATED 05/01/03 AND DRAWING NR AIPSAC-N784AL-02/03. ISSUED FAA FORM 8110-3. NO LEAKS WERE NOTED IAW MM 21-31-0. 2L74 4F 4A25 20030917000202003091700020WP 2003 9 17 0301329156 120030725A5330 SKIN DOUG DC9 DC914 3022034WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018915E 45832 DURING "L" CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 RBL 19. REPAIRED IAW EA 91-195858. 2L72 4F A6WE 20030917000272003091700027WP 2003 9 17 03FDEA01160 120030728A5350UNK CLIP DOUG DC10 DC1010 3022110WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 NR 359 LT FUSELAGE UPPER WING TO BODY SUPPORT RIB ATTACH ANGLES 2EA CRACKED AT STA 1361. CLOSING ACTION ON 07/20/03 REMOVED AND REPLACED BODY SUPPORT ATTACH ANGLES IAW SRM 53-31-01. 2L73 4F A22WE 20030917000282003091700028WP 2003 9 17 03FDEA01153 120030725A5321FXRAM141617 FLOOR PANEL DOUG DC10 DC1010 3022110WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 FORWARD PIT FLOOR PANEL DELEMINATED WITH CORROSION. RECEIVED PANEL AND FAB ON TRAVELER T2/351475 IAW DWG SRZ 25-005. 2L73 4F A22WE 20030917000312003091700031WP 2003 9 17 03FDEA01147 120030725A5710ARB21762 BRACKET DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 NR 1010 RIGHT WING LOWER SPAR-TO-RIB FITTING IS CRACKED AT STA XORS 402 LWR SPAR S36. CLOSING ACTION ON 07/23/03, REMOVED BUTTERFLY BRACKET IAW SRM 51-33-01, INSTALLED NEW BRACKET IAW SRM 51-33- 01. TORQUE HI-LOCKS IAW SRM 51-31-01. SEALED IAW SRM 51-41-01. 2L73 4F A22WE 20030917000332003091700033SW 2003 9 17 GXPA0304 120030617A7920 LINE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE331* 01514WP ENGINE OIL SYS LOOSE E GXPAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL23616GA TC377 54075 NR 2 ENGINE SLOWLY LOST OIL PRESSURE, SHUT DOWN IN FLIGHT. FOUND OIL LINE TO LOWER COWL LOOSE. TIGHTENED LINE AND REMOVED CONICAL SEAL. GROUND RUN AND LEAK CHECKED, OK. 2L72 4T3 TRTA8SW E2WE 20030917000462003091700046EU 2003 9 17 03FDEA01178 120030730A5330 DOUBLER AIRBUS300 A300F4605R 3930327EU FUSELAGE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25683FE 801 RT CREW ENTRY DOOR CUTOUT FAILSAFE DOUBLER GOUGED/WORN FROM FORWARD TO AFT CUTOUT BLENDED AREA AND PERFORMED HFEC (NO CRACKS INDICATED). CHECK PRELOAD ON COVER PLATE IAW DRW A007 10134. REPROTECTED AREA AND REFINISHED. ALL WORK DONE IAW EA 6-5312-71388 AND RAS NR AS-179-2003. 2L72 4F RTA35EU 20030912001152003091200115NM 2003 9 12 AWXA200300882 120030728A53206935365 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND FLOOR SUPPORT SHEAR WEB AT BS 540, LBL 45. MAINTENANCE REMOVED FLOOR SUPPORT SHEAR WEB AT BS 540, LBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SHEAR WEB; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-01, PG 1. 2L72 4F RTA16WE 20030912001812003091200181WP 2003 9 12 AALA20030879 120030820A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21513AA 49890 EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 20 TO BACK OF AIRCRAFT. CLEANED AND SECURED CONNECTION AT ROW 20 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030917000622003091700062NE 2003 9 17 HEEA089035 220030827A7200CT72A ENGINE BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 2 MALFUNCTIONED B HEEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW03598069574 28140 ENROUTE FROM GB-426, AIRCRAFT LOST POWER ON NR 2 ENGINE. CONTINUED TO MCY AND PERFORMED SINGLE ENGINE LANDING. 2G72 4U4 U H10SW E8NE 20030917000632003091700063SW 2003 9 17 ALGA089042 120030908A6210206015001115 BLADE BELL 206 206L4 1182110SW MAIN ROTOR DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03177AL905 52157 LOWER SURFACE GRIP FINGERS FOUND DEBONDED AT STA.38 - 43.5. DAMAGE APPEARS TO BE MANUFACTURING DEFECT. BLADE ASSY. WAS SENT TO BELL HELICOPTERS FORTWORTH. CUSTOMER PROPERTY RETURN. 1G71 3U NCH2SW 20030917000732003091700073EU 2003 9 17 BAQA088153 120030904A672041800876800 ACTUATOR UROCOPEC135 EC135T1 5620026EU TAIL ROTOR FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH1973 0131 YAW SAS FAILURE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031118001132003111800113NM 2003 11 18 AWXA200301189 120030912A5321144N533025 FLOOR PANEL BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL N-2 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 146N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1. 2L72 4F4 FRTA2NM A12EU 20031119000112003111900011NM 2003 11 19 UPS03241379 120031010A5312 PRESSURE PANEL BOEING727 7271A7C 13840X2NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 INSPECTION TYPE: C, 3 CRACKS AT ADJACENT RIVETS ABOVE DECAL AT LT AFT PRESS PANEL CUTOUT. AREA CUTOUT I.A.W. SRM 51-40-2 FIG.1. 2L73 4F A3WE 20031119000132003111900013WP 2003 11 19 UPS03841370 120030923A53403758497U2 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STATION 1140 LONGERON 35R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 3758497,AND SRM.51-1-20D 2L74 4F4 FRT4A25 E2GL 20031119000322003111900032SO 2003 11 19 LR7A03081 120031009A53153982435 FLOORBEAM LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 463 4606 DURING SCHEDULED B1 INSPECTION 02/GEN/16 ACCOMPLISHMENT FOUND FS 737, BL 0, WL 146 'D' RING PULLED. FURTHER ACCESS REVEALED FLOORBEAM UPPER CAP CORRODED. REPLACED CAP IAW SRM SMP 583 53-40-06. NR 0012. 2H74 4T4 T A1SO E282 20031119000412003111900041EU 2003 11 19 AWXA200301204 120030924A5320D539116032000 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON FWD CARGO COMPARTMENT RT PROFILE BETWEEN FR 28 AND FR 31, AT FASTENER HOLES. MAINTENANCE CUTOUT CORROSION ON RT PROFILE BETWEEN FR 28 AND FR 31; FABRICATED A PROFILE REPAIR SECTION AND SPLICE DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5320-03154-SS1 2L72 4F RTA28NM 20031119000752003111900075WP 2003 11 19 ABXA030390 120030923A534059516853 FITTING DOUG DC9 DC932F 3022067WP LONGERON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 CRACKED LONGERON END FITTING STA. 756, LONGERON 29 LEFT. REPLACED LONGERON 29 LEFT END FITTING IAW DC-9 SRM. 2L72 4F A6WE 20031119000812003111900081NM 2003 11 19 QXEA200301228 120031010A561017180003 WINDOW DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 CRACKED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09350PH1455714557 488 ON FLIGHT 2192 CLIMBING THROUGH 18,000 THE CAPTIANS SIDE WINDOW CRACKED FROM TOP TO BOTTOM. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CAPTIANS SIDE WINDOW. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031119000842003111900084NM 2003 11 19 QXEA200301267 120031009A3397 WIRE DHAV DHC8 DHC8202 2809007NM ZONE 200 EXPOSED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09364PH 524 ON FLIGHT 2046 FLIGHT ATTENDENT'S PREFLIGHT, FOUND WIRES EXPOSED ON EMERGENCY TRACK LIGHTING. REPLACED MISSING CLEAR PLASTIC COVER STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031119000912003111900091EU 2003 11 19 AWXA200301211 120031010A3230 CONTROL UNIT AIRBUS320 A320232 3930326EU MLG FAILED A AWXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP28659AW 1166 ON SHORT AND FINAL APPROACH INTO EWR EN ROUTE FROM PHX RECEIVED LANDING GEAR CONTROL AND INTERFACE UNIT (LGCIU) FAULT. EXECUTED MISSED APPROACH AND DECLARED EMERGENCY ON SECOND APPROACH. CONTRACT MAINTENANCE PERFORMED A LANDING GEAR BITE TEST IAW AMM 32-69-00, PG. 501, NO. 2 LGCIU TESTED GOOD, NO DEFECTS NOTED. 2L72 4F RTA28NM 20031119000942003111900094EU 2003 11 19 AWXA200301214 120030924A5320D5347048120000 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT PROFILE BETWEEN FR 51 AND FR 52. MAINTENANCE REMOVED DAMAGED AREA ON RT PROFILE BETWEEN FR 51 AND FR 52; FABRICATED A REPAIR SPLICE AND DOUBLER; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5320-03154-SS1. 2L72 4F RTA28NM 20031119001002003111900100NM 2003 11 19 QXEA200301270 120031009A7120 SUPPORT DHAV DHC8 DHC8202 2809007NM ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 GOUGES ON INBOARD LOWER ENGINE SUPPORT STRUT ON NR 1 NACELLE. REPAIRED IAW HORIZON AIR EA 2-54-189. 2H72 4T RTA13NM 20031119001012003111900101NM 2003 11 19 PCAA0310123 120031012A26113023143 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY FALSE INDICATIONA PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13844EX236023151 339 CREW REPORTED THAT THE BAG BAY SMOKE LIGHTS HAD ILLUMINATED IN FLIGHT FOR APPROXIMATELY 10 SECONDS. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THE CAGE ON THE FORWARD DETECTOR WAS FOUND TO BE SLIGHTLY DENTED. THE FORWARD SMOKE DETECTOR WAS REPLACED AND THE CAGE WAS STRAIGHTENED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031110000672003111000067SO 2003 11 10 C2XA03SH440 120031110A521014524131011 BRACKET EMB 145 EMB145LR 3260212SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110000702003111000070EU 2003 11 10 AWXA200301373 120031106A3350321452 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28626AW45583 65 TPA - EEL - DURING TAXI FOR DEPARTURE FLIGHT ATTENDANT CALLED SAYING THAT THE L-2 + R-2 DOOR EMERGENCY EXIT SIGNS WERE NOT ILLUMINATED. ALSO FOUND OVERHEAD EXIT SIGN BETWEEN LAVATORIES INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031119001112003111900111NM 2003 11 19 C1HA200394023 120031013A3350 BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSY IAW 727 MM 33-50-22, ALL OPS NORMAL. 2L73 4F A3WE 20031110002022003111000202 2003 11 10 SWAA032228 420031009A25656557463 ATTACH FITTING BOEING737 7377H4 1384404NM ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29730SW 27862 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACHMENT FITTING LOOSE. SECURED ATTACHMENT FITTING PER MM. 2L72 4F RTA16WE 20031110002142003111000214EU 2003 11 10 AALA20031060 120030924A33506104789 BATTERY PACK FOKKERF28 F28MK0100 4990807EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW211425A 11408 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE IN THE FLOOR PROX LIGHTING. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031118000712003111800071WP 2003 11 18 MWEA030412 120031008A2797 WIRE DOUG DC9 DC932 3022066WP RUDDER BROKEN A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31302ME 47102 AFTER CONTROL CHECK, THE RUDDER TRAVEL UNRESTRICTED LIGHT WENT OUT, WHEN LEFT RUDDER IS MOVED 3 INCHES THE LIGHT ILLUMINATED AND WHEN THE RIGHT PEDAL IS MOVED FULL TRAVEL THE LIGHT STAYS OUT. REMOVED AND REPLACED SWITCH AND BROKEN WIRES. 2L72 4F A6WE 20031118000782003111800078NM 2003 11 18 P5CA0300962 120031008A7830 THRUST REVERSER BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 2 ENGINE DEPLOYED A P5CAK NONE O OTHER TOTAKEOFF 1 WP23921FT 21575 689184 NR 2 ENG THRUST REVERSER DEPLOYED ON T/O ROLL AT 80 KTS. NR 2 ENG T/R DEACTIVATED PER DDPG 78-1 AND MM 78-31-00. ACCOMPLISHED HIGH ENERGY STOP HEAT DAMAGE CONDITIONAL INSP PER MM 5-51-10. 2L74 4F4 F A20WE E3NE 20031118000972003111800097CE 2003 11 18 54992 120031006A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT TORQUE FAILED A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07126YV UE126 RIGHT TORQUE GAUGE FAILED ON TAKE OFF DURING INITIAL POWER UP. RETURNED TO GATE AND CALLED MX. REPLACED GAUGE OPS CK GOOD P/N 114-3800-653 SN 390MU. 2L72 4T3 TRTA24CE E2NE 20031118001022003111800102NM 2003 11 18 AWXA200301178 120030919A5420311N5002127 SUPPORT ANGLE BOEING757 7572S7 1384962NM NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MINOR REPAIR - DURING C-09 CHECK A .625 INCH CRACK WAS FOUND ON NR 1 ENGINE PYLON FORWARD OUTBOARD SUPPORT ANGLE. MAINTENANCE REMOVED CRACKED FORWARD OUTBOARD SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE PER DWG 311N5002; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PARA 7-D. 2L72 4F RTA2NM 20031118001142003111800114NM 2003 11 18 AWXA200301190 120030912A5321144N533042 FLOOR PANEL BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL K-4 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 144N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1. 2L72 4F4 FRTA2NM A12EU 20031119000382003111900038EU 2003 11 19 AWXA200301201 120030924A5320D5347048120000 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT PROFILE AT FR 49. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF RT PROFILE AT FR 49; FABRICATED PROFILE REPAIR SECTION AND REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5320-03154-SS1 2L72 4F RTA28NM 20031119000522003111900052NM 2003 11 19 CALA0300586 120031011A5310 SUPPORT BEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714324 23375 INSPECTION FOUND MAIN DECK LT AND RT LAV WALL SUPPORT BEAMS CORRODED AT STA 993, LBL14-44 AND RBL 14-44. NEW SUPPORT BEAMS WERE INSTALLED IAW SRM 51-10-2. 2L72 4F RTA16WE 20031119000562003111900056NM 2003 11 19 CALA0300590 120031012A5350 SUPPORT ANGLE BOEING737 7373T0 1384582NM FAIRING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A 2 INCH CRACK IN LT WING TO BODY FAIRING SUPPORT ANGLE AT BS 535. THE ANGLE WAS REPAIRED IAW ECRA 5350-01227. 2L72 4F RTA16WE 20031119000762003111900076WP 2003 11 19 MWEA030421 120031013A2420914F5655 CONTROL PANEL DOUG DC9 DC932 3022066WP E/E BAY INOPERATIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31209ME 47730 ON START OF RT ENGINE, AC CROSS-TIE LOCK OUT CAME ON, UNABLE TO RESET. REMOVED AND REPLACED AC BUSS CONTROL PANEL. 2L72 4F A6WE 20031119000772003111900077WP 2003 11 19 MWEA030414 120031013A532199365853 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 RIGHT CABIN FLOOR BOARD BETWEEN SEAT TRACK 3 AND 4 IS CRACKED APPROXIMATELY 18 INCHES FROM FORWARD END. -- REPAIRED. 2L72 4F A6WE 20031119000892003111900089 2003 11 19 AWXA200301209 420031011A23706176001004 MODULE AIRBUS320 A320232 3930326EU SEAT ROW 11 RT DEFECTIVE A AWXADH RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP28638AW247179 455 SMOKE IN CABIN - WHILE TAXIING TO RUNWAY, SEAT ROW 11 RT VIDEO SCREEN DID NOT COME DOWN AND WAS FOLLOWED BY SMOKE IN THE CABIN, AIRCRAFT RETURNED TO GATE. ISSUED MEL 25-22-03, COND. 2 (VIDEO SAFETY DEMO SYSTEM INOP). WHEN AIRCRAFT RETURNED TO PHX ON 10/11/2003 MAINTENANCE REMOVED AND REPLACED THE VIDEO MONITORING AND TAPING UNIT IAW AMM 23-36-22, AND 23-36-44, OPERATIONAL CHECK WAS GOOD. PART NAME; TAPING UNIT, MFG; SONY TRANS; P/N; 700-1545-001, S/N; 2513, TT; 33331, TC; 13707 2L72 4F RTA28NM 20031119000952003111900095EU 2003 11 19 AWXA200301215 120030924A5320D5347047220600 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT LT PROFILE AT FR 57. MAINTENANCE REMOVED DAMAGED LT PROFILE BETWEEN FR 56 AND FR 57; INSTALLED NEW REPLACEMENT PROFILE IAW A320 SRM 51-42-11, PG. 21-22, FIG. 8, PG. 8-10, FIG. 2, AND PG. 12, FIG. 3. 2L72 4F RTA28NM 20031110001512003111000151NM 2003 11 10 AWXA200301350 120031101A2120 ODOR BOEING737 737301 1384611NM CABIN DETECTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28326AW 23258 SLC - DIVERSION - FLT 0587 - EN ROUTE FROM PHX TO GEG FLIGHT ATTENDANTS NOTICED A STRONG SULFUR ODOR IN THE CABIN THAT SEEMED TO COME AND GO, DIVERTED TO SLC. MAINTENANCE RAN AIR CONDITIONING PACKS, PRESSURIZED THE AIRCRAFT AND INSPECTED THE INTERIOR LIGHTING SYSTEM, NO SMELLS WERE NOTED. 2L72 4F RTA16WE 20031110001672003111000167NM 2003 11 10 03FDEA01870 120031105A5310 SHEAR TIE BOEING727 727200 138407ENM GE CF6 CF680 30025NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE ON AFT SIDE OF BS 700 FRAME RBL 9 WL 148. REPAIR PER SRM 53-10-4 FIG 13 SHT 1 AT BS 700, RBL 9, WL 148. 2L73 4F4 FRTA3WE E13NE 20031110002092003111000209EU 2003 11 10 AALA20030973 120030908A3397 WIRE AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2140064 507 MIA - FLT 984 - EMERGENCY EXIT LIGHT INOPERATIVE AT ROWS 35C. RESECURED WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031110002102003111000210NM 2003 11 10 AALA20030984 120030909A5320 SUPPORT BEAM BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21184AN 29594 TUL - FOUND SUPPORT BEAM UNDER DOOR SILL PLATE CORRODED, AFT CARGO STATION 1380 TO 1440. (M) 2L72 4F RTA2NM 20031110002152003111000215WP 2003 11 10 AALA20031084 120030930A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE AFT SERVICE DOOR LOCATION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031119001162003111900116NM 2003 11 19 2003UALA00744 120031003A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29791UA 26933 EMERGENCY LIGHT ON MOVABLE ARMREST OF SEAT 3E DAMAGED. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20031119001222003111900122NM 2003 11 19 2003UALA00751 120031006A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 FUSELAGE SKIN DENTED AT BS 1690 AND STRINGER S-20L LAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031119001442003111900144NM 2003 11 19 QXEA200301232 120031002A5410 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX- REPLACE EXISTING LOWER RIGHT COWL PARTS WITH THICKER ONES. REPAIRED IAW HORIZON AIR EO 6-71-103. 2H72 4T RTA13NM 20031120000052003112000005SO 2003 11 20 SWIA200312490 120030904A5310 WINDOW FRAME EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07218SW 120287 LEFT DV WINDOW AFT BRACKET CRACK FRAME 12/13 DAMAGE OUT OF LIMITS. DISCOVERED DURING C-CHECK. REPLACED BRACKET AT FRAME 12/13 CENTER OF LEFT DV WINDOW PER SRM 51-40-00. 2L72 4T4 TRTA31SO E20NE 20031120000152003112000015NM 2003 11 20 AWXA200301224 120030920A532069353654 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MINOR REPAIR - DURING C-17 CHECK A .875 INCH CRACK WAS FOUND ON L-ANGLE FOR VERTICAL FLOOR SUPPORT BS 500-520, BL 0. MAINTENANCE REMOVED CRACKED L-ANGLE FOR VERTICAL FLOOR SUPPORT BS 500-520, BL 0; FABRICATED A NEW REPLACEMENT L-ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1. 2L72 4F RTA16WE 20031120000172003112000017NM 2003 11 20 AWXA200301226 120030922A53206546812174 ANGLE BOEING737 737301 1384611NM LAV MOUNT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY AFT MOUNT SUPPORT ANGLE BS 1028, RBL 18, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT LAV MOUNT SUPPORT ANGLE BS 1028, RBL 18, WL 208; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1, FIG 12. 2L72 4F RTA16WE 20031120000222003112000022NM 2003 11 20 AWXA200301231 120030920A5312651630051 FRAME BOEING737 737301 1384611NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 PERCENT CRACK WAS FOUND ON INBOARD RADIUS OF BS 178 BULKHEAD VERTICAL WEB AT LBL 5.7, WL 186. MAINTENANCE CUT OUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB AT LBL 5.7, WL 186; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY AND NO CRACKS EXIST. FABRICATED A FILLER, 4 EACH REPAIR ANGLES, AND 2 EACH STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG 221-240, FIG 205. 2L72 4F RTA16WE 20031120000542003112000054NM 2003 11 20 QXEA200301242 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 SMALL NICK AND SCRATCHES 5 INCHES LONG ON TOP FLANGE OF NR 3 SEAT TRACK 12 INCHES FORWARD OF AFT END. REPAIRED IAW DHC-8 SRM 51-00-06, 51-70-36 AND RD 8-53-3644. 2H72 4T RTA13NM 20031120000562003112000056NM 2003 11 20 QXEA200301245 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 5 SEAT TRACK TOP FLANGE IS SCRATCHED 3 INCHES LONG AT STATION X445.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20031120000692003112000069EU 2003 11 20 025251 120031014A3020 THERMISTER SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE RT INTAKE FAILED A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17104CQ 340A104 357 DRG876684 FLIGHT 4556 PIT-FWA. DURING CLIMBOUT AT APPROXIMATELY 5000 FT, THE RT ENGINE INTAKE HEAT WARNING LIGHT ILLUMINATED. A/C RETURNED TO PIT. A/C TAKEN OUT OF SERVICE 10-14-03 AT 1750 (LT). PIT MX SWAPPED TO A SPARE THERMISTOR ON THE RT INTAKE HEAT SYSTEM AND SEALED THE RT EXHAUST NOZZLE. GROUND RAN A/C FOR 15 MINUTES WITH NO FAIL. A/C RETURNED TO SERVICE 10-14-03 AT 1840 (LT). 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20031120000712003112000071NM 2003 11 20 QXEA200301259 120030928A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NUMEROUS ROCK CHIPS AND SCRATCHES IN LOWER FUSELAGE SKIN AT STATIONS 312.0 THROUGH 396.0 AND STRINGERS 29 LEFT HAND AND RIGHT HAND. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16, 51-20-36 AND 51-20-51. 2H72 4T RTA13NM 20031120000872003112000087CE 2003 11 20 4516210142003 120031014A2740 WARNING SYSTEM LEAR 45 45LEAR 5170805CE PRIMARY TRIM MALFUNCTIONED E J7SAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW05426CX 45162 PRIMARY TRIM FAILURE INDICATION ON EICAS SYSTEM. CREW HAD JUST INITIATED TAKE-OFF ROLL. TAKE-OFF ABORTED AND RETURNED TO BLOCK. CREW CLEARED FAULT ON EICAS SYSTEM. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. FSR RECOMMENDATION TO SWAP IC-600 COMPUTERS AND PERFORM TEST FLIGHT. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASE FROM MAINTENANCE. 2L72 4F RTT00008WI 20031120000922003112000092NM 2003 11 20 DHL2003745020 120031014A3260 LIGHT BOEING727 727224 1384076NM PWA JT8 JT8D* NE MLG INDICATOR INOPERATIVE A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01745DH 20665 RIGHT GEAR GREEN LIGHT FAILED TO ILLUMINATE DURING EXTENSION. GREEN LIGHT CAME ON AFTER CYCLING THE GEAR. CLEANED AND CHECKED CONNECTION TO MASTER DIM AND TEST SWITCH OPS NORMAL IAW B-M/M 33-15-00. OK FOR SERVICE. 2L73 4F4 F A3WE E2EA 20031120001082003112000108EA 2003 11 20 03286667 120031013A335064643 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27667BR 7535 DURING INSPECTION THE EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT POWER STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031120001092003112000109NM 2003 11 20 AWXA200301250 120030919A5330654578988 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A .7500 INCH CRACK WAS FOUND ON LOWER FUSELAGE SKIN AT COUNTERSUNK FASTENER HOLE BS 436, (0) BL. MAINTENANCE CUTOUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED A FILLER, DOUBLER, SPACER RING, AND REINFORCING RING; INSTALLED REPAIR PARTS IAW 03-5331-03268-ES1. 2L72 4F RTA16WE 20031120001132003112000113NM 2003 11 20 PCAAO311139 120031110A5320 SILL DHAV DHC8 DHC8102 2809003NM FUSELAGE DAMAGED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13809EX 302 WHILE AIRCRAFT 809EX WAS IN ROUTINE MAINTENANCE, IT WAS FOUND THAT THE BAGGAGE DOOR UPPER SILL HAD BEEN DAMAGED FROM THE BAGGAGE DOOR HANDLE COMING IN CONTACT WITH THE SILL. MAINTENANCE COMPLIED WITH REPAIR DRAWING8-53-3334 ISSUE 2. AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2H72 4T RTA13NM 20031120001222003112000122 2003 11 20 03313331 420031109A31607011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU NR 2 INOPERATIVE A VTZAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 EA27331UE 41099 DURING FLIGHT 7800 CLIMB THE NR 2 SYMBOL GENERATOR FAILED CAUSING A LOSS OF CENTRAL DISPLAY OF INSTRUMENTS. THE SYMBOL GENERATOR WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK OF THE FLIGHT DISPLAY SYSTEM WAS ACCOMPLISHED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031120001312003112000131NM 2003 11 20 AWXA200301456 120031029A5320651758243 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 DURING C-13 CHECK A 1 INCH CRACK WAS FOUND IN VERTICAL WEB AT BS 184, LBL 17.1, WL 235. MAINTENANCE CUT OUT DAMAGE IN WEB AT BS 184, LBL 17.1; FABRICATED A NEW SECTION OF WEB, 2 EACH STIFFENERS, AND A TAPERED SHIM; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08 FIG 212 PG 288K-288N, 288Q, AND 288T. 2L72 4F RTA16WE 20031121000132003112100013NM 2003 11 21 SWAA032463 120031106A53116546569 BELTFRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED C4 CHECK, FOUND CORROSION ON BELTFRAME AT BS 967 BETWEEN STR 27R AND 27L. REPAIRED PER EA. 2L72 4F RTA16WE 20031121000182003112100018 2003 11 21 SWAA032481 420031109A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031121000262003112100026NM 2003 11 21 VNAA0311004 120031111A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07429JS908 164 3043 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 6 TO 9 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031121000272003112100027EA 2003 11 21 03320677 120031116A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FALSE INDICATIONA VTZAO OTHER F FLT CONT AFFECTED LDLANDING 1 EA27677BR 7652 DURING LANDING OF FLIGHT 7401 TO SYR CREW REPORTED A FLAP FAIL AT ZERO DEGREES. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. A SATISFACTORY OPERATIONAL CHECK OF THE FLAP SYSTEM WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031121000302003112100030NE 2003 11 21 DXTA200300158 220031109A7200 ENGINE BRAERO1000 HAWKER1000 7450005EU PWA 305 PW305B 52128NE LEFT MALFUNCTIONED E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL07550QS 259050 PCE305114 DURING CLIMB OUT HEARD SEVERAL RAPID POPS LASTING 3-4 SECONDS, TWO EVENTS SPACED 10-15 SEC APART. LEFT ENG N1, ITT, N2 FLUCTUATED, ALSO EXPERIENCED SOME AIRFRAME VIBRATIONS. DECLARED EMERGENCY AND ACCOMPLISHED AIR TURNBACK TO VNY. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA3EU E35NE 20031121000382003112100038 2003 11 21 HNAA0300067 420031106A3442071131900 ANTENNA DHAV DHC8 DHC8102 2809003NM RADAR INOPERATIVE A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07906HA30213970 9 LOST RADAR SHORTLY AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD, WITHOUT TALKING TO MAINTENANCE. PILOT REPORTED RADAR STAB INOP, PLUS OTHER FAULTS. CREW TURNED RADAR OFF AND BACK ON, NO FIX. REPLACED RADAR RT. 2H72 4T RTA13NM 20040113001972004011300197SO 2004 1 13 RAIA00312308 120031210A304090024252 CONTROL BOX EMB 145 EMB145LR 3260212SO WINDSHIELD WIPERFAILED A RAIAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03814HK 145046 STL- CAPT SIDE WINDSHIELD WIPER INOP. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S WIPER CONTROL BOX. 2L72 4T RTT00011AT 20040113002362004011300236NM 2004 1 13 QXEA200301477 120031125A3620 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM BLEED AIR SYS FAULTY A QXEAO OTHER N FALSE WARNING DEDESCENT 1 NM09414QX 4061 PDX- ON FLIGHT 2255 NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED DURING DESCENT. TURNED BLEED OFF IAW CHECKLIST AND CAUTION LIGHT WENT OUT. CLEANED AND REPINNED CANNON PLUG 2121-P4. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040114000432004011400043NM 2004 1 14 DL757030957 120031024A5320146N851210 SILL BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27617DL 22907 THE OUTBOAD CHORD OF THE C2 DOOR OPENING LOWER SILL WAS FOUND CORRODED. TO FACILITATE REPLACEMENT OF THE SILL CHORD, THE OUTER CHORD AND WEB OF THE FS 1440 FRAME WERE CUT NEAR THE LOWER SILL AND THE LOWER SECTIONS REMOVED. A NEW SILL CHORD WAS INSTALLED AND THE FRAME WEB AND CHORDS SPLICED BACK IN WITH ALUMINUM REPAIR DOUBLERS PER ER/A 385725-14, REV A. 2L72 4F RTA2NM 20040114000442004011400044NM 2004 1 14 DL757030958 120031024A5330146N351112 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27617DL 22907 THE FUSELAGE SKIN WAS FOUND DENTED BELOW THE C2 DOOR OPENING BETWEEN FS 1420 &1440 AND BETWEEN STRINGERS 29L & 28R. THE DENTED AREA WAS REMOVED WITH A 25.25 X 7.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385730-14, REV A. 2L72 4F RTA2NM 20040114000592004011400059NM 2004 1 14 DLM88030976 120031031A2121251301 FAN DOUG MD88 MD88 3023688NM E/E BAY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27912DE 49997 ON CLIMBOUT OF BHM TWO STANDBY RADIO RACK FAN CIRCUIT BREAKERS POPPED AT APPROX 6000 FT. THIS WAS FOLLOWED BY ELECT SMOKE SMELL IN COCKPIT AND CABIN. NO VISIBLE SMOKE PRESENT. SHORTLY AFTER THE 3RD STBY FAN CIRCUIT BREAKER POPPED. THE CREW THEN SELECTED VENTURI POSITION OF RADIO RACK COOLING AND RETURNED TO BHM. REPLACED STANDBY RADIO RACK FAN AND R2-296 RELAY. 2L72 4F RTA6WE 20040114000722004011400072NM 2004 1 14 DLM88030988 120031107A2432203BC1021 CHARGER DOUG MD88 MD88 3023688NM E/E BAY FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27964DL 49983 UPON ARRIVAL, FOUND COCKPIT FULL OF SMOKE. CABIN HAD SOME SMOKE VISIBLE WITH A SMOKEY ODOR. A/C BATTERY WAS ON POWER AND AIR WAS PROVIDED BY GRD UNITS. OPENED E+E ACCESS DOOR FOR T/S CKD E+E DOOR. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY CHARGER RELAY R2-56. BATTERY CHARGER OPS NORMAL. STARTED APU TO DRAW DOWN BATTERY. BATTERY VOLTAGE AND AMPS CHECK NORMAL. 2L72 4F RTA6WE 20040114001582004011400158WP 2004 1 14 AAL20031474 120031228A33500211720004 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 DFW DURING OVERNIGHT MAINTENANCE FOUND SEAT MOUNTED EMERGENCY PATH LIGHTING AT 10D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040114001612004011400161NM 2004 1 14 AALA20031476 120031227A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21634AA 24592 MIA DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY LIGHTS SEAT 24D AND AFT INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040114001732004011400173EU 2004 1 14 MALA030605 120031229A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4Y/2Y INSPECTION IN LCQ, FS 640-686 RT OB SEAT TRACK HAS CORROSION. MECHANIC REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW EO NR S53060 DATED 3 NOV 2003 REV II. A/C RELEASE DATE 01/09/04. REFER TO NR 1196389 FOR ADDITIONAL DETAIL. 2L72 4T RTA52EU 20040114002162004011400216NM 2004 1 14 MWEA030490 120031215A5330593602229 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FUSELAGE SKIN AT STATION 1107 REQUIRES REPAIR BETWEEN LONGERON 28 AND 29 LT AND 28 AND 29 RT DUE TO THE DEACTIVATION OF THE VERIZON PHONES. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20040115000112004011500011NM 2004 1 15 03FDEA02026 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 1 FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000182004011500018NM 2004 1 15 03FDEA02033 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 1 I/B UNFLANGE SIDE CORRODED COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000202004011500020NM 2004 1 15 03FDEA02035 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 1 I/B BUSHING LOOSE & HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000992004011500099WP 2004 1 15 03FDEA02282 120031227A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 COMPLY WITH EA 8-5310-73862. FUSELAGE MAINFRAME- MINOR DEVIATION TO SRM SEAT TRACK SPLICE. CLOSING ACTION ON 12/24/03. ON N/R S00031. COMPLIED WITH EA 8-5310-73862. 2L73 4F A22WE 20040115001362004011500136NM 2004 1 15 DLM88031102 120031217A3350RPS1 POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27953DL 49884 ROWS 10-13 EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY AND BATTERY PACK. 2L72 4F RTA6WE 20040115001372004011500137NM 2004 1 15 03FDEA02148 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. ACCESS FROM PNL 364MR. RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS PER SRM51-33-01 VOL2 2L73 4F RTA22WE 20040115001472004011500147NM 2004 1 15 DLM88031110 120031219A2450947F9453 CONTROL PANEL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE ELECTRICAL SYS FAULTY A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO27934DL 49721 718124 RIGHT GENERATOR OFF LIGHT AT 8000 FT CLIMBING OUT OF CVG. RESET PER POM, NO JOY. REPLACED RT ENGINE GENERATOR CONTROL PANEL PER ELECTRICAL DISTRIBUTION PANEL FAULT LIGHT. RAN ENGINES, ALL GENERATORS CK OK. 2L72 4F4 FRTA6WE E9NE 20040115001522004011500152NM 2004 1 15 DL76S031113 120031218A5312141T2110123 BULKHEAD BOEING767 767332 1382001NM FUSELAGE BIRD STRIKE A DALAK NONE O OTHER ININSP/MAINT 1 SO27119DL 23278 THE WEB OF THE FWD PRESSURE BULKHEAD AT FS 132.5 WAS PUNCTURED AS A RESULT OF A BIRD STRIKE BETWEEN LBL 10.6 & 16. THE VERTICAL BEAMS AT LBL 10.6 & 16 WERE DENTED. THE DAMAGED AREA OF WEB WAS REMOVED WITH A CUTOUT AND THE DENTED FLANGES OF THE BEAMS TRIMMED OUT. THE WEB WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER AND THE FLANGES WITH ALUMINUM REPAIR ANGLES PER ER/A 087969-14, REV A. 2L72 4F RTA1NM 20040115001642004011500164NM 2004 1 15 DLM88031119 120031221A3350 LIGHT DOUG MD88 MD88 3023688NM CABIN MISSING A DALAK NONE L NO TEST ININSP/MAINT 1 SO27924DL 49711 DURING LAYOVER CHECK FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. FOUND ALL BULBS MISSING FROM ASSEMBLY. RELAMPED, OPS CHECKS NORMAL. 2L72 4F RTA6WE 20040115001662004011500166SO 2004 1 15 RAIA00312310 120031211A32347455501 CONTROL LEVER EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03810HK1738 145231 PIT- LANDING GEAR DISAGREE MESSAGE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER. 2L72 4T RTT00011AT 20040115001712004011500171SO 2004 1 15 RAIA00312313 120031213A30409001827 MOTOR EMB 145 EMB145 3260210SO WINDSHIELD WIPERINOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03827HK9856 STL- CAPTAIN'S WINDSHIELD WIPER INOP. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S WINDSHIELD WIPER MOTOR. 2L72 4F RTT00011AT 20040115001722004011500172NM 2004 1 15 03FDEA02164 120031211A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 STRINGER CLIP CRACKED, STR 6R, BS 950C. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STRINGER 6R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040122000412004012200041NM 2004 1 22 ASAA040122B 120030324A532069434561 STRAP BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01703AS 28893 DURING C-CHECK, FOUND CORROSION ON STRAP AT NUT-PLATE LOCATION AT BS 842-852, RBL 19.5 AND WL 155. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040116000032004011600003EA 2004 1 16 QXEA200301534 120031209A4950WE38007703 APU CNDAIRCL600 CL6002C10 1390015EA ZONE 400 ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09603QX4334 4334 10011 PDX FLIGHT 2482 BURNING OIL ODOR IN AIRPLANE WHILE APU IS SUPPLYING BLEED AIR. DEFERRED APU. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040116000102004011600010WP 2004 1 16 UPS03841649 120031210A2612 FIRE DETECTOR DOUG DC8 DC871F 302199DWP CARGO BAY FALSE INDICATIONA IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01804UP 46004 AFTER ROTATION, LOWER CARGO FIRE LIGHT ILLUMINATED, MX DISPLAY INDICATED FIRE COMP C, AFTER I MINUTE INDICATION CLEARD, TEST PASSED, RETURNED TO PHL FOR CARGO PIT INSPECTION. INSPECTED COMP C, FOUND NO EVIDENCE OF FIRE OR SMOKE. 2L74 4F RT4A25 20040116000112004011600011CE 2004 1 16 DXTA200300180 120031211A3411 PITOT LINE CESSNA750 750 2076810CE AIRSPEED MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07923QS 7500023 ON TAKEOFF ROLL AMBER CAS MESSAGE CAME ON FOR YAW-DAMPER AND FADEC FAILURE. ABORTED TAKEOFF. TROUBLESHOT AND PURGED OUT BOTH PITOT SYSTEMS, RAN AIRSPEED TO BOTH ADC’'S TO COMPARE AIRSPEED AS REQUIRED AFTER PURGING LINES. CARRIED OUT ENGINE RUNS AND NO FAULT FOUND, A/C IS SCHEDULE FOR AN OPERATIONAL CHECK FLIGHT ALL WORK DONE IAW CESSNA 750 MM CHAPTER 34-11-01 & 34-11-08. 2L72 4J RTT00007WI 20040127001582004012700158NM 2004 1 27 ASAA0310237 120030326A5310 BEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AFT PIT DOOR BEAM WEB AT BS 807-827, STRINGER 19R CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040127001592004012700159WP 2004 1 27 ASAA0380680 120031015A5321BAC150910035 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK - DURING 15K CHECK, FLOOR PANEL IS CORRODED AT FS 1155-1174. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-70-3. (M) 2L72 4F RTA6WE 20040127001792004012700179WP 2004 1 27 ASAA0380644 120031015A531359364321 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, STRINGER IS CORRODED IN AFT CARGO BAY AT FS 1136-1146. INSTALLED REPAIR CHANNEL PER SRM 53-02. (M) 2L72 4F A6WE 20040127001882004012700188NM 2004 1 27 ASAA0310195 120030321A532069353501 STRINGER CLIP BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER TIE CLIP AT BODY STATION 520, STRINGER 26R CORRODED. REMOVED AND REPLACED CLIP PER SRM. (M) 2L72 4F RTA16WE 20040127001892004012700189WP 2004 1 27 ASAA0380786 120031119A53135936037501 STRINGER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND STRINGER CORRODED AT FS 1155-1212. REPLACED DAMAGED SECTION PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040127001962004012700196NM 2004 1 27 ASAA0310209 120030325A53126561374 BLOWOUT PANEL BOEING737 737298C 1384490NM BULKHEAD CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO PIT BULKHEAD BLOWOUT PANEL WEB AT BS 360, STRINGER 22L CRACKED 6 INCHES. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040127002052004012700205WP 2004 1 27 ASAA0380601 120031003A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 PDX - DURING PREFLIGHT CHECK, FOUND INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040127002162004012700216NM 2004 1 27 ASAA0390011 120030824A33508100022608 LIGHT BOEING737 737990 NM AFT CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01302AS 30017 SEA - LAST TWO EMERGENCY TRACK LIGHTS ARE INOPERATIVE. CONNECTED TRACK LIGHT WIRING. TRACK LIGHTS OPERATE NORMALLY. (M) 2L74 4F RTA16WE 20040127002192004012700219WP 2004 1 27 ASAA0380596 120030926A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS37312 53022 OAK LINE CEHCK, FOUND OVERWING EMERGENCY EXIT LIGHTS FAILED LUMINOSITY CHECK. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040127002372004012700237WP 2004 1 27 ASAA0380659 120031015A53109955752419 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND L1 DOOR FRAME CRACKED. REPLACED FRAME. (M) 2L72 4F A6WE 20040127002382004012700238WP 2004 1 27 ASAA0380661 120031015A5313391477507 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND LONGERON SPLICE AT 28L STATION 689 IS CRACKED. INSTALLED NEW FITTING IAW SRM. (M) 2L72 4F A6WE 20040128000402004012800040WP 2004 1 28 ABXA030486 120031212A53409923455 FITTING DOUG DC9 DC941 302207NWP LT WHEEL WELL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 FITTING INSIDE OF KEEL AT STA 737 CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040128000462004012800046WP 2004 1 28 ABXA030485 120031212A5415591326213 ATTACH ANGLE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 NR 1 ENGINE UPPER PYLON ATTACH ANGLE WAS CRACKED AT STA 1056 AND HAD 1 SHEARED FASTENER. REPAIRED IAW DC-9 SRM 54-04. 2L72 4F A6WE 20040128000602004012800060NM 2004 1 28 03360420 120031226A3250 CONNECTOR DORNERDO32 DO328300 NM NLG STEERING DIRTY A VTZAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27420FJ 3178 DURING TAXI THE CREW REPORTED AN UNCOMMANDED RIGHT HAND TURN. THE CONNECTOR ON THE NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT WAS FOUND DIRTY AND WAS CLEANED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040128000622004012800062EA 2004 1 28 03361650 120031227A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27650BR 7418 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040128001302004012800130EU 2004 1 28 0302193301 120031228A2450Z285H0121111 CONVERTER AIRBUS330 A330323 3930335EU SEAT 12HJ FAILED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01801NW 00524 ELECTRICAL FUMES IN AREA OF DOOR 2R AND RIGHT HALF IFE SYSTEM FAILED. DEACTIVATED ENTIRE PASSENGER IFE SYSTEM AND FUMES/BURNING SMELL DISSIPATED. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. SEAT 12HJ PED SUPPLY SUSPECTED OF CAUSING FUMES. DEACTIVATED 12HJ PED POWER AND DEFERRED. 2L72 4F RTA46NM 20040129000062004012900006EA 2004 1 29 COMA0360577 120031227A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01956CA19994 7105 THE LEFT LOWER WING PLANK FUEL DRAIN FORWARD SCREW HOLE AT WS 85.5 HAD AN INDICATION WHILE PERFORMING EDDY CURRENT INSPECTION (FUEL BOOST PUMP DRAIN VALVE FORWARD SCREW HOLE). DRILLED THE SCREW HOLE TO .3125 INCH TO REMOVE THE INDICATION. FABRICATED AND INSTALLED A FREEZE PLUG IAW REO 601R-57-21-392. 2L72 4F RTA21EA 20040129000462004012900046EU 2004 1 29 MALA030603 120031220A5320 SILL BAC 146 AVRO146RJ85A1500097EU PAX DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, REAR PAX DOOR SILL HAS CORROSION IN THREE SPOTS. MAINTENANCE REMOVED AND INSTALLED NEW PARTS IAW BAE 146RJ85 SRM 51-43-001, REMOVED AND INSTALLED GIRT BAR MOUNTS IAW BAE RH 85 SRM 51-43-00-1. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000492004012900049EU 2004 1 29 MALA030584 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 5E & 5F FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEATS 5E, 5F IAW MESABA EO A25031 DATED 6/FEB/01. REFER 409 NR 1196437 FOR DETAIL. A/C RELEASE DATE 12/31/03. 2H74 4F RTA49EU 20040129001012004012900101NM 2004 1 29 DHL2003742536 120031205A5312 BULKHEAD BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, BS 1183 BL 36 RT WL 237 FWD SIDE BULKHEAD HAS VERTICAL BEAM IS CRACKED IN RADIUS. STOP DRILLED CRACK & INSTALLED REPAIR KIT 65C34406-13 PO 3348157 PER S/B 727-53-0192 & DRAWING 65C34406. 2L73 4F A3WE 20040129001212004012900121NE 2004 1 29 COMA0470001 220031228A7230 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ENGINE DAMAGED A COMAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO01340CA 10062 965358 FLIGHT 5646 RIGHT ENGINE VIBRATION 1.5 TO 2.1. REPLACED ALL 28 FAN BLADES. 2L72 4F4 FRTA21EA EOOO63EN 20040129001552004012900155NM 2004 1 29 2003UALA00988 120031223A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STRINGER TIES ARE CRACKED AT BS 460 S16L, BS 480 S16L AND BS 500A S15L. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER TIES. 2L72 4F4 FRTA16WE E2GL 20040129001562004012900156NE 2004 1 29 2003UALA00990 220031228A7297 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT ENGINE CONTAMINATED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29552UA 26641 RIGHT ENG PRI CONT AND AUTO THROTTLE EICAS STATUS MESSAGE. AFTER TROUBLESHOOTING THE ENTIRE WIRING SYSTEM, A SMALL WIRE-LIKE FILAMENT WAS FOUND CROSSED BETWEEN TWO PINS INSIDE AN EEC CONNTECTOR. UPON CLEANING THE CONNECTOR AND RE-POSITIONING THE PINS, TESTS WERE OK. EEC REMOVED AND SENT TO THE SHOP FOR TESTING. NO FAILURE RESULTS. 2L72 4F4 FRTA2NM E17NE 20040130000082004013000008NM 2004 1 30 SWAA032839 120031230A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND STRINGER 26L CRACKED AT BS 1020. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040130000102004013000010NM 2004 1 30 SWAA032841 120031230A53206551699 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE 4R CRACKED AT BS 908. REPAIRED STRINGER SPLICE SECTION PER SRM. 2L72 4F RTA16WE 20040203003262004020300326EA 2004 2 3 MASA200300475 120031203A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA T/O CONFIG FALSE INDICATIONA MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW077291Z 7291 ASH PHX, ABORTED TAKEOFF AND RETURNED TO GATE REPORTING AN AILRON CONFIG EICAS MESSAGE. MX PERFORMED A FUNCTIONAL TEST OF THE AILRON SYSTEM ON THE GROUND BUT COULD NOT DUPLICATE THE PROBLEM AND RETURNED THE AIRCRAFT TO SERVICE. NO PARTS USED. 2L72 4F RTA21EA 20040204000532004020400053NM 2004 2 4 AWXA200301267 120031007A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER OF AFT CARGO COMPARTMENT FLOORBEAM AROUND NUT PLATES AT BS 727+5, LBL 3. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOORBEAM BS 727+5, LBL 3; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG. 201. 2L72 4F4 FRTA16WE E2GL 20040204000812004020400081NM 2004 2 4 AWXA200301272 120031007A532065C320747 FLOOR SUPPORT BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT BS 993.5, LBL 33.80. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOOR SUPPORT FROM BS 986.5 TO BS 1006, LBL 33.80; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT IAW DWG 65C32074; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA. 7.D.6. 2L72 4F4 FRTA16WE E2GL 20040204000992004020400099NM 2004 2 4 AWXA200301279 120031009A531565C326778 FLOORBEAM BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 993, LBL 15 TO LBL 20.70. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM AT BS 993, LBL 15 TO LBL 20.70; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM IAW DWG 65C32677; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PARA. 7D2, AND 7D6. 2L72 4F4 FRTA16WE E2GL 20040204001022004020400102NM 2004 2 4 AWXA200301282 120031009A53306545769 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .8750 INCH CRACK WAS FOUND ON FUSELAGE EXTERNAL SKIN AT AFT SIDE OF RADIO ALTIMETER ANTENNA CUTOUT BS 396, BL "0". MAINTENANCE CUTOUT CRACK ON EXTERNAL SKIN AT AFT SIDE OF CUTOUT BS 396, BL "0"; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5331-03293-SS1. 2L72 4F RTA16WE 20040204001092004020400109NM 2004 2 4 QXEA200301306 120031015A5210 SEAL BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA PAX DOOR FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09411QX 4055 ON DESCENT BETWEEN 9,000 FT AND 8,000 FT LOST CABIN PRESSURE, HEARD SWOOSHING SOUND AND SAW RATE NEEDLE PEGGED OUT. AFTER LEVELING AT 8,000 FT PRESSURIZATION RETURNED AND STARTED REPRESSURIZING. UPON DESCENT TO 7,000 FT LOST PRESSURE AGAIN AND LANDED WITHOUT PRESSURIZATION. THERE WERE NO CAUTION OR WARNING LIGHTS ILLUMINATED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SEAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040204001122004020400112NM 2004 2 4 03286430 120031013A2910 WARNING LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE B HYD SYS ILLUMINATED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27430FJ 6250 DURING CRUISE THE CREW REPORTED A HYDRUALIC SYSTEM B PUMP FAIL MESSAGE. CREW DIVERTED TO BOS AND LANDED UNEVENTFULLY, PASSENGERS DEPLANED NORMALLY AT GATE. 2H72 4T4 FRTA55NM E35NE 20040204001142004020400114NM 2004 2 4 F3LA200300152 120031020A5420 SUPPORT BOEING737 737301 1384611NM NR 1 PYLON CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03578US 2672 23257 DURING C-5 CHECK, INSPECTION REPORTED ATTACH ANGLE CRACKED AT LOWER AFT END OF NR 1 PYLON. REPLACED DAMAGED SUPPORT IAW SRM 51-40-02. 2L72 4F RTA16WE 20040204001172004020400117CE 2004 2 4 DXTA200300141 120031017A7830 PROXIMITY SWITCH CESSNA560 560XL 2076702CE THRUST REVERSER OUT OF ADJUST E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07687QS 5605187 RT T/R ARM LIGHT ILLUMINATED IN FLIGHT ACCOMPANIED BY A CONSTANT HYDRAULIC PRESSURE ANNUNCIATOR, FOLLOWED BY INTERMITTENT UNLOCK LIGHT OF LANDING GEAR CAUSING SYSTEM TO RETRACT GEAR. - FOUND RT T/R STOW / DEPLOY SWITCH IN QUADRANT TO BE OUT OF ADJUSTMENT. READJUSTED RT T/R STOW / DEPLOY SWITCH, OPS CHECK GOOD. COULD NOT DUPLICATE LANDING GEAR UNLOCK LIGHT, ALL OPS CHECK GOOD IAW CE560XL M/M CH 78-31-00. 2L72 4F RTA22CE 20040204001212004020400121EU 2004 2 4 MALA030476 120031011A211012506083 MOTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COMPRESSOR FAN FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15425XJ 340B425 DURING PREFLIGHT OF FLIGHT NR 2732, SMOKE IN THE CABIN ON PREFLIGHT. NO PASSENGERS WERE LOADED. MAINTENANCE REMOVED AND REPLACED COMPRESSOR MOTOR FAN PN 1250608-3 AND MOTOR FAN SHROUD PN 1250611 IAW CMM 8.8 OPS CHECK GOOD REMOVED FROM DMR MXC NOTIFIED 8328. 2L72 4T4 TRTA52EU E8NE 20040204001232004020400123EU 2004 2 4 MALA030477 120031020A36109303688100 DUCT SAAB SF340 340B 7860101EU LT BLEED LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15444XJ 340B444 DURING FLIGHT NR 3322, LT BLEED AIR LEAK LIGHT ILLUMINATED,LIGHT EXTINGUISHED AFTER CLOSING BLEED VALVE. AIR RETURN TO MEM. MAINTENANCE FOUND LOOSE CLAMP ON RUBBER DUCT P/N 9303688-100. TIGHTEN CLAMP,RUN ENGINES WITH BLEEDS ON NO FAULT FIND.LEAK CHECK IS GOOD.ALL CHECKS GOOD IAW SF340 CHAPTER 36. 2L72 4T RTA52EU 20040204001282004020400128NM 2004 2 4 EIA2003119 120030930A5312 BULKHEAD BOEING747 747212B 1384886NM MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 LT WING MLG WELL CORROSION ON BS 1241 BULKHEAD AT CANTED BULKHEAD TO 1241 BULKHEAD HORIZONTAL SPLICE LBL 96, APPROX W.L. 171. REPAIRED IAW ECRA 482-57-170-2. 2L74 4F A20WE 20040204001392004020400139NM 2004 2 4 EIA2003123 120031003A5311 FRAME BOEING747 747212B 1384886NM FUEL TANK CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 LT WING GEAR WHEEL WELL STATION 1241, LBL 88 (APPROX), BELOW LOWER CANTED FRAME HAS EXFOLIATED CORROSION ON TANK SKIN. REPAIR IAW ECRA NR 482-57-170-2. 2L74 4F A20WE 20040204001452004020400145NM 2004 2 4 EIA2003129 120031020A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 BS. 340 RT UPPERDECK FLOORBEAM UPPER CHORD TO FRAME INTERFACE CRACKED AT 2ND IB HOLE. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-160-1. 2L74 4F A20WE 20040204001492004020400149NM 2004 2 4 EIA2003136 120031020A5230 STRUCTURE BOEING747 747212B 1384886NM CARGO DOOR DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 AFT CARGO DOOR FWD, LOWER CORNER, REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED EXTERNAL DOUBLER, FABRICATED, ALODINED AND INSTALLED NEW REPAIR DOUBLER IAW ECRA 482-52-031-2 AT AFT CARGO DOOR, FWD LOWER CORNER. 2L74 4F A20WE 20040204001522004020400152NM 2004 2 4 EIA2003135 120031020A5310 STRUCTURE BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 BS 1760 STR 49 RT HAS CORROSION ON STRUCTURE LOWER SURFACE. REPLACED DAMAGED STR FROM BS 1740-1770 IAW B747 SRM 53-10-03 FIG 8. 2L74 4F A20WE 20040204001642004020400164NE 2004 2 4 NACA20030119 220031028A7421 SPARK PLUG PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 3 ENGINE CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL0343872375 375 533294 P32204 NR 3 ENGINE SHUT DOWN DUE TO BACK FIRING AND RUNNING ROUGH. NR 1 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED NR 1, NR 2 AND NR 4 CYLINDERS SPARK PLUGS DUE TO FOULING AND CRACKED CERAMICS. 2L74 4R4 R A781 5E8 20040204001652004020400165EA 2004 2 4 SWIA200312534 120031019A4950 CLAMP CNDAIRCL600 CL6002B19 1900309EA APU FAILED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07465SW 7845 EMERGENCY RETURN TO FIELD AFTER TAKEOFF BECAUSE OF APU FIRE INDICATION. APU FIRE INDICATION REMAINED AFTER APU BOTTLE FIRED. INDICATION WENT OUT WHEN THRUST LEVERS BROUGHT BACK TO ABOUT 60 PERCENT N1. FOUND UPPER CLAMP ON APU LCV FAULTY. REMOVED AND REPLACED UPPER CLAMP ON LCV AS REQUIRED. OPS CHECK GOOD IAW MM 49-51-01. 2L72 4F RTA21EA 20040204001672004020400167WP 2004 2 4 0301979940 120031028A216060714622 CONTROLLER DOUG DC9 DC932 3022066WP AC SYSTEM MALFUNCTIONED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL013322L 47031 DURING CLIMBOUT, A BURNING ODOR AND LIGHT HAZE PERMEATED THE CABIN. THE LT PACK VALVE WAS PEGGED FULL RT AND THE LT DUCT TEMPERATURE REACHED 120 DEGREES. FLIGHT CREW SWITCHED THE LT PACK TO MANUAL CONTROL AND ODOR DISSIPATED. FLIGHT RETURNED TO CMH AND ON DESCENT, THE BURNING ODOR RETURNED WITH LT DUCT TEMPERATURE AT 150 DEGREES. LANDING WAS UNEVENTFUL AND MAINTENANCE REPLACED THE TEMPERATURE CONTROLLER AND BOTH WATER SEPARATORS. ALSO, FOUND A LOOSE DUCT ON THE AFT SIDE OF THE WATER SEPARATOR. ALL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040204001842004020400184EA 2004 2 4 SWIA200312503 120031010A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CRACKED CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 FS 484 RT INTERCOSTAL OB FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV (A) RII 53-401. 2L72 4F4 FRTA21EA E15NE 20040204001872004020400187CE 2004 2 4 110303 120031027A325066082781 COMPUTER LEAR 25 25C 5170513CE STEERING FAILED E ESUAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE0325MT 129 UPON SELECTING THE LANDING GEAR UP THE NOSE GEAR UNSAFE LIGHT WOULD NOT GO OUT. THE LANDING GEAR WAS RECYCLED ONCE AGAIN WITH NO CHANGE IN THE SITUATION. WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION (THREE GREEN LIGHTS) WAS ACHIEVED. THE AIRCRAFT LANDED AND AT THE END OF THE LANDING ROLL AS THE AIRCRAFT WAS EXITING THE RUNWAY ONTO A TAXIWAY AND THE AIRCRAFT TOOK A UNCOMMANDED TURN TO THE RIGHT AT ABOUT 5-10 MPH AND CAME TO A STOP WITH JUST THE NOSE WHEEL OFF THE PAVEMENT. IT WAS FOUND THAT THE (GEAR UNSAFE) LIGHT WAS CAUSED BY A BROKEN NOSE GEAR DOOR ACTUATING ROD. IT WAS FOUND THAT THE STEERING PROBLEM WAS CAUSED BY A FAULTY VARIABLE AUTHORITY STEERING COMPUTER P/N 6608278-1. 2L72 4J A10CE 20040204001882004020400188NE 2004 2 4 0301995646 220031104A7200 ENGINE BOEING757 757251 1384970NM PWA 2037 PW2037 NE NR 1 FLAMED OUT A NWAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL01546US 26493 728799 DURING CRUISE FLIGHT, THE NR 1 ENGINE FLAMED OUT. FLIGHT RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL CONTROL, FUEL PUMP, AND EEC. MAINTENANCE ALSO INSPECTED THE EEC ALTERNATOR AND PMA STATOR. NO TROUBLE FOUND. 2L72 4F4 FRTA2NM E17NE 20040204001892004020400189CE 2004 2 4 DXTA200300155 120031105A3230 STRUT CESSNA560 560XL 2076702CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07652QS 5605152 GEAR UNLOCK INDICATOR REMAINED ON AFTER GEAR RETRACTION. TROUBLESHOT TO NOSE GEAR NOT GETTING ON THE UPLOCK STRUT WAS NOT FULLY EXTENDED. PERFORMED A COMPLETE SERVICING OF STRUT IT IS NOW FULLY EXTENDED AND THE GEAR OPERATIONAL CHECK WAS GOOD. ALL WORK PERFORMED IAW MFG 560XL M/M CHAPTER 12-10-00. 2L72 4F4 FRTA22CE E00059EN 20040210000122004021000012WP 2004 2 10 UPS03841583 120031114A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 1700 LONGERON 11L IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 1690-1700, FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE IAW SRM. 53-2-2 FIG. 10. 2L74 4F RT4A25 20040210000252004021000025WP 2004 2 10 UPS03841599 120031116A5315577263885 FLOORBEAM DOUG DC8 DC871F 302199DWP AFT CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1 STATION 1766 FWD SIDE OF AFT PRESSURE BULKHEAD FLOORBEAM ANGLE IS CORRODED BEYOND LIMITS BL 0 TO RBL26. REMOVED,FABRICATED AND REPLACED ANGLE IAW DWG. 5772638 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040210000292004021000029WP 2004 2 10 UPS03841605 120031107A5347S475539524000N SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, CORROSION ON SEAT TRACK FS 570, LBL46. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 5 3-2-3. INSTALLED NEW SEAT TRACK S4755395 AND 4 FITTING SEAT TRACK SUPPORT AND 2 SPLICES IAW UPS EO DC8-5320-8309-D AND DC8-5320-5167-C. 2L74 4F RT4A25 20040210000312004021000031WP 2004 2 10 UPS03841607 120031015A5210 SKIN DOUG DC8 DC873F 302199FWP PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, L2 AFT PAX DOOR LOWER AFT CORNER HAS SEVERAL AREAS OF CRACK INDICATION ON EXTERNAL SKIN AREAS MARKED CRACK AND BULGING SKIN NOTED IAW DC8 SID NDT MAN 53-10-12 PSE 53.08.04 1. CUT OUT CRACKED 2 EA AREAS; PERFORMED HFEC, NO CRACKS AFTER CUT OUT; FAB DBLR, TRIPLER, AND FILLERS; ALODINED, PRIMED AND INSTALLED DOUBLER, TRPLR, AND FILLERS; ALL IAW DC8 SRM 53-2-0, TR 53-134,53-185, NDT SRM 06-10- 01.001, DC8 SRM 51-1-8, REO G09548. 2L74 4F RT4A25 20040210001192004021000119WP 2004 2 10 ASAA0380756 120031118A532199365521 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FLOORBOARD DELAMINATED. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M) 2L72 4F RTA6WE 20040211000142004021100014NM 2004 2 11 USAA030318 120031211A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US52098 22958 PIT - FOUND SKIN WRINKLE CRACK 2.5 INCHES LONG, STATION 747 STRINGER 22R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 PG 205, FIG 202. (M) 2L72 4F RTA16WE 20040212000362004021200036CE 2004 2 12 120803 120031207A276066082413 COMPUTER LEAR 35 35A 5170602CE SPOILER MALFUNCTIONED E ESUAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CE03298NE 298 UPON DEPARTURE THE PILOT EXPERIENCED A UNCOMMANDED ROLL. IT WAS FOUND THAT ONE SPOILER HAD DEPLOYED. THE CREW WENT THROUGH THE CHECKLIST AND MADE A NO FLAP LANDING. 2L72 4F A10CE 20040212000412004021200041NM 2004 2 12 COOSDR030160 120031201A5311 FRAME BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23395AJ 21100 RT MAIN GEAR WHEEL WELL, STA 940 WL 201, FORGING FRAME, VERTICAL FLANGE, NBOARD SURFACES CORRODED. 2L73 4F4 FRTA3WE E2EA 20040212000422004021200042NM 2004 2 12 COOSDR030159 120031201A5311 FRAME BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23395AJ 21100 RT MAIN GEAR WHEEL WELL, STA 950 WL 201, FORGING FRAME, HORIZONTAL FLANGE, LOWER SURFACES CORRODED. 2L73 4F4 FRTA3WE E2EA 20040212000452004021200045CE 2004 2 12 DJFA20030006 120031208A243523080005 STARTER GEN RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP NR 2 ENGINE FAILED E DJFAE ENGINE SHUTDOWN E VIBRATION/BUFFET DEDESCENT 1 EA23843CW611 611 258543 P107137 AIRCRAFT DESCENDING THROUGH 11,000 FT, VIBRATION WAS NOTED. ENGINE NR 2 WAS SHUT DOWN AND VIBRATION WENT AWAY. AIRCRAFT LANDED AND IT WAS FOUND THAT THE STARTER GENERATOR BEARINGS HAD FAILED. 2L72 4F4 FRTA3EU E6WE 20040212000502004021200050CE 2004 2 12 HYI2003F00022 120030930A3310RC206F151K RHEOSTAT CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO COCKPIT LIGHTS UNSERVICEABLE E HYIAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NE012714M 402C0211 AFTER REACHING CRUISE ALTITUDE, CREW NOTICED SMOKE FROM PEDESTAL LIGHTING RHEOSTATS. DAY/NIGHT SWITCH TURNED OFF, CIRCUIT BREAKERS PULLED, SMOKE STOPPED. DIVERTED TO MECHANIC BASE. MECHANIC REMOVED AND REPLACED DIMMER ASSY AND RETURNED AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20040212000522004021200052EU 2004 2 12 UO22003F00012 120031202A2720 INDICATOR AMD FALCONFALCON20 2730103EU GARRTTTFE731TFE731* 01518WP RUDDER TRIM MISREPAIRED B UO2RK NONE W INADEQUATE Q C ININSP/MAINT 1 GL19470G 470 ORDERED AND RECEIVED A REPAIRED CONDITION PART. ITS RUDDER TRIM INDICATOR INDICATED OPPOSITE OF RUDDER TRAVEL DIRECTION. THE INDICATOR WAS CHECKED AND FOUND TO FAIL CMM 27-09-02 TESTS, WHICH WERE LISTED ON THE ATTACHED 8130-3. RETURNED PART TO VENDOR TO BE EXCHANGED. 2L72 4F4 FRTA7EU E6WE 20040212000612004021200061CE 2004 2 12 GLBA20030514 120031205A3397 WIRE BEECH 1900 1900D 1154162CE TAXI LIGHT CHAFED A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03253GL UE253 WHEN TURNING ON TAXI LIGHT THERE WAS SPARK AND SMOKE, REPAIRED CHAFED WIRE REF 33-40-00. OPS CK GOOD. 2L72 4T RTA24CE 20040212000762004021200076NM 2004 2 12 DHL2003782014 120031209A5230 CONTROL ROD BOEING727 727227 1384078NM DOOR HANDLE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LWR PIT DOOR HANDLE CONTROL ROD HAS SURFACE CORROSION. REMOVED CORROSION, TREATED, AND PRIMED IAW B727 SRM 51-10-2. 2L73 4F A3WE 20040212000902004021200090SW 2004 2 12 JIKA200300003 120031209A53112722093137 FRAME SWRNGNSA227 SA227AC 8780603SW ZONE 100 CRACKED E JIKAK NONE O OTHER ININSP/MAINT 1 WP01421MA25031 AC634 CRACKS FOUND ON LT AND RT SIDES OF FUSELAGE FRAME, P/N 27-22104-046, DURING LETTER CHECK E AT FS 392.271. 2L72 4T RTA8SW 20040212001032004021200103NM 2004 2 12 CALA0300709 120031211A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714341 23579 INSPECTION FOUND A 12 INCH CRACK IN RT PRESSURE DECK AT STA 670, RBL 43, WL 200. THE PRESSURE DECK WAS REPAIRED IAW ECRA 5312-01031 AND SRM 53-60-51. 2L72 4F RTA16WE 20040212001042004021200104NM 2004 2 12 F3LA200300174 120031210A5320 WEB BOEING737 73736E 138443ANM FUSELAGE BROKEN A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED WEB BEHIND MOP SILL AT STA. 294.5, RBL 56, BROKEN. INSTALLED REPAIR PARTS FOR TYPICAL WEB REPAIR IAW SRM 51-70-13, PAGE 3, FIG. 1, SHEET 3 AND NEW ANEL PER SRM 51-40-02. 2L72 4F RTA16WE 20031029000522003102900052NM 2003 10 29 ASAA0310432 120030512A5320655965819 ANGLE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND ANGLES AT BODY STATION 947, STRINGER 45L CORRODED. REPLACED TWO ANGLES PER SRM. (M) 2L72 4F A16WE 20031029000532003102900053NE 2003 10 29 ASAA0380478 220030519A7250 BLADE DOUG MD80 MD83 3023681NM PWA JT8 JT8D217C 52053NE TURBINE ASSY FAILED A C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 NM01981AS 53472 P725848D ON TAKEOFF ROLL FROM MZT, NR 2 ENGINE VIBRATION OCCURRED ABORTED TAKEOFF AND RETURNED TO THE GATE SUBSEQUENT ENGINE CHANGE INITIATED. A LOUD BANG AND VIBRATION FROM RIGHT ENGINE OCCURRED ON TAKEOFF ROLL AT 80 KNOTS. ABORTED TAKEOFF. REPLACED ENGINE. SUBSEQUENT SHOP INVESTIGATION REVEALED TURBINE FAILURE. PRELIMINARY INDICATIONS ARE THAT A SINGEL T-4 BLADE FAILED (SEPARATED), PRECIPITATING THE FAILURE OF ALL OTHER T-4 BLADES AND THE T-4 VANES. DAMAGE ALSO PROPAGATED FORWARD TO THE T-3 BLADES AND VANES. A FAIURE ANALYSIS IS BEING CONDUCTED TO DETERMINE THE EXACT MODE OF FAILURE OF THE SINGLE T-4 BLADE. (M) 2L72 4F4 FRT E9NE 20031029001022003102900102EU 2003 10 29 MALA030436 120030927A242051634002 GCU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE AC SYSTEM INOPERATIVE A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15427XJ 340B427 AFTER TAKEOFF ON FLIGHT NR 3286, LT AC GEN FAILED, AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED LT AC/GCU ALL CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20031029001162003102900116SO 2003 10 29 C2XA03SH362 120030930A531014522226003 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE LT BUTTSTRAP IN THE CARGO COMPARTMENT AT FR 65-68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031029001192003102900119EU 2003 10 29 KBM2003F00014 120030810A2497DHS77516040 SWITCH SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE BATTERY STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 BATTERY SWITCH STUCK. REMOVED AND REPLACED WITH NEW SWITCH.(K) 1G71 3U3 UNCH9EU E19EU 20031029001252003102900125EU 2003 10 29 KBM2003F00020 120030711A2842647510033 PROBE SNIAS 350 AS350BA 8680817EU FUEL SYSTEM STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 FUEL GAUGE IS STICKING. REPLACED WITH SERVICEABLE GAUGE.(K) 1G71 3U NCH9EU 20031029001282003102900128EU 2003 10 29 KBM2003F00023 120030726A6720350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 LAMINATE BEARINGS HAVE MULTIPLE CUTS. REPLACED WITH NEW LAMINATE BEARING KIT.(K) 1G71 3U3 UNCH9EU E19EU 20031030000012003103000001EU 2003 10 30 KBM2003F00031 120030905A6321 SHOE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 NO COLLECTIVE FRICTION. REPLACED WITH NEW FRICTION SKID SHOES PN 350A27-136820, COVER PN 350A27-1344-00, FRICTION HANDLE 350A27-00-1221. 1G71 3U3 UNCH9EU E19EU 20031030000092003103000009NE 2003 10 30 NACA20030113 220030930A732239138418 CARBURETOR DOUG DC6 C118A 3021710WP PWA R2800 R2800CB3 52026NE ENGINE FIRE A NACAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 AL031377K56 56 44596 P34459 NR 2 ENGINE INDUCTION FIRE DURING START-UP. CO2 BOTTLES DISCHARGED. INSPECTED NR 2 ENGINE AND MOUNT FOR INTEGRITY, NO DAMAGE FOUND. REPLACED NR 2 ENGINE CARBURETOR. 2L74 4R4 R 6A3 5E8 20031030000132003103000013NE 2003 10 30 QEM2003F00001 220030911A7250 TURBINE BLADES BOEING747 747400 NM RROYCERB211 RB211524* NE ENGINE DAMAGED B QEMYO OTHER O OTHER NRNOT REPORTED 1 EA35 GCIVH 13383 DURING ENGINE DISASSEMBLY, AND FOLLOWING REMOVAL OF THE 02 MODULE SPLITTER FAIRING, QTY 43 BOLTS OUT OF 90 WERE FOUND TO BE MISSING/FAILED ON THE 02/07 FLANGE. REMOVAL OF THE 02 MODULE REVEALED DAMAGE TO THE STAGE 6 AND 7 ROTOR PATHS. IN ADDITION, CRACKING OF THE IPC CASES WAS NOTED IN LINE WITH THE STAGE 4 AND 5 ROTOR BLADES. MOD DISASSEMBLY REVEALED HEAVY CONTACT BETWEENT THE BLADES AND THE CASES. DURING DETAIL INSP THE STAGE 4 IPC DISC WAS SEEN TO EXHIBIT HEAVY CRACKING TO 7 OF DOVETAIL POSTS. PN UL27090 SN STDC17571 TSN 19975/4529. THE DISC WILL BE RETURNED TO MFG FOR INVESTIGATION. PROBABLE CAUSE WAS APPARENT LOSS OF LOCATION OF THE IPC CASES.(K) 2L74 4F4 FRTA20WE E12EU 20031030000182003103000018NM 2003 10 30 UPS03441276 120030906A5740 RIB BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 6 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C LHW - NR 6 V/C FLAP OB UNKAGE IB RIB NR 4 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION ( COUNT FROM IB CLOCKWISE ). NR4 MOUNTING HOLE REPAIRED IAW RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F4 F A20WE E20EA 20031030000312003103000031NM 2003 10 30 UPS03441289 120030905A5712 RIB BOEING747 747121 1384871NM NR 10 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 10 V/C FLAP I/B LINKAGE O/B RIB NR 4, NR 5 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). BOLT HOLE NR 4, NR 5 AND NR 7 REPAIRED AS PER RS 574135066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000322003103000032NM 2003 10 30 UPS03441290 120030905A5712 RIB BOEING747 747121 1384871NM NR 10 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING - NR 10 V/C FLAP I/B LINKAGE I/B RIB NR 1 TO NR 5 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 5 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000342003103000034NM 2003 10 30 UPS03441292 120030905A5712 RIB BOEING747 747121 1384871NM NR 9 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 9 V/C FLAP I/B UNKAGE O/B RIB NR 2, NR 3 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2, NR 3 AND NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000422003103000042NM 2003 10 30 UPS03441300 120030905A5712 RIB BOEING747 747121 1384871NM NR 2 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 2 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000452003103000045NM 2003 10 30 UPS03441303 120030905A571265B078315 RIB BOEING747 747121 1384871NM NR 5 V/C FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 5 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 5 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS NR R57-41-35067 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000542003103000054NM 2003 10 30 UPS03441317 120030827A7830 SKIN BOEING747 747121 1384871NM THURST REVERSER DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, DMI : D252292 - NR 4 ENG FAN THRUST REVERSER I/B SLEEVE DENTED, LOCATED 12 INCHES OF SEAM 6 O'CLOCK POS AND 11 INCHES FROM FWD EDGE 3 INCHES FROM AFT EDGE 4 W X 4 L X 0.032 D (REF EO B747-7830-18117). REPAIRED AS PER RS NR R-78-30-35071 AND AS PER EO B747-7830-19255-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20030917001222003091700122CE 2003 9 17 2003F00519 120030801A2150 FLANGE CESSNA500 550 2076604CE A/C PACK CRACKED E FUBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23792MA 5500302 THE PROBLEM STARTED WITH THE FREON AIR CONDITIONER CYCLING IN FLIGHT. AT THE SAME TIME THE LEFT PRE-COOL LITE ILLUMINATED MOMENTARLY UPON TAKE OFF. INVESTAGATION REVEALED A CRACK IN THE LEFT FLOW PACK OUTBOARD SIDE FLANGE. HEAT FROM THE CRACK VENTED IN THE TAILCONE CAUSING THE HIGH PRESS SWITCH ON THE FREON AIR CONDITIONER TO CYCLE ON AND OFF. CORRECTIVE ACTION-REMOVED AND INSTALLED OVERHAULED LEFT FLOW PACK. OPS CHECK GOOD. 1L72 4F A22CE 20030917001302003091700130 2003 9 17 DL757030689 420030723A2565 SLIDE BOEING757 757232 1384965NM INOPERATIVE A DALAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO27620DL 191 22910 2L SLIDE DEPLOYED BY MAINT. SLIDE REPLACEMENT IN PROGRESS. 2L72 4F RTA2NM 20030917001392003091700139NM 2003 9 17 DL757030703 120030729A3244B757N TIRE BOEING757 757232 1384965NM NLG DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO27643DL 23997 LT NOSE TIRE HAS FOD DAMAGE - REPLACED SAME 2L72 4F RTA2NM 20030918000252003091800025WP 2003 9 18 GTIA030419 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 8015 FOUND CABIN FLOOR SUPPORT CORRODED FS 1309-1338 RBL 17 INCHES. REMOVED DAMAGED SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030918000282003091800028NM 2003 9 18 GAIA03031SP 120030719A5311 FRAME BOEING727 727* NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS A DENT AND CRACK BETWEEN STRINGERS 7R AND 8R FASI N/R 35751. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR FROM 7075-T6 .050, PO NR 9911488 DIM 11 INCH BY 5.5 INCH. INSTALLED REPAIR IAW B727 SRM 51-30-2 AND 53-10-4. (M) 2L73 4F RTA3WE 20030918000312003091800031NM 2003 9 18 GAIA03037SP 120030719A5315 SPLICE BOEING727 727* NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CARGO DECK BS 600, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS FASI N/R 35931. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE 179850 DTD 4-7-93. (M) 2L73 4F RTA3WE 20030918000352003091800035NM 2003 9 18 GAIA03029SP 120030719A53117075T6 FRAME BOEING727 727* NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 520 HAS A DENT INTO THE RADIUS AT STRINGER 16R FASN/R 35745. CUT OUT DAMAGED AREA, FABRICATED FILLER FROM MATERIAL 7075-T6 .050 PO NR 991420, DIM 2.5 INCH BY 3 INCH, DOUBLER FROM MATERIAL 7075-T6 .063, PO NR 9912495 DIM 7 INCH BY 5.5 INCH INSTALLED IAW SRM 51-10-2. (M) 2L73 4F RTA3WE 20030918000432003091800043NM 2003 9 18 2003F00569 120030423A5313 STRINGER BOEING737 7372L9 1384497NM E/E BAY CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO27464AT 21278 DURING C-CHECK INSPECTION, FOUND CORROSION WAS FOUND AT STRINGER 24L BETWEEN BS 330.7 AND BS 334 IN THE E/E COMPARTMENT. THE DAMAGE WAS REPAIRED ON NON-ROUTINE 031078 IAW WITH SRM 53-10-3 FIGURE 1. TOTAL AIRCRAFT TIME 46985.2, TOTAL CYCLES 41351. (M) 2L72 4F RTA16WE 20031117000342003111700034NM 2003 11 17 QXEA200301216 120031006A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX- MOST FORWARD EMERGENCY TRACK LIGHT RIGHT SIDE CARPET COVER STRIP IS BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY TRACK LIGHT. 2H72 4T RTA13NM 20031117000422003111700042EU 2003 11 17 2003UALA00734 120030930A5520 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ELEVATOR CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29401UA 435 8 AREAS OF WATER INGRESS WERE FOUND ON THE RT ELEVATOR. UPPER SURFACE - 5 EACH AREAS 2 BY 2 INCHES, ALL 3.5 INCHES FWD OF THE TE, AND 132, 153.5, 1 61,168.8, 175 INCHES FROM IB EDGE. 3 EACH AREAS 2 BY 2 INCHES ON THE LWR SURFACE, ALL 3.5 INCHES FROM TE AND 153.5, 160.8, AND168 INCHES FROM IB END. REPAIRED DAMAGED AREAS IAW SRM 55-21-11 TO ELIMINATE WATER INGRESSION. 2L72 4F4 FRTA28NM E40NE 20031117000452003111700045NM 2003 11 17 2003UALA00738 120031003A5230 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 BULK PIT DOOR EXTERNAL SKIN DENTED AT 2 PLACES. MAJOR REPAIR. REPAIRED WITH EXTERNAL DOUBLER. 2L72 4F4 FRTT0001SE E46NE 20031117000652003111700065NM 2003 11 17 DHL2003749506 120030919A5730 SKIN BOEING727 7272J0 138407ENM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK, WS 464 UPPER LT WING L/E SURF IS CRACKED AT RIVET. REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 2.375 X 1.25 INCH AND FABBED DOUBLERS FROM 2024 T3 .050 INCH PO 90096 DIM 7.25 X 6 X 7.25 X 4.5 INCH AND FILLER FROM 2024 T3 .040 PO 90024 DIM 2.375 X 1.25 INCH IAW B-727 SRM 57-30-4 FIG 4 SHEET 6 REPAIR III. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 57-30-4 FIG 4. 2L73 4F RTA3WE 20031117000662003111700066EA 2003 11 17 QXEA200301220 120031006A7830 VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 400 MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09601QX 10009 ON FLIGHT 2467 AFTER SETTING TAKEOFF THRUST AND AT 65 KIAS, RECEIVED LT THRUST REVERSER UNSAFE CAUTION LIGHT. ABORTED TAKE OFF. REMOVED AND REPLACED LEFT HAND ICV. OPERATIONAL CHECKS GOOD AND AIRCRAFT WAS RETURN TO SERVICE. 2L72 4F RTA21EA 20031117000672003111700067NM 2003 11 17 QXEA200301221 120031004A2610 VALVE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 WILL NOT TEST A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09413QX 4060 ON FLIGHT 2336 AFT BAGGAGE FIRE PROTECTION VALVE OUTLET WILL NOT TEST. LIGHT BULB CHECKS GOOD. PERFORMED OPS TEST IAW Q400 MM 26-22-00-720-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031117000722003111700072NE 2003 11 17 ALG2003F00085 120030901A32977655200110109 WIRE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL RT MLG DAMAGED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03741SW 760070 CAE890236S AFTER TAKE OFF, WHILE RETRACTING GEAR THE RED GEAR UNLOCK LIGHT STAYED ILLUMINATED. RECYCLED GEAR SEVERAL TIMES WITH THE SAME RESULT. RETURNED TO FOURCHON WHERE MAINTENANCE TROUBLESHOT THE LANDING GEAR, REMOVED AND REPLACED CABLE ASSY PN 76552-00110-109 IAW MM. GROUND CHECKED, OK. 1G72 3U3 U H1NE E1GL 20031030000632003103000063WP 2003 10 30 UPS03841307 120030922A5321561229855 FINGER DOUBLER DOUG DC8 DC873F 302199FWP COCKPIT SUBFLOORCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 RT SIDE COCKPIT SUBFLOOR STA 100 NEXT TO FUSELAGE ON FLOOR FINGER DOUBLER CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5612298 AND SRM 51-1-20D. 2L74 4F RT4A25 20031030000652003103000065WP 2003 10 30 UPS03841309 120030922A5311 FRAME DOUG DC8 DC873F 302199FWP AFT CABIN WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STATION 1723 CANTED FRAME AT LONG 21L HAS A HOLE WORN THRU FRAME. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 -5310-11728-A APPROX A. 2L74 4F RT4A25 20031030000662003103000066WP 2003 10 30 UPS03841310 120030929A33506012235 BATTERY PACK DOUG DC8 DC873F 302199FWP FLIGHT DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01803UP 46073 EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK, OPS CHECK NORMAL. 2L74 4F RT4A25 20031030000882003103000088SO 2003 10 30 C2XA03SH365 120031002A532014522459003 ANGLE EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 SHV- DURING C-CHECK THE RAMP ANGLE AT FR 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031030001022003103000102EU 2003 10 30 2003F00592 120030924A21609738132212 SWITCH PILATSPC12 PC1245 7090551EU DUCT TEMP FAILED E I CABIN DEPRESSURIZATION B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP07613NA 197 TEMP CONTROL SYSTEM SENT SIGNAL TO TEMP CONTROL VALVE TO GO FULL HOT. DUCT TEMP SWITCH FAILED TO ILLUMINATE ECS LIGHT AND SHUT DOWN SYSTEM. CHANGED DUCT TEMP SWITCH AND TEMP CONTROLLER, SYSTEM OPS GOOD. 1L71 3T RTA78EU 20031030001042003103000104NM 2003 10 30 03FDEA01538 120030908A5740NRC6066 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OUTBOARD FLAP VANE NR 2 FITTING FROM INBOARD FOUND FORWARD HOLE CORRODED. LT OUTBOARD FLAP VANE NR 2 FITTING FROM INBOARD FOUND FORWARD HOLE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-72700, TITLE - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP NR 2 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20031030001062003103000106NM 2003 10 30 03FDEA01541 120030910A5740NRC6066 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OUTBOARD FLAP VANE NR 4 FITTING (FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE. RT OUTBOARD FLAP VANE NR 4 FITTING (FROM INBOARD) ON FORWARD HOLE BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-72701, TITLE - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP. NR 2 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20031030001172003103000117NM 2003 10 30 03FDEA01626 120030924A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 BS 950F FRAME DAMAGED BETWEEN STR 25L AND 27L. *S/D* DAMAGE ON FRAME AT BS 950F BETWEEN 25L & 27L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 950F FRAME BETWEEN STR 25L AND 27L IAW SRM 51-40-3. 2L73 4F RTA3WE 20031031000172003103100017EA 2003 10 31 SWIA200312470 120030930A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS OUT OF RIG A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07441SW 7602 FLAP CAUTION MESSAGE ENROUTE. RIGGED LEFT AND RIGHT BPSU IAW MM 27-51-10. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20031031000242003103100024SO 2003 10 31 C2XA03SH367 120031003A531014522460013 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE RT CENTER BUTT STRAP FROM FR 20 TO FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 53-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031028000392003102800039EA 2003 10 28 SWIA200312452 120030903A5340 PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07916SW 7634 FS 589.0; LBL 38; FLOOR LANDING PLATE HAS A CRACK EXTENDING FROM RIVET. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-433 REV NC. 2L72 4F RTA21EA 20031028000602003102800060SO 2003 10 28 C2XA03SH355 120030930A531014522460015 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031029000482003102900048NM 2003 10 29 ASAA0310400 120030506A5320 FLOOR SUPPORT BOEING737 737290C 138448VNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 663.73, LEFT BUTTOCK OINE 24.5 CORRODED. REMOVED DAMAGED FLOOR SUPPORT AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031029000982003102900098EU 2003 10 29 KBM2003F00013 120030710A21210400048 BLOWER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE AIR CONDITIONER STOPPED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH2390 2884 A/C STOPPED BLOWING COLD AIR. REMOVED SQUIRREL CAGE AND REPLACED WITH SERVICEABLE UNIT.(K) 1G71 3U3 U H9EU E19EU 20031029001182003102900118NM 2003 10 29 PCAA0309118 120030930A33501013073 LIGHT DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE SEAT 2DF DAMAGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13845EX 344 DURING ROUTINE MAINTENANCE VISIT AN EMERGENCY FLOOR LIGHT WAS FOUND TO BE OUT AT SEAT 2DF. A NEW LIGHT ASSEMBLY WAS RESPLICED INTO WIRING USING ENVIROMENTAL SPLICES. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031117000902003111700090NE 2003 11 17 ALG2003F00095 120030905A6340 CHIP DETECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL GEARBOX CONTAMINATED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03717AL 760221 CAE890773S ON CLIMB OUT, ON MISSED APPROACH OFF ILS LAKE CHARLES, NR 2 ENGINE CHIP LIGHT ILLUMINATED, THE PILOT FOLLOWED EMERGENCY PORCEDURE CHECKLIST AND THE LANDING WAS UNEVENTFUL AND NOTIFIED MAINTENANCE. THE MECHANIC REMOVED THE NR 2 ENGINE LOWER FORWARD GEARBOX CHIP DETECTOR, HE CLEANED THE FUZZ, REINSTALLED THE CHIP DETECTOR AND C/W 30 MINUTE PENALTY RUN IAW MM AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20031118000062003111800006NM 2003 11 18 UPS03241350 120031006A3350 LIGHT BOEING727 72730C 1384009NM EVAC SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 EVACUATION SLIDE ILLUMINATION LIGHT IS INOPERATIVE. REF TO WDM 33-50-02, EVACUATION SLIDE ILLUMINATION LIGHT IS ONLY A PROVISION. 2L73 4F A3WE 20031118000222003111800022EU 2003 11 18 AWXA200301137 120031005A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 5 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 5 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040106001982004010600198WP 2004 1 6 GTIA030982 120031114A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN STATION 905-927 STRINGER 17L DAMAGED WEB AND FASTENERS INSTALLED INCORRECTLY. FABRICATED NEW WEB. INSTALLED WEB. (M) 2L72 4F A6WE 20040106002052004010600205WP 2004 1 6 GTIA030990 120031123A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND CABIN FLOOR PANEL LEFT STATION 180-200 DELAMINATED AND EDGE DAMAGE. FABRICATED NEW CABIN FLOOR PANEL. (M) 2L72 4F RTA6WE 20040106002142004010600214NM 2004 1 6 SWAA032687 120031209A53206559664 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 CYXX - DURING SPECIAL VISIT CRACKED STRINGER SPLICE AT BS 360 STRINGER 4L, 4R AND 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. (M) 2L72 4F RTA16WE 20040106002242004010600224WP 2004 1 6 GTIA031033 120031124A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND COCKPIT RUDDER PEDAL FLOOR PANEL CRACKED. REPAIRED COCKPIT RUDDER PEDAL FLOOR PANEL. (M) 2L72 4F RTA6WE 20040106002262004010600226WP 2004 1 6 GTIA030975 120031115A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 180 8 INCHES -43 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20040108000662004010800066CE 2004 1 8 ACE0918021 120030918A2820 DIAPHRAGM BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE FUEL PUMP PERFORATED E YADAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AL031563C 2973 B774019 UC20 ON PREFLIGHT INSPECTION, PILOT NOTICED FUEL LEAKING FROM THE ENGINE GANG DRAIN. MAINTENANCE REPLACED THE LOW PSI FUEL PUMP DUE TO FUEL DRAINING FROM THE DRY SIDE OF THE PRESSURE RELIEF VALVE ASSEMBLY. DISASSEMBLY OF THE PUMP REVEALED MULTIPLE HOLES IN THE DIAPHRAGM IN THE AREA AROUND THE RELIEF VALVE CONTROL SPRING SEAT. 2L72 4T4 TRTA24CE E4EA 20040108000672004010800067SO 2004 1 8 IPM2003F00000 220031008A7314 RELIEF VALVE BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO FUEL PUMP FAILED D IPMEO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 WP112367P 3314RA TC2367 ENGINE WOULD LOOSE POWER INTERMITTENTLY AND DURING CLIMB AFTER TAKEOFF. DETERMINED TO BE DEFECTIVE RELIEF VALVE AND SEAT IN ENGINE FUEL PUMP. (WP11200400873) 1L72 3O3 ORT3A16 3E1 20040108001072004010800107NE 2004 1 8 KBM2003F00057 220031012A75329550161210 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV497 3296 BLEED VALVE WILL NOT CLOSE IN FLIGHT. BLEED VALVE DEFECTIVE. INSTALLED OVERHAULED BLEED VALVE. 1G71 3U3 U H9EU E19EU 20040108001252004010800125CE 2004 1 8 KZ52003F00002 120031013A5320504400287877 STIFFENER BEECH 65 65 1152802CE LYC O720 IO720* 41546EA AFT BULKHEAD CRACKED B KZ5RO OTHER O OTHER NRNOT REPORTED 1 GL155078N11858 LF16 INSPECTION REVELAED THE PARTS TO BE CRACKED BETWEEN RIVET HOLES WHERE STIFFENER WAS ATTACHED TO AFT BULKHEAD. NO FURTHER DAMAGE WAS NOTED AFTER PART WAS REMOVED. 1L72 3O3 O 3A20 1E15 20040108001582004010800158NE 2004 1 8 Z1R2003F00008 120031028A1430SS5305L4G08 SCREW SKRSKYS76 S76C 8143008NE BLADE TIP CAP CRACKED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF 760523 MAIN ROTOR TIP CAP SCREWS/ MAIN ROTOR BLADE. HAD ONE (1) SCREW CRACKED, NR 1 UPPER POSITION LEADING EDGE. REPLACED AT 292.2 A/C HOURS. HAD ONE (1) SCREW CRACKED NR 1 BOTTION POSITION LEADING EDGE. 1G72 3U NCH1NE 20040109000032004010900003NE 2004 1 9 ALG2003F00104 120031014A29137665009808102 PUMP SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 2 FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03709AL612 760278 AIRCRAFT RUNNING ON THE PLATFORM. THE NR 2 HYDRAULIC FAILED WHILE THE AIRCRAFT WAS ON THE PLATFORM, MAINTENANCE WAS NOTIFIED. THE MECHANIC REMOVED AND REPLACED THE NR 2 HYDRAULIC PUMP DUE TO A SHEERED SHAFT, GROUND RUN WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.(K) 1G72 3U3 U H1NE E1GL 20040109000132004010900013CE 2004 1 9 MK92003F00000 120031102A272012604563 BAR CESSNA206 U206 2073306CE CONT O520 IO520* 17032SO RUDDER BROKEN E MK9AO OTHER O OTHER NRNOT REPORTED 1 WP135286U9391 U2060286 FLANGE ON RUDDER BAR BROKEN. LT SIDE, LT BRAKE PEDAL ATTACHMENT. PILOT WAS LANDING AIRCRAFT WHEN IT BROKEN. LANDED AND TAXIED SAFETLY. CLOSE INSPECTION OF ALL FLANGES AND SPRAYING PENTRATING OIL DOWN RUDDER PEDAL BAR WOULD HELP PREVENT INTERIOR CORROSION WHICH CAUSED THIS PROBLEM.(K) 1H71 3O3 O A4CE E5CE 20040109000172004010900017SW 2004 1 9 AKG2003F00002 120031030A2742740018003007 ACTUATOR MOONEYM20 M20K 5870220SW CONT O360 TSIO360* 17025SO STAB TRIM WORN B AKGRO OTHER O OTHER NRNOT REPORTED 1 CE055254G3328 251180 THE THREADS IN THE ACTUATOR NUT ARE WORN AND ALLOWING THE NUT TO MOVE ON THE JACK SCREW AND BECOME JAMMED WHEN IT CONTACTS THE STOP ON EITHER END OF TRAVEL NOSE UP OR NOSE DOWN. PART LOCATION IS BETWEEN THE PILOT AND COPILOT SEATS UNDER THE FLOOR PANEL. 1L71 3O3 O 2A3 E9CE 20040109000452004010900045NM 2004 1 9 TSAA0255265 120030905A55006554821 SKIN BOEING737 737282 13844ATNM EMPENNANGE DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13824AL 23045 CUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040112000652004011200065NM 2004 1 12 TSAA0253258 120031218A531065458181 WINDOW FRAME BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2 INCH INSIDE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-79 TYPE II, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION A1. AIRCRAFT RETURNED TO SERVICE. WINDOW FRAME P/N 65-458181 BS 360L UPPER AND LOWER AND P/N 65-46525 BS 380L UPPER AND LOWER.(M) 2L72 4F RTA16WE 20040112000852004011200085NM 2004 1 12 AWXA200301575 120031204A531066142101 SHEAR TIE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON L-1 DOOR (INTERIOR) FORWARD INTERCOSTAL CLIP (SHEAR TIE) AT BS 294.5, STR 11 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL SHEAR TIE AT L-1 DOOR BS 294.5, STR 11 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 66-14210; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 4. 2L72 4F RTA16WE 20040112001002004011200100SO 2004 1 12 C2XA03SH510 120031222A335078812 STRIP EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE NR 4 AND NR 5 EMERGENCY PROXIMITY AISLE LIGHTS WOULD NOT ILLUMINATE DURING FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 5 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. MAINTENANCE OPERATIONALLY CHECKED ALL LIGHT STRIPS AND WERE FOUND TO BE GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040112001032004011200103SO 2004 1 12 C2XA03SH513 120031223A532013500469403 CROSSBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV- DURING C-CHECK THE CROSS BEAM AT FR 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040112001062004011200106EU 2004 1 12 2004F00024 120031205A3243 MASTER CYLINDER BAG JETSTMJETSTM3101 1500215EU BRAKES LOW A B16AO OTHER O OTHER TXTAXI/GRND HDL 1 NE05538PA 751 FLT 3849 - PSM - CAPTAINS LT BRAKE PEDAL HAS NO PRESSURE WHEN DEPRESSED, ALL INDICATIONS APPEAR NORMAL FOR BRAKE PRESSURE AND EMERGENCY PRESSURE. FIRST OFFICERS LEFT BRAKE PEDAL HAS PRESSURE WHEN DEPRESSED. SERVICED CAPTAINS LT AND RT BRAKE MASTER BRAKE CYLINDERS, BLED BRAKE, OPS CHECKED NORMAL IAW AMM 32-40-00. (M) 2L72 4T RTA21EU 20040112001162004011200116EU 2004 1 12 USAASA03136 120031208A5220 BELLCRANK AIRBUSA321 A321211 3930370EU EMERGENCY DOOR FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19179UW 1521 PHL - DURING INSPECTION, THE R3 EMERGENCY EXIT DOOR FAILED THE BELLCRANK DISTANCE CHECK WHEN THE BELLCRANK FAILED TO MOVE. WITHOUT BELLCRANK MOVEMENT, THE SLIDE WOULD NOT HAVE DEPLOYED. MAINTENANCE FOUND THE OVER-RIDE CLUTCH TRIPPED. THE CLUTCH WAS RESET AND THE BELLCRANK DISTANCE CHECK PASSED THE OPERATIONAL TEST. (M) 2L72 4F RTA28NM 20040112001222004011200122WP 2004 1 12 GTIA031008 120031115A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND MAIN CABIN F/B STATION 807-927 RIGHT OUTBOARD IS CRACKED AT BOTH ENDS. TRIMMED DAMAGED AREA AT FORWARD END WITHIN LIMITS. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F A6WE 20040112001352004011200135SO 2004 1 12 C2XA03IA114 120031218A33501317 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 FLIGHT 2021, THE LEFT FORWARD EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFFECTED LIGHT ASSEMBLY AND OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM. 2L72 4T RTT00011AT 20040112001362004011200136SO 2004 1 12 C2XA03CL209 120031221A3230MS277891A SWITCH EMB 135 EMB135LR 3260305SO COCKPIT DIRTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2714516 145323 IAH FLIGHT 2831 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND CLEANED THE GEAR EXTENSION OVERRIDE SWITCH. PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. 2L72 4F RTT00011AT 20040112001382004011200138CE 2004 1 12 2004F00033 120030902A3260AO7 LAMP LEAR 25 25D 5170514CE NLG INDICATOR BURNED OUT A POSAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA0341H 217 ON FINAL APPROACH INTO ROCHESTER, NY, THE FLIGHT CREW NOTICED THE GREEN NOSE GEAR LIGHT WAS NOT ILLUMINATED. AFTER DETERMINING THE LIGHT WAS BURNED OUT AND THE NOSE GEAR WAS DOWN AND LOCKED, THE FILGHT CREW PROCEEDED TO LAND WITHOUT INCIDENT. (M) 2L72 4J A10CE 20040112001432004011200143NM 2004 1 12 CALA0300720 120031222A5230 BEAM BOEING737 737824 13844BZNM CARGO DOOR TORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2712225 28934 TEAR DAMAGE WAS DISCOVERED TO THE MACHINED BEAM ON THE FORWARD CARGO DOOR DURING A 4C CHECK. A BROKEN CABLE CUTTING THROUGH THE WEB CAUSED THE TEAR DAMAGE. THE DAMAGE WAS TRIMMED OUT AND A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5232-01041. 2L72 4F RTA16WE 20040112001542004011200154NM 2004 1 12 TSAA0253267 120030924A5330656259442 SKIN BOEING737 737282 13844ATNM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13824AL 23045 CLEANED OUTER SKIN AT EACH MOUNTING HOLE. OVER-DRILLED ELONGATED HOLES TO RESTORE HOLES TO CIRCULAR SHAPE. TRIMMED OUT CRACK DAMAGED HOLE LARGE ENOUGH TO REMOVE CRACK TO RECTANGULAR SHAPE. HFEC VERIFIED HOLES CRACK FREE. FABRICATED CIRCULAR AND RECTANGULAR DOUBLERS FROM .25 INCH THICK, MIL-T-9046, CONDITION ANNEALED TYPE III, COM C TITANIUM SHEET. WET INSTALLED DOUBLERS WITH MBS 5-63 SEALANT AND 5/32 MONEL RIVETS. REPAIR COMPLETED IAW ECO 3302. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040108000852004010800085EU 2004 1 8 KBM2003F00035 120031002A6321350A32501000 PAD SNIAS 350 AS350B2 8680813EU ROTOR BRAKE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 ROTOR BRAKE PAD WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE BRAKE PAD. 1G71 3U H9EU 20040108001542004010800154NE 2004 1 8 Z1R2003F00004 120031028A1430SS5305L4G08 SCREW SKRSKYS76 S76C 8143008NE M/R TIP CAP CORRODED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF881 A08602684 760523 HAD ONE SCREW BREAK ON REMOVAL. NR 1 BOTTOM POSITION LEADING EDGE. CORROSION AND EXCESSIVE BREAKING, TORQUE NOTED ON ALL MAIN ROTOR BLADES. ALL ATTACHMENT REPLACED AS PRE-CAUTION.(K) 1G72 3U NCH1NE 20040109000242004010900024WP 2004 1 9 MEX2003403 120030831A76033916322663 CONTROL CABLE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE RT ENGINE FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23216AM 49586 AIRCRAFT AIR TURN BACK, WHEN AIRBORE RT ENGINE BECAME ACCELERATING, IT WASN`T ABLE TO CONTROL IT, THROTTLE AT IDLE AND ENGINE AT MAXIMUM TRUST AND ENGINE WAS SHUT DOWN. DURING REVISION WAS DETECTED WITHOUT RT CONTROL ACCELERATOR AND THE 53C CABLE WAS FOUND BROKEN. THE 53C CABLE WAS REPLACED IAW MM 76-1100, ALL CORRECT. DURING OVERNIGHT SERVICE BOTH ENGINES TRIM WERE CHECKED IAW MM 71-00-00, ALL CORRECT.(K) 2L72 4F4 FRTA6WE E2EA 20040109000272004010900027WP 2004 1 9 MEX2003488 120031014A7830593806503 DOOR DOUG DC9 DC982 3022082WP THRUST REVERSER DAMAGED W ASMFO OTHER O OTHER LDLANDING 1 SW23491SH 49150 AFTER AIRCRAFT LANDED THRUST REVERSERS WERE EXTENDED BEFORE NOSE LANDING GEAR HAD BEEN CONTACT ON THE GROUND, SCRATCHING THE THRUST REVERSES LOWER DOORS OF BOTH ENGINES (LARGE: 12 INCH, WIDE 1.5 INCHES APPROX). PERSONNEL WAS SENT TO REPAIR THE DAMAGES. BOTH THRUST REVERSES LOWER DOORS WERE REPLACED IAW MM 78-30-04. DURING OVERNIGHT SERVICE, THRUST REVERSERS MECHANISMS WERE CHECKED FOR CONDITION AND OPERATION IAW MM 78-30-00, ALL CORRECT.(K) 2L72 4F A6WE 20040109000652004010900065SW 2004 1 9 2004F00012 120030920A323054510291 SHAFT SWRNGNSA227 SA227AC 8780603SW MLG SCISSOR BROKEN A I7WAO OTHER O OTHER NRNOT REPORTED 1 NM05378PH MAIN LANDING GEAR SCISSOR SHAFT BROKEN, DRILLED RETAINING PIN HOLES. (M) 2L72 4T RTA8SW 20040112000342004011200034CE 2004 1 12 2004F00018 120030119A3260 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE MLG ACTUATOR INOPERATIVE A YADAO OTHER P NO WARNING INDICATION LDLANDING 1 AL031563C UC20 AT LANDING IN ANCHORAGE, THE GEAR GREEN SAFE LIGHT DID NOT ILLUMINATE. THE LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE CONFIRMED THE PROBLEM WAS THE NOSE GEAR ACTUATOR DOWNLOCK SWITCH. (M) 2L72 4T RTA24CE 20040112000512004011200051EA 2004 1 12 03356646 120031222A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27646BR 7392 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000552004011200055SO 2004 1 12 C2XA03CL204 120031219A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716571 145633 DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LAMP. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040112000612004011200061WP 2004 1 12 AALA20031238 120031108A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217535A 49989 DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY OVERHEAD LIGHTS IN COCKPIT DIM WHEN ACTIVATED. REPLACED EMERGENCY OVERHEAD LIGHTS IN COCKPIT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112001192004011200119CE 2004 1 12 2004F00027 120030124A53121144100266 BULKHEAD BEECH 1900 1900C 1154161CE FUSELAGE CRACKED A YADAK NONE O OTHER ININSP/MAINT 1 AL031566C UC36 MAINTENANCE DISCOVERED MULTIPLE CRACKS ON THE FORWARD PRESSURE BULKHEAD, LOWER RT CORNER OF P/N 114-410026-6 WEB ASSY, AT THE UPPER END OF STIFFENER P/N 114-410026-55 AND AT STATION 84. THIS CRACK WAS APPROX 2 INCHES LONG. ANTICIPATE FINDING THAT THERE WAS A RIVET MISSING AT MANUFACTURE THAT WOULD ATTACH P/N 114-410026-23 STIFFENER TO ANGLE P/N 114-410026-9. (M) 2L72 4T RTA24CE 20040112001792004011200179 2004 1 12 03FDEA02235 420031223A344146160008000801 IRU AIRBUS310 A310 EU E/E BAY MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25450FE21719 162 ON TAKEOFF ROLL CAPT'S PFD, NAV DISPLAY, NR 1 YAW DAMPER, NR 1 IRU FAILED. REMOVED, REPLACED AND THEN OPS CHECKED NR 3 IRU AS PER A-310 M/M 34-25-00-5 AND 34-25-14 OKAY FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 461600-0800-0801, POS 3 SRL 0093, TAG 999804 ON MFG 461600-0800-0801 SRL 0359, TAG 999737. 2L72 4F RTA35EU 20040112001822004011200182EU 2004 1 12 033513031 120031217A3350 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGNECY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27303UE 41015 DURING INSPECTION THE FORWARD RT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040112001832004011200183 2004 1 12 HEEA087805 420030612A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH7578 760078 CHATTERING EXCESSIVELY. INSPECTED BY ACCESSORY SHOP AND FOUND UNIT SLOW TO RESPOND AND STICKING. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U3 U H1NE E19EU 20040112001932004011200193NM 2004 1 12 SWAA032819 120031228A783094P11 PRESSURE SWITCH BOEING737 7372H4 138448CNM NR 1 ENG T/R LEAKING A SWAAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW29083SW 22732 DECLARED EMERGENCY, HYD A-SYS FAILURE. LOW PRESS LIGHT ILLUMINATED FOR BOTH PUMPS. FOUND NR 1 ENG T/R HYD PRESS SWITCH LEAKING AT UNION FITTING. REMOVED AND REPLACED PRESS SWITCH IAW MM. 2L72 4F A16WE 20040112001942004011200194EU 2004 1 12 2003UALA00953 120031213A5520 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT ELEVATOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29406UA 454 RT ELEVATOR MR55500-006 HAD 4 AREAS OF WATER INGRESS FOUND DURING ACP OF COA 40535. UPPER SURFACE HAD AN AREA 2.6 BY 1.3 INCH LOCATED 160.5 INCHES FROM I/B EDGE, AND 3.5 INCHES FROM T/E LWR SURFACE HAD 3 AREAS, ONE 4.0 BY 1.5 INCH FROM 113 INCHES FROM I/B EDGE, ONE 1.4 BY .7 INCH, 116 INCHES FROM I/B EDGE, AND ONE 1.1 BY 1 INCH, 161 INCHES FROM I/B EDGE. ALL WERE 3.5 INCHES FWD OF THE T/E. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205, SHEETS 3 & 4. 2L72 4F4 FRTA28NM E40NE 20040112002192004011200219NM 2004 1 12 2003UALA00967 120031218A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29653UA 25391 EXTERIOR EMERGENCY LIGHT INOPERABLE AT DOOR 4L. RELAMPED, OPS CHECKED NORMAL. 2L72 4F4 FRTA1NM E24NE 20040112002302004011200230EU 2004 1 12 BAQA091533 120030916A26129560129980 FIRE DETECTOR AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE FALSE INDICATIONB BAQAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA0389SM 6425 FALSE FIRE WARNINGS WHEN DAMP. REMOVED FROM ENGINE 12104. THIS UNIT BEING SENT BACK WITH TURBOMECA WARRANTY CLAIM FORM. REPLACED WITH SERVICEABLE UNIT. 12/16/03 1G72 3U3 U H10EU E19EU 20040112002352004011200235WP 2004 1 12 AALA20031446 120031219A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2173444 49470 FORWARD GALLEY AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY AND COCKPIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002382004011200238WP 2004 1 12 AALA20031448 120031219A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 LT AND RT AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-105 FOR LT AND RT AFT OVERWING EMERGENCY EXIT SIGN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002742004011200274WP 2004 1 12 AALA20031410 120031210A335060030451 BATTERY DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 STL) FORWARD GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY B5-23 FOR FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F4 F A6WE E2EA 20040112002752004011200275WP 2004 1 12 AALA20031411 120031210A335060030451 BATTERY DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 STL) OVERHEAD EMERGENCY LIGHTS BETWEEN FORWARD GALLEY AND FIRST CLASS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY B5-23 FOR OVERHEAD EMERGENCY LIGHTS BETWEEN FORWARD GALLEY AND FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F4 F A6WE E2EA 20040112002772004011200277EU 2004 1 12 AALA20031413 120031210A3350 LIGHT FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY65015 54557NE CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW211425A 11408 DFW) EMERGENCY LIGHT FORWARD OF FORWARD SERVICE DOOR IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FORWARD OF FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F4 FRT E25NE 20040112002802004011200280NM 2004 1 12 AALA20031433 120031215A3350B215 FUSE BOEING777 777223 1385213NM BATTERY PACK BLOWN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21790AN 30251 EZE EMERGENCY LIGHTS AT SEATS BETWEEN 3LR AND 4LR DOOR INOPERATIVE. REPLACED FUSE FOR EMERGENCY LIGHTS AT BATTERY PACK AT 3R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040113000062004011300006EU 2004 1 13 BAQA091589 120031209A6420 TORSION BAR UROCOPEC135 EC135P1 8680990EU TAIL ROTOR BENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME 0009 TAIL ROTOR TORSION BAR BENT OUT OF TOLERANCE. REPLACE SERVICEABLE UNIT. 1G72 3U O H88EU 20040113000122004011300012SW 2004 1 13 I05R091954 120031208A6330L633M2010105A001MOUNT CLARK 1000 1000CLARK 2230102SW M/R GEARBOX FAILED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05 21 MAIN ROTOR GEARBOX MOUNT FAILED. REPLACED PART. 1Q71 3R 2A6 20040113000192004011300019EU 2004 1 13 BAQA091597 120031219A21402811T1001 VALVE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE HEATER STUCK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME564 0009 WILL NOT BLOW HOT AIR, VALVE STUCK. PART REPLACED WITH SERVICABLE UNIT. 12/30/2003 1G72 3U3 UO H88EU E42NE 20040113000232004011300023 2004 1 13 HEEA087814 420030621A2340A3016W INTERPHONE BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 COPILOT ICS BOX IS NOT RECEIVING. SHOP REPAIR. 1G72 4U4 U H4SW E22EA 20040113000282004011300028SW 2004 1 13 HEEA087826 120030622A243239563001 BATTERY PACK BELL 412 412 1182202SW PWA PT6 PT6* 52043EA MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 DOES NOT HOLD CHARGE. REPLACED WITH SERVICEABLE PART. 1G72 4U3 T H4SW E2NE 20040113000352004011300035NM 2004 1 13 2003UALA00955 120031213A5753 SUPPORT BEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE T/E FLAP DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29171UA 24322 FIXED T/E SUPPORT BEAM WBL 235.20 FINAL REAM EXCEEDED THE MAX BORE SIZE ALLOWED. MAJOR REPAIR. REPLACED DAMAGED SECTION PER UAL EVA IMC-30172 AND MOBILE AEROSPACE ENGINEERING EA 47-5751-13-A1059. 2L74 4F4 FRTA20WE E24NE 20040113000432004011300043EA 2004 1 13 COMA0360562 120031217A5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01446CA1901 7546 FLIGHT 5333 PILOTS WINDSHIELD SHATTERED DURING FLIGHT. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20040108000802004010800080NM 2004 1 8 HALA0300876 120031002A3260 PROXIMITY SENSOR BOEING767 767300 1385204NM MLG FAILED A HALAO OTHER N FALSE WARNING APAPPROACH 1 WP13584HA 24258 LEFT MLG DOOR LIGHT REMAINED ILLUMINATED WITH 3 DOWN AND GREEN CYCLED GEAR AND PROBLEM REPEATED BUT LIGHT WENT OUT AFTER 10 SECONDS. RUN UP ON ELEVATOR TO PUT DOWN LOAD ON AIRCRAFT EXTINGUISHED GEAR DOOR LIGHT. REMOVED AND REPLACED LEFT GEAR UP LATCH PROX SENSOR (S233 IAW AMM. OPS CHECKED OK. 2L72 4F RTA1NM 20031030000362003103000036NM 2003 10 30 UPS03441294 120030905A5712 RIB BOEING747 747121 1384871NM NR 8 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 8 V/C FLAP O/B UNKAGE I/B RIB NR 2 AND NR 3 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 AND NR 3 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000472003103000047NM 2003 10 30 UPS03441305 120030905A571265B078516 RIB BOEING747 747121 1384871NM NR 26 V/C FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 26 V/C FLAP I/B LINKAGE I/B AND O/B SUPPORT RIBS FOUND CRACKED. RT WING NR 26 V/C FLAP I/B LINKAGE BOTH I/B AND O/B RIBS REPLACED IAW SRM 51-10-01 PG 8. 2L74 4F A20WE 20031030000582003103000058NM 2003 10 30 UPS03441321 120030906A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 540 - 541, STR 25R, STRINGER FOUND CRACK AS MARKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20031030000722003103000072NM 2003 10 30 0301865503 120030930A3350 POWER SUPPLY BOEING757 757251 1384970NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01503US 23192 AFT CABIN EMERGENCY FLOOR PROXIMITY LIGHTING INOPERATIVE. REPLACED POWER SUPPLY (M9004). OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20031031000192003103100019SO 2003 10 31 SWIA200312472 120030910A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07297SW 120327 RT ANGLE CRACKED COCKPIT ENTRY BELOW FLOOR. (DISCOVERED DURING C-CHECK INSPECTION)APPLIED DOUBLER TO RT BRACKET BELOW FLOOR AT COCKPIT IAW SRM 12051-10-02. 2L72 4T4 TRTA31SO E20NE 20031031000392003103100039NM 2003 10 31 UPS03441330 120030917A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, CRACK INDICATION REVEALED ON BS 2250 S28L FUSELAGE SKIN AREA AS MARKED UNDER REPAIR DOUBLER. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1 WITH FWD MOST EXISTING FASTENERS 7EA OVERSIZED .0625 INCH AND FASTENERS INSTALLED IAW SRM 51-00-06 AND 51-30-02 AFTER INSPECTED BY HFEC. SUBEQUENT INSPECTION ARE NECESSARY DUE TO THIS REPAIR CLASSIFY AS CATEGORY B REPAIR. REINSPECT IAW EO B747-5330-17977-B. 2L74 4F A20WE 20031031000432003103100043WP 2003 10 31 UPS03841325 120030920A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STA 1730, LONG 14R CRACKED. REMOVED LONGERON SECTION 14R BETWEEN STA 1720-1766, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG10. 2L74 4F RT4A25 20031031000472003103100047NM 2003 10 31 QXEA200301203 120030925A5311 FRAME DHAV DHC8 DHC8202 2809007NM ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FRAME 4 IS CRACKED IN REAR FUSLEAGE AT LT HAND STRINGER 4. REPAIRED IAW DHC-8 RD 8-55-199. 2H72 4T RTA13NM 20031031000482003103100048NM 2003 10 31 F3LA200300149 120030929A5330 SKIN BOEING737 73736E 138443ANM FUSELAGE CANNING A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED OIL CANNING ON SKIN BETWEEN TWO EXISTING PATCH REPAIRS AT STA. 340-350, STR. 20R. NUMEROUS TIPPED FASTENER HEADS ON PREVIOUS SKIN PATCHES AT STA. 340-360, STR. 19R. CUT OUT DAMAGED AREAS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-01, FIG. 229. 2L72 4F RTA16WE 20031031000492003103100049NM 2003 10 31 0301875526 120031002A3350 WIRE BOEING757 757251 1384970NM EMERGENCY LIGHT CRUSHED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01526US 23620 EMERGENCY LIGHTS INOPERATIVE IN CABIN FLOOR MOUNTED LIGHTING FROM DOOR 1R TO ROW 14. RE-SPLICED CRUSHED JIFFY SPLICE AT D9061P/J AND D9062J/P IAW. WDM 33-51-12, PG 1 2L72 4F RTA2NM 20031031000532003103100053NM 2003 10 31 QXEA200301204 120030925A5311 FRAME DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FRAME 4 IS CRACKED IN REAR FUSELAGE AT RIGHT HAND STRINGER 4. REPAIRED IAW DHC-8 RD 8-55-199. 2H72 4T4 TRTA13NM E20NE 20031103000052003110300005 2003 11 3 DL757030857 420030920A2565 GIRT BAR BOEING757 757232 1384965NM 3L CABIN DOOR UNSECURE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27637DL 23760 ACFT PARKED AT GATE AND JUST PRIOR TO DEPARTURE FLT ATT CLOSED 3L CABIN DOOR AND NOTICED THAT THE GIRT BAR APPEARED ABNORMAL. MTC SECURED GIRT BAR ATTACH BRACKETS TO SLIDE ASSY AS PER MM. 2L72 4F RTA2NM 20031103000122003110300012NM 2003 11 3 DL73S030864 120030922A2121215201 GASPER FAN BOEING737 737232 1384475NM CARGO COMP FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27305DL 23077 ON CLIMBOUT FLIGHT ATTENDANTS REPORTED SMOKE ODOR IN CABIN, STRONGER IN AFT PART OF CABIN, NO SMOKE VISIBLE. GASPER FAN WAS TURNED OFF AND ODOR DISSIPATED. FOUND GASPER FAN AT FAULT. REPLACED SAME. 2L72 4F RTA16WE 20031103000182003110300018NM 2003 11 3 DL75K030872 120030923A5330146N378014 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27644DL 23998 THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED JUST BELOW STRINGER 25R AT FS 1690 NEAR THE AFT LAVATORY SERVICE CUTOUT. THE DAMAGED AREA WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087337-14, REV A. 2L72 4F RTA2NM 20031103000292003110300029NM 2003 11 3 DLM88030886 120030930A2130 A/C PACK DOUG MD88 MD88 3023688NM AFT FAILED A DALAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO27944DL 49817 NO PACK PRESSURE- LT AND RT ON INITIAL CLIMB TO 6000 FT. NO CABIN DIFF PRESSURE, CABIN ALT ALTITUDE AT AIRCRAFT ALT. COULD NOT REGAIN NORMAL PACK OPERATION. RETURNED TO KSTL. REPAIRED AUTO-SHUTOFF SYSTEM. 2L72 4F RTA6WE 20031103000302003110300030NM 2003 11 3 DL76L030888 120030930A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM ROWS 1-6 INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27181DN 25986 ON LAYOVER FOUND EMERGENCY TRACK LIGHTING INOP ON SEATS 1-6. REPLACED LIGHT POWER SUPPLY. 2L72 4F RTA1NM 20031103000372003110300037NM 2003 11 3 DL76G030895 120030920A7997 WIRE BOEING767 7673P6 1385105NM LEFT ENGINE CHAFED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO271501P 24983 REJECTED TAKEOFF DUE TO LOW OIL PRESSURE LIGHT ILLUMINATED. MAINTENANCE FOUND THE WIRING TO THE LOW OIL PRESSURE SWITCH CHAFED. REPAIRED SAME. 2L72 4F RTA1NM 20031103000392003110300039NM 2003 11 3 DLM90030897 120031002A2622892480 EXTINGUISHER DOUG MD90 MD9030 3023690NM CABIN LEAKING A DALAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO27909DA 53389 FD POSITION H2O PORTABLE FIRE EXTINGUISHER LEAKING FLUID. DAL LEAD SEAL INTACT WITH NO EVIDENCE OF ACTIVATION OR TAMPERING. CARTRIDGE CKS OK. REPLACED SAME. 2L72 4F RTA6WE 20031103000542003110300054NM 2003 11 3 03275406 120031002A3350 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHTSDISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27406FJ 3156 DURING INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL FOUND THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH IN THE ON POSITION AND RECHARGED THE EMERGENCY BATTERIES VIA AIRCRAFT DC POWER. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031103000732003110300073NM 2003 11 3 DHL2003748010 120031003A5210 ROLLER BOEING727 727225 1384077NM PAX DOOR OUT OF ADJUST A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01748DH 22440 FORWARD ENTRY DOOR DOES NOT SHUT VERY EASY, OUT OF ADJUSTMENT. LUBRICATED FORWARD ENTRY DOOR ROLLERS, HINGES AND LINKAGE IAW M/M 12-25-11. OPS CHECKED GOOD IAW DHL B-727 M/M 52-11-01. 2L73 4F A3WE 20031028001312003102800131EA 2003 10 28 ASOA03484 120031004A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT FS 484 INTERCOSTALS AT BL 27 TO 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT FS 484 INTERCOSTALS AT BL27 TO 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20031028001412003102800141NM 2003 10 28 GAIA03087 120030910A5311 FRAME BOEING727 727223 1384074NM FUSLAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CARGO CABIN FRAME BS 540 HAS A DENT IN THE RADIUS BELOW STRINGER 16RT. REF FASI N/R 53130 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 53-10-2 FIG 2. (M) 2L73 4F A3WE 20031028001552003102800155NM 2003 10 28 GAIA03091 120030910A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK FUOND MAIN CABIN STRINGER 15 LT CRACKED FORWARD OF BS 720C. REF FASI N/R 53134 ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M) 2L73 4F A3WE 20031028001572003102800157NM 2003 10 28 GAIA03109OP 120030924A3230NAS1304 BOLT BOEING727 727223 1384074NM LT MLG SHEARED A GAIAO OTHER O OTHER APAPPROACH 1 SW07854AA 20995 FLT 714 - FWA-MCO - DURING GEAR EXTENSION ON APPROACH TO MCO THE LEFT MAIN GEAR DID NOT EXTEND. THE CREW PERFORMED THE ABNORMAL CHECKLIST AND MANUALLY LOWERED THE GEAR. AN UNEVENTFUL LANDING WAS MADE. THE LANDING GEAR WAS PINNED IN THE DOWN POSITION AND THE AIRCRAFT WAS REPOSITIONED ON A SPECIAL AIRWORTHINESS EPRMIT TO JAX. INSPECTION REVEALED THAT A BOLT ON THE LEFT MAIN LANDING GEAR SEQUENCE VALVE REACTION ROD WAS SHEARED. REMOVED AND REPLACED THE BOLT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031028001642003102800164NM 2003 10 28 ASAA0340099 120030301A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727D RBL 1 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001712003102800171EU 2003 10 28 ASOA03470 120031001A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11634AS 370 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031028001732003102800173EA 2003 10 28 ASOA03469 120030930A3350BF50110002 COVER CNDAIRCL600 CL6002B19 1900309EA EXIT LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER AT THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031028001842003102800184NM 2003 10 28 ASAA0340111 120030301A532065479609 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON UPPER FLANGE OF INTERCOSTAL AT BS 847-867 WL 156 AND RBL 22. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000062003102900006NM 2003 10 29 ASAA0340105 120030301A5720694754220 ANGLE BOEING737 7374Q8 138447QNM RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CRACKED INBOARD UPPER RIGHT WING TRAILING EDGE PANEL INBOARD SUPPORT ANGLE AFT END. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000342003102900034EU 2003 10 29 USAASA03112 120030910A3350321430 BATTERY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19118US 1264 RECEIVED 'EPSU BATTERY EMER R' MESSAGE WHEN PERFORMING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE BATTERY IN THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031029000672003102900067 2003 10 29 ASAA0380541 420030723A25653961896501 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 PREFLIGHT CHECK, FOUND FORWARD ENTRY L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20031029000752003102900075NM 2003 10 29 ASAA0340072 120030227A531065C32396 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727G BETWEEN STRINGER 25R AND 26R. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031030001132003103000113NM 2003 10 30 03FDEA01621 120030924A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 DENT IN FRAME BS 660, ABOVE STR 25L. *S/D* REPAIRED DENT IN FRAME BS 660 ABOVE STR 25L PER FED EX EA 7-5310-70526A AND APPLIED BMS 3-23 PER FED EX JOB CARD 71C209-01. 2L73 4F RTA3WE 20031031000292003103100029NM 2003 10 31 03FDEA01669 120031001A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 N01698, BS 950F FRAME DAMAGED BETWEEN STR 25L AND 27L, REPAIR AND FASTENERS NOT INSTALLED WITH SEALANT, MECHANICAL DAMAGE ON FAIL SAFE CHORD AT TOP HORZ FASTENER, LARGE GAP BETWEEN DOUBLER AND FRAME, 1 FASTENER TO SHORT WITH GAPPED COLLAR, 1 FASTENER WITH NUT AND WASHER ON EDGE OF BRACKET. ** SD ** COMING 2L73 4F4 FRTA3WE E2EA 20031031000312003103100031NM 2003 10 31 03FDEA01685 120031002A532065453152 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CRACK IN STRINGER CLIP AT BS 950C STRINGER 6RT. ** SD ** COMING 2L73 4F RTA3WE 20031031000672003103100067NM 2003 10 31 DL764030832 120030912A2750271004110 FSEU BOEING767 767432ER 1385134NM FLAPS UNSERVICEABLE A DALAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 SO27836MH D01026 29709 WHEN SELECTING FLAPS 20, GOT A T/E FLAP DISAGREE MSG AND T/E FLAP SHUTDOWN STATUS MSG. ACCOMPLISHED BITE ON FSEU BITE SHOWED 27-51104. RESET BOX. ACCOMPLISHED A FULL VISUAL INSPECTION OF FLAPS/SLATS ASSY LOCKOUT. NO DEFECTS NOTED. CK ALL T/E ACT OVER TORQUE IND. FSEU SENSOR/LOAD RELIEF GND TEST OK. R/R FSEU PER M/M. T/E XMITTER VALUES WITHIN M/M LIMITS. CYCLED FLAPS SEVERAL TIME, OPS NORMAL. 2L72 4F RTA1NM 20031031000692003103100069NM 2003 10 31 DL76L030834 120030911A2510832200603 SEAT BOEING767 767332 1382001NM COCKPIT FAULTY A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27179DN 63 25144 FIRST OFFICERS SEAT MOTOR INOP/ HAD SMELL OF BURNT ELECTRICAL ON FINAL APPROACH. DEACTIVATED MOTORS. MANUAL OPERATION NORMAL. FWD TO MCO AND PLACARD MEL 25-11-01A. REMOVED AND REPLACED FIRST OFFICERS SEAT ASSY, OPS CHECK OK. MCO AND PLACARD REMOVED. 2L72 4F RTA1NM 20031031000812003103100081NM 2003 10 31 DL757030847 120030916A5620563201077 WINDOW BOEING757 757232 1384965NM CABIN BROKEN A DALAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO27678DL 25983 A/C ARRIVED WITH P/R WINDOW AT 45A CRACKED. ON INSPECTION FOUND UPPER HALF OF OUTER PANE MISSING,AND SEVERAL SMALLER PIECES HELD IN THE SEAL. REPLACED WINDOW. 2L72 4F RTA2NM 20031103000272003110300027NM 2003 11 3 DL73S030883 120030928A3010693732082 CONTROL PANEL BOEING737 737232 1384475NM COCKPIT OVERHEADSMOKE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27316DL 23088 PRIOR TO PUSHBACK FLT 1111 CREW SMELLED ELEC BURNING ODOR IN COCKPIT THEN NOTICED SMOKE COMING FRM F/O EYEBROW WINDOW AREA. FOUND SMOKE TO COMING FROM ENG/WING ANTI-ICE PANEL. REPLACED PANEL. 2L72 4F RTA16WE 20031103000432003110300043 2003 11 3 DL733030901 420031005A3410066500011001 INDICATOR BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE COCKPIT MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NRNOT REPORTED 1 SO27948WP 23259 CAPTS VSI STARTED SPARKING WHEN AT THE GATE IN SLC BRIEF ELECTRICAL FIRE FOLLOWED BY SMOKE IN COCKPIT. C PERFORMED EXTERNAL LEAK CHECK OF AREA ABOVE CAPT'S INSTRMENT CLUSTER NO FLUID LEAKS DETECTED. FOUND AN EMPTY SCREW HOLE IN THE GLARE SHIELD ABOVE THE INSTREMENT CLUSTER THAT HAD A BROWN FLUID IN IT. INITIALLY THE FLUID ON THE EXTERIOR CASE OF THE IVSI WAS WET. IT HAS DRIED TO A STICKY TEXTURE. SUSPECT IT TO BE COLA PRODUCT. REPLACED IVSI TESTED OK. 2L72 4F4 FRTA16WE E2GL 20031103000932003110300093WP 2003 11 3 ABXA030381 120031001A5730 SKIN DOUG DC8 DC861 3021952WP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 11 EACH HOLES HAD CRACK INDICATION ON RIGHT WING 505F PANEL. REMOVED -19 CLIP, FABRICATED NEW CLIP, ALODINED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND DWG NR 5613609. FABRICATED EXTERNAL DOUBLER AND INNER DOUBLER IAW REA D857-48044MR, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8 AND REA D857-48044MR. FABRICATED 11 EACH FREEZE PLUGS AND INSTALLED IAW DC-8 SRM 51-1-25. 2L74 4F 4A25 20031103000952003110300095WP 2003 11 3 ABXA030383 120031001A3213 STRUT DOUG DC8 DC861 3021952WP MLG CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 RT MAIN LANDING GEAR CYLINDER FORWARD LUG AFT SIDE HAD EVIDENCE OF CORROSION. CORROSION ON RIGHT MAIN LANDING GEAR CYLINDER WAS OUT OF LIMITS. REPLACED RIGHT GEAR WITH A SERVICEABLE ASSEMBLY. TRANSFERRED BRAKE ASSEMBLY 4 EA. IAW DC-8 MM 32-42-01. TRANSFERRED WHEEL ASSEMBLY 4 EA. IAW DC-8 MM 32-40-01. TRANSFERRED 2 EA. ANTI-SKID MANIFOLDS IAW DC-8 MM 32-43-03. TRANSFERRED GEAR STRUT DOOR IAW DC-8 MM 51-3-0. REMOVAL, INSTALL AND OPS CHECK OF THE RT MAIN LANDING GEAR WAS PERFORMED ON N/R 20892/YU892, AND IAW DC-8 MM. 2L74 4F 4A25 20031103000972003110300097WP 2003 11 3 ABXA030379 120031002A531357501982 LONGERON DOUG DC8 DC861 3021952WP RT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 RT MAIN LANDING GEAR WHEEL WELL LONGERON 24 AT STA. 875 TO 900 TRIPLER SHOWED EVIDENCE OF CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-2, AND REA D853-48-35MR. 2L74 4F 4A25 20031103001102003110300110NM 2003 11 3 AWXA200301134 120030905A53122024T3050 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK HFEC INSPECTION IDENTIFIED A 1.1250 INCH CRACK IN BS 178 BULKHEAD WEB AT WL 219, LBL 5.7. MAINTENANCE CUTOUT CRACK ON BS 178 BULKHEAD WEB AT WL 219, LBL 5.7; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG. 275-285, FIG. 210. 2L72 4F RTA16WE 20031103001242003110300124NM 2003 11 3 03FDEA01732 120031008A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031103001462003110300146NM 2003 11 3 03FDEA01777 120031009A5753ARC0503 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP O/B HINGE BRACKET (WING SIDE) - I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION AND CMM 57-44-09 2L73 4F RTA22WE 20031105000072003110500007SO 2003 11 5 C2XA03CL179 120031023A49304951830 FUEL NOZZLE EMB 135 EMB135LR 3260305SO APU COKED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2712530 145533 CLE FLIGHT NR 2827 THE CREW REPORTED A VERY STRONG FUEL SMELL AFTER STARTING APU. MAINTENANCE INSPECTED AND REPLACED THE NR 4 AND NR 6 APU FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031029001142003102900114NM 2003 10 29 QXEA200301194 120030928A3350AC4LW LIGHT DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09364PH 524 ALL THREE EMERGENCY EXIT BETA LIGHTS FAIL FUNCTIONING BRIGHTNESS CHECK. REMOVED AND REPLACED ALL THREE BETA LIGHTS. 2H72 4T4 TRTA13NM E20NE 20031030000102003103000010 2003 10 30 FFS2003F00020 420030912A6122B3166 SPOOL HARTZL PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA PROP GOVERNOR BROKEN E FFSAO OTHER O OTHER NRNOT REPORTED 1 AL014112K E206T 318353006 ENGINE OVERSPEED DUE TO INTERNAL FAILURE OF THE PROPELLER GOVERNOR. SPOOL B-3166 SEPARATED FROM SPOOL EXTENSION A-3167, CAUSING GOVERNOR TO ACT AS IF IN AN UNDERSPEED CONDITION, SENDING BOOST OIL PRESSURE TO FORCE PROPELLER TO LOW PITCH. SEPARATION MAY HAVE BEEN CAUSED BY LOSS OF SPRING PIN B61320250. 1L72 3O3 O A20SO E14EA 20031030000942003103000094NM 2003 10 30 03FDEA01667 120031001A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 N01643, CORROSION ON UPPER SURFACE OF LOWER SECTION OF FLOORBEAM BS 1070 LBL 7 WL 200. ** SD ** COMING 2L73 4F4 FRTA3WE E2EA 20031031000362003103100036NM 2003 10 31 UPS03441264 120030903A5347BAC1503100147 SEAT TRACK BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D SEAT TRACK FOUND CORRODED AT SEVERIAL LOCATIONS AS MARKED. REF WAN NR 796157. CORROSION BLEND OUT 0.039 INCH X 1 INCH X 4 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, CORROSION REMOVED IAW SRM 51-10-01 AND SEAT TRACK REPAIRED REFER TO SRM 53-10-05 FIG.1A. CIC APPLIED IAW EO M-5100-2780. 2L74 4F4 F A20WE E20EA 20031031000382003103100038NM 2003 10 31 UPS03441329 120030907A5320 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CHIPPED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D - BS 340 STR 13R FRAME FLOOR SUPPORT ANGLE CHIPPED. CHIPPED AREA TRIMMED OFF AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02, HFEC INSPECTED NO CRACK FOUND INSPECTION CARRIED OUT IAW EO B747-5320-17558-B AND UPS-HKG-03-00217H, RESULT - N - CRACK REVEALED, CRES STRAPS INSTALLED IAW EO 747-5320-17558-B IAW RS R-53-15-35074 AND UPS EO B747-5320-17558-C. 2L74 4F A20WE 20040212001112004021200111EU 2004 2 12 ABO2003F00000 120031203A2820 SENSOR EXTRA EA400 EA400 7021804EU FUEL SYSTEM LEAKING B ABORO OTHER K FLUID LOSS NRNOT REPORTED 1 GL15400EX 24 INVESTIGATED FUEL LEAK, FOUND BOTH FUEL SENDING UNITS LEAKING INTO AVIONICS BAY WITH STANDING FUEL, THIS BAY IS LOCATED BETWEEN THE WINGS, THIS IS A FIRE HAZARD. 1H71 3O RTA43CE 20040212001122004021200112NM 2004 2 12 03FDEA02165 120031211A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 N01305 CORROSION ON FLOORBEAM AT BS 480 LBL 45 TO RBL 45 UPPER AND LOWER SURFACE ** SD ** COMING 2L73 4F RTA3WE 20040212001172004021200117NM 2004 2 12 CNMA200300009 120031212A33201165377 TRANSFORMER BOEING757 75728A 1384976NM ROWS 20DEF&24DEFARCED A CNMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07369AX 28161 ELECTRICAL (ARCING) AND STRONG FUMES ROWS 20DEF AND 24DEF. 2L72 4F RTA2NM 20040212001202004021200120GL 2004 2 12 ALG2003F00105 220031130A7261 CHIP DETECTOR SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL ENGINE CONTAMINATED E ALGAA UNSCHED LANDING J WARNING INDICATION HOHOVERING 1 SW03707AL 760189 CAE890466S AT A HOVER READY FOR TAKEOFF, NUMBER ONE ENGINE CHIP LIGHT ILLUMATED AT A HOVER. HAD LANDED AT GALLIANO TO REFUEL. MAINTENANCE FOUND ONE SLIVER ON AFT CHIP PLUG. CLEANED PLUG AND COMPLIED WITH 30 MINUTE RUN AND LEAK CHECK. OPS CHECK GOOD. 1G72 3U3 U H1NE E1GL 20040212001362004021200136NM 2004 2 12 DHL2003742517 120031121A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FWD CARGO COMPT CABIN SEAT TRACK AND SPLICE PARTS ARE CORRODED BETWEEN STA 680-700 RBL 45. REMOVED SPLICE OF SEAT TRACK BETWEEN STA 680-700 RBL 45 AND FABRICATED NEW SPLICE FROM MAT 7075-T6 .250 PO 9911344 DIM 6.75 X 2 INCH IAW B-727 SRM 53-10-5 FIG 1 AND 51-30-2. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED SPLICE IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040212001382004021200138NM 2004 2 12 DHL2003742519 120031121A5320 FLOOR SUPPORT BOEING727 727225 1384077NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, AFT CARGO STA 1110 BLL O FLOOR SUPPORT BENT AND TWO SHEARED FASTENERS. REMOVED FASTENERS AS REQUIRED FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA 2.25 X .875 INCH AND FABRICATED REPAIR ANGLE FROM BAC 1517-1360, EXTRUSION 10.5 X .75 X .75 INCH PO 318843 AND FILLER FROM 2.375 X .875 INCH PO 318843 IAW B-727 SRM 51-40-3 FIG 1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. PARTS INSTALLED IAW B-727 SRM 51-40-3 FIG 1 AND 51-30-2. 2L73 4F A3WE 20040212001452004021200145CE 2004 2 12 DJFA200300007 120031204A3244220K281 TIRE CESSNA500 560CESSNA 2076750CE ZONE 700 FAILED E DJFAO OTHER O OTHER LDLANDING 1 EA23501CW247 5600050 DURING LANDING AIRCRAFT PULLED TO THE LT. AFTER THE AIRCRAFT SLOWED THERE DIRECTIONAL CONTROL WAS LOST AND THE AIRCRAFT WENT OFF THE LT SIDE OF THE RUNWAY DUE TO THE LT TIRE BEING FLAT. 2L72 4F RTA22CE 20040212001612004021200161EU 2004 2 12 MALA030555 120031215A302044730501 DEICE SYSTEM SAAB SF340 340B 7860101EU LT INTAKE INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15452XJ 340B452 DURING FLIGHT, THE LT INTAKE HEAT LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE PERFORMED OHMS CHECKS OF LT INTAKE HEAT ONLY FAULT HAS HIGH READINGS ON TEST BOX PINS G TO E AND E TO M FOUND PROBLEM TO BE DEICE MODULE REMOVED AND REPLACED DEICE MODULE PN 44730-501 SN OFF A00632 SN ON A00301 IAW ATC MM 30-21-03 OPS CHECKS GOOD. 2L72 4T RTA52EU 20040212001642004021200164NE 2004 2 12 P5CA0301010 220031221A7320 FCU BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 3 ENG FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23923FT 22769 702031 NR 3 ENG WOULD NOT START, NO FUEL FLOW. CHECKED FUEL CONDITION MOTOR OPS NRML S/OFF VALVE ON FRONT SPAR CHECKED NORMAL. PERFORMED FUEL PUMP PRESS TEST ON FP 12 PORT, CHECKED GOOD. BLED FUEL LINES ON FUEL CONTROL UNIT, ENGINE RAN UP OK 71-00-00. 2L74 4F4 FRTA20WE E3NE 20040329000392004032900039NM 2004 3 29 ASAA0340323 120030725A53206552878102 ANGLE BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND CHINE ANGLE AT STATION 947 TO 992 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040401000452004040100045NM 2004 4 1 AALA20031193 120031029A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21697AN 26977 MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS INOPERATIVE WHEN TESTED. (M) 2L72 4F RTA2NM 20040407000412004040700041NM 2004 4 7 TSAA0353210 120031105A53306545450 SKIN BOEING737 737230 1384401NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. AT EXISTING RIVET LOCATION, INSTALL 1/32 INCH OVERSIZE. RESTORE AERODYNAMIC SURFACE BY FILLING THE AREA WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 3389. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031112000142003111200014NM 2003 11 12 03FDEA01859 120031103A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION ON LOWER CROSS BRACE INSIDE DELTA KEELBEAM, BS 762, WL 148. REMOVED CORROSION ON LOWER CROSS BRACE INSIDE DELTA KEELBEAM BS 762, WL 148. FABRICATED NEW L-ANGLE AND REPLACED CORRODED PART WITH NEW PART PER 727 SRM 53-30-2, 51-40-2, 51-10-2, 51-20-1. 2L73 4F RTA3WE 20031112000512003111200051SO 2003 11 12 SWIA200312582 120031015A5320 CLIP EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07566SW 120341 LEFT SKIN SUPPORT CLIP CRACKED AT FRAME 12, BEHIND DV WINDOW. DISCOVERED DURING C-CHECK. REMOVED AND REPLACED LEFT SKIN SUPPORT CLIP AT FRAME 12 BEHIND DV WINDOW WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00. 2L72 4T RTA31SO 20031112000562003111200056SO 2003 11 12 SWIA200312586 120031028A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07197SW 120186 AFTER LANDING NAC FLAPS CONTROL FAULTED AND WOULD NOT RESET. REMOVED FLAP COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD. P/N: 307500-1007, S/N OFF: 169. 2L72 4T RTA31SO 20031112000922003111200092 2003 11 12 BAQA090327 420031031A3421109290 GYRO BOLKMSBK117 BK117C1 5626025EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP3121 7508 SOUNDS LIKE BEARING GOING BAD IN GYRO UNIT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20031112001052003111200105EU 2003 11 12 BAQA090341 120031028A2140JBS8803 VALVE UROCOPEC135 EC135T1 5620026EU HEATER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH466 0131 HEATER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031112001282003111200128 2003 11 12 UPS03541450 420031019A3417 ADC BOEING757 75724APF 1384969NM E/E BAY FAULTY A IPXAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01454UP 25475 INSPECTION TYPE:N/A F/O'S AIRSPEED DIFFERS BY 20 KNOTS IN FLIGHT ALTERNATE ADC SELECTED CURES INDICATION PROBLEMS. RT ADC SEEMS INACCURATE, ASSOCIATED MACH SPEED TRIM AND RUDDER RATIO EICAS MSGS DISPLAYED. T/S SYSTEM AND REPLACED RIGHT ADC PER FIM 34-12-00 AND MM 34-12-01-4 ACCOMPLISHED MCD TEST 30 CURRENT FAULT REPORT. NO FAULTS REPORTED ALL M MSG CLEARED PER MM 22-00-02/201. 2L72 4F RTA2NM 20031118000112003111800011NM 2003 11 18 UPS03641351 120031004A3350 LIGHT BOEING767 767300 1385204NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01316UP 27744 EMERGENCY DOOR LIGHT AT MAIN COCKPIT DOOR NOT WORKING. RELAMPED FIXTURE AT MAIN ENT DOOR. OPS CHECK GOOD IAW PSI CHK. 2L72 4F RTA1NM 20031118000282003111800028NM 2003 11 18 AWXA200301143 120030906A5753694065710 CARRIAGE BOEING737 7373Q8 1384670NM ZONE 600 - RIGHTCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT WING INBOARD MID FLAP INBOARD CARRIAGE ASSEMBLY INNER MOST SPINDLE RETAINER FITTING. MAINTENANCE REMOVED AND REPLACED RT WING INBOARD MIDFLAP INBOARD CARRIAGE ASSEMBLY INNER MOST SPINDLE RETAINER FITTING IAW BMM 27-51-14, FIG 202. 2L72 4F RTA16WE 20031118000302003111800030NM 2003 11 18 AWXA200301145 120030906A5753BACB30NR6K6 BOLT BOEING737 7373Q8 1384670NM ZONE 500 - LEFT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK CORROSION WAS FOUND ON LT WING INBOARD MID FLAP INBOARD CARRIAGE ASSEMBLY BOLTS. MAINTENANCE REMOVED AND REPLACED LT WING INBOARD MID FLAP INBOARD CARRIAGE ASSEMBLY BOLTS IAW BMM 20-50-11. 2L72 4F RTA16WE 20031118000402003111800040EU 2003 11 18 AWXA200301155 120030924A5315D53112087203 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF Y254 FLOORBEAM AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, CUT OUT CORRODED SECTION OF Y254 FLOORBEAM AT FR 20; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 202-203 & 205-206, FIG 201. 2L72 4F RTA28NM 20031118000462003111800046EU 2003 11 18 AWXA200301161 120030924A5315D53472189200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y1162 FLOORBEAM BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1162 FLOORBEAM FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 23-28 & 39-41 FIG 9-12, & 18. 2L72 4F RTA28NM 20031118000482003111800048EU 2003 11 18 AWXA200301163 120030924A5315 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y1292 FLOORBEAM AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1292 FLOORBEAM FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 23-28 & 39-41 FIG 9-12 & 18. 2L72 4F RTA28NM 20031118000822003111800082NM 2003 11 18 252TR0012 120031008A33501000679 LIGHT BOEING737 737228 13844AGNM PWA JT8 JT8D* NE CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 R2 DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED EMERGENCY LIGHT IAW MM 33-51-81. 2L72 4F4 FRTA16WE E2EA 20031118000992003111800099CE 2003 11 18 XGN2003F00003 120030929A5754501100034 HINGE BEECH 55 95C55 1152708CE CONT O520 IO520* 17032SO LT WING LE BROKEN E XGNAO OTHER O OTHER NRNOT REPORTED 1 SW055740V20390 TE103 LT WING LEADING EDGE ASSY SAGGING AND FLEXING BETWEEN W/S 49.131 AND 91.131. WE WERE UNABLE TO DISASSEMBLE LEADING EDGE ASSEMBLY FROM THE FORWARD SPAR CAP DUE TO BROKEN (105774C-ZG18700) HINGE PIN. NOT ABLE TO DISASSEMBLE THE LEADING, COULD ONLY GUESS THAT THE HINGE AND PIN BOTHER WERE WORN. THIS WAS DISCOVERED DURING A 100 HOUR INSPECTION. 1L72 3O3 O 3A16 E5CE 20031118001002003111800100EA 2003 11 18 03275685 120031002A324450105711 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG OUT OF TOLERANCEA VTZAK NONE O OTHER LDLANDING 1 EA27687BR 7720 NR 2 MAIN TIRE SHREDDED ON LANDING. REVISED 10-09-03 MAINTENANCE PERSONNEL REMOVED AND REPLACED THE TIRE. AIRCRAFT WAS GROUNDED FOR ADDITIONAL REPAIRS AS A RESULT OF TIRE SHREDDING 2L72 4F4 FRTA21EA E15NE 20031112000502003111200050SO 2003 11 12 SWIA200312581 120031015A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07566SW 120341 LEFT FRAME 9 CLIP UNDER DV WINDOW CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FRAME 9 LEFT SIDE PER SERVICE BULLETIN 120-53-0073 REV 00 DATED 21 JUL 99. 2L72 4T RTA31SO 20031112000692003111200069NM 2003 11 12 CALA0300632 120031109A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND A .5 INCH CRACK IN MAIN FRAME AT STA 616 AT RT SIDE BELOW FLOOR LINE. A STIFFENER WAS INSTALLED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20031112001122003111200112NM 2003 11 12 AWXA200301386 120031028A53209086105 CLIP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE REMOVED THE CRACKED FRAME ATTACH CLIP AT BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 90-8610; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 PG 1. 2L72 4F RTA16WE 20031112001372003111200137NE 2003 11 12 C1HA200393018 220031026A7230 COMPRESSOR BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE ENGINE STALLED A C1HAK NONE R PARTIAL RPM/PWR LOSS LDLANDING 1 GL15293AS 21348 FLIGHT ATTENDANTS REPORTED A POSSIBLE COMPRESSOR STALL UPON LANDING ROLLOUT. RAN ALL 3 ENG AT RUN PAD CHECKED COMPRESSOR BLEED SYSTEM OPERATION IAW B727 MM 75-31-00. NO STALLS NOTED. OK FOR SERVICE. 2L73 4F4 F A3WE E2EA 20031112001382003111200138NM 2003 11 12 UPS03241533 120031016A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE:C AREA OF SURFACE CORROSION ON SKIN AT BS 1090 S12L. AREA REPAIRED IAW SMRO EO 2003-055-002 AND UPS FILE 727-53-20131. 2L73 4F A3WE 20031113000102003111300010EU 2003 11 13 BAQA089870 120031013A2435150SG117Q STARTER GEN AEROSPAS355 AS355F1 8680810EU ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035797X213 5182 STARTER GEN HAS INTERMITTENT ROTATION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20031117000332003111700033NM 2003 11 17 QXEA200301215 120031006A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09352PH 494 PDX- MOST AFT SECTION OF EMERGENCY TRACK LIGHT MISSING 2 FEET OF CARPET COVER ON LEFT SIDE. REMOVED AND REPLACED AFT EMERGENCY LIGHT TRACK. 2H72 4T RTA13NM 20031118000082003111800008NM 2003 11 18 UPS03241355 120030916A5320 ANGLE BOEING727 7271A7C 13840X2NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 INSPECTION TYPE: C, CORROSION BETWEEN ANGLE SUPPORT AND WWW TORQUE BOX AT RBL 14.5 APPRO X AND BS 294 APPROX ON INVESTIGATION ANGLES FOUND CORRODED. ANGLES REMOVED IAW SRM 51-3 0-2. ANGLES FABRICATED IAW DRAWING 65-18415 AND 65-18417. ANGLES INS TALLED IAW SRM 51-30-2 2L73 4F A3WE 20031118000172003111800017EU 2003 11 18 154931 120031003A6123 AUTOCOARSEN SYS SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE COCKPIT WILL NOT ARM A UHLAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL1743SZ 340A043 407 DRG342689 ON 10/03/03 AT APPROX. 1040Z, FLT 4597 TOL-PIT, AIRCRAFT N43SZ ABORTED TAKEOFF FOR THE AUTOCOARSEN SYSTEM DID NOT ARM. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20031118000762003111800076NM 2003 11 18 DHL2003751011 120031008A3350 LIGHT BOEING727 727264 138408MNM PWA JT8 JT8D* NE CABIN DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01751DH 22982 EMERGENCY EXIT LIGHT ASSEMBLY IN MAIN ENTRY FELL OUT. RE-SECURED LIGHT ASSEMBLY. OPS TEST NORMAL IAW MM 25-00. 2L73 4F4 F A3WE E2EA 20031119000122003111900012NM 2003 11 19 UPS03441381 120031008A5330 SKIN BOEING747 747212B 1384886NM PWA JT9 JT9D* NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 DENT AT NOSE ACFT JACK PAD MOUNT PROTRUDING OUTWARD POSSIBLE CORROSION FMS STA 405 STRINGER 38RT. USED LFEC INSP OF AREA. INDICATION OF APPX 20 PERCENT MATERIAL LOSS. QC 10445/ (2) DEMENTIONS OF DENT IS .045 IN DEPTH. 75705/ THE DAMAGE ALLOWED REF EO. B747-5330-19344A. FOR FIFTY FLT HRS. REF D268037. SMOOTHED OUT AS PER SRM 51-10-01 AND 51-10-02. DEPTH 0.003, WIDTH 2 INCHES, LENGTH 3 INCH WITHIN SRM 53-30-01 FIG 1 LIMIT. HFEC INSP C/OUT PER NTM PART 6 51-00-00 FIG 4 AND NO CRACK FOUND. DMI 268037 (CLOSED) 2L74 4F4 F A20WE E20EA 20031119000372003111900037EU 2003 11 19 AWXA200301200 120030924A5320D53470475200 PROFILE AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LT PROFILE BETWEEN FR 48 AND FR 49. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF LT PROFILE BETWEEN FR 48 AND FR 49; FABRICATED PROFILE REPAIR SECTION AND REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5320-03154-SS1 2L72 4F RTA28NM 20031119000452003111900045NM 2003 11 19 QXEA200301227 120031008A3230860TS09Y00 CONTROL PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09401QX5607 5607 4031 DURING FLIGHT 2493 AIRCRAFT RETURNED TO FIELD, AFTER TAKEOFF THE RT MAIN LANDING GEAR INDICATED IT WAS STILL DOWN. WE RAN THE LANDING GEAR FAILS TO RETRACT CHECKLIST WHICH DID NOT HELP. FLIGHT ATTENDENT VISUALLY CONFIRMED RIGHT MAIN LANDING GEAR LOOKED FULLY RETRACTED WITH DOORS CLOSED. RIGHT MAIN LANDING GEAR DOWN WAS STILL INDICATED ON PANEL. FINISHED EMERGENCY CHECKLIST WHICH REQUIRES GEAR BE EXTENDED. FLIGHT ATTENDENTS VISUALLY CONFIRMED RIGHT MAIN LANDING GEAR DOWN. CONFIRMED GEAR DOWN BY LOOKING AT ALTERNATE GEAR EXTENSION INDICATORS ON FLOOR, SAW THREE GREEN. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031119000572003111900057NM 2003 11 19 CALA0300591 120031013A5320 WEB BOEING737 7373T0 1384582NM RAM AIR INLET CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A 1 INCH CRACK IN LT WING RAM AIR INLET SUPPORT WEB AT STA 530. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-13. 2L72 4F RTA16WE 20031119000682003111900068EA 2003 11 19 COMA0360455 120031009A284073664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01709CA21050 7238 FLIGHT 5557 LEFT FUEL INDICATION INOP. REPLACED THE FUEL COMPUTER. 2L72 4F RTA21EA 20031119000692003111900069EA 2003 11 19 COMA0370035 120031010A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01398CA356 10112 LEFT FS 1098.20 BULKHEAD BETWEEN STRINGERS 8L AND 9L IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW MFG REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031119000702003111900070EA 2003 11 19 COMA0370036 120031012A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01625CA205 10113 FS 1098.20 BULKHEAD RT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW MFG REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031119000932003111900093NM 2003 11 19 AWXA200301213 120031012A2930350E5500202 CONCENTRATOR AIRBUSA319 A319132 3930340NM ZONE 120 FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28829AW5476 1694 1563 ON CLIMB OUT OF PHX EN ROUTE FOR YVR YELLOW HYDRAULIC OVERHEAT INTERMITTENTLY FLASHED ON HYDRAULIC PAGE, TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED THE NR 1 SYSTEM DATA AQUISITION CONCENTRATOR (SDAC) IAW AMM 31-55-34, OPERATIONAL CHECK WAS GOOD. MANUFACTURER RECOMMENDED REPLACEMENT OF WIRE ASSEMBLY (P/N LA1E50200HW0100), INPUT BOARD (P/N LA1E50100H3320C, AND INPUT CONVERSION BOARD (P/N LA1E50100H3310A). PARTS WERE REPLACED AND UNIT WAS TESTED IAW CMM 31-55-44, REV. 3. 2L72 4F RTA28NM 20031119000982003111900098NM 2003 11 19 AWXA200301218 120031002A552365C2579715 TAB BOEING737 7373G7 1384595NM ELEVATOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON LT ELEVATOR TAB INBOARD LOWER LEADING EDGE. MAINTENANCE PERFORMED A BOND REPAIR ON LT ELEVATOR TAB INBOARD LOWER LEADING EDGE IAW B737-300 SRM 51-70-17, REPAIR 10, FIG. 18. 2L72 4F RTA16WE 20031118000422003111800042EU 2003 11 18 AWXA200301157 120031007A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 263 WILL NOT TEST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW4754 79 053 PHX - EEL - DURING INSPECTION THE AFT LT EMERGENCY LIGHT BATTERY PACK FAILED SELF-TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (13WL) AND EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031118001012003111800101NM 2003 11 18 AWXA200301177 120030913A5320146N518048 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK 3 EACH CRACKS WERE FOUND AT FASTENER HOLES ON CABIN FLOOR SUPPORT ANGLE BETWEEN BS 1200 TO BS 1210, BL 0. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ANGLE AT BS 1200 TO BS 1210, BL 0; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51, PG 214-215 FIG 204. 2L72 4F RTA2NM 20031119000012003111900001CE 2003 11 19 X5E2003F00000 120030915A5610PAS23112603 WINDSHIELD LEAR 25 25 5170506CE GE CJ610 CJ6101 30006NE COCKPIT FAILED B X5ERO OTHER O OTHER NRNOT REPORTED 1 SW05999MF 050 LEFT WINDSHIELD WAS REPLACED WITH A PMA PART ON 12/8/1999. ON 7/3/2001 A BLISTER/ BUBBLE HAD FORMED IN THE INNER PLY AND WAS POLISHED OUT BY THE WINDOW MANUFACTURER. ON 9/3/2003 THE WINDSHIELD BEGAN TO BLISTER IN THE SAME AREA WITH SEVERAL DEFECTS EXTENDING HALFWAY INTO THE WINDSHIELD IN THE SAME AREA WHICH HAD ALREADY BEEN REDUCED. THE WINDSHIELD WAS SCRAP. 2L72 4J4 J A10CE 1E16 20031119000342003111900034SO 2003 11 19 LR7A03083 120031009A53433700317 FITTING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 463 4606 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB3200 FOUND FS 196 NLG LT DRAG BRACE ATTACH FITTING CRACKED AT LBL 4, WL 146. REPLACED FITTING IAW SRM SMP 583 51-70 AND DWG 370031. NR 0067. 2H74 4T4 T A1SO E282 20031119000652003111900065EA 2003 11 19 COMA0360451 120031010A53116003603032 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01963CA17437 7127 718 FRAME DOUBLER CRACKED, COMPLIED WITH EO 53-077, IAW MAJOR WORK ORDER NR 71396. 2L72 4F RTA21EA 20031119000732003111900073WP 2003 11 19 ABXA030387 120030923A551099118621 PLATE DOUG DC9 DC932F 3022067WP HORIZONTAL STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 HORIZONTAL STABILIZER REMOVABLE STRESS PLATE HAD LEVEL II CORROSION, PITTING, ON EXTERIOR SURFACE AND LOWER LIP. REPAIRED AREA IAW DC-9 JOB CARD 9341004, AND DC-9 SRM. 2L72 4F A6WE 20031119001102003111900110NM 2003 11 19 C1HA200394022 120031013A3350 BATTERY BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 OVERHEAD EMERGENCY LIGHT IN AFT AIRSTAIRS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY AND BATTERIES IAW 727 MM 33-50-61. ALL OPS NORMAL. 2L73 4F A3WE 20031103000102003110300010NM 2003 11 3 DL757030862 120030919A5330146N330540 BEAR STRAP BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27686DA 27589 THE SKIN AND UNDERLYING BEAR STRAP WERE DENTED BY GROUND EQUIPMENT AT THE LOWER EDGE OF THE C2 DOOR CUTOUT AT FS 1430 JUST ABOVE THE LOWER DOOR SILL AT STRINGER 27R. THE DENTED AREA OF SKIN AND BEAR STRAP WERE CUTOUT WITH A 7 X 1.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087312-14. 2L72 4F RTA2NM 20031103000402003110300040NM 2003 11 3 DL76L030898 120031002A2760NAS1602910 PACKING BOEING767 767332 1382001NM SPOILER FAILED A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO271201P 28458 CENTER HYD SYS LEAK, QTY DECREASED STEADILY DURING FLT. FOUND PACKING ON SPOILER PCA FAILED. REPLACED SAME. 2L72 4F RTA1NM 20031103000512003110300051NM 2003 11 3 03FDEA01540 120030910A5753NRC6066 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OUTBOARD FLAP VANE NR 2 FITTING (FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE. RT OUTBOARD FLAP VANE NR 2 FITTING (FROM INBOARD) ON FORWARD HOLE BORE REPAIR CARRIED OUT AS PER EA 1-5750-72701 : WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP NR 2 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20031103001392003110300139EA 2003 11 3 SWIA200312478 120031002A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 484 RT INTERCOSTAL ON FLANGE RBL 36 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV ''A'' & RII 53-401. REPAIR ANGLE P/N: S6144-14 2L72 4F RTA21EA 20031105000132003110500013NM 2003 11 5 03FDEA01839 120031030A3260189915 PROXIMITY SWITCH BOEING727 727200 138407ENM RT MLG MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25494FE 21532 RIGHT GEAR GREEN AND UNSAFE LIGHT REMAIN ILLUMINATED AFTER T/O WITH GEAR HANDLE UP. FOLLOWED QRF AND CYCLED GEAR WITH SAME RESULTS. LOWERED GEAR AND LANDED UNEVENTFULLY. 2L73 4F RTA3WE 20031105000162003110500016NM 2003 11 5 03291421 120031018A7330 WARNING SYSTEM DORNERDO32 DO328300 NM COCKPIT ACTIVATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27421FJ 3179 DURING CLIMB THE CREW REPORTED A FADEC FAULT AND NO ITT INDICATION. 2H72 4T RTA55NM 20031105000252003110500025SO 2003 11 5 C2XA03CL172 120031002A33501317 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712528 145504 CLE FLIGHT NR 3217 THE CREW REPORTED THE EMERGENCY LIGHT OVERHEAD OF EXIT ROW IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BULB ON THE OVERHEAD EMERGENCY LIGHT AT EXIT ROW 9. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031105000322003110500032NM 2003 11 5 AWXA200301297 120031002A5320654795711 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LOWER DOOR SURROUND STRAP BS 787-847. MAINTENANCE REMOVED AFT CARGO COMPARTMENT LOWER DOOR STRAP BS 787-847; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1, 26, 32, & 37-38, FIG 8. 2L72 4F RTA16WE 20031105000332003110500033EU 2003 11 5 AWXA200301298 120031021A5240FE1740011 DAMPER AIRBUS320 A320231 3930325EU R1 DOOR FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW3467916967 053 MCN - DURING C-03 CHECK THE R-1 DOOR DAMPER FAILED TO OPERATE CORRECTLY WHEN MOVED TO CLOSED POSITION. MAINTENANCE REMOVED AND REPLACED R-1 DOOR DAMPER CYLINDER IAW AMM TASK 52-11-14-000-001, OPERATIONAL CHECK WAS GOOD. SDR WILL BE SUBMITTED UPON RECEIPT OF VENDOR TEARDOWN REPORT. 2L72 4F RTA28NM 20031105000542003110500054NM 2003 11 5 SWAA032307 120031020A2560P2070001 RETAINER BOEING737 7373A4 1384585NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 FWD EMERGENCY FLASHLIGHT BASE ASSY BROKEN. REMOVED AND REPLACED BASE ASSY PER MM. 2L72 4F RTA16WE 20031105000592003110500059NM 2003 11 5 SWAA032312 120031020A335007912 COVER BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29757LV 29850 DURING SCHEDULED MS CHECK, FOUND SEVERAL EEPLS TRACK COVERS DAMAGED. REMOVED AND REPLACED TRACK COVERS PER MM. 2L72 4F RTA16WE 20031105000792003110500079NM 2003 11 5 03FDEA01832 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE PIVOT LUG BORE INBOARD SURFACE FOUND CORROSION. 2L73 4F RTA22WE 20031106000422003110600042 2003 11 6 SWAA032293 420031017A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20031106000492003110600049SO 2003 11 6 C2XA03BT101 120031026A335074441 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712922 145338 DURING WALKAROUND, CREW FOUND EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20031106000562003110600056NM 2003 11 6 03FDEA01816 120031022A5710 STOP FITTING DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. 2L73 4F RTA22WE 20031106000742003110600074NM 2003 11 6 03FDEA01824 120031029A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION ON LOWER SECTION OF FLOORBEAM BS 1070, LBL 1-42, WL 201. REMOVED CORROSION LOWER SECTION OF FLOORBEAM BS 1070, LBL 1-42, WL 201 (14 AREAS) 1 X 1 X NO MORE THAN .018 FROM ORIGINAL .150 EXCEPT AREAS AT LBL 28 .208 REMOVED AND LBL 38 .082 REMOVED. ALL AREAS EXCEPT AT LBL 28 AND LBL 38 FOUND IN LIMITS PER SRM 53-10-1. AREA AT LBL 28 AND 38 FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED OUT OF LIMITS PER SRM 53-10-8. 2L73 4F RTA3WE 20031106000782003110600078SO 2003 11 6 SWIA200312526 120031026A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER UKUNKNOWN 1 NM07237SW 120314 ONE OF TWO RED LIGHTS INOP AT FORWARD MAIN CABIN DOOR. REPLACED BULB AT INOP (RED) FORWARD FLOOR EMERGENCY LIGHTING STRIP. OPS CHECK GOOD. 2L72 4T RTA31SO 20031106000952003110600095NM 2003 11 6 AWXA200301342 120031022A5350654657715 TAIL CONE BOEING737 737277 1384570NM FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MINOR REPAIR - DURING C-21 CHECK THE TAIL CONE WAS FOUND DELAMINATED AT LOWER CENTER 7 INCHES, 11 INCHES, & 24 INCHES FROM FORWARD END, 7.5 INCHES LT LOWER SIDE 12.5-15 INCHES FROM FORWARD END, 4-7 INCHES RT SIDE OF CENTER LOWER 16.5 INCHES FROM FORWARD END, AND 10.5 INCHES RT FROM CENTER. MAINTENANCE PERFORMED BOND REPAIR IAW B737-200 SRM 51-40-09 FIG 002 & 003. 2L72 4F RTA16WE 20031106001162003110600116SO 2003 11 6 C2XA03SH388 120031016A531314528737001 STRINGER EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAME 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031031000402003103100040NM 2003 10 31 UPS03441331 120030912A5330 SKIN BOEING747 747121 1384871NM LAP JOINT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, FX - LOWER FUSELAGE EXTERNAL SKIN LAP JOINT ATT RIVET HOLE FOUND OUT OF OVERSIZE CONTERSINK AT STA 2070 TO STA 2080 STRG 46L ( ONE EA ) ( DURING SKIN PANEL REMOVED ). SKIN REPAIRED IAW SRM 53-30-03 FIG 17 SUBSEQUENT INSPECTION ARE NECESSARY FOR THIS CATEGORY B REPAIR REFER TO SRM 53-30-03 FIG 17 TABLE III FOR INSP REQUIREMENT AND EO B747-5330-17977-B. 2L74 4F A20WE 20031031000452003103100045WP 2003 10 31 UPS03841327 120030922A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP MAIN CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 SEAT TRACK CORRODED STA 1000-1040 LBL60. REMOVED SEAT TRACK STA 990-1050 LBL60, FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM 53-2-3 FIG14 AND 8. 2L74 4F RT4A25 20031031000462003103100046NM 2003 10 31 QXEA200301202 120030925A5311 FRAME DHAV DHC8 DHC8202 2809007NM ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FRAME 4 APPEARS TO BE CRACKED IN REAR FUSELAGE OUTBOARD OF STRINGER 4R. REPAIRED IAW RD-8-53-4811. 2H72 4T RTA13NM 20031031000552003103100055NM 2003 10 31 QXEA200301206 120030925A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 TWO GOUGES 10 INCHES AFT OF FORWARD END OF NR 10 SEAT TRACK. ONE GOUGE DOWN IN CHANNEL AND ONE ON TOP FLANGE. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11 AND RD 8-53-1342. 2H72 4T RTA13NM 20031031000582003103100058NM 2003 10 31 FEM030001 120031003A29101U10652 COMPENSATOR BOEING737 737 UTILSYSNM DAMAGED B O OTHER J WARNING INDICATION NRNOT REPORTED 1 WP23 POPPET, PISTON, AND BODY ASSEMBLY OF COMPENSATOR DAMAGE. APPEARS TO BE SIMILAR TO THE PROBLEM REPORTED IN EMERGENCY AIRWORTHINESS DIRECTIVE 2002-19-51. HOWEVER, THE SERIAL NUMBER OF THE UNIT IS NOT IN THE EFFECTIVE RANGE OF THE SERIAL NUMBER. 2L72 4F RTA16WE 20031103000022003110300002NM 2003 11 3 DL757030854 120030915A5321146N51116 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27658DL 24420 THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION ALONG ITS LENGTH. THE ENTIRE UPPER CAP WAS TRIMMED OFF FROM LBL 61 TO RBL 61 TO REMOVE THE CORRSOSION. A NEW CAP WAS MADE FROM ALUMINUM EXTRUSION AND INSTALLED PER ER/A 385627-14, REV A. 2L72 4F RTA2NM 20031103000092003110300009NM 2003 11 3 DL73S030861 120030920A5330 BEAR STRAP BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 THE FUSELAGE SKIN AND BONDED DOUBLER WERE FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT OF THE L1 DOOR OPENING. THE UNDERLYING BEAR STRAP WAS UNCRACKED. THE CRACK WAS REMOVED WITH A 1.7 INCH CUTOUT IN THE SKIN AND BONDED DOUBLER AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER ER/A 087355-14, REV A. 2L72 4F RTA16WE 20031103000342003110300034NM 2003 11 3 DL76L030892 120031001A2121 FILTER BOEING767 767332 1382001NM CABIN DIRTY A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27191DN 28448 APPROX 2 1/5 HRS IN FLIGHT PAX AROUND 33FG REPORTED ODOR WHICH DISSIPATED THIS RE-OCCURRED TWICE MORE WITHIN 15-20 MINUTES TURNED OFF UTIL BUS PLUS RECIRC FANS AND PROCEEDED TO CDG/C BITE CHECK ON TEMP CONTROLLERS PACK CONTROLLERS AND BLEED AIR SUPPLY UNITS NO FAULTS VERIFY PACK COMPARTMENTS ALL NORMAL RAN BOTH ENGINES ALL NORMAL INSPECTED CABIN AREA OVERHEAD BINS AND UNITS UNDER SEATS ALL NORMAL. ALL FLUIDS QTY NORMAL. FOUND ZONE SENSORS FILTERS IN AFT CABIN VERY DIRTY. CLEANED SAME. 2L72 4F RTA1NM 20031103000772003110300077EU 2003 11 3 ALG2003F00071 120030630A6510C651A2001101 COUPLING UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE TAIL ROTOR CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL1077 1263 34280 COUPLING IS CRACKED. FOUND DURING PHASE 1 INSPECTION 1G72 3U3 UNCR0001RD E34NE 20031105000172003110500017EA 2003 11 5 03291670 120031018A7830 PDU CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27670BR 7561 DURING CRUISE THE CREW REPORTED A RT THRUST REVERSER UNLOCKED MESSAGE. CREW DIVERTED TO ALTERNATE FIELD. FLIGHT LANDED UNEVENTFULLY AND PASSENGER WERE DEPLANED NORMALLY. THE ENGINE PDU WAS REPLACED 2L72 4F RTA21EA 20031105000602003110500060SO 2003 11 5 C2XA03SH419 120031028A711014576631007 RIB EMB 145 EMB145LR 3260212SO LT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711539 145536 SHV-DURING C-CHECK THE LEFT LOWER COWLING CENTER RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031106000442003110600044WP 2003 11 6 UPS03841506 120031023A532037558451N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 BATHTUB FITTING CORRODED AT STA 1152, LONG 36R-35R. REMOVED CORRODED BATHTUB FITTING IAW SRM 53-2-0 FIG 2D, FABRICATED REPAIR ANGLE AND REPAIR SPLICES IAW SRM 53-2-0 FIG 2D, INSTALLED NEW BATHTUB FITTING AND REPAIR SPLICES IAW SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20031106000632003110600063NM 2003 11 6 03FDEA01820 120031029A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 DENT WITH GOUGE IN EXTERNAL FUSELAGE SKIN AT BS 500 AT STR 25 RIGHT. REWORKED DENT AND BLENDED GOUGE IN REWORKED AREA ON EXTERNAL FUSELAGE SKIN AT BS 500 AT STR 25 RIGHT. AREA REMOVED 1 X .8 X .020 INCH. FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRIMED, AND INSTALLED REPAIR DOUBLER PER SRM 51-40-1, 53-30-1, 53-30-3. 2L73 4F RTA3WE 20031106000672003110600067NM 2003 11 6 SWAA032297 120031018A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 500 AT STR 16R, BS 500B AT STR 26R AND BS 967 AT STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031106000802003110600080WP 2003 11 6 UPS03841508 120031025A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 A-PIT INTERNAL DOUBLER CRACKED LONGERON 34R, STA 330. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AT STA 330, LONG 34 RIGHT IAW SRM 53-2-2 AND 53-1-20D AND 53-2-2 FIG 10. 2L74 4F RT4A25 20031106001072003110600107NM 2003 11 6 QXEA200301377 120031101A2120 DUCT BOMBDRDHC8 DHC8401 1390041NM CABIN PRESSURE OUT OF POSITION A QXEAB EMER. DESCENT O OTHER CRCRUISE 1 NM09414QX 4061 SEA- ON FLIGHT 2345 AT 22,000 FEET RAPID DEPRESSURIZATION. RAN DEPRESSURIZATION CHECKLIST. EMERGENCY DESCENT. RAN MANUAL PRESSURIZATION CHECKLIST, NOTHING WORKED. NO HEAT OR PRESSURIZATION. NO DOOR WARNING LIGHTS. AIRCRAFT LANDED SAFELY. CABIN TO RECIRCULATION OUTLET DUCT BLOWN OFF MIXING BOX. INSTALLED NEW DUCT AND SEALS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031106001252003110600125 2003 11 6 SWAA032268 420031016A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031106001462003110600146EA 2003 11 6 SWIA200312533 120031020A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM FAULTY A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07465SW 7845 AILERON TRIM STUCK AT 1/3 TRAVEL RIGHT WING DOWN. RETURNED TO DFW. REMOVED AND REPLACED AILERON TRIM CONTROL PANEL AS REQUIRED. OPS CHECK GOOD IAW MM 27-00-00. 2L72 4F RTA21EA 20031106001592003110600159NM 2003 11 6 03FDEA01847 120031101A323269163395 SUPPORT FITTING BOEING727 727200 138407ENM NLG DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-3220-73848 LANDING GEAR - NLG - ELONGATED HOLES IN 69-16339-5 SUPPORT FITTING. COMPLIED WITH EA 7-3220-73848 LANDING GEAR - NLG - ELONGATED HOLES IN 69-16339-5 SUPPORT FITTING, AT MAE. 2L73 4F RTA3WE 20031106001612003110600161NM 2003 11 6 03FDEA01849 120031021A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACH LUG, OUTBOARD HOLE FOUND CORRODED. 2L73 4F RTA22WE 20031106001662003110600166NM 2003 11 6 03FDEA01854 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR LUG INBOARD HOLE HFEC INSPECTION FOUND CORROSION. 2L73 4F RTA22WE 20031202000702003120200070EU 2003 12 2 USAASA03120 120031013A335032146210 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19718UW 1077 FOUND THE AFT LEFT AND FORWARD RIGHT EPSU'S INTERNALLY FAULTED. MAINTENANCE RESET THE EPSU'S. SYSTEM OPERATES NORMALLY. (M) 2L72 4F RTA28NM 20031106001852003110600185SO 2003 11 6 C2XA03SH385 120031014A532014522460015 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A NEW SECTION IAW EMB 135 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031106001952003110600195 2003 11 6 SWAA032259 420031015A2565D31354 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031106001972003110600197EA 2003 11 6 ASOA03465 120030929A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11869AS 7479 FLT 4512 - DURING A HANGAR INSPECTION IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031106001992003110600199NM 2003 11 6 ASAA0340120 120030309A53206549631 SUPPORT ANGLE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT AT BS 500G LBL 24-28 AND WL 156. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031106002082003110600208NM 2003 11 6 ASAA0340310 120030626A33508100022605 TERMINAL BOEING737 737490 1384715NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01788AS 28885 SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 16-18 INOPERATIVE AT TEST. RESECURED LOOSE TERMINALS AT ROW 16, OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20031106002102003110600210NM 2003 11 6 ASAA0310509 120030603A5347BAC15201432 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 360-480, RIGHT BUTTOCK LINE 24 CORRODED. REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20031106002172003110600217NM 2003 11 6 ASAA0310462 120030515A53106546596122 DOOR FRAME BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE AFT CARGO DOOR FRAME AT FUSELAGE STATION 727B, STRINGER 20L GOUGED. REMOVED DAMAGED AREA AND REPAIRED DOOR FRAME PER SRM. (M) 2L72 4F A16WE 20031103000892003110300089GL 2003 11 3 ALG2003F00081 220030827A7200 ENGINE CESSNASTC STC206C 1182107CE ALLSN 250C 250C28 03013GL NACELLE FAILED E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW031067D 45435 CAE866158 DURING TAKE OFF, THE PILOT CALLED ON THE PHONE AND REPORTED THAT DURING TAKE OFF AND CLIMB AFTER FUELING, THE AIRCRAFT EXPERIENCED FOUR LOUD BANGS AND ENGINE CHIP LIGHT. PILOT MADE A 360 DEGREE TURN AND LANDED AT SMI-128A AND SHUT THE ENGINE DOWN. MAINTENANCE REMOVED AND REPLACED THE ENGINE ASSEMBLY. 1H71 3O3 UNTA4CE E1GL 20031103000942003110300094WP 2003 11 3 ABXA030382 120031001A57432598308 BUSHING DOUG DC8 DC861 3021952WP LT MLG TRUNION CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 LEFT MAIN LANDING GEAR ATTACH FITTING HAD BROWN GREASE EMITTING FROM LUGS AT BOTH ATTACH POINTS. REMOVED LEFT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45 AND DC-8 SRM 51-1-8. REINSTALLED LEFT MAIN LANDING GEAR IAW DC-8 MM 32-11-01, 32-32-10, 32-32-02, 32-11-03, 32-43-02, AND 32-41-01. OPS CHECKED GOOD IAW DC-8 MM 32-30-0, 32-43-00, 32-32-02. LUBIRCATED LEFT MAIN LANDING GEAR IAW DC-8 MM 12-81-01. LEAK CHECK GOOD IAW DC-8 MM 29-10-00-6. LEFT MAIN LANDING GEAR STRUT SERVICE COMPLIED WITH ON JOB CARD 8761001. 2L74 4F 4A25 20031103001052003110300105NM 2003 11 3 AWXA200301129 120030905A5313BAC1498162 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 RT AT BS 1006. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED STRINGER 27 RT, BS 1006 TO BS 1016; FABRICATED A NEW REPLACEMENT STRINGER; INSTALLED REPAIR PART IAW B737-300 SRM 51-20-01, PARA 6. 2L72 4F RTA16WE 20031105000062003110500006SO 2003 11 5 C2XA03SH414 120031025A532014521725013 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711539 145536 SHV-DURING C-CHECK THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED AT AFT END. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031105000632003110500063WP 2003 11 5 UPS03841499 120031023A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 C-PIT TORQUE WEB IS WORN BEYOND LIMITS AT STATION 1215-1220 LONG 33R TO 35R. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 23. 2L74 4F RT4A25 20031105000652003110500065WP 2003 11 5 UPS03841504 120031022A5210 INTERCOSTAL DOUG DC8 DC873F 302199FWP PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STRUCTURE INSIDE FWD ENTRY DOOR SNUBBER POCKET CRACKED, STA 15 LONG 16L. REMOVED DAMAGED INTERCOSTALS, FABRICATED REPAIR DOUBLER, FILLERS AND INSTALLED IAW SRM 53-2-0 FIG 2, AT FWD ENTRY DOOR SNUBBER POCKET STA 15, LONG 16L. 2L74 4F RT4A25 20031105000942003110500094NM 2003 11 5 SWAA032289 120031019A57546573714 SLAT BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND NR 2 AND NR 3 L/E SLATS DELAMINATED. REPAIRED NR 2 AND NR 3 L/E SLATS PER MM. 2L72 4F RTA16WE 20031106002342003110600234NM 2003 11 6 ASAA0310456 120030515A5313BAC1498107 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND STRINGER 26L, FUSELAGE STATION 807-827 CORRODED. REPAIRED STRINGER PER SRM. (M) 2L72 4F A16WE 20031107000282003110700028NM 2003 11 7 QXEA200301390 120031103A7110 RIB BOMBDRDHC8 DHC8401 1390041NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 PDX- NR 2 ENGINE LOWER COWL HAS CRACK ON UPPER FLANGE OF AFT CONE CENTER SUPPORT RIB. REPAIRED IAW RD8-4-71-016. 2H72 4T RTA13NM 20031107000382003110700038NM 2003 11 7 HNAA0300062 120031028A533085320106 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07930HA 126 MAJOR REPAIR; REPAIR FOR BELLY SKIN EXTERNAL CORROSION. 2H72 4T RTA13NM 20031107000412003110700041SO 2003 11 7 C2XA03SH433 120031107A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK STRINGER 19 LEFT BETWEEN FRAME 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031107000552003110700055EA 2003 11 7 03301660 120031028A5320 ISOLATOR CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27660BR 7519 DURING INSPECTION THE ISOLATOR AT FS 621 WAS IDENTIFIED AS BEING BROKEN. 2L72 4F RTA21EA 20031107000652003110700065EA 2003 11 7 03278655 120031005A3213 AXLE CNDAIRCL600 CL6002B19 1900309EA NLG CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 DURING HEAVY CHECK CORROSION WAS IDENTIFIED AT THE NOSE LANDING GEAR AXLE ASSEMBLY. THE AXLE ASSEMBLY WAS REMOVED AND REPLACED. 2L72 4F RTA21EA 20031107000982003110700098EA 2003 11 7 03305620 120031101A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27620BR 7179 DURING INSPECTION THE EMERGENCY LIGHT AT THE PASSENGER DOOR WAS FOUND INOPERATIVE. 2L72 4F RTA21EA 20031107001312003110700131 2003 11 7 MEX2003456 420030110A3417 CONNECTOR DOUG MD88 MD88 3023688NM NR 2 ADC DISCONNECTED A ASMFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW23168PL 53174 FLT 262 - MEX-REX - AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF DIFFERENCE BETWEEN VELOCIMETERS. CAPTAIN REPORTED THAT RIGHT VELOCIMETER DID NOT HAVE INDICATION SUSPENDING TAKEOFF AT 80 KNOTS. DURING REVISION THE DYNAMIC SIGNAL OF CADC NR 2 WAS FOUND DISCONNECTED. IT WAS RECONNECTED AND TESTED IAW MM 34-16-01, ALL CORRECT. ADDITIONALLY, REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-56-00. DURING OVERNIGHT SERVICE, CADC PNEUMATIC CONNECTIONS WERE REVISED IAW MM 34-16-00, ALL CORRECT. (M) 2L72 4F RTA6WE 20031105000112003110500011NM 2003 11 5 03FDEA01841 120031031A5311 FRAME BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25124FE 19360 AFT CARGO BAY CRACK IN FRAME AT FASTENER HOLE BS 1090 STR 27L UNDER FLOOR TO SIDEWALL SUPPORT. SUPP INFO: AIRCRAFT IS BEING SCRAPPED AND WILL NOT BE LEAVING THIS FACILITY. 2L73 4F RTA3WE 20031105000462003110500046NM 2003 11 5 03FDEA01714 120031007A5754ARB2850505 FITTING DOUG MD11 MD11 3023602NM L/E SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LEFT WING - FOUND NR 16 SLAT TRACK INBOARD FITTING WITH CRACK. LEFT WING NR 16 SLAT TRACK INBOARD FITTING CRACK RIB REMOVED AND REPLACED AS PER DWG ARB7565, SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20031105000762003110500076NM 2003 11 5 03FDEA01835 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD ACTUATOR LUG BORE FOUND CORROSION. 2L73 4F RTA22WE 20031106000642003110600064SO 2003 11 6 C2XA03TY180 120031016A143014527175005 NUT PLATE EMB 145 EMB145LR 3260212SO DOOR SILL CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713994 145291 TYS DURING A SCHEDULED 2C INSPECTION THE CENTER SERVICE DOOR SILL NUT PLATES WERE CORRODED. MAINT REPAIRED THE CENTER DOOR SILL IAW EMB 135/145 GST-1927-02A AND SRM 51-21-05;06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20031106000712003110600071NM 2003 11 6 03FDEA01821 120031029A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 OUTER EXTERIOR SKIN IS DENTED AT STA 1148 BETWEEN STR 24L AND 25L. REPAIRED OUTER EXTERIOR SKIN AT STA 1148 BETWEEN STR 24L AND 25L. ALL WORK DONE IAW SRM 53-30-1, SRM 53-30-3. 2L73 4F RTA3WE 20031106000792003110600079WP 2003 11 6 UPS03841507 120031025A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STA 270-280, LONGERON 32L IS CORRODED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION STA 270 TO 290 LONG 32L IAW SRM 51-1-20D AND DRWG 9754913. 2L74 4F RT4A25 20031106001702003110600170NM 2003 11 6 QXEA200301388 120031024A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX- RIGHT HAND LOWER FUSELAGE SKIN HAS OUTWARD DENT ONE INCH AFT OF X366.050 BETWEEN STRINGERS 29 AND 30. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-7600. 2H72 4T RTA13NM 20031106002252003110600225NM 2003 11 6 ASAA0310482 120030521A532065479573 WEB BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE SUB THRESHOLD WEB AT FUSELAGE STATION 792-847, STRINGER 26R CORRODED. REPLACED WEB PER SRM. (M) 2L72 4F A16WE 20031107001072003110700107EU 2003 11 7 AALA20030577 120030517A3397 WIRE AIRBUS300 A300B4605R 3930308EU CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2119059 469 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 15G INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 15G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031110000442003111000044SO 2003 11 10 C2XA03SH438 120031109A532014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 15 AND 17 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110000452003111000045SO 2003 11 10 C2XA03TY194 120031008A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 TYS DURING A SCHEDULED 3C INSPECTION THE CENTER OMEGA BEAM AT FR 20 WAS CORRODED. MAINT INSTALLED A NEW OMEGA BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031106001282003110600128NM 2003 11 6 SWAA032270 120031015A53306545877 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR FWD LOWER CUT OUT, BS 296 AND STR 17R. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20031106001962003110600196NM 2003 11 6 SWAA032260 120031015A30973205319E039 WIRE BOEING737 7377H4 1384404NM COCKPIT OVERHEATED A SWAAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW29756SA 27872 ELECTRICAL ODOR DETECTED FOLLOWED BY L2 COCKPIT WINDOW HEAT LIGHT INDICATION. REMOVED AND REPLACED L2 COCKPIT WINDOW HEAT CONTROLLER COILED WIRE PER MM. 2L72 4F RTA16WE 20031107001042003110700104NM 2003 11 7 AALA20031056 120030921A33500202365001 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21750AN 30259 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT THE FIRST CLASS GALLEY. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20031107001062003110700106EU 2003 11 7 AALA20030532 120030505A3350 SIGN AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2133069 512 MIA - DURING OVERNIGHT MAINTENANCE, CENTER AISLE EMERGENCY EXIT SIGN AT 3L DOOR INTERMITTENT. TIGHTENED EMERGENCY EXIT LIGHT SIGN ASSEMBLY AT 3L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031110000642003111000064SO 2003 11 10 C2XA03SH439 120031110A533014520551005 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE NICKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE OUTER SKIN WAS FOUND TO BE NICKED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110000692003111000069NM 2003 11 10 AWXA200301372 120031106A335020131A BATTERY PACK BOEING757 757225 1384959NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28914AW 22208 BWI - EEL - R-4 DOOR AND RT AFT CABIN EMERGENCY EXIT CEILING LIGHTS INOPERATIVE SEAT ROWS 27-34. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK AT R-4 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20031110000712003111000071NE 2003 11 10 AWXA200301374 220031105A7200V2527A5 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 MALFUNCTIONED A AWXAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP28663AW9378 1419 V10918 DURING CRUISE, A LOUD BANG HEARD & A/C SHUDDERED, FOLLOWED BY ECAM MESSAGE NR 2 ENG STALL & NR 2 ENG OIL FILTER CLOG MESSAGE. NR 2 ENG SHUTDOWN INFLT, DIVERTED, A/C LANDED SAFELY & TAXIED TO GATE UNDER OWN POWER. MAINT FOUND DEBRIS ON CHIP DETECTORS & IN OIL FILTER, SUSPECT NR 3 BEARING FAILURE. R & R NR 2 ENG IAW T/C R5M71302, OPS CHK GOOD PER T/C. TEARDOWN FINDINGS OF ENG CONFIRMED EVENT CAUSED BY NR 3 BEARING FAILURE. SECTION OF OUTER RING FOUND SEPARATED WITH AN ADDITIONAL AXIAL CRACK RUNNING DOWN CENTER OF RACEWAY. FRACTURE APPEARED TO ORIGINATE FROM A WORN LOCATION ON ID FORWARD SHOULDER & PROGRESSED OUTWARD RAPIDLY IN OVERSTRESS MODE. EVENT CAUSED AS RESULT OF SINGLE BALL SPALL FOLLOWED BY LOCALIZED 2L72 4F4 FRTA28NM E40NE 20031110000812003111000081WP 2003 11 10 MWEA030442 120031104A2560 SWITCH DOUG DC9 DC914 3022034WP TAILCONE INTERMITTENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 INTERIOR TAIL CONE RELEASE HANDLE SWITCH IS INTERMITTENT. REMOVED AND REPLACED SWITCH. 2L72 4F A6WE 20031110000862003111000086NM 2003 11 10 XNOA1163 120031101A2612 FIRE WARNING BOEING727 727200 138407ENM ENGINE MALFUNCTIONED A XN0ACE ABORTED TAKEOFF ENGINE SHUTDOWN N FALSE WARNING TOTAKEOFF 1 GL23793A 20774 REJECTED T/O AT KMCO AT 125 KNOTS FOR ENG FIRE WARN BELL. NO FIRE HANDLE, LIGHTS ILLUMINATED WITH AN ASSOC AUTO PACK TRIP AND ENG FAIL LIGHTS ILLUMINATED. ALL ENG PARAMETERS NORMAL. PERFORMED ALL APPROPRIATE ENG CHECK LISTS AND CALCULATED BRAKE COOLING FROM BRAKE COOLING CHART. PERFORMED OP'S CHECK OF ENG FIRE WARNING SYS AS PER B727 MM 26-11-0 AND PERFORMED OP'S CHECK OF AUTO PACK TRIP SYS AS PER B727 MM 21-11-0. INSPECTED A/C FOR REJECTED T/O AS PER B727 MM 5-21-121. NO DEFECTS NOTED AT THIS TIME. A/C IS OK FOR FLT. 2L73 4F RTA3WE 20031110001022003111000102NM 2003 11 10 03FDEA01828 120031029A3260 CLAMP BOEING727 727200 138407ENM COCKPIT OUT OF POSITION A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25217FE 22938 FLIGHT TEST: NOSE GEAR INDICATOR LIGHT FLICKERS & IS INTERMITTENTLY OFF WITH GEAR DOWN & LOCKED. FOUND IF PRESSURE IS APPLIED TO INBOARD EDGE OF MASTER DIM AND TEST SWITCH, LIGHTS (NOSE GEAR AND NR 3 OIL PRESSURE LIGHT) WOULD FLICKER, LOOSENED PANEL, AND FOUND HOSE CLAMP IN CLOSE PROXIMITY TO MASTER DIM AND TEST SWITCH. RELOCATED CLAMP, RESECURED INSTRUMENT PANEL AND TRIED TO DUPLICATE DISCREPANCY AGAIN, NOTED TO REPEAT OF DISCREPANCY, ALSO NOTED NO ARCING ON CLAMP OR CONTACTS ON MASTER DIM AND TEST SWITCH. 2L73 4F RTA3WE 20031110001152003111000115SO 2003 11 10 C2XA03SH422 120031029A533014520554003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714542 145547 SHV- DURING C-CHECK THE LEFT SIDE FUSELAGE SKIN WAS FOUND TO BE DENTED. MAINTENANCE RESTORED DENTED AREA TO ORIGINAL SHAPE AND PERFORMED A DOUBLER REPAIR IAW EC5330-01285. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110001232003111000123NM 2003 11 10 AWXA200301345 120031103A2560P4010021 BATTERY BOEING757 7572S7 1384962NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28906AW 23568 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT L-2 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE L-2 DOOR EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20031110001452003111000145NM 2003 11 10 03FDEA01749 120031015A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 HORZ STAB LT NR 36 BORE FOUND BEARING, SIDEWALL AND BOTTOM WITH CORROSION. BLEND OUT CORROSION FOUND EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20031110001462003111000146NM 2003 11 10 03FDEA01782 120031009A5753ARC41252 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT O/B FLAP FWD UP STOP FITTING FOUND CRACKED. RT O/B FLAP FWD UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51- 33-01 VOL. II. 2L73 4F RTA22WE 20031110001482003111000148NM 2003 11 10 03FDEA01868 120031029A2822 SHROUD DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 DURING THE PRESSURE TEST OF TAIL TANK FUEL SHROUD DRAIN SYSTEM FOUND TAIL TANK TRANSFER FUEL SHROUD TUBING LOCATED AT STA. Y 1801 LT SIDEWALL OF CENTER CARGO WITH A CRACK LINE MEASURED APPROX. 2.0 INCHES IN LENGTH. COMPLIED WITH EA 1-2822-71762 FUEL SYSTEM, FUEL SHROUD & DRAIN - CRACK REPAIR ON TUBE FOR TAIL TANK. 2L73 4F4 FRTA22WE E13NE 20031110001532003111000153NM 2003 11 10 C1HA200392006 120031027A3350 LIGHT BOEING727 727212 138407GNM CABIN MALFUNCTIONED A C1HAK NONE L NO TEST TXTAXI/GRND HDL 1 GL15292AS 21458 EMERGENCY EXIT LIGHTS ILLUMINATED DURING TAXI. RAN ALL 3 ENGINES UNDER NORMAL ELEC POWER CONFIG, EMERGENCY LIGHTS DID NOT ILLUMINATE. OPERATION NORMAL. COULD NOT DUPLICATE. OK FOR SERVICE. REF MM 33-50-01. 2L73 4F A3WE 20031110001642003111000164NM 2003 11 10 SWAA032246 120031013A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 5, WL 198. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031110001822003111000182NM 2003 11 10 SWAA032253 120031014A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 763, WL 148 AND LBL 3. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031110001992003111000199NM 2003 11 10 SWAA032244 120031012A53106546560 SHEAR TIE BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 947, STR 23L TO STR 24L. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F A16WE 20031112000022003111200002NM 2003 11 12 2003UALA00811 120031027A5330 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29374UA 24639 STR 4 LT IS CRACKED BETWEEN RIVETS FROM STA. 917 TO 918. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION AND SPLICE PIECES. 2L72 4F4 FRTA16WE E2GL 20031112000062003111200006NM 2003 11 12 2003UALA00815 120031028A5311148W45061 FAILSAFE BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29776UA 26937 STA 2260 LT FUSELAGE STA 2260 LONGERON FAILSAFE STRAP CRACKED. MAJOR REPAIR. STRAP REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20031119001422003111900142 2003 11 19 QXEA200301230 420031005A3400 ANTENNA BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 NUT PLATE IS DAMAGED FOR THE UPPER FORWARD AIR TRAFFIC CONTROL ANTENNA AT STATION X136.0. REPAIRED IAW Q400 SRM 51-42-05 AND 51-25-15. 2H72 4T RTA13NM 20031120000272003112000027NM 2003 11 20 AWXA200301236 120030922A5320656731147 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT FORWARD LEG BS 992, LBL 28-45, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 992, LBL 28-45, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51, PG 111, FIG 101. 2L72 4F RTA16WE 20031120000302003112000030NM 2003 11 20 AWXA200301239 120030922A53206546812104 STRAP BOEING737 737301 1384611NM SUBFLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT SUBFLOOR UPPER STIFFENER AT BS 1019-1023, RBL 27.5, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED RT AFT SUBFLOOR UPPER STIFFENER AT BS 1019-1023, RBL 27.5, WL 208; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031120000382003112000038NM 2003 11 20 AWXA200301247 120030922A5320BAC1496377 SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT SUPPORT ZEE AROUND NUT PLATE HOLES BS 727D-767, RBL 17. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CARGO COMPARTMENT SUPPORT ZEE BS 727D-767, RBL 17; INSTALLED A NEW REPLACEMENT SUPPORT ZEE IAW B737-300 SRM 51-40-02, FIG 8. 2L72 4F RTA16WE 20031120000582003112000058NM 2003 11 20 QXEA200301247 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 5 SEAT TRACK CHANNEL HAS LITE PITTING AND SCRATCHES AT STATION X456.500. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20031120000602003112000060NM 2003 11 20 QXEA200301249 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 5 SEAT TRACK CHANNEL HAS LITE PITTING 12 INCHES FORWARD OF AFT END 1.5 INCHES LONG. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20031120000792003112000079EU 2003 11 20 MALA030452 120031007A7603 CONTROL ROD SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE POWER LEVER CONTAMINATED A MALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL15106XJ 340A106 DURING FLIGHT NR 2733, INFLIGHT BOTH POWER LEVERS EXTREMELY DIFFICULT TO MOVE. CONDITION LEVERS OK. POWER LEVERS SUPPOSELY STICKING CONSIDERABLY, EVEN WITH FRICTION LEVER OFF. MAINTENANCE CLEANED CONTAMINANTS OFF OF POWER LEVER AND CONDITION LEVER CONTROL ROD ENDS AT PCU'S ON BOTH ENGINES. OPS CHECK OF POWER LEVERS GOOD AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20031120001002003112000100NM 2003 11 20 03FDEA01707 120031007A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 RT FUSELAGE SKIN GOUGE STRINGER 19R LAP BS 720D 14. REPAIRED RT FUSELAGE SKIN GOUGE PER SRM 53-30-3, AND SR DRAWING SR 27-57-056. 2L73 4F RTA3WE 20031120001102003112000110NM 2003 11 20 AWXA200301251 120030930A5315654541015 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A 2.2500 INCH CRACK WAS FOUND ON CABIN FLOORBEAM AT BS 660, BL (0), WL 208. MAINTENANCE PERFORMED A HFEC INSPECTION OF CRACK AND FOUND UPPER CHORD (REINFORCING ANGLE) SEVERED; REMOVED STIFFENERS, ANGLE AND SECTION OF WEB AND DOUBLER; CUTOUT CRACKED AREA OF REINFORCING ANGLE; FABRICATED A NEW REPLACEMENT SECTION OF REINFORCING ANGLE, 2 EACH SPLICE PLATES, A WEB AND FILLER, 3 EACH STRAPS, AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS AND REINSTALLED 2 EACH STIFFENERS IAW 03-5715-03284-ES2. 2L72 4F RTA16WE 20031120001162003112000116SO 2003 11 20 C2XA03BT107 120031116A3350110049 BATTERY EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714905 145476 CREW REPORTED EMERGENCY LIGHTS FAILED. EWR MAINTENANCE REMOVED AND REPLACED BATTERIES FOR THE EMERGENCY LIGHTS IAW EMB145 AMM 33-50-04. OPS CHECKED SYSTEM GOOD. NOTE: (ALL FOUR EMERGENCY BATTERY PACKS PART NUMBER: 11-0049, SERIAL NUMBERS: 73451/72621/68201/75812) 2L72 4T RTT00011AT 20031120001202003112000120NM 2003 11 20 SWAA032458 120031106A53116545409 BELTFRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BELTFRAME WEB BS 639 STR 17 WL 208. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20031121000052003112100005CE 2003 11 21 AMWA75 120031103A27311295260337 ACTUATOR BEECH 1900 1900D 1154162CE ELEVATOR TRIM STIFF A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE073199Q N3199Q DURING FLIGHT, CREW DISCOVERED THE ELEVATOR TRIM WAS STIFF AND HAD DIFFICULTY MOVING THE ELEVATOR TRIM WHEEL. THE LT ELEVATOR CLEVES WAS ADJUSTED AND THE ACFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 20031121000162003112100016 2003 11 21 SWAA032466 420031106A2565D31354 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 DURING SCHEDULED C3 CHECK, FOUND R1 ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031121000322003112100032EU 2003 11 21 03318313 120031114A3350S34C12ST6S0S0 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27313UE 41026 DURING INSPECTION THE FOWARD MID EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE LIGHT STRIP WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040113001602004011300160EU 2004 1 13 BAQA091494 120031204A6720 BUSHING BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE T/R ACTUATOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03587MC 00222 7086 TAIL ROTOR ACTUATOR LOWER ATTACHMENT FITTING BUSHING BEARING WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20031112000082003111200008NM 2003 11 12 2003UALA00817 120031029A5330 SKIN BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29619UA 21879 DENT IN SKIN AT STA 651, STR 32R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & TRIPLER REPAIR. 2L72 4F4 FRTA1NM E3NE 20031112000192003111200019NM 2003 11 12 2003UALA00824 120031030A2897 WIRE HARNESS BOEING757 757222 1384956NM PWA 2037 PW2037 NE BOOST PUMP DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 RT CENTER BOOST PUMP OVERRIDE CB POPS ON P6-4 PANEL. WIRING DAMAGE IN THE RH WHEEL WELL AS A RESULT OF ELECTRICAL ARCING. THE EVENT OCCURRED DURING A "C" CHECK VISIT WHEN TECHNICIANS WERE PERFORMING A ROUTINE INSULATION RESISTANCE CHECK OF THE FUEL PUMP. ANALYSIS OF THE DAMAGE REVEALED THAT AN UNUSUALLY SHARP BEND IN THE HARNESS SERVICE LOOP DETERIORATED THE PROTECTIVE INSULATION. THE EXPOSED CONDUCTORS ARCED TO THE SURROUNDING STRUCTURE CAUSING SEVERAL WIRES TO BE DAMAGED. DAMAGED WIRING WAS REPAIRED AND/OR REPLACED. 2L72 4F4 FRTA2NM E17NE 20031112000202003111200020SO 2003 11 12 C2XA03SH449 120031112A711014576631621 STRUCTURE EMB 145 EMB145LR 3260212SO LT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV-DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031112000212003111200021SO 2003 11 12 C2XA03SH448 120031112A532014525381009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 64 WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE CENTER BUTTSTRAP IAW EMB 145 SRM 53-31-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031112000302003111200030 2003 11 12 SWIA200312578 420031103A3417607300001 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07403SW1050 1050 7028 STALL FAIL CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED LEFT MACH TRANSDUCER IAW CRJ MM 27-35-25. OPS CHECK GOOD. 2L72 4F RTA21EA 20031112000362003111200036NM 2003 11 12 03FDEA01756 120031014A5753ARC0502506 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE WING SIDE LOWER MOUNT O/B CAVITY FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71748 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031112000372003111200037NM 2003 11 12 03FDEA01772 120031009A5753ARC0502505 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING O/B FLAP I/B HINGE (WING SIDE) - O/B LOWER ATTACHMENT TO REAR SPAR, HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS - LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031107000682003110700068EA 2003 11 7 03301628 120031028A322016040107 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NLG CORRODED A VTZAO OTHER J WARNING INDICATION UKUNKNOWN 1 EA27628BR 477 7240 DURING FLIGHT CREW RECEIVED A NOSE GEAR DISAGREE WARNING MESSAGE. UPON TROUBLESHOOTING ON GROUND THE NOSE LANDING GEAR ASSEMBLY WAS FOUND TO BE CORRODED AND GOUGED. THE BRACKETS AND STRUCTURE ON WHICH THE PROXIMITY SENSORS WERE MOUNTED WERE ALSO FOUND CORRODED AND CRACKED. AIRCRAFT WAS RELEASED FROM HEAVY CHECK ON 08-11-03. 2L72 4F RTA21EA 20031107001462003110700146WP 2003 11 7 GTIA030736 120030923A5321 FLOORBOARD DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW FOUND MAIN CABIN STATION 408 TO STATION 446 RBL 44 INCHES FLOORBOARD HAS CRACKS ON EDGE AND DAMAGED. FABRICATED NEW FLOORBOARD. 2L72 4F4 F A6WE E2EA 20031107001552003110700155NM 2003 11 7 ASAA0310470 120030515A5755654645171 SPOILER BOEING737 737290C 138448VNM WING DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND THE NR 8 SPOILER AT WING STATION 395.47 - 447.47 DELAMINATED. CUT OUT DAMAGED AREA AND REPAIRED PER EA. (M) 2L72 4F A16WE 20031112000482003111200048NM 2003 11 12 DXTA200300143 120031019A7830DS23267 CIRCUIT CARD AMD FALC50FALCON2000 2730170NM THRUST REVERSER FAILED E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07255QS1890 155 DURING CRUISE AMBER "THRUST REVERSER" WARNING LIGHT CAME ON, NO AIRCRAFT BUFFETING OR ENGINE POWER REDUCTION NOTED. - INSPECT LT THRUST REVERSER IAW FALCON SERVICE ADVISORY FSA2000 78-30/03 ALL ITEMS GOOD AT THIS TIME. FOUND L40ER PC CARD BAD, REMOVED AND INSTALLED A REPAIRED CARD, FOUND LT UPPER OUTBOARD SEAL RIPPED REMOVED AND INSTALLED NEW SEAL PN DS252-11 ALL WORK DONE IAW FALCON 2000 MM CHAPTER 78-00-00. 2K73 4F RTA50NM 20031112000732003111200073NM 2003 11 12 AWXA200301397 120031030A5311651768537 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FRAME CHORD, AFT OF L-1 DOOR BS 344, STR 15 LT. MAINTENANCE REMOVED DAMAGED FUSELAGE FRAME CHORD AFT OF L-1 DOOR BS 344, STR 15 LT; FABRICATED A NEW REPLACEMENT FUSELAGE FRAME CHORD; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 & 11 PG 1. 2L72 4F RTA16WE 20031112000752003111200075NM 2003 11 12 AWXA200301398 120031030A532069265553 CLIP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.5 INCH CRACK WAS FOUND IN RADIUS OF INTERCOSTAL CLIP ANGLE BS 344, STR 16 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT FUSELAGE CLIP ANGLE; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 & 11 PG 1. 2L72 4F RTA16WE 20031112000792003111200079EA 2003 11 12 SWIA200312501 120031010A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 OVERHEAD CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. (DISCOVERED DURING C-CHECK)REMOVED AND REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW HARTWELL CORP. CMM 52-22-03. 2L72 4F4 FRTA21EA E15NE 20031112000842003111200084NM 2003 11 12 C1HA200394033 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 741 - 757 LBL 45.5 HAS BARE METAL, CORROSION AND WORN AREAS. 2L73 4F A3WE 20031112001222003111200122EU 2003 11 12 BAQA090117 120031017A2435 SHAFT AEROSPAS355 AS355F1 8680810EU STARTER GEN SHEARED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911KY379 1883 5101 STARTER SHAFT SHEARED. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20031112001242003111200124CE 2003 11 12 BAQA089500 120031004A2750100384040 MOTOR BEECH 100 100BEECH 1152916CE PWA PT6 PT6A27 52043EA TE FLAPS OVERHEATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 2 B144 MOTOR OVERHEATED. REPLACED WITH SERVICEABLE UNIT. 1L72 3T4 T A14CE E4EA 20031112001262003111200126 2003 11 12 BAQA089759 420031009A3421060001301 GYRO UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE COCKPIT MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME442 0009 GYRO TAKES 10 MINUTES TO SPOOLUP AND IS NOISY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 UO H88EU E42NE 20031112001342003111200134NE 2003 11 12 HEEA090149 120030916A24327655000902103 CONTACTOR SKRSKYS76 S76A 8143006NE MASTER BATTERY FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 AFTER ENGINE START AND PRIOR TO TAKE OFF, BATTERY OFF CAUTION LIGHT ILLUMINATED AND WOULD NOT GO OUT. MAINTENANCE REPLACED BATTERY RELAY. 1G72 3U H1NE 20031113000042003111300004EU 2003 11 13 BAQA090072 120031009A6730SC7282 SERVO AEROSPAS365 AS365N2 8680815EU SERVO SYSTEM LEAKING B BAQAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA03915ME2998 6417 SERVO IS LEAKING. PART ON AIRCRAFT FOR ONLY 1.1 HOURS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20031113000252003111300025 2003 11 13 BAQA089833 420031015A34516223672001 INDICATOR BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101* NE DME INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03391813066 7003 DME INDICATOR UNIT WILL NOT FUNCTION AT ALL. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20031107001342003110700134SO 2003 11 7 SIMA200327902 120030927A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTER 53-24-02, EMB STATEMENT IC2003-145/3093A AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031107001622003110700162EU 2003 11 7 AALA20030838 120030806A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 JFK - DURING OVERNIGHT MAINTENANCE, SEAT 25G EMERGENCY PATH LIGHT INOPERATIVE. FOUND LOOSE CONNECTOR UNDER SEAT. REPAIRED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031110000602003111000060SO 2003 11 10 RAIA00310274 120031028A3250852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO NLG DEFECTIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03816HK11086 145055 5709-STL- NOSE WHEEL STEERING INOP. MAINTENANCE REMOVED AND REPLACED RUDDER STEERING PROX SENSOR. 2L72 4T RTT00011AT 20031110001562003111000156NM 2003 11 10 03FDEA01856 120031021A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORE FOUND CORROSION. REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5750-73337. 2L73 4F RTA22WE 20031112000522003111200052NE 2003 11 12 03294317 220031021A726131041092 LINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE ENGINE WORN A VTZAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27317UE 41031 DURING CLIMB CREW RECEIVED LT OIL PRESSURE LOW INDICATION. CREW PERFORMED IN FLIGHT SHUT DOWN AND DECLARED EMERGENCY FLIGHT LANDED UNEVENTFULLY. THE TURBINE BEARING SUPPLY AND SCAVENEGE LINES 2L72 4T4 TRTA41NM E18NE 20031112000832003111200083NM 2003 11 12 C1HA200394032 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK AT BS 344 - 380 RBL 56 HAS BARE METAL AND CORROSION. 2L73 4F A3WE 20031112000882003111200088NM 2003 11 12 C1HA200394036 120031108A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 480 - 689.45 LBL 45.5 HAS CORROSION AND WORN AREAS. 2L73 4F A3WE 20031112000902003111200090NM 2003 11 12 C1HA200394024 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 852 - 868, LBL-45.5 HAS LIGHT CORROSION AS MARKED. 2L73 4F A3WE 20031112001192003111200119CE 2003 11 12 BAQA088981 120031013A32335081016418 ACTUATOR BEECH 90 C90 1152913CE PWA PT6 PT6* 52043EA MLG FAILED W BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0390LF 1324 LJ852 GEAR ACTUATOR FAILED END PLAY INSPECTION. 1000 CYCLE/ 30 MONTH INSPECTION. REPLACED WITH SERVICEABLE UNIT.10/20/03 1L72 3T3 T 3A20 E2NE 20040113001952004011300195SO 2004 1 13 RAIA00312306 120031207A3610S2U2226 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS WORN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03819HK 145062 STL- BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING IN CARGO AREA RT SIDE. 2L72 4T RTT00011AT 20040113002122004011300212SO 2004 1 13 C2XA03SH500 120031217A532014522460009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040113002342004011300234NM 2004 1 13 QXEA200301305 120031021A2810 VALVE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS NRNOT REPORTED 1 NM09348PH 484 PDX - FUEL DRIP FROM RIGHT NACELLE REFUELING PORT. INSPECTED AND FOUND LOWER WIGGINS FITTING ON REFUEL/DEFUEL VALVE OFFSET AND LEAKING. REPLACED REFUEL/DEFUEL VALVE AND O-RINGS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040114000022004011400002CE 2004 1 14 GLBA2003145 120031105A5350 RADOME BEECH 1900 1900D 1154162CE NOSE BIRD STRIKE A GLBAO OTHER C F.O.D. LDLANDING 1 NM03195GL UE195 BIRD STRIKE, DAMAGED RT I/B WING, RT O/B WING AND RADOME. REPLACED LT INBD LEADING EDGE PN 114-120028-23 2L72 4T RTA24CE 20040114000382004011400038NM 2004 1 14 DL757030950 120031025A3411 SENSE LINE BOEING757 757232 1384965NM ELEVATOR CHAFED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27677DL 25982 ELEVATOR FEEL MSG CLIMBING THROUGH 28K. NO MEL RELIEF. RETURNED TO SLC. FOUND LEFT STATIC SENSE LINE FOR ELEVATOR FEEL CHAFED THROUGH. REPLACED SAME. 2L72 4F RTA2NM 20040114002012004011400201NM 2004 1 14 MWEA030457 120031125A5347593054770 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 SEAT TRACK NR 6 AT STATION 491 HAS CORROSION. FABRICATED AND INSTALLED REPAIR PARTS. 2L72 4F RTA6WE 20040114002282004011400228EA 2004 1 14 03334664 120031130A4990 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY LEAKING A VTZAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27664BR 7528 DURING PREFLIGHT INSPECTION OF FLT NR 7394, THE CREW NOTED A SMOKE SMELL IN THE CABIN. CREW NOTIFIED MX CONTROL OF PROBLEM AND MAINTENANCE WAS DISPATCHED PROBLEM WAS FOUND TO BE APU OIL ENTERING THE AIR INTAKE AND CAUSING SMOKE IN THE PACS. THE APU IS CURRENTLY DEFERRED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE WITH THE APU DIFFERED. 2L72 4F RTA21EA 20040115000522004011500052NM 2004 1 15 DL73S031078 120031212A53306545767103 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 DENTS WERE NOTED IN THE SKIN PANEL AT APPROXIMATELY BS 380 AND BETWEEN S15L AND S18L. DENTS WERE CUTOUT AND REPAIRED PER ERA 385947-14. 2L72 4F RTA16WE 20040115000962004011500096NM 2004 1 15 03FDEA02284 120031229A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, I/B FLAP O/B AFT HINGE LOWER SIDE LOAD ROLLER BOLT ATTACHMENT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75226, TITLE: WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBOARD FLAP AFT OUTBOARD HINGE UPSTOP BRACKET REPAIR. 2L73 4F RTA22WE 20040115001312004011500131NM 2004 1 15 DL73S031096 120031216A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 FOUND ON W2 LETTER CK, CORROSION ON FORMER STA 967 O/B OF STR 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11. 2L72 4F RTA16WE 20040115001392004011500139NM 2004 1 15 DL76G031105 120031216A242163178 GENERATOR BOEING767 767332 1382001NM LEFT FAULTY A DALAK NONE O OTHER ININSP/MAINT 1 SO271605 30198 DURING PDC FOUND HYD GEN VOLTS LOW DURING TEST. REPLACED HYD MOTOR GENERATOR PER MM. 2L72 4F RTA1NM 20040115001452004011500145NM 2004 1 15 DL73S031109 120031218A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT REVEALED 15 CRACK INDICATIONS IN THE SKIN PANEL BETWEEN FS 540 & 727. THE INSPECTIONS WERE PERFORMED PER AD 2003-08-15. THE ENTIRE LAP JOINT WAS TRIMMED OUT AND REPAIRED PER BAC S/B 737-53A1177. THE REPAIR WAS DOCUMENTED PER ER/A 087962-14AD. 2L72 4F RTA16WE 20040115001482004011500148NM 2004 1 15 03FDEA02152 120031209A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 STRINGER CLIP CRACKED, STR 6R, BS 950F. REMOVED CRACKED STRINGER CLIP BS 950F, STR 6 RT PER SRM 51-30-2. FABRICATED, LOCATED, ALODINED, PRIMED, DRILLED AND INSTALLED NEW STRINGER CLIP BS 950F, STR. 6 RT PER SRM 51-20-1. NEW CLIP FABRICATED FROM .032 7075-T6 LOT 508473. 2L73 4F RTA3WE 20040115001492004011500149NM 2004 1 15 03FDEA02153 120031209A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 STRINGER CLIP CRACKED, STR 4L, BS 950F. REMOVED CRACKED STRINGER CLIP BS 950F, STR 4L PER SRM 51-30-2. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED NEW STRINGER CLIP BS 950F, STR 4L PER SRM 51-20-1, 51-10-2, 51-30-2 AND FED EX MM 51-20-151-7. CLIP WAS FABRICATED FROM .032 7075 T6. 2L73 4F RTA3WE 20040115001592004011500159 2004 1 15 DL738031114 420031219A3417C17001BA01 ADC BOEING737 737832 13844CFNM E/E BAY MALFUNCTIONED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO273737C 30799 AFTER PUSHBACK, F/O SPD AND ALT TAPES WERE LOST, CAME BACK INTERMITTENTLY. SWITCHING FMC NAV SWITCH TO BOTH ON L SEEM TO WORK FOR ABOUT 2 SEC ON T/O, A/T ARM SWITCH WENT TO OFF. AIRBORNE, CAPT LOST F/D AUTO PILOT WOULD ENGAGE IN CWS ONLY HAD FAINT ODOR OF SMOLDERING WIRE. REPLACED AIR DATA MODULE PER FIM, ALL CHECKS GOOD. 2L72 4F RTA16WE 20040115001602004011500160NM 2004 1 15 DL73S031115 120031220A2497 WIRE HARNESS BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE SHORTED A DALAO OTHER H ELECT. POWER LOSS-50 PC LDLANDING 1 SO27243WA 23517 709174 ON APPROACH, THE LEFT GEN TRIPPED. RT BUS ATTEMPTED TO PICK UP AND TRIPPED ALSO. DOWN TO STBY POWER. CREW DECLARED EMERGENCY. FOUND LT GENERATOR CABLE SHORTED. REPLACED GENERATOR FEEDER HARNESS. 2L72 4F4 F A16WE E2EA 20040115001622004011500162NM 2004 1 15 DL76L031118 120031221A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27171DN 24759 EMERGENCY AISLE LIGHTS AFT OF L1 AND R1 DOOR INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY M735, OPS NORMAL. 2L72 4F RTA1NM 20040115001672004011500167NM 2004 1 15 03FDEA02162 120031211A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 STRINGER CLIP CRACKED, STR 5L, BS 950E. REMOVED AND REPLACED STRINGER CLIP AT BS 950E, STR 5L IAW SRM 51-30-2 2L73 4F RTA3WE 20040115001692004011500169SO 2004 1 15 RAIA00312312 120031211A801135059105 STARTER EMB 145 EMB145LR 3260212SO NR 1 ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03812HK7117 145373 MSP- NR 1 ENGINE NO START. MAINTENANCE REMOVED AND REPLACED NR 1 STARTER. 2L72 4T RTT00011AT 20040115001752004011500175NE 2004 1 15 UIEA200300060 220031011A7200 ENGINE BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 3 MAKING METAL A UIEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 EA15506MC 21252 517334 IN CRUISE, ENGINE NR 3 COMPRESSOR STALLS WITH N1, N2 AND EGT FLUCTUATION. PERFORMED ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECK IAW FLIGHT HANDBOOK 3.70.1. SHUTDOWN ENGINE AND RETURNED. FUEL DUMPED 6,000 KGS. VISUAL INSPECTION OF NR 3 ENGINE, FOUND METAL IN TAILPIPE. REMOVED AND REPLACED NR 3 ENGINE IAW FORM 01-AA-44B AND IAW MM 72-00-00. ACCOMPLISHED ENGINE RUN. ALL PARAMETERS CHECKED NORMAL. (M) 2L74 4F4 FRTA20WE E23EA 20040115001952004011500195NM 2004 1 15 03FDEA02341 120031229A5753ARC42301 BRACKET DOUG MD11 MD11 3023602NM T/E FLAP BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING O/B FLAP I/B HINGE (FLAP LOWER SIDE) FAIRING SUPPORT BRACKET FOUND BROKEN. FLAP I/B HINGE (FLAP LOWER SIDE) FAIRING SUPPORT BRACKET REMOVED AND REPLACED AS PER AMM 20-50-02. 2L73 4F RTA22WE 20040115001962004011500196NM 2004 1 15 03FDEA02342 120031229A5744ARC77171 BRACKET DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING O/B FLAP O/B HINGE (WING SIDE) FAIRING SUPPORT O/B FWD BRACKET FOUND CRACKED. LT WING O/B FLAP O/B HINGE (WING SIDE) FAIRING SUPPORT O/B FWD BRACKET REMOVED AND REPLACED AS PER AMM 20-50-02. 2L73 4F RTA22WE 20040116000042004011600004NM 2004 1 16 03FDEA02170 120031211A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 INTERIOR FUSELAGE STRINGER CLIP IS CRACKED AT STR 4L, BS 783. REMOVED AND REPLACED STRINGER CLIP BS 783, STR 4L IAW SRM 51-30-02 2L73 4F RTA3WE 20040116000092004011600009NM 2004 1 16 03FDEA02178 120031212A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 344 RBL 19. REMOVED AFT LAV WALLS FOR ACCESS. CUT OUT AND REPLACED DAMAGED FLOORBEAM BS 344, RBL 6 - RBL 65. MATERIAL BAC 1505-29222, LOT 525160 DRILLED AND COUNTERSUNK FASTENER HOLES. ALODINED, PRIMED FLOORBEAM. INSTALLED FLOORBEAM. REINSTALLED AFT LAV WALLS. IAW SRM 53-10-1, SRM 51-30-2, SRM 51-30-5, SRM 51-30-8, SRM 51-10-2. 2L73 4F RTA3WE 20040127001532004012700153NM 2004 1 27 ASAA0310198 120030321A5230 WEB BOEING737 737298C 1384490NM CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO DOOR WEB AT BODY STATION 847, STRINGER 19R-20R CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040127001812004012700181WP 2004 1 27 ASAA0380646 120031015A532199365811 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FLOORBOARD IS CORRODED AND HAS DEFECTIVE INSERTS AT FS 1174-1250. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20040127001832004012700183NM 2004 1 27 ASAA0310196 120030321A5320655572650 ATTACH ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND BULKHEAD ATTACH ANGLE AT BS 727, LEFT BUTTOCK LINE 50, RIGHT BUTTOCK LINE 50 CORRODED. REMOVED AND REPLACED ATTACH ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040128000582004012800058EU 2004 1 28 03360305 120031226A33506047051 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27305UE 41019 DURING INSPECTION THE AFT SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLY WAS FOUND TO BE FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040128001772004012800177CE 2004 1 28 DXTA200300210 120031227A3260387 BULB CESSNA560 560XL 2076702CE MLG INDICATOR INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION DEDESCENT 1 GL07676QS 5605176 RIGHT LANDING GEAR DOWN & LOCKED INDICATOR DID NOT ILLUMINATE WHEN GEAR LOWERED, WHEN CHECKED ON ROTARY TEST, OR WHEN GEAR WAS BLOWN DOWN. LIGHT ILLUMINATED UPON LANDING. FOUND BOTH BULBS IN RIGHT GEAR DOWN & LOCKED INDICATOR TO BE INOPERATIVE. REPLACED BULBS WITH NEW BULBS & OPS CHECKED LANDING GEAR INDICATION PER CESSNA 560XL MM CHAPTER 32-60-00. EXTENDED & RETRACTED GEAR TO BLEED LANDING GEAR HYDRAULIC SYSTEM PER CESSNA 560XL MM CHAPTER 32-30-00, OPS CHECK GEAR NORMAL. SERVICED EMERGENCY GEAR / BRAKE PNEUMATIC BOTTLE PER CESSNA 560XL MM CHAPTER 12-13-01. 2L72 4F RTA22CE 20040129001072004012900107NM 2004 1 29 DHL2003742543 120031120A5311 FRAME BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD CORNER AREA WITH DENTS. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABED NEW ONE FROM BAC1503-100274 PO334880 DIM 42 INCHES & SPLICE ANGLE 9 INCHES IAW B727 SRM 51-40-4 FIG 1. CUT OUT DAMAGED WEB & FABBED NEW FROM 7075-T6 .071 DIM 31 X 4.25 INCH PO900242 & 2 EA SPLICE DOUBLERS SAME MAT DIM 8.5 X 4.25 INCH IAW 727 SRM 53-10-2 & 51-40-2 FIG 1, REPAIR PARTS TREATED & PRIMED IAW 727 SRM 51-10-2. INSTALLED IAW 727 SRM 51-40-2 FIG 1 & 51-40-4 FIG 1. 2L73 4F A3WE 20031112001392003111200139NM 2003 11 12 UPS03241534 120031019A5312 PRESSURE PANEL BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE:C NLG W/W BS 290 LBL 0 SUSPECT CRACKS IN ROW OF RIVETS AT NLG CEILING. AREA CUTOUT IAW SRM 51-40-2 FIG 1, HFEC NDF. REPAIRED CUTOUT IAW SRM 51-10-2 FIG 1. 2L73 4F A3WE 20031117000472003111700047NM 2003 11 17 583CC0001 120030926A33501000677 BATTERY PACK BOEING737 737291 138448WNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05583CC 21069 LT OVERWING EMERGENCY EXIT LIGHT AND EMERGENCY EXIT LIGHT OVER R1 DOOR INOP. REPLACED BATTERY CHARGER IN AFT CARGO AND REPLACED BATTERY PACK AT R1 DOOR. LIGHTS CHECK GOOD IAW MM 33-51-02. 2L72 4F A16WE 20031117000502003111700050WP 2003 11 17 CALA0300575 120031006A5310 DOOR FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714831 49491 INSPECTION FOUND AFT CARGO COMPARTMENT LOWER DOOR JAMB CORRODED. A SPACER WAS FABRICATED AND INSTALLED IAW SRM 53-05. 2L72 4F4 F A6WE E2EA 20031117000542003111700054NM 2003 11 17 DHL2003749502 120030919A5330 SKIN BOEING727 727200 138407ENM FUSELAGE PUNCTURED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK, RT SIDE FUSELAGE STA 1340 AIRSTAIR CUTOUT HOLE PUNCTURED IN SKIN. CUT OUT DAMAGED SKIN AND FABBED FILLER FROM 2024 T3 .050 PO 90098 DIM 14.625 X 12.25 INCH AND DOUBLERS FROM 2024 T3 .063 PO 90024 DIM 6.125 X 4.5 X 5.5 X 4.25 INCH IAW B-727 SRM 53-30-3 FIG 3. CUT OUT DAMAGED LWR ANGLE AND FABBED NEW FROM 7075-T6 PO 9911868 .080 DIM 12 X 5 INCHES AND 3 EACH SLICE ANGLES FROM SAME MAT DIM 7.25 X 4.5 INCHES EACH IAW B-727 SRM 51-40-4 FIG 1. ALL PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED IAW B-727 SRM 53-30-3 FIG 3 AND 51-40-4 FIG 1. 2L73 4F RTA3WE 20031117000632003111700063EA 2003 11 17 COMA0370034 120031003A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01390CA683 10106 FS 1098.20 BULKHEAD BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031117000692003111700069SO 2003 11 17 C2XA03SH375 120031008A531013500469403 CROSSBEAM EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 DURING C-CHECK THE CROSSBEAM AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031117000712003111700071NE 2003 11 17 ALG2003F00084 120030827A2120 ODOR SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL COCKPIT DETECTED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03703AL 760266 CAE89796S ON TAKE OFF. JUST AS AIRCRAFT CLEARED HELIPORT DEPARTING EI333; DETECTED ODOR SIMILAR TO OVERHEATED BRAKE OIL OR CLUTCH MATERIAL. HAD NO CAUTION, WARNING OR ADVISORY LIGHTS OR INOP EQUIP, CONTINUED 12 MINUTE FLIGHT TO EI 365. ODOR LINGERED AND BECAME ACRID, LIKE BURNING PLASTIC. AFTER LANDING ON GORILLA VI AT EI 365, 2 PASSENGERS IN THE AFT ROW OF SEATS SAID THEY SAW A LITTLE SMOKE AT THE FWD CABIN CEILING. SHUTDOWN AND CALLED MAINT. THE MECH REMOVED OVERHEAD INTERIOR PANELS AS REQUIRED AND FOUND STRONGEST ELECTRICAL TYPE ODOR COMING FROM ROLL PITCH AND YAW ACTUATOR AREA. NO BURNING SIGNS NOTICED, ALL SYSTEMS NORMAL. AC FLOWN TO BASE, FLIGHT NORMAL, AC RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20031117000762003111700076SW 2003 11 17 ALG2003F00087 120030825A7712222375177119 TRANSMITTER BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE FAILED E ALGAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03497AL 53172 CAE847053 IN LEVEL FLIGHT, CHECK INSTRUMENT LIGHT ILLUMINATED, I TOOK POWER AWAY AND THE LIGHT WENT OUT. CHECK INSTRUMENT LIGHT ILLUMINATED AGAIN AND THE TORQUE GAUGE CYCLED FROM ZERO TO PEGGED OUT. EXCEDANCE SHOWED 63 PERCENT OVER TORQUE. LOWERED TEMP TO 200 DEGREES BELOW NORMAL AND RETURNED TO INTRACOASTAL. MADE MINIMUM POWER LANDING. THE MECHANIC REPLACED TORQUE TRANSMITTER AND TORQUE INDICATORS. THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20031117000772003111700077NM 2003 11 17 DHL2003749509 120030920A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C CHECK, PIT FLOOR SUPPORT FROM STA. 950E TO STA. 990 LBL 18 HAS SEVERAL DENTS. REMOVED AFT. CARGO PIT SUPPORT FROM STA. 950E TO 990 LBL 18 I.A.W. B-727 SRM 51-30-2. 2) DRILLED NEW FLOOR SUPPORT P.O.NR 328319, P/N BAC 1500-6199 DIM. 5', 10 INCHES IAW SAMPLE I.A.W. B-727 SRM 51-20-2. 3) ALODINED AND PRIMED I.A.W. B-727 SRM 51-10-2. 4) INSTALLED NEW FLOOR SUPPORT I.A.W. B-727 SRM 51-30-2. 2L73 4F RTA3WE 20031117000802003111700080NM 2003 11 17 P5CA0300959 120031004A5511 RIB BOEING747 7472U3B 1384846NM HORIZONTAL STAB DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23923FT 22769 LT HORIZONTAL STABILIZER RIB CRACKED STABILIZER L/E STA 285 - 4 INCH CRACK. REMOVED LT HORIZONTAL STABILIZER DUE TO FOUND DENTED & REPAIRED RIB (4 INCH CRACK) AT LEADING EDGE STA 285. 2L74 4F RTA20WE 20031117000882003111700088CE 2003 11 17 ALG2003F00094 120030913A6340 CHIP DETECTOR CESSNASTC STC206C 1182107CE ALLSN 250C 250C28B 03013GL TRANSMISSION MALFUNCTIONED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03206SL 45245 CAE860023 DURING TAKE-OFF, THE TRANSMISSION CHIP LIGHT ILLUMINATED. RETURNED TO BRA7. PILOT PULLED, INSPECTED AND CLEANED CHIP PLUG. LEAK CHECKED AND GROUND RAN IAW OPS MANUAL. NO DEFECTS NOTED. 1H71 3O3 UNTA4CE E1GL 20031118000032003111800003NM 2003 11 18 CALA0300577 120031007A5347 SEAT TRACK BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND RT IB CABIN SEAT TRACK CORRODED AT STA 916-935. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204. 2L72 4F4 FRTA16WE E2GL 20031118000092003111800009NM 2003 11 18 UPS03241356 120030915A5754 RIB BOEING727 7271A7C 13840X2NM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 INSPECTION TYPE: C, NR 6 SLAT RIB 2ND FROM O/B END CRACKED AT AFT END. REPAIR CARRIED OUT IAW SRM 57-50-03 FIG 9. 2L73 4F A3WE 20031118000122003111800012WP 2003 11 18 UPS03841335 120031002A33506012235 LIGHT DOUG DC8 DC873F 302199FWP COCKPIT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01840UP 46140 EMERGENCY LIGHTS WILL NOT TEST. REMOVE AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW 33-50-01-2 OPS CK OKAY. P/N 60-1223-5, S/N 322 OFF, P/N 5708458-503, S/N FTL010 ON. 2L74 4F RT4A25 20031118000212003111800021EU 2003 11 18 MALA030445 120031004A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING LC1 NOTED ALL EMERGENCY LIGHTS AFT OF WINGS WOULD NOT STAY ON. MAINTENANCE REPLACED POWER SUPPLY 24W. OPS CHECK GOOD. P/N 3301-51, S/N OFF 1318, S/N ON 2087. 2L72 4T RTA52EU 20040129001122004012900112SO 2004 1 29 DHL200374248 120031216A5260 STEP PIPER PA18 PA18150 7101828SO AIRSTAIR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742 188146 DURING C-CHECK, RIGHT AFT AIRSTAIR STEP SUPPORT AT STEP 10 FROM THE BOTTOM IS CORRODED. REMOVED DAMAGED ANGLE FROM RT AFT AIRSTAIR NR 10 STEP AND FABRICATED NEW ANGLE FROM 60-3783 PO 3348236 DIM 9 X 2 INCH IAW B727 SRM 51-40-4 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED NEW ANGLE IAW B727 SRM 51-30-2. 1H71 3O 1A2 20040129001152004012900115EA 2004 1 29 COMA0460003 120031224A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01991CA 7216 FLIGHT 5230 NLG FAILED TO EXTEND, USED EMERGENCY RELEASE SYSTEM. COULD NOT DUPLICATE. REPLACED NLG PRIORITY VALVE FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20040129001422004012900142NM 2004 1 29 MWEA040003 120031219A5321995252184 FLOOR PANEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CABIN RIGHT OUTBOARD FLOOR PANEL LOCATED BETWEEN STATION 256 AND 313 HAS CORROSION ON FORWARD END. FABRICATED AND INSTALLED NEW PANEL AND FILLER. INSTALLED NEW HAT CHANNEL. 2L72 4F RTA6WE 20040129001542004012900154NM 2004 1 29 2003UALA00987 120031223A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STRINGER TIES ARE CRACKED AT BS 706 S11R BS 440 S16R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER TIES. 2L72 4F4 FRTA16WE E2GL 20040129001622004012900162CE 2004 1 29 DXTA200300202 120031215A3242 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07344QS 5600344 ON LANDING, PILOT’S FELT BRAKES WERE HARD WITH LITTLE OR NO BRAKING, TRANSFERRED BRAKES TO CO-PILOT, HAD HARD BRAKES THEN THE BRAKES STARTED TO WORK ON THE ROLL OUT. BRAKES WERE NORMAL DURING TAXI. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040129001802004012900180NM 2004 1 29 DHL2003753500 120031231A5320 ANGLE BOEING727 727223 1384074NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, NOSE LANDING GEAR W/W BOTTOM OF UPPER DECK STA 259 THRU PRESS ACCESS OPENING LBL 8 END OF ANGLE IS CRACKED AT FASTENER. REMOVED FASTENERS AND CRACKED ANGLE IAW B-727 SRM 51-30-2. FABRICATED ANGLE AS PER EXAMPLE, MATERIAL USED 2024-T3 .040 PO 900489 DIMENSION 10 X 1.5 INCH IAW B-727 SRM 51-20-1 AND 51-10-1. ALODINED AND PRIMED NEW ANGLE IAW B-727 SRM 51-10-2. INSTALLED FABRICATED ANGLE AT NOSE W/W COCKPIT FLOOR IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040130000092004013000009NM 2004 1 30 SWAA032840 120031230A53306545772 STRAP BOEING737 7373H4 1384600NM FUSELAGE SKIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN STRAP CRACKED AT BS 908, STR 4L. REPAIRED STRAP PER SRM. 2L72 4F RTA16WE 20040130000112004013000011NM 2004 1 30 SWAA032842 120031230A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, LBL 20 TO LBL 32. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040130000132004013000013 2004 1 30 SWAA032806 420031224A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 R2 DOOR EVACUATION SLIDE IS OUT OF ADJUSTMENT. ADJUSTED R2 SLIDE PER MM. 2L72 4F A16WE 20040203000912004020300091WP 2004 2 3 ASAA0380792 120031119A532199365841 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS EDGE DAMAGE AT FS 256-313. REPLACED FLOORBOARD IAW SRM 53-05. (M) 2L72 4F RTA6WE 20040203003332004020300333EA 2004 2 3 MASA200300498 120031217A2621 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY DISCHARGED A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW077305V 7305 ASH 6146 COS-LAS, RETURNED TO GATE DUE TO A CARGO BOTTLE LOW MSG. MX INSPECTED CARGO COMP AND FOUND NO EVIDENCE OF FIRE SUPPRECSENT. MX PERFORMED AN OPERATIONAL CHECK. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040204000142004020400014NM 2004 2 4 C1HA200394046 120031130A3350 BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 4. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-22 ALL OPS NORMAL. 2L73 4F A3WE 20040204000722004020400072CE 2004 2 4 55100AMWA 120031010A32401143880251 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07142YV UE142 DURING TAXING IN FROM FLT 701 ABQ TO FMN. THE RT BRAKE PEDAL WAS SOFT AND MUSHY DURING THE TAXI. RT BRAKE PEDAL FEELS MUSHY/RT BRAKE IS GRABBING P/N1143880251, APR89-594 WHEEL ASSY MAIN(ABS P/N 5006028). 2L72 4T RTA24CE 20040204000912004020400091SO 2004 2 4 SWIA200312507 120031014A27203211001003 PCU EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RUDDER MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DEDESCENT 1 NM07189SW2390 2390 120048 WHILE IN DESCENT AT 250KTS, UNABLE TO TRIM THE AIRCRAFT WITH THE RUDDER TRIM. TURNED OFF A/P AND YAW DAMPER, STILL NO GOOD. TURNED OFF BLUE SYSTEM HYDRAULICS AND IT WORKED. REMOVED AND REPLACED RUDDER PCU IAW MM 27-22-01. OPS CHECKS AND LEAK CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040204000942004020400094NM 2004 2 4 NACA20030117 120031021A5270 SWITCH BOEING727 72723 1384004NM PWA JT8 JT8D* NE CARGO DOOR LOOSE A NACAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL03992AJ 19428 MAIN CARGO DOOR UNLOCKED LIGHT ILLUMINATED ON TAKE OFF ROLL. FOUND TWO LATCH INDICATOR SWITCHES LOOSE WHILE LATCHED. TIGHTENED SWITCHES AND ROLLER CONTACTOR, OP CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040106002032004010600203WP 2004 1 6 GTIA030977 120031115A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 6 INCHES RBL - 6 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20040108000822004010800082EU 2004 1 8 DXJ2003F00000 120030115A5541423026402 RIB ISRAEL1124 1124 4500102EU GARRTTTFE731TFE731* 01518WP RUDDER CRACKED E DXJRO OTHER O OTHER NRNOT REPORTED 1 EA1110MV 7088 300 RUDDER OF A/C WAS REMOVED FOR REPAIRS DUE TO CRACKS FOUND BY X-RAY INSP IAW INSTRUCTIONS IN SB. X-RAY INSP REVEALED APPROX 30 CRACKS OF INTERNAL RIB RIVET HOLE DIMPLES AT VARIOUS RIB LOCATIONS THROUGHOUT RUDDER ASSY. UPON DISASSEMBLY OF RUDDER, A VISUAL INSP OF INTERIOR OF RUDDER REVEALED THAT OVER 80 PERCENT OF DIMPLES IN RUDDER RIBS WERE CRACKED(OVER 125 CRACKS WERE NOTED). NUMEROUS DIMPLE HOLES EXHIBITED MULTIPLE CRACKS, SOME EXTENDING WELL BEYOND DIMPLED AREA. THESE CRACKS WERE NOT DETECTED BY X-RAY INSP. CRACKS FOUND IN RIBS, SAME NATURE WERE ALSO FOUND BY VISUAL INSP IN AFT SPAR AND UPPER AND LWR END CAPS. THESE LOCATIONS WHERE CRACKS WERE FOUND WERE NOT REQUIRED TO BE X-RAY INSPECTED IAW SB. 2M72 4F4 F A2SW E6WE 20040108001012004010800101EU 2004 1 8 KBM2003F00051 120031009A6420350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR YOKE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 T/R YOKE SPHERICAL LAMINATES SPLIT AND WORN. REPLACED WITH NEW TAIL ROTOR HINGE LAMINATES. 1G71 3U3 U H9EU E19EU 20040108001202004010800120NE 2004 1 8 UO22003F00009 220031003A727030607424 DUCT AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE NR 2 ENGINE CRACKED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL192425 3617 32 P112205 NR 2 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 OCLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAL MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K) 2L73 4F4 FRTA46EU E1NM 20040108001392004010800139EU 2004 1 8 KBM2003F00073 120031020A6710XEMRE8RSA8 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE M/R PITCH LINK WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 UPPER END BEARINGS WORN BEYOND LIMITS. REPLACED WITH NEW UPPER END BEARINGS.(K) 1G71 3U3 UNCH9EU E19EU 20040109000072004010900007EU 2004 1 9 CDN2003F00000 120031017A31106226342024 DISPLAY BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE731* 01518WP COCKPIT FAILED E CDNAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA0573WF NA0429 EFD FAILED, CAUSING SMOKE IN COCKPIT DURING FLT. CRT WENT BLACK, SPECIFIC PART THAT BURNED IS UNKNOWN. 2L72 4F4 FRTA3EU E6WE 20040112000332004011200033EA 2004 1 12 A6WA200340174 120031118A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 TEMPORARY REPAIR ON RT FORWARD FUSELAGE SKIN JUST FORWARD OF FS 202.75 BULKHEAD, DENT 4 INCH LOG BY .062 INCH DEEP, TEMP REPAIR WS PERFORMED PER REO 601R-53-11-327. COMPLIED WITH STEPS 1 THROUGH 3 OF WVAC EO NR 601R-53-4413. PERFORMED EDDY CURRENT INSPECTION TO COMPLY WITH STEP 24 OF WVAC EO 601R-53-4413 OF RIGHT FWD FUSELAGE REPAIR. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 5 AND 6 OF WVAC EO 601R-53-4413. (M) 2L72 4F RTA21EA 20040112000352004011200035SO 2004 1 12 MASA200300461 120031122A2740 PITCH CONTROL EMB 145 EMB145LR 3260212SO HORIZ STAB MALFUNCTIONED A MASAD RETURN TO BLOCK F FLT CONT AFFECTED CLCLIMB 1 SW07840MJ 145429 ASH 2972 PHL, AIRCRAFT RETURNED TO FIELD FOR BACK-UP PITCH TRIM FAILURE IN-FLIGHT. MX RESET SYSTEM IAW FAULT ISO MAN AND OP CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040112000442004011200044 2004 1 12 03353634 420031219A22116229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS FAULTY A VTZAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 EA27634BR 7287 DURING AIRCRAFT OPERATION THE CREW REPORTED UNCOMMANDED RUDDER MOVEMENT. THE FLIGHT CONTROL COMPUTER WAS IDENTIFIED AS THE SOURCE OF THE PROBLEM AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000622004011200062WP 2004 1 12 GTIA030999 120031113A53219936639413 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND CABIN CENTER FLOOR SUPPORT PANEL MISSING EDGE FILLER, TWO METAL SIDE SUPPORTS CRACKED, BAD INSERTS STATION 807-886. FABRICATED NEW CABIN CENTER FLOOR PANEL. (M) 2L72 4F A6WE 20040112000812004011200081NM 2004 1 12 AWXA200301571 120031209A5321D5367180500500 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT LOWER SURFACE OF FLOOR PANEL 262FF. MAINTENANCE REMOVED CORROSION AND TRIMMED AWAY CORRODED AREA ON AFT LOWER SURFACE OF FLOOR PANEL 262FF; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 25-5302-03353-TB3. 2L72 4F RTA28NM 20040112001022004011200102SO 2004 1 12 C2XA03SH512 120031223A532014521725015 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040112001122004011200112EA 2004 1 12 RU3A03015 120031010A29106017523812 TUBE CNDAIRCL600 CL6002B16 1900305EA HYD SYSTEM CRACKED A RU3AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2187 5190 NR 1 HYDRAULIC SYSETM FAILED IN FLIGHT WITH COMPLETE LOSS OF FLUID WITHING THAT SYSTEM. FOUND HYDRAULIC LINE WITH CRACK AT BEND RADIUS. REPLACED HYDRAULIC LINE. ALSO, REPLACED HYDRAULIC PUMP AND FILTERS DUE OT LOSS OF FLUID. (M) 2L72 4F RTA21EA 20040112001202004011200120WP 2004 1 12 AALA20031246 120031110A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21961TW 53611 SEA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS DRIVEN BY B5-106 AND B5-107 EMERGENCY LIGHT BATTERIES INOPERATIVE. REPLACED BOTH B5-106 AND B5-107 BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20040112001292004011200129EA 2004 1 12 A6WA200340188 120031208A5753 VANE CNDAIRCL600 CL6002B19 1900309EA TE FLAP CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 RIGHT INBOARD FLAP VANE LEADING EDGE IS CHAFED 3 PLACES, WS 56.177= .004 INCH DEEP, WS 104.429= .003 INCH DEEP AND WS 140.364 = .003 INCH DEEP. BLENDED DAMAGE AREAS, RESTORE FINISH AND APPLIED TEFLON FILLED ABRASION RESISTANT COATING IAW BOMBARDIER, INC REO 601R-57-52-004 REV B. (M) 2L72 4F RTA21EA 20040204001202004020400120EU 2004 2 4 MALA030471 120031016A3510 OXYGEN BOTTLE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CREW SYSTEM LOW A MALAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL15435XJ 340B435 AFTER TAKEOFF ON FLIGHT NR 3068, CREW 02 LOW MASTER CAUTION ILLUMINATED . AIR RETURN TO TRI. MAINTENANCE SERVICED 02 TO REQUIRED LEVEL CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20040204001222004020400122EU 2004 2 4 MALA030475 120031014A3397 WIRE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE TAXI LIGHTS ARCED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15513XJ E2329 ARCING WIRE ABOVE PANEL (PRINTED CIRCUIT BOARD) AT BUNDLE ON TO PANEL CORNER. ARCING WIRE ABOVE PANEL (PRINTED C/B PANEL AT BUNDLE ON THE IB CORNER. MAINTENANCE REPAIRED WIRE AS REQUIRED. WIRE NR LD003 FOR RT TAXI/LANDING LIGHTS OPS CHECK GOOD. 2H74 4F4 FRTA49EU E6NE 20040204001352004020400135NE 2004 2 4 0301959987 220031023A7261 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D15 52051NE NR 2 MAKING METAL A NWAAA UNSCHED LANDING KMJFLUID LOSS OVER TEMP WARNING INDICATION CRCRUISE 1 GL01987US46765435 47458 700628A DURING CRUISE FLIGHT, NR 2 ENGINE OIL QUANTITY WENT TO ZERO, OIL TEMP CLIMBED INTO THE RED ZONE. THE NR 2 ENGINE WAS SHUT DOWN. FLIGHT CREW DIVERTED AIRCRAFT TO MBS AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND METAL IN THE OIL FILTER AND ON THE CHIP DETECTORS. REPLACED THE NR 2 ENGINE. 2L72 4F4 F A6WE E2EA 20040204001382004020400138NM 2004 2 4 EIA2003120 120031002A2697 CIRCUIT CARD BOEING747 747132 1384882NM FIRE DECTECT SYSFIRE A EIAAA UNSCHED LANDING BAGSMOKE/FUMES/ODORS/SPARKS FLAME/FIRE MULTIPLE FAILURE CRCRUISE 1 NM09479EV 19898 WHILE AT CRUISE, FL 400, THE RT WING OVHT LIGHT ILLUMINATED. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST. THE NR 3 AND NR 4 FIRE LOOPS FAILED FIVE MINUTES LATER. DISPATCH AND TECH CENTER NOTIFIED. AN ACRID ODOR WAS DETECTED BY THE CREW, SHORTLY AFTER THIS. SMOKE WAS SEEN COMING FROM BEHIND THE P-6 CIRCUIT BREAKER PANEL, FOLLOWED BY A SMALL FIRE IN THE FIRE DETECTION CARD FILE. THIS SDR TO REMAIN OPEN UNTIL CAUSE IS DETERMINED. 2L74 4F A20WE 20040204001432004020400143NM 2004 2 4 EIA2003131 120031020A5420 WEB BOEING747 747212B 1384886NM PWA JT9 JT9D* NE NR 1 PYLON CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 NR 1 PYLON LOWER WEB CRACKED AT NAC STA 210 LT SIDE AFT OF STIFFER FOR PNEU. DUCT. STOP DRILLED CRACK AND FABBED AND INSTALLED REPAIR PLATE AND FILLERS IAW B747 SRM 54-10-03 FIG 2 2L74 4F4 F A20WE E20EA 20040204001602004020400160NM 2004 2 4 AWXA200301332 120031008A53206545855 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 LCQ - MAJOR REPAIR - DURING -15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT R-2 DOOR BS 986, RBL 55. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT FROM BS 937 TO BS 1006, RBL 55; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51, PG. 105, FIG. 101. 2L72 4F RTA16WE 20040204001622004020400162 2004 2 4 751PA0024 420031025A256569B148551 SPRING BOEING757 757200 1384950NM RROYCERB211 RB211* 54555NE GIRT BAR FAILED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05751PA 23928 L1, R1, AND L4 DOOR GIRT BAR LEAF SPRINGS FAILED INSPECTION IAW MM-7200-03-00917 AND PACE MO NR B757-52-21003. REPLACED LEAF SPRINGS IAW MM 25-66-14. 2L72 4F4 FRTA2NM A12EU 20040204001692004020400169CE 2004 2 4 GLBA2003139 120031029A77203034857 CONTROLLER BEECH 1900 1900D 1154162CE ENG TEMP FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0396UX UE96 BOTH ENG TEMP LIMITED, CALIBRATED LT TRIM STICK AND REMOVED AND REPLACED RT TRIM STICK. 2L72 4T RTA24CE 20040204001852004020400185WP 2004 2 4 P8UF200300002 120031104A2612ASL0163511 FIRE LOOP DOUG DC10 DC1030 3023501WP NR 3 ENGINE CHAFED W P8UFEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO23833LA 46937 AFTER 30 MINUTES OF TAKE OFF DURING CLIMB FIRE WARNING ON ENGINE NR 3, REDUCED POWER AND WARNING SOUND AND LIGHT OFF. IAW OPERATIONAL PROCEDURES, AIRCRAFT RETURN TO DEPARTURE POINT. LINE MAINT. FOUND UPPER LOOP SENSOR CHAFING WITH PYLON. CORRECTIVE ACTION: REPOSITIONED LOOP AND ACCOMPLISHED ENGINE RUN UP IAW AMM 71-00-00 AND TAFI 26-11-00 2L73 4F A22WE 20040210000222004021000022WP 2004 2 10 UPS03841596 120031113A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, RT WING LE UPPER SKIN IS CRACKED AT XFS 304. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. SRM.57-2-1 FIG. 38 2L74 4F RT4A25 20040210000382004021000038WP 2004 2 10 UPS03841616 120031118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 1750 LONGERON 14L IS CRACKED. REMOVED DAMAGED LONGERON SECTION STA 1736 TO 1760, FABRICATED AND INSTALLED REPLACEMENT SECTION AND STRAPS IAW SRM. 53-2-2 FIG. 10. 2L74 4F RT4A25 20040210001052004021000105EU 2004 2 10 USAA030274 120031206A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED 1 SQUARE INCH BY .060 INCH DEEP, AT LBL 17.75, FRAME 57.2. REPLACED SEAT TRACK SECTION PER SRM 53-00-15 FIG 101. (M) 2L72 4F RTA46NM 20040210001242004021000124CE 2004 2 10 WK92003F00000 120031120A5260NAS110321D BOLT BEECH 300 300BEECH 1152930CE PWA PT6 PT6* 52043EA FWD LATCH HOOK SHEARED E WK9AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO14917WA FA77 DURING CRUISE FLIGHT AT ATTITUDE, CABIN ALTITUDE BEGAN TO CLIMB AS CABIN PRESSURE WAS LOST. A NOISE WAS OBSERVED AT CABIN AIRSTAIR DOOR. FLIGHT WAS CONTINUED AT A LOWER ALTITUDE WHERE PRESSURIZATION WAS NOT REQUIRED. UPON REACHING DESTINATION, DOOR WAS DISASSEMBLED AS NECESSARY TO EVALUATE DAMAGE. FORWARD LATCH HOOK LINKAGE BOLT PN NAS1103-21D WAS FOUND TO BE SHEARED AND SEPARATED FROM BRACKET PN 50-430062-19. INSPECTION OF BOLT INDICATED A CRACK HAD FORMED PREVIOUSLY AND ALLOWED FURTHER DETERIORATION OF THE BOLT CROSS-SECTION. THE RESPECTIVE BOLT ON AFT LATCH HOOK WAS INSPECTED BY MAGNAFLUX METHOD WITH NO CRACKS INDICATED. BOTH BOLTS WERE REPLACED WITH NEW PN NAS6203-21D BOLTS AND PN 130909N15 NUTS. 2L72 4T3 T A24CE E2NE 20040211000112004021100011NM 2004 2 11 USAA030316 120031125A5414 SKIN BOEING737 737401 1384701NM NR 1 NACELLE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US39263 23990 FOUND SKIN CRACKED 1 INCH, NR 1 ENGINE PYLON PANEL 5727L. INSTALLED DOUBLER PER TR 54-30-07. (M) 2L72 4F RTA16WE 20040211000442004021100044WP 2004 2 11 AMTA200301437 120031129A5210 SOLENOID LKHEED1011 10113853 5265020WP L2 DOOR LOCK FAILED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND L2 DOOR WILL NOT FULLY CLOSE. REMOVED AND REPLACED L2 DOOR LOCK MECHANISM SOLENOID IAW AMM 52-12-25. OPS CHECK NORMAL. (M) 2L73 4F A23WE 20040212000592004021200059 2004 2 12 AK02003F00002 420030829A25624520133 BATTERY CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO MCAULYD3A34 D3A34C402 GL ELT INOPERATIVE B AK0MO OTHER O OTHER NRNOT REPORTED 1 AL036192U199 01221 U20605377 283227R 951527 DURING AN ANNUAL INSPECTION OF THE ELT UNIT, THE ELT WAS FUNCTIONAL CHECKED BY THE REMOTE SWITCH ON THE PANEL. THERE WAS NO LED LIGHT INDICATION WHEN SWITCHED TO THE ON POSITION. THE ELT UNIT WAS REMOVED FROM THE AIRCRAFT AND TESTED AGAIN, THE UNIT WAS INOPERATIVE. THE BATTERY PACK WAS DISCONNECTED AND CHECKED WITH A VOLTMETER. VOLTAGE WAS NOT PRESENT AT THE CONNECTION PLUG POWER TERMINAL END. THE BATTERY PACK POWER AND GROUND ARE ROUTED THROUGH A CIRCUIT BOARD GLUED INSIDE OF THE HOUSING, ONE OF TWO FUSES SOLDERED ON THE BOARD TESTED (OPEN). CAUSE UNKNOWN (AL03200320188) 1H71 3O3 O A4CE E8CE 5 CP47GL 20040212000702004021200070NM 2004 2 12 HNAA0300077 120031205A5313 STRINGER DHAV DHC8 DHC8102 2809003NM FUSLEAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07914HA 53 DURING C-CHECK, FOUND CORROSION ON STR 31S THAT REQUIRED REMOVAL AND REPLACEMENT OF STR. FRAME SEGMENT AT X291 REMOVED TO FACILITATE INSTALLATION OF REPLACEMENT STR SECTION. IAW EO8-53-03-1062 2H72 4T RTA13NM 20040212000752004021200075NM 2004 2 12 F3LA200300167 120031205A5347 GALLEY TRACK BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON GALLEY TRACK, STA. 344, LBL 20-23. REPAIRED GALLEY TRACK IAW SRM 53-00-52. 2L72 4F RTA16WE 20040212000952004021200095NM 2004 2 12 EIA2003167 120031205A3320 SIGN BOEING747 747273C 1384896NM PWA JT9 JT9D* NE CABIN SHORTED A EIAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09471EV 20651 ON DECENT TO JFK, FASTEN SEAT BELT SIGN TURNED ON AND OFF SMELLED SMOKE IN COCKPIT AND CIRCUIT BREAKER POPPED. TO REMAIN OPEN TILL FIX IS ACCOMPLISHED. 2L74 4F4 F A20WE E20EA 20040212001062004021200106WP 2004 2 12 DHL2003805013 120031211A2820 WARNING LIGHT DOUG DC8 DC873F 302199FWP FUEL TRANSFER ILLUMINATED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01805DH 46125 IN FLIGHT WHEN ATTEMPTING TO TRANSFER FUEL TO NR 3 TANK, NR 3 MAIN SHUTOFF LIGHT INITIALLY AND RE-ILLUMINATED IN FIVE SECONDS WITH FILL VALVE IN OPEN POSITION AS A RESULT FUEL CANNOT BE TRANSFERRED TO NR 3 TANK. ABNORMAL PROCEDURE COMPLETED DID NOT CORRECT PROBLEM. SUMPED NR 3 FUEL TANK. TRANSFER FUEL SHUT OFF LIGHT. OPS OK IAW M/M 28-21-00 IN OPEN OR CLOSE POSITION. 2L74 4F RT4A25 20040212001132004021200113SO 2004 2 12 IF12003F00001 120031205A2897430878091 PETCOCK KNOB GULSTMG1159 GIV 3980115SO RROYCETAY TAY6108 NE COCKPIT SHORTED E IF1AO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA23614RD4045 1006 PILOT DISCREPANCY, WARNING LIGHTS POWER NR 7 CIRCUIT BREAKER POPPED. FOUND LT HP FUEL COCK KNOB SHORTING TO LEVER ARM (HANDLE IS LIGHTED) KNOB WAS PROBABLY BROKEN BY TWISTING MOTION FROM PILOT WING STARTING OR SHUTTING DOWN ENGINE. NO RECOMMENDATIONS FOR PREVENTION OF REOCCURRENCE. 2L72 4F4 FRTA12EA E25NE 20040212001152004021200115NM 2004 2 12 ANCF200300028 120031211A324650078973 WHEEL DOUG MD80 MD83 3023681NM MLG FAILED W ANCFO OTHER O OTHER TXTAXI/GRND HDL 1 SO23593AN10847127 53093 AFTER VACATING THE RUNWAY THE AIRPLANE FELT LIKE SOME ONE WAS USING THE BRAKES UNTIL THE AIRPLANE COME TO A COMPLETE STOP. DURING INSPECTION WHEEL BEARING NR 2 WAS FOUND WITH DAMAGES (BLOCKED). THE MAIN WHEEL ASSY NR 2 WAS REMOVED AND REPLACED IAW A.M.M. 32-40-01 PAG202 P/N 5007897-3 S/N JUN88-0270 S/N MAR88-0074. BRAKE ASSY NR 2 WAS REPLACED IAW AMM 32-42-01 PAGE 202 AND PERFORMED THE ANTISKID TEST WAS PERFORMED IAW AMM 32-42-00 PAGE 202 P/N 5004565-3 S/N OFF JUN 88-0108 S/N ON JUN 89-0288 THE BRAKE TEMPERATURE SENSOR NR 2 WAS FOUND INOPERATIVE. IT WAS DEFERRED TO DMI 502 MEL 502 CAT (C). 2L72 4F RT 20040212001262004021200126WP 2004 2 12 ABXA030474 120031212A3260 PROXIMITY SENSOR DOUG DC8 DC863F 302198FWP MGL DIRTY A ABXAO OTHER N FALSE WARNING CRCRUISE 1 GL23811AX 46113 LANDING GEAR UNSAFE LIGHT ILLUMINATED IN CRUISE. NOT LATCHED LIGHT ON FLIGHT ENGINEER'S PANEL ILLUMINATED WITH SELECTION RT GEAR POSITION. PERFORMED ABNORMAL. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS CYCLED. MAINTENANCE FOUND RT MAIN LANDING GEAR DOOR NOT LATCHED PROXIMITY SWITCH SENSOR DIRTY. CLEANED PROX SWITCH SENSOR OF DIRT AND DEBRIS. PERFORMED OPERATIONAL CHECK OF MAIN LANDING GEAR DOOR PROX SWITCHES MM 32-60-00-2. ALL SYSTEMS CHECKED GOOD. 2L74 4F 4A25 20040212001282004021200128EU 2004 2 12 MALA030549 120031212A242051634002 GCU SAAB SF340 340B 7860101EU AC GENERATOR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15425XJ 340B425 DURING FLIGHT, RT AC GEN FAILED INFLIGHT. AIR RETURN TO MAINTENANCE, REPLACED RT AC GEN AND GCU ALSO OHMED WIRES BETWEEN GEN AND GCU AC GEN, OPS CHECK GOOD IAW SF3 MM CHAP 24, AND JC 242102. P/N 31342-003, S/N ON 1262. REPLACED RIGHT AC GCU P/N ON/OFF 51634-002, S/N ON 335, S/N OFF 97030. 2L72 4T RTA52EU 20040212001372004021200137NM 2004 2 12 DHL2003742518 120031119A5713 STRINGER BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 59874 CABIN STR 15L CRACKS STA 724D. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA AS REQUIRED FOR REPAIR IAW B-727 SRM 53-10-3 FIG 5. FABRICATED FUSELAGE STRINGER REPAIR 1 CHANNEL MAT USED 7075 T6 .040 PO 9912620 DIM 4.5 X 3 INCH AND TAPED FILLER AND RADIUS FILLER MAT USED 2024 T3 .080 PO 900103 IAW B-727 SRM 53=10-3 FIG 1. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. 2L73 4F A3WE 20040212001492004021200149NM 2004 2 12 ANCF200300029 120031216A4910 DUCT BOEING767 767* NM APU CONTAMINATED W ANCFO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO23421 25421 DURING CRUISE, BOTH RECIRCULATION FANS WERE TURNED OFF FOR AIR RECIRCULATION JUST AFTER THAT A ELECTRICAL SMOKE ODOR BEGAN IN ALL THE AIRPLANE IMMEDIATELY RECIRCULATION FANS WERE TURNED ON AND ODOR DISAPPEAR. WERE CHECKED FWD APU AIR DUCTS AND CHECK VALVE APU AIR AND FOUND OIL CONTAMINATION WERE CLEANED SYSTEM OIL CONTAMINATION IAW AMM 21-00-21 PAGE 201 AND ADDITIONAL WERE CHECKED PANELS 31, 32, 34, 35, 36 AND P37 AND FOUND IN NORMAL CONDITION IAW WDM 24-51-1324-21-11,21-45-11 AND 21-45-21. PACKS WERE OPERATE WITH APU AND ENG, AND NO ODOR TO OIL OR WIRE BURNED WERE DETECTED. 2L72 4F RTA1NM 20040212001562004021200156EA 2004 2 12 WVE2003F00024 120031207A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE LT ENG NACELLE LOOSE A WVERO OTHER O OTHER NRNOT REPORTED 1 EA09614QX 10049 LT ENGINE PYLON HAS A TOTAL OF 8 LOCK FASTENERS THAT ARE LOOSE. PYLON IS SUSCEPTIBLE TO STRESS AND VIBRATION FROM THE ENGINE. REMOVE EXISTING FASTENERS AND ENLARGE THE HOLES TO A .2606 INCH - .26636 INCH IN DIAMETER. INSTALL HST111AG8XX LOCK FASTENERS INTO THE ENLARGED HOLE USING HST1488TP8 COLLARS IAW EA R-54-42 AND EO 601R-54-4444 DATED 12/03/03. (EA09200401171) 2L72 4F4 FRTA21EA E15NE 20040212001572004021200157CE 2004 2 12 WVE2003F00025 120031203A5720232507913 SUPPORT BRACKET LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE LT WING CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09233FX 154 WHILE PERFORMING IRN 27-50-26 REPLACEMENT OF LT WING FLAP NOSE ROLLER ATTACHMENT FITTINGS, THE LT FLAP ACTUATOR UPPER ATTACHMENT BRACKET WAS FOUND TO BE CRACKED. THIS BRACKET IS LOCATED UNDER ACCESS PANEL 540EB WHICH IS NOT REQUIRED TO BE REMOVED FOR THE 1200 HR OR 2400 HR INSPECTION. PROBABLE CAUSE: UNKNOWN RECOMMENDATION: REMOVE PANELS 540EB ON LT WING AND 640 EB ON RT WING FOR INSPECTION OF BRACKETS EVERY 1200 HR INSPECTION. 2L72 4F4 FRTA10CE E35NE 20040212001592004021200159EU 2004 2 12 CX7A194J0355 120031221A27307255201601 ELEVATOR SAAB SF340 340B 7860101EU WING LOOSE A CX7AO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL03315CE 340B343 VIBRATION FELT ABOVE 230 KNOTS WORSE WITH AUTO PILOT ENGAGED. 2L72 4T RTA52EU 20040212001622004021200162EU 2004 2 12 MALA030558 120031215A3211 LANDING GEAR SAAB SF340 340B 7860101EU MAINS FROZEN A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15425XJ 340B425 DURING FLIGHT, GEAR INTRANSIT LIGHT STAYED ON AFTER GEAR RETRACTION. AIR RETURN TO MSP. MAINTENANCE REMOVED ICE BUILD-UP FROM ALL GEAR. JACKED AIRCRAFT AND CYCLED SYSTEM SEVERAL TIMES. OPS CHECKS GOOD. 2L72 4T RTA52EU 20040212001692004021200169NM 2004 2 12 2003UALA00972 120031218A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STA. 380 SRT 8L AND 9L HAS CRACKED SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20040212001732004021200173NM 2004 2 12 P5CA0301016 120031221A5230 SKIN BOEING747 7472U3B 1384846NM CARGO DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 MAIN DECK CRG DOOR FAILED TO CLOSE - DOOR SKIN DAMAGED. PERFORMED TIME LIMITED REPAIR TO DOOR IAW SL TLS-JFK 03-00243H AND SRM COI WAS ISSED AND DOOR DEFERRED ELECTRICALLY IAW DDPG. 2L74 4F RTA20WE 20040212001752004021200175NM 2004 2 12 AWXA200301586 120031206A53136545767512 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .2500 INCH CRACK WAS FOUND ON STRINGER 16 RT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE REMOVED DAMAGE FROM END OF STRINGER 16 RT AT BS 500C; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A RADIUS FILLER AND REPAIR CHANNEL; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5312-01019-DD1. 2L72 4F RTA16WE 20040329000252004032900025NM 2004 3 29 USAA030287 120031122A5347 SEAT TRACK BOEING737 737201 1384454NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19223US17500 21665 CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH AREA, FRAME 63 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F A16WE 20040401000162004040100016NM 2004 4 1 USAA030327 120031218A5347 SEAT TRACK BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 CLT - FOUND SEAT TRACK CORRODED 6 INCHES, STATION 1468, RBL 88. REMOVED CORROSION, ALODINED, PRIMED AND PAINTED PER SRM 53-00-52 FIG 101. (M) 2L72 4F RTA1NM 20031112000182003111200018NM 2003 11 12 2003UALA00823 120031030A2910 LINE BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 1 HYD SYSTEM LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29174UA 24381 NR 1 HYDRAULIC QUANTITY SYSTEM READ ZERO WITH NO PRESSURE. FOUND LT LCCA HYDRAULIC LINE LEAKING. REPLACED LINE WITH NEW MANUFACTURED LINE. RESERVICED NR 1 SYSTEM. LEAK CHECKED NEW INSTALLED LINE, CHECKED OK. 2L74 4F4 FRTA20WE E24NE 20031112000402003111200040CE 2003 11 12 DXTA200300157 120031106A3240 BRAKE ASSY CESSNA560 560XL 2076702CE MLG CONTAMINATED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07664QS 5605264 LEFT BRAKE PEDAL FLUCTUATES IN TRAVEL REQUIRED TO GET THE BRAKE TO APPLY. VERIFIED SQUAWK, ACCOMPLISHED BRAKE BLEEDING PER CESSNA 560XL MM CHAPTER 32-42-00. ACCOMPLISHED TAXI CHECKS FOUND BRAKE PEDAL ACTION EVEN, OPS CHECKED GOOD, NO DEFECTS NOTED. 2L72 4F RTA22CE 20031112000412003111200041NM 2003 11 12 373PA0023 120031107A3350873100212 LIGHT BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 LEFT OVERWING EMERGENCY EXIT LIGHT WILL NOT TEST. RIGHT OVERWING EMERGENCY EXIT LIGHT WILL NOT TEST. FORWARD RIGHT ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED LEFT OVERWING EXIT BATTERY PACK PER MM 33-51-01. REPLACED RIGHT OVERWING EXIT LIGHT ASSY AND FORWARD RIGHT ENTRY DOOR LIGHT ASSEMBLY PER MM 33-51-01. ALL TEST OK. 2L72 4F RTA16WE 20031112000632003111200063NM 2003 11 12 CALA0300627 120031107A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND WEB GOUGED IN PIT ON FORWARD CARGO DOOR JAMB AT S26R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-00. 2L72 4F RTA16WE 20031112000682003111200068NM 2003 11 12 CALA0300631 120031109A5345 MOUNT BOEING737 737824 13844BZNM G-2 GALLEY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718223 28932 INSPECTION FOUND AFT I/B G-2 GALLEY MOUNT CORRODED. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW ECRA 2531-01056. 2L72 4F RTA16WE 20031112000762003111200076NM 2003 11 12 AWXA200301399 120031022A783017310211 FAIRING BOEING737 737277 1384570NM THRUST REVERSER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 2 INCH CRACK WAS FOUND ON NR 1 THRUST REVERSER LOWER DEFLECTOR DOOR LT FAIRING AT 2ND FASTENER HOLE FROM FORWARD END. MAINTENANCE CUT OUT DAMAGE SECTION OF NR 1 THRUST REVERSER LOWER DEFLECTOR DOOR LT FAIRING; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-30-02 FIG 7 PG 1 AND 51-40-03 FIG 001 PG 1. 2L72 4F RTA16WE 20031112001082003111200108EU 2003 11 12 BAQA090677 120031028A28221176415103 PUMP BOLKMS117 BK117A1 5626010EU FUEL BOOST INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME3207 7243 FUEL BOOSTER PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031112001302003111200130NM 2003 11 12 UPS03641449 120031017A2780 CONTROL ROD BOEING767 76734AF 1385212NM L/E SLAT BROKEN A IPXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01322UP 27748 INSPECTION TYPE:N/A VIBRATION IN NOSE GEAR NOTED IN T/O. DURING FLAP RETRACTION W/ FLAP LEVER AT 1 RECVD EICAS MSG/LIGHT FOR LE SLAT ASSMY L/E LIGHT ILLUM WITH THE FLAP POINTERS CORRECT. DECLARED EMERGENCY AND REQUESTED THE RESCUE EQUIPMENT. FOUND BROKEN CONTROL RED AT SLAT NR 7 O/B POS BEAT AND REMOVED PER MM 27-81-01-4. INSTALLED CONTROL ROD AT NR 7 SLAT O/B ROD PER MM 27-81-01-4. OPS CHECKED GOOD. NO EICAS MESG AND NO FAULTS ON FSEU. 2L72 4F RTA1NM 20031112001332003111200133NE 2003 11 12 HEEA090146 120030930A32977655200904041 WIRE HARNESS SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL MLG DAMAGED E HEEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW031546G 760076 DURING APPROACH, DID NOT GET A GREEN LIGHT FOR NOSE GEAR. ABORTED LANDING. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED DOWN LOCK HARNESS. 1G72 3U3 U H1NE E1GL 20040108000982004010800098 2004 1 8 KBM2003F00048 420031006A34215040032902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 ATTITUDE INDICATOR FLUCTUATES AND SITS NOSE HIGH ABOUT 12 DEGREES IN FLIGHT. 1G71 3U3 U H9EU E19EU 20040109000212004010900021 2004 1 9 P9R2003F00001 420031104A2565 SLIDE BOEING757 757236 1384971NM RROYCERB211 RB211* 54555NE L1 DOOR DISLODGED A P9RAK NONE O OTHER ININSP/MAINT 1 SO11958PG 24118 L1 DOOR SLIDE-RAFT OUT OF CASING. INSTALLED L1 SLIDE-RAFT IAW BMM 52-11. HARNESS ASSEMBLY PN 416N25035.(K) 2L72 4F4 FRTA2NM A12EU 20040109000532004010900053WP 2004 1 9 GTIA031022 120031125A5315 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND PAX CABIN FLOORBEAM WEB CRACKED AT STATION 120 LBL 6. CUT OUT DAMAGED AREA. FABRICATED NEW WEB SECTION AND DOUBLER. INSTALLED NEW WEB SECTION AND DOUBLER. (M) 2L72 4F RTA6WE 20040112000062004011200006CE 2004 1 12 2004F00011 120030119A53121144100266 BULKHEAD BEECH 1900 1900C 1154161CE FUSELAGE CRACKED A YADAK NONE O OTHER ININSP/MAINT 1 AL031563C UC20 ON OPERATIONAL CHECK FLIGHT FOR PRESSURIZATION CHECKOUT, AIRCRAFT FAILED TO MAINTAIN MAXIMUM CABIN PRESSURE ON SINGLE ENGINE BLEED AIR. MAINT DISCOVERED MULTIPLE CRACKS ON FORWARD PRESSURE BULKHEAD, LOWER RT CORNER OF P/N 114-410026-6, WEB ASSY AT UPPER END OF STIFFENER P/N 114-410026-55 AND AT STA 84. THIS CRACK WAS APPROX 7 INCHES LONG. AN ADDITIONAL CRACK WAS DISCOVERED THAT RAN ALONG UPPER JOGGLE OF P/N 114-410026-6. THIS CRACK WAS ALSO APPROX 7 INCHES LONG. BOTH CRACKS WERE THEN REPAIRED IAW B1900C STRUCTURAL REPAIR MANUAL WITH A SINGLE SURFACE PATCH. ANTICIPATE FINDING THAT THERE WAS A RIVET MISSING AT MANUFACTURE THAT WOULD ATTACH PIN 114-410026-23 STIFFENER TO ANGLE P/N 114-410026-9. (M) 2L72 4T RTA24CE 20040112000432004011200043EA 2004 1 12 033286252 120031124A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE GOUGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING HEAVY CHECK A GOUGE WAS FOUND ON THE FUSELAGE SKIN BETWEEN STRINGERS 21 AND 22. THE GOUGE WAS 5 INCHES LONG BY 2.5 INCHES WIDE, WITH A 4 INCH CREASE IN SKIN AND MEASURED .090 IN DEPTH. THE REPAIR WAS MADE IN ACCORDANCE WITH SRM PROCEDURES AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000882004011200088NM 2004 1 12 AWXA200301578 120031203A5320651758267 WEB BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD VERTICAL BEAM WEB AT BS 181, RBL 17.1, WL 182. MAINTENANCE REMOVED DAMAGED AREA OF VERTICAL BEAM WEB AT BS 181, RBL 17.1, WL 182; FABRICATED NEW REPLACEMENT SECTION OF WEB AND A SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08 FIG 212, SHEETS 1-8. 2L72 4F RTA16WE 20040112001052004011200105NM 2004 1 12 MWEA030495 120031220A2432888703 CHARGER BOEING717 717200 1383700NM NR 2 ENGINE FAILED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31910ME 55174 ENGINE STARTED AND GENERATOR CAME ON LINE ALERTS BUS TIE LEFT AND RIGHT LOCKOUT EMERGENCY POWER ON BUS AC GROUND SPEED OFF ILLUMINATED. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER. 2L72 4F TRA6WE 20040112001762004011200176 2004 1 12 03FDEA02234 420031223A344146160008000801 IRU AIRBUS310 A310 EU E/E BAY MALFUNCTIONED A FDEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO25451FE3275610 303 NR 1 ATT ON PFD FROZEN, NR 1 FD FAILED, NR 1 A/P & NR 1 YAW DAMPER TRIPPED. SUSPECT NR 1 ADC FAILED. ON SHUTDOWN IRS MONITOR SHOWED NR 1 IRU, FOR DRIFT & GS. REMOVED AND REPLACED NR 1 ADC IAW MM 34-11-34-4. TESTED PER 34-10-00 P BLOCK 501. REMOVED AND REPLACED NR 1 IRU IAW MM 34-25-34-4. TESTED PER 34-25-34-5. AFS & LAND TEST PERFORMED PER MM 22-40-00-5. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 461600-0800-0801, POS 1 SRL 0033, TAG 998311. 2L72 4F RTA35EU 20040113000332004011300033EU 2004 1 13 BAQA091749 120031213A6720741C000005 ACTUATOR BOLKMS117 BK117A4 5626017EU TAIL ROTOR LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA039024Z5360 7134 ACTUATOR LEAKING HYD FLUID FROM WEEP HOLE OVER DATA PLATE. PART REPLACED WITH SERVICABLE UNIT. 01/07/2004 1G72 3U H13EU 20040113000472004011300047EA 2004 1 13 COMA0360565 120031218A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA OXYGEN SERVICE OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01918CA 7018 FLIGHT 5400 STALL FAIL WARNING AFTER T/O. LOUD BUZZ FROM NOSE AREA. FOUND 02 SERVICE DOOR OPEN. CLOSED SERVICE DOOR. 2L72 4F RTA21EA 20040113000482004011300048EA 2004 1 13 COMA0360566 120031220A3040601R3303312 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01920CA11442 7022 FLIGHT 5808 RT WINDOW HEAT CAUTION MESSAGE. REPLACED CO-PILOTS SIDE WINDOW. 2L72 4F RTA21EA 20040113000492004011300049EA 2004 1 13 COMA0360567 120031220A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION ININSP/MAINT 1 SO01810CA 7370 FLIGHT 5825 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031117000372003111700037SO 2003 11 17 C2XA03TY173 120031005A531514521699001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712540 145537 DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04/05/06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20031117000442003111700044NM 2003 11 17 2003UALA00736 120031002A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 AFT PIT STA 1540 LT SIDE FLOORBEAM, STIFFENER IS CRACKED BELOW L-2 DOOR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW STIFFENER. 2L72 4F4 FRTA1NM E24NE 20031117000462003111700046NM 2003 11 17 03FDEA01607 120030916A5753ARC050213 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OB FLAP IB HINGE, WING MOUNTED; LOWER OB ATTACH HOLE FOUND CORRODED AT BORE AND FWD/ AFT FACES. LT OB FLAP IB HINGE, WING MOUNTED LOWER OB ATTACH HOLE REPAIR CARRIED OUT IAW CMM 57-44-08, FWD / AFT FACES CORROSION REMOVED AND FOUND WITHIN LIMITS IAW DWG ARC0502. 2L73 4F RTA22WE 20031117000482003111700048WP 2003 11 17 CALA0300573 120031004A5310 DOOR FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714831 49491 INSPECTION FOUND MID BAGGAGE BIN LOWER DOOR JAMB CORRODED. A SPACER WAS FABRICATED AND INSTALLED IAW SRM 53-05. 2L72 4F4 F A6WE E2EA 20031117000512003111700051NM 2003 11 17 CALA0300576 120031003A5230 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 THE FORWARD CARGO DOOR INNER SKIN WAS FOUND WITH THREE EXISTING REPAIRS AND ADDITIONAL DAMAGE TO THE INNER SKIN WHILE AIRCRAFT WAS IN 4C CHECK AT HOU. THE THREE SMALL REPAIR DOUBLERS WERE REMOVED. ONE REPAIR DOUBLER INCORPORATING THE PREVIOUS REPAIRS AND THE DAMAGE FOUND DURING THIS CHECK WAS INSTALLED IAW ECRA 5232-01035. 2L72 4F4 FRTA16WE E2GL 20031117000592003111700059NM 2003 11 17 DHL2003749504 120030918A5230MS2000116 HINGE BOEING727 727200 138407ENM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK, MAIN CARGO DOOR AFT HINGE IS CRACKED (MARKED). REMOVED DAMAGED SECTION AND INSTALLED NEW HINGE SECTION 18 INCHES LONG. 2L73 4F RTA3WE 20031117000932003111700093SW 2003 11 17 ALG2003F00098 120030625A7712407375003107 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE MALFUNCTIONED E ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW03507AL 53103 ON TAKE OFF, DURING CLIMB THE TORQUE INDICATION WENT TO 103 PERCENT FOR 3-5 SECONDS AND (CHECK) INSTRUMENT LIGHT ILLUMINATED. TORQUE WAS REDUCED TO 93 PERCENT WITH MGT OF 650 DEGREES. CLIMB SPEED WAS 500 FPM, AIRCRAFT WAS RETURNED TO BASE. THE MECHANIC TROUBLESHOT THE SYSTEM WITH THE MAINTENANCE COMPUTER, REMOVED AND REPLACED THE TORQUE INDICATOR AND PRESSURE TRANSMITTER. AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20031118000012003111800001WP 2003 11 18 MWEA030411 120031007A5347593056675 SEAT TRACK DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 LOWER SIDE OF NR 2 SEAT TRACK IS CORRODED AT NUTPLATE, APPROXIMATELY STATION 1268. REMOVED AND REPLACED REPAIR PLUG. 2L72 4F4 F A6WE E2EA 20031118000142003111800014WP 2003 11 18 UPS03841357 120030919A5754 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, RT WING LE. UPPER RIB IS CRACKED AT XFS 835. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20031118000372003111800037EU 2003 11 18 AWXA200301152 120030924A5321D5367180500300 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON CABIN FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED CORRODED CABIN FLOOR PANEL 262FF IAW AWA T/C C1D25310, ZONE 1D. 2L72 4F RTA28NM 20031118000502003111800050EU 2003 11 18 AWXA200301165 120030924A5350D5323022620100 PLATE AIRBUS320 A320232 3930326EU WING TO BODY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK A .25 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING SUPPORT STRUCTURE CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7, SECT 6, PARA B, FIG 2 & 3. 2L72 4F RTA28NM 20031118000572003111800057EU 2003 11 18 AWXA200301172 120031005A5414D54530052202 SKIN PANEL AIRBUS320 A320232 3930326EU NR 2 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN. MAINTENANCE REMOVED NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-12, & 21-22, FIG 2, 3. 2L72 4F RTA28NM 20031118000752003111800075NM 2003 11 18 CALA0300581 120031008A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND EXTERIOR FUSELAGE SKIN WORN AT FORWARD DORSAL FIN FAIRING, TOP OF FUSELAGE STARTING AT BL 0, BS 860 THROUGH L & R BL6, BS 885. THE SKIN WAS REPAIRED USING A DOUBLER REPAIR IAW SRM 53-00-01. 2L72 4F RTA16WE 20031118000872003111800087NM 2003 11 18 C1HA200394020 120031009A3350 POWER SUPPLY BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 OVERWING EMERGENCY EXIT LIGHT (UPPER) INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW CHAMPION AMM 33-51-00; OPS CHECK GOOD. 2L73 4F A3WE 20031118000892003111800089SO 2003 11 18 SWIA200312473 120030910A5712 RIB EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LT WING LE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07297SW 120327 LT IB LEADING EDGE RIB IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED REINFORCEMENT DOUBLER ON LEFT IB LEADING EDGE RIB IAW 51-10-02. 2L72 4T4 TRTA31SO E20NE 20031118000942003111800094EA 2003 11 18 COMA0360450 120031008A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01487CA 7729 FLIGHT 5368 EMERGENCY FLOOR PATH LIGHTING IS INOP AT ROW 1. REPLACED THE FLEXIBLE LAMP ASSY. 2L72 4F RTA21EA 20031118000962003111800096 2003 11 18 54987 420031006A3414 INDICATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA AIRSPEED FLUCTUATES A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07242YV UE242 ON TAKE OFF CREW NOTICED A 4O TO 50 KNT SPLIT BETWEEN THE CPT AND FO AIRSPEED IND. FO READING LOW DREW ABORTED TAKEOFF AND RETURNED TO GATE. 2L72 4T3 TRTA24CE E2NE 20031112000442003111200044NM 2003 11 12 03FDEA01780 120031009A5753ARC0503 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - SIDE ATTACHMENT BARREL NUT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745 - WINGS LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION AND CMM 57-44-09 2L73 4F RTA22WE 20031112000592003111200059NM 2003 11 12 AWXA200301395 120031020A5330654580026 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 .375 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE LOWER AFT CORNER OF L-1 DOOR, BS 344. MAINTENANCE CUTOUT DAMAGE ON FUSELAGE SKIN AT LOWER AFT CORNER OF L-1 DOOR; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS AND 2 EACH REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW ER 15-5300-03311-TB2. 2L72 4F RTA16WE 20031112000622003111200062NM 2003 11 12 CALA0300626 120031107A5311 FRAME BOEING757 757224 1384958NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2729124 27565 INSPECTION FOUND AFT CARGO PIT FRAME PUNCTURED AT BS 1340, S25R. REPAIRED IAW SRM 51-70-11. 2L72 4F RTA2NM 20031112001272003111200127WP 2003 11 12 ABXA030434 120031028A532099234178 ANGLE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 VERTICAL ANGLE CRACKED AND HAD SHEARED RIVETS FS 696 RIGHT BUTTLINE 44. REMOVED AND REPLACED ANGLE IAW DC-9 SRM. 2L72 4F A6WE 20031112001352003111200135EU 2003 11 12 BAQA089617 120031014A7160430110217 ACTUATOR BOLKMS117 BK117B1 5626012EU ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G637 7179 MLG ACTUATOR FAILED AFTER 13.6 HOURS. 1G72 3U H13EU 20031113000332003111300033EU 2003 11 13 BAQA089976 120031010A7712117902121 INDICATOR BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101750B1 41560NE TORQUE STUCK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03300CP119 7249 PART REMOVED LASTED ONLY 119.0 HOURS. ENGINE NR 1 NEEDLE STICKS AT +/- 20 PERCENT. REPLACED WITH SERVICEABLE UNIT. 10/15/03 1G72 3U3 U H13EU E5NE10 20031113000732003111300073NE 2003 11 13 AALA20031075 220030928A7310 FUEL LINE BOEING757 757223 1384957NM RROYCERB211 RB211* 54555NE NR 1 ENGINE DAMAGED A AALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW21669AA 25334 MIA - FLT 863 - EN ROUTE SJU-STL, AIRCRAFT DEVELOPED FUEL LEAK ON THE NR 1 ENGINE. DECLARED EMERGENCY SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT FOR OVERWEIGHT LANDING. REPLACED THE FUEL LINE BETWEEN THE FUEL OIL COOLER AND THE HIGH PRESSURE FUEL PUMP. LEAK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA2NM A12EU 20031117000602003111700060EA 2003 11 17 COMA0360448 120031004A29106017523843 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA RT PYLON CUT A COMAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO01959CA 7116 FLIGHT 5510 HYDRAULIC SYSTEM NR 2 LOW PRESSURE WARNING. REPLACED LEAKING PRESSURE LINE IN RT PYLON. 2L72 4F RTA21EA 20031117000852003111700085NM 2003 11 17 DHL2003749510 120030920A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK AT FLIGHTSTAR IN JACKSONVILLE, FL., AFT PIT FLOOR SUPPORT FROM STA 950E TO STA 990 RBL 10 HAS SEVERAL DENTS. REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH BAC 1500-6199 FLOOR SUPPORT APPROXIMATELY 5 FT 8 INCHES LONG PO 328319 IAW B-727 SRM 51-30-2 AND 51-20-1. ALODINED AND PRIMED FLOOR SUPPORT IAW B-727 SRM 51-10-2. INSTALLED ON A/C IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20031118000272003111800027NM 2003 11 18 AWXA200301142 120030903A53206546547629 INTERCOSTAL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK A 3.3125 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT BULKHEAD INTERCOSTAL AT BS 727, 15 INCHES ABOVE STR 23 RT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT BS 727, 15 INCHES ABOVE STR 23 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-46547; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PARA 7D. 2L72 4F RTA16WE 20031118001152003111800115NM 2003 11 18 AWXA200301191 120030912A5313146N5444 STRINGER BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FLOOR STRINGER IN AFT CARGO COMPARTMENT BS 1500 TO BS 1560, LBL 18 TO RBL 18. MAINTENANCE CUTOUT CORRODED AREAS OF FLOOR STRINGER BS 1500 TO BS 1560, LBL 18 TO RBL 18; FABRICATED REPAIR PLATES AND FILLERS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG. 1, FIG. 1. 2L72 4F4 FRTA2NM A12EU 20031119000242003111900024NE 2003 11 19 NAFA20030002 220031009A7421URHB32E SPARK PLUG DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 16 CYLINDER CRACKED I N32BE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL017780B181 181 45372 P35317 NR 1 PRECAUTIONARY ENGINE SHUT DOWN DUE TO NR 16 CYLINDER DOUBLE SHORTED SECONDARY. REMOVED AND REPLACED NR 16 CYLINDER FRONT AND REAR SPARK PLUGS. CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20031119000252003111900025SO 2003 11 19 GLBA2003137 120031009A33501013073 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A GLBAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM0396ZK 120096 EMERGENCY LIGHTING INOPERATIVE, REMOVED AND REPLACED LIGHT ASSY, FUSE AND BULBS. OPS CK GOOD. 2L72 4T RTA31SO 20031119000262003111900026NE 2003 11 19 NACA20030114 220031008A8550 SHAFT DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE OIL PUMP SHEARED A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AL03993301924 1924 43576 P33821 NR 4 ENGINE SHUT DOWN DUE TO 0 BMEP INDICATION AND EXCESSIVE LOSS OF OIL. REPLACED ENGINE DUE TO NOSE CASE OIL PUMP FAILURE AND HIGH METAL. 2L74 4R4 R 6A3 5E8 20031119000302003111900030NE 2003 11 19 0068494 320031010A6111RFC11M1R6A BLADE HAMSTD EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF19 NE PROPELLER CRACKED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 852106 CRACK AT BLADE SHANK FILLET RADIOUS. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20031119000352003111900035EU 2003 11 19 AWXA200301197 120031009A2120 SMOKE AIRBUS320 A320231 3930325EU CABIN DETECTED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28645AW 238 EN ROUTE FROM PHX TO ATL THE FLIGHT ATTENDANT REPORTED A STRONG BURNING ODOR AND ANOTHER FLIGHT ATTENDANT SAID SHE SAW SMOKE AT SEAT ROWS 9 AND 10 RT SIDE. ODOR DISSIPATED AFTER 1 TO 2 MINUTES. MAINTENANCE INSPECTED THE FORWARD GALLEY OVENS, PASSENGER CALL AND READING LIGHTS, AND FORWARD AND AFT CARGO COMPARTMENTS, NO ABNORMALITIES NOTED. 2L72 4F RTA28NM 20031119000392003111900039EU 2003 11 19 AWXA200301202 120030924A5320D53911600202203 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON FWD CARGO COMPARTMENT LT PROFILE BETWEEN FR 31 AND FR 34, AT FASTENER HOLES. MAINTENANCE REMOVED DAMAGED L/H PROFILE BETWEEN FR 31 AND FR 34; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW AWA E.R. 26-5320-03154-SS1 2L72 4F RTA28NM 20031119000502003111900050NM 2003 11 19 CALA0300583 120031010A5347 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND LT TIEDOWN RAIL CORRODED AT STA 787, S26L. A NEW TIEDOWN RAIL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20031119000542003111900054NM 2003 11 19 CALA0300588 120031011A5347 SEAT TRACK BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND CENTER FLOOR RAIL CORRODED AT TOP AND INSIDE CHANNEL AT FLOOR STRAP AFT OF STA 847. THE FLOOR RAIL WAS REPAIRED IAW ECRA 5320-01603. 2L72 4F4 FRTA16WE E2GL 20031119000642003111900064WP 2003 11 19 MWEA030420 120031010A2611G718902 CONTROL PANEL DOUG DC9 DC932 3022066WP SMOKE DETECTOR INOPERATIVE A MWEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL31207ME 47794 MASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS. SMOKE DETECTOR PANEL CIRCUIT BREAKER POPPED. INSPECTED OVERHEAD PANEL WIRING AND CARGO FIRE SUPPRESSION CONTROL PANEL. NO VISIBLE DEFECTS NOTED, ALSO INSPECTED CARGO PIT SMOKE DETECTOR. NO VISIBLE DEFECTS NOTED. REMOVED AND REPLACED CONTROL PANEL. 2L72 4F A6WE 20031119000742003111900074WP 2003 11 19 ABXA030388 120030923A53205956034538 ATTACH FITTING DOUG DC9 DC932F 3022067WP INTERCOSTAL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 CRACKED FITTING ON INTERCOSTAL STA. 996, BETWEEN LONGERON 28 - 27 RT. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20031119001032003111900103WP 2003 11 19 DHL2003805011 120031009A269787823902 CONNECTOR DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FIRE LOOP DAMAGED A DHLAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01805DH 46125 DURING CRUISE NR 1 FIRE LIGHT ILLUMINATED, WARNING BELL SOUNDED. PERFORMED PHASE ONE ITEMS LIGHT REMAINED ON (BLEW BOTH BOTTLES). DUMPED 19000 LBS. OF FUEL AND LANDED SAFE. R AND R NR 1 AND 2 ENG FIRE BOTTLES IAW MM 26-20-01. OPS CHECKED GOOD. NR 1 FIRE LOOP "B" ILLUMINATED DURING FLIGHT. DEFERRED FIRE LOOP "B" IAW MEL 26-2-3 DMI NR 14402 PLACARD INSTALLED. REF. DMI NR 14402 FIRE LOOP "B" ILLUMINATED DURING FLIGHT (NR 1 ENG). FOUND "B" FIRE LOOP CONNECTOR AT FAN SECTION NEAR START VALVE WITH EXPOSED WIRE. FOUND BOTH "B" LOOP CONNECTORS AT HOT SECTION PYLON BURNED AND BROKEN INTERNALLY. REPLACED ALL THREE IAW DACO M/M 20-50-1. "B" FIRE LOOP TEST GOOD IAW DC-8 26-10-1. DMI NR 14402 CLEARED. PLACARD REMOVED. 2L74 4F4 FRT4A25 E2GL 20031119001082003111900108EU 2003 11 19 DHL2003367008 120031011A56106052 WINDSHIELD AIRBUS300 A300B4203 3930306EU COCKPIT CRACKED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01367DH 265 ON PUSH BACK L1 (CAPTAIN'S FRONT WINDSCREEN) CRACKED. REMOVED AND REPLACED CAPTAIN'S FRONT WINDOW (WINDSHIELD L1) IAW A-300 M/M 56-11-11. REMOVED AND REPLACED L1 TEMPERATURE REGULATOR CONTROLLER. GROUND OPS CHECKED NORMAL IAW A-300 M/M 30-42-00. 2L72 4F RTA35EU 20031119001182003111900118NM 2003 11 19 2003UALA00747 120031006A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 AFT PIT STA 1439 LT SIDE AT LBL 23, FLOORBEAM IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND FILLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20031118000662003111800066NM 2003 11 18 03FDEA01630 120030924A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 BS 440 STR 3 LT STRINGER CLIP CRACKED. REMOVED AND REPLACED STR CLIP AT BS 440 STR 3 LT PER SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20031118000842003111800084NE 2003 11 18 DHL2003720010 220031009A7261 ENGINE BOEING727 727228 1384083NM PWA JT8 JT8D* NE NR 1 LEAKING A DHLAE ENGINE SHUTDOWN K FLUID LOSS NRNOT REPORTED 1 SO01720DH 19544 NR 1 OIL QUANTITY DECREASED FROM 4 GAL. TO 1.5 GAL. PERFORMED ABNORMAL. NR 1 OIL BYPASS LIGHT ILLUMINATED. COMPLETED IN-FLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURE. OPERATED ENGINE AT 1.4 EPR NO VISIBLE LEAKS NOTED EXTERNALLY. INSPECTED TAILPIPE NO EVIDENCE OF LEAKAGE NOTED. REMOVED NOSE DOME IN INLET NO LEAKS NOTED. 2L73 4F4 FRTA3WE E2EA 20031118000922003111800092 2003 11 18 SWIA200312481 420030930A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07250YV7126 5677 120250 FO'S FLIGHT DIRECTOR ERRATIC. REPLACED FO'S APC-65B AUTOPILOT COMPTUER. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T4 TRTA31SO E20NE 20031119000042003111900004SO 2003 11 19 C2XA03SH379 120031009A33507287580503 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C-CHECK THE AFT EMERGENCY LIGHT PROXIMITY STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031119000662003111900066EA 2003 11 19 COMA0360452 120031009A53116003603031 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01963CA17437 7127 FRAME 718 DOUBLER CRACKED. COMPLIED WITH EO 53-027, PER MAJOR WORK ORDER 71396. 2L72 4F RTA21EA 20031119000992003111900099 2003 11 19 QXEA200301269 420031008A3420 INDICATOR CNDAIRCL600 CL6002C10 1390015EA ZONE 100 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09612QX 10042 YEG- ON FLIGHT 2462 EFIS CAUTION LIGHT CLIMBING THROUGH 15,000, COMPLIED WITH EMEREGNCY CHECKLIST. CAUTION LIGHT WENT OUT. FIVE MINUTES LATER RECEIVED ANOTHER EFIS CAUTION. DETERMINED FIRST OFFICER'S HEADING INDICATOR DIFFERED FROM STANDBY COMPASS. COMPLIED WITH EMERGENCY CHECKLIST. COMPLIED WITH CRJ-700 AMM TASK 34-21-00-720-801-A01. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031119001152003111900115NM 2003 11 19 2003UALA00743 120031004A2120 SEAL SEAT BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 3 SEAL DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29595UA 28748 FLT DIVERTED DUE TO SMOKE IN CABIN. ENGINE REMOVED AND NR 1, 2&3, NR 3 FORWARD & NR 3 AFT CARBON SEALS ALL REMOVED AND CHECKED. ALL CARBON SEALS CHECKED GOOD, MATING SURFACES OF SEAL SEATS OF NR 3 FWD & NR 3 AFT WERE FOUND TO HAVE HEAT CRACKS. MICROCRACKS ARE TYPICAL OF SEAL SEATS & ALTHOUGH THEY PRESSURE TESTED GOOD, STILL HAVE CONTRIBUTED TO SLIGHT LEAKAGE. IN ADDITION, SEAL SEATS ALSO FOUND TO BE SLIGHTLY OUT OF SPEC FOR FLATNESS. COMBINATION OF INCONTIGUOUS FLATNESS & MICROCRACKS IS BELIEVED TO HAVE CAUSED THE INTERMITTANT SEAPAGE OF OIL INTO GAS PATH. 2L72 4F4 FRTA2NM E17NE 20031119001342003111900134NM 2003 11 19 2003UALA00766 120031009A5711 SPAR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 LT WING SPAR UPPER CHORD CRACKED AT MLG BEAM SUPPORT FITTING. MAJOR REPAIR ACCOMPLISHED. SPLICED NEW CHORD. 2L72 4F4 FRTA16WE E2GL 20031120000062003112000006EA 2003 11 20 SWIA200312491 120031012A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07403SW 7028 FLAPS HALF SPEED STATUS MESSAGE ILLUMINATED. REPLACED FLAP PDU WITH SERVICEABLE UNIT IAW CRJ MM 27-52-01. OPS CHECK NORMAL. S/N OFF: 109. 2L72 4F RTA21EA 20031120000292003112000029NM 2003 11 20 AWXA200301238 120030922A5310654681282 SHEAR TIE BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT OUTBOARD SHEAR WEB BS 986-1016, LBL 38-46, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED LT AFT OUTBOARD SHEAR WEB BS 986-1016, LBL 38-46, WL 208; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 38 & 55, FIG 8. 2L72 4F RTA16WE 20031120000332003112000033NM 2003 11 20 AWXA200301242 120031001A53206546812 WEB BOEING737 737301 1384611NM SUBFLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MINOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON RT AFT OUTBOARD SUBFLOOR WEB BS 992, RBL 60, WL 206. MAINTENANCE CUT OUT DAMAGE ON RT AFT OUTBOARD SUBFLOOR WEB BS 992, RBL 60, WL 206; FABRICATED A FILLER AND REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, SHEET 1-3, FIG 1. 2L72 4F RTA16WE 20031120000442003112000044NM 2003 11 20 QXEA200301240 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 SMALL NICKS AND SCRATCHES 3 INCHES LONG ON TOP FLANGE OF NR 3 SEAT TRACK 12 INCHES AFT OF FWD END. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-3644. 2H72 4T RTA13NM 20031120000462003112000046SO 2003 11 20 SWIA200312494 120031007A275012064207611 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07587331257 1257 120197 DURING DESCENT INTO IAH THERE WERE NUMEROUS CONTROL FAULT ON OVERHEAD WITH FLAP AND ADVANCED SWS ON MAP THAT APPEARED FOR A COUPLE SECONDS THEN CLEARED ITSELF. REMOVED AND REPLACED FLAP CONTROL LEVER PER MM 27-00-00. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031120000492003112000049 2003 11 20 SWIA200312497 420031006A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07221SW5343 5343 120290 CAPTAIN'S AUTOPILOT DISCONNECTS INFLIGHT, FOLLOWED BY RED COMPUTER FLAG. INSTALLED SERVICEABLE APC-65B IN NR 1 POSITION. OPS CHECK GOOD. PN ON 622-8315-402, S/N ON 3788 OFF 1534. 2L72 4T RTA31SO 20031120000502003112000050SO 2003 11 20 SWIA200312498 120031010A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07227SW3840 3840 120304 FLAP CONTROL FAULT AND ADVANCED SWS DURING TAXI OUT. RESET ONCE, REPEATED FAULT WHEN SELECTED TO 15 DEGREES. REPLACED FLAP SELECTOR SWITCH. OPS CK GOOD. 2L72 4T RTA31SO 20031120000622003112000062NM 2003 11 20 QXEA200301251 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 9 SEAT TRACK CHANNEL IS PITTED AT STATION X545.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-784. 2H72 4T RTA13NM 20031120000972003112000097WP 2003 11 20 ABXA030392 120031014A3260 SWITCH DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE MLG DIRTY A ABXAO OTHER N FALSE WARNING DEDESCENT 1 GL23819AX 45927 DURING DESCENT, LANDING GEAR WAS EXTENDED TO FACILITATE DESCENT. WHEN GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING "NOT LATCHED" LIGHT ILLUMINATED WITH SELECTOR IN LEFT DOOR POSITION. PERFORMED ABNORMAL PROCEDURE. WHEN GEAR LEVER SELECTED TO UPLATCH CHECK POSITION, DOOR LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED FOR REMAINDER OF FLIGHT. CLEANED AND OPS CHECKED LEFT MAIN LANDING GEAR DOOR LATCH SWITCH IAW DC-8 AMM 32. OPS CHECKED GOOD. 2L74 4F4 F 4A25 1E8 20031120001062003112000106NM 2003 11 20 CALA0300597 120031010A5210 GATE BOEING737 737724 13844BYNM L-1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727724 28791 INSPECTION FOUND A DENT WITH A 0.60 INCH CRACK IN THE L-1 DOOR LOWER GATE AT AFT END. THE GATE WAS REPAIRED IAW ECRA 5210-01711. 2L72 4F RTA16WE 20031120001142003112000114NM 2003 11 20 AWXA200301448 120031106A532069451562 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN TIE CLIP AT BS 578, STR 11 RT. MAINTENANCE REMOVED CRACKED TIE CLIP AT BS 578, STR 11 RT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW SRM 51-40-02 PG 1 & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031120001212003112000121NM 2003 11 20 SWAA032459 120031106A53106547978 BEAM BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727A RBL 44 AND 47 WL 208. REPAIRED PER ER. 2L72 4F RTA16WE 20031121000012003112100001NM 2003 11 21 AWXA200301459 120031029A575365C2630933 STIFFENER BOEING737 7373G7 1384595NM NR 3 FLAP TRACK CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 DURING C-13 CHECK A .4375 INCH CRACK WAS FOUND NR 3 FLAP TRACK INNER STIFFENER AT WBL 191. MAINTENANCE REMOVED DAMAGED STIFFENER AT WBL 191 LT; FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 11. 2L72 4F RTA16WE 20031121000092003112100009CE 2003 11 21 AMWA79 120031104A1430114430002217 RIVET BEECH 1900 1900D 1154162CE FUSELAGE CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127YV UE127 WHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, RIVET HEAD CHAFED WAS FOUND TO THE LEFT PRESSURE PLATE, LBL 30.28. 2L72 4T RTA24CE 20031112001362003111200136 2003 11 12 BAQA089970 420031016A3422206075606103 GYRO BELL 206 206L3 1182108SW COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03206CJ573 51579 DIRECTIONAL GYRO INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20031113000012003111300001SW 2003 11 13 HEEA090147 120030916A6730212076004101 SERVO BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA TAIL ROTOR BINDING E HEEAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 SW0333008 36004 FIVE MILES SOUTH OF MORGAN CITY STARTED HAVING TROUBLE WITH THE TRIM. LANDED AT MORGAN CITY. MAINTENANCE FOUND THE TAIL ROTOR SERVO BINDING. REPLACED SERVO. 1G72 4U4 U H4SW E22EA 20031113000062003111300006 2003 11 13 BAQA089638 420031006A3444066305401 ALTIMETER BOLKMS117 BK117A1 5626010EU RADAR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118NC278 7067 LOOSE HARDWARE IN FACE AND DENT ON BOTTOM. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031113000162003111300016NE 2003 11 13 BAQA090549 220031029A74209550171530 IGNITION LEAD AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE ENGINE INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037YL 880 11502 IGNITER LEAD INTERMITTENT. REMOVED FROM ENGINE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 URTH7EU E42NE 20031113000212003111300021 2003 11 13 BAQA089831 420031013A341006604211111 SYMBOL GENERATOR BOLKMS117 BK117A1 5626010EU DISPLAY MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03300CP927 7249 ERROR CODES (SG) ON ELECTRONIC DISPLAY. ALSO CHECK CONFIGURATION CODE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031113000292003111300029EU 2003 11 13 BAQA090584 120031030A2435 BRUSHES AEROSPSA365 SA365N 8680669EU STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365KY1269 3031 6529 STARTER GENERATOR BRUSHES WORN BEYOND LIMITS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 11/3/03 1G72 3U H10EU 20031117000702003111700070GL 2003 11 17 ALG2003F00083 220030827A7230 COMPRESSOR BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ENGINE STALLED E ALGAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW0369AL 52139 AS AIRCRAFT PREPARED TO TAXI FROM A HOVER, AIRCRAFT HAD WHAT WAS TO BE A COMPRESSOR STALL. PUT THE AIRCRAFT BACK ON PARKING PAD AND THE MECHANIC INSPECTED THE INLET AREA AND COMPRESSOR AND FOUND EVIDENCE OF FROG INGESTION. NO VISUAL DAMAGE WAS FOUND, ZOCKED ENGINE AND PILOT PERFORMED POWER CHECK, CHECKED GOOD. 1G71 3U3 UNCH2SW E1GL 20031117000782003111700078SW 2003 11 17 ALG2003F00088 120030825A7712407379003107 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE MALFUNCTIONED E ALGAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03497AL 53172 CAE847053 IN LEVEL FLIGHT CHECK INSTRUMENT LIGHT ILLUMINATED, TOOK POWER AWAY AND THE LIGHT WENT OUT. CHECK INSTRUMENT LIGHT ILLUMINATED AGAIN AND THE TORQUE GAUGE CYCLED FROM ZERO TO PEGGED OUT EXCEDANCE SHOWED 63 PERCENT OVER TORQUE. LOWERED TEMP TO 200 DEGREES BELOW NORMAL AND RETURNED TO INTRACOASTAL. MADE MINIMUM POWER LANDING. THE MECHANIC REPLACED TORQUE TRANSMITTER AND TORQUE INDICATORS. THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20031030000212003103000021NM 2003 10 30 UPS03441279 120030906A5712 RIB BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 3 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 3 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM IB CLOCKWISE). NR 2 TO NR 7 BOLT HOLES REPAIRED IAW RS 574135066 AND REFER EO B747574019269A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F4 F A20WE E20EA 20031030000292003103000029NM 2003 10 30 UPS03441287 120030905A5712 RIB BOEING747 747121 1384871NM NR 19 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 19 V/C FLAP I/B LINKAGE I/B RIB NR 1 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000922003103000092SO 2003 10 30 CX2A03RI003 120030930A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716911 145446 ROUTINE INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT OVER THE LEFT HAND WING WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB AND PERFORMED A SATISFACTORY OPERATIONAL TEST. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031030001142003103000114NM 2003 10 30 03FDEA01623 120030924A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 DENT IN FRAME BS 1030 AT STR 26L. *S/D* DAMAGE ON FRAME AT BS 1030 AT STR 26L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE ON FRAME AT BS 1030, STR 26L IAW SRM 51-40-3. 2L73 4F RTA3WE 20031031000332003103100033WP 2003 10 31 MWEA030402 120030310A5311591287039 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CANNING A MWEAK NONE O OTHER ININSP/MAINT 1 GL31216ME 47740 EVIDENCE OF OIL CANNING ON LEFT SIDE OF FUSELAGE STATION 1025. INSTALLED DOUBLER. 2L72 4F A6WE 20031031000602003103100060NM 2003 10 31 QXEA200301210 120030930A7710V319 SWITCH DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 400 FAILED A QXEAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM09357PH 504 ON FLIGHT 2200 AIRCRAFT RETURNED TO FIELD, ON TAKEOFF, AFTER GEAR UP ABOUT 5 SECONDS NR 2 ENGINE TORQUE FROM 45 TO 129, MAYBE HIGHER UP AND DOWN. SHUT DOWN NR 2 ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 POWER LEVER SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031031000632003103100063NM 2003 10 31 QXEA200301212 120031001A3397 WIRE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 400 MISINSTALLED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09359PH 514 DURING OPERATIONAL CHECK OF NR 1 ENGINE NACELLE LOWER WING ANTI-ICE LIGHT, OBSERVED SMOKE COMING FROM SCREW HEAD AT LIGHT ASSY. REVERSED POWER AND GROUND WIRES AT LIGHT SOCKET. 2H72 4T4 TRTA13NM E20NE 20031121000122003112100012NM 2003 11 21 SWAA032462 120031106A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND DENT IN SKIN AT BS 847 BETWEEN STR 25L AND 26L. REMOVED AND REPLACED PER ER. 2L72 4F RTA16WE 20031121000242003112100024NM 2003 11 21 VNAA0311003 120031111A3260870004MODB PSEU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07433JS1129989 3047 DURING FLIGHT, THE CREW FELT A VIBRATION AND RETURNED TO YUL. MAINTENANCE INSPECTED AND FOUND THE FORWARD NOSE LANDING GEAR DOOR LATCHED OPEN. MAINTENANCE THEN REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031121000472003112100047NM 2003 11 21 SWAA032485 120031109A3250 ACTUATOR BOEING737 7372T4 1384492NM NLG STEERING WORN A SWAAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 SW29702ML 22054 NOSE STEERING SYS INOP. C/W FOURTH LIFE PER MT, REMOVED AND REPLACED UPPER AND LOWER STEERING PLATES AND ACTUATOR ASSY PER MM. 2L72 4F A16WE 20031121000412003112100041WP 2003 11 21 0302039153 120030927A5411 RIB DOUG DC9 DC914 3022034WP PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING L-CHECK FOUND CRACK IN PYLON CLOSING RIB AT STATION YN 165 LT. REPAIRED PER EA 91-196348. 2L72 4F A6WE 20031121000482003112100048 2003 11 21 SWAA032486 420031107A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031121000552003112100055NM 2003 11 21 SWAA032493 120031110A53126546568 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED ABOVE STR 7L. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031121000562003112100056NE 2003 11 21 VNAA0311001 220031109A72003033509 PROBE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RIGHT ENGINE FAILED A VNAAO OTHER O OTHER CLCLIMB 1 GL07462PS 3084 AFTER TAKEOFF, THE CREW RECEIVED A RIGHT HAND ENGINE NL INDICATION OF ZERO AND FLIGHT 2458 RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NL PROBE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031121000662003112100066NM 2003 11 21 03FDEA01951 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 RIGHT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR MOUNT HOLE O/B CORRODED (WING SIDE) N0682 RHW O/B FLAP, I/B HINGE FITTING O/B ACTUATOR MOUNT HOLE CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5740-74250 TITLE : WINGS - LEFT & RIGHT O/B FLAP - I/B HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031121000682003112100068EA 2003 11 21 COMA0360495 120031111A2613 DETECTOR CNDAIRCL600 CL6002B19 1900309EA OVERHEAT SYS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01427CA 7460 FLIGHT 5579 DURING CLIMBOUT OF ATL RECEIVED A MLG BAY OVERHEAT CAUTION, AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT TRI. DEFERRED THE MLG BAY OVERHEAT DETECTION SYSTEM PER MEL. 2L72 4F RTA21EA 20031121000922003112100092NM 2003 11 21 03FDEA01940 120031113A5740 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR MOUNT HOLE OUTBOARD CORRODED (WING SIDE). LT OUTBOARD FLAP, INBOARD HINGE FITTING ACTUATOR MOUNT HOLE OUTBOARD CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5740-74250 2L73 4F RTA22WE 20031124000012003112400001NM 2003 11 24 QXEA200301442 120031118A2720 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 300 ILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09410QX 4053 ON FLIGHT 2328 NR 1 RUDDER HYDRAULIC CAUTION LIGHT ILLUMINATED AFTER CHECKLIST. COMPLIED WITH Q400 SERVICE LETTER 31-001R12. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031124000042003112400004EU 2003 11 24 037181 120031120A2913 PUMP SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE HYD SYSTEM FAILED A UHLAO OTHER J WARNING INDICATION CLCLIMB 1 GL17157SD 157 DURING CLIMBOUT FROM YIP WITH HYDRAULIC PUMP FAILED WHILE IN OVERRIDE, IN OVERRIDE DUE TO HYD PUMP AUTO MODE MEL. GEAR WAS NOTED UP AND LOCKED WITH THE GEAR TRANSIT LIGHT STILL ILLUMINATED. CREW CYCLED PUMP SWITCH AND C/B. THE PUMP WAS STILL INOPERATIVE. THE CREW THEN FOLLOWED THE QRH AND MANUALLY PUMPED THE SYSTEM PRESSURE UP TO OPERATIONAL PRESSURE. THE A/C LANDED AND TAXIED TO A SAFE POSITION WHERE MX COULD PIN THE GEAR AND SAFELY TOW THE A/C. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20031124000052003112400005 2003 11 24 SWIA200312592 420031108A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07209SW9003 9003 120269 F/O AUTOPILOT CONTINUES TO MAKE UNCOMMANDED SMALL FORE AND AFT PITCH CHANGES. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER WITH A SERVICEABLE COMPUTER. OPS CHECK GOOD IAW 22-10-00. 2L72 4T RTA31SO 20031124000072003112400007SO 2003 11 24 SWIA200312594 120031110A2120 SMOKE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE CABIN DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07189SW 120048 SMOKE IN CABIN WITH LEFT SIDE PACK FAIL AND DUCT OVERHEAT. ON THE RIGHT SIDE DUCT LEAKAGE, PACK FAIL, AND DUCT OVER RAN BOTH PACKS ON APU AND ENGINE BLEEDS AND FOUND SYSTEM TO OPERATE NORMALLY WITH NO SMOKE IN CABIN. INSPECTED IAW EMB120 MM 21-60-00. 2L72 4T4 TRTA31SO E20NE 20031124000162003112400016NM 2003 11 24 QXEA200301444 120031117A5270 BRACKET BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR OUT OF ADJUST A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09411QX 4055 ON FLIGHT 2285 AIRCRAFT RETURNED TO FIELD DUE TO FORWARD BAGGAGE DOOR WARNING LIGHT ILLUMINATED WHILE CLIMBING THROUGH 16,000 FEET AND THEN CONTINUED TO INTERMITTENTLY ILLUMINATE UNTIL FINAL APPROACH. PRESSURE WAS NORMAL. AIRCRAFT LANDED SAFELY. ADJUSTED TARGET CLEARANCE BETWEEN BRACKET AND RETAINING RING. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031031000782003103100078NE 2003 10 31 DLM90030844 220030909A7532 BLEED VALVE DOUG MD90 MD9030 3023690NM IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A DALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO27906DA24102 53386 V20022 NR 2 ENG COMPRESSOR STALLS LESS THAN 1.2 EPR. REPLACED 7TH STAGE BLEED VALVE. 2L72 4F4 FRTA6WE E311NE 20031103000042003110300004NM 2003 11 3 DL757030856 120030919A2420100201021000 STATIC INVERTER BOEING757 757232 1384965NM FORWARD E & E SHORTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27676DL 25981 CREW REPORTED AT FL390 A/P DROPPED OFF AND LOST THE STANDBY BUS. STARTED TO SMELL A VERY SLIGHT ELECTRICAL BURNING ODOR IN COCKPIT. F/A ALSO STARTED SMELLING SOMETHING IN CABIN. CREW PERFORMED POM PROCEDURE AND DIVERTED INTO FAT. LANDING WAS UNEVENTFUL. AFTER LANDING, REPORTED A STANDBY INVERTED STATUS MESSAGE. ALL OTHER SYSTEM INDICATIONS REPORTED AS NOMINAL. REPLACED STATIC INVERTER PER MM. OPS CHECKS OK. EICAS MSG ERASED. ITEM CLEARED. 2L72 4F RTA2NM 20031103000322003110300032NM 2003 11 3 DL738030890 120030930A5330143A32128 SKIN BOEING737 737832 13844CFNM FUSELAGE PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27394DA 30562 THE FUSELAGE SKIN WAS PUNCTURED BY FOD NEAR FS 500D AND STRINGER 18L. THE DAMAGE WAS REMOVED WITH A 11 X 9 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087371-14, REV A. 2L72 4F RTA16WE 20031103000872003110300087SW 2003 11 3 ALG2003F00079 120030708A6720 RIVET BELL 206 206L4 1182110SW ELEVATOR CONTROLSHEARED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03266AL17 52281 DISCOVERED WHEN AIRCRAFT WAS BEING PREPARED FOR PAINT. CONTROL TUBE SHEAR RIVET SHEARED WHEN LIGHT CONTROLS WERE MOVED. NO EXCESSIVE FORCES ON CONTROLS WERE APPLIED WHEN THIS OCCURRED. 1G71 3U NCH2SW 20031103001002003110300100NM 2003 11 3 AWXA200301124 120031005A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM ZONE 900 - LAVATDISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28805AW 1049 EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT LT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031103001022003110300102NM 2003 11 3 AWXA200301126 120031004A335020121 CHARGER BOEING737 73733A 1384673NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LAX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEAT ROWS 1 - 5 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031103001082003110300108NM 2003 11 3 AWXA200301132 120030904A5320655169824 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 21 RT AT BS 908. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AT BS 908, STR 21 RT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, G. 38, FIG. 8. 2L72 4F RTA16WE 20031103001192003110300119EU 2003 11 3 AWXA200301116 120030925A5414D54530052202203 SKIN AIRBUS320 A320232 3930326EU NR 2 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING AND PITTED ON THE INBOARD SIDE AT STA. 4067. MAINTENANCE FOUND IT TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE SKIN IAW A320 SRM 54-54-11 PG 2 AND 3 FIG1, 54-50-00 PGS. 103,105,106 AND 110 FIG 101 TABLE 101 FIG 104. 2L72 4F RTA28NM 20031103001272003110300127NM 2003 11 3 03FDEA01727 120031009A5753ARC2512503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING I/B FLAP O/B HINGE- O/B HINGE LUG HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-71744 - WINGS - LT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20031103001282003110300128NM 2003 11 3 03FDEA01755 120031014A5753ARC0502506 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE WING SIDE - LOWER MOUNT I/B CAVITY FOUND CORRODED. COMPLIED FEDEX EA 1-5740-71748, WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031103001292003110300129NM 2003 11 3 03FDEA01750 120031009A5753ARC0502506 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE FITTING (WING SIDE)- SIDE ATTACHMENT BARREL NUT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71748, WINGS - RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031103001312003110300131NM 2003 11 3 03FDEA01758 120031009A5753ARC29244 SKIN DOUG MD11 MD11 3023602NM TE FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING I/B FLAP LEADING EDGE I/B FLAP VANE TRACK CAVITY FOUND WITH CHAFING MARKS ON FITTING AND SKIN. RT WING I/B FLAP LEADING EDGE I/B FLAP VANE TRACK CAVITY ON FITTING AND SKIN AS PER FEDEX EA 1-5750-74240, WINGS - RIGHT INBOARD FLAP VANE SUPPORT - RIB CHAFED. 2L73 4F RTA22WE 20031103001422003110300142NM 2003 11 3 03FDEA01729 120031008A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG AND HOLE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031117000582003111700058NM 2003 11 17 DHL2003749503 120030918A5320 WEB BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C CHECK, AFT AIRSTAIR TORQUE BOX VERTICAL WEB HAS A CRACK COMING FROM LIGHTNING HOLE AT STA. 1323 LT SIDE. STOP DRILLED CRACK IAW B-727 SRM 51-10-1. 2) NDT STOP DRILLED HOLE IAW B-727 N.D.T. PT-6 51-00-00 FIG. 23, CRACK STOPS AT HOLE. FABRICATED REPAIR DOUBLER FROM 7075-T6 .040 INCH, ( 3 INCHES X 1.6250 INCH ) , P.O. NR 9912620 I.A.W. B-727 SRM 53-10-2 FIG. 6 AND SRM 51-40-2 FIG. 1. TREATED AND PRIMED REPAIR DOUBLER AND WORKING AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR DOUBLER AT LT AIR STAIRS STA. 1323 I.A.W. B-727 SRM 51-30-2. 2L73 4F4 FRTA3WE E2EA 20031105000022003110500002SO 2003 11 5 C2XA03SH377 120031009A711014576608045 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 SHV-DURING C-CHECK THE LEFT LOWER ENGINE COWLING SKIN WAS FOUND TO CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031030000052003103000005SW 2003 10 30 E5W2003F00000 120030910A6220407010105101 STUD BELL 407 407 1182206SW ALLSN 250C 250C47B GL DROOP STOP CRACKED A E5WRO OTHER O OTHER NRNOT REPORTED 1 GL21508MT 53326 CRACK-LIKE INDICATION DETECTED AT STUD RADIUS. CRACK LIKE INDICATION FOUND BY FLUORESCENT MAGNETIC PARTICLE EXAMINATION. 1G71 3U3 UO H2SW E1GL 20031030000612003103000061NM 2003 10 30 UPS03441324 120030905A571265B101486 RIB BOEING747 747121 1384871NM NR 18 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RIGHT WING - NR 18 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). FINAL HOLE SIZE 0.434 INCH AT HOLE NR 4. RIGHT WING NR 18 V/C FLAP O/B LINKAGE I/B RIB REPLACED IAW SRM 51-10-01 PG 8. 2L74 4F A20WE 20031030000762003103000076NM 2003 10 30 03FDEA01267 120030719A5330 SKIN BOEING727 727100 1384036NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25103FE 19199 L 2FH NLG 2F SKIN CRACKED AT STA 242 BELOW PANEL CUTOUT. 2L73 4F RTA3WE 20031030000852003103000085NM 2003 10 30 QXEA200301200 120030923A5330 SKIN DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 TWO DENTS IN FUSELAGE SKIN BELOW LAVATORY SERVICE DOOR AT STATION 222.5 AND 210.0. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-26 AND RD 8-53-2181. 2H72 4T4 TRTA13NM E20NE 20031030000932003103000093NM 2003 10 30 0301476312 120030619A335020131A POWER SUPPLY BOEING757 757251 1384970NM DOOR 2R INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01511US 23199 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE SEATS 1-32. REPLACED POWER SUPPLY AT DOOR 2R M732, P/N 2013-1A. 2L72 4F RTA2NM 20031030001072003103000107NM 2003 10 30 03FDEA01545 120030916A5320A5A7116503 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CTR CARGO COMPT - POSSIBLE CRACK AT STA 1541 STRINGER SPLICE 45R. CTR CARGO STA 1541 STR 45R STRINGER CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG NSA6774 & SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20031030001092003103000109NM 2003 10 30 03FDEA01551 120030916A5320A5A7114523 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 POSSIBLE CRACK AT STR 51R STA 1540 UNDER PANEL 183CF JUST AFT OF TRANSVERSE SPLICE. CTR CARGO STA 1540 S51R CRACK SPLICE FITTING REMOVED AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20031103000482003110300048WP 2003 11 3 03FDEA01695 120031003A5753 BRACKET DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25397FE 46631 COMPLY WITH E.A.8-5750-73196. WINGS-RT IB REWORK OF 3EA FLAP TRACK ATTACH BRACKETS. CLOSING ACTION ON 10/02/03. ON N/R S00010.COMPLIED WITH E.A.8-5750-73196.WINGS-RT, IB FLAP REWORK OF 3EA FLAP TRACK ATTACH BRACKETS. 2L73 4F A22WE 20031103001412003110300141 2003 11 3 SWIA200312516 420031011A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07291SW6807 6807 120318 DURING DESCENT YAW DAMPER DISENGAGES, CAPTAIN'S SIDE ONLY, WITH ASSOCIATED AMBER DISENGAGE LIGHT AND AMBER ''R'' LIGHT ON A/P CONTROL PANEL. ATTEMPTED TO RE-ENGAGE, BUT DOES NOT STAY ENGAGED.REPLACED APP65. OPS CHECK GOOD IAW MM 22-10-00. 10/16/03 UPDATE: REMOVED & REPLACED CAPT'S AUTO PILOT CONTROL PANEL IAW EMB 120 MM 22-00-00. OPS CHECKS GOOD. PN :622-5798-013 SN ON: 2072 SN OFF: 1668 2L72 4T4 TRTA31SO E20NE 20031105000182003110500018SO 2003 11 5 C2XA03CL175 120031022A3350 CONNECTOR EMB 145 EMB145ER 3260211SO CABIN DIRTY A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2715932 145015 CLE FLIGHT 2163 THE CREW REPORTED THE EXIT SIGN OVER ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE CONNECTOR FOR THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031105000222003110500022EU 2003 11 5 MALA030461 120031006A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, FOUND SEAT TRACK NR 3 CORRODED. MAINTENANCE CARRIED OUT EO A53026 ON SEAT TRACK NR 3. REFER TO LOG PAGE 189910 FOR DETAIL. A/C RELEASE DATE 10/12/03. 2H74 4F RTA49EU 20031105000342003110500034NM 2003 11 5 AWXA200301299 120031002A532065C3267723 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF WEB BS 986 TO BS 1006, RBL 35, WL 208. MAINTENANCE REMOVED CORRODED WEB BS 986 TO BS 1006, RBL 35, WL 208; FABRICATED A NEW REPLACEMENT WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3 & 6. 2L72 4F RTA16WE 20031105000442003110500044NM 2003 11 5 03FDEA01717 120031008A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B HINGE PIN HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-71761 - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20031105000572003110500057NM 2003 11 5 SWAA032310 120031020A5311BAC1495 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727 LBL 7 TO RBL 3. REPAIRED FRAME PER SRM AND ERO. 2L72 4F RTA16WE 20031105000752003110500075NM 2003 11 5 03FDEA01836 120031030A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-224-01, 3) FLOORBEAM BS 1030, LBL 9, WL 208. CORROSION ON FLOORBEAM BS 1030, LBL 9, WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM BS 1030, LBL 9, WL 208 IAW SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 20031105000902003110500090NM 2003 11 5 2003UALA00806 120031026A2910 MODULE BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT HYD SYSTEM LEAKING A UALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 WP29508UA 24744 LT HYDRAULIC SYSTEM QUANTITY DECREASE. THE CAUSE OF THIS EVENT WAS AN INCORRECT UNION/SEAL COMBINATION ON THE LT SLAT/FLAP DEPRESSURIZATION MODULE. THE SEAL/RETAINER WAS REPLACED WITH THE CORRECT PACKING. 2L72 4F4 FRTA2NM E17NE 20031105000912003110500091 2003 11 5 2003UALA00807 420031025A3442 RADAR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE WEATHER RADAR INOPERATIVE A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29648UA 25285 RETURNED TO FIELD DUE TO INOP WEATHER RADAR. THE WX RADAR R-T. SHOP FINDINGS FOR THE REMOVED WX RADAR R-T WERE LOW POWER OUT. THIS CONDITION WAS CORRECTED IN THE SHOP BY REALIGNING THE FREQUENCY MULTIPLIER OF THE UNIT. 2L72 4F4 FRTA1NM E24NE 20031106000142003110600014EA 2003 11 6 COMA0360478 120031031A2140 RELAY CNDAIRCL600 CL6002B19 1900309EA CABIN HEAT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01796CA 7338 FLT 6716 DURING CRUISE FLIGHT TO CVG RECEIVED A DISPLAY COOL CAUTION MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND DIVERTED TO ALB. REPLACED RELAY K7HK. 2L72 4F RTA21EA 20031106000512003110600051NM 2003 11 6 03FDEA01812 120031022A5753 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - INBOARD FLAP SIDELOAD FITTING FOUND CRACKED. INBOARD FLAP SIDELOAD FITTING REMOVED AND REPLACED AS PER MM 20-50-02 AND OPERATION CHECK REFER WORK CARD NO : E 1-5750-7-5003A,PT 2, INSPECT AND REFURBISH INBOARD TRAILING EDGE FLAP & VANE ASSEMBLY. 2L73 4F RTA22WE 20031106000912003110600091EU 2003 11 6 AWXA200301340 120031031A26133551848400 OVERHEAT LOOP AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 PYLON FAULTY A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28628AW 67 PHX - ABORTED TAKEOFF - FLT 0567 - ON APPLICATION OF TOGA POWER FOR BLEEDS OFF TAKEOFF AT PHX EN ROUTE FOR MCO, RECEIVED ECAM MESSAGES FOR ENGINE NR 1 BLEED LEAK FOLLOWED BY APU BLEED FAULT & AIR PACK NR 1 FAULT. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED BLEED MONITOR COMPUTER BITE TEST THAT FAULTED NR 1 ENGINE PYLON LOOP. FOLLOWED TSM 36-22-15 AND REPLACED NR 1 PYLON OVERHEAT SENSING ELEMENT (1HF1). REPLACED APU LOAD CONTROL VALVE IAW AMM 49-51-51, APU BLEED FAULT STILL EXISTS, REPLACED APU BLEED SWITCH IN FLIGHT DECK AND SYSTEM OPERATION CHECK WAS NORMAL. PART NAME; SWITCH, MFG; ECE L'EQUIPEMENT, P/N; 2FCC2FEA0B01263, CONDITION; LOOSE 2L72 4F4 FRTA28NM E311NE 20031031000822003103100082NM 2003 10 31 DL764030849 120030908A3240S459 SWITCH BOEING767 767432ER 1385134NM COCKPIT FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27827MH 29698 TAKEOFF WARNING AT 25K ON TAKEOFF ROLL. REJECTED TAKEOFF AND FOUND THE PARKING BRAKE SWITCH FAILED. REPLACED SAME. 2L72 4F RTA1NM 20031103000252003110300025NM 2003 11 3 DL75K030880 120030927A3350 CONNECTOR BOEING757 757232 1384965NM EMERGENCY LIGHT LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO27650DL 24390 CABIN EMERGENCY LIGHTS SWITCH INOP. COCKPIT EMERGENCY LIGHT SWITCH WORKS OK. T/S PER FIM. RESEATED AND CLEANED CONNECTOR ABOVE SEAT 1A. SYS CHECKS OK. 2L72 4F RTA2NM 20031103000522003110300052NM 2003 11 3 03FDEA01603 120030910A5753ARC2512503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT IB FLAP OB HINGE (FLAP MOUNTED) IB AND OB PIVOT HOLES FOUND CORRODED AT BORES AND SPOT FACES. SNRM N0797 : LT IB FLAP OB HINGE (FLAP MOUNTED) IB AND OB PIVOT HOLES BORES AND SPOT FACES CORRODED AREAS REPAIR CARRIED OUT IAW EA NR 1-5750-72702 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT IB FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031103000642003110300064NM 2003 11 3 03FDEA01680 120031001A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 STA 680 FRAME IS DENTED BETWEEN STRS 24 - 25R. REPAIRED IAW SRM 51-40-3 AND EA 7-5310-70536 2L73 4F RTA3WE 20031103000652003110300065NM 2003 11 3 03FDEA01635 120030915A5710ARC41251 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT OUTBOARD FLAP FWD RIB SUPPORT ISLAND FOUND ONE ADDITIONAL CRACK APPROX .1875 INCH IN LENGTH AT OUTBOARD UPPER SIDE. LT OUTBOARD FLAP FWD RIB SUPPORT ISLAND REPAIR CARRIED OUT AS PER EA 1-5750-71897, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT OUTBD FLAP SECONDARY UP STOP REPAIR. 2L73 4F RTA22WE 20031103001492003110300149NM 2003 11 3 03FDEA01723 120031008A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING OB FLAP OB HINGE FITTING (FLAP SIDE)- IB HINGE LUG HOLE AND SURFACE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE)- I/B HINGE LUG HOLE AND SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031105000012003110500001WP 2003 11 5 UPS03841497 120031023A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 C-PIT TORQUE WEB IS CORRODED BEYOND LIMITS BETWEEN STATION 1160-1200 BETWEEN LONG 35R AND LONG 36. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 23. 2L74 4F RT4A25 20031105000052003110500005SO 2003 11 5 C2XA03SH410 120031024A532014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714542 145547 SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FR 20-23 WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031105000152003110500015GL 2003 11 5 C2XA03CL182 220031027A720023070401 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XAK NONE O OTHER LDLANDING 1 SW2714902 145496 CAE311853 DAY FLIGHT NR 2239 THE CREW REPORTED NR 1 OIL PRESSURE IN AMBER IN CLIMB MODE FOR 3-4 MINUTES. ALSO FUEL SMELL NOTED AFTER LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20031106000362003110600036NM 2003 11 6 QXEA200301365 120031024A5420 STRUCTURE DHAV DHC8 DHC8202 2809007NM LT NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX- LEFT HAND NACELLE GRAVEL GUARD LOWER ATTACHMENT POINTS HAVE CHAFE MARKS ON AFT WALL OF NACELLE. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16, 51-20-36 AND 51-20-41. 2H72 4T RTA13NM 20040112001322004011200132WP 2004 1 12 GTIA031009 120031113A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FS CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN CENTER FLOOR PANEL STATION 886-946 MISSING EDGE FILLER, TWO METAL SIDE SUPPORTS CRACKED/WORN. BAD INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040112001402004011200140NM 2004 1 12 CALA0300717 120031222A5514 FITTING BOEING737 7373T0 1384582NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 INSPECTION FOUND LT HORIZONTAL STABILIZER ATTACH LUG FWD UPPER BUSHING FACE PITTED. REMOVED BUSHING AND FOUND CORROSION ON AFT FACE. SPOT FACED 0.023 INCH AND INSTALLED NEW BUSHING PER SRM 55-10-10. 2L72 4F RTA16WE 20040112001482004011200148NM 2004 1 12 KPVA200339 120031002A2611 CONNECTOR DHAV DHC8 DHC8103 1386005NM SMOKE DETECTOR DIRTY A KPVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP13808WP 026 SMOKE LIGHT CAME ON DURING TAXI IN FOR LESS THAN 2 SECONDS. PRESSED MASTER WARNING, SMOKE LIGHT CLEARED. CLEANED AND TIGHTENED NR 2 CONNECTOR. OPS CHECK IAW DHC 8MM 26-12-00 PAGE 201. (M) 2H72 4T RTA13NM 20040108000792004010800079NM 2004 1 8 HALA0300840 120031001A2497 WIRE BOEING767 767300 1385204NM GCU BURNED A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13585HA 24257 NR 2 GEN DID NOT COME ON LINE UPON ENGINE START. BITE TEST ON BPCU SHOWED ( OPEN POR/FRD/GEN) RT. GCU FAIL. REPLACED GCU/BPCU. RUN UP CHECK, CONDITION SAME. REPLACED RT IDG IAW MM. OPS CHECK RUN, CHECK CONDITION SAME. REPLACED GCU CONTROL BREAKER OPS/ RUN CHECK SAME. RUN UP CHECK WITH LT GCR IN RT GCR POS. CONDITION SAME. FOUND T-1 CABLE AT STATION 425-412 BURNED. FERRIED A/C BACK TO HNL. REPAIRED BURNED WIRE AT SPLICE SM-7. ENGINE RUN UP CHECKED GOOD. OK FOR SERVICE.(K) 2L72 4F RTA1NM 20040108001322004010800132NE 2004 1 8 Z1R2003F00002 120031020A14307615009143041 SCREW SKRSKYS76 S76C 8143008NE M/R TIP CAP BROKEN E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11761AF903 760524 BLUE BLADE TIP CAP M/R SCREW. CORROSION AROUND ALL SCREWS, FIRST TWO THREADS. SEVERAL SCREWS APPEARED TO NO HAVE A FLUSH MOUNTING UNDER THE SCREW END. LENDING EDGE TOP SCREW HAD DEVELOPED A CRACK ( 90 PERCENT THROUGH SCREW) AND BROKE UPON REMOVAL. LARGE SCREWS, INSTALLATION TORQUE 100 IN/LBS BREAK AWAY TORQUE UPON REMOVAL WAS 170-100 IN/LBS.(K) 1G72 3U NCH1NE 20040108001452004010800145EU 2004 1 8 KBM2003F00079 120031022A6220704A33640021 SPACER SNIAS 350 AS350B2 8680813EU SCISSOR LINK WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 127 3403 SCISSOR LINK SPACER IS WORN. INSTALLED 2 EACH SERVCIEABLE SCISSOR LINK SPACERS.(K) 1G71 3U H9EU 20040109000562004010900056NM 2004 1 9 UIEA200300052 120030816A575365B1706419 FLAP TRACK BOEING747 747271C 1384869NM WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 DURING C-CHECK AT AMS, IB FLAP TRACK POS NR 4 CORROSION AT FORWARD BOLT HOLES. OVERSIZE AFFECTED HOLES TO REMOVED DAMAGE. NDT INSPECT TO ENSURE CRACK AND DEFECT FREE CONDITION. INCORPORATE INSURANCE CUT TO HOLES. RE-FINISH FLAP TRACK AND FAIL/SAFE BAR. INSTALLED SLEEVED OR OVERSIZE FASTENERS AS APPLICABLE. ALL IAW REF 1 THRU 4, WHICH DEALS WITH LETTERS (E-MAILS) REQUESTING STRUCTURALLY ACCEPTABLE REPAIR TO THE BOLT HOLES IB FLAP TRACK POS NR 4. REF 5 THRU 7, REF 8 DETAIL VISUAL AND ULTRASONIC INSPECT AT THE INSTALLED FASTENER LOCATIONS (8 HOLES PER TRACK) AT INTERVALS NOT TO EXCEED 18 MONTHS OR 1200 CYCLES, WHICHEVER IS EARLIER. (M) 2L74 4F A20WE 20040109000642004010900064EA 2004 1 9 A6WA200340173 120031123A5522 SKIN CNDAIRCL600 CL6002B19 1900309EA RT ELEVATOR LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31403AW 7288 FOUND DAMAGE ON RIGHT ELEVATOR UPPER SKIN CAUSED BY LIGHTNING STRIKE. REPAIRED BY PERFORMING WVAC EO NR 601R-55-4418. BLENDED AREA, PERFORMED NDI EDDY CURRENT AND APPLIED PROTECTIVE TREATMENT. (M) 2L72 4F RTA21EA 20040112000262004011200026CE 2004 1 12 2004F00015 120031119A5410MS20426AD4 RIVET LEAR 25 25D 5170514CE FIRE LOOP CLIP LOOSE A CEDAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW05213CA 241 AIRCRAFT WAS EN ROUTE FROM BUFFALO, NY TO PONTIAC, MI AND GOT AN INDICATION OF A FIRE ON THE NR 2 ENGINE. PILOT DECLARED AN EMERGENCY AND LANDED AT MTC SELFRIDGE AFB. UPON RECOVERY INSPECTION IT WAS FOUND THAT A FIRE LOOP CLIP HAD CAME LOOSE AND GROUNDED THE FIRE LOOP, CAUSING A FALSE FIRE INDICATION. RESECURED CLIP AND FIRE LOOP OPERATIONAL CHECK NORMAL. (M) 2L72 4J A10CE 20040112000372004011200037SO 2004 1 12 MASA200300494 120031215A5210 CABLE EMB 145 EMB145LR 3260212SO PAX DOOR LOOSE A MASAK NONE O OTHER ININSP/MAINT 1 SW07827MJ 145217 ASH 2793 CLT, CREW REPORTED THE MAIN CABIN DOOR BINDING AND COULD NOT OPEN FROM THE INSIDE. MX RESECURED THE DOOR CABLE INSIDE THE DOOR. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040112000662004011200066WP 2004 1 12 GTIA031030 120031106A5730 PANEL DOUG DC9 DC983 3022083WP RT WING DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND RT WING INBOARD LOWER T/E PANEL CRACKED/DELAMINATED AT BOTTOM SIDE ABOVE RIGHT MLG. REMOVED RT WING INBOARD LOWER TRAP PANEL. REPAIRED CRACKED, DELAMINATED AREA. INSTALLED RT WING INBOARD LOWER T/E PANEL. (M) 2L72 4F RTA6WE 20040112001922004011200192NM 2004 1 12 2003UALA00952 120031213A5313 STRINGER BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29171UA 24322 STRINGER 43AR CRACKED AT FUSELAGE STATION 240. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SPLICE REPAIR. 2L74 4F4 FRTA20WE E24NE 20040112001962004011200196 2004 1 12 ARWA20031004 420031024A3418 CONNECTOR DOUG DC8 DC862 3021970WP STALL WARN COMP DIRTY A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO198968U 46069 ON TAKE OFF FROM MGGT, RECEIVED A STICK SHAKE AT 40 KTS. ON ROLL. ABORTED TAKEOFF AND RETURNED TO RAMP. NOTE: ALSO HAD MAIN GEAR SPOILERS INOPERATIVE; LIGHT ILLUMINATED. CLEANED ELECTRICAL CONNECTORS ON STALL WARNING COMPUTER IAW MM 34-16-2 AND OPERATIONAL CHECKED STALL WARNING SYSTEM. OPERATIONAL CHECK NORMAL IAW MM 41-10-02; COULD NOT DUPLICATE FAIL. RESET SPOILER LOCKOUT C/B IAW MM 27-60-0; GROUND OPERATIONAL NORMAL. 2L74 4F 4A25 20040112001992004011200199NM 2004 1 12 PCAA031436 120031201A3230 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003NM MLG FAILED A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13845EX 344 FLIGHT 3691, ON APPROACH TO SYR, THE NOSE LANDING GEAR WOULD NOT EXTEND NORMALLY. AFTER ATTEMPTING FLIGHT MANEUVERS TO EXTEND THE GEAR, THE ALTERNATE EXTENSION SYSTEM WAS USED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE DISCOVERED AN INOPERATIVE NOSE DOOR SEQUENCING VALVE AND REPLACED IT. THE AIRCRAFT WAS TEST FLOWN AND RETURNED TO SERVICE. 2H72 4T RTA13NM 20040112002032004011200203CE 2004 1 12 FPI2003F00015 120031209A7921654585 MOUNT CESSNA210 T210L 2073449CE CONT O520 TSIO520* 17040SO OIL COOLER CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 CE07732HN102 21061527 821036R TOP FORWARD MOUNT FLANGE CRACKED UNDER NORMAL OPERATION. TOP AT BOTTOM FLANGES ARE NOT TRUE. 1H71 3O3 O 3A21 E8CE 20031106000452003110600045SO 2003 11 6 C2XA03SH402 120031022A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714542 145547 SHV- DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE GOUGED AT FRAME 52. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031106000572003110600057NM 2003 11 6 03FDEA01817 120031023A5753 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING INBOARD FLAP TRACK SIDE LOAD FITTING FOUND CRACKED. 2L73 4F RTA22WE 20031106001242003110600124NM 2003 11 6 SWAA032267 120031016A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031106001542003110600154SO 2003 11 6 C2XA03TY174 120031005A531514522760013 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713994 145291 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR SUPPORT CENTER OMEGA TOP CAP. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 41-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20031106001622003110600162NM 2003 11 6 03FDEA01850 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP FWD INBOARD HINGE OUTBOARD ACTUATOR ATTACH LUG BORE FOUND CORROSION. 2L73 4F RTA22WE 20031106001632003110600163NM 2003 11 6 03FDEA01851 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP FWD INBOARD HINGE INBOARD ACTUATOR LUG BORE FOUND CORROSION. 2L73 4F RTA22WE 20031106001692003110600169NM 2003 11 6 SWAA032275 120031016A53116546551 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BL 0. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031106001752003110600175NM 2003 11 6 03FDEA01865 120031103A5320 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CRACKED STR CLIP BS 950C STR 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 950C, STRINGER 5R PER SRM 51-30-2. LOCATED AND DRILLED HOLES PER SRM 51-30-5. 2L73 4F RTA3WE 20031106001822003110600182NM 2003 11 6 03FDEA01863 120031103A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 FUSELAGE UPPER LOBE, BS 720B 4.5, STR 15R, CRACKED. REMOVED DAMAGED SECTION OF STRINGER 15R, BS 720B 4.5 AND REPAIRED STRINGER PER SRM 53-10-3 FIG 5. 2L73 4F RTA3WE 20031106001882003110600188NM 2003 11 6 SWAA032276 120031016A53206547978 CREASE BEAM BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 617, RT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031106002032003110600203EA 2003 11 6 ASOA03462 120030928A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX STAIRS CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 FLT 4235 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031106002132003110600213NM 2003 11 6 ASAA0340313 120030707A33978100022605 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 1-6 INOPERATIVE. RECONNECTED WIRES, OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20031106002182003110600218NM 2003 11 6 ASAA0310460 120030515A5310HFAB53ST011 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE SHEAR TIE AT FUSELAGE STATION 987, STRINGER 24L-25L CORRODED. REPAIRED SHEAR TIE PER SRM. (M) 2L72 4F A16WE 20031106002192003110600219NM 2003 11 6 ASAA0310443 120030514A53116554956 FRAME BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE FRAME AT BS 727B, STRINGER 24L-25L DENTED. CUT OUT DAMAGED SECTION AND REPAIRED FRAME PER SRM. (M) 2L72 4F A16WE 20031106002272003110600227NM 2003 11 6 ASAA0310444 120030514A534765549693 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE SEAT TRACK AT BODY STATION 540-727B, WATERLINE 208 CORRODED. REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20031103000982003110300098NM 2003 11 3 PCAA0310119 120031003A3350 CONNECTOR DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DISCONNECTED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13845EX 344 MAINTENANCE DISCOVERED 5 EMERGENCY LIGHTS AT ROW 4 WERE INOPERATIVE AND THE DOOR EMERGENCY LIGHTS FLICKER OFF. ALL 6 EMERGENCY LIGHT BATTERIES WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 04 OCTOBER, MDT-FLIGHT NR 3725.CREW REPORTED TWO EMERGENCY LIGHTS WERE OUT ON THE RIGHT CABIN WALL. MAINTENANCE RELAMPED FORWARD EMERGENCY LIGHTS ON THE RIGHT HAND WALL. ALSO FOUND WAS THE CONNECTOR WAS OFF OF THE AFT EMERGENCY LIGHT AND 4 FLOOR LIGHTS WERE INOPERATIVE. FUSE IN POWER SUPPLY WAS REPLACED AT POSITION 200. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031103001072003110300107NM 2003 11 3 AWXA200301131 120030906A5311651630086 FRAME BOEING737 7373Q8 1384670NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK HFEC INSPECTION IDENTIFIED A CRACK IN RADIUS OF LT SIDE FRAME ON BS 178 BULKHEAD AT WL 207. MAINTENANCE REMOVED CRACKED LT SIDE FRAME ON BS 178 BULKHEAD; FABRICATED A NEW REPLACEMENT SIDE FRAME; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA. 4B. 2L72 4F RTA16WE 20031103001382003110300138CE 2003 11 3 DXTA200300138 120031015A3242 SCREW CESSNA500 560CESSNA 2076750CE RT SPEED XDUCER LOOSE E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07330QS 5600329 AFTER LANDING AT BUY, BRAKES FAILED ON BOTH PILOT’S AND FIRST OFFICER’S SIDES, HAD TO USE EMERGENCY BRAKE TO STOP AIRCRAFT. FOUND LOOSE SCREW ON RT SPEED TRANSDUCER AND PINS LOOSE, ALSO FOUND LT SPEED TRANSDUCER VERY HARD TO TURN AND DRIVE CAP BAD. REMOVED AND REPLACED RT SPEED TRANSDUCERS, RH ELECTRICAL CONNECTOR AND LT DRIVE CAP. ALL MAINTENANCE DONE IAW CESSNA 560 MM CHAPTER 32-42-07. 2L72 4F RTA22CE 20031103001402003110300140EA 2003 11 3 SWIA200312479 120031002A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 625 RT INTERCOSTAL ANGLE STR14R CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52 2L72 4F RTA21EA 20031103001432003110300143NM 2003 11 3 03FDEA01731 120031008A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750- 71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031105000682003110500068NM 2003 11 5 SWAA032283 120031017A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 771, RBL 8. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20031105000712003110500071NM 2003 11 5 SWAA032286 120031018A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED (3 EA) BETWEEN BS 859 AND BS 861, RBL 8, LBL 3 AND LBL 8. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20031105000922003110500092NM 2003 11 5 QXEA200301367 120031027A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX- REPLACE NR 1 SEAT TRACK DUE TO CORROSION DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-51-102. 2H72 4T RTA13NM 20031106000342003110600034NM 2003 11 6 2003UALA00809 120031024A5534 ATTACH FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE VERTICAL STAB CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29374UA 24639 VERTICAL STAB RIGHT O/B ATTACH LOG AND BOLT CORRODED. MAJOR REPAIR ACCOMPLISHED. REWORKED STAB ATTACHED LOG. 2L72 4F4 FRTA16WE E2GL 20031106001422003110600142SO 2003 11 6 SWIA200312531 120031022A3297 WIRE HARNESS EMB 120 EMB120ER 3260203SO RT MLG FAULTY A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07190SW 120050 WHEN SELECTING THE GEAR DOWN, ONLY THE RIGHT MAIN EXTENDED. RIGHT GREEN B-LIGHT AND ALL DISAGREEMENTS ILLUMINATED. THE ELECTRICAL OVER RIDE PROCEDURE IN THE QRH WAS CONDUCTED, RESULTING IN A SUCCESSFUL EXTENSION. REMOVED & REPLACED RIGHT MAIN GEAR SYSTEM-A PROX SENSOR HARNESS WITH A SERVICEABLE PART PER MM 32-61-01 401. CHECKS NORMAL. 2L72 4T RTA31SO 20031106001812003110600181NM 2003 11 6 03FDEA01864 120031103A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-111-01, 2) FWD CARGO COMPARTMENT SHEAR TIE ON AFT SIDE OF BS 700 FRAME LBL 9 WL 148. 2L73 4F RTA3WE 20031106001872003110600187SO 2003 11 6 C2XA03SH387 120031014A532014521699003 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 SHV- DURING C-CHECK THE LEFT BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031106002262003110600226NM 2003 11 6 ASAA0310445 120030514A71106940731802 GUSSET BOEING737 737290C 138448VNM NR 2 FAIRING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND NR 2 ENGINE FAIRING GUSSET AT NACELLE STATION 99.25 CRACKED. REPLACED GUSSET PER SRM. (M) 2L72 4F A16WE 20031106002282003110600228NM 2003 11 6 ASAA0310480 120030520A53116573746 FRAME BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 887, STRINGER 24L-25L CORRODED. CUT OUT DAMAGED SECTION AND REPAIRED FRAME PER SRM. (M) 2L72 4F A16WE 20031106002312003110600231NM 2003 11 6 ASAA0310409 120030508A53206546528 SUPPORT BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND SIDEWALL SUPPORT AT BS 500A-520, STRINGER 26R CORRODED. REPLACED SUPPORT PER SRM. (M) 2L72 4F A16WE 20031124000172003112400017NM 2003 11 24 QXEA200301446 120031118A5210 SKIN DHAV DHC8 DHC8202 2809007NM PAX DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX- PASSENGER DOOR SKIN DENTED TWO INCHES ABOVE RED LIVERY STRIPE. REPAIRED DHC-8 RD 8-53-53-84 AND SRM 51-00-06. 2H72 4T RTA13NM 20031124000292003112400029NM 2003 11 24 03FDEA01935 120031110A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT INBOARD FLAP, OUTBOARD HINGE, FOUND PIVOT HOLE NR 1 INBOARD CORRODED. RT I/B FLAP O/B HINGE PIVOT HOLE NR 1 I/B CORROSION REPAIRED AS PER FEDEX EA 1-5750- 74251, WING - RT I/B TRAILING EDGE FLAP- HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20031124000302003112400030NM 2003 11 24 03FDEA01934 120031110A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT INBOARD FLAP, OUTBOARD HINGE, FOUND PIVOT HOLE NR 1 OUTBOARD CORRODED. RT INBOARD FLAP, OUTBOARD HINGE, PIVOT HOLE NR 1 OUTBOARD CORROSION REPAIRED AS PER EA 1-5750-74251. 2L73 4F RTA22WE 20031124000402003112400040CE 2003 11 24 DXTA200300161 120031109A3213 STRUT CESSNA560 560XL 2076702CE MLG DAMAGED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07690QS3011 5605090 AFTER TAKEOFF DURING GEAR RETRACTION GEAR UNLOCK LIGHT STAYED ON. TROUBLESHOT AND FOUND NOSE STRUT NOT FULLY EXTENDING WITH WEIGHT OFF WHEELS. REMOVED STRUT AND REPACKED. REINSTALLED AND SERVICED IAW CESSNA 560XL CMM CHAPTER 32-20-01, PERFORMED GEAR SWING. OPS CHECK GOOD. 2L72 4F RTA22CE 20031124000422003112400042NM 2003 11 24 03FDEA01933 120031111A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT INBOARD FLAP, FOUND OUTBOARD HINGE PIVOT HOLE NR 1 OUTBOARD FLANGED SIDE CORRODED. RT I/B FLAP O/B HINGE PIVOT HOLE NR 1 O/B FLANGED SIDE CORROSION REPAIRED AS PER FEDEX EA 1-5750-74251, WING - RT I/B TRAILING EDGE FLAP- HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20031124000692003112400069NM 2003 11 24 BJ6A 120031111A5320 BUSHING BOEING737 7377BC NM CFMINTCFM567CFM567B2US 13802NE MOUNT BRACKET BROKEN E BJ6AK NONE O OTHER ININSP/MAINT 1 NE03171QS1354 30572 HOT WATER TANK ATTACHMENT FAILURE DISCOVERED. REVIEW OF FAILED PARTS SHOWED CLEVIS PIN PULLED THROUGH WEB, BUSHING DISLODGED. BUSHING FOUND INTACT ON PIN IN CLEVIS. THE HOLE IN WEB AT FAILURE POINT SHOWED UNDAMAGED WEB MATERIAL GREATER THAN 180 DEGREES AROUND HOLE. REVIEW OF STRESS ANALYSIS SHOWS JOINT IS GOOD FOR ALL LOADING CONDITIONS IF BUSHING IS IN PLACE. FAILURE HAPPENED ON LATERAL SUPPORT, THERE WAS NO SAFETY OF FLIGHT ISSUE BECAUSE OF FOUR OTHER SUPPORTS HOLDING THE TANK. TANK SUPPORTS REDESIGNED TO INSURE BUSHINGS DO NOT DISLODGE. ACCOMPLISHED BY RIVETING PLATES ON EITHER SIDE OF BUSHED WEB, THUS, CAPTURING BUSHING & PREVENTING FROM WORKING LOOSE. 2L72 4F4 FRTA16WE E2GL 20040113000542004011300054EA 2004 1 13 COMA0360570 120031220A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01926CA 7027 FLIGHT 5659 EMERGENCY LIGHTS INOP. REPLACED 1ST SECTION OF FLOOR PATH LIGHTING. 2L72 4F RTA21EA 20040113000572004011300057EA 2004 1 13 COMA0360572 120031219A53206007522195 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01713CA13275 7245 THERE WAS A CRACKED INTERCOSTAL SUPPORT BRACKET BEHIND HYDRAULIC SYSTEM NR 1 RETURN FILTER BOWL. REMOVED THE CRACKED BRACKET. FABRICATED AND INSTALLED A NEW BRACKET IAW WVAC EO 601R-53-4486. 2L72 4F RTA21EA 20040113000632004011300063NM 2004 1 13 AWXA200301582 120031222A2560P2070001214 FLASHLIGHT BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28334AW 23747 LAS - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK THE FORWARD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040113000642004011300064NM 2004 1 13 AWXA200301583 120031202A575365C263204SP STRUCTURE BOEING737 73733A 1384673NM T/E FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND ON RT OUTBOARD MIDFLAP LEADING EDGE AT OPENING FOR EXHAUST GATE ACTUATING ROD, WBL 210. MAINTENANCE TRIMMED OUT CRACK ON RT OUTBOARD MIDFLAP LEADING EDGE WBL 210 IAW B737-300 SRM 57-53-01 FIG 102, SHEET 8. 2L72 4F RTA16WE 20040113000682004011300068EA 2004 1 13 033286255 120031124A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING HEAVY CHECK INSPECTION THE FLOORBEAM WAS IDENTIFIED WITH CORROSION AT FS 319 LBL 25. FLOORBEAM WAS REPAIRED PER REO AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE UPON COMPLETION OF HEAVY CHECK INSPECTION. 2L72 4F RTA21EA 20040113001032004011300103 2004 1 13 BAQA091138 420031117A3421 LIGHT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE ATTITUDE GYRO INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME702 5040035921250009 ATTITUDE GYRO BACK LIGHTING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 11/18/03 1G72 3U3 UO H88EU E42NE 20040113001122004011300112EU 2004 1 13 BAQA091185 120031118A2121ES730732 BLADE BOLKMSBK117 BK117C1 5626025EU LYC O320 IO320* 41508EA BLOWER FAN INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY230 7544 FAN BLADES CAME OFF. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 ONCH13EU 1E12 20040113001172004011300117 2004 1 13 F3LA200300187 420031219A256561620468 BATTERY PACK BOEING737 73736N 1384408NM EVAC SLIDE FAILED A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03306FL 28563 DURING C-7 CHECK, INSPECTION REPORTED FWD GALLEY DOOR ESCAPE SLIDE BATTERY PACK FAILED VOLTAGE TEST. REPLACED FWD GALLEY DOOR ESCAPE SLIDE. 2L72 4F RTA16WE 20040113001282004011300128EU 2004 1 13 BAQA091499 120031208A771230802012 INDICATOR BOLKMS117 BK117B1 5626012EU FLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G420 7179 TORQUE INDICATOR FLUCTUATES. REPLACED WITH SERVICEABLE UNIT. 12/12/03 1G72 3U H13EU 20040113001312004011300131NM 2004 1 13 03FDEA02251 120031226A5744ARC050213 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LEFT WING - O/B FLAP I/B FWD HINGE ACTUATOR MOUNT O/B LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75208, WINGS TRAILING EDGE AND TRAILING EDGE DEVICES- LT OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113001452004011300145EU 2004 1 13 BAQA090342 120031028A672011731822 PITCH LINK BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE TAIL ROTOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME735 7235 TAIL ROTOR PITCH LINK WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20040113001462004011300146NM 2004 1 13 03FDEA02278 120031226A5710 STOP FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, INBOARD FLAP VANE INBD STOP FITTING ATTACHMENT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75225 - WINGS - TRAILING EDGES AND TRAILING EDGE DEVICES - RT INBOARD FLAP VANE STOP SUPPORT FABRICATION. 2L73 4F RTA22WE 20040112000362004011200036SO 2004 1 12 MASA200300488 120031213A2120 SMOKE EMB 145 EMB145LR 3260212SO CABIN DETECTED A MASAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW07837MJ 145367 ASH 9435 CLT, CAPT WROTE UP SMOKE IN THE CABIN. MX FOUND NO DEFECTS AT THIS TIME. NO PARTS USED. 2L72 4T RTT00011AT 20040112000682004011200068WP 2004 1 12 GTIA031020 120031202A5310 SHEAR TIE DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND MID PIT BILGE, SHEAR TIE CORRODED AT STATION 579. CUT OUT DAMAGED SHEAR TIE. SUB CHART FOR 2014-T6 IS 7075-T6. FABRICATED NEW SHEAR TIE AND DOUBLERS. INSTALLED SHEAR TIE AND TWO DOUBLERS. (M) 2L72 4F A6WE 20040112000732004011200073NM 2004 1 12 DHL2003780017 120031221A5270 SWITCH BOEING727 727223 1384074NM PAX DOOR LACK OF LUBE A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01780DH 22006 UPON LANDING THE FORWARD ENTRY ANNUNCIATOR LIGHT ILLUMINATED. LUBRICATED SWITCH PLUNGER TO FORWARD ENTRY AND OPS CHECKED OK PER 52-11-01. 2L73 4F A3WE 20040112001102004011200110EA 2004 1 12 SMPA03001 120030903A243523048004TM STARTER GEN DHAV DHC6 DHC6300 2802606EA LEFT INOPERATIVE A SMPAO OTHER GH MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CRCRUISE 1 WP13805AS 805 PPG - FLT 912/913 - LEFT GENERATOR DROP OFFLINE EN ROUTE. FOUND LEFT ENGINE STARTER GENERATOR INOPERATIVE. REPLACED LEFT STARTER GENERATOR. LEFT ENGINE POWER LOSS ON FINAL APPROACH. OIL PRESSURE AND TEMP NORMAL, NO POWER AVAILABLE WITH POWER LEVER ADVANCEMENT. INSPECTED LEFT ENGINE AND FOUND P3 LINE BROKEN. REMOVED AND REPLACED P3 LINE. GROUND RUNUP CHECK SATISFACTORY. RELEASED FOR TEST FLIGHT. TESTED FOR POWER LOSS AND ANY ABNORMAL CONDITION ON FINAL APPROACH. TEST FLIGHT OK, NO DISCREPANCIES NOTED. (M) 1H72 3T RTA9EA 20040112002042004011200204EA 2004 1 12 SWIA200312718 120031223A2721 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA LT RUDDER DAMAGED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07595SW 7292 RUDDER TRIM SPORATIC TO LT SIDE, HARD TO USE. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL IAW CRJ MM 27-12-10. OPS. CHECK GOOD. 2L72 4F RTA21EA 20040112002472004011200247WP 2004 1 12 AALA20031455 120031221A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21428AA 49340 CABIN CEILING EMERGENCY LIGHTS AT ROWS 17 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK B5-104 FOR CABIN CEILING EMERGENCY LIGHTS AT ROWS 17 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20040112002532004011200253NM 2004 1 12 AALA20031431 120031214A3350 BATTERY BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21658AA 24616 MIA) ABOVE DOOR EMERGENCY EXIT SIGN INOPERATIVE AT L2 INTERIOR SIDE. REPLACED POWER SUPPLY M733 FOR ABOVE DOOR EMERGENCY EXIT SIGN AT L2 INTERIOR SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20040113000082004011300008EU 2004 1 13 BAQA091493 120031217A6410365A12002002 BLADE AEROSPSA365 SA365N 8680669EU TAIL ROTOR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM 6396 TAIL ROTOR BLADE NEEDS PAINT REPAIR. REPLACED WITH SERVICEABLE UNITS. 1G72 3U H10EU 20040113000102004011300010EU 2004 1 13 BAQA091479 120031210A243523032022 STARTER GEN BOLKMS117 BK117A3 5626015EU NR 2 ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LG212 7032 NR 2 ENGINE WOULD NOT CRANK/START. PART REPLACED WITH SERVICABLE UNIT. 12/30/2003 1G72 3U H13EU 20040113000552004011300055EA 2004 1 13 COMA0360571 120031219A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01967CA 7134 FLIGHT 5582 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040113000842004011300084NM 2004 1 13 AWXA200301596 120031203A532065458078 INTERCOSTAL BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL WEB AT BS 277, STR 14 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL WEB AT BS 277, STR 14 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45807; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 PG 1 AND SRM 51-40-03 FIG 14 PG 38. 2L72 4F RTA16WE 20040113000892004011300089 2004 1 13 BAQA091212 420031118A3160L316M30C1003 DISPLAY UROCOPEC135 EC135P1 8680990EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911BG978 0015 UNIT REMOVED OFF THE RENTAL SHIP. SEGMENTS IN WARNING. DISPLAY INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20040113001542004011300154NM 2004 1 13 QXEA200301578 120031225A3260858601 PSEU DHAV DHC8 DHC8202 2809007NM LANDING GEAR FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09357PH1400314003 504 SEA - FLIGHT 2077 - LANDING GEAR INOP CAUTION LIGHT WITH LEFT GEAR DOOR LIGHT WHILE IN CRUISE FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PSEU. OPERATION CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040113001622004011300162EA 2004 1 13 QXEA200301580 120031224A2824T99B38601 EJECTOR CNDAIRCL600 CL6002C10 1390015EA LT CENTER TANK FAILED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09610QX4625 10033 SFO - FLIGHT 2436 - AFTER FUELING, THE CENTER TANK QUANTITY INCREASED FROM 10 LBS TO 25 LBS IN APPROXIMATELY 6 MINUTES DURING REQUIRED FUNCTIONAL TEST (REF 2ND NOTE ON CRJ FSM PAGE 3-75). MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT CENTER TANK TRANSFER EJECTOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040113001632004011300163WP 2004 1 13 AALA20031466 120031223A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21400AA 49311 DFW FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERWING BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. 2L72 4F A6WE 20040113001712004011300171WP 2004 1 13 WRLA200321 120031111A3260806125 CONTROL BOX DOUG DC10 DC1030 3023501WP MLG PROX FAILED A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11526MD 46998 AFTER TAKEOFF WITH GEAR HANDLE UP RIGHT MAIN GEAR RED UNSAFE LIGHT ON PILOT AND F/E PANEL. ACCOMPLISHED ABNORMAL PROCEDURES 2602.83 WITH NO HELP. SELF TEST OF PROX BOX SHOWED THAT PROX BOX WAS BAD. CHECKED ALL PROX SENSORS FOR DAMAGE BUT NO DAMAGE FOUND. REMOVED AND REPLACED PROX BOX. ACCOMPLISHED SELF TEST ON THE NEW BOX IT PASSED ALL TESTS. CYCLED GEAR WITH GEAR PINS INSTALLED. COULD NOT DUPLICATE PROBLEM OPS CHECK OK. REMOVED AND REPLACED PROXIMTY CONTROL BOX. (M) 2L73 4F A22WE 20040113001732004011300173WP 2004 1 13 AALA20031469 120031223A33970201720003 WIRE HARNESS DOUG DC9 DC982 3022082WP CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21574AM 53152 DFW EMERGENCY LIGHT INOPERATIVE AT SEAT 16D. REPLACED LIGHT HARNESS AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040113001842004011300184 2004 1 13 RAIA00312299 420031204A3421501156616 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU COCKPIT DEFECTIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03567HK15554110 41085 STL- STAND BY ATTITUDE INDICATOR DRIFTING. MAINTENANCE REMOVED AND REPLACED STAND BY ATTITUDE INDICATOR. 2L72 4T RTA41NM 20040113001992004011300199SO 2004 1 13 C2XA03SH514 120031226A532014522459003 ANGLE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV- DURING C-CHECK THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AT FRAME 20 IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040113002002004011300200SO 2004 1 13 C2XA03SH515 120031226A531214526850401 FIREWALL EMB 135 EMB135LR 3260305SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040113002022004011300202SO 2004 1 13 C2XA03SH526 120031231A541114576599003 RIB EMB 145 EMB145LR 3260212SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 DURING C CHECK THE AFT EDGE MEMBER WAS FOUND TO BE GOUGED AT THE SIX O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040113002042004011300204SO 2004 1 13 C2XA03BT104 120031104A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714542 145547 BTV---CO2943, DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD EMERGENCY LIGHT IAW EMB145 MM NR 33-50-08. OPS. CHECKED GOOD. 2L72 4T RTT00011AT 20040113002202004011300220SO 2004 1 13 C2XA03CL197 120031205A21214611028900 FAN EMB 145 EMB145 3260210SO A/C BAY SEIZED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2713968 145138 CLE FLIGHT NR 2123) THE CREW REPORTED A VERY STRONG SMELL OF SMOKE FROM CABIN ON APPROACH. TURNED OFF NR 2 PACK AND SMELL DISSIPATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED SYSTEM AND FOUND THE NR 2 RECIRCULATION FAN WAS SEIZED. MAINTENANCE REPLACED THE NR 2 RECIRCULATION FAN. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040113002332004011300233NM 2004 1 13 QXEA200301562 120031215A5541 RIB DHAV DHC8 DHC8202 2809007NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX - FORE RUDDER LOWER CLOSING RIB IS CRACKED. REPLACED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040113002452004011300245NM 2004 1 13 QXEA200301490 120031122A5420 BRACKET DHAV DHC8 DHC8202 2809007NM LT NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- LT NACELLE WHEEL WELL BOTTOM OB GRAVEL GUARD BRACKET IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-40-11. 2H72 4T RTA13NM 20040113002502004011300250NM 2004 1 13 QXEA200301494 120031120A5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- CORROSION ON TOP OF OB FLOOR SUPPORT FROM LT HAND STATIONS X215 TO X222. REPAIRED IAW DHC-8 SRM 21-20-11. 2H72 4T RTA13NM 20040113002522004011300252NM 2004 1 13 QXEA200301287 120031010A5311 FRAME DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX- AFT BAGGAGE COMPARTMENT AFT FRAME 653.349 CHAFED AT FLOOR LEVEL AT OUTBOARD SIDE. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-36. 2H72 4T4 TRTA13NM E20NE 20040113002542004011300254SO 2004 1 13 C2XA03TY218 120031226A531514530627001 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS DURING A SCHEDULED 3C INSPECTION THE LT OMEGA BEAM WAS CORRODED AT BOLT HOLES BETWEEN FR 20 AND FR 25. MAINT REMOVED AND REPLACED THE OMEGA BEAM AT DAMAGE AREA AND REINSTALL THE TOPCAP IAW EMB 135/145 AMM 20-10-01 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040114000062004011400006WP 2004 1 14 IXXA0300077S 120031117A2710 BRACKET DOUG DC8 DC871F 302199DWP AILERON CONTROL CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX814301291 45993 DURING A ROUTINE B-CHECK INSPECTION MAINTENANCE FOUND RT AILERON INBOARD CONTROL TAB CABLE BRACKET CRACKED. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED INBOARD AILERON, RT AILERON MANUAL REVERSION CONTROL ROD, 5 EACH RT AILERON BUS CABLE, RT INNERCONNECT EYEBOLT AND RT AILERON CONTROL ACTUATOR PER ALL APPLICALBE MANUALS. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040112001562004011200156WP 2004 1 12 GTIA031029 120031105A5730 SKIN DOUG DC9 DC983 3022083WP RT WING ERODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND RIGHT WING INBOARD FLAP LOWER SKIN BEHIND TIRES HAS LIGHT EROSION. REMOVED DAMAGED SKIN AT INBOARD FLAP REMOVAL PANEL. REMOVED CORRODED SKIN AT OUTBOARD FLAP REMOVAL PANEL. FABRICATED NEW SKIN PANELS. INSTALLED NEW SKIN ON INBOARD FLAP PANEL AT RIGHT INBOARD FLAP. INSTALLED NEW SKIN ON OUTBOARD FLAP PANEL AT RIGHT INBOARD FLAP. (M) 2L72 4F RTA6WE 20040112001712004011200171WP 2004 1 12 GTIA031027 120031123A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND CABIN CENTER FLOOR PANEL 200-256 SEVERAL CORRODED INSERTS, DAMAGE/DELAMINATED AT EDGES. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040112002122004011200212GL 2004 1 12 ERAA091802 220031101A7250 BEARING BOLKMS105 BO105A EU ALLSN 250C 250C20 03013GL NR 4 FAILED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH15735 S675 METAL ON BOTTOM PLUG. BROKEN NR 4 BEARING CAGE. INSTALLED SERVICEABLE GEARBOX. COMPLIED WITH E CHECK 1G72 3U3 U H3EU E4CE 20040112002132004011200213NM 2004 1 12 2003UALA00964 120031217A5414 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 NR 2 PYLON OUTBOARD WEB CRACKED AT FORWARD ACCESS PANEL INBOARD SKIN LOWER AFT RADIUS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REPAIR OF PYLON SKIN PER MM 54-31-99 FIGURE 803. 2L72 4F4 FRTA2NM E17NE 20040112002692004011200269WP 2004 1 12 AALA20031465 120031222A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21429AA 49341 TWO EMERGENCY FLOOD LIGHTS ABOVE TAIL SLIDE, INOPERATIVE. REPLACED BATTERY PACK B5-28 FOR TWO EMERGENCY FLOOD LIGHTS ABOVE TAIL SLIDE. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2L72 4F A6WE 20040113000052004011300005EU 2004 1 13 BAQA091587 120031209A3310LRA15 CONTROL UNIT UROCOPEC135 EC135T1 5620026EU INSTUMENT LIGHTSINTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135LC82 0296 INSTRUMENT LIGHTS INTERMITTENT, FLASH ON AND OFF ONCE EVERY 1 OR 2 FLIGHTS. REPLACE SERVICEABLE UNIT. 12/18/2003 1G72 3U H88EU 20040113000392004011300039NM 2004 1 13 QXEA200301574 120031217A27423994001011 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB FAILED A QXEAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM09406QX5052 5052 4048 PDX - FLIGHT 2310 - ON APPROACH TO PDX, CREW RECEIVED A PITCH TRIM CAUTION. TRIM INDICATOR WENT TO FULL NOSE UP AND AUTO TRIM MESSAGES APPEARED ON BOTH PFD'S. NO TRIM WAS AVAILABLE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PITCH TRIM ACTUATOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040113000652004011300065NM 2004 1 13 AWXA200301584 120031207A5350654657711 SKIN BOEING737 737301 1384611NM TAIL CONE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MINOR REPAIR - DURING C-18 CHECK A FOUND UPPER SURFACE OF TAIL CONE DISBONDED 28 INCHES FROM FORWARD EDGE BS 1185 TO BS 1188, WL 289. MAINTENANCE PREPARED TAIL CONE UPPER SURFACE BS 1185 TO BS 1188, WL 289; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16, FIG 21, 37, & 51, REPAIR 11. 2L72 4F RTA16WE 20040113000732004011300073EA 2004 1 13 03357372 120031223A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27672BR 7594 DURING INSPECTION THE SERVICE DOOR EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040113000922004011300092NM 2004 1 13 AWXA200301602 120031216A521069101401 CLIP BOEING737 737301 1384611NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING -18 CHECK A 1 INCH CRACK WAS FOUND ON L-1 DOOR LOWER HINGE SPRING COVER ATTACH CLIP. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR LOWER HINGE SPRING COVER ATTACH CLIP IAW SOPM 20-50-01 PG 1-9. 2L72 4F RTA16WE 20040114000132004011400013 2004 1 14 DHL2003746014 420031118A3444 SWITCH BOEING727 727224 1384076NM GPWS CORRODED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01746DH 22252 WINDSHEAR/GPWS INOPERATIVE. LIGHT ILLUMINATED DURING TAKE-OFF ROLL. RTO CONDUCTED WINDSHEAR IN AREA. A/C WEIGHT 154,200 LBS., OAT 19 DEGREES C., PA 280, & BRAKE ENERGY ZONE CAUTION. TRANSFERRED TO DMI 14774 MEL 34-29 CAT. (A) PLACARD INSTALLED. INSPECTED BRAKES IAW MM, NO DEFECTS NOTED. SUSPECT GPWS COMPUTER. NO STOCK. SWAPPED GPWS COMPUTER & RADIO ALTIMETER, NO HELP. ORIGINAL GPWS & RADIO ALTIMETER BOXES REINSTALLED. REMOVED INSTRUMENT PANEL ON F/O'S FORWARD LT SIDE. FOUND GPWS TEST/INHIBIT SWITCH CORRODED. PARTS ON ORDER. REINSTALLED & PERFORMED PITOT-STATIC LEAK CK IAW MM, NO LEAKS NOTED. REPLACED F/O'S GPWS KORRY LIGHT, GPWS NOW OPS CKS GOOD PER MM. THIS CLEARS DMI 14774. 2L73 4F A3WE 20040114000152004011400015NM 2004 1 14 2003UALA00828 120031103A3411 PITOT TUBE BOEING757 757222 1384956NM PWA 2037 PW2037 NE AIRSPEED OBSTRUCTED A UALAC ABORTED TAKEOFF CS F.O.D. AFFECT SYSTEMS TOTAKEOFF 1 WP29558UA 26654 CAPTAINS AIRSPEED INDICATOR FAILED TO ADVANCE PAST 80 KNOTS. RUDDER RATIO AND MACH SPEED TRIM MESSAGES ILLUMINATED. MECHANIC FOUND LARGE BUG NESTING INSIDE CAPTS PITOT PROBE. ( RESTRICTING RAM PRESSURE). REMOVED AND CLEANED OUT BUG. THE BUG WAS LIKELY INSERTED BY A MUD DAUBER DURING LAYOVER. ACCOMPLISHED LOW RANGE PITOT STATIC CK. RUDDER RATIO AND MACH SPEED MESSAGES ALL RELATED TO CLOGGED PITOT. 2L72 4F4 FRTA2NM E17NE 20040114000522004011400052NM 2004 1 14 DL73S030967 120031029A5311654577055 FRAME BOEING737 737232 1384475NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27324DL 23096 DURING REPAIR OF STA 663 FRAME AT S3L AN EXISTING FASTENER LOCATION WAS NOTED TO HAVE SHORTED ALONG WITH STANDOFFS THAT INTERFERED WITH REPAIR ACCOMPLISHMENT. REPAIR INSTRUCTIONS WERE ISSUED VIA ERA 385749-14. 2L72 4F RTA16WE 20040114000682004011400068NM 2004 1 14 DL73S030983 120031106A5754 WEDGE BOEING737 737232 1384475NM L/E SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312DL 23084 FOUND ON W-1 LETTER CK, REPAIR LIFTING NUMBER 6 L/E SLAT T/E WEDGE 6 INCHES FROM O/B EDGE. REPAIRED PER SRM 51-40-20 AND OPERATION 1000. 2L72 4F RTA16WE 20040114001052004011400105NM 2004 1 14 DL757031042 120031118A5330143N33203 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27604DL 22811 THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 627 & 639 AND BETWEEN STRINGERS 15L & 16L. THE DAMAGE WAS REMOVED WITH A 9 X 12.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385913-14, REV A. 2L72 4F RTA2NM 20040114001082004011400108NM 2004 1 14 DLM88031044 120031121A3350100865 POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27904DL 49535 ON INSPECTION FOUND AFT CABIN EMERGENCY SEAT ROW LIGHTS RT SIDE WOULD NOT TEST. REPLACED BATTERY AND PWR SUPPLY. OPS NORMAL. 2L72 4F RTA6WE 20040114001352004011400135NM 2004 1 14 DL757031066 120031202A2560BACP18T441 PIN BOEING757 757232 1384965NM EVAC SLIDE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 ON HMV-3 OPN 5726, PIN CORRODED BS 1181 STR 21L ON OVERWING SLIDE ACTIVATION/DEACTIVATION LEVER. LEVER WAS STIFF IN INITIAL OPERATION. REMOVED PINS FOR INSPECTION. OK TO INSTALL. INSTALLED NEW PINS AND OPN NOW NORMAL. REPLACED PINS WERE BACP18T4-41 AND BACP18T4-38 ITEMS 230. 2L72 4F RTA2NM 20040113001002004011300100 2004 1 13 BAQA090704 420031110A3416C19269AA CONTROL UNIT UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ALTIMETER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME2120 0144 BARO SET KNOB INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 11/11/03 1G72 3U3 U H88EU E34NE 20040113001072004011300107 2004 1 13 BAQA091366 420031204A3422060001301 GYRO UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118WS195 0089 IN NORMAL SLAVE MODE, DIRECTIONAL GYRO DID NOT FOLLOW HEADING CHANGE. ONLY IN FAST SLAVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H88EU E34NE 20040113001262004011300126NE 2004 1 13 BAQA091292 220031201A7310430167601 MANIFOLD BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101650B1 41560NE FUEL SYSTEM MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03136AE718 7234 ENGINE HARD TO LIGHT OFF. REMOVED FUEL MANIFOLD FROM ENGINE. REPLACED WITH SERVICEABLE UNIT. 12/10/03 1G72 3U3 U H13EU E5NE 20040113001362004011300136NM 2004 1 13 03FDEA02257 120031226A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, I/B FLAP O/B HINGE FITTING O/B PIVOT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75213. TRAILING EDGE & TRAILING EDGE DEVICES. RT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113001592004011300159EU 2004 1 13 BAQA091485 120031123A6340L771M40C1014 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE TACH INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135LC48 0296 N2 NEEDLE INOPERATIVE. REPLACED WITH CANNED UNIT FROM AN AIRCRAFT. 1G72 3U H88EU 20040113001692004011300169WP 2004 1 13 GTIA031039 120031211A216160714622 CONTROLLER DOUG DC9 DC982 3022082WP CABIN TEMP FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 AIRCRAFT WOULDN'T HOLD CABIN PRESSURE. CABIN WARNING VOICE FLOW LIGHT ON. LEFT VALVE TEMP FULL HOT (AUTO) REDUCED TEMP BOTH PACKS LEFT PACK ON 30 SEC FLOW LIGHT ON MASK DROPPED. MANUAL MODE ON OUTFLOW VALVE. PERFORMED TEST ON TEMP CONTROLLER SYSTEM WITH TEST BOX. CONFIRMED LEFT CONTROLLER TO BE BAD. REMVOED AND REPLACED TEMP CONTROLLER. OPS CHECKS GOOD. PERFORMED LEAK CHECK OF DUCTING AND PRESSURIZATION CHECK. FOUND NO OTHER DEFECTS NOTED AT THIS TIME. (M) 2L72 4F A6WE 20040113001812004011300181WP 2004 1 13 WRLA200320 120031021A5320 CHANNEL DOUG DC10 DC1030 3023501WP R3 DOOR CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11352WL 47838 BULGING CONDITION UNDER SCUFF PLATE AT INBOARD AFT EDGE OF R-2 DOOR. OPEN UP AREA, REMOVED SCUFF PLATE, DRAIN PAN 2ND AFT R3 DOOR SURROUND AND REMOVED FLOOR PANEL AFT OF R3 DOOR IAW SRM 51-31-01. REMOVED CORROSION OUT OF LIMIT CHANNEL IAW SRM 51-33-01. REMOVED SURFACE CORROSION ON WEB UNDER CHANNEL NO MEASUREABLE MATERIAL LOSS NOTED IAW SRM 51-21-01 TREATED AND PRIMED AREA IAW SRM 51-21-01. FABRICATED AND INSTALLED REPLACEMENT CHANNEL IAW AEA 0665 AND SRM 51-33-01. REINSTALLED SCUFF PLATE, PAN, FLOORBOARD AND DOOR SURROUND IAW SRM 51-31-01. FABRICATED AND INSTALLED REPLACEMENT CHANNEL. (M) 2L73 4F A22WE 20040113001852004011300185SO 2004 1 13 RAIA00312300 120031204A3610V854A7257226 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS WORN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03815HK 145048 5663-STL- BLEED 1 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED FWD SEAL UNDER CARGO FLOORING. 2L72 4T RTT00011AT 20040113001932004011300193SO 2004 1 13 RAIA00312304 120031205A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO E/E BAY MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03815HK13428 145048 STL- AIR-GROUND FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT. 2L72 4T RTT00011AT 20040114000182004011400018NE 2004 1 14 2003UALA00842 220031107A72301663M24P01 FAN BLADE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE BENT A UALAA UNSCHED LANDING CE F.O.D. VIBRATION/BUFFET CLCLIMB 1 WP29381UA 24656 RETURNED TO ORD DUE TO A SLIGHT VIBRATION. VISUALLY CHECKED NR 1 ENGINE AND FOUND EVIDENCE OF BIRDSTRIKE IN THE ENGINE INLET. ACCOMPLISHED A BIRDSTRIKE INSPECTION AND BORESCOPE ON THE ENGINE. FOUND TWO FAN BLADES BENT BEYOND LIMITS WITH NO OTHER DISCREPANCIES OR EVIDENCE OF FURTHER BIRD INGESTION INTO THE ENGINE. CLEANED BIRSTRIKE DEBRIS FROM THE ENGINE INLET AND REPLACED BENT FAN BLADES (2 PAIRS). 2L72 4F4 FRTA16WE E2GL 20040114000532004011400053NE 2004 1 14 DL733030968 220031029A7200CFM563 ENGINE BOEING737 737347 1384647NM GE CFM56 CFM563B1 13802NE NR 1 ENGINE OVERTEMP A DALAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO27312WA43124 23598 721164 ON TAKEOFF ROLL, NR 1 ENGINE EGT WAS INCREASING TO 954 DEGREE CELSIUS. THROTTLES (AUTO THROTTLES) HAD TO BE DISCONNECTED TO KEEP ENGINE EGT FROM CLIMBING HIGHER. N1 WAS 91 PERCENT, N2 WAS 102 PERCENT AND INCREASING. FUEL FLOW NORMAL ON T/O ROLL. REPLACED ENGINE. 2L72 4F4 FRTA16WE E2GL 20031106002322003110600232NM 2003 11 6 ASAA0310481 120030521A526065544566 CASE BOEING737 737290C 138448VNM AFT AIRSTAIR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE AFT AIRSTAIR HANDLE CASING AT FUSELAGE STATION 967, LEFT BUTTOCK LINE 65 CRACKED. REPAIRED HANDLE CASING PER EA. (M) 2L72 4F A16WE 20031106002382003110600238WP 2003 11 6 GTIA030721 120030828A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND RIGHT INBOARD SEAT TRACKS CORRODED FROM STATION 790-1200 IN SEVERAL PLACES. REMOVED SEAT TRACK RIGHT INBOARD STATION 1032 TO STATION 1309. FABRICATED NEW SEAT TRACK. INSTALLED RIGHT INSTALLED RIGHT INBOARD SEAT TRACK. (M) 2L72 4F A6WE 20031107000302003110700030NM 2003 11 7 XNOA1164 120031104A2497 WIRE BOEING727 727200 138407ENM ELECTRICAL SYS DAMAGED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23793A 20774 AFTER STARTER CUTOUT ON ALL THREE ENGINES, FUEL FLOW DROPPED TO ZERO ON ALL THREE ENGINES. REPAIRED WIRING AT R51 RELAY IN J9 BATT SHIELD PER B727 WD 24-53-11. ENG GROUND RUN CHECKS GOOD IAW B727 72-00-00. (CLOSED) 2L73 4F RTA3WE 20031107000322003110700032NM 2003 11 7 QXEA200301389 120031105A5414 PANEL DHAV DHC8 DHC8202 2809007NM NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX- CREASE IN PANEL 261GT AND HOLE IN NACELLE SKIN JUST ABOVE LEFT HAND COWL DOOR. REPAIRED IAW HORIZON AIR EA 2-54-194 AND RD8-54-1851. 2H72 4T RTA13NM 20031107001172003110700117EU 2003 11 7 SIMA200327502 120031001A33506013211 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21254AE 340B254 DFW - FLT 3357 - EMERGENCY LIGHTS INOPERATIVE. RAI EMERGENCY BATTERY PACK AT 20LN OPERATIONAL CHECK GOOD IAW MM 33-50-00. (M) 2L72 4T RTA52EU 20031107001252003110700125EA 2003 11 7 REXA03007 120031016A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT FAILED A REXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO258423C 7423 RIGHT AIR CYCLE MACHINE FAILED IN FLIGHT PRODUCING SMOKE INTO CABIN. FOLLOWED QRH RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. REMOVED AND REPLACED THE RIGHT ACM. (M) 2L72 4F RTA21EA 20031107001292003110700129SO 2003 11 7 SIMA200327905 120031001A5330AL2024T3 SKIN EMB 135 EMB135KL 3260302SO FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 ABI - DURING AN MBV INSPECTION, TWO GOUGES WERE FOUND IN FUSELAGE SKIN BETWEEN FRAMES 19 AND 20 AND STRINGERS 1L AND 2L, CENTER FUSELAGE 1. BLENDED THE GOUGED AREAS AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 ERV 22, CHAPTER 53-21-01, EMB REPAIR STATEMENT IC2003-145/3231 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031105000412003110500041WP 2003 11 5 ABXA030404 120031010A532039135821 FITTING DOUG DC9 DC931 3022065WP LT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 FITTING IN LEFT WHEEL WELL STA 699, LEFT BUTT LINE '10' CRACKED. REPLACED FITTING IAW DC-9 SRM. 2L72 4F A6WE 20031105000472003110500047NM 2003 11 5 CALA0300611 120031030A53116558280 BELTFRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912318 23369 E&E COMPARTMENT HAS 5 INCHES OF CORROSION ON BELTFRAME BETWEEN STRINGER S27L AND S27R AT STA 360. REPAIRED BELTFRAME PER SRM 53-00-07. 2L72 4F RTA16WE 20031105000852003110500085EA 2003 11 5 QXEA200301354 120031027A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT INTERMITTENT A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09615QX 10065 ON FLIGHT 2502 INTERMITTENT FIRE SYSTEM FAULT. COMPLIED WITH CRJ SRM 26-15-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031106000112003110600011NM 2003 11 6 AWXA200301357 120031014A5315146N5484 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1503-1540, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1503 TO BS 1540, LBL 2; FABRICATED A REPLACEMENT FLOORBEAM AND SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1. 2L72 4F RTA2NM 20031106000252003110600025NM 2003 11 6 03FDEA01809 120031028A5412AUB7520 BULKHEAD DOUG MD11 MD11 3023602NM NR 1 PYLON DAMAGED A FDEAK NONE K FLUID LOSS ININSP/MAINT 1 SO25585FE22904 48481 MX REPORTED FINDING HYDRAULIC FLUID ACCUMULATED INSIDE OF THE NR 1 ENGINE PYLON DUE TO THE LEAK AT AUK7617-5001 HYDRAULIC LINE. HYDRAULIC LEAK WAS FIXED AND PYLON VISUALLY INSPECTED FOR INTEGRITY/SECURITY PRIOR TO ANC/LAX LEG. A FOLLOW UP CONDITIONAL INSPECTION FOR SUSPECTED TITANIUM MEMBERS THAT MIGHT HAVE OR WOULD MORE THAN LIKELY BECOME HYDROGEN EMBRITTLED DUE TO HOT HYDRAULIC FLUID CONTAMINATION WAS REQUESTED PER EA 1-5450-74134. REMOVED AND REPLACED NR 1 ENG PYLON BULKHEADS (4 EA) EA 1-5450-74184 STEPS 1 THRU 11. AIRCRAFT RELEASED FOR REVENUE SERVICE. 2L73 4F RTA22WE 20031106000392003110600039NM 2003 11 6 SWAA032290 120031019A53116546570 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1006, WL 195 AT LBL 29-33 AND WL 196 AT RBL 30. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031106000402003110600040NM 2003 11 6 SWAA032291 120031018A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 4, ABOVE STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031106000432003110600043 2003 11 6 SWAA032294 420031018A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031106000612003110600061SO 2003 11 6 C2XA03TY178 120031016A532014520600003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713994 145291 DURING A SCHEDULED 2C INSPECTION THERE WAS EVIDENCE OF CORROSION BENEATH THE CARBON FIBER FLOOR SUPPORT AT FR 20. MAINT REMOVED AND REPLACED THE RAMP ANGLE IN THE GALLEY AT FR 20. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-40-02. A/C WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040112002052004011200205NM 2004 1 12 2003UALA00961 120031215A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 BODY STATION 588 TO 624 STR 15L TO 17L HAS A DOUBLER INSTALLED WITH DENTS NEXT TO IT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040112002072004011200207NM 2004 1 12 KPVA200342 120031103A33506104781 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE EMERGENCY LIGHT INOPERATIVE A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13808WP16 026 LT AFT EGRESS LIGHT AND AFT CEILING AISLE LIGHT INOPERATIVE. MECHANIC REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY (3351-PS3). PERFORMED OPERATION TEST OF EMERGENCY LIGHT SYSTEM IAW DHC 8 MM 33-55-00 PG. 201-202, PAR.2A. NO DEFECTS NOTED. 2H72 4T4 TRTA13NM E20NE 20040112002112004011200211SW 2004 1 12 HEEA087824 120030624A6220206011139001 ARM BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL MAIN ROTOR STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 BOTH ARMS STICK IN THE DOWN POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20040112002142004011200214NM 2004 1 12 2003UALA00965 120031217A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 CABIN FLOORBEAM 365 AT RBL 10 TO RBL 45.5 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. CORROSION WAS REMOVED AND FLOORBEAM WAS REPAIRED. 2L72 4F4 FRTA2NM E17NE 20040112002162004011200216EU 2004 1 12 BAQA091744 120031211A6330L633M2010104 MOUNT UROCOPEC135 EC135P1 8680990EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03577LF880 0140 MAIN ROTOR GEARBOX MOUNT LEAKING. PART REPLACED WITH SERVICABLE UNIT. 01/06/2004 1G72 3U O H88EU 20040112002182004011200218EU 2004 1 12 BAQA091367 120031126A6720 BEARING BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE BELLCRANK ASSY WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME6531 7235 TEFLON WORN IN BEARING. PART REPLACED WITH SERVICEABLE UNIT. 01/08/2004 1G72 3U3 U H13EU E5NE 20040112002202004011200220NM 2004 1 12 2003UALA00968 120031218A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 FUSE SKIN IS CRACKED AT THE FWD GALLEY DOOR CUTOUT LOWER AFT CORNER PAST 2 FASTENERS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040112002232004011200223NM 2004 1 12 SWA2004F00000 120031031A5753654792327 SPAR BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE LT MIDFLAP CRACKED D SWAAO OTHER O OTHER NRNOT REPORTED 1 NM01379SW 1897 26585 CRACKED AT O/B AFT FLAP TRACK LOWER ATTACH HOLES. 2L72 4F4 FRTA16WE E2GL 20040112002262004011200226NM 2004 1 12 SWAA032800 120031222A3397BR2013 WIRE BOEING737 7377H4 1384404NM CABIN EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29417WN 29822 EEPLS WIRES EXPOSED AT FWD END. SECURED EEPLS WIRES PER MM. 2L72 4F RTA16WE 20040112002312004011200231 2004 1 12 BAQA084041 420031210A225041600293110 COMPUTER UROCOPEC135 EC135P1 8680990EU SAS SYSTEM INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03577LF 0140 SAS COMPUTER HAS INTERMITENT KICK. REPLACED WITH SERVICEABLE ASSET PART. 1G72 3U O H88EU 20040112002622004011200262WP 2004 1 12 AALA20031454 120031221A3397 WIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21969TW 53619 FORWARD EMERGENCY PATH AISLE LIGHT IN AFT ACCESSORY RAMP AREA INOPERATIVE. RECONNECTED LOOSE WIRES TO FORWARD EMERGENCY PATH AISLE LIGHT IN AFT ACCESSORY RAMP AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E2EA 20040112002762004011200276WP 2004 1 12 AALA20031412 120031210A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217539A 49993 LAX) EMERGENCY LIGHTS POWERED BY POWER SUPPLY B5-107 INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY B5-107 BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F4 F A6WE E2EA 20040113000042004011300004EU 2004 1 13 BAQA091574 120031212A6710 BEARING UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE CONTROL ROD WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME800 0009 BEARINGS WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 UO H88EU E42NE 20040113000092004011300009EU 2004 1 13 I05R091604 120031208A6330L633M2010105A001MOUNT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE M/R GEARBOX DEFLATED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05603ME21 0284 MAIN ROTOR GEARBOX Z-ARIS MOUNT, PART DEFLATED REPLACED PART. 1G72 3U3 UO H88EU E42NE 20040113000262004011300026 2004 1 13 HEEA087807 420030609A34424000038 CONTROL HEAD BELL 206 206L3 1182108SW WX RADAR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610C 51425 RECEIVE VOLUME TOO LOW AND CANNOT BE ADJUSTED HIGHER TO IMPROVE PILOT RECEPTION. SHOP REPAIR. 1G71 3U H2SW 20040113000272004011300027 2004 1 13 HEEA087816 420030614A3442MI5852013 INDICATOR BELL 412 412 1182202SW PWA PT6 PT6* 52043EA WX RADAR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 WEATHER RADAR INOPERATIVE IN WX AND MAP MODES. REPAIRED. 1G72 4U3 T H4SW E2NE 20040109000062004010900006CE 2004 1 9 LX52003F00002 120031001A2400 POWER SUPPLY BEECH B300 B300 1159232CE PWA PT6 PT6A6 52043EA CABIN ODOR B LX5RO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL19991LL3561 FL142 THE POWER SUPPLY EMITTED A FOUL ODOR THAT WAS NOTICED THROUGH OUT AIRCRAFT AND THEN UNIT FAILED. 2L72 4T3 TRTA24CE E4EA 20040109000422004010900042NM 2004 1 9 GAIA03160OP 120031107A33501000679 LIGHT BOEING727 727224 1384076NM PWA JT8 JT8D9 52048NE L1 DOOR INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW0769739 20667 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. C/A: REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040112000142004011200014 2004 1 12 2004F00009 420030814A3425066031252500 DISPLAY PILATSPC12 PC1245 7090551EU EHSI INOPERATIVE A S4WAO OTHER L NO TEST NRNOT REPORTED 1 WP07308NA4028 226 CO-PILOTS EHSI DISPLAY DOES NOT POWER UP. MOVED THE DISPLAY TO ANOTHER POSITION AND THE PROBLEM FOLLOWED. REMOVED AND REPLACED WITH SERVICEABLE AND OPS CHECK OK. (M) 1L71 3T RTA78EU 20040112000392004011200039NM 2004 1 12 AALA20031451 120031220A33501060091101 LIGHT BOEING767 767323 1385205NM CABIN MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21392AN 29429 LAX FLIGHT DECK DOOR EMERGENCY LIGHT ASSEMBLY MISSING. INSTALLED NEW FLIGHT DECK DOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040112000742004011200074SO 2004 1 12 C2XA03CL206 120031220A33507287100507 CONTROL PANEL EMB 145 EMB145ER 3260211SO CABIN FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715941 145035 CLE FLIGHT 3253 THE CREW REPORTED THE EMERGENCY LIGHT AISLE PATH LIGHTING STAYED ON. MAINTENANCE REPLACED THE FLIGHT ATTENDANT'S CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040112000762004011200076NM 2004 1 12 AWXA200301566 120031220A2560P4010021 BATTERY BOEING737 73733A 1384673NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28175AW 23634 DEN - EMERGENCY EQUIPMENT - DURING INSPECTION FOUND THE EMERGENCY FLASHLIGHT IN AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040112000782004011200078NM 2004 1 12 AWXA200301568 120031220A33503114981 REFLECTOR BOEING737 737277 1384570NM EXTERIOR DEFECTIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - EEL - DURING 4-DAY CHECK THE RT LOWER EXTERNAL GROUND ILLUMINATION EMERGENCY ESCAPE LIGHT WAS FOUND INOPERATIVE, BULB REPLACEMENT HAD NO EFFECT. MAINTENANCE REMOVED AND REPLACED RT LOWER EXTERNAL GROUND ILLUMINATION EMERGENCY ESCAPE LIGHT REFLECTOR ASSEMBLY. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040112000862004011200086NM 2004 1 12 AWXA200301576 120031202A5330654580046 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON FUSELAGE SKIN BONDED DOUBLER AT R-1 DOOR LOWER HINGE CUTOUT AT BS 295, STR 15 RT. MAINTENANCE REMOVED CRACKED SKIN AT R-1 DOOR LOWER HINGE CUTOUT AT BS 295, STR 15 RT; FABRICATED A DOUBLER & FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01 FIG 208 PG 225-226. 2L72 4F RTA16WE 20040112001262004011200126EU 2004 1 12 2004F00028 120030915A3350311701 POWER SUPPLY BAG JETSTMJETSTM3101 1500215EU EMERGENCY LIGHT DISCHARGED A B16AO OTHER L NO TEST TXTAXI/GRND HDL 1 NE05538PA 751 FLT 3803 - PSM - AFTER ENGINE SHUTDOWN, EMERGENCY LIGHTS AT VESTIBULE AND ROWS VERY DIM. REMOVED AND REPLACED BOTH AFT EMERGENCY LIGHT BATTERIES IAW J-31 AMM 33-50-00. OPS CHECKED GOOD IAW J-31 AMM 33-50-00. (M) 2L72 4T RTA21EU 20040112001472004011200147EU 2004 1 12 MALA030553 120031215A3260 UPLOCK SWITCH SAAB SF340 340B 7860101EU LANDING GEAR OBSTRUCTED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15425XJ 340B425 DURING FLIGHT 3078, AFTER DEPARTURE GEAR INTRANSIT LIGHT WOULD NOT GO OUT. CREW DIVERTED TO BRD. MAINTENANCE REMOVED ICE FROM GEAR UPLOCK SWITCH BOSS ICE WAS COMPRESSED BETWEEN UPLOCK SWITCH BOSS AND LANDING GEAR BOSS. 2L72 4T RTA52EU 20040112001532004011200153NM 2004 1 12 MEX2003513 120030911A3230833605 PSEU DOUG MD88 MD88 3023688NM E/E BAY FAILED A ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23161PL 49764 FLT 431 - LAX-PVR - CAPTAIN REPORTED DURING CRUIST EHT LIGHT 'SLAT DISAGREE' WAS TURNED ON, AND SOMETIMES THE AURAL ALARM OF 'FLAP OVERSPEED' WAS SOUNDED. AT PVR, THE SYSTEM WAS CHECKED AND THE PROXIMITY SWITCH CONTROL UNIT WAS REPLACED IAW MM 34-60-04, TEST OK. (M) 2L72 4F RTA6WE 20040112001882004011200188NM 2004 1 12 AWXA200301254 120031002A531569770172 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND ON FLOOR SUPPORT ATTACH BRACKET AT LOWER OUTBOARD RADIUS FORWARD SIDE OF BS 1006, LBL 22, WL 206. MAINTENANCE REMOVED FLOOR SUPPORT ATTACH BRACKET FORWARD OF BS 1006, LBL 22, WL 206; FABRICATED A NEW REPLACEMENT ATTACH BRACKET; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3, SHT 1-3, & FIG. 8, SHT 1. 2L72 4F RTA16WE 20040112001912004011200191NM 2004 1 12 03FDEA02304 120031228A5730ARC07883 PANEL DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT FOUND CRACKED APPROXIMATELY 1.5 INCHES IN LENGTH. C/A: SNRM N0235 LT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT CRACKED PANEL REMOVED IAW AMM 20-50-02, REPLACED WITH NEW PANEL BY FABRICATION IAW EA 1-5750-75180, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, WING PANEL FABRICATION. 2L73 4F4 FRTA22WE E13NE 20031106000662003110600066NM 2003 11 6 SWAA032296 120031018A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031106001152003110600115NM 2003 11 6 03FDEA01826 120031029A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-224-01, 3) FLOORBEAM BS 1050, LBL 27, WL 208. BLENDED CORROSION ON TOP CHORD OF FLOORBEAM IN A 1 X 1 X .029 INCH FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 4. REMOVED TOP OF CHORD FROM LBL 19 TO 30.5 AND INSTALLED REPAIR PER SRM 53-10-8 FIG 1. 2L73 4F RTA3WE 20031106002352003110600235EU 2003 11 6 ASOA03456 120030923A3250GA62055 BRACKET AEROSPATR72 ATR72212 8680945EU NLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE STEERING UNIT BRACKET ON THE NOSE STRUT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE STEERING UNIT BRACKET ON THE NOSE STRUT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031107000172003110700017SO 2003 11 7 C2XA03SH430 120031107A532014525480003 THRESHOLD EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK THE CARGO DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031107000202003110700020WP 2003 11 7 MWEA030438 120031103A53475936663503 CARGO TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 REMOVED AFT CARGO PIT TIE DOWN RAIL ABOVE LONGERON 27 LEFT TO FACILITATE OTHER MAINTENANCE, FOUND CARGO RAIL CORRODED. FABRICATED AND INSTALLED REPAIR SPLICE. 2L72 4F A6WE 20031107001022003110700102EA 2003 11 7 03307620 120031103A33503071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27620BR 7179 DURING INSPECTION THE RIGHT BULKHEAD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE BULB WAS REPLACED. 2L72 4F RTA21EA 20031107001232003110700123EA 2003 11 7 ASOA03504 120031002A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11717EV 10088 FLT 4247 - DURING CLIMB-OUT FROM PHF-ATL, THE FLIGHT ATTENDANT REPORTED A JET FUEL ODOR IN THE CABIN FOR APPROXIMATELY FIVE MINUTES AFTER TAKEOFF. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSPECTED THE EXTERIOR OF THE AIRCRAFT WITH NO FUEL LEAKS FOUND. MAINTENANCE ALSO INSPECTED THE INTERIOR OF THE AIRCRAFT AND RAN THE RIGHT PACK ON FULL HOT WITH NO ODORS DETECTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031107001352003110700135SO 2003 11 7 SIMA200327904 120030930A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. REMOVED CORROSION CREATING A CUTOUT IN THE FLANGED AND WEB AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 22, 53-21-10 FIG 201 SHEET 2 AND CPM 51-21-06. (M) 2L72 4F RTT00011AT 20031107001432003110700143WP 2003 11 7 GTIA030735 120030923A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND MAIN CABIN STATION 674 TO STATION 593 HAS CRACKED/DAMAGED ON EDGE. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20031107001442003110700144WP 2003 11 7 AMTA200301279 120030806A5743 SUPPORT LKHEED1011 10113851 5265010WP LT WING DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 INTERIM REPAIR OF LEFT MUG TRUNNION LOWER SUPPORT FLANGE REQUIRES PERMANENT REPAIR. APPLIED PERMANENT REPAIR TO BLENDOUTS PER ER/A L10-57R-4752. (M) 2L73 4F A23WE 20031107001472003110700147WP 2003 11 7 GTIA030743 120030825A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FORWARD PIT CEILING FS 225 LBL 57 FEET WEB CRACKED AND CORRODED. REMOVED DAMAGED WEB. DRILLED AND LOCATED NEW WEB AND DOUBLER. INSTALLED NEW WEB/DOUBLER. (M) 2L72 4F A6WE 20031107001632003110700163NM 2003 11 7 AALA20031061 120030924A33500201991008 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21646AA 24604 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT 29D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031107001642003110700164NM 2003 11 7 AALA20031062 120030924A33500201991008 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21646AA 24604 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT 27D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031110000582003111000058SO 2003 11 10 C2XA03SH434 120031109A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110000592003111000059SO 2003 11 10 RAIA00309269 120030920A7830 THRUST REVERSER EMB 145 EMB145 3260210SO NR 1 OUT OF RIG A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03805HK 145096 5310-MKE- NR 1 THRUST REVERSER DISAGREE. MAINTENANCE DEFERRED T/R NR 1 IAW MEL 78-34-00. SUBSEQUENTLY CLEARED DMI BY PERFORMING THRUST REVERSER RIGGING PER EMB 78-31-01. 2L72 4F RTT00011AT 20031110000612003111000061SO 2003 11 10 RAIAOO3O9268 120030914A79304352432 INDICATOR EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03811HK 145256 5299-MDT- ENGINE NR 2 IMPENDING BYPASS MESSAGE. MAINTENANCE INSPECTED NR 2 ENGINE OIL FILTER BYPASS PIN AND DEFERRED PER MEL 79-35-1. SUBSEQUENTLY CLEARED DMI BY REMOVING ELECTRICAL OIL IMPENDING BYPASS INDICATOR. 2L72 4T RTT00011AT 20040112002502004011200250WP 2004 1 12 AALA20031458 120031221A2560 SHIELD DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21410AA 49321 AFT EMERGENCY FLASHLIGHT LOWER RETAINING STRAP BROKEN. REPLACED AFT EMERGENCY FLASHLIGHT SHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040113000242004011300024SW 2004 1 13 HEEA087815 120030320A6730C4264215 SLEEVE BELL 206 206L1 1182107SW CYLINDER FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032761N RH0949 45277 SLIDE AND SLEEVE CAUSING EXCESSIVE LEAKAGE AND PROOF PRESSURE DURING FINAL TEST. REPLACED. 1G71 3U H2SW 20040113000382004011300038EU 2004 1 13 YENA200342 120031219A3234114079016 SELECTOR VALVE AIRBUS320 A320232 3930326EU LANDING GEAR MALFUNCTIONED A YENAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA15544JB5473 1835 DURING EXECUTION OF MISSED APPROACH AT LAS, RECEIVED L/G GEAR NOT UPLOCKED ECAM STAYED IN RADAR PATTERN FOR VISUAL, PUT GEAR DOWN GOT 3 GREEN, DOWN AND LOCKED ON 2ND APPROACH. NO INDICATIONS ON WHEEL PAGE OTHER THAN AMBER L/G ON INITIAL MESSAGE. REMOVED AND REPLACED L/G DOOR SELECT VALVE PER AMM 32-31-34. PERFORMED OPERATIONAL EXTENSION RETRACTION PER 32-31-00-710, OPS CHECK OK. 2L72 4F RTA28NM 20040113000512004011300051EA 2004 1 13 COMA0360568 120031220A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO01798CA 7348 FLIGHT 5745 CONFIG SPOILERS CAUTION DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040113000522004011300052EA 2004 1 13 COMA0360569 120031220A27507805013 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01967CA14786 7134 FLIGHT 5753 FLAPS FAIL MESSAGE. REPLACED THE FLAP CONTROL LEVER. 2L72 4F RTA21EA 20040113000592004011300059EU 2004 1 13 MALA030566 120031204A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4K INSPECTION IN LAKE CITY, FS 294 RIGHT SEAT TRACK HAS CORROSION. REMOVED AND REPLACED CORRODED SEAT TRACK SECTION FROM FS 284 TO FS 339 IAW MESABA EO 53060 DATED NOV 3, 2003 REV II. 2L72 4T RTA52EU 20040113000612004011300061EU 2004 1 13 MALA030567 120031204A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4K INSPECTION, SEAT TRACK ON RIGHT SIDE BETWEEN STA 240 AND 258 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED CORROSION SEAT TRACK, FABRICATED NEW SEAT TRACK FROM RIGHT STA 215 TO 225 BUTTLINE 12 P/N 7253721-459 IAW SRM 51-40-40 & 51-40-27. 2L72 4T RTA52EU 20040113000622004011300062EU 2004 1 13 MALA030563 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C0-CHECK INSPECTION, FOUND 14A AND 14D FRAMES CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAMES 14A & 14D IAW MESABA EO A25031. DATED FEB 6, 2001 REV IR. 2H74 4F RTA49EU 20040113000692004011300069EU 2004 1 13 BAQA091660 120031219A5330L633M2010104 MOUNT UROCOPEC135 EC135P2 EU M/R GEARBOX LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03868ME12 0288 MAIN ROTOR GEARBOX MOUNT LEAKING. PART REPLACED WITH SERVICABLE UNIT. 1G72 3U H88EU 20040113000802004011300080NM 2004 1 13 03FDEA02241 120031223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR INBOARD MOUNT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75217 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS 2L73 4F RTA22WE 20040113001302004011300130EU 2004 1 13 BAQA091137 120031205A6710L673M40A1001 ACTUATOR UROCOPEC135 EC135P1 8680990EU FENESTRON WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME1875 0009 WARRANTY. WORN BEYOND LIMITS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 12/8/03 1G72 3U O H88EU 20040113001402004011300140EU 2004 1 13 BAQA091408 120031206A6720 BUSHING BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE T/R ACTUATOR DEFECTIVE D BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117NC1997 00566 7517 TAIL ROTOR ACTUATOR LOWER BUSHING DEFECTIVE. REPLACED WITH SERVICEABLE UNIT. 12/11/03 1G72 3U3 UNCH13EU E19EU 20040113001422004011300142NM 2004 1 13 03FDEA02262 120031226A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT WING, O/B FLAP I/B FWD HINGE ACTUATOR MOUNT I/B LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75209, TRAILING EDGE AND TRAILING EDGE DEVICES - RH OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113001472004011300147 2004 1 13 BAQA090343 420031030A3120JB15307 CLOCK BOLKMS117 BK117B1 5626012EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME1688 7235 CLOCK INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20040112000972004011200097NM 2004 1 12 F3LA200300182 120031219A5310 SHEAR TIE BOEING737 73736N 1384408NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED SHEAR TIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20040112001552004011200155WP 2004 1 12 GTIA031001 120031113A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - CABIN METAL FLOOR PANEL IS CRACKED AT FS 484 RIGHT OUTBOARD PANEL. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040112001632004011200163NM 2004 1 12 03FDEA02225 120031220A5720ARB0029507N STRAP DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 CRACK FOUND ON THE LOWER EDGE OF THE BOTTOM BOLT HOLE / OUTBD FLAP INBOARD HINGE TENSION STRAP SUPPORT - LT WING. DAMAGED HINGE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. NEW TENSION STRAP INSTALLED AS PER SRM 51-33-01 VOL. II. REFER TO FEDEX EO 1-5750-7-5004 , OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORTS. 2L73 4F RTA22WE 20040112001662004011200166WP 2004 1 12 AALA20031235 120031109A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217537A 49991 DFW - DURING OVERNIGHT MAINTENANCE, FOUND AFT TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT TAIL COMPARTMENT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112002082004011200208EA 2004 1 12 A6WA200340165 120031111A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31401AW 7280 RT FUSELAGE SKIN AT FS 680.5 STRINGER 24R HAS LIGHTNING DAMAGE AND TEMPORARY REPAIR IAW REO 601R-53-00-084 REV. A. REMOVED DAMAGED AREA OF SKIN, FABRICATED FILLER AND A DOUBLER FROM 2024-T3 .063 INCH WVAC PO NR 27603/1, INSTALLED IAW WVAC 601R-53-4388. 2L72 4F RTA21EA 20040112002372004011200237WP 2004 1 12 AALA20031447 120031219A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 AFT CABIN CEILING EMERGENCY LIGHTS AT STATION 1336 INOPERATIVE. REPLACED AFT CABIN CEILING EMERGENCY EXIT LIGHT ASSEMBLY L2-671. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20040112002392004011200239WP 2004 1 12 AALA20031449 120031219A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN FAULTY A AALAK NONE O OTHER ININSP/MAINT 1 SW21291AA 49303 FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT WILL NOT EXTINGUISH WITH SWITCH IN OFF POSITION. REPLACED FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002492004011200249WP 2004 1 12 AALA20031457 120031221A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21428AA 49340 SEAT MOUNTED EMERGENCY LIGHT AT 28D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040113000442004011300044EA 2004 1 13 COMA0360563 120031218A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01926CA 7027 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040113000912004011300091 2004 1 13 BAQA090687 420031107A23126226389001 RADIO AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE VHF INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 71 6036 VHF RADIO DOES NOT TRANSMIT. PART INSTALLED ON 9/24/03. LASTED ONLY 71.2 HOURS. REPLACED WITH SERVICEABLE UNIT. 11/24/03 1G72 3U3 U H10EU E19EU 20040113001132004011300113EU 2004 1 13 BAQA091189 120031028A3150C19209VG11 DISPLAY UROCOPEC135 EC135T1 5620026EU COCKPIT INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH551 0131 DISPLAY UNIT INOPERATIVE. F CODE ON START UP. INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040113001772004011300177EU 2004 1 13 MALA030568 120031219A3230D49412001 CONTROL UNIT SAAB SF340 340B 7860101EU E/E BAY FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15417XJ 340B417 DURING FLIGHT 3114, ON GEAR RETRACTION HYDRAULIC PUMP DID NOT RUN AND INTRANSIT LIGHT DID NOT COME ON. AIR RETURN TO MSP. MAINTENANCE REPLACED LANDING GEAR CONTROL UNIT P/N D494-12-001, S/N OFF 620/10-96, S/N ON 619/10-96, IAW AMM 32-31-05-2, OPS CHECKS GOOD. 2L72 4T RTA52EU 20040113001872004011300187EU 2004 1 13 RAIA00312302 120031205A2913384925 PUMP JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03572HK2441314621 41091 PIT- HYDRAULIC PRESSURE LOW NR 2. MAINTENANCE REMOVED AND REPLACED NR 2 HYD PUMP. 2L72 4T RTA41NM 20040113002302004011300230NM 2004 1 13 QXEA200301587 120031226A5330 SKIN DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 RT FORWARD FUSELAGE SKIN DENTED AT STATION X226.20 AND Z140.00. DENT IS 1.5 INCHES LONG, 1.3 INCHES WIDE AND 0.073 INCHES DEEP. REPAIRED IAW DHC-8 RD 8-53-2181. 2H72 4T4 TRTA13NM E20NE 20040113002382004011300238NM 2004 1 13 QXEA200301301 120031019A242111522184 GENERATOR BOMBDRDHC8 DHC8401 1390041NM NR 2 FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09408QX5030 4050 SEA-ON FLIGHT NUMBER 2387, NR 2 AC GEN CAUTION LIGHT ILLUMINATED JUST AFTER ROTATION, RAN CHECKLIST AND NR 2 AC GEN CAUTION REMAINED ILLUMINATED AFTER RESET. REMOVED AND REPLACED NR 2 AC GEN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040113002422004011300242NM 2004 1 13 QXEA200301312 120031020A5411 FRAME BOMBDRDHC8 DHC8401 1390041NM NR 1 NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX - NR 1 ENGINE FORWARD HORSE SHOCK MOUNT FRAME HAS CHAFED AREA AT ONE O'CLOCK POSITION ON AFT EDGE OF FRAME. REPAIRED IAW HORIZON AIR EA 6-54-275. 2H72 4T RTA13NM 20040113002432004011300243NM 2004 1 13 QXEA200301313 120031020A7110 WEB BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX - NR 1 LOWER COWLING CENTER SUPPORT WEB CRACKED. REPAIRED IAW RD 8/4-71-016 AND RD 8/4-71-053. 2H72 4T RTA13NM 20040113002482004011300248NM 2004 1 13 QXEA200301499 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- NR 3 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF LT RAIL AT X531. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD'S 8-53-3644 AND 8-53-1342. 2H72 4T RTA13NM 20040113002492004011300249NM 2004 1 13 QXEA200301357 120031029A3030C16193AB PROBE BOMBDRDHC8 DHC8401 1390041NM PITOT/STATIC SYSFAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09400QX 4030 SEA- PITOT HEAT STANDBY CAUTION LIGHT ILLUMINATED. WENT THROUGH CHECKLIST AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED STANDBY PITOT-STATIC PROBE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040113002562004011300256SO 2004 1 13 C2XA03SH516 120031226A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A FILLER AND SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040114000032004011400003CE 2004 1 14 DXTA200300159 120031110A2435 STARTER GEN CESSNA560 560XL 2076702CE PWA 545 PW545A NE LT ENGINE FAILED E DXTAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07625QS 5605319 PCEDB0653 LEFT ENGINE FAILED TO START ON FIRST ATTEMPT N2 DID NOT INCREASE PAST 10 PERCENT. SECOND ATTEMPTED START NR N2 INDICATION AT ALL DISCONNECTED START SEQUENCE BLEW FIRE BOTTLES AS A PRECAUTIONARY MEASURE DUE TO EXCESSIVE SMOKE FROM ENGINE. TROUBLESHOT AND FOUND LT STARTER GENERATOR DEFECTIVE, REMOVED & REPLACED LT STARTER GENERATOR. REMOVED & REPLACED BOTH FIRE BOTTLES, RAN ENGINE AND OPS CHECKS GOOD IAW CE560XL MM 80-10-00, 26-21-01. 2L72 4F4 FRTA22CE E00059EN 20040114000072004011400007NM 2004 1 14 AWXA200301427 120031115A56105893543130 WINDSHIELD BOEING737 7373G7 1384595NM COCKPIT FAILED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28308AW15667 24710 EN ROUTE, 1ST OFFICERS WINDSHIELD ARCED THEN A LOUD THUD WAS HEARD RESULTING IN NUMEROUS CRACKS TO OUTER PANE, TURNED BACK TO PHX & LANDED WITHOUT EVENT. MAINT R & R 1ST OFFICERS WINDSHIELD IAW T/C R1B56001, & WINDOW HEAT CONTROL UNIT IAW BMM, OPS CK GOOD. VENDOR DID NOT PERFORM FAILURE ANALYSIS OF 1ST OFFICERS WINDSHIELD BUT DID FIND WINDOW FAILED DUE TO MOISTURE INGRESSION THAT REACHED ELECTRICAL SYSTEM CAUSING THE WINDOW TO ARC & FRACTURE OUTBOARD PLY GLASS. VENDOR ALSO CONFIRMED FAILURE OF WINDOW HEAT CONTROL UNIT FOR FAILING OUTPUT TEST. TEARDOWN REVEALED VARISTORS RV1 THRU RV4, AND DIODES CR39 & CR40 DEFECTIVE. REPLACED 4 EACH VARISTORS & 2 EACH DIODES. UNIT WAS CLEANED, REPAIRED, & REASSEMBLED IAW CMM.2L72 4F RTA16WE 20031119001272003111900127NM 2003 11 19 2003UALA00757 120031007A5330 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 FUSELAGE SKIN 30 INCHES AFT OF L4 DOOR, WL 200.3 WAS GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIR WITH DOUBLER AND FILLER. 2L72 4F4 FRTT0001SE E46NE 20031119001282003111900128NM 2003 11 19 2003UALA00760 120031005A5320 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 STRINGER CLIP AT STA 727C LBL 52 CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20031119001312003111900131NM 2003 11 19 2003UALA00763 120031005A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 FORWARD CARGO DOOR FRAME GOUGED STA 490. MAJOR REPAIR ACCOMPLISHED. BLENDED AREA AND INSTALLED REPAIR PARTS. 2L72 4F4 FRTA16WE E2GL 20031119001372003111900137WP 2003 11 19 MWEA030417 120031013A532199365821 FLOOR PANEL DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE CABIN DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 ELEVEN SMALL HOLES IN CENTER FLOOR PANEL STATION 258. REPAIRED FLOOR PANEL. 2L72 4F4 F A6WE E2EA 20031119001412003111900141NM 2003 11 19 QXEA200301229 120031006A5410 SPAR DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX- BRACKET CRACKED AT YW128.0R, RIGHT HAND FWD SPAR NEXT TO NR 2 ENGINE NACELLE. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20031120000112003112000011NM 2003 11 20 AWXA200301220 120030921A532069353521 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP BS 380, STR 7 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP BS 380, STR 7 LT; INSTALLED NEW REPLACEMENT TIE CLIP IAW B737-300 SRM 51-40-02, PG 1, FIG 8. 2L72 4F RTA16WE 20031120000132003112000013NM 2003 11 20 AWXA200301222 120030919A53306545778104 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON FUSELAGE SKIN OF LOWER R-2 DOOR HINGE CUTOUT BS 947. MAINTENANCE CUTOUT CRACK ON FUSELAGE SKIN OF LOWER R-2 DOOR HINGE CUTOUT BS 947 AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER, TRIPLER, AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG 207, SHEETS 1 & 5. 2L72 4F RTA16WE 20031120000202003112000020NM 2003 11 20 AWXA200301229 120030922A57536546431280 SKIN BOEING737 737301 1384611NM TE FLAP CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK THE UPPER SURFACE OF RT OUTBOARD FORE FLAP HAS A CHAFE MARK AT OUTBOARD END OF NR 7 SPOILER. MAINTENANCE REMOVED DAMAGE RT OUTBOARD FORE FLAP AT OUTBOARD END OF NR 7 SPOILER; CLEANED AND PREPARED SURFACE; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, REPAIR 7, FIG 16. 2L72 4F RTA16WE 20031120000252003112000025NM 2003 11 20 AWXA200301234 120030924A53126516300294 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB ON FORWARD SIDE AT EDGE OF STRAP RUNNING VERTICALLY, RBL 4.75, WL 212. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB ON FORWARD SIDE AT RBL 4.75, WL 212; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG 287-288J, FIG 211. 2L72 4F RTA16WE 20031106001392003110600139EA 2003 11 6 SWIA200312528 120031025A3230 ROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG LACK OF LUBE A SWIAO OTHER O OTHER DEDESCENT 1 NM07958SW 7833 LEFT MLG WOULD NOT COME DOWN WHEN THE GEAR LEVER WAS SELECTED DOWN. USED THE MANUAL GEAR RELEASE PER QRH. CLEANED AND LUBED ROLLER AS REQUIRED. ALL OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031106001672003110600167SO 2003 11 6 C2XA03CL181 120031027A335078241 INVERTER EMB 145 EMB145ER 3260211SO ALLSN AE3007AE3007C GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712946 145052 DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT SIGN INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031107000232003110700023SO 2003 11 7 C2XA03TY189 120031104A532014525480003 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR SILL. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-20-03 AND 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031107000352003110700035NM 2003 11 7 HNAA0300064 120031105A531385530150 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE DAMAGED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07930HA 126 MAJOR REPAIR: SPLICE OF STR 31S IN AFT FUSELAGE. 2H72 4T RTA13NM 20031107000592003110700059NM 2003 11 7 03303421 120031030A801135059783 STARTER DORNERDO32 DO328300 NM LT ENGINE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27421FJ 3179 DURING INSPECTION THE AIR TURBINE STARTER ON LEFT HAND ENGINE HAD CORROSION IDENTIFIED ON THE OUTLET FLANGE. 2H72 4T RTA55NM 20031107001412003110700141NM 2003 11 7 ASAA0310489 120030526A5313 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND STRINGER 27L AT FUSELAGE STATION 807-827 CORRODED. REPAIRED STRINGER PER EA. (M) 2L72 4F A16WE 20031107001542003110700154WP 2003 11 7 GTIA030738 120030923A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND MAIN CABIN RIGHT SIDE OUTBOARD STATION 1174 TO STATION 1193 FLOOR PANEL CRACKED/DAMAGED ON EDGE. FABRICATED FLOOR PANEL. (M) 2L72 4F A6WE 20031110000722003111000072CE 2003 11 10 AMWA69 120031105A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE23 WHILE PERFORMING AND INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE NEAR THE FWD, CENTER STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031110000842003111000084NM 2003 11 10 03FDEA01882 120031024A5315651627910 FLOORBEAM BOEING727 72723 1384004NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270 22035 CORROSION AROUND SEVERAL NUT PLATE HOLES IN LONG FLOORBEAM LBL 25, WL 208, BS 760-850. 2L73 4F A3WE 20031110001442003111000144NM 2003 11 10 AWXA200301196 120031008A21216067723 FAN BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE ZONE 126 FAILED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28913AW4039 22207 ON DEPARTURE OUT OF PHX EN ROUTE FOR DFW ELECTRICAL ODOR FILLED THE FLIGHT DECK, TURNED BACK & LANDED WITHOUT FURTHER EVENT. FLT ATTENDANT REPORTED A BURNING ELECTRICAL ODOR FROM SEAT ROW 27 AFT. MAINTENANCE INSPECTED BOTH FORWARD AND AFT EQUIPMENT CENTERS, NO DEFECTS OR CIRCUIT BREAKERS WERE POPPED. REMOVED AND REPLACED RT RECIRCULATION FAN IAW T/C R2B21601, OPERATIONAL CHECK WAS GOOD. VENDORS FUNCTIONAL CHECK OF CIRCULATION FAN S/N 1348 WAS NO FAULT FOUND. RECEIVING INSPECTION IDENTIFIED A BROKEN MOUNT EAR, UNIT WAS DISASSEMBLED AND WORN BEARINGS WERE ALSO IDENTIFIED. REPLACED MOUNT BRACKET, AND 2 EACH BEARINGS. UNIT REPAIRED AND RETURNED TO SERVICE IAW CMM 21-25-04, REV. 5. 2L72 4F4 FRTA2NM A12EU 20031110001522003111000152SO 2003 11 10 C2XA03BT097 120031019A32347455501 CONTROL LEVER EMB 145 EMB145 3260210SO COCKPIT FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149721071410714 145151 EWR---CO3418, CREW REPORTED, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. EICAS MESSAGE LDG GEAR DISAGREE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM 32-32-00, AND PERFORMED SEVERAL LANDING GEAR EXTENSIONS AND RETRACTIONS IAW EMB145 MM 32-30-00. NO FURTHER FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031110001702003111000170NM 2003 11 10 UPS03441447 120031012A532065B0793684 SUPPORT ANGLE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D - BS 400, BET STR 22 - 24R FRAME I/B CHORD O/B FACE ATT SUPPORT ANGLE FOUND CRACK. M/D STA 400 BTN STR 22R - 24R FRAME I/B CHORD SUPPORT ANGLE REPLACED WITH SERVICEABLE PART AS PER SRM 51-30-02. 2L74 4F RTA20WE 20031110001782003111000178NM 2003 11 10 SWAA032249 120031013A335065C27095 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED C3 CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHT ASSY INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20031110001942003111000194NM 2003 11 10 SWAA032239 120031012A575465C26686 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED OUTBD OF MAIN TRACK. REPAIRED SLAT SKIN PER SRM. 2L72 4F RTA16WE 20031110001972003111000197NM 2003 11 10 SWAA032242 120031010A25606557463 BRACKET BOEING737 7373H4 1384600NM R1 ENTRY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED SPECIAL VISIT, FOUND R1 DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM. 2L72 4F RTA16WE 20031120000312003112000031NM 2003 11 20 AWXA200301240 120030922A532065C10592158 FILLER BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FILLER PLATE BS 951, RBL 49, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FILLER PLATE BS 951, RBL 49, WL 208; FABRICATED A TAPERED FILLER PER DWG 65C10592; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031120000352003112000035NM 2003 11 20 AWXA200301244 120030921A532069434772 CHANNEL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A .75 INCH CRACK WAS FOUND ON FLOOR ATTACH CHANNEL BS 787, ABOVE STRINGER 26 RT. MAINTENANCE REMOVED CRACKED FLOOR ATTACH CHANNEL BS 787, STR 26 RT; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20031120000362003112000036NM 2003 11 20 AWXA200301245 120030919A53136972495 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON STRINGER 18A RT HORIZONTAL LEG, AT BS 725. MAINTENANCE CUT OUT CRACKED SECTION OF STRINGER 18A RT AT BS 725 AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR FILLER AND RADIUS FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5314-03284-ES1. 2L72 4F RTA16WE 20031120000572003112000057NM 2003 11 20 QXEA200301246 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 5 SEAT TRACK TOP FLANGE IS GOUGED AND DENTED AT CUTOUT AT STATION X445.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20031120000722003112000072NM 2003 11 20 QXEA200301260 120030928A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NUMEROUS ROCK CHIPS AND SCRATCHES IN LOWER FUSELAGE SKIN AT STATION 302.0 THROUGH 312.0 AND STRINGER 29 RIGHT HAND AND LEFT HAND. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16, 20-32-02, 20-34-08, 51-20-16, 51-20-36 AND 51-20-51. 2H72 4T RTA13NM 20031120000752003112000075NM 2003 11 20 QXEA200301263 120030929A5320 WEB DHAV DHC8 DHC8202 2809007NM ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 TURTLEBACK SUPPORT STRUCTURE WEB IS WORN THROUGH AT BLEED AIR SUPPORT ANGLE. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-5437. 2H72 4T RTA13NM 20031120000772003112000077NM 2003 11 20 HN62003F00001 120030929A2897 WIRE BOEING767 76733A 1385209NM FUEL BOOST PUMP ARCED B HN6RO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM01583HA 25531 WHILE WORKING SB NR 767-28A0077, THE MECHANIC REMOVED 2 EACH LT WING AND 2 EACH RT WING FUEL BOOST PUMPS. HE DISCOVERED ELECTRICAL ARCING DAMAGE ON BOTH LT WING AND BOTH RT WING BOOST PUMPS. UPON FURTHER INVESTIGATION FOUND ADDITIONAL ELECTRICAL ARCING ON BOTH LT WING AND RT WING BOOST PUMP SLEEVES AND BOOST PUMP HOUSINGS. EO 28-03-01-72. 2L72 4F RTA1NM 20031120000902003112000090NM 2003 11 20 P5CA0300967 120031014A2410 CSD BOEING747 7472U3B 1384846NM NR 2 & 4 MALFUNCTIONED A P5CAD RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 WP23923FT 22769 ON TAXI, NOTED NR 2 & 4 GENERATOR SHOWED NO KW'S AND NO VOLTAGE FREQUENCY. ALSO, NR 3 CSD LIGHT ON FLIGHT ENGINEER'S PANEL - READ ANNUNCIATOR. SERVICED NR 2 & 4 CSD'S. RAN ENGINES AND DISCONNECTED NR 2 & 4 CSD'S. RECONNECTED NR 2 & 4 CSD'S. RE-RACKED GCU AND BPCU. CHECKED VOLTS AND OHMS ON CONNECTOR TO AC VOLTMETER PANEL, ALL CHECKS SATISFACTORY. DMI CLEARED. 2L74 4F RTA20WE 20031120001152003112000115NM 2003 11 20 SWAA032454 120031106A53206551698 ANGLE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TO FRAME ANGLE CRACKED AT BS 294.5 STR 23L. REPAIRED PER SRM. 2L72 4F RTA16WE 20031120001282003112000128NM 2003 11 20 AWXA200301453 120031104A55236562635415A TAB BOEING737 7373G7 1384595NM ELEVATOR TRIM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK A .375 INCH CRACK WAS FOUND ON LT ELEVATOR TRIM TAB IN UPPER CORNER AT INBOARD ATTACH POINT. MAINTENANCE PERFORMED BOND REPAIR ON LT ELEVATOR TRIM TAB IN UPPER CORNER AT INBOARD ATTACH POINT IAW B737-300 SRM 51-70-17 FIG 8 PG 2 REPAIR 10. 2L72 4F RTA16WE 20031120001322003112000132NM 2003 11 20 AWXA200301457 120031028A575465C2670128 ANGLE BOEING737 7373G7 1384595NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 DURING C-13 CHECK A .375 INCH CRACK WAS FOUND IN ZEE ANGLE AT RT WING LEADING EDGE, INSIDE ACCESS PANEL 5848, ON OUTBOARD SIDE AT SLAT STA 2.5. MAINTENANCE REMOVED DAMAGED ZEE ANGLE AT RT WING LEADING EDGE INSIDE ACCESS PANEL 5848; FABRICATED A NEW REPLACEMENT ZEE ANGLE PER DWG 65C26701; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4 & 8 PG 1, 28-29 & 38. 2L72 4F RTA16WE 20031121000282003112100028EA 2003 11 21 03317709 120031113A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27709BR DURING CLIMB OF FLIGHT 7471 CREW REPORTED A NOSE WHEEL STEERING INOPERATIVE AND NOSE GEAR DOOR OPEN MESSAGE. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY AT GATE. MAINTENANCE PERFORMED A NWS SYSTEM OPERATIONAL CHECK AND FOUND NO FAULTS. 2L72 4F RTA21EA 20031121000362003112100036CE 2003 11 21 AMWA80 120031104A533011443000002200 PRESSURE PANEL ABACUS BEECH 1900 1900D 1154162CE FUSELAGE CHAFED A AMWAO OTHER O OTHER ININSP/MAINT 1 CE07127YV UE127 WHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, RIVET HEAD CHAFED WAS FOUND TO THE RIGHT PRESSURE PLATE, RBL 30.28. 2L72 4T RTA24CE 20031121000492003112100049NM 2003 11 21 SWAA032487 120031110A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED A2 CHECK, FOUND LT WING OUTBD T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20031121000532003112100053 2003 11 21 SWAA032491 420031110A25651061323 SLIDE BOEING737 7373H4 1384600NM R2 DOOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVACUATION SLIDE GIRT ASSY WORN. REMOVED AND REPLACED SLIDE ASYY PER MM. 2L72 4F RTA16WE 20031121000622003112100062CE 2003 11 21 DXTA200300163 120031114A3260327 LIGHT CESSNA500 560CESSNA 2076750CE MLG INDICATOR INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07396QS 5600396 ON APPROACH LT MAIN LANDING GEAR GREEN LOCKED LIGHT DID NOT ILLUMINATE, EMERGENCY GEAR BLOW DOWN ACCOMPLISHED. FOUND LT MLG COCKPIT GEAR WARNING LIGHT INOP. REMOVED AND REPLACED LAMP, OPS CHECK GOOD IAW CITATION 560 MM CHAPTER 32-60-00. JACKED AIRCRAFT IAW CITATION 560 MM CHAPTER 7-10-01, CYCLED THE LANDING GEAR IAW CITATION 560 MM 32-01-00, DOWN JACKED AIRCRAFT, SERVICED HYDRAULIC RESERVOIR IAW CITATION 560 MM CHAPTER 12-12-01, SERVICED PNEUMATIC BOTTLE IAW CITATION 560 MM CHAPTER 12-13-01. 2L72 4F RTA22CE 20031121000712003112100071SO 2003 11 21 C2XA03SD003 120031107A79307013348940 DAU EMB 145 EMB145LR 3260212SO ENGINE FALSE INDICATIONA C2XAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SW272991710318 145414 AT TAKEOFF PRIOR TO 80 KNOTS BOTH ENGINE PRESSURE IN AMBER AT 105 PSI AND RIGHT ENGINE IN THE RED. NO ALARMS. ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 DAU IAW EMB AMM 31-41-01. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20031121000782003112100078NM 2003 11 21 03FDEA01944 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 LEFT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING ACTUATOR MOUNT HOLE OUTBOARD CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20031121000872003112100087NM 2003 11 21 CALA0300651 120031118A5342 ATTACH ANGLE BOEING737 737524 1384721NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711651 28912 INSPECTION FOUND ATTACH ANGLE ON LT SIDE OF VERTICAL STABILIZER ON FUSELAGE EXTERIOR AT STA 1121 GOUGED. A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013. 2L72 4F RTA16WE 20031121000912003112100091NM 2003 11 21 03FDEA01941 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 LEFT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING BARREL NUT BOLT HOLE UPPER CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031124000062003112400006EA 2003 11 24 SWIA200312593 120031109A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM DISCONNECT FAILED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07590SW 7077 STAB TRIM AND MACH TRIM FAILED SHORTLY AFTER TAKEOFF AND WOULD NOT RESET. RETURNED TO FIELD. REMOVED AND REPLACED COPILOT'S STAB TRIM DISCONNECT SWITCH IAW MM 27-41-30. OPS CHECK GOOD. P/N ON & OFF 996-0013. 2L72 4F RTA21EA 20031124000102003112400010 2003 11 24 SWIA200312597 420031110A3418C818022 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE STICK SHAKER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM0757734 120199 CAPTAINS STICK SHAKER INOP. REMOVED AND REPLACED CAPTAIN'S STICK SHAKER. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031124000112003112400011EA 2003 11 24 SWIA200312598 120031114A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07926SW752 752 7687 STAB 1 CH INOP STATUS MESSAGE DISPLAYED ON FINAL APPROACH. REMOVED AND REPLACED HSTCU IAW CRJ MM 27-40-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20031124000462003112400046EA 2003 11 24 03307625 120031103A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING INSPECTION THE AFT STRIP OF EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. 2L72 4F RTA21EA 20031124000482003112400048EA 2003 11 24 03319705 120031115A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 DURING INSPECTION THE FOWARD EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE EMERGENCY PATH LIGHTING STRIP WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031124000532003112400053NM 2003 11 24 03FDEA01891 120031107A5315 FLOORBEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 CORROSION ON UPPER CHORD OF FLOORBEAM BS 1130 RBL 61 WL 208. *S/D* REMOVED CORROSION FROM UPPER CHORD BS 1130 FLOORBEAM, RBL 61, WL 208 AND FOUND OUT OF LIMITS. REMOVED CORRODED SECTION OF BEAM. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS. ALL WORK DONE IAW SMR 53-10-8. 2L73 4F RTA3WE 20031124000582003112400058NE 2003 11 24 MASA200300440 220031106A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 DAMAGED A MASAE ENGINE SHUTDOWN E VIBRATION/BUFFET DEDESCENT 1 SW074720213529 7202 872295 ON DESCENT TO YOW PILOT FELT THE A/C SHUTTER. THE PILOT THAN NOTICED THE NR 2 ENGINE VIBS FOLLOWED BY HIGH ITT AND LOW OIL PRESSURE. AN IN-FLIGHT SHUTDOWN WAS INITIATED. AFTER AN UNEVENTFUL LANDING MX WAS CALLED. AFTER A BORESCOPE OF THE ENGINE IT WAS DETERMINED THAT THE ENGINE NEEDS TO BE REPLACED. MX IN THE PROCESS OF REPLACING THE ENGINE. ERTS 11/9/2003. 2L72 4F4 FRTA21EA E15NE 20031124000722003112400072NM 2003 11 24 CALA0300646 120031114A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME FITTING JUST BELOW CABIN FLOOR AT BOTTOM TWO FASTENERS, STA 616, W/ 200, LT SIDE. REPAIRED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20031124000862003112400086WP 2003 11 24 DHL2003807543 120031019A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLOT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RT WING INBD VANE SLOT UPPER SKIN CORRODED AT STA XILD 0.7095. (MAJOR REPAIR) PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW NDT STANDARD PRACTICE MANUAL PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW ASTAR ED EDU21-11, ASTAR DWG U21-R11. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ASTAR ED EDU21-11, ASTAR DWG U21-R11, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031124000922003112400092WP 2003 11 24 DHL2003802521 120031117A53203754473U1 SPLICE DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 FWD CARGO COMPT SPLICE FITTING 2.000 CRACK (STA 380.000-400.000, L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031124000992003112400099WP 2003 11 24 DHL2003802509 120031110A534752772660 CARGO TRACK DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT NR 4 TRACK FLANGE CORRODED, STA 952.000. REMOVED FASTENERS IAW SRM 51-3-0 PG 1. REMOVED CORROSION FROM NR 4 TRACK FLANGE, STA 952.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-3 FIG 12. CUT OUT NR 4 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 49-50. FABRICATED SPLICES IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES AND FASTENERS IAW SRM 53-2-3 PG 49-50 FIG 14. 2L74 4F RT4A25 20031124001212003112400121WP 2003 11 24 DHL2003805500 120030811A5320 CHANNEL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 NOSE SECTION INTERIOR LEFT TUNNEL CHANNEL CRACKED 2.000, STA 17.000, L32L - L35L. REMOVED CRACKED CHANNEL IAW SRM 51-1-20C AND SRM 51-1-21 PG 1. FABRICATED CHANNEL IAW SRM 51-1-4 PG 1-5, SRM 53-3-3 FIG 2. PERFORMED HEAT TREATMENT TO CHANNEL IAW SRM 51-1-1 PG 17. CLEANED, TREATED AND PRIMED CHANNEL IAW SRM 51-1-8B. INSTALLED NEW CHANNEL ON NOSE SECTION INTERIOR LEFT TUNNEL STA 17.000, L32L - L35L IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031124001252003112400125NE 2003 11 24 2003F00610 220030902A7230 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ENGINE DAMAGED A FDKAC ABORTED TAKEOFF EMRVIBRATION/BUFFET OVER TEMP PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW07507MJ 10077 GEE965376 FLT 6758 - LGB-PHX - ABORTED TAKEOFF, RIGHT ENGINE HAD A COMPRESSOR STALL ON TAKEOFF ROLL. MAINTENANCE PERFORMED BORESCOPE REVEALING COMPRESSOR BLADE DAMAGE AND REPLACED ENGINE. (M) 2L72 4F4 FRTA21EA EOOO63EN 20031124001432003112400143EU 2003 11 24 03289324 120031016A2611 PIN JETAIRJETSTMJETSTM4101 1500501EU CONNECTOR LOOSE A VTZAK NONE N FALSE WARNING ININSP/MAINT 1 EA27324UE 41017 DURING INSPECTION THE CARGO SMOKE DETECTION SYSTEM WAS GIVING A CONSTANT LOOP A FIRE ALARM. MAINTENANCE PERSONNEL RESECURED A PIN IN THE CONNECTOR. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031124001452003112400145NM 2003 11 24 CALA0300598 120031010A5311 BELTFRAME BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 FBB BELTFRAME AT STATION 500D HAS CORROSION OUTBOARD OF STRINGER S27L. INSTALLED REPAIR FBB BELTFRAME AT STATION 500D. 2L72 4F4 FRTA16WE E2GL 20031124001502003112400150NM 2003 11 24 CALA0300604 120031019A5320BAC1496377 PANEL BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 CORROSION ON LEFT TRANSITION PANEL FROM STA 727E TO 767. FABRICATED AND INSTALLED NEW PANEL IAW SRM 53-60-53. 2L72 4F4 FRTA16WE E2GL 20031124001512003112400151NM 2003 11 24 CALA0300605 120031019A5320654795711 STRAP BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 AFT CARGO DOOR STRAP ON TO OF WEB AT STA 773 - 859 CORRODED. REMOVED OLD STRAP. INSTALLED NEW STRAP IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031124001532003112400153NM 2003 11 24 QXEA200301283 120031008A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-LEFT INBOARD TRACK NR 5 SEAT ATTACH AREA CORROSION UNDER OUTBOARD LUG. REPAIRED IAW RD8-53-1339. 2H72 4T4 TRTA13NM E20NE 20031125000042003112500004WP 2003 11 25 DHL2003802501 120031107A5712 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING L/E FORMER CRACKED 0.500 AT STA XFS 735.000. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031125000062003112500006WP 2003 11 25 DHL2003805586 120030823A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD EXTENDED L/E SHOWS CORROSION AND ELONGATED HOLES AROUND STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. CUT OUT CORRODED AREA. PERFORMED NDT INSPECTION. FABRICATED FILLER AND REPAIR DOUBLER IAW DHL-EDT66-1, DWGT66-R01. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 9. INSTALLED FILLER AND REPAIR DOUBLER WITH NEW FASTENERS IAW DHL-EDT66-1, DWGT66-R01, SRM 51-1-21 PG 1 SRM 51-1-20D PG 9 SRM 51-1-15 PG 1. REFER TO NR 0119 FOR RIGHT OUTER WING INBD LE REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031121000672003112100067NM 2003 11 21 VNAA0310020 120031028A3350 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT MALFUNCTIONED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07459PS 3070 THE CREW REPORTED THAT ON ENGINE START THE EMERGENCY LIGHTS ROW 7, 8, & 9 GO OUT. MAINTENANCE SWAPPED POWER SUPPLIES 6LK & 7LK. OPERATION OF THE SYSTEM WAS CHECKED IN ACCORDANCE WITH DORNIER MANUAL 33-00-00 AND NO FAULTS FOUND. THE AIRCRAFT WAS RELEASED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031121000812003112100081WP 2003 11 21 ABXA030440 120031030A52303914025502N FITTING DOUG DC9 DC914 3022034WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 AFT LOWER CARGO DOOR, TRAILING EDGE NR 5 BEAM END FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20031121000832003112100083WP 2003 11 21 ABXA030442 120031031A53209911520385 FLOOR SUPPORT DOUG DC9 DC914 3022034WP FWD CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 STA 218 FLOOR SUPPORT WAS CORRODED ABOVE LONGERON 30. REPAIRED FRAME AT FS 218, LONGERON 30 IAW DC-9 SRM 53-03. 2L72 4F A6WE 20031125000132003112500013WP 2003 11 25 DHL2003805519 120030804A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING INBD L/E FORMER CRACKED 0.500 AT XFS 641.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LT OUTER WING INBD L/E FORMER AT STA XFS 641.250 IAW SRM 57-2-0 PG 9, 10 SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000142003112500014WP 2003 11 25 DHL2003805528 120030818A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING OTBD STUB WING L/E FORMER WORN AT XW 454.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 17. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON RIGHT WING OTBD STUB WING 57-2-0 PG 9-10 SRM 51-1-21 PG 1. FOR REMOVAL AND INSTALLATION OF RIGHT OTBD STUB WING SEE N/R 2030. 2L74 4F RT4A25 20031125000172003112500017WP 2003 11 25 DHL2003807520 120031010A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLOT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING L/E SLOT UPPER SKIN CORRODED BETWEEN STA XFS 220.000 - XFS 232.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 TR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17, 18. FOUND OUT OF LIMITS IAW SRM 57-2-0 FIG 2G. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38 TR 57-85. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38 TR 57-85, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031110002052003111000205GL 2003 11 10 SWAA032231 220031005A75327064004 MOTOR BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563B1US GL NR 2 ENGINE FAULTY A SWAAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW29630WN 27705 AIR TURN BACK, NR 2 ENGINE EGT WENT TO 946 FOR 3 SECONDS. REMOVED AND REPLACED VBV MOTOR, MECHANICS AND SHAFT PER MM. 2L72 4F4 FRTA16WE E2GL 20031110002172003111000217NM 2003 11 10 AALA20031035 120030909A25308609020000 OVEN BOEING767 767223 1385123NM GALLEY MALFUNCTIONED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21339AA 22336 LAX - FLT 33 - HEAVY SMOKE EMERGING FROM THE FIRST CLASS GALLEY. MAINTENANCE FOUND RESIDUE IN CONTACT WITH THE OVEN HEATING ELEMENT. REMOVED AND REPLACED OVEN. GROUND OPS CHECK NORMAL. (M) 2L72 4F RTA1NM 20031112000092003111200009NM 2003 11 12 2003UALA00818 120031029A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT PIT, STA 1520 & STR 29R AND 29L, SHEAR TIE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20031112000122003111200012NM 2003 11 12 03FDEA01767 120031020A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 FLOOR TRACK AT STA 635 LT X = 8.5 CRACKED. FLOOR TRACK AT STA 635 LT X = 8.5 CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-70-00, VOL. I, FIGURE 1. 2L73 4F RTA22WE 20031112000162003111200016EU 2003 11 12 2003UALA00821 120031029A2611 SMOKE DETECTOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO BAY MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29409UA 462 RETURN TO FIELD DUE FWD CARGO SMOKE ECAM MESSAGE. REPLACED FORWARD CARGO DETECTOR AS FAULTED BY CENTRALIZED SMOKE DETECTOR CONTROL UNIT. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20031112000252003111200025SO 2003 11 12 C2XA03SH447 120031112A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV-DURING C-CHECK THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031112000312003111200031NM 2003 11 12 03FDEA01720 120031008A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LH WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR LUG AND HOLE CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, LEFT AND RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031112000382003111200038CE 2003 11 12 DXTA200300156 120031106A2810 FLOAT CESSNA750 750 2076810CE RT WING STUCK E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07947QS 7500047 AFTER TAKEOFF, AMBER CAS MESSAGE WING O FULL RT ILLUMINATED. FUEL CAN BE VISUALLY SEEN DUMPING OUT OF RIGHT WING FROM VICINITY OF SURGE TANK VENT. FUEL IMBALANCE BECAME EVIDENT AT A RATE OF APPROX 100 LBS PER MIN. PRESSURIZED RIGHT WING, FOUND NO LEAKS IN DRY BAYS BETWEEN FUEL & SURGE TANKS. REMOVED SURGE TANK VENT FLOAT PANEL, FOUND VENT FLOAT STUCK TO OUTBOARD FLAP JACKSCREW DRAIN LINE, FREED VENT FLOAT FOR UNOBSTRUCTED FLOAT MOVEMENT. RE-INSTALLED ALL PANELS, ALL WORK DONE IAW CESSNA 750 MM CHAPTER 28-10-04, OPS CHECK GOOD. 2L72 4J RTT00007WI 20031107001272003110700127SO 2003 11 7 SIMA200327906 120030927A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02, EMB STATEMENT IC2003-145/3098A AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031107001372003110700137NM 2003 11 7 ASAA0310438 120030512A5320BAC1509100146 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 859, LEFT BUTTOCK LINE 8 CORRODED. REPLACED FLOOR SUPPORTS PER SRM. (M) 2L72 4F A16WE 20031107001382003110700138EU 2003 11 7 SIMA200327203 120030926A33506013211 BATTERY SAAB SF340 340B 7860101EU CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21339SB 340B339 LAX - FLT 3062 - EMERGENCY LIGHT OVER 8A INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY AND REPAIRED A WIRE BEHIND FUSE ON NR 3 BATTERY IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20031112000422003111200042NM 2003 11 12 03FDEA01774 120031009A5753ARC0502505 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING O/B FLAP I/B HINGE (WING SIDE) O/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS LT OUTBOARD FLAP- INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031112000462003111200046CE 2003 11 12 ACE110503 120031105A2120 ODOR CESSNA207 207A 2073604CE COCKPIT DETECTED E YADAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL039957M 20700764 PILOT REPORTED THAT HE BEGAN SMELLING EXHAUST FUMES AND BEGAN FEELING SICK AFTER DEPARTURE. RETURNED TO THE ORIGINAL AIRPORT AND LANDED SAFELY. MAINTENANCE VERIFIED THE SMELL OF EXHAUST IN THE AIRCRAFT AFTER LANDING AND WAS INFORMED BY THE PILOT THAT HE THOUGHT THAT TURNING OFF CABIN HEAT HAD REDUCED THE FUMES IN THE CABIN. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AND REPLACED THE LEFT MUFFLER (CABIN HEAT) FOR CONVENIENCE. THE REMOVED MUFFLER HAS BEEN INSPECTED AND WAS NOT NOTED AS HAVING ANY DISCREPANCIES. 1H71 3O A16CE 20031112000822003111200082NM 2003 11 12 C1HA200394031 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK AT BS 344 - 480 RBL 45 HAS BARE METAL AND CORROSION. 2L73 4F A3WE 20031112000862003111200086NM 2003 11 12 C1HA200394035 120031108A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 480 - 689.45 LBL 24.75 HAS CORROSION AND WORN AREAS. 2L73 4F A3WE 20031112000952003111200095WP 2003 11 12 ABXA030426 120031027A53205912494501 PAN DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 LEVEL 2 CORROSION ALONG BOTTOM OF FORWARD LOWER CARGO DOOR CUTOUT. REMOVED CORRODED AND CRACKED PAN SECTION. INSTALLED NEW PAN SECTION IAW DC-9 SRM 53-05. 2L72 4F A6WE 20031112001012003111200101 2003 11 12 BAQA090606 420031028A3423KCA0105W COMPASS BOLKMS117 BK117B1 5626012EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME6467 7235 COMPASS LIGHT WILL NOT WORK. REPLACED WITH SERVICEABLE ASSET. 1G72 3U H13EU 20031112001212003111200121WP 2003 11 12 ABXA030433 120031027A5553591214160 ATTACH ANGLE DOUG DC9 DC941 302207NWP VERT STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 VERTICAL STABILIZER RIGHT ATTACH ANGLE WAS CRACKED AT 99. REPAIRED CRACK ON VERTICAL STABILIZER RIGHT ATTACH ANGLE AND SEAM SEALED IAW DC-9 SRM. 2L72 4F A6WE 20031112001252003111200125EU 2003 11 12 BAQA089932 120030920A2140JBS8802 VALVE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE HEATER MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911BG 0015 MIXING VALVE MALFUNCTIONED, HEATER WILL NOT GIVE HEAT. REPLACED WITH SERVICEABLE UNIT. 10/17/03 1G72 3U3 UO H88EU E42NE 20031112001312003111200131 2003 11 12 MALA030486 420031101A34256227713004 COMPUTER SAAB SF340 SF340A 7850100EU NR 1 MALFUNCTIONED A MALAO OTHER O OTHER CRCRUISE 1 GL15106XJ 340A106 DURING FLIGHT 3141, WHILE IN CRUISE, CAPT EADI & EHSI BOTH WENT DARK. RECEIVED A DCP FLAG. RAN QRH WENT TO DRIVE XFER. SCREENS CAME BACK ON. MAINTENANCE REMOVED AND REPLACED NR 1 DPU ALL CHECKS GOOD IAW SAAB MM CH 34. P/N 622-7713-004, S/N OFF 5248, S/N ON 7054. 2L72 4T RTA52EU 20031113000072003111300007NE 2003 11 13 BAQA090337 220031023A73140319928670 PUMP AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE FUEL SYSTEM MALFUNCTIONED B BAQAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 EA037YL 444 11502 ENGINE WOULD NOT START. REPLACED FUEL PUMP. 1G72 3U3 URTH7EU E42NE 20031113000092003111300009CE 2003 11 13 BAQA090299 120031023A6121213618 SYNCHROPHASER BEECH 100 100BEECH 1152916CE HARTZLHCB4T HCB4TN5 GL PROPELLER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 10019 B144 PROPELLER SYCHROPHASER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 6 CP40EA 20031113000152003111300015EU 2003 11 13 BAQA090123 120031022A71700174078030 DRAIN VALVE AEROSPAS365 AS365N2 8680815EU ENGINE LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03915ME568 6417 FAILED ENGINE CHECK. LEAKS . PART ONLY LASTED 9 MONTHS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20031107001612003110700161NM 2003 11 7 ASAA0310450 120030515A78301731021 SKIN BOEING737 737290C 138448VNM THRUST REVERSER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER LOWER BUCKET SKIN AT THRUST REVERSER STATION 200.70 CRACKED. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031110000572003111000057SO 2003 11 10 C2XA03SH441 120031110A521014524131009 BRACKET EMB 145 EMB145LR 3260212SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031110000632003111000063EU 2003 11 10 RAIA00310276 120031029A3320 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN MALFUNCTIONED A RAIAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE03562HK 41078 MX-CHO- SMOKE IN CABIN. MAINTENANCE DEFERRED SIDEWALL WASH LIGHT PER MEL 33-7. 2L72 4T RTA41NM 20031110001952003111000195NM 2003 11 10 SWAA032240 120031010A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED, WL 199, RBL 6.5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031110002182003111000218NM 2003 11 10 AALA20031008 120030915A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21672AA 25337 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROWS 24 THROUGH 34. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031112000982003111200098EU 2003 11 12 AWXA200301379 120031108A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW4427454 091 LAX - MAJOR REPAIR - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2 AND 5 LT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LT EMERGENCY LIGHT BATTERY PACK AND EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031112001102003111200110NM 2003 11 12 AWXA200301385 120031106A5320652981818 BRACKET BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN A BRACKET AT BS 334, LBL 56, WL 206. MAINTENANCE REMOVED THE CRACKED BRACKET AT BS 334, LBL 56, WL 206; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, AND SRM 51-30-05, FIG 4. 2L72 4F RTA16WE 20031112001182003111200118NE 2003 11 12 HEEA090305 220030525A72000292005250 ENGINE SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE MALFUNCTIONED W HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 ENGINE LIGHTS OFF INTERMITTENTLY. AFTER IT DOES LIGHT OFF IT WILL NOT ACCELERATE PAST 29 PERCENT, N1. THIS HAS BEEN A ON GOING PROBLEM WITH THIS ENGINE. ALL TROUBLESHOOTING EFFORTS HAVE BEEN EXHAUSTED. FROM CHANGING START VALVE, PRESSURIZING VALVE, FUEL CONTROL, IGNITERS, BLEED VALVE BORE SCOPING ENGINE. INSPECTED AIRFRAME COMPONENTS ASSOCIATED WITH START. ALL TO NO AVAIL. REMOVED ENGINE ASSEMBLY. SENT TO MFG FOR WARRANTY REPAIR. 1G72 3U3 U H1NE E19EU 20031113000172003111300017NE 2003 11 13 BAQA090551 220031027A72000319958180 VALVE AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037YL 880 11502 ENGINE SLOW TO START. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 URTH7EU E42NE 20031117000322003111700032EA 2003 11 17 QXEA200301214 120031005A5210 MECHANISM CNDAIRCL600 CL6002C10 1390015EA PAX DOOR DIRTY A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09615QX 10065 CREW REPORTS MAIN CABIN DOOR HARD TO OPEN. CLEANED AND LUBED MATELING SURFACES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031117000392003111700039NM 2003 11 17 PCAA0310120 120031006A7810 PIPE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE OUT OF POSITION A PCAAF ACTIVATE FIRE EXT. AJ FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 EA13844EX327267 339 120042 CREW REPORTED A FIRE INDICATION ON THE NR 1 ENGINE DURING TAXI IN. FIRE BOTTLE WAS DISCHARGED. MAINTENANCE INSPECTED THE ENGINE AREA AND FOUND DRAIN LINES BURNED AND JET PIPE SLID BACK. DRAIN LINE WAS REPLACED AND JET PIPE WAS REINSTALLED IAW 008-7810-312. FORWARD FIRE BOTTLE WAS REPLACED IAW DASH 8 MM. FIRE DETECTION SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT GROUND RUN OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031117000412003111700041NM 2003 11 17 2003UALA00733 120031001A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29559UA 26657 RT AFT DOOR EXTERIOR EMERGENCY-SLIDE RAFT LIGHT IS INOPERATIVE. RELAMPED. CHECKS OK. 2L72 4F4 FRTA2NM E17NE 20031117000492003111700049NM 2003 11 17 CALA0300574 120031006A5311 FRAME BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A .5 INCH CRACK AT FASTENER IN RT FRAME AT STA 616. REPAIRED IAW ECRA 5311-01158. 2L72 4F4 FRTA16WE E2GL 20030912001052003091200105NM 2003 9 12 AWXA200300863 120030713A532065C3267714 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT LAVATORY FLOOR WEB DOUBLER (STRAP) BS 1016-1029, LBL 3, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED STRAP BS 1016-1029, LBL 3; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3-5, AND 10-11. 2L72 4F RTA16WE 20030912001702003091200170WP 2003 9 12 AALA20030880 120030820A33505874278 SWITCH DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21276AA 49273 ORD - EMERGENCY LIGHT ARMING SWITCH AT FORWARD FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030912001782003091200178WP 2003 9 12 AALA20030887 120030822A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217546A 53028 FORWARD ENTRY EMERGENCY LIGHT INOPERATIVE AT LOCATIONS B5-23. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030917000512003091700051NE 2003 9 17 SIMA200311316 220030422A73206071T0P12 CONTROL UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE INOPERATIVE A SIMAC ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 SW21393AE 340B393 TAKEOFF WAS ABORTED DUE TO THE RIGHT ENGINE TORQUE WENT TO ZERO. THE ENGINE FEATHERED AND SHUT DOWN BY ITSELF. ALL PARAMETERS WERE NORMAL PRIOR TO ENGINE SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE DIGITAL ELECTRONIC CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200305090) 2L72 4T4 TRTA52EU E8NE 20030917000742003091700074EU 2003 9 17 BAQA089008 120030905A7430L311M1009103 SWITCH UROCOPEC135 EC135T1 5620026EU ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME432 0157 NR 1 ENGINE WILL NOT SHUT OFF ALL THE TIME. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030917000812003091700081EA 2003 9 17 ASOA03381 120030817A5320601R352051 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE CARGO DOOR ENTRANCE SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR ENTRANCE SEAL PLATE IAW SRM 51-00. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030917000822003091700082EA 2003 9 17 ASOA03390 120030821A2612GG670801031 FIRE LOOP CNDAIRCL600 CL6002C10 1390015EA RT ENGINE MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11707EV 10057 DURING CLIMB-OUT FROM ATL-AGS, THE CREW RECEIVED A RIGHT BLEED DUCT WARNING MESSAGE. QRH WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE READJUSTED THE LOOP ELEMENTS AT MT143 AND 144 AND MT204 AND 205 WHICH WERE FOUND TO BE TOUCHING THE DUCTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030917000932003091700093EU 2003 9 17 ASOA03391 120030821A5313 STRINGER AEROSPATR72 ATR72 EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING A GROUND INSPECTION IN AVL, THE FORWARD CARGO DOOR HINGE POINT STRINGER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD CARGO DOOR HINGE POINT STRINGER IAW SRM 52-31-00 AND 51-25-02. (M) 2H72 4T RT 20030917000952003091700095NM 2003 9 17 GAIA03022SP 120030719A53302024T3 SKIN BOEING727 7272J0 138407ENM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND FUSELAGE RIGHT SIDE STATION 675 STRINGER R19 HAS PILLOWING AT FASTENERS. CUT OUT DAMAGED SKIN 3 INCHES BY 2.75 INCHES, ACCOMPLISHED DOUBLER REPAIR IAW B727 SRM 53-30-3 FIG 14. DOUBLER 2024 T-3, .071, FILLER 2024 T-3 .063. (M) 2L73 4F RTA3WE 20040114001162004011400116NE 2004 1 14 SW07200300001 220030416A72504120T01P02 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE DAMAGED G MASAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW07506MJ962 10073 E965370 THE CREW REPORTED N2 VIBRATION AFTER WHICH THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPE INSPECTION WHERE THEY DISCOVERED THE HIGH PRESSURE TURBINE BLADE DAMAGE. 2L72 4F4 FRTA21EA EOOO63EN 20040114001392004011400139WP 2004 1 14 AALA2003104A 120030920A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21405A 49316 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE IN THE TAIL COMPARTMENT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040114001482004011400148CE 2004 1 14 DXTA200300174 120031128A3230991446110 CONTROL MODULE CESSNA750 750 2076810CE NLG FAILED E DXTAO OTHER O OTHER DEDESCENT 1 GL07989QS 7500089 UPON DESCENT INTO SMO CREW OBSERVED THE GEAR UNLOCK LIGHT ILLUMINATED AND A DISTINCTIVE SOUND FROM NOSE GEAR AREA. THIS OCCURRED AT FL 26, FL 20 AND FL 11.5. REMOVED AND REPLACED INOP LANDING GEAR CONTROL MANIFOLD. PERFORMED OPERATIONAL AND LEAK CHECK IAW CESSNA 750 MM CHAPTER 32-30-02. 2L72 4J RTT00007WI 20040114001702004011400170 2004 1 14 MALA030557 420031213A3416 SWITCH BAC 146 AVRO146RJ85A1500097EU COCKPIT FAILED A MALAG O2 MASK DEPLOYED O OTHER TXTAXI/GRND HDL 1 GL15525XJ E2350 UPON PUSHBACK ALL THE PASSENGERS OXYGEN MASKS DROPPED DOWN. MAINTENANCE REPLACED ALTITUDE SWITCH. 2H74 4F RTA49EU 20040114001902004011400190SO 2004 1 14 MASA200300429 120031027A2560P207003001 FLASHLIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ 145218 ASH 2947 DCA. CREW REPORTED F/A EMERGENCY LIGHT INOPERATIVE. MECHANIC REPLACED FLASHLIGHT. 2L72 4T RTT00011AT 20040114002002004011400200NM 2004 1 14 MWEA030456 120031125A5347593054770 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 SEAT TRACK NR 6 AT STATION 507 HAS CORROSION. CUT OUT DAMAGE AND REPAIRED SEAT TRACK. 2L72 4F RTA6WE 20040114002022004011400202NM 2004 1 14 MWEA030458 120031125A5347593056675 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 THE NR 3 SEAT TRACK HAS AN AREA OF CORROSION AT STATION 1195. FABRICATED AND INSTALLED REPAIR PARTS. 2L72 4F RTA6WE 20040115000142004011500014NM 2004 1 15 03FDEA02029 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 3 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000152004011500015NM 2004 1 15 03FDEA02030 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 3 I/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000162004011500016NM 2004 1 15 03FDEA02031 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 2 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000172004011500017NM 2004 1 15 03FDEA02032 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 2 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000332004011500033NM 2004 1 15 PCAA0312146 120031201A3231 RELAY DHAV DHC8 DHC8102 2809003NM NLG FAILED A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13845EX 344 ON APPROACH, NLG WOULD NOT EXTEND NORMALLY. AFTER ATTEMPTING FLT MANEUVERS TO EXTEND GEAR, ALTERNATE EXTENSION SYSTEM WAS USED & A/C LANDED SAFELY. MAINT DISCOVERED AN INOPERATIVE NOSE DOOR SEQUENCING VALVE & REPLACED IT. A/C TEST FLOWN & RETURNED TO SERVICE. ON APPROACH, SAME CONDITION EXISTED. ONCE A/C ARRIVED, MAINT R&R NOSE GEAR DOOR ACT, DUE TO ACT BYPASSING ON DOWN SIDE. A/C OPS CHECKED & RETURNED TO SERVICE. LATER THAT DAY, HAD SAME DISCREPENCY. MAINT R&R 3261-K7 RELAY & RETURNED A/C TO SERVICE. NO DISCREPENCIES TO DATE. 2H72 4T RTA13NM 20040115000362004011500036NM 2004 1 15 03FDEA02046 120031204A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION ON FRAME STA 540 RBL 5 WL 147. FRAME AT BS 540, RBL 5, WL 147 FOUND TO BE OUT OF LIMITS DUE TO CORROSION REMOVAL. REPAIRED FRAME SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 12. 2L73 4F RTA3WE 20040115000372004011500037NM 2004 1 15 03FDEA02047 120031204A5310 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION ON FRAME BS 1148 BETWEEN STR 25-26 LT. BLENDED CORROSION FROM FRMAE BS 1148 BETWEEN STR 25-26 LT. REMOVED .040 FROM ORIGINAL THICKNESS OF .065. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE MATERIAL 1 X 2.5 INCH. FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 USING LOT 518135 AND ER NO. 03-4723 AND FED EX EA 7-5310-55168. 2L73 4F RTA3WE 20040115000412004011500041EU 2004 1 15 03FDEA02053 120031204A2420 GENERATOR AIRBUS310 A310 EU NR 1 INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25801FD 539 REJECTED T/O IN CDG DUE TO NR 1 IDG HIGH OIL TEMP ALERT. DISCONNECTED PER MAINT & DEFERRED PER MEL. GEN NR 1 INOP. APU GEN MUST BE USED TO POWER AFFECTED BUSS THROUGHOUT FLT. VERIFY & RECORD IN AML/EAML THAT OIL QTY OF IDG IN DISCONNECT MODE, REMAINING OPERATIVE IDG, & APU GEN ARE CHECKED ONCE EACH FLT DAY. DUE TO IDG 2L72 4F RTA35EU 20040115000602004011500060NM 2004 1 15 DL73S031089 120031215A53126546568524 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD AT BS 1016 AND BL 0, BETWEEN S26L AND 26R. CORROSION WAS REMOVED THEN REPAIRED PER ERA 385921-14AD. 2L72 4F RTA16WE 20040115001172004011500117NM 2004 1 15 03FDEA02094 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 3363RL. LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20040115001222004011500122NM 2004 1 15 03FDEA02099 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 361CL. LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACK LOCK BOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040115001242004011500124NM 2004 1 15 03FDEA02101 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION BETWEEN NR 1 & 2 BANJO FITTINGS SUPPORT CLIP FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION BETWEEN NR 1 & 2 BANJO FITTING SUPPORT CLIP 2 CRACKED LOCKBOLT COLLARS REMOVED & REPLACED AS PER SRM 51-32-01 VOL2 & SRM 51-33-01 VOL2 RESPECTIVELY. 2L73 4F RTA22WE 20031212000102003121200010NM 2003 12 12 SWAA032479 120031107A5320BAC1506 STRUCTURE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND FUSELAGE Z CHORD CORRODED AT BS 270, RBL 11, WL 208. REMOVED AND REPLACED CHORD PER SRM. 2L72 4F RTA16WE 20031212000572003121200057NM 2003 12 12 AWXA200301417 120031112A21216067726 FAN BOEING757 757225 1384959NM CABIN FAILED A AWXAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 WP28913AW240 240 22207 EN ROUTE FROM DFW TO PHX THE FLIGHT ATTENDANTS REPORTED AN ELECTRICAL BURNING ODOR IN CABIN, 5 MINUTES LATER RECEIVED R RECIRC FAN EICAS MESSAGE. MAINTENANCE ISSUED DPI MEL 21-25-1, COND. 1, RT RECIRC FAN INOP. ON 11/12/2003 MAINTENANCE REMOVED AND REPLACED RT RECIRCULATION FAN IAW T/C R2B21601, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL CHECK OF RECIRCULATION FAN S/N 72-810 CONFIRMED FAILURE OF UNIT. TEARDOWN OF UNIT REVEALED THE BEARINGS WERE SEIZED. REMOVED AND REPLACED BOTH BEARINGS IAW CMM 2-25-04, REV. 5. 2L72 4F RTA2NM 20031212000622003121200062NM 2003 12 12 QXEA200301420 120031113A5260 CAM BOMBDRDHC8 DHC8401 1390041NM AFT AIRSTAIRS OUT OF POSITION A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09401QX 4031 SEA- AFT AIRSTAIR INOPERATIVE. REALIGNED FOLLOWING CAM TO TRACK. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031212000652003121200065SO 2003 12 12 C2XA03SH457 120031116A532014525422001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 61 AND 64 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031212000662003121200066NM 2003 12 12 03040 120031114A2824 VALVE BOEING747 7472B4B 138481BNM FUEL SYSTEM MALFUNCTIONED A KCSAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 GL23710CK 21097 NR 4 ENGINE SHUT-DOWN DUE TO CROSSFEED VALVE MALFUNCTION. ALL OTHER INDICATIONS NORMAL, AND ACCOMPLISHED NORMAL APPROACH AND LANDING. 2L74 4F RTA20WE 20031212001022003121200102NM 2003 12 12 SWAA032397 120031030A53106546557 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 887, STRINGER 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031212001092003121200109NM 2003 12 12 SWAA032443 120031105A53116546554 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21 IN AFT CARGO COMPT. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031212001462003121200146WP 2003 12 12 AALA20030937 120030902A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21492AA 49730 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WERE INOPERATIVE AT ROW 28. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001482003121200148WP 2003 12 12 AALA20030924 120030829A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21276AA 49273 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT SEAT 17D. REPLACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001692003121200169WP 2003 12 12 AALA20030914 120030831A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21475AA 49650 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY LIGHTS WERE INOPERATIVE IN AFT FLIGHT ATTENDANT AREA. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001792003121200179EA 2003 12 12 COMA0370054 120031124A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA E/E BAY FAULTY A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01379CA1561 10102 FLIGHT 5903) DURING CLIMB OUT OF STL RECEIVED AN IB FLIGHT SPOILER AND IB SPOILER CAUTION MESSAGE, AIRCRAFT RETURNED TO STL. REPLACED THE SPOILER/STABILIZER CONTROL UNIT. 2L72 4F RTA21EA 20030917000972003091700097EU 2003 9 17 ASOA03389 120030820A5330 DOUBLER AEROSPATR72 ATR72 EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR DOUBLER ON THE FORWARD LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAITNENANCE REPAIRED THE PASSENGER DOOR DOUBLER ON THE FORWARD LOWER STEP IAW SRM 52-11-00. (M) 2H72 4T RT 20030917001012003091700101NM 2003 9 17 GAIA03044SP 120030719A5542 SKIN BOEING727 727 UTILSYSNM RUDDER CHAFED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND LOWER RUDDER LOWER L/E CLOSE OUT WEB CHAFED THROUGH FASI N/R 36010. REPLACED WEB P/N 65-16830-4 IAW B-727 SRM 51-30-2. (M) 2L73 4J RTA3WE 20030917001102003091700110NM 2003 9 17 GAIA03047SP 120030719A5542 SKIN BOEING727 7272J0 138407ENM RUDDER CHAFED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND UPPER AND LOWER RUDDERS LEADING EDGES TEFLON ANTI-CHAFE PAINT WORN OUT, BOTH RUDDERS HAVE AREAS OF CHAFING. FOUND 6 AREAS ON LOWER RUDDER OUT OF LIMITS, FABRICATED 6 DOUBELRS, TWO 21.5 AND 14.25, TWO 15.25 BY 23.5, TWO 13.5 BY 15.5 ALL FROM 301 ONE QUARTER HARD AND INSTALLED IAW B727 SRM 55-40-3 FIG 1. UPPER RUDDER NO DAMAGE NOTED, REPAINTED IAW B727 MM 51-20-71. (M) 2L73 4F RTA3WE 20030917001202003091700120NM 2003 9 17 PCAA0307088 120030730A3350 SOCKET DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DAMAGED A PCAAK NONE L NO TEST NRNOT REPORTED 1 EA13812EX 312 LGA-FLIGHT 3800. CREW REPORTED THAT THE REAR SECTION OF EMERGENCY FLOOR LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED WIRING ON FLOOR AND RECONNECTED ONE CANNON PLUG, AFTER WHICH THE LAST RED FLOOR LIGHT WAS FOUND TO BE STILL INOPERATIVE. MEL 33-13 WAS ISSUED AND AIRCRAFT RETURNED TO SERVICE. AIRCRAFT WAS IN MAINTENANCE THAT EVENING AND A NEW BULB SOCKET FOR LAST FLOOR EMERGENCY LIGHT WAS INSTALLED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030917001252003091700125NM 2003 9 17 DLM88030677 120030720A3260 WARNING LIGHT DOUG MD88 MD88 3023688NM MLG ILLUMINATED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27948DL 49879 AFTER T/O GEAR WOULD NOT RAISE, HANDLE NML 3 RED, AURAL INDICATIONS GEAR DOWN. TOWER CONFIRMED ALL GEAR DOWN. DROP GEAR 3 GREEN, ALL HYD INDICATIONS NML. GROUND SENSE DID NOT SENSE WEIGHT ON WHEELS, SPOILER DEPLOYED MANUALLY. DEPRESSURIZED MANUALLY. ON W/A FOUND DOOR BYPASS HANDLE OPEN SECURED SAME. JACKED A/C OPENED BYPASS HANDLE AND VERIFIED PROBLEM. CLOSED BY PASS HANDLE AND CYCLED GEAR SEVERAL TIMES ALL INDICATIONS NORMAL, OK FOR SERVICE. 2L72 4F RTA6WE 20030917001272003091700127NM 2003 9 17 DL73S030680 120030718A5711654948818 SPAR BOEING737 737232 1384475NM RT WING GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 RT WING / MLG AFT SUPPORT FITTING / WBL 157, TOOLING DAMAGE. THE MLG AFT SUPPORT FITTING ON THE RT WING SUFFERED TOOLING DAMAGE DURING REMOVAL OF FASTENERS FOR INSPECTION. THE BORE OF ONE OF THE FASTENERS WAS DAMAGED IN THE AFT FITTING, REAR SPAR UPPER CHORD, REAR SPAR WEB AND THE FWD MLG FITTING. IAW ER/A 385269-14, THE AFT FITTING WAS REPLACED, THE REMAINING LAYERS WERE BUSHED AND AN EXTERNAL STRAP WAS INSTALLED OVER THE REAR SPAR UPPER CAP. 2L72 4F RTA16WE 20030917001282003091700128NM 2003 9 17 DL73S030681 120030718A53306545769158 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 A SCRATCH AND DENT WAS FOUND IN THE FUSELAGE SKIN JUST BELOW THE C1 CARGO DOORWAY EXTENDING FROM FS 460 TO FS 500. AN EXISTING REPAIR WAS FOUND AT THE FORWARD LOWER CORNER OF THE DOORWAY. THIS REPAIR WAS REMOVED AND AN EXTERNAL ALUMINUM DOUBLER TRIPLER AND FILLER WERE INSTALLED OVER THE PREVIOUS REPAIR AREA AND INCORPORATING THE CUT OUT DENT/SCRATCH AREA. WORK WAS DONE IN ACCORDANCE WITH ER/A 385217-14. 2L72 4F RTA16WE 20030917001322003091700132NM 2003 9 17 DL757030692 120030723A3240326001194 TIRE BOEING757 757232 1384965NM NLG CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO27648DL 24372 LT. NOSE TIRE HAS FOD DAMAGE - REPLACED SAME 2L72 4F RTA2NM 20030917001332003091700133NM 2003 9 17 DLM88030693 120030723A3320 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27906DL 49537 EMERGENCY PATH POWER SUPPLY INOP ROWS 31-38. REPLACED POWER SUPPLY 2L72 4F RTA6WE 20030918000012003091800001NM 2003 9 18 03FDEA01429 120030901A5510ALC81072 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 HOR STAB RT UPPER CENTER PLANK NR 26 RT BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. HORIZONTAL STAB RT UPPER CENTRE PLANK NR 26 RT FITTING REMOVED AND REPLACED AS PER EA 1-5510-72642 STABILIZERS - HORIZONTAL STABILIZER - FITTING ALC 8107-2 FABRICATION. 2L73 4F RTA22WE 20030918000192003091800019NM 2003 9 18 2003F00562 120030427A5320 STIFFENER BOEING737 7372L9 1384497NM AFT CARGO BAY CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO27464AT 21278 DURING C-CHECK INSPECTION, FOUND A .625 INCH CRACK IN AFT CARGO FLOOR OUTER EDGE STIFFENER AT LEFT SIDE BS 727B. THE DAMAGED WAS CORRECTED ON NON ROUTINE 031140. A NEW PART WAS FABRICATED AND INSTALLED. TOTAL AIRCRAFT TIME 46985.2. TOTAL CYCLES 41351. (M) 2L72 4F RTA16WE 20030918000342003091800034NM 2003 9 18 GAIA03028SP 120030719A5311 FRAME BOEING727 727* NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 540 HAS DENT INTO THE RADIUS AT STRINGER 16 RT, FASI N/N 35744. CUT OUT DAMAGED AREA, FABRICATED SECTION OF FRAME MATERIAL USED 7075-T6 .063 P/O NR 991245 DIM 12 INCHES BY 3.5 INCHES, DOUBLER 7075-T6 .071 P/O NR 991208 DIM 12 INCH BY 5.5 INCH AND FILLER 2024-T3 .032 P/O NR 991813 DIM 2.5 INCH, INSTALLED IAW SRM 51-40-3. (M) 2L73 4F RTA3WE 20030918000622003091800062NM 2003 9 18 DLM88030718 120030801A27404034237916 SERVO DOUG MD88 MD88 3023688NM E/E UNSERVICEABLE A DALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO27983DL 53247 DURING CRUISE FL350 A/P TRIM LT ILLUM. WHILE IN HOLDING TURN. A/P DISENGAGED. A/P TRIM LT. ON THROUGHOUT DESENT. REQUIRED DISENGAGEMENT A/P AND RETRIMMED AGAIN DURING FINAL APPROACH. DURING INITIAL PROBLEM, EGT ON BOTH ENGINES IN REDBAND FOR APPROX. 15 SEC. WHILE AT FL350. DUE TO LOST IN ALT. AND AIRSPEED. WHEN A/P KICKED OFF WHILE HOLDING IN TURN. FOUND ALT TRIM B PHASE C/B POPPED. REPLD R20-12,R20-13NO.2 DFGC AND RUDDER SERVO. BOROSCOPE NR 1 ENG. OK. REPLACED NR 2 ENG DUE TO EGT EXCEDANCE. 2L72 4F RTA6WE 20030918000642003091800064CE 2003 9 18 DXTA20030076 120030801A2120 ODOR CESSNA560 560XL 2076702CE COCKPIT DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07639QS 5605139 UPON DESCENT STRONG EXHAUST ODOR OF JET FUMES, APU WAS NOT RUNNING AT THE TIME, AND ENVIRONMENTAL SOURCES SHOWED 50 DEGREES. - ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20030919000032003091900003GL 2003 9 19 0075982 320030724A6110A1877 BEARING RACE BEECH 300 300BEECH 1152930CE PWA PT6 PT6* 52043EA HARTZLHCB4M HCB4MP3 GL PROPELLER CORRODED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 FWA3141 PROPELLER HAS CORROSION ON BEARING RACE. 2L72 4T3 T A24CE E2NE 6 CP56GL 20031215000112003121500011NM 2003 12 15 QXEA200301424 120031113A21218209361 FAN BOMBDRDHC8 DHC8401 1390041NM CABIN FAULTY A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09414QX4599 1956 4061 SEA- ON FLIGHT 2307 ELECTRICAL SMELL AROUND MAIN CABIN DOOR. DETERMINED SMELL TO BE COMING FROM GASPERS. SELECTED RECIRCULATION FAN OFF. RAN APU WITH ENGINE BLEEDS WITH NO ODOR. RESELECTED RECIRCULATION FAN ON, ODOR RETURNED. REMOVED AND REPLACED RECIRCULATION FAN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000482003121500048NM 2003 12 15 2003UALA00829 120031103A5534 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE VERTICAL STAB CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29373UA 24638 VERT STAB LT FWD AND AFT DRAG FITTINGS HAVE CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED BOTH FITTINGS. 2L72 4F4 FRTA16WE E2GL 20031215000642003121500064EA 2003 12 15 COMA0370051 120031114A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA 10062 PRESSURE BULKHEAD WEB AT FS 1098 STR 8L - 9L IS CRACKED AT NR 4 HYD LINE CONNECTION. PERFORMED MAJOR REPAIR IN ACCORDANCE WITH CANADAIR REO 670-53-61-034 REV B AND DEVIATION ENG ORDER (WVAC) 601R-53-4406. 2L72 4F RTA21EA 20031215000662003121500066NM 2003 12 15 AWXA200301446 120031117A3350BR8164005 LIGHT AIRBUSA319 A319132 3930340NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28822AW 1410 LAX - EEL - DURING 8-DAY CHECK AT LAX EMERGENCY LIGHT ON LT FORWARD PARTITION FLOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED & REPLACED EMERGENCY LIGHT AT LT FORWARD PARTITION FLOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031215000712003121500071 2003 12 15 03274402 420031001A31607014300902 DISPLAY DORNERDO32 DO328300 NM COCKPIT FAULTY A VTZAK NONE O OTHER NRNOT REPORTED 1 EA27402FJ 3147 THE NR 4 DISPLAY UNIT WAS IDENTIFIED AS FLASHING ON AND OFF. THE DISPLAY UNIT WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE FLIGHT DISPLAY SYSTEMS WAS ACCOMPLISHED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031215001002003121500100NM 2003 12 15 MWEA030449 120031120A2760 WARNING SYSTEM BOEING717 717200 1383700NM COCKPIT FALSE INDICATIONA MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31910ME 55174 GROUND SPOILER WOULD NOT ARM. PERFORMED RETURN TO SERVICE TEST. ALL TEST PASSED, OK FOR SERVICE. 2L72 4F TRA6WE 20031215001142003121500114WP 2003 12 15 AALA20030989 120030910A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21576AA 53153 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT OVERWING CABIN SECTION. RESEATED BATTERIES IN PACK B5-105. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001272003121500127WP 2003 12 15 AALA20031101 120031003A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21431AA 49343 RDU - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001452003121500145WP 2003 12 15 AALA20031069 120030925A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED PORTABLE EMERGENCY LIGHT AT FORWARD PASSENGER DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001462003121500146WP 2003 12 15 AALA20031070 120030925A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE AFT OVERHEAD LOCATION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001562003121500156WP 2003 12 15 AALA20031185 120031029A3350EMBS1392 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21455AA 49560 ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 18 TO 21. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001752003121500175EA 2003 12 15 ASOA03535 120031025A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11835AS 7258 FLT 4242 - DURING HANGAR INSPECTION IN BTR, THE RIGHT EXTERIOR EMERGENCY LIGHT FORWARD OF THE EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT LAMP FORWARD OF THE EMERGENCY EXIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031215001822003121500182EA 2003 12 15 ASOA03531 120031021A5210601R3807413 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11860AS 7433 DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR THE CRACK AND REPLACE THE ANCHOR WITHIN 100 FLIGHT HOURS PER REO 601R-52-11-272. (M) 2L72 4F RTA21EA 20031215001952003121500195EU 2003 12 15 USAA030258 120031030A5315D5347219020300 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND CORROSION ON BEAM 1.9 INCH BY 1.3 INCH BY .050 INCH DEEP, FRAME 64 INBOARD OF -Y1114 CABIN FLOOR SUPPORT. CORROSION LEVEL 2 TASK NR JA 260-53500. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11 AND 51-72-11. (M) 2L72 4F RTA28NM 20031216000132003121600013NM 2003 12 16 QXEA200301451 120031105A5410 STRUT DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- UPPER OUTBOARD ENGINE STRUT IS CHAFED AT TWO LOCATIONS AT INBOARD AFT END OF NR 2 NACELLE. REPAIRED IAW DHC-8 RD 8-54-036. 2H72 4T RTA13NM 20031216000302003121600030NM 2003 12 16 SWAA032600 120031122A3520417N3137 BALL BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29765SW 29805 DURING SCHEDULED RON CHECK, (DUE TO SWA SDR SWAA03-2584) FOUND PAX O2 SYS SWEDGED BALLS PULLED AT PSU'S 13 ABC AND 10 DEF. REATTACHED BALLS PER MM. 2L72 4F RTA16WE 20031216000362003121600036NM 2003 12 16 SWAA032552 120031119A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C3 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS, BS 797, STR 7L AND BS 500A, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031216000572003121600057NM 2003 12 16 SWAA032543 120031118A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND BS 188 RT FUSELAGE FRAME CRACKED AT WL 207. REMOVED AND REPLACED FRAME PER SRM. 2L72 4F RTA16WE 20031216000772003121600077NM 2003 12 16 SWAA032573 120031120A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 7L. REPAIRED BULKHEAD WEB PER SRM AND ERO. 2L72 4F RTA16WE 20031216000852003121600085NM 2003 12 16 SWAA032581 120031122A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031216000922003121600092EA 2003 12 16 03334669 120031130A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE BURNED OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031216001022003121600102SO 2003 12 16 C2XA03IA107 120031128A33501317 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712530 145533 DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THAT THE LAST OVERHEAD EMERGENCY LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED LAMP AND OPERATIONALLY CHECKED THE LIGHT. 2L72 4F RTT00011AT 20031217000192003121700019EA 2003 12 17 COMA0360502 120031106A5321601R3114627 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01949CA20501 7080 PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102. 2L72 4F RTA21EA 20031217000242003121700024EA 2003 12 17 COMA0360508 120031119A2621346000371 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01781CA11246 7312 FLIGHT 5133 CARGO FIRE BOTTLE LOW MESSAGE. REPLACED THE RT CARGO FIRE BOTTLE. 2L72 4F RTA21EA 20031217000382003121700038WP 2003 12 17 DHL2003805509 120030803A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT WING CTR L/E FRAME 1.000 CRACKED, STA XFS 454.976. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.042) (2024-T3 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031217000422003121700042WP 2003 12 17 DHL2003805505 120030812A573056488931 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XA 450.000 - XA 475.000). REMOVED UPPER PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ON LT WING T/E, STA XA 450.000 - XA 475.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031215000992003121500099EA 2003 12 15 QXEA200301436 120031113A2121AE0804A04 FAN CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09614QX3536 3536 10049 PDX- ON FLIGHT 2436 DISPLAY COOL CAUTION MESSAGE APPEARED AFTER TAKEOFF. COMPLIED WITH CHECKLIST SELECTION TO FLIGHT ALT FAN. MESSAGE EXTINGUISHED. REMOVED AND REPLACED COCKPIT DISPLAY FAN 1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031215001282003121500128WP 2003 12 15 AALA20030976 120030908A33508039001 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21407AA 49318 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE AT THE FORWARD AUXILIARY LIGHT POSITION. REPLACED BATTERY B5-103. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001882003121500188WP 2003 12 15 AALA20031197 120031101A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21591AA 53254 DEN - DURING OVERNIGHT MAINTENANCE, FOUND CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 18-20 INOPERATIVE. REPLACED BATTERY PACK AT B5-103. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031216000262003121600026NM 2003 12 16 SWAA032596 120031123A2121215201 GASPER FAN BOEING737 7372H4 138448CNM A/C BAY OVERHEATED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29090SW 22905 SMELL IN THE CABIN TURNED GASPER FAN OFF AND SMELL DECREASED. REMOVED AND REPLACED GASPER AIR FAN ASSY PER MM. 2L72 4F A16WE 20031217000152003121700015NM 2003 12 17 CALA0300658 120031121A5311 BELTFRAME BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711651 28912 INSPECTION FOUND BELTFRAME CORRODED AT STA 992, S17-18R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20031217000172003121700017EA 2003 12 17 03324621 120031120A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY SIGN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27621BR 7186 DURING INSPECTION, THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB IN THE SIGN WAS IDENTIFIED AS THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED ON THE EMERGENCY LIGHTING SYSTEM AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031217000282003121700028WP 2003 12 17 DHL2003805597 120030904A57203755028503 CLIP DOUG DC8 DC873F 302199FWP WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 NR 2 MAIN TANK CLIP CRACKED 1.000 AT STA XRS 22.750, S-61. REMOVED 505F, 560F ACCESS DOOR (INTERNAL). REMOVED CRACKED CLIP IAW SRM 51-1-20D PG 21. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9. REINSTALLED 560F, 505F ACCESS DOOR IAW MM 20-16-0 PG 201-202. FOR LEAK CHECK SEE NR 1894. 2L74 4F RT4A25 20031217000312003121700031WP 2003 12 17 DHL2003807537 120031021A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD ACCESSORY COMPT FRAME 1.000 CRACK AT STA 55.000 L-24L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT FRAME CRACKED SEGMENT AND FABRICATED NEW FRAME SEGMENT AND 2EA SPLICE ANGLES (ALCLAD 7075-0 0.071) IAW SRM 53-2-0 FIG 2. HEAT TREATED FRAME SEGMENT AND SPLICE ANGLES IAW SRM 51-1-1. CLEANED, TREATED AND PRIMED AREA, FRAME SEGMENT AND SPLICE ANGLES IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND SPLICE ANGLES APPLYING PRC SEALANT IAW SRM 53-2-0 FIG 2, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031217000562003121700056WP 2003 12 17 DHL2003805577 120030825A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING OTBD FLAP UPPER PLATING HAS INTERIM REPAIR AROUND STA XF 225.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGMENT (2024-T4 AL0.071) AND A SPLICE STRAP (2024-T3 AL0.080). CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT INTERIOR SURFACE AND THE SPLICE STRAP. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE NEW SKIN SEGMENT AND THE SPLICE STRAP ON LEFT WING OTBD FLAP UPPER FWD PLATING (AROUND STA XF 225.000) USING NEW FASTENERS. SEE N/R 2042 FOR NR 4 FLAP VANE REMOVAL AND REINSTALLATION. 2L74 4F RT4A25 20031217000672003121700067WP 2003 12 17 DHL2003807522 120031014A5730 DOUBLER DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT OTBD L/E STUB WING DOUBLER CRACKED AT STA XOLDO 67.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 2. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED DOUBLER (7075-T6AL 0.125) IAW SRM 57-2-1A FIG 2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031217000732003121700073WP 2003 12 17 DHL2003807530 120031025A57205644973502 SPLICE DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING SPLICE FITTING LOWER PLATING CRACKED AT STA XW 408.000, S-59 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-20D. REMOVED SPLICE FITTING (CRACKED) IAW SRM 51-1-20D PG 21. INSTALLED NEW SPLICE FITTING ON RIGHT WING, STA XW 408.000, S-59 WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, FOR LEAK CHECK SEE N/R 1482. 2L74 4F RT4A25 20031217000792003121700079NM 2003 12 17 CALA0300668 120030717A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND E&E COMPARTMENT CEILING STRAP CRACKED BETWEEN STA 312 AND 328, BL 0. REPAIRED IAW SRM 51-70-13. 2L72 4F RTA16WE 20031217000982003121700098NM 2003 12 17 CALA0300675 120031122A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND UPPER SURFACE OF O/B FLANGE OF LEFT KEELBEAM CORRODED AT STA 720. A REPAIR WAS INSTALLED IAW ECRA 5311-01177. 2L72 4F RTA16WE 20031217001032003121700103WP 2003 12 17 ABXA030446 120031121A2497 WIRE DOUG DC9 DC932 3022066WP BUSS PANEL BURNED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 WIRE BURNED ON PHASE C, GROUND SERVICE BUS POWER PANEL, WIRE HV X22810C. REMOVED BURNED AREA OF WIRE AND REPLACED WIRE END CONNECTOR. INSTALLED WIRE TO GROUND SERVICE BUS PHASE C IAW DC9 MM 20-50-01-2-0001. OPS CHECK GOOD. 2L72 4F A6WE 20031217001062003121700106SO 2003 12 17 C2XA03CL191 120031124A326023092900001 UPLOCK SENSOR EMB 145 EMB145ER 3260211SO NLG FAULTY A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW2712934 145019 CLE FLIGHT 2104 THE CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT ON THE FIRST ATTEMPT AFTER TAKEOFF. THE GEAR WAS CYCLED AND OPERATED NORMALLY THE 2ND TIME. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK BOX AND THE PROXIMITY SWITCHES ON THE UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD. P/N PROXIMITY SWITCHES 8-527-01, S/N A22621 AND 4922. 2L72 4F RTT00011AT 20031217001072003121700107NE 2003 12 17 03FDEA01900 220031106A7200 ENGINE AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE NR 2 INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25455FE 331 716107 TAKEOFF WAS ABORTED AT 70 KTS DURING TAXI NR 2 ENG HAD TO BE VWD OF NR 1 ENG BY 1 1/2 THROTTLE WIDTHS TO MAKE 40 PERCENT N1. DURING TAKEOFF NR 2 ENG WOULD ONLY MAKE 75 PERCENT PWR WITH THROTTLE ALL THE WAY FWD. NO ENG PARAMETERS WERE CLOSE TO THE LIMITS. POWERPLANT ENG HAS APPROVED THIS NR 2 ENG FOR CHANGE. 2L72 4F4 FRTA35EU E3NE 20031217001132003121700113NM 2003 12 17 2003UALA00851 120031112A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29563UA 26665 FUSELAGE RIGHT SIDE LOWER SKIN DENTED AND CREASED BS 215, STR 26R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031217001222003121700122WP 2003 12 17 AALA20031157 120031019A3350 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21571AA 49353 DFW - MAINTENANCE OBSERVED EMERGENCY LIGHT IN TAIL INOPERATIVE. SPLICED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031217001342003121700134NM 2003 12 17 SWAA032716 120031211A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 859, RBL 3 AND LBL 17. REPAIRED CORROSION PER SRM. 2L72 4F RTA16WE 20031217001472003121700147SO 2003 12 17 LR7A03085 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND CENTER FUSELAGE SKIN WARPED FS 697-737, RBL 60, WL 140-180. REPLACED RT FUSELAGE SKIN FS 697-737E IAW SRM SMP 583 51-60 & 51-70. NR 2020. 2H74 4T A1SO 20031217001492003121700149SO 2003 12 17 LR7A03087 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND LT FWD FUSELAGE SKIN CRACKED FS 160, LBL 50, WL 236. REPAIRED IAW SRM SMP 51-140-10. NR 2022. 2H74 4T A1SO 20031217001562003121700156GL 2003 12 17 P5CA0301005 220031213A73212718326 SOLENOID BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 3 ENGINE FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23452PA 30810 706221 NR 3 ENG FAILED TO START. REMOVED AND REPLACED NR 3 HMM SOLENOID SHUT OFF VLV IAW 73-21-20. ENG RUN-UP AND LEAK CK OK. 2L74 4F4 FRTA20WE E23EA 20031217001582003121700158NM 2003 12 17 0302166315 120031209A2530 CONTROLLER BOEING747 747451 1384940NM GALLEY OVEN SMOKE A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01675NW 33001 DURING FLIGHT, SMOKE EMITTED FROM THE NR 1 GALLEY AS BOTH OVENS IN THE NR 1 GALLEY TURNED OFF AND ON TRIPPING THE NR 1 CIRCUIT BREAKER. THE CIRCUIT BREAKERS ON BOTH OVENS WERE PULLED AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 OVEN AND CONTROLLER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031217001622003121700162EU 2003 12 17 AWXA200301535 120031214A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU EMERGENCY LIGHT MALFUNCTIONED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28627AW41876347 66 DURING INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEAT ROWS 13, 17, 19, & 24. MAINTENANCE REMOVED AND REPLACED AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), ALSO FOUND SHORT TO GROUND AT SEAT ROW 19 AT 6690VN DCI; REPAIRED BROKEN WIRES AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. PART NAME: CABLE, MFG; AIRBUS, P/N; ABS0374A24, REASON; SHORTED, LOC; SEAT ROW 19 LT. 2L72 4F RTA28NM 20031217002012003121700201NM 2003 12 17 AWXA200301495 120031113A5743656717217 FITTING BOEING737 7373G7 1384595NM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR WING DOOR ATTACH ANGLE AFT SUPPORT FITTING AT INBOARD AND OUTBOARD FACES. MAINTENANCE REMOVED CORRODED LT MAIN LANDING GEAR WING DOOR ATTACH ANGLE AFT SUPPORT FITTING; FABRICATED A NEW REPLACEMENT SUPPORT FITTING PER DWG 65-67172; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, FIG 401 PG 1-8 & FIG 402 PG 4. 2L72 4F RTA16WE 20031217001272003121700127WP 2003 12 17 ABXA030465 120031124A531099577397N SHEAR TIE DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 SHEAR TIE REPAIR CRACKED FS 1021, BETWEEN LONGERON 15 LEFT AND LONGERON 16 LEFT. REMOVED CRACKED SECTION, LOCATED AND DRILLED NEW FRAME FORMER IAW DC-9 SRM 51-1-4 AND 53-03, INSTALLED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20031217002112003121700211EA 2003 12 17 SWIA200312618 120031124A2760 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07460SW 7803 INBOARD GROUND SPOILERS WILL NOT RETRACT AFTER LANDING. REMOVED AND REPLACED GROUND SPOILER MANIFOLD IAW MM 27-63-00. OPS AND LEAK CHECK GOOD. P/N: 60175124-, S/N OFF: 1193. 2L72 4F RTA21EA 20031217002142003121700214EA 2003 12 17 SWIA200312621 120031124A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 484 RIGHT INTERCOSTAL INBOARD AND OUTBOARD ANGLES RBL 27 AND RBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. ''A'' AND RII 53-401. 2L72 4F RTA21EA 20031218000062003121800006NE 2003 12 18 P5CA0300992 220031119A731438690113 PUMP BOEING747 747236B 1384804NM PWA JT9 JT9D7Q 52054NE NR 1 ENGINE LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 WP23924FT 21730 702032 ON ARRIVAL NR 1 ENG HAS HEAVY FUEL LEAK OUT OF DRAIN. REPLACED NR 1 ENGINE FUEL PUMP RUN UP & LEAK OK PER MM 73-11-01 AND 71-00-00. 2L74 4F4 F A20WE E3NE 20031218000082003121800008 2003 12 18 P5CA0300995 420031122A2397 WIRE BOEING747 747200 1384847NM CONTROL PANEL SHORTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 UNABLE TO GET F/O'S MACH TO WORK PROPERLY (F/O'S YOKE MIKE SWITCH INOP). REPAIRED WIRES AT F/O'S MASK TACH PNL REF 23-51-00. 2L74 4F RTA20WE 20031218000142003121800014NM 2003 12 18 MWEA030451 120031124A49504951922 VALVE BOEING717 717200 1383700NM APU INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31903ME 55167 AUXILIARY POWER UNIT DISAGREE ALERT ON START ATTEMPT AND LOW AIR PRESSURE INDICATED. REMOVED AND REPLACED AUXILIARY POWER UNIT BLEED AIR VAVLE. 2L72 4F TRA6WE 20031218000332003121800033EA 2003 12 18 SWIA200312628 120031122A2741 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM ILLUMINATED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07452SW 7716 RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES IN FLIGHT. COMPLIED WITH QRH, COULD NOT RE-ENGAGE ANY STAB TRIM SYSTEM. TESTED AND FUNCTIONALLY CHECKED STAB TRIM AND HSTCU SYSTEM IAW MM 27-40-00. NO FAULTS FOUND. 2L72 4F RTA21EA 20031218000412003121800041WP 2003 12 18 03FDEA01984 120031126A2160 REGULATOR VALVE DOUG DC10 DC1030 3023501WP TRIM AIR INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25316FE 48314 SHORTLY AFTER TAKEOFF TRIM AIR OFF LIGHT ILLUMINATED COURIER SUPPLY TEMP INCREASED TO 215 DEG IT THEN DROPPED AND TRIM AIR OFF LIGHT EXTINGUISHED. SUPPLY TEMP ROSE AGAIN, CYCLED REPEATED MULTIPLE TIMES. RETURNED TO BASE. BOTH TRIM AIR PRESSURE REGULATOR VALVES INOP. TRIM AIR SWITCH MUST BE SELECTED. 2L73 4F A22WE 20031218000462003121800046NE 2003 12 18 03323621 220031119A7320 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE OUT OF ADJUST A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27621BR 7186 DURING UNKNOWN PHASE OF AIRCRAFT OPERATION THE RT THRUST REVERSER WAS REPORTED BINDING AT MAX POWER AND UPON DEPLOYMENT OF THRUST REVERSER. THE FUEL CONTROL RIGGING WAS FOUND TO BE OUT OF ADJUSTMENT AND WAS RE-RIGGED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031218000552003121800055WP 2003 12 18 0302121232 120031109A5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01232NW 46961 DURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 1521 L42R. REPAIRED PER EA 12-196599. 2L73 4F A22WE 20030919000152003091900015WP 2003 9 19 03FDEA01237 120030810A5753ARC0502 HINGE DOUG DC10 DC1030 3023501WP RT FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 MDIS 311 57-10 0008867 06AUG03 BFM CLOSE R COMPLLY WITH EA 8-5750-72247 WINGS- RT OUTBOARD FLAP -INBD HINGE CORROSION REPAIR (P/N ARCO502). FACT 08AUG03 19:35 BFM R COMPLIED WITH EA 8-5750-72247 WINGS-RT OUTBOARD FLAP -INB'D HINGE CORROSION REPAIR (P/N ARC0502). 2L73 4F A22WE 20030919000332003091900033EU 2003 9 19 U30A200300032 120030808A2751 WARNING LIGHT AIRBUS320 A320212 3930322EU TE FLAPS ILLUMINATED A U30AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA17265AV 427 ON THE GROUND AFTER FLT 304, BWI- PUJ, THE CREW RECEIVED AN ECAM MESSAGE " F/CTL SYS NR 2 SLAT FAULT". MAINTENANCE ACCOMPLISHED TASK PER AMM 27-80-00-869-004. RECYCLED FLAPS A COUPLE OF TIMES AND SYSTEM PERFORMED NORMAL, WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030919000362003091900036CE 2003 9 19 ACE080903 120030809A3710D9141 FILTER CESSNA207 207A 2073604CE VACUUM SYS CLOGGED E YADAA UNSCHED LANDING O OTHER CRCRUISE 1 AL0375941285 20700656 AFTER DEPARTURE, PILOT REPORTED VACUUM INOP, RETURN TO AIRPORT. REPLACED CENTRAL VACUUM FILTER, D.G. AND ATTITUDE GYROS DUE WATER CONTAMINATION. 1H71 3O A16CE 20031006001442003100600144 2003 10 6 SWAA032010 420030905A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING PREFLIGHT INSP, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031006001552003100600155NM 2003 10 6 SWAA032021 120030909A3350BR2013 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED CHECK, FOUND SEVERAL EEPLS LIGHTS INOP AND FWD END CAP BROKEN. REMOVED AND REPLACED EEPLS LIGHTS AND FWD END CAP PER MM. 2L72 4F A16WE 20031007000222003100700022NM 2003 10 7 AALA20030902 120030820A5320149T7686 INTERCOSTAL BOEING767 767323 1385205NM FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21363AA 24044 INTERCOSTAL ASSEMBLY HAS DAMAGE AS SHOWN ON SKETCH INTERCOSTAL CRACKED IN TWO LOCATIONS, BS 1112 AND 1128. CLEAN UP DAMAGE, ROUTE OUT CRACK, REMOVED ALL SHARP EDGES, VERIFY CRACKS COMPLETELY REMOVED. FABRICATE REPAIR PARTS FROM 301 .5 HARD, .050 INCH. FINISH WITH TWO COATS B195 10-11 PRIMER. APPLY ALODINE AND PRIMER TO ALL BARE ALUMINUM SURFACES. INSTALL ALL FASTENERS AND REPAIR PARTS WET WITH BMS 5-95 SEALANT. REFER TO FIGURE FOR REPAIRS CONFIGURATION AND FASTENER TYPES. (M) 2L72 4F RTA1NM 20031007000472003100700047NM 2003 10 7 GAIA03080OP 120030902A2910BAC65P0341CCW HOSE BOEING727 727223 1384074NM NR 1 ENGINE LEAKING A GAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07858AA 21085 AFTER TAKEOFF FROM ATL AT 1000 FT AGL THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC FLUID WAS LOST. THE CREW RETURNED TO ATL MANUALLY EXTENDING THE LANDING GEAR AND FLAPS. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 1 ENGINE DRIVEN PUMP CASE DRAIN LINE AND NR 1 AND NR 2 ENGINE DRIVEN PUMP CASE DRAIN FILTERS. REMOVED AND REPLACED 'A' SYSTEM MAIN FILTER AND SERVICED HYDRAULIC SYSTEM. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031007000582003100700058NM 2003 10 7 03FDEA01617 120030924A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT . REMOVED CORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT OF A AREA 2 X 2 X .005 OF ORIGINAL .063 MATERIAL. FOUND IN LIMITS I.A.W. BOEING SRM 53-30-1. WORK DONE IAW BOEING 727 SRM 53-10-1, BOEING 727 SRM 53-30-3, BOEING 727 SRM 51-30-2, BOEING 727 SRM 51-10-6. 2L73 4F4 FRTA3WE E2EA 20031007000832003100700083NM 2003 10 7 SWAA031957 120030830A5240BAC1490 GUSSET BOEING737 7373H4 1384600NM FWD SVC DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER GUSSET CRACKED AT OUTBD FASTENER. REPAIRED AFT LOWER GUSSET PER SRM. 2L72 4F RTA16WE 20031007001272003100700127WP 2003 10 7 MWEA030375 120030916A533059102285 SKIN DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY .25 INCH OUT OF RIVER HOLE AT STATION 1437 BETWEEN LONGERON 2 AND 3 LEFT. REMOVED CRACK IN SKIN, FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F A6WE 20031008000052003100800005EA 2003 10 8 03251644 120030908A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27644BR 7379 DURING MAINTENANCE INSPECTION THE RIGHT HAND EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031008000182003100800018EA 2003 10 8 03256695 120030913A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27695BR 7772 DURING MAINTENANCE INSPECTION THE LT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031008000652003100800065WP 2003 10 8 MEX2003433 120030917A3241392491 CONTROL VALVE DOUG DC9 DC987 3022087WP ANTI SKID SYS MALFUNCTIONED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23214AM 49585 AIRCRAFT RETURN TO PLATFORM DUE TO DURING TAXI THE FOURTH ANTI-SKID LIGHT TURNED ON. CIRCUIT BREAKERS WERE RESET AND ANTI-SKID BOX CONNECTORS WERE CLEANED NON REPRODUCING THE FAIL. AFTER WORKS, CAPTAIN REPORTED THE ANTISIDE LIGHTS TURNED ON AGAIN. DURING CHECK, IT WAS DETECTED THAT THE DUAL PRESS CONTROL VALVE WAS OUT OF SERVICE. IT WAS REPLACED IAW MM 32-43-03, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20031009000642003100900064 2003 10 9 SWIA200312388 420030903A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTO-PILOT MALFUNCTIONED A SWIAO OTHER LF NO TEST FLT CONT AFFECTED UKUNKNOWN 1 NM07292UX6727 6727 120292 FD FLAG CAPT SIDE, FOS FD ERATIC WILL NOT CAPTURE AUTOPILOT, EITHER SIDE. DOES NOT TEST ON GROUND. REPLACED CAPT APC 65B AUTOPILOT COMPUTER. OPS CHECK GOOD IAW MM 22-10-00. PN ON 622-8315-402 SN ON 3332 OFF 131. 2L72 4T RTA31SO 20031009000702003100900070NE 2003 10 9 00112 220030911A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05977TW 13 PILOT REPORTED LT ENGINE FLAMED OUT DURING CLIMB. NORMAL RESTART PERFORMED. POST FLIGHT INSPECTION REVEALED NO DAMAGE. WILL UPDATE THIS REPORT WHEN AIRCRAFT GOES INTO MAINTENANCE. 2L72 4F4 F A7EU E7EA 20031125000292003112500029WP 2003 11 25 DHL2003805567 120030730A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E CORRODED BETWEEN STA XFS 422.750 AND XOLDI-6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG 38. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. REFER TO NR 0184 FOR LEFT WING CTR L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031125000322003112500032WP 2003 11 25 DHL2003805564 120030814A5313S1616757 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 AFT FUSELAGE SECTION L-17L AT STA 1770.000 CRACKED 4.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED L-17L WITH CRACK IN IT IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031125000412003112500041WP 2003 11 25 DHL2003805531 120030829A573056110101 SKIN PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED (STA XW.5.000 - 47.00). REMOVED AND REPLACED LWR WING T/E LWR PANEL (STA XW.5.000 - 47.000) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000442003112500044WP 2003 11 25 DHL2003805522 120030808A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 416.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER ON LT WING CTR L/E FORMER (STA XFS 416.500) IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000872003112500087WP 2003 11 25 DHL2003805544 120030731A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING OUTBD L/E FORMER 0.500 CRACKED, STA XFS 753.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. FOR REMOVAL AND REINSTALLATION OF OTBD L/E SEE NR 0345. 2L74 4F RT4A25 20031125001032003112500103WP 2003 11 25 AALA20031292 120031118A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21494AA 49732 DFW AFT SEAT MOUNTED EMERGENCY LIGHT AT 7D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031125001132003112500113SW 2003 11 25 2003F00616 120030606A212039290811 CONTROL VALVE FRCHLDSA227 SA227DC 3377521SW A/C BAY MALFUNCTIONED A BSAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM05453LA DC852B WITH BLEEDS OFF, CREW WAS GETTING AIRFLOW INTO CABIN THAT SMELLED OF SMOKE. CREW FOLLOWED PROCEDURES AND LANDED AT THE NEXT STATION, WHICH WAS THE CLOSEST. IT WAS SUSPECTED THAT A FLOW CONTROL VALVE STUCK OPEN, THE ENVIRONMENTAL AIR DUCTING GOT HOT, WHICH CAUSED SMOKE. REPLACED THE FLOW CONTROL VALVE, SYSTEM OPS CHECKED GOOD. (M) 2L72 4T RTA18SW 20031125001312003112500131NM 2003 11 25 ASAA0310157 120030318A532065559061 FITTING BOEING737 737210C 1384459NM FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FITTING AT BS 947, LEFT BUTTOCK LINE 65 BENT. REMOVED AND REPLACED FITTING PER BOEING DRAWING. (M) 2L72 4F A16WE 20031125001412003112500141NM 2003 11 25 ASAA0340119 120030308A532065C30424 SUPPORT ANGLE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 PAE - DURING C-CHECK, FOUND CORROSION ON AFT BULKHEAD OF FLOOR SUPPORT. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031125001432003112500143NM 2003 11 25 ASAA0310520 120030724A335086210144 BATTERY BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHT TESTED NORMAL. (M) 2L72 4F RTA16WE 20031125001492003112500149NM 2003 11 25 ASAA0310150 120030317A5315655490510 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM FLANGE AT BS 480, LEFT BUTTOCK LINE 43 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040311000232004031100023NM 2004 3 11 ASAA0310122 120030307A7110657377414 FRAME BOEING737 737298C 1384490NM NR 2 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 179 CHAFED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20040311000602004031100060NM 2004 3 11 ASAA0310139 120030314A53106545855507 CREASE BEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CREASE BEAM WEB AT BODY STATION 907-947, RIGHT BUTTOCK LINE 66 CORRODED AND HAS ELONGATED HOLES. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. (M) 2L72 4F RTA16WE 20040311000442004031100044NM 2004 3 11 ASAA0310102 120030306A5311BAC14902807 FRAME BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 SW21745AS 20794 OKC - DURING D-CHECK, FOUND FRAME AT BS 947, STRINGER 19R-20R CORRODED. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031125001582003112500158NM 2003 11 25 ASAA0310493 120030601A335088210144 BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - DURING INSPECTION, FOUND OVERWING EXIT IDENTIFIERS WITH DISCHARGED BATTERY. REMOVED AND REPLACED BATTERIES, THEN EXIT IDENTIFIERS OPERATED NORMALLY. (M) 2L72 4F A16WE 20031125001642003112500164NM 2003 11 25 ASAA0310513 120030603A53156567140139 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 549-727A, LEFT BUTTOCK LINE 24.5 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER EA. (M) 2L72 4F RTA16WE 20031126000082003112600008SO 2003 11 26 RAIA00311285 120031110A7830 ACTUATOR EMB 145 EMB145 3260210SO THRUST REVERSER OUT OF ADJUST A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03802HK 145066 5321-PIT- THRUST REVERSER DISAGREE RT SIDE. MAINTENANCE DEFERRED NR 2 THRUST REVERSER PER MEL 78-30-00. SUBSEQUENTLY CLEARED DMI BY ADJUSTING UPPER AND LOWER DOOR ACTUATOR READING. 2L72 4F RTT00011AT 20031126000182003112600018EA 2003 11 26 QXEA200301399 120031104A7120 YOKE CNDAIRCL600 CL6002C10 1390015EA NR 1 ENGINE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX- NR 1 ENGINE MOUNT YOKE LOWER LOBE GOUGED ON TOP SIDE FORWARD EDGE ABOVE LOWER BEARING. REPAIRED IAW CRJ 700 NDTM 51-20-06. 2L72 4F RTA21EA 20031126000292003112600029WP 2003 11 26 DHL2003805595 120030830A53305656352505 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT LOWER FUSELAGE PANEL NR 736 INTERNAL SKIN DELAMINATED STA 1040.000 - STA 1060.000. REMOVED AND REPLACED LEFT LOWER FUSELAGE PANEL NR 736 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031126000422003112600042EA 2003 11 26 COMA0360492 120031029A531160036030 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA18882 7123 RT 718 FRAME CRACKED. REPAIRED IAW SERVICE BULLETIN 601R-53-055. 2L72 4F RTA21EA 20031126000682003112600068NM 2003 11 26 AWXA200301478 120031122A2560P4010021 BATTERY BOEING737 737301 1384611NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031126000752003112600075SO 2003 11 26 C2XA03SH451 120031112A532014525681011 ANGLE EMB 145 EMB145ER 3260211SO FUSELAGE WARPED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE ANGLE ON THE CARGO CUT FRAME 67 WAS FOUND TO BE WARPED OUT OF CONFIGURATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126000922003112600092SO 2003 11 26 C2XA03SH452 120031112A532014522226003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE OMEGA BEAM BUTTSTRAP AT FRAME 58 TO 62 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126000972003112600097SO 2003 11 26 C2XA03SH405 120031022A532014522459003 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040415001642004041500164NM 2004 4 15 ASAA024015G 120030318A5330656571035 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION AT BS 727D PLUS 2-12, RBL 0 WL 148 ON ANTENNA DOUBLER. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040419000782004041900078WP 2004 4 19 ASAA0380813 120031126A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS PUNCTURE AT FS 920-1003. BOND-REPAIRED PER SRM 51-70-3. (M) 2L72 4F RTA6WE 20040112001732004011200173WP 2004 1 12 GTIA031007 120031116A5340 FITTING DOUG DC9 DC981 3022081WP FUSELAGE WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN STATION 1309 LBL 34 - LBL 49 B/H L BRACKET WORN IN SEVERAL AREAS. UPON FURTHER EVALUATION, FOUND FITTING CRACKED AT STATION 1309 LBL 34. REMOVED FITTING. DRILLED AND LOCATED NEW FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20040112001772004011200177NM 2004 1 12 EIA2003147 120031026A7932699923 HOSE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 1 ENGINE OIL FAILED A EIAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09482EV 20713 NR 1 ENGINE OIL QUANTITY DECREASED RAPIDLY ON CLIMB OUT FROM EROS. REDUCED NR 1 ENGINE TO IDLE AND DECREASED LESSEND , PERFORMED FUEL JETTISON AND RETURNED TO EROS. CORRECTIVE ACTION SECURED CLAMP MID POSITION NR 4 BEARING SCAVENGE LINE RETORQUED MID (B) NUT ASSY LINE. LINE CHECK GOOD AFTER ENGINE RUN IAW MM 71-00-00, 79-15-01, 12-13-03, OIL TANK SERVICE TO FULL. 2L74 4F4 F A20WE E20EA 20040112002282004011200228EU 2004 1 12 BAQA091530 120031211A2612 PROBE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE WIRE HARNESS BROKEN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365KY1269 5154B5160B 6529 PROBE BROKEN FROM HARNESS. RETAINING NUT ON PROBE BROKEN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H10EU E19EU 20040112002632004011200263WP 2004 1 12 AALA20031468 120031224A33970201720003 WIRE HARNESS DOUG DC9 DC982 3022082WP CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21475AA 49650 EMERGENCY PATH LIGHTING SEAT 7D INOPERATIVE. REPLACED EMERGENCY PATH LIGHTING HARNESS AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040112002652004011200265NM 2004 1 12 AALA20031419 120031213A3350 CONNECTOR BOEING767 767223 1385123NM CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21328AA 22328 SFO EMERGENCY LIGHT AT SEAT 33B INOPERATIVE. REPLACED EMERGENCY LIGHT CONNECTOR AT SEAT 33A/B. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA1NM 20040112002672004011200267NM 2004 1 12 AALA20031463 120031222A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21174AA 31308 AFT RT ENTRY DOOR FUSELAGE MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT MOO756 FOR AFT RT ENTRY DOOR FUSELAGE MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040112002702004011200270NE 2004 1 12 AALA20031436 220031215A7510 DUCT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT ENGINE BLOWN A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21455AA 49560 DFW T1527/15 ENROUTE DFW-SEA AT 2500 FEET LT ENGINE ILLUMINATED. AT 3000 FEET FIRE LIGHT EXTINGUISHED AND LT THROTTLE JAMMED FOR ABOUT TWO MINUTES AT 1.5 EPR SETTING AND THEN RETURNED TO NORMAL. RETURNED DFW AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED DEBRIS FROM UPPER COWL DAMAGE FROM BLOWN ENGINE ANTI ICE DUCT MIGRATED TO FUEL CONTROL LINKAGE. REMOVED DEBRIS AND REPLACED ANTI ICE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F4 F A6WE E9NE 20040113000142004011300014EU 2004 1 13 BAQA090673 120031203A671010513221 DRIVE LINK BOLKMS117 BK117B1 5626012EU MAIN ROTOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 DRIVE LINK HAS PLAY. REPLACED WITH SERVICEABLE UNIT. 12/3/03 1G72 3U H13EU 20040113000182004011300018EU 2004 1 13 BAQA091877 120031229A2497 WIRE AEROSPSA365 SA365N 8680669EU STARTER GEN SHORTED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 151 3111 6425 "D" WIRE SHORTED TO "C" CONNECTOR. GENERATOR WILL NOT LOADSHARE. HARD CARD ENCLOSED. PART REPLACED WITH SERVICABLE UNIT. 01/08/2004 1G72 3U H10EU 20040113000342004011300034GL 2004 1 13 BAQA089603 220031105A732023070606 FUEL CONTROL AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20F 03013GL ENGINE MALFUNCTIONED B BAQAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 EA03912KY260 5500 FUEL CONTROL PRODUCING HUNG STARTS, OCCURING BETWEEN 50 PERCENT AND 60 PERCENT. REPLACED WITH SERVICEABLE UNIT. 11/10/03 1G72 3U3 U H11EU E4CE 20040113000532004011300053 2004 1 13 BAQA091155 420031125A3455066107204 RECEIVER AEROSPAS355 AS355F2 8680812EU ADF FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03941MS5304 5495 RECEIVER DISPLAY DOES NOT WORK. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20040113000862004011300086NM 2004 1 13 AWXA200301598 120031208A531565528941 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK THE CENTER LT FLOORBEAM T-CAP ANGLE WAS DISBONDED AT BS 540, LBL 22. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 540, LBL 22; FABRICATED A NEW REPLACEMENT T-CAP ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 16 PG 1, ITEM 9D. 2L72 4F RTA16WE 20040113000952004011300095NM 2004 1 13 UPS03M41654 120031212A5753 WEDGE DOUG MD11 MD11F 3023600NM T/E FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 INSPECTION TYPE:N/A LEFT O/B FLAP I/B TRAILING EDGE WEDGE HAS DELAMINATION (MRK). REMOVED AND REPLACED LEFT OUTBOARD FLAP INBOARD TRAILING EDGE WEDGE. THIS CLOSES DEFER RAL D272416 PER 57-50-03. REFERENCE LP33934. 2L73 4F RTA22WE 20040113000962004011300096NM 2004 1 13 QXEA200301577 120031222A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH1473414734 494 PDX- EMERGENCY LIGHT BATTERY PACK AT PS3 THROUGH PS6 REQUIRES REPLACEMENT DUE TO LOW VOLTAGE. REMOVED AND REPLACED POWER SUPPLY. 2H72 4T RTA13NM 20040113001182004011300118GL 2004 1 13 ALGA091474 220031209A725023007157 BEARING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C47B GL TURBINE SECTION ROUGH B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAG95112 TURBINE SECTION BEARING FOUND TO BE ROUGH AFTER INSTALLATION. 1Q71 3R3 U 2A6 E1GL 20040113001612004011300161EU 2004 1 13 BAQA091260 120031124A28221176415103 PUMP BOLKMS117 BK117A1 5626010EU BOOSTER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME6563 7243 PUMP IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20040113001822004011300182SO 2004 1 13 RAIA00312297 120031202A361014531637003 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS WORN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03818HK 145059 STL- BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING IN CARGO AREA UNDER FLOOR RIGHT SIDE. 2L72 4T RTT00011AT 20040113002112004011300211SO 2004 1 13 C2XA03SH498 120031217A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 16 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040113002262004011300226NM 2004 1 13 QXEA200301569 120031215A2697 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM FIRE DETECTION FAULTY A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09410QX 4053 CHECK FIRE DETECTION WARNING LIGHT ILLUMINATED EN ROUTE ALONG WITH RT SIDE A AND B ILLUMINATED. REMOVED AND REPLACED FIRE DETECTOR WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040113002352004011300235NM 2004 1 13 QXEA200301476 120031127A5210 MECHANISM BOMBDRDHC8 DHC8401 1390041NM PAX DOOR OUT OF ADJUST A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09404QX 4046 SEA- ON FLIGHT 2374 DURING LANDING, HANDLE ON AFT PASSENGER STAIR DOOR POPPED OPEN AND VENT OPENED. DOOR WARNING PANEL SHOWED UNSAFE. ADJUSTED VENT DOOR MECHANISM IAW TASK 52-00-00-830-801 AND HANDLE FORCES CHECK GOOD IAW TASK 52-00-00-830-802. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040114000202004011400020 2004 1 14 03314331 420031110A3160 AHRS JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP NR 2 FAILED A VTZAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 EA27331UE 41099 DURING CLIMB PHASE OF FLIGHT 7844 THE CREW REPORTED A NR 2 AHRS FAILED RESULTING IN THE LOSS OF PRIMARY FLIGHT INFORMATION FOR THE FIRST OFFICER. 2L72 4T3 TRTA41NM E2WE 20040114000212004011400021NM 2004 1 14 03FDEA01954 120031117A5753ARC0154502 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT INBOARD FLAP FOUND OUTBOARD HINGE UPPER O/B MOUNTING HOLE WING SIDE WITH CORROSION. RT I/B FLAP O/B HINGE UPP O/B MOUNTING HOLE WING SIDE CORROSION REPAIRED AS PER FEDEX EA 1-5740-74253, 2L73 4F RTA22WE 20040114000232004011400023EA 2004 1 14 SWIA200312587 120031112A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 FS 280 LEFT FLOORBOARD LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11 & RII 53-401. 2L72 4F RTA21EA 20040114000252004011400025EA 2004 1 14 SWIA200312589 120031112A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 FS 484 RIGHT INTERCOSTAL OUTBOARD FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV ''A'' & RII 53-401. 2L72 4F RTA21EA 20040114000612004011400061NM 2004 1 14 DLM88030978 120031101A3510359701025 HOSE DOUG MD88 MD88 3023688NM COCKPIT LEAKING A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27919DL 49584 CAPT`S O2 MASK HAS LEAK IN HOSE 6 INCHES BELOW MASK. REPLACED MASK/HOSE ASSY. 2L72 4F RTA6WE 20040114000632004011400063NM 2004 1 14 DL76L030979 120031102A2510832200602 SEAT BOEING767 767332 1382001NM COCKPIT MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27183DN 27110 DURING OPERATION OF CAPT SEAT WHEN REACHING THE AFT MOST POSITION THE ELEC SWITCH REMAINED ON AND THE MOTOR EMITTED AN ELEC SMELL AND THE P6 CB POPPED. THE SEAT COULD NOT BE MOVED MANUALLY AND REMAINS IN THE AFT POSITION. REMOVED AND REPLACED CAPTS SEAT. OPS CHECK GOOD. 2L72 4F RTA1NM 20040114000662004011400066 2004 1 14 DL73G030981 420031105A34414618000208 IRU BOEING737 73735B 13844BMNM NR 1 FAILED A DALAA UNSCHED LANDING G MULTIPLE FAILURE APAPPROACH 1 SO27221DL 23970 DIV DUE TO LOSS OF ALL HEADING INFORMATION. REPLACED NR 1 IRU. 2L72 4F RTA16WE 20040114000802004011400080NM 2004 1 14 2003UALA00855 120031113A21401168171 HEATER BOEING777 777222 1385219NM PWA PW4077PW4077 NE DOOR 2 RT FAILED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29771UA31592 26932 BURNING RUBBER ODOR COMING FROM OVERHEAD VENTS IN NR 2 GALLEY. RECIRC FANS OFF, ODOR DISSIPATED. ODOR COMPLAINTS COMPLETELY STOPPED AFTER REPLACEMENT OF AREA HEATER AT DOOR 2 RIGHT. 2L72 4F4 FRTT0001SE E46NE 20040114000822004011400082WP 2004 1 14 UPS03841575 120031125A5610 ANGLE DOUG DC8 DC871F 302199DWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 WINDOW FRAME ZEE CHANNEL LT LWR CORNER PITTED AND CORRODED. REMOVED AND INSTALLED NEW ZEE ANGLE IAW UPS EO DC8-5330-19614-A. FERRY TO GSO FOR REPAIR REFERENCE GSO NRC 632693 2L74 4F RT4A25 20040114000852004011400085NM 2004 1 14 03FDEA01991 120031126A5510ALC8103 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB RIGHT UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION EXCEEDED EO LIMITATION. HOR STAB RH UPPER AFT PLANK 27R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1- 5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. 2L73 4F RTA22WE 20040114000942004011400094NM 2004 1 14 03FDEA01988 120031126A5314 KEELBEAM DOUG MD11 MD11 3023602NM FUSELAGE CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 WITH RESPECT TO OIL CANNING INSP AS PER EA 1-5310-55649 REV NO A POS P2 ON RIGHT KEEL WEB STA Y 1431 THRU 1441 BET STA Z -97.00 THRU -78.00 FOUND VALUE MEASURED TO BE 0.320 INCHES (EXCEEDED PER THE STATED 0.190 INCH LIMITS). RE-INSPECTION ON RH KEEL WEB STA Y1431 THRU 1441 BET STA Z -97.00 THRU -78.00 OIL CANNING AS PER EA 1-5310-55649B MEASURED TO BE 0.185 INCH FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20040114000992004011400099NM 2004 1 14 DLM88031038 120031120A4940AHSCXA034 RELAY DOUG MD88 MD88 3023688NM APU STARTER FAILED A DALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SO27968DL 53161 JUST PRIOR TO DEPARTURE, SMOKE COMING FROM APU COMPARTMENT. FOUND APU STARTER ON FIRE. DISCHARGED BOTH ENG/APU FIRE BOTTLES. REPLACED APU. 2L72 4F RTA6WE 20040114001132004011400113NM 2004 1 14 DL733031048 120031124A2530 OVEN BOEING737 737301 1384611NM FWD GALLEY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27948WP 23259 ON TAKEOFF, SMOKE FROM FWD GALLEY OVEN. REPLACED SAME. 2L72 4F RTA16WE 20040114001282004011400128NM 2004 1 14 2003UALA00868 120031117A2420 IDG BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29546UA 25367 DIVERTED TO HNL WITH RIGHT ENGINE GENERATOR PROBLEM. RIGHT INTEGRATED DRIVE GENERATOR (IDG) FAILURE. REPLACED RIGHT IDG. NORMAL WEAR, FOUND ONE BAD DIODE. 2L72 4F4 FRTA2NM E17NE 20040114001362004011400136NE 2004 1 14 SW07200300003 220030508A72504120T01P01 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE DAMAGED G FDKAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW07503MJ743 10058 E965325 BOROSCOPE INSPECTION WAS REQUIRED BECAUSE OF VIBRATION PEAK. THE INSPECTION REVEALED DAMAGE HIGH PRESSURE TURBINE FAILURE. 2L72 4F4 FRTA21EA EOOO63EN 20040113001342004011300134NM 2004 1 13 03FDEA02255 120031226A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP O/B FWD HINGE ACTUATOR MOUNT I/B LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75210. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040113001382004011300138NM 2004 1 13 03FDEA02259 120031226A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, O/B FLAP I/B FWD HINGE AFT MOUNT LOWER MATING SURFACE CORRODED. O/B FLAP I/B FWD HINGE AFT MOUNT LOWER MATING SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DRAWING ARC0502 IN ACCORDANCE WITH FEDEX EA 1-5750-75209, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT O/B FLAP I/B HINGE BRACKET REPAIR 2L73 4F RTA22WE 20040113001682004011300168EU 2004 1 13 I05R091298 120031023A6240SVEURO4 AMPLIFIER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE MAST MOMENT FAILED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05551BA1383 188 SENSOR AMPLIFIER FAILURE, REPLACED PART. 1G72 3U3 UO H88EU E42NE 20040113001862004011300186SO 2004 1 13 RAIA00312301 120031204A5242 ACCESS DOOR EMB 145 EMB145 3260210SO EXTERNAL POWER UNSECURE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03806HK 145112 STL- LOUD RATTLING NOISES COMING FROM LEFT FWD NOSE SECTION. MAINTENANCE SECURED GPU ACCESS DOOR. 2L72 4F RTT00011AT 20040113001982004011300198NM 2004 1 13 AALA20031265 120031113A2612 FAN BOEING767 767323 1385205NM AFT CARGO INOPERATIVE A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW21382AN 25451 ORD - FLT 189 - EN ROUTE BOS-LAX - CARGO COMPARTMENT FIRE DETECTION SYSTEM INOPERATIVE. LANDED ORD WITHOUT INCIDENT. REPLACED AFT CARGO DET FAN 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040114000372004011400037NM 2004 1 14 DL777030949 120031025A5220258040002 SLIDE BOEING777 777232 1385232NM L-2 DOOR UNSERVICEABLE A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27865DA 29737 AT DEPARTURE L-2 DOOR SLIDE CAME OFF THE DOOR. REPLACED L2 DOOR SLIDE ASSEMBLY. 2L72 4F RTT00001SE 20040114000732004011400073NM 2004 1 14 DLM90030989 120031107A2913623337 PUMP DOUG MD90 MD9030 3023690NM LT ENGINE FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27910DN 53390 LT HYDRAULIC PRESSURE WENT TO ZERO SHORTLY AFTER TAKEOFF. FOLLOWED POM PROCEDURE BUT LT PRESSURE WOULD NOT RETURN. AFTER A FEW MINUTES RT HYD TEMP HI MSG CAME ON. REPLACED LT ENG HYD PUMP AND FILTERS. 2L72 4F RTA6WE 20040114001142004011400114CE 2004 1 14 DXTA200300173 120031126A3246314901 WHEEL CESSNA500 560CESSNA 2076750CE PWA JT15 JT15* 52060NE MLG FAILED E DXTAO OTHER O OTHER LDLANDING 1 GL07376QS 5600276 SHORTLY AFTER LANDING BOTH MAIN TIRES BLEW OUT ON LANDING. AIRCRAFT CAME TO A COMPLETE STOP ON ACTIVE RUNWAY AND NEEDED TO BE REMOVED BY AIRPORT OPERATIONS. PEFORMED FOD, HIGH DRAG SIDE LOAD AND HARD LANDING INSPECTION, FOUND AIRCRAFT HAD BOTH MLG DOORS AND LIGHTS DAMAGED, BOTH WING TIPS DAMAGED. REMOVED AND REPLACED BOTH MLG WHEEL AND BRAKE ASSEMBLIES. PERFORMED INTERIM REPAIR, SECURED AIRCRAFT FOR A ONE TIME FERRY FLIGHT TO ICT FOR PERMANENT REPAIR. 2L72 4F4 TRTA22CE E1NE 20040114001472004011400147CE 2004 1 14 DXTA200300171 120031122A215073838433 ACM CESSNA750 750 2076810CE CABIN COOLING FAILED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07944QS 7500144 DURING DESCENT HAD SMOKE IN COCKPIT TURNED OFF LEFT CABIN PAC AND SMOKE CLEARED, LANDED SAFELY AT GSO. TROUBLESHOT AND FOUND FAULTY COCKPIT ACM TURBINE, REMOVED AND REPLACED ACM, SYSTEM OPS CHECKED GOOD IAW CESSNA 750 MM CHAPTER 21-51-00. 2L72 4J RTT00007WI 20040114001672004011400167EU 2004 1 14 MALA030571 120031229A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING EMERGENCY BATTERY CAPACITANCE CHECK, NOTED 21LN LED FLASHING. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY PN 3301-51, SN/ON 1414, SN/OFF 1366 IAW SAAB AMM CHAP 33-50-10-4(1). OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20040114001872004011400187EA 2004 1 14 MASA200300509 120031223A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF341A NE CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0787353 7353 CAPTAIN REPORTED A CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MECHANIC RELAMPED. OP CHECKS GOOD 2L72 4F4 FRTA21EA E15NE 20040114001932004011400193SO 2004 1 14 MASA200300438 120031106A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07840MJ 145429 PAX DOOR EMERGENCY OVERHEAD LIGHT INOP - RELAMPED 2L72 4T RTT00011AT 20040114001962004011400196NM 2004 1 14 MASA200300410 120031015A521080080103101 MECHANISM DHAV DHC8 DHC8202 2809007NM PAX DOOR LACK OF LUBE A MASAK NONE O OTHER UKUNKNOWN 1 SW07447YV 447 PHX-YUM CREW REPORTED PAX DOOR VERY DIFFICULT TO OPEN. MECHANIC INSPECTED, CLEANED AND LUBED PAX DOOR. OP CHECKS GOOD. 2H72 4T RTA13NM 20040114002082004011400208WP 2004 1 14 MWEA030431 120031023A552299184808 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE RT ELEVATOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 RIGHT ELEVATOR HAS DAMAGE AT INBOARD TRAILING EDGE 1INCH X .5000 HOLE IN TOP SKIN. EXTERNAL SKIN REPAIR. 2L72 4F4 F A6WE E2EA 20040114002212004011400221NM 2004 1 14 MWEA030487 120031215A1430995301630 FASTENER DOUG MD88 MD88 3023688NM FUSELAGE MISSING A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 STATION 1437 BETWEEN LONGERON 1 AND 3 RT HAS A MISSING FASTENER. REPAIRED AREA. 2L72 4F RTA6WE 20040114002222004011400222EA 2004 1 14 03364671 120031230A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27671BR 7572 DURING INSPECTION THE EMERGENCY LIGHTS IN THE BACK ROW WERE FOUND INOPERATIVE. THE POWER SUPPLY WAS FOUND DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040114002262004011400226EA 2004 1 14 03337636 120031203A33502013A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27636BR 7307 DURING INSPECTION THE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE PROBLEM WAS FOUND TO BE THE BATTERIES WERE DISCHARGED AND THEY WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHT WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040114002312004011400231NM 2004 1 14 03358429 120031224A3250 CONNECTOR DORNERDO32 DO328300 NM NLG STEERING LOOSE A VTZAA UNSCHED LANDING O OTHER TOTAKEOFF 1 EA27429FJ 3194 DURING TAKEOFF, THE CREW REPORTED AN AMBER NWS MESSAGE. THE FAULT WAS CAUSED BY A LOOSE CONNECTOR LEADING TO THE STEERING MANIFOLD. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040114002332004011400233NM 2004 1 14 03362410 120031228A32502304700000 POTENTIOMETER DORNERDO32 DO328300 NM NLG STEERING FAULTY A VTZAK NONE O OTHER LDLANDING 1 EA27410FJ 6239 DURING FLIGHT 6239 THE CREW REPORTED ON LANDING THAT THE NOSE WHEEL WAS TURNED TO THE LEFT. THE FLIGHT LANDED SAFELY AND PASSENGERS DEPLANED NORMALLY. THE NWS POTENTIOMETERS WERE REPLACED AND A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED. THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE ON 12/30/93 2H72 4T RTA55NM 20040115000022004011500002NM 2004 1 15 03FDEA02017 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 2 O/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000082004011500008NM 2004 1 15 03FDEA02023 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, O/B HINGE ACTUATOR HOLE NR 2 O/B WITH WORN CHROME PLATING AT HOLE. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000482004011500048WP 2004 1 15 UPS03841628 120031113A575356423422 FITTING DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE:C3 FLAP SUPPORT ASSY 5642342-2 CRACKED RT WING STA XW3.125 LOC AND DRILL NEW FITTING, ALODINED, PRIMED, AND INSTALLED 2 EA BUSHINGS, 1 EA BEARING, FITTING, AND ALL PARTS REMOVED FOR ACCESS; ALL IAW DC8 51-1-24, 51-1-8, 51-1-20, 51-1-21, 51-3-1, AND DAC DWG(S) 5642342. VERIFIED ALIGN OF TORQUE TUBE ARM; TORQUED DRIVE LINK TO FLAP FITTING; TENSIONED CABLES; ALL IAW DC8 MM 27-51-06, 27-50-00, AND DAC DWG 5642900. 2L74 4F RT4A25 20040115000512004011500051NM 2004 1 15 DL75K031077 120031212A56101401N48901 WINDSHIELD BOEING757 757232 1384965NM COCKPIT CRACKED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO276706Q 30422 AT FL 390 LEFT SIDE WINDOW HEAT INOP LIGHT ILLUMINATED. WHILE PERFORMING EMERGENCY PROCEDURE, WINDOW MADE A LOUD POP AND CRACKED. DIVERTED TO DFW. REPLACED WINDOW. 2L72 4F RTA2NM 20040115000822004011500082NM 2004 1 15 03FDEA02072 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM FUSELAGE MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LOWER SECTION OF NR 1 BANJO FITTING (AJC7051-505) AFT FACE LONGITUDINAL ATTACHED STIFFENER FOUND WITH 01 EA FASTENER MISSING. GAIN ACCESS FROM PNL 364AR. RT LOWER SECTION OF NR 1 BANJO FITTING AJC7051-505 AFT FACE LONGITUDINAL STIFFENER MISSING HEAD FASTENER REPLACED AS PER SRM 51-33-01 VOL2. 2L73 4F RTA22WE 20040115000982004011500098NM 2004 1 15 03FDEA02074 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LOWER SECTION OF NR 3 BANJO FITTING (AJC7053-503) FWD FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT LOWER SECTION OF NR 3 BANJO FITTING AJC7053-503 FWD FACE FLANGE 5 CRACKED LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II. 2L73 4F RTA22WE 20040115001062004011500106NM 2004 1 15 03FDEA02082 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 01 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY. 2L73 4F RTA22WE 20040115001162004011500116NM 2004 1 15 03FDEA02089 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 3 LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 3 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20040115001192004011500119NM 2004 1 15 03FDEA02096 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 361EL. LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20040115001202004011500120NM 2004 1 15 03FDEA02097 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 9 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363CL. LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 9 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20031212000312003121200031NM 2003 12 12 SWAA032427 120031103A3350BR2013 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED PM CHECK, FOUND EEPLS INOP AT ROW 3 AND ROW 8. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20031212000332003121200033EU 2003 12 12 037023 120031112A7720 CONNECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE DISCONNECTED A UHLABEA EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17157SD 157 146 MX CHECK FLIGHT 9404 A/C PERFORMING MX CHECK FLIGHT DUE TO LEVEL C MX INSPECTION LAN-LAN. RIGHT AFTER TAKEOFF LT ENGINE OIL TEMP, ITT, AND NG ALL PEGGED OUT THE ENGINE OVERTEMP LIGHT ILLUMINATED. CREW SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY. A/C TAKEN OUT OF SERVICE 11-12-03 AT 1839. AFTER LANDING THE ENGINE INDICATION CANNON PLUG P4 WAS FOUND TO BE DISCONNECTED. CONNECTOR WAS RECONNECTED OPERATIONAL CHECK WAS SATISFACTORY. A/C RETURNED TO SERVICE 11-12-03 AT 2200. 2L72 4T4 TRTA52EU E8NE6 20031212000822003121200082NM 2003 12 12 SWAA032430 120031103A53126516300 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 187, RBL 1. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031212000912003121200091NM 2003 12 12 SWAA032408 120031031A3230M988 CIRCUIT CARD BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SW29349SW 24408 AIR TURNBACK, LT MLG UNSAFE LIGHT WOULD NOT EXTINGUISH, CYCLED THE LANDING GEAR AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED M988 LOGIC CARD AND LEFT MLG UPLOCK SWITCH PER MM. 2L72 4F RTA16WE 20031212001162003121200116NM 2003 12 12 SWAA032451 120031106A2121215201 FAN BOEING737 7373A4 1384585NM E/E BAY DAMAGED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW29675AA 23253 ACRID SMELL IN COCKPIT. REMOVED AND REPLACED REC FAN PER MM AND OPS CK GOOD PER MM. 2L72 4F RTA16WE 20031212001232003121200123EU 2003 12 12 AWXA200301429 120031116A3350321452 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW423995724 091 DFW - EEL - DURING 4-DAY CHECK THE FORWARD AND AFT EMERGENCY POWER SUPPLY UNITS WERE FOUND INOPERATIVE DURING EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED THE FORWARD (10WL) AND AFT (13WL) EMERGENCY POWER SUPPLY UNITS, OPERATIONAL CHECK WAS GOOD. PART NAME; EPSU, MFG; DIEHL GMBH, P/N; 3214-54, S/N; 2338, TT; 30713, TC; 13010, TSR; 357. 2L72 4F RTA28NM 20031212001362003121200136WP 2003 12 12 AALA20030936 120030902A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21492AA 49730 DFW - DURING OVERNIGHT MAINTENANCE, UPPER EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT ROW 20. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215000032003121500003NM 2003 12 15 AWXA200301439 120031107A532069353521 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND IN TIE CLIP AT BS 380, STR 26 LT. MAINTENANCE REMOVED CRACKED TIE CLIP AT BS 380, STR 26 LT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW SRM 51-40-02 PG 1, 11, 38 & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031215000172003121500017NM 2003 12 15 QXEA200301432 120031114A3233465507 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM NR 2 MLG MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09400QX6 6 4030 SEA- ON FLIGHT 2281 AFTER TAKEOFF FROM GEG RIGHT DOOR ADVISORY LIGHT REMAINED ON AFTER GEAR RETRACTION. AIRSPEED WAS HELD AT 185 OR BELOW AND LEVELED OFF AT 15,000 FEET TO RUN THE CHECKLIST. AS SOON AS LEVELED AT 15,000 FEET THE DOOR RETRACTED ON IT'S OWN AND FLIGHT WAS CONTINUED ON TO SEA. REMOVED AND REPLACED NR 2 MLG RETRACTION ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000302003121500030 2003 12 15 SWAA032507 420031113A256563550101 SLIDE BOEING737 7377H4 1384404NM L1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29794SW 30605 L1 DOOR EVACUATION SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031215000312003121500031NM 2003 12 15 SWAA032508 120031113A53306545819 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND 2 LONG CRACK AT NLG W/W SIDE PANEL FWD AND BELOW RT ACCESS PANEL CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031215001772003121500177EU 2003 12 15 ASOA03529 120031021A33507012210 LIGHT AEROSPATR72 ATR72 EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11630AS 336 FLT 4183 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031215001782003121500178EA 2003 12 15 ASOA03538 120031025A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11827AS 7212 FLT 4823 - DURING A GROUND INSPECTION IN SHV, THE RIGHT WING AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031215001862003121500186NM 2003 12 15 AALA20031178 120031021A3350 CONNECTOR BOEING767 767223 1385123NM CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21328AA 22328 AAX - MAINTENANCE OBSERVED EMERGENCY LIGHT AT SEAT 25H INOPERATIVE. REPLACED CONNECTOR PLUG AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031216000042003121600004NM 2003 12 16 AWXA200301475 120031104A57126573769 RIB BOEING737 737277 1384570NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 LCQ - MINOR REPAIR - DURING C-14 CHECK 1.1875 INCH CRACK WAS FOUND IN LT WING LEADING EDGE RIB, INBOARD OF NR 1 ENGINE AT L/E STA 222.7. MAINTENANCE REMOVED CRACKED LT WING LEADING EDGE RIB AT L/E STA 222.7; FABRICATED A NEW REPLACEMENT RIB PER DWG 65-49353; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PARA 9B. 2L72 4F RTA16WE 20031216000082003121600008NM 2003 12 16 QXEA200301440 120031116A2420 PIN BOMBDRDHC8 DHC8401 1390041NM ELECTRICAL SYS WORN A QXEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 NM09546DS 4017 PDX- ON FLIGHT 9852 IN CRUISE NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. RESET NR 2 AC GENERATOR PER CHECKLIST. NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED AGAIN THEN FLICKERED RANDOMLY. SHUT DOWN NR 2 AC GENERATOR AS BY CHECKLIST AND LEFT IT SHUT DOWN FOR REMAINDER OF FLIGHT. NOTICED PIN E INSIDE ELECTRICAL CONNECTOR 3421-P16-2 IS WORN. REPLACED PIN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031216000152003121600015NM 2003 12 16 QXEA200301454 120031104A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- FIVE INVERTED DENTS FROM STATIONS X409.75 TO X417.75 BETWEEN STRINGERS 29 AND 31. REPAIRED IAW DHC-8 SRM 51-00-06, 51-00-05 RD 8-53-7629 AND HORIZON AIR EA 2-53-502. 2H72 4T RTA13NM 20031216000172003121600017NM 2003 12 16 QXEA200301459 120031104A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 NR 10 SEAT TRACK REQUIRES REPLACMENT DUE TO DAMAGE THAT IS OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-51-102. 2H72 4T RTA13NM 20031216000372003121600037NM 2003 12 16 SWAA032553 120031119A53106545785 WINDOW FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND NR 1 AND NR 2 LT SIDE PAX WINDOW FRAMES CRACKED AT FASTENER HOLE. REMOVED AND REPLACED WINDOW FRAMES PER SRM. 2L72 4F RTA16WE 20031216000462003121600046 2003 12 16 SWAA032532 420031117A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031216000492003121600049NE 2003 12 16 SWAA032535 220031117A7250JT8D9AHK TURBINE BLADES BOEING737 7372H4 138448CNM PWA JT8 JT8D9 52048NE NR 1 ENGINE DAMAGED A SWAAA UNSCHED LANDING RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CLCLIMB 1 SW29095SW 23054 707395 AIR TURNBACK, DURING TAKEOFF, NR 1 ENGINE LOST POWER AND HIGH VIBRATION FELT. FOUND LPT BLADES DAMAGED. REMOVED AND REPLACED NR 1 ENG PER MT. 2L72 4F4 F A16WE E2EA 20031216000602003121600060NM 2003 12 16 SWAA032546 120031118A53306545768 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C2 CHECK, FOUND 1.25 LONG FUSELAGE SKIN CRACK AT BS 475, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031216000702003121600070NM 2003 12 16 SWAA032566 120031120A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FLOORBEAM CRACKED AT BS 747, RBL 14. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031216000962003121600096SO 2003 12 16 C2XA03SH488 120031211A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 SHV- DURING C-CHECK STRINGER 19 RIGHT AT FRAME 53 WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031217000102003121700010WP 2003 12 17 CALA0300653 120031120A5711 SPAR DOUG DC9 DC982 3022082WP RT WING CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND RT WING FORWARD SPAR CORRODED AT STA XRS 258-335. REPAIRED IAW ECRA 5731-01040. 2L72 4F A6WE 20031217000202003121700020EA 2003 12 17 COMA0360505 120031118A5240 SERVICE DOOR CNDAIRCL600 CL6002B19 1900309EA FUSELAGE OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01986CA 7174 AIR SPEED AND MACH TRIM CAUTION, STALL FAIL CAUTION. THE 02 SERVICE DOOR FOUND OPEN. CLOSED SERVICE DOOR. 2L72 4F RTA21EA 20031217000212003121700021WP 2003 12 17 IXXA0300078O 120031121A311037534391D PANEL DOUG DC8 DC873F 302199FWP COCKPIT FAILED A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW11605AL* 1880 46106 DURING FLIGHT, BACK GROUND LIGHT FOR STAB TRIM STARTED SMOKING. THEN LIGHTS OFF, REPOSITIONED BACK GROUND PANEL STOPPED SMOKING BUT HALF THE LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED STAB TRIM LIGHT PANEL PER ALL APPLICABLE MANUALS AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20031217000262003121700026NM 2003 12 17 AWXA200301477 120031103A532069434961 SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK CORROSION WAS FOUND AT FASTENER HOLES ON AFT CARGO COMPARTMENT SUPPORT ZEE FROM BS 847 TO BS 867, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT SUPPORT ZEE FROM BS 847 TO BS 867, RBL 20; FABRICATED A NEW REPLACEMENT SUPPORT ZEE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 38, 41 & 45 FIG 8, 9 & 12. 2L72 4F RTA16WE 20031215000892003121500089NM 2003 12 15 03FDEA01958 120031120A2612 DETECTION SYS BOEING727 727200 138407ENM NR 1 ENGINE FAULTY A FDEAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25223FE 20935 ENGINE FIRE WARNING NR 1 ENGINE DURING CLIMBOUT. LIGHT & HORN INTERMITTENT AT FIRST, THEN BOTH CAME ON STEADY. AFTER EXECUTING QRH PROCEDURES AND DISCHARGING BOTH BOTTLES, FIRE WARNING AND HORN STAYED ON UNTIL SHORT FINAL, THEN WENT OUT FOR GOOD. INSPECTED INTAKE AND EXHAUST, NO DAMAGE FOUND. OPENED COWLING INSPECTED UPPER AND LOWER SECTIONS OF ENGINE, NO EVIDENCE OF FIRE NOTED. REMOVED & REPLACED 2 EA ENGINE FIRE BOTTLES. REMOVED & REPLACED ENGINE NR 1 FIRE DETECTION ELEMENT. ALSO REMOVED & REPLACED THE FIRE DETECTION BOX. REMOVED & REPLACED ENGINE FIRE BOTTLE DETECTION DISC. RAN ENGINES, PERFORMED HIGH POWER RUN NR 1 ENGINE ALL PARAMETERS GOOD. 2L73 4F RTA3WE 20031215001472003121500147WP 2003 12 15 AALA20031225 120031105A3350 CONNECTOR DOUG DC9 DC982 3022082WP TAILCONE LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21285AA 49297 DFW - DURING OVERNIGHT MAINTENANCE, FOUND TAIL CONE AREA EMERGENCY LIGHTS INOPERATIVE. REPAIRED LOOSE BATTERY CONNECTION FOR TAILCONE AREA EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001582003121500158WP 2003 12 15 AALA20031201 120031102A3350P4010049 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21964TW 53614 DFW - DURING OVERNIGHT MAINTENANCE FOUND ALL SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED 4 STRIP LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031215001652003121500165WP 2003 12 15 AALA20031135 120031011A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21586AA 53249 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHT INOPERATIVE IN THE TAILCONE WALKWAY. REPAIRED ELECTRICAL WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031216000012003121600001NM 2003 12 16 AWXA200301471 120031009A532065C327076 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 CRACK WAS FOUND ON AFT CABIN FLOOR SHEAR WEB AT BS 1029, BL 0. MAINTENANCE REMOVED AFT CABIN FLOOR SHEAR WEB AT BS 1029, BL 0; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32707; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20031216000632003121600063NM 2003 12 16 SWAA032549 120031118A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED PM CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT STRINGER 23L, BS 747, AND BS 727E. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031216000802003121600080NM 2003 12 16 SWAA032576 120031121A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM CORRODED AT BS 877. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031216000992003121600099SO 2003 12 16 C2XA03SH470 120031123A532014522460009 BUTTSTRAP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712528 145504 SHV- DURING C-CHECK THE INBOARD BUTTSTRAP BETWEEN FRAMES 14 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031216001002003121600100SO 2003 12 16 C2XA03SH472 120031123A532014522460013 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031217000272003121700027SO 2003 12 17 C2XA03IA105 120031120A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714953 145071 DURING SCHEDULED MAINTENANCE THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE-SECURED THE LAMP IN THE LIGHT FIXTURE. THE LIGHT OPERATIONALLY CHECKED GOOD. 2L72 4T RTT00011AT 20031217000542003121700054WP 2003 12 17 DHL2003805548 120030723A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OUTBD L/E FORMER 0.500 CRACKED, STA XFS 753.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER AND NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO NR 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031217000592003121700059WP 2003 12 17 DHL2003805580 120030828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT INNER WING CTR EXTENDED L/E SLOT OUTER PLATING SHOWS ELONGATED HOLES AROUND STA XW.257.000 (MAJOR REPAIR). PERFORMED MAJOR REAPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075-T6 AL0.071) AND TWO FILLERS (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE EXTERNAL REPAIR DOUBLER AND FILLERS ON RIGHT INNER WING CTR EXTENDED L/E SLOT OUTER PLATING (AROUND STA XW 257.000) USING NEW FASTENERS. SEE N/R 0211 FOR CTR L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031217000702003121700070WP 2003 12 17 DHL2003802504 120031110A5711 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING L/E FORMER CRACKED 0.500 AT STA 797.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031217000752003121700075WP 2003 12 17 DHL2003802522 120031117A57205769857U614 FITTING DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RT WING L/E FITTING (ZEE PAN) CRACKED 2.000, STA XW 454.000. REMOVED AND REPLACED FITTING (ZEE PAN) ON RIGHT WING L/E, STA XW 454.000 IAW SRM 51-1-20D PG 9, 21. 2L74 4F RT4A25 20031217000902003121700090EA 2003 12 17 COMA0360511 120031120A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01443CA 7539 FLIGHT 5332 FLAPS FAILED WARNING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031217000942003121700094EA 2003 12 17 QXEA200301469 120031121A2612 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 ACTIVATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09615QX 10065 ON FLIGHT 2452 FIRE SYSTEM FAULT. THIS SDR IS WAITING FOR FURTHER INFORMATION. 2L72 4F RTA21EA 20031217000972003121700097NM 2003 12 17 CALA0300674 120031121A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND STRINGERS 26R AND 27R IN FORWARD CARGO AREA CORRODED AT STA 535-539. A STRINGER SECTION REPAIR WAS INSTALLED IAW SRM 53-00-03. 2L72 4F RTA16WE 20031217000992003121700099NM 2003 12 17 737DX0002 120031110A5320 STRINGER CLIP BOEING737 737400 138449ANM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05737DX 24804 STRINGER TO FRAME TIE DAMAGED, FORWARD SIDE OF BS 400 FRAME AT STR 28 LT. REPLACED STRINGER TO FRAME TIE PER SRM 51-40-02. 2L72 4F RTA16WE 20031217001142003121700114NM 2003 12 17 2003UALA00852 120031112A3350 LAMP BOEING777 777222 1385219NM EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29782UA 26948 AFT EMERGENCY LIGHT INOPERATIVE AT SEAT 1E. RELAMPED EMERGENCY LIGHT. 2L72 4F RTT0001SE 20031217001192003121700119EU 2003 12 17 YENA200341 120031216A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAO OTHER O OTHER CRCRUISE 1 EA15506JB13798 1235 INFLIGHT THE EMERGENCY LIGHTS OVER L1 AND R1 REMAINED ON. ALL OTHERS OFF PER FLIGHT DECK SWITCH POSITION. CONFIRMED FWD LEFT EPSU FAILED ON CIDS EMERGENDY LIGHT SYSTEM TEST. REMOVED AND REPLACED EPSU BASE ASSY. REINSTALLED OLD BATTERY ON NEW UNIT. ACCOMPLISHED IAW AMM 33-51-38 CIDS TEST PASSED. OK FOR SERVICE. 2L72 4F RTA28NM 20031217001202003121700120WP 2003 12 17 AALA20031003 120030912A2612 FIRE LOOP DOUG DC9 DC982 3022082WP APU FAILED A AALAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW21495AA 49733 APU FIRE LOOP A ILLUMINATED DURNIG NR 2 ENGINE START. FOLLOWED FIRE DETECTION LOOP LIGHT PROCEDURE, NO TEST FOR LOOP B. MOVED SWITCH TO LOOP A AND OBSERVED APU FIRE LIGHT. FOLLOWED PROCEDURE FOR APU FIRE. LIGHT STAYED ON FOR 30 SECONDS AFTER FIRST BOTTLE, PULLED SECOND BOTTLE SWITCH AND NO HELP. NO EXTERNAL INDICATION FROM RAMP CREW OF FIRE. MAINTENANCE REPLACED RIGHT APU FIRE LOOP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031217001232003121700123NE 2003 12 17 AALA20031156 220031019A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RIGHT SHUTDOWN A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW21461AA 49566 CLIMBING OUT RT ENGINE SHUTDOWN. DECLARED EMERGENCY LANDED WITHOUT FURTHER INCIDENT. NOT OVER WEIGHT. REMOVED AND REPLACED RIGHT ENGINE. PERFORMED LEAK AND RUN UP, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20031217001262003121700126 2003 12 17 03339329 420031205A34257011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27329UE 41097 DURING AIRCRAFT OPERATION THE FIRST OFFICERS FLIGHT DISPLAY WENT BLANK. THE NR 2 SYMBOL GENERATOR WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031217001512003121700151NM 2003 12 17 CALA0300710 120031112A5312 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 AN IMPROPER REPAIR WAS DISCOVERED ON THE AFT PRESSURE BULKHEAD DOME WEB JUST AFT OF THE Y-CHORD BETWEEN S9R AND S11R DURING A 4C CHECK AT HOBBY. THE AREA WAS REPAIRED IAW ECRA 5311-01174. 2L72 4F RTA16WE 20031217001642003121700164WP 2003 12 17 DHL2003801091 120031212A5210 DOOR DOUG DC8 DC873F 302199FWP PAX OUT OF ADJUST A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 MAIN ENTRY DOOR UPPER AFT CORNER OF DOOR HANGS UP ON DOOR FRAME SKIN IS PULLED OUT 2.5 INCH LONG X .50 HIGH. RE-ALIGNED DOOR SKIN CORNER TO CLEAR FRAME. OPS CHECKED DOOR PER M/M 52-11-1, OK. 2L74 4F RT4A25 20031217001702003121700170NM 2003 12 17 SWAA032644 120031202A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, 3 EACH STRINGER CLIPS CRACKED AT BS 747, STR 11R, BS 767, STR 13R, BS 767, STR 11R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20031217001762003121700176NM 2003 12 17 F3LA200300170 120031211A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 952, LBL 25. REPLACED INTERCOSTAL FROM STA 947 - 967, LBL 24.5, WL 208, PER SRM 51-40-2, 53-60-5 FIG 101 AND 51-4-5. 2L72 4F RTA16WE 20031217001802003121700180 2003 12 17 ABXA030450 420031124A34456228973001 ANTENNA BOEING767 767281 1385109NM TCAS MISSING A ABXAK NONE L NO TEST NRNOT REPORTED 1 GL23783AX2739 23016 TCAS TEST SHOWED UPPER ANTENNA FAIL. DISCOVERED UPPER ANTENNA MISSING. MAINTENANCE INSTALLED TCAS ANTENNA IAW REA B634-47860. 2L72 4F RTA1NM 20031217001842003121700184SO 2003 12 17 SWIA200312603 120031102A2730C818061 COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07581SW 120349 STALL SYSTEM 2 INOPERTIVE. REMOVED AND REPLACED STALL WARNING COMPUTER IAW 27-00-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20031217001872003121700187SO 2003 12 17 SWIA200312606 120031113A3350 CONTACTOR EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT FAILED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07584SW 120352 EMERGENCY LIGHT CIRCUIT BREAKER POPPED. REPLACED EMERGENCY BUS CONTACTOR K0028. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031217001982003121700198NM 2003 12 17 AWXA200301491 120031106A532065C327075 WEB BOEING737 7373G7 1384595NM LAV FLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF LT AFT LAVATORY SUB FLOOR SHEAR WEB BETWEEN BS 1016 AND BS 1029, LBL 5-15, WL 208. MAINTENANCE REMOVED CORRODED SUB FLOOR SHEAR WEB BETWEEN BS 1016 AND BS 1029, LBL 5-24; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32707; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1. 2L72 4F RTA16WE 20031217002002003121700200NM 2003 12 17 AWXA200301494 120031106A532065C3267714 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF RT AFT LAVATORY SUB FLOOR STRAP BETWEEN BS 1006 AND BS 1016, RBL 5, WL 208. MAINTENANCE REMOVED CORRODED SUB FLOOR STRAP BETWEEN BS 1006 AND BS 1016, RBL 5; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32707; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51 FIG 101. 2L72 4F RTA16WE 20031217002022003121700202NM 2003 12 17 AWXA200301496 120031113A574365494427 FITTING BOEING737 7373G7 1384595NM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR WING DOOR ATTACH ANGLE FWD SUPPORT FITTING AT INBOARD AND OUTBOARD FACES AT REAR SPAR. MAINTENANCE REMOVED CORRODED LT MAIN LANDING GEAR WING DOOR ATTACH ANGLE FWD SUPPORT FITTING AT REAR SPAR; INSTALLED A NEW REPLACEMENT SUPPORT FITTING IAW B737-300 SRM 51-40-05 FIG 401 PG 1-8 & FIG 2 PG 4. 2L72 4F RTA16WE 20031217002042003121700204NM 2003 12 17 AWXA200301498 120031113A5280655223535 STRUCTURE BOEING737 7373G7 1384595NM MLG DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR WING DOOR ATTACH STABILIZING ASSEMBLY WBL 114. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR WING DOOR ATTACH STABILIZING ASSEMBLY IAW AMM 57-15-00. 2L72 4F RTA16WE 20031217002062003121700206SO 2003 12 17 SWIA200312613 120031119A27503082001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM0757734 120199 CAPTAIN REPORTS CONTROL FAULT INDICATION ON FLAP WARNING PANEL. REPLACED LT NACELLE FLAP ACTUATOR PER AMM 27-50-08. OPS AND LEAK CHECKS GOOD. 2L72 4T RTA31SO 20031217001152003121700115NM 2003 12 17 2003UALA00853 120031113A5753 HINGE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE TE FLAPS CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29673UA 29241 RT WING INBD FLAP CENTER HINGE EXTERNAL IS CRACKED ON BOTH SIDES, (FLANGE REAR SPAR MID FLAP). MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE FITTING PER SRM 57-53-02, FIG 201. INSTALLED FITTING PER MM 27-51-06. 2L72 4F4 FRTA1NM E24NE 20031217001412003121700141NM 2003 12 17 SWAA032653 120031203A53206545409 WEB BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED STA 663, LBL 32. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031217001432003121700143NM 2003 12 17 03FDEA02176 120031128A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 CENTER CARGO LT TUNNEL BETWEEN STA 1821 TO STA 1841 APPROX LONGERON 37 INTERCOSTAL FOUND CRACKED. AIR CONDITIONING - HEATING - WELD REPAIR BAFFLE / AFT CARGO COMPARTMENT HAS BEEN COMPLIED WITH. 2L73 4F RTA22WE 20031217001882003121700188SO 2003 12 17 SWIA200312607 120031027A28971C717 WIRE EMB 120 EMB120ER 3260203SO FUEL BOOST PUMP CHAFED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07393SW8506 8506 120330 LEFT FORWARD FUEL BOOST PUMP HAS CHAFED WIRE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD FUEL BOOST PUMP IAW MM 28-21-02. 2L72 4T RTA31SO 20031217002082003121700208EA 2003 12 17 SWIA200312615 120031120A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07464SW 7827 AFTER TAKEOFF RECEIVED A I/B GRD SPLR FAULT AND SPOILERONS FAULT STATUS MESSAGE. REMOVED AND REPLACED SECU NR 2 IAW RJ MM 27-61-04. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20031217002122003121700212EA 2003 12 17 SWIA200312619 120031124A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. 2L72 4F RTA21EA 20031218000042003121800004NM 2003 12 18 P5CA0300994 120031121A2797 CONNECTOR BOEING747 747249F 1384849NM COCKPIT LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 BOTH GREEN BAND & STAB TRIM GREEN BAND LIGHT CAME ON DURING TAXI BEFORE T/O. FOUND R586 LOOSE RESET R586, OPS CKS GOOD PER 27-48-00. 2L74 4F A20WE 20031218000122003121800012NM 2003 12 18 MWEA030455 120031125A5345993653433 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 J-CHANNEL AT STATION 200 FROM RIGHT SIDE OF CENTERLINE OUTBOARD HAS SERVERAL FASTENER HOLE LOBES CORRODED ON UPPER AND LOWER SIDE OF LOBES. FABRICATED AND INSTALLED NEW J-CHANNEL. 2L72 4F RTA6WE 20031218000192003121800019EU 2003 12 18 MALA030505 120031124A7700 WARNING SYSTEM SAAB SF340 SF340A 7850100EU RT ENGINE FALSE INDICATIONA MALAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 GL1598XJ 340A098 AFTER START ON FLIGHT 3093, CREW REPORTED FIRE IN RT ENGINE. CREW TURNED ON THE HIGH PRESSURE BLEED THE ENGINE TEMP WAS 800, HP FELL OFF LINE, AND NG STARTED TO DROP TO 30 PERCENT, TEMP WENT TO 840 PROP STAYED AT 1040. CREW RECEIVED THE FIRE SIGNAL AND DID FIRE SHUTDOWN AND BLEW THE FIRE BOTTLE. MAINTENANCE REMOVED AND REPLACED FIRE BOTTLE, COMPLETED GROUND RUN OFF ENGINE HIGH PRESSURE BLEED WORKED NORMALLY. NO DISCREPANCIES NOTED. 2L72 4T RTA52EU 20031218000492003121800049EA 2003 12 18 03327702 120031123A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27702BR 7462 DURING INSPECTION THE OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031218000842003121800084NM 2003 12 18 2003UALA00867 120031117A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 3F INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29229UA 30557 EMERGENCY LIGHT INOP AT SEAT 3F AFT MOST. REPLACED EMERGENCY LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20031218000922003121800092NM 2003 12 18 2003UALA00880 120031119A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29589UA 28707 FRAME RETURN FLANGE HAD DENT DAMAGE 2 PLACES BS 1400 AND BS 1420, BETWEEN STRINGERS 25L-27L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031218000952003121800095NM 2003 12 18 2003UALA00884 120031120A5320 PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO BAY DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29303UA 23644 AFT CARGO PIT MOLDED PANEL ON FWD WALL COVERING APU SUPPLY DUCT HAS EVIDENCE OF HEAT DAMAGE. APU SUPPLY DUCT HEAT SHROUD DAMAGE WAS CAUSED BY CONTACT WITH THE APU SUPPLY DUCT AND INFERIOR DESIGN OF HEAT SHROUD. THE HEAT SHROUD WAS REPLACED AND CONTACT WITH THE APU SUPPLY DUCT WAS ELIMINATED. A MODIFIED HEAT SHROUD IS AVAILABLE AND WILL BE INSTALLED ON THIS AIRCRAFT IN THE FUTURE. 2L72 4F4 FRTA16WE E2GL 20031218001042003121800104NM 2003 12 18 2003UALA00892 120031122A7930 WARNING SYSTEM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENG OIL MALFUNCTIONED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 WP29388UA 24663 DIVERTED TO LAX DUE TO NR 1 ENGINE HIGH OIL TEMPERATURE. SHUTDOWN ENGINE AND LANDED UNDER AMBER ALERT. R & R OIL TEMP BULB AND EIS. SHOP TESTS SHOWED BOTH COMPONENTS WERE WELL WITHIN SHOP TEST SPECIFICATIONS. ALSO, ACCOMPLISHED WIRE CHECK ON THE OIL TEMP BULB CIRCUIT WITH NO FAULTS FOUND. NO ABSOLUTE CAUSE FOUND. POSSIBLE DIRTY CONNECTOR ON THE TEMP BULB CIRCUIT WAS THE CAUSE OF THE PROBLEM. PRIOR TO THE IFSD EVENT ECM SHOWED AND INCREASE OF 10-20 DEGREES IN ECM TREND IN PREVIOUS DAYS FLIGHT (STILL WAY BELOW FLAG LIMITS) . AFTER COMPONENTS WERE REPLACE OIL TEMP NORMALIZED BACK TO WERE IT WAS. 2L72 4F4 FRTA16WE E2GL 20031218001202003121800120SO 2003 12 18 C2XA03BT114 120031128A3260852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO LANDING GEAR FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW27139908267 8267 145277 CREW REPORTED, AFTER GEAR RETRACTION, LANDING GEAR INDICATED UP. OBVIOUS WIND NOISE SUSPECTED GEAR DOORS DID NOT RETRACT. AIRCRAFT REPORTEDLY HAD EXCESSIVE DRAG IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SENSOR IAW EMB145 MM 32-63-03, OPS CHECKED GOOD IAW EMB145 MM 32-30-00. 2L72 4T RTT00011AT 20031218001372003121800137WP 2003 12 18 UPS03841587 120031119A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 965 AT LBL 64. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-7-1 FIG 10 AND SRM 51-1-21. 2L74 4F RT4A25 20031218001382003121800138NM 2003 12 18 QXEA200301492 120031125A5310 SILL DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 CORROSION AROUND NUT PLATES ON BOTTOM OF MAIN CABIN DOOR SILL. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20031218001422003121800142WP 2003 12 18 CALA0300686 120031203A531353110113201 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 STRINGER CRACKED AT STATION 1429 AT STRINGER 2 RIGHT (1 INCH). INSTALLED NEW STRINGER SECTION AND SPLICE PER EC/RA 5311-01132. 2L72 4F A6WE 20031218001562003121800156NM 2003 12 18 QXEA200301511 120031203A6120311717503 MFC DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09364PH1266 524 NR 1 AC GENERATOR CAUTION LIGHT AND NR 1 ENGINE AUTOFEATHER ACTIVATED THROUGH 1000 FEET AFTER DEPARTING PDX. AIRCRAFT RETURNED TO FIELD. REMOVED AND REPLACED NR 1 MFC. AIRCRAFT RETURNED TO FIELD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031217001422003121700142WP 2003 12 17 03FDEA02175 120031208A3600 PRESSURE SWITCH DOUG DC10 DC1010 3022110WP PNEUMATIC SYS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25364FE 46600 RECEIVED NR 1 MANIFOLD FAIL ALERT AT FL350. COULD NOT MAINTAIN CABIN PRESSURE. RAN RED TABS AND DIVERTED TO DEN. FOUND LEFT WING PRESSURE SWITCH FAULT BALL NO LEAKS NOTED. PERFORMED DECAY CHECK PER MD-10 MM 36-00-01-5 DECAY CHECK WITHIN LIMITS. REMOVED AND REPLACED PNEUMATIC MANIFOLD FAULT INDICATOR IAW FIM 36-23. PER MOCC REQUEST, REMOVED AND REPLACED LOOP 1A D1-88 SENSING ELEMENT IAW MM 36-23-02-4. ACCOMPLISHED PNEUMATIC SYSTEM ADJUSTMENT AND TEST AS REQUIRED PER MM 36-00-03-5. OPS CHECKED NORMAL NO DEFECTS NOTED. NO MANIFOLD FAIL INDICATION. RAN ENGS NR 1, 2, 3 DURING CHECK PER MD-10 JRH. 2L73 4F A22WE 20031218000022003121800002NM 2003 12 18 03FDEA01982 120031125A3350MISC062 BATTERY BOEING727 727100 1384036NM EMERGENCY LIGHT DISCHARGED A FDEAK NONE L NO TEST ININSP/MAINT 1 SO25136FE 19855 FWD ENTRY AND COCKPIT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES FOR OVERHEAD LIGHT ASSY'S PER FEDEX MM 33-50-101-2. CHECKS GOOD PER FEDEX MM 33-50-101-2. 2L73 4F RTA3WE 20031218000132003121800013NM 2003 12 18 UPS03541574 120031123A3350 LIGHT BOEING757 75724APF 1384969NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 EMERGENCY EXIT WARNING LIGHT INOP. RELAMPED & OPS CHECKS GOOD. 2L72 4F RTA2NM 20031218000892003121800089NM 2003 12 18 2003UALA00877 120031116A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 DENT AFT AND LOWER OF DOOR 3R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031218000942003121800094NM 2003 12 18 2003UALA00882 120031121A5230 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29645UA 25280 BULK CARGO DOOR LOWER AFT SKIN IS DENTED AND GOUGED BS 1450. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20031218001122003121800112EU 2003 12 18 2003UALA00901 120031125A5522 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT ELEVATOR CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29404UA 450 RT ELEVATOR UPPER SKIN HAD 2 AREAS OF WATER INGRESS. MAJOR REPAIR ACCOMPLISHED. DAMAGE REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205 SHEET 3 & 4. 2L72 4F4 FRTA28NM E40NE 20031218001652003121800165NM 2003 12 18 MWEA030465 120031203A5530591218836 ANGLE DOUG MD88 MD88 3023688NM VERTICAL STAB CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 VERTICAL STABILIZER RT FORWARD INSIDE ATTACH ANGLE IS CRACKED. FABRICATED AND INSTALLED NEW ANGLE. 2L72 4F RTA6WE 20031219000362003121900036SO 2003 12 19 SWIA200312638 120031130A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07568SW 120343 EXIT SIGN ON FRONT OF SEAT 1B AND C DOES NOT ILLUMINATE WITH THE EMERGENCY LIGHTS. REPLACED FORWARD EXIT SIGN WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20031219000382003121900038EA 2003 12 19 SWIA200312640 120031125A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA MACH TRIM STICKING A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07913SW 7597 AFTER ROTATION, STAB TRIM CH 1 AND CH 2 AND MACH TRIM DISCONNECTED AND WOULDN'T RE-ENGAGE. PERFORMED QRH PROCEDURES AND RETURNED TO DENVER. FOUND CAPT'S DISCONNECT BUTTON WAS STICKY (ON YOKE). CLEANED AND CYCLED REPEATEDLY. SYSTEM FUNCTIONING NORMALLY NOW. 2L72 4F RTA21EA 20031219000432003121900043SO 2003 12 19 C2XA03SH487 120031207A532014522459003 SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 SHV- DURING C-CHECK THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031009000792003100900079SO 2003 10 9 SWIA200312401 120030809A5720 CLIP EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07298SW 120328 RIGHT OUTBOARD WING, STATION 15, LOWER WING CLIP (MIDDLE) CRACKED AT FWD END. (DISCOVERED DURING C-CHECK INSPECTION)REMOVED AND REPLACED RIGHT OUTBOARD WING, STATION 15, LOWER WING MIDDLE CLIP WITH A SERVICEABLE UNIT IAW EMB SRM 51-40-01 & 51-40-02. 2L72 4T RTA31SO 20031009000872003100900087EA 2003 10 9 SWIA200312409 120030911A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07925SW2393 2393 7682 ON FINAL TO DEN, SPOILERONS FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES CAME ON. INSTALLED SERVICEABLE NR 2 SECU IAW CRJ MM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20031009000962003100900096EA 2003 10 9 COMA0360394 120030902A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA23585 7027 DURING COMPLIANCE OF TASK NR 002-53-160-610, 4 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL9.0 AND RBL9.0 THE CRACKS RANGE FROM 2.5 INCHES TO 3.25 INCHES IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IAW MFG REO NR 601R-53-41-102, REV B., DATED 6-8-2003, AND REO NR 601R-53-41-162, DATED 6-9-2003. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20031009001002003100900100CE 2003 10 9 00111 120030910A2131162972 CONTROLLER LEAR 25 25 5170506CE CABIN PRESSURE INOPERATIVE E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05525TW 011 PILOT REPORTED PRESSURIZATION PROBLEMS CABIN ALTITUDE INCREASING WITH ALTITUDE, RETURN TO DEPARTURE AIRPORT. WILL UPDATE REPORT AFTER MAINTENANCE. REMOVED AND REPLACED CABIN ALT CONTROLLER. AIRCRAFT RETURN TO SERVICE. 2L72 4J A10CE 20031009001082003100900108NM 2003 10 9 C1HA200395068 120030917A2750 JACKSCREW BOEING727 727290 138408WNM TE FLAPS LACK OF LUBE A C1HAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL15295AS 22147 DURING FLAP RETRACTION AFTER TAKEOFF OUTBOARD FLAPS RETRACTED TO 2 DEGREE POSITION WHILE INBOARDS REMAINED AT 5 DEGREE POSITION. RAN SPLIT FLAP EMERGENCY PROCEDURE INBOARDS REMAINED AT 5 WITH ALTERNATE FLAPS. RETURNED TO ELP, VERIFIED INBOARD FLAPS LOCKED OUT. INSPECTED FLAPS AND FLAP DRIVE MECHANISM & FOUND TO BE OK. RESEATED INBOARD FLAP INDICATOR ELEC CONNECTOR AND ALTERNATE FLAP DRIVE MOTOR CONNECTOR. FLAPS RETRACTED AND EXTENDED TO 30 DEGREES, LUBED FLAP AND JACKSCREWS AND TRACK CYCLED 15 MORES TIMES, OPS CHECKS GOOD IAW 727 MM 27-51-141 AND 27-52-00. 2L73 4F A3WE 20031010000012003101000001NM 2003 10 10 QXEA200301140 120030916A49304503139B FUEL CONTROL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 MALFUNCTIONED A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09408QX4395 4395 4050 APU IS LEAKING FUEL. REMOVED AND REPLACED FUEL CONTROL ASSEMBLY. 2H72 4T RTA13NM 20031010000282003101000028NM 2003 10 10 USAABB03167 120030916A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 6, 9, 13, 23, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031010000302003101000030NM 2003 10 10 USAABB03147 120030825A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 FOUND RIGHT FORWARD SECTION OF FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. (M) 2L72 4F RTA1NM 20031010000312003101000031NM 2003 10 10 USAABB03149 120030827A335020131A BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 FOUND L3 AND L4 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2L72 4F RTA2NM 20031010000322003101000032NM 2003 10 10 USAABB03150 120030830A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 FOUND L1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031010000432003101000043 2003 10 10 219PA0008 420030917A221010618162 LIMITER BOEING737 737222 1384473NM AUTOPILOT INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05219PA 19956 AUTOPILOT ROLL CHANNEL WILL NOT ENGAGE. REPLACED AILERON FORCE LIMITER IAW MM 22-12-10. OPS CHECKS OK. 2L72 4F A16WE 20031010000462003101000046NM 2003 10 10 03FDEA01577 120030918A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON FLOOR BEAM UPR SURFACE BS 328, LBL 29, WL 208. **SD** COMING 2L73 4F RTA3WE 20031010000512003101000051NM 2003 10 10 03FDEA01566 120030918A531165103326 FAILSAFE BOEING727 727200 138407ENM FRAME FAILED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 FRAME FAIL SAFE CRACKED AT BS 890 STR 14R ATTACH POINT. **SD** COMING. 2L73 4F RTA3WE 20031010000582003101000058NM 2003 10 10 03FDEA01556 120030917A361010614261 PRECOOLER BOEING727 727200 138407ENM ZONE 400 CRACKED A FDEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 SO25207FE 22929 ENG NR 1 STRUT OVERHEAT LIGHT CAME ON AFTER TAKEOFF FROM PHX. ENG ANTI ICE WAS NOT ON. WITH REDUCTION OF POWER TO QUIET EPR LIGHT WENT OUT. LIGHT WAS ON FOR A TOTAL OF 15 SECONDS. SYSTEM TESTED GOOD. CONSULTED QRH. NO FURTHER ACTION TAKEN. FOUND LEAK AT IB CLAMP ON PRECOOLER . FLANGE CRACK REMOVED PRECOOLER IAW MM 36-11-051-4, DUCTS IN AFT STAIR GOING TO PRECOOLER REMOVED . INSTALLED NEW PRECOOLER AND SECURED ALL DUCTING AND ALL ASSOCIATED HARDWARE. RAN ENGINE AT IDLE, IDLE LEAK CHECK IS GOOD IAW MM 36-11-051-4. 2L73 4F RTA3WE 20031010000592003101000059NM 2003 10 10 03FDEA01558 120030918A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 LOWER FWD CARGO BAY FRAME IS DENTED AT STA 600 BETWEEN STR 24 AND 25, WL 160 **SD** COMING 2L73 4F RTA3WE 20031007000402003100700040NM 2003 10 7 AALA20030737 120030710A2781 WARNING LIGHT BOEING737 737823 13844BZNM LE FLAPS FALSE ACTIVATIONA AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21924AN 29525 LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED FOLLOWING FLAP RETRACTION AFTER TAKEOFF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA WITHOUT FURTHER INCIDENT. PERFORMED FSWV BITE CHECK. THE SLAT RETRACT HYDRAULIC FUSE WAS RESET. SLAT RETRACT/EXTEND TIMES AND TEMPERATURES WERE CHECKED. LUBED LEADING EDGE SLAT TRACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20031007000432003100700043EU 2003 10 7 ASOA03399 120030826A7910 CAP AEROSPATR72 ATR72 EU LT ENGINE MISSING A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SO11640AS 405 DURING CRUISE FROM ATL-MYR, AT APPROX 19,000 FT CREW RECEIVED A LT ENGINE OIL PRESSURE WARNING ON GAUGE AND CREW ALERT PANEL. OIL PRESSURE DROPPED SLOWLY TO BOTTOM OF GAUGE AND AN ASSOCIATED CYCLIC REDUNDANCY CODE AND A RED ENGINE OIL PRESSURE WARNING MESSAGE. CREW COMPLIED WITH QRH PROCEDURES, SHUT DOWN LT ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED TO AGS, LANDING SAFELY. MAINTENANCE FOUND THE OIL CAP NOT INSTALLED ON LT ENGINE, CLEANED AND SERVICED IT WITH 9 QUARTS OF OIL. MAINTENANCE ALSO REMOVED AND REPLACED MAIN AND SCAVENGER OIL FILTERS AS A PRECAUTION. LT ENGINE CHIP DETECTORS WILL BE INSPECTED DAILY FOR 65 HOURS. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031007000672003100700067NM 2003 10 7 SWAA031981 120030831A53126545819 BULKHEAD BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 DURING SCHEDULED PM CHECK, FOUND SIDE BULKHEAD WEB CRACKED IN NLG W/W AT BS 259, WL 174 LT SIDE. REPAIRED SIDE WEB PER SWA EA. 2L72 4F A16WE 20031007001242003100700124WP 2003 10 7 MWEA030372 120030916A533059114065 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGEW DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 DENT LOCATED AT 1 INCH BELOW LONGERON 4 LEFT AND SEVERAL VERY SMALL DENTS LOCATED AROUND THIS DENT AT STATION 219. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20031008000262003100800026NM 2003 10 8 HOC2003F00023 120030826A5311 FRAME BOEING727 727224 1384076NM FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0779749 22451 DURING A C-CHECK CORROSION WAS NOTED ON CIRCUMFRENTIAL AND ATTACH FRAME STA 344 RT. 2L73 4F A3WE 20031008000332003100800033WP 2003 10 8 ARWA20030911 120030915A2920 DRAIN LINE LKHEED1011 1011385115 5265015WP ENGINE LEAKING A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19307GB 193U1131 SYSTEM B REVERSER QTY LOW AND DECREASING. SWITCHED POWERS OFF, STOPPED FLUID LOSS. REMOVED AND REPLACED 2R SYSTEM CASE DRAIN LINE. RAN ENGINE OPERATIONAL CHECK NORMAL, NO LEAKS NOTED. 2L73 4F A23WE 20031008000362003100800036NM 2003 10 8 VNAA0309001 120030901A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ROW 1 FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07437JS 3055 THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT ROW 1 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031008000372003100800037NM 2003 10 8 VNAA0309002 120030901A3260 BULB DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NLG INDICATOR FAILED A VNAAO OTHER P NO WARNING INDICATION LDLANDING 1 GL07431JS 3028 THE CREW ABORTED LANDING DUE TO A NOSE GEAR LIGHT NOT INDICATING DOWN AND LOCKED. FLIGHT 4143 DID A GO-AROUND AND ASKED THE TOWER TO LOOK AT THE NOSE GEAR TO ENSURE IT WAS DOWN. FLIGHT 4143 THEN LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE BULB FOR THE NOSE GEAR INDICATION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031008000482003100800048NM 2003 10 8 P5CA0300941 120030913A80127263746 START VALVE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23920FT 22237 702186 AFTER PUSH BACK NR 4 ENG FAILED TO START WITH IGNITION SWITCH IN NR 1 OR NR 2 POS. REMOVED AND REPLACED NR 4 ENG START VALVE PER MM 80-11-01. NO LEAKS NOTED, ENG START NORMAL. 2L74 4F4 F A20WE E3NE 20031008000662003100800066NM 2003 10 8 USAA030193 120030910A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU 23514 FOUND SKIN CRACKED .750 INCH, FUSELAGE JUST ABOVE S24R FORWARD OF FS 727E. INSTALLED DOUBLR/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M) 2L72 4F RTA16WE 20031009000072003100900007WP 2003 10 9 MEX2003440 120030921A291354143861 PUMP DOUG DC9 DC983 3022083WP HYD SYSTEM FAILED A ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23583MD 49659 DURING CRUISE AT 33,000 FT, THE RUDDER TRAVEL UNRESTRICTED LIGHT TURNS 'ON'. AFTER LANDING THE HYDRAULIC PRESSURE INDICATES 2500 PSI. THE ELECTRIC MOTOR DRIVEN PUMP WAS REPLACED IAW MM 29-10-06, THE PRESSURE TRANSMITTER WAS REPLACED IAW MM 29-30-02 AND THROW LIMITER RUDDER WAS REPLAFED IAW MM 27-20-06, LINES WAS VERIFIED IAW MM 27-20-00, ALL CORRECT. (M) 2L72 4F RTA6WE 20031009000212003100900021SO 2003 10 9 SIMA200320201 120030718A335078241 INVERTER EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21707EB 145195 BGR - FOUND EMERGENCY EXIT SIGN FOR LEFT OVERWING EXIT WOULD NOT ILLUMINATE. MAINTENANCE INSTALLED NEW INVERTER, OPS CHECK GOOD AND RETURNED A/C TO SERVICE. (M) 2L72 4F RTT00011AT 20031009000382003100900038SO 2003 10 9 SIMA200321604 120030731A3350 BATTERY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT DISCHARGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21847AE 145707 CREW REPORTED THE LAST THREE FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE CHARGED THE BATTERY AND AN OPERATIONAL CHECK WAS COMPLIED WITH. AICRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031009000562003100900056NM 2003 10 9 03FDEA01628 120030924A532065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 STRINGER CLIP 7R CRACKED AT B.S 720B. REPLACED STR CLIP AT BS 720B STR 7R, PER SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20031009000732003100900073EA 2003 10 9 SWIA200312395 120030909A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07409SW 7056 RUDDER TRIM TEST FAILED DURING ORIGINATING CHECK, TRIM WOULD NOT TRIM BACK TO LEFT. REMOVED AND REPLACED RUDDER/AILERON TRIM CONTROL PANEL. OPS CHECK GOOD. P/N: 601R51226-23. 2L72 4F RTA21EA 20031009000752003100900075EA 2003 10 9 SWIA200312397 120030807A322216124101 AXLE CNDAIRCL600 CL6002B19 1900309EA NLG CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 NLG AXLE ASSY HAS PITTING CORROSION AROUND BOLT HOLES. DISCOVERED DURING C-CHECK INSPECTION. NLG AXLE ASSY REPLACED IAW CRJ MM 32-21-15-000-801 AND 32-21-15-400-801. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031009000882003100900088SO 2003 10 9 SWIA200312410 120030905A3230 LANDING GEAR EMB 120 EMB120ER 3260203SO LEFT MALFUNCTIONED A SWIAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM07566SW 120341 LEFT LANDING GEARS A AND B RED AND A AND B GREEN REMAINED ILLUMINATED AFTER LANDING GEAR LEVER WAS RETRACTED. ALSO FELT VIBRATION COMING FROM LEFT SIDE OF AIRCRAFT. ALL LIGHTS NORMAL WHEN LEVER WAS IN DOWN POSITION. PERFORMED SEVERAL GEAR SWINGS WITH NO PROBLEMS FOUND. ALL WORK PERFORMED IAW EMB MM CHAPTER 32. UNABLE TO DUPLICATE DISCREPANCY. 2L72 4T RTA31SO 20031010000142003101000014NM 2003 10 10 USAASB03165 120030912A3260806002 CIRCUIT CARD BOEING737 7373B7 1384580NM MLG INDICATOR MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19530AU 24412 ON CLIMB-OUT FROM PIT, EN ROUTE TO MSY, CREW REPORTED HEARING A LOUD NOISE FORWARD OF CAPTAINS RUDDER PEDALS. ABOUT TEN MINUTES LATER, THE NOSE GEAR GREEN LIGHT AND THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATED. THE NOSE GEAR GREEN LIGHT THEN WENT OUT. CREW FOLLOWED CHECKLIST, EXTENDED GEAR AND RECEIVED NORMAL GEAR INDICATION OF THREE GREEN LIGHTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE SWUNG LANDING GEAR NUMEROUS TIMES. NO FAULTS FOUND. REMOVED AND REPLACED M1214 LOGIC CARD FOR PRECAUTIONARY REASONS. PERFORMED TEST OF M1214 LOGIC CARD PER MM 32-09-20. OPS TEST GOOD. (M) 2L72 4F RTA16WE 20031010000152003101000015NM 2003 10 10 USAASB03161 120030908A27501817389 TRANSMITTER BOEING737 7373B7 1384580NM TE FLAP MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19519AU 23705 AFTER TAKEOFF FROM ORD, EN ROUTE TO PHL, CREW WAS UNABLE TO RETRACT THE FLAPS. FLAPS LOCKED OUT AT 5 UNITS. FLIGHT RETURNED TO FIELD AT ORD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLAP TRANSMITTER AND THE FLAP POSITION INDICATOR, P/N 2061-14-1. ALSO, REPAIRED A LOOSE BONDING JUMPER FOR THE RIGHT FLAP TRANSMITTER. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031010000642003101000064SO 2003 10 10 SWIA200312415 120030914A2530 CONNECTOR EMB 120 EMB120ER 3260203SO COFFEMAKER BURNED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07215SW 120281 SMOKE COMING FROM TOP OF COFFEE JUG (NR 2). STOPPED WHEN SWITCH WAS TURNED OFF. CLEANED GALLEY COFFEE JUG CONNECTOR. OPS CHECK GOOD. 2L72 4T RTA31SO 20031010000672003101000067SO 2003 10 10 SWIA200312418 120030911A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07560SW6786 6786 120334 THREE EMERGENCY EXIT SIGN LIGHTS INOP - 2C, F/A JUMPSEAT AND MAIN CABIN DOOR. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. S/N OFF: 1270/08-96. 2L72 4T RTA31SO 20031010000712003101000071CE 2003 10 10 FPI2003F00010 120030812A8000643109 CLUTCH SPRING CESSNA210 210N 2073453CE CONT O520 IO520* 17032SO STARTER ADAPT BROKEN A FPIAO OTHER O OTHER NRNOT REPORTED 1 SO154637Y262 21063965 295268R WITH IGNITION SWITCH CLOSED STARTER MOTOR SPINS BUT WILL NOT TURN ENGINE. UPON REMOVAL OF STARTER ADAPTER FOUND CLUTCH SPRING BROKEN. PILOT REPORTED (STARTER INOP). 1H71 3O3 O 3A21 E5CE 20031010000822003101000082 2003 10 10 BAQA089301 420030920A3100281810615 RELAY LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 322 092 REQUEST WARRANTY CONSIDERATION. PART LASTED ONLY 321.8 HOURS. K4 RELAY KEEPS RT STANDBY PUMP ON WITH SWITCH OFF. MRA NR: 1125180-000020 REPLACED WITH SERVICEABLE UNIT. 9/22/03 2L72 4F4 F A10CE E6WE 20031010000842003101000084 2003 10 10 BAQA089304 420030918A34006226521016 CONTROL HEAD AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE NAVIGATIONAL MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 532 6036 WILL NOT HOLD FREQUENCY IN MEMORY. REPLACED WITH SERVICEABLE UNIT. 9/23/03 1G72 3U3 U H10EU E19EU 20031010000882003101000088EU 2003 10 10 BAQA089269 120030922A2611 WIRE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE FIRE DETECTION BROKEN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 5609 6036 FIRE FAIL LIGHT WIRE BROKEN/LOCK IN BACK OF CONNECTOR BROKEN. REPLACED WITH SERVICEABLE UNIT. 9/25/03 1G72 3U3 U H10EU E19EU 20031010000942003101000094 2003 10 10 BAQA089470 420030918A2210117884141 COMPUTER BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE CSAS INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G168 7179 COMPUTER UNIT IS INOP. REPLACED WITH SERVICABLE ASSET. 1G72 3U3 U H13EU E5NE 20031010000992003101000099EU 2003 10 10 BAQA089526 120030923A6210L621M1010054 BLADE UROCOPEC135 EC135P1 8680990EU MAIN ROTOR CONTAMINATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH460 0069 REQUEST WARRANTY REPAIR . WATER IN BLADE. PART HAS ONLY 460.0 HOURS ON IT. REPLACED WITH SERVICEABLE RENTAL. 1G72 3U O H88EU 20031014000182003101400018NM 2003 10 14 UPS03541238 120030906A5330 SKIN BOEING757 75724APF 1384969NM FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01449UP 27738 INSPECTION TYPE: C1, FUSELAGE SKIN HAS LIGHTNING STRIKE AT BS 762 STR 8L. REPAIRED PER ER 03-2498 DATED 09/15/03. 2L72 4F RTA2NM 20031014000212003101400021NM 2003 10 14 UPS03541241 120030906A5330 SKIN BOEING757 75724APF 1384969NM FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01449UP 27738 INSPECTION TYPE: C1, FUSELAGE SKIN HAS LIGHTNING STRIKES AT BS 1743 BETWEEN STR 23L AND 24L. REPAIRED IAW ER 03-3472 DATED 09/15/03 2L72 4F RTA2NM 20031117000872003111700087GL 2003 11 17 ALG2003F00093 220030904A7532 BLEED VALVE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW0315Q 2235 CAE823305 ON CLIMB OUT, AT 300 FT, THE PILOT REDUCED POWER FROM 90 PERCENT TORQUE TO 80 PERCENT TORQUE AND STARTED A RIGHT TURN, HE HEARD A LOUD NOISE AND THE HELICOPTER YAWED 20 FT TO THE LT, HE REDUCED POWER TO 50 PERCENT AND LANDED, UPON LANDING THE MECHANIC CHECKED THE ENGINE COMPRESSOR AND REPLACED THE BLEED VALVE, HE ALSO COMPLIED WITH PNEUMATIC CHECK, OPS CHECK AND POWER CHECK WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 20031218000562003121800056SO 2003 12 18 C2XA03CL192 120031126A335074441 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711536 145520 CREW REPORTED THE EMERGENCY EXIT LIGHTS WILL NOT ARM PROPERLY. MAINTENANCE INSPECTED AND REPLACED THE EXIT IDENTIFIER SIGN OVER THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20031218000632003121800063NM 2003 12 18 03FDEA02001 120031128A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN CARGO DECK RIGHT STA 495 AT X=75.25 SEAT TRACK DAMAGED. DAMAGED SEAT TRACK AT MAIN CARGO DECK RH STA 495, REFERENCE 75.25. REMOVED AND REPLACED WITH NEW SEAT TRACK AS PER SRM 51-31-01, VOL.II. 2L73 4F RTA22WE 20031218000672003121800067SO 2003 12 18 C2XA03TY199 120031202A5320 FLOOR SUPPORT EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727506 145206 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT JUST AFT OF MAIN DOOR. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031218000722003121800072EU 2003 12 18 AWXA200301507 120031121A5320D5323028120140 ANGLE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 DURING C-06 CHECK A .5 INCH CRACK WAS FOUND ON ANGLE AT FORWARD LOWER OUTBOARD CORNER UNDER PANEL 192E AT FR 34. MAINTENANCE REMOVED CRACKED ANGLE AT FR 34; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-8, A2, 21 FIG 2 & 59. 2L72 4F RTA28NM 20031218000772003121800077SO 2003 12 18 C2XA03BT113 120031130A32348271013 LEVER EMB 145 EMB145ER 3260211SO MLG FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27129461209612096 145052 CREW REPORTED, AFTER TAKEOFF GEAR HANDLE WOULD NOT RETRACT. DOOR LOCK RELEASED LOUD NOISE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER IAW EMB145 AMM 32-32-02. GEAR SWING PERFORMED, NO FAULTS FOUND. OPS CHECKED GOOD IAW EMB145 AMM 32-32-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031218000822003121800082NM 2003 12 18 2003UALA00865 120031117A5753 FITTING BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT WING TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29676UA 30028 LEFT WING INBD FLAP CENTER EXTERNAL HINGE FITTING CRACKED ON INBD SIDE FLANGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE FITTING PER SRM 57-53-02, FIG 201 AND INSTALLED REPAIR PER SRM 51-40-2. 2L72 4F4 FRTA1NM E24NE 20031218000882003121800088NM 2003 12 18 2003UALA00875 120031118A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CANNING A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 FUSELAGE SKIN OIL CANNED ON RT SIDE AT STA 912 STRINGER 18R, CAUSED BY DENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031218000902003121800090NM 2003 12 18 2003UALA00878 120031119A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29507UA 24743 TWO SMALL DENTS FWD OF DR2L. DENTS ARE APPROX 3 X .062 INCH D. SMOOTH, CRACK FREE AND NO PULLED FASTENERS. LOCATED APPROX 3 INCHES ABOVE WATERLINE BETWEEN STA 600 AND 620. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031218001062003121800106NM 2003 12 18 2003UALA00894 120031124A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29645UA 25280 SEAT TRACK BETWEEN STA 764-784, LBL 62 IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF SEAT TRACK AND FABRICATED SPLICE REPAIR PER BAC DWG 145T2222-4 AND SRM 51-40-2. 2L72 4F4 FRTA1NM E24NE 20031218001212003121800121WP 2003 12 18 DHL2003809008 120031202A3350 BATTERY DOUG DC8 DC873F 302199FWP FUSELAGE DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01604AL 46047 EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOPERATIVE. RECHARGED BATTERY AND OPS CHECKED GOOD PER M/M 33-50-0. 2L74 4F RT4A25 20031218001242003121800124NM 2003 12 18 03FDEA02004 120031130A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 CENTER CARGO BETWEEN STA 5-113 TO STA 1541, NR 49L LONGERON SPLICE FOUND CRACKED. 2L73 4F RTA22WE 20031218001302003121800130SO 2003 12 18 RAIA00311291 120031124A3610 FILTER EMB 145 EMB145LR 3260212SO CARGO BAY DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03811HK 145256 5251 PIT- BLEED 1 OVERTEMP ADVISORY. MAINTENANCE REMOVED AND REPLACED FAN AIR VALVE FILTER. 2L72 4T RTT00011AT 20031218001522003121800152NM 2003 12 18 DHL2003765004 120031204A5270 SWITCH BOEING727 727264 138408MNM AIRSTAIR DIRTY A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01765AT 23014 AFT AIRSTAIR LIGHT CAME ON DURING TAKEOFF ROLL. INSPECTED & CLEANED AFT AIRSTAIR UP POSITION SWITCH AND TESTED IAW M/M 52-70-01. ALL LIGHTS OUT, OPS CHECKED NORMAL. REJECTED T/O PARAMETERS: PRESSURE ALTITUDE 0, TEMPERATURE -2 DEGREES C, WEIGHT 172,300 AND INDICATED AIRSPEED 70 KNOTS. FOR INFORMATION PURPOSES ONLY. 2L73 4F A3WE 20031218001602003121800160SO 2003 12 18 C2XA03SH481 120031204A541314576094009 LONGERON EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 DURING C-CHECK THE LEFT LOWER ENGINE COWLING AFT STRINGER THIRD FROM INBOARD WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031218001682003121800168NM 2003 12 18 03FDEA02049 120031204A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 380 RBL 45 TO 56. 2L73 4F RTA3WE 20031218001712003121800171WP 2003 12 18 CALA0300691 120031204A533059114323 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 SKIN CRACKED AT RIVET STA 1418 JUST OUTBOARD OF LEFT VERTICAL ATTACH ANGLE. FABRICATED AND INSTALLED DOUBLER AT STA 1418 FUSELAGE SKIN PER SRM 53-04 FIG 4D SHEET 1. 2L72 4F A6WE 20031219000022003121900002NM 2003 12 19 CALA0300694 120031205A52476550904 SKIN BOEING737 737524 1384721NM APU DOOR GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916649 28910 APU ACCESS DOOR INNER SKIN GOUGED LT SIDE FORWARD OF AFT LATCH. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 5200-01. 2L72 4F RTA16WE 20031217001212003121700121WP 2003 12 17 AALA20031158 120031019A2140 DUCT DOUG DC9 DC982 3022082WP TAIL LEAKING A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21408AA 49319 EN ROUTE DFW-LAS, TAIL COMPARTMENT INDICATED HIGH TEMPERATURE DURING CLIMB-OUT. DECLARED EMERGENCY AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION. INSPECTION OF AIRCRAFT FOUND LEFT AND RIGHT TEMPERATURE CONTROL VALVE DUCT BOOTS LEAKING. TIGHTENED CLAMPS FOR DUCTS BOOTS. PERFORMED LEAK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031217001452003121700145EA 2003 12 17 COMA0360552 120031211A53116003603032 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01979CA16390 7159 RIGHT SIDE FS 718.0 AFT FRAME DOUBLER IS CRACKED. REMOVED CRACKED DOUBLER AND INSTALLED NEW DOUBLER P/N 600-36030-32 IAW BOMBARDIER, INC REO 601R-53-61-193 REV A. 2L72 4F RTA21EA 20031218000072003121800007NE 2003 12 18 P5CA0300993 220031123A73217552101 FUEL CONTROL BOEING747 747283B 1384867NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 WP23921FT 21575 689184 ON ENG START NR 2 ENGINE ACCELERATED TO HIGH IDLE 75 PERCENT N2. REMOVED AND REPLACED NR 2 ENG FCU AND THE TT2 SENSOR UNIT IAW 73-21-01 AND AMM 73-21-04, OPS CK AND LEAK CHECK SATISFACTORY. 2L74 4F4 F A20WE E20EA 20031218000212003121800021WP 2003 12 18 IXXA0300081O 120031125A5270BAN70241 SWITCH DOUG DC8 DC871F 302199DWP MLG DOOR SHORTED A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11830BX753172076 45973 AFTER TAKEOFF FROM KTOL GEAR DOORS LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE R / R LT GEAR DOOR SWITCH AND CONNECTOR. AN INSPECTION OF THE KEELBEAM LOWER BRACKETS WAS ACCOMPLISHED WITH NO DEFECT FOUND. JACKED AIRCRAFT, LANDING GEAR AND DOOR INDICATION OPERATIONAL CHECK GOOD ON SEVERAL EXTENSIONS AND RETRACTIONS PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20031218000312003121800031SO 2003 12 18 SWIA200312626 120031102A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07567SW 120342 LEFT FRAME 9 SKIN SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REWORKED LEFT SIDE FRAME 9 PER SERVICE BULLETIN NR 120-53-0073 REV 00 DATED 21 JUL 99. 2L72 4T RTA31SO 20031218000482003121800048EA 2003 12 18 03328665 120031124A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27665BR 7534 DURING INSPECTION THE CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031218001352003121800135WP 2003 12 18 ZW0A0306401 120031203A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139404V 53140 THE AFT CABIN EGRESS LIGHTING WAS INOPERATIVE. REPAIRED DAMAGED FLOOR CONNECTION AND RESEATED BATTERIES IN THE POWER SUPPLY. CHECK-C 9-15-03 MCI. 2L72 4F RTA6WE 20031219000422003121900042SO 2003 12 19 C2XA03SH486 120031207A531314528737001 TEE FITTING EMB 145 EMB145LR 3260212SO LONGERON GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 DURING C-CHECK THE TEE REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031219000522003121900052NE 2003 12 19 C1HA200381034 220031207A7230 COMPRESSOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A C1HAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL15681CA 22020 COMPRESSOR STALL NR 2 ENGINE ON THROTTLE ADVANCE AT 1.4 EPR TEMPS NORMAL. ALL PARAMETERS NORMAL WIND WAS A CROSSWIND, RUNWAY 25R = WIND WAS 180 AT 14 GUSTING TO 19 INSPECTED INLET AND EXHAUST NR 2 ENG. NO DISCREPANCIES NOTED. RAN ENG TO 1.4 EPR - INTO WIND, NO STALL NOTED. PARAMETERS NORMAL. REF MM 71-00. 2L73 4F4 F A3WE E2EA 20031219000632003121900063WP 2003 12 19 CALA0300697 120031120A5312 BEAM DOUG DC9 DC982 3022082WP BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772821 49481 INSPECTION FOUND STA 110 BULKHEAD BEAM WEB CORRODED AT MAIN BATTERY GROUND STUD HOLE. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387. 2L72 4F A6WE 20031219000642003121900064NM 2003 12 19 CALA0300698 120031203A5330 SKIN BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714235 28947 INSPECTION FOUND THE FUSELAGE SKIN IMMEDIATELY FORWARD OF THE AFT JACKING PAD FITTING INSTALLATION DENTED WITH A CRACK AT STA 1086, S24R-25R. THE SKIN WAS REPAIRED IAW ECRA 5330-03305. 2L72 4F RTA16WE 20031219000882003121900088NM 2003 12 19 2003UALA00916 120031128A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29658UA 27113 LT SIDE OF CABIN EEL LIGHT FLOOR PATH LIGHTING IS INOP INCLUDING OVERWING EXIT MARKERS STARTING AT COACH SEATS. REPLACED BATTERY PACK. TESTS OK. 2L72 4F4 FRTA1NM E24NE 20031219000922003121900092NM 2003 12 19 2003UALA00920 120031126A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29375UA 24640 TWO EACH DENTS IN FUSELAGE AT STA 460 BETWEEN STRINGER 18L AND 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031219000962003121900096NM 2003 12 19 2003UALA00924 120031201A5210 SEAL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE R2 DOOR OBSTRUCTED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29934UA 26662 RETURNED TO LAS DUE TO LOUD DOOR SQUEAL FROM DOOR 2R. FOUND DEBRIS AND CLEARED. INSPECTED DOOR SEAL, NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E2GL 20031219001002003121900100 2003 12 19 2003UALA00929 420031202A2565 BATTERY PACK BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE ESCAPE SLIDE MISINSTALLED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29669UA 30025 RIGHT EMERGENCY ESCAPE SLIDE SQUIB WILL NOT TEST. EVENT CAUSED BY IMPROPERLY INSTALLED BATTERY PACK. 2L72 4F4 FRTA1NM E24NE 20031219001192003121900119NM 2003 12 19 03FDEA02064 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73352, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001222003121900122NM 2003 12 19 03FDEA02067 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT POINT, SPOT FACE CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT POINT, SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001242003121900124WP 2003 12 19 03FDEA02069 120031205A243231433001 BATTERY DOUG DC10 DC1010 3022110WP MASTER MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25393FE 46627 FIFTY MIN INTO FLT AT FL370 RECEIVED AT LEVEL BATTERY DISCHARGING ALERT. ALERT STAYED ON ABOUT 30 SEC 10 MIN LATER IT CAME ON AND STAYED ON. A/C DIVERTED TO CHS. DURING DESCENT (FL 200) ALERT WENT AWAY AND DID NOT RE-OCCUR. REPEAT WRITE-UP. NEEDS NEW A/C BATTERIES. ORDERED SAME. REMOVED AND REPLACED AIRCRAFT BATTERIES IAW MD-10 MM. REMOVED AND REPLACED EPCU IAW MD-10 MM 24-08-01-4, REMOVED AND REPLACED B1-134 RCCB IAW MD-10 MM 24-50-01. ALSO FOUND TERMINALS ON SHUNT S4-1 LOOSE TIGHTENED TERMINALS, FOUND TEMP SENSOR ON LT BATTERY BAD, A/C BATTERIES ON ORDER. 2L73 4F A22WE 20031219001412003121900141NM 2003 12 19 03FDEA02122 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001562003121900156NM 2003 12 19 03FDEA02142 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73355 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031219001602003121900160NM 2003 12 19 03FDEA02146 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE BORE CORRODED. OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT, OUTBOARD HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73356, WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031219001662003121900166NM 2003 12 19 QXEA200301503 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 2 SEAT TRACK HAS LITE SURFACE CORROSION ON RAILS AND IN BOTTOM OF CHANNEL FROM X467 TO 4 INCHES AFT OF X467. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20031219001832003121900183NM 2003 12 19 MWEA030477 120031209A521099557529 ANGLE DOUG MD88 MD88 3023688NM PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FORWARD PASSENGER DOOR TOP BEAM IS CRACKED AT AFT END. FABRICATED AND INSTALLED NEW ANGLE. 2L72 4F RTA6WE 20031218000092003121800009NM 2003 12 18 MWEA030452 120031125A53459936534165 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 J-CHANNEL FRAME STATION 160-200 SIXTEEN INCHES INBOARD OF FORWARD GALLEY DOOR IS CORRODED ALONG TOP SURFACE. FABRICATED AND INSTALLED NEW J-CHANNEL. 2L72 4F RTA6WE 20031218000242003121800024EA 2003 12 18 COMA0360512 120031125A5610NP1393225 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A COMAO OTHER O OTHER CRCRUISE 1 SO01641CA207 10122 FLIGHT 5677 DURING CRUISE FLT AT 24,000 FT THE CAPTAINS SIDE WINDOW INNER PANE SHATTERED. AIRCRAFT CONTINUED TO DESTINATION (CVG) CITY AND LANDED SAFELY. REPLACED THE CAPTAINS SIDE WINDOW. 2L72 4F RTA21EA 20031218000272003121800027EA 2003 12 18 SWIA200312622 120031124A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401. P/N: 601R-53-61-117-2, 601R-53-61-117-4 2L72 4F RTA21EA 20031218000362003121800036EA 2003 12 18 SWIA200312631 120031125A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07967SW 7872 STAB TRIM CH 2 WILL NOT TEST. TRIM WILL KICK OFF WHEN ATTEMPTING TO RUN THE TRIM WITH JUST STAB TRIM CH 2 AND MACH TRIM ENGAGED. REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR AND HORIZONTAL STABILIZER MOTOR CONTROL UNIT IAW MM 27-42-05. OPS CHECK GOOD. S/N OFF: 1152. MOTOR CONTROL UNIT P/N OFF: 7062-3, S/N OFF: 1184. 2L72 4F RTA21EA 20031218000732003121800073NM 2003 12 18 AWXA200301508 120031103A5754 SKIN BOEING737 7373G7 1384595NM RT WING SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW16964 24012 DURING C-15 CHECK 2 EACH CRACKS WERE FOUND ON NR 6 SLAT LOWER SKIN BELOW CENTER AUXILIARY TRACK. MAINTENANCE REMOVED AND REPLACED NR 6 LEADING EDGE SLAT PER BMM 27-81-21. 2L72 4F RTA16WE 20031218000742003121800074EU 2003 12 18 AWXA200301509 120031124A5320D53974749000 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 DURING C-06 CHECK A .5 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT RIGHT UPPER PROFILE, FORWARD OF FR 47. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY CRACK END; STOP DRILLED CRACK ON RIGHT UPPER PROFILE; RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND TAPERED SHIM; INSTALLED REPAIR PARTS IAW AWA ER 26-5314-00011-JS4. 2L72 4F RTA28NM 20031218000752003121800075EU 2003 12 18 AWXA200301510 120031124A5320D5397467200000 PROFILE AIRBUS320 A320232 3930326EU CARGO BAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 MCN - MINOR REPAIR - DURING C-06 CHECK 2 EACH .5 INCH CRACKS WERE FOUND ON AFT CARGO COMPARTMENT LT UPPER PROFILE, FORWARD OF FR 47. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY CRACK END; STOP DRILLED CRACK ON LT UPPER PROFILE; RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND TAPERED SHIMS; INSTALLED REPAIR PARTS IAW AWA ER 26-5314-00011-JS4. 2L72 4F RTA28NM 20031218000852003121800085NM 2003 12 18 2003UALA00871 120031114A8011 STARTER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAILED A UALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP29925UA 26646 NR 2 ENGINE STARTER DISINTEGRATED ON STARTUP. ISOLATED SOURCE OF FAILURE TO NR 2 ENGINE STARTER. STARTER HAD AN UNLOADED FREEWHEEL TURBINE FAILURE EVENT WITH PARTS EXITING THE HOUSING AND PENETRATING COWLING, WING ROOT FAIRING, FUSELAGE AND SHUTOFF VALVE WHICH IS LOCATED OVER STARTER HOUSING. ACCOMPLISHED REPAIR TO THE FUSELAGE SKIN UNDER THE LEADING EDGE WINGROOT FAIRING. REPLACED STARTER, STARTER VALVE AND LT COWLING HALF. 2L72 4F4 FRTA16WE E2GL 20031218001342003121800134CE 2003 12 18 DXTA200300172 120031129A2120 ODOR CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07330QS 5600329 LOUD BANG WAS HEARD AND FELT WHILE CLIMBING THROUGH FL 37 AN ODOR WAS MOMENTARILY ASSOCIATED WITH IT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAS. UPON LANDING THE FIRE PERSONNEL REPORTED LARGE QUANTITIES OF SMOKE EMANATING FROM THE ENGINE AREA. O2 MASKS WERE DEPLOYED. THIS IS STILL UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20031218001622003121800162NM 2003 12 18 MWEA030460 120031203A53209910078627 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 J-CHANNEL FLOOR SUPPORT AT STATION 200 NEAR AFT LOWER CORNER OF FORWARD PASSENGER DOOR IS CORRODED. FABRICATED AND INSTALLED NEW FLOORBOARD. 2L72 4F RTA6WE 20031219000082003121900008WP 2003 12 19 ABXA030455 120031114A532059516855 FITTING DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 LONGERON 29 RIGHT END FITTING CRACKED ON OUTBOARD SIDE FS 756. REPAIRED LONGERON 29 RIGHT AT STA 756 IAW DC-9 SRM 53-02. 2L72 4F A6WE 20031219000752003121900075SO 2003 12 19 C2XA03TY203 120031207A574114522141407 TIE ROD EMB 135 EMB135ER 3260203SO LT WING ROOT CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717507 145215 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND WING TO FUSELAGE TIE ROD ASSEMBLE. MAINTENANCE REMOVED AND REPLACED THE TIE ROD IAW EMB IC 2003-145/4092. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031219000802003121900080WP 2003 12 19 MWEA030475 120031206A3411 PITOT LINE DOUG DC9 DC981 3022081WP COCKPIT LEAKING A MWEAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL31804ME 48030 CAPTAIN'S MACH INDICATOR HAS .14 MACH SPLIT AND EIGHT KNOTS SPLIT BETWEEN FIRST OFFICER'S AIRSPEED. SELECTING CENTRAL AIR DATA COMPUTER TO BOTH ON ONE AND TWO CORRECTED THE SPLIT. FOUND MASSIVE LEAK IN PITOT ON NUMBER ONE PITOT SYSTEM, TIGHTENED FITTINGS, LEAK CHECKED GOOD. 2L72 4F A6WE 20031219001302003121900130NM 2003 12 19 03FDEA02111 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. LT WING OUTBD FLAP INBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001322003121900132NM 2003 12 19 03FDEA02113 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348 : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001472003121900147NM 2003 12 19 03FDEA02131 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT POINT BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73359. TRAILING EDGE & TRAILING EDGE DEVICES. LT INBOARD FLAP HINGE BRACKET REPAIR 2L73 4F RTA22WE 20031219001772003121900177EU 2003 12 19 MALA030523 120031207A302044730501 CONTROL MODULE SAAB SF340 340B 7860101EU DEICE SYSTEM MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15433XJ 340B433 DURING FLIGHT 3177 RIGHT INTAKE HEAT MSTER CAUTION COME ON WITH THE RIGHT ENGINE ANTI-ICE SELECTED ON AFTER RESETTING THE SWITCH THE CAUTION LIGHT COMES BACK ON AFTER A FEW MINUTES. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RIGHT INTAKE HEAT DEICE CONTROL MODULE P/N 44730-501, S/N OFF L258945, S/N ON L248464. OPS CHECK GOOD. 2L72 4T RTA52EU 20031222000022003122200002WP 2003 12 22 ARWA20031202 120031206A3411 PITOT HEAD DOUG DC8 DC862 3021970WP FAILED A ARWAA UNSCHED LANDING SG AFFECT SYSTEMS MULTIPLE FAILURE CLCLIMB 1 SO198969U 46070 ON CLIMBOUT OF KMIA, CAPTAIN LOST ALTIMETER, AIRSPEED, AND VSI INDICATIONS. 2L74 4F 4A25 20031222000042003122200004WP 2003 12 22 ARWA20031204 120031206A5711 SPAR DOUG DC8 DC862 3021970WP LT WING CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19810BN 45905 DURING ACCOMPLISHMENT OF RB 17284 SB 57-090 INSPECTION. LEFT WING FRONT SPAR XFS 517 & XFS 518, LOWER CAP HOLES (2 EACH) WITH CRACKS. 2L74 4F 4A25 20031222000112003122200011NM 2003 12 22 F3LA200300158 120031204A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 312, BL 0. REMOVED DAMAGED UPPER T-CHORD AT STA 312, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51 AND 51-40-02. 2L72 4F RTA16WE 20031117000922003111700092SW 2003 11 17 ALG2003F00097 120030628A6340B4678 CHIP DETECTOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL GEARBOX MALFUNCTIONED E ALGAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW03362AL 51471 ON DEPARTURE, THE TRANSMISSION CHIP LIGHT FLICKERED TWICE, THE AIRCRAFT WAS RETURNED TO INTRACOASTAL BASE. THE MECHANIC FOUND HAIR LIKE SLIVER ON THE LOWER CHIP PLUG, HE REPLACED THE OIL AND FILTER AND C/W PENALTY RUN AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E1GL 20031117000952003111700095NM 2003 11 17 XNOA01157 120031007A3260 WARNING LIGHT BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE MLG ILLUMINATED A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL23793A 20774 AFTER GEAR RETRACTION OUT OF FLL, ALL RED WARNING LTS ILLUM FOR ENTIRE FLIGHT. ALSO THE TAIL SKID LT ILLUM FOR THE ENTIRE FLIGHT. LG ACC UNIT FAILED PART(4) SECTION (F) OF FUNCTIONAL TEST. REMOVED AND REPLACED LG ACC, OPS CK GOOD IAW B727 MM 32-09-121. STATUS (ORIG/CLOSED) 2L73 4F4 F A3WE E2EA 20031118000022003111800002NM 2003 11 18 AT0300030 120031007A2612 FIRE LOOP BOEING717 717200 1383700NM NR 2 ENGINE MALFUNCTIONED A ZZDAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 SO15924AT 55080 AFTER SEVERAL MOMENTARY (FIRE DETECTION RIGHT FAIL) INDICATIONS AS WE APPROACHED MYR HAD BELL AND LIGHTS RIGHT FIRE HANDLE. SECURED RIGHT ENGINE AND INDICATIONS STOPPED FOR SEVERAL MINUTES. LIGHT AND BELL RETURNED SO WE PULLED THE FIRE HANDLE WHICH AGAIN STOPPED INDICATIONS LANDING COMPLETED WITH FIRE DEPARTMENT RESPONSE. REMOVED AND REPLACED TE UPPER FIRE LOOP SPLITTER. 2L72 4F TRA6WE 20031118000242003111800024NM 2003 11 18 AWXA200301139 120030904A5315657748875 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM AT BS 305, FORWARD FLIGHT ATTENDANT SEAT MOUNT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM AT BS 305 BETWEEN LBL 10 AND LBL 40; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG 65-77488; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1-6, FIG 16. 2L72 4F RTA16WE 20031118000832003111800083EU 2003 11 18 XNOA01159 120031009A2760 INDICATOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE LT SPOILER STUCK A XN0AD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL23372PC 196 LT SPOILER INDICATOR STICKS WITH FLT CONTROL CHECK INTERMITTENT. ACTION TAKEN: CYCLED LT SPOILERS AND FLT CONTROL UPPER SURFACES THROUGH SEVERAL TIMES, VISUALLY INSPECTED FLT CONTROL SURFACES. ALL ASPECTS INCLUDING INDICATION OPS CK GOOD ON GROUND IAW A-300 AMM 27-15-00 NO DEFECTS NOTED. 2L72 4F4 FRTA35EU E23EA 20031118000902003111800090SO 2003 11 18 SWIA200312474 120030910A5712 RIB EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RT WING LE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07297SW 120327 RT IB LEADING EDGE RIB IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) DOUBLER REINFORCEMENTS ADDED TO ABOVE MENTIONED RIB AREA IAW EMB120 SRM 51-10-02. 2L72 4T4 TRTA31SO E20NE 20031118000912003111800091 2003 11 18 SWIA200312480 420030928A22156225734002 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RUDDER MALFUNCTIONED A SWIAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM07291SW8210 8210 120318 RUDDER PEDALS JAMMED DURING TAKEOFF ROLL. TAKEOFF ABORTED. REMOVED AND REPLACED RUDDER SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031118001072003111800107NM 2003 11 18 AWXA200301183 120030912A5321146N575011 FLOOR PANEL BOEING757 7572S7 1384962NM CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK CABIN FLOOR PANEL S-6 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 146N5750, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1. 2L72 4F RTA2NM 20031118001122003111800112NM 2003 11 18 AWXA200301188 120030912A5321144N533049 FLOOR PANEL BOEING757 7572S7 1384962NM CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL N-5 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 146N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1. 2L72 4F RTA2NM 20031112000572003111200057NM 2003 11 12 AWXA200301393 120031110A3350BR964411 LIGHT BOEING757 7572S7 1384962NM CABIN INTERMITTENT A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - EEL - DURING INSPECTION FOUND AN INTERMITTENT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20031112000612003111200061WP 2003 11 12 UPS03841480 120031026A5320 FITTING DOUG DC8 DC873F 302199FWP CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 CENTER ZEE FITTING STRUCTURE CRACKED. R&R CENTER WINDSHIELD LOWER CENTER CHANEL PER EO DC8-532019452A. PERMANENT TO BE INSTALLED AT NEXT C-CHECK PER ITEM 2 THIS SAME LOGPAGE. 2L74 4F RT4A25 20031112000652003111200065NM 2003 11 12 03FDEA01879 120031105A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 FUSELAGE UPPER LOBE, BS 720B 15.5, STR 15R, CRACKED BS 720B 15.5, STR 16 R/H CRACK FOUND TO BE OUT OF LIMITS. REPAIR DAMAGE STR. 15 RT PER SRM 53-10-3. 2L73 4F RTA3WE 20031112000672003111200067NM 2003 11 12 CALA0300630 120031109A5512 SKIN BOEING737 7373T0 1384582NM HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A 1 INCH CRACK AND A 1.25 INCH CRACK IN LT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN BETWEEN STAB STA 147 AND 157. THE SKIN WAS REPAIRED IAW ECRA 5510-01699. 2L72 4F RTA16WE 20031113000052003111300005EU 2003 11 13 BAQA085097 120031022A5320L713M2071105 CHANNEL UROCOPEC135 EC135T1 5620026EU FUSELAGE CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME2065 0143 CHANNEL CRACKED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031113000132003111300013 2003 11 13 BAQA090537 420031029A3497 COAX BOLKMS117 BK117A1 5626010EU RADAR ALT ANTENNBROKEN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118NC 13794 7067 COAX CABLE BROKE. REPLACED WITH SERVICEABLE PART. 1G72 3U H13EU 20031222000142003122200014 2003 12 22 SWIA200312643 420031121A34186005915615 STICK SHAKER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER PF NO WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07906SW 7510 STALL STICK PUSHER DOES NOT TEST PROPERLY. REMOVED AND REPLACED STICK PUSHER. OPS CHECK GOOD PER CRJ MM 27-35-15. 2L72 4F RTA21EA 20031222000222003122200022EA 2003 12 22 SWIA200312651 120031203A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AIL/RUDDER TRIM FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07935SW 7725 RUDDER TRIM WILL NOT TRIM PROPERLY TO THE LEFT. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL PANEL. OPS CHECK GOOD. 2L72 4F RTA21EA 20031222000252003122200025NM 2003 12 22 F3LA200300161 120031205A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 344, LBL 13. REPLACED FLOORBEAM UPPER CAP PER EA B3-53R-10237. 2L72 4F RTA16WE 20031222000312003122200031NM 2003 12 22 QXEA200301531 120031208A5751 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 RT AILERON HAS A SMALL .25 INCH CRACK IN OUTBOARD TAB HINGE CUTOUT. REPAIRED IAW DHC-8 SRM 57-60-71 AND HORIZON AIR EA 2-57-244. 2H72 4T RTA13NM 20031222000572003122200057WP 2003 12 22 ASAA0380607 120031007A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, FLIGHT DECK FLOORBOARD DELAMINATED AND CORRODED AT FS 125-160. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031222000592003122200059WP 2003 12 22 ASAA0380610 120031007A53219932816501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, FLOOR PANEL DISBONDED AT EDGE AT FS 769-826. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20031222000642003122200064WP 2003 12 22 ASAA0380613 120031007A532199365451 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, FLOORBOARD HAS CORRODED AND SOME MISSING INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031222000742003122200074WP 2003 12 22 AALA20030979 120030908A25302510000405 OVEN DOUG DC9 DC982 3022082WP GALLEY SMOKE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21216AA 49167 FOUND GALLEY INBOARD OVEN PRODUCES LARGE AMOUNT OF SMOKE WITH STRONG BURNING ODOR WHEN IN OPERATION. PULLED CIRCUIT BREAKER, NO SMOKE. OVEN REPLACED BY MAINTENANCE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031222000862003122200086NE 2003 12 22 AALA20031031 220030920A7532 BLEED VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 1 ENGINE DAMAGED A AALAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW21968TW 53618 AIRCRAFT EN ROUTE ENCOUNTERED TWO LARGE VIBRATIONS THROUGHT OUT THE ENTIRE AIRCRAFT, PRESSURE FLOW LIGHT WENT ON WITH CABIN CLIMBING AT 1500 FT PER MINUTE. ANTI-ICE WAS IN THE ON POSITION. APPEARED TO BE COMPRESSOR STALL ON ENGINE NR 1. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS NOT OVERWEIGHT. REPLACED THE PRBS VALVES AND ACCOMPLISHED BLEED LUBE. LEAK AND SYSTEM GROUND CHECKED NORMAL. (M) 2L72 4F4 FRTA6WE E9NE 20031222000912003122200091EU 2003 12 22 USAABA03038 120031114A3240C2029338D8D8D CONTROL UNIT AIRBUS330 A330323 3930335EU MLG BRAKES MALFUNCTIONED A USAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA19675US10875 0370 UPON TAXIING TO THE GATE AFTER LANDING, THE BRAKES HAD NO RESPONSE UNTIL FULLY DEPRESSED. CREW REPORTED A NORMAL BRAKE INOP MESSAGE. MAINTENANCE FOUND THE NR 2 BSCU BLANK. THE BSCU WAS RESET. BITE FAULTED THE SELECTOR VALVE. THE BSCU AND VALVE WERE PROGRAMMED FOR REPLACEMENT. NOV 15, MAXIMUM BRAKES WERE NEEDED BEFORE ANY BRAKING RESPONSE WAS NOTED. BOTH THE BSCU AND NORMAL BRAKE SELECTOR VALVE WERE REPLACED. (M) 2L72 4F RTA46NM 20031222001152003122200115NM 2003 12 22 2003F00645 120031110A2612692383219 MODULE BOEING727 727200 138407ENM COCKPIT INTERMITTENT A P9RAO OTHER N FALSE WARNING LDLANDING 1 SO11906PG 20728 UPON LANDING TOUCHDOWN, THE APU FIRE HANDLE RED LIGHT CAME ON AND AN INTERMITTENT FIRE BELL SOUNDED FOR SEVERAL SECONDS. START SEQUENCE HAD NOT BEEN INITIATED AND APU HAD BEEN SHUT DOWN FOR APPROXIMATELY 1 HOUR. AFTER SEVERAL SECONDS THE INDICATIONS DISAPPEARED. FIRE HANDLE WAS PULLED. REMOVED AND REPLACED APU FIRE TEST CONTROL MODULE IAW BMM. OPS TESTED NORMAL. (M) 2L73 4F RTA3WE 20031218000302003121800030SO 2003 12 18 SWIA200312625 120031102A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07567SW 120342 SKIN SUPPORT BRACKET AT FRAME 12 BEHIND LEFT DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT BRACKET AT FRAME 12 BEHIND LEFT DV WINDOW IAW EMB SRM 51-10-02, 51-40-00. P/N: 120-12545-001. 2L72 4T RTA31SO 20031218000872003121800087NM 2003 12 18 2003UALA00874 120031118A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29362UA 24455 STA 616 FRAME IS CRACKED AND THE WEB IS DAMAGED JUST BELOW STR 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031219000302003121900030SO 2003 12 19 SWIA200312632 120031123A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07583SW7345 7345 120351 FORWARD SECTION OF EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED FORWARD ELBP. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031219000342003121900034SO 2003 12 19 SWIA200312636 120031123A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07188SW128702596 120039 FLAP DISAGREEMENT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW MM 27-50-01. OPS CHECK GOOD. 2L72 4T RTA31SO 20031219000452003121900045 2003 12 19 SWAA032605 420031126A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20031219000602003121900060WP 2003 12 19 UPS03841643 120031118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C1 STATION 879 LONG 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-2 FIG 5. 2L74 4F RT4A25 20031219000832003121900083NE 2003 12 19 2003UALA00911 220031130A7261 OIL COOLER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 ENGINE FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29850UA 1653 FLIGHT DIVERTED DUE TO LOSS OF OIL IN NUMBER 1 ENGINE. FUEL COOLED OIL COOLER FAILED AND ALLOWED THE OIL TO ESCAPE INTO THE FUEL SIDE OF THE COOLER. REPLACED FCOC PER AMM 79-21-43. 2L72 4F4 FRTA28NM E40NE 20031219000862003121900086NM 2003 12 19 2003UALA00914 120031126A3350 BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29510UA 24780 FIRST CLASS EEL LIGHTS TURN OFF AFTER 1 MINUTE. REPLACED POWER SUPPLY & BATTERY PACK M732. 2L72 4F4 FRTA2NM E17NE 20031219000872003121900087NM 2003 12 19 2003UALA00915 120031130A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29508UA 24744 LEFT EXTERNAL FUSELAGE SKIN, BS 600 ABOVE STR 18L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER EVA MOC1-8454. 2L72 4F4 FRTA2NM E17NE 20031219001142003121900114NM 2003 12 19 03FDEA02059 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001252003121900125GL 2003 12 19 03FDEA02070 220031205A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C 30018GL NR 1 FAILED A FDEAA UNSCHED LANDING EJMVIBRATION/BUFFET WARNING INDICATION OVER TEMP CLCLIMB 1 SO25310FE 48299 530356 AT LEVEL OFF FL 330 EXPERIENCED HARD THUMP FOLLOWED BY GRINDING VIBRATION. IMMEDIATELY SHUT NR 1 DOWN. FOLLOWED QRH PROCEDURES, LANDED KPHX. PHX U C/W MD10-30 WORK CARD 71T0101-1, AND 71T0701-1. 2L73 4F4 F A22WE A23EA 20031222000372003122200037SO 2003 12 22 C2XA03TY207 120031209A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 ON CREW PREFLIGHT, REPORTED THAT THE EMERGENCY SIDE WALL LIGHT WAS OUT. MAINTENANCE FOUND THE CANNON PLUG LOOSE TO AN INVERTER, RESECURED THE CANNON PLUG ON THE INVERTER ASSY LOCATED LEFT SIDE, JUST AFT OF ST14513.6, OPERATIONAL CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2L72 4F RTT00011AT 20031222000612003122200061WP 2003 12 22 ASAA0380630 120031011A53105936038501 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, AFT CARGO BAY DOOR BEAM IS CORRODED IN SEVERAL PLACES. REPLACED DOOR BEAM PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20031222000952003122200095NM 2003 12 22 USAA030236 120031001A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU36295 27145 FOUND FLOORBEAM CORRODED 24 INCH, BS 700, LBL 50 CABIN FLOOR LEVEL. REPAIRED FOR TYPICAL REPAIR 53-15-01. CORROSION LEVEL 1. (M) 2L72 4F RTA2NM 20031222001172003122200117NM 2003 12 22 AMTA200301392 120031114A2612 TERMINAL BOEING757 75723N 1384973NM FIRE WARNING SHORTED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11524AT 30233 STATUS MSG (R TURB OH DET 2) DISPLAYED. FOUND A PIECE OF SAFETY WIRE SHORTING ACROSS THE TERMINALS OF OVERHEAT DETECTION SWITCH. REMOVED WIRE. OPS CHECK GOOD IAW FIMM 26-13-00. (M) 2L72 4F RTA2NM 20031222001242003122200124NE 2003 12 22 MEX2003539 220031128A72615007436C PUMP BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE NR 2 ENGINE OIL FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803AM 26268 AIRCRAFT RETURNED TO GATE DUE TO LOW OIL PRESSURE INDICATION ON NR 2 ENGINE DURING STARTING. SYSTEM WAS VERIFIED AND THE OIL PUMP WAS REPLACED IAW MM 79-21-04, TESTS WERE PERFORMED IAW MM 71-00-00, ALL OK. DURING THE OVERNIGHT SERVICE. THE ENGINE WAS VERIFIED BY LEAKAGES AND ITS RESPECTIVE PARAMETERS IAW MM 71-00-00, ALL OK. (M) 2L72 4F4 FRTA2NM E17NE 20031222001282003122200128NM 2003 12 22 AMTA200301407 120031120A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11526AT 30735 EGRESS FLOOR LIGHT INOPERATIVE AT ROW 5. CONNECTED LOOSE WIRE AS NEEDED, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20031222001402003122200140EA 2003 12 22 COMA0360540 120031204A2410 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA IDG ILLUMINATED A COMAC ABORTED TAKEOFF JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01458CA 7613 FLIGHT 5159 IDG AND GENERATOR NR 2 CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20031223000012003122300001NM 2003 12 23 03FDEA02159 120031209A2933EA1093A2408 TRANSMITTER BOEING727 727200 138407ENM HYD QTY IND MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 SO25489FE8242 6031 21492 DESCENDING THRU FL190, HYDRAULIC SYSTEM -A- QUANTITY INDICATED ZERO (PRESSURE GOOD AT 3000 PSI). COMPLIED WITH QRH. AFTER 15 MINUTES AND BEING LEVEL AT 12,000 FOR OVER 5 MINUTES. HYD SYSTEM -A- QUANTITY SLOWLY BEGAN MOVING TO 6.0 GALLONS AND THEN 5.5 GALLONS. MANUAL GEAR EXTENSION WAS COMPLETED PER QRH. REMOVED AND REPLACED SYSTEM -A- HYD QTY TRANSMITTER REF 29-33-001-4, OPS CHECK GOOD. 2L73 4F RTA3WE 20031219000492003121900049NM 2003 12 19 P5CA0301003 120031207A2410 CSD BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 4 ENGINE LEAKING A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP23354MC 23394 517287 NR 4 ENGINE CSD LIGHT ON. CSD DISCONNECTED. TRANSFERRED TO DMI 31912 PER MEL 24-1 1A CSD AND GENERAL REMOVED PER MM 24-11-00. 2L74 4F4 FRTA20WE E23EA 20031219000552003121900055WP 2003 12 19 UPS03841638 120031118A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C1 INTERCOSTAL WAS BROKEN BETWEEN STATION 500-520 BETWEEN LONG 33R AND 34R. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5750726 AND SRM 51-1-21. 2L74 4F RT4A25 20031219000612003121900061WP 2003 12 19 UPS03841644 120031118A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE NICKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, FRAME IS NICKED BEYOND LIMITS AT STATION 620 LONG 35L-35R. BLENDED AREA, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED DOUBLER, FILLER AND STRAP IAW DC8-53A-011,DC8-5310-11728-A 2L74 4F RT4A25 20031219000622003121900062WP 2003 12 19 UPS03841645 120031118A53205616520217N INTERCOSTAL DOUG DC8 DC871F 302199DWP DOOR FRAME CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, CARGO DOOR CUTOUT INTERCOSTAL IS CORRODED BEYOND LIMITS STATION 558 LONG 33R. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5616520 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20031219000652003121900065WP 2003 12 19 CALA0300699 120031205A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716806 49260 INSPECTION FOUND A 1.25 INCH CRACK IN TAIL COMPARTMENT LONGERON 2L AT STA 1418. THE CRACK WAS LOCATED AT BELTFRAME FASTENER. THE CRACKED END OF LONGERON WAS CUT OFF AND A NEW END WAS SPLICED ON IAW SRM 53-02, FIGURE 18 AND ECRA 5311-01132. 2L72 4F A6WE 20031219000712003121900071SO 2003 12 19 C2XA03CL198 120031207A21004504113 APU EMB 145 EMB145LR 3260212SO AFT FUSELAGE SMOKE A C2XAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW27159124439 145439 CREW REPORTED THAT ON TAXI OUT THE LAV SMOKE INDICATION CAME ON EICAS AND FLIGHT ATTENDANT REPORTED SMOKE IN AFT CABIN. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE APU. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20031219000932003121900093NM 2003 12 19 2003UALA00921 120031129A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29375UA 24640 STA 967-986.5 CREASE BEAM AT R2 DOOR HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2L72 4F4 FRTA16WE E2GL 20031219000952003121900095NM 2003 12 19 2003UALA00923 120031201A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29375UA 24640 FRAME CRACKED AT INNER CHORD JUST BELOW FLOOR AT STA 616 L&R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031219000992003121900099NM 2003 12 19 2003UALA00928 120031201A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29785UA 26954 EMERGENCY LIGHT INOPERATIVE AT SEAT 2F AFT POSITION. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20031219001122003121900112NM 2003 12 19 03FDEA02056 120031205A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION ON STRINGER BS 1166 STR 24 RT. REMOVED CORROSION & FOUND OUT OF LIMITS. REPAIRED STRINGER BS 1166, STRINGER 24 RT PER SRM 53-10-3 AND 53-10-1. 2L73 4F RTA3WE 20031219001152003121900115NM 2003 12 19 03FDEA02060 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. OUTBOARD FLAP OUTBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001202003121900120NM 2003 12 19 03FDEA02065 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORRODED. LT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73352, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001212003121900121NM 2003 12 19 03FDEA02066 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT POINT, SPOT FACE CORRODED. LT WING OUTBD FLAP INBOARD HINGE (FLAP SIDE) INBD PIVOT POINT, SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348, WINGS. TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001262003121900126NM 2003 12 19 03FDEA02085 120031207A5340 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 3 BANJO FITTING (AJC7053-503) FWD FACE FLANGE FOUND WITH 08 EA LOCK BOLT COLLARS CRACKED. 2L73 4F RTA22WE 20031219001342003121900134NM 2003 12 19 03FDEA02115 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031117001012003111700101WP 2003 11 17 MWEA030407 120031007A5320591768629 STIFFENER DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 SKIN TO FRAME AT STATION 1474, STIFFENER ABOVE ELEVATOR ACCUMULATOR ACCESS DOOR CRACKED AT AFT FASTENER. FABRICATED AND INSTALLED STIFFENER. 2L72 4F4 F A6WE E2EA 20031118000162003111800016WP 2003 11 18 UPS03841359 120030929A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 EMERGENCY EXIT LTS INOPERATIVE. REMOVED AND REPLACED EMERG EXIT LTS BATTERY PACK. OPS CK GOOD IAW MM CH 33-50. P/N 60-1223-5, S/N ON 350, S/N OFF 10385, P/N OFF 5708458-503 2L74 4F RT4A25 20031118000442003111800044EU 2003 11 18 AWXA200301159 120030924A5320D53472188200000 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF UPPER LEG OF Y1162 LONGITUDINAL BEAM FR 68-69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y1162 BEAM FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM PER DWG D53472188; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 25, 39-41. 2L72 4F RTA28NM 20031118000552003111800055EU 2003 11 18 AWXA200301170 120030924A5350D5323022620000 PLATE AIRBUS320 A320232 3930326EU FAIRING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MINOR REPAIR - DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON LT WING TO BODY FAIRING SUPPORT STRUCTURE CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CLOSING PLATE AT FR 34, AND U-CHANNEL ABOVE CLOSING PLATE; FABRICATED A NEW REPLACEMENT CLOSING PLATE AND U-CHANNEL, INSTALLED REPAIR PARTS IAW A320 SRM 53-25-11 PG 5-7. 2L72 4F RTA28NM 20031118000722003111800072CE 2003 11 18 CVU2003F00000 120030920A3710442CW PUMP BEECH 80 65B80 1152812CE LYC O720 IO720A1B 41546EA RT ENGINE VACUUMFAILED E CVUAO OTHER O OTHER NRNOT REPORTED 1 WP1344MA 833 LD412 PUMP FAILED UNDER NORMAL OPERATING CONDITIONS (VFR DAY). 1L72 3O3 O 3A20 1E15 20031118001172003111800117NM 2003 11 18 AWXA200301193 120030912A5321144533045 FLOOR PANEL BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK CABIN FLOOR PANEL M-5 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 144N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1. 2L72 4F4 FRTA2NM A12EU 20031119000052003111900005NM 2003 11 19 DHL2003743015 120031008A33501000679 BATTERY BOEING727 727225 1384077NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOPERATIVE ON PREFLIGHT. REMOVED AND REPLACED LIGHT BATTERIES, OPS GOOD IAW M/M 33-50-01. 37007-001 BATS. 2L73 4F A3WE 20031119000072003111900007NM 2003 11 19 250TR0025 120031001A5754 SKIN BOEING737 7372K5 138448XNM NR 1 SLAT DELAMINATED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 137 22597 NR 1 LEADING EDGE SLAT FOUND DELAMINATED. REPLACED NR 1 LEADING EDGE SLAT ASSY PER MM 27-81-21. 2L72 4F RTA16WE 20031119000172003111900017WP 2003 11 19 UPS03841374 120030920A5712 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RIGHT WING LE. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, RT WING LE RIBS ARE CRACKED AT XFS 610 AND XFS 616.25. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILL TERMINATES CRACKS,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 57-2-0 FIG. 2 2L74 4F4 FRT4A25 E2GL 20031119000202003111900020WP 2003 11 19 UPS03841378 120030922A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE MAIN CABIN WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, SEAT TRACK IS WORN BEYOND LIMITS BETWEEN STA. 480-500 AT LBL 24. REMOVED WORN SEAT TRACK STA. 470 -530, FABRICATED AND REPLACED SEAT TRACK SECTION IAW DC8-5320-5167-C,AND DC8-53B-003 2L74 4F4 FRT4A25 E2GL 20031119000222003111900022NM 2003 11 19 DHL2003784005 120031007A52106937418502 ROLLER BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE PAX DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01767AT 22001 AFTER TAKEOFF MAIN ENTRY DOOR HAD LARGE PRESSURE LEAK TILL DIFF REACHED 3.1 CABIN RATE OF CLIMB WAS 1+ TILL DOOR RESEATED. REPLACED MAIN ENTRY DOOR AFT UPPER AND LOWER ROLLER CAM CRANKS P/N 69-37418-502 AND ROLLERS FOR THE SAME PN KRP139805VT IAW BMM 52-11-01. ADJUSTED L-1 DOOR IAW B727 M/M 52-11-01. OPS AND LEAK CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20031119000312003111900031NE 2003 11 19 MWEA030413 220031010A7421CH347601 IGNITER BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LT ENGINE INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31904ME 55168 13363 LT ENGINE FAILED TO START. REMOVED AND REPLACED A & B IGNITOR PLUGS. 2L72 4F4 FTRA6WE E00061EN 20031119000592003111900059NE 2003 11 19 PCAA0310121 220031010A7532 VALVE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RT ENGINE STICKING A PCAAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 EA13846EX234534733 326 121297 CREW REPORTED THAT WHILE IN CRUISE FLIGHT THE NR 2 ENGINE HAD CAUSED A VIBRATION AND THE OIL PRESSURE DROPPED TO 40 PSI. THE NR 2 ENGINE WAS SHUT DOWN, AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED A STICKING P3/2,5 AIR SWITCHING VALVE AND REPLACED THE PROPELLER SHAFT SEAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031119000802003111900080WP 2003 11 19 MWEA030423 120031013A53305924802509 DOUBLER DOUG DC9 DC981 3022081WP STA DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 TWO EACH DENTS ARE NOT WITHIN THE CRITERIA AT STATION 447 LONGERON 15 LEFT. FABRICATED AND INSTALLED DOUBLER, CLIP AND FILLER IN SKIN. 2L72 4F A6WE 20031119000862003111900086NM 2003 11 19 AWXA200301206 120031011A2913 PUMP BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 2 ENGINE INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28183AW 22650 ON CLIMB OUT OF PHX EN ROUTE FOR SJC LOST (A) SYS HYDS, TURNED BACK TO PHX & LANDED WITHOUT EVENT. MAINT R & R NR 2 EDP IAW T/C R5M29001. R & R (A) HYD SYS CASE DRAIN, PRESSURE, & RETURN FILTERS, FLUSHED SYSTEM IAW BMM 29-11-0, PG. 204. LEAK AND OPERATIONAL CHECK OF (A) HYD SYS WAS GOOD. CONFIRMED FAILURE OF EDP. VISUAL INSPECTION OF UNIT FOUND INTERNAL DRIVE SHAFT DAMAGED DUE TO BEARING FAILURE, PRETEST NOT ACCOMPLISHED. TEARDOWN OF UNIT FOUND O-RINGS HARD SET & WORN, CYLINDER BARREL, NOSE & FACE SEALS, HOLD DOWN & WEAR PLATES, PISTON & SHOE SUB ASSY DAMAGED BY BEARING FAILURE, & HANGAR TRUNNIONS, STROKING & RATE PISTONS, AND SPRING 195 WORN BEYOND LIMITS. REPLACED DAMAGED PARTS, MAINT & TEST ACCOMPLISHED. 2L72 4F4 FRTA16WE E2EA 20031119000922003111900092NM 2003 11 19 AWXA200301212 120031011A7730AC69674 SOLENOID VALVE AIRBUSA319 A319132 3930340NM NR 1 ENGINE LOOSE A AWXAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP28805AW6866 1049 DURING CLIMB OUT OF CMH EN ROUTE FOR LAS RECEIVED NR 1 ENGINE SYSTEM FAULT AT 6000 FT, EGT AT 617 DEGREES, PLACED NR 1 ENGINE THRUST LEVER TO IDLE AND MAINTAINED 567 DEG EGT UNTIL LANDING AND SHUTDOWN. MAINTENANCE FOUND THE 10TH STAGE BLEED SOLENOID VALVE BOTTOM PLATE LOOSE AT CONNECTOR, REMOVED AND REPLACED 10TH STAGE BLEED SOLENOID VALVE IAW AMM 75-23-52, ALSO REPLACED IGNITION RELAY BOX. OPS CK NR 1 ENG GOOD, NO DEFECTS NOTED. FUNCTIONAL CHECK OF IGNITION BOX S/N 2151 WAS NO FAULT FOUND, UNIT TESTED GOOD UNDER ALL TEMPERATURES. VENDORS FUNCTIONAL TEST OF 10TH STAGE BLEED SOLENOID VALVE CONFIRMED FAILURE OF UNIT. PISTON SEALS FOUND WORN & PISTON SEALING SURFACE WAS DAMAGED BEYOND REPAIR. 2L72 4F RTA28NM 20031119001022003111900102SO 2003 11 19 C2XA03CL174 120031013A335074441 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715932 145015 CREW REPORTED A CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE CABIN EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031119001072003111900107WP 2003 11 19 IXXA0300061O 120031012A3260 UPLOCK SENSOR DOUG DC8 DC862 3021970WP MLG CONTAMINATED A IXXAO OTHER N FALSE WARNING APAPPROACH 1 SW11728PL846652797 45918 ON APPROACH, WITH ALL 3 MLG'S DOWN AND LOCKED, BOTH (DOOR NOT LATCHED, GEAR NOT LATCHED) LIGHTS WERE ILLUMIN, ALSO AUDIBLE WARNING HORN. GEAR WAS RECYCLED TWICE, THIS CORRECTED PROBLEM. MAINT INSPECTED LANDING GEAR, GEAR DOOR WARNING SYS. NO DEFECTS WERE NOTED. MAINT THEN PERFORMED TEST OF LANDING GEAR DOOR POSITIONS AND WARING SYS IAW ALL APPLICABLE MANUALS. THEY CLEANED ELECTRICAL CONNECTORS AT NOSE AND MAIN GEAR UPLIMIT SWITCHES, LUBED NOSE, MAIN GEAR UPLATCH MECHANISMS. UNABLE TO DUPLICATE PROBLEM ON GROUND. REVIEW OF LOG NOTED A/C HAD BEEN WASHED AT PREVIOUS STATION. SUSPECT MOISTURE RELATED PROBLEM. ALL SWITCHES INSPECTED, ANY MOISTURE REMOVED. SYS OPS CHECK NORMAL ON GROUND. A/C WAS RETURNED TO SERVICE.2L74 4F 4A25 20031119001242003111900124NM 2003 11 19 2003UALA00753 120031006A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 LWR FUSELAGE SKIN DENTED AT STA 927 BELOW STR 20L. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031119001252003111900125EU 2003 11 19 2003UALA00755 120031007A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29422UA 503 ROWS 21ABC AND 19ABC EEL LIGHTS ARE INOPERATIVE. REPLACED EEL LIGHTS. 2L72 4F4 FRTA28NM E40NE 20031118001052003111800105NM 2003 11 18 AWXA200301181 120030918A5320141N827145 PAN BOEING757 7572S7 1384962NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK 3 EACH CRACKS WERE FOUND AT MOUNT HOLES ON EXTERNAL POWER PANEL PAN ASSEMBLY BS 419. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY CRACK ENDS; STOP DRILLED CRACKS; RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACKS CONTAINED; PERFORMED WELD REPAIR IAW AWA ER 19-5316-03265-SS2. 2L72 4F RTA2NM 20031119000192003111900019WP 2003 11 19 UPS03841377 120030924A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE MAIN CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, SEAT TRACK IS CORRODED BEYOND LIMITS AT STA. 1325 LBL. 50. REMOVED SEAT TRACK SECTION STATION 1270 TO 1470, FABRICATED AND INSTALLED SEAT TRACK SECTION DC8-5320-8309 2L74 4F4 FRT4A25 E2GL 20031119000282003111900028EA 2003 11 19 WVE2003F00015 120030908A5280CC670105723 RIB CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE LT MLG DOOR CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09610QX 10033 LT MAIN GEAR DOOR LOWER DOOR ASSY. MOST INBOARD CROSS MEMBER RIB PN CC670-105723 IS CRACKED APPROX. 3 INCHES FROM AFT END OF WEB AREA. POSSIBLE STRESS RELIEF CRACK IN RIB AREA, DUE TO AIR LOAD ON DOOR. BEEF UP RIB PN CC670-10572-3 FOR LEFT HAND GEAR DOOR TO CARRY AIR LOAD. (EA092003F00015) 2L72 4F4 FRTA21EA E15NE 20031119000292003111900029WP 2003 11 19 0301899868 120031008A5754 BEARING DOUG DC9 DC951 3022051WP SLAT CARRIAGE LACK OF LUBE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01777NC 47787 DURING APPROACH FOR LANDING AFTER SLATS WERE SELECTED TO EXTEND, THE FLIGHT CREW NOTICED THE AIRCRAFT ROLLING AND ONE SLAT DID NOT EXTEND. THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND COM PROCEDURES WERE FOLLOWED. LANDING AT DTW WAS UNEVENTFUL. MAINTENANCE FOUND THE RIGHT SLAT CARRIAGE ROLLER BEARINGS DRY. LUBED BEARINGS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20031119000512003111900051NM 2003 11 19 CALA0300584 120031010A5320 SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A 3INCH CRACK IN NOSE WHEEL WELL RETRACT ACTUATOR SUPPORT TEE WEB AT STA 233. A WEB REPAIR WAS INSTALLED IAW SRM 51-70-13. 2L72 4F RTA16WE 20031119000902003111900090 2003 11 19 AWXA200301210 420031011A2565DHE1141 DETECTOR AIRBUSA319 A319132 3930340NM R-2 DOOR INOPERATIVE A AWXAO OTHER S AFFECT SYSTEMS NRNOT REPORTED 1 WP28825AW 1527 FLIGHT CREW REPORTED R-2 DOOR SLIDE NOT ARMED ON LOWER ECAM, SLIDE INDICATED ARMED AT DOOR. MAINTENANCE REMOVED AND REPLACED R-2 DOOR ARMING HANDLE PROXIMITY SWITCH (7WN2), ADJUSTMENT AND OPERATIONAL CHECK C/W IAW AMM SUBTASK 52-71-00-820-002. 2L72 4F RTA28NM 20031119001322003111900132NM 2003 11 19 2003UALA00764 120031007A3350 BATTERY PACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29318UA 23950 SECTION OF EEL LIGHTS INOP FROM SEATS 3ABC TO 9ABC. REPLACED BATTERY PACK AND INVERTER. 2L72 4F4 FRTA16WE E2GL 20031119001452003111900145NM 2003 11 19 QXEA200301233 120030924A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 PDX- LEFT HAND WING NR 4 FLAP TRACK HAS CORROSION ON INBOARD AND OUTBOARD SIDES OF TRACK. REPAIRED IAW HORIZON AIR EA 2-57-235. 2H72 4T RTA13NM 20031119001462003111900146NM 2003 11 19 QXEA200301234 120030925A5410 TRUSS DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 PDX- THREE CHAFE MARKS ON BOTTOM SIDE OF UPPER NR 1 ENGINE TRUSS 26 INCHES AFT OF FORWARD ATTACH POINT. REPAIRED IAW DHC-8 RD 8-54-036. 2H72 4T RTA13NM 20031119001502003111900150 2003 11 19 SWIA200312486 420031002A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07212SW8608 8608 120276 F/O AUTO PILOT COMMAND BARS WENT DOWN (PITCH), ALSO ATTITUDE INDICATOR F/O SIDE SHOWED 15 DEGREES CLIMB. A/C FOLLOWED F/O COMMAND BARS AND PITCHED DOWN. DISCONNECTED A/P. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER APC 65B. OPS CHECK GOOD. 2L72 4T RTA31SO 20031120000012003112000001EA 2003 11 20 EON2003F00000 120030827A7120A39783B LOCK DHAV DHC2 DHC2* 2800108EA PWA R985 R985* 52008NE ENGINE FRACTURED E EONAO OTHER O OTHER NRNOT REPORTED 1 AL03622301234 707 DURING THE 100 HOUR COMPRESSION TEST, THE ENGINE STOPPED BETWEEN TWO POSITIONS OF APPROXIMATELY 60 DEGREES OF PROP ROTATION FROM HARD INTERNAL CONTACT, FURTHER INVESTIGATION REVELLED THAT THE LOCK BAR ON THE NR 4 ROD LINK PIN HAD FRACTURED AND ALLOWED THE ROD PIN TO BACK OUT OF THE MASTER ROD. THE LOCKED CONDITION WAS CAUSED BY THE ROD PIN CONTACTING THE COUNTER WEIGHT. FURTHER INVESTIGATION FOUND THE LOCK BAR FOR THE ROD LINK PINS ON CYLINDERS 6 AND 7 HAD ALSO FRACTURED WITH NO PIN MIGRATION NOTED. NO PROBABLE CAUSE, NOW. 1H71 3R3 R A806 5E1 20031120000022003112000002SO 2003 11 20 SWIA200312487 120030904A5411 DOOR FRAME EMB 120 EMB120ER 3260203SO NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07218SW 120287 LEFT GEAR, FORWARD OUTBOARD DOOR NACELLE FRAME CHANNEL DENTED AND CRACKED BY DOOR TENSIONER. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT GEAR, FORWARD OUTBOARD DOOR NACELLE FRAME CHANNEL BY DOOR TENSIONER WITH A SERVICEABLE UNIT IAW SRM 51-10-02. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031120000232003112000023NM 2003 11 20 AWXA200301232 120030922A53206546812109 STRAP BOEING737 737301 1384611NM SUBFLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CENTER SUBFLOOR PAN UPPER STRAP AT BS 1006-1029, LBL 5 TO RBL 5, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SUBFLOOR PAN UPPER STRAP AT BS 1006-1029, LBL 5 TO RBL 5, WL 208; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-05, FIG 4. 2L72 4F RTA16WE 20031120000242003112000024NM 2003 11 20 AWXA200301233 120030920A5311651630086 FRAME BOEING737 737301 1384611NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD LT SIDE CHORD AT WL 207. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD LT SIDE CHORD AT WL 207; FABRICATED A NEW REPLACEMENT SIDE CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3-4, & 38, FIG 8, AND 51-40-05, FIG 3. 2L72 4F RTA16WE 20031120000402003112000040NM 2003 11 20 AWXA200301249 120030921A532069468314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 360, STR 4 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 360, STR 4 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-46831; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11 PG 1 & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031120000422003112000042NM 2003 11 20 QXEA200301238 120030928A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 BELLY SKIN HAS ROCK CHIP/SCRATCHES AT STATION X313.500, Z81.6 & Y2.1. REPAIRED IAW DHC-8 SRM 51-00-06. 2H72 4T RTA13NM 20031120000432003112000043NM 2003 11 20 QXEA200301239 120030928A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 BELLY SKIN HAS ROCK CHIP/SCRATCH AT STATION X364.5, Z90.0 & Y5.5. REPAIRED IAW DHC-8 SRM 53-00-16 AND 51-00-06. 2H72 4T RTA13NM 20031120000512003112000051SO 2003 11 20 SWIA200312499 120031008A27206225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07583SW8537 8537 120351 STICKING IN RUDDER PEDALS. REPLACED RUDDER SERVO IAW MM 22-10-05. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031120000632003112000063NM 2003 11 20 QXEA200301252 120030929A5340 STANCHION DHAV DHC8 DHC8202 2809007NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 LEFT HAND STANCHION LUG IS DAMAGED OR DENTED AT INBOARD FORWARD RADIUS OF LUG AT AFT END OF NR 6 SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-784. 2H72 4T RTA13NM 20031120000652003112000065NM 2003 11 20 QXEA200301254 120030929A5340 STANCHION DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 RIGHT HAND CARGO BAY STANCHION LUG HAS NICKS AND SCRATCHES .5 INCH FORWARD OF STACHION LUG ON NR 9 SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-784. 2H72 4T RTA13NM 20031120000672003112000067NM 2003 11 20 QXEA200301256 120030930A5753 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 RIGHT HAND WING OUTBOARD FLAP UPPER SURFACE IS CHAFED AT INBOARD END. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-51 AND RD 8-57-1734. 2H72 4T RTA13NM 20031120000682003112000068NM 2003 11 20 QXEA200301257 120030928A5753 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 ON INBOARD END OF THE LEFT HAND OUTBOARD FLAP THE UPPER SKIN HAS A CHAFED AREA AND A GOUGE AREA 2.5 INCHES FROM INBOARD END. REPAIRED IAW DHC-8 SRM RD 8-57-1734 AND 8-57-464. 2H72 4T RTA13NM 20031120000762003112000076NM 2003 11 20 QXEA200301264 120031001A1430 RIVET DHAV DHC8 DHC8202 2809007NM ZONE 400 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 EIGHT RIVETS ON TOP FORWARD NACELLE JUST AFT OF TOP FORWARD MOUNT ARE LOOSE AND STICKING UP. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20031120000802003112000080EU 2003 11 20 MALA030455 120031009A5320 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN CWA, CORROSION FOUND ON FRAME 294 RBL14, AND LBL10. MAINTENANCE COMPLETED REPAIR IAW EO NR 53102. REFER TO LOG PAGE NR 195764 FOR DETAIL. A/C RELEASE DATE 10/12/03. 2L72 4T4 TRTA52EU E8NE 20031120000832003112000083EU 2003 11 20 MALA030458 120031010A5311 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN CWA, FRAME TOP AT STA 272 HAS CORROSION RT OF BL0. MAINTENANCE COMPLETED REPAIR IAW EO NR 53102. A/C RELEASE DATE 10/12/2003. REFER 409 NR 195719 FOR DETAIL. 2L72 4T4 TRTA52EU E8NE 20031120000892003112000089 2003 11 20 P5CA0300964 420031013A3431G692503 CONTROL PANEL BOEING747 747341 13848AMNM COCKPIT INOPERATIVE A P5CAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 WP23355MC 23395 ON PREFLIGHT, F/O'S VHF NAV PANEL LIGHTS INOP. REPLACED F/O'S VHF NAV CONTROL PANEL, TESTS NORMAL PER MM 34-31-01. 2L74 4F RTA20WE 20031120000912003112000091 2003 11 20 P5CA0300966 420031014A34142082051 INDICATOR BOEING747 7472U3B 1384846NM AIRSPEED FLUCTUATES A P5CAD RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 WP23923FT 22769 FIRST OFFICER'S BARBER POLE IN AIRSPEED INDICATOR FLUCTUATES, CAUSING MACH WARNING TO GO OFF. REPLACED A/S INDICATOR. 2L74 4F RTA20WE 20031120000962003112000096CE 2003 11 20 ZHE2003F00000 120030825A3240S116740124 HOSE CESSNA188 188B 2073007CE CONT O520 IO520* 17032SO BRAKE LEAKING G ZHEGO OTHER K FLUID LOSS NRNOT REPORTED 1 SW115647G 18801129 BRAKE HOSE HAD HOLE IN IT, HAD SIGN OF CHAFING FROM UNKNOWN OBJECT. 1L71 3O3 O A9CE E5CE 20031120001112003112000111NM 2003 11 20 AWXA200301252 120031007A3150 WARNING SYSTEM BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE COCKPIT MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28306AW 24633 ON TAKEOFF ROLL AT GEG EN ROUTE FOR PHX WITH THRUST LEVERS MOVING TOWARD TAKEOFF THRUST, THE TAKEOFF WARNING CONFIGURATION WARNING HORN SOUNDED, REJECTED TAKEOFF LESS THAN 60 KTS. FLAPS AT 1, TRIM SET AT 4.8, SPEED BRAKE WAS DOWN, PRIOR TO LOW SPEED ABORT TAPPED ON SPEED BRAKE HANDLE, HORN STILL SOUNDED. MAINTENANCE PERFORMED A TAKEOFF WARNING SYSTEM TEST IAW T/C A1B31009, SYSTEM CHECK WAS GOOD, COULD NOT DUPLICATE PROBLEM. 2L72 4F4 FRTA16WE E2GL 20031120001122003112000112NM 2003 11 20 SWAA032453 120031106A53306545835 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT AFT EDGE OF COOLING FAN EXHAUST. REPAIRED PER EA. 2L72 4F RTA16WE 20031120001262003112000126NM 2003 11 20 AWXA200301451 120031106A532065528941 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN FLOOR SUPPORT CHANNEL ON UPPER AFT LEG AT INBOARD END, BS 540, LBL 0.5, WL 207.85. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT CHANNEL FROM BS 540 TO BS 560, LBL 0.5; INSTALLED NEW REPLACEMENT CHANNEL IAW SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20031121000102003112100010NM 2003 11 21 SWAA032460 120031106A5315141A5170 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 1017 BL 0 - RBL 30. REPLACED UPPER CHORD PER ER. 2L72 4F RTA16WE 20031121000342003112100034NE 2003 11 21 COMA0360501 220031117A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT OVERTEMP A COMAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO01927CA13102 7031 807526 FLIGHT 5075 RIGHT ENGINE WOULD NOT ACHIEVE CLIMB THRUST WITHOUT OVER TEMPING. REPLACED RIGHT ENGINE. 2L72 4F4 FRTA21EA E15NE 20031121000422003112100042WP 2003 11 21 0302029959 120031006A5330 SKIN PANEL DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01919RW 47162 DURING SPECIAL VISIT FOR INSPECTION OF BELLY SKINS CORROSION WAS FOUND ON SKIN PANEL BETWEEN BS 110-134 L27L TO L29R. REPAIRED PER EA 99-196522. 2L72 4F A6WE 20031121000442003112100044NM 2003 11 21 SWAA032516 120031113A53116546547 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND 4 EA FUSELAGE FRAMES CRACKED AT BS 827, STR 9R, BS 867, STR 9R, BS 867, STR 9L, AND BS 360, STR 8R. REPAIRED FRAMES PER BFG ER. 2L72 4F RTA16WE 20031121000692003112100069EA 2003 11 21 COMA0360496 120031111A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01427CA 7460 FLIGHT 5579 DURING CLIMBOUT OF TRI RECEIVED A GEAR DISAGREE WARNING MESSAGE, AIRCRAFT RETURNED TO THE FIELD. ADJUSTED THE NOSE LANDING GEAR PROXIMITY SWITCH. 2L72 4F RTA21EA 20031121000852003112100085NM 2003 11 21 CALA0300649 120031117A5510 BUSHING BOEING737 737524 1384721NM HORIZONTAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711651 28912 INSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD LUG HAD CORROSION AFT BUSHING. REMOVED AND REPLACED BUSHINGS ON LT HORIZONTAL STABILIZER FWD UPPER IAW SRM 55-10-10. 2L72 4F RTA16WE 20031121000862003112100086NM 2003 11 21 CALA0300650 120031118A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2761304 23355 INSPECTION FOUND A 5 INCH CRACK IN FUSELAGE BELLY SKIN AFT OF E&E COOLING DUCT AT BS 380, S28L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5330-02894. 2L72 4F RTA16WE 20031124000122003112400012SO 2003 11 24 SWIA200312599 120031116A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER KF FLUID LOSS FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07237SW8653 8653 120314 GREEN HYDRAULIC SYSTEM LOST ALL FLUID AFTER LANDING. NOTICED ASSOCIATED ALARMS AND LIGHTS. REPLACED RIGHT OUTBOARD ACTUATOR IAW AMM 27-53-05. OPS AND LEAK CHECKED GOOD. 2L72 4T RTA31SO 20031124000142003112400014 2003 11 24 SWIA200312601 420031109A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER MALFUNCTIONED A SWIAO OTHER P NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07295SW5388 5388 120322 F/O SIDE CLACKER IS INOP. REPLACED F/O'S SIDE STICK SHAKER. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031219001372003121900137NM 2003 12 19 03FDEA02118 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001422003121900142NM 2003 12 19 03FDEA02125 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED. AREA REPAIR CARRIED OUT AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001672003121900167NM 2003 12 19 QXEA200301504 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 2 SEAT TRACK HAS LITE SURFACE CORROSION ON TOP OF RAILS AND IN THE BOTTOM OF CHANNEL FROM 7 TO 10 INCHES AFT OF STATION X445. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20031219001682003121900168NM 2003 12 19 QXEA200301505 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 2 SEAT TRACK HAS LITE SURFACE CORROISON ON TOP OF RAILS FROM X434 TO 4 INCHES AFT OF X434. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20031219001762003121900176 2003 12 19 MALA030522 420031205A2350 RADIO SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15414XJ 340B414 DURING FLT 3177 CREW REPORTED RADIO DEAD SPOTS WHEN TRANSMITTING ON COMM NR 1 OR 2 FROM CAPT OR F/O'S SIDE. AIR RETURN TO MSP. MAINTENANCE REMOVED & REPLACED REU P/N ON/OFF 5170-1-9, S/N ON 223, S/N OFF 221. REU OPS CHECK GOOD IAW SF340 MM CHAPTER 23. ALSO REMOVED & REPLACED CAPT'S HEADSET. OPS CHECK GOOD IAW SF340 MM CH 23. P/N ON H10-30, P/N OFF H10-40. 2L72 4T RTA52EU 20031219001782003121900178EU 2003 12 19 MALA030526 120031130A7933522794 DETECTOR SAAB SF340 340B 7860101EU LT ENG OIL FLUCTUATES A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15363PX 340B260 DURING FLIGHT 3268, LEFT ENGINE OIL TEMPERATURE FLUCTUATING BETWEEN 100-148C. OIL PRESSURE READING NORMAL. WHILE INFLIGHT, PILOT NOTED TEMPERATURE DROPPED DOWN TO NORMAL RANGE THEN WENT BACK TO READING HIGH. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE OIL TEMP DETECTOR P/N 522794, S/N OFF EGNAB468, OPS CHECK GOOD IN THE GROUND ALL IAW SAAB MM 79. 2L72 4T RTA52EU 20031219001802003121900180EU 2003 12 19 MALA030524 120031208A30103D238162 EJECTOR VALVE SAAB SF340 340B 7860101EU DEICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15364PX 340B262 DURING FLIGHT 2741, DURING FLIGHT THE LEFT I/B DEICE BOOT WOULD NOT INFLATE WITH THE AUTO CYCLE SWITCH SELECTED. THE TIME LIGHT WOULD COME ON, THE TIMER LIGHT WOULD ALSO ILLUMINATE PRESSING THE MANUAL BOTTON AFTER SEVERAL ATTEMPTS. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LEFT I/B LOWER EJECTOR VALVE IAW AMM 30-10-31-4. P/N 3D2381-62, S/N OFF 161, S/N ON N1432. OPS CHECK GOOD OF I/B BOOTS CHECKS GOOD. 2L72 4T RTA52EU 20031217001402003121700140NM 2003 12 17 SWAA032652 120031201A575365C35703 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED C2 CHECK, FOUND DELAMINATION AT RT WING O/B FORE FLAP UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20031217001542003121700154CE 2003 12 17 DXTA200300198 120031214A3260 WARNING LIGHT CESSNA560 560XL 2076702CE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07622QS 5605286 AFTER TAKEOFF OUT OF IAD FOR BCT, WITH GEAR HANDLE SELECTED UP GOT GEAR UNLOCKED WARNING LIGHT BUT GEAR STAYED DOWN. ACCOMPLISHED AIR TURNBACK TO IAD AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20031217001672003121700167NM 2003 12 17 DHL2003742501 120031120A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CABIN STRINGER 15 RT CRACKED STA 736D. REMOVED FASTENERS AS REQUIRED FOR ACCESS STRINGER 15R STA 736D IAW B-727 SRM 51-30-2. CUT OUT DAMAGED END OF STRINGER 15R DIM 7 INCHES AND FABRICATED ONE U-CHANNEL DIM 1 INCH X 1 INCH X 1 INCH X 4 INCH USING 7075 T6 .040 PO 900226 AND TWO EACH CHIMS 1 INCH X 1 INCH AND 1 INCH X 2.5 INCH USING 2024 T3 .080 PO 900103 IAW B-727 SRM 53-10-3 FIG 5. TREATED, ALODINED AND PRIMED ALL PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIRS IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20031217001682003121700168NM 2003 12 17 SWAA032642 120031203A212121520 FAN BOEING737 7372H4 138448CNM FWD CARGO COMP FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29073SW 22673 GASPER FAN CB TRIPPED, HAD BAD ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F A16WE 20031217001922003121700192 2003 12 17 SWIA200312611 420031118A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07234SW7439 7439 120308 F/O ADI SHOWS COMPUTER FLAG. AUTO PILOT DOES NOT ENGAGE ON F/O SIDE. REPLACED APC-65B. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031218000292003121800029SO 2003 12 18 SWIA200312624 120031102A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07567SW 120342 RT FRAME 9 SKIN SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REWORKED RIGHT SIDE FRAME 9 PER SB NR 120-53-0073 REV 00 DATED 21 JUL 99. 2L72 4T RTA31SO 20031218000372003121800037SO 2003 12 18 C2XA03SH475 120031126A531014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031218000802003121800080NE 2003 12 18 2003UALA00861 220031116A7230 COMPRESSOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 ENGINE DAMAGED A UALAO OTHER R PARTIAL RPM/PWR LOSS APAPPROACH 1 WP29840UA 1522 NUMBER 2 ENGINE COMPRESSOR STALLS WHEN OPERATED ABOVE IDLE. UPON ENGINE TEARDOWN SIGNIFICANT DAMAGE WAS FOUND TO THE FRONT OF THE HIGH PRESSURE COMPRESSOR, WHICH CAUSED THE ENGINE TO EXPERIENCE A COMPRESSOR STALL WHEN ADVANCED ABOVE IDLE POWER. SIGNIFICANT BIRD REMAINS WERE FOUND INSIDE THE ENGINE. 2L72 4F4 FRTA28NM E40NE 20031218001142003121800114NM 2003 12 18 2003UALA00903 120031125A3350 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT ILLUMINATED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29827UA 1022 EMERGENCY LIGHTS SYSTEM TEST FAILS WITH MESSAGE EPSU INT LOAD EMERGENCY L DISPLAYED. RESET SYSTEM C-B'S AND EMERGENCY LIGHTS PER MM 33-51-00. TESTS NORMAL. 2L72 4F4 FRTA28NM E40NE 20031218001172003121800117NM 2003 12 18 2003UALA00908 120031125A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29370UA 24539 AFT CARGO COMPT SHEAR TIE CRACKED BS 747 RBL 32. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20031219000202003121900020NE 2003 12 19 COMA0360528 220031203A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT LEAKING A COMAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SO01987CA14716 7199 807502 RT ENGINE LOW OIL PRESSURE WARNING DURING T/O. REPLACED THE RIGHT ENGINE. 2L72 4F4 FRTA21EA E15NE 20031219000412003121900041SO 2003 12 19 C2XA03SH484 120031206A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031219001462003121900146NM 2003 12 19 03FDEA02129 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. REMOVED CORROSION AS PER EA 1-5750-73351, WINGS, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001712003121900171NM 2003 12 19 QXEA200301519 120031207A5554 HINGE DHAV DHC8 DHC8202 2809007NM ZONE 300 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 SMALL GOUGES ON AFT RUDDER LOWER HINGE BRACKET UNDERSIDE OF LOWER TANG AT ATTACH POINT FOR FORWARD/AFT INTERCONNECT ROD. REPAIRED IAW DHC-8 RD 8-55-132. 2H72 4T RTA13NM 20031219001732003121900173NM 2003 12 19 QXEA200301523 120031201A5753 FLAP TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 LEFT HAND OUTBOARD FLAP FRONT SPAR FITTINGS AT FLAP TRACK NR 4 IS CHAFED. REPAIRED IAW Q400 RD 8/4-57-228. 2H72 4T RTA13NM 20031222000072003122200007EU 2003 12 22 AWXA200301519 120031123A5414D54530052203 SKIN AIRBUS320 A320232 3930326EU NR 2 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 DURING C-06 CHECK, CORROSION WAS FOUND ON OUTBOARD SKIN OF NR 2 PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED CORRODED SKIN PANEL FROM NAC STA 8370 TO NAC STA 9782, OUTBOARD; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG D54530052; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 1. 2L72 4F RTA28NM 20031222000232003122200023NM 2003 12 22 F3LA200300160 120031205A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 294.5, RBL 38.5. FABRICATED AND INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. 2L72 4F RTA16WE 20031222000242003122200024WP 2003 12 22 AALA20031403 120031208A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217539A 49993 SAT ALL EMERGENCY LIGHTS INOPERATIVE DUE TO COCKPIT EMERGENCY LIGHTS SWITCH LEFT IN ON POSITION OVERNIGHT. REPLACED ALL EMERGENCY BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031222000332003122200033SO 2003 12 22 C2XA03IA110 120031204A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2729906 145472 DURING PREFLIGHT INSPECTION THE CREW FOUND A CABIN EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFFECTED EMERGENCY LIGHT ASSEMBLY AND OPERATIONALLY CHECKED THE LIGHT. 2L72 4T RTT00011AT 20031222000342003122200034SO 2003 12 22 C2XA03TY206 120031208A554112007244001 SPAR EMB 135 EMB135ER 3260203SO RUDDER CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727506 145206 DURING A SCHEDULED INSPECTION DAMAGE WAS FOUND ON THE RUDDER 1 AFT SPAR. MAINTENANCE ACCOMPLISHED A SPLICE REPAIR IAW EC 5540-01022 AND EMB CPM 51-21-04/05, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031222000382003122200038NM 2003 12 22 F3LA200300164 120031205A5320 ANGLE BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND 3 NUT PLATES BELOW MOP SILL, STA 344-360, LBL 60. REPLACED REINFORCING ANGLE UNDER L-1 MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20031222000512003122200051WP 2003 12 22 ASAA0380618 120031007A532199365531 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS SEVERAL WATER DAMAGED INSERTS AT FS 218-256. REPLACED FLOORBOARD IAW SRM 53-05. (M) 2L72 4F RTA6WE 20031222000522003122200052WP 2003 12 22 ASAA0380619 120031007A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS DELAMINATED IN TWO PLACES BETWEEN FS 465-541. REPLACED FLOORBOARD IAW SRM 53-05. (M) 2L72 4F RTA6WE 20031222000582003122200058WP 2003 12 22 ASAA0380608 120031007A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, FLOOR SUPPORT CORRODED AT FS 1098-1193. REPLACED FLOOR TRACK PER SRM 51-30-1, 51-10-2, 51-10-4, AND 51-10-3. (M) 2L72 4F RTA6WE 20031222000712003122200071WP 2003 12 22 AALA20031033 120030919A4920 APU DOUG DC9 DC982 3022082WP AFT FUSELAGE DAMAGED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW217546A 53028 AIRCRAFT EN ROUTE ORD TO YYC, CREW OBSERVED SMOKE IN THE CABIN THAT WOULD NOT DISSIPATE. AIRCRAFT RETURNED TO ORD. REPLACED APU PERFORMED PACK BURN OUT AND CHANGED COALESCER BAGS. LEAK CHECKED AND SYSTEM GROUND CHECKED NORMAL. (M) 2L72 4F A6WE 20031222000762003122200076WP 2003 12 22 2003F00650 120030815A532039178521 FITTING DOUG DC9 DC915F 3022037WP ENTRY DOOR CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 FOUND 4C CHECK SERVICE, CARGO CABIN ENTRANCE DOOR, BEAM NR 4 END FITTING CRACKED FITTING PN 3917852-1. FITTING WAS REPLACED BY A NEW ONE. (M) 2L72 4F A6WE 20031222000842003122200084NM 2003 12 22 AMTA200301421 120031123A2150 A/C PACK BOEING757 75733N 1384931NM RIGHT INOPERATIVE A AMTAO OTHER J WARNING INDICATION DEDESCENT 1 GL11560TZ 33525 RT PACK QUIT ON DESCENT WOULD NOT RESET. PERFORMED BITE OF THE RT PACK CONTROLLER, NO FAULTS SYS, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20031222000942003122200094NM 2003 12 22 USAA030238 120031103A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU59971 22204 FOUND FRAME CRACKED 1 INCH, BS 680 BETWEEN S21L AND S22L. INSTALLED DOUBLER IAW EA 94697. (M) 2L72 4F RTA2NM 20031222001012003122200101WP 2003 12 22 AALA20030826 120030802A49205940405503 APU DOUG DC9 DC982 3022082WP AFT ODOR A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21445AA 49471 JUST AFTER TAKEOFF STRONG ODOR IN COCKPIT AND THEN CALLS FROM CABIN INDICATED ODOR AND SMOKE DEVELOPING. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. DISCOVERED APU HYDRAULIC FLUID INGESTION. REMOVED AND REPLACED APU. REPLACED WATER SEPARATOR SOCKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031222001062003122200106WP 2003 12 22 AALA20030901 120030821A2910 O-RING DOUG DC9 DC983 3022083WP HYD SYSTEM LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21562AA 49344 AFTER TAKEOFF DURING GEAR RETRACT, RT HYDRAULIC PRESSURE LOW LIGHT CAME ON, GEAR DOOR OPEN LIGHT CAME ON AND HYDRAULIC QUANTITY DROPPED TO ZERO. CREW DECLARED AN EMERGENCY AND RETURNED WITHOUT FURTHER INCIDENT. REPLACED RUDDER SHUTOFF VALVE O-RING AND PLUG AND SERVICED SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031217002092003121700209EA 2003 12 17 SWIA200312616 120031123A32347179015 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG MALFUNCTIONED A SWIAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 NM07409SW2 2 7056 NOSE DOOR OPENED AT 20,000 FT. GEAR DISAGREE MESSAGE AND PROX SENSOR FAIL MESSAGE. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. OPS CHECK GOOD IAW MM 32-31-01. 2L72 4F4 FRTA21EA E15NE 20031218000152003121800015NM 2003 12 18 MWEA030459 120031125A361032049941 ISOLATION VALVE BOEING717 717200 1383700NM ENGINE NOT OPENED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31907ME 55171 ISOLATION VALVE WOULD NOT OPEN TO START ENGINE. PERFORMED FAULT ISOLATION TEST, NO FAULTS NOTED. OPERATIONS CHECK GOOD. 2L72 4F TRA6WE 20031218000392003121800039SO 2003 12 18 C2XA03SH477 120031126A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712528 145504 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031218000602003121800060EU 2003 12 18 033293091 120031125A3350 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27309UE 41022 DURING INSPECTION THE RIGHT AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNED OUT AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031218000662003121800066EA 2003 12 18 QXEA200301482 120031125A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 LIGHTING STRIKE BURN MARK AT FUSELAGE STATION 173.00 ON THE MATING SURFACE FOR PANEL 211AL. REPAIRED IAW CRJ SRM 53-00-01. 2L72 4F RTA21EA 20031218001082003121800108NM 2003 12 18 2003UALA00896 120031124A5414 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29645UA 25280 NR 2 PYLON OUTBOARD SIDE, FWD TORQUE BOX, NACELLE STA 240 AND WL 150, EXTERIOR SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SIDE SKIN WITH DOUBLER-TRIPLER PER SRM 54-53-01. 2L72 4F4 FRTA1NM E24NE 20031218001282003121800128EU 2003 12 18 MALA030520 120031120A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION. CABIN AFT LT AISLE SEAT TRACK AT STA 575 TO STA 686 HAS GOUGES. MAINTENANCE RECEIVED NEW SECTION OF SEAT TRACK, CUT, TRIMMED, ALODINED AND PRIMED, INSTALLED NEW SECTION OF SEAT TRACK IAW MESABA EO NR A53060 DATED 11/3/03. A/C RELEASE DATE 12/2/03. REFER 409 NR 1206073 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20031218001392003121800139NM 2003 12 18 QXEA200301496 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 11 SEAT TRACK HAS CORROSION ON INSIDE AT STATION X486.45, 466.45 AND 454.45. REPAIRED IAW DHC-8 SRM 51-20-16, 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031124000192003112400019NM 2003 11 24 QXEA200301460 120031104A5514 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 300 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 LEFT HAND AILERON OUTBOARD TIP HAS HOLE IN FIBER. REPAIRED IAW DHC-8 SRM 51-20-61, 51-30-70, 51-20-26 AND 57-60-71. 2H72 4T RTA13NM 20031124000242003112400024NM 2003 11 24 03FDEA01938 120031113A5710 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE INBOARD FLANGE FACE CORRODED (WING SIDE). LT O/B FLAP INBD HINGE FITTING LOWER MOUNT BOLT HOLE I/B FLANGE FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 NAD DWG ARC0502. 2L73 4F RTA22WE 20031124000322003112400032NM 2003 11 24 QXEA200301418 120031105A49304503139B FUEL CONTROL BOMBDRDHC8 DHC8401 1390041NM APU LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09407QX4624 4623 4049 APU DRIPPING FUEL CONTINUOUSLY FROM DRAIN WHEN STARTED. REMOVED AND REPLACED APU FUEL CONTROL ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031124000332003112400033NM 2003 11 24 AWXA200301423 120031111A278125EN556 SWITCH BOEING737 7373Y0 1384671NM LE FLAPS FALSE INDICATIONA AWXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 WP28323AW 23684 ON DESCENT INTO GEG EN ROUTE FROM PHX FLAPS WOULD NOT COME DOWN, CHECKED CIRCUIT BREAKER, NONE WERE TRIPPED, LOWERED FLAPS USING ALTERNATE FLAP OPERATION. AFTER CONSULTING MAINTENANCE RAISED FLAPS USING ALTERNATE SYSTEM, THEN RESET THE LEADING EDGE & TRAILING EDGE CIRCUIT BREAKERS, FLAP EXTENSION OPERATED NORMALLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM PER T/C F1B27016; OPERATIONAL CHECK WAS GOOD. A FOLLOW-UP WAS WRITTEN AND WHEN AIRCRAFT RETURNED TO PHX 11/13/2003 THE WIRING WAS TROUBLESHOT FROM E11 RACK TO SWITCH S138, AND MAINTENANCE REPLACED SWITCH S138 IAW BMM 31-26-12, OPERATIONAL CHECK OF SYSTEM WAS GOOD. 2L72 4F RTA16WE 20031124000372003112400037SO 2003 11 24 C2XA03TY196 120031116A532014523461003 GUSSET EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 DURING A SCHEDULED 3C INSPECTION THE GUSSET ON THE RT FLOORBEAM FOR PANEL 247AF WAS CORRODED. MAINT REMOVED OLD GUSSET AND FAB A NEW GUSSETT. ALODINED, PRIMED AND INSTALL NEW FAB GUSSET IAW EMB 135/145 SRM 51-40-04 AND 51-40-06, CPM 51-21-04-05-06 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISH AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031124000382003112400038WP 2003 11 24 IXXA0300071O 120031108A36101944302 HEAT EXCHANGER DOUG DC8 DC871F 302199DWP PNEU SYS FAILED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11822BX868355 45813 DURING CLIMB FROM KGSO TO KTOL NR 2 ENGINE PNEUMATIC SYSTEM OVERHEATED WITH LOW OR HIGH STAGE BLEED AND PACK FLOW AT MIN. CREW RETURNED TO KGSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 PRECOOLER PER ALL APPLICABLE MANUALS. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20031124000472003112400047NM 2003 11 24 03319410 120031115A3350321430 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27410FJ 3165 DURING INSPECTION THE EMERGENCY LIGHTING SYSTEM AT ROWS 6-8 WERE FOUND INOPERATIVE. THE BATTERY WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031124000542003112400054NM 2003 11 24 03FDEA01898 120031110A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 FWD LWR CARGO FRAME IS DENTED AT STA 600, STR 24L. REMOVED AND REPLACED DAMAGED FRAME SECTION BS 600, STR 21L TO STR 25L PER SRM 51-30-2. 2L73 4F RTA3WE 20031124000562003112400056NM 2003 11 24 03FDEA01902 120031111A5531 SPAR BOEING727 727200 138407ENM VERTICAL STAB CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 VERTICAL STAB STRINGER 7 CHAFED UNDER AFT CORNER OF ACCESS PANEL 9601. REPAIRED DAMAGE TO LT VERTICAL FIN MID SPAR AT FIN STA 229 PER SRM 55-30-06 FIGURE 3. 2L73 4F RTA3WE 20031117000522003111700052NM 2003 11 17 DHL2003749500 120030924A5730 SKIN BOEING727 7272J0 138407ENM LT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C CHECK, SKIN DENT LT WING L/E AT LEADING EDGE STA. 130 ( ABOVE IB EDGE OF NR 3 LE FLAP ). CUT-OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .040 P.O. NR 90024 DIM 2.5 INCH X 1.5 INCH AND DOUBLER FROM 2024 T3 .050 P.O. NR 90096 DIM. 6.5 INCH X 6 INCH IAW B-727 SRM 57-30-4 FIG. 5. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED I.A.W. B-727 SRM 57-30-4 FIG.5. 2L73 4F RTA3WE 20031117000552003111700055EA 2003 11 17 COMA0360445 120031005A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA FLAP FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01458CA 7613 FLIGHT 5821 FLAPS FAILED AT 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031117000642003111700064NM 2003 11 17 DHL2003749505 120030919A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE PUNCTURED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C CHECK, RT SIDE FUSELAGE STA. 1340 AIRSTAIR CUTOUT HOLES PUNCTURED IN SKIN. CUT-OUT DAMAGED SKIN AND FABBED FILLER FROM 2024 T3 .050 14.6250 INCH AND 12.2500 INCH AND DOUBLERS FROM 2024 T3 .063. 1250 INCH X 4.5 INCH X 5.5 INCH X 4.2500 INCH IAW B-727 SRM 53-30-3 FIG. 3. 2) CUTOUT DAMAGED LWR ANGLE AND FABBED NEW FROM 7075 T6 P.O. NR 9911868 .080 DIM. 12 INCHES X 5 INCHES AND 2 EA. SLICE ANGLES FROM SAME MAT. DIM. 7.2500 X 4.2500 EACH I.A.W. B-727 SRM 51-40-4 FIG. 1. 3) ALL PARTS TREATED AND PRIMED I.A.W. B-727 SRM 51-10-2 AND INSTALLED I.A.W. B-727 SRM 53-30-3 FIG. 3 AND 51-40-4 FIG. 1. 2L73 4F4 FRTA3WE E2EA 20031117000682003111700068SO 2003 11 17 C2XA03SH370 120031007A531014522460015 BUTTSTRAP EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031117000812003111700081NM 2003 11 17 P5CA0300960 120031005A7931 INDICATOR BOEING747 747236B 1384804NM PWA JT9 JT9D7Q 52054NE OIL PRESSURE MALFUNCTIONED A P5CAK NONE R PARTIAL RPM/PWR LOSS ININSP/MAINT 1 WP23924FT 21730 702031 OIL PRESSURE LIGHT NR 3 ENG FLICKED WITH CORRESPONDING FLUCUATION OIL PRESSURE. CLEANED, INSPECTED CONNECTOR CHECKED OIL FILTER FOR OBSTRUCTIONS AND NO DEFECTS FOUND. ALL INDICATIONS CHECKED NORMAL. 2L74 4F4 F A20WE E3NE 20031117000842003111700084SW 2003 11 17 ALG2003F00091 120030823A77209009000102 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL MGT MALFUNCTIONED E ALGAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW03537AL 53230 CAE847257 IN CRUISE FLIGHT, EXCEDENCE ON MGT WITH CHECK INSTRUMENT LIGHT DURING CRUISE WITH INSTRUMENT INDICATOR IN THE GREEN (704 TO 714). THE MECHANIC CHECKED COMPUTER FOR EXCEDENCE, HAD NO EXCEDENCE OR FAULTS RECORDED, REPLACED INDICATOR MGT. 1G71 3U3 UO H2SW E1GL 20031117000962003111700096NM 2003 11 17 DHL2003749512 120030920A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK AT FLIGHTSTAR IN JACKSONVILLE, FL., AFT PIT SUPPORT FROM STA 950 E TO 990 RBL 6 HAS SEVERAL DENTS. REMOVED AFT PIT FLOOR SUPPORT FROM 950E TO 990 RBL 6 IAW B-727 SRM 51-30-2. DRILLED NEW FLOOR SUPPORT PO 328319 P/N BAC 1500-6199 DIMENSION 5FT 10 INCHES AS PER SAMPLE IAW B-727 SRM 51-20-1. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED NEW FLOOR SUPPORT IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20031117000972003111700097NM 2003 11 17 DHL2003749513 120030920A5320 FLOOR SUPPORT BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE DENGED DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C CHECK, PIT FLOOR SUPPORT FROM STA. 950E TO STA. 990 RBL 14 HAS SEVERAL DENTS. CUT-OUT DAMAGED AREA AND FABBED FILLER FROM 7075 T6 .050 P.O. NR 9912793 DIM. 1.7500 INCH X 1INCH AND DOUBLER FROM 7075 T6 .063 P.O.NR 9912793 DIM. 6 INCHES X 2.500 INCHES IAW B-727 SRM 53-10-2 FIG. 8 AND 51-40-3 FIG. 1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-40-3 FIG. 1. 2L73 4F4 FRTA3WE E2EA 20031117000982003111700098NM 2003 11 17 DHL2003749514 120030924A5730 SKIN BOEING727 7272J0 138407ENM LEFT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK, SKIN DENT LT WING LEADING EDGE AT LEADING EDGE STA 130 (ABOVE I/B EDGE OF NR 3 L/E FLAP). CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .040 PO 90020 DIM 2.5 X 1.5 INCHES AND DOUBLER FROM 2024 T3 .050 PO 90096 DIM 6.5 X 6 INCHES IAW B-727 SRM 57-30-4 FIG 5. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 57-30-4 FIG 5. 2L73 4F RTA3WE 20031117000992003111700099WP 2003 11 17 MWEA030405 120031007A5313591140516 LONGERON DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGWE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 LONGERON 3 LT HAS A CRACK AT STATION 160. FABRICATED AND INSTALLED REPAIR SPLICE AND LONGERON SECTION. 2L72 4F4 F A6WE E2EA 20031117001022003111700102WP 2003 11 17 MWEA030408 120031007A5313593643611 LONGERON DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 LONGERON 12 RIGHT AT STATION 1309 IS CRACKED AT LOWER FRAME ATTACH FASTENER. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPAIR SPLICE AND INSTALLED REPLACEMENT LONGERON. 2L72 4F4 F A6WE E2EA 20031118000042003111800004NM 2003 11 18 CALA0300578 120031008A5347 SEAT TRACK BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 910-927. THE SEAT TRACK WAS REMOVED AND REPLACED USING SPLICES AND FILLER IAW SRM 53-00-52, FIGURE 204. 2L72 4F4 FRTA16WE E2GL 20031118000052003111800005 2003 11 18 DXTA200300135 420030923A34252888011 CDU CESSNA560 560XL 2076702CE PWA 545 PW545A NE COCKPIT INOPERATIVE E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07621QS 5605280 DURING FLIGHT FMS CIRCUIT BREAKER TRIPPED AND ELECTRICAL ODOR WAS PRESENT IN COCKPIT. - INSPECTED COCKPIT AND FOUND CDU INOPERATIVE, REPLACED UNIT IAW WITH CESSNA 560XL MM CHAPTER 34-10-00. 2L72 4F4 FRTA22CE E00059EN 20031118000132003111800013WP 2003 11 18 UPS03841353 120031002A3350 LIGHT DOUG DC8 DC873F 302199FWP EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 NR 2 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY DISARM/ARM SWITCH ASSY. SWITCH TESTS OK. 2L74 4F RT4A25 20031118000182003111800018NE 2003 11 18 150094 220031008A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE RIGHT MALFUNCTIONED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 GL17340SZ 340A004 401 DRG189789 FLIGHT 4580 BED-TTN. DURING TAKEOFF ROLL AFTER CTOT WAS ENGAGED THE CREW FELT THE RT ENGINE SURGE AND NOTICED THE RT TORQUE INDICATION WAS AT 120 PERCENT. THE CREW IMMEDIATELY RETARDED THE POWER LEVERS AND ABORTED THE TAKEOFF. TORQUE WAS AT 120 PERCENT FOR APPROXIMATELY 2-3 SECONDS. A/C RETURNED TO GATE IN BED AND TAKEN OUT OF SERVICE 10-08-03 AT 1543(LT). 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040108001092004010800109EU 2004 1 8 KBM2003F00059 120031013A6220704A33633208 THRUST BEARING SNIAS 350 AS350B1 8680811EU MAIN ROTOR DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 RED ELASTOMERIC BEARING DISBONDED BEYOND LIMITS. INSTALLED 3 EACH SERVICEABLE SPHERICAL THRUST BEARINGS. 1G71 3U H9EU 20040108001442004010800144EU 2004 1 8 KBM2003F00078 120031022A6220350A37112602 BUSHING SNIAS 350 AS350B2 8680813EU SCISSORS WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 ROTATING SCISSOR LINK BUSHING WORN. INSTALLED SERVICEABLE SCISSOR LINK BLOCK.(K) 1G71 3U H9EU 20040108001522004010800152NM 2004 1 8 AMTA200301252 120030923A5330 DOUBLER BOEING727 72723 1384004NM FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 FUSELAGE SKIN EXTERNAL REPAIR DOUBLER DENTED. REPAIRED SKIN IAW MFG ER 03-3497.(K) 2L73 4F A3WE 20040108001612004010800161EA 2004 1 8 FF22003F00000 220031101A7200 ENGINE BEECH 90 C90 1152913CE PWA PT6 PT6A20 52043EA LEFT MAKING METAL B FF2RO OTHER O OTHER NRNOT REPORTED 1 SW1965KA LJ611 PCE2405152 DURING A PREFLIGHT INSPECTION, THE LT PROPELLER WAS FOUND TO BE SEIZED. THIS LED TO AN INSPECTION OF THE CHIP DETECTOR WHICH REVEALED METAL CHIPS. THE RT ENGINE CHIP DETECTOR WAS THEN INSPECTED. METAL CHIPS WERE ALSO PRESENT. BOTH ENGINES WERE REMOVED AND TAKEN FOR TEARDOWN. 1L72 3T3 T 3A20 E4EA 20040109000142004010900014SO 2004 1 9 Z372003F00002 220031023A8520 CRANKSHAFT CESSNA180 180 2072602CE CONT O470 O470R 17026SO MCAULY2A36C 2A36C18 GL ENGINE BROKEN B Z37EO OTHER O OTHER NRNOT REPORTED 1 GL014652B 31550 98976ORR PILOT FLEW A/C IN FOR GENERATOR REPAIR AND REPORTED TO MAINT THAT THE ENGINE WAS MAKING A CLUNKING NOISE. UPON FURTHER INVESTIGATION WITH A BORESCOPE THE CRANK SHAFT WAS FOUND TO BE BROKE AT APPROX. THE NR 6 PISTON CONNECTING ROD JOURNAL. ENGINE HAS NOT YET BEEN DISASSEMBLED FOR FURTHER FINDINGS.(K) 1H71 3O3 ONC5A6 E273 5 CP880 20031219000322003121900032EA 2003 12 19 SWIA200312634 120031128A2721601R515687 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07408SW 7055 ON DEPARTURE FROM BZN AT ABOUT 500 FT RUDDER TRIM DEFLECTED ALMOST FULL SCALE NR RUDDER TRIM SWITCH WAS ABLE TO BRING TRIM BACK TO LESS THAN 1/2 DEFLECTION. REMOVED AND REPLACED RUDDER/AILERON TRIM CONTROL PANEL. RUDDER TRIM SYSTEM OPS CHECK GOOD. P/N: 601R51226-23SW. 2L72 4F RTA21EA 20031219001042003121900104NM 2003 12 19 2003UALA00934 120031204A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29128UA 30023 EXTERNAL FUSELAGE SKIN HAS A BURN MARK AT BS 400 AND STR 11L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FILLER & DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20031219001162003121900116NM 2003 12 19 03FDEA02061 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. OUTBOARD FLAP OUTBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001272003121900127NM 2003 12 19 03FDEA02103 120031207A5340 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 02EA LOCK BOLT COLLARS CRACKED. 2L73 4F RTA22WE 20031219001332003121900133NM 2003 12 19 03FDEA02114 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001402003121900140NM 2003 12 19 03FDEA02121 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031222000152003122200015 2003 12 22 SWIA200312644 420031201A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07298SW6128 6128 120328 CAPTAINS FLIGHT DIRECTOR COMMAND BARS PITCH UP ABRUPTLY IN FLIGHT TO 20 DEGREES AND NOSE UP AND 20 DEGREES LEFT AND RIGHT TURN. INSTALLED SERVICEABLE AUTOPILOT COMPUTER ON CAPTS SIDE. OPS CHECK GOOD. 2L72 4T RTA31SO 20031222001132003122200113SO 2003 12 22 SIMA200330901 120031103A5347 SEAT TRACK EMB 135 EMB135LR 3260305SO COCKPIT DIRTY A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21734EK 145371 CAPTAIN REPORTED HIS SEAT LATCH DOES NOT REMAIN LATCHED, SEAT UNLATCHES AT TIMES BY ITSELF. COMPLIED WITH COCKPIT SEAT LOCKING PIN AND SEAT TRACK CLEANING AND LUBRICATION. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031222001192003122200119WP 2003 12 22 2003F00647 120030907A5340995510509 FITTING DOUG DC9 DC915F 3022037WP RT MLG WW CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 DURING 4 C CHECK, FOUND RT MAIN WHEEL WELL, Y STATION 577-727, FITTING CRACKED. THE DAMAGED PART WAS REPLACED BY A NEW ONE. (M) 2L72 4F A6WE 20031222001232003122200123NM 2003 12 22 AALA20031232 120031106A2910 LINE BOEING757 757223 1384957NM HYD SYSTEM LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21629AA 24587 EN ROUTE, LOST CENTER SYSTEM HYDRAULIC QUANTITY. LANDED WITHOUT INCIDENT. REPLACED 2 CENTER HYDRAULIC MODULE FLEX LINES AND SERVICED CENTER HYDRAULIC OIL QUANTITY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031222001272003122200127NM 2003 12 22 AMTA200301408 120031120A77117898301 TRANSMITTER BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE EPR MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CLCLIMB 1 GL11558TZ 32592 31858 DURING CLIMB LEFT ENGINE POWER FLUCTUATES. OPERATION WITH EEC OFF NOT CHECKED DURING CLIMB. CRUISE OPS NORMAL. ON DESCENT ENGINE UNSTABLE WITH EEC OFF. REMOVED AND REPLACED LEFT ENGINE EPR X-MITTER PER MM 77-11-01-4. OP CHECK GOOD. (M) 2L72 4F4 FRTA2NM E12EU 20031222001332003122200133EA 2003 12 22 COMA0360534 120031205A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23645 7031 THERE WAS A CRACKED OBLIQUE ANGLE AT FS 625.0, STR 14R AND WL 85. REMOVED CRACKED ANGLE. INSTALLED A NEW ANGLE IAW CRJ SRM 51-40-11 AND 51-42-21. 2L72 4F RTA21EA 20031223000142003122300014NM 2003 12 23 SWAA032656 120031203A33506574550 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20031223000182003122300018NM 2003 12 23 SWAA032650 120031202A3350311500 LENS BOEING737 7373H4 1384600NM OVERWING EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 RT OVERWING EXIT LIGHT LENS IS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20031223000262003122300026 2003 12 23 SWAA032629 420031201A2565 INDICATOR BOEING737 7377H4 1384404NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29790SW 30604 R2 DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031223000032003122300003NM 2003 12 23 AWXA200301521 120031208A29135718610 PUMP BOEING737 73733A 1384673NM NR 2 HYD SYS FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28175AW 23634 EN ROUTE FROM PHX TO PDX B-SYSTEM HYD OVERHEAT LIGHT ILLUMINATED, FOLLOWED CHECKLIST TO CLEAR DISCREPANCY, OVERHEAT LIGHT REMAINED ON, DIVERTED TO LAS. MAINTENANCE REMOVED AND REPLACED B-SYSTEM ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP IAW R4M29002 (PUMP WAS BORROWED FROM UAL IN LAX TWO DAYS EARLIER). FLUSHED HYDRAULIC SYSTEM AND REPLACED FILTERS IAW BMM 29-15-00, LEAK AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031223000052003122300005NM 2003 12 23 AWXA200301523 120031203A575365C2630936 DOUBLER BOEING737 737301 1384611NM RT WING FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON RT WING NR 6 FLAP TRACK FAIRING TRACK GUIDE DOUBLER AT WBL 204.4. MAINTENANCE REMOVED AND REPLACED THE RT WING NR 6 FLAP TRACK FAIRING TRACK GUIDE DOUBLER AT WBL 204.4 IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20031223000082003122300008EU 2003 12 23 03340319 120031206A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27319UE 41042 DURING INSPECTION THE EMERGENCY LIGHT AT SEAT 9A WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031223000372003122300037NM 2003 12 23 SWAA032640 120031130A1430BACB30LJ14438 BOLT BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND VERT FIN REAR SPAR ATTACH BOLTS (4 EA) CORRODED. REMOVED AND REPLACED BOLTS PER MM. 2L72 4F RTA16WE 20031223000592003122300059NM 2003 12 23 SWAA032680 120031208A53206919140 ANGLE BOEING737 7373A4 1384585NM FWD FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 178, WL 207, LBL 5. REPAIRED PER SRM. 2L72 4F RTA16WE 20031223000602003122300060 2003 12 23 SWAA032681 420031208A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND L2 ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED L2 SLIDE PER MM. 2L72 4F RTA16WE 20031223000632003122300063NM 2003 12 23 F3LA200300168 120031208A3260655825029 CIRCUIT CARD BOEING737 73736E 138443ANM MLG INDICATOR DAMAGED A F3LAO OTHER P NO WARNING INDICATION CLCLIMB 1 NM03316FL 1387 25264 FLIGHT CREW REPORTED RT RED GEAR LIGHT DID NOT ILLUMINATE IN FLIGHT. JACKED AIRCRAFT AND SWUNG GEAR. PERFORMED GEAR WARNING CHECK AND FOUND PROBLEM WITH CIRCUIT CARD M986, GEAR RED WARNING LIGHT. REPLACED CIRCUIT CARD M986, SWUNG GEAR AND OPS CHECKED NORMAL. 2L72 4F RTA16WE 20031223000852003122300085 2003 12 23 VNAA0312002 420031202A31407013348937 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07425JS6208 955 3037 DURING TAKEOFF, THE CREW RECEIVED A LEFT AND RIGHT HAND SHAKER FAIL AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031223000942003122300094NM 2003 12 23 SWAA032705 120031210A3350 LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED C3 CHECK, FOUND SEVERAL LIGHTS INOP ON EEPLS IN CENTER LOUNGE, AFT AND FWD GALLEY. RELAMPED EEPLS PERMM. 2L72 4F A16WE 20031219000812003121900081WP 2003 12 19 MWEA030476 120031208A52805914985537 DOOR DOUG DC9 DC982 3022082WP NLG NOISY A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31810ME 48072 AFTER GEAR RETRACTION, NOISE AND VIBRATION CONTINUED FROM NOSE WHEEL AREA. SUSPECT DOORS NOT FULLY CLOSED AND LOCKED AFTER FLIGHT CREW SECURITY INSPECTION PRIOR TO DEPARTURE. PERFORMED GENERAL VISUAL INSPECTION ON BOTH NOSE GEAR DOOR AND LATCHES, NO DAMAGE OF ANY KIND NOTED. CLOSED AND SECURED BOTH GEAR DOORS. 2L72 4F A6WE 20031219001572003121900157NM 2003 12 19 03FDEA02143 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. RT WING, O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73356 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031222000052003122200005NM 2003 12 22 AWXA200301517 120031208A2597 CIRCUIT BOARD AIRBUSA319 A319132 3930340NM FWD GALLEY ARCED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28829AW7846 37 1563 EN ROUTE FROM PHX TO DTW THE FLIGHT ATTENDANT OBSERVED A ELECTRICAL BURNING ODOR IN THE FORWARD GALLEY, NR 1 COFFEEMAKER CIRCUIT BREAKER WAS FOUND TRIPPED, BURNING ODOR DISSIPATED. ISSUED MEL 25-22-03, COND 1 COFFEEMAKER INOP. WHEN AIRCRAFT ARRIVED BACK IN PHX, MAINTENANCE REMOVED AND REPLACED THE NR 1 COFFEEMAKER IAW T/C R1D25303. VENDORS FUNCTIONAL TEST OF COFFEE MAKER S/N 5999 CONFIRMED FAILURE OF UNIT. TEARDOWN OF UNIT FOUND LOWER PC BOARD SHORTED, REPLACED LOWER PC BOARD, CLEANED AND TESTED UNIT IAW CMM 25-30-09, REV. 5. 2L72 4F RTA28NM 20031222000192003122200019EA 2003 12 22 SWIA200312648 120031202A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GROUND SPOILERS FAILED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07907SW 7511 OUTBOARD GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT STATUS MESSAGE ON GROUND. RETURNED TO GATE. REPLACED NR 1 SECU. OPS CHECKS GOOD IAW 27-00-00. P/N: 44-164-05, S/N OFF: 1244. 2L72 4F4 FRTA21EA E15NE 20031222000392003122200039EA 2003 12 22 03337664 120031203A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA DEFECTIVE A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA27664BR 7528 DURING OPERATION OF THE AIRCRAFT THE LAVATORY SMOKE MESSAGE WAS PRESENT INTERMITTENTLLY ON THE FLIGHT DISPLAYS. 2L72 4F RTA21EA 20031222000412003122200041NM 2003 12 22 ABXA030459 120031208A3260 WARNING SYSTEM BOEING767 767281 1385109NM MLG MALFUNCTIONED A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23786AX 23019 INFLT, COMPLETING AFTER TAKEOFF CHECKLIST, UPON MOVING GEAR LEVER TO OFF, EICAS MESSAGE GEAR DOOR AND AMBER DOOR LIGHT ILLUMINATED. PUSHED LOCK OVERRIDE AND RETURNED HANDLE TO UP POSITION. LIGHTS EXTINGUISHED. GEAR WAS CYCLED. COULD NOT VERIFY. INSPECTED MAIN AND NOSE GEAR DOORS FOR SECURITY. CHECKED PSEU FOR PROXIMITY SENSOR FAULTS AND TARGET TESTED, NEAR-FAR, BOTH MAINS AND NOSE PER AMM 32-09-04-4. NO FAULT FOUND. CHECKED LANDING GEAR POSITION INDICATION AND WARNING SYSTEM PER 32-61-00-5-11. CHECKED GOOD. 2L72 4F RTA1NM 20031222000552003122200055WP 2003 12 22 GTIA030953 120031124A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 EMERGENCY LIGHT IN TAIL COMPARTMENT BELOW WATER SEPARATORS HAS BROKEN WIRE. REPAIRED BROKEN WIRE TO EMERGENCY LIGHT IN TAIL COMPARTMENT, BELOW WATER SEPARATORS. OPS CHECK OK. (M) 2L72 4F A6WE 20031222001412003122200141EA 2003 12 22 COMA0360541 120031204A3260 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG DAMAGED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01967CA 1 7134 FLIGHT 5501 GEAR DISAGREE WARNING, NLG DID NOT RETRACT. NLG STRUT WAS INCORRECTLY SERVICED. RESERVICED STRUT AND RETRACT CHECK WAS SATISFACTORY. 2L72 4F RTA21EA 20031223000752003122300075NM 2003 12 23 AWXA200301526 120031125A532065C35652 WEB BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 LCQ - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FASTENER HEADS OF AFT CARGO DOOR THRESHOLD ALONG ENTIRE SURFACE, FORWARD CORNER 100 PERCENT EXFOLIATED MATERIAL LOSS INCLUDING UPPER STRAP, BS 807-847. MAINTENANCE REMOVED AFT CARGO DOOR THRESHOLD WEB, UPPER REINFORCEMENT STRAP, AND LOWER FORWARD AND AFT REINFORCEMENT STRAPS; FABRICATED A NEW REPLACEMENT UPPER REINFORCEMENT STRAP; INSTALLED REPAIR PART, AND REINSTALLED AFT CARGO DOOR THRESHOLD WEB AND LOWER FORWARD AND AFT REINFORCEMENT STRAPS IAW B737-300 SRM 51-40-02, PARA 5. 2L72 4F RTA16WE 20031223001012003122300101EA 2003 12 23 SWIA200312654 120031031A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07594SW 7285 FS 280 RIGHT FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ SRM 51-40-11 & RII 53-401. P/N: 601R31113-58. 2L72 4F RTA21EA 20031223001032003122300103EA 2003 12 23 SWIA200312656 120031031A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07594SW 7285 PULLEY INTERCOSTAL ANGLE CRACK AT STA 484 LBL 27 O/B. REPAIRED INTERCOSTAL ANGLE IAW CRJ REO 601R-53-41-059 & RII 53-401 ON LBL 27.0. P/N: 601R31171-17. 2L72 4F RTA21EA 20031223001112003122300111EA 2003 12 23 COMA0360546 120031208A27507455001 SELECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01420CA6055 7451 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR LEVER. 2L72 4F RTA21EA 20031223001252003122300125EU 2003 12 23 MALA030538 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 9B FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 9B IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001422003122300142CE 2003 12 23 DXTA200300188 120031127A2710666000161 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS BROKEN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07628QS 5605305 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001512003122300151CE 2003 12 23 DXTA200300191 120031126A2710666000162 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS BROKEN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07637QS 5605137 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001582003122300158EA 2003 12 23 A6WA200340169 120031116A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG FALSE ACTIVATIONA A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31401AW 7280 GEAR DISAGREE AFTER RETRACTION ON CLIMB-OUT. NO OTHER WARNINGS OR CAUTIONS. RAN CHECKLIST FOR GEAR UP DISAGREE. EXTENDED GEAR RECEIVED 3 GREEN LANDED AT 49400, NO OTHER PROBLEMS. PERFORMED OPS CHECKS IAW AMM 32-30-00. CYCLED GEAR NUMEROUS TIMES, COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME. CHECKED ALL PSEU INPUTS CODES, NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031223001622003122300162EA 2003 12 23 ASOA03547 120031029A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11862AS 7445 DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SPIDER DUCT BRACKET IN THE EQUIPMENT BAY IAW AMM 21-52-00. (M) 2L72 4F RTA21EA 20031223001632003122300163 2003 12 23 ASOA03548 420031029A31706229820009 DCU CNDAIRCL600 CL6002B19 1900309EA SMOKE DETECTION MALFUNCTIONED A ASOAO OTHER N FALSE WARNING CLCLIMB 1 SO11886AS1457 7531 DURING CLIMB-OUT FROM ABY-ATL, AT APPROXIMATELY 12,000 FEET THE CREW RECEIVED A SMOKE CARGO WARNING MESSAGE ACCOMPANIED WITH AURAL AND VISUAL INDICATIONS. THE MESSAGE LASTED APPROXIMATELY THREE TO FIVE SECONDS AND THEN EXTINGUISHED. THE CREW DID NOT ACTIVATE THE FIRE BOTTLES AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE SWAPPED AROUND THE NR 1 AND NR 2 DATA CONCENTRATOR UNITS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031223001682003122300168EA 2003 12 23 A6WA200340166 120031111A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31401AW 7280 RIGHT FUSELAGE SKIN AT STATION 379 STRINGER HAS LIGHTNING DAMAGE AND PREVIOUS REPAIR BLENDED IN EXCESS OF 10 PERCENT MATERIAL THICKNESS. CUT OUT DAMAGED SECTION OF FUSELAGE SKIN, FABRICATED REPAIR DOUBLERS FROM 2024 T3 .063 INCH WVAC PO NR 27603/1 AND INSTALLED IAW WVAC EO 601R-53-8386. (M) 2L72 4F RTA21EA 20031223001732003122300173EA 2003 12 23 ASOA03543 120031027A5320601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11862AS 7445 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20031223001812003122300181WP 2003 12 23 GTIA030832 120031006A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FORWARD CABIN STATION 200 TO 256 CENTER FLOORBOARD HAS SEVERAL INSERTS BROKEN OUT/CORRODED SOFT/MUSHEY AND DAMAGED ALL CORNERS. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031223001872003122300187WP 2003 12 23 GTIA030810 120030907A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND SEAT TRACKS RIGHT STATION 826 TO STATION 1307 BARE METAL, NICKS, LIGHT CORRODED, ALL THREE TRACKS. SEAT TRACK RBL 22 AND RBL 54 FROM 826 TO 1307 IS OUT OF LIMITS. REMOVED OUTBOARD SEAT TRACK STATION 826 TO 1307 RBL 54. REMOVED SEAT TRACK STATION 200 TO 1307 RIGHT INBOARD. DRILLED AND LOCATED HOLES IN SEAT TRACK FROM STATION 826 TO 1307 RBL 22. DRILLED AND LOCATED HOLES IN SPLICES. INSTALLED INBOARD SEAT TRACK AND SPLICES AT RBL 22 FS 826-1307. DRILLED AND LOCATED HOLES IN SEAT TRACK FROM STATION 1032-1307 RBL 54. FABRICATED SPLICES. INSTALLED SEAT TRACK AND SPLICES STATION 826-1307 RBL 54. (M) 2L72 4F A6WE 20031223001892003122300189WP 2003 12 23 GTIA030808 120030906A5310 BEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND AFT PIT DOOR BEAM CORRODED ENTIRE LENGTH. REMOVED AFT PIT DOOR BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW AFT PIT DOOR BEAM. (M) 2L72 4F A6WE 20031223002002003122300200WP 2003 12 23 GTIA030812 120030822A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND AFT PIT LOWER DOOR JAMB BEAM CORRODED. (M) 2L72 4F A6WE 20031224000182003122400018WP 2003 12 24 GTIA030756 120030908A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FOUND FORWARD CABIN STATION 200 TO 218 LBL 45 INCHES HAS CORROSION ON WEB, UNDER SEAT TRACK ATTACH. REMOVED CABIN WEB. FABRICATED WEB. INSTALLED CABIN WEB. (M) 2L72 4F A6WE 20031224000252003122400025WP 2003 12 24 AMTA200301443 120031201A3350 CONNECTOR LKHEED1011 10113853 5265020WP EMERGENCY LIGHT DIRTY A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 AFT EMERGENCY EGRESS GALLEY PATH LIGHTING INOPERATIVE. CLEANED AND RESECURED EGRESS LIGHTING AS REQUIRED. OPS CHECK GOOD. OK FOR SERVICE. (M) 2L73 4F A23WE 20031224000272003122400027NM 2003 12 24 USAASB03205 120031122A3350210310005 FUSE BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US 23992 BDL - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS, AT SEAT ROWS 10 AND 11ABC, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FUSE, AT STATION 598, ABOVE SEAT ROW 11 DEF. ALSO, REPLACED BATTERY PACK ASSEMBLY, P/N 2013-1A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031224000282003122400028WP 2003 12 24 AMTA200301444 120031201A3350 CONNECTOR LKHEED1011 10113853 5265020WP EMERGENCY LIGHT DIRTY A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 FORWARD GALLEY EMERGENCY PATH LIGHTING TO ROW 6 A/C RIGHT DIM. CLEANED AND RESECURED EGRESS LIGHTING AS REQUIRED. OPS CHECK GOOD. OK FOR SERVICE. (M) 2L73 4F A23WE 20031222000882003122200088WP 2003 12 22 AALA20031141 120031010A2120 CLAMP DOUG DC9 DC982 3022082WP CUSTOMER AIR DAMAGED A AALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW21408AA 49319 AIRCRAFT EN ROUTE, OBSERVED HIGH TEMPERATURE LIGHT COMING ON FOR TAIL COMPARTMENT. RETURNED TO LAND, LIGHT WENT OUT ON DESCENT AND LANDING. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. FOUND AIR LEAK AND REPLACED CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031222000972003122200097NM 2003 12 22 USAA030231 120031030A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU 22205 FOUND INTERCOSTAL CORRODED 2 INCHES BY 15 INCHES, CABIN FLOOR INTERCOSTAL AT LBL 24.75, BS 310.5-324. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER AMM SRM 51-10-2. CORROSION LEVEL 2, TASK NR C53-221-02. (M) 2L72 4F RTA2NM 20031222001102003122200110EU 2003 12 22 USAA030242 120031031A5310D5347047400300 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND SUPPORT PLATE CRACKED .62 INCH, FRAME 47/51 S39R FLOOR SUPPORT PLATE. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-72-11. (M) 2L72 4F RTA28NM 20031223000392003122300039NM 2003 12 23 SWAA032660 120031120A335090083 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SPECIAL VISIT FOUND EMERGENCY LIGHT IN FWD CABIN INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20031223000542003122300054NM 2003 12 23 SWAA032675 120031207A53116546538 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20031223001452003122300145CE 2003 12 23 DXTA200300186 120031126A2710666000161 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07695QS 5605293 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001972003122300197WP 2003 12 23 GTIA030821 120030930A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FLOORBOARD SUPPORT BROKEN AND CRACKED AT STATON 864 OVER CENTER WING TANK. REMOVED FLOORBOARD SUPPORT. FABRICATED NEW FLOORBOARD SUPPORT. INSTALLED NEW SUPPORT. (M) 2L72 4F A6WE 20031224000032003122400003WP 2003 12 24 GTIA030834 120031006A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FORWARD CABIN STATION 200 TO 256 LBL 21 TO LBL 44 FLOORBOARD HAS SEVERAL INSERTS BROKEN OUT/CORRODED SOFT/MUSHEY AND DAMAGE ALONG EDGE. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031224000312003122400031WP 2003 12 24 ASAA0380624 120031007A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOOR INSERTS ARE DAMGED, SOME BROKEN AND SOME PULLED, BETWEEN FS 1117 AND 1174. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031224000342003122400034WP 2003 12 24 ASAA0380627 120031011A54145930649503 SKIN DOUG DC9 DC983 3022083WP NACELLE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, LT ENGINE UPPER COWL IS CRACKED. REPAIRED PER EA 7110-01208 AND SRM 54-06. (M) 2L72 4F RTA6WE 20031224000452003122400045WP 2003 12 24 ASAA0380609 120031007A53219952521506 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, FLOOR PANEL HAS MULTIPLE CRACKS AND PUNCTURES ON BOTTOM SURFACE AT FS 796-826. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20031224000592003122400059NM 2003 12 24 2003F00660 120031115A3232274579 ACTUATOR BOEING757 757236 1384971NM RT MLG DOOR MALFUNCTIONED A P9RAO OTHER J WARNING INDICATION APAPPROACH 1 SO11522NA 25133 AFTER GEAR EXTENSION GOT GEAR DOOR LIGHT. AT POST FLIGHT INSPECTION, FOUND RIGHT MAIN GEAR DOOR DOWN, BLED ACTUATOR OF AIR AND PERFORMED OPS CHECK OF GEAR DOORS IAW BMM 32-12-10, ALL CHECKED NORMAL. (M) 2L72 4F RTA2NM 20031224000672003122400067NM 2003 12 24 VNAA0311008 120031121A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07423JS2545 14 3032 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031229000142003122900014NM 2003 12 29 SWAA032709 120031210A32601899 PROXIMITY SENSOR BOEING737 7372H4 138448CNM RT MLG INOPERATIVE A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29083SW 22732 RT MLG LIGHT SLOW TO EXTINGUISH (RED LIGHT) NO DIFFERENTIAL YAW. REMOVED AND REPLACED DOWNLOCK PROXIMITY SENSOR PER MM. 2L72 4F A16WE 20031229000152003122900015 2003 12 29 SWAA032710 420031211A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 L1 DOOR SLIDE OUT OF ADJUSTMENT. READJUSTED L1 SLIDE PER MM. 2L72 4F RTA16WE 20031229000222003122900022GL 2003 12 29 371PA0032 220031211A7321 O-RING BOEING737 737306 13844BGNM CFMINTCFM56 CFM563B1US GL FUEL CONTROL CUT A PIDAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO05371PA 23543 FUEL LEAKING UNDER NR 2 ENGINE. FOUND LOW IDLE ADJUSTMENT O-RING CUT. REPLACED O-RING. LEAK CHECKS OK DURING TEST NR 4, IDLE SPEED CHECK, PER MM 71-00-00. OPS CHECKS OK. 2L72 4F4 FRTA16NE E2GL 20031229000242003122900024EA 2003 12 29 COMA0360550 120031210A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS INTERMITTENT A COMAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO01783CA 7315 FLIGHT 5416 FLIGHT SPOILER FAULT MESSAGE. RESET SPOILERS - COULD NOT DUPLICATE FAULT. 2L72 4F RTA21EA 20031229000282003122900028SO 2003 12 29 LR7A03089 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND RT AFT FUSELAGE SKIN WRINKLED FS 737-761, RBL 60, WL 170-186. REPLACED RT FUSELAGE SKIN FS 737-773 IAW SRM SMP 583 51-60 & 51-70. NR 2043. 2H74 4T A1SO 20031229000442003122900044NM 2003 12 29 QXEA200301550 120031213A6120699018002 CONTROL UNIT BOMBDRDHC8 DHC8401 1390041NM ZONE 500 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09407QX4628 4628 4049 POWER PLANT MESSAGE ON CLIMBOUT. DIVERTED TO PDX. REPLACED THE NR 1 PEC. OPERATIONAL CHECK FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031229000592003122900059 2003 12 29 QXEA200301552 420031205A2210C18112AA DAMPENER BOMBDRDHC8 DHC8401 1390041NM ZONE 300 FAILED A QXEAO OTHER O OTHER CRCRUISE 1 NM09409QX3345 3345 4051 AUTO-PILOT DISENGAGED AT CRUISE FLIGHT AS WELL AS THE YAW DAMPER DISCONNECTED. COMPLIED WITH CHECKLIST AND UNABLE TO RESET YAW DAMPER OR AUTOPILOT. REMOVED AND REPLACED YAW DAMPER ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031229000682003122900068NM 2003 12 29 03FDEA02182 120031213A2910 FITTING DOUG MD11 MD11 3023602NM HYDRAULIC LINE LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25610FE 48603 AIRBORNE 1.5 HRS AT FL333 HYD SYSTEM 1 FLUID LEVEL DROPPED TO 0.0 LEVEL II HYD 1 FAIL ILLUMINATED, QRH REVIEWED. FOUND NIPPLE FITTING LEAKING, FWD OUTBOARD FITTING ON THE TOP OF HYD MANIFOLD WHERE THE 4 FILTERS ARE LOCATED. REMOVED RT PUMP'S PRESSURE LINE THAT RUNS FROM RT PUMP TO HYD MANIFOLD DUE TO LINE LEAKING. REMOVED AND REPLACED BOTH UPPER AND LOWER HYD PUMP PER MD-11 MM 29-11-20-4 AND INSTALLED NEW PRESSURE LINE. REMOVED AND REPLACED ALL FILTERS ON THE MANIFOLD PER MD-1129-12-41-2. INSTALLED NEW FILTERS PER MD-11 M/M 29-12-41-2. 2L73 4F RTA22WE 20031229000702003122900070NM 2003 12 29 03FDEA02184 120031214A5754 FAIRING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING FIX LEADING EDGE FAIRING ADJACENT TO NR 8 SLAT OUTBOARD END FOUND WORN. COMPLIED WITH FEDEX EA 1-5720-73367, OUTER WING, FIXED LEADING EDGE SKIN. 2L73 4F RTA22WE 20031229000742003122900074NM 2003 12 29 03FDEA02190 120031215A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFY WING - INBOARD FLAP VANE, INBOARD TRACK ATTACHMENT FITTING, BOLT HOLES (3 EA) FOUND EXCEED LIMIT. 2L73 4F RTA22WE 20031229000752003122900075NM 2003 12 29 03FDEA02195 120031214A5320 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 SUPPORT BRACKETS FOR TOILET SHROUD CRACKED. 2L73 4F RTA22WE 20031229000792003122900079SO 2003 12 29 C2XA03TY209 120031215A3230355022002MOD3 CONTROL UNIT EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A C2XAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW27169115959 145446 PILOT REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM 32-32-01. THE OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20031229000822003122900082NE 2003 12 29 251TR0005 220031215A73208TJ85GAZ TRANSMITTER BOEING737 737228 13844AGNM PWA JT8 JT8D15A 52051NE FUEL FLOW LEAKING A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 NR 1 ENGINE LEAKING FUEL OUT OF FWD SIDE OF FUEL FLOW TRANSMITTER. REPLACED NR 1 ENGINE FUEL FLOW TRANSMITTER PER MM 73-31-12. LEAK AND OPS CHECK OK DURING ENGINE RUN PER MM 71-00. 2L72 4F4 FRTA16WE E2EA 20031229000952003122900095NM 2003 12 29 AWXA200301539 120031208A532065535953 REVEAL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN R-1 DOOR UPPER REVEAL BS 298-328. MAINTENANCE REMOVED R-1 DOOR UPPER REVEAL BS 298-328; FABRICATED A NEW REPLACEMENT UPPER REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 11-12, 38, FIG 8. 2L72 4F RTA16WE 20031229001002003122900100NM 2003 12 29 AWXA200301544 120031208A5320654538470 STRAP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN TIE STRAP BELOW CABIN FLOOR IN E&E COMPARTMENT BS 328, BL -0-. MAINTENANCE STOP DRILLED CRACK IN TIE STRAP BS 328, BL -0-; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51, PG 1, & 219, FIG 204. 2L72 4F RTA16WE 20031222001182003122200118NM 2003 12 22 2003F00646 120031114A3350RPS1B POWER SUPPLY BOEING727 7272J4 1384006NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE O OTHER ININSP/MAINT 1 SO11288SC 20765 MAIN CABIN DOOR, SERVICE DOOR AND FORWARD, BULKHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. (M) 2L73 4F RTA3WE 20031223000282003122300028NM 2003 12 23 SWAA032631 120031201A3234A420060283 SWITCH BOEING737 7373A4 1384585NM MLG SELECTOR OUT OF ADJUST A SWAAO OTHER N FALSE WARNING APAPPROACH 1 SW29677AA 23289 DURING LANDING GEAR EXTENSION, 3 RED LIGHTS WITH 3 GREEN LIGHTS INDICATIONS WITH GEAR HANDLE DOWN. RECYCLED LANDING GEARS AND REGAINED NORMAL INDICATION. CLEANED AND ADJUSTED LANDING GEAR CONTROL LEVER POSITION SWITCH. OPS CK GOOD PER MM. 2L72 4F RTA16WE 20031223000352003122300035NM 2003 12 23 SWAA032638 120031129A3350BR2013 COVER BOEING737 7372H4 138448CNM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 EEPLS COVERS BROKEN BETWEEN ROWS 4 AND 5. REPAIRED EEPLS PER MM 2L72 4F A16WE 20031223000692003122300069NM 2003 12 23 QXEA200301535 120031210A2910 LINE BOMBDRDHC8 DHC8401 1390041NM HYD SYSTEM FAILED A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM09402QX5822 4032 SEA - FLIGHT 2399 - ON APPROACH THE NR 2 HYDRAULIC ISO VALVE CAUTION LIGHT ILLUMINATED. THE NR 2 HYDRAULIC QUANTITY FELL TO 10-15 PERCENT. AT NO TIME DID THE HYDRAULIC QUANTITY REACH ZERO. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LANDING GEAR RETRACT ACTUATOR LINE FOR THE LEFT MAIN LANDING GEAR WAS BROKE. THE LINE WAS REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031223001052003122300105NM 2003 12 23 QXEA200301540 120031206A1430 RIVET BOMBDRDHC8 DHC8401 1390041NM ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 CHERRY RIVET AT INBOARD EDGE OF NR 5 FLAP TRACK FITTING SIDE ANGLE THROUGH LOWER SKIN DOES NOT HAVE SHOP HEAD. REMOVED AND REPLACED RIVET IAW Q400 SRM 51-42-45. 2H72 4T RTA13NM 20031223001082003122300108NM 2003 12 23 QXEA200301544 120031206A5720 ATTACH FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 RIGHT HAND OUTBOARD FLAP NR 4 FLAP CARRIAGE FRONT SPAR ATTACH BRACKET INBOARD FITTING AND OUTBOARD LUG IS CHAFED. REPAIRED IAW Q400 RD 8/4-57-228. 2H72 4T RTA13NM 20031223001182003122300118WP 2003 12 23 MWEA030480 120031211A2751V3601 SWITCH DOUG DC9 DC982 3022082WP COCKPIT OUT OF TOLERANCEA MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31809ME 48071 WHEN ADVANCING POWER LEVERS FOR TAKEOFF, RECEIVED TAKEOFF WARNING FOR FLAPS. PERFORMED TAKEOFF WARNING TEST, TEST OK. DURING FURTHER INVESTIGATION, FOUND FLAP TAKEOFF WARNING SWITCH OUT OF TOLERANCE. ADJUSTED SWITCH AND RESECURED LOOSE BRACKET. 2L72 4F A6WE 20031223001282003122300128EU 2003 12 23 MALA030541 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 11A FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 11A IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001342003122300134EU 2003 12 23 MALA030536 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 7A FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 7A IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001432003122300143CE 2003 12 23 DXTA200300181 120031123A2710666000161 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07668QS 5605268 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LT AND RT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001502003122300150CE 2003 12 23 DXTA200300193 120031124A2710666000164 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS BROKEN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07645QS 5605145 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LT AND RT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20040109000442004010900044NM 2004 1 9 TSAA0253268 120030910A53306546533 LAP JOINT BOEING737 737282 13844ATNM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13824AL 23045 TRIMMED BONDED DOUBLER ABOVE EXISTING FASTENER PATTERN LEAVING ED FOR FINAL FASTENER INSTALL. OPENED DISCREPANT COUNTERSINK HOLE TO .75 INCH DIAMETER. VERIFIED CRACK FREE USING HFEC. HOLE OPENED UP TO 1 INCH INSURANCE CUT. FABBED .032/.036 INCH THICK CIRCULAR FILLER, .040 INCH THICK TEAR STRAP SPLICE-STRAP, .036/.040 INCH THICK FILLER FOR BONDED DOUBLER, TWO .40 INCH THICK TAPERED FILLERS FROM 2024 T-3 CLAD ALUMINUM. ALODINED, PRIMED ALL BARE EDGES AND REPAIR PARTS WITH BMS 10-11 TYPE 1 PRIMER. INSTALL FILLERS AS SHOWN IN FIGURE 1 AND REPAIR PARTS IAW SB 737-53A1177, REV 6 REQUIREMENTS MAINTAINING A 2 INCH MINIMUM RADIUS AND .5 INCH MAXIMUM EXTERNAL RADIUS ON DOUBLER, TRIPLER. AC RETURNED TO SERVICE. (M)2L72 4F RTA16WE 20040112000012004011200001EA 2004 1 12 A6WA200340187 120031208A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 FOUND LT FS 625 OBLIQUE ANGLE P/N 601-35012-51 IS CRACKED. (M) 2L72 4F RTA21EA 20040112000402004011200040WP 2004 1 12 AALA20031452 120031221A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21969TW 53619 DFW OVERHEAD EMERGENCY PATH AISLE LIGHTS AFT OF ACCESSORY RAMP AREA INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY PATH AISLE LIGHTS AFT OF ACCESSORY RAMP AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040112000422004011200042EA 2004 1 12 033286251 120031124A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27625BR 7214 DURING INSPECTION THE CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000492004011200049SO 2004 1 12 C2XA03CL202 120031219A5244 ACCESS DOOR EMB 135 EMB135ER 3260203SO COCKPIT STICKING A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 CLE FLIGHT 2438 THE CREW REPORTED, COULD NOT OPEN THE LANDING GEAR EMERGENCY EXTENSION ACCESS DOOR LOCATED IN THE COCKPIT. MAINTENANCE INSPECTED AND LUBED AND UNSTUCK THE ACCESS DOOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040112000722004011200072WP 2004 1 12 GTIA031005 120031114A5315 FLOORBEAM DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND RIGHT AFT LAV FLOORBEAM CORRODED AT FS 1322 27 INCHES RBL AND 3 CORRODED BROKEN NUT PLATES. (M) 2L72 4F A6WE 20040112000832004011200083NM 2004 1 12 AWXA200301573 120031207A531565468101 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 967, RBL 18, WL 208. MAINTENANCE REMOVED CORROSION; FABRICATED A STRAP REPAIR; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 203 PG 212-214. 2L72 4F RTA16WE 20040112000872004011200087NM 2004 1 12 AWXA200301577 120031205A5330655298878 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND COMING FROM FASTENER HOLE ON FUSELAGE SKIN AT BS 958, STR 16-17 LT, WL 215. MAINTENANCE REMOVED FASTENER AND PERFORMED HFEC INSPECTION TO VERIFY CRACK END, STOP DRILLED CRACK AND RE-ACCOMPLISHED HFEC TO VERIFY CRACK WAS CONTAINED; INSTALLED HOLE FILLER IN SKIN; FABRICATED A DOUBLER & TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 203 PG 205-207. 2L72 4F RTA16WE 20040112000942004011200094WP 2004 1 12 AALA20031236 120031110A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGNECY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21510AM 49804 PHX - DURING OVERNIGHT MAINTENANCE, FOUND AFT LEFT AND RIGHT OVERWING EXIT SIGNS INOPERATIVE. REPLACED AFT ELFT AND RIGHT OVERWING EXIT SIGN BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112000952004011200095NM 2004 1 12 AWXA200301581 120031203A5312651758350 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BULKHEAD VERTICAL BEAM WEB BETWEEN BS 178 AND BS 179.5, LBL 5.7, WL 178. MAINTENANCE CUT OUT CRACKED AREA OF BULKHEAD WEB BETWEEN BS 178 AND BS 179.5, LBL 5.7, WL 178; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, FIG 212. 2L72 4F RTA16WE 20040112001082004011200108NM 2004 1 12 HALA0300760 120030916A32301C3360 CHECK VALVE BOEING717 717200 1383700NM NLG FAILED A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13476HA 55118 FLT 513 - HNL - NOSE GEAR WOULD NOT RETRACT, CONFIRMED DOWN WITH CONFIG PAGE. RECYCLED, STILL STAYED DOWN. REMOVED AND REPLACED NLG BUNGEE CYL PER AM 32-35-02, S/N OFF EFS37385, CONDITION SAME. REMOVED AND INSTALLED NOSE GEAR RETRACT CYL PER AMM 32-35-01, CONDITION SAME. REMOVED NOSE STEERING T-FITTING LEFT TUNNEL. FOUND CHECK VALVE FAILED IN NOSE GEAR RETRACT LINE. REPLACED CHECK VALVE AND REINSTALLED 'T'. (M) 2L72 4F TRA6WE 20040112001092004011200109NM 2004 1 12 KPVA200338 120030920A335061047811 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGNECY LIGHT INOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13805WP 353 HNL - RIGHT AFT EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT 3351-PS4 IAW DHC-8 CMM CHAP 33-50-67. OPS CHECK GOOD IAW DHC-8 CHAP 33-51-00 PAGE 201-202. (M) 2H72 4T RTA13NM 20040112001152004011200115WP 2004 1 12 AALA20031251 120031111A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21454AA 49559 DEN - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY CEILING LIGHTS AT 8A-16 INOPERATIVE. REPLACED BATTERY PACKS AT 8DEF AND 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112001372004011200137NM 2004 1 12 DHL2003780018 120031222A5210 DOOR BOEING727 727223 1384074NM FWD ENTRY OPEN A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01780DH 22006 FORWARD ENTRY DOOR OPENED UPON LANDING. PERFORMED OPERATIONAL CHECK PER M/M 52-11-01. NO DEFECTS NOTED. INSPECTED DOOR AND FOUND TO BE OK FOR SERVICE. 2L73 4F A3WE 20040112001392004011200139NM 2004 1 12 CALA0300716 120031222A5514 FITTING BOEING737 7373T0 1384582NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT UPPER ATTACH FWD LUG CORRODED AROUND BUSHING AND FACE OF LUG. REMOVED BUSHING, FOUND CORROSION ON ID AND BOTH FACES. SPOT FACE 0.013 INCH DEEP AND REAMED BORE ID TO 1.5795 INCH. FABRICATED AND INSTALLED OVERSIZE BUSHING PER SRM 55-10-10. 2L72 4F RTA16WE 20040112001442004011200144NE 2004 1 12 2004F00034 220031105A7261 HELICOIL BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE OIL FILTER DAMAGED A RYNAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE077644U 20038 DURING CRUISE, ENGINE NR 3 LOST ALL OIL PRESSURE AND ALL OIL QUANTITY. PERFORMED NR 3 ENGINE INFLIGHT SHUTDOWN CHECKLIST. DIVERTED TO STL. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED HELICOIL AT OIL FILTER BYPASS UNION TO ACCESSORY GEARBOX. (M) 2L73 4F4 F A3WE E2EA 20040112001522004011200152CE 2004 1 12 2004F00035 120031027A541050910275947 DOOR BEECH 99 99 1154002CE LT NACELLE DEPARTED A TIMAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 NM0724BH U67 LEFT ENGINE COWLING SIDE DOOR DEPARTED FROM AIRCRAFT DURING FLIGHT. INSPECTION REVEALED THAT THE CAUSE WAS MOST LIKELY, FAILURE TO SECURE DOOR PANEL PRIOR TO FLIGHT NM-SLC-FSDO. (M) 1L72 3T A14CE 20040108000842004010800084EU 2004 1 8 KBM2003F00034 120030930A6420350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 TAIL ROTOR HINGE LAMINATE WORN TO LIMITS. REPLACED WITH NEW HINGE LAMINATES. (K) 1G71 3U3 UNCH9EU E19EU 20040108001032004010800103 2004 1 8 KBM2003F00053 420031010A3423KCA0113W COMPASS SNIAS 350 AS350B1 8680811EU COCKPIT INACCURATE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 MAGNETIC COMPASS IS MORE THAN 20 DEGREES OFF. INSTALLED NEW COMPASS. 1G71 3U H9EU 20040108001102004010800110 2004 1 8 KBM2003F00060 420031014A2312064105430 RADIO BELL 206 206B 1181511SW VHF SYSTEM MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV81 2704 VHF NR VOL. CONTROL SCRATCHY. INSTALLED SERVICEABLE VHF RADIO. 1G71 3U H2SW 20040108001342004010800134EU 2004 1 8 KBM2003F00066 120031007A2842647510033 PROBE SNIAS 350 AS350BA 8680817EU FUEL SYSTEM READS HIGH E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP1937SH 776 2300 FUEL CAPACITY CHECK FAILED. 10 GALLONS HIGHER ON FUEL ACTUAL QUANTITY. FUEL PROBE REQUIRES REPLACEMENT. REPLACED FUEL PROBE WITH SERVICEABLE OVERHAULED.(K) 1G71 3U NCH9EU 20040109000262004010900026NM 2004 1 9 MEX2003487 120031014A7920 SEAL DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE ENGINE OIL LEAKING W ASMFO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW23169PL 53175 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING, BEFORE TAKEOFF, LT ENGINE OIL QUANTITY DROPPED TO ZERO. LT ENGINE WAS SHUT DOWN WHEN LT OIL PRESS ANNUNCIATOR WAS ILLUMINATED. AIRCRAFT WAS SENT TO THE HANGAR WHERE THE HOUSING OIL FILTER WAS REPAIRED IAW MM 72-00-0 AND SEAL WAS REPLACED IAW MM 79-20-06, TESTS CORRECT.(K) 2L72 4F4 FRTA6WE E2EA 20040109000362004010900036NE 2004 1 9 CHI2003F00002 220030314A7230210133105 COMPRESSOR WHEEL BOEING234 234 1385049EA LYC AL5512AL5512 41581NE ENGINE CRACKED B CHIRO OTHER O OTHER NRNOT REPORTED 1 NM09242CH3132 MJ023 TWO CRACKS WERE FOUND IN THE 1ST STAGE COMPRESSOR DISC (PN210133105) DURNG AN INSPECTION. THE CRACKS ARE LOCATED IN TWO OF THE COMPRESSOR BLADE RETENTION SLOTS. THIS IS THE SECOND TIME CRACKS HAVE BEEN FOUND EMANATING FROM THE BLADE RETENTION SLOTS OF THIS PN DISC. AFTER THE FIRST OCCURRENCE, THE MANUFACTURER CHANGED MANFACTURING PROCESSES AND REIDENTIFIED THE COMPRESSOR DISC. NO CRACKS HAVE BEEN DETECTED IN THE IMPROVED DISCS. WILL CONDUCT A ONE TIME DETAILED INSP OF ALL OLD STYLE COMPRESSOR DISCS. CONSIDERATION WILL BE GIVEN TO ACCELERATING THE REPLACEMENT OF ALL 1ST STG COMP DISC WITH THE IMPROVED DISC.(K) 2G72 4U4 U H9EA E4NE 20040112000582004011200058NM 2004 1 12 DHL2003765006 120031219A3260 SWITCH BOEING727 727264 138408MNM RT MLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01765AT 23014 RIGHT GEAR DOOR LIGHT ILLUMINATED WHEN GEAR HANDLE WAS IN OFF. PERFORMED THE LANDING GEAR OR DOOR WILL NOT STAY UP WITH GEAR LEVER OFF ABNORMAL PROCEDURE. RIGHT GEAR DOOR LIGHT THEN STAYED OFF. ADJUSTED RIGHT GEAR DOOR UNLOCK SWITCH, OPS CHECKED NORMAL IAW M/M 32-12-1. 2L73 4F A3WE 20040112000632004011200063SO 2004 1 12 C2XA03CL205 120031216A49504952375 SERVO VALVE EMB 145 EMB145 3260210SO APU FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2714974 145161 IAH FLIGHT 2627 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND CABIN WHEN THE APU WAS STARTED. MAINTENANCE REPLACED THE APU BLEED SERVO CONTROL VALVE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040112000712004011200071WP 2004 1 12 GTIA031013 120031117A5310 STRAP DOUG DC9 DC981 3022081WP CARGO DOORWAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND AFT CARGO DOOR JAMB BEAM AND REPAIR STRAP CORRODED. JAMB BEAM REPAIR STRAP IS FOUND TO BE OUT OF LIMITS. REMOVED JAMB BEAM REPAIR STRAP. FABRICATED NEW REPAIR STRAP. INSTALLED NEW JAMB BEAM REPAIR STRAP. (M) 2L72 4F A6WE 20040112001072004011200107NE 2004 1 12 2004F00025 220031113A7200 COMPRESSOR AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE NR 2 ENGINE STALLED A RJEFC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO23EITAB 1624 HAV - FLT 130 - DURING TAKEOFF FLIGHT CU130, HAV-MEX, AN ENGINE STALL OCCURRED ON ENGINE NR 2. TAKEOFF PROCEDURE WAS ABORTED, AIRCRAFT RETURNED TO GATE. AT THE PRESENT AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE. (M) 2L72 4F4 FRTA28NM E40NE 20040112001212004011200121WP 2004 1 12 AALA20031237 120031109A33500201720003 LIGHT DOUG DC9 DC983 3022083WP SEAT 9D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21568AA 49349 DTW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY AISLE LIGHTS AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20040112001252004011200125WP 2004 1 12 GTIA031011 120031116A5320 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND NLG W/W STATION 69.5 LEFT AND RIGHT UPPER TEE FITTINGS HAVE CORRODED AT RBL 16 AND LBL 16 AND WEB CORRODED AT LEFT SIDE. REMOVED DAMAGED FITTING. FURTHER INVESTIGATED LEFT FITTING CRACKED, REMOVED CRACKED FITTING. INSTALLED TWO TEE FITTINGS. (M) 2L72 4F A6WE 20040112001342004011200134EA 2004 1 12 2004F00032 120031125A56106003303025 WINDSHIELD CNDAIRCL600 CL6002A12 1900304EA LEFT CRACKED A N38AA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA05163WG 3057 LEFT WINDSHIELD FAILED IN FLIGHT, OUTER PANE CRACKED AND SEPARATED. CREW FOLLOWED CHECKLIST PROCEDRUES AND LANDED AT A SUITABLE AIRFIELD. (M) 2L72 4F RTA21EA 20040112001582004011200158NE 2004 1 12 AALA20031460 220031220A7250 TURBINE BLADES DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RT ENGINE FAILED A AALAEC ENGINE SHUTDOWN ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW21484AA 49677 725853 ORD EN ROUTE ORD-AUS ON TAKEOFF RIGHT ENGINE FAILED AT NOSE ROTATION. ENGINE SHUT DOWN AND AIRCRAFT RETURNED ORD WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE DUE TO TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20031223000292003122300029NM 2003 12 23 SWAA032632 120031201A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND 1 INCH LONG FUSELAGE SKIN CRACK AT BS 764, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031223000322003122300032 2003 12 23 SWAA032635 420031129A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 R2 DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. REPOSITIONED R2 SLIDE PER MM. 2L72 4F A16WE 20031223000452003122300045NM 2003 12 23 SWAA032666 120031204A53116545808 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND FWD CABIN FRAME AT BS 303.9 CRACKED AT LOWER STOP PAD INTERCOSTAL CUTOUT. REPAIRED DAMAGE PER SRM. 2L72 4F RTA16WE 20031223000482003122300048 2003 12 23 SWAA032669 420031206A2565D31354 SLIDE BOEING737 7372T4 1384492NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASY PER MM. 2L72 4F A16WE 20031223000492003122300049NM 2003 12 23 SWAA032670 120031206A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED C1 CHECK, FOUND BS 378.5 FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031223000662003122300066NM 2003 12 23 F3LA200300172 120031211A5347 MOUNT BOEING737 73736E 138443ANM GALLEY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON GALLEY MOUNT AT STA 990, RBL 32. REPLACED GALLEY MOUNT PER SRM 51-40-02. 2L72 4F RTA16WE 20031223000732003122300073NM 2003 12 23 F3LA200300173 120031211A5320 FLOOR SUPPORT BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON UPPER CHORD FLOOR SUPPORT IN AFT GALLEY, STA 986.5 TO STA 1006, LBL 31. REPLACED CHORD PER SRM 51-40-02 AND REINSTALLED FLOOR SUPPORT ASSY PER SRM 51-40-02. 2L72 4F RTA16WE 20031223000762003122300076NM 2003 12 23 AWXA200301527 120031203A531265163007 BULKHEAD BOEING737 73733A 1384673NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD FORWARD FACE WEB AT BUTTON HEAD HI-LOK HOLES AT 6 O'CLOCK POSITION WL 234 LBL 9 AND LBL 11. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD FORWARD FACE WEB AT WL 234 LBL 9 AND LBL 11; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG 265-269, FIG 209. 2L72 4F RTA16WE 20031223000772003122300077NM 2003 12 23 AWXA200301528 120031203A5755654645262 PANEL BOEING737 73733A 1384673NM LT WING SPOILER DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK FOUND PREVIOUS REPAIR DISBONDED AT OUTBOARD UPPER SURFACE OF NR 4 SPOILER FROM WBL 174.75 TO WBL 107.75. MAINTENANCE REMOVED PREVIOUS REPAIR AT OUTBOARD UPPER SURFACE OF NR 4 SPOILER FROM WBL 174.75 TO WBL 107.75; PERPARED SURFACE AND APPLIED A NEW BOND REPAIR IAW B737-300 SRM 51-70-10, REPAIR 21, FIG 30, PG 88C, D, & E, AND PG 7-31. 2L72 4F RTA16WE 20031223000782003122300078EA 2003 12 23 COMA0360542 120031209A5315601R350313 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 FS 589 TO FS 621 LBL 27 FLOORBEAM UPPER CAP IS CORRODED. REPAIRED BY REMOVING CAP AND REPLACING IAW WVAC EO 601R-53-4451A. 2L72 4F RTA21EA 20031223000812003122300081NM 2003 12 23 VNAA0312005 120031209A3350321431 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07424JS60 3033 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERIES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031223000862003122300086NM 2003 12 23 SWAA032697 120031210A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 1 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29407WN 29817 EEPLS TRACK LOOSE AT ROW 1. SECURED TRACK PER MM. 2L72 4F RTA16WE 20031223000892003122300089NM 2003 12 23 SWAA032700 120031210A53116546565 FRAME BOEING737 7373A4 1384585NM AFT FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND CORROSION ON RT AFT GALLEY DOOR FRAME AT BS 996, RBL 48, WL 208. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031223000962003122300096NM 2003 12 23 SWAA032707 120031210A5310AND10137 BEAM BOEING737 7372H4 138448CNM LWR FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED C3 CHECK, FOUND NOSE WHEEL WELL CEILING BEAM CRACKED. REPAIRED BEAM PER SRM. 2L72 4F A16WE 20031219000902003121900090NM 2003 12 19 2003UALA00918 120031126A5270 TARGET BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO DOOR OUT OF ADJUST A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29919UA 25386 FLIGHT RETURNED TO THE FIELD IN ABQ FOR PRECAUTIONARY MEASURES, AFT CARGO DOOR LIGHT INDICATION CAME ON PASS INITIAL 9500 FEET AND REMAINED ON. NO PREVIOUS HISTORY. FOUND TARGET OUT OF ADJUSTMENT. RE-ADJUSTED AND NO PROBLEMS SINCE. TYPICAL CAUSE OF TARGETS BEING OUT OF ADJUSTMENT IS DUE TO CARGO LOADING AND ACCIDENTALLY HITTING/BENDING THE TARGET BRACKET. 2L72 4F4 FRTA16WE E2GL 20040112001652004011200165WP 2004 1 12 MEX2003510 120030411A7922P320115 VALVE DOUG DC9 DC983 3022083WP RT ENG OIL FAILED A ASMFA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW23838AM 49397 FLT 214 - MEX-HMO - UNSCHEDULED LANDING AT BJX DUE TO THE RIGHT ENGINE OIL TEMP INCREASED TO 145 DEGREES CELSIUS DURING 15 MINUTES. AT BJX WHEN THE ENGINE WAS TURNED OFF, THE TEMPERATURE INCREASED UNTIL 165 DEGREES CELSIUS. BOTH GAUGES WERE SWAPPED, AND THE OIL LEVEL AND THE FUEL HEATING VALVE WERE CHECKED, DETECTING THAT SUCH VALVE REMAINS IN THE OPEN POSITION. THE VALVE WAS REPLACED AND TESTED IAW MM 73-14-02. (M) 2L72 4F RTA6WE 20040112001702004011200170WP 2004 1 12 GTIA031023 120031106A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND RIGHT INBOARD SEAT TRACK HAS NICKS, GOUGES, CORRODED AND BARE METAL ROM STATION 200 TO 237. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK. (M) 2L72 4F RTA6WE 20040112001802004011200180NM 2004 1 12 MASA200300512 120031225A33506519020 LIGHT DHAV DHC8 DHC8202 2809007NM ROW 6,7 & 8 BURNED OUT A MASAO OTHER L NO TEST ININSP/MAINT 1 SW07456YV 456 ASH 7030 GJT. DURING INITIAL TEST THE EMERGENCY LIGHTS AT ROWS 6,7,AND 8 WERE INOPERATIVE. MECHANIC REPLACED THE LIGHT STRIP. 2H72 4T RTA13NM 20040112001862004011200186NM 2004 1 12 03FDEA02237 120031223A5744 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR OUTBOARD MOUNT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75217 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS 2L73 4F RTA22WE 20040112002152004011200215EU 2004 1 12 BAQA091876 120031222A2420SPC10HD STATIC INVERTER UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE AC SYSTEM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH460 0131 INVERTER FAILED. PART REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H88EU E34NE 20040112002222004011200222 2004 1 12 SWAA032798 420031222A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20040112002292004011200229EU 2004 1 12 BAQA091532 120031203A26129560129970 FIRE DETECTOR AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE FALSE INDICATIONB BAQAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA03911UF 6338 ENGINE UNDER CONTRACT. FALSE FIRE WARNINGS OCCUR WHEN IT IS DAMP. THIS IS BEING SENT BACK UNDER A MFG WARRANTY CLAIM. REPLACED WITH SERVICEABLE UNIT. 12/16/03 1G72 3U3 U H10EU E19EU 20040112002342004011200234NM 2004 1 12 AALA20031445 120031218A3350 LIGHT BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 EMERGENCY LIGHT LENS LOOSE ON SEAT 20B. REPLACED LIGHT ASSEMBLY AND BACK PLATE ON SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA1NM 20040112002402004011200240NM 2004 1 12 AALA20040001 120031231A3397 WIRE BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139367 25194 EMERGENCY FLOOR SEAT LIGHTS AT SEAT 34H INOPERATIVE. REPAIRED BROKEN WIRES FOR EMERGENCY FLOOR SEAT LIGHTS AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA1NM 20040112002422004011200242WP 2004 1 12 AALA20040003 120031231A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21224AA 49174 FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002782004011200278WP 2004 1 12 AALA20031414 120031210A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217520A 49897 DFW FORWARD SEAT MOUNTED EMERGENCY LIGHTS AT 27D INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20040113000022004011300002EU 2004 1 13 BAQA091570 120031212A6710 BEARING UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE M/R CONTROL ROD WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME800 0009 MAIN ROTOR CONTROL ROD BEARINGS WORN. 1G72 3U3 UO H88EU E42NE 20040113000072004011300007EU 2004 1 13 BAQA091379 120031205A6720 BUSHING BOLKMS117 BK117B1 5626012EU ACTUATOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE874 00365 7219 TAIL ROTOR ACTUATOR BUSHING AND CARDAN JOINT ARE WORN. REPLACED WITH SERVICABLE UNIT 12/18/2003 1G72 3U H13EU 20040113000152004011300015EU 2004 1 13 BAQA091639 120031228A2140JBS8803 EJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE HEATER FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118WS428 0089 HEATER EJECTOR PRODUCING NO HEAT. VALVE STOPPED WORKING. PART REPLACED WITH SERVICABLE UNIT. 01/06/2004 1G72 3U3 U H88EU E34NE 20040113000172004011300017SW 2004 1 13 ERAA091806 120031020A3212D24922117 FLOAT BELL 412 412 1182202SW MLG LEAKING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03417EH3137 33031 MLG FLOAT BAG LEAKS DOWN. FLOAT WAS INSPECTED. REPAIRED AND TESTED SERVICEABLE IAW 412-SI-2. 1G72 4U H4SW 20031219001022003121900102EU 2003 12 19 2003UALA00931 120031203A5320 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29405UA 452 R-2 DOOR SILL PLATE CORRODED. MAJOR REPAIR ACCOMPLISHED. AREA REPAIRED PER EVA IMC 30161 AND MAE EA 20-5341-13-A1060. 2L72 4F4 FRTA28NM E40NE 20031219001362003121900136NM 2003 12 19 03FDEA02117 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031222000532003122200053WP 2003 12 22 ASAA0380620 120031007A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 DURING 15K CHECK FOUND CABIN FLOOR PANEL IS DISBODED AT CORNER AND CREASED THROUGH MIDDLE AT FS 465-522. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031222000632003122200063WP 2003 12 22 ASAA0380612 120031007A532199365491 FLOORBOARD DOUG DC9 DC983 3022083WP FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS CORRODED AND SOME MISSING INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M0 2L72 4F RTA6WE 20031222001362003122200136EA 2003 12 22 COMA0360537 120031206A3350 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01949CA 7080 THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. SECURED LOOSE WIRING CONNECTION. 2L72 4F RTA21EA 20031222001372003122200137EA 2003 12 22 COMA0360538 120031207A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01938CA 7046 FLAPS FAILED AT ZERO. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031223000092003122300009EA 2003 12 23 03339703 120031205A335064643 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 DURING INSPECTION THE FLOOR EMERGENCY LIGHTS WERE DIM. THE POWER STRIP WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031223000242003122300024NM 2003 12 23 SWAA032627 120031130A57536546481 CARRIAGE BOEING737 7373A4 1384585NM LT WING TE FLAP CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C4 CHECK, FOUND NR 1 T/E FLAP SPINDLE CORRODED AT SHAFT UNDER THRUST BEARING. REMOVED AND REPLACED NR 1 T/E FLAP CARRIAGE ASSY PER MM. 2L72 4F RTA16WE 20031223000432003122300043NM 2003 12 23 SWAA032664 120031204A53106546569 SHEAR TIE BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED BETWEEN STR R 26 AND R 27, BS 947. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F A16WE 20031223000552003122300055NM 2003 12 23 SWAA032676 120031207A53116516301 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND BOTH LEFT AND RIGHT FRAMES CRACKED AT BS 188. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20031223001062003122300106EA 2003 12 23 COMA0360544 120031204A2750860D1018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01967CA197373400 7134 FLIGHT 5894 FLAPS FAILED AT ZERO. REPLACED THE FECU. 2L72 4F RTA21EA 20031223001122003122300112NM 2003 12 23 QXEA200301546 120031208A5410 FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX- LEFT HAND NACELLE AFT FINGERNAIL DECK FRAME IS CRACKED. REPAIRED IAW Q400 RD 8/4-54-033. 2H72 4T RTA13NM 20031223001132003122300113 2003 12 23 COMA0360548 420031209A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01989CA 7215 FLIGHT 5279 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20031223001162003122300116NM 2003 12 23 AWXA200301531 120031209A5411D5453003220000 RIB AIRBUSA319 A319132 3930340NM NR 2 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908. MAINTENANCE REMOVED AND REPLACED CRACKED NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908 IAW A319 SRM 51-42-11, FIG 2, 3, & 8, PG 8-10, 12, & 22, AND TABLES 1, 4, 7 5, FIG 8. 2L72 4F RTA28NM 20031223001172003122300117NM 2003 12 23 VNAA0311006 120031116A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07463PS 3087 DURING FLIGHT, THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. THE FLIGHT ATTENDANT INSPECTED THE LAV AND THERE WAS NO SMOKE OR EVIDENCE OF FIRE OR SMOKE. UPON ARRIVAL, MAINTENANCE INSPECTED AND DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH 26-4 CODE C, MAINTENANCE FUNCTION WAS COMPLIED WITH. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031223001232003122300123EU 2003 12 23 MALA030533 120031201A5320 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 11D, 11E, 11F, FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 11D, 11E, 11F IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001272003122300127EU 2003 12 23 MALA030540 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 13A, 13D FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 13A, 13D IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001302003122300130EU 2003 12 23 MALA030543 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 6B FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 6B IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001482003122300148CE 2003 12 23 DXTA200300196 120031212A2710666000164 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS BROKEN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07663QS 5605263 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001542003122300154SO 2003 12 23 C2XA03SH492 120031213A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 DURING C-CHECK THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031223001562003122300156SO 2003 12 23 C2XA03SH483 120031213A531514522459003 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 SHV- DURING C-CHECK THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031223001642003122300164EA 2003 12 23 A6WA200340161 120031111A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31401AW 7280 RT FUSELAGE SKIN AT STATION 310 BETWEEN STRINGERS 24R AND 25R HAS LIGHTNING DAMAGE WITH A TEMPORARY REPAIR INSTALLED IAW BOMBARDIER, INC REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER FROM 2024T3 .063 INCH WVAC PO NR 27603/1 AND INSTALLED IAW WVAC EO 601R-53-4387A. (M) 2L72 4F RTA21EA 20031223001692003122300169EA 2003 12 23 A6WA200340162 120031111A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31401AW 7280 RIGHT FUSELAGE SKIN AT FS 409-116 STRINGER 23R HAS LIGHTNING DAMAGE AND A TEMPORARY REPAIR INSTALLED IAW BOMBARDIER, INC REO 601R-53-00-084 REV A. CUT OUT DAMAGED SECTION OF SKIN. PERFORMED EDDY CURRENT OF CUTOUT, FABRICATED REPAIR DOUBLER FROM 2024 T3 .063 AND REPAIR FILLER FROM 2024 T3 .063. INSTALLED FILLER AND DOUBLER IAW WVAC EO 601R-53-4380 REV A. (M) 2L72 4F RTA21EA 20031223001772003122300177NM 2003 12 23 MEX2003542 120031130A291041003106 PTU DOUG MD88 MD88 3023688NM HYD SYSTEM FAILED A ASMFO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL 53175 AFTER LANDING THE LIGHT OF (L HYD TEMP HI) CAME ON. THE SYSTEM WAS VERIFIED AND THE POWER TRANSFER UNIT WAS FAULTY. THE PTU WAS REPLACED AND THE SYSTEM WAS TESTED IAW MM 29-10-07, ALL CORRECT. (M) 2L72 4F RTA6WE 20031223001952003122300195WP 2003 12 23 GTIA030823 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FLOOR SUPPORT CORRODED AT FS 148-200, 0 INCHES BL, FLIGHT COMPARTMENT. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED HOLES AT NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031223001982003122300198WP 2003 12 23 GTIA030814 120031010A5340 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND MID PIT STATION 693 TEE FITTING CORRODED/ELONGATED HOLES. FABRICATED NEW T-FITTING. (M) 2L72 4F A6WE 20031224000122003122400012WP 2003 12 24 GTIA030802 120030904A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND E/E BAY STATION 200 CEILING WEB CRACKED RBL 17 INCHES. REMOVED DAMAGED AREA. FABRICATED WEB DOUBLER. INSTALLED WEB DOUBLER. (M) 2L72 4F A6WE 20031224000202003122400020NM 2003 12 24 HALA0301083 120031119A2420755359C IDG BOEING767 76733A 1385209NM NR 1 ENGINE FAILED A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13582HA2179 28139 GEN DRIVE LIGHT AND GEN DRIVE EICAS MESSAGE ON STEADY BUT WENT OUT WHEN LEFT GEN CONT SWITCH TURNED OFF RESULTING IN AIR TURNBACK AT 50 NM EAST OF DUETS. BITE CHECK BPCU FOUND PRESSURE SWITCH WIRING REMOVED AND REPLACED NR 1 ENG IDG PER HAL CARD 767-3-405001 AND MM 24-11-01, OPS CHECK NORMAL OK FOR SERVICE. (M) 2L72 4F RTA1NM 20031224000362003122400036WP 2003 12 24 GTIA030945 120031110A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND CABIN FLOORBOARD STATION 400-480 HAT CHANNEL CRACKED, DELAMINATING. STOP DRILLED THE CRACK AT FLOORBOARD. LOCATED AND DRILLED REPAIR CHANNEL. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20031222000202003122200020EA 2003 12 22 SWIA200312649 120031130A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07443SW4427 4427 7638 SPOILERONS FAULT ON TAXI OUT. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILERON PCU IAW CRJ AMM 27-62-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20031222000352003122200035NM 2003 12 22 DHL2003745027 120031208A5754 SKIN BOEING727 727224 1384076NM LE SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 8336 20665 NR 6 LEADING EDGE SLAT BOTTOM SKIN CRACKED 30 INCHES FROM INBOARD EDGE. REMOVED AND REPLACED NR 6 LEADING EDGE SLAT ASSEMBLY IAW B-727 M/M 27-81-11, OPS CHECKED GOOD IAW B-727 M/M 27-81-0. P/N OFF: 65-16222-2, S/N:BN939, P/N ON: 65-16222-92, S/N: BN3. 2L73 4F A3WE 20031222000362003122200036CE 2003 12 22 344031 120031210A3260 BULB BEECH 1900 1900D 1154162CE MLG INDICATOR BURNED A NSVAO OTHER N FALSE WARNING APAPPROACH 1 EA27155CJ UE55 LANDING GEAR INDICATION LIGHT NOT WORKING. REMOVED AND REPLACED LIGHT BULBS, OP CHECKED GOOD. 2L72 4T RTA24CE 20031222000662003122200066WP 2003 12 22 ASAA0380615 120031007A532199365501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS DISBONDING AROUND INSERTS AT FS 190-256. REPLACED FLOORBOARD [ER SRM 53-05. (M) 2L72 4F RTA6WE 20031222000692003122200069WP 2003 12 22 ASAA0380605 120031007A5320 STRUCTURE DOUG DC9 DC983 3022083WP SUB FLOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND SUB FLOORING IS CRACK AT FS 200. REPLACED DAMAGED SUB-FLOORING SECTION PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20031222000722003122200072NE 2003 12 22 AALA20031029 220030918A7261 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 ENGINE MALFUNCTIONED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21559AA 53089 AIRCRAFT EN ROUTE FROM ORD-MIA, LOSS ENGINE OIL PRESSURE ON CLIMB-OUT. EMERGENCY DECLARED AND AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED. REMOVED AND REPLACED THE NR 2 ENGINE. LEAK AND SYSTEM GROUND CHECKED NORMAL. (M) 2L72 4F4 F A6WE E9NE 20031222000872003122200087WP 2003 12 22 AALA20031006 120030915A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217546A 53028 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE ABOVE FORWARD OVERWING EXITS. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031222001302003122200130WP 2003 12 22 AMTA200301415 120031121A3397 WIRE LKHEED1011 10113853 5265020WP EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EMERGENCY PATH LIGHT AT AFT GALLEY FLOOR INOPERATIVE. POWER SUPPLY STRIP DISCONNECTED BETWEEN STRIPS RECONNECTED AND SECURED. OPS CHECK GOOD. (M) 2L73 4F A23WE 20031223001202003122300120EU 2003 12 23 MALA030545 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 7D, 7E, 7F FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 7D, 7E, 7F IAW MESABA EO NR A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001602003122300160EA 2003 12 23 ASOA03552 120031031A5320601R3807413 ANCHOR CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANANCE REMVOED AND REPLACED THE AFT ANCHOR ON THE PASSENGER DOOR, AND ALSO REMOVED AND REPLACED THE DOOR ANCHOR GUIDE SHAFT WHICH WAS WORN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031223001762003122300176EA 2003 12 23 A6WA200340183 120031123A5522 SKIN CNDAIRCL600 CL6002B19 1900309EA ELEVATOR LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 SO11403AW 7288 FOUND DAMGE ON RIGHT ELEVATOR UPPER SKIN CAUSED BY LIGHTNING STRIKE. REPAIRED BY PERFORMING WVAC EO NR 601R-55-4418. BLENDED AREA, PERFORMED NDT EDDY CURRENT AND APPLIED PROTECTIVE TREATMENT. (M) 2L72 4F RTA21EA 20031223001792003122300179WP 2003 12 23 GTIA030836 120031006A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FS CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 180 RBL 8 INCHES TO RBL 44 FLOOR PANEL HAS SEVERAL INSERTS BROKEN OUT/CORRODED/SOFT/MUSHEY. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031224000262003122400026NM 2003 12 24 USAASB03207 120031124A335020121 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19371US 22950 MAINTENANCE REPORTED THE LT OVERWING EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031224000412003122400041 2003 12 24 ASAA0380686 420031017A25653961896501 LANYARD DOUG MD80 MD83 3023681NM ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01982AS 53473 PREFLIGHT CHECK, FOUND FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RT 20031224000432003122400043WP 2003 12 24 GTIA030948 120031108A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND AFT PIT-INTERCOSTAL CRACKED AT CABIN FLOOR PANEL SCREWS AT FS 1271-1287 2 INCHES LBL. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2L72 4F RTA6WE 20031224000442003122400044WP 2003 12 24 GTIA030947 120031025A531059360381 BEAM DOUG DC9 DC983 3022083WP DOOR FRAME CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND MID PIT STRINGER 28R JAMB BEAM CORRODED AT DOOR OPENING. REMOVED DOOR JAMB BEAM. DRILLED AND LOCATED NEW JAMB BEAM. INSTALLED NEW DOOR JAMB BEAM. (M) 2L72 4F RTA6WE 20031224000472003122400047WP 2003 12 24 GTIA030951 120031107A5315 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 GTIA - FOUND CABIN STATION 148 RBL 45 - RBL 52 FLOORBEAM CORRODED AND STATION 146 RBL 52 FLOOR SUPPORT CORRODED. REMOVED CORROSION AT STATION 146 RBL 52. MATERIAL LOSS FOUND WITHIN LIMITS. FABRICATED FLOORBEAM AT STATION 148 RBL 45-52. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20031224000522003122400052NE 2003 12 24 AMTA200301398 220031118A7320 EEC BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE MALFUNCTIONED A AMTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL11558TZ 32592 ON CLIMB LT ENGINE SURGING EPRS 1.52 TO 1.63 N1 91.9 TO 94.0 SAT -16. SWAPPED RT ENGINE EEC MPN 356A70655G181, S/N 01L0432 WITH LEFT ENGINE EEC MPN 356A7065G181 S/N 01J0417 PER GMM CHAP 8 PLUS MM 73-21-07-4. OPS CHECK NORMAL. (M) 2L72 4F4 FRTA2NM E12EU 20031224000632003122400063NM 2003 12 24 2003F00656 120031208A77117898301 TRANSMITTER BOEING757 757236 1384971NM EPR FAILED A P9RAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11521NA 25592 NR 2 ENGINE ROLL BACK AT CRUISE ALTITUDE, ENROUTE. AIRCRAFT DIVERTED AND LANDED UNEVENTFULLY. PLACED NR 2 ENGINE EEC ON MEL 4013. CONTINUED ON, TROUBLESHOT SYSTEM AND FOUND NR 2 ENGINE EPR TRANSMITTER FAULTY. REMOVED AND REPLACED TRANSMITTER IAW BMM 77-11-0. OPS CHECKED GOOD. REF LOGBOOK PAGE 38064. ACTION CLEARS MEL 4013. (M) 2L72 4F RTA2NM 20031224000642003122400064SO 2003 12 24 C2XA03SH495 120031213A531214547494607 FIREWALL EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW EA 5340-01015 AND EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031229000012003122900001NE 2003 12 29 VNAA0311010 220031126A7320 ECU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07436JS 3052 DURING TAKEOFF, WHEN THE CONTROL LEVERS WERE ADVANCED THE LT ENGINE ECU FAILED AND THE CREW ABORTED TAKEOFF. THE CREW RESET THE ECU AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT WHICH WAS SUCCESSFUL. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031229000132003122900013NM 2003 12 29 SWAA032708 120031210A2750MS21260S3 CABLE BOEING737 7373H4 1384600NM RT WING BROKEN A SWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW29356SW 25251 DURING CLIMBOUT NOTICED UNUSUAL VIBRATION. VIBRATION DECREASED WHEN AIRSPEED LESS THAN 250 KNOTS. FOUND MIDFLAP BOOM CABLE BROKEN. REMOVED AND REPLACED BOOM CABLE PER MM. 2L72 4F RTA16WE 20031229000172003122900017 2003 12 29 SWAA032712 420031210A2565D31354 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29787SA 29812 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031229000202003122900020 2003 12 29 250TR0026 420031210A22104038891916 COMPUTER BOEING737 7372K5 138448XNM NR 1 FCC MALFUNCTIONED A PIDAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO05250TR 22597 CAPTAIN'S FLIGHT DIRECTOR FLAG IN VIEW. REPLACED NR 1 FLIGHT CONTROL COMPUTER PER MM 22-11-331. OPS CHECKS GOOD. 2L72 4F RTA16WE 20031229000272003122900027SO 2003 12 29 LR7A03088 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND CENTER FUSELAGE SKIN WARPED FS 697-737E, LBL 60, WL 142-185. REPLACED LT FUSELAGE SKIN FS 697-737E IAW SRM SMP 583 51-60 & 51-70. NR 2039. 2H74 4T A1SO 20031229000372003122900037SO 2003 12 29 LR7A03102 120031121A5310 RING LKHEED382 382G 526414USO FUSELAGE DEFORMED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND RT CENTER FUSELAGE RING SEGMENT DEFORMED AT FS 747E, 752E & 762E, RBL 60, WL 142-148. REPAIRED IAW SRM SMP 583 51-140-23. NR 2238. 2H74 4T A1SO 20031229000392003122900039SO 2003 12 29 LR7A03104 120031121A5522 SKIN LKHEED382 382G 526414USO ELEVATOR LOOSE A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND RT ELEVATOR LOWER SKIN REPAIR WITH LOOSE FASTENERS AT HSS 67. REPLACED ELEVATOR SKIN FROM HSS 51 -90 IAW SMP 583 51-60 & 51-70. NR 2241. 2H74 4T A1SO 20031229000432003122900043NM 2003 12 29 UPS03641656 120031215A5210 DOOR BOEING767 767300 1385204NM MAIN PAX INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01320UP 27747 MAIN CABIN DOOR INOPERABLE. 2L72 4F RTA1NM 20031229000452003122900045EU 2003 12 29 03542 120031215A3150 WARNING SYSTEM SAAB SF340 SF340A 7850100EU CONFIGURATION ACTIVATED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1740 40 ON T/O ROLL AT 60 KIAS, CONFIGUATION WARNING SOUNDED. T/O ABORTED. AC RETURNED TO GATE WITH NO INCIDENT. 2L72 4T RTA52EU 20031229000542003122900054NM 2003 12 29 AALA20031426 120031212A3350 LIGHT BOEING767 767323 1385205NM L4 EXTERIOR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21371AA 25198 DFW EXTERIOR EMERGENCY LIGHT AT L4 IS INOPERATIVE. RECLAMPED AND SECURED EXTERIOR EMERGENCY LIGHT ASSEMBLY AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031229000562003122900056WP 2003 12 29 AALA20031428 120031214A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21447AA 49473 SEAT MOUNTED EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 18D. REPLACED SEAT MOUNTED EMERGENCY PATH LIGHT ASSEMBLY AT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031229000582003122900058NM 2003 12 29 QXEA200301555 120031212A2930 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM HYD SYSTEM ILLUMINATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09347PH 480 THE CREW ABORTED TAKEOFF AFTER RECEIVING A NR 2 HYD PUMP CAUTION LIGHT DURING THE TAKEOFF ROLL. MAINTENANCE INSPECTED THE AIRCRAFT AND WAS NOT ABLE TO DUPLICATE THE DISCREPANCY. OPERATIONAL AND SYSTEMS CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED BACK TO SERVICE. 2H72 4T RTA13NM 20031229000612003122900061NM 2003 12 29 QXEA200301553 120031209A242011522184 GENERATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09408QX5388 5388 4050 NR 1 AC GENERATOR CAUTION LIGHT WOULD NOT RESET PER CHECKLIST. LOAD ON ELECTRICAL PAGE FOR NR 1 AC GENERATOR IS ZERO. REMOVED AND REPLACED NR 1 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031229000942003122900094NM 2003 12 29 AWXA200301538 120031208A5320D5323028120140 ANGLE AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 DURING C-04 CHECK A .5 INCH CRACK WAS FOUND IN LOWER RADIUS OF L-ANGLE ON RT AFT SIDE OF FR 34 UNDER PANEL 192AT, BS 14836. MAINTENANCE REMOVED CRACKED -L- ANGLE ON RT AFT SIDE OF FR 34; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 6-7, A20-A23, & A27. 2L72 4F RTA28NM 20031222001322003122200132EA 2003 12 22 COMA0360533 120031202A5320601R31171117 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 FS 484 ANGLE OUTBOARD SIDE OF RBL 27 IS CRACKED. REPAIRED BY REMOVING AND REPLACING ANGLE IAW BOMBARDIER, INC REO 601R-53-41-059 REV A AND WVAC EO 601R-53-4445. 2L72 4F RTA21EA 20031223000252003122300025NM 2003 12 23 SWAA032628 120031130A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 21 INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29783SW 29809 DURING SCHEDULED MS CHECK, FOUND EEPLS INOP AT ROW 21. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20031223000872003122300087NM 2003 12 23 SWAA032698 120031210A53406549892 FITTING BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND CORROSION IN AFT CARGO COMP BS 1011, STRINGER 20 R, AT 1016 BULKHEAD ATTACHMENT. REPAIRED BULKHEAD ATTACHMENT PER SRM. 2L72 4F RTA16WE 20031223000992003122300099 2003 12 23 SWIA200312652 420031204A221012049625001 CONTROL BOX EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07268UE533 533 120207 CAPTAIN'S AND FIRST OFFICER'S AUTOPILOT INOP. REPLACED AP TRANSFER BOX AS REQUIRED. SYSTEM OPS CHECK GOOD IAW CH 22-10-00 EMB 120 MM. 2L72 4T RTA31SO 20031223001322003122300132EU 2003 12 23 MALA030534 120031201A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 9D, 9E FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 9D, 9E IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001532003122300153SO 2003 12 23 C2XA03IA112 120031209A279714570504409 WIRE HARNESS EMB 145 EMB145LR 3260212SO PROXIMITY SWITCHCHAFED A C2XAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW2716559 145603 PILOT REPORTED THAT DURING TAKEOFF THE SPOILERS DEPLOYED AND DID NOT RETRACT EVEN AFTER STOPPING THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE LEFT SPOILER PROXIMITY SWITCH HARNESS, OPERATIONALLY CHECKED THE SPOILER SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20031223001712003122300171EA 2003 12 23 ASOA03541 120031026A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11912EV 7728 DURING DESCENT INTO DFW FROM MGM, AT APPROX 18,000 FT THE PAX REPORTED AN ODOR OF SMOKE IN CABIN AROUND ROWS 4 - 6 WITH NO VISIBLE SIGNS. QRH PROCEDURES WERE COMPLIED WITH & AN EMERGENCY LANDING MADE SAFELY INTO DFW. ODOR DISSIPATED APPROXIMATELY THREE MINUTES PRIOR TO LANDING WITH NO PASSENGER EVACUATION NECESSARY UPON LANDING. MX INSPECTED AVIONICS BAY, MLG BAYS, PROX SENSOR ELECTRONIC UNITS ON THE LT & RT SIDES & ACM WITH NO DEFECTS NOTED. PACKS AND APU WAS ALSO INSPECTED AND OPERATED WITH NO DEFECTS NOTED. MAINTENANCE SUSPECTS THE ODOR CAME FROM THE TEMP RISE IN THE PACKS WHEN SWITCHING FROM THE ENGINE TO THE AUXILIARY POWER UNIT. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031223001752003122300175EA 2003 12 23 A6WA200340184 120031129A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA TE FLAP CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31423AW 7636 FOUND LEFT OUTBOARD FLAP HAS DEEP CHAFF IN FIXED VANE AT FAR OUTBOARD END LEADING EDGE .050 TO .075 DEPTH. PERFORMED A MAJOR REPAIR TO THE LEFT OUTBOARD FLAP LEADING EDGE FIXED VANE BY REMOVING AND REPLACING LEADING EDGE CAP, P/N 601R-14574-7 IAW CRJ SRM 57-30-00, 51-40-11 AND 51-42-13. (M) 2L72 4F RTA21EA 20031223001802003122300180WP 2003 12 23 GTIA030833 120031006A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FORWARD CABIN STATION 200 TO 256 RBL 45.5 TO RBL 55 METALLIC PANEL HAS CRACKED/DAMAGED AT HAT CHANNEL AND EXPANSION JOINT CRACK/DISBONDED. FABRICATED REPAIRS. INSTALLED HAT CHANNEL REPAIRS. REPAIRED DISONDED AREA. (M) 2L72 4F A6WE 20031223001822003122300182WP 2003 12 23 GTIA030831 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 218 0 INCHES - 22 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031224000482003122400048 2003 12 24 AMTA200301403 420031116A2565 GIRT BAR BOEING757 75723N 1384973NM ESCAPE SLIDE DIRTY A AMTAK NONE O OTHER ININSP/MAINT 1 GL11527AT 30886 L2 SLIDE LIGHT GIRT BAR ENGATE IS INOPERATIVE. PERFORMED TROUBLESHOOTING IAW FIM 25-66-00. FOUND DEBRIS IN GIRT BAR ENGAGEMENT AREA, CLEANED AND LUBRICATED GIRT BAR ENGAGEMENT SLIDER. LIGHT AND OPS CHECK OK. (M) 2L72 4F RTA2NM 20031229000472003122900047NM 2003 12 29 AALA20031421 120031213A3350S283T0143 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21374AA 25201 EMERGENCY LIGHTING INOPERABLE FROM ROWS 20 TO 24. REPLACED BATTERY PACK AT 23A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031229000652003122900065NM 2003 12 29 03FDEA02179 120031209A7600 LINKAGE BOEING727 727200 138407ENM NR 1 ENG CONTROLMISSING A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO25495FE 21669 INFLIGHT TOTAL LOSS OF NR 1 ENGINE THROTTLE CONTROL. ENGINE NR 1 ACCELERATED TO 90 PERCENT N1 & N2, SUSPECT ZERO SPEED PROTECTION HAS ENGAGED. ENGINE SHUTDOWN IAW CHECKLIST. FOUND NR 1 ENG THROTTLE CONTROL LINKAGE AFT ROD-END BEARING MISSING. CAPT CONFIRMED SHUTDOWN DURATION OF LESS THAN 20 MINUTES WITH A POSITIVE OIL PRESSURE ABOVE 10 PSI DURING WINDMILLING. ACCOMPLISHED THE ENGINE WINDMILLING INSPECTION REFERENCING THE P & W JT8D MAINTENANCE MANUAL 72-00. T/S FOUND THAT THE BOLT WHICH ATTACHES THRUST LEVER INPUT ROD TO NR 1 ENG FUEL CONTROL HAD FALLEN OUT. INSTALLED NEW BOLT, NUT, WASHER AND COTTER KEY TO INPUT ROD. RIGGING WAS NOT AFFECTED REF M/M 76-11-001-4. OK FOR SERVICE. 2L73 4F RTA3WE 20040113000212004011300021SW 2004 1 13 HEEA087825 120030625A3340212075139001 LANDING LIGHT BELL 412 412 1182202SW EXTERIOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 LANDING LIGHT WILL NOT TURN OFF. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20040113000222004011300022 2004 1 13 HEEA087813 420030620A2340A3016W INTERPHONE BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA CABIN INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 INTERPHONE BOX, NO SIDE TONE. SHOP REPAIR. 1G72 4U4 U H4SW E22EA 20040108000832004010800083EU 2004 1 8 KBM2003F00033 120030928A71700174078030 DRAIN VALVE SNIAS 350 AS350BA 8680817EU ENGINE LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 ENGINE START DRAIN VALVE LEAKING INTERNALLY TO OVERBOARD DRAIN. INSTALLED OVERHAULED START DRAIN VALVE. 1G71 3U NCH9EU 20040108001112004010800111EU 2004 1 8 KBM2003F00061 120031014A7931642790041 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE OIL PRESSURE LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19345SH 3345 OIL PRESSURE TRANSMITTER LEAKING OIL AND INOPERATIVE. INSTALLED SERVICEABLE OVERHAULED OIL PRESSURE TRANSMITTER. 1G71 3U3 U H9EU E19EU 20040108001222004010800122CE 2004 1 8 S9K2003F00000 120031007A5330103912 SKIN CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO HARTZLHCC3Y HCC3YF2 GL WINGLET DEBONDED E S9KAO OTHER O OTHER NRNOT REPORTED 1 NM09414CS2228 414A0230 L228479R EB2486E DURING A ROUTINE PHASE INSPECTION ON A CESSNA 414A WITH RAM WINGLETS, INSTALLED UNDER STC NR SA4943SW A 6 INCH CRACK WAS DISCOVERED IN THE BOND LINE WHERE THE BOTTOM WINGLET SKIN IS BONDED TO THE BOTTOM OF THE WINGLET MAIN SPAR, ON THE FORWARD AND AFT SIDE. A .5 INCH CRACK ON THE OPPOSITE WINGLET IN THE SAME AREA WAS ALSO DISCOVERED. THE CRACKS START AT THE WINGLET MAIN SPAR FITTING PN 1088-5 AND GO OUTBOARD. THE CRACKS APPEAR TO BE CAUSED BY FATIGUE. BOTH WINGLETS WERE REMOVED AND SENT TO THE MANUFACTURE FOR REPAIR.(K) 1L72 3O3 O A7CE E8CE 5 CP25EA 20040108001492004010800149NM 2004 1 8 AMTA200301248 120030920A5315 FLOORBEAM BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE FUSELAGE CORRODED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11519AT 27975 MAIN CABIN FLOORBEAM UPPER CHORD CORRODED. REPAIRED FLOORBEAM IAW ER033585.(K) 2L72 4F4 FRTA2NM A12EU 20040109000102004010900010NM 2004 1 9 MEX2003505 120031027A300039244421 VALVE DOUG MD80 MD83 3023681NM ANTI ICE SYSTEM FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23945AS11128 49643 CAPTAIN REPORTED THAT DURING AIR FOIL ICE PROTECT WAS TURNED ON, THERE WAS A PRESSURIZATION LEAK WITH FLOW LIGHT ON AND CLIMB RATE BETWEEN 500 AND 800 FPM. TO ATTEND THE FAIL, THE TECH PERSONNEL REPLACED THE PNEUMATIC AUGMENTATION VALVE, PRESSURE REGULATOR VALVE OF LEFT AIR CONDITIONING AN THE ICE PROTECTION VALVE IAW MM 36-1001, 21-31-01 AND 31-10-01 RESPECTIVELY, TESTS CORRECT.(K) 2L72 4F RT 20040109000472004010900047WP 2004 1 9 GTIA031025 120031105A3220 DEFLECTOR DOUG DC9 DC983 3022083WP NLG BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND NLG WATER SPRAY DEFLECTOR, BOTH LT AND RT LOWER DEFLECTORS BROKEN, AFT END. REMOVED AND REPLACED RT OB WATER DEFLECTOR SIDE PLATE. REMOVED AND REPLACED LT OB WATER DEFLECTOR SIDE PLATE. (M) 2L72 4F RTA6WE 20040112000042004011200004NM 2004 1 12 TSAA0253257 120031218A531065458181 WINDOW FRAME BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INSIDE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-79 TYPE III, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2, AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AL. AIRCRAFT RETURNED TO SERVICE. WINDOW FRAME P/N 65-458181, 65-46525, 65-46526 AND 65-46530, BS 360R UPPER, BS 380R, BS 400R, AND BS 460R. (M) 2L72 4F RTA16WE 20040112000202004011200020WP 2004 1 12 GTIA031015 120031113A5313 LONGERON DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND FORWARD NOSE WHEEL WELL LONGERON AT NWW DOOR CUTOUT HAS A CRACK IN THE WEB AT FORWARD RT CORNER AT DOOR JAMB. UPON FURTHER INVESTIGATION, FOUND WEB NOT TO BE CRACKED, BUT DID FIND WEB SUPPORT ANGLE CRACKED. REMOVED SUPPORT ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW SUPPORT ANGLE. (M) 2L72 4F A6WE 20040112000232004011200023WP 2004 1 12 DHL2003802537 120031118A278037701441 TORQUE TUBE DOUG DC8 DC873 302199CWP L/E SLOT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT O/B SLOT TORQUE TUBE CRANK 2.000 CRACK. REMOVED RIGHT O/B SLOT TORQUE TUBE. REMOVED AND REPLACED CRANK AND REINSTALLED TORQUE TUBE IAW SRM 51-1-21 PG 1, OHM 27-37-6 PG 1-2. REFER TO N/R 1546 FOR OPS CHECK. 2L74 4F RT4A25 20040112000412004011200041EA 2004 1 12 03328625 120031124A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27625BR 7214 DURING INSPECTION THE LT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000452004011200045EA 2004 1 12 03353654 120031219A2752853D10018 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A VTZAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 EA27654BR 7454 DURING APPROACH TO YYZ ON FLT 7218 CREW REPORTED FLAP FAIL WHEN SELECTING FLAPS 8 DEGREES. CREW DECLARED AN EMERGENCY AND PERFORMED A ZERO FLAP LANDING. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY AT GATE. THE BPSU AND FLAP ACTUATOR WERE FOUND TO BE THE CAUSE OF THE FLAP FAIL AND WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000542004011200054EA 2004 1 12 03354675 120031220A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27675BR 7635 DURING INSPECTION THE RT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000562004011200056EA 2004 1 12 03353644 120031219A2710 PULLEY CNDAIRCL600 CL6002B19 1900309EA AILERON DIRTY A VTZAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 EA27644BR 7379 DURING OPERATIONAL OF AIRCRAFT CREW REPORTED DIFFICULTY UTILIZING THE AILERON CONTROLS. MAINTENANCE PERSONNEL FOUND HEAVY DEPOSITS OF DIRT ON THE CONTROL CABLES AND PULLEYS. THE CABLES AND PULLEYS WERE CLEANED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031224000532003122400053SO 2003 12 24 SIMA200332402 120031114A27503631001007 FCU EMB 135 EMB135LR 3260305SO TE FLAPS FAILED A SIMAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 SW21723AE 145288 FLAP FAIL ON APPROACH, FLAPS STUCK AT ZERO. REPLACED FECU OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031229000092003122900009WP 2003 12 29 ABXA030472 120031202A534039573171AX FITTING DOUG DC9 DC941 302207NWP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23960AX 47762 FITTING WAS CRACKED AT STA 366 LONGERON 29 RT. REMOVED AND REPLACED FITTING AT STA 366 LONGERON 29 RIGHT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20031229000122003122900012WP 2003 12 29 ABXA030467 120031125A5420995816145 STIFFENER DOUG DC9 DC941 302207NWP NR 1 NACELLE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 NR 1 PYLON INTERNAL UPPER HORIZONTAL STIFFENER CRACKED ON INBOARD END, ABOVE FUEL LINE SHROUD. REPAIRED AREA NOTED IAW DC-9 SSRM K05159 AND DC-9 SRM 51-30-5. 2L72 4F A6WE 20031229000292003122900029SO 2003 12 29 LR7A03090 120031121A5350 FAIRING LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND FS 476 AERODYNAMIC FAIRINGS CRACKED AT LBL 30 AND RBL 30, WL 283. REPAIRED IAW SRM SMP 583 51-140-12. NR 2060. 2H74 4T A1SO 20031229000342003122900034SO 2003 12 29 LR7A03095 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WRINKLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND LT AFT FUSELAGE SKIN WRINKLED FS 737-814, LBL 60, WL 142-170. REPLACED FUSELAGE SKIN FS 737-814 IAW SRM SMP 583 51-60 & 51-70. NR 2075. 2H74 4T A1SO 20031229000872003122900087NM 2003 12 29 DHL2003742507 120031203A5330 DOUBLER BOEING727 727225 1384077NM FUSLEAGE CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, N/R 60758 FUSELAGE DOUBLER BETWEEN STA 720C-720D LBL 6 STR 28L IS CHAFED BY RAM AIR DUCT. REMOVED OLD DOUBLER REPAIR IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR FROM MAT 2024-T3 .125 PO 9912571 DIM 12.5 INCH X 8.875 INCH IAW B-727 SRM 53-30-2 FIG 3. TREATED AND PRIMED DOUBLER REPAIR IAW B-727 SRM 51-10-2. INSTALLED DOUBLER IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20031229001012003122900101NM 2003 12 29 AWXA200301545 120031208A5320654583469 STRAP BOEING737 737301 1384611NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN TIE STRAP BELOW CABIN FLOOR IN E&E COMPARTMENT BS 328, LBL 12. MAINTENANCE STOP DRILLED CRACK IN TIE STRAP BS 328, LBL 12; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51, PG 1, & 219, FIG 204. 2L72 4F RTA16WE 20031229001072003122900107NM 2003 12 29 AWXA200301551 120031202A5320654583317 WEB BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND AT FRAME FLANGE RELIEF CUTOUT ON FLIGHT COMPARTMENT FLOOR WEB 4 INCH INBOARD OF FUSELAGE SKIN AT BS 194 RT, WL 207.5. MAINTENANCE REMOVED CRACKED WEB AT BS 194 RT, WL 207.5; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45833; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031229001122003122900112EU 2003 12 29 MALA030547 120031210A56107256100503 WINDSHIELD SAAB SF340 340B 7860101EU COCKPIT CRACKED A MALAO OTHER O OTHER CRCRUISE 1 GL15415XJ 340B415 DURING CRUISE ON FLIGHT 3044, AT 16,000 MSL IN ICING CONDITIONS OUTER PANEL OF CAPT FRONT WINDSHIELD CRACKED. LEFT FRONT WINDSHIELD HEAT FAILED SHORTLY AFTER. MAINTENANCE REPLACED CAPT WINDSCREEN P/N 7256100-503. S/N ON 03254H4099. PERFORMED OPS CHECKS, ALL CHECKS GOOD REF 409 CARD 067248 FOR DETAILS. PER SAAB AMM CHAP 30/56. 2L72 4T RTA52EU 20031229001162003122900116 2003 12 29 SWAA032722 420031214A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 GAUGE ON SLIDE AT L2 DOOR OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20031229001232003122900123NM 2003 12 29 SWAA032729 120031213A33502013 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT LIGHT BATTERY PACK. 2L72 4F RTA16WE 20031229001252003122900125EA 2003 12 29 MASA200300482 120031208A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775983 7481 DURING A TEST OF THE EMERGENCY ESCAPE LIGHTING, THE RT EXTERIOR LIGHT WOULD NOT TEST. MX REPLACED THE LAMP. OP CHECKS GOOD. 2L72 4F RTA21EA 20031229001412003122900141NM 2003 12 29 SWAA032736 120031214A57436567172 FITTING BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SC RT MLG WALKING BEAM OUTBOARD FWD HANGER FITTING ON REAR SPAR CORRODED IN THE BORE. REPAIRED FITTING PER SRM. 2L72 4F RTA16WE 20031229001472003122900147NM 2003 12 29 UPS03241663 120031215A2612 FIRE DETECTOR BOEING727 72722C 138400FNM CARGO BAY WILL NOT TEST A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 LOWER CARGO FIRE MX LIGHT ON. CODES A7418A, A9051A 26-18-02 SYSTEM OK. TESTED AND RESET LOWER CARGO SMOKE DETECTOR SYSTEM IAW MM 26-18-02 SYSTEM OK. 2L73 4F A3WE 20031229001552003122900155EA 2003 12 29 SWIA200312660 120031205A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 280 TRANSVERSE BEAM LBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV ''NC''. 2L72 4F RTA21EA 20031229001612003122900161EA 2003 12 29 SWIA200312666 120031205A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 TRANSVERSE BEAM REMOTE ANGLE FOR DOOR STOP FITTING IS CRACKED; FS 589.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 & RII 53-401. 2L72 4F RTA21EA 20031229001662003122900166NM 2003 12 29 03FDEA02204 120031217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN CARGO DECK LT STA 839 SEAT TRACK REF X=27.5 BENEATH FLOOR PANEL 241JF SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2 & SRM 53-70-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20031229001732003122900173EA 2003 12 29 SWIA200312668 120031205A7120 SUPPORT CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 ENGINE SUPPORT BEAM UPPER WEB RBL 6 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. UPPER WEB REPAIRED IAW CRJ REO 601R-53-61-345 REV ''C'' AND RII 53-401. 2L72 4F RTA21EA 20031229001762003122900176SO 2003 12 29 SWIA200312671 120031114A5415 BULKHEAD EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07568SW 120343 RIGHT ENGINE AFT OUTBOARD SIDE LOWER NACELLE BULKHEAD CRACKED AT HYDRAULIC LINE CONNECTIONS. LOCATION REF: S/B 120-29-0049 PAGE 15, FIG 2, DET D. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED OUTBOARD LOWER RIGHT NACELLE FIREWALL IAW EMBRAER INSTRUCTIONS PER EACS REF 1C2003-120/3922. 2L72 4T RTA31SO 20031223001242003122300124EU 2003 12 23 MALA030531 120031208A30103D238162 EJECTOR VALVE SAAB SF340 340B 7860101EU DEICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15364PX 340B262 DURING FLIGHT 2741, THE LEFT I/B DEICE BOOT WOULD NOT INFLATE, WITH THE AUTO CYCLE SWITCH SELECTED THE TIMER LIGHT WOULD COME ON. THE TIMER LIGHT ALSO WOULD ILLUMINATED PRESSING THE MANUAL BUTTON. AFTER SEVERAL ATTEMPTS, THE LEFT I/B BOOT SECTION DID INFLATE NORMALLY. AIR RETURN TO MSP. MAINTENANCE REPLACED LEFT I/B (LOWER) EJECTOR VALVE IAW AMM 30-10-31-4. P/N OFF 3D2381-62, S/N OFF 161. P/N ON 3D2381-62, S/N ON N1432, OPS CHECK OF I/B BOOT CHECK GOOD. 2L72 4T RTA52EU 20031224000322003122400032WP 2003 12 24 ASAA0380625 120031011A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS LARGE SOFT, DEBONDED, AREA FROM FS 1117 TO 1174. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031229000072003122900007WP 2003 12 29 ABXA030469 120031130A5712991932915 RIB DOUG DC9 DC941 302207NWP LT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23960AX 47762 CRACK IN LT WING RIB UPPER CLIP AT X0S 447. REPLACED CLIP IAW DC-9 SRM 51-30. 2L72 4F A6WE 20031229000192003122900019EA 2003 12 29 COMA0360549 120031213A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO01979CA16390 7159 THE RT FORWARD SIDE OF THE AFT PRESSURE BULKHEAD AT FS 621 IS CHAFED .012 INCH DEEP X .150 INCH WIDE AT RBL 36, WL 103. THE DAMAGE WAS CAUSED FROM BAGGAGE BAY LINER HARDWARE BEING TOO LONG. THE DAMAGED AREA WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW WVAC EO 601R-53-4465. 2L72 4F RTA21EA 20031231000132003123100013NM 2003 12 31 TSAA0253246 120031107A53206532195 WEB BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 TRIMMED OUT DAMAGED WEB. HFEC INSPECTED THE EDGE OF CUTOUT. ENLARGED TRIM BY .04 AS A INSURANCE CUT. FABRICATED A .50 INCH THICK REPAIR WEB, TOW .063 INCH THICK DOUBLERS AND A .063 INCH THICK TAPER FILLER FROM 2024-T3 CLAD SHEET. FABRICATED THREE EACH REPAIR STIFFENERS FROM7075-T6511 EXTRUSION. FABRICATED A 50:1 TAPER FILLER FROM 2024-T3 CLAD. FLAT PEENED REPAIR T-STIFFENERS. ALODINED AND PRIMED REPAIR PARTS AND BARE ALUMINUM. INSTALLED REPAIR PARTS IAW FIGURE 3, USING FASTENERS IDENTIFIED, WET WITH BMS 5-95 SEALANT MAINTAINING 5D TO 6D SPACING AT NEW LOCATIONS. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000192003123100019NM 2003 12 31 TSAA0333051 120030310A33509221009 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 REPLACED AFT ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000262003123100026NE 2003 12 31 AMTA200301465 220031206A7323FFG022AC GOVERNOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LT ENGINE MALFUNCTIONED A AMTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL11524AT 30233 ON ENGINE RUNUP FOR TAKEOFF, THE RIGHT ENGIEN WOULD NOT MAKE TAKEOFF POWER IT STAYED AT 1.1 EPR WHILE LEFT ENGINE MADE TAKEOFF POWER 1.61 ALL RIGHT ENGINE INSTRUMENTS INDICATIONS LOOKED NORMAL. ABORTED TAKEOFF AT 60 KNOTS. REMOVED AND REPLACED NR 2 ENGINE FUEL FLOW GOVERNOR, PER AMM 73-21-01-4. LEAK AND OPS CHECK ON DIS NR 7100-432. (M) 2L72 4F4 FRTA2NM E12EU 20031231000512003123100051EA 2003 12 31 ASOA03577 120031113A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FALSE INDICATIONA ASOAO OTHER N FALSE WARNING CLCLIMB 1 SO11886AS 7531 DURING CLIMB-OUT, AT APPROXIMATELY 20,000 FEET THE CREW RECEIVED A SMOKE CARGO MESSAGE. AFTER TURNING OFF THE CARGO FAN WHLE COMPLYING WITH THE IMMEDIATE ACTION ITEMS, THE SMOKE CARGO MESSAGE, CARGO FIRE X NORMAL AND STAND BY RED LIGHTS ALL EXTINGUISHED. NO FURTHER MESSAGES WERE NOTED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS PRECAUTIONARY MEASURE, MAINTENANCE REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS. OPS CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000552003123100055WP 2003 12 31 GTIA030901 120031029A3350BR9661116 LIGHT DOUG DC9 DC982 3022082WP L1 DOOR INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 L1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED NEW SERVICEABLE EMERGENCY LIGHT ASSEMBLY. (M) 2L72 4F A6WE 20031231000582003123100058EU 2003 12 31 ASOA03561 120031015A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING A C-CHECK, THE INTERCOSTALS ON THE LT SIDE UNDER THE FLOOR BETWEEN FS 39 AND 40 AND ON THE RT SIDE BETWEEN FS 40 AND 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS ON THE LT SIDE UNDER THE FLOOR BETWEEN FS 39 AND 40 AND ON THE RT SIDE BETWEEN FS 40 AND 41 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20031231000662003123100066EA 2003 12 31 A6WA200340180 120031118A5753 VANE CNDAIRCL600 CL6002B19 1900309EA TE FLAP CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 LEFT OUTBOARD FLAP FIXED VANE LEADING EDGE CAP, P/N 601R-14574-7 IS CHAFED AT WS 297 APPROXIMATELY .25 INCH BY .5 INCH AND .001 DEEP. PERFORMED MAJOR REPAIR TO THE LEFT OUTBOARD FLAP LEADING EDGE FIXED VANE BY REMOVING AND REPLACING LEADING EDGE CAP P/N 601R-14574-7 IAW CRJ200 SRM 57-53-00, 51-40-11 AND 51-42-13. (M) 2L72 4F RTA21EA 20031231000672003123100067EA 2003 12 31 ASOA03574 120031109A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA AIRSTAIR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000742003123100074EA 2003 12 31 ASOA03575 120031110A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A HANGAR INSPECTION IN BTR, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000772003123100077WP 2003 12 31 GTIA030923 120031031A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND DENT AT FS 1207 BETWEEN LONGERONS 25 AND 26L, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. (M) 2L72 4F RTA6WE 20031231000852003123100085WP 2003 12 31 GTIA030921 120031030A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - AFT PIT STATION 1309 TO STATION 1322 HAD RIGHT SIDE INTERCOSTAL CORROSION. REMOVED INTERCOSTAL. LOCATED AND DRILLED HOLES IN NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. (M) 2L72 4F RTA6WE 20031224000602003122400060NM 2003 12 24 2003F00661 120031123A3232274579 ACTUATOR BOEING757 757236 1384971NM RT MLG DOOR FAILED A P9RAO OTHER J WARNING INDICATION APAPPROACH 1 SO11522NA 25133 RIGHT MAIN GEAR DOOR EICAS MESSAGE. REMOVED AND REPLACED RT MLG DOOR ACTUATOR IAW BMM 32-32-12. (M) 2L72 4F RTA2NM 20031229000322003122900032SO 2003 12 29 LR7A03093 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE SCRATCHED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND LT CENTER FUSELAGE SKIN SCRATCHED FS 777E-817E, LBL 60, WL 142-170. REPLACED FUSELAGE SKIN FS 777E-817E IAW SRM SMP 583 51-60 & 51-70. NR 2073. 2H74 4T A1SO 20031229000602003122900060NM 2003 12 29 QXEA200301556 120031211A5410 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 LT LOWER COWL HAS Z-ANGLE CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-16 AND SRM 51-42-05 AND SRM 51-40-15. 2H72 4T RTA13NM 20031229000662003122900066NM 2003 12 29 03FDEA02180 120031211A3233651781213 ACTUATOR BOEING727 727200 138407ENM NLG MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25222FE1222512225 20933 NOSE GEAR DID NOT EXTEND ON 1ST TRY. RECYCLED GEAR AND IT CAME DOWN. JACKED NOSE GEAR PER 727-200 MM 07-11-000-2. REMOVED AND REPLACED NOSE GEAR ACTUATOR PER 727-200 MM 32-33-001-4. LUBRICATED ALL GEAR COMPONENTS. REMOVED AND REPLACED LANDING GEAR ACC WARNING UNIT. PERFORMED NOSE GEAR EXTENSION AND RETRACTION PER 727-200 MM 32-33-000-5. GROUND OPS CHECKS NORMAL. LEAK CHECKS GOOD. REMOVED MAIN GEAR PINS AND TAIL SKID. RETURNED A/C TO SERVICE. 2L73 4F RTA3WE 20031229001342003122900134EA 2003 12 29 MASA200300465 120031126A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER L NO TEST ININSP/MAINT 1 SW077291Z 7291 PILOT REPORTED AN OVERHEAD EMERGENCY EXIT LIGHT INOP. MX RELAMPED. 2L72 4F RTA21EA 20031231000402003123100040EU 2003 12 31 A6WA20030069 120031209A5330 SKIN BAC 146 146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVET LOCATIONS. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF FAX 1734-6070004. (M) 2H74 4F A49EU 20031231000962003123100096WP 2003 12 31 GTIA030936 120031030A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND AFT PIT STATION 1309 TO STATION 1287 HAS CORROSION AT THE WEB. CUT OUT DAMAGED AREA. DRILLED AND LOCATED HOLES AT REPAIR. INSTALLED FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20031231001202003123100120WP 2003 12 31 GTIA030918 120031028A5410K2219PSA31 ISOLATOR DOUG DC9 DC983 3022083WP RT NACELLE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND RIGHT ENGINE FORWARD LOWER ISOLATOR CORRODED. REMOVED ISOLATOR. INSTALLED NEW ISOLATOR. (M) 2L72 4F RTA6WE 20031231001332003123100133EU 2003 12 31 DXTA200300205 120031218A2750 CONTROLLER BRAERO1000 BAE1251000A 1500104EU TE FLAPS MALFUNCTIONED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS DEDESCENT 1 GL07540QS DURING FLIGHT FROM TEB TO ADS DURING DESCENT FLAPS WILL NOT LOWER WHEN SELECTED TO 15, 25, OR 45 DEGREES. DIVERTED TO DFW AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20040105000182004010500018 2004 1 5 03360316 420031226A22107010680938 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AUTOPILOT SYS FAULTY A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27316UE 41055 DURING AIRCRAFT OPERATION THE CREW REPORTED OSCILLATIONS WITH THE AUTOPILOT SYSTEM ENGAGED. THE AUTOPILOT COMPUTER WAS FOUND TO BE FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040105000362004010500036EU 2004 1 5 MALA030550 120031211A3260200876279 WIRE HARNESS BAC 146 AVRO146RJ85A1500097EU NLG WOW FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15518XJ E2337 DURING FLIGHT 3614, RUDDER LIMITER LIGHT ILLUMINATED INFLIGHT. AIR RETURNED TO DTW. MAINTENANCE REMOVED AND REPLACED NLG WEIGHT ON WHEEL HARNESS P/N 200876279 AND PERFORMED ADJUSTMENT AND TEST IAW AVRO MM 32-. ALL CHECKS GOOD SEE MM 409 067253 FOR DETAILS. 2H74 4F RTA49EU 20040105000682004010500068NM 2004 1 5 2003UALA00948 120031212A5414 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 CRACK ON FWD UPPER PYLON SKIN INSIDE ACCESS PNL 432BR, NR 1 ENG. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20040105000702004010500070NM 2004 1 5 2003UALA00950 120031210A3350 CHARGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29533UA 25073 EMERGENCY LIGHTS INOP, OUTSIDE OF AFT CARGO DOOR, AISLE LIGHT AT ROW 25, EXIT SIGN ON CEILING PANEL AT ROW 16. REPLACED EMERGENCY BATTERY CHARGER AND BATTERY PACK. 2L72 4F4 FRTA2NM E17NE 20040105000762004010500076EA 2004 1 5 03350621 120031216A27203A2237B TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA RUDDER INTERMITTENT A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27621BR 7186 DURING AIRCRAFT OPERATION THE CREW REPORTED INTERMITTENT UNCOMMANDED RUDDER MOVEMENT. THE RUDDER POSITION TRANSMITTER WAS FOUND TO BE CAUSING THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040105000812004010500081WP 2004 1 5 AALA20031444 120031218A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 18D INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21266AN 49291 EMERGENCY PATH LIGHT ON SEAT 18D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20040105000862004010500086NM 2004 1 5 QXEA200301567 120031218A8010 FLANGE DHAV DHC8 DHC8202 2809007NM LT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX - LEFT HAND NACELLE 414AR STARTER/GENERATOR INTAKE MATING FLANGE IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20040105000962004010500096WP 2004 1 5 DHL2003802545 120031124A57203645612U BRACKET DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING NR 4 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON RIGHT WING NR 4 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9, 21. 2L74 4F RT4A25 20040105001052004010500105WP 2004 1 5 DHL2003802531 120031120A53203758496U2 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 2.000, STA1160.000 - 1180.000, L-35R. REMOVED CRACKED FITTING FROM AFT CARGO COMPT (STA 1160.000 - 1180.000, L-35R) IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031229001222003122900122NM 2003 12 29 SWAA032728 120031212A55116550578 SPAR BOEING737 7373A4 1384585NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB REAR SPAR LOWER CHORD CORRODED. REPAIRED SPAR PER SRM. 2L72 4F RTA16WE 20031229001512003122900151SO 2003 12 29 C2XA03CL200 120031215A49204504113A APU EMB 145 EMB145 3260210SO AFT FAILED A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2713956 145078 EWR FLIGHT 2526 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN AFTER PUSHBACK. MAINTENANCE INSPECTED AND REPLACED THE APU. THE APU WAS SEIZED AND CAUSED BURNING SMELL IN COCKPIT AND CABIN. OPERATIONAL CHECKS WERE GOOD. THE APU WAS REMOVED FROM MEL. 2L72 4F RTT00011AT 20031229001842003122900184NM 2003 12 29 AWXA200301557 120031209A5347D534722090237 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF FLOORBEAM AT FR 66, Y1292, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM FROM FR 64 TO FR 66, Y1292, Z240; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D534-72209; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7, AND SRM 51-49-00 PG 5-6. 2L72 4F RTA28NM 20031229001852003122900185NM 2003 12 29 AWXA200301558 120031211A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LOWER SIDE OF FLOOR PANEL 261FF FROM BS 31577 TO BS 32571, Y1600 TO Y1898, Z240. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF FROM BS 31577 TO BS 32571, Y1600 TO Y1898, Z240 IAW AWA T/C C1D25310. 2L72 4F RTA28NM 20031231000022003123100002WP 2003 12 31 GTIA030909 120031107A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND FLOOR PANEL RIGHT STATION 130-133 CORNER DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20031231000102003123100010EU 2003 12 31 USAASA03126 120031108A3350321430 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19164UW 1425 LOW BATTERY VOLTAGE WAS DETECTED WHILE PERFORMING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE RIGHT SIDE EMERGENCY EXIT DOOR BATTERY PACK. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031231000342003123100034NM 2003 12 31 TSAA0329044 120030309A29171225P62 PRESSURE SWITCH BOEING737 73776N 13844CHNM 'A' HYD SYS FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13744AL 32582 AFTER TAKEOFF THE 'A' SYSTEM HYDRAULIC PUMP LIGHT CAME ON. THE AIRCRAFT RETURNED TO HNL AND MADE AN OVERWEIGHT LANDING WITH NO FURTHER INCIDENT. MAINTENANCE VERIFIED THE LOW PRESSURE LIGHT. THE 'A' SYSTEM ELECTRIC PUMP PRESSURE SWITCH, NR 2 ELECTRIC MOTOR DRIVEN PUMP AND SYSTEM FILTERS WERE REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. AN OVERWEIGHT LANDING INSPECTION WAS COMPLETED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231001012003123100101NM 2003 12 31 TSAA0357059 120030404A57546546422229A SKIN BOEING737 7372T4 1384492NM NR 2 SLAT DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13807AL 23443 GAINED ACCESS TO DENTED AREA. CUTOUT DAMAGE BY SLICING THE LEADING EDGE SKIN PER FIGURE 1. INSTALLED A SPLICE REPAIR AT SS205.46 AND SS 238.71. REPAIR COMPLETED IAW SRM 57-50-3, FIGURE 7 AND ECO 3354. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231001042003123100104NM 2003 12 31 TSAA0353046 120030225A53136545818 STRINGER BOEING737 737282C 13844AUNM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13826AL 23051 REMOVED DAMAGED PART OF STRINGER. FABRICATED REPAIR PARTS PER TABLE 1 FROM 2024-T4 AND 7075-T6 CLAD. ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 53-10-3, FIGURE 1. (M) 2L72 4F RTA16WE 20040105000132004010500013 2004 1 5 DL757031005 420031112A2565MS35650302 NUT BOEING757 757232 1384965NM ESCAPE SLIDE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 EMERGENCY ESCAPE MANUAL RELEASE CABLE JAM NUT CORRODED BELOW AND BETWEEN EXIT CUTOUTS STA 984-996 AND STRINGER 17R. REMOVED SAFETY WIRE, CLEANED AREA OF CORROSION. OK TO INSTALL NEW HARDWARE. INSTALLED NEW HARDWARE. 2L72 4F RTA2NM 20040105000612004010500061NM 2004 1 5 2003UALA00941 120031207A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 SEAT 17L AFT EEL LIGHT STRIP WILL NOT LIGHT. REPLACED AND TESTED 17L EEL LIGHT ASSY, CHECKS OK. 2L74 4F4 FRTA20WE E24NE 20040105001302004010500130NM 2004 1 5 SWAA032770 120031217A3350BR2013 STRIP BOEING737 7373L9 1384470NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C4 CHECK, FOUND AFT LEFT EEPLS STRIP BROKEN. REMOVED AND REPLACED EEPLS STRIP PER SRM. 2L72 4F RTA16WE 20040105001412004010500141NM 2004 1 5 SWAA032759 120031216A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED PM CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT STR 18L, BETWEEN BS 763 AND BS 780. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040105001442004010500144WP 2004 1 5 ABXA030480 120031208A532099577263 INTERCOSTAL DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 INTERCOSTAL FS 756, LEFT BUTTLINE 22 WAS CRACKED. REPLACED INTERCOSTAL WEB IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040105001582004010500158CE 2004 1 5 AMWA97 120031216A532011443010653 DOUBLER BEECH 1900 1900D 1154162CE FUSELAGE DELAMINATED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT DOUBLER WAS FOUND TO BE DISBONDED. 2L72 4T RTA24CE 20040105001702004010500170CE 2004 1 5 AMWA95 120031216A143050420066380 RIVET BEECH 1900 1900D 1154162CE FUSELAGE SHEARED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE HEAVY ANGLE HAD ONE SHEARED RIVET. 2L72 4T RTA24CE 20040105001722004010500172WP 2004 1 5 ARWA20031206 120031218A2612P1136P CONNECTOR DOUG DC8 DC863F 302198FWP NR 2 ENGINE DAMAGED A ARWAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SO19906R 46087 MASTER FIRE WARNING ILLUMINATED NR 2 FIRE SHUTOFF LEVER LIGHT ON, DISCHARGED BOTH FIRE BOTTLES. THREE ENGINE APPROACH AND LANDING WAS COMPLETED. DURING TROUBLESHOOTING FOUND NR 2 ENGINE FIRE WARNING CONNECTION P1-136 DAMAGE. REMOVED AND REPAIR CONNECTION IAW MM 20-50-1. OPS CHECK IAW MM 26-10-0, FOUND NORMAL. CHECKED ON ENGINE RUN-UP, CHECKED SATISFACTORY. REMOVED AND REPLACED NR 1 POS AND NR 2 POS FIRE EXTINGUISHING AGENT, TESTING AND FUNCTIONAL CHECKED SATISFACTORY. ALL SYSTEMS TESTED, AND AIRCRAFT RETURNED TO NORMAL. 2L74 4F 4A25 20040105001792004010500179NM 2004 1 5 AWXA200301623 120031210A53116546533 FRAME BOEING737 737301 1384611NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK A HOLE WAS FOUND CHAFED THROUGH FRAME AT BS 500A BETWEEN STR 1 LT AND STR 1 RT. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 500A BETWEEN STR 1 LT AND STR 1 RT; FABRICATED 2 EACH REPAIR CHANNELS AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG 201 PG 202. 2L72 4F RTA16WE 20040106000102004010600010WP 2004 1 6 DHL2003802576 120031204A5751 HINGE FITTING DOUG DC8 DC873 302199CWP LT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 NR 6 LEFT AILERON HINGE FITTING CRACK. REMOVED NR 6 LEFT AILERON HINGE FITTING IAW MM 20-16-0 PG 208. REFER TO JC 8-27-11-026 FOR NEW NR 6 LEFT AILERON HINGE FITTING INSTALLATION. 2L74 4F RT4A25 20040106000112004010600011WP 2004 1 6 DHL2003802564 120031213A573056110012 SKIN DOUG DC8 DC873 302199CWP RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA XW 5.000 - XW 33.000. REMOVED AND REPLACED RIGHT WING T/E UPPER PANEL (STA XW 5.000 - XW 33.000) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040106000362004010600036WP 2004 1 6 GTIA030914 120031031A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND DENT AT FS 328 AT L24R, DENT HAS PREVIOUSLY INSTALLED FASTENERS WITH IMPROPER RIVET PITCH, AND REQUIRES REPAIR. CUT OUT DAMAGED AREA. FABRICATED NEW -15 SKIN SECTION, -19 FINGER DOUBLER, AND -5 DOUBLER. INSTALLED REPAIR PARTS. (M) 2L72 4F RTA6WE 20040106000562004010600056NM 2004 1 6 AWXA200301562 120031209A5315D5347218820200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1193, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM AT FR 68, Y1193, Z240; RECEIVED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20040106000572004010600057NM 2004 1 6 AWXA200301563 120031209A5315D5347217220390 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 MCN - MAJOR REPAIR - DURING C-04 CHECK 4 AREAS OF GALVANIC CORROSION WERE FOUND ON FLOORBEAM 279MM AFT OF FR 67 AT Y1219, 431MM AFT OF FR 67 AT Y1143, 330MM AFT OF FR 67 AT Y1143, AND 220MM AFT OF FR 66 AT Y1292, Z240. MAINTENANCE REMOVED AND REPLACED FLOORBEAM FROM BS 31030 TO BS 33200, Y1143 TO Y1292, Z240 IAW A319 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20031231000252003123100025NE 2003 12 31 AMTA200301447 220031201A7323 GOVERNOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE NR 2 ENGINE MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11520AT 27976 DURING SHUTDOWN, NR 2 RT ENGINE WOULD NOT SHUTDOWN WITH FUEL CONTROL SHUTOFF SWITCH IN CUT OFF POSITION. ALSO, NR 2 ENGINE WOULD NOT SHUT DOWN WITH NR 2 FIRE HANDLE PULLED. ENGINE SHUT DOWN AFTER CYCLING SWITCHES. PERFORMED FIM 73-21-00. REMOVED AND REPLACED FUEL FLOW GOVERNOR SOLENOID VALVE PER MM 73-21-15-4. OPS CHECK GOOD, AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA2NM E12EU 20040112000602004011200060NM 2004 1 12 DHL2003780015 120031219A5270 SWITCH BOEING727 727223 1384074NM PAX DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01780DH 22006 DURING TAXI IN FORWARD ENTRY DOOR LIGHT ILLUMINATED. ADJUSTED DOOR UNLATCH SWITCH OUT FURTHER IAW BMM CHAPTER 52-11-01, OPS CHECKED GOOD. 2L73 4F A3WE 20040112000702004011200070NM 2004 1 12 QXEA200301572 120031218A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY WILL NOT TEST A QXEAO OTHER L NO TEST UKUNKNOWN 1 NM09362PH325933022 518 BOI - FLIGHT 2209 - NR 2 BAGGAGE SMOKE WARNING TEST DOESN’T CHECK. MAINTENANCE REPLACED THE NR 2 SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040112000842004011200084NM 2004 1 12 AWXA200301574 120031203A531065458715 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON AFT SIDE OF R-1 DOOR FRAME, 3RD STOP CUTOUT FROM THE BOTTOM AT INBOARD SIDE, BS 327, STR 12 RT. MAINTENANCE REMOVED DAMAGE AT AFT SIDE OF R-1 DOOR FRAME, 3RD STOP CUTOUT FROM THE BOTTOM BS 327, STR 12 RT; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11 FIG 1, PG 1-6. 2L72 4F RTA16WE 20040112001302004011200130 2004 1 12 2004F00031 420030925A61228210261 GOVERNOR CASA C212 C212CC 2410204EU NR 1 ENGINE STICKING A EHAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 AL03423CA 240 NR 1 ENGINE STUCK AT 102 PERCENT RPM, COULD NOT SET CRUISE TQ WITHOUT RPM CLIMBING TO 104 PERCENT RPM. A/C RETURNED TO SKBO AND LANDED. (M) 2H72 4T A43EU 20040112001422004011200142NM 2004 1 12 CALA0300719 120031222A5320 STIFFENER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 INSPECTION FOUND CHANNEL STIFFENER ON AFT PRESSURE BULKHEAD CORRODED AT STA 1016, BL 0, BETWEEN S27L AND S27R. THE STIFFENER WAS REPAIRED IAW BOEING DRAWING 65C28106 AND EA 5310-04045, OPERATION 2. 2L72 4F RTA16WE 20040112001452004011200145NE 2004 1 12 UIEA200300066 220031114A7261 ENGINE BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 3 LEAKING A UIEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15524MC 21784 517591 DOV-RMS - NR 3 ENGINE SHUTDOWN DUE TO ZERO OIL QUANTITY AND PERSSUER BELOW 10 PSI WITH LOW OIL PRESSURE LIGHT ON AT 1509Z. AFTER SHUTDOWN OIL PRESSURE WENT TO ZERO WHILE WINDMILLING. AIRCRAFT DIVERTED TO AMS. REMOVED AND REPLACED ENGINE NR 3 ACCORDING TO MM 71-00-02 AND ATLAS AIR FORM 01-AA-45 PAGE 1 TO 68. ACCOMPLISHED ENGINE RUN, ALL PARAMETERS CHECK NORMAL. (M) 2L74 4F4 FRTA20WE E23EA 20040113000372004011300037 2004 1 13 BAQA090686 420031107A237093A10083 RECORDER LEAR 55 55LEAR 5170702CE COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 11343 092 VOICE RECORDER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 11/11/03 2L72 4F A10CE 20040113000602004011300060EU 2004 1 13 MALA030565 120031204A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4K INSPECTION, FS 630 TO 686 LEFT O/B SEAT TRACK HAS CORROSION. REMOVED AND REPLACED CORRODED SEAT TRACK SECTION FROM FS 630 TO FS 686 IAW MESABA EO S 53060 DATED NOV 3, 2003 REV II. 2L72 4T RTA52EU 20040113000742004011300074EA 2004 1 13 03358687 120031224A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27687BR 7720 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040113000822004011300082SW 2004 1 13 BAQA091650 120031222A2435200SGL124Q STARTER GEN BELL 230 230 1182149SW ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03870SF 23018 STARTER GEN PRODUCING LOW STARTING SPEED, SPARKS ON STARTUP, LOUD RADIO NOISE. PART REPLACED WITH SERVICABLE UNIT. 1G72 3U NCH9SW 20040113000832004011300083NM 2004 1 13 AWXA200301595 120031206A53136545767512 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER 16 LT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE TRIMMED OUT CRACK ON STRINGER 16 LT AT LIGHT ASSEMBLY BS 500C; FABRICATED A REPAIR CHANNEL AND RADIUS FILLER; INSTALLED REPAIR PART IAW AWA ER 03-5312-01094-DD1. 2L72 4F RTA16WE 20040113000942004011300094WP 2004 1 13 UPS03841670 120031222A29107614032716 HYDRAULIC LINE DOUG DC8 DC871F 302199DWP HYD SYSTEM RUPTURED A IPXAA UNSCHED LANDING KF FLUID LOSS FLT CONT AFFECTED CRCRUISE 1 SO01798UP 45898 INSPECTION TYPE:N/A IN FLIGHT HYD QT INDICATOR DROPPED RAPIDLY TO AUX LEVEL. RAN CHECK LIST TO ISOLATED LOSS. QUANTITY REMAINED AT AUX LEVEL, BUT AFTER CONFIGURING FOR LANDING (LAST 5 MINUTES) QUANTITY DROPPED TO ZERO. PRESSURE FELL OFF AFTER LANDING. FOUND HYD LINE RUPTURED AT PITCH TRIM CONTROL VALVE (IPC 27-40-00/040 ITEM 35). REMOVED DAMAGE LINE AND INSTALLED FLEX LINE. DEFER CONTROL D273079. 2L74 4F RT4A25 20040113001052004011300105EU 2004 1 13 BAQA091406 120031208A243523081043 STARTER GEN BOLKMSBK117 BK117C1 5626025EU ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY537 7544 STARTER WILL NOT ROTATE. REPLACED WITH SERVICEABLE UNIT. UNIT BEING RETURNED DIRECT. 12/9/03 1G72 3U NCH13EU 20040113001152004011300115NM 2004 1 13 F3LA200300185 120031219A3520S417T40127 OXYGEN BOTTLE BOEING737 73736N 1384408NM CABIN DISCHARGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 28563 DURING C-7 CHECK, INSPECTION REPORTED SEAT 7 ABC OXYGEN CANISTER DISCHARGED. REPLACED OXYGEN GENERATOR CANISTER PER MM 35-22-11, PAGE 201, STEPS 1-3 AND MM 35-22-11, PAGE 401, STEPS 1-3. 2L72 4F RTA16WE 20040113001252004011300125NM 2004 1 13 03FDEA02250 120031226A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING O/B FLAP I/B FWD HINGE LOWER AFT MOUNT MATING SURFACE CORRODED. REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DRAWING ARC0502 IN ACCORDANCE WITH FEDEX EA 1-5750-75208, TRAILING EDGE AND TRAILING EDGE DEVICES, LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113001392004011300139NM 2004 1 13 03FDEA02260 120031226A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, O/B FLAP I/B FWD HINGE ACTUATOR MOUNT O/B LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75209, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113001512004011300151NM 2004 1 13 AWXA200301604 120031225A33501012721 LIGHT BOEING737 737277 1384570NM CABIN DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 PHX - EEL - DURING A-01 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT WAS FOUND HANGING FROM SEAT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH SEAT LIGHT ASSEMBLY AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040113001522004011300152NM 2004 1 13 AWXA200301605 120031208A531565528942 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND AT RT CENTER FLOORBEAM T-CAP ANGLE BS 540, BL-0. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 540, BL-0; FABRICATED A NEW REPLACEMENT T-CAP ANGLE PER DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 16 PG 1. 2L72 4F RTA16WE 20040112000962004011200096WP 2004 1 12 GTIA031018 120031129A5320 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND LONGERON 28L END FITTING CORRODED AT APB. REMOVED END FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20040112001132004011200113WP 2004 1 12 ZIAA03004 120031103A57308005501 PANEL LKHEED188 188A 5262602WP RT WING CRACKED A K NONE O OTHER ININSP/MAINT 1 GL23346HA 188A1043 CRACK NOTED IN CENTER DRY BAY RIGHT WING AT PLANK SEAM 5-6 AT BL37R. ROUTED OUT CRACK AND INSTALLED FILLET PER L-188 SRM 51-2-7. REPAIRED PER L-188 SRM 57-2-1 FIG 3 SHEET 15. (M) 2L74 4T RT4A22 20040112001572004011200157WP 2004 1 12 GTIA031000 120031115A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN FLOOR SUPPORTS CORRODED THREE AT FS 160 15 INCHES, 32 INCHES, AND 42 INCHES LBL. MATERIAL LOSS ON CABIN FLOOR SUPPORT FS 160 15 INCHES AND 42 INCHES LBL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED TWO CABIN FLOOR SUPPORT AT FS 160 15 INCHES AND 42 INCHES LBL. (M) 2L72 4F A6WE 20040112001682004011200168NM 2004 1 12 03FDEA02227 120031223A5744 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, INBOARD FLAP OUTBD HINGE FITTING OUTBOARD PIVOT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75213 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBOARD. FLAP HINGE BRACKET REPAIR 2L73 4F RTA22WE 20040112001692004011200169WP 2004 1 12 GTIA031017 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT COCKPIT FLOOR PANEL, EDGE BROKEN, METAL L ANGLE BRACKET CORRODED, PLASTIC BARRIER BROKEN. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040112002002004011200200NM 2004 1 12 2003UALA00957 120031214A2422 STATIC INVERTER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN OVERHEATED A UALAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29944UA 26683 DIVERTED TO IND DUE TO ELECTRICAL BURNING ODOR IN CABIN. STATIC INVERTER REMOVED AS SOURCE OF ODOR, REPORTED UNIT EXTREMELY HOT. REPLACED WITH SERVICABLE UNIT FROM STOCK, CHECKS GOOD. 2L72 4F4 FRTA16WE E2GL 20040112002612004011200261WP 2004 1 12 AALA20031453 120031221A3397 WIRE DOUG DC9 DC983 3022083WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21969TW 53619 AFT ACCESSORY RAMP AREA EMERGENCY PATH AISLE LIGHT INOPERATIVE. CONNECTED LOOSE WIRES TO AFT ACCESSORY RAMP AREA EMERGENCY PATH AISLE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040112002642004011200264WP 2004 1 12 AALA20031416 120031214A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21556AA 53086 DFW SEAT MOUNTED EMERGENCY LIGHT AT 7D INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20040113000112004011300011EU 2004 1 13 BAQA091301 120031120A65204649001007 GEARBOX UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE TAIL ROTOR MAKING METAL W BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH1679 0131 TAIL ROTOR GEARBOX IS MAKING METAL. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. PART BEING RETURNED. 1G72 3U3 U H88EU E34NE 20040113000762004011300076EU 2004 1 13 BAQA091321 120031203A7430L311M1009103 SWITCH UROCOPEC135 EC135T1 5620026EU NR 2 FADEC INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME1573 132 NR 2 FADEC SWITCH FAILED INTERMITTENTLY. PART REPLACED WITH SERVICABLE UNIT. 01/07/2004 1G72 3U H88EU 20040113000772004011300077EU 2004 1 13 ERAA091808 120030916A3212D24762102 FLOAT BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL MLG LEAKING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03292EH1102 562 FLOAT BAG LEAKING AT BULKHEAD NR 3. SENT TO OFFSHORE HELICOPTERS FOR REPAIR IAW OHSS 100-1 AND C/W INSPECTION IAW 25-60-95. 1G72 3U3 U H3EU E4CE 20040113000782004011300078EU 2004 1 13 03FDEA02240 120031223A3240 CONTROL LEVER AIRBUS310 A310 EU BRAKE SYS FAULTY A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25405FE 237 DURING TAKEOFF ROLL, GOT TAKEOFF CONFIGURATION WARNING WITH ECAM PARKING BRAKE ON WARNING. REJECTED TAKEOFF PRIOR TO TAKEOFF. TAKEOFF CONFIG CHECK SHOWED NORM FOR T/O. NOTE ACARS FLIGHT LOG PAGE NEVER SHOWED BLOCK OUT. REMOVED AND REPLACED 7GG PARKING BRAKE CONTROL LEVER & SWITCH ASSY, RIG AND OPS CHECKED REF AMM 32-45-11-4 AND OPS CK AMM 32-45-00-5 & 32-42-00-5. 2L72 4F RTA35EU 20040113000812004011300081NM 2004 1 13 03FDEA02242 120031223A5753 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, OUTBOARD FLAP VANE NR 4 T-FITTING ECCENTRIC HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75216, TITLE: WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP NR 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20040113001242004011300124NM 2004 1 13 03FDEA02249 120031226A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING O/B FLAP I/B FWD HINGE SIDE SUPPORT MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75208, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113001432004011300143EU 2004 1 13 BAQA089978 120031017A6220365A31199802 PITCH HORN AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR CORRODED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911UF 6338 PITCH HORN HAS PITS IN BOLT HOLES. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H10EU E19EU 20040113001552004011300155NM 2004 1 13 QXEA200301579 120031225A32605352011 PANEL DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09363PH9714 1307 520 SEA - FLIGHT 2105 - THE LANDING GEAR DID NOT GIVE A GREEN NOSE DOWN INDICATION WHILE ON APPROACH. THE BULB WOULD NOT TEST. THE CREW BROUGHT THE GEAR BACK UP AND THEN RELOWERED. THE EXTENSION AND ALL INDICATIONS WERE NORMAL. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED SEVERAL EXTENSION AND RETRACTION CHECKS. ALL INDICATIONS AND CHECKS WERE NORMAL WITH NO DEFECTS NOTED. THE LANDING GEAR SELECTOR PANEL WAS REPLACED AS A PRECAUTION. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040113001582004011300158EU 2004 1 13 BAQA091477 120031211A6320 BEARING UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE LEVER WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME800 0009 BEARINGS AND BUSHINGS WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 UO H88EU E42NE 20040113001662004011300166EU 2004 1 13 I05R091297 120031008A6321L635M1021001 CALIPER UROCOPEC135 EC135P1 8680990EU ROTOR BRAKE FAILED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05552BA214 190 ROTOR BRAKE CALIPER UNIT FAILURE, REPLACED PART. 1G72 3U O H88EU 20040113001672004011300167WP 2004 1 13 AALA20031467 120031223A339702501720003 WIRE HARNESS DOUG DC9 DC982 3022082WP CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 DFW SEAT 22 EMERGENCY SEAT MOUNTED LIGHTS INOPERATIVE. REPLACED LIGHT HARNESS AT SEAT 22. SYSTEM GROUND CHECK NORMAL OPERATION. 2L72 4F A6WE 20040113001942004011300194WP 2004 1 13 AALA20031234 120031106A2910 HYDRAULIC SYSTEM DOUG DC9 DC983 3022083WP RIGHT LEAKING A AALAO OTHER K FLUID LOSS CRCRUISE 1 SW21597AA 53287 ORD - EN ROUTE LGA-LAX - RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. LANDED ORD WITHOUT INCIDENT. AUXILIARY TRANSFER PUMP TURNED ON FOR LANDING AND TURNED OFF AFTER LANDING. (M) 2L72 4F RTA6WE 20040113002442004011300244NM 2004 1 13 QXEA200301314 120031021A1430 RIVET DHAV DHC8 DHC8202 2809007NM LT ELEVATOR LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - ROW OF SIX (6) SMOKING RIVETS AT INBOARD END OF LEFT HAND ELEVATOR LOWER SURFACE. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20040113002472004011300247NM 2004 1 13 QXEA200301497 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- NR 5 SEAT TRACK HAS SURFACE CORROSION IN BOTTOM OF CHANNEL FROM 6 TO 9 INCHES AFT OF X510. REPAIRED IAW DHC-8 SRM 51-20-16, 51-00-06 AND RD 8-53-1339. 2H72 4T RTA13NM 20040113002532004011300253NM 2004 1 13 QXEA200301285 120031011A5210 BRACKET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE PAX DOOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-BRACKET FOR PASSENGER DOOR LOWER FORWARD STOP BOLT HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-36. 2H72 4T4 TRTA13NM E20NE 20040114000042004011400004NM 2004 1 14 03FDEA01909 120031108A5712 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT WING LEADING EDGE NR 16 SLAT TRACK INBOARD RIB WITH CRACK. LT WING LEADING EDGE NR 16 SLAT TRACK INBOARD RIB CRACK REMOVED & REPLACED AS PER SRM51-31-01VOL2 & SRM513301VOL 2. 2L73 4F RTA22WE 20040114000082004011400008EA 2004 1 14 QXEA200301425 120031115A261247359719 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09615QX2485 2360 10065 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED AFT SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040114000102004011400010NM 2004 1 14 03FDEA01926 120031117A5511 SPAR CAP DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STABILIZER RT UPPER AFT SPAR CAP NR 36R BARREL NUT BORE FOUND CORROSION ON BOTTOM AND SIDEWALL SURFACES BEYOND EO 1- 5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-74245, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000 2L73 4F4 FRTA22WE E13NE 20040114000122004011400012NM 2004 1 14 03FDEA01924 120031117A5510 STRUCTURE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STABILIZER LT UPPER FWD PLANK NR 5L BARREL NUT BORE FOUND CORROSION ON BOTTOM SURFACE BEYOND EO 1-5510-7-5000 LIMITS. HORIZONTAL STAB LT UPPER FWD PLANK NR 5L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245. HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. 2L73 4F4 FRTA22WE E13NE 20031229000842003122900084NM 2003 12 29 DHL2003742504 120031130A5720 SUPPORT ANGLE BOEING727 727225 1384077NM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, N/R 60546 LT WING PLANK FAIRING SUPPORT ANGLE AT NR 3 FLAP TRACK PORTION IS CRACKED WBL 203 AND SPOILER BEAM. CUT OUT DAMAGED AREA AT NR 3 FLAP TRACK MOUNT DIMENSIONS 5.5 INCH X 3 INCH AND FABRICATED ONE FILLER DIMENSION AND FABRICATED ONE STRAP 12 INCH X 1 INCH AND ONE SHIM 6.5 INCH X 1 INCH AND ONE ANGLE FILLER 2.5 INCH X 5 INCH USING 7075 T6 .063 PO 900226 IAW B-727 SRM 51-40-3 FIG 1 AND 57-20-2 FIG 4. INSTALLED REPAIRS AT NR 3 FLAP TRACK IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20031229001032003122900103NM 2003 12 29 AWXA200301547 120031204A532265496525 ANGLE BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN RADIUS OF AFT MOUNT ANGLE OF L-1 DOOR UPPER LINER ATTACH PAN ASSEMBLY BS 316, STR 6 LT. MAINTENANCE REMOVED CRACKED AFT MOUNT ANGLE BS 316, STR 6 LT; RECEIVED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1, FIG 8. 2L72 4F RTA16WE 20031229001212003122900121NM 2003 12 29 SWAA032727 120031214A57436567172 FITTING BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 WALKING BEAM OUTBOARD FWD HANGER FITTING ON REAR SPAR HAS CORROSION IN THE BORE. REPAIRED FITTING PER EA. 2L72 4F RTA16WE 20031229001272003122900127EA 2003 12 29 MASA200300479 120031206A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717275 7275 FWD CABIN OVERHEAD EMERGENCY LIGHT INOP. MX RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20031229001402003122900140NM 2003 12 29 SWAA032735 120031214A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 DURING SCHEDULED C4 CHECK, FOUND EEPLS FLOOR TRACK CRACKED AT ROWS 3, 12, 16 AND 17. REMOVED AND REPLACED EEPLS FLOOR TRACK PER MM. 2L72 4F RTA16WE 20031229001592003122900159EA 2003 12 29 SWIA200312664 120031205A7120 BEAM CNDAIRCL600 CL6002B19 1900309EA LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 ENGINE SUPPORT BEAM LOWER WEB LT SIDE LBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'' AND RII 53-401. 2L72 4F RTA21EA 20031229001792003122900179EA 2003 12 29 SWIA200312674 120031207A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07431SW 7536 AT 800 FT AFTER TAKEOFF, BOTH STAB TRIM CHANELS DISENGAGED (AND MACH TRIM), FOLLOWED QRH PROCEDURE, COULD NOT CLEAR MSGS. RETURNED TO DFW. PERFORM SYSTEM CHECK ON HSTCU. SYSTEM CHECK OF HSTCU, PERFORMED NORMALLY. OPERATED STAB TRIM & MACH TRIM. BOTH SYSTEMS CHECK GOOD IAW CL 600 MM 27-40-00. COULD NOT DUPLICATE SQUAWK. 2L72 4F RTA21EA 20031223001152003122300115EU 2003 12 23 AWXA200301530 120031211A3232114122010 ACTUATOR AIRBUS320 A320231 3930325EU ZONE 190 FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28622AW6407 054 ON CLIMBOUT, EN ROUTE, WHEN MLG SELECTED UP, RECEIVED ECAM MESSAGE THAT MLG DOORS WERE NOT CLOSED. RECYCLED MLG & NEW ECAM MESSAGE APPEARED FOR MLG NOT UPLOCKED, LOWERED MLG & RETURNED. MAINT PULLED UP PREFLT REPORT MLG NOT UPLOCKED. FAILURE MESSAGE RT MLG DOOR OPEN PROX SENSOR 34GA TARGET POSITION, & 32GA. MAINT ADJUSTED BOTH 32GA & 34GA PROX SENSORS, R & R RT MLG DOOR ACTUATOR IAW AMM 32-31-35-401, OPS & LEAK CHECK GOOD. VENDORS FUNCTIONAL TEST OF RT MLG DOOR ACTUATOR S/N DH070399 WAS NO FAULT FOUND. VISUAL INSPECTION DID FIND 2 EACH BEARINGS MIGRATED LOOSE, R & R 2 EACH BEARINGS IAW CMM 32-31-35, REV. 12. 2L72 4F RTA28NM 20031223001392003122300139CE 2003 12 23 DXTA200300189 120031127A2710666000164 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07630QS 5605130 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001572003122300157EA 2003 12 23 A6WA200340171 120031116A2150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA A/C PACK FALSE ACTIVATIONA A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31432AW 7257 RIGHT PACK HI PRESSURE CAUTION MESSAGE. PERFORMED PACK OPS CHECK WITH ENGINES IAW AMM 21-50-863-805 AND PERFORMED OPS CHECK IAW AMM 21-50-863-801. OPS CHECK GOOD. OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031223001722003122300172EA 2003 12 23 ASOA03545 120031029A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11862AS 7445 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20031224000292003122400029WP 2003 12 24 ASAA0380622 120031007A53219936599511 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOORBOARD IS CORRODED BETWEEN FS 598-636. REPLACED FLOORBOARD PER SRM 53-24-0. (M) 2L72 4F RTA6WE 20031229000022003122900002NM 2003 12 29 VNAA0311011 120031128A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07423JS 3032 THE CREW REPORTED A LAV SMOKE FAIL INDICATION. MAINTENANCE THEN DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH 26-3 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031229000482003122900048NM 2003 12 29 AALA20031418 120031214A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21347AN 33086 EMERGENCY LIGHT INOPERABLE AT SEAT 20B. REPLACED LIGHT ASSEMBLY AT SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031229000572003122900057NE 2003 12 29 QXEA200301551 220031213A7532GG670800025 BLEED VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 ENGINE INOPERATIVE A QXEAK NONE J WARNING INDICATION DEDESCENT 1 NM09603QX4527 10011 PDX FLIGHT 2452 ON DESCENT INTO PDX RIGHT COWL ANTI ICE AND RIGHT BLEED CAUTION MESSAGE ILLUMINATED. ANTI ICE SYNOPTIC PAGE SHOWED RIGHT BLEED VALVE AND RIGHT ENGINE ANTI ICE VALVES CLOSED. PERFORMANCE OF RIGHT COWL ANTI ICE AND RIGHT BLEED CAUTION MESSAGE CHECKLISTS CAUSED MESSAGES TO EXTINGUISH. REPLACED NR 2 PRSOV. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040114000142004011400014NM 2004 1 14 2003UALA00826 120031102A2150 ACM BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE RIGHT SEIZED A UALAJA DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29795UA 26927 RT AIR CYCLE MACHINE CMC MESSAGE AND SMOKE ODOR REPORTED IN CABIN. SMOKE & ODOR REPORT IN THE CABIN WAS DUE TO HAZE & ODOR OF HOT METAL RELEASED BY SEIZED RT ACM. SUSPECT RT ACM FAILURE WAS DUE TO CLOGGED RT COND/REHEATER. RT ACM & RT COND/REHEATER WERE REPLACED. RH ACM: HAM. STD P/N 810209-4, S/N: 950972, PTT: 25,922 HRS, PTC: 3,999. CONDITION: SEIZED. RT CONDENSER/REHEATER: HAM. STD P/N 810210-1, S/N: 9708173, PTT: 26,255 HRS, PTC: 4079. CONDITION: DIRTY. 2L72 4F4 FRTT0001SE E46NE 20040114000162004011400016NM 2004 1 14 2003UALA00838 120031104A335060243 LAMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29307UA 23668 AFT CABIN EEL LIGHTS INOP ROW 16 TO AFT GALLEY. REPLACED EEL LIGHT AT SEAT 30C. 2L72 4F4 FRTA16WE E2GL 20040112001592004011200159WP 2004 1 12 GTIA030997 120031211A3350 LIGHT DOUG DC9 DC981 3022081WP TAIL CONE INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 MCO - FOUND EMERGENCY LIGHT OVER SLIDE IN TAIL CONE INOPERATIVE. CLEAN ALL SOCKET CONTACTS AND TERMINAL ENDS, OPS CHECK OK. (M) 2L72 4F A6WE 20040112002092004011200209EU 2004 1 12 2003UALA00963 120031216A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29459UA 1192 ROW 21 ABC ESCAPE PATCH EEL LIGHT IS INOPERATIVE. REPLACED EEL PATCH LIGHT. 2L72 4F4 FRTA28NM E40NE 20040113000202004011300020 2004 1 13 BAQA091640 420031223A2210117884141 CONTROL UNIT BOLKMS117 BK117A4 5626017EU AUTOPILOT FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA039024Z 7134 UNIT FAILED OUT OF BOX UPON INSTALLATION REPLACED WITH SERVICABLE ASSET. 1G72 3U H13EU 20040113000462004011300046EU 2004 1 13 BAQA091054 120031112A67307012409901 ACTUATOR BOLKMSBK117 BK117C1 5626025EU DUPLEX PITCH MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP3130 7508 ACTUATOR OSCILLATES WHEN ENGAGED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20040113000702004011300070EA 2004 1 13 033286257 120031124A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING HEAVY CHECK INSPECTION THE FLOORBEAM AT FS 335 LBL 9 WAS IDENTIFIED CORRODED. FLOOR BEAM WAS REPAIRED PER SRM AND AIRCRAFT WAS RELEASED FOR SERVICE UPON COMPLETION OF HEAVY CHECK INSPECTION. 2L72 4F RTA21EA 20040113000882004011300088NM 2004 1 13 AWXA200301600 120031219A5320146N5140 INTERCOSTAL BOEING757 7572G7 1384963NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK A 3 INCH CRACK WAS FOUND ON CABIN FLOOR INTERCOSTAL BS 780-800, BL-0. MAINTENANCE REMOVED CRACKED INTERCOSTAL BS 780-800, BL-0-; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51, FIG 204, PG 214-215. 2L72 4F RTA2NM 20040113001162004011300116NM 2004 1 13 F3LA200300186 120031219A5320 INTERCOSTAL BOEING737 73736N 1384408NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED MAIN DECK FLOOR INTERCOSTAL CRACKED BETWEEN STA 294 AND STA 312 AT RBL 32. REPLACED DAMAGED UPPER CHORD OF FLOOR INTERCOSTAL PER SRM 51-40-2. 2L72 4F RTA16WE 20040113001442004011300144NM 2004 1 13 03FDEA02277 120031226A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT WING - OUTBD FLAP OUTBD HINGE ACTUATOR INBD MOUNT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, TRAILING EDGE AND TRAILING EDGE DEVICES- RT OUTBD FLAP, OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040113001482004011300148SO 2004 1 13 C2XA03TY217 120031224A75408166243 SENSOR EMB 135 EMB135LR 3260305SO BLEED AIR SYS FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2717524 145399 TYS, AIRCRAFT DIVERTED INTO TYS FOR A BLEED 1 OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE FAN AIR CONTROL SENSOR, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040113001492004011300149EU 2004 1 13 BAQA091232 120031121A6420105317381 SLEEVE BOLKMS117 BK117A1 5626010EU TAIL ROTOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME6563 7243 TAIL ROTOR SLEEVE WORN IN O-RING CONTACT AREA. CORROSION INSIDE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20040113001722004011300172CE 2004 1 13 ACE122403 120031224A781011895002331 EXHAUST DUCT BEECH 1900 1900C 1154161CE NR 1 ENGINE DISCONNECTED E YADAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 AL03111AX UC81 PILOT REPORTED EXHAUST SMELL IN CABIN ON TAKEOFF AND CLIMB. MAINTENANCE LOCATED A DISCONNECTED NR 1 ENGINE INTAKE HEATED LIP (EXHAUST DUCT) TUBE. EXHAUST COULD HAVE BEEN INGESTED BY THE ENGINE AND THEN MIXED WITH THE BLEED AIR. NO PART FAILURE WAS OBSERVED. 2L72 4T RTA24CE 20040113001782004011300178SO 2004 1 13 RAIA00311294 120031123A361014531637003 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS WORN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03818HK 145059 STL- BLEED 2 LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED O-RINGS LOWER FUSELAGE BLEED LINE. 2L72 4T RTT00011AT 20040113002402004011300240NM 2004 1 13 QXEA200301300 120031021A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM AFT PAX DOOR DIRTY A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09402QX 4032 PDX-AFT PASSENGER DOOR IS JAMMED, WILL NOT OPEN. CLEANED AND LUBED AFT PASSENGER DOOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040114000192004011400019 2004 1 14 2003UALA00843 420031106A25651341W18131202 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE GIRT BAR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29770UA 26925 DOOR 2R WAS DIFFICULT TO DISARM AND OPEN. GIRT BAR LIFT MECHANISM AFT BRACKET WAS FOUND TO BE BROKEN IN THE RADIUS. REPLACED BRACKET PER AMM 52-11-17. 2L72 4F4 FRTT0001SE E46NE 20040114000312004011400031SO 2004 1 14 C2XA03CL213 120031226A33501317 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714542 145547 DURING ROUTINE MAINTENANCE THE LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT AFT LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040114000492004011400049NE 2004 1 14 DLM88030964 220031028A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 FAILED A DALAAF UNSCHED LANDING ACTIVATE FIRE EXT. R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO27973DL29641 53241 725945 CLIMBING THRU 180 RIGHT ENGINE LOST POWER, NO FIRE INDICATION. REDUCED THRUST AND LANDED. UPON LANDING FIRED BOTH BOTTLES. REPLACED NR 2 ENG S/N 725945 PER TRANS 9T102. ALSO REPLACED BOTH FIRE BOTTLES, SEPARATE LOG ITEM. 2L72 4F4 FRTA6WE E9NE 20040114000552004011400055NM 2004 1 14 DL73S030970 120031029A5551 ATTACH FITTING BOEING737 737232 1384475NM HORIZ STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27324DL 23096 DURING INSPECTIONS PER EO 03-069697-03 AND 03-053025-03AD THE HORIZ STAB ATTACH FITTINGS, SEVERAL LUG BORES WERE OVERSIZED TO REMOVE CORROSION. CORROSION DAMAGE WAS CLEANED UP AND REWORKED PER ERA 38580314AD. 2L72 4F RTA16WE 20040114000622004011400062CE 2004 1 14 328031 120031123A2721 WHEEL BEECH 1900 1900D 1154162CE RUDDER TRIM LOCKED A NSVAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27221CJ UE221 AIR RETURN DUE TO MANUAL RUDDER TRIM WHEEL LOCKING UP IN CENTER POSITION, PILOTS RUDDER PEDALS RESPONDED NORMAL. 2L72 4T RTA24CE 20040114000652004011400065NM 2004 1 14 DLM88030980 120031105A3610 DUCT DOUG MD88 MD88 3023688NM A/C BAY LEAKING A DALAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SO27973DL 53241 TAIL COMPARTMENT TEMP HI LIGHT CAME ON DURING CLIMB THRU FL250. FOUND HIGH PRESSURE DUCT LEAKING AT CLAMP. SECURED SAME. 2L72 4F RTA6WE 20040114000692004011400069NM 2004 1 14 DL73S030984 120031106A5532 PANEL BOEING737 737232 1384475NM VERTICAL STAB DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312DL 23084 FOUND ON W-1 LETTER CHECK, VERTICAL STAB COMPOSITE T/E PANEL DELAMINATED 2 PLACES LEFT SIDE, 1 PLACE RIGHT SIDE. REPAIRED PER SRM 55-30-3 FIG 3. 2L72 4F RTA16WE 20040114000792004011400079NM 2004 1 14 03FDEA01959 120031119A2782651781822 ACTUATOR BOEING727 727200 138407ENM ZONE 500 FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25216FE1833 157 22937 ON PUSHBACK MEM AFTER DISCONNECT WITH A PUMPS ON, L/E FLAPS REMAINED UNSAFE. CYCLED FLAPS 2-5 DEGREES WENT GREEN. CYCLED FLAPS BACK UP, UNSAFE WENT OUT. PASSING 10K UNSAFE L/E FLAPS RE-ILLUMINATED. CYCLED DOWN AND BACK LIGHT WENT OUT. PASSING 19K, UNSAFE L/E FLAP RE-ILLUMINATED RETURNED TO MEM. LOWERING FLAPS FOR LANDING, L/E FLAP UNSAFE OUT SELECTING FLAPS 5. REMAINS UNSAFE FLAPS 2 OPERATED L/E SEVERAL TIMES. L/E FLAP LIGHT REMAINED LIT WHEN SLATS WERE UP. CHECKED LED PANEL AND CONFIRMED NR 4 SLAT NOT UP INDICATION. T/S PER WDM AND DETERMINED NR 4 SLAT ACT SW IS BAD. REMOVED AND REPLACED NR 4 SLAT ACT REF 727-200MM 27-81-032-4, OPS CHECKS GOOD AT THIS TIME. 2L73 4F RTA3WE 20040114000832004011400083NM 2004 1 14 QXEA200301474 120031119A49504951960 FILTER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09400QX 4030 PDX-ON FLIGHT NUMBER 2310, APU BLEED AIR UNUSEABLE DUE TO FOUL MUSTY ODOR. NO ODOR USING ENGINE BLEED AIR. REMOVED AND REPLACED FUEL FILTER ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040114000862004011400086NM 2004 1 14 DL73S031028 120031119A555365474506 FITTING BOEING737 737232 1384475NM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 CORROSION DAMAGE WAS FOUND ON THE VERTICAL STAB NR 2 FIN LUG AND THE NR 11 BODY CLEVIS LUG. CORROSION WAS REMOVED AND REWORKED PER ERA 385810-14. 2L72 4F RTA16WE 20040114000912004011400091NM 2004 1 14 DL777031032 120031119A3350 FUSE BOEING777 777232 1385232NM BATTERY PACK BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27865DA 29737 EMERGENCY CEILING LIGHT AT SEAT ROW 38 IS OUT. FOUND FUSE BLOWN IN BATTERY PACK. REPLACED FUSE EMERGENCY LIGHTS CHECKS GOOD. 2L72 4F RTT00001SE 20040114000952004011400095NM 2004 1 14 DLM88031034 120030519A57545922533503 ATTACH FITTING DOUG MD88 MD88 3023688NM L/E SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27933DL 49720 NR 3 SLAT MIDDLE ATTACH FITTING CRACKED BETWEEN ATTACH POINT AND EDGE OF FITTING 100 PERCENT. REPLACED SAME. 2L72 4F RTA6WE 20040114001002004011400100NM 2004 1 14 DL73S031039 120031121A5551 ATTACH FITTING BOEING737 737232 1384475NM HORIZ STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 DURING ACCOMPLISHMENT OF 03-069697-03 NUMEROUS ATTACHMENT LUGS REQUIRED MACHINING BEYOND THE LIMITS PROVIDED, IN ORDER TO REMOVE ALL CORROSION DAMAGE FOUND. LUGS WERE REWORKED PER INSTRUCTIONS CONTAINED IN ERA 385802-14AD. 2L72 4F RTA16WE 20040114001032004011400103NM 2004 1 14 03FDEA01985 120031126A1430MS21042L08 COLLAR DOUG MD11 MD11 3023602NM FASTENER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 AFT FUSELAGE COMPT: AFT BODY BULKHEAD FRONT FACE STA Y2014 CAN NOT BE FOUND WITH MANY LOCK BOLT COLLARS CRACKED AXIALLY AS MARKED. AFT FUSELAGE COMPT : AFT BODY BULKHEAD FRONT FACE STA Y2014 CRACK FASTENERS REMOVED & REPLACED AS PER SRM 51-33--01 VOL2. 2L73 4F RTA22WE 20040114001072004011400107NM 2004 1 14 XNOA1166 120031127A3097 WIRE BOEING727 727227 1384078NM ANTI ICE SYS CHAFED A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23793A 20774 ON TAXI-OUT ANTI-ICE DUCT OVERHEAT LIGHT CAME ON. TRANSFERRED TO DMI CONTROL 3689 IAW ENA MEL 21-39 CAT-C PLACARDS INSTALLED. REPAIRED CHAFED WIRE AT S157 SWITCH, OPS CK GOOD ON GROUND IAW B727 WD 30-12-03. THIS ACTION CLEARS DMI 3689. PLACARDS REMOVED.(STATUS:ORIGINAL/CLOSED) 2L73 4F A3WE 20031229000762003122900076NM 2003 12 29 03FDEA02197 120031215A2741418575 MOTOR DOUG MD11 MD11 3023602NM HORIZONTAL STAB LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25596FE9552 9552 48554 DURING CLIMB, NEAR TOP OF CLIMB FL360, VMC SMOOTH AIR LEVEL 1 HYD ELEV OFF LVL 2 (HYD 3 QTY LOW) & LVL 2 (HYD 3 FAIL). ALERTS APPEARED COMPLIED WITH RED TABS FOR MANUAL GEAR EXT. ON ARRIVAL A/C HAS HYD OIL LEAK FROM STAB ACCESS COMPT, FOUND CRACK NR 2 TRIM MOTOR HOUSING. REMOVED AND REPLACED NR 2 TRIM MOTOR ASSY, QTY NR 3 SYS IND WAS 0 GAL, PERFORMED HYD FILTER INSPECTION, NO METAL FOUND ON THE GROUND. REMOVED AND REPLACED NR 3 SYS ALL HYD FILTER. REMOVED AND REPLACED LT ENG DRIVE PUMP. 2L73 4F RTA22WE 20031229000812003122900081NM 2003 12 29 DHL2003742502 120031120A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, N/R 59873 CABIN STR 15 R CRACK STA 724D. REMOVED FASTENERS AS REQUIRED FOR ACCESS STR 15R STA 724D IAW B-727 SRM 51-30-2. CUT OUT DAMAGE END OF STR 15R DIM 7 INCHES AND FABRICATED ONE U-CHANNEL DIMENSIONS 1 INCH X 1 INCH X 1 INCH X 4 INCHES USING 7075T6 .040 PO 900226 AND TWO EACH CHIMS 1 INCH X 1 INCH AND 1 INCH X 2.5 INCH USING .080 2024T-3 PO 900103 IAW B-727 SRM 53-10-3 FIG 5. TREATED, ALODINED AND PRIMED ALL REPAIR PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIRS IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20031229001332003122900133EA 2003 12 29 MASA200300464 120031124A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775993 7372 CAPT REPORTED LT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE INOP DURING TEST. MX RELAMPED. OP CHECKS GOOD. 2L72 4F RTA21EA 20031229001622003122900162EA 2003 12 29 SWIA200312667 120031205A5320 SILL CNDAIRCL600 CL6002B19 1900309EA CARGO PIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 CARGO PIT CARGO DOOR FLOOR LANDING SILL IS CRACKED UNDER STEP PLATE ASSY PIN STOP FITTING; FS 576.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 & RII 53-401. 2L72 4F RTA21EA 20031229001782003122900178SO 2003 12 29 SWIA200312673 120031114A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07568SW 120343 LEFT SIDE AFT SECTION OF SEAT TRACK NEEDS TO BE REPLACED DUE TO CORROSION ABOVE SCREW HOLES. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LT SIDE AFT SECTION OF SEAT TRACK AS REQUIRED. 2L72 4T RTA31SO 20031231000182003123100018NM 2003 12 31 TSAA0333052 120030213A335086210066 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13817AL 39735 REPLACED NR 2 FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000352003123100035NM 2003 12 31 TSAA0377041 120030311A7722 PRESSURE SWITCH BOEING737 737230 1384401NM NR 1 ENGINE MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13820AL 22138 DURING TAKEOFF, WITH TAKEOFF POWER SET THE NR 1 ENGINE EPR WAS 0.25 TOO HIGH. THE AIRCRAFT RETURNED TO HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FOD IN THE NR 1 ENGINE PT2 LINE. THE PT2 LINE WAS CLEANED, AND ENGINE PERFORMANCE RUN WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000362003123100036EU 2003 12 31 A6WA200360068 120031209A5753 FLAP TRACK BAC 146 146200A 1500266EU NR 1 WORN A K NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 RT NR 1 FLAP TRACK WEAR UPPER AND LOWER RAILS OUTBOARD FACE. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1734-6070003. LPI C/O ON BLENDED FLAP TRACK AS REQUIRED IAW BARA/AVR/6606/03-DC, NO CRACKS FOUND. (M) 2H74 4F A49EU 20031231000412003123100041NM 2003 12 31 TSAA0225225 120031126A2450 CIRCUIT BREAKER BOEING737 73776N 13844CHNM GALLEY MALFUNCTIONED A TSAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13743AL 28654 EN ROUTE TO HNL, THE CREW COULD NOT GET THE GALLEY POWER TO COME ON. THE AIRCRAFT RETURNED TO OAK AND MADE AN OVERWEIGHT LANDING WITH NO FURTHER INCIDENT. MAINTENANCE RESET THE GALLEY POWER CIRCUIT BREAKERS ON THE P-92 PANEL LOCATED IN THE E/E COMPARTMENT. GROUND OPERATIONAL CHECK FOR THE FORWARD AND AFT GALLEYS WERE GOOD. AN OVERWEIGHT LANDING INSPECTION WAS COMPLETED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L72 4F RTA16WE 20031231000522003123100052EA 2003 12 31 ASOA03562 120031102A3230864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11829AS 7232 DURING CLIMB-OUT, AFTER SELECTING THE LANDING GEAR UP, THE CREW RECEIVED A GEAR DISAGREE WARNING AND ASSOCIATED ENGINE INDICATION AND CREW ALERT SYSTEM MESSAGES. THE NOSE GEAR FAILED TO RETRACT BUT THE GEARS WERE CONFIRMED AS BEING DOWN BY THE TOWER. THE CREW REQUESTED EMERGENCY EQUIPMENT BE ON STANDBY AS A PRECAUTION AND THE AIRCRAFT RETURNED, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. MAINTENANCE ALSO PERFORMED A FLIGHT FUNCTIONAL CHECK OF THE LANDING GEAR SYSTEM, CYCLED THE GEAR SEVERAL TIMES AT SPEEDS OF 160-200 KNOTS AND AT VARIOUS PITCH ATTITUDES WITH OUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000762003123100076WP 2003 12 31 GTIA030938 120031103A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND CABIN STATION 237-427 LEFT CENTER SEAT TRACK HAS AREAS OF CORROSION, NICKS, GOUGES AND BARE METAL. REMOVED SEAT TRACK FROM STATION 200-510. FABRICATED SEAT TRACK. LOCATED AND DRILLED SPLICE REPAIR AT STATION 370, 270, 510. INSTALLED SEAT TRACK. INSTALLED SPLICE REPAIR AT STATION 370, 270, 510. (M) 2L72 4F RTA6WE 20031231000792003123100079WP 2003 12 31 GTIA030933 120031110A5321 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND FLOOR PANEL LEFT SIDE AT FS 446-522, CENTER BRACKET SUPPORT CRACKED, SIDE STRIP DISBONDED, FORWARD CORNER BENT. REMOVED CENTER SUPPORT. FABRICATED CENTER SUPPORT. INSTALLED CENTER SUPPORT. (M) 2L72 4F RTA6WE 20031231000802003123100080WP 2003 12 31 GTIA030934 120031028A7830 EXHAUST DUCT DOUG DC9 DC983 3022083WP THRUST REVERSER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND RIGHT ENGINE T/R ACCOUSTIC EXHAUST DUCT DELAMINATED IN SEVERAL AREAS. REPAIRED DAMAGED AREA. (M) 2L72 4F RTA6WE 20031229000042003122900004NM 2003 12 29 F3LA200300176 120031213A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL, STA 328-344, LBL 10, FWD GALLEY. INTERCOSTAL FOUND TO BE OUT OF LIMITS PER SRM 51-10-51. MATERIAL ID FOR NEW INTERCOSTAL WAS BAC 1505-100403 PER BOEING DRAWING 65-48834. COVER PLATE WAS 2024-T3 .090 PER EA B3-53R-10241. INSTALLED COVER PLATE PER EA B3-53R-10241 AND SRM 51-40-02. TREAT PRIMED AND PAINTED PER EA B3-53R-10241 AND MM 51-21-21. INSTALLED PER SRM 51-40-02 AND EA B3-53R-10241. 2L72 4F RTA16WE 20031229000182003122900018NM 2003 12 29 QXEA200301549 120031213A3260858601 PROXIMITY SENSOR DHAV DHC8 DHC8202 2809007NM ZONE 700 FAILED A QXEAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 NM09364PH1335413354 524 DURING INITIAL DESCENT FROM 14,000 FEET, ALL 3 RED GEAR WARNING LIGHTS ILLUMINATED AS WELL AS THE GEAR HANDLE UNSAFE LIGHTS. DURING APPROACH, LANDING GEAR INOP CAUTION ILLUMINATED WITH LEFT AMBER GEAR UNSAFE ALSO ILLUMINATED. CREW WENT *MISSED APPROACH*. THE CREW RAN AND ACCOMPLISHED THE ALTERNATE GEAR EXTENSION-METHOD 1. LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND FAULT CODE 53 CARD FAIL ON THE PSEU. THE PSEU WAS REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031229000332003122900033SO 2003 12 29 LR7A03094 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WRINKLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND LT CENTER FUSELAGE SKIN WRINKLED FS 737E-777E, LBL 60, WL 142-175. REPLACED FUSELAGE SKIN FS 737E-777E IAW SRM SMP 583 51-60 & 51-70. NR 2074. 2H74 4T A1SO 20031229000512003122900051EU 2003 12 29 AALA20031423 120031212A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2114061 471 EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20031229000552003122900055WP 2003 12 29 AALA20031427 120031211A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21275AA 49272 OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT SEATS 29 THROUGH 31. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEATS 29 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031229000622003122900062NM 2003 12 29 QXEA200301554 120031214A243051539008D GCU DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09358PH11932900 506 NR 2 DC GENERATOR HOT CAUTION FLICKERING IN TURBULANCE. RAN HOT CAUTION CHECKLIST. REMOVED AND REPLACED NR 2 GCU AND DC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031229000732003122900073NM 2003 12 29 03FDEA02189 120031214A5350 FRAME DOUG MD11 MD11 3023602NM ZONE 300 DEBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 AFT TAIL CONE INTERIOR LEFT SIDE FRAME ASSEMBLY FOUND DISBONDED. AFT TAIL CONE INTERIOR LT SIDE FRAME ASSEMBLY CARRIED OUT. REPAIR AS PER FEDEX EA 1-5240-75188, SERVICE DOORS, AFT EXTENDED TAILCONE PANEL ASSY REPAIR. 2L73 4F RTA22WE 20031229000832003122900083NM 2003 12 29 DHL2003742503 120031129A5310 PLATE BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, N/R 60481 UPPER CABIN SHEAR PLATE BS 1175 RBL 45 OLD TOILET DUMP CAP AREA CORRODED. DAMAGE FOUND TO BE OUT OF LIMIT IAW B-727 SRM 53-10 FIG 1. CUT OUT DAMAGE AREA AND FABRICATED DOUBLER FROM 7075 T6 .071 PO 9912380 DIM 10.5 INCH X 9 INCH AND FILLER FROM 7075 T6 .160 PO 314676 DIM 7.5 INCH X 6.125 INCH IAW B-727 SRM 51-10-2 FIG 5 AND 51-40-2 FIG 1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. PARTS INSTALLED IAW B-727 SRM 51-40-2 FIG 8. 2L73 4F A3WE 20031229001022003122900102NM 2003 12 29 AWXA200301546 120031208A53206545834107 STRAP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN TIE STRAP BELOW CABIN FLOOR IN E&E COMPARTMENT BS 344, LBL 45. MAINTENANCE STOP DRILLED CRACK IN TIE STRAP BS 344, LBL 45; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 PG 1 & 219, FIG 204. 2L72 4F RTA16WE 20031229001092003122900109NM 2003 12 29 AWXA200301553 120031202A53206545833 WEB BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-04 CHECK A 2.125 INCH CRACK WAS FOUND AT FRAME FLANGE RELIEF CUTOUT ON FLIGHT COMPARTMENT FLOOR WEB 4 INCHES INBOARD OF FUSELAGE SKIN AT BS 194 LT, WL 207.5. MAINTENANCE REMOVED CRACKED WEB AT BS 194 LT, WL 207.5; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45833; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031229001292003122900129EA 2003 12 29 MASA200300491 120031215A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775999 7471 ASH 2961 PHL-SDF. DURING PREFLIGHT, THE AFT CABIN EMERGENCY FLOOD LIGHT WAS INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4F RTA21EA 20031229001322003122900132EA 2003 12 29 MASA200300459 120031120A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER L NO TEST ININSP/MAINT 1 SW0737218 7218 CREW REPORTED CEILING EMERGENCY INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4F RTA21EA 20031229001632003122900163NM 2003 12 29 03347413 120031213A52707144003 PROXIMITY SWITCH DORNERDO32 DO328300 NM MLG FAILED A VTZABA EMER. DESCENT UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 EA27413FJ 3168 DURING CRUISE, RECEIVED AN INTIAL DOOR RED WARNING PANEL INDICATION, A PROXIMITY SYSTEM FAIL MESSAGE, PROXIMITY SYSTEM B FAIL, HYDRAULIC QUANTITY B FAIL, AND GROUND SPOILER NOT STOWED WARNING MESSAGES. RETURNED TO CVG. SHORTLY AFTER THE FLIGHT HAD TURNED BACK TOWARDS CVG CREW EXPERIENCED A LOSS OF CABIN PRESSURE. THE CREW DEPLOYED OXYGEN MASK, DECLARED AN EMERGENCY, AND PROCEEDED WITH AN EMERGENCY DESCENT. DIVERTED TO IND FOR SAFETY REASONS, ON APPROACH DID NOT RECEIVE INDICATIONS THAT ALL LANDING GEAR WERE DOWN AND LOCKED. PERFORMED FLY BY, TOWER CONFIRMED ALL GEAR DOWN. FLT LANDED UNEVENTFULLY. A FAILURE OF PROXIMITY SWITCH ELECTRONIC UNIT FOUND TO BE CAUSE. UNIT REPLACED, SATISFACTORY OPS CHECK. 2H72 4T RTA55NM 20031231000432003123100043WP 2003 12 31 GTIA030906 120031107A5320 WEB DOUG DC9 DC983 3022083WP SUB FLOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND CABIN STATION 167 LBL 50 SUB FLOOR CRACKED-DENTED. FABRICATED DOUBLER. DOUBLER INSTALLED. (M) 2L72 4F RTA6WE 20031231000462003123100046EA 2003 12 31 ASOA03568 120031105A5210601R319119 SPRING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A GROUND INSPECTION IN MGM, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE AND UPON OPENING IT FELL RAPIDLY. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR COUNTER BALANCE GAS SPRINGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000642003123100064WP 2003 12 31 GTIA030912 120031105A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND FLOOR PANEL STATION 864-896 CORNERS DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20031231000782003123100078WP 2003 12 31 GTIA030916 120031101A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FS BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND FLOOR PANEL STATION 1003-1041 CENTER, INSERT BROKEN OUT. UPON FURTHER EVALUATION FLOORBOARD IS OUT OF LIMITS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20031231000892003123100089WP 2003 12 31 GTIA030926 120031031A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FLUSH REPAIR AT FS 1255 BETWEEN LONGERONS 25 AND 26R, PREVIOUS REPAIR HAS SUSTAINED ADDITIONAL DAMAGE AROUND REPAIR AREA AND REQUIRES A NEW EXTENDED REPAIR TO BE INSTALLED. REMOVED DAMAGE SKIN. FABRICATED REPAIR PARTS. INSTALLED FILLER, DOUBLERS, FINGER DOUBLERS. (M) 2L72 4F RTA6WE 20031231000992003123100099NM 2003 12 31 TSAA0353027 120030118A53306545818 SKIN BOEING737 7372T4 1384492NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 REMOVED ALL EXISTING REPAIRS COMMON TO THE LAP JOINT AREAS. ACCOMPLISHED A HFEC OF FASTENERS HOLES TO ASSURE CRACK FREE CONDITION. FABRICATED TWO TAPERED FILLERS, A .032 INCH THICK FILLER AND FOUR .071 INCHE THICK FILLERS, A .032 INCH THICK SPLICE STRAP, A .032 INCH THICK DOUBLER AND .050 INCH THICK TRIPLER. INSTALLED REPAIR PARTS ALONG STRINGER 4L AND 4R FROM BS 360 TO BS 908, ALONG STRINGER 10L AND 10R FROM BS 360-540 AND BS 727 TO BS 908, AND ALONG STRINGER 14L AND 14R FROM BS 360-540 AND BS 727 TO BS 908 P/N'S 6545818, 6546535, 6546547, 6546558, LAP JOINT REPAIR MODICICATION COMPLETED IAW ECO 3080, WITH DEVIATIONS BJ, BK, BL, BM BN, BO, BP, BQ, BR AND BS. 2L72 4F A16WE 20031231001162003123100116NM 2003 12 31 UIEA200300069 120031121A2612 FIRE LOOP BOEING747 747243B 1384830NM NR 2 ENGINE SHORTED A UIEAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 EA15516MC 22507 NR 2 ENGINE INDICATED FIRE ON APPROACH, SHOT BOTH BOTTLES, INDICATIONS CONTINUED. FOLLOWED FHB PROCEDURES FOR ENGINE FIRE CHECKLISTS. DISCHARGED FIRST BOTTLE, TIMED 30 SECOND LIGHT REMAINED ON. DISCHARGED SECOND BOTTLE, LIGHT REMAINED ON. B-LOOP REMAINED OFF SCALE HIGH. INSPECTED ENGINE FOUND NO EVIDENCE OF FIRE, FOUND BOTH A AND B LOOPS SHORTED TO LOCAL GROUND. REPLACED B LOOP UPPER AND REPAIRED SHORT, OPERATION CHECK OK PER MM 26. 2L74 4F A20WE 20031231001222003123100122NM 2003 12 31 TSAA0355034 120030115A551065499271 FITTING BOEING737 7372T4 1384492NM HORIZONTAL STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER FITTING ASSEMBLY FAIL/SAFE AND LOWER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW SLEEVE BUSHING AND FLANGE BUSHING PER DRAWING. SHOT PEENED, REFINISHED THE LUG FACES, AND INSTALLED BUSHINGS. REPAIR COMPLETED AIW ECO 3331. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040105000012004010500001 2004 1 5 03349311 420031215A22107010680938 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AUTOPILOT MALFUNCTIONED A VTZAO OTHER F FLT CONT AFFECTED DEDESCENT 1 EA27311UE 41029 DURING DESCENT THE CREW REPORTED THE AIRCRAFT PITCHING UP AND DOWN WHILE ON THE GLIDESLOPE. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE AUTOPILOT COMPUTER WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040105000172004010500017WP 2004 1 5 UPS03841674 120031227A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTDISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: PFLT, EMERGENCY LIGHTS COME ON INITIALLY WHEN SELECTED, BUT EXTINGUISH WITHIN ONE MINUTE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK AS REQUIRED REF M M 33-50-01. OPS CHECK NORMAL. 2L74 4F RT4A25 20040105000272004010500027NM 2004 1 5 AALA20031441 120031216A3350 FUSE BOEING737 737823 13844BZNM EMERGENCY LIGHT DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21958AN 30091 OVERWING EXIT SIGN EMERGENCY LIGHT INOPERATIVE AT ROW 12, 13, 14DEF. REPLACED FUSE IN BATTERY PACK FOR OVERWING EXIT SIGN EMERGENCY LIGHTS AT ROWS 12, 13, AND 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040105000642004010500064NM 2004 1 5 2003UALA00944 120031209A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 SKIN DENTED AT STA 732, STRINGER 28R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040105000792004010500079NM 2004 1 5 AALA20031443 120031106A3350 CHARGER BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAO OTHER O OTHER CRCRUISE 1 SW21197AN 32391 UNCOMMANDED ILLUMINATION OF EMERGENCY LIGHTS FOR ROWS 16 THROUGH 24. REPLACED EMERGENCY LIGHTS CHARGER AND BATTERY FOR ROW 16 THROUGH 24. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20040105000822004010500082NE 2004 1 5 MASA200300492 220031215A7200CF343B1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 SEIZED A MASAO OTHER EY VIBRATION/BUFFET ENGINE STOPPAGE DEDESCENT 1 SW077291Z10813 7291 872612 ASH 6021 ICT-PHX. ON DESCENT FROM FLT 310 TO 290 NR 1 ENGINE ABRUPTLY SHUT DOWN WITH A LOUD VIBRATION NOISE. THE CREW ADVISED MX CNTRL OF THE ENGINE FAILURE WITH N2 -0- ROTATION. AFTER AN UNEVENTFUL LANDING MX WAS CALLED TO INSPECT THE ENGINE. MX REPLACING THE ENGINE. 2L72 4F4 FRTA21EA E15NE 20040105000902004010500090WP 2004 1 5 DHL2003802539 120031101A5720 SUPPORT ANGLE DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING RIB OTBD STUB WING SUPPORT ANGLE CRACKED 0.500 AT STA XS 520.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW SUPPORT ANGLE IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED SUPPORT ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040105001012004010500101SO 2004 1 5 C2XA03BT123 120031228A335020131A BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT MALFUNCTIONED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 CREW REPORTED, (VARIOUS EMERGENCY LIGHTS IN FORWARD CABIN ARE INOPERATIVE.) MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB135 AMM NR 33-50-04. OPS. CHECKED GOOD. 2L72 4F RTT00011AT 20031229001432003122900143EU 2003 12 29 UPS03141653 120031213A5210 BOTTLE AIRBUSA300 A300F4622R 3930360EU MAIN ENTRY DOOR DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0810 INSPECTION TYPE:N/A MAIN ENTRY DOOR DAMPNER/EMERGENCY OPERATION CYLINDER NITROGEN BOTTLE READS 0 PSI. REPLACED DIAPHRAM 10 SHEAR PIN 15 AND O-RINGS 7-8-9 AND RESERVICED MAIN ENTRY DOOR DAMPNER AND EMERGENCY OPERATING CYL PER 52-10-14-3. 2L72 4F RTA35EU 20031229001492003122900149WP 2003 12 29 UPS03841665 120031217A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 EMERGENCY LIGHTS DOME COCKPIT DOME COURIER FAIL TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK WITH REF TO MM 33-50-01, CKS GOOD AT THIS TIME. 2L74 4F RT4A25 20031229001702003122900170EU 2003 12 29 DHL2003364016 120031120A5330 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING A-CHECK, 3 FT GOUGE IN SKIN AFT OF FWD CARGO DOOR FRAME 27 BETWEEN STRINGER 34R AND 35R. BLENDED GAUGE PER SRM 51-41-10. NDT PER NTM 51-20-13. FOUND TO BE BEYOND LIMITS. REPAIRED PER A-300 SRM 53-10-10 FIG 711. PRIMED AND PAINTED PER A-300 SRM 51-75-10 AT FRAME 26 TO 27 BETWEEN STR 34 R AND 35 R. 2L72 4F RTA35EU 20031229001832003122900183NM 2003 12 29 AWXA200301556 120031207A532065C10592 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 954, RBL 43, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BS 954, RBL 43, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C10592; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12, PG 1. 2L72 4F RTA16WE 20031231000092003123100009NM 2003 12 31 USAABB03223 120031209A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 4 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 FOUND FLOOR LEVEL EMEREGNCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20031231000172003123100017NM 2003 12 31 TSAA0352053 120030318A5240 GUIDE BOEING737 7372T4 1384492NM SERVICE DOOR MISALIGNED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13807AL 23443 AFTER TAKEOFF, THE CABIN HAD AN EXCESSIVE RATE OF CLIMB, (2,500 FPM). AUTO FAILED ON THE PRESSURIZATION SYSTEM. LANDED HNL WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD SERVICE DOOR WAS IMPROPERLY CLOSED AND LOWER LEFT GUIDE MISALIGNED. MAINTENANCE REALIGNED THE DOOR GUIDE. GROUND OPERATIONAL AND PRESSURIZATION CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231000532003123100053WP 2003 12 31 GTIA030904 120031111A3520 OXYGEN MASK DOUG DC9 DC982 3022082WP LAVATORY WILL NOT TEST A GTIAO OTHER L NO TEST NRNOT REPORTED 1 GL23830NK 49932 AFT LAV LT OXYGEN MASK DIDN'T DROP. ADJUSTED DOOR, OXYGEN DROP CHECK GOOD. (M) 2L72 4F A6WE 20040105000052004010500005NM 2004 1 5 DLM88030996 120031110A5270 PROXIMITY SWITCH DOUG MD88 MD88 3023688NM AIRSTAIR DOOR OUT OF ADJUST A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27939DL 49812 AFT STAIRWAY DOOR LIGHT CAME ON INITIATION OF TAKEOFF ROLL. ADJUSTED PROX SWITCH. 2L72 4F RTA6WE 20040105000452004010500045SO 2004 1 5 SWIA200312679 120031127A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 RIGHT NACELLE FRAME NR 1 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME NR 1 IAW SB 120-54-0036 PART 2. C/W CARD RII 54-301. 2L72 4T4 TRTA31SO E20NE 20040105000592004010500059EU 2004 1 5 2003UALA00933 120031207A3350 BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29446UA 834 EMERGENCY LIGHT TEST FAILS. REPLACED BATTERY PACK 10WL. 2L72 4F4 FRTA28NM E40NE 20040105000872004010500087 2004 1 5 MEX2003517 420031113A3417HG280D80 ADC DOUG MD88 MD88 3023688NM NR 1 FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23162PL864 851 49765 AIRCRAFT RETURNED TO PLATFORM DUE TO LOSS OF VELOCIMETER INDICATION. THE ADC NR 1 WAS REPLACED AND TESTED IAW MM 34-16-0, ALL OK. 2L72 4F RTA6WE 20040105001022004010500102WP 2004 1 5 DHL2003802543 120031121A5313 LONGERON DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LONGERON 24R WITH 3.500 LENGTH CRACK AFTER STOP HOLE, STA 898.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAX BOEING DHL XXX-03-00023H 18 NOV 03, SRM 53-2-2 FIG 5. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. STOP DRILLED CRACK IN L-24R IAW FAX BOEING XXX-03-00023H, SRM 53-2-2 FIG 5. PERFORMED HFEC METHOD INSP IAW BOEING DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040105001082004010500108WP 2004 1 5 DHL2003802533 120031124A57203645611 BRACKET DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON RIGHT WING NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9, 21. 2L74 4F RT4A25 20040105001232004010500123NM 2004 1 5 SWAA032762 120031218A2560PL22300LH00 STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 ON LANDING F/A DISCOVERED EEPLS STRIP LOOSE. REPAIRED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20040105001242004010500124NM 2004 1 5 SWAA032763 120031217A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 FOUND CRACK IN FUSELAGE SKIN AT BS 780 STRINGER 18L AND BS 763, STRINGER 18L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040105001322004010500132NM 2004 1 5 SWAA032772 120031218A3350610478 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29787SA 29812 FWD SECTION OF EEPLS AT ROWS 1 AND 2 INOP. REPLACED EEPLS BATTERY PACK PER MM. 2L72 4F RTA16WE 20040105001342004010500134NM 2004 1 5 SWAA032752 120031215A3040571764 WINDOW BOEING737 7373H4 1384600NM COCKPIT ARCED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29646SW 28331 ARCING AT R4 COCKPIT WINDOW. OK TO CONTINUE PER MEL. 2L72 4F RTA16WE 20040105001362004010500136 2004 1 5 SWAA032754 420031216A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20040105001492004010500149CE 2004 1 5 AMWA101 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED D-STRUCTURAL INSPECTION, THREE FASTENERS AT RWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040105001522004010500152CE 2004 1 5 AMWA90 120031212A5347114430074141 SEAT TRACK BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 DURING AN ABC STRUCTURAL INSPECTION, THE FORWARD SEAT TRACK WAS FOUND TO BE CRACKED. 2L72 4T RTA24CE 20040105001552004010500155CE 2004 1 5 AMWA100 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 124 WERE FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040105001612004010500161CE 2004 1 5 AMWA91 120031212A5320114430002180 ANGLE BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 DURING AN ABC STRUCTURAL INSPECTION, THE RIGHT HEAVY ANGLE WAS FOUND TO BE CRACKED. 2L72 4T RTA24CE 20040105001642004010500164CE 2004 1 5 AMWA104 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 124 WAS FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040106000082004010600008WP 2004 1 6 DHL2003802566 120031210A532037584951 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING WITH 0.500 CRACK AT STA 1280.000 L-35L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IN AFT CARGO COMPT STA 1280.000 L-35L IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000342004010600034WP 2004 1 6 DHL2003802567 120031212A5753 SKIN DOUG DC8 DC873 302199CWP T/E FLAP BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT INBD FLAP UPPER AFT SKIN BROKEN STA XW 2.000 CANT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-7, DWG U38-R07. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN SEGMENT IAW ED EDU38-7, DWG U38-R07. COUNTERSUNK NEW SKIN SEGMENT IAW SRM 51-1-22. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN SEGMENT IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED NEW SKIN SEGMENT WITH NEW FASTENERS IAW ED EDU38-7, DWG U38-R07, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040106000442004010600044WP 2004 1 6 DHL2003802575 120031129A552256549704N PANEL DOUG DC8 DC873 302199CWP RT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT ELEVATOR UPPER PANEL CRACK 0.250, STA XE 65.156 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-4-1 PG 1, 2. REMOVED CRACKED UPPER PANEL FROM RT ELEVATOR STA XE 65.156 IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 1, 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 1, 4. REFER TO NR 2235 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20040106000452004010600045WP 2004 1 6 DHL2003802536 120031119A5420 ANGLE DOUG DC8 DC873 302199CWP NR 4 PYLON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 NR 4 PYLON UPPER PART ANGLE CRACKED 0.500, STA YN 188.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D PG 21. FABRICATED NEW ANGLE IAW SRM 54-2-0 PG 1. PERFORMED HEAT TREATMENT TO ANGLE IAW SRM 51-1-4 PG 1-3, SRM 51-1-1 PG 1-13, 17. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 54-2-0 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000462004010600046NM 2004 1 6 DHL2003742523 120031126A5542 SKIN BOEING727 727225 1384077NM RUDDER CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER RUDDER L/E LEFT/RIDE SIDE WORE OUT / CHAFING AREAS. DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B-727 SRM 55-40-1 FIG 1. FABRICATED REPAIR DOUBLER IAW B-727 SRM 55-40-3 FIG 1. METAL TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBLER IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040106000482004010600048NM 2004 1 6 DHL2003742524 120031212A5544 WEB BOEING727 727225 1384077NM RUDDER CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, LWR RUDDER UPPER WEB AND FASTENERS CHAFED. REMOVED DAMAGED WEB AND FASTENERS IAW B-727 SRM 51-30-2. FABBED NEW WEB IAW B-727 SRM 55-40-2 FIG 2. NEW WEB TREATED AND PRIMED IAW B-727 SRM 51-10-2. WEB AND FASTENERS INSTALLED IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040106000502004010600050NM 2004 1 6 DHL2003742525 120031204A5312 BULKHEAD BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, AFT PRESS BULKHEAD BS 1183 BS 1183 VERTICAL BEAM LBL 36 CRACKED IN THE RADIUS WL 249. REPAIRED BS 1183 VERTICAL BEAM LBL 36 USING KIT 65C34406-12 PO 3348172 IAW B-727 S/B 727-53-0192 REVISION AND DWG 65C34406. 2L73 4F A3WE 20040106000552004010600055NM 2004 1 6 AWXA200301561 120031208A531365C347784 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER 10 RT AT BS 294. MAINTENANCE REMOVED CRACKED STRINGER 10 RT FROM BS 280 TO BS 294; FABRICATED A NEW REPLACEMENT STRINGER PER DWG 65C34778; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1. 2L72 4F RTA16WE 20031231000272003123100027NM 2003 12 31 USAASB03212 120031207A2913 PUMP BOEING737 7374B7 1384702NM HYD SYSTEM FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19776AU 24934 DURING CRUISE, EN ROUTE, CAPTAIN SENT AN ACARS MESSAGE THAT THE B-SYSTEM ELECTRIC HYD PUMP OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND TURNED THE PUMP OFF. FLT RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE OPERATIONALLY CHECKED THE SYSTEM. SYSTEM OPERATIONALLY CHECKS GOOD. (M) 2L72 4F RTA16WE 20031231000332003123100033NM 2003 12 31 TSAA0333058 120030405A335086210066 BATTERY PACK BOEING737 7372S2C 138448GNM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13806AL 21927 REPLACED FORWARD EMERGENCY EXIT DOOR LIGHT DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231000492003123100049EA 2003 12 31 ASOA03580 120031115A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000732003123100073EA 2003 12 31 ASOA03576 120031110A5210601R380742 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND CRACKED. MAINTENANCE REMVOED AND REPLACED THE PASSENGER DOOR FORWARD ANCHOR FITTING. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040114001102004011400110EU 2004 1 14 YENA200339 120031127A2460630CC01Y1 CONTACTOR AIRBUS320 A320232 3930326EU DC BUSS MALFUNCTIONED A YENAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15517JB12303 1327 AT START OF TAKEOFF ROLL GOT ECAM, MADE A LOW SPEED, ABORT AT APPROX 80 KNOTS & RETURNED TO GATE. REMOVED AND REPLACED THE DC SHED ESSENTIAL BUSS CONTACTOR 8PH IAW 24-62-55-000-001. OPS CHECK OK. 2L72 4F RTA28NM 20040114001242004011400124 2004 1 14 DL73S031058 420031126A3421344002742 GYRO BOEING737 737232 1384475NM E/E BAY DEFECTIVE A DALAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 SO27315DL 23087 ON ROTATION, AIRPLANE PITCHED UP CAPTS GYRO WHICH WAS SELECTED TO AUX. PER MEL DID NOT OPERATE NORMAL, STRAIGHT AND LVL BUT DID NOT WORK WITH PITCH CHANGES. REPLACED NR 3 VG AS PER M/M, CKS GOOD. 2L72 4F RTA16WE 20040114001252004011400125NM 2004 1 14 DL757031059 120031127A3244B757M TIRE BOEING757 757232 1384965NM NR 4 BLOWN A DALAK NONE O OTHER LDLANDING 1 SO27622DL25200 22912 P1292 AUTO BRAKES WERE SET AT 3 FOR LANDING, AT 80 KTS WITH BOTH REVERSERS OPERATING AS MANUAL BRAKES WERE APPLIED, RIGHT FWD OUTBOARD TIRE BLEW NR 4 TIRE. REPLACED TIRES AND ANTISKID VALVE. 2L72 4F RTA2NM 20040114001312004011400131NM 2004 1 14 DL757031063 120031129A525010C10F SWITCH BOEING757 757232 1384965NM MID LAVATORY FAULTY A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27603DL 22810 CENTER LAV DOOR LATCH HOT AND EMITTING SMOKEY O-ZONE SMELL. REPLACED DOOR LATCH SWITCH. 2L72 4F RTA2NM 20040114001382004011400138NM 2004 1 14 DL75K031067 120031202A3412341702042 PROBE BOEING757 757232 1384965NM TAT SYSTEM FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27650DL 24390 ON T/O ROLL, RECEIVED EICAS MSG TAT PROBE AND TAT LIGHT ILLUMINATED ON OVERHEAD PANEL. REPLACED TAT PROBE. 2L72 4F RTA2NM 20040113001022004011300102EU 2004 1 13 BAQA091136 120031124A28201176417301 FUEL TANK BOLKMS117 BK117A1 5626010EU LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME6563 7243 FUEL TANK LEAKING. REPLACED WITH SERVICEABLE UNIT. 11/25/03 1G72 3U H13EU 20040113001412004011300141NM 2004 1 13 03FDEA02261 120031226A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, O/B FLAP I/B FWD HINGE SIDE SUPPORT MOUNT MATING SURFACE CORRODED. O/B FLAP I/B FWD HINGE SIDE SUPPORT MOUNT MATING SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DRAWING ARC0502 IN ACCORDANCE WITH FEDEX EA 1-5750-75209, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040114000392004011400039NM 2004 1 14 DL76G030951 120031026A3246 TIE BOLT 321002928 BOEING767 767332 1382001NM WHEEL SHEARED A DALAK NONE O OTHER ININSP/MAINT 1 SO271609 DL1137 30574 SIX TIRE TIEBOLTS SHEARED. WHEEL ASSY 6 REPLACED PER MM. 2L72 4F RTA1NM 20040114000412004011400041NM 2004 1 14 DL757030953 120031026A2161216001221 CONTROLLER BOEING757 757232 1384965NM A/C BAY MALFUNCTIONED A DALAA UNSCHED LANDING M OVER TEMP CRCRUISE 1 SO27687DL 27586 LT PACK WENT FULL HOT UNCONTROLLABLE. DUCT TEMPS WERE 120 DEGREES WITH PACK CONTROLLER IN AUTO AND STBY. SELECTED PACK CONTROLLER TO COLD AND DECREASED DUCT TEMP. INSPECTED SENSORS, RAN BITE ON TEMP CONTROLLER, NO FAULTS. REPLACED PACK TEMP VALVE, ZONE TEMP CONTROLLER AND OVERHEAD CONTROL PANEL. SYSTEM CHECKS GOOD. 2L72 4F RTA2NM 20040114001292004011400129NM 2004 1 14 DL75K031062 120031126A3350 COVER BOEING757 757232 1384965NM CABIN DAMAGED A DALAK NONE O OTHER CRCRUISE 1 SO2767171 30839 RED EMERGENCY LIGHT BY FRONT GALLEY ON F/O SIDE COVER DAMAGED. REPLACED SAME. 2L72 4F RTA2NM 20040114001602004011400160NM 2004 1 14 03FDEA02011 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 N0310 LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 3 IB UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040114001712004011400171EU 2004 1 14 MALA030561 120031219A7920 LINE SAAB SF340 340B 7860101EU LT ENGINE LOOSE A MALAK NONE J WARNING INDICATION CRCRUISE 1 GL15369PX 340B295 DURING FLIGHT, LT ENGINE OIL LIGHT ILLUMINATED AND ENGINE OIL GAUGE WAS FLUCTUATING BETWEEN 25-35 PSI, ENGINE WAS NOT SHUTDOWN. DURING TROUBLESHOOTING FOUND B-SUMP AIR LINE LOOSE RESECURED AND REPLACED PACKINGS. GROUND RUN A/C, ALL CKS GOOD NO LEAKS NOTED. C/W LOSS OF OIL SPEC PRO CHIP DETER AND SEVE SCREEN, ALL CKS GOOD. 2L72 4T RTA52EU 20031124000832003112400083WP 2003 11 24 DHL2003807518 120031014A53203750257U1 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SPLICE FITTING 8.500 CRACK (STA 440.000 - 460.000, L-31R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS AND PRC SEALANT IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20031124001012003112400101WP 2003 11 24 DHL2003802507 120031113A573056110121 SKIN DOUG DC8 DC873 302199CWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING T/E LOWER PANEL LOWER SKIN DELAMINATED STA XW 97.000 - XRS 162.000. REMOVED AND REPLACED LOWER PANEL ASSY ON LEFT WING T/E STA XW 97.000 XRS 162.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031124001022003112400102WP 2003 11 24 DHL2003802500 120031107A5712 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING L/E FORMER CRACKED 0.500, STA XFS 747.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031124001062003112400106WP 2003 11 24 DHL2003805554 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING INBD L/E FORMER CRACKED 0.500 STA XFS.622.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031231000382003123100038NM 2003 12 31 TSAA0333049 120030310A33509221009 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHTSDISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 REPLACED FORWARD ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000602003123100060WP 2003 12 31 GTIA030919 120031028A5410K22199SA32 ISOLATOR DOUG DC9 DC983 3022083WP LT NACELLE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 LT ENGINE PYLON AFT ISOLATOR RUSTY. REMOVED LT ENGINE PYLON AFT ISOLATOR ASSEMBLY. INSTALLED NEW LT ENGINE PYLON AFT ISOLATOR. (M) 2L72 4F RTA6WE 20040105001072004010500107WP 2004 1 5 DHL2003802541 120031124A5311 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 FWD ACCY COMPT FRAME CRACKED 1.000, STA 55.000, L-24R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. TRIMMED OUT CRACKED FRAME IAW SRM 53-2-0 FIG 2. FABRICATED FRAME SEGMENT AND SPLICE ANGLES (02 EA) IAW SRM 53-2-0 FIG 2. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 1, 13, 17 IAW SRM 51-1-4 PG 1-3. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND SPLICE ANGLES WITH NEW FASTENERS IAW SRM 53-2-0 FIG 2, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000142004010600014WP 2004 1 6 DHL2003802565 120031212A5753 SKIN DOUG DC8 DC873 302199CWP T/E FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT OUTBD FLAP L/E PLATING WORN STA XF 163.000- 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-8, DWG U38-R08. REMOVED DAMAGED PLATING, RUB STRIPS AND RIBS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, ED EDU38-8, DWG U38-R08. HEAT TREATED IAW SRM 51-1-1 PG 1, 13, 17, SRM 51-1-4 PG 1, 3, DPS 3.69-4. PERFORMED COUNTERSINK TO NEW PLATING IAW SRM 51-1-22. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INNER SIDE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED NEW PLATING AND REINSTALLED RUB STRIP AND RIBS WITH NEW FASTENERS IAW ED EDU38-8, DWG U38-R08, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040106000382004010600038WP 2004 1 6 DHL2003802560 120031124A53204751820 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT FWD FITTING CRACK 1.500, STA 781.500 RBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 781.500 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201843 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000392004010600039WP 2004 1 6 DHL2003802563 120031202A53203754051501N FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT T-BOLT FITTING CRACKED 0.500 AT STA 1240.000. REMOVED CRACKED T-BOLT FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW T-BOLT FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000782004010600078SO 2004 1 6 C2XA03SH504 120031218A531514530633003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030918000852003091800085EU 2003 9 18 0301483248 120030805A5320 FLOOR SUPPORT AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01348NW 410 DURING "L" CHECK FOUND CORROSION ON RT FLOOR SUPPORT WEB AT FRAME 20. REPAIRED IAW EA 32-195961. 2L72 4F RTA28NM 20030918000982003091800098WP 2003 9 18 IXXA0300053O 120030805A3260H141003 PROXIMITY SWITCH DOUG DC8 DC873F 302199FWP ZONE 700 WORN A IXXAO OTHER J WARNING INDICATION DEDESCENT 1 SW11603AL911901190 46003 WHEN MLG WAS EXTENDED NO LEFT GEAR OR DOOR UNLATCHED LIGHTS NOTED.PERFORMED ABNORMAL PROCEDURE PER ATI COM, NO HELP. AFTER SEVERAL GEAR CYCLES ALL LIGHTS INDICATED NORMALLY. CREW LANDED WITHOUT INCIDENT IN KTOL.UPON INSEPCTION MAINTENANCE NOTED L/H MLG DOWNLATCH SWITCH CONDITION DETERIORATED AND REPLACED THIS COMPONENT. MAINTENANCE PERFORMED CHECK AND ALL INDICATIONS WERE WITHIN LIMITS. ALL WORK COMPLETED PER APPLICABLE MANUALS AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20030918001342003091800134NM 2003 9 18 0301516717 120030630A5410 FRAME BOEING747 747251F 1384898NM NR 1 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING "L" CHECK FOUND CRACK IN BULKHEAD NR 1 PYLON FRAME WEB. REPAIRED PER EA 67-165077. 2L74 4F A20WE 20030919000022003091900002NM 2003 9 19 0301536301 120030806A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01661US 23719 DURING LINE CHECK, FOUND 'D' ZONE RIGHT AND UPPER DECK FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRES. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030919000302003091900030 2003 9 19 374PA0003 420030809A22104084042906 COUPLER BOEING737 73736M 138443BNM YAW DAMPER FAILED A PIDAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO05374PA 28333 YAW DAMPER OFF LIGHT ILLUMINATED (YAW DAMPER DC CIRCUIT BREAKER POPPED). REPLACED YAW DAMPER COUPLER PER MM 22-13-00. OPS CHECKS GOOD. 2L72 4F RTA16WE 20030919000422003091900042NM 2003 9 19 IU62003F00026 120030530A3240607751 HOUSING BOEING737 737* NM MLG BRAKE SYS CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 MLG BRAKE SYS HOUSING CRACKED. FATIGUE. MAKE A STRONGER HOUSING. (NR 177802) 2L72 4F RTA16WE 20030919000492003091900049CE 2003 9 19 DXTA200300081 120030811A324066710034 LINE CESSNA560 560XL 2076702CE EMERGENCY BRAKE CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07694QS 5605194 WHILE PERFORMING NJA'S ONE TIME INSPECTION OF THE HYDRAULIC/PNEUMATIC LINES IN THE WHEEL WELLS, FOUND THE RT EMERGENCY BRAKE LINE CHAFFED THROUGH, THE LT EMEGENCY BRAKE LINE, LT AND RT HAND FLAP RETRACT AND EXTEND LINES, SPEED BRAKE RETRACT AND EXTEND LINES CHAFFED BEYOND LIMITS. - REMOVED AND REPLACED DEFFECTIVE HYDRAULIC AND PNEUMATIC LINES IAW MM CH 27-51-00 AND 32-42-09, SYSTEM OPS AND LEAK CHECKED GOOD. 2L72 4F RTA22CE 20031006000662003100600066CE 2003 10 6 AMWA40 120030907A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127ZV UE127 RIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-47 STRG P/N 101-640000-46 ON RT SIDE STRG P/N 101-640000-41 STRG P/N 101-640000-37 LT SIDE (4EA CRACK ON THIS RIB). 2L72 4T RTA24CE 20031006001052003100600105NM 2003 10 6 2003UALA00673 120030909A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29368UA 24537 AFT CARGO DOOR, AFT EDGE OF CUTOUT IS DAMAGED APROX 16 INCHES FROM LWR EDGE, WORN ON INSIDE AND CUT BACK ON OUTSIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER-TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031006001682003100600168NM 2003 10 6 SWAA031971 120030903A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 307, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031007000372003100700037 2003 10 7 AALA20030811 420030723A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21677AN 29427 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000522003100700052NM 2003 10 7 AALA20030725 120030706A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21617AM 24525 FOUND SEAT MOUNTED EMERGENCY PATH LIGHTING AT 22D INOPERATIVE. REPAIRED CONNECTOR UNDER SEAT 22F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000812003100700081NM 2003 10 7 SWAA031955 120030902A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031007001092003100700109NM 2003 10 7 03242405 120030830A3350 LAMP DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27405FJ 3155 DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ABOVE SEAT 11A WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031007001112003100700111EA 2003 10 7 03243629 120030831A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27629BR 7251 DURING MAINTENANCE INSPECTION THE FLOOR EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031009000242003100900024SO 2003 10 9 SIMA200323003 120030817A335074441 LIGHT EMB 135 EMB135KL 3260302SO EXIT SIGN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21834AE 145631 FLIGHT ATTENDANT REPORTED THE EXIT SIGN ABOVE THE SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTION ON LUMINSCENT STRIP TO BE SHEARED OFF. MAINTENANCE REPLACED TEH LIGHT STRIP. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031009000402003100900040EU 2003 10 9 SIMA200326201 120030916A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21345SB 340B345 FOUND ROW 4 AND 5 ADJACENT EMERGENCY FLOOR LIGHTS INOPERATIVE. REMOVED AND INSTALLED BATTERY POWER SUPPLY AT 20LN IAW 33-50-10. PERFORMED OPS CHECK OF SYSTEM WITH NO DEFECTS. (M) 2L72 4T RTA52EU 20031009000432003100900043SO 2003 10 9 SIMA200322302 120030808A2120 ODOR EMB 135 EMB135KL 3260302SO COCKPIT DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21807AE 145506 DURING CLIMB CREW REPORTED A BURNING ELECTRICAL ODOR. NO SMOKE WAS REPORTED. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED WITH NO FURTHER INCIDENTS. THE ODOR DISSIPATED DURING DESCENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN INSPECTION OF THE ELECTRICAL SYSTEM AND AN OPERATIONAL CHECK OF THE AVIONICS SYSTEM SHOWED NO DEFECTS. NO INDICATION OF SMOKE OR ODOR OF SMOKE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031009000602003100900060NM 2003 10 9 03FDEA01622 120030924A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 DENT IN FRAME BS 600, ABOVE STR 25L. REPAIRED DENT IN FRAME BS 600 ABOVE STR 25L PER FED-EX E.A. 7-5310-70526A. 2L73 4F RTA3WE 20031009000692003100900069EA 2003 10 9 SWIA200312393 120030903A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07930SW5886 5886 0407 7713 DURING FLIGHT WE RECEIVED (FLT SPOILER FAULT) MESSAGE ON FLT CONTROL PAGE INDICATED WITH A WHITE RT FLIGHTER SPOILER. WE HAD TO USE 20 PERCENT LEFT AILERON, TRIM AND RT RUDDER TRIM TO TRIM A/C. REPLACED RT IB FLIGHT SPOILER PCU. OPS CHECKS GOOD. NO LEAKS NOTED. S/N OFF: 6009 2L72 4F RTA21EA 20031009000842003100900084 2003 10 9 SWIA200312406 420030914A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTO PILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07288SW6549 6549 120316 ALTITUDE HOLD ON CAPT SIDE WILL DRIFT 150' DOWN. REPLACED AUTO PILOT COMPUTER APC-65B. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20031009000892003100900089SO 2003 10 9 SWIA200312411 120030825A5415 CHANNEL EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07214SW 120280 LT MLG INSIDE WELL FORWARD OUTBOARD CRACK ON NACELLE. (DISCOVERED DURING C-CHECK INSPECTION) LT MLG OUTBOARD CHANNEL REPLACED SRM120 51-10-02. 2L72 4T RTA31SO 20031009000952003100900095CE 2003 10 9 DJFA200300004 120030828A540045A30024603 COWLING BEECH MU300 400A 1155402CE LT ENGINE MISSING E DJFAA UNSCHED LANDING DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 EA23746TA5246 RK146 AFTER DEPARTURE FROM WEST PALM THE PILOTS EXPERIENCED A VIBRATION AND A YAW IN THE AIRCRAFT. THE PILOTS DECIDED TO RETURN TO WEST PALM, AND AFTER LANDING WHEN THEY GOT OUT OF THE AIRCRAFT THEY NOTICED THE LT ENGINE COWL WAS COMPLETELY MISSING. THIS HAS HAPPENED SEVERAL TIMES ON OUR FLEET. THE CAUSE IS UNKNOWN, BUT COULD BE THE AIR GOT UNDER THE COWL AND STARTED TO PEEL IT BACK UNTIL THE COWL WAS COMPLETELY GONE. 2H72 4F RTA16SW 20031009000972003100900097EA 2003 10 9 COMA0360417 120030914A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAD RETURN TO BLOCK JS WARNING INDICATION AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01518CA 7816 FLT 5760 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01. 2L72 4F RTA21EA 20031009001042003100900104NE 2003 10 9 QXEA200301134 220030915A73204120T00P15 FADEC CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09603QX636 28 10011 AFTER TAKEOFF LEFT THRUST REVERSER CAUTION MESSAGE CAME ON. TURNED LEFT THRUST REVERSER SWITCH OFF PER CHECKLIST. MESSAGE WENT AWAY AFTER ABOUT 3 MINUTES. REMOVED AND REPLACED NR 1 FADEC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20031009001122003100900112WP 2003 10 9 CALA0300530 120030817A21216054577 FAN DOUG DC9 DC982 3022082WP AIR DISTRIBUTIONSEIZED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW271281135387 49265 A/C HAD A CHRONIC INFLT PROBLEM WITH AN ELECTRICAL ODOR AFT. TROUBLESHOOTING PERFORMED. SOURCE OF ODOR APPEARED TO BE COMING FROM AFT GALLEY. COFFEEMAKERS, OVENS, & ACCESS PANELS INSPECTED, NO EVIDENCE OF BURNING. PACK BURNOUT PERFORMED & COALESCER BAGS R & R. ALL OVERHEAD LIGHTS & ELECTRICAL PANELS IN 1ST CLASS INSPECTED, NO ODOR OR BURNING. FOUND RECIRC FAN "FROZEN" CAUSING CIRCUIT BREAKERS TO POP. RECIRC FAN R & R, OPS CHK GOOD IAW MM 21-20-12. MAINT CHKED ALL 3 AFT GALLEY OVENS, NO INDICATION OF LOOSE TERMINALS OR ARCING WIRES. TERMINAL STRIP CONNECTIONS & GROUND STUDS SECURE. 2 FLTS FLOWN SINCE REPLACE OF RECIRC FAN, NO CABIN OR GALLEY ODOR REPORTED. SOURCE OF ODOR ATTRIB TO A FAULTY RECIRC FAN. 2L72 4F A6WE 20031009001182003100900118EA 2003 10 9 QXEA200301135 120030916A3150 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 ILLUMINATED A QXEAO OTHER N FALSE WARNING LDLANDING 1 NM09612QX 10042 ON FLT 2504 ON LANDING ROLLOUT GOT 'DISPLAY COOL' AMBER CAUTION MESSAGE. PERFORMED CHECKLIST, WENT TO GROUND ALTERNATE ON DISPLAY FAN AND 'DISPLAY COOL' MESSAGE EXTINGUISHED. INTEROGATED MDC WITH NO FAULTS FOUND. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031009001202003100900120WP 2003 10 9 510082703 220030827A725031026552 BLADE FRCHLDSA227 SA227CC 3377522SW GARRTTTPE331TPE33111U 01514WP TURBINE WHEEL BROKEN E STZAK NONE O OTHER ININSP/MAINT 1 AL03510FS CC842B P44710C DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT APPROXIMATELY .7500 OF ONE THIRD STAGE TURBINE BLADE HAD BROKEN OFF AND EXITED OUT THE TAIL PIPE CAUSING DAMAGE TO THE TAIL PIPE AND SCAVENGE PUMP COVER. THE THIRD STAGE T-WHEEL ASSEMBLY HAS A SERVICE LIFE OF 6,000 CYCLES AND HAD BEEN IN SERVICE FOR 1,599 CYCLES. ENGINE REMOVED FROM AIRCRAFT AND SENT TO MFG PHX FOR FURTHER EVALUATION AND REPAIR. 2L72 4T4 TRTA18SW E4WE 20031010000172003101000017NM 2003 10 10 USAABB03160 120030714A3350873100151 LIGHT BOEING757 7572B7 1384964NM SEAT 18D INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT 18D STAYED ON. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND BATTERY. OPS CHECKS OK. (M) 2L72 4F RTA2NM 20031010000272003101000027NM 2003 10 10 USAABB03163 120030910A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031010000422003101000042NE 2003 10 10 MWEA030378 220030917A7200BR700715A130 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LEFT SMOKE A MWEAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31902ME 55166 SMOKE REPORTED FROM LEFT ENGINE, SHUTDOWN ENGINE. ALL ENGINES INDICATES NORMAL, CHECKED INLET AND EXHAUST, CHECKED COWLING FOR LEAKS, HAD CREW GROUND RUN ENGINES, NORMAL SMOKE FROM EXHAUST ENGINE BREATHER. TESTED FIRE DETECTION SYSTEM. NO DEFECTS NOTED OK FOR SERVICE. 2L72 4F4 FTRA6WE E00061EN 20031010000452003101000045NM 2003 10 10 03FDEA01583 120030917A27524059005901 ACTUATOR DOUG MD11 MD11 3023602NM FLAPS INOPERATIVE A FDEAJA DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25618FE3112331123 48754 ON DEPARTURE FLAPS NO RETRACT PLEASE. REMOVED AND REPLACED FLAP LIMITER DUPLEX ACTUATOR IAW MM 27-56-01-0 4. PERFORMED ADJUSTMENT OF FLAP LIMITER ACTUATOR IAW MM 27-50-00-5, ALSO PERFORMED FUNCTIONAL TEST OF THE FLAP LIMITER ACTUATOR IAW MM 27-50-00-5, CHECKED GOOD. REMOVED AND REPLACED FLAP CONTROL VALVE (INBOUND) IAW MM 27-52-03-4 . PERFORMED TEST OF FLAP SYS OPERATION / RANGE MOVEMENT IAW MM 27-50-00-5, CHECKED GOOD. LEAK OPS CHECK OK. 2L73 4F RTA22WE 20031010000532003101000053NM 2003 10 10 03FDEA01564 120030918A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 N00564 DENT IN FWD CARGO FRAME, BS 500 BETWEEN STR 23L AND 24L. **SD** COMING 2L73 4F RTA3WE 20031010000572003101000057NM 2003 10 10 03FDEA01560 120030918A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 N00561 DENT IN FWD CARGO FRAME BS 660 AT STR 22R. **SD** COMING 2L73 4F RTA3WE 20031006001942003100600194NM 2003 10 6 03FDEA01590 120030919A5340 HINGE DOUG MD11 MD11 3023602NM TAIL CONE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 FWD EXTENDED TAILCONE LT HINGE UPPER ATTACHED FITTING MOUNTED AT FWD FACE OF AFT BULKHEAD STA Y2164 (AFT ACCESSORY COMPT) FOUND WITH 02 EA HAIR LINE CRACKS AS MARKED. FWD EXT TAILCONE LT HINGE UPPER ATTACHED CRACKED FITTING WHICH MOUNTED AT FWD FACE OF AFT BULKHEAD STA Y2164 (AFT ACCESSORY COMPT) REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-33-01 VOL2 & SRM 51-35-01 VOL2 IAW EA 1-5310-73319. NEW FITTING FABRICATED AS PER DWG AJC7346 IAW EA 1-5310-73319 WITH TITLE FUSELAGE - MAIN FRAME - TAILCONE HINGE SUPPORT FABRICATION. 2L73 4F RTA22WE 20031007000292003100700029EU 2003 10 7 ASOA03408 120030831A7500 SERVO VALVE AEROSPATR72 ATR72212 8680945EU LT ENGINE MALFUNCTIONED A ASOAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO11632AS 338 DURING CLIMB-OUT FROM ATL-FAY, THE LT ENGINE ROLLED BACK AFTER TAKEOFF WITH THE TORQUE DROPPING AS LOW AS FORTY PERCENT ALONG WITH ALL OTHER GAUGED DROPPING ALSO. THE ENGINE POWER CAME BACK WITH SMALL FLUCTUATIONS BOTH IN THE AIR AND ON THE GROUND. QRH PROCEDURES WERE COMPLIED WITH, AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE INTERCOMPRESSOR BLEED SERVO VALVE (P/N 311864201) AND THE NR 2 TORQUE SENSOR (P/N 3116499-02) ON THE LEFT ENGINE. OPS CHECKS GOOD. AIRCRAFT FOR SERVICE. (M) 2H72 4T RTA53EU 20031007000312003100700031EU 2003 10 7 ASOA03405 120030831A5412 FIREWALL AEROSPATR72 ATR72 EU NACELLE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11640AS 405 DURING HANGAR MAINTENANCE IN MCN, THE RT ENGINE NACELLE UPPER AFT FIREWALL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ENGINE NACELLE UPPER AFT FIREWALL IAW SRM 51-00. (M) 2H72 4T RT 20031007000342003100700034 2003 10 7 AALA20030813 420030702A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21627AA 24585 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000352003100700035NM 2003 10 7 AALA20030804 120030727A2751 WARNING LIGHT BOEING757 757223 1384957NM TE FLAPS ILLUMINATED A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21661AA 25295 AIRCRAFT INTERRUPTED DUE TO FLAP DISAGREE EICAS MESSAGE. AIRCRAFT RETURNED VVI AND LANDED WITHOUT INCIDENT. PERFORMED BITE TEST WITH NO FAULTS NOTED. MESSAGE CLEARED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000922003100700092NM 2003 10 7 SWAA031990 120030904A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED ON AFT SIDE AT STR 5R. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20031008000212003100800021CE 2003 10 8 GLBA2003132 120030916A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE TORQUE FAILED A GLBAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 NM03195GL17487 UE195 NR 1 TORQUE GAUGE QUIT AFTER TAKEOFF, REMOVED AND REPLACED TORQUE INDICATOR. 2L72 4T RTA24CE 20031009000142003100900014WP 2003 10 9 AALA20030951 120030902A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217517A 49894 FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT CABIN. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031009000452003100900045SO 2003 10 9 SIMA200325309 120030908A2510 LOCKPIN EMB 135 EMB135KL 3260302SO COCKPIT SEAT LACK OF LUBE A SIMAO OTHER O OTHER TOTAKEOFF 1 SW21830AE 103 145615 DURING TAKEOFF, CRWE REPORTED THE CAPTAINS SEAT PINS FAILED TO ENGAGE AND PILOTS SEAT SLIDE TO THE AFT POSITION. MAINTENANCE CLEANED THE CAPTAINS SEAT TRACKS AND LUBRICATED THE SEAT PINS. OPS CHECK WAS GOOD IAW CMM 25-21. (M) 2L72 4F RTT00011AT 20031009000922003100900092EA 2003 10 9 03259633 120030916A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27633BR 7274 DURING INSPECTION THE AFT UPPER EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031010000472003101000047NM 2003 10 10 03FDEA01572 120030918A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON FLOORBEAM AT BS 1070, RBL 10.5, WL 208. **SD** COMING 2L73 4F RTA3WE 20031010000692003101000069WP 2003 10 10 DHL2003804007 120030918A2830 MOTOR DOUG DC8 DC873F 302199FWP FUEL DUMP STALLED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01804DH 46124 DURING FUEL DUMP, ELECTRIC MOTOR STALLED APPROXIMATELY 1/3 OF THE WAY DOWN. PULLED CIRCUIT BREAKER PER ABNORMAL PROCEDURE. A 170 LBS FORCE REQUIRED PER 1/4 TURN OF MANUAL DUMP HANDLE. DUMP CHUTES RETRACT NORMALLY. FOUND FUEL DUMP HOOKS DIRTY WITH SAND AND ANTI-CORROSION SPRAY. CLEANED, LUBED HOOKS AND DUMP VALVES. OPEN ELECTRIC AND MANUAL AS PER M/M 28-30-0. GROUND OPS NORMAL. 2L74 4F RT4A25 20031010000912003101000091SW 2003 10 10 BAQA089240 120030919A7712430110212 MODULE BELL 222 222U 1182140SW LYC LTS101LTS101600A 41560NE AIR FLOW FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03277LF466 47520 ENGINE TORQUE FLUCTUATES. REPLACED WITH SERVICEABLE UNIT. 9/29/03 1G72 3U3 U H9SW E5NE 20031010000922003101000092EU 2003 10 10 BAQA089499 120030929A7922ZRB2010010 TRANSDUCER UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE OIL PRESSURE FLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118WS1747 0089 REMOVED DUE TO FLUCTUATING OIL PRESSURE AT NR 1 ENGINE. REPLACED WITH SERVICEABLE UNIT. 9/29/03 1G72 3U3 U H88EU E34NE 20031014000012003101400001EU 2003 10 14 BAQA089517 120030804A6200E4165F01 ADAPTER AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE FREQUENCY TORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 663 6425 FREQUENCY ADAPTER IS TORN. REPLACED WITH SERVICEABLE UNIT. 9/30/03 1G72 3U3 U H10EU E19EU 20031014000272003101400027EU 2003 10 14 CCHA745C 120030830A2150 GEARBOX UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE A/C PACK SEIZED E CCHAO OTHER J WARNING INDICATION CLCLIMB 1 SO19911CK3580 244 0138 3016972 UPON TAKEOFF OF AN INTER-FACILITY TRANSPORT, THE AIR CONDITIONING 90 DEGREE GEARBOX SEIZED CAUSING SHAFT TO SHEAR IN GEARBOX AND COUPLING TO SHEAR ON DRIVESHAFT. COUPLING SHEAR CAUSED SEVERE VIBRATIONS FORCING PILOT TO RETURN TO TAKEOFF POINT AND LANDED WITHOUT INCIDENT. PROBABLE CAUSE SHAFT SHEAR STRENGTH TOO HIGH. LOWER SHEAR STRENGTH, BELIEVE THIS WAS AN ISOLLATED OCCURANCE. 1G72 3U3 U H88EU E34NE 20031014000372003101400037EU 2003 10 14 MALA030423 120030912A25604566N37B42NM PBE BAC 146 AVRO146RJ85A1500097EU COCKPIT DAMAGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15532XJ E2366 PBE ON FLIGHT DECK HAS LOST IT VACCUM SEAL. MAINTENANCE REMOVED AND REPLACED FLIGHT DECK PBE AS REQUIRED PN 4566N37B-42NM. 2H74 4F RTA49EU 20031014000482003101400048NM 2003 10 14 SWAA032186 120031001A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LEFT AND RIGHT FUSELAGE FRAME ASSY'S CRACKED AT BS 188, WL 207. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20031014000692003101400069NM 2003 10 14 SWAA032205 120031003A53306545767129 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 14, STR 16L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031014000732003101400073 2003 10 14 SWAA032201 420031002A256565C19901 CABLE BOEING737 7375H4 138449DNM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20031014000762003101400076 2003 10 14 SWAA032198 420031002A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031014000782003101400078NM 2003 10 14 SWAA032196 120031002A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FRAME PER SRM. 2L72 4F RTA16WE 20031014000802003101400080 2003 10 14 SWAA032194 420031004A2565D31354 INDICATOR BOEING737 7373G7 1384595NM SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED AFT SVC DOOR EMERGENCY EVAC SLIDE PER MM. 2L72 4F RTA16WE 20031014000872003101400087NM 2003 10 14 SWAA032215 120031003A7603BACB10A27 BEARING BOEING737 7372T4 1384492NM PWA JT8 JT8D* NE NR 2 THROTTLE WORN A SWAAK NONE P NO WARNING INDICATION NRNOT REPORTED 1 SW29702ML 22054 NR 2 ENGINE THROTTLE STIFF AND WILL NOT STAY AT IDLE. REMOVED AND REPLACED NR 2 ENGINE THROTTLE CONTROL CROSS SHAFT BEARING PER MM. 2L72 4F4 F A16WE E2EA 20031009000302003100900030SO 2003 10 9 SIMA200313205 120030509A2520727712050 CIRCUIT BOARD EMB 135 EMB135LR 3260305SO PSU INOPERATIVE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21717AE 145272 DURING CRUISE FLIGHT, THE CREW REPORTED THE OVERHEAD LIGHT AT 12C FLASHING OFF AND ON WITH A BURNING ELECTRICAL ODOR. MAINTENANCE REMOVED AND REPLACED DIODE BOARD FOR THE PASSENGER SERVICE UNIT AT SEAT 12C IAW CMM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031009000412003100900041EA 2003 10 9 SIMA200326202 120030918A3350 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCONNECTED A SIMAO OTHER L NO TEST NRNOT REPORTED 1 SW21503AE 10021 CEILING EMERGENCY LIGHT ABOVE FLIGHT ATTENDANT NR 2 NOT COMING ON. TROUBLESHOT AND FOUND J361/P361 DISCONNECTED. RECONNECTED CONNECTOR AND PERFORMED OPS CHECK ON EMERGENCY INTERIOR LIGHT SYSTEM IAW CRJ 700 33-51-00, OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20031009000862003100900086SO 2003 10 9 SWIA200312408 120030914A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07187SW7201 7201 120037 CONTROL FAULT WITH FLAP AND ADVANCED SWS IN FLIGHT INBOARD FLAPS FLASHING. CLEARED WITH RESET IAW QRH. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR AND REPLACED FCU IAW 27-80-08. OPS AND LEAK CHECKS GOOD. PN: 320300-1005 SN OFF: 0885 2L72 4T RTA31SO 20031009000912003100900091EA 2003 10 9 SWIA200312413 120030911A3260864808 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07908SW2453 2453 7540 GEAR DISAGREEMENT AND NOSE DOOR WARNING INFLIGHT. WARNINGS WENT AWAY AFTER APPROX. 5 MIN. ENROUTE TO DENVER. INSTALLED SERVICEABLE PSEU IAW CRJ MM 32-61-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031009000932003100900093EA 2003 10 9 03259639 120030916A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 DURING INSPECTION THE PAX DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031009001132003100900113WP 2003 10 9 CALA0300531 120030917A5350 HANDLE DOUG DC9 DC982 3022082WP TAILCONE LACK OF LUBE A CALAK NONE O OTHER ININSP/MAINT 1 SW2716806 49260 THE TAIL CONE HANDLE AFT ENTRY DOOR REQUIRED EXCESSIVE FORCE TO OPEN. THE DOOR HINGES AND HANDLE MECHANISM WERE LUBRICATED. A PULL TEST WAS PERFORMED IAW MM 53-53-00 AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F A6WE 20031010000192003101000019NM 2003 10 10 USAASB03148 120030823A2612100012701MOD5 CONTROL UNIT BOEING737 7373B7 1384580NM CARGO FIRE INOPERATIVE A USAAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 EA19391US 23313 EN ROUTE FROM PHL-MSP, THE CREW REPORTED VIA ACARS THAT THEY HAD AN AFT CARGO COMPARTMENT FIRE BELL, BUT THE INDICATION WENT OUT BEFORE THE FIRE PROCEDURE COULD BE INITIATED. ALL WAS OK, SO THE FLIGHT PROCEEDED. HOWEVER, AS THE FLIGHT BEGAN DESCENT INTO MSP, THE INDICATION RETURNED. CAPTAIN FIRED THE BOTTLES AND DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. AT THE TIME OF THE INCIDENT, THE AFT CARGO COMPARTMENT SMOKE DETECTION WAS ON MEL 26-19B. MAINTENANCE REMOVED AND REPLACED THE CARGO FIRE EXTINGUISHING CENTRAL CONTROL UNIT, BOTH FIRE BOTTLES, P/N 34200409-1, METERING VALVE ASSEMBLY P/N 52000857-1, DIVERTER VALVE ASSEMBLY P/N 52000859-2, AND UNIT P/N 100-0649-04,2L72 4F RTA16WE 20031010000962003101000096EU 2003 10 10 BAQA089177 120030925A6240645142081 INDICATOR AEROSPSA365 SA365N 8680669EU TRIPLE TACH ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 6425 TRIPLE TACH INDICATOR ERRATIC AT LOW RANGE. SPLIT AT 360/350. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20031014001132003101400113NM 2003 10 14 SWAA032154 120030925A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001142003101400114NE 2003 10 14 SWAA032153 220030925A7320570908 SPACER BOEING737 7372H4 138448CNM PWA JT8 JT8D9 52048NE NR 1 ENGINE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 NR 1 ENGINE THROTTLE BINDING AT ABOUT HALF-WAY. REMOVED AND REPLACED SPACER BETWEEN TWO CONTROL CABLES PER MM. 2L72 4F4 F A16WE E2EA 20031231000982003123100098NM 2003 12 31 TSAA0355032 120030115A5510 FITTING BOEING737 7372T4 1384492NM HORIZONTAL STAB CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR ATTACHMENT FITTING CLEVIS LUGS BUSHINGS REMOVED. EDDY CURRENT INSPECTED LUGS FOR CRACKS BEFORE AND AFTER OVERSIZING AND SHOT PEENING. MACHINED, SHOT PEENED, AND FINISHED THE LUG/CLEVIS. INSTALLED BUSHING/SLEEVE WET WITH MBS 5-95 SEALANT. APPLIED A FILLET SEAL USING BMS 5-95 AND CORROSION INHIBITING COMPOUND BMS 3-23 TO THE BUSHINGS AND LUG FACES. MODIFICATION COMPLETE IAW ECO 2887. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231001142003123100114WP 2003 12 31 GTIA030943 120031118A5210 SKIN DOUG DC9 DC981 3022081WP PAX DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23805NK 48058 DTW - FOUND AFT CABIN DOOR HAS CRACK ON UPPER EDGE. REPAIRED AFT CABIN DOOR PIECE MISSING. (M) 2L72 4F A6WE 20031231001212003123100121NM 2003 12 31 UIEA200300070 120031124A5754 SKIN BOEING747 74747UF 1384949NM RT LE FLAP BIRD STRIKE A UIEAO OTHER O OTHER NRNOT REPORTED 1 EA15415MC 32837 RIGHT INBOARD FLAP FOREFLAP DAMAGE. BIRD STRIKE ON RIGHT WING L/E FLAPS. PERFORMED INSPECTION PER MM 5-51-14, FOUND RIGHT INBOARD FLAP FOREFLAP DAMAGED OUT OF SRM LIMITS. REMOVED FLAP AND REPAIRED IAW SRM 51-70-07 AND MM 57-52-31. INSTALLED FLAP AS EPR MM 27-51-02. (M) 2L74 4F RT1384945 20031231001292003123100129NM 2003 12 31 AWXA200301632 120031212A5313655292898 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 26 LT BETWEEN BS 727A & BS 727B. MAINTENANCE CUT OUT DAMAGED STRINGER 26 LT BETWEEN BS 727A & BS 727B; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER PER DWG 65-52928 AND A STRINGER SPLICE CHANNEL; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201 PG 201-207. 2L72 4F RTA16WE 20040105000242004010500024NM 2004 1 5 DL767031012 120031112A5753113T122620 SUPPORT FITTING BOEING767 767232 1385132NM RT INBD FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27102DA 22214 CORROSION WAS FOUND IN THE HOLE BORES OF THE 6 FASTENERS WHICH ATTACH THE INBOARD FLAP TO THE OUTBOARD SUPPORT FITTINGS. THE HOLES WERE OVERSIZED, HFEC INSPECTED, AND BUSHED. THE ASSEMBLY WAS REINSTALLED WITH ORIGINAL STYLE HARDWARE. THE REPAIR WAS ACCOMPLISHED PER ER/A 087692-14. 2L72 4F RTA1NM 20040105000252004010500025NM 2004 1 5 03362420 120031228A3244 TIRE DORNERDO32 DO328300 NM NLG WORN A VTZAK NONE O OTHER TXTAXI/GRND HDL 1 EA27420FJ 3178 DURING TAXI THE CREW REPORTED THE AIRCRAFT PULLING HARD TO THE RIGHT. THE NOSE TIRES WERE FOUND TO BE WORN UNEVENLY AND WERE REPLACED. THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030916001442003091600144WP 2003 9 16 ARWA20030505 120030527A53205894282501 CLIP DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CRACKED A ARWAO OTHER O OTHER ININSP/MAINT 1 SO19784AL 46135 NR 194. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND;FORWARD LOWER CARGO COMPARTMENT STATION 300, BETWEEN L-33R & L-34R FITTING WITH CRACK. REMOVED AND REPLACED FITTING ON FOWARD LOWER CARGO COMPARTMENT STA.300 BETWEEN L-33R & L-34R IAW WITH SRM 51-1-20 (D) AND 51-1-21. 2L74 4F4 F 4A25 1E8 20030917000412003091700041CE 2003 9 17 S2YA03015 120030416A2750DT2PA7 SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA FLAP LIMIT INOPERATIVE A S2YAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL13881SK UE88 DURING TAKEOFF OF FLIGHT 1076, THE CREW HEARD A LOAD POP FROM WHAT THEY REPORTED WAS THE LEFT ENGINE. THEY NOTED STRONG FUMES IN THE COCKPIT AND DONNED THEIR OXYGEN MASKS. THE CREW TURNED OFF THE ENVIRONMENTAL AIR, IAW THE QRH AND MADE AN AIR-TURN-BACK. MECHANIC INSPECTED THE AIRCRAFT, FOUND THE FLAP MOTOR HAD BURNED OUT AND EMITTED THE ODOR. MECHANIC MEL-ED THE FLAP SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. ON 04/19/03 MECHANIC CLEARED THE MEL BY REPLACING THE FLAP MOTOR, GEAR BOX AND UP LIMIT SWITCH. THE UP LIMIT HAD FAILED, ENABLING THE FLAP MOTOR TO KEEP RUNNING AND BURN OUT, CAUSING THE FUMES. 2L72 4T3 TRTA24CE E2NE 20030917000502003091700050NE 2003 9 17 SIMA200316401 220030611A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT INOPERATIVE A SIMAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 SW21329AE22926 340B329 AT 11,000 RT ENGINE MADE A LOUD BANG. OIL PRESSURE LIGHT CAME ON AS OIL PRESSURE DROPPED. ITT EXCEEDED 1200C AND INCREASING RAPIDLY, ENGINE SHUT DOWN PERFORMED. SUP-MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW WORK CARD. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (PTRS NR: SW21200305091) 2L72 4T4 TRTA52EU E8NE 20030912001442003091200144NM 2003 9 12 AWXA200300902 120030725A53206546592 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 770, LBL 5. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF FLOOR SUPPORT BS 770, LBL 5; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-70-53 FIG. 201, PG 1. 2L72 4F RTA16WE 20030912001762003091200176NM 2003 9 12 AALA20030868 120030819A3350 PIN BOEING757 757223 1384957NM CONNECTOR LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21175AN 32394 SFO - AISLE EMERGENCY LIGHTS BOTH INOPERATIVE AT 16D. RESECURED PIN IN CONNECTOR AT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030912001802003091200180WP 2003 9 12 AALA20030878 120030820A3350 BATTERY PACK DOUG DC9 DC983 3022083WP LAVATORY DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21974TW 53624 MULTIPLE AFT CABIN EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED AFT BATTERY PACK IN LEFT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030917000602003091700060SW 2003 9 17 ALGA089171 120030912A6320204040785003 SPIDER BELL 412 412 1182202SW MAIN ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XATAM 33169 TRANSMISSION DISASSEMBLED FOR METAL IN OIL, FOUND LOWER PLANETARY SPIDER CRACKED.REMOVED AND REPLACED LOWER PLANETARY SPIDER. 1G72 4U H4SW 20030917000852003091700085NM 2003 9 17 2003F00559 120030906A2910AE7079101 FLEX LINE AIRBUSA319 A319132 3930340NM NR 2 ENGINE DAMAGED A RJEFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO23473TA 1140 DURING CRUISE FLIGHT, AN ECAM WARNING MSG 'HYD YELLOW RESERVOIR LOW LEVEL' WAS DISPLAYED, ALSO A YELLOW HYDRAULIC SYSTEM LOW PRESS MESSAGE CAME, THE AIRCRAFT DEVIATED ITS SCHEDULE FLIGHT TO EL SALVADOR STATION FOR MAINTENANCE. AFTER LANDING AT SAL STATION, TECHS PERFORMED INSPECTION OF THE AIRCRAFT AND FOUND A LEAK ON HYDRAULIC LINE OF THE PRESSURE TRANSDUCER ON ENGINE NR 2. THE HYDRAULIC LINE WAS REPLACED, TESTED AND LEAK CHECK AS PER AMM 29-11-17. ALSO, BLEEDING PROCEDURES OF THE YELLOW HYDRAULIC SYSTEM WAS PERFORMED AS PER AMM 29-00-00-870-004. ALL RESULTS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20030917000872003091700087NM 2003 9 17 AMTA200301123 120030901A2840 INDICATOR BOEING757 75733N 1384931NM RT FUEL CELL MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11550TZ 32584 FUEL TANK, RIGHT, QTY INDICATOR EICAS MSG FUEL QTY IND DISPLAYED. DEFERRED PER MEL 28-41-11 AUTH NR D28SE01-0103. (M) 2L72 4F RTA2NM 20030917000892003091700089NM 2003 9 17 AMTA200301084 120030823A2560 BATTERY BOEING737 73783N 13844HINM MEGAPHONE DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11304TZ 30675 MEGAPHONE IN COMPT 704 NEEDS BATTERIES REPLACED. REMOVED AND REPLACED MEGAPHONE BATTERIES PER MM 25-34-00. OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030917000942003091700094NM 2003 9 17 GAIA03043SP 120030719A5310 BEAM BOEING727 7272J0 138407ENM BULKHEAD CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND VERTICAL BEAM BULKHEAD 1183 RBL 36.5 WL 249 INBOARD CHORD HAS A CRACK. REMOVED FASTENERS FOR ACCESS IAW 727 SRM 51-30-2. STOP DRILLED CRACK IAW B727 SRM 51-10-1. ACCOMPLISHED 727 HFEC INSPECTION. INSTALLED VERTICAL BEAM REPAIR IAW S/B 727 53-0192, DYG NR 65C34406 AND 51-30-2 AND BOEING REPAIR KIT 65C 34406-13. (M) 2L73 4F RTA3WE 20030917000962003091700096NM 2003 9 17 GAIA03023SP 120030719A5313 STRINGER BOEING727 7272J0 138407ENM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND FASI NR 35734, AT MAIN CABIN FRAME 720B, STRINGER 15R IS CRACKED FORWARD OF THE WING LIGHT. CUT OUT CRACK FROM STRINGER 15R IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 4.7 INCH BY 3.2 INCH, TWO FILLERS .100 7075-T6 4.7 BY .8 IAW SRM 53-10-3 FIG 5, INSTALLED PARTS IAW SRM 51-10-3 FIG 5. (M) 2L73 4F RTA3WE 20030917001112003091700111NM 2003 9 17 UIEA200300040 120030720A2610 CONNECTOR BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE NR 4 ENGINE LOOSE A UIEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA15518MC 23476 517877 DURING CRUISE, NR 4 ENGINE NACELLE TEMP INDICATOR SHOWED 5.9. STARTED FLUCTUATING TO 6.5, EVENTUALLY READING 7.0. ACCOMPLISHED ABNORMAL PROCEDURES IAW 3.26.10. AIRCRAFT DIVERTED. NO FUEL DUMPED. TROUBLESHOOTING FOUND 1 CONNECTOR LOOSE ON LT LOWER DETECTOR AFT (B) LOOP, UPPER FORWARD DETECTOR RT (A) LOOP. 2 EACH GROMMET RIVETS MISSING FROM LT LOWER DETECTOR AT 7 O`CLOCK. 3 HOT AIR LEAKING TRACES FROM 15TH STAGE TO HPT COOLING AIR MANIFOLD CLAMPS AT 5 AND 6 OCLOCK. CLEANED CONNECTORS AND RESECURED AND SECURED LOOP GROMMET TO THE TUBE. RETIGHTENED CLAMPS. FIRE SYSTEM TEST NORMAL. INDICATION NORMAL WITH ENGINE RUN IAW 26-11-00. 2L74 4F4 F A20WE E23EA 20030918000132003091800013NM 2003 9 18 03FDEA01512 120030911A532065453132 STRINGER CLIP BOEING727 727200 138407ENM BS 720F CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CRACKED STRINGER CLIP, BS 720F, STR 4 RT. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720F, STR 4R PER SRM 51-30-2. 2L73 4F RTA3WE 20030918000452003091800045NM 2003 9 18 GAIA03035SP 120030719A5720 STIFFENER BOEING727 7272J0 138407ENM LT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND LEFT WING FRONT SPAR STATION 475 VERTICAL STIFFENER CRACKED TWO FASI N/R 35923. FABRICATED STIFFENERS FROM MATERIAL 7075-T6 STRUT P/N 1505-29063, PO NR 3146124 DIM 10.125 INCH BY 2.25 INCH TWO EACH, INSTALLED IAW B727 SRM 51-30-2. (M) 2L73 4F RTA3WE 20030918000472003091800047NM 2003 9 18 2003F00570 120030701A5315 FLOORBEAM BOEING737 7372L9 1384497NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO27464AT 21278 DURING C-CHECK INSPECTION, THE FLOORBEAM UPPER CHORD WAS FOUND TO BE CORRODED AT THE L1 DOOR AT STATION 344 LBL 24. THE DAMAGE EXCEEDS THE ALLOWABLE DAMAGE LIMITATIONS AND IS BEING REPAIRED ON NON ROUTINE 031642. (M) 2L72 4F RTA16WE 20030918000552003091800055NM 2003 9 18 DL76G030710 120030729A5753113T11671 SUPPORT BOEING767 7673P6 1385105NM RT WING TE FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27154DL 25241 RT WING INBOARD FLAP, INBOARD SUPPORT BEAM NR 5 HAS HOLE BORE CORROSION. CORROSION WAS FOUND IN THE 4 FLAP ATTACH FASTENER HOLES ON THE INBD SUPPORT BEAM OF THE INBD FLAP AT THE NR 5 SUPPORT LOCATION. THE HOLES WERE OVERSIZED TO REMOVE CORROSION, HFEC INSPECTED, BUSHED, AND NEW FASTENERS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385478-14, REV A. 2L72 4F RTA1NM 20030918000602003091800060 2003 9 18 DL75K030716 420030803A3442 RADAR BOEING757 757232 1384965NM WX RADAR SYS INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO276713Y 30777 WX RADAR INOPERATIVE. 2L72 4F RTA2NM 20030918000762003091800076NM 2003 9 18 2003F00554 120030804A324026094724 STATOR DOUG MD11 MD11 3023602NM MLG BROKEN B K NONE O OTHER ININSP/MAINT 1 SO25620 BRAKE HAD THERMAL OXIDATION, 1 STATOR WAS BROKEN. 2L73 4F RTA22WE 20030918000862003091800086SO 2003 9 18 IMJ2003F00000 120030703A2710870005002 ACTUATOR GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY511* 54523EU AILERON RESTRICTED B IMJRO OTHER O OTHER NRNOT REPORTED 1 EA2533PJ 57 CREW REPORTS ROLL CONTROL STIFF OR BINDING ON APPROACH. FOUND RIGHT AILERON ACTUATOR CAUSING PROBLEM. SYSTEM CHECKED FREE UNTIL HYDRAULIC PRESSURE APPLIED, THEN RESTRICTION NOTICED UPON QUICK APPLICATION OF INPUT. UNIT CURE DATE OF 4Q77, TNS/TSO UNK 15150.4 ACTT, 10479 LDGS. 2L72 4F4 FRTA12EA E2EU 20030918001022003091800102SW 2003 9 18 FZO2003F00000 120030718A6510204040623011 DRIVE SHAFT BELL 205 205A1 1181414SW LYC T53 T5317A 41549NE TAIL ROTOR CHAFED E FZOAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 NM056288Y 30034 PILOT FELT HARMONIC VIBRATION DURING REDUCE POWER DECENT INTO DIP SITE. FOUND T/R DRIVE SHAFT PN 204-040-623-011 RUBBING ON 205-060-923-001 BOOT ASSY. BOOT SEAL ECE-300-3/3 OIL SOAKED AND DEBONDED FROM BOOT LETTING BOOT SIDE. DOWN AND AMAKING CONTACT WITH T/R DRIVE SHAFT. BOOT AND SEAL ARE BONDED WITH M-24 BOND MASTER. BHT-IPC-71-5-39. 1G71 4U4 U H1SW E17EA 20030918001422003091800142NM 2003 9 18 PCAA0308097 120030807A3397 LIGHT DHAV DHC8 DHC8102 2809003NM CABIN DISCONNECTED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13832EX 280 DURING ROUTINE MAINTENANCE VISIT THE EMERGENCY LIGHT IN AISLE ABOVE SEATS 4AC AND 4DF WAS FOUND NOT TO BE ILLUMINATING. CEILING PANEL WAS REMOVED ABOVE EMERGENCY LIGHT AND FOUND THAT A PLUG WAS DISCONNECTED. PLUG WAS RECONNECTED, AND THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030919000102003091900010SO 2003 9 19 CHQA000415 120030808A2611 SMOKE DETECTOR EMB 145 EMB145 3260210SO LAVATORY MALFUNCTIONED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11264 ON CLIMBOUT EICAS WARNING "LAV SMOKE" ACCOMPANIED BY FLIGHT ATTENDANT GALLEY HORN. AFTER INSPECTION BY FLIGH ATTENTDANT FOUND NO INDICATION OF SMOKE. REMOVED DEBRIS AROUND SMOKE DETECTOR IN LAV BY CLEANING GRND RAN W/CREW NO FAULTS NOTED PERF SMOKE IAW EMB 145AMM 26-14-000 NO DEFECTS 2L72 4F RTT00011AT 20030919000132003091900013WP 2003 9 19 03FDEA01239 120030810A5347 CARGO TRACK DOUG DC10 DC1030 3023501WP CARGO DECK GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 MAIN CARGO DECK CARGO TRACK GOUGED STA 575-675 2C RBL 47.50. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 26+51-33-01. 2L73 4F A22WE 20030919000142003091900014WP 2003 9 19 03FDEA01238 120030810A5753ARC050451 BRACKET DOUG DC10 DC1030 3023501WP LT FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 LT WING O/B FLAP IB FWD HINGE PANEL BRACKET CRACKED. REMOVED 2C FABRICATED AND INSTALLED BRACKET IAW SRM 51-31-01. 2L73 4F A22WE 20030919000392003091900039NM 2003 9 19 IU62003F00023 120030604A29102671716 HOUSING BOEING737 737* NM CHECK VALVE BROKEN B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 VALVE BODY IS BROKEN IN HALF. METAL FATIGUE. MAKE BODY STRONGER. (NR 177979) 2L72 4F RTA16WE 20030919000452003091900045NM 2003 9 19 IU62003F00029 120030613A2761654494710 HOUSING BOEING737 737* NM SPOILER ACTUATORCRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 3942 SPOILER ACTUATOR CRACKED AROUND SHOULDER ON THE INSIDE DIAMETER OF THE HOUSING. OLD STYLE HOUSING IS SUSCEPTIBLE TO CRACKING. REPLACE WITH NEW STEEL HOUSING. (NR 178307). 2L72 4F RTA16WE 20030919000472003091900047NM 2003 9 19 IU62003F00031 120030613A2710654484511 MANIFOLD BOEING737 737* NM AILERON PCU CRACKED A IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 5286A CRACKED MANIFOLD. OVER PRESSURIZED FILTER BOWL. (NR 178182) 2L72 4F RTA16WE 20030919000512003091900051SO 2003 9 19 CHQA00417 120030811A2611 WARNING LIGHT EMB 145 EMB145 3260210SO LAV SMOKE DETECTILLUMINATED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11264 DURING CLIMB OUT AFTER TAKEOFF, CREW RECIEVED "LAV SMOKE" INDICATION ON THE EICAS. WE HAD THE F/A GO BACK AND CHECK IT OUT, AND SHE TOLD US THERE WAS NO SMOKE, BUT SHE TOLD US IT WAS HOTTER THAN NORMAL BACK THERE. WE DECIDED NOT TO TAKE ANY CHANCES AND RETURN TO THE FIELD AND HAVE IT LOOKED AT BY MAINTANCE. THE LOG BOOK INDICATED SEVERAL DAYS BACK CREWS WERE RECIEVING SIMULAR INDICATIONS. RR'D APU. 2L72 4F RTT00011AT 20031006000832003100600083WP 2003 10 6 ARWA20030909 120030915A5410 STRUCTURE DOUG DC8 DC863F 302198FWP PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON WITH CRACK, AFT OF RT FORWARD MOUNT. 2L74 4F 4A25 20031006000962003100600096CE 2003 10 6 DXTA200300084 120030813A323399144522 ACTUATOR CESSNA750 750 2076810CE ALLSN AE300 AE3007A GL NLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07912QS4051 7500012 WHEN LANDING GEAR WAS RETRACTED ON TAKEOFF ALL THREE GEAR GREEN LIGHTS EXTINGUISHED BUT RED UNLOCK LIGHT REMAINED ON, GEAR WAS CYCLED , ALL INDICATIONS NORMAL. - TROUBLESHOT AND FOUND NLG ACTUATOR FAILED, REPLACED NOSE LANDING GEAR ACTUATOR IAW CE750 M/M CHAPTER 32-30-03 OPS AND LEAK CHECKED GOOD. 2L72 4J4 FRTT00007WITE6CH 20031006001412003100600141NM 2003 10 6 SWAA032007 120030909A53116516309 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED (2 EA) BS 277, BETWEEN STR 14R AND STR 16R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20031006001422003100600142NM 2003 10 6 SWAA032008 120030909A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) BS 277 AT STR 15R, BS 807 AT STR 26R AND BS 727B AT STR 18L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20031006001652003100600165NM 2003 10 6 SWAA031968 120030904A53116516301 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND BOTH LEFT AND RT FUSELAGE FRAMES CRACKED AT BS 188, STR 17R AND STR 17L. REMOVED AND REPLACED FRAMES PER SRM. 2L72 4F RTA16WE 20031007000152003100700015WP 2003 10 7 GTIA030684 120030920A3260833605 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP MLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23826NK 49391 ON DEPARTURE TPA, GEAR RETRACTION RED NOSE GEAR LIGHT STAYED ON. FOLLOWED QRH ON RETRACTING SECOND TIME, LEFT MAIN RED LIGHT ON, RECYCLED ALL LIGHTS WENT OUT CONT TO DTW. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS UNIT. PERFORMED GEAR SWING. GEAR INDICATION CHECKS OK. (M) 2L72 4F RTA6WE 20031007000202003100700020NM 2003 10 7 AALA20030706 120030630A2910272T45002362 LINE BOEING767 767223 1385123NM METERING VALVE LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21338AA 22335 APPROX 5 MINUTES INTO CRUISE ALTITUDE, 37,000 FT, AN EICAS MESSAGE APPEARED INDICATING LOW QUANTITY IN THE CENTER HYDRAULIC SYSTEM. AT THAT TIME THE QUANTITY INDICATED .57 AND CONTINUED TO DECREASE TO .28. THE GEAR AND FLAPS WERE DEPLOYED USING ALTERNATE PROCEDURES. RETURNED AND LANDED LAX WITHOUT INCIDENT. REPLACED LEFT BRAKE METERING VALVE LINE. SYSTEM GROUND CHECKED NROMAL OPERATION. (M) 2L72 4F RTA1NM 20031008000532003100800053NM 2003 10 8 UPS03441235 120030904A5347BAC15201566 CARGO TRACK BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, BS 500 - 520 RBL 46 TIE DOWN TRACK RT FLANGE CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 10 EXCEED SRM 53-10-01 FIG 1 LIMITS FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 6. CIC APPLIED IAW EO M5100-2780-E 2L74 4F4 F A20WE E20EA 20031009000162003100900016WP 2003 10 9 AALA20031005 120030914A3350HPD52751315 BALLAST DOUG DC9 DC983 3022083WP EMERGENCY LIGHT FAILED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21972TW 53622 POSSIBLE ELECTRICAL BURNING ODOR REPORTED COMING FROM ROW 24. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LIGHT BALLAST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031009000472003100900047SO 2003 10 9 SIMA200318103 120030628A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21631AE 145139 CREW REPORTED ALL OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. (M) 2L72 4T RTT00011AT 20031009000592003100900059NM 2003 10 9 03FDEA01627 120030924A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 STRINGER CLIP 5 RT CRACKED AT BS 720C. REMOVED AND REPLACED STRINGER CLIP AT BS 720C, STR 5R PER SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20031009000672003100900067SO 2003 10 9 SWIA200312391 120030907A27223081401003 ACTUATOR EMB 120 EMB120ER 3260203SO LINEAR MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07561SW8112 8112 120335 INFLIGHT, MOMENTARILY WAS NOT ABLE TO GET MORE THAN 1 INCH TRAVEL OUT OF RIGHT RUDDER PEDAL. RAN QRH, CYCLED BLUE RUDDER SYSTEM AND PROBLEM COMPLETELY ELIMINATED WITH NO FURTHER PROBLEMS. REMOVED AND REPLACED BLUE HYD SYSTEM RUDDER ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-22-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20031009000812003100900081SO 2003 10 9 SWIA200312403 120030809A5610 BRACKET EMB 120 EMB120ER 3260203SO COCKPIT WINDOW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07298SW 120328 CRACKED BRACKET AT CAPTAIN'S DV WINDOW AFT FRAME. (DISCOVERED DURING C-CHECK INSPECTION)REMOVED AND REPLACED CAPTAIN'S DV WINDOW AFT FRAME BRACKET WITH A SERVICEABLE UNIT IAW EMB SRM 51-10-02. 2L72 4T RTA31SO 20031009000822003100900082SO 2003 10 9 SWIA200312404 120030809A5415 CHANNEL EMB 120 EMB120ER 3260203SO NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07298SW 120328 BLUE HYDRAULIC PACK LOWER SUPPORT CHANNEL CRACKED IB EDGE. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED LOWER SUPPORT CHANNEL WITH SERVICEABLE UNIT FOR BLUE HYDRAULIC PACK. 2L72 4T RTA31SO 20031009000982003100900098EA 2003 10 9 COMA0360418 120030914A2150 ACM CNDAIRCL600 CL6002B19 1900309EA CABIN COOLING INOPERATIVE A COMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01967CA 7134 FLT 5674, SMOKE IN THE CABIN - RT AC PACK TEMP AT 120 DEGREES C. DEFERRED MAINT ON RT AC PACK IAW MEL. 2L72 4F RTA21EA 20031009001032003100900103NM 2003 10 9 QXEA200301133 120030914A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 BROKEN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09365PH 526 ON FLIGHT 2079 EMERGENCY LIGHTS AT FORWARD CABIN ARE BROKEN. LENS IS SHATTERED. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031009001052003100900105NM 2003 10 9 PCAA0309111 120030917A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13842EX 341 WHILE PERFORMING MAINTENANCE POSTFLIGHT INSPECTION, ONE FLOOR LEVEL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. A BROKEN WIRE WAS FOUND AND REPAIRED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031009001092003100900109SO 2003 10 9 C2XA03BT092 120030911A3350110049 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712567 145623 CREW REPORTED, FIRST TWO SETS OF EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW EMB145 AMM 33-50-04. 2L72 4T RTT00011AT 20031009001142003100900114WP 2003 10 9 CALA0300532 120030917A5350 CABLE DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW2716806 49260 THE TAIL CONE INNER RELEASE HANDLE REQUIRED EXCESSIVE FORCE TO PULL. THE TAIL CONE CABLE WAS ADJUSTED, CLEANED AND LUBRICATED IAW MM 53-53-00. AN OPERATIONAL CHECK WAS GOOD. 2L72 4F A6WE 20031009001232003100900123NM 2003 10 9 QXEA200301136 120030916A6120YD4N RELAY DHAV DHC8 DHC8202 2809007NM ZONE 400 FAILED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09345PH 476 ON FLIGHT 2175 DURING NR 1 AUTOFEATHER TEST, THE UPTRIM AND ALTERNATE FEATHER LIGHTS ILLUMINATED, BUT THE NP RPM DOES NOT DECREASE TOWARDS FEATHER. REMOVED AND REPLACED 6121-K1 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031009001252003100900125NM 2003 10 9 QXEA200301138 120030916A5260 TRACK BOMBDRDHC8 DHC8401 1390041NM AIRSTAIR LACK OF LUBE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09413QX 4060 ON FLIGHT 2365 AFT AIRSTAIR IS DIFFICULT TO EXTEND. CLEANED AND LUBED TRACKS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031009001262003100900126EU 2003 10 9 AWXA200301063 120030918A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 221 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM THE FORWARD LT EMERGENCY LIGHT BATTERY PACK WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031010000082003101000008NM 2003 10 10 USAABB03157 120030905A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031010000102003101000010NM 2003 10 10 USAABB03159 120030905A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT LOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 FOUND EMERGENCY LIGHT AT ROW 7 INOPERATIVE. MAINTENANCE REPAIRED A CONNECTION AT ROW 7 RIGHT. (M) 2L72 4F RTA1NM 20031010000162003101000016NM 2003 10 10 USAABB03155 120030903A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19633AU 27811 FOUND EXIT IDENTIFIER AT R3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031010000222003101000022NM 2003 10 10 USAASB03153 120030825A2750 CONTROL UNIT BOEING737 737301 1384611NM TE FLAPS MALFUNCTIONED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19585US 23930 AFTER TAKEOFF FROM TPA, CREW REPORTED UNABLE TO RETRACT FLAPS BEYOND 2 UNITS. CREW RECYCLED FLAP HANDLE AND FLAPS CIRCUIT BREAKER SEVERAL TIMES WITH NO HELP. FLIGHT RETURNED TO FIELD AT TPA WITH 2 UNITS FLAPS AND FULL SLATS. FLIGHT LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED. (M) 2L72 4F RTA16WE 20031010000252003101000025NM 2003 10 10 USAABB03165 120030914A3350873203193REV9 CONTROL MODULE BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 FOUND ALL TEN FLOOR LEEL EMERGENCY LIGHTS AND ALL EIGHT EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REPLACED THE R2 DOOR EMERGENCY LIGHT CONTROL MODULE, CONTROL MODULE BATTERIES, EXIT IDENTIFIER BATTERIES ADN FLOOR LEVEL LIGHT BATTERIES. (M) 2L72 4F RTA2NM 20031010000292003101000029NM 2003 10 10 USAABB03146 120030823A3350873100151REV12 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU 27123 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 23 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031010000412003101000041SO 2003 10 10 C2XA03IA094 120030917A282014528796001 FITTING EMB 145 EMB145XR SO NR 1 ENGINE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718102 145643 DURING POST FLIGHT THE CREW NOTED EVIDENCE OF A FUEL LEAK ON NR 1 ENGINE. MAINTENANCE FOUND A CRACKED FITTING ON THE NR 1 ENGINE FPMU. THE FITTING WAS REMOVED AND REPLACED, AND A LEAK CHECK WAS PERFORMED, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20031010000442003101000044NM 2003 10 10 03FDEA01584 120030919A5230 HANDLE BOEING727 727200 138407ENM CARGO DOOR INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25280FE 22347 MAIN CARGO DOOR LIGHT ILLUMINATED AIRBORNE. RETURNED TO DLH. LANDING OK AND PRESSURIZATION OK. FOUND SHORT IN LIGHT IN VENTRAL DOOR STAIR HANDLE AFT COMPARTMENT ON A/C. REPAIRED AS REQUIRED. OPS CHECK NORMAL. 2L73 4F RTA3WE 20031010000482003101000048NM 2003 10 10 03FDEA01570 120030918A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION INSIDE STRINGER CHANNEL BS 1090, STR 27 LT. **SD** COMING 2L73 4F RTA3WE 20031006001802003100600180NM 2003 10 6 03FDEA01646 120030926A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON FLOORBEAM BS 344, LBL 42, WL 208. REMOVED CORROSION ON FLOORBEAM BS 344, LBL 42, WL 208. AREA REMOVED 2 X 1 X .022 INCH. ORIGINAL THICKNESS .125 OUT OF LIMITS CUT OUT DAMAGED AREA. 2 X 1 INCH FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PARTS PER SRM 51-10-6, 53-10-1, DRAWING SR 27-53-017A. 2L73 4F RTA3WE 20031007000182003100700018NM 2003 10 7 AALA20030978 120030908A3350D71702001 BATTERY BOEING777 777223 1385213NM EMERGENCY LIGHT FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21766AN 32880 EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROWS 20 THROUGH 25. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20031007000232003100700023NM 2003 10 7 AALA20030534 120030505A5753 WEDGE BOEING767 767223 1385123NM TE FLAP DELAMINATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21327AA 22327 DURING OVERNIGHT MAINTENANCE, RIGHT OUTBOARD TRAILING EDGE FLAP TRAILING EDGE WEDGE HAS .75 BY .375 INCH HOLE AND 41 INCH CRACK IN THE LOWER SKIN SURFACE OUTBOARD OF THE OUTBOARD HINGE FAIRING. DAMAGE COVERED WITH SPEED TAPE FOR FERRY TO AFW FOR FURTHER EVALUATION/REPAIR. (M) 2L72 4F RTA1NM 20031007000332003100700033EA 2003 10 7 ASOA03404 120030831A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CONTAMINATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A GROUND IN ATL, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS TWO AND FOUR WERE FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED WATER AND DIRT FROM THE EMERGENCY FLOOR LIGHT CONNECTORS BETWEEN ROWS TWO AND FOUR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031007000382003100700038 2003 10 7 AALA20030812 420030715A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21621AM 24579 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST OT CHEKC GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, SIX GIRT BAR SPRINGS NEED REPLACEMENT. REPLACED SIX GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NROMAL OPERATION. (M) 2L72 4F RTA2NM 20031007001192003100700119CE 2003 10 7 DXTA200300118 120030915A3260 WARNING LIGHT CESSNA750 750 2076810CE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07942QS 7500024 AT FL 340 CREW HEARD THE NOSE GEAR EXTEND AND OBSERVED THE GEAR UNLOCK LIGHT ILLUMINATED, UPON WHICH IT RETRACTED BACK AND INDICATIONS WENT OUT. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20031008000632003100800063NM 2003 10 8 USAABB03170 120030922A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20031009001112003100900111SO 2003 10 9 C2XA03BT094 120030915A33501317 LIGHT EMB 145 EMB145ER 3260211SO CABIN FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 CREW REPORTED, OVERHEAD EMERGENCY EXIT LIGHT AFT SIDE, WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ON THE AFT SIDE IAW EMB145 AMM . OPS CHECKED GOOD. 2L72 4F RTT00011AT 20031009001212003100900121WP 2003 10 9 0301769937 120030915A27805919526 DUCT DOUG DC9 DC931 3022065WP RT WING DAMAGED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01908H 47517 RT LEADING EDGE SLAT DID NOT EXTEND DURING APPROACH FOR LANDING. THE SLAT DISAGREEMENT LIGHT DID ILLUMINATE AND THE SLAT EXTEND LIGHT DID NOT. THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO THE RIGHT UNTIL SLATS WERE RETRACTED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT (T) DUCT AND RIGGED THE LEADING EDGE SLAT SYSTEM. AIRCRAFT STILL OUT OF SERVICED AT THIS TIME. 2L72 4F A6WE 20031010000762003101000076EA 2003 10 10 03260648 120030917A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27648BR 7406 DURING INSPECTION THE FOWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031010000852003101000085 2003 10 10 BAQA089232 420030918A22117004206901 COMPUTER BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101* NE CSAS FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911WS 7068 PITCH AND ROLL CSAS KEEP KICKING ON AND OFF. REPLACED WITH SERVICEABLE UNIT. 9/23/03 1G72 3U3 U H13EU E5NE 20031124001102003112400110WP 2003 11 24 DHL2003805543 120030731A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING OUTBD L/E FORMER 0.500 CRACKED AT STA XFS 760.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REMOVAL AND INSTALLATION OF OTBD L/E SEE NR 0345. 2L74 4F RT4A25 20031124001202003112400120WP 2003 11 24 DHL2003802514 120031115A5712 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING L/E FORMER CRACK 0.500, STA XFS 641.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031124001362003112400136NM 2003 11 24 USAA030221 120031002A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 CLT - FOUND FLOORBEAM CORRODED 24 INCHES LONG, BS 700 LBL 50 CABIN FLOOR LEVEL. REPAIRED PER TYPICAL REPAIR 53-15-01. (M) 2L72 4F RTA2NM 20031125000022003112500002WP 2003 11 25 DHL2003802515 120031115A5712 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING L/E FORMER CRACK 0.500 STA XFS 578.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031121000502003112100050 2003 11 21 SWAA032488 420031110A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031121000592003112100059CE 2003 11 21 55918 120031107A3260 UPLOCK SWITCH BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 CE07171ZV UE171 CREW REPORTED WITH LANDING GEAR RAISED INTRANSIT LIGHTS REMAINED ILLUM. CREW DECLARED AN EMERGENCY, AND RETURNED TO FIELD WITH NO FURTHER INCIDENTS. ACFT FERRIED TO DUJ FOR MAINTENANCE. GEAR INTRANSIT LIGHT W/N EXTINGUISH WHEN UP. REMOVED AND REPLACED RT GEAR UP LOCK SWITCH, CKS GOOD. PART REPLACE IEN412-3, TOOK OFF AN-3-5A M81829/12. 2L72 4T RTA24CE 20031121000612003112100061EU 2003 11 21 DXTA200300164 120031116A3232 ACTUATOR ISRAELGALAXYGALAXY 4500307EU MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07702QS 070 AFTER TAKEOFF DURING FLAP RETRACTION THE LEFT AND NOSE GEAR UNLOCK LIGHTS ILLUMINATED AND THE RIGHT GEAR WENT TO RED, ACCOMPLISHED AIR TURNBACK TO LAS. ADJUSTED RIGHT HAND MLG ACTUATOR LOCK PRESSURE TO THE GULFSTREAM -200 MM CHAPTER 32-10-10, PERFORMED FUNCTIONAL CHECK OF LANDING GEAR PER IAW MM CHAPTER 32-30-00, OPS CHECK GOOD. 2L72 4F RTA53NM 20031121000642003112100064NM 2003 11 21 03FDEA01922 120031026A5753ARC2517501 STRAP DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD STRAP NEAR PIVOT BORE FOUND CORROSION. LEFT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD STRAP REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. STRAP WAS FABRICATED AS PER DRAWING ARC2517. 2L73 4F RTA22WE 20031121000652003112100065NM 2003 11 21 03FDEA01952 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 RIGHT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR HOLE MOUNT I/B CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, I/B HINGE FITTING I/B ACTUATOR HOLE MOUNT CORROSION R & R AS PER FEDEX EA 1-5740-74250. WINGS - LT & RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031121000802003112100080 2003 11 21 VNAA0310022 420031029A22107015327905 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AUTOPILOT FAILED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL07433JS15209389 3047 SMOKE IN AIRCRAFT FROM AUTOPILOT CONTROL PANEL. SMOKE CLEARED AFTER AP/YD TURNED OFF. MAINTENANCE INSPECTED AND REPLACED THE AP CONTROL PANEL IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031125000272003112500027WP 2003 11 25 DHL2003805561 120030806A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS 635.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON RT OUTER WING INBD L/E STA XFS 635.000 (UPPER PART) IAW SRM 57-2-0 PG 9-10 SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000462003112500046WP 2003 11 25 DHL2003805571 120030811A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING OTBD FLAP LWR SKIN SHOWS INTERIM REPAIR, STA XF 333.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 AND SRM 57-7-1 FIG 4. REMOVED INTERIM REPAIR AND OLD PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 4. CLEANED, TREATED AND PRIMED THE NEW PLATING INTERIOR SURFACE IAW SRM 51-1-8B. INSTALLED NEW PLATING ON LT WING OTBD FLAP LOWER SURFACE (STA XF 333.000) IAW SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031125000622003112500062WP 2003 11 25 DHL2003802513 120031113A53204758514520N FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 1.000, STA 1190.000, L32R - L33R. REMOVED CRACK FITTING AT STA 1190.000, L-32R TO L-33R IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING AND FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000652003112500065WP 2003 11 25 DHL2003807506 120031007A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING CTR L/E UPPER FORMER 0.250 CRACK AT XFS 460.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000742003112500074WP 2003 11 25 DHL2003805594 120030829A535057103681 SKIN DOUG DC8 DC873F 302199FWP FAIRING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING-FUSELAGE NR 708 UPPER FAIRING INTERNAL SKIN DELAMINATED, STA 1040.000 - STA 1080.000. REMOVED AND REPLACED LEFT WING TO FUSELAGE UPPER FAIRING NR 708 (STA 1040.000 - 1080.000) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000812003112500081WP 2003 11 25 DHL2003805568 120030802A573056110111 SKIN PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED (STA XW.5.000 - 90.000). REMOVED AND REPLACED PANEL ASSY ON LEFT WING T/E LWR PART STA XW 5.000 - 90.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000912003112500091WP 2003 11 25 DHL2003805587 120030827A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLOT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING EXTENDED L/E OUTBD VANE FWD PLATING ELONGATED HOLES AROUND STA XOLDO.67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, THE EXISTING INTERIM REPAIR AND FILLER. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR EXTERNAL DOUBLER, AN INTERNAL DOUBLER AND A FILLER. CLEANED, TREATED AND PRIMED THE REPAIR EXTERNAL DOUBLER INTERIOR SURFACE, FILLER AND INTERNAL DOUBLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE EXTERNAL DOUBLER AND INTERNAL DOUBLER AND FILLER ON LEFT WING EXTENDED L/E OTBD VANE FWD PLATING (AROUND STA XOLDO.67) USING NEW FASTENERS. 2L74 4F RT4A25 20031125000962003112500096NM 2003 11 25 AALA20031287 120031117A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21790AN 30251 DFW EMERGENCY PATH LIGHT FIXTURE IN GALLEY NEXT TO L1 DOOR BROKEN. REPLACED EMERGENCY PATH LIGHT FIXTURE IN GALLEY NEXT TO L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031125001072003112500107NE 2003 11 25 QXEA200301408 220031106A73104120T03P04 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT ENGINE LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09606QX 10023 965294 PDX- ON FLIGHT 2439 LEFT ENGINE FUEL LEAK. REMOVED AND REPLACED SLAVE COMPRESSOR VARIABLE GEOMETRY ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20031125001112003112500111SW 2003 11 25 2003F00614 120030721A5270 WARNING SYSTEM FRCHLDSA227 SA227DC 3377521SW COCKPIT ACTIVATED A BSAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM05853LS DC853B HLN - FLT 2583 - CARGO DOOR WARNING LIGHT CAME ON IN FLIGHT, CREW DIVERTED TO NEAREST STATION. DOOR CLOSING PROCEDURES OF DOOR IS HARD TO CLOSE. MAINTENANCE INSPECTED THE CARGO DOOR AND LATCHING SYSTEM. FOUND NO OBVIOUS DEFECTS. CLEANED, LUBED AND CHECKED CLICK CLACKS AND SWITCHES. NO PROBLEMS WERE FOUND. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED. NO DEFECTS WERE NOTED DURING THE OCF. (M) 2L72 4T RTA18SW 20031125001342003112500134NM 2003 11 25 ASAA0310266 120030401A53116545815531 FRAME BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FRAME AT BS 344, LEFT BUTTOCK LINE 62, RIGHT BUTTOCK LINE 62 CORRODED. REMOVED DAMAGE AND REPAIRED FRAME PER SRM. (M) 2L72 4F RTA16WE 20031125001512003112500151NM 2003 11 25 ASAA0310506 120030603A5313 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE STRINGER 25L AT FUSELAGE STATION 352 CORRODED. REMOVED DAMAGED SECTION OF STRINGER AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031125001612003112500161NM 2003 11 25 ASAA0310510 120030603A5315BAC15061702 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 520, BUTTOCK LINE 0, LEFT BUTTOCK LINE 24.5 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER EA. (M) 2L72 4F RTA16WE 20031125001622003112500162NM 2003 11 25 ASAA0310511 120030603A5311 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 747, STRINGER 19L - 20L CRACKED AND CHAFED. REMOVED AND REPLACED SECTION AND REPAIRED FRAME PER SRM. (M) 2L72 4F RTA16WE 20031126000242003112600024NM 2003 11 26 03FDEA01928 120031117A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB RIGHT UPPER FWD PLANK NR 2R BARREL NUT BORE FOUND CORROSION ON BOTTOM & SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-74245, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000 2L73 4F RTA22WE 20031126000312003112600031WP 2003 11 26 DHL2003807515 120031014A53203754220503N SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SPLICE FITTING 9.000 CRACK (STA 220.000 - 240.000 L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS AND PRC SEALANT IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20031126000572003112600057NM 2003 11 26 CALA0300662 120030716A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND FLOORBEAM CORRODED IN AFT LAV AREA AT STA 1016, RBL 10. INSTALLED REPAIR STRAP IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20031126000672003112600067NM 2003 11 26 AWXA200301473 120031007A531165465951 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 LCQ - MAJOR REPAIR - DURING C-14 CHECK 2 EACH CRACKS WERE FOUND IN FASTENER HOLES ON THE RT FUSELAGE FRAME AT BS 727, BETWEEN WL 195 AND WL 202. MAINTENANCE OVERSIZED HOLES AND PERFORMED HFEC INSPECTION TO VERIFY CRACKS CONTAINED, NO CRACK INDICATIONS WERE NOTED. MAINTENANCE ACCOMPLISHED IAW AWA ER 15-5331-03267-SS2. 2L72 4F RTA16WE 20031126000782003112600078SO 2003 11 26 C2XA03SH391 120031017A711014576631622 STRUCTURE EMB 145 EMB145 3260210SO NR 2 COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV-DURING C-CHECK THE NR 2 LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126001032003112600103SO 2003 11 26 C2XA03SH462 120031119A531514532637401 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER REINFORCEMENT REPAIR IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040415000102004041500010EU 2004 4 15 ERAA093691 120030503A642010531714 ROTOR HEAD BOLKMS105 BO105A EU ALLSN 250C 250C20 03013GL TAIL ROTOR DAMAGED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH S675 INNER SLEEVE BUSHINGS DEBONDED. OB BUSHINGS 2 EA ON INNER SLEEVE CRACKED. BOTH RINGS IN BOTTOM OF GRIPS MECHANICALLY DAMAGED. IB INNER SLEEVE BUSHINGS WORN. TEETER BUILT BUSHINGS WORN AND MECHANICALLY DAMAGED . ALL FOUR TEFLON GRIP BUSHINGS WORN. ONE GRIP CAP BROKEN. DISASSEMBLED, CLEANED, REMOVED PAINT AND PRIMER AND VISUALLY INSPECTED ALL PARTS. C/W NDT INSPECTION REPLACED ALL PARTS WORN, CORRODED, OR MECHANICALLY DAMAGED BEYOND LIMITS. REASSEMBLED T/R ASSY WITH NEW NUTS, WASHERS, AND COTTER PINS. INSTALLED SERVICEABLE BLADES AND STATIC BALANCED. C/W 1200/2400 6 YR INSPECTION 300/2400 HR BLADE INSPECTION. CW BY AEC C/W ASB 105-10-116 TABLE 1 INSP. 1G72 3U3 U H3EU E4CE 20040415000772004041500077WP 2004 4 15 ASAA0380746 120031114A53219936688503 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD STATION 808 TO 823, RBL 22 TO RBL 44 DELAMINATED AT CORNER. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20040419000452004041900045EU 2004 4 19 USAABA03022 120030702A4997 WIRE HARNESS AIRBUS330 A330323 3930335EU APU IDG FAILED A USAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA19673UW 0337 LGW - FLT 99 EN ROUTE LGW-PHL, THE LEFT GENERATOR WENT INOPERATIVE AND COULD NOT BE RESET. THE APU WAS STARTED, BUT PERFORMED AND AUTO SHUTDOWN AFTER FIVE MINUTES OF OPERATION. FLIGHT RETURNED TO LGW. EN ROUTE BACK TO LGW, THE APU WAS RESTARTED, BUT SHUTDOWN AGAIN. MAINTENANCE REPLACED THE IDG WIRING HARNESS. THE FUEL FLOW DIVIDER, FUEL CONTROL UNIT AND ELECTRONIC CONTROL BOX WERE REPLACED. IT IS NOT KNOW WHICH COMPONENT FIXED THE PROBLEM. (M) 2L72 4F RTA46NM 20040419001132004041900113EA 2004 4 19 A6WA200340207 120031223A2701 YOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT LOOSE A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31401AW 7280 CHECKED THAT PLAY EVIDENT IN CONTROL YOKE PITCH AXIS IS WITHIN ACCEPTABLE LIMITS. COMPLIED WITH AMM TASK 27-32-00-720-801. FOUND CONTROL YOKE BACKLASH AT .28 DEGREES. BACKLASH LIMITS ACCEPTABLE. (M) 2L72 4F RTA21EA 20031124000432003112400043NM 2003 11 24 03FDEA01932 120031110A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE NR 1 OUTBOARD CORRODED. LT WING I/B FLAP, O/B HINGE PIVOT HOLE NR 1 O/B CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5750-74248. WINGS - LEFT I/B TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20031124000652003112400065NM 2003 11 24 03FDEA01930 120031110A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE NR 1 INBOARD FLANGE SIDE CORRODED. LT WING I/B FLAP, O/B HINGE PIVOT HOLE NR 1 I/B FLANGED SIDE CORROSION. R & R AS PER FEDEX EA 1-5750-74248. WINGS - LEFT I/B TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20031124000812003112400081WP 2003 11 24 DHL2003807533 120031024A572036169322 CLIP DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NR 4 MAIN TANK INTERNAL PART CLIP CRACKED STA XRS 172.000, S-74, REF ACCESS DOOR 505D. REMOVED AND REPLACED CRACKED CLIP ON NR 4 MAIN TANK INTERNAL PART STA XRS 172.000, S-74 (ACCESS DOOR 505D) IAW SRM 51-1-20D. FOR LEAK CHECK SEE NR 1482. 2L74 4F RT4A25 20031124001142003112400114WP 2003 11 24 DHL2003807521 120031013A53209754055U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SHROUD COVER FITTING CRACKED 1.000 AT STA 280.000 L-35R. REMOVED CRACKED COVER FITTING STA 280.000 L-35R IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW COVERT FITTING IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031124001162003112400116WP 2003 11 24 DHL2003802523 120031115A5753 PLATE DOUG DC8 DC873 302199CWP T/E FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT I/B FLAP FWD UPPER PLATING SHOWS DENTS (STA XW 104.000-122.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF NEW PLATING IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031124001242003112400124NM 2003 11 24 GAIA03147ST 120031024A5311 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME DENTED BS 500 ABOVE STRINGER 17 RT. REF FASI N/R NR 61829, CUT OUT DAMAGE AND INSTALLED 9 INCH BY 6 INCH REPAIR DOUBLER PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20031124001392003112400139NM 2003 11 24 2003F00612 120030206A382097109323015 MOUNT BOEING737 737* NM WATER HEATER CRACKED A BJ6AK NONE O OTHER ININSP/MAINT 1 NE03127QS 30327 STRUCTURE FOR WATER HEATER AFT MOUNT FOUND DAMAGED. WATER HEATER IS SUSPENDED BY 6 POINTS. THE REAR MOUNTING STRUCTURE PREVENTS LATERAL MOVEMENT. IT APPEARS THE POSSIBLE CAUSE FOR THE DAMAGE IS A BURR AT THE SUBJECT MOUNTING HOLE. ALSO COULD BE DUE TO IMPROPER INSTALLATION/PRELOAD. THIS HEATER AND ASSOCIATED MOUNT STRUCTURE IS ADDED DURING AIRCRAFT COMPLETION. PART REPLACED. (M) 2L72 4F RTA16WE 20031125000152003112500015WP 2003 11 25 DHL2003807540 120031018A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT OUTER WING INBD L/E UPPER SKIN CORRODED XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED AND REMOVED DAMAGED AREAS IAW ASTAR ED EDU21-10, DWG U21-R10. PERFORMED NDT INSPECTION IAW DCO NDT SPM PART 6-10-01-001. FABRICATED (3) FILLERS, DOUBLER AND TRIPLER IAW ASTAR ED EDU21-10, ASTAR DWGU21-R10. CLEANED, TREATED AND PRIMED AREA, FILLER, DOUBLER AND TRIPLER INNER FACE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLERS, DOUBLER, TRIPLER WITH NEW FASTENER IAW ASTAR ED EDU21-10, ASTAR DWG U21, R10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000252003112500025WP 2003 11 25 DHL2003807546 120031018A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT OUTBOARD STUB WING UPPER SKIN CORRODED, STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED AND REMOVED DAMAGED AREA IAW ASTAR ED EDU21-7, ASTAR DWG U21-R07. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW ASTAR ED EDU21-7, ASTAR DWG U21-R07. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INNER FACE IAW SRM 561-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ASTAR ED EDU21-7, ASTAR DWG U21-R07, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000362003112500036WP 2003 11 25 DHL2003805517 120030808A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 461.372. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LEFT WING CTR L/E FORMER, STA XS 461.372 IAW SRM 57-2-0 PG 9, 10 SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000492003112500049WP 2003 11 25 DHL2003807549 120031019A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NOSE SECTION EXTERNAL SKIN SHOW INTERIM REPAIR AT STA 32.000, L-32R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ASTAR ED EDU21-12, ASTAR DWG U21-R12. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. TRIMMED OUT IAW ASTAR ED EDU21-12, ASTAR DWG U21-R12. PERFORMED NDT INSPECTION IAW DC8 NDT STANDARD PRACTICE MANUAL PART 6-10-01-001. FABRICATED 2 EA FILLERS AND DOUBLER IAW ASTAR ED EDU21-12, ASTAR DWG U21-R12. CLEANED, TREATED AND PRIMED AREA, FILLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ASTAR ED EDU21-12, ASTAR DWG U21-R12, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000692003112500069WP 2003 11 25 DHL2003807552 120031018A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT WING OUTBD L/E EXTERIOR SKIN CORRODED AT STA XW 761.695 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF PERMISSIBLE LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ASTAR ED EDU21-2, ASTAR DWG U21-R02. PERFORMED NDT INSPECTION IAW NDT STANDARD PRACTICE MANUAL PART 6.10-01-001. FABRICATED FILLER AND DOUBLER IAW ASTAR ED EDU21-2 AND ASTAR DWG U21-R02. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ASTAR ED EDU21-2, ASTAR DWG U21-R02, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000802003112500080WP 2003 11 25 DHL2003805566 120030814A5313S1616757 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 AFT FUSELAGE SECTION L-17R AT STA 1770.000 CRACKED 3.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED CRACKED L-17R IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031125000992003112500099NM 2003 11 25 QXEA200301414 120031109A5210D5D592395926 STRUT BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DEFECTIVE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09411QX841 841 4055 SEA- MAIN CABIN DOOR IS STIFF, DIFFICULT TO CLOSE. REMOVED AND REPLACED FORWARD AND AFT GAS SPRING STRUTS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031125001332003112500133NM 2003 11 25 ASAA0310261 120030401A5260656739320 SUPPORT ANGLE BOEING737 737298C 1384490NM AFT AIRSTAIRS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIRS SUPPORT ANGLE AT BS 947-948, WATERLINE 206-208 CORRODED AND HAS ELONGATED HOLES. REPLACED SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031125001382003112500138NM 2003 11 25 ASAA0310147 120030317A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 887-947, BUTTOCK LINE 0 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040311000102004031100010NM 2004 3 11 ASAA0310125 120030307A532069366771 SUPPORT ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SUPPORT ANGLE AT BS 986, STRINGER 24R-27R CORRODED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031126000062003112600006EU 2003 11 26 RAIA00311284 120031109A3241 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU ANTI-SKID SYS LOOSE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03560HK 41076 5523-STL- BRAKE ANTI-SKID INOP. MAINTENANCE REMOVED AND RECONNECTED CANNON PLUG ON NR 1 WHEEL SPEED TRANSDUCER. 2L72 4T RTA41NM 20031126000252003112600025EU 2003 11 26 MALA030499 120031029A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434XJ 340B434 DURING 4K INSPECTING IN LCQ, LEFT NR 2 SEAT TRACK STA 302 HAS HEAVY CORROSION. VENDOR REMOVED AND REPLACED CORRODED SEAT TRACK IAW MESABA EO S53060, DATED 7 NOV 2000. RELEASE DATE 11/18/03. 2L72 4T RTA52EU 20031126000272003112600027EU 2003 11 26 MALA030501 120031111A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15527XJ E2352 DURING C-CHECK INSPECTION IN LCQ, FRAME 18 HAS AN 8 INCH CRACK RUNNING HORIZONTALLY. VENDOR REPAIRED FRAME 18, PER EO A53140. 2H74 4F RTA49EU 20031126000462003112600046SO 2003 11 26 C2XA03CL187 120031118A27403621005009 CONTROL UNIT EMB 145 EMB145XR SO HORIZ STAB FAILED A C2XAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW2711109 145657 CLE FLIGHT 2169 THE CREW REPORTED THAT THE BACK-UP TRIM WAS INOP IN FLIGHT. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20031126000912003112600091SO 2003 11 26 C2XA03SD002 120031109A801135059105 STARTER EMB 145 EMB145LR 3260212SO NR 1 ENGINE LEAKING A C2XAK NONE K FLUID LOSS APAPPROACH 1 SW2711547291 145563 LOST OIL NR 1 ENGINE ON FINAL APPROACH. QUANTITY AT 3 QUARTS. CONTRACT MAINTENANCE FOUND THE AIR TURBINE STARTER LEAKING. IAH MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR TURBINE STARTER IAW EMB 145 AMM 80-10-01. OPS AND LEAK CHECKED GOOD. 2L72 4T RTT00011AT 20031126000952003112600095SO 2003 11 26 C2XA03CL185 120031103A3260852701 PROXIMITY SWITCH EMB 145 EMB145XR SO LT MLG FAULTY A C2XAB EMER. DESCENT O OTHER CLCLIMB 1 SW2721130 145704 EWR FLIGHT 2106 THE CREW REPORTED A LOUD BANGING NOISE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE UPLOCK BOX PROXIMITY SWITCHES IN THE LEFT GEAR. MAINTENANCE ALSO REPLACED THE LGEU. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20031126000992003112600099SO 2003 11 26 C2XA03SH466 120031119A711014576057622 STRUCTURE EMB 145 EMB145ER 3260211SO RT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE RIGHT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126001112003112600111SO 2003 11 26 C2XA03SH394 120031018A711014576631622 STRUCTURE EMB 145 EMB145 3260210SO NR 2 COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE NR 2 LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126001232003112600123NM 2003 11 26 ASAA0310440 120030512A532065596593 STRAP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND STRAP AT BODY STATION 440, STRINGER 24R-26R CORRODED. REPLACED STRAP PER SRM. (M) 2L72 4F A16WE 20031202000102003120200010NE 2003 12 2 AMTA200301270 220031006A7200430101 PCU BOEING757 75723N 1384973NM RROYCERB211 RB211535E4B3 NE LT ENGINE FAILED A AMTAO OTHER J WARNING INDICATION DEDESCENT 1 GL11523AT 30232 ON DESCENT, LT EEC AND LT ENG LIMITER INOP LIGHTS ILLUMINATED. EICAS MSG LT ENG EEC AND LT ENG LIMITER DISPLAYED. ON ENGINE START STARTER DID NOT DISENGAGE AT 49 PERCENT. BIT BVCU FOUND CODE 06, REPLACED PCCU. ENGINE START AND OPS SATIS MM 73-21-10-4. (M) 2L72 4F4 FRTA2NM E12EU 20031202000172003120200017NM 2003 12 2 ASAA0340311 120030701A3350 CONNECTOR BOEING737 7374Q8 138447QNM ROW 20-25 DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01782AS 25113 DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 20-25. REPLACED CONNECTOR, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20031202000212003120200021EA 2003 12 2 ASOA03476 120031003A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11909EV 7658 DURING APPROACH INTO DFW FROM HSV, TEH CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WHEN SELECTING THE FLAPS TO 30 DEGREES FOR LANDING. QRH PROCEDURES WERE COMPLIED WITH AND A NORMAL LANDING ACHIEVED WITH FLAPS SELECTED AT 20 DEGREES. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031202000282003120200028NM 2003 12 2 ASAA0310496 120030602A551265737831 SKIN BOEING737 7372X6C 1384552NM FS 75 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 DURING SCHEDULED C-CHECK, FOUND THE HORIZONTAL STABILIZER LEADING EDGE AT FUSELAGE STATION 1049.602, STABILIZER STATION 75 DENTED. (M) 2L72 4F RTA16WE 20040311000532004031100053NM 2004 3 11 ASAA0310093 120030305A53156554913501 FLOORBEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOORBEAM WEB AT BS 947, LEFT BUTTOCK LINE 50 CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040311000462004031100046NM 2004 3 11 ASAA0310115 120030307A7110 ANGLE BOEING737 737298C 1384490NM NR 1 COWLING TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL ANGLE AT NACELLE STATION 105 TORN. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031202000302003120200030NM 2003 12 2 ASAA0340091 120030228A531065C25230 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE AT BS 727D RBL 8 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031202000322003120200032NM 2003 12 2 ASAA0310494 120030602A5347BAC15201430 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 727-727B, RIGHT BUTTOCK LINE 60 CORRODED. REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20031202000342003120200034NM 2003 12 2 ASAA0340086 120030228A53476548699175 CARGO TRACK BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON CARGO TIE DOWN FITTING. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031202000362003120200036NM 2003 12 2 ASAA0340089 120030228A53206547690 SUPPORT FITTING BOEING737 7374Q8 138447QNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM TO SIDEWALL SUPPORT AT BS 727E PLUS 8. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040114001842004011400184NM 2004 1 14 MASA200300502 120031219A3350 CONNECTOR DHAV DHC8 DHC8202 2809007NM CONTROL PANEL LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07455YV 455 CREW REPORTED THEY COULD NOT TEST THEIR EMERGENCY EXIT LIGHTS. MECHANIC RESECURED A LOOSE CONNECTOR TO THE TEST PANEL. OP CHECKS GOOD NO PARTS USED. 2H72 4T RTA13NM 20040114001922004011400192SO 2004 1 14 MASA200300435 120031103A335020131A CHARGER EMB 145 EMB145LR 3260212SO E/E BAY INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ3714 145218 RON IN CLT MX DISCOVERED 2 EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MECHANIC REPLACED THE NR 3 EMERGENCY LIGHTING BATTERY CHARGER. OPS CHECKS GOOD. 2L72 4T RTT00011AT 20040114001982004011400198NM 2004 1 14 MASA200300420 120031020A2560S16371 BATTERY DHAV DHC8 DHC8202 2809007NM FLASHLIGHT DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07449YV 449 PHX-DRO CREW REPORTED F/A EMERGENCY FLASHLIGHT INOPERATIVE. MECHANIC REPLACED THE BATTERY. 2H72 4T RTA13NM 20040114001992004011400199NM 2004 1 14 MASA200300437 120031104A243328VS200Y4DH TRU DHAV DHC8 DHC8202 2809007NM E/E BAY FAILED A MASAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW07444YV5012 444 DEN A/C POWER INDICATOR PANEL WAS SMOKING. MECHANIC REPLACED THE NR 1 TRU AND THE A/C POWER MONITOR POWER PANEL. OP CHECKS GOOD. 2H72 4T RTA13NM 20040114002042004011400204WP 2004 1 14 MWEA030435 120031024A3397 WIRE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE CABIN BROKEN A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31203ME 47673 EMERGENCY LIGHTS NOT WORKING. FOUND BROKEN WIRE AND REPAIRED. 2L72 4F4 F A6WE E2EA 20031014001162003101400116NM 2003 10 14 SWAA032151 120030924A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001172003101400117NM 2003 10 14 SWAA032150 120030925A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 EEPLS SECTION LOOSE IN CABIN. SECURED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20031014001192003101400119NM 2003 10 14 SWAA032173 120030928A2910272A4452182 LINE BOEING737 7377H4 1384404NM NR 2 SPOILER CRACKED A SWAAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW29707SA 27841 DECLARED EMERGENCY, ENGINE NR 1 'A' HYD LOW PRESS LIGHT ILLUMINATED, 'A' SYSTEM LEVEL DROPPED TO ZERO. FOUND, HOLE IN HYD DOWN LINE AT NR 3 SPOILER AUTUATOR. REMOVED AND REPLACED HYD LINE PER MM. 2L72 4F RTA16WE 20031014001272003101400127NM 2003 10 14 SWAA032165 120030928A57536546435273 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C4 CHECK, FOUND LT OUTBD T/E AFT FLAP DELAMINATED ON LOWER SIDE. REMOVED AND REPLACED LT OUTBD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20031014001332003101400133NM 2003 10 14 SWAA032159 120030925A3350BR2013 LIGHT BOEING737 7372H4 138448CNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED C1 CHECK, FOUND EEPLS SECTION LOOSE AND MISSING END CAP. SECURED EEPLS AND INSTALLED END CAP PER MM. 2L72 4F A16WE 20031014001412003101400141 2003 10 14 SWAA032052 420030914A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT SVC DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20031014001452003101400145 2003 10 14 SWAA032062 420030914A25651061323468 BOTTLE BOEING737 7373H4 1384600NM ESCAPE SLIDE LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING PREFLIGHT INSP, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20031014001472003101400147NM 2003 10 14 SWAA032060 120030916A335010126211 LIGHT BOEING737 7373H4 1384600NM AFT SVC DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20031014001482003101400148 2003 10 14 SWAA032059 420030911A2565 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031014001662003101400166NM 2003 10 14 SWAA032088 120030918A3350610478 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20031014001682003101400168NM 2003 10 14 SWAA032086 120030918A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, RBL 67, WL 206. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20031014001702003101400170NM 2003 10 14 SWAA032084 120030918A53306552988 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED, BS 942, STRINGER 24L. REPAIRED SKIN PER MM. 2L72 4F A16WE 20040106000962004010600096NM 2004 1 6 PCAA0312151 120031217A5210 ROLLER DHAV DHC8 DHC8102 2809003NM PAX DOOR DIRTY A PCAAK NONE O OTHER NRNOT REPORTED 1 EA13828EX 392 FLIGHT 3972, CLEVELAND, MAIN PASSENGER DOOR WAS VERY DIFFICULT TO OPEN REPORTED THE FLIGHT ATTENDANT. BLEEDS WERE OFF. ASSISTANCE WAS NEEDED TO GET THE DOOR OPEN. MAINTENANCE CLEANED AND LUBED DIRTY AND STICKING TRACK ROLLERS. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040106001132004010600113WP 2004 1 6 0302179885 120031212A5315 FLOORBEAM DOUG DC9 DC951 3022051WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 1167 LBL 50. REPAIRED PER EA 98-197346. 2L72 4F RTA6WE 20040106001182004010600118CE 2004 1 6 DXTA200300200 120031215A4960651586819 CONTROL PANEL RAYTHNDH125 HAWKER800XP 7150012CE COCKPIT DEFECTIVE E DXTAO OTHER BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TXTAXI/GRND HDL 1 GL07805QS2171 258505 TEN MINUTES AFTER STARTING APU, SMOKE, SPARKS, AND FLAME CAME OUT OF APU PANEL. IT STOPPED AFTER APU SHUTDOWN AND POWER WAS SHUT OFF, NO EXTINGUISHER WAS USED. INSPECTED AREA AND FOUND THE APU CONTROL PANEL BURNT. REPLACED WITH NEW PANEL IAW PATS INC HAWKER 800XP GTCP36-150W MM CHAPTER 49-11-00, OPERATIONAL CHECKED SATISFACTORY. 2L72 4F RTA3EU 20040106001382004010600138EA 2004 1 6 COMA0360556 120031215A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01821CA 7420 FLIGHT 5739 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040106001412004010600141EA 2004 1 6 COMA0360560 120031217A2421 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 ENGINE MALFUNCTIONED A COMAC ABORTED TAKEOFF JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01868CA 7427 FLIGHT 5044 NR 2 IDG CAUTION AND NR 2 GENERATOR CAUTION, T/O ABORTED. DEFERRED MAINT ON NR 2 IDG PER MEL. 2L72 4F RTA21EA 20031231001342003123100134NM 2003 12 31 AWXA200301609 120031227A5270 PROXIMITY SENSOR BOEING757 7572S7 1384962NM L4 DOOR DIRTY A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28903AW 23323 ON TAKEOFF ROLL AT PHX EN ROUTE FOR FLL DOOR WARNING SYSTEM INDICATED THE L-4 DOOR WAS OPEN, REJECTED TAKEOFF AT 100 KTS. MAINTENANCE CLEANED AND LUBRICATED TARGETS AND PROXIMITY SENSORS, DOOR WARNING SYSTEM OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040105000102004010500010NM 2004 1 5 DL73S031002 120031108A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312DL 23084 THE FUSELAGE SKIN WAS FOUND WITH A 2.5 INCH CRACK JUST BELOW STRINGER 18R AT FS 750. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385880-14, REV A. 2L72 4F RTA16WE 20040105000982004010500098WP 2004 1 5 DHL2003802550 120031125A57203645611U BRACKET DOUG DC8 DC873 302199CWP WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040105001062004010500106WP 2004 1 5 DHL2003802542 120031124A5311 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 FWD ACCY COMPT FRAME CRACKED 1.000, STA 55.000, L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. TRIMMED OUT DAMAGED FRAME IAW SRM 53-2-0 FIG 2. FABRICATED FRAME SEGMENT AND SPLICE ANGLE (02 EA) IAW SRM 53-2-0 FIG 2. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 1, 13, 17 SRM 51-1-4 PG 1-3. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT (WITH NEW FASTENERS) AND SPLICE ANGLES IAW SRM 53-2-0 FIG 2, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040105001132004010500113WP 2004 1 5 DHL2003802551 120031117A53203758498U2 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 1.000, STA 1280.000 L-35R. REMOVED CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW HI-LOKS IAW SRM 51-1-20D PG 21-9. 2L74 4F RT4A25 20040105001562004010500156CE 2004 1 5 AMWA105 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 128 WAS FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040105001682004010500168CE 2004 1 5 AMWA93 120031212A53141149800239 KEELBEAM BEECH 1900 1900D 1154162CE FUSELAGE WORN A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 DURING A DETAIL INSPECTION, THE FORWARD LEFT INBOARD LOWER KEEL WAS WORN AT THE GRAVEL FENDER ATTACH BRACKET. 2L72 4T RTA24CE 20040106000492004010600049SO 2004 1 6 C2XA03BT118 120031216A5250 LOCK EMB 135 EMB135LR 3260305SO COCKPIT DOOR MALFUNCTIONED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW2717521 145378 CREW REPORTED, DEADBOLT LOCK FOR COCKPIT DOOR JAMMED IN FLIGHT, DIVERTED AIRCRAFT AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTED AND OPS CHECK DEADBOLT LOCK IAW EMB135/145 VCMM 52-51-11, NO DEFECTS FOUND/ COULD NOT DUPLICATE PROBLEM. NOTE: AIRCRAFT TEST FLOWN, TESTED DOOR AND LOCK NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040106001232004010600123WP 2004 1 6 DXTA200300203 220031215A7200 ENGINE CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP LEFT FLAMED OUT E DXTAK NONE X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 GL07710QS 6507100 P102268 ON ENGINE START LEFT ENGINE FLAMED OUT AT IDLE SPEED. PERFORMED ENGINE INSPECTION FOR ENGINE FLAME OUT ON START, SUMPED WING TANKS IAW CESSNA 650 MM CHAPTER 12-10-10, INSPECTED ENGINE FUEL FILTER. CHECKED DEEC FOR FAULTS AND RUN ENGINE TO POWER IAW TFE731 MM CHAPTER 72-00-00, 73-21-02, ALL ENGINE PARAMETERS CHECKED GOOD. 2L72 4F4 F A9NM E6WE 20040106001272004010600127NM 2004 1 6 DHL2003742534 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSELAGE SKIN TWO LIGHT GAUGES STA 670 BETWEEN STR 5 R TO STR 6 R. CLEANED GAUGES AT BS 670 STR 5 R TO 6 R MATERIAL LOSS 0.010 FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-3 FIG (1). CUT OUT DAMAGED AREA DIM APPROX 4 BY 1 INCH IAW B-727 SRM 53-30-2 FIG (1) IAW B-727 SRM 53-30-2. PART MADE IAW B-727 SRM 53-30-3 FIG (1) AND 53-30-2 FIG (2). PART AND BARE METAL TREATED WITH ALODINED AND PRIMER IAW B-727 SRM 51-10-2. FAB AND INSTALLED COUNTERSINK WASHER REPAIR AND DOUBLER AT BS 670 STR 5R TO 6R IAW B-727 SRM 53-30-3 FIG (1) AND 51-30-8. 2L73 4F A3WE 20040106001342004010600134NM 2004 1 6 03FDEA02215 120031219A5753 RIB DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LEFT WING OUTBOARD FLAP NOSE RIB ISLAND STOP BARREL NUT BORE CRACKED. COMPLIED WITH FEDEX EA 1-5750-75228, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBD FLAP SECONDARY UP STOP REPAIR. 2L73 4F RTA22WE 20040106001822004010600182NM 2004 1 6 SWAA032684 120031209A531065478509 WINDOW FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 CYXX - DURING SPECIAL VISIT, FOUND CRACK INDICATION AT WINDOWS 28 AND 29, BS 777 AND BS 787. REPAIRED CRACK PER ERO. (M) 2L72 4F RTA16WE 20040106001852004010600185NM 2004 1 6 SWAA032696 120031209A3233273A2101 ACTUATOR BOEING737 7377H4 1384404NM RT MLG MALFUNCTIONED A SWAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW29708SW 27842 IND - FLT 2770 - ON LANDING, RIGHT GEAR RED LIGHT ILLUMINATED WITH NO GREEN LIGHT AND GEAR WARNING HORN. CYCLED GEAR DID THE SAME, ON GO AROUND GEAR CAME DOWN, COMPLETED CHECKLIST AND LANDED. REMOVED AND REPLACED RIGHT GEAR ACTUATOR PER MM. (M) 2L72 4F RTA16WE 20040106001872004010600187NM 2004 1 6 AALA20031222 120031104A3350S283T0143 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21391AA 27451 LAX - DURING OVERNIGHT MAINTENANCE, FOUND SEAT PATHWAY AND AISLE EMERGENCY LIGHTS BETWEEN ROWS 2H THROUGH 6H INOPERATIVE. REPLACED SEAT PATHWAY AND AISLE EMERGENCY LIGHT BATTERY PACK AT M730. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040106001912004010600191NM 2004 1 6 AALA20031227 120031106A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHT AT SEATS 27AB INOPERATIVE. REPAIRED BROKEN CONNECTOR AT SEATS 27AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040106001972004010600197WP 2004 1 6 GTIA030983 120031113A57535935915201 BAR DOUG DC9 DC981 3022081WP T/E FLAP CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND LEFT WING FLEX JOINT HAS CORROSION AT UPPER LUG, AND LOWER BAR. REMOVED LEFT FLEX JOINT BAR ASSEMBLY. INSTALLED SERVICEABLE LEFT FLEX JOINT BAR ASSEMBLY. (M) 2L72 4F A6WE 20040106002002004010600200WP 2004 1 6 GTIA030980 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND FLOOR PANEL STATION 148-160 EDGES SEPARATING. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040106002102004010600210WP 2004 1 6 GTIA030985 120031113A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN CENTER FLOOR PANEL STATION 946-1003 MISSING EDGE FILLER/DELAMINATED UPPER SURFACE TORN OFF. FABRICATED NEW CABIN CENTER FLOOR PANEL. (M) 2L72 4F A6WE 20040106002212004010600221NM 2004 1 6 SWAA032683 120031208A27616544851 ACTUATOR BOEING737 7373H4 1384600NM LT SPOILER BROKEN A SWAAK NONE E VIBRATION/BUFFET LDLANDING 1 SW29323SW 23344 TPA - FLT 1817 - ON LANDING FELT VIBRATION COMING FROM LEFT WHEEL WELL AREA. REMOVED AND REPLACED SPOILER ACTUATOR AND SPOILER PANEL PER MM. (M) 2L72 4F RTA16WE 20040105001102004010500110WP 2004 1 5 DHL2003802538 120031125A5712 FRAME DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING L/E LOWER FORMER CRACKED, STA XFS 423.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 21. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040105001292004010500129NM 2004 1 5 SWAA032769 120031218A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND AFT PAX CABIN CREASE BEAM WEB CORRODED. REPAIRED BEAM PER SRM. 2L72 4F RTA16WE 20040105001542004010500154CE 2004 1 5 AMWA99 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED D-STRUCTURAL INSPECTION, SEVEN FASTENERS AT RWS 125-131 WERE FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040105001712004010500171CE 2004 1 5 AMWA102 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENERS AT LWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040106000332004010600033WP 2004 1 6 DHL2003802562 120031124A53204751820 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 702.875 LBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 702.875 LBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201843 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000532004010600053NM 2004 1 6 AWXA200301559 120031217A3350BR964411 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28915AW 22209 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040106000582004010600058NM 2004 1 6 AWXA200301564 120031209A5315D5347218920200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1219, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM AT FR 68, Y1219, Z240; FABRICATED A NEW REPLACEMENT FLOOR BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20040106000632004010600063 2004 1 6 SWIA200312690 420031213A2297 WIRE EMB 120 EMB120ER 3260203SO AUTOPILOT SYS DAMAGED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM0757734 120199 A/P FAILED DURING FLIGHT. A/P FAIL ON MAP AND MASTER WARNING. FOLLOWED QRH. A/P WOULD NOT TRANSFER. REPAIRED WIRE ON CAPTAIN'S TRANSFER SWITCH IAW 22-10-11. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040106000642004010600064SO 2004 1 6 SWIA200312691 120031212A32331959500007 ACTUATOR EMB 120 EMB120ER 3260203SO RT MLG FAILED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM0715732 120195 RIGHT LANDING GEAR WOULD NOT RETRACT AFTER T/O. BOTH A & B DISAGREEMENT LIGHTS REMAINED ILLUMINATED. REMOVED AND INSTALLED SERVICEABLE MLG ACTUATOR FOR RIGHT MLG PER MM 32-32-10 S/N OFF: 287. INSTALLED SERVICEABLE RELAY AT K0205 POSITION AS REQUIRED. REMOVED AND REPLACED SERVICEABLE WOW PROX SENSOR WIRING HARNESS FOR RIGHT MLG. OPS CHECK GOOD. 2L72 4T RTA31SO 20040106002322004010600232WP 2004 1 6 GTIA031032 120031101A5310 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND MID CARGO DOOR LOWER JAMB HAS CORROSION FS 674-693. REMOVED JAMB BEAM. LOCATED AND DRILLED JAMB BEAM. INSTALLED MID PIT JAMB BEAM. (M) 2L72 4F RTA6WE 20040108000602004010800060EA 2004 1 8 WVE2003F00018 120030928A5320 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09611QX 10041 LEFT INTERCOSTAL PN MM670-36511-001 FS 1069.75 TO FS 1088.20, STRINGER 10L, WL 120 AND BETWEEN LBL 34 TO 41 IS CRACKED 1.5 INCH LONG. POSSIBLE STRESS RELIEF CRACK. REMOVE AND REPLACE INTERCOSTAL PN MM670-36511-001 IAW CRJ 700 SRM. (EA09200301583) 2L72 4F RTA21EA 20040108000642004010800064 2004 1 8 EHH2003F00000 420031007A25624520130 BATTERY PACK BEECH 36 A36 1151604CE CONT O550 IO550* SO ELT CRACKED B EHHRO OTHER O OTHER NRNOT REPORTED 1 EA17798JB538 6760362551 E3468 TWO OCCURENCES WITHIN A WEEK. TWO ELT-110-4 WITH LEAKING BATTERY PACKS THAT ALSO CRACKED CASE OF BATTERY PACK. LISTED THE SERIAL NUMBERS OF BOTH ELT. ELT 67603 HAD AN EXPIRATION DATE OF 8/03 AND ELT 62551 HAD AN EXPIRATION DATE OF 4/04. 1L71 3O3 O 3A15 E3SO 20040108000692004010800069EA 2004 1 8 IKR2003F00000 220031016A853071699 INTAKE PIPER PA32 PA32260 7103206SO LYC O540 O540E4B5 41532EA NR 1 WORN D IKRRK NONE O OTHER ININSP/MAINT 1 GL15998MM 306 321035 L1850940 AT ANNUAL INSPECTION, FOUND NR 1 INTAKE TUBE PN 71699 AT NR 1 INTAKE LOCATION EXCESSIVELY LOOSE, MOVEMENT, IN AND OUT, AND SIDEWAYS. MASSIVE AIR LEAKAGE INTO INDUCTION SYSTEM. PN 71699 IS SWEDGED (AIRTIGHT) INTO SUMP ASSY. PN LW-13901 AT 6 EA LOCATIONS. ENGINE WAS OVERHAULED 306 HOURS AGO. 1L71 3O3 O A3SO E295 20040108000732004010800073NE 2004 1 8 UO22003F00005 220031013A727030607424 DUCT AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE NR 1 ENGINE CRACKED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19377SC3101 66 P112313 NR 1 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS. 2L73 4F4 FRTA46EU E1NM 20040108000742004010800074NE 2004 1 8 UO22003F00006 220031013A727030607424 DUCT AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE NR 3 ENGINE CRACKED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19377SC3101 66 P112311 NR 3 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.(K) 2L73 4F4 FRTA46EU E1NM 20040106000692004010600069SO 2004 1 6 SWIA200312696 120031215A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07560SW 120334 EMERGENCY LIGHTS - FLOOR LIGHTING INOP (IN FRONT OF GALLEY). RELAMPED AND SECURED FLOOR LIGHTING EMERGENCY IN FRONT OF GALLEY. OPS TEST GOOD. 2L72 4T RTA31SO 20040106002042004010600204WP 2004 1 6 GTIA030991 120031119A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND CO-PILOTS FLOOR PANEL, HAS CORROSION, NO NON-SKID, RUBBER STRIPS DELAMINATED, PLASTIC BARRIER BROKEN, CONE SEAL MISSING, AND PANEL BENT AND DENTED. FABRICATED PANEL. (M) 2L72 4F RTA6WE 20040106002062004010600206WP 2004 1 6 GTIA030989 120031119A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND FLOOR PANEL STATION 1250-1309 HAT CHANNEL DELAMINATED. REBONDED HAT CHANNEL. (M) 2L72 4F RTA6WE 20040108000572004010800057CE 2004 1 8 F2P2003F00001 120030925A3240510010769 LINE CESSNA414 414 2075908CE CONT O520 TSIO520* 17040SO RT BRAKE CORRODED E F2PAO OTHER O OTHER NRNOT REPORTED 1 SO17414AW5322 4140520 PILOT REPORTED LOSS OF RIGHT SIDE BRAKE PRESSURE UPON LANDING. FOUND RT BRAKE MASTER CYLINDER EMPTY. FOUND HYDRAULIC LEAK UNDER COPILOT SIDE FLOOR. COURSE OF LEAK DUE TO CORRODED ALUMINUM BRAKE LINE, BRAKE LINE CORROSION CAUSED BY SCATT DUCT STEEL SUPPORT WIRE IN CONTACT WITH BRAKE LINE. FOUND SIMILARLY CORRODED OXYGEN LINES IN HEADLINER ON SAME AIRCRAFT LAST YEAR. SAME CAUSE. AIR DUCTS IN CONTACT WITH ALUMINUM LINES. CAREFUL INSPECTION AND REPLACEMENT OF ALUMINUM LINES THAT ARE IN CONTACT WITH SCATT TYPE AIR DUCTS. 1L72 3O3 ORTA7CE E8CE 20040108000882004010800088EU 2004 1 8 KBM2003F00038 120031002A7931704A47270101 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE OIL PRESSURE ERRATIC E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP1937SH 2300 OIL PRESSURE CABLE ERRATIC IN FLIGHT. REMOVED AND REPLACED CLUSTER GAUGE.(K) 1G71 3U3 UNCH9EU E19EU 20040108000902004010800090 2004 1 8 KBM2003F00040 420031004A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE VHF SYSTEM NOISY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH1222 2957 VHF RADIO, AFTER .5 HOUR OF FLYING, MAKES CONTINUOUS DESQUELCHING NOISE. NOTE: DID NOT FIX PROBLEM (REMOVED AND REPLACED REPAIRED VHF RADIO). 1G71 3U3 UNCH9EU E19EU 20040108000972004010800097 2004 1 8 KBM2003F00047 420031006A3422200DC GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT PRECESSES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 DIRECTIONAL GYRO PRECESSES AND SPINS. INSTALLED NEW DIRECTIONAL GYRO. 1G71 3U3 U H9EU E19EU 20040108001042004010800104 2004 1 8 KBM2003F00054 420031010A34225050031904 GYRO SNIAS 350 AS350B1 8680811EU COCKPIT PRECESSES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 7465 2009 DIRECTIONAL GYRO PRECESSES TOO FAR IN FLIGHT. INSTALLED SERVICEABLE DIRECTIONAL GYRO. 1G71 3U H9EU 20040108001122004010800112EU 2004 1 8 KBM2003F00062 120031017A6730AC67244 SERVO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH1629 2957 BINDING IN LT CYCLIC CONTROL. SUSPECTED LT SERVO BAD. REMOVED AND REPLACED WITH OVERHAULED. 1G71 3U3 UNCH9EU E19EU 20040108001182004010800118EA 2004 1 8 Z372003F00001 220031001A74141059474 IMPULSE COUPLING BBAVIA7 7FC 2110124SW LYC O235 O235C1 41505EA MAGNETO BROKEN D Z37EO OTHER O OTHER NRNOT REPORTED 1 GL017581E 816727 7FC269 512415 PILOT REPORTED LOSS OF POWER ON TAKEOFF, RETURNED TO AIRPORT. AFTER LANDING HE AGAIN CHECKED HIS MAG DROP AND REPORTED HIS LT MAG DROP TO BE ABOUT 300 RPM. FURTHER INVESTIGATION FOUND THE ONE OF THE IMPULSE COUPLING PAWLS ON THE LT MAG HAD BROKE IN HALF AT THE PIVOT POINT. THE PIECES FELL HARMLESSLY INTO THE OIL SUMP AND WERE REMOVED. (K) 1H71 3O3 O A759 E223 20040108001192004010800119NE 2004 1 8 UO22003F00008 220031003A727030607424 DUCT AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE ENGINE CRACKED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL192425 3617 32 P112200 NR 3 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 O`CLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAN MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K) 2L73 4F4 FRTA46EU E1NM 20040108001212004010800121CE 2004 1 8 PAZ2003F00000 120031007A494099104771 RELAY CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP APU STARTER BURNED B PAZRO OTHER O OTHER NRNOT REPORTED 1 CE0372ST 6209 6500072 DURING MAINTENANCE GROUND RUN, ATTEMPTED TO START APU. APU DID NOT START. ON NEXT ATTEMPT TO START, APU DID NOT START AND START RELAY WOULD NOT DISENGAGE. BEFORE POWER COULD BE SHUT OFF BY DISCONNECTING SHIPS BATTERIES, NOTICED SMOKE COMING FROM APU J-BOX. UPON FURTHER INSPECTION, FOUND APU POWER RELAY (K114) WELDED OR MELTED IN CLOSED POSITION. THIS CAUSED AN OVERHEAT CONDITION OF RELAY CAUSING SEVERAL OTHER COMPONENTS TO BE DAMAGED WITHIN J-BOX AND ASSOCIATED WIRING. ALSO FOUND WIRES WITH DAMAGE IN THE IMMEDIATE AREA AND/OR CHANGE INTERVAL INSTITUTED TO PREVENT RELAYS FROM DETERIORATING TO THE POINT OF CAUSING THIS CONDITION.(K) 2L72 4F4 F A9NM E6WE 20040108001272004010800127GL 2004 1 8 ALG2003F00100 220031007A7230 COMPRESSOR BELL 206 206L3 1182108SW ALLSN 250C 250C30S 03013GL ENGINE MALFUNCTIONED E ALGAO OTHER E VIBRATION/BUFFET HOHOVERING 1 SW03361AL 51212 CAE895014 AT HOVER. DURING INITIAL HOVER PRIOR TO TAKE-OFF THE PILOT NOTICED A HIGH PITCH SCREECHING NOISE THAT WAS EVIDENT ONLY DURING HOVER, AT FLAT PITCH THE NOISE GOES AWAY. MAINTENANCE WAS NOTIFIED AND THE MECHANIC CHANGED THE COMPRESSOR, TURBINE AND GEARBOX ASSEMBLY AND THE AIRCRAFT WAS RETURNED TO SERVICE.(K) 1G71 3U3 U H2SW E1GL 20040108001282004010800128NE 2004 1 8 ALG2003F00101 120031012A2620M835362024M RELAY SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL FIRE EXTING FAILED E ALGAK NONE L NO TEST ININSP/MAINT 1 SW03709AL 760278 ON PRE-FLIGHT, THE FIRE EXTINGUISHER SYSTEM FAILED. MAINTENANCE WAS INFORMED AND THE MECHANIC REMOVED AND REPLACED THE K2 RELAY IN THE NR 1 RELAY IN THE OVERHEAD PANEL IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE.(K) 1G72 3U3 U H1NE E1GL 20040108001302004010800130NE 2004 1 8 Z1R2003F00000 120031020A14307615009143041 SCREW SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE M/R BLADE TIPCAPCORRODED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11761AF903 760524 YELLOW BLADE(COLOR CODE) TIP CAP M/R SCREWS. FORWARD PAR OF ALL SCREWS HAVE A .002 INCH GAP BETWEEN THE HEAD OF SCREW AND MATING SURFACE. (AS MEASURED) SCREW IS NOT CONTACTING COMPLETELY AROUND THE HEAD OF SCREW. CORROSION IS APPEARING AT THE FIRST THREE THREADS OF ALL SCREWS. THE LARGE SCREWS, INSTALLATION TORQUE-100 IN/LBS. BREAKING TORQUE RANGED FROM 200 IN/LBS TO 110 IN/LBS. 1G72 3U3 UNCH1NE E00054EN 20040108001372004010800137SW 2004 1 8 KBM2003F00069 120031019A28977G547 CIRCUIT BREAKER BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUEL PUMP MALFUNCTIONED E KBMAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP19667JM499 3444 FORWARD FUEL PUMP CIRCUIT BREAKER DOES NOT ILLUMINATE MASTER CAUTION LIGHT WHEN PULLED. REPLACED.(K) 1G71 3U3 U H2SW E4CE 20040108001382004010800138SW 2004 1 8 KBM2003F00070 120031019A772212444412 INDICATOR BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TOT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 TOT GAUGE LIGHT INOPERATIVE. INSTALLED SERVIEABLE GAUGE.(K) 1G71 3U3 U H2SW E4CE 20040108001482004010800148EU 2004 1 8 PG9A118869 120030918A2821174364001 FUEL FILTER UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE ENGINE FAILED E PG9AO OTHER X ENGINE FLAMEOUT NRNOT REPORTED 1 WP19135PH171 3695 FUEL FILTER FAILED AND CAUSED ENGINE TO FLAMED OUT, (K) 1G72 3U3 U H9EU E00054EN 20040108001552004010800155NE 2004 1 8 Z1R2003F00005 120031028A1430SS530SL4G08 SCREW SKRSKYS76 S76C 8143008NE BLADE TIP CAP CRACKED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11761AF481 A0862703 760524 ONE (1) SREW CRACKED NR 1 BOTTOM POSITION LENDING EDGE. 1G72 3U NCH1NE 20040108001572004010800157NE 2004 1 8 Z1R2003F00007 120031028A1430SS5305L4G08 SCREW SKRSKYS76 S76C 8143008NE BLADE TIP CAP CRACKED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF459 760523 ONE (1) SCREW CRACKED NR 1 BOTTOM POSITION FROM LEADING EDGES. 1G72 3U NCH1NE 20040109000022004010900002NE 2004 1 9 J0F2003F00000 220031020A8500126299 CASE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE LT MAG MOUNT CRACKED E J0FAO OTHER K FLUID LOSS NRNOT REPORTED 1 AL05471PM7803 1060 1366 P226597 OWNER/OPERATOR REPORTED OIL LEAKING FROM REAR OF ENGINE. AFTER THOROUGH CLEANING OF SUSPECTED OIL LEAK AREA, AC ENGINE WAS RUN-UP AND OIL WAS FOUND TO BE LEAKING FROM LT MAGNETO MOUNTING PAD AREA AND DRIPPING OFF OF AFT MAGNETO MOUNTING BOLTS. UPON REMOVAL OF THE LT MAGNETO, A CRACK WAS DISCOVERED IN THE LT MAGNETO MOUNTING PAD. CRACK MEASURED 3.25 INCHES AND RAN DIAGONALLY FROM INSIDE EDGE OF FORWARD MAGNETO MOUNTING BOLT HOLE THROUGH IB AFT MAGNETO MOUNTING BOLT HOLE. SUSPECT CRACK IS AGE RELATED OR DUE TO WARPED MOUNT PAD. LT MAGNETO HAD NOT BEEN REMOVED FROM ENGINE SINCE ENGINE OH AND MAGNETO MOUNTING BOLTS APPEARED TO BE PROPERLY TORQUED.(K) 1H71 3R3 R A806 5E1 20040109000122004010900012 2004 1 9 HYI2003F00018 420031031A6122DCF290D7CT3 GOVERNOR CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO LT ENG PROP UNSERVICEABLE E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01771EA 1607 402C0046 823465 CREW REPORTED, DURING CRUISE LEVEL FLIGHT, 658 ENGINE BEGAN TO SURGE +/- 400 RPM. AFTER REDUCING POWER, AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC FOUND 6 FT PROP GOVERNOR FAILED. MECHANIC CHANGED GOVERNOR AND RELEASED AIRCRAFT BACK TO SERVICE.(K) 1L72 3O3 O A7CE E8CE 20040109000202004010900020NM 2004 1 9 P9R2003F00000 120031108A33501317 LAMP BOEING757 757236 1384971NM RROYCERB211 RB211* 54555NE EMERGENCY LIGHT BURNED OUT A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11958PG 24118 L1 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED LAMPS IAW BMM 33-00. (K) 2L72 4F4 FRTA2NM A12EU 20040109000292004010900029NE 2004 1 9 MEX2003492 220031015A7200 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE LEFT MALFUNCTIONED W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23803ML 49726 AIRCRAFT RETURNED TO PLATFORM, AFTER LT ENGINE START, IT HAD HIGH TEMPERATURE INDICATIONS (447 WITHOUT BLEED AND 491 WITH BLEEDS). ENGINE WAS TESTED AND IT HAD 450 WITHOUT BLEED AND 460 WITH BLEEDS BEING WITHIN LIMITS IAW MM 72-00-00. DURING OVERNIGHT SERVICE, LT ENGINE WAS RUN UP AND IDLE TEMPERATURE WAS WITHIN OPERATION LIMITS IAW MM 71-00-01.(K) 2L72 4F4 FRTA6WE E2EA 20040109000322004010900032 2004 1 9 MEX2003468 420031006A34326223255001 RECEIVER DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE VOR SYSTEM FAILED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW23751RA7233 49779 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING. VOR FLAGS ON RDMI INSIGHT IN BOTH INSTRUMENTS. TX RX VOR/ILS WAS REPLACED BUT FAIL CONTINUED. RETURN TO SERVICE TEST WAS PERFORMED SHOWING 375 FAILURE CODE (VOR/DFGC FAILURE). AIRCRAFT WAS SENT TO THE HANGAR WHERE BOTH TX RX VOR/ILS WERE REPLACED IAW MM 34-32-02.(K) 2L72 4F4 FRTA6WE E2EA 20040109000352004010900035WP 2004 1 9 CHI2003F00001 120030805A6210369D21100516A BLADE HUGHES369 369 4470702WP MAIN ROTOR CRACKED B CHIRK NONE O OTHER ININSP/MAINT 1 NM09 3340 WHILE PERFORMING OFF AIRCRAFT INSPECTION OF MAIN ROTOR BLADE UTILIZING EDDY CURRENT METHOLOGY. DISCOVERED ONE CRACK EMANATING FROM FIRST LIGHTING HOLE AT APPROX. STA 36.5 IN (C) CHANNEL. SECTIONED BLADE TO VERIFY EDDY CURRENT FINDINGS. CRACK EXTENDS FROM ID OF LIGHTING HOLE UP TO START OF BEND RADIUS. AC PARKED STATIC WITHOUT OR IMPROPER BLADE TIE DOWNS DURING GUSTING WINDS OR AROUND OTHER OPERATING A/C. EXCESSIVE TENSION ON BLADE TIE DOWNS. MANUFACTURE DEFECT OR PRACTICES. PERFORMING EDDY CURRENT INSP AS TIME ALLOWS WHEN AC ARE IN FACILITY FOR EXTENDED TIME PERIODS. (CHI2741) 1G71 3U H3WE 20040109000392004010900039NM 2004 1 9 UIEA200300061 120031107A2612 FIRE LOOP BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 2 ENGINE MALFUNCTIONED A UIEAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 EA15509MC 21221 530276 DURING DESCENT INTO ANC, NR 2 ENGINE HAD A FIRE WARNING PASSING THROUGH 16000 FT AT IDLE POWER. NR ENGINE (A) LOOP IS PLACARDED INOPERATIVE. PERFORMED EMERGENCY FIRE CHECK LIST AND SHUTDOWN ENGINE. FIRE HANDLE WAS PULLED AT 1946Z, TT EDP IN DEPRESSURIZE MODE WAS 19 MIN. DUCT PRESSURE DROPPED TO 10 PSI AND NO ADP RUN LIGHT. EVENTUALLY DUCT PRESSURE CAME BACK TO NORMAL. NACELLE TEMPERATURE WAS NORMAL. FOUND PYLON DETECTOR FORWARD SECTION LOOSE, RETORQUED FASTENERS IAW MM 70-51-01, GROUND OPS CHECK 2A, B LOOPS OK IAW MM 26-11-00.(K) 2L74 4F4 F A20WE E23EA 20040109000492004010900049EA 2004 1 9 R33A03015 120031010A2910601752381 LINE CNDAIRCL600 CL6002B16 1900305EA HYDRAULIC SYS BROKEN A RU3AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2187 5190 NR 1 HYDRAULIC SYSTEM FAILED IN FILGHT WITH COMPLETE LOSS OF FLUID WITHIN THAT SYSTEM. FOUND HYDRAULIC LINE SNAPPED OFF. REPLACED HYDRAULIC LINE. ALSO, REPLACED HYDRAULIC PUMP AND FILTERS DUE TO LOSS OF FLUID. (M) 2L72 4F RTA21EA 20040109000622004010900062EU 2004 1 9 2004F00005 120031102A3233 ACTUATOR AMD FALC50FALCON50MYST2730106EU MLG MALFUNCTIONED A EHBAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA25978W 49 CREW EXTENDED GEAR, GOT 2 GREEN DOWN AND LOCKED IND LIGHTS. LT DOWN/LOCKED LANDING LIGHT DID NOT ILLUM. PULLED TEH D-RING TO PERFORM A MANUAL MAIN GEAR RELEASE AND LT LIGHT ILLUM APPROX 10 MINUTES LATER, HAD ALL OF GEAR DOWN/LOCKED WITH 3 GREEN LIGHTS. AC LANDED WITHOUT INCIDENT. VISUAL INSP OF ALL OF LANDING GEAR WAS PERFORMED AFTER LANDING TO VERIFY THAT GEAR WAS DOWN/LOCKED. FOLLOWING COMPONENTS WERE REMOVED AND REPLACED, LT MAIN RETRACT ACTUATOR, P/N C23925-1104 S/N U42, LANDING GEAR HANDLE RELAY P/N ON CP2-5E2B, LT MAIN GEAR EMERGENCY EXTENSION D RING CABLE P/N ON F50B796001110A4 S/N 2781. PERFORMED FUNCTION AND OPS CHECK OF LANDING GEAR, ALL CHECKS WERE OK. A/C WAS RETURNED TO SERVICE. (M) 2L73 4F A46EU 20040109000672004010900067WP 2004 1 9 GTIA031037 120031204A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT CROSSED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND LT FORWARD LOWER AIRSTAIR EMERGENCY LIGHT INOPERATIVE, BAD SOCKET. TROUBLESHOT SYSTEM FOUND WIRES CROSSED AT POWER SUPPLY. REWIRED POWER SUPPLY AND LIGHT SOCKETS. (M) 2L72 4F RTA6WE 20040112000032004011200003WP 2004 1 12 AALA20031228 120031106A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21413AA 49324 DURING OVERNIGHT MAINTENANCE, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 23-26 INOPERATIVE. REPLACED BATTERY FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23-26. GROUND SYSTEM CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112000212004011200021WP 2004 1 12 GTIA031021 120031126A5310 SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FRAME SUPPORT CRACKED STATION 218 STRINGER 18L-17L, HIDDEN DAMAGE. REMOVED CRACKED SHEAR CLIP. FABRICATED SHEAR CLIP. INSTALLED FRAME, SHEAR CLIP. (M) 2L72 4F A6WE 20040112000222004011200022WP 2004 1 12 GTIA031019 120031202A5310 SHEAR TIE DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND MID PIT BILGE, SHEAR TIE CORRODED AT STATION 598. CUT OUT SHEAR TIE. FABRICATED NEW SHEAR TIE. SUB CHART FOR 2014-T6 IS 7075-T6. INSTALLED NEW SHEAR TIE. (M) 2L72 4F A6WE 20040114000512004011400051NM 2004 1 14 DL757030966 120031029A3340233N321422 CONTROL PANEL BOEING757 757232 1384965NM COCKPIT OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27653DL 24393 SMOKE OBSERVED DURING FINAL APPROACH, AFTER NOSE GEAR LANDING LIGHT, TAXI LIGHT AND TURNOFF LIGHT WERE ILLUM. SMOKE OBSERVED AT LWR PORTION OF O/H PNL JUST BELOW LIGHT SWITCH. FOUND WIRE CONNECTORS AT TURNOFF LIGHT SWITCHES S1 AND S2 OVERHEATED. CHECKED AND REPLACED RUNWAY TURNOFF LIGHT BULBS. INSPECTED WIRING AT NOSE GEAR ALL NORMAL. REPLACED LIGHT CONTROL PNL. OPERATED LIGHT FOR 30 MINS, ALL NORMAL. 2L72 4F RTA2NM 20040114000782004011400078NM 2004 1 14 DL76L031020 120031116A3350 LIGHT BOEING767 767332 1382001NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27182DN 25987 SEAT 6 F/G EMERGENCY ESCAPE PATH MARKING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY AT 6F/G, OPS CHECKS GOOD. 2L72 4F RTA1NM 20040114000902004011400090NM 2004 1 14 DL75K031031 120031119A3350BPS73 POWER SUPPLY BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27685DA 27588 EMERGENCY EXIT SIGNS INOP AT R2 DOOR OVERHEAD & CENTER AISLE OVERHEAD. REMOVED AND REPLACED POWER SUPPLY RACK & BATTERY AT R2 DOOR PER M/M. OPS CHECK GOOD. 2L72 4F RTA2NM 20040114000962004011400096NM 2004 1 14 DL73S031035 120031117A5330654580034 SKIN BOEING737 737232 1384475NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED NEAR FS 178 AND STRINGER 24R. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 087582-14, REV A. 2L72 4F RTA16WE 20040114001202004011400120NM 2004 1 14 DLM88031054 120031122A5320 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27938DL 49811 CORROSION ON RIGHT CUSP WEB AT STATION Y=579. REPLACED DAMAGED SECTION OF RIGHT CUSP WEB FROM STA 560 TO STA 598 PER DELTA DRD 53-20-02D PAGE 801 DUE TO CORROSION OUT OF LIMITS AT STA 578. 2L72 4F RTA6WE 20031010000892003101000089SW 2003 10 10 BAQA089482 120030920A7922222375016101 INDICATOR BELL 222 222U 1182140SW LYC LTS101LTS101* NE OIL TEMP ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03223HX 47511 TEMPERATURE READING ERRATIC. REPLACED WITH SERVICEABLE UNIT. 9/26/03 1G72 3U3 U H9SW E5NE 20031010000932003101000093EU 2003 10 10 BAQA089260 120030922A6730SC7282 SERVO AEROSPAS365 AS365N2 8680815EU LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME2529 6417 SERVO LEAKING. EXCESSIVE PLAY AT CONTROL ARM. REPLACED WITH SERVICEABLE UNIT. 9/23/03 1G72 3U RTH10EU 20031010000952003101000095EU 2003 10 10 I05R089503 120030925A6240SVEURO4 AMPLIFIER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE MAST MOMENT IND INOPERATIVE E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05551BA1321 188 SENSOR AMPLIFIER INOPERATIVE REPLACED PART 1G72 3U3 UO H88EU E42NE 20031014000042003101400004 2003 10 14 BAQA089312 420030930A3160L316M30C1003 CDU UROCOPEC135 EC135P1 8680990EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH240 0069 TOP SEGMENTS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20031014000102003101400010NE 2003 10 14 BAQA085910 220030409A7323430121205 GOVERNOR BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117CJ 7051 GOVERNOR MALFUNCTIONED, REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H13EU E5NE 20031014000122003101400012NE 2003 10 14 BAQA089599 220030929A73130319307840 INJECTOR AGUSTAA109 A109E 0260119EU TMECA ARRIUSARRIUS2K1 NE ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037YL 11502 ENGINE FIVE STAR PROGRAM. TROUBLESHOOTING. SLOW START ENGINE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 URTH7EU E34NE 20031014000142003101400014EU 2003 10 14 BAQA089636 120030925A25203100 SEAT UROCOPEC135 EC135P1 8680990EU CABIN CRUSHED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH504 0179 NEW EC135 AIRCRAFT. SEAT IS CRUSHED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20031014000192003101400019NM 2003 10 14 UPS03541239 120030906A5330 SKIN BOEING757 75724APF 1384969NM FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01449UP 27738 INSPECTION TYPE: C1, FUSELAGE SKIN HAS LIGHTNING STRIKE AT BS 1260 BETWEEN STR 10L AND 11L. REPAIRED AREA PER ER 03-3476 DATED 09/16/03. 2L72 4F RTA2NM 20031014000282003101400028SO 2003 10 14 XGN2003F00002 220030819A85206525384 CRANKCASE BEECH 55 95C55 1152708CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAO OTHER WK INADEQUATE Q C FLUID LOSS NRNOT REPORTED 1 SW055740V 865 TE103 CRACK WAS DISCOVERED WHILE LOOKING FOR OIL LEAK DURING 100 HOUR INSPECTION. THIS HAS BEEN GOING ON FOR YEARS WITH MFG ENGINES. THEIR ATTEMPTS OF HEAVIER CRANKCASES AND 7TH STUD APPLICATIONS HAVE DOEN NOTHING TO GET RID OF THE PROBLEM. 1L72 3O3 O 3A16 E5CE 20040105000552004010500055EA 2004 1 5 SWIA200312685 120031208A2612 FIRE WARNING CNDAIRCL600 CL6002B19 1900309EA COCKPIT FALSE INDICATIONA SWIAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 NM07413SW 7102 APU FIRE WARN IN FLIGHT. COMPLIED WITH QRH. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE OR HEAT DAMAGE. REMOVED AND REPLACED THE APU FIRE BOTTLE ASSY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 897889, S/N OFF: 60810EL, P/N: 897776-01, S/N OFF: 01659. 2L72 4F RTA21EA 20040105001172004010500117WP 2004 1 5 DHL2003802553 120031204A57305611002502 SKIN DOUG DC8 DC873 302199CWP RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, STA XW 5.000 - XW 47.000. REMOVED AND REPLACED PANEL ON RIGHT WING T/E STA XW 5.000 - XW 47.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040105001252004010500125NM 2004 1 5 SWAA032764 120031217A57546546421 WEDGE BOEING737 7372H4 138448CNM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 NR 1 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM. 2L72 4F A16WE 20040105001602004010500160CE 2004 1 5 AMWA89 120031210A541211498007319 FIREWALL BEECH 1900 1900D 1154162CE LT NACELLE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07166YV UE166 FOUND LEFT ENGINE FIREWALL CRACKED. REPAIRED CRACK IN FIREWALL IN ACCORDANCE WITH SRM 54-90-01 BY INSTALLING DOUBLER. 2L72 4T RTA24CE 20040105001752004010500175NM 2004 1 5 AWXA200301619 120031207A532065C10592154 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 961, RBL 25. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 961, RBL 25; FABRICATED A T-ANGLE AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12, PG 1 & 45. 2L72 4F RTA16WE 20040106000792004010600079SO 2004 1 6 C2XA03SH505 120031218A531514532636401 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040106000802004010600080SO 2004 1 6 C2XA03SH506 120031218A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040106001062004010600106NM 2004 1 6 CALA0300714 120031218A5311 BELTFRAME BOEING737 737524 1384721NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716650 28911 INSPECTION FOUND LT BELT FRAME PUNCTURED IN TWO PLACES AT STA 847. THE DAMAGE WAS ROUTED OUT AND A BELT FRAME REPAIR WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20040106001082004010600108NM 2004 1 6 CALA0300715 120031218A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, RBL 18-42. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20040106001372004010600137EA 2004 1 6 COMA0360555 120031213A2613434419883 SWITCH CNDAIRCL600 CL6002B19 1900309EA RT WING FAULTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01982CA 7168 FLIGHT 5491 WING OVERHEAT WARNING. REPLACED THE RT WING OVERHEAT SWITCH. 2L72 4F RTA21EA 20040106001492004010600149 2004 1 6 AWXA200301565 420031217A2216654997025 TRIM MOTOR BOEING737 7373S3 1384711NM HORIZ STAB BINDING A AWXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP28312AW2121917238 24060 ON C/O, CAPTAINS EFIS IND SPEED TRIM WARNING LIGHT. A/C COULD NOT ATTAIN FL 290 IN MODE CONTROL PANEL, A/C DESCENDED & AIRSPEED DECREASED AS STAB OUT OF TRIM LIGHT ILLUM. TURNED OFF AUTOPILOT, STAB WOULD NOT TRIM IN ELECTRIC OR MANUAL MODE. LOWER ALTITUDE & SPEED TRIM SYS OPS NORM, TURNED BACK & LANDED WITHOUT EVENT. MX R & R AUTOPILOT STAB TRIM MOTOR & STAB TRIM G/B ASSY. HOR STAB TRIM CONTROL ADJUST & TEST ACCOMPLISHED. TEARDOWN OF STAB TRIM ACT FOUND WORN RINGS, SEALS, O-RINGS, UMBRELLA, BEARINGS, BRAKE PLATES & SHOES, SPRINGS, AND WIPERS. UNIT OVERHAULED IAW CMM. CONFIRMED FAILURE OF AUTOPILOT JACKSCREW SERVO MOTOR FOR NO OUTPUT SHAFT ROTATION DUE TO GEAR, PINION, & MOTOR ROTOR DAMAGED. 2L72 4F RTA16WE 20040106001582004010600158EA 2004 1 6 033536471 120031219A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27647BR 7399 DURING INSPECTION A SECTION OF EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. A BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040106001642004010600164EA 2004 1 6 03347641 120031213A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27641BR 7349 DURING INSPECTION THE FLOOR EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS FOUND TO BE BROKEN AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040106001662004010600166EA 2004 1 6 03347669 120031213A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING FROM ROW 8 FORWARD WAS FOUND INOPERATIVE. THE LIGHT STRIP WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031231000902003123100090WP 2003 12 31 GTIA030928 120031110A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSLEAGE TORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND CABIN FLOORBOARD 320-400 METAL TORN AT FASTENER HOLE, DELAMINATED AT RUB STRIPS AND HAT CHANNEL. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20031231001192003123100119NM 2003 12 31 TSAA0351031 120030115A53206554893 SPLICE BOEING737 7372T4 1384492NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 TRIMMED LEFT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PRESSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOUR DOUBLER I BEAM TIE STRAPS AND TEE STIFFENERS. ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS. INSTALLED REPAIR PARTS PER SRM 53-60-51, FIGURE 203. REPAIR COMPLETED IAW ECO 3328, PART II AND V. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040105000202004010500020 2004 1 5 DL76S031008 420031112A3460341080110 FMC BOEING767 767332 1382001NM COCKPIT ODOR A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27134DL 25123 FLT 1790 RTB WITH ODOR/SMOKE I9N COCKPIT. BY ARRIVAL AT GATE ALL EVIDENCE HAD DISSIPATED. FOUND F/O FMS CDU BLANK AND COMPLETELY INOP. REPLACED F/O CDU AND OK. NO REOCCURANCE OF SMOKE OR ODOR DURING GATE TIME, APPROX 45 MIN. 2L72 4F RTA1NM 20040105000562004010500056 2004 1 5 SWIA200312686 420031209A3418 WARN PANEL EMB 120 EMB120ER 3260203SO COCKPIT FAULTY A SWIAO OTHER P NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07581SW 120349 RIGHT STALL WARNING INOP. REMOVED AND REPLACED THE STALL WARNING PANEL ASSEMBLY. OPS CHECKS GOOD. P/N: 120-34428-505. 2L72 4T RTA31SO 20040105000832004010500083EA 2004 1 5 MASA200300493 120031215A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAK NONE O OTHER ININSP/MAINT 1 SW0747202 7202 ASH 2690 SDF-PHL. DURING PREFLIGHT THE MAIN CABIN DOOR W/N OPEN NORMALLY WITH THE HANDLE FROM THE INSIDE. MX CLEANED AND LUBED THE DOOR. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040105000922004010500092WP 2004 1 5 DHL2003802544 120031127A5310 DOOR FRAME DOUG DC8 DC873 302199CWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 FWD PASSENGER DOOR JAMB UPPER FWD CORNER INTERIM REPAIR, STA 25.000 L-9L TO L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR, SERVICE REWORK DWG SRO 8530021, DWG 5750776. REMOVED INTERIM REPAIR. TRIMMED OUT AFFECTED AREA IAW SRM 53-2-0 FIG 15, SERVICE REWORK DWG SRO 8530021, DWG 5750776. FABRICATED DOUBLER, TRIPLER, FILLER IAW SRM 53-2-0 FIG 15, SERVICE REWORK DWG SRO 8530021, DWG 7570776. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER AND TRIPLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER AND TRIPLER WITH NEW FASTENERS IAW SRM 53-2-0 FIG 15, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040105000972004010500097WP 2004 1 5 DHL2003802546 120031114A5310 DOOR FRAME DOUG DC8 DC873 302199CWP FSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 EXTERNAL FUSELAGE FWD SVC DOOR JAMB LOWER AFT CORNER CRACKED .750 STA 190.000, L20 - L21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 14, SERVICE REWORK DWG SRO8530021, DWG 5750776. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG.14, SERVICE REWORK DWG SRO8530021, DWG 5750776. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER AND TRIPLER IAW SRM 51-1-8B. INSTALLED CONICAL WASHER. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER AND TRIPLER. 2L74 4F RT4A25 20040105001272004010500127NM 2004 1 5 SWAA032766 120031218A53206976022 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND FLOOR WEB CORRODED AT BS 1016, LBL 5, WL 208. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20040106001552004010600155EU 2004 1 6 DHL2003364017 120031112A5411 SPAR AIRBUS300 A300B4203 3930306EU NR 2 PYLON CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING CLEANING OF PYLON AREA DUE TO HYD LEAKAGE FOUND POSSIBLE CORROSION BETWEEN STA 726/RIB 8 AND STA 837 RIB 12 OF PYLON NR 2. REPAIRED NR 2 PYLON LOWER SPAR PER AIRBUS DRAWING 41R54610300, REFER EADS NR 141-15082 AND LOG PAGE 358326 ITEM 1M & 2M. 2L72 4F RTA35EU 20040106001842004010600184NM 2004 1 6 SWAA032693 120031208A53206553878 SUPPORT BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 PAE - DURING SCHEDULED D-CHECK, FOUND CORROSION ON TORQUE BOX UPPER SUPPORT CHORD BS 1088 WL 250, RBL 20. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040106002202004010600220NM 2004 1 6 SWAA030282 120031209A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29608SW 27928 SAT - FLT 33 - AFT UPPER FLASH LIGHT CHARGE LIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY PER MM. (M) 2L72 4F RTA16WE 20040106002252004010600225WP 2004 1 6 GTIA031031 120031102A5310 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - AFT CARGO LOWER DOOR JAMB HAS CORROSION FS 1155-1231. REMOVED JAMB BEAM FS 1117-1250. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED AFT PIT JAMB BEAM. (M) 2L72 4F RTA6WE 20040105001162004010500116WP 2004 1 5 DHL2003802526 120031118A5330 SKIN DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 EXTERNAL FUSELAGE CRACKED 0.375, STA1756.000, L-16 - L17R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 PG 99-100 FIG 7, SHEET 1. CLEANED, TREATED AND PRIMED REPAIRED AREA IAW SRM 51-1-8B. FABRICATED FILLER, FINGER DOUBLER, DOUBLER IAW SRM 53-2-1 PG 99-100 FIG 7. CLEANED, TREATED, PRIMED FILLER AND FINGER DOUBLER & DOUBLER IAW SRM 51-1-8B. INSTALLED CONICAL WASHERS IAW SRM 51-1-26 FIG 1. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, FINGER DOUBLER AND DOUBLER WITH NEW FASTENERS IAW SRM 53-2-1 PG 99-100 FIG 7, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040105001212004010500121WP 2004 1 5 DHL2003802554 120031130A5754 SKIN DOUG DC8 DC873 302199CWP L/E SLAT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 ELONGATED HOLES IN RT WING EXTENDED L/E INBD VANE FORWARD PLATING AROUND STA XILD 7095 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AND EXTERNAL REPAIR DOUBLER (7075-T6AL 0.071), A FILLER (7075-T6AL 0.063), AN INTERNAL DOUBLER (7075-T6AL 0.050). CLEANED, TREATED AND PRIMED THE EXTERNAL REPAIR DOUBLER INTERIOR SURFACE, THE FILLER AND INTERNAL DOUBLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE EXTERNAL REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER ON RT WING EXTENDED L/E INBD VANE FWD PLATING (AROUND XILD 7095) USING NEW FASTENERS. 2L74 4F RT4A25 20040106000352004010600035WP 2004 1 6 DHL2003802556 120031130A5754 SKIN DOUG DC8 DC873 302199CWP L/E VANE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING EXTENDED L/E INBD VANE FWD OUTER PLATING ELONGATED HOLES AROUND STA XS 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-3 AND DWG U38-R03. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA , FABRICATED AN EXTERNAL REPAIR DOUBLER, A FILLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED THE EXTERNAL REPAIR DOUBLER INTERIOR SURFACE, FILLER AND INTERNAL DOUBLER. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS ON EXTENDED L/E INBD VANE (RT WING STA XS 247.000) USING NEW FASTENERS IAW ED EDU38-3 AND DWG U38-R03, SRM 51-1-21 PG 1 AND SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040106000472004010600047SO 2004 1 6 C2XA03BT117 120031216A33501317 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717928 145007 DURING 2A INSPECTION MAINTENANCE FOUND THE CABIN ENTRANCE DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LAMP IAW EMB145 AMM 33-50-06. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040106000512004010600051NM 2004 1 6 DHL2003742526 120031125A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 5 SEAT TRACK AT BS 850 IS DAMAGED. REMOVED AND REPLACED NR 5 SEAT TRACK AT BS 850 IAW B-727 SRM 53-10-5 FIG 7 AND 51-30-2. NOTE N/R 60205 REPLACES SEAT TRACK FROM BS 760 TO 850. 2L73 4F A3WE 20040106000912004010600091SO 2004 1 6 C2XA03TY213 120031218A531514522226003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS DURING A SCHEDULED 3C INSPECTION THE CENTER TOP CAP IN LAV WAS CORRODED. MAINT REMOVED AND REPLACED THE CENTER TOP-CAP IN THE LAV, ALL WORK WAS IAW SRM 51-40-02 AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040106000952004010600095SO 2004 1 6 C2XA03SH485 120031207A532014528737001 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK STRINGER 19L T-REINFORCEMENT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040106001602004010600160EU 2004 1 6 03351303 120031217A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27303UE 41015 DURING INSPECTION THE LT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040106001752004010600175WP 2004 1 6 03FDEA02220 120031220A5740ARC0153 BRACKET DOUG DC10 DC1010 3022110WP WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 COMPLY WITH EA 8-5740-73859 REV A WINGS - RT OUTBOARD HINGE BRACKET - SIDE LOAD FITTING HOLE REPAIR (P/N ARC0153). COMPLIED WITH EA 8-5740-73859. 2L73 4F A22WE 20040106001992004010600199WP 2004 1 6 GTIA030981 120031117A5313 LONGERON DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - E/E COMPARTMENT STATION 160 L25L CRACKED. REMOVED SHEAR TIE SECTION AT STATION 148 LONGERON 26L-24L. REMOVED LONGERON SECTION FROM STATION 141-170. FABRICATED LONGERON SECTION AND TWO LONGERON SPLICES. FABRICATED SHEAR TIE SPLICE. INSTALLED NEW LONGERON SECTION. INSTALLED NEW SHEAR TIE SPLICE. (M) 2L72 4F A6WE 20040108000552004010800055NM 2004 1 8 IU62003F00038 120030917A2910511531 HOUSING BOEING737 737* NM SHUTTLE VALVE CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 CRACKED INNER DIAMETER OF MOUNT HOLE. OVER TORQUE, OVER PRESSURE OF POOR DESIGN. ENGINEER NEW DESIGN OF MATERIAL TYPE. 2L72 4F RTA16WE 20040108000582004010800058EA 2004 1 8 WVE2003F00016 120030928A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FS CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09611QX 10041 FS 1098.20 BULKHEAD LEFT HAND SIDE BETWEEN STRINGERS 8L AND 9L, LBL 34 TO 41 AND WATER LINE 120 TO 125.42 IS CRACKED 1 INCH LONG IN WEB AREA. POSSIBLE STRESS RELIEF CRACK. RECOMMENDATION: REMOVE DAMAGE AND INSTALL BATHTUB FITTING IAW MM REO 670-53-61-034 REV B. (EA09200301584) 2L72 4F RTA21EA 20040108000612004010800061SO 2004 1 8 HLF2003F00000 220031006A8520 CRANKCASE CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO ENGINE CRACKED B HLFRO OTHER O OTHER NRNOT REPORTED 1 SW17149AF1242 421C0098 292494R CRACKED CRANKCASE AT NR 5 CYLINDER, CRACK IS 6 INCHES LONG, EXCEEDING THE MAX ALLOWED IAW SB 90-17. PROBABLE CAUSE: IMPROPER TORQUE OR DEFECTIVE CRANKCASE. REPORTED TO MFG. 1L72 3O3 O A7CE E7CE 20040108000682004010800068EU 2004 1 8 X6U2003F00000 120031008A2740543502501 ACTUATOR ISRAEL1124 1124 4500102EU GARRTTTFE731TFE7313 01518WP PITCH TRIM FAILED B X6URK NONE O OTHER ININSP/MAINT 1 SW15274HM 1196 342 P77430 DURING ROUTINE 200 HOUR AIRFRAME INSPECTION, FOUND APPROX 0.125 INCH VERTICAL MOVEMENT OF THE LT AND RT ROD END ADAPTERS. TIE BOLT IS LOOSE AND BENT WHERE IT PASSES THROUGH EACH ADAPTER. ALSO FOUND VERTICAL MOVEMENT OF THE JACKSHAFT THREADS. BOTH ROD ENDS JAMB NUTS WERE LOOSE. FLIGHT CREW REPORTED A CYCLIC (10 SEC TIME LENGTH) VIBRATION IN THE AIRCRAFT AT 300 KTS BELOW 18,000 FT. DOCUMENTED THE VERTICAL MOVEMENT ON VIDEO. PITCH TRIM ACTUATOR WAS REMOVED FROM SERVICE AS UN-AIRWORTHY. THIS UNIT WAS AT 40 PERCENT OF SERVICE LIFE OF 2500 CYCLES (ACTUAL CYCLES/LANDINGS = 971). THIS UNIT WAS CLOSE TO ATTACHMENT FAILURE, WHICH WOULD RESULTED IN AN UNCONTROLLED CRASH. 2M72 4F4 F A2SW E6WE 20040106001362004010600136NM 2004 1 6 03FDEA02217 120031219A1430 COLLAR DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 AFT UPPER FUSELAGE STA 2014 CANTED BULKHEAD FRONT FACE FOUND WITH 11 EA LOCKBOLT COLLARS CRACKED. REMOVED CRACKED FASTENERS 11EA AS PER SRM 51-32-01 VOL. II AND INSTALLED NEW FASTENERS 11EA AT AFT UPPER FUSELAGE STA 2014 CANTED BULKHEAD FRONT FACE AS PER SRM 51-32-01 VOL. II. 2L73 4F RTA22WE 20040106001522004010600152NM 2004 1 6 UPS03M41655 120031212A5753 FLAP DOUG MD11 MD11F 3023600NM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 INSPECTION TYPE:N/A RIGHT O/B FLAP HAS DELAMINATION AT I/B END (MRK). 2L73 4F RTA22WE 20040106001562004010600156EU 2004 1 6 DHL2003363006 120031218A7620 A/C PACK AIRBUS300 A300B4203 3930306EU CONNECTOR LOOSE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01363DH 85 UNABLE TO SHUT NR 2 ENGINE DOWN WITH FUEL SHUT-OFF & FIRE HANDLE. FOUND PIN BB ON P SIDE OF 432VC LOOSE (105VU). SECURED PIN. OPS CHECKED NORMAL ON ENGINE RUN AS PER 76-12-11. 2L72 4F RTA35EU 20040106002022004010600202WP 2004 1 6 GTIA030978 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND COCKPIT CENTER FLOOR PANEL, INSERT DRILLED THROUGH, INSERT MISSING, DELAMINATED AT EDGES. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040106002112004010600211WP 2004 1 6 GTIA030976 120031115A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN SUBFLOOR CORRODED AT FS 200 6 INCHES LBL TO 6 INCHES RBL. REMOVED CORRODED WEB. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040108000782004010800078NM 2004 1 8 HALA0300875 120031002A2820MA20A10011 ACTUATOR BOEING767 767300 1385204NM FUEL CROSSFEED FAILED A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13584HA 24258 FUEL CROSS FEED VALVE REMAINED ILLUMINATED WHEN OPEN OR CLOSED. FUEL CROSS FEED EICAS LIGHT ILLUMINATED. REMOVED AND REPLACED FUEL CROSS FEED ACTUATOR IAW AM. REPLACED CONNECTOR D1544. OPS CHECK OK IAW AMM, MPN, SN ON 439391; SN OFF 3696(K) 2L72 4F RTA1NM 20040108000812004010800081EU 2004 1 8 PA03005 120030123A5412 BULKHEAD BRAERODH125 HS125700A 4230170EU LT NACELLE CRACKED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL2348FB 9630 6354 257129 THE LT ENGINE NACELLE AFT BULKHEAD IS CRACKED AT THE 6 O`CLOCK POSITION. PROBABLE CAUSE IS VIBRATION.(K) 2L72 4F A3EU 20040108000862004010800086EU 2004 1 8 KBM2003F00036 120031002A6420350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 TAIL ROTOR PC BEARING, PLAY BEYOND LIMIT. REPLACED WITH 2 OVERHAULED PITCH LINKS.(K) 1G71 3U3 U H9EU E19EU 20040108000932004010800093EU 2004 1 8 KBM2003F00043 120031005A21210500521 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE FAN INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 A/C DOES NOT BLOW AIR HARD ENOUGH. REMOVED AND REPLACED WITH NEW SERVICEABLE MOTOR. 1G71 3U3 UNCH9EU E19EU 20040108000942004010800094EU 2004 1 8 KBM2003F00044 120031005A6710XEMRE8RSA8 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE M/R PITCH LINK WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 3 EACH UPPER ROD END ON MAIN ROTOR PITCH CHANGE LINK ARE WORN BEYOND LIMITS. REPLACED WITH 3 EACH NEW UPPER ROD END BEARINGS. 1G71 3U3 UNCH9EU E19EU 20040108000962004010800096EU 2004 1 8 KBM2003F00046 120031005A6420355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 TAIL ROTOR HALF SHELL BEARINGS WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW BEARING KIT. 1G71 3U3 UNCH9EU E19EU 20040108001002004010800100EU 2004 1 8 KBM2003F00050 120031007A2110SD507 BLOWER MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COMPRESSOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH1461 2957 A/C (BLOWER MOTOR) QUITS WORKING, CLUTCH COIL FOUND DEFECTIVE. REPLACED WITH SERVICEABLE COMPRESSOR. 1G71 3U3 UNCH9EU E19EU 20040108001062004010800106 2004 1 8 KBM2003F00056 420031012A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU VHF SYSTEM MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 86 3403 VHF RADIO HAS REAR CONSTANT SQUELCH FROM FREQUENCY 120.25 TO 120.75. DID NOT FIX PROBLEM, RETURNED TO STOCK. INSTALLED REPAIRED VHF RADIO.(K) 1G71 3U H9EU 20040108001172004010800117CE 2004 1 8 J7B2003F00001 120031010A6121C20722 COIL MCAULY CESSNA421 421C 2076016CE CONT O520 GTSIO520N 17032SO MCAULY3FF32 3FF32C501 GL SYNCHROPHASER SEPARATED D J7BAO OTHER O OTHER NRNOT REPORTED 1 SW01421GF8544 507 811117 421C1110 276386R 941289 ON TAKE OFF THE RT ENGINE FEATHERED. INSPECTION REVEALED PROPELLER SYNCROPHASER COIL HAD BECOME SEPARATED FROM THE GOVERNOR BODY, CAUSING THE PROPELLER TO FEATHER. THE ATTACHING STUDS ON THE COIL HAD SHEARED AND BECAME BOUND UP WITH THE FLYWEIGHT ASSY. PULLING THE METERING ROD NTO THE FEATHER POSITION. RECOMMEND A CLOSER INSPECTION OF THE (PN C20722) COIL OR POSSIBLY REPLACEMENT AT OVERHAUL. (K) 1L72 3O3 O A7CE E7CE 5 CP45GL 20040108001242004010800124CE 2004 1 8 KZ52003F00001 120031002A5320504400287778 STIFFENER BEECH 65 65 1152802CE AFT BULKHEAD CRACKED D KZ5RO OTHER O OTHER NRNOT REPORTED 1 GL155080L10359 LF59 INSPECTION REVEALED THE PARTS TO BE CRACKED BETWEEN RIVET HOLES WHERE STIFFENER WAS ATTACHED TO AFT BULKHEAD. NO FURTHER DAMAGE WAS NOTED AFTER PART WAS REMOVED.(K) 1L72 3O 3A20 20040108001262004010800126NE 2004 1 8 UO22003F00010 220031003A727030607424 DUCT AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE NR 1 ENGINE CRACKED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL192425 3617 32 NR 1 ENGINE AFT BY-PASS DUCT CRACK AROUND 9 O’CLOCK RIB DUCT, ALLOWED MOMENTARY DISENGAGEMENT OF OIL TRANSFER TUBE AND ORING FAILURE. OIL LEAK CAUSED LOSS OF OIL PRESSURE AT TAKEOFF. PILOT SHUT DOWN ENGINE AND LANDED AT NEAREST AIRPORT. AT REPLACEMENT OF DUCT THE AIRCRAFTS ADDITIONAL ENGINES WERE INSPECTED AND LIKE DEFECTS WERE FOUND ON BOTH ENGINES A 3 AND 9 O’CLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAL MDRS DATED 10-03-03 ON FALCON 900EX, SN 032.(K) 2L73 4F4 FRTA46EU E1NM 20040108001292004010800129NE 2004 1 8 ALG2003F00102 120030924A2620 WIRE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL FIRE EXT SBOX SHORTED E ALGAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW03522AL 760236 CAE890100S IN CRUISE FLIGHT, SMELLED SMOKE AND SAW SMOKE FLOWING OUT OF OVERHEAD QUADRANT FRONT BY FIRE HANDLES. EXECUTED TURN AROUND TO INTRACOASTAL AND SMOKE STOPPED. FIRE EXTINGUISHER CIRCUIT BREAKERS POPPED. RETURNED TO INTRACOASTAL, EVERYTHING ELSE NORMAL INDICATIONS. MAINTENANCE FOUND SCREW CHAFED INTO THE WIRE IN THE FIRE EXTINGUISHER SWITCH BOX. REPLACED WIRE, REPOSITIONED WIRES AND SECURED. OPS CHECKED OK. (K) 1G72 3U3 U H1NE E1GL 20040108001332004010800133NE 2004 1 8 Z1R2003F00003 120031020A14307615009143041 SCREW SKRSKYS76 S76C 8143008NE M/R TIP CAP BROKEN E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11761AF903 760524 BLACK BLADE (COLOR CODED) TIP CAP SCREWS M/R LEADING EDGE AND BOTTOM ROW. NR 1 SCREW BROKEN. CORROSION AROUND SHANK OF SCREWS (ALL) SCREW HAD BEENN WORKING WITH BREAK ABOUT 90 PERCENT THROUGH THE SCREW WITH THE LAST 10 PERCENT BREAKING WHEN SCREW REMOVED. FIRST FIVE SCREWS FROM LEADING EDGE TOP AND BOTTOM, INSTALLATION TORQUE IS (BOOK) 100 IN/LBS BREAKAWAY TORQUE TO REMOVE THESE SCREWS WAS RANGING FROM 130-170 IN/LBS. (LARGE SCREW) LAST FOUR, SMALL SCREWS, TOP AND BOTTOM (8) INSTALL TORQUE 30 IN/LBS, REMOVE BREAKAWAY TORQUE 30-50 IN/LBS.(K) 1G72 3U NCH1NE 20040108001402004010800140EU 2004 1 8 KBM2003F00074 120031020A6710126891P BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 LOWER END BEARINGS WORN BEYOND LIMITS. REPLACED WITH NEW LOWER END BEARINGS.(K) 1G71 3U3 UNCH9EU E19EU 20040108001502004010800150NM 2004 1 8 AMTA200301254 120030929A5313 STRINGER BOEING757 75723N 1384973NM FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 MAIN CABIN STRINGER DENTED. REPAIRED STRINGER IAW MFG ER 03-3629 AND SRM 53-00-03, FIG. 201.(K) 2L72 4F RTA2NM 20040108001532004010800153NM 2004 1 8 AMTA200301253 120030930A5315 FLOORBEAM BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 MAIN CABIN FLOORBEAM UPPER SURFACE OF UPPER CHORD CORRODED. REPAIRED FLOORBEAM IAW MFG ER 03-3507. 2L72 4F RTA2NM 20040108001602004010800160SO 2004 1 8 UC22003F00000 120031025A534367271800 ATTACH BRACKET PIPER PA28 PA28R201 7102816SO MLG SEPARATED B UC2RA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 GL195321U884 2844042 DURING A TRAINING FLIGHT THE PILOT REPORTED THAT HE HEARD A LOUD BANG WHEN THE LANDING GEAR WAS RETRACTED. THE LANDING GEAR UNSAFE LIGHT THEN CAME ON. THE PILOT THEN EXTENDED THE GEAR AND MADE AN EMERGENCY LANDING. THE AIRPLANE WAS INSPECTED AND THE NOSE GEAR ACTUATOR REAR ATTACH WAS FOUND SEPARATED AT THE JACK POINT WELD. THE PROBABLE CAUSE IS THAT THE NOSE GEAR ACTUATOR HAS TOO MUCH TRAVEL IN THE RETRACT POSITION. THESE ACTUATORS HAVE BEEN BENDING THE NOSE GEAR ACTUATOR HARDWARE AND MASHING THE NOSE GEAR UP STOPS ON OUR FLEET OF SIX ARROWS ON A RECURRING BASIS. RECOMMEND THAT AN EMERGENCY AD IS ISSUED AND THAT THE MFG TAKE SOME CORRECTIVE MEASURES IMMEDIATELY. NOTE AC SN: 2844028 AND UP. (GL192004009411L71 3O 2A13 20040109000052004010900005EA 2004 1 9 WVE2003F00019 120031021A5754 VANE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE RT FLAP CHAFED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09612QX 10042 RT OUTBOARD FLAP VANE IS CHAFED ON THE OUTBOARD LEADING EDGE OF THE VANE CAP APPROXIMATELY 2 INCHES FROM THE END. THE CHAFE IS .025 INCHES X .003 INCHES DEEP. CHAFING AGAINST THE BUTE DOORS WHEN FLAPS EXTEND AND RETRACT. RECOMMENDATION: BLEND CHAFED AREA TO SMOOTH THE SURFACE, PERFORM EDDY CURRENT TO ENSURE THAT NO CRACKS EXIST ALODINE, PRIME, AND PAINT TO MATCH SURROUNDING STRUCTURE IAW EA R57-50.(K) 2L72 4F4 FRTA21EA E15NE 20040109000092004010900009NM 2004 1 9 MEX2003506 120031028A27806010N000104 ACTUATOR DOUG MD80 MD83 3023681NM SLATS FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23945AS 49643 AIRCRAFT RETURNED TO PLATFORM DURING TAXING, WHEN SLATS WERE EXTENDED AUTO SLAT FAIL LIGHT TURNED ON. SYSTEM WAS CHECKED WITH OTHER COMPUTERS, CONFIRMING THE FAIL IN BOTH AUTO-SLAT ACTUATORS. ACTUATORS WERE REPLACED IAW MM27-80-08, TEST CORRECT. FURTHER. WHEN THE AIRCRAFT WAS DISPATCHED ART INOP LIGHT TURNED ON FAIL REPORT WAS DEFERRED IAW MEL 73-8.(K) 2L72 4F RT 20040109000112004010900011NM 2004 1 9 W321581A5 120031006A532097109323015 BEAM BOEING737 737* NM GE CFM56 CFM56* 13802NE AFT CARGO COMP BROKEN E BJ6AO OTHER O OTHER NRNOT REPORTED 1 NE03171QS1354 30572 STABILIZING ROD END ON PORTABLE WATER TANK BROKE OUT OF BEAM. DURING NON-ROUTINE MAINTENANCE IN THE AFT LOWER CARGO COMPARTMENT FOUND TURNBUCKLE ASSY PN 971093025 HAD BROKE FREE OF BEAM PN 97109323015. LOCATION IS APPROX FS887, RBL 10.75, WL 202. OPERATOR INDICATED THIS IS A REPEAT OCCURRENCE AS THIS ALSO OCCURRED ON OTHER AIRCRAFT. SB IS BEING PREPARED.(K) 2L72 4F4 FRTA16WE E2GL 20040109000192004010900019 2004 1 9 CA52003F00000 420031016A2565D14090119 HOSE AIRCRUISERS BOEING757 757* NM ESCAPE SLIDE CRUSHED B CA5YO OTHER O OTHER NRNOT REPORTED 1 EA35 0540 THE ESCAPE SLIDE WAS RECEIVED. THE INFLATION HOSE HAD BEEN BROKEN, AND THE RELIEF VALVE HAD CUT THROUGH THE FABRIC. THIS DAMAGE WAS CAUSED BY EXCESSIVE FORCE DURING PACKING. THE ESCAPE SLIDE WOULD NOT HAVE OPERATED. IT IS NOT KNOW WHO CARRIED OUT THE PREVIOUS OVERHAUL.(K) 2L72 4F RTA2NM 20040109000382004010900038NE 2004 1 9 CHI2003F00004 220030727A7200 ENGINE BOEING234 234 1385049EA LYC AL5512AL5512 41581NE NR 2 MAKING METAL B CHIRO OTHER O OTHER NRNOT REPORTED 1 NM09246CH10676681 MJ017 DURING FLIGHT NR 2 ENGINE CHIP LIGHT CAMP ON. PILOTS REF EMERGENCY CHECKLIST AND IT INSTRUCTED THEM TO MONITOR ENGINE OIL PRESSURE AND TEMP, THEN LAND AS SOON AS PRACTICAL. AFTER LANDING THE NR 2 ENGINE CHIP DETECTOR WAS INSPECTED AND 2 METALLIC SLIVERS AND 1 FLAKE WERE FOUND ON THE CHIP DETECTOR. THE MAIN OIL FILTER WAS THEN INSPECTED AND A COUPLE MORE SMALL FLAKES WERE FOUND REF MM. ENGINE WAS THEN DETERMINED TO BE UNSERVICEABLE. NR 2 ENGINE WAS REMOVED AND REPLACED AND AC RETURNED TO SERVICE. THE ENGINE SHOP IS COMPLETING AN EVALUATION INSP TO DETERMINE THE SOURCE OF THIS METAL. 2G72 4U4 U H9EA E4NE 20040109000482004010900048WP 2004 1 9 GTIA031003 120031115A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND MAIN CABIN F/B STATION 807-927 RT OB IS CRACKED AND SPACER MISSING. FABRICATED MAIN CABIN OB FLOOR PANEL. (M) 2L72 4F A6WE 20040109000502004010900050EA 2004 1 9 2004F00000 220030318A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA NR 1 MAKING METAL A YADAO OTHER J WARNING INDICATION NRNOT REPORTED 1 AL035632C UC81 PILOT REPORTED NR 1 ENGINE OIL PRESSURE SLOWLY DROPPED TO RED LINE AND THE LOW OIL PRESSURE LIGHT CAME ON. ENGINE WAS SECURED AND THE AIRCRAFT WAS LANDED AT ANCHORAGE WITHOUT INCIDENT. INSPECTION REVEALED HEAVY METAL CONTAMINATION IN THE OIL FILTER, FERROUS AND NON-FERROUS METAL. SPECIFIC SOURCE OF FAILURE NOT YET DETERMINED. ENGINE REMOVED FOR OVERHAUL. (M) 2L72 4T4 TRTA24CE E4EA 20040109000522004010900052NM 2004 1 9 USAABB03225 120031216A335020131A BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 FOUND THE L3 AND R3 DOOR EXTERIOR EMERGENCY ILGHTS INOPERATIVE. MAINTENANCE REPLACED BOTH BATTERIES. (M) 2L72 4F RTA2NM 20040109000552004010900055NE 2004 1 9 2004F00003 220031201A7200 ENGINE AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE NR 2 FIRE A RJEFK NONE A FLAME/FIRE ININSP/MAINT 1 SO23455TA 874 V10404 DURING ENGINE NR 2 TESTS AFTER THE ENGINE FIRE, IAW NORMAL PROCEDURE BOTH ENGINE FIRE EXTINGUISHING BOTTLES WERE USED AND SOME OTHER CHEMICAL EXTINGUISHERS WERE USED ON ENGINE NR 2. THE ENGINE WAS REPLACED AND SENT TO A REPAIR STATION FOR REPAIRS. ENGINE WAS TESTED IAW AMM 71-00-20. ALL RESULTS WERE NORMAL. (M) 2L72 4F4 FRTA28NM E40NE 20040109000702004010900070NM 2004 1 9 2004F00008 120031101A3350MS1557081 LAMP BOEING727 727200 138407ENM EMERGENCY LIGHT BURNED OUT A P9RAK NONE O OTHER ININSP/MAINT 1 SO11288SC 20765 EMERGENCY EXIT OVERWING LIGHT HAS 3 LAMPS INOPERATIVE. RELAMPED EMERGENCY OVERWING EXIT LIGHT IAW B727 MM 33-50-11. (M) 2L73 4F RTA3WE 20040112000072004011200007NM 2004 1 12 TSAA0255266 120030905A55126554821 SKIN BOEING737 737282 13844ATNM HORIZONTAL STAB GOUGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13824AL 23045 CUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040112000162004011200016NM 2004 1 12 USAASB03216 120031216A3350110049 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US 23314 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 22 AND AT BOTH AFT DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND REPLACED ALL BULBS. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040112000302004011200030SO 2004 1 12 CHQA000431 120031218A2740 PITCH CONTROL EMB 135 EMB135LR 3260305SO HORIZ STAB MALFUNCTIONED A CHQAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL11844 145620 DURING INITIAL CLIMBOUT OF TLH THE AIRCRAFT PRESENTED WITH A PITCH UP ATTITUDE. NOSE DOWN TRIM WAS APPLIED AND RECEIVED A TRIPLE CHIME, MASTER WARNING, AND EICAS MESSAGES INDICATING FAILURES OF MAIN AND STANDBY PITCH TRIM SYSTEMS. TRIM WAS AT +4° AT TIME OF FAILURE. FOLLOWED QRH AND TURNED OF MAIN AND STANDBY PITCH TRIM SYSTEMS. CONTINUED FLIGHT TO MCO, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED AND RESET THE PITCH TRIM SYSTEM PER FIM 27-43-00 AND OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040112000312004011200031 2004 1 12 2004F00017 420030107A3416 INDICATOR BEECH 1900 1900C 1154161CE ALTIMETER FAILED A YADAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 AL031566C UC36 AIR RETURN DUE PILOTS ENCODING ALTIMETER FAILURE, FLAGGED. (M) 2L72 4T RTA24CE 20040112000322004011200032NM 2004 1 12 DHL2003754023 120031217A3240 LINE BOEING727 727223 1384074NM NR 3 & 4 BRAKE CONTAMINATED A DHLAK NONE O OTHER TXTAXI/GRND HDL 1 SO01754DH 22008 WHEN TAXIING IN (CVG) BRAKES STICKS WHEN RELEASED, FELT LIKE THE RIGHT SIDE. BLED NR 3 & 4 MAIN GEAR BRAKES PER 727 M/M 32-41-0. TAXIED AIRCRAFT AND EXERCISED BRAKES. NO DEFECTS NOTED. BRAKES FOUND TO BE IN SERVICEABLE CONDITION IAW 32-41-0. 2L73 4F A3WE 20040114000282004011400028SO 2004 1 14 C2XA03CL210 120031224A3350 CONNECTOR EMB 145 EMB145ER 3260211SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 CLE FLIGHT 2498 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE ON THE BULKHEAD IN FRONT OF SEAT 3B. MAINTENANCE INSPECTED AND RESECURED A LOOSE CONNECTOR ON EMERGENCY LIGHT INVERTER NR 3, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040114000302004011400030SO 2004 1 14 C2XA03CL212 120031226A335020131A BATTERY EMB 135 EMB135ER 3260203SO CABIN DISCHARGED A C2XAK NONE O OTHER NRNOT REPORTED 1 SW2716510 145251 CLE FLIGHT 2026 THE CREW REPORTED THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040114000542004011400054NM 2004 1 14 DL73S030969 120031029A53306545767531 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27324DL 23096 A DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 380 BETWEEN S17L AND S17A. DENT WAS REPAIRED PER ERA 385801-14. 2L72 4F RTA16WE 20040114000842004011400084WP 2004 1 14 IXXA0300083O 120031126A5280 HINGE DOUG DC8 DC871F 302199DWP MLG DOOR LOOSE A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11830BX753182077 45973 DURING TAKEOFF FROM GEAR DOOR LIGHT REMAINS ON WITH GEAR HANDLE IN UP POSITION. ABNORMAL CHECKLIST COMPLIED WITH LIGHT REMAINED ON. CREW DUMPED FUEL & RETURNED KTOL. UPON INSPECTION MAINTENANCE NOTED L/H MAIN GEAR DOOR HINGE ATTACH POINT AT KEEL & ADJACENT AREA HAD LOOSE FASTNERS. ALL FASTNERS WERE REPLACED PER APPLICABLE MANUALS.MAINTENANCE INSPECTED MLG DOOR POSITION WARNING SYSTEM AND NO DEFECTS NOTED. JACKED AIRCRAFT, SWUNG GEAR MULTIPILE TIMES GEAR & INDICATION OPS CHECK NORMAL. UPLATCH CHECK NORMAL WITH AND WITHOUT HYDS, GEAR FREEFALL CHECK NORMAL. NO DEFECTS NOTED ON ALL GEAR AND OPERATIONAL CHECKED GOOD PER APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040114000872004011400087NM 2004 1 14 DL76S031029 120031117A5512185T10012 SKIN BOEING767 767332 1382001NM HORIZ STAB DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27121DE 23435 DELAMINATION FOUND ON HORIZONTAL STABILIZER, FWD TORQUE BOX, UPPER SKIN, RT SIDE, IN SECOND RIB BAY OUTBD FROM FUSELAGE. INNER SKIN OF THE ALUM HONEYCOMB PANEL WAS DELAMINATED FROM THE CORE. REPAIRED PER ERA 426746-14. 2L72 4F RTA1NM 20040114002122004011400212NM 2004 1 14 MWEA030484 120031215A53149930582113 TEE FITTING DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 KEEL BEAM CLIP CRACKED AT STATION 826 LONGERON 29 LEFT EXTERNAL. FABRICATED AND INSTALLED NEW TEE. 2L72 4F RTA6WE 20040114002172004011400217NM 2004 1 14 MWEA030492 120031215A552299378045 SKIN DOUG MD88 MD88 3023688NM LT ELEVATOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 LT ELEVATOR UPPER SKIN HAS A 1 INCH CREASE AT STATION XE=148 2.5 INCHES AFT OF THE FORWARD SPAR. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20040114002202004011400220NM 2004 1 14 MWEA030486 120031215A531059360381 DOOR FRAME DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 MID CARGO DOOR JAMB HAS CORROSION AROUND SEVERAL FASTENERS FOR THE SCUFF PLATE. FABRICATED AND INSTALLED REPAIR NUT STRIPS. 2L72 4F RTA6WE 20040115000122004011500012NM 2004 1 15 03FDEA02027 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 4 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000222004011500022NM 2004 1 15 03FDEA02037 120031203A5310 CREASE BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CREASE BEAM WEB BS 740 TO BS 730F IS CORRODED. REMOVED CORROSION ON CREASE BEAMM WEB BS 740 TO 720F, LBL 65, WL 208. 1X2 INCH. MAXIMUM MATERIAL WAS .020. ORIGINAL THICKNESS .040. OUT OF LIMITS. CUT OUT DAMAGE. FABRICATED FILLER AND DOUBLER LOT 519938. 7075 T6 .040. ALODINED AND PRIMED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-10-1/ SRM 53-10-1/ SRM 51-40-2/ SRM 51-10-2/ SRM 51-30-2/ FED EX MM 51-20-151-7. 2L73 4F RTA3WE 20040115000262004011500026NM 2004 1 15 03FDEA02013 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 N0318 LT OB FLAP, OB HINGE ACTUATOR HOLE NR 1 I/B CORRODED.COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000282004011500028NE 2004 1 15 SW07200300007 220030727A7250 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE DAMAGED G FDKAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW07509MJ 10094 GEE965415 THE CREW DISCOVERED FOD DAMAGE TO NR 13 AND NR 14 FAN BLADES, FAN RUB STRIP, AND STATORS. THE ENGINE WAS REMOVED AND REPLACED. 2L72 4F4 FRTA21EA EOOO63EN 20040115000392004011500039NM 2004 1 15 03FDEA02051 120031204A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 WHILE WORKING FOUND UPPER FLANGE OF FRAME BS 1070 LBL 18 WL 150 TO BE DOUBLE HOLED. REMOVED DAMAGE ON FRQME QT BW 1070, LBL 18, WL 150 UPPER FLANGE. INSTALLED NEW FABRICATED DOUBLER FOR FRAME AT BS 1070, WL 150, LBL 18 IAW SRM 51-40-3. 2L73 4F RTA3WE 20040115000532004011500053NM 2004 1 15 DL76G031079 120031213A3246767ERM WHEEL BOEING767 767332 1382001NM NR 1MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO271612T 30575 LEFT SHEARED ON MAIN WHEEL. REPLACED NR 1 MAIN WHEEL AS PER MM REF 32-45-004-001. 2L72 4F RTA1NM 20040115000542004011500054NM 2004 1 15 DL764031080 120031212A14301617T7200501 BOLT BOEING767 767432ER 1385134NM LT MLG SHEARED A DALAK NONE O OTHER ININSP/MAINT 1 SO27839MH 29712 FOUND ON TRANSIT CHECK LEFT MLG UPLOCK FITTING ATTACH BOLT SHEARED. CLEANED AND INSPECTED UPLOCK FITTING NO ADDITIONAL DAMAGE NOTED. REPLACED LEFT MLG UPLOCK FITTING BOLT. 2L72 4F RTA1NM 20031212000152003121200015NM 2003 12 12 SWAA032436 120031104A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, WL 208, RBL 5. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031212000162003121200016NM 2003 12 12 SWAA032437 120031104A53156546804 FLOORBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031212000202003121200020NM 2003 12 12 SWAA032416 120031031A53126550781 PRESSURE PANEL BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER UKUNKNOWN 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND 0.5 INCH CRACK IN PRESSURE WEB AT BS 665, LBL 32.5. REPAIRED PER SRM. 2L72 4F RTA16WE 20031212000232003121200023NM 2003 12 12 SWAA032419 120031031A52406545871 DOOR FRAME BOEING737 737317 138447PNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED R1 DOOR FRAME AT DOOR STOP BRACKET THIRD FROM TOP. REPAIRED PER SRM 2L72 4F RTA16WE 20031212000492003121200049NM 2003 12 12 03FDEA01905 120031111A5311 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 GOUGE ON BS 540 FRAME, I/B FLANGE, ONE INCH ABOVE STR 22L. BLENDED GOUGE AREA ON FRAME AT BS 540 ABOVE STR 22L, 1 X 1 X .008 INCH ORIGINAL THICKNESS .045 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 1 FIG 1, DETAIL I. REMOVED AND REPLACED LOWER LEFT FRAME SEGMENT IAW SRM 51-30-2. LOT NR 524482 2L73 4F RTA3WE 20031212000842003121200084NM 2003 12 12 SWAA032432 120031103A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED PM CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 895 AND BS 835, STRINGER 25L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031212001242003121200124NM 2003 12 12 AWXA200301430 120031029A53206552264502 FITTING BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1 INCH CRACK WAS FOUND ON FRAME FITTING AT BS 616, RBL, 65, WL 200. MAINTENANCE REMOVED DAMAGED AREA ON FRAME FITTING AT BS 616, RBL, 65; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-001. 2L72 4F RTA16WE 20031212001292003121200129NM 2003 12 12 AWXA200301435 120031021A5330659187911 SKIN PANEL BOEING737 7373G7 1384595NM FUSELAGE DISTORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK FOUND KEEL BEAM SKIN PANEL AND FAIRING DISTORTED AT BS 661.75 TO BS 726.75, LBL 6 TO RBL 6. MAINTENANCE REMOVED KEEL BEAM SKIN PANEL AND FAIRING FROM BS 661.75 TO BS 726.75, LBL 6 TO RBL 6; FABRICATED A NEW REPLACEMENT SKIN PANEL; INSTALLED REPAIR PART IAW AWA ER 03-5310-03090-TB1. 2L72 4F RTA16WE 20031212001402003121200140WP 2003 12 12 AALA20030931 120030902A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21564AA 49346 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT WAS INOPERATIVE LEFT SIDE FORWARD OF THE AFT ACCESSORY DOOR. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031212001452003121200145WP 2003 12 12 AALA20030938 120030902A3350AA3255A CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21410AA 49321 IAD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 14. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001502003121200150WP 2003 12 12 GTIA030853 120030927A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND E/E BAY FS 216 CEILING WEB CORRODED AND CRACKED. CUT OUT CORRODED AND CRACKED AREA. FABRICATED NEW WEB SECTION AND DOUBLER. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20031212001592003121200159WP 2003 12 12 GTIA030855 120030907A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND SEAT TRACKS LEFT STATION 200 TO STATION 826 BARE METAL, NICKS, LIGHT CORRODED. INBOARD SEAT TRACK LBL 24 STATION 226-826 OUT OF LIMITS. OUTBOARD SEAT TRACK LBL 54 STATION 465-826 OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK LBL 54 STATION 200-826. REMOVED INBOARD SEAT TRACK FROM STATION 226-826. LOCATED AND DRILLED SEAT TRACK. FABRICATED 9-13 SPLICE PARTS. FABRICATED 9-15 SPLICE PARTS. INSTALLED NEW INBOARD SEAT TRACK STATION 226-826. LOCATED AND DRILLED SEAT TRACKS LEFT OUTBOARD. INSTALLED SEAT TRACK STATION200-826 LBL 54. (M) 2L72 4F A6WE 20031212001752003121200175EA 2003 12 12 COMA0360523 120031202A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01967CA 7134 FLIGHT 5346) RECEIVED A FLAP FAIL CAUTION AT 20 DEGREE FLAP POSITION DURING QBS APPROACH. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20031215000282003121500028NM 2003 12 15 SWAA032527 120031116A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031215000372003121500037NM 2003 12 15 SWAA032514 120031113A52406969854 GUSSET BOEING737 737317 138447PNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REPAIRED GUSSET PER BAC DRAWING. 2L72 4F RTA16WE 20031215000392003121500039NM 2003 12 15 0320046302 120031114A381060B500126 COMPRESSOR BOEING747 747451 1384940NM POTABLE WATER MALFUNCTIONED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01662US42795262 23720 DURING CRUISE, AN ELECTRICAL BURNING SMELL EMITTED IN THE CABIN AND FLIGHT DECK. TURNED OFF CABIN VIDEO AND FOLLOWED COM PROCEDURES FOR ELECTRICAL SMOKE AND REMOVED POWER TO THE RECIRCULATION AND GASPER FANS. SMELL DISSIPATED AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE POTABLE WATER COMPRESSOR AND PRESSURE SWITCH. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031215000972003121500097NM 2003 12 15 MWEA030447 120031120A5320393653435 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 J-CHANNEL AT STATION 168 HAS CORROSION ON FASTENER HOLE LOBES. FABRICATED AND INSTALLED NEW J-CHANNEL. 2L72 4F RTA6WE 20031215001012003121500101NM 2003 12 15 MWEA030450 120031120A27603F2201F MODULE BOEING717 717200 1383700NM SPOILER INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31910ME 55174 GROUND SPOILER WOULD NOT ARM. REMOVED AND REPLACED SPEED BRAKE MODULE. 2L72 4F TRA6WE 20031215001062003121500106NM 2003 12 15 AWXA200301468 120031104A5320654797321 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON LT SURFACE OF SHEAR WEB AT OUTBOARD EDGE OF RIVET ROW FROM BS 616 TO BS 619, LBL 70, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 616 TO BS 639, LBL 70; FABRICATED A NEW REPLACEMENT SECTION OF SHEAR WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 38. 2L72 4F RTA16WE 20031215001322003121500132WP 2003 12 15 AALA20031177 120031021A3397 WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21489AA 49682 ORD - MAINTENANCE OBSERVED EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 22 AND 23. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001402003121500140WP 2003 12 15 AALA20031089 120030930A3397 WIRE HARNESS DOUG DC9 DC983 3022083WP CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21433AA 49451 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 9D. REPLACED WIRING HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031215001572003121500157WP 2003 12 15 AALA20031203 120031102A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21292AA 49304 BOS - DURING OVERNIGHT MAINTENANCE FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001592003121500159WP 2003 12 15 AALA20031126 120031008A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21557AN 53087 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT AFT AIR STAIR. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001672003121500167WP 2003 12 15 AALA20031224 120031105A3350AAP3274A BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21285AA 49297 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY CEILING LIGHTS OVER ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS OVER ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001802003121500180EA 2003 12 15 ASOA03540 120031025A3350BF10044004 LENS CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS COVER BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031216000202003121600020EA 2003 12 16 MASA200300428 120031026A3350 COVER CNDAIRCL600 CL6002B19 1900309EA CABIN MISSING A MASAK NONE O OTHER ININSP/MAINT 1 SW0727314 7314 PHX, OVERWING EMERGENCY EXIT SIGN MISSING COVER. MX FOUND COVER AND INSTALLED IT, OP CHECKS GOOD. 2L72 4F RTA21EA 20031216000542003121600054NM 2003 12 16 SWAA032540 120031118A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND BS 540 FUSELAGE STRINGER SPLICE CRACKED AT 10R. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20031216000552003121600055NM 2003 12 16 SWAA032541 120031118A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM CORRODED AT BS 947 AND BS 967. REPAIRED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20031216000582003121600058NM 2003 12 16 SWAA032544 120031118A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CRACKED AT BS 616. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031216000982003121600098SO 2003 12 16 C2XA03TY201 120031202A532014521725001 FLOOR SUPPORT EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717507 145215 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FRAMES 18 TO 23. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031215000732003121500073 2003 12 15 03317308 420031113A31607011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INTERMITTENT A VTZAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27308UE 41023 DURING TAXI THE CREW REPORTED THE FIRST OFFICERS FLIGHT DISPLAYS FLICKERING. THE NR 2 SYMBOL GENERATOR WAS IDENTIFIED AS THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED OF THE FLIGHT DISPLAY SYSTEM AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031215000772003121500077 2003 12 15 AWXA200301463 420031102A256560592101 CABLE AIRBUSA319 A319132 3930340NM EVAC SLIDE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28824AW9065 1490 PHX - EES - DURING P-09 CHECK THE CABLE END WAS FOUND BROKEN ON THE LT OVER WING SLIDE BOTTLE. MAINTENANCE REMOVED AND REPLACED LT OVERWING SLIDE RESERVOIR ASSEMBLY IAW AMM 25-62-46. 2L72 4F RTA28NM 20031215000902003121500090 2003 12 15 SWIA200312590 420031117A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS FAULTY A SWIAO OTHER O OTHER CRCRUISE 1 NM07295UX7580 7580 120295 CAPTAIN'S COMMAND BARS ON THE FLIGHT DIRECTOR ALWAYS INDICATE ABOUT 4 DEGREES TOO LOW. REPLACED APC-65B COMPUTER. OPS CHECK GOOD IAW MM 22-11-00. 2L72 4T RTA31SO 20031215001172003121500117WP 2003 12 15 AALA20030980 120030909A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT SERVICE DOOR EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001222003121500122WP 2003 12 15 AALA20030969 120030907A33500201720004 SOCKET DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217528A 49920 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WAS INOPERATIVE AT SEAT 7D. REPLACED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001232003121500123WP 2003 12 15 AALA20030968 120030907A3397 WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21457AA 49562 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT SEAT 26G. REPAIRED BROKEN WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001602003121500160WP 2003 12 15 AALA20031123 120031003A33503015643 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21274AA 49271 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 9D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001842003121500184NM 2003 12 15 USAABB03201 120031029A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU 27123 CLT - FOUND SIX FLOOR LEVEL EMERGENCY LIGHTS WERE ILLUMINATED WITH THE SWITCH OFF. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031216000212003121600021EA 2003 12 16 MASA200300446 120031109A3397 WIRE CNDAIRCL600 CL6002C10 1390015EA COCKPIT SHORTED A MASAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07512MJ 10109 EUG-DEN, A/C RETURNED TO GATE AFTER SMOKE WAS OBSERVED EMANATING FROM THE F/O'S FLOOD LIGHT CONTROL PANEL. MX FOUND 2 WIRES HAD TOUCHED AND CAUSED THE SMOKE. MX INSPECTED AND PLACED THE SYSTEM ON MEL. 2L72 4F RTA21EA 20031216000532003121600053NM 2003 12 16 SWAA032539 120031118A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED PM CHECK, FOUND 4 IN LONG FUSELAGE SKIN CRACK AT BS 727E, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031216000652003121600065NM 2003 12 16 SWAA032560 120031120A53306523693 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269, ABOVE STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031216001032003121600103SO 2003 12 16 C2XA03SH471 120031123A532014522460009 BUTTSTRAP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712528 145504 SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031217000482003121700048WP 2003 12 17 DHL2003805589 120030804A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING INBD L/E CORRODED BETWEEN STA XFS 572.250 - XFS.603.750. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT CORRODED AREA IAW SRM 57-2-1 FIG 44. FABRICATED SKIN SPLICE (7075-T6 0.050) IAW SRM 57-2-1 FIG 44. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF SKIN SPLICE IAW SRM 51-1-8B. INSTALLED SKIN SPLICE WITH NEW FASTENERS IAW SRM 57-2-1 FIG 44, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. REFER TO N/R 0185 FOR LEFT OUTER WING INBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031217000612003121700061WP 2003 12 17 DHL2003807504 120031007A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING CENTER L/E LOWER PART FORMER CRACKED 0.500 AT XFS 316.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RIGHT CENTER L/E LOWER PART FORMER XFS 316.000 IAW SRM 57-2-0 PG 9, 10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031217000622003121700062WP 2003 12 17 DHL2003807511 120031007A5720 CLIP DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT WING CTR L/E FORMER CLIP CRACKED AT STA XOLD 6.2246. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED CLIP (2024-T3AL 0.050) IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 57-2-0 PG 9, 10, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031217000652003121700065WP 2003 12 17 DHL2003805591 120030807A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 442.185. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9-10 (2024-T3 0.032, 2024-T3 0.040). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLERS WITH NEW FASTENERS ON LEFT WING CTR L/E FORMER, STA XS 442.185 IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031217000842003121700084NM 2003 12 17 737DX0001 120031103A335020131A BATTERY PACK BOEING737 737400 138449ANM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05737DX 24804 NEXT TO AFT RT BULLNOSE EMERGENCY EXIT LIGHT, RT AFT EXTERIOR DOOR EMERGENCY LIGHT, AND AFT RT GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD PER MM 33-51-02. 2L72 4F RTA16WE 20031217000962003121700096NM 2003 12 17 CALA0300673 120031121A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 INSPECTION FOUND A 2 INCH CRACK IN LT KEELBEAM AT STA 727. A NEW KEELBEAM SECTION WAS SPLICED IN IAW ECRA 5311-01176. 2L72 4F RTA16WE 20031217001052003121700105WP 2003 12 17 IXXA0300082O 120031125A7722 WARNING LIGHT DOUG DC8 DC873F 302199FWP NR 3 ENG PANEL ILLUMINATED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11605AL929071884 46106 DURING CLIMB FROM KTOL NR 3 ENGINE EGT STARTED TO FLUCUATE AND WENT OFF SCALE, IT THEN WENT BLANK AND STARTED WORKING AGAIN. ALL OTHER INDICATION NORMAL. CREW RETURNED AIRCRAFT TO KTOL. AN INSPECTION IS ON GOING AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. 2L74 4F RT4A25 20031217001102003121700110 2003 12 17 2003UALA00848 420031111A3417 ADC BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE COCKPIT FAILED A UALAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 WP29913UA 25291 RETURNED DUE TO F/O AIRSPEED INDICATOR FLAG, MACH INDICATOR, VMO INDICATOR FLAG. ATTEMPTS TO CLEAR THE FLAGS WERE UNSUCCESFUL. THE AIR DATA COMPUTER WAS REPLACED. SUBSEQUENT WRITE-UPS INDICATE THAT THE COMPUTER IS NOT THE SOURCE OF THIS INCIDENT. 2L72 4F4 FRTA16WE E2GL 20031217001252003121700125 2003 12 17 03339307 420031205A34207003110901 DISPLAY JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27307UE 41021 DURING AIRCRAFT OPERATION THE FIRST OFFICERS FLIGHT DISPLAY WENT BLANK. THE DISPLAY UNIT WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE FLIGHT DISPLAY WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031217001382003121700138EA 2003 12 17 03343670 120031109A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27670BR 7561 DURING INSPECTION THE AFT CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031217001392003121700139NM 2003 12 17 SWAA032651 120031203A304083000 CONTROLLER BOEING737 7373TO 138447GNM COCKPIT FAULTY A SWAAO OTHER O OTHER CRCRUISE 1 SW29697SW 23838 R1 COCKPIT WINDOW BURNED AND CRACKED. REMOVED AND REPLACED R1 COCKPIT WINDOW ASSY AND HEAT CONTROLLER. 2L72 4F RTA16WE 20031217001442003121700144NM 2003 12 17 DHL2003749009 120031213A5270 SWITCH BOEING727 727200 138407ENM PAX DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01749DH 22013 ON LANDING FORWARD ENTRY DOOR LIGHT ILLUMINATED ON S/O'S PANEL. ADJUSTED SWITCH IAW B-727 M/M 52-70-501. OPS CHECKED GOOD IAW B-727 M/M 52-70-01. 2L73 4F RTA3WE 20031217001752003121700175NM 2003 12 17 SWAA032649 120031202A53116546541 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 663, STRINGER 1. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031217001852003121700185 2003 12 17 SWIA200312604 420031103A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07291SW486 486 120318 WHEN AUTO PILOT ENGAGED ON CAPTAIN'S SIDE- YAW DAMPER DISENGAGES. WORKS OK WHEN AUTO PILOT SELECTED TO F/O. REPLACED CAPTAIN'S AUTOPILOT COMPUTER. OPS CHECKED GOOD. 2L72 4T RTA31SO 20031217001332003121700133NM 2003 12 17 SWAA032715 120031211A53406546546 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER CLIP BS 847, RBL 13.8. REPAIRED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031217001692003121700169NM 2003 12 17 SWAA032643 120031202A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP+DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD AFT FLAP DISBONDED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20031217001992003121700199NM 2003 12 17 AWXA200301493 120031103A5320655384444 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 747, STR 26 RT, UNDER SHEAR CLIP. MAINTENANCE REMOVED AFT CARGO COMPARTMENT FLOOR SUPPORT FROM BS 727 TO BS 767, STR 26 RT; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-53, FIG 201 PG 201. 2L72 4F RTA16WE 20031217002072003121700207EA 2003 12 17 SWIA200312614 120031120A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERONS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07448SW 7678 LEFT SPOILERON FAULT STATUS MESSAGE WOULD NOT CLEAR AFTER SEVERAL ATTEMPTS. REMOVED AND REPLACED LEFT SPOILERON INBOARD ACTUATOR IAW CRJ MM 27-62-01. OPS CHECKED GOOD. S/N OFF: MAL-5772. 2L72 4F RTA21EA 20031217002102003121700210EA 2003 12 17 SWIA200312617 120031124A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07441SW 7602 EMERGENCY LIGHTS DO NOT COME ON DURING ORIGINATING CHECK. REMOVED AND REPLACED ALL 4 ELBP'S IAW MM 33-51-04. OPS CHECK GOOD. S/N OFF: (1) 83365 (2) 33912 (3) 72649 (4) 77744. 2L72 4F RTA21EA 20031218000182003121800018 2003 12 18 MALA030508 420031124A34204066300911 SYMBOL GENERATOR BAC 146 AVRO146RJ85A1500097EU EFIS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15519XJ E2344 AFTER TAKEOFF ON FLIGHT 3414, CREW REPORTED THE CAPT EFIS DISPLAYS WENT BLANK. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED NR 2 SYMBOL GENERATOR P/N 4066300-911, S/N ON 94090418, S/N OFF 92030294, OP CHECKS GOOD IAW AMM 34-27-17. 2H74 4F RTA49EU 20031218000222003121800022NE 2003 12 18 DHL2003754018 220031125A7230 COMPRESSOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE NR 2 ENGINE STALLED A DHLACDO ABORTED TAKEOFF RETURN TO BLOCK OTHER O OTHER TOTAKEOFF 1 SO01754DH 22008 AFTER ADVANCING THRUST LEVERS FOR TAKEOFF HEARD A COMPRESSOR STALL AND REJECTED THE TAKEOFF AT 16,100 GTW AND ZERO INDICATED AIRSPEED. OAT WAS 9 C AND PRESS ALT +100 FT. THIS WAS FIRST ATTEMPT AT T/O. AFTER ADVANCING THRUST LEVERS FOR TAKEOFF HEARD A COMPRESSOR STALL, AUTO PACK TRIP SYSTEM TRIPPED THE PACKS, ENGINE FAIL CAME ON, AND REJECTED AT 163,500 GTW ZERO IAS 9 DEG C AND 100 PA FT. PERFORMED ENGINE RUN IAW JRH CHAPTER 5 INTO WIND ALL ENGINES CHECKED NORMAL. SUSPECT CROSSWIND CONDITIONS CAUSING SURGE. LUBRICATED COMPRESSOR BLEED NR 2 ENGINE PRECAUTIONARY IAW P&W M/M 75-30-00. INSPECTED INLETS/EXHAUST, NO DEFECTS FOUND. COULD NOT DUPLICATE PROBLEM. RUN SHEET FAXED TO MX CONTROL. 2L73 4F4 F A3WE E2EA 20031218000382003121800038SO 2003 12 18 C2XA03SH476 120031126A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 DURING C-CHECK THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER CARGO DOOR CUTOUT BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031218000402003121800040EU 2003 12 18 009081 120031127A7540 WARNING LIGHT SAAB SF340 SF340A 7850100EU COCKPIT ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17146 FLT 4528 FROM PIT TO HGR AFTER T/O ON GEAR RETRACT, FI STOP OPEN LIGHT ILLUM. CREW WAS ADVISED TO RETURN TO FIELD. AC RETURNED TO FIELD WITH NO INCIDENT. 2L72 4T RTA52EU 20031218000432003121800043EU 2003 12 18 013042 120031128A2701 YOKE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE COCKPIT VIBRATION A UHLAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL17152CQ 152 217 DRG202488 ON CLIMBOUT, A STRONG (FWD-AFT) VIBRATION WAS FELT ON THE CAPTAIN YOKE. CREW LEVELED OFF AT 2000 FT, VIBRATION CONTINUED FROM 150-200 KTS. CREW REDUCED SPEED TO 180 KTS, RETURNED TO FIELD WITH VIBRATION CONTINUING UNTIL FLAPS RETRACTED. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20031218000502003121800050EA 2003 12 18 03316678 120031112A2701600902601 BEARING CNDAIRCL600 CL6002B19 1900309EA CONTROL COLUMN OUT OF ADJUST A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27678BR 7653 DURING UNKNOWN PHASE OF AIRCRAFT OPERATION THE CONTROL COLUMN WAS REPORTED CLICKING AND BUMPING UPON ELEVATOR MOVEMENT. THE FAULT WAS TRACED TO LT FORWARD AND AFT YOKE MOUNTING NUTS ON THE FIRST OFFICERS CONTROL COLUMN. THE NUTS WERE RETORQUED PER A BOMBARDIER SERVICE LETTER AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031218000572003121800057EU 2003 12 18 03331317 120031127A3350S22C12ST6S0S6 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27317UE 41031 DURING INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE LIGHTING STRIP WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031218000642003121800064NM 2003 12 18 QXEA200301478 120031129A5210 SEAL BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DIRTY A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09402QX 4032 AFT PASSENGER DOOR IS VERY DIFFICULT TO CLOSE. CLEANED DOOR SEAL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031218000652003121800065NM 2003 12 18 QXEA200301480 120031128A243023088002A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09345PH103491277 476 ON FLIGHT, NR 2 DC GENERATOR ILLUMINATED. ACCOMPLISHED CHECKLIST. CAUTION LIGHT ILLUMINATED AGAIN AFTER ABOUT 5 MINUTES. REMOVED AND REPLACED NR 2 STARTER GENERATOR AND NR 2 GCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031218001012003121800101NM 2003 12 18 2003UALA00889 120031121A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29589UA 28707 EXTERNAL FUSELAGE SKIN DENTED SEVERAL LOCATIONS FWD OF DOOR 2L AT APPROX BS 608-627 BETWEEN STR 15L AND 17L. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING SMALL DOUBLER AND INCORPORATED INTO LARGE EXTERNAL DOUBLER. 2L72 4F4 FRTA2NM E17NE 20031218001022003121800102NM 2003 12 18 2003UALA00890 120031123A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29589UA 28707 ARCING ON EXTERNAL FUSELAGE SKIN AT STA 319.5, STR 2 RT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031218001032003121800103NM 2003 12 18 2003UALA00891 120031119A2612 FIRE LOOP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 ENGINE WILL NOT TEST A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 FLIGHT CREW REPORTS NR 1 ENGINE B-FIRE LOOP DOES NOT TEST PROPERLY. FOUND WIRE W1508-007-16R OPEN 2 INCHES FROM ENGINE CORE LOOP M1122. REPLACED WIRE. 2L72 4F4 FRTA16WE E2GL 20031218001072003121800107NM 2003 12 18 2003UALA00895 120031124A5753 HINGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT WING TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29645UA 25280 RIGHT WING INBOARD FLAP, AFT FLAP HINGE MID ATTACH FITTING, OUTBD AND INBD SIDES CRACKED AT LOWER ENDS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE PER SRM 57-53-02, FIG 201 AND REINSTALLED FITTING PER MM 27-51-06. 2L72 4F4 FRTA1NM E24NE 20031218001112003121800111EU 2003 12 18 2003UALA00900 120031125A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29403UA 442 LEFT FUSE SKIN IS CREASED & DENTED AT STA 359 (FR 23), STR 22L. MAJOR REPAIR ACCOMPLISHED. REPAIR ACCOMPLISHED PER MAE EA 47-5381-13-A1053 & UAL EVA IMC 30150. 2L72 4F4 FRTA28NM E40NE 20031218001222003121800122NM 2003 12 18 03FDEA02002 120031129A5350 FRAME DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 FORWARD TAIL CONE MOST AFT STA 2244 LOWER RT SIDE FRAME FOUND CRACKED. TRIMMED OUT DAMAGED FRAME AS PER SRM 53-00-01, FIG.9, VOL.I. FABRICATED FRAME AS PER DRAWING AKC5739. FABRICATED REPAIR ANGLE AS PER SRM 53-00-01, FIG.9, VOL.I. INSTALLED FRAME AND REPAIR ANGLE AT FORWARD TAIL CONE MOST AFT STA 2244 LOWER RH SIDE AS PER SRM 51-31-01, VOL.II AND 53-00-01, FIG.9, VOL.I. 2L73 4F RTA22WE 20031218001262003121800126EU 2003 12 18 MALA030515 120031120A5320 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION, CABIN AFT AT RT FRAME CHAFED STA 630. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE IAW MESABA EO S53152 DATED 11/21/03. A/C RELEASE DATED 12/2/03. REFER TO 409 NR 1206073 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20031218001292003121800129EU 2003 12 18 MALA030513 120031119A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION. STA 294 BL 0 SEAT TRACK CORRODED. MAINTENANCE REMOVE DAMAGED SEAT SECTION AND INSTALLED NEW SECTION, IAW MESABA EO A53060, DATED 11/3/03. A/C RELEASE DATE 12/2/03. REFER TO 409 NR 1206073 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20031218001332003121800133NM 2003 12 18 P5CA0301001 120031202A3610 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C GL NR 4 ENGINE ILLUMINATED A P5CAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 WP23450PA 30808 706198 NR 4 ENG START BLEED 4 OVERHEAT / PRV MESSAGE STATUS MESSAGE BLEED PRV4. TRANSFERRED TO DMI 31879, MEL 36-11-86 CAT C. ALSO NR 4 REVERSER DEACTIVATED PER MEL REQUIREMENTS. 2L74 4F4 FRTA20WE E23EA 20031218001452003121800145NM 2003 12 18 P5CA0301002 120031202A27811267629 PDU BOEING747 74747UF 1384949NM NR 3 MALFUNCTIONED A P5CAO OTHER J WARNING INDICATION LDLANDING 1 WP23496MC 29257 STATUS MESSAGE L/E MULTIDRIVE. REPLACED NR 3 L/E PDU, OPS CHECK NORMAL PER MM 27-81-00. 2L74 4F RT1384945 20031218001462003121800146WP 2003 12 18 ARWA20031106 120031128A3260 UPLOCK SENSOR LKHEED1011 1011385115 5265015WP LT MLG OUT OF ADJUST A ARWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19308GB 193U1133 THE RED LANDING GEAR DOOR AND INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION AND THE LT GEAR ON DOOR LIGHT ON THE F/E PANEL REMAINED ON. SHIMMED AND RESECURED MAIN LANDING GEAR LT DOOR UPLOCK SENSOR IAW MM 32-61-07. GEAR SWING OPERATIONAL CHECK GOOD IAW MM 32-30-00. 2L73 4F A23WE 20031218001482003121800148NM 2003 12 18 0300076 120031113A533085320313 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE BUCKLED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07914HA 53 A/C SUFFERED HARD LANDING RESULTING NUMEROUS AREAS OF BUCKLED FUSELAGE SKIN ON LHS. REPAIR IS TO HEAVY WINDOW BETWEEN THE F/SPAR AND R/SPAR. 2H72 4T RTA13NM 20031218001502003121800150NM 2003 12 18 F3LA200300155 120031130A5270DHE1141 PROXIMITY SWITCH AIRBUSA319 A319111 3930336NM R1 DOOR INOPERATIVE A F3LAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03912FR 4207 1803 FLIGHT CREW REPORTED R1 DOOR OPEN INDICATION IN FLIGHT. COMPLETED ECAM PROCEDURES. DIVERTED TO IND AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECK OF R1 DOOR PER MM 52-71-00-801. NO DEFECTS NOTED. PLACARD AS PRECAUTIONARY MEASURE PER MM 52-70-01B. PERFORMED OVERWEIGHT LANDING INSPECTION PER WORK CARD MP055104. NO DEFECTS NOTED. VISUALLY CHECKED DOOR WAS CLOSED AND LOCKED AT DEPARTURE. UPON ARRIVAL IN DEN, REPLACED F1 DOOR SLIDE ARMED HANDLE PROXIMITY SWITCH 4WN2 AND R1 DOOR PROXIMITY SWITCH 13WV2 PER MM 52-71-11. OPS CHECKED NORMAL AND PLACARD WAS REMOVED. 2L72 4F RTA28NM 20031218001542003121800154NM 2003 12 18 03FDEA02042 120031204A523052FX502 BELLCRANK BOEING727 727100 1384036NM ZONE 800 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25168FE 18865 COMPLY WITH EA 7-5230-73854A DOOR MAIN CARGO DOOR TORQUE TUBE ELONGATED HOLES REPAIR BS 489 THROUGH BS 610. COMPLIED WITH EA 7-5230-73854A DOOR-MAIN CARGO DOOR TORQUE TUBE ELONGATED HOLES REPAIR BS 489 THRU BS 610, AT MAE. 2L73 4F RTA3WE 20031218001632003121800163NM 2003 12 18 MWEA030462 120031203A53205930544133 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FLOORBOARD SUPPORT Z-CHANNEL AT FRAME STATION 256 IS CORRODED BETWEEN SEAT TRACK NR 3 AND 4. FABRICATED AND INSTALLED FLOOR SUPPORT. 2L72 4F RTA6WE 20031219000012003121900001WP 2003 12 19 CALA0300693 120031205A5320991186021N ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 FRAME AT STA 1451 UNDER RIGHT VERTICAL ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED FORMER PER SRM 51-10-1. 2L72 4F A6WE 20031219000032003121900003WP 2003 12 19 CALA0300695 120031205A53159936580505 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 INTERCOSTAL BETWEEN STA 1287 AND 1309 CABIN FLOORBEAM CRACKED AT CLIP NUTS. INSTALLED INTERCOSTAL STA 1287 - 1309 AFT BAG BIN CABIN FLOORBEAM PER SRM 51-30-0. 2L72 4F A6WE 20031219000042003121900004WP 2003 12 19 CALA0300696 120031203A53159936580515 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 INTERCOSTAL BETWEEN STA 1271 - 1287 CABIN FLOORBEAM CRACKED AT CLIP NUTS. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 FIG 2 SHEET 4. 2L72 4F A6WE 20031219000072003121900007WP 2003 12 19 ABXA030454 120031114A531159114481 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 LEVEL II CORROSION OF FRAME FS 218, LONGERON 28 LT. REMOVED DAMAGED FRAME AND INSTALLED NEW SECTION OF FRAME STA 218, LONGERON 26 LT LONGERON 26 RT IAW DC-9 SRM 53-03. 2L72 4F A6WE 20031219000092003121900009WP 2003 12 19 ABXA030458 120031204A3310 LIGHT DOUG DC9 DC941 302207NWP COCKPIT SHORTED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23951AX 47616 ODOR OF WIRES BURNING FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPED, AND LOSS OF THOSE LIGHTS. ODOR WENT AWAY. CAPTAIN'S MAP LIGHT LENS ASSEMBLY SHORTED ON MOUNTING PLATE. REPOSITIONED AND SECURED LENS ASSEMBLY. OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 20031219000112003121900011WP 2003 12 19 ABXA030456 120031114A532059516853 FITTING DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 LONGERON 29 LEFT END FITTING CRACKED ON OUTBOARD SIDE FS 756. REPAIRED LONGERON 29 LEFT AT STA 756 IAW DC-9 SRM 53-02. 2L72 4F A6WE 20031217001182003121700118EU 2003 12 17 USAABA03039 120031114A2910A253130021 SELECTOR VALVE AIRBUS330 A330323 3930335EU RT MLG WW MALFUNCTIONED A USAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA19675US 0370 UPON TAXIING TO THE GATE AFTER LANDING, THE BRAKES HAD NO RESPONSE UNTIL FULLY DEPRESSED. CREW REPORTED A NORMAL BRAKE INOP MESSAGE. MAINTENANCE FOUND THE NR 2 BSCU BLANK. THE BSCU WAS RESET. BITE FAULTED TEH SELECTOR VALVE. THE BSCU AND VALVE WERE PROGRAMMED FOR REPLACEMENT. ON NOV 15, FLT 781, MAXIMUM BRAKES WERE NEEDED BEFORE ANY BRAKING RESPONSE WAS NOTED. BOTH THE BSCU AND NORMAL BRAKE SELECTOR VALVE WERE REPLACED. (M) 2L72 4F RTA46NM 20031217001952003121700195EU 2003 12 17 AWXA200301488 120031124A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU SEAT ROW 11 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031218000032003121800003NM 2003 12 18 03FDEA01981 120031125A534053FX14282 FITTING BOEING727 727200 138407ENM ZONE 800 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25257FE 20939 COMPLY WITH EA 7-5340-73853 FUSELAGE FITTINGS MAIN CARGO DOOR UPPER JAMB LIFT FITTING GOUGES. COMPLIED WITH EA7-5340-73853 DATED 11/20/03 FUSELAGE FITTINGS MAIN CARGO DOOR UPPER JAMB LIFT FITTING GOUGES. 2L73 4F RTA3WE 20031218000532003121800053NE 2003 12 18 NACA20030124 220031128A8500R2800 ENGINE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 1 MAKING METAL A NACAE ENGINE SHUTDOWN RK PARTIAL RPM/PWR LOSS FLUID LOSS CLCLIMB 1 AL03779TA406 406 45529 CP450668 NR 1 ENGINE PRECAUTIONARY SHUT DOWN DUE TO DOUBLE SHORTED SECONDARY AND LOSS OF OIL. REPLACED NR 1 ENGINE DUE TO MAKING METAL. 2L74 4R4 R A781 5E8 20031218000782003121800078NM 2003 12 18 2003UALA00859 120031116A3397 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT WORN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29656UA 25394 EMERGENCY EXIT LIGHTS - FLOOR STRIPS ON. ALSO FLASHING ON AND OFF. FOUND SEVERAL LOCATIONS WHERE STRIP WAS TORN AND PINS PUSHED IN. REPAIRED WITH SPLICE TOOL. OPS CK NORMAL. 2L72 4F4 FRTA1NM E24NE 20031218000982003121800098EU 2003 12 18 2003UALA00886 120031123A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29403UA 442 AFT PIT STRINGER 43 LT CORRODED BETWEEN FRAMES 56 & 57. MAJOR REPAIR ACCOMPLISHED. EXTRUDED STRINGER REPAIR. 2L72 4F4 FRTA28NM E40NE 20040114001792004011400179SO 2004 1 14 MASA200300415 120031017A2560P2070003001 FLASHLIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07831MJ 145273 ASH- 2615 CLT. FA FWD FLASHLIGHT INOPERATIVE, REPLACED FLASHLIGHT. 2L72 4T RTT00011AT 20040114001832004011400183EA 2004 1 14 MASA200300497 120031217A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775996 7357 ASH NR 2687 MGM-CLT. CAPT REPORTED THE LT HAND REAR OVERWING EMERGENCY EXIT LIGHT INOP. MECHANIC RELAMPED. OP CHECKS GOOD 2L72 4F RTA21EA 20040114002302004011400230NM 2004 1 14 03289451 120031016A21504068B000002 CONTROL VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE A/C SYSTEM MALFUNCTIONED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27451FJ 3205 DURING ENGINE START THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE AIR FLOW CONTROL VALVE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T4 FRTA55NM E35NE 20040115000272004011500027NE 2004 1 15 SW07200300006 220030611A72504120T0P02 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE MISSING G FDKAO OTHER O OTHER NRNOT REPORTED 1 SW07508MJ672 10087 GEE965400 WHILE INVESTIGATING A HIGH PEAK VIBRATION WHICH WAS DISCOVERED BY ECTM, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPE INSPECTION AND FOUND BLADES MISSING FROM THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL. 2L72 4F4 FRTA21EA EOOO63EN 20040115001262004011500126NM 2004 1 15 03FDEA02104 120031207A1430ARC7053503 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM51-33-01 VOL 2 2L73 4F RTA22WE 20040116000012004011600001NM 2004 1 16 03FDEA02167 120031211A5533 STRINGER BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 VERTICAL FIN STR 8L AT FIN STA 157 IS CRACKED. REPAIRED CRACK IN STRINGE 8 LT AT FIN STA 157 PER SRM 55-30-4 FIG 1. 2L73 4F RTA3WE 20040116000062004011600006CE 2004 1 16 DXTA200300178 120031209A3240 ACCUMULATOR CESSNA500 560CESSNA 2076750CE MLG BRAKE SYS LOW E DXTAO OTHER WJ INADEQUATE Q C WARNING INDICATION LDLANDING 1 GL07358QS 5600455 ON LANDING AT LAS POWER BRAKE ACCUMULATOR AND ANTI-SKID ANUNCIATORS ILLUMINATED, BRAKES WERE INOP ON LANDING. AIRCRAFT CAME TO REST WITHOUT INCIDENT. SERVICED BRAKE ACCUMULATOR IAW CESSNA CITATION 560 MM CHAPTER 12-12-02, BLED BRAKES IAW CHAPTER 32-42-00, OPERATIONAL CHECK OF BRAKE AND ANTI-SKID SYSTEM SATISFACTORY ON TAXI CHECK. 2L72 4F RTA22CE 20040116000122004011600012SO 2004 1 16 DXTA200300192 120031129A2710666000161 CONTROL CABLE GRUMAVG21 G21A 3951204SO AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07641 B115 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 1H72 3R TC654 20040120000152004012000015NM 2004 1 20 03FDEA02218 120031217A5320AWE95172 CHANNEL DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN CARGO DECK RIGHT STA 735 TO STA 755 HAT SECTION BEHIND BUMPER STRIP DAMAGED. MAIN CARGO DECK RT STA 735 TO STA 755 HAT SECTION REMOVED AS PER SRM 51-35-01, VOL.II AND NEW HAT SECTION INSTALLED AS PER SRM 51-35-01, VOL.II & MM 20-50-02. 2L73 4F RTA22WE 20031124000792003112400079NM 2003 11 24 QXEA200301431 120031116A2130 PROXIMITY SWITCH BOMBDRDHC8 DHC8401 1390041NM ZONE 100 FROZEN A QXEAO OTHER O OTHER CLCLIMB 1 NM09400QX 4030 ON FLIGHT 2347 DURING CLIMB AT 10500 FT CABIN LOST PRESSURIZATION FOR 30 SECONDS THEN WORKED NORMALLY. IAS 220K AND OAT -8 DEGREES. SUSPECT FROZEN PROXIMITY SWITCH TEMP. CLEANED AND LUBED SWITCH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031124000852003112400085WP 2003 11 24 DHL2003807536 120031026A5280 SKIN DOUG DC8 DC873F 302199FWP LT MLG DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT MLG DOOR LOWER PART INTERNAL SKIN CRACKED 1.000 AT STA 910.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER IAW SRM 52-2-0 PG 1, 2. PERFORMED HEAT TREATMENT TO DOUBLER IAW SRM 51-1-1. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-1-21A PG 3. 2L74 4F RT4A25 20031124000902003112400090WP 2003 11 24 DHL2003807554 120031103A5720 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NR 3 MAIN TANK INTERIOR FITTING CRACKED STA XRS 22.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM PO201734, DWG 5615910. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW FITTING IAW ATM PO201734, DWG 5615910. HEAT TREATED NEW FITTING IAW SRM 51-1-1. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND APPLIED FUEL COATING MATERIAL IAW SRM 51-1-12 PG 12. INSTALLED FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-3-1 PG 1, 2. REFER TO NR 1482 FOR LEAK CHECK. 2L74 4F RT4A25 20031124000912003112400091WP 2003 11 24 DHL2003807556 120031106A2720 DRUM DOUG DC8 DC873F 302199FWP RT MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT MLG W/W FLAP TO RUDDER SYSTEM DRUM BASE CRACKED. REMOVED AND REPLACED HOUSING ASSY ON RIGHT MLG W/W FLAP TO RUDDER SYSTEM IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. ADJUSTED FLAP TO RUDDER SYSTEM IAW MM 27-50-0 PG 508-513. FOR OPS CHECK SEE NR 2035. 2L74 4F RT4A25 20031124000962003112400096WP 2003 11 24 DHL2003805590 120030806A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS.635.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031124001002003112400100WP 2003 11 24 DHL2003805501 120030813A5314 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 KEEL BEAM LWR SECTION CLIP 0.500 CRACKED, STA 960.000. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG 21. FABRICATED CLIP (EXTRUSION LS4031) IAW SRM 53-2-0 PG 2E, 2F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CLIP ON KEEL BEAM, STA 960.000 IAW SRM 53-2-0 PG 2E, 2F SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031218000992003121800099EU 2003 12 18 2003UALA00887 120031123A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29403UA 442 FUSELAGE SKIN DENTED FROM FRAME 23 TO FRAME 24 BETWEEN STRINGERS 21L & 23L. DIMENSIONS ARE LENGTH 24.8 INCHES BY 10 INCHES HEIGHT WITH 5 SMALLER SHARP EDGES. MAJOR REPAIR ACCOMPLISHED. REPLACED STR 22L & FABRICATED EXTERNAL DOUBLER REPAIR UTILIZING SHIMS & FILLERS. 2L72 4F4 FRTA28NM E40NE 20031218001162003121800116NM 2003 12 18 2003UALA00907 120031125A5320 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29370UA 24539 STA 194 RT WEB CRACKED AT STR 17. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20031218001582003121800158NM 2003 12 18 QXEA200301514 120031201A21404100S02801 HEATER BOMBDRDHC8 DHC8401 1390041NM ZONE 400 FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09403QX 4037 ON FLIGHT 2370 DURING TAXI OUT STRONG ODOR PRESENT IN COCKPIT AND CABIN. NR 1 ENGINE ADAPT HEAT CAUTION LIGHT CAME ON AND FOUND INTAKE LIP HEATER ENGINE 1 CIRCUIT BRAKER POPPED. REMOVED AND REPLACED NR 1 ENGINE INTAKE HEATER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031218001672003121800167NM 2003 12 18 03FDEA02048 120031204A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 FRAME AT BS 950D BETWEEN STR 26-27 LT HAS HOLE IN UPPER FLANGE RADIUS. 2L73 4F RTA3WE 20031219000472003121900047NM 2003 12 19 SWAA032607 120031126A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C4 CHECK, FOUND 3 INCH LONG FUSELAGE SKIN CRACK AT BS 967, BELOW STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031219000542003121900054NE 2003 12 19 C1HA200396020 220031205A7261 ENGINE BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE LEAKING A C1HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15696CA OIL QUANTITY DECREASED TO .1 GALLONS IN FLIGHT. OIL TEMP 112 AT POWER PRESSURE 49. AIRCRAFT DIVERTED INTO DFW. MAINTENANCE FOUND OIL COMING OUT OF THE COMBUSTION DRAIN, ENGINE CHANGE IN PROGRESS. 2L73 4F4 FRTA3WE E2EA 20031219000582003121900058WP 2003 12 19 UPS03841641 120031118A53403779762U501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 680 LONG 6R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20031219000732003121900073NM 2003 12 19 AWXA200301515 120031111A5530BAC15063124 BEAM BOEING757 7572G7 1384963NM VERTICAL STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28908AW 24233 DURING C-12 CHECK 2 EACH CRACKS WERE FOUND ON VERTICAL STABILIZER TRAILING EDGE BEAM AT RT SIDE OF YAW DAMPER CAVITY INTERIOR, APPROXIMATELY RIB STA 100. MAINTENANCE REMOVED CRACKED SECTION OF VERTICAL STABILIZER BEAM AT RT SIDE OF YAW DAMPER CAVITY INTERIOR, RS 100; FABRICATED A NEW SECTION OF REPLACEMENT BEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG 1-6, FIG 1. 2L72 4F RTA2NM 20031219000762003121900076SO 2003 12 19 C2XA03TY204 120031207A574114522141407 TIE ROD EMB 135 EMB135ER 3260203SO RT WING ROOT CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717507 145215 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND WING TO FUSELAGE TIE ROD ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE TIE ROD IAW EMB IC 2003-145/4092. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031219000792003121900079WP 2003 12 19 MWEA030474 120031205A575459267474 SLAT TRACK DOUG DC9 DC932 3022066WP WING BROKEN A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31202ME 47672 SLATS WERE RETRACTED, THE AMBER SLAT DISAGREEMENT LIGHT STAYED ON. FOUND SLAT TRACK DOOR AT NUMBER TWO AND NUMBER THREE SLAT JUNCTION BENT AND BROKEN. REMOVED AND REPLACED SLAT TRACK DOOR. 2L72 4F A6WE 20031219000822003121900082EU 2003 12 19 2003UALA00808 120031028A2133VFT300A1 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29402UA 439 RETURN TO FIELD DUE TO INABILITY TO PRESSURIZE AIRCRAFT. REPLACED FAULTY SKIN AIR OUTFLOW VALVE. 2L72 4F4 FRTA28NM E40NE 20031219000892003121900089NM 2003 12 19 2003UALA00917 120031130A5330 SKIN BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29620UA 21880 AFT CARGO PIT AT BS 1080-1087 BETWEEN STR 37L- 38L, SKIN IS CORRODED AROUND DRAIN FITTING. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2L72 4F4 FRTA1NM E3NE 20031219000972003121900097NM 2003 12 19 2003UALA00926 120031128A2121 FAN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN ODOR A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29181UA 25278 ELECTRICAL BURNING ODOR WITH ASSOCIATED STATUS MESSAGE RECIRC FAN UPPER L DISPLAYED. THE UPPER RIGHT RECIRCULATION FAM MOTOR BEARINGS FAILED.THE RECIRCULATION FAN WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 20031219001062003121900106NM 2003 12 19 2003UALA00936 120031203A3350 WIRE HARNESS BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29645UA 25280 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT NEAR GALLEY 402. ACCOMPLISHED WIRE BUNDLE REPAIR PER MM 33-51-10-301. DEVICE WORKS FINE. 2L72 4F4 FRTA1NM E24NE 20031219001072003121900107NM 2003 12 19 2003UALA00937 120031204A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 TWO DENTS LT FUSELAGE AT STA 606, STR 15L AND 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031124001052003112400105WP 2003 11 24 DHL2003805553 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING INBD L/E FORMER CRACKED 0.500, STA XFS 610.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LEFT OUTER WING INBD L/E XFS 610.000 IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031124001092003112400109WP 2003 11 24 DHL2003805537 120030728A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 803.750. REMOVED FASTENERS IAW SRM 51-1-21G PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. REFER TO NR 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031124001172003112400117WP 2003 11 24 DHL2003802524 120031113A53203750257U1 SPLICE DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT SPLICE FITTING 3.000 CRACK (STA1040.000-1060.000, L-31R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACK SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 1. 2L74 4F RT4A25 20031124001232003112400123WP 2003 11 24 DHL2003802511 120031115A5712 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING L/E FORMER CRACKED 0.500, STA 810.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031124001272003112400127NM 2003 11 24 GAIA03141ST 120031024A5320 FLOOR SUPPORT BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CRACKED AT BS 950F RBL 8. REF FASI N/R NR 61698, ACCOMPLISHED ANGLE REPAIR IAW B727 SRM 51-40-3. INSTALLED DOUBLER, CHANNEL PER B727 SRM 51-40-3 BS 950F - 970. (M) 2L73 4F RTA3WE 20031124001282003112400128NM 2003 11 24 GAIA03137ST 120031024A5311 FRAME BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME CRACKED BS 480 LEFT SIDE IN AREA OF SILL BEAM. REF FASI N/R NR 61678, CUT OUT DAMAGE AND INSTALLED REPAIR PER B727 SRM 53-10-4 FIG 11. (M) 2L73 4F RTA3WE 20031124001352003112400135NM 2003 11 24 AALA20031108 120031008A2120 SMOKE BOEING767 767323 1385205NM CABIN DETECTED A AALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21390AA 27450 DFW - FLT 1941 - EN ROUTE DFW-LAS, CREW OBSERVED SMOKE IN THE CABIN. EMERGENCY DECLARED AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT NOT OVERWEIGHT. PERFORMED OPERATIONAL CHECKS ON CHILLERS, OVENS, READING LIGHTS, SIDE AND CEILING LIGHTS, VIDEO CAMERAS, ALL ELECTRICAL COMPONENTS LEFT ON FOR 36 HOURS. RAN BOTH ENGINES TO TAKEOFF N1 ISOLATED BLEED AND PACKS, SWITCH BACK AND FORTH BETWEEN APU AIR AND ENGINE AIR. TEMPERATURES WERE RUN FROM FULL COLD TO FULL HOT, SUPPLIED FROM EARLIER ENGINE. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031124001422003112400142EA 2003 11 24 03673 120030725A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE DAMAGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27673BR 7599 DURING HEAVY INSPECTION MULTIPLE REDUNDANT HOLES AND GOUGES WERE FOUND IN THE AFT PRESSURE BULKHEAD AT FS621. DAMAGE WAS REPAIRED IAW REO 601R-53-61-748. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031124001522003112400152NM 2003 11 24 QXEA200301282 120031008A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-LEFT INBOARD TRACK NR 5 SEAT ATTACH AREA CORROSION BETWEEN INBOARD X487.00. REPAIRED IAW RD8-53-1339. 2H72 4T4 TRTA13NM E20NE 20031124001542003112400154NM 2003 11 24 QXEA200301222 120031001A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE LAVATORY FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09365PH 526 SEA- LAVATORY SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031124001592003112400159NM 2003 11 24 QXEA200301281 120031007A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-LT INBOARD TRACK NR 6 HAS CORROSION AROUND NUT PLATE AT STATION X564.00 AND X580.00. REPAIRED IAW RD8-51-103 AND SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20031125000092003112500009WP 2003 11 25 DHL2003805515 120030807A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 347.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS ON LEFT WING CTR L/E FORMER AT STA XFS 347.750 IAW SRM 57-2-0 PG 9, 10 SRM 51-1-21 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031121000602003112100060CE 2003 11 21 AMWA82 120031015A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE23 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED ON THE LEFT SIDE NEAR THE FWD STRINGER INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031121000722003112100072NM 2003 11 21 C1HA20039701 120031112A3350 CHARGER BOEING727 727270 138408PNM EMER LITE BATT FAILED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 EMERGENCY LIGHTS OUT BETWEEN ROW 11 TO ROW 20. REMOVED & REPLACED BATTERY CHARGER PER M/M 33-50-01. OPS CHECK GOOD. P/N 11-0049 2L73 4F RTA3WE 20031121000742003112100074NM 2003 11 21 UPS03M41567 120031115A2612 DETECTION SYS DOUG MD11 MD11F 3023600NM NR 2 FIRE MALFUNCTIONED A IPXAK NONE N FALSE WARNING ININSP/MAINT 1 SO01273UP 48574 DURING APU FIRE TEST NR 2 ENG FIRE HANDLE ILLUMINATED AND WOULD NOT EXTINGUISH. T/S SYS PER FIM 26-11-00 PG 106-111. CLEANED AND SECURED ASSOCIATED CONNECTORS. INSPECTED NR 2 PYLON JUNCTION BOX. NO DEFECTS NOTED IN THIS AREA. OPS CKS GOOD. 2L73 4F RTA22WE 20031219001132003121900113NM 2003 12 19 03FDEA02058 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD BORE CORRODED. OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001442003121900144NM 2003 12 19 03FDEA02127 120031208A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25276FE 22041 CORROSION AFT CARGO BAY LEFT KEELBEAM LWR O/B FLANGE BS 1000, STR 29L . FOUND CORRODED KEELBEAM OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STR 29L KEELBEAM IAW FED EX EA 7-5330-55160. 2L73 4F RTA3WE 20031219001482003121900148NM 2003 12 19 03FDEA02132 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT POINT BORE CORRODED. LT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT POINT BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73359 WINGS -TRAILING EDGE & TRAILING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031219001512003121900151NM 2003 12 19 03FDEA02137 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LINK SPOT FACE CORROSION REMOVED & FOUND WITHIN LIMITS AS PER CMM 57-44-08 & DRAWING ARC0502, AND EA 1-5750-73357, TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031219001542003121900154NM 2003 12 19 03FDEA02140 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. O/B FLAP I/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73357 WINGS. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031219001592003121900159NM 2003 12 19 03FDEA02145 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE BORE CORRODED. WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT, OUTBOARD HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73358, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031219001612003121900161NM 2003 12 19 03FDEA02147 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING, INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT BEARING HOUSING, SPOT FACE CORRODED. I/B FLAP O/B HINGE (WING SIDE) PIVOT BEARING HOUSING SPOT FACE CORROSION REMOVED AS PER FEDEX EA 1-5750-73360 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031219001692003121900169NM 2003 12 19 QXEA200301506 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 1 SEAT TRACK HAS DAMAGED LUGS FROM 2 TO 5 INCHES AFT OF X387. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031219001752003121900175EU 2003 12 19 MALA030521 120031202A302044730501 CONTROL MODULE SAAB SF340 SF340A 7850100EU DEICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15110XJ 340A110 DURING FLIGHT 3183, LEFT INTAKE CAUTION LIGHT ILLUMINATES, MOVING POWER LEVER WILL EXTINGUISH LIGHT FOR APPROXIMATELY 2 MINUTES THEN COMES ON AGAIN. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED DEICE CONTROL MODULE (LT) P/N44730-501, S/N OFF A0072, S/N ON A00301. OPS CHECK GOOD. 2L72 4T RTA52EU 20031219001792003121900179EU 2003 12 19 MALA030528 120031128A2131 CONTROLLER BAC 146 AVRO146RJ85A1500097EU CABIN PRESSURE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15513XJ E2329 DURING FLIGHT 3405, CREW REPORTS WHITE AND AMBER PSI LIGHT ON AT 23000 FT. AIR RETURN TO MSP. MAINTENANCE REPLACED CONTROLLER FOR PRECAUTION P/N 304A000-003 (OFF), P/N 3040A000-004, S/N OFF 0032, S/N ON 0007, OPS CHECK AND INSTALL IAW 21-30-02. 2H74 4F RTA49EU 20031219001822003121900182EU 2003 12 19 MALA030529 120031124A3350 SWITCH SAAB SF340 340B 7860101EU EMERGENCY LIGHT STUCK A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15410XJ 340B410 EMERGENCY LIGHT SWITCH STUCK IN ARMED POSITION. MAINTENANCE REPLACED PANEL P/N 7239050-802. OPS CHECK GOOD. 2L72 4T RTA52EU 20031217001282003121700128WP 2003 12 17 ABXA030470 120031202A5310401559198 DOOR FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23960AX 47762 CRACKS EMANATING FROM OPEN HOLE ON LEFT AFT EMERGENCY DOOR JAMB LOWER WEB AT FS 711 BETWEEN LONGERONS 16 AND 17 LEFT. INSTALLED DOUBLER REPAIR IAW DC-9 SRM 51-30-2 AND REPAIRED AREA IAW DC-9 53-01. 2L72 4F A6WE 20031217001522003121700152NM 2003 12 17 SWAA032719 120031211A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 727, BS 767, BS 787 AND LBL 9, LBL 18, LBL 4 THROUGH RBL 4. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031217001602003121700160EU 2003 12 17 AWXA200301533 120031212A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 241 FAULTY A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28650AW382449943 856 LT OVERWING EMERGENCY POWER SUPPLY UNIT INDICATES INTERNAL FAULT. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031217001722003121700172NM 2003 12 17 SWAA032646 120031202A53106546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND 2 EACH SHEAR TIES CORRODED AT BS 747 AND 827, RBL 1 AND RBL 5, BOTH AT WL 147. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20031217001792003121700179NM 2003 12 17 DHL2003721011 120031125A3350 LIGHT BOEING727 727228 1384083NM CABIN BROKEN A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01721DH 19545 EMERGENCY EXIT LIGHT BROKEN. REPLACED EMERGENCY EXIT LIGHT IAW B-M/M 33-50-01. OPS CHECKED GOOD. REMOVED FROM A/C 753 IN SERVICEABLE CONDITION. 2L73 4F RTA3WE 20031217001812003121700181EU 2003 12 17 MALA030506 120031122A242031342003 GENERATOR SAAB SF340 340B 7860101EU LT AC FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15444XJ 340B444 DURING FLT, LT INTAKE HEAT CAUTION LIGHT ILLUMINATED. LEFT INTAKE CAUTION LIGHT ON. RECYCLED SWITCH. CWP ICEPROT LIGHT REMAINS ON EVEN WITH SWITCH OFF AND LEFT INTAKE LIGHT. LIGHT TURNS ON AS SOON AS SWITCH IS SELECTED. AIR RETURN TO ABR. MAINTENANCE REPLACED LT AC GEN P/N 31342-003, S/N ON Y0048 OFF98032. REPLACED LT PROP ON DRAWING 15887/87 OFF DAP0074 REFERENCE 409 CARD 215429 FOR DETAILS. OPS CHECK GOOD. RELAMPED, OPS AND SECURITY CHECKS GOOD. REMOVED AND REPLACED LT AC GEN P/N 31342-003, S/N ON Y0048 OFF 98032 IAW JC 242102, OPS CHECKS GOOD. 2L72 4T RTA52EU 20031217001892003121700189SO 2003 12 17 SWIA200312608 120031111A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT FAILED A SWIAO OTHER O OTHER CRCRUISE 1 NM07220SW7057 7057 120288 F/A REPORTS THAT 3 TIMES DURING THE FLIGHT SOME OF THE EMERGENCY LIGHTS ILLUMINATED FOR 30-60 SEC BEFORE GOING OUT. NO ABNORMAL INDICATIONS IN THE COCKPIT. REPLACED FORWARD ELBP BATTERY PACK. OPS CHECKS GOOD. S/N OFF: 1041-02/92. 2L72 4T RTA31SO 20031218000972003121800097EU 2003 12 18 2003UALA00885 120031122A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29403UA 442 AFT CARGO COMPARTMENT STRINGER 42 LEFT CORRODED BETWEENN FRAMES 59 & 60. MAJOR REPAIR ACCOMPLISHED. EXTRUDED STRINGER SPLICE REPAIR. 2L72 4F4 FRTA28NM E40NE 20031218001322003121800132NM 2003 12 18 CALA0300685 120031202A5510697203932 BUSHING BOEING737 737524 1384721NM HORIZONTAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916649 28910 CORROSION ON FORWARD LOWER HORIZONTAL STAB CENTER SECTION LUG ON AFT CLEVIS ON AFT FACE AT BUSHING. REMOVED AND REPLACED BUSHING PER SOPM 20-50-03. 2L72 4F RTA16WE 20031219000252003121900025CE 2003 12 19 56120 120031113A3210 SWITCH BEECH 1900 1900D 1154162CE MLG VALVE DIRTY A AMWAO OTHER J WARNING INDICATION APAPPROACH 1 CE07173YV UE173 DURING LANDING APPROACH MAIN LANDING GEARS FAILED TO EXTEND. THE CREW MANUALLY PUMPED DOWN THE GEARS. RECEIVED 3 GREEN INDICATIONS, LANDED WITH NO FURTHER INCIDENTS. CLEANED CONTACT ON SERVICE VALVE SWITCH. 2L72 4T RTA24CE 20031219000352003121900035EA 2003 12 19 SWIA200312637 120031128A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07961SW 7857 STAB CHANNEL 1 INOPERATIVEDL2428M4 STATUS MESSAGE UPON EXTENSION OF FLAPS, WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU PER CRJ MM 27-40-00. 2L72 4F RTA21EA 20031219000662003121900066WP 2003 12 19 CALA0300700 120031206A5342 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716806 49260 INSPECTION FOUND A 2.75 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1474. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23B. 2L72 4F A6WE 20031219001112003121900111NM 2003 12 19 03FDEA02055 120031205A5310 SHEAR TIE BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25198FE 19154 CRACKED SHEAR TIE AT BS 336 WL 124 LBL 16 INSIDE TORQUE BOX. *S/D* REMOVED AND REPLACED SHEAR TIE AT BS 336, LBL 16, WL 124 PER SRM 51-20-1, 51-30-2, MM 51-20-021-7, 51-20-151-7. 2L73 4F RTA3WE 20031219001172003121900117NM 2003 12 19 03FDEA02062 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. 2L73 4F RTA22WE 20031222000082003122200008EU 2003 12 22 AWXA200301520 120031123A5414D54530052201 SKIN AIRBUS320 A320232 3930326EU NR 1 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 DURING C-06 CHECK CORROSION WAS FOUND ON INBOARD SKIN OF NR 1 PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED CORRODED SKIN PANEL FROM NAC STA 8370 TO NAC STA 9782, INBOARD; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG D54530052; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 1. 2L72 4F RTA28NM 20031222000212003122200021SO 2003 12 22 SWIA200312650 120031206A3397 TERMINAL EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DAMAGED A SWIAO OTHER P NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07237SW 120314 EXIT ROW 9 OVERHEAD BIN MOUNTED EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REPAIRED WIRE TERMINAL IN OVERHEAD. OPS CHECKS OKAY. 2L72 4T RTA31SO 20031222000262003122200026NM 2003 12 22 F3LA200300162 120031205A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CAP AT STA 986.5, LBL 45 TO RBL 12, UPPER AND LOWER SURFACES. REPLACED FLOORBEAM UPPER CAP PER EA B3-53R-10237. 2L72 4F RTA16WE 20031222000282003122200028NM 2003 12 22 QXEA200301528 120031207A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 NR 11 SEAT TRACK IS CORRODED BETWEEN X469 AND X473. REPAIRED IAW DHC-8 SRM 51-20-36. 2H72 4T RTA13NM 20031222000422003122200042NM 2003 12 22 0302136315 120031209A2530 SMOKE BOEING747 747451 1384940NM GALLEY DETECTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01675NW 33001 DURING FLIGHT, SMOKE EMITTED FROM THE NR 2 OVEN IN NR 1 GALLEY. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. RESET THE CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031222000752003122200075WP 2003 12 22 2003F00649 120030818A5320 FLOOR SUPPORT DOUG DC9 DC915F 3022037WP CARGO BAY CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 FOUND FORWARD AND AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLES, CRACKED AT STA'S 275, 294, 313, 370, 389, 427, 465, 661, 669, 680, 758, 786 AND 801. (M) 2L72 4F A6WE 20031222000782003122200078WP 2003 12 22 2003F00652 120030813A5751 SKIN DOUG DC9 DC915F 3022037WP LT WING AILERON DAMAGED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 FOUND C-CHECK SERVICE, LEFT WING AILERON UPPER SKIN WITH WEAR, STA 370, INBOARD HINGE. (M) 2L72 4F A6WE 20031222000822003122200082SO 2003 12 22 SIMA200332702 120031120A272015793101 PRESSURE SWITCH EMB 135 EMB135KL 3260302SO NR 2 RUDDER INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21827AE 145602 DURING CLIBM CREW REPORTED RUDDER SYSTEM 1/2 INOPERATIVE MESSAGE ON EICAS FOLLOWED BY A YAW DAMPNER FAIL. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031222000832003122200083WP 2003 12 22 AMTA200301413 120031121A3350 WIRE LKHEED1011 10113853 5265020WP EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EMERGENCY EGRESS PATH LIGHT FROM SEAT ROW 1HJK TO 5HJK INOPERATIVE. POWER SUPPLY LINE DISCONNECTED BETWEEN STRIPS RECONNECTED AND SECURED, OPS CHECK GOOD. (M) 2L73 4F A23WE 20031222000852003122200085WP 2003 12 22 MEX2003537 120031127A5270 SENSOR DOUG DC9 DC982 3022082WP E/E BAY DOOR DIRTY A ASMFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW23505MD 49149 FLIGHT RETURNED DUE TO THE 'E/E DOOR OPEN' LIGHT TURNED ON AFTER 15 MINUTES. DURING REVISION AT MLM STATION THE DOOR WAS FOUND CLOSED. THE MECHANISM, DOOR AND THE SENSOR WERE CLEANED, TESTS WERE PERFORMED IAW MM 52-30, ALL CORRECT. (M) 2L72 4F A6WE 20031222000932003122200093NM 2003 12 22 USAASB03198 120031108A3350210310005 FUSE BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US 23992 MAINTENANCE REPORTED THE AFT RIGHT EMERGENCY ESCAPE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TEH 5 AMP FUSE IN POWER SUPPLY M1479. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031222001042003122200104NM 2003 12 22 AMTA200301391 120031116A2612 CIRCUIT CARD BOEING757 75723N 1384973NM LT ENGINE FIRE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11523AT 30232 LT ENGINE FIRE LP-1 DISPLAYED. RERACKED AFOLTS CARD IAW FIM 26-11-00. RERACKED IAW AMM 26-10-01. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20031222001112003122200111SO 2003 12 22 SIMA200331401 120031108A27303631001005M0D ECU EMB 135 EMB135LR 3260305SO AVIONIC BAY INOPERATIVE A SIMAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SW21717AE 145272 DURING APPROACH, CREW REPORTED FLAPS FAILED TO DEPLOY WHEN LEVER SELECTED TO NINE DEGREES. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH ZERO FLAPS. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031218000522003121800052 2003 12 18 03328632 420031124A3444 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA RADAR ALTIMETER LOOSE A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27632BR 7268 DURING UNKNOWN PHASE OF FLIGHT THE SPOILERS WERE REPORTED DEPLOYING UNCOMMANDED. DURING TROUBLESHOOTING THE RADAR ALTIMETER TRANSCEIVER CONNECTOR WAS FOUND LOOSE CAUSING 50 FOOT ALTITUDE FLUCTUATIONS. THE CANNON PLUG WAS RESECURED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031218000862003121800086NM 2003 12 18 2003UALA00873 120031118A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29362UA 24455 STA 500D STR 25L FRAME HAS CORROSION ON UNDERSIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031218001442003121800144NM 2003 12 18 CALA0300688 120031203A3350252005 FUSE BOEING767 767224 1385170NM EMERGENCY LIGHT BLOWN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0968155 30434 AISLE LIGHT INOP AT ROW 29 THROUGH 37. REPLACED FUSE AT ROW 35 BATTERY CHARGER, OPS CHECK GOOD. 2L72 4F RTA1NM 20031219000502003121900050EU 2003 12 19 XNOA1170 120031206A2781 INDICATOR AIRBUS300 A300B4203 3930306EU SLATS MALFUNCTIONED A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23224KW 073 ON TAXI OUT NO SLAT EXTENDED INDICATION. VISUAL INSP OF SLATS CHECK GOOD ON GROUND AND INDICATOR IN COCKPIT WORKING NORMAL IAW A-300 AMM 27-15-00. 2L72 4F RTA35EU 20031219000682003121900068WP 2003 12 19 CALA0300702 120031207A5720 SPLICE DOUG DC9 DC982 3022082WP WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716806 49260 INSPECTION FOUND A 1 INCH CRACK IN WING SPLICE STRAP AT WING SPAR STA XRS 164 JUST O/B OF RIGHT VORTILION. THE WING SPLICE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2L72 4F A6WE 20031219001392003121900139NM 2003 12 19 03FDEA02120 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001642003121900164NM 2003 12 19 QXEA200301501 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 2 SEAT TRACK HAS LITE SURFACE CORROSION ON RIGHT HAND RAIL AND IN BOTTOM OF CHANNEL 8 TO 12 INCHES FORWARD OF STATION X510. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20031219001742003121900174NM 2003 12 19 QXEA200301526 120031201A5753 FLAP TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX- RIGHT HAND OUTBOARD FRONT SPAR FITTING AT FLAP TRACK NR 4 IS CHAFED. REPAIRED IAW Q400 RD 8/4-57-228. 2H72 4T RTA13NM 20031121000752003112100075NM 2003 11 21 03FDEA01949 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 RIGHT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING ACTUATOR HOLE O/B CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20031121000842003112100084WP 2003 11 21 ABXA030443 120031031A53205956034517 FLOOR SUPPORT DOUG DC9 DC914 3022034WP AFT CARGO BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 FLOOR SUPPORT STRAP, ATTACH ANGLE CRACKED, FS 768 AT LONGERON 27 RIGHT. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20031125000112003112500011WP 2003 11 25 DHL2003805520 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 461.372 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW RIVET AND HI-LOK IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000242003112500024EU 2003 11 25 DHL2003366515 120030521A7830 DRAIN AIRBUS300 A300B4203 3930306EU THRUST REVERSER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01336DH36541 249 NR 1 ENG INBOARD T/R UPPER RELIEF HOLE IS CRACKED, (TOP OF PYLON)=FWD RUBSTRIP. REMOVED DAMAGED AREA IAW A300 SRM 51-41-30. FABBED ANGLE AND FILLER IAW A300 SRM 51-41-30, ALODINED AND PRIMED ANGLE AND FILLER IAW A300 SRM 51-40-12. INSTALLED REPAIR IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20031125000312003112500031WP 2003 11 25 DHL2003805542 120030731A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING OTBD L/E SHOWS FORMER CRACKED, STA XFS 822.500 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10 SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000352003112500035WP 2003 11 25 DHL2003807551 120031024A53204640111U2 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NOSE SECTION INTERIOR RIGHT SIDE SHOW FITTING CRACKED 5.000, STA 8.000 - STA 12.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D, SRM 51-1-21, SRM 51-3-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000402003112500040WP 2003 11 25 DHL2003805529 120030807A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON LEFT CTR L/E FORMER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10 SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000512003112500051WP 2003 11 25 DHL2003802510 120031110A534774529523 CARGO TRACK DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT TRACK PLUG WORN, STA 684.000. REMOVED NR 4 TRACK PLUG, STA 684.000 IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000572003112500057WP 2003 11 25 DHL2003805525 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1-2. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS (02 EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 51-1-21 PG 1-2, SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000592003112500059WP 2003 11 25 DHL2003805583 120030806A5720 CLIP DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 CRACKED CLIP IN LEFT WING TO FUSELAGE INTERNAL STRUCTURE, STA 640.000 BETWEEN S-23L AND S-24L. REMOVED CRACKED CLIP IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW CLIP IAW SRM 53-2-0 FIG 1F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-3-0 PG 1, SRM 51-1-21. 2L74 4F RT4A25 20031125000602003112500060WP 2003 11 25 DHL2003802503 120031106A5712 FRAME DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING L/E UPPER FORMER CRACKED 0.500 AT STA XFS 431.000. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER IAW SRM 51-1-20D PG 9, SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031125000662003112500066WP 2003 11 25 DHL2003807507 120031007A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING CTR L/E FORMER 0.250 CRACK AT STA XFS 483.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER ON RIGHT WING CTR L/E FORMER AT STA XFS 483.750 IAW SRM 57-2-0 PG 9, 10 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000682003112500068WP 2003 11 25 DHL2003807534 120031024A572036169622 CLIP DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NR 4 MAIN TANK INTERIOR (1EA) CLIP CRACKED, STA XRS 172.000 S-76R (INSIDE ACCESS DOOR 505D). REMOVED AND REPLACED CRACKED CLIP IN NR 4 MAIN TANK STA XRS 172.000 S-76R (REF ACCESS DOOR 505D) IAW SRM 51-1-20D PG 21, 9. REFER TO NR 1482 FOR LEAK CHECK. 2L74 4F RT4A25 20031125000922003112500092NM 2003 11 25 PCAA0311140 120031117A2611PU90461S DETECTOR DHAV DHC8 DHC8102 2809003NM LAVATORY FAULTY A PCAAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING ININSP/MAINT 1 EA13806EX31573 263 WHILE AIRCRAFT 806EX WAS IN MANCHESTER NEW HAMPSHIRE CREW NOTED THAT THE LAVATORY SMOKE ALARM WAS ACTIVATED AND WOULD NOT EXTINGUISH. CREW THEN COMPLIED WITH MEL BY PULLING C/B AND PLACARD LAV AS REQUIRED. LATER LAQUARDIA MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE ALARM AND OPERATIONAL CHECK WAS GOOD. 2H72 4T RTA13NM 20031125000982003112500098NM 2003 11 25 QXEA200301413 120031104A5260 TRACK BOMBDRDHC8 DHC8401 1390041NM AFT AIRSTAIRS DIRTY A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09414QX 4061 SEA- ON FLIGHT 2292 FLIGHT ATTENDANT `B` REPORTS AFT STAIRS ARE DIFFICULT TO OPERATE. CLEANED SLIDE TRACKS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031125001012003112500101NM 2003 11 25 AALA20031290 120031117A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21790AN 30251 DFW AFT COACH SEATS EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT COACH SEATS EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031222000892003122200089WP 2003 12 22 AALA20030831 120030803A3230SS093200147001 BUNGEE CYLINDER DOUG DC9 DC982 3022082WP NLG DAMAGED A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21251AA 49270 EN ROUTE, AFTER LANDING GEAR RETRACTION THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED FOR 15-20 SECONDS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE BUNGEE CYLINDER. JACKED NOSE OF AIRCRAFT AND SWUNG NOSE GEAR SEVERAL TIMES. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031222001352003122200135NM 2003 12 22 UPS03241647 120031209A7330 WARNING LIGHT BOEING727 72751C 1384015NM NR 3 ENG FUEL ILLUMINATED A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01905UP 18947 NR 3 ENG FUEL FILTER WARNING LIGHT ILLUMINATED. 2L73 4F A3WE 20031222001392003122200139NM 2003 12 22 QXEA200301532 120031206A3060699009003 CONTROL UNIT BOMBDRDHC8 DHC8401 1390041NM PROP DEICE SYS INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09409QX5658 4051 SEA FLIGHT 2340 PROP DE-ICE CAUTION LIGHT ILLUMINATED IN ICING CONDITIONS. COMPLIED WITH CHECK LIST AND APPEARS THE NR 1 PROP HEAT WORKS NORMALLY, BUT THE NR 2 PROP HEAT NEVER CAME ON. REPLACED NR 2 TMCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031223000022003122300002NM 2003 12 23 03FDEA02160 120031205A2497 WIRE HARNESS DOUG MD11 MD11 3023602NM ZONE 400 IDG DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 NR 1 ENGINE PYLON IDG HARNESS NEAR YN = 315.5 FOUND DAMAGED. NR 1 ENGINE PYLON IDG HARNESS WIRE NR U01003-3/OC REMOVED AND REPLACED AS PER AMM 54-51-01-4 AND SWPM 20-10-01 AND NR 1 ENGINE POWER ASSURANCE CHECK CARRIED OUT AS PER AMM 71-00-00 FOUND 'SATIS'. 2L73 4F RTA22WE 20031223000172003122300017 2003 12 23 SWAA032659 420031203A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVACUATION SLIDE PRESS INDICATOR NOT VISIBLE. READJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031223000192003122300019 2003 12 23 SWAA032622 420031129A256522D22901 SLIDE BOEING737 7372H4 138448CNM L2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F A16WE 20031223000272003122300027NM 2003 12 23 SWAA032630 120031201A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND 3.4 LONG FUSELAGE SKIN CRACKED AT BS 415, STR 26L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031223000342003122300034NM 2003 12 23 SWAA032637 120031129A3350079123 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29753SW 29848 DURING SCHEDULED C2 CHECK, FOUND EELPS LIGHT COVERS CRACKED. REMOVED AND REPLACED EELPS TRACK COVERS PER MM. 2L72 4F RTA16WE 20031223000362003122300036NM 2003 12 23 SWAA032639 120031130A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20031223000512003122300051 2003 12 23 SWAA032672 420031207A256522D22901151 SLIDE BOEING737 7372H4 138448CNM L2 DOOR LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F A16WE 20031223000522003122300052NM 2003 12 23 SWAA032673 120031207A5313BAC1498 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27R CORRODED AT BS 947. REPAIRED STRINGER PER SRM. 2L72 4F A16WE 20031223000532003122300053NM 2003 12 23 SWAA032674 120031207A53306551625 SKIN BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947, STR 27R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031223000622003122300062NM 2003 12 23 ABXA030460 120031206A3350BPS73 BATTERY BOEING767 767281 1385109NM EMERGENCY LIGHT DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23784AX 23017 DURING MAINTENANCE INSPECTION, FOUND SPARE EMERGENCY BATTERY CHARGER INOP, LOWER UNIT. REPLACED EMERGENCY BATTERY CHARGER IAW AMM 33-51-00-210. OPS GOOD. 2L72 4F RTA1NM 20031223000672003122300067NM 2003 12 23 QXEA200301533 120031210A324021599 BRAKE DHAV DHC8 DHC8202 2809007NM ZONE 700 MISALIGNED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09358PH435 435 506 SEA - FLIGHT 2136 - BRAKES SHUDDERING WITH CONTINUOUS BUMPING DURING WHEEL ROTATION. THIS HAPPENED DURING SLOW TAXI ON RUNWAY FOR POSITION AND HOLD. MAINTENANCE INSPECTED THE WHEELS AND BRAKES AND FOUND THE NR 2 BRAKE ROTOR HAD JUMPED THE LUGS ON THE WHEEL ASSEMBLY. THE NR 2 WHEEL AND BRAKE WERE THEN REPLACED IAW THE MAINTENANCE TASK CARDS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031223000712003122300071NM 2003 12 23 03FDEA02171 120031211A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 STR 4 LT BS 720A STRINGER CLIP IS CRACKED. 2L73 4F RTA3WE 20031223000842003122300084NM 2003 12 23 VNAA0312003 120031205A3010 BOOT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT DEICE SYS FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07459PS 3070 DURING FLIGHT, THE CREW RECEIVED A LEFT HAND MIDDLE LEADING EDGE BOOT FAILING IN ALL MODES AND DIVERTED TO DAY. MAINTENANCE INSPECTED AND PATCHED THE LEFT HAND MIDDLE LEADING EDGE DE-ICE BOOT IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031223000952003122300095NM 2003 12 23 SWAA032706 120031210A5330AND10133 SKIN BOEING737 7372H4 138448CNM LWR FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED AT BS 227.8 AT CEILING OF NOSE WHEEL WELL. REPAIRED CHORD PER SRM. 2L72 4F A16WE 20031219000312003121900031EA 2003 12 19 SWIA200312633 120031128A2730DL2428M4 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA PITCH FEEL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07433SW6141 6141 7550 FLIGHT CONTROL MOVEMENT IS MUCH HEAVIER THAN NORMAL (PITCH). REPLACED CO-PILOT'S PITCH FEEL LINEAR ACTUATOR IAW CRJ MM 27-31-23. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031219000462003121900046NM 2003 12 19 SWAA032606 120031126A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C4 CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20031219000482003121900048CE 2003 12 19 DXTA200300177 120031204A3260 BULB CESSNA750 750 2076810CE MLG INDICATOR MALFUNCTIONED E DXTAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL07964QS 7500164 AFTER GEAR RETRACTION UNLOCK LIGHT STAYS ON. GEAR EXTENDS NORMALLY WITH NORMAL INDICATIONS, PILOT STATED, EN ROUTE TO HOU FROM DAL. DIVERTED INTO SAT AS A PRECAUTION. THERE WERE NO PASSENGERS ON BOARD AND NO EMERGENCY ACTION TAKEN. REMOVED 1 INOP BULB AND INSTALLED A NEW BULB, OPS CHECK GOOD. REF FAS WO 03-2256 FOR DETAILS. THIS ITEM IS STILL UNDER INVESTIGATION. 2L72 4J RTT00007WI 20031219000532003121900053NM 2003 12 19 C1HA200385013 120031207A3350 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 LEFT AFT LOWER BODY EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-21, OPS CK GOOD. 2L73 4F A3WE 20031219000572003121900057WP 2003 12 19 UPS03841640 120031117A534037558421 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 320 BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755824 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20031219000852003121900085EU 2003 12 19 2003UALA00913 120031128A5522 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT ELEVATOR CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29405UA 452 LT ELEVATOR HAD 3 AREAS OF WATER INGRESS. ALL AREAS ABOUT 1 INCH BY 1 INCH IN SIZE. TWO AREAS ON UPPER SURFACE: 1 LOCATED 98 INCHES FROM I/B EDGE & 2.5 INCHES FROM T/E, & 1 AT 177 INCHES FROM T/E & 10.5 INCHES FROM T/E, ONE AREA ON LWR SKIN 53 INCHES FROM I/B EDGE, & 4 INCHES FROM T/E. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 55-21-11 REP 5E, PG 226, FIG 205, SHEET 3 & 4. 2L72 4F4 FRTA28NM E40NE 20031219000942003121900094NM 2003 12 19 2003UALA00922 120031201A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29375UA 24640 CABIN SHEAR TIE CRACKED STA 597, STR 8L & 11L. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20031219001082003121900108NM 2003 12 19 2003UALA00939 120031204A5320 WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE THRESHOLD CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 AFT PIT CARGO DOOR CUTOUT THRESHOLD SILL WEB CORRODED UNDER THRESHOLD PLATE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED WEB REPAIR. 2L72 4F4 FRTA2NM E17NE 20031222000132003122200013EA 2003 12 22 SWIA200312642 120031118A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07908SW122 122 7540 AFTER TAKEOFF, FLIGHT SPOILER FAULT STATUS MESSAGE PERSISTED TO DESTINATION. REMOVED AND REPLACED RIGHT INBOARD FLIGHT SPOILERS PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECKS GOOD. 2L72 4F RTA21EA 20031222000432003122200043WP 2003 12 22 0302149150 120031205A213110256861 CONTROLLER DOUG DC9 DC914 3022034WP CABIN PRESSURE MALFUNCTIONED A NWAAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL018908E 45749 DURING CLIMBOUT ON DEPARTURE, THE OUTFLOW VALVE STARTED FLUCTUATING FULL OPEN TO FULL CLOSE. AT FL240, THE AIRCRAFT LOST PRESSURIZATION ACCOMPANIED WITH MASK DEPLOYMENT. ALL WARNING INDICATORS ILLUMINATED, AN EMERGENCY DESCENT WAS PERFORMED, AND THE FLIGHT RETURNED TO AN UNEVENTFUL LANDING AT MSP. MAINTENANCE REPLACED A LEAKING CABIN PRESSURE SENSE LINE, PRESSURE RESET REGULATOR, PRESSURE CONTROLLER, PRESSURE AMPLIFIER, AND ALL OF THE USED OXYGEN GENERATORS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20031222000452003122200045EA 2003 12 22 COMA0360531 120031207A5311601R53055K1 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01721CA 7259 CRACK NOTED AT FS 718.00 LT AND DOUBLER BETWEEN STRINGER 10 -12. REPAIRED PER EO 53 027 AND SERVICE BULLETIN 601R-53-055 PD. 2L72 4F RTA21EA 20031222000732003122200073WP 2003 12 22 AALA20031105 120031005A1430 DOME NUT DOUG DC9 DC983 3022083WP LEFT WING LEAKING A AALAB EMER. DESCENT K FLUID LOSS CRCRUISE 1 SW2176200 53290 AIRCRAFT EN ROUTE PDX-ORD OBSERVED FUEL LEAK IN THE LEFT WING ROOT. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT NOT OVERWEIGHT. MAINTENANCE SEALED UPPER WING TANK PLATE DOME NUT AND LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031222000962003122200096NM 2003 12 22 USAA030232 120031030A5320 FLOOR SUPPORT BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 FOUND SUPPORT CORRODED .5 INCH BY .5 INCH, BL 0 CABIN FLOOR SUPPORT FROM BS 345-377.7. REPLACED SUPPORT IAW SRM 53-10. CORROSION LEVEL 2, TASK NR C53-221-02. (M) 2L72 4F RTA2NM 20031125001022003112500102WP 2003 11 25 AALA20031291 120031118A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21428AA 49340 DFW OVERHEAD EMERGENCY LIGHTS AFT OF ROW 31 INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHTS AFT OF ROW 31 BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031125001092003112500109NM 2003 11 25 QXEA200301402 120031105A5411 FRAME BOMBDRDHC8 DHC8401 1390041NM NR 2 NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX- NR 2 NACELLE MID FRAME ASSEMBLY HAS FRETTING DAMAGE ON RIGHT AND LEFT SIDES. REPAIRED IAW HORIZON AIR EA 6-54-278. 2H72 4T RTA13NM 20031125001102003112500110NM 2003 11 25 USAA030223 120031111A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US52258 22952 PIT - FOUND SKIN CRACKED 2.5 INCHES STATION 765 ABOVE STRINGER 19R. CRACK CUT OUT AND DOUBLER INSTALLED PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20031125001252003112500125NM 2003 11 25 ASAA0310140 120030315A531565548971 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 867, LEFT BUTTOCK LINE 65 RIGHT BUTTOCK LINE 65 CORRODED. REMOVED DAMAGED AREA AND REPAIRED PER EA. (M) 2L72 4F A16WE 20031125001262003112500126NM 2003 11 25 ASAA0310472 120030515A5313BAC1493519 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND STRINGER 28R AT FUSELAGE STATION 500B CORRODED. CUT OUT DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031125001402003112500140NM 2003 11 25 ASAA0310471 120030515A53306545866688 SKIN BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND THE ANTENNA PANEL AT FUSELAGE STATION 585, BUTTOCK LINE 0 CORRODED. REPAIRED SKIN PER EA. (M) 2L72 4F A16WE 20031125001552003112500155NM 2003 11 25 ASAA0310260 120030330A33508621004 BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS BLINKING THROUGH OUT CABIN. REPLACED FIVE BATTERY PACKS, THEN LIGHT TESTED NORMAL. (M) 2L72 4F RTA16WE 20040311000122004031100012NM 2004 3 11 ASAA0310123 120030307A532065457818 SUPPORT ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SUPPORT ANGLE AT BS 986, STRINGER 24R-27R CORRODED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031126000122003112600012EU 2003 11 26 RAIA00311282 120031105A3260 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU LANDING GEAR MALFUNCTIONED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03556HK 41073 5483-SGF- LANDING GEAR WARNING ALARM SOUNDED AND STALL CAPTIONS ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE. REMOVED AND REPLACED AOG SLAVE RELAY. 2L72 4T RTA41NM 20031126000202003112600020NM 2003 11 26 QXEA200301403 120031105A7110 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX- NR 2 LOWER COWL, AFT CONE SUPPORT BRACKET CRACKED. REPAIRED IAW RD8-4-71-016. 2H72 4T RTA13NM 20031126000502003112600050NM 2003 11 26 03FDEA01979 120031125A7714 PROBE BOEING727 727200 138407ENM NR 1 ENGINE CONTAMINATED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25235FE 21329 DURING T/O, NR 1 ENG INDICATED LOW N1 RPM (APPROX 80 PERCENT) WHEN STD EPR SET. ABORTED T/O AT APPROX 90 KTS, 138400 LBS, 600 FT PA, -3 DEGREES C. RAN ALL APPROPRIATE CHECKLISTS AND AFTER COORDINATION WITH GROUND CONTROL RAN UP NR 1 ENG. DURING RUN-UP NR 1 ENG RAN NORMAL. DUE TO CREW INFO ABOVE, A/C DID MAKE POWER ON 2ND ATTEMPT. A/C SAT TODAY IN FREEZING RAIN. SUSPECT ICE ON EPR PROBE. INSPECTED INLET AND EXHAUST FOR ICE DAMAGE, NONE FOUND. CREW RUN ENGINE AGAIN TO VERIFY N1 GAUGE IS WORKING CORRECTLY. ALL INDICATIONS NORMAL ON ENG RUN. REQUIRED BRAKE COOLING TIME WAS ACCOMPLISHED. A/C OK TO CONTINUE. 2L73 4F RTA3WE 20031126000562003112600056NM 2003 11 26 CALA0300661 120030716A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND AFT CABIN FLOORBEAM CORRODED AT STA 986.5, RBL 46. REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20031126000832003112600083SO 2003 11 26 C2XA03SH429 120031104A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031126000902003112600090SO 2003 11 26 C2XA03SH409 120031023A532014521721009 BUTTSTRAP EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 25 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031126000932003112600093SO 2003 11 26 C2XA03BT103 120031024A3320BR90002 BALLAST EMB 145 EMB145 3260210SO CABIN DEFECTIVE A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2713956 145078 CREW REPORTED ON TAXI, ELECTRICAL BURNING SMELL IN (THE VICINITY OF) ROW FOUR IN THE CABIN. MAINTENANCE REMOVED AND REPLACED LIGHT BALLAST AND WIRING FOR SEAT 4A AND 5A SIDEWALL LIGHTS. OPS CHECKED GOOD, NO BURNING SMELL NOTED IAW EMB145 MM NR 3321-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031126001072003112600107SO 2003 11 26 C2XA03SH459 120031119A532014522460011 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE AFT DIGITAL PANEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT DIGITAL PANEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040415000182004041500018SW 2004 4 15 ERAA093712 120031221A6720 BEARING BELL 412 412 1182202SW BELLCRANK DEFECTIVE A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 FL320921 BAD BEARING FROM STOCK. REMOVED DEFECTIVE BEARING FROM BELLCRANK. INSTALLED NEW BEARING IAW MFG-ALL-SPM. 1G72 4U H4SW 20040419000122004041900012WP 2004 4 19 ASAA0380846 120031229A561046412472 LINKAGE DOUG DC9 DC983 3022083WP COCKPIT WINDOW OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 SEA - DURING PREFLIGHT CHECK, FOUND RIGHT SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED UPPER LOCK BAR LINKAGE. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040419000262004041900026WP 2004 4 19 ASAA0380843 120031220A38208921460G3 WATER HEATER DOUG DC9 DC983 3022083WP AFT LAVATORY SHORTED A ASAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM01950AS 53023 LAS - DURING TAXI TO GATE, SMOKE OBSERVED IN RIGHT AFT LAVATORY. DETERMINED TO BE ELECTRICALLY SHORTED WATER HEATER CAUSE BY LEAKING HEATER ASSEMLBY HOSE. TURNED OFF ALL AIRCRAFT ELECTRICAL POWER DURING REMAINDER OF TAXI. REPLACED WATER HEATER. (M) 2L72 4F RTA6WE 20040420001342004042000134GL 2004 4 20 ERAA094065 220030612A7320252464431 FUEL CONTROL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL ENGINE OVERHEATED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03152EH S701 FUEL CONTROL CLOSE TO EXPIRATION TIME. UNIT OVERHEATED. VERY DIRTY / CORRODED INTERNALLY. OVERHAULED IAW MFG OHM FORM 15-602E. 1G72 3U3 U H3EU E4CE 20031124000092003112400009NE 2003 11 24 SWIA200312596 220031112A7200 SHAFT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE ENGINE FAILED A SWIAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 NM07290SW8279 5161 120317 115465 ENGINE SHUTDOWN BY ITSELF ON TAXI. INSTALLED SERVICEABLE ENGINE ASSY IAW 71-00-00 AND 61-00-00. OPS CHECKS GOOD. STANDARD AERO CONFIRMED TOWER SHAFT FAILURE DUE TO TORSIONAL FATIGUE. THIS IS A PRODUCT OF STRESS AND TIME. 2L72 4T4 TRTA31SO E20NE 20031124000662003112400066NE 2003 11 24 MASA200300448 220031112A73206078T55P18 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE OUT OF RIG A MASAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 SW072731410836 7314 872491 CREW REPORTED NR 1 ENG FLAME-OUT AFTER LANDING AND TURN OFF ON TAXI WAY. MX WAS CALLED. MX RIGGED FUEL CONTROL, OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031124000702003112400070NM 2003 11 24 CALA0300644 120031114A5330 SKIN BOEING757 757224 1384958NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734131 28971 INSPECTION FOUND AFT FUSELAGE EXTERNAL SKIN PUNCTURED JUST BELOW LEFT STATIC PORT AT STA 1365, S23-24L. REPAIRED SKIN IAW SRM 53-00-01, FIGURE 204 AND 51-10-01, FIGURE 7. 2L72 4F RTA2NM 20031124001622003112400162NM 2003 11 24 QXEA200301277 120031015A242131708001A GENERATOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE NR 2 ENGINE FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09359PH145302586 514 MFR- NR 2 AC GENERATOR LIGHT ILLUMINATED. RESET IAW CHECKLIST AND RE-ILLUMINATED IN 5 SECONDS. REMOVED AND REPLACED AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031125000372003112500037WP 2003 11 25 DHL2003805518 120030730A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 497.491 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000422003112500042WP 2003 11 25 DHL2003805532 120030816A53209754022U504 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 FWD CARGO COMPT FITTING ATTACHING CUSP EXTRUSION TO FLOORBEAM WITH TWO CRACKS OF 3.000 AND 1.000 AT STA 340.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACK FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125001182003112500118NM 2003 11 25 ASAA0310109 120030306A553465548426 ANGLE BOEING737 737210C 1384459NM VERTICAL STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND VERTICAL STABILIZER SKATE ANGLE AT BS 1016-1056, RIGHT BUTTOCK LINE 12 CHAFED. REMOVED AND REPLACED SKATE ANGLE PER SRM. (M) 2L72 4F A16WE 20031125001452003112500145NM 2003 11 25 ASAA0340121 120030309A575365C26309 SUPPORT ANGLE BOEING737 737490 1384715NM T/E FLAP CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 PAE - DURING C-CHECK, FOUND CRACKED SUPPORT ANGLE FOR LEFT INBOARD FLAP TRACK FAIRING. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031202000042003120200004NM 2003 12 2 ASAA0310469 120030515A5315BAC1518434 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 967, LEFT BUTTOCK LINE 40 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20031202000052003120200005NM 2003 12 2 ASAA0310467 120030515A5315BAC1518434 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 947, LEFT BUTTOCK LINE 26, LEFT BUTTOCK LINE 30 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20031202000092003120200009NM 2003 12 2 ASAA0310439 120030512A53306545769 SKIN PANEL BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND SKIN PANEL AT BS 360-366, STRINGER 27R CORRODED. CUT OUT DAMAGED SKIN AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031202000202003120200020EA 2003 12 2 ASOA03466 120030929A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11904EV 7628 DURING A GROUND INSPECTION IN MGM, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040311000622004031100062NM 2004 3 11 ASAA0310096 120030305A52306547952537 SKIN BOEING737 737298C 1384490NM CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AFT CARGO DOOR INTERNAL SKIN AT BS 845, STRINGER 24R DENTED. CUT OUT DAMAGE AND INSTALLED REPAIR AND FILLER PER SRM. (M) 2L72 4F RTA16WE 20040311000172004031100017NM 2004 3 11 ASAA0310101 120030306A5320BAC15032730 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND LANDING GEAR ANGLE AT BS 663-727, RIGHT BUTTOCK LINE 24.75 CORRODED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040311000162004031100016NM 2004 3 11 ASAA0310002 120030105A326065446916 MODULE BOEING737 737290C 138448VNM NLG DIRTY A ASAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM01740AS 22578 ANC - AFTER TAKEOFF WITH LANDING GEAR UP, NOSE GEAR LIGHT WENT RED WITH GEAR OFF, NOSE GEAR EXTENDED BY ITSELF. REMOVED AND REPLACED NOSE LANDING GEAR TRANSFER CYLINDER (P/N 69141067, S/N DA687) AND LANDING GEAR MODULE. PERFORMED NOSE LANDING EXTENSION AND RETRACTION AND OPS CHECK NORMAL. SUBSEQUENTLY VENDOR CLEANED AND REASSEMBLED NLG MODULE AND ANOTHER VENDOR OVERHAULED TRANSFER CYLINDER. (M) 2L72 4F A16WE 20040311000502004031100050NM 2004 3 11 ASAA0310136 120030312A5247 DOOR FRAME BOEING737 737210C 1384459NM APU DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND APU ACCESS DOOR FRAME WEB AT BS 1098, RIGHT BUTTOCK LINE 20 GOUGED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F A16WE 20040311000332004031100033NM 2004 3 11 ASAA0310130 120030310A53206550568503 SILL BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND AFT ENTRY DOOR MOPSILL AT BS 986.5, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED MOPSILL PER SRM. (M) 2L72 4F A16WE 20031202000402003120200040NM 2003 12 2 USAASB03191 120031017A335020131A BATTERY BOEING737 7373B7 1384580NM EMERGENCY SIGN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 FOUND L2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACE THE BATTERY. (M) 2L72 4F RTA16WE 20031202000452003120200045NM 2003 12 2 2003F00599 120031017A26111014A POWER UNIT BOEING727 727200 138407ENM FIRE WARNING SYSFAILED A P9RAK NONE O OTHER ININSP/MAINT 1 EA11906PG 20728 APU FIRE ALARM DID NOT TEST ON GROUND. REMOVED AND REPLACED OPERATING POWER UNIT IAW B727 MM 26-15-00. OPERATIONALLY CHECKED GOOD. (M) 2L73 4F RTA3WE 20031202000502003120200050NM 2003 12 2 USASB03177 120031012A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US 23232 MAINTENANCE REPORTED SEVERAL CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN CEILING ABOVE SEAT ROW 10R. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031202000572003120200057EU 2003 12 2 USAASA03119 120031007A49004950488 SWITCH AIRBUSA321 A321211 3930370EU APU LEAKING A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19176UW 1499 EN ROUTE PHL-NAS, PRIOR TO FLIGHT, WITH APU BLEED ON, A STRONG ODOR CAME FROM THE AIR CONDITIONING PACKS. THE ODOR DISSIPATED ONCE THE BLEED SOURCES WERE SWITCHED TO ENGINE. AFTER FLIGHT TOOK OFF, THE ODOR RETURNED THROUGHOUT THE AIRCRAFT. TEH FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LEAKING APU OIL SWITCH. REPLACED THE SWITCH AND BOTH RECIRCULATION FILTERS, AND PERFOREMD THE APPLICABLE ENVIRONMENTAL CONTROL SYSTEM DECONTAMINATION TASK. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031202000652003120200065GL 2003 12 2 USAASB03187 220031017A7200 ENGINE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B1US GL NR 2 OVERTEMP A USAAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA19374US 22953 ON CLIMB-OUT FROM IAH, EN ROUTE TO PHL, CREW SHUTDOWN THE NR 2 ENGINE DUE TO HIGH OIL TEMPERATURE. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT IAH AND LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. 2L72 4F4 FRTA16WE E2GL 20031202000682003120200068 2003 12 2 USAABB03173 420030920A2565 CONNECTOR BOEING767 767201 1385125NM R2 DOOR OVERHEADLOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19646US 23898 THE RIGHT OVERWING EXIT FAILED THE SQUIB TEST. MAINTENANCE FOUND A LOOSE CONNECTION (S1) ON THE M1136 CONTROL MODULE AND TIGHTENED IT. (M) 2L72 4F RTA1NM 20031124000182003112400018NM 2003 11 24 QXEA200301456 120031104A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 NR 5 SEAT TRACK HAS A CHAFE ON THE INBOARD FACE OF RIGHT HAND LUG 12 INCHES FORWARD OF FRAME X467. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36, RD 8-53-2636 AND HORIZON AIR EA 2-53-507. 2H72 4T RTA13NM 20031124000212003112400021EA 2003 11 24 03325633 120031121A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27633BR 7274 DURING INSPECTION THE AFT SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE FAULT WAS IDENTIFIED AS A LOOSE CONNECTOR AT THE AFT SECTION OF TRACK LIGHTING. THE CONNECTOR WAS RESECURED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040114000932004011400093NM 2004 1 14 DL73S031033 120031120A53156545410137138 FLOORBEAM BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 DURING MODIFICATION OF THE BL 24 FLOORBEAMS PER EO 03-056673-03AD ADDITIONAL WORK WAS REQUIRED DUE TO ADDITIONAL DAMAGE INCURRED. ERA 385831-14AD IMPLEMENTS THE LBL 24 BEAM MOD, PROVIDES NEW REPAIRS FOR THE BEAM WEBS AND ADDRESSES INCURRED DAMAGE. 2L72 4F RTA16WE 20040114001062004011400106NM 2004 1 14 DL76L031043 120031121A3350 LIGHT BOEING767 767332 1382001NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27184DN 27111 E-PATH LENS AND LIGHT BULB MISSING AT SEAT 10FG. REPLACED SAME, OPS NORMAL. 2L72 4F RTA1NM 20031124000502003112400050NM 2003 11 24 03FDEA01914 120031112A5753 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT WING, FOUND OUTBOARD FLAP, STOP FITTING FWD RIB WITH CRACK. APPROX 0.125 IN LENGTH. LT WING O/B FLAP STOP FITTING FWD RIB CRACK REPAIRED AS PER FEDEX EA 1-5750-74244 WING - TRAILING EDGE FLAPS - LT & RT O/B FLAP SECONDARY STOP BOSS REPAIR. 2L73 4F RTA22WE 20031124000672003112400067EA 2003 11 24 MASA200300445 120031109A2150GG670950513 A/C PACK CNDAIRCL600 CL6002B19 1900309EA CABIN SMOKE A MASAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW0727318 7318 DURING T/O ROLL THE CAPT NOTICED SMOKE EMINATING FROM THE AIR CONDITIONING VENTS. RETURNED TO FIELD WERE CONTRACT MX DETERMINED THE CAUSE WAS THE LEFT HAND AIR CONDITIONING PACK. 2L72 4F RTA21EA 20031124000882003112400088WP 2003 11 24 DHL2003802508 120031113A534774529523 SEAT TRACK DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT NR 2 TRACK LUG WORN, STA 65.000. CUT OUT DAMAGED SECTION OF TRACK NR 2 IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG AND CHANNEL IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031124001082003112400108WP 2003 11 24 DHL2003805535 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING INBD L/E FORMER CRACKED 0.500, STA XFS 616.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 9 SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031124001122003112400112WP 2003 11 24 DHL2003805555 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 822.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO N/R 0249 FOR LT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031125000102003112500010WP 2003 11 25 DHL2003805516 120030807A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 448.561. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9, 10 SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000582003112500058WP 2003 11 25 DHL2003807517 120031014A53203750257U1 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SPLICE FITTING 4.000 CRACK (STA 580.000 - 600.000, L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, 51-1-20D PG 9, 21. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS AND PRC SEALANT IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20031125001662003112500166 2003 11 25 SWAA032494 420031111A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031125001722003112500172 2003 11 25 SWAA032469 420031106A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031125001732003112500173NM 2003 11 25 SWAA032470 120031107A5753654648195 SPINDLE BOEING737 7372H4 138448CNM T/E FLAP BROKEN A SWAAK NONE EF VIBRATION/BUFFET FLT CONT AFFECTED APAPPROACH 1 SW29073SW 22673 NR 7 AND NR 8 T/E MID FLAP CARRIAGE SPINDLES BROKEN. REMOVED AND REPLACED BOTH T/E FLAP SPINDLES PER MM. 2L72 4F A16WE 20031126000152003112600015SO 2003 11 26 RAIA00311281 120031105A5270 WARNING SYSTEM EMB 145 EMB145 3260210SO COCKPIT ACTIVATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03802HK 145066 5291-BGM- SERVICE DOOR OPEN INDICATION. MAINTENANCE DEFERRED PER MEL 52-70-00. SUBSEQUENTLY, CLEARED DMI, OPS CHECK SERVICE DOOR WARNING SYSTEM, OPS CHECK OKAY. 2L72 4F RTT00011AT 20031126000322003112600032WP 2003 11 26 DHL2003807513 120031016A53203750257U1 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SPLICE FITTING 9.000 CRACK (STA 620.000 - 640.000 L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING WITH NEW FASTENERS AND PRC SEALANT IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20031126001092003112600109SO 2003 11 26 C2XA03SH460 120031119A531514521721009 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE FORWARD DIGITAL PANEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL PANEL IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126001182003112600118NM 2003 11 26 ASAA0310455 120030515A5315BAC15061702 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 540-706, RIGHT BUTTOCK LINE 24.5 CORRODED. REMOVED DAMAGE AND REPAIRED PER EA. (M) 2L72 4F A16WE 20031202000012003120200001NE 2003 12 2 AALA20030943 220030829A7230 COMPRESSOR WHEEL BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE RT ENGINE DAMAGED A AALAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW21643AA 24601 AIRCRAFT VIBRATION FELT AND LOUD THUMP WAS HEARD AT 20,000 ON CLIMB-OUT. RIGHT ENGINE VIBRATED INTO THE AMBER RANGE. RETARDED THROTTLE BACK INTO NORMAL RANGE ATTEMPTS TO ADVANCE THE THROTTLE CAUSED VIBRATION TO RETURN INITIAL THUMP WITH SLIGHT CONTROL MOVEMENT. SLIGHT BURNED SMELL. ALL OTHER INDICATIONS NORMAL. DAMAGE FOUND TO ENGINE C1 DISK, NOSE COWLING AND THRUST REVERSERS. REMOVED AND REPLACED THR NR 2 ENGINE. SYSTEM GROUND OPERATIONS AND LEAK CHECKED CONDUCTED NORMAL FOR OPERATION. (M) 2L72 4F4 FRTA2NM E12EU 20031202000022003120200002NM 2003 12 2 AALA20030905 120030824A3213 TRUCK BOEING757 757223 1384957NM LT MLG FAILED A AALAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21609AA 27447 ON TAXI OUT, LEFT MAIN LANDING GEAR BOGIE TRUCK FAILED. AIRCRAFT UNABLE TO MOVE FROM TAXIWAY. NO EMERGENCY DECLARED. REPLACED BOGIE ASSEMBLY FOR LEFT MLG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031202000112003120200011WP 2003 12 2 GTIA030733 120030923A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND MAIN CABIN STATION 864 TO STATION 884 LBL 24 INCHES TO 44 INCHES FLOORBOARD CRACK/DAMAGE ON EDGE. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031202000182003120200018WP 2003 12 2 ASAA0380505 120030620A33500105603 MODULE DOUG DC9 DC982 3022082WP ROW 29 INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 EMERGENCY TRACK LIGHTING INOPERATIVE AT ROW 29. REPLACED LIGHT MODULE (HOLDER AND LAMP). LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20031202000272003120200027NM 2003 12 2 ASAA0310484 120030521A3350J883200312 RECEIVER BOEING737 737210C 1384459NM AFT CABIN INOPERATIVE A ASAAO OTHER O OTHER LDLANDING 1 NM01744AS 21822 EMERGENCY FLOOR TRACK LIGHTS ILLUMINATED MOMENTARILY AFTER LANDING. REPLACED AFT CABIN REMOTE ASSEMBLY RECEIVER, THEN LIGHTS OPERATED NORMAL. (M) 2L72 4F A16WE 20031202000382003120200038NM 2003 12 2 ASAA0340087 120030228A53146549886176 KEELBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON RT KEELBEAM AT BS 500G PLUS 3. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040311000322004031100032NM 2004 3 11 ASAA0310129 120030310A53156546811514 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 1006, LEFT BUTTOCK LINE 10, RIGHT BUTTOCK LINE 28 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040311000302004031100030NM 2004 3 11 ASAA0310132 120030310A5347BAC15201432 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 344-400, LEFT BUTTOCK LINE 25 CORRODED. REMOVED CORROSION AND REPAIRED SEAT RACK PER SRM. (M) 2L72 4F A16WE 20040311000372004031100037NM 2004 3 11 ASAA0310112 120030306A53206573746 FLOOR SUPPORT BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 967-986.5, RIGHT BUTTOCK LINE 18, LEFT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20040311000152004031100015NM 2004 3 11 ASAA0310110 120030306A54206573771 ANGLE BOEING737 737210C 1384459NM NR 2 NACELLE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 2 ENGINE FIXED FAIRING ANGLE AT NACELLE STATION 145 GOUGED. REPAIRED ANGLE PER SRM. (M) 2L72 4F A16WE 20031202000432003120200043NM 2003 12 2 USAASB03183 120031016A335020121 POWER SUPPLY BOEING737 737401 1384701NM MID CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US 23988 MAINTENANCE REPORTED THE AFT RIGHT ESCAPE HATCH EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1136 POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031202000462003120200046NM 2003 12 2 USAASB03188 120031019A33501010428 SOCKET BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US 23318 DURING EMERGENCY LIGHT, BULLNOSE, AT ROW 9 INOPERATIVE. MAINTENANCE REPAIRED A SHORT AT THE LIGHT SOCKET AND PROGRAMMED THE SOCKET FOR REPLACEMENT. (M) 2L72 4F RTA16WE 20031202000542003120200054EU 2003 12 2 USAA030203 120031007A5753D575712502 SKIN AIRBUS320 A320214 3930316EU RT TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND LOWER SKIN RIGHT OUTBOARD FLAP AT RIB 10 FORWARD FO REAR SPAR AT T/E, HAS DELAMINATION 1.25 INCH BY 1.75 INCH. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER AND INTERNAL 'L' ANGLE PER EA 76991A. (M) 2L72 4F RTA28NM 20031202000602003120200060NM 2003 12 2 USAASB03182 120031015A3260189929 PROXIMITY SENSOR BOEING737 737301 1384611NM NLG INOPERATIVE A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19589US 23934 ON CLIMB-OUT FROM CLT, EN ROUTE TO IAH, CREW RECEIVED A NOSE LANDING GEAR RED UNSAFE LIGHT WHEN GEAR WAS RETRACTED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND RECYCLED GEAR. RECEIVED THREE GREEN LIGHTS WHEN GEAR WAS DOWN AND WHEN GEAR WAS BROUGHT UP THEY RECEIVED TEH NOSE LANDING GEAR RED UNSAFE LIGHT AGAIN. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOWN PROXIMITY SENSOR (S845) PER MM 32-51-51. SWUNG GEAR. INDICATION CHECKS GOOD. (M) 2L72 4F RTA16WE 20031222001122003122200112SO 2003 12 22 SIMA200330902 120031104A27503631101997 SELECTOR EMB 135 EMB135KL 3260302SO COCKPIT INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW21830AE 145615 DURING APPROACH TO SNA CREW REPORTED A FLAP FAIL MESSAGE ON EICAS AND THE FLAPS STAYED AT 9 DEGREES. AIRCRAFT DIVERTED TO LAX. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031223000412003122300041NM 2003 12 23 SWAA032662 120031204A53156546804 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 312 LBL 11 TO RBL 37, WL 208 CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031223000582003122300058NM 2003 12 23 SWAA032679 120031208A335090083 BATTERY PACK BOEING737 7373T5 1384608NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 MID CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20031223000702003122300070NM 2003 12 23 DHL2003755011 120031211A5270 SWITCH BOEING727 727225 1384077NM MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01755DH 21857 AFTER T/O, GEAR LEVER MOVED FROM UP TO OFF, THE RED DOORS LIGHT AND THE AMBER RIGHT GEAR DOOR ILLUMINATED. PERFORMED ABNORMALS. ALL DOOR LIGHTS EXTINGUISHED. ADJUSTED RIGHT MLG DOOR SWITCH IAW B-727 M/M 32-62-11. OPS CHECKED GOOD IAW B-727 M/M 32-62-11. 2L73 4F A3WE 20031223000822003122300082NM 2003 12 23 VNAA0312006 120031211A3060 LEAD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT PROP DEICE FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07438JS 3056 DURING FLIGHT, THE CREW RECEIVED A RIGHT HAND PROP DE-ICE FAIL INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND ADJUSTED THE BRUSHBLOCK THEN REPLACED THE PROP LEAD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031223000912003122300091NM 2003 12 23 SWAA032702 120031210A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SPECIAL VISIT FOUND STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R AND 4L. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031223001022003122300102EA 2003 12 23 SWIA200312655 120031031A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07594SW 7285 FS 280 LEFT FLOORBEAM LBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED. REPLACED ANGLES IAW CRJ SRM 51-40-11 & RII 53-401. P/N: 601R31113-57. 2L72 4F RTA21EA 20031223001092003122300109EA 2003 12 23 COMA0360545 120031208A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS NRNOT REPORTED 1 SO01420CA 7451 FLAPS FAILED WHEN SELECTED 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031223001592003122300159EA 2003 12 23 A6WA200340160 120031111A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31401AW 7280 THE RIGHT FUSELAGE SKIN AT FS 272 STRINGER 24R HAS LIGHTNING STRIKE DAMAGE WITH A TEMPORARY REPAIR INSTALLED IAW BOMBARDIER, INC REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED SECTION OF FUSELAGE SKIN. FABRICATED REPAIR DOUBLER AND FILLER FROM 2024 T42 .063 INCH WVAC PO NR 16956/2 AND INSTALLED IAW WVAC EO 601R-53-4379. (M) 2L72 4F RTA21EA 20031223001612003122300161EA 2003 12 23 ASOA03549 120031030A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11862AS 7445 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING TEH CARGO DOOR FLOOR LANDING PLATE IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20031223001662003122300166EA 2003 12 23 ASOA03550 120031030A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11862AS 7445 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20031223001962003122300196WP 2003 12 23 GTIA030822 120030930A5714 ANGLE DOUG DC9 DC982 3022082WP CENTER WINGBOX CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND WEB ANGLE ATTACHMENT STATION 864 OVER CENTER WING TANK CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2L72 4F A6WE 20031224000012003122400001WP 2003 12 24 GTIA030811 120031009A5260 WEB DOUG DC9 DC982 3022082WP AIRSTAIR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND AFT AIRSTAIRS CUT OUT AFT SIDE WEB HAS TWO CRACKS IN IT. CUT OUT TWO DAMAGED AREAS. FABRICATED TWO FILLERS, TWO DOUBLERS. INSTALLED TWO FILLER AND DOUBLER. (M) 2L72 4F A6WE 20031224000052003122400005WP 2003 12 24 GTIA030819 120030930A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND RIGHT AFT LAV STATION 1322 RBL 19-54, FLOORBEAM CORRODED. TRIMMED OUT DAMAGED AREA. DRILLED AND LOCATED ANGLE/FILLER. INSTALLED REPAIR ANGLE AND FILLER. (M) 2L72 4F A6WE 20031224000062003122400006WP 2003 12 24 GTIA030818 120030929A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND LEFT AFT LAV STATION 1338 LBL 19 LBL 54 FLOORBEAM CORRODED. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR ANGLE AND FILLER. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20031224000082003122400008WP 2003 12 24 GTIA030816 120031019A2560 SIGN DOUG DC9 DC983 3022083WP EMERGENCY EXIT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 ORD - FOUND SAFETY GLO EXIT SIGN AT C-4 GALLEY IS MISSING ARROW. INSTALLED EXIT SIGN ARROW AT 64 GALLEY GLOW. (M) 2L72 4F RTA6WE 20031224000092003122400009WP 2003 12 24 GTIA030804 120030907A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND SEAT TRACKS RIGHT STA 200-826 BARE METAL, NICKS LIGHT CORROSION. SEAT TRACKS COMMON TO RBL 22 & 54 FROM STA 200-826 OUT OF LIMITS. REMOVED OUTBOARD SEAT TRACK RBL 54 FROM STA 200-826. REMOVED INBOARD SEAT TRACK RBL 22 FROM STA 200-826. FABBED SEAT TRACK COMMON TO RBL 22 STA 266-436. DRILLED & LOCATED HOLES IN SEAT TRACK & SPLICE RBL 22 FROM STA 436-826. INSTALLED INBOARD TRACK & SPLICES COMMON TO RBL 22 FROM FS 200-826. FABRICATED OUTBOARD TRACKS STA 200-323, 400-550, 550-627, 627-741, 741-798 & STAT 798-922. INSTALLED OTBD SEAT TRACK RBL 54 FROM STA 200-332. FABBED SPLICES FROM STATION 200-826 RBL 54. INSTALLED SEAT TRACKS FROM STA 332-826 RBL 54. INSTALLED SPLICES FROM STA 200-826 RBL 54. 2L72 4F A6WE 20031224000132003122400013WP 2003 12 24 GTIA030801 120030829A5420 ANGLE DOUG DC9 DC982 3022082WP LT NACELLE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND LT ENGINE PYLON BOTTOM SIDE AT FUSELAGE ATTACH ANGLE CRACKED. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. (M) 2L72 4F A6WE 20031224000172003122400017WP 2003 12 24 GTIA030799 120030907A3350 LIGHT DOUG DC9 DC982 3022082WP TAIL COMPARTMENTINOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND TAIL COMPARTMENT EMERGENCY EXIT LIGHTS UPPER AND LOWER INOPERATIVE, MIDDLE LIGHT GOOD. REMOVED AND REPLACED BOTH LIGHT ASSEMBLIES. (M) 2L72 4F A6WE 20031224000232003122400023NM 2003 12 24 USAABB03213 120031121A495038760355 SENSOR BOEING757 757225 1384959NM APU FAILED A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19606AU 22202 BOS - FLT 834 - EN ROUTE PHL-BOS, WITH THE RIGHT IDG ON MEL, THE APU PERFORMED AN AUTO SHUTDOWN. THE FLIGHT CONTINUED TO BS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN BOS REPLACED THE P2 SENSOR. THE APU WAS PROGRAMMED FOR REPLACEMENT FOR AN ON-GOING PNEUMATICS PROBLEM. (M) 2L72 4F RTA2NM 20031224000302003122400030WP 2003 12 24 ASAA0380623 120031007A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOOR EDGES HAVE BEEN WATER DAMAGED BETWEEN FS 1003 AND 1074. REPLACED FLOORBOARD PER SRM 53-24-0. (M) 2L72 4F RTA6WE 20031224000352003122400035WP 2003 12 24 GTIA030946 120031025A5313 STRINGER DOUG DC9 DC983 3022083WP CARGO DOOR FRAMECORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND AFT PIT DOOR STRINGER 28R JAMB BEAM CORRODED AT DOOR OPENING. (M) 2L72 4F RTA6WE 20031219001862003121900186NM 2003 12 19 CALA0300705 120031206A3233273T63511 ACTUATOR BOEING767 767424ER 1385270NM RT MLG BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW275905312786 29448 THE LANDING GEAR DISAGREE AND GEAR DOOR DISAGREE EICAS MESSAGES CAME ON AFTER TAKEOFF FROM GRU. THE GEAR WAS CYCLED TWICE WITH NO CORRECTION. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO GRU WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING PER MM 32-32-00 FOUND THE RIGHT MLG DRAG BRACE ACTUATOR BROKEN AT THE ROD END. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-02-401. OPERATIONAL AND LEAK CHECKS WERE GOOD. 2L72 4F RTA1NM 20031222000172003122200017EA 2003 12 22 SWIA200312646 120031130A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA YOKE DIRTY A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07941SW 7750 AFTER LIFTOFF, RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. UNABLE TO RESET STAB TRIM CH1 OR CH2 OR MACH TRIM. RETURNED TO LAX. CLEANED CAPT'S SIDE DISCONNECT SWITCH ON YOKE. OPS CHECK GOOD. 2L72 4F RTA21EA 20031222000682003122200068WP 2003 12 22 ASAA0380617 120031007A532199365441 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOORBOARD JUST INSIDE L1 ENTRY IS CORRODED AROUND INSERTS AT FS 148-196. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031222001002003122200100EU 2003 12 22 USAA030244 120031103A5320D5348004320401 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT CORRODED 1.250 INCH SQUARE INCH AREA, FRAME 68 FORWARD OF L2 DOOR AFT GIRT BAR LATCH. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR IAW SRM 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR IAW SRM 51-42-11. (M) 2L72 4F RTA28NM 20031223000072003122300007EA 2003 12 23 03340665 120031206A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27665BR 7534 DURING INSPECTION THE FOWARD SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE NR 1 INVERTER WAS FOUND TO CAUSE THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031223000222003122300022NM 2003 12 23 SWAA032625 120031130A33506556633 LIGHT BOEING737 7377H4 1384404NM LT OVERWING INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20031223000442003122300044NM 2003 12 23 SWAA032665 120031204A3350100067 LIGHT BOEING737 7372H4 138448CNM L2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F A16WE 20031223001142003122300114NM 2003 12 23 AWXA200301529 120031211A33501012621 LIGHT BOEING737 737277 1384570NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 EN ROUTE TO PHX THE L-2 DOOR EMERGENCY EXIT LIGHT HOUSING AND LENS FELL OFF. MAINTENANCE REMOVED AND REPLACED L-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031124000352003112400035NM 2003 11 24 AWXA200301425 120031028A5320654583469 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 DURING C-13 CHECK A .5625 INCH CRACK WAS FOUND ON TIE STRAP AT BS 323, RBL 31. MAINTENANCE REMOVED CRACKED TIE STRAP AT BS 323, RBL 31; FABRICATED A NEW REPLACEMENT TIE STRAP PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8, PG 1. 2L72 4F RTA16WE 20031124000392003112400039 2003 11 24 YENA200335 420031108A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU SEAT 21E INOPERATIVE A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15547JB2620 444 1849 UNUSUAL ODOR/SMELL FROM ROW 20 BACK. SEEMED TO DISSIPATE AFTER LIVE TV SHUTDOWN. ISOLATED ODOR TO SEB 21E, SEB HAD STRONG BURNING ODOR. REMOVED AND REPLACED SEB AT 21E. PERFORMED A FULL INTEGRITY CHECK AS PER INFORMATION NOTICE 2003-T-T050TRA. NO OTHER EVIDENCE OF BURNING OR DAMAGE OTHER THAN SMELL FROM SEB. NEW SEB CHECK GOOD AS PER LIVE TV MM 23-39-00. LTV SYSTEM FULL FUNCTION CHECK NORMAL SEB ROUTED THROUGH JB STORES TO LIVE TV ENGINEERING FOR ANALYSIS. 2L72 4F RTA28NM 20031124000452003112400045EA 2003 11 24 COMA0360498 120031115A2750 CONTROL MODULE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01931CA 7037 FLIGHT 5226 FLAPS FAIL AT 27 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20031124000602003112400060NM 2003 11 24 QXEA200301441 120031117A2697 WIRE HARNESS DHAV DHC8 DHC8202 2809007NM SMOKE DETECTOR INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09362PH 518 2 BAGGAGE SMOKE DETECTOR INOPERATIVE. FOUND NR 2 BAGGAGE SMOKE DETECTOR WIRE HARNESS SEVERED BY CARGO DOOR AT PLUG 2612-P3. REMOVED AND REPLACED WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031124000632003112400063NM 2003 11 24 C1HA200394043 120031114A5320 CHANNEL BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 RIGHT AFT LAV HAT CHANNEL AT BS 1140 RBL 45.5 HAS CORROSION. 2L73 4F A3WE 20031124000642003112400064NM 2003 11 24 C1HA200394044 120031114A5340 FITTING BOEING727 727290 138408WNM LAVATORY CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 RIGHT AFT LAV GUITAR FITTING BS 1140 HAS CORROSION. 2L73 4F A3WE 20031124000782003112400078NM 2003 11 24 QXEA200301423 120031112A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 WILL NOT TEST A QXEAO OTHER L NO TEST NRNOT REPORTED 1 NM09364PH 524 NR 1 SMOKE WARNING DOES NOT TEST. NO LIGHTS ILLUMINATE. REMOVED AND REPLACED BEACON AND TESTED LAMPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031124000842003112400084WP 2003 11 24 DHL2003807539 120031018A5730 PLATE DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RT WING CTR L/E OUTER PLATING LOWER PART HAS CORROSION AROUND STA XFS 404.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW NDT STANDARD PRACTICE MANUAL PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW ASTAR ED EDU21-13, ASTAR DWG U21-R13. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ASTAR ED EDU21-13, ASTAR DWG U21-R13, SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031124001462003112400146NM 2003 11 24 CALA0300600 120031008A5320654583475 INTERCOSTAL BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 CORROSION ON INTERCOSTAL ANGLE BETWEEN STA 344 AND 360 AT LBL 12. REMOVED AND INSTALLED NEW CHORD IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031124001552003112400155EA 2003 11 24 QXEA200301350 120031023A261247359719 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09615QX2703 2703 10065 PDX- FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 1 FIRE DETECTOR IN AFT CARGO BAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031125000262003112500026WP 2003 11 25 DHL2003802517 120031105A5320 INTERCOSTAL DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 FWD CARGO COMPT - AFT PRESSURE BLKD INTERCOSTAL CRACK 1.000, STA 640.000 LBL 45. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 PG 2E/2F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000392003112500039WP 2003 11 25 DHL2003805530 120030807A5720 INTERCOSTAL DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E INTERCOSTAL CRACKED 2.000, STA XS 454.976 - XS 461.372. REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED INTERCOSTAL IAW SRM 57-1-0 PG 1 SRM 57-3-3 PG 15. CLEANED, TREATED AND PRIMED INTERCOSTAL IAW SRM 51-1-8B. INSTALLED INTERCOSTAL ON RIGHT WING CTR L/E, XS 454.976 - XS 461.372 IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000472003112500047WP 2003 11 25 DHL2003807523 120031009A534774529527 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MAIN CARGO COMPT NR 1 TRACK LUG WORN AT STA 1120.000. CUT OUT NR 1 TRACK DAMAGED SECTION, STA 1120.000 IAW SRM 53-2-3 PG 17, FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG AND CHANNEL IAW SRM 53-2-3 PG 17, FIG 6D, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125001002003112500100NM 2003 11 25 AALA20031289 120031117A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21790AN 30251 DFW FORWARD COACH SEATS EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD COACH SEATS EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031125001082003112500108NM 2003 11 25 QXEA200301401 120031105A5411 FRAME BOMBDRDHC8 DHC8401 1390041NM NR 2 NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX- NR 2 NACELLE FORWARD FRAME ASSEMBLY HAS FRETTING DAMAGE ON RIGHT AND LEFT SIDES. REPAIRED IAW HORIZON AIR EA 6-54-278. 2H72 4T RTA13NM 20031125001162003112500116NM 2003 11 25 USAASB03195 120031101A2611100064904 SMOKE DETECTOR BOEING737 7374B7 1384702NM CARGO BAY MALFUNCTIONED A USAAK NONE N FALSE WARNING CRCRUISE 1 EA19435US 24557 CLT - FLT 892, EN ROUTE FROM BOS TO CLT, CREW REPORTED THE FIRE BELL SOUNDED FOR TWO TO FIVE SECONDS ALONG WITH A FIRE WARNING AND MASTER CAUTION CARGO FIRE INDICATION. WARNING STOPPED WITH SYSTEM TESTING OK AND SYSTEM OK LIGHT ON. FLIGHT CONTINUED ONTO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED SYSTEM SMOKE TEST, BOTH INDIVIDUAL AND DUAL DETECTOR UNITS IN AFT CARGO BIN FOR LOW DECIBEL READINGS PER MM 26-15-01-01. ALSO, REMOVED AND REPLACED CONTROL DISPLAY UNIT P/N 100-0120-12, PER MM 26-15-01-03. SYSTEM CHECKS GOOD. (M) 2L72 4F RTA16WE 20040311000412004031100041NM 2004 3 11 ASAA0310144 120030316A5320BAC15061922 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 907-947.5, RIGHT BUTTOCK LINE 66 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031125001502003112500150NM 2003 11 25 ASAA0310146 120030316A5320654661123 FLOOR SUPPORT BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOOR SUPPORT AT BODY STATION 540, BUTTOCK LINE 0 RIGHT BUTTOCK LINE 46 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M) 2L72 4F RTA16WE 20031125001562003112500156NM 2003 11 25 ASAA0310517 120030611A5330 SKIN PANEL BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING A-CHECK, FOUND THE FUSELAGE SKIN PANEL AT BODY STATION 747-748, STRINGER 17R CRACKED. REPAIRED SKIN PER SRM. (M) 2L72 4F A16WE 20031125001672003112500167NM 2003 11 25 SWAA032495 120031111A2560P2070001 FLASHLIGHT BOEING737 7373A4 1384585NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM. 2L72 4F RTA16WE 20031125001702003112500170NM 2003 11 25 SWAA032498 120031111A3350079012 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29732SW 27864 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 3, 4, AND 23. REMOVED AND REPLACED TRACK COVERS PER MM. 2L72 4F RTA16WE 20031126000092003112600009SO 2003 11 26 RAIA00311286 120031111A21508152401 ACM EMB 145 EMB145LR 3260212SO A/C BAY OVERHEATED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03810HK 145231 5301-RIC- LEFT PACK SMELLS OVERHEATED. MAINTENANCE REMOVED AND REPLACED ACM. 2L72 4T RTT00011AT 20031126000162003112600016EA 2003 11 26 QXEA200301464 120031120A3150 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT ACTIVATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09614QX 10049 PDX- ON FLIGHT 2523 ABORTED TAKEOFF DUE TO CONFIGURATION AILERON WARNING MESSAGE DURING TAKEOFF ROLL. AILERON TRIM INDICATORS CENTERED AND GREEN. TAKEOFF CONFIGURATION OK ADVISORY MESSAGE DISPLAYED PRIOR TO TAKEOFF ROLL. TROUBLESHOOT WARNING IAW FIM 27-12-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031126000302003112600030WP 2003 11 26 DHL2003805558 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER CRACKED 1.000, STA XFS 404.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, 2. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS (02 EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, 2 SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031126000332003112600033WP 2003 11 26 DHL2003807514 120031014A532037552221 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MAIN CARGO COMPT FITTING CRACKED 1.000 AT STA 822.000, RBL 24. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031126000892003112600089SO 2003 11 26 C2XA03SH392 120031017A532014529150003 CROSSBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE UPPER CROSS BEAM AT FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE UPPER CROSS BEAM AT FR 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126001012003112600101SO 2003 11 26 C2XA03SH465 120031119A532014521699003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE LEFT OMEGA BEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126001122003112600112SO 2003 11 26 C2XA03SH395 120031018A711014576631609 RIB EMB 145 EMB145 3260210SO NR 1 COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE NR 1 LOWER ENGINE COWLING AFT RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031202000132003120200013WP 2003 12 2 GTIA020734 120030923A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FS 1250-1307 DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 MAIN CABIN STATION 1250 TO STATION 1307 LBL 24 TO 44 FLOORBOARD SOFT/MUSHEY NO EDGE FILLER. FABRICATED FLOORBOARD. (M) 2L72 4F A6WE 20031202000242003120200024NM 2003 12 2 ASAA0310486 120030526A53306562109503 BEAR STRAP BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND THE BEAR STRAP AT FUSELAGE STATION 360, LEFT BUTTOCK LINE 65 CRACKED. REPAIRED BEAR STRAP PER EA. (M) 2L72 4F A16WE 20040311000572004031100057NM 2004 3 11 ASAA0310095 120030305A53206026019 SUPPORT BRACKET BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND DOOR THRESHOLD SUPPORT BRACKET AT BS 967, STRINGER 17R CORRODED. REMOVED AND REPAIRED SUPPORT BRACKET PER SRM. (M) 2L72 4F RTA16WE 20031223001462003122300146CE 2003 12 23 DXTA200300184 120031122A2710666000163 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07690QS 5605090 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001852003122300185WP 2003 12 23 GTIA030828 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 16 INCHES-20 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031223001922003122300192WP 2003 12 23 GTIA030826 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 0-36 INCHES RBL. REMOVED CABIN FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031224000152003122400015EA 2003 12 24 A6WA200340172 120031113A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31402AW 7281 CLIP IS CRACKED. REPAIRS ACCOMPLISHED BY FABRICATON OF REPLACEMENT ANGLE. WORK ACCOMPLISHED IAW FAA 81103 PER WVAC EO 601R-53-4403. (M) 2L72 4F RTA21EA 20031224000212003122400021EU 2003 12 24 USAASA03128 120031112A3220 LANDING GEAR AIRBUS320 A320214 3930316EU NOSE LACK OF LUBE A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19121UW 1294 AFTER TAKEOFF, THE LANDING GEAR HAD TO BE CYCLED A SECOND TIME TO GET IT TO RETRACT. THE FLT CONTINUED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE LUBED THE LANDING GEAR, JACKED THE AIRCRAFT, AND PERFOREMD A GEAR SWING. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031224000382003122400038 2003 12 24 ASAA0380600 420031002A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 SEA PREFLIGHT CHEC, AFT SERVICE R-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20031224000492003122400049NM 2003 12 24 AALA20031168 120031024A2750285A12001 CONTROL UNIT BOEING737 737823 13844BZNM TE FLAPS INOPERATIVE A AALAO OTHER J WARNING INDICATION DEDESCENT 1 SW21972AN 30097 ON APPROACH TO DFW FLAPS FAILED TO DEPLOY HYDRAULICALLY. CREW ACCOMPLISHED NO FLAP LANDING WITHOUT INCIDENT. REPLACED FLAP/SLAT ELECTRIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20031224000512003122400051SO 2003 12 24 SIMA200332705 120031121A261147359713 SMOKE DETECTOR EMB 135 EMB135KL 3260302SO CARGO BAY MALFUNCTIONED A SIMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21834AE 145631 DURING CRUISE THE CREW REPORTED A BAGGAGE SMOKE WARNING. CREW FOLLOWED EMERGENCY PROCEDURES AND USED THE FIRE BOTTLES. SMOKE INDICATION THEN WENT OUT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE SMOKE DETECTOR WAS REMOVED AND REPLACED IAW EMB MM. OPS CHECK WAS GOOD. THE FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031224000582003122400058NM 2003 12 24 TSAA0253247 120031118A531065465271 WINDOW FRAME BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 FILLERS AND REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN, MIN .5 INCH OUTSIDE CORNER RADIUS WITH 2.0 INCH INSIDE CORNER RADIUS AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1, PRIMER. INSTALLED FILLERS AND REPAIR DOUBLER WITH FASTENERS INDICATED IN FIGURES 1, 2, AND TABLE 1. APPLIED FILLET SEAL OF BMS'S 5-95 SEALANT AROUND EDGES OF REPAIR, BS 420, 440, 460, 480 AND 767. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO3250, DEVIATION AF. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031224000662003122400066SO 2003 12 24 C2XA03SH497 120031213A531514522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURUNG C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031229000032003122900003NM 2003 12 29 VNAA0311012 120031130A7931 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE TRANSDUCER FAILED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07462PS 3084 DURING TAKEOFF, THE CREW RECEIVED A RT ENGINE OIL PRESSURE OF 0 AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND PERFORMED A OIL LEVEL CHECK SHOWED A CORRECT LEVEL THEN CLEANED THE TRANSDUCER CONNECTOR IN ACCORDANCE WITH 79-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031229000052003122900005NM 2003 12 29 DHL2003740007 120031212A3260327 BULB BOEING727 7272Q9 138448MNM MLG INDICATOR BURNED OUT A DHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO01740DH 21930 RTO DUE TO LOSS OF RIGHT MAIN GEAR DOWN & LOCKED INDICATION. REPLACED TWO BULBS, OPS CHECKED GOOD. T.O.W 159.6, IAS O K.T.S, O.A.T 8 C, BRAKE ENERGY ZONE - NORMAL. RELAMPED INDICATOR LIGHT IAW M/M 33-10-51, OPS CHECKED NORMAL. 2L73 4F RTA3WE 20031229000112003122900011WP 2003 12 29 ABXA030466 120031124A531099577399 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 SHEAR TIE REPAIR HAD CRACK INDICATION FS 1021, BETWEEN LONGERON 15 RT AND LONGERON 14 RT. REPAIRED AREA IAW DC-9 SRM 53-03. 2L72 4F A6WE 20031229000232003122900023NM 2003 12 29 250TR0027 120031212A33506104789 BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 RIGHT HAND OVERWING & FLAP EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK M193 AND REFLECTOR. OPS CHECKS GOOD PER MM 33-51-1. 2L72 4F RTA16WE 20031229000382003122900038SO 2003 12 29 LR7A03103 120031121A5310 RING LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND LT CENTER FUSELAGE RING SEGMENT CORRODED AND CRACKED AT FS 762E, 767E AND 772E, LBL 60, WL 142-148. REPAIRED IAW SRM SMP 583 51-140-23. NR 2240. 2H74 4T A1SO 20031229000502003122900050NM 2003 12 29 AALA20031422 120031211A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21791AN 30254 SEAT MOUNTED EMERGENCY PATH LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS SEAT MOUNTED EMERGENCY PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031229000532003122900053EU 2003 12 29 AALA20031425 120031212A3350P4010051129 CHARGER FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211413A 11376 EMERGENCY LIGHT INOPERATIVE AT AFT LEFT OVERWING. REPLACED BATTERY CHARGER MODULE AT AFT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20031229000722003122900072NM 2003 12 29 03FDEA02186 120031214A5753 TRACK DOUG MD11 MD11 3023602NM ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING, INBOARD FLAP CENTER VANE TRACK CUTOUT DENTED. INBOARD FLAP CENTER VANE TRACK CUTOUT REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-75185, TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBOARD, FLAP/CTR RIB ASSY AND SKIN. 2L73 4F RTA22WE 20031229000862003122900086EA 2003 12 29 QXEA200301560 120031211A2610 SCREEN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX4245 27 10041 MAINTENANCE FOUND THE FORWARD CARGO COMPARTMENT FIRE DETECTOR CHIMNEY MESH TORN. THE CHIMNEY WAS REPLACED WITH NEW. 2L72 4F RTA21EA 20031229000882003122900088NM 2003 12 29 DHL2003742508 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE MISREPAIRED A DHLAO OTHER W INADEQUATE Q C ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSELAGE EXTERIOR BS 620 STR 10R LAP SEAM VERIFY REPAIR DONE FOR STRUCTURAL REPAIRS MANUAL COMPLIANCE. EVALUATED REPAIR AND FOUND IT TO BE NON-COMPLIANT IAW B-727 SRM 53-30-3 FIG 24. REMOVED PREVIOUS REPAIR AND FABBED NON STRUCTURAL FILLER FROM 2024 T3 .063 PO 90024 DIM 12.25 INCH X 5.75 INCH AND DOUBLER FROM 2024 T3 .071 PO 90024 DIM 10.25 INCH X .25 INCH X 9.25 INCH IAW B-727 SRM 53-30-3 FIG 24. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED IAW B-727 SRM 53-30-3 FIG 24. 2L73 4F A3WE 20031229000932003122900093NM 2003 12 29 AWXA200301537 120031208A5320D5323028120040 ANGLE AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28803AW 931 DURING C-04 CHECK A .5 INCH CRACK WAS FOUND IN LOWER RADIUS OF L- ANGLE ON LT SIDE OF FR 34 UNDER PANEL 191A, BS 14836. MAINTENANCE REMOVED CRACKED -L- ANGLE ON LT SIDE OF FR 34; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 6-7, A23, & A27. 2L72 4F RTA28NM 20031229000972003122900097NM 2003 12 29 AWXA200301541 120031205A534069353521 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER CLIP BS 847, STR 10 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 847, STR 10 LT; RECEIVED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 45 & 64, FIG 12 & 14. 2L72 4F RTA16WE 20031229000992003122900099NM 2003 12 29 AWXA200301543 120031204A532066142081 INTERCOSTAL BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK A .625 INCH CRACK WAS FOUND IN FORWARD INTERCOSTAL AT L-1 DOOR OPENING BS 294.5, STR 11 LT. MAINTENANCE REMOVED CRACKED FORWARD INTERCOSTAL AT L-1 DOOR OPENING BS 294.5, STR 11 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 66-14208; INSTALLED REPAIR PART IAW B737-300 SRM 51-20-01, PG 45, 47, & 63, FIG 2, 12, & 14. 2L72 4F RTA16WE 20031223000122003122300012NM 2003 12 23 SWAA032654 120031203A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED C1 CHECK, FOUND RT WING O/B FLAP I/B END DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20031223000682003122300068NM 2003 12 23 DHL2003765005 120031210A2612 WARNING LIGHT BOEING727 727264 138408MNM CARGO FIRE DET FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01765AT 23014 CARGO FIRE DETECTION FAULT LIGHT ILLUMINATED DURING FLIGHT. NO FAULT NOTED. CARGO DETECTION IN BAGGAGE AREA CHECKED NORMAL. DETECTION BOX SHOWS NO FAULTS. SYSTEM CHECKED NORMAL. REF M/M 26-00-00. 2L73 4F A3WE 20031223000742003122300074NM 2003 12 23 AWXA200301525 120031209A2820316A102035 LINE BOEING737 7373S3 1384711NM FUEL SYSTEM CHAFED A AWXAK NONE K FLUID LOSS ININSP/MAINT 1 WP28312AW 24060 LAS - FUEL LEAK - DURING B-3 CHECK FUEL WAS FOUND DRIPPING FROM RT ENGINE PYLON AFT DRAIN LINE, UPON FURTHER INVESTIGATION A FUEL LEAK WAS FOUND ON RT ENGINE FUEL FEED LINE AT 90 DEGREE ELBOW APPROXIMATELY 2 INCHES FROM ADEL CLAMP UNDER THE HOT AIR BLEED DUCT AND BELL CRACK MECHANISM AT WS 247. LEAK WAS CAUSED BY INBOARD SIDE OF -Y- DUCT CHAFING THROUGH ENGINE FUEL FEED LINE. MAINTENANCE REPLACED RT ENGINE FUEL FEED LINE IAW BMM 28-22-15, LEAK AND PRESSURE CHECKS WERE GOOD. 2L72 4F RTA16WE 20031223000982003122300098NM 2003 12 23 VNAA0311007 120031124A2720001A272A4020 LEVER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RUDDER CRACKED A VNAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL07430JS 3044 RUDDER PEDEL HAD EXCESSIVE PLAY BEFORE RUDDER MOVES. CAN NOT GET FULL LT DEFLECTION. MAINTENANCE INSPECTED AND FOUND SPRING TAB LEVER ASSY CRACKED AND REPLACED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031223001402003122300140CE 2003 12 23 DXTA200300190 120031124A2710666000161 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS BROKEN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07632QS 5605132 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001412003122300141CE 2003 12 23 DXTA200300182 120031125A2710666000164 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS BROKEN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07671QS 5605071 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031223001742003122300174EA 2003 12 23 ASOA03542 120031027A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52-00. (M) 2L72 4F RTA21EA 20040311000212004031100021NM 2004 3 11 ASAA0310259 120030327A523065468619 STOP FITTING BOEING737 737298C 1384490NM CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO DOORSTOP FITTING AT BS 440, STRINGER 23R GOUGED. REMOVED AND REPLACED FITTING PER SRM. (M) 2L72 4F RTA16WE 20040311000392004031100039NM 2004 3 11 ASAA0310142 120030316A5313 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 24R AT BS 1016 CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20040311000512004031100051NM 2004 3 11 ASAA0310135 120030311A78306573778 FAIRING BOEING737 737210C 1384459NM THRUST REVERSER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER FAIRING AT THRUST REVERSER STATION 185 DENTED. REMOVED AND REPLACED SKIN ON NR 1 ENGINE THRUST REVERSER FAIRING PER SRM. (M) 2L72 4F A16WE 20031125000752003112500075WP 2003 11 25 DHL2003807538 120031021A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD ACCESSORY COMPT FRAME CRACK 1.000 STA 55.000 L-24R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT FRAME CRACKED SEGMENT AND FABRICATED NEW FRAME SEGMENT AND 2EA SPLICE ANGLES IAW SRM 53-2-0 FIG 2. HEAT TREATED FRAME SEGMENT AND SPLICE ANGLES IAW SRM 51-1-1. CLEANED, TREATED AND PRIMED AREA, FRAME SEGMENT AND SPLICE ANGLES IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND SPLICE ANGLES APPLYING PRC SEALANT IAW SRM 53-2-0 FIG 2, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031125001192003112500119NM 2003 11 25 ASAA0310108 120030306A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 986.5-1006, RIGHT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20031125001222003112500122NM 2003 11 25 ASAA0310262 120030401A532065566562 FITTING BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIR TORQUE BOX AT BS 947-948, WATERLINE 206-208 CORRODED. REPLACED FITTING PER SRM. (M) 2L72 4F RTA16WE 20031125001232003112500123NM 2003 11 25 ASAA0310264 120030410A532069366771 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIR INTERCOSTAL ANGLE AT BS 847-986, WATERLINE 188-208 CORRODED. REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031125001302003112500130NM 2003 11 25 ASAA0310154 120030318A53156554908501 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 787, LEFT BUTTOCK LINE 65, RIGHT BUTTOCK LINE 65 CORRODED. REMOVED DAMAGED AREA AND REPAIRED TRACK PER EA. (M) 2L72 4F A16WE 20031125001692003112500169NM 2003 11 25 SWAA032497 120031111A335065C34691 LIGHT BOEING737 737317 138447PNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 13 ABC. SECURED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20031126000222003112600022EA 2003 11 26 QXEA200301405 120031029A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 CKB- DURING DNT INSPECTION OF THE PRESSURE BULKHEAD AT FS 1098.20 RIGHT HAND SIDE SHOWS INDICATIONS OF CRACK. REPAIRED IAW BOMBARDIER EO 670-53-61-034, AND HORIZON AIR EO 53-44B. 2L72 4F RTA21EA 20031126000232003112600023EA 2003 11 26 QXEA200301406 120031029A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 CKB- DURING INSPECTION OF THE PRESSURE BULKHEAD LEFT HAND SIDE, NDT SHOWED INDICATIONS OF CRACK. REPAIRED IAW BOMBARDIER EO 670-53-61-034 AND HORIZON AIR EO 53-44B. 2L72 4F RTA21EA 20031126000352003112600035NM 2003 11 26 AWXA200301388 120031021A5320654652816 ANGLE BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR ZEE ANGLE AT BS 520, RBL 20. MAINTENANCE CUT OUT DAMAGED SECTION OF ZEE ANGLE AT BS 520, RBL 20; FABRICATED A ZEE ANGLE AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW AWA ER 15-5327-03310-TB1. 2L72 4F RTA16WE 20031126000632003112600063CE 2003 11 26 DXTA200300168 120031122A3297 WIRE CESSNA650 650 2076802CE NLG BROKEN E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07797QS 6507097 AFTER TAKEOFF ATTEMPTED TO RETRACT GEAR AND FOUND GEAR HANDLE WOULD NOT COME UP. ACCOMPLISHED AIR TURNBACK TO HPN. INSPECTED WIRING IN NOSE WHEEL WELL, FOUND NOSE WHEEL OFF CENTERED SWITCH WIRES BROKEN AT PLUG JN2 PINS (A + B). REMOVED BROKEN WIRES FROM PLUG JN2 PINS (A + B), REPINNED PLUG JN2 PINS (A + B) IAW CESSNA 650 WIRE DIAGRAM MANUAL CHAPTER 32-50-01-01. PERFORMED GEAR RETRACTION CHECK IAW CESSNA 650 MM CHAPTER 32-00-01, NO DEFECTS NOTED AT THIS TIME. 2L72 4F A9NM 20031126000812003112600081SO 2003 11 26 C2XA03SH424 120031104A533014523058005 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE NICKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK, THE RIGHT SIDE OF THE FUSELAGE WAS FOUND TO BE NICKED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 53-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031202000332003120200033NM 2003 12 2 ASAA0310507 120030603A53306545829505 SKIN PANEL BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 DURING SCHEDULED C-CHECK, FOUND THE INTERNAL SKIN PANEL AT FUSELAGE STATION 334, STRINGER 28L CORRODED. REMOVED CORROSION AND REPAIRED SKIN PER SRM AND EA. (M) 2L72 4F RTA16WE 20031202000442003120200044NM 2003 12 2 USAASB03186 120031017A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031223001912003122300191WP 2003 12 23 GTIA030806 120031008A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 WEB FOUND CABIN STATION 207 STRINGER 15L AND 11L WEB CRACKED. FABRICATED WEB REPAIR. INSTALLED WEB REPAIR. (M) 2L72 4F A6WE 20031223001932003122300193WP 2003 12 23 GTIA030825 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 180, 0-36 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031224000162003122400016WP 2003 12 24 GTIA030800 120030831A5753 SKIN DOUG DC9 DC982 3022082WP RT WING TE FLAP CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND RT WING INBOARD FLAP TRAILING EDGE CRACKED AND DELAMINATED. REPAIRED RIGHT WING INBOARD FLAP TRAILING EDGE. (M) 2L72 4F A6WE 20031224000422003122400042WP 2003 12 24 AMTA200301335 120030923A5330 SKIN LKHEED1011 1011385115 5265015WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 193B1230 FOUND LOWER GALLEY BILGE CORRODED IN INNER SKIN AND HEAVY BULGING ON TEAR STRAP FS 854 RBL 28, ALSO 2 RIVET HEADS MISSING FROM OUTER SKIN. REPAIRED FUSELAGE SKIN IAW ER/A L10-53R-5328. (M) 2L73 4F A23WE 20031224000542003122400054WP 2003 12 24 MEX2003541 120031130A2821699151 STRAINER DOUG DC9 DC987 3022087WP RT ENGINE CLOGGED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23751RA 49779 AIRCRAFT RETURNED TO GATE DUE TO THE 'RT OIL STRAINER CLOGGING' CAME ON. STRAINER ASSY RESTRICTOR UNITS LPG AND LP5 AND THE OIL FILTER DIFFERENTIAL SWITCH WERE REPLACED AND THE ENGINE WAS TESTED IAW MM 79-35-01, 79-36-01 AND 79-20-06, ALL CORRECT. (M) 2L72 4F RTA6WE 20031229000642003122900064NM 2003 12 29 QXEA200301558 120031210A5753 FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 DAMAGE TO INBOARD FITTING OF OUTBOARD LUG ON NR 4 FLAP TRACK FITTINGS. REPAIRED IAW Q400 RD 8/4-57-228. 2H72 4T RTA13NM 20031229001042003122900104NM 2003 12 29 AWXA200301548 120031127A531065479576 BEAM BOEING737 737375 13844BNNM CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM BS 787-847, STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM BS 787-847, STR 25 RT; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20031229001112003122900111NM 2003 12 29 AWXA200301555 120031125A53126516300 BULKHEAD BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 LCQ - MAJOR REPAIR - DURING C-04 CHECK A .625 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 13.5, WL 183. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT LBL 13.5, WL 183; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08 PG 1, FIG 203. 2L72 4F RTA16WE 20031229001142003122900114NM 2003 12 29 SWAA032720 120031212A57436582770 FITTING BOEING737 737301 1384611NM LT MLG CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C4 CHECK, FOUND LT MLG ACTUATOR BEAM HANGER FWD MOUNT FITTING CRACKED. REMOVED AND REPLACED HANGER MOUNT FITTING PER MM. 2L72 4F RTA16WE 20031229001262003122900126EA 2003 12 29 MASA200300476 120031203A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER L NO TEST ININSP/MAINT 1 SW0727173 7173 AN EXTERNAL FUSELAGE EMERGENCY EXIT LIGHT INOP. MAINT RELAMPED THE LAMP. 2L72 4F RTA21EA 20031229001372003122900137NM 2003 12 29 SWAA032732 120031214A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 927, STRINGER 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031229001482003122900148WP 2003 12 29 UPS03841664 120031212A3350 LIGHT DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:N/A EMERGENCY LIGHTS ON. PACK REPLACED PART. 2L74 4F RT4A25 20031229001572003122900157EA 2003 12 29 SWIA200312662 120031205A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 460 RIGHT FLOORBEAM RBL 9.0 O/B FITTING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21 & RII 53-401. 2L72 4F RTA21EA 20031229001642003122900164NM 2003 12 29 03FDEA02207 120031217A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE L NO TEST ININSP/MAINT 1 SO25287FE 21849 STRINGER 27R CORRODED AT BS 740. 2L73 4F RTA3WE 20031229001672003122900167NE 2003 12 29 03FDEA02203 220031217A7230 CASE DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE COMPRESSOR CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 NEW ENGINE AT 4 O'CLOCK AFT FAN CASE AREA FOUND CHAFING MARK. CHAFING MARK AT NR 3 ENGINE ON 4 O'CLOCK POSITION, AFT FAN CASE 'T' RIB SMOOTHED OUT WITH FINAL DIMENSION : LENGTH = 0.470, WIDTH = 0.300 AND DEPTH APPROX. = 0.120, FOUND WITHIN LIMITS AS PER GE MANUAL 72-23-01. 2L73 4F4 FRTA22WE E31N3 20031202001112003120200111SO 2003 12 2 SIMA200329703 120031021A531514525381003 FLOORBEAM EMB 145 EMB145 3260210SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING AN MBV INSPECTION, FOUND CORROSION ON LEFT FLOORBEAM, PREV REPAIR, AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO UPPER DOUBLER ANGLE OF PREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE. REPAIR DONE IAW EMB 145, SRM 145/1142 REV 23, CHAPTER 53-21-10 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031202001172003120200117NM 2003 12 2 GAIA03116OP 120031025A33501000679 LIGHT BOEING727 727224 1384076NM L1 DOOR INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW0779748 22450 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031202001192003120200119SO 2003 12 2 SIMA200329701 120031021A5347 SEAT TRACK EMB 135 EMB135KL 3260302SO COCKPIT DIRTY A SIMAK NONE O OTHER ININSP/MAINT 1 SW21830AE 145615 FIRST OFFICERS SEAT DIFFICULT TO LOCK IN PLACE. SEAT MOVED BACK IN FLIGHT. CLEANED DEBRIS FROM SEAT TRACK, OP CHECK GOOD. (M) 2L72 4F RTT00011AT 20031202001412003120200141EA 2003 12 2 A6WA200340153 120031028A5753 FITTING CNDAIRCL600 CL6002B19 1900309EA TE FLAP DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RIGHT WING FLAP HINGE FITTING ASSEMBLY AT WS 178, P/N 601R10088-8 LOWER SURFACE FORWARD EDGE HAS MUSHROOMED METAL AND GOUGES. BLENDED AREAS SMOOTH, PERFORMED EDDY CURRENT INSPECTION OF AREAS, PERFORMED ROTO/FLAP PEEN OF REPAIR AREAS AND RESTORED ORIGINAL FINISH IAW WVAC EO 601R-57-4318 B. (M) 2L72 4F RTA21EA 20031202000692003120200069EU 2003 12 2 USAASA03121 120031016A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGNECY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19116US 1210 RIGHT MID EPSU FAILED TEST. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA28NM 20031202000802003120200080NM 2003 12 2 USAABB03199 120031025A2780 POWER SUPPLY BOEING767 767201 1385125NM SLAT SYSTEM FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19645US 23897 AFTER TAKEOFF, CREW RECEIVED THE EICAS MESSAGE 'LE SLAT DISAGREE' AND THE ASSOCIATED LIGHT. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A BITE OF THE FSCU AND PSEU. NO PROBLEMS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR FLIGHT. (M) 2L72 4F RTA1NM 20031202000822003120200082NM 2003 12 2 USAA030209 120030922A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48518 23319 FOUND STRINGER CRACKED 3 INCHES, BS 520 STRINGER 12 RT. INSTALLED DOUBLER PER EA 77007. (M) 2L72 4F RTA16WE 20031202001092003120200109EA 2003 12 2 ASOA03508 120031003A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11861AS 7445 DURING APPROACH INTO DFW FROM DTW, THE CREW NOTICED A BURNING SMELL IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031202001462003120200146SO 2003 12 2 SIMA200328805 120031008A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 DURING AN IMBV INSPECTION, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED THE CORROSIN BY CREATING A CUT OUT IN THE DAMAGED FLANGE AND WEB OF THE LEFT OMEGA BEAM. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3320, EMB SRM, SRM 145/1142 REV 23, CHAPTERS 53-21-1, FIG 201 SHEET 1 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031202001592003120200159 2003 12 2 2003F00603 420030901A23307002246001 ELECTRICAL BOX BOEING737 737800* NM SEAT ROW 21 BURNED A MYWAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO19733MA 30619 DURING PREFLIGHT TRANSIT CHECK, SMELLED SMOKE AT ROW 21 ENTERTAINMENT SYSTEM. TROUBLESHOT SYSTEM. FOUND BURNED OUT SEAT ELECTRONIC BOX AT ROW 11DEF. REMOVED AND REPLACED SEAT ELECTRONIC BOX AT ROW 11 DEF. ENTERTAINMENT SYSTEM CHECKED NORAML IAW 23-34-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031203000032003120300003EU 2003 12 3 AALA20031071 120030925A5610PPGNP1752013 WINDOW AIRBUS300 A300B4605R 3930308EU COCKPIT CRACKED A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW2170072 515 CAPTAIN'S L1 WINDSCREEN DEVELOPED ARCING IN THE OUTER PAIN. WINDOW CRACKED SEVERELY. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED CAPTAINS WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031203000082003120300008SO 2003 12 3 SIMA200328801 120031010A5350 RADOME EMB 145 EMB145LR 3260212SO FUSELAGE BIRD STRIKE A SIMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW21618AE 145097 DURING TAKEOFF FROM BUF, CREW REPORTED A BIRD STRIKE TO THE NOSE AREA. MAINTENANCE REMOVED AND REPLACED FRAMES 3, 4, 5 AND 6, STRINGER 4R, RIGHT FORWARD NOSE TOP SKIN PANEL, RIGHT AFT NOSE TOP SKIN PANEL IAW EMB SRM 51-42-01 AND REPAIRED SKIN FORWARD OF RIGHT WINDSHIELD AFT OF FRAME 6 BETWEEN STRINGERS 4R AND 6R IAW EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031203000112003120300011NM 2003 12 3 AALA20031111 120031007A3350 BATTERY BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21362AA 24043 EMERGENCY ESCAPE FLASH LIGHT INOPERATIVE AT AFT FLIGHT ATTENDANT SEAT. REPLACED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203000262003120300026NM 2003 12 3 GAIA03125ST 120031024A5313BAC1498132 STRINGER BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND STRINGER 15 RT CRACKED AT BS 720B PLUS 10. REF FASI N/R NR 61422, INSTALLED DOUBLER REPAIR PER B727 SRM 53-10-3 FIG 5. (M) 2L73 4F RTA3WE 20031203000302003120300030EU 2003 12 3 COEA0303742 120031024A3230200798304 LINKAGE FOKKERF27 F27MK600 4990706EU MLG BROKEN A COEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM13742FE 10349 AFTER TAEKOFF, THE NOSE WHEEL FAILED TO UNLOCK FOR RETRACTION. CREW ELECTED TO RETURN TO RAP, NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND EYE END BROKEN THAT CONNECTS TO GEAR UNLOCK LATCH. REMOVED AND REPLACED EYE END. A/C RETURNED TO SERVICE. (M) 2H72 4T A817 20031203000602003120300060EU 2003 12 3 A6WA200360055 120031015A5280 RIVET BAG BAE146BAE146200A 1500266EU RT MLG DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31183US E2043 RT MLG DOOR RIVETS, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830003. (M) 2H74 4F RTA49EU 20031203000702003120300070NM 2003 12 3 USAA030208 120030515A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US42530 23314 PIT - FOUND ON WALKAROUND SKIN AND KEEL BEAMS CORRODED 1 FT BY .5 INCH AREA, AT FASTENERS STATION 727, L STR 27 AND R STR 28. REPLACED LEFT AND RIGHT BEAMS SPLICED AT STATION 540 PER TYP REP 53-60-07 AND EA 76192. CORROSION LEVEL 2, TASK NR C53-212-01. (M) 2L72 4F RTA16WE 20031203000712003120300071NM 2003 12 3 AALA20031132 120031010A5210 PUSHROD BOEING767 767323 1385205NM PAX DOOR OUT OF ADJUST A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21352AA 24033 AIRCRAFT CLIMB-OUT FROM EZE CREW OBSERVED L1 DOOR AIR LEAK. LANDED EZE WITH IN NORMAL WEIGHT LIMITS. ACCOMPLISHED OVERCENTER PUSHROD MECHANISM ADJUSTMENT TO L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203000742003120300074 2003 12 3 2003F00620 420031013A34212588423905 AMPLIFIER FOKKERF27 F27MK500 4990629EU ATTITUDE IND INOPERATIVE A COEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM13711FE 10383 ON TAKEOFF FROM ANCHORAGE, THE RT ATTITUDE INDICATOR FAILED, RIGHT AFTER ROTATION. THE AIRCRAFT RETURNED TO ANC. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. THE RACK INSTRUMENT AMPLIFIER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A817 20031203000942003120300094SW 2003 12 3 2003F00629 120030811A5270 WARNING LIGHT FRCHLDSA227 SA227DC 3377521SW CARGO DOOR FALSE INDICATIONA BSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM05853LS DC853B CARGO DOOR WARNING LIGHT CAME ON AT FL120, CREW FOLLOWED CHECKLIST PROCEDURES AND RETURNED TO STATION. SUSPECT DOOR CLOSING PROCEDURES OR DOOR IS HARD TO CLOSE. NO DEFECT WAS FOUND. MAINTENANCE DISPATCHED FROM MAIN BASE TO INSPECT AND EVALUATE. VISUALLY INSPECTED CARGO DOOR RODS AND CLICK CLACKS, DOOR OPS CHECKED REPEATED TIMES, NO DEFECTS NOTED AT THIS TIME. NO FURTHER DISCREPANCIES HAVE BEEN RECORDED ON THIS AIRCRAFT SINCE THIS DISCREPANCY. (M) 2L72 4T RTA18SW 20031203000982003120300098NM 2003 12 3 USAASB03193 120031026A2697 WIRE HARNESS BOEING737 7373B7 1384580NM E/E BAY MELTED A USAAO OTHER MJ OVER TEMP WARNING INDICATION APAPPROACH 1 EA19521AU 23856 ON APPROACH TO CLT, AT 1,500 FT, ENTIRE FIRE CONTROL PANEL ILLUMINATED & ALL FIRE BELLS SOUNDED EXCEPT FOR APU. CREW ALSO RECEIVED A LT WING BODY OVERHEAT INDICATION. CREW COULD NOT SILENCE BELLS OR EXTINGUISH LIGHTS. CABIN CREW VERIFIED NO SMOKE PRESENT, NOTED CABIN LIGHTS BLINKING. FLT LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINT FOUND WIRE BUNDLES MELTED & BURNED BEHIND EQUIPMENT RACK E3. REWIRED BUNDLES PER SWPM & EA NR 94861. OPS CHECKED ENG FIRE WARNING SYS PER MM & APU FIRE WARNING SYS PER MM. OPERATIONALLY CHECKED EQUIPMENT COOLING SYSTEM PER MM & WINDOW HEAT SYSTEM PER MM. ALL OPERATIONALLY CHECKED GOOD. ALSO, R & R FAULTY FIRE DETECT MODULE, PER MM. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031203001012003120300101NM 2003 12 3 USAA030234 120031022A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48590 23319 FOUND SKIN CRACKED 1.1 INCH, STATION 754 ABOVE S21R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20031203001052003120300105NM 2003 12 3 USAA030226 120031103A5320 WEB BOEING737 7373B7 1384580NM FUSELAGE FLOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU48203 23595 FOUND WEB CRACKED, FLOOR WEB BETWEEN STATION 616 AND 639 S17L. REMOVED AND REPLACED WEB PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20031203001342003120300134EU 2003 12 3 A6WA200360049 120031004A2731 SERVO BAC 146 146200A 1500266EU ELEVATOR TAB DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 LT AND RT ELEVATOR SERVO TABS MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810005. (M) 2H74 4F A49EU 20031203001392003120300139NM 2003 12 3 AMTA200301261 120031001A33501010428 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 EGRESS LIGHTS ON OVERHEAD BIN AT ROW 9ABC AND 14ABC ARE INOPERATIVE. FOUND LIGHT AT 9ABC SHORTED CAUSING BOTH LIGHTS TO FAIL. INSTALLED NEW LIGHT ASSEMBLY AT SEAT 9ABC IN OVERHEAD BIN BULLNOSE IAW AMM 33-51-05-2 AND BOTH LIGHTS. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20031203001682003120300168WP 2003 12 3 GTIA030898 120031101A7120K22199SA31 ISOLATION MOUNT DOUG DC9 DC981 3022081WP ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 RIGHT ENGINE FORWARD UPPER VIBRATION ISOLATOR NEEDS TO BE REPLACED. REMOVED AND REPLACED RIGHT ENGINE FORWARD UPPER VIBRATION ISOLATOR. (M) 2L72 4F A6WE 20031203001712003120300171WP 2003 12 3 GTIA030885 120031009A7120K22199SA31 YOKE DOUG DC9 DC982 3022082WP ENGINE MOUNT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - NR 2 YOKE ASSEMBLY UPPER ISOLATOR CONICAL SURFACE WORN. REMOVED NR 2 UPPER FORWARD ISOLATOR. INSTALLED NEW ISOLATOR. UPON INSTALLATION OF YOKE ASSEMBLY FOUND UPPER ISOLATOR INNER ASSEMBLY LOOSE. FOUND ISOLATOR INNER ASSEMBLY STILL LOOSE. REMOVED UPPER YOKE PLATE AND ISLOATOR. REMOVED NR 2 ENGINE PYLON YOKE. INSTALLED SERVICEABLE YOKE PLATE AND ISOLATOR. INSTALLED NR 2 YOKE ASSEMBLY. (M) 2L72 4F A6WE 20031203001762003120300176WP 2003 12 3 GTIA030865 120031025A3260 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23804NK 49104 NOSE GEAR RED INDICATOR LIGHT REMAINED ON FOR APPROX 3 MINUTES AFTER GEAR EXTENSION NLG INDICATOR FULLY EXTENDED. INSPECTED AND CLEANED NOSE GEAR PROX SENSORS JACKED NOSE GEAR AND PERFORMED RETRACTION SEVERAL TIMES. GEAR LIGHTS OPERATED NORMAL. (M) 2L72 4F A6WE 20031203001772003120300177WP 2003 12 3 GTIA030895 120031105A2120 ODOR DOUG DC9 DC982 3022082WP CABIN DETECTED A GTIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL23820NK 49126 LEFT AND RIGHT AIR COND SUPPLY TEMP HIGH LIGHTS CAME ON WITH BURNING ODOR IN CABIN WHEN AIRFOIL ANTI-ICE TURNED ON. ACCOMPLISHED QRH PROCEDURES LIGHTS WENT OUT, CONTINUED FLIGHT. PER COMPANY REQUEST AND ITEM ABOVE PERF EXTRA ENGINE RUN UP AT CRUISE PLUS POWER. PERFORMED TEST DISTRIBUTION SYSTEM, ICE PROTECTION SYSTEM OPERATION WITH BOTH ENGINE RUNNING. OPERATIONAL CHECK GOOD. ACCOMPLISHED TEST DISTRIBUTION SYSTEM, ICE PROTECTION SYSTEM. NO BURNING ODOR NOTED PLUS AIR CONDITION SUPPLY TEMP HIGH LIGHT NEVER CAME ON. FOUND AIRFOIL ANTI-ICE SYSTEM NORMAL. (M) 2L72 4F A6WE 20031204000032003120400003WP 2003 12 4 GTIA030889 120031026A3397 WIRE DOUG DC9 DC982 3022082WP RT OVERWING BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND FORWARD RIGHT OVERWING EXTI LIGHT INOPERATIVE. T/S FOUND BROKEN WIRE. REPAIRED WIRE. (M) 2L72 4F A6WE 20040120000212004012000021NM 2004 1 20 DHL2003781006 120031217A2897 WIRE BOEING727 727227 1384078NM PRESSURE SWITCH CHAFED A DHLAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01781DH 21996 ON PRE-DEPARTURE CHECK NOTICED SMOKE EMANATING BEHIND NR 2 KRUEGER FLAP. FOUND WIRE CHAFING AGAINST TANK NR 2 FWD LT FUEL PRESSURE SWITCH TUBE. REPAIRED WIRE, NOTICED TUBE HAD CHAFED THRU. REPLACED TUBE. LEAK CHECKED GOOD REPLACED SEVERAL SUSPECT ADEL CLAMPS. FOUND PORTION OF WIRE NR 260-003-20 UNDER NR 2 KRUEGER DEFECTIVE. REPLACED APPROXIMATELY 4 FEET OF WIRE.DURING OPS CHECK OF BOOST PUMP PRESSURE SWITCH FUELING GAGE CIRCUIT BREAKER IN E&E BAY WOULD NOT RESET. REPLACED CIRCUIT BREAKER. EDDY CURRENT CARRIED OUT IN AFFECTED AREA. 2L73 4F A3WE 20040120000302004012000030NM 2004 1 20 03FDEA02296 120031226A5350AKC75067 PANEL DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT TAILCONE UPPER DOOR FORWARD MOST ACCESS PANEL FOUND CHAFED. RT TAILCONE UPPER DOOR FWD MOST ACCESS PANEL FABBRICATED AS PER DWG AKC 7506. PANEL REMOVED AND REPLACED AS PER MM 20-50-02. 2L73 4F4 FRTA22WE E13NE 20040120000332004012000033NM 2004 1 20 03FDEA02292 120031229A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, OB FLAP, IB HINGE FITTING OB PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F4 FRTA22WE E13NE 20040120000342004012000034NM 2004 1 20 03FDEA02245 120031226A5744ARC7484 FITTING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, IB FLAP VANE IB UP STOP FITTING ATTACHMENT BORE CORRODED. LT WING - I/B FLAP VANE I/B UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F4 FRTA22WE E13NE 20040120000492004012000049NM 2004 1 20 03FDEA02291 120031229A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP I/B HINGE FITTING O/B PIVOT I/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200. TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040120000542004012000054NM 2004 1 20 03FDEA02228 120031223A5753ARC2512503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 SNRM N0586: LT WING - IB FLAP OB HINGE FITTING IB PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75212, TRAILING EDGE AND TRAILING EDGE DEVICES. LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040120000592004012000059NM 2004 1 20 03FDEA02286 120031229A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP I/B HINGE ACTUATOR I/B MOUNT O/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200 - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040114001442004011400144NM 2004 1 14 DL738031073 120031209A2621 BUTTON BA24180R1 BOEING737 737832 13844CFNM FIRE BOTTLE MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO273748Y 19365 30489 COCKPIT HALON BOTTLE GREEN BUTTON MISSING. REPLACED SAME. 2L72 4F RTA16WE 20040114001632004011400163NM 2004 1 14 03FDEA02015 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT O/B FLAP, O/B HINGE ACTUATOR HOLE NR 1 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000052004011500005NM 2004 1 15 03FDEA02020 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 3 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000072004011500007NM 2004 1 15 03FDEA02022 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 3 I/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000382004011500038NM 2004 1 15 03FDEA02050 120031204A5310 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 WHILE WORKING FOUND UPPER FLANGE OF FRAME BS 1090 LBL 18 WL 150 TO BE TRIPLE HOLED. REMOVED DAMAGE ON UPPER FLANGE OF FRAME BS 1090, LBL 18, WL 150. INSTALLED NEW FABRICATED DOUBLER FOR FRAME AT BS 1090, WL 150, LBL 18 IAW SRM 51-40-3. 2L73 4F RTA3WE 20040115000552004011500055NM 2004 1 15 DL78K031081 120031213A2751 INDICATOR BOEING737 737832 13844CFNM COCKPIT DEFECTIVE A DALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO27398DA 30774 ON FINAL 9R ATL WHEN LANDING FLAPS WERE SELECTED 40, FLAP INDICATOR ONLY SHOWED FLAPS AT 15. EXECUTED A GO-AROUND AND TRIED TO RAISE FLAPS TO 10, FLAPS STAYED AT 15. ACCOMPLISHED 15 FLAP LANDING. TROUBLESHOT WITH NTF. REPLACED INDICATOR. 2L72 4F RTA16WE 20040115002112004011500211NM 2004 1 15 FDE2004F00000 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM BANJO FITTING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LOWER SECTION OF NR 1 BANJO FITTING (AJC7051-505 ) AFT FACE FLANGE FOUND WITH 02 EA LOCKBOLT COLLARS CRACKED (GAIN ACCESS FROM PNL 364AR). RIGHT LOWER SECTION OF NR 1 BANJO FITTING (AJC7051-505 ) AFT FACE FLANGE 02 EA CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL II AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040116000162004011600016NM 2004 1 16 03FDEA02194 120031215A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RIGHT WING - INBOARD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES (3) FOUND EXCEED LIMIT. RT WING - INBD FLAP VANE, OUTBD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-75176, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT INBD. FLAP VANE ATTACH FITTINGS REWORK. 2L73 4F RTA22WE 20040116000172004011600017NM 2004 1 16 03FDEA02196 120031214A5320ACA70494 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 FORWARD CARGO RIGHT TUNNEL BETWEEN STA 6-30 TO STA 6-50 AROUND NR 41 LONGERON, INTERCOSTAL FOUND CRACKED. REMOVED CRACKED INTERCOASTAL AS PER SRM 51-31-01, VOL.II AND FABRICATED NEW INTERCOASTAL AS PER DRAWING ACA7049. INSTALLED NEW INTERCOASTAL AT FORWARD CARGO R/H TUNNEL BETWEEN STA 6-30 TO STA 6-50 AROUND NO. 41 LONGERON AS PER SRM 51-31-01, VOL.II. 2L73 4F RTA22WE 20040120000062004012000006NM 2004 1 20 03FDEA02205 120031217A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 WHILE WORKING FOUND DAMAGED SHEAR TIE AT BS 720A LBL 12 WL 156. REPAIRED SHEAR TIE AT BS 720A, LBL 12, WL 156 PER SRM 53-10-4 FIG 15 AND FED EX EA 7-5310-55179. 2L73 4F RTA3WE 20040121000162004012100016NM 2004 1 21 03FDEA02272 120031226A5744ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING - O/B FLAP O/B HINGE ACTUATOR O/B MOUNT LUG I/B AND O/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES- RT OUTBOARD. FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000192004012100019NM 2004 1 21 03FDEA02275 120031226A5744ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING O/B FLAP O/B HINGE FITTING O/B MOUNT I/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD. FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000442004012100044NM 2004 1 21 ASAA0310181 120030321A5315 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND FLOORBEAM AT BS 1016, LT BUTTOCK LINE 8, LEFT BUTTOCK LINE 13 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040121000702004012100070EA 2004 1 21 ASOA03611 120031201A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040121000752004012100075EA 2004 1 21 ASOA03618 120031202A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11907EV 7648 DURING A C-CHECK IN MCN, THE CARGO AFT WALL FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO AFT WALL FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT SIDE IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040121000802004012100080EA 2004 1 21 ASOA03608 120031129A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11856AS 7404 DURING A GROUND INSPECTION IN MTY, THE PASSENGER DOOR BOTTOM STEP BRACKET WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121000862004012100086SO 2004 1 21 SIMA200332704 120031120A272015793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO RUDDER INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21619AE 145101 DURING CRUISE FILGHT CRWE REPORTED THE RUDDER 1/2 TO BE INOPERATIVE. AIRCRAFT WAS DIVERTED TO STL AND LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040121000892004012100089EA 2004 1 21 A6WA200340189 120031210A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 FOUND FS 640 LT SIDE BETWEEN STRINGER 9 AND STRINGER 17 CRACK ON DOUBLER. INSPECTED AND REPAIRED DOUBLER AS BOMBARDIER SB 601R-53-061. (M) 2L72 4F RTA21EA 20040121000902004012100090EA 2004 1 21 A6WA200340192 120031209A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31434AW 7322 AFTER TAKEOFF AND GEAR RETRACTION GOT RED DISAGREE ALONG WITH GEAR DOWN, GOT THREE GEAR DOWN INDICATORS AND RETURNED TO DAY. REMOVED AND REPLACED MLG SELECTOR VALVE IAW MM 32-32-10. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040121001002004012100100NM 2004 1 21 UIEA200300065 120031119A7603 THROTTLE BOEING747 7472D7B 1384803NM NR 3 ENGINE STUCK A UIEAE ENGINE SHUTDOWN F FLT CONT AFFECTED DEDESCENT 1 EA15526MC 22337 NR 3 ENGINE THROTTLE STUCK AT POSITION IT WAS IN AT CRUISE POWER. IT FINALLY CAME LOOSE AT 10,000 FT. SHUT DOWN ENGINE AT 10,000 FT AND RESTARTED BETWEEN 10,000 FT AND 4,000 FT. OPERATED OK AFTER START. INSPECTED NR 3 ENGINE FOR WINDMILLING PER MM 72-00-00 PATE 682, NO DEFECTS NOTED. INLET AND EXHAUST INSPECTED AND THROTTLE FEEDBACK CABLE CLEANED CLEANED PER MM 72-00-00. ENGINE RUN COMPLIED WITH PER MM 73-00-00, NO DEFECTS NOTED. OK FOR CONTINUED SERVICE. (M) 2L74 4F RTA20WE 20040122000012004012200001NM 2004 1 22 03FDEA02303 120031226A5350AKC75981 PLATE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 TAILCONE AFT SNUBBER TOP AND BOTTOM SUPPORT PLATE FOUND WORN. REMOVED WORN SUPPORT PLATE AS PER SRM 51-31-01 VOL. II AND INSTALLED NEW SUPPORT ASSY AT TAILCONE AFT SNUBBER TOP AND BOTTOM AS PER SRM 51-35-01 VOL. II. 2L73 4F4 FRTA22WE E13NE 20040122000042004012200004NM 2004 1 22 03FDEA02297 120031226A5350AKC75287 BEAM DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 TAILCONE UPPER DOOR CUTOUT AFT HORIZONTAL BRACKET LT AND RT AREA ADJACENT TO TAIL CONE LADDER SUPPORT FITTING FOUND CHAFED. REMOVED CHAFED SUPPORT AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW BEAM AS PER DRAWING AKC 7528. INSTALLED BEAM AT TAILCONE UPPER DOOR CUT- OUT AFT HORIZONTAL TO TAILCONE AS PER SRM 51-31-01 VOL. II. 2L73 4F4 FRTA22WE E13NE 20040115001272004011500127NM 2004 1 15 03FDEA02105 120031207A1430ARC7053503 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040115001402004011500140NM 2004 1 15 03FDEA02149 120031209A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25276FE 22041 CRACKED FRAME AT BS 640, RBL 9, WL 155.5. CUT OUT CRACK ON FRAME AT BS 640, RBL 9, WL 155.5. REMOVED 2 X 2 INCHES. FABRICATED REPAIR PARTS FROM 7075-T6 .063 LOT 516678. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30- 2, 53-10-1, 51-40-3. 2L73 4F RTA3WE 20031229001682003122900168NM 2003 12 29 03FDEA02202 120031216A3230 ACCESSORY UNIT BOEING727 727200 138407ENM MLG FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25483FE 21465 AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT RAISE PAST THE OFF POSTION. RT GEAR DOOR LIGHT WAS ILLUMINATED. PERFORMED LANDING GEAR LEVER LATCH FAILED TO RELEASE CHECKLIST. AURAL WARNING HORN SOUNDED WHEN CHECKLIST CALLED FOR RAISING FLAPS TO 2 DEG. RECONFIGURED AND LANDED AT DEPARTURE AIRPORT. LANDING GEAR ACCESSORY UNIT FAILED AIR SENSING TEST. SUSPECT LANDING GEAR ACCESSORY UNIT BAD OR AIR SENSING SWITCH IN GEAR WELL. ORDERED PARTS REF WDM 32-31-01 PAGE 5. RANG AIR SENSING SENSOR AT D1890B FROM PINS 35 AND 36. FOUND SENSOR NG REMOVED AND REPLACED AIR SENSOR PER 32-09-221-4. PERFORMED ALTERNATE TEST PROCEDURE PER EA 7-3210-75019. OPS CHECK WAS NORMAL. 2L73 4F RTA3WE 20031229001722003122900172EU 2003 12 29 009491 120031217A3150 WARNING LIGHT SAAB SF340 SF340A 7850100EU FLT IDLE STOP ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17146SD 146 FLIGHT IDLE STOP LIGHT OPEN ILLUMINATED AFTER ROTATION. AIRCRAFT RETURNED TO PIT. TAKEN OUT OF SERVICE 12/17/03 AT 15:15. 2L72 4T RTA52EU 20031229001742003122900174NE 2003 12 29 SWIA200312669 220031206A7200 ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LEFT FLAMED OUT A SWIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 NM07196SW 120151 LEFT ENGINE FLAMEOUT ON TAKEOFF AT 50 FEET AGL. RETURNED TO DEN. REMOVED AND REPLACED LEFT ENGINE ASSY PER MM 71-00-00. ENGINE S/N AP0018 SHUT ITSELF DOWN DUE TO A FAILED NR 29 BEARING. 2L72 4T4 TRTA31SO E20NE 20031229001752003122900175SO 2003 12 29 SWIA200312670 120031114A2720 PIN EMB 120 EMB120ER 3260203SO RUDDER ROD FROZEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07568SW 120343 FORWARD FEEDBACK ROD (RUDDER) CONCENTRIC PIN FROZEN WITHIN BOLT. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FORWARD FEEBACK ROD (RUDDER) CONCENTRIC PIN AND BOLT WITH SERVICEABLE UNIT IAW EMB120 MM 27-21-00. 2L72 4T RTA31SO 20031223001332003122300133EU 2003 12 23 MALA030535 120031201A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 10F FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 10F IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001942003122300194WP 2003 12 23 GTIA030824 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FLT COMPARTMENT FLOOR SUPPORT CORRODED AT FS 160 0 INCHES TO 11 INCHES LBL. REMVOED FLOOR SUPPORT. FABRICATED NEW PART. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031224000502003122400050NM 2003 12 24 AALA20031257 120031110A2934019012001 TRANSMITTER BOEING757 757223 1384957NM LT HYD QTY INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21671AA 25336 EN ROUTE LT HYD QTY LIGHT ILLUMINATED. LANDED ORD WITHOUT INCIDENT. REPLACED LT HYD QTY TRANSMITTER PER MM 29-33-01-4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031224000562003122400056 2003 12 24 2003F00659 420031119A2565 SLIDE BOEING757 757236 1384971NM L1 DOOR DISLODGED A P9RAK NONE O OTHER ININSP/MAINT 1 SO11958PG 24118 L1 DOOR SLIDE FOUND OUT OF CASING. REMOVED AND REPLACED L1 DOOR SLIDE HARNESS ASSEMBLY IAW BMM 32-32-12. (M) 2L72 4F RTA2NM 20031224000622003122400062NM 2003 12 24 2003F00655 120031120A3350BPS73 POWER SUPPLY BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE O OTHER ININSP/MAINT 1 SO11522NA 25133 EMERGENCY LIGHT ABOVE R2 DOOR INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW 33-50-0. (M) 2L72 4F RTA2NM 20031229000252003122900025GL 2003 12 29 C2XA03TY208 220031214A753232158861 BLEED VALVE EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW2727506 145192 AIRCRAFT ABORTED TAKEOFF FOR NR 1 BLEED INDICATION. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE BLEED VALVE. OPERATIONAL CHECKED GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031229001132003122900113EU 2003 12 29 MALA030548 120031210A7930523535 SENSOR SAAB SF340 340B 7860101EU OIL TEMP MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15427XJ 340B427 DURING FLIGHT 3230, LT PROP OIL TEMP GUAGE IS FLUCTUATING BETWEEN NORMAL AND FULL HOT WITH TORQUE AT 60 PERCENT AND HIGHER SETTINGS. ALL OTHER INDICATIONS ARE NORMAL. AIR RETURN TO MEM. MAINTENANCE OHMED OUT WIRE TO WHITE HARNESS AT PGB OIL TEMP SENSOR, FIRE WALL AND WING ROOT. WIGGLED WIRES, ALL CHECKS GOOD. CLEANED CONNECTOR AT PGB OIL TEMP SENSOR REMOVED AND REPLACED LT PGB PRESS/TEMP INDICATOR IAW AMM 79-30=15-2 P/N 523535, S/N OFF 9803696A, S/N ON 221. RAN AC FOR 30 MINUTES VERY SLIGHT MOVEMENT IN NEEDLE, ALWAYS IN GREEN. 2L72 4T RTA52EU 20031229001192003122900119NM 2003 12 29 SWAA032725 120031214A53116545812 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED 1/4D CHECK, FOUND FWD R1 DOOR UPPER HINGE CUTOUT SHOWS CRACK INDICATION. REPAIRED R1 DOOR PER SB. 2L72 4F RTA16WE 20031229001242003122900124 2003 12 29 SWAA032730 420031214A2565DS31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 L2 DOOR SLIDE PRESSURE GAUGE IN THE RED. REMOVED AND REPLACED L2 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20031231000032003123100003WP 2003 12 31 GTIA030908 120031106A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND FLOOR PANEL RT STATION 130-135 INSERT BROKEN OUT. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20031231000042003123100004EA 2003 12 31 ASOA03565 120031104A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040115001412004011500141NM 2004 1 15 DL757031106 120031218A3810 WATER HEATER BOEING757 75726D 1384907NM LAVATORY OVERHEATED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27900PC 28446 FLIGHT ATTENDANT REPORTED, SMOKE, HAZE AND HEAT FROM 1ST CLASS LAV. FOUND WATER HEATER OVERHEATING AND SMELL OF BURNING PLASTIC. REPLACED HEATER. 2L72 4F RTA2NM 20040115001432004011500143NM 2004 1 15 DL73S031108 120031217A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 867. THE CRACK WAS REMOVED WITH A CUTOUT TO THE SKIN WITH ADDITIONAL INSPECTIONS TO ENSURE NO FURTHER CRACKS. THE AREA WAS REPAIRED PER B737 SRM 53-30-3, FIG 42 AN DOCUMENTED PER ER/A 087963-14AD. 2L72 4F RTA16WE 20040115001552004011500155NM 2004 1 15 03FDEA02156 120031209A5320 INTERCOSTAL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION ON INTERCOSTAL, BS 312-344, LBL 29, WL 208. REMOVED CORROSION ON INTERCOSTAL STA 312-344, LBL 29, WL 208. REMOVED .001 1X1 INCH FROM .075. IN LIMITS. REMOVED CORROSION ON SHIM STA 328-344, LBL 29, WL 208. REMOVED .013 1 X1 INCH FROM .100. OUT OF LIMITS. FABRICATED & INSTALLED NEW SHIM. 2L73 4F RTA3WE 20040120000432004012000043NM 2004 1 20 03FDEA02334 120031230A5321 FLOOR PANEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 FLOOR PANEL 232PF FOUND TOP SURFACE CORROSION. DAMAGED FLOOR PANEL NR 232PF REMOVED AND REPLACED AS PER MM 53-21-04-4. 2L73 4F RTA22WE 20040120000502004012000050NM 2004 1 20 03FDEA02290 120031229A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP I/B HINGE FITTING I/B PIVOT I/B AND O/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200. WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121001102004012100110NM 2004 1 21 03FDEA02343 120031229A5750ARC7717512 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING O/B FLAP I/B HINGE (WING SIDE) FAIRING SUPPORT FWD I/B BRACKET FOUND CRACKED. REMOVED & REPLACED AS PER AMM 20-50-02. 2L73 4F RTA22WE 20040122000072004012200007EA 2004 1 22 SWIA200312727 120031224A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 FS 484 RT INTERCOSTAL I/B CLIP RBL 27 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CLIP REPLACED IAW REO 601R-53-41-059 REV ''A''. 2L72 4F RTA21EA 20040122000432004012200043NM 2004 1 22 ASAA040122D 120030324A532069434562 STRAP BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01703AS 28893 DURING C-CHECK, FOUND CORROSION ON STRAP AT NUT-PLATE AT BS 787-794, RBL 19.5 AND WL 155. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040122000442004012200044EA 2004 1 22 ASOA03607 120031127A2780 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLATS FAILED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11716EV 10084 DURING APPROACH THE CREW SELECTED SLATS TO 8 DEGREES AND THEN RECEIVED SLAT FAIL CAUTION AND SLATS MECHANICAL JAMMED MESSAGES. AN EMERGENCY WAS NOT DECLARED. THE AIRCRAFT DIVERTED TO ONT AND LANDED SAFELY. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE SLATS WITHOUT ANY DEFECTS NOTED AND HAD THE CREW POWER DOWN AND UP THE AIRCRAFT WHICH CLEARED THE FAULT MESSAGES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122000552004012200055EA 2004 1 22 ASOA03647 120031214A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040122000602004012200060NM 2004 1 22 GAIA03161A 120031106A2120 PLENUM BOEING727 727214 138407RNM AIR CON SYS CONTAMINATED A GAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07750US 21512 FERRY FLIGHT NR 750 - MZJ-JAX - DURING CRUISE, THE CREW NOTICED AN OIL ODOR IN THE COCKPIT FROM THE AIRCONDITIONING. AN UNEVENTFUL LANDING WAS MADE. CLEANED THE A/C DUCTING AND PLENUM AREA IAW THE AIRCRAFT MM. OPS CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040122000642004012200064EA 2004 1 22 ASOA03649 120031214A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING A C-CHECK, THE FS 640 FORWARD ON THE RT SIDE BETWEEN STRINGERS 13R AND 14R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 640 FORWARD ON THE RT SIDE BETWEEN STRINGERS 13R AND 14R IAW ASA EO 600-53-0088. (M) 2L72 4F RTA21EA 20040122000752004012200075WP 2004 1 22 GTIA030958 120031201A3350 SWITCH DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FLL - FORWARD EMERGENCY EXIT ILGHT ASSEMBLY HAS BAD ON/OFF SWITCH. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20040122000762004012200076WP 2004 1 22 GTIA030961 120031108A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND CABIN STATION 200 RBL 25 RBL 42 FLOOR SUPPORT CORRODED AND DOUBLE DRILLED FASTENER HOLES. FABRICATED NEW SUPPORT. INSTALLED SUPPORT. (M) 2L72 4F RTA6WE 20040122000902004012200090NM 2004 1 22 AALA20031233 120031106A29104700004A FITTING BOEING767 767323 1385205NM LT HYD SYSTEM LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2139365 24046 LOST LT HYDRAULIC SYSTEM QUANTITY. STOPPED LOSS AT .48 BY TURNING OFF LT PUMPS IAW PROCEDURE. RETURNED AND LANDED WITHOUT INCIDENT. REPLACED LEAKING CENTER RUDDER RATION SERVO FITTING AND SERVICED LT HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040122001302004012200130WP 2004 1 22 GTIA030954 120031127A3330 LIGHT DOUG DC9 DC983 3022083WP EMERGENCY EXIT INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 MCO - EMERGENCY EXIT IDENTIFIER LIGHT FOR AFT CABIN DOOR INOPERATIVE. REPAIRED WIRES FOR EMERGENCY EXIT IDENTIFIER AT AFT CABIN DOORS, OPS CHECK OK. (M) 2L72 4F RTA6WE 20031231000062003123100006EA 2003 12 31 ASOA03566 120031104A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LT AND RT SIDES IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20031231000072003123100007CE 2003 12 31 2003F00662 120031126A21326608506004 INDICATOR LEAR 60 60LEAR 5170707CE CABIN PRESSURE MALFUNCTIONED A UG8AA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL23699DA 237 PRESSURIZATION SYSTEM LIGHT ON. CABIN ALTITUDE RATE GAUGE FLUCTUATING WILDLY. CABIN PRESSURE INDICATOR INOPERATIVE. TROUBLESHOT PRESSURIZATION SYSTEM IAW MM CHAPTER 21-30-00 PAGE 216 STEPS 1 THROUGH 25. FOUND NO DEFECTS WITH PRESSURIZATION CONTROLLING SYSTEM. OBSERVED CABIN PRESSURE INDICATOR FLUCTUATING FROM PLUS 2000 FEET TO -2000 FEET WITH ONLY APU OPERATING. INSTALLED SERVICEABLE CABIN PRESSURE INDICATOR AND PERFORMED SUCCESSFUL OPERATIONAL CHECK OF THE CABIN PRESSURIZATION SYSTEM IAW THE MM CHAPTER 21-30-00 PATE 201 STEP A. RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4F RTA10CE 20031231000112003123100011EU 2003 12 31 USAASA03131 120031119A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19719US 1084 THE EMERGENCY LIGHT TEST INDICATED EPSU EMER R FAIL. MAINTENANCE REPLACED THE EPSU AT THE RT EMERGENCY EXIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031231000142003123100014NM 2003 12 31 TSAA0333048 120030310A335086210066 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000202003123100020NM 2003 12 31 TSAA0253245 120031107A53106550578 STRUCTURE BOEING737 737230 1384401NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 BLENDED REWORK AREA TO A 10 TO 1 RATION SPANWISE. PERFORMED 10X VISUAL TO ENSURE CORROSION COMPLETELY REMOVED. FLAT PEENED, ALODINED AND PRIMED REWORKED AREA WITH BMS 10-11, TYPE 1. FABRICATED EXTERNAL DOUBLER AND REPAIR STRAP FROM .150 INCH 7075-T7351 PLATE. FABRICATED REPAIR FILLERS FROM 7075-T6. SHOT PEENED, ALODINED AND PRIMED ALL REPAIR PARTS. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. APPLIED FINISH COAT. REPAIR COMPLETED IAW ECO 2513. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000212003123100021NM 2003 12 31 TSAA0334192 120031202A7700 WARNING LIGHT BOEING737 73776N 13844CHNM COCKPIT FALSE INDICATIONA TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13744AL 32582 ON TAKEOFF ROLL, ABORTED TAKEOFF AT 70 KTS DUE TO ENGINE MASTER CAUTION LIGHT, DIDN'T NOTE SOURCE OF LIGHT. ONLY ABNORMAL INDICATION WAS 99 CELSIUS TAT. SMOKE OBSERVED FROM BRAKES, NORMAL TAXI TO GATE. PERFORMED HIGH ENERGY STOP/HEAT DAMAGE CONDITION INSPECTION IAW GMM 05-51-07-2. AIRCRAFT OK FOR SERVICE. PERFORMED ENGINE 1 AND 2 BITE TEST IAW 73-00-801. FOUND PITOT PROBE HEAT WAS OFF. PERFORMED ADIRS BITE 34-21 TAT PROBE SIGNAL FIM 34-21-00-810. FOUND NO FAULT. PHYSICALLY CHECK PITOT PROBLE FOR PROPER OPERATION. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231000392003123100039NM 2003 12 31 TSAA0333066 120030412A335086210066 BATTERY PACK BOEING737 7372S2C 138448GNM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13806AL 21927 REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231000422003123100042EA 2003 12 31 ASOA03569 120031105A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING A C-CHECK IN MCN, THE INTERCOSTALS ON THE LEFT AND RIGHT SIDES AT FS 484, BL 27-36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS ON THE LEFT AND RIGHT SIDES AT FS 484, BL 27-36 IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20031231000452003123100045EA 2003 12 31 A6WA200340182 120031118A5753 VANE CNDAIRCL600 CL6002B19 1900309EA TE FLAP CHAFED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11419AW 7633 LT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE HAS 2 MINOR CHAFF AREAS AT WS 56.177 AND WS 104.429. BOTH CHAFES ARE LESS THAN .001 INCH DEEP. PERFORMED A MAJOR REPAIR TO LEFT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE AT WS 56.177 AND WSL 104.429 BY BLENDING DAMAGED AREAS, RESTORING FINISH AND APPLYING TEFLON FILLED ABRASION RESISTANT COATING IAW BOMBARDIER, INC REO 601R-57-52-004 REV. (M) 2L72 4F RTA21EA 20031231000572003123100057WP 2003 12 31 GTIA030902 120030904A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FORWARD PIT CEILING WEB CRACKED LBL 57 INCHES FS 224. REMOVED DAMAGE WEB. FABRICATED NEW WEB. INSTALLED NEW WEB. (M) 2L72 4F A6WE 20031231000682003123100068EA 2003 12 31 ASOA03570 120031105A5260601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA AIRSTAIR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000712003123100071EA 2003 12 31 ASOA03572 120031108A5210AN386110 PIN CNDAIRCL600 CL6002B19 1900309EA DOOR HANDLE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURNG AGROUND INSPECTION IN DTW, PASSENGER DOOR INNER HANDLE WOULD NOT STOP AND THE DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR HANDLE SHEAR PIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031224000612003122400061 2003 12 24 2003F00654 420031201A2565140N27549 LIFTER BOEING757 757236 1384971NM L2 DOOR GIRT BARBROKEN A P9RAK NONE O OTHER ININSP/MAINT 1 SO11521NA 25592 12 DOOR GIRT BAR DOES NOT DISENGAGE WHEN EMERGENCY SLIDE DOOR LEVER IS MOVED TO DISARM POSITION. FOUND FORWARD GIRT BAR LIFTER BROKEN. REMOVED AND REPLACE LIFTER IAW BMM 52-11-25. (M) 2L72 4F RTA2NM 20031229001422003122900142 2003 12 29 SWAA032737 420031214A3460166891 CDU BOEING737 7377H4 1384404NM COCKPIT FAULTY A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29781WN 30601 DURING CRUISE AT FL 370, SMOKE WAS FOUND COMING FROM RIGHT FWD CONTROL PEDESTAL. DIVERTED TO MCI. REMOVED AND REPLACED CDU PER MM. 2L72 4F RTA16WE 20031229001692003122900169NM 2003 12 29 P5CA0301007 120031216A2750 CONTROL UNIT BOEING747 7472U3B 1384846NM TE FLAPS MALFUNCTIONED A P5CAO OTHER F FLT CONT AFFECTED CLCLIMB 1 WP23923FT 22769 AFTER T/O - INBOARD TRAILING EDGE FLAPS HUNG AT 5 DEGREES RETRACTED BY ALTS SYS ON EXTENSION I/B FLAPS HUNG AT 5 DEGREES EXTENDED BY ALT SYS. REPLACED NO COAST DRAG BRAKE PER MM 27-51-42, OP'S CK GOOD. 2L74 4F RTA20WE 20031229001772003122900177SO 2003 12 29 SWIA200312672 120031114A5410 STRUCTURE EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07568SW 120343 RIGHT ENGINE INBOARD SIDE NACELLE DECK CHAFED AND CRACKED AT HYDRAULIC PRESSURE HOSE NIPPLE CONNECTION (REF: S/B 120-29-0049 PAGE 2, FIG 1, DET B). DISCOVERED DURING C-CHECK INSPECTION. DOUBLER ADDED TO AREA, INBOARD NACELLE DECK IAW SRM120 51-10-02 PG 2 SEC 2B. 2L72 4T RTA31SO 20040123000052004012300005 2004 1 23 ASAA0380703 420031104A2565D29982107 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01967AS 49103 SEA PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. CABLE TO SLIDE FORWARD GALLEY ENTRANCE IS BROKE. RECONNECTED LANYARD, REINSTALLED TOGGLE R-1 DORO SLIDE. (M) 2L72 4F A6WE 20040123000112004012300011WP 2004 1 23 ASAA0380694 120031027A531359360281 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD END AT FS 1060. REPLACED LONGERON SPLICE PER EA 5310-01717. (M) 2L72 4F RTA6WE 20040123000212004012300021EA 2004 1 23 A6WA200340199 120031224A3250 LINK CNDAIRCL600 CL6002B19 1900309EA NLG STEERING DISCONNECTED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31407AW 7424 NOSE GEAR OPEN GEAR DISAGREE, WOW YELLOW MESSAGE AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATED DOWN. INSPECTED NOSE GEAR FOUND STEERING LINK DISCONNECTED, RECONNECTED STEERING LINKAGE, NO FURTHER DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040123000222004012300022SO 2004 1 23 CDM2003F00000 120031109A29131213HBG310A SEAL PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA HYD PUMP SHAFT LEAKING B CDMRO OTHER K FLUID LOSS NRNOT REPORTED 1 EA1727666 1202 317852097 PILOT REPORTED NO LT GEAR DOWN LIGHT, AND GEAR SELECTOR HANDLE WOULD NOT RETURN TO NEUTRAL BY PILOT AND AIRCRAFT WAS ROCKED. GEAR DOWN LIGHT CAME ON AND AIRCRAFT LANDED. WHEN CHECKING FOR CAUSE HYD FLUID WAS FOUND COMING FROM LT ENGINE HYD PUMP DRAIN. AIRCRAFT RETRACTION TEST WITH HYD TEST UNIT WAS NORMAL. REPLACED LT ENGINE HYD PUMP, RAN ENGINE AND PRESSURE CHECKED SYSTEM BY OPERATING GEAR SELECTOR HANDLE TO DOWN POSITION, INDICATING GEAR HYD SYSTEM PRESSURE, OK. A FLIGHT TEST WAS DONE AND GEAR OPERATION WAS NORMAL. PROBABLE CAUSE WAS AIR GETTING INTO SYSTEM FROM LEAKING HYD PUMP AT SHAFT SEAL. 1L72 3O3 O A20SO E14EA 20040123000392004012300039EA 2004 1 23 A6WA200340164 120031111A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31401AW 7280 RT FUSELAGE SKIN AT FS 409 AND 64 STRINGER 23R HAS LIGHTNING DAMAGE AND A TEMPORARY REPAIR IAW MFG REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED SECTION OF SKIN FABRICATED FILLER FROM 2024-T3 .050 INCH WVAC PO NR 296691 FABRICATED DOUBLER FROM 2024T-42. .063 INCH WVAC PO NR 169562 AND INSTALLED IAW CRJ200 SRM 53-00-31 REPAIR NR 1 AND WVAC EO 601R-53-4381. 2L72 4F4 FRTA21EA E15NE 20040123000412004012300041EU 2004 1 23 KBM2003F00105 120031113A6420350A27119123 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 NR 1, 2, AND 3 PUSH PULL TUBE BEARINGS WORN. REPLACED WITH 3 NEW BEARINGS. 1G71 3U3 UNCH9EU E19EU 20040123000462004012300046CE 2004 1 23 I5W2003F00000 120031105A3233257063 CLEVIS BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60 52043NE ACTUATOR FAILED E I5WAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO057250L164 123 FA81 PILOT REPORTS DURING TAKE OFF LANDING GEAR RETRACTED HARD AND MADE LOUD NOISE, AFTER LANDING A VISUAL INSPECTION WAS PERFORMED. THE NOSE ACTUATOR CLEVIS PN 257063 WAS FOUND TO BE SHEARED OFF JUST ABOVE THE THREADED SECTION OF CLEVIS FITTING. ACTUATOR SHAFT WAS JAMMED AGAINST THE NOSE LANDING GEAR DRAGLEG PREVENTING GEAR FROM COLLAPSING. NOSE ACTUATOR WAS INSTALLED 164.0 HOURS AND 116.0 HOURS AND 116 CYCLES BEFORE FAILURE. 2L72 4T4 T A24CE E4EA 20040123000482004012300048EU 2004 1 23 KBM2003F00102 120031117A2910350A35020171 DRIVE BELT SNIAS 350 AS350B2 8680813EU HYD SYSTEM DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 HYDRAULIC BELT HAS DAMAGE. INSTALLED NEW HYDRAULIC BELT. 1G71 3U H9EU 20040120000142004012000014NM 2004 1 20 03FDEA02213 120031219A5740ARC7490501 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING INBOARD FLAP VANE OUTBOARD TEE FITTING FOUND CRACK, LENGTH APPROX 0.5 INCH. LH WING INBD FLAP VANE OUTBD TEE FITTING REMOVED AND REPLACED AS PER MM 27-50-22. 2L73 4F RTA22WE 20040121000172004012100017NM 2004 1 21 03FDEA02273 120031226A5744ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT WING O/B FLAP O/B HINGE FITTING O/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD. FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000212004012100021NM 2004 1 21 03FDEA02279 120031226A5744ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING OUTBOARD FLAP OUTBOARD HINGE ACTUATOR MOUNT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBD. FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000292004012100029NM 2004 1 21 03FDEA02318 120031228A5510ALC81071 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB LT UPPER CENTER PLANK NR 26L BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-75196: HORIZONTAL STAB BARREL NUT BORE 26 LT FITTING FABRICATION. 2L73 4F RTA22WE 20040121000942004012100094SO 2004 1 21 SIMA200331102 120031106A3320101086 LAMP EMB 145 EMB145LR 3260212SO GALLEY FAILED A SIMAO OTHER BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CRCRUISE 1 SW21640AE 145183 ORD - FLT 4128 - FLIGHT ATTENDANT OBSERVED SMOKE SMELL IN GALLEY AREA. REPLACED SERVICE DOOR COURTESTY LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4T RTT00011AT 20040122000592004012200059NM 2004 1 22 UIEA200300068 120031118A3610 DUCT BOEING747 747243B 1384830NM NR 3 ENGINE LEAKING A UIEAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA15517MC 23300 ON CLIMB-OUT, NR 3 ENGINE NACELLE TEMPERATURE WENT TO 6.0, LOOPS A/B. WITH POWER PULLED BACK TO CRUISE TEMPERATURE DROPPED TO 3.5 - 4.0. REMOVED AND REPLACED FORWARD 8TH STAGE DUCT ASSEMBLY AS PER MM 36, ACCOMPLISHED LEAK CHECK ON ABOVE IDLE RUN UP, ALL NORMAL. (M) 2L74 4F A20WE 20040122000612004012200061EA 2004 1 22 A6WA20340190 120031210A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 FOUND RIGHT FS 64 BETWEEN STRINGER 9 AND STRINGER 12 ON AFT SIDE OF FRAME CRACK FOUND ON SKIN DOUBLER. (M) 2L72 4F RTA21EA 20031231000832003123100083WP 2003 12 31 GTIA030925 120031101A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND FLOOR PANEL, LEFT OUTBOARD STATION 541-617 HAT CHANNEL CRACKED IN HALF. REMOVED DAMAGED H-SECTION FORMED FILLER AND SPLICES. INSTALLED FILLER AND SPLICES. (M) 2L72 4F RTA6WE 20031231001032003123100103NM 2003 12 31 TSAA0353060 120030407A53306545808 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13817AL 39735 CUT OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR PLATE. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS USING FASTENERS IDENTIFIED IN TABLE II. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231001082003123100108NM 2003 12 31 TSAA0357062 120030410A572069406625 LEG ASSY BOEING737 737209 13844AENM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 CUTOUT THE DAMAGED FROM THE VERTICAL LEG. BLENDED OUT REMAINING AREA OF THE CHORD MAINTAINING A GREATER THAN .050 INCH THICKNESS. PERFORMED 10X VISUAL AND HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAP PEENED REWORKED SURFACES. FABRICATED REPAIR PARTS 1, 2, 3 AND 4 FROM 2024-0 PER FIGURE 1. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II PRIMER TO ALL BARE SURFACES. INSTALLED REPAIR PARTS WITH FASTENERS IDENTIFIED. REPAIR COMPLETED IAW ECO 2948 R4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231001122003123100112WP 2003 12 31 GTIA030941 120031105A3150 WARNING LIGHT DOUG DC9 DC982 3022082WP COCKPIT ILLUMINATED A GTIAK NONE N FALSE WARNING ININSP/MAINT 1 GL23804NK 49104 AIRCRAFT HAD TWO INBOUND ITEMS, 'AFT CABIN DOOR' LIGHT CAME ON AT ALT PRESSURE NORMAL, STAYED ON FOR APPROX 1 HOUR. DOOR WAS LATCHED PROPERLY, CAME BACK ON LAST HOUR OF FLIGHT. 'AUTO SLAT FAIL' CAME ON DEP/AND APP. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F A6WE 20031231001262003123100126NM 2003 12 31 TSAA0353026 120030111A53306546556 SKIN BOEING737 7372T4 1384492NM FUSELAGE CANNING A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 TRIMMED OUT THE SKIN SNAP DAMAGE AND OIL-CANNING. VISUALLY INSPECTED FOR DISBONDING. FABRICATED AND INSTALLED THREE STRUCTURAL FILLERS, AND DOUBLER AND TEARSTRAP PER FIGURE 1. ALODINED AND PRIMED. APPLIED CORROSION INHIBITING COMPOUND. REPAIR COMPLETED IAW ECO 3315. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231001272003123100127NM 2003 12 31 TSAA0351036 120030115A53206554893 SPLICE BOEING737 7372T4 1384492NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 TRIMMED WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PERSSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOUR DOUBLER I BEAM TIE STRAPS AND TEE STIFFENERS. ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS. INSTALLED REPAIR PARTS PER SRM 53-60-51, FIGURE 203. REPAIR COMPLETED IAW ECO 3328. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231001322003123100132SO 2003 12 31 SWIA200312697 120031218A5330 SKIN EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07221SW 120290 FUSELAGE SKIN CORRODED BY FRAME 23 BY 21L STRINGER. DISCOVERED DURING C-CHECK INSPECTION. 2L72 4T RTA31SO 20040105000022004010500002NM 2004 1 5 DL757030994 120031108A5754 SKIN BOEING757 757232 1384965NM RT WING SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 NR 9 SLAT DENTED ON I/B END. COMPLETED PERMANENT REPAIR PER SRM 51-70-10D REF SRM 57-42-02D. C/W REPAIR ON OPN 1000 CARDS 1126-1134. 2L72 4F RTA2NM 20040105000142004010500014 2004 1 5 DL757031006 420031111A2565MS358121 CLEVIS BOEING757 757232 1384965NM ESCAPE SLIDE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 NR 915 HMV-3 VISIT INSPECTION OPN 5876, HARDWARE CORRODED ON CABLE FOR MANUAL EMERGENCY RELEASE CABLE LT SIDE OF FUSELAGE BETWEEN OVERWING EXITS STA 984-996 STRINGER 17L. REMOVED SAFETY WIRE, CLEANED AREA OF CORROSION. OK TO INSTALL NEW HARDWARE. INSTALLED NEW HARDWARE AND RESAFTIED. IPC ITEMS NR 150/155/160/173/175 REPLACED. P/N'S MS24665-132/MS20392-2C17/BACW10P270L/AN960-10/MS35650-302/MS35812-1. 2L72 4F RTA2NM 20040105000192004010500019NM 2004 1 5 DLWOA031007 120031110A5330NGA6313515 SKIN DOUG MD11 MD11 3023602NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27804DE 48475 THE FUSELAGE SKIN AT THE AFT EDGE OF THE C2 CARGO DOOR CUTOUT WAS FOUND WITH A DENT AND GOUGE IN AN EXISTING SRM REPAIR DOUBLER. THE DOUBLER WAS REMOVED AND UNDERLYING STRUCTURE INSPECTED. ALL EXISTING AND NEW DAMAGE WAS REMOVED WITH A 14.5 X 6 INCH CUTOUT IN THE SKIN AND UNDERLYING DOUBLERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087661-14, REV B. 2L73 4F RTA22WE 20040105000212004010500021NM 2004 1 5 DL75K031009 120031112A3350 COVER BOEING757 757232 1384965NM EMERGENCY EXIT MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27684DA 27104 AFT RT OVERWING EXIT SIGN COVER MISSING. REPLACED RT AFT OVERWING EXIT COVER. 2L72 4F RTA2NM 20040105000222004010500022NM 2004 1 5 DL73S031010 120031112A53156546803504 FLOORBEAM BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 THE FS 520 FLOORBEAM WAS FOUND WITH 1 INCH TO 2 INCH CRACKS NEAR THE UPPER CAP FLANGE AT RBL & LBL 24 & 45. THE CRACKS WERE TYPICAL OF BAC S/B 737-53-1120. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL CRACKS. A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED PER ER/A 087489-14, REV A. 2L72 4F RTA16WE 20040105000342004010500034NM 2004 1 5 DL777031018 120031115A331081411 BALLAST BOEING777 777232 1385232NM AFT CREW REST OVERHEATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27861DA 29952 DOOR 3 OVERHEAD CREW REST MODULE FLIGHT ATTENDANT SIDEWALL LIGHT INOP WITH ELECTRICAL ODOR. REPLACED BALLAST PART NUMBER 8184-1, SERIAL NUMBER 146235 AS PRECAUTION. ALSO REQUIRES LIGHT ASSEMBLY PART NUMBER 10-1428-5. 2L72 4F RTT00001SE 20040105000352004010500035NM 2004 1 5 QXEA200301573 120031219A5270 SPRING BOMBDRDHC8 DHC8401 1390041NM ZONE 800 LOOSE A QXEAO OTHER N FALSE WARNING DEDESCENT 1 NM09546DS373 4017 DESCENDING OUT OF 3500 FT, THE FUSELAGE DOOR MASTER WARNING LIGHT KEPT GOING FROM ON TO OFF. THE DOORS PAGE INDICATED THE AFT PAX DOOR. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED AND LUBED THE SPRING PORTION OF THE PROX SENSOR. THE SPRINGS ON EXTERNAL DOOR HANDLE MECHANISM WERE FOUND TO HAVE NO TENSION. THE SPRINGS WERE REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040105000372004010500037EU 2004 1 5 MALA030551 120031213A7931 TRANSDUCER SAAB SF340 340B 7860101EU OIL PRESSURE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15434XJ 340B434 DURING FLIGHT 2938, LT PROP OIL PRESSURE FLUCUATED. AIR RETURN TO MEM. MAINTENANCE CLEANED OIL PRESSURE TRANSDUCER CONNECTOR OF EXCESS OIL, RAN AIRCRAFT 30 MINS, COULD NOT DUPLICATE. SWAPPED PRESSURE GAUGES FOR TROUBLESHOOTING PURPOSES, OK FOR CONTINUED SERVICE. 2L72 4T RTA52EU 20040105000392004010500039NE 2004 1 5 DL76S031013 220031110A7310 GASKET BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 ENGINE FAILED A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO27126DL35888 580394 24076 580394 ON LANDING ROLL TOWER REPORTED SMOKE AND FUEL COMING FROM LT ENG AFTER TOUCHDOWN ALL LEFT ENGINE INDICATION VERY LOW. TURNED FUEL SWITCH OFF. MTC FOUND FUEL LINE FROM PUMP TO MEC GASKET BAD. REPLACED GASKET. RAN ENGINE. CHECKS GOOD. 2L72 4F4 FRTA1NM E13NE 20040123000552004012300055WP 2004 1 23 AMTA200301364 120031105A7830 WARNING LIGHT LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE NR 2 ENG T/R MALFUNCTIONED A AMTAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL11162AT 1220 14839 NR 2 THRUST REVERSER PRESSURE LIGHT CAME ON INFLIGHT. NO INDICATION THRUST REVERSER DEPLOYED. LIGHT COMES ON AT 95 PERCENT N1. 2L73 4F4 F A23WE E12EU 20040123000642004012300064CE 2004 1 23 WVE2003F00023 120031123A242030728692 SPLINE ADAPTER LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP ALTERNATOR CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09425FX 147 DURING 600 HOUR INSPECTION OF THE ALTERNATOR SPLINE ADAPTOR, DISCOVERED ADAPTER TO BE CRACKED IN TWO LOCATIONS. PROBABLE CAUSE: FATIGUE. (EA09200401170) 2L72 4F4 FRTT00008WIE6WE 20040123000782004012300078SW 2004 1 23 E5W2003F00001 120031105A6220407010105101 STUD BELL 407 407 1182206SW ALLSN 250C 250C47B GL DROOP STOP CRACKED B E5WRO OTHER O OTHER NRNOT REPORTED 1 GL21407SM 53289 CRACK-LIKE INDICATIONS AT STUD RADIUS CONTINUING TO HOLES ON SOME OF THE STUDS. IMPERFECTIONS, DEFECTS DETECTED BY FLUORESCENT PENT. 1G71 3U3 UO H2SW E1GL 20040126000402004012600040SW 2004 1 26 HEEA087821 120030605A6230206010450119FM SWASHPLATE BELL 206 206L3 1182108SW MAIN ROTOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036161A17829 51611 MAIN ROTOR SWASHPLATE HAS GREASE COMING FROM UPPER SLEEVE. REPAIRED. 1G71 3U H2SW 20040126000472004012600047EU 2004 1 26 BAQA091615 120031211A2822P94C16606 PUMP AEROSPAS365 AS365N2 8680815EU FUEL BOOST INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME1044 6417 FUEL BOOST PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 01/08/2004 1G72 3U RTH10EU 20040126000552004012600055NE 2004 1 26 HEEA087803 120030624A32442071A900 TIRE SKRSKYS76 S76C 8143008NE MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 TIRE WORN. REPLACED WITH SERVICEABLE TIRE. 1G72 3U NCH1NE 20040126000562004012600056NE 2004 1 26 HEEA087804 120030624A32442071A900 TIRE SKRSKYS76 S76C 8143008NE MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 TIRE WORN. REPLACED WITH SERVICEABLE TIRE. 1G72 3U NCH1NE 20040121000422004012100042NM 2004 1 21 03FDEA02294 120031226A5350AKC75435 STIFFENER DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT TAILCONE TOP MOST HORIZONTAL STIFFINER BELOW THE UPPER DOOR HINGE ASSY FOUND CHAFED AT ITS END AREA. LT TAILCONE TOP MOST HORIZONTAL STIFFINER BELOW CHAFED TEE SUPPORT REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II AND DRAWING AKC7543. 2L73 4F4 FRTA22WE E13NE 20040121000642004012100064EU 2004 1 21 USAASA03077 120030711A2421558CA01Y1 CONTACTOR AIRBUSA319 A319112 3930323EU COCKPIT FAILED A ASOAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 SO11723UW 1109 EN ROUTE THE NR 1 AC SYSTEM WENT OFFLINE. RECEIVED GEN 1 FAULT AC ESS BUS FAULT, AC BUS 1 FAULT, EXTRACT FAULT, AND NW STEER FAULT ECAM MESSAGES. ALL SIX DISPLAY UNITS BRIEFLY BECAME BLANK, AND THEN STARTED INDICATING AGAIN. ON THE ELECTRICAL PAGE, THE TR 1 INDICATED ZERO VOLTS IN AMBER AND THE GEN 1 INDICATED OFF IN AMBER. ALSO, AN ELECTRICAL ODOR WAS NTOED IN THE AFT GALLEY. FLIGHT DIVERTED TO STL FOR LANDING, WHERE IT WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE NR 1 TRANSFORMER RECTIFIER UNIT, NR 1 GENERATOR CONTROL UNIT, AND NR 1 GENERATOR LINE CONTRACTOR AND CONTACTOR BASE. ALSO, REPLACED A LIGHTNING PROTECTION MODULE. AIRCRAFT OK FOR SERVICE. SUBSEQUENT INVESTIGATIONS FOUND THAT THE NR 1 GENE2L72 4F RTA28NM 20040121000982004012100098SO 2004 1 21 SIMA200333201 120031125A3350375911 LIGHT EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 CREW REPORTED THE ROW 11 EMERGENCY EXIT ILGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040121001032004012100103NM 2004 1 21 03FDEA02328 120031230A5744ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD MOUNT INBOARD AND OUTBOARD SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75201, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP. OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040122000082004012200008EA 2004 1 22 SWIA200312728 120031224A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-51 2L72 4F RTA21EA 20040122000692004012200069EA 2004 1 22 ASOA03594 120031120A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72 - FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72 - FS 589.00 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20031204000062003120400006WP 2003 12 4 GTIA030888 120031026A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND TAIL CONE EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE. REPAIRED WIRE. (M) 2L72 4F A6WE 20031202000722003120200072NM 2003 12 2 USAABB03185 120031013A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19629AU 27807 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031202000962003120200096NM 2003 12 2 USAA030216 120031023A5311 FRAME BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US 23992 FOUND FRAME CRACKED .75 INCH, STATION 360 1 INCH BELOW STRINGER 14R CLIP. REPAIRED PER SRM 53-00-07. (M) 2L72 4F RTA16WE 20031202001052003120200105EA 2003 12 2 ASOA03518 120031017A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20031202001062003120200106EA 2003 12 2 ASOA03517 120031017A5312 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE FS 718 BETWEEN STRINGERS 10-12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 718 BETWEEN STRINGERS 10-12 ON THE RIGHT SIDE IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20031202001102003120200110NM 2003 12 2 GAIA03113SP 120031022A5311 FRAME BOEING727 727223 1384074NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076831 20184 DURING B-CHECK AT DFW, A FUSELAGE FRAME AT BS 560 WAS FOUND DENTED BY STRINGER 17R. THE FRAME WAS REPAIRED PER THE B727 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031202001202003120200120EU 2003 12 2 A6WA200360057 120031020A5730 SKIN BAG BAE146BAE146200A 1500266EU RT & LT WING DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31183US E2043 LEFT AND RIGHT WING DENTED, SPOILERS AND T/E PANEL'S, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830005. (M) 2H74 4F RTA49EU 20031202001262003120200126EA 2003 12 2 SIMA200326501 120030919A3230533407 VALVE CNDAIRCL600 CL6002C10 1390015EA MLG FAILED A SIMAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 SW21508AE 10072 LANDING GEAR WOULD NOT EXTEND HAD TO EXTEND GEAR MANUALLY. RT LANDING GEAR SELECTOR VALVE. PERFORMED GEAR SWING, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20031202001272003120200127EA 2003 12 2 SIMA200326808 120030913A5280CC670105106 DOOR CNDAIRCL600 CL6002C10 1390015EA RT MLG SEPARATED A SIMAO OTHER D INFLIGHT SEPARATION APAPPROACH 1 SW21504AE 10044 RIGHT MAIN GEAR DOOR DEPARTED AIRCRAFT CAUSING DAMAGE TO FLAP AND FUSELAGE IN ADJACENT AREA, DISCOVERED DURING POST FLIGHT INSPECTION. MAINTENANCE REPLACED THE RIGHT MLG DOOR IAW CRJ MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE AFTER FLAP AND FUSELAGE DAMAGE WAS REPAIRED. (M) 2L72 4F RTA21EA 20031202001682003120200168SO 2003 12 2 SIMA200328804 120031008A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 ABI - DURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED THE CORROSION BY CREATING A CUT OUT IN THE DAMAGED FLANGE AND WEB OF THE RIGHT FLOORBEAM. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3320, EMB SRM, SRM EMB 145/1142 REV 23, CHAPTER 53-21-10 FIG 201 SHEET 1 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031203000182003120300018NM 2003 12 3 GAIA03159OP 120031030A324026011825 BRAKE ASSY BOEING727 727251 138408HNM LT MLG SEPARATED A GAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW07279US 21158 DURING TAXI TO DEPARTURE THE CAPTAIN NOTICED THAT THE LEFT BRAKES WERE DRAGGING. THE AIRCRAFT TAXIED BACK TO THE RAMP. THE NR 2 BRAKE DISK WAS FOUND SEPARATED AND JAMBED. THE NR 2 BRAKE AND DEBOOSTER VALVE WERE REPLACED. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031203000202003120300020NM 2003 12 3 GAIA03119ST 120031003A5711BAC150529D63 STIFFENER BOEING727 727243 138408DNM RT FRONT SPAR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION, FOUND RIGHT WING FRONT SPAR VERTICAL STIFFENER CRACKED JUST OUTBOARD OF NR 6 SLAT INBOARD TRACK CAVITY. REF FASI N/R NR 61212, REPLACED STIFFENER BAC 1505-29D63 PO NR 314624 IAW B727 SRM 51-30-2. (M) 2L73 4F RTA3WE 20031203000252003120300025NM 2003 12 3 GAIA03136ST 120031024A5311BAC1505100612 FRAME BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND C-2 DOOR CUTOUT AFT FRAME BS 990 INNER CHORD IS CRACKED AND CORRODED AT STR 27 RT. REF FASI N/R NR 61484, CUT OUT DAMAGE AND INSTALLED ANGLE REPAIR PER B727 SRM 51-40-4 FIG 3. (M) 2L73 4F RTA3WE 20031203000382003120300038NM 2003 12 3 AMTA200301299 120031015A3150 WARNING LIGHT BOEING757 75733N 1384931NM LT ENGINE ILLUMINATED A AMTAO OTHER J WARNING INDICATION CLCLIMB 1 GL11550TZ 32584 LEFT ENGINE OH LP1 DISPLAYED AFTER TAKEOFF. (M) 2L72 4F RTA2NM 20031203000552003120300055NM 2003 12 3 GAIA03143ST 120031024A5347BAC1520841 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND CABIN SEAT TRACK RBL 24.75 BS 760 TO 850 CORRODED. REF FASI N/R NR 61759, REPLACED SEAT TRACK PER B727 SRM 53-10-5 FIG 7 AND 53-10-2 FIG 7. (M) 2L73 4F RTA3WE 20031203000902003120300090NM 2003 12 3 USAA030217 120031028A5315 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 FOUND FLOORBEAM WORN 1 INCH BY 1 INCH, STATION 780, LBL 18 FWD SIDE OF T-CAP. REPAIR ANGLE FABRICATED AND INSTALLED PER EA 94780. (M) 2L72 4F RTA2NM 20031203001022003120300102EU 2003 12 3 ASOA03559 120031015A5320 ANGLE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING A C-CHECK IN BNA, THE ANGLE ON THE RIGHT SIDE AT FS 39 ABOVE THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE ON THE RIGHT SIDE AT FS 39 ABOVE THE SERVICE DOOR IAW SRM 51-21-42 AND 51-25-01. (M) 2H72 4T RTA53EU 20031203001452003120300145EA 2003 12 3 A6WA200340156 120031031A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31452AW 7835 FUSELAGE SKIN DAMAGED AT FS 605 BETWEEN STRINGERS 24L TO 25L. RECONTOURED SKIN, PERFORMED EDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-435OA. (M) 2L72 4F RTA21EA 20040105000402004010500040NM 2004 1 5 DLM88031019 120031116A21216054578 FAN DOUG MD88 MD88 3023688NM RECIRCULATION ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27903DE 53380 AIR TURNBACK. AFTER T/O, CLIMB 8000 FT NOTICED SMOKE IN COCKPIT. RETURNED TO PHL. DURING DEBRIEF F/AS REPORTED SLIGHT SMOKE ODOR IN CABIN, ALSO NO SMOKE DETECTORS SOUNDING IN LAVS. PERFORMED TROUBLESHOOTING PER TROUBLESHOOTING TREE OPN 5088. FOUND LIKELY SOURCE WAS RECIRCULATION FAN. CONTINUED WITH TROUBLESHOOTING THROUGH TAKEOFF POWER ENGINE RUN. NO OTHER SOURCES OF SMOKE, FUMES OR VAPORS FOUND. REPLACED AIR CONDITIONING MOISTURE BAGS FOR PRECAUTIONARY. FWD RECIRCULATION FAN AND PLACARDED PER MEL 21-00-43. PULLED AND COLLARED RECIRC FAN CONT CB J7. 2L72 4F RTA6WE 20040105000432004010500043EA 2004 1 5 QXEA200301564 120031215A3620 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09606QX 10023 BOI- ON FLIGHT 2430 AFTER LEFT COWL ANTI-ICE ON EN ROUTE, LEFT ENGINE BLEED CAUTION AND LEFT COWL ANTI-ICE CAUTION ON. RAN CHECKLIST. TESTED COWL ANTI-ICE SYSTEM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040105000442004010500044SO 2004 1 5 SWIA200312678 120031116A5420 CHANNEL EMB 120 EMB120ER 3260203SO LT ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07227SW 120304 LEFT ENGINE AFT OUTBOARD SUPPORT CHANNEL FOR AFT EXHAUST FAIRING CRACKED. STOP-DRILLED CRACK LEFT ENGINE AFT OUTBOARD SUPPORT CHANNEL. FABRICATED AND INSTALLED REPAIR DOUBLER PER EMB120 SRM 51-40-02, 51-70-04. 2L72 4T RTA31SO 20040105000512004010500051EA 2004 1 5 SWIA200312680 120031208A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILER FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07912SW4910 4910 7595 ON TAXI OUT, SPOILERON FAULT MESSAGE DISPLAYED, WOULD NOT RESET W/ APPLICABLE CBS. REPLACED RIGHT INBOARD AND OUTBOARD SPOILERON PCU'S IAW MM 27-62-01, OPS CHECK & LEAK CHECK GOOD. S/N OFF MAL-5553. 2L72 4F RTA21EA 20040105000522004010500052EA 2004 1 5 SWIA200312682 120031208A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA COCKPIT BROKEN A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07441SW 7602 WIRE LEADING TO STALL PUSHER MOTOR ON CAPTAIN'S YOKE IS BROKEN. REPAIRED WIRING TO NR 1 STICK SHAKER AS REQUIRED. OPS CHECK GOOD. 2L72 4F RTA21EA 20040105000542004010500054 2004 1 5 SWIA200312684 420031208A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07564SW8190 8190 120339 AUTOPILOT WILL NOT CAPTURE OR HOLD ALTITUDE USING EITHER LEFT OR RIGHT FLIGHT DIRECTOR. FLIGHT DIRECTORS APPEAR TO WORK, BUT AP WANDERS OFF. REPLACED ELEVATOR SERVO WITH SERVICEABLE UNIT. BOTH APS & CPS CHECKED GOOD IAW MM 22-11-00. 2L72 4T RTA31SO 20040105000572004010500057 2004 1 5 SWIA200312687 420031212A22116229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07405SW5185 5185 7029 AUTOPILOT SELF-DISCONNECTED SEVERAL TIMES ON APPROACH. REMOVED AND REPLACED FCC NR 2 IAW MM 22-12-14. AUTOPILOT OPS CHECK GOOD IAW MM 22-11-00. 2L72 4F RTA21EA 20040105000622004010500062NM 2004 1 5 2003UALA00942 120031208A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29375UA 24640 STA 639 AT LBL 45.5 OVERWING FLOORBEAM IS CRACKED AT THE STA 639 STUB FRAME ATTACH POINT ON THE I/B FLANGE. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP INSTALLED. 2L72 4F4 FRTA16WE E2GL 20040105000672004010500067NM 2004 1 5 2003UALA00947 120031209A3242 BOLT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 BRAKE MISSING A UALAA UNSCHED LANDING JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 WP29656UA 25394 RETURN TO FIELD DUE TO GEAR DISAGREEMENT EICAS MESSAGE. DAMAGE INCURRED FROM HANGING BRAKE ROD AFTER SEPARATION FROM BRAKE. ROD BELIEVED TO HAVE DETACHED FROM TORQUE ARM DUE TO MIGRATION OF BRAKE TORQUE ARM PIN. SAFETY BOLT BELIEVED TO HAVE COME LOOSE OR POSSIBLY NOT INSTALLED RESULTING IN KEEPER PIN DETACHMENT AND SUBSEQUENT PIN MIGRATION. BRAKE PIN AND KEEPER ASSEMBLY WERE FOUND AND REFLECTED NO DAMAGE INDICATIVE OF MATERIAL FAILURE. 2L72 4F4 FRTA1NM E24NE 20040105000712004010500071NM 2004 1 5 03FDEA02211 120031216A2530NWM67881 PANEL DOUG MD11 MD11 3023602NM GALLEY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 GALLEY MODULE CHILLER SECTION, BOTTOM PANEL (FLOOR) BULGING, FOUND WITH CORROSION. GALLEY MODULE CHILLER SECTION, BOTTOM PANEL (FLOOR) REMOVED AND REPLACED WITH NEW PLATE AS PER FEDEX EA 1-2530-75179, EQUIPMENT/FURNISHINGS - GALLEY - G3B GALLEY MODULE CHILLER COMPARTMENT FLOOR REPAIR / REMOVAL / REPLACEMENT. 2L73 4F RTA22WE 20040105000752004010500075EA 2004 1 5 03352632 120031218A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING INSPECTION THE RT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040105000772004010500077 2004 1 5 P5CA0300996 420031128A25657A1323111 SLIDE BOEING747 747341 13848AMNM DEPLOYED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23354MC 23394 WHILE ATTEMPTING TO INSERT SAFETY PIN IN SLIDE, FOR SLIDE TIME CHANGE, SLIDE INADVERTENTLY DEPLOYED INSIDE A/C. SLIDE MANUALLY DEFLATED/REPLACED WITH SERVICEABLE UNIT. 2L74 4F RTA20WE 20040105001042004010500104WP 2004 1 5 DHL2003802534 120031118A5311 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT ACCY COMPT FORMER FLANGE CRACKED 2.000, STA 640.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. TRIMMED OUT CRACKED FORMER IAW SRM 53-2-0 PG 11. FABRICATED NEW FORMER AND SPLICE PLATE IAW SRM 53-2-0 PG 11. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FORMER AND SPLICE PLATE WITH NEW FASTENERS IAW SRM 53-2-0 PG 11, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031229001562003122900156EA 2003 12 29 SWIA200312661 120031205A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 280 TRANSVERSE BEAM RBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV ''NC''. 2L72 4F RTA21EA 20031231000282003123100028NM 2003 12 31 TSAA0333050 120030310A33509221009 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHT DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 REPLACED AFT SERVICE DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031204000092003120400009WP 2003 12 4 GTIA030881 120031001A5340 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200 48 INCHES RBL. FLOOR SUPPORT ATTACHMENTS 2 AT FS 165 AND 200 48 INCHES RBL OUT OF LIMITS. REMOVED FLOOR SUPPORT ATTACHMENTS TWO, LOCATED AND DRILLED NEW FITTINGS. INSTALLED FLOOR SUPPORT AT ATTACHMENTS TWO. 2L72 4F A6WE 20031204000242003120400024WP 2003 12 4 GTIA030863 120030927A5320 PAN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FORWARD PIT DOOR PAN CORRODED FS 372-376 STRINGER 28R. FABRICATED TWO EACH 23 AND TWO EACH 25 REPAIR ANGLES. LOCATED AND DRILLED REPLACEMENT SEC OF FORWARD DOOR PAN AND TWO EACH 23 AND 25 SPLICE REPAIR ANGLES. INSTALLED REPAIR ANGLES 23 AND 25 FORWARD PIT PAN AND WEB. (M) 2L72 4F A6WE 20031204000282003120400028WP 2003 12 4 AMTA200301276 120030827A5754 SKIN LKHEED1011 10113851 5265010WP NR 5 SLAT DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND 5R SLAT L/E SKIN DENTED AT MID SECTION. REPAIRED SLAT L/E SKIN IAW SRM 57-51-00, FIG 807. (M) 2L73 4F A23WE 20031204000702003120400070EA 2003 12 4 03285708 120031012A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 DURING INSPECTION THE RT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031204000712003120400071NM 2003 12 4 03286402 120031013A3350PS835C POWER SUPPLY DORNERDO32 DO328300 NM EMERGNECY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27402FJ 3147 DURING INSPECTION THE EMERGENCY LIGHTING BATTERY PACK WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031204000752003120400075NM 2003 12 4 C1HA200393016 120031016A3350 BATTERY PACK BOEING727 727212 138407GNM EMERGENCY EXIT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15293AS 21348 LT OVERHEAD (ABOVE OVERWING) EMERGENCY EXIT LIGHTS DO NOT COME ON. POSSIBLE BAD BATTERY. REMOVED/REPLACED LT OVERWING DOOR EMERGENCY EXIT BATTERY PACK AS PER MM 33-50-22, OPS CHECKS OK. 2L73 4F A3WE 20031204000762003120400076NM 2003 12 4 QXEA200301275 120031015A5210 LINKAGE BOMBDRDHC8 DHC8401 1390041NM ZONE 800 OUT OF ADJUST A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 GEG- MAIN CABIN DOOR WILL NOT OPEN. REPOSITIONED AFT SIDE OF RAIL LINKAGE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031204000792003120400079EA 2003 12 4 03288621 120031015A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 DURING INSPECTION THE LT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031204000802003120400080WP 2003 12 4 UPS03841387 120030921A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, MAIN CABIN STA 1100 RT CUSP IS CRACKED AT LONG 21R. CUT OUT CRACKED CUSP SECTION BETWEEN STA 1080-1120, FABRICATED AND INSTALLED CUSP SECTION, DOUBLER AND SPLICES IAW SRM 53-2-5 FIG 15. 2L74 4F RT4A25 20031204000812003120400081WP 2003 12 4 UPS03841388 120030923A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STATION 565 LONG 33R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON BETWEEN STATION 450 TO 610 IAW DWG 3750539 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20031204000822003120400082WP 2003 12 4 UPS03841391 120031001A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STATION 1350 LBL 60. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION BETWEEN STATION 1270 TO 1370 AT LBL 60 IAW DC8-5320-5167-C, DC8-53B-003. 2L74 4F RT4A25 20031203000062003120300006NE 2003 12 3 2003F00606 220030810A73217436025 FUEL CONTROL BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A FX7AJEA DUMP FUEL ENGINE SHUTDOWN UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO1954348 21967 LEVELING OFF AT 330 WHEN NR 2 ENGINE WAS THROTTLED BACK TO CRUISE POWER, THE FUEL FLOW WENT TO ZERO, AND THE EPR WENT TO 2.24 ENGINE FLAMED OUT. FUEL WAS DUMPED AND EMERGENCY DECLARED A/C LANDED WITHOUT INCIDENT. THE FUEL CONTROL WAS CHANGED PER MM 73-21 AND A/C WAS RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (M) 2L72 4F4 FRTA16WE E2EA 20031203000512003120300051NM 2003 12 3 GAIA03153ST 120031024A5347BAC1520792 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND CABIN SEAT TRACK RBL 24.75 HAS CORROSION AND INCORRECT SPLICE BS 480 TO 670. REF FASI N/R NR 61857, REPLACED SEAT TRACK AND SPLICES RBL 24.75 FROM BS 480 TO 740 IAW B727 SRM 53-10-5 FIG 7. (M) 2L73 4F RTA3WE 20031203000892003120300089NM 2003 12 3 USAASB03196 120031102A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19778AU 24980 MAINTENANCE REPORTED SEVERAL SEAT MOUNTED EMERGENCY LIGHTS IN THE AFT LEFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031203001652003120300165WP 2003 12 3 AALA20031134 120031011A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21443AA 49469 DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT SEAT 30D. REPLACED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031231001242003123100124NM 2003 12 31 TSAA0357064 120030410A57206545455 FLANGE BOEING737 737209 13844AENM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 REMOVED CORROSION DAMAGE BY SMOOTHLY BLENDING REWORK AREA. PERFORMED HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAT PEENED REWORKED SURFACE. FABRICATED A FILLER FROM 2024-T3 SIZED TO FIT BLENDOUT AREA AND RESTORE TO ORIGINAL CONTOUR. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II PRIMER TO BARE SURFACES. WET INSTALLED FILLER AND BMS 5-95 SEALANT ON ALL FRAYING SURFACES. REPAIR COMPLETED IAW ECO 3073. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040105000112004010500011 2004 1 5 DL764031003 420031110A23301301273110 POWER SUPPLY BOEING767 767432ER 1385134NM SEAT 11 CDE OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27825MH 29696 ENTERTAINMENT POWER UNIT UNDER SEAT 11D WARM TO THE TOUCH WITH NOTICEABLE ODOR. SHUTDOWN THE ENTERTAINMENT SYS UNIT UNDER 11D. REPLACED 11 CDE AVU LOADED SOFTWARE, CHECKS OK . 2L72 4F RTA1NM 20040105000122004010500012NM 2004 1 5 DL75K031004 120031111A335020131A BATTERY PACK BOEING757 757232 1384965NM EMERGENCY LIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27648DL 24372 DOOR 4R OVERHEAD EXIT SIGN EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND BAD BATTERY ASSY. REPLACED SAME. 2L72 4F RTA2NM 20040105000892004010500089WP 2004 1 5 DHL2003802530 120031120A53204758514U519 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 2.000 STA 1265.000, L32 - L33R. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040105000942004010500094WP 2004 1 5 DHL2003802549 120031128A5720 ANGLE DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT OUTBD STUB WING WEB REINFORCING ANGLE CRACK 2.000, STA XS 503.000. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040105001332004010500133 2004 1 5 SWAA032773 420031218A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 L2 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. ADJUSTED L2 DOOR EVACUATION PER MM. 2L72 4F A16WE 20040105001382004010500138 2004 1 5 SWAA032756 420031217A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF POSITION. ADJUSTED SLIDE ASSY PER MM. 2L72 4F A16WE 20040105001452004010500145WP 2004 1 5 ABXA030482 120031210A532059203321 FITTING DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 STA 604, LONGERON 28 LEFT END FITTING CORRODED. REPLACED END FITTING 28 LEFT, STA 604 IAW DC-9 SRM 51-10-4 AND 51-30-5. 2L72 4F A6WE 20040105001512004010500151CE 2004 1 5 AMWA107 120031222A553110164000069 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07139ZV UE139 DURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON THE LT SIDE AT STRINGER TO RIB INTERSECTION STRINGER. P/N 101-640000-39. 2L72 4T RTA24CE 20040105001632004010500163CE 2004 1 5 AMWA103 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED STRUCTURAL INSPECTION, TWO FASTENERS AT LWS 55 WERE FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040106000022004010600002WP 2004 1 6 DHL2003802570 120031201A5280 SKIN DOUG DC8 DC873 302199CWP RT MLG DOOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT MLG DOOR INTERNAL SKIN AFT PART CORRODED, STA 960.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 52-2-0 PG 20. TRIMMED OUT CORRODED AREA IAW SRM 52-2-0 PG 18. FABRICATED INTERNAL DOUBLER, FILLER IAW SRM 52-2-0 PG 18. CLEANED, TREATED AND PRIMED AREA, DOUBLER AND FILLER IAW SRM 51-1-8B. INSTALLED DOUBLER AND FILLER IAW SRM 52-2-0 PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040106000052004010600005WP 2004 1 6 DHL2003802552 120031120A5730 SKIN DOUG DC8 DC873 302199CWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LT OUTER WING OTBD EXTENDED L/E OUTER PLATING CORROSION DAMAGE AROUND STA XW 761.695 (MAJOR REPAIR). REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER AND A FILLER IAW ED-EDU 38-1, DWG U38-R01. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED THE REPAIR DOUBLER AND FILLER ON LT WING EXTENDED L/E OUTER PLATING XW 761-695 USING NEW FASTENERS IAW ED EDU38-1, DWG U38-R01 AND SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000622004010600062EA 2004 1 6 SWIA200312689 120031211A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07587SW1049 1049 7062 FLAPS HALF SPEED MESSAGE ON TAXI OUT. REMOVED AND REPLACED PDU IAW MM CH 27-52-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20040106000652004010600065EA 2004 1 6 SWIA200312692 120031212A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAULTY A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07457SW 7773 AFTER TAKEOFF WHILE MOVING THE FLAPS FROM 20 TO 8, HAD A FLAPS FAIL CAUTION MSG. COMPLETED THE QRH AND RETURNED TO TUS WITHOUT INCIDENT. REMOVED AND REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD PER MM 27-51-05. 2L72 4F RTA21EA 20031231000372003123100037NM 2003 12 31 TSAA0356043 120030307A56105893543129 WINDSHIELD BOEING737 7372Q9 138448MNM COCKPIT CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 THE CAPTAIN'S FORWARD WINDSHIELD CRACKED WHILE CRUISING AT FL350. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAINS FORWARD WINDSHIELD. GROUND OPERATIONAL AND PRESSURIZATION CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031203001672003120300167 2003 12 3 GTIA030899 420031111A2565D29985103 SLIDE DOUG DC9 DC983 3022083WP L2 DOOR TORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 LGA - L2 DOOR ESCAPE SLIDE HAS RIP ALONG GIRT BAR HOLDER. REMOVED AND REPLACED L2 EVACUATION DOOR SLIDE. (M) 2L72 4F RTA6WE 20031204000102003120400010WP 2003 12 4 GTIA030880 120030928A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND AFT FUSELAGE EXTERNAL AIR CONDITION DOOR OPENING TWO CRACKS. REMOVED CRACKED DOUBLER. FABRICATED DOUBLER. INSTALLED FABRICATED DOUBLER. (M) 2L72 4F A6WE 20031204000152003120400015WP 2003 12 4 GTIA030883 120031027A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND EMERGENCY LIGHTS INOPERATIVE O/H STATION 800-1200 AND LEFT SIDEWALL LIGHTS INOPERATIVE IN VENTRAL STAIRWELL AREA. TROUBLE SHOT, FOUND LOOSE WIRE. RE-INSTALL LOOSE TERMINAL. (M) 2L72 4F A6WE 20031204000162003120400016WP 2003 12 4 GTIA030882 120030928A5730 PANEL DOUG DC9 DC982 3022082WP LT WING DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND LEFT WING LOWER TRAP PANEL MLG DELAMINATED. REMOVED LEFT WING LOWER TRAP PANEL. REPAIRED LEFT TRAP PANEL. INSTALLED PANEL. (M) 2L72 4F A6WE 20031204000562003120400056NM 2003 12 4 GTIA030848 120031002A3350 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 MCO - EMERGENCY LIGHTS ABOVE L-2 DOOR AND ON OVERHEAD AT MID F/A STATION INOPERATIVE. SECURED LOOSE CONNECTION O BATTERY PACK FOR EMERGENCY LIGHTS. (M) 2L72 4F RT 20031204000832003120400083WP 2003 12 4 UPS03841392 120030923A5320 SUPPORT DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, LOWER FUSELAGE FRAME SUPPORT C-CHANNEL IS CRACKED AT STA 1000 AT LONG 28R. REMOVED, FABRICATED AND REPLACED SUPPORT FRAME C-CHANNEL IAW SRM 53-4-1 FIG 51. 2L74 4F RT4A25 20031204000882003120400088WP 2003 12 4 UPS03841399 120030929A5321 FLOOR PANEL DOUG DC8 DC873F 302199FWP STA 120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, FLOOR PANELS CORRODED FS 120 RBL 36. REMOVED CORR IAW DC8 SRM 51-1-8, CUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW DC8 SRM 53-2-3, INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-21. FABRICATED SPLICE IAW DC8 SRM 53-2-3. INSTALLED FLOOR PANEL & SPLICE PLATE IAW DC8 SRM 51-3-0, INSTALLED FLOOR BOARD IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20031204001002003120400100WP 2003 12 4 UPS03841411 120030911A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT FUSE INTERIOR L10LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED L10LT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20031204001022003120400102WP 2003 12 4 UPS03841413 120030911A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 LEFT CRACKED BETWEEN FS 1768-1777. REMOVE CRACKED LONGERON IAW UPS DC8 SRM 51-1-20 & 51-1-21. LOCATE NEW LONGERON AND DRILL EXISTING FASTENER HOLES IAW UPS DC8 SRM 51-3-2. INSTALLED NEW LONGERON IAW UPS DC8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20031204001082003120400108WP 2003 12 4 UPS03841426 120030919A531297516493 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, BULKHEAD AT STA 680 LONG 33L AFT SIDE OF PRESSURE DOME CRACKED IN RADIUS (LOWER). REMOVED AND REPLACED PRESSURE DOME STA 680 LT SECTION IAW DC8 SRM 51-1-202D AND 51-3-0. 2L74 4F RT4A25 20031204001232003120400123NM 2003 12 4 AWXA200301264 120031007A53156546592 FLOORBEAM BOEING737 7373G7 138447JNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM AND NUT PLATES AT BS 727D+5, LBL 8. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT DAMAGED SECTION OF FLOORBEAM BS 727D+5, LBL 8; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 FIG 201. 2L72 4F RTA16WE 20031204001382003120400138NM 2003 12 4 C1HA200397015 120031019A3350 BATTERY PACK BOEING727 727270 138408PNM EXTERIOR EMER INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 RIGHT FWD EXTERIOR WING LIGHT INOP. REMOVED & REPLACED BATTERY PACK AT STA 835. REF M/M CH 33-50-23, OPS OK. 2L73 4F RTA3WE 20031204001432003120400143NE 2003 12 4 COMA0370037 220031014A7200CF348C1 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LEFT VIBRATES A COMAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO01331CA2514 10061 965649 FLIGHT 5080 LEFT ENGINE VIBRATION, INDICATED AS HIGH AS 3.2. REPLACED LEFT ENGINE. 2L72 4F4 FRTA21EA EOOO63EN 20031204001542003120400154SO 2003 12 4 CHQA000426 120031017A21508152403 ACM EMB 145 EMB145LR 3260212SO NR 1 FROZEN A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11841 857 857 145737 DURING CLIMBOUT OF DFW AT 10,000 MSL, SMOKE APPEARED IN THE COCKPIT WITH A STRONG BURNING ODOR. APPROPRIATE CHECKLISTS WERE ACCOMPLISHED AND TURNED BACK TO DFW. PACK NR 1 AND BLEED 1 WERE SECURED AND THE ODOR SUBSIDED IMMEDIATEDLY. UNEVENTFUL LANDING IN DFW. UPON INSPECTION FOUND NR 1 ACM LOCKED UP. REMOVED AND REPLACED NR 1 ACM AND SYSTEM OPS CHECKED GOOD PER AMM 21-51-03. 2L72 4T RTT00011AT 20031204001552003120400155EU 2003 12 4 AWXA200301269 120031008A5414D5430052200201 SKIN AIRBUS320 A320231 3930325EU ZONE 420 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-03 CHECK THE NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN WAS FOUND PITTED. MAINTENANCE REMOVED DAMAGED NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN; FABRICATED NEW REPLACEMENT SKIN PER A320 SRM 51-26-71, PG 1-13, FIG 1-5; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-10, & 12, FIG 2, 7, 3. 2L72 4F RTA28NM 20031231000482003123100048EA 2003 12 31 ASOA03579 120031115A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031231000612003123100061WP 2003 12 31 GTIA030911 120031105A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND CABIN FLOOR PANEL CENTER STATION 807-826 CORNERS DELAMINATED. FABRICATED NEW CABIN FLOOR PANEL. (M) 2L72 4F RTA6WE 20031231000842003123100084WP 2003 12 31 GTIA030931 120031103A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSLEAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND CABIN STATION 389 RIGHT OUTBOARD FLOOR PANEL CRACKED. FABRICATED NEW RIGHT OUTBOARD FLOOR PANEL. (M) 2L72 4F RTA6WE 20031231001232003123100123NM 2003 12 31 TSAA0357061 120030410A57306545457 ACCESS DOOR BOEING737 737209 13844AENM LT WING FUEL CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 REMOVED CORROSION DAMAGE BY BLENDOUT REPAIR PER GUIDANCE IN SRM 57-30-3, FIGURE 5, DETAL III. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II TO BLENDOUT LOCATIONS. FILLED DEPRESSION WITH BMS 5-26, TYPE II SEALANT TO RESTORE SURFACE TO ORGINAL CONTOUR. REPAIR COMPLETED IAW ECO 2268 WITH DEVIATION A. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040105000232004010500023NM 2004 1 5 DL76L031011 120031113A3350 LIGHT BOEING767 767332 1382001NM AFT RT LAV AISLEDETACHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27190DN 28447 DURING EPDC - FOUND ESCAPE PATH EXIT IDENTIFIER SIGN (RED) PULLED LOOSE WITH BROKEN WIRES AT AFT RIGHT LAVATORY, ADJACENT TO AISLE. RE-ATTACHED LIGHT ASSY PER BOEING STD WIRE PRACTICES. LIGHT OPERATES OK. 2L72 4F RTA1NM 20040105000382004010500038 2004 1 5 MALA030552 420031213A3410 CONTROL UNIT BAC 146 AVRO146RJ85A1500097EU RUDDER LIMITER MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15518XJ E2337 DURING FLIGHT 3440, RUDDER LIMITER LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED ADAU ALL CHECKS GOOD IAW RJ-85 MM CH 34. S/N OFF 644/WDFD/98, P/N OFF WDFD-ATEL-1025-000, S/N ON 561WDFD97, P/N ON HC396HO485-008. 2H74 4F RTA49EU 20040105000502004010500050NM 2004 1 5 DL73S031025 120031117A53306545767103 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 A DENT WAS NOTED IN THE FUSELAGE SKIN AT BS 380, BETWEEN S17L AND S18-L. THE DENT WAS CUT OUT AND REPAIRED PER ERA 385827-14. 2L72 4F RTA16WE 20040105000652004010500065NM 2004 1 5 2003UALA00945 120031209A5230 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29370UA 24539 AFT CARGO DOOR OUTER SKIN IS DENTED APPROX 12 INCHES AFT OF FWD EDGE AND 12 INCHES UP FROM BOTTOM EDGE. W=1.7, D=.085, RATIO=20. DENT DOES NOT HAVE ANY SHARP CREASES, TOTAL DENT LENGTH IS APPROX 5 INCHES IN LENGTH. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040105000992004010500099WP 2004 1 5 DHL2003802540 120031126A5310 DOOR FRAME DOUG DC8 DC873 302199CWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT PASSENGER DOOR JAMB LWR FWD CORNER INTERIM REPAIR, STA 1620.000 L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18, SERVICE REWORK DWG SR08530021, DWG 5750776. REMOVED INTERIM REPAIR IAW SRM 51-1-20D PG 21. FABRICATED DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 18, SERVICE REWORK DWG SR08530021, DWG 5750776. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND TRIPLER AND NEW FASTENERS IAW SRM 53-2-0 FIG 18, SERVICE REWORK DWG SR08530021, DWG 5750776, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040105001672004010500167CE 2004 1 5 AMWA92 120031212A5330114430002199 PLATE BEECH 1900 1900D 1154162CE FUSELAGE CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 DURING AN ABC STRUCTURAL INSPECTION, THE LEFT AND RIGHT PRESSURE PLATES HAD EVIDENCE OF RIVET CHAFE. 2L72 4T RTA24CE 20040105001732004010500173NM 2004 1 5 AWXA200301617 120031204A551265C2514515 TIP CAP BOEING737 737301 1384611NM HORIZ STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MINOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LT HORIZONTAL STABILIZER TIP LEADING EDGE LBL 252.10. MAINTENANCE BLENDED OUT CRACK ON LT HORIZONTAL STABILIZER TIP LEADING EDGE; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16, REPAIR 11. 2L72 4F RTA16WE 20040105001782004010500178NM 2004 1 5 AWXA200301622 120031207A53156546811 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM BS 1016, LBL 4 TO LBL 16. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM BS 1016, LBL 4 TO LBL 16; FABRICATED 2 EACH SUPPORT ANGLES & 4 EACH STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51 FIG 202, PG 207 & 211. 2L72 4F RTA16WE 20040106000092004010600009WP 2004 1 6 DHL2003802573 120031204A53505656351401 SKIN PANEL DOUG DC8 DC873 302199CWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING TO FUSELAGE NR 706 PANEL EXTERNAL SKIN DELAMINATED STA 912.000 - STA 980.000. REMOVED DELAMINATED PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED LPS3 IAW SRM 51-1-8 PG 35-36. INSTALLED NEW PANEL ASSY ON LEFT WING TO FUSELAGE IAW SRM 51-3-0 PG 1 (STA 912.000-980.000). 2L74 4F RT4A25 20040106000412004010600041WP 2004 1 6 DHL2003802574 120031128A575497532974 RIB DOUG DC8 DC873 302199CWP L/E SLAT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT OUTBD STUB WING RIB HOLES ELONGATED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM 201846, DWG 9753297. REMOVED DAMAGED RIB IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED RIB IAW ATM 201846, DWG 9753297. HEAT TREATED IAW SRM 51-1-1 PG 13, 21 SRM 51-1-4 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-20D PG 9 SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040106000432004010600043WP 2004 1 6 DHL2003802569 120031120A5311 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 NOSE SECTION FRAME WITH 0.500 AND 1.000 CRACK IN IT, STA -131.000 L-31L TO L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-3 PG 9. REMOVED DAMAGED FRAME IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. FABRICATED FRAME IAW SRM 53-3-3 PG 1. HEAT TREATED FRAME IAW SRM 51-1-1 PG 1, 13, 17 SRM 51-1-4 PG 1, 2, 3. CLEANED, TREATED AND PRIMED AREA AND FRAME IAW SRM 51-1-8B. INSTALLED NEW FRAME IAW SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040106000702004010600070NM 2004 1 6 F3LA200300178 120031216A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CAP, LBL 17 TO RBL 13. REPAIRED UPPER CHORD ON STA 947 PER EA B3-53R-10228. 2L72 4F RTA16WE 20040106001042004010600104NM 2004 1 6 CALA0300712 120031216A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 INSPECTION FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 328, LBL 30. A REPAIR WAS INSTALLED IAW SRM 53-10-51. 2L72 4F RTA16WE 20040106001152004010600115NM 2004 1 6 DHL2003742531 120031120A5330 SKIN BOEING727 727225 1384077NM FUSELAGE WRINKLED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSELAGE EXTERNAL SKIN BS 400 TO 420 STR 24R TO 23R SKIN WRINKLE. REMOVED PREVIOUS REPAIR AND ADJACENT FASTENERS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA IAW B-727 SRM 53-20-3 FIG 23, SHEET 10, DETAIL IX (19 X 1.5 INCH). FABRICATED NEW DOUBLER REPAIR IAW B-727 SRM 53-30-3, FIG 23, SHEET 10 AND 7. TREATED AND PRIMED REPAIR DOUBLER AND REWORKING AREA IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-30-2 AND SRM 51-20-4. 2L73 4F A3WE 20040106001262004010600126NM 2004 1 6 DHL2003742533 120031203A5310 DOOR FRAME BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE, FLORIDA DISCREPANCY AS FOLLOWS, N/R 60776 C-2 DOOR CUT OUT AFT FRAME STA 990, INNER CHORD LOWER SURFACE HAS HEAVY CORROSION BETWEEN STR 25R-26R. CORROSION ON AFT FRAME ON C2 DOOR CUT OUT FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA 2.5 X 1 INCH AND FABRICATED ONE FILLER SAME DIMENSIONS AND ONE DOUBLER IAW B-727 SRM 53-10-2 FIG 6 AND 51-40-3. ALODINED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR AT C-2 DOOR CUTOUT AFT FRAME UPPER DOOR IAW B-727 SRM 51-40-3. 2L73 4F A3WE 20040106001392004010600139EA 2004 1 6 COMA0360557 120031213A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01976CA 7151 FLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040106001432004010600143NE 2004 1 6 COMA0370056 220031213A72304114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ENGINE DAMAGED A COMAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO01317CA2538 10055 965372 FLIGHT 5043 RT ENGINE FAN VIB CAUTION MESSAGE. REPLACED THE RT ENGINE FAN BLADES. 2L72 4F4 FRTA21EA EOOO63EN 20040106001542004010600154NE 2004 1 6 DHL2003805014 220031218A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 1 FLAMED OUT A DHLAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 SO01805DH 46125 693219 NR 1 ENGINE FAILED / FLAMED OUT AFTER START & STABILIZED. INSPECTED NR 1 ENGINE FUEL SHUT-OFF RIGGING, SPECIFIC GRAVITY SETTING, AND FOR LEAKAGE. NO DEFECTS NOTED. CHECKED IGNITION -A- AND -B- FOR PROPER OPERATION. PERFORMED 3 EACH STARTS. RAN ENGINE AT VARIOUS POWER SETTINGS. PERFORMED ENGINE ACCELERATION CHECK. NO DEFECTS NOTED. WORK DONE IAW CFM M/M 71-00-00 & JRH CHAPTER 13. 2L74 4F4 FRT4A25 E2GL 20040106001592004010600159EA 2004 1 6 03352669 120031218A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE CABIN OVERHEAD EMERGENCY LAMP AT ROWS 2 AND 4 WERE FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040106001672004010600167EA 2004 1 6 QXEA200301570 120031218A26129847101505 SCREEN CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX- CENTER CHIMNEY IN FORWARD CARGO BAY HAS TORN SCREEN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040106001702004010600170SO 2004 1 6 C2XA03TY216 120031220A532014521725013 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS DURING A SCHEDULED 3C INSPECTION THE FORWARD SERVICE DOOR SILL WAS FOUND CORRODED. MAINT CLEANED UP THE CORROSION, REPAIRED, ALODINED, PRIMED AND PAINTED IAW EMB 135/145 EC 2003-145/1158; SRM 53-21-10; CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040106001712004010600171NM 2004 1 6 P5CA0301009 120031219A523065B73296 ROD BOEING747 7472U3B 1384846NM CARGO DOOR DEFECTIVE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 SIDE CARGO DOOR FAILS TO CLOSE. REPLACED INPUT ROD TO FWD HOOK TORQUE TUBE IAW 52-32-11. 2L74 4F RTA20WE 20031231001252003123100125NM 2003 12 31 TSAA0253253 120030114A53306546559 SKIN BOEING737 737230 1384401NM FUSLEAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 CUTOUT DAMAGED SKIN ARE AT BS 908 MAINTAINING A .50 INCH MINIMUM RADIUS AND 2D EDGE MARGIN. VERIFIED CRACK REMOVED USING HFEC METHOD. ENLARGED TRIMMED AREA BY .04 INCH AS AN INSURANCE CUT. FABRICATED TWO STRUCTURAL FILLERS, A REPAIR FILLER, DOUBLER, AND TRIPLER FROM 2024-T3 CLAD MATERIAL. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT BETWEEN THE FRAYING SURFACES. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, SHEET 55. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040105000152004010500015NM 2004 1 5 DL738030999 120031110A3350D71701100 BATTERY PACK BOEING737 737832 13844CFNM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER L NO TEST ININSP/MAINT 1 SO273754A 29626 EMERGENCY LIGHTS INOP ROW 10 -15. FOUND SEAT HARNESS SHORTED AT ROW 13. REPLACED SEAT HARNESS, REPLACED FUSES AND BATTERY PACK IN M1676. 2L72 4F RTA16WE 20040105000162004010500016NM 2004 1 5 UPS03241673 120031229A2613 OVERHEAT LOOP BOEING727 72725C 138400HNM NR 1 ENGINE FALSE INDICATIONA IPXAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 SO01937UP 19302 NR 1 ENGINE 1 STRUT OVERHEAD ILLUMINATED IN FLIGHT. ENGINE SHUT DOWN. REMOVED AND REPLACED NR 1 ENG OVERHEAT DETECT LOOPS PER MM 26-14-12. OPS CHECKS GOOD PER MM 26-14-00. REMOVED AND REPLACED FIRE AND OVERHEAT DETECTION BOX FOR PRECAUTION PER MM 26-14-00. 2L73 4F A3WE 20040105000462004010500046NM 2004 1 5 DL76S031021 120031116A2121 CIRCUIT BREAKER BOEING767 767332 1382001NM FAN TRIPPED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27135DL 1224334 25145 AT CRUISE, F/A REPORTED ELECTRICAL ODOR THRU OUT CABIN. DID ELECTRICAL SMOKE CHECKLIST AND PULLED C/BS ON VIDEO SYS. TURNED OFF RT RECIR FAN, THAT WAS REPORTED TO BE CAUSING VIBRATION AND PULLED C/B ON GASPER FAN (OFF LIGHT APPEARED IN GASPER LIGHT SWITCH AND FAILED AFTER RESTTING. ELECTRICAL ODOR WENT AWAY AFTER TURNING OFF UTILITY BUSSES. FWD GASPER FAN MCO AND PLACARD PER MEL 21-24-01. REMOVED AND REPLACED GASPER FAN PER AMM. MCO / PLACARD REMOVED. 2L72 4F RTA1NM 20031204001632003120400163EU 2003 12 4 MALA030459 120031013A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15363PX 340B260 DURING 4Y-2Y INSPECTION IN CWA, RT CARGO FRAME STA 658.5, 11.5 INCHES ABOVE SL 1620 CHAFE. MAINTENANCE REPAIRED DAMAGE IAW EO S53152 INSTALLATION OF DOUBLER. 2L72 4T RTA52EU 20031204001812003120400181SO 2003 12 4 C2XA03TY185 120031020A531514522226003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM CAP AT FRAME 61 WAS FOUND TO BE CORRODED AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031204001842003120400184EU 2003 12 4 MALA030468 120030929A5753 BUSHING BAC 146 AVRO146RJ85A1500097EU FLAP TRACK CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, FOUND LEFT FLAP POSITION TRACK NR 2 AFT LINK AFT /IB BUSHING CORRODED. FOUND LEFT FLAP, POSITION TRACK NR 4 AFT LINK O/B BUSHING CORRDED. MAINTENANCE REPLACED BUSHINGS IAW EO AD 020307. REFER TO 189958 AND 189959 FOR ADDITIONAL INFORMATION. 2H74 4F RTA49EU 20031204001852003120400185EU 2003 12 4 MALA030467 120030929A5753 BUSHING BAC 146 AVRO146RJ85A1500097EU LT FLAP TRACK CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, FOUND LEFT FLAP POSITION TRACK NR 4 FWD LINK, FWD BUSHING CORRODED. MAINTENANCE REPLACED BUSHING IAW EO AD020307. REFER TO 189960 FOR ADDITIONAL INFORMATION. 2H74 4F RTA49EU 20031204001932003120400193EA 2003 12 4 03291648 120031018A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27648BR 7406 DURING INSPECTION THE FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031204001962003120400196EA 2003 12 4 032936542 120031020A5315601R5361004 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 DURING HEAVY INSPECTION THE FLOOR SUPPORT ANGLE AT FS 621 BL 41 WAS FOUND CRACKED. 2L72 4F RTA21EA 20031204002032003120400203WP 2003 12 4 UPS03841451 120031012A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 CORROSION FOUND IN LONGERON 31 STATION 1338 AFT PIT FLOOR PANEL TEMP. INSTALLED REPAIR LONGERON 31L AT FS 1350 IAW REO G09527. 2L74 4F RT4A25 20031205000082003120500008NM 2003 12 5 PCAA0310127 120031022A2930 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM HYD SYSTEM FALSE ACTIVATIONA PCAAB EMER. DESCENT N FALSE WARNING DEDESCENT 1 EA13843EX 335 WHILE ON DESCENT, FLIGHT 3540, INTO YUL (MONTREAL) PILOT NOTICED HYDRAULIC ISOLATION VALVE LIGHT AND INBOARD ROLL SPOILER LIGHTS BOTH ILLUMINATED AND NOTICED NR 1 SIDE HYDRAULIC QUANTITY SHOWED LESS THAN 1.5 QUARTS. AN EMERGENCY DESCENT WAS DECLARED INTO YUL. MAINTENANCE INSPECTED FOR HYDRAULIC LEAKS, NONE FOUND. NR 1 HYDRAULIC SYSTEM WAS BLED, AND GROUND RUNS WERE CARRIED OUT. ALL RUN CHECKS NORMAL. ALSO ASSOCIATED CONNECTORS WERE INSPECTED AND CLEANED. NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031205000102003120500010NM 2003 12 5 C1HA200393017 120031022A2910 LINE BOEING727 727212 138407GNM HYD SYSTEM LEAKING A C1HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL15293AS 21348 DURING CLIMB ENG NR 1 HYD SYSTEM A LOW PRESSURE LIGHT ILLUMINATED WHILE PERFORMING COM PROCEDURES SYSTEM-A QUANTITY WAS OBSERVED TO BE 0. PERFORMED HYD SYSTEM FLUID LOSS PROCEDURE. RETURNED TO MDPC REMOVED AND REPLACED PRESSURE LINE NR 1 ENG A PUMP REF 29-32-00. RAN ENG, LEAK CHECKS GOOD. REMOVED AND REPLACED NR 1 ENG PUMP IAW 29-11-41. REMOVED AND REPLACED CASE DRAIN FILTERS REF 29-11-30. RAN ENG, NO LEAKS NOTED. GOOD SYSTEM PRESSURE. 2L73 4F A3WE 20031205000112003120500011WP 2003 12 5 0301949992 120031011A2910DWG7920134785 LINE DOUG DC9 DC931 3022065WP HYD SYSTEM BROKEN A NWAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01896OE 45869 DURING CRUISE FLIGHT, BOTH THE LEFT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO INDICATION. CREW APPLIED COM PROCEDURES, VERIFIED COMPLETE LOSS OF SYSTEM, AND LANDED UNEVENTFULLY AT MSP. MAINTENANCE FOUND A BROKEN ELEVATOR PRESSURE LINE AND REPLACED IT. ALSO, REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND RESERVICED THE SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20031205000182003120500018 2003 12 5 DL757030904 420031006A3100233T42467 PANEL BOEING757 757232 1384965NM COCKPIT UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27658DL 24420 SQUIB TEST PANEL INOP IN BOTH 1 AND 2 POSITIONS. REPLACED PANEL. 2L72 4F RTA2NM 20031205000242003120500024NM 2003 12 5 DL76K030911 120031009A335002031461201 LIGHT BOEING767 767332 1382001NM FWD ENTRY DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27175DZ 29696 FOUND FWD RT EMERGENCY EXIT IDENTIFIER DAMAGED. REPLACED FWD EMERGENCY EXIT IDENTIFIER. 2L72 4F RTA1NM 20031205000272003120500027NE 2003 12 5 DLM88030917 220031011A7314 PUMP DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO27945DL 49818 726015 AT LEVEL OFF (FL230) RT ENG FLAMED OUT, LT ENGINE BECAME UNSTABLE, BUT RECOVERED. RIGHT ENG FAILED COMPLETELY. NO VIBES NOTED. REPLACED FUEL PUMP AND CONTROL. 2L72 4F4 FRTA6WE E9NE 20031205000342003120500034NM 2003 12 5 DL73S030924 120031010A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307DL 23079 A TYPICAL CRACK WAS FOUND IN THE LOWER FORWARD CORNER OF THE L2 DOOR CUTOUT THROUGH THE SKIN, BONDED DOUBLER, AND UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 1 X 2 INCH CUTOUT THROUGH THE STACK-UP. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER B737 SRM 53-30-3 FIG 24 AND ER/A 087496-14, REV A. 2L72 4F RTA16WE 20031205000382003120500038NM 2003 12 5 DLM88030928 120031014A53305920323211 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27908DL 49539 THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CRACKED AT THE FWD EDGE OF THE C1 DOOR CUTOUT BETWEEN LONGERON 24 & 25. THE CRACK WAS CUT OUT OF THE SKIN AND DOUBLER. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385745-14. 2L72 4F RTA6WE 20031205000442003120500044 2003 12 5 DLM11030934 420031018A2340230616510 AMPLIFIER DOUG MD11 MD11 3023602NM PA SYSTEM ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27807DE 48478 PA FAILED IN FLT. PA AMP NR 1 CB PULLED AND AMP REMOVED DUE TO COMPLAINTS OF ELECTRICAL ODOR. REPLACED PA AMP. 2L73 4F RTA22WE 20031205000522003120500052NM 2003 12 5 DL757030944 120031021A5330146N351112 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27659DL 24421 THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED BETWEEN FS 1420 & 1440 AND BETWEEN STRINGERS 27R & 29L. THE DAMAGE WAS REMOVED WITH A 14.9 X 2.75 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385709-14, REV A. 2L72 4F RTA2NM 20031204000452003120400045WP 2003 12 4 GTIA030838 120031006A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FORWARD CABIN FLOOR BOARD STATION 200 TO STATION 160 RBL 44 TO RBL 55 HAS SEVERAL INSERTS CORRODED/SOFT MUCHEY. FABRICATED NEW FORWARD CABIN FLOOR BOARD. (M) 2L72 4F A6WE 20031204000472003120400047WP 2003 12 4 AALA20031046 120030921A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21972TW 53622 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROW 20. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031204000582003120400058WP 2003 12 4 GTIA030843 120031010A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND SUBFLOOR CORRODED STATION 195 LBL 50. REMVOED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M) 2L72 4F A6WE 20031204000842003120400084NM 2003 12 4 UPS03541439 120031013A5610 WINDOW BOEING757 75724APF 1384969NM COCKPIT OUT OF RIG A IPXAK NONE O OTHER ININSP/MAINT 1 SO01465UP 28269 INSPECTION TYPE:ASV WHEN L2 WINDOW IS LATCHED CLOSED LINK ARM WILL NOT STAY PERPENDICULAR TO THE WINDOW TRACK. ADJUSTED L2 WINDOW OPERATING MECHANISM CLUTCH WITH REF TO MM 56-11-02- 5 WINDOW OPERATES NORMALLY. 2L72 4F RTA2NM 20031204001342003120400134EU 2003 12 4 0301933209 120031015A2131 OUTFLOW VALVE AIRBUS320 A320211 3930320EU CABIN PRESSURE MALFUNCTIONED A NWAAB EMER. DESCENT O OTHER CRCRUISE 1 GL01309US 118 AT CRUISE FL350, LOST CABIN PRESSURE. CABIN PRESSURE CLIMBED TO 11,000 FT DURING EMERGENCY DESCENT. DESCENDED TO 10,000 FT AT 10,000 FT CABIN RE-PRESSURIZED NORMALLY. PACKS FUNCTIONED NORMALLY AND OUTFLOW VALVE WAS CLOSED DURING EMERGENCY DESCENT. FLIGHT CONTINUED TO MSP WITH AN UNEVENTFUL LANDING. REPLACED PRESSURIZATION OUTFLOW VALVE (32-2130-9-0007, S/N OFF 3143) AND CABIN PRESSURE CONTROLLER (32-2130-9-0004, S/N OFF 54554). OPERATIONAL CHECK GOOD. AIRCRAFT EXPERIENCED A RAPID DEPRESSURIZATION ON THE FOLLOWING FLIGHT. FOUND FORWARD CARGO DOOR SEAL INFLATION HOLES FILLED WITH SEALANT. REPLACED SEAL. 2L72 4F RTA28NM 20031204001352003120400135NM 2003 12 4 252TR0013 120031018A33501104441 RECEPTACLE BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 EMERGENCY LIGHT OVER L1 DOOR INOP. REPLACED EMERGENCY LIGHT RECEPTACLE OVER L1 DOOR. OPS CHECKS GOOD. 2L72 4F RTA16WE 20031204002002003120400200NM 2003 12 4 252TR0014 120031021A33501000677 LIGHT BOEING737 737228 13844AGNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 EMERGENCY EXIT LAMP IN COCKPIT OVERHEAD WILL NOT MAINTAIN BATTERY CHARGE. REPLACED EMERGENCY EXIT LIGHT AT CAPT OVERHEAD POSITION. OPS CHECKS OK. 2L72 4F RTA16WE 20031205000562003120500056WP 2003 12 5 CNMA200300004 120031017A2820234125 RELIEF VALVE DOUG DC10 DC1030 3023501WP FUEL SYSTEM LEAKING A CNMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0749082 47927 FUEL REPORTED LEAKING INFLIGHT FROM RIGHT AILERON AREA- FUEL QUANTITY LOSS CONFIRMED. AIR TURNBACK TO FRA. 2L73 4F A22WE 20031205000592003120500059SO 2003 12 5 SWIA200312518 120031015A2120 SMOKE EMB 120 EMB120ER 3260203SO COCKPIT DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07583SW 120351 ON THE GROUND, CABIN AND COCKPIT FILLED UP WITH SMOKE WITH APU RUNNING. RAN BOTH PACKS INDEPENDANTLY, NO SMOKE NOTED. RAN BOTH PACKS IN MAN AND AUTO, NO SMOKE. PACKS OPERATE NORMALLY. 2L72 4T RTA31SO 20031205000682003120500068NM 2003 12 5 2003UALA00777 120031015A5754 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 1 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 NR 1 SLAT DELAMINATED OB END OF LOWER SURFACE OF T/E WEDGE OF AREA 3.3 INCHES CHORDWISE X 1.6 INCHES SPANWISE. THE ABOVE NOTED DELAM CONDITION WAS DUE TO WEAR FROM NORMAL LOADS EXPERIENCED DURING A FLIGHT OVER A PERIOD OF TIME. THE TRAILING EDGE WEDGE OF THE SLAT WAS REPAIRED USING AN ADHESIVE INJECTION METHOD. 2L72 4F4 FRTT0001SE E46NE 20031208000052003120800005NM 2003 12 8 03FDEA01950 120031119A5753 FITTING DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 RT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNTING MATING SURFACE CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, I/B HINGE FITTING LOWER MOUNTING MATING SURFACE CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5740-74250. WINGS - LT & RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031208000082003120800008CE 2003 12 8 DXTA200300153 120031105A3240NAS161216 O-RING CESSNA560 560XL 2076702CE BRAKE SYSTEM FAILED E DXTAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07610QS 5605210 DURING TAXI "LO BRAKE PRESS" AND "ANTISKID INOP" ILLUMINATED. LOST BRAKE PEDAL PRESSURE, STOPPPED AIRCRAFT WITH EMERGENCY BRAKES. HAD AIRCRAFT TOWED TO PARKING POSITION, POST FLIGHT INSPECTION FOUND LEAKING OIL FROM AVIONICS BAY AND NOSE GEAR ASSEMBLY. - FOUND O-RING AT ANTI SKID POWER PACK FILTER BOWL LEAKING, INSTALLED NEW O-RING AND APPLIED POWER TO ANTI SKID NO LEAKS NOTED. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20031208000132003120800013EA 2003 12 8 SWIA200312511 120031021A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R31113-58 2L72 4F RTA21EA 20040105000482004010500048NM 2004 1 5 DLM88031023 120031116A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27909DE 53418 A 6 INCH CRACK IN FUSELAGE SKIN AT PREVIOUS GOUGE BLEND REPAIR FS 1236 TO FS 1242 BETWEEN LONGERONS 22R AND 23R. REPAIRED SAME. 2L72 4F RTA6WE 20040105000632004010500063NM 2004 1 5 2003UALA00943 120031208A2425 SOLENOID BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 1 GEN ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29613UA 21874 ABORTED TAKEOFF DUE TO A NR 1 ENGINE GENERATOR INDICATION. REPLACED THE IDG. SHOP FINDINGS REVEALD THAT THE DISCONNECT SOLENOID FAILED. SOLENOID AND FILTER WERE REPLACED. 2L72 4F4 FRTA1NM E3NE 20040105001002004010500100WP 2004 1 5 DHL2003802532 120031124A5720 BRACKET DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING CTR L/E NR 1 ENG FIREWALL S/O VALVE SUPPORT ARM BRACKET CRACKED. REMOVED CRACKED BRACKET FROM NR 1 ENG FIREWALL S/O VALVE SUPPORT ARM AND FABRICATED A NEW ONE IAW SRM 51-3-0 PG 1, SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040105001422004010500142WP 2004 1 5 ABXA030479 120031209A523059101415 PAN DOUG DC9 DC932 3022066WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 FORWARD LOWER CARGO DOOR CRACKED AT PAN EDGE UNDER AFT DOOR LATCH. REPLACED DOOR ON NON ROUTINE 0155 AND DC-9 SRM. 2L72 4F A6WE 20040105001762004010500176NM 2004 1 5 AWXA200301620 120031207A53206546812161 STRAP BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT LAVATORY MAIN DECK STIFFENER STRAP BS 1016, LBL 6 TO RBL 6. MAINTENANCE REMOVED CORRODED STIFFENER STRAP BS 1016, LBL 6 TO RBL 6; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 9, PG 39. 2L72 4F RTA16WE 20040106000832004010600083SO 2004 1 6 C2XA03SH502 120031218A532014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 15. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR EMB IC2003-145/4250. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040106001692004010600169SO 2004 1 6 C2XA03SH509 120031220A532014528737001 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 R WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040106001812004010600181NM 2004 1 6 03FDEA02221 120031220A2781106081918 SWITCH BOEING727 727200 138407ENM KRUEGER FLAP FAULTY A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25469FE 21581 DURING FLAP RETRACTION NR 3 KRUEGER FLAP FAILED TO RETRACT, RECYCLED WITH NO CHANGE. NO RESTRICTION NR 3 KRUEGER FLAP HAS THE RETRACT SWITCH JUMPER INSTALLED. RAN FLAPS THRU, FWD & AFT INDICATOR LIGHTS CK NORMAL. REPLACED NR 3 KRUEGER FLAP INDICATION SWITCH REF 27-82-001-4. GROUND OPS CK NORMAL AT THIS TIME. JUMPER INSTALLED BACK IN F/E DESK. CLEARS CONTROL NR 182339. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20040106001902004010600190NM 2004 1 6 AALA20031261 120031112A335060030451 BATTERY BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, FOUND RIGHT AFT FLIGHT ATTENDANT EMERGENCY LIGHT LED NOT FLASHING. REPLACED BATTERY FOR RIGHT AFT FLIGHT ATTENDANT EMERGENCY LIGHT LED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040106001922004010600192NM 2004 1 6 USAABB03211 120031120A3350873100151REV12 BATTERY BOEING757 757225 1384959NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19604AU 22199 TPA - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 9 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20040106001942004010600194WP 2004 1 6 GTIA030993 120031030A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND AFT PIT STATION 1231 RIGHT SIDE CORRODED AT END FRAME ATTACHED TO JAMB BEAM. REMOVED DAMAGED SECTION OF FRAME. FABRICATED 2 EACH REPAIR ANGLES. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR ANGLES DOUBLERS AND FRAME SEGMENT. (M) 2L72 4F RTA6WE 20040106002082004010600208WP 2004 1 6 GTIA030987 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND FLOOR PANEL CENTER STATION 945-980, DETERIORATING, MISSING INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040106002132004010600213NM 2004 1 6 SWAA032686 120031209A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SPECIAL VISIT FOUND SHEAR TIES CRACKED AT BS 807 STRINGER 14L, BS 767 STRINGER 14L, BS 360 STRINGER 14L. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040106002152004010600215NM 2004 1 6 SWAA032688 120031209A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 CYXX - DURING SPECIAL VISIT FOUND SKIN CRACKED AT BS 787 BELOW STRINGER 13R. REPAIRED SKIN PER ERO. (M) 2L72 4F RTA16WE 20040106002172004010600217NM 2004 1 6 SWAA032694 120031207A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 PAE - DURING SCHEDULED D-CHECK, FOUND CORROSION ON BS 272 STRINGER 22. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040106002182004010600218NM 2004 1 6 SWAA032695 120031209A53126516300 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 PAE - DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 178.5, LBL 24, WL 207. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040106002232004010600223NM 2004 1 6 SWAA032691 120031209A575465C26602 STRUCTURE BOEING737 7373A4 1384585NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 PHX - DURING SCHEDULED C4 CHECK, FOUND NR 6 SLAT TRAILING EDGE DELAMINATED AT INBOARD END. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031014000222003101400022NM 2003 10 14 UPS03541242 120030906A5330 SKIN BOEING757 75724APF 1384969NM FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01449UP 27738 INSPECTION TYPE: C1, FUSELAGE SKIN HAS 3 LIGHTNING STRIKES AT BS 1745 BETWEEN STR 24L AND STR 25L. REPAIRED IAW ER 03-3472 DATED 09/15/03 2L72 4F RTA2NM 20031014000262003101400026CE 2003 10 14 54446AMWA 120030916A3242 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE0726YV UE26 AFTER LANDING IN PNC, CAPT'S BRAKES WHERE SPONGING ON LANDING BRAKES WHERE WRITTEN UP MAINT WAS CALLED A/C WAS FERRIED TO LIT FOR REPAIR. BLEED BRAKES. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20031014000312003101400031CE 2003 10 14 AMWA57 120030910A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE073199Q UE3199Q FIVE CRACKS FOUND IN THE RIB IN JOGGLED PARTS OF RIB AT STRING INTERSECTIONS. STRING P/N 101-640000-46, 101-640000-39, 101-640000-45, 101-640000-38. CRACKS RUN HORIZONTAL TO RIB FROM LAST RIVET HOLE TO EDGE OF RIB. 2L72 4T RTA24CE 20031014000352003101400035SO 2003 10 14 ENHA2003005 220030820A8530 PUSHROD CESSNA207 T207A 2073614CE CONT O520 IO520F 17032SO NR 6 CYLINDER BENT B ENHAO OTHER O OTHER NRNOT REPORTED 1 AL038NZ 20700421 821581R NR 6 CYLINDER EXHAUST PUSHROD BENT. 1H71 3O3 O A16CE E5CE 20031014000462003101400046 2003 10 14 SWAA032222 420031003A2565D31354 SLIDE BOEING737 7372T4 1384492NM AFT SVC DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM. 2L72 4F A16WE 20031014000502003101400050NM 2003 10 14 SWAA032184 120031001A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20031014000662003101400066NM 2003 10 14 SWAA032208 120031005A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 10R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031014000742003101400074NM 2003 10 14 SWAA032200 120031002A53306545774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014000792003101400079NM 2003 10 14 SWAA032195 120031002A335065C27093 BULB BOEING737 7372H4 138448CNM FWD CABIN EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD CEILING EMERGENCY EXIT LIGHT BULB IN FWD CABIN INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F A16WE 20031014000812003101400081 2003 10 14 SWAA032193 420031004A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT SVC DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED RON, AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED AFT SVC DOOR EMERGENCY ECAV SLIDE PER MM. 2L72 4F RTA16WE 20031014000832003101400083 2003 10 14 SWAA032219 420031005A2565D31354 GIRT BAR BOEING737 7377H4 1384404NM FWD CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH CABIN DOOR SLIDES PER MM. 2L72 4F RTA16WE 20031014000842003101400084NM 2003 10 14 SWAA032218 120031006A3350BR2013 LIGHT BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C2 CHECK, FOUND EEPLS SECTION INOP IN CABIN. REPAIRED EEPLS PER MM. 2L72 4F RTA16WE 20031014000852003101400085NM 2003 10 14 SWAA032217 120031006A552365C26384 TAB BOEING737 7373H4 1384600NM RT ELEVATOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 2 HINGE CUTOUT LOWER SURFACE. REMOVED AND REPLACED TAB PER MM. 2L72 4F RTA16WE 20031208000232003120800023NE 2003 12 8 DXTA200300151 220031102A7200PW545A ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE MAKING METAL E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07605QS633 5605321 DB0655 AFTER TAKEOFF CLIMBING THRU 3000 FT OIL PRESS LIGHT CAME ON. REDUCED POWER AND LIGHT WENT OUT, ADDED POWER AND INDICATION WAS NORMAL, OIL PRESS AND OIL GAGE AGREED. INSPECTED RT ENGINE CHIP DETECTOR & OIL FILTER FOUND NO DEFECTS, SERVICED ENGINE OIL TO FULL LEVEL WITH 3 QUARTS OIL. GROUND RAN ENGINES AND FOUND NO EVIDENCE OF LEAKS AT ACCESSORY DRIVE DRAINS BUT ENGINE CONSUMED .6 QT OIL IN 30 MIN. DUPLICATED PROBLEM MULTIPLE TIMES, REPLACED RIGHT ENGINE IAW CESSNA 560XL MM CHAPTER 71-00-01 & 71-00-03, OPS CHECKED GOOD. 2L72 4F4 FRTA22CE E00059EN 20031208000282003120800028CE 2003 12 8 DXTA200300145 120031022A2150 SWITCH CESSNA560 560XL 2076702CE ACM OVERHEAT FAILED E DXTAB EMER. DESCENT M OVER TEMP CRCRUISE 1 GL07670QS 5605170 DURING FLIGHT AT FL370 THE ACM OVERHEATED FOLLOWED BY ACTIVATION OF EMERGENCY PRESSURIZATION . EMERGENCY DECLARED, AIRCRAFT DIVERTED TO CRW AND LANDED SAFELY. REMOVED & REPLACED ACM OVERHEAT SWITCH AND OPS CHECKED GOOD IAW CESSNA 560XL M/M CHAPTER 21-51-00. 2L72 4F RTA22CE 20031208000362003120800036EU 2003 12 8 AWXA200301304 120031024A3150350E017271616 COMPUTER AIRBUS320 A320231 3930325EU ZONE 120 INTERMITTENT A AWXAO OTHER JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 WP28625AW10833 064 ON TAKEOFF OUT OF SJC EN ROUTE FOR PHX AT 75 FT WITH GEAR RAISED, RECEIVED GEAR NOT DOWN WARNING & BELL & AIRCRAFT WAS NOT PRESSURIZING, ALSO HAD NO FLIGHT DIRECTOR, AUTOPILOT OR AUTOTHRUST. AT 400 FT RECYCLED LANDING GEAR & ALL SYSTEMS RETURNED TO NORMAL, ACARS NEVER LOGGED OFF TIME. MAINTENANCE REMOVED AND REPLACED NR 1 & 2 FLIGHT WARNING COMPUTERS IAW T/C R2A31303, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST OF FLIGHT WARNING COMPUTERS S/N'S 317 & 1262 WERE BOTH NO FAULT FOUND. BOTH UNITS WERE TEST AND RETURNED TO SERVICE IAW CMM 31-53-34, REV 14. 2L72 4F RTA28NM 20031208000372003120800037NM 2003 12 8 QXEA200301299 120031017A2440 FIRE DHAV DHC8 DHC8202 2809007NM ZONE 100 DETACHED A QXEAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 NM09347PH 480 AFTER COMPLETION OF FLIGHT 2146 (MRF TO PDX) AIRCRAFT TAXIED TO GATE, PASSENGERS DEPLANED NORMALLY, GROUND SERVICE AGENT HOOKED UP GPU PLUG TO THE AIRCRAFT, FLIGHT ATTENDANT NOTICED WHAT APPEARED TO BE A FIRE AROUND GPU PLUG AREA ON AIRCRAFT SIDE. FLIGHT ATTENDANT UTILIZED ON BOARD FIRE EXTINGUISHERS TO EXTINGUISH FIRE. AIRCRAFT WAS RELEASED TO MAINTENANCE FOR INSPECTION. REPAIRED IAW DHC-8 TASK 23-50-00-710-801 AND 24-41-00-710-801. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031208000452003120800045NM 2003 12 8 VNAA0310010 120031014A2400230GC02Y02 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT GENERATOR FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07460PS1054 8 3061 DURING TAKEOFF, THE CREW RECEIVED A LT GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031208000502003120800050NM 2003 12 8 VNAA0310005 120031006A26115D9422AOAO01 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07439JS197657715 3057 THE CREW REPORTED RECEIVEING A LAV SMOKE FAIL INDICATION. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031208000572003120800057EU 2003 12 8 03FDEA01794 120031023A7830683L293G01 THRUST REVERSER AIRBUS300 A300F4605R 3930327EU NR 1 ENGINE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25660FE 759 COMPLY WITH EA 6-7830-73846 EXHAUST SYSTEM -THRUST REVERSER - CORE COWL PUMP PAN DOWN DENT/GOUGE. COMPLIED WITH EA 6-7830-73846 EXHAUST SYSTEM - THRUST REVERSER - CORE COWL PUMP PAN DOWN DENT/GOUGE AT MAE. 2L72 4F RTA35EU 20031208000672003120800067EA 2003 12 8 03051620 120030220A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A VTZAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA27620BR 7179 DURING HEAVY CHECK SEVERAL HOLES WERE DISCOVERED DRILLED THROUGH THE AFT PRESSURE BULKHEAD AT FS 621. MAINTENANCE PERSONNEL REPAIRED HOLES IAW BOMBARDIER REO. 2L72 4F RTA21EA 20031208000722003120800072NM 2003 12 8 AWXA200301293 120031013A5315146N5416 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1330, RBL 14. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM AT BS 1330, RBL 14; FABRICATED REPAIR ANGLES AND A FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 1. 2L72 4F RTA2NM 20031208000822003120800082NM 2003 12 8 DHL2003740005 120031025A5210 STRAP BOEING727 7272Q9 138448MNM PAX DOOR MISINSTALLED A DHLAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SO01740DH 21930 CABIN ENTRY DOOR HARD TO CLOSE. FOUND DOOR TO BE BINDING ON WARNING STRAP DUE TO INCORRECT INSTALLATION OF STRAP. INSTALLED STRAP IAW B-727 M/M 52-11-01. OPS CHECK OF FORWARD ENTRY DOOR IAW B-727 M/M 52-11-01. 2L73 4F RTA3WE 20031208000902003120800090NM 2003 12 8 QXEA200301322 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 LEFT OUTBOARD TRACK NR 3 SEAT ATTACH AREA CORROSION AND BARE METAL APPROXIMATELY X541.00. REPAIRED IAW SRM 51-20-16 AND 51-20-36. 2H72 4T RTA13NM 20031208001052003120800105NM 2003 12 8 AWXA200301301 120031024A2560P4010021 BATTERY BOEING737 737277 1384570NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031208001322003120800132SO 2003 12 8 C2XA03SH412 120031025A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711539 145536 DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FR 20. MAINTENANCE REMOVED AND REPLACED AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031208001382003120800138NM 2003 12 8 2003UALA00787 120031021A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FUSELAGE SKIN AT STATION 525 & STRINGER 3R IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031208001402003120800140 2003 12 8 2003UALA00790 420031002A2565 TUBE BOEING747 747422 1384935NM PWA 4056 PW4056 NE ESCAPE SLIDE FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 DURING THE OVER-PRESSURIZATION TEST OF THE UPPER DECK SLIDE THE TOP TUBE FAILED. FAILURE OCCURRED AT 3.13 PSI. SLIDE WAS RETURNED TO THE OEM (GOODRICH) FOR ANALYSIS. UNABLE TO DETERMINE CAUSE OF FAILURE OR ACTION. PORTION OF THIS SLIDE HAS BEEN SCRAPPED. 2L74 4F4 FRTA20WE E24NE 20031208001462003120800146NM 2003 12 8 2003UALA00801 120031022A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 CRACK IN STR FRAME SHEAR TIE AT BS 663.75. MAJOR REPAIR ACCOMPLISHED. REPLACED STR SHEAR CLIP. 2L72 4F4 FRTA16WE E2GL 20031208001482003120800148NM 2003 12 8 2003UALA00803 120031023A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 CRACK IN STR 11R FRAME ANGLE AT BS 706. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2L72 4F4 FRTA16WE E2GL 20031208001502003120800150NM 2003 12 8 QXEA200301347 120031026A5270 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 100 LOOSE A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09409QX 4051 CLIMBING THROUGH FL200 FUSELAGE DOORS WARNING LIGHT CAME ON AND REMAINED ON FOR APPROXIMATELY 40 SECONDS. DURING THIS TIME STARTED TO COMPLY WITH THE CHECKLIST SPECIFIC TO AFT BAGGAGE DOOR INDICATION. JUST BEFORE, STARTED TO DESCEND THE WARNING LIGHT WENT OUT AND THE AFT BAG DOOR INDICAITON TURNED GREEN. THE WARNING LIGHT CAME ON AGAIN ALMOST IMMEDIATELY THEN WENT OUT. LIGHT CAME ON ONE MORE TIME VERY BRIEFLY ON DESCENT AND WENT OUT JUST AS QUICKLY AND REMAINED OUT FOR THE REMAINDER OF THE TRIP. FOUND LOOSE ELECTRICAL CONNECTOR. TIGHTENED CONNECTOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031204000492003120400049WP 2003 12 4 AALA20031041 120030921A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21576AA 53153 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROW 2B. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204001472003120400147NE 2003 12 4 03FDEA01762 220031016A7261 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE OIL SYSTEM FAILED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25309FE 48298 APPROX 1710Z FL330 CRUISE, RECEIVED A NR 1 ENG OIL LOW LIGHT, WITH L/O PSI & 0 OIL QUANTITY. ENG WAS SHUT DOWN IAW RED TABS. WINDMILL RPM REMAINED THROUGH OUT FLT. PER FLIGHT CREW EMP 447288 THE NR 1 ENG WAS RUN AT IDLE FOR A MINIMUM OF 2 MIN PER MM REF 72-00-00-6-1. THE ENG WAS OPERATED WITHOUT OIL PRESSURE IN IDEL FLIGHT OR GROUND FOR 2 MINS. THE ENG MUST BE REMOVED. REMOVED AND REPLACED NR 1 ENG PER W/C 71T0101-1 & 71T0. 2L73 4F4 F A22WE E23EA 20031204001722003120400172EA 2003 12 4 QXEA200301293 120031016A5240 DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 800 UNSECURE A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09608QX 10026 BOI- ON FLIGHT 2571 GPU PLUG-IN DOOR UNSECURED IN FLIGHT. AIRCRAFT RETURNED TO FIELD. INSPECTED GPU DOOR AND SECURED DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031205000042003120500004SO 2003 12 5 C2XA03SH383 120031011A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FR 20. MAINTENANCE REMOVED AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 53-21-20. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031205000222003120500022NM 2003 12 5 DL73S030909 120031009A25305374E COFFEEMAKER BOEING737 737232 1384475NM GALLEY OVERHEATED A DALAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27308DL 23080 PASSING 10,000 FT ON CLIMB STRONG BURNING ODOR. F/A'S CONFIRMED OVENS OFF, ODOR STRONGER, RETURNED TO ATL. FOUND FIRST CLASS COFFEEMAKER OVERHEATING. REPLACED COFFEEMAKER, OPERATION GOOD. 2L72 4F RTA16WE 20031205000352003120500035NM 2003 12 5 DL73S030925 120031010A53126546568520 STIFFENER BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27313DL 23085 INSPECTION OF THE FS 1016 AFT PRESSURE BULKHEAD PER AD 2002-10-11 REVEALED CORROSION ON THE RT BL 0 STIFFENER. NO OTHER DAMAGE WAS FOUND. THE DAMAGED AREA OF STIFFENER WAS TRIMMED AWAY AND REPAIRED PER BAC S/B 737-53A1075 AND ER/A 087493-14AD. 2L72 4F RTA16WE 20031208000192003120800019WP 2003 12 8 ARWA20031102 120031114A32461542511 WHEEL DOUG DC8 DC862F 3021972WP MLG SHEARED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 ON POST-FLIGHT FOUND NR 3 MAIN WHEEL SHEARED OFF. REMOVED AND REPLACED NR 3 MAIN WHEEL ASSEMBLY IAW MM 32-40-1. ALSO, REMOVED AND REPLACED NR 4 MAIN WHEEL ASSEMBLY IAW MM 32-40-1. 2L74 4F 4A25 20031208000242003120800024NM 2003 12 8 03FDEA01929 120031026A5753ARC2518501 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBD STRAP NEAR PIVOT BORE FOUND CORROSION. CORROSION AT LT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD STRAP NEAR PIVOT BORE (FLAP SIDE) REPAIR CARRIED OUT AS PER EA 1-5750-73338, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - INBOARD FLAP OUTBOARD HINGE STRAP FABRICATION DIFFERENCES. 2L73 4F RTA22WE 20031208000592003120800059NM 2003 12 8 03FDEA01796 120031023A531265163387 STRUCTURE BOEING727 727200 138407ENM BULKHEAD CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-5310-73206 FUSELAGE - MAIN FRAME - BS 950 BULKHEAD LOWER STRUCTURE CORROSION REPAIR, P/N 65-16338-7. COMPLIED WITH EA 7-5310-73206 FUSELAGE - MAIN FRAME - BS 950 BULKHEAD LOWER STRUCTURE CORROSION REPAIR P/N 65-16338-7, AT MAE. 2L73 4F RTA3WE 20031208001292003120800129SO 2003 12 8 RAIA00310267 120031023A321323092050003 AXLE EMB 145 EMB145LR 3260212SO MLG SHEARED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03822HK 145069 DISCOVERED LT MAIN LANDING GEAR SHOCK ABSORBER TO SWING ARM AXLE BROKEN. MAINTENANCE REMOVED AND REPLACED AXLE. 2L72 4T RTT00011AT 20031208001532003120800153NM 2003 12 8 DHL2003751013 120031028A3350 BATTERY BOEING727 727264 138408MNM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 DURING PREFLIGHT CHECK FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. FOUND THE BATTERIES TO BE DISCHARGED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER 33-50-00 PAGE 501. OPS CHECKED GOOD. OK FOR SERVICE. 2L73 4F A3WE 20031208001592003120800159NM 2003 12 8 AWXA200301321 120031026A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 FLIGHT CREW REPORTED 2 EACH AFT EMERGENCY FLASHLIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN 2 EACH AFT FLASHLIGHTS, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031014000902003101400090NM 2003 10 14 SWAA032212 120031006A53116935365 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031014000932003101400093NM 2003 10 14 SWAA032209 120031004A335065C27093 BULB BOEING737 7377H4 1384404NM EXIT LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20031008000172003100800017NM 2003 10 8 03FDEA01537 120030908A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 MAIN DECK CARGO COMPARTMENT , CARGO TRACK AT STA 755, X = 47 INCHES FOUND CROWN WORN. 2L73 4F RTA22WE 20031008000342003100800034EA 2003 10 8 QXEA200301130 120030915A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX- FORWARD BAG PIT SMOKE DETECTOR CHIMNEY IS DAMAGED. REMOVED AND REPLACED SMOKE DETECTOR CHIMNEY. 2L72 4F RTA21EA 20031008000412003100800041NM 2003 10 8 VNAA0309004 120030907A2430 GENERATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NR 1 FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07424JS 3033 DURING TAKEOFF, THE CREW RECEIVED A NR 1 DC GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW THEN RESET THE GENERATOR AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 2568 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031008000592003100800059WP 2003 10 8 UPS03841231 120030828A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, STATION 55 BELTFRAME IS CRACKED AND CORRODED BETWEEN LONG. 35L TO 35R. REMOVED DAMAGED AREA,FABRICATED AND INSTALLED REPAIR J-ANGLES I.A.W. DC8-53A-011,AND SRM 51-1-20D 2L74 4F RT4A25 20031009000112003100900011NM 2003 10 9 USAABB03169 120030919A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031009000202003100900020SO 2003 10 9 SIMA200320502 120030722A3350744436 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21642AE 145193 EMERGENCY LIGHT AT EXIT 12 C INOPERATIVE. CLEANED CONNECTORS ON THE EMERGENCY LIGHT AT EXIT 12C. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031009000262003100900026SO 2003 10 9 SIMA200320812 120030727A335078812 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21727AE 145326 CREW REPORTED THE FORWARD MOST FLOOR PROXIMTIY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031009000852003100900085EA 2003 10 9 SWIA200312407 120030910A3260 SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07588SW 7069 GEAR DISAGREE, NOSE GEAR WOULD NOT RETRACT, STAYED DOWN AND LOCKED. ALSO NOSE DOOR WARNING. ADJUSTED S2GA SWITCH ON LEFT SIDE IAW CRJ MM 32-61-15. OPS CHECK GOOD. 2L72 4F RTA21EA 20031009001162003100900116NM 2003 10 9 CALA0300534 120030917A5551 ATTACH FITTING BOEING737 7373T0 1384582NM HORIZONTAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND THE RT HORIZONTAL STABILIZER CENTER SECTION FORWARD UPPER LUG CORRODED AT AFT SIDE AROUND BUSHING. AN OVERSIZED BUSHING WAS INSTALLED IAW CMM 55-10-06 AND SRM 55-10-10. 2L72 4F RTA16WE 20031010000032003101000003NE 2003 10 10 QXEA200301142 220030917A72204114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 VIBRATION A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 NM09603QX3867 3867 10011 GEE965240 ON FLIGHT 2469 SEA TO FAT AIRCRAFT DIVERTED TO PDX DUE TO RIGHT ENGINE VIBRATION INDICATION OF 1.9 VIBRATION FELT IN AIRFRAME. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED ALL FAN BALDES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUREND TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20031010000122003101000012NM 2003 10 10 USAASB03152 120030825A261320035008300 ACCESSORY UNIT BOEING737 737301 1384611NM E/E BAY FAILED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA19558AU 23512 ON APPROACH TO PHL FROM ALB, CREW REPORTED A STRONG ELECTRICAL ODOR IN THE CABIN. CREW PERFORMED ISOLATION PROCEDURES STARTING WITH GALLEY POWER THEN CABIN LIGHTS AND THOUGHT ODOR WAS FROM VICINITY OF SEAT ROWS 5 AND 6, RIGHT SIDE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. EMERGENCY VEHICLES ESCORTED THE AIRCRAFT TO THE GATE WHERE PASSENGERS DEPLANED UNEVENTFULLY. MAINTENANCE FOUND THE M237 COMPARTMENT OVERHEAT ACCESSORY UNIT WITH FAULT. REMOVED AND REPLACED SAME. OPS CHECK GOOD. LOADED APU AND RAN PACKS. PERFORMED HIGH POWER RUNS. NO ODORS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20031010000392003101000039NM 2003 10 10 USAABB03172 120030920A2421739515C IDG BOEING767 7672B7 1385107NM RT ENGINE FAILED A USAAO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19656US21064 26847 EN ROUTE PHL-MCO, WITH THE APU ON MEL, THE CREW RECEIVED THE RIGHT GENERATOR 'DRIVE' LIGHT. FLIGHT LANDED IN MCO WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT IDG. THE APU HAD THE BATTERY REPLACED ON THE 19TH AND WAS WAITING FOR A VERIFICATION FLIGHT. THE VERIFICATION FLIGHT WAS COMPLETED SATISFACTORILY ON THE 21ST. (M) 2L72 4F RTA1NM 20031010000772003101000077EA 2003 10 10 03260654 120030917A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 DURING INSPECTION THE EMERGENCY LIGHT 2ND FROM REAR WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031124000232003112400023NM 2003 11 24 03FDEA01939 120031113A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP, INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE MATING SURFACE CORRODED (WING SIDE). LT OUTBOARD FLAP, INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE MATING SURFACE CORROSION REMOVED & REPAIRED AS PER CMM 57-44-08 AND DWG ARC0502. 2L73 4F RTA22WE 20031124000252003112400025NE 2003 11 24 P5CA0300984 220031109A7230 STRIP BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 1 ENGINE WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23354MC 23394 517365 NR 1 ENG FAN STATOR ASSY ABRADALE STRIP DAMAGE AT 4 TO 5 O'CLOCK POS. ENG CHANGE REPLACEMENT REQ'D PER ATLAS AIR FORM 01-AA-45. ACCOMPLISH PYLON INSP PER CF6-50E2 R/R WORK CARD OK TO INSTALL. REPAIRED ABRADALE STRIP PER MM 72-31-04. 2L74 4F4 FRTA20WE E23EA 20031124000282003112400028NM 2003 11 24 03FDEA01936 120031113A5710 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR MOUNT HOLE INBOARD CORRODED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74250 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031124000682003112400068WP 2003 11 24 DHL2003807015 120031118A5250 HANDLE DOUG DC8 DC873F 302199FWP COCKPIT STICKING A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01807DH 45990 COCKPIT DOOR STICKS HARD TO GET BACK IN COCKPIT, HAD TO USE BALL POINT TO MOVE LATCH FROM INSIDE COCKPIT. ADJUSTED COCKPIT DOOR PER NASI M/M 52-10-0 PAGE 501. ALL CHECKS GOOD. 2L74 4F RT4A25 20031124000942003112400094WP 2003 11 24 DHL2003802518 120031106A5712 FRAME DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING L/E UPPER FORMER CRACKED, STA XFS.295.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED NEW ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031124001152003112400115WP 2003 11 24 DHL2003807531 120031017A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT WING INBD L/E EXTERIOR SKIN CORRODED AT STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED EXISTING DOUBLER AND TRIPLER. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED AND REMOVED DAMAGED AREAS. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. FABRICATED (3) FILLERS AND DOUBLER AND TRIPLER IAW ASTAR ED EDU21-1, ASTAR DWG U21-R01. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER AND TRIPLER INNER FACE IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER AND TRIPLER IAW ASTAR ED EDU21-1, ASTAR DWG U21-R01, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031124001302003112400130NM 2003 11 24 GAIA03150ST 120031024A5311 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME DENTED IN RADIUS BS 700 ABOVE STR 17 RT. REF FASI N/R NR 61833, CUTOUT DAMAGE AND INSTALLED REPAIR DOUBLER 8 INCH BY 5.5 INCH PER B727 SRM 51-40-3 FIG 3. (M) 2L73 4F RTA3WE 20031124001332003112400133NM 2003 11 24 GAIA03140ST 120031024A5330 SKIN BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENT BS 460 BELOW STR 17RT. REF FASI N/R NR 61687, CUT OUT DAMAGE, 4 INCHES BY 4 INCHES, INSTALLED DOUBLER REPAIR PER B727 SRM 53-30-3 FIG 3. (M) 2L73 4F RTA3WE 20031124001382003112400138NM 2003 11 24 2003F00611 120031002A382097109323015 MOUNT BOEING737 7377BC NM WATER HEATER CRACKED A BJ6AK NONE O OTHER ININSP/MAINT 1 NE03171QS895 30572 DURING MAINTENANCE IT WAS NOTED THAT THE FORWARD AND AFT MOUNT STRUCTURES FOR THE AFT WATER HEATER WERE FOUND DAMAGED. WATER HEATER IS SUSPENDED AT 6 POINTS. THE REAR MOUNT WHICH PREVENTS LATERAL MOVEMENT AND THE FORWARD MOUNT WAS FOUND TO BE CRACKED. THE HEATER AND ASSOCIATED MOUNT STRUCTURE IS ADDED DURING AIRCRAFT COMPLETION. THE MANUFACTURER OF THIS INSTALLATION IS RATHEON E-SYSTEMS. THIS IS THE SECOND TIME THIS PART STRUCTURE CRACKS ON THIS AIRCRAFT TYPE. REMOVED AND REPLACED CRACKED MOUNT. L3 COMMUNICATIONS IS EVALUATING THIS PROBLEM. (M) 2L72 4F RTA16WE 20031124001482003112400148NM 2003 11 24 CALA0300602 120031009A5320655254749 STRAP BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 MAIN DECK FLOOR WEB STRAP HAS CORROSION AFT OF STA 1016. INSTALLED NEW STRAP PER SRM 51-40-02 AND 51-10-02. 2L72 4F4 FRTA16WE E2GL 20031124001582003112400158NM 2003 11 24 QXEA200301279 120031012A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX- RT INBOARD SEAT TRACK NR 7 HAS DEEP PITTING CORROSION ON TOP RAIL AROUND FASTENER HOLES BETWEEN STATION X196 AND X202. REPAIRED IAW RD8-53-1339, RD8-53-1102, RD8-53-4473 AND SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20031124001612003112400161NM 2003 11 24 QXEA200301288 120031010A5330 SKIN DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX- SCRATCHES AND NICKS IN FUSELAGE SKIN FROM X539 TO X549 BETWEEN 23L AND 26L. REPAIRED IAW DHC-8 SRM 53-00-16 AND SRM 51-20-16. 2H72 4T4 TRTA13NM E20NE 20031125000182003112500018WP 2003 11 25 DHL2003807524 120031009A534774529523 PLUG DOUG DC8 DC873F 302199FWP CARGO BAY WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MAIN CARGO COMPT NR 4 TRACK PLUGS LUGS WORN, STA 865.000. REMOVED WORN PLUG OF NR 4 TRACK, STA 865.000 IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000192003112500019WP 2003 11 25 DHL2003807542 120031019A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH83293 45990 LEFT WING OUTBD L/E EXTERIOR SKIN CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED AND REMOVED DAMAGED AREA IAW ASTAR ED EDU21-4, ASTAR DWG U21-R04. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED (3) FILLERS AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-11 PG 9. INSTALLED FILLERS AND DOUBLERS IAW ASTAR ED EDU21-4, ASTAR DWG U21-R04, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000532003112500053WP 2003 11 25 DHL2003807503 120031010A5720 SUPPORT ANGLE DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT OUTBD L/E STUB WING SUPPORT ANGLE CRACKED AT STA XOLDO 67.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D PG 21. FABRICATED NEW ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE ON LEFT OUTBD L/E STUB WING AT XOLDO 67.000 IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031014000032003101400003EU 2003 10 14 BAQA089546 120030919A249745043006 BUSS TIE UROCOPEC135 EC135T1 5620026EU ELECTRICAL OPEN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME1737 0144 BUS TIE OPEN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031014001112003101400111NM 2003 10 14 SWAA032132 120030923A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001182003101400118NM 2003 10 14 SWAA032174 120030928A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 2610 27936 DURING SCHEDULED C4 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED AT OUTBD CORNER. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20031014001422003101400142NM 2003 10 14 SWAA032065 120030916A575465C26602312A SKIN BOEING737 7373H4 1384600NM NR 5 LE SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C1 CHECK, FOUND NR 5 L/E SLAT DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2L72 4F RTA16WE 20031014001512003101400151NM 2003 10 14 SWAA032076 120030917A2130BACC10JJ400E CLAMP BOEING737 7375H4 138449DNM AIR DUCT BROKEN A SWAAK NONE J WARNING INDICATION CRCRUISE 1 SW29501SW 24178 DECLARED EMERGENCY, CABIN ALTITUDE WARNING HORN SOUNDED AT CRUISE. FOUND, KEELBEAM DUCT CLAMP BROKEN. REMOVED AND REPLACED DUCT CLAMP AND SEAL PER MM. 2L72 4F RTA16WE 20031014001802003101400180NM 2003 10 14 SWAA032098 120030921A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 EELPS FWD END CAP CRACKED AND LOOSE. REMOVED AND REPLACED EEPLS END CAP PER MM. 2L72 4F RTA16WE 20031014001912003101400191NM 2003 10 14 SWAA032106 120030920A53106558280 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STRINGER 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031014002062003101400206EU 2003 10 14 BAQA089816 120031002A249745023502 MASTER SWITCH UROCOPEC135 EC135P1 8680990EU WILL NOT TEST B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03137MH583 0179 MASTER SWITCH WOULD NOT SELF TEST OR WOULD TEST ON ITS OWN. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20031014002092003101400209 2003 10 14 BAQA089524 420031004A3420H140CWM INDICATOR AEROSPSA365 SA365N 8680669EU COCKPIT ADI DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 312 6425 ADI CAGE KNOB SPRING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20031014002142003101400214CE 2003 10 14 BAQA089805 120031005A27501005240731 MOTOR BEECH 100 100BEECH 1152916CE TE FLAP INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 3 B144 UNIT ONLY LASTED 2.6 HOURS. MOTOR IS INTERMITTENT. WILL RUN IF AND WHEN IT WANTS TO. WE DO NOT NEED ANOTHER UNIT. 1L72 3T A14CE 20031015000072003101500007NM 2003 10 15 USAASB03164 120030912A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US 23988 MAINTENANCE REPORTED A SECTION OF THE INTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1137 BATTERY CHARGER ASSEMBLY DUE TO A BLOWN FUSE. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031015000102003101500010NM 2003 10 15 USAASA03168 120030916A3350606171 SOCKET BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 MAINTENANCE REPORTED THE EMERGENCY EXIT ILGHT AT SEAT ROW 4, RIGHT SIDE, INOPERATIVE. MAINTENANCE REPLACED THE LIGHT SOCKET. (M) 2L72 4F RTA16WE 20031015000132003101500013NM 2003 10 15 USAASB03159 120030905A335020121 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19527AU 23862 FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE CHARGER ASSEMBLY. (M) 2L72 4F RTA16WE 20031015000182003101500018EA 2003 10 15 ASOA03437 120030913A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11875AS 7559 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000262003101500026EA 2003 10 15 ASOA03413 120030904A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031208001622003120800162NM 2003 12 8 AWXA200301324 120031014A5420313A1380125 ANGLE BOEING737 7373G7 1384595NM NR 1 NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON NR 1 PYLON OUTBOARD ACCESS COVER ATTACH ANGLE, NAC STA 279.50. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT NAC STA 279.50, DURING REMOVAL FOUND SPLICE PLATE ATTACHED TO ANGLE WORN BEYOND LIMITS, REMOVED SPLICE PLATE; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 313A1380, AND A NEW REPLACEMENT SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG 1. 2L72 4F RTA16WE 20031208001682003120800168NM 2003 12 8 AWXA200301330 120031008A53206935371 PAN BOEING737 7373G7 1384595NM FUSELAGE FLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR PAN AT BS 986 TO 1006, RBL 40-47. MAINTENANCE REMOVED FLOOR PAN AT BS 986 TO 1006, RBL 35-46; FABRICATED A NEW REPLACEMENT FLOOR PAN; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-20-01 PARA 2 & 3 AND SRM 51-40-05 PARA 1-4. 2L72 4F RTA16WE 20031208001712003120800171NE 2003 12 8 P5CA0300969 220031026A7200JT9D7J ENGINE BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE NR 4 STALLED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP23524UP 21446 702000 NR 4 ENGINE STALLED AT FL 310, GOING TO 340. INSPECTED INLET/EXHAUST GAS PATH IAW 72-00-00. NO DEFECTS NOTED. REPLACED ENGINE M7100-002. 2L74 4F4 FRTA20WE E20EA 20031209000022003120900002NM 2003 12 9 UPS03441467 120031013A531265B132243 PANEL BOEING747 747200 1384847NM BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, M/D- BS 1241 - 1265 CANTED BULKHEAD APU FUEL LINE CLOSURE PANEL CRACKED. CLOSURE PANEL REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F RTA20WE 20031209000192003120900019NM 2003 12 9 C1HA200381032 120031027A2612 FIRE LOOP BOEING727 7272S7 138407ZNM NR 3 ENGINE GROUNDED A C1HAO OTHER N FALSE WARNING CLCLIMB 1 GL15681CA 22020 ENGINE NR 3 FIRE WARNING GRD FAULT DETECTION LIGHT ILLUMINATED IN FLIGHT PERFORMED ENG FIRE TEST A OR B SYSTEM FAULT DETECTOR PER COM 2.26.24 TEST PROCDURE TESTED NORMAL. INSPECTED AND RESCHEDULED PER MEL 26-9 CTL C05478 ASSIGNED CAT 'C' ITEM PLACARDS INSTALLED (ITEM RESOLVE UNDER MDDR: C05478) T/S FOUND FIRE LOOP GROUNDING TO COWL TOWARDS AFT OUTBOARD SIDE REPOSITION NR 3 FIRE LOOP. OPS CHECKED PER CHAMPION M/M 26-11 CLEARS MEL 26-9 C/N C05478 MXC NOTIFIED REMOVED PLACARDS. 2L73 4F A3WE 20031209000232003120900023EA 2003 12 9 COMA0370043 120031024A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA2599 10064 FS 1098.20 BULKHEAD RT WEB BETWEEN STRINGERS 8R AND 9R ARE CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B AND REO 670-53-61-089. 2L72 4F RTA21EA 20031209000262003120900026 2003 12 9 COMA0360465 420031021A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01818CA 7408 FLIGHT 9397 STALL FAIL CAUTION MESSAGE. RESET STALL COMPUTER, NO DEFECTS NOTED. 2L72 4F RTA21EA 20031209000282003120900028NE 2003 12 9 COMA0360468 220031023A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO01956CA6811 536 7105 870646 FLIGHT 5308 LOUD BANG FOLLOWED BY LEFT ENGINE FAILURE. REPLACED LEFT ENGINE. 2L72 4F4 FRTA21EA E15NE 20031209000312003120900031EU 2003 12 9 MALA030480 120031024A2560 BATTERY SAAB SF340 340B 7860101EU FLASHLIGHT INOPERATIVE A MALAO OTHER L NO TEST NRNOT REPORTED 1 GL15406XJ 340B406 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED F/A EMERGENCY LIGHT BATTERY P/N P4-01-0021. 2L72 4T RTA52EU 20031209000332003120900033EU 2003 12 9 MALA030479 120031025A3020NH264668165 DUCT SAAB SF340 340B 7860101EU INTAKE HEAT DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15410XJ 340B410 DURING FLIGHT 3328, LT INTAKE HEAT INOPERATIVE. AIR RETURN TO MSP. MAINTENANCE REPLACED LT LOWER DUCT P/N NH24668-165, S/N OFF - L180866, S/N ON - L211754. OPS CHECK GOOD IAW JOB CARD 7160-301. REPLACED DEICE CONTROL MOD P/N 44730-501, S/N OFF - A00012, S/N ON - A00162. ALL CHECKS GOOD IAW CHP 30. REFER TO 409 NR 071419 FOR DETAILS. 2L72 4T RTA52EU 20031209000352003120900035SO 2003 12 9 SWIA200312542 120031016A2752 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM0758733 120197 CONTROL FAULT AT 16,000 & STAYED ON AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR AND RIGHT NACELLE FLAP ACTUATOR. OPS CHECK GOOD. 2L72 4T RTA31SO 20031209000602003120900060NM 2003 12 9 SWAA032360 120031026A3350300432 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED PM CHECK, FOUND LOWER AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20031209000762003120900076 2003 12 9 SWAA032342 420031025A25656556681 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 R2 DOOR EVACUATION SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031209000832003120900083NM 2003 12 9 SWAA032349 120031024A53116545805 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, WL 208, RBL 53. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20031209001032003120900103NE 2003 12 9 SWAA032323 220031019A7532 BLEED VALVE BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 2 ENGINE MALFUNCTIONED A SWAACD ABORTED TAKEOFF RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW29093SW 22965 687770 NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF POWER. REMOVED AND REPLACED NR 2 ENG P/D VALVE AND PRESS RATIO BLEED CONTROL VALVE, NO HELP. REMOVED AND REPLACED NR 2 ENG PER MM. 2L72 4F4 F A16WE E2EA 20031015000332003101500033EA 2003 10 15 ASOA03417 120030904A53206013600130 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING HANGAR MAINTENANCE IN BTR, THE SUPPORT DOUBLER AT FS 640 BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED IN THE RADIUS BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE REINFORCEMENT ANGLE AT FS 640 BETWEEN STRINGERS 9 AND 12. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000472003101500047EA 2003 10 15 ASOA03452 120030918A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING A ROUTINE CHECK IN SHV, THE RIGHT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR OVERWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000732003101500073WP 2003 10 15 GTIA030683 120030918A261172130000010 SMOKE DETECTOR DOUG DC9 DC983 3022083WP LAVATORY MALFUNCTIONED A GTIAO OTHER N FALSE WARNING LDLANDING 1 GL23814NK 49619 AFTER LANDING, RIGHT AFT LAV CALL BUTTON DINGING CONSTANTLY. REMOVED AND REPLACED RIGHT AFT LAVATORY SMOKE DETECTOR. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20031009000622003100900062EA 2003 10 9 COMA0360415 120030912A5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01809CA5805 7366 FLIGHT 5133 PILOTS WINDSHIELD SHATTERED DURING TAXI. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20031009000762003100900076EA 2003 10 9 SWIA200312398 120030911A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS 280 RT FLOORBEAM RBL 9.0 I/B ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20031009001012003100900101WP 2003 10 9 MWEA030377 120030917A801239279611 START VALVE DOUG DC9 DC932 3022066WP RT ENGINE INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31301ME 47190 RIGHT ENGINE HIGH-PRESSURE COMPRESSOR SHAFT SPEED WOULD NOT RISE ABOVE 13 PERCENT, HIGH-PRESSURE COMPRESSOR SHAFT SPEED ABORTED START. REMOVED AND REPLACED RIGHT ENGINE START VALVE. 2L72 4F A6WE 20031009001192003100900119EA 2003 10 9 COMA0370030 120030916A3240 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA BRAKE TEMP DIRTY A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01376CA 10092 FLIGHT OVERHEAT WARNING. COULD NOT DUPLICATE, CLEANED BRAKE TEMPERATURE MONITORING SYSTEM WIRING CONNECTOR. 2L72 4F RTA21EA 20031010000382003101000038NM 2003 10 10 USAABB03151 120030830A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU 22192 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 23 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031010000612003101000061NM 2003 10 10 CALA0300536 120030918A491038042814 APU BOEING737 7373T0 1384582NM A/C TAIL FIRE A CALAF ACTIVATE FIRE EXT. AJ FLAME/FIRE WARNING INDICATION CRCRUISE 1 SW271433428881 23572 APU FIRE LT ILLUMINATED WHILE AT CRUISE FLT ENROUTE. FIRE BOTTLE WAS DISCHARGED, LT EXT. FLT CONTINUED W/O FURTHER PROBLEM. MAINT INSP APU AND FOUND EVIDENCE OF SMALL FIRE AT BOTTOM REAR OF APU (EXH AREA). FIRE APPEARED TO BE CONTAINED. WIRES FROM APU EGT PROBE, FIRE DETECTION LOOP WERE DAMAGED. REAR SEAL ON EXH BAFFLE WAS DAMAGED. APU SHROUD AND MOUNTS WERE INSP WITH NO FAULTS NOTED, NO EXT DAMAGE NOTED. APU TAIL PIPE OVERHEAT DET WAS REMOVED AND REPLACED IAW MM 26-15-14. WIRE HARNESS TO CONNECTOR D1876 AND D1878 WAS REPAIRED, MUFFLER DET WAS REPLACED. APU FIRE EXT BOTTLE WAS R AND R IAW MM 26-22-11, PAGE 401-406. APU WAS R AND R IAW MM 49-11-00. APU LEAK AND OPS CHECKS WERE GOOD. 2L72 4F RTA16WE 20031014000252003101400025CE 2003 10 14 AMWA55 120030919A553110164000059 RIB BEECH BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE075YV 25820 UE5 FOUND TWO CRACKS ON RIB P/N 101-640000-59 AT THE RIVETS BESIDE THE STRINGERS INTERSECTIONS. THE STRINGER THAT INTERSECT THE RIB ARE P/N 101-640000-39 AND 101-640000-46. BOTH CRACKS WERE REAIRED IAW THE MFG STRUCTURAL REPAIR MANUAL. 2L72 4T RTA24CE 20031014000322003101400032CE 2003 10 14 54388AMWA 120030914A2916 RESERVOIR BEECH 1900 1900D 1154162CE HYD SYSTEM MALFUNCTIONED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143YV UE143 LANDING GEAR FAILED TO EXT & MANUAL EXTENDED (MSS). REMOVED AND REPLACED HYD RESERVOIR & POWER PACK ASSY TEST NORM. 2L72 4T RTA24CE 20031014000412003101400041EU 2003 10 14 AWXA200301065 120030909A3221D5311398820000 FITTING AIRBUS320 A320232 3930326EU MLG DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK FOUND UPPER OUTBOARD MOUNTING HOLE ELONGATED FROM WEAR ON STRUT ATTACH FITTING AT UPPER AFT CORNER OF NOSE WHEEL WELL AT FR 20, Z120. MAINTENANCE REMOVED DAMAGED STRUT ATTACH FITTING AT UPPER AFT CORNER OF NOSE WHEEL WELL AT FR 20, Z120; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 29-30, PARA B (1-2), SRM 51-76-11 PG 6-7, PARA B (1-2), AND SRM 51-76-11 PG 9-10, PARA E. 2L72 4F RTA28NM 20031014000512003101400051NM 2003 10 14 SWAA032183 120030929A531069353656 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031014000552003101400055NM 2003 10 14 SWAA032179 120030929A53116541529 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, BETWEEN STR 13R AND STR 14R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031014000582003101400058NM 2003 10 14 SWAA032176 120030930A27816544651 ACTUATOR BOEING737 7377H4 1384404NM NR 3 LE SLAT FAULTY A SWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29776WN 30591 AIR TURN BACK, NR 3 L/E SLAT WOULD NOT RETRACT. REMOVED AND REPLACED ALL L/E SLAT ACTUATORS PER MM. 2L72 4F RTA16WE 20031014001922003101400192NM 2003 10 14 SWAA032105 120030918A56105717623074 WINDOW BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAO OTHER O OTHER CRCRUISE 1 SW29606SW 27926 R2 COCKPIT WINDOW CRACKED AND ARCING. REMOVED AND REPLACED R2 COCKPIT WINDOW ASSY PER MM. 2L72 4F RTA16WE 20031015000512003101500051NE 2003 10 15 ASOA03440 220030915A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT FAILED A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO11826AS 7210 DURING CLIMB-OUT FROM CHS-DFW, AT APPROXIMATELY 21,000 FT THE CREW RECEIVED A LOW OIL PRESSURR WARNING ON THE LT ENGINE. BEFORE THE CREW COULD BEGIN INITIATING QRH PROCEDURES, OIL PRESSURE ON THE LT ENGINE DROPPED RAPIDLY AND SUBSEQUENTLY SHUT ITSELF DOWN, FOLLOWED BY A STRONG YAW TO THE LT. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT DIVERTING TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20031015000622003101500062NM 2003 10 15 USAASB03154 120030827A335020131A BATTERY BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US 22959 FOUND FIRST CLASS CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2L72 4F RTA16WE 20031015000642003101500064NM 2003 10 15 USAASB03149 120030824A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU 23551 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 10ABC AND THE LEFT EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031015000672003101500067NM 2003 10 15 USAASB03141 120030821A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU 23595 MAINTENANCE REPORTED THE MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT OVERHEAD PANEL ABOVE SEAT ROW 11, RIGHT SIDE. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031020000822003102000082NM 2003 10 20 VNAA0309017 120030930A2450230GC02Y02 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07429JS1045 3043 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031020000832003102000083NM 2003 10 20 VNAA0309016 120030925A3350501122803 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DISCHARGED A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07462PS16932942 3084 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY HAD NO POWER. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031020000892003102000089NE 2003 10 20 CALA0300571 220031002A72603353000100 GEARBOX BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE FAILED A CALAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 SW276933340022 23571 723132 THE NR 2 ENGINE SUDDENLY AUTO SHUTDOWN WHILE CLIMBING THROUGH 19K AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TRANSFER GEARBOX AT FAULT. THE NR 2 ENGINE TRANSFER GEARBOX WAS REMOVED AND REPLACED IAW MM 72-62-01. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA16WE E2GL 20031020001042003102000104WP 2003 10 20 ABXA030375 120030916A5320D0489835 WEB DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 CUSP WEB STA 908 - 965, LEFT BUTT LINE 44 - 54, LIGHT HOLES CORRODED LOWER SURFACE. REPLACED CUSP WEB IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 20031020001152003102000115EA 2003 10 20 COMA0360447 120031002A322216144101 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG DISCONNECTED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01959CA 7116 FLIGHT 5319 GEAR DISAGREE WARNING WITH STEERING INOP AND WOW INPUT MESSAGE. FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS AND TAXI OPS CHECK, NO DEFECTS NOTED. 2L72 4F RTA21EA 20031020001532003102000153NM 2003 10 20 DL764030804 120030902A3230272T4507112 SEQUENCE VALVE BOEING767 767432ER 1385134NM LT MLG WW CRACKED A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO27827MH 29698 HYD C-SYS FLUID LEAK TO .25 INFLT. SYS-C HYD QTY READS .41 ON GROUND. FOUND MAIN LANDING GEAR OPERATED SEQUENCE VALVE GEAR UP TUBE LEAKING HYD FLUID. PERFORMED TEMP REPAIR PER ERA727766-14 AMM20-10-09-201. REINSPECT FOR SECURITY AND LEAK CHECK WITHIN 175 FLT HRS. PERMANENT REPAIR WITHIN 350 FLT HOURS. SERVICED CENTER HYD SYS RES AND PERFORMED SEQUENCE VALVE OPERATION. NO LEAKS. TUBE ASSY 272T4507-112 IPC 32-32-55-02 ITEM 371. 2L72 4F RTA1NM 20031010000682003101000068NM 2003 10 10 F3LA200300137 120030909A3350RPSIB BATTERY PACK AIRBUSA319 A319111 3930336NM EMERGENCY LIGHT INOPERATIVE A F3LAO OTHER O OTHER NRNOT REPORTED 1 NM03902FR 1515 FLIGHT CREW REPORTED EMERGENCY FLOOR PATH LIGHTING AT SEAT ROWS 1, 2, 5 AND 6 INOPERATIVE. REPLACED BATTERY POWER SUPPLY. 2L72 4F RTA28NM 20031010000872003101000087 2003 10 10 BAQA089390 420030923A23004000155250101 RADIO BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE COCKPIT FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME8 7243 WILL NOT TRANSMIT. PART LASTED ONLY 7.7 HOURS. REPLACED WITH SERVICEABLE, CANNED, ASSET S/N: 2253 1G72 3U3 U H13EU E5NE 20031020001642003102000164NM 2003 10 20 DLM88030790 120030828A32225920603505 PISTON DOUG MD88 MD88 3023688NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27997DL 30085 53364 NLG PISTON HAS HAD DIA 9 MACHINED TO 2.8045 INCH. DAMAGE REWORKED PER 339514-14. 2L72 4F RTA6WE 20031020001752003102000175NM 2003 10 20 DL76K030810 120030903A2121732591F FAN BOEING767 767332 1382001NM CARGO BAY INOPERATIVE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27174DZ 29693 ON CLIMBOUT FUMES IN COCKPIT, GOT STATUS MSG FWD EQUIPMENT EXH FAN. RETURNED TO FLL. 09:35 INSPECTED FAN AREA AND RECEIVED DISPATCH APPROVAL FOR MEL 21-58-04B. 09:50 COMPLETED CONFERENCE CALL WITH MA AND SHIFT SUPERVISOR 10:15 MTC COMPLETE, REPLACED FAN. OPS NORMAL. REMOVED MCO/PLAC. 2L72 4F RTA1NM 20031020001782003102000178NM 2003 10 20 DL757030812 120030904A2910296201703 HYDRAULIC LINE BOEING757 757232 1384965NM HYD SYSTEM LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27614DL 22821 LT HYD QTY WENT TO 00-HAD PRESURE ON LT SIDE GOOD AT 3100. RETURNED TO CVG AFTER COORDINATING WITH MTC. EICAS MSGS LT HYD SYS PRESS, RUDDER RATIO, LT HYD QTY. REPLACED FLEX LINE AT LEFT SIDE ELECTRIC PUMP. 2L72 4F RTA2NM 20031020002162003102000216WP 2003 10 20 UPS03841364 120030925A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 LEFT WING L/E RIB IS CRACKED AT XFS 735. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20031020002392003102000239WP 2003 10 20 UPS03841344 120030923A5320 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 MAIN CABIN SUBFLOOR FINGER DOUBLER IS CRACKED AT STA 930 AT BL 0. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5646674 AND SRM 53-7-3 FIG 4, 51-1-20D. 2L74 4F RT4A25 20031020002562003102000256EA 2003 10 20 03282671 120031009A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27671BR 7572 DURING INSPECTION THE LT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002652003102000265EA 2003 10 20 03264701 120030921A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27701BR 7448 DURING INSPECTION THE AISLE CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002762003102000276EA 2003 10 20 03267689 120030924A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27689BR 7737 DURING INSPECTION THE LT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002932003102000293NM 2003 10 20 2003UALA00722 120030925A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29351UA 24319 FLOOR EMERGENCY EXIT LIGHTS INOP FROM ROW 15 TO AFT END OF CABIN. REPLACED POWER STRIP. 2L72 4F4 FRTA16WE E2GL 20031020002982003102000298NE 2003 10 20 2003UALA00726 220030928A7261 LINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 ENG OIL CRACKED A UALAK NONE K FLUID LOSS CRCRUISE 1 WP29595UA 28748 NR 2 ENGINE OIL QUANTITY DROPPED STEADILY IN FLIGHT. REPLACED CRACKED & LEAKING FUEL/OIL HEAT EXCHANGER RETURN LINE. LINE CRACKED DUE TO LIBERATED TUBE CLAMP. 2L72 4F4 FRTA2NM E17NE 20031020003082003102000308EU 2003 10 20 2003UALA00699 120030920A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29463UA 1282 EEL LIGHTS ARE OUT AT 6ABC AND 17ABC. REPLACED BAD EEL LIGHTS. 2L72 4F4 FRTA28NM E40NE 20031020003152003102000315EA 2003 10 20 SWIA200312451 120030921A3231 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA NLG DOOR DISCONNECTED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07460SW 7803 RETRACTED GEAR AFTER TAKEOFF AND NOSE GEAR DOOR AURAL WARNING SOUNDED. RETURNED TO DFW. FOUND CANNON PLUG FOR NOSE DOOR SELECTOR VALVE DISCONNECTED. RECONNECTED CANNON PLUG. OPS CHECK GOOD IAW MM 33-22-20. 2L72 4F RTA21EA 20031021000282003102100028WP 2003 10 21 GTIA030690 120030907A5320 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND CRACKED ANGLE AT FS 826 40 INCHES RBL ON TOP CTR FUEL TANK. STOP DRILLED CRACK. FORMED NEW ANGLE REPAIR. INSTALLED ANGLES. (M) 2L72 4F A6WE 20031021000612003102100061 2003 10 21 USAASA03111 420030909A2565 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19745UW 1289 PHL - THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY ESCAPE SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031021000662003102100066EA 2003 10 21 A6WA200340139 120030924A3310LH10B POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31430AW 7719 APU LOAD CONTROL VALVE LIGHT, ISOLATION VALVE LIGHT, APU AVAILABLE LIGHT ALL INTERMITTENT, ELECTRICAL SMELL. REMOVED AND REPLACED BRIGHT/DIM POWER SUPPLY. (M) 2L72 4F RTA21EA 20031021001502003102100150NM 2003 10 21 AALA20030946 120030903A33500201991008 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21195AN 32389 DFW - EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 10D. REPLACED SEAT MOUNT EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030915000412003091500041EU 2003 9 15 I05R089181 120030722A2621L262M1805101 BRACKET UROCOPEC135 EC135P1 8680990EU FIRE BOTTLE CRACKED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05552BA 190 FIRE BOTTLE BRACKET CRACKED BEYOND LIMITS REPLACED PART 1G72 3U O H88EU 20031209001062003120900106NM 2003 12 9 SWAA032335 120031023A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED C2 CHECK, RT ELEV TAB FAILED FREEPALY CHECK INSPECTION. REMOVED AND REPLACED TAB HINGE ATTACH BUSHINGS PER SI 11139-55. 2L72 4F RTA16WE 20031209001102003120900110NM 2003 12 9 SWAA032339 120031023A3350BR2013 RECEPTACLE BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 DURING SCHEDULED RON, FOUND EEPLS INOP BETWEEN ROWS 6 AND 10. REMOVED AND REPLACED LIGHT RECEPTACLE PER MM. 2L72 4F RTA16WE 20031209001272003120900127EA 2003 12 9 QXEA200301320 120031010A5730 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 LT INBOARD WING LEADING EDGE IS CHAFED JUST ABOVE PANEL 522DB. REPAIRED IAW HORIZON AIR EA R-57-48A, EO 601R-57-4253A AND CRJ-700 AMM TASK 27-50-00-710-801. 2L72 4F RTA21EA 20031209001352003120900135NM 2003 12 9 QXEA200301349 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - RIGHT INBOARD TRACK NR 8 SEAT ATTACH AREA CORROSION UNDER LUG OUTBOARD APPROXIMATELY X500.00. REPAIRED IAW RD 8-53-1339. 2H72 4T RTA13NM 20031204001132003120400113WP 2003 12 4 UPS03841431 120030926A574097531973 ATTACH FITTING DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, LT WING CENTER L/E, O/B ATTACH POINT THAT ATTACHES L/E TO STUB WING IS CRACKED. REMOVED CRACKED ANGLE IAW DC8 SRM 51-3-0, MAT ID IAW DC8 DWG 9753297-7, .080 7075-0 PO 422932. RECEIVED PART FROM HEAT TREAT .080 7075-0-TO .080 7075-T6, FABRICATED ANGLE IAW DC8 DWG 9753197, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ANGLE IAW DC8 SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20031204001222003120400122EU 2003 12 4 AWXA200301263 120031008A5210FE1740011 DAMPER AIRBUS320 A320231 3930325EU R-2 DOOR OUT OF TOLERANCEA AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW16411 053 DURING C-03 CHECK FUNCTIONAL CHECK OF EMERGENCY EVACUATION SYS, IDENTIFIED A WEAK DOOR DAMPER CYLINDER AT R-2 DOOR. MAINT R&R R-2 DOOR DAMPER CYLINDER IAW AMM. ADJUSTED PERCUSSION BELL CRANK FINGER IAW AMM, OPERATIONAL CHECK C/W IAW AMM SUBTASK 52-10-00-614-050. VENDOR TEARDOWN OF DAMPER CYLINDER ASSEMBLY S/N 455 CONFIRMED FAILURE OF UNIT. THE FRONT AND REAR CUPS WERE FOUND LEAKING DUE TO WORN SEALS, THE PERCUSSION ASSY FOUND CONTAMINATED, & ALSO FOUND RUSTED SPRING WASHERS IN REGULATOR VALVE ASS. REPLACED 15 EACH VARIOUS SEALS, 12 EACH SPRING WASHERS, UNIT WAS REPAIRED PER CMM. 2L72 4F RTA28NM 20031204001682003120400168CE 2003 12 4 AMWA62 120031015A553111464000069 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGES AT CANTED STAB 24.973 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031204001752003120400175EA 2003 12 4 QXEA200301297 120031017A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX- CHIMNEY AT FORWARD BAGGAGE DOOR ENTRANCE AREA IS DAMAGED. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20031205000152003120500015EA 2003 12 5 MASA200300421 120031022A493038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY INOPERATIVE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0775991126381562 7422 PILOT REPORTED AN APU AUTO SHUTDOWN FOLLOWED BY A FUEL ODOR IN THE CABIN. MX APPLIED MEL 49-10-01 AND CLEARED THE FUMES FROM THE CABIN. 2L72 4F RTA21EA 20031205000502003120500050NM 2003 12 5 DL757030941 120031020A5330146N37506 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27659DL 24421 THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 1701 BETWEEN STRINGERS 15R & 16R. THE DENT WAS REMOVED WITH A 3 X 6.2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385710-14, REV A. 2L72 4F RTA2NM 20031208000262003120800026NM 2003 12 8 03FDEA01790 120031022A3411 PITOT TUBE BOEING727 727200 138407ENM PITOT STATIC OBSTRUCTED A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25206FE3225 3225 22928 F/O AIRSPEED INDCATOR INOP ON T/O UPON ARRIVAL CHECKED FOR OBTRUCTIONS IN BOTH CAPTS & F/O'S PITOT TUBES NO BLOCKAGE NOTED. R&R F/O'S AIRSPEED INDICATOR.OPS CHECKS GOOD PER B727-200_M.M. CHAPT.34-12-000-5. 2L73 4F RTA3WE 20031208000772003120800077 2003 12 8 SWAA032225 420031007A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031208000872003120800087NM 2003 12 8 UPS03441465 120031014A5310 ANGLE BOEING747 747200 1384847NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, BS 380 LEFT STR 1 VERTICAL SUPPORT ANGLE FOUND CRACKED AS MARKED. COCKPIT BS 380 LEFT STR 1 VERTICAL SUPPORT ANGLE REPLACED AS PER SRM 51-10-01. 2L74 4F RTA20WE 20031208000982003120800098NM 2003 12 8 QXEA200301330 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - RIGHT INBOARD TRACK NR 8 CHAFED IN BOTTOM FROM X446.00 TO X455.00 AND FROM X506.00 TO X515.00. REPAIRED IAW RD8-53-1339. 2H72 4T RTA13NM 20031208001202003120800120NM 2003 12 8 AWXA200301318 120031007A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT NUT PLATE HOLES BS 727D, RBL 8. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF FLOORBEAM BS 727D, RBL 8; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 PG 1 FIG 201. 2L72 4F RTA16WE 20030915000522003091500052SW 2003 9 15 HEEA088960 120030903A2140S9242EC2 HEATER BELL 407 407 1182206SW CABIN CRACKED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 HEATER SHROUD CRACKED AND PIECES MISSING. 1G71 3U O H2SW 20030915000662003091500066SW 2003 9 15 HEEA088962 120030729A243523046020 STARTER GEN BELL 212 212 1181420SW ENGINE INOPERATIVE B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03102PH24458 30899 GENERATOR WILL NOT COME ON. 1G71 4U H4SW 20030915000852003091500085NE 2003 9 15 HEED089063 120030905A53027620105502101 SPAR SKRSKYS76 S76C 8143008NE TAIL PYLON CRACKED B HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03478X 5403 760493 CRACKED IN TAIL PYLON AFT SPAR WEB. RUN FROM LT SPAR TO RT SPAR. 1G72 3U NCH1NE 20030915000932003091500093SW 2003 9 15 ALGA089086 120030910A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03647AL 53357 DISC PACK FOUND TO HAVE A CRACKED DISC. REMOVED AND REPLACED. 1G71 3U O H2SW 20030916000022003091600002WP 2003 9 16 MEX2003392 120030825A3260 PROXIMITY SENSOR DOUG DC9 DC987 3022087WP MLG WILL NOT TEST W ASMFO OTHER L NO TEST NRNOT REPORTED 1 SW23803ML 49726 AIRCRAFT RETURNED TO PLATFORM DURING TAXING, NOSE LANDING GEAR RED LIGHT CAME ON. THE BITE WAS PERFORMED TO PROXIMITY SWITCH, SENSOR AND CONNECTOR WERE CLEANED AND CHECKED IAW MM, ALL CORRECT. 2L72 4F RTA6WE 20030916000962003091600096NM 2003 9 16 C7WA200300046 120030714A29102S5304 CHECK VALVE BOEING737 737231 1384079NM 'A' HYD SYSTEM LEAKING A C7WAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO1754354 21986 AIR TURNBACK, DURING CLIMB-OUT COCKPIT HAD A HEAVY CHEMICAL ODOR SHORTLY AFTER CABIN BEGAN TO FILL WITH A SMOKEY MIST, SMOKE BEGAN TO CLEAR WHEN ENGINE POWER WAS REDUCED TO IDLE. PROBLEM GOT WORSE AS POWER WAS APPLIED DURING FINAL APPROACH. REPLACED THREE EACH 'A' HYDRAULIC RESERVOIR PRESSURIZATION CHECK VALVES. LEAK AND OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040105001352004010500135NM 2004 1 5 SWAA032753 120031216A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 24R. REPAIRED SKIN PER SRM AND SWA EA. 2L72 4F A16WE 20040105001432004010500143WP 2004 1 5 ABXA030481 120031210A532059101300391 TEE FITTING DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 AFT PRESSURE BULKHEAD TEE NR 6 FORWARD SIDE HAD A 1.125 INCH CRACK AT APPROXIMATELY LONGERON 14 LEFT. REPLACED AFT PRESSURE BULKHEAD TEE NR 6 IAW JOB CARD EA 53120037 AND DC-9 MM. 2L72 4F A6WE 20040106000882004010600088SO 2004 1 6 C2XA03TY211 120031218A5313145338880002 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714543 145553 TYS DURING A SCHEDULED 1C INSPECTION DAMAGE WAS FOUND ON STR 19L AND 19R AT FR 53. MAINT BLENDED OUT DAMAGE, PERFORMED A NDI TEST, NO CRACK FOUND. FABBED A EXTERNAL DOUBLER AND SHIMS; ALODINED, PRIMED THE EXTERNAL DOUBLER. INSTALL THE FAB PARTS IAW EMB 135/145 SRM 53-21-02; CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040106001682004010600168NM 2004 1 6 QXEA200301571 120031217A33506138001 BATTERY BOMBDRDHC8 DHC8401 1390041NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09405QX5589 1731 4047 PDX- EMERGENCY LIGHTS AT MAIN CABIN DOOR AND FORWARD CEILING OVERHEAD AND FRONT LEFT HAND EGRESS LIGHT ILLUMINATED MOMENTARILY WHEN SWITCH TURNED ON AND THEN GO OUT. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY BATTERIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040108000522004010800052CE 2004 1 8 FPI2003F00014 120031107A7921654585 OIL COOLER CESSNA210 T210L 2073449CE CONT O550 IO550* SO ENGINE OIL CRACKED E FPIAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO15732HN561 21061527 821036R BOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION. 1H71 3O3 O 3A21 E3SO 20040108000632004010800063CE 2004 1 8 GNB2003F00000 120031008A30406041H261 RELAY CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO WINDSHIED HEAT FAILED E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW012713X 99026H7780 402C0207 PILOT TURNED ON HEATED WINDSCREEN PANEL. AFTER 3-4 MINUTES LIGHT STILL ON, BUBBLE APPEARED. RELAY STUCK IN CLOSED POSITION NOT ALLOWING A STANDARD CYCLE TIME. 1L72 3O3 O A7CE E8CE 20040108000702004010800070SO 2004 1 8 RTA2003F00000 220031010A7414K3823 DISTRIBUTOR BLK SLICK CIRRUSSR SR20 05628AJGL CONT O360 IO360ES SO MAGNETO FAILED B RTARO OTHER O OTHER NRNOT REPORTED 1 SW03111RT645 01040152 1156 OWNER REPORTED ENGINE APPEARED DOWN ON POWER. MAG CHECK AND COMPRESSION GOOD. CHECKED MAG TIMING AND FOUND LEFT MAG ADVANCED 32 DEGREES, FACTORY TIMING IS 22. WITNESS PUTTY STILL ON MAG BASE FROM FACTORY. REMOVED MAG FOR INTERNAL INSPECTION. FOUND POINTS AND FOLLOWER WORN OUT, DISTRIBUTOR AND GEAR ASSY BURNT UP FROM ARCING. THIS MAG SHOULD NOT HAVE BEEN WORKING, IT WAS BURNED UP. OWNER STATED THE OTHER MAG WAS REPLACED RECENTLY FOR THE SAME PROBLEM. 1L71 3O3 ONTA00009CHE1CE 20040108000772004010800077NM 2004 1 8 UIEA200300059 120031004A2820MA11A1194 ACTUATOR BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL TRANSFER VALVE FAILED A UIEAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA15498MC 29259 DIVERSION TO ANC, ENROUTE CREW REPORTED EICAS MESSAGE FUEL IMBALANCE 1-4. CHECKLIST COMPLETED. NR 4 CONTINUED TO DECREASE, NR 3 REMAINED CONSTANT QUANTITY. SYSTEM CONTROL ADVISED AND AIRCRAFT DIVERTED TO ANC DUE TO FUEL LEAK FROM NR 4 MAIN TANK. MAINTENANCE ADVISED FLIGHT CREW TO SHUT DOWN NR 4 ENGINE. UPON ARRIVAL THE CAPTAIN ADVISED THAT HE WAS UNABLE TO MONITOR FUEL USE AND HAD TO SHUT DOWN NR 4 ENGINE. NO FUEL DUMPED. FOUND NR 4 TRANSFER VALVE PARTIALLY OPEN. REMOVED AND REPLACED TRANSFER VALVE ACTUATOR IAW MM. CMC GROUND OPS CHECKED OK. VISUALLY VERIFIED VALVE OPERATION OK. 2L74 4F4 FRT1384945 E23EA 20040106001352004010600135NM 2004 1 6 03FDEA02216 120031218A5753 RIB DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, OUTBOARD FLAP NOSE RIB SUPPORT ISLAND BARREL NUT BORE CRACKED. OUTBOARD FLAP NOSE RIB SUPPORT REMOVED AND REPLACED NEW RIB SUPPORT AS PER 51-33-01 VOL. II AND COMPLIED WITH FEDEX EA 1-5750- 75228, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP SECONDARY UP STOP REPAIR. 2L73 4F RTA22WE 20031208001222003120800122NM 2003 12 8 AWXA200301320 120031003A531265175837 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON EDGE OF LIGHTENING HOLE ON BS 178 BULKHEAD VERTICAL WEB AT RBL 17.1, WL 193. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD VERTICAL WEB AT RBL 17.1, WL 193; FABRICATED A NEW REPLACEMENT VERTICAL WEB PER DWG 65-17583; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12 PG 1. 2L72 4F RTA16WE 20031208001582003120800158WP 2003 12 8 IXXA0300067O 120031027A2720 GEAR DOUG DC8 DC871F 302199DWP RUDDER DIRTY A IXXAO OTHER O OTHER LDLANDING 1 SW11822BX87364356 45813 DURING LANDING TO RJTY RUDDER TRIM BOUND. CREW COULD NOT CENTER RUDDER TRIM, IT BOUND AT 3 UNITS LEFT. AFTER LANDING ROTATED RUDDER TRIM TO FULL LEFT DEFLECTION. CREW NOTED METALLIC NOISE FROM PEDESTAL AREA AND RUDDER TRIM CENTERED OKAY. MAINTENANCE FOUND DEBRIS IN RUDDER TRIM GEAR TEETH. THE DEBRIS WAS REMOVED AND AN OPERATIONAL CHECK FOR THE RUDDER TRIM SYSTEM WAS GOOD ON GROUND PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20031208001702003120800170NE 2003 12 8 PCAA0310128 220031026A73207898423008 EEC DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1ENGINE FAULTY A PCAAEC ENGINE SHUTDOWN ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA13848EX2213 331 121222 AIRCRAFT HAD NR 1 ENGINE SHUTDOWN AS A PRECAUTIONARY MEASURE DUE TO NR 1 ENGINE TORQUE FLUXING BETWEEN 50 AND 90 PERCENT. CABIN WAS ADVISED OF EMERGENCY, BUT DID NOT ASSUME THE BRACE POSITION. MAINTENANCE GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE. MAINTENANCE REMOVED AND REPLACED NR 1 ELECTRONIC ENGINE CONTROL UNIT. GROUND RAN AIRCRAFT, ALL CHECKS GODD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031208001782003120800178WP 2003 12 8 ABXA030403 120031009A533059114063 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 FUSELAGE SKIN CRACKED AT MAIN ENTRY DOOR UPPER/AFT STOP. REPAIRED AREA IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 20031209000082003120900008WP 2003 12 9 UPS03841473 120031022A5512 DOUBLER DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 REPAIR DOUBLER IS CRACKED AT LT HORIZONTAL STAB L/E AT XFS 60. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 55-2-0 FIG 22. 2L74 4F RT4A25 20031209000842003120900084 2003 12 9 SWAA032350 420031023A256565C19901 CABLE BOEING737 7373H4 1384600NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20031209001232003120900123NM 2003 12 9 AWXA200301337 120031028A533065458001255 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK 4 EACH CRACKS WERE FOUND AT FASTENER HOLES ON FUSELAGE SKIN FORWARD OF L-1 DOOR LOWER HINGE BS 304-305, WL 223 TO WL 207. MAINTENANCE CUT OUT DAMAGE ON SKIN, DOUBLER AND STRAP AT L-1 DOOR LOWER HINGE BS 304-305, WL 223 TO WL 207; PERFORMED HFEC INSPECTION OF CUTOUT; FABRICATED 3 EACH FILLERS & 2 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-03300-SS1. 2L72 4F RTA16WE 20031209001342003120900134NM 2003 12 9 QXEA200301339 120031013A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 RIGHT HAND OUTBOARD TRACK NR 11 REQUIRES REPLACEMENT. REPLACED NR 11 SEAT TRACK IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20031209001492003120900149NM 2003 12 9 QXEA200301364 120031026A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 REPLACE RIGHT HAND OUTBOARD SEAT TRACK NR 10 DUE TO NUMEROUS DISCREPANCIES. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-40-00. 2H72 4T RTA13NM 20031209001582003120900158SO 2003 12 9 C2XA03SH423 120031031A3350110049 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714542 145547 SHV- DURING C-CHECK THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND NOT TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW EMB AMM 145 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031209001682003120900168EU 2003 12 9 CX7A194J0351 120030702A5200 DOOR SAAB SF340 340B 7860101EU RT NACELLE UNSECURE A CX7AEC ENGINE SHUTDOWN ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL03311CE 340B214 RIGHT O/B ENGINE COWL WAS NOT PROPERLY SECURED. 2L72 4T RTA52EU 20031209001772003120900177WP 2003 12 9 ABXA030406 120031013A575499193018 RIB DOUG DC9 DC941 302207NWP RT WING L/E CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 RIGHT WING LEADING EDGE NOSE RIB INBOARD SIDE OF NR 1 SLAT DRIVER HAD 2 CRACKS ON REPAIR MARKED, REA 43261, CRACKED IN FORWARD RADIUS AND AFT BETWEEN HI-LOKS. REPLACED LEADING EDGE RIB IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20031209001882003120900188WP 2003 12 9 UPS03841489 120031021A52305754075502 FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, C-PIT DOOR UPPER AFT LATCH PIN FITTING IS CRACKED INSIDE DOOR AT APPROX STA 1215 LONG 22R. REMOVED AND REPLACED FITTING IAW DWG 5754075 AND SRM 51-1-20D, 51- 1-21A, 51-3-0. 2L74 4F RT4A25 20031209001942003120900194WP 2003 12 9 UPS03841495 120031025A5313975491333N LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 350 LONGERON 36 INBOARD AND OUTBOARD SECTIONS ARE CRACKED. REMOVED AND REPLACED LONGERONS BETWEEN STATION 210 TO 370 IAW DWG 9754913 AND SRM 51-1-20D. 2L74 4F RT4A25 20031209002072003120900207SO 2003 12 9 SWIA200312557 120030930A5320 CLIP EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07565SW 120340 SKIN CLIP CRACKED AT FRAME 9, BELOW RIGHT DV WINDOW. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT FRAME 9 IAW SB 120-53-0073. 2L72 4T RTA31SO 20031125000542003112500054WP 2003 11 25 DHL2003807508 120031007A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT WING CENTER L/E FORMER CRACKED 0.500 AT STA 304.000. REMOVED FASTENER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON LEFT CENTER L/E FORMER AT STA 304.000 IAW SRM 57-2-0 PG 9, 10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000702003112500070WP 2003 11 25 DHL2003805602 120030728A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 MAIN CARGO COMPT NR 6 SEAT TRACK LUG WORN AT STA 207.000. CUT OUT NR 6 DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000732003112500073WP 2003 11 25 DHL2003805593 120030808A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD L/E UPPER SKIN SURFACE CORRODED STA XFS 568.000 - 633.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG 44. FABRICATED SKIN SPLICE IAW SRM 57-2-1 FIG 44. CLEANED, TREATED AND PRIMED INNER SIDE OF SKIN SPLICE IAW SRM 51-1-8B. INSTALLED SKIN SPLICE WITH NEW FASTENERS IAW SRM 57-2-1 FIG 44, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. REFER TO NR 0119 FOR RIGHT OUTER WING INBD L/E REMOVAL/INSTALLATION. 2L74 4F RT4A25 20031125000892003112500089WP 2003 11 25 DHL2003805581 120030823A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLOT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING INBD EXTENDED L/E OUTER PLATING CORRODED AROUND STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA IAW DHL-EDT66-3, DHL-DWGT66-R03. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER IAW DHL-EDT66-3, DWGT66-R03. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND REPAIR DOUBLER IAW DHL-EDT66-3, DWGT66-R03, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-15 PG 1. FOR LEFT OUTER WING INBD L/E REMOVAL/REINSTALLATION SEE N/R 0185. 2L74 4F RT4A25 20031125001172003112500117EA 2003 11 25 SIMA200321606 120030803A27615120011 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA LT SPOILER FAILED A SIMAB EMER. DESCENT FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SW21501BG 10017 TYS - FLT 3718 - DURING DESCENT INTO TYS CREW RECEIVED AN OUTBOARD SPOILERON AND OUTBOARD FLIGHT SPOILER CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY WITH NO OTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD SPOILER ACTUATOR IAW CRJ MM. OPS AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20031125001462003112500146NM 2003 11 25 ASAA0340118 120030308A552365C340662 FAIRING BOEING737 737490 1384715NM ELEVATOR TAB CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 PAE - DURING C-CHECK, FOUND RIGHT ELEVATOR TAB AFT MAST FAIRING CRACKED AT OUTBOARD CORNER. REMOVED AND REPLACED RIGHT ELEVATOR TAB AFT MAST FAIRING. (M) 2L72 4F RTA16WE 20031126000102003112600010 2003 11 26 RAIA00311288 420031119A3425HG2010AC02 AHRS EMB 145 EMB145LR 3260212SO NR 2 FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK 145044 5657-EWR- AHRS NR 2 FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS. 2L72 4T RTT00011AT 20031126000212003112600021EA 2003 11 26 QXEA200301404 120031029A5320 FITTING CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 CKB- PERFORMED EDDY CURRENT INSPECTION OF RIGHT HAND PYLON SHEAR DECK LUNCH BOX. NOTED INDICATION OF CRACK APPROXIMATELY 2 INCHES LONG AT AFT FITTING IN CARGO BAY. REPAIRED IAW CRJ SRM 51-42-06 AND SRM 51-42-21. 2L72 4F RTA21EA 20031126000402003112600040WP 2003 11 26 DHL2003805559 120030806A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD L/E FORMER CRACKED 2.000, STA XFS 672.500 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031126000412003112600041WP 2003 11 26 DHL2003805575 120030808A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 1.000 AT STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER WITH NEW FASTENERS ON LEFT WING CTR L/E FORMER IAW SMR 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031126000432003112600043EA 2003 11 26 COMA0370049 120031109A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01371CA2100 10082 FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031126000472003112600047NM 2003 11 26 375PA0021 120031106A335020131A BATTERY PACK BOEING737 73739A 138447PNM CABIN DISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 MID TO AFT EMERGENCY FLOOR LIGHTING INOP. REPLACED BATTERY PACK LEFT SIDE MID CABIN. OPS NORMAL PER MM 33-51-00. 2L72 4F RTA16WE 20031126000522003112600052WP 2003 11 26 03FDEA01977 120031124A2752AMB7252501 ATTACH FITTING DOUG DC10 DC1010 3022110WP T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 REMOVE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING STEP'S 1 THRU 8 LEFT SIDE. REMOVED AND INSTALLED FLAP ACTUATOR IAW MM 25-52-01-2 AND ACCOMPLISHED EO 8-5720- 7-2302 STEP NR 1 THRU NR 8 LEFT SIDE FLAP ACTUATOR CYLINDER ATTACH FITTING REPLACEMENT. 2L73 4F A22WE 20031126000582003112600058NM 2003 11 26 CALA0300663 120030716A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND AFT CABIN FLOORBEAM CORRODED AT STA 1006, LBL 15. A STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20031126001142003112600114NM 2003 11 26 ASAA0310449 120030515A575365495053 SKIN BOEING737 737290C 138448VNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND RIGHT WING FORE FLAP SKIN AT WING STATION 395.47 DENTED. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031126001162003112600116NM 2003 11 26 ASAA0310447 120030515A57536546435 SKIN BOEING737 737290C 138448VNM LT WING TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND LEFT WING AFT FLAP SKIN AT WING STATION 417 CREASED. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20040106001422004010600142EA 2004 1 6 COMA0360561 120031216A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01933CA 7040 FLIGHT 5073 FLAPS DID NOT MOVE WHEN SELECTED TO 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040106002292004010600229WP 2004 1 6 GTIA031035 120031031A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FLUSH REPAIR AT FS 1255 BETWEEN LONGERONS 25 AND 26R, PREVIOUS REPAIR HAS SUSTAINED ADDITIONAL DAMAGE AROUND REPAIR AREA AND REQUIRES A NEW EXTENDED REPAIR TO BE INSTALLED. REMOVED DAMAGE SKIN. CUT OUT IS 8 INCHES BY 12 INCHES. FABRICATED REPAIR PARTS. FABRICATED STRAPS. INSTALLED NEW SKIN FILLER, DOUBLERS, FINGER DOUBLERS STRAPS. (M) 2L72 4F RTA6WE 20040108000562004010800056NM 2004 1 8 IU62003F00039 120030827A2760654494710 HOUSING BOEING737 737* NM SPOILER ACTUATORCRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 7564520880 2280 ACTUATOR HOUSING HAS A PIN HOLE CRACK UNDER THE RETRACT PORT. METAL FATIGUE. USE IMPROVED HOUSING.(K) 2L72 4F RTA16WE 20040108000592004010800059EA 2004 1 8 WVE2003F00017 120030928A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09611QX 10041 FS 1098.20 BULKHEAD RT SIDE BETWEEN STINGERS 8R AND 9R, RBL 34 TO 41 AND WATER LINE 120 TO 125.42 IS CRACKED 1 INCH LONG IN WEB AREA. POSSIBLE STRESS RELIEF CRACK. REMOVE DAMAGE AND INSTALL BATHTUB FITTING IAW MFG REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20040108000992004010800099EU 2004 1 8 KBM2003F00049 120031006A6420350A33214501 PITCH LINK SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 TAIL ROTOR P/C LINK WORN BEYOND LIMITS. INSTALLED SERVICEABLE PC LINK. 1G71 3U3 UNCH9EU E19EU 20040108001422004010800142EU 2004 1 8 KBM2003F00076 120031021A6220126892P ROD END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 ROD END IS WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW ONES. (K) 1G71 3U3 U H9EU E19EU 20040108001472004010800147EU 2004 1 8 PG9A118870 120030925A2435150SG122Q STARTER GEN UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE ENGINE FAILED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19130PH 3670 (STARTER GENERATOR) UNIT FAILED, REMOVED AND REPLACED.(K) 1G72 3U3 U H9EU E00054EN 20040109000152004010900015CE 2004 1 9 PCZ2003F00000 120031010A5720 BRACE BEECH 18 TC45G 1151016CE PWA R985 R985* 52008NE LT WING CORRODED G PCZAO OTHER O OTHER NRNOT REPORTED 1 SW17445DM24009 AF152 DURING A 100 HOUR INSPECTION, THE UPRIGHT VERTICAL BRACE AT STATION 61 IN THE LEFT WHEEL WELL WAS FOUND CORRODED AND CRACKED. THE CORROSION WAS INTERNAL. THE BRACE (TUBULAR) WAS CRACKED COMPLETELY AROUND ITS CIRCUMFERENCE AT TWO PLACES APPROXIMATELY FOUR INCHES APART. THE SECTION OF THE BRACE WAS DISPLACED SLIGHTLY. THIS BRACE IS NOT SUBJECT TO THE X-RAY INSPECTION REQUIRED ON THIS AIRCRAFT WING.(K) 1L72 3R3 R A765 5E1 20040109000252004010900025NM 2004 1 9 MEX2003405 120030831A2781 WARNING LIGHT BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE FLAP-SLAT SYS ILLUMINATED W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23804AM 26271 AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF EICAS MESSAGE FLAP-SLAT ELEC. ONCE WE HAVE ADDITIONAL INFORMATION WE WILL SEND YOU AS SUPPLEMENT TO THIS REPORT.(K) 2L72 4F4 FRTA2NM E17NE 20040109000372004010900037NE 2004 1 9 CHI2003F00003 220030723A7200 ENGINE BOEING234 234 1385049EA LYC AL5512AL5512 41581NE MAKING METAL B CHIRO OTHER O OTHER NRNOT REPORTED 1 NM09246CH4850 127 MJ017 ENGINE CHIP LIGHT CAME ON IN FLIGHT, PILOTS REFERENCED EMERGENCY CHECKLIST AND IT INSTRUCTED THEM TO MONITOR ENGINE TEMP AND OIL PRESSURE AND TO LAND AS SOON AS PRACTICAL. INSPECTED CHIP DETECTOR AND FOUND A SINGLE METALLIC SLIVER, ALSO MAIN OIL FILTER BUTTON WAS POPPED. REF MM. REMOVED AND REPLACED OIL FILTER AND PERFORMED AN ENGINE GROUND RUN. REINSPECTED OIL FILTER AND FOUND MORE PARTICLES ON FILTER. ENGINE WAS DETERMINED TO UNSERVICEABLE. ENGINE WAS CHANGED AND AC RETURNED TO SERVICE. HAVE NOT YET DETERMINED THE SOURCE THE METAL SLIVER. (2003-001) 2G72 4U4 U H9EA E4NE 20040109000412004010900041NM 2004 1 9 GAIA03161OP 120031106A2120 ODOR BOEING727 727214 138407RNM PWA JT8 JT8D9 52048NE COCKPIT DETECTED A GAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07750US 21512 FERRY FLIGHT NR 750 MCJ TO JAX: DURING CRUISE THE CREW NOTICED AN OIL SMELL IN THE COCKPIT FROM THE AIR CONDITIONING. AN UNEVENTFUL LANDING WAS MADE. 2L73 4F4 F A3WE E2EA 20040109000662004010900066EA 2004 1 9 ASOA03584 120031116A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11850AS 7355 DURING A C-CHECK IN MCN, THE REAR PRESSURE BULKHEAD FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE REAR PRESSURE BULKHEAD FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040109000692004010900069EA 2004 1 9 2004F00007 220030606A7261MS938222 O-RING STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA LT ENGINE DAMAGED A DATAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13390GA SH3077 PCE84099 AIRCRAFT CLIMBED NORMALLY THROUGH 5000 FT WHEN LT OIL LIGHT ON CWP CAME ON. RIGHT AFTER CWP LIGHT CAME ON THE LT OIL PRESSURE GAUGE STARTED SHOWING AN ERRATIC INDICATION. POWER WAS REDUCED ON LT SIDE AND THERE WAS NO CHANGE WITH GAUGE. SHORTLY AFTER THAT CUMULATIVE OIL PRESSURE DROPPED BELOW 90 PSI. CREW ASKED FOR VECTORS TO VOR APPROACH AND TURNED BACK TO AIRPORT. DURING THE APPROACH THE OIL PRESSURE WENT BELOW 60 PSI. THE LT ENGINE WAS SHUTDOWN AND FLEW THE APPROACH SINGLE ENGINE INTO RUNWAY 33. THE AIRCRAFT WAS LANDED WITHOUT INCIDENT. THE BTV MECHANIC REPLACED THE DAMAGED O-RING ON THE OIL FILTER CAP IAW THE PWC MM CHAPTER 79 AND SERVICE THE OIL LEVEL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T4 T A41EU E4EA 20040112000052004011200005NM 2004 1 12 TSAA0255264 120030905A55126547511 SKIN BOEING737 737282 13844ATNM FUSELAGE GOUGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13824AL 23045 CUT AND REMOVED GOUGE AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040112000132004011200013WP 2004 1 12 AALA20031247 120031110A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21573AA 53092 DURING OVERNIGHT MAINTENANCE, FOUND EMEREGNCY PATH LIGHTS IN TAILCONE AREA INOPERATIVE. REPLACED EMERGENCY PATH LIGHTS IN TAILCONE AREA BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112000152004011200015EU 2004 1 12 ASOA03583 120031116A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11633AS 344 DURING A GROUND INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040112000272004011200027NM 2004 1 12 TSAA0253251 120031107A53306547952 SKIN BOEING737 737230 1384401NM FUSELAGE GOUGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 TRIMMED OUT DAMAGED AREA. HFEC INSPECTED THE EDGE OF CUTOUT. ENLARGED TRIM BY .04 AS AN INSURANCE CUT. ALODINED AND PRIEMD REWORKED AREA WITH BMS 10-11, TYPE 1. FABRICATED EXTERNAL DOUBLER FROM .063 INCH 2024-T3 CLAD. FABRICATED REPAIR FILLERS FROM 2024-T3 CLAD. ALODINED AND PRIMED ALL REPAIR PARTS. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. APPLIED FINISH COAT AND VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3317. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040114000262004011400026EU 2004 1 14 RAIA00312309 120031210A3230 LANDING GEAR JETAIRJETSTMJETSTM4101 1500501EU NLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03552HK 41057 JLN- NOSE GEAR WOULD NOT RETRACT. MAINTENANCE PERFORMED RETRACTION CHECK AND COULD NOT DUPLICATE CONDITION. 2L72 4T RTA41NM 20040114001042004011400104NM 2004 1 14 DLM88031041 120031119A533029525251 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27909DE 53418 INSPECTION OF A BLENDED GOUGE AND DENT AREA BETWEEN FS 1231 & FS 1265 AND BETWEEN STRINGERS 21R & 22R REVEALED A 6 INCH CRACK. THE CRACK AND BLENDED SKIN AREA WAS REMOVED WITH A 37 X 8.5 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM REPAIR DOUBLER PER THE MD-88 SRM AND PER ER/A 087782-14. 2L72 4F RTA6WE 20040114001092004011400109NM 2004 1 14 DLM88031045 120031121A2560 BATTERY DOUG MD88 MD88 3023688NM FLASHLIGHT WEAK A DALAK NONE O OTHER ININSP/MAINT 1 SO27927DA 49714 EMERGENCY FLASHLIGHT AT AFT ATTENDANT SEAT HAS WEAK BATTERY. REPLACED BATTERY. CHECKS GOOD. 2L72 4F RTA6WE 20040114001172004011400117NM 2004 1 14 DL757031050 120031125A2560MS203973C25 PIN BOEING757 757232 1384965NM EVAC SLIDE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 ON HMV-3 INSPECTION OPN 5726. PIN CORRODED BS 1180 S21-R/L BL 48R/L ON OVERWING ESCAPE SLIDE ACTIVATION/DEACTIVATION HANDLE RIGHT/LEFT SIDE. DEACTIVATION HANDLE HARD TO MOVE DUE TO CORROSION ON ATTACH PIN FOR BELLCRANK. BOTH SIDES FOUND CORRODED. REPLACED SAME. 2L72 4F RTA2NM 20040114001222004011400122NM 2004 1 14 DLM90031056 120031125A335020131A BATTERY DOUG MD90 MD9030 3023690NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27915DN 53395 FWD SECTION OF FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, NOW OPS NORMAL. 2L72 4F RTA6WE 20040114001752004011400175EA 2004 1 14 MASA200300409 120031015A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST TXTAXI/GRND HDL 1 SW0737228 7228 ASH NR 6320 PHX-BFL. FLT CREW NOTICED AN INTERIOR OVHD EMERGENCY LIGHT INOP. MX RELAMPED. OP CHECKS GOOD 2L72 4F RTA21EA 20040114001762004011400176NM 2004 1 14 MASA200300412 120031015A335001079009900 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07447YV 447 ASH NR 6203. PHX-CLD. CREW REPORTED THAT THE AFT EMERGENCY FLOODLIGHT WAS INOP. MECHANIC REPLACED THE POWER SUPPLY. OP CHECKS GOOD. 2H72 4T RTA13NM 20040114001822004011400182SO 2004 1 14 MASA200300427 120031025A2612MS24166D1 RELAY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FIRE DETCTION FAILED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07831MJ 145273 ASH 2638 CLT CARGO FIRE EXTINGUISHING SYSTEM WILL NOT TEST. MECHANIC REPLACED CARGO DETECTOR CIRCUIT RELAY. OP CHECKS GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040114001852004011400185SO 2004 1 14 MASA200300505 120031221A335066368 STRIP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07834MJ7551 145340 DURING ROUTINE MAINTENANCE INSPECTION MECHANIC FOUND LT EMERGENCY LIGHT STRIP INOPERATIVE. MECHANIC REPLACED LIGHT STRIP. OP CHECKS GOOD 2L72 4T4 FRTT00011ATTE6CH 20040114002272004011400227EA 2004 1 14 03338638 120031204A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27638BR 7311 DURING INSPECTION THE LT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040114002342004011400234EA 2004 1 14 03316681 120031112A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HORIZ STAB MALFUNCTIONED A VTZAK NONE F FLT CONT AFFECTED NRNOT REPORTED 1 EA27681BR 7680 DURING OPERATION OF THE AIRCRAFT THE MACH TRIM SYSTEM DISENGAGED DURING STABILIZER TRIM ACTUATION. THE FAULT WAS TROUBLESHOT TO THE HSTCU AND UNIT WAS REPLACED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20040115000252004011500025NM 2004 1 15 03FDEA02012 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 4 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000292004011500029NE 2004 1 15 SW07200300008 220030801A72504120T01P02 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE DAMAGED G FDKAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW07510MJ671 10101 GEE965440 ENGINE WAS REMOVED FOR HIGH VIBRATION AND DAMAGED 2ND STAGE HIGH PRESSURE TURBINE BLADES. 2L72 4F4 FRTA21EA EOOO63EN 20040115000342004011500034NM 2004 1 15 MWEA030467 120031203A5522 SKIN DOUG MD88 MD88 3023688NM LT ELEVATOR DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 LEFT ELEVATOR LOWER SKIN SURFACE OUTBOARD AREA HAS THREE DENTS. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20040115000402004011500040NM 2004 1 15 03FDEA02052 120031204A5320 SPLICE BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25198FE 19154 CORROSION ON STR 26R AFT OF SPLICE AT BS 486. REPAIRED STRINGER PER SRM 53-10-2, 51-30-5 & 51-30-2, 53-10-3 2L73 4F RTA3WE 20040115001082004011500108NM 2004 1 15 03FDEA02084 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 01 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCK BOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II. 2L73 4F RTA22WE 20040115001542004011500154NM 2004 1 15 03FDEA02155 120031209A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 STRINGER CLIP CRACKED, STR 6L, BS 950C. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STR 6L IAW SRM 51-30-2. 2L73 4F RTA3WE 20040115001632004011500163NM 2004 1 15 03FDEA02161 120031211A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 STRINGER CLIP CRACKED, STR 4L, BS 950C. REMOVED & REPLACED STRINGER CLIP AT BS 950C, STR 4L IAW SRM 51-30-2 2L73 4F RTA3WE 20040116000082004011600008SO 2004 1 16 GLBA20030515 120031211A324431544 TIRE EMB 120 EMB120ER 3260203SO MLG FAILED A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM0396ZK 120096 NR 1 AND NR 2 TIRES BLEW OUT ON TAKEOFF ROLL. R&R NR 1 & 2 TIRES REPLACED THE LT AFT INBOARD MAIN GEAR DOOR WITH NEW AND RIGGED CYCLED GEAR OPS CK GOOD 2L72 4T RTA31SO 20040116000152004011600015NM 2004 1 16 03FDEA02192 120031215A5710 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RIGHT WING - INBOARD FLAP VANE, INBOARD TRACK ATTACHMENT FITTING, BOLT HOLES (3) FOUND EXCEED LIMIT. RT WING - INBD FLAP VANE, INBD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-73366, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT INBD. FLAP VANE ATTACH FITTINGS REWORK. 2L73 4F RTA22WE 20040120000022004012000002NM 2004 1 20 03FDEA02199 120031216A2170 COALESCER BAG DOUG MD11 MD11 3023602NM AIR DISTRIBUTIONDAMAGED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25606FE 48602 DEPARTED CDG, ENGINE ANTI-ICE ON MAX PWR AT 3000 AGL SMOKE ODOR DETECTED THEN SMOKE ENTERED THE COCKPIT TURNED ON THE LIGHTS AND THE COCKPIT HAUL FILLED WITH SMOKE. WENT ON OXYGEN, RAN APPROPIATE CHECKLISTS. RAN NR 1 ENG FOR 20 MIN AND HAD A VERY LITE ODOR. PRECAUTIONARY DEFERRED NR 1 PNEU SUPPLY. ALSO CHANGED ALL 3 COALESCER BAGS PER MM 21-54-05-2. ALL 3 FOUND BLACK. 2L73 4F RTA22WE 20040120000032004012000003NM 2004 1 20 03FDEA02201 120031216A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION ON STRINGER CLIP BS 990 STR 27 LT. REMOVED & REPLACED STRINGER CLIP AT BS 990, STR 27 LT THAT WAS OUT OF LIMITS PER SRM 51-20-1 & SRM 51-30-2. 2L73 4F RTA3WE 20040120000282004012000028NE 2004 1 20 03FDEA02299 220031229A7200PW4152 ENGINE AIRBUS310 A310 EU PWA 4152 PW4152 NE INOPERATIVE A FDEACE ABORTED TAKEOFF ENGINE SHUTDOWN OAPOTHER FLAME/FIRE NO WARNING INDICATION TOTAKEOFF 1 SO25801FD2569025690 539 717763 HEARD LOUD BANG, NOSE MOVED TO RT SHARPLY. FOLLOWED REJECTED TAKEOFF PROCEDURE. ALL ENGINE INSTRUMENTS NORMAL AT 105 KTS. IAW TROUBLESHOOTING MANUAL AND POWERPLANT ENGINEERING CONCURRENCE, ENGINE WILL BE CHANGED. SHIPPING INFO TENATIVE FOR REPLACEMENT ENGINE FROM MEMPHIS VIA 9004/1 TO CDG THEN 5081/2 TO DXB. REQUIRES GOCC/CREW SCHEDULING CONCURRENCE. 2L72 4F RTA35EU E24NE 20040120000422004012000042NM 2004 1 20 03FDEA02333 120031230A5321 FLOOR PANEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 FLOOR PANEL 231PF FOUND TOP SURFACE WITH CORROSION. DAMAGED FLOOR PANEL NR 231PF REMOVED AND REPLACED AS PER MM 53-21-04-4. 2L73 4F RTA22WE 20040120000512004012000051NM 2004 1 20 03FDEA02289 120031229A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP I/B HINGE ACTUATOR O/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200. WINGS TRAILING EDGE AND TRAILING EDGE DEVICES, LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040120000532004012000053NM 2004 1 20 03FDEA02287 120031229A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING O/B FLAP I/B HINGE ACTUATOR I/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200. WINGS TRAILING EDGE AND TRAILING EDGE DEVICES, LT OUTBOARD FLAP/INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000092004012100009NM 2004 1 21 03FDEA02252 120031226A5744ARC050213 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING O/B FLAP I/B FWD HINGE ACTUATOR MOUNT I/B LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75208, TRAILING EDGE AND TRAILING EDGE DEVICES- LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040121000122004012100012NM 2004 1 21 03FDEA02266 120031226A5744ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING O/B FLAP I/B HINGE FITTING I/B MOUNT I/B AND O/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR 2L73 4F RTA22WE 20040121000202004012100020NM 2004 1 21 03FDEA02276 120031226A5744ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING OUTBOARD FLAP OUTBOARD HINGE FITTING INBOARD PIVOT MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, WINGS TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD. FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000242004012100024NM 2004 1 21 03FDEA02323 120031229A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 CORROSION IN FWD CARGO BAY ON STR 27L BS 550-560. FOUND CORROSION ON STR 27L BS 550 TO 560 TO PENETRATE 100 PERCENT OF ORIGINAL .040 THICKNESS. CUT AND REMOVED STRINGER BS 549 TO BS 567 AND INSTALLED REPAIR MADE FROM BAC 1498-132 LOT 507364 AND BAC 1498-140 7075 F6 LOT 507364 IAW SRM 53-10-3 FIG. 2. 2L73 4F RTA3WE 20040121000262004012100026NM 2004 1 21 03FDEA02321 120031229A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 CORROSION AT STRINGER 29 LT, BS 970-990. BLENDED OUT CORROSION AT STRINGER 29 LT BS 970-990 AND INSTALLED REPAIR STRAP PER SR 27-53-023. 2L73 4F RTA3WE 20040114001412004011400141NM 2004 1 14 DLM88031069 120031204A575359359011 HINGE FITTING DOUG MD88 MD88 3023688NM T/E FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27907DL 49538 OUTBOARD FLAP INBOARD HINGE FITTING DAMAGED AT PIVOT POINT AND PIVOT BOLT IS MISSING NUT AND COTTER PIN. REPLACED SAME. 2L72 4F RTA6WE 20040114001622004011400162NM 2004 1 14 03FDEA02014 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 1 I/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040114001682004011400168EU 2004 1 14 MALA030570 120031218A5512 SKIN SAAB SF340 340B 7860101EU HORIZ STAB DELAMINATED A MALAK NONE O OTHER NRNOT REPORTED 1 GL15435XJ 340B435 RT HORIZONTAL STAB HAS DENT AT HS 99.92, FOUND TO BE DELAMINATED. MAINTENANCE REMOVED AND REPLACED RT HORIZONTAL STAB LOWER SKIN AT HS 99, IAW EO NR S55038 DATED 19 DEC 03. REF TO WORK CARD NR 184027 30272, 253007 FOR ADDITIONAL REPAIR INFORMATION. 2L72 4T RTA52EU 20040114002072004011400207WP 2004 1 14 MWEA030430 120031023A53305911412191 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 EXTERNAL FUSELAGE SKIN HAS SEVERAL LIGHTING STRIKES AT FRAME STATION 256 LONGERON 29 LEFT. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR. 2L72 4F4 F A6WE E2EA 20040115000032004011500003NM 2004 1 15 03FDEA02018 120031203A5750ARC1991 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 2 O/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP -OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000102004011500010NM 2004 1 15 03FDEA02025 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 2 FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000132004011500013NM 2004 1 15 03FDEA02028 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 3 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000432004011500043NM 2004 1 15 UPS03541632 120031204A5230 SKIN BOEING757 75724APF 1384969NM MAIN CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01436UP 25467 MAIN CARGO DOOR HAS A DAMAE SKIN AFT UPPER CORNER BEHING AFT ACTUATOR. REPAIRED DAMAGED SKIN ON MCD AFT UPPER PER SRM 52-30-01-2. 2L72 4F RTA2NM 20040115000452004011500045CE 2004 1 15 DXTA200300176 120031204A3260 BULB CESSNA560 560XL 2076702CE MLG INDICATOR BURNED OUT E DXTAO OTHER P NO WARNING INDICATION LDLANDING 1 GL07603QS 5605203 DURING FINAL APPROACH BOTH MAIN GEAR INDICATIONS, DID NOT SHOW DOWN AND LOCKED. AIRCRAFT DIVERTED TO SMF AND ACCOMPLISHED A QRH PROCEDURE. NO EMERGENCY WAS DECLARED, BUT CFR WAS ROLLED BY ATC. TROUBLESHOT MLG LIGHTS, FOUND RIGHT AND LEFT MAIN LIGHT BULBS INOP. REPLACED BULBS & PERFORMED GEAR FUNCTIONAL OP'S. CHECK SATISFACTORY RESULTS. WORK PERFORMED IAW CITATION 560XL MM, CHJP 32-60-00 &32-01-00-720. GEAR N2 BOTTLE WAS SERVICED IAW 560XL MM, CHP 12-13-01. THIS ITEM IS STILL UNDER INVESTIGATION. 2L72 4F RTA22CE 20040115000712004011500071NM 2004 1 15 03FDEA02057 120031205A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION (C53-113-01), IN STRINGER BS 1010-1030 STR 27 LT. FOUND CORROSION ON STRINGER BS 1010-1030, STR 27LT TO BE OUT OF LIMITS PER SRM 53- 10-1. REPAIRED STRINGER IAW SRM 53-10-3. 2L73 4F RTA3WE 20040115001092004011500109NM 2004 1 15 DL757031092 120031215A3610366001036 SHUTOFF VALVE BOEING757 757232 1384965NM NR 1 ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO27619DL 22909 ON TAKEOFF GOT LT ENG BLEED ALERT ON EICAS, AND OFF LIGHT ON OVERHEAD BLEED PANEL. REPLACED LEFT PRSOV. 2L72 4F RTA2NM 20040115001102004011500110 2004 1 15 DL757031093 420031216A2565D30654131 SLIDE BOEING757 757232 1384965NM R1 DOOR FAULTY A DALAK NONE J WARNING INDICATION ININSP/MAINT 1 SO27674DL 25979 THE 1R DOOR SLIDE LIGHT REMAINS ILLUMINATED AFTER SLIDE IS IN DISARMED POSITION. SLIDE DID NOT DEPLOY PROPERLY. REPLACED SLIDE, ASSIST BOTTLE, FWD PROX SWITCH AND FWD GIRT BAR FOOT. 2L72 4F RTA2NM 20040115001112004011500111NM 2004 1 15 DL73S031094 120031216A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 FOUND ON W-2 LETTER CK, SKIN BULGED/ RIVETS SHEARED AT FRAME STA 847 BETWEEN STR 27 LEFT AND 27 RIGHT. FOUND FORMER CORRODED AT THIS LOCATION. REPAIRED PER SRM 53-10-4 FIG 9A. 2L72 4F RTA16WE 20040115001332004011500133 2004 1 15 DL777031098 420031217A23301301851100 MONITOR BOEING777 777232 1385232NM CABIN FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27863DA 29735 SMOKE COMING FROM VIDEO SCREEN OVERHEAD AT SEAT ROW 33G/32G ATL AMT'S. REMOVED AND REPLACED OVERHEAD MONITOR 32H AND VDU 5. OPS CHECK NORMAL. 2L72 4F RTT00001SE 20040115001382004011500138NM 2004 1 15 DL757031104 120031218A525010C10F SWITCH BOEING757 757232 1384965NM LAVATORY SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27636DL 23763 MID LAV DOOR SWITCH SHORTED. REPLACED SWITCH. 2L72 4F RTA2NM 20040115001792004011500179EU 2004 1 15 2004F00039 120030915A261273040102 FIRE DETECTOR AIRBUS320 A320232 3930326EU E/E BAY MALFUNCTIONED A RYNAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE07391LF 676 DURING CRUISE FLIGHT, NR 2 ENGINE FIRELIGHT AND REPEATER LIGHT ILLUMINATED. NO MASTER CAUTION OR ECAM MESSAGES PRODUCED. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED FIRE DETECTION UNIT. OPERATIONAL CHECKED NORMAL. (M) 2L72 4F RTA28NM 20040122000402004012200040EU 2004 1 22 USAA040122A 120031126A3350 BULB AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19181UW 1531 PHL - THE EMERGENCY LIGHTS WOULD NOT PASS THE LIGHT TEST. MAINTENANCE REPLACED BULBS IN THE MID CABIN EXIT SIGN. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040120000012004012000001CE 2004 1 20 2003F00640 120031210A3230BZ7RT04 LIMIT SWITCH CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO MLG ACTUATOR STUCK E DUFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL273729C 402B0589 FOLLOWING DEPARTURE, THE PILOT SELECTED THE LANDING GEAR UP POSITION. THE GEAR IN TRANSIT LIGHT ILLUMINATED AND THE GEAR RETRACTED AS NORMAL UNTIL IT REACHED THE FULL UP POSITION. THE PILOT HEARD THE GEAR MOTOR PULL HARD AND THEN THE GEAR MOTOR CIRCUIT BREAKER POPPED. THE PILOT THEN SELECTED GEAR DOWN AND RESET THE CIRCUIT BREAKER. THE GEAR EXTENDED NORMALLY AND THE THREE GREEN, “GEAR DOWN AND LOCKED” LIGHTS ILLUMINATED. HE THEN RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION BY MAINTENANCE PERSONNEL, IT WAS DETERMINED THAT THE GEAR UP LIMIT SWITCH HAD FAILED. 1L72 3O3 O A7CE E8CE 20040120000092004012000009NM 2004 1 20 2003UALA00971 120031218A21216067726 FAN BOEING757 757222 1384956NM PWA 2037 PW2037 NE RIGHT FAILED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29555UA 26647 RT RECIRCULATING FAN SENT BURNING ODOR THROUGHOUT THE CABIN. THE BEARING FAILED RESULTING IN FAN BLADE CONTACT WITH THE CASE. FAN REPLACED 2L72 4F4 FRTA2NM E17NE 20040120000132004012000013NM 2004 1 20 2003UALA00991 120031230A35108315625020R TRANSDUCER BOEING777 777222 1385219NM PWA PW4077PW4077 NE CREW O2 DEFECTIVE A UALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 WP29781UA 26945 LOST ALL CREW OXYGEN. DEFECTIVE O2 TRANSDUCER. REPLACED TRANSDUCER. 2L72 4F4 FRTT0001SE E46NE 20040121000142004012100014NM 2004 1 21 03FDEA02270 120031226A5744ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING O/B FLAP I/B HINGE ACTUATOR MOUNT LUG I/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000472004012100047EA 2004 1 21 ASOA03589 120031119A5210601R3807413 ANCHOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A C-CHECK IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040121000582004012100058EA 2004 1 21 ASOA03592 120031120A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11850AS 7355 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20040121000622004012100062EA 2004 1 21 ASOA03593 120031120A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, BL 27.00-36.00 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, BL 27.00-36.00 IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20040121000682004012100068EA 2004 1 21 ASOA03595 120031120A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A C-CHECK IN MCN, THE FLOORBEAM SUPPORT ANGLE AT FS 280, LBL 9 INBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM SUPPORT ANGLE AT FS 280, LBL 9 INBOARD IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040121000692004012100069EU 2004 1 21 ASOA03613 120031106A5320 CHANNEL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN BNA, THE FLOOR LEVEL U-CHANNEL JUST INBOARD OF THE PASSENGER DOOR SPRINGS BETWEEN FRAMES 39 AND 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR LEVEL U-CHANNEL JUST INBOARD OF THE PASSENGER DOOR SPRINGS BETWEEN FRAMES 39 AND 40 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040121000772004012100077EU 2004 1 21 ASOA03615 120031106A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN BNA, THE FLOOR FLANGE AT THE RT SIDE WALL BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR FLANGE AT THE RIGHT SIDE WALL BETWEEN FRAMES 39 AND 41 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20031202000392003120200039NM 2003 12 2 USAASB03192 120031016A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 ORD - FOUND AISLE EMERGENCY LIGHT AT SEAT 22 INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT 22. (M) 2L72 4F RTA16WE 20031202000552003120200055NM 2003 12 2 2003F00600 120031017A3350GE767 BULB BOEING757 757236 1384971NM EMERGENCY LIGHT BURNED OUT A P9RAK NONE O OTHER ININSP/MAINT 1 EA11958PG 24118 ON DAILY CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB IAW B757 MM 33-51-12. (M) 2L72 4F RTA2NM 20031202000582003120200058NM 2003 12 2 2003F00601 120031017A2750 CONTROL UNIT BOEING757 757236 1384971NM TE FLAPS MALFUNCTIONED A P9RAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA11522NA 25133 DURING APPROACH SELECTED FLAPS 20 DEGREES. STOPPED AT 15 DEGREES. PERFORMED ABNORMAL/EMERGENCY CHECKLIST WITH A NORMAL LANDING. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM 3 TIMES AND ALL CHECKS GOOD IAW B757 MM 27-51-00. (M) 2L72 4F RTA2NM 20031202000622003120200062 2003 12 2 USAABA03037 420031021A2565 SLIDE AIRBUS330 A330323 3930335EU R2 DOOR MALFUNCTIONED A K NONE L NO TEST ININSP/MAINT 1 EA19677UW 0380 DURING THE ANNUAL SLIDE DEPLOYMENT CHECK, THE R2 DOOR SLIDE DID NOT DEPLOY AUTOMATICALLY. THE SLIDE DID FUNCTION NORMALLY WHEN DEPLOYED MANUALLY. NO DEFINITIVE REASON FOR THE AUTOMATIC FAILURE WAS FOUND. SUBSEQUENT SLIDE DEPLOYMENTS WERE FREE OF THIS DISCREPANCY. (M) 2L72 4F RTA46NM 20031124000492003112400049NM 2003 11 24 03FDEA01915 120031112A5753 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT WING, FOUND OUTBOARD FLAP STOP FITTING FWD RIB WITH CRACK APPROX 0.125 INCHES IN LENGTH. RT WING O/B FLAP STOP FITTING FWD RIB CRACK REPAIRED AS PER FEDEX EA 1-5750-74244 WING - TRAILING EDGE FLAPS - LT & RT O/B FLAP SECONDARY STOP BOSS REPAIR. 2L73 4F RTA22WE 20031124001042003112400104WP 2003 11 24 DHL2003805552 120030728A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA 797.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. REFER OT N/R 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031124001222003112400122WP 2003 11 24 DHL2003807544 120031019A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT WING OTBD INNER L/E EXTERNAL SKIN HAS CORROSION AT STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW NDT STANDARD PRACTICE MANUAL PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW ASTAR ED EDU21-3, ASTAR DWG U21-R03. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ASTAR ED EDU21-3, ASTAR DWG U21-R03, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000332003112500033WP 2003 11 25 DHL2003805565 120030806A5730 PLATE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 ELONGATED HOLES IN UPPER PLATING OF LEFT WING CTR L/E STA XS 520.168. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12. REMOVED UPPER PLATING WITH ELONGATED HOLES IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW PLATING IAW SRM 57-3-3 PG 12. CLEANED, TREATED AND PRIMED INNER FACE OF NEW PLATING IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. REFER TO N/R 0184 FOR REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031125000382003112500038WP 2003 11 25 DHL2003805523 120030806A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 478.897. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED AN ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000632003112500063WP 2003 11 25 DHL2003807526 120031022A532037552222 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MAIN CARGO COMPT FITTING CRACKED 0.500 AT STA 782.000 RBL 24 (CENTER WING SECTION). REMOVED AND REPLACED CRACKED FITTING ON MAIN CARGO COMPT STA 782.000 RBL 24 (CENTER WING SECTION) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000882003112500088WP 2003 11 25 DHL2003805545 120030728A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OUTBD L/E FORMER 0.500 CRACKED, STA XFS 766.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. REFER TO NR 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031125001212003112500121NM 2003 11 25 ASAA0310263 120030401A532069554371 PLATE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIR TORQUE BOX PLATE AT BS 947-948, WATERLINE 206-208 CORRODED. REPLACED PLATE PER SRM. (M) 2L72 4F RTA16WE 20031125001282003112500128NM 2003 11 25 ASAA0310152 120030317A7110657019424 GUSSET BOEING737 737210C 1384459NM NR 2 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL GUSSET AT NACELLE STATION 236 CHAFED. REMOVED AND REPLACED GUSSET PER SRM. (M) 2L72 4F A16WE 20031125001322003112500132NM 2003 11 25 ASAA0310158 120030318A491065689405 LINER BOEING737 737210C 1384459NM APU BAY CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND APU TORQUE BOX LINER AT BS 1104, RIGHT BUTTOCK LINE 20 GOUGED AND CRACKED. REPAIRED TORQUE BOX LINER PER EA. (M) 2L72 4F A16WE 20031126000342003112600034NM 2003 11 26 AWXA200301387 120031022A5320657094773 CLIP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE REMOVED THE CRACKED FRAME ATTACH CLIP AT BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 90-8610; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 PG 1. 2L72 4F RTA16WE 20031126000662003112600066CE 2003 11 26 DXTA200300166 120031119A3242 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07313QS 5600325 POWER BRAKE LOW PRESS AND ANTI-SKID INOP LIGHT REMAINED ILLUMINATED ON MASTER CAUTION PANEL AFTER GEAR WAS LOWERED; BRAKES FELT SOFT, HAD TO USE EMERGENCY BRAKE TO COMPLETELY STOP THE AIRCRAFT. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20031202000122003120200012WP 2003 12 2 GTIA030732 120030823A3150 WARNING LIGHT DOUG DC9 DC982 3022082WP SLAT SYSTEM ILLUMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 A/C 823 HAS AUTO SLAT FAIL LIGHT ON TAXI OUT. UNSCHEDULED CHANGE A/C EN ROUTE. (M) 2L72 4F A6WE 20031202000222003120200022NE 2003 12 2 AMTA200301238 220030927A7323FFG022AC GOVERNOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE ENGINE MALFUNCTIONED A AMTAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 GL11528AT 30887 31398 GENERATOR DROPPED OFF LINE, FOLLOWED BY ENGINE PARAMETERS THAT INDICATED THE ENGINE HAD FLAMED OUT. REPLACED FFG PER MM 73-21-01. REPLACED HP FUEL PUMP PER MM 73-11-03. REPLACED LP FUEL PUMP PER MM 73-11-01. REPLACED FUEL PRESSURE SWITCH PER MM 73-35-01. REPLACED LP FUEL PUMP SCAVENGE FILTER PER MM 73-11-10. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA2NM E12EU 20040311000182004031100018NM 2004 3 11 ASAA0310100 120030306A52106554960505 TORQUE BOX BOEING737 737298C 1384490NM L1 DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND L1 DOOR TORQUE BOX WEB AT BS 351.2, STRINGER 18L CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040311000472004031100047NM 2004 3 11 ASAA0310114 120030307A7110655226323 ANGLE BOEING737 737298C 1384490NM NR 2 COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL ANGLE AT NACELLE STATION 200 CRACKED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040311000112004031100011NM 2004 3 11 ASAA0310124 120030307A78301731011513 SKIN BOEING737 737298C 1384490NM THRUST REVERSER CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE THRUST REVERSER SKIN AT THRUST REVERSER STATION 96.47-121.47 PITTED. REMOVED AND REPLACED DAMAGED SKIN PER SRM. (M) 2L72 4F RTA16WE 20040311000252004031100025NM 2004 3 11 ASAA0310120 120030307A523065622542 SUPPORT ANGLE BOEING737 737298C 1384490NM CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND MAIN CARGO DOOR SUPPORT ANGLE AT BS 426, STRINGER 14L CRACKED. CUT OUT DAMAGED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031125000782003112500078WP 2003 11 25 DHL2003805557 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 828.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO NR 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031125000932003112500093 2003 11 25 HNAA0300066 420031103A3442071131333 DISPLAY DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 EA07935HA2727210818 142 DURING PASSENGER BOARDING, CAPTAIN SAW SMOKE COMING FROM AROUND RADAR GRAPHICS UNIT, POWERED DOWN AIRCRAFT, SMOKE DISSIPATED. PERFORMED HIDDEN DAMAGE INSPECTION AND DEACTIVATED RADAR GRAPHICS UNIT IAW EO8-24-03-0979. REPLACED RADAR GRAPHICS UNIT. 2H72 4T RTA13NM 20031125001042003112500104WP 2003 11 25 AALA20031293 120031118A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21489AA 49682 SAN FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED FIRST CLASS OVERHEAD EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031125001242003112500124NM 2003 11 25 ASAA0310107 120030306A5320654585554 SILL BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND AFT GALLEY DOOR MOP SILL AT BS 907-1006, RIGHT BUTTOCK LINE 52 CORRODED. REMOVED AND REPLACED MOP SILL PER SRM. (M) 2L72 4F A16WE 20031125001542003112500154NM 2003 11 25 ASAA0310505 120030603A53116546595140 FRAME BOEING737 7372X6C 1384552NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 727A, STRINGER 25L-26L CORRODED. REMOVED DAMAGED SECTION OF FRAME AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031125001572003112500157NM 2003 11 25 ASAA0310498 120030602A5347BAC15201434 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 420-480, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20040311000132004031100013NM 2004 3 11 ASAA0310117 120030307A53136550540501 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 20R AT BS 994-1006 CORRODED. REMOVED DAMAGED SECTION AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040311000272004031100027NM 2004 3 11 ASAA0310254 120030327A5730 SKIN BOEING737 737298C 1384490NM RT WING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND RIGHT WING LEADING EDGE SKIN AT WING STATION 227 WORN AND CHAFED. REMOVED DAMAGED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031126000022003112600002NM 2003 11 26 QXEA200301467 120031121A3233465507 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM RT MLG FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09401QX2773 30 4031 PDX- ON FLIGHT 2381 RIGHT MAIN GEAR DOOR AMBER CAUTION LIGHT ILLUMINATED AFTER GEAR RETRACTION. COMPLIED WITH CHECKLIST AND AMBER CAUTION LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 2 MLG RETRACTION ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031126000822003112600082SO 2003 11 26 C2XA03SH426 120031104A532014522460015 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031126001192003112600119NM 2003 11 26 ASAA0310454 120030515A57536571909109 SKIN BOEING737 737290C 138448VNM TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND LEFT WING MID FLAP SKIN AT WING STATION 204.4 CHAFED. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031126001212003112600121NM 2003 11 26 ASAA0310452 120030515A5315BAC15061702 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 590, LEFT BUTTOCK LINE 24.5 CORRODED. REMOVED CORROSION AND REPAIRED PER EA. (M) 2L72 4F A16WE 20031202000292003120200029NM 2003 12 2 ASAA0340090 120030228A53206553844 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR TO SIDEWALL SUPPORT BS 747-767 RBL 21 TO WL 158. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031125000162003112500016WP 2003 11 25 DHL2003807550 120031028A321357591681 ARM DOUG DC8 DC873F 302199FWP RT MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT MLG UPPER TORQUE ARM CRACKED. REMOVED AND REPLACED TORQUE ARM ON RIGHT MLG IAW MM 32-11-4 PG 202-205. FOR OPS CHECK SEE JC 8-32-00-003. 2L74 4F RT4A25 20031125000202003112500020WP 2003 11 25 DHL2003807516 120031016A53203750257U1 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SPLICE FITTING 2.500 CRACK (STA 600.000 - 620.000, L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING WITH NEW FASTENERS AND PRC SEALANT IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20031125000232003112500023WP 2003 11 25 DHL2003807529 120031018A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 A-BELLY DOOR EXTERNAL SKIN CRACKED .750 AT STA 280.000, L30R - L31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ASTAR ED EDU21-6, ASTAR DWG U21-R06. PERFORMED NDT INSPECTION IAW NDT STANDARD PRACTICE MANUAL PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW ASTAR ED EDU21-6, ASTAR DWG U21-R06. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ASTAR ED EDU21-6, ASTAR DWG U21-R06, SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000642003112500064WP 2003 11 25 DHL2003807501 120031009A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 EXTERNAL FUSELAGE INTERIM REPAIR STA 500.000 - STA 520.000, L21 - L24R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA AND FABRICATED FINGER DOUBLER AND DOUBLER IAW SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMED AREA, FINGER DOUBLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FINGER DOUBLER AND DOUBLER WITH NEW FASTENERS IAW SRM 53-2-1 FIG 7 SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000822003112500082WP 2003 11 25 DHL2003805572 120030825A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 FWD ACCY COMPT FRAME CRACKED 3.000 AT STA 55.000, L-25R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. TRIMMED OUT CRACKED FRAME SEGMENT IAW SRM 53-2-0 FIG 2. FABRICATED FRAME SEGMENT AND SPLICES (02 EA) IAW SRM 53-2-0 FIG 2. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND SPLICES WITH NEW FASTENERS IAW SRM 53-2-0 FIG 2, SRM 51-1-2 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125001152003112500115SW 2003 11 25 2003F00618 120030627A2120 ODOR FRCHLDSA227 SA227DC 3377521SW COCKPIT DETECTED A BSAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM051119K DC830B BIL - FLT 1424 - FLIGHT CREW NOTED STRONG SMELL OF ELECTRICAL SMOKE IN COCKPIT AT START OF DESCENT. SMELL DISSIPATED BY LANDING TIME. (M) 2L72 4T RTA18SW 20031125001372003112500137NM 2003 11 25 ASAA0310156 120030318A531565546057 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM FLANGE AT BS 420, LEFT BUTTOCK LINE 2, LEFT BUTTOCK LINE 42 CORRODED. REMOVED DAMAGED AREA AND REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20031125001532003112500153NM 2003 11 25 ASAA0310503 120030602A57306546419185 SKIN BOEING737 7372X6C 1384552NM LT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING LEADING EDGE AT WING STATION 505 CHAFED. REMOVED DAMAGED SECTION OF LEADING EDGE AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031126000032003112600003NM 2003 11 26 QXEA200301470 120031114A5753 SPAR BOMBDRDHC8 DHC8401 1390041NM T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX- DAMAGE FOUND ON FRONT SPAR OF RIGHT HAND FLAP UNDER NR 5 FITTING. REPAIRED IAW HORIZON AIR EO 6-27-147. 2H72 4T RTA13NM 20031126000112003112600011SO 2003 11 26 RAIA00311287 120031114A361014541376401 DUCT EMB 145 EMB145LR 3260212SO BLEED AIR SYS CRACKED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03819HK 145062 5700-STL- BLEED LEAK INDICATION NR 2. MAINTENANCE REMOVED AND REPLACED PRECOOLER DUCT. 2L72 4T RTT00011AT 20031126000602003112600060NM 2003 11 26 CALA0300664 120030716A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 16. REPAIRED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031126001082003112600108NM 2003 11 26 ASAA0340123 120030310A5720654543928 WEB BOEING737 737490 1384715NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 DURING C-CHECK, FOUND GOUGE IN WEB AT RIGHT AIR CONDITIONING BAY 1 INCH BELOW THE AFT RT HEAT EXCHANGER OUTBOARD FLANGE INBOARD SIDE OF WEB. REPAIRED IAW SRM. 2L72 4F RTA16WE 20031126000172003112600017NM 2003 11 26 QXEA200301462 120031117A5210 RETAINER BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DEFECTIVE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09413QX 4060 GEG- ON FLIGHT 2365 AFT LEFT HAND PASSENGER WILL NOT CLOSE PROPERLY. FOUND RETAINER SEAL NOT ENGAGED IN HANDLE SHAFT. REMOVED AND REPLACED RETAINER RING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031126000372003112600037EA 2003 11 26 COMA0360489 120031030A2910601R7514785 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01966CA 7132 FLIGHT 5255 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED SUCTION LINE IN LT PYLON. 2L72 4F RTA21EA 20031126000392003112600039NE 2003 11 26 COMA0360491 220031110A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT FAILED A COMAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01924CA13668 7026 807478 FLIGHT 5195 LOUD BANG AFTER TAKEOFF, THEN HEAVY VIBRATION FROM RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE. 2L72 4F4 FRTA21EA E15NE 20031126000542003112600054NM 2003 11 26 QXEA200301472 120031122A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM AFT LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09413QX 4060 PDX- ON FLIGHT 2307 AFT AIRSTAIRS ARE STIFF TO SLIDE OUT AND NEED LUBE. CLEANED AND LUBED SLIDING TRACKS ON AFT AIRSTAIRS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031126000742003112600074SO 2003 11 26 2XA03SH450 120031112A532014525681607 ANGLE EMB 145 EMB145ER 3260211SO FUSELAGE WARPED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE CARGO DOOR CUTOUT FRAME 66 ANGLE WAS FOUND TO BE WARPED OUT OF CONFIGURATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031126000802003112600080SO 2003 11 26 C2XA03SH416 120031027A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711539 145536 SHV- DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031126001132003112600113NM 2003 11 26 AALA20031016 120030916A2497 RECEPTACLE BOEING757 757223 1384957NM POWER PORT MALFUNCTIONED A AALAO OTHER O OTHER CRCRUISE 1 SW21194AA 32388 ABOUT 1 1/2 HOURS INTO FLT, 30 MINUTES AFTER LEVELING FL390, F/A'S REPORTED A LOUD SQUEALING NOISE COMING FROM OVERHEAD IN 1ST CLASS, ROW 1 & 2. SOUND WASN`T AFFECTED BY DESCENT. TALKED TO TULSA, TURNED OFF 1 PACK AT A TIME, TRIM & RECIRC FANS, NO CHANGE, FL200, WHILE DIVERTING TO MIA SOUND STOPPED. PRESSURIZATION A/C ALL SEEMED TO OPERATE NORMAL. CONTINUED TRIP 601 MIA DFW FLT CREW REPORTED SAME CONDITION ON 5DL SEAT 2B. PAX HAD A COMPUTER PLUGGED INTO POWERPORT SYS. UNPLUGGED, NOISE STOPPED. PERFORMED OPERATIONAL TEST OF ALL 1ST CLASS POWERPORTS UTILIZING POWERPORT TEST KIT. REPORT ALL FINDINGS IN FMR. ACCOMPLISHED TFI. ALL OPS TESTS FOUND SYS OK FOR ALL 1ST CLASS SEATS. (M) 2L72 4F RTA2NM 20031202000262003120200026WP 2003 12 2 GTIA030716 120030928A3297 CONDUIT DOUG DC9 DC982 3022082WP LT MLG WW OUT OF POSITION A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23812NK 48021 LEFT MAIN RED GEAR LIGHT ON WITH LANDING GEAR HANDLE UP. QRH PROCEDURE FOLLOWED, NO CHANGE. REPOSITIONED LT MAIN GEAR UPLOCK SENSOR CONDUIT AND OPS CHECKED. NO DEFECTS NOTED. OK FOR SERVICE. (M) 2L72 4F A6WE 20040311000522004031100052NM 2004 3 11 ASAA0310098 120030306A5313BAC1498158 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 21L AT BS 767 CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20040311000432004031100043NM 2004 3 11 ASAA0310134 120030310A532069612651 SUPPORT ANGLE BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND BULKHEAD SUPPORT ANGLE AT BS 500B, LEFT BUTTOCK LINE 35, RIGHT BUTTOCK LINE 35 CORRODED. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE PER SRM. (M) 2L72 4F A16WE 20031202000642003120200064NM 2003 12 2 USAABB03194 120031019A33506210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19630AU 27808 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031202000662003120200066EU 2003 12 2 USAASA03124 120031018A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW 0844 LEFT CENTER EPSU FAILED TEST. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA28NM 20031202000672003120200067EU 2003 12 2 USAASA03123 120031018A3350321431 BATTERY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW 0844 FORWARD LEFT EPSU FAILED TEST. MAINTENANCE REPLACED THE EPSU BATTERY. (M) 2L72 4F RTA28NM 20031202000762003120200076NM 2003 12 2 USAABB03190 120031014A3397 CONNECTOR BOEING757 7572B7 1384964NM R4 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 FOUND R4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED THE CONNECTOR AT THE LIGHT. (M) 2L72 4F RTA2NM 20031202000772003120200077NM 2003 12 2 USAABB03183 120031010A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 TPA - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20031202000852003120200085EA 2003 12 2 ASOA03525 120031018A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484 INBOARD SIDE OF LBL 36 AND RBL 36 AND OUTBOARD OF LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTALS AT FS 484 INBOARD SIDE OF LBL 36 AND RBL 36 AND OUTBOARD OF LBL 27 AND RBL 27 IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20031202000872003120200087NM 2003 12 2 USAA030211 120031003A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48518 23319 FOUND SKIN CRAKCED .375 INCH, LOWER HINGE CUT OUT AFT SERVICE DOOR. REMOVED DAMAGE, INSTALLED TRIPLERS PER SRM 53-60-01. (M) 2L72 4F RTA16WE 20031202000932003120200093EA 2003 12 2 ASOA03527 120031020A5210 LINKAGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE INTERNAL LINKAGE ON THE PASSENGER DOOR. NO OTHER RESISTANCE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031202000952003120200095NM 2003 12 2 USAA030215 120031021A5230 SKIN BOEING737 7373B7 1384580NM CARGO DOOR CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US51167 22959 FOUND SKIN CHAFED .5 INCH LONG, INNER SKIN, FORWARD CARGO DOOR BETWEEN BEAM 2 AND 3, NEAR CENTER. DAMAGE TRIMMED, DOUBLERS INSTALLED PER EA 77218 AND SRM 51-70-13. (M) 2L72 4F RTA16WE 20031202001012003120200101EA 2003 12 2 ASOA03521 120031019A5320CRACKED FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE LT AND RT FLOOR SUPPORT ANGLE AT FS 621 IN THE CARGO COMPARTMENT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLE AT FS 621 IN THE CARGO COMPARTMENT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20031202001222003120200122EA 2003 12 2 A6WA200340148 120031020A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS MISRIGGED A A6WAO OTHER J WARNING INDICATION CLCLIMB 1 GL31454AW 7842 FLAP FAIL CAS MESSAGE AT ZERO FLAPS ON CLIMB, DECLARED EMERGENCY. RE-RIGGED, FLAPS. (M) 2L72 4F RTA21EA 20031202001252003120200125EA 2003 12 2 A6WA200340144 120031016A2150601R952081 DUCT CNDAIRCL600 CL6002B19 1900309EA NR 2 PACK CRACKED A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31418AW 7618 EXCESSIVE ENGINE EXHAUST ODOR IN COCKPIT AND CABIN WHILE RUNNING APU. INSPECTION AND FOUND NR 2 PACK COMPRESSOR OUTLET TEMP SWITCH DUCT CRACKED. REMOVED AND REPLACED DUCT ASSEMBLY. (M) 2L72 4F RTA21EA 20031202001282003120200128EU 2003 12 2 SIMA200330102 120031025A3350MS274061 SWITCH SAAB SF340 340B 7860101EU COCKPIT INTERMITTENT A SIMAK NONE O OTHER ININSP/MAINT 1 SW21392AE 340B392 DURING A SCHEDULED CHECK, MAINTENANCE REPORTED THE EMERGENCY LIGHTING SYSTEM TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SELECTOR SWITCH IN THE COCKPIT IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20031202001332003120200133EU 2003 12 2 A6WA20030060 120031022A5753 PLATE BAC 146 146200A 1500266EU NR 1 FLAP DAMAGED A ATWAK NONE O OTHER ININSP/MAINT 1 GL31291UE E2084 NR 1 FLAP LANDING PLATE DAMAGED, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910002. (M) 2H74 4F A49EU 20031202001352003120200135EU 2003 12 2 ASOA03506 120030928A5320 CHANNEL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING A C-CHECK IN BNA, THE C-CHANNEL UNDER THE SERVICE DOOR THRESHOLD BETWEEN FS 38/39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE C-CHANNEL UNDER THE SERVICE DOOR THRESHOLD BETWEEN FS 38/39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20031202001482003120200148NE 2003 12 2 MEX2003496 220031017A732076960615 FUEL CONTROL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LT ENGINE FAILED A ASMFA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW23162PL 49765 AIRCRAFT RETURNED DUE TO LEFT ENGINE HIGH TEMPERATURE INDICATIONS. DURING STARTING BOTH ENGINES REACHED 475 DEGREES CELSIUS WITHOUT BLEEDS AND ALMOST 480 WITH BLEEDS ON IDLE. DURING INITIAL CLIMB, EPR'S MANUAL RE-EDITION WAS PERFORMED REACHING BOTH ENGINES MINUS THAN 610 DEGREES CELSIUS. AFTER LANDING WITH BOTH ENGINES ON IDLE, RIGHT ENGINE REACHED 490 DEGREES CELSIUS AND LEFT ENGINE 475 DEGREES CELSIUS. TRIM WAS PERFORMED TO BOTH ENGINES IAW MM 71-00-00, ALL CORRECT. OVERWEIGHT INSPECTION WAS ACCOMPLISHED IAW MM 05-51-04. DURING OVERNIGHT SERVICE, FCU WAS REPLACED AND BOROSCOPE INSPECTION WAS PERFORMED IAW MM 73-20-01 AND 72-0000, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20031202001562003120200156SO 2003 12 2 SIMA200327201 120030925A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21635AE 145158 CMH - REARE CABIN EMERGENCY LIGHTS INOPERATIVE. RAI NR 4 EMERGENCY BATTERY, OPS CHECK GOOD. (M) 2L72 4T RTT00011AT 20031202001132003120200113EU 2003 12 2 A6WA200360059 120031022A5753 TAB BAG BAE146BAE146200A 1500266EU TE FLAP DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31291UE E2084 RIGHT OUTBOARD FLAP TAB TRAILING EDGE DAMAGED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS RED AVMAX FAX 1698-6910001. (M) 2H74 4F RTA49EU 20031202001652003120200165NM 2003 12 2 AALA20031133 120031011A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21376AN 25445 OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHT INOPERATIVE AT SEAT 24B. CONNECTED ELECTRICAL WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203000022003120300002NM 2003 12 3 AALA20031137 120031013A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT UNSECURE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 MIA - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT SEAT 32H. SECURED ELECTRICAL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031126001172003112600117NM 2003 11 26 ASAA0310466 120030515A5410 STRUCTURE BOEING737 737290C 138448VNM NR 1 PYLON DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND NR 1 ENGINE PYLON AT WING STATION 191 DENTED. REMOVED DAMAGED AREA AND REPAIRED PER EA. (M) 2L72 4F A16WE 20031202000142003120200014WP 2003 12 2 GTIA030731 120030821A3150 WARNING LIGHT DOUG DC9 DC982 3022082WP COCKPIT ILLUMINATED A GTIAO OTHER J WARNING INDICATION APAPPROACH 1 GL23823NK 48020 ON STABILZED APPROACH WITH FLAPS UP THE STALL INDICATION FAILURE LIGHT ILLUMINATED FOR ONE MINUTE THEN LIGHT REMAINED ON FOR REST OF THE APPROACH, ALSO HEADING LIGHT ON BOTH FMA'S WAS ILLUMINATED, HEADINGS WERE SPLIT 6-7 DEGREES BOTH LIGTHS ON STEADY. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F A6WE 20040310000072004031000007NM 2004 3 10 ASAA0310256 120030327A532065558274 FLANGE BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND EXHAUST DUCT FLANGE AT BS 312-360, STRINGER 23L-24L CRACKED. WELDED CRACK PER EA. (M) 2L72 4F RTA16WE 20040311000362004031100036NM 2004 3 11 ASAA0310113 120030307A53206546816 FLOOR SUPPORT BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 994, LEFT BUTTOCK LINE 16 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20031202000412003120200041NM 2003 12 2 USAASB03178 120031012A335030043229 SOCKET BOEING737 7374B7 1384702NM EMERGENCY LIGHT CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 MAINTENANCE REPORTED THE EXTERIOR EMERGENCY LIGHT, JUST AFT OF AFT ENTRY DOOR, INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM THE LIGHT ASSEMBLY SOCKET AND RELAMPED, P/N 1618. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031202000422003120200042NM 2003 12 2 USAASB03184 120031016A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 MAINTENANCE REPORTED THE AISLE EMERGENCY LIGHTS AT SEAT 22L INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT 22L. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031202000512003120200051 2003 12 2 USAASB03181 420031014A34257725005009 INDICATOR BOEING737 7373B7 1384580NM COCKPIT OVERHEATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19531AU3366112625 24478 CREW REPORTED THE NR 2 ADI WAS PRODUCING SMOKE. THE CIRCUIT BREAKER POPPED. MAINTENANCE REPLACED THE ADI. (M) 2L72 4F RTA16WE 20031202000752003120200075NM 2003 12 2 USAABB03192 120031017A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031202000782003120200078NM 2003 12 2 USAABB03189 120031014A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031202000892003120200089NM 2003 12 2 USAA030213 120031002A5320 ANGLE BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US40566 23992 FOUND Z-ANGLE CORRODED IN SEVERAL AREAS 1 INCH AREA OF CORROSION, L26L BS 787 TO BS 898. CORRODED LEVEL 1, TASK NR C53-202-01. REPLACED Z-ANGLE FROM BS 727D TO BS 898 PER SRM 53-60-03. (M) 2L72 4F RTA16WE 20031202001002003120200100NM 2003 12 2 USAA030206 120031004A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU36295 27145 FOUND FLOORBEAM CORRODED 24 INCHES, BS 700, LBL 50, CABIN FLOOR LEVEL. REPAIRED PER TYPICAL REPAIR 53-15-01. (M) 2L72 4F RTA2NM 20031202001032003120200103EA 2003 12 2 ASOA03523 120031020A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM PASSENGER DOOR STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM PASSENGER DOOR STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031202001152003120200115NM 2003 12 2 GAIA03112SP 120031022A5320 WEB BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076831 20184 DURING B-CHECK AT DFW, A CRACK WAS FOUND IN A LIGHTNING HOLE BY THE AFT AIRSTAIRS BS 1303. THE CRACK WAS REPAIRED PER THE B727 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031202001322003120200132EA 2003 12 2 ASOA03507 120031003A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO CLOSE FROM THE INSIDE. MAINTENANCE LUBRICATED THE OUTER DOOR HANDLE AND PERFORMED SEVERAL OPERATIONAL CHECKS WITHOUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031202001432003120200143EU 2003 12 2 ASOA03515 120031016A2120 ODOR AEROSPATR72 ATR72212 8680945EU CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11634AS 370 DURING APPROACH INTO VPS FROM ATL, THE CREW NOTICED AN ELECTRICAL SMOKE ODOR IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN VPS. MAINTENANCE INSPECTED BEHIND THE RELAY, MULTIFUNCTIONAL COMPUTER AND AVIONICS PANELS WITH NO EVIDENCE OF BURNED WIRING. GROUND RUNS WERE ALSO PERFORMED WITHOUT DUPLICATING THE ELECTRICAL SMOKE ODOR. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031202001512003120200151NM 2003 12 2 AALA20031145 120031014A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21384AA 26996 MAINTENANCE OBSERVED EMERGENCY LIGHT AT DOOR R1 INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031202001072003120200107EU 2003 12 2 ASOA03522 120031019A5343S53975102205 SUPPORT BRACKET AEROSPATR72 ATR72 EU MLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT MAIN LANDING GEAR UPSTOP UPPER SUPPORT BRACKET ON THE TOP SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPSTOP UPPER SUPPORT BRACKET IAW SRM 51-00. (M) 2H72 4T RT 20031202001362003120200136EU 2003 12 2 ASOA03505 120030927A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING A C-CHECK IN BNA, THE RIGHT SEAT TRACK FROM FS 36-39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACK FROM FS 36-39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20031202001422003120200142SO 2003 12 2 SIMA200329301 120031017A2120 ODOR EMB 135 EMB135KL 3260302SO CABIN DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21827AE 145602 DURING CRUISE FLIGHT, THE CREW REPORTED A BURNING INSULATION ODOR. AIRCRAFT WAS DIVERTED TO LIT. (M) 2L72 4F RTT00011AT 20031202001442003120200144 2003 12 2 SIMA200328803 420031014A22103621005009 CONTROL UNIT EMB 145 EMB145LR 3260212SO TAIL COMPARTMENTINOPERATIVE A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21614AE 145086 DURNG TAKEOFF AT 800 AGL CREW REPORTED PITCH TRIM ONE INOPERATIVE WITH CAS MESSAGE. WHEN AIRCRAFT WAS LEVELED BACKUP PITCH TRIM BECAME INOPERATIVE WITH NO MESSAGE. COMPLIED WITH APPROPRIATE CHECKLIST AND RECOVERED ALL PITCH TRIMS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND THE BACK UP TRIM SWITCH (P/N 145-34177-401) IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031202001542003120200154SO 2003 12 2 SIMA20326801 120030923A33507287103507 CONTROL MODULE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A SIMAO OTHER L NO TEST LDLANDING 1 SW21649PP 145234 DURING TAXI IN EMERGENCY LIGHT NOT ARMED MSG APPEARED ON EICAS NUMEROUS TIMES. R/R CONTROL MODULE ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4T RTT00011AT 20031203000092003120300009SO 2003 12 3 SIMA200329302 120031012A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BEYOND SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A, EMB SRM SRM EMB-145/1142 REV 23, 53-24-02 PAGES 201-204 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031203000232003120300023NM 2003 12 3 GAIA03117ST 120031024A53302024T3 SKIN BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND, FUSELAGE SKIN BULGE AT BS 294 TO 306 BELOW STRINGER 24RT. REF FASI N/R NR 61145, CUT OUT DAMAGED SKIN 12.5 INCH BY 4 INCH. INSTALLED FILLER 12.5 INCH BY 4 INCH 2924 T-3.050 PO NR 90096 AND DOUBLER 2024 T-3 .050 INCH PO90096 IAW B727 SRM 53-30-3. (M) 2L73 4F RTA3WE 20031203000282003120300028NM 2003 12 3 GAIA03126ST 120031024A5315BAC1498132 STRINGER BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND STRINGER 15 LT CRACKED AT BS 720B PLUS 10. REF FASI N/R NR 61424, INSTALLED DOUBLER REPAIR PER B727 SRM 53-10-5 FIG 5. (M) 2L73 4F RTA3WE 20031203000352003120300035NE 2003 12 3 WRLA200319 220030920A7311471111204 COOLER DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 3 ENGINE FAILED A WRLAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA27275WA 48631 AFTER TWO HRS INTO FLT LVL 2 HIGH OIL TEMP ON NR 3 ENG MAX TEMP 163 FOR APPROXIMATELY 3 MINUTES POWER REDUCED TO REDUCE TEMP. DEU'S WERE CHECKED FOR EXCEEDENCES NONE WERE NOTED. NR 3 ENGINE EEC CH A/B CHECKED FOR RELATED OIL SYTEM CONTROL OR SENSING FAULTS NONE RECORDED FOR LAST OR ANY 'LEGS' T/S PER FIM 79-00-03-3 WITH NO FAULTS NOTED. R7R NR 3 ENG FOC, REMOVED AND REPLACED NR 3 ENG FOC BYPASS VALVE AND SOLENOID ASSYS. REMOVED AND REPLACED NR 3 ENGINE SCAVENGE THERMOCOUPLE AND NR 3 BEARING TEMP BULB. GROUND OPERATION FOR OVER 30 MIN AT 1.2 EPR OIL TEMP 101C INSPECTED CHIP DETECTORS AND SERVICED ENGINE OIL TO FULL. REMOVED AND REPLACED FUEL OIL COOLER. (M) 2L73 4F4 FRTA22WE E24NE 20031203000442003120300044EA 2003 12 3 2003F00634 120030908A5297 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA PAX DOOR WARNINGLOOSE A FDKAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW07505MJ 10070 PASSENGER DOOR, PASSENGER DOOR WARNING MESSAGE ON EICAS WITH DOOR CLOSED. MAINTENANCE SECURED HARNESS CONNECTOR, CLEARED EICAS FAULT, OPS AND FUNCTIONAL CHECK GOOD. (M) 2L72 4F RTA21EA 20031203000682003120300068 2003 12 3 AALA20031182 420031020A3421 INDICATOR BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21366AA 25193 FIRST OFFICERS HSI DISPLAY INOPERATIVE SHORTLY AFTER TAKEOFF DISPLAY INTERMITTENT FOR .5 OF FLIGHT, INOPERATIVE REMAINDER OF FLIGHT. TROUBLESHOT FOUND FAULTY SYMBOL GENERATOR. REPLACED RIGHT SYSTEM GEN AS PER MM. ACCOMPLISHED ALL REQ CHECKS OPS CHECKED NORMAL OF EHSI SYSTEM. (M) 2L72 4F RTA1NM 20031203000732003120300073NM 2003 12 3 2003F00613 120030206A5523183A81003 TRIM TAB BOEING737 737* NM ELEVATOR DAMAGED A BJ6AK NONE O OTHER ININSP/MAINT 1 NE03127QS 30327 DURNG ELEVATOR CLEANING AS REQUIRED BY AD 2002-08-20, SOME HAIRLINE PAINT CRACKS WERE NOTICED AT THE LEFT AND RIGHT ELEVATOR TRIM TAB HINGE NR 2 AND NR 3 CUTOUTS. REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM TABS DUE TO A POSSIBLE DELAMINATION AT NR 2 AND NR 3 HINGE CUTOUTS. ELEVATOR TRIM TABS SENT TO BOEING FOR FURTHER ANALYSIS. TEARDOWN REPORTS REQUESTED. (M) 2L72 4F RTA16WE 20031203000832003120300083NM 2003 12 3 USAASB03197 120031105A2910 HYDRAULIC SYSTEM BOEING737 7373B7 1384580NM A SYSTEM CONTAMINATED A USAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA19514AU 23700 DURING GEAR RETRACTION AFTER TAKEOFF FROM PIT, MASTER CAUTION HYD LIGHT ILLUMINATED ALONG WITH BOTH 'A' SYSTEM LOW PRESSURE LIGHTS. PRESSURE IN 'A' SYSTEM READ ZERO. CREW NOTICED A STRONG HYD FLUID ODOR DURING THIS TIME. ONCE LANDING GEAR RETRACTED, ALL RETURNED TO NORMAL WITH ODOR DISSIPATING. FLT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. LANDING GEAR & FLAP EXTENSION NORMAL. NO EMERGENCY DECLARED. MAINT CHECKED FLUID LEVELS & CHECKED FOR LEAKS. RAN BOTH ENGINES & EXERCISED ALL FLT CONTROLS SEVERAL TIMES. PRESSURES REMAINED NORMAL, NO ODOR OR LEAKS PRESENT. IT WAS BELIEVED THAT THERE WAS POSSIBLE AIR IN THE HYD SYS AS AN ENGINE CHANGE WAS COMPLETED PRIOR TO FLT. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20031203000872003120300087SW 2003 12 3 2003F00624 120030809A792031080801 LINE SWRNGNSA227 SA227AC 8780603SW RT ENGINE LEAKING A BSAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM05430MA AC710B DURING CRUISE THE RT ENGINE OIL PRESS WARN LIGHT CAME ON, THIS VERIFIED WITH THE OIL PRESSURE GAUGE. CREW FOLLOWED CHECKLIST PROCEDURES AND SHUTDOWN THE ENGINE. OIL TEMPERATURE STAYED IN THE NORMAL RANGE THROUGH THE SHUTDOWN. CREW DIVERTED TO CLOSEST STATION AND LANDED WITHOUT FURTHER INCIDENT. ENGINE OIL LEAK AT THE RT ENGINE. REPLACED LINE, OPS AND LEAK CHECK GOOD. RESEARCHED LAST INSPECTION AND FOUND NO MAINTENANCE ACTION IN THIS AREA. (M) 2L72 4T RTA8SW 20031203000992003120300099NM 2003 12 3 USAASB03200 120031110A3260189929 DOWNLOCK SENSOR BOEING737 737401 1384701NM RT MLG MALFUNCTIONED A USAAA UNSCHED LANDING O OTHER DEDESCENT 1 EA19409US 23879 ON DESCENT INTO DCA FROM RSW, CREW RECEIVED A RIGHT MLG UNSAFE LIGHT WHEN GEAR HANDLE WAS PLACED IN DOWN POSITION. GEAR WAS CYCLED SEVERAL TIMES WITH SAME RESULT. CREW DECLEARED AN EMERGENCY AND DECIDED TO DIVERT TO IAD WHERE A TOWER FLYBY WAS ACCOMPLISHED TO CONFIRM GEAR WAS DOWN. ONCE CONFIRMED, FLIGHT LANDED SAFELY AT IAD. AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE INSPECTED AIRCRAFT AND FOUND IN SAFE CONDITION FOR MAINTENANCE FERRY FLIGHT TO DCA. MAINTENANCE IN DCA REMOVED AND REPLACED THE RIGHT MLG DOWNLOCK SENSOR PER MM 32-61. OPS CHECK AND INDICATION CHECK GOOD. (M) 2L72 4F RTA16WE 20031203001002003120300100SW 2003 12 3 2003F00632 120030716A79008674795 PUMP SWRNGNSA227 SA227AC 8780603SW RT ENG OIL MALFUNCTIONED A BSAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM05430MA AC710B RT ENGINE OIL PRESSURE LIGHT DIDN'T GO OUT AFTER 50 PERCENT RPM DURING START. OIL PRESSURE WAS ALSO LOW. MAINTENANCE FOUND OIL LEVEL LOW AND OIL IN THE TAIL PIPE. REPLACED REAR OIL SCAVENGE PUMP. OPS CHECK AND FLIGHT CHECK. (M) 2L72 4T RTA8SW 20031203001062003120300106EU 2003 12 3 ASOA03560 120031015A5320 ANGLE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING A C-CHECK IN BNA, THE T-ANGLE ON THE LT SIDE AT THE PASSENGER DOOR THRESHOLD BETWEEN FS 36 AND FS 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE T-ANGLE ON THE LEFT SIDE AT THE PAX DOOR THRESHOLD BETWEEN FS 36 AND FS 38 IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20031203001072003120300107EU 2003 12 3 ASOA03557 120031015A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING A C-CHECK IN BNA, THE RIGHT SEAT TRACKS FROM FS 36 TO FS 39 AND BETWEEN FS 39 AND FS 40, INCLUDING THE LEFT SEAT TRACK FROM FS 39 TO FS 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACKS FROM FS 36 TO FS 39 AND BETWEEN FS 39 AND FS 40, INCLUDING THE LEFT SEAT TRACK FROM FS 39 TO FS 41 IAW SRM 51-25-01 AND 51-25-04. (M) 2H72 4T RTA53EU 20031203001182003120300118NM 2003 12 3 USAA030227 120031104A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US51167 22959 FOUND Y-CHORD STRINGER CORRODED 1 INCH BY 4 INCH, STATION 1016 AT Y CHORD ON AFT PRESS BULKHEAD AFT SIDE. REPAIRED IAW EO 5302V112 AND DWG 65C28106. (M) 2L72 4F RTA16WE 20031203001192003120300119NM 2003 12 3 USAA030228 120031111A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU48203 23595 FOUND FLOORBEAM CORRODED 1 INCH BY 6 INCH AREA, AFT LAV FLOOR AREA BS 985.5 T-CAP. CORROSION LEVEL 1, TASK NR C53-107-02. INSTALLED REPAIR T-CAPS PER TR 53-10-05 B UPPER FLANGE REPAIR OF BAC 1518-399 EXTRUSION. (M) 2L72 4F RTA16WE 20031203001382003120300138EU 2003 12 3 A6WA200360065 120031028A5310 DOOR FRAME BAC 146 146300A 1500267EU PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31614AW E3132 AFT PAX DOOR, AFT SIDE FRAME, HAS TWO CRACKS APPROXIMATELY .75 INCH LONG NEAR DOOR SNUBBER ATTACHMENT AREA. MAINTENANCE COMPLIED WITH PERMANENT REPAIR. INSTALLED REPAIR PLATE HC521H9032-200 IAW BAE FAX BARA/AVR/6571/03-MK. (M) 2H74 4F RTA49EU 20031203001412003120300141EU 2003 12 3 A6WA200360047 120031004A5523 TAB BAC 146 146200A 1500266EU STAB DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 LEFT AND RIGHT TRIM TABS DENTS MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810003. (M) 2H74 4F A49EU 20031203001422003120300142WP 2003 12 3 AMTA200301266 120030816A5313 STRINGER LKHEED1011 10113851 5265010WP FUSELAGE GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND C2 PIT STRINGER GOUGED AND HAS ENLARGED HOLE. REPAIRED STRINGER IAW SRM 51-50-02 AND 51-21-02. (M) 2L73 4F A23WE 20031203001432003120300143EU 2003 12 3 A6WA200360044 120031002A5330 SKIN BAG BAE146BAE146300A 1500267EU FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 DAMAGE NOTED ON LEFT SIDE OF FUSELAGE DURING LIGHTNING STRIKE INSPECTION. EXIT BURN MARK LOCATED 8 INCHES AFT OF FRAME 19C BETWEEN STRINGER 21 AND 22 AT CENTER AND APPROX .375 INCH IN DIAMETER BY .010 INCHES DEPTH. MAINTENANCE BLENDED DAMAGE TO A SMOOTH MIRROR FINISH TO A DEPTH OF .010 INCH PER BAE SYSTEMS FAX BARA/AVR/6534/03-DC ET PROVED CRACK FREE. (M) 2H74 4F RTA49EU 20031203001482003120300148WP 2003 12 3 AMTA200301268 120031006A3350 LIGHT LKHEED1011 10113853 5265020WP GALLEY MALFUNCTIONED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 LEFT AFT EGRESS DIM BY GALLEY. REMOVED AND REPALCED AFT GALLEY EGRESS SECTION IAW MM 33-50-01. OPS CHECK GOOD. (M) 2L73 4F A23WE 20031203001542003120300154WP 2003 12 3 AALA20030998 120030912A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21581AA 53158 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE ON THE AFT CEILING. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001582003120300158WP 2003 12 3 GTIA030841 120030927A5310 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND MID PIT STATION 636, STATION 30-29L FRAME SUPPORT CORRODED AND STRINGER 29R-30 FRAME SUPPORT CORRODED. REMOVED SHEAR TIE. DRILL AND LOCATE NEW SHEAR TIE. INSTALLED NEW SHEAR TIE. (M) 2L72 4F A6WE 20031203001642003120300164WP 2003 12 3 GTIA030846 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT CORROSION AT FS 160-200 62 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20031203001662003120300166WP 2003 12 3 AALA20031140 120031010A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21408AA 49319 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT THE AFT STAIRWAY. REPAIRED ELECTRICAL WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001702003120300170CE 2003 12 3 DJFA200300005 120031113A274299140563 ACTUATOR CESSNA650 650 2076802CE ELEVATOR JAMMED E DJFAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA23386CW6726 1939 6500186 AT 20,000 FT THE ELEVATOR TRIM DOWN ANNUNCIATOR ILLUMINATED. THE PILOTS DISCONNECTED THE AUTOPILOT, THE AIRCRAFT PITCHED DOWN AND WAS UNABLE TO MAINTAIN LEVEL FLIGHT. PILOTS DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER PROBLEMS. 2L72 4F A9NM 20031203001732003120300173WP 2003 12 3 GTIA030871 120030928A5310 DOOR FRAME DOUG DC9 DC982 3022082WP L1 DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND L1 DOOR LOWER JAMB CORRODED AT MATING SURFACE WHERE THRESHOLD ATTACHS. REMOVED LOWER DOOR JAMB. FABRICATED NEW PART. INSTALLED L1 LOWER DOOR JAMB. (M) 2L72 4F A6WE 20031209002122003120900212EA 2003 12 9 SWIA200312562 120031029A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07597SW 7293 ON APPROACH APPROX 2 MIN AFTER SELECTING FLAPS 45 A FLIGHT SPOILERS CAUTION MESSAGE IS DISPLAYED. REMOVED AND REPLACED INBOARD PCU OF LEFT FLIGHT SPOILER. OPS AND LEAK CHECK GOOD. S/N OFF 4719. 2L72 4F RTA21EA 20031209002292003120900229EU 2003 12 9 MALA030484 120031027A302044730501 CONTROL MODULE SAAB SF340 340B 7860101EU DEICE SYSTEM MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15454XJ 340B454 DURING FLIGHT 2776, RT INTAKE LIGHT ILLUMINATED INFLIGHT. RECYCLED PER QRH AND LIGHT CONTINUED TO CYCLE. MAINTENANCE REMOVED AND REPLACED RT INTAKE DEICE CONTROL MODULE IAW ACT MM 30-21-03, OPS CHECK GOOD. P/N 44730-501, S/N OFF A00031, S/N ON A00072. 2L72 4T RTA52EU 20031208000122003120800012EA 2003 12 8 SWIA200312510 120031021A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 280 LT FLOORBEAM LBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R31113-57 2L72 4F RTA21EA 20031208000292003120800029EU 2003 12 8 1409061 120031129A7330 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE AUTOCOARSEN ILLUMINATED A UHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL17104CQ 340A104 357 DRG876684 ON 11/29/03, FLT 4624 CMH-PIT, AIRCRAFT N104CQ RETURNED TO GATE. PRIOR TO TAKEOFF WITH POWER LEVERS JUST ABOVE FLIGHT IDLE NR 2 ENGINE SUDDENLY MADE A LOUD ROARING SOUND AND ENGINE OVERTEMP LIGHT ILLUMINATED. AFTER MOVING NR 2 CONDITION LEVER TO FEATHER ENGINE INDICATIONS WERE THE NORMAL. AUTOCOARSEN ARM LIGHT ON STATUS PANEL ILLUMINATED AS WELL AS AUTOCOARSEN LIGHT ON CWP. THROUGHTOUT EVENT CONDITION LEVERS WERE AT MIN. POSITION. CTOT WAS SET FOR 108, BUT WAS NOT ON. ANTI-ICE WAS ON ANS HP BLEEDS WERE CLOSED. NO MASTER WARNING OR CAUTIONS WERE OBSERVED. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20031208001342003120800134NM 2003 12 8 2003UALA00783 120031018A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29666UA 29238 CABIN FLOORBEAM WEB CRACKED STATION 1439, LBL 25. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE DOUBLER. 2L72 4F4 FRTA1NM E24NE 20031208001562003120800156NM 2003 12 8 HNAA0300057 120031020A323282970018013 ACTUATOR DHAV DHC8 DHC8102 2809003NM MLG DEFECTIVE A HNAAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA07908HA2574412083 015 WHEN GEAR RETRACTED, AMBER LEFT DOOR REMAINED ON AND DOOR VERIFIED OPEN. REPLACED FORWARD GEAR DOOR ACTUATOR. 2H72 4T RTA13NM 20031209000172003120900017 2003 12 9 YENA200332 420031029A2565D30665309 BOTTLE AIRBUS320 A320232 3930326EU ESCAPE SLIDE DISCHARGED A YENAK NONE O OTHER ININSP/MAINT 1 EA15569JB555 1948 L2 SLIDE RAFT BOTTLE PRESSURE LOW FOUND DURING WEEKLY CHECK. REMOVED AND REPLACED L2 SLIDE RAFT IAW 25-62-44. 2L72 4F RTA28NM 20031209000292003120900029EA 2003 12 9 COMA0360469 120031024A5610NP1393226 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01964CA18125 7129 FLIGHT 5441 CO-PILOT SIDE WINDSHIELD SHATTERED. REPLACED SIDE WINDOW. 2L72 4F RTA21EA 20031209000382003120900038 2003 12 9 SWIA200312545 420031021A22156225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07585SW8528 8528 120353 RUDDER FEELS FIRM DURING TAXI. WITH RIGHT RUDDER PRESSURE, RUDDERS POP BACK INTO DIFFERENT POSITIONS. REMOVED AND REPLACED RUDDER SERVO MOTOR. REFERENCE EMB120 MM 22-10-05. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20031209000532003120900053NM 2003 12 9 UPS03441482 120031017A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, DURING RAP INSPECTION ITEM N525UP-42-03 AT BS 600-620 STR 39R-40R FWD CARGO DOOR LOWER EDGE AREA REPAIR FASTENER ROWS LESS THAN 2 ROWS. REPAIR REQ'D AT BS 600-620 S39R-40R FWD CARGO DOOR LOWER EDGE EXTERIOR PREVIOUSLY DOUBLER REMOVED AS PER SRM 51-30-02. ALL FASTENER HOLES AND DOOR SKIN REPAIR CUTOUT NDT BHFC & HFEC ACCOMPLISHED AS PER NTM PT.6 51-00-00 FIG 16 & 4. NO CRACK FOUND. DOOR SKIN REPAIR DOUBLER FABRICATED & INSTALLED AS PER SRM 52-30-06 FIG 1. 2L74 4F A20WE 20031209000582003120900058 2003 12 9 DXTA200300148 420031025A2330 AUDIO VIDEO UNIT CESSNA750 750 2076810CE CABIN FAILED E DXTAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07999QS 7500203 WHILE ON GROUND AT ASE PRIOR TO BOARDING PASSENGERS, CREW NOTICED SMOKE COMING OUT FROM THE AFT CLOSET AREA, CREW DISCHARGED FIRE BOTTLE INTO AREA. TROUBLESHOT AND FOUND AIRSHOW SYSTEM INOPERATIVE AND AUDIO VIDEO AMP BREAKER POPPED, INSPECTED MONITORS AND FOUND FOIL FROM RIGHT AFT MONITOR PINS. INSPECTED AFT CLOSET AND FOUND THE PASSENGER ENTERTAINMENT AUDIO AMPLIFIER WAS THE SOURCE OF THE SMOKE AND ODOR. REPLACED AMPLIFIER. SYSTEM NOW OPERATIONAL BUT NO AUDIO OR VIDEO. DEACTIVATED PASSENGER ENTERTAINMENT SYSTEM AND SECURED AV AMP BREAKER. 2L72 4J RTT00007WI 20031209001262003120900126WP 2003 12 9 ARWA20031002 120031016A3222 STRUT DOUG DC8 DC862 3021970WP NLG DISCHARGED A ARWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO198968U 46069 AFTER SETTING RED POWER ON TAKEOFF ROLL STICK SHAKER CAME ON, ABORTED TAKEOFF (PRIOR 40K). CHECKED PALLET WEIGHTS, LOADING, WEIGHT AND BALANCE; SERVICE NOSE STRUT IAW MM 32-21-2. PERFORMED OPERATIONAL CHECK OF STALL WARNING SYSTEM IAW DC8 MM 41-10-02, NO FURTHER FAULT. 2L74 4F 4A25 20031209001442003120900144NM 2003 12 9 QXEA200301359 120031022A5511 FRAME DHAV DHC8 DHC8202 2809007NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 FRAME NR 4 HAS A CRACKED CASTELLATION AT RIVET ON STRINGER 4RH. REPAIRED IAW DHC-8 RD 8-55-199 AND SRM 51-00-06. 2H72 4T RTA13NM 20031209001652003120900165NM 2003 12 9 03FDEA01775 120031009A5753ARC0502505 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LEFT WING O/B FLAP I/B HINGE (WING SIDE), I/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS - LEFT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031209001952003120900195WP 2003 12 9 UPS03841496 120031023A53403755842U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 1220 AT LONG 29L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3754842 AND SRM 51-1-20D, 53-2-0 FIG 2D. 2L74 4F RT4A25 20031209002402003120900240NM 2003 12 9 HNAA0300059 120031027A3320BV0330211150 SOCKET DHAV DHC8 DHC8201 2809001NM CABIN LIGHT BURNED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07986HA 421 STRONG ELECTRICAL BURNING ODOR AROUND ROW 7. 2H72 4T RTA13NM 20031209002542003120900254NM 2003 12 9 UPS03441521 120031014A533065B04118 SKIN BOEING747 747212B 1384886NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, CENTER E&E COMPT DOOR RT SIDE CUTOUT FOUND CORROSION AT BS 800-820 S46R-S47R. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT THROUGH THK, WIDTH 1.5 INCH, LENGTH 4.75 INCH EXCEED SRM 53-30-01 FIG 1 LIMITS FOR REPAIR REF RS R53-21-35091 & UPS EO B747-5330-19424-A. CIC APPLIED. NOTE: POST REPAIR INSPECTION IS REQUIRED. INITIAL INSPECTION THRESHOLD AT 10000 FLIGHTS WITH REPEAT INSPECTION EVERY 3000 FLIGHTS USING LFEC METHOD. 2L74 4F A20WE 20031209002582003120900258WP 2003 12 9 UPS03841525 120031023A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, FRAME CRACKED ACROSS UPPER FLANGE AT STATION 1440 AT LONG 25R. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE IAW EO DC8-5310-11728. 2L74 4F RT4A25 20031209002622003120900262NM 2003 12 9 AWXA200301363 120031021A532069514113 ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON ANGLE (CLIP) FORWARD SIDE OF BS 500B FRAME, ABOVE STR 26 LT. MAINTENANCE REMOVED CRACKED ANGLE FORWARD SIDE OF BS 500B FRAME, ABOVE STR 26 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-51411; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 PG 8-10 FIG 7. 2L72 4F RTA16WE 20031209002642003120900264NM 2003 12 9 AWXA200301365 120031027A53206546812189 FLOOR SUPPORT BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1003, LBL 38. MAINTENANCE REMOVED FLOOR SUPPORT FROM BS 986.5 TO BS 1006, LBL 38; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 11 SHEET 02. 2L72 4F RTA16WE 20031209002692003120900269NM 2003 12 9 AWXA200301369 120031102A53156548851 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 986.5, RBL 0.5 TO RBL 45. MAINTENANCE REMOVED UPPER T-CAP REPAIR AT BS 986.5, LBL 11 TO RBL 51; FABRICATED A NEW REPLACEMENT T-CAP; INSTALLED REPAIR PART IAW B737-200 SRM 53-10-9 FIG 2 PG 7-11. 2L72 4F RTA16WE 20031210000022003121000002NM 2003 12 10 03FDEA02076 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AJC7052-501AFT FACE FLANGE 5 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II. 2L73 4F RTA22WE 20031210000162003121000016EA 2003 12 10 QXEA200301485 120031201A2611 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09611QX 10041 PDX- FORWARD CARGO CHIMNEY HAS BROKEN MESH. REPAIRED FORWARD CARGO SMOKE DETECTOR PROTECTIVE COVER IAW CRJ AMM 26-17-03-340-801-A01. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031210000232003121000023NM 2003 12 10 CALA0300683 120031202A5514697203928 BUSHING BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916649 28910 FORWARD LEFT UPPER STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT THE BUSHING ON FORWARD EDGE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10. 2L72 4F RTA16WE 20031210000242003121000024NM 2003 12 10 CALA0300684 120031202A5514697203932 BUSHING BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916649 28910 FORWARD LEFT LOWER HORIZONTAL STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT BUSHING ON FORWARD FACE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10. 2L72 4F RTA16WE 20031210000252003121000025NM 2003 12 10 AWXA200301481 120031122A2751655280776 MODULE BOEING737 7373G7 1384595NM E/E BAY FAULTY A AWXAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 WP28322AW421552843 25400 ON DESCENT INTO PHX EN ROUTE FROM MSP FLAPS LOCKED OUT AT DETENT POSITION 15 AND NR 3 SLAT WAS STUCK IN INTERMEDIATE POSITION, AMBER INDICATION ON BOTH OVERHEAD INDICATORS, MISSED FIRST APPROACH AND LANDED ON SECOND APPROACH AT FLAP 15, NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED LEADING EDGE SLAT AND FLAP POSITION INDICATION MODULE IAW BMM 27-88-41, OPERATIONAL CHECK WAS GOOD. VENDORS PRE-TEST OF SLAT AND FLAP POSITION INDICATION ACCESSORY MODULE S/N D00748 CONFIRMED FAILURE OF UNIT. UNIT FAILED TO FULLY EXTEND SLAT NR 3. TEARDOWN OF UNIT IDENTIFIED NR 8 CIRCUIT BOARD DEFECTIVE, REPLACED NR 8 CIRCUIT BOARD AND OVERHAULED UNIT PER CMM 27-56-40, REV. 39. 2L72 4F RTA16WE 20031210000292003121000029NM 2003 12 10 AWXA200301485 120031104A532065476902 SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MINOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LEFT SUPPORT ZEE FROM BS 747E TO BS 807. MAINTENANCE REMOVED DAMAGE AFT CARGO COMPARTMENT LT SUPPORT ZEE FROM BS 747E TO BS 807; FABRICATED A NEW REPLACEMENT SUPPORT ZEE; INSTALLED REPAIR PART IAW B737-200 SRM 53-60-53, FIG 204. 2L72 4F RTA16WE 20031210000332003121000033NM 2003 12 10 MWEA030470 120031203A5241991158221 BEAM DOUG MD88 MD88 3023688NM GALLEY DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FORWARD GALLEY SERVICE DOOR BOTTOM BEAM IS CRACKED AT FORWARD END. FABRICATED AND INSTALLED REPAIR. 2L72 4F RTA6WE 20031210000472003121000047WP 2003 12 10 AALA20031298 120031119A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21232AA 49179 LAX INTERIOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 18-21 INOPERATIVE. REPLACED BATTERY PACK FOR INTERIOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210000522003121000052SO 2003 12 10 C2XA03SH479 120031204A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 SHV- DURING C-CHECK THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031202000832003120200083NM 2003 12 2 USAA030210 120030927A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48518 23319 FOUND SKIN CRACKED 2 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR OPENING. ROUTED OUT DAMAGE, INSTALLED FILLER/DOUBLER/TRIPLER PER SRM 53-10-01. (M) 2L72 4F RTA16WE 20031202001142003120200114EA 2003 12 2 A6WA200340154 120031028A5710 BEAM CNDAIRCL600 CL6002B19 1900309EA RT WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RT WING FLAP HINGE BEAM AT WS 178 FORWARD EDGE AND LOWER SURFACE HAS MUSHROOMED METAL AND GOUGES. BLENDED AREAS SMOOTH, PERFORMED EDDY CURRENT INSPECTION OF AREAS, PERFORMED ROTO/FLAP PEEN OF REPAIR AREAS AND RESTORED FINISH TO ORIGINAL CONFIGURATION IAW WVAC EO 601R-57-4318 B. (M) 2L72 4F RTA21EA 20031202001472003120200147NM 2003 12 2 GAIA03110OP 120031017A3200656021132 ACCESSORY UNIT BOEING727 727225 1384077NM E/E BAY LOOSE A GAIAO OTHER N FALSE WARNING APAPPROACH 1 SW07936PG 22441 ON APPROACH TO PHX, THE RIGHT MLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE ON GEAR EXTENTION. THE SECONDARY MLG LIGHTS INDICATED DOWN AND LOCKED. THE CREW PERFORMED A MANUAL GEAR EXTENTION WITH NO CHANGE IN GEAR INDICATION. AN UNEVENTFUL LANDING WAS MADE. RERACKED THE LANDING GEAR ACCESSORY BOX. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031202001532003120200153NM 2003 12 2 ASAA0310251 120030327A5311 FRAME BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 DURING D-CHECK, FOUND FRAME AT BS 500, STRINGER 24R-26R DENTED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031202001572003120200157WP 2003 12 2 MEX2003501 120031022A29101474252 SHUTOFF VALVE DOUG DC9 DC987 3022087WP HYD SYSTEM LEAKING A ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23204AM 49404 DURING TRANSIT CHECK DETECTED A HYDRAULIC LEAK AT THE SPOILER SHUTOFF VALVE, RIGHT SIDE. VALVE WAS REPLACED IAW MM 29-10-26, TESTS CORRECT. DURING OVERNIGHT SERVICE SYSTEM WAS TESTED IAW MM 29-10-26, ALL CORRECT. (M) 2L72 4F RTA6WE 20031203000052003120300005NM 2003 12 3 AALA20031110 120031006A33503015643 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21389AA 27449 DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROW 38H. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203000072003120300007SO 2003 12 3 SIMA200329303 120031015A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 DURING AN MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 23, CHAPTER 53-21-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20031203000122003120300012NM 2003 12 3 GAIA03131ST 120031024A5347BAC1520792 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND SEAT TRACK CORRODED BS 580 TO 690 AT LBL 45.6. REF FASI N/R NR 61432, REPLACED DAMAGED SEAT TRACK PER B727 53-10-5 FIG 7. (M) 2L73 4F RTA3WE 20031203000192003120300019NM 2003 12 3 GAIA03118ST 120031024A53302024T3 SKIN BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 362 ABOVE STRINGER 21 RT. REF FASI N/R NR 61146, CUTOUT DAMAGE, INSTALLED EXTERNAL DOUBLER 6 INCH BY 9 INCH 2024 T3, PO NR 90024 IAW B727 SRM 53030-3 PAGE 14D, 14E. (M) 2L73 4F RTA3WE 20031203000332003120300033NM 2003 12 3 GAIA03124ST 120031024A5313BAC1498132 STRINGER BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND MAIN CABIN STRINGER 15 LT CRACKED AT BS 720B. REF FASI N/R NR 61420, ACCOMPLISHED ANGLE DOUBLER REPAIR IAW B727 SRM 53-10-3 FIG 5. (M) 2L73 4F RTA3WE 20031203000432003120300043NM 2003 12 3 GAIA03151ST 120031024A53117075T6 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME DENTED IN RADIUS BS 720A ABOVE STR 17 LT. REF FASI N/R NR 61834, CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER 8 INCH BY 4 INCH AND INSTALLED REPAIR DOUBLER 8 INCH BY 4 INCH PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20031203000592003120300059EA 2003 12 3 2003F00622 120030730A5610NP1393225 WINDSCREEN CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A FDKAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07510MJ 10101 RETURNED TO FIELD WITH THE LT COCKPIT WINDOW SHATTERED. MAINTENANCE REPLACED THE WINDOW. (M) 2L72 4F RTA21EA 20031203000722003120300072 2003 12 3 AALA20031162 420031019A2565 GIRT BAR BOEING767 767223 1385123NM L2/R2 DOOR OUT OF RIG A AALAK NONE O OTHER ININSP/MAINT 1 SW21335AA 22333 MAINTENANCE OBSERVED DURING THE ACCOMPLISHMENT OF B-CHECK CARD 2403, THE L2 DOOR SLIDE S/N A-4018 AND R2 DOOR SLIDE S/N A-5725 GIRT BARS BEING IN THE SHIPPING POSITION, RATHER THAN BEING ATTACHED TO THE GIRT BAR CARRIER. THE L2 AND R2 SLIDE WERE CORRECTED PER THE MAINTENANCE MANUAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203000912003120300091SW 2003 12 3 2003F00625 120030813A3150 WARNING LIGHT FRCHLDSA227 SA227DC 3377521SW COCKPIT NO INDICATION A BSAACD ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TOTAKEOFF 1 NM05854LS DC854B NR 1 CAWI LIGHT DID NOT COME ON AT TAKEOFF, TORQUE RISE WAS NOTED. BLEED AIR OUT OF SYSTEM. OPS CHECKED OK. (M) 2L72 4T RTA18SW 20031203000922003120300092SW 2003 12 3 2003F00626 120030702A8200 WATER INJECTION SWRNGNSA227 SA227AC 8780603SW ENGINE FAILED A BSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM05430MA 710B CAWI DID NOT FIRE ON TAKEOFF ROLL. LIGHTS OPERATE NORMALLY BUT NO RISE IN PERCENT TORQUE. DEFERRED CAWI SYSTEM. NO DEFECTS NOTED WHEN AIRCRAFT CAME IN FOR REPAIR. (M) 2L72 4T RTA8SW 20031203001222003120300122EA 2003 12 3 A6WA200340130 120030902A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER FAILED A A6WAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL31404AW 7294 CAPTAINS SIDE PILOTS 'ROLL' LIGHT ILLUMINATED WITH ASSOCIATED ADVISORY MESSAGE ON ED2 ON ARRIVING IN GATE. MESSAGE CLEARED WITH SECU BITE TEST. PERFORMED SYSTEM TEST AND FOUND INTERNAL SECU (SPOILER ELECT CONTROL UNIT) FAILURE. REPLACED NR 1 SECU IAW AMM. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20031210000562003121000056NM 2003 12 10 03FDEA02092 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 INTERCOSTAL STIFFENERS (AJC7581-11 & AJC7581-19) FOUND WITH 02 EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 INTERCOSTAL STIFFENERS AJC7581-11 & AJC7581-19, 02 EA. CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20031210000662003121000066NM 2003 12 10 UPS03441577 120031127A5414 SKIN BOEING747 747212B 1384886NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: PFLT CRACK NR 3 ENGINE PYLON OUTBOARD SIDE AT PYLON EMERGENCY DRAIN TUBE. REPAIRED CRACK IAW 54-34-03 FIG 7. 2L74 4F A20WE 20031210000702003121000070NM 2003 12 10 03FDEA01969 120031121A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 2 O/B FLANGE SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031210000742003121000074WP 2003 12 10 AALA20031318 120031124A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21567AM 53293 ORD CEILING EMERGENCY LIGHTS OVER ROWS 29D AND 28D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS OVER ROWS 29D AND 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031210000772003121000077NM 2003 12 10 AALA20031300 120031119A3350 CONNECTOR BOEING757 757223 1384957NM CARGO BAY LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21674AN 29424 MIA AFT CARGO DOOR EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR DISCONNECTED AT BATTERY PACK. REPOSITIONED AND SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031210000842003121000084NM 2003 12 10 SWAA032617 120031127A335020131A BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED PM CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20031209000442003120900044NM 2003 12 9 373PA0022 120031028A335087310022 LIGHT BOEING737 7373Y0 1384671NM PAX DOOR INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 L1 DOOR EMERGENCY EXIT IDENTIFIER ANNUNCIATOR STROBE LIGHT INOPERATIVE. REPLACED L1 DOOR EXIT ANNUNCIATOR AND OPS CHECKS NORMAL. 2L72 4F RTA16WE 20031209000702003120900070NM 2003 12 9 SWAA032370 120031027A53406557463 BRACKET BOEING737 737317 138447PNM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM. 2L72 4F RTA16WE 20031209001092003120900109 2003 12 9 SWAA032338 420031023A2565D31354 SLIDE BOEING737 7373G7 1384595NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031209001242003120900124NM 2003 12 9 AWXA200301338 120031023A532069353521 STRINGER CLIP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 380, STR 25 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 380, STR 25 LT IAW B737-300 SRM 51-30-02, PG 2-3, & 8-10. 2L72 4F RTA16WE 20031209001892003120900189WP 2003 12 9 UPS03841490 120031025A53403755827501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 270 LONG 32R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755827 AND SRM 51-1-20D. 2L74 4F RT4A25 20031209001912003120900191WP 2003 12 9 UPS03841492 120031022A53403649114U FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, RIGHT FUSELAGE FITTING IS CRACKED AT STA 925 AT RBL 68. REMOVED AND REPLACED FITTING IAW DWG 36491144 AND SRM 51-1-20D. 2L74 4F RT4A25 20031210000272003121000027NM 2003 12 10 AWXA200301483 120031114A541265800371 FIREWALL BOEING737 737277 1384570NM NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 LCQ - MAJOR REPAIR - DURING C-14 CHECK 5 EACH CRACKS WERE FOUND ON NR 1 ENGINE PYLON FORWARD FIREWALL. MAINTENANCE PERFORMED WELD REPAIR ON FORWARD FIREWALL PAN ASSEMBLY IAW AWA ER 15-5412-03322-SS1. 2L72 4F RTA16WE 20031210000382003121000038SO 2003 12 10 C2XA03CL188 120031122A2530 ODOR EMB 145 EMB145XR SO COFFEEMAKER DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2727152 145759 CLE FLIGHT 3320 THE CREW REPORTED SMOKE AND BURNING RUBBER SMELL EMITTING FROM COFFEE POTS. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL 25-60-02/3. 2L72 4F RT 20031210000492003121000049EA 2003 12 10 COMA0360517 120031127A3232AIR917103 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01929CA23327 7035 FLIGHT 5745 AFTER TAKEOFF AND GEAR RETRACTION RECEIVED A NLG DISAGREE CAUTION WITH A NOSE GEAR DOOR OPEN MESSAGE. AIRCRAFT RETURNED TO DEPARTING CITY (CVG). REPLACED THE NLG DOOR ACTUATOR. 2L72 4F RTA21EA 20031210000572003121000057NM 2003 12 10 QXEA200301515 120031203A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX - CORROSION AND PITTING ON SKIN SURFACE AROUND BOLT HOLES FOR THE LOWER TCAS ANTENNA, UNDER FUSELAGE AT STATION X501.000. REPAIRED IAW DHC-8 SRM 51-20-16. 2H72 4T RTA13NM 20031210000692003121000069NM 2003 12 10 03FDEA01970 120031121A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 1 I/B FLANGE SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031210001122003121000112NM 2003 12 10 AWXA200301505 120031124A335020131A BATTERY PACK BOEING737 7373G7 1384595NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28305AW 24012 MCN - EEL - DURING C-15 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 18 THRU 23 LT WOULD NOT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031210001142003121000114SO 2003 12 10 C2XA03BT111 120031122A2810 SWITCH EMB 135 EMB135LR 3260305SO REFUELING PANEL OUT OF POSITION A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW2716510 145251 CREW REPORTED, FUEL NR 1 LOW LEVEL MESSAGE CAME ON INFLIGHT ON ARRIVAL INTO EWR. NR 1 FUEL QTY INDICATOR SHOWS ZERO FUEL. DECLARED EMERGENCY AND LANDED UNEVENTFULLY IN EWR. MAINTENANCE FOUND REFUELING SWITCH TO BE IN THE OPEN POSITION ON THE REFUELING PANEL. CLOSED SWITCH OPS, CHECKED GOOD IAW EMB135 AMM 28-11-00, INDICATION CHECKS GOOD. 2L72 4F RTT00011AT 20031210001162003121000116WP 2003 12 10 AALA20031321 120031121A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21599AA 53289 ORD FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5 FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031210001192003121000119NM 2003 12 10 MWEA030468 120031203A532099525215 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RIGHT FLOOR PANEL BETWEEN SEAT TRACK NR 5 AND NR 6 FROM STATION 465-541 HAT CHANNEL IS CRACKED. FABRICATED AND INSTALLED NEW HAT CHANNEL. 2L72 4F RTA6WE 20031210001242003121000124EU 2003 12 10 QXEA200301487 320031129A6140 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM ROTOL R408 CR4086123F17EU CABIN MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09400QX 4030 GEG- ON FLIGHT 2371 DURING AUTOFEATHER TEST, NR 1 ENGINE SHOWED FAILED MESSAGE. POWER DOWN AND BACK UP. PERFORMED AUTOFEATHER TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP17BO 20031210001252003121000125EA 2003 12 10 COMA0360518 120031127A3221 PIVOT CNDAIRCL600 CL6002B19 1900309EA NLG LACK OF LUBE A COMAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SO01929CA 7035 FLIGHT 5689 AFTER TAKEOFF AND GEAR RETRACTION THE NLG INDICATED DOWN AND LOCKED WITH THE HANDLE IN THE UP POSITION. AIRCRAFT RETURNED TO DEPARTING CITY (CVG). CLEANED AND LUBRICATED THE NLG PIVOT POINTS. 2L72 4F RTA21EA 20031210001362003121000136NM 2003 12 10 AALA20031344 120031130A3397 WIRE BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21385AM 27059 SFO EMERGENCY LIGHTS AT SEATS 5HJ INOPERATIVE. REINSTALLED LOOSE WIRE FOR EMERGENCY LIGHTS AT SEATS 5HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA1NM 20031210001372003121000137WP 2003 12 10 AALA20031345 120031130A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219625W 53595 DFW OVERHEAD EMERGENCY EXIT LIGHT BETWEEN ROWS 18-20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXIT LIGHT BETWEEN ROWS 18-20. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA6WE 20031210001452003121000145NE 2003 12 10 AALA20031355 220031126A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT MALFUNCTIONED A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW219621A 53592 DFW T1357/26 EN ROUTE DFW-TUS LEFT HAND ENGINE LOW OIL PRESSURE. CREW REDUCED POWER OF ENGINE TO IDLE. LANDED ELP WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20031210001642003121000164WP 2003 12 10 AALA20031383 120031204A335060030451 BATTERY DOUG DC9 DC982 3022082WP COCKPIT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21294AA 49306 DTW COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR COCKPIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001652003121000165NM 2003 12 10 AALA20031189 120031027A2910 COUPLING BOEING757 757223 1384957NM HYD SYSTEM SPLIT A AALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21659AA 24617 ENROUTE KIN-MIA LOST LEFT HYDRAULIC SYSTEM QUANTITY. DECLARED EMERGENCY AND LANDED MIA WITHOUT INCIDENT. REPLACED LT PUMPS AND FILTERS AS WELL AS SPLIT HYDRAULIC COUPLING AT TOP OF LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (SW21200401055) 2L72 4F RTA2NM 20031210001772003121000177NM 2003 12 10 CALA0300677 120031127A5280113A82003 DOOR BOEING737 737824 13844BZNM LT MLG CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724224 28933 INSPECTION FOUND A .1250 INCH CRACK IN LT MLG DOOR. THE DOOR WAS REPAIRED IAW ECRA 5280-01311. 2L72 4F RTA16WE 20031210001782003121000178NM 2003 12 10 CALA0300678 120031129A553465538344 FITTING BOEING737 737524 1384721NM VERTICAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716648 28909 INSPECTION FOUND VERTICAL STABILIZER RT REAR SPAR FORWARD DRAG ANGLE FITTING CORRODED AT OB MOUNTING BOLT AREA. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20031210001802003121000180NM 2003 12 10 CALA0300610 120031027A53156545810 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912318 23369 CABIN FLOORBEAM (BS 312) TOP CHORD CORRODED AT FASTENER HOLES. INSTALLED NEW FLOORBEAM UPPER CHORD IAW SRM 53-10-51. 2L72 4F4 FRTA16WE E2GL 20031203001322003120300132EU 2003 12 3 A6WA200360045 120031006A5730 SKIN BAG BAE146BAE146200A 1500266EU LT & RT WING DELAMINATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 DENTS ON THE LEFT AND RIGHT WING NOW SHOWING SIGNS OF DELAMINATION. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810001. (M) 2H74 4F RTA49EU 20031203001352003120300135EA 2003 12 3 REXA03006 120031010A2613356024310 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA RT PYLON MALFUNCTIONED A REXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO258409N 7409 14TH STAGE BLEED AIR LIGHT IN FLIGHT, QRH FOLLOWED, UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE RIGHT PYLON DETECTION LOOP. (M) 2L72 4F RTA21EA 20031203001442003120300144EA 2003 12 3 A6WA200340158 120031031A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31452AW 7835 FUSELAGE SKIN DAMAGED AT FS 621 BETWEEN STRINGERS 22L AND 25L. RE-CONTOURED SKIN, PERFORMED EDDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-4350A. (M) 2L72 4F RTA21EA 20031203001472003120300147NM 2003 12 3 AMTA200301327 120031027A335020121 BATTERY BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11522AT 29330 R3 EXTERIOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY M374 IAW MM 33-51-00. (M) 2L72 4F RTA2NM 20031203001552003120300155WP 2003 12 3 AALA20031129 120031008A33501001191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21486AA 49679 OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE L1 DOOR EXIT. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001572003120300157WP 2003 12 3 GTIA030845 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200-255 22 INCHES LBL. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20031204000172003120400017WP 2003 12 4 GTIA030875 120030923A5310 BEAM DOUG DC9 DC982 3022082WP CARGO DOOR FRAMECORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND MID CARGO DOOR JAMB BEAM CORRODED AT FS 636-693. REMOVED JAMB BEAM. LOCATE AND DRILLED NEW JAMB BEAM. INSTALLED NEW JAMB BEAM. (M) 2L72 4F A6WE 20031204000272003120400027EU 2003 12 4 A6WA200360061 120031028A5523 SKIN BAG BAE146BAE146200A 1500266EU ELEV TRIM TAB DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31291UE E2084 FOUND DENTS LEFT AND RIGHT ELEVATOR SERVO AND TRIM TABS, LEFT AND RIGHT TRAILING EDGE PANELS RIB 14A TO 15, LEFT WING INBOARD CENTER, OUTBOARD SPOILERS, RT WING INBOARD, CENTER, SPOILERS. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 1698-6910003. (M) 2H74 4F RTA49EU 20031204000312003120400031NM 2003 12 4 AMTA200301321 120031024A3350 SOCKET BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11515AT 27598 EGRESS PATH INOPERATIVE 1 THROUGH 5 SEATS, POOR CONNECTION AT SEAT 5. RESECURED SOCKET AT LIGHT 5 AND RELAMPED SEAT 1. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20031204000362003120400036NM 2003 12 4 AMTA200301262 120031003A2612 FIRE DETECTOR BOEING757 75723N 1384973NM LT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11523AT 30232 LEFT ENGINE FIRE LP 1. PERFORMED FIM PROCEDURE 26-11-00, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20031204000542003120400054WP 2003 12 4 AALA20031053 120030922A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21436AA 49454 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031204000632003120400063NM 2003 12 4 03FDEA01757 120031009A5753 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT WING I/B FLAP LEADING EDGE O/B FLAP VANE TRACK CAVITY FOUND CHAFE MARKS ON RIB. 2L73 4F RTA22WE 20031204000722003120400072NE 2003 12 4 GLBA2003140 320031014A6110 RING BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE PROPELLER MISMANUFACTURED A GLBAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM03251GL UE251 TORQUE WAS HIGH, REMOVED PROPELLER, INSPECTION FOUND INTERNAL SPACER RING NOT DRILLED AND RESULTED IN A PIN NOT BEING INSTALLED AND SPACER RING BACKED-OFF CAUSING TORQUE ISSUE. LAST OVERHAUL WAS AT HARTZELL TSO 438.0. 2L72 4T RTA24CE 5 CP10NE 20031204000932003120400093WP 2003 12 4 UPS03841404 120030909A5313975491318 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, LONGERON 36 CORRODED AT STA 220-240 FWD PIT. REMOVED CORR IAW DC8 SRM 51-1-8 ORIG .080 INCH, REMOVED .027 INCH, REMAINING .053 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE IAW DC8 SRM 53-2-2. RECEIVED LONG SECTION, LOCATED, DRILLED, & TRIMMED IAW DC8 SRM 53-2-2. ALODINED & PRIMED AND INSTALLED SPLICE, LONGER SECTION AND -33 SPLICE IAW DC8 SRM 51-1-8, 53-2-2, & DAC DWG 9754913. 2L74 4F RT4A25 20031203000012003120300001WP 2003 12 3 MEX2003497 120031019A3231 LINKAGE DOUG DC9 DC983 3022083WP MLG DOOR OUT OF ADJUST A ASMFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW23838AM 49397 AIRCRAFT RETURNED DUE TO A STRONG VIBRATION WITH NOSE LANDIG GEAR UP AND NORMAL INDICATIONS. TECHNICAL PERSONNEL DETECTED BOTH NOSE LANDING GEAR FORWARD DOORS OPENED. MECHANISM WAS CHECKED IAW MM 32-22-01, FINDING IT CORRECT. RIGHT NOSE LANDING GEAR LINKAGE DOOR WAS ADJUSTED IAW MM 32-22-01. OVERWEIGHT INSPECTION WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. (M) 2L72 4F RTA6WE 20031203000312003120300031NM 2003 12 3 GAIA03128ST 120031024A5347 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND CABIN SEAT TRACK CORRODED BS 870 TO 1070, LBL 45.5. REF FASI N/R NR 61426, REPLACED SEAT TRACK PER B727 SRM 53-10-5 FIG 1. (M) 2L73 4F RTA3WE 20031210001932003121000193NM 2003 12 10 03FDEA01745 120031015A5320 FITTING BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE53392 20935 STA 1183 STR 20L UPPER AND LOWER TERMINATING FITTINGS HAVE CORROSION AND GOUGES AT FASTENER HOLES. REMOVED AND REPLACED STRINGER 20 TERMINATING FITTINGS IAW B727 SRM 51-30-2 AND 727-200 AMM 20-80-001-2 2L73 4F RTA3WE 20031210001972003121000197NM 2003 12 10 03FDEA01874 120031105A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 N00817) FWD LWR CARGO FRAME DENTED AT STA 520 STR 22L TO 25L ** SD ** COMING 2L73 4F RTA3WE 20031210002072003121000207NM 2003 12 10 UPS03641440 120031003A5330 SKIN BOEING767 767300 1385204NM FUSELAGE PUNCTURED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01311UP 27741 INSPECTION TYPE:SPV PUNCTURE TO FUSELAGE SKIN ON RT SIDE OF THE FWD CARGO DOOR BETWEEN STR 25R AND 26R AT BS 460. TRIMMED OUT DAMAGE REPAIRED SKIN IAW SRM 53-00-01 FIG 212 AND FIG 2 OF ER 03-3883. 2L72 4F RTA1NM 20031210002102003121000210WP 2003 12 10 UPS03841542 120031023A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSP TYPE:C2 STATION 1755 LONG 14R IS CRACKED REMOVED LONGERON SECTION STATION 1740 TO 1760,FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE IAW SRM 53-2-2 FIG 10 2L74 4F RT4A25 20031209001412003120900141EA 2003 12 9 QXEA200301316 120031001A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 TWO CHAFE MARKS ON FORWARD CARGO DOOR INNER SKIN FORWARD AND AFT LOWER CORNERS. REPAIRED IAW HORIZON AIR EA R-52-122. 2L72 4F RTA21EA 20031209001622003120900162NM 2003 12 9 03FDEA01718 120031008A5753ARC198413 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B LUG AND HOLE FOUND CORRODED. LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031209001732003120900173WP 2003 12 9 ABXA030413 120031015A5320991224645 ANGLE DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 CRACK IN FRAME ATTACH ANGLE AT STA 1038 ABOVE LONGERON 18 LT. REPAIRED ANGLE IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20031209001972003120900197NM 2003 12 9 QXEA200301382 120031101A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09347PH3051 416 480 FIRST AND THIRD CEILING LIGHTS AND AFT EGRESS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK RS3-OP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031209002062003120900206SO 2003 12 9 SWIA200312556 120030930A5320 CLIP EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07565SW 120340 SKIN CLIP CRACKED AT FRAME 9, BELOW LEFT DV WINDOW. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED LEFT FRAME 9 IAW SB 120-53-0073. 2L72 4T RTA31SO 20031209002182003120900218NM 2003 12 9 CALA0300614 120031031A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 INSPECTION FOUND STRINGER 28L CORRODED AT STA 500D. THE CORROSION WAS REMOVED AND THE AREA WAS REPAIRED IAW SRM 53-30-12. 2L72 4F RTA16WE 20031209002452003120900245NM 2003 12 9 UPS03241526 120031018A5340 FITTING BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, TO REMOVE RT BS 930 FITTING, PARTIAL SHELF ATTACHING BS 930 TO 940 MUST BE REMOVED, ON REMOVAL OF PARTIAL SHELF AT STR 14 BS 930-940, 3 SUSPECT CRACKS WERE DETECTED ON MOST UPPER HORIZONTAL FLANGE (FWD SIDE) ON BS 940 FITTING. REPAIR CARRIED OUT IAW SRM 51-20-2 & BOEING DRAWING 65C15732. 2L73 4F A3WE 20031209002672003120900267NM 2003 12 9 AWXA200301367 120031022A5320654529623 SPLICE BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR ATTACH STRAP BS 771, STR 26 LT TO STR 26 RT. MAINTENANCE REMOVED DAMAGED FLOOR ATTACH STRAP BS 771, STR 26 LT TO STR 26 RT; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02. 2L72 4F RTA16WE 20031209002722003120900272NM 2003 12 9 03FDEA01887 120031107A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 WHILE WORKING CARD N01482, FOUND CORROSION ON FLOORBEAM, STA 328 LBL 23 WL 208. 2L73 4F RTA3WE 20031210000602003121000060SO 2003 12 10 C2XA03TY197 120031124A553414504980602 FITTING EMB 145 EMB145 3260210SO VERTICAL STAB DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 TYS AFTER REAMING THE RT VERTICAL STAB SPHERICAL BEARING CASTING, THE HORIZ STAB FAIL THE DIHEDRAL CHECK. REMOVED AND REPLACED THE RT VERTICAL HINGE FITTING IAW EC 5510-01067 C/W BACKLASH CHECK IAW EMB 145 AMM27-40-00; C/W INCIDENCE AND DIHEDRAL CHECKS IAW EMB 145-AMM 51-50-01; ALSO C/W A TEST FLIGHT TO ASSURE ALL FLIGHT CONTROLS WERE IN A SAFE MANNER. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031210000782003121000078EU 2003 12 10 AALA20031301 120031120A33509EL40434201 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW211414D 11377 ORD EMERGENCY FLOOR LIGHTING STRIP AT ROW 16 PULLED LOOSE. REPAIRED EMERGENCY FLOOR LIGHTING STRIP AT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20031210000802003121000080NM 2003 12 10 AALA20031303 120031119A2751S256A40450 TRANSMITTER BOEING737 737823 13844BZNM T/E FLAP FAULTY A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21968AN 30095 LAX T2196/19 EN ROUTE DFW-SNA FLAP/SLAT DISAGREE. PLACED FLAP HANDLE TO 10 DEGREES AT 180 KNOTS FLAPS STUCK AT 5 DEGREES. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT FLAP POSITION TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20031203000342003120300034NM 2003 12 3 GAIA03130ST 120031024A5347BAC1503100122 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND SEAT TRACK CORRODED BS 480 TO 690 AT LBL 24.75. REF FASI N/R 61431, REPLACED DAMAGED SEAT TRACKPER B727 SRM 53-10-5 FIG 1. (M) 2L73 4F RTA3WE 20031203000392003120300039NM 2003 12 3 AMTA200301303 120031016A2751 WARNING LIGHT BOEING757 75733N 1384931NM TE FLAPS ILLUMINATED A A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11551TZ 32585 AFTER TAEKOFF ON FLAP RETRACTION FROM 20 DEGREE TO 5 DEGREE GOT EICAS MSG 'TE FLAP ASSYM-FLAPS STOPPED AT 10 DEGREE. REMOVED AND REPLACED FLAP/SLAT ACCESSORY MODULE IAW MM 27-59-11-4, OPS CHECK NORMAL. REF FIM 27-51-00 FIG 106 BLOCK 1 AND FIM 27-51-00 FIG 119 SHEET 2 BK 45. (M) 2L72 4F RTA2NM 20031203000782003120300078EU 2003 12 3 A6WA200360054 120031015A5330 SKIN BAC 146 146200A 1500266EU FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31183US E2043 RIGHT FUSELAGE DENTS MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830002. (M) 2H74 4F A49EU 20031203000792003120300079NM 2003 12 3 USAASB03175 120031004A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19784AU 25023 MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS, AT ROWS 24 AND 25, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031203000822003120300082SW 2003 12 3 2003F00619 120030802A5210 GATE FRCHLDSA227 SA227DC 3377521SW PAX DOOR DIRTY A BSAAO OTHER N FALSE WARNING CLCLIMB 1 NM05853LS DC853B CARGO DOOR WARNING LIGHT CAME ON IN FLIGHT, CLIMBING THROUGH 17,000 FT, WITH 4.0 PSID, CREW RETURNED TO STATION. LIGHT WENT OUT ABOUT 600 FEET ABOVE FIELD ELEVATION. DOOR CLOSING PROCEDURES OR DOOR IS HARD TO CLOSE. MAINTENANCE INSPECTED THE CARGO DOOR AND LATCHING SYSTEM. FOUND NO OBVIOUS DEFECTS. CLEANED, LUBED, AND CHECKED CLICK CLACKS AND SWITCHES. PERFORMED GROUND RUN AND PRESSURIZED AIRCRAFT TO 5 PSID. NO PROBLEMS WERE FOUND. (M) 2L72 4T RTA18SW 20031203001312003120300131WP 2003 12 3 AMTA200301256 120030923A5320 THRESHOLD LKHEED1011 1011385115 5265015WP GALLEY CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 193B1230 FOUND LOWER 5 GALLEY, BOX BEAM THRESHOLD TO GALLEY LIFT HAS SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES LBL 26 - RBL 26. REMOVED AND REPLACED BOX BEAM PER MANUAL 51-40-02. (M) 2L73 4F A23WE 20031204000132003120400013 2003 12 4 GTIA030877 420031101A2565 GIRT BAR DOUG DC9 DC983 3022083WP R1 DOOR SLIDE OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 LGA - R1 DOOR GIRT BAR HOLDER WILL NOT HOLD GIRT BAR. ADJUSTED GIRT BAR HOLDER, OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20031204000322003120400032EU 2003 12 4 A6WA200360062 120031028A5530 ANGLE BAC 146 146200A 1500266EU VERTICAL STAB CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31291UE E2084 FOUND VERTICAL STAB CLOSING ANGLE RT HAS CRACK. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910004. (M) 2H74 4F A49EU 20031204000942003120400094WP 2003 12 4 UPS03841405 120030909A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, FRAME CORRODED AT STA 260 BETWEEN LONGERONS 35L-35R. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE SECTION OF FRAME IAW DC8 SRM 53-2-0. FABBED FRAME, 4 EA RPR ANGLES, & STRAPS IAW DC8 SRM 51-1-1, 53-4-1, DC8 TEMP REV 53-125, DRILLED & TRIM IAW DC8 SRM 51-1-20D, 53-2-0 & TEMP REV 53-125. ALODINED & PRIMED AND INSTALLED IAW DC8 SRM 51-1-8 & 51-1-20D. 2L74 4F RT4A25 20031204000952003120400095WP 2003 12 4 UPS03841406 120031001A5313975491318 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, LONGERON 35L CORRODED AT STA 280-300 FWD PIT. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE L-ANGLE IAW DC8 SRM 53-2-2. RECEIVED LONG SECT, LOCATED, DRILLED & TRIMMED LONG SECTION & -31 SPLICES IAW DC8 SRM 53-2-2. ALODINED, PRIMED AND INSTALLED LONGERON SECTION AND SPLICE IAW DC8 SRM 51-1-8 & 53-2-2. 2L74 4F RT4A25 20031204000972003120400097WP 2003 12 4 UPS03841408 120030911A57403645611U ATTACH FITTING DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, NR 4 ALT HAS FWD BOOST PUMP MOUNT FITTING CRACKED AT S-59. REMOVED AND REPLACED FITTING WITH NEW FITTING PO SP0938702 IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20031204001052003120400105WP 2003 12 4 UPS03841423 120030918A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, CANTED FRAME AT FS 1746 AT LONG 34R FWD SIDE OF FRAME HAS CORROSION. FRAME SPLICE ANGLES CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0. FABBED NEW CHANNEL IAW DC8 DWG 56212148, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW UPS DC8 SRM 51-1-20. 2L74 4F RT4A25 20031204001102003120400110WP 2003 12 4 UPS03841428 120030919A53476015176 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, SEAT TRACK -E- FROM FS 1000-1300 IS CORRODED. REMOVED CORROSION ON SEAT TRACK IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED REPAIR SPLICES AND SEAT TRACKS IAW DC8 EO D C8-5320-5167 AND DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0, REINSTALLED FLOOR BOARDS RBL 36 AND 27 IAW DC8 SRM 51-3-0 STA 1000-1380. 2L74 4F RT4A25 20031204001172003120400117WP 2003 12 4 UPS03841435 120030929A5321 FLOOR PANEL DOUG DC8 DC873F 302199FWP FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C3 FLOOR PANEL CORRODED FS 1300 LBL 12. CUT AND REMOVED SECTION OF FWD PANEL, FABBED NEW SECT OF FLOOR PANEL AND SPLICE PLATES ALL IAW DC8 SRM 53-2-3 FIG 9. ALODINED & PRIMED IAW DC 8 SRM 51-1-8, INSTALLED NEW SECT OF FLOOR PANEL AND SPLICE PLATES IAW DC8 SRM 53-2-3 FIG 9. CUT OUT CORROSION ON AFT PANEL, FAB REPAIR DOUBLER & FILLER, ALODINED, PRIMED & INSTALLED IAW DC8 SRM 53-2-3, 51-1-8. 2L74 4F RT4A25 20031204001192003120400119WP 2003 12 4 UPS03841438 120031002A5347DC853B003501 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C3 AFT RT SEAT TRACK CORRODED AT STA 1680 I/B LOWER SIDE BLENDED SEAT TRACK TO 100 PERCENT MAT LOSS AND FOUND OUT OF LIMITS IAW DC8 53-2-0 FIG 1F. DRILLED, LOCATED NEW SEAT TRACK IAW DC8 SRM 51-1-24 AND 5 3-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK AND SPLICE IAW DC8 SRM 51-3-0 AND 53-2-3. REINSTALLED FLOOR PNL F216 AND ADJACENT PLANKS IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20031204001212003120400121NM 2003 12 4 AWXA200301262 120031016A33506104789 BATTERY PACK BOEING737 737277 1384570NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING INSPECTION THE L-2 & R-2 DOOR EMERGENCY EXIT EXTERIOR LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT ESCAPE SLIDES BATTERY BACK IN THE AFT CARGO COMPARTMENT BS 920 IAW BMM 33-51-71, OPERATIONAL CHECK C/W IAW BMM 33-51-11. 2L72 4F RTA16WE 20031204001362003120400136NM 2003 12 4 C1HA200397014 120031019A3350 POWER SUPPLY BOEING727 727270 138408PNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 FOUND EMERGENCY EXIT LIGHT (FLOOR TRACK) INOP FROM ROWS 12 TO 20. REMOVED & REPLACED POWER SUPPLY AT STATION 440. REF MM CH 33-50-23, OPS OK. 2L73 4F RTA3WE 20031204001412003120400141EA 2003 12 4 COMA0360462 120031016A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01821CA 7420 FLIGHT 5248 FLAPS FAIL WARNING WHEN SELECTED TO 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031204001492003120400149WP 2003 12 4 03FDEA01766 120031018A5754ARB14682 LINK DOUG DC10 DC1010 3022110WP ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 SLATS NR 14 SLAT TRACK INBOARD LINK (RT WING) WEAR REWORK P/N ARB1468-2. COMPLIED WITH EA 8-5750-73213 WINGS - SLATS NR 14 SLAT TRACK INBOARD LINK (RT WING) WEAR REWORK P/N ARB 1468-2. 2L73 4F A22WE 20031204001562003120400156NM 2003 12 4 AWXA200301270 120031008A53206546568519 STIFFENER BOEING737 7373G7 1384595NM CARGO COMPART CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT CHANNEL STIFFENER AT BS 1016, BL 0. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED 2 EACH CENTER BULKHEAD SUPPORT CHANNEL STIFFENERS AT BS 1016, BL 0; FABRICATED 2 EACH REPLACEMENT CHANNEL STIFFENERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PARA 4B & 9B. 2L72 4F RTA16WE 20031204001702003120400170CE 2003 12 4 AMWA64 120031010A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07218YV UE218 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT SIDE NEAR AFT STRINGERS INTERSECTION REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031204001742003120400174NM 2003 12 4 QXEA200301295 120031018A243011521062 GENERATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09404QX3946 560 4046 ON FLIGHT 2273 NR 1 DC GENERATOR LIGHT ILLUMINATED IN FLIGHT. RAN EMERGENCY CHECKLIST AND CYCLED NR 1 DC GENERATOR CONTROL SWITCH WITH NO CHANGE TO CAUTION LIGHT. ALL CIRCUIT BREAKERS ARE IN. REMOVED AND REPLACED NR 1 DC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031204001772003120400177SO 2003 12 4 C2XA03TY181 120031020A532014522184005 CHANNEL EMB 145 EMB145 3260210SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING A SCHEDULED INSPECTION SEVERAL AREAS OF CORROSION WERE FOUND ON THE SERVICE DOOR CUTOUT SILL. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2L72 4F RTT00011AT 20031204001782003120400178SO 2003 12 4 C2XA03TY182 120031020A532014521725015 SILL EMB 145 EMB145 3260210SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 51-10-02, 53-21-10 AND CPM 51-21-05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031204001802003120400180SO 2003 12 4 C2XA03TY184 120031020A532014521725013 SILL EMB 145 EMB145 3260210SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-60 AND CPM 51-21-04, 51-21-05 AND 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031204001822003120400182SO 2003 12 4 C2XA03TY186 120031020A532014522464007 STRINGER CLIP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING A SCHEDULED INSPECTION SEVERAL SIGNS OF CORROSION WERE FOUND ON THE STRINGER CLIP BETWEEN FRAME 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE STRINGER CLIP AT FRAME 60 BETWEEN STRINGERS 20L AND 21L IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031204001832003120400183NM 2003 12 4 03FDEA01770 120031009A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LEFT WING O/B FLAP O/B HINGE (WING SIDE) - I/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED. 2L73 4F RTA22WE 20031204001942003120400194EA 2003 12 4 03292633 120031019A335064643 POWER STRIP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27633BR 7274 DURING INSPECTION THE EMERGENCY PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT POWER STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031205000032003120500003NM 2003 12 5 03290421 120031017A3150 WARNING LIGHT DORNERDO32 DO328300 NM LT ENGINE MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27421FJ 3179 DURING CLIMB THE CREW REPORTED A LT ENGINE FADEC WITH NO INDICATION. 2H72 4T RTA55NM 20031205000062003120500006NM 2003 12 5 372PA0036 120031022A335020121 POWER SUPPLY BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY/BATTERY CHARGER PER MM 33-51-51. OPS CHECKS OK. 2L72 4F RTA16NE 20031205000162003120500016NM 2003 12 5 372PA0037 120031023A335058674 POWER UNIT BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 RIGHT OVERWING EXIT LOWER LUMINESCENT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT POWER UNIT PER MM 33-51-51. OPS CHECKS NORMAL. 2L72 4F RTA16NE 20031210000822003121000082SO 2003 12 10 C2XA03IA109 120031201A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2712569 145630 FLIGHT 2082 - THE FLIGHT CREW REPORTED THAT A STRONG BURNING SMELL WAS EMITTED FROM THE ENVIRONMENTAL SYSTEM. THE SMELL WENT AWAY WHEN THE POWER LEVERS WERE PUSHED FORWARD. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE ENVIRONMENTAL SYSTEM. THE DISCREPANCY COULD NOT BE DUPLICATED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20031210001182003121000118WP 2003 12 10 AALA20031323 120031121A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21489AA 49682 LAX INTERIOR CEILING EMERGENCY LIGHTS AT STATION 650-750 INOPERATIVE. REPLACED BATTERY PACK FOR INTERIOR CEILING EMERGENCY LIGHTS AT STATION 650-750. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210001222003121000122NM 2003 12 10 P5CA0300997 120031130A34110856CC12 PROBE BOEING747 747200 1384847NM PITOT/STATIC SYSFAULTY A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23524UP 21446 FOUND FO MAIN PITOT PROBE ANTI-ICE LIGHT ON. REPLACED PITOT PROBE PER MM 30-31-01. OPS CK AND LEAK CK OK. 2L74 4F RTA20WE 20031210001412003121000141WP 2003 12 10 AALA20031351 120031130A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21495AA 49733 DFW OVERHEAD EMERGENCY AISLE LIGHTS FORWARD OF VAULT DOOR BETWEEN RT AND LT LAVS INOPERATIVE. RESEATED BATTERY PACK FOR OVERHEAD EMERGENCY AISLE LIGHTS FORWARD OF VAULT DOOR BETWEEN RIGHT AND LEFT LAVS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001422003121000142WP 2003 12 10 AALA20031352 120031130A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21495AA 49733 DFW OVERHEAD EMERGENCY PATH LIGHTS AT ROWS 4 5 AND 7 INOPERATIVE. RESEATED BATTERY PACKS FOR OVERHEAD EMERGENCY PATH LIGHTS AT ROWS 4 5 AND 7. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001632003121000163WP 2003 12 10 AALA20031382 120031204A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21251AA 49270 MIA CEILING EMERGENCY LIGHTS AT ROWS 18-21 INOPERATIVE. RESEATED BATTERY PACK IN S3-334 FOR CEILING EMERGENCY LIGHTS AT ROWS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001892003121000189WP 2003 12 10 03FDEA01803 120031025A5712ARD108620 RIB DOUG DC10 DC1010 3022110WP RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 NR S 22 COMPLY WITH EA 8-5710-73203. REWORK OF GOUGES IN WING LEADING EDGE RIB. CLOSING ACTION ON 10/22/03. COMPLIED WITH EA 8-5710-73203. 2L73 4F A22WE 20031210001922003121000192NM 2003 12 10 03FDEA01746 120031015A1430 BOLT BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE53392 20935 STA 1183, FORWARD BULKHEAD LOWER TENSION FITTINGS STR 26L, 27L, 26R, 27R, AND 29R HAVE CORRODED .3750 INCH BOLTS. REMOVED AND REPLACED BOLTS IAW WORK CARD 71C716-00 2L73 4F RTA3WE 20031210002132003121000213WP 2003 12 10 UPS03841545 120031023A1430BACB30US1034 BOLT DOUG DC8 DC873F 302199FWP RT CENTER TANK SHEARED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STRINGER END FITTING BOLT IS SHEARED OFF AT XCW 69 AT STRINGER 54 IN RT CENTER TANK. REMOVED AND REPLACED BOLT IAW UPS ENGINEERING FILE NUMBER DC8-57- 20098A DATED 11/03/03,AND SAA SK 867-195 DATED 11/05/03 2L74 4F RT4A25 20031211000022003121100002WP 2003 12 11 ABXA030415 120031106A335060030451 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23929AX307 45874 EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK IAW DC-9 MM 32-53-02. 2L72 4F A6WE 20031211000072003121100007NM 2003 12 11 CALA0300624 120031107A5730 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734131 28971 INSPECTION FOUND A 6 INCH CRACK IN RT WING L/E SKIN PANEL AT WS 421.5. THE SKIN PANEL WAS REMOVED AND REPLACED IAW EA 5731-01010, OP 3. 2L72 4F RTA2NM 20031211000192003121100019WP 2003 12 11 ABXA030416 120031106A3040306311 SWITCH DOUG DC9 DC931 3022065WP COCKPIT DEFECTIVE A ABXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23937AX 47074 FUMES IN COCKPIT, UNABLE TO DETERMINE EXACT SOURCE. INSPECTED BOTH LEFT AND RIGHT AMC'S AND LEFT AND RIGHT DUCTING. INSPECTED E&E COMPARTMENT FOR GENERAL CONDITION AND OBVIOUS DEFECTS. INSPECTED FORWARD ACCESSORY COMPARTMENT FOR GENERAL CONDITION AND OBVIOUS DEFECTS. INSPECTED COCKPIT LIGHTING AND COCKPIT BREAKERS, NO DEFECTS FOUND. INSPECTED WINDSHIELD HEAT, FOUND FIRST OFFICER'S CLEARVIEW WINDOW OVERHEATING CAUSING THE FUMES IN COCKPIT. REPLACED FIRST OFFICER'S CLEARVIEW THERMAL SWITCH IAW DC-9 MM 30-41-02-2. OPS CHECKED GOOD. MAINTENANCE PROCEDURES COMPLIED WITH IAW DC-9 MEL 30-20-2. PLACARD REMOVED, NO FUMES DETECTED IN COCKPIT WITH WINDOW HEAT ON. 2L72 4F A6WE 20031211000202003121100020WP 2003 12 11 ABXA030420 120031103A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 L2 AFT PASSENGER LOWER FORWARD DOOR JAMB CORNER HAD CRACKS ON EXTERNAL SKIN AND INTERNAL DOUBLERS, LENGTH RANGE FROM 2 - 4 INCHES APPROXIMATELY. REMOVED DAMAGE FROM AREA, PERFORMED HFEC ON EXTERNAL SKIN AND TITANIUM DOUBLER, NO CRACKS PAST CUTOUT. FABRICATED DOUBLERS AND FILLERS, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21, 51-1-20D AND REA D853-48059MR. 2L74 4F 4A25 20031211000222003121100022NM 2003 12 11 DHL2003751101 120031028A33501000677 LIGHT BOEING727 727264 138408MNM COCKPIT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 DURING PREFLIGHT CHECK FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER 33-50-00 PG 501. OPS CHECK OK. 2L73 4F A3WE 20031211000322003121100032NM 2003 12 11 AWXA200301390 120031030A53206916970501 ATTACH ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 2.875 INCH CRACK WAS FOUND IN STRINGER 15 LT TO FRAME 344 ATTACH ANGLE. MAINTENANCE REMOVED THE CRACKED ATTACH ANGLE BS 344, STR 15 LT; FABRICATED A NEW REPLACEMENT ATTACH ANGLE DWG 69-16970; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 11 PG 1. 2L72 4F RTA16WE 20031211000332003121100033NM 2003 12 11 AWXA200301391 120031030A532069265552 ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN CLIP ANGLE ON TOP OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACKED CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP ANGLE PER DWG 69-26555; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 & 11 PG 1. 2L72 4F RTA16WE 20031205000212003120500021NM 2003 12 5 DLM88030907 120031008A2781 SENSOR DOUG MD88 MD88 3023688NM LT WING SLAT OUT OF ADJUST A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27981DL 53268 AFTER T/O ON SLAT RETRACTION, GOT THE SLAT DISAGREE LIGHT. FLAPS WERE UP. RECYCLED FLAPS TO NO AVAIL. FOLLOWED POM PROCEDURE AND RETURNED TO DFW. REQUIRED 2 UNITS OF RUDDER TRIM TO THE LEFT FOR LEVEL FLIGHT. OPERATED NORMALLY DURING EXTENSION FOR LANDING. FOUND LEFT WING SENSOR OUT OF ADJUSTMENT. ADJUSTED SAME. 2L72 4F RTA6WE 20031205000322003120500032NM 2003 12 5 DLM88030922 120031012A535059401635051 TAIL CONE DOUG MD88 MD88 3023688NM UNSECURE A DALAK NONE O OTHER ININSP/MAINT 1 SO27999DN 53371 OPS REPORTED TAIL CONE HANGING FROM A/C. CONTRACT MTC FOUND TAIL CONE PARTIALLY DEPLOYED. ONE PIN STILL ENGAGED. SLIDE DID NOT DEPLOY AND WAS DISCONNECTED. TAIL CONE REMOVED AND REINSTALLED. 2L72 4F RTA6WE 20031205000532003120500053NM 2003 12 5 DLM88030945 120031022A3240 BRAKE ASSY DOUG MD88 MD88 3023688NM MLG FAILED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27944DL 49817 NR 1 BRAKE ASSY FAILED INTERNALLY AND CAME APART WHICH LOCKED THE BRAKE. REPLACED SAME. 2L72 4F RTA6WE 20031204001202003120400120SO 2003 12 4 C2XA03IA102 120031015A2731 SWITCH EMB 145 EMB145LR 3260212SO PITCH TRIM DIRTY A C2XAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SW2714573 145638 DURING CRUISE THE CREW REPORTED THAT THERE WAS A TOTAL PITCH TRIM FAILURE. THE AIRCRAFT RETURNED AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE PITCH TRIM SYSTEM, RESET CIRCUIT BREAKERS ASSOCIATED WITH THE PITCH TRIM SYSTEM, AND CLEANED THE THE FIRST OFFICER'S AUTOPILOT DISCONNECT SWITCH. THE PITCH TRIM SYSTEM WAS OPERATIONALLY TESTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20031204001292003120400129SO 2003 12 4 C2XA03SH397 120031019A532014521725615 SILL EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031204001452003120400145WP 2003 12 4 03FDEA01760 120031016A3620 MANIFOLD DOUG DC10 DC1010 3022110WP NR 2 AIR SYS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25550FE 46521 AIR SYSTEM 2 MANIFOLD FAIL AFTER TAKEOFF. RETURNED TO AUS AS PER CHECKLIST. RELEASED FOR SERVICE PER MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 26OCT03 MEL 36-10-02-A: PNEUMATIC SYS NR 2 - INOP. 2L73 4F A22WE 20031204001512003120400151EU 2003 12 4 03FDEA01769 120031020A5330 SKIN AIRBUS300 A300F4605R 3930327EU FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25660FE 759 FUSELAGE SKIN REPAIR OF DENT AFT OF FR 26 AT STR 37-R. COMPLIED WITH EA 6-5330-73212 FUSELAGE SKIN REPAIR OF DENT AFT OF FR 26 AT STR 37-R. 2L72 4F RTA35EU 20031204001972003120400197EA 2003 12 4 032936543 120031020A5320601R5361004 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 DURING INSPECTION THE LT HAND FLOOR SUPPORT ANGLE AT FS 621 BL 41 WAS FOUND CRACKED. 2L72 4F RTA21EA 20031205000012003120500001NM 2003 12 5 QXEA200301304 120031018A3150 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 200 ILLUMINATED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09411QX 4055 FLIGHT 2361 ON ROLLOUT, PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED. RAN CHECK LIST LIGHT STILL ON. CYCLED PUSHER CIRCUIT BREAKERS. COMPLIED WITH STALL WARN TEST. CAUTION LIGHT EXTINGUISHED. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031205000172003120500017NM 2003 12 5 DL757030903 120031004A5314146N35601 KEELBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27621DL 22911 THE AFT END OF THE STRINGER 29R KEELBEAM WAS FOUND CORRODED AT FS 1400. THE BEAM WAS CUT AT FS 1390 AND THE AFT SECTION REMOVED. A NEW SECTION WAS INSTALLED AND SPLICED WITH STEEL REPAIR CHANNELS PER ER/A 087429-14, REV D. 2L72 4F RTA2NM 20031205000232003120500023 2003 12 5 DL73S030910 420031009A2230 AUTOTHROTTLE SYS BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO27379DL 23606 717173 ON T/O ROLL AFTER TOGA THROTTLES REQUIRED MANUAL SET WITH NORMAL FD/AP/AT. F/O TURNED THROTTLE OVER TO CAPT NR 1 AND 2 THROTTLES SPLIT WITH AN INCREASE ON 1. EGT WENT UP TO 630 ON NR 1 WITH A 2.12 SETTING 2.1 AT SET. NR 2 WAS AT 2.04. EVENED THROTTLES AT 2.10 W/STD OPS. 630 IN EXCESS FOR T/O LIMIT. INSPECTED NR 1 ENG PER M/M FOR EGT, NO ACTION REQUIRED M/M. AUTO THROTTLES FWD TO MCO AND PLAC PER MEL 22-00-04. PULLED AND SECURED AUTO THROTTLE AC AND DC C/BS PER MEL. 2L72 4F4 F A16WE E2EA 20031205000542003120500054NM 2003 12 5 DL757030946 120031021A5312 BULKHEAD BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27659DL 24421 THE BREAK RING SECTION OF THE FS 1720 BULKHEAD WAS FOUND WITH AREAS OF CORROSION AND CRACK INDICATIONS NEAR STRINGER 18R. THE SECTION WAS CUT OUTBOARD OF THE DAMAGE AND THE SECTION FROM STRINGER 18R TO 12R WAS REMOVED. A NEW SECTION WAS FABRICATED AND SPLICED IN WITH ALUMINUM SPLICE STRAPS PER ER/A 385748-14. 2L72 4F RTA2NM 20031205000572003120500057 2003 12 5 SWIA200312515 420031008A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07188SW 120039 STALL WARNING LIGHT WON'T EXTINGUISH ON PANEL. REMOVED AND REPLACED STALL WARNING CONTROL PANEL. OPS TESTED GOOD. P/N: 120-34428-505, S/N OFF: 386792. 2L72 4T RTA31SO 20031205000582003120500058SO 2003 12 5 SWIA200312517 120031012A5280 DOOR EMB 120 EMB120ER 3260203SO NLG UNSECURE A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07196SW 120151 AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. FOUND LEFT NOSE GEAR DOOR NOT PROPERLY LATCHED. RESECURED LATCH AS REQUIRED. FUNCTIONAL CHECK OF NOSE GEAR DOORS FOUND GOOD. 2L72 4T RTA31SO 20031208000012003120800001NM 2003 12 8 2003UALA00778 120031015A5754 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 2 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 NR 2 SLAT DELAMINATED AT OB END LWR SURFACE OF T/E WEDGE. AREA IS 1.6 INCHES CHORDWISE X 1.3 INCHES SPANWISE AT 1.3 INCHES FROM OB END AND 1.6 INCHES FROM T/E. THE ABOVE NOTED DELAM CONDITION WAS DUE TO WEAR FROM NORMAL LOADS EXPERIENCED DURING A FLIGHT OVER A PERIOD OF TIME. THE TRAILING EDGE WEDGE OF THE SLAT WAS REPAIRED USING AN ADHESIVE INJECTION METHOD. 2L72 4F4 FRTT0001SE E46NE 20040121000782004012100078EU 2004 1 21 ASOA03604 120031124A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11637AS 383 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040121000882004012100088WP 2004 1 21 GTIA030973 120031029A7120K22199SA31 ISOLATION MOUNT DOUG DC9 DC983 3022083WP LT ENGINE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND LT ENGNE PYLON YOKE ASSEMBLY UPPER AND LOWER ISOLATORS ALIGNMENT MARKS DETERIORATED. UNABLE TO DETERMINE MISMATCH. REMOVED LEFT ENGINE PYLON YOKE ASSEMBLY UPPER AND LOWER VIBRATION ISOLATOR. INSTALLED UPPER VIBRATION ISOLATOR. INSTALLED LOWER VIBRATION ISOLATOR. (M) 2L72 4F RTA6WE 20040121000932004012100093NE 2004 1 21 2004F00047 220031118A7250 TURBINE BLADES BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE BROKEN A GUUAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO1787552 UE216 PS114455 DURING TAKEOFF, LOUD BANG OCCURRED ON LT ENGINE. ABORTED TAKEOFF. SEPARATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF. REPLACED LEFT POWER SECITON MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. (M) 2L72 4T4 TRTA24CE E26NE 20040121000952004012100095SO 2004 1 21 SIMA200331001 120031105A335020131A BATTERY PACK EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21828AE 145604 DURING TAXI IN CRWE NOTED FORWARD PORTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. RAI NR 1 EMERGENCY BATTERY PACK P/N 20131A, S/N 67884, NR 2 BATTERY PACK P/N 20131A S/N 69700, AND NR 3 EMERGENCY BATTERY PACK P/N 20131A AND S/N 71003, OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20040121001092004012100109NM 2004 1 21 03FDEA02340 120031231A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 CORROSION ON SKIN STA 1090 STR 27R - 29R. REMOVED CORROSION ON SKIN AT BS 1090, STR 27R-29R AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20040122000022004012200002NM 2004 1 22 03FDEA02301 120031226A5350AKC786836 STIFFENER DOUG MD11 MD11 3023602NM ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT TAILCONE UPPER DOOR FORWARD MOST VERTICAL STIFFENER FOUND CHAFED. REMOVED DAMAGED STIFFENER AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW STIFFENER AS PER DRAWING AKC 7868. INSTALLED NEW STIFFENER AT RT TAILCONE UPPER DOOR FED MOST AS PER SRM 51-35-01 VOL. II. 2L73 4F RTA22WE 20040115001572004011500157NM 2004 1 15 03FDEA02157 120031209A2810 FUEL TANK BOEING727 727200 138407ENM CENTER CELL CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25276FE 22041 FOUND CORROSION ON UPPER SURFACE OF WING CENTER TANK BS 825 RBL 12. REMOVED CORROSION ON UPPER SURFACE OF WING CENTER TANK AT BS 825, RBL 12 PER SRM 51-10-06. FOUND DAMAGE AREA TO BE OUT OF LIMITS PER SRM 53-10-1, FIG 1. REMOVED DAMAGE AND REPAIRED PER SRM 57-30-3. 2L73 4F RTA3WE 20040115001582004011500158EA 2004 1 15 033337648 120031203A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY INTERMITTENT A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27648BR 7406 DURING TAKEOFF THE LAVATORY SMOKE MESSAGE APPEARED ON THE FLIGHT DISPLAY'S. CREW ABORTED TAKEOFF AND RETURNED TO GATE FLIGHT LANDED UNEVENTFULLY. FOUND TO BE A FAULTY SMOKE DETECTOR AND IT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE LAVATORY SMOKE DETECTOR AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040120000562004012000056NM 2004 1 20 03FDEA02231 120031223A5753ARC050214 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, OB FLAP IB FWD HINGE ACTUATOR MOUNT OB LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75209, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040121000342004012100034NM 2004 1 21 03FDEA02313 120031229A5311AFA0022 LONGERON DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 FRAME ADJACENT TO LONGERON 12 LT, STA 1561 FOUND WITH DENT. STA 1561 LONGERON 12L DENT FRAME REPAIRED AS PER SRM 53- 30-00 FIG. 1 VOL. I AND FEDEX EA 1-5310-75223. REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NO. 1-2520-7- 3308). 2L73 4F RTA22WE 20040121000722004012100072EU 2004 1 21 ASOA03617 120031106A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN BNA, THE LT AND RT SEAT TRACKS BETWEEN FRAMES 39 AND 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT SEAT TRACKS BETWEEN FRAMES 39 AND 41 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20040122000532004012200053EA 2004 1 22 ASOA03640 120031211A5210601R3807413 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11908EV 7654 DURING A C-CHECK IN MCN, THE FORWARD AND AFT CABLE ANCHOR FITTINGS ON THE PASSENGER DOOR WERE FOUND TO BE CRACKED. MAINT IS REMOVING AND REPLACING THE FORWARD AND AFT CABLE ANCHOR FITTINGS ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040122000562004012200056EA 2004 1 22 2004F00051 120031019A5270840534 PROXIMITY SWITCH CNDAIRCL600 CL6002C10 1390015EA LT EMERG DOOR OUT OF ADJUST A FDKAO OTHER N FALSE WARNING CRCRUISE 1 SW07507MJ 10077 LEFT EMERGENCY DOOR CAUTION MESSAGE INTERMITTENT DURING FLIGHT. MAINTENANCE APPLIED MEL 52-70-03. MAINTENANCE ADJUSTED DOOR PROXIMITY SWITCH. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040122000672004012200067EU 2004 1 22 SIMA200334404 120031108A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21390AE 340B390 DURING AN MBV INSPECTION A PREVIOUS REPAIR ON FRAME 258 UNDER THE GALLEY FLOOR WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED THE EXISTING REPAIR PARTS, CLEANED, AND TREATED THE REPAIR AREA. FABICATED A REPAIR ANGLE, FILLER AND TRIPLER. REPAIR DONE IAW 340 SRM, CHAPTERS 53-70-30-2. (M) 2L72 4T RTA52EU 20040122000702004012200070EA 2004 1 22 ASOA03586 120031117A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11875AS 7559 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP ACTUATING ROD WAS FOUND BROKEN FROM THE BOTTOM STEP. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122000732004012200073EU 2004 1 22 USAASA03135 120031203A3350321430 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19180US 1525 CLT - THE AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST WITH THE MESSAGE 'EPSU COMM AFT L'. MAINTENANCE REPLACED TEH EMERGENCY POWER SUPPLY UNIT BATTERY AT THE AFT PASSENGER CABIN POSITION. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040122000742004012200074EA 2004 1 22 ASOA03628 120031204A5320601R38303239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT THE SERVICE DOOR ON THE RIGHT SIDE AT APPROXIMATELY FS 319 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOOR SUPPORT ANGLE AT THE SERVICE DOOR ON THE RIGHT SIDE AT APPROXIMATELY FS 319. (M) 2L72 4F RTA21EA 20040122000802004012200080NM 2004 1 22 USAASB03219 120031222A3350 CONNECTOR BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS, AT ROWS 12 THROUGH 16, INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR AT SEAT ROW 12 LOOSE. RESEATED CONNECTOR. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040122000842004012200084NM 2004 1 22 USAABB03226 120031220A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 9 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU 27124 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20040122000962004012200096EA 2004 1 22 ASOA03635 120031207A5210601R3167011 PANEL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11907EV 7648 DURING A C-CHECK IN MCN, THE PASSENGER DOOR LOWER PANEL ON THE TOP STEP DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP LOWER PANEL ASSEMBLY ALONG WITH THE LOWER HINGE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001092004012200109WP 2004 1 22 GTIA030971 120031031A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND THREE DENTS AT FS 218.5, 218 AND 222 AT LONGERON 19L. THESE DENTS ARE WITHIN ONE INCH OF STRUCTURE AND REQUIRE REPAIR. CUT OUT DAMAGED AREA OF SKIN. FABRICATED SKIN, DOUBLER AND FINGER. INSTALLED REPAIR. (M) 2L72 4F RTA6WE 20040122001222004012200122EA 2004 1 22 ASOA03656 120031216A2760855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11885AS 7521 FLT 4783 - DURING APPROACH FROM DFW-AMA, THE CREW SELECTED THE FLAPS TO EIGHT DEGREES AND RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW ABORTED THE APPROACH TO COMPLY WITH THE QRH, PERFORMED A GO AROUND AND REQUESTED EMERGENCY VEHICLES BE ON STAND-BY. THE TOWER DECLARED AN EMERGENCY AS PRECAUTIONARY MEASURE AND THE AIRCRAFT LANDED SAFELY IN AMA. MAINTENANCE REMOVED AND REPLACED THE LEFT BRAKE POSITION SENSOR UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001262004012200126EA 2004 1 22 ASOA03624 120031203A78301267587 PDU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11871AS 7537 DURING CRUISE FROM IND-DFW, AT APPROXIMATELY 31,000 FEET THE CREW RECEIVED A RIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH, AN EMERGENCY DECLARED AND THE AIRCRAFT DIVERTED INTO LIT, LANDING SAFELY. MX DEFERRED THE RIGHT THRUST REVERSER ON 12/3/2003 UNDER MEL NR 78-30-01, AND CLEARED THE DEFERRAL ON 12/5/2003 BY REMOVING AND REPLACING THE POWER DRIVE UNIT ON THE RIGHT THRUST REVERSER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001422004012200142NE 2004 1 22 MDR03023 120030728A6210641520201050 BLADE SKRSKYS64 S64E 8142604NE MAIN ROTOR CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09189AC5543 641001 THE BLADE WAS REMOVED FROM THE AIRCRAFT FOR BIM INDICATION. A 10-DAY LEAK CHECK WAS PERFORMED AND A CRACK WAS FOUND IN THE SPAR 117.75 INCHES FROM THE TIP END AND 4.50 INCHES FROM THE LEADING EDGE ON THE BOTTOM SIDE OF THE BLADE. CAUSE: UNKNOWN 2G72 4U H4EA 20040122001452004012200145CE 2004 1 22 BSY2003F00026 120031022A3297 WIRE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO SQUAT SWITCH BROKEN E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0717708 TH813 8V6851 GEAR WOULD NOT GO UP. FOUND BROKEN WIRE IN WHEEL WELL COMING FROM SQUAT SWITCH. 1L72 3O3 O 3A16 E5CE 20040123000172004012300017WP 2004 1 23 ASAA0380761 120031121A533059114013 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 DURING 15K CHECK, FOUND FUSELAGE SKIN DENTED AT STATION 182. INSTALLED DOUBLER PER SRM 53-04, 51-10-3, AND 51-30-2. (M) 2L72 4F RTA6WE 20040123000192004012300019 2004 1 23 A6WA200340193 420031211A34177858062 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA ADH SENSOR MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31431AW9324 7256 TAT PROBE HEAT CAUTION ILLUMINATED INFLIGHT AFTER TAKEOFF. REPLACED AIR DATA HEAT SENSOR CONTROL UNIT. (M) 2L72 4F RTA21EA 20040123000252004012300025NE 2004 1 23 MDR03031 120031002A6220SB3251A1 BEARING SKRSKYS64 S64F 8142610NE MAIN ROTOR HEAD FAILED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09164AC653 A2015 64034D CREW REMOVED M/R HEAD AFTER LOCK SCREW SECURING LOCK SHEARED FOR SECOND TIME ON SPINDLE ASSY DESIGNATED AS GREEN. DURING TEARDOWN OF GREEN SPINDLE ASSY AFTER REMOVING NUT, SECURING HORIZ HINGE PIN. IT WAS NOTICED BONDED SPLIT LINERS WERE DEBONDED FROM SPINDLE. NO PLAY NOTICED IN HORIZ HINGE PIN. REMOVING HORIZ HINGE PIN, ROLLER BRG AGAINST WASHER AND NUT FAILED. REMOVAL OF ROLLER TAPER BRGS SHOWED EXTENSIVE DAMAGE CONSISTING OF MISSING MATERIAL ON THE BEARING CONE AND CUP IN AREA BETWEEN 4 OCLOCK AND 8 OCLOCK ALSO HAVE SIGNS OF WEAR AND BRINELLING. ROLLER CAGE FOR BRG CONE BROKEN IN MULTIPLE PIECES, ROLLERS EXHIBITED FLAT SPOTS W/MISSING MATERIAL, GOUGED AND SCORED INNER SPACER. 2G72 4U H6EA 20040123000332004012300033EU 2004 1 23 KBM2003F00084 120031109A3110704A47270101 INDICATOR SNIAS 350 AS350B1 8680811EU COCKPIT MALFUNCTIONED E KBMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP1953SH 2009 FUEL AND ENGINE OIL PRESSURE GAUGES ARE INDICATING HIGH WITH BATTERY POWER ONLY. REMOVED AND REPLACED 1G71 3U H9EU 20040123000382004012300038EU 2004 1 23 KBM2003F00085 120031101A2560AFG0582730 INERTIA REEL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT SEATBELTFAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH2913 2884 INERTIA REEL ON PILOTS SEAT WILL NOT RETRACT. INSTALLED O/H UNIT. 1G71 3U3 U H9EU E19EU 20031203000042003120300004SO 2003 12 3 SIMA200328807 120031015A5347 SEAT TRACK EMB 135 EMB135KL 3260302SO COCKPIT DIRTY A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21832AE 145627 ORD - WHILE TAXIING AIRCRAFT, CAPTAINS SEAT INTERMITTENTLY WOULD SLIDE BACK FROM A LOCKED POSITION. MAINTENANCE CLEANED DEBRIS FROM SLIDE TRACK. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031203000272003120300027NM 2003 12 3 GAIA03127ST 120031024A5313BAC1498132 STRINGER BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURNG C-CHECK INSPECTION FOUND STRINGER 15 LT CRACKED AT BS 720B PLUS 15. REF FASI N/R NR 61452, INSTALLED REPAIR DOUBLER PER B727 SRM 53-10-3 FIG 5. (M) 2L73 4F RTA3WE 20031203000322003120300032NM 2003 12 3 GAIA03129ST 120031024A5347BAC1520792 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND SEAT TRACK CORRODED LBL 24.75 BS 1090-1130. REF FASI N/R NR 61427, REPLACED CORRODED SEAT TRACK PER B727 SRM 53-10-5 FIG 1. (M) 2L73 4F RTA3WE 20031203000362003120300036NM 2003 12 3 C7WA200300047 120031017A3213651765718 STRUT BOEING727 72731 1384010NM RT MAIN GEAR FRACTURED A C7WAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO17220NE 18905 DURNG TAXI, INTERMITTENT GEAR HORN WITH INTERMITTENT RED UNSAFE LIGHT. FOUND RT MAIN LANDING GEAR SIDE STRUT FRACTURED AT STRUT SWIVEL CLEVIS. REMOVED AND REPLACED RT MLG LWR, SIDE STRUT IAW B727 MM 32-11-41. 2L73 4F A3WE 20031203000462003120300046EA 2003 12 3 2003F00636 120030915A5270 SWITCH CNDAIRCL600 CL6002D24 EA EMERGENCY EXIT DIRTY A FDKAO OTHER N FALSE WARNING CRCRUISE 1 SW07905FJ 15005 CREW REPORTED RIGHT AFT EMERGENCY EXIT INDICATION ILLUMINATES UNCOMMANDED. MAINTENANCE CLEANED THE SWITCH AND PERFORMED OPERATIONAL CHECKS ON THE DOOR WARNING SYSTEM. (M) 2L72 4F RTA21EA 20031203000482003120300048NM 2003 12 3 GAIA03152ST 120031024A5315BAC150510067 FLOORBEAM BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND CABIN FLOORBEAM CORRODED BS 1070 BETWEEN RBL 48 AND RBL 60. REF FASI N/R NR 61850, CUTOUT DAMAGE AND INSTALLED REPAIR PER B727 SRM 53-10-8 FIG 3. (M) 2L73 4F RTA3WE 20031203000612003120300061NM 2003 12 3 USAA030205 120031003A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND SKIN CRACKED 1 INCH, STATION 727D S23L. REPAIRED CRACK PER TYPICAL REPAIR 53-60-03. (M) 2L72 4F RTA16WE 20031203000622003120300062NM 2003 12 3 AALA20031169 120031024A3350 LIGHT BOEING777 777223 1385213NM ESCAPE SLIDE INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21757AN 32636 DURING OVERNIGHT MAINTENANCE, EMERGENCY SLIDE LIGHT AT DOOR 4L INOPERATIVE. REPLACED EMERGENCY SLIDE LIGHT AT DOOR 4L. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20031203000652003120300065EA 2003 12 3 2003F00623 120030202A5610NP1393225 WINDSCREEN CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A FDKAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07507MJ539 10077 RETURNED TO THE FIELD CAPTAINS WINDSHIELD CRACKED IN FLIGHT. MAINTENANCE REPLACED THE WINDSHIELD. (M) 2L72 4F RTA21EA 20031203000812003120300081EA 2003 12 3 2003F00633 120031019A7830TY214810A ISOLATION VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE THRUST REVERSER MALFUNCTIONED A FDKACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW07902FJ1186 15002 GEE194202 FLT 6747 - PHX-TUS - CAPTAIN ABORTED TAKEOFF DUE TO LEFT REVERSER UNSAFE CAUTION. MAINTENANCE TROUBLESHOT TO ISO CONTROL VALVE, R2 ISO CONTROL VALVE OPS CHECK GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20031203000852003120300085EU 2003 12 3 SIMA200321801 120030802A5310 STRUCTURE SAAB SF340 340B 7860101EU E/E BAY BURNED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21376AE 340B376 DURING OXYGEN BOTTLE CHANGE THE LOWER RT FUSELAGE AVIONIC COMPARTMENT CAUGHT FIRE. AIRCRAFT WAS REPAIRED IAW ENGINEERING ORDERS G1-5300-436, G1-53MA-732, G1-53MR-735R1, AND G1-5300-736. (M) 2L72 4T RTA52EU 20031203000862003120300086SO 2003 12 3 SIMA200330401 120031030A25101391001619 LOCK PIN EMB 145 EMB145LR 3260212SO CAPTAINS SEAT LACK OF LUBE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21633AE 145148 CAPTAIN SEAT WILL NOT STAY LOCKED CAUSING FORE/AFT MOVEMENT IN FLIGHT. CLEANED AND LUBRICATED SEAT LOCK PIN AND SEAT RAILS IAW AE WORK CARD 25-200-07. (M) 2L72 4T RTT00011AT 20031203000882003120300088 2003 12 3 USAABB03187 420031013A2565 BELLCRANK BOEING757 757225 1384959NM L2 DOOR MISINSTALLED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 PHL - L2 DOOR ARMED INDICATION INTERMITTENT. MAINTENANCE FOUND A LOWER GIRT BAR BELLCRANK INCORRECTLY INSTALLED A REPOSITIONED IT. (M) 2L72 4F RTA2NM 20031203000952003120300095SW 2003 12 3 2003F00630 120031031A26121734361600 PROBE FRCHLDSA227 SA227DC 3377521SW FIRE DETECTOR LOOSE A BSAAO OTHER J WARNING INDICATION CLCLIMB 1 NM05847LS DC847B ENGINE FIRE WARNING LIGHT FOR THE NR 2 ENGINE CAME ON DURING CLIMB-OUT AS CREW COMPLETED CHECKLIST. AS THE CREW STARTED EMERGENCY CHECKLIST PROCEDURES, THE FIRE LIGHT WENT OUT. CREW COMPLETED APPLICABLE EMERGENCY CHECKLIST ITEMS, AND RETURNED TO STATION. CREW EVALUATED THE SITUATION AND DIDN'T SHUT DOWN THE ENGINE. FIRE WARNING SYSTEM FAULT. THE FIRE WARNING LIGHT WAS STILL OUT AFTER THE CREW LANDED. MAINTENANCE RAN THE AIRCRAFT AND COULDN'T DUPLICATE THE DISCREPANCY. INSPECTION OF THE FIRE DETECTORS ON THE RIGHT ENGINE REVEALED THE CENTER FIRE DETECTOR PROBLEM WAS LOOSE. THIS FIRE DETECTOR WAS REPLACED, AN ADDITIONAL RUN WAS COMPLETED WITH NO DISCREPANCIES NOTED. (M) 2L72 4T RTA18SW 20031203000962003120300096EU 2003 12 3 USAASB03194 220031027A73209387M15P12 EEC BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 1 ENGINE FAILED A USAAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 EA19784AU 25023 721118 ON DESCENT, AT APPROXIMATELY FL180, CAPTAIN REPORTED THE NR 1 ENGINE WAS NOT RESPONDING TO THRUST INPUT. ENGINE INDICATIONS WERE ABNORMALLY SLOW AND LOW. AFTER A FEW MINUTES, CREW ATTEMPTED A RESTART, BUT THE PROBLEM PERSISTED. CREW SHUTDOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO BWI. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS APPROX 25 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE MAIN ENGINE CONTROL AND FUEL PUMP, P/N 9375M82P04, AND CIT SENSOR P/N 9334M96P02. OPS CHECK, LEAK CHECK AND ENGONE RUN-UP NORMAL. (M) 2L72 4F4 FRTA16WE E21EU 20031203001032003120300103NM 2003 12 3 USAA030224 120031002A5330 DOUBLER BOEING737 737401 1384701NM FUSELAGE SKIN CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US40937 23985 FOUND FUSELAGE SKIN DOUBLER CRACKED 3.5 INCH, AFT FUSELAGE BS 1138 STRINGER 12 LT. INSTALLED DOUBLER .63 CRES 301 1/2 HARD PER 53-00-01 PAGE 262 BOEING DWG 65-46585. (M) 2L72 4F RTA16WE 20031203001092003120300109EA 2003 12 3 ASOA03555 120031101A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031203001282003120300128NM 2003 12 3 AMTA200301322 120031026A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11527AT 30886 EGRESS LIGHT OUT AT ROW 21-23 AND 26. RESECURED WIRE FOR EGRESS LIGHTS AT SEAT 21-23 AND 26. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20031203001462003120300146WP 2003 12 3 AMTA200301280 120031002A5312 BULKHEAD LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 APPROXIMATELY 3 INCH CRACK IN BULKHEAD WEB FS 1989, 8 O'CLOCK POSITION. REPAIRED BULKHEAD WEB AT FS 1989, AS PER ERA L10-53R-5324. (M) 2L73 4F A23WE 20031203001532003120300153WP 2003 12 3 AALA20030999 120030912A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217518A 49895 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE OVERWING EMERGENCY EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001602003120300160WP 2003 12 3 AALA20031038 120030920A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217546A 53028 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001742003120300174WP 2003 12 3 GTIA030867 120031021A5350 HINGE DOUG DC9 DC981 3022081WP TAILCONE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FOUND TAILCONE RELEASE ARM DOOR IN AFT F/A STATION BROKEN. RESECURED HINGE. REPLACED RIVETS. (M) 2L72 4F A6WE 20031203001782003120300178WP 2003 12 3 AALA20031147 120031015A3350BPS73 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21285AA 49297 MAINTENANCE OBSERVED OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001792003120300179WP 2003 12 3 AALA20031146 120031016A3350 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21570AA 49352 MAINTENANCE OBSERVED SEAT MOUNTED ESCAPE PATH LIGHT INOPERATIVE AT SEAT 18D. REPLACED WIRE HARNESS AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031203001822003120300182WP 2003 12 3 AALA20031103 120031003A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21489AA 49682 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE OVERWING DOOR SECTION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204000072003120400007WP 2003 12 4 GTIA030887 120031023A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND LEFT AFT ESCAPE HATCH EMERGENCY LIGHT INOPERATIVE. FOUND GROUND WIRE BROKEN. TERMINATED GROUND WIRE. (M) 2L72 4F A6WE 20031204000142003120400014NE 2003 12 4 GTIA030876 220031031A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217A 52053NE RIGHT FAILED A GTIAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 GL23811NK 48017 696406 RIGHT ENGINE FAILURE AT 80 KTS. REMOVED AND REPLACED NR 2 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20031202000922003120200092EA 2003 12 2 ASOA03493 120031017A5210601R3807423 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11838AS 7276 DURING A HANGAR INSPECTION IN MCN, THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR CRACK AND REPLACE DOOR CABLE ANCHOR FITTING WITHIN 100 FLIGHT HOURS PER REO 601R-52-11-416. MAINTENANCE REMOVED AND REPLACED THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031202000972003120200097NM 2003 12 2 USAA030218 120031028A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US49988 23316 FOUND SKIN CRACKED 2.375 INCH, STATION 740 AND S23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20031202001162003120200116NM 2003 12 2 GAIA03111SP 120031022A5320 WEB BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076831 20184 DURING B-CHECK AT DFW, A CRACK WAS FOUND IN A LIGHTNING HOLE BY THE AFT AIRSTAIRS BS 1283. THE CRACK WAS REPAIRED PER THE B727 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031211000382003121100038NM 2003 12 11 QXEA200301397 120031106A2932 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM HYD SYSTEM DEFECTIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09367PH 511 SEA- ON FLIGHT NUMBER 2008, RETURNED TO FIELD ON TAKEOFF, MASTER CAUTION RUD LIMIT FULL PRESSURE. UNABLE TO RESET MASTER CAUTION. CAUTION LIGHT WENT DIM TO BRIGHT THEN BACK TO DIM. HYDRAULIC PRESSURE AND QUANTITY NORMAL. REMOVED AND REPLACED HYDRAULIC PRESSURE SWITCH AT P3-P4. RAN ENGINES TO PRESSURE SYSTEM. OPERATED RUD LEFT/RIGHT TO OPERATIONAL CHECK SWITCHES WITH FLAP AT 0 & 5 DEGREES. LIGHTS ILLUMINATED, RESET MASTER CAUTION, RESET RUD PRESSURE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031211000422003121100042NM 2003 12 11 DHL2003741011 120031108A5250 DOOR BOEING727 7272Q9 138448MNM COCKPIT BINDING A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01741DH 21931 DURING FLIGHT COCKPIT ENTRY DOOR BECOMES DIFFICULT TO OPEN. DOOR RUBS AGAINST DOOR JAMB. PROBLEM SEEMS TO IMPROVE AFTER AIRCRAFT IS ON THE GROUND, BUT STILL RUBS THE DOOR JAMB A LITTLE. CLEANED EXCESS PAINT FROM DOOR JAMB. LUBED DOOR AND LATCH ASSEMBLY PER DHL B-727 M/M 52-50-1. OPS CHECKED GOOD. 2L73 4F RTA3WE 20031211000442003121100044NM 2003 12 11 P5CA0300982 120031107A7333 CONNECTOR BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE FUEL SYSTEM DIRTY A P5CAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP23524UP 21446 662320 ON PUSHBACK NR 3 ENG FUEL FLOW RESPONDED ERRATICALLY. CLEANED CONNECTOR ON FUEL FLOW TRANSMITTER, OPS NORMAL ON RELIABILITY CHECK PER MM 73-00-00. 2L74 4F4 FRTA20WE E20EA 20031211000472003121100047NM 2003 12 11 C1HA200385011 120031107A3350 BATTERY PACK BOEING727 7272S7 138407ZNM CABIN DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15685CA 22492 FWD SECTION OF FLOOR TRACK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW 727 MM 33-50-51, ALL OPS NORMAL. 2L73 4F A3WE 20031211000532003121100053NM 2003 12 11 AWXA200301405 120031014A5315146N5444 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT NUT PLATES BETWEEN BS 1500 TO BS 1510, LBL 14. MAINTENANCE REMOVED CORRODED FLOORBEAM CAP BETWEEN BS 1500 TO BS 1510, LBL 14; FABRICATED A NEW REPLACEMENT CHANNEL AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-1 FIG 1. 2L72 4F RTA2NM 20031211000572003121100057NM 2003 12 11 C1HA200394029 120031107A5320 INTERCOSTAL BOEING727 727290 138408WNM FUSELAGE BROKEN A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 INTERCOSTAL BETWEEN BS 970 - 990, BL-0 ATTACH ANGLE BROKEN IN SEVERAL PLACES. 2L73 4F A3WE 20031211000732003121100073EU 2003 12 11 AWXA200301407 120031111A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW1391329 091 DFW - EEL - DURING INSPECTION FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031211000752003121100075NM 2003 12 11 AWXA200301410 120031028A573065C2630936 DOUBLER BOEING737 7373G7 1384595NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK A 1.3125 INCH CRACK WAS FOUND ON NR 6 FLAP TRACK FAIRING INNER DOUBLER AT AFT END WBL 191 RT. MAINTENANCE REMOVED CRACKED INNER DOUBLER AT WBL 191 RT; FABRICATED A NEW REPLACEMENT INNER DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 2 & 3. 2L72 4F RTA16WE 20031211000882003121100088 2003 12 11 03FDEA01893 420031108A2210A718822 AUTOPILOT SYS BOEING727 727200 138407ENM COCKPIT MALFUNCTIONED A FDEAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CRCRUISE 1 SO25463FE 22551 AT ALTITUDE FL280 CREW NOTICED AN UNUSUAL VIBRATION OF AIRCRAFT. ALL ENGINES / INSTRUMENTS INDICATED NORMALLY. ELECTED TO DIVERT TO SDF. VIBRATION / SHUTTER CONTINUED DURING TAXI IN. ACN RELEASED FOR SERVICE PER MEL/CDL: 22-06-A CATEGORY: C EXPIRATION: 18NOV03 MEL 22-06-A: UPPER YAW DAMPER INOP. FOUND UPPER RUDDER SHUTTERING BACK AND FORTH. TURNED UPPER YAW DAMPER OFF SHUTTERING STOP. DEFERRED UPPER YAW DAMPER. SWAPPED YAW DAMPER COUPLERS, NO HELP RETURNED TO ORIGINAL POSITIONS. REF B727-200 MM 22-11-131-4, NEEDS CONTINUED T/S. 2L73 4F RTA3WE 20031211000922003121100092NM 2003 12 11 03FDEA01876 120031105A53116556123 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION FOUND ON FORWARD SIDE OF 950E FRAME AT STRINGER 29 LT. REPAIRED PER B727 SRM 53-10-4 FIG 15. 2L73 4F RTA3WE 20031211000962003121100096EU 2003 12 11 038181 120031112A7722 CONNECTOR SAAB SF340 SF340A 7850100EU LT NACELLE LOOSE A UHLAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17157 DURING CLIMBOUT ON FLT 9404, L ENG OVER TEMP LIGHT ILLUM, L END NG WENT TO 0, L ENG ITT PEGGED AT MAX, ENGINE WAS SHUT DOWN AND EMERGENCY DECLARED, AIRCRAFT RETURNED TO BLOCK WITH NO INCIDENT. FOUND ELECTRICAL CONNECTOR P4 LOOSE IN LT NACELLE, RESECURED CANNON PLUG, OPS CHECK GOOD. 2L72 4T RTA52EU 20031211000992003121100099 2003 12 11 SWAA032472 420031107A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031014001742003101400174NM 2003 10 14 SWAA032080 120030918A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 AFT LOWER EMERGENCY FLASHLIGHT POWER IND INOP. REMOVED AND REPLACED FLASLIGHT ASSY PER MM. 2L72 4F RTA16WE 20031014001892003101400189NM 2003 10 14 SWAA032108 120030920A575465C26602 SKIN BOEING737 7373Q8 1384670NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2L72 4F RTA16WE 20031014002102003101400210EU 2003 10 14 BAQA089834 120031013A6340645142081 INDICATOR AEROSPSA365 SA365N 8680669EU TRIPLE TACH CONTAMINATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 12 6425 CONDENSATION IN GAUGE FACE. THIS IS A NEW AEC PART. 1G72 3U H10EU 20031015000152003101500015 2003 10 15 USAASA03093 420030817A2565C37103103 RELEASE CABLE AIRBUSA319 A319112 3930323EU GIRT BAR WRONG PART A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19760US 1354 THE AFT RT EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20031015000282003101500028EA 2003 10 15 ASOA03431 120030910A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11880AS 7606 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP PUSH PULL ROD BRACKET WAS FOUND LOOSE AND THE BOTTOM STEP CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP AND ADJUSTED THE BOTTOM STEP PUSH-PULL ROD BRACKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000352003101500035EA 2003 10 15 ASOA03422 120030907A5260601R3190169 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE HYDRAULIC ASSIST ON THE MAIN CABIN DOOR CABLE WAS INOPERATIVE. UPON INSPECTION MAINTENANCE FOUND THE BOTTOM STEP ON THE PASSENGER DOOR BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000722003101500072NM 2003 10 15 USAASB03146 120030823A3397 CONNECTOR BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US 22954 PHL - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 19ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR AT ROW 19ABC. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031016000012003101600001WP 2003 10 16 ABXA030386 120031007A324226014122 BRAKE ASSY DOUG DC8 DC863 302198AWP MLG BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX200 46155 NR 8 BRAKE COMPENSATING LINK ATTACH POINT BROKE. REMOVED AND REPLACED BRAKE AND TIRE ASSEMBLY IN THE NR 8 POSITION IAW DC-8 MM 32-40-0. 2L74 4F 4A25 20031016000022003101600002NM 2003 10 16 03FDEA01665 120031001A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 LT 930 FRAME CRACKED AT LOWER SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 LT, PER SRM 53-10-4, EA 7-5310-55032. 2L73 4F4 FRTA3WE E2EA 20031016000032003101600003NM 2003 10 16 03FDEA01696 120031003A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 FWD CARGO SIDE FRAME DENTED STA 680, LBL 33, WL 160 . OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED FRAME BS 680, LBL 33, WL 160 PER SRM 53-10- 1, 51-40-3 FIG 1 AND FED EX EA 7-5310-55028. 2L73 4F RTA3WE 20031009000742003100900074EA 2003 10 9 SWIA200312396 120030909A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07432SW 7548 RUDDER TRIM INOP NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM PANEL. OPS CHECK GOOD. P/N: 601R51226-23/01 2L72 4F RTA21EA 20031009000832003100900083SO 2003 10 9 SWIA200312405 120030809A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07298SW 120328 RT FRAME 9 CRACKED BY FO'S O2 STORAGE BOX, UPPER RADIUS. (DISCOVERED DURING C-CHECK INSPECTION) COMPLIED WITH SERVICE BULLETIN NR 120-53-0073 IAW EMB SRM 51-40-00 THRU 51-40-08. 2L72 4T RTA31SO 20031010000092003101000009NM 2003 10 10 USAABB03158 120030905A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU 27124 FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 18 AND 32. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031010000132003101000013NM 2003 10 10 USAASB03150 120030825A3260106180350 SOCKET BOEING737 7373B7 1384580NM MLG INDICATOR LOOSE A USAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA19389US 23311 MSP - FLT 374 - DURING TAKEOFF AT CLT, THE RIGHT MLG GREEN LIGHT ASSEMBLY POPPED OFF THE P2 PANEL IN THE COCKPIT. CREW PUT ASSEMBLY BACK TOGETHER TO VERIFY THE GEAR WAS SAFE WITH THREE GREEN LIGHTS, BUT THE LIGHT WOULD NOT WORK, EVEN WHEN HELD BACK IN POSITION. UPON ENTERING THE MSP AREA, THE CREW INITIALLY DECLARED AN EMERGENCY AND WHILE HOLDING, EXTENDED THE LANDING GEAR. THIS TIME THEY WERE ABLE TO GET THE RIGHT MAIN LANDING GEAR GREEN LIGHT TO ILLUMINATE. CREW THEN CANCELLED THE EMERGENCY AND VERIFIED GEAR WAS DOWN AND LOCKED THROUGH THE VIEWING PORTS. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG GREEN LIGHT SOCKET ASSEMBLY. OPERATION2L72 4F RTA16WE 20031010000352003101000035NM 2003 10 10 USAABB03145 120030823A3350873100151REV12 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU 27148 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031014000422003101400042CE 2003 10 14 GLBA2003134 120030917A3297 WIRE BEECH 1900 1900D 1154162CE MLG BROKEN A GLBAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM0397UX UE97 GEAR WILL NOT GO UP WHEN SELECTED. REPAIRED BROKEN WIRE BY POWER PACK. 2L72 4T RTA24CE 20031014000452003101400045NM 2003 10 14 SWAA032223 120031007A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 10. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20031014000472003101400047 2003 10 14 SWAA032221 420031007A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031202001582003120200158NM 2003 12 2 2003F00602 120030917A5210 ROLLER BOEING737 737800* NM PAX DOOR DISLODGED A MYWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19732MA 30618 AFTER TAKEOFF FROM PHX AND DURING CLIMB THE COCKPIT WAS INFORMED THE L1 DOOR WAS NOT SEALED. THE AIRCRAFT WOULD NOT PRESSURIZE. FOLLOWED ABNORMAL PROCEDURES AND CHECKLIST. RETURNED TO PHX WITHOUT INCIDENT. FOUND L1 DOOR UPPER AFT ROLLER NOT IN CHANNEL. INSPECTED ALL ROLLERS AND DOOR FRAME AND SEAL, NO DEFECTS FOUND. CYCLE DOOR SEVERAL TIMES, ALL OPS NORMAL IAW MM 52-11-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031202001602003120200160NM 2003 12 2 2003F00604 120030810A3220 SKID BOEING727 727231 1384079NM TAIL MALFUNCTIONED A FX7AJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1964346 21633 AFTER TAKEOFF WITH THE LANDING GEAR RETRACTED THE TAIL SKID REMAINED EXTENDED, RETURNED TO MIAMI DUMPED 15000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. CHECKED TAIL SKIN OPERATION AFTER CHECKING AREA AROUND TAIL SKIN FOR OBSTRUCTION PER MM 32-30-0 AND 32-00-11 WITH THE GEAR PINNED OPERATION WAS NORMAL AND A/C WAS RETURNED TO SERVICE WITH NOR FURTHER INCIDENT. (M) 2L73 4F A3WE 20031202001632003120200163SO 2003 12 2 SIMA200328806 120031008A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 DURING AN IMBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION, FABRICATED TWO DOUBLERS, SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 23, 53-21-10 PARA 4, AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031202001692003120200169NM 2003 12 2 AALA20031113 120031007A33503015643 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21382AN 25451 DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 22 THROUGH 34. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203000142003120300014NM 2003 12 3 GAIA03132ST 120031024A5347BAC1503100122 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND SEAT TRACK CORRODED BS 870 TO 1140 RBL 45 INCHES IN NUMEROUS SPOTS. REF FASI N/R NR 61567, REPLACED CORRODED SEAT TRACK PER B727 SRM 53-10-5 FIG 1. (M) 2L73 4F RTA3WE 20031203000372003120300037NM 2003 12 3 2003F00609 120030828A2910BACH8A08NN0360T LINE BOEING727 727212 138407GNM HYD SYSTEM WORN A PCSAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO17598AJ 21947 AFTER TAKEOFF, AIRCRAFT LOST SYSTEM 'A' HYDRAULICS. AIRCRAFT DIVERTED BACK TO MMUN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN ACTUATOR GEAR HYDRAULIC LINE WITH TEMPORARY FLEX LINE IAW MM 20-10-5, OPS CHECK AND LEAK CHECK NORMA. ITEM TRANSFER TO WDR NR 12704 IAW GMM CHAPTER 4 PAGE 12-1 EXPIRE AT NEXT AMERJET 'B' CHECK. AIRCRAFT WAS RETURNED BACK TO SERVICE. (M) 2L73 4F A3WE 20031203000402003120300040NM 2003 12 3 HALA0300965 120031026A2910 LINE BOEING717 717200 1383700NM HYD SYSTEM RUPTURED A HALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP13486HA 55131 ATB - EN ROUTE TO OGG GOT HYD RT PRESS LOW LIGHT FOLLOWED BY HYD RT QT LOW LIGHT HYD QUANTITY WHEN TO ZERO. RETURNED TO HNL AND PERFORMED APPROPRIATE QRH AND CHECK LIST. FOUND AUX PUMP PRESSURE LINE RUPTURED. REPLACED AUX PUMP PRESS LINE, LEAK OPS CHECK PENDING. OPS AND LEAK CHECK OK. (M) 2L72 4F TRA6WE 20031203000642003120300064NM 2003 12 3 AALA20031180 120031016A5347143T521142 SEAT TRACK BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21374AA 25201 FOUND SEAT TRACK AT STATION 764 LBL 11 HAD CORROSION BLENDED ON UPPER SURFACE OF FLANGES. BLEND OUT CORROSION. DYE CHECK FOR CRACKS. ALODINE THE BLENDED AREA. APPLY 2 COATS OF PRIMER. REINSTALL FASTENERS PER MRB 767-2527 DATED 10/07/2003. (M) 2L72 4F RTA1NM 20031203000692003120300069NM 2003 12 3 AALA20031161 120031019A33500201820001 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21388AA 27448 MAINTENANCE OBSERVED EMERGENCY LIGHT IN FRONT OF SEAT 21C INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203000752003120300075NM 2003 12 3 USAA030201 120030918A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US 23232 FOUND SKIN CRACKED .25 INCH LONG, LEFT ENTRY DOOR LOWER HINGE CUTOUT, AFT ENTRY DOOR. DAMAGE REMOVED, FILLER, DOUBLER AND TRIPLER FABRICATED AND INSTALLED PER SRM 51-40 AND EA 77022. (M) 2L72 4F RTA16WE 20031203000802003120300080NM 2003 12 3 USAASB03176 120031008A335020131A BATTERY BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19335US 23232 FOUND AFT GALLEY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2L72 4F RTA16WE 20031203001082003120300108EA 2003 12 3 ASOA03556 120031101A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52-00. (M) 2L72 4F RTA21EA 20031203001132003120300113EA 2003 12 3 A6WA200340131 120030815A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 FOUND FS 625 RIGHT UPPER OBLIQUE ANGLE, STRINGER 14 IS CRACKED APPROXIMATELY 2 INCHES. REMOVED AND REPLACED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M) 2L72 4F RTA21EA 20031203001252003120300125NM 2003 12 3 USAA030235 120031104A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US49565 23317 FOUND SKIN 2.75 INCH CRACK BS 882-884, 3/4 ABOVE STRINGER 26R. CUT OUT DAMAGE, INSTALLED DOUBLER, TRIPLER AND FILLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20031203001512003120300151WP 2003 12 3 AALA20031002 120030912A3350 LIGHT DOUG DC9 DC982 3022082WP EMERGENCY EXIT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2159523 49915 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE FORWARD GALLEY AISLE FLOOR. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040120000352004012000035NM 2004 1 20 03FDEA02246 120031226A5753ARC0154501 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, IB FLAP OB FWD HINGE PIVOT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75211, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040120000572004012000057NM 2004 1 20 03FDEA02232 120031220A5753ARC074414 ANGLE DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, FOUND OB FLAP WING SIDE IB HINGE, IB MOST FIXED FAIRING ATTACHING L ANGLE FWD LOCATION CRACKED. RT WING O/B FLAP WING SIDE I/B HINGE I/B MOST FIXED FAIRING ATTACHING L ANGLE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040120000582004012000058NM 2004 1 20 03FDEA02338 120031231A5510ALC81311 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STABILIZER LEFT UPPER AFT SPAR CAP 36L BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-7522, HORIZONTAL STABILIZER BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2L73 4F RTA22WE 20040120000642004012000064SO 2004 1 20 C2XA04IA001 120030103A33503104404 FUSE EMB 145 EMB145XR SO EMERGENCY LIGHT BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712126 145693 DURING PREFLIGHT INSPECTION THE CREW FOUND THE LEFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK FUSE AND OPERATIONALLY TESTED THE LIGHTING SYSTEM. 2L72 4F RT 20040121000072004012100007NM 2004 1 21 DHL2003748013 120031223A3260 DOWNLOCK SENSOR BOEING727 727225 1384077NM MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01748DH 22440 DURING ROLLOUT, LT GEAR UNSAFE LIGHT ILLUMINATED AND GEAR WARNING HORN SOUNDED. GREEN LIGHT ALSO REMAINED ILLUMINATED. AFTER CLEARING RUNWAY, LIGHT AND HORN EXTINGUISHED. WHEN TAXIING, HORN SOUNDED AND LIGHT ILLUMINATED AGAIN. AFTER BLOCK IN RED GEAR LIGHT ILLUMINATED. REMOVED AND REPLACED LT MAIN GEAR DOWNLOCK SENSOR IAW B-727 M/M CHAPTER 32-61-91, AND PERFORMED OPS CHECK IAW B-727 M/M CHAPTER 32-61-91 ITEM 5, OPS CHECKED GOOD. AURAL WARNING CIRCUIT BREAKER RESET. GEAR PINS REMOVED AND STOWED. 2L73 4F A3WE 20040121000252004012100025NM 2004 1 21 03FDEA02322 120031229A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 CORROSION AT SHEAR TIE BS 950F LBL 9, COMMON TO STR 29 LT. REMOVED CORROSION FROM SHEAR TIE 1 X2 X.009 INCHES FROM ORIGINAL OF .071. OUT OF LIMITS PER SRM 53-10-1. CUT OF SHEAR TIE AT BS 950F, LBL 9, COMMON TO STR 29 LT. AND REPAIRED FRAME IAW SRM 53-10-4 USEING .080 7075-T6 LOT 146378. 2L73 4F RTA3WE 20040121000362004012100036NM 2004 1 21 03FDEA02311 120031227A5753ARC74801 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING INBOARD FLAP VANE INBOARD SUPPORT FITTING INBD & OUTBD MOUNT HOLES WORN. COMPLIED WITH FEDEX EA 1-5750-75205 - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT INBOARD. FLAP VANE ATTACH FITTINGS REWORK. 2L73 4F RTA22WE 20040121000872004012100087EA 2004 1 21 A6WA200340198 120031221A2910 TUBE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A A6WAO OTHER K FLUID LOSS LDLANDING 1 GL31414ZW 7586 NR 2 HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED, FLUID INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC TUBE ASSEMBLY. (M) 2L72 4F RTA21EA 20040122000722004012200072NM 2004 1 22 ASAA0310180 120030321A53156546811516 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 986.5, LEFT BUTTOCK LINE 17, RIGHT BUTTOCK LINE 43 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040122000812004012200081SO 2004 1 22 SIMA200330201 120031028A335020131A BATTERY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 CREW REPORTED THE EMERGENCY LIGHTING BREAKER POPS OUT. DURING TROUBLESHOOTING MAINTENANCE FOUND THE NR 1 EMERGENCY BATTERY WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040122001132004012200113WP 2004 1 22 GTIA030960 120031108A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND AFT PIT INTERCOSTAL CRACKED AT CABIN FLOOR PANEL SCREWS AT FS 1287-1309 0 BL AND 2, MICARTA FLOOR PANEL SPACER DISBONDED. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2L72 4F RTA6WE 20040123000202004012300020WP 2004 1 23 ASAA0380822 120031210A52105910081167 SKIN DOUG DC9 DC983 3022083WP L1 DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS2083620836 53024 SEA PREFLIGHT CHECK, FOUND FORWARD PAX DOOR DENTED, CAUSING DOOR TO BE DIFFICULT TO OPEN. REPAIRED DENT PER SRM 52-05. RERIGGED DOOR. DOOR THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040123000752004012300075CE 2004 1 23 HYI2003F00019 120031107A573052220125 SEAL CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO RT WING UNSERVICEABLE D HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01402VN 402C0488 DURING FLIGHT, CREW NOTICED FUEL ESCAPING FROM RT UPPER ACCESS PANEL. ENGINES RUNNING NORMAL, EMERGENCY WAS DECLARED, LANDED WITHOUT INCIDENT. MECHANIC REMOVED AND REPLACED PANEL SEALS AND RELEASED AIRCRAFT BACK TO SERVICE. 1L72 3O3 O A7CE E8CE 20040123000772004012300077CE 2004 1 23 HYI2003F00020 120031111A324006600600 LINER CESSNA402 402C 207590RCE LT MLG BRAKE DAMAGED D HYIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NE016813J216 402C0641 AFTER LANDING, ON ROLLOUT, AIRCRAFT STARTED VEERING TO THE LEFT. CREW WAS UNABLE TO STRAIGHTEN OR TURN RIGHT EVEN WITH DIFFERENTIAL POWER OR RT RUDDER. AIRCRAFT WAS SHUTDOWN ON RUNWAY. TOWED TO HANGER. MECHANIC UNABLE TO DUPLICATE CONDITION, REMOVED AND REPLACED LT WHEEL AND BOTH BRAKE ASSEMBLIES AS A PRECAUTIONARY MEASURE. TAXI CHECK, OK. 1L72 3O A7CE 20040126000342004012600034SW 2004 1 26 HEEA087818 120030620A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X19 51412 BATTERY DEAD. TO BE SENT FOR WARRANTY REPAIR. 1G71 3U H2SW 20040126000482004012600048EU 2004 1 26 BAQA091854 120031229A33401179203103 CONTROL UNIT BOLKMS117 BK117A1 5626010EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME94 7243 CONTROL UNIT POPPING BREAKER, LIGHTS INTERMITTENT. PART REPLACED WITH SERVICEABLE UNIT. 01/08/2004 1G72 3U H13EU 20040126000522004012600052 2004 1 26 HEEA087799 420030616A2312N0001552 ANTENNA SKRSKYS76 S76A 8143006NE VHF SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 ANTENNA INTERMITTENT RECEPTION. REPAIRED. 1G72 3U H1NE 20040126000542004012600054 2004 1 26 HEEA087801 420030608A2340PHI20004 MIXER BOX SKRSKYS76 S76A 8143006NE COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 MIXER BOX CAUSING STATIC IN CABIN ICS. FOUND VOLUME KNOB, SELECTOR KNOB AND LIGHT PANEL BAD. REPLACED. BENCH CHECK GOOD. 1G72 3U H1NE 20040126000592004012600059 2004 1 26 HEEA087811 420030617A34225050010902 GYRO BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038587X 51464 GYRO SPINS EXCESSIVELY. SHOP REPAIR. 1G71 3U H2SW 20040121000742004012100074EA 2004 1 21 ASOA03605 120031125A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA RT AC PACK DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11865AS 7507 DURING CRUISE FROM DFW-ORD, THE FLT ATTENDANT AND CREW NOTICED A STRONG ODOR IN THE CABIN EMANATING FROM THE PACK. THE CREW TURNED OFF THE RIGHT PACK AND THE ODOR WENT AWAY. THE AIRCRAFT LANDED SAFELY IN ORD. MAINTENANCE OPERATED THE LEFT AND RIGHT PACKS WITHOUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121000962004012100096CE 2004 1 21 2004F00048 120031204A5311 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1753545 UE185 AT SCHEDULED EMPENNAGE ZONE INSPECTION, FOUR CRACKS FOUND RADIATING FROM PASSAGE HOLE IN FORWARD WEB OF THE HORIZONTAL STABILIZER FORWARD SPAR. STOP DRILLED CRACKS. FABRICATED AND INSTALLED AND EXTERNAL DOUBLER IAW FAA APPROVED DATA CONTAINED IN THE BEECH 1900D AIRLINER SERIES STRUCTURAL REPAIR MANUAL, CHAPTER 55-91-02. (M) 2L72 4T RTA24CE 20040122000912004012200091WP 2004 1 22 AALA20031245 120031107A2170 COALESCER BAG DOUG DC9 DC982 3022082WP AIR CON SYS INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21227AA 49177 SMOKE IN CABIN. RETURNED BWI AND LANDED WITHOUT INCIDENT. REPLACED COALESCER BAG AND REPLACED APU DRAIN O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040122001002004012200100EA 2004 1 22 ASOA03637 120031208A53306013600130 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11861AS 7445 DURING AN A-CHECK IN BTR, THE DOUBLER ON FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ANGLE ON FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE IAW SRM 51-00-00 AND 51-42-06. (M) 2L72 4F RTA21EA 20040122001182004012200118EA 2004 1 22 ASOA03631 120031206A5210601R31903319 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11859AS 7421 DURING A GROUND INSPECTION IN DFW, THE MAIN PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE AND THE OUTER HANDLE WOULD NOT ROTATE. MAINTENANCE ADJUSTED THE MAIN PASSENGER DOOR LATCH MECHANISM IAW AMM 52-11-02. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001192004012200119EA 2004 1 22 ASOA03632 120031206A5220600313941 FITTING CNDAIRCL600 CL6002B19 1900309EA EMERGENCY DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 FLT 4643 - DURING A TRAINING EXERCISE IN ATL, THE LEFT OVERWING EMERGENCY EXIT DOOR AT ROW 8 A/B COULD NOT BE OPENED. MAINTENANCE ADJUSTED THE BEYONET LATCH FITTINGS ON THE LEFT OVERWING EMERGENCY EXIT DOOR AT ROW 8 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001212004012200121EA 2004 1 22 ASOA03630 120031204A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE FLOOR SILL AT FS 349 TO FS 364 ON THE RIGHT SIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SILL AT FS 349 TO FS 364 ON THE RIGHT SIDE IAW ASA EO 600-53-0129. (M) 2L72 4F RTA21EA 20040123000012004012300001EA 2004 1 23 A6WA200340133 120030904A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM01403AW 7288 AFTER TAKEOFF ON GEAR RETRACTION GOT RED GEAR DISAGREE AND RED NOSE GEAR DOORS CAS MESSAGE. REMOVED AND REPLACED NOSE LANDING GEAR ASSEMBLY. OPS AND LEAK CHECK GOOD. (M) 2L72 4F RTA21EA 20040123000042004012300004 2004 1 23 ASAA0380749 420031117A25653961896501 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01934AS 49235 SEA PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20040123000602004012300060NE 2004 1 23 MDR03018 120030703A64106516000025101 STRAP SKRSKYS64 S64F 8142610NE PWA JFTD12JFTD12A4A 52047NE TAIL ROTOR BLADECRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09223AC1632 64V63133541464086 THE STRAP IS CRACKED N THE OUTBOARD SIDE OF THE BLADE, APPROXIMATELY 9.125 INCHES FROM THE TRAILING EDGE. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS APPROXIMATELY 1.25 INCHES TOWARDS THE TIP END OF THE BLADE. THE CRACK STARTS WHERE THE BACK WALL OF THE SPAR AND THE LEADING EDGE OF THE FAIRING INTERSECT. CAUSE NOT KNOWN, MFG IS INVESTIGATING. 2G72 4U4 U H6EA E15EA 20040122000872004012200087NM 2004 1 22 ASAA0310183 120030321A5315 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND FLOORBEAM AT BODY STATION 540-616, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040114001152004011400115NM 2004 1 14 DL75K031049 120031124A2740285T0015116MODC MODULE BOEING757 757232 1384965NM E/E BAY FAULTY A DALAK NONE F FLT CONT AFFECTED APAPPROACH 1 SO276709 30481 ON SHORT FINAL, UNSCHEDULED STAB TRIM LIGHT ILLUMINATED WITH AURAL WARNING. AIRCRAFT WAS BEING HAND FLOWN, AUTO-PILOT OFF. ON ROLLOUT STAB TRIM INDICATED 11 DEG NOSE UP. THERE WAS NO TRIM INPUT BY PILOT FLYING DURING FINAL APPROACH. REPLACED RT SAM. 2L72 4F RTA2NM 20040114001192004011400119NM 2004 1 14 DLM88031052 120031125A2450595663951 CONTROL PANEL DOUG MD88 MD88 3023688NM E/E BAY DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27924DL 49711 FOUND E/E DOOR DENTED POWER CONTROL PANEL AT DOOR HOLD OPEN SUPPORT BRACKET. FOUND RELAY WIRES ARCHING BEHIND PANEL ASSY ON RACK SUPPORT BRACKET. REPAIRED WIRING. 2L72 4F RTA6WE 20040114001372004011400137NE 2004 1 14 SW07200300002 220030416A72504120T01P02 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE MISSING G FDKAK NONE O OTHER ININSP/MAINT 1 SW07504MJ1136 10066 E965322 BOROSCOPE INSPECTION REVEALED THE LOSS OF HIGH PRESSURE TURBINE BLADES. 2L72 4F4 FRTA21EA EOOO63EN 20040114001592004011400159WP 2004 1 14 AALA20031475 120031228A33500211720004 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 DFW DURING OVERNIGHT MAINTENANCE FOUND AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 6E INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040114001652004011400165NM 2004 1 14 DL73S030975 120031029A52306546861X STOP FITTING BOEING737 737232 1384475NM CARGO DOOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 DURING ACCOMPLISHMENT OF EO 3-059252-3AD, OPN 0301, (S/B 737-52A1100), A 65-46861-0) FITTING WAS FOUND. EO INSTRUCTIONS REQUIRE ENGINEERING EVALUATION. EVALUATION FOUND THAT FITTING REQUIRED REPLACEMENT PER S/B 737-52-1065. FITTING REPLACED PER S/B 737-52-1065 PER DELTA ERA 423638-14AD. 2L72 4F RTA16WE 20040114002112004011400211NM 2004 1 14 MWEA030482 120031215A53305911406501 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FUSELAGE SKIN DENTED AT STATION 218 LONGERON 18 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F RTA6WE 20040114002132004011400213NM 2004 1 14 MWEA030485 120031215A57535930496508 SKIN DOUG MD88 MD88 3023688NM FLAP VANE DELAMINATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RT FLAP OUTBOARD FIXED VANE APPROXIMATELY 3 INCHES SQUARE OF DELAMINATION ON BOTTOM FACE. FABRICATED AND INSTALLED FILLERS AND DOUBLER. 2L72 4F RTA6WE 20040114002322004011400232EA 2004 1 14 03361625 120031227A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27625BR 7214 DURING CRUISE, CREW REPORTED THE CAPTAINS SIDE WINDOW CRACKED. THE AIRCRAFT WAS FERRIED TO ORD WERE THE WINDOW WAS REPLACED AND A SATISFACTORY PRESSURIZATION CHECK WAS PERFORMED ON THE AIRCRAFT. THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040115000352004011500035NM 2004 1 15 03FDEA02045 120031204A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION ON BS 312 FLOORBEAM UPPER CHORD, LBL 19.5, WL 208. REMOVED CORROSION ON BS 312 FLOOR BEAM UPPER CHORD AT LBL 19.5 IN AREA OF 1 X 1 X .025 INCH MAX REMOVED. FOUND TO BE OUT OF LIMITS. FABRICATED THE REPAIR PART MADE FROM 7075-T6 0.063, AND INSTALLED THE REPAIR PARTS IAW SR DRAWING 27-53-0 2L73 4F RTA3WE 20040115000572004011500057NE 2004 1 15 DL757031084 220031214A7200PW2037RTC ENGINE BOEING757 75726D 1384907NM PWA 2037 PW2037 NE NR 2 FAILED A DALAC ABORTED TAKEOFF RA PARTIAL RPM/PWR LOSS FLAME/FIRE TOTAKEOFF 1 SO27900PC15447 727298 28446 727298 AFTER THROTTLE UP TO T/O POWER AND AS BRAKES RELEASED FOR T/O FROM SNA THE RIGHT ENG HAD AN AUDIBLE COMPRESSOR STALL, IT COULD ALSO BE FELT IN COCKPIT. FLAMES REPORTED TO BE SEEN OUT OF TAILPIPE. ENG CONTINUED TO OPERATE AT 62 PERCENT, N2 WITH EGT HIGH OF 580 DEG. ABORTED T/O BELOW 30 KTS. MTC INSPECTED ENG AT GATE AND FOUND METAL/BLADES IN TAILPIPE. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20040115000702004011500070EU 2004 1 15 03FDEA00016 120030111A7830 THRUST REVERSER AIRBUS300 A300B4605R 3930308EU NR 1 ENGINE INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25683FE 801 ON TAKEOFF ROLL, CYMX, RWY27, ECAM MEMO PAGE DISPLAYED WARNING THAT NR 1 REVERSER SYSTEM WAS PRESSURIZED. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A ENGINE NR 1 THRUST REVERSER INOP, THRUST (1 OR 2). REVERSER DEACTIVATED IN FORWARD THRUST POSITION. NR 1 THRUST REVERSER OPS CHECK GOOD PER A300 AMM 78-31-00-5. RETURNED NR 1 THRUST REVERSER TO OPERATIONAL STATUS. 2L72 4F RTA35EU 20040115001022004011500102NM 2004 1 15 03FDEA02075 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 3 BANJO FITTING (AJC7053-503) FWD FACE FLANGE FOUND WITH 02 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 3 BANJO FITTING AJC7053-503 FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL2 & REPLACED AS PER SRM 51-33-01 VOL2 & SRM 51-38-01 VOL2. 2L73 4F RTA22WE 20040115001782004011500178NM 2004 1 15 TSAA0336200 120031207A36201296662 SWITCH BOEING737 73776N 13844CHNM NR 1 ENGINE FAILED A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13743AL 28654 CLIMBING THROUGH ABOUT 7000 FEET THE LT ENGINE BLEED TRIP LIGHT ILLUMINATED. QRH ACCOMPLISHED. A RESET WAS ATTEMPTED THREE TIMES. RETURNED TO HNL. OVERWEIGHT LANDING AT 147,500 LBS. TOUCHDOWN RATE OF DESCENT LESS THAN 300 FPM. REMOVED AND REPLACED 390 DEGREES FAHRENHEIT PRE-COOLER VALVE SENSOR P/N 975-0172-006, IAW 36-12-03-4. OPS CHECK GOOD. VERIFIED NO BLEED TRIP OFF LIGHT ILLUMINATED. REPLACED 490 DEGREES FAHRENHEIT OVERTEMP SWITCH. RAN ENGINES OPS CHECK GOOD. ACCOMPLISHED OVERWEIGHT LANDING CONDITIONAL INSPECTION IAW 05-51-35-2. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040120000042004012000004NE 2004 1 20 AALA20031435 220031215A7230 BLADE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE COMPRESSOR DAMAGED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21709TW 28168 EWR T785/15 EN ROUTE, ON CLIMBOUT AT 20,000 FT EXPERIENCED TWO COMPRESSOR STALLS FROM RT ENGINE. RT ENGINE LT AT IDLE AND LANDED EWR WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. ON BOROSCOPE OF 6TH STAGE COMPRESSOR BLADES FOUND 18 DAMAGED BLADES AND 1/4 OF 1 BLADE MISSING. NINTH STAGE 30 DAMAGED BLADES AND 1/4 OF 1 BLADE MISSING. FIFTEENTH STAGE ALL BLADES DAMAGED. RT ENGINE REPLACED PER WORKCARD M577101. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F4 FRTA2NM E17NE 20040120000052004012000005 2004 1 20 03FDEA02208 420031216A220025887221 COUPLER BOEING727 727100 1384036NM YAW DAMPER FAILED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25107FE 19202 LOWER YAW DAMPER RUNAWAY - LT AND RT AFTER TAKEOFF - LYD SWITCH TURNED OFF. REMOVED AND REPLACED LOWER YAW DAMP COUPLER IAW 727-100 MM CH 22-11-131-4. OPS CHECKS NORMAL ON GROUND. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20040122001312004012200131 2004 1 22 GTIA030955 420031127A2565D29982121 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FLL - R-1 DOOR EMERGENCY/ESCAPE SLIDE WILL NOT STOW PROPERLY, GIRT OPENING DRAGS. REMOVED AND REPLACED R-1 DOOR EMERGENCY/SLIDE. (M) 2L72 4F A6WE 20040123000322004012300032EU 2004 1 23 KBM2003F00083 120031109A2913P94B12209 PUMP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE FUEL SYSTEM INOPERATIVE E KBMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP19313LV 3296 FUEL PRESSURE LIGHT FLICKERS IN FLIGHT. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040123000422004012300042 2004 1 23 KBM2003F00108 420031119A3423CB2100T4 COMPASS BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL COCKPT LOW E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 COMPASS FLUID LEVEL LOW. INSTALLED OVERHAULED COMPASS. 1G71 3U3 U H2SW E4CE 20040126000182004012600018EU 2004 1 26 BAQA091972 120031228A6340L771M40C1014 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE RPM MALFUNCTIONED B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03911NH7 0273 TRIPLE TACH INDICATOR N2 WILL NOT PERFORM SWEEP CHECK. UNIT ONLY LASTED 6.8HRS WHEN INSTALLED. REPLACED WITH SERVICEABLE UNIT. 01/14/2004 1G72 3U H88EU 20040126000332004012600033SW 2004 1 26 HEEA087817 120030613A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034179152 51465 BATTERY WEAK. SENT FOR WARRANTY REPAIR. 1G71 3U H2SW 20040126000372004012600037SW 2004 1 26 HEEA087808 120030608A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032260813056 33075 UPPER TRAILING EDGE FRETTING PAD IS SEPARATED. SENT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20040127001442004012700144NM 2004 1 27 ASAA0310219 120030325A49106550904278 FRAME BOEING737 737298C 1384490NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND APU COWLING FRAME AT BS 1088-1156, STRINGER 18R CHAFED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20040127001572004012700157NM 2004 1 27 ASAA0310202 120030321A5313BAC1498516 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 22L AT BS 957, CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20040127001642004012700164NM 2004 1 27 ASAA0310174 120030320A53207075T6040 WEB BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CUSP WEB AT BS 344-360, RIGHT BUTTOCK LINE 62 CRACKED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040127001662004012700166NM 2004 1 27 ASAA0310172 120030320A5310 DOOR FRAME BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND E/E DOOR FRAME WEB AT BS 320, STRINGER 28L-28R CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031208000032003120800003NM 2003 12 8 2003UALA00781 120031016A2730 CONTROL CABLE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ELEVATOR OBSTRUCTED A UALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 WP29905UA 25005 CREW REPORTS THAT ELEVATOR BINDS WHEN PULLING CONTROL COLUMN BACK. STICKS AND BINDS TO THE POINT OF HAVING TO USE EXCESSIVE PRESSURE TO GO BACK TO NEUTRAL. FLIGHT CREW REPORTED THAT COLUMN WAS TOTALLY STUCK AT ONE POINT. DURING AN INSPECTION OF THE ELEVATOR CONTROL SYSTEM A LARGE PIECE OF VELCRO WAS FOUND LODGED BETWEEN AN ELEVATOR CABLE PULLEY AND CABLE RETAINER IN THE FORWARD E&E COMPARTMENT. THE ELEVATOR SYSTEM WAS CYCLED AND FOUND TO OPERATE NORMALLY AFTER FOD REMOVAL. 2L72 4F4 FRTA16WE E2GL 20031208000092003120800009 2003 12 8 DXTA200300154 420031105A221699141977 CONTROL MODULE CESSNA650 650 2076802CE AUTOPILOT FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07779QS6 6507079 AFTER .5 HRS CRUISE, AT FL370 WITH AUTOPILOT ON , MASTER WARNING LIGHT WOULD COME ON, WITH NO OTHER FAULT LIGHTS, AUTOPILOT REMAINED ON EACH TIME. AFTER DISENGAGING AUTOPILOT IN DESCENT, PRIMARY TRIM FAIL AND MASTER WARNING LIGHT ILLUMINATED EACH TIME TRIM WAS ENGAGED. REPLACED K237 PN MS83536/9-024 S/N N/A. REPLACED STAB ACTUATOR CONTROL UNIT. OPS CHECKED GOOD IAW CE 650 CHAPTER 27-40-01. 2L72 4F A9NM 20031208000172003120800017NM 2003 12 8 UPS03M41576 120031127A3350 LIGHT DOUG MD11 MD11F 3023600NM CABIN WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01270UP INSPECTION TYPE:PFLT EMERGENCY LIGHTS WILL NOT TEST. DEFERRED PER MEL 33-50-2. REF M271306. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM. OPS CHECKED NORMAL. THIS CLEARS M271306. REF LP675424 2L73 4F RTA22WE 20031208000182003120800018WP 2003 12 8 ARWA20031104 120031128A323269003213 ACTUATOR LKHEED1011 1011385115 5265015WP MLG DOOR FAILED A ARWAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO19308GB 193U1133 LT GEAR, IN TRANSITION, DOOR. FE DOOR LIGHTS ON; GEAR RETRACTED. REMOVED AND REPLACED LANDING GEAR DOOR LT ACTUATOR IAW MM 32-33-08. COMPLETED TEST IAW MM 32-61-07. ALL SYSTEMS CHECKED NORMAL, NO GEAR SWING. 2L73 4F A23WE 20031208000272003120800027NM 2003 12 8 03FDEA01789 120031021A5712ARB2850505 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LT WING SLAT TRACK NR 16 INBOARD SUPPORT RIB CRACKED. LT WING SLAT TRACK NR 16 INBOARD SUPPORT CRACKED RIB REMOVED AND REPLACED AS PER SRM 51-31-01, VOL. II. 2L73 4F RTA22WE 20031014000592003101400059NM 2003 10 14 SWAA032175 120030930A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SERVICE CHECK, FOUND RT OUTBOARD T/E AFT FLAP DELAMINATED AND SECTION OF INSIDE CORE MISSING. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20031014001642003101400164NM 2003 10 14 SWAA032090 120030918A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CORRODED AT BS 859. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031014001752003101400175NM 2003 10 14 SWAA032079 120030918A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 FUSELAGE SKIN CRACKED AT BS 516D, STRINGER 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014002002003101400200EU 2003 10 14 BAQA089652 120030716A2435 BRUSHES BOLKMS117 BK117A1 5626010EU STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME621 23688 7243 BRUSHES WORN BEYOND SERVICEABLE LIMIT. REPLACED WITH SERVICEABLE(ASSET)UNIT. 10/8/03 1G72 3U H13EU 20031015000692003101500069NM 2003 10 15 AMTA200301241 120030930A2421727792M IDG BOEING757 75723N 1384973NM GENERATOR INOPERATIVE A AMTAO OTHER J WARNING INDICATION DEDESCENT 1 GL11516AT 27972 EICAS MSG GEN DRIVE DISPLAYED GEN DRIVE LIGHT ILLUMINATED AFTER START OF DESCENT. GEN DRIVE DISCONNECTED. REMOVED AND REPLACED LT IDG PER M57-2401, MM 24-11-01 LEAK CHECKED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20031020000462003102000046EU 2003 10 20 RAIA00310256 120031007A3350334 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03558HK 41071 5494-COU- EMERGENCY ESCAPE PATH LIGHT INOP AT 8A. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. 2L72 4T RTA41NM 20031020000682003102000068NE 2003 10 20 VNAA0310002 320031003A6140 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PROP INDICATING CONTAMINATED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07422JS 3018 DURING TAKEOFF, THE CREW RECEIVED A PROP OVERSPEED CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND FOUND FLUID ON THE CONNECTOR. MAINTENANCE CLEANED THE CONNECTOR IN ACCORDANCE WITH STANDARD MAINTENANCE PRACTICES AND THE DEFICIENCY COULD NOT BE DUPLICATED. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031020000942003102000094SO 2003 10 20 C2XA03SH374 120031008A532013500469403 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 SHV- DURING C-CHECK THE RIGHT HAND SILL AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031020000952003102000095SO 2003 10 20 C2XA03SH376 120031008A532014522460011 STRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 SHV- DURING C-CHECK THE CENTER STRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031020001182003102000118NM 2003 10 20 SCNA03008 120031004A3350 LIGHT BOEING737 7378Q8 13844BXNM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15805SY 30032 FOUND RIGHT FWD OVERWING EMERGENCY LIGHT INOP. RELAMPED RIGHT FWD OVERWING EMERGENCY LIGHT, OPS CHECKED GOOD. 2L72 4F RTA16WE 20031020001192003102000119EA 2003 10 20 JBXA03018 120031004A2720 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A JBXAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO05571ML 7209 RDU- FLIGHT 5206- ON TAKEOFF ROLL HAD RUDDER CONFIGURATION MESSAGE. RETURNED TO GATE. MAINTENANCE SYSTEM CHECKED RUDDER IAW CRJ AMM 27-21-00-710. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031020001202003102000120 2003 10 20 RAIA00309249 420030930A34257003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03573HK5015 3284 41092 5583-STL- AHRS NR 2 FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 2 AHRS COMPUTER. 2L72 4T RTA41NM 20031020001472003102000147NM 2003 10 20 DL78K030797 120030830A3350D71702001 POWER SUPPLY BOEING737 737832 13844CFNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO273734B 30776 FOUND RT AFT OVERWING ESCAPE HATCH EXIT LIGHT INOP. REPLACED POWER SUPPLY. 2L72 4F RTA16WE 20031020001512003102000151NM 2003 10 20 DL777030802 120030902A33500201728001 LIGHT BOEING777 777232 1385232NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27862DA 29734 PASSENGER SEAT 38G SEAT MOUNTED ESCAPE PATH LIGHTING INOP. RELAMPED, DID NOT HELP. REMOVED AND REPLACED LIGHT ASSEMBLY AT SEAT 38G. OPS CHECKS OK. 2L72 4F RTT00001SE 20031020001632003102000163NM 2003 10 20 DL76L030789 120030828A5753113N280095H FLAP BOEING767 767332 1382001NM LT WING DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27178DN 25143 LEFT WING INBOARD AFT FLAP DISBONDED. REPAIRED PER ER/A 423421-14. 2L72 4F RTA1NM 20031208000412003120800041WP 2003 12 8 UPS03841463 120031024A2612 BATTERY DOUG DC8 DC871F 302199DWP FIRE DETECTION INOPERATIVE A IPXAO OTHER N FALSE WARNING DEDESCENT 1 SO01702UP 45902 THE LOWER COMPARTMENT FIRE LIGHT CAME ON FOR THE FORWARD A COMPARTMENT. THE FIRE WARNING LIGHT WENT OUT & CHANGED TO A MAINT LIGHT. THE LOWER COMPARTMENT LIGHT WAS ON LESS THAN 20 SEC BEFORE IT CHANGED TO MAINT LIGHT. PERFORMED T/S TO THE LOWER CARGO FIRE WARNING SYS FOUND CCU FAULTY BUT DID NOT FIX PROBLEM. WITH FWD A BELLY 31 STILL SHOWS INOPERATIVE BATTERY FA 12560 SHOWS LOW DEFERRED PIT 31. 2L74 4F RT4A25 20031208000522003120800052NM 2003 12 8 03FDEA01785 120031021A2780 SWITCH BOEING727 727200 138407ENM TE FLAPS MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25273FE 22038 ON FLAP RETRACTION FROM 5 DEG TO 2 DEG, LED NR 5 (RT SIDE) DID NOT FULLY RETRACT. AMBER LIGHT ILLUMINATED ON LED POSITION INDICATOR AFT BULKHEAD. COMPLIED WITH RED TABS, DID NOT CORRECT PROBLEM. REMOVED AND REPLACED NR 5 L/E FLAP POSITION SWITCH IAW MM 27-82-001-4. FLAP/SLAT INDICATION NORMAL WITH NUMEROUS EXTENSION AND RETRACTION. 2L73 4F RTA3WE 20031208000582003120800058NE 2003 12 8 03FDEA01795 220031023A7261 PRECOOLER AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE NR 1 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25660FE 759 COMPLY WITH EA 6-5452-73216 NACELLES/PYLONS - REPAIR OF CRACKS IN NR 1 ENGINE PYLON PRECOOLER PANEL. COMPLIED WITH EA 6-5452-73216 NACELLES/PYLONS - REPAIR OF CRACKS IN NR 1 ENGINE PYLON PRECOOLER PANEL AT BFM/MAE. 2L72 4F4 FRTA35EU E13NE 20031208000622003120800062EU 2003 12 8 03FDEA01799 120031024A5730EADSRS72491521 SKIN AIRBUS310 A310203 3930313EU ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25442FE 353 MEM MX REPORTS A .8 CRACK IN THE LT LOWER WING SKIN AT RIB 11. COMPLIED WITH WORK CARD T6-5710-66977 WRI 57105494 AT CWF BY INSTALLING NEW DOUBLER PER EA6-5710-66977 PT3 AND AIRBUS DRAWING R57249152 AND EA6-5710-73414A AND NRC S00002. 2L72 4F RTA35EU 20031208000652003120800065EA 2003 12 8 QXEA200301315 120031021A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 MAIN CABIN DOOR OUTER SKIN BENT AT LOWER FORWARD CORNER. REPAIRED IAW HORIZON AIR EA R-52-132. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031208000662003120800066EA 2003 12 8 03295708 120031022A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27708BR 7575 DURING INSPECTION THE EMERGENCY TRACK LIGHTING AFT OF ROW 8 WAS FOUND INOPERATIVE. 2L72 4F RTA21EA 20031208000802003120800080SO 2003 12 8 MASA200300405 120031012A3350AE20131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07842MJ 145457 THE EMERGENCY EXIT LIGHTS INOP. A/C FERRIED TO PIT. MX REPLACED THE BATTERY PACKS. 2L72 4T RTT00011AT 20031208000832003120800083NM 2003 12 8 C1HA200396019 120031026A5240 DOOR BOEING727 7272J4 1384006NM SERVICE NOT CLOSED A C1HAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15696CA 22574 SHORTLY AFTER TAKEOFF A LOUD NOISE FROM AIRCRAFT FORWARD WAS HEARD. THE AIRCRAFT WAS NOT PRESSURIZING. THE 1R DOOR APPEARED NOT TO BE PROPERLY SEALED. NO DOOR LIGHTS WHERE ILLUMINATED ON THE F/E'S PANEL. AN EMERGENCY WAS DECLARED. FUEL WAS DUMPED, LANDING WAS SMOOTH. INSPECTED CARGO/PASSENGER DOOR, FOUND 1R DOOR PARTIALLY OPEN DOWN POSITION TO CHECK DOOR NORMAL OPERATION CLOSED AND OPEN TO CONTINUE OPERATION. REF LOG PAGE B11021 ITEM 1. EMERGENCY MAINT PERFORMED IN PUJ FOUND EMERGENCY MAINT THAT WAS PERFORMED IN PUJ TO BE WITHIN CHAMPION AIR STANDARDS, NO DEFECTS NOTED. 2L73 4F RTA3WE 20031208000922003120800092NM 2003 12 8 QXEA200301324 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 LEFT OUTBOARD TRACK NR 2 SEAT ATTACH AREA CORROSION UNDER INBOARD LUG, APPROXIMATELY X455.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2H72 4T RTA13NM 20031208001032003120800103NM 2003 12 8 QXEA200301332 120031002A5320 THRESHOLD DHAV DHC8 DHC8202 2809007NM ZONE 800 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - ALL NUT PLATES UNDER PASSENGER DOOR THRESHOLD SHOW EVIDENCE OF CORROSION. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20031208001082003120800108NM 2003 12 8 AWXA200301306 120031002A532069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK .125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN AFT CARGO COMPARTMENT AT BS 727E, STR 25 RT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 727E, STR 25 RT IAW B737-300 SRM 51-40-02 PG 1, 38, & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031208001232003120800123EA 2003 12 8 QXEA200301351 120031023A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09615QX2683 2683 10065 BOI- ON FLIGHT 2430 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 2 AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031208001242003120800124EA 2003 12 8 QXEA200301352 120031024A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09615QX2390 2265 10065 ON FLIGHT 2547 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 2 AFT SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031208001302003120800130SO 2003 12 8 C2XA03SH417 120031027A541114576631621 STRUCTURE EMB 145 EMB145LR 3260212SO LT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711539 145536 SHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 145 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031208001332003120800133EU 2003 12 8 YENA200328 120031027A5242 DOOR AIRBUS320 A320232 3930326EU E/E BAY OPEN A YENAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA15527JB 1557 ON CLIMBOUT DOOR AVIONICS BAY OPEN INDICATION ON ECAM. RETURNED TO JFK. CLOSED AND SECURED MAIN AVIONIC DOOR, NO ABNORMALITIES. 2L72 4F RTA28NM 20040120000072004012000007NM 2004 1 20 EIA2003170 120031216A335090085 POWER SUPPLY BOEING747 747SR46 1384816NM EMERGENCY LIGHTSINOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BOTH EMERGENCY LIGHTS ON CREW SERVICE DOOR INOPERATIVE. R & R POWER SUPPLY, OPS CHECKED GOOD IAW MM 33-51-00. 2L74 4F RTA20WE 20040120000102004012000010 2004 1 20 2003UALA00958 420031214A2330 CIRCUIT BOARD BOEING777 777222 1385219NM PWA PW4077PW4077 NE SEAT 13F VDU FAILED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29781UA 26945 SMOKE COMING OUT OF SEAT ELECTRONIC UNIT. DISCONNECTED WIRES TO UNIT AND POWER SWITCHED OFF TO ENTERTAINMENT SYS AND LAPTOP POWER. THE VIDEO DISTRIBUTION BOX AT SEAT 13F FAILED. THE UNIT WAS REPLACED AND ENTERTAINMENT SYSTEM OP CHECKED OKAY. THE UNIT WAS EXAMINED IN COMPONENT SHOP AND FOUND CHIP FAILURE ON THE MAIN CIRCUIT BOARD. 2L72 4F4 FRTT0001SE E46NE 20040120000202004012000020CE 2004 1 20 DXTA200300207 120031221A3213 STRUT CESSNA750 750 2076810CE NLG DISCHARGED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07956QS 7500156 AFTER TAKE-OFF ATTEMPTED TO RETRACT GEARS AND FOUND LANDING GEAR HANDLE WOULD NOT GO UP. ACCOMPLISHED AIR TURN BACK. FOUND NOSE STRUT NITROGEN PRESSURE LOW, NOT ALLOWING STRUT TO FULLY EXTEND TO MAKE SQUAT SWITCH. SERVICED NOSE STRUT AS REQUIRED IAW CESSNA 750 MM CHAPTER 12-10-38, OPS CHECKED GOOD WITH GEAR SWING. 2L72 4J RTT00007WI 20040120000262004012000026NM 2004 1 20 03FDEA02305 120031227A5740 FITTING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, IB FLAP VANE IB TEE FITTING MOUNT HOLES (3 EA.) WORN. COMPLIED WITH FEDEX EA 1-5750-75214, TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBOARD FLAP VANE ATTACH FITTING REWORK. 2L73 4F4 FRTA22WE E13NE 20040120000372004012000037NM 2004 1 20 03FDEA02248 120031226A5753ARC2512503 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING - IB FLAP OB HINGE FITTING IB PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75212, TITLE: WINGS TRAILING EDGE AND TRAILING EDGE DEVICES- LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F4 FRTA22WE E13NE 20040120000442004012000044NM 2004 1 20 03FDEA02335 120031230A5321WSP0786501 FLOOR PANEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK FLOOR PANEL 233VF FOUND TOP SURFACE WITH CORROSION. FLOOR PANEL 233VF REMOVED AND REPLACED AS PER MM 53-21-04-4. 2L73 4F RTA22WE 20040120000452004012000045NM 2004 1 20 03FDEA02337 120031230A5512ALC81032 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STABILIZER RT UPPER AFT PLANK 35R BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-7522, HORIZONTAL STAB BARREL NUT BORE REWORK A.D. 2003-22-08. 2L73 4F RTA22WE 20040120000652004012000065EU 2004 1 20 03FDEA02243 120031224A215032910481 ACTUATOR AIRBUS300 A300F4605R 3930327EU A/C PACK FAILED A FDEAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO25667FE11386 771 ON LANDING AT YMX COCKPIT AND COURRIER AREA FILLED WITH SMOKE AND MAIN DECK CARGO SMOKE DET SYSTEM ACTIVATED IN ALL ZONES. SMOKED CLEARED AFTER 5 MIN. SUSPECT EXHAUST FUMES ENTERED AIR CONDITIONING SYS, RELEASED FOR SERVICE PER MEL/CDL: 21-11-08-B MEL 21-11-08-B: PACK (IDENTIFY 1 OR 2). FOUND LEFT PACK OVERHEATING IN AUTO MODE, OPS NORMAL IN MANUAL MODE. FURTHER T/S FOUND BY-PASS VALVE ACTUATOR MODULATING WITH NO PACK AIR APPLIED, SWAPPED PACK TEMP CONTROLLERS, NR 1 PACK ACTUATOR STILL MODULATING, REMOVED CANNON PLUG FROM BY-PASS VALVE, ACTUATOR CONTINUED MODULATING, ONLY STOPPING BLEED PROBLEM ON NR 1 ENGINE, WHEN REPAIRED CLEARED LT PACK PROBLEM. NR 1 PACK OPS. 2L72 4F RTA35EU 20040121000112004012100011NM 2004 1 21 03FDEA02265 120031226A5710ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT WING - O/B FLAP I/B HINGE FITTING I/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000282004012100028NM 2004 1 21 03FDEA02319 120031228A5511 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB RT UPPER AFT SPAR CAP 36 RT BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-75222, HORIZONTAL STAB BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2L73 4F RTA22WE 20040121000312004012100031NM 2004 1 21 03FDEA02316 120031226A5510ALC81032 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB RT UPPER AFT PLANK 30R BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-7522, HORIZONTAL STAB BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2L73 4F RTA22WE 20040114001402004011400140NM 2004 1 14 DL75A031068 120031202A2621346000104 BOTTLE BOEING757 757212 1384951NM CARGO BAY DEFECTIVE A DALAK NONE J WARNING INDICATION ININSP/MAINT 1 SO27757AT 23127 NOTICED AFTER COCKPIT INDICATOR LIGHTS TEST, CARGO BOTTLE 1 DISCHARGE LIGHT REMAINED ILLUMINATED WITH ASSOCIATED MESSAGE ON EICAS. REPLACED BOTTLE. 2L72 4F RTA2NM 20040114001422004011400142NM 2004 1 14 DL757031071 120031209A21216067723 FAN BOEING757 757232 1384965NM CABIN OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27627DL 25319 22917 FLIGHT ATTENDANT CALLED FLT DECK WITH REPORT OF SMOKE COMING OUT OF THE FLOOR VENT FWD. NOTED THE RIGHT RECIR FAN ICAS MSG WAS ILLUMINATED. TURNED L AND R RECIR FANS OFF. TURNED L AND R UTILITY SWITCH OFF AND SMOKE DISSIPATED. PROBLEM OCCURRED ON 12/09/03, RIGHT RECIR FAN OVERHEATED. REPLACED RT RECIRC FAN. 2L72 4F RTA2NM 20040114001452004011400145CE 2004 1 14 DXTA200300175 120031202A215022066101 ACM CESSNA560 560XL 2076702CE AIR DISTRIBUTIONODOR E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07681QS 5605181 AFTER TAKE OFF AN ACRID SMELL WAS DETECTED IN COCKPIT. THIS WAS FOLLOWED BY A BURNING IN THE THROATS AND EYES OF PASSENGERS AND CREW. DECLARED AN EMERGENCY, O2 GEAR WAS DONNED AND RETURNED TO KLNK. NO SMOKE WAS EVER VISIBLE. TROUBLESHOT TO FIND SOURCE FOR ODOR, BORESCOPED #1 AND #2 ENGINE BLEED PORTS AND FOUND NO TRACES OF OIL OR RESIDUE. INSPECTED COELESCER SOCK FOUND NO ODOR OR RESIDUE, REMOVED AND REPLACED ACM, PERFORMED ENGINE RUN UP AT ALL POWER SETTINGS , NO SIGN OF ANY ODORS, SYSTEM LEAK AND OPS CHECK GOOD IAW CESSNA 560XL MM TASK 21-51-00 , 12-19-02-161. 2L72 4F RTA22CE 20040114002052004011400205WP 2004 1 14 MWEA030428 120031023A531199115381 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 CRACK AT FUSELAGE FRAME STATION 718 LEFT OUTBOARD FORWARD FLANGE HAS GROWN FROM 6 INCHES TO 7.6250. -- INSTALLED DOUBLER. 2L72 4F A6WE 20031010000652003101000065SO 2003 10 10 SWIA200312416 120030910A3260 INDICATOR EMB 120 EMB120ER 3260203SO MLG MALFUNCTIONED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07188SW 120039 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ALL GREEN LIGHTS REMAINED ILLUMINATED, ALL RED LIGHTS REMAINED ILLUMINATED EXCEPT RIGHT B-LIGHT. TRIED TO CYCLE THE GEAR SEVERAL TIMES. REMOVED AND REPLACED RIGHT A-SYSTEM UP/DOWN HARNESS ASSEMBLY PER EMB120 MM 32-61-01. OPS CHECKS GOOD. P/N: 120-22623-501. 2L72 4T RTA31SO 20031020002132003102000213WP 2003 10 20 UPS03841362 120030924A53203755822U505 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 STA 340 BETWEEN LONG 33L-34L BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20031020002492003102000249NM 2003 10 20 DLM88030827 120030909A7920AC9806F65 OIL FILTER DOUG MD88 MD88 3023688NM NR 2 ENGINE CLOGGED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27914DE 49957 DURING CRUISE AT FL330 RT OIL STRAINER CLOG MESSAGE ILLUMINATED. LIGHT EXTINGUISHED WITH ENGINE AT IDLE POWER. CONTINUED OPERATION WITH ENGINE AT IDLE. CHECKED RIGHT ENGINE CHIP DETECTOR, ALL OK. REPLACED RIGHT ENGINE OIL FILTER, LEAK CHECK GOOD AT IDLE AND CRUISE POWER SETTINGS. 2L72 4F RTA6WE 20031020002522003102000252NM 2003 10 20 DL757030828 120030909A3350BPS73 POWER SUPPLY BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27609DL 22816 ON L/O FOUND EMERGENCY EXIT LIGHTS INOP AT RT OVERWING EXIT, RT AISLE, RIGHT AFT WING ILUM, AND RIGHT MID WING ILLUM POSITIONS. REPLACED PWR SUPPLY M10568 AND BATTERY. EMERGENCY LIGHTS NOW CHECK GOOD. 2L72 4F RTA2NM 20031020002552003102000255EA 2003 10 20 03281669 120031008A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE RT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020002822003102000282 2003 10 20 VNAA0309012 420030918A34427008470922 RADAR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE WEATHER RADAR FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07472PS186441953 3008 EN ROUTE, THE CREW REPORTED THAT THE WEATHER RADAR HAD GONE INOP AND DUE TO THE WEATHER ASSOCIATED WITH HURRICANE ISABEL, FLIGHT 2454 DIVERTED TO PIT. MAINTENANCE THEN INSPECTED AND REPLACED THE WEATHER RADAR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031020002832003102000283NM 2003 10 20 VNAA0309011 120030918A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN INOPERATIVE A VNAAK NONE L NO TEST TXTAXI/GRND HDL 1 GL07436JS 3052 THE CREW REPORTED THAT THE ROW 10 EMERGENCY FLOOR LIGHTING STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031020003072003102000307NM 2003 10 20 2003UALA00698 120030921A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29118UA 28811 AFT PIT FRAME UPPER CHORD AND WEB DAMAGED AT STA 1700, RBL 45.5. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB AT RBL 45 PER SRM 53-60-01 FIG 205, AND REPLACED ENTIRE UPPER CAP. 2L74 4F4 FRTA20WE E24NE 20031021000322003102100032NM 2003 10 21 USAABB03153 120030830A2121732591D FAN BOEING767 7672B7 1385107NM CARGO BAY FAILED A USAABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19653US 24894 SNN - FLT 306 - EN ROUTE PHL TO DUB, CREW NOTED A LOUD MOTOR SOUND FROM THE R1 DOOR AREA. APPROXIMATELY SIXTY SECONDS LATER, THE CREW NOTED AND ELECTRICAL ODOR IN THE COCKPIT AND SMOKE IN THE FORWARD CABIN AREA. CREW DONNED SMOKE GOGGLES AND PERFORMED THE APPROPRIATE CHECKLIST. FLIGHT DESCENDED TO FL100. SMOKE DISSIPATED. FLIGHT DIVERTED TO SNN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE CIRCUIT BREAKER FOR THE FORWARD EQUIPMENT COOLING EXHAUST FAN POPPED. THE FAN WAS INSPECTED AND FOUND TO HAVE BAD BEARINGS AND IMPELLER CHATTER. THE FAN WAS REPLACED. (M) 2L72 4F RTA1NM 20031021000462003102100046EU 2003 10 21 USAASA03109 120030905A21501263A000003 ACM AIRBUSA319 A319112 3930323EU A/C BAY OVERHEATED A USAAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 EA19719US 1084 SEA - FLT 185 - EN ROUTE PHL-SEA, ON APPROACH, SMOKE BEGAN TO ENTER THE CABIN. SMOKE DISSIPATED AND CLEARED OUT PRIOR TO LANDING. DURING ROLL OUT, RECEIVED ECAM MESSAGE 'PACK 2 OVHT'. TURNED OFF THE NR 2 PACK PER ECAM ACTION. FLIGHT CONTINUED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLAEFD NR 2 PACK AIR CYCLE MACHINE. LEAK AND OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031021000702003102100070EU 2003 10 21 SIMA200309901 120030407A2910AE7064588 HYDRAULIC LINE SAAB SF340 340B 7860101EU HYD SYSTEM BROKEN A SIMAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW21313AE 340B313 LAX - FLT 3241 - DURING CLIMB CREW REPORTED A HYDRAULIC QUANTITY AND PRESSURE LOW. AN EMERGENCY WAS DECLARED AND CREW RETURNED TO LAX. DURING PARKING WHEN THE PROPELLERS WERE FEATHERED THE AIRCRAFT JUMPED CHOCKS AND THE RIGHT PROPELLER STRUCK A TUG. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK ACTUATOR RETRACT LINE IAW SAAB MM. OPS CHECK WAS GOOD, FURTHER WORK WAS DONE TO THE AIRCRAFT PRIOR TO AIRCRAFT RETURNING TO SERVICE. (M) 2L72 4T RTA52EU 20031021000752003102100075 2003 10 21 AALA20031032 420030803A2565 SLIDE BOEING757 757223 1384957NM L2 DOOR FAILED A AALAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21183AN 29593 SNA - FLT 1599 - FLIGHT ATTENDANT OPENED THE L2 DOOR WITHOUT DISARMING THE SLIDE. SLIDE SEPARATED FROM PACK. NO DEPLOYMENT OF INFLATION OF THE SLIDE. DOOR ASSIST BOTTLE WAS FOUND TO BE FLAT. REPLACED THE L2 DOOR SLIDE AND DOOR ASSIST BOTTLE. GROUND CHECKED NORMAL. (M) 2L72 4F RTA2NM 20031021000882003102100088SO 2003 10 21 SIMA200326505 120030912A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21720AE 145279 ABI - DURING AN IMBV INSPECTION, THE TOP OF THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20 REMOVED CORROSION BY CREATING A CUT OUT IN THE OTP OF THE CENTER OMEGA BEAM AT FRAME 20. FABRICATED A U-SHAPED EXTERNAL DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, 53-21-10 FIG 204 SHEET 2. (M) 2L72 4F RTT00011AT 20031021000892003102100089EU 2003 10 21 SIMA200326803 120030920A531514525381003 FLOORBEAM BAG JETSTMJETSTM3201 1500217EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21921AE 921 DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGE SECTION OF LEFT BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. PERFORMED REPAIR IAW EMB SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-10 FIG 201 AND CPM 51-61-00. (M) 2L72 4T RTA56EU 20031021000992003102100099SO 2003 10 21 SIMA200325102 120030907A21508152403 ACM EMB 135 EMB135KL 3260302SO A/C BAY SEIZED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21838AE 145651 SYR - FLT 4320 - DURING CRUISE FLIGHT, THE FLIGHT ATTENDANT REPORTED LOUD NOISE UNDER THE FLOORBOARD FOLLOWED BY A BURNING SMELL AND SMOKE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT AIR CYCLE MACHINE. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTT00011AT 20031208001412003120800141NM 2003 12 8 2003UALA00791 120031022A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 CRACK IN STRINGER-FRAME SHEAR TIE AT BS 663.75. MAJOR REPAIR ACCOMPLISHED. REPLACED STR SHEAR CLIP. 2L72 4F4 FRTA16WE E2GL 20031208001432003120800143NM 2003 12 8 2003UALA00798 120031023A3397 WIRE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT DETACHED A UALAK NONE O OTHER ININSP/MAINT 1 WP29793UA 26946 WIRES DETACHED FROM EMERGENCY EVAC LIGHTS ON SEAT SHROUD. REPLACED AFT EMERGENCY LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20031204000332003120400033EU 2003 12 4 A6WA200360063 120031028A5753 FLAP TRACK BAG BAE146BAE146200A 1500266EU WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31291UE E2084 INSTALL OF FLAP TRACK NR 1 LANDING PLATE FASTENERS. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910005. (M) 2H74 4F RTA49EU 20031204000502003120400050WP 2003 12 4 AALA20031049 120030922A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21597AA 53287 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 4 THROUGH 6. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031204001762003120400176NM 2003 12 4 QXEA200301298 120031015A5540 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX- TRAILING RUDDER IS CRACKED ON LEFT HAND SIDE ALONG UPPER RIB. REPAIRED IAW Q400 RD 8/4-55-075. 2H72 4T RTA13NM 20031204001882003120400188WP 2003 12 4 MWEA0302424 120031021A532059174637 PAN DOUG DC9 DC981 3022081WP PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 AFT ENTRANCE DOOR STAIRWELL DOOR JAMB HAS A CRACK ON THE FORWARD RIGHT INBOARD SIDE APPROXIMATELY FIVE FEET FROM THE FLOOR. FABRICATED AND INSTALLED NEW PAN. 2L72 4F A6WE 20031205000622003120500062EA 2003 12 5 SWIA200312521 120031014A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07418SW 7446 ON CLIMBOUT OF SLC (35 NM), BOTH STAB TRIMS AND MACH TRIM DISENGAGED. TRIMS WOULD NOT RESET AS PER QRH. RETURN TO SLC. REMOVED AND REPLACED STAB TRIM DISCONNECT SWITCH IAW 27-41-30. OPS CHECK GOOD. 2L72 4F RTA21EA 20031205000642003120500064EA 2003 12 5 SWIA200312523 120031016A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07464SW724 724 7827 STAB TRIM CHANNEL ONE WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STABILIZER TRIM CONTROL UNIT IAW AMM CH 27-41-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031208000862003120800086NM 2003 12 8 UPS03441464 120031008A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, FX, SKIN HAS A CRACK AT RIGHT BS 2678 WL 319 (BELOW APU INLET DOOR). SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A AT BS 2678 WL 319. 2L74 4F RTA20WE 20031208000912003120800091NM 2003 12 8 QXEA200301323 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 LEFT OUTBOARD NR 2 SEAT TRACK CORROSION IN SEAT ATTACH AREA TOP AND BOTTOM, APPROXIMATELY S438.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20031208001112003120800111NM 2003 12 8 AWXA200301309 120031007A53476546815 SEAT TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 LCQ - MINOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER FLANGE OF SEAT TRACK AT LBL 45, BS 767-947. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT SEAT TRACK AT LBL 45, BS 767-947; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND REPAIR SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-52 FIG 204. 2L72 4F RTA16WE 20031208001552003120800155EA 2003 12 8 HNAA0300056 120031020A33501013079 SOCKET DHAV DHC8 DHC8311 1386006EA EMERGENCY LIGHT BROKEN A HNAAO OTHER O OTHER NRNOT REPORTED 1 EA07336EN2532125321 336 TWO RED FLOOR EMERGENCY LIGHTS AT ROW 2AC ARE INOP. REMOVED AND REPLACED LIGHT SOCKETS AND REPAIRED BROKEN WIRES. 2H72 4T RTA13NM 20031208001732003120800173NM 2003 12 8 751PA0026 120031025A3350 FUSE BOEING757 757200 1384950NM EMERGENCY LIGHT BLOWN A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 R1 EMERGENCY EXIT LIGHT (EXTERIOR) INOP AND FLOOR PATH LIGHTING INOP AT ROWS 7 THRU 13. REPLACED BLOWN FUSE IN M730 POWER SUPPLY FOR R1 EXTERIOR LIGHT AND RECONNECTED WIRING SOCKET AT BASE FOR FLOOR LIGHTS 7 THRU 13. 2L72 4F RTA2NM 20031209000032003120900003WP 2003 12 9 UPS03841394 120031010A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: ASV, LOWER BELLY SKIN CORROSION; LONGERON L31 STA 1338. TRANSFERRED TO NRC 547382 AT TCO. 2L74 4F RT4A25 20031209000042003120900004WP 2003 12 9 UPS03841469 120031020A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, RT WING L/E RIB IS CRACKED AT XRS 267. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20031021001042003102100104SO 2003 10 21 SIMA200325303 120030904A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21717AE 145272 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF THE OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2917. (M) 2L72 4F RTT00011AT 20031021001222003102100122 2003 10 21 USAASA03099 420030829A2565 FRAME AIRBUSA319 A319112 3930323EU EVAC SLIDE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19769US 1391 BWI - THE LEFT OVERWING SLIDE WAS FOUND TO HAVE A CRACK IN THE OUTER FRAME. MAINTENANCE REPLACED THE LEFT OVERWING SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031021001232003102100123 2003 10 21 USAASA03113 420030917A2565 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19744US 1287 PHL - THE FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE FORWARD RIGHT EMERGENCY ESCAPE SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031021001382003102100138NM 2003 10 21 AALA20031007 120030914A3397 WIRE BOEING767 767223 1385123NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21312AA 22315 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE IN THE AFT CABIN. REPAIRED ELECTRICAL WIRE CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030915000952003091500095EU 2003 9 15 ALGA089088 120030910A6510C651A2001101 DISC PACK UROCOPEC120 EC120B 8680987EU TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL1077 1263 FOUND DISC CRACKED. REMOVED AND REPLACED. 1G72 3U NCR0001RD 20030916000252003091600025NM 2003 9 16 03FDEA01090 120030711A5510NLC6725 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT HORIZONTAL STABILIZER NR 34 BORE CORROSION EXCEEDED CONDITION "3". CORROSION ON RT HORIZONTAL STABILIZER NR 34 BORE REMOVED AND REPAIR CARRIED OUT IAW EA 1-5510-71839 (STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL - BORE 34 RIGHT. 2L73 4F RTA22WE 20030916000932003091600093EA 2003 9 16 ASOA03398 120030823A5720GG670806123 MOUNT CNDAIRCL600 CL6002C10 1390015EA PICCOLO TUBE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11716EV 10084 DURING A GROUND INSPECTION IN ATL, THE LT INBOARD TELESCOPIC LEADING EDGE ANTI-ICE SUPPLY MOUNT ON THE PICCOLO TUBE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT INBOARD TELESCOPIC LEADING EDGE ANTI-ICE SUPPLY MOUNT ON THE PICCOLO TUBE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030916001342003091600134WP 2003 9 16 GTIA030645 120030810A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FOUND CABIN FLOORBOARD RIGHT STATION 541-617 CRACKED. FABRICATED CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20030916001432003091600143NM 2003 9 16 NACA20030096 120030722A278240142 SWITCH BOEING727 727100 1384036NM LE FLAPS FALSE INDICATIONA NACAK NONE N FALSE WARNING CRCRUISE 1 AL03930FT 19387 NR 2 SLAT INDICATES FORWARD AMBER LIGHT AND F.E. TRANSITE LIGHT WITH FLAPS UP. REPLACED NR 2 SLAT EXTEND SWITCH. 2L73 4F RTA3WE 20030917000342003091700034EA 2003 9 17 GXPA0303 220030509A8550 ENGINE PIPER PA60 PA60601 7106010NM LYC O540 IO540* 41532EA NR 2 LEAKING E GXPAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL23220BC 610031 L1542648A AIRCRAFT DOWN IN EL DORADO, AR DUE TO LOW OIL PRESSURE IN RT ENGINE. CORRECTIVE ACTION WILL BE COMMUNICATED WHEN TROUBLESHOOTING IS COMPLETED. 1M72 3O3 ORTA17WE 1E4 20030917000532003091700053CE 2003 9 17 DXTA200300110 120030905A2823 CLAMP CESSNA750 750 2076810CE FUEL DIST LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07998QS 7500198 WHILE IN CRUISE AT FL290 THE "WING O'FULL L" CAS MESSAGE CAME ON. ABOUT 30 SECONDS LATER WE GOT THE SAME MESSAGE FOR THE RIGHT WING, FUEL WAS NOTED TO BE DUMPING OUT OF BOTH WINGS. AFTER WE SHUT OFF THE CENTER TANK TRANSFER SWITCHES IT TOOK ABOUT A MINUTE FOR THE RIGHT WING TO STOP DUMPING, THE LEFT WING CONTINUED TO DUMP FUEL FOR AN ADDITIONAL 11 MINUTES BEFORE FINALLY STOPPING, LOST ALMOST 300 LBS. OF FUEL FROM THE LEFT SIDE. - INSPECTED BOTH LEFT AND RIGHT WING FUEL VENT SYSTEMS, PRESSURIZED FUEL VENT PLUMBING NOTED TOW WIGGINS CLAMPS UNSEAT AND LEAKING. SECURED UNSEATED WIGGINS CLAMPS, LEAK CHECKED GOOD, WORK PERFORMED IAW CHAPTER 28-10-04 OF THE CITATION 750 MM. 2L72 4J RTT00007WI 20030918000382003091800038NM 2003 9 18 GAIA03040SP 120030719A5320 WEB BOEING727 7272J0 138407ENM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND LOWER FORWARD CARGO COMPARTMENT BS 620 FRAME WEB DOUBLER HAS PIECES BROKEN OFF FASI N/R 35707. REMOVED BROKEN PART, FABRICATED DOUBLER REPAIR FROM MATERIAL 7075-T6 .063 PO NR 991396 DIM 14 INCH BY 5.25 INCH. INSTALLED IAW B727 SRM 51-30-2. (M) 2L73 4F RTA3WE 20030918000392003091800039NM 2003 9 18 GAIA03041SP 120030719A5330 SKIN BOEING727 7272J0 138407ENM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 MAIN CABIN FRAME BS 580 DENTED BELOW STRINGER 8 RT FASI N/R 36052, FOUND DURING C-CHECK. CUT OUT DAMAGE 1 INCH BY 1.5 INCH, DOUBLER REPAIR 7075 T-6 IAW B-727 SRM 53-10-4 FIG 1. (M) 2L73 4F RTA3WE 20030918000952003091800095CE 2003 9 18 IZ22003F00004 120030711A2130692254513 SOLENOID VALVE MTSBSIMU2 MU2B36A 5780413CE GARRTTTPE331TPE331* 01514WP ENGINE LEAKING B IZ2RO OTHER O OTHER NRNOT REPORTED 1 SW15777LP426 719SA SOLENOID VALVE LEAKING EXCESSIVE OIL BETWEEN SOLENOID AND VALVE BODY. 1H72 3T3 T A10SW E2WE 20030919000542003091900054SO 2003 9 19 GLBA2003115 120030806A5320 DRAIN VALVE EMB 120 EMB120ER 3260203SO FUSELAGE INOPERATIVE A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03108UX 120108 CABIN DIFF. DROPPED TO ZERO UNABLE TO CONTROL IN AUTO OR MANUAL MASK DEPLOYED, CLEANED/REPLACED 3 DRAIN VALVES OPS CK GOOD 2L72 4T RTA31SO 20040114002092004011400209WP 2004 1 14 MWEA030433 120031023A2450914F5674 RELAY DOUG DC9 DC981 3022081WP APU FAILED A MWEAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 GL31814ME 48010 RIGHT END GENERATOR WILL NOT PICK UP BUSS. REMOVED AND REPLACED RIGHT APU RELAY. 2L72 4F A6WE 20040114002152004011400215NM 2004 1 14 MWEA030489 120031215A552259304972 SKIN DOUG MD88 MD88 3023688NM ELEVATOR TAB CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RT ELEVATOR ANTI-FLOAT TAB SKIN IS CRACKED AT OUTBOARD HINGE POINT CUTOUT. FABRICATED AND INSTALLED FILLER AND DOUBLER. 2L72 4F RTA6WE 20040115000472004011500047NM 2004 1 15 QXEA200301518 120031205A329747151 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM MLG FAILED A QXEAO OTHER O OTHER CLCLIMB 1 NM09407QX5401 4049 LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. NO CAUTION LIGHTS OR OTHER ABNORMAL CONDITIONS NOTED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NOSE LANDING GEAR WOW HARNESS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040115001772004011500177SO 2004 1 15 2004F00038 120030924A5730 SKIN GULSTMG1159 G1159A 3970109SO LT & RT WING CORRODED A PJVAK NONE O OTHER ININSP/MAINT 1 EA17724DB 372 DURING INSPECTION SEVERAL AREAS OF CORROSION FOUND ON LT/RT WING PLANK UPPER LEADING EDGE. REPAIRED BY BLENDING AND REPAIR IAW MFG DRAWINGS SE45632105, SE35803160, SE35803176 AND SE35803002. (M) 2L72 4F A12EA 20040115001902004011500190NM 2004 1 15 03FDEA02269 120031226A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT WING - O/B FLAP I/B HINGE ACTUATOR I/B MOUNT BORE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040115002072004011500207NM 2004 1 15 03FDEA02280 120031226A5744ARC050311 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING - O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B HOLE BORE CORRODED. LEFT WING - O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73355 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040120000122004012000012NM 2004 1 20 2003UALA00980 120031220A3610 CLAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE BLEED DUCT LOOSE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29548UA 25396 UPON LEVEL OFF AT FL340 RECIEVED A RT BLEED DUCT LEAK EICAS MESSAGE. DUCT LEAK BITE PRODUCED STORED FAULT 64 (RT WING LEADING EDGE - BOTH LOOPS IN ZONE BAD) . ERASED CODE FROM MEMORY & CLEARED STATUS MSG. FOUND BLEED DUCT CLAMP IN THE RIGHT LEADING EDGE TO BE LEAKING. REPLACED CLAMP. 2L72 4F4 FRTA2NM E17NE 20040120000632004012000063NE 2004 1 20 DXTA200300208 220031222A732181973505 FUEL CONTROL CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE RT ENGINE FAILED E DXTAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 GL07804QS 5600610 PCEDC0147 RIGHT ENGINE FLAMED OUT DURING DESCENT (THROUGH 22000) PERFORMED RESTART WITHOUT EVENT. ENGINE OPERATION WAS NORMAL THROUGH THE REST OF FLIGHT, AIRCRAFT CONTINUED TO DESTINATION. SUMPTED RT FUEL TANK TO CHECK FOR WATER OR CONTAMINATION, SYSTEM CHECKED GOOD, INSPECTED FUEL FILTER AND CHECKED GOOD. REPLACED RT ENGINE FUEL FILTER IAW 560 MM. TROUBLESHOT TO BAD FUEL CONTROL UNIT, REMOVED AND REPLACED RT ENGINE FCU IAW P&WC MM CHAPTER 73-20-01, OPS AND LEAK CHECK GOOD. 2L72 4F4 FRTA22CE E00053EN 20040121000432004012100043NM 2004 1 21 03FDEA02325 120031230A5510ALC81061 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB LT UPPER FWD PLANK NR 14L BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-75204: HORIZONTAL STABILIZER BARREL NUT BORE 14 LH FITTING FABRICATION. 2L73 4F RTA22WE 20040121000552004012100055NM 2004 1 21 BJNA031102 120031117A335015AT17 SWITCH BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11789TM 23046 DURING A PREFLIGHT CHECK, EXTERIOR EMERGENCY EXIT LIGHTS DID NTO ILLUMINATE. MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHT SWITCH WAS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT SWITCH IAW BOEING MM 33-51-01. EXTERIOR EMERGENCY LIGHTS NOW ILLUMINATE. (M) 2L72 4F RTA16WE 20040121000612004012100061EA 2004 1 21 ASOA03599 120031123A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11859AS 7421 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121000632004012100063EA 2004 1 21 ASOA03590 120031119A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A C-CHECK IN MCH, THE FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040121000662004012100066EA 2004 1 21 ASOA03601 120031124A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11872AS 7542 FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY CEILING LIGHT AT ROW TEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TEN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121000812004012100081EA 2004 1 21 ASOA03612 120031201A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11917EV 7769 DURING HANGAR MAINTENANCE IN MCN, THE EXTERIOR EMERGENCY LIGHT ON THE RT MID FUSELAGE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT LAMP ON THE RT MID FUSELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121000842004012100084EA 2004 1 21 A6WA200340196 120031220A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 FOUND FLOOR STRUCTURE CRACKED AT FS 621, LT AND RT SIDE ANGLE, P/N 601R35032-239. PERFORMED A MAJOR REPAIR BY CUTTING AWAY DAMAGES PORTION OF ANGLE AND INSTALLING REPAIR ANGLE AND STRAP IAW BOMBARDIE REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20030919000602003091900060EA 2003 9 19 COMA0360354 120030808A2497HA4A039 CONTACTOR CNDAIRCL600 CL6002B19 1900309EA JUCT BOX 6 MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01495CA 7774 FLIGHT 5009 AC ESS BUS MESSAGE. REPLACED CONTACTOR K3XD. 2L72 4F RTA21EA 20030919000652003091900065NM 2003 9 19 HALA0300632 120030717A2750 CONTROL UNIT BOEING767 76733A 1385209NM TE FLAPS MALFUNCTIONED A HALAO OTHER J WARNING INDICATION LDLANDING 1 WP13582HA 28139 TE FLAP DISAGREE LIGHT ILLUMINATED WHEN SELECTING MORE THAN FLAPS ONE. FSUE FAULTS OUTBOARD FLAP RVDT NR 1 M544. REPLACED O/B FLAP RVDT NR 1 IAW MM 27-81-11. OPERATE FLAPS AND SLATS NORMAL AND ALTERNATE, ALL INDICATIONS AND OPERATIONAL NORMAL. SYSTEM OPS NORMAL. TEST FLIGHT REQUIRED. TEST FLIGHT COMPLETED, OPS CHECK GOOD. 2L72 4F RTA1NM 20030919000952003091900095CE 2003 9 19 GLBA2003120 120030814A3210 LANDING GEAR BEECH 1900 1900D 1154162CE MAIN INOPERATIVE A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0394GL UE94 LANDING GEAR WOULD NOT RETRACT, CND CHECK FLIGHT SATISFACTORY. 2L72 4T RTA24CE 20030919000972003091900097EU 2003 9 19 3602060203 120030602A215005000846 BLOWER MOTOR SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE A/C CONDENSOR SEIZED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07820NA597 3602 22342 A/C CONDENSOR BLOWER MOTOR SEIZED. 1G71 3U3 U H9EU E00054EN 20030919001172003091900117CE 2003 9 19 00104 120030813A2910 LINE LEAR 24 24B 5170306CE HYD SYSTEM LEAKING E HAEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW05233TW 24221 ON APPROACH, ATTEMPTED NORMAL GEAR EXTENSION BUT HYDRAULIC PRESSURE WAS TO LOW TO EXTEND THE GEAR. EXTENDED GEAR USING EMERGENCY GEAR PROCEDURE AND LANDED WITH NO PROBLEM. FOUND RT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE LEAKING. REMOVED AND REPLACED HOSE ASSEMBLY. LEAK AND OPS CHECKS GOOD. 2L72 4J A10CE 20030919001192003091900119NM 2003 9 19 QXEA200300977 120030813A2612 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FALSE INDICATIONA QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09404QX 4046 ON FLIGHT 2308 DURING FLIGHT AT RANDOM TIMES ON APU FIRE CONTROL PANEL AND MASTER WARNING PANEL, BOTTLE LOW LIGHT ILLUMINATED ALONG WITH CHECK FIRE DETECTION LIGHT AND MASTER WARNING LIGHTS ILLUMINATED FOR A VERY SHORT TIME AND DURING CRUISE FLIGHT. SHOOK CONNECTOR AND WIRES TO REAR PRESSURE BULKHEAD AND BULKHEAD CONNECTOR. NO PARTS REPLACE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030915000502003091500050SO 2003 9 15 GLBA2003129 120030910A523012023348005 SEAL EMB 120 EMB120ER 3260203SO CARGO DOOR LOOSE A GLBAB EMER. DESCENT O OTHER CRCRUISE 1 NM0371GL 120071 O2 MASKS DEPLOYED CARGO DOOR SEAL CAME LOOSE, R&R CARGO DOOR SEAL 2L72 4T RTA31SO 20030915000572003091500057NE 2003 9 15 HEEA089004 120030812A21217650007901103 BLOWER SKRSKYS76 S76A 8143006NE CABIN BURNED OUT B HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW034253S 760035 BLOWER CREATING BURNING ODOR IN COCKPIT. 1G72 3U H1NE 20030916001032003091600103EU 2003 9 16 ASOA03397 120030823A3210S3238006120100 SUPPORT BRACKET AEROSPATR72 ATR72212 8680945EU LT MLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11535AS 464 DURING HANGAR MAINTENANCE IN MCN, THE LT MLG TOP LEFT AFT UPLOCK SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR TOP LEFT AFT UPLOCK SUPPORT BRACKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030917000612003091700061SW 2003 9 17 HEEA089034 120030812A2120 ODOR BELL 412 412 1182202SW COCKPIT DETECTED B HEEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03800Y 33134 ENROUTE FROM MORGAN CITY TO GC-158, CREW SMELLED BURNING ELECTRICAL INSULATION. NO SMOKE REPORTED. MADE PRECAUTIONARY LANDING AT GC-65. 1G72 4U H4SW 20030917001132003091700113EA 2003 9 17 A6WA200340112 120030715A2740 MOTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE STB TRIM CHANNELINOPERATIVE A O OTHER O OTHER CRCRUISE 1 GL31415AW 7593 STAB TRIM CHANNEL 1 INOPERATIVE REMOVED AND REPLACED MOTOR CONTROL UNIT IAW MM 27-42-05. OPS CHECK GOOD. SHOP REPORT REMARKS, COMPLAINT VERIFIED, REMOVED AND REPLACED DEFECTIVE RESISTOR, INTEGRATED CIRCUIT, DIODE AND CRACKED INDUCTOR. INSPECTED UNIT IAW CMM 27-43-05 REV 01. (M) 2L72 4F4 FRTA21EA E15NE 20030917001342003091700134NE 2003 9 17 DL76L030695 220030725A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4090 PW4090 52119NE NR 2 LEAKING A DALAK NONE K FLUID LOSS ININSP/MAINT 1 SO27180DN26328 25985 727726 FOUND EVIDENCE OF OIL LEAKING FROM INTERNAL AIR COMPARTMENT OF THE NBR 3 BEARING SCAVENGE LINE. REPLACING ENGINE TO FACILITATE REPAIR. 2L72 4F4 FRTA1NM E46NE 20030918000222003091800022NM 2003 9 18 2003F00565 120030502A5310 DOOR FRAME BOEING737 7372L9 1384497NM AIRSTAIR CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO27464AT 21278 DURING C-CHECK INSPECTION A 2.5 INCH CRACK WAS FOUND THROUGH TWO FASTENERS AT THE FORWARD AIRSTAIR DOOR UPPER STOP FRAME. THE REPAIRS WHERE ACCOMPLISHED ON NON ROUTINE 031245. (M) 2L72 4F RTA16WE 20030918000422003091800042NM 2003 9 18 2003F00568 120030422A5310 RIB BOEING737 7372L9 1384497NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37464AT 21278 DURING C-CHECK INSPECTION, A CRACKED RIB WAS FOUND AT BS 400 ABOVE STRINGER 20L. THE REPAIRS HAVE BEEN ACCOMPLISHED ON NON ROUTINE 031072. AIRCRAFT TOTAL TIME 46985.2. TOTAL CYCLES 41351. (M) 2L72 4F RTA16WE 20030918000632003091800063NM 2003 9 18 DL76L030719 120030803A3320 BALLAST BOEING767 767332 1382001NM FWD GALLEY UNSERVICEABLE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27180DN 25985 ELEC SMOKE FUMES EMITTING FROM GASPER VENT NEXT TO OVERHEAD LIGHT IN FWD GALLEY. AFTER LIG TURNED OFF FUMES DISSAPATED SUSPECT LIGHT BALLAST. R/R BOTH BALLAST FOR F/C OVHD GALLEY LIGHT. BALLASTS ROBBED FROM A/C 187. LIGHT CHECKS GOOD. 2L72 4F RTA1NM 20040121000922004012100092NE 2004 1 21 2004F00046 220031118A7200 TURBINE BLADES BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GUUAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO1781536 UE152 114332 AFTER CLEARANCE FOR TAKEOFF, LT ENGINE FAILED. ENGINE IMMEDIATELY SECURED. ABORTED TAKEOFF. AIRCRAFT RETURNED TO THE GATE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAD MAJOR INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODUEL AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. (M) 2L72 4T4 TRTA24CE E26NE 20040121001022004012100102NM 2004 1 21 03FDEA02327 120031230A5744ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD MOUNT INBOARD AND OUTBOARD SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75201, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBD. FLAP / OUTDB SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121001062004012100106NM 2004 1 21 03FDEA02331 120031230A5753ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING OUTBOARD FLAP OUTBOARD HINGE FITTING INBOARD PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75201, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD. FLAP. OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121001072004012100107NM 2004 1 21 03FDEA02332 120031230A5753ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING OUTBOARD FLAP OUTBD HINGE FITTING INBOARD PIVOT INBOARD AND OUTBOARD SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75201, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP. OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121001082004012100108 2004 1 21 AWXA200301627 420031228A2230 THROTTLE BOEING757 757225 1384959NM ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28907AW 22691 ON TAKEOFF, AUTO THROTTLE FAILED TO ENGAGE WHEN EPR MODE SELECTED, AUTO THROTTLE MODE NOT DISPLAYED ON ADI. CYCLED AUTO THROTTLE ARM SWITCH, NO HELP. REJECTED TAKEOFF BELOW 40 KTS. DPI ISSUED MEL 22-30-01, COND 1, THRUST MANAGEMENT SYSTEM INOP. WHEN AIRCRAFT ARRIVED IN BWI MAINTENANCE PULLED UP MAINTENANCE CONTROL DISPLAY PANEL (MCDP) FAULT FOR LAST FLIGHT A/T DISC TMC CODE 310800. THRUST MANAGEMENT COMPUTER (TMC) SELF TEST FOUND TMC FAILURE, MCDP TESTS 2 & 10 CHECKED GOOD. PREVIOUS TROUBLESHOOTING FOUND PIN 14 ON CONNECTOR D40674P EXCESSIVELY LOOSE 28 VOLT DC INPUT SERVO COMMAND ORDERED CONNECTOR & TMC. 2L72 4F RTA2NM 20040115001302004011500130NM 2004 1 15 03FDEA02108 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 364MR. RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2 2L73 4F RTA22WE 20040115001442004011500144NM 2004 1 15 03FDEA02150 120031209A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25276FE 22041 LOWER FUSELAGE, BS 1090, 1 INCH ABOVE AND 4 INCHES BELOW STR 24 RT, EXTERNAL SKIN IS DENTED, GOUGED AND POSSIBLY CRACKED. DAMAGE ON SKIN FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW FED-EX EA 7-5330-55172. 2L73 4F RTA3WE 20040115001512004011500151NM 2004 1 15 DL73S031112 120031218A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 INSPECTIONS REQUIRED PER AD 2003-08-15 REVEALED SEVERAL CRACKS IN THE STRINGER 4R SKIN LAP JOINT BETWEEN FS 380 & 420. THE CRACKS WERE REMOVED WITH CUTOUTS AND REPAIRED PER B737 SRM 53-30-3, 42. THE REPAIR WAS DOCUMENTED PER ER/A 087961-14AD. 2L72 4F RTA16WE 20040115001822004011500182NM 2004 1 15 DHL2003742544 120031121A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, DISCREPANCY IS AS FOLLOWS; N/R 59972 STR 27 L BETWEEN STA 620-640 AT POWER CABLE STAND-OFF. REMOVED FASTENERS FOR ACCESS AS REQ'D IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT STA 630 STR 27L, CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. AREA OF CUT OUT 3 INCHES AND FABRICATED STRINGER REPAIR USING BAC 1498-25 PO 335792 DIM 13 INCHES AND ONE FILLER USING BAC1498-25 PO 335792 DIM 3 INCHES IAW B727 SRM 53-10-3 FIG 1. ALODINED AND PRIMED ALL REPAIR PARTS IAW B727 SRM 51-10-2 AND INSTALLED REPAIR AND STAND-OFF IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20040120000362004012000036NM 2004 1 20 03FDEA02247 120031226A5753ARC2512503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, IB FLAP OB HINGE FITTING OB PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75212, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040122000202004012200020EU 2004 1 22 2003UALA00989 120031229A2782830A000002 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SLATS OUT OF LIMITS A UALAO OTHER J WARNING INDICATION DEDESCENT 1 WP29421UA31702 500 SLATS FAILED TO DEPLOY, S-CTRL FAULT ILLUMINATED. THE TORQUE LIMITER OF THE LT NR 2 SLAT OUTBOARD ACTUATOR WAS FOUND TRIPPED. THE SLAT STOP TO FWD ROLLER DIMENSION WAS ALSO FOUND OUT OF LIMIT. REPLACEMENT OF THE FAULTY SLAT ACTUATOR AND SUBSEQUENT ADJUSTMENT OF THE SLAT RIG WERE ACCOMPLISHED WITHOUT FURTHER ANOMALY. 2L72 4F4 FRTA28NM E40NE 20040122000482004012200048WP 2004 1 22 WRLA200324 120031121A3260805501 PROXIMITY SENSOR DOUG DC10 DC1030 3023501WP RT MLG INOPERATIVE A WRLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO11526MD 46998 RT MAIN GEAR LIGHT IN BOTH POSITIONS REMAINED RED AFTER GEAR RETRACTED. ADJUSTED SHIMS/GAP (.160) PROX SENSOR MAIN GEAR DOOR LATCH MECHANISM. OPS CHECKED OK. REMOVED AND REPLACED THE SENSOR MAIN GEAR DOOR LATCH MECHANISM. OPS CHECK. FOLLOWED PROCEDURE IAW MM 32-61-00/32-34-03. REMOVED AND REPLACED RT MAIN LANDING UP AND DOOR LOCK SENSOR. (M) 2L73 4F A22WE 20040122000492004012200049NM 2004 1 22 USAABB03228 120031223A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 FOUND FLOOR AISLE LIGHTS INOPERATIVE ON THE RIGHT SIDE, ROWS 1 THROUGH 5 AND AT THE FORWARD CROSSOVER. MAINTENANCE REPAIRED A WIRE AT THE WALL AT STATION 476, AND REPLACED THE CHARGER AND BATTERY. (M) 2L72 4F RTA1NM 20040122000572004012200057NE 2004 1 22 GTIA030995 220031118A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217A 52053NE FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 709816 FOUND ENGINE HAS LEAK AT N1 TACH GENERATORS. ENGINE FAILED BORESCOPE INSPECTION ENGINE TO BE SENT OSV FOR REPAIR. (M) 2L72 4F4 F A6WE E9NE 20040122000682004012200068EA 2004 1 22 ASOA03596 120031121A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031001001232003100100123NM 2003 10 1 03FDEA01618 120030924A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION AND DOUBLE HOLE IN FLOORBEAM AT BS 950E.75, BL 0, WL 201. CORROSION AND DOUBLE HOLE IN FLOORBEAM AT BS 950E .75, BL 0, WL 201 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA OF LWR CHORD OF FLOORBEAM BS 950E .75", BL 0, WL 208 AND REPAIRED FLOOR BEAM LWR CHORD B S950E .75", BL 0, WL 208 PER SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 20030919000992003091900099EU 2003 9 19 PH92003F00000 120030723A6410355A12004008 BLADE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED E PH9AO OTHER O OTHER NRNOT REPORTED 1 NM05911KR2740 2094 TAIL ROTOR BLADE HAS 4000 HOURS TBR(SLL). UNIT FAILED AT 2740.3 TTSN. MASSIVE SPAR CRACK ON LAMINATED SPAR. UNIT RETURNED. 1G71 3U3 UNCH9EU E19EU 20030919001062003091900106EU 2003 9 19 36020602033 120030602A6720350A33214501 PITCH LINK SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR WORN E S4WAK NONE O OTHER ININSP/MAINT 1 WP07820NA597 3602 22342 T/R PC LINK WORN. 1G71 3U3 U H9EU E00054EN 20030919001382003091900138EU 2003 9 19 9015081003 120030810A2110 BELT SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE A/C COMPRESSOR DETERIORATED E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP07350R 76 9015 9667 AIR CONDITIONER COMPRESSOR BELT BURNED/DETERIATED DUE TO COMPRESSOR FAILURE. 1G71 3U3 U H9EU E00054EN 20030919001472003091900147NE 2003 9 19 2904050203 220030502A75329550164960 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE DEFECTIVE E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP074027Q3147 2904 9456 BLEED VALVE OPENING AT 71 PERCENT NG. 1G71 3U3 U H9EU E19EU 20030919001482003091900148NM 2003 9 19 AWXA200300927 120030815A3830 BAFFLE AIRBUSA319 A319132 3930340NM LAVATORY CLOGGED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28821AW 1406 AT CRUISE ALTITUDE EN ROUTE FROM IAD TO PHX FLIGHT ATTENDANTS REPORTED ALL LAVATORIES INOPERATIVE. LAVATORIES WOULD NOT FLUSH PROPERLY. AIRCRAFT DIVERTED TO CMH WHERE MAINTENANCE FOUND EXCESSIVE PAPER TOWELS CLOGGING THE DUCTING AT AN ELBOW TO TANK CONNECTION BAFFLE ASSEMBLY. MAINTENANCE REMOVED DEBRIS AND OPERATIONAL CHECK OF THE LAVATORY SYSTEM NORMAL. 2L72 4F RTA28NM 20030919001592003091900159 2003 9 19 AWXA200300939 420030817A2565 LANYARD AIRBUS320 A320231 3930325EU L-2 DOOR TORN A AWXAO OTHER O OTHER DEDESCENT 1 WP28646AW382584495 271 ON DECENT, EN ROUTE FROM PHX THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL COMING FROM THE L-2 DOOR. MAINTENANCE FOUND THE L-2 DOOR SLIDE LOWER LANYARD TORN AND IN THE DOOR SEAL, AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE THE L-2 DOOR SLIDE WAS REMOVED AND REPLACED IAW T/C R1C25304. 2L72 4F RTA28NM 20030922000102003092200010CE 2003 9 22 HYI2003F00010 120030718A2400CM358950 MASTER SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO COCKPIT FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01375R 686 402C0468 AVIONIC SWITCH FAILED MAINTENANCE REPLACED SWITCH AND RETURNED THE AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20030922000282003092200028EU 2003 9 22 2003UALA00625 120030813A2120 FILTER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COOLING FAN CLOGGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29429UA 539 RETURN TO FIELD DUE TO AVIONICS VENT FAULT. AVIONICS COOLING SYSTEM FILTER REPLACED. 2L72 4F4 FRTA28NM E40NE 20030922000312003092200031NM 2003 9 22 AWXA200300940 120030818A2560P2070001214 FLASHLIGHT BOEING737 73733A 1384673NM ZONE 900 - LAVATINOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28175AW 23634 EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030922000352003092200035 2003 9 22 RAIA00307201 420030728A23127510700806 RADIO JETAIRJETSTMJETSTM4101 1500501EU VHF SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03557HK11799 41074 COMM NR 1 WILL NOT TRANSMIT. MAINTENANCE REMOVED AND REPLACED THE THE NR 1 COMM UNIT. 2L72 4T RTA41NM 20030922000372003092200037EU 2003 9 22 RAIA00307203 120030730A3246AN59474 TIRE AEROSPATR72 ATR72202 8680940EU NLG UNSERVICEABLE A RAIAO OTHER E VIBRATION/BUFFET LDLANDING 1 CE03722TE 220 LARGE SHIMMY ON TAKE OFF FROM MSN ON NOSE GEAR AND MADE EMERGENCY LANDING AT STL. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLIES. 2H72 4T RTA53EU 20030922000392003092200039NE 2003 9 22 RAIA00307205 220030731A732031059008 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE DEFECTIVE A RAIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CE03571HK5980 41090 76098 RT ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL. 2L72 4T4 TRTA41NM E18NE 20030922000412003092200041EU 2003 9 22 RAIA00308207 120030803A2422PC125123B STATIC INVERTER JETAIRJETSTMJETSTM4101 1500501EU RIGHT INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03555HK15849 41072 RT INVERTER FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED THE RIGHT STATIC INVERTER. 2L72 4T RTA41NM 20030915000782003091500078SW 2003 9 15 ALGA089029 120030908A712023051106 SUPPORT BELL 407 407 1182206SW ALLSN 250C 250C47B GL COMPRESSOR DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03647AL 53357 RECEIVED NEW FROM AVIALL. C/W PRESSURE CHECK,LEAKED INTERNALLY ON PRESSURE CHECK TEST. RETURNED PART TO VENDOR FOR WARRANTY EXCHANGE.SUBMITTED BY:PRESTON BARZARE 1G71 3U3 UO H2SW E1GL 20030915000822003091500082CE 2003 9 15 BAQA088914 120030903A21331036481 OUTFLOW VALVE BEECH 90 C90 1152913CE CABIN PRESSURE CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0390LF 3387 LJ852 VALVE HAS A CRACK IN FILTER ASSEMBLY MOUNTING PAD. REPLACED WITH SERVICEABLE UNIT. 1L72 3T 3A20 20030915001132003091500113NM 2003 9 15 ANCF200300025 120030907A32414062575 TRANSDUCER DOUG MD80 MD83 3023681NM ANTI SKID DAMAGED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 SO23583AN 53183 DURING TAKE-OFF ROLL BELOW 60 KNOTS WHEEL NOT TURNING LIGHT CAME ON; REJECTED TAKE-OFF PERFORMED. MAIN WHEEL NR 1 WAS FOUND THE TRANSDUCER ANTI-SKID IN BAD CONDITION. IT WAS REPLACED IAW AMM 32-43-02 PAGE 201 2L72 4F RT 20030916000182003091600018WP 2003 9 16 MEX2003367 120030814A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23505MD 49149 DURING OVERNIGHT CHECK WAS DETECTED LIGHTNING IMPACT AT FUSELAGE LEFT SIDE. LIGHTNING INSPECTION WAS DETECTING DAMAGES AT STATION Y332 AND LONGERON 15 WITH EIGHT RIVETS DAMAGED. THE FOLLOWING PARTS WERE REPLACED IAW. 2 FASTENERS AT FORWARD ENTRANCE LT DOOR SKIN LOWER AREA. 17 FASTENERS AT STA Y=237 TO Y=351 BETWEEN LONGERONS 15 TO 18 LT. 1 FASTENER AT STA Y 150 BETWEEN LONGERONS 16 TO 17 LT. 4 FASTENERS AT STA Y =218 TO 237 BETWEEN 16 TO 18 LT. BEAM NR 8 AT 2.750 INCHES FROM AFT SKIN EDGE. 2L72 4F A6WE 20030916000282003091600028NM 2003 9 16 731PA0028 120030715A3350 LAMP BOEING737 737306 13844BGNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 R2 EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED R2 EMERGENCY EXIT LIGHT. OPS CHECK OK. 2L72 4F4 FRTA16NE E2GL 20030916000472003091600047NM 2003 9 16 03FDEA01073 120030625A5753ARC050213 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FORWARD HINGE FITTING FOUND HYDRAULIC ACTUATOR ASSEMBLY MOUNT HOLE INBOARD SIDE WITH CORROSION (WING SIDE FITTING). LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FORWARD HINGE FITTING HYDRAULIC ACTUATOR ASSY MOUNT HOLE INBOARD ( WING SIDE FITTING ) CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5750-69355. WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030916001202003091600120WP 2003 9 16 AALA20030883 120030821A3350 LIGHT DOUG DC9 DC983 3022083WP TAIL BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21571AA 49353 DFW - FOUND LEFT AFT STAIRWELL EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED AFT STAIRWELL EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030916001262003091600126NM 2003 9 16 AALA20030515 120030430A335002031461201 LIGHT BOEING737 737823 13844BZNM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21931AN 30079 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT FORWARD ENTRY DOOR OUTBOARD OF FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHTING ASSEMBLY AT FORWARD ENTRY DOOR OUTBOARD OF FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030916001352003091600135WP 2003 9 16 GTIA030655 120030817A3350 LIGHT DOUG DC9 DC983 3022083WP EXIT SIGN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND R-1 EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY BROKEN. REMOVED R-1 EMERGENCY EXIT IDENTIFIER. INSTALLED NEW EXIT IDENTIFIER. (M) 2L72 4F RTA6WE 20030917000022003091700002 2003 9 17 234TR0006 420030725A2297 WIRE BOEING737 737228 13844AGNM FLT CON COMP MALFUNCTIONED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05234TR 23004 FLIGHT CONTROL COMPUTER FAILS LRU INTERFACE TEST 25.21 SUBTEST 1 AND 2. REMOVED E1-1 SHELF AND CORRECTED WIRING. OPS NORMAL. 2L72 4F RTA16WE 20030917000832003091700083CE 2003 9 17 S2YA03025 120030713A261224412886 FIRE LOOP BEECH 1900 1900D 1154162CE RT ENGINE INOPERATIVE A S2YAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 GL1379SK UE79 FLT 1023 - MKE-ATW - DURING APPROACH, THE CREW NOTED THE NR 2 ENGINE T-HANDLE ILLUMINATED. THE CREW FOLLOWED THE QRH AND PULL THE T-HANDLE, SHUTTING DOWN THE RIGHT ENGINE. THE CREW ALSO DISCHARGED THE FIRE BOTTLE AND DECLARED AN EMERGENCY. MAINTENANCE INSPECTED THE A/C AND DETERMINED THE CAUSE TO BE A FAULTY FIRE LOOP, IT WAS FERRIED BACK TO MKE. MKE MAINTENANCE REPLACED THE FIRE LOOP AND BOTTLE AND RETURN THE A/C TO SERVICE. (M) 2L72 4T RTA24CE 20030917000902003091700090EU 2003 9 17 2003F00560 120030906A3260848401 PROXIMITY SENSOR AIRBUS320 A320233 3930329EU E/E BAY MALFUNCTIONED A RJEFA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO23461TA 1300 DURING CRUISE STAGE LIGHT, MESSAGES 'ENG 2 REVERSER FAULT' AND 'ANTI ICE F/O PITOT INOPERATIVE' WERE DISPLAYED ON ECAM. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAT STATION, TECHS PERFORMED INSPECTION OF THE REVERSER SYSTEM. POST FLIGHT REPORT SHOWED THAT THE SENSOR 22GA AS FAULTY AND ALSO THE LGCIU NR 2 HAD AN UNRELIABLE OPERATION. THE SENSOR WAS REPLACED AS PER AMM 32-31-73. ALSO, AIRCRAFT LANDING GEAR RETRACTION AND EXTENSION TEST WAS PERFORMED AS PER AMM 32-30-00. THE LGCIU (P/N 664700500A4D S/N 2458) NR 2 WAS REPLACED AS PER AMM 32-31-00. SYSTEM FOUND OPERATING NORMAL AND THE AIRCRAFT RETURNED TO NORMA OPERATION. (M) 2L72 4F RTA28NM 20030917000992003091700099NM 2003 9 17 GAIA03048SP 120030719A5730 SKIN BOEING727 7272J0 138407ENM RT WING DEBONDED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND RT WING LOWER TRAILING EDGE PANEL 8605 HAS DISBONDED SPOT OUTER SKIN. CUT OUT 3 INCHES BY 48 INCHES, FABRICATED FILLER 3 INCHES BY 48 INCHES, LOWER DOUBLER 3 INCHES BY 48 INCHES 2024 T-3 .016 UPPER DOUBLER 4.5 BY 50 INCHES 2024 T-3 .020, REPAIRED IAW B727 SRM 57-30-1 FIG 1, 57-30-2 FIG 4, 51-40-6 FIG 1 AND 2, 51-40-20 FIG 13 AND 14. (M) 2L73 4F RTA3WE 20030917001142003091700114EA 2003 9 17 A6WA200340111 120030719A3320 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE OVERHEAD LIGHT ODOR A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31444ZW 7788 BURNING ODOR AT APPROXIMATELY ISLE 7 NEAR OVERHEAD FLOURESCENT LIGHTING. IN PROGRESS. 2L72 4F4 FRTA21EA E15NE 20030917001312003091700131NM 2003 9 17 DL78K030691 120030722A3397 CIRCUIT BREAKER BOEING737 737832 13844CFNM RIGHT OVERWING POPPED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO273734B 30776 RIGHT FWD AND AFT OVERWING LIGHT CAME ON DURING TAKE OFF ROLL - FOUND CIRCUIT BREAKER OUT - RESET SAME AND INSPECTED SYSTEM - ALL OK 2L72 4F RTA16WE 20030918000372003091800037NM 2003 9 18 GAIA03026SP 120030719A5311 FRAME BOEING727 7272J0 138407ENM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, MAIN CABIN FRAME BS 720 HAS A DENT INTO THE RADIUS BELOW STRINGER 16R. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR DOUBLER IAW B727 SRM 53-10-4 FIG 1, MAT USED .050 7075-T6 P/O NR 9911488 DIM 10 INCH BY 5 INCH. INSTALLED REPAIR IAW SRM 52-30-2. (M) 2L73 4F RTA3WE 20040122000782004012200078WP 2004 1 22 GTIA030963 120031118A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND FLOOR PANEL STATION 1250-1309 CORNERS DELAMINATED INSERTS PULLING OUT. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040122000852004012200085EA 2004 1 22 A6WA200340194 120031220A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 FOUND CRACKED BRACKETS, QTY 2, AT FS 484 RIGHT FUSELAGE, FLOOR LEVEL. REMOVED AND FABRICATED TWO BRACKETS AS PER SAMPLE MATERAL 6144-13 (2024-T42.050) WVAC PO 27909/1 IAW WVAC EO601R-53-4502 RT SIDE FS 484 RBL 9 AND RBL 27 AND INSTALLED SAME BRACKETS IAW WVAC EO 601R-53-4502 ALL STOPS COMPLIED WITH. (M) 2L72 4F RTA21EA 20040122000922004012200092EU 2004 1 22 USAASA03133 120031126A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19723UW 1109 THE LT OVERWING EMERGENCY LIGHT BATTERY FAILS THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LT OVERWING EMERGENCY LIGHT BATTERY. SYSTEM OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040122001052004012200105WP 2004 1 22 ASAA0380802 120031123A561046536091 SPRING DOUG DC9 DC983 3022083WP WINDOW BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 LAX PREFLIGHT CHECK, LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPLACED UPPER LOCK BAR SPRING. WINDOW THE OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040122001112004012200111WP 2004 1 22 GTIA030969 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND FLOOR PANEL STATION 207-256, CORNERS DELAMINATED, INSERTS MISSING, EDGE SEAL MISSING. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040122001282004012200128NM 2004 1 22 TSAA0326199 120031209A2612356044400 FIRE DETECTOR BOEING737 7372T4 1384492NM MLG WW FAILED A TSAAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP13808AL 23445 APPROXIMATELY 25 MILES FROM HNL, A WHEEL WELL FIRE LIGHT CAME ON. DEFER IAW MEL 26-4, SYSTEM DEACTIVATED IAW MEL. PLACARDS INSTALLED. REMOVED AND REPLACED WHEEL WELL FIRE AND OVERHEAT ELEMENT. OPS CHECK OK. PLACARD REMOVED FROM AIRCRAFT AND LOGBOOK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040122001372004012200137CE 2004 1 22 2004F00052 120031113A3010SM600BA40A1 CIRCUIT BREAKER LEAR 60 60LEAR 5170707CE DE ICE BOOT FAILED A RU3AO OTHER AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW1557 039 THE A/C WAS IN THE HANGAR AND A SMALL AMOUNT WAS DETECTED ABOVE THE AIRCRAFT, ON INVESTIGATION THE LT HORIZONTAL STAB DE-ICER BOOT WAS FOUND SMOKING AND ON FIRE. POWER WAS REMOVED FROM THE AIRCRAFT AND THE FLAMES AND SMOKE QUICKLY DIED OUT. THE STAB HEAT SWITCH WAS FOUND IN THE OFF POSITION. THE AVIONICS TECH WORKING ON THE AIRCRAFT HAD EXTERNAL POWE ON FROM TIME TO TIME WHILE TROUBLESHOOTING AN UNRELATED PROBLEM. FOUND CONTACTS WELDED SHUT ON REMOTE CONTROL CIRCUIT BREAKER. REPLACED RCCB AND HORIZONTAL STAB DE-ICE BOOT. (M) 2L72 4F RTA10CE 20040123000132004012300013WP 2004 1 23 ASAA0380696 120031027A531359360281 LONGERON DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD AT FS 1041-1060. REPLACED LONGERON SPLICE PER SRM 51-10-3. (M) 2L72 4F RTA6WE 20040123000232004012300023EU 2004 1 23 NTQA112779 120031114A6220350A31191600 STARFLEX SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR FAILED E NTQAO OTHER O OTHER NRNOT REPORTED 1 WP25922RJ1603 3422 PART FAILED WITH 597 HOURS REMAINING. STARFLEX HAS A KNOWN PROBLEM AND ACTIVE AD 2003-14-12. STAINLESS BUSHING DISBONDED. 1G71 3U3 U H9EU E19EU 20040123000472004012300047NE 2004 1 23 MEX2003548 220031210A7261B19151 OIL FILTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D217A 52053NE NR 2 ENGINE CLOGGED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23158PL 49761 AC RETURNED THIRTY MINUTES AFTER TAKEOFF, THE (RT OIL STRAINER CLOGGING) LIGHT CAME ON. CAPTAIN INFORMED THAT THE ENGINE WAS NOT TURNED OFF AND IT WAS PUT AT FLIGHT IDLE POWER. AT PLATFORM THE MAIN FILTER ASSY AND THE CHIP DETECTORS WERE INSPECTED, THE FILTER WAS FOUND CONTAMINATED WITH COAL. THE FILTER WAS CLEANED AND THE PROCEDURE OF FILTER PRESS SENSING WAS PERFORMED IAW MM. AT STATION THE MAIN OIL FILTER, DIFFERENTIAL PRESSURE ALARM, RESTRICTORS P5 AND P6 AND FLIGHT DATA RECORDER WERE REPLACED IAW MM, TESTS OK, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040121000222004012100022NM 2004 1 21 03FDEA02264 120031226A5744ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING O/B FLAP I/B HINGE FITTING O/B MOUNT I/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040121000302004012100030NM 2004 1 21 03FDEA02317 120031228A5510ALC81041 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB LT UPPER CENTER PLANK NR 18L BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-7522, HORIZONTAL STAB BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2L73 4F RTA22WE 20040121000322004012100032NM 2004 1 21 03FDEA02315 120031226A5510ALC81041 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB LT UPPER CENTER PLANK 25L BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-75222, HORIZONTAL STAB BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2L73 4F RTA22WE 20040121000972004012100097SO 2004 1 21 SIMA200331402 120031106A2120 ODOR EMB 135 EMB135KL 3260302SO CABIN DETECTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 DURING APU START, THE APU FAILED TO START. WHEN BATTERY SWITCHES WERE RETURNED TO AUTO CREW REPORTED A STRONG BURNING ELECTRICAL ODOR. MEL WAS ISSUED AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK OF THE APU SYSTEM WAS COMPLIED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031203001842003120300184WP 2003 12 3 GTIA030897 120031101A7120K22199SA31 ISOLATION MOUNT DOUG DC9 DC981 3022081WP ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 RT ENGINE FORWARD LOWER VIBRATION ISOLATOR NEEDS TO BE REPLACED. REMOVED AND REPLACED RT ENGINE FORWARD LOWER VIBRATION ISOLATOR. (M) 2L72 4F A6WE 20030918000402003091800040NM 2003 9 18 2003F00567 120030502A5315 FLOORBEAM BOEING737 7372L9 1384497NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO27464AT 21278 DURING C-CHECK INSPECTION SURFACE CORROSION WAS FOUND TO BE BEYOND LIMITS AT FLOORBEAM BS 947.5. DURNG EVALUATION OF THE AREA A PREVIOUS WAS NOTED ON THE SAME FLOORBEAM. IN ORDER TO REPAIR THIS SKYKING OPTED TO REPLACE THE ENTIRE FLOORBEAM CAP. AIRCRAFT CHANGE ORDER WAS GENERATED (ACO 035334) AND FLIGHT VEHICLES CONSULTING DRAWING NR 53-03246-1. ALL WORK WAS ACCOMPLISHED ON NON ROUTINE 031249. (M) 2L72 4F RTA16WE 20030918000962003091800096SW 2003 9 18 EPD2003F00001 120030615A2130TIGMSI1CWHC SWITCH GULSTM690TP 690C 7630517SW GARRTTTPE331TPE331* 01514WP COCKPIT FAILED B EPDRO OTHER O OTHER NRNOT REPORTED 1 NM1373EF 5179 11617 ROCKER SWITCH WHICH CONTROLS THE AIR CONDITIONING AND THE ENVIROMENTAL FANS WAS FOUND OVERHEATED. THE SWITCH HAS LOOSE TERMINALS AND CHECK WITH HIGH RESISTANCE. THE CIRCUIT BREAKER DID NOT TRIP AND IS LOCATED IN THE AFT ELECTRICAL COMPARTMENT. 1H72 3T3 T 2A4 E2WE 20030918001152003091800115WP 2003 9 18 NACA20030102 120030806A77122210525A51 TRANSMITTER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE READS LOW A NACAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL0399330476 476 43576 28737 TAKE OFF ABORTED DUE TO NR 2 ENGINE LOW BMEP. NR 2 ENGINE BMEP DEFERRED: REPLACED BMEP TRANSMITTER. 2L74 4R4 R A781 5E8 20030918001442003091800144NM 2003 9 18 NACA20030103 120030806A793042D107A2 PRESSURE SWITCH BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE NR 1 ENGINE FALSE INDICATIONA NACAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AL03930FT580 580 19387 P657108 NR 1 ENGINE OIL PRESSURE WARNING LIGHT(BYPASS), FLICKERING DURING CLIMB. INSPECTED NR 1 ENGINE MAIN OIL FILTER. NO METAL FOUND, INSTALLED NEW FILTER. DEFERRED OIL FILTER BYPASS INDICATION. OIL FILTER ON 12 HOUR INPECTION INTERVAL I.A.W. 727 MEL 79-2. 2L73 4F4 FRTA3WE E2EA 20030919000112003091900011WP 2003 9 19 03FDEA01241 120030810A5531AMC7107AMC7185 SPAR CAP DOUG DC10 DC1030F 3023504WP GE CF6 CF650* 30018NE VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 MDIS 311 55-30 0008866 05AUG03 BFM CLOSE COMPLY WITH E.A.8-5530-72245. STABILIZER-VERT-REWORK OF CORROSION ON SPARS AMC7107 AND AMC7185 ENT BY3A 60601C RPT BY 3A 60601C. FACT 08AUG03 19 PERCENT 3A29 BFM COMPLIED WITH EA 8-5530-72245 STABILIZER-VERT-REWORK OF CORROSION ON SPAR CAPS AMC7107 AND AMC7185 ENT BY 3A 39017C RPT BY 3A 39017C. 2L73 4F4 FRTA22WE E23EA 20030919000402003091900040NM 2003 9 19 IU62003F00024 120030530A278165447525 HOUSING BOEING737 737* NM ACTUATOR CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 1886C SLAT ACTUATOR HOUSING CRACKED. ADD TO DNT REQUIREMENTS IN OHM. (NR 177263) 2L72 4F RTA16WE 20030919000622003091900062NM 2003 9 19 HALA0300647 120030722A2750 PSEU BOEING767 76733A 1385209NM PWA 4060 PW4060 52119NE TE FLAP INOPERATIVE A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13582HA 28139 TRAILING EDGE FLAP LIGHT ON. FLAPS SELECTED TO 5 DEGREES, FLAPS ONLY EXTENDED TO 1 DEGREE. PSEU CODE 27-81041. REPLACED NR 1 OUTBOARD RDVT IAW MM 27-31-11 OPS CHECK FLAP/SLAT OK. 2L72 4F4 FRTA1NM E24NE 20030919000892003091900089NM 2003 9 19 375PA0018 120030810A3397 WIRE BOEING737 737317 138447PNM EMERGENCY LIGHT OPEN A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05375PA 23812 FIRST EMERGENCY LIGHT ON LEFT AISLE FLOOR POPPED OFF. FOUND OPEN ON WIRE AT FIRST EMERGENCY LIGHT. RE-SPLICED WIRE. FLOOR PATH OPS CHECKS GOOD. 2L72 4F RTA16WE 20030919001022003091900102SO 2003 9 19 QY52003F00000 120030801A243538370213 STARTER GEN GULSTMG1159 G1159 3953505SO ENGINE FAILED A QY5RO OTHER O OTHER NRNOT REPORTED 1 NE01105TB6609 31 NR 1 ENGINE FAILED TO START. ON INVESTIGATION OF PROBLEM, FOUND STARTER CENTRIFUGAL SWITCH HAD MALFUNCTIONED. ORDERED NEW STARTER. WHEN OLD STARTER WAS REMOVED, IT WAS DISCOVERED THAT THE STARTER SHAFT BEARINGS HAD FAILED, THIS IS MOST LIKELY WHAT TOOK OUT THE CENTRIFUGAL SWITCH. 2L72 4F RTA12EA 20030919001032003091900103EU 2003 9 19 36020602032 120030602A6720350A33214501 PITCH LINK SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR WORN E S4WAK NONE O OTHER ININSP/MAINT 1 WP07820NA597 3602 22342 TAIL ROTOR PITCH CONTROL LINKS WORN. 1G71 3U3 U H9EU E00054EN 20030919001072003091900107EU 2003 9 19 36020602034 120030602A6730SC5084 SERVO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE MAIN ROTOR LEAKING E S4WAK NONE K FLUID LOSS ININSP/MAINT 1 WP07820NA597 3602 22342 M/R PITCH SERVO LEAKING EXCESSIVLY. 1G71 3U3 U H9EU E00054EN 20030919001572003091900157EU 2003 9 19 AWXA200300937 120030803A5320D5347047720400 PROFILE AIRBUS320 A320232 3930326EU CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 MCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LT TRANSITION PROFILE BETWEEN FR 56-60. MAINTENANCE REMOVED LT TRANSITION PROFILE FROM FR 56 TO FR 60; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-12, FIG. 2 & 3. 2L72 4F RTA28NM 20030922000212003092200021NM 2003 9 22 2003UALA00618 120030812A5314 KEELBEAM BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29618UA 21878 KEELBEAM WEB DRAIN HOLE HAS CORROSION AT BS 786, BL0. 2L72 4F4 FRTA1NM E3NE 20030922000252003092200025NM 2003 9 22 2003UALA00622 120030812A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA 29239 E/E BAY AT BS 246 BEAM STIFFENER CRACKED AT FWD FACE OF BEAM, LBL 26. 2L72 4F4 FRTA1NM E24NE 20030922000272003092200027NM 2003 9 22 2003UALA00624 120030813A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29541UA 25253 EXTERNAL FUSELAGE DAMAGED AT STA 620 STR 8R. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20030922000492003092200049NM 2003 9 22 PCAA0308100 120030819A7920 B-NUT DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RT ENG OIL LEAKING A PCAAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA13980HA269825 376 120988 CREW REPORTED THAT THE RT ENGINE OIL PRESSURE FLUXUATED BETWEEN 40 AND 50 PSI AT CRUISE FLT OF 11,000 FT. NR 2 ENGINE WAS SHUT DOWN AND FLIGHT DIVERTED TO ACY. MAINTENANCE TROUBLESHOT AIRCRAFT AND FOUND A B-NUT FOR THE OIL PRESSURE TRANSMITTER TO BE LOOSE. B-NUT WAS TIGHTENED, AREA OF ENGINE WAS CLEANED. PERFORMED MFG LOSS OF OIL PRESSURE / LOW OIL PRESSURE INSPECTION IAW MFG MM 05-50-00. AIRCRAFT GROUND RAN AT 80 PERCENT WITH NO DEFECTS NOTED. NR 2 ENGINE OIL CAP ADJUSTED. NO LEAKS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030922000562003092200056CE 2003 9 22 081903 120030813A32601CH16 SWITCH LEAR 25 25D 5170514CE MLG OUT OF RIG E ESUAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE039QM 286 AFTER DEPARTURE THE GEAR WOULD NOT RETRACT, THE AIRCRAFT RETURNED TO THE AIRPORT WITHOUT AN INCIDENT. AFTER INVESTIGATION, THE LEFT GEAR DOOR SWITCH WAS OUT OF RIG. THE SWITCH WAS RIGGED AND GEAR WAS FUNCTION CHECKED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4J A10CE 20030922000572003092200057NE 2003 9 22 N382003F00001 220030801A73216047T74P13 FUEL CONTROL CNDAIRCL600 CL6002A12 1900304EA GE CF34 CF34* NE LT ENGINE FAILED E N38AA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA05163WG 3057 AT APPROXIMATELY 0650 PACIFIC TIME, WHILE ON CLIMB OUT AND CLIMBING THROUGH 5500 FT MSL THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE LEFT ENGINE. ALL CHECKLISTS AND PROCEDURES WERE FOLLOWED. AN EMERGENCY WAS DECLARED, AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE WAS CONTRACTED AND ALL PROCEDURES VIA OPS AND MAINTENANCE WERE ACCOMPLISHED. REPRESENTATIVES WERE DISPATCHED TO AIRCRAFT. A/C WAS GROUND RUN AFTER INCIDENT WITH NO ABNORMAL EFFECTS. ENGINE FUEL CONTROL UNIT WAS REPLACED AT ENGINE MFG RECOMMENDATION. 2L72 4F4 FRTA21EA E15NE 20030922000662003092200066NM 2003 9 22 AWXA200300941 120030819A21317638101 CONTROLLER BOEING737 737277 1384570NM CABIN PRESSURE MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28182AW384841660 22649 ON INITIAL TAKEOFF ROLL EN ROUTE, THE CABIN CLIMB INDICATOR NEEDLE WENT TO RAPID RATE OF DESCENT OF ABOUT 4000 FPM, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, PERFORMED OPERATIONAL CHECK IAW T/C F1B21001. RAN ENGINE AT TAKEOFF POWER, AIRCRAFT PRESSURIZATION WAS NORMAL. VENDOR FUNCTIONAL TEST OF CABIN PRESSURE CONTROLLER, CONFIRMED FAILURE OF UNIT. R & R 2 CAPACITORS. UNIT WAS TEST AND RETURNED TO SERVICE IAW CMM 21-31-11, REV. 13. 2L72 4F RTA16WE 20030922000712003092200071NM 2003 9 22 AWXA200300948 120030804A5320D53924966200 PROFILE AIRBUSA319 A319132 3930340NM CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 61, BETWEEN STR 39 LT AND 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 61, BETWEEN STR 39 LT AND 39 RT ; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12, & 21-22. 2L72 4F RTA28NM 20030922000762003092200076NM 2003 9 22 AWXA200300953 120030804A5320D53974967200 PROFILE AIRBUSA319 A319132 3930340NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 59, STR 39 LT - 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 59, STR 39 LT - 39 RT; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12, & 21-22, FIG. 3 & 8. 2L72 4F RTA28NM 20030917001022003091700102NM 2003 9 17 GAIA03045SP 120030719A5311 FRAME BOEING727 7272J0 138407ENM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 580 HAS A DENT AT STRINGER 16 RT, FASI N/R 36051. CUT OUT DAMAGE 1 INCH BY 1.5 INCH, REPAIR DOUBLER 7075 T-6 INSTALLED IAW B-727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20030917001072003091700107NM 2003 9 17 AMTA200301054 120030812A3350S417N5101007 LENS BOEING737 73783N 13844HINM EMERGENCY LIGHT MISSING A AMTAK NONE O OTHER ININSP/MAINT 1 GL11310TZ 28243 RIGHT SIDE OVERWING AFT LOWER EMERGENCY LIGHT LENSE ASSEMBLY MISSING. INSTALLED NEW LIGHT ASSEMBLY, OPS CHECK GOOD REF MM 33-51-01-2. (M) 2L72 4F RTA16WE 20030918000542003091800054NM 2003 9 18 DL76G030709 120030729A5753113T11671 SUPPORT BOEING767 7673P6 1385105NM LT WING TE FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27154DL 25241 LT WING INBOARD FLAP, INBOARD SUPPORT BEAM NR 4 HAS HOLE BORE CORROSION, CORROSION WAS FOUND IN THE 4 FLAP ATTACH FASTENER HOLES IN THE INBD SUPPORT BEAM OF THE INBOARD FLAP AT THE NR 4 SUPPORT LOCATION. THE HOLES WERE OVERSIZED TO REMOVED CORROSION, HFEC INSPECTED, BUSHED, AND NEW FASTENERS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385477-14, REV A. 2L72 4F RTA1NM 20030918000672003091800067NE 2003 9 18 NACA20030100 220030802A7421URHB32E SPARK PLUG DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL032907F461 461 44636 33553 NR 4 ENGINE SHUT DOWN DUE TO NR 2 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED NR 4 ENGINE NR 2 CYLINDER FRONT AND REAR SPARK PLUGS. 2L74 4R4 R A781 5E8 20030918001042003091800104CE 2003 9 18 DLD2003F00000 120030616A781017500115 SHROUD CESSNA177 177B 2073708CE LYC O360 O360A1F6 41514EA MCAULY2D34C B2D34C208 GL EXHAUST FAILED D DLDGO OTHER O OTHER NRNOT REPORTED 1 SO05342292444 17701721 L1656036A 720649 THE SCREEN THAT KEEPS FOREIGN MATERIAL FROM ENTERING CARBURETOR WHEN CARB HEAT IS ON. SPOT WELDS THAT HOLD SCREEN IN PLACE ARE COMING LOOSE AND LETTING SCREEN VIBRATE AND COME APART. THIS WOULD LET PIECES OF THE SCREEN GO INTO ENGINE WHEN CARB HEAT IS ON. 1H71 3O3 O A13CE E286 5 CP7EA 20030919000162003091900016EU 2003 9 19 03FDEA01230 120030809A5310 STRUCTURE AIRBUS310 A310 EU AIRFRAME VIBRATION A FDEAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO25415FE 349 AIRFRAME VIBRATION STARTED CLIMBING OUT AT FL22.5 2CD A330 KIAS. ENGINE DATA N1-104.1 2C104.23A EGT 832 2C 841 3A VIBES 0.62C+0.2 3A N2 VIBES 2.0 2C0.4. VIBRATION REMAINED THROUGHOUT FLIGHT UNTIL DESCENDING PAST FT.VIBRATION WOULD DECREASE AS POWER WAS REMOVED BUT CAME BACK AS POWER WAS REAPPLIED. ACFT SLOWED FIRST TO .78 MACH 2C THEN TO 275 KIAS NO HELP. ALL FLIGHT CONTROLS APPEARED OK EXCEPT STAB APPEARED TO VIBRATE VERY SLIGHTLY UP AND DOWN CHANGING AUTOPILOTS DID NOT HELP. 2L72 4F RTA35EU 20030919000222003091900022 2003 9 19 EA332003B0977 420030630A2565 LOCKING PLATE BOEING747 747400 NM GE CF6 CF680 30025NE ESCAPE SLIDE BENT B LU7FK NONE L NO TEST ININSP/MAINT 1 EA33494MC 29255 DURING AN OPERATIONAL CHECK OF THE INFLATABLE EVACUATION SYSTEM AT THE RT UPPER DECK DOOR ACCORDING MS 23-66-00-040-100 THE RESERVOIR WAS NOT ACTIVATED AND THE SLIDE DID NOT INFLATE. FURTHER INVESTIGATION REVEALED THAT THE PACKBOARD LOCKING PLATE WAS RELEASED DUE TO A BENT MECHANISM. THEREFORE, THE LOCKING PLATE SLIPPED OVER THE LOCKLEVER AND WAS NOT ABLE TO FULLFIL THE ORIGINAL FUNCTION. CHANGED BENT LOCKING PLATE. 2L74 4F4 FRTA20WE E13NE 20030919000482003091900048CE 2003 9 19 53300 120030806A2720 RUDDER BEECH 1900 1900D 1154162CE TAIL MALFUNCTIONED A AMWAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CE075YV UE5 AFTER DEPARTURE, ON FLIGHT 5530, THE CREW HAD A HARD RT THEN LAT UNCOMMANDED RUDDER BOOST. WHILE EXECUTING THE UNCOMMANDED RUDDER BOOST ACTIVATION EMERGENCY PROCEDURE CHECKLIST A THIRD SEVERE RUDDER BOOST ACTIVATION OCCURRED, FOLLOWED BY SEVERE OSCILLATIONS ON THE HORIZONTAL AXIS. THEY IMMEDIATELY REDUCED SPEED TO 170 KNOTS AND THEN COMPLETED THE EMERGENCY CHECKLIST. DUE TO THE SEVERITY OF THE OSCILLATIONS AND PASSENGER CONCERNS, THE REQUESTED FROM IAH AIR TRAFFIC CONTROL TO RETURN AS A PRECAUTION. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS MEL'D AND RETURNED TO SERVICE. STILL AWAITING MORE INFORMATION. 2L72 4T RTA24CE 20030919000662003091900066EU 2003 9 19 COE2003F00002 120030723A3250AC61906 CONTROL VALVE FOKKERF27 F27MK600 4990706EU RROYCEAVON AVON532R 54517EU NLG STEERING INTERMITTENT A COEAO OTHER J WARNING INDICATION CLCLIMB 1 NM13742FE 10349 36114136 DEPARTING, AFTER TAKEOFF, NOSE GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED UP. GEAR DOWN WAS SELECTED AND NORMAL ILLUMINATED. FLIGHT CONTINUED. MAINTENANCE OPERATIONALLY CHECKED STEERING AND RETRACTION SYSTEMS AND COULD NOT DUPLICATE MALFUNCTION. THE STEERING FOLLOW UP CONTROL VALVE WAS REPLACED AS A PRECAUTIONARY MEASURE DUE TO PREVIOUS HISTORY WITH THIS VALVE. NO FURTHER PROBLEM AS OF 7/30/03. 2H72 4T4 J A817 E307 20030919000832003091900083CE 2003 9 19 YBS2003F00000 120030724A3213514110314 BARREL CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO RT MLG SHEARED E YBSAO OTHER O OTHER NRNOT REPORTED 1 EA1736911 402C0314 UPON LANDING, PILOT REPORTED RT MLG COLLAPSED. MECHANIC FOUND RT MLG UPPER BARREL SHEARED ABOVE UPPER TORQUE LINK ATTACH POINT. MECHANIC REMOVED AND REPLACED MLG ASSY, RT PROP, RT ENGINE, C/W MINOR SHEET METAL REPAIRS TO FLAPS, AND REPLACED RT MLG DOOR. INSPECTION OF RUNWAY AT LANDING AREA FOUND MANY POT HOLES AND RUTS. 1L72 3O3 O A7CE E8CE 20030922000532003092200053SO 2003 9 22 T1O2003F00000 220030806A8520649134 CRANKSHAFT CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO ENGINE FAILED B T10RO OTHER O OTHER NRNOT REPORTED 1 EA112PC 203 21060251 242857R CRANKSHAFT FRACTURED AT NR 2 CHECK. ENGINE TORN-DOWN. CRANKSHAFT AND OTHER ENGINE COMPONENTS SENT TO MFG ANALYSIS LAB. CRANKSHAFT HAD PREVIOUSLY UNDERGONE AND PAST METALURGY INSPECTION IAW MSB-00-5D AND AD 200-23-26. MORE STRINGENT TESTING ON ENTIRE SHAFT SHOULD BE CONSIDERED. 1H71 3O3 O 3A21 E5CE 20030922000622003092200062EU 2003 9 22 XNOA01145 120030819A7722 INDICATOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE EGT INOPERATIVE A XN0AD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 GL23474AS 219 NR 1 EGT GAUGE INOPERATIVE. RED FLAG. NO INDICATION ON DIGITAL OR ANALOG DURING START. ACTION TAKEN: REMOVE AND REPLACE EGT INDICATOR. OPS CHECK GOOD IAW A300 MM 77-21-11. 2L72 4F4 FRTA35EU E23EA 20030922000682003092200068EU 2003 9 22 AWXA200300945 120030819A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSFAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28619AW11776 527 OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED STEP 5B (2), TEST PANEL INDICATED (INT. LOADS EMER L). MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030922001212003092200121EA 2003 9 22 COMA0360378 120030813A2497D18ZZA CONTACTOR CNDAIRCL600 CL6002B19 1900309EA UTILITY BUSS BURNED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01451CA4450 7562 FLIGHT 5374 DURING CRUISE FLIGHT THE ADG AUTO DEPLOYED, RECEIVED AN AC NR 1 TRU MESSAGE FOLLOWED BY SMOKE IN THE COCKPIT, AIRCRAFT DIVERTED TO RDU AND LANDED SAFELY. IT IS BELIEVED THAT THE UTILITY BUS CONTACTOR IK4XD OVERHEATED CAUSING COLLATERAL DAMAGE TO THE LT CONTACTOR TRAY AND WIRING. 2L72 4F RTA21EA 20030922001292003092200129NM 2003 9 22 AWXA200300961 120030805A5315D53472172204 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON PANEL MOUNTING HOLE OF FLOORBEAM Y1792, AFT OF FR 66, INBOARD OF L-2 DOOR FORWARD GIRT BAR MOUNTING BLOCK. MAINTENANCE ENLARGED MOUNTING HOLE TO MAXIMUM ALLOWABLE DIAMETER, CORROSION STILL PRESENT; CUTOUT DAMAGE ON FLOORBEAM Y1792, AFT OF FR 66; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A319 SRM 53-41-14, PG. 201-213, FIG. 201. 2L72 4F RTA28NM 20030923000062003092300006SO 2003 9 23 WVBA2003002 120030709A2731 JACKSCREW PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA ELEVATOR TRIM BINDING E WVBAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AL0142WP 318252038 WHILE DEPARTING, ELEVATOR TRIM WHEEL JAMMED AND PILOT WAS UNABLE TO FREE SYSTEM. ELEVATOR TRIM WAS STUCK IN A NOSE DOWN CONFIGURATION. PILOT WAS ABLE TO COUNTERACT TRIM PRESSURES AND CONTINUED TO WHERE AIRPORT EMERGENCY CREWS WERE AVAILABLE. MAINTENANCE FOUND THE ELEVATOR TRIM JACK SCREW BOUND UP TO TRIM CABLE DRUM. JACK SCREW WAS DISCONNECTED FROM TAB AND FUNCTIONED WITH NO PROBLEMS. MAINTENANCE RERIGGED ELEVATOR TRIM SYSTEM IAW SM. FLIGHT CHECK WAS COMPLIED WITH GOOD RESULTS. AC WAS RELEASED TO OPERATIONS. INSPECTORS MET AC ON LANDING, INVESTIGATION WAS CONDUCTED, ACCUMULATIVE WEAR IN SYSTEM ALLOWED THE ELEVTOR TAB JACKSREW TO EXCEED ITS NORMAL LIMIT CAUSING THE JAM. NO RECENT WORK HAD BEEN DONE. 1L72 3O3 O A20SO E14EA 20030923000072003092300007EU 2003 9 23 MALA030377 120030817A2121 FAN SAAB SF340 340B 7860101EU CABIN COOLING FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15363PX 340B260 DISC NR 9M STRONG ODOR SIMILAR TO OZONE ASSOCIATED WITH ELECTRICAL MALFUNCTION. DETECTED PRIOR TO ENGINE STARTS. PAX AND CREW EVACUATED. REARMOST PAX EXPERIENCED GREATEST DISCOMFORT. MAINTENANCE DEFERRED BOTH AFT AND FWD SUPP AIR, AIR REF MM1 PG 177815 FOR DETAILS. FOUND AFT SUPP AIR COMPRESSOR MOTOR COOLING FAN SHATTERED AND SHROUD MELTED CAUSING ODER. ALSO FOUND FWD COMPRESSOR BELT AND SHROUD DAMAGED SEE CONTINUATION CARD NR 061478 AND 071616 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20030923000152003092300015NM 2003 9 23 AWXA200300968 120030821A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROWS 19-23 BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28311AW 24712 EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 19 THRU 23 LT ARE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030923000182003092300018EU 2003 9 23 RAIA00308216 120030809A3260AIR136070 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU NLG MALFUNCTIONED A RAIAO OTHER J WARNING INDICATION CRCRUISE 1 CE03558HK 41071 RED LIGHT IN GEAR HANDLE WITH GEAR UP. MAINTENANCE REMOVED AND REPLACED NLG UNLOCK SWITCH. 2L72 4T RTA41NM 20030923000192003092300019SO 2003 9 23 RAIA00308217 120030820A326023092900001 UPLOCK EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03822HK10553 145069 GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX. 2L72 4T RTT00011AT 20030923000322003092300032WP 2003 9 23 DHL2003604586 120030528A5730 SKIN DOUG DC8 DC873F 302199FWP LT CENTER WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT INNER WING CENTER EXTENDED L/E UPPER SKIN CORRODED AROUND STA. XFS.341.500 TO XODI 6.2245. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.11-12. TRIMMED OUT CORRODED AREA. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.071) AND SIX FILLERS (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER AND FILLERS ON LT. INNER WING CTR. EXTENDED L/E UPPER SKIN AROUND STA. XFS.341.500 TO XODI. 6.2246 USING NEW FASTENERS. 2L74 4F RT4A25 20030923000372003092300037WP 2003 9 23 DHL2003604578 120030526A53473657503501 SEAT TRACK DOUG DC8 DC873F 302199FWP COCKPIT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 NAVIGATOR FWD SEAT TRACK WITH ELONGATED HOLES. REMOVED NAVIGATOR FWD. SEAT TRACK WITH ELONGATED HOLES IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW NAVIGATOR FWD. SEAT TRACK IAW SRM 51-3-0 PG.1 2L74 4F RT4A25 20030923000382003092300038WP 2003 9 23 DHL2003604595 120030525A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT INNER WING UPPER SKIN CORRODED AROUND STA XRS 184.000 BETWEEN CTR SPAR AND S-9R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED SKIN AREA IAW EODHL-030534, ED-3356. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.125) IAW EODHL-030534, ED-3356. CLEANED, TREATED AND PRIMED DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON RT INNER WING UPPER SKIN AROUND STA XRS 184.000 USING NEW FASTENERS IAW EODHL-030534, ED-3356 AND SRM 51-1-21 PG 1. SEE N\R 3824 FOR LEAK CHECK. 2L74 4F RT4A25 20030923000402003092300040WP 2003 9 23 DHL2003604629 120030522A5730 VANE DOUG DC8 DC873F 302199FWP LT WING ELONGATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR L/E VANE SLOT HOLES ELONGATED AT XOLDI 6.224. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. TRIMMED OUT THE ELONGATED HOLES SKIN AREA. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR EXTERNAL DOUBLER (7075-T6 AL0.071), A FILLER (7075-T6 AL0.063) AND INTERNAL DOUBLER (7075-T6 AL0.050). CLEANED, TREATED AND PRIMED THE REPAIR EXTERNAL DOUBLER INTERIOR SURFACE, FILLER AND INTERNAL DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED INTERNAL DOUBLER AND FILLER AND REPAIR EXTERNAL DOUBLER ON LT WING CTR L/E VANE SLOT WITH NEW FASTENERS IAW EODHL-030544, ED-3301 SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030923000412003092300041WP 2003 9 23 DHL2003604749 120030521A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING CTR. EXTENDED L/E SLOT HAS ELONGATED HOLES AT STA. XFS.526.000. (MAJOR REPAIR) PERFORMED MAJOR REPAIR IAW EODHL-030550, ED-3353. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. BLENDED OUT THE ELONGATED HOLES SKIN AREA IAW EODHL-030550, ED-3353. PEFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER ON LT. OUTER WING CTR. EXTENDED L/E SLOT STA. XFS.526.000 USING NEW FASTENERS IAW EODHL-030550, ED-3353 AND SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030923000472003092300047WP 2003 9 23 DHL2003604759 120030527A5310 STRINGER CLIP DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT ACCESSORY COMPT. CLIP ATTACHING FRAME TO SKIN AT STA.660.000 L-22R WITH 2.000 CRACK IN IT. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG.21. FABRICATED NEW CLIP (STEEL 301 0.500 H0.050) IAW SRM 53-1-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-20D PG.9, SRM 51-1-14A. 2L74 4F RT4A25 20030923000622003092300062WP 2003 9 23 DHL2003604658 120030604A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FUSELAGE NOSE SECTION EXTERNAL AC POWER RECEPTACLE COMPARTMENT OUTER SKIN WORN STA -39.000 L-31R TO L-33R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030551, ED-3295. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6AL 0.063), A FILLER (7075-T6AL 0.050) IAW EO DHL 030551, ED-3295. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT CON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER ON EXTERNAL A/C POWER RECEPTACLE COMPARTMENT OUTER SKIN, STA -39.000 L-31R TO L-33R USING NEW FASTENERS IAW EO DHL 030551, ED-3295 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000652003092300065WP 2003 9 23 DHL2003604714 120030608A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LOWER FUSELAGE EXTERIOR SKIN SHOWS SEVERAL SPOTS OF CORROSION BETWEEN STA 510.000 AND 570.000, L-31R - L-34R. PERFORMED MAJOR REPAIR IAW EODHL-030541, ED-3310. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT CORRODED AREA IAW EODHL-030541, ED-3310. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED DOUBLER (7075-T6 AL0.071) IAW EODHL-030541, ED-3310. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER WITH NEW FASTENERS IAW EODHL-030541, ED-3310, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030922000222003092200022NM 2003 9 22 2003UALA00619 120030812A5310 SHEAR TIE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA 29239 AFT CARGO PIT AT BS 1197+66 BETWEEN STR 39L TO STR 39R, SHEAR TIE IS CORRODED. 2L72 4F4 FRTA1NM E24NE 20030922001032003092200103EU 2003 9 22 BAQA088894 120030828A2150SD508 COMPRESSOR AEROSPAS365 AS365N2 8680815EU AIR CONDITIONER FROZEN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 AIR CONDITIONER COMPRESSOR FROZE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030922001262003092200126EU 2003 9 22 0301583226 120030815A2910 LINE AIRBUS320 A320211 3930320EU HYD SYSTEM CHAFED A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01326US 282 IN MODERATE TURBULENCE, AUTOPILOT KICKED OUT AND RECEIVED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL MESSAGE ON ECAM. FOLLOWED COM PROCEDURE AND LANDED AT DTW UNEVENTFULLY. FOUND YELLOW SYSTEM COMPLETELY EMPTY. FOUND SPOILER HYDRAULIC PRESSURE LINE CHAFED ON WIRING RACEWAY. REPAIRED LINE WITH RING-LOK REPAIR PER AMM. SERVICED YELLOW HYDRAULIC RESERVOIR. SYSTEM LEAK CHECK OIK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030923000242003092300024WP 2003 9 23 DHL2003604571 120030529A57305705518504 SKIN DOUG DC8 DC873F 302199FWP RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING T/E LOWER PANEL EXT. SKIN DELAMINATED (NR 540 ACCESS) REMOVED AND REPLACED LOWER PANEL ON RT WING T/E (NR 540 ACCESS) IAW SRM 51-3-0 PG.1 2L74 4F RT4A25 20030923000342003092300034WP 2003 9 23 DHL2003604584 120030610A5714 ACCESS DOOR DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT C/W AUX TANK - PERFORM ANTI-CORROSION TREATMENT TO LT 5056 ACCESS DOOR. REMOVED CORROSION ON LT 5056 ACCESS DOOR IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG.43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (7075-T6 AL0.080) IAW SRM 57-2-1 FIG.43. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ON LT 5056 ACCESS DOOR IAW SRM 51-1-21 PG.1. SEE N/R 3824 FOR FUEL LEAK CK. 2L74 4F RT4A25 20030923000572003092300057WP 2003 9 23 DHL2003604728 120030515A53204641324N SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT AFT SPLICE FITTING WITH 1.000 CRACK IN IT (STA 1690.000 A 1700.000, L-30L). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030923000892003092300089WP 2003 9 23 DHL2003604683 120030506A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP SERVICE DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 A 1.000 CRACK IN FWD UPPER CORNER OF FWD SERVICE DOOR JAMB. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-127, DWG 5750776, DWG SR08530021. CUT OUT DAMAGED AREA; FABRICATED (2) FILLERS (7075-T6 AL0.050) (7075-T6 AL0.063) AND (2) DOUBLER (7075-T6 AL0.063) (7075-T6 AL0.080) IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-127, DWG 5750776, DWG SR08530021. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLERS AND DOUBLERS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-127, DWG 5750776, DWG SR08530021, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000932003092300093WP 2003 9 23 DHL2003604684 120030507A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP SERVICE DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT UPPER CORNER OF RT AFT SERVICE DOOR JAMB WITH 2 CRACKS 1.000 APPROX IN IT. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 16 SHEET 4, TR 53-131, DWG 5750776, DWG SR08530021. CUT OUT DAMAGED AREA AND FABRICATED, FILLER (7075-T6 AL0.032) (7075-T6 AL0.080) AND (2) DOUBLERS (7075-T6 AL0.090) (7075-T6 AL0.125) IAW SRM 53-2-0 FIG 16 SHEET 4 TR 5-131, DWG 5750776, DWG SR08530021. CLEANED, TREATED AND PRIMED AREA AND FILLERS AND DOUBLERS IAW SRM 51-1-8B. INSTALLED FILLERS AND DOUBLERS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 16 SHEET 4, TR 53-131, DWG 5750776, DWG SR08530021, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000962003092300096WP 2003 9 23 DHL2003604663 120030616A5751 SKIN DOUG DC8 DC873F 302199FWP LT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBD. AILERON L/E UPPER PLATING HAS THREE CRACKS OF 0.750, 0.500, 0.500 AT STA. XA 487.000 - XA 569.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-8-1 FIG.1. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG. 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW PLATING (7075-T6AL 0.040) IAW SRM 57-1-0 PG.1, SRM 57-8-1 FG.1. CLEANED, TREATED AND PRIMED NEW PLATING INTERNAL SURFACE IAW SRM 51-1-8B. INSTALLED NEW PLATING WITH NEW FASTENERS IAW SRM 51-1-21 PG.1. FOR W/B SEE NR 4049. 2L74 4F RT4A25 20030923001052003092300105WP 2003 9 23 DHL2003604762 120030622A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD CTR SECTION SHOWS SEVERAL SPOTS OF CORROSION AND DOUBLER REPAIR (03 EA.) BETWEEN STA.660.000 AND STA.725.000, L-34L TO L-34R. PERFORMED MAJOR REPAIR IAW EODHL-030564, ED-3389. REMOVED FASTENERS AND DOUBLER REPAIRS, REMOVED CORROSION. FOUND OUT OF LIMITS. BLENDED OUT CORRODED AREA IAW. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6 AL0.125), DOUBLER (7075-T6 AL0.125) IAW EODHL-030564, ED-3389. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS. 2L74 4F RT4A25 20030923001282003092300128CE 2003 9 23 DXTA200300100 120030823A3230 CONTROL UNIT CESSNA650 650 2076802CE MLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07789QS 6507089 AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT DUE TO THE LANDING GEAR HANDLE WOULD NOT MOVE UP. - REMOVED AND REPLACED LANDING GEAR CONTROL UNIT IAW CESSNA 650 MM CHAPTER 32-30-01, PERFORMED GEAR RETRACTION TEST, SYSTEM OPS CHECKED GOOD. 2L72 4F A9NM 20030923001422003092300142EU 2003 9 23 EJYA566D 120030801A2612B432M FIRE DETECTOR AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL NR 1 ENGINE DIRTY C EJYAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 WP07911NW 5082 ENG FIRE WARNING LIGHT ILLUMINATED IN FLT. PILOT PERFORMED REQUIRED EMER PROCEDURES AND PERFORMED EMER LANDING. WHEN MAINT ARRIVED, FIRE WARNING LIGHT HAD EXTINGUISHED. FIRE WARNING SYSTEM WAS INSPECTED AND NO DEFECTS FOUND. MECH CLEANED ALL FIRE DETECTORS REMOVING EXTERIOR CONTAMINATIONS. AC WAS GROUND RUN WITHOUT FIRE LIGHTS ILLUMINATING AND AC WAS RETURNED TO SERVICE. 3 MINUTES INTO RETURN FLIGHT, ENG FIRE LIGHT ILLUMINATED A SECOND TIME. AGAIN FIRE WARNING LIGHT WAS EXTINGUISHED WHEN MAINT ARRIVED. AGAIN A DETAILED INSPECTION WAS PERFORMED AND NO DEFECTS FOUND. MAINT AGAIN CLEANED ALL DETECTORS AND RETURNED THE AIRCRAFT TO SERVICE. NO ADDITIONAL FIRE WARNING HAS OCCURRED ON PROCEEDING FLIGHTS. 1G72 3U3 U H11EU E4CE 20030923001472003092300147NM 2003 9 23 AWXA200300974 120030822A3150 WARNING HORN BOEING737 7373G7 1384595NM COCKPIT ACTIVATED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28303AW 24010 ON TAKEOFF AT PHX EN ROUTE FOR AUS TAKEOFF WARNING HORN SOUNDED WHEN THROTTLES WERE ADVANCED, REJECTED TAKEOFF. FLIGHT CREW RECONFIGURED TAKEOFF SETTINGS, AIRCRAFT DEPARTED WITHOUT FURTHER PROBLEMS. 2L72 4F RTA16WE 20030923001502003092300150NE 2003 9 23 AWXA200300975 220030822A7321ESL10101A1 LIMITER BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE NR 1 ENGINE INOPERATIVE A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28914AW 22208 ON TAKEOFF AT DFW EN ROUTE FOR PHX THE NR 1 ENGINE LIMITER LIGHT ILLUMINATED WITH EICAS MESSAGE LT ENGINE LIMITER DISPLAYED. NR 1 ENGINE WOULD NOT DEVELOP TAKEOFF THRUST, REJECTED TAKEOFF AND RETURNED TO BLOCK. MAINTENANCE REMOVED THE NR 1 ENGINE ELECTRONIC CONTROL (EEC) LIMITER AND INSTALLED THE EEC LIMITER FROM NR 2 ENGINE IAW AMM 73-21-02, PG. 401-404. PERFORMED ENGINE RUN AT TAKEOFF POWER, OPERATIONAL TEST OF BOTH ENGINES WAS GOOD. 2L72 4F4 FRTA2NM A12EU 20030923001512003092300151NM 2003 9 23 AWXA200300976 120030823A293310033000002 INDICATOR BOEING737 7373Y0 1384671NM ZONE 200 FALSE INDICATIONA AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP28323AW15915 23684 AT TOP OF CRUISE EN ROUTE FROM LAS TO MEX "A" SYS HYD QTY INDICATED FLUID LEVEL AT THE REFILL LINE, SOON AFTER QUANTITY FELL TO .7500 FULL AND WAS INDICATING A DECREASING TREND, DIVERTED TO PHX AS PRECAUTION. MAINTENANCE INSPECTED THE AIRCRAFT FOR FLUID LEAKAGE, NO LOSS OF FLUID WAS FOUND, RAN BOTH ENGINES WHILE CYCLING THE FLIGHT CONTROLS, NOSE WHEEL STEERING, BRAKES, AND LANDING GEAR LEVER (WITH PINS INSTALLED), NO LEAKS WERE FOUND. "A" SYSTEM HYD QTY INDICATOR WAS OBSERVED TO STICK AT CERTAIN POSITIONS, REMOVED AND REPLACED QUANTITY INDICATOR IAW BMM 29-33-11, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN, CONFIRMED FAILURE OF UNIT. FOUND THE MECHANISM ASSEMBLY STICKING AND THE POINTER BROKEN. 2L72 4F RTA16WE 20030923001542003092300154NE 2003 9 23 AWXA200300979 220030824A7314GP202MK1 PUMP BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE FUEL SYSTEM INOPERATIVE A AWXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 WP28913AW331705466 22207 ON PUSH BACK AT GATE THE NR 2 ENGINE AUTO SHUTDOWN, RT ENGINE LOW PRESSURE FUEL PUMP DISPLAYED ON EICAS. MAINT TROUBLESHOT & REPLACED NR 2 ENGINE FUEL FLOW GOVERNER IAW T/C R5M73603, OPS CHECK GOOD IAW T/C F5M73601. REPLACED NR 2 ENGINE HIGH PRESSURE FUEL PUMP IAW T/C R5M73602; OPS CHECK GOOD.VENDOR CONFIRMED FAILURE OF FFG S/N 2119684. FOUND DAMAGED VALVE (P/N 3575-068), TORN DOUBLE SEAL (P/N 1391-508), AND 2 EA. TORN PACKINGS (P/N 182650), NUMEROUS PARTS FOUND WORN BEYOND LIMITS (I.E. GOVERNOR PRELOAD ADJUSTER, FUEL VALVE, BLEED SENSOR DIAPHRAGM, AND CAM ASSEMBLY. UNIT WAS OVERHAULED IAW CMM 73-21-02, REV. 5. VENDORS FAILURE ANALYSIS OF HP FUEL PUMP S/N B271 CONFIRMED FAILURE OF THE UNIT. BEARING BLOCKS, SOLI2L72 4F4 FRTA2NM A12EU 20030923001582003092300158EU 2003 9 23 AALA20030856 120030813A21216459951 FAN FOKKERF28 F28MK0100 4990807EU ACM BAY DEFECTIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW211456D 11468 EN ROUTE DFW-DSM - DUIRNG CRUISE SMELLED STRONG ELECTRICAL SMELL, THEN SMOKE STARTED COMNG FROM AIR CONDITIONING OUTLETS. STRONG ELECTRICAL SMELL ALL THROUGH CABIN. TURNED OFF RECIRCULATION FANS, SMOKE THEN STARTED TO DISSIPATE. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT PACK RECIRCULATION FAN. PERFORMED REQUIRED INSTALLATION AND OPERATIONS TESTS. SYTEM GROUND CHECKED NORMAL OPERAITON. (M) 2L72 4F RT 20030923001672003092300167NM 2003 9 23 AALA20030824 120030731A3397 WIRE BOEING777 777223 1385213NM RROYCERB211 RB211* 54555NE EMERGENCY LIGHT SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21798AN 30797 FIRST CLASS GALLEY EMERGENCY LIGHTS INOPERATIVE. FOUND FORWARD LEFT LIGHT WIRES SHORTED. REPAIRED WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTT00001SEA12EU 20030923001682003092300168WP 2003 9 23 AALA20030687 120030623A243260030451 BATTERY DOUG DC9 DC982 3022082WP E/E COMPT DEFECTIVE A AALAD RETURN TO BLOCK MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21462AA 49592 WHEN PARKING AT GATE, SMOKE EMITTED FROM E/E COMPARTMENT. USED EXTERNAL FIRE EXTINGUISHER IN E/E COMPARTMENT. SMOKE WAS COMING FROM BATTERIES. REPLACED BOTH SHIP BATTERIES AND BATTERY CHARGER. CHECKED FOR ANY SIGNS OF WIRING DAMAGE AROUND BATTERY AREA, NONE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030923001702003092300170NM 2003 9 23 AALA20030708 120030702A3397 WIRE BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21901AN 29503 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 20-21 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE SPLICES AT ROW 19-20 AND RESET PINS IN EMERGENCY EXIT LIGHT CONNECTOR. (M) 2L72 4F RTA16WE 20030923001782003092300178WP 2003 9 23 AALA20030847 120030809A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21289AA 49301 DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS INOPERATIVE AT ROWS 11/12. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030923001832003092300183EU 2003 9 23 AALA20030849 120030808A5610PPGD20543406 WINDSHIELD FOKKERF28 F28MK0100 4990807EU COCKPIT FAILED A AALAO OTHER O OTHER CRCRUISE 1 SW211440A 11435 EN ROUTE F/O FRONT WINDOW BEGAN TO ARC FOLLOWED SEVERAL SECONDS LATER WITH OUTER PANE CRACKING IN SPIDER WEB PATTERN. AIRCRAFT LANDED ATL WITHOUT INCIDENT. REMOVED AND REPLACED F/O FRONT WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030923001902003092300190EU 2003 9 23 USAABA03030 120030815A3350Z041H0000110 DECODER AIRBUS330 A330323 3930335EU EMERGENCY LIGHT MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 DURING EMERGENCY LIGHT CHECK, RECEIVED CLASS 1 FAULTS. REPLACED RIGHT AFT DECODER/ENCODER UNIT. (M) 2L72 4F RTA46NM 20030923001922003092300192NM 2003 9 23 USAABB03139 120030818A335020131A BATTERY BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 FOUND LEFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE M736 BATTERY PACK. (M) 2L72 4F RTA1NM 20031209000102003120900010WP 2003 12 9 UPS03841475 120031025A53403755822513 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 340 LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 51-1-20D. 2L74 4F RT4A25 20031209000132003120900013 2003 12 9 YENA200330 420031017A3417PG1152BC02 ADC AIRBUS320 A320232 3930326EU NR 2 INOPERATIVE A YENAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 EA15516JB11958 1302 NO AIRSPEED INDICATION ON F/O SIDE ON TAKEOFF ROLL. RETURNED TO GATE. BITE CHECK OF ADIRU OK. PERFORMED PITOT STATIC CHECK OF ADR 2, NO AIRSPEED RESPONSE. ASSIGNED MEL FOR ADR 2 CAT III. REMOVED AND REPLACED ADR NR 2 IAW AMM 34-11-17. OPERATIONAL CHECK GOOD. CLEARED MEL. 2L72 4F RTA28NM 20031209000202003120900020WP 2003 12 9 NACA20030120 120031029A7933122803 THERMOSTAT DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 OIL TEMP MALFUNCTIONED A NACAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 AL03779TA9 9 45529 36710 NR 2 ENGINE SHUT DOWN DUE TO EXCESSIVE OIL TEMPERATURE. REPLACED NR 2 ENGINE OIL TEMPERATURE THERMOSTAT. CHECKED GOOD. 2L74 4R4 R A781 5E8 20031209000222003120900022EA 2003 12 9 COMA0370041 120031022A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA2599 10064 FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031209000372003120900037 2003 12 9 SWIA200312544 420031023A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER P NO WARNING INDICATION CRCRUISE 1 NM07226SW 120296 NR 1 STALL WARNING SYSTEM FAILS IN FLIGHT. REPLACED STALL WARNING PANEL WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 120-34428-505. 2L72 4T RTA31SO 20031209000542003120900054NM 2003 12 9 UPS03441483 120031018A5415 ATTACH FITTING BOEING747 747212B 1384886NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, NR 2 PYLON DIAGONAL BRACE STEEL ATTACH FITTING HORIZONTAL FLANGE ATTACH BOLTS 6EA TORQUE CHECK FOUND LOOSE AS MARKED. THE BOLT HOLE ID MEASURED, NR 5, 7, 9 ARE 0.314 INCH NR 8, 10 ARE 0.313 INCH & NR 15 IS 0.316 INCH NDT HFEC INSP CONFIRMED CRACK FREE PER NTM PT6, 51-00-00 FIG 17. ONLY NR 5, 7, 9 & 15 BOLT HOLES WERE REAMED TO 0.328 INCH PER SB747A2196 & OVERSIZE BOLTS OF THESE 4 BOLT HOLE WERE INSTALLED & STANDARD BOLTS FOR BOLT HOLE NR 8 & 10 WERE REFITTED PER SB747A2196R. 2L74 4F A20WE 20031209000562003120900056NM 2003 12 9 UPS03441485 120031017A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, DURING RAP INSPECTION ITEM N525UP-46-17 BS 1775-1790 AT STR 34R-36R 2EA HOLES SHORT EDGE MARGIN FOUND. BS 1775-1790 S34R-S36R PREVIOUSLY FX SKIN EXTERIOR DOUBLER REMOVED AS PER SRM 51-30-02 AND SKIN CUTOUT ENLARGED AS PER SRM 53-30-03 FIG 1. FASTENER HOLES AND SKIN CUTOUT HFEC ACCOMPLISHED AS PER NTM PART 6 51-00-00 FIG 16 AND FIG 4. NO CRACK FOUND. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 53-30-03 FIG 1. 2L74 4F A20WE 20031209000662003120900066NM 2003 12 9 SWAA032366 120031027A21216454051 FAN BOEING737 7373H4 1384600NM A/C COMPT OVERHEATED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29348SW 24375 ELECTRICAL ODOR THROUGH OUT THE CABIN. REMOVED AND REPLACED A/C RECIRC FAN PER MM. 2L72 4F RTA16WE 20031209000672003120900067 2003 12 9 SWAA032367 420031027A2565D31354 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 R1 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031209000692003120900069NM 2003 12 9 SWAA032369 120031027A55306547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING AFT SPAR CLEVIS LUGS CORRODED. REPAIRED CLEVIS LUGS PER SRM AND BFG ER. 2L72 4F RTA16WE 20031209000722003120900072NM 2003 12 9 SWAA032372 120031027A53156540804 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER STRUCTURE CORRODED AT BS 328, WL 208, RBL 50. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031209000772003120900077NM 2003 12 9 SWAA032343 120031025A3397BR2013 WIRE BOEING737 7377H4 1384404NM EMERGENCY LIGHT EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29760SW 27874 EEPLS WIRES EXPOSED THROUGH OUT CABIN FLOOR. REPOSITIONED WIRES PER MM. 2L72 4F RTA16WE 20031209000882003120900088NM 2003 12 9 SWAA032354 120031025A33506104781 BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP NEXT TO FWD GALLEY AND ENTRY DOORS. REMOVED AND REPLACED BATTERY PACK. 2L72 4F RTA16WE 20031209000992003120900099NM 2003 12 9 SWAA032319 120031021A5755 SKIN BOEING737 7372H4 138448CNM RT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 5829 22965 DURING SCHEDULED SERVICE CHECK, FOUND NR 7 FLT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER ASSY PER MM. 2L72 4F A16WE 20031209001172003120900117NM 2003 12 9 QXEA200301356 120031029A7600 CONDITION LEVER BOMBDRDHC8 DHC8401 1390041NM ZONE 400 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09407QX 4049 ON FLIGHT 2301 UNCOMMANDED NP OF 1020 WHEN 850 SELECTED. ALL OTHER ENGINE FUNCTIONS NORMALLY. RESET CONDITION LEVERS TO 1020 AND RESET AT 850 WITH NO FURTHER OCCURRENCE. NO POWER PLANT MESSAGE ON NR 2 ENGINE. REMOVED AND REPLACED FUEL CONTROL WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031209001252003120900125NM 2003 12 9 AWXA200301339 120031008A7830315A130 FAIRING BOEING737 7373G7 1384595NM THRUST REVERSER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK A 3 INCH CRACK WAS FOUND ON NR 2 ENGINE INBOARD TRANSLATING SLEEVE FAIRING. MAINTENANCE PERFORMED BOND REPAIR IAW AWA ER 03-7830-03289-TB2. 2L72 4F RTA16WE 20031209001332003120900133NM 2003 12 9 QXEA200301338 120031013A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 RIGHT HAND OUTBOARD TRACK NR 10 REQUIRES REPLACEMENT. REPLACED SEAT TRACK IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20031204001092003120400109WP 2003 12 4 UPS03841427 120030919A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, END FITTING AT STA 1766 L28R MISSING FASTENER. AFTER FURTHER INSP, CRACKED. REMOVED END FITTING AT STA 1766 L28R IAW DC8 SRM 51-1-20D. LOCATED, DRILLED, AND DEBURRED NEW PART P/N 4772397-1N PO 423837.1 IAW DC8 SRM 51-1-24. INSTALLED NEW PART (END FITTING) AT STA 1766 L28R IAW DC8 SRM 51-1-20D. END FITTING CRACKED OUT OF LIMITS IAW DC8 SRM 53-2-0 AND DAC DWG 4772397U1. 2L74 4F RT4A25 20031204001262003120400126SO 2003 12 4 C2XA03SH393 120031018A541314576094020 LONGERON EMB 145 EMB145 3260210SO NR 2 NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 DURING C-CHECK THE NR 2 LOWER ENGINE COWLING INBOARD LONGERON WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031204001322003120400132SO 2003 12 4 C2XA03SH400 120031020A532014521725013 SILL EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031204001442003120400144NE 2003 12 4 PCAA 220031018A7397 CONNECTOR DHAV DHC8 DHC8* NM PWA 120 PW120 NE NR 2 ENGINE DIRTY A PCAAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 EA13846 326 NR 2 ENGINE CONTROL MANUAL LIGHT CAME ON PROPS DROPPING TO 650 ON TAKEOFF ROLL. CLEANED ELECTRICAL CONNECTOR ON ENGINE CONTROL UNIT AND TORQUE SIGNAL CONDITION UNIT, RAN AIRCRAFT OPERATIONAL CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20031204001652003120400165CE 2003 12 4 AMWA59 120031015A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE CANTED STAB STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RIGHT SIDE NEAR THE FORWARD, CENTER AND AFT STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031204001662003120400166CE 2003 12 4 AMWA60 120031015A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT SIDE NEAR THE AFT STRINGER INTERSECTION AND TWO CRACKS ON THE LEFT SIDE AT THE FORWARD AND CENTER STRINGS INTERSECTIONS. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031204001992003120400199SO 2003 12 4 SWIA200312506 120030922A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07299SW 120329 OBS SEAT FRAME, BELOW FLOOR, AFT SIDES CRACKED AS MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME BELOW FLOOR IAW SRM 120 51-10-02 PG 2 SEC 2B. 2L72 4T RTA31SO 20031205000132003120500013SO 2003 12 5 C2XA03BT099 120031022A32347455501 LEVER EMB 145 EMB145LR 3260212SO MLG SELECTOR FAULTY A C2XAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW27299065230 5230 145472 CREW REPORTED, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM 32-32-02. OPS CHECKED GOOD. GEAR SWUNG CHECKS GOOD. AIRCRAFT TEST FLOWN AND CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20031205000422003120500042NE 2003 12 5 DL76L030932 220031017A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 BIRD INGESTION A DALAA UNSCHED LANDING CB F.O.D. SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO271201P15389 28458 727894 AT FL 2000 F/A REPORTED STRONG ODOR THROUGH OUT CABIN, LIKE ELECTRICAL BURNING ODOR. CABIN LIGHTS, GALLEY COMPONENTS AND IFE WERE ALL OFF AT THE TIME OF THE ODOR. NO C/BS TRIPPED. WITH ENGS RUNNING AND PACKS ON, POWERED UP GALLEY COMPONENTS, CABIN LIGHTING AND IFE. NO ODORS NOTED. RECIRCULATION FANS AND GASPER FAN CHECK NORMAL. DURING OVERWEIGHT INSPECTION FOUND RT ENG HAD INGESTED A BIRD INTO THE ENGINE CORE. SUSPECT ODOR CAME FROM RT ENG. 2L72 4F4 FRTA1NM E24NE 20031208000942003120800094NM 2003 12 8 QXEA200301326 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - LEFT OUTBOARD TRACK NR 2 SEAT ATTACH AREA HAS CORROSION TOP AND BOTTOM, APPROXIMATELY X487.00. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20031208001002003120800100NM 2003 12 8 QXEA200301333 120031011A5210 BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - AFT PASSENGER DOOR STOP BRACKET HAS CHAFE DAMAGE. REPAIRED IAW DHC-8-200 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20031208001062003120800106NM 2003 12 8 AWXA200301302 120031025A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 13 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRE SPLICES FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031208001602003120800160NM 2003 12 8 AWXA200301322 120031027A3350BR964411 LIGHT BOEING737 7373Y0 1384671NM SEAT ROW 21 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DEN - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030923001942003092300194EU 2003 9 23 ASOA03382 120030722A5260 NUT PLATE AEROSPATR72 ATR72 EU DOOR STAIR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING A C-CHECK IN BNA, THE PASSENGER DOOR OUTBOARD CENTER AND FORWARD NUTPLATE ON THE FIRST AND FOURTH STEPS, THE OUTBOARD CENTER AND INBOARD AFT NUT PLATE ON THE SECOND AND THIRD STEPS, AND THE OUTBOARD AFT NUT PLATE ON THE FOURTH STEP WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR OUTBOARD CENTER AND FORWARD NUT PLATE ON THE FIRST AND FOURTH STEPS, THE OUTBOARD CENTER AND INBOARD AFT NUT PLATE ON THE SECOND AND THIRD STEPS, AND THE OUTBOARD AFT NUT PLATE ON THE FOURTH STEP IAW ASA EO 72-52-0030. (M) 2H72 4T RT 20030924000062003092400006WP 2003 9 24 03FDEA01383 120030825A78309690M05G04 THRUST REVERSER DOUG DC10 DC1010 3022110WP NR 2 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 COMPLY WITH EA 8-7832-72265 EXHAUST-THRUST REV- FIXED BODY UPPER ANGLE CRACK REPAIR. EXHAUST-THRUST REV FIXED BODY UPPER ANGLE CRACK REPAIR. 2L73 4F A22WE 20030924000202003092400020NM 2003 9 24 DLM88030727 120030807A7312765404 BRACKET DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE BROKEN A DALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO27915DL 49546 726894 LOUD NOISE FROM AFT LAV / LEFT ENGINE AREA. DIVERTED. FOUND FUEL HEAT SUPPORT BRACKET BROKEN ON LEFT ENGINE. REPLACED BRACKET RAN ENGINE. ALL ENGINE INDICATIONS NORMAL 2L72 4F4 FRTA6WE E9NE 20030924000212003092400021NM 2003 9 24 DL76G030728 120030807A33500201961002 LIGHT BOEING767 767332 1382001NM AFT RT DOOR BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27169DZ 29689 DURING PDC WHILE PERFORMING AN EMERGENCY LIGHTS TEST. WE FOUND THE AFT RIGHT DOOR RED EMERGENCY LIGHT ASSEMBLY BROKEN. WE REPLACED THE LIGHT ASSY. PERFORMED THE EMERGENCY LIGHT TEST AGAIN, OPS CHECKS GOOD. 2L72 4F RTA1NM 20030924000362003092400036NM 2003 9 24 DL757030749 120030813A3350BPS73 POWER SUPPLY BOEING757 757232 1384965NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27623DL 22913 ALL F/C EMERGENCY SEAT LIGHTS AND 2L/2R DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY-OPS GOOD. 2L72 4F RTA2NM 20030924000412003092400041NM 2003 9 24 DL757030754 120030812A5412311N32711 BULKHEAD BOEING757 757232 1384965NM NACELLE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27616DL 22823 OVERSIZE HOLE REPAIR WHILE ACCOMPLISHING THE PYLON MODIFICATION REQUIRED BY AD 2000-20-09, SEVERAL HOLES IN THE NAC STA 203 BULKHEAD COMMON TO THE MIDSPAR ATTACH FITTING WERE DAMAGED. THE HOLES WERE OVERSIZED, HFEC INSPECTED, AND LARGER DIAMETER FASTENERS INSTALLED IAW ER/A 385451-14AD. 2L72 4F RTA2NM 20030924000532003092400053NM 2003 9 24 DL76L030768 120030818A3260321003061 PSEU BOEING767 767332 1382001NM E/E BAY FAILED A DALAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO27180DN 25985 AIR TURN BACK- ON CLIMBOUT GOT A FLAP CONFIGURATION WARNING LIGHT. THE LIGHT WAS ACCOMPANIED BY NUMEROUS LIGHTS. THE LIGHT CAME ON AND WENT OUT ON 3 SEPARATE OCCASIONS. REPLACED THE PSEU. 2L72 4F RTA1NM 20030924000602003092400060NM 2003 9 24 DL73G030775 120030820A5754 SKIN BOEING737 7373L9 1384470NM LT WING LE FLAP DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27231DN BN867 23717 LT WING OUTBOARD FORE FLAP DISBONDED. TE WEDGE REBUILT IAW ER/A 423088-14. 2L72 4F RTA16WE 20030922000722003092200072NM 2003 9 22 AWXA200300949 120030804A5320D5347047700800 PROFILE AIRBUSA319 A319132 3930340NM CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON LT TRANSITION PROFILE IN AFT CARGO COMPARTMENT BETWEEN FR 52 AND FR 55. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED LT TRANSITION PROFILE BETWEEN FR 52 AND FR 55; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12, & 21-22, FIG. 3 & 8. 2L72 4F RTA28NM 20030922000802003092200080NM 2003 9 22 AWXA200300957 120030806A5420D54630462203 ANGLE AIRBUSA319 A319132 3930340NM RT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK A 1/4 INCH CRACK WAS FOUND ON RT PYLON PANEL ATTACH ANGLE AT RIB 08, OUTBOARD SIDE. MAINTENANCE CUTOUT DAMAGED AREA OF ATTACH ANGLE AT RIB 08; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A319 SRM 51-42-11, PG. 6 & 7. 2L72 4F RTA28NM 20030922000952003092200095NM 2003 9 22 03FDEA01433 120030904A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAINDECK - SEAT TRACK AT STA 1701, LBL 47 FOUND WORN. MAINDECK - SEAT TRACK AREA SMOOTHEN BY HAND CLEAN AS PER SRM 51-21- 01 VOL. 2 FOUND WITH IN LIMIT AS PER SRM 53-70-00 VOL. 1. 2L73 4F RTA22WE 20030922001082003092200108EU 2003 9 22 BAQA089244 120030919A672011731822 BEARING BOLKMS117 BK117A1 5626010EU PITCH LINK ASSY WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME351 7243 PITCH LINK ASSY BEARING WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030922001122003092200112CE 2003 9 22 DXTA200300086 120030815A7603 THROTTLE CESSNA500 560CESSNA 2076750CE RT ENGINE STUCK E DXTAO OTHER S AFFECT SYSTEMS CRCRUISE 1 GL07293QS 5600293 AT ALTITUDE OF 39,000FT, THE RIGHT THROTTLE LEVER BECAME STUCK. CREW REGAINED THROTTLE LEVER MOVEMENT BELOW 6000FT. THE RAM AIR TEMP AT FL WAS -38C. FOUND RIGHT THROTTLE TO BE STIFF, ADJUSTED AND SECURED DETENT AT THE STOW DIVIDER. REMOVED AFT THROTTLE CABLE, INSPECTED FOUND NO DEFECTS, COMPLIED WITH THROTTLE CABLE LUBRICATION, REASSEMBLED AND FOUND THROTTLE MOVING SMOOTHLY AT ALL SETTINGS. PERFORMED ENGINE RUN AND FOUND OPERATIONAL CHECK OF THROTTLE SYSTEM TO BE GOOD AT THIS TIME, ALL WORK DONE IAW CESSNA 560 MM CHAPTER 76-11-04 AND 12-21-04. 2L72 4F RTA22CE 20030922001322003092200132EU 2003 9 22 AWXA200300964 120030820A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU EMERGENCY LIGHT BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28636AW 098 EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT BROKEN. MAINTENANCE FOUND BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROW 11 R/H, RE-TERMINATED BROKEN WIRES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030922001332003092200133NM 2003 9 22 AWXA200300966 120030805A5315D5347218820000 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y1162 FLOORBEAM FORWARD OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED CORRODED Y1162 FLOORBEAM FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 53-00-14, PG. 105-106, PARA 4B, & SRM 51-42-11, PG. 6 & 7. 2L72 4F RTA28NM 20031208001652003120800165NM 2003 12 8 AWXA200301327 120031001A534765538444 CARGO TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT TIE DOWN TRACK AT BS 794 TO 807, AND BS 827 TO 847, RBL 17. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CARGO COMPARTMENT TIE DOWN TRACK FROM BS 727 TO 947, RBL 17; FABRICATED A NEW REPLACEMENT SECTION OF TIE DOWN TRACK; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20031208001672003120800167NM 2003 12 8 AWXA200301329 120031001A53476545410200 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND ON FLOORBEAM AT FASTENER HOLE BS 727B, RBL 45. MAINTENANCE TRIMMED OUT CRACK ON FLOORBEAM BS 727B, RBL 45; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR STRAPS; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-03289-TB6. 2L72 4F RTA16WE 20031209000142003120900014 2003 12 9 YENA200331 420031020A3417PG1152BC02 ADC AIRBUS320 A320232 3930326EU NR 2 INOPERATIVE A YENAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 EA15533JB7030 1652 ON TAKEOFF ROLL AT 115 KTS CAPTS AIRSPEED, F/O AIRSPEEDS READ 60 KTS, ABORTED TAKEOFF. F/O PITOT PROBES INSPECTED, NO EVIDENCE OF OBSTRUCTION NOTED. ADIRU 2, OPS CHECK PERFORMED PER MM 34-13-00 AS PRECAUTIONARY, F/O ADR TRANSFERRED TO MEL 34-10-01 CAT III DOWNGRADED, REMOVED FROM RVSM. REMOVED AND REPLACED ADR NR 2 PER 34-11-17 AND PERFORMED ADR TEST PER 34-13-00, MEL REMOVED. 2L72 4F RTA28NM 20031209000802003120900080NM 2003 12 9 SWAA032346 120031024A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 15L CRACKED AT BS 509. REPAIRED STR PER SRM. 2L72 4F RTA16WE 20031209000982003120900098 2003 12 9 SWAA032318 420031021A256563550101 SLIDE BOEING737 7377H4 1384404NM L1 DOOR LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29725SW 27857 L1 DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031209001012003120900101NM 2003 12 9 SWAA032321 120031021A3350 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 1/4D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULBS PER MM. 2L72 4F RTA16WE 20031209001532003120900153NM 2003 12 9 QXEA200301370 120031022A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 RT OUTBOARD NR 10 SEAT TRACK ATTACH AREA HAS CORROSION ON BOTTOM OF STATION X342.00. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20031209001812003120900181NM 2003 12 9 AT0300034 120031102A323039576395001 BUNGEE CYLINDER BOEING717 717200 1383700NM NLG MALFUNCTIONED A ZZDAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15989AT 55152 NOSE LANDING GEAR WOULD NOT RETRACT. FOUND NOSE STRUT LOW ON SERVICE. REMOVED AND REPLACED NOSE GEAR BUNGEE CYLINDER AND SERVICED NOSE STRUT. PERFORMED GEAR SWING AND ALL CHECKED GOOD. 2L72 4F TRA6WE 20031209001832003120900183NM 2003 12 9 UPS03441501 120031010A541165B9041247 FRAME BOEING747 747200 1384847NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, NR 3 PYLON NACELLE REAR ENGINE MOUNT BULKHEAD FRAME CRACK IS FOUND AT FWD AND REAR O/B SIDE. FOUR EACH MOUNTING FRAME REPAIRED AS PER RS R54-53-35086 AT NR 3 PYLON NACELLE REAR ENGINE MOUNT BULKHEAD AND UPS ENGINEERING FILE 747-54-20042. 2L74 4F RTA20WE 20031209001872003120900187NM 2003 12 9 UPS03441513 120031015A541265B90412 BULKHEAD BOEING747 747212B 1384886NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT WEB (NAC 221 TO 221). NR 3 PYLON REAR ENG MOUNT BULKHEAD LWR ASSY FRAME WEB INTERIM REPAIR ACCOMPLISHED AS PER RS R54-53-35090 & UPS AUTH 747-54-20043. 2L74 4F A20WE 20031209001982003120900198NM 2003 12 9 QXEA200301383 120031101A243023088002B GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09367PH7876 483 511 YVR- ON FLIGHT 2233 ON CLIMBOUT OF SEA NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY CHECKLIST. UNABLE TO RESET NR 1 DC GENERATOR. REMOVED AND REPLACED NR 1 ENGINE STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031209002212003120900221NM 2003 12 9 CALA0300617 120031101A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 INSPECTION FOUND RIGHT O/B FLOOR RAIL CORRODED AT BS 827. A FLOOR RAIL REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20031209002232003120900223NM 2003 12 9 CALA0300619 120031103A521069584321 ROLLER BOEING737 737724 13844BYNM R-1 DOOR WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2724715 28786 INSPECTION FOUND THE R-1 DOOR HOLD OPEN MECHANISM INOPERATIVE, THE ROLLER WAS FOUND WORN. THE R-1 DOOR HOLD OPEN ASSEMBLY WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20031209002242003120900224NM 2003 12 9 CALA0300620 120031020A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 MAINTENANCE DISCOVERED AN EXISTING REPAIR TO THE INNER SKIN OF THE FORWARD CARGO DOOR AT A LIGHTENING HOLE LOCATION. THE EXISTING REPAIR WAS NOT INSTALLED PER CURRENT FAA REQUIREMENTS. PREVIOUS ECRA 5232-01031 REPAIRED A LARGER AMOUNT OF DAMAGE TO THE SAME AREA AS THE CURRENT DAMAGE USING A DOUBLER INSTALLATION. A REPAIR DOUBLER WAS INSTALLED AS A PERMANENT REPAIR TO THE INNER SKIN IAW ECRA 5232-01036. 2L72 4F RTA16WE 20031209002312003120900231EU 2003 12 9 MALA030482 120031028A3097 WIRE SAAB SF340 340B 7860101EU INTAKE HEAT DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15429XJ 340B429 DURING FLIGHT 3165, LT INTAKE HEAT CYCLING ON AND OFF EVERY 15 SECONDS. AIR RETURN TO DTW. MAINTENANCE REPAIRED WIRING TO LT EXHAUST NOZZLE ALL CHECKS GOOD. 2L72 4T RTA52EU 20031209002342003120900234EU 2003 12 9 MALA030487 120031101A2150 ODOR BAC 146 AVRO146RJ85A1500097EU COCKPIT DETECTED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15529XJ E2363 DURING FLIGHT 3420, CREW REPORTED FUMES IN COCKPIT. A STRONG BURNED OIL ODOR COMING FROM CABIN AIR SYSTEM. COULD NOT ISOLATE TO ONE PACK OR ENGINE AIR COMMON TO ALL. AIR RETURN TO YQR. MAINTENANCE DETERMINED FOUL ODOR TO BE COMING FROM STATION GROUND CARD IT RAN ALL NIGHT FILLING ENTIRE A/C AND SYSTEMS. PERFORMED TWO PACK BURNS AND SANITIZED AIR. ODOR CHECK GOOD. 2H74 4F RTA49EU 20031204000022003120400002WP 2003 12 4 GTIA030890 120030928A5320 WEB DOUG DC9 DC982 3022082WP AFT STAIRS BUCKLED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND AFT STAIRS RIGHT SIDE WEB BUCKLED. REMVOED TRIMMED OUT DAMAGED SECTION OF WEB. LOCATED AND DRILLED DOUBLER/FILLER. INSTALLED REPAIR DOUBELR/FILLER. (M) 2L72 4F A6WE 20031204000122003120400012 2003 12 4 GTIA030878 420031031A25652024063 CLIP DOUG DC9 DC981 3022081WP GIRT BAR BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 DTW - FLT 461 - R1 DOOR SLIDE COVER RIGHT GIRT BAR CLIP BROKEN. REMOVED BROKEN CLIP. INSTALLED NEW CLIP ASSY. (M) 2L72 4F A6WE 20031204000192003120400019WP 2003 12 4 GTIA030873 120031019A5320 WEB DOUG DC9 DC982 3022082WP CABIN SUBFLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND PAX CABIN SUBFLOOR CORRODED AT RBL 40 TO 54 STATION 180 TO 200. REMOVED DAMAGED WEB. FABRICATED NEW WEB. FABRICATED NEW SPLICE. INSTALLED NEW WEB AND SPLICE. (M) 2L72 4F A6WE 20031204000352003120400035NM 2003 12 4 AMTA200301237 120030928A3150 WARNING LIGHT BOEING757 75723N 1384973NM COCKPIT ILLUMINATED A AMTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL11528AT 30887 RETURNED TO GATE DUE TO LOWER EICAS STATUS MESSAGE LEFT ENGINE OH LP 2. TROUBLESHOT PER FIM 26-11-00, NO FAULTS NOTED AT THIS TIME. ALL INDICATINOS NORMAL T THIS TIME. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20031204000402003120400040WP 2003 12 4 AALA20031082 120030928A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW213515 49892 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT GALLEY LOCATION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204000512003120400051WP 2003 12 4 AALA20031078 120030927A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT 9D. REPLACED BATTERY PACK. SYSTM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204000522003120400052WP 2003 12 4 AALA20031077 120030926A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21491AA 49684 SAT - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE SEAT ROW 22B CEILING LIGHT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204000612003120400061WP 2003 12 4 AALA20031012 120030916A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21594AA 53284 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROW 31. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031204000622003120400062WP 2003 12 4 AALA20031011 120030916A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21567AM 53293 DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 8 THROUGH 11. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031204000782003120400078NM 2003 12 4 HNAA0300054 120031012A528085420006001 DOOR DHAV DHC8 DHC8102 2809003NM MLG DAMAGED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07937HA392295741 148 WHEN LANDING GEAR WAS RETRACTED THE LEFT MAIN GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR AND LIGHT WENT OUT. AIRCRAFT RETURNED TO FIELD. FOUND THE BOLT FOR THE LT FWD MAIN GEAR DOOR PUSH ROD TO DOOR ATTACH POINT WORN INTO AND JAMMED AGAINST THE ADJACENT NACELLE FRAME. REPLACED THE FRAME AND THE LEFT FWD MAIN GEAR DOOR. 2H72 4T RTA13NM 20031204000922003120400092WP 2003 12 4 UPS03841403 120030909A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE MISREPAIRED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, L1 DOOR CORNER UPPER FWD CORNER IS NOT PER SRM. FABBED -15 -17 DOUBLERS, -19 FILLER IAW DC8 SRM 53-2-0 FIG 15 TR 53- 155. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS & FILLER IAW DC8 SRM 51-1-20D. RE-INSTALLED FOM PARTS IAW DC8 SRM 51-1-21, 51-1 -21A, 51-1-20D, 51-3-0. 2L74 4F RT4A25 20031203001292003120300129WP 2003 12 3 AMTA200301281 120031002A5312 BULKHEAD LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 BULKHEAD, REF 5310-1482 ADDITIONAL CRACK FOUND IN LENGTH IN BULKHEAD WEB FS 1989, 8 O'CLOCK POISTION. REPAIRED BULKHEAD WEB AT FS 1989, 8 O'CLOCK POSITION AS PER ERA L10-53R-5324. (M) 2L73 4F A23WE 20031203001632003120300163WP 2003 12 3 AALA20031018 120030917A3350AA3255A CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21498AA 49736 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT EXIT SIGN LOCATION. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001862003120300186WP 2003 12 3 GTIA030893 120031028A3350BR9661106 LIGHT DOUG DC9 DC982 3022082WP RT OVERWING INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND RT OVERWING EXIT LIGHT INOPERATIVE. LT OVERWING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT OVERWING EXIT LIGHT. REMOVED AND REPLACED RIGHT OVERWING EXIT LIGHT. (M) 2L72 4F A6WE 20031204000042003120400004WP 2003 12 4 AALA20031079 120030926A3350P4010051111 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21465A 49595 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE AFT HALF OF THE CABIN. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030923000212003092300021WP 2003 9 23 DHL2003604594 120030527A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING OB L\E SHOWS CORROSION AT STA. XW.761.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED CORROSION ON LT OUTER WING OB. L\E IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA IAW EODHL-030547, ED-3313. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) A FILLER (7075-T6 AL0.050) IAW EODHL-030547, ED-3313. CLEANED, TREATED AND PRIMED DOUBLER INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER AND FILLER ON LT. OUTER WING OTBD. L\E (STA. XW.761.000) USING NEW FASTENERS. 2L74 4F RT4A25 20030923000252003092300025WP 2003 9 23 DHL2003604541 120030430A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING OUTBD. L/E FORMER 0.250 CRACKED AT STA. XFS.797.000. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG.9-10, SRM 51-1-20D PG.9, SRM 51-1-21 PG.1 2L74 4F RT4A25 20030923000492003092300049WP 2003 9 23 DHL2003604655 120030510A5753 PLATE DOUG DC8 DC873F 302199FWP RT TE FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OTBD FLAP LOWER PLATING HAS SEVERAL DENTS BETWEEN, STA. XF 415.000 AND XW 408.000. PERFORMED MAJOR REPAIR IAW EODHL 030512, ED-3382. REMOVED FASTENERS IAW SRM 51-1-21 PAGE1, SRM 51-1-21A PAGE4. REMVOED DAMAGED SKIN PANEL IAW EODHL 030512, ED-3382. CLEANED TREATED & PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL (2024 T3 AL 0.050") IAW EO DHL 030512, ED-3382. CLEANED REATED AND PRIMED NEW SKIN PANEL IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW SKIN PANEL ON RT OTBD FLAP LWR PLATING, STA XF 415.000 TO XW 408.000 USING NEW FASTENERS IAW EODHL-030512, ED-3382, SRM 51-1-21 PAGE 1 AND SRM 51-1-21A PAGE 3 2L74 4F RT4A25 20030923000512003092300051WP 2003 9 23 DHL2003604747 120030714A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FUSELAGE NOSE SECTION EXTERNAL SKIN CORRODED & DENTED BETWEEN STA 35.000 AND STA 70.000, L-31L TO L-31R. REMOVED FASTENERS & EXISTING EXTERNAL DOUBLER. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED SKIN PANEL SEGMENT. PERFORMED EDDY CURRENT INSPECTION. FABRICATED NEW SKIN PANEL SEGMENT 7075-T6 AL0.050 AND 2 EXTERNAL DOUBLERS 7075-T6 AL0.190, 7075-T6 AL0.063 & 1 FINGER DOUBLER 7075-T6 AL0.032 AND 11 INTERNAL DOUBLER 7075-T6 AL0.050. CLEANED, TREATED, PRIMED AREA, NEW SKIN PANEL SEGMENT, INTERNAL/EXTERNAL DOUBLERS & FINGER DOUBLER. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FINGER DOUBLER, INTERNAL DOUBLERS, NEW SKIN PANEL SEGMENT, EXTERNAL DOUBLERS WITH NEW FASTENERS. 2L74 4F RT4A25 20030923000782003092300078WP 2003 9 23 DHL2003604685 120030531A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP PAX DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 INTERIM REPAIR ON FWD UPPER CORNER OF FWD PASSENGER DOOR JAMB. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 15 SHEET 4, TR 53-129, DWG 5750776, DWG SR08530021. CUT OUT DAMAGED AREA AND FABRICATED FILLER (7075-T6 AL0.050) AND (2) DOUBLERS (7075-T6 AL0.063) (7075-T6 AL0.080) IAW SRM 53-2-0 FIG 15, SHEET 4, TR 53-129, DWG 5750776 DWG SR08530021. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-0 FIG 15 SHEET 4, TR 53-129, DWG 5750776, DWG SR08530021, SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000882003092300088WP 2003 9 23 DHL2003604605 120030509A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR L/E UPPER SKIN SHOWS INTERIM REPAIR & CORROSION BETWEEN STA XFS 360.250 AND XFS 379.000. REMOVED FASTENERS AND INTERIM REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.071) AND A FILLER (7075-T6 AL0.063) IAW EODHL-030503, ED-3284. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLER WITH NEW FASTENERS ON LT WING CTR L/E UPPER SURFACE IAW EODHL-030503, ED-3284, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030923001062003092300106WP 2003 9 23 DHL2003604767 120030612A5350 SKIN DOUG DC8 DC873F 302199FWP TAIL CONE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 TAIL CONE EXTERNAL SKIN SHOWS INTERIM REPAIR AND SEVERAL CORROSION SPOTS BETWEEN STA.1916.000 AND STA.1951.000. PERFORMED MAJOR REPAIR IAW EODHL-030565, ED-3394. REMOVED FASTENERS AND INTERIM REPAIRS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030565, ED3394. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGMENT (2024-T3 AL0.032), TWO DOUBLER SPLICES (2024-T3 AL0.040. CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT AND DOUBLER SPLICES. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED NEW SKIN SEGMENT AND DOUBLER SPLICES ON TAIL CONE EXTERNAL SKIN (BETWEEN STA.1916.000 - 1951.000) USING NEW FASTENERS. 2L74 4F RT4A25 20030923001122003092300112WP 2003 9 23 DHL2003604730 120030609A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP CARGO DOOR WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 CARGO DOOR JAMB SHOWS WEAR OUT OF LIMITS AT STA.1440.000 L-29R - L30R. PERFORMED MAJOR REPAIR IAW EODHL-03557, ED-3317. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. BLENDED OUT DAMAGED AREA IAW EODHL-03557, ED-3317. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED DOUBLER (7075-T6 AL0.080) IAW EODHL-030557, ED-3317. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER WITH NEW FASTENERS IAW EODHL-030557, ED-3317, SRM 51-1-20D PG.9, SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030923001552003092300155WP 2003 9 23 AALA20030860 120030816A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21218AA 49168 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT ROW 18-21 INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030924000282003092400028NM 2003 9 24 DL764030736 120030809A2751 TRANSMITTER BOEING767 767432ER 1385134NM TE FLAP OUT OF ADJUST A DALAO OTHER N FALSE WARNING LDLANDING 1 SO27834MH 29707 IRREG/ TE FLAPS DISAGREE AFTER SELECTING 20. FOUND M475 M492 M490 M489 FLAP POS TRANSMITTERS OUT OF ADJ. ADJ SAME OPS CK NORMAL IAW MM. 2L72 4F RTA1NM 20030924000502003092400050NM 2003 9 24 DLM88030764 120030818A53135910228527 STRINGER DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27904DL 49535 SPLICE REPAIRS SEVERAL STRINGERS WERE FOUND WITH ELONGATED OR OVERSIZE HOLES AT THE INTERFACE WITH FS 1446 DUE TO LOCAL FRAME REPAIRS. THE DAMAGED SECTIONS OF STRINGERS WERE CUTOUT AND NEW SECTIONS WERE SPLICED. THE STRINGER SPLICES WERE MADE IN THE SAME FRAME BAY BETWEEN CANTED FS 1431 AND 1446. THE REPAIRS WERE ACCOMPLISHED IAW SRM AND IAW ER/A 385473-14. 2L72 4F RTA6WE 20030924000562003092400056NM 2003 9 24 DL73S030771 120030816A531265465682 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27322DL 23094 WEB CORROSION REPAIR INSPECTION OF THE FS 1016 BULKHEAD WEB REVEALED CORROSION AT THE BL 0 STIFFENER NEAR THE BOTTOM OF BULKHEAD AT WL 190-200. AN OIL CAN CONDITION WAS DISCOVERED JUST OUTBOARD OF THE CORROSION AREA. BOTH DAMAGES WERE REMOVED WITH A WEB CUTOUT AND REPAIRED WITH ALUMINUM REPAIR DOUBLERS IAW BAC S/B 737-53A1075 AND IAW ER/A 385542-14AD, REV A. 2L72 4F RTA16WE 20030924000812003092400081EA 2003 9 24 QXEA200301020 120030825A2420 GENERATOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TRIPPED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09607QX 10024 ON FLIGHT 2481 GENERATOR 2 OFF CAUTION MESSAGE ILLUMINATED ON APPROACH DURING FLAP MOVEMENT FROM 20 DEGREES TO 30 DEGREES. AFTER LANDING SUCCESSFULLY RESET GENERATOR IAW EMERGENCY CHECKLIST. INTEROGATED MDC AND FOUND (GCU2) FAILED. COMPLIED WITH FIM TASK 24-21-01-810-801-A01. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030924000892003092400089NM 2003 9 24 AWXA200300981 120030825A3150 WARNING HORN BOEING737 7373G7 1384595NM COCKPIT ACTIVATED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28303AW 24010 ON TAKEOFF ROLL AT PHX EN ROUTE FOR OAK TAKEOFF WARNING CONGIURATION HORN SOUNDED, REJECTED TAKEOFF AT 55 KTS. AFTER CLEARING THE RUNWAY CHECKED SETTINGS, ALL WERE NORMAL, CYCLED FLAPS AND RAN UP TO POWER, NO HORN. SUBSEQUENT TAKEOFF WAS NORMAL. A FOLLOW UP WAS WRITTEN TO PERFORM A TAKEOFF WARNING SYSTEM TEST, WHEN AIRCRAFT ARRIVED BACK IN PHX TAKEOFF WARNING SYSTEM TEST WAS C/W IAW T/C A1B31009, TEST PASSED WITH NO DEFECTS NOTED. 2L72 4F RTA16WE 20030924000902003092400090EU 2003 9 24 AWXA200300982 120030819A5414D546305220020 PANEL AIRBUS320 A320231 3930325EU NR 1 NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-03 CHECK 2 EACH 1/4 INCHES CRACKS WERE FOUND ON NR 1 ENGINE PYLON PANEL (413DL) ON INBOARD SIDE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 54-52-12, PG. 221-225, AND SRM 51-42-11, PG. 8-10, & 12. 2L72 4F RTA28NM 20030924000962003092400096NM 2003 9 24 AWXA200300988 120030813A5343654581945 GUSSET BOEING737 737277 1384570NM MLG MOUNT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 2 INCH CRACK WAS FOUND IN RADIUS OF NOSE LANDING GEAR ACTUATOR MOUNT FITTING ATTACH ANGLE. MAINTENANCE REMOVED AND REPLACED DAMAGED NOSE LANDING GEAR ACTUATOR MOUNT FITTING ATTACH ANGLE IAW B737-200 SRM 51-30-02, PG. 1, FIG. 007, & SRM 51-30-05, PG. 1, FIG. 004. 2L72 4F RTA16WE 20030924001032003092400103NM 2003 9 24 03FDEA01283 120030807A5753ARC0502205 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING O/B FLAP I/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES FOUND CORROSION. LT WING O/B FLAP I/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES REPAIRED AS PER FEDEX EA 1-5740-63185. 2L73 4F RTA22WE 20030924001042003092400104NM 2003 9 24 03FDEA01282 120030807A5753ARC0503503 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING O/B FLAP O/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES FOUND CORROSION. LT WING O/B FLAP O/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES REPAIRED AS PER FEDEX EA 1-5740-63182. 2L73 4F RTA22WE 20030924001122003092400112CE 2003 9 24 226050303 120030503A5532 SKIN BOEING75 A75N1 1380134CE VERTICAL STAB CRACKED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07308 753063 3 INCH CRACK FOUND ON LT SIDE OF VERTICAL STAB. CRACK LOCATED APPROXIMATELY 1 INCH FROM UPPER AFT CORNER OF VERTICAL STAB GOING FORWARD. 1Q71 3R A743 20030924001192003092400119WP 2003 9 24 BSY2003F00021 220030729A7261307194911 PUMP LEAR 35 35A 5170602CE GARRTTTFE731TFE7312 01518WP RT ENGINE INOPERATIVE E BSYAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL0731WR 313 P74230 RT ENGINE ON STEEP DECENT, HAD OIL PRESSURE LIGHTS COME ON AND GAUGE DROPPED TO 10 PSI. SHUT DOWN ENGINE AND LANDED. RESTARTED ENGINE AFTER THEY WERE ON GROUND. OPS NORMAL. HAD DIRECT READING OIL PRESSURE GAUGE ON AND ADJUST TO THE TOP END LIMIT. 2L72 4F4 F A10CE E6WE 20030924001232003092400123NE 2003 9 24 AALA20030711 220030704A7200 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE LEFT LEAKING A AALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW21631AA 24589 31051 EN ROUTE LIM-DFW AT CRUISE, SMOKE DEVELOPED IN THE AIRCRAFT. RECEIVED EICAS LOW OIL PRESSURE FOR LT ENGINE. OIL QUANTITY DECREASED RAPIDLY. EMERGENCY DECLARED AND RETURNED TO LIM WITHOUT FURTHER INCIDENT. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA2NM E12EU 20030924001272003092400127EU 2003 9 24 AALA20030457 120030413A3260DSB11021 PROXIMITY SWITCH AIRBUS300 A300B4605R 3930308EU LT MLG MALFUNCTIONED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2177080 626 LEFT MLG DID NOT RETRACT WITH 3 ATTEMPTS. RETURNED SJU AND LANDED WITHOUT INCIDENT. REPLACED LEFT MLG PROXIMITY BOX. BITE TEST AND RECALL SHOWS NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030924001292003092400129 2003 9 24 AALA20030753 420030702A2565 SPRING BOEING757 757231 1384950NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21711ZX 28481 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWELVE GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWELVE GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000012003092500001NM 2003 9 25 USAA030166 120030819A5415310U20331 FITTING BOEING767 7672B7 1385107NM NACELLE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655US10418 25257 FOUND PITTING ON LOWER BEARING BORE .5 INCH BY .5 INCH. MACHINED BEARING BORE PER 71-21-14, MAJOR REPAIR PER 925-90. (M) 2L72 4F RTA1NM 20030925000022003092500002NM 2003 9 25 USAABB03128 120030731A2420727792E IDG BOEING757 757225 1384959NM LEFT FAILED A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19605AU39204 22201 ENROUTE BWI-PIT, WITH TEH APU GENERATOR ON MEL, THE CREW RECEIVED THE EICAS MESSAGE 'L GEN DRIVE' AND THE ASSOCICATED LIGHT. CREW COULD NOT RESET THE IDG. FLIGHT CONTINUED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE IDG. THE APU GENERATOR WORKED SATISFACTORILY AFTER REPLACEMENT OF THE APU BATTERY. (M) 2L72 4F RTA2NM 20030925000042003092500004NM 2003 9 25 USAABB03133 120030813A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19633AU 27811 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030925000062003092500006NM 2003 9 25 USAABB03138 120030817A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT WEAK A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4 AND 13 WEAK. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030925000112003092500011EU 2003 9 25 AALA20030785 120030722A28222052C23 PUMP AIRBUS300 A300B4605R 3930308EU RT WING INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2114061 471 AIRCRAFT DIVERTED TO MIA DUE TO RT WING FUEL DISTRIBUTION PROBLEM. REMOVED AND REPLACED RT CENTER PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030925000192003092500019 2003 9 25 AALA20030759 420030711A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21632AA 24590 TUL - FOUND DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000262003092500026EU 2003 9 25 SIMA200324403 120030831A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY SIGN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21392AE 340B392 THE EMERGENCY EXIT SIGN ON WALL ADJACENT TO SEAT 8A IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 23LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030925000272003092500027EU 2003 9 25 SIMA200323901 120030824A3397 WIRE SAAB SF340 340B 7860101EU EMERGENCY LIGHT BROKEN A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21247AE 340B247 CREW REPORTED THE MAIN CABIN EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPAIRED WIRE ON SOCKET FOR EMERGNECY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030925000302003092500030NM 2003 9 25 USAA030152 120030727A5320657376221 SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US 23557 PHL - FOUND UPPER SUPPORT CORRODED TOP AND BOTTOM, .004 INCH TOP AND BOTTOM TOTAL OF .008 INCH. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20030925000352003092500035NM 2003 9 25 USAA030167 120030819A57536546434301MC1R SKIN BOEING737 737401 1384701NM TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US 23984 FOUND C-CHECK DELAMINATED AFT FLAP TOP SKIN 4 INCHES BY 6 INCHES, INBOARD END TOP SURFACE. INTERIM REPAIR PER T/R 57-53-01A. (M) 2L72 4F RTA16WE 20030925000392003092500039NM 2003 9 25 USAA030168 120030827A5320 ANGLE BOEING737 737301 1384611NM BULKHEAD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US 23237 FOUND L-ANGLE WITH CORROSION 2 INCHES BY 2 INCHES, STATION 727 FORWARD BULKHEAD AFT FACE IN AFT CARGO, UNDER POTTING COMPOUND. FABRICATED AND INSTALLED NEW STRINGER END FITTINGS AND STRAP PER EA 76684, SRM 53-00-01. (M) 2L72 4F RTA16WE 20030925000452003092500045 2003 9 25 AALA20030769 420030710A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21175AN 32394 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS NEEDING REPLACED. REPLACED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000462003092500046 2003 9 25 AALA20030770 420030707A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21611AM 24487 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS NEEDING REPLACED. REPLACED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030923000282003092300028WP 2003 9 23 DHL2003604539 120030505A5730 DOUBLER DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING IB L/E LWR DOUBLER CRACKED 2.000, XFS.597.500. REMOVED DAMAGED DOUBLER IAW SRM 51-1-21 PG.1. FABRICATED NEW DOUBLER (7075-T6 AL 0.080) IAW SRM 57-1-0 PG.1, SRM 57-3-3 PG.16. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030923000302003092300030WP 2003 9 23 DHL2003604558 120030516A5511 FRAME DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT. HORIZONTAL STABILIZER L/E INNER FRAME CRACKED 0.500 AT XFS. 47.500. (INNER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. STOP DRILLED CRACK AT XFS.47.500 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 55-2-0 PG.7,8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D PG.9, SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030923000422003092300042WP 2003 9 23 DHL2003604750 120030222A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR. L/E VANE SLOT HOLES ELONGATED AT XOLDI 6.224 PERFORMED MAJOR REPAIR IAW EODHL-030544, ED-3301. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. TRIMMED OUT ELONGATED HOLES SKIN AREA IAW EODHL-030544, ED-3301. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR EXTERNAL DOUBLER, FILLER AND INTERNAL DOUBLER IAW EODHL-030544, ED-3301. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE, FILLER AND INTERNAL DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED INTERNAL DOUBLER AND FILLER AND REPAIR EXTERNAL DOUBLER ON LT. WING CTR. L/E VANE SLOT WITH NEW FASTENERS. 2L74 4F RT4A25 20030923000462003092300046WP 2003 9 23 DHL2003604755 120030527A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING EXTENDED L/E INBD. VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA. XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030563, ED-3312. REMOVED FASTENERS AND EXISTING DOUBLER IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED AREA IAW EODHL-030563, ED-3312. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (7075-T6 AL0.071) AND FILLER (7075-T6 AL0.063) AND INTERNAL DOUBLER (7075-T6 AL0.050). CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF REPAIR DOUBLER, INTERNAL DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED REPAIR DOUBLER, INTERNAL DOUBLER AND FILLER WITH NEW FASTENERS. 2L74 4F RT4A25 20030923000752003092300075WP 2003 9 23 DHL2003604765 120030613A53405646955504 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT FRAME FITTING CRACKED 4.500 AT STA 960.000 BETWEEN L-18L AND L-22L. PERFORMED MAJOR IAW SRM 53-1-0 PG 1, ATM PO201390, DWG 5646955. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW FITTING IAW DWG 5646955. PERFORMED LIQUID PENETRANT INSPECTION TO NEW FITTING IAW DC8 NDT SPM PART 08-00-02/06. CLEANED, TREATED AND PRIMED NEW FITTING IAW SRM 51-1-8B. INSTALLED FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030923000942003092300094WP 2003 9 23 DHL2003604694 120030527A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT FITTING CRACKED 2.000, STA. 1177.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, SRM 51-1-20D PG.9, 21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG.9. 2L74 4F RT4A25 20030923001142003092300114WP 2003 9 23 DHL2003604647 120030520A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT HORIZONTAL STAB. LE EXTERNAL SKIN SHOWS CORROSION ON SEVERAL SPOTS AT STA. XFS.178.750. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION ON LT HORIZ. STAB. L/E EXTERNAL SKIN IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 55-2-1 FIG.3. TRIMMED OUT DAMAGED AREA . PERFORMED EDDY CURRENT INSP IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER, TRIPLER AND A FILLER. CLEANED, TREATED AND PRIMED DOUBLER AND TRIPLER INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLER, TRIPLER AND FILLER ON LT. HORIZ. STAB. LE EXTERNAL SKIN (STA. XFS.178.750) USING NEW FASTENERS. 2L74 4F RT4A25 20030923001202003092300120WP 2003 9 23 DHL2003604674 120030624A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT ELEVATOR LOWER PART EXTERNAL SKIN SHOWS DEFLECTION AND CORROSION FROM STA. XAR.0.000 TO XE.132.000. PERFORMED MAJOR REPAIR IAW EODHL-030521, ED-3405. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG.1, SRM 51-1-21A PG.4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL (2024-T3 AL0.032) IAW EODHL-030521, ED-3405. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN PANEL WITH NEW FASTENERS IAW EODHL-030521, ED-3405, SRM 51-1-21 PG.1, SRM 51-1-21A PG.4, FOR WEIGHT AND BALANCE SEE N/R 4037. FOR REMOVAL AND REINSTALLATION SEE J.C 8-27-60-016. 2L74 4F RT4A25 20030923001792003092300179 2003 9 23 AALA20030848 420030810A23301301273109 VIDEO DISPLAY BOEING777 777223 1385213NM ENTERTAIN SYS OVERHEATED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21795AN 30257 EN ROUTE VIDEO SCREENS AT RG/F WENT BLANK FOLLOWED BY SMOKE AND FUMES FROM 4G. MASTER POWER TURNED OFF AND SMOKE/FUMES DISSIPATED. AIRCRAFT LANDED LGW WITHOUT INCIDENT. MAINTENANCE DISCOVERED AVU OVERHEATED. REPLACED AVU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030924000082003092400008EU 2003 9 24 197012403 120030124A2750952D1007 PDU PILATSPC12 PC1245 7090551EU TE FLAPS FAILED E S4WAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP07613NA3625 197 FLAPS STUCK AT 0 DEGREES. 1L71 3T RTA78EU 20030924000302003092400030NM 2003 9 24 DLM90030743 120030807A3397 WIRE DOUG MD90 MD9030 3023690NM EMERGENCY LIGHT DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27911DA 53391 EMERGENCY CABIN LIGHT L2-746 WOULD NOT ILLUMINATE - FOUND A OPEN WIRE AT L2474A16N ALSO FOUND POWER SUPPLY B5-227 WITH A SUSPECTED BLOWN INTERNAL FUSE - REPAIRED WIRE AND REPLACED POWER SUPPLY / OPERATION NOW NORMAL. 2L72 4F RTA6WE 20031204000742003120400074NM 2003 12 4 QXEA200301274 120031014A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 CRACK ON TOP RIGHT HAND SIDE OF FIRE WALL. REPAIRED IAW DHC-8 RD 8-54-806. 2H72 4T RTA13NM 20031204000902003120400090WP 2003 12 4 UPS03841401 120030908A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT PIT AT STA 1040 STR 34R FRAME HAS CORROSION UNDER NUT PLATE. REMOVED CORR IAW DC8 SRM 51-1-8 ORIG .080 INCH, REMOVED .070 INCH, REMAINING .010 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB RPR ANGLE AND 2 FILLERS IAW UPS EO DC8-5310-11728. REMOVED DAMAGED AREA IAW UPS EO DC8-5310-11728. ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED RPR ANGLE AND FILLERS IAW DC 8 SRM 51-1-20D AND UPS EO DC8-5310-11728. 2L74 4F RT4A25 20031204001072003120400107WP 2003 12 4 UPS03841425 120030918A534752772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, MAIN CABIN CENTER LINE SEAT TRACK FS 1338 TO 1357 HAS CORROSION. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. INSTALLED CENTER SEAT TRACK & 8 SPLICES AND 1 SPLICE FITTING STA 1270-1350 IAW DC8 SRM 51-3-0. FLOOR BOARD AT STA 1270 1350 LT WAS REMOVED FOR FOM, REINSTALL FLOOR BOARD IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20031204001242003120400124NM 2003 12 4 AWXA200301265 120031007A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM AROUND NUT PLATES AT BS 727D+5, RBL 3. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT DAMAGED SECTION OF FLOORBEAM BS 727D+5, RBL 3; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 FIG 201. 2L72 4F RTA16WE 20031204001302003120400130SO 2003 12 4 C2XA03SH398 120031019A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031204001372003120400137NM 2003 12 4 C1HA203385010 120031018A3350 BATTERY BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 AFT OUTSIDE LEFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED M955 PWR SUPPLY AND BATTERY OPS CHECKED GOOD PER M/M 33-50-22. 2L73 4F A3WE 20031204001642003120400164NM 2003 12 4 QXEA200301292 120031016A3260 BULB DHAV DHC8 DHC8202 2809007NM MLG INDICATOR BURNED OUT A QXEAO OTHER L NO TEST APAPPROACH 1 NM09374PH 528 ON FLIGHT 2140 DURING APPROACH RIGHT MAIN GEAR GREEN DOWN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. GEAR CONFIRMED DOWN THROUGH ALTERNATE EXTENSION LIGHTS. RIGHT MAIN GEAR DOWN LIGHT WILL NOT TEST. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND MAIN LANDING GEAR DOWN INDICATION BULBS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031204001712003120400171CE 2003 12 4 AMWA65 120031010A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07218YV UE218 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT AND ONE PLACE ON THE LEFT SIDE NEAR THE CENTER STRINGER INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031204001922003120400192EA 2003 12 4 03289638 120031016A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27638BR 7311 DURING INSPECTION THE NR 2 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. 2L72 4F RTA21EA 20031204001982003120400198EA 2003 12 4 SWIA200312505 120030910A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07915SW 7615 PASSENGER DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE REMOVED AND REPLACED IAW CRJ MM 52-11-03. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031204002012003120400201EU 2003 12 4 29341 120031022A7931 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ENGINE OIL ILLUMINATED A UHLAD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL17149SZ 340A149 367470 FLIGHT 4554 FROM PIT TO FWA, AFTER TAKEOFF AT 1000 FT, AIRCREW GOT A LT OIL PRESSURE LIGHT. A/C RETURNED SAFETY BACK TO PIT. 2L72 4T4 TRTA52EU E8NE6 20031204002022003120400202NM 2003 12 4 UPS03441452 120031019A2611 CIRCUIT CARD BOEING747 747123F NM NR 1 FIRE WARN INOPERATIVE A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01677UP 20391 INSPECTION TYPE:N/A FIRE AND FAULT ON NR 1 ENGINE. B-NACELLE ILLUMINATED INTERMITTENTLY ON CLIMB AND APPROACH. CLEANED 3 RESEATED FIRE WARNING CARDS A-13 A-10. OPS TEST GOOD PER 26-10-00. 2L74 4F A20WE 20031205000052003120500005SO 2003 12 5 C2XA03CL176 120031022A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2711565 145621 CLE FLIGHT 2317 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20031205000252003120500025NM 2003 12 5 DL76K030912 120031009A335002019241005 LIGHT BOEING767 767332 1382001NM AFT LT ENTRY DR DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27175DZ 29696 FOUND AFT LT EMERGENCY WHITE FLOOD LIGHT DAMAGED. REPLACED AFT LT EMERGENCY WHITE FLOOD LIGHT. 2L72 4F RTA1NM 20031205000282003120500028NM 2003 12 5 DL73S030918 120031011A2121214001040 GASPER FAN BOEING737 737232 1384475NM CABIN FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27317DL 23089 GASPER FAN C/B POPPED IN CLIMB WITH A BURNED METAL ODOR. REPLACED FAN. 2L72 4F RTA16WE 20031209002362003120900236EA 2003 12 9 COMA0360479 120031101A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A COMAK NONE L NO TEST ININSP/MAINT 1 SO01403CA 7428 FLIGHT 5228 DURING INSPECTION FOUND MAIN CABIN DOOR EMERGENCY EXIT SIGN INOPERATIVE. CLEANED CONNECTOR. 2L72 4F RTA21EA 20031209002492003120900249NM 2003 12 9 UPS03241531 120031104A2612 FIRE DETECTOR BOEING727 72725C 138400HNM CARGO BAY MALFUNCTIONED A IPXAK NONE N FALSE WARNING ININSP/MAINT 1 SO01951UP 19850 MX LIGHT ILLUMINATED IN FLT ON LOWER CARGO COMPARTMENT FIRE DETECTION / PROTECTION SYSTEM. SYS OK LIGHT ILLUMINATED, NO MESSAGES DISPLAYED IN MX DISPLAY. PERFORMED INITIALIZATION PROCEDURE PER MM 26-18-05. OPS CHECK OK. 2L73 4F A3WE 20031209002502003120900250NM 2003 12 9 UPS03241535 120031019A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, NLG WW BS 263 AND BS 267 ROW OF RIVETS HAVE SUSPECT CRACKS ABOVE RT AFT PRESSURE PANEL. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC NDF REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1. 2L73 4F A3WE 20031208000512003120800051NM 2003 12 8 03FDEA01783 120031021A5330 SKIN BOEING727 727200 138407ENM FUSELAGE MISREPAIRED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 FUSELAGE SKIN PRE-EXISTING OPEN HOLES NEAR MAIN CARGO DOOR CUTOUT. FUSELAGE SKIN PRE-EXISTING OPEN HOLES NEAR MAIN CARGO DOOR CUTOUT. (INITIAL ACTION, PART 1 COMPLIED WITH ONLY). 2L73 4F RTA3WE 20031208000692003120800069EU 2003 12 8 AWXA200301290 120031009A5414D5453005200201 SKIN AIRBUS320 A320231 3930325EU ZONE 480 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-03 CHECK FOUND THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN PITTED. MAINTENANCE REMOVED PITTED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW SECTION OF SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8 PG 8-12. 2L72 4F RTA28NM 20031208000752003120800075SO 2003 12 8 C2XA03SH415 120031025A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714542 145547 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031208001362003120800136NM 2003 12 8 2003UALA00785 120031018A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 EXTERNAL FUSELAGE SKIN HAS 2EA GOUGES AT BOTTOM OF 3 INCH LONG BY 2 INCH HIGH DENT, AT STA 770 BETWEEN STR 15L AND 16L. 2L72 4F4 FRTA2NM E17NE 20031208001542003120800154SO 2003 12 8 C2XA03CL183 120031027A3350110049 CHARGER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714940 145033 FLIGHT 2306 THE CREW REPORTED THE EMERGENCY LIGHTING LAST 5 ROWS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AND CHARGING BASE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031208001762003120800176 2003 12 8 757BJ0001 420031028A256569B1485513 SPRING BOEING757 757236 1384971NM GIRT BAR FAILED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 R1, R2, AND L4 GIRT BAR LEAF SPRINGS FAILED INSPECTION PER BOECOM M-7200-03-00917 AND PACE AIRLINES MO NR B757-52-21003. REPLACED LEAF SPRINGS PER MM 25-66-14. 2L72 4F RTA2NM 20031209000072003120900007WP 2003 12 9 UPS03841472 120031022A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 867 TO 873 MLG WHEEL WELL PRESSURE PANEL HAS A FINGER DOUBLER CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5645332 AND SRM 51-1-20D. 2L74 4F RT4A25 20031209000112003120900011WP 2003 12 9 UPS03841476 120031025A534037540231N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 305 AT LONG 33R NR 3 T-BOLT BACKUP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754023 AND SRM 51-1-20D. 2L74 4F RT4A25 20031209000322003120900032NE 2003 12 9 MALA030478 220031025A7220 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT SURGES A MALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL15366PX 340B267 E785734 DURING FLT, SHORTLY AFTER T/O, LT ENGINE SURGED TO OVER 100 PERCENT TORQUE, THEN BACK TO 80 PERCENT. ITT FOLLOWED SAME TREND. PERFORMED ERRATIC. ENGINE QRH INFLIGHT AND LOCKED OUT TORQUE MOTOR, ENGINE AND INDICATIONS STABILIZED EXCEPT FOR TORQUE. TORQUE GAUGE CONTINUED TO BOUNCE 20 PERCENT ON TAXI IN, POWER LEVERS AT GROUND IDLE TORQUE IND WAS AT 0-20 PERCENT. AIR RETURN TO MSP. MAINTENANCE REPLACED LT ENGINE P/N CT7-9B IAW JOB CARD 7100-301 AND PROP P/N R390/4-123-F/27 IAW JOB CARD 6110-303 ENG S/N ON GE-E785734 PROP S/N ON DAP0192, ALL OPS CHECKS GOOD. CREW MUST ESTABLISH NEW BASE LINE FOR DDT. 2L72 4T4 TRTA52EU E8NE 20031209000392003120900039EA 2003 12 9 SWIA200312546 120031027A2760270007 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07597SW5742 5742 7293 ON APPROACH FLT SPOILERS FAULT STATUS MESSAGE. FLT SPOILERS OPERATE NORMALLY. REMOVED AND REPLACED LT FLIGHT SPOILER INBOARD ACTUATOR PER RJ MM 27-62-01. NO LEAKS NOTED. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031209000782003120900078 2003 12 9 SWAA032344 420031024A2565 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSTIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20031209000872003120900087NM 2003 12 9 SWAA032353 120031025A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, BETWEEN STR 28L AND STR 28R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031209001542003120900154NM 2003 12 9 QXEA200301372 120031026A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 REPLACE NR 11 SEAT TRACK DUE TO CORROSION DAMAGE. REPAIRED IAW DHC-8 RD 8-51-103. 2H72 4T RTA13NM 20031209001632003120900163NM 2003 12 9 03FDEA01776 120031009A5753ARC41251 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LEFT O/B FLAP FWD UP STOP FITTING FOUND CRACKED. LEFT O/B FLAP FWD UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20031209001742003120900174WP 2003 12 9 ABXA030414 120031015A531159135955 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 FRAME CRACKED AT FS 1076 AND LONGERON 19 LEFT. REPAIRED FRAME AT FS 1076 IAW DC-9 SRM 53-03. 2L72 4F A6WE 20031209001762003120900176WP 2003 12 9 ABXA030408 120031014A553199118315 RIB DOUG DC9 DC932 3022066WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB TOWARD THE TOP END OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20031209001792003120900179NE 2003 12 9 HEEA090474 220030930A732332448851 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 1 ENGINE FAILED B HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW03412SM1937 33197 CPPSTH0281 DURING CRUISE FLIGHT NR 1 ENGINE ITT WENT TO 970 DEGREES AND NR 2 ENGINE TORQUE WENT TO ZERO. PLACED NR 1 ENGINE GOVERNOR IN MANUAL AND LANDED AT NEAREST AIRPORT. REPLACED THE NR 1 ENGINE AND AFCU DUE TO HIGH SIDE GOVERNOR FAILURE. REPLACED THE NR 1 ENGINE DUE TO OVERTEMP. ALSO REPLACED FUEL CONTROL P/N 3244883-7, S/N C43612, TT 1937.10. 1G72 4U4 U H4SW E22EA 20031209001852003120900185NM 2003 12 9 UPS03441511 120031017A531265B1028110 BULKHEAD BOEING747 747212B 1384886NM LT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, LT MLG WW BS 1241 BULKHEAD CORRODED AT WL 143 BETWEEN LBL 1 & 3 AREA AS MARKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.059 X 1 X 1 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO RS R57-12-35092 & UPS AUTH 747-57-20049. CIC APPLIED IAW EO M5100 -2780-E. 2L74 4F A20WE 20031209001932003120900193WP 2003 12 9 UPS03841494 120031022A5510SE085500093 FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 TEE FITTING CRACKED AT LT HORIZONTAL STAB FRONT SPAR INBOARD LOWER CORNER NEAR XFS 60. REMOVED AND REPLACED FITTING IAW DWG SE08550009 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20031209002012003120900201 2003 12 9 SWIA200312551 420031022A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07936SW241 241 7726 STALL FAIL CAUTION MESSAGE ILLUMINATED INFLIGHT. REPLACED STALL PROTECTION COMPUTER. OPS CHECK GOOD. 2L72 4F RTA21EA 20031209002272003120900227NM 2003 12 9 03FDEA01715 120031007A5754ARB2850506 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT WING - SLAT TRACK NR 16 I/B FITTING FOUND CRACKED. RIGHT WING - SLAT TRACK NR 16 I/B FITTING REMOVED AND REPLACED AS PER DRAWING ARB 7565 AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20031209002442003120900244NM 2003 12 9 UPS03241518 120031011A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, CABIN AIR PRESS LEAK FROM NR 1 VHF ANTENNA CUTOUT (AFT). ON INVESTIGATION A SUSPECT CRACK FOUND AT ANTENNA CUTOUT. HFEC INSPECTION CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM PT 6 51-00-00 FIG 4. CRACKEDCONFIRMED & MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3. SSID FORM SL V BL 8-10 HAS BEEN SUBMITTED. 2L73 4F A3WE 20031209002682003120900268NM 2003 12 9 AWXA200301368 120031020A52106545871515 FRAME BOEING737 737277 1384570NM PAX DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK A .3125 INCH CRACK WAS FOUND ON AFT SIDE OF R-1 DOOR INBOARD OF THE 3RD AFT STOP FITTING FROM THE BOTTOM BS 327, STR 14 RT. MAINTENANCE CUT OUT DAMAGE ON AFT SIDE OF R-1 DOOR 3RD AFT STOP FITTING FROM THE BOTTOM BS 327, STR 14 RT; FABRICATED A FILLER & DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-30-02 FIG 13 PG 1. 2L72 4F RTA16WE 20031209002742003120900274EA 2003 12 9 COMA0360484 120031105A2840 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA FUEL INDICATOR CONTAMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01709CA 7238 FLIGHT 5484 DURING CLIMBOUT OF MCO RECEIVED A FUEL IMBALANCE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. CLEANED MOISTURE FROM CONNECTOR J425/P425. 2L72 4F RTA21EA 20031210000012003121000001NM 2003 12 10 SWAA032609 120031126A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND 3 EA FUSELAGE SHEAR TIES CORRODED AT BS 747, LBL 7 TO LBL 14, WL 146. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20031210000072003121000007NM 2003 12 10 03FDEA02079 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) FWD FACE FLANGE FOUND WITH 01 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY. 2L73 4F RTA22WE 20031210000112003121000011NM 2003 12 10 SWAA032610 120031126A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND STR 15L CORRODED AT BS 500B. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20031210000132003121000013NE 2003 12 10 SWAA032612 220031124A7261CFM56 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 3 LEAKING A SWAAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SW29647SW 27717 858561 SMOKE SMELL IN THE CABIN. SUSPECTED NR 2 ENG, NR 3 BEARING OIL SEAL FAILURE. REMOVED AND REPLACED NR 2 ENG PER MT. 2L72 4F4 FRTA16WE E2GL 20031210000442003121000044NM 2003 12 10 AWXA200301500 120031113A57206569646102 PANEL BOEING737 7373G7 1384595NM RT WING CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MINOR REPAIR - DURING C-15 CHECK FOUND THE RT WING OUTBOARD FLAP WELL BOX PANEL CHAFED AT RS 275.03. MAINTENANCE REMOVED THE RT WING OUTBOARD FLAP WELL BOX PANEL AT RS 275.03; FABRICATED A NEW REPLACEMENT PANEL; INSTALLED REPAIR PART IAW AWA ER 03-5752-03317-DL1. 2L72 4F RTA16WE 20031210000462003121000046WP 2003 12 10 AALA20031297 120031119A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21232AA 49179 LAX FORWARD LEFT HAND OVERWING INTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD LEFT HAND OVERWING INTERIOR EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210000592003121000059NM 2003 12 10 QXEA200301517 120031203A5720 ANGLE DHAV DHC8 DHC8202 2809007NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX - CRACKED Z-ANGLE RIGHT HAND WING FORWARD SPAR AT TOP FROM FIRST RIVET TO TOP EDGE OF STATION YW45-00. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20031210000612003121000061SO 2003 12 10 C2XA03SH474 120031123A532014522459003 ANGLE EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV- DURING C-CHECK THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031210000642003121000064WP 2003 12 10 AALA20031299 120031119A3350P401005111 MODULE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21241AA 49254 DFW AFT RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED AFT RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY AND MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210000712003121000071NM 2003 12 10 03FDEA01968 120031121A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 2 O/B CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031210000792003121000079NM 2003 12 10 AALA20031302 120031118A2750 FLAP BOEING737 737823 13844BZNM WING JAMMED A AALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW21926AN 29527 YYZ T1586/18 EN ROUTE LAX-YYZ FLAP HANDLE SET TO 5 DEGREES, LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED AND FLAPS STOPPED AT 1 DEGREE WHILE LEADING EDGE DEVICES INDICATED NORMAL EXTENSION. TRAILING EDGE FLAP DISAGREE CHECKLIST ACCOMPLISHED. ACCOMPLISHED TRAILING EDGE FLAPS UP LANDING AT YYZ WITHOUT INCIDENT. BITE TEST FLAP/SLAT ELECTRIC UNIT AND NO FAULT FOUND. CYCLED SYSTEM TWICE ALL INDICATIONS NORMAL. NO DEFECT OR DAMAGE FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20031210000862003121000086NM 2003 12 10 SWAA032619 120031127A261233007507 FIRE LOOP BOEING737 7373H4 1384600NM APU FAULTY A SWAAK NONE N FALSE WARNING UKUNKNOWN 1 SW29606SW 27926 DECLARED EMERGENCY, APU FIRE WARNING INDICATION WITH APU NOT RUNNING. FOUND APU TAIL PIPE DETECTOR LOOP SHORTED TO GROUND. REMOVED AND REPLACED APU TAIL PIPE FIRE LOOP AND APU FIRE LOOP PER MM. 2L72 4F RTA16WE 20031210000882003121000088NM 2003 12 10 SWAA032621 120031130A335030131A BATTERY PACK BOEING737 7373H4 1384600NM CABIN FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29358SW 26595 AFT EMERGENCY EXIT LIGHT ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED BOTH AFT EMERGENCY LIGHT BATTERY PACKS PER MM. 2L72 4F RTA16WE 20031209000742003120900074NE 2003 12 9 SWAA032340 220031023A7210717000 GEARBOX BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE LEAKING A SWAAE ENGINE SHUTDOWN KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW29105SW 23249 707371 IN FLT SHUT DOWN, DECLARED EMERGENCY NR 1 ENG OIL PRESS IND BELOW LIMITS AND OIL TEMP IND INCREASE. REMOVED AND REPLACED NR 1 ENG GEAR BOX PER MM. 2L72 4F4 F A16WE E2EA 20031209001082003120900108NM 2003 12 9 SWAA032337 120031023A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 2419 27937 DURING SCHEDULED C1 CHECK, FOUND RT WING AFT INBD TE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20031209001372003120900137NM 2003 12 9 QXEA200301346 120031008A5551 ATTACH FITTING DHAV DHC8 DHC8202 2809007NM ZONE 300 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 HORIZONTAL STAB LEFT HAND FORWARD ATTACH FITTING HAS SCRATCH MARKS AND SMALL DRILL START ON OUTBOARD FACE OF LUG. REPAIRED IAW RD 8-55-847. 2H72 4T RTA13NM 20031209002262003120900226NM 2003 12 9 CALA0300622 120031020A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 MAINTENANCE DISCOVERED AN EXISTING REPAIR TO THE INNER SKIN OF THE FORWARD CARGO DOOR AT A LIGHTENING HOLE LOCATION THAT WAS NOT INSTALLED PER CURRENT FAA REQUIREMENTS. A PERMANENT REPAIR TO THE INNER SKIN WAS INSTALLED IAW ECRA 5232-01038. 2L72 4F RTA16WE 20031209002332003120900233NM 2003 12 9 QXEA200301385 120031102A7712311835404 SIGNAL COND UNIT DHAV DHC8 DHC8202 2809007NM ZONE 400 MALFUNCTIONED A QXEAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 NM09369PH8216 8216 513 ON TAKEOFF NOTICED POWER UPTRIM LIGHT ILLUMINATED. ALL OTHER INDICATIONS NORMAL. NR 2 POWER LEVER 1 INCH SPLIT BEHIND NR 1 POWER LEVER. SELECTING AUTOFEATHER OFF NR 2 LOSS OF -10 PERCENT TORQUE. REMOVED AND REPLACED TSCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031209002372003120900237EA 2003 12 9 COMA0360480 120031101A2400820465 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA ADG FAULTY A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01806CA9560 7359 FLT 5103 THE AIR DRIVE GENERATOR DEPLOYED DURING CLIMBOUT OF DCA. CREW DECLARED AN EMERGENCY AND DIVERTED TO ROA. REPLACED THE ADG AUTO DEPLOYMENT CONTROL PANEL. 2L72 4F RTA21EA 20031209002702003120900270NM 2003 12 9 AWXA200301370 120031022A531565498851 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 967, RBL 10 TO RBL 48. MAINTENANCE REMOVED UPPER T-CAP REPAIR AT BS 967, RBL 10 TO RBL 48; FABRICATED A NEW REPLACEMENT T-CAP; INSTALLED REPAIR PART IAW B737-200 SRM 53-10-9 FIG 2 PG 7-11. 2L72 4F RTA16WE 20031210000212003121000021NM 2003 12 10 03FDEA02090 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 BETWEEN UPPER SECTION OF BANJO FITTINGS NR 1 & 2 ATTACHED HORIZONTAL WEB FOUND WITH 02EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPP SECTION OF BANJO FITTINGS NR 1 & 2 ATTACHED HORIZONTAL WEBS 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL2 & REPLACED AS PER SRM 51-33-01 VOL2. 2L73 4F RTA22WE 20031210000302003121000030NM 2003 12 10 MWEA030461 120031203A53205930544143 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 J-CHANNEL BETWEEN SEAT TRACK NR 2 AND NR 3 AT STATION 256 HAS CORROSION AROUND FASTENER HOLE. FABRICATED AND INSTALLED NEW J-CHANNEL. 2L72 4F RTA6WE 20031210000412003121000041WP 2003 12 10 03FDEA01974 120031121A5753ARC0154 HINGE FITTING DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 NR S 16 COMPLY WITH EA 8-5740-73852. WINGS INBD FLAP OUTBD HINGE SUPPORT FITTING TO WING ATTACH HOLES REWORK P/N ARC0154. COMPLIED WITH EA8-5740-73852. 2L73 4F A22WE 20031210000892003121000089EA 2003 12 10 COMA0360513 120031127A2752852D10011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01443CA8913 7539 FLIGHT 5768 DURING DESCENT TO ERI RECEIVED A FLAP FAIL CAUTION MESSAGE AT TWO DEGREES FLAP POSITION. REPLACED THE RIGHT NR 2 INBOARD FLAP ACTUATOR. 2L72 4F RTA21EA 20031210001032003121000103NM 2003 12 10 03FDEA01993 120031128A5712 RIB DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING LEADING EDGE SLAT TRACK NR 16 INBOARD SUPPORT RIB WITH A CRACK. DAMAGED SUPPORT RIB REMOVED AS PER SRM 51-31-01, VOL 2 & NEW RIB INSTALLED AS PER SRM 51-31-01 VOL 2 & DWG ARB 2873. 2L73 4F RTA22WE 20031210001082003121000108NM 2003 12 10 03FDEA01998 120031128A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 AFT PRESSURE BULKHEAD LOWER EXTRUDED LONGERON RIGHT SIDE FOUND CRACKED. REMOVED CRACKED LONGERON AS PER SRM 51-31-01 VOL 2 & FABRICATED NEW LONGERON AS PER DRAWING AJC7001. INSTALLED NEW LONGERON AT FX - AFT PRESSURE BULKHEAD LOWER EXTRUDED RT SIDE AS PER SRM 51-35-01 VOL2 & SRM 51-33-01 VOL2. 2L73 4F RTA22WE 20031210001102003121000110NM 2003 12 10 AWXA200301503 120031129A33501012621 LIGHT BOEING737 7373G7 1384595NM CABIN SHORTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28309AW 24711 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY EXIT SIGN JUST FWD OF R-1 DOOR AT WAIST LEVEL WAS INOPERATIVE. MAINTENANCE FOUND LIGHT ASSEMBLY SHORTED OUT. REMOVED AND REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031210001212003121000121NM 2003 12 10 03FDEA01964 120031121A5730 PANEL DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT WING UPPER SURFACE O/B OF FUEL TANK PANEL 533 AT FOUND CORROSION. LT WING UPPER SURFACE O/B OF FUEL TANK PANEL 533 AT CORROSION REPAIRED AS PER FEDEX EA 1-5710-74260. 2L73 4F RTA22WE 20031210001282003121000128NM 2003 12 10 AALA20031331 120031125A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21759AN 32638 DFW FIRST CLASS SEATS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS SEATS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTT00001SE 20031210001302003121000130NM 2003 12 10 AALA20031333 120031127A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21662AA 25296 MIA RIGHT AFT DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AFT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20031210001322003121000132NM 2003 12 10 AALA20031335 120031127A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21662AA 25296 MIA EMERGENCY LIGHTS AT ROW SEAT 25B TO 34D DIM. REPLACED AFT CABIN BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20031210001332003121000133NE 2003 12 10 AALA20031285 220031115A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 MALFUNCTIONED A AALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21228AA 49178 718435 IAD T646/14 EN ROUTE MIA-YYZ AIRCRAFT LOST OIL PRESSURE AND QUANTITY IN NUMBER ONE ENGINE. LANDED AT IAD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F4 F A6WE E9NE 20031210001432003121000143WP 2003 12 10 AALA20031353 120031126A2934ST12AE TRANSMITTER DOUG DC9 DC982 3022082WP HYD SYSTEM FAULTY A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW2170529 49921 ORD T650/26 EN ROUTE PHX-ORD RT HYDRAULIC PRESSURE LIGHT AND RT REV ACCUMULATOR LIGHT ON WHEN EXTENDING FLAPS AND SLATS. LANDED ORD WITHOUT INCIDENT. INSPECTION FOUND RT AND LEFT HYDRAULIC LEVELS WITHIN LIMITS. REPLACED RIGHT HAND FLUID QUANTITY TRANSMITTER AND INDICATING SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031205000332003120500033NM 2003 12 5 DL73S030923 120031010A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307DL 23079 A 2 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BELOW STRINGER 19R AT FS 765. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087498-14. 2L72 4F RTA16WE 20031205000372003120500037NM 2003 12 5 DL73S030927 120031014A55146547528505 WEB BOEING737 737247 138448DNM HORIZONTAL STAB WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27377DL 23604 FOUND ON R1 LETTER CK,OUTBOARD BALANCE BAY I/B WEB CHAFED THRU AT LT HORIZ STAB. REPAIRED PER SRM 51-40-20 FIG 11. 2L72 4F A16WE 20031205000412003120500041NM 2003 12 5 DLM90030931 120031016A2170V1211 COALESCER BAG DOUG MD90 MD9030 3023690NM RIGHT UNSERVICEABLE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27911DA 53391 AFTER T/O FLT ATTENDANT A/C LEFT MX HANGER. FUMES WERE NOT GETTING STRONGER BUT WERE MORE NOTICEABLE NEAR FLOOR. CONTINUED THROUGHOUT FLIGHT. ADVISED BY MAINT NOT TO START APU ON GROUND. REPLACED RT COALESCER BAG FOR T/S. PERFORMED PNEUMATIC HIGH PRESSURE BURNOUT PER MM. 2L72 4F RTA6WE 20031205000472003120500047 2003 12 5 DLM11030937 420031019A3100RDAV2906 POWER SUPPLY DOUG MD11 MD11 3023602NM COCKPIT BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27807DE 48478 IN FLIGHT SMOKE FROM POSER SUPPLY/ MONITOR ASSY POWER SUPPLY HAS A DISTINCT ODOR OF SMOKE. REPLACED ASSY. 2L73 4F RTA22WE 20031205000482003120500048NM 2003 12 5 DL777030939 120031019A253072077500 OVEN BOEING777 777232 1385232NM GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27864DA 29736 NR 2 OVEN MID GALLEY HAD ELECTRICAL ODOR. FWD TO MCO IAW MEL 25-20-01H. 2L72 4F RTT00001SE 20031205000492003120500049NM 2003 12 5 DL757030940 120031019A5330146N351111 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27617DL 22907 FUSELAGE SKIN WAS FOUND DENTED AND GOUGED BETWEEN FS 1380 & 1400 AND BETWEEN STRINGERS 28L & 28R. THE DAMAGE WAS REMOVED WITH A 18.75 X 12.25 INCHES CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385729-14, REV A. 2L72 4F RTA2NM 20031205000512003120500051 2003 12 5 DL764030943 420031021A23301301273110 AUDIO VIDEO UNIT BOEING767 767432ER 1385134NM SEATS 35 CDE ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27838MH 29711 STRONG ODOR REPORTED VICINITY AT SEAT 36B AS PREVIOUSLY REPORTED. F/A REPORTS ELECTRICAL ODOR IN ADJACENT AREA. BOTH RECIRC FANS AND ENTERTAINMENT SYSTEM TURNED OFF. ODOR DISSIPATED WITH RECIRCS OFF. LONG HISTORY OF PROBLEM. INSPECT CABIN OVERHEAD AT SEAT 35-36 ABC. NO ODOR NOTED. RAN ENTERTAINMENT SYSTEM TURNED RECIRC FANS/GASPER FAN AND ALL LIGHTS FOR 1 HR. NO ODOR NOTED. AFTER OPERATING ENTERTAINMENT SYSTEM FOR 4 HRS FOUND THE AVU AT SEAT 35 CDE VERY HOT AND THE COOLING FANS INOP INSIDE THE AVUS. REMOVED AND REPLACED AVUS. 2L72 4F RTA1NM 20031204000232003120400023 2003 12 4 GTIA030868 420031027A2565 GIRT BAR DOUG DC9 DC983 3022083WP ESCAPE SLIDE DETACHED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 ORD - FOUND L1 GIRT BAR DEATTACHED. RESECURED L-1 GIRT BAR, OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20031204000292003120400029WP 2003 12 4 AMTA200301274 120030825A5740 ATTACH FITTING LKHEED1011 10113851 5265010WP AILERON ACTUATORBROKEN A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 LT OUTBOARD AILERON OUTBOARD ACTUATOR WING SIDE ATTACH POINT ANTI-ROTATION TAB BROKEN. REPLACED AILERON ACTUATOR ATTACH FITTING IAW SRM 51-10-01 AND SRM 51-40-01. (M) 2L73 4F A23WE 20031204000862003120400086WP 2003 12 4 UPS03841396 120031001A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, L2 AFT PAX DOOR UPPER AFT CORNER HAS CRACK INDICATION. REMOVED CRACKED INTERNAL STEEL DOUBLER, MATERIAL ID FOR NEW DBLR IS 17-7 DH .025 INCH LOT 360348 IAW DAC DWG 5750985 AND 4751734, HEAT TREATED TO HT170 IAW DAC DWG 4751734, PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 51-1-21. 2L74 4F RT4A25 20031204001152003120400115WP 2003 12 4 UPS03841433 120030925A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, L2 AFT PASSENGER UPPER AFT DOOR JAMB CORNER EXT FUSELAGE SKIN CRACKED AT 2 FASTENERS CRACKS MARKED. REPAIRED IAW DC8 SRM 53-2-0; REMOVED FASTENERS, TRIMMED OUT CRACKS IAW DC 8 SRM 53-2-0, PERFOMRED E/C INSP IAW DAC NDT SPM 06-10-01.001. NO CRACKS NOTED. FABBED RPR PARTS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PARTS IAW DC8 SRM 53-2-0. 2L74 4F RT4A25 20031204001522003120400152NM 2003 12 4 03FDEA01759 120031016A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25493FE 21531 CORROSION ON STRINGER 28 LT, BS 950E 3, OUTBOARD SIDE OF STRINGER. 2L73 4F RTA3WE 20031205000022003120500002 2003 12 5 03287307 420031014A2210 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ILLUMINATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27307UE 41021 DURING CLIMB THE CREW RECEIVED A FLIGHT CONTROL DISCONNECT MESSAGE. CREW RETURNED TO DEPARTURE FIELD AND LANDED UNEVENTFULLY. 2L72 4T RTA41NM 20031205000662003120500066SO 2003 12 5 GLBA2003150 120031117A2150310848401A VALVE EMB 120 EMB120ER 3260203SO LT PACK FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03293UX 120293 LT PACK FAILED ON CLIMBOUT SMOKE IN COCKPIT, R&R LT ENG P2.5 VALVE ASSY PN 310848401A OPS CK GOOD 2L72 4T RTA31SO 20031208000022003120800002NM 2003 12 8 2003UALA00779 120031015A5754 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 4 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 NR 4 SLAT DELAMINATED AT OB END LOWER SURFACE OF T/E WEDGE. AREA 2.2 INCH CHORDWISE X 3.0 INCH SPANWISE LOCATED 1.5 INCH FROM OB END AND 3.0 INCH FROM T/E. THE ABOVE NOTED DELAM CONDITION WAS DUE TO WEAR FROM NORMAL LOADS EXPERIENCED DURING A FLIGHT OVER A PERIOD OF TIME. THE TRAILING EDGE WEDGE OF THE SLAT WAS REPAIRED USING AN ADHESIVE INJECTION METHOD. 2L72 4F4 FRTT0001SE E46NE 20031210001492003121000149WP 2003 12 10 AALA20031365 120031201A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21411AA 49322 STL FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001512003121000151WP 2003 12 10 AALA20031367 120031202A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21516AM 49893 DEN MID CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR MID CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001522003121000152EU 2003 12 10 AALA20031368 120031201A2782 JACKSCREW AIRBUS300 A300B4605R 3930308EU L/E SLAT INOPERATIVE A AALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW2119059 469 JFK T610/01 EN ROUTE SJU-JFK DUAL SLAT FAULT. VISUALLY CHECKED SLATS NOT EXTENDED. LANDED JFK WITHOUT INCIDENT. REPLACED NR 3 RIGHT LEADING EDGE SLAT JACKSCREW IAW MM 27-84-22-4. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA35EU 20031210001532003121000153NM 2003 12 10 AALA20031358 120031201A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21633AA 24591 MIA SEAT MOUNTED PATH LIGHT AT SEATS 13DEF INOPERATIVE. RESECURED LOOSE CONNECTOR FOR SEAT MOUNTED PATH LIGHT AT SEATS 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20031210001562003121000156WP 2003 12 10 AALA20031357 120031201A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21584AA 53247 PHX FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001572003121000157NM 2003 12 10 AALA20031315 120031123A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 MIA) FIRST CLASS LOWER AISLE WALL EMERGENCY LIGHT INOPERATIVE. REPLACED FIRST CLASS LOWER AISLE WALL EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20031210001662003121000166NM 2003 12 10 AALA20031183 120031024A275138760854 TRANSMITTER BOEING757 757223 1384957NM PWA 2037 PW2037 NE T/E FLAP DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 SW21693AA 26973 AIR INTERRUPTED INTO IAD DUE TO TRAILING EDGE FLAP DISAGREE MESSAGE WHEN FLAPS SELECTED. FLAPS STUCK AT 1 DEGREE. REPLACED LEFT FLAP TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (SW21200401056) 2L72 4F4 FRTA2NM E17NE 20031210001682003121000168NE 2003 12 10 AALA20031260 220031113A7532CON3023 TPU BOEING757 757223 1384957NM RROYCERB211 RB211* 54555NE ENGINE FAILED A AALAO OTHER O OTHER CRCRUISE 1 SW21691AA 25697 APPROX 1 HOUR AFTER DEPARTURE AT COMPLETION OF CLIMB TO FL 380, THE THROTTLES RETARD TO 1.35 EPR A POSSIBLE COMPRESSOR STALL HAPPENED AT THAT POINT AS WE HEARD A POP AND THE AIRCRAFT BOUNCED. NEITHER PILOT WAS LOOKING AT ENGINE INSTRUMENTS TO SEE ANY INDICATIONS. ENGINES RAN SMOOTHLY AND NO OTHER INDICATIONS ON INSTRUMENTS. T/S IAW FIM AND FOUND RT TPU AT FAULT, REPLACED TPU AND ACCOM ALL REG CKS IAW MM. ALL CKS NORMAL. OK FOR SERVICE. REPLACED RT TPU. (SW21200401256) 2L72 4F4 FRTA2NM A12EU 20031210001992003121000199NM 2003 12 10 03FDEA01877 120031105A53116516343 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 N00509) DENT IN FRAME BS 1050 ABOVE STR 25L ** SD ** COMING 2L73 4F RTA3WE 20031210002152003121000215WP 2003 12 10 UPS03841547 120031104A53204653726501 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 210 LONGERON 22R SPLICE IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4653726,AND SRM 51-1-20D 2L74 4F RT4A25 20031210002162003121000216WP 2003 12 10 UPS03841548 120031103A532046519081 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 230 LONGERON 18R SPLICE IS BROKEN. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4651908,AND SRM 51-1-20D 2L74 4F RT4A25 20031210002212003121000221WP 2003 12 10 UPS03841551 120031023A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED AT STATION 1766 AT RBL 26 65.5 INCHES ABOVE FLOOR LEVEL CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRO8530007 AND SRM 53-2-5 FIG 14A. 2L74 4F RT4A25 20031211000052003121100005NM 2003 12 11 DHL2003754017 120031106A3350 LIGHT BOEING727 727223 1384074NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 FORWARD ENTRY EMERGENCY LIGHT WILL NOT HOLD A CHARGE. REMOVED AND REPLACED FORWARD ENTRY EMERGENCY LIGHT, REF M/M 33-50-111 AND OPS CHECKED GOOD. 2L73 4F A3WE 20031209001452003120900145NM 2003 12 9 QXEA200301360 120031023A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 CRACK IN NR 2 ENGINE FIREWALL AT 10 O'CLOCK POSITION. REPAIRED IAW DHC-8 RD 8-54-806. 2H72 4T RTA13NM 20031209001522003120900152NM 2003 12 9 QXEA200301369 120031022A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 LT INBOARD NR 5 SEAT TRACK ATTACH AREA HAS CORROSION ON TOP OF STATION X518.00. REPAIRED IAW DHC-8 RD 8-53-1339. 2H72 4T RTA13NM 20031209002132003120900213 2003 12 9 SWIA200312563 420031029A3497 WIRE EMB 120 EMB120ER 3260203SO STICK SHAKER BROKEN A SWIAO OTHER PF NO WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07284YV 120284 F/O'S STICK SHAKER IS INOP. REPAIRED BROKEN WIRE AT SERVO SHAKER. OPS CHECK OKAY. 2L72 4T RTA31SO 20031210000202003121000020NE 2003 12 10 03FDEA02043 220031202A7200CF680C2A5F ENGINE AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE NR 2 FAILED A FDEAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 SO25652FE11653 735 705231 DURING ROTATION NR 2 ENG FAILED NO UNUSUAL ENG INDICATIONS. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD 64T0700-2, ENGINE LEAK AND OPS CHECKS OK. PERFORMED T/O ASSURANCE RUN PER JRH. 2L72 4F4 FRTA35EU E13NE 20031210000832003121000083NM 2003 12 10 SWAA032616 120031127A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5 BETWEEN STRINGERS 2 AND 3. REPAIRED RIB PER SRM AND T1-257-008. 2L72 4F RTA16WE 20031210000932003121000093 2003 12 10 MALA030503 420031119A3442 TRANSCEIVER BAC 146 AVRO146RJ85A1500097EU WEATHER RADAR MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15534XJ E2370 DURING FLIGHT 3406, WEATHER RADAR FAILED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE CND PROBLEM. CHANGED R/T AS A PRECAUTION, OP CHECKS GOOD. 2H74 4F RTA49EU 20031210000972003121000097EU 2003 12 10 MALA030517 120031120A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION PERFORMED BY TIMCO, LAKE CITY, FL. CABIN AFT CENTER SEAT TRACK CORRODED AT STA 649-686. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION IAW MESABA EO A53060. A/C RELEASE DATE 12/2/03. 2L72 4T RTA52EU 20031210001002003121000100NM 2003 12 10 AALA20031325 120031121A2750 TRANSMISSION BOEING757 757223 1384957NM T/E FLAP MALFUNCTIONED A AALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW21656AA 24614 MIA T921/21 EN ROUTE MCO-MIA TRAILING EDGE FLAP DISAGREE. FLAPS INDICATED 20 DEGREES WITH HANDLE AT 25 DEGREE POSITION. LEFT HAND OUTBOARD GEAR BOX TRANSMISSION POPPED. RESET INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031210001092003121000109NM 2003 12 10 AWXA200301502 120031128A3350900835A BATTERY BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 AUS - EEL - DURING 4-DAY CHECK THE EMERGENCY EXIT SIGN ABOVE THE L-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031210001442003121000144NE 2003 12 10 AALA20031354 220031129A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RIGHT MALFUNCTIONED A AALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW217539A 49993 ATL T1679/29 EN ROUTE ATL-MIA RIGHT HAND ENGINE LOW OIL PRESSURE. RETURNED ATL WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F4 F A6WE E9NE 20031210001712003121000171NM 2003 12 10 CALA0300599 120031008A53206953971 CHANNEL BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 CRACK ON C2 DOOR HOLD OPEN LATCH SUPPORT CHANNEL. REMOVED AND REPLACED SUPPORT CHANNEL IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20031210001762003121000176NM 2003 12 10 CALA0300676 120031127A5730 FAIRING BOEING737 737524 1384721NM RT WING DAMAGED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2762631 27535 THE RT RED GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT I/B FLAP FAIRING HANGING BY FORWARD END ATTACH HARDWARE WHICH OBSTRUCTED GEAR ON RETRACTION. IT APPARENTLY WAS DISLODGED BY DAMAGED ELEPHANT EAR AT FLAP RETRACTION. THE FAIRING WAS REPLACED IAW MM 27-51-32. A GEAR SWING WAS PERFORMED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20031210002022003121000202NM 2003 12 10 03FDEA01742 120031015A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE53392 20935 EXTERIOR SKIN 12 INCH FORWARD OF BS 1183 BETWEEN STRINGERS 22L AND 23L CORRODED AND FASTENERS CORRODED AND AREA BULGED. REPAIRED DOUBLER FOR AFT LAV SERVICE PAN AREA IAW EA 7-5330-55022. 2L73 4F RTA3WE 20031211000042003121100004EA 2003 12 11 COMA0360485 120031105A284073664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM FAULTY A COMAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SO01709CA192 7238 FLIGHT 5485 - DURING CLIMBOUT OF MCO RECEIVED A FUEL IMBALANCE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE FUEL COMPUTER. 2L72 4F RTA21EA 20031211000172003121100017WP 2003 12 11 ABXA030422 120031029A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 R1 DOOR UPPER FORWARD CORNER HAD A REPAIR THAT DID NOT CONFORM TO SERVICE REWORK DRAWING SR08530021 OR ENG SKETCH ES00863. REMOVED EXISTING DOUBLER AND TRIPLER, PERFORMED X-RAY AND ELC INSPECTION, NO CRACKS. FABRICATED DOUBLER AND TRIPLER REPAIR, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D AND REA D853-48055MR. 2L74 4F 4A25 20031211000312003121100031NM 2003 12 11 AWXA200301389 120031102A532065176856 TIE CLIP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 .5 INCH CRACK WAS FOUND IN TIE CLIP BS 344-350, STR 16 LT. MAINTENANCE REMOVED THE CRACKED TIE CLIP BS 344-350, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-17685; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 & 11 PG 1. 2L72 4F RTA16WE 20031211000392003121100039EA 2003 12 11 QXEA200301398 120031105A3610 SEAL CNDAIRCL600 CL6002C10 1390015EA BLEED AIR SYS LEAKING A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09612QX 10042 SEA-ON FLIGHT NUMBER 2508, DURING CLIMB A WARNING MESSAGE APPEARED AND DISAPPEARED TO QUICKLY TO READ. THIS WAS FOLLOWED BY A RT BLEED DUCT CAUTION MESSAGE. PACK 2 ON THE SYNOPTIC PAGE CONTINUOUSLY FLICKERED BETWEEN GREEN AND WHITE. THE SHUTOFF VALVE REMAINED CLOSED. AFTER COMPLETING THE RT BLEED DUCT AND MANUAL CHECKLISTS, RIGHT BLEED DUCT PRESSURE INDICATES 25 PSI. FOUND BLEED LEAK. INSTALLED NEW SEALS AT STUB DUCT. PERFORMED OPERATIONAL TEST OF THE BLEED AIR LEAK DETECTION. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031211000552003121100055NM 2003 12 11 QXEA200301411 120031105A5260 TRACK BOMBDRDHC8 DHC8401 1390041NM AFT AIRSTAIR LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09402QX 4032 SEA- ON FLIGHT 2345 REAR AIRSTAIR DOOR IS DIFFICULT TO DEPLOY. LUBED STAIR TRACK. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031211000592003121100059NM 2003 12 11 C1HA200394040 120031108A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 1010 - 1148 LBL 45.5 HAS HEAVY CORROSION. 2L73 4F A3WE 20031211000652003121100065NM 2003 12 11 ASM2003F00004 120031028A27826010N000104 ACTUATOR DOUG MD80 MD83 3023681NM L/E SLAT FAILED W ASMFD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS37018 49643 AIRCRAFT RETURNED TO PLATFORM DURING TAXI, WHEN SLATS WERE EXTENDED AUTO SLAT FAIL LIGHT TURNED ON. SYSTEM WAS CHECKED WITH OTHER COMPUTERS, CONFIRMING THE FAIL IN BOTH AUTO SLAT ACTUATORS. ACTUATORS WERE REPLACED IAW MM 27-80-08 TESTS CORRECT. FURTHER, THEN THE AIRCRAFT WAS DISPATCHED ART INOP LIGHT TUNED ON FAIL REPORT WAS DEFERRED IAW MEL 73-8. 2L72 4F RT 20031211000772003121100077NM 2003 12 11 AWXA200301412 120031027A5320655384420 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK 2 EACH CRACKS WERE FOUND ON AFT CARGO COMPARTMENT FLOOR CHANNEL AT BS 747 AND BS 767, RBL 13.80. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL FROM BS 727 TO BS 945, RBL 13.80; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 10. 2L72 4F RTA16WE 20031211000862003121100086NM 2003 12 11 03FDEA01895 120031109A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20935 CORROSION ON FRAME 910 LEFT BL 71 AT STR 17. REPAIRED IAW BOEING SRM 53-10-4 FIG 13 AND EA 7-5310-55092. 2L73 4F RTA3WE 20030916000982003091600098NM 2003 9 16 2003F00556 120030520A2131 CONTROLLER BOEING727 727233 138408ANM CABIN PRESSURE MALFUNCTIONED A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17395AJ 21100 CREW REPORTED, UNABLE TO PRESSURIZE AIRPLANE AFTER TAKEOFF. FLIGHT CREW RETURNED AIRCRAFT TO TJSJ AND LANDED WITHOUT FURTHER INCIDENT. A GROUND PRESSURIZATION CHECK WAS PERFORMED, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20030916001002003091600100EU 2003 9 16 ASOA03385 120030724A5320 SILL AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING A C-CHECK IN BNA, THE RIGHT AFT SILL WEB FROM FS 39-41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT SILL WEB FROM FS 39-41 IAW SRM 51-25-00. (M) 2H72 4T RT 20030916001492003091600149NE 2003 9 16 NACA20030097 220030723A7421 SPARK PLUG DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE ENGINE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL0343872315 315 44665 P34767 NR 4 ENGINE NR 2 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED FRONT AND REAR SPARK PLUGS ON NR 2 CYLINDER. 2L74 4R4 R 6A3 5E8 20030917000042003091700004WP 2003 9 17 GTIA030038 120030204A3244 DEFLECTOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE LT MLG WHEEL BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23824NK 53015 LEFT MAIN NR 1, WHEEL SPRAY DEFLECTOR BROKE OFF. REMOVED AND REPLACED LEFT MAIN NR 1 WHEEL SPRAY DELFECTOR. 2L72 4F4 FRTA6WE E2EA 20030917000392003091700039NM 2003 9 17 0301386311 120030729A3350 LIGHT BOEING747 747451 1384940NM CABIN INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01671US 26477 DURING LINE CHECK, FOUND 'C' ZONE LT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030917000782003091700078EU 2003 9 17 BAQA089093 120030902A63401179406101 CONTROL UNIT BOLKMS117 BK117A4 5626017EU RPM MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911WS7333 7068 NO AUDIBLE TONE FOR LOW ROTOR RPM. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030917001082003091700108NM 2003 9 17 AMTA200301055 120030814A3350 SIGN BOEING737 73783N 13844HINM EMERGENCY LIGHT DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11316TZ 32609 EMERGENCY EXIT INDICATOR AFT OF R4 DOOR DAMAGED. REMOVED AND REPLACED EMERGENCY INDICATOR ASSEMBLY AFT OF R4 DOOR, OPS CHECK GOOD PER AMM 33-51-01. (M) 2L72 4F RTA16WE 20030918000042003091800004NM 2003 9 18 03FDEA01501 120030911A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 N01557 STR CRACKED B/S 720B 15 STR 15L. REPAIRED IAW SRM 53-10-3 FIG 5. 2L73 4F RTA3WE 20030918000082003091800008NM 2003 9 18 03FDEA01505 120030911A5315BAC1518338 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 STA 950F LBL 97 TO 54 WL 208 FLOORBEAM HAS DAMAGE ON UPPER FLANGE. TOOLING MARKS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER SRM 51-30-5, 53- 10-1, & FED EX EA 7-5310-54997, BS 950F, LBL 35 - 65, WL 208. 2L73 4F RTA3WE 20030918001412003091800141NM 2003 9 18 PCAA0308096 120030807A33506038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAK NONE L NO TEST NRNOT REPORTED 1 EA13845EX25731 344 CREW REPORTED EMERGENCY LIGHTS ON FLOOR AT ROW 4 HAS SEVERAL LIGHT BULBS BAD. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND POWER SUPPLY 33-52-PS2 TO BE BAD IN RIGHT FORWARD OVERHEAD POSITION. RIGHT FORWARD OVERHEAD EMERGENCY LIGHT POWER SUPPLY WAS REPLACED. OPERATIONAL CHECK WAS GOOD. 2H72 4T RTA13NM 20030918001452003091800145WP 2003 9 18 03FDEA01206 120030803A7197AVN70023 HEAT SHIELD DOUG DC10 DC1030 3023501WP NR 3 ENG CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 NR 473 NR 3 ENG AFT ELECTRICAL JUNCTION BOX HEAT SHIELD IS CRACKED. REMOVED AND REPLACED HEAT SHIELD IAW SRM 51-31-01 @ MAE ON N/R N00473. 2L73 4F A22WE 20030919000082003091900008CE 2003 9 19 DXTA200300080 120030807A3610662710034 LINE CESSNA560 560XL 2076702CE PNEUMATIC SYSTEMCHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07632QS 5605132 WHILE PERFORMING NJA'S ONE TIME INSPECTION OF THE HYDRAULIC/PNEUMATIC LINES IN THE WHEEL WELLS, FOUND THE RT EMERGENCY BRAKE LINE CHAFED THROUGH, AND FLAP RETRACT LINE CHAFED BEYOND LIMITS. - REMOVED AND REPLACED DEFECTIVE HYDRAULIC AND PNEUMATIC LINES IAW CESSNA 560XL MM CH 27-51-00 AND 32-42-09, SYSTEM OPS AND LEAK CHECKED GOOD. 2L72 4F RTA22CE 20030919000382003091900038NM 2003 9 19 IU62003F00022 120030603A32304105E1 HOUSING BOEING737 737* NM VALVE CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 S17 CRACKED FROM THREADED PORT TO LEE PLUG. WEAK HOUSING. MAKE HOUSING STRONGER AND THICKER BETWEEN THE THREADED PORT AND THE LEE PLUG. (NR 177851) 2L72 4F RTA16WE 20030919000712003091900071NM 2003 9 19 QXEA200300963 120030809A2160BYLF51514 SENSOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09366PH* 3367 510 FLIGHT 2167 AIRCRAFT DIVERTED, ENROUTE NO AIRFLOW COMING OUT OF COCKPIT VENTS. FA NOTED A TRICKEL OF AIR OUT OF CABIN VENTS. CABIN PRESS WAS NORMAL TO ABOUT 10,000 FT. AFTER CABIN RATE OF CLIMB STOPPED AND PRESSURE DIFFERENTIAL CONTINUED WITH NO GAIN IN CABIN ALTITUDE. LEVELED AT 15,000 AND FA REPORTED TEMP UNBEARABLY HOT, SHORTLY AFTER REPORTED HOT SMELL AND SMOKE IN CABIN. BLEED WERE ON AND SELECTED TO MAX. CABIN DUCT TEMP GUAGE READ FULL COLD. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AIR DUCTING FROM AFT PRESSURE BULK HEAD AND FOUND COCKPIT DUCTING TO BE OFF AT 'Y' DUCT. RECONNECTED DUCTING. REMOVED AND REPLACED COCKPIT ZONE TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030919000872003091900087NM 2003 9 19 0301566302 120030813A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21-31. RECONNECTED WIRES. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030919001082003091900108 2003 9 19 3602061703 420030617A3425066304600 INDICATOR SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE HSI DEFECTIVE E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP07820NA653 3602 22342 PILOT'S HEADING/NAV INDICATOR DRIFTS. 1G71 3U3 U H9EU E00054EN 20030919001092003091900109EU 2003 9 19 AWXA200300920 120030803A5320D53470479200 PROFILE AIRBUS320 A320232 3930326EU CARGO DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LT TRANSITION PROFILE BETWEEN FR 59 AND FR 60. MAINTENANCE REMOVED LT TRANSITION PROFILE BETWEEN FR 59 AND FR 60; FABRICATED A NEW REPLACEMENT PROFILE AND A REPAIR SPLICE; INSTALLED REPAIR PART IAW AWA E.R. 26-5320-03154-SS1. 2L72 4F RTA28NM 20030915000582003091500058 2003 9 15 HEEA089005 420030729A34578143902240B GPS SKRSKYS76 S76A 8143006NE COCKPIT WILL NOT TEST B HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW031545X 760050 2 YEAR INSPECTION. INSPECTED AND FOUND UNIT WOULD NOT PASS GPS TEST. RESET MEMORY AND RETESTED. NO HELP. 1G72 3U H1NE 20030915000602003091500060GL 2003 9 15 ALGA089012 220030905A725023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE GALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO N1 COUPLING FOUND TO HAVE INTERNAL SPLINES GALLED. RETURNING PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20030915000682003091500068SW 2003 9 15 HEEA088964 120030822A243523046020 STARTER GEN BELL 212 212 1181420SW ENGINE FAILED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736D6868 31135 GENERATOR LIGHT BEGAN FLASHING AFTER LANDING. AFTER SHUTDOWN STARTER WOULD NOT MOTOR. REPLACED STARTER GENERATOR. TO BE SENT TO VENDOR FOR REPAIR. 1G71 4U H4SW 20030915000732003091500073EU 2003 9 15 BAQA088913 120030830A240045033500 MASTER BOX UROCOPEC135 EC135T1 5620026EU ELECTRICAL MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME1969 0143 GENERATOR DISCONNECT LIGHT STAYS ON. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030915000922003091500092EU 2003 9 15 ALGA089085 120030910A6510C651A2001107 DISC PACK UROCOPEC120 EC120B 8680987EU TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03510AL895 1251 DISC PACK FOUND TO HAVE CRACKED LAMINATE. REMOVED AND REPLACED. 1G72 3U NCR0001RD 20030916000052003091600005NM 2003 9 16 S03453044 120030606A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJFO OTHER O OTHER NRNOT REPORTED 1 WP03 29219 FUSELAGE SKIN IMPACT DAMAGE BETWEEN BS 2684 AND BS 2689, LBL 6. REPAIRED IAW EO 744-53-10-0018 2L74 4F4 FRTA20WE E24NE 20030916000262003091600026WP 2003 9 16 0301319862 120030716A2710 CONTROL CABLE DOUG DC9 DC951 3022051WP PWA JT8 JT8D9 52048NE AILERONS BINDING A NWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL01771NC 47769 CREW EXPERIENCED SIGNIFICANT BINDING OF THE AILERONS IMMEDIATELY AFTER TAKEOFF. AS AIRSPEED INCREASED, THE CONTROLLABILITY IMPROVED AND LESS FORCE WAS NEEDED TO MOVE THE CONTROL YOKE. FLIGHT RETURNED TO AN UNEVENTFUL LANDING BACK AT DTW. MAINTENANCE CONFIRMED BIND AT ABOUT 10 DEGREES OF RT AILERON DEFLECTION BUT DISAPPEARED AFTER MOVING THE YOKE SEVERAL TIMES. FOUND EVIDENCE OF CHAFING OR BINDING ON CABLE SECTOR ON FIRST OFFICER'S CONTROL COLUMN AND AGAINST A HYDRUALIC LINE IN THE WING. 2L72 4F4 FRTA6WE E2EA 20030916001382003091600138WP 2003 9 16 GTIA030631 120030727A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND R-1 DOOR ENTRY FLOORBOARD SUPPORT CORRODED AND WORN. FABRICATED R-1 DOOR ENTRY FLOOR BOARD SUPPORT. (M) 2L72 4F RTA6WE 20031208000072003120800007NM 2003 12 8 MWEA030472 120031203A5330591024287 DOUBLER DOUG MD88 MD88 3023688NM ACCESS PANEL CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 AFT MATING SURFACE FOR THE WRAP AROUND ACCESS PANEL AT THE BASE OF THE VERTICAL STABILIZER LEADING EDGE IS CHAFED AND CRACKED. FABRICATED AND INSTALLED WRAP AROUND DOUBLER. 2L72 4F RTA6WE 20031208000102003120800010WP 2003 12 8 IXXA0300076S 120031117A5753 FITTING DOUG DC8 DC871F 302199DWP FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX814301292 45993 DURING A ROUTINE "B" CHECK INSPECTION, MAINTENANCE FOUND LT FLAP SUPPORT FITTING CRACKED AT STATION 219. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED L/H FLAP OUTBOARD SECTION PER ALL APPLICABLE MANUALS. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20031208000112003120800011WP 2003 12 8 03FDEA01948 120031118A3234 SELECTOR VALVE DOUG DC10 DC1010 3022110WP MLG FAILED A FDEAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 SO25386FE 46620 AT 180 KTS ON FINAL DROPPED LANDING GEAR AND GOT UNSAFE ON BOTH PRI-SEC. CYCLED GEAR WITH SAME RESULT. INITIATED GO-AROUND. AT 210 KTS ON VECTORS CYCLED GEAR AND GOT 3 GREEN. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE PER AMM 32-31-03-2 OPS CHECK NORMAL PER AMM 32-30-00-5. LEAK CHECKED NORMAL. 2L73 4F A22WE 20031208000152003120800015EA 2003 12 8 SWIA200312513 120031021A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 621.00, LBL 42, FLOOR SUPPORT ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV ''A'', RII 53-401. P/N: 601R-53-61-117-3 2L72 4F RTA21EA 20031208000212003120800021NM 2003 12 8 03FDEA01963 120031121A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT OUTBOARD FLAP FOUND VANE TO TRACK ATTACHMENT NR 4 WITH SLOT CORRODED AS MARKED. RT OUTBD FLAP VANE TO TRACK ATTACHMENT NR 4 CORROSION REPAIRED AS PER FEDEX EA 1-5750-74256, WING RT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20031208000402003120800040NM 2003 12 8 UPS03441462 120031009A5320141U109250 CLIP BOEING747 747200 1384847NM NWW BS 320 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, RT SIDE BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB NR 4 ATTACH CLIP ONE FA FASTENER HOLE CRACK FOUND AT O/B CHORD AREA, WL 140 TO 160. DEFECT CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20031208000442003120800044NM 2003 12 8 VNAA0310012 120031019A261251653151 CONTROL UNIT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE APU FIRE DETECT FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07426JS3099 3038 THE CREW REPORTED RECEIVING A APU FIRE LOOP FAIL AND A FALSE FIRE INDICATION. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTION CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031208000462003120800046 2003 12 8 VNAA0310009 420031013A3400 COMPUTER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION AND A LEFT HAND PROP OVERSPEED CAS INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CYCLED THE INTEGRATED AVIONICS COMPUTER CIRCUIT BREAKERS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031208000482003120800048NM 2003 12 8 VNAA0310007 120031008A5210 BOLT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07434JS 3051 DURING CLIMBOUT, THE CREW RECEIVED A PASSENGER DOOR UNLOCK INDICATION AND RETURNED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE OVERCENTER SWITCH AND SHOOT BOLT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031208000632003120800063EU 2003 12 8 03FDEA01800 120031024A5730EADS2572491521 SKIN AIRBUS310 A310203 3930313EU ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25442FE 353 MEM MX REPORTS A 1.9 INCH CRACK IN THE RT LOWER WING SKIN AT RIB 11. ACCOMPLISHED WORK CARD T6-5610-66979 A PT3 AT CWF BY INSTALLING DOUBLER AT RIB 11 PER EA 6-571066979 PT 3 AND EA6-5710-73414A AND NRC S00025. 2L72 4F RTA35EU 20031208000742003120800074NM 2003 12 8 AWXA200301295 120031013A5315146N5417 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1470, RBL 2. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM BETWEEN BS 1450 AND BS 1480, RBL 2; FABRICATED 4 EACH REPAIR ANGLES AND 2 EACH CHANNELS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 1. 2L72 4F RTA2NM 20031208000762003120800076NM 2003 12 8 SWAA032301 120031019A5320BAC1509 FLOOR SUPPORT BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED 1/4D CHECK, FOUND 4 EA LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 771, LBL 3, LBL 8, LBL 12 AND LBL 17. REPAIRED FLOOR SUPPORT PER SWA EA. 2L72 4F RTA16WE 20031208000812003120800081NM 2003 12 8 DHL2003745023 120031025A3260 WARNING SWITCH BOEING727 727224 1384076NM MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION GEAR DOOR LIGHT ILLUMINATED WHEN GEAR HANDLE POSITIONED TO OFF. RAN ABNORMAL PROCEDURE, LIGHT WENT OUT. ADJUSTED LEFT-HAND LANDING GEAR DOOR WARNING SWITCH IAW M/M 32-62-11. OPS CHECK IS GOOD. 2L73 4F A3WE 20031208001182003120800118NM 2003 12 8 AWXA200301316 120031002A532069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .375 INCH CRACK WAS FOUND STRINGER TIE CLIP IN AFT CARGO COMPARTMENT BS 727A, STR 25 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP IN AFT CARGO COMPARTMENT BS 727A, STR 25 LT IAW B737-300 SRM 51-40-02 PG 1, 38, & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031208001212003120800121NM 2003 12 8 AWXA200301319 120031017A532065794063 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK .625 INCH CRACK WAS FOUND ON UPPER ANGLE AT FORWARD AVIONICS RACK BS 294 TO BS 320. MAINTENANCE REMOVED CRACKED ANGLE AT FORWARD AVIONICS RACK BS 294 TO BS 320; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-79406; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20030916001602003091600160NE 2003 9 16 JYD2003F00001 120030304A53126510111016041 PRESSURE PANEL SKRSKYS64 S64F 8142610NE FUSELAGE CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09158AC1911 754 64081 PRESSURE PLATE (PN 65101-11016-041) FOUND CRACKED. MAIN ROTOR HEAD (MRH) REMOVED FROM SERVICE DUE TO SEVERE STORM DAMAGE WITH A TT 3772.9 AND A TSO 754. DURING OVERHAUL OF MRH, A CRACK INDICATION WAS DETECTED IN PRESSURE PLATE (PN 65101-11016-041) DURING FLUORESCENT PENETRANT INSP. CRACK LOCATED ON EAR/LUG STARTING AT THE INTERSECTION OF .120 INCH AND .060 INCH RADIUS TRANSITION APPROXIMATELY .300 INCH IN LENGTH. PROBABLE CAUSE: SHARP RADIUS IN AN AREA WHERE THREE RADII INTERSECT. RECOMMENDATIONS TO PREVENT RECURRENCE: HOLD RADIUS DIMENSIONS TO HIGH END OF TOLERANCE. REWORK TO APPROVED REPAIR PROCEDURE WHICH HAS BEEN ESTABLISHED. 2G72 4U H6EA 20030917000212003091700021WP 2003 9 17 0301339991 120030718A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING "L" CHECK FUSELAGE SKIN WAS FOUND TO HAVE SIX HI-LOKS WITH DAMAGED HEAD AND TWO FASTENER HOLES WITH CRACKS AT BS 192 L22L. REPAIRED PER EA 99-191013. 2L72 4F A6WE 20030917000862003091700086EA 2003 9 17 ASOA03388 120030817A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DUIRNG A C-CHECK IN MCN, THE SECOND FROM AFT CARGO WALL BULKHEAD TRANSFER BEAM UNDER THE SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM AFT CARGO WALL BULKHEAD TRANSFER BEAM UNDER THE SEAL PLATE IAW SRM 51-42-70. (M) 2L72 4F RTA21EA 20030917000882003091700088NM 2003 9 17 AMTA200301036 120030808A2120 ODOR BOEING737 73783N 13844HINM COCKPIT DETECTED A AMTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL11331TZ 30660 LIGHT ODOR OF SMOKE IN ROWS 24 PLUS 25, NO VISABLE SMOKE IN CABIN. OPERATED PACKS WITH ENGIENS PLUS APU INSPECTED OVERHEAD PANELS FOR ROWS 23 THROUGH 26, NO ODOR OF SMOKE OF EVIDENCE OF SMOKE NOTED. (M) 2L72 4F RTA16WE 20030918000882003091800088EU 2003 9 18 V9B2003F00002 120030620A27224AS5830510013 ACTUATOR ISRAELGALAXYGALAXY 4500307EU RUDDER TRIM INOPERATIVE E V9BAO OTHER O OTHER NRNOT REPORTED 1 SW0583EJ 2501 009 RUDDER TRIM INOPERATIVE. FOUND LOWER RUDDER TRIM ACTUATOR RECEIVING ELECTRICAL POWER BUT THE TRIM ACTUATOR WOULD NOT MOVE. 2L72 4F RTA53NM 20030918001362003091800136EU 2003 9 18 XNOA01142 120030807A2730 CONNECTOR AIRBUS300 A300B4203 3930306EU ELEVATOR DIRTY A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23372PC 196 ELEVATOR FCPI STUCK IN FULL DOWN POSITION. CLEANED CONNECTOR ON FCPI SYS. OPS CHECK GOOD IAW A300 MM 27-15-00. 2L72 4F RTA35EU 20030919000462003091900046NM 2003 9 19 IU62003F00030 120030613A2761654494710 HOUSING BOEING737 737* NM SPOILER ACTUATORCRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 1399 SPOILER ACTUATOR CRACKED AROUND SHOULDER ON THE INSIDE DIAMETER OF THE HOUSING. OLD STYLE HOUSING IS SUSCEPTIBLE TO CRACKING. REPLACE WITH NEW STEEL HOUSING. (NR 178253) 2L72 4F RTA16WE 20030919000842003091900084CE 2003 9 19 YBS2003F00001 120030729A5520NAS464P38 BOLT CESSNA402 402C 207590RCE ELEV TRIM TAB MISSING E YBSAO OTHER O OTHER NRNOT REPORTED 1 EA17818AN 402C0501 SHORTLY AFTER ROTATION AND GEAR SELECT UP (APPROX 200MSL) CREW REPORTED SEVERE ELEVATOR VIBARATION. EMERGENCY WAS DECLARED, LANDING W/O FURTHER PROBLEMS. MECHANIC INSPECTED ENTIRE ELEVATOR TRIM CONTROL SYSTEMS AND HORIZONTAL STABILIZER. MECHANIC FOUND ELEVATOR TRIM TAB ACTUATOR PUSH PULL ROD TO TAB HORN BOLT MISSING. CREW CONFIRMED HARDWARE WAS PRESENT ON ALL CONTROL TABS DURING PREFLIGHT. MECHANIC REPLACED MISSING BOLT AND RETURNED AIRCRAFT TO SERVICE. 1L72 3O A7CE 20030919000982003091900098NM 2003 9 19 373PA0019 120030813A3350 BATTERY PACK BOEING737 7373Y0 1384671NM EMERGENCY LIGHTSINOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05373PA 23749 CREW REPORTS THAT EMERGENCY LIGHT TEST TAKES A FEW ATTEMPTS TO TEST CORRECTLY. REPLACED ALL THREE TRANSMITTER BATTERY PACKS IN OVERHEAD PANELS. PERFORMED SYSTEM TEST IAW SERVICE CHECK. TEST NORMAL. 2L72 4F RTA16WE 20030919001142003091900114EU 2003 9 19 AWXA200300925 120030802A5350D5323022620100 PLATE AIRBUS320 A320232 3930326EU FAIRING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK A .3750 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FAIRING CLOSING PLATE AT FR 34, Y1600, Z1610. MAINTENANCE REMOVED CRACKED CLOSING PLATE AT FR 34, Y1600, Z1610; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-10, 12, FIG. 2 & 3. 2L72 4F RTA28NM 20030919001232003091900123NM 2003 9 19 03FDEA01209 120030729A5753ARC70541 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RT WING O/B FLAP VANE- TEE FITTING NR 2 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 2 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71878, 2L73 4F RTA22WE 20030919001322003091900132NM 2003 9 19 PCAA0308098 120030725A534785320490 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13845EX 344 DURING C INSPECTION A FLOOR SUPPORT FLANGE AT THE RT INBOARD SEAT TRACK LOCATION WAS FOUND CORRODED BETWEEN STATION 182.0 AND 270.5. CORROSION WAS REMOVED IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 STRUCTURAL REPAIR MANUAL 51-20-11. AREA WAS REINSPECTED AND FOUND TO BE BEYOND DAMAGE LIMITS OF REPAIR DRAWING RD8-53-1339 FROM STATION 182.0 TO 270.5. THE RIGHT INBOARD SEAT TRACK SECTION WAS REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-3074. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030919001582003091900158NM 2003 9 19 AWXA200300938 120030808A5340D53230281200 ATTACH ANGLE AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON ATTACH ANGLE UNDER PANEL 191 AT AT BS 1483. MAINTENANCE REMOVED CRACKED ATTACH ANGLE UNDER PANEL 191AT AT BS 1483; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-24-00, PG. 3, FIG. 1, & SRM 51-42-11, PG. 7-10, FIG. 2. 2L72 4F RTA28NM 20030922000052003092200005EU 2003 9 22 ZES2003F00002 120030808A324050028053 BRAKE ASSY ISRAEL1124 1124 4500102EU RT MLG FAILED E ZESAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA03351C 249 264 DURING TAKE OFF ROLL FROM DLHA, VIBRATION WAS FELT FROM THE RT MLG. PILOT ABORTED TAKE OFF AND BROUGHT THE AIRCRAFT TO A STOP AT THE END OF THE RUNWAY. SUBSEQUENT INVESTIGATION REVEALED THAT THE RT BRAKE HAD FAILED. REPLACED BRAKE ASSEMBLY WITH AN OVERHAULED UNIT. NO FURTHER OCCURANCE. 2M72 4F A2SW 20030922000062003092200006CE 2003 9 22 ZES2003F00003 120030708A261224403915 FIRE LOOP LEAR 35 31A 5170531CE GARRTTTFE731TFE731* 01518WP LT ENGINE FAILED E ZESAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA0370AE 1737 188 PILOT REPORTED THAT THE LT FIRE WARNING CAME ON TWICE FOR APPROX 5 SECONDS THEN EXTINGUISHED. TROUBLESHOT AND FOUND THE LT ENGINE FIRE (ACESSORY DRIVE) LOOP TO FAIL THE RESISTANCE AND INSULATION TEST. REPLACED THE FIRE LOOP WITH NEW. 2L72 4F4 FRTA10CE E6WE 20030922000192003092200019NM 2003 9 22 2003UALA00614 120030808A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29176UA 24383 AFT CARGO COMPARTMENT FLOORBEAM STA. 1580 RBL 57 DENTED IN TWO PLACES. INSTALLED NEW WEB AND DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20030922000382003092200038SO 2003 9 22 RAIA00307204 120030731A25105041314021028 SHOULDER BELT EMB 145 EMB145LR 3260212SO COCKPIT STUCK A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03812HK 145373 FO SHOULDER HARNESS WOULD NOT EXTEND. MAINTENANCE REMOVED AND REPLACED FO'S SHOULDER HARNESS. 2L72 4T RTT00011AT 20030915000402003091500040EU 2003 9 15 I05R089179 120030801A6710L673M20A1005 ACTUATOR UROCOPEC135 EC135P1 8680990EU MAIN ROTOR LEAKING E I05RO OTHER K FLUID LOSS NRNOT REPORTED 1 WP05551BA1158 188 MAIN ROTOR ACTUATOR LATERAL STIFF AND LEAKING REPLACED PART 1G72 3U O H88EU 20030916000812003091600081WP 2003 9 16 GTIA030628 120030725A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND CABIN FLOOR PANEL STATION 886-927 DELAMINATED. FORMED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030916000942003091600094EU 2003 9 16 ASOA03395 120030823A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11535AS 464 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030916001502003091600150WP 2003 9 16 IXXA0300049O 120030724A7720 SENSOR DOUG DC8 DC871F 302199DWP NR 1 EGT DAMAGED A IXXAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW11823BX854342663 46064 DURING FLIGHT FROM KBWA TO KTOL THE NR 1 ENGINE EGT ROSE ABNORMALLY. RETARDED THROTTLE, N1.N2, AND FUEL FLOW FOLLOWED. CREW DID A PRECAUTIONARY SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EGT PIGTAIL IAW ALL APPLICABLE MANUALS. MAINTENANCE RAN THE NR 1 ENGINE IAW ALL APPLICABLE MANUALS AND OPERATIONAL CHECK CONFIRMED CAUSE AND VERIFIED INDICATION PROBLEM ONLY. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030917000052003091700005 2003 9 17 BAQ2003F00002 420030702A2210SCB034 ROLL SERVO AEROSPAS365 AS365N2 8680815EU AUTO FLIGHT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA17915ME2990 6417 REMOVED AND REPLACED SERVO WITH AN OVERHAULED SERVO. UPON GROUND RUN AND LEAK CHECK, PILOT STATED: ON START, AIRCRAFT CYCLIC WENT FULL LEFT. COULD NOT GET CENTERED. PILOT SHUT DOWN AIRCRAFT BEFORE POSSIBLE ROLL-OVER. REMOVED AND INSPECTED SERVO. FOUND PILOT VALVE ON SERVO HITTING COVER PLATE OF SERVO. SENT BACK TO REPAIR OPERATOR FOR EVALUATION. 1G72 3U RTH10EU 20030917000422003091700042EU 2003 9 17 00101 120030728A3297 RELAY AMD FALC20FALCON 2720302EU MLG LOOSE E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05158TW 158 LANDING GEAR WOULD NOT RETRACT ON DEPARTURE FROM ATL, AIRCRAFT RETURNED TO ATL. WILL UPDATE AFTER MAINTENANCE. MAINTENANCE FOUND RELAY LOOSE. SECURED AND OPS CHECK GEAR SWING GOOD. 2L72 4F A7EU 20030917000472003091700047NM 2003 9 17 03FDEA01177 120030730A5270 PROXIMITY SENSOR BOEING727 727200 138407ENM MAIN CARGO DOOR OUT OF ADJUST A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25280FE 22347 LEVEL FL 190 280 KTS OCN LT TURB MAIN CARGO DOOR WARNING LIGHT ILLUMINATED STEADY THEN WENT DIM AND EXTINGUISHED AFTER 30 SEC AS WE COMPLIED WITH RED TABS. CHECKED OPERATION AND INDICATION OF MAIN CARGO DOOR, ONLY DISCREPANCY NOTED WAS INCORRECT ADJUSTMENT OF THE NR3 AND NR 5 OVERCENTER PROXIMITY SWITCHES. LATCHES ALIGNED WITH WHITE STRIPES IAW MM, DOWN SEQUENCE SWITCH WITHIN ADJUSTMENT. ADJUSTED NR 3 AND NR 5 OVERCTR. PROX SWITCHES IAW B727MM 52-34-009-5 PARA. 1 F.(1). MAIN CARGO DOOR OPERATES AND INDICATES NORMAL. 2L73 4F RTA3WE 20030917001382003091700138NM 2003 9 17 DL764030702 120030725A2121732591 FAN BOEING767 767432ER 1385134NM E/E BAY DAMAGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27832MH 29704 FWD EQUIP COOLING MESSAGE IN AUTO AND STANDBY. REPLACED COOLING FAN 2L72 4F RTA1NM 20030918000752003091800075EU 2003 9 18 U30A200300025 120030803A5210 BOTTLE AIRBUS320 A320214 3930316EU PAX DOOR DISCHARGED A U30AK NONE O OTHER ININSP/MAINT 1 EA17264AV 1867 DURING "DAILY" CHECK, IN ORD, THE R2 CREW/PAX DOOR EMERGENCY OPERATION ASSIST/DAMPER BOTTLE HAD LOW PRESURE. MAINTENANCE SERVICED THE R2 EMERGENCY OPERATION ASSIST/DAMPER BOTTLE IAW AMM 52-10-00-614. ON 8/4/03 DURING THE NEXT "DAILY CHECK, SRTC (SPECIAL REQUEST TASK CARD) 52-03-005 WAS ISSUED TO REPLACE THE DIAPHRAGM AND ASSOCIATED SEALS IN THE PERCUSSION MECHANISM. THE DIAPHRAGM (P/N FE240-221-001) AND SEALS WERE REPLACED AND THE BOTTLE RESERVICED. 2L72 4F RTA28NM 20030918001332003091800133WP 2003 9 18 0301509943 120030708A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011308T 47315 DURING "L" CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 LBL 18-19 AND BS 76.5 LBL 18-20. REPAIRED PER EA 99-195678. 2L72 4F A6WE 20030919000012003091900001 2003 9 19 0301526627 420030806A233020133 DISPLAY BOEING747 747251B 1384892NM 'B' ZONE LEFT FAILED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01627US6282 4675 21709 LEFT 'B' ZONE VIDEO SCREEN WAS TURNED OFF DURING FLIGHT DUE TO A BURNING ODOR COMING FROM IT. FLIGHT CONTINUED TO KIX AND LANDED WITHOUT INCIDENT. REPLACED 21 INCH PLASMA DISPLAY PANEL. AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 20030919000052003091900005GL 2003 9 19 0065686 320030321A6111L104DSZ BLADE BCRAFTHB HONEYBEEHB 1110102WP PWA PT6 PT6* 52043EA MCAULY5JFR365JFR36C1003 GL PROPELLER CORRODED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 920485 PROPELLER HAS CORROSION ON BLADE. 1H71 3O3 T 4A11 E2NE 6 CP15NE 20030919000062003091900006GL 2003 9 19 0067341 320030719A6111114HCA BLADE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MCAULY5JFR36B5JFR36C1103GL PROPELLER CRACKED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 41076 952540 CRACK ON PROPELLER BLADE 2L72 4T3 TRTA41NM E2WE 6 CP15NE 20030919000072003091900007EU 2003 9 19 MALA030371 120030804A2420 GCU SAAB SF340 SF340A 7850100EU AC SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15068XJ DURING FLIGHT, LT AC GEN FALLING OFF LINE. AIR RETURN TO DTW. MAINTENANCE REPLACED LH AC GEN CONTROL UNIT. IAW MM ALL CHECKS GOOD. 2L72 4T RTA52EU 20030919000172003091900017EU 2003 9 19 03FDEA01228 120030808A2611 SMOKE DETECTOR AIRBUS310 A310 EU AFT CARGO AREA ACTIVATED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25414FE 400 CRUISE ALTITUDE 2C ENROUTE MEM 2 FLAS 22 CARGO COMPD SMOKE DETECT 22 AFT SMOKE LIGHT ILLUMINATED WITH ECAM DEPICTION. DECLARED EMER 7 DIVERTED TO DISCHARGED AGENT 1 PER CHECKLIST 2C FOLLOWED BY AGENT 2 PER CHECKLIST. A CAPT AND FO REPORTED SMOKE INDICATION ON OF HD AND ECAM FOR AFT CARGO. CREW SAID THEY NEVER SMELLED SMOKE IN COCKPIT. AD SMELL ODOR WHEN THE AFT CARGO DOOR WAS FIRST OPENED. NO SMOKE OR ODOR WAS FOUND IN ANY OTHER COMPARTMENT. R 27D LT AND RT WATER SEPARATOR BAGS PRECAUTIONARY REF MM 21-51-16- REPLACED ALL 4 SMOKE DETECTORS IN THE AFT AND BULK CARGO PITS IAW MM 26-16-11-4 2L72 4F RTA35EU 20030919000522003091900052EU 2003 9 19 VJ32003F00028 120030730A2434115TA600311 BRACKET GROB 120 G120A 1660208EU LYC O540 AEIO540D4D5 EA ALTERNATOR CRACKED B VJ3RK NONE O OTHER ININSP/MAINT 1 WP07861AF993 85001 L2802348A DURING ROUTINE INSPECTION, FOUND THE ALTERNATOR MAOUNTING BRACKET CRACKED. SUSPECT VIBRATION CAUSED CRACK. RECOMMEND GUSSETS BE WELDED INTO RADIUS OF BRACKET OR CHANGE IN MATERIAL/MANUFACTURING PROCESS. 1L71 3O3 ORTA49CE 1E4 20031001001242003100100124WP 2003 10 1 ARWA20030912 120030915A5755 PANEL LKHEED1011 1011385115 5265015WP SPOILER BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19308GB 193U1133 ON POST-FLIGHT FOUND RT WING INBOARD SPOILER PANEL NR 2 INBOARD WING TRAILING EDGE BRACKET BROKEN. REMOVED AND REPLACED UPPER CAP AT T/E STATION 137.0 & 226.6 IAW SR SRM 57-22-00. REMOVED AND RE-INSTALLED T/E UPPER PANELS AT NR 2 SPOILER AREA IAW SRM 51-40-1. REMOVED AND REPLACED RT WING NR 2 SPOILER PANEL ASSEMBLY IAW MM 27-61-26. OPERATIONAL CHECKED NORMAL IAW MM 27-61-26. 2L73 4F A23WE 20030919001182003091900118NM 2003 9 19 QXEA200300975 120030813A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 LEFT AFT FUSELAGE HAS IMPACT DAMAGE, JUST AFT OF STATION X736.096. REPAIRED IAW HORIZON AIR EA 2-53-465. 2H72 4T RTA13NM 20030919001552003091900155EU 2003 9 19 AWXA200300935 120030803A5320D5347048200200 PROFILE AIRBUS320 A320232 3930326EU CARGO DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT TRANSITION PROFILE BETWEEN FR 56-58. MAINTENANCE REMOVED RT TRANSITION PROFILE BETWEEN FR 56-58; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 8-12, FIG. 2 &3. 2L72 4F RTA28NM 20030922000232003092200023NM 2003 9 22 2003UALA00620 120030812A5310 SHEAR TIE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA 29239 AFT CARGO PIT AT BS 1197+44 BETWEEN STR 39L-39R SHEAR TIE IS CORRODED. 2L72 4F4 FRTA1NM E24NE 20030922000522003092200052CE 2003 9 22 FUK2003F00000 120030805A56101014200805 WINDOW BEECH 90 F90 1152909CE PWA PT6 PT6* 52043EA COCKPIT CRACKED E FUKAO OTHER O OTHER NRNOT REPORTED 1 NE03448827402 LA102 NOTICED CRACKS BETWEEN WINDOW LATCH BRACKET HOLES DURING A PHASE 1 CHECK. REMOVED BOTH STORM WINDOWS AND FOUND INNER PLY CRACKS IN BETWEEN ALL 5 DRILLED MOUNTING HOLES IN ADDITION TO THE LATCH BRACKET CRACKS. THE WINDOW ALSO EXHIBITS STRESS CRACKS IN THE MILLED RADIUS AROUND THE WINDOW PERIMETER. SUGGEST A CYCLE LIMIT OR DETAILED INSPECTION. MOST CRACKS ARE NOT VISIBLE UNTIL SEPARATING THE WINDOW FROM ITS HINGE MOUNT. 6853 CYCLES/22 YEARS 1L72 4T3 T A31CE E2NE 20030922000582003092200058EU 2003 9 22 IXXA0300056O 220030820A7200 ENGINE DOUG DC8 DC873F 302199FWP CFMINTCFM56 CFM563B2 13802EU NR 3 FLUCTUATES A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11603AL912252225 46003 DURING CLIMB FROM KTOL TO KBNA THE NR 3 ENGINE EGT BEGAN TO FLUCUATE BOTH ANALOG AND DIGITAL +/- 50 DEGREES C. CREW RETURNED AIRCRAFT TO KTOL AND FLUCUATION CONTINUED THROUGH DESCENT AND LANDING. AIRCRAFT LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. 2L74 4F4 FRT4A25 E21EU 20030922000782003092200078NM 2003 9 22 AWXA200300955 120030804A5320D53974971200 PROFILE AIRBUSA319 A319132 3930340NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 53, STR 39 LT - 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 53, STR 39 L/H - 39 R/H; FABRICATED A NEW REPLACEMENT PROFILE PER DWG 17-D53974971; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12. 2L72 4F RTA28NM 20030922000792003092200079NM 2003 9 22 AWXA200300956 120030805A5347D53112827202 CARGO TRACK AIRBUSA319 A319132 3930340NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y503 DUMMY RAIL BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y503 DUMMY RAIL BETWEEN FR 14 AND FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 24-25, FIG. 9. 2L72 4F RTA28NM 20030917000522003091700052NM 2003 9 17 UIEA200300034 120030713A3260834503 SENSOR BOEING747 74747UF 1384949NM GE CF6 CF680 30025NE MLG DOOR DAMAGED A UIEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15494MC 29255 AFTER TAKEOFF DURING CLIMB/CRUISE, FAULT CODE 32 32 03 00 (GEAR DOOR). LEFT BODY GEAR DOOR POSITION INDICATOR SHOWED INTRANSIT IN BOTH GEAR UP AND GEAR DOWN POSITIONS. AIRCRAFT RETURNED TO HKG. FUEL DUMPED 36,500 KGS. FOUND LEFT BODY GEAR ALT SENSOR S428 DAMAGED. SENSOR REPLACED AND ADJUSTED REF AMM 32-61-31. GROUND CHECK INDICATES NORMAL. 2L74 4F4 FRT1384945 E13NE 20030917001162003091700116NE 2003 9 17 AMTA200300955 220030719A73148283004 PUMP BOEING737 73783N 13844HINM GE CFM56 CFM56* 13802NE LT ENGINE INOPERATIVE A AMTAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 GL11306TZ5766 32348 889536 ON DESCENT THE LT ENG FAIL ILLUMINATED FOLLOWED BY SOURCE OFF, LEFT ENGINE RE-LIT. MOVING THRUST LEVER TO IDLE RESULTED IN LEFT ENGINE FAIL AGAIN. MOVING THRUST LEVER FORWARD MADE ENGINE LIGHT OFF AGAIN. REMOVED AND REPLACED FUEL PUMP IAW MM. PACKAGE REMOVE AND REPLACE PERFORMED ENGINE RUN IAW 71-00-00-800-801-F00. OPS CHECK GOOD, NO LEAKS NOTED. 2L72 4F4 FRTA16WE E2GL 20030917001292003091700129NM 2003 9 17 DL76S030685 120030722A5330 SKIN BOEING767 767332 1382001NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27128DL 24078 SKIN DENT AND GOUGE FOUND AT STATION 1370 AND STR 29R. REPAIR PER ER/A 385435-14 2L72 4F RTA1NM 20030918000572003091800057NM 2003 9 18 DLM88030713 120030801A3620UNK VALVE DOUG MD88 MD88 3023688NM TAIL LEAKING A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27919DL 49584 TAIL COMPT OVERHEAT LIGHT CAME ON AT 10000 FT. CONT TO CYCLETHE REST OF FLIGHT. LIGHT EXT ON THE GROUND. FOUND LEAKS AT LT AUG VALVE AND LT HEAT EXCHANGER. THIGHTENED CLAMPS, PERFORMED HIGH POWER ENGINE RUN WITH BOTHENGINES NO LEAKS NOTED. 2L72 4F RTA6WE 20031208001422003120800142NM 2003 12 8 2003UALA00793 120031021A3350 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29784UA 26951 SEAT 1E, AFT EMERGENCY LIGHT INOP. RELAMPED. 2L72 4F4 FRTT0001SE E46NE 20031208001442003120800144NE 2003 12 8 2003UALA00799 220031023A7261 O-RING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE MISSING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29662UA 27159 DIVERTED DUE TO OIL LOSS IN NR 1 ENGINE. NR 3 CHIP DETECTOR FALLING OUT OF THE DETECTOR HOUSING AND A MISSING O-RING ON THE CHECK VALVE IN THE HOUSING CAUSED THE LOSS OF OIL. THERE WAS NO WEAR ON THE HOUSING TO CAUSE THE DETECTOR TO BECOME FREE. A COA WILL REPLACE THE OLD DESIGN OF THE CHIP DETECTOR WITH AN IMPROVED DESIGN. 2L72 4F4 FRTA1NM E24NE 20031204001602003120400160EU 2003 12 4 MALA030463 120030925A5260 HAND RAIL BAC 146 AVRO146RJ85A1500097EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, O/B AIRSTAIR RAIL CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED RAIL. REFER TO 409 189916 FOR ADDITIONAL DETAIL. 2H74 4F RTA49EU 20031204001892003120400189WP 2003 12 4 MWEA030425 120031021A52303614118503 STRUCTURE DOUG DC9 DC981 3022081WP DOOR HANDLE GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 MID CARGO DOOR HANDLE RECESS CUP HAS A DEEP GOUGE FROM HANDLE WHEN IT ROTATES. FABRICATED AND INSTALLED PAN. 2L72 4F A6WE 20031204001912003120400191WP 2003 12 4 MWEA030427 120031021A532199365993 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 FLOORBOARD IN AFT BAG-PIT AT STATION 1155 HAS AREA WORN AND DETERIORATED AT FORWARD EGDE OF LOWER CENTER PANEL, JUST INSIDE BAG-PIT DOOR. FABRICATED AND INSTALLED NEW FLOORBOARD. 2L72 4F A6WE 20031205000122003120500012NM 2003 12 5 F3LA200300151 120031020A5410 CHANNEL BOEING737 737301 1384611NM NR 1 NACELLE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03578US 2672 23257 DURING C-5 CHECK, INSPECTION REPORTED NR 1 ENGINE CHANNEL CRACKED OUTBOARD LOWER AFT END LT PYLON AT STA 320. REPLACED CHANNEL PER SRM 51-40-02. 2L72 4F RTA16WE 20031205000312003120500031NE 2003 12 5 DL757030921 220031012A7321 FUEL CONTROL BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27620DL45254 22910 716526 LT ENG FAILED TO ACHIEVE T/O EPR 1.43 SCHEDULED W/NORMAL PWR GOT TO 1.3, COMMAND SELECT SHOWING, THROTTLE AT FIRE-WALL. AFTER ABORTED GOT STATUS LT ENG CONT. REPLACED FUEL CONTROL. 2L72 4F4 FRTA2NM E17NE 20031205000692003120500069NM 2003 12 5 ASAA0240134A 120030315A5300BAC1509100146 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FS 860 CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 860, RBL 8 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031208001772003120800177WP 2003 12 8 DHL2003805012 120031028A2612 CONTROL UNIT DOUG DC8 DC873F 302199FWP NR 1 FIRE DETECTMALFUNCTIONED A DHLAB EMER. DESCENT J WARNING INDICATION NRNOT REPORTED 1 SO01805DH 46125 ENGINE FIRE ON NR 1. PERFORMED EMERGENCY CHECKLIST. FIRE INDICATION STILL CONTINUED. PER CREW REPORT B-LOOP AT FAULT. INSPECTED ENGINE NO SIGNS OF FIRE EVIDENT. DEFERRED B-LOOP PER MEL 26-2-3 DMI NR 14565. FIRE BOTTLE NR 1 WAS DISCHARGED REF ITEM 1P LOG PAGE 360357. FIRE BOTTLE NR 2 WAS DISCHARGED REF ITEM 1P LOG PAGE 360357. REMOVED AND REPLACED NR 1 FIRE BOTTLE IAW SMM 26-20-01. OPS CHECKED GOOD. REMOVED AND REPLACED NR 2 FIRE BOTTLE IAW SMM 26-20-01. OPS CHECKED GOOD. REPLACE NR 1 ENGINE FIRE DETECTOR CONTROL UNIT PRECAUTIONARY. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTOR CONTROL UNIT IAW 26-10-2. OPS GOOD. DMI 14565 ENGINE FIRE ON NR 1 PERFORMED EMERGENCY (PER CREW LOOP-B). 2L74 4F RT4A25 20031209000052003120900005WP 2003 12 9 UPS03841470 120031022A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C1, INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN STATION 355 TO 450 AT LONG 31L. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5773863 AND SRM 51-1-20D. 2L74 4F RT4A25 20031209000092003120900009WP 2003 12 9 UPS03841474 120031020A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING LE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, RT WING L/E LOWER RIB IS CRACKED AT STA 616.25. STOPDRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20031209000122003120900012WP 2003 12 9 UPS03841477 120031023A5531 RIB DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, VERTICLE FIN LOWER L/E SECTION HAS A RT RIB CRACKED AT ZFS 98.250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM 55-2-0 FIG 2. 2L74 4F RT4A25 20031209000342003120900034 2003 12 9 SWIA200312541 420031017A3418 STICK SHAKER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING WILL NOT TEST A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07906SW 7510 STICK PUSHER WILL NOT TEST. REMOVED AND REPLACED STICK PUSHER IAW CRJ MM 27-35-15. OPS CHECKS GOOD. P/N: 600-59156-15, S/N OFF: 1649. 2L72 4F RTA21EA 20031209000472003120900047NM 2003 12 9 P5CA0300970 120031028A532065B832537 SUPPORT BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RBG - WING TO BODY SEAL - HYDRAULIC GANG CLAMP SUPPORT BLOCK CORRODED. REMOVED AND REPLACED SEAL BLOCK SUPPORT BLOCK PER SRM 51-10-01. CORROSION REMOVED WITH SEAL BLOCK. BASIC STRUCTURE NOT CORRODED. 2L74 4F A20WE 20031209000592003120900059NM 2003 12 9 SWAA032359 120031026A3350BR2013 BULB BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 EEPLS INOP AND COVER LOOSE AT ROW 15. RELAMPED AND INSTALLED LENS COVER PER MM. 2L72 4F A16WE 20030924001162003092400116EU 2003 9 24 226072203 120030722A24345243212137 SHAFT PILATSPC12 PC1245 7090551EU NR 2 GENERATOR WORN E S4WAK NONE O OTHER ININSP/MAINT 1 WP07308NA 226 NR 2 GENERATOR DRIVE SHAFT WORN AND PITTED. 1L71 3T RTA78EU 20030924001352003092400135 2003 9 24 AALA20030749 420030712A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21686AA 25343 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001412003092400141 2003 9 24 AALA20030751 420030709A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21693AA 26973 JFK - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001422003092400142 2003 9 24 AALA20030756 420030712A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21615AM 24491 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS OUT OF ADJUSTMENT AND TWO NEEDING REPLACED. ADJUSTED FOUR GIRT BAR SPRINGS AND REPLACED TWO. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000232003092500023EU 2003 9 25 ASOA03411 120030816A5320 A/C PACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11633AS 344 DURING A C-CHECK IN BNA, THE RT SIDE C-CHECK CHANNEL AT THE SERVICE DOOR BETWEEN FRAMES 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE 'C' CHANNEL AT THE SERVICE DOOR BETWEEN FRAMES 38 AND 39 IAW SRM 51-24-01 AND 51-25-04. (M) 2H72 4T RTA53EU 20030925000372003092500037 2003 9 25 AALA20030763 420030708A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21653A 24611 DFW - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS NEEDING REPLACED. REPLACED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000542003092500054SO 2003 9 25 SIMA200323004 120030812A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 DURING AN IMBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED ARAE. FABRICATED A REPAIR DOUBLER, FILLER AND TWO SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-22-10, 51-40-02, 51-40-04 AND 51-40-06. (M) 2L72 4F RTT00011AT 20030925000582003092500058NM 2003 9 25 USAA030161 120030818A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US 23318 FOUND SKIN CRACKED 3 INCHES, FORWARD OF FS 520, .500 INCH BELOW S12L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040122000982004012200098EA 2004 1 22 ASOA03646 120031214A5200601R3807413 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING A C-CHECK IN MCN, THE FORWARD CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040122001142004012200114EA 2004 1 22 ASOA03638 120031208A27419960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA MACH TRIM INOPERATIVE A ASOAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO11919EV 7780 DURING TAKEOFF FROM ATL-CHA, WHILE IN TRANSITION TO CLIMB THE CREW RECEIVED A STAB TRIM AND MACH TRIM AMBER CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH, BUT THE TRIM WOULD NT RE-ENGAGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE CO-PILOTS PITCH TRIM DISCONNECT SWITCH. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001152004012200115EA 2004 1 22 ASOA03633 120031207A5210H341427 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 FLT 4378 - DURING A GROUND INSPECTION IN ATL, THE MAIN PASSENGER DOOR WAS VERY DIFFICULT TO OPEN FROM THE OUTSIDE. MAINTENANCE ADJUSTED THE OUTER AND INNER HANDLE ASSEMBLIES ON THE MAIN PASSENGER DOOR IAW AMM 52-11-02 AND AMM 52-11-03. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001202004012200120EA 2004 1 22 ASOA03622 120031203A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 FLT 4829 - DURING AROUND INSPECTION IN DFW, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE ACTUATOR ARM CONNECTION. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001272004012200127EA 2004 1 22 ASOA03655 120031216A2910601R7528661 TUBE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM CRACKED A ASOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11823AS 7196 DURING CRUISE FROM ATL-YUL, AT APPROXIMATELY 29,000 FT THE CREW RECEIVED A HYDRAULIC NR 1 LOW PRESSURE AMBER CAUTION MESSAGE, WITH A PRESSURE DROP FROM 1500 PSI TO ZERO AND A QUANTITY READING OF ZERO. THE CREW COMPLIED WITH QRH PROCEDURES AND THE AIRCRAFT DIVERTED INTO CVG, LANDING SAFELY. THE TOWER ROLLED EMERGENCY VEHICLES AS A PRECAUTIONARY MEASURE. MAINTENANCE REMOVED AND REPLACED THE SYSTEM 1 PUMP PRESSURE TUBE ASSEMBLY, CASE DRAIN TUBE ASSEMBLY, ENGINE HYDRAULIC PUMP, AND FOUR LINE STAND-OFF ISOLATORS. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001292004012200129WP 2004 1 22 GTIA030967 120031107A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND DENT AT FS 446-468 BETWEEN LONGERONS 25 AND 26R DENT IS IN RVSM CONTROLLED AREA AND REQUIRES REPAIR. CUT OUT DAMAGED AREA BETWEEN STATION 443-477.5. FABRICATED 5 EACH DOUBLERS, 7 STRAPS, 1 FINGER DOUBLER AND 11 NEW SECTION OF SKIN AND 13 STRAPS. INSTALLED REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20040122001332004012200133WP 2004 1 22 GTIA030965 120031107A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND FLOOR PANEL CENTER 826-886, METAL EDGE WORN THROUGH, METAL EDGE HAS GOUGE MARKS, CRACKED AT FASTENER HOLE, SURFACE CORROSION. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20031209000952003120900095NM 2003 12 9 SWAA032315 120031018A53306545773 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STR 14R. REPAIRED SKIN PER ERO. 2L72 4F RTA16WE 20031209000962003120900096NM 2003 12 9 SWAA032316 120031018A53146545866 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE KEELBEAM CRACKED, RT SIDE, BS 727+10. REPAIRED KEEL BEAM PER ERO. 2L72 4F RTA16WE 20031209001022003120900102NM 2003 12 9 SWAA032322 120031021A53106546525 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND SHEAR TIE DAMAGED AT BS 400, STRINGER 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031209001132003120900113NM 2003 12 9 VNAA0310015 120031021A3350321473 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07427JS194842967 3039 THE CREW REPORTED THAT THE EMERGENCY LIGHTING FAILED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031209001152003120900115NM 2003 12 9 VNAA0310017 120031022A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07429JS15725190 3043 THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AND BOARDING LIGHTS FADE. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RLEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031209001282003120900128NM 2003 12 9 QXEA200301336 120031009A5310 DOOR FRAME DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 WEB CHAFED ABOVE BAG DOOR CUTOUT AT FRAME X564.5. REPAIRED IAW RD 8-53-5461. 2H72 4T RTA13NM 20031209001292003120900129NM 2003 12 9 QXEA200301340 120031008A5753 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 CHAFE MADE ON RIGHT HAND OUTBOARD FLAP, FORWARD OF TRAILING EDGE. REPAIRED IAW DHC-8-200 RD8-57-1738. 2H72 4T RTA13NM 20031209001382003120900138NM 2003 12 9 QXEA200301341 120031015A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 RT OUTBOARD TRACK NR 12 SEAT ATTACH AREA CORROSION ON TOP AT APPROXIMATELY X518.00. REPAIRED IAW RD 8-53-3644. 2H72 4T RTA13NM 20031204001402003120400140EA 2003 12 4 COMA0360461 120031016A2710600908002 PULLEY CNDAIRCL600 CL6002B19 1900309EA AILERON CONTROL FROZEN A COMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01735CA 7267 FLIGHT 5530 AILERON CONTROLS BINDING, THEN BROKE FREE AT 6000 FT. REPLACED FROZEN CONTROL PULLEY IN LEFT WING. 2L72 4F RTA21EA 20031204001582003120400158EU 2003 12 4 MALA030465 120030929A5753 SLEEVE BAC 146 AVRO146RJ85A1500097EU FLAP TRACK CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, FOUND RIGHT FLAP, POSITION TRACK NR 2 AFT LINK FWD O/B SLEEVE CORRODED. FOUND RIGHT FLAP, POSITION TRACK NR 4 AFT LINK, AFT O/B BUSHING CORRODED. MAINTENANCE REPLACED IAW EO AD020307. REFER TO 409 189965, 189966 FOR ADDITIONAL DETAIL. 2H74 4F RTA49EU 20031204001872003120400187EU 2003 12 4 MALA030470 120031001A5753 BOLT BAC 146 AVRO146RJ85A1500097EU FLAP CARRIAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, RT FLAP NR 2 CARRIAGE BOLT IS CORRODED (AFT ATTACH BOLT). MAINTENANCE REPLACED CARRIAGE BOLT IAW AD 020307. A/C RELEASE DATE 10/12/2003. REFER TO 189984 FOR ADDITIONAL INFORMATION. 2H74 4F RTA49EU 20031205000432003120500043NM 2003 12 5 DL733030933 120031018A215020405011 ACM BOEING737 7373B7 1384580NM LT AC BAY FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27951WP 464676 22951 ON CLIMBOUT FROM SLC UNABLE TO MAINTAIN PRESSURIZATION ON ONE PACK - LT PACK ON MCO FOR LOW FLOW - HISTORY ITEM. REPLACED LT ACM AND ACM DISCHARGE TEMP SW, RAN PACK CK GOOD. PRESSURIZED A/C CK GOOD. 2L72 4F RTA16WE 20031208000792003120800079WP 2003 12 8 ABXA030394 120031023A793141800141 TRANSMITTER DOUG DC8 DC863 302198AWP PWA JT3D JT3D3B 52039NE NR 4 ENG OIL DEFECTIVE A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23825AX 93 46115 669202 NR 4 ENGINE OIL PRESSURE INDICATED + 100 PSI AT TOP OF CLIMB. SECURED ENGINE AT 0325Z, RETURNED TO 22 PSI AT 0345. REPLACED NR 4 OIL PRESSURE TRANSMITTER, NR 4 OIL PRESSURE RELIEF VALVE AND MAIN ENGINE OIL FILTER. RAN NR 4 ENGINE, OIL PRESSURE AT IDLE 41 PSI AND 50 PSI AT POWER. LEAK AND OPS CHECKED GOOD IAW DC-8 MM. 2L74 4F4 F 4A25 1E8 20031208000962003120800096NM 2003 12 8 QXEA200301328 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - LEFT OUTBOARD TRACK NR 1 SEAT ATTACH AREA CORROSION UNDER INBOARD AND OUTBOARD LUGS, APPROXIMATELY X393.00. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20031208001122003120800112NM 2003 12 8 AWXA200301310 120031007A53476573746 SEAT TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK CORROSION WAS FOUND ON UPPER FLANGE OF SEAT TRACK AT LBL 45, BS 540 TO 727. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT SEAT TRACK AT LBL 45, BS 584.5-596.5; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-52 FIG 206. 2L72 4F RTA16WE 20040123000102004012300010WP 2004 1 23 ASAA0380693 120031027A53135962776 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD END AT FS 237. REPLACED DAMAGED SECTION WITH SPLICE REPAIR PER SRM 53-02. (M) 2L72 4F RTA6WE 20040123000242004012300024EU 2004 1 23 KBM2003F00103 120031113A6720704A34130184 CONTROL CABLE SNIAS 350 AS350BA 8680817EU TAIL ROTOR BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH7090 2337 TAIL ROTOR CONTROL CABLE FEELS ROUGH AND BINDING. REPLACED WITH NEW TAIL ROTOR CONTROL CABLE. 1G71 3U NCH9EU 20040123000312004012300031WP 2004 1 23 MEX2003527 120031119A324261791 VALVE DOUG DC9 DC983 3022083WP NR 3 BRAKE SYS CRACKED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23838AM 49397 AIRCRAFT RETURNED TO PLATFORM DUE TO, DURING TAXI, THE (RT HYD PRESSURE LOW) LIGHT TURNED ON AND RIGHT HYD QTY DROPPED TO ZERO. DURING INSPECTION OF NR 3 BRAKE SYSTEM, LOCKOUT VALVE WAS CRACKED. VALVE WAS REPLACED IAW MM 32-42-06, TEST CORRECT. 2L72 4F RTA6WE 20040126000302004012600030 2004 1 26 HEEA087796 420030619A2350A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 INTERPHONE BOX ICS GOES MUTE. SHOP REPAIR. 1G72 3U H1NE 20040126000412004012600041SW 2004 1 26 ERAA091810 120030602A6210412015300109 BLADE BELL 412 412 1182202SW FUSELAGE DAMAGED B ERAAO OTHER O OTHER NRNOT REPORTED 1 SW03419EH11542 UNABLE TO TRACK, DIVES OVER 40 KNOTS WITH ANY ADJUSTMENT. SENT FOR REPAIR. INSPECTED, PERFORMED 2500 HOUR INSPECTIONS IAW BHT-412-MM CHAPTER 5: XRAY INSPECTION OF TRAILING EDGE CORE IN AREA OF OB TRIM TAB REVEALS APPROX 50-75 CELLS OF MOISTURE INGRESSION IAW ASTM E 94; MOISTURE REMOVED; REPLACED OB AND CENTER TRIM TABS IAW 204-099-223 APPENDIX B SECTION 2 PARAGRAPH 2.7 REV L; REPAIRED SKIN DAMAGE ON UPPER SURFACE AT STA 194.125 TO STA 195.250 INCLUDING DAMAGE UNDER TRIM TAB IAW DAL-637 AND 8110-26727; REPLACED IB SPLICE COVER IAW BHT 412 CR AND O PAGE 86B; REMOVED AND REINSTALLED TIP CAP IAW 8110-38493 AND CTI PROCEDURE 412-62-10-800. 1G72 4U H4SW 20040126000572004012600057EU 2004 1 26 BAQA091483 120031210A65407052A3632279 CHIP DETECTOR UROCOPEC135 EC135T1 5620026EU T/R GEARBOX LOOSE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135LC66 0296 CHIP DETECTOR STAKE IN PLUG LET GO ALLOWING CONNECTOR END TO ROTATE. ERIC SAID TO SCRAP ON SITE. FAX SCRAP CERT. AND MMIR TO HIM. THIS WAS DONE 12/10/03. 1G72 3U H88EU 20040122000062004012200006EA 2004 1 22 SWIA200312726 120031224A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 PAX DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE INSTALLED IAW CRJ MM 52-11-03-400-802. 2L72 4F RTA21EA 20040122000542004012200054EA 2004 1 22 ASOA03645 120031213A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING HANGAR MAINTENANCE, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122000632004012200063EA 2004 1 22 ASOA03648 120031214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING A C-CHECK, THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040122000652004012200065NE 2004 1 22 ASOA03642 220031212A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT FAILED A E ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO11828AS 7213 DURING DESCENT, AT APPROX 24,000 FT THE CREW HEARD A LOUD POP FOLLOWED BY A VIBRATION INDICATION ON THE RT ENGINE GAUGE. QRH PROCEDURES WERE COMPLIED WITH. THE CREW REDUCED RT ENGINE POWER TO BELOW FIFTY PERCENT AND THE VIBRATION SUBSIDED. AN EMERGENCY WAS DECLARED AND THE CREW PERFORMED A TWENTY DEGREE FLAPS APPROACH AND LANDING. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. BUSED ON THE TEAR DOWN REPORT RESULTS, IT WAS CONCLUDED THE ENGINE SUSTAINED FOREIGN OBJECT DAMAGE FROM THE INGESTION OF ICE. THE ENGINE IS BEING REPAIRED AND WILL RETURN TO SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040123000022004012300002WP 2004 1 23 ASAA0380698 120031028A53475936663503 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15 CHECK, FOUND AFT CARGO BAY CARGO TRACK IS CORRODED AROUND CLIP NUT HOLES AT FS 1231. REPLACED CARGO TRACK PER SRM 50-31-1. (M) 2L72 4F RTA6WE 20040123000182004012300018EA 2004 1 23 A6WA200340201 120031227A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 LT WING LOWER SKIN PLANK HAS CORROSION AT PANEL OPENING 540CB, FORWARD AND AFT OF PANEL OPENING. PERFORMED A MAJOR REPAIR BY BLENDING OUT CORROSION AND TREATING METAL IAW REO 601R-57-21-030. (M) 2L72 4F RTA21EA 20040126000012004012600001EU 2004 1 26 BAQA091880 120031228A6320L633M2010101A004MOUNT UROCOPEC135 EC135P1 8680990EU MAIN ROTOR DISCHARGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH214 0069 MAIN ROTOR MOUNT DEPRESSURIZED. PART REPLACED WITH SERVICABLE UNIT. 01/09/2004 1G72 3U O H88EU 20040126000232004012600023EU 2004 1 26 BAQA091997 120031227A6330L633M2010104 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX COLLAPSED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135LC1200 0296 MAIN ROTOR GEARBOX MOUNT COLLAPSED. REPLACED WITH SERVICEABLE UNIT. 01/15/2004 1G72 3U H88EU 20040126000362004012600036SW 2004 1 26 HEEA087820 120030610A6220206011100159 HUB BELL 206 206L1 1182107SW MAIN ROTOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0345RP 14891 45521 M/R GRIP SLINGING GREASE. REPAIRED. 1G71 3U H2SW 20040127001682004012700168WP 2004 1 27 ASAA0380649 120031015A53475934615567 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND SEAT TRACK CORRODED AT 1144-1182. REPLACED DAMAGED SECTION WITH SPLICE REPAIR PER SRM 53-05. (M) 2L72 4F A6WE 20040127001722004012700172WP 2004 1 27 ASAA0380639 120031015A532199366401 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD CRACKED AT FS 889-927. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040127001952004012700195NM 2004 1 27 ASAA0310169 120030320A531165548922 FRAME BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FRAME AT BS 328-344, RIGHT BUTTOCK LINE 30, RIGHT BUTTOCK LINE 30 CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20040127002002004012700200WP 2004 1 27 ASAA0380666 120031015A5313593666717 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND AFT CARGO COMPARTMENT CORROSION IN STRINGER BOTTOM FLANGE 28L STATION 1193-1211. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040127002112004012700211WP 2004 1 27 ASAA0380660 120031015A53204911383U504 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FRAME FITTING CORRODED. REPLACED FITTING. (M) 2L72 4F A6WE 20040127002182004012700218WP 2004 1 27 ASAA0380656 120031015A5347993607331 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FRAME CORRODED. REPLACED FRAME SEGMENT. (M) 2L72 4F A6WE 20040127002302004012700230WP 2004 1 27 ASAA0380642 120031015A5753591955507 HINGE FITTING DOUG DC9 DC982 3022082WP TE FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND LEFT OUTBOARD FLAP HINGE FITTING AT OUTBOARD ACTUATOR POINT BEARING HOUSING IS CORRODED ON INNER SURFACE. REBORED FITTING AND INSTALLED OVERSIZED BUSHING PER OHM 27-50-5. (M) 2L72 4F A6WE 20040127002352004012700235WP 2004 1 27 ASAA0380647 120031015A53219936582503 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK FLOORBOARD IS DELAMINATED AT FS 826-886. REPLACED FLOORBOARD PER SRM 53-04. (M) 2L72 4F A6WE 20040127002362004012700236WP 2004 1 27 ASAA0380657 120031015A531359365151 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND LONGERON CORRODED. SPLICED IN NEW SEGMENT. (M) 2L72 4F A6WE 20040126000272004012600027NE 2004 1 26 HEEA087792 120030620A77007645001076111 INDICATOR SKRSKYS76 S76A 8143006NE COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 T5 INDICATOR, FLUCTUATED AND WENT TO ZERO. SHOP REPAIR. 1G72 3U H1NE 20040126000582004012600058SW 2004 1 26 HEEA087823 120030623A6720 BEARING BELL 206 206L3 1182108SW PITCH LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20040127001472004012700147WP 2004 1 27 ASAA0380679 120031015A534049113832 FITTING DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK - FOUND 15K CHECK, FRAME TO CUSP FITTING IS CORRODED AT FS 1174. REPLACED FITTING PER SRM 51-10-4 AND 51-30-1. (M) 2L72 4F RTA6WE 20040127001672004012700167NM 2004 1 27 ASAA0310171 120030320A5313BAC1498158 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 21L AT BS 1016 CORRODED. REMOVED DAMAGE AND REPAIRED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20040127002222004012700222WP 2004 1 27 ASAA0380671 120031015A532199366481 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS CORRODED INSERTS. REPLACED FLOORBOARD. (M) 2L72 4F A6WE 20040127002552004012700255 2004 1 27 AC2A092340 420030106A2210060002600 GYRO BELL 430 430 1182150SW COCKPIT MALFUNCTIONED B AC2AO OTHER O OTHER CRCRUISE 1 SO07430CT2165 49089 IN CRUISE FLIGHT WITH NR 1 AUTOPILOT ENGAGED THE AIRCRAFT EXPERIENCED AN UNCOMMANDED RIGHT HAND DESCENDING TURN. VERTICAL GYRO REPLACED. 1G72 3U RTH9SW 20040128000062004012800006SW 2004 1 28 HEEA092088 120031124A7797M8372395K1624N CONNECTOR BELL 230 230 1182149SW NR2 OVRSPD CONT CONTAMINATED B HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03911RC 23037 DURING FLIGHT, NR2 ENGINE OVERSPEED LIGHT ILLUMINATED. MAINTENANCE CLEANED OIL CONTAMINATION FROM THE CONNECTOR TO THE NR 2 ENGINE OVERSPEED CONTROL. 1G72 3U NCH9SW 20040128000162004012800016EU 2004 1 28 BAQA092330 120031229A6220 BEARING BOLKMS117 BK117A1 5626010EU ROD END WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1360 7243 MAIN ROTOR ROD END BEARINGS WORN. REPLACED WITH SERVICABLE UNIT. 1G72 3U H13EU 20040128000292004012800029CE 2004 1 28 DXTA200300209 120031223A3246315381 WHEEL CESSNA750 750 2076810CE NLG OUT OF BALANCE E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07904QS 7500210 ON TAKEOFF ROLL AT 80 KNOTS FELT STRONG VIBRATION AT THE NOSE GEAR AREA, ABORTED TAKEOFF. REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES DUE TO OUT OF BALANCE. OPS CHECK GOOD, WORK DONE IAW 750 MAINTENANCE MANUAL CHAPTER 32-41-00. 2L72 4J RTT00007WI 20040128000492004012800049NM 2004 1 28 AWXA200301610 120031205A532065516983 CHANNEL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT SPLICE CHANNEL UNDER STR 21 LT, AT BS 907, LBL 45. MAINTENANCE REMOVED CORRODED SPLICE CHANNEL UNDER STR 21 LT, FROM BS 901 TO BS 913, LBL 45; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, PG 4 & 38. 2L72 4F RTA16WE 20040128000612004012800061EA 2004 1 28 033606311 120031226A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27631BR 7261 DURING INSPECTION THE AFT CEILING EMERGENCY FLOOD LAMP WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040128000642004012800064EA 2004 1 28 QXEA200301582 120031227A3320 ODOR CNDAIRCL600 CL6002C10 1390015EA ROW 5 AB DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09607QX 10024 SBA- FLUORESCENT LIGHT OVER ROW 5AB IS INOPERATIVE. A SLIGHT ELECTRICAL WIRE ODOR WAS NOTICED. INSPECTED INOPERATIVE LIGHTING WITH NO SIGNS OF OVERHEATING FOUND. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040128000732004012800073SO 2004 1 28 C2XA03SH523 120031230A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV-DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040128000752004012800075NM 2004 1 28 ABXA030491 120031226A5610 WINDOW BOEING767 767231 1385131NM COCKPIT STUCK A ABXAK NONE O OTHER ININSP/MAINT 1 GL23707AX 22570 FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED FIRST OFFICER'S WINDOW IAW B767 MM. 2L72 4F RTA1NM 20040128000802004012800080SO 2004 1 28 C2XA03CL216 120031228A4920M4504113A APU EMB 145 EMB145LR 3260212SO AFT FUSELAGE ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2712563 145612 DURING ROUTINE MAINTENANCE A STRONG FUEL ODOR IN THE COCKPIT WAS NOTED WHEN THE APU WAS STARTED. MAINTENANCE RELEASED THE A/C IAW MEL 49-00-00. MAINTENANCE REPLACED THE APU ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040128000832004012800083SO 2004 1 28 C2XA03BT121 120031229A2560 CHARGER EMB 145 EMB145LR 3260212SO FLASHLIGHT OVERHEATED A C2XAK NONE M OVER TEMP ININSP/MAINT 1 SW2713553 145585 CREW REPORTED SMELL IN FORWARD CABIN AREA, INSPECTED FORWARD CABIN AREA AND FOUND FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT CHARGER OVERHEATING. PLACED FORWARD EMERGENCY FLASHLIGHT AND HOLDER ON MEL 25-60-05 CONTROL 037554 CATEGORY-C (CIRCUIT BREAKER FOR FLIGHT ATTENDANTS FLASHLIGHT PULLED). MAINTENANCE REMOVED AND REPLACED FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT UNIT. OPS CHECKED GOOD IAW EMB145 AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040128000842004012800084CE 2004 1 28 364032 120031230A61216014300 SWITCH BEECH 1900 1900D 1154162CE PROP SYNC SYS SPARKS A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA27172MJ UE72 WHEN THE NR 2 FLIGHT DIRECTOR PITCH SYNC BUTTON WAS PUSHED IT CAUSED ELECTRICAL SPARKS. REMOVED AND REPLACED NR 2 FLIGHT DIRECTOR PITCH SYNC BUTTON, SPARKS WHERE CAUSED BY LOOSE BUTTON WHICH SHORTED AGAINST YOKE. 2L72 4T RTA24CE 20040128001022004012800102NM 2004 1 28 AALA20031480 120031229A3350P4010049 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21932AN 29530 DFW DURING OVERNIGHT MAINTENANCE FOUND SEAT MOUNTED EMERGENCY LIGHTS ROWS 7D-11D INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS ROWS 7D-11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040128001092004012800109EA 2004 1 28 SWIA200312703 120031217A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07720SW 7297 UPON GEAR RETRACTION, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. FOLLOWED QRH. GEAR EXTENDED NORMALLY. RETURNED TO AIRPORT. REMOVED AND REPLACED NLG SELECTOR VALVE IAW 32-33-10. OPS CHECK GOOD IAW 32-33-10. 2L72 4F RTA21EA 20040128001172004012800117 2004 1 28 SWIA200312709 420031220A22166225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07268UE8145 8145 120207 INFLIGHT GOT TRIM FAIL LIGHT ON FCP AND AURAL WARNING, PERFORMED QRH PROCEDURE, STILL GOT TRIM FAIL. ELECTRIC TRIM DOES NOT WORK, MANUAL TRIM WORKS FREE AND SMOOTH. REPLACED PITCH TRIM SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-11-00. 2L72 4T RTA31SO 20040128001212004012800121EA 2004 1 28 SWIA200312713 120031223A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07449SW3430 3430 7699 SPOILERON FAULT MESSAGE ON EICAS. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPS AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20040127001542004012700154NM 2004 1 27 ASAA0310220 120030325A52476550904U254 FRAME BOEING737 737298C 1384490NM DOOR LATCH GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND APU ACCESS DOOR LATCH CUTOUT FRAME AT BS 1138, STRINGER 18L GOUGED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20040128001242004012800124SO 2004 1 28 SWIA200312716 120031217A2750 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAPS DIRTY A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07188SW 120039 ON SELECTING FLAPS 45 DEGREES OUTBOARD FLAPS STAY AT 25 DEGREES WITH FLAP DISAGREEMENT LIGHT. FOUND CONNECTOR TO BOTH INBOARD AND OUTBOARD FLAP ACTUATOR TO BE WET WITH DEICE FLUID. CLEANED ALL 4 CONNECTORS. OPS CHECKED GOOD. 2L72 4T RTA31SO 20040128001712004012800171EU 2004 1 28 AWXA200400006 120031224A5411D54530025200 RIB AIRBUS320 A320231 3930325EU NR 2 ENG PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 MCN - MINOR REPAIR - DURING C-02 CHECK A 1.25 INCH CRACK WAS FOUND ON NR 2 PYLON AFT FIXED FAIRING (RIB 12) AT OUTBOARD ANGLE. MAINTENANCE REMOVED CRACKED RIB AT NR 2 PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-10, 12, & 28. 2L72 4F RTA28NM 20040128001792004012800179SO 2004 1 28 LR7A03112 120031231A2422IC25001HCM1629 STATIC INVERTER LKHEED382 382G 526414USO COCKPIT FAILED A LR7AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 AL03404LC 4763 INVERTER FAILED DURING START. ON ENGINE START THE FLIGHT DECK FILLED WITH SMOKE. PROBLEM WAS ISOLATED TO A FAILED STATIC INVERTER. REPLACED ENGINE INSTRUMENT (2500 VA) INVERTER PER SMP581 24-20. 2H74 4T A1SO 20040128001962004012800196NM 2004 1 28 P5CA0401021 120031220A7830 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL THRUST REVERSER ILLUMINATED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23452PA 30810 706201 NR 4 ENG REVERSER STATUS MESSAGE DISPLAYED AFTER LANDING. TRANSFERRED TO DMI 31988 AND MEL 78-31-01 PER DDPG. 2L74 4F4 FRTA20WE E23EA 20040128002022004012800202NM 2004 1 28 DHL200342540 120031124A5754 MOUNT BOEING727 727225 1384077NM KRUGER FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK; N/R60111 NR 5 KRUEGER FLAP ACT MOUNT IS CRACKED INBD 2 PLACES, OTBD 1 PLACE. REMOVED NR 5 L/E FLAP ACT SUPPORT BRACKETS IAW B727 SRM 51-30-02, FABRICATED PER SAMPLE I/B & O/B SUPPORT BRACKETS 7075-T6, .063 PO900226 (6 X 8 INCH) IAW B727 SRM 57-20-02 FIG 1. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-02, INSTALLED BOTH I/B & O/B SUPPORT BRACKETS IAW B727 SRM 51-30-02, OP/LEAK CHECK GOOD IAW B727 MM 27-81-00. 2L73 4F A3WE 20040128002122004012800212WP 2004 1 28 DHL2003809011 120031231A335023661001 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01604AL 46047 DURING BISE CHECK - EMERGENCY LIGHT SWITCH MUST BE RECYCLED ONCE BEFORE EMERGENCY LIGHTS FUNCTION NORMALLY. REMOVED AND REPLACED AIRCRAFT BATTERY, OPS CHECKED GOOD PER DC-8 M/M 24-30-1. 2L74 4F RT4A25 20040129000092004012900009EA 2004 1 29 COMA0360580 120031228A1220 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE OVERSERVICED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING MJWOVER TEMP WARNING INDICATION INADEQUATE Q C CLCLIMB 1 SO01716CA 7250 FLIGHT 5904 RIGHT ENGINE OIL PRESSURE DROPPING AND TEMP INCREASING IFSD. ENGINE WAS OVERSERVICED 6 QTS OF OIL. DRAINED EXCESS OIL. 2L72 4F RTA21EA 20040129000182004012900018EA 2004 1 29 COMA0370058 120031223A3010 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ANTI ICE SYSTEM ILLUMINATED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01391CA 10108 FLT 5213 LT WING ANTI ICE MESSAGE. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20040129000392004012900039EU 2004 1 29 MALA030597 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 13A & 13B FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 13A, 13B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000542004012900054EU 2004 1 29 MALA030586 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 6D, 6E, & 6F FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 6D, 6E AND 6F IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000642004012900064 2004 1 29 SWIA200312736 420031225A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07581SW7078 7078 120349 WHEN BATTERY POWER IS APPLIED, SHAKER OPERATES CONTINUOUSLY ON F/O'S SIDE. REPLACED STALL WARNING COMPUTER AND PANEL. OPS CHECK GOOD. STALL WARNING PANEL P/N: 120-34428-001. 2L72 4T RTA31SO 20040129000822004012900082NM 2004 1 29 DHL200342542 120031121A5320 INTERCOSTAL BOEING727 727225 1384077NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER LOBE INTERIOR STIFFENER BUCKLED AT STA 360 STR 5 R. REMOVED UPPER LOBE INTERCOSTAL BS 360 STR 5 R AS REQUIRED FOR FAB NEW IAW B727 SRM 51-30-02, FABRICATED NEW WEB INTERCOSTAL MAT IDENTIFICATION 7075-T6 .032 PO 991238 DIMENSIONS 19 X 5.5 INCH IAW B727 SRM 53-10-2 FIG 3. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW INTERCOSTAL WEB AT STA 360 STR 5 R IAW B727 SRM 51-40-2. 2L73 4F A3WE 20040129000842004012900084NM 2004 1 29 DHL200342543 120031120A5311 FRAME BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD CORNER AREA WITH DENTS. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABED NEW ONE FROM BAC1503-100274 PO334880 DIM 42 INCHES & SPLICE ANGLE 9 INCHES IAW B727 SRM 51-40-4 FIG 1. CUT OUT DAMAGED WEB & FABBED NEW FROM 7075-T6 .071 DIM 31 X 4.25 INCH PO900242 & 2 EA SPLICE DOUBLERS SAME MAT DIM 8.5 X 4.25 INCH IAW 727 SRM 53-10-2 & 51-40-2 FIG 1. REPAIR PARTS TREATED & PRIMED IAW 727 SRM 51-10-2. INSTALLED IAW 727 SRM 51-40-2 FIG 1 & 51-40-4 FIG 1. 2L73 4F A3WE 20040128000052004012800005SW 2004 1 28 HEEA092086 120031207A7920AS3209114 PACKING BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 1 ENG OIL LEAKING B HEEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW032149S 36002 CPPS63146 DURING CRUISE FLIGHT THE NR 1 ENGINE OIL PRESSURE DROPPED BELOW RED LINE. SHUT DOWN ENGINE AND RETURNED TO BASE. 1G72 4U4 U H4SW E22EA 20030918000652003091800065CE 2003 9 18 DXTA200300077 120030726A323399141693 ACTUATOR CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP MLG INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07713QS2186 6507103 ON APPROACH WHEN SELECTING GEAR DOWN, NO RT MAIN GEAR GREEN LIGHT ILLUMINATED NOSE AND LEFT MAIN NORMAL. TOWER STATED RIGHT GEAR COCKED AND GPWS ' TOO LOW GEAR' DURING FLYBY. ALL CB'S OK. AUX GEAR HANDLE PULLED AND WHEN A/C YAWED RT MAIN LIGHT ILLUMINATED. - REMOVED AND REPLACED RH MLG SIDE BRACE ACTUATOR IAW 650 MM CHAPTER 32-30-04. OPS CHECK AND LEAK CHECK GOOD. 2L72 4F4 F A9NM E6WE 20030918000922003091800092NM 2003 9 18 PCAA0308091 120030804A2611 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM SMOKE DETECTOR FALSE INDICATIONA PCAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA13814EX 318 CREW REPORTED THAT THE SMOKE WARNING LIGHT ILLUMINATED FOR THE CARGO COMPARTMENT. MAINTENANCE PERFORMED A OPERATIONAL TEST OF THE BAGGAGE SMOKE DETECTION SYSTEM IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 MAINTENENCE MANUAL. NO DEFECTS WERE NOTED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030918001352003091800135NM 2003 9 18 XNOA01141 120030806A3260 CONNECTOR BOEING727 727227 1384078NM MLG LOOSE A XN0AO OTHER N FALSE WARNING CLCLIMB 1 GL2376753 21249 AFTER GEAR RETRACTION, RED RIGHT GEAR DOOR LIGHT ON AFTER GEAR HANDLE IN OFF POSITION. AND R GEAR DOOR LT. ON ENGINEER'S PANEL ON. PERFORMED CHECKLIST. LIGHT WENT OUT. CLEANED AND RESEATED CONNECTOR ON RIGHT GEAR DOOR UPLOCK SWITCH IAW B727 MM 32-62-11. GEAR DOORS OPS CHECKS GOOD. 2L73 4F A3WE 20030919000552003091900055NE 2003 9 19 ARWA20030801 220030805A7532563883 BLEED VALVE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE INOPERATIVE A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19441J 45688 671243 COMPRESSOR STALL NR 2 ENGINE COMMENCING THE TAKE OFF ROLL. REJECTED TAKE OFF (RTO). REMOVED AND REPLACED NR 2 PRESSURE RATIO SURGE BLEED VALVE IAW MM 75-30-3. OPERATIONAL CHECK ON RUN UP IAW MM 71-0 FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20030919000572003091900057NM 2003 9 19 C8GA20030019 120030808A361039271611 CLAMP BOEING727 727230 1384080NM CUSTOMER AIR FAILED A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15357KP63548 20675 AFTER TAKEOFF, NR 3 BLEED AIR TRIP LIGHT ON, FOLLOWED BY NR 3 ENGINE STRUT OVERHEAT LIGHT ON. ACCOMPLISHED ABNORMAL PROCEDURES CHECKLIST, AIR TURN BACK AND AC LANDED WITHOUT INCIDENT. A/C WAS INSPECTED AND FOUND CLAMP ON NR 3 BLEED RIGHT SIDE AIR STAIRS AREA LOOSE. TIGHTENED CLAMP AND RAN ENGINE TO 1.6 EPR, LEAK CHECK OK IAW MM. NO OTHER DEFECT NOTED AND AC RETURNED TO SERVICE. FLT 707. ON TAKE OFF ROLL, THE NR 1 AND NR 3 BLEED OVERHEAT LIGHT CAME ON, THE RIGHT PACK TRIP. ABORTED TAKE OFF AND AC RETURNED TO BLOCK. CANCELLED FLIGHT, TROUBLESHOOT AC AND REPLACED THE 13TH STAGE MODULATING VALVE AND THE RIGHT REGULATOR DIFFERENTIAL PRESSURE UNIT IAW MM 36-12-01. AC RETURNED TO SERVICE. 2L73 4F A3WE 20030919000912003091900091GL 2003 9 19 PG92003F00000 220030727A732123065104 FUEL CONTROL BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FLUCTUATES E PG9RE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 WP1990065 284 1572 CAE821275 DURING PART 135 OPS, AIRCRAFT HAD FLUCTUATING N1 IDLE, MAINTENANCE WAS NOTIFIED AND ADJUSTED IDLE. AIRCRAFT WAS THEN SHUT DOWN AND RESTARTED WITH NI IDLE FLUCTUATIONS ACCURING FOR A SECOND TIME. FUEL CONTROL WAS THEN REPLACED AND AIRCRAFT WAS GROUND RAN AND LEAK CHECKED WITH NO N1 FLUCTUATIONS. AIRCRAFT WAS TEST FLOWN AND WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 20030919001102003091900110EU 2003 9 19 AWXA200300921 120030803A5347D53472133200 SEAT TRACK AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON MAIN CABIN SEAT RAIL FR 64-66, Y1292, AT CLIP NUT HOLE JUST INBOARD OF R-2 DOOR GIRT BAR HOLD DOWN FITTING. MAINTENANCE REMOVED MAIN CABIN SEAT RAIL Y1292 BETWEEN FR 64 & FR 66; FABRICATED A NEW REPLACEMENT SEAT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-23-11, PG. 20, AND SRM 51-42-11, PG. 6-7. 2L72 4F RTA28NM 20030919001402003091900140CE 2003 9 19 ACE081603 120030816A3230MS24171D1 RELAY BEECH 1900 1900C 1154161CE HYD POWER PACK CONTAMINATED E YADAO OTHER O OTHER APAPPROACH 1 AL03112AX539 UC45 PILOT REPORTED THAT IT TOOK MULTIPLE ATTEMPTS TO EXTEND THE GEAR WITH THE ELECTRO/HYDRAULIC SYSTEM. GEAR DID EXTEND AND UNEVENTFUL LANDING ACCOMPLISHED IN ANC. MAINTENANCE REPLACED THE HYD. POWER PACK RELAY (HEAVY CONDENSATION). 2L72 4T RTA24CE 20030922000202003092200020EU 2003 9 22 3144070703 120030707A6730SC5083 SERVO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE MAIN ROTOR LEAKING E S4WAK NONE K FLUID LOSS ININSP/MAINT 1 WP075226R2196 3144 22043 MAIN ROTOR SERVO LEAKING. 1G71 3U3 U H9EU E00054EN 20030922000592003092200059CE 2003 9 22 G73A200358G01 120030817A2612 FIRE WARNING LEAR 35 35A 5170602CE RT ENGINE FALSE ACTIVATIONE G73AFEA ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING APAPPROACH 1 NM0958GL 599 CREW EXPERIENCED FIRE WARNING ON RT ENGINE DURING APPROACH. BOTH FIRE BOTTLES FIRED; ENGINE WAS SHUT DOWN WITHOUT CHANGE OF FIRE-WARNING INDICATION. LANDED, WITHOUT INCIDENT. NO EVIDENCE OF ACTUAL FIRE FOUND. AIRCRAFT FLOWN ON SPECIAL FLIGHT PERMIT; FALSE FIRE-WARNING COULD NOT BE DUPLICATED. 2L72 4F A10CE 20030922000602003092200060WP 2003 9 22 ARWA20030804 120030819A3260 PROXIMITY SENSOR DOUG DC8 DC861 3021952WP MLG OUT OF ADJUST A ARWAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO1929UA 46159 DURING FINAL APPROACH, AFTER GEAR EXTENSION, NOSE LANDING GEAR LIGHT DID NOT ILLUMINATED. RETARDING POWER LEVERS CAN'T GET THE AURAL WARNING TO COME ON. EXECUTED GO-AROUND, DURING GO AROUND NOSE LANDING GEAR LIGHT STARTED TO FLICKER. VISUAL INSPECTION OF THE NOSE GEAR DOWN AND LOCK MARKINGS DISPLAYED LOCKED POSITION. FLIGHT LANDED UNEVENTFUL. VISUAL CHECK NOSE GEAR, FOUND ALL OK. ADJUSTED NOSE GEAR DOWN AND LOCK PROX. SENSOR. TESTED SYSTEM AS IAW MM 32-60-0 PAR. 3B, NO GEAR SWING REQUIRED. 2L74 4F 4A25 20030922000932003092200093NM 2003 9 22 03FDEA01436 120030902A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - SEAT TRACK AT STA 755, LBL 8 FOUND CROWN AREA DAMAGED. CORRECTIVE ACTION : SNRM N0379 : MAIN DECK - SEAT TRACK AT STA 755 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL. 1. 2L73 4F RTA22WE 20030922001012003092200101 2003 9 22 BAQA089183 420030910A830070BM013100 GEARBOX BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE ACCESSORY DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP5415 7508 ACCESSORY GEARBOX REMOVED FROM ENGINE DUE TO HIGH OIL CONSUMPTION. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 UNCH13EU E19EU 20030922001092003092200109EU 2003 9 22 I05R089282 120030724A6310350A35109120 COUPLING AEROSPAS355 AS355* EU TRANSMISSION DAMAGED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05557CB345 3431 COUPLING HAS HEAT DAMAGE, REPLACED 1G72 3U H11EU 20030922001312003092200131EU 2003 9 22 AWXA200300963 120030820A2597D30665103 WIRE AIRBUS320 A320231 3930325EU ESCAPE SLIDE BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28620AW338163861 052 PHX - EES - L-2 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE FOUND PINS PULLED FROM CONNECTOR ON L-2 DOOR EMERGENCY ESCAPE SLIDE. REMOVED AND REPLACED L-2 DOOR EMERGENCY ESCAPE SLIDE, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030923000082003092300008EU 2003 9 23 MALA030378 120030812A5330 SKIN SAAB SF340 340B 7860101EU TAIL CONE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15366PX 340B267 DURING 4K INSPECTION IN CWA, RT TAIL CONE UPPER SKIN 1050 HAS A DEEP DENT, 1 DIA AT RT STA 828.25, 20.5 INCH, ABOVE SL1614. MAINTENANCE REPAIRED DAMAGE IAW EO NR S53176. 2L72 4T RTA52EU 20030923000092003092300009NM 2003 9 23 QXEA200301011 120030812A5210D5D592395926001 STRUT DHAV DHC8 DHC8202 2809007NM PAX DOOR STIFF A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09359PH32 514 CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED BOTH CABIN DOOR GAS SPRING STRUTS. DOORS OPEN AND CLOSE SMOOTHLY. AIRCRAFT RETUNED TO SERVICE. 2H72 4T RTA13NM 20030923000172003092300017EU 2003 9 23 RAIA00308215 120030819A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03561HK 41077 EMERGENCY PATH LIGHTS INOP ROWS 1 TO 3. RE-SECURED LOOSE CONNECTION AT LIGHT STRIP. 2L72 4T RTA41NM 20030923000392003092300039WP 2003 9 23 DHL2003604593 120030509A5753 PLATE DOUG DC8 DC873F 302199FWP RT WING TE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING OTBD FLAP FWD UPPER PLATING WORN ON TWO AREAS BETWEEN STA XF 213.000 TO XF 201.500 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030507, ED-3281. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN SEGMENT (2024-T3 AL0.040) AND A SPLICE STRAP (2024-T3 AL0.050) IAW EODHL-030507, ED-3281. CLEANED, TREATED AND PRIMED NEW SKIN SEGMENT INTERIOR SURFACE AND THE SPLICE STRAP IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SEGMENT AND SPLICE STRAP ON RT WING OTBD FLAP FWD UPPER PLATING, STA XF 213.000 TO XF 201.500 USING NEW FASTENERS IAW EODHL-030507, ED-3281 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000452003092300045WP 2003 9 23 DHL2003604725 120030619A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP EMERGENCY EXIT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 SECTION AROUND EMERGENCY EXIT DOOR AFT LOWER JAMB HAS TWO CRACKS OF 0.750 AND 0.500 AT STA. 415.250 BETWEEN L-19L AND L-22L PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM. PERFORMED STOP HOLE ON CRACKS END USING A 0.250 DIA. DRILL AND TRIMMED OUT THE CRACK DAMAGE OF THE OUTER PLATING. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, A REPAIR TRIPLER AND A FILLER, CLEANED, TREATED AND PRIMED APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR DOUBLER, TRIPLER AND FILLER ON THE OUTER PLATING OF EMERGENCY EXIT DOOR AFT LWR. JAMB USING NEW FASTENERS IAW SRM. 2L74 4F RT4A25 20030923000502003092300050WP 2003 9 23 DHL2003604758 120030628A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT ELEVATOR UPPER PLATING CTR. SECTION HAS DENTS FROM XE. 132.000 TO XE. 246.000 PERFORMED MAJOR REPAIR IAW EODHL-030525, ED-3276. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030525, ED-3276. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL (2024-T3 AL0.032) IAW EODHL-030525, ED-3276. CLEANED, TREATED AND PRIMED NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN PANEL ON RT ELEVATOR UPPER SURFACE CTR. SECTION (FROM STA. XE.132.000 TO XE.246.000) USING NEW FASTENERS IAW EODHL-030525, ED-3276, SRM 51-1-21 PG.1. SEE N/R 4037 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20030923000552003092300055WP 2003 9 23 DHL2003604661 120030608A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING CTR L/E LWR EXTERNAL SKIN SHOWS CORROSION, XFS 341.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT DAMAGED SKIN SECTION IAW EODHL-030531, ED-3304. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6 AL0.063) AND DOUBLER (7075-T6 AL0.071) IAW EODHL-030531, ED-3304. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL-030531, ED-3304, SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000712003092300071WP 2003 9 23 DHL2003604598 120030524A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING OTBD EXTENDED L/E OUTER PLATING LOWER SURFACE CORRODED AROUND STA XFS 710.000. REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED SKIN AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063), A FILLER (7075-T6 AL0.050) IAW EODHL-030554, ED-3315. CLEANED, TREATED AND PRIMED DOUBLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER ON LT OUTER WING EXTENDED L/E OUTER PLATING LOWER SURFACE, AROUND STA XFS 710.000 USING NEW FASTENERS. 2L74 4F RT4A25 20030922000302003092200030EU 2003 9 22 AWXA200300928 120030815A3350321452 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 241 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW44809 65 DURING INSPECTION LT OVER WING SLIDE LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL) AT LT OVER WING EXIT IAW AMM SUB TASK 33-51-38-400-001, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030922000362003092200036EU 2003 9 22 RAIA00307202 120030729A3222D56797 AXLE AEROSPATR42 ATR42300 8680920EU MLG BROKEN A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03426TE 228 LT FRONT WHEEL CAME OFF. MAINTENANCE DISCOVERED NOSE WHEEL AXEL BROKEN, REMOVED AND REPLACED AXLE AND BOTH NOSE TIRES. 2H72 4T RTA53EU 20030923000442003092300044WP 2003 9 23 DHL2003604602 120030524A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING EXTENDED L/E OTBD. VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA. XOLDI 67.000 PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED EXISTING INTERIM REPAIR AND FILLER. TRIMMED OUT DAMAGED SKIN AREA IAW EODHL-030545, ED-3302. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED EXTERNAL DOUBLER (7075-T6 AL0.071) AND INTERNAL DOUBLER (7075-T6 AL 0.050) AND FILLER (7075-T6 AL 0.063) IAW EODHL-030545, ED-3302. CLEANED, TREATED AND PRIMED INNER SIDE OF INTERNAL/EXTERNAL DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED INTERNAL/EXTERNAL DOUBLER AND FILLER WITH NEW FASTENERS IAW SRM. 2L74 4F RT4A25 20030923000842003092300084WP 2003 9 23 DHL2003604785 120030617A531146110671 FRAME DOUG DC8 DC873F 302199FWP BULKHEAD CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD CARGO COMPT PRESSURE BULKHEAD FRAME CORRODED STA 70.000, L-28L - L-32L. REMOVED FASTENERS AND ATTACH FITTING (04 EA). REMOVED CORROSION ON FRAME STA.70.000, L-28L - L-32L, FOUND OUT OF LIMITS. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED REPAIR ANGLES (02 EA) (301 0.500H STEEL 0.050). FABRICATED ATTACH FITTINGS (04 EA). PERFORMED LIQUID PENETRANT INSPECTION TO NEW FITTINGS. CLEANED, TREATED AND PRIMED NEW FITTINGS. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR ANGLE AND NEW ATTACH FITTING WITH NEW FASTENERS IAW EODHL-030510, ED-3380, EODHL-030571, EODHL-030572, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923001002003092300100WP 2003 9 23 DHL2003604671 120030527A551037014271 ATTACH FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT HORIZONTAL STAB. FITTING WITH 1.000 CRACK IN IT AT FWD. LWR. SECTION STA. XFS.60.000. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1, SRM 51-1-20D PG.9,21, SRM 51-1-21 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1. SRM 1-1-20D PG.21. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9 2L74 4F RT4A25 20030923001032003092300103WP 2003 9 23 DHL2003604675 120030708A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT CARGO COMPT. DOOR NR 4 FRAME ANGLE BROKEN, STA.1440.000. REMOVED BROKEN ANGLE IAW SRM 51-3-0 PG.1. FABRICATED NEW ANGLE (2024-T3 AL0.040) IAW SRM 53-2-0 PG.1-2. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-0 PG.1 2L74 4F RT4A25 20030923001182003092300118WP 2003 9 23 DHL2003604672 120030625A5751 SKIN DOUG DC8 DC873F 302199FWP LT AILERON DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT IB AILERON LWR SURFACE WITH INTERIM REPAIR BETWEEN STA.XA441.000 AND XA.502.000. PERFORMED MAJOR REPAIR IAW EODHL-030569, ED-3399. REMOVED FASTENERS AND DAMAGED SKIN SEGMENT INCLUDING INTERIM REPAIR IAW SRM 51-1-21 PG.1. FABRICATED NEW SKIN SEGMENT (2024-T3 AL0.050) AND SPLICE STRAP (2024-T3 AL0.050) IAW EODHL-030569, ED-3399. CLEANED, TREATED, AND PRIMED AREA AND INNER SIDE OF SKIN SEGMENT AND SPLICE STRAP IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TIO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN SEGMENT AND SPLICE STRAP WITH NEW FASTENERS IAW EODHL-030569, ED-3399, SRM 51-1-21 PG.1. REFER TO N/R 2199 FOR WEIGHT AND BALANCE. FOR REMOVAL AND REINSTALLATION SEE J/C 8-27-11-020 2L74 4F RT4A25 20030923001212003092300121WP 2003 9 23 DHL2003604700 120030527A575157630902 SUPPORT FITTING DOUG DC8 DC873F 302199FWP RT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT INBD AILERON INBD SUPPORT FITTING ASSY AT STA. XA.448.000 WITH 1.000 CRACK IN IT. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 51-1-20D PG.9,21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG.9. 2L74 4F RT4A25 20031208001132003120800113NM 2003 12 8 AWXA200301311 120031010A532069539711 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK 3.1875 INCH CRACK WAS FOUND ON CABIN FLOOR STRUCTURE INTERCOSTAL AT RBL 19, BS 787 TO 807. MAINTENANCE REMOVED THE DAMAGED INTERCOSTAL AT RBL 19, FROM BS 787 TO BS 807; INSTALLED NEW REPLACEMENT SECTION OF INTERCOSTAL IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031208001142003120800114NM 2003 12 8 AWXA200301312 120031009A53206935359 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK 1.125 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL AT RBL 20, BS 767. MAINTENANCE REMOVED THE DAMAGED INTERCOSTAL AT RBL 20, FROM BS 747 TO BS 767; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER B737-300 SRM 53-60-04, FIG 1; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 FIG 2. 2L72 4F RTA16WE 20031208001162003120800116NM 2003 12 8 AWXA200301314 120031002A531265175823 BEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD VERTICAL BEAM (WEB) AT LBL 17.1, WL 230. MAINTENANCE TRIMMED OUT CRACK BS 178 BULKHEAD VERTICAL WEB AT LBL 17.1, WL 230; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED AND INSTALLED BEAM REPAIR PARTS IAW B737-300 SRM 53-10-08 FIG 212 PG 288K-288X. 2L72 4F RTA16WE 20031208001262003120800126EU 2003 12 8 RAIA00310264 120031019A3250190600 CONTROL CABLE JETAIRJETSTMJETSTM4101 1500501EU NLG STEERING BROKEN A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03558HK 41071 NOSE WHEEL STEERING WILL NOT TURN LEFT. MAINTENANCE REMOVED AND REPLACED STEERING CABLE. 2L72 4T RTA41NM 20031208001802003120800180WP 2003 12 8 ABXA030400 120031008A520039178531 DOOR DOUG DC9 DC931 3022065WP BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 AFT PRESSURE BULKHEAD DOOR CRACKED AT LOWER HINGE. REPLACED AREA NOTED IAW DC-9 SRM 52-05, 51-30-5 AND 51-30-1. 2L72 4F A6WE 20031209000152003120900015NM 2003 12 9 PCAA0310130 120031028A33506104781 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAK NONE O OTHER ININSP/MAINT 1 EA13812EX 312 AIRCRAFT 812EX, WHILE IN LGA, ALLEGHENY MAINTENANCE NOTICED DURING CHECK THAT 2 EMERGENCY FLOOR PROXIMITY LIGHTS WERE OUT. MAINTENANCE FOUND ASSOCIATED BATTERY INOP. REMOVED AND REPLACED BATTERY AND SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031209000622003120900062 2003 12 9 SWAA032362 420031026A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED C4 CHECK, FOUND BOTH L1 AND R1 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED SLIDE ASSY'S PER MM. 2L72 4F RTA16WE 20031209000902003120900090NM 2003 12 9 SWAA032356 120031025A575365C263202 SKIN BOEING737 7373T5 1384608NM RT WING TE FLAP BULGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND RT WING OUTBD MID FLAP SKIN BULGED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20031209000972003120900097 2003 12 9 SWAA032317 420031021A2565D31354 SLIDE BOEING737 7373Y0 1384671NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031209001572003120900157NM 2003 12 9 QXEA200301375 120031023A5522 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 300 LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 LIGHTNING STRIKE EXIT ON RIGHT HAND AILERON TOP, 11 INCHES INBOARD OF OUTBOARD SIDE 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED IAW DHC-8 SRM 51-00-06, RD 8-57-2687 AND HORIZON AIR EA 2-57-238. 2H72 4T RTA13NM 20031209001612003120900161NM 2003 12 9 03FDEA01771 120031009A5753ARC0503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LEFT WING O/B FLAP O/B HINGE (WING SIDE) - O/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031209001692003120900169EU 2003 12 9 CX7A194J0353 120031102A26121734362450 FIRE DETECTOR SAAB SF340 340B 7860101EU RT ENGINE MALFUNCTIONED A CX7AEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL03304CE 340B198 RIGHT TAIL PIPE HOT CWP ON IN FLIGHT, SHUTDOWN RIGHT ENGINE CWP WENT OUT. 2L72 4T RTA52EU 20031209001962003120900196EA 2003 12 9 COMA0370046 120031102A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01368CA2349 10075 FS 1098.20 BULKHEAD WEB BETWEEN STRINGERS 8L AND 9L IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031209002022003120900202 2003 12 9 SWIA200312552 420031024A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07250YV7770 7770 120250 AUTOPILOT FAILED AND DISCONNECTED, INTERMITTENT CAPT F/D FLAG AND ERRATIC FD MOVEMENT ON BOTH SIDES. REMOVED AND REPLACED APP-65A IAW EMB 120 MM 22-10-04. OPS CHECK GOOD. 2L72 4T RTA31SO 20031209002032003120900203 2003 12 9 SWIA200312553 420031023A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07268UE7656 7656 120207 FD FLAG ON F/O ADI. CANNOT ENGAGE YAW WITH AP TRANSFER SELECT ON F/O SIDE. REPLACED NR 1 APC-69B AUTOPILOT COMPUTER. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20030923001272003092300127NM 2003 9 23 C8GA20030021 120030821A34110851CM2 PITOT TUBE BOEING727 7272J0 138407ENM EXTERIOR OBSTRUCTED A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15713AA2634 22469 FLT 744 FROM TOL TO MEM. CLIMBING THROUGH 15,000 FT, THE ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT CAME ON IN FLIGHT. ACCOMPLISHED THE APPROPRIATE CHECKLIST, RETURNED TO TOL AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND THE LEFT HAND ELEVATOR PITOT TUBE OBSTRUCTED. REPLACED THE LEFT HAND ELEVATOR PITOT TUBE, PERFORMED SYSTEM CHECKS IAW MM 27-30-105 AND 27-30-0 AND THE ELEVATOR FEEL SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20030923001402003092300140NM 2003 9 23 UPS03M41143 120030506A5753 SKIN DOUG MD11 MD11F 3023600NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 INSPECTION TYPE: C, RT WING, UPPER SURFACE, FWD O/B FLAP FIXED PANEL STA XORS=799 FOUND CORROSION. CORROSION REMOVED AND PROTECTED AT REAR SPAR UPPER CAP AFT LEG FROM ST A XORS 780 TO STA 826 PER SRM 51-21-01 REV 32 VOL II. MATERIAL REMOVED 0.025 INCH, ORIGINAL THK 0.262 INCH, LEAVE THE BLENDOUT AREA 'AS IS' PER EN1014-03 AND UPS REPAIR/ALTERATION AUTH. ENGINEERING FILE NUMBER : MD11-57-20010. 2. HFEC INSP C/OUT ON REWORK AREA, NO CRACK FOUND. 2L73 4F RTA22WE 20030923001432003092300143NM 2003 9 23 NACA20030107 120030813A793142D107A2 PRESSURE SWITCH BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE NR 3 ENG OIL FALSE INDICATIONA NACAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 AL03992AJ1 1 19428 649003 NR 3 ENGINE SHUT DOWN DUE TO OIL FILTER BYPASS/LOW OIL PRESSURE LIGHT ILLUMINATED. INSPECTED FILTER, CHECKED GOOD AND WAS REPLACED. REPLACED LOW OIL PRESSURE SWITCH. OP & LEAK CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20030923001462003092300146 2003 9 23 AWXA200300973 420030823A2565DHE1141 PROXIMITY SENSOR AIRBUSA319 A319132 3930340NM ESCAPE SLIDE DEFECTIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28819AW 1395 FLIGHT CREW REPORTED THE L-2 DOOR SLIDE WOULD NOT ARM FOR DEPARTURE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ARM PROXIMITY SENSOR (7WN1) IAW AMM 52-73-11-401, OPERATIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20030923001532003092300153 2003 9 23 AWXA200300978 420030825A3414 INDICATOR BOEING737 7373B7 1384580NM AIRSPEED INOPERATIVE A AWXACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP28328AW 23377 AS AIRCRAFT PULLED ON RUNWAY AT BUR FOR TAKEOFF FIRST OFFICERS AIRSPEED INDICATOR WAS FROZEN AT 315 KIAS, REJECTED TAKEOFF AND RETURNED TO GATE. CONTRACT MAINTENANCE INSPECTED AND RECYCLED THE FIRST OFFICERS AIRSPEED INDICATOR CIRCUIT BREAKER (C5) ON THE P6-1 PANEL, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030923001572003092300157NM 2003 9 23 AALA20030855 120030813A3350 LIGHT BOEING777 777223 1385213NM CABIN SHORTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21755AN 30263 DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT PROX-LIGHTS IN FORWARD GALLEY AREA INOPERATIVE. REPLACED TWO EMERGENCY EXIT LIGHT ASSEMBLIES IN FORWARD GALLEY ARE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030923001742003092300174 2003 9 23 AALA20030823 420030722A3442TRA7133 TRANSCEIVER BOEING767 767323 1385205NM WX RADAR SYSTEM FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21357AA 24038 WEATHER RADAR DISPLAYED RT WEAK AND THEN WX FAIL BOTH SIDES, RADAR WAS COMPLETELY INOPERATIVE. REMOVED ND REPLACED WX RADAR TRANSCEIVER AS PER MM ACCOMPLISHED REQ'D TESTS, ALL CHECKS NORMAL. (M) 2L72 4F RTA1NM 20030923001842003092300184SW 2003 9 23 2003F00579 120030324A5270 DOOR FRCHLDSA227 SA227DC 3377521SW CLICK CLACK OUT OF ADJUST A BSAAO OTHER J WARNING INDICATION CRCRUISE 1 NM051119K DC830B CARGO DOOR WARNING LIGHT CAME ON WHEN CABIN ALTITUDE WAS ADJUSTED DOWN TOWARD THE END OF CRUISE. CREW DESCENDED AND LANDED DESTINATION AIRPORT. ADJUSTED BOTTOM FORWARD CLICK CLACK PER MM. DOOR OPS CHECK GOOD. (M) 2L72 4T RTA18SW 20030924000022003092400002NM 2003 9 24 QXEA200301018 120030823A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 SCRATCH IN FUSELAGE THROUGH PAINT BELOW FORWARD EDGE OF RIGHT AFT SERVICE DOOR TREAD PLATE. REPAIRED IAW Q400 SRM 51-14-00 TASK NR 350-803. 2H72 4T RTA13NM 20030924000152003092400015 2003 9 24 DL75K030722 420030805A2564D806627 LIFE RAFT BOEING757 757232 1384965NM CABIN DEPLOYED A DALAO OTHER O OTHER TOTAKEOFF 1 SO276703D 30234 FORWARD CABIN LIFE RAFT PARTIALLY INFLATED DURING FLIGHT, CAUSING SOME SHEET METAL DAMAGE TO THE LIFE RAFT COMPARTMENT. REPAIRED COMPARTMENT AND REPLACED RAFT. 2L72 4F RTA2NM 20030924000182003092400018NM 2003 9 24 DLM88030725 120030805A3350110049 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27959DL 49978 ON LAYOVER, FOUND SEAT ROWS 25-30, EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED AFT FLOOR PATH LIGHTING POWER SUPPLY AND BATTERY PACK. 2L72 4F RTA6WE 20030924000252003092400025NM 2003 9 24 DL76L030733 120030808A3350 BULB BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27191DN 28448 1L DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS CHECK GOOD. 2L72 4F RTA1NM 20030924000352003092400035NM 2003 9 24 DL76S030748 120030813A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27133DN 24982 IRREG/ LIGHT OUTSIDE MID LAV (AREA 215) ELECTRICAL BURNING/ BALLAST ODOR. INSPECTED BALLASTS IN AREA AND IFE SYSTEM, NO ELECTRICAL BURNING ODOR. LIGHTS AND IFE SYS OPS OK. NO ODOR IN AREA UPON ARRIVAL. CHECKED ACOVE CEILING PANELS IN AREA AND IN LAV. ALL OK. 2L72 4F RTA1NM 20030924000402003092400040NM 2003 9 24 DL757030753 120030814A5610141T480014 WINDSHIELD BOEING757 757232 1384965NM R-1 FAILED A DALAO OTHER O OTHER CRCRUISE 1 SO27616DL 22823 R1 WINDOW SHATTERED IN FLIGHT. REPLACED SAME. 2L72 4F RTA2NM 20030924000492003092400049NM 2003 9 24 DL73S030763 120030817A335020131A BATTERY PACK BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27320DL 23092 EMERGENCY SEAT LIGHTS ROW 1-16 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS NORMAL. 2L72 4F RTA16WE 20030924000552003092400055NM 2003 9 24 DLM90030770 120030819A2410242010063 CONTROL UNIT DOUG MD90 MD9030 3023690NM NR 1 ENGINE FAILED A DALAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SO27913DN 53393 LT ENG GEN INOPERATIVE REPLACED EPCU AND LT SYS GEN RELAY ELECTRICAL SYS OPS NML. 2L72 4F RTA6WE 20030924000572003092400057NM 2003 9 24 DL764030772 120030819A2752256T63101 ROTARY ACTUATOR BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 3 FAULTY A DALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO27837MH 29710 FLAP DISAGREE ON T/O OUT OF LAX. CREW FOLLOWED PROCEDURES AND CONTINUED TO OGG. IAW OPERATIONS MANUAL A/C WILL REQUIRE A FLAP 20 LANDING. DISPATCH WILL NOT ALLOW A FLAP 20 LANDING IN OGG DUE TO SHORT RUNWAY SO A/C DIVERTED TO HNL FOR MTC. FOUND NR 3 ROTARY ACTUATOR POPPED. RESET IAW M.M. CYCLED FLAP CKS OK. NO FURTHER FAULTS ON FSEU. 2L72 4F4 FRTA1NM E13NE 20030924000612003092400061NM 2003 9 24 DL76G030776 120030822A212121100547238 FAN BOEING767 7673P6 1385105NM RECIRCULATION FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27154DL 25241 GOT LT RECIRCULATION FAN EICAS MSG AND ODOR OF HOT WIRES. SHUT OFF RECIRC FAN AND ODOR WENT AWAY. REPLACED FAN. 2L72 4F RTA1NM 20030924000622003092400062NM 2003 9 24 DL76L030777 120030822A3350BPOS73 POWER SUPPLY BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27184DN 27111 SEAT ROW 21 TO ROW 30 EMERGENCY ESCAPE PATH LIGHTS INOP. T/S FOUND POWER SUPPLY HAS BLOWN FUSE. REPLACED POWER SUPPLY. OPS CKD GOOD. 2L72 4F RTA1NM 20030924000642003092400064NM 2003 9 24 DL76G030779 120030823A2432 CHARGER BA0601 BOEING767 767332 1382001NM FWD AVIONICS BAYOVERHEATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO271603 091312 29695 AT ABOUT 1420 ATLANTA TIME DURING APPROACH A STRONG ELECTRICAL ODOR IN THE COCKPIT. DURING APPROACH WITH A MAIN BATTERY CHARGER STATUS MESSAGE THE SHIPS MAIN BATTERY AND CHARGER WERE VERY HOT AND APPEAR TO BE THE SOURCE OF THE ODOR THE MAIN BATTERY AND CHARGER WERE REPLACED THE STANDBY POWER PANEL WAS REPLACED AS A PRECAUTION. 2L72 4F RTA1NM 20030922000472003092200047SO 2003 9 22 RAAIA00308213 120030816A3230 SQUAT SWITCH EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03822HK 145069 GEAR DID NOT RETRACT MSG AIR TO GRN FAIL, IC 1-2 WOW INOP. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK OF LANDING GEAR SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20030922000812003092200081NM 2003 9 22 AWXA200300958 120030804A5320D53974968200 PROFILE AIRBUSA319 A319132 3930340NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 58, STR 39 L/H - 39 R/H. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 58, STR 39 L/H - 39 R/H; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12, & 22, FIG. 3 & 8. 2L72 4F RTA28NM 20030922000922003092200092EA 2003 9 22 HNAA0300041 120030903A612078249047 PCU DHAV DHC8 DHC8311 1386006EA HAMSTD14SF 14SF23 NE ZONE 400 DEFECTIVE A HNAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA07342 107373334 395 940804 AFTER TAKEOFF APPROX. 300 FT. NR 1 ENGINE TQ WENT TO 137 PERCENT. 2H72 4T RTA13NM 6 CP7NE 20030922000962003092200096NM 2003 9 22 03FDEA01435 120030902A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - SEAT TRACK AT STA 755, LBL 47 FOUND CROWN AREA WORN. DAMAGE SEAT TRACK AT STA 755, LBL 47 REMOVED & REPLACED WITH NEW SEAT TRACK AT STA 765 - 800 LBL AS PER SRM 53-70-00 VOL. 1. 2L73 4F RTA22WE 20030922000992003092200099CE 2003 9 22 2003F00575 120030813A53121144100266 PRESSURE BLKHD BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 CE07139ZV17786 UE139 WHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FORWARD PRESSURE BULKHEAD AT FS. 84, BELOW SELF. THE CRACK RUNS LATERLY 4 INCHES, ON RT LOWER WEB, UNDERNEATH STIFFENER P/N 114-410026-55 (REF BEECH IPC ATA 53-11-00-13 ITEM 240.) 2L72 4T RTA24CE 20030922001252003092200125EU 2003 9 22 B1E2003F00000 120030811A77143038224 SENSOR UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE REDUCTION GB INOPERATIVE E B1EAO OTHER O OTHER NRNOT REPORTED 1 SO17158BC1800 RGB207002 0134 ENGINE NR 2 ENCOUNTERED A FADEC FAILURE AT 50 PERCENT TORQUE DUE TO LOSS OF ELECTRICAL SIGNAL FROM COMPRESSOR TURBINE SPEED SENSOR. REPLACED SENSOR WITH PREVIOUSLY OVERHAULED UNIT WITH 1015.20 HOURS SINCE NEW. OPERATIONAL CHECK GOOD NO OTHER DEFECTS NOTICED AT THIS TIME. 1G72 3U3 UO H88EU E42NE 20030923000012003092300001NM 2003 9 23 QXEA200301005 120030819A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09364PH 524 PSC- FORWARD EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030923000222003092300022WP 2003 9 23 DHL2003604596 120030518A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 UPPER FUSELAGE EXTERIOR SKIN WITH 1.000 CRACK AT STA. 1745.000, L-16R - L-17R. CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-1 PG.99-100. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 PG.99-100. FABRICATED FILLER (7075-T6 0.063) AND INTERNAL DOUBLER (7075-T6 0.040) AND DOUBLER (7075-T6 0.071) IAW SRM 53-2-1 PG.99-100. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER AND INTERNAL DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER AND INTERNAL DOUBLER IAW SRM 53-2-1 PG.99-100, SRM 51-1-20D PG.9, SRM 51-1-21 PG.1 2L74 4F RT4A25 20030923000332003092300033WP 2003 9 23 DHL2003604587 120030610A55404713011503 FITTING DOUG DC8 DC873F 302199FWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RUDDER FITTING ASSY IN RUDDER INNER STRUCTURE CRACKED STA. 104.000 (WATER DRAIN) REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG.1 2L74 4F RT4A25 20030923000432003092300043WP 2003 9 23 DHL2003604748 120030624A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT ELEVATOR OUTER LOWER SKIN HAS DENTS ON SEVERAL SPOTS FROM STA. XE.132.000 TO XE.246.000. PERFORMED MAJOR REPAIR IAW EODHL-030522, ED-3406. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG.1, SRM 51-1-21A PG.4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL (2024-T3 AL0.032) IAW EODHL-030522, ED-3406. CLEANED, TREATED AND PRIMED INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN PANEL WITH NEW FASTENERS IAW EODHL-030522, ED-3406, SRM 51-1-21 PG.1, SRM 51-1-21A PG.3. FOR WIEGHT AND BALANCE SEE N/R 4037. FOR REMOVAL AND REINSTALLATION SEE J/C 8-27-60-016. 2L74 4F RT4A25 20031209002142003120900214EA 2003 12 9 SWIA200312564 120031029A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07406SW995 995 7030 AFTER T/O HAD SPOILERON FAULT AND OUTBOARD GROUND SPOILER FAULT. REMOVED AND REPLACED BOTH SECU'S IAW CRJ MM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20031209002202003120900220NM 2003 12 9 CALA0300616 120031101A5347 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 INSPECTION FOUND A 1 INCH CRACK IN FLANGE ON LT TIE DOWN RAIL AT BS 727D. THE CRACKED SECTION OF TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20031209002352003120900235EA 2003 12 9 COMA0360477 120031103A5330601R5321180 DOUBLER CNDAIRCL600 CL6002B19 1900309EA LT FUSELAGE DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01964CA 7129 PREVIOUS REPAIR OF FUSELAGE SKIN LHS FS 310.00 BETWEEN STR 16-17 HAS SUSTAINED FURTHER DAMAGE DUE TO CONTACT WITH DOOR PINS. PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED REPAIR DOUBLERS AND FILLER. FABED NEW DOUBLERS AND FILLER WITH 2024T3.063 AND 2024T3.050 INSTALLED NEW REPAIR PARTS IAW BOMBARDIER INC REO 601R-53-21-180 REV NC. 2L72 4F RTA21EA 20031209002412003120900241NM 2003 12 9 HNAA0300060 120031031A3350OL3071BPEGPL LAMP DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07940HA 156 EMERGENCY FLOOR LIGHT OUT ON ROW 1. 2H72 4T RTA13NM 20031209002472003120900247NM 2003 12 9 UPS03241528 120031003A3220 FITTING BOEING727 72731C 1384011NM NLG DRAG BRACE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, REPLACED NLG DRAG BRACE FITTING AS PER EO B727-5340-0167. 2L73 4F A3WE 20031209002532003120900253NM 2003 12 9 UPS03241538 120031010A5340652196894 FITTING BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE:C SUSPECT CRACK ON ACTUATOR FITTING I/B LUG I/B FACE BELOW BOLT HOLE AIRSTAIRS ACTUATOR. HFEC CONFIRMED CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-30-02 AND DRAWING 65C13874. BOLT ALSO FOUND WORN, REPLACED IAW 52-62-71. OPS CHECKED SATISFACTORY, RIG CHECKED SATISFACTORY. 2L73 4F A3WE 20031208000682003120800068NM 2003 12 8 AWXA200301289 120031022A3397BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 3 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT, REPAIRED BROKEN WIRE, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031208000972003120800097NM 2003 12 8 QXEA200301329 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - RIGHT INBOARD TRACK NR 8 SEAT ATTACH AREA CORROSION BOTTOM OUTBOARD, APPROXIMATELY X487.00. REPLACED SEAT TRACK. 2H72 4T RTA13NM 20031208000992003120800099NM 2003 12 8 QXEA200301334 120031009A5230 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - TOP FORWARD PRESSURE STOP FITTING FOR BAG DOOR IS WORN APPROXIMATELY .020 INCH. REPAIRED IAW DHC-8 SRM 51-20-26. 2H72 4T RTA13NM 20031208001742003120800174NM 2003 12 8 751PA0027 120031025A5246344N51201 PANEL BOEING757 757200 1384950NM RT WING CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05751PA 23928 RIGHT WING FUELING PANEL HAS CORROSION AROUND QUANTITY GAGE MOUNT SCREWS AND AROUND BONDING JUMPER MOUNT BOLT. REPLACED FUELING PANEL PER MM 28-21-08. 2L72 4F RTA2NM 20031209000482003120900048NE 2003 12 9 P5CA0300974 220031025A7200 ENGINE BOEING747 74747UF 1384949NM GE CF6 CF680C2B6F 30025NE NR 3 SHUTDOWN A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP23496MC 29257 704718 NR 3 ENGINE SHUTDOWN DUE TO NO OIL QTY - FL 350 OIL PRESSURE 45. DURATION OF SHUTDOWN - 45 MINUTES. REMOVED AND REPLACED NR 3 ENGINE PER MM 71-00-00 AND ATLAS MX JOB CARD A71710GTI. ENGINE OPS CHECK GOOD PER MM 71-00-00. 2L74 4F4 FRT1384945 E13NE 20031209000492003120900049NM 2003 12 9 P5CA0300972 120031028A5753 PANEL BOEING747 747283B 1384867NM TE FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RIGHT O/B MID FLAP, I/B LOWER AREA HAS A 12 INCH CRACK IN LOWER PANEL. FIBERGLASS REPAIR CARRIED OUT ON LOWER AREA OF MID FLAP AS PER SRM 51-40-09. 2L74 4F A20WE 20031209000652003120900065 2003 12 9 SWAA032365 420031026A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29716SW 27850 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031209000792003120900079NM 2003 12 9 SWAA032345 120031024A53206551698 SPLICE BOEING737 7373H4 1384600NM STRINGER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE 10R CRACKED AT BS 540. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20031209001142003120900114NM 2003 12 9 VNAA0310014 120031021A3397 WIRE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07463PS 3087 THE CREW REPORTED THAT THE EMERGENCY LIGHT STRIP AT THE GALLEY IS INOP. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE LIGHT STRIP DUE TO A BAD WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031209001712003120900171WP 2003 12 9 ABXA030411 120031014A553199118276 RIB DOUG DC9 DC932 3022066WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20031209001802003120900180NM 2003 12 9 AT0300033 120031030A323039281575001 CYLINDER BOEING717 717200 1383700NM NLG MALFUNCTIONED A ZZDAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15989AT 55152 NOSE WHEEL WOULD NOT RETRACT AFTER TAKEOFF IN ATLANTA. REMOVED AND REPLACED NOSE LANDING GEAR RETRACT CYLINDER PER B717 AMM 32-35-01, NO LEAKS AT THIS TIME. 2L72 4F TRA6WE 20031209002042003120900204 2003 12 9 SWIA200312554 420031025A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07393SW4521 4521 120330 AUTOPILOT FAILED WHEN SELECTED TO CAPTAIN'S SIDE. COMPUTER FLAG SHOWING ON CAPTAIN'S ADI. REPLACED CAPTAIN'S AUTOPILOT COMPUTER. OPS CHECK GOOD PER 22-11-00. 2L72 4T RTA31SO 20031209002082003120900208SO 2003 12 9 SWIA200312558 120030930A5320 BRACKET EMB 120 EMB120ER 3260203SO LT WINDOW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07565SW 120340 BRACKET CRACKED AFT OF LEFT DV WINDOW. REMOVED AND REPLACED SUPPORT BRACKET AFT MIDDLE OF DV WINDOW REF SRM 51-10-02 & 51-40-00 EMB SRM. 2L72 4T RTA31SO 20031209002652003120900265NM 2003 12 9 C1HA200382010 120031105A3350 BATTERY BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15682CA 22019 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES (2EA) FOR EMERGENCY EXIT IAW MM 33-50-71, OPS CHECKS GOOD. 2L73 4F A3WE 20031210000392003121000039 2003 12 10 03FDEA01976 420031121A34142083121 INDICATOR BOEING727 727200 138407ENM COCKPIT MALFUNCTIONED A FDEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO25221FE9771 9771 20932 CAPT`S A/S INDICATOR FAILED AT 80 KNOTS. REJECTED THE T/O. ACCOMPLISHED RTO CHECK LIST ON TAXI BACK, CYCLED THE APP CIRCUIT BREAKER AND IT WORKED NORMALLY. REMOVED AND REPLACED CAPTAIN A/S INDICATOR AS PER 727-200 AMM 34-12-021-4. PERFORMED GROUND TEST AS PER 727-200 AMM 34-12-001-0. TEST ON GROUND OK. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20031210000502003121000050NM 2003 12 10 AALA20031311 120031123A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 MIA THE 1L AND 1R SIDEWALL EMERGENCY LIGHTS INOPERATIVE. REPLACED 1L AND 1R SIDEWALL EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031210000512003121000051NM 2003 12 10 F3LA200300156 120031202A5753 SUPPORT BOEING737 7373L9 1384470NM T/E FLAP BROKEN A F3LAK NONE F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM03312FL 1423 24569 DURING WALK-AROUND, FLIGHT CREW REPORTED NR 7 FLAP TRANSMISSION FLAP TRACK FAIRING A-FRAME ATTACH POINTS BROKEN. REPLACED NR 7 FLAP TRACK FAIRING A-FRAME AND SUPPORT STRUTS, ADJUSTED AND TESTED NR 7 FLAP, AND OPS CHECKED GOOD PER MM 27-51-52 AND OHM 57-53-35. 2L72 4F RTA16WE 20031210000532003121000053SO 2003 12 10 C2XA03SH469 120031123A531514521713003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712528 145504 SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED T-FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031210000652003121000065NM 2003 12 10 03FDEA01973 120031121A302039270811 THERMOSTAT BOEING727 727200 138407ENM ANTI-ICE SYS INOPERATIVE A FDEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25461FE9610 1643 22548 PASSING THROUGH 7500 FT ANTI ICE DUCT OVERHEAT NR 2 LIGHT ILLUMINATED. TEMP WAS FULL HOT 250 DEG C, THEN EXTINGUISHED SHORTLY AFTER (30 SEC) NR 2 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. DUCT OVERHEAT LIGHT ILLUMINATED ONCE AGAIN AFTER LANDING. REMOVED AND REPLACED NR 2 ENG THERMOSTATIC VALVE PER MM 30-21-021-4. RAN ENGINES AT HIGH PWR ANTI-ICE TEMP INDICATION WAS AT 219 DEG C; WELL BELOW 490 DEG C THRESHOLD PER MM 30-21-001-0 WHICH ILLUMINATES THE OVERHEAT LIGHT. 2L73 4F RTA3WE 20031208001722003120800172NM 2003 12 8 751PA0025 120031025A3350 SOCKET BOEING757 757200 1384950NM EMERGENCY LIGHT DISCONNECTED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 FWD THREE FLOOR PATH LIGHTS OUT IN FWD CABIN AND BULB INOP IN LOWER EMERGENCY EXIT LIGHT AT L3 DOOR. RECONNECTED SOCKETS AT 2ND AND 3RD FLOOR LIGHT AND REPLACED SOCKET BASE AT 1ST LIGHT AND REPLACED BULBS IN LIGHT AT L3 DOOR. 2L72 4F RTA2NM 20031209000242003120900024EA 2003 12 9 COMA0370044 120031029A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA2508 10069 FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031209000512003120900051NM 2003 12 9 P5CA0300976 120031028A2822 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C GL NR 4 ENGINE ILLUMINATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23454PA 30812 706485 EICAS MESSAGE, ENG 4 FUEL VALVE, AFTER ENGINE START. CYCLED NR 4 ENGINE FIRE HANDLE PER MM 26-21-00/01, FUEL VALVE RESET. ENGINE WET BLEED, FOUND FUEL VALVE OPERATING NORMALLY. 2L74 4F4 FRTA20WE E23EA 20031209000862003120900086NM 2003 12 9 SWAA032352 120031025A33506104781 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN OVHD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20031209001112003120900111NM 2003 12 9 VNAA0310019 120031022A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07459PS17827282 3070 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 5-10 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031209001202003120900120NM 2003 12 9 AWXA200301334 120031030A33501012623 LIGHT BOEING737 737301 1384611NM SEAT ROW 11 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031209001222003120900122NM 2003 12 9 AWXA200301336 120031023A3150 HANDLE BOEING737 7373G7 1384595NM SPEED BRAKE OUT OF POSITION A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28154AW 23776 ON TAKEOFF AT LAS EN ROUTE FOR SFO TAKEOFF CONFIGURATION WARNING HORN SOUNDED, REJECTED TAKEOFF AND PULLED OFF ON TAXIWAY. RESET SPEED BRAKE HANDLE AND RAN UP THRUST LEVER, NO WARNING HORN SOUNDED. SUBSEQUENT TAKEOFF WAS NORMAL. 2L72 4F RTA16WE 20031209001752003120900175WP 2003 12 9 ABXA030409 120031014A553199118275 RIB DOUG DC9 DC932 3022066WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20031209002562003120900256NM 2003 12 9 UPS03441523 120031017A1430BACB30US8K31 FASTENER BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE:C RIGHT BS 1480 BULKHEAD ONE EACH FASTENER NR 5 WAS CRACKED AT SPLICE FITTING AREA RUNNING AFT APPROX 0.065 INCH LONG. RIGHT BS 1480 BULKHEAD SPLICE FTG NR 5 HOLE OVERSIZED TO 0.625 INCH & HFEC CONFIRMED NO CRACK. REPAIR BUSHING FABRICATED & INSTALLED. NR 5 BOLT REPLACED. THE HOLE DIAMETER & EDGE/END MARGIN REF RS R53-43-35093 & EO B747-5310-19423A. BS 1480 BULKHEAD SPLICE HOLES 1 TO 26 REQUIRED REPEAT INSPECTION EVERY 6000 FLT CYCS PER SB747-53A2390. 2L74 4F A20WE 20031210000952003121000095EU 2003 12 10 MALA030514 120031120A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION PERFORMED BY TIMCO, LAKE CITY, FL CABIN AFT RT FRAME STA 658 GOUGED. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53152. A/C RELEASE DATE 12/2/03. REFER TO 409 1206073 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20031210001052003121000105NM 2003 12 10 03FDEA01995 120031127A5710 STOP FITTING DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP STOP FITTING FOUND CRACK. LT WING OUTBOARD FLAP STOP FITTING CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73349, - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT OUTBOARD FLAP SECONDARY UP STOP REPAIR. 2L73 4F RTA22WE 20031210001152003121000115NM 2003 12 10 AT0300036 120031121A2120 ODOR BOEING717 717200 1383700NM CABIN DETECTED A ZZDAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO15954AT 55016 RIGHT AFTER TAKEOFF A STRONG BURNING SMELL WAS FELT THROUGHOUT CABIN BEING THE STRONGEST IN THE BACK ALL THE WAY TO THE COCKPIT. AIR TURNBACK, LANDING WITH A WEIGHT OF 105100 AT TOUCHDOWN, SMOOTH LANDING. RAN APU, RT AND LT PACKS WITH VARIOUS TEMPERATURES ADJUSTMENTS AND PACKS OP'D TOGETHER, RAN ENGINES AT HIGH POWER FOR 30 MINUTES. PACK TEMPS AND PRESSURES NORMAL. NORMAL SMELL THROUGHOUT THE CABIN, NO ABNORMAL SMELL NOTED. REF 36-10. 2L72 4F TRA6WE 20031210001172003121000117EU 2003 12 10 AALA20031322 120031123A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW211400H 11340 ORD RIGHT HAND FORWARD OVERWING EXIT AND AFT LEFT HAND OVERWING EXIT AND CENTER AISLE OVERWING EMERGENCY EXIT AND LOWER RIGHT HAND FUSELAGE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040122000662004012200066EU 2004 1 22 ASOA03639 120031209A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING HANGAR INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040122001042004012200104EU 2004 1 22 ASOA03603 120031124A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040123000162004012300016WP 2004 1 23 ASAA0380692 120031027A532099367184 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND INTERCOSTAL CORRODED IN AFT CARGO BAY AT FS 1309-1322. REPLACED INTERCOSTAL PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040123000512004012300051NE 2004 1 23 MDR03017 120030612A7120643520278047 SUPPORT SKRSKYS64 S64E 8142604NE RT ENGINE CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09CGESG1381 64065 FIFTH MOUNT FOUND CRACKED BY FIELD CREW. DURING INSPECTION, FIELD CREW VISUALLY NOTICED CRACK IN FIFTH MOUNT SUPPORT FOR THE RT ENGINE. FURTHER INSPECTION OF FIFTH MOUNT SUPPORT SHOWED CRACK BEGINNING IN .500 INCH RADII OF RT RIB, PN 6435-20278-110 EXTENDING 1.700 INCH THROUGH WELD INTO THE TUBE ASSY, PN 6435-20278-115. PROBABLE CAUSE IS A DEFICIENT WELD. 2G72 4U H4EA 20040123000532004012300053 2004 1 23 KBM2003F00101 420031117A34245070020910 INDICATOR SNIAS 350 AS350B1 8680811EU TURN COORDINATORINOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 1140 2009 TURN INDICATOR IS INOPERATIVE. INSTALLED SERVICEABLE TURN CORDINATOR. 1G71 3U H9EU 20040126000122004012600012SW 2004 1 26 HEEA092083 120031231A2913MS21924W4 COUPLER BELL 214 214ST 1182106SW HYD SYSTEM BROKEN B HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0359806 28140 ENROUTE THE OIL COOLER CAUTION LIGHT ILLUMINATED. MAINTENANCE FOUND A UNION BROKEN CAUSING THE LOSS OF ALL HYDRAULIC FLUID. REPLACED UNION AND UTILITY HYDRAULIC PUMP. 2G72 4U H10SW 20040126000322004012600032 2004 1 26 HEEA087827 420030618A3452066011560101 TRANSPONDER BELL 407 407 1182206SW ATC SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 ATC TRANSPONDER FAILS; LOW POWER. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20040128000372004012800037NM 2004 1 28 DHL2003743017 120031227A3350 BATTERY PACK BOEING727 727225 1384077NM EMERGENCY LIGHTSINOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 MAIN ENTRY DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. EMERGENCY EXIT LIGHTS CHECKED GOOD IAW B-727 M/M 33-50-71. 2L73 4F A3WE 20040128000562004012800056NM 2004 1 28 AWXA200301625 120031205A532069353593 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT INTERCOSTAL AT RBL 21, BETWEEN BS 927 AND BS 947. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT RBL 21, BS 927 TO BS 947; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-35359; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8, PG 38. 2L72 4F RTA16WE 20040128001472004012800147EU 2004 1 28 MALA030576 120031228A2920 PTU BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM OVERTEMP A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15536XJ E2372 DURING FLIGHT 3443, YELLOW SYSTEM HI TEMP INFLIGHT. A/C DIVERTED TO DENVER. MAINTENANCE REPLACED PTU. NO OTHER INFORMATION AT THIS TIME. 2H74 4F RTA49EU 20040128001552004012800155EA 2004 1 28 SWIA200312723 120031124A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 700 AFT EQUIPMENT DOOR CUTOUT RT ANGLE CRACKED STR 25R. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35013-12. 2L72 4F RTA21EA 20040128001602004012800160NM 2004 1 28 QXEA200301604 120031218A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- CRACK IN FIREWALL JUST OUTBOARD OF CLOSING ANGLE AND ABOVE FIRE LOOP BRACKET. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-54-806. 2H72 4T RTA13NM 20040128001932004012800193NM 2004 1 28 P5CA0401018 120031230A3610 WARNING LIGHT BOEING747 74746NF 13848BTNM COCKPIT FALSE ACTIVATIONA P5CAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP23450PA 30808 EICAS BLEED NR 4 OVERHEAT / PVT MESSAGE DISPLAYED AFTER START. TRANSFERRED ITEM TO DMI 32027 PER DDG MEL 36-11-8B THRUST REVERSER TRANSFERRED TO DMI 32028 PER DDG MEL 78-31-01. 2L74 4F RTA20WE 20040129000312004012900031EU 2004 1 29 MALA030594 120031218A2520 SEAT BACK BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, ROW 11 SEATS D, E, & F HAVE SEVERAL CRACKS IN THE SEAT BACK AND HEAD REST SEAT F HAS A CRACK IN THE SEAT FRAME AROUND THE WELD. REPAIRED SEATBACKS IAW EO A 25039. REPAIRED HEADRESTS IAW EO A25041 AND REPAIRED SEAT FRAME IAW EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000352004012900035EU 2004 1 29 MALA030587 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 7A & 7B FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 7A, 7B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000912004012900091SO 2004 1 29 MASA200300515 120031227A25604566M37B042NM PBE EMB 145 EMB145LR 3260212SO CABIN OPEN A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ5641 3609 145572 ASH 2695, AFT CABIN PBE REQUIRES REPLACEMENT DUE TO LOSS OF PACKAGE VACUUM. MX REPLACED PBE. 2L72 4T RTT00011AT 20040129000992004012900099NM 2004 1 29 DHL200374245 120031208A5751 RIB BOEING727 727225 1384077NM LT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, LT WING O/B AILERON INTERNAL RIB CRACKED (11TH) FROM O/B. REMOVED AILERON INTERNAL RIB CRACKED 11TH FROM O/B IAW B727 SRM 51-30-2, FABRICATED NEW RIB 11TH FROM MAT 7075-T6 .025 PO 9912281 DIM 14.125 X 5.5 INCH IAW B727 SRM 57-20-2 FIG 8. TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED NEW WEB 11TH IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040130000162004013000016 2004 1 30 SWAA032809 420031224A2565D31354 SLIDE BOEING737 7372H4 138448CNM CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20040130000192004013000019NM 2004 1 30 SWAA032813 120031224A53156546804 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 947, RBL 42, WL 208. REPAIRED DAMAGED AREA PER ER. 2L72 4F RTA16WE 20040130000382004013000038NM 2004 1 30 SWAA032832 120031229A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING FRONT SPAR LEFT AND RIGHT AFT BODY CLEVICES CORRODED. REPAIRED FITTING PER BFG ER. 2L72 4F RTA16WE 20040130000422004013000042NM 2004 1 30 SWAA032797 120031221A3350079123 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29789SW 29816 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD END. REMOVED AND REPLACED TRACK COVER PER MM. 2L72 4F RTA16WE 20040130000452004013000045NM 2004 1 30 VNAA0312013 120031221A2611 SMOKE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY DETECTED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07432JS 3045 THE CREW RECEIVED A LAV SMOKE FAIL INDICATION. THE CREW CYCLED THE CIRCUIT BREAKER AND THE MESSAGE CLEARED, THERE WAS NO EVIDENCE OF SMOKE. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040130000852004013000085NM 2004 1 30 DHL2003742564 120031123A5310 DOOR FRAME BOEING727 727225 1384077NM E/E BAY CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, MAIN E&E COMPARTMENT DOOR CUTOUT FWD FRAME CORRODED/EXFOLIATED 100 PERCENT MATERIAL LOSS BS 424, BL 0-RBL 5 WL 150. REMOVED FASTENERS FOR ACCESS AS REQUIRED, FABRICATED NEW FWD FRAME IAW B727 SRM 51-30-2, FABRICATED NEW FWD FRAME AT BS 424 BL 0 RBL 5 WL 150 MAT USED 7075-T6,.040 PO 9912620 DIM 23.75 X 7 INCH IAW B727 SRM 53-10-8 FIG 3 AND 51-40-2. ALODINE AND PRIME IAW B727 SRM 51-10-2. INSTALLED NEW FWD FRAME IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040130000892004013000089NM 2004 1 30 DHL2003742568 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER FUSELAGE EXTERIOR SKIN BS 390 BETWEEN 6TH LEFT AND 7TH SKIN IS DENTED. DENT AT BS 390 STR 6L TO STR 7L FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA DIM 3 X 2 INCH IAW B727 SRM 53-30-3 FIG 3. REMOVED PREVIOUS REPAIR FOR INCORPATION INTO NEW REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER, DIM 25 X 12 INCH, USING 2024-T3 .050 PO 900408 IAW B727 SRM 53-30-3 FIG 3. ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR AT BS 390 STR 6 TO 7L IAW B727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20040128001282004012800128SO 2004 1 28 LR7A03111 120031204A5531 LONGERON LKHEED382 382G 526414USO VERTICAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 5025 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND FS 902 DORSAL FIN LONGERON CRACKED AT LBL 13 & RBL 13, WL 285. REPAIRED IAW LAC MEA 382-53-03-076. NR 2054. 2H74 4T A1SO 20040128001442004012800144NM 2004 1 28 QXEA200301597 120031229A5753 STRUCTURE DHAV DHC8 DHC8202 2809007NM TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH12058 513 PDX - MAINTENANCE FOUND A HALF-INCH PUNCTURE IN THE HONEYCOMB STRUCTURE OF THE LEFT OUTBOARD FLAP. THE FLAP WAS REPAIRED IAW EA-2-57-246. 2H72 4T RTA13NM 20040128001502004012800150NM 2004 1 28 QXEA200301599 120031218A5711 SPAR DHAV DHC8 DHC8202 2809007NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- RIGHT HAND LEADING EDGE LOWER FORWARD SPAR HAS CHAFE DAMAGE AT INBOARD END, 3 INCHES LONG AT WING STATION YW57.000. REPAIRED IAW DHC-8 RD8-57-811 AND SRM 51-20-26. 2H72 4T RTA13NM 20040128001562004012800156EA 2004 1 28 SWIA200312724 120031124A5320 CHANNEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 NR 2 HYDRAULIC MANIFOLD SUPPORT CHANNEL FS 718 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CHANNEL IAW CRJ REO 601R-53-62-031 REV NC. P/N: 2024T3. 2L72 4F RTA21EA 20040128001582004012800158EA 2004 1 28 SWIA200312731 120031228A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA H/STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 STAB TRIM CH 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW CRJ MM 27-41-01. OPS CHECK NORMAL. S/N OFF: 1057. 2L72 4F RTA21EA 20040128002042004012800204WP 2004 1 28 UPS04841679 120031219A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 685. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040128002092004012800209WP 2004 1 28 UPS04841684 120031229A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LT WING L/E UPPER RIBS ARE CRACKED AT XFS 635, XFS 641.25, XFS 647.5, XFS 653.75, XFS 660. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATED CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040129000362004012900036EU 2004 1 29 MALA030592 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 9D & 9F FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 9D, 9F IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000562004012900056NM 2004 1 29 MWEA030501 120031230A3260891901 SQUAT SWITCH BOEING717 717200 1383700NM ZONE 700 INOPERATIVE A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31908ME 55172 PROXIMITY SENSING ELECTRONIC UNIT FAIL ON STATUS CONFIGURATION PAGE, ASSOCIATED SPOILER FAULT ON STATUS PAGE, AND AUTOMATIC BRAKE SYSTEM FAIL ON CENTRAL FAULT DISPLAY. REMOVED AND REPLACED LEFT WEIGHT ON WHEELS SENSOR. 2L72 4F TRA6WE 20040129000652004012900065 2004 1 29 SWIA200312737 420031228A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLT CONTROL MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07589SW6007 6007 7072 F/O'S FD FAIL MESSAGE. AP KICKS OFF IN FLIGHT ALONG WITH YD NR 2. AP DOES NOT RE-ENGAGE. REMOVED AND REPLACED THE NR 2 FCC 4000 IAW AMM 22-12-14. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040129000872004012900087WP 2004 1 29 0402 220031230A7261 SEAL LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP SCAV LINE LEAKING E BSYAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07701AS 047 P74216 RIGHT ENGINE LOST OIL PRESSURE, SHUT ENGINE DOWN AND DIVERTED TO LITTLEROCK. FOUND OIL LEAK NR 6 BEARING SCAVANGE LINE SEAL LEAKING. REMOVED AND REPLACED ASSOCIATED O-RINGS AND GASKETS, OPS CHECKS GOOD. 2L72 4F4 F A10CE E6WE 20040129000902004012900090 2004 1 29 P5CA0401024 420031231A3140 WARNING LIGHT BOEING747 74747UF 1384949NM EICAS FALSE INDICATIONA P5CAR AUTOROTATION J WARNING INDICATION TXTAXI/GRND HDL 1 WP23496MC 29257 ON PUSHBACK ACARS DIDN'T BLOCK OUT. SENSORS INDICATED DOOR OPEN. EICAS INDICATED DOOR CLOSED. ALL DOORS CYCLED AND PHYSICALLY CHECKED CLOSED, EICAS INDICATED ALL DOORS CLOSED. 2L74 4F RT1384945 20040129001352004012900135EA 2004 1 29 COMA0470003 120031231A3260895304 PSEU CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01391CA1211 10108 FLIGHT 5299 GEAR DISAGREE WARNING DURING CRUISE. REPLACED THE PSEU. 2L72 4F RTA21EA 20040130000202004013000020NM 2004 1 30 SWAA032814 120031224A53136546560 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND CORROSION ON SHEAR TIE BS 947.5, STR 23L AND 24L. REPAIRED SHEAR TIE PER BFG ER. 2L72 4F RTA16WE 20040130000402004013000040NM 2004 1 30 SWAA032795 120031221A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C4 CHECK, FOUND 3 INCH LONG FUSELAGE SKIN CRACK AT BS 747, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040130001092004013000109EU 2004 1 30 MALA030606 120031229A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4Y/2Y INSPECTION IN LCQ, FS 640-686 CENTER SEAT TRACK HAS CORROSION. MX REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060 DATED 3 NOV 2003 REV II. A/C RELEASE DATE 01/09/04. REFER TO 1196389 FOR ADDITIONAL DETAIL. 2L72 4T RTA52EU 20040130001102004013000110EU 2004 1 30 MALA030604 120031222A71209394817 MOUNT SAAB SF340 SF340A 7850100EU ENGINE FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL1598XJ 340A098 AS MAINTENANCE WAS PREPARING TO INSTALL THE ENGINE/PGB ASSEMBLY ON THE LT SIDE OF 098XJ, AFTER INSPECTION THE PGB MOUNTS, NOTICED THE LOWER ONE (-17) HAD FAILED. MX REMOVED THE CANNISTER FROM THE MOUNT AND THE CURE DATE IS DIFFERENT THAT ONES SPELLED OUT IN THE BUILD SPEC. CURE DATES 9801-9825 INCLUSIVE PER AD99-04-07 AND 0214, 0216, AND 0228 PER SB SF 340-71-059. THE CURE DATE ON THIS CANNISTER IS 0239. MX STATED INNER CAN SLID OUT VERY EASY FROM THE OUTER WHEN THE MOUNT BOLTS WERE REMOVED FROM THE OLD MOUNT. TSN 6858:44 TSO: 1947:40. PN/OFF 93948-17, SN/OFF 4056 2L72 4T RTA52EU 20040130001782004013000178NM 2004 1 30 DHL2004752500 120030106A5315 STRAP BOEING727 727223 1384074NM FLOORBEAM CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, CABIN FLOORBEAM SUPPORT STRAP CRACKED AT BS 328 0 (SEEN FROM BELOW). CABIN FLOORBEAM SUPPORT STRAP AT BS 328 BL 0 CRACKED IN HALF OUT OF LIMITS IAW B-727 SRM 53-10-1. FABRICATED REPAIR STRAP FROM 7075-T6 .050 SIZE 2.5 INCH X 8 INCH PO 900489 IAW B-727 SRM 53-10-2 FIG 7 AND 51-40-3 FIG 6. TREATED AND PRIMED PART AND AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR IAW B-727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040129001132004012900113EA 2004 1 29 COMA0460001 120031231A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT & RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01956CA19994 7105 THE LEFT AND RIGHT LOWER WING TANK ACCESS PANEL CUTOUTS HAD CORROSION AT PANELS 640AB, 640CB, 640DB, 640FB, 640BB, 540BB, 540FB, 550AB AND 550BB. REMOVED CORROSION AND RESTORED THE FINISH IAW REO 601R-57-21-030 REV C. 2L72 4F RTA21EA 20040130002382004013000238EU 2004 1 30 MALA040104 120031227A5310 DOOR FRAME SAAB SF340 340B 7860101EU COCKPIT DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, FS 225 COCKPIT DOOR LOWER FRAME CORRODED. REMOVED CORRODED SECTION OF DOOR FRAME FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW MESABA EO S53190. REFER TO NR 1195871 FOR ADDITIONAL INFO. A/C RELEASE DATE 01/06/04. 2L72 4T RTA52EU 20040202000312004020200031CE 2004 2 2 57708 120030107A32331143800419 ACTUATOR BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER APAPPROACH 1 CE07126YV UE126 APPROACH, L/G HANDLE MOVED TO LWR GEAR, RED INTRANSIT LAMPS FLICKERED, 5-AMP L/G IND ON RT C/B PANEL POPPED. L/G EXTENDED, 3 GEAR DOWN LIGHTS FAILED TO ILLUM, WOULD NOT RESET. TOWER VERIFIED NOSE L/G EXTENDED. MALFUNCTION NOT DUPLICATED ON GROUND. L/G IND CB, A316 TIME DELAY PCB, & L/G HANDLE LAMPS REPLACED. TEST FLT FAILED. L/G IND CB POPPED & PWR PACK LOST POWER, MANUAL EXTENSION FOR LANDING. THE 60-AMP PWR PACK MOTOR (CB11) CB FOUND POPPED. RESET, GEAR EXTENDED. PROBLEM NOT DUPLICATED ON GROUND. LT MLG UPLOCK SWITCH & L/G UP/DOWN HANDLE ASSEMBLY REPLACED. TEST FLT FAILED. L/G IND POPPED, PWR PACK MOTOR (CB11) DID NOT. LT MLG ACTUATOR P/N: 114-380041-9 & ASSOCIATED HARDWARE REPLACED. 2L72 4T RTA24CE 20040130000732004013000073NM 2004 1 30 DHL2003742571 120031120A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, LOWER FUSELAGE EXTERIOR BS 277 TO 178 AREAS SKIN DEEP BLEND OUTS STR 25R TO 26R. STRIPPED PAINT IAW B-727 MM 51-20-01 AND FOUND LIGHTNING STRIKES DRILLED 6 EACH AREAS TO .250 AND INSTALLED FASTENERS IAW B-727 SRM 53-30-3 FIG 20. ONE EACH AREA FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED REPAIR FILLER FROM 2024 T3 .040 PO 90024 DIM 3.75 X .75 INCH AND DOUBLER FROM 2024-T3 .050 PO 900414 DIM 10.25 X 8 INCHES IAW B-727 SRM 53-30-3 FIG 3. BARE METAL AND REPAIR PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED IAW B-727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20040130002022004013000202WP 2004 1 30 ABXA040009 120031125A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 R1 DOOR UPPER FORWARD CORNER HAD A REPAIR THAT DID NOT RESEMBLE REWORK DRAWING SR08530021 OR ENGINEERING SKETCH ES00863. REMOVED DOUBLER AND TRIPLER, FABRICATED DOUBLER REPAIR, PRIMED, ALODINED AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D, 51-1-21A AND REA D853-48469MR. 2L74 4F 4A25 20040202001352004020200135NM 2004 2 2 UPS04541727 120031231A5347 SEAT TRACK BOEING757 75724APF 1384969NM EXPANSION LINK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE: C, CORROSION ON EXPANSION LINK SEAT TRACK BS 880 - 900 LBL 25 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED LINK, FABRICATED AND INSTALLED REPLACEMENT LINK IAW SRM 53-00-52, SRM 51-10-02 & SRM 51-40-02. 2L72 4F RTA2NM 20040130001052004013000105NM 2004 1 30 DHL200374276 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSE SKIN TWO DENTS STA 430 BETWEEN STR 2R AND 3R. MEASURED DENT AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA, DIM 4 X 1.375 INCH AND FABRICATED ONE DOUBLER DIM 14 X 9.5 INCH USING 2024-T3 .050 PO 900226 IAW B727 SRM 53-30-3 FIG 1. ALODINE AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040130002132004013000213NM 2004 1 30 ABXA040022 120031113A3231149T695511 FITTING BOEING767 767281 1385109NM RT MLG CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23783AX 23016 RIGHT MAIN LANDING GEAR DOOR RETRACT FITTING CRACKED NEAR RIGHT SIDE KEEL BEAM. REMOVED AND REPLACED BELLCRANK FITTING IAW B767 MM 32-12. 2L72 4F RTA1NM 20040130002272004013000227NM 2004 1 30 AWXA200400040 120031224A5340112N700533 FITTING BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK PITTING CORROSION WAS FOUND ON INBOARD FACE AROUND BORE OF NR 1 ENGINE PYLON OUTBOARD WING SIDE LOAD ATTACH FITTING. MAINTENANCE INCREASED BORE REMOVING CORROSION DAMAGE ON OUTBOARD WING SIDE LOAD ATTACH FITTING; FABRICATED A REPAIR BUSHING PER DWG 112N7005; INSTALLED REPAIR PART IAW AWA ER 19-5704-04008-ES1. 2L72 4F RTA2NM 20040202000782004020200078NM 2004 2 2 AWXA200400049 120031226A5314659187911 SKIN BOEING737 7373B7 1384580NM KEELBEAM DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LCQ - MAJOR REPAIR - DURING C-17 CHECK FASTENERS WERE FOUND PULLING THROUGH KEEL BEAM SKIN, SKIN LOOSE AT BS 724 TO BS 726, RBL 4. MAINTENANCE REMOVED KEEL SKIN FROM BS 661.75 TO BS 726.75; FABRICATED A NEW REPLACEMENT KEEL SKIN PANEL AND 3 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA ER 03-5310-02085-051. 2L72 4F RTA16WE 20040202001402004020200140NM 2004 2 2 UPS04541748 120031231A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE:C, CORROSION ON SEAT TRACK AROUND FASTENER HOLES BETWEEN BS 560 AND BS 620 LBL 26 WL 208. REMOVED CORROSION IAW SRM 53-00-52 FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK PER GOODRICH ER 04-1022. 2L72 4F RTA2NM 20040203000092004020300009WP 2004 2 3 ASAA0380582 120030910A278099375195 CONTROL CABLE DOUG DC9 DC983 3022083WP NR 4 SLAT WORN A K NONE O OTHER ININSP/MAINT 1 NM01973AS 53449 OAK LINE CHECK, FOUND LT NR 4 SLAT CABLE FOUND TO BE WEARING INTO WING LEADING EDGE. REPLACED LEADING EDGE STRUCTURE IAW EA 5740-01361. (M) 2L72 4F RTA6WE 20040203000192004020300019WP 2004 2 3 ASAA0380581 120030910A575499375192 FITTING DOUG DC9 DC983 3022083WP NR 4 SLAT WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01973AS 53449 OAK LINE CHECK, FOUND LT NR 4 SLAT CABLE FOUND TO BE WEARING INTO WING LEADING EDGE. REPLACED LEADING EDGE STRUCTURE IAW EA 5740-01361. (M) 2L72 4F RTA6WE 20040203000242004020300024NM 2004 2 3 ASAA0380589 120030913A33500105603 LIGHT DOUG MD80 MD83 3023681NM ROW 30 INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01982AS 53473 PDX LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED AT ROW 30. RECONNECTED WIRING AT ROW 30. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040203000342004020300034NM 2004 2 3 ASAA0310166 120030320A53206554916 WEB BOEING737 737210C 1384459NM DOOR FRAME CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND MAIN CARGO DOOR WEB AT BS 480, LT BUTTOCK LINE 36 CRACKED. FABRICATED AND INSTALLED REPAIR SRM. (M) 2L72 4F A16WE 20040203000452004020300045WP 2004 2 3 ASAA0380567 120030828A531199360715 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 OAK - DURING C-CHECK, FOUND FRAME CORRODED AT FS 1212 BETWEEN LONGERON 28L AND 29R. REPLACED FRAME IAW SRM 51-30-2 AND 51-30-5. (M) 2L72 4F A6WE 20040203000652004020300065WP 2004 2 3 ASAA0380795 120031119A531359360225 STRINGER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND STRINGER IS CORRODED AT FS 1136-1145. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER IAW SRM 53-02. (M) 2L72 4F RTA6WE 20040203000692004020300069WP 2004 2 3 ASAA0380796 120031119A53109955752419 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FORWARD PAX DOOR UPPER BEAM IS CRACKED AT FORWARD AND AFT CORNERS. REPLACED BEAM IAW SRM 51-30-2. (M) 2L72 4F RTA6WE 20040203000822004020300082WP 2004 2 3 ASAA0380593 120030920A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 ONT PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED AT ROW 6. RECONNECTED WIRING AT ROW 6. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000482004020300048NM 2004 2 3 ASAA0340330 120030922A531065C1054344 PANEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01780AS 25112 GYR - DURING C-CHECK FOUND CORROSION AT ELECTRICAL DISCONNECT PANEL. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040203000772004020300077WP 2004 2 3 ASAA0380584 120030911A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS5465411950 53076 SEA LINE CHECK, FOUND OVERWING EMERGENCY LIGHT BATTERY PACK DISCHARGED. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000812004020300081WP 2004 2 3 ASAA0380580 120030909A33501001191 LIGHT DOUG DC9 DC983 3022083WP PAX CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01977AS5658412690 53453 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000892004020300089WP 2004 2 3 ASAA0380586 120030912A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 SEA LINE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE, BATTERY PACK DISCHARGED. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040203000922004020300092WP 2004 2 3 ASAA0380592 120030920A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 SAN PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED AT ROW 3. RECONNECTED WIRING AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040202001412004020200141NM 2004 2 2 UPS04541749 120031231A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE:C CORROSION ON SEAT TRACK AROUND FASTENER HOLES BETWEEN BS 580 AND BS 620 LBL 45 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REPAIRED SEAT TRACK PER GOODRICH ER 04-1022. 2L72 4F RTA2NM 20040202001432004020200143WP 2004 2 2 UPS04841718 120031231A534037558452N FITTING DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, STA 1228 LONG 34L - 35L BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755845 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20040121000392004012100039NM 2004 1 21 03FDEA02307 120031227A5744ARC74821 FITTING DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING INBOARD FLAP VANE OUTBOARD SUPPORT FITTING INBOARD MOUNT HOLES WORN. COMPLIED WITH FEDEX EA 1-5750-75206. TRAILING EDGE AND TRAILING EDGE DEVICES LT AND RT INBOARD. FLAP VANE ATTACH FITTING REWORK. 2L73 4F RTA22WE 20040122000712004012200071SO 2004 1 22 SIMA200334406 120031127A5330 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21653AE 145433 AIRCRAFT ARRIVED FOR REPAIR OF LIGHTNING STRIKE DAMAGE BETWEEN FRAMES 25 AND 26 AND STRINGERS 19 AND 21. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3988, DATED NOVEMBER 25, 2003 AND EMB 145 SRM, SRM EMB 145/1142 REV 24, CHAPTER 53-22-01. (M) 2L72 4T RTT00011AT 20040122001162004012200116EA 2004 1 22 ASOA03625 120031204A78301267587 PDU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11871AS 7537 FLT 4766 - DURING CLIMB-OUT FROM RDU-DFW, AT APPROXIMATELY 14,000 FEET THE CREW RECEIVED A RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH, AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO RDU, LANDING SAFELY. MAINTENANCE DEFERRED THE RIGHT THRUST REVERSER ON 12/3/2003 UNDER MEL NR 78-30-01. THE ABOVE DISCREPANCY WAS UNDER CONTINUED DEFERRAL WITH THE REPAIRS PERFORMED ON 12/5/2003 AND THE CORRECTIVE ACTION SHOWN ON MRR NR 03624, IN WHICH MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT SHOWN BELOW AT THAT TIME. (M) 2L72 4F RTA21EA 20040122001342004012200134EA 2004 1 22 ASOA03621 120031203A52101039687 CLIP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAO OTHER O OTHER TXTAXI/GRND HDL 1 SO11833AS 7246 FLT 4801 - AT THE GATE AFTER LANDING IN ATL FROM FAY, THE CREW WAS UNABLE TO OPEN THE MAIN PASSENGER DOOR. RAMP PERSONNEL OPENED THE DOOR FROM THE OUTSIDE AND THE PASSENGERS DEPLANED SAFELY. MAINTENANCE ADJUSTED THE OUTER DOOR HANDLE PUSH BUTTON SPRING CLIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001352004012200135WP 2004 1 22 GTIA030956 120031128A4920360452425 BURNER CAN DOUG DC9 DC983 3022083WP APU DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FOUND CREW MENTIONED STRONG FUEL ODOR IN CABIN DURING APU OPERATION. STRONG FUEL ODOR IN CABIN. FUEL LEAKING FROM FUEL ATOMIZER. FOUND A.N. FITTING FROM FUEL LINE TO FUEL ATOMIZER LOOSE. TIGHTEN JAM NUT ON A.N. FITTING. LEAK CHECK GOOD, NO FUEL ODOR NOTED. REMOVED AND REPLACED APU BURNER CAN ASSY. OPS AND LEAK CHECK GOOD. (M) 2L72 4F RTA6WE 20040123000092004012300009WP 2004 1 23 ASAA0380678 120031022A5347SRO953301157001 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND SEAT TRACK IS CORRODED AT FS 1136-1174. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040122000892004012200089EA 2004 1 22 A6WA200340143 120031011A7700 SENSOR CNDAIRCL600 CL6002B19 1900309EA NR 2 ENGINE CONTAMINATED A A6WAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL31427ZW 7685 EN ROUTE AT 29,000 FT N' (+2/-5) ITT/N2 FLUX ABNORMAL ON NR 2 ENGINE. REMOVED AND REPLACED SPEED CONTROL AMP, NO FIX, FOUND T2 SENSOR CANNON PLUGS CONTAMINATED. CLEANED AND OPS CHECK NORMAL. (M) 2L72 4F RTA21EA 20040122001082004012200108EA 2004 1 22 ASOA03629 120031204A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE PILOTS BULKHEAD FLOORBEAM AT FS 280, LBL 9.0 TO RBL 9.0 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD FLOORBEAM AT FS 280, LBL 9.0 TO RBL 9.0 IAW ASA EO 600-53-0130. (M) 2L72 4F RTA21EA 20040122001122004012200112WP 2004 1 22 GTIA030968 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND FLOOR PANEL LEFT MID DETERIORATING, WRONG INSERTS, MISSING INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040123000122004012300012WP 2004 1 23 ASAA0380695 120031027A53133914677507 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD AT FS 1193. REPLACED LONGERON SPLICE PER SRM 51-10-3. (M) 2L72 4F RTA6WE 20040123000142004012300014WP 2004 1 23 ASAA0380833 120031216A5310993607317 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01975AS 53451 DURING C-CHECK SHEAR TIE FOUND CORRODED AT FS 1212. REMOVED DAMAGED AREA AND INSTALLED DOUBELR PER SRM'S 51-10-2, 51-10-4, 51-30-2, AND 51-30-5. (M) 2L72 4F RTA6WE 20040123000632004012300063NE 2004 1 23 MDR03019 120030721A64106516100025101 STRAP SKRSKYS64 S64E 8142604NE TAIL ROTOR BLADECRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09CFCRN2120 64V63345476 64061 THE STRAP IS CRACKED ON THE OUTBOARD SIDE OF THE BLADE APPROXIMATELY 9.187 INCHES FROM THE TRAILING EDGE OF THE BLADE. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARDS THE TIP END OF THE BLADE APPROXIMATELY 1 INCH. THE CRACKS START WHERE THE LEADING EDGE OF THE FAIRING. PN 6516100011042 (ON THE OUTBOARD SIDE), SLIDES BETWEEN THE STRAP, PN 6516000025101 AND THE CHANNEL ASSY, PN 65160-00029-081. CAUSE: UNKNOWN 2G72 4U H4EA 20040126000462004012600046GL 2004 1 26 ERAA091801 220031124A7200 ENGINE BELL 412 412 1182202SW ALLSN 250C 250C20B 03013GL MAKING METAL B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03423EH CAE832946 ENGINE MAKING METAL. HEAVY WEAR ON TORQUE METER GEAR AND PINION. INSTALLED SERVICEABLE GEARBOX. COMPLIED WITH E CHECK. 1G72 4U3 U H4SW E4CE 20040127001432004012700143NM 2004 1 27 ASAA0310192 120030321A5315BAC1505100246 FLOORBEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOORBEAM TOPCAP AT BS 328, STRINGER 62L-62R CORRODED. FABRICATED AND INSTALLED NEW FLOORBEAM TOPCAP PER SRM. (M) 2L72 4F RTA16WE 20040127001552004012700155NM 2004 1 27 ASAA0310203 120030321A533065516287 SKIN BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN PANEL AT BS 986, STRINGER 23R CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20030923000742003092300074WP 2003 9 23 DHL2003604764 120030607A53404611067N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD CARGO COMPT END FITTING AT STA 70.000, L-27L CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-1-21 PG 1. REMOVED CORROSION FROM END FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG 21. REMOVED END FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000922003092300092WP 2003 9 23 DHL2003604708 120030509A53403779762U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT BATHTUB FITTING AT STA 680.000 L-6R WITH 1.500 CRACK IN IT. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-1-21 PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923001112003092300111WP 2003 9 23 DHL2003604729 120030617A53204653726501 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD CARGO COMPT. SPLICE FITTING CRACKED 1.000, STA.200.000 - 220.000, L-27R. (MAJOR REPAIR) CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, ATM NR P0201388, DWG. 4653726. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG.21, SRM 51-1-21 PG.1. FABRICATED SPLICE FITTING IAW DWG.4653726. PERFORMED LIQUID PENETRANT INSPECTION IAW DC8 NDT SPM PART 08-00-02/06. CLEANED, TREATED AND PRIMED AREA AND NEW SPLICE FITTING IAW SRM 51-1-8B. INSTALLED SPLICE FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG.9 AND SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030923001242003092300124WP 2003 9 23 DHL2003604667 120030624A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT ELEVATOR UPPER SKIN INBD SECTION SHOW CORROSION, SEVERAL DENTS AND INTERIM REPAIR FROM STA XAR 0.000 TO XE 132.000. REMOVED FASTENERS AND THE DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL (2024-T3AL 0.032) IAW EO DHL 030573, ED 3410. CLEANED, TREATED AND PRIMED THE NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED THE NEW SKIN PANEL ON RT ELEVATOR UPPER SURFACE INBD SECTION (STA XAR 0.000 TO XE 132.000) USING NEW FASTENERS IAW EO DHL 030573, ED 3410 AND SRM 51-1-21 PG 1. SEE NR 4037 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20030923001322003092300132CE 2003 9 23 GLBA2003123 120030823A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE ENGINE TORQUE STUCK A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM03255GL4693 UE255 RT TORQUE INDICATOR IS STUCK AT 300LB, REMOVED AND REPLACED RT TORQUE GAUGE. OPS CHECK GOOD. 2L72 4T RTA24CE 20030923001752003092300175WP 2003 9 23 AALA20030825 120030731A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW217531A 49923 DURING OVERNIGHT MAINTENANCE, SEAT 13D EMERGENCY LIGHT SOCKET BROKEN. REMOVED AND REPLACED SEAT 13D EMERGENCY LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030924000032003092400003NM 2003 9 24 252TR0008 120030824A33509008358 BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAO OTHER L NO TEST NRNOT REPORTED 1 SO05252TR 23001 CENTER CABIN EMERGENCY OUTBOARD EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK FOR OVER WING HATCH POSITION. CHECKS OK. 2L72 4F RTA16WE 20030924000842003092400084NM 2003 9 24 QXEA200301022 120030824A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 DENT/GOUGE IN FUSELAGE BELLY SKIN AT STATION X747.602 BETWEEN STRINGERS 27R TO 30R. REPAIRED IAW HORIZON AIR EA 6-53-236. 2H72 4T RTA13NM 20030924000942003092400094NM 2003 9 24 AWXA200300986 120030813A575369507651 BRACKET BOEING737 737277 1384570NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 3/16 INCH CRACK WAS FOUND ON NR 2 SLAT INBOARD AUXILIARY TRACK CLOSE-OUT DOOR AFT SPRING ATTACH BRACKET AT WS 404.8. MAINTENANCE REMOVED AND REPLACED THE CRACKED NR 2 SLAT INBOARD AUXILIARY TRACK CLOSEOUT DOOR AFT SPRING ATTACH BRACKET AT WS 404.8 IAW B737-200 SRM 51-30-02, PG. 1, DETAIL 1, FIG. 007. 2L72 4F RTA16WE 20030924001062003092400106NM 2003 9 24 03FDEA01280 120030806A5753ARC0502506 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR ATTACH LUGS CORRODED AT INBOARD AND OUTBOARD BORES AND SPOT FACES. RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR ATTACHMENT LUGS CORRODED AT INBOARD AND OUTBOARD BORES AND SPOT FACES REPAIRED AS PER FEDEX EA 1- 5740-63184. 2L73 4F RTA22WE 20030924001102003092400110EU 2003 9 24 226021403 120030214A30109598901014 TIMER PILATSPC12 PC1245 7090551EU DE ICE SYS FAILED E S4WAO OTHER J WARNING INDICATION CRCRUISE 1 WP07308NA 226 DE-ICE BOOT CAWS ILLUMINATED DURING FLIGHT. 1L71 3T RTA78EU 20030924001242003092400124 2003 9 24 AALA20030757 420030711A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21620AA 24578 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, EIGHT GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED EIGHT GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001262003092400126 2003 9 24 AALA20030713 420030630A2565 GIRT BAR BOEING757 757223 1384957NM ESCAPE SLIDE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21639AA 24597 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION. FOUND THE R1 DOOR GIRT BAR LEAF SPRINGS NOT WORKING PROPERLY. REPLACED GIRT BAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001362003092400136 2003 9 24 AALA20030755 420030708A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21613AA 24489 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, THREE GIRT BAR SPRINGS OUT OF ADJUSTMENT AND ONE NEEDING REPLACED. ADJUSTED THREE GIRT BAR SPRINGS AND REPLACED ONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001392003092400139 2003 9 24 AALA20030714 420030630A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21685AA 25342 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUND THE L2 DOOR GIRT BAR LEAK SPRINGS NOT WORKING PROPERLY. REPLACED GIRT BAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000152003092500015SW 2003 9 25 2003F00581 120030601A5270 SENSOR SWRNGNSA227 SA227AC 8780603SW CARGO DOOR OUT OF ADJUST A BSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM0527465 AC755B THE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB TO ALTITUDE, CREW FOLLOWED CHECKLIST PROCEDURES AND RETURNED TO STATION. CREW LANDED WITH NO FURTHER INCIDENT. PERFORMED RIG CHECK OF CLICK CLACKS USING STUN1-5 TASK CARD, ADJUSTED LOWER FORWARD CLICKCLACK, AND LOWER CLICKCLACK SWITCHES. PERFORMED AN EXTENSIVE OPERATOINAL CHECK FLIGHT TO VERIFY OPERATION OF CARGO DOOR, WENT TO MAXIMUM DIFFERENTIAL CABIN PRESSURE, SYSTEM OPS CHECK GOOD. (M) 2L72 4T RTA8SW 20030925000222003092500022SW 2003 9 25 2003F00582 120030601A5230 MECHANISM SWRNGNSA227 SA227AC 8780603SW MCD CLICK CLACK LACK OF LUBE A BSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0527465 AC755B THE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB AT 11,000 FEET, CREW FOLLOWED CHECKLIST PROCEDURES AND RETURNED TO STATION. DESCENDING THROUGH 6,000 FT, THE CARGO DOOR LIGHT WENT OUT. CREW LANDED WITH NO FURTHER INCIDENT. INSPECTED CARGO DOOR CLICK CLACKS AND BAYONETS IN GOOD CONDITION, BUT SUSPECTED THAT THEY WERE DRY. CLICK CLACKS AND BAYONETS WERE THEN LUBRICATED. GROUND PRESSURIZATION CHECK TO 7 PSID WAS PERFORMED, NO PROBLEMS WERE NOTED. (M) 2L72 4T RTA8SW 20030925000342003092500034NM 2003 9 25 USAA030156 120030805A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US47187 23237 PIT - FOUND STRINGER CRACKED 1 INCH, BS 1138 S5R. CUT OUT DAMAGE AND SPLICED IN NEW PER TYPICAL REP 53-80-04. (M) 2L72 4F RTA16WE 20030923000022003092300002 2003 9 23 QXEA200301008 420030820A2210 AUTOPILOT SYS CNDAIRCL600 CL6002C10 1390015EA ZONE 300 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09609QX 10031 ON DESCENT RECEIVED AN AURAL TRIM IN MOTION WARNING FOLLOWED BY STAB CHANNEL 2 INOPERATIVE WHITE MESSAGE AND AUTOPILOT PITCH TRIM CAUTION MESSAGE. FOLLOWED CHECKLIST AND DISENGAGED AUTIOPILOT. RE-TRIMMED THE AIRCRAFT MANUALLY. PERFORMED FIM OPERATIONAL TEST OF THE HORIZONTAL STABILIZER TRIM SYSTEM IAW CRJ-700 AMM 27-40-00-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030923000272003092300027WP 2003 9 23 DHL2003604597 120030612A5350 TIE DOUG DC8 DC873F 302199FWP TAIL CONE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FUSELAGE TAIL CONE INTERIOR - LT TIE 1.000 CRACKED AT STA. 1951.000. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 PG.1-2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-21A PG.3, SRM 51-3-0 PG.1. 2L74 4F RT4A25 20030923000692003092300069WP 2003 9 23 DHL2003604794 120030430A5347S4929147 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE DETERIORATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT NR 1 TRACK WITH LUGS (02 EA) DETERIORATED, STA 116.000 - STA 118.000. REMOVED DAMAGED NR 1 TRACK PLUG IAW SRM 51-3-0 PG 1. FABRICATED NEW TRACK PLUG IAW SRM 53-2-3 PG 17-19. INSTALLED NEW PLUG ON NR 1 TRACK IAW SRM 53-2-3 PG 17-19, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030923000982003092300098WP 2003 9 23 DHL2003604645 120030527A5730 VANE DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING OB SLOT VANE OUTER PLATING SHOWS ELONGATED HOLES AT STA. XOLDI.6.224. PERFORMED MAJOR REPAIR IAW EODHL-030552, ED-3292. REMOVED FASTENERS. TRIMMED OUT THE ELONGATED HOLES SKIN AREA IAW EODHL-030552, ED-3292. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL DOUBLER (7075-T6 AL0.071), AN INTERNAL DOUBLER (7075-T6 AL0.050) AND A FILLER (7075-T6 0.063) IAW EODHL-030552, ED3292. CLEANED, TREATED AND PRIMED THE REPAIR EXTERNAL DOUBLER INTERIOR SURFACE, INTERNAL DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND BOTH DOUBLERS ON RT. OTBD. SLOT VANE OUTER PLATING, STA. XOKDI.6.224, WITH NEW FASTENERS. 2L74 4F RT4A25 20030923001442003092300144EA 2003 9 23 QXEA200301016 120030823A2611 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 ILLUMINATED A QXEAO OTHER NB FALSE WARNING SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 NM09607QX 10024 ON FLIGHT 2431 SMOKE AFT LAVATORY WARNING MESSAGE CAME ON AFTER TAKEOFF AND REMAINED ON FOR 1.5 MINUTES. FLIGHT ATTENDANT THOUGHT SHE COULD DETECT AN ODOR. GROUND RAN AIRCRAFT AT HIGH POWER WITH NO FURTHER WARNINGS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030924000222003092400022NM 2003 9 24 DL76L030730 120030807A4990380029817 O-RING BOEING767 767332 1382001NM OIL CAP CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO27179DN9899 25144 DURING CRUISE EICAS STATUS MSG APU OIL QTY CAME ON. DURING DESCENT FOR APPROACH THE APU AUTO SHUTDOWN WITH APU FAULT ON EICAS. FOUND OIL CAP O-RING FLAT AND CRACKED. REPLACED SAME RAN APU NO LEAKS NOTED. 2L72 4F RTA1NM 20030924000232003092400023NM 2003 9 24 DL757030731 120030807A5742112N700324 FITTING BOEING757 757232 1384965NM RT WING GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27616DL 22823 GOUGE REPAIR THE INBD SURFACE OF THE INBD SIDE LOAD FITTING ON THE RT WING NACELLE ATTACH STRUCTURE WAS GOUGED DURING ACCOMPLISHMENT OF THE STRUT INPROVEMENT MODIFICATION IAW AD 2000-20-09. THE GOUGE WAS BLENDED SMOOTH AND ROTO PEENED AND THE ADJACENT FASTENER HOLE SPOTFACED TO REMOVE THE DAMAGE. THE REPAIR WAS ACCOMPLISHED IAW ER/A 385419-14AD. 2L72 4F RTA2NM 20030924000662003092400066NM 2003 9 24 DL73K030782 120030824A3397 WIRE BOEING737 737247 138448DNM EMERGENCY LIGHTSCHAFED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 5 TO 9. FOUND BROKEN WIRE CHAFING AT SEAT 5D. REPAIRED WIRE IAW MM. REPLACED FUSES IN FWD AND AFT BATTERY PACKS. LIGHTS NOW OPS NORMAL. 2L72 4F A16WE 20030924000752003092400075NM 2003 9 24 2003UALA00634 120030818A3150 WARNING SYSTEM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE TE FLAPS ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29676UA 30028 ABORTED TAKEOFF AT 80 KTS TWICE DUE TO FLAPS CONFIGURATION WARNING. CAUSE OF CONFIGURATION WARNING IS UNKNOWN. THE TAKEOFF CONFIGURATION MODULE WAS REPLACED. SHOP TESTING SHOWED NO FAULT FOUND. 2L72 4F4 FRTA1NM E24NE 20030924001112003092400111 2003 9 24 226032303 420030323A22209754421421 PROBE PILATSPC12 PC1245 7090551EU AOA FAILED E S4WAK NONE L NO TEST ININSP/MAINT 1 WP07308NA 226 LEFT AOA PROBE FAILS TO HEAT. 1L71 3T RTA78EU 20030924001402003092400140 2003 9 24 AALA20030715 420030630A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21685AA 25342 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUND THE R4 DOOR GIRT BAR LEAF SPRINGS NOT WORKING PROPERLY. REPLACED GIRT BAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000122003092500012 2003 9 25 AALA20030745 420030709A2565A5211060101000 GIRT BAR AIRBUS300 A300B4605R 3930308EU ESCAPE SLIDE STUCK A AALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW217076A 610 UPON ARRIVAL BOS FROM MIA, L1 DOOR STUCK IN ARMED MODE. REMOVED BURRS AND NICKS FROM GIRT BAR ENGAGEMENT SLIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20040127001902004012700190WP 2004 1 27 ASAA0380676 120031015A532199366525 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1155-1250. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20040127001602004012700160WP 2004 1 27 ASAA0380681 120031015A534759305478 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK - FOUND DURING 15K CHECK, SEAT TRACK IS CORRODED AT FS 200-220. REMOVED DAMAGED AREA AND SPLICED IN NEW TRACK PER SRM 53-05. (M) 2L72 4F RTA6WE 20040127001632004012700163NM 2004 1 27 ASAA0310236 120030326A532065621004 CHANNEL BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOOR SUPPORT CHANNEL AT BS 277-344, LEFT BUTTOCK LINE 43 CORRODED. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM. (M) 2L72 4F RTA16WE 20040127001742004012700174NM 2004 1 27 ASAA0310222 120030325A53306545778 SKIN BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN PANEL AT BS 1000, STRINGER 21R-22 DENTED. REMOVED DENT AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040127001752004012700175WP 2004 1 27 ASAA0380637 120031015A57535930496510 VANE DOUG DC9 DC983 3022083WP TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC DURING 15K CHECK, FOUND RIGHT WING INBOARD FLAP VANE, FOREFLAP, IS PUNCTURED. INSTALLED DOUBLER PER SRM 51-70-2 AND EA 5750-01876. (M) 2L72 4F RTA6WE 20040127001922004012700192WP 2004 1 27 ASAA0380791 120031119A532199365811 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DISBONDED AT FS 294-370. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040127002032004012700203WP 2004 1 27 ASAA0380670 120031015A53219936646501 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS CORRODED INSERTS. REPLACED FLOORBOARD. (M) 2L72 4F A6WE 20040127002042004012700204WP 2004 1 27 ASAA0380672 120031015A5311591148525 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND EDGE OF FRAME CHAFED. REPAIRED FRAME. (M) 2L72 4F A6WE 20040127002062004012700206NM 2004 1 27 ASAA0310214 120030325A4910 WEB BOEING737 737298C 1384490NM APU BAY CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, APU COMPARTMENT CEILING WEB AT BS 1142, RIGHT BUTTOCK LINE 6.25 CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20040127002102004012700210WP 2004 1 27 ASAA0380664 120031015A5320993053833 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND RIGHT CUSP WEB AT STATION 218 CRACKED AT INBOARD CORNER. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040127002202004012700220NM 2004 1 27 ASAA0310212 120030325A5311654582936 FRAME BOEING737 737298C 1384490NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FRAME TIE AT BS 360, RIGHT BUTTOCK LINE 15 CHAFED. REMOVED AND REPLACED FRAME TIE PER SRM. (M) 2L72 4F RTA16WE 20040127002252004012700225WP 2004 1 27 ASAA0380652 120031015A53309912455505 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FORWARD CARGO DOOR CUTOUT LOWER INNER DOUBLER IS CORRODED. REPLACED DOUBLER. (M) 2L72 4F A6WE 20040127002262004012700226WP 2004 1 27 ASAA0380683 120031015A5321BAC1509100135 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND FLOOR PANEL, MEMBRANE, IS CORRODED AT FS 522. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-10-3. (M) 2L72 4F RTA6WE 20040127002272004012700227WP 2004 1 27 ASAA0380684 120031015A53203914677507 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND LONGERON SPLICE CORRODED AT FS 1193-1212. REPLACED LONGERON SPLICE PER SRM 51-10-4 AND 51-30-5. (M) 2L72 4F RTA6WE 20040123000582004012300058NE 2004 1 23 MDR03020 120030721A64106516000025101 STRAP SKRSKYS64 S64E 8142604NE TAIL ROTOR BLADECRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM03CFCRN1700 64V21502231 64061 STRAP IS CRACKED ON THE OB SIDE OF THE BLADE APPROXIMATELY 9.125 INCHES FROM THE TRAILING EDGE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROXIMATELY 1 INCH. THE CRACKS START WHERE THE LEADING EDGE OF THE FAIRING, PN 65161-00011-042 (ON THE OB SIDE) SLIDES BETWEEN THE STRAP, PN 65160-00025-101, AND THE CHANNEL ASSEMBLY, PN 65160-00029-081. CAUSE: UNKNOWN 2G72 4U H4EA 20040126000032004012600003NE 2004 1 26 ERAA091803 120031028A26217630607901101 FIRE BOTTLE SKRSKYS76 S76A 8143006NE MAIN MISREPAIRED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03575EH885 760366 FIRE BOTTLE NEEDS TO BE SERVICED. INCORRECT GAUGE INSTALLED. HYDRO TESTED, OVERHAULED, INSTALLED GAUGE, FILLED, LEA AND WEIGHT CHECKED. 1G72 3U H1NE 20040127002072004012700207NM 2004 1 27 ASAA0310215 120030325A5320 STRINGER CLIP BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER TIE AT BS 947, STRINGER 19L CORRODED. REMOVED AND REPLACED STRINGER TIE PER SRM. (M) 2L72 4F RTA16WE 20040127002142004012700214WP 2004 1 27 ASAA0380788 120031119A532199365811 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD UPPER SURFACE IS DISBONDED AT FS 541-579. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040127002212004012700221WP 2004 1 27 ASAA0380669 120031015A53132911432103 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND LONGERON CRACKED. SPLICED IN NEW LONGERON SECTION. (M) 2L72 4F A6WE 20040127002292004012700229WP 2004 1 27 ASAA0380674 120031014A5230591014167 FLANGE DOUG DC9 DC982 3022082WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - FOUND 30K CHECK, AFT CARGO BAY DOOR FLANGE IS CHAFED AT LOWER STOPS. BLENDED CHAFED AREA PER EA 5230-01205. (M) 2L72 4F A6WE 20040127002322004012700232WP 2004 1 27 ASAA0380654 120031015A531059360759 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND AFT CARGO SHEAR TIE IS CORRODED. REPLACED SHEAR TIE. (M) 2L72 4F A6WE 20040127002342004012700234WP 2004 1 27 ASAA0380650 120031015A5313593666715 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND STRINGER IS CORRODED AT FS 1193-1211. REPLACED DAMAGED SECTION WITH SPLICE REPAIR PER SRM 53-02. (M) 2L72 4F A6WE 20040127002442004012700244NM 2004 1 27 ASAA0310217 120030325A5313BAC1498156 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 26R AT BODY STATION 1016 CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20040127002452004012700245NM 2004 1 27 ASAA0310179 120030320A5411BAC15171854 FRAME BOEING737 737298C 1384490NM NR 1 NACELLE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 100.60 CRACKED. REMOVED DAMAGED SECTION AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040127002472004012700247SW 2004 1 27 AC2A092331 120031120A7810230063301102 EXHAUST STACK BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE ENGINE CRACKED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CH 49037 844110 EXHAUST STACK IS CRACKED. REPLACED EXHAUST STACK 1G72 3U3 URTH9SW E1GL 20040123000542004012300054SW 2004 1 23 KBM2003F00106 120031115A2432MS24171D1 RELAY BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL BATTERY INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 BATTERY RELAY OPERATES INTERMITTENTLY. REPLACED WITH SERVICEABLE. 1G71 3U3 U H2SW E4CE 20040123000612004012300061CE 2004 1 23 S492004F00000 120031213A2750082227555 BRACKET CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO BELLCRANK CRACKED E S49AO OTHER J WARNING INDICATION APAPPROACH 1 SW13422BK9284 0332 ON APPROACH TO LAND, EXTENDED 10 DEGREE FLAPS. AIRCRAFT IMMEDIATELY ROLLED RT APPROX 30 DEGREES. PILOT RETRACTED FLAPS AND LANDED WITHOUT INCIDENT WITH NO FLAPS. POST FLT INSPECTION REVEALED RT FLAP BELLCRANK BRACKET BROKEN IN HALF. (SW13200401983) 1L72 3O3 O A7CE E8CE 20040123000732004012300073NM 2004 1 23 KPVA200341 120031028A2611376AS15 LAMP DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NR 2 SMOKE DETECFAILED A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13807WP 023 BAGGAGE SMOKE WARNING DOES NOT TEST IN NR 2 POSITION. REMOVED AND REPLACED LAMP (SELF TEST) AT NR 2 BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECK GOOD IAW DHC8 MM 26-12-00, PG 201. 2H72 4T4 TRTA13NM E20NE 20040126000252004012600025EU 2004 1 26 XG3R087787 120030630A2432135000A FUSE UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE BATTERY BAY OVERHEATED B XG3RO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP0526LB 1115 3514 23017 FUSE ASSEMBLY OVERHEATED FOR UNKNOWN REASON REPLACED FUSE ASSEMBLY WITH FACTORY NEW PART. 1G72 3U3 U H9EU E00054EN 20040126000442004012600044GL 2004 1 26 ERAA091798 220031120A73135233333 FUEL NOZZLE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03134EH9209 635 FUEL NOZZLE STREAKS. INSTALLED NEW METER SET AND OUTER AIR SHROUD. 1G72 3U3 U H3EU E4CE 20040127001612004012700161NM 2004 1 27 ASAA0310191 120030321A5320BAC1505100298 SUPPORT FITTING BOEING737 737298C 1384490NM FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK FOUND SUPPORT FITTING AT BS 350, STRINGER 11L BROKEN. REMOVED AND REPLACED FITTING PER SRM. (M) 2L72 4F RTA16WE 20040127001622004012700162NM 2004 1 27 ASAA0310224 120030325A5420657377442 WEB BOEING737 737298C 1384490NM NR 2 NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL WEB AT NACELLE STATION 102.25 CHAFED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040127001862004012700186WP 2004 1 27 ASAA0380640 120031015A5311SR09530057U25 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC - DURING 15K CHECK, FRAME IS CRACKED IN AFT CARGO BAY AT FS 1231. REPLACED DAMAGED SECTION AND SPLICED IN NEW SECTION PER SRM 53-05. (M) 2L72 4F RTA6WE 20040127002492004012700249SW 2004 1 27 AC2A092333 120031120A6220430010122101 STUD BELL 430 430 1182150SW M/R HEAD CRACKED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH 49037 STUD IS CRACKED.ALL FOUR STUDS WERE CRACKED AROUND SHANK AND HEAD TRANSITION. STUDS WERE REPLACED. 1G72 3U RTH9SW 20040128000172004012800017NM 2004 1 28 2003UALA00938 120031202A5320 WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE THRESHOLD CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 AFT PIT CARGO DOOR CUTOUT THRESHOLD SILL WEB CORRODED UNDER THRESHOLD PLATE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED WEB REPAIR. 2L72 4F4 FRTA2NM E17NE 20040128000232004012800023EU 2004 1 28 RAIA00312318 120031215A2910 LINE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM DAMAGED A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03572HK 41091 BWI- LOST HYDRAULIC QUANTITY AND PRESSURE. MAINTENANCE REPAIRED HYDRAULIC PRESSURE TUBE. 2L72 4T RTA41NM 20040128000272004012800027EU 2004 1 28 RAIA00312324 120031219A36101158200 PRESSURE SWITCH AEROSPATR72 ATR72202 8680940EU BLEED AIR SYS INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03723TE257143729 283 STL- AIR BLEED FAULT. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCH. 2H72 4T RTA53EU 20040128000342004012800034NM 2004 1 28 DHL2003740009 120031225A3240 CONTROL VALVE BOEING727 7272Q9 138448MNM AUTO BRAKING MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01740DH 21930 RTO - AIRCRAFT WEIGHT 143.1, AIRSPEED 5 KTS, OAT 01C, PRESSURE ALTITUDE 900 FT, BRAKE ENERGY CHART - NORMAL. BRAKES WOULD NOT RELEASE WITH 85 PERCENT N1 ON ALL 3 ENGINES FOR APPROX 6 SEC. AFTER REPLACING AUTO BRAKING CONTROL VALVE BRAKING OPS CHECKED GOOD. REMOVED AND REPLACED NR 3 BRAKE DE-BOOST VALVE, OPS AND LEAK CHECKED GOOD. REMOVED AND REPLACED MAIN GEAR BRAKE METERING VALVE. PERFORMED OPS CHECK, VALVE WAS NO HELP. REMOVED AND REPLACED AUTO BRAKE CONTROL MODULE IAW B-727 M/M 32-46-21. OPS AND LEAK CHECKED GOOD. REMOVED AND REPLACED RT BRAKE SHUTTLE VALVE IAW B-727 M/M 32-41-51. OPS AND LEAK CHECKED GOOD. 2L73 4F RTA3WE 20040128000512004012800051NM 2004 1 28 AWXA200301612 120031215A531565528941 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON FLOOR SUPPORT CHANNEL AT BS 540, LBL 0 TO LBL 25. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT CHANNEL AT BS 540, LBL 0 TO LBL 25; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 FIG 2 PG 4. 2L72 4F RTA16WE 20040128000692004012800069SO 2004 1 28 C2XA03SH519 120031230A532014524131011 BRACKET EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV-DURING C-CHECK THE MAIN DOOR THRESHOLD FORWARD AND AFT U-BRACKETS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BRACKETS IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040128000702004012800070SO 2004 1 28 C2XA03SH520 120031230A532014522459003 ANGLE EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV-DURING C-CHECK THE RIGHT RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040128000772004012800077EA 2004 1 28 MASA200300516 120031227A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717175 7175 ASH 3899 DEN-ONT, LEFT OVERWING EXTERIOR EMERGENCY LIGHT WAS INOP. MX REPLACED BULB. OP CHECKS GOOD. 2L72 4F RTA21EA 20040128000782004012800078SO 2004 1 28 MASA200300517 120031228A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ1297 145481 ASH 2795 PIT, FWD EMERGENCY EXIT CEILING LIGHT INOP. MX REPLACED THE BATTERY CHARGER. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040128000822004012800082WP 2004 1 28 MWEA030499 120031227A3320P323B634 TRANSFORMER DOUG DC9 DC981 3022081WP LAVATORY BURNED OUT A MWEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL31812ME 48006 SMOKE DETECTOR IN AFT LEFT LAVATORY AURAL WARNING AND SMOKE WAS VERIFIED BY FLIGHT ATTENDANT. REMOVED AND REPLACED TRANSFORMER. 2L72 4F A6WE 20040128000862004012800086NM 2004 1 28 AWXA200301629 120031203A575465C2660297 WEDGE BOEING737 737301 1384611NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK THE LT WING NR 2 SLAT WAS FOUND DELAMINATED AT OUTBOARD UPPER TRAILING EDGE, SLAT STA 246.27-254.27. MAINTENANCE CUT OUT DELAMINATED SKIN AT OUTBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TO SLAT SKIN IAW B737-300 SRM 51-70-10, FIG 16, PG 67-69. 2L72 4F RTA16WE 20040128000912004012800091NM 2004 1 28 AWXA200301637 120031203A57536546435277 SKIN BOEING737 737301 1384611NM LT TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW156605708 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK THE LT WING OUTBOARD AFT FLAP WAS FOUND DELAMINATED FROM WS 480 TO WS 495. MAINTENANCE REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP IAW T/C R85M27002. 2L72 4F RTA16WE 20040128000932004012800093NM 2004 1 28 AWXA200301639 120031201A522050797843 SKIN BOEING737 73733A 1384673NM EMERGENCY EXIT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN CENTER AFT SECTION OF LT OVERWING EMERGENCY EXIT DOOR BS 638, LBL 60. MAINTENANCE TRIMMED OUT CRACK IAW B737-300 SRM 52-20-01 FIG 101, PG SHEET 3; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; TREATED, PRIMED, AND PAINTED. 2L72 4F RTA16WE 20040128000992004012800099WP 2004 1 28 AALA20031477 120031228A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21253AA 49286 DFW DURING OVERNIGHT MAINTENANCE FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040128001012004012800101CE 2004 1 28 AALA20031479 120031228A3350P4010049 BATTERY PACK MTSBSIMU2 MU2B35 5780411CE EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21503AA 633 ATL DURING OVERNIGHT MAINTENANCE FOUND EXIT SIGN ABOVER EMERGENCY EXIT DOOR ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 1H72 3T RTA10SW 20040128001032004012800103WP 2004 1 28 AALA20031481 120031228A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 DFW DURING OVERNIGHT MAINTENANCE FOUND TAIL CONE LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040128001102004012800110SO 2004 1 28 SWIA200312704 120031220A2721 CONTROL CABLE EMB 120 EMB120ER 3260203SO RUDDER TRIM DAMAGED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07583SW 120351 DURING FLIGHT RUDDER TRIM JAMMED AND WOULD NOT TURN LEFT OR RIGHT. REMOVED AND REPLACED FORWARD RUDDER TRIM CABLES WITH NEW SERVICEABLE CABLES AND TENSIONED IAW EMB 120 MM 27-00-01. 2L72 4T RTA31SO 20040128001132004012800113 2004 1 28 SWIA200312707 420031216A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTO PILOT MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07291SW 120318 WITH AUTOPILOT ENGAGED PASSING 15,000 FT AIRPLANE PITCHED UP UNCOMMANDED. AFTER LEVELING AT 16,000 FT, RECONNECTED A/P. ALTITUDE LIGHT ALT ON FCP (CA AND F/O SIDES) WOULD NOT REMAIN ILLUMINATED. REMOVED AND REPLACED AUTO PILOT CONTROL PANEL IN CENTER CONSOLE. SYSTEM OPS CHECKS GOOD. P/N: 622-6684-006, S/N ON: 2804, S/N OFF: 8544 2L72 4T RTA31SO 20040128001142004012800114NM 2004 1 28 QXEA200301590 120031228A2130 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CONTAMINATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09411QX 4055 SEA- ON FLIGHT 2330 AIRCRAFT RETURNED TO FIELD. WHILE CLIMBING THROUGH 17,500 FEET CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN PRESSURE WAS NORMAL. CABIN ALTITUDE 4000 FT AND CABIN DIFFERENTIAL 5.2 PSI. ALL BLEEDS, VALVES AND DOORS NORMAL. FOUND WATER/CONDENSATION ON CONNECTOR 2. CLEANED CONNECTOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040128001232004012800123SO 2004 1 28 SWIA200312715 120031222A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07196SW5991 5991 120151 FOUR EMERGENCY LIGHTS (CENTER SECTION) AND EXIT LIGHTS INOP. REMOVED AND REPLACED CENTER ELBP, OPS CHECK GOOD. 2L72 4T RTA31SO 20040127001502004012700150NM 2004 1 27 ASAA0310186 120030321A532065524572 WEB BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOOR WEB AT BS 1016, BUTTOCK LINE 0, LEFT BUTTOCK LINE 40 CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040127001822004012700182WP 2004 1 27 ASAA0380682 120031015A57545922500505 PANEL DOUG DC9 DC983 3022083WP LT WING SLAT PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK - FOUND 15K CHECK, LEFT WING SLAT NR 1 INBOARD LOWER PANEL IN PUNCTURED. REPLACED SLAT PANEL. (M) 2L72 4F RTA6WE 20040128000082004012800008SW 2004 1 28 HEEA092090 120031113A2910AS5230W0604 REDUCER BELL 214 214ST 1182106SW NR 2 HYD SYS SHEARED B HEEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW0359806 28140 DURING FLIGHT NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND A REDUCER SHEARED ALLOWING A LOSS OF ALL HYDRAULIC FLUID. 2G72 4U H10SW 20040128001312004012800131NM 2004 1 28 HNAA0300088 120031221A28215905587 FILTER DHAV DHC8 DHC8201 2809001NM FUEL SYSTEM BYPASSING A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07985HA 479 NUMBER 2 ENGINE FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED. REMOVED AND REPLACED HP FILTER AND SWITCH. REPAIRED BROKEN WIRE AT SWITCH C/P, OPS CHECK, LEAK CHECK GOOD. 2H72 4T RTA13NM 20040128001342004012800134SO 2004 1 28 C2XA03BT124 120031230A3350375901 SIGN EMB 145 EMB145ER 3260211SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714939 145030 CREW REPORTED, EMERGENCY EXIT SIGN IN FORWARD CABIN NOT WORKING. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN IN FORWARD CABIN IAW EMB145 MM 33-50-01. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040128001652004012800165SO 2004 1 28 PNSA031103 120031119A2497 WIRE PIPER PA31 PA31350 7103110SO ALTERNATOR BROKEN E PNSAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 AL0315PR 318352011 WHILE IN IFR CRUISE EXPERIENCED TOTAL ELECTRICAL FAILURE. BY SHUTING OFF ANTI-ICE EQUIPMENT WAS ABLE TO RESTORE POWER. RECEIVED PRIOITY ATC HANDLING LANDED IN DLG WITHOUT INCIDENT. MX FOUND A BROKEN WIRE ON BACK OF RIGHT HAND ALTERNATOR. 1L72 3O A20SO 20040128001742004012800174WP 2004 1 28 AALA20040005 120031224A3231 DOOR DOUG DC9 DC982 3022082WP NLG OPEN A AALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW21292AA 49304 PHL EN ROUTE PHL-ORD VIBRATIONS AND LOUD NOISE COMING FROM NOSE GEAR AREA. RETURNED PHL AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR DOORS DOWN AND OPEN. INSPECTED NOSE GEAR DOORS AND NO DAMAGE FOUND. CLOSED DOORS AND RE-DEPARTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040128001982004012800198NM 2004 1 28 DHL200342536 120031205A5312 BULKHEAD BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK , N/R 60796 BS 1183 BL 36 RT WL 237 FWD SIDE BULKHEAD HAS VERT BEAM IS CRACKED IN RADIUS. STOP DRILLED CRACK & INSTALLED REPAIR KIT 65C34406-13 PO 3348157 PER S/B 727-53-0192 & DRAWING 65C34406. 2L73 4F A3WE 20040129000042004012900004EA 2004 1 29 COMA0360575 120031219A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01712CA 7244 FRETTING DAMAGE ON LEFT HAND LOWER WING PLANK FUEL ACCESS HOLE CUTOUT AT 550EB. BLENDED DAMAGE OUT AND ROTO-PEENED AFT OUTBAORD HATCHED AREA IN ACCORDANCE WITH REO 601R-57-21-030. 2L72 4F RTA21EA 20040129000112004012900011EA 2004 1 29 MASA200300520 120031230A3397 WIRE CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT BROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW07907FJ 15007 DURING OVERNIGHT MX IT WAS DISCOVERED THAT THE PAX DOOR EMERGENCY FLOOD LIGHT WAS INOP. MX REPAIRED A BROKEN WIRE. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040129000192004012900019EA 2004 1 29 COMA0370059 120031225A2751 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLATS FALSE INDICATIONA COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01379CA 10102 FLIGHT 5649 SLATS FAIL MESSAGE. NO FAULTS LOGGED IN COMPUTER, COULD NOT DUPLICATE. SYSTEM OPERATES NORMAL. 2L72 4F RTA21EA 20040129000212004012900021NM 2004 1 29 AWXA200400008 120031221A5320654957319 ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD OUTBOARD DUCT SUPPORT (TEE ANGLE) BS 530, LBL 58, WL 156. MAINTENANCE REMOVED CRACKED TEE ANGLE BS 530, LBL 58, WL 156; FABRICATED A NEW REPLACEMENT TEE ANGLE PER DWG 65-49573; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 4 & 8 PG 1, 29, & 38. 2L72 4F RTA16WE 20040129000242004012900024NM 2004 1 29 AWXA200400011 120031203A575369743236 CHANNEL BOEING737 73733A 1384673NM TE FLAP TRACK CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON NR 6 FLAP TRACK FAIRING SPRING DOOR ANCHOR BRACKET (CHANNEL) WBL 197 RT. MAINTENANCE REMOVED CRACKED NR 6 FLAP TRACK FAIRING SPRING DOOR CHANNEL AT WBL 197 RT; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 PG 1-45. 2L72 4F RTA16WE 20040129000252004012900025NM 2004 1 29 AWXA200400012 120031227A53126516300 BEAM BOEING737 7373B7 1384580NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND AT INSULATION HOLE ON BS 178 BULKHEAD VERTICAL BEAM WEB RBL 17.1, WL 183. MAINTENANCE CUT OUT DAMAGED AREA ON BS 178 BULKHEAD VERTICAL BEAM WEB RBL 17.1, WL 183; FABRICATED A NEW SECTION OF WEB AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG 212. 2L72 4F RTA16WE 20040129000332004012900033EU 2004 1 29 MALA030578 120031225A5260900050 ACTUATOR SAAB SF340 340B 7860101EU AIRSTAIR FAILED A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15365PX 340B265 LEFT FWD EMERGENCY EXIT AIRSTAIRS WILL NOT EXTEND. INSPECTED AND FOUND STAIRS WILL NOT COME DOWN. STAIRS WILL EXTEND, INSPECTED AND FOUND NO DAMAGE, PUT STAIRS IN THE STOWED POSITION. INSPECTED A/C AND FOUND SAFE FOR SAFE FOR FERRY FLIGHT FROM FNT TO DTW. MAINTENANCE REMOVED AND REPLACED AIRSTAIRS KICK OUT ACTUATOR P/N 900050, IAW SF340 MM CHAP 52. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040129000412004012900041EU 2004 1 29 MALA030599 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 14B FRAME CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAME 14B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000472004012900047EU 2004 1 29 MALA030582 120031216A5310 DOOR FRAME BAC 146 AVRO146RJ85A1500097EU CARGO BAY CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, AFT CARGO DOOR TOP FRAME CRACKED ON THE LT & RT SIDE AT GUIDE PIN LOCATION. TIMCO REPLACED AFT CARGO DOOR TOP FRAME REPLACED AT GUIDE PIN LOCATION IAW ARVO SRM 52-32-11-201. REFER 409 NR 1196437 FOR ADDITIONAL INFO. A/C RELEASE DATE 12/31/03. 2H74 4F RTA49EU 20040129000922004012900092CE 2004 1 29 04001 120031229A2612 FIRE LOOP LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP RT ENGINE MALFUNCTIONED E BSYAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL0727BL 163 P74333 RT ENGINE INDICATED A FIRE, SHUT DOWN RIGHT ENGINE AND FIRED BOTH FIRE BOTTLES. MAINTENANCE TROUBLESHOOT SYSTEM, DISCONNECED ALL THREE LOOPS, ALL CHECKED OUT GOOD. RECONNECTED SYSTEM, CHECKED OUT NORMAL. RETURNED TO SERVICE. 2L72 4F4 F A10CE E6WE 20040128000282004012800028SO 2004 1 28 RAIA00312325 120031223A329714554585403 WIRE HARNESS EMB 145 EMB145 3260210SO MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03827HK STL- LEFT MLG WOULD NOT LOCK UP AFTER RETRACTION. MAINTENANCE REMOVED AND REPLACED WOW WIRING HARNESS. 2L72 4F RTT00011AT 20040128000392004012800039WP 2004 1 28 DHL2003809010 120031228A5210 BELLCRANK DOUG DC8 DC873F 302199FWP PAX DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL 46047 MAIN ENTRY DOOR IS DIFFICULT TO OPEN AND CLOSE. FOUND BAYONET BELLCRANK CRACKED, ALSO FOUND DAMAGED ROLLER ASSEMBLY ON DOOR SEAL ACTUATING CRANK. REMOVED BAD PARTS. 2L74 4F RT4A25 20040128000412004012800041WP 2004 1 28 ABXA030487 120031213A53103914025502N FITTING DOUG DC9 DC941 302207NWP CARGO DOOR BEAM CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 CARGO DOOR BEAM NR 2 AFT END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040128000542004012800054NM 2004 1 28 AWXA200301615 120031207A53206546812187 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1011-1016, RBL 6. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 1011 TO BS 1016, RBL 6; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12, PG 45. 2L72 4F RTA16WE 20040128001412004012800141EU 2004 1 28 AWXA200301645 120031230A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 263 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28647AW 762 ATL - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13, 17, 22, 26 AND EMERGENCY EXIT SIGNS AT L-2 & R-2 DOORS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD. 2L72 4F RTA28NM 20040128001532004012800153NM 2004 1 28 QXEA200301602 120031219A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- RIGHT HAND AFT FUSELAGE AFT OF FRAME 3 HAS DENT IN SKIN. REPAIRED IAW DHC-8 SRM 51-20-91, 53-30-24, 51-00-06 AND 51-20-26. 2H72 4T RTA13NM 20040128001992004012800199NM 2004 1 28 DHL200342537 120031120A5743 FITTING BOEING727 727225 1384077NM LT MLG DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK , N/R 59858 LEFT MLG SUPPORT FITTING RETAINER BOLT LUGS ELONGATED. ACCOMPLISHED REPAIR TO LEFT MLG SUPPORT FITTING IAW B727 S/B 57-0153 REV 4, LEAK CHECK GOOD. 2L73 4F A3WE 20040129000222004012900022NM 2004 1 29 AWXA200400009 120031219A532069372542 CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD DUCT SUPPORT CLIP AT BS 530, LBL 56, WL 158. MAINTENANCE REMOVED CRACKED CLIP AT BS 530, LBL 56, WL 158; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-37254; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 4 & 8 PG 1, 29, & 38. 2L72 4F RTA16WE 20040129000662004012900066 2004 1 29 SWIA200312738 420031230A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLT CONTROL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07951SW96 96 7795 A/P DISCONNECTED IN FLIGHT WHEN FLIGHT DIRECTOR FAILED ON F/O'S SIDE. A/P WOULD NOT RE-ENGAGE ON CAPTAIN'S SIDE. AFTER 15 MINUTES F/O'S FLIGHT DIRECTOR CAME BACK AND RE-ENGAGED A/P. REMOVED AND REPLACED FCC NR 2. OPS CHECKS GOOD IAW CRJ MM 22-12-14. 2L72 4F RTA21EA 20040129000932004012900093SO 2004 1 29 MASA200300484 120031211A261147359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO CARGO BAY FALSE INDICATIONA MASAO OTHER N FALSE WARNING CRCRUISE 1 SW07851MJ4264 145572 ASH 2773, MEM REPORTED A CARGO SMOKE DETECTOR CAUSING A FALSE BOTTLE DISCHARGE/DETECTION MESSAGE. MX CONFIRMED NO PRESENCE OF SMOKE. MX REPLACED SMOKE DETECTOR AND THE TEST RELAY. TEST RELAY P/N M83536/13-008L. 2L72 4T RTT00011AT 20040129001192004012900119EA 2004 1 29 COMA0460005 120031230A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01810CA 7370 FLIGHT 5486 LEFT THRUST REVERSER UNLOCK WARNING. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040129001772004012900177NM 2004 1 29 DHL200374265 120031121A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, AFT CARGO FLOOR SUPPORT BENT STA 955E LBL 12. REMOVED DAMAGED FLOOR SUPPORT STA 955E LBL 12 AND MADE NEW FROM BAC1500-6199.7075-T6 (68.5 X .75 X 1.25 X 1.25 X 1.25 X .75 INCH) PO 335824 AS PER SAMPLE IAW B727 SRM 53-10-2 FIG 8, PART TREATED AND PRIMED IAW B727 SRM 51-10-2, PART INSTALLED IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040129001812004012900181NM 2004 1 29 DHL200374268 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER FUSELAGE EXTERIOR SKIN BS 390 BETWEEN 6TH LEFT AND 7TH SKIN IS DENTED. DENT AT BS 390 STR 6L TO STR 7L FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA DIM 3 X 2 INCH IAW B727 SRM 53-30-3 FIG 3. REMOVED PREVIOUS REPAIR FOR INCORPATION INTO NEW REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER, DIM 25 X 12 INCH, USING 2024-T3 .050 PO 900408 IAW B727 SRM 53-30-3 FIG 3. ALODINE AND PRIMED IAW B727 SRM 51-10-2, INSTALLED REPAIR AT BS 390 STR 6 TO 7L IAW B727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20040130000122004013000012NM 2004 1 30 SWAA032843 120031230A53306552874 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20040130000172004013000017NM 2004 1 30 SWAA032810 120031224A53306545866 SKIN BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND LOWER EXT FUSELAGE SKIN BULGED AT BS 527, LBL 7. REPAIRED DAMAGED AREA PER BFG ER. 2L72 4F RTA16WE 20040130000212004013000021NM 2004 1 30 SWAA032816 120031225A3350079123 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 FWD EEPLS COVER OUT OF POSITION. REPOSITIONED COVER PER MM. 2L72 4F RTA16WE 20040130000332004013000033NM 2004 1 30 SWAA032826 120031226A57536546481 CARRIAGE BOEING737 7373H4 1384600NM RT WING TE FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED PM CHECK, FOUND RT WING OUTBD T/E MID FLAP INBD CARRIAGE SPINDLE CRACKED. REMOVED AND REPLACED CARRIAGE ASSY PER MM. 2L72 4F RTA16WE 20040130000432004013000043NM 2004 1 30 SWAA032802 120031222A53156545410 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 25, WL 206. REPAIRED BEAM PER BFG ER. 2L72 4F RTA16WE 20040130000442004013000044NM 2004 1 30 VNAA0312015 120031231A28234068B000002 SHUTOFF VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT ENGINE FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07462PS2198010579 3084 DURING FLIGHT, THE CREW OBSERVED A RIGHT HAND ENGINE TORQUE FLUX OF 5 TO 7 PERCENT AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND FUEL CONTROL SHUTOFF VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040126000292004012600029 2004 1 26 HEEA087794 420030621A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 AFCS ACTUATOR ERRATIC THEN QUIT. TO BE SENT TO VENDOR. 1G72 3U H1NE 20040126000512004012600051GL 2004 1 26 BAQA091613 220031223A723023057142 CASE AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL COMPRESSOR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03941MS446 5495 CASE HALVES OF COMPRESSOR, COATING LIFTING. PART REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H11EU E4CE 20040127001462004012700146NM 2004 1 27 ASAA0310188 120030321A54117075T6062 FRAME BOEING737 737298C 1384490NM NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 116.25 CHAFED. FABRICATED AND INSTALLED REPAIR TO FRAME PER SRM. (M) 2L72 4F RTA16WE 20040127001492004012700149NM 2004 1 27 ASAA0310185 120030321A55126552493 SKIN BOEING737 737298C 1384490NM HORIZONTAL STAB PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND LEFT HORIZONTAL STABILIZER SKIN AT STABILIZER SECTION 10L PUNCTURED. APPLIED FIBERGLASS OVERLAY TO STABILIZER SKIN PER SRM. (M) 2L72 4F RTA16WE 20040127001702004012700170NM 2004 1 27 ASAA0310193 120030321A53476019392 SEAT TRACK BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SEAT TRACK AT BODY STATION 520-540, RIGHT BUTTOCK LINE 46 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20040127001852004012700185NM 2004 1 27 ASAA0310170 120030320A57302024T3050 SKIN BOEING737 737298C 1384490NM LT WING LE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND LEFT WING FIXED LEADING EDGE SKIN AT WING STATION 225-345.14 CHAFFED. REMOVED AND REPLACED SKIN PER SRM. (M) 2L72 4F RTA16WE 20040127001932004012700193NM 2004 1 27 ASAA0310210 120030325A531065207232 BEAM BOEING737 737298C 1384490NM FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FORWARD PIT DOOR BOX BEAM AT BS 490, STRINGER 19R WORN. FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040127002082004012700208WP 2004 1 27 ASAA0380662 120031015A532199365851 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND RIGHT FLOOR PANEL AT STATION 920-1000 EDGE AND STIFFENER CRACKED AND DISBONDED. REPAIRED IAW SRM. FABRICATED AND BONDED REPAIR PLATE. (M) 2L72 4F A6WE 20040128000112004012800011NE 2004 1 28 HEEA092084 220031228A73210164248820 FUEL CONTROL AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1D1 NE ENGINE MALFUNCTIONED B HEEAO OTHER J WARNING INDICATION APAPPROACH 1 SW03404662232 3004 9510 WHEN COLLECTIVE WAS LOWERED TO LAND, THE ENGINE WOULD OVERSPEED. MAINTENANCE REPLACED THE FUEL CONTROL UNIT. 1G72 3U3 U H11EU E19EU 20040128000192004012800019NM 2004 1 28 DLM90031090 120031214A2612 WARNING LIGHT DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 2 ENGINE INOPERATIVE A DALAE ENGINE SHUTDOWN P NO WARNING INDICATION TXTAXI/GRND HDL 1 SO27905DA21823 53385 020007 AFTER ARRIVAL AT GATE AND DURING PASSENGER NORMAL EXIT, RAMP STATED, A TAILPIPE FIRE IN NR 2 ENG. NO FIRE INDICATION OR LIMIT EXCEEDENCE NOTED. TAILPIPE FIM PROCEDURE ACCOMPLISHED IAW POM. ENG WAS ALREADY SHUT DOWN. CLEANED NR 5 BEARING CAVITY AND RAN ENGINE PER PFHB. 2L72 4F4 FRTA6WE E40NE 20040128000202004012800020EU 2004 1 28 RAIA00312314 120031214A24301050032 BPCU AEROSPATR72 ATR72202 8680940EU MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03723TE5367 24 283 UTILITY SHED BUSS FAIL. MAINTENANCE REPLACED BPCU. 2H72 4T RTA53EU 20040128000532004012800053NM 2004 1 28 AWXA200301614 120031207A53206546812187 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 1011-1016, LBL 6. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 1011 TO BS 1016, LBL 6; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12, PG 45. 2L72 4F RTA16WE 20040128000742004012800074SO 2004 1 28 C2XA03SH524 120031230A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV-DURING C-CHECK THE LOWER CARGO DOOR CUT OUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040128000762004012800076EA 2004 1 28 MASA200300514 120031226A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727318 7318 ASH 6430 FWD CABIN FLOOR LEVEL EMERGENCY FLOOD LIGHT INOP. MX REPLACED THE LAMP. OP CHECKS GOOD. 2L72 4F RTA21EA 20040128000792004012800079SO 2004 1 28 C2XA03IA115 120031228A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718557 145596 DURING SCHEDULED MAINTENANCE THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. THE LAMP IN THE LIGHT ASSEMBLY WAS REPLACED AND THE LIGHT OPERATIONALLY CHECKED. 2L72 4T RTT00011AT 20040130000472004013000047NM 2004 1 30 VNAA0312010 120031217A2612 FIRE LOOP DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE APU FAILED A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL07427JS 3039 THE CREW REPORTED THAT THE APU FIRE TEST WAS NOT TESTING. MAINTENANCE THEN DEFERRED THE APU FIRE TEST IN ACCORDANCE WITH 49-1 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040130000482004013000048EA 2004 1 30 VNAA0312011 120031220A5220 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT ILLUMINATED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07209PS 7874 THE CREW RECEIVED A RIGHT HAND OVERWING EMERGENCY EXIT INDICATION. MAINTENANCE THEN DEFERRED THE RIGHT HAND OVERWING EMERGENCY EXIT INDICATION IN ACCORDANCE WITH 52-70-3C. 2L72 4F RTA21EA 20040130000772004013000077NM 2004 1 30 DHL2003742549 120031209A5754 ACCESS PANEL BOEING727 727225 1384077NM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 4 SLAT IS CRACKED AT ACCESS PANEL LOWER ATTACH ANGLE AT THE RIB INBD OF ANTI ICE DUCT. REMOVED DAMAGED AREA DIM 1.125 INCHES AND FABRICATED NEW DOUBLER FROM 2024 T3 .050 PO 900274 DIM 6 X 1 INCH AND FILLER FROM 2024-T3 .040 PO 900471, 1.125 X 1 INCH IAW B727 SRM 51-40-3. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER AND FILLER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040130000792004013000079NM 2004 1 30 DHL2003742550 120031123A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE, FLORIDA DISCREPANCY IS AS FOLLOWS; N/R 60029 CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM LBL 50 RBL 50 WL 208, AS VIEWED FROM NWW DOGHOUSE AREA. REMOVED 9G BULKHEAD, FLOORBOARDS AND SHEAR WEB FOR ACCESS IAW B727 SRM 51-30-2 AND MM 53-20-11. REMOVED DAMAGED UPPER CHORDS BS 344 AND FABBED NEW FROM BAC 1505-29222 PO 3348139 DIM 11.75 INCH LONG IAW B727 SRM 51-20-1 & 53-10-2 FIG 7. NEW CHORD TREATED AND PRIMED IAW B727 SRM 51-10-2, AND INSTALLED IAW B727 SRM 51-30-2. REINSTALLED SHEAR WEB, FLOORBOARDS AND 9G BULKHEAD IAW B727 SRM 51-30-2 & MM 53-20-11. 2L73 4F A3WE 20040130000822004013000082NM 2004 1 30 DHL2003742560 120031125A5754 MOUNT BRACKET BOEING727 727225 1384077NM NR 2 SLAT TRACK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 2 SLAT INBD TRACK UPPER MOUNT INBD L-ANGLE IS CRACKED. REMOVED DAMAGED ANGLE AND FABRICATED NEW FROM BAC1505-100617 PO 900411 DIM 9.25 X 1.25 INCH AS PER SAMPLE IAW 727 SRM 57-10-2 FIG 3. NEW ANGLE TREATED AND PRIMED IAW 727 SRM 51-10-2, INSTALLED IAW 727 SRM 51-30-2. LEAK CHECK GOOD IAW B727 MM 27-81-00. 2L73 4F A3WE 20040130000832004013000083NM 2004 1 30 DHL2003742562 120031123A5230 SKIN BOEING727 727225 1384077NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 1 CARGO DOOR AFT SIDE SKIN BEHIND THE REPAIR IS DENTED. CUT OUT DAMAGED LWR SECTION OF SKIN & FABED NEW FROM 2024-T3 .040, PO 900355 DIM 58.5 X 14.375 INCH AND DOUBLERS 6 EA FROM 2024-T3 .063, PO 900355, DIM 5 X 8 INCH, 5.5 X 4.5 INCH, 8.875 X 4.5 INCH, 6.75 X 4.5 INCH, 5.125 X 4.75 INCH, AND 8 X 4.75 INCH, IAW B727 SRM 52-00-3 FIG 1. ALL REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW REPAIR PARTS IAW B727 SRM 52-00-3 FIG 1. 2L73 4F A3WE 20040130000842004013000084NM 2004 1 30 DHL2003742563 120031123A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM, LBL 50 RBL 50,WL 208,AS VIEWED FROM NWW DOGHOUSE AREA. REMOVED 9G BULKHEAD,AND SHEAR WEB FOR ACCESS, IAW B727 SRM 51-30-2 AND MM 53-20-11. REMOVED DAMAGED UPPER CHORD BS 344 AND FABED NEW FROM BAC1505-29222 PO 3348139 DIM 11.75 FT LONG IAW 727 SRM 51-20-1 & 53-10-2 FIG 7. NEW CHORD TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2 REINSTALLED SHEAR WEB, FLOORBOARDS AND 9G BULKHEAD IAW 727 SRM 51-30-2 & MM 53-20-11. 2L73 4F A3WE 20040130000952004013000095NM 2004 1 30 DHL2003742570 120031120A5310 FRAME BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD, CORNER AREA WITH DENTS. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABBED NEW ONE FROM BAC 1503-100274 PO 3344880 DIM 42 INCHES & SPLICE ANGLE DIM 9 INCHES IAE B727 SRM 51-40-1 FIG 1. CUT OUT DAMAGED WEB & FABBED NEW FROM 7075-T6 .071 DIM 31 X 4.25 PO 900242 & 2 EA SPLICE DOUBLERS SAME MATL DIM 8.5 X 4.25 INCH IAW B727 SRM 53-10-2 FIG 3, 51-40-2 FIG 1. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2, AND INSTALLED IAW B727 SRM 51-40-2 FIG 1 & 51-40-4 FIG 1. 2L73 4F A3WE 20040130001002004013000100NM 2004 1 30 DHL200374273 120031129A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER CABIN NR 5 SEAT TRACK BS 380 TO BS 344 RBL 45 WITH CORROSION. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 3. REMOVED DAMAGED SEAT TRACK & INSTALLED NEW P/N BAC1520-792 PO 990203 DIM135.5 INCHES LONG IAW 727 SRM 53-10-5 FIG 7. 2L73 4F A3WE 20040128001262004012800126SO 2004 1 28 LR7A03109 120031204A5312 PRESSURE PANEL LKHEED382 382G 526414USO MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 5025 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND FS 517 LT MLG WHEEL WELL SKIN CRACKED AT BELLY SKIN ATTACHMENT LBL 35, WL 126. REPAIRED IAW SRM SMP 583 51-140-12. NR 2017. 2H74 4T A1SO 20040128001362004012800136NM 2004 1 28 QXEA200301592 120031229A7930 CONNECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 DIRTY A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09346PH 477 BLI FLIGHT 2158 ON SHORT FINAL, MASTER WARN NR 2 ENGINE OIL PRESSURE CAME ON. RAN CHECKLIST, LIGHT WENT OUT AFTER 5 SECONDS. OIL PRESSURE GAUGE READING NORMAL, IN GREEN ARC. FOUND OIL CONTAMINATION IN NR 2 OIL ENGINE OIL PRESSURE SWITCH CONNECTOR. CLEANED CONNECTOR. GROUND RAN AIRCRAFT AT VARIOUS POWER/CONDITION LEVER SETTING. NR 2 OIL PRESSURE NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040128001392004012800139NM 2004 1 28 QXEA200301596 120031229A242011522183 GENERATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM09539DS3670 3670 4016 SEA- ON FLIGHT 2396 DURING TAKEOFF ROLL THE NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. RAN EMERGENCY CHECKLIST, LIGHT REMAINED ON. REMOVED AND REPLACED NR 1 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040128001522004012800152NM 2004 1 28 QXEA200301601 120031220A5753 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- LEFT HAND OUTBOARD FLAP HAS A CHAFE ON TOP SURFACE TWO INCHES FROM END OF FLAP FORWARD OF TRAILING EDGE. REPAIRED IAW DHC-8 RD 8-57-1734 AND RD 8-57-1549. 2H72 4T RTA13NM 20040128001542004012800154NM 2004 1 28 QXEA200301603 120031215A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- WEB HAS OVERSIZED HOLE BELOW NR 7 SEAT TRACK AT STATION X399. REPAIRED IAW DHC-8 SRM 51-00-06, RD 8-53-7685 AND HORIZON AIR EA 2-53-520. 2H72 4T RTA13NM 20040128001682004012800168NM 2004 1 28 AWXA200400003 120031202A57206569846150 PLATE BOEING737 73733A 1384673NM RT MLG WW CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK FOUND INSPECTION COVER AT INBOARD END OF RT OUTBOARD FLAP WELL CHAFED WS 205 RT. MAINTENANCE REMOVED CHAFED INSPECTION PLATE AT INBOARD END OF RT OUTBOARD FLAP WELL WS 205 RT; FABRICATED A NEW REPLACEMENT PLATE; INSTALLED REPAIR PART IAW AWA ER 03-5750-03352-TB3. 2L72 4F RTA16WE 20040128002052004012800205WP 2004 1 28 UPS04841680 120031229A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:C3 LT WING L/E HAS UPPER RIBS CRACKED AT XFS 835, XFS 822.5, XFS 803.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATED CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040128002112004012800211WP 2004 1 28 UPS04841686 120031231A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING LE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, INTERGRANULAR CORROSION ON RT WING L/E UPPER SKIN AT AFT END AT XFS 347. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8-5720-7767-A. 2L74 4F RT4A25 20040129000272004012900027NM 2004 1 29 AWXA200400014 120031227A5311651630087 FRAME BOEING737 7373B7 1384580NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LCQ - MAJOR REPAIR - DURING C-17 CHECK HFEC INSPECTION INDICATED A CRACK ON BS 178 BULKHEAD RT SIDE FRAME, RBL 70, WL 207. MAINTENANCE REMOVED DAMAGED RT SIDE FRAME AT RBL 70, WL 207; FABRICATED A NEW REPLACEMENT FRAME; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8, PG 38. 2L72 4F RTA16WE 20040129001102004012900110NM 2004 1 29 DHL2003742553 120031126A5510 STRUCTURE BOEING727 727225 1384077NM RUDDER WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, LOWER RUDDER L/E WORE-OUT LT AND RT SIDES/CHAFING AREAS. REMOVED LWR RUDDER FOR ACCESS IAW B-727 MM 27-20-1. REMOVED 2 EACH PREVIOUS REPAIR AND FABBED NEW FROM 301 1/4 HD .016 PO 3348 101 DIM 21.5 X 11 INCH AND 21.5 X 11.375 INCH IAW B-727 SRM 55-40-3 FIG 1. DOUBLERS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 55-40-3 FIG 1. REINSTALLED LWR RUDDER IAW B-727 MM 27-20-1. OP'S AND LEAK CHECK GOOD IAW B-727 MM 27-20-00. 2L73 4F A3WE 20040129001232004012900123EA 2004 1 29 COMA0470002 120031229A3020 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ANTI ICE SYSTEM FALSE ACTIVATIONA COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01642CA 10125 FLIGHT 5773 LEFT ENGINE COWL ANTI ICE CAUTION MESSAGE. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY AFTER CLEARING DEFERRED MAINT ON LEFT ACM. 2L72 4F RTA21EA 20040130000242004013000024 2004 1 30 SWAA032803 420031223A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF POSITION. READJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040130000992004013000099NM 2004 1 30 DHL200374272 120031129A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER CABIN SEAT TRACK NR 4 BS 344 TO BS 360 RBL 24 WITH CORROSION. DAMAGED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 3. REMOVED DAMAGED SEAT TRACK & INSTALLED NEW P/N BAC 1520-792 PO 900203 DIM 135.5 INCH LONG IAW 727 SRM 53-10-5 FIG 7. 2L73 4F A3WE 20040130001042004013000104NM 2004 1 30 DHL200374275 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER FUSELAGE EXTERIOR SKIN BS 390 BETWEEN STR 6L AND 7L SKIN IS DENTED. DENT AT BS 390 STR 6L TO STR 7L FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA, DIMENSIONS 3 X 2 INCH IAW B727 SRM 53-30-3 FIG 3. REMOVED PREVIOUS REPAIR FOR INCORPATION INTO NEW REPAIR IAW B727 51-30-2. FABRICATED NEW DOUBLER DIM 25 X 12 INCH USING 2024-T3 .050 PO 900408 IAW B727 SRM 53-30-3 FIG 3. ALODINED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR AT BS 390, STR 6L TO 7L IAW B727 SRM 53-30 FIG 3. 2L73 4F A3WE 20040130001062004013000106NM 2004 1 30 DHL200374277 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSELAGE SKIN TWO LIGHT GOUGES STA 670 BETWEEN STR 5R TO 6R. CLEANED GAUGE AT BS 670 STR 5R TO 6R MATERIAL LOSS 0.010 FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-3 FIG 1. CUT OUT DAMAGED AREA DIM APPROX 4 X 1 INCH IAW B727 SRM 53-30-3 FIG 1. PART MADE FROM 2024-T3 .050 PO 900471 DIM APPROX 7.875 X 11.75 INCH IAW B727 SRM 53-30-3 FIG 1 & 53-30-2 FIG 2, PART WITH BARE METAL TREATED WITH ALODINE & PRIMED IAW B 727 SRM 51-10-2. FAB & INSTALLED COUNTERSINK WASHER REPAIR & DOUBLER AT BS 670 STR 5R TO 6R IAW B727 SRM 53-30-3 FIG 1 & 51-30-8. 2L73 4F A3WE 20040129001052004012900105NM 2004 1 29 DHL2003742541 120031203A5320 WEB BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, STA 870 BELOW RT 70.5 FITTING, WEB IS CRACKED ON FWD SIDE. REMOVED AT STA 870 R/T 70.5 FITTING WEB ON FWD SIDE IAW B727 SRM 51-30-2. FABRICATED NEW WEB DIMENSIONS 12 X 6 INCHES USING 7075-T6 .050 PO 90096 IAW B727 SRM 51-10-2 FIG 3. ALODINED AND PRIMED NEW WEB IAW B727 SRM 51-10-2 AND INSTALLED NEW WEB IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040129001202004012900120EA 2004 1 29 COMA0460006 120031231A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01815CA 7397 FLIGHT 5937 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040129001242004012900124NM 2004 1 29 DHL2003742555 120031123A5310 STRUCTURE BOEING727 727225 1384077NM NLG WW CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CORROSION ON LOWER SURFACE OF LEFT NOSE WHEEL WELL MID-CHORD BS 296, LBL 20, WL 165 AS VIEWED THROUGH FWD LEFT DOGHOUSE FLOOR PRESSURE PANEL. REMOVED AND REPLACED LT NOSE WHEEL WELL AND CHORD BS 296 USING P/N 65-19862-19 PO3348224 IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040129001792004012900179NM 2004 1 29 DHL200374266 120031123A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 5 SEAT TRACK AT BS 480 IS DAMAGED. REMOVED DAMAGED SEAT TRACK AND FABBED NEW FROM BAC1520-792 PO 902203 DIM 158.5 INCH AND TWO SPLICE ANGLES FROM BAC1503-100122 PO 900221 DIM 14 INCH X 2.5 INCH AND 1 EA SPLICE PLATE FROM 7075-T6 .250 PO 99112793 DIM 7 X 2 INCH, IAW B727 SRM 53-10-1 FIG 1. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 53-10-5 FIG 1. 2L73 4F A3WE 20040130000502004013000050NM 2004 1 30 VNAA0312014 120031224A3220 DOOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NLG OPEN A VNAAO OTHER O OTHER CLCLIMB 1 GL07438JS 3056 DURING FLIGHT, THE CREW REPORTED THE NOSE LANDING GEAR DOOR WAS OPEN AND RETURNED TO LEX. MAINTENANCE INSPECTED AND LATCHED THE NOSE LANDING GEAR DOOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040202000182004020200018WP 2004 2 2 UPS04841711 120031230A5313 LONGERON DOUG DC8 DC873F 302199FWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LONGERON STATION 1726 AND 1746 LONG 15R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040202000382004020200038NM 2004 2 2 EIA203172 120031216A3350 LAMP BOEING747 747SR46 1384816NM EMERGENCY LIGHT MALFUNCTIONED A EIAAO OTHER O OTHER NRNOT REPORTED 1 NM09478EV 21033 L1 EMERGENCY AFT LIGHT DIM. DMI 33-13. RELAMPED 12-20-2003. 2L74 4F RTA20WE 20040130000362004013000036 2004 1 30 SWAA032830 420031229A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040130000872004013000087NM 2004 1 30 DHL2003742566 120031123A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 5 SEAT TRACK AT BS 480 IS DAMAGED. REMOVED DAMAGED SEAT TRACK AND FABED NEW FROM BAC1520-792 PO 902203 DIM 158.5 INCH AND TWO SPLICE ANGLES FROM BAC1503-100122 PO 900221 DIM 14 X 2.5 INCH AND 1 EA SPLICE PLATE FROM 7075-T6 .250 PO 99112793 DIM 7 X 2 INCH, IAW B727 SRM 53-10-1 FIG 1. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 53-10-5 FIG 1. 2L73 4F A3WE 20040130002402004013000240 2004 1 30 SWIA200312754 420031228A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07212SW8639 8639 120276 F/O'S YAW SYSTEM DISENGAGES. REPLACED NR 2 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20040202001482004020200148WP 2004 2 2 UPS04841723 120031230A5754 RIB DOUG DC8 DC871F 302199DWP LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LEFT WING NR 2 STUB WING UPPER RIB IS CRACKED AT XS 250.089. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040202001642004020200164EU 2004 2 2 MALA040114 120031230A5350 RADOME SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15407XJ 340B407 DURING INSPECTION IN LCQ, LEFT HAND FWD FUSELAGE AT STA 126 JUST AFT OF RADOME SUSTAINED A DENT. MAINTENANCE REMOVED DENT AT STA 126. PERFORMED HFEC TO DENTED AREA, NO RELEVANT INDICATIONS NOTED. FORMED REPAIR DOUBLER, TREATED AREA, INSTALLED DOUBLER, APPLIED TOP COAT IAW EO S53192. 2L72 4T RTA52EU 20040202002862004020200286NM 2004 2 2 DHL2003753508 120031230A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, FUSELAGE EXTERIOR BS 720E RT TOP SEAM SHOW DENTED AREA STR 19R. REMOVED RIGHT WING ROOT L/E, RIGHT L/E ANTI ICE DUCT WS 90.5 TO 130.7, HYD LINES, REMOVED, FASTENER & CUT OUT DAMAGED AREA 3 X 3 INCH IAW B727 M/M 36-00, 29-00, SRM 51-30-2 & 53-30-3 (6). PARTS MADE FROM 2024T3 063 PO 90024. DOUBLERS (12 X 8.75 INCH) FILLER (7.25 X 12 INCH) (12 X 3 INCH) IAW B727 SRM 53-30-3 (6). TREATED & PRIMED AREA, & REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS AT EXT FUS B/S 720E STR 19R IAW B727 SRM 53-30-3 (6). REINSTALLED RIGHT WING ROOT L/E, RIGHT, L/E DUCT WS 90.5 TO 130.7 & MID LINES FROM WS 90.3 TO 130.7, REMOVED & REINSTALLED WIRE BUNDLE FROM WS 171.5 TO 0 IAW B727 SRM 51-30-2 M/M 29-2L73 4F A3WE 20040130002152004013000215WP 2004 1 30 ABXA040006 120031201A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 CRACK IN OUTER SKIN AT LOWER FORWARD CORNER OF AFT PASSENGER DOOR. REMOVED CRACKED OUTER SKIN, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D AND REA D853-48472MR. 2L74 4F 4A25 20040130002262004013000226NM 2004 1 30 AWXA200400039 120031227A5320141N516078 FLOOR SUPPORT BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATES ON FLOOR SUPPORT CHANNEL AT R-1 DOOR THRESHOLD BS 332 TO BS 360, RBL 59. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT CHANNEL FROM BS 332 TO BS 360, RBL 59; FABRICATED A NEW REPLACEMENT SUPPORT CHANNEL PER DWG 141N1560; INSTALLED REPAIR PART IAW B757 SRM 51-40-02 FIG 8 PG 1. 2L72 4F RTA2NM 20040202000202004020200020WP 2004 2 2 UPS04841713 120031231A534047585141N SUPPORT FITTING DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, INTERCOSTAL SUPPORT FITTING IS CRACKED AT STATION 1140 LONG 33R INBOARD. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D. 2L74 4F RT4A25 20040202001302004020200130 2004 2 2 AWXA200300967 420030821A2312Z010H0005119 CONTROL UNIT AIRBUSA319 A319132 3930340NM ZONE 120 FAILED A AWXAA UNSCHED LANDING GSPMULTIPLE FAILURE AFFECT SYSTEMS NO WARNING INDICATION CRCRUISE 1 WP28828AW7362 1552 DURING CRUISE SELECTIVE CALLING SYSTEM TONE SOUNDED CONTINUOUSLY WITH NOBODY CALLING, UNABLE TO RESET. PULLED SEVERAL CIRCUIT BREAKERS & TONE STOPPED. TONE SOUNDED AGAIN, UNABLE TO RESET. SELCAL TONE COULD NOT RECEIVE OVER CAPTS HEADSET THRU ACP NR 1. USED AUDIO SWITCHING TO ACP NR 3, CAPT UNABLE TO TRANSMIT OR RECEIVE. FOUND TONE IN COCKPIT TO BE FROM CABIN TO FLT DECK CALL ATT (LIGHT WOULD EXTINGUISH, BUT TONE WOULD NOT RESET). R&R CIDS DIRECTOR NR 2 & AUDIO MGT UNIT. P/N AMU, MFG; TEAM, P/N; AMU2790CB06, S/N; 1393. *SUPP* VENDORS TEST OF AUDIO MGT UNIT S/N 1393, NO FAULT FOUND. UNIT TESTED & CLEANED. TEST OF CIDS DIRECTOR S/N 010H00004402, NO FAULT FOUND. UNIT MODIFIED S/B Z010H-23-028. 2L72 4F RTA28NM 20040203000152004020300015NM 2004 2 3 ASAA0380578 120030905A33500105603 LIGHT DOUG MD80 MD83 3023681NM ROW 30 INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01982AS 53473 RNO - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED/DAMAGED AT ROW 30. SPLICED WIRING AT ROW 30. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040203000392004020300039NM 2004 2 3 ASAA0310208 120030322A53406546543509 FITTING BOEING737 737210C 1384459NM FS CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND LT UPLOCK SUPPORT FITTING AT BS 685, LT BUTTOCK LINE 70 CORRODED. REMOVED AND REPLACED SUPPORT FITTING IAW MFG DWG. (M) 2L72 4F A16WE 20040203000432004020300043WP 2004 2 3 ASAA0380574 120030902A5320593666723 STRAP DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 DURING C-CHECK, FOUND FIELD SPLICE STRAP CORRODED AT FS 1183 BETWEEN LONGERON 29L AND 29R. REPLACED STRAP. (M) 2L72 4F A6WE 20040203000442004020300044NM 2004 2 3 ASAA0310178 120030320A542065709402 FAIRING BOEING737 737298C 1384490NM NR 1 PYLON CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 DURING D-CHECK, FOUND NR 1 ENGINE PYLON FAIRING AT WING STATION 191 CRACKED. REMOVED DAMAGED SECTION AND REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040203000492004020300049NM 2004 2 3 ASAA0340003 120030108A521090100722 SNUBBER BOEING737 7374Q8 138447QNM FWD ENTRY DOOR BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01754AS 25095 SIT - DURING PREFLIGHT CHECK, THE L1 DOOR SNUBBER WAS FOUND BROKEN. SNUBBER WAS REPLACED. DOOR THEN OPERATED NORMALLY. (M) 2L72 4F RTA16WE 20040203000532004020300053WP 2004 2 3 ASAA0380634 120031012A335060030451 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 OAK LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE BETWEEN ROWS 19 AND 24. CLEANED ELECTRICAL CONNECTOR IN THE AREA. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040128000812004012800081SO 2004 1 28 C2XA03CL218 120031229A4920 ODOR EMB 145 EMB145LR 3260212SO APU DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW2748901 145501 CLE FLIGHT 2327 THE CREW REPORTED A MOMENTARILY SMOKE ODOR IN THE CABIN ON LANDING WHEN SELECTING THE APU BLEED. MAINTENANCE INSPECTED AND PLACED THE APU BLEED SYSTEM ON MEL. 2L72 4T RTT00011AT 20040128000952004012800095NM 2004 1 28 AWXA200301641 120031203A5312651630084 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, AFT SIDE AT RBL 75, WL 187. MAINTENANCE CUT OUT CRACKED SECTION OF BS 178 BULKHEAD WEB AT RBL 75, WL 187; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, FILLER AND SHIM; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG 203, PG 210-215. 2L72 4F RTA16WE 20040128000972004012800097NM 2004 1 28 AWXA200301643 120031204A532065458076 SUPPORT ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON SUPPORT ANGLE BS 295.5, STR 7 RT. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE BS 295.5, STR 7 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45807; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040128000982004012800098 2004 1 28 AALA20031473 420031227A3444849704 PSEU BOEING767 767223 1385123NM COCKPIT DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW21320AA 22321 JFK T003/27DEC03 EN ROUTE JFK-LAX AFTER TAKEOFF, LANDING GEAR MONITOR MESSAGE WITH AURAL WARNING. UNABLE TO SILENCE. AIRCRAFT RETURNED JFK LANDING WITHOUT INCIDENT. REPLACED GROUND PROXIMITY ELECTRONIC UNIT. SYSTEM GROUND CHECKED OPERATION NORMAL. 2L72 4F RTA1NM 20040128001052004012800105EA 2004 1 28 SWIA200312699 120031215A7830 TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE T/R ACTUATOR LOOSE A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07958SW 7833 ON CLIMBOUT THROUGH 15,000 FT RIGHT REV UNLOCK MESSAGE. RETURNED TO FIELD. FOUND (2) BOLTS AT LOWER INBOARD THRUST REVERSER ACTUATOR TRACK LOOSE. REPOSITIONED ACTUATOR TRACK AND TIGHTENED BOLTS IAW 78-32-05 AND 78-37-01. ALL OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040128001072004012800107SO 2004 1 28 SWIA200312701 120031216A27503431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07270YV8883 6095 120270 FLAP DISAGREEMENT ILLUMINATES DURING FLAP RETRACTION, NACELLE FLAPS APPEAR TO BE LAGGING. REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT, OPS CHECK GOOD PER EMB 120 MM 27-50-08. 2L72 4T RTA31SO 20040128001112004012800111SO 2004 1 28 SWIA200312705 120031219A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07224SW804 804 120294 EMERGENCY LIGHT NEAR MAIN CABIN DOOR INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY IAW MM 33-50-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20040128001122004012800112 2004 1 28 SWIA200312706 420031216A2210 COMPUTER EMB 120 EMB120ER 3260203SO NR 1 AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07216SW 120285 CAPTAINS AUTOPILOT WILL NOT ENGAGE. INSTALLED SERVICEABLE NR 1 AUTOPILOT COMPUTER AS NEEDED. OPS CHECKS GOOD. P/N ON 622-8315-403, S/N OFF 2901. 2L72 4T RTA31SO 20040128001162004012800116 2004 1 28 SWIA200312708 420031221A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07410SW5418 5418 7066 AP PITCH TRIM CAUTION MESSAGE AT 6500 FEET MSL (2300 AGL) ON FINAL. REMOVED AND REPLACED FCC 4000 CARDS 1A & 2A IAW MM 22-12-14. OPS CHECK GOOD. P/N: 622-9815-704, S/N OFF: 854. 2L72 4F RTA21EA 20040128001182004012800118SO 2004 1 28 SWIA200312710 120031221A2750 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07188SW 120039 RIGHT INBOARD FLAP WON'T COME UP. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06, OPS CHECK GOOD. P/N ON 307500-1007, S/N OFF 0133. 2L72 4T RTA31SO 20040128001192004012800119EA 2004 1 28 SWIA200312711 120031225A2751855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07459SW 7782 AFTER TAKEOFF AT FLAP RETRACTION RECEIVED FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED RIGHT BPSU IAW CRJ AMM 27-51-10, OPS CHECK GOOD. 2L72 4F RTA21EA 20040127001522004012700152NM 2004 1 27 ASAA0310200 120030321A5340101362001 ATTACH ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND ATTACH ANGLES AT BS 947, STRINGER 25L-25R CORRODED. REMOVED AND REPLACED ANGLES PER SRM. (M) 2L72 4F RTA16WE 20040127002412004012700241WP 2004 1 27 ASAA0380603 120031006A335060030451 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 19. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040128000662004012800066NM 2004 1 28 QXEA200301585 120031226A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 500 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09408QX 4050 SEA- ON FLIGHT 2331 FLAP POWER CAUTION LIGHT ILLUMINATED WITH FLAP HANDLE SELECTED TO 15 DEGREES AND FLAPS INDICATING 10 DEGREES. CIRCUIT BREAKER RESET PER CHECKLIST AND CAUTION LIGHT EXTINGUISHED. RESET IAW SL-DH8-401-SL-31-01R13. GROUND RAN AIRCRAFT TO CHECK FLAPS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040128000922004012800092NM 2004 1 28 AWXA200301638 120031219A7110314A10102 INLET BOEING737 737301 1384611NM NR 1 ENGINE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK NR 1 ENGINE NOSE COWL WAS FOUND DELAMINATED AT 12:00 POSITION. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-08, FIG 7 & 9, PG 28-29, 47-49. 2L72 4F RTA16WE 20040128000942004012800094NM 2004 1 28 AWXA200301640 120031202A5720656827017 SUPPORT ANGLE BOEING737 73733A 1384673NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND ON ANGLE AT RT WING INBOARD UPPER TRAILING EDGE PANEL, JUST INBOARD OF NR 5 SPOILER AT WBL 71.24. MAINTENANCE STOP DRILLED CRACK ON ANGLE AT RT WING INBOARD UPPER TRAILING EDGE PANEL WBL 71.24; FABRICATED A REPAIR ANGLE PER DWG 65-68270; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11 FIG 1 PG 1-5. 2L72 4F RTA16WE 20040128001292004012800129 2004 1 28 0302181237 420031228A2330 PROJECTOR DOUG DC10 DC1030 3023501WP CABIN CONTAMINATED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01237NW 47844 STRONG ELECTRICAL BURNING ODOR DETECTED AT ROW 22CDEF. TURNED OFF PROJECTION SYSTEM AND ODOR DISSIPATED. FLT CONTINUED AND LANDED WITHOUT INCIDENT. RAN PROJECTOR FOR ONE HOUR, INSPECTED OVERHEAD CABIN ABOVE PROJECTOR, AND CLEANED LINT FROM PROJECTOR EXHAUST VENT. COULD NOT DUPLICATE ODOR. 2L73 4F A22WE 20040128001322004012800132NM 2004 1 28 DHL2003747015 120031230A5310 DOOR FRAME BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 MAIN CARGO DOOR FRAME AFT ACT AREA HAS CRACK. REPAIRED IAW AERONAUTICAL SOLUTIONS REPORT 03-011 IR DTD 12/30/03. MATERIAL USED 2024-T3 .090 PO 21582, FASTENERS USED 1103-11 BOLTS, AND HL62-6-9. THIS REPAIR IS A MAJOR REPAIR. 2L73 4F A3WE 20040128001422004012800142NM 2004 1 28 AWXA200301646 120031230A33501000679 LIGHT BOEING737 737277 1384570NM L2 DOOR WORN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28186AW 22653 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT OVER THE L-2 DOOR FLICKERS ON AND OFF DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE L-2 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040128001432004012800143NM 2004 1 28 AWXA200301647 120031204A532065479577 INTERCOSTAL BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT INTERCOSTAL (WEB) BETWEEN BS 847 AND BS 867, RBL 21 AT DOOR CUTOUT FRAME. MAINTENANCE CUT OUT CORRODED WEB BETWEEN BS 847 AND BS 867, RBL 21; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12 PG 1. 2L72 4F RTA16WE 20040128001732004012800173EU 2004 1 28 UPS04141677 120031230A3350 LIGHT AIRBUS300 A300B4622R 3930312EU EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01138UP 0821 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS, DISARM LIGHT INOP. REPLACED DISARM LIGHT ASSY IAW ESPM 20-45-11. OPS CHECK GOOD. 2L72 4F RTA35EU 20040129000132004012900013EA 2004 1 29 MASA200300525 120031231A3350 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717275 7275 ASH FLT 6156 PHX-SBA, EMERGENCY ESCAPE PATH MARKING SYSTEM INOP. MX RECONNECTED THE FLOOR STRIP, OPS CHECK GOOD. NO PART USED. 2L72 4F RTA21EA 20040129000152004012900015EA 2004 1 29 MASA200300523 120031231A3350 COVER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MISSING A MASAK NONE O OTHER ININSP/MAINT 1 SW0775987 7405 ASH FLT 2959 PHL-SDF, EMERGENCY LIGHT COVER ON THE FLOOR MISSING AND LIGHT DISCONNECTED. MX REPLACED LIGHT ASSY. 2L72 4F RTA21EA 20040129000302004012900030EU 2004 1 29 MALA030585 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 6A & 6B FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEATS 6A, 6B IAW MESABA EO A25031 DATED 6/FEB/01. REFER TO NR 1196437 FOR DETAIL. A/C RELEASE DATE 12/31/2003. 2H74 4F RTA49EU 20040129000432004012900043EU 2004 1 29 MALA030601 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 15B FRAME CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAME 15B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000452004012900045EU 2004 1 29 MALA030593 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 11A & 11B FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 11A, 11B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000482004012900048EU 2004 1 29 MALA030583 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEAT 5B FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 5B IAW MESABA EO A25031 DATED 6 FEB 2001. 2H74 4F RTA49EU 20040129000512004012900051EU 2004 1 29 MALA030589 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 8A & 8B FRAMES CRACKED. ACCOMPLISHED WELD REAPAIRS ON SEAT FRAMES 8A, 8B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000522004012900052EU 2004 1 29 MALA030590 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 8D & 8E FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 8D, 8E IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20031014000382003101400038EU 2003 10 14 MALA030424 120030914A760020GA RELAY SAAB SF340 340B 7860101EU DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15363XJ DURING FLIGHT NR 3168, AFTER TAKEOFF WHEN THE GEAR WAS RETRACTED THE FLT STOP LIGHT ILLUMINATED AND KNOB POPPED UP. AIR RETURN TO DTW. MAINTENANCE PERFORMED TROUBLESHOOTING OF FLIGHT IDLE STOP SYSTEM, IAW MM 76, FOUND RELAY 20GA OUTER SHELL DAMAGED, REPLACED RELAY 20GA, IAW MM, PERFORMED GEAR SWINGS, ALL CHECKS GOOD. 2L72 4T RTA52EU 20031014000392003101400039NE 2003 10 14 MALA030421 220030912A7200LF5071F ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 MALFUNCTIONED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15509XJ E2321 DURING FLT 3691, NR 3 ENGINE LOST OIL PRESSURE. SHUTDOWN INFLIGHT. MAINTENANCE REMOVED AND REPLACED NR 3 ENGINE ASSEMBLY IAW TASK CARD 7100-502. IAW TASK CARD 7100-502.LK AND OPS CHECKS GOOD. PN ON AND OFF LF507-1F SNON P07811 SN OFF LF-07629. 2H74 4F4 FRTA49EU E6NE 20031014000642003101400064NM 2003 10 14 SWAA032188 120031001A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 780, STR 18L AND STR 18 R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014000722003101400072 2003 10 14 SWAA032202 420031002A256565C19901 CABLE BOEING737 7375H4 138449DNM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20031014001002003101400100NM 2003 10 14 SWAA032143 120030923A53306547952 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR CRACKED ON OUTER SKIN AT UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001042003101400104NM 2003 10 14 SWAA032139 120030923A2781285A12001 FSEU BOEING737 7377H4 1384404NM E/E COMP FAULTY A SWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW29783SW 29809 AIR TURN BACK, L/E SLATS WILL NOT RETRACT. REMOVED AND REPLACED FSEU PER MM. 2L72 4F RTA16WE 20031008000102003100800010NM 2003 10 8 03FDEA01555 120030913A3260189915 SENSOR BOEING727 727200 138407ENM ZONE 700 FAILED A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25487FE 21490 AT FL270 AND .84 MACK, THE RED AND GREEN RIGHT GEAR LIGHTS ILLUMINATED. THE LANDING GEAR HANDLE WAS PLACED UP. ALSO THE LEFT GREEN GEAR LIGHT WOULD NOT TEST INFLIGHT. PER FLIGHT CREW DEBRIEF: WHEN GEAR HANDLE WAS MOVED FROM "OFF" TO "UP" THERE WAS NO CHANGE. ALL INDICATION RETURNED TO NORMAL WITH GEAR EXTENSION AND LANDING WAS UNEVENTFUL. R&R'D UPLOCK PROX SENSOR PER MM 32-61-081-4. OPS NORMAL. 2L73 4F RTA3WE 20031008000222003100800022WP 2003 10 8 ABXA030362 120030912A3260 CONNECTOR DOUG DC9 DC932 3022066WP MLG DOWNLOCK LOOSE A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23989AX 47314 NO INDICATION OF NOSE GEAR DOWN AND LOCKED. CHANGED LIGHT BULBS AND RAN ABNORMAL CHECK-LIST. DETERMINED INDICATION PROBLEM. FOUND CONNECTOR PLUG LOOSE ON THE NOSE DOWNLOCK SWITCH. CLEANED AND RECONNECTED PLUG. SYSTEM OPS CHECK GOOD IAW DC-9 MM 32-60-00. 2L72 4F A6WE 20031010000342003101000034NM 2003 10 10 USAABB03143 120030821A5210800637 DISC BOEING757 757225 1384959NM L2 DOOR RUPTURED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 FOUND L2 DOOR EMERGENCY POWER RESERVOIR READING ZERO. MAINTENANCE FOUND THE BLOW-OUT DISC RUPTURED, REPLACED IT AND SERVICED THE BOTTLE. (M) 2L72 4F RTA2NM 20031010000742003101000074SO 2003 10 10 UPV2003F00000 120030403A321365319004 STRUT PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA MLG CRACKED E UPVAO OTHER O OTHER NRNOT REPORTED 1 CE0983416 288116160 EARS BROKEN OFF ON LANDING. STRUT DROPPED OUT ON BALLOON. NO OTHER DAMAGE TO AIRCRAFT. CHECKED THE OTHER STRUT AND FOUND CRACKED, REPLACED BOTH. 1L71 3O3 O 2A13 E274 20031014001062003101400106NM 2003 10 14 SWAA032137 120030923A53406557463 BRACKET BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR RETAINER BRACKET LOOSE. SECURED RETAINER PER MM. 2L72 4F RTA16WE 20031014001152003101400115NM 2003 10 14 SWAA032152 120030924A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014001232003101400123NM 2003 10 14 SWAA032169 120030928A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031014001372003101400137NM 2003 10 14 SWAA032056 120030915A7603315A1040 THROTTLE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 2 ENGINE FOD A SWAABA EMER. DESCENT UNSCHED LANDING CY F.O.D. ENGINE STOPPAGE CLCLIMB 1 SW29638SW 27711 856162 DECLARED EMERGENCY, AIR TURNBACK, IN FLIGHT SHUTDOWN, NR 2 ENGINE THROTTLE LEVER COULD NOT BE REDUCED BELOW 89.5 PERCENT. FOUND FOREIGN OBJECT DEBRIS INSIDE THROTTLE QUADRANT BOX. REMOVED DEBRIS, OPS CHECKED GOOD PER MM. 2L72 4F4 FRTA16WE E2GL 20031014001392003101400139NM 2003 10 14 SWAA032054 120030915A335065C27093 LIGHT BOEING737 7373H4 1384600NM AFT CABIN DOORS INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED A2 CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20031014001522003101400152NM 2003 10 14 SWAA032075 120030917A531465621258 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED 1/4D CHECK, FOUND RT KEELBEAM CORRODED BETWEEN BS 500D AND BS 520,STR 28R. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20031014001852003101400185NE 2003 10 14 SWAA032112 220030922A7230JT8D9AHK COMPRESSOR BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE STALLED A SWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW29096SW 23055 707413 ABORTED TAKEOFF, ALL NR 1 ENG INDICATORS ROLLED BACK WITH EPR SET AT 1.82. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 F A16WE E2EA 20040202002922004020200292NM 2004 2 2 2003753509 120031230A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, FUSELAGE EXTERIOR LT BS 720E TOP SEAM SHOW DENTED AREA OUT OF LIMITS STR 19L. REMOVED FAIRING 5338-3339, LT WING ANTI ICE DUCT STA 90.3-130, LT WING ROOT L/E REMOVED/DISC HYD LINES WS 90.5 TO 130.7, DUCT A/C LT FUSELAGE. REMOVED FASTENERS & MAKE CUT OUT DAMAGED AREA 3 INCHES. 0-3 (6) PARTS MADE FROM 2024T3.063 PO 900355 DIM (DOUBLER) 10.5 X 10 INCH (FILLER) 3 X 10 INCH & 7.5 X 10.5 INCH. TREATED & PRIMED PARTS & AREA IAW B727 SRM 51-10-2. INSTALLED PARTS REPAIR IAW B727 SRM 53-30-3 (6). INSTALLED LT WING ROOT L/E ASSY, INSTALLED HYD LINES FROM 90.3 TO 130.7, PNEU DUCTING (LT WING ANTI ICE), REMOVED & REINSTALLED L/W STA WING FROM L/E STA 0 TO L/E STA 171. 2L73 4F A3WE 20040203000112004020300011NM 2004 2 3 ASAA0310176 120030320A5411657377391 FRAME BOEING737 737298C 1384490NM NR 2 NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 DURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 124.25 CHAFED. REMOVED AND REPLACED FRAME IAW SRM. (M) 2L72 4F RTA16WE 20040203000202004020300020 2004 2 3 ASAA0380590 420030914A25653961896501 LANYARD DOUG DC9 DC982 3022082WP L1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20040203000372004020300037NM 2004 2 3 ASAA0310207 120030322A54106573771 RIB BOEING737 737210C 1384459NM NR 2 NACELLE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND NR 2 ENGINE COWL RIB REPAIR AT NACELLE STATION 139.04 GOUGED. REMOVED PREVIOUS REPAIR AND INSTALLED DOUBLER IAW SRM. (M) 2L72 4F A16WE 20040203000842004020300084 2004 2 3 ASAA0380560 420030821A25653961896501 LANYARD DOUG DC9 DC982 3022082WP R1 DOOR SLIDE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01953AS 49386 SEA PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND BROKEN. REPLACED LANYARD. (M) 2L72 4F A6WE 20040203003272004020300327EA 2004 2 3 MASA200300483 120031210A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW0727173 7173 ASH 2686 PHL, CREW REPORTED, UNABLE TO OPEN THE PAX DOOR. MX MANAGED TO OPEN THE DOOR, LUBED THE LATCHING MECHANISMS AND PERFORMED THE OPERATIONAL CHECK ON THE DOOR. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040203003292004020300329EA 2004 2 3 MASA200300486 120031212A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0727318 7318 ASH 6231 SAT, RETURNED TO FIELD. LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. A/C FERRIED TO PHX FOR MX 12/12/2003. MX COULD NOT DUPLICATE DISCREPANCY. NO PARTS USED. 2L72 4F RTA21EA 20040203000182004020300018 2004 2 3 ASAA0380579 420030905A25653961896501 LANYARD DOUG DC9 DC982 3022082WP L1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS 49111 PREFLIGHT CHECK, FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20040203000212004020300021 2004 2 3 ASAA0380591 420030914A25653961896501 LANYARD DOUG DC9 DC983 3022083WP R1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 ON PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040203000282004020300028WP 2004 2 3 ASAA0380547 120030730A335060030451 LIGHT DOUG DC9 DC983 3022083WP ROWS 29 & 30 INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FOUND INOPERATIVE BETWEEN ROWS 29 AND 33. REPLACED BATTERIES IN AFT RT POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000292004020300029WP 2004 2 3 ASAA0380559 120030819A33500105603 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 PREFLIGHT CHECK, FOUND ONE WHITE EMERGENCY FLOOR TRACK LIGHT INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000752004020300075WP 2004 2 3 ASAA0380552 120030812A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS351946943 49111 PHX PREFLIGHT CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REPLACED POWER SUPPLIES, BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040204000072004020400007NM 2004 2 4 DHL2003753509 120031230A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DISCREPANCY DURING (C) CHECK. FUSELAGE EXTERIOR LT. BS720E. TOP SEAM SHOW DENTED AREA OUT OF LIMITS. ST19L. C/A; REMOVED FAIRING 5338-3339, LT WING ANTI ICE DUCT STA 90.3-130, LT WING ROOT LE REMOVED DISC HYDRAULIC LINES WS 90.5 TO 130.7, DUCT AC LT FUS.. REMOVED FASTENERS AND MAKE CUT OUT DAMAGED AREA (3 INCHES). (6) PARTS MADE FROM 2024T3.063 PO NR 900355 DIM. (DOUBLER) 10.5 INCH X 10 INCH (FILLER) 3 INCH X 10 AND 7.5 INCH X 10.5 INCH(6). TREATED AND PRIMED PARTS AND AREA. INSTALLED PARTS REPAIR (6). INSTALLED LT WING ROOT LE ASSY, INSTALLED HYD LINES FROM 90.3 TO 130.7, PNEN. DUCTING (LT WING ANTI ICE) REMOVED AND REINSTALLED L/W. STA W. RING FROM LE STA 0 TO LE STA 171. 2L73 4F A3WE 20040204000122004020400012NM 2004 2 4 C1HA200392007 120031129A3350 BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 OVERHEAD EMERGENCY LIGHT BETWEEN L2 AND R2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW 727 MM 33-50-22 ALL OPS NORMAL. 2L73 4F A3WE 20040204000242004020400024NM 2004 2 4 DHL2003748012 120031125A3350100067 LIGHT BOEING727 727225 1384077NM PAX DOOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01748DH 22440 EMERGENCY EXIT LIGHTS OVER MAIN ENTRY DOOR ARE INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT IAW TSI M/M 33-50-101. OPS CHECKED GOOD. 2L73 4F A3WE 20040204000342004020400034NM 2004 2 4 QXEA200301272 120031012A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 200 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09403QX 4037 PDX-ON FLIGHT NUMBER 2358, FLAP POWER CAUTION LIGHT ILLUMINATED AFTER ENGINE START. RESETTING CIRCUIT BREAKER L7 ACCORDING TO CHECKLIST DID NOT CURE PROBLEM. CYCLED FLAP CONTROL CIRCUIT BREAKER AND RESET NON-VOLATILE MEMORY AT MAINTENANCE PANEL. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040204000402004020400040EU 2004 2 4 AWXA200301259 120031011A5522D5528000100052 SKIN AIRBUS320 A320231 3930325EU LT ELEVATOR DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-03 CHECK THE LT ELEVATOR UPPER SKIN WAS FOUND DISBONDED AT ELEV STA 406.4. MAINTENANCE CUTOUT DAMAGE ON LT ELEVATOR UPPER SKIN AT ELEV STA 406.4; CLEANED AND PREPARED SURFACE; PERFORMED BOND REPAIR IAW A320 SRM 55-21-11, PG. 233-236, FIG. 206. 2L72 4F RTA28NM 20040204000462004020400046EA 2004 2 4 03287646 120031014A3350 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSTRIPPED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27646BR 7392 DURING INSPECTION THE EMERGENCY LIGHTS WERE FOUND TO OPERATE WITH AIRCRAFT POWER APPLIED. MAINTENANCE PERSONNEL FOUND EMERGENCY LIGHT CIRCUIT BREAKER OPEN AND RESET IT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040204000482004020400048NM 2004 2 4 HNAA030054 120031012A5310 DOOR FRAME DHAV DHC8 DHC8102 2809003NM MLG DAMAGED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07937HA392295741 148 WHEN LANDING GEAR WAS RETRACTED THE LEFT MAIN GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR AND LIGHT WENT OUT. AIRCRAFT RETURNED TO FIELD. FOUND THE BOLT FOR THE LT FWD MAIN GEAR DOOR PUSH ROD TO DOOR ATTACH POINT WORN INTO AND JAMMED AGAINST THE ADJACENT NACELLE FRAME. REPLACED THE FRAME AND THE LT FWD MAIN GEAR DOOR. 2H72 4T RTA13NM 20040204000502004020400050WP 2004 2 4 UPS03841384 120030922A534058942822 SUPPORT FITTING DOUG DC8 DC873F 302199FWP LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, A-PIT DOOR FWD. LOWER FORWARD T-BOLT SUPPORT FITTING HAS A BACKUP FITT ING CORRODED BEYOND LIMITS AT STA. 290 AT LONG. 33R. REMOVED AND REPLACED FITTING IAW DWG. 5894282,AND SRM. 53-2-0 FIG. 2D 2L74 4F RT4A25 20040203003242004020300324EA 2004 2 3 MASA200300473 120031203A2781 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LE FLAPS ILLUMINATED A MASAO OTHER J WARNING INDICATION DEDESCENT 1 SW0775993 7372 ASH 2794 PHL-YUL, FLAP FAIL CAUTION MSG ON DESENT CONTRACT MX PERFORMED MAINT PROCEDURE PART A OF AD 98-20-01. SYSTEM RESET AND FLAPS OPERATED NORMAL. 2L72 4F RTA21EA 20040203003362004020300336EA 2004 2 3 MASA200300507 120031222A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM IMBALANCED A MASAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SW07773027150 7150 7302 ASH 6164 SLC, ABORTED T/O FOR NR 1 ENG N2 VIB INDICATION DURING TAKEOFF. MX IS TROUBLESHOOTING. MX REPLACED THE EDP. OP CHECKS GOOD. 2L72 4F RTA21EA 20040204000252004020400025NM 2004 2 4 AWXA200301303 120031024A7931SEL0C4W INDICATOR BOEING737 73733A 1384673NM OIL PRESSURE INACCURATE A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28164AW520784067 23625 PHX - - FLT 0769 - ON TAKEOFF ROLL OUT OF PHX EN ROUTE FOR SMF NR 1 ENGINE OIL PRESSURE WAS LOW, REJECTED TAKEOFF, ON TAXI BACK TO GATE OIL PRESSURE RETURNED TO NORMAL. MAINTENANCE INSPECTED THE NR 1 ENGINE OIL PRESSURE WIRING, NO DISCREPANCIES WERE NOTED, REMOVED AND REPLACED THE NR 1 ENGINE OIL PRESSURE INDICATOR, ENGINE RUN OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST OF OIL PRESSURE INDICATOR S/N 464A WAS NO FAULT FOUND. UNIT TESTED AND INSPECTED IAW CMM 31-00-31. 2L72 4F RTA16WE 20040204000412004020400041EU 2004 2 4 AWXA200301260 120031010A5411D54530034200 RIB AIRBUS320 A320231 3930325EU NR 2 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-03 CHECK A 1.1250 INCH CRACK WAS FOUND LOWER END OF RIB NR 13 ON NR 2 PYLON AT AFT FIXED FAIRING. MAINTENANCE REMOVED NR 13 RIB AT AFT FIXED FAIRING, NR 2 PYLON; FABRICATED A NEW REPLACEMENT RIB IAW DWG D54530034200; INSTALLED REPAIR PART IAW 54-54-12, PG. 2 AND 5, FIG. 1. 2L72 4F RTA28NM 20040204000542004020400054NM 2004 2 4 AWXA200301268 120031001A3520417N381016 CONTAINER BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE LAV O2 MASK WILL NOT TEST A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK THE FORWARD LAVATORY OXYGEN MASK DOOR CONTAINER TEST STOP BUTTON FAILED TEST. MAINTENANCE REMOVED AND REPLACED FORWARD LAVATORY OXYGEN MASK ASSEMBLIES IAW BMM TASK 35-22-31-004-059, AND TASK 35-22-31-404-051, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040204000552004020400055 2004 2 4 RAIA00310260 420031015A23507511001945 AUDIO PANEL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03558HK127541784 41071 5631-STL- AFT F/A HEAD SET INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AUDIO CONTROL PANEL. 2L72 4T3 TRTA41NM E2WE 20040204000842004020400084NM 2004 2 4 AWXA200301275 120031009A53206546812169 FLOOR SUPPORT BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 967 TO BS 986.5, LBL 17.61. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOOR SUPPORT AT BS 967 TO BS 986.5, LBL 17.61; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1, AND 44-45, FIG. 12 AND 14. 2L72 4F4 FRTA16WE E2GL 20040204001132004020400113NM 2004 2 4 F3LA200300150 120031020A5411 FRAME BOEING737 737301 1384611NM NR 1 PYLON CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03578US 2672 23257 DURING C-5 CHECK, INSPECTION REPORTED AFT LOWER END OF NR 1 ENGINE PYLON AT STA. 363 CRACKED. REPLACED NR 1 ENGINE AFT LOWER END "A" FRAME IAW SRM 51-40-02. 2L72 4F RTA16WE 20040204001462004020400146NM 2004 2 4 EIA2003138 120031020A5414 SKIN BOEING747 747212B 1384886NM NR 2 PYLON CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 INSIDE LOWER SURFACE OUTBOARD SIDE NR 2 PYLON APPROX. 15 INCHES AFT OF ENGINE REAR MOUNT HAS LARGE CHAFED AREA. OB SIDE OF NR 2 PYLON SKIN REPAIRED IAW ECRA 482-54-177-2. 2L74 4F A20WE 20040204001942004020400194 2004 2 4 SWIA200312568 420031028A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07250YV 120250 RED AP LIGHT ON AFCP KEPT FLASHING WITH ASSOCIATED TRIPLE CHIME IN FLIGHT. REPLACED CAPTAIN'S SIDE AUTOPILOT COMPUTER. OPS CHECK GOOD ON GROUND CHECK. 2L72 4T4 TRTA31SO E20NE 20040203000702004020300070WP 2004 2 3 ASAA0380561 120030819A2621 LINE DOUG DC9 DC982 3022082WP NR 1 FIRE BOTTLEBLOCKED A ASAAO OTHER L NO TEST NRNOT REPORTED 1 NM01935AS 49236 PDX LINE CHECK, NR 1 FIRE BOTTLE WAS DISCHARGED TO EXTINGUISH APU FIRE. DISCOVERED LINE WAS PARTIALLY BLOCKED WITH DISCHARGE HEAD SHRAPNEL. REPLACED FLEX LINE. (M) 2L72 4F A6WE 20040203000782004020300078WP 2004 2 3 ASAA0380566 120030828A532099367183 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 OAK - DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT FS 1309-1322 ON LEFT SIDE BETWEEN LONGERON L28 AND L27. REPLACED INTERCOSTAL. (M) 2L72 4F A6WE 20040203000802004020300080WP 2004 2 3 ASAA0380798 120031119A5347593054790 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND RT SEAT TRACK IS GOUGED AT FS 200-275. REPLACED TRACK IAW SRM 53.05. (M) 2L72 4F RTA6WE 20040130002362004013000236EU 2004 1 30 MALA040102 120031226A5310 SPAR SAAB SF340 340B 7860101EU LT MLG WW CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, LT MLG W/W FWD RT SPAR ANGLE AND RIVETS CHAFED. MX REMOVED CHAFED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW MESABA EO S54071. A/C RELEASE DATE 1/6/04. REFER TO NR 1195871 FOR ADDITIONAL INFO. 2L72 4T RTA52EU 20040203000232004020300023WP 2004 2 3 ASAA0380598 120030929A56104616968501 ROD DOUG DC9 DC983 3022083WP WINDOW DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 SJC - PREFLIGHT CHECK, FOUND LT CAPTAINS SLIDING CLEARVIEW WINDOW ACTUATING ROD FOUND DISCONNECTED. RECONNECTED ACTUATING ROD. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000512004020300051NM 2004 2 3 ASAA0310239 120030327A3350873203041 CONTROL MODULE BOEING737 737210C 1384459NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 AFTER RECON FOUND EMERGENCY FLOOR TRACK LIGHTS BLINKING. REMOVED AND REPLACED MID AND AFT CABIN CONTROL MODULES, THEN LIGHTS OPERATED NORMAL. (M) 2L72 4F A16WE 20040203000562004020300056NM 2004 2 3 ASAA030164 120030320A532065516983 STRINGER CLIP BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND STRINGER TIE AT BS 907, STRINGER 19L CORRODED. REMOVED AND REPLACED STRINGER TIE IAW SRM. (M) 2L72 4F A16WE 20040203000792004020300079WP 2004 2 3 ASAA0380794 120031119A532199579212 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS FASTENER HOLE BLOWN OUT AT FS 826-926. INSTALLED DOUBLER IAW SRM 53-01. (M) 2L72 4F RTA6WE 20040202001342004020200134NM 2004 2 2 UPS04541726 120031231A5347 SEAT TRACK BOEING757 75724APF 1384969NM EXPANSION LINK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE: C, CORROSION ON EXPANSION LINK SEAT TRACK BS 880 - 900 BL 0 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED LINK, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 53-00-52, SRM 51-10-02 & SRM 51-40-02. 2L72 4F RTA2NM 20040203000472004020300047WP 2004 2 3 ASAA0380569 120030829A53119957739137 FRAME DOUG DC9 DC982 3022082WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 DURING C-CHECK, FOUND FRAME CORRODED AT FS 1287 BETWEEN LONGERON 28L AND 28R. REPLACED DAMAGED SECTION IAW SRM 53-03 AND 53-01. (M) 2L72 4F A6WE 20040203000582004020300058NM 2004 2 3 ASAA0310162 120030320A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND SEAT TRACK AT BS 663-727A, LT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM. (M) 2L72 4F A16WE 20040203001072004020300107NM 2004 2 3 UPS04441765 120031231A532065B05002270 REVEAL BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C - BS 1664, BETWEEN STR 24 - 26R R4 DOOR CUTOUT FWD LWR REVEAL FOUND CRACK. DOOR CUTOUT REVEAL REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20040203003342004020300334EA 2004 2 3 MASA200300500 120031217A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA PAX INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07511MJ 10104 ASH 7120 DEN-BNA, THE CREW WAS UNABLE TO CLOSE THE DOOR. MX WAS CALLED. MX WENT OUT TO THE A/C AND OPERATED THE DOOR WITH NO PROBLEMS. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040203000352004020300035NM 2004 2 3 ASAA0310204 120030322A531565671406 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 540-727B, LT BUTTOCK LINE 45 CORRODED. REMOVED DAMAGE AND REPAIRED IAW EA. (M) 2L72 4F A16WE 20040203000412004020300041NM 2004 2 3 ASAA0310184 120030321A531565671407 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 663-727, LT BUTTOCK ONE 25 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM. (M) 2L72 4F A16WE 20040203000552004020300055NM 2004 2 3 ASAA0310205 120030322A78306573778 FAIRING BOEING737 737210C 1384459NM THRUST REVERSER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER FAIRING AT NACELLE STATION 185 DENTED. REMOVED AND REPLACED FAIRING IAW SRM. (M) 2L72 4F A16WE 20040204002002004020400200EA 2004 2 4 SWIA200312574 120031101A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07446SW5688 4045 7666 SPOILER FAULT MESSAGE INBOARD GROUND SPOILERS AND FLIGHT SPOILERS. REMOVED AND REPLACED NR 2 SECU IAW 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20040204002102004020400210EU 2004 2 4 038161 120031111A3020 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT AIR VALVE ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1719XS 340A019 122 FLIGHT 4593 PIT-TOL. DURING FLIGHT, THE RT AIR VALVE WARNING LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETARDED THE RT POWER LEVER AND THE WARNING LIGHT WENT OUT. AC RETURNED TO PIT AND TAKEN OUT OF SERVICE 11-11-03 AT 1655 (LT). 2L72 4T4 TRTA52EU E8NE6 20040204002162004020400216WP 2004 2 4 UPS03841555 120031022A53309755878 DOUBLER DOUG DC8 DC873F 302199FWP LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, FWD LOWER CARGO INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN STATION 360 TO 400 LONG. 29R TO LONG. 35L. REMOVED, FABRICATED AND REPLACED DOUBLER I.A.W. DWG. 9755878 AND SRM. 51-1-21 2L74 4F RT4A25 20040204002252004020400225WP 2004 2 4 DHL2003809005 120031112A5270 HANDLE DOUG DC8 DC873F 302199FWP CARGO DOOR UNSECURE A DHLAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 SO01604AL 46047 AT BEGINNING OF TAKEOFF ROLL BELLY DOOR LIGHT ILLUMINATED. DURING TAXI DOOR LIGHT ILLUMINATED INTERMITTENTLY. FOUND B PIT DOOR HANDLE NOT SECURED. RE-SECURED HANDLE. OPS CHECKED NORMAL IAW M/M 25-51-0. REJECTED T/O RWY 27 AT 271,000 LBS. AT 70 KTS. / ZONE 2. PERFORMED REJECTED T/O CHECK IAW DC-8 SM/M 05-51-0. BRAKE TEMPERATURES CHECKED WITHIN LIMITS. AIRCRAFT OK FOR SERVICE. 2L74 4F RT4A25 20040204002332004020400233WP 2004 2 4 FEF200300003 120031010A57115911301 SPAR CAP DOUG DC9 DC982 3022082WP RT WING CORRODED W FE5FK NONE O OTHER ININSP/MAINT 1 WP03 16038 53167 DURING THE C7 CHECK, PERFORMING THE TASK NR 0805, AND LOCAL CORROSION WAS FOUND AT RT LOWER SPAR CAP. XRS262~XRS267 L=5" W=1.2" D=0.8" ACTION TAKEN: REQUEST MFG ASSISTANCE FOR PERMANENT REPAIR AND IAW MFG RESPONSE REPAIR THE CORROSION. MANUFACTURER OFFERED FAA FORM 8110-3 AND APPROVED REPAIR PROCESS. 2L72 4F A6WE 20040204002352004020400235NM 2004 2 4 AALA20031384 120031204A2820 FUEL TANK BOEING777 777223 1385213NM LEFT MALFUNCTIONED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21772AN 29580 EN ROUTE SJC-NRT AN UNWANTED FUEL TRANSFER AS A GRADUAL DECREASE IN FUEL NOTED IN LEFT TANK AND STABILIZED AT 63300 POUNDS WHILE INCREASING IN RIGHT TANK FROM 64500 TO 66900 WHILE USING CENTER TANK. LANDED LAX WITHOUT INCIDENT. A/C FERRY TO DFW FOR FURTHER EVALUATION.--OPEN-- 2L72 4F RTT00001SE 20040205000012004020500001NM 2004 2 5 DHL2003721010 120031114A5270 SWITCH BOEING727 727228 1384083NM PWA JT8 JT8D* NE ANNUNCIATOR LACK OF LUBE A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01721DH 19545 AT 500 FT OFF CVG, FORWARD ENTRY ON S/O'S ANNUNCIATOR PANEL ILLUMINATED. NO CHANGE IN PRESSURE DIFFERENTIAL. AT APPROXIMATELY 1000 FT FORWARD ENTRY LIGHT EXTINGUISHED. INSPECTED AND LUBED SWITCH. TESTED IAW B-727 M/M CHAPTER 52. GROUND CHECKED NORMAL AT THIS TIME. 2L73 4F4 FRTA3WE E2EA 20040205000062004020500006NM 2004 2 5 P5CA0300986 120031114A7931SEL0C4G INDICATOR BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23923FT 22769 702193 ON ENGINE START NR 2 INDICATED NO OIL PRESS ON F/E PANEL OR FORWARD PANEL. REPLACED NR 2 ENGINE OIL PRESS INDICATOR SYSTEM CHECKS GOOD IAW MM 79-30-00. 2L74 4F4 FRTA20WE E3NE 20040205000112004020500011NM 2004 2 5 03FDEA01920 120031117A7920 B-NUT DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ENGINE OIL LOOSE A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25607FE 48547 ABOUT 2 HRS AFTER DEPARTURE NOTICED NR 1 OIL QTY DROPPING AND GOING TO ZERO. AT THAT TIME PRESSURE AND TEMP WERE NORMAL, 1 HR AFTER THAT NR 1 OIL PRESSURE STARTED A VERY SLOW DROP, EVENTUALLY TURNED AMBER. DIVERTED TO BKK. ON DESCENT PRESSURE DROPPED TO RED LINE, DID ENGINE SHUTDOWN IN FLT. CHECK LIST AND SECURED NR 1 ENG LANDING UNEVENTFUL ON ARR FOUND OIL QTY AT TANK ZERO TOP UP 23 QTS. ENG MOTORIZED FOR OIL LEAK CHECK FOUND OIL LINE FROM OIL PRESS TRANSMITTER TO OIL PRESS SW LOOSE WHICH CAUSED OIL LEAK. TIGHTENED B-NUT AND LEAK CHECKED PERFORMED. NO LEAK FOUND. MASTER CHIP DETECTOR INSP FOR METAL, NO ABNORMALITY FOUND. 2L73 4F4 FRTA22WE E13NE 20040205000142004020500014EU 2004 2 5 YENA200338 120031117A71602607MK2 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENG VSV FAILED A YENAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15507JB124153787 1240 V10739 ENGINE ONE COMPRESSOR VANE ECAM ON TAKEOFF AT ABOUT 50 KTS. DID LOW SPEED RTO. REMOVED AND REPLACED NR 1 ENG VARIABLE STATOR ACTUATOR IAW AMM 75-32-41, AS PART OF TSM 75-30-00. PERFORMED TEST NR 11 (HIGH POWER ASSURANCE TEST) ON NR 1 ENGINE IAW 71-00-00-710-013A, OPS CHECK GOOD. NO ABNORMAL INDICATIONS WARNINGS NOTED. 2L72 4F4 FRTA28NM E40NE 20040205000282004020500028NM 2004 2 5 EIA2003149 120031105A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 CRACK IN FS 300 FRAME RADIATING FROM LT STRINGER 14 CUTOUT. PERFORMED REPAIR ON F S 300 FRAME WEB AT STRINGER 14 CUTOUT LT IAW SRM 53-10-02 PAGE 43 FIGURE 11, 51-30-02 PAGE 8-9,2-3, 51-30-05 PAGE 5, 51-10-02 PAGE 7-8 AND BSOPM 20-41-02 PAGE 7-9. 2L74 4F A20WE 20040205000322004020500032WP 2004 2 5 CNMA200300006 120031120A2612 WARNING LIGHT DOUG DC10 DC1030 3023501WP NR 3 FIRE ILLUMINATED A CNMAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07540AX 46595 AT FL 310 ENGINE NR 3 LOOP (B) LIGHT ILLUMINATED, AFTER NOTIFING THE CAPT THE LOOP (A) LIGHT CAME ON WITH ENGINE FIRE WARNING. EMERGENCY AND IRREGULAR PROCEDURES ACCOMPLISHED, GROSS WEIGHT ADJUSTED AND RETURN TO AIRPORT. NO FURTHER PROPLEMS NOTED. 2L73 4F A22WE 20040205000352004020500035NM 2004 2 5 EIA2003154 120031021A5315 FLOORBEAM BOEING747 747132 1384882NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 EXISTING REPAIR AT UPPER DECK FLOORBEAM UPPER CHORD STA. 520 LBL 12- LBL 32 REWORK PER EIA ENGINEERING. REMOVED EXISTING REPAIR, NDT AREA, FABBED AND INSTALLED NEW REPAIR IAW ECRA 479-53-182-2. 2L74 4F A20WE 20040205000372004020500037CE 2004 2 5 TIM2003F00001 120031105A53121144400261 BULKHEAD BEECH 1900 1900C 1154161CE FUSELAGE CRACKED E TIMAO OTHER O OTHER NRNOT REPORTED 1 NM07195GA31681 UB65 BULKHEAD FOUND TO BE CRACKED AT INSPECTION. (CNTRL NR 81) 2L72 4T RTA24CE 20040205000452004020500045EU 2004 2 5 206541 120031121A2710 AILERON SAAB SF340 SF340A 7850100EU WINGS MALFUNCTIONED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL1740SZ 34040SZ FLT NR 4568 FROM LYH TO PIT. ON TAKE-OFF, AFTER PASSING CONTROL OF AIRCRAFT FROM CAPTAIN TO FIRST OFFICER. AIRCREW EXPERIENCED GRINDING IN AILERONS. AIRCREW ABORTED TAKE-OFF AND RETURNED TO GATE. 2L72 4T RTA52EU 20040205000522004020500052EA 2004 2 5 ASOA03674 120031226A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 582.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO BAY FLOOR SILL AT FS 582.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040205000632004020500063EA 2004 2 5 ASOA03667 120031222A5210601R3198055 PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11908EV 7654 DURING A C-CHECK IN MCN, THE TOP STEP PANEL ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP PANEL ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000662004020500066EA 2004 2 5 ASOA03664 120031220A3350BF10044004 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURNIG A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT IN THE GALLEY BY THE SERVICE DOOR AND THE EMERGENCY EXIT FLOOR FLOODLIGHT AT THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE GALLEY BY THE SERVICE DOOR AND THE EMERGENCY EXIT FLOOR FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000682004020500068EA 2004 2 5 ASOA03672 120031225A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA AIR DISTRIBUTIONDIRTY A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11827AS 7212 FLT 4526 - DURING CRUISE FROM MGM-ATL, A SMALL AMOUNT OF SMOKE WAS NOTICED IN THE CABIN WHEN THE RIGHT ACM WAS SELECTED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT COALESCER BAG, AND CLEANED THE COALESCER BAG COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE (M) 2L72 4F RTA21EA 20040205000732004020500073EA 2004 2 5 ASOA04005 120030104A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 FLT 4312 - DURING A GROUND INSPECTION IN DFW, THE ATTACH POINT ON THE LOWER RETRACTABLE PASSENGER DOOR STEP BRACKET WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000782004020500078EU 2004 2 5 ASOA03650 120031215A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING A HANGAR INSPECTION IN MCN, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AT 43WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040204000642004020400064EU 2004 2 4 00118 120031017A2497 WIRE AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE CHAFED E HAEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05232TW 32 PILOT REPORTED AFTER DEPARTURE FROM AMA BOTH GENERATORS WENT OFF LINE AND SMOKE IN COCKPIT, RETURNED TO AMA UNEVENTFUL LANDING. MAINTENANCE FOUND POWER WIRE TO LT RAIN REPELLENT SWITCH CHAFING AIRFRAME, REPOSITION AND INSULATE WIRE AT CONNECTOR, AIRCRAFT RAN AND OPS CHECK NORMAL. 2L72 4F4 F A7EU E7EA 20040204000952004020400095NM 2004 2 4 03FDEA01713 120031008A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8* 52044NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 CORROSION BS 320-340, RBL 40, WL 208 ON TOP OF FLOORBEAM AND INTERCOSTAL REMOVED AND REPLACED FLOORBEAM. 2L73 4F4 FRTA3WE E2EA 20040204001952004020400195 2004 2 4 SWIA200312569 420031030A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM0716731 120190 NR 1 STALL LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED STALL WARNING PANEL. OPS CHECKS GOOD. REF MFG 120 MM 27-50-00. 2L72 4T4 TRTA31SO E20NE 20040204001972004020400197SO 2004 2 4 SWIA200312571 120031031A27503431001001 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LT NACELLE FLAP MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07288SW1664 1664 120316 AFTER LANDING, BOTH NACELLE FLAPS WERE SLOW TO RETRACT, CAUSING DISAGREEMENT. NACELLE FLAPS EVENTUALLY RETRACTED ON THEIR OWN. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECKS GOOD. PN: 343100-1001, SN ON: 0228, SN OFF: 0175 2L72 4T4 TRTA31SO E20NE 20040204002062004020400206NE 2004 2 4 2003F00598 220030903A7200 ENGINE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE SEIZED B HXSDK NONE O OTHER ININSP/MAINT 1 AL0557954 1127 909 ENGINE REMOVED DUE TO TURBINE SEIZURE. MO 2 AND 3 209.3 HOURS OUT OF OVERHAUL . 1G71 3U3 UNCH9EU E19EU 20040205000022004020500002NM 2004 2 5 ABXA030444 120031113A3231149T695511 FITTING BOEING767 767281 1385109NM BELLCRANK CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23783AX 23016 RIGHT MAIN LANDING GEAR DOOR RETRACT FITTING CRACKED NEAR RIGHT SIDE KEELBEAM. CRACK LENGTH .7500 INCH FROM FASTNER HOLE TO EDGE OF FITTING. REPLACED BELLCRANK FITTING. 2L72 4F RTA1NM 20040205000392004020500039NE 2004 2 5 GLBA2003152 320031121A6111C7921B BEARING RACE BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3I NE PROPELLER BROKEN A GLBAK NONE O OTHER ININSP/MAINT 1 NM03208GL138752302 UE208 KX38 LOOSE BLADES FOUND DURING SCHEDULED INSPECTION, REPLACED PROPELLER ASSEMBLY, TEARDOWN RESULTS FOUND BROKEN LOWER BEARING RACE PN C-792-1B REV (H) SN H123. 2L72 4T RTA24CE 5 CP10NE 20040205000432004020500043CE 2004 2 5 GLBA2003153 120031120A77221303800415 INDICATOR BEECH 1900 1900D 1154162CE ITT MALFUNCTIONED A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM03154GL11136 UE154 LT ENGINE ITT EXCEEDED 900C ON ADVANCEMENT OF POWER ON TAKE OFF ROLL, REMOVED AND REPLACED LT ITT GAUGE. 2L72 4T RTA24CE 20040205000922004020500092WP 2004 2 5 AMTA200301324 120031027A5210128T10033 ACTUATOR LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE L1 DOOR INOPERATIVE A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11163AT 1229 PASSENGER DOOR DOES NOT OPEN ELECTRICALLY, MECHANICALLY, OR MANUALLY. REMOVED AND REPLACED L1 DOOR ACTUATOR IAW MM 52-12-01. OK FOR FLIGHT. 2L73 4F4 F A23WE A12EU 20040205000992004020500099NM 2004 2 5 HNAA0300072 120031120A282082820077003 LINE DHAV DHC8 DHC8201 2809001NM LEFT WING FUEL DETECTED A HNAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA07965HA1072210722 450 INTERMITTENT NR 1 FUEL PRESSURE CAUTION LIGHT DURING CLIMB OUT. (OCCURRED AFTER TURNING OFF AUX FUEL PUMP) INSTALLED NEW MOTIVE FLOW LINES FROM COLLECTOR BAY TO ENGINE FIREWALL. 2H72 4T RTA13NM 20040205001052004020500105NM 2004 2 5 PCAA0311144 120031122A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGNECY LIGHT BROKEN A PCAAK NONE O OTHER ININSP/MAINT 1 EA13815EX 321 PILOT REPORTED EMERGENCY FLOOR LIGHTING ADJACENT TO SEAT 1D WAS BROKEN. MAINTENANCE FOUND ONE RED ROW 1 LIGHT INOPERATIVE, AND REPAIRED AFFECTED WIRE. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040205001062004020500106EU 2004 2 5 UPS03141572 120031119A7830 COWLING AIRBUSA300 A300F4622R 3930360EU RT T/REVERSER DAMAGED A IPXAO OTHER O OTHER LDLANDING 1 SO01122UP 0807 BOTH THRUST REVERSERS LOCKED OUT DUE TO LT CASCADE VANE AND TRANSLATING COWL DAMAGE. REMOVED NR 1 ENGINE RT TAIL ROTOR COWL ASSY IAW MM 71-13-03-4. RB 04126. INSTALLED REVERSER HALF, THROUGH 71-13-03-4 C. 1-19, 21 AND 22,32,33. JDS 81085. C/W STEP 31 OF 71-13-03 & REMOVED AND REPLACED NR1 T/R 78-31-00. 51783 COMPLIED W/REMAINING STEPS IAW MM 71-13-03-4. 2L72 4F RTA35EU 20040205001082004020500108 2004 2 5 ANCF200300026 420031125A3436 COMPUTER DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE WINDSHEAR WILL NOT TEST W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23583AN 53183 TAKE OFF WAS ABORTED DUE TO TAIL WINDSHEAR ALERT. ART WAS ACTIVATED. WINDSHEAR COMPUTER SELF TEST WAS NOT SATISFACTORY. IT WAS DEFERRED TO DMI 410 MEL 34-44 CAT C. C/A TO CLOSE DMI 410. DMI WAS CLOSED DURING NIGHT SERVICE. WINDSHEAR COMPUTER WAS REMOVED AND RE-INSTALLED. BITE WAS PERFORMED TO BOTH STALL WARNING COMPUTERS AND FAULTS WERE ERASED IAW AMM 34-19-00 PAGE 201. SELF TEST TO WINDSHEAR SYSTEM WAS ACCOMPLISHED IN ACCORDING WITH AMM 34-47-0 PAGE 202. SATISFACTORY TEST. 2L72 4F4 FRT E9NE 20040205001132004020500113SO 2004 2 5 BSY2003F00027 220031030A8520649898 CRANKSHAFT BEECH 58 58 1152740CE CONT O520 IO520C 17032SO LT ENGINE FAILED E BSYAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 GL071859K TH1299 299450R LT ENGINE SHUT DOWN IN FLIGHT, FEATHERED ENGINE. RETURNED TO (CMH). CRANKSHAFT FAILED IN NR 1 AND NR 2 PISTONS NOT MOVING IN CYLINDERS. 1L72 3O3 O 3A16 E5CE 20040205001262004020500126NM 2004 2 5 HNAA0300074 120031130A2923731840 PUMP DHAV DHC8 DHC8102 2809003NM HYD SYSTEM FAILED A HNAAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TXTAXI/GRND HDL 1 EA07943HA 167 AFTER STBY HYD PUMP SELECTED ON, NR 1 STBY HYD PUMP CAUTION LIGHT ILLUMINATED. FOLLOWING NR 1 ENG S/D WHILE TAXI TO GATE , NORMAL BRAKES WHERE NOT AVAILABLE. 2H72 4T RTA13NM 20040205001272004020500127NM 2004 2 5 HNAA0300075 120031201A323282970018013 ACTUATOR DHAV DHC8 DHC8102 2809003NM MLG DOOR MALFUNCTIONED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07934HA 139 AFTER TAKEOFF LEFT GEAR DOOR AMBER LT REMAINED ON, CREW CONFIRMED ALL GEAR DOORS CLOSED. 2H72 4T RTA13NM 20040205001302004020500130CE 2004 2 5 GLBA20030506 120031201A3610 TUBE BEECH 1900 1900D 1154162CE LT BLEED FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03195GL UE195 LT BLEED FAIL, REPAIRED EVA TUBING PN 131823E6M02060. 2L72 4T RTA24CE 20040205001352004020500135GL 2004 2 5 P5CA0300999 220031201A7200CF680C2 ENGINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 4 BIRD INGESTION A P5CAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 WP23450PA 30808 706213 NR 4 ENGINE DAMAGE DUE TO BIRDSTRIKE. REMOVED AND REPLACED NR 4 ENGINE AND THE NAI DUCT ON NOSE COWL. 2L74 4F4 FRTA20WE E23EA 20040206000082004020600008 2004 2 6 KBM2003F00082 420031023A3422103002201 GYRO BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL COCKPIT PRECESSES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM675 3444 DIRECTIONAL GYRO PRECESSES N 30 DEGREES WITHIN 10 SECONDS AFTER BEING SET ON PROPER HEADING. REPLACED WITH SERVICEABLE GYRO. 1G71 3U3 U H2SW E4CE 20040206000112004020600011EU 2004 2 6 KBM2003F00089 120031108A5220350A25109521 ROD SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE JETTISON DOOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 LEFT SIDE DOOR STRUT WILL NOT HOLD DOOR OPEN. REPLACED WITH NEW LT DOOR STRUT. 1G71 3U3 UNCH9EU E19EU 20040206000172004020600017SO 2004 2 6 SIMA200334410 120031112A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE 145301 DURING AN IMBV INSPECTION STRINGER 19 WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52R AND 53R. BLENDED THE CHAFE ON STRINGER 19R AND PERFORMED AN NDT INSPECTION. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIRS DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A. (M) 2L72 4F RTT00011AT 20040206000302004020600030SO 2004 2 6 SIMA200335201 120031215A276014533022409 CONTROL UNIT EMB 135 EMB135KL 3260302SO SPOILERS INOPERATIVE A SIMAO OTHER J WARNING INDICATION CRCRUISE 1 SW21821AE 145577 LAX - FLT 3159 - DURING CRUISE FLIGHT CREW REPORTED AN UNCOMMANDED DEPLOYMENT OF SPOILERS AT HIGH SPEED RESULTING IN A 15 DEGREE BANK TO THE RIGHT. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB MM. AIRCRAFT WAS RELEASED FOR AND PASSED A FUNCTIONAL CHECK FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE (M) 2L72 4F RTT00011AT 20040206000732004020600073NM 2004 2 6 C8GA20030028 120031125A7710 B-NUT BOEING727 7272A1 138407FNM NR 1 ENGINE LOOSE A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15287SC 21345 FLT 737 FROM MMGL TO MMMY. DURING CLIMB, THE NR 1 ENGINE EPR INDICATION WENT EXCESSIVELY HIGH. AIRCRAFT DIVERTED TO KBRO AND LANDED WITHOUT INCIDENT. UPON LANDING, FOUND THE B-NUT ON THE PT-2 LINE AND A SENSE LINE ON THE PRVC LOOSE. TIGHTENED BOTH LINES AND AS A PRECAUTIONARY PLACED THE NR 1 EPR ON DMI IAW MEL 77-1-1. AIRCRAFT RETURNED TO SERVICE. CLEARED MEL 77-1-1 ON 11/25/03 UPON ARRIVING IN TOL AND FURTHER TROUBLESHOOTING SHOWED THAT THE PT-2 LINE HAD SOME OBSTRUCTION. CLEARED OBSTRUCTION ON THE PT-2 LINE AND PERFORMED NR 1 ENGINE EPR SYSTEM CHECKS IAW B727 MM 77-11-0. GROUND RUN CHECKS GOOD AND MEL 77-1-1 WAS CLEARED AND AIRCRAFT RETURNED TO SERVICE. (K) 2L73 4F A3WE 20040206000842004020600084WP 2004 2 6 DHL2003806501 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 7 FLOOR TRACK PLUG LUG WORN AT STA 320.000. REMOVED PLUG WITH WORN LUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040204001052004020400105NM 2004 2 4 AWXA200301285 120031002A5311651630087 FRAME BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A .3750 INCH CRACK WAS FOUND ON BS 178 BULKHEAD SIDE CHORD AT RBL 30, WL 207. MAINTENANCE REMOVED R/H SIDE CHORD BS 178, RBL 30, WL 207; FABRICATED A NEW REPLACEMENT RT SIDE CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3, 4, 12-14, PG. 26, 29,38, 44, 50, AND 55. 2L72 4F4 FRTA16WE E2GL 20040204001742004020400174WP 2004 2 4 U2RB102903 120031029A57115597838502 SPAR CAP DOUG DC8 DC863F 302198FWP RT WING CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23921R 67301916 46145 DURING REPETITIVE COMPLIANCE WITH A/D 2001-06-02 & S/B 57-90 R5 DETECTED 2 EACH CRACK INDICATIONS IN NON ADJACENT ATTACHMENT HOLES OF THE FORWARD LEG OF THE RIGHT WING FRONT SPAR LOWER CAP. REPAIRED 2 EACH CRACKED HOLES IAW DC-8 S/B 57-90 R5 TABLE 4, CONDITION NR 2 AND STRESS COINED REMAINING HOLES TO CONDITION NR 1,OPTION 2. 2L74 4F 4A25 20040204002242004020400224NM 2004 2 4 DHL2003721009 120031113A3260 SWITCH BOEING727 727228 1384083NM NLG DOOR DIRTY A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01721DH 19545 AFTER TAKEOFF AT ORD WHEN GEAR HANDLE IS PLACED IN THE OFF POSITION NOSE GEAR DOOR LIGHT (RED) IS ON. HANDLE CYCLED UP AND OFF A 2ND TIME WITH SAME RESULTS. ABNORMAL PROCEDURE WAS PERFORMED AND THE GEAR HANDLE WAS LT IN THE UP POSITION. CLEANED NOSE GEAR DOOR SWITCHES AND TESTED IAW M/M 32-62-0. NO DEFECTS NOTED. 2L73 4F RTA3WE 20040205000162004020500016EA 2004 2 5 03316660 120031112A27501104SD100001 SHAFT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A VTZAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA27660BR 7519 DURING APPROACH THE FLAP CONTROL SYSTEM FAILED AT ZERO DEGREES. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. FAILURE WAS TROUBLESHOT TO THE RT FLAP FLEX CABLE AND UNIT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20040205000232004020500023NM 2004 2 5 EIA2003160 120031018A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 LARGE CRACKS IN RT FS 340 FRAME WEB BETWEEN STR. 24 THRU 26. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 479-53-183-2. 2L74 4F A20WE 20040205000692004020500069EA 2004 2 5 ASOA03662 120031218A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN AIR DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11848AS 7339 FLT 4511 - DURING CRUISE FROM CHS-DFW, THE CREW NOTICED A SLIGHT OILY AND MOLDY ODOR WHEN THE PACKS WERE OPERATED OFF THE TENTH STAGE BLEEDS WITH NO VISIBLE SIGNS OF SMOKE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE COULD NOT DUPLICATE THE ODOR ON THE GROUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000912004020500091NE 2004 2 5 KPVA200340 220031021A732078639110 HYDROMECH UNIT DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE NR 1 ENGINE FAILED A KPVAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP13808WP215 026 SUBSTANTIAL LOSS OF TORQUE NR 1 ENGINE 2 TIMES. C/W WALK AROUND INSPECTION AND HAVE DETERMINED THIS AIRCRAFT TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT FROM OGG TO HNL ONLY. REMOVED AND REPLACED NR 1 ENGINE HMU IAW PWC MM 72-01-40 PAR 5A PG 403 AND PAR 5D PAGES 407-410. LEAK CHECK AND OPS CHECK GOOD IAW DHC 8MM 71-00-00 PAR 3F AND TABLE 505 PAGES 534-552. NO DEFECTS NOTED. 2H72 4T4 TRTA13NM E20NE 20040205001072004020500107EA 2004 2 5 JIKA200300002 220031116A73103040637 LINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE CHAFED E JIKAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP0131701 UB2 AFTER SHUT DOWN OF LT ENGINE GROUND CREW OBSERVED FUEL LEAKING FROM LT ENGINE COWLING. UPON INVESTIGATION MAINTENANCE FOUND THE FUEL FLOW TRANSDUCER INLET LINE CHAFED AND LEAKING FROM THE CHAFED AREA. THE STARTER GENERATOR COOLING DUCT SCAT TUBING WAS THE CAUSE OF THE CHAFING. 2L72 4T4 TRTA24CE E4EA 20040206000442004020600044WP 2004 2 6 ASAA0380804 120031123A532199365451 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040206000722004020600072WP 2004 2 6 ASAA0380818 120031201A5321993061287 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - FOUND 15K CHECK, FOUND FLOOR PANEL CRACKED AT FS 1287-1309. INSTALLED DOUBLER PER SRM 53-05. (M) 2L72 4F RTA6WE 20040205000152004020500015NM 2004 2 5 03305412 120031101A2120 SMOKE DORNERDO32 DO328300 NM PWA 306 PW306B NE CABIN DETECTED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27412FJ 3167 DURING PREFLIGHT PREPARATION OF THE AIRCRAFT CREW REPORTED SMOKE IN THE CABIN OF THE AIRCRAFT. 2H72 4T4 FRTA55NM E35NE 20040205000462004020500046NM 2004 2 5 UIA9210 120031123A2130396582232249961 CONTROL VALVE DOUG MD90 MD9030 3023690NM PACK FLOW MALFUNCTIONED Z O OTHER J WARNING INDICATION CLCLIMB 1 TW0017922 53601 IN AIR 8000 FT CABIN PRESSURE (FLOW) LIT,BOTH PACK OFF. A/C AIR TURNED BACK. IAW AMM 21-51-04 REPLACED R/L FLOW CONTROL VALVE AND GRD ENG RUN-UP FUNCTION TEST NORMAL. 2L72 4F RTA6WE 20040205000482004020500048WP 2004 2 5 ASAA0380764 120031121A53209930538502 WEB DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CUSP WEB IS CORRODED AT FS 560-579. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 53-01 AND 51-10-3. (M) 2L72 4F RTA6WE 20040205000772004020500077EA 2004 2 5 ASOA03652 120031215A3350B100976 LAMP CNDAIRCL600 CL6002C10 1390015EA ROW 1 INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11702EV 10035 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW ONE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW ONE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000972004020500097NM 2004 2 5 757BJ0002 120031123A3350 CHARGER BOEING757 757236 1384971NM EMERGENCY LIGHT SHORTED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05757BJ 22176 EMERGENCY LIGHTS CHARGER, LT CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. REPAIRED SHORT AT FLIGHT ATTENDANT STATION AT L1 DOOR. OPS CHECKS OK IAW MM 33-50-01. 2L72 4F RTA2NM 20040205001162004020500116NE 2004 2 5 030971 320031201A6140 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE LT TORQUE FAILED A UHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL1735SZ 35 508 DRG342189 ON 12/01/03, AT 1515Z FLT 4523, AIRCRAFT ABORTED TAKEOFF WHEN THE LEFT TORQUE INDICATOR WENT TO ZERO AT V1. CREW RETURNED AIRCRAFT TO FIELD. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040205001382004020500138WP 2004 2 5 DHL2003809007 120031129A5250 DOOR DOUG DC8 DC873F 302199FWP COCKPIT OUT OF ADJUST A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01604AL 46047 COCKPIT DOOR BINDING OUTSIDE KNOB SO SMOOTH YOU CAN NOT PULL DOOR OPEN WHEN UNLOCKED. ADJUSTED DOOR IAW SMM 52-51-01 OPS CHECKED OK. 2L74 4F RT4A25 20040206000152004020600015NM 2004 2 6 USAABB03231 120031227A335086210066 BATTERY BOEING767 767201 1385125NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19645US 23897 CLT - FOUND THE EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA1NM 20040206000262004020600026SO 2004 2 6 SIMA200333501 120031201A27503632001003 PDU EMB 135 EMB135LR 3260305SO TE FLAPS INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW21723AE 145288 FLAPS FAILED TO EXTEND. REMOVED AND REPLACED FPDU PERFORMED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE. S/D - THIS SDR WAS DUPLICATED WHEN THE REPAIR WAS COMPLIED WITH. IT CLOSED UNDER SDR 200334406. (M) 2L72 4F RTT00011AT 20040206000652004020600065WP 2004 2 6 ASAA0380816 120031126A53209911593 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND FLOOR MEMBRANE CORRODED AT FS 763. REMOVED DAMAGED AREA. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20040206000792004020600079WP 2004 2 6 DHL2004806507 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 6 TRACK PLUG LUG WORN AT STA 250.000. REMOVED PLUG WITH LUGS WORN IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 6 FLOOR TRACK IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206002152004020600215SO 2004 2 6 MASA200400031 120030114A3350 LIGHT EMB 145 EMB145LR 3260212SO ROWS 1-3 INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07836MJ 145359 ASH 2807 YYZ - CABIN EMERGENCY FLOOR LIGHT INOP ROWS 1 THRU 3. MX COULD NOT DUPLICATE. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040209000892004020900089NM 2004 2 9 AWXA200400120 120031231A5330657374681 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN SKIN AT R-2 DOOR LOWER HINGE CUTOUT, BS 948, RBL 62, WL 230. MAINTENANCE CUT OUT CRACKED SKIN AT R-2 DOOR LOWER HINGE CUTOUT, BS 948, RBL 62, WL 230; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, & TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 207 PG 217-224. 2L72 4F RTA16WE 20040206001022004020600102WP 2004 2 6 DHL2004806512 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 6 FLOOR TRACK PLUG LUGS WORN STA 1310.000. REMOVED NR 6 FLOOR TRACK PLUG STA 1310.000 IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040210000082004021000008WP 2004 2 10 UPS03841579 120031118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 1746 LONGERON 15L IS CRACKED. REMOVED DAMAGE FROM LONGERON,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. SRM. 53-2-2 FIG. 11. 2L74 4F RT4A25 20040210000272004021000027WP 2004 2 10 UPS03841603 120031015A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, FWD PIT STA 280 TORQUE BOX HAS AREA OF LIGHT CORROSION. ACCOMPLISHED REPAIR IAW REO G09550 REV A. 2L74 4F RT4A25 20040210000302004021000030WP 2004 2 10 UPS03841606 120031018A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, AFT PIT FS 1020 CORROSION UNDER NUTPLATES ON LOWER SURFACE OF UPPER FRAME FLANGE FROM L36-L34R. REMOVED CORROSION IAW DC8 SRM 51-1-8. ORIG .080, REMOVED .060 REMAIN .020 FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FRAME CAP OUT OF LIMITS IAW DC8 53-2- 0. FABBED REPAIR ANGLE -3 & -5 FILLER IAW REO G09556. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, RECEIVED, LOCATED, AND DRILLED NEW FRAME CAP IAW DC 8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040210000352004021000035WP 2004 2 10 UPS03841613 120031113A5320 WEB DOUG DC8 DC873F 302199FWP RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, CORROSION FOUND IN RT W/W OB WEB STA 3 JUST BEHIND FLAP BUSS DRUM. 5643403-4 PANEL AND -6 DBLR FOUND CORRODED OUT OF LIMITS; CUTOUT CORR ARE A OF -4 PANEL AND -6 DBLR;FAB -4 PANEL AND -6 DBLR;HEAT TREAT;LOC, DRILL 2EA REPAIR DBLRS AND 2 EA RPR FILLERS;ALODINED AND PRIMED;INSTALLED DBL RS, FILLERS, AND 2 EA STIFFNERS;ALL IAW DC8 SRM 53-2-0, 51-1-24, 51-1-8, 51-1-20D, AND TR 53-166. 2L74 4F RT4A25 20040210000402004021000040WP 2004 2 10 UPS03841618 120031115A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, MAIN CABIN STA 1756, LONGERON 15R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION AND STRAPS IAW SRM. 53-2-2 FIG. 10. 2L74 4F RT4A25 20040210000452004021000045CE 2004 2 10 GLBA2003068 120030529A2110 PLUG BEECH 1900 1900D 1154162CE BLEED AIR MISSING A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03253G 253 LT BLEED AIR FAIL, INSPECTED LT BLEED SYSTEM FOUND EVA TUBING PLUG PN 129-550077-7 MISSING REPLACED AND RUN. OPS CHECK GOOD. 2L72 4T RTA24CE 20040210000572004021000057SO 2004 2 10 GLBA2003077 120030602A7810 EXHAUST STACK EMB 120 EMB120ER 3260203SO LT ENGINE DAMAGED A GLBAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03299UX 120299 DAMAGE TO LT STACK AND FUSELAGE, REPAIRED FUSELAGE DAMAGE AND REPLACED EXHAUST STACK PN 120-35309-001. 2L72 4T RTA31SO 20040210000582004021000058WP 2004 2 10 ASAA0380778 120031119A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FLOORBOARD AT STATION 541 TO 617 LBL 44 HAS TWO RIVETS PULLED THROUGH. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20040210000602004021000060WP 2004 2 10 ASAA0380780 120031119A53219957918501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FLOORBOARD AT STATION 927 TO 1003 HAS SCREW HOLE BLOWN OUT. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20040210000632004021000063NM 2004 2 10 TSAA0333203 120031129A33501000679 BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHT DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 REPLACED RIGHT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040210000652004021000065NM 2004 2 10 TSAA0333205 120031129A335086210066 BATTERY PACK BOEING737 7372Y5 1384554NM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13810AL 24031 REPLACED AFT ENTRY DOOR IDENT EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4U RTA16WE 20040210000662004021000066EA 2004 2 10 REXA03009 120031226A3830 ODOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY DETECTED A REXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO258783E 7783 AMMONIA ODOR/SMOKE COMING FROM LAV REPORTED BY F/A. PERFORMED COMPLETE INSPECTION OF ENTIRE LAV SYSTEM FLUSHED LAV HOLDING TANK TWICE RESERVICED WITH BLUE JUICE. COMPLETE EXTENSIVE GROUND RUN A/C RELEASED FOR FLIGHT. (M) 2L72 4F RTA21EA 20040210000672004021000067WP 2004 2 10 ASAA0380759 120031118A53205936071 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND INTERCOSTAL CORROSION. INSTALLED NEW INTERCOSTAL PER SRM. (M) 2L72 4F RTA6WE 20040210000722004021000072WP 2004 2 10 ASAA0380781 120031119A533059360211 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND DENT IN EXT FUSELAGE AFT OF AFT CARGO DOOR BELOW LONGERON AT 22R. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20040210000742004021000074WP 2004 2 10 ASAA0380784 120031119A531139364451 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURNG 15K CHECK, FOUND CORROSION ON FRAME ANGLE AT STATION 731 ABOVE LONGERON 29L. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20040210000862004021000086EU 2004 2 10 USAA030299 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 FOUND SEAT TRACK CORRODED .175 SQUARE INCH AREA, FRAME 67 PLUS 5 INCHES LBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210000922004021000092EU 2004 2 10 USAA030297 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .175 SQUARE INCH AREA, FRAME 57.2 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210001132004021000113EU 2004 2 10 USAA030290 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .150 SQUARE INCH, FRAME 61 PLUS 10 INCHES RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210000342004021000034WP 2004 2 10 UPS03841611 120031022A5711 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, ATTACH FITTING AT XRS 624.000 REAR SPAR CRACKED. PERFORMED HFEC IAW MD NDT SPM 06-10-01.001. CRACK NOTED. REMOVED AILERON SUPPORT FITTING CRACKED ATTACH FITTING AND MOUNTING STUD IAW DC8 SRM 51-1-20 AND 51-3-0. LOCATED AND DRILLED ATTACH FITTING IAW DC8 SRM 51-1-24 . INSTALLED ATTACH FITTING, REINSTALLED MOUNTING STUD AND REINSTALLED AILERON SUPPORT FITTING AND TORQUED IAW DC8 MM 20-10-00. 2L74 4F RT4A25 20040210000482004021000048EU 2004 2 10 03FDEA02008 120031202A7830 THRUST REVERSER AIRBUS310 A310 EU GE CF6 CF6* 30020GL NR 1 ENGINE MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25412FE 360 1 ENG ON T/O, N1 DID NOT REACH T/O PWR. ENG N1 90 PRCT. ENG 2 N1 100 PRCT. TRIED TO MATCH N1 BY PUSHING UP 1 THROTTLE WHICH CAUSED 1 EGT TO RISE TO CAUTION RANGE ABOUT 890, RETARDED THROTTLES AT THAT TIME ECAM WARNING HP VALVE FAULT -OFF, 1 HP VALVE SELECTED OFF , 1 HP VALVE SWITCH FAULT LIGHT CAME ON. ECAM ADVISORY TEMP 245 FOLLOWED BY 1 ENG LOOP B LIGHT, FOLLOWED BY NR 1 ENG FIRE INDICATION ON ECAM AND OVERHEAD PANEL. REDUCE THROTTLES TO IDLE. FIRE INDICATION WENT OUT. RETURNED TO LAND KMIA. PYLON INSPECTION SEE WRI 05-50/6316. REVERSER REMOVED AND REPLACED SEE WRI 78-30/6317. CORE COWL REMOVED AND REPLACED SEE WRI 71-10/6321. 2L72 4F4 FRTA35EU E23EA 20040210000622004021000062NM 2004 2 10 TSAA0333202 120031129A33501000679 BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHT DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 REPLACED LT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040210001042004021000104EU 2004 2 10 USAA030279 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .225 SQUARE INCH, FRAME 71 RBL 17.75. DAMAGED TRACK REMOVED, REPLACED WITH NEW PER SRM 51-74-0 AND 51-72-11. (M) 2L72 4F RTA46NM 20040211000062004021100006EU 2004 2 11 USAA030272 120031201A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED APPROX .150 SQUARE INCH AREA, FRAME 53.8, LBL 17.75. INSTALLED NEW SECTION OF SEAT RACK PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20040211000172004021100017WP 2004 2 11 GTIA031040 120031213A2560 STRIP DOUG DC9 DC983 3022083WP G3 GALLEY DETACHED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FLL - FOUND SAFETY GLOW STRIP CAME OFF BY G3 GALLEY. CLEANED AND REINSTALLED SAFETY GLOW STRIP. (M) 2L72 4F RTA6WE 20040211000232004021100023WP 2004 2 11 AMTA200301464 120031206A335020131A BATTERY LKHEED1011 1011385115 5265015WP EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11194AT 193B1230 FOUND EGRESS TRACK LIGHTS DIM AFTER 4 MINUTES OF OPERATION FROM SEAT ROWS 1-7 ON THE LEFT AND RIGHT SIDE. REMOVED AND REPLACED BATTERY PACK AT RIGHT FORWARD SIDE. OPS CHECK GOOD, REF MM33-59-03. (M) 2L73 4F A23WE 20040211000422004021100042EU 2004 2 11 ASOA03694 120031230A3397M2275941249 WIRE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING HANGAR MAINTENANCE IN MCN, THE SERVICE DOOR EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE BACK OF THE SERVICE DOOR EXIT LIGHT ASSEMBLY AND REPINNED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040210000512004021000051SW 2004 2 10 2003F00639 120031016A6240430340003101 CHIP DETECTOR BELL 430 430 1182150SW MAIN XMSN FAILED D O OTHER N FALSE WARNING CRCRUISE 1 SO07430CM1810 49090 C/FL (CHIP DETECTOR FAILURE) LIGHTS INTERMITTENT. 1G72 3U RTH9SW 20040210001002004021000100EU 2004 2 10 USAA030280 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .175 SQUARE INCH AREA, FRAME 69 PLUS 10 INCH RBL 17.75. DAMAGED TRACK REMOVED, REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210001202004021000120WP 2004 2 10 ASAA0380757 120031118A532199365811 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FLOORBOARD DELAMINATING. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M) 2L72 4F RTA6WE 20040212000012004021200001CE 2004 2 12 56041 120031111A6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162CE RT ENGINE MALFUNCTIONED A AMWAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 CE07142YV UE142 DURING APPROACH TO LANDING IN PNC. THE RIGHT PROPELLER AUTOFEATHER SYS CYCLED THE PROP IN AND OUT OF FEATHER SEVERAL TIMES. WHILE THE ENGINE CONTINUED TO PRODUCE POWER. 2L72 4T RTA24CE 20040212000102004021200010WP 2004 2 12 UPS03841627 120031119A533057503223N1 SKIN DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, WHILE REMOVING FASTENERS AT STATION 1160-1220,LONG.32R-35R FOUND CORROSION BETWEEN SKIN AND INTERNAL DOUBLER. REMOVED AND REPLACED SKIN BETWEEN STATION 1050 TO 1350 BETWEEN LONG.31L TO 31R IAW DWG. 5750322 AND SRM. 53-1-0,51-1-20D,51-1-21. 2L74 4F RT4A25 20040212000132004021200013WP 2004 2 12 UPS03841637 120031201A3350 LIGHT DOUG DC8 DC871F 302199DWP CABIN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONNECTIONS AT CONNECTOR ON BATTERY. SYSTEM OPS CHECKS NORMAL IAW MM 33-50-01. 2L74 4F RT4A25 20040212000152004021200015CE 2004 2 12 AMWA84 120031114A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0710675 UE10675 WHILE PERFORMING AN INSPECTION IN THE VERT STAB., THE RIB FLANGES AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE LEFT SIDE AT THE CENTER STRINGER. REPAIRED CRACKS TO RIB FLANGE IAW BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20040212000162004021200016CE 2004 2 12 AMWA85 120031126A553110164000017 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07138YV UE138 DURING THE D-6 INSPECTION. THERE WAS TWO CRACKS FOUND AT THE UPPER RIB LT AT BOTH SLOTS FOR STRINGER. REPAIRED CRACKS IAW BMM. P/N 101-640000-17,69.184 2L72 4T RTA24CE 20040212000202004021200020NE 2004 2 12 SW07200300004 220030516A72504120T01P02 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE 2ND STAGE DAMAGED G FDKAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW07508MJ324 10087 E965387 WHILE PERFORMING A BOROSCOPE INSPECTION AFTER A PEAK VIBRATION, THE MAINTENANCE PERSONNEL DISCOVERED 2ND STAGE HIGH PRESSURE TURBINE BLADES DAMAGE. 2L72 4F4 FRTA21EA EOOO63EN 20040212000212004021200021WP 2004 2 12 CNMA200300007 120031202A3350AD3119 BATTERY PACK DOUG DC10 DC1030 3023501WP EMERGENCY LIGHT FAILED A CNMAK NONE L NO TEST ININSP/MAINT 1 SW0717085 47957 EMERGENCY EGRESS LIGHTS FAIL TO TEST. BATTERY PACK FAILED. 2L73 4F A22WE 20040203003212004020300321EA 2004 2 3 MASA200300463 120031123A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX OPEN A MASAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 SW0775995 7361 ASH 2644 CHS-PHL, RETURNED TO GATE DUE TO THE FLT ATTENDANT NOTIFIED THE CREW THAT THEY DID NOT FEEL THE PAX DOOR CLOSED AND LOCKED PROPERLY. A/C WAS FERRYING TO PHL FOR MX. MX COULD NOT DUPLICATE THE DISC. NO PARTS USED. 2L72 4F RTA21EA 20040203003612004020300361WP 2004 2 3 UPS04841776 120031231A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, STATION 1240 LONGERON 34R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND SPLICES BETWEEN STATION 1210 TO 1270 IAW UPD ENGINEERING FILE NUMBER DC8-53-20384, AND SAA SK 702-146. 2L74 4F RT4A25 20040204000292004020400029NM 2004 2 4 S03453082 120030720A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE CORRODED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 29906 B18209 DATUM AIRPLANE WAS INSPECTED DURING OVERNIGHT INSPECTION BECAUSE TWO OTHER AIRPLANES IN THEIR FLEET HAD CORROSION COMMON TO THE BELLY SKIN.THE CORROSION WAS FOUND ON THE BELLY SKIN FROM BS 1660 TO 1695,S-51L,S-51R. THIS CORROSION HAS BEEN BLENDED FROM THE BELLY SKIN AND ENSURE THE DAMAGE FREE CONDITION BY HFEC SURFACE INSPECTION AND REPAIR IAW EO 744-53-06-0003 AND IAW TELEX: CHI-TPE-03-00504. 2L74 4F4 FRTA20WE E24NE 20040204000312004020400031NM 2004 2 4 S03427088 120030821A5753 STRUCTURE BOEING747 747400 NM PWA 4056 PW4056 NE RT TE FLAP DAMAGED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 29219 WALK AROUND CHECK FOUND RT WING OB TRAILING EDGE FLAP WAS DAMAGED. RT OB MID AND AFT FLAP DAMAGED DUE TO OB SPINDLE DISCONNECTED. RT OB AFT FLAP ABOUT 4 FT LONG MEASURED FROM OB EDGE. RT OB MID FLAP ABOUT 5 FT LONG MEASURED FROM OB EDGE. ONE ROD BETWEEN MID FLAP OB AND AFT FLAP OB WAS BROKEN. ONE ROD BETWEEN OB FLAP CARRAGE AND MID FLAP OB WAS BENT. REPLACED THE DAMAGE PARTS WITH PARTS REMOVED FROM B18203. THE DAMAGED SPINDLE ASSY WAS SENT TO MFG FOR INVESTIGATION. AWAIT THE INVESTIGATION REPORT. 2L74 4F4 FRTA20WE E24NE 20040204000572004020400057 2004 2 4 RAIA00310262 420031016A3420HG2010AC02 INDICATOR EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL AHRS MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03813HK10991 145044 5689-STL- EADI NR 2 ROLLS CONTINUOUSLY. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS. 2L72 4T4 FRTT00011ATTE6CH 20040204000602004020400060NM 2004 2 4 XNOA1160 120031018A5610 WINDSHIELD BOEING727 727200 138407ENM COCKPIT FAILED A XN0AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23793A 20774 CRACKED R-1 WINDSHIELD, ARCING AS WELL. REMOVED AND REPLACED F/O R-1 WINDSHIELD IAW B727MM 56-11-11 AS REQ NO DEFECTS NOTED. (STATUS: ORIG/CLOSED) 2L73 4F RTA3WE 20040204000662004020400066WP 2004 2 4 UPS03841443 120030923A534037540252 FITTING DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, TORQUE BOX VERTICLE LEG SUPPORT FITTING IS CRACKED AT STA. 1220 LONG. 27R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. 3754025,AND SRM. 51-1-20D,AND SRM. 51-3-0 2L74 4F RT4A25 20040204000702004020400070CE 2004 2 4 55177AMWA 120031013A2750 CONTROL UNIT BEECH 1900 1900D 1154162CE T/E FLAPS FAILED A AMWAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CE07133YV UE133 AFTER TAKE OFF CREW TRIED TO RETRACT THE FLAPS. THE FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS. 2L72 4T RTA24CE 20040204000132004020400013NM 2004 2 4 C1HA200392008 120031127A3350 POWER SUPPLY BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 EXTERIOR EMERGENCY LIGHTS FOR DOORS L2 AND R2 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M983 AND BOTH OPS CKD GOOD IAW MM 33-50-01. 2L73 4F A3WE 20040204000362004020400036WP 2004 2 4 IXXA0300062O 120031014A5270 WARNING LIGHT DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE CARGO DOOR FALSE INDICATIONA IXXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW11606AL900971850 46044 CREW REJECTED TAKE-OFF FROM KEWR WHEN BELLY DOOR OPEN LIGHT CAME ON DURING TAKE-OFF ROLL. LIGHT EXTINGUISHED AFTER REJECT. MAINTENANCE INSPECTED ALL DOORS AND SWITCHES IAW ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20040204000652004020400065WP 2004 2 4 UPS03841442 120031006A53403755841501 FITTING DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STA 1180 BATHTUB FITTING IS CRACKED BETWEEN LONG. 33R TO 34R. R & R FITTING IAW SRM. 53-2-0 FIG. 2D AND DWG. 3755841 2L74 4F RT4A25 20040204000932004020400093SO 2004 2 4 SWIA200312509 120031017A3350 BATTERY EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER P NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07223SW 120291 EMERGENCY LIGHTS BEHIND ROW 8 WOULD NOT ILLUMINATE. COCKPIT AND FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCHES BOTH TESTED. REPLACED AFT BATTERY. ALL EMERGENCY LIGHTS OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040204001062004020400106NM 2004 2 4 AWXA200301286 120031007A532065C326772 WEB BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1INCH CRACK WAS FOUND ON SHEAR WEB AT BS 1003, LBL 42, WL 208.1. MAINTENANCE REMOVED CRACKED SHEAR WEB AT BS 1003, LBL 42, WL 208.1; FABRICATED A NEW REPLACEMENT SHEAR WEB IAW DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3, 6, AND 7. 2L72 4F4 FRTA16WE E2GL 20040204001982004020400198 2004 2 4 SWIA200312572 420031029A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STALL WARNING MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07918SW 7645 STALL FAIL MESSAGE AFTER TAKEOFF. REPLACED STALL COMPUTER. OPS CHECK GOOD. S/N OFF: 887 2L72 4F4 FRTA21EA E15NE 20040204002042004020400204NM 2004 2 4 P5CA0300977 120031031A5311151716587075T6 FRAME BOEING747 7472U3B 1384846NM FUSELAGE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 MAIN DECK CARGO AREA, FUSELAGE FRAME, STA 1700 RT SIDE S-1 TO S-11 FRAME DAMAGE. REMOVED DAMAGED PORTION OF FRAME SECTION. REPAIR ACCOMPLISHED IAW SRM 53-10-04. 2L74 4F RTA20WE 20031014001872003101400187NM 2003 10 14 SWAA032110 120030920A3350079123 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROW NR 8, NR 13, NR 18, NR 21, AND NR 23. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20031014002022003101400202EU 2003 10 14 BAQA089025 120030907A243523032048 STARTER GEN BOLKMS117 BK117B1 5626012EU ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G784 7179 STARTER GEN INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031015000092003101500009NM 2003 10 15 USAASB03170 120030918A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU 23228 MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY LIGHT EXTINGUISHES AFTER APPROXIMATELY FIVE SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031015000122003101500012NM 2003 10 15 USAASB03163 120030911A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT SEAT ROWS 5, 6, 7 AND 8, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE EXIT ROW. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031015000362003101500036EU 2003 10 15 ASOA03421 120030907A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURNG AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031015000442003101500044EA 2003 10 15 ASOA03441 120030915A5210601R3198041 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR TOP STEP HINGE WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP HINGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000502003101500050EA 2003 10 15 ASOA03449 120030910A5347 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MC, THE LEFT AND RIGHT 9.00 AND 27.00 FLOORBEAMS BETWEEN FS 280.00 AND FS 409.00 PLUS 5.00 IAW ASA EO 600-53-0052A. (M) 2L72 4F RTA21EA 20031009000552003100900055NM 2003 10 9 03FDEA01690 120031002A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON OUTBOARD FLANGE OF S28-L KEELBEAM, STA 720E TO 720F. REPAIRED PER E.A. 7-5310-55007. 2L73 4F RTA3WE 20031009000572003100900057WP 2003 10 9 DHL2003801090 120030918A5270H2024B SWITCH DOUG DC8 DC873F 302199FWP MLG DOOR FAILED A DHLAO OTHER N FALSE WARNING DEDESCENT 1 SO01801DH 46033 ON DECENT INTO CVG AT 7000 FEET LEFT GEAR DOOR UNSAFE LIGHT ILLUMINATED, RAN ABNORMAL PROCEDURE, AND LEFT GEAR DOOR UNSAFE LIGHT STILL CAME ON. REMOVED AND REPLACED LEFT MLG DOOR SWITCH, OPS CHECKED GOOD IAW DC-8 M/M 32-60-0. 2L74 4F RT4A25 20031009001152003100900115NM 2003 10 9 CALA0300533 120030917A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND AN 8 INCH CRACK IN INTERCOSTAL AT STA 380-400, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031009001272003100900127NM 2003 10 9 QXEA200301139 120030916A61235008269H MFC DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 400 MALFUNCTIONED A QXEAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 NM09357PH1006410064 504 AG0054 ON FLIGHT 2200 RDM TO SEA AIRCRAFT RETURNED TO FIELD AFTER ACCOMPLISHING NR 2 ENGINE SHUTDOWN DUE TO, AFTER ROTATION ON TAKEOFF NR 2 PROP ROLLED BACK TO MINUS 87 PERCENT AND SURGED CONTINUOUSLY PLUS OR MINUS 15 PERCENT. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 MFC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031010000112003101000011NM 2003 10 10 USAASB03171 120030917A2133322684003 OUTFLOW VALVE BOEING737 7373B7 1384580NM E/E COMPT INOPERATIVE A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19533AU 24515 EN ROUTE FROM MCI-PHL, AT FL370, THE CABIN ALTITUDE BEGAN TO SLOWLY CLIMB 200 FEET PER MINUTE TO 9,000 FT. CREW BEGAN DESCENT AND WAS ABLE TO REDUCE CABIN ALTITUDED TO 8,000 FEET BUT NOT UNTIL LEVEL AT FL290. CREW NOTED THAT AIRCRAFT SEEMS TO MAINTAIN ONLY 6.3 DIFFERENTAIL IN AUTO, STANDBY OR MANURAL PRESSURIZATION MODES. NO OBVIOUS LEAKS WERE NOTED. FLIGHT CONTINUED ONTO PHL WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD OUTFLOW VALVE INOPERATIVE. REMOVED AND REPLACED FORWARD OUTFLOW VALVE PER MM 21-43-11. OPS CHECK GOOD. CHECKED AIRCRAFT FOR LEAKS. DUCTING, PACKS, DOORS AND HATCHES CHECK GOOD. PERFORMED AIRCRAFT CONFIDENCE CHECK PER JOB CARD J321-00-01. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031010000372003101000037EU 2003 10 10 USAABA03033 120030917A3350321430 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 EPSU 17WL FAILED CAPACITY TEST. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA46NM 20031010000402003101000040NM 2003 10 10 USAA030189 120030904A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU60023 22202 FOUND FRAME CRACKED 1.5 INCHES, FORWARD CARGO UPPER FLANGE OF FS 760, ABOVE STRINGER 24L. FABRICATED NEW LOWER PORTION OF FRAME AND SPLICE IT IN PER EA 94596. (M) 2L72 4F RTA2NM 20031010001002003101000100EU 2003 10 10 BAQA089530 120031002A2140JBS8803 VALVE UROCOPEC135 EC135P1 8680990EU HEATER MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH537 0179 "BLEED AIR" STAYS ON, ON CAD. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20040204002122004020400212NE 2004 2 4 2603 220030811A72617938314501 LINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE OIL SYSTEM CRACKED H EA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO21BGI 49940 725651 IN LEVEL FLIGHT AT 33,000 FT, LT ENG OIL PRESS LIGHT ON. FEW SECONDS RED LIGHT FOLLOWED BY LOSS OF OIL QUANTITY. ENGINE SHUTDOWN. RETURNED TO DEPARTURE POINT AND NORMAL LANDING. ENGINE INSPECTION REVEALED CRACKED OIL PRESS TUBE, PN 7938314-501. ENGINE REPLACED DUE TO EXTENDED WINDMILLING TIME 2L72 4F4 FRTA6WE E9NE 20040204002152004020400215EU 2004 2 4 U30A200300037 120031111A5311D53112752202 FRAME AIRBUS320 A320212 3930322EU ZONE 841 CORRODED A U30AK NONE O OTHER ININSP/MAINT 1 EA17265AV3517335173 427 CORROSION WAS FOUND AT FRAME 16, RT (R1 PAX/CREW DOOR FWD FRAME) UNDER SAFETY BARRIER ATTACH POINT. CORROSION WAS REMOVED IAW SRM 51-74-00. HFEC AND A ROTO TEST INSPECTION TO ENSURE NIL CRACKS.REWORK AREA WAS REPROTECTED IW SRM, CORROSION PREVENTATIVE COMPOUND WAS APPLIED. NEW NUTPLATES WERE INSTALLED. E.O.03-53-006 HAS BEEN CREATED TO ACCOMPLISH THIS DVI AT 5 YR INTERVALS, AND THEREBY INCORPORATES IT INTO THE CONTINUOUS AIRWORTHINESS MAINTENANCE REQUIREMENTS OF THIS AIRCRAFT. THE REWORK AND REINSPECTION DATA REQUIREMENTS ARE DGAC APPROVED IAW MFG RAS (REPAIR DESIGN APPROVAL SHEET) 026456/009/2003 AND THEREFORE FAA APPROVED. 2L72 4F RTA28NM 20040204002222004020400222NM 2004 2 4 DHL2003753006 120031112A2612 WARNING SYSTEM BOEING727 727223 1384074NM CARGO BAY FALSE ACTIVATIONA DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01753DH 22468 DURING CLIMB OUT FROM CVG AT APPROXIMATELY 300 FT AGL THE LOWER CARGO FIRE WARNING SYSTEM ILLUMINATED AND WARNING BELL SOUNDED. THE DISPLAY READ FIRE IWD. THIS CONDITION LASTED FOR APPROXIMATELY 2 MINUTES. CHECK LIST PROCEDURES COMPLETED. PERFORMED SYSTEM TEST AND ACQUIRED ALL SENSORS. NOTED SOME CONDENSATION IN LOWER PITS. FOUND NO EVIDENCE OF COMBUSTION. LOWER CARGO FIRE WARNING SYSTEM TESTED OKAY. OKAY FOR CONTINUED SERVICE IAW B-M/M 26-16-01. 2L73 4F A3WE 20040205000082004020500008NM 2004 2 5 P5CA0300989 120031116A3241 CONTROL UNIT BOEING747 747283B 1384867NM ANTI SKID SYSTEMMALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23921FT 21575 LT WING RT REAR ANTI-SKID WARNING LIGHT ILLUMINATED ON P-2 PANEL. REPLACED ANTI-SKID CONTROL UNIT AND TRANSDUCER IAW MM 32-41-00. SYSTEM CHECK GOOD. 2L74 4F A20WE 20040205000202004020500020NM 2004 2 5 EIA2003157 120031019A5330 SKIN BOEING747 747132 1384882NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 LT WING GEAR WW BAY UPPER CEILING SKIN WEB CORRODED AT STA. 1301 AND 1319 LBL 120. CUT OUT DAMAGED AREAS, NDT AREAS, FABBED AND INSTALLED REPAIR IAW SRM 53-10-07 FIGURE 2. 2L74 4F A20WE 20040205000412004020500041WP 2004 2 5 MEX2003518 120031113A291341003108 PUMP DOUG DC9 DC987 3022087WP RT HYD SYSTEM FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23803ML7776 7776 49726 AIRCRAFT RETURNED TO PLATFORM DUE TO HIGHT TEMPERATURE ON RT HYDRAULIC SYSTEM. THE RT HYDRAULIC PUMP WAS REPLACED. DURING OVERNIGHT SERVICE THE PTU AND RELIEF VALVE WERE REPLACED IAW MM 29-10-12 RESPECTIVELY. 2L72 4F RTA6WE 20040205000562004020500056NE 2004 2 5 ASOA03669 220031224A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT MALFUNCTIONED A ASOAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO11848AS 7339 FLT 4162 - DURING TAKEOFF ROLL FROM ATL TO PHL, THE CAPTAIN REPORTED THE LT ENGINE OIL PRESSURE WAS 20 LBS LESS THAN THE RT ENGINE, BUT STILL WITHIN LIMITS. AFTER TAKEOFF THE LT ENGINE OIL PRESSURE CONTINUED TO DECREASE WITH THE LOWEST PRESSURE BEING 49 LBS. THE CREW ALSO REPORTED AN OIL BURNING ODOR WHEN THE PACKS SWITCHES WERE SELECTED FROM APU TO ENGINE. AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE. (M) 2L72 4F4 FRTA21EA E15NE 20040205000572004020500057EA 2004 2 5 ASOA03696 120031231A5320601R3895721 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE SERVICE DOOR AIRFRAME SILL PLATE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPALCED THE SERVICE DOOR AIRFRAME SILL PLATE. (M) 2L72 4F RTA21EA 20040204000442004020400044NM 2004 2 4 S03453084 120030812A5312 BULKHEAD BOEING747 747200 1384847NM PWA JT9 JT9D7R4G2 52054NE FUSELAGE CORRODED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 22299 B18752 FUSELAGE BULKHEAD 1480 WEB CORROSION AT LBL 47.7. REPAIR IAW EO 742-53-10-0043. 2L74 4F4 FRTA20WE E3NE 20040204000582004020400058EU 2004 2 4 PNSA031001 120031015A2731D97439 ACTUATOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE MAIN TRIM BINDING A PNSAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 AL03675PA 340B206 DURING CRUISE 20 MINUTES AFTER DEPARTURE FROM AKN FLIGHT CREW RECEIVED AN AUTO TRIM WARNING WITH AN ASSOCIATED AUTO PILOT DISCONNECT. FLT CREW WAS UNABLE TO TRIM AIRCRAFT WITH MAIN TRIM SYSTEM IN THE NOSE DOWN POSITION, STANDBY TRIM SYSTEM WAS USED TO TRIM AIRCRAFT. MAINTENANCE WAS CONTACTED BY RADIO FOR FURTHER TROUBLESHOOTING AND ADVISED CREW TO ONLY OPERATE WITH STANDBY SYSTEM AND RETURN TO AKN. LANDING WAS UNEVENTFUL AND MAINTENANCE DISCOVERED MAIN TRIM ACTUATOR WAS WORKING INTERMITTENT IN THE NOSE DOWN POSITION AND PITCH TRIM INDICATOR WAS INCORRECTLY SHOWING MORE NOSE UP TRIM THAN ACTUAL. MAINTENANCE REPLACED MAIN TRIM ACTUATOR AND AIRCRAFT RELEASE FOR SERVICE. 2L72 4T4 TRTA52EU E8NE 20040204000792004020400079NM 2004 2 4 2003UALA00773 120031013A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE SEAT 1F MISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP29769UA 26921 SEAT 1F OB SIDE EMERGENCY LIGHT HAS SECTION MISSING. REPLACED LIGHT. 2L72 4F4 FRTT0001SE E46NE 20040204001012004020400101NM 2004 2 4 AWXA200301281 120031003A53476546813 SEAT TRACK BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK CORROSION WAS FOUND ON SEAT TRACK FROM BS 440 TO BS 500A, RBL 45. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED SEAT TRACK FROM BS 360 TO BS 500A, RBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-52, FIG. 202, PG. 202-205. 2L72 4F4 FRTA16WE E2GL 20040204001032004020400103NM 2004 2 4 AWXA200301283 120031008A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 LCQ - MAJOR REPAIR - DURING C-15 CHECK FOUND AFT CARGO COMPARTMENT FLOORBEAM EXFOLIATED AND SPLIT AT BS 773, RBL 13. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 773, RBL 13; FABRICATED A REPAIR PLATE, EXTRUSION, ANGLE, AND CHANNEL FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG. 201. 2L72 4F4 FRTA16WE E2GL 20040204001402004020400140NM 2004 2 4 DHL2003745024 120031028A3260 WARNING LIGHT BOEING727 727224 1384076NM PWA JT8 JT8D* NE MLG GEAR FALSE ACTIVATIONA DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 GEAR DOOR LIGHT ON PILOTS PANEL AND RIGHT GEAR DOOR LIGHT ON S/O'S PANEL ILLUMINATED WHEN GEAR LEVER MOVED TO OFF. PERFORMED ABNORMAL PROCEDURE AND LIGHT EXTINGUISHED. OPS CHECKED RIGHT MAIN LANDING GEAR DOOR INDICATING SYSTEM. SYSTEM CHECKED GOOD IAW MM 32-12-1. 2L73 4F4 F A3WE E2EA 20031014000442003101400044NM 2003 10 14 QXEA200301144 120030916A5510 SHIM BOMBDRDHC8 DHC8401 1390041NM ZONE 300 SPLIT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 FORWARD LT HAND HORIZONTAL STABILIZER SHIM IS SPLIT AND STARTING TO SEPERATE. REPAIRED IAW Q400 SRM 55-10-00 AND TASK 55-10-00-400-801. 2H72 4T RTA13NM 20031014000532003101400053NM 2003 10 14 SWAA032181 120030930A3350PH22300L STRIP BOEING737 7373H4 1384600NM PHOTOLUMINESCENTDAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DISCOLORED BETWEEN ROW NR 7 AND ROW NR 9. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20031014001672003101400167NM 2003 10 14 SWAA032087 120030918A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND AFT CABIN FLOORBEAMS CORRODED AT BS 986, AND BS 1016. REPAIRED FLOORBEAMS PER BFG ER. 2L72 4F RTA16WE 20031014001712003101400171 2003 10 14 SWAA032083 420030918A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED PM CHECK, FOUND BOTH AFT DOOR EVAC SLIDES OUT OF POSITION. REPOSITIONED BOTH SLIDES PER MM. 2L72 4F A16WE 20031014001732003101400173 2003 10 14 SWAA032081 420030918A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 FWD SERVICE DOOR EVACUATION SLIDE OUT OF POSITION. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031015000602003101500060NM 2003 10 15 USAASB03156 120030831A335020121 POWER SUPPLY BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19784AU 25023 FOUND LAST TWO SEAT MOUNTED EMERGENCY LIGHTS AND RIGHT AFT DOOR EXTERIOR LIGHT INOPERATIVE. MAINTENANCE REPLACED THE NR 6 POWER SUPPLY. (M) 2L72 4F RTA16WE 20031020000562003102000056NE 2003 10 20 RAIA00310258 220031009A7320 CONTROL UNIT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03570HK 41089 75089 5616-STL- RIGHT INTERGRADED ENGINE CONTROL MALFUNCTION INDICATION. MAINTENANCE CLEARED IEC FAULTS AND PERFORMED GROUND RUN WITH NO DEFECTS NOTED. 2L72 4T4 TRTA41NM E18NE 20031020000612003102000061SO 2003 10 20 C2XA02SH382 120031011A532014590070004 DOUBLER EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 SHV-DURING C-CHECK THE SILL REINFORCEMENT DOUBLER AFT OF THE SERVICE DOOR AT FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED SILL REINFORCEMENT DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031020000912003102000091NM 2003 10 20 CALA0300572 120031003A5310 DOOR FRAME BOEING777 777224 1385225NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777014 29862 INSPECTION FOUND A 7 INCH CRACK IN FORWARD CARGO FORWARD DOOR FRAME CUTOUT POST AT STA 500. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5310-04374. A DIP WAS ISSUED TO INSTALL A PERMANENT REPAIR WITHIN 4000 CYCLES NOT TO EXCEED 24 MONTHS. 2L72 4F RTT00001SE 20031020000922003102000092SO 2003 10 20 C2XA03SH371 120031007A532014522460013 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031020000982003102000098WP 2003 10 20 ABXA030374 120030909A5310995773914 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 SHEAR TIE CRACKED, FS 1021 AT LONGERON 14 RIGHT. REPLACED SECTION OF SHEAR TIE IAW DC-9 SRM. 2L72 4F A6WE 20031020001062003102000106WP 2003 10 20 ABXA030372 120030912A528059107839 CHANNEL DOUG DC9 DC941 302207NWP LT MLG DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 LEFT MAIN LANDING GEAR INBOARD DOOR CRACKED AT FORWARD HINGE. REPLACED PAN SECTION AND REPAIRED AREA, REINSTALLED DOOR IAW DC-9 MM 32-12-01-2 AND SRM 52-05, 53-05, AND 51-30-1. 2L72 4F A6WE 20031020001232003102000123 2003 10 20 RAIA00309250 420030929A3418C850176 VANE JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03561HK115872866 41077 5596-STL- RIGHT STALL WARNING CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE RIGHT STALL VANE. 2L72 4T RTA41NM 20031020001442003102000144EU 2003 10 20 MALA030441 120030930A5220 SKIN SAAB SF340 SF340A 7850100EU EMERGENCY EXIT DENTED A MALAK NONE O OTHER NRNOT REPORTED 1 GL1568XJ 340A068 RT FORWARD EMERGENCY EXIT DOOR OUTER SKIN HAS SMALL DENT AFT OF LOWER RELEASE HANDLE THAT FAILED BOND MASTER INSPECTION. MAINTENANCE REPAIRED IAW EO S52028. A/C RELEASE DATE 10/2/03. 2L72 4T RTA52EU 20031020001462003102000146NM 2003 10 20 0301416627 120030731A3350 BATTERY PACK BOEING747 747251B 1384892NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01627US 21709 DURING LINE CHECK, FOUND A-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040204001422004020400142NM 2004 2 4 EIA2003128 120031020A5330 SKIN BOEING747 747212B 1384886NM PWA JT9 JT9D* NE FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 LT OUTFLOW VALVE STA. 2240 HAS 2 SKIN BULGES AT OPPOSITE CORNERS UPPER AFT AND LWR FWD. REMOVED AND REPLACED DAMAGED SKIN IAW B747 SRM 51-30-02 AND ECRA 482-53-169-2. 2L74 4F4 F A20WE E20EA 20040204001442004020400144NM 2004 2 4 EIA2003133 120031020A5330 SKIN BOEING747 747212B 1384886NM PWA JT9 JT9D* NE FUSELAGE WORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 FUSEALAGE SKIN WORN AT INTERFACE OF VERT STAB SEAL LT SIDE BS 2280-2416. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2 2L74 4F4 F A20WE E20EA 20040204001532004020400153NM 2004 2 4 EIA2003139 120031020A5530 FRAME BOEING747 747212B 1384886NM ACCESS PANEL BROKEN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 VERTICAL STAB RT SIDE ACCESS PANEL 324 DR AFT SECTION OF PANEL ATTACH FRAME HAS SECTION BROKEN OFF. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-55-196-2 2L74 4F A20WE 20040204001992004020400199 2004 2 4 SWIA200312573 420031031A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM0758733 120197 LT STICK SHAKER INOPERATIVE. REPLACED SHAKER. OPS CHECK GOOD. SN OFF: 518 2L72 4T RTA31SO 20040205000052004020500005GL 2004 2 5 P5CA0300987 220031116A7320 WARNING SYSTEM BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL EICAS ACTIVATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23454PA 30812 706485 ON ENGINE START EICAS MESSAGE ENGINE 4 FUEL VALVE WAS DISPLAYED. RESEATED LOGIC CARD Y5BA12 IN ACC WITH MM 73-22-14 WET MOTORED ENGINE IAW MM 71-00-00 ENG PERFORMED NORMAL MESSAGE ERASED. 2L74 4F4 FRTA20WE E23EA 20040205000102004020500010NM 2004 2 5 03FDEA01923 120031117A5512 SKIN DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB RIGHT UPPER FWD PLANK NR 6R BARREL NUT BORE FOUND CORROSION ON SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. 2L73 4F4 FRTA22WE E13NE 20040205000292004020500029NM 2004 2 5 EIA2003150 120031107A3350S1356B37 LIGHT BOEING747 747SR46 1384816NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09478EV 21033 1 CENTER ISLE EMERGENCY LIGHT INTERMITTENT. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD IAW MM 33-51-00. 2L74 4F RTA20WE 20040205000762004020500076EU 2004 2 5 ASOA03659 120031217A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11633AS 344 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040205000952004020500095NE 2004 2 5 GLBA2003157 320031123A61401303800445 INDICATOR BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE NR 1 PROP INOPERATIVE A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM03219GL UE219 NR 1 PROP INDICATOR NEVER WENT ABOVE 1000 ON TAKEOFF ROLL, GROUND RUN OPS CK GOOD. 2L72 4T RTA24CE 5 CP10NE 20040205001022004020500102CE 2004 2 5 FPI2003F00012 120031107A7921654585 OIL COOLER CESSNA210 T210N 2073456CE CONT O550 IO550* SO ENGINE CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO154673C1225 21063586 821018R TOP AND BOTTOM COOLER TO TO ENGINE MOUNTING EARS CRACKED. OCCURRED UNDER NORMAL OPERATION. 1H71 3O3 O 3A21 E3SO 20040205001102004020500110EU 2004 2 5 038431 120031129A2701 CONTROL COLUMN SAAB SF340 SF340A 7850100EU COCKPIT VIBRATION A UHLAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL1719 19XS DURING CLIMB OUT AND CRUISE FLT 4514 FROM PIT TO LYH EXPERIENCED ABNORMAL RAPID VIBRATION IN CONTROL YOKES. CREW WAS ADVISED TO RETURN TO PIT, NO INCIDENT. 2L72 4T RTA52EU 20040205001172004020500117SO 2004 2 5 GLBA2003154 120031121A2150 A/C PACK EMB 120 EMB120ER 3260203SO RIGHT SMOKE A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03293UX 120293 RT PACK BLOWING SMOKE INTO CABIN, REMOVED AND REPLACED RT ENG P2.5 VALVE ASSY OPS CK GOOD. 2L72 4T RTA31SO 20040205001202004020500120NE 2004 2 5 C1HA200381033 220031130A753232146421 BLEED VALVE BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 3 ENGINE MALFUNCTIONED A C1HAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15681CA 22020 ENGINE NR 3 BLEED AIR TRIP LIGHT ILLUMINATED PERFORMED COM PROCEDURE 2.36.2. REMOVED AND REPLACED NR 3 ENGINE BLEED VALVE OPS CHECKS NORMAL IAW MM 36-10-01 OK TO CONTINUE SERVICE. 2L73 4F4 F A3WE E2EA 20040205001282004020500128NM 2004 2 5 MEX2003533 120031123A2934 TRANSMITTER DOUG MD88 MD88 3023688NM HYD QTY LOOSE W ASMFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW23158PL 49761 AIRCRAFT RETURNED AFTER TAKEOFF, RT HYDRAULIC QUANTITY DROPPED TO TWO WITH PRESSURE CORRECT. DURING CHECK IT WAS DETECTED THAT THE MECHANISM BAR OF THE HYDRAULIC QUANTITY INDICATOR TRANSMITTER WAS DISCONNECTED. RIGHT HYDRAULIC QUANTITY INDICATOR TRANSMITTER, BOLT END NUT WERE REINSTALLED IAW MM, TESTS CORRECT. 2L72 4F RTA6WE 20040206000072004020600007CE 2004 2 6 KBM2003F00080 120031029A5610206540023 WINDOW CESSNA501 501 2076603CE PWA JT15 JT15D1 52060NE COCKPIT CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19677JM 5010052 LT FORWARD WINDOW CRACKED AND CRAZED. REMOVED AND REPLACED. 1L72 4F4 F A27CE E1NE 20040206000122004020600012EU 2004 2 6 KBM2003F00090 120031108A6720VG95343T05A010A CONTROL TUBE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 HEAT SHRINK ON TAIL ROTOR FLIGHT CONTROL TUBE WORN AND TORN. REPLACED WITH NEW HEAT SHRINK. 1G71 3U3 UNCH9EU E19EU 20040206000232004020600023EU 2004 2 6 USAASA03142 120031228A3350321431 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19186US 1701 PHL - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST WITH MESSAGE EPSU BAT AFT L. MAINTENANCE REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040206000322004020600032SO 2004 2 6 SIMA200333801 120031203A2600 DUCT EMB 135 EMB135LR 3260305SO PAX AIR CONTAMINATED A SIMAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW21709GB 145211 BOS - FLT 4534 - LAV SMOKE WARNING AND SMOKE IN CABIN REPORTED. VISUALLY INSPECTED ALL CEILING/WALL FLOURESCENT BULBS/SOCKETS/RECEPTICLE ASSEMBLIES AND FOUND NO DEFECTS. FOUND LEFT BLEED DUCT FUSELAGE PASS THROUGH ASSEMBLY TO HAVE FOREIGN FLUID BAKING AROUND DUCT AREA, CLEANED AREA AND RAN ACM NR 1 AND NR 2 FOR 5 HOURS AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040206000372004020600037SO 2004 2 6 SIMA200334501 120031210A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HOIZONTAL STAB FAILED A SIMAO OTHER J WARNING INDICATION CRCRUISE 1 SW21810AE 145525 DFW - FLT 3544 - PITCH TRIM SYSTEM 1-2 INOPERATIVE ON EICAS. COMPLIED WITH ETN EB27-022 AND PERFORMED TROUBLESHOOTING IAW EMB FAULT ISOLATION MANUAL. REMOVED AND INSTALLED HSCU. OPERATIONAL CHECK GOOD IAW 27-40-01. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040206000452004020600045SO 2004 2 6 SIMA200334402 120031128A531112010732001 FRAME EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21725AE 145312 ABI - DURING AN IMBV INSPECTION, FOUND FRAME 81 CHAFED BELOW SRM LIMITS. REMOVED LOWER SECTION OF FRAME. INSTALLED NEW FRAME IAW EMB 145 SRM, SRM EMB-145/1142 REV 24, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20040206000492004020600049WP 2004 2 6 ASAA0380769 120031121A57539957578501 SKIN DOUG DC9 DC983 3022083WP TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND RIGHT INBOARD FLAP LOWER SURFACE IS DENTED. INSTALLED DOUBLER PER SRM 57-01. (M) 2L72 4F RTA6WE 20040206000822004020600082NM 2004 2 6 DHL200342538 120031124A5754 BRACKET BOEING727 727225 1384077NM KRUEGER FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 6 KRUEGER FLAP INBOARD ACT MOUNT CRACKED 2 PLACES. REMOVED SUPPORT BRACKETS IAW B727 SRM 51-30-02, FABRICATED AT 2 EA SUPPORT BRACKETS, 7075-T6 .063 PO 900226 PER SAMPLE DIM 3.5 X 7 INCHES IAW B727 SRM 57-20-02. ALODINED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED SUPPORTS IAW B727 SRM 51-30-02. OPS CHECK GOOD IAW B727 MM 27-81-00. 2L73 4F A3WE 20040204000762004020400076NM 2004 2 4 PCAA0310126 120031020A33506013211 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EMERGENCY LIGHT INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13834EX3486 285 WHILE AIRCRAFT WAS IN MAINTENANCE BASE HAVING EMERGENCY LIGHT TEST PERFORMED IT WAS NOTICED THAT SECOND AND THIRD CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY AT POSITION NR 3. SYSTEM OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040204000892004020400089NM 2004 2 4 QXEA200301290 120031011A5320 BRACKET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-AFT DOOR STOP BRACKET SECOND FROM BOTTOM, HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T4 TRTA13NM E20NE 20040204001502004020400150NM 2004 2 4 EIA2003137 120031020A5330 SKIN BOEING747 747212B 1384886NM FUSLEAGE CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 VERTICAL STABILIZER TO FUSELAGE RIGHT BELOW RUDDER HAS CHAFE CONDITION FROM STA 2605-2608. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2. 2L74 4F A20WE 20040204001612004020400161WP 2004 2 4 ABXA030395 120030927A57209919343 ATTACH FITTING DOUG DC9 DC931 3022065WP LEFT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 INBOARD RIB OF NR 5 SLAT DRIVE LINK HAD AN AFT ATTACH FITTING ATTACHED VERTICALLY TO SPAR AND RIB CRACKED IN 3 PLACES. REPAIRED ATTACH FITTING IAW DC-9 SRM 57-09. 2L72 4F A6WE 20040204001782004020400178NM 2004 2 4 374PA0004 120031102A33505106 LAMP BOEING737 73736M 138443BNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05374PA 28333 RT EMERGENCY OVERWING EXIT SIGN LOCATOR LIGHT INOPERATIVE. RE-LAMPED LOCATOR LIGHT IAW MM 33-51-11. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20040205000932004020500093SO 2004 2 5 GLBA2003155 120031121A3010211C117183 PRESSURE SWITCH EMB 120 EMB120ER 3260203SO VERTICAL STAB FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03108UX 120108 VERTICAL FIN ANNUNCIATOR FAIL ILLUMINATED IN FLIGHT WOULD NOT RESET IN OFF POSITION, REMOVED AND REPLACED VERTICAL FIN PRESS SWITCH, PN 211C117-183. OPS CK GOOD. 2L72 4T RTA31SO 20040205001392004020500139SW 2004 2 5 22811290376 120031128A7603C810242 CONTROL CABLE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCB3T HCB3TN5 GL ZONE 400 CHAFED E D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW17228AM33082166 TC300 P54062 BVA7662 DURING TAKE OFF PREPARATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWER LEVER CABLE HAD BROKEN INSIDE THE CABLE HOUSING IN THE ENGINE COMPARTMENT. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20040206000182004020600018NM 2004 2 6 USAABB03233 120031228A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 PHL - FOUND THE FLOOR EMERGENCY LIGHTS AT SEAT ROWS 19 TO 27, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND WIRE DISCONNECTED FROM SEAT ROW 26 AND BULB BURNED OUT AT SEAT ROW 27. RECONNECTED WIRE AND RELAMPED BULB. OPS CHECK GOOD. (M) 2L72 4F RTA1NM 20040206000202004020600020EU 2004 2 6 USAASA03146 120031231A335032145510 POWER SUPPLY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19174US 1492 LAX - DURING THE EMERGENCY LIGHT TEST, THE MID, RIGHT, FORWARD TEST OF THE EMERGENCY LIGHTING SYSTEM FAILED. MAINTENANCE REPLACED THE RIGHT MID FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONLLY CHECKS OK. (M) 2L72 4F RTA28NM 20040206000412004020600041WP 2004 2 6 ASAA0380828 120031216A52802024T3063 SKIN DOUG DC9 DC983 3022083WP NLG DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND NLG DOOR SKIN IS CREASED ON BOTTOM EDGE. REPLACED DOOR SKIN PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040206000462004020600046EU 2004 2 6 SIMA200335703 120031221A3350 CONNECTOR SAAB SF340 340B 7860101EU EMERGENCY LIGHT LOOSE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21273AE 340B273 PSP - FLT 3048 - FORWARD EXIT SIGN FLICKERS WHEN TESTED. RESECURED CONNECTOR ON POWER SUPPLY NR 21LN. (M) 2L72 4T RTA52EU 20040206000502004020600050SO 2004 2 6 SIMA200335701 120031221A2121 FAN EMB 145 EMB145LR 3260212SO COCKPIT FAILED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21648AE 145225 UPON ENTERING THE A/C THE CREW NOTICED A BURNING ODOR NEAR THE FORWARD CABIN OR COCKPIT. REPLACED NR 1 AND 2 RECIRCULATION FANS, P/N 4611028900 S/N 0729 AND P/N 4611028900 S/N 556. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040206000542004020600054WP 2004 2 6 ASAA0380770 120031121A53135936071503 LONGERON DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND LONGERON CORRODED AT FS 1287. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 53-02 AND 51-10-1. (M) 2L72 4F RTA6WE 20040206000622004020600062WP 2004 2 6 ASAA0380824 120031212A5320993053866 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OKC - DURING C-CHECK, FOUND CUSP WEB CORRODED ON RIGHT SIDE FS 1250. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20040206000642004020600064WP 2004 2 6 ASAA0380810 120031125A5320593056031 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 1099 TO 1212. REPLACED FLOOR SUPPORT PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040206000682004020600068WP 2004 2 6 ASAA0380809 120031123A53305953050547 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OKC - DURING C-CHECK, FOUND SKIN DAMAGED, DENTED, AT FS 229. COLD-WORKED DENT AND INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040206001012004020600101WP 2004 2 6 DHL2004806508 120031229A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 4 FLOOR TRACK PLUG LUGS WORN STA 1140.000. REMOVED NR 4 FLOOR TRACK PLUG STA 1140.000 IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206001042004020600104WP 2004 2 6 DHL2004806514 120030106A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 1 FLOOR TRACK LUG WORN AT STA 290.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED PLUG AND CHANNEL IAW SRM 51-3-0 PG 1, SRM 53-2-3 PG 17. 2L74 4F RT4A25 20040206001142004020600114WP 2004 2 6 DHL2004806502 120031229A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 4 FLOOR TRACK PLUG LUG WORN AT STA 1130.000. REMOVED PLUG WITH WORN LUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 4 FLOOR TRACK IAW SRM 51-3-0. 2L74 4F RT4A25 20040204002032004020400203NM 2004 2 4 P5CA0300978 120031104A324426070812 TIRE BOEING747 747236B 1384804NM MLG FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23924FT 21730 NR 6 MAIN TIRE WORN TO LIMITS (SHREDDED.) REPLACED NR 6 MAIN TIRE AND ALSO NR 5 MAIN TIRE IAW MM 32-45-01. 2L74 4F A20WE 20040204002082004020400208EA 2004 2 4 5427110203 120031102A3397 OVERLAY CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE CONTROL PANEL MISINSTALLED E J7SAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW05321FX 5427 A/C EXPERIENCING AN EMERGENCY LANDING. DISCREPANCY WRITTEN BY CREW DETAILED ELECTRICAL SMOKE, SPARKS FROM AREA OF AUDIO WARNING / OXYGEN CONTROL UNIT PANEL ON FO SIDE OF COCKPIT. TROUBLESHOOTING REVEALED BURNED OUT MATERIAL IN AREA OF BACKLIGHTING PEANUT BULBS IN THE OXYGEN CONTROL UNIT OVERLAY PANEL. WHEN POWER WAS APPLIED, TECH GOT A READING OF 115V AC ON WIRE GOING TO DIMMER CONTROL MODULE. ELECTRICAL PRINTS SHOW THIS WIRE HAVING MAX VOLTAGE OF 5V AC. TRACING WIRE TO SOURCE REVEALED IT WAS SOLDERED TO WRONG SIDE OF STEP DOWN TRANSFORMER, THUS WAS RECEIVING FULL BUSS VOLTAGE. NEW OVERLAY PANEL WAS INSTALLED, WIRE MOVED TO CORRECT POSITION, OPS CHECK, NORMAL. 2L72 4F4 FRTA21EA E15NE 20040204002322004020400232 2004 2 4 GLBA2003149 420031113A2300 CONTROL PANEL EMB 120 EMB120ER 3260203SO COMMS DISCONNECTED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03293UX 120293 CAPTS COMM INOPERATIVE, COULD NOT TRANSMIT, RECONNECTED CAPTS AUDIO PANEL COMM PN 5091-1-1. 2L72 4T RTA31SO 20040205000302004020500030NM 2004 2 5 EIA2003151 120031108A26117400111 FIRE WARNING BOEING747 747SR46 1384816NM WILL NOT TEST A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09478EV 21033 FIRE WARNING TEST WILL NOT SOUND BELL. REMOVED AND REPLACED AURAL WARNING DEVICE IAW MM 31-26-02 PG 41. OPERATION CHECK GOOD IAW MM 31-26-00 PG 502 2L74 4F RTA20WE 20031010000702003101000070NM 2003 10 10 F3LA200300138 120030918A5320 FLOOR SUPPORT BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED AT STA. 486.5 TO 1006, LBL 31.5. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-60-51. 2L72 4F RTA16WE 20031020001662003102000166NM 2003 10 20 DL777030792 120030829A2121218040002 FAN BOEING777 777232 1385232NM RIGHT FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27865DA 29737 RT LOWER RECIRC FAN TRIPPED IN FLT HEAVY ELECTRICAL SMELL DETECTED PRIOR TO FAILURE. REMOVED AND REPLACED RECIRC FAN. SYSTEM OPS CHECK NORMAL. 2L72 4F RTT00001SE 20031020001872003102000187WP 2003 10 20 MWEA030401 120030930A2781H61034 SWITCH DOUG DC9 DC932 3022066WP L/E SLAT INOPERATIVE A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31202ME 47672 NO SLAT EXTEND LIGHT WITH SLATS OUT, SLAT DISAGREEMENT LIGHT INTERMITTENT. REMOVED AND REPLACED LEFT SLAT EXTEND SWITCH. 2L72 4F A6WE 20031020002172003102000217WP 2003 10 20 UPS03841365 120030920A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 760, XFS 785, XFS 797.5, XFS803.75, XFS 810. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20031020002192003102000219WP 2003 10 20 UPS03841367 120030924A532037558452N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 1160 BETWEEN LONG 35R AND LONG 36. REMOVED AND REPLACED FITTING IAW DWG 3755845, AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20031020002262003102000226WP 2003 10 20 UPS03841340 120030923A53203754220503N SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 STA 210 LONG 31L SPLICE FITTING IS BROKEN. REMOVED AND REPLACED FITTING IAW DWG 3754220 AND SRM 51-1-20D. 2L74 4F RT4A25 20031020002362003102000236WP 2003 10 20 UPS03841343 120030924A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 SEAT TRACK IS CORRODED BEYOND LIMITS AT REPAIR PLUG AT STA 1400 AT RBL 46. CUT OUT SEAT TRACK BETWEEN STA 1370 TO 1410, FABRICATED AND REPLACED SEAT TRACK SECTION IAW DC8-5320-8309 APPX B. 2L74 4F RT4A25 20031020002542003102000254NE 2003 10 20 AT0300029 220031001A7250 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 FIRE A ZZDAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SO15977AT 55036 TAIL PIPE FIRE WHILE ATTEMPTING TO START NR 2 ENGINE. PERFORMED STEP'S OT LINED IN ROLLS ROYCE TECHNICAL VARIANCE 5974. INSPECTED AND CLEANED ENGINE IAW MM CHP 71-00-2 AND STARTED ENGINE WITH SUCCESSFUL TIMES, NO FAULTS NOTED ON EEC NR 2 ENGINE FOR SERVICE AT THIS TIME. 2L72 4F4 FTRA6WE E00061EN 20031020003042003102000304NM 2003 10 20 2003UALA00730 120030927A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29369UA 24538 THREE DENTS IN FUSELAGE SKIN ABOUT 24 INCHES AFT OF DOOR 2R, JUST FWD OF APU INLET. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPLACEMENT PANEL. 2L72 4F4 FRTA16WE E2GL 20031021000352003102100035WP 2003 10 21 GTIA030701 120030908A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND FORWARD CABIN, STATION 200, LBL 22 INCHES HAS CORROSION AT SUPPORT END FITTING INBOARD SEAT TRACK ATTACH. REMOVED TRACK STATION 200 TO 234. FABRICATED NEW TRACK. FABRICATED ATTACH FITTING. INSTALLED NEW TRACK AND ATTACH FITTING. (M) 2L72 4F A6WE 20031021000392003102100039WP 2003 10 21 GTIA030703 120030909A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND PASSENGER CABIN STATION 826-864, FLOOR PNL LEFT SIDE INBOARD HAS PUNCTURE/CRACKS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20031021000402003102100040WP 2003 10 21 GTIA030704 120030909A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND PAX CABIN FLOOR PANEL RBL 44 INCHES STATION 465-547 HAS CRACKED/DAMAGE ON EDGE/INSERT BROKEN OUT. FABRICATED FLOOR PANEL. (M) 2L72 4F A6WE 20031021000902003102100090SO 2003 10 21 SIMA200326807 120030920A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 22, CHAPTERS 53-24-02 AND EMB IC2003-145/3093A. (M) 2L72 4F RTT00011AT 20031021000922003102100092SO 2003 10 21 SIMA200323902 120030824A49204504113 APU EMB 145 EMB145LR 3260212SO APU BAY FIRE A SIMAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TXTAXI/GRND HDL 1 SW21615AE 145087 ORD - FLT 4036 - DURING GROUND OPERATIONS, CREW RECEIVED AN APU FIRE WARNING. APU WAS SHUTDOWN. MAINTENANCE INSPECTION REVEALED EVIDENCE OF FIRE WITH THE WIRING HARNESS AND COWLING BURNED. MAINTENANCE COMPLIED WITH AN APU FIRE INSPECTION IAW EMB MM FOLLOWED BY REMOVING AND REPLACING THE APU IAW EMB MM. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031021001282003102100128NM 2003 10 21 AALA20030985 120030910A335030234117 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21794AN 30256 DFW - DURING OVERNIGHT MAINTENANCE, TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE AFT GALLEY FORWARD WALL LEFT MOUNTED LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030915000812003091500081EU 2003 9 15 BAQA089051 120030908A77149550165760 SENSOR UROCOPEC135 EC135T1 5620026EU NR 1 ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME2001 0157 FADEC FAIL CODE N2B AND N2A ON NR 1 ENGINE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030916000032003091600003WP 2003 9 16 ANCF200300022 120030819A5310 STRUCTURE DOUG DC9 DC983 3022083WP FUSELAGE VIBRATION W ANCFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO23593AN 53093 DURING INITIAL CLIMB THERE WAS HARD NOISE AND LOW VIBRATIONS IN THE FRONT WINDOW (CENTER WINDSHIELD). CENTER WINDSHIELD WAS CHECKED FOR CONDITION. THIS AREA WAS SEALED AND IT WAS INSTALLED TAPE IAW AMM 56-10-01 PAG 201 - 213 (ITEM 12). 2L72 4F RTA6WE 20030916000072003091600007NM 2003 9 16 S03453041 120030620A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE CORRODED W SAJFO OTHER O OTHER NRNOT REPORTED 1 WP03 29219 B-18207 FUSELAGE SKIN CORROSION COMMON TO BS 781.1 TO BS 802, STRINGER 47L TO STRINGER 47R REPAIRED PER EO 744-53-10-0019R1 2L74 4F4 FRTA20WE E24NE 20030916000532003091600053NE 2003 9 16 52767AMWA02 220030720A7532 BLEED VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE INOPERATIVE A AMWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE07144ZV UE144 DURING TAKE OFF ON FLIGHT 5578, THE POWER ADDED TO THE RT ENGINE WOULD NOT DEVELOP MORE THAN 1000 FT LBS TORQUE. THE CREW ABORTED TAKE OFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BLEED VALVE AND THE PROP GOVERNOR. STILL AWAITING MORE INFORMATION TO COME. REFER TO SDR 52767. 2L72 4T4 TRTA24CE E26NE 20030916001542003091600154NM 2003 9 16 03FDEA00979 120030624A5754ARC2850505 SLAT TRACK DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 SUSPECT HAIRLINE CRACK ON LT WING NR 16 SLAT TRACK INBOARD FITTING. REMOVED AND REPLACED RIB AT LT WING LEADING EDGE INBOARD SLAT TRACK NR 16 SUPPORT IAW SRM 51-31-01 VOL. II AND DRAWING NR ARC2850. 2L73 4F RTA22WE 20030916001562003091600156NM 2003 9 16 PCAA0307084 120030722A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13849EX 337 DURING A ROUTINE MAINTENANCE VISIT 1 FLOOR PATH EMERGENCY LIGHT WAS FOUND INOPERATIVE AT ROW 7. A BROKEN WIRE WAS REPAIRED IN EMERGENCY LIGHTING SYSTEM. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030917000452003091700045NM 2003 9 17 S2YA03017 120030428A2430230GC02Y04 PANEL DORNERDO32 DO328300 NM LT GENERATOR INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13351SK 105 3108 DURING TAKEOFF OF FLIGHT 2274, A CAS MESSAGE ILLUMINATED FOR LT DC GENERATOR FAIL. THE CREW ABORTED THE TAKEOFF. SINCE THE LEFT GENERATOR CAN NOT BE MEL-ED THE FLIGHT WAS CANCELLED AND THE AIRCRAFT WAS FERRIED BACK. MECHANIC REPLACED THE DC POWER CONTROL UNIT (1VE PANEL) AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DEFECTS. 2H72 4T RTA55NM 20030917000542003091700054CE 2003 9 17 DXTA200300082 120030811A2840 WARNING LIGHT CESSNA750 750 2076810CE FUEL SYSTEM ILLUMINATED E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07909QS 7500009 "WING TANK O' FULL -R" MESSAGE CAME ON AT CRUISE . RT TANK SHOWED APPROX 3100 LBS , LT WING APPROX 200 LBS . TOTAL QUANTITY DECREASED APPROX 300 LBS IN LESS THAN A MINUTE. FUEL OBSERVED DUMPING FROM RIGHT WING OUTBOARD VENT, VENTING STOPPED DURING DECENT. POWERED UP AIRCRAFT, NO "WING TANK O'FULL R" MESSAGE, OPENED RT WING PANELS TO GAIN ACCESS TO VENT LINES FROM WING TANK TO SURGE TANK IN DRY BAY AREA, FOUND SOME FUEL IN DRY BAYS. GAINED ACCESS TO OUTBOARD WING VENT FLOAT VALVE REMOVED AND REPLACED VALVE, OUTBOARD WING FLAPPER/CHECK VALVE O.K. CLOSED ACCESS PANELS. ALL WORK DONE IAW CE750 MM CHAPTER 28-10-00. 2L72 4J RTT00007WI 20030917000802003091700080EU 2003 9 17 BAQA089102 120030911A6330L633M2010105 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135QC17 0281 MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030917000912003091700091NM 2003 9 17 AMTA200301122 120030831A2840300710505 COMPUTER BOEING757 75733N 1384931NM E/E BAY MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11550TZ 32584 FUEL TANK AND TOTAL FUEL QTY INDICATORS BLANK, INTERMITTENT, EICAS MSG FUEL QTY IND DISPLAYED FUEL QTY TEST NOT CHECKED. T/S PER FIM 28-41-00 FIG 117. REMOVED AND REPLACED FQIS PROCESSOR. INSPECTED THE HI-Z LO-Z PLUG CONNECTION AT LEFT MAIN TANK RECEPT. OPS CHECK GOOD. NO FAULTS OR MSG'S. (M) 2L72 4F RTA2NM 20030917001192003091700119CE 2003 9 17 ENHA20038411 120030724A5520 HINGE BEECH 90 65A901 1152901CE ELEVATOR CRACKED E ENHAK NONE O OTHER ININSP/MAINT 1 AL0370841 LM73 ELEVATOR OUTBOARD HINGE AREA CRACKED. FOUND DURING INSPECTION PER AD. REPLACED ELEVATOR ASSY WITH SERVICEABLE. 1L72 3T 3A20 20030918000022003091800002NM 2003 9 18 03FDEA01499 120030911A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON FLOORBEAM BS 1030 RBL 25-0 WL 208 INSTALLED REPAIR PARTS PER/ UPPER CHORD PER SRM 53-10-8 2L73 4F RTA3WE 20030918000062003091800006NM 2003 9 18 03FDEA01503 120030911A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON FLOORBEAM UPPER FLANGE UPPER & LOWER SURFACE AT NUTCLIP HOLES STA 950D LBL 10 & 21 WL 208. CUT OUT FLOORBEAM & REPAIRED PER SRM 53-10-8. 2L73 4F RTA3WE 20030918000102003091800010NM 2003 9 18 03FDEA01507 120030911A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON UPPER CHORD OF FLOORBEAM BS 1130 LBL 32 AND 37 WL 208. REMOVED DAMAGED AREA OF FLOORBEAM, FABRICATED REPAIR ALODINED, PRIMED, PAINTED & INSTALLED REPAIR IAW SRM 53-10-8 FIG 10 BS 1130 LBL 32-38 WL 208. 2L73 4F RTA3WE 20030918000142003091800014NM 2003 9 18 03FDEA01511 120030911A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION BS 1070, WL 201, LBL 25-45 AROUND AND IN NUT CLIP HOLES. CORROSION ON FLOORBEAM BS 1070, WL 201, LBL 25-45 AROUND END IN NUT CLIP HOLES FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOOR BEAM IAW SRM 53-10-8. 2L73 4F RTA3WE 20030918000272003091800027NM 2003 9 18 GAIA03030SP 120030719A5311 FRAME BOEING727 727* NM FUSELAGE DAMAGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 460 HAS A TOOLING HOLE INTO THE RADIUS AT STRINGER 17R FASI N/R 35747. CUT OUT DAMAGE AREA, FABRICATED DOUBLER FROM 7075-T6 .063 PO NR 9912495 DIM 3.5 INCH BY 7.75 INCH, INSTALLED REPAIR IAW B727 SRM 51-30-2. (M) 2L73 4F RTA3WE 20031002000472003100200047WP 2003 10 2 UPS03841203 120030828A53403754041501 FITTING DOUG DC8 DC873F 302199FWP LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, STATION 300 LONG. 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3754041,SRM.53-2-0 FIG. 1B, DWG. 9751879. 2L74 4F RT4A25 20030918001102003091800110NM 2003 9 18 PCAA0308095 120030806A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13849EX 337 DURING ROUTINE MAINTENANCE VISIT ONE EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE BY ROW 8DF. MAINTENANCE REPLACED THE BULB AND REPAIRED A BROKEN WIRE AT THE BULB SOCKET. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030918001382003091800138SO 2003 9 18 GLBA2003117 120030807A499732540 RELAY EMB 120 EMB120ER 3260203SO APU BURNED OUT A GLBAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03293UX 120293 PILOT REPORTS ELECTRICAL ODOR IN COCKPIT, R&R APU RELAYS 2L72 4T RTA31SO 20030919000562003091900056WP 2003 9 19 ARWA20030802 120030810A32600080004003 PROXIMITY SWITCH DOUG DC8 DC862F 3021972WP MLG INOPERATIVE A ARWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19791AL 46150 GEAR NOT LATCHED; LIGHT ILLUMINATED AFTER GEAR UP. FOLLOWED ABNORMAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED PROXIMITY SWITCH BOX SYSTEM BITE TEST NORMAL AND OPERATIONAL CHECK NORMAL WITH GEAR SWING IAW MM 32-60-0. 2L74 4F 4A25 20030919000582003091900058CE 2003 9 19 T0DR200300002 120030809A2720S3381 FAIRLEAD CESSNA CB3 CESSNA310 310Q 2074242CE ALIDSGTFE731TFE7313AR WP ZONE 100 BROKEN E T0DRA UNSCHED LANDING F FLT CONT AFFECTED TOTAKEOFF 1 CE03122E 5953 310Q0984 RUDDER JAMMED UPON ROTATION. (RUDDER SYS JAM) CHECKLIST. ALL KNOWN SYSTEMS SUSPECTED OF HAVING BRG ON RUDDER SYS. ALL OTHER FLIGHT CONTROL SYS OPERATED NORMALLY AND AC CONTROL WAS NEVER IN DOUBT. EMERG WAS DECLARED, 2 TOWER FLY-BYS WERE EXECUTED TO ALLOW TOWER TO VISUALLY INSPECT GEAR. AC WAS WITHIN LANDING WEIGHT, EMERG EQUIPMENT WAS IN PLACE, NORMAL LANDING WAS EXECUTED. RUDDER CONTROL SYSTEM (UNJAMMED) ON TOUCHDOWN. NOSEWHEEL STERRING SYS OPERATED NORMALLY AND AC WAS TAXIED BACK TO HANGER. A COMPLETE INSP OF RUDDER CONTROL SYS WAS ACCOMPLISHED. FOUND RUDDER GUSTLOCK ASSEMBLY CABLE FAIRLEAD BROKEN WITH VERY CONVINCING EVIDENCE VIA CABLE IMPRINT INTO PIECES THAT BROKEN FAIRLEAD JAMMED CABLE. 1L72 3O4 F 3A10 E6WE 20031210001202003121000120NM 2003 12 10 03FDEA01966 120031121A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT OUTBOARD FLAP FOUND INBOARD HINGE PIVOT BOLT HOLE NR 3 INBOARD SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031210001272003121000127NM 2003 12 10 ABXA030449 120031123A2560 CLIP BOEING767 767281 1385109NM L1 DOOR BROKEN A ABXAK NONE O OTHER NRNOT REPORTED 1 GL23789AX 5682 23022 L1 DOOR EMERGENCY ESCAPE SLIDE ACCIDENTALLY DEPLOYED BY FLIGHT CREW MEMBER. DOOR BUSTLE PHENOLIC GUIDE CLIPS ALSO BROKEN. MAINTENANCE REPLACED THE L1 SLIDE AND BUSTLE ASSEMBLIES IAW B767 MM 25-66-00-2. DOOR OPERATION OPS CHECKED GOOD. 2L72 4F RTA1NM 20031210001292003121000129NM 2003 12 10 AALA20031332 120031126A3397 WIRE BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21355AA 24036 LAX SEAT MOUNTED EMERGENCY LIGHT AT 11H INOPERATIVE. REPLACED BROKEN WIRE AT CONNECTOR AT SEAT MOUNTED EMERGENCY LIGHT AT 11H. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA1NM 20031210001502003121000150NM 2003 12 10 AALA20031366 120031201A3397 WIRE BOEING767 767323 1385205NM GALLEY BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21380AN 25449 SFO ARROW EMERGENCY LIGHT BEHIND AFT RT GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR ARROW EMERGENCY LIGHT BEHIND AFT RT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA1NM 20031210001602003121000160NM 2003 12 10 AALA20031268 120031114A3397 WIRE BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21374AA 25201 LAX FORWARD GALLEY RT AISLE EMERGENCY FLOOR FLOOD LIGHT INOPERATIVE. REPAIRED WIRING FOR FORWARD GALLEY RT AISLE EMERGENCY FLOOR FLOOD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA1NM 20031210001612003121000161WP 2003 12 10 AALA20031267 120031114A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21432AA 49350 DFW FOUND OVERHEAD TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERHEAD TAIL CONE EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210001702003121000170WP 2003 12 10 CALA0300681 120031202A335060030451 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2771828 49488 THE BATTERY CHARGER FOR EMERGENCY EXIT LIGHTS AT THE L-2 DOOR WAS FOUND INOPERATIVE. THE CHARGER WAS REMOVED AND REPLACED IAW MM 33-53-00, PAGE 401. 2L72 4F A6WE 20031210001812003121000181NM 2003 12 10 CALA0300633 120031110A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND FORWARD SIDE OF LOWER ATTACH STRAP CORRODED AT STA 1016 BETWEEN STRINGER 26 AND 27. THE ATTACH STRAP WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031210001842003121000184NM 2003 12 10 CALA0300636 120031108A5753 FITTING BOEING737 737824 13844BZNM T/E FLAP GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718223 28932 TWO GOUGES WERE FOUND ON THE BRIDGE FITTING FOR THE LT INBOARD FLAP OUTBOARD CARRIAGE DURING A FLAP CHANGE. THE GOUGES WERE IN THE CENTER OF THE PART DIRECTLY BELOW THE BALLSCREW AND APPEARED TO BE CAUSED BY CONTACT WITH THE BALLSCREW. THE BRIDGE FITTING WAS REPAIRED IAW ECRA 2751-01122. 2L72 4F RTA16WE 20040210001232004021000123EA 2004 2 10 WVB2003F00001 220031112A8520 CRANKSHAFT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT ENGINE BROKEN E WVBAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 AL0159764 317652037 L785161A ON APPROACH, ON 10 NOVEMBER 2003, THE PILOT NOTICED FUEL FLOW FLUCTUATIONS AND AN ABRUPT LOSS OF OIL PRESSURE ON THE LT ENGINE AND IMMEDIATELY SHUT THE ENGINE DOWN. PILOT CONTINUED FLIGHT AND LANDED SAFELY WITHOUT FURTHER INCIDENT. PILOT IMMEDIATELY REPORTED THIS PROBLEM TO MAINTENANCE, WHO CAME IMMEDIATELY TO INVESTIGATE THE REPORTED DEFICIENCY. THE MECHANIC DISCOVERED THAT BOTH CASE HALVES WERE CRACKED IN THE VICINITY OF THE SHARED INTAKE CAME LOBE FOR NR 3 AND NR 4 CYLINDERS. FURTHER INVESTIGATION IS NECESSARY TO DETERMINE THE EXACT NATURE OF THE FAULT. WE ARE PROVIDING THIS AMENDMENT TO HELP EXPLAIN THE REASONS BEHIND THE SDR REPORT DATED 11/12/03 REGARDING THE ENGINE PROBLEMS. PURCHASED THIS ENGINE1L72 3O3 O A20SO E14EA 20040212000682004021200068NE 2004 2 12 MDR03036 120031120A65206535807053043 HOUSING SKRSKYS64 S64F 8142610NE PWA JFTD12JFTD12A4A 52047NE T/R GEARBOX CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09223AC 1313 64086 THE TGB CENTER HOUSING WAS FOUND CRACKED WHILE INSTALLED ON THE AIRCRAFT. IT WAS REMOVED PREMATURELY ON DECEMBER 20, 2000. THE SHOP DETECTED THE CRACK VISUALLY. THE CRACK BEGAN AT THE SECOND ROSAN STUD CLOCKWISE FROM THE ROSAN SEAT PAD LOCATED 34 DEGREES FROM CENTERLINE OF INPUT BORE. THE CRACK EXTENDED RADIALLY THROUGH 3.8-16 NC TAPPED BORE ABOUT .7500 OF AN INCH THROUGH THE WEB. PROBABLE CAUSE IS UNKNOWN AT THIS TIME. 2G72 4U4 U H6EA E15EA 20040212000972004021200097WP 2004 2 12 EIA2003169 120031208A2560118075 SMOKE GOGGLES DOUG DC9 DC933F 302207AWP PWA JT8 JT8D9 52048NE COCKPIT TORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09944F 47194 SECONDARY OBSERVERS SMOKE GOGGLES FOUND ON INSPECTION TO BE TORN AND UNUSABLE. DMI NR 673 ISSUED IAW MEL 25-10-2 WITH PLACARD INSTALLED. CAT D DUE 4/08/04 2359Z. DMI CLEARED 12/9/03 AND PLACARD REMOVED ON SUBSEQUENT STOP IN SEA. 2L72 4F4 F A6WE E2EA 20040212001162004021200116NM 2004 2 12 0302156745 120031210A5497BACC63AF2430S8 CONNECTOR BOEING747 747222B 1384904NM PWA JT9 JT9D7R4G2 52054NE NR 1 NACELLE SHORTED A NWAAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 GL01645NW 23736 715251 DURING NR 1 ENGINE START, THE GROUND CREW REPORTED A FIRE IN THE NR 1 ENGINE. THE FLIGHT CREW DISCHARGED BOTH FIRE BOTTLES AND THE GROUND CREW USED GROUND FIRE EXTINGUISHING AGENT TO SUPPRESS THE FIRE. MAINTENANCE INSPECTED THE ENGINE AND FOUND PYLON PLUG D0014J INTERNALLY SHORTED. THE CONNECTOR WAS REPLACED AND THE ENGINE CONDITION MOTOR OPERATION WAS NORMAL. THE AIRCRAFT WILL BE FERRIED TO ORD AND THE ENGINE REPLACED DUE TO INGESTION OF THE GROUND FIRE EXTINGUISHING AGENT. 2L74 4F4 FRTA20WE E3NE 20040212001552004021200155EA 2004 2 12 WVE2003F00022 120031207A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE RT ENG NACELLE LOOSE A WVERO OTHER O OTHER NRNOT REPORTED 1 EA09614QX 10049 RT ENGINE PYLON HAS A TOTAL OF 8 LOCK FASTENERS THAT ARE LOOSE. PYLON IS SUSCEPTIBLE TO STRESS AND VIBRATION FROM THE ENGINE. REMOVE EXISTING FASTENERS AND ENLARGE THE HOLES TO A .2606 INCH-.026636 INCH DIAMETER. INSTALL HST111AG8XX HI-LITE INTO THE ENLARGED HOLE USING HST1488TP8 COLLARS IAW EA R5442 AND EO 601R544444 DATED 12/03/03. (EA09200401173) 2L72 4F4 FRTA21EA E15NE 20040212001822004021200182NM 2004 2 12 AWXA200301593 120031202A575465C26602217 SKIN BOEING737 73733A 1384673NM SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK FOUND THE NR 2 LEADING EDGE SLAT DISBONDED AT OUTBOARD CORNER. MAINTENANCE CUTOUT DAMAGED AREA NR 2 LEADING EDGE SLAT AT OB CORNER; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. 16, PG. 67-69. 2L72 4F RTA16WE 20040212001912004021200191NE 2004 2 12 ANCF200300030 220031219A731442D39542D362 PRESSURE SWITCH BOEING767 767259 1385136NM PWA 4056 PW4056 NE FUEL PUMP ACTIVE W ANCFO OTHER J WARNING INDICATION CRCRUISE 1 SO23985AN 24618 EICAS MSG R ENG FUEL FILTER DISPLAYED. C/A: WAS REPLACED FUEL FILTER ELEMENT IN RT ENGINE IAW A-M-M 73-11-02. FUEL PUMP FILTER DIFFERENTIAL PRESSURE SWITCH WAS REMOVED AND REPLACED IAW AMM 73-34-01 PAGE 401. P/N ON AND OFF 42D395//42D362, S/N ON 0111, S/N OFF 1810. 2L72 4F4 FRTA1NM E24NE 20040212001942004021200194GL 2004 2 12 S03J72100 220031222A7230 COMPRESSOR WHEEL BOEING747 747400 NM GE CF6 CF680C2* GL NR 4 ENGINE DAMAGED W SAJFD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP03 30765 DURING TAXING TO RUNWAY, NR 4 ENGINE SPOOLED DOWN, AND COULD NOT ACCELERATE TO IDLE WITH AUTOSTART. NR 3 ENGINE SPOOLED DOWN AND EGT RAISED TO 977 DEGREE DURING AIRCRAFT TAXING BACK TO PARKING SPACE. BORESCOPE INSPECTION FOUND BOTH ENGINES, HPC WERE DAMAGED. AOG TEAM, SPARE ENGINES, TOOL AND REQUIRED MATERIAL WAS LEAVING FOR ENGINE REPLACEMENT. 2L74 4F4 FRTA20WE E23EA 20040212001952004021200195EU 2004 2 12 CX7A194J0356 120031228A26131734362450 DETECTOR SAAB SF340 340B 7860101EU TAIL PIPE ACTIVATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03303CE 340B194 ABORTED TAKEOFF DUE TO TAILPIPE HOT LIGHT ILLUMINATING ON LT SIDE. 2L72 4T RTA52EU 20040212001962004021200196EU 2004 2 12 CX7A194J0357 120031228A26131734362450 DETECTOR SAAB SF340 340B 7860101EU TAILPIPE ACTIVATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03307CE 340B204 ABORTED TAKEOFF DUE TO RT TAILPIPE HOT LIGHT. 2L72 4T RTA52EU 20040212001992004021200199NM 2004 2 12 CALA0300721 120031223A5415 FITTING BOEING737 7373T0 1384582NM NR 2 PYLON CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND NR 2 ENGINE PYLON OB CROSSBEAM MOUNT FITTING CORRODED. THE FITTING WAS REPAIRED IAW ECRA 5440-01235. 2L72 4F RTA16WE 20040212000062004021200006WP 2004 2 12 UPS03841623 120031117A53403755822U515 FITTING DOUG DC8 DC871F 302199DWP FWD. LOWER CARGOCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, BATHTUB FITTING IS CRACKED AT STATION 320 BETWEEN LONG. 27L AND 28L. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822 AND SRM.53-2-0 FIG.2D. 2L74 4F RT4A25 20040212000542004021200054SW 2004 2 12 KBM2003F00096 120031119A5415206031594003 BEARING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL RT PYLON MOUNT WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP1973DP 2513 RT SIDE PYLON MOUNT FORWARD/AFT BEARING WORN. INSTALLED 2 NEW BEARINGS. 1G71 3U3 U H2SW E4CE 20040212001322004021200132NM 2004 2 12 DHL2003742514 120031104A5711 FRAME BOEING727 727225 1384077NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, RT WING L/E 130 INT FRAME IS CRACKED ON LOWER SKIN ATTACH ANGLE. STOP DRILL IAW B-727 SRM 51-10-1. REMOVED FASTENERS ON RT WING BL 92 INT FRAME VERT STIFFENER IAW B-727 SRM 51-30-2. FABRICATED DOUBLER FROM 7075 T6 .040 PO 900226 DIM 4.625 INCH X 2.25 INCH IAW B-727 B-727 SRM 51-40-3. TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED DOUBLER IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040205000552004020500055EU 2004 2 5 ASOA03670 120031224A33503012140 LENS AEROSPATR72 ATR72 EU CABIN CEILING MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 FLT 4268 - DURING A GROUND INSPECTION IN ATL, THE EXTERIOR EXIT LIGHT AT THE REAR SERVICE DOOR WAS MISSING THE COVER. MAINTENANCE REPLACED THE MISSING EXIT LIGHT COVER. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040205000652004020500065EA 2004 2 5 ASOA03665 120031220A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11914EV 7752 FLT 4351 - DURING AGROUND INSPECTION IN MGM, THE RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKES GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205001192004020500119 2004 2 5 MEX2003530 420031122A2565 LIGHT BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE ESCAPE SLIDE INOPERATIVE W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23806AM 26273 AIRCRAFT RETURNED TO PLATFORM DURING TAXIING RT AFT SLIDE ARMED LIGHT DID NOT TURN ON. AT PLATFORM, TECH PERSONNEL SWAPPED BOTH AFT SLIDE LIGHTS, AND CLEANED PROXIMITY SENSOR IAW MM 25-10-00, TESTS CORRECT. 2L72 4F4 FRTA2NM E17NE 20040205001372004020500137NM 2004 2 5 DHL2003765002 120031129A3260 POSITION SWITCH BOEING727 727264 138408MNM MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01765AT 23014 AFTER SELECTING GEAR UP, RT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, LIGHT WHEN OUT. CLEANED RT MAIN GEAR DOOR POSITION SWITCH, OPS MAIN GEAR DOOR GOOD IAW B-MM 32-12-1. 2L73 4F A3WE 20040206000132004020600013EU 2004 2 6 KBM2003F00092 120031022A6730123668P BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH3568 2337 END BEARINGS WORN. REPLACED WITH NEW BEARINGS. 1G71 3U3 UNCH9EU E19EU 20040206000192004020600019EU 2004 2 6 USAASA03147 120031231A3350321431 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19174US 1492 LAX - DURING THE EMERGENCY LIGHT TEST, THE MID, RIGHT, AFT TEST OF THE EMERGENCY LIGHTING SYSTEM FAILED. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AT RIGHT SIDE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040206000212004020600021EU 2004 2 6 USAASA03145 120031228A3350321431 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19182UW 1536 LAX - THE R-3 EMERGENCY DOOR EMERGENCY POWER SUPPLY UNIT DID NOT TEST DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE BATTERY FOR THE EMERGENCY POWER SUPPLY UNIT. (M) 2L72 4F RTA28NM 20040206000512004020600051WP 2004 2 6 ASAA0380766 120031121A531099360737 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT FS 693. REPLACED SHEAR TIE PER SRM 51-10-2, 3, 4, 5. (M) 2L72 4F RTA6WE 20040206000612004020600061WP 2004 2 6 ASAA0380691 120031026A5330593602229 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND AFT CARGO BAY SKIN IS CORRODED AROUND FASTENERS AT FS 1079. INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F A6WE 20040206002312004020600231NM 2004 2 6 AWXA200400092 120030104A5330654577678 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN STR 27 LT AND STR 27 RT, BL 0. MAINTENANCE TRIMMED OUT DAMAGED SECTION OF SKIN BETWEEN BS 747 AND BS 767, BL 0; FABRICATED A FILLER AND REPAIR PLATE; INSTALLED REPAIR PARTS IAW AWA ER 03-5331-04017-ES1. 2L72 4F RTA16WE 20040205001212004020500121NM 2004 2 5 QXEA200301479 120031126A2440 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09405QX 4047 AFTER STARTING NR 2 ENGINE NOTICED DISCHARGE OF BATTERIES FOLLOWED BY OBSERVATION OF SMOKE FROM GPU RECEPTICAL. INSPECTED AND FOUND GROUND POWER UNIT PLUG MALFUNCTIONED. CLEANED RECEPTICAL AND REMOVED AND REPLACED PLUG. 2H72 4T RTA13NM 20040205001342004020500134NE 2004 2 5 P5CA0301000 220031121A753077385649 CHECK VALVE BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE 8TH STAGE FAILED A P5CAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23505MC 21251 517343 NR 1 ENG AT TOP OF DESCENT, FL 380, ENG. STALLED. ENG. RECOVERED AT FL 330 AND STALLED AGAIN. ENGINE SHUT DOWN. REMOVED AND REPLACED 8TH STAGE CHECK VALVE RUN UPPER LEAK CHECK, OK IAW MM 36-11-02 AND 71-00-43. 2L74 4F4 FRTA20WE E23EA 20040210000202004021000020WP 2004 2 10 UPS03841594 120031115A53403758497U1 FITTING DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 1140 LONG. 35L FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG.3758497 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040210000232004021000023WP 2004 2 10 UPS03841597 120031117A53403754041U501 FITTING DOUG DC8 DC871F 302199DWP CARGO DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, A-PIT DOOR FWD. BUMPER SUPPORT FITTING IS CRACKED AT STA. 300 LONG. 27L. REMOVED AND REPLACED FITTING IAW DWG. 3754041 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040210000242004021000024WP 2004 2 10 UPS03841598 120031121A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS ATATION 1050 TO 1120 AT LONGERON 31R. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM. 53-4-1 FIG. 17, 51-1-20D,51-1-21. 2L74 4F RT4A25 20040212001602004021200160NM 2004 2 12 UIA9214 120031222A57535910043511 VANE DOUG MD90 MD9030 3023690NM TE FLAP CRACKED Z K NONE O OTHER ININSP/MAINT 1 TW0017922 53601 DURING ROUTINE CHECK, CORROSION WAS FOUND ON LT IB FLAP OB VANE TRAILING EDGE LOWER SURFACE,LT OB FLAP OB VANE TRAILING EDGE LOWER SURFACE, AND RT IB FLAP OB VANE TRAILING EDGE LOWER SURFACE. REMOVE THE CORRODED AREAS AND MAKE THE REPAIR. 2L72 4F RTA6WE 20040217000192004021700019EU 2004 2 17 ASOA03686 120031204A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE LEFT AND RIGHT OUTBOARD SEAT TRACKS BETWEEN FS 29-36 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SEAT TRACKS BETWEEN FS 29-36 IAW SRM 51-25-01 AND 53-00-00. (M) 2H72 4T RT 20040217000202004021700020EU 2004 2 17 ASOA03684 120031201A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FS 36-39 NEAR FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FS 36-39 IAW SRM 51-25-02. (M) 2H72 4T RT 20040217000432004021700043 2004 2 17 2004F00069 420031017A2210 SWITCH BOEING727 727222 1384073NM CAPT'S YOKE MALFUNCTIONED A RYNAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW077639U 19912 DURING FLIGHT, AIRCRAFT DECLARED EMERGENCY ON DESCENT TO PHX. AUTOPILOT FAILED TO DISCONNECT. AIRCRAFT LANDED AT PHX WITHOUT FURTHER INCIDENT. CLEANED AUTOPILOT DISENGAGE SWITCH ON YOKE AND OPERATIONAL CHECK NORMAL. (M) 2L73 4F A3WE 20040217000782004021700078SO 2004 2 17 ZLW2004F00000 120030923A3411 PITOT LINE GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU AIRSPEED IND CLOGGED B ZLWRO OTHER N FALSE WARNING CLCLIMB 1 SW1536MW 89 AC WAS ON TAKEOFF ROLL WHEN THE FLIGHT CREW NOTED A SUBSTANTIAL SPLIT BETWEEN AIRSPEED INDICATORS. AC WAS TAXIED BACK FOR TROUBLESHOOTING. PITOT/STATIC CHECKS WERE ACCOMPLISHED AND DISCREPANCY DUPLICATED. ALL PITOT AND STATIC LINES WERE DISCONNECTED AND NITROGEN WAS BLOWN INTO THE LINES. SEVERAL BUGS WERE REMOVED FROM THE LINES. ALL LINES WERE RECONNECTED AND PITOT/STATIC CHECKS RE ACCOMPLISHED AND ALL CHECKS NORMAL IAW MFG MM. (SW15200402394) (K) 2L72 4F4 FRTA12EA E2EU 20040217000892004021700089SO 2004 2 17 AYQ2004F00000 220030123A7414 IMPULSE COUPLINGSLICK PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO MAGNETO INOPERATIVE E AYQAO OTHER O OTHER NRNOT REPORTED 1 GL13969WA1200 348070112 311312 DEAD MAGNETO ON RUN UP. FOUND MAGNETO ROTATED IN ITS CLAMPS, TIMING WAY OFF. REMOVED MAG AND FOUND IMPULSE COUPLING MISSING CORNER OF PAWL PLATE. 1L72 3O3 O A7SO E9CE 20040217000912004021700091SW 2004 2 17 EHA2004F00000 120030917A6321412040123101 QUILL ASSY BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA ROTOR BRAKE WORN E EHAAO OTHER O OTHER NRNOT REPORTED 1 AL03827MS2485 874 ABW40418 31205 27 MINUTES INTO THE FLIGHT, STRAIGHT AND LEVEL, TQ 85 PERCENT, ALT 5700 FT, THE TRANSMISSION CHIP LIGHT ILLUMINATED. MIDDLE CAT EYE WAS WHITE. TURNED AROUND, REDUCED POWER TO 65 PERCENT AND RETURNED WITHOUT FURTHER NOTICE. 1G71 4U4 U H4SW E22EA 20040212000652004021200065NM 2004 2 12 FE5F200300004 120031117A5730 SKIN BOEING757 75729J NM LT WING LE CRACKED W FE5FK NONE O OTHER ININSP/MAINT 1 WP03 27204 DURING SC12 CHECK, A 4.6250 INCHES LONG SPAN WISE CRACK IS REVEALED BETWEEN OSS 831.5 AND OSS 836 ON LT WING LEADING EDGE LOWER SURFACE SKIN. ACTION: REQUEST MFG ASSISTANCE AND IAW MFG'S RESPONSE, REPAIR THE CRACK. 2L72 4F RTA2NM 20040212001212004021200121NE 2004 2 12 KBM2003F00104 220031113A742109550175400 IGNITER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE RT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 RIGHT SIDE IGNITER INOPERATIVE. REPLACED WITH NEW IGNITER. 1G71 3U3 UNCH9EU E19EU 20040212001462004021200146NM 2004 2 12 2003F00653 120031218A573044305 SKIN LKHEEDP2V P2V7 5260112NM WRIGHTR3350 R3350* 67040EA CENTER WING CRACKED F K NONE O OTHER ININSP/MAINT 1 NM04140HP9960 140443 CRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUTOUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE IB CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF THE SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NACELLE WALLS AT WING STATIONS RT 128.5, 171.5 AND LT 128.5,171.5. 2M72 4R4 RRTA1RM E272 20040212001512004021200151EU 2004 2 12 00122 120031219A2120 ODOR AMD FALC20FALCON 2720302EU COCKPIT DETECTED E HAEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05221TW 221 PILOT REPORTED SHORTLY AFTER TAKEOFF THE CABIN HAD AN ODOR OF SMOKE OR MELTING PLASTIC. CREW PERFORMED EMERGENCY CHECK LIST AND RETURNED TO DEPARTURE AIRPORT WITH NO FURTHER SMOKE OR ODOR IN COCKPIT. UPDATE THIS REPORT AFTER MAINTENANCE. 2L72 4F A7EU 20040212001532004021200153NM 2004 2 12 F3LA200300180 120031219A27506546481113 SPINDLE BOEING737 7373S1 138447SNM TE FLAP WORN A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1432 24856 INSPECTION REPORTED EXCESSIVE PLAY AND WEAR IN RT OB NR 8 FLAP CARRIAGE SPINDLE. REPLACED SPINDLE, SPINDLE BEARING AND BUSHINGS AND FLAP SADDLE. 2L72 4F RTA16WE 20040217001812004021700181NE 2004 2 17 NACA20030129 220031228A7421 SPARK PLUG PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 16 CYLINDER FOULED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL0343872203 203 537201 533294 P32204 DISCREPANCY: NR 3 ENGINE SHUT DOWN DUE TO NR 16 CYLINDER DOUBLE SHORTED SECONDARY. CA: REPLACED NR 3 ENGINE, NR 16 CYLINDER FRONT AND REAR SPARK PLUGS. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040218000312004021800031NM 2004 2 18 UPS04441729 120031231A5347 CARGO TRACK BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, MAIN DECK - BS 240-250, RBL 56 TIE DOWN TRACK CROWN LIP FOUND CRACK. CARGO TRACK REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20040212001772004021200177 2004 2 12 AWXA200301588 420031222A2565D31517113 SLIDE AIRBUSA319 A319132 3930340NM AFT, L-2 DOOR MISALIGNED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW145771726 924 WHILE CATERING WAS OPENING THE L-2 DOOR THE EMERGENCY ESCAPE SLIDE UNRAVELED ON GALLEY FLOOR AND CATERING TRUCK RAMP, DOOR WAS NOT OPENED ALL THE WAY AND SLIDE NEVER DEPLOYED. MAINTENANCE WAS CALLED OUT AND FOUND THE GIRT BAR NEVER DETACHED FROM THE AIRCRAFT EVEN THOUGH THE DOOR SLIDE HANDLE WAS IN THE DISARM POSITION. REMOVED AND REPLACED L-2 DOOR EMERGENCY ESCAPE SLIDE IAW T/C R1C25305, OPERATIONAL CHECK OF DOOR WAS GOOD. 2L72 4F RTA28NM 20031210001862003121000186NM 2003 12 10 EIA2003142 120031020A5315 FLOORBEAM BOEING747 747212B 1384886NM PWA JT9 JT9D* NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 UPPER DECK FLOORBEAM WEB AT BS 440 RBL CRACKED, RBL 66 CORROSION, RBL 40 CRACKED, RBL 55 CRACKED. UPPER DECK FLOORBEAM WEB BS 440, RBL 8 TO RBL 72 REPLACED IAW ECRA 482-53-191-2 2L74 4F4 F A20WE E20EA 20031210001872003121000187NM 2003 12 10 03FDEA01805 120031009A5753 FLAP TRACK DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE T/E FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 SNRM N0776 - LT WING IB FLAP LEADING EDGE OB FLAP VANE TRACK CAVITY FOUND CHAFING MARKS ON FITTING AND SKIN. ** S/D ** COMING 2L73 4F4 FRTA22WE E13NE 20031210001912003121000191NM 2003 12 10 03FDEA01753 120031009A5744 HINGE FITTING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 SNRM N0825 - RT WING OB FLAP IB HINGE FITTING (WING SIDE)- LOWER OB ATTACHMENT TO REAR SPAR, HOLE AND LUG SURFACE FOUND CORRODED. ** S/D ** COMING 2L73 4F4 FRTA22WE E13NE 20031210001952003121000195NM 2003 12 10 03FDEA01867 120031104A2611774001 SMOKE DETECTOR BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE CARGO BAY ACTIVATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25215FE5071 5071 22936 AT 2000 FEET AGL ON TAKEOFF AT BIL ZONE 5 MAIN CARGO SMOKE LIGHT CAME ON WITH BELL. S/O PANEL RESET PUSHED, LIGHT AND BELL CAME ON AGAIN. RESET AGAIN, LIGHT AND BELL CAME ON A THIRD TIME AND THEN WERE RESET AND STAYED OUT. 2L73 4F4 FRTA3WE E2EA 20031210002002003121000200NM 2003 12 10 03FDEA01878 120031105A5330 SKIN BOEING727 727200 138407ENM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 N00148 OUTER EXTERIOR SKIN HAS BULGE AT STA 1050 STR 28L ** SD ** COMING 2L73 4F RTA3WE 20031210002042003121000204NM 2003 12 10 03FDEA02007 120031201A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 FORWARD CARGO LT TUNNEL BETWEEN STA 840 TO STA 859, NR 33 LONGERON SPLICE FOUND CRACKED. REMOVED CRACKED LONGERON SPLICE AS PER SRM 51-31-01, VOL.II AND FABRICATED NEW SPLICE AS PER DRAWING ADA8423. INSTALLED NEW SPLICE AT FWD CARGO LT TUNNEL BETWEEN STA 840 TO 859, NR 34 LONGERON AS PER NDA6712. 2L73 4F RTA22WE 20031210002062003121000206WP 2003 12 10 UPS03841573 120031124A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:N/A .2500 INCH CRACK IN PIT 31 DOOR FRAME AT STA NR 2A. C/W EO DC8-5330-19579 INSTALLED TEMP REPAIR, PERMANENT REPAIR TO BE IN STALLED AT NEXT C CHECK. 2L74 4F RT4A25 20031210002192003121000219NM 2003 12 10 UPS03641541 120031108A2697 WIRE BOEING767 767300 1385204NM GE CF6 CF680 30025NE RT ENGINE FAULTY A IPXAK NONE N FALSE WARNING LDLANDING 1 SO01324UP 27750 INSPECTION TYPE: N/A FIRE PROTECTION SYSTEM FAIL LIGHT ILLUMINATED. EICAS MSG: FIRE/OVHT SYS DISPLAYED. EICAS STATUS MSG: R ENG FIRE LP1 DISPLAYED. INDICATION APPEARED ON SHORT FINAL TO LANDING. TESTED SYSTEM, INDICATION EXTINGUISHED. REPLACED ALL WIRING FOR RT ENG OVERHEAT DETECTION AND FIRE DETECTION FROM FIREWALL TO DETECTOR IAW WDM 26-11-02 AND 26-11-21 AND EO M2000-7 889-5. 2L72 4F4 FRTA1NM E13NE 20031209001392003120900139NM 2003 12 9 QXEA200301342 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM 99126H6840 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 RIGHT OUTBOARD TRACK NR 12 SEAT ATTACH AREA CORROSION UNDER OUTBOARD LUG. REPAIRED IAW RD 8-53-3644. 2H72 4T RTA13NM 20031209001422003120900142EA 2003 12 9 QXEA200301318 120031007A5754 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 RIGHT WING INBOARD FLAP LEADING EDGE MOVEABLE VANE INBOARD LEADING EDGE CHAFED. REPAIRED IAW EO 601R-57-44255 AND HORIZON AIR EA R-57-49. 2L72 4F RTA21EA 20031209001642003120900164NM 2003 12 9 03FDEA01779 120031009A5753ARC0503 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT WING O/B FLAP O/B HINGE BRACKET (WING SIDE) CORRODED ON SURFACE IN LOWER O/B ATTACHMENT HOLE CAVITY. COMPLIED WITH FEDEX EA 1-5740-71745, WINGS - LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031209002102003120900210 2003 12 9 SWIA200312560 420031027A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA YAW DAMPER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07437SW5579 5579 7564 TAXI OUT, YAW DAMPER NR 1 WOULD NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW WMM 22-22-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031210000262003121000026NM 2003 12 10 AWXA200301482 120031120A2721810A000005 SERVO AIRBUSA319 A319132 3930340NM RUDDER WORN A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28813AW13145 1350 EN ROUTE AIRFRAME VIBRATION WAS FELT IN ALL PHASES OF FLIGHT, MOST NOTICEABLE IN CLIMB & CRUISE AT SPEED OF 310 KTS. MX VISUALLY INSPECTED WING TO BODY FAIRING SEALS, MLG DOORS, AIR COND & PAX ENTRY DOORS, NO DEFECTS NOTED. PERFORMED ELEVATOR FREE PLAY CHECK, NO DEFECTS NOTED. PERFORMED RUDDER FREE PLAY CHECK & FOUND YELLOW & BLUE RUDDER SERVO CONTROLS OUT OF LIMITS. R & R YELLOW & BLUE RUDDER SERVO CONTROLS. OPS CHECK GOOD. TEST OF RUDDER SERVO CONTROL CONFIRMED FAILURE OF UNIT FOR FAILING DAMPING TEST. UNIT WAS FOUND LEAKING AT ROD END, SWIVEL BEARING, & BALL BEARING ON LEVER ARM ASSEMBLY, SWIVEL BEARING AT END EYE & CYLINDER HOUSING WERE ALL WORN, & BOTH CONTROL & BYPASS VALVES WORN BEYOND LIMITS. 2L72 4F RTA28NM 20031210000482003121000048WP 2003 12 10 AALA20031310 120031123A3350AAP3274A CHARGER DOUG DC9 DC983 3022083WP TAILCONE INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21968TW 53618 DFW AFT TAIL CONE COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT TAIL CONE COMPARTMENT BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031210000622003121000062NM 2003 12 10 QXEA200301513 120031201A5210 SLIDE DHAV DHC8 DHC8202 2809007NM PAX DOOR LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09363PH 520 PDX- ON FLIGHT 2120 MAIN CABIN DOOR IS HARD TO LATCH AND UNLATCH FROM INSIDE. CLEANED AND LUBED DOOR SLIDES AND CAM POINTS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040213000182004021300018NM 2004 2 13 2003UALA00978 120031221A3350 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29659UA 27114 EMERGENCY LIGHT INOP AT DR1 FWD CROSSAISLE. REPLACED BROKEN FEEDER CABLE. OPS CKD NORMAL. 2L72 4F4 FRTA1NM E24NE 20040217000372004021700037EU 2004 2 17 2004F00063 120030926A5313D5348004420401 STRINGER AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND AFT CABIN FUSELAGE STRINGER FLOOR LEVER UPPER SURFACE CORRODED BETWEEN FRAMES 68-69 AT STATION 3280. REMOVED AND REPLACED STRINGER 21L BETWEEN FRAMES 68 AND 69 STATION 3280. (M) 2L72 4F RTA28NM 20040217000522004021700052NM 2004 2 17 2004F00074 120031230A3260 CONNECTOR BOEING727 727222 1384073NM ACCESSORY UNIT DAMAGED A RYNAO OTHER J WARNING INDICATION LDLANDING 1 SW077645U 20039 ON LANDING INTO MSY, THE FORWARD PILOT PANEL INDICATOR LIGHT FOR THE LT MAIN LANDING GEAR SHOWED A RED UNSAFE LIGHT ILLUMINATED WITHOUT THE GREEN DOWN AND LOCKED INDICATION. THE FLIGHT ENGINEER'S PANEL SHOWED ALL THREE GEAR DOWN AND LOCKED. FLIGHT CREW DECLARED AN EMERGENCY AND ACCOMPLISHED. APPROPRIATE CHECKLISTS. AIRCRAFT LANDED AT MSY WITHOUT FURTHER INCIDENT. REMOVED AND CLEANED CONNECTOR ON LANDING GEAR ACCESSORY UNIT. REINSTALLED UNIT. OPERATIONAL CHECK NORMAL. (M) 2L73 4F A3WE 20040217000102004021700010EA 2004 2 17 ASOA03679 120031227A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 38 IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20040301000122004030100012EU 2004 3 1 KBM2004F00009 120031213A2435150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813EU ENGINE INOPERATIVE E KBMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP19751H 316 3403 GEN LIGHT WENT ON IN FLIGHT. BATTERY VOLTAGE WENT TO 13 VOLT DC. REMOVED AND REPLACED WITH OVERHAULED PART.(K) 1G71 3U H9EU 20040301000172004030100017 2004 3 1 KBM2004F00014 420031223A34241234T1007TZ INDICATOR SNIAS 350 AS350BA 8680817EU TURN & SLIP MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 TURN AND SLIP INDICATOR MAKING NOISE AND EXCESSIVELY HOT, REMOVED AND REPLACED. 1G71 3U NCH9EU 20040301001012004030100101EU 2004 3 1 RYN2004F00003 120031019A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R IN FORWARD CARGO COMPARTMENT. FABRICATED NEW FLOORBOARD SUPPORT. TREATED, PRIMED, TOP COATED AND INSTALLED FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R. 2L72 4F4 FRTA28NM E40NE 20040301001052004030100105EU 2004 3 1 RYN2004F00006 120030915A5220D227908520200 LATCH AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE EMERGENCY DOOR DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK, FOUND GOUGE ON FORWARD LT EMERGENCY EXIT DOOR LOWER AFT FITTING LATCH. REMOVED AND REPLACED FORWARD LT EMERGENCY EXIT DOOR, LOWER AFT LATCH FITTING. 2L72 4F4 FRTA28NM E40NE 20040301001072004030100107EU 2004 3 1 RYN2004F00008 120030915A5210D5348015900500 ATTACH FITTING AIRBUS320 A320233 3930329EU IAE V2500 V2500A1 NE RT NR 2 DOOR CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY AFT GIRT BAR ATTACH FITTING PLATE WITH CORROSION. REMOVED AND REPLACED AFT GIRT BAR ATTACH FITTING PLATE ON AFT CABIN NR 2 RT DOORWAY. 2L72 4F4 FRTA28NM E311NE 20040301001092004030100109EU 2004 3 1 RYN2004F00010 120030907A5320MS20426AD58 THRESHOLD AIRBUS320 A320233 3930329EU IAE V2500 V2500A1 NE R2 DOOR CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK FOUND R2 DOOR THRESHOLD HAS 5 CORRODED RIVETS. REMOVED AND REPLACED CORRODED RIVETS AT R2 DOOR THRESHOLD. 2L72 4F4 FRTA28NM E311NE 20040301001792004030100179WP 2004 3 1 GTIA031049 120031223A2697 CONNECTOR DOUG DC9 DC983 3022083WP FIRE LOOP INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FLL - FLT 900 - FIRE WARNING LT ENGINE B-LOOP CONNECTOR P1-863 ON THE NR 1 ENGINE. OPS CHECK GOOD ON THE NR 1 ENGINE FIRE LOOP TEST. (M) 2L72 4F RTA6WE 20040301001822004030100182NM 2004 3 1 ASAA0340337 120031027A53115717712019 FRAME BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01708AS 28895 SEA - DURING L4 WINDOW REPLACEMENT, FOUND FRAME AT FUSELAGE STATION 219.5, LEFT BUTTOCK LINE 16 CRACKED. REPAIRED FRAME PER EA. (M) 2L72 4F RTA16WE 20040301001832004030100183WP 2004 3 1 GTIA030448 120030609A7160 DUCT DOUG DC9 DC983 3022083WP NR 1 ENG INTAKE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 DTW - NR 1 ENGINE DIFFUSER FAN DUCT SOUND LINER TOP SHEET MISSING 20 SQUARE INCHES 8 O'CLOCK POSITION, INBOARD NR 4 BEARING OIL TUBE FAIRING. SPIRIT AIRLINES EA 7230-0304 HAS BEEN COMPLIED WITH. (M) 2L72 4F RTA6WE 20040227000122004022700012NM 2004 2 27 DHL2003753512 120031229A5754 RIB BOEING727 727223 1384074NM SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 N/R 65147 NR 8 SLAT AT ACTUATOR ATTACH MOUNT IB. RIB IS CRACKED ABOUT 2.5 INCHES LONG SLAT STA. 390. REMOVED NR 8 SLAT IAW M/M 27-81-11. REMOVED NR 8 SLAT ACTUATOR IAW MM 27-81-22. REMOVED ACCESS PANELS AND RIBS AT NR 8 SLAT IAW SRM 51-30-2. REMOVED RIBS AND BRACKET SUPPORT IAW SRM 51-30-2. DRILLED NEW HOLES AT RIBS AND BRACKET SUPPORT IAW SRM 51-30-5. INSTALLED RIBS AND BRACKET SUPPORT P/N 65-17327-4, P/N 65-17327-3, AND 65-1727-7 P.O. NR 3421114, 342115, 3345442 IAW SRM 51-30-2. REINSTALLED INT. PANELS AT NR 8 SLAT IAW SRM 51-30-2. REINSTALLED NR 8 SLAT ACTUATOR AND SLAT IAW MM. 27-81-11 AND 27-81-22. OPS AND LEAK CHECKED GOOD IAW MM 27-81-0. 2L73 4F A3WE 20040303000032004030300003NM 2004 3 3 GTIA030624 120030811A256011900311 PBE DOUG MD80 MD83 3023681NM FIRE A GTIAO OTHER A FLAME/FIRE NRNOT REPORTED 1 GL23 PBE REMOVED FROM FLIGHT ATTENDANT AND FIRE EXTINGUISHED. DURING FLIGHT ATTENDANT CLASSROOM TRAINING, A FLIGHT ATTENDANT PUT ON A PBE (PORTABLE BREATHING EQUIPMENT) FOR A DEMONSTRATION. DURING THE DEMONSTRATION, THE FLIGHT ATTENDANT ACTIVATED THE O2 GENERATOR DISCHARGE PIN. SECONDS LATER, THE PBE CAUGHT ON FIRE. THE PBE HAS BEEN FORWARDED TO THE MANUFACTURER FOR ANALYSIS. CURRENTLY STILL UNDER INVESTIGATION. 2L72 4F RT 20040210000432004021000043NE 2004 2 10 MDR03033 120031118A6730156564302000 HOUSING SKRSKYS64 S64E 8142604NE T/R SERVO CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09CFCRN A1961 64061 TAIL GB AND SERVO ASSY WAS REMOVED FROM AC FOR 2ND STAGE HYD FLUID LEADING INTO THE T/R GB. T/R SERVO ASSY WAS REMOVED FROM THE T/R GB ASSY. THE HYD SHOP, REVEALED HEAVY SCORING ON EXPOSED AREA OF PISTON. ONCE PRESSURIZED TO SIMULATE OPERATION CONDITION, AT APPROX 600 PSI, A LEAK WAS DETECTED IN THE HOUSING AT THE 2ND STAGE PRESSURE/RETURN PORT ON OD OF HOUSING. LOCAL FPI CONFIRMED THAT A .7500 INCH CRACK AT THE CURVATURE AT THE END OF THE PRESSURE/RETURN PORT CASTING. THROUGH CRACK BEGINS AT THE 2ND STAGE PRESSURE/RETURN PORT IN THE HOUSING ID AND TRAVELS APPROX .7500 INCH TOWARDS THE THREADED END OF THE HOUSING. AFTER DISASSEMBLY THE 2ND STAGE SERVO VALVE AND SLEEVE ASSY, WERE FOUND SEVERELY SCORED. 2G72 4U H4EA 20040210000472004021000047NM 2004 2 10 QXEA200301489 120031121A5410 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- LT SIDE OF LT NACELLE OUTBOARD GRAVEL GUARD MOUNT ON TOP PANEL OF WHEEL WELL IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-40-11. 2H72 4T RTA13NM 20040210000692004021000069WP 2004 2 10 ASAA0380772 120031119A532199579182 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FLOOR PANEL DELAMINATED AT FS 1193. REPAIRED IAW SRM. (M) 2L72 4F RTA6WE 20040210000712004021000071WP 2004 2 10 ASAA0380774 120031119A5313593666715 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CORROSION ON BOTTOM OF LONGERON 29L UNDER FRAME AT STATINO 1231. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20040210000732004021000073WP 2004 2 10 ASAA0380783 120031119A5310993607317 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT STATION 1212. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20040210000772004021000077WP 2004 2 10 ASAA0380776 120031119A52605936675502 ARM DOUG DC9 DC983 3022083WP AIRSTAIR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND RIGHT ARM ON AFT AIRSTAIR IS GOUGED. REPAIRED IAW EA. (M) 2L72 4F RTA6WE 20040210000802004021000080NE 2004 2 10 HALA0301199 220031223A72708910418 BYPASS VALVE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RT ENGINE MALFUNCTIONED A HALAO OTHER J WARNING INDICATION CRCRUISE 1 WP13487HA 55132 FLT 119 - HNL - 'ENG RT SYSTEM FAIL' ILLUMINATE EN ROUTE, STAYED ON ENTIRE TIME. INTERROGATED EEC-2. FOUND FAULT 731304, BYPASS AND VENT VALVE MECHANICAL FAULT. TROUBLESHOT PER FIM 73-13, TASK 804. REPLACED BYPASS AND VENT VALVE PER AMM 73-13-04. LEAK AND OPS CHECK GOOD. EEC-2 BITE CHECK, NO FAULTS FOUND. OK FOR SERVICE. (M) 2L72 4F4 FTRA6WE E00061EN 20040210000812004021000081NM 2004 2 10 USAABB03227 120031223A335086210066 SIGN BOEING757 757225 1384959NM R4 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU 22199 PHL - FOUND R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20040210000842004021000084NM 2004 2 10 HALA0301183 120031218A27202704693 CONTROL MODULE BOEING717 717200 1383700NM RUDDER MALFUNCTIONED A HALAO OTHER O OTHER CRCRUISE 1 WP13485HA 55130 FLT 345 - OGG - AILERON TRIM WILL NOT TRIM LEFT WING DOWN. RIGHT WING TRIMS DOWN NORMALLY. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL MODULE. OPS CHECK GOOD. ALL WORK DONE IAW FIM 27-10 TASK801, AMM 27-10-07-4, AMM 27-11-01-5. OK FOR SERVICE. (M) 2L72 4F TRA6WE 20040210000852004021000085EU 2004 2 10 USAA030300 120031123A5347 SEAT TRACK AIRBUS330 A330323 3940030EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH, FS 55 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NWE PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210000882004021000088EU 2004 2 10 USAA030306 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .150 INCH AREA, FS 59 LBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210000942004021000094EU 2004 2 10 USAA030292 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH, FRAME 60 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M0 2L72 4F RTA46NM 20040210001122004021000112EU 2004 2 10 USAA030301 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .150 INCH AREA, FRAME 66 PLUS 10 INCHES LBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTIN PER SRM 51-74-00. (M) 2L72 4F RTA46NM 20040209000022004020900002NM 2004 2 9 DHL2003753510 120031230A5740 MOUNT BOEING727 727223 1384074NM NR 5 SLAT ACT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, NR 5 SLAT AT ACTUATOR ATTACH MOUNT INBOARD SIDE PREVIOUS REPAIR AND RIB ARE CRACKED SLAT STA 60. REMOVED NR 5 RT WING SLAT IAW B-727 M/M 27-81-11. REMOVED INNER SHIM PANELS AND RIBS IAW B-727 SRM 51-30-2. DRILLED NEW PARTS (RIBS) P/N 65-93155-1088 (65-17276-12) PO 342198 AND P/N 65-17276-10 PO 342192 IAW B-727 SRM 51-30-5. INSTALLED RIBS AT NR 5 SLAT AND APPLY CIC IAW B-727 SRM 51-30-2 AND M/M 51-20-16. INSTALLED INNER SKIN PANELS IAW B-727 SRM 51-30-2. INSTALLED RT WING NR 5 SLAT IAW B-727 M/M 27-81-11. OP'S CHECK GOOD IAW B-727 M/M 27-81-11. 2L73 4F A3WE 20040209000922004020900092CE 2004 2 9 AMWA113 120030102A54111141200333 RIB BEECH 1900 1900D 1154162CE LT NACELLE CRACKED A AMWAO OTHER O OTHER ININSP/MAINT 1 CE07174YV UE174 DURING INSPECTION THE LEFT I/B WING OF ENG NACELLE RIB THAT SUPPORTS LANDING GEAR POWER PACK WAS FOUND TO BE CRACKED ON TOP SIDE IN RADIOUS OF RIB APPROX 3 INCHES LONG. REPAIRED BY REPLACING RIB ASSY. 2L72 4T RTA24CE 20040210000112004021000011WP 2004 2 10 UPS03841582 120031114A5310 BULKHEAD DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1 AFT PRESSURE BULKHEAD IS CRACKED AT STATION 1766 AT RBL 36, 65 INCHES ABOVE FLOOR LEVEL. REMOVED EXISTING REPAIR, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND REPLACEMENT DOUBLER I.A.W. DWG. SRO8530007 2L74 4F RT4A25 20040210000182004021000018WP 2004 2 10 UPS03841592 120031116A5310 SHEAR TIE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, SHEAR TIE IS CRACKED AT STATION 1380 LONG. 29L TO 30L. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED SHEAR TIE REPAIR IAW SRM. 53-2-0 FIG. 2A. 2L74 4F RT4A25 20040210000462004021000046EA 2004 2 10 COMA0360524 120031202A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 FUSELAGE SKIN FS 602.5 BETWEEN STRINGERS 21L TO 22L HAS GOUGE APPROX .004 INCH DEEP. REPAIRED BY REMOVING DAMAGE, PERFORMING EDDY CURRENT INSPECTION, FABRICATING EXTERNAL REPAIR DOUBLER FROM 2024-T3 .063 INCH AND INSTALLING IAW CRJ 200 SRM 53-00-31 REPAIR NR 1. 2L72 4F RTA21EA 20040210000612004021000061NM 2004 2 10 TSAA0321201 120031217A5210 SEAL BOEING737 73773A 1384606NM PAX DOOR FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13739AL 28500 FLT 482 - SNA-RNO - ON TAKEOF, THE FORWARD ENTRY DOOR FAILED TO SEAL. DIVERTED TO BUR. ON ARRIVAL OF AIRCRAFT, NOTICED L1 DOOR NOT CLOSED PROPERLY AND SEALED, NOTICED GAP BETWEEN FLOOR. OPEN/CLOSED DOOR, NO DEFECTS NOTED. DOOR IMPROPERLY CLOSED. FLIGHT VERIFICATION OK. (M) 2L72 4F RTA16WE 20040210001262004021000126 2004 2 10 COMA0360527 420031203A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01989CA 7215 FLGIHT 5675 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20040211000192004021100019WP 2004 2 11 GTIA031042 120031117A5312 PRESSURE PANEL DOUG DC9 DC981 3022081WP RT MLG WW CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND RIGHT MLG W/W CEILING PRESSURE WEB HAS CORROSION RUNNING UNDER STIFFENERS IN NUMEROUS AREAS. FABRICATED PRESSURE FLOOR DOUBLER AND INTERNAL FINGER DOUBLER. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20040211000212004021100021NM 2004 2 11 USAA030323 120031219A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US47931 23237 CLT - FOUND SKIN CRACKED 3 INCHES, BS 727 D PLUS 13 INCHES S-24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20040211000382004021100038EU 2004 2 11 ASOA03693 120031230A3397M2275941249 WIRE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY AND REPINNED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040211000432004021100043EU 2004 2 11 USAA030315 120031217A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW17615 0315 FOUND SEAT TRACK CORRODED 5 INCHES BY .5 INCH BY .030 INCH DEEP AREA, FRAME 36, LBL 75 UNDER COAT CLOSET AFT OF L AT DOOR. TWO REPAIR SPLICES INSTALLED AND NEW TRACK INSTALLED PER EA 95034 AND SRM 53-00-15 FIG 202. (M) 2L72 4F RTA46NM 20040211000902004021100090NM 2004 2 11 CALA0400071 120030131A5330 SKIN BOEING737 737724 13844BYNM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713718 28937 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 403, S17L. REPAIRED IAW ECRA 5331-01136. 2L72 4F RTA16WE 20040210000502004021000050NM 2004 2 10 QXEA200301495 120031120A5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- CORROSION ON TOP OF ANGLED FLOOR SUPPORT OUTBOARD OF NR 4 SEAT TRACK FIVE INCHES FORWARD OF X222. REPAIRED IAW DHC-8 SRM 51-20-11. 2H72 4T RTA13NM 20040210000972004021000097EU 2004 2 10 USAA030295 120031122A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH, FRAME 57.4 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210001062004021000106EU 2004 2 10 USAA030311 120031124A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .125 INCH AREA, FRAME 57.1 LBL 17.75. DAMAGED TRACK REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040212000112004021200011WP 2004 2 12 UPS03841629 120031114A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 1760 LONG. 16L IS CRACKED. CUTOUT CRACKED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION I.A.W. SRM. 53-2-2 FIG.10. 2L74 4F RT4A25 20040212000292004021200029NM 2004 2 12 DHL2003783014 120031205A5753 SKIN BOEING727 727227 1384078NM TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 LT WING INBOARD AFT FLAP HAS POSSIBLE CRACK AT L/E BEHIND NR 4 TEAR DROP FAIRING. STOP DRILLED CRACK 2.5 IN. AND INSTALLED REPAIR DOUBLER IAW B-727 SRM 57-50-4. DOUBLER MATERIAL 2024-T3 .050 P/O 40000-498. FASTENERS CR 3212-5-2. MAJOR REPAIR. 2L73 4F A3WE 20040210001272004021000127EU 2004 2 10 XNOA1168 120031205A3210 DAMPER AIRBUS300 A300B4203 3930306EU MLG PITCH MALFUNCTIONED A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23224KW 073 AFTER TAKEOFF GEAR WOULD NOT RETRACT IN SYSTEM 1 OR 2. REMOVED AND REPLACED RT MLG PITCH DAMPER IAW A300 AMM 32-11-15. OPS CK NORMAL IAW A300 AMM 32-30-00. (CLOSED) 2L72 4F RTA35EU 20040211000222004021100022WP 2004 2 11 AMTA200301515 120031223A3350 LIGHT LKHEED1011 10113851 5265010WP ROW 39H DAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11188AT 193C1078 FOUND EGRESS TRACK DAMAGED AFT OF 39H. REPAIRED DAMAGED EGRESS TRACK AS REQUIRED. (M) 2L73 4F A23WE 20040211000452004021100045NM 2004 2 11 AMTA200301427 120031126A77006672M452 MONITOR BOEING757 75723N 1384973NM COCKPIT FAILED A AMTAK NONE J WARNING INDICATION CLCLIMB 1 GL11523AT 30232 EICAS MSG ENGINE VIB DISPLAYED, INTERMITTENLY CAME ON IN CLIMB, WENT OUT IN CRUISE FAILED TO .1 CAME BACK 1.0-1.1. T/S PER FIM 77-31-00. REMOVED AND REPLACED AVM SYSTEM IAW M/M 77-31-00. (M) 2L72 4F RTA2NM 20040212000232004021200023CE 2004 2 12 55727 120031031A3260 SQUAT SWITCH BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07167YV UE167 AFTER TAKE OFF GEAR UP. SELECTED GEAR WOULD NOT RETRACT. C/B RESEATED AND ANOTHER ATTEMP WAS MADE WITH THE SAME RESULT. ACFT RETURNED TO FIELD WITH 3 GREENS LANDED WITH NO FURTHER INCIDENTS.(REMOVED AND REPLACED RIGHT SQUAT SWITCH) 2L72 4T RTA24CE 20040212000442004021200044CE 2004 2 12 DJFA20030003 120031208A243523080005 BEARING RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP STARTER GEN FAILED E DJFAE ENGINE SHUTDOWN E VIBRATION/BUFFET DEDESCENT 1 EA23843CW611 611 258543 P107137 AIRCRAFT DESCENDING THROUGH 11,000 FT, VIBRATION WAS NOTED. ENGINE NR 2 WAS SHUT DOWN AND VIBRATION WENT AWAY. AIRCRAFT LANDED AND IT WAS FOUND THAT THE STARTER GENERATOR BEARINGS HAD FAILED. 2L72 4F4 FRTA3EU E6WE 20040212000672004021200067NE 2004 2 12 MDR03035 120031120A65206535807053043 HOUSING SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE T/R GEARBOX CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09164AC5681 1593 64034D TGB CENTER HOUSING WAS FOUND CRACKED WHILE INSTALLED ON THE AIRCRAFT. IT WAS REMOVED PREMATURELY ON OCTOBER 20, 2000. THE SHOP DETECTED THE CRACK VISUALLY. THE CRACK BEGAN AT THE SECOND ROSAN STUD CLOCKWISE FROM THE ROSAN SEAT PAD LOCATED 34 DEGREES FROM CENTERLINE OF INPUT BORE. THE CRACK EXTENDED RADIALLY THROUGH .3750-16 NC TAPPED BORE AND ABOUT 3.2500 OF AN INCH THROUGH THE WEB. PROBABLE CAUSE IS UNKNOWN AT THIS TIME. 2G72 4U4 U H4EA E15EA 20040212000992004021200099NE 2004 2 12 121103 220031210A8530116733 CYLINDER DOUG DC3 DC3C 3021457WP PWA R1830 R1830* 52020NE RT ENGINE SEPARATED E VLLAE ENGINE SHUTDOWN D INFLIGHT SEPARATION CRCRUISE 1 GL0536AP 257 13439 BP432589 AT CRUISE POWER ENROUTE DET-HEF RT ENGINE DEVELOPED A VIBRATION WITH A LOSS OF MANIFOLD PRESSURE. OIL LEAK FROM THE TOP OF THE ENGINE WAS VISUALLY NOTED. AIRCRAFT DIVERTED TO LPR. FOUND NR 13 CYLINDER HEAD SEPARATED AND LINK ROD BROKEN. 2L72 4R4 R A669 5E4 20040212001012004021200101NM 2004 2 12 CALA0300707 120031210A5730 SKIN BOEING737 737824 13844BZNM RT WING LE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717229 28793 INSPECTION FOUND A DENT IN RT WING L/E SKIN BETWEEN NR 2 ENGINE AND WING ROOT. A FLUSH REPAIR WAS INSTALLED USING REPAIR PLATE AND FILLER IAW SRM 57-41-01-201. 2L72 4F RTA16WE 20040212001472004021200147CE 2004 2 12 DJFA200300009 120031217A3260 UPLOCK SWITCH BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112NE MLG ICED E DJFACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA23792TA RK264 AFTER TAKEOFF, PILOTS WERE NOT ABLE TO GET THE GEAR UP AND LOCK. AFTER SEVERAL ATTEMPTS THEY RETURNED TO THE DEPARTURE AIRPORT. MAINTENANCE FOUND ICE BUILT UP AROUND THE UPLOCK SWITCH. 2H72 4F4 FRTA16SW E25EA 20040212001842004021200184CE 2004 2 12 DEBA4324V1 120031212A2810363800951 FUEL CAP BEECH 58 58 1152740CE LT CELL OUT OF ADJUST E DEBAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE034324V503 TH2014 FUEL VENTED FROM LT IB FUEL CAP ON TAKEOFF. AIRCRAFT RETURNED TO BASE AND UPON INSPECTION FOUND THE CAP WAS LOOSE WHEN LATCHED. THE COTTER PIN WAS MISSING AND IT AND THE ADJUSTMENT NUT HAD LOOSENED. ADJUSTED CAP AND REPLACED COTTER PIN. 1L72 3O 3A16 20040212001852004021200185NE 2004 2 12 S03272099 220031219A7200 ENGINE BOEING747 747200 1384847NM PWA JT9 JT9D7R4G2 52054NE NR 1 DAMAGED W SAJFD RETURN TO BLOCK E VIBRATION/BUFFET CLCLIMB 1 WP03 24308 P725323 ENGINE 1 ALL PARAMETERS VIBRATED WITH T/L FORWARDED AND RETARDED. VIB RAISED UP TO 3.0 UNIT AT IDLE POWER. ATB TO SIN AND GROUND INSPECTION FOUND MASSIVE METAL CHIPS IN THE TAIL PIPE AND EVIDENCE OF LPT DAMAGE AND ENGINE CHANGED. WAITING FOR SHOP INVESTIGATION REPORT. 2L74 4F4 FRTA20WE E3NE 20040212001982004021200198EA 2004 2 12 HNAA0300083 120031219A2731 ACTUATOR DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE ELEVATOR TRIM LACK OF LUBE A HNAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA07327EN 261 UNABLE TO MOVE ELEVATOR TRIM TO NOSE DOWN POSITION IN FLIGHT , OPS NORMAL ON THE GROUND. LUBED ELEVATOR TRIM ACTUATOR AS REQ, OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20040212002002004021200200NM 2004 2 12 CALA0300722 120031224A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND KEEL BEAM LT LOWER CHORD CORRODED FROM STA 699-727. REPAIRED IAW ECRA 5310-03740. 2L72 4F RTA16WE 20040212002022004021200202NM 2004 2 12 HNAA0300085 120031225A26128006221 WARNING SYSTEM DHAV DHC8 DHC8102 2809003NM FIRE WARNING INTERMITTENT A HNAAO OTHER N FALSE WARNING APAPPROACH 1 EA07914HA 53 SMOKE WARNING AND FIRE DETECT WARNING LIGHT ILLUMINATED ON SHORT FINAL. REMOVED AND REPLACED MASTER WARNING CONTROL BOX AND MASTER WARNING PANEL. 2H72 4T RTA13NM 20040213000212004021300021CE 2004 2 13 GLBA20030520 120031229A3060 BRUSH BLOCK BEECH 1900 1900D 1154162CE PROP DE ICE INOPERATIVE A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03201GL26 UE201 RT PROP DEICE AND PILOT AND COPILOT W/S NOT HEATING, REMOVED AND REPLACED BRUSH BLOCK PN 4E3196-1GLA AND PROP AMP IND PN 114-380049-5. 2L72 4T RTA24CE 20040213000252004021300025EU 2004 2 13 CX7A194J0358 120031229A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03307CE 340B204 ON TAKEOFF ROLL GOT LT TAILPIPE HOT. ABORTED TAKEOFF, MOISTURE PRESENT. 2L72 4T RTA52EU 20031210000982003121000098EU 2003 12 10 MALA030518 120031121A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION PERFORMED BY TIMCO, LAKE CITY, FL. CABIN AFT FRAME STA 649 WL 79 GOUGED. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA, EO S53152. A/C RELEASE DATE 12/2/2003. 2L72 4T RTA52EU 20031210001312003121000131NM 2003 12 10 AALA20031334 120031127A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21662AA 25296 MIA LEFT AFT DOOR EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK FOR LEFT AFT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20031210001392003121000139NM 2003 12 10 AALA20031347 120031130A3397 WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21327AA 22327 SFO) RT SIDE MID GALLEY EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE UNDER CARPET FOR RIGHT SIDE MID GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA1NM 20031210001822003121000182NM 2003 12 10 CALA0300634 120031111A3350 BATTERY PACK BOEING757 757324 NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2775851 32810 THE EMERGENCY LIGHTS AT SEAT ROWS 1, 2, 3 AND AT L-1 DOOR EXTERIOR WERE FOUND INOPERATIVE. THE M731 BATTERY PACK AND CHARGER ASSEMBLY WAS REPLACED IN REFERENCE TO WDM 33-51-12. OPERATION OF THE EMERGENCY LIGHTS WAS RESTORED. 2L72 4F RTA2NM 20031210002202003121000220WP 2003 12 10 UPS03841550 120031104A53204653726501 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 210 LONGERON 23R SPLICE IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4653726,AND SRM 51-1-20D 2L74 4F RT4A25 20031211000082003121100008 2003 12 11 0302003302 420031106A25657A1539117 SLIDE AIRBUS330 A330323 3930335EU L2 DOOR FAILED A NWAAK NONE L NO TEST UKUNKNOWN 1 GL01802NW1027 1027 00533 UPON ARRIVAL, THE FLIGHT ATTENDANT PULLED THE WRONG LEVER AT DOOR 2L AND BLEW THE SLIDE, HOWEVER THE SLIDE DID NOT DEPLOY AUTOMATICALLY. THE SLIDE WAS REPLACED BY MAINTENANCE. 2L72 4F RTA46NM 20031211000242003121100024EA 2003 12 11 COMA0360490 120031108A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION ININSP/MAINT 1 SO01710CA 7241 FLIGHT 5144 FLAPS FAIL WARNING MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031211000632003121100063WP 2003 12 11 ABXA030438 120031111A323027748431 LATCH DOUG DC8 DC863F 302198FWP LT MLG WORN A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23826AX 46061 RED GEAR UNSAFE LIGHT AND LEFT GEAR DOOR NOT LATCHED LIGHT CAME ON. BOTH LIGHTS WENT OUT AFTER PERFORMING ALTERNATE UPLATCH CHECK ABNORMAL, THRU FLAP EXTENSION. GEAR CYCLED. CHECKED GEAR DOOR LATCH MECHANISM, CHECKED TARGET, CLEANED AND LUBED SWITCH AND CYCLED GEAR DOOR SEVERAL TIMES. OPS CHECKED GOOD, LIGHT OUT ON GROUND. NO DEFECTS NOTED IAW 32-31-04. 2L74 4F 4A25 20031211000662003121100066WP 2003 12 11 UPS03841559 120031020A53209754022503N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 280 MAIN CARGO FLOORBEAM END FITTING IS CRACKED AT RT SIDE RBL 67 APPROX. REMOVED AND REPLACED FITTING IAW DWG 9754022 AND SRM 51-1-20D. 2L74 4F RT4A25 20031211000742003121100074NM 2003 12 11 AWXA200301409 120031027A552365C2638416A TAB BOEING737 7373G7 1384595NM ELEVATOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK A .375 INCH CRACK WAS FOUND ON THE RT ELEVATOR TRIM TAB AT NR 2 HINGE POINT ELEV STA 94.27. MAINTENANCE PERFORMED BOND REPAIR ON RT ELEVATOR TRIM TAB AT NR 2 HINGE POINT ELEV STA 94.27 IAW B737-300 SRM 51-70-17, REPAIR 10, FIG 8. 2L72 4F RTA16WE 20031211000822003121100082WP 2003 12 11 IXXA0300073O 120031112A7797C65039ATI WIRE HARNESS DOUG DC8 DC871F 302199DWP NR 1 ENGINE BROKEN A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11820BX837681081 46065 DURING CLIMB FROM FJDG NR 1 ENGINE EGT WENT TO ZERO. CREW RETURNED AIRCRAFT TO FJDG AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED EGT PIGTAIL FROM THERMOCOUPLE JUNCTION TO PYLON. OPERATIONAL CHECK OKAY PER ALL APPLICABLE MANUALS. ACCOMPLISHED ENGINE RUN IN ACCORDANCE WITH ATI ENGINE RUN HANDBOOK. ALL PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20031211001102003121100110NM 2003 12 11 AALA20031398 120031207A3350 CHARGER BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21787AL 30010 DFW FLOOR PATH LIGHTING AT FED GALLEY CLOSET AREA INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FLOOR PATH LIGHTING AT FED GALLEY CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031211001112003121100111NM 2003 12 11 AALA20031399 120031208A3350S283T0143 BATTERY PACK BOEING757 7572Q8 1384972NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21709TW 28168 SNA SEVERAL AFT GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR SEVERAL AFT GALLEY AREA EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031211001132003121100113WP 2003 12 11 AALA20031391 120031206A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21554AA 53084 DFW SEAT MOUNTED EMERGENCY LIGHT AT SEAT 30D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001252003121100125NM 2003 12 11 AALA20031405 120031205A2934AAP1874D TRANSMITTER BOEING767 767223 1385123NM HYD SYSTEM INOPERATIVE A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW21327AA 22327 JFK T019/05 EN ROUTE JFK-LAX LOSS OF LEFT SYSTEM HYDRAULIC QUANTITY AND PRESSURE. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT SYSTEM HYDRAULIC QUANTITY TRANSMITTER PER MM 29-33-02-4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031209002592003120900259NM 2003 12 9 AWXA200301360 120031013A5315146N5447 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM BS 1460-1480, RBL 18. MAINTENANCE REMOVED DAMAGED T-ANGLE AND ATTACH BRACKETS FROM BS 1460-1480, RBL 18; FABRICATED A NEW REPLACEMENT ANGLE AND ATTACH BRACKETS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-40-05 PG 5 FIG 3. 2L72 4F RTA2NM 20031210000082003121000008NM 2003 12 10 03FDEA02080 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 04 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 4 CRACKED LOCKBOLT COLLARS REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY. 2L73 4F RTA22WE 20031210000282003121000028NM 2003 12 10 AWXA200301484 120031031A53306573746 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 LCQ - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727, STR 16 RT. MAINTENANCE REMOVED DAMAGED SKIN FROM BS 727 TO BS 777, STR 16 RT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS, 4 EACH DOUBLERS, AND A TRIPLER; INSTALLED REPAIR PARTS IAW IAW AWA ER 15-5331-03267-SS2. 2L72 4F RTA16WE 20031210001672003121000167NM 2003 12 10 AALA20031176 120031021A2913 PUMP BOEING757 757223 1384957NM HYD SYSTEM FAILED A AALAK NONE K FLUID LOSS APAPPROACH 1 SW21643AA 24601 ENROUTE CUN-MIA AND APPROACHING MIA FOR LANDING LOST ENTIRE LEFT HYDRAULIC SYSTEM. LANDED WITHOUT FURTHER INCIDENT. REPLACED ENGINE DRIVEN HYDRAULIC PUMP. PERFORMED LEAK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (SW21200401054) 2L72 4F RTA2NM 20031210001752003121000175WP 2003 12 10 CALA0300609 120031021A3350110049 CHARGER DOUG DC9 DC982 3022082WP PWA JT8 JT8D17 52049NE CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0983870 48056 EMERGENCY PATH LIGHTS INOPERATIVE FROM 6DEF THROUGH 14DEF. REMOVED AND REPLACED FORWARD BATTERY PACK CHARGER IAW MM 33-53-00. 2L72 4F4 F A6WE E2EA 20031210002032003121000203NM 2003 12 10 03FDEA02005 120031130A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 CENTER CARGO BETWEEN STA 5-113 TO STA 1541, NR 52 L LONGERON SPLICE FOUND CRACKED. REMOVED DAMAGED LONGERON SPLICE AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SPLICE AT CENTER CARGO BETWEEN STA 5-113 TO STA 1541, NO.52 LONGERON AREA AS PER DRAWING N5A6774. 2L73 4F RTA22WE 20031211000152003121100015WP 2003 12 11 ABXA030421 120031104A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 L2 LOWER AFT DOOR CORNER HAD A REPAIR THAT DID NOT CONFORM TO SERVICE REWORK DWG SR08530021 OR ENG SKETCH ES00863. REMOVED EXISTING REPAIR AND STRUCTURAL COMPONENTS TO FOM. FABRICATED REPAIR DOUBLERS, ALODINED, PRIMED AND REINSTALLED COMPONENTS IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0 AND REA D853-48057MR. 2L74 4F 4A25 20031211000502003121100050NM 2003 12 11 AWXA200301402 120031013A5315146N6447 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1474, RBL 9. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM FROM BS 1474, RBL 9; FABRICATED REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 6 FIG 1. 2L72 4F RTA2NM 20031211000802003121100080NM 2003 12 11 AWXA200301415 120031027A5320654659260 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR CHANNEL AT BS 860, RBL 3. MAINTENANCE REMOVED DAMAGE SECTION OF FLOOR CHANNEL AT BS 860, RBL 3; FABRICATED A NEW REPLACEMENT SECTION OF CHANNEL AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 FIG 201. 2L72 4F RTA16WE 20031211001032003121100103CE 2003 12 11 AMWA67 120031024A553111464000061 RIB BEECH 1900 1900D 1154162CE VRTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07174YV UE174 3 CRACKS FOUND ON THIS RIB AT STRINGER TO RIB INTERSECTION. 1 AT STRINGER P/N 101-640000-37 FIRST RIVET HOLE ON RIB RT SIDE. 1 LOCATED LT STRINGER 101-640000-39 AND 1 RT STRINGER 101-640000-42. BOTH AT FIRST RIVET HOLE OF RIB. 2L72 4T RTA24CE 20031211001202003121100120NM 2003 12 11 AALA20031314 120031123A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 MIA EMERGENCY LIGHTS AT SEATS 1E TO 14D INOPERATIVE. REPLACED FIRST CLASS AND MID SECTION EMERGENCY LIGHT BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031211001282003121100128WP 2003 12 11 AALA20031400 120031208A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219617R 53564 DFW OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031211001392003121100139WP 2003 12 11 AALA20031387 120031205A335060030451 BATTERY DOUG DC9 DC982 3022082WP AFT AIRSTAIRS DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21411AA 49322 DFW AFT AIRSTAIRS CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT AIRSTAIRS CATWALK EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001422003121100142WP 2003 12 11 AALA20031390 120031206A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21420AA 49332 TPA EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK B5-27 INOPERATIVE. REPLACED BATTERY PACK B5-27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001442003121100144WP 2003 12 11 AALA20031270 120031115A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213507A 49801 SAT FORWARD GALLEY COCKPIT CENTER EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD GALLEY COCKPIT CENTER EMERGENCY LIGHT BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001512003121100151WP 2003 12 11 AALA20031277 120031116A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21473AA 49648 LGA L1 DOOR EMERGENCY LIGHT BATTERY WILL NOT HOLD A CHARGE. REPLACED L1 DOOR EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001562003121100156WP 2003 12 11 AALA20031278 120031116A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21473AA 49648 LGA EMERGENCY AISLE PATH LIGHTING MODULE AT L1 DOOR WILL NOT HOLD A CHARGE. REPLACED EMERGENCY AISLE PATH LIGHTING MODULE AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001582003121100158NM 2003 12 11 AALA20031280 120031116A3350S283W2031 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21756AM 30264 DFW L1 DOOR EMERGENCY LIGHT BATTERY PACK IS INOPERATIVE. REPLACED L1 DOOR EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031211001602003121100160WP 2003 12 11 AALA20031282 120031116A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21417AA 49328 SAT EMERGENCY CEILING LIGHTS ABOVE ROWS 8, 9 AND 10 ILLUMINATING VERY DIM. REPLACED BATTERY FOR EMERGENCY CEILING LIGHTS ABOVE SEATS 9D, 9E AND 9F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001632003121100163EU 2003 12 11 AALA20031284 120031117A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2140064 507 MIA EMERGENCY LIGHT AT SEAT 14G INOPERATIVE. REINSTALLED CONNECTION FOR EMERGENCY LIGHT AT SEAT 14G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20031211001702003121100170WP 2003 12 11 AALA20030912 120030826A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21982TW 53632 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS INOPERATIVE ON SIDES OF SEATS FROM SEAT ROW 20D BACK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031211001772003121100177NM 2003 12 11 USAABB03205 120031031A3397W3054000320 WIRE BOEING757 7572B7 1384964NM CABIN LOOSE A USAAK NONE O OTHER NRNOT REPORTED 1 EA19611AU 27123 CLT - EMERGENCY LIGHTS IN ZONE C ILLUMINATE IN TURBULENCE. FOUND WIRE W3054-0003-20 CHAFING IN THE P62 PANEL. SECURED WIRE AND REPAIRED CHAFE. (M) 2L72 4F RTA2NM 20031211001992003121100199EU 2003 12 11 USAA030243 120031103A5320 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND CORRODED SILL 3.4 CM BY 3.3 CM, .049 INCH DEEP, FRAME 66, PLUS Y 104. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. (M) 2L72 4F RTA28NM 20031212000192003121200019 2003 12 12 SWAA032415 420031031A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R2 DOOR EVACUATION SLIDE LOOSE. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031212000512003121200051WP 2003 12 12 UPS03841565 120031019A533057552713N1 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 LOWER FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 200 TO 380 LONG 31L-31R. REMOVED AND REPLACED LOWER SKIN IAW DWG 5755271 AND SRM 53-1-0, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20031212000552003121200055EU 2003 12 12 MALA030492 120031029A5320 SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434XJ 340B434 DURING A SCHEDULED 4K-INSPECTION TIMCO FOUND CORROSION AT STA 225.0 WL 70.0 VERTICAL SUPPORT LT SIDE OF COCKPIT DOOR. MAINTENANCE CUT OUT DAMAGED AREA FABRICATED AND INSTALLED T-ANGLE REPAIR IAW MESABA EO S53185. 2L72 4T RTA52EU 20031212000682003121200068EA 2003 12 12 MASA200300430 120031030A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT FALSE INDICATIONA MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0775993 7372 ASH 2672 BTV-PHL. DURING T/O ROLL PASSENGER DOOR WARNING LIGHT ILLUMINATED. A/C ABORTED T/O AND RETURNED TO GATE. MX PERFORMED HIGH SPEED TAXI. NO DEFECTS NOTED. 2L72 4F RTA21EA 20031212000742003121200074NM 2003 12 12 03FDEA01912 120031113A5320 WEB BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 CORROSION ON AFT RIGHT WEB AT BS 1130, RBL 61, WL 208. CORROSION ON AFT RIGHT WEB BS 1130, RBL 61, WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED WEB IAW SRM 51-40-2. 2L73 4F RTA3WE 20031212000792003121200079EU 2003 12 12 MALA030496 120031107A7931IPTE1191000200 TRANSMITTER SAAB SF340 340B 7860101EU RT ENGINE FAULTY A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15423XJ 340B423 DURING FLIGHT 2925, RIGHT ENGINE OIL PRESSURE DROPPED TO ZERO. AIR RETURN TO MEM. MAINTENANCE INSTALLED NEW PSI TRANSMITTER OIL P/N ON IPTE119-1000-200D1, S/N ON 4181-4-428/382 IAW AMM 79-30-05-4. OPS AND LEAK CHECK GOOD. 2L72 4T RTA52EU 20031212000812003121200081 2003 12 12 SWAA032429 420031103A2565D31354 SLIDE BOEING737 7373Y0 1384671NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031212000852003121200085NE 2003 12 12 SWAA032402 220031031A73211853M33POS5 EEC BOEING737 7377H4 1384404NM GE CFM56 CFM567B24 NE NR 1 ENGINE FAULTY A SWAAK NONE R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW29406WN 27894 888427 NR 1 ENG WOULD NOT REACH CLIMB POWER, THROTTLE LEVER HAD 4 KNOBS AHEAD OF NR 2 ENG. RECYCLED NR 1 EEC AND NR 1 ENG OPERATED NORMALLY. C/W BITE CK AND REMOVED AND REPLACED NR 1 EEC PER MM. 2L72 4F4 FRTA16WE E00055EN 20031210000992003121000099WP 2003 12 10 AALA20031324 120031123A2923861555 PUMP DOUG DC9 DC982 3022082WP HYD SYSTEM INOPERATIVE A AALAO OTHER K FLUID LOSS CRCRUISE 1 SW21496AA 49734 ORD T702/23 EN ROUTE DEN-ORD RIGHT HYDRAULIC QUANTITY DECREASED TO 4 QUARTS. RIGHT QUANTITY WENT TO ZERO AFTER GEAR WAS EXTENDED. LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT HAND ELECTRIC AUXILIARY HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210001352003121000135WP 2003 12 10 AALA20031343 120031130A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21493AA 49731 MIA, CABIN EMERGENCY LIGHTS INOPERATIVE. RECHARGED BATTERIES FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210002112003121000211WP 2003 12 10 UPS03841543 120031023A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 1740 LONG 17R IS CRACKED REMOVED LONGERON SECTION BETWEEN STATION 1735 TO 1760, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10 2L74 4F RT4A25 20031211000342003121100034NM 2003 12 11 AWXA200301392 120031030A53206916509906 ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND IN CLIP ANGLE ON BOTTOM OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACKED CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP ANGLE PER DWG 69-16509; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 & 11 PG 1. 2L72 4F RTA16WE 20031211000512003121100051NM 2003 12 11 AWXA200301403 120031013A5320453N163239 SUPPORT BRACKET BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM SUPPORT BRACKET BS 1310, LBL 14. MAINTENANCE REMOVED CORRODED FLOORBEAM SUPPORT BRACKET BS 1310, LBL 14; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 7A. 2L72 4F RTA2NM 20031211000642003121100064NM 2003 12 11 ABXA030439 120031109A2560101623203 GIRT BAR BOEING767 767281 1385109NM L1 DOOR DIRTY A ABXAK NONE O OTHER UKUNKNOWN 1 GL23793AX 154 23143 L-1 DOOR EMERGENCY SLIDE WOULD NOT ARM WITH DOOR CLOSED. FOUND DEBRIS IN GIRT BAR MECHANISM. CLEANED DEBRIS FROM GIRTH BAR MECHANISM. EMERGENCY ESCAPE SLIDE ARMING MECHANISM OPS CHECKED GOOD IAW B767 AMM 25-66-00-2. 2L72 4F RTA1NM 20031211000792003121100079NM 2003 12 11 AWXA200301414 120031027A5320654659259 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR CHANNEL AT BS 860, RBL 8.10. MAINTENANCE REMOVED DAMAGE SECTION OF FLOOR CHANNEL AT BS 860, RBL 8.10; FABRICATED A NEW REPLACEMENT SECTION OF CHANNEL AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG 201. 2L72 4F RTA16WE 20031211001012003121100101 2003 12 11 SWAA032474 420031106A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031211001292003121100129WP 2003 12 11 AALA20031401 120031208A3397 WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21415AA 49326 DFW FORWARD SERVICE EXIT DOOR EXIT IDENTIFYING LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AT FORWARD SERVICE EXIT DOOR IDENTIFYING LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001812003121100181NM 2003 12 11 USAABB03197 120031027A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19628AU 27806 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 13 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031211001862003121100186WP 2003 12 11 2003F00642 120030806A5330 DOUBLER DOUG DC9 DC915F 3022037WP FUSELAGE CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 AFT CARGO COMPARTMENT YSTA 718, BETWEEN LONGERON 22 LEFT AND LONGERON 23 LEFT, OUTFLOW CUTOUT REINFORCEMENT DOUBLER CORRODED. (M) 2L72 4F A6WE 20031212000952003121200095NM 2003 12 12 SWAA032412 120031101A53116546550 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031212000972003121200097NM 2003 12 12 SWAA032414 120031102A3350417A5700 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29408WN 27895 EEPLS INOP AT ROW 1. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20031212000982003121200098NM 2003 12 12 SWAA032393 120031029A26126566207 FIRE WARNING BOEING737 7373Q8 1384670NM APU BAY FAULTY A SWAAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SW29663SW 23256 APU FIRE WARN LIGHT ILLUMINATED DURING FLIGHT. INSPECTED APU AREA. NO EVIDENCE OF FIRE OR DAMAGE. DEFERRED APU AND APU FIRE WARN SYS'S PER MEL. 2L72 4F RTA16WE 20031212001012003121200101NM 2003 12 12 SWAA032396 120031030A3350101073 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 4. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20031212001032003121200103NM 2003 12 12 SWAA032398 120031030A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 925, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040213000262004021300026 2004 2 13 SWIA200312719 420031225A2297 WIRE EMB 120 EMB120ER 3260203SO AUTOPILOT SYS DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07292UX 120292 WITH AUTOPILOT ON FO'S SIDE, THE COMMAND BARS WILL NOT PITCH UP WITH ROCKER SWITCH ON AUTOPILOT CONTROL PANEL. IF GO AROUND BUTTON IS PRESSED, COMMAND BARS WILL NOT PITCH UP. REPAIRED WIRING TO P0144. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040213000282004021300028SO 2004 2 13 SWIA200312721 120031225A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO LT NACELLE MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07295UX8889 8889 120295 ON TAXI IN TO GATE, FLAP RETRACTION CAUSED DISAGREEMENT - NACELLE FLAPS LAGGING. REMOVED AND REPLACED LT NACELLE ACTUATOR IAW MM 27-50-08. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040213000372004021300037NM 2004 2 13 AALA20040177 120031201A5330143T3520 SKIN BOEING767 767223 1385123NM FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21328AA 22328 MCI FUSELAGE SKIN HAD A TEMPORARY REPAIR WITH BLIND FASTENERS PER AARD 53-00-50-3. ORIGINAL REPAIR IS 18 INCHES AFT OF EXISTING REPAIR. DAMAGE IS LOCATED RIGHT SIDE OF FUSELAGE AFT OF C-1 DOOR ON THE PART NUMBER 143T3520 SKIN AFT OF STATION 654 BETWEEN 29R AND 30R. AREA IS 3.0 X 3.0 INCH. REMOVED PREVIOUS REPAIR INSTALLED WITH BLIND FASTERNERS. CLEANED UP PREVIOUS TRIMOUT AND INSTALLED PERMANENT REPAIR PER SRM 53-00-01-2, FIGURE 214 FOR PERMANENT REPAIR AND MRB 767-2544 FOR MINIMUM LENGTH REQUIREMENT BETWEEN REPAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040212000042004021200004NM 2004 2 12 UPS03641620 120031202A2150 CLAMP BOEING767 767300 1385204NM LT HEAT EXCHANGEBROKEN A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01315UP 27743 INSPECTION TYPE:ETOP ATB - LT PACK INOPERATIVE LIGHT ILLUM AND LT (PACK TEMP) EICAS MESSAGE. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED AND RESET PUSHED. REMOVED AND REPLACED BROKEN CLAMP TO HEAT EXCHANGER RVM, LT PACK. OPS CHECK NORMAL IAW MM 21-50-00. 2L72 4F RTA1NM 20040212000192004021200019NE 2004 2 12 0068494A 320031009A6111RFC11M1M1R6A BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF* NE PROPELLER CRACKED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 852106 CRACK AT PROPELLER BLADE SHANK FILLET RADIUS. 2L72 4T4 TRTA31SO E20NE 6 CP7NE 20040212000802004021200080NE 2004 2 12 MDR03025 220030812A7230670802 COMPRESSOR WHEEL SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE ENGINE CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09HCCAT2889 64058 672549 ONE EACH CRACK INDICATION FOUND BY EDDY CURRENT INSPECTION. INDICATION IS IN THE LOCATION OF THE BLADE RETENTION PIN HOLE, ON THE CENTER FLANGE. INDICATION COULD NOT BE DETECTED BY FPI WHICH IS THE METHOD OF INSPECTION CALLED FOR IN THE OVERHAUL MANUAL. CAUSE: UNKNOWN 2G72 4U4 U H4EA E15EA 20040212000822004021200082NE 2004 2 12 MDR03027 120030812A64106516000025103 STRAP SKRSKYS64 S64F 8142610NE TAIL ROTOR BLADECRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09158AC192 64V30272930 64081 ON THE INBOARD SIDE OF THE BLADE, THERE IS A CRACK IN THE STRAP AND POCKET. THE CRACK STARTS AT THE ROOT END SIDE OF THE STRAP AND EXTENDS 3.75 INCHES TOWARD THE TIP END, INTO THE POCKET. THE CRACK IS 9.25 INCHES FROM THE TRAILING EDGE OF THE FAIRING. CAUSE: UNKNOWN 2G72 4U H6EA 20040212000832004021200083NE 2004 2 12 MDR03028 120030812A64106516000025103 STRAP SKRSKYS64 S64F 8142610NE TAIL ROTOR BLADECRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09158AC225 64V47474083 64081 THE STRAP IS CRACKED ON THE INBOARD SIDE OF THE BLADE APPROXIMATELY 9.25 INCHES FROM THE TRAILING EDGE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE APPROXIMATELY 1.5 INCHES. THE CRACK STARTS WHERE THE LEADING EDGE OF THE FAIRING, PN 65161-00011-042, SLIDES BETWEEN THE STRAP, PN 65160-00025-103, AND THE CHANNEL ASSEMBLY, PN 65160-00029-081. CAUSE: UNKNOWN 2G72 4U H6EA 20040217000142004021700014EA 2004 2 17 ASOA03690 120031228A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT SHORTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11845AS 7324 FLT 4232 - DURING A GROUND INSPECTION IN DFW, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND A SCREW SHORTING AGAINST THE BULB ON THE PASSENGER DOOR FLOODLIGHT AND ADJUSTED THE FLOODLIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000162004021700016EU 2004 2 17 ASOA03682 120031201A5320 ANGLE AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE TEE ANGLE AT THE INBOARD SIDE OF THE SERVICE DOOR THRESHOLD BETWEEN FS 36-38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TEE ANGLE AT THE INBOARD SIDE OF THE SERVICE DOOR THRESHOLD BETWEEN FS 36-38 IAW SRM 51-25-01. (M) 2H72 4T RT 20040217000182004021700018EU 2004 2 17 ASOA03685 120031201A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE RIGHT SEAT TRACKS BETWEEN FS 38-39 AND FS 39-40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACKS BETWEEN FS 38-39 AND FS 39-40 IAW SRM 51-25-02. (M) 2H72 4T RT 20040217000382004021700038EU 2004 2 17 2004F00064 120030926A5330 SKIN AIRBUS320 A320233 3930329EU CROWN DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND UPPER FUSELAGE CROWN AREA BETWEEN FRAMES 52 AND 53 STRINGER 1 LT AND 1 RT VHF ANTENNA MOUNT SURFACE HAS TOOL MARKS AROUND PERIPHERY. UPON FURTHER EVALUATION OF UPPER FUSELAGE CROWN AREA BETWEEN FRAME 52 AND FRAME 53, STRINGER 1L AND 1R, VHF ANTENNA MOUNT SURFACE, FOUND TOOLING MARKS TO BE CHIPPED PAINT AND NO DAMAGE TO STRUCTURE NOTED. TREATED AND PRIMED BARE METAL. (M) 2L72 4F RTA28NM 20040217000442004021700044NM 2004 2 17 2004F00070 120031224A3020577957 DUCT BOEING727 727225 1384077NM NR 2 ENGINE DAMAGED A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07801EA 22432 AFTER TAKEOFF OF SEATTLE, WA, NR 2 ENIGNE FIRE INDICATION WITH FIRE BELL AND LIGHT. ACCOMPLISHED APPROPRIATE CHECKLIST. EMERGENCY DECLARED AND AIRCRAFT LANDED SEA WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE HEATER-FUEL DE-ICE DUCT. ENGINE RUN AND LEAK CHECK NORMAL. (M) 2L73 4F A3WE 20040217000532004021700053NM 2004 2 17 2004F00075 120031218A5330 SKIN BOEING727 727222 1384073NM FUSELAGE TORN A RYNAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW077645U 20039 IN CRUISE FLIGHT, CABIN CLIMBS 1000 FPM IN BOTH AUTO AND STANDBY MODES. FOUND FOUR INCH CRESCENT TEAR IN FUSELAGE SKIN ON RIGHT SIDE OF FUSELAGE AT STATION 420, BETWEEN STRINGERS 20R AND 21R. REMOVED DAMAGED SKIN SECTION AND REPAIRED USING AN EXTERNAL REPAIR WITH SOLID FASTENERS. REPAIRED FUSELAGE AND ZEE FRAME AND SHEAR TIE AT STATION 420. (M) 2L73 4F A3WE 20040212000932004021200093NM 2004 2 12 EIA2003165 120031201A3350S153610A BATTERY BOEING747 747212B 1384886NM PWA JT9 JT9D* NE EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 UPPER DECK CREW SERVICE DOOR EMERGENCY SILL LIGHTS INOPERATIVE. REMOVED AND REPLACED UPPER DECK CREW SERVICE DOOR EMERGENCY LIGHT IAW B747MM 33-51-07. OPS CHECKED GOOD. 2L74 4F4 F A20WE E20EA 20040212001102004021200110NM 2004 2 12 ANCF200300027 120031209A4910 APU BOEING767 767* NM APU BAY LEAKING W ANCFO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO23421AV 25421 SMOKE ODOR THROUGH THE PASSENGER CABIN WITH NO SMOKE EVIDENCE. SMOKE DETECTORS ACTIVATED ON THE AFT AND FORWARD LAVATORIES. UTILITY BUSES WERE TURNED OFF WITH NO HELP ON THE SITUATION. LT AND RT RECIRCULATING FANS WERE TURNED OFF AS WELL AS THE RIGHT HAND. PACK AND THE ODOR DISAPPEARED. ENGINE BLEED AIR TUBE LINES AND PACKS BLEED AIR TUBE LINES WERE INSPECTED IAW AMM 20-20-00. OIL LEAK EVIDENCE WAS FOUND INTO THE APU BLEED AIR TUBE LINES. APU WAS DEFERRED TO DMI.N°1 MEL 49-11-1 CAT "C". 2L72 4F RTA1NM 20040213000112004021300011CE 2004 2 13 57206 120031220A3242 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG MALFUNCTIONED A AMWAO OTHER O OTHER LDLANDING 1 CE07140ZV UE140 AFTER LANDING IN PIT. CREW REPORTED THAT THE LT BRAKE HAD VERY LITTLE PRESSURE ON TAXI. BLEED LT BRAKES SYS. IAW MM 32-40-00. OPS AND LEAK CK GOOD. 2L72 4T3 TRTA24CE E2NE 20040217000212004021700021EU 2004 2 17 ASOA03683 120031201A5310 CROSSBEAM AEROSPATR72 ATR72 EU FS 36 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE CROSSBEAM AT FS 36 BETWEEN THE LEFT AND RIGHT SIDE WALLS WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CROSSBEAM AT FS 36 BETWEEN THE LEFT AND RIGHT SIDE WALLS IAW SRM 51-24-00 AND 51-25-01. (M) 2H72 4T RT 20040217000452004021700045NM 2004 2 17 2004F00071 120030926A5754 SKIN BOEING727 727225 1384077NM KRUGER FLAP DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07801EA 22432 DURING SERVICE CHECK, FOUND DENT ON LEADING EDGE OF SKIN OF LEFT WING AT STATION 180 ABOVE NR 3 KRUGER FLAP. CUT OUT DENTED SECTION OF WING, FIXED LEADING EDGE SKIN AND INNER SKIN AT STATION 180. FABRICATED A FLUSH REPAIR FILLER AND DOUBLER. FABRICATED SKIN FOR INNER SKIN REPAIR AND FABRICATED RIB REPAIR. TREATED AND PRIMED ALL PARTS. INSTALLED ALL PARTS TO COMPLETE LEADING EDGE REPAIR. (M) 2L73 4F A3WE 20040217001412004021700141CE 2004 2 17 J4P2004F00000 120030627A2841DSFG1710 INDICATOR CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO FUEL QTY INCORRECT E J4PAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO13427CC 421C0348 L243007 AC WAS LOADED FOR A TRIP WITH ENGINES STARTED. THE FUEL QUANTITY INDICATOR FOR THE AIRCRAFT LT AND RT TANKS WAS STEADY, BUT QUANTITY WAS LOW WITH A FULL FUEL LOAD ON BOARD, VISUALLY VERIFIED BY PILOT. TAXIED BACK TO THE HANGER AND UNLOADED PASSENGERS TO DIFFERENT AC AND CONTINUED CHARTER OPERATIONS. THE FUEL GAUGE WAS FOUND TO BE FAULTY AND A NEW GAUGE WAS ORDERED AND INSTALLED. THEY FOUND THE AIRCRAFT TO BE IN LIMITS AND SIGNED OFF THE WRITE UP IN AIRCRAFT DISCREPANCY LOG ON 7/1/03. THE AC THEN RETURNED TO SERVICE. 1L72 3O3 O A7CE E7CE 20040217001682004021700168CE 2004 2 17 DXTA200300136 120031013A2810 FLOW DIVIDER CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT ENGINE OUT OF RIG E DXTAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 GL07320QS 5600321 PCE500130 DURING GROUND CHECK BY CREW LT ENGINE FLAMED OUT WHEN POWER BROUGHT BACK TO IDLE. FOUND RIGGING ON FUEL FLOW DIVIDER SLIGHTLY OUT. ADJUSTED RIGGING ON FUEL FLOW DIVIDER FOR A SLIP FIT IN IDLE DETENT POSITION IAW 560 MM CHAPTER 76-11-00 ALSO ADJUSTED LOW END IDLE SCREW TO BRING IDLE SETTING INTO REQUIRED RANGE IAW 560 MM CHAPTER 71-01-02, ENGINE OPS CHECKED GOOD. 2L72 4F4 FRTA22CE E25EA 20040217001872004021700187CE 2004 2 17 GLBA20030521 120031230A3150 WARNING LIGHT BEECH 1900 1900D 1154162CE COCKPIT ILLUMINATED A GLBAG O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 NM03192GL UE192 PULLED O2 MASKS FOR PAX WITH CAB ALT HI ANNUNCIATORS COULD NOT DESCANT DUE TO ICING, REINSTALLED MASKS CAB ALT HIGH LIGHT CAME ON DUE TO RT BLEED SYS IN OFF. OPS CK GOOD. 2L72 4T RTA24CE 20040218000092004021800009NM 2004 2 18 2003UALA00982 120031225A2421729825J IDG BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT GENERATOR INOPERATIVE A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29597UA 28750 ABORTED TAKEOFF DUE TO LT IDG LIGHT. LEFT INTEGRATED DRIVE GENERATOR (IDG) FAILED. REPLACED THE LEFT IDG. NORMAL WEAR, REPLACED THE PUMP AND MOTOR ASSEMBLY. 2L72 4F4 FRTA2NM E17NE 20040212001812004021200181NM 2004 2 12 AWXA200301592 120031205A575465C26601179 SKIN BOEING737 73733A 1384673NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD MAIN TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. 16, PG. 67-69. 2L72 4F RTA16WE 20040212001832004021200183EU 2004 2 12 AWXA200301594 120031222A5230 LATCH AIRBUS320 A320232 3930326EU CARGO DOOR LACK OF LUBE A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28640AW 448 ABORTED TAKEOFF, SHORTLY AFTER TAKEOFF ROLL, EN ROUTE, THE AFT CARGO DOOR INDICATED OPEN, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND DOOR SECURED, APPLIED MEL 52-70-01, COND. 8, AND VISUALLY VERIFIED DOOR SECURE. UPON ARRIVAL, MAINTENANCE CLEANED AND LUBRICATED DOOR LATCH MECHANISM, CYCLED DOOR A DOZEN TIMES, DOOR INDICATION WAS GOOD. 2L72 4F RTA28NM 20040212001922004021200192NM 2004 2 12 ANCF200300031 120031219A5610 SEAL BOEING757 757236 1384971NM RROYCERB211 RB211* 54555NE COCKPIT WINDOW OUT OF POSITION W ANCFC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO23951PG 22185 DURING TAKEOFF ROLL A STRONG NOISE CAME IN TO COCKPIT, LT SIDE WINDOW, WAS NOT FUSELAGE. SEAL WAS REPOSITIONED IAW AMM 56-11-00 PAGE 401. 2L72 4F4 FRTA2NM A12EU 20040217000402004021700040EU 2004 2 17 2004F00066 120030926A5340D53470269200000 FITTING AIRBUS320 A320233 3930329EU FLOOR SUPPORT CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56, LBL 12 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT FITTING AT FRAME 56, LBL 12, IN AFT CARGO PIT. (M) 2L72 4F RTA28NM 20040217001942004021700194CE 2004 2 17 57453 120031229A3242 BRAKE BEECH 1900 1900D 1154162CE MLG INOPERATIVE A AMWAO OTHER O OTHER LDLANDING 1 CE07176YV UE176 UPON LANDING RT BRAKES FELT SOFT. MAINTENANCE CALLED. BRAKES WERE BLEED. OPS CK NORMAL. 2L72 4T RTA24CE 20040217000042004021700004NM 2004 2 17 2004F00057 120030930A5740659892433 ANGLE BOEING727 727222 1384073NM SPOILER ACTUATORCRACKED A FDKAK NONE O OTHER ININSP/MAINT 1 SW077640U 19913 AT B-CHECK, FOUND NR 2 SPOILER ACTUATOR IB MOUNT BRACKET CRACKED. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR IB MOUNT BRACKET. RIGG AND LEAK CHECKED NORMAL. (M) 2L73 4F A3WE 20040217000152004021700015EA 2004 2 17 ASOA03689 120031228A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCH, THE FLOOR SUPPORT CLIP JUST INBOARD OF THE CARGO THRESHOLD WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIP JUST INBOARD OF THE CARGO THRESHOLD IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040303001632004030300163NE 2004 3 3 00068494 320031009A6111RFC11M1M1R6A BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF* NE PROPELLER CRACKED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 852106 CRACK AT BLADE SHANK FILLET RADIUS. PROP 2L72 4T4 TRTA31SO E20NE 6 CP7NE 20040304001402004030400140WP 2004 3 4 ASAA0380800 120031119A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001432004030400143WP 2004 3 4 ASAA0380832 120031216A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS39201 53016 SEA LINE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001522004030400152WP 2004 3 4 ASAA0380719 120031112A3397 CONNECTOR DOUG DC9 DC983 3022083WP LIGHT MODULE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 1 IN FIRST CLASS CABIN. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040329000062004032900006EU 2004 3 29 USAASA03141 120031225A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19704US16103 0922 PHL - THE EMERGENCY POWER SUPPLY UNIT IN THE AFT POSITION FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040329000182004032900018WP 2004 3 29 ASAA0380395 120030421A52805930583247 TIE DOUG DC9 DC982 3022082WP MLG DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND LT MLG DOOR FRAME TIE CRACKED INTERNAL STRUCTURE JUST BELOW GEAR BUMPER. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040401000012004040100001NM 2004 4 1 AALA20031256 120031110A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21697AN 26977 MIA - DURING OVERNIGHT MAINTENANCE, FOUND FIRST LAST EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401000192004040100019NM 2004 4 1 AALA20031171 120031022A33500201991020 LIGHT BOEING757 757223 1384957NM ROW 31D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21694AN 26974 DFW - MAINTENANCE OBSERVED SEAT MOUNTED EMERGENCY LIGHTING INOPERATIVE AT ROW 31D. REPLACED THE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401000242004040100024WP 2004 4 1 ASAA0380411 120030425A532199365991 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR PANEL 3C3 IS CORRODED. REPLACED FLOOR PANEL PER EA 2550-01066. (M) 2L72 4F RTA6WE 20040401000392004040100039WP 2004 4 1 ASAA0380406 120030421A523059360641 FITTING DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND CORROSION ON CARGO DOOR BEAM TEE FITTING. REPLACED TEE FITTING PER SRM. (M) 2L72 4F A6WE 20040401001322004040100132EU 2004 4 1 23431924 120030917A5320D5348004320401 SILL AIRBUS320 A320233 3930329EU IAE V2500 V2500A1 NE L2 DOOR CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK, FOUND L2 DOOR SILL HAS RIVET HEADS THAT HAVE EXFOLIATED CORROSION BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITTING, DRAINS AND ANGLE AT FRAME 67, LT LOWER UNDER SILL. (SDR NR 23431924) 2L72 4F4 FRTA28NM E311NE 20040401001432004040100143EU 2004 4 1 TRB2004F00004 120031229A3350AQS1000 BATTERY PACK AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT DISCHARGED A TRBAK NONE L NO TEST ININSP/MAINT 1 SO21355AT 355 PASSENGER CABIN AND EXITS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2H72 4T RTA53EU 20040304001392004030400139WP 2004 3 4 ASAA0380847 120031227A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 LAS PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE BETWEEN ROW 17 AND 21. RECONNECTED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001482004030400148WP 2004 3 4 ASAA0380803 120031124A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 23. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040308001452004030800145NM 2004 3 8 ASAA0310230 120030326A5730BAC15171539 SKIN BOEING737 737298C 1384490NM LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND TANK SKIN AT WING STATION 117L, STRINGER 9L CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040217000362004021700036EA 2004 2 17 ASOA03680 120031227A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11850AS 7355 DURING A GROUND INSPECTION IN ATL, AN EMERGENCY FLOOR LIGHT STRIP WAS FOUND BROKEN AT THE FRONT OF THE STRIP. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000412004021700041EU 2004 2 17 2004F00067 120030926A7120 CROSSBEAM AIRBUS320 A320233 3930329EU NR 1 ENGINE DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT CROSSBEAM HAS NICKS, SCRATCHES, AND GOUGING. INSPECTED AND CLEANED DAMAGED AREA. REPAIRED NR 1 ENGINE FORWARD MOUNT CROSSBEAM BY REMOVING AND REPLACING BUSHING. (M) 2L72 4F RTA28NM 20040217001692004021700169CE 2004 2 17 DXTA200300137 120031014A3242 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07330QS 5600329 ON TAXI OUT FIRST 5 BRAKE APPLICATIONS WERE NORMAL, ON THE SIXTH APPLICATION BRAKE PEDALS WENT TO THE FLOOR, CO-PILOTS BRAKES WERE SPONGY BUT AFTER PUMPING BRAKES WAS ABLE TO STOP AIRCRAFT, TAXI AIRCRAFT AND APPLIED BRAKES 30-40 TIMES FOUND BRAKES TO OPERATE NORMALLY, CHECKED BRAKE PRE-CHARGE AND RESERVOIR, FOUND BRAKES FIRM, BLED BRAKES IAW CE-560 MM CHAPTER 32-42-00 NO AIR DETECTED. OPERATIONAL CHECKED GOOD. 2L72 4F RTA22CE 20040218000102004021800010NM 2004 2 18 AALA20031482 120031228A2751 WARNING LIGHT BOEING767 767323 1385205NM TE FLAPS ILLUMINATED A AALAO OTHER N FALSE WARNING CLCLIMB 1 SW21384AA 26996 ORD T088/28 EN ROUTE ORD TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED DURING FLAP RETRACTION. ORD MAINTENANCE EXERCISED FLAPS SEVERAL TIMES ON GROUND. NO LIGHT ILLUMINATED DURING RETRACTION. UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F RTA1NM 20040225001782004022500178NM 2004 2 25 DLM88031147 120031229A3350RPS1 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGNECY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27952DL 49883 AFT CABIN EMERGENCY PATH LIGHTS ALL INOP FROM SEAT ROW 31 AFT. TROUBLESHOT EMERGENCY LIGHT SYSTEM IN AFT CABIN, FOUND BAD BATTERY CHARGER ASSEMBLY IN OVERHEAD AT ROW 36-37. REMOVED AND REPLACED BATTERY CHARGER. ALL EMERGENCY LIGHTS OPERATE NORMAL. 2L72 4F RTA6WE 20040301000652004030100065CE 2004 3 1 IMJ2004F00002 120030721A2422PC251123E INVERTER CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NR 2 FAILED E IMJAO OTHER O OTHER NRNOT REPORTED 1 EA2515SK 3998 5600395 NR 2 INVERTER FAILED INTERMITTNETLY IN FLIGHT. 2L72 4F4 FRTA22CE E25EA 20040301001022004030100102EU 2004 3 1 RYN2004F00004 120031019A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 A (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 28 TO 31 AT STRINGER 34R. 2L72 4F4 FRTA28NM E40NE 20040301001062004030100106EU 2004 3 1 RYN2004F00007 120030912A5321 FLOOR PANEL AIRBUS320 A320233 3930329EU IAE V2500 V2500A1 NE AFT LAV CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK FOUND AFT LAV FLOOR PANEL WITH CORROSION AT NUMEROUS LOCATIONS AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REPAIRED AFT LAV FLOOR PANEL, CORROSION AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REMOVED AND REPLACED INSERTS. 2L72 4F4 FRTA28NM E311NE 20040227001032004022700103CE 2004 2 27 2004F00054 120031219A5730 SKIN BEECH B300 B300 1159232CE LT WING LE DEBONDED E K NONE O OTHER ININSP/MAINT 1 NE03904MC FL44 LEFT IB LEADING EDGE WING PANEL WAS REMOVED TO REPLACE THE DE-ICE BOOT AND IT WAS DISCOVERED THAT SUBSTANTIAL DEBONDING OF THE LOWER HALF OF THIS PANEL HAD OCCURRED. THERE WAS NO APPARENT DAMAGE TO THE OUTSIDE SKIN THAT WOULD EXPLAIN THIS AND ITS UNLIKELY THAT THE LINE PERSONNEL FUELING THE AUX TANK CAUSED THIS DUE TO THE DEBONDING ISOLATED TO THE LOWER SKIN. TECH SUPPORT REQUIRES REPLACING THIS SKIN WITH A NEW UNIT. 2L72 4T RTA24CE 20040301000102004030100010EU 2004 3 1 KBM2004F00007 120031104A2140350A27012821 CONNECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HEATER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 HEATER INOPERATIVE, BLOW A/C AIR. REMOVED AND REPLACED WITH NEW. (K) 1G71 3U3 U H9EU E19EU 20040301000302004030100030EU 2004 3 1 PG92004F00009 120031110A6230704A33640021 SPACER UROCOPEC130 EC130B4 8680989EU BUSHING SEIZED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19130PH465 3670 SPACER SEIZED IN BUSHING. (RMA NR R045786) 1G72 3U H9EU 20040301000632004030100063CE 2004 3 1 IMJ2004F00001 120030722A213113035616 CONTROLLER CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE CABIN PRESSURE FAILED E IMJAO OTHER J WARNING INDICATION CRCRUISE 1 EA25550KM S5500081 CABIN LOST PRESSURIZATION AT FL27 IN CRUISE WHEN CONTROLLER WAS ADJUSTED FOR DESCENT. 1L72 4F4 FRTA22CE E1NE 20040227000542004022700054NM 2004 2 27 ASAA0370019 120031228A249710321751 CABLE BOEING737 737790 13844CNNM E/E BAY BURNED A ASAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM01647AS 33012 SEA - DURING TAKEOFF OUT OF SEATTLE, FLIGHT ATTENDANT REPORTED STRONG ACRID BURNING ODOR IN 1ST CLASS CABIN THEN IT SPREAD THROUGH OUT THE AIRCRAFT. PERFORMED AN AIR TURN BACK TO SEATTLE AND LANDING WITHOUT INCIDENT. UPON INSPECTION FOUND BURNED POWER FEEDER CABLE AT THE TERMINAL LUG OF THE P91 PANEL IN THE E/E COMPARTMENT CAUSED BY LOOSE TERMINAL LUGS. REPLACED TRANSFORMER AND TERMINAL PLATE IN RIGID BUSS ASSEMBLY OF P91 PANEL. REACCOMPLISHED TERMINAL STUD TORQUE AT P91 AND P92 PANELS. SYSTEM OPERATED NORMAL UPON OPS CHECK. (M) 2L72 4F RTA16WE 20040301000372004030100037EU 2004 3 1 KBT2004F00000 120030916A6720 BEARING SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE T/R CONTROL ROD FAILED B KBTRK NONE O OTHER ININSP/MAINT 1 NM07353MH1227 4122 3267 2111 DURING INSPECTION OF TAIL ROTOR CONTROL ROD, FOUND ELASTOMERIC BEARING HAD FAILED. INNER BUSHING HAD BECOME UNBONDED, SHIFTED FULLY TO ONE SIDE (NOT CENTERED). 1G71 3U3 U H9EU E00054EN 20040301000432004030100043CE 2004 3 1 IMJ2004F00000 120031118A3241MS24166D2 RELAY CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE ANTI SKID SYS CONTAMINATED A IMJAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA2515SK 5600395 ON TAXI (POWER BRAKE) AND (ANTI SKID) LIGHTS ILLUMINATED INTERMITTENTLY. FOUND ANTI SKID RELAY TO BE AT FAULT. SUSPECT THAT SKYDROL HAD MIGRATED INTO THE RELAY AND DAMAGED THE CONTACTS. PERHAPS A RELAY THAT IS BETTER PROTECTED AGAINST THE INGRESS OF FOREIGN MATTER (FLUIDS AND WATER) WOULD BE A BETTER CHOICE FOR THIS APPLICATION. 2L72 4F4 FRTA22CE E25EA 20030919000752003091900075 2003 9 19 53367 420030808A3442 CONNECTOR BEECH 1900 1900D 1154162CE WX RADAR SYS DIRTY A AMWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE0713ZV UE13 UPON TAKEOFF ON FLIGHT 5576 THE WEATHER RADAR FAILED. THE CREW RETURNED TO THE FIELD WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND RESEATED THE ANTENNA CONNECTOR. NO PARTS WERE USED THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030919000812003091900081NE 2003 9 19 NACA20030108 220030812A8530404481 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 8 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 AL03438722389 2389 533294 P35404 NR 2 ENGINE SHUT DOWN ON GROUND, NR 8 CYLINDER CRACKED. REPLACED NR 2 ENGINE, NR 8 CYLINDER. 2L74 4R4 R A781 5E8 20031002000512003100200051WP 2003 10 2 UPS03841207 120030826A534037552221 FITTING DOUG DC8 DC873F 302199FWP SUBFLOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, SEAT TRACK TO FLOORBEAM ATTACH FITTING IS CRACKED AT STA. 700 LBL. 24. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755222,AND SRM. 51-1-20D. 2L74 4F RT4A25 20030919000862003091900086EU 2003 9 19 HXS2003F00004 120030718A7603 ROLL PIN SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE TORQUE TUBE FAILED B HXSRO OTHER O OTHER NRNOT REPORTED 1 AL05405AE615 295 3286 22245 AIRCRAFT FAILED POWER CHECKS DUE TO TORQUE FAILURE. INVESTIGATED SITUATION AND DETERMINED THAT A ROLL PIN FAILURE HAD OCCURED. 1G71 3U3 U H9EU E19EU 20030919000902003091900090CE 2003 9 19 GLBA2003119 120030813A2612 FIRE DETECTOR BEECH 1900 1900D 1154162CE LT ENGINE MALFUNCTIONED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03220GL UE220 LT FIRE LOOP ANNUNCIATOR ILLUMINATED FOLLOWED BY LT FIRE HANDLE FLICKERING, INSPECTION LT ENG FIRE LOOP AND CONNECTORS, OPS CK GOOD 2L72 4T RTA24CE 20030919001112003091900111EU 2003 9 19 AWXA200300922 120030803A5315D5347217220390 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON MAIN CABIN FLOORBEAM AFT OF FR 64, Y1292. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED MAIN CABIN FLOORBEAM FROM FR 66-67, Y1292; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-44-11, PG. 1-2, AND SRM 51-42-11, PG. 6-7, & 28-30. 2L72 4F RTA28NM 20030919001262003091900126EU 2003 9 19 3602072103 120030721A6720350A331526006 BELLCRANK SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR WORN E S4WAK NONE O OTHER ININSP/MAINT 1 WP07820NA811 3602 22342 T/R PITCH BELLCRANK WORN BEYOND ACCEPTABLE LIMITS 1G71 3U3 U H9EU E00054EN 20030919001302003091900130EU 2003 9 19 160191 120030814A2751 WARNING LIGHT SAAB SF340 SF340A 7850100EU TE FLAPS FALSE ACTIVATIONA UHLAO OTHER N FALSE WARNING DEDESCENT 1 GL17104CQ 340A104 ON DESCENT INTO PIT, AIRCREW RECEIVED A FLAP CAUTION LIGHT. FLAP INDICATOR WAS READING ZERO AND THE HANDLE WAS SET AT ZERO. AIRCREW DECLARED AN EMERGENCY AND LANDED SAFELY IN PIT. MAINTENANCE INSPECTED FAULT AND FOUND NOTHING WRONG. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 20030915000512003091500051EU 2003 9 15 CCHA088957 120030902A2150510286C GEARBOX UROCOPEC135 EC135T1 5620026EU A/C PACK SEIZED B CCHAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO19911CK245 0138 METRO AVIATION VAPOR AIR CONDITIONING SYSTEM: 90 DEGREE GEARBOX SIEZED CAUSING INTERNAL SHAFT SHEER. ALSO FLEX DRIVESHAFT TO 90 DEGREE GEARBOX COUPLING SHEERED. REPLACED 90 DEGREE GEARBOX, FLEX DRIVESHAFT, AND COMPRESSOR. 1G72 3U H88EU 20030915000542003091500054EU 2003 9 15 BAQA088839 120030825A243523032048 STARTER GEN BOLKMS117 BK117B2 5626013EU ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA031174U778 7146 STARTER GENERATOR FAILED. WOULD NOT TEST. REPLACED WITH SERVICEABLE UNIT. 9/4/03 1G72 3U NCH13EU 20030915000892003091500089NE 2003 9 15 BAQA089070 220030729A73130319307840X INJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE FUEL SYS CLOGGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH2296 0131 30188 FUEL INJECTOR CLOGGED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H88EU E19EU 20030917000262003091700026NM 2003 9 17 03FDEA01167 120030728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 SNRM N0934 - RT WING- O/B FLAP (FLAP SIDE) O/B HINGE O/B PIVOT HOLE AND I/B AND O/B ACTUATOR ATTACHMENT HOLES FOUND BUSHING LOOSE. ** S/D ** COMING 2L73 4F RTA22WE 20030917000982003091700098NE 2003 9 17 S2YA03027 220030819A723030B428501 BLADE DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE BENT A S2YAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 GL13356SK 3163 SHORTLY AFTER TAKEOFF, THE CAPTAIN SAW A BIRD GO BY THE LEFT SIDE, THEN HEARD A BOOM AND THEN A SCRAPING SOUND. THE CREW PERFORMED AN AIR TURNBACK TO OMA. MAINTENANCE INSPECTED THE A/C AND FOUND TWO FAN BLADES BEN BUT NO OTHER DAMAGE. MAINTENANCE BORESCOPED THE ENGINE BUT FOUND NO FURTHER DEFECTS. MAINTENANCE REPLACED THE TWO BLADE IAW PRATT AND WHITNEY'S INSTRUCTION ON FAN BALANCE. MAINTENANCE RAN THE ENGINE WITH ENGINE VIBRATION WITHIN LIMITS AND NO OTHER DEFECTS. (M) 2H72 4T4 FRTA55NM E35NE 20030917001262003091700126NM 2003 9 17 DLM88030678 120030720A2910AE7055381 LINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE CHAFED A DALAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27908DL 49539 718171 DURING CLIMBOUT PASSING FL250. THE LT HYD PRESS LOW MSG ILLUMINATED ON OAP. LT HYD QTY DROPPED TO 3 QTS, ACCOMPLIHED POM PROCEDURE FOR HYD PRESS LOW,HYD QTY LOW OR DECREASING AND FINALLY LT HYD SYS FAILURE. PRIOR TO ENG START THE HYD QTY READ L-16..RT-14. FOUND LT ENG CENTER HYD FLEX LINE FROM PYLON TO ENG BADREPLACED HYD LINE LEAK CHECKS GOOD 2L72 4F4 FRTA6WE E9NE 20030917001362003091700136NM 2003 9 17 DL76L030700 120030728A4920 APU BOEING767 767332 1382001NM AFT SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO271200K25222 28457 SMOKE IN CABIN WHEN APU STARTED AT GATE PRIOR TO PUSH BACK. SHUT DOWN APU SMOKE CEASED. FOUND OIL IN APU EXHAUST, APU CHANGE IN PROGRESS. 2L72 4F RTA1NM 20030918000032003091800003NM 2003 9 18 03FDEA01502 120030911A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 STR 15L CRACKED AT 720B 4. REPAIRED IAW SRM 53-10-3 FIG 5 2L73 4F RTA3WE 20030918000322003091800032NM 2003 9 18 GAIA03038SP 120030719A5315 SPLICE BOEING727 727* NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CARGO DOOR DECK BS 640, FLOORBEAM SPLICE PLATE CRACKED FROM SLOT RADIUS FASI N/R 35932. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE179850 DTD 4-7-93. (M) 2L73 4F RTA3WE 20030918000812003091800081WP 2003 9 18 A4J2003F00001 120030710A335060030431 POWER SUPPLY DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE OVERWING EXIT INOPERATIVE A A4JAO OTHER O OTHER NRNOT REPORTED 1 SO35934LK 48157 DURING B CHECK PIE MAINTENANCE FOUND BOTH FORWARD OVER WING ENERGENCY LIGHTS COME ON AN WILL NOT EXTINGUISH WHEN BATTERY IS TURNED OFF. REMOVED AND REPLACED POWER SUPPLY FOR FORWARD OVER WING EMERGENCY C4 LIGHTS IAW DC9 MM 33-53-0, OPERATES NORMAL IAW DC9 MM 33-53-0. 2L72 4F4 F A6WE E2EA 20030918000942003091800094NE 2003 9 18 PCAA0308093 220030804A7200PW120A ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RIGHT LEAKING A PCAAO OTHER K FLUID LOSS DEDESCENT 1 EA13851EX227938053 343 121300 ITH-FLIGHT NR 3682. CREW REPORTED A STRONG BURNING ODOR ON INITIAL POWER REDUCTION ON DECENT. SUSPECT BLEEDS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW AIRLINES JOBCARD 008-71-01-349. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030919000502003091900050SO 2003 9 19 CHQA000416 120030811A5210 SEAL EMB 145 EMB145 3260210SO PAX DOOR FAILED A CHQAA UNSCHED LANDING O OTHER CLCLIMB 1 GL11264 WHILE CLIMBING OUT OF DC AND PASSING 10,000 FT, THE F/A CALLED UP FRONT TO TELL US THE MAIN CABIN WAS MAKING A VERY LOUD NOISE. WHILE ON THE P/A WITH HER, IT WAS OBVIOUS THERE WAS A MAJOR PROMLEM WITH THE DOOR. THE NOISE WE HEARD WAS VERY LOUD AND MADE IT VERY DIFFICULT TO TALK TO HER. WE STOPPED THE CLIMB AT ABOUT 12,000 FT, REQUESTED LOWER ALTITUDE AND RETURN TO THE FIELD. UPON FURTHER INSPECTION BY MAINTANCE, THEY FOUND THE DOOR SEAL TO BE BAD. REMOVED AND REPLACED MAIN DOOR RUBBER TRIM SEAL. 2L72 4F RTT00011AT 20030919001122003091900112EU 2003 9 19 AWXA200300923 120030805A5315D53472172203 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES OF AFT CABIN FLOORBEAM Y1292 L/H, FR 66 TO 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CABIN FLOORBEAM FROM FR 66-68, Y1292 L/H; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 29-30, 39-41, FIG. 18. 2L72 4F RTA28NM 20030919001252003091900125NM 2003 9 19 03FDEA01212 120030729A5753ARC70571 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RT WING O/B FLAP VANE- TEE FITTING NR 5 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 5 FROM INBOARD CORROSION IN HOLE, REPAIRED IAW EA 1-5750-71878. 2L73 4F RTA22WE 20030919001272003091900127 2003 9 19 3602012303 420030123A3425066304600 HSI SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP07820NA153 3602 22342 HEADING INDICATOR INOPERATIVE. 1G71 3U3 U H9EU E00054EN 20030919001312003091900131 2003 9 19 161971 420030811A2340 INTERPHONE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE CABIN INOPERATIVE A UHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL17152CQ 152 217 08/11/03, AT APPROX. 1845(UTC) FLT 4506 PIT-CRW, AIRCRAFT 152CQ HAD PERFORMED A RETURN TO GATE FOR COCKPIT TO CABIN INTERPHONE INOPERATIVE. FLIGHT ATTENDANT COULD NOT TRANSMIT TO CREW. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030919001452003091900145 2003 9 19 9015042703 420030427A34215040017901 GYRO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP07350R 1249 9015 9667 DIRECTIONAL GYRO, INOPERATIVE. 1G71 3U3 U H9EU E00054EN 20030919001462003091900146NE 2003 9 19 NACA20030110 220030816A8530356994 CYLINDER HEAD DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE CRACKED A NACAE ENGINE SHUTDOWN K FLUID LOSS TXTAXI/GRND HDL 1 AL031377K623 623 44596 P33708 NR 3 ENGINE SHUT DOWN DUE TO OIL LOSS AND LOW COMPRESSION ON NR 3 CYLINDER. REPLACED NR 3 ENGINE NR 3 CYLINDER DUE TO CRACKED HEAD. 2L74 4R4 R A781 5E8 20030922000092003092200009CE 2003 9 22 HYI2003F00009 120030724A809799103971 RELAY CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO STARTER FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01812AN678 402C0229 AIRCRAFT LOST ELECTRICAL POWER, AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC FOUND RT START RELAY FAILED IN CLOSED POSITION, CHANGED RELAY, STARTER AND BATTERY. AIRCRAFT RETURNED TO SERVICE. 1L72 3O3 O A7CE E8CE 20030922000172003092200017EA 2003 9 22 HNAA0300040 120030811A32345352011 SELECTOR DHAV DHC8 DHC8311 1386006EA MLG INOPERATIVE A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07342EN18191 395 NOSE GEAR CYCLED WHEN GEAR WAS RETRACTED. REPLACED GEAR SELECTOR. 2H72 4T RTA13NM 20030922000292003092200029NM 2003 9 22 2003UALA00626 120030813A2751 INDICATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE TE FLAP INOPERATIVE A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29311UA 23672 RETURN TO FIELD DUE TO A FLAP POSITION INDICATOR. FLAP SYSTEM MALFUNCTION WAS CAUSED BY INTERNAL FAILURE OF THE FLAP POSITION INDICATOR. THE INDICATOR WAS REPLACED AND THE FLAP SYSTEM WAS TESTED FOR PROPER OPERATION. THE INDICATOR PASSED A BENCH TEXT, HOWEVER AMTS BELIEVED THE BRUSH TENSION WAS TOO HIGH. UPON DISASSEMBLY, THE BEARING AND SHAFT WERE FOUND MISALIGNED. THIS RESULTED IN THE BRUSHES CONTACTING THE SLIP RING AT AN ANGLE APPROXIMATELY 20 DEGREES FROM PERPENDICULAR. 2L72 4F4 FRTA16WE E2GL 20030922000332003092200033NM 2003 9 22 AWXA200300943 120030805A5315D53070011 FLOORBEAM AIRBUSA319 A319132 3930340NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y1292 FLOORBEAM AT FR 16. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOORBEAM FR 16 TO FR 18; FABRICATED A NEW SECTION OF FLOORBEAM AND 2 EACH REPAIR SPLICES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-15, PG. 207-212, FIG. 202. 2L72 4F RTA28NM 20040303000402004030300040NE 2004 3 3 BAQA091386 220031010A73140292105230X PUMP BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE FUEL SYSTEM INOPERATIVE B BAQAK NONE O OTHER ININSP/MAINT 1 EA03117UP522 7508 FUEL PUMP PRODUCING LOW OIL PRESSURE. REPLACED WITH SERVICEABLE UNIT. 02/03/2004 1G72 3U3 UNCH13EU E19EU 20040301000662004030100066SO 2004 3 1 GLBA2003147 120031107A526012040696001 DOOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE AIRSTAIR OPEN A GLBAA UNSCHED LANDING W INADEQUATE Q C TOTAKEOFF 1 NM03299UX 120299 AIRSTAIR DOOR PANEL OPEN ON T/O, INSP AIRSTAIR DOOR CLOSING ACCESS PANEL AND FUSELAGE. NO DAMAGE NOTED, SECURED PANEL ACCESS COVER AS REQD IAW EMM 52-12-00. 2L72 4T4 TRTA31SO E20NE 20040301001772004030100177NM 2004 3 1 GTIA030561 120030718A7160 ACCOUSTIC LINER DOUG MD80 MD83 3023681NM NR 1 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 FTW - FOUND THE NR 1 ENGINE HAS APPROX 12 SQUARE INCHES OF ACCOUSTIC LINING MISSING AFT OF THE NR 4 BEARING STRUT AT THE 7 O'CLOCK POSITION. COMPLIED WITH EA 7230-0305. (M) 2L72 4F RT 20040304000422004030400042EA 2004 3 4 TZR2004F00003 220031210A8520 CRANKCASE PIPER PA60 PA60601 7106010NM LYC O540 IO540S1A5 41532EA NR 5 CYL CRACKED E TZRAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW05601TE9357 1516 610264102 L1878748A PILOT REPORTED A HARD DOWNDRAFT (REPORTED THAT HE HIT HIS HEAD ON CEILING) APPROX 20 SECONDS LATER NR 2 ENGINE LOST POWER AND HE SHUT THE ENGINE DOWN. HE LANDED WITHOUT INCIDENT. INSPECTION OF THE ENGINE IN HANGAR REVEALED A CRACKED CASE UPPER SIDE BY NR 5 CYLINDER. AT TEAR DOWN THE ENGINE SHOP REPORTED THAT THE NR 5 CONNECTING ROD HAD LET GO. 1M72 3O3 ORTA17WE 1E4 20040304000582004030400058EU 2004 3 4 TRB2004F00002 120031225A3233D228470004 ACTUATOR AEROSPATR72 ATR72212 8680945EU PWA 120 PW120 NE NLG INTERMITTENT A TRBAO OTHER J WARNING INDICATION LDLANDING 1 SO21342AT9830 N160 345 WHEN SELECTING GEAR DOWN FOR LANDING, THE NOSE GEAR UNLOCKED BUT DID NOT EXTEND. CREW RECYCLED THE GEAR UNTIL GEAR CAME DOWN AND LOCKED. REMOVED AND REPLACED NLG ACTUATOR CYLINDER ASSEMBLY. 2H72 4T4 TRTA53EU E20NE 20040304001412004030400141WP 2004 3 4 ASAA0380821 120031209A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 SEA - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 6-10. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001552004030400155WP 2004 3 4 ASAA0380720 120031113A335041B004AD07 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A K NONE L NO TEST ININSP/MAINT 1 NM01960AS 53074 DURING 15K CHECK, FOUND 1ST CLASS EMERGENCY FLOOR TRACK LIGHTS ILLUMINATE WHEN EXTERNAL POWER IS TURNED OFF, EVEN THOUGH EMERGENCY SWITCH REMAINS IN 'OFF' POSITION. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001632004030400163WP 2004 3 4 ASAA0380823 120031211A3397 CONNECTOR GULTON DOUG DC9 DC983 3022083WP LIGHT MODULE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01961AS 53075 SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE NEAR AFT GALLEY. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040329001802004032900180NM 2004 3 29 2003UALA00951 120031130A2910 LINE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE HYD SYSTEM FAILED A UALAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29657UA 27112 C-HYDRAULIC SYSTEM QTY SLOWLY DECREASING. LEFT MAIN GEAR HYDRAULIC LINE FOUND LEAKING AT UPPER TRUNNION LOCATION. RESERVICED CENTER SYSTEM TO NORMAL. RYNGLOK REPAIR ACCOMPLISHED ON BRAKE HYDRAULIC LINE/TUBE. SPECIFIC HYDRAULIC LINE AND CAUSE OF LEAK NOT IDENTIFIED. SERVICE BULLETIN 767-32-0162 IS RELATED TO HYDRAULIC LEAK EVENTS IN THIS AREA. DUE TO LACK OF PART IDENTIFICATION, UNABLE TO DETERMINE IF THIS EVENT RELATED TO SPECIFIC SERVICE BULLETIN APPLICATION. 2L72 4F4 FRTA1NM E24NE 20040401000152004040100015NM 2004 4 1 USAA030328 120031218A5347 SEAT TRACK BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US55490 24894 CLT - FOUND SEAT TRACK CORRODED 2 INCHES, STATION 1437 AND RBL 88. REMOVED CORROSION, ALODINED, PRIMED AND PAINTED PER SRM 53-00-52 FIG 101. (M) 2L72 4F RTA1NM 20040401000312004040100031WP 2004 4 1 ASAA0380398 120030421A5320993658045 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT INTERCOSTAL BETWEEN 1287 AND 1309 HAS THREE CRACKS IN RADIUS. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040401000382004040100038WP 2004 4 1 ASAA0380403 120030421A5542 SKIN DOUG DC9 DC982 3022082WP RUDDER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RUDDER HAD DENT JUST ABOVE LOWER HINGE. REMOVED DAMAGED AND HOT BONDED REPAIR DOUBLER PER SRM. (M) 2L72 4F A6WE 20040401000432004040100043NM 2004 4 1 AALA20031202 120031101A335060030451 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21623AA 24581 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS AT ROWS 17 TO 23 INOPERATIVE. REMOVED AND REPLACED M10800 BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401000632004040100063NM 2004 4 1 UIEA200300072 120031229A7603 CONTROL CABLE BOEING747 747228F 1384895NM NR 3 THROTTLE ICED A UIEAE ENGINE SHUTDOWN F FLT CONT AFFECTED DEDESCENT 1 EA15536MC 21576 NR 3 ENGINE THROTTLE UNABLE TO SELECT IDLE DURING DESCENT. THROTTLE STUCK AT 4 DEGREE THROTTLE ANGLE AND 80 PERCENT N1. ENGINE SHUTDOWN USING ENGINE FAILURE/SHUTDOWN CHECKLIST. PERFORMED INSPECTION IAW 73-21-01 AND 76-11-03 THRUST CONTROL CABLE INSPECTED ALL NORMAL. SUSPECT MOISTURE ICING BUILD INSIDE. RUN ENGINE ALL NORMAL. (M) 2L74 4F A20WE 20040401000642004040100064NE 2004 4 1 HALA0301146 220031202A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 1 MAKING METAL A HALAK NONE O OTHER ININSP/MAINT 1 WP13485HA 55130 DURING MCD INSPECTION OF NR 1 ENGINE, FOUND LARGE AMOUNTS OF METAL FUZZ ON CHIP DETECTOR. NR 1 ENGINE ASSEMBLY REMOVED PER HAL M144-717 STANDARD PRACTICE. (M) 2L72 4F4 FTRA6WE E00061EN 20030922000432003092200043EU 2003 9 22 RAIA00308209 120030807A27201415501517 ARM JETAIRJETSTMJETSTM4101 1500501EU RUDDER BROKEN A RAIAO OTHER O OTHER NRNOT REPORTED 1 CE03570HK 41089 DURING ROUTINE MAINTENANCE CHECK FOUND RUDDER STOP ARM BROKEN AND RUDDER STOP LYING IN THE TAIL CONE AREA. SUBSEQUENT FLEET INSPECTION IDENTIFIED TWO ADDITIONAL RUDDER STOP ARMS BENT. REMOVED AND REPLACED RUDDER STOP ARMS. 2L72 4T RTA41NM 20030915000652003091500065SW 2003 9 15 HEEA088951 120030902A5260212075418107 ACTUATOR CLARK 1000 1000CLARK 2230102SW STEP INOPERATIVE B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO LT STEP WON'T COME UP. REPLACED STEP ACTUATOR. 1Q71 3R 2A6 20030915000672003091500067SW 2003 9 15 HEEA088963 120030801A243523046020 STARTER GEN BELL 212 212 1181420SW ENGINE DAMAGED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03102PH858 30899 STARTER GEN WILL NOT ENGAGE. ARCING BRUSHES. 1G71 4U H4SW 20030916001052003091600105WP 2003 9 16 GTIA030638 120030727A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND RIGHT AFT LAVATORY INBOARD ASSEMBLY FLOOR PANEL DAMAGED AND DISBONDED. REPAIRED FLOOR PANEL. (M) 2L72 4F RTA6WE 20030917000242003091700024CE 2003 9 17 A8J2003F00001 120030501A3246LM29749 BEARING BFGOODRICH CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP NLG WHEEL LACK OF LUBE E A8JAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW09926CR 5904P 6500008 NOSE WHEEL BEARING FAILURE. PROBABLE CAUSE: LACK OF GREASE ON BEARING. RECOMMENDATION, HEAVIER GREASE THAT WILL NOT SPIN OUT OF BEARING OR INTERNAL GREASE SEALS. 2L72 4F4 F A9NM E6WE 20030917000302003091700030WP 2003 9 17 03FDEA01151 120030725A5753NRC60551 FLAP TRACK DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 NR S 21 COMPLY WITH E.A.8-5750-70986A. WINGS-INBOARD FLAP-INBOARD TRACK SUPPORT BRACKETS CORROSION REPAIR. CLOSING ACTION ON 07/22/03 COMPLIED WITH EA 8-5750-70986A. 2L73 4F A22WE 20030918000482003091800048NM 2003 9 18 GAIA03033SP 120030719A5313 STRINGER BOEING727 7272J0 138407ENM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS WEB CRACKED AT STRINGER 16L FASI N/R 35753. FABRICATED REPAIR DOUBLER FROM MATERIAL 7075-T6 .063 PO NR 9911488 DIM 3.5 INCH BY 4 INCH. INSTALLED REPAIR IAW B727 SRM 51-40-2. (M) 2L73 4F RTA3WE 20030918000822003091800082WP 2003 9 18 A4J2003F00002 120030608A3350AD4002P BATTERY DOUG DC9 DC931 3022065WP OVERWING LIGHT DISCHARGED A A4JAO OTHER O OTHER NRNOT REPORTED 1 SO35933JK 48159 DURING DAILY WALK-AROUND AT PIE, MAINTENANCE FOUND EMERGENCY LIGHTS ON BOTH SIDES FORWARD MOST OVER WING EXCAPE HATCHES INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES FOR THE FORWARD LIGHTS OF EACH OVER WING EXCAPE PATH, IAW DC9 33-53-0, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 20030919000612003091900061NM 2003 9 19 IU62003F00032 120030523A2760654494710 HOUSING BOEING BOEING737 737* NM ACTUATOR DAMAGED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 4723 PIN HOLES IN HOUSING ASSEMBLY. WEAK MATERIAL, EROSION. USE THE IMPROBED HOUSING WHICH IS MADE OF STEEL. (NR 177675) 2L72 4F RTA16WE 20030919001362003091900136EU 2003 9 19 9015070103 120030701A2110590008 COMPRESSOR SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE AIR CONDITIONER INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP07350R 283 9015 9667 AIR CONDITIONER COMPRESSOR, INOPERATIVE. 1G71 3U3 U H9EU E00054EN 20030922000442003092200044EU 2003 9 22 RAIA00308210 120030812A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK 41040 EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. SECURED CONNECTOR TO PATH LIGHT STRIP 2L72 4T RTA41NM 20030922000632003092200063EU 2003 9 22 MALA030375 120030815A2750OFF8532 POTENTIOMETER SAAB SF340 SF340A 7850100EU TE FLAPS INOPERATIVE A MALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL1579XJ 340A079 DURING CLIMBOUT ON FLIGHT NR 3321, AT LEVEL FLIGHT THE FLAPS BEGAN UNCONTROLLED MOVEMENT CAUSING THE AIRCRAFT TO PITCH. THE FLAP MOVEMENT WAS CONFIRMED WITH THE FLAP INDICATOR. AIR RETURN TO MSP MAINTENANCE WITH FLAPS 0 DEG, SIMULATED AIR LOAD ON FLAPS AND NOTED FLAPS EXTENDED UNCOMMANDED THEN RETRACTED. COMPLETED FLAP CONTROL RIGGING IAW AMM 27-51-00-5. RE-RIGGED FLAP CONTROL BOX AND FLAP POSITION TRANSDUCERS. REPLACED LT FLAP POSITION POTENTIOMETER 7DE PN/ON 8565M1, PN/OFF 8532, SN/ON 94040026, SN/OFF 250 IAW AMM 27-53-05 DUE TO LOOSE SHAFT. 2L72 4T RTA52EU 20030922000692003092200069NM 2003 9 22 AWXA200300946 120030805A5320D53230281200 ANGLE AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK A 1/2) CRACK WAS FOUND ON RT UPPER SIDE OF ANGLE, AFT OF FR 34, UNDER PANEL 192AT. MAINTENANCE REMOVED CRACKED ANGLE; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG C3 D53230281; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 22, 23, 25, & 28, FIG. 8, 9, & 12. 2L72 4F RTA28NM 20030922000732003092200073NM 2003 9 22 AWXA200300950 120030804A5320D5347047700800 PROFILE AIRBUSA319 A319132 3930340NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON LT TRANSITION PROFILE IN AFT CARGO COMPARTMENT BETWEEN FR 56 AND FR 58. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED TRANSITION PROFILE BETWEEN FR 56 AND FR 58; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12, & 22. 2L72 4F RTA28NM 20030922000742003092200074NM 2003 9 22 AWXA200300951 120030805A5315D5347112420100 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF RT OUTBOARD FLOOR SHEAR PLATE WEB BETWEEN FR 69 AND FR 70, AFT OF FLOORBEAM Y1792. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED SHEAR PLATE WEB BETWEEN FR 69 AND FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE WEB; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 8-12, FIG. 2 & 3. 2L72 4F RTA28NM 20030917000572003091700057EU 2003 9 17 DXTA200300109 120030902A2751 INDICATOR BRAERO1000 BAE1251000A 1500104EU TE FLAP ERRATIC E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07540QS 85335 ON TAKEOFF ROLL FLAP POSITION INDICATOR HAD ERRATIC MOVEMENT, FROM THE SET POSITION OF 15 DEGREES THEN MOVED TO 20 DEGREES THEN TO 25 DEGREES AND THEN BACK TO 15 DEGREES, FOLLOWED IMMEDIATELY BY IT MOVING BACK TO 25 DEGREES AND THEN CONTINUING DOWN TO 45 DEGREES. ABORTED AT APPROX. 100 KTS. - FOUND FLAP TRANSMITTER BAD, REMOVED AND REPLACED FLAP TRANSMITTER IAW BAE 1000 MM CHAPTER 27-50-40 OPS CHECKED GOOD. 2L72 4F RTA3EU 20030918000182003091800018NM 2003 9 18 03FDEA01515 120030911A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 N01551 CRACKED STRINGER BS 720 STR 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720 STR 5R PER SRM 51-30-02. 2L73 4F RTA3WE 20030918000292003091800029NM 2003 9 18 GAIA03034SP 120030719A5311 FRAME BOEING727 727* NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 560 HAVE DENTS INTO THE RADIUS AT STRINGER 16R AND STRINGER 8R FASI N/R 35743. CUT OUT DAMAGED AREAS, FABRICATED DOUBLERS FROM MAT 7075-T6 .063 PO NR 9912495, DIM 7 INCH BY 4.5 INCH AND 10 INCH BY 3 INCH. INSTALLED DOUBLERS IAW B727 SRM 53-10-4 FIG 1 AND 51-30-2. (M) 2L73 4F RTA3WE 20030918000512003091800051 2003 9 18 DL76S030706 420030730A2565 SQUIB BOEING767 767332 1382001NM ESCAPE SLIDE FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27134DL 25123 EMERGENCY ESCAPE SQUIBS DO NOT TEST - REPLACED SQUIB BATTERY PACKS 2L72 4F RTA1NM 20030918000522003091800052NE 2003 9 18 DLM88030707 220030731A7261JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 MALFUNCTIONED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27913DE37976 49956 718129 ON CLIMB, LT ENG OIL TEMP HI - ATB TO ATL - REPLACED ENGINE 2L72 4F4 FRTA6WE E9NE 20030918000722003091800072EU 2003 9 18 MALA030347 120030722A2930HE832731 SWITCH BAC 146 AVRO146RJ85A1500097EU HYD TEMP MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15506XJ E2314 DURING FLIGHT 3478, GREEN HYDRAULIC SYSTEM TEMP HIGHT LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE REPLACED HIGH TEMP SWITCH.P/N HE83273-1 S/N OFF 1046TW S/N ON 1067TW OPS CHECK GOOD FOR HI TEMP. 2H74 4F RTA49EU 20030918000832003091800083NM 2003 9 18 A4J2003F00003 120030715A33500105606003SMI MODULE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE ROW 17 SHORTED A A4JAO OTHER O OTHER NRNOT REPORTED 1 SO3511FQ 49759 DURING (A) CHECK PIE MAINTENANCE FOUND FLOOR EMERGENCY LIGHT AT ROW 17 WHITE LIGHT NOT WORKING. REMOVED AND REPLACED LAMP MODULE IAW MD80 MM 33-53-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA6WE E2EA 20030919000252003091900025NE 2003 9 19 NACA20030104 220030802A7421URHB32E SPARK PLUG DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE FOULED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F461 461 533265 33553 NR 4 ENGINE , NR 17 CYLINDER BOTH PLUGS SHOWING LOW COMPRESSION PATTERNS. REPLACED NR 2 & NR 9 CYLINDER FRONT & REAR PLUGS DUE TO FOULING. CHECKED GOOD. 2L74 4R4 R A781 5E8 20030919001292003091900129NE 2003 9 19 NACA20030109 220030815A8530356996 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 11 MAKING METAL A NACAED ENGINE SHUTDOWN RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 AL03993301118 1118 43576 P33821 NR 3 ENGINE DOUBLE SHORTED SECONDARY, ENGINE SHUT DOWN ON TAXI-IN. REPLACED NR 3 ENGINE ASSY. DUE TO NR 11 CYLINDER RING LAND/PISTON FAILURE. METAL IN SCREEN. 2L74 4R4 R A781 5E8 20030919001342003091900134NM 2003 9 19 PCAA0308099 120030813A3397 DIODE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT FAILED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13839EX 226 DURING ROUTINE MAINTENANCE VISIT FOUR RED FLOOR EMERGENCY LIGHTS AT ROW 4 WERE FOUND TO BE INOPERATIVE. ALSO, FORWARD AND AFT LEFT AND RIGHT UPPER SIDEWALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. EMERGENCY LIGHTING SYSTEM WAS TROUBLESHOT AND A BURNT WIRE ON A POST CONNECTOR FOR POSITION 500 POWER SUPPLY WAS FOUND. POWER SUPPLY WAS REPLACED AT POSITION 500. ALSO FOUND WAS A BAD DIODE FOR THE RED FLOOR LIGHTS. DIODE WAS REPLACED. ALL EMERGENCY LIGHT BATTERIES WERE REPLACED DURING TROUBLESHOOTING. OPERATIONAL CHECK OF ALL EMERGENCY LIGHTS WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030919001372003091900137EU 2003 9 19 9015070403 120030704A2432RG350 BATTERY SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE RT BAGGAGE INOPERATIVE E S4WAK NONE L NO TEST NRNOT REPORTED 1 WP07350R 228 9015 9667 AIRCRAFT BATTERY, UNSERVICEABLE. 1G71 3U3 U H9EU E00054EN 20030919001522003091900152EU 2003 9 19 AWXA200300932 120030803A5320D53974644002 PROFILE AIRBUS320 A320232 3930326EU CARGO DOORWAY BUCKLED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK THE FORWARD CARGO COMPARTMENT LT PROFILE WAS FOUND BUCKLED IN 2 AREAS AT FR 30. MAINTENANCE REMOVED DAMAGED SECTION OF PROFILE FR 30; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND 2 EACH REPAIR SPLICES; INSTALLED REPAIR PART IAW AWA E.R. 26-5320-03154-SS1. 2L72 4F RTA28NM 20030919001532003091900153EU 2003 9 19 AWXA200300933 120030801A5320D53475765202 SILL AIRBUS320 A320232 3930326EU PAX DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON TWO SCREW HOLES AT THE AFT SIDE OF DOOR SILL OF AFT BULK CARGO CUTOUT FR 61-62. MAINTENANCE BLENDED OUT CORROSION IN TWO AREAS, MATERIAL LOSS EXCEEDED 50 PERCENT; CUTOUT DAMAGED AREA FR 61-62; FABRICATED 2 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49, PG. 221-222, FIG. 203. 2L72 4F RTA28NM 20030922001222003092200122EA 2003 9 22 COMA0370026 120030819A5610NP1393226 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A COMAO OTHER O OTHER APAPPROACH 1 SO01331CA2084 10061 FLIGHT 5742 COPILOTS SIDE WINDOW SHATTERED. REPLACED WINDOW. 2L72 4F RTA21EA 20030922001242003092200124EU 2003 9 22 0301573248 120030816A3213201375008030 STRUT AIRBUS320 A320212 3930322EU MLG FAILED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01348NW336941523 410 GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM MSP. RECEIVED SHOCK ABSORBER FAULT MESSAGE. COMPLIED WITH COM, BURNED DOWN FUEL, AND LANDED UNEVENTFULLY AT MSP. CHECKED RIGHT MLG STRUT PRESSURE AND FOUND 1250 PSI WITH 3-3/32 INCHES OF EXTENSION. JACKED AIRCRAFT AND STRUT WOULD NOT EXTEND. REMOVED RIGHT MLG STRUT, REPLACED SEALS, REASSEMBLED STRUT, AND SERVICED PER AMM. GEAR SWING CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20031006001792003100600179NM 2003 10 6 03FDEA01647 120030926A572064833830 STIFFENER BOEING727 727200 138407ENM BS 171.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 RT WING FUEL TANK RIB, OB VERTICAL STIFFENER CRACKED, UPPER END, WS 171.5 BETWEEN STR 9 AND STR 10. REMOVED DAMAGED VERTICAL RIB STIFFNER AT WS 171.5 BETWEEN STR 9 & 10 RIGHT. DRILLED UP & INSTALLED NEW STIFFNER (P/N 65-8338-30) IAW SRM 51-30-5, SRM 51-30-2 & SRM 51-40-4. 2L73 4F RTA3WE 20030923000612003092300061WP 2003 9 23 DHL2003604657 120030530A5730 PLATE DOUG DC8 DC873F 302199FWP LT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBD FLAP LOWER PLATING HAS DENTS ON SEVERAL SPOTS BETWEEN STA XW 5.000 AND XW115.250. PERFORMED MAJOR REPAIR IAW EODHL-030568, ED-3293. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030568, ED-3293. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL (2024-T3 AL0.063) IAW EODHL-030568, ED-3293. CLEANED, TREATED, AND PRIMED NEW SKIN PANEL IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON LT WING INBD FLAP LOWER SURFACE, STA XW 5.000 - XW 115.250 WITH NEW FASTENERS IAW EODHL-030568, ED-3293, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000662003092300066WP 2003 9 23 DHL2003604716 120030614A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 B-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR IN IT. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1, SRM 52-4-1 PG 4, BOEING MESSAGE DHL-CVG-0079H. REMOVED EXTERNAL SKIN WITH INTERIM REPAIR IN IT IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SKIN (7075-T6M AL0.063) IAW SRM 52-1-0 PG 1, SRM 52-4-1 PG 4, BOEING MESSAGE DHL-CVG-0079H. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030923000702003092300070WP 2003 9 23 DHL2003604768 120030624A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT ELEVATOR UPPER PLATING OTBD SECTION SHOWS INTERIM REPAIR AND CORROSION FROM STA XE 246.000 TO XH 285.000. REMOVED FASTENERS, REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PANEL, CLEANED, TREATED AND PRIMED AREA. FABRICATED NEW SKIN PANEL (2024-T3 AL0.032) IAW EODHL-030523, ED-3404. CLEANED, TREATED AND PRIMED NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON RT ELEVATOR UPPER PLATING OTBD SECTION STA XE 246.000 TO XH 285.000) USING NEW FASTENERS IAW EODHL-030523, ED-3404, SRM 51-1-21 PG 1. SEE N/R 4037 FOR WEIGHT AND BALANCE. FOR REMOVAL AND RE-INSTALLATION SEE J/C 8-27-60-016. 2L74 4F RT4A25 20030923000762003092300076WP 2003 9 23 DHL2003604766 120030529A53403616789N ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD ACCESSORY COMPT FITTING ATTACHING FLOORBEAM TO FRAME AT STA 35.000 L-21R CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030922000072003092200007EU 2003 9 22 MALA030373 120030810A3350 LIGHT BAC 146 AVRO146RJ85A1500097EU CABIN DETACHED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15503XJ E2310 EMERGENCY TRACK LIGHTING LIGHT OUT WITH TRACK DETACHED. MEM MAINTENANCE INSTALLED TRACK IN EMERGENCY LIGHT TRACK OPS CHECKS OK. 2H74 4F RTA49EU 20030922000262003092200026NM 2003 9 22 2003UALA00623 120030812A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA 29239 E/E COMPT, BS 246 FLOORBEAM, STIFFENER CRACKED AT FWD FACE OF BEAM, RBL 16, AT PULLEY CLOSURE RIB ATTACH POINT. 2L72 4F4 FRTA1NM E24NE 20030922001002003092200100SO 2003 9 22 S4EA2003001 120030709A2910LSM1491 O-RING PIPER PA32 PA32R300 7103213SO LYC O540 IO540K1A5 41532EA HARTZLHCC3Y HCC3YR GL HYD VALVE LEAKING E S4EAO OTHER O OTHER NRNOT REPORTED 1 AL01753112149 32R7680291 L1795348AC DY4916B VALVE THAT IS ACTUATED BY NOSE GEAR DRAG BRACE DEPRESSING A PLUNGER WHEN NOSE GEAR IS RETRACTED. HYDR ACT TO CLOSE SEC NOSE GEAR DOOR. WHEN GEAR IS EXTENDED, PLUNGER EXTENDS RELEASING PRESSURE ON ACTUATOR, DOOR IS SPRING LOADED TO OPEN. PROBLEM OCCURRED WHEN ORING ON PLUNGER FAILED DUMPING HYDR FLUID OVERBOARD, MANUAL EXTENSION OF LANDING GEAR. PLUGER REMAINED IN DEPRESSED POSITION THUS TRAPING PRESSURE IN DOOR ACTUATOR WHICH HELD DOOR CLOSED. THIS CAUSED DIFFICULTY IN MANUALLY EXTENDING GEAR AND EXCITED PILOT. VALVE WHICH FAILED AND SECONDARY (FWD) NOSE GEAR DOOR ARE BOTH PARTS INSTALLED VALVE WITH STC SA00953AT. VALVE WAS REMOVED AND REPLACED, SYSTEM TESTED SATISFACTORY AND AC RETURNED TO SERVICE. 1L71 3O3 O A3SO 1E4 5 CP25EA 20030922001102003092200110CE 2003 9 22 KC82003F00002 120030729A7500261903728 SEAL LEAR 35 36A 5170603CE GARRTTTFE731TFE731* 01518WP BLEED DUCT LEAKING E KC8AO OTHER O OTHER NRNOT REPORTED 1 GL2371CK 035 PILOT REPORTED RIGHT BLEED AIR LIGHT ALUMINATED DURING FLIGHT. FOUND SEALS WERE LEAKING AND CAUSED THE RT BLEED ANNUNCIATOR TO LIGHT. PYLON AREA WAS INSPECTED IAW MM. SEALS WERE CHANGED, ENGINE RUNS PERFORMED AND DUCT LEAK CHECKED. 2L72 4F4 F A10CE E6WE 20030922001232003092200123EA 2003 9 22 WVE2003F00011 120030801A5312MM6703618200500 PRESSURE BLKHD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE FUSELAGE CRACKED A WVERO OTHER O OTHER NRNOT REPORTED 1 EA09501MJ1910 10047 THE LT AND RT SIDE WEBS OF THE AFT PRESSURE BULKHEAD ARE CRACKED AROUND HYDRAULIC UNION CUT OUTS AT FS 1098.2, BETWEEN STRINGERS 8 AND 9. CAUSE: STRESS. THE CRACKED AREAS WERE CUT-OUT AND REPAIR PARTS (MACHINED FITTINGS) WERE INSTALLED IAW REO. 2L72 4F4 FRTA21EA E15NE 20030923000732003092300073WP 2003 9 23 DHL2003604763 120030611A53405755032113 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT T-FITTING ATTACHING NR 4 TRACK TO FLOORBEAM AT STA 1704.000 CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 ATM NR P0201387, DWG 5755032. REMOVED CORRODED FITTING IAW SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED NEW FITTING IAW DWG 5755032. PERFORMED LIQUID PENETRANT INSPECTION IAW DC8 NDT SPM PART 08-00-02/06. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED FITTING WITH NEW FASTENERS IAW SRM 51-3-1 PG 1. 2L74 4F RT4A25 20030923000872003092300087WP 2003 9 23 DHL2003604784 120030610A55235644440 SKIN DOUG DC8 DC873F 302199FWP ELEVATOR TAB DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT ELEVATOR CONTROL TAB UPPER SKIN DELAMINATED. REMOVED AND REPLACED LT ELEVATOR CONTOL TAB IAW MM 27-30-2 PG 201-204. REFER TO N/R 0531 FOR OPS CHECK. 2L74 4F RT4A25 20030923001022003092300102WP 2003 9 23 DHL2003604698 120030528A53403754918U1 ATTACH FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT. FITTING CRACKED 1.000 AT STA. 1170.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, SRM 51-1-20D PG.9,21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG.9. 2L74 4F RT4A25 20030923001042003092300104WP 2003 9 23 DHL2003604761 120030611A5330 SKIN DOUG DC8 DC873F 302199FWP FUSLAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 EXTERIOR SKIN WITH DENT AND WEAR OUT OF LIMITS BETWEEN STA. 120.000 AND STA. 210.000, L-20L TO L-22L. PERFORMED MAJOR REPAIR IAW EODHL-030528, ED-3316. REMOVED FASTENERS AND EXISTING REPAIR DOUBLER. BLENDED OUT AFFECTED AREA. PERFORMED EDDY CURRENT INSPECTION. FABRICATED (09) FINGER DOUBLERS (7075-T6 AL0.040) AND (04) FILLERS (7075-T6 AL0.071) AND (1) DOUBLER (7075-T6 AL0.080) IAW EODHL-030528, ED-3316. CLEANED, TREATED AND PRIMED FINGER DOUBLERS AND FILLERS AND DOUBLER AND AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FINGER DOUBLERS AND FILLERS AND DOUBLER WITH NEW FASTENERS IAW EODHL-030528, ED-3316. 2L74 4F RT4A25 20030923001102003092300110WP 2003 9 23 DHL2003604709 120030617A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 "A" CARGO DOOR EXTERNAL SKIN HAS (2) INTERIM REPAIR AND DENTS AT SEVERAL SPOTS. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG.1, SRM 52-4-1 FIG.2 BOEING MESSAGE DHL-CVG 03-00079H. REMOVED DAMAGED SKIN IAW SRM 51-1-21 OG,1, SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN (7075-T6 AL0.050) IAW SRM 52-1-0 PG.1, SRM 52-4-1 FIG.2, BOEING MESSAGE DHL-CVG-03-00079H. CLEANED, TREATED AND PRIMED NEW SKIN IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-20D PG.9, SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030923001342003092300134NM 2003 9 23 03FDEA01328 120030808A5754ARC0154501 HINGE FITTING DOUG MD11 MD11 3023602NM TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING, IB FLAP, OB FORWARD HINGE FITTING HAS HYD ACTUATOR'S UPPER OB MOUNT LUG HOLE WITH TOOL MARK. LT WING IB FLAP OB HINGE (WING SIDE) HYD ACTUATOR ATTACHMENT OB HOLE REPAIRED IAW CMM 57-44-07. 2L73 4F RTA22WE 20030923001362003092300136EU 2003 9 23 030387 120030823A5523 RETAINER SAAB SF340 340B 7860101EU TRIM TAB BEARINGDAMAGED A MALAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL15360PX 340B220 FLUTTER IN ELEVATOR STARTED DURING DESCENT. SLOWED TO 180 KNOTS AND IT STOPPED. SPEED BACK TO 185 AND IT STARTED AGAIN WITH FLAPS 15. FLUTTERED AGAIN AT 165 KONTS. SAME INDICATION WITH AP ON OR OFF. TRIMS APPEARED NORMAL. REPLACED TRIM TAB INBOARD BEARING RETAINER 2L72 4T RTA52EU 20030923001492003092300149NM 2003 9 23 03FDEA01415 120030901A5753ARC70541 SUPPORT FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING- O/B FLAP VANE SUPPORT FITTING NR 2 FROM I/B ATTACH HOLE FOUND CORRODED. CORROSION ON LT WING, O/B FLAP VANE SUPPORT FITTING #2 FROM I/B ATTACH HOLE REMOVED AND REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-73298. 2L73 4F RTA22WE 20030923001522003092300152EU 2003 9 23 AWXA200300977 120030823A2843SIC5059040107 COMPUTER AIRBUS320 A320231 3930325EU FUEL QTY FALSE INDICATIONA AWXACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP28620AW262811922 052 ON TAKEOFF AT PHX EN ROUTE FOR MCO RECEIVED ECAM WARNING FOR RT OUTBOARD FUEL TANK LOW TEMPERATURE, FUEL PAGE INDICATES 54 DEGREES, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INITIATED MEL 28-40-09, COND. 2 (TANK LO TEMP CAUTION ON ECAM). ON 08/24/2003 IN PHX MECHANIC FOUND PREVIOUS LEG FAULTS OF: LEG 1 FQIC 3QT, FLSCU1 9QJ & FLSCU2 7QJ. REMOVED AND REPLACED FUEL QUANTITY INDICATION COMPUTER (FQIC) IAW AMM 28-42-34, BITE CHECK WAS GOOD. 2L72 4F RTA28NM 20030923001592003092300159WP 2003 9 23 AALA20030858 120030817A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217548A 53030 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE IDENTIFIER BETWEEN FORWARD GALLEY AND FIRST CLASS ARROWS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030923001622003092300162 2003 9 23 AALA20030705 420030626A25655A33073 SLIDE BOEING737 737823 13844BZNM CABIN DEPLOYED A AALAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SW21921AN 29522 FORWARD ENTRY ESCAPE SLIDE PARTIALLY DEPLOYED WHEN THE DOOR WAS OPENED, DID NOT INFLATE. GIRT BAR FELL OUT AS DOOR WAS BEING OPENED. REPLACED FORWARD ENTRY ESCAPE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030923001762003092300176WP 2003 9 23 AALA20030837 120030806A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21286AA 49298 DURING OVERNIGHT MAINTENANCE, AFT STAIRWELL AND TAILCONE EMERGENCY LIGHT ASSEMBLIES INOPERATIVE. REPAIRED WIRE L795D16 AND REPLACED CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030923001772003092300177 2003 9 23 AALA20030818 420030731A3416ALT7008 ALTIMETER BOEING767 767323 1385205NM COCKPIT FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21348AN 33087 CAPTAIN ALTIMETER IS STUCK AT 100, AFTER TAKEOFF FLAG WAS DISPLAYED OFF FLAGG NOT DISPLAYED ON GROUND. REPLACED CAPTAINS BARO ALTIMETER PER MM 34-13-01, SYSTEM CHECKS NORMAL. (M) 2L72 4F RTA1NM 20030923001812003092300181 2003 9 23 AALA20030841 420030804A3417HG280D80 COMPUTER DOUG DC9 DC982 3022082WP COCKPIT MALFUNCTIONED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21237AA 49253 AFTER TAKEOFF, FIRST OFFICERS AIRSPEED PEGGED AND ALTIMETER WENT TO 10000 ERRONIOUS SPEED INFORMATION. AIRCRAFT RETURNED MCO AND LANDED WITHOUT INCIDENT. REPLACED NR 2 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030923001892003092300189 2003 9 23 AALA20030493 420030422A2330 VIDEO DISPLAY BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21903AN 29505 EN ROUTE ORD-LAX, SMOKE WAS COMING OUT OF THE FORWARD CABIN VIDEO MONITOR AND CONTROL BOX. THE SMOKE STOPPED AFTER THE CIRCUIT BREAKERS WERE PULLED. THE VIDEO SYSTEM WAS TURNED OFF IMMEDIATELY. LANDED LAX WITHOUT INCIDENT. REPLACED FORWARD LEFT VIDEO MONITOR AND CONTROL UNIT. RESET CIRCUIT BREAKERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030924000042003092400004GL 2003 9 24 03FDEA01387 220030826A72109035M39P003 SUPPORT DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 1ENG STATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 COMPLY WITH E.A. 8-7210-72270- ENGINE-BASIC- FAN STATOR SUPPORT HALF, CRACK REPAIR. ENGINE-BASIC FAN STATOR SUPPORT HALF CRACK REPAIR. CLOSED ON 08/25/2003 FEDEX . 2L73 4F4 F A22WE E23EA 20030924000072003092400007NE 2003 9 24 5300063003 220030630A726030J200102 SEAL CESSNA560 560XL 2076702CE PWA 545 PW545A NE GEN DRIVE LEAKING E S4WAK NONE K FLUID LOSS ININSP/MAINT 1 WP07613GY452 5605300 LT AND RT ENGINE AC GENERATOR DRIVE SEALS LEAKING OIL. 2L72 4F4 FRTA22CE E00059EN 20030924000122003092400012NE 2003 9 24 197032103 220030321A7210 SEAL PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE REDUCTION GB LEAKING E S4WAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP07613NA129 197 PCEPR0052 OIL LEAKING FROM REDUCTION GEARBOX AREA. 1L71 3T4 TRTA78EU E26NE 20030924000142003092400014NM 2003 9 24 DLM88030721 120030804A3350RPS1 CHARGER DOUG MD88 MD88 3023688NM EMERGENCY LIGHT UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27908DE 53417 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE, 31DE THRU 38DE. REPLACED BATTERY CHARGER. 2L72 4F RTA6WE 20030924000162003092400016 2003 9 24 DLM88030723 420030805A25653961899501 LANYARD DOUG MD88 MD88 3023688NM ESCAPE SLIDE BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27901DL 49532 1R SLIDE LANYARD CABLE WORN THROUGH (BROKEN) AT GIRT BAR ATTACH POINT - REPLACED SAME. 2L72 4F RTA6WE 20040304001372004030400137NM 2004 3 4 ASAA0340357 120031210A33508100022601 LIGHT BOEING737 7374Q8 138447QNM ROW 13-15 INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01784AS 28199 SAN PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING FOUND INOPERATIVE AT ROW 13-15. REATTACHED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA16WE 20040304001472004030400147NM 2004 3 4 ASAA0340349 120031201A3397 CONNECTOR BOEING737 7374Q8 138447QNM EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 ANC - DURING LINE CHECK, FOUND NEAR ROW 14-19 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, REPLACED LAMP, SYSTEM OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20031211001002003121100100NM 2003 12 11 SWAA032473 120031106A323369355005 ACTUATOR BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAK NONE J WARNING INDICATION CLCLIMB 1 SW29365SW 26576 DURING INITIAL MLG RETRACTION, RT MLG RED LIGHT IND WOULD NOT EXTINGUISH, CYCLED GEAR ANG LIGHT REMAINED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20031211001062003121100106WP 2003 12 11 AALA20031327 120031121A3242 BRAKE DOUG DC9 DC982 3022082WP RT MLG MALFUNCTIONED A AALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW21479AA 49654 ORD T2301/21 EN ROUTE ORD-DFW ON TAKEOFF RIGHT BRAKE DRAGS AND TEMPERATURE ROSE TO 200 DEGREES. ABORTED TAKEOFF. REPLACED RIGHT WHEEL, BRAKE AND SLEEVE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001192003121100119NM 2003 12 11 AALA20031313 120031123A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 MIA EMERGENCY LIGHT OVER SEAT 10D INOPERATIVE. REPLACED MID SECTION BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031211001242003121100124 2003 12 11 AALA20031404 420031206A256531393109 SLIDE BOEING757 757223 1384957NM CABIN FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21187AN 32381 DFW UNSUCCESSFUL SLIDE DEPLOYMENT. DIRECTIONAL EXIT HANDRAIL DID NOT FULLY INFLATE AND DID NOT STAY INFLATED. REPLACED RIGHT HAND MAIN OFFWING EVACUATION SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031211001262003121100126WP 2003 12 11 AALA20031348 120031130A335060030451 BATTERY DOUG DC9 DC982 3022082WP COCKPIT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21577AA 53154 DFW COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY FOR COCKPIT OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210000182003121000018SO 2003 12 10 C2XA03SH468 120031123A532014522549001 ANGLE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712528 145504 SHV-DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031210000582003121000058NM 2003 12 10 QXEA200301516 120031203A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX - TRACK 3 TOP FLANGE HAS AREAS OF LIGHT PITTING AT STATION X510.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20031210000632003121000063NM 2003 12 10 SWAA032615 120031127A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031210000722003121000072NM 2003 12 10 03FDEA01967 120031121A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 1 I/B CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031210000912003121000091EA 2003 12 10 COMA0360515 120031128A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01781CA 7312 FLIGHT 5215 CEILING EMERGENCY LIGHT, 2ND FROM FRONT IS INOPERATIVE. DEFERRED INOPERATIVE EMERGENCY LIGHT PER MEL 33-51-01. 2L72 4F RTA21EA 20031210002172003121000217WP 2003 12 10 UPS03841549 120031023A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 1750 LONGERON 15L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN 1730 TO 1750 IAW SRM 53-2-2 FIG 10 2L74 4F RT4A25 20031210002242003121000224WP 2003 12 10 UPS03841554 120031024A53203754041U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 BANANNA FITTING IS CRACKED AND CORRODED BEYOND LIMITS STATION 320 AT LONG 26L. REMOVED AND REPLACED FITTING IAW DWG 3754041 AND SRM 51-1-20D 2L74 4F RT4A25 20031211000142003121100014WP 2003 12 11 ABXA030417 120031105A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 L1 DOOR FORWARD UPPER CORNER HAD A B-CLASS REPAIR IAW ABX JC NEA 53100102-002. REMOVED EXISTING REPAIR, PERFORMED X-RAY INSPECTION TO CUTOUT. NO CRACKS NOTED. FABRICATED DOUBLERS AND FILLER IAW DC-8 SRM 53-2-0. INSTALLED REPAIR AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21, 51-1-21A, AND REA D853-48060MR. 2L74 4F 4A25 20031211000252003121100025 2003 12 11 COMA0370048 420031106A2210 DAMPER CNDAIRCL600 CL6002C10 1390015EA AUTOPILOT SYS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01368CA 10075 FLIGHT 5666 DURING TAKEOFF ROLL RECEIVED A YAW DAMPER NR 2 MESSAGE. REJECTED TAKEOFF AND AIRCRAFT RETURNED TO THE GATE. CYCLED POWER TO THE LEFT AND RIGHT AUTOMATIC FLIGHT CONTROL SYSTEM. 2L72 4F RTA21EA 20040401000702004040100070NM 2004 4 1 AALA20031118 120031005A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21698AN 26980 SFO - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROW 25D. SECURED CONNECTOR FOR SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031211000872003121100087NM 2003 12 11 03FDEA01894 120030924A2613 WARNING LIGHT BOEING727 727200 138407ENM OVERHEAT SYS ACTIVATED A FDEAO OTHER J WARNING INDICATION CRCRUISE 1 SO25492FE 21530 LOWER AFT BODY OVERHEAT LIGHT AT CRUISE. FOLLOWED QRH- RIGHT PACK SECURED, RIGHT (NR 3) BLEED SECURED, LIGHT WENT OUT. RAN ALL 3 ENGINES AT 40 PERCENT N1 FOR APPROX 25 MINUTES (WITH AIRSTAIRS RETRACTED) NO LEAKS DETECTED AND COULD NOT GET LIGHT. OK FOR CONTINUED SERVICE. REQUEST CREW TO ISOLATE WITH BODY OVERHEAT SELECTOR ROTARY SWITCH IF PROBLEM REOCCURS ENT BY: 102445 RPT BY: 102445. 2L73 4F RTA3WE 20031211000902003121100090NM 2003 12 11 03303410 120031030A3250 STEERING SYS DORNERDO32 DO328300 NM NLG MALFUNCTIONED A VTZAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27410FJ 3165 DURING TAXI THE AIRCRAFT EXPERIENCED A MOMENTARY LOSS OF STEERING ACTUATING FORCE DURING TURNING. AIRCRAFT RETURNED TO GATE AND DEPLANED PASSENGERS NORMALLY. 2H72 4T RTA55NM 20031211000932003121100093EU 2003 12 11 03FDEA01883 120031106A3230D221270005 DAMPER AIRBUS310 A310 EU RT MLG MALFUNCTIONED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25423FE 281 REPEAT WRITE-UP, GEAR WOULD NOT RETRACT. AFTER BLOCK IN, LOOKED AT GEAR TRIM CYLINDERS AGAIN AND THE RIGHT GEAR TRIM CYLINDER WAS POPPED AGAIN. PARTS ORDERED, ADDED MPN D22127000-5 CPN 3212339 QTY 1 DAMPER MSN 862119. REMOVED AND REPLACED RIGHT MLG BOGIE BEAM PITCH DAMPER IAW A310-200 SUPP AMM 32-11-15-4, AND EA 6-3210-74064. NO DISCREPANCIES NOTED. 2L72 4F RTA35EU 20031211000972003121100097EA 2003 12 11 COMA0360494 120031112A5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT ARCED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01798CA10298 7348 FLIGHT 6835 DURING CRUISE FLIGHT, NOTICED ARCING EMANATING FROM THE LEFT CORNER OF THE LEFT WINDSHIELD. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT CVG. REPLACED THE LEFT WINDSHIELD. 2L72 4F RTA21EA 20031211001022003121100102CE 2003 12 11 AMWA66 120031024A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07174YV UE174 5 CRACKS LOCATED ON THIS RIB. 2LT AND 3 RT LOCATED AT STRINGER TO RIB INTERSECTIONS ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-38, 101-640000-42, 101-640000-46. LT STRINGER P/N 101-640000-39, 101-640000-37 2L72 4T RTA24CE 20031211001142003121100114NM 2003 12 11 AALA20031392 120031206A2560 BATTERY PACK BOEING777 777223 1385213NM FLASHLIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21773AN 29583 ORD LEFT SIDE FIRST CLASS FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK IN LEFT SIDE FIRST CLASS FLIGHT ATTENDANT EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031211001152003121100115WP 2003 12 11 AALA20031393 120031206A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217531A 49923 SEA EMERGENCY CEILING LIGHTS AT AFT GALLEY DOOR BACK TO SEATING FROM AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK B5-107. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031209002712003120900271NM 2003 12 9 03FDEA01888 120031107A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 WHILE DRILLING UP NEW SEAT TRACK AT BS 1050 LBL 25 DRILLED THROUGH RADIUS OF FLOORBEAM REPAIR ANGLE. 2L73 4F RTA3WE 20031210000352003121000035NM 2003 12 10 AALA20031308 120031121A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21385AM 27059 SFO FORWARD EMERGENCY LIGHT AT SEAT 5H INOPERATIVE. RECONNECTED LOOSE FORWARD EMERGENCY LIGHT CONNECTOR AT SEAT 5H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031210000682003121000068NM 2003 12 10 03FDEA01971 120031121A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT OUTBOARD FLAP FOUND INBOARD HINGE PIVOT HINGE HOLE NR 4 O/B SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031210000872003121000087NM 2003 12 10 SWAA032620 120031128A53106545785 WINDOW FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND RT NR 2 PAX WINDOW FRAME CRACKED. REMOVED AND REPLACED RT NR 2 PAX WINDOW FRAME PER SRM AND ERO. 2L72 4F RTA16WE 20031210001732003121000173NM 2003 12 10 CALA0300607 120031020A5320BAC1496377 PANEL BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 RT TRANS PANEL CORRODED BETWEEN STA 727 AND 767. FABRICATED AND INSTALLED NEW TRANS PANEL IAW SRM 53-60-53. 2L72 4F4 FRTA16WE E2GL 20031211000562003121100056NM 2003 12 11 C1HA200394038 120031108A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 868 - 950+9 LBL 24.75 HAS LIGHT CORROSION AND WORN AREAS. 2L73 4F A3WE 20031211000672003121100067WP 2003 12 11 UPS03841560 120031027A574456423421 HINGE FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 LEFT WING FLAP HINGE STATION 3 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D, 51-1-21, 51-3-0. 2L74 4F RT4A25 20031211000602003121100060NM 2003 12 11 QXEA200301416 120031110A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR OUT OF POSITION A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX 4046 RDD- ON FLIGHT 2310 AIRCRAFT RETURNED TO FIELD DUE TO FORWARD BAGGAGE WARNING LIGHT ILLUMINATED WHILE CLIMBING THROUGH FL 180. AIRCRAFT LANDED SAFELY. UPON INSPECTION FOUND DOOR HANDLE PROTRUDING .25 INCH. RECYCLED HANDLE, HANDLE FLUSH WITH DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031211001272003121100127WP 2003 12 11 AALA20031349 120031130A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21577AA 53154 DFW FORWARD ENTRY AISLE GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD ENTRY AISLE GALLEY OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001332003121100133WP 2003 12 11 AALA20031338 120031128A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21407AA 49318 SFO CENTER AND AFT POSITIONS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ABOVE ROW 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001452003121100145WP 2003 12 11 AALA20031271 120031115A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21580AA 53157 DFW AFT VAULT DOOR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT VAULT DOOR OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001542003121100154WP 2003 12 11 AALA20031371 120031203A33501001191 FLASHLIGHT DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21203AA 49145 SAT HOLD DOWN TAB FOR L1 DOOR EMERGENCY LIGHT/FLASHLIGHT BROKEN. REPLACED L1 DOOR EMERGENCY LIGHT/FLASHLIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001762003121100176EA 2003 12 11 ASOA03532 120031023A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT FLOOR LIGHT AND COVER FORWARD OF THE PASSENGER DOOR WAS FOUND DAMAGED AND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT FOOL FLIGHT ASSEMBLY FORWARD OF THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031211001922003121100192EU 2003 12 11 USAA030246 120031030A5320D53112811520200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT CORRODED 1.9 INCH LONG BY .80 INCH WIDE, MAX DEPTH .047 INCH, FRAME 16, -Y 70. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EA 94782 AND SRM 51-42-11. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20031211001932003121100193NM 2003 12 11 USAABB03208 120031004A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19621AU 27200 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031212000212003121200021NM 2003 12 12 SWAA032417 120031031A53156545410 FLOORBEAM BOEING737 737317 138447PNM FUSELAGE SEVERED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER T-CHORD SEVERED AT BS 660, BL-0, WL 207. REPAIRED PER SWA EA. 2L72 4F RTA16WE 20031212000242003121200024NM 2003 12 12 SWAA032420 120031031A335065C27093 LENS BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29747SA 29799 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT LENS OUT IN OVERHEAD NEAR SEAT ROW 13 ABC. REINSTALLED LIGHT LENS PER MM. 2L72 4F RTA16WE 20031212000292003121200029NM 2003 12 12 SWAA032425 120031102A2121215201 GASPER FAN BOEING737 7373H4 1384600NM A/C BAY OVERHEATED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29625SW 27701 FUMES IN PAX CABIN. REMOVED AND REPLACED A/C GASPER FAN PER MM. 2L72 4F RTA16WE 20031212000392003121200039NM 2003 12 12 CALA0300639 120031112A5320 ATTACH ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND ATTACH ANGLE AND FLANGES ON ATTACH ANGLE CORRODED AT FORWARD SIDE APB STA 1016, BL 0. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW EA 5310-04045. 2L72 4F RTA16WE 20031212000402003121200040NM 2003 12 12 CALA0300640 120031112A5753 SKIN BOEING757 757224 1384958NM T/E FLAP GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2729124 27565 INSPECTION FOUND RT TRAILING EDGE O/B MAIN FLAP NOSE SKIN GOUGED AT WBL 558. THE FLAP NOSE SKIN WAS REPAIRED IAW SRM 57-53-01 FIGURE 202. 2L72 4F RTA2NM 20031212000412003121200041NM 2003 12 12 CALA0300641 120031113A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT STA 314, S27L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2L72 4F RTA16WE 20031212000482003121200048NM 2003 12 12 DHL2003753007 120031113A3350 BATTERY BOEING727 727223 1384074NM CABIN DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01753DH 22468 MAIN ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED WORN BATTERIES. OPS CHECKED SERVICEABLE IAW M/M 25-60. OK FOR CONTINUED SERVICE. 2L73 4F A3WE 20031212000542003121200054EU 2003 12 12 00121 120031111A2131133007 CONTROLLER AMD FALC20FALCON 2720302EU CABIN PRESSURE FAILED E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05158TW 158 PILOT REPORTED UNABLE TO CONTROL PRESSURIZATION AFTER DEPARTURE FROM KYIP, RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED CABIN PRESSURE CONTROLLER OPS CK GOOD AT THIS TIME. 2L72 4F A7EU 20031212000562003121200056EU 2003 12 12 MALA030493 120031111A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15527XJ E2352 DURING A C2 INSPECTION, TIMCO FOUND NR 2 MAIN CABIN SEAT RAIL WAS EXFOLIATED. REPLACED SEAT RAIL AND INSTALLED REPAIR PER EO A53026. 2H74 4F RTA49EU 20031212000592003121200059NM 2003 12 12 AWXA200301419 120031021A5320654681282 WEB BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON SHEAR WEB AT FORWARD INBOARD SIDE END OF CREASE BEAM BS 995.5, LBL 43.5. MAINTENANCE REMOVED CRACKED SHEAR WEB AT FORWARD INBOARD SIDE END OF CREASE BEAM BS 995.5, LBL 43.5; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-22 SRM 51-30-02 FIG 2, 3, 7, & 11 AND SRM 51-30-05, FIG 2. 2L72 4F RTA16WE 20031212000602003121200060EU 2003 12 12 AWXA200301420 120031113A33501012881 LIGHT AIRBUS320 A320232 3930326EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28653AW 1003 SAN - EEL - DURING INSPECTION FOUND A SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOPERATIVE IN FORWARD RT PASSENGER CABIN. MAINTENANCE REMOVED AND REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT IN THE FORWARD RT PASSENGER CABIN, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031212000612003121200061EU 2003 12 12 AWXA200301421 120031113A5210FE240221001 DIAPHRAGM AIRBUS320 A320231 3930325EU R-1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 PHX - EES - DURING 8-DAY INSPECTION THE R-1 DOOR ASSIST BOTTLE WAS FOUND AT ZERO PSI. MAINTENANCE REMOVED AND REPLACED R-1 DOOR ASSIST BOTTLE DIAPHRAGM IAW 52-10-00, OPERATIONAL AND LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20031212000712003121200071WP 2003 12 12 03FDEA01919 120031117A5230 STRUCTURE DOUG DC10 DC1010 3022110WP CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 COMPLY WITH EA 8-5310-73850 FUSELAGE - CORROSION ON LWR AFT CARGO DOOR LWR RAIL EXTENSION. CLOSING ACTION ON 11/17/03, ON N/R S00011. COMPLIED WITH EA 8-5310-73850. 2L73 4F A22WE 20031212000752003121200075SO 2003 12 12 MASA200300439 120031106A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07838MJ 145384 ASH 2767 CLT-MEM. EMERGENCY LIGHTS INOP. MX RELAMPED. OP CHECKS GOOD. 2L72 4T RTT00011AT 20031212000772003121200077EU 2003 12 12 MALA030497 120031110A242131342003 GENERATOR SAAB SF340 340B 7860101EU LT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15364PX 340B262 DURING FLIGHT 3016, LEFT AC GENERATOR FELL OFF LINE. AIR RETURN TO DTW. MAINTENANCE REPLACED LEFT AC GENERATOR P/N 31342-003, S/N ON -96099; S/N OFF-97087 PER TECH REP'S ADVICE IAW SAAB MM. ALL CHECKS ARE GOOD AT THIS TIME. 2L72 4T RTA52EU 20031212000882003121200088NM 2003 12 12 SWAA032405 120031101A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND 2 EA FLOORBEAM UPPER CHORDS CORRODED AT BS 987, RBL 43, WL 208, AND BS 1016, RBL 36, WL 208. REPAIRED FLOORBEAMS PER SRM. 2L72 4F RTA16WE 20031212000892003121200089NM 2003 12 12 SWAA032406 120031101A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 867 TO BS 887, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031212000932003121200093NM 2003 12 12 SWAA032410 120031031A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C1 CHECK, FOUND RT KEEL BEAM EXTERNAL SKIN CRACKED BETWEEN MLG W/W CUTOUTS. REPAIRED KEEL BEAM SKIN PER SRM. 2L72 4F RTA16WE 20031210001582003121000158WP 2003 12 10 AALA20031316 120031123A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 DFW) ONE OF THREE TAILCONE EMERGENCY ILLUMINATION LIGHTS INOPERATIVE. REPLACED BATTERY FOR TAILCONE EMERGENCY ILLUMINATION LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031210002052003121000205NM 2003 12 10 03FDEA01226 120030805A5210 FRAME BOEING727 7272S2F 1384O81NM ENTRY DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 N 1099 WHILE WORKING CARD N 281 FND CRACK ON LT LWR CORNER WEB OF ENTRY DOOR. REMOVED AND REPLACED FRAME. 2L73 4F A3WE 20031210002232003121000223WP 2003 12 10 UPS03841553 120031108A532037558272N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 280 AT LONG 29R BANANA FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755827 AND SRM 51-1-20D 2L74 4F RT4A25 20031211000012003121100001EA 2003 12 11 COMA0360482 120031105A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01526CA 7824 FLIGHT 5664 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING TAXI OUT, AIRCRAFT RETURNED TO THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20031211000182003121100018WP 2003 12 11 ABXA030424 120031025A5534 STRUCTURE DOUG DC8 DC861 3021952WP VERTICAL STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 VERTICAL STABILIZER REAR SPAR RIGHT CHORD HAD CORROSION AT ZR 270. REMOVED CORROSION AT REAR SPAR RIGHT CHORD, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48068MR. 2L74 4F 4A25 20031211000272003121100027WP 2003 12 11 ABXA030430 120031027A523059101419 PAN DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 FORWARD LOWER CARGO DOOR OUTER PAN HAD CRACK INDICATION IN RADIUS AT AFT LOWER STOP. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM. 2L72 4F A6WE 20031211001232003121100123WP 2003 12 11 AALA20031385 120031204A2822 PUMP DOUG DC9 DC982 3022082WP FUEL SYSTEM DEFECTIVE A AALAO OTHER O OTHER CRCRUISE 1 SW217537A 49991 MSP T1510/04 EN ROUTE MSP-DFW AFT CENTER FUEL TANK BOOST PUMP POPPING CIRCUIT BREAKER. RETURNED MSP AND LANDED WITHOUT INCIDENT. PLACARDED AFT CENTER FUEL TANK BOOST PUMP PER MEL. 2L72 4F A6WE 20031211001472003121100147WP 2003 12 11 AALA20031273 120031115A335060030451 BATTERY DOUG DC9 DC982 3022082WP AFT AIRSTAIRS DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21580AA 53157 DFW AFT OVERHEAD AIRSTAIRS CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT AIRSTAIRS CATWALK EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001532003121100153NM 2003 12 11 AALA20031370 120031203A3350 CONNECTOR BOEING767 767323 1385205NM CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21360AA 24041 MIA EMERGENCY LIGHT AT 12B INOPERATIVE. RESEATED HARNESS CONNECTOR FOR EMERGENCY LIGHT AT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031211001622003121100162WP 2003 12 11 AALA20031055 120030922A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21419AA 49331 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 18 THROUGH 22. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031211001642003121100164WP 2003 12 11 ABXA030462 120031205A1430 FASTENER DOUG DC8 DC861 3021952WP COCKPIT LOOSE A ABXAK NONE O OTHER NRNOT REPORTED 1 GL23843AX 46017 CAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD WAS LOOSE AND INTERMITTENTLY INOPERATIVE. TIGHTENED LOOSE MOUNTING HARDWARE FOR CAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD REF DC-8 MM 20-00. 2L74 4F 4A25 20031211001652003121100165WP 2003 12 11 ABXA030452 120031126A3260 PROXIMITY SWITCH DOUG DC9 DC931 3022065WP NLG OUT OF ADJUST A ABXAO OTHER N FALSE WARNING DEDESCENT 1 GL23943AX 47528 UPON FIRST GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE AND RED GEAR UNSAFE LIGHT WAS LIT. CYCLED GEAR AND RECEIVED 3 GREEN. FOUND GAP AT NOSE GEAR DOWNLOCK PROX SWITCH EXCESSIVE. ADDED SHIMS AS NEEDED IAW DC-9 MM 32-60-01-2-0201. OPS CHECKED GOOD IAW DC-9 MM 32-60-00-2-101. 2L72 4F A6WE 20031211001782003121100178NM 2003 12 11 USAABB03206 120031102A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19603AU 22198 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20031211001832003121100183NM 2003 12 11 USAABB03202 120031030A3350873203193REV9 TRANSMITTER BOEING757 7572B7 1384964NM CABIN DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU 27123 CLT - EMERGENCY LIGHTS IN ZONE C FLASH INTERMITTENTLY IN FLIGHT. REPLACED AFT CABIN EMERGENCY LIGHT TRANSMITTER. (M) 2L72 4F RTA2NM 20031211001942003121100194EU 2003 12 11 USAA030245 120031031A5320D5347217220300 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND ATTACHMENT HOLED CORRODED 5.3 INCH LONG BY 2.0 INCH WIDE, DEPTH .028, FRAME 64-66, -Y 1114 FLOOR SUPPORT. DEFECTIVE PART REPLACED WITH IDENTICAL APRT NR PER SRM 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500-10. (M) 2L72 4F RTA28NM 20031212000142003121200014NM 2003 12 12 SWAA032435 120031104A53116545815 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 348.5, STR 6L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031212000182003121200018NM 2003 12 12 SWAA032439 120031104A53116546554 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, WL 157, RBL 20 TO RBL 26. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20031212000262003121200026NM 2003 12 12 SWAA032422 120031103A521065299946 GUIDE ARM BOEING737 7373H4 1384600NM L1 DOOR WORN A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29397SW 27691 AIR TURNBACK, PRESSURIZATION LEAK AT L1 DOOR. REMOVED AND REPLACED L1 DOOR UPPER GUIDE ARM PER MM. 2L72 4F RTA16WE 20031212000352003121200035SO 2003 12 12 C2XA03BT106 120031109A3350110049 CHARGER EMB 145 EMB145 3260210SO CABIN FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712967 145133 EWR---DURING PREFLIGHT INSPECTION, FOUND RIGHT FRONT EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSY IAW EMB145 MM 33-50-04 AND EXTERNAL EMERGENCY LIGHT ASSY (PART NUMBER 1317) IAW EMB145 MM 33-50-10. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20031212000372003121200037EU 2003 12 12 YENA200336 120031113A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN FAILED A YENAK NONE O OTHER ININSP/MAINT 1 EA15533JB7337 1652 DURING EMERGENCY LIGHT SYS TEST EPSU (L) FAILED. REMOVED & REPLACED (L) CABIN EPSU (11WL) IAW AMM 33-51-38. EMERGENCY LIGHT SYS TEST OK. 2L72 4F RTA28NM 20031212000632003121200063SO 2003 12 12 C2XA03SH455 120031116A532014521725001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031212000642003121200064SO 2003 12 12 C2XA03SH456 120031116A532014525381003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV- DURING C-CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 65 AND 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031211000622003121100062WP 2003 12 11 ABXA030437 120031107A251056410321 SEAT DOUG DC8 DC863F 302198FWP COCKPIT DEFECTIVE A ABXAK NONE O OTHER TOTAKEOFF 1 GL23814AX 504 46041 FLIGHT ENGINEER'S SEAT VERTICAL HOLD WOULD NOT HOLD WHILE SEAT WAS FACING FORWARD. FELL 3 TIMES DURING TAKEOFF AND INITIAL CLIMB. REPLACED SYSTEMS ENGINEER SEAT PER ABX DC8 AMM 25-11-06-2-001. LUBED AND OPS CHECKED GOOD. 2L74 4F 4A25 20031211001412003121100141WP 2003 12 11 AALA20031389 120031205A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21411AA 49322 DFW FORWARD LEFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD LEFT OVERWING EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001522003121100152WP 2003 12 11 AALA20031369 120031203A3350AAP3274A CHARGER DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2176200 53290 DFW AFT LAV AREA CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR AFT LAV AREA CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031212001062003121200106NM 2003 12 12 SWAA032440 120031105A335079012 LENS BOEING737 7372T4 1384492NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS MISSING AT ROW 19. INSTALLED LENS PER MM. 2L72 4F A16WE 20031212001072003121200107NM 2003 12 12 SWAA032441 120031105A53306551625 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031212001212003121200121 2003 12 12 SWAA032505 420031112A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031212001222003121200122NM 2003 12 12 AWXA200301428 120031114A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28828AW8263 1552 SEA - EEL - DURING 4-DAY CHECK THE LT MID CABIN EMERGENCY POWER SUPPLY UNIT FAULTED DURING EMERGENCY PATHWAY LIGHT OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED LT MID CABIN EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031212001262003121200126NM 2003 12 12 AWXA200301432 120031028A575369737595 STIFFENER BOEING737 7373G7 1384595NM T/E FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK A 1 INCH CRACK WAS FOUND ON NR 3 FLAP TRACK FIXED FAIRING AFT END INBOARD STIFFENER AT WBL 185. MAINTENANCE REMOVED CRACKED STIFFENER WBL 185; FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 11. 2L72 4F RTA16WE 20031212001352003121200135WP 2003 12 12 AALA20031214 120031105A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21216AA 49167 DEN - DURING OVERNIGHT MAINTENANCE, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 24, 25 AND 25 INOPERATIVE. REPLACED BATTERY PACK ABOVE ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001382003121200138WP 2003 12 12 AALA20030934 120030902A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21405A 49316 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE IN AFT CABIN. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001422003121200142WP 2003 12 12 AALA20031205 120031102A3350AAP3274A CHARGER DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21964TW 53614 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY B5-27 AND B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031212001432003121200143WP 2003 12 12 AALA20031215 120031104A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21234AA 49181 DFW - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD EMERGENCY ESCAPE DOOR LIGHTS INOPERATIVE. REPLACED FORWARD EMERGENCY ESCAPE DOOR LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001522003121200152WP 2003 12 12 GTIA030851 120031010A5320 PLATE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND TWO CORRODED FLOOR PLATES AT FS 160, 18 INCHES LBL. FABRICATED FLOOR PLATE. TWO FLOOR PLATES ARE REMOVED AND INSTALLED ON SAS W/C B00104 18-R-15. (M) 2L72 4F A6WE 20031212001632003121200163WP 2003 12 12 AALA20030954 120030903A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21597AA 53287 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT NUMEROUS ROWS. REPLACED THREE BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031212001652003121200165WP 2003 12 12 AALA20030926 120030829A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21598AA 53288 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT SEAT ROW 25 AND 26. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031212001732003121200173EA 2003 12 12 COMA0370039 120031019A2701601R901012 CONTROL COLUMN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE COCKPIT BINDING A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01340CA2767 10062 FLIGHT 5877 AILERON CONTROLS WERE BINDING DURING FLIGHT. LOOSENED AND THEN RETORQUED CO-PILOTS CONTROL YOKE. NO DEFECTS NOTED. 2L72 4F4 FRTA21EA E15NE 20031215000022003121500002EA 2003 12 15 COMA0360457 120031014A3040601R5153811 DIODE CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01962CA 7123 FLIGHT 5771 RT WINDSHIELD HEAT CAUTION MESSAGE. REPLACED THE DIODE BOARD ASSY. 2L72 4F RTA21EA 20031215000092003121500009NM 2003 12 15 AWXA200301445 120031106A532069353521 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN TIE CLIP AT BS 663.75, STR 10 LT. MAINTENANCE REMOVED CRACKED TIE CLIP AT BS 663.75, STR 10 LT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW SRM 51-40-02 PG 1, 11, 38 & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031215000122003121500012NM 2003 12 15 QXEA200301426 120031114A6123 SWITCH DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09353PH 496 PDX- ON FLIGHT 2135 AUTO FEATHER TEST DOES NOT TEST PROPERLY. WHEN THE AUTO FEATHER SWITCHES ARE PULLED UP, BOTH PROPELLERS DROP DOWN INTO THE PROHIBITED RANGE AND THE UP TRIM DOES NOT ACTIVATE AND NOTHING HAPPENS WITH THE AUTO FEATHER. LUBRICATED AUTO FEATHER SWITCHES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000142003121500014NM 2003 12 15 QXEA200301428 120031114A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8401 1390041NM NR 1 MALFUNCTIONED A QXEAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 NM09400QX 4030 SEA- ON FLIGHT 2390 NR 1 AUTO FEATHER FAILED ON INITIAL FLIGHT OF THE DAY. COMPLIED WITH PROPELLER AUTO FEATHER AND UPTRIM SYSTEM TEST. NO PARTS REPLACED. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000332003121500033NM 2003 12 15 SWAA032510 120031113A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10L. REMOVED AND REPLACED SPLICE PER SRM. 2L72 4F RTA16WE 20031215000382003121500038NM 2003 12 15 HNAA030069 120031116A32518800135 FUSE DHAV DHC8 DHC8102 2809003NM NLG BROKEN A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07943HA9739 6340 167 UPON GEAR RETRACTION THE NOSE GEAR FAILED TO RETRACT AND MAIN GEAR DOORS REMAINED OPEN. THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD. FOUND STEERING FUSE BROKEN AND CABLE SUPPORT BROKEN DUE TO OVER STEERING. PERFORMED TOWING FUSE BREAKAGE INSPECTION PER MM 32-50-00. REPAIRED AND REPLACED DAMAGED PARTS AS NECESSARY. 2H72 4T RTA13NM 20031215000412003121500041NM 2003 12 15 03FDEA01916 120031114A5311 FRAME BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 FOUND FRAME CRACKED AROUND OPEN HOLE BS 1070 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1070, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 & FED EX EA 7-5310-55117. 2L73 4F RTA3WE 20031215000442003121500044NM 2003 12 15 2003UALA00795 120031021A335058807 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29312UA 23673 AFT GALLEY EEL STRIP INOP. REPLACED AFT GALLEY EEL STRIP. 2L72 4F4 FRTA16WE E2GL 20031215000582003121500058NE 2003 12 15 2003UALA00841 220031103A7520 ROD END BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 3 ENGINE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29127UA 28813 NR 3 ENG TURBINE CASE COOLING (TCC) CABLE FWD SUPPORT LINK ROD END WORN OUT AND DISCONNECTED. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT LINK ROD END. 2L74 4F4 FRTA20WE E24NE 20031211000162003121100016WP 2003 12 11 ABXA030419 120031029A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 R1 FORWARD SERVICE DOOR LOWER AFT CORNER HAD CRACK INDICATION ON EXTERNAL SKIN. CUT OUT DAMAGED AREA, PERFORMED HFEC AFTER DAMAGE REMOVAL. NO CRACKS NOTED. FABRICATED DOUBLERS AND FILLER, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21, AND REA D853-48054MR. 2L74 4F 4A25 20031211000712003121100071NM 2003 12 11 03313402 120031109A2121AE1716D02 COOLING FAN DORNERDO32 DO328300 NM CABIN FAILED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27402FJ 3147 DURING PREFLIGHT PROCEDURES CREW REPORTED SMOKE IN THE LAVATORY AND NOTED A HX FAN FAIL. THE HX FAN WAS CONFIRMED AS THE CAUSE OF SMOKE AND WAS REPLACED. 2H72 4T RTA55NM 20031211001092003121100109NM 2003 12 11 AALA20031397 120031207A3350S283T0143 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 LAX SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24B THROUGH 35B INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24B THROUGH 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031211001502003121100150WP 2003 12 11 AALA20031276 120031116A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21598AA 53288 STL INSEAT EMERGENCY LIGHTS AT SEAT 13 INOPERATIVE. REPLACED ROW 13 OVERHEAD EMERGENCY LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031211001912003121100191EU 2003 12 11 USAA030252 120031101A5320D5361019720140 STRAP AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND STRAP CORRODED 1.5 INCH BY 2 FT AREA, STRAP ON FLOOR SUPPORT PANEL AT R-1 DOOR. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. (M) 2L72 4F RTA28NM 20031215000622003121500062SO 2003 12 15 C2XA03BT108 120031116A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO LANDING GEAR FAULTY A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2713538 145527 EWR---CO2255, CREW REPORTED LANDING GEAR AIR/GROUND FAILURE. MAINTENANCE REMOVED AND REPLACED LGEU IAW EMB145 MM 32-32-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20031212000762003121200076SO 2003 12 12 MASA200300441 120031107A2560P207003001 FLASHLIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07839MJ 145416 ASH 2681. CLT CABIN FWD FLASHLIGHT INOP. MX REPLACED THE FLASHLIGHT. 2L72 4T RTT00011AT 20031212000802003121200080EU 2003 12 12 MALA030494 120031106A79977292533681 WIRE HARNESS SAAB SF340 340B 7860101EU LT ENGINE FAULTY A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15423XJ 340B423 DURING FLIGHT 2923, NR 1 PROP OIL TEMP OVER 100 DEGREES. AIR RETURN TO MEM. MAINTENANCE REPLACED LEFT ENGINE WHITE HARNESS P/N 7292533-681 IAW AMM PBM 71-00-02. PERFORMED ALL REQUIRED RUNS IAW AMM 71-50-00-0. OPS CHECK GOOD. A/C GOOD FOR CONTINUED SERVICE. 2L72 4T RTA52EU 20031212000922003121200092NM 2003 12 12 SWAA032409 120031101A32336977496 ACTUATOR BOEING737 7372H4 138448CNM LT MLG FAULTY A SWAAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SW29085SW 22826 AIR TURNBACK, LT MLG UNSAFE LIGHT WOULD NOT EXTINGUISH, CYCLED THE LANDING GEAR AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LT MLG TRANSFER VALVE AND LT MLG RETRACT ACTUATOR PER MM. 2L72 4F A16WE 20031210000942003121000094EU 2003 12 10 MALA030511 120031129A2160782602 CONTROL VALVE SAAB SF340 340B 7860101EU A/C SYSTEM FAULTY A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15452XJ 340B452 DURING FLIGHT 3245, RT TEMP UNCONTROLLABLE IN AUTO AND MANUAL. DUCT OVERTEMP IN BOTH MODES. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED DUAL TEMP CONTROL VALVE P/N 78260-2, SN/ON 9807169. 2L72 4T RTA52EU 20031210000962003121000096EU 2003 12 10 MALA030516 120031120A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION PERFORMED BY TIMCO, LAKE CITY, FL, CABIN AFT RT FRAME STA 686 CHAFED/GOUGED. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53152. A/C RELEASE DATE 12/2/03. REFER TO 409 NR 1206073 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20031210001042003121000104NM 2003 12 10 03FDEA01994 120031127A5710 STOP FITTING DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73349, TRAILING EDGE AND TRAILING EDGE DEVICES. LT & RT OUTBOARD FLAP SECONDARY UP STOP REPAIR. 2L73 4F RTA22WE 20031210001592003121000159NM 2003 12 10 AALA20031269 120031114A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21774AN 29581 DFW BUSINESS CLASS SEATS EMERGENCY LIGHTS INOPERATIVE. REPLACE BUSINESS CLASS SEATS BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTT00001SE 20031211000092003121100009 2003 12 11 AWXA200301375 420031106A3414 INDICATOR BOEING757 7572S7 1384962NM COCKPIT FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28902AW 23322 SJD - ABORTED TAKEOFF - FLT 0052 - ON TAKEOFF AT SJD EN ROUTE FOR PHX THE CAPTAINS AIRSPEED INDICATOR FAILED, REJECTED TAKEOFF AT 85 KTS. MAINTENANCE PERFORMED BACKFLOW OF STATIC DRAIN LINES, NO MOISTURE NOTED, PERFORMED AIR DATA COMPUTER BITE TEST, SYSTEM OPERATES NORMALLY PER BMM 34-12-00 PG 110-113. WHEN AIRCRAFT ARRIVED IN PHX MAINTENANCE RE-INSPECTED SYSTEM AND CHECKED ALL CONNECTIONS FOR SECURITY. PROBLEM COULD NOT BE DUPLICATED. 2L72 4F RTA2NM 20031211000132003121100013WP 2003 12 11 ABXA030423 120031025A5534 STRUCTURE DOUG DC8 DC861 3021952WP VERTICAL STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 VERTICAL STABILIZER REAR SPAR LEFT CHORD HAD CORROSION ON AFT LEG BETWEEN ZR 262 AND ZR 268. REMOVED CORROSION ON REAR SPAR LEFT CHORD, FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48067MR. 2L74 4F 4A25 20031211000692003121100069WP 2003 12 11 UPS03841562 120031022A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STATION 190-355 AT LONGERON 31L. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5773863 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20031211001612003121100161WP 2003 12 11 AALA20031283 120031117A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217542A 49996 DFW OVERHEAD EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR OVERHEAD EMERGENCY LIGHTS FOR ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001712003121100171WP 2003 12 11 AALA20030911 120030828A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP A/C BAY DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212000082003121200008NM 2003 12 12 SWAA032476 120031107A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, BETWEEN STR'S 21L AND 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031212000992003121200099NE 2003 12 12 SWAA032394 220031030A7320442124 HMU BOEING737 7377H4 1384404NM GE CFM56 CFM567B24 NE NR 1 ENGINE FAULTY A SWAAK NONE R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW29406WN 27894 888427 DURING TAKEOFF, NR 1 ENG POWER SURGE INDICATION, REDUCED POWER AT CLIMB ALTITUDE OF 13000 FT, NR 1 ENG STABILIZED. REMOVED AND REPLACED NR 1 ENG HMU AND T12 SENSOR PER MM. 2L72 4F4 FRTA16WE E00055EN 20031212001152003121200115NM 2003 12 12 SWAA032450 120031106A276165C268642 ACTUATOR BOEING737 7373H4 1384600NM SPOILER LEAKING A SWAAK NONE KF FLUID LOSS FLT CONT AFFECTED APAPPROACH 1 SW29356SW 25251 ON FINAL LOSE OF RT HYDRAULIC QUANTITY AND PRESSURE. REMOVED AND REPLACED NR 1 SPOILER ACTUATOR PER MM. LK CHECK OK PER MM. 2L72 4F RTA16WE 20031212001272003121200127NM 2003 12 12 AWXA200301433 120031109A573065C267019 SKIN BOEING737 7373G7 1384595NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND ON RT WING LEADING EDGE SKIN PANEL WS 0 TO WS 12. MAINTENANCE REMOVED CRACKED RT WING LEADING EDGE SKIN PANEL WS 0 TO WS 12; FABRICATED NEW REPLACEMENT SKIN PER DWG 65C26701; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 SHEET 1 FIG 4, SHEET 1 & FIG 8, SHEET 1. 2L72 4F RTA16WE 20031212001322003121200132NM 2003 12 12 AWXA200301438 120031105A5311651758243 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN FRAME WEB VERTICAL BEAM AT FASTENER HOLE AT BS 178, RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE IN FRAME WEB VERTICAL BEAM AT BS 178, RBL 17.1, WL 230; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A SPLICE; INSTALLED REPAIR PARTS IAW SRM 53-10-08, PG 288K-288X, FIG 212. 2L72 4F RTA16WE 20031212001392003121200139NM 2003 12 12 AALA20030933 120030902A33508039001 LIGHT RAVEN S55 S55A 7480402NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21405AA S55A252 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY LIGHT WAS INOPERATIVE AT SEAT 16D. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 1B00 A15CE 20031212001412003121200141WP 2003 12 12 AALA20030928 120030829A3350P4010051111 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21513AA 49890 LAS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE NOT OPERATING PROPERLY. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001532003121200153WP 2003 12 12 GTIA030861 120030928A5210 STRUCTURE DOUG DC9 DC982 3022082WP L1 DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND L1 DOOR CRACKED 2 PLACES IN RADIUS AT AFT SIDE 2ND ACCESS FROM TOP AND FORWARD SIDE 2ND ACCESS HOLE FROM TOP. STOP DRILLED CRACKS. (M) 2L72 4F A6WE 20031212001542003121200154WP 2003 12 12 GTIA030860 120031012A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND PAX CABIN FLOORBOARD DELAMINATED AT FORWARD F/A SEAT AREA. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031212001662003121200166WP 2003 12 12 AALA20030925 120030829A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21598AA 53288 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 23 AND 24. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031212001762003121200176EA 2003 12 12 COMA0370053 120031130A77324120T14P02 ACCELEROMETER CNDAIRCL600 CL6002C10 1390015EA LT ENGINE FAULTY A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01367CA2740 10069 FLIGHT 5043) DURING CRUISE FLIGHT THE LT ENGINE FAN VIBRATION ENTERED THE AMBER CAUTION RANGE REACHING 2.1. AIRCRAFT RETURNED TO THE DEPARTING CITY (CVG). REPLACED THE LT ENGINE VIBRATION/ACCELEROMETER. 2L72 4F RTA21EA 20031212001802003121200180NE 2003 12 12 COMA0360463 220031018A73218063488 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE MALFUNCTIONED A COMAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO01779CA10927 7306 FLIGHT 5243 RT ENGINE HUNG AT 79 DEGREES N1 DURING T/O 3 INCHES POWER LEVER SPLIT. REPLACED THE RT FUEL CONTROL. 2L72 4F4 FRTA21EA E15NE 20031215000212003121500021NM 2003 12 15 SWAA032520 120031114A80122730426 START VALVE BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAULTY A SWAAE ENGINE SHUTDOWN J WARNING INDICATION UKUNKNOWN 1 SW29092SW 22964 687787 INFLIGHT ENG SHUTDOWN, NR 1 ENG START VALVE LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED NR 1 ENG START VALVE PER MM. 2L72 4F4 F A16WE E2EA 20031215000222003121500022NM 2003 12 15 SWAA032521 120031114A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 ONE EA EEPLS INOP AT ROW 12. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20031215000232003121500023 2003 12 15 SWAA032522 420031116A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20031215000262003121500026NM 2003 12 15 SWAA032525 120031116A3350BR2013 LIGHT BOEING737 7372H4 138448CNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED PM CHECK, FOUND EEPLS LOOSE AT FWD END. SECURED EEPLS PER MM 2L72 4F A16WE 20031215000352003121500035NM 2003 12 15 SWAA032512 120031113A57126545445 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WS 135.5, BETWEEN STRINGERS 2 AND 3. REPAIRED RIB PER BFG ER. 2L72 4F RTA16WE 20031215000432003121500043NM 2003 12 15 2003UALA00758 120031007A499038223642 CARBON SEAL BOEING777 777222 1385219NM APU DAMAGED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP29796UA1476 1476 26931 P1003 OIL SMELL IN COCKPIT ON DESCENT. APU WAS REPLACED AND SHOP DISASSEMBLED GEARBOX AND LOAD COMPRESSOR. ENGINEERING FOUND INDICATIONS THAT THE LOAD COMPRESSOR FRONT CARBON SEAL TO BE THE ROOT CAUSE FOR SMELL IN CABIN. THE LOAD COMPRESSOR CARBON SEAL HOUSING WAS FOUND BULGED AND WITH HEAT DAMAGE TO INNER LIP SEAL RESULTING IN COKING ON SEAL ROTOR. CARBON SEAL, SEAL ROTOR, BEARING AND BACK SHROUD REPLACED. 2L72 4F RTT0001SE 20031215000462003121500046NM 2003 12 15 2003UALA00797 120031023A213327406504 ACTUATOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE OUTFLOW VALVE FAILED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29767UA 26918 COULD NOT PRESSURIZE AIRCRAFT ON CLIMBOUT. DOWNLINKED CMC DATABASE SHOWED MAINTENANCE MESSAGE 21-39080, THE CABIN PRESSURE COULD NOT BE CONTROLLED DUE TO FAILED AFT OUTFLOW VALVE CONTROL UNIT (VCU). AFTER REPLACING THE FAILED ACTUATOR ASSY (COMPRISED OF THE VCU) WITH A SERVICEABLE ONE, THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT0001SE E46NE 20031215000502003121500050NE 2003 12 15 2003UALA00831 220031101A7230 COMPRESSOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE LEAKING A UALAK NONE R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP29652UA 25390 NR 1 ENGINE SURGE ON TAKEOFF. ENGINE SELF RECOVERED AND CONTINUED NORMAL OPERATION. ENGINE EXPERIENCED GROUP 3 SURGE ON TAKE OFF. CAUSE OF THE SURGE IS OPEN CLEARANCES IN THE REAR OF THE HPC. FINAL FIX FOR SURGE ISSUES IS THE OVERHAUL OF THE ENGINE TO A RING CASE CONFIGURATION. 2L72 4F4 FRTA1NM E24NE 20031215000552003121500055NM 2003 12 15 2003UALA00836 120031102A2560 BATTERY PACK BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN NOT SEATED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29669UA 30025 RIGHT WING OVERWING SLIDE SQUIB FAILS TO TEST. RESEATED BATTERY PACK ON RIGHT SIDE, TESTS OK. 2L72 4F4 FRTA1NM E24NE 20031211000112003121100011NM 2003 12 11 AWXA200301377 120031029A53206552264501 FITTING BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK A .75 INCH CRACK WAS FOUND RUNNING VERTICALLY FROM FASTENER HOLE ON FRAME FITTING BS 616, LBL 65. MAINTENANCE CUT OUT DAMAGE ON FRAME FITTING BS 616, LBL 65; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PART IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20031211000352003121100035EU 2003 12 11 MALA030490 120031104A3520 SELECTOR SAAB SF340 340B 7860101EU OXYGEN CYLINDER LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15365PX 340B265 DURING FLIGHT NR 2735 FROM LOG PAGE: OXYGEN LIGHT ILLUM. GAUGE IND 750 PSI, 1700 PSI AT ACCEPTANCE OF AIRCRAFT. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED LT AND RT AFT OXYGEN CYLINDERS (DUE TO LEAKING AT ON/OFF SELECTOR) & REPLACED BROKEN PRESSURE INDICATING CAPILLARY LINE. LEAK CHECKS GOOD. 2L72 4T RTA52EU 20031211000462003121100046 2003 12 11 P5CA0300980 420031110A34257771397001 HSI BOEING747 747200 1384847NM COCKPIT FAILED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23524UP 21446 DURING ENG START AT PUSHBACK CAPT'S CDI COMPASS FLAG IN VIEW COMPASS FROZE ON HSI. HSI WAS PREVIOUSLY CHANGED ON PRIOR ITEM & PLACED ON SOS. ORIGINAL HSI INSTALLED, OPS CK OK PER MM 34-41-06. 2L74 4F RTA20WE 20031211000612003121100061NM 2003 12 11 QXEA200301415 120031109A2810 O-RING DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM OUT OF POSITION A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09374PH 528 PDX- ON FLIGHT 2044 FUEL LEAK AT SPR. RESET AND SEATED BLUE O-RING ON FUELING ADAPTER POPPET VALVE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031211000912003121100091WP 2003 12 11 DHL2003806014 120031111A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01806DH 46002 EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECKED GOOD IAW M/M 33-50-1. 2L74 4F RT4A25 20031211001072003121100107NM 2003 12 11 AALA20031328 120031124A3411 PITOT TUBE BOEING737 737823 13844BZNM PITOT/STATIC SYSCLOGGED A AALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW21902AN 29504 MIA T651/24 EN ROUTE MIA-BGI 30 KNOT AIRSPEED SPLIT NOTICED ON TAKEOFF ROLL. CAPTAINS AIRSPEED INDICATED 60 KNOTS AND FIRST OFFICERS AIRSPEED INDICATED 90 KNOTS. REPLACED CAPTAINS PITOT TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20031211001322003121100132WP 2003 12 11 AALA20031337 120031127A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219625W 53595 TUL LEFT AND RIGHT OVERWING ESCAPE HATCH EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT OVERWING ESCAPE HATCH EXIT SIGN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031211001572003121100157WP 2003 12 11 AALA20031279 120031116A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21473AA 49648 LGA EMERGENCY AISLE PATH LIGHT MODULE WILL NOT HOLD A CHARGE. REPLACED EMERGENCY AISLE PATH LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001962003121100196EU 2003 12 11 USAA030250 120031101A5320D5347208900200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND FLOOR SUPPORT/BEAM CORRODED 5 CM BY 3 CM, .149 INCH DEEP, FRAME 68, -Y 114. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11 AND 51-72-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20031215000782003121500078 2003 12 15 AWXA200301464 420031102A256560592101 CABLE AIRBUSA319 A319132 3930340NM EVAC SLIDE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28824AW 1490 PHX - EES - DURING P-09 CHECK THE CABLE END WAS FOUND BROKEN ON THE RT OVERWING SLIDE BOTTLE. MAINTENANCE REMOVED AND REPLACED RT OVERWING SLIDE RESERVOIR ASSEMBLY IAW AMM 25-62-46. 2L72 4F RTA28NM 20031215000792003121500079 2003 12 15 AWXA200301465 420031118A34414650203030312 IRU AIRBUS320 A320232 3930326EU NR 1 FAULTY A AWXAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 WP28670AW1511 2029 DURING TAKEOFF ROLL AT JFK EN ROUTE FOR PHX LOST CAPTAINS PRIMARY FLIGHT DISPLAY AND NAVIGATION DISPLAY, NAV IR 1 FAULT INDICATED, REJECTED TAKEOFF AT 95 KTS. MAINTENANCE ISSUED MEL 34-10-01, COND 2 IRS NR 1 NAV MODE INOP. WHEN AIRCRAFT ARRIVED IN PHX MAINTENANCE REMOVED AND REPLACED AIR DATA INERTIAL REFERENCE UNIT (ADIRU) NR 1 IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAILURE OF ADIRU S/N 4325. UNIT WAS FOUND TO EXPERIENCE VERTICAL ACCELERATION FAILURE (FID396), PERFORMED SERVICE BULLETIN SB101-34-57, RECALIBRATED UNIT & PERFORMED FUNCTIONAL TEST IAW CMM TP1011, REV. 23. 2L72 4F RTA28NM 20031215000872003121500087NM 2003 12 15 03FDEA01956 120031113A5753 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT OUTBOARD FLAP FOUND INBOARD HINGE FITTING LOWER MOUNTING MATING SURFACE CORRODED. RT WING O/B FLAP, INBD HINGE FITTING LOWER MOUNTING MATING SURFACE CORROSION REMOVED & REPAIRED AS PER EA 1-5740-74250 TITLE : WINGS - LT & RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030924000192003092400019NE 2003 9 24 DL76S030726 220030806A7532 BLEED VALVE BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 2 ENGINE INOPERATIVE A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27138DL 25409 580385 REJECTED TAKEOFF SHORTLY AFTER TAKEOFF POWER APPLIED. (LESS THAN 30 KTS) FOR MASTER CAUTION LIGHT AND AURAL WARNING. EICAS MSG RT ENGINE BLEED VALVE AND BLEED ANNUNCIATOR LIGHT IN OVERHEAD PANEL ILLUMINATED. REPLACED VALVE 2L72 4F4 FRTA1NM E13NE 20030924000342003092400034NM 2003 9 24 DL73S030747 120030812A3397 WIRE BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27316DL 23088 SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT ROWS 18-21. REPAIRED WIRING NOW OPS, NORMAL. 2L72 4F RTA16WE 20030924000442003092400044NM 2003 9 24 DLM88030757 120030815A3222H1410160234 SWITCH DOUG MD88 MD88 3023688NM NLG UNSERVICEABLE A DALAO OTHER J WARNING INDICATION LDLANDING 1 SO27947DL 49878 ON APPROACH WHEN GEAR HANDLE LOWERED, HAD ONLY TWO MAIN GEAR GREEN LIGHTS - NO NOSE GEAR LIGHT RED OR GREEN. FOLLOWED CHECKLIST WITH GOOD NLG PIN .2500 INCH AND MAINT CONCURANCE SHOWED GOOD GEAR. NOSE GEAR LIGHT REMAINED OFF ENTIRE TAXI UNTIL POWER SWAPPED OVER AT GATE. REMOVED AND REPLACED PROX BOX. NO HELP - REINSTALLED ORIGINAL. REPLACED NOSE GEAR INTERLOCK SWITCH. COMPLETED GEAR SWING. CHECKS OK. 2L72 4F RTA6WE 20030924000582003092400058NM 2003 9 24 DL757030773 120030820A5330146N31111 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27625DL 22915 LIGHTING STRIKE REPAIR LIGHTING STRIKE DAMAGE WAS FOUND ON THE UPPER SKIN AT THE STRINGER 4R SKIN LAP JOINT AT FS 1242. THE DAMAGE WAS REMOVED WITH A CUTOUT TO THE UPPER SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED IAW ER/A 087125-14, REV A. 2L72 4F RTA2NM 20030924000632003092400063NM 2003 9 24 DL73S030778 120030823A2530253003955 COFFEEMAKER BOEING737 737232 1384475NM AFT GALLEY BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27317DL 23089 BURNING ODOR IN AFT GALLEY, TURNED GALLEY POWER OFF, ODOR WENT AWAY. REPLACED AFT GALLEY NR 2 COFFEE DISPENSER. 2L72 4F RTA16WE 20030922000982003092200098 2003 9 22 UPS03141228 420030915A2565 LIGHT AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE EVAC SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01136UP 0820 CREW DISCOVERED EVAC SLIDE LIGHT (WARNING LIGHT) INOPERATIVE. DEFERRED UNDER MEL 52-73-01 01 W/CONTROL NR M266526 PLACARD INSTALLED. 2L72 4F4 FRTA35EU E24NE 20030923000262003092300026WP 2003 9 23 DHL2003604542 120030502A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING OB L/E FRAME CRACKED (0.500) STA. XFS.753.000. STOP DRILLED CRACK AT XFS.753.000 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG.9-10, SRM 51-1-20D PG.9, SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030923000352003092300035WP 2003 9 23 DHL2003604588 120030611A5350 FRAME DOUG DC8 DC873F 302199FWP TAIL CONE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 TAIL CONE SECTION - FRAME CRACKED 1.000 STA. 1937.000 LH SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 FIG.2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1 2L74 4F RT4A25 20030923000542003092300054WP 2003 9 23 DHL2003604771 120030601A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT INNER WING CTR EXTENDED L/E UPPER SKIN CORRODED AROUND STA XFS 354.000 - XFS 385.250. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE CORRODED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.071) AND TWO FILLERS (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLERS AND DOUBLER ON RT INNER WING CTR EXTENDED L/E UPPER SKIN (AROUND STA XFS 354.000 - XFS 385.000) USING NEW FASTENERS IAW EODHL-030519, ED-3355, SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030923001092003092300109WP 2003 9 23 DHL2003604727 120030609A53205773275169 STIFFENER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT. FLOORBEAM INTERCOSTAL JOINT SHOWS STIFFENER CRACKED (1.000) STA.702.000 BL-0. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, ATM P0201384, DWG.5773275. REMOVED CRACKED STIFFENER IAW SRM 51-1-20D PG.21, SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW DWG.5773275. PERFORMED LIQUID PENETRANT INSPECTION IAW DC8 NDT SPM PART 08-00-02/06. CLEANED, TREATED AND PRIMED AREA AND STIFFENER IAW SRM 51-1-8B. INSTALLED STIFFENER WITH NEW FASTENERS IAW SRM 51-1-20D PG.9 AND SRM 51-1-21 PG.1 2L74 4F RT4A25 20030923001332003092300133NM 2003 9 23 03FDEA01298 120030807A5754 HINGE FITTING DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT WING FLAP HINGE FITTING 28 WING SIDE 29 REAR SPAR LOWER MOUNT BOLT HOLE FOUND CORROSION. 2L73 4F RTA22WE 20030923001662003092300166WP 2003 9 23 AALA20030808 120030729A3350P4010051111 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT MALFUNCTIONED A AALAK NONE O OTHER ININSP/MAINT 1 SW21435AA 49453 DURING OVERNIGHT MAINTENANCE, THE SEAT MOUNTED EMERGENCY PATH LIGHTS FROM THE FRONT OF THE AIRCRAFT TO SEAT ROW 19 COME ON WHEN THE FORWARD LIGHT ATTENDANT EMERGENCY LIGHT SWITCH IS PUT IN THE 'ON' POSITION. REPLACED CONTROL MODULE AT STATION 850. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030923001692003092300169NM 2003 9 23 AALA20030701 120030628A3350 CONNECTOR BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21940AN 30598 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030923001862003092300186NM 2003 9 23 AALA20030320 120030319A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21969AN 29546 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030924000672003092400067NM 2003 9 24 DL73S030783 120030822A53306545768265 SKIN BOEING737 737232 1384475NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27321DL 23093 SKIN GOUGE CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND GOUGED NEAR THE FWD EDGE OF THE C1 DOOR CUTOUT BETWEEN FS 430 AND 440 AT STRINGER 22R. THE DAMAGE WAS REMOVED WITH A 10.5 X 1.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 385464-14, REV A. 2L72 4F RTA16WE 20030924000772003092400077NM 2003 9 24 2003UALA00638 120030820A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29366UA 24535 STA 161 RT INBOARD FRAME CRACKED AT BOTTOM FASTENER MAJOR REPAIR ACCOMPLISHED, INSTALLED ANGLE AND FILLER. 2L72 4F4 FRTA16WE E2GL 20030924000782003092400078NM 2003 9 24 2003UALA00639 120030819A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 DENT AND GOUGE APPROX. 4 & ONE-HALF INCHES LONG IN FWD LEFT FUSELAGE 2 INCHES ABOVE ORANGE STRIPE BELOW 2ND WINDOW . MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030924000862003092400086 2003 9 24 223032503 420030325A2216065005680 SERVO PILATSPC12 PC1245 7090551EU SERVO YAW FLUCTUATES E S4WAO OTHER F FLT CONT AFFECTED CRCRUISE 1 WP07317NA 223 RUDDER TRIM FLUCUATES IN FLIGHT. 1L71 3T RTA78EU 20030924000872003092400087 2003 9 24 223020203 420030402A22200012ACIO PROBE PILATSPC12 PC1245 7090551EU AOA FAILED E S4WAK NONE L NO TEST ININSP/MAINT 1 WP07317NA 223 RT AOA PROBE DOES NOT HEAT. 1L71 3T RTA78EU 20030924000932003092400093NM 2003 9 24 AWXA200300985 120030815A532069429494 ATTACH ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 5/8 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT SILL WEB TO FRAME ATTACH ANGLE UPPER LEG AT BS 807, RBL 19.5. MAINTENANCE REMOVED CRACKED FRAME ATTACH ANGLE AT BS 807, RBL 19.5; FABRICATED A NEW REPLACEMENT FRAME ATTACH ANGLE; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 1, AND SRM 51-30-04, FIG. 2. 2L72 4F RTA16WE 20030924001132003092400113CE 2003 9 24 BSY2003F00018 120030808A3411 LINE BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO PITOT TUBE OBSTRUCTED E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL076573K TH1369 823817R AIRSPEED INOPERATIVE ON TAKEOFF. REMOVED LINE FROM PITOT TUBE, BLEW BACK THRU TUBE , REMOVE OBSTRUCTION, RECONNECTED. LEAKED CHECKED. OPS CHECK GOOD. 1L72 3O3 O 3A16 E5CE 20030924001172003092400117NE 2003 9 24 179152 220030827A7261 CHIP DETECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE LT ENGINE CONTAMINATED A UHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL17150CN 150CN 367434 FLT 4451 FROM PIT TO CMH. AIRCREW RECEIVED A CHIP DETECTOR LIGHT IN FLIGHT ON THE LT ENGINE. ALL PERIMETERS WERE NORMAL. ON RETURN TO PIT, WITH POWER BROUGHT BACK TO 30 PERCENT, LIGHT WENT OUT. AIRCREW RETURNED TO PIT SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE LOOKED AT A/C AND FOUND SMALL AMOUNTS OF CARBON, CLEANED CHIP DETECTOR AND SCREEN. GROUND RAN AND OPS CHECKED GOOD 2L72 4T4 TRTA52EU E8NE 20030924001382003092400138NM 2003 9 24 AALA20030712 120030707A2120 ODOR BOEING757 757223 1384957NM CABIN DETECTED A AALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21633AA 24591 CREW OBSERVED BURNED PLASTIC ODOR IN CABIN. EMERGENCY DECLARED AND RETURNED TO PIT WITHOUT FURTHER INCIDENT. GROUND RAN AIRCRAFT WITH BOTH AIR CONDITIONING PACKS ON HIGH. INSPECTED E/E BAY, CARGO BAYS, AFT ACCESSORY COMPARTMENT, AND BOTH MAIN LANDING GEAR BAYS. CHECKED CABIN LIGHTS BALLASTS. CHECKED LAVATORIES AND TRASH BINS. UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001452003092400145EU 2003 9 24 AALA20030846 120030809A2900 O-RING AIRBUS300 A300B4605R 3930308EU HYD SYSTEM CUT A AALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2180052 460 AIRCRAFT LOST GREEN SYSTEM HYDRAULIC QUANTITY. AIRCRAFT LANDED BOS WITHOUT INCIDENT. FOUND GREEN SYSTEM PRESSURE LINE TO MANIFOLD O-RING CUT AND LEAKING. REPLACED O-RING AND BACK UP RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030925000082003092500008NM 2003 9 25 AALA20030716 120030707A7932 TRANSMITTER BOEING737 737823 13844BZNM OIL QTY DIRTY A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21902AN 29504 ENROUTE MIA-PHL, AFTER TAKEOFF, NR 1 ENGINE OIL QUANTITY DROPPED RAPIDLY TO THREE QUARTS AND NR 2 ENGINE OIL QUANTITY DROPPED TO 6 QUARTS. POWER WAS REDUCED AND QUANTITIES REMAINED AT 5 QUARTS AND 8 RESPECTIVELY. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO MIA WITHOUT FURTHER INCIDENT. CHECKED ENGINE OIL QUANTITY FOR BOTH ENGINES. LT ENGINE READS ELEVEN AND RT ENGINE READS THIRTEEN. SERVICED BOTH ENGINES. CHECKED BOTH ENGINES FOR LEAKS AND FOUND NONE. CLEANED BOTH ENGINE OIL QUANTITY TRANSMITTER CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030925000092003092500009NM 2003 9 25 AALA20030544 120030505A5610141A48107 WINDOW BOEING737 737823 13844BZNM COCKPIT CRACKED A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21902AN 29504 EN ROUTE AT 37,000 FT, THE L2 WINDOW CRACKED AND SPARKED UNTIL WINDOW HEAT WAS TURNED OFF. RETURNED AND LANDED DFW WITHOUT INCIDENT. INSTALLED L2 WINDOW ASSEMBLY AND RIGGED FOR PROPER FIT AND CLOSURE. INSTALLED NEW WINDOW HEAT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030925000292003092500029SO 2003 9 25 SIMA200323005 120030812A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 DURING AN IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED FLOORBEAM. FABRICATED A REPAIR ANGLE, FILLER, FORWARD SHIMS, AFT SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-20 PAGE 201 ITEM 2 FIG 201. (M) 2L72 4F RTT00011AT 20030925000432003092500043 2003 9 25 AALA20030767 420030710A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21679AN 29589 JFK - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT SPRINGS NEEDING REPLACED. REPLACED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000472003092500047 2003 9 25 AALA20030771 420030710A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21634AA 24592 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING NEEDING REPLACED. REPLACED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030923000952003092300095WP 2003 9 23 DHL2003604695 120030604A5340 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT MLG W/W FITTING ATTACHING LONGERON 24L AT STA. 940.000 WITH 5.000 CRACK IN IT. PERORMED MAJOR REPAIR IAW SRM 53-2-0 FIG.8. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. CUT OUT NEW FITTING SRM 53-2-0 FIG.8. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FITTING AND (4 EA) SPLICE FITTING AND DOUBLER FITTING AND FILLER WITH NEW FASTENERS IAW SRM 53-2-0 FIG.8, SRM 51-1-21 PG.9. 2L74 4F RT4A25 20030923001222003092300122WP 2003 9 23 DHL2003604752 120030520A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING CTR EXTENDED L/E SLOT INNER DOUBLER CRACKED (0.063) AT STA. XFS. 526.000. PERFORMED MAJOR REPAIR IAW EODHL-030532, ED-3350. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. STOP DRILLED ON CRACK END (0.250 DIA) IAW EODHL-030532, ED-3350. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) IAW EODHL-030532, ED-3350. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER ON RT. OUTER WING CTR. EXTENDED L/E SLOT STA. XFS.526.000 USING NEW FASTENERS. 2L74 4F RT4A25 20030923001712003092300171EU 2003 9 23 AALA20020717 120030517A2611 SMOKE DETECTOR AIRBUS300 A300B4605R 3930308EU E/E COMPT INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2111060 470 EN ROUTE MIA-BOS, AVIONICS SMOKE WARNING ON ECAM. NO SMOKE OR HEAT NOTED IN AVIONICS COMPARTMENT. LANDED IN RDU WITHOUT INCIDENT. TROUBLESHOT AND REPLACED SMOKE DETECTOR 11WA. SYSTEM ROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030923001852003092300185NM 2003 9 23 USAASB03137 120030813A335020131A BATTERY PACK BOEING737 737301 1384611NM MID CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU 23551 ATL - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY EXIT LIGHTING, AT THE LEFT OVERWING EXIT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE LEFT OVERWING EXIT POSITION. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030924000112003092400011 2003 9 24 197031103 420030311A34219759611241 INDICATOR PILATSPC12 PC1245 7090551EU ATTITUDE WORN E S4WAK NONE O OTHER ININSP/MAINT 1 WP07613NA361 197 STANDBY ATTITUDE INDICATOR WILL NOT CAGE. 1L71 3T RTA78EU 20030924000262003092400026 2003 9 24 DL75K030734 420030809A2564D806627 LIFE RAFT BOEING757 757232 1384965NM CABIN DEPLOYED A DALAK NONE O OTHER ININSP/MAINT 1 SO276709 30481 DURING NIGHT TIME TRANSIT CHECK MAINTENANCE WAS PERFORMING A CHECK OF THE 10 MAN LIFE RAFTS AND FOUND THE FORWARD LIFE RAFT PARTIALLY INFLATED. REPLACED RAFT. 2L72 4F RTA2NM 20030924000762003092400076NM 2003 9 24 2003UALA00636 120030820A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29366UA 24535 SKIN CRACKED BELOW LT STA 188 SIDE DOUBLER STA 178 BULKHEAD AT WL193. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR 2L72 4F4 FRTA16WE E2GL 20030924000802003092400080NE 2003 9 24 223012703 220030127A73148256015 PUMP PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE FUEL SYS FOD E S4WAK NONE C F.O.D. ININSP/MAINT 1 WP07317NA 223 PCEPR0079 FOD FOUND IN FUEL OUTLET FILTER. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL. 1L71 3T4 TRTA78EU E26NE 20030924000852003092400085NM 2003 9 24 QXEA200301023 120030823A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 DENT IN FUSELAGE AT STATION X697.600. REPAIRED IAW HORIZON AIR EA 6-53-289. 2H72 4T RTA13NM 20030924000982003092400098EU 2003 9 24 223082303 120030823A21509599020111 ACM PILATSPC12 PC1245 7090551EU A/C SYSTEM NOISY E S4WAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP07317NA 223 AIR CYCLE MACHINE IS MAKING UNUSUAL NOISES. 1L71 3T RTA78EU 20030924001002003092400100NM 2003 9 24 03FDEA01329 120030808A5753ARC0155503 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING I/B T/E FLAP, O/B FWD HINGE FITTING ASSY HAS PIVOT BEARING MOUNT LUG SPOT FACES RUSTY. LT WING I/B T/E FLAP, O/B FWD HINGE FITTING ASSY HAS PIVOT BEARING MOUNT LUG SPOT FACES REPAIRED AS PER FEDEX EA 1-5750-63187, TITLE: WINGS- TRAILING EDGE FLAPS- LH I/B FLAP, O/B HINGE LUG SURFACE REWORK. 2L73 4F RTA22WE 20030924001442003092400144EU 2003 9 24 AALA20030605 120030429A5343D232430002 BEAM AIRBUS300 A300B4605R 3930308EU LT MLG DEFECTIVE A AALAO OTHER J WARNING INDICATION LDLANDING 1 SW2114065 508 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. WOULD NOT GO PASS MID-POSITION. LANDING RETRACTION INOPERATIVE MESSAGE ON ECAM. LANDED TULE WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR BOGIE BEAM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030925000172003092500017EU 2003 9 25 AALA20030906 120030827A2910 O-RING FOKKERF28 F28MK0100 4990807EU HYD SYSTEM LEAKING A AALAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW211473K 11515 DURING DESCENT, THE NR 1 HYD SYSTEM WENT TO 36 PERCENT AND THE HYD SYSTEM NR 1 LOW LIGHT ILLUMINATED. THE ALTERNATE FLAP AND LANDING GEAR EXTENSION PROCEDURES WAS USED. CREW DECLARED AN EMERGENCY AND LANDED AT YYZ WITHOUT FURTHER INCIDENT. REPLACED THE NR 1 HYD PUMP PRESSURE LINE O-RING. SERVICED WITH HYD FLUID. SYSTEM GROUND CHECKED FOR NORMAL OPERATION. (M) 2L72 4F RT 20030925000412003092500041 2003 9 25 AALA20030765 420030702A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21685AA 25342 DFW - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST OT CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS NEEDING REPLACED. REPLACED GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000512003092500051NM 2003 9 25 USAA030158 120030731A5320 INTERCOSTAL BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US40913 23987 FOUND INTERCOSTAL CRACKED 1 INCH, BS 328 LBBL 45 CABIN FLOOR. REPLACED INTERCOSTAL PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20030925000522003092500052SO 2003 9 25 SIMA200333303 120030809A4997 WIRE HARNESS EMB 145 EMB145LR 3260212SO APU DAMAGED A SIMAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW21615AE 145087 CREW REPORTED AN APU FIRE WARNING ON GROUND WITH BLACK SMOKE COMING FROM EXHAUST. GROUND EMERGENCY DECLARED. NO EVIDENCE OF FIRE WAS FOUND AND APU WAS PUT ON MEL. MAINTENANCE FOUND THE APU HARNESS DAMAGED. HARNESS WAS REPLACED IAW EMB MM AND OPERATIONAL CHECK WAS COMPLIED WITH, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030925000662003092500066 2003 9 25 AALA20030899 420030824A2565 SPRING BOEING757 757223 1384957NM GIRT BAR WORN A AALAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21178AA 32398 UPON ARRIVAL JFK, R4 DOOR ASSIST BOTTLE BLOWN. SLIDE DID NOT DEPLOY. FOUND AFT SPRING ON GIRT BAR WORN. REPLACED GIRT BAR ASSEMBLY AND DOOR ASSIST BOTTLE AND SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000722003092500072NM 2003 9 25 AALA20030893 120030821A29105981115 O-RING BOEING767 767323 1385205NM RT MLG WW CUT A AALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21385AM 27059 AFT APPROX 1 HOUR OF FLIGHT CENTER HYD QTY EICAS MSG DISPLAYED. PUMPS SELECTED OFF IAW PROCEDURE STOPPED FLUID LOSS AT .40. UPON INSPECTION, FOUND DPI FOR ADP PRESS MODULE LOOSE WITH A CUT O-RING. REPLACED O-RING, NO LEAKS NOTED. SERVICED CTR HYDRAULIC QUANTITY TO FULL. (M) 2L72 4F RTA1NM 20030925000832003092500083EU 2003 9 25 2003F00583 120030806A6320 FILTER SNIAS 350 AS350B2 8680813EU M/R GEARBOX DAMAGED A HXSAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 AL056052F1088 M1868 2587 PILOT REPORTED THAT THE INDICATOR LIGHT FOR THE MAIN GEAR BOX PRESSURE. PILOT REPORTED THAT HE FOUND A LANDING SPOT AND LANDED, BUT BEFORE HE LANDED THE LIGHT WENT BACK OUT. LOOKED THROUGH THE AMERICAN EUROCOPTER MM FOR THIS SITUATION AND FOUND NOTHING. CALLED AEC TECH REP AND WAS TOLD THERE IS NO COVERAGE FOR THIS. CHANGED OIL AND FILTER ON THE SIDE OF SAFETY. DID 10 MIN HOVER AND FOUND NO MORE PROBLEMS. AIRCRAFT WAS RELEASED TO SERVICE. (M) 1G71 3U H9EU 20030925000962003092500096NM 2003 9 25 2003UALA00681 120030710A5751 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE AILERONS CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29770UA 26925 LT AILERON PCU FITTING CRACKED IN 3 PLACES AND RT AILERON PCU FITTING CRACKED IN 1 PLACE. REPLACED BOTH AILERONS. 2L72 4F4 FRTT0001SE E46NE 20030925001002003092500100CE 2003 9 25 DXTA200300123 120030920A2611 CONNECTOR RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP SMOKE DETECTOR LOOSE E DXTAO OTHER N FALSE WARNING CRCRUISE 1 GL07861QS 258361 DURING FLIGHT TOILET SMOKE DETECTION LIGHT AND BAGGAGE FIRE DETECTION LIGHT CAME ON ERRONEOUSLY, SYSTEMS WILL NOT TEST. GAINED ACCESS TO THE FORWARD AND AFT BAGGAGE COMPARTMENT SMOKE DETECTORS, FOUND BOTH CONNECTORS LOOSE, TIGHTEN BOTH CONNECTORS. GAINED ACCESS TO THE LAVATORY SMOKE DETECTOR, INSPECTED AND FOUND CONNECTOR IS SECURED. ALL WORK DONE IAW HAWKER 800XP MM CHAPTER 26-11-00. 2L72 4F4 FRTA3EU E6WE 20030925001022003092500102EU 2003 9 25 174042903A 120030429A7797311221401 WIRE HARNESS PILATSPC12 PC1245 7090551EU ENGINE IND DEFECTIVE E SRWAK NONE O OTHER ININSP/MAINT 1 WP07562NA 174 TREND REPORTS SHOWED ITT FLUCTUATING. FOUND ITT HARNESS RESISTANCE OUT OF LIMITS. 1L71 3T RTA78EU 20030925001052003092500105NM 2003 9 25 QXEA200301024 120030825A2810 POPPET VALVE DHAV DHC8 DHC8202 2809007NM ZONE 400 LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09362PH 518 FUEL LEAK FROM END OF NR 2 NACELLE. FOUND POPPET VALVE ON SPR UNSEATED TO NR 1 SIDE AND LEAKING. RESEATED AND NO FURTHER LEAKS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030926000022003092600002EU 2003 9 26 S9H2003F00001 120030716A29131502780 PUMP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE HYD SYSTEM FAILED E S9HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP19355NT186 2053 DURING A REGULAR TOUR FLIGHT, THE PILOT EXPERIENCED A HYDRAULIC FAILURE. PILOT AND AIRCRAFT PERFORMED RECOMMENDED PROCEDURES AND UPON INSPECTION OF THE SYSTEM IT WAS CONFIRMED THAT THE COUPLING HAD FAILED. HYDRAULIC PUMP, COUPLING, AND BEARING WERE REPLACED. 1G71 3U3 UNCH9EU E19EU 20030926000352003092600035NM 2003 9 26 03FDEA01391 120030826A5530 PANEL SUPPORT BOEING727 727200 138407ENM VERTICAL STAB CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 VERTICAL STAB LT TEE SUPPORT IS CHAFED WHERE PANEL 8603 LWR ATTACHMENT ANGLE, ATTACHES TO THE PANEL SUPPORT. CUT OUT DAMAGED AREA 3 X 1 INCH ON LT VERTICAL STAB SUPPORT AT PANEL 9603'S AFT ATTACH ANGLE MOUNT HOLE. FABRICATED AND INSTALLED REPAIR IAW SRM 55-30-6 FIG 3. 2L73 4F RTA3WE 20030926000422003092600042CE 2003 9 26 GLBA2003125 120030827A77221303800415 INDICATOR BEECH 1900 1900D 1154162CE ITT INOPERATIVE A GLBAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 NM03184UX999 UE184 RT ITT INDICATOR NOT WORKING, REMOVED AND REPLACED INDICATOR. 2L72 4T RTA24CE 20030926000452003092600045NM 2003 9 26 AMTA200301021 120030711A5330 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE FUSELAGE GOUGED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11525AT 30548 FUSELAGE SKIN HAS GOUGES AT CROWN. REPAIRED SKIN IAW ER/A 757-53R-5239. 2L72 4F4 FRTA2NM A12EU 20030926000512003092600051NM 2003 9 26 MWEA030334 120030827A5330593602229 SKIN DOUG MD88 MD88 3023688NM DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FUSELAGE SKIN AT STATION 1107 BETWEEN LONGERON 28 AND 29 RIGHT REQUIRE'S A REPAIR TO THE HOLE DUE TO THE REMOVAL OF THE AIRPHONE ANTENNA. FABRICATED AND INSTALLED DOUBLER AND TRIPLER. 2L72 4F RTA6WE 20030926000532003092600053EA 2003 9 26 COMA0360381 120030826A4990387600106 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA APU MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01781CA 7312 FLIGHT 5254 APU LOW OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU LOW OIL PRESSURE SWITCH. 2L72 4F RTA21EA 20030926000602003092600060 2003 9 26 COMA0360389 420030824A22116229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT MALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO01924CA4852 1 7026 FLIGHT 5307 RUDDER YAWS IN FLIGHT WITH AUTO-PILOT OFF. REPLACED THE NR 1 FCC CARD. 2L72 4F RTA21EA 20030926000612003092600061NM 2003 9 26 QXEA200301039 120030826A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 PDX- ESCAPE PATH LIGHTING STRIP AT ROW 1 IS DAMAGED. REMOVED AND REPLACED LIGHT STRIP. 2H72 4T4 TRTA13NM E20NE 20030926000622003092600062NM 2003 9 26 AWXA200300993 120030826A3350 FUSE BOEING757 757225 1384959NM POWER SUPPLY BLOWN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 DURING INSPECTION THE EMERGENCY ESCAPE LIGHTS AT OVERHEAD BINS SEAT ROWS 2 LT, 3 RT & 6 RT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED 3 EACH FUSES ON POWER SUPPLY UNIT M730 IAW BMM 33-51-07; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030923001132003092300113WP 2003 9 23 DHL2003604741 120030620A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBD. L/E SLANT PANEL UPPER CAP SHOWS CORROSION FROM XFS.63.750 TO XFS.82.500 AND REPAIR DOUBLER FROM XFS.201.000 TO XFS.207.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-2-1 FIG.37, SRM 57-3-3 FIG.2. REMOVED CORROSION ON UPPER CAP IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG.347. REMOVED CORRODED UPPER CAP IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CLEANED AND APPLIED PRC ON FAYING SURFACES IAW SRM 51-1-12 PG.1. INSTALLED NEW UPPER CAP WITH NEW FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. FOR LEAK CHECK SEE N/R 3824. 2L74 4F RT4A25 20030923001152003092300115WP 2003 9 23 DHL2003604615 120030510A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING IB L/E CORRODED AT STA. XFS.710.000. PERFORMED MAJOR REPAIR IAW EODHL-030509, ED-3314. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.11-12. TRIMMED OUT CORRODED SKIN AREA IAW EODHL-030509, ED-3314. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (7075-T6 AL0.063) AND FILLER (7075-T6 AL0.050) IAW EODHL-030509, ED-3314. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER AND FILLER INNER SIDE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL-030509, ED-3314, SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. 2L74 4F RT4A25 20030923001372003092300137WP 2003 9 23 0301609997 120030822A2130 CLAMP DOUG DC9 DC931 3022065WP CABIN PRESSURE LOOSE A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL018933E 47142 DURING CRUISE AT FL290, CABIN PRESSURE LIGHT AND MASTER WARNING LIGHT ILLUMINATED DUE TO CABIN PRESS AT 10,500 FT. CREW INITIATED AN EMERGENCY DESCENT AND PERFORMED COM PROCEDURES. AC HAD DEPRESSURIZED BY TIME 10,000 FT WAS REACHED AND MAX CABIN ALTITUDE HAD BEEN 12.000 FT. CREW HAD LITTLE CONTROL OF PRESSURIZATION IN MANUAL. LANDING AT GSP WAS UNEVENTFUL. MAINT DID BITE ON BOTH PRESSURE CONTROLLERS; NO FAULTS FOUND. FOUND PERI SEALS LEAKING AT BOTH LEFT AND RIGHT HEAT EXCHANGERS, FOUND A BROKEN CLAMP AT AFT RIGHT RAM AIR DUCT, AND A LOOSE CLAMP AT LEFT RAM AIR DUCT TO HEAT EXCHANGER. REPLACED BROKEN CLAMP, TIGHTENED LOOSE CLAMP, AND REPLACED 4 PERI SEALS. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. 2L72 4F A6WE 20030923001722003092300172NM 2003 9 23 AALA20030773 120030716A3397 WIRE BOEING727 72781 1384025NM EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21901AN 29503 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 20 INOPERATIVE. SPLICED WIRE AT RIGHT SIDEWALL ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 20030923001872003092300187WP 2003 9 23 AALA20030861 120030816A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21447AA 49473 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON FORWARD GALLEY WALL INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030924000242003092400024NM 2003 9 24 DL76L030732 120030808A33970201875003 WIRE HARNESS BOEING767 767332 1382001NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27191DN 28448 SEAT 24A/B EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT HARNESS. OPS CHECK GOOD. 2L72 4F RTA1NM 20030924000322003092400032NM 2003 9 24 DL73G030745 120030812A3240 FLANGE BOEING737 73735B 13844BMNM MLG BRAKE ASSY CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27222DZ 23971 DURING OVERHAUL OF THE MLG PISTON IAW CMM 32-11-11, THE BRAKE FLANGE FACE WAS LOCALLY BLENDED. SUBJECT CMM, FIGURE 403 NOTES NO BLENDING IS ALLOWED, AND TO CONTACT OEM. NOTE: GEAR IS SCHEDULED TO BE INSTALLED ON AC 222. BLEND WAS SUBMITTED TO OEM, AND SUBSEQUENTLY PROCESSED IAW ERA 339500-14AD. 2L72 4F RTA16WE 20030924000422003092400042NM 2003 9 24 DL73S030755 120030815A3230 ACCESSORY UNIT BOEING737 737232 1384475NM MLG FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27318DL 23090 IRR LANDING GEAR LEVER LOCK WOULD NOT RELEASE WHEN GEAR HANDLE WAS RAISED AFTER T/O. REPLACED LANDING GEAR ACCESSORY UNIT. 2L72 4F RTA16WE 20030924001052003092400105NM 2003 9 24 03FDEA01281 120030806A5753ARC0503504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBOARD FLAP OUTBD HINGE (FLAP SIDE) ACTUATOR ATTACH LUGS CORRODED AT INBD AND OUTBD BORES. RT WING OUTBOARD FLAP OUTBD HINGE (FLAP SIDE) ACTUATOR ATTACH LUGS INBOARD AND OUTBOARD BORES REPAIRED AS PER FEDEX EA 1-5740-63186, 2L73 4F RTA22WE 20030924001312003092400131 2003 9 24 AALA20030748 420030709A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21650AA 24608 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000142003092500014 2003 9 25 AALA20030758 420030713A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21630AA 24588 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040129000612004012900061 2004 1 29 SWIA200312733 420031217A346022312664C FDAU EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM07584SW5121 5121 120352 ON DEPARTURE, SMOKE EMITTED FROM FDAU CB ON OVERHEAD PANEL, CEASED WHEN CIRCUIT BREAKER WAS OPENED. REPLACED FDAU CB. SPLICED IN WIRE NR WE01-0023-22 ON RIGHT HAND SIDE. REMOVED AND REPLACED FDAU. SYSTEM OPS CHECK GOOD. 2L72 4T RTA31SO 20040129000622004012900062SO 2004 1 29 SWIA200312734 120031227A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07209SW1185811629 120269 FLAP DISAGREEMENT WHEN RETRACTING FLAPS AFTER TAKEOFF. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06. ALSO REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08 AND RII CARD 27-307. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040129000682004012900068SO 2004 1 29 SWIA200312740 120031231A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07284YV 120284 CENTER CABIN SECTION (ROWS 4-7) EMERGENCY LIGHTS; FLOOR, SIDE AND CEILING; WILL INTERMITTENTLY FAIL BY DIMMING OUT AFTER ILLUMINATING FOR SEVERAL SECONDS DURING TEST. REMOVED AND REPLACED MID BATTERY PACK IAW 33-50-02. OPS CHECK GOOD. S/N OFF: 1076/06-92. 2L72 4T RTA31SO 20031215001162003121500116WP 2003 12 15 AALA20030987 120030909A3350L20191009 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21445AA 49471 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT ENTRY DOOR. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001502003121500150WP 2003 12 15 AALA20031194 120031030A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21241AA 49254 DEN - DURING OVERNIGHT MAINTENANCE, FOUND CEILING EMERGENCY LIGHTS AT STATION 909 INOPERATIVE. REPLACED BATTERY PACK B5-104. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001682003121500168WP 2003 12 15 AALA20031223 120031105A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21412AA 49323 DFW - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY CEILING LIGHTS OVER ROWS 8 THROUGH 11 INOPERATIVE. REPAIRED LOOSE BATTERY CONNECTION FOR EMERGENCY CEILING LIGHTS OVER ROWS 8 THROUGH 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001692003121500169WP 2003 12 15 AALA20031063 120030924A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21462AA 49592 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROWS 13 THROUGH 20. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001722003121500172WP 2003 12 15 AALA20031143 120031010A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21567AM 53293 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHT INOPERATIVE AT SEAT 9D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031215001852003121500185NM 2003 12 15 USAABB03195 120031023A33509221009 BATTERY BOEING757 757225 1384959NM L3 DOOR DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19602AU 22196 PHL - FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031215002022003121500202EU 2003 12 15 USAA030260 120031103A5320D5311278220001 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT CORRODED 6.25 CM LENGTH BY 2.5 CM WIDE BY .125 CM DEEP, LONGITUDINAL FLOOR SUPPORT BETWEEN FRAME 14 AND 21 APPROX BL Y- 1200. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. (M) 2L72 4F RTA28NM 20031216000162003121600016NM 2003 12 16 QXEA200301458 120031104A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- NR 11 SEAT TRACK REQUIRES REPLACEMENT DUE TO DAMAGE THAT IS OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11 AND RD 8-51-102. 2H72 4T RTA13NM 20031216000192003121600019EA 2003 12 16 MASA200300423 120031023A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777302 7302 PHX-BIL, SERVICE DOOR EMERGENCY EXIT SIGN HAD TWO BULBS BURNT OUT. MX RELAMPED THE SIGN, OP CHECKS GOOD. 2L72 4F RTA21EA 20040401000722004040100072NM 2004 4 1 AALA20031112 120031007A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21642AA 24600 LAX - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 10 THROUGH 14. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401000112004040100011EU 2004 4 1 USAA030324 120031230A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW17591 0323 CLT - FOUND SEAT TRACK CORRODED .25 INCH BY .25 INCH, FRONT INBOARD LEG OF SEAT 31 EF. BURNISHED CORRODED AREA PER 53-00-15, .025 INCH REMOVED PER SRM 51-74-00. (M) 2L72 4F RTA46NM 20040401000132004040100013EU 2004 4 1 AALA20031093 120031001A33506104789 BATTERY FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211413A 11376 SAT - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM THE FORWARD TO THE MID CABIN. REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20040401000322004040100032WP 2004 4 1 ASAA0380402 120030421A57535930495504 VANE DOUG DC9 DC982 3022082WP TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP, OUTBOARD VANE PUNCTURED LOWER SKIN AT INBOARD END. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040401000402004040100040EU 2004 4 1 AALA20031221 120031105A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211452B 11464 MSP - DURING OVERNIGHT MAINTENANCE, FOUND AFT LAVATORY AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT LAVATORY AREA EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20040401001342004040100134CE 2004 4 1 E812004F00001 120031222A7500131823EM1400 TUBE BEECH B300 B300 1159232CE BLEED AIR CHAFED B E81RO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL03447TF226 FL364 PILOT REPORTED LT ENGINE BLEED AIR WARNING ANNUNCIATOR ILLUMINATED. DURING TROUBLESHOOTING, FOUND CHAFED LT ENGINE BLEED AIR WARNING EVA TUBING UNDER NR 1R CABIN SEAT AREA. SMALL AIR LEAK FROM AREA CHAFING ON ADJACENT STRUCTURE. SPLICED REPAIRED TUBING AFTER VERIFYING NO BLEED AIR LEAKS IN AREA IAW MM. RETURNED AIRCRAFT TO SERVICE. 2L72 4T RTA24CE 20040401001442004040100144EU 2004 4 1 TRB2004F00005 120031230A3150350A23008314 COMPUTER AEROSPATR42 ATR42300 8680920EU AVIONICS BAY FAULTY A TRBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO21319AM 319 DURING TAKEOFF ROLL THE PITCH ASSYMETRIC WARNING CAME ON. REMOVED AND REPLACED THE CREW ALERTING COMPUTER. 2H72 4T RTA53EU 20031215000722003121500072 2003 12 15 03319309 420031115A6113 SPINNER JETAIRJETSTMJETSTM4101 1500501EU PROPELLER VIBRATES A VTZAK NONE E VIBRATION/BUFFET CRCRUISE 1 EA27309UE 41022 DURING FLIGHT CREW REPORTED A VIBRATION. THE PROPELLER SPINNER WAS IDENTIFIED AS THE SOURCE OF THE PROBLEM AND WAS SHIMMED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031215000742003121500074NM 2003 12 15 03316419 120031112A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27419FJ 3173 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLY WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031215000802003121500080NM 2003 12 15 AWXA200301466 120031105A532065C161215 BRACKET BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - EES - DURING C-15 CHECK CORROSION WAS FOUND ON L-1 DOOR FORWARD GIRT BAR ATTACH BRACKET ASSEMBLY AT BS 304. MAINTENANCE REMOVED AND REPLACED L-1 DOOR FORWARD GIRT BAR ATTACH BRACKET ASSEMBLY IAW B737-300 SRM 51-40-02, PG 1. 2L72 4F RTA16WE 20031215000812003121500081SO 2003 12 15 C2XA03SH467 120031119A711014576057621 STRUCTURE EMB 145 EMB145ER 3260211SO LT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE LEFT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031215000832003121500083NM 2003 12 15 PCAA0311142 120031119A323282970018007 ACTUATOR DHAV DHC8 DHC8102 2809003NM LT MLG DOOR FAULTY A PCAAO OTHER J WARNING INDICATION CLCLIMB 1 EA13821EX462 173 DURING CLIMB, AIRCRAFT 821EX, FLIGHT 3651 IN MIDDLETOWN HAD LEFT GEAR DOOR LIGHT REMAIN ILLUMINATED AFTER THE GEAR WAS RETRACTED. GEAR WAS CYCLED PER CHECKLIST, LIGHT STILL EXISTED. LAGUARDIA MAINTENANCE REPLACED THE LEFT GEAR DOOR ACTUATOR AND RIGGED AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000982003121500098NM 2003 12 15 MWEA030448 120031120A5320993053865 WEB DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 SUBFLOOR BELOW FORWARD LEFT LAVATORY HAS A CRACK AT LIGHTNING HOLE WHERE DRAIN LINE GOES THROUGH. 2L72 4F RTA6WE 20031215001112003121500111WP 2003 12 15 AALA20030997 120030914A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21581AA 53158 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTING INOPERATIVE, ON CEILING AT SEAT ROWS 16 THROUGH 22. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001182003121500118WP 2003 12 15 AALA20030975 120030908A33508039001 BATTERY DOUG DC9 DC982 3022082WP AFT AIRSTAIRS DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21407AA 49318 SAT - FLT 1854 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE AT AFT STAIRS. REPLACED BATTERY B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001202003121500120WP 2003 12 15 AALA20030990 120030910A3350203BC1021 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21489AA 49682 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROW 20 THROUGH 22. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001302003121500130WP 2003 12 15 AALA20031102 120031003A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217519A 49896 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE AFT GALLEY DOOR SECTION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001312003121500131WP 2003 12 15 AALA20031115 120031006A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 AUS - FOUND DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT PACK B5-2. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001342003121500134WP 2003 12 15 AALA20031167 120031026A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21262AA 49290 RDU - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY OVERHEAD LIGHTS 29 DEF TO 33 DEF INOPERATIVE. REPLACED BATTERY PACK AT B5-10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040308001362004030800136NM 2004 3 8 ASAA0310241 120030327A71102024T42032 ANGLE BOEING737 737298C 1384490NM NR 1 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL ANGLE AT NACELLE STATION 143.60 CHAFED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040309001602004030900160WP 2004 3 9 GTIA031057 120031203A5753 VANE DOUG DC9 DC981 3022081WP T/E FLAP DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT WING INBOARD FLAP INBOARD FIXED VANE DELAMINATED. REPAIRED RIGHT WING INBOARD FLAP FIXED VANE. (M) 2L72 4F A6WE 20040309001612004030900161WP 2004 3 9 GTIA031059 120031112A57535935915501 JOINT DOUG DC9 DC981 3022081WP T/E FLAP CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT WING FLEX JOINT CORRODED. REMOVED RIGHT WING FLEX JOINT BAR. INSTALLED NEW RIGHT WING FLEX JOINT BAR. (M) 2L72 4F A6WE 20040309001622004030900162WP 2004 3 9 GTIA031060 120031112A5755 STRUCTURE DOUG DC9 DC981 3022081WP SPOILER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT WING GROUND SPOILER DELAMINATED. REPAIRED DELAMINATION. (M) 2L72 4F A6WE 20040129000802004012900080NM 2004 1 29 P5CA0401022 120030105A3620 WARNING LIGHT BOEING747 74746NF 13848BTNM BLEED OVERHEAT ILLUMINATED A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23450PA 30808 BLEED OVERHEAT / PRU EICAS MESSAGE NNC 2.3. GROUND TESTED PER MM 36-11-00 TEST PASSED. NO MESSAGE FOUND ON EICAS WHEN RETURNED TO BLOCKS. 2L74 4F RTA20WE 20040129000832004012900083EU 2004 1 29 DHL2003802015 220031231A7532 BLEED VALVE DOUG DC8 DC873 302199CWP CFMINTCFM56 CFM563C 13802EU ENGINE MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01802DH 46076 ENGINE NR 3 AND 4 OVER PRESSURE LIGHTS ILLUMINATED AFTER BRAKE RELEASE DURING TAKEOFF ROLL. RTO PERFORMED. CONFERRED WITH MX AFTER LIGHTS EXTINGUISHED AND CONTINUED FLIGHT. NOTED BY MX NO REJECTED T/O INSPECTION REQUIRED DUE TO ZERO AIRSPEED AND MINIMAL BRAKING. PERFORMED THE NECESSARY TROUBLESHOOTING TO ISOLATE NR 3 AND NR 4 ENGINE OVERPRESSURE LIGHT ILLUMINATING AT TAKEOFF POWER. NO FAULT FOUND PER WDM 36-3-2. REMOVED AND REPLACED NR 4 BLEED AIR REGULATOR VALVE PER DC-8 M/M 36-12-1. OPS CHECKED SERVICEABLE PER JRH 12.2 OF NR 3 AND 4 ENGINE. 2L74 4F4 FRT4A25 E21EU 20040129000852004012900085NM 2004 1 29 CALA0300727 120031231A53216552457502 FLOOR PANEL BOEING737 7373T0 1384582NM AFT LAV CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912322 23373 REMOVED AFT LAV WEBS TO FACILITATE REPAIR OF APB. REMOVED AND REPLACED WEBS PER SRM 51-10-02. CRACKED 2 X 5 INCH. 2L72 4F RTA16WE 20040129000892004012900089NE 2004 1 29 P5CA0401023 220031221A7230 BLADE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE BIRD STRIKE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 702186 DURING POST FLT INSPECTION FOUND BIRD STRIKE DAMAGE TO NR 4 ENG. REMOVED AND REPLACED FAN BLADE SET PER WIC M 7111-001. REPLACED NOSE COWL PER WIC M 7220-001 ENG INSPECTION CARRIED OUT PER 72-00-00 NIL DEFECTS. 2L74 4F4 F A20WE E3NE 20040128000252004012800025 2004 1 28 RAIA00312322 420031218A3418 COMPUTER EMB 145 EMB145LR 3260212SO STALL WARNING MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03832HK 145771 RIC- ANGLE OF ATTACK NR 1 FAIL INDICATION. MAINTENANCE RERACKED STALL PROTECTION COMPUTER. 2L72 4T RTT00011AT 20040128000432004012800043WP 2004 1 28 ABXA030489 120031212A5330591143263 SKIN DOUG DC9 DC941 302207NWP AFT FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 FUSELAGE SKIN WAS CRACKED AT LONGERON 3 RIGHT, STA 1163. REPAIRED SKIN WITH DOUBLER IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040128000872004012800087NM 2004 1 28 AWXA200301630 120031208A53206545402581 ANGLE BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MINOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON RT AIR CONDITIONING BAY AFT WALL L-ANGLE AT INBOARD END ABOVE TURBO FAN BS 663, RBL 23. MAINTENANCE REMOVED CRACKED L-ANGLE AT BS 663, RBL 23; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45402; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12, PG 38 & 1. 2L72 4F RTA16WE 20040128000892004012800089NM 2004 1 28 AWXA200301635 120031229A261365528087 CONTROL UNIT BOEING737 7373G7 1384595NM ZONE 205 MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28309AW601391058 24711 ON CLIMBOUT OF PHX EN ROUTE FOR RNO RT WING TO BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH BOOK PROCEDURES AND SYSTEM RETURNED TO NORMAL, THEN LIGHT CAME BACK ON, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED VISUAL INSPECTION OF RT AIR CONDITIONING BAY AND RT WING LEADING EDGE AREAS, NO DEFECTS WERE NOTED. RAN PACK WITH ENGINES RUNNING TO CLIMB POWER FOR 20 MINUTES, NO DEFECTS NOTED. AS A PRECAUTION REMOVED AND REPLACED ACCESSORY COMPARTMENT OVERHEAT CONTROL UNIT IAW BMM 26-10-02, OPERATIONAL CHECK WAS GOOD. BENCH TEST OF ACCY BAY OVERHEAT CONTROL UNIT WAS NO FAULT FOUND. PERFORMED SB 65-52808-26-01 REPLACING A2 & A4 MODULES, UNIT TESTED GOOD PER CMM 26-10-32, REV. 12. 2L72 4F RTA16WE 20040128001492004012800149NM 2004 1 28 QXEA200301589 120031220A5310 MOUNT DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- LOWER INNER TRUSS MOUNT TUBE HAS FIVE CHAFED SPOTS IN A FOUR INCH AREA NEAR THE FUEL FLOW TRANSMITTER. REPAIRED IAW DHC-8 RD 8-54-0361 AND 8-54-1869. 2H72 4T RTA13NM 20040128001622004012800162NM 2004 1 28 QXEA200301606 120031219A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- RIGHT HAND INBOARD NR 7 SEAT TRACK HAS CORROSION AT STATION X226.0. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-1102. 2H72 4T RTA13NM 20040128001692004012800169NM 2004 1 28 AWXA200400004 120031205A5315654583475 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM AT FASTENER HOLE BS 344, RBL 7. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM CHORD; FABRICATED A NEW REPLACEMENT SECTION OF CHORD, 2 EACH REPAIR ANGLES, & 3 EACH WEB STIFFENERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, FIG 205, PG 221-223. 2L72 4F RTA16WE 20040128001782004012800178NM 2004 1 28 SCNA03009 120031225A3350 LENS BOEING737 737800* NM EMER EXIT SIGN MISSING A SCNAK NONE O OTHER ININSP/MAINT 1 GL15PHHZI 28380 DURING ROUTINE MAINTENANCE FOUND THE R2 DOOR MISSING LENS FOR EMERGENCY EXIT. INSTALLED EXTIT LENS AT R-2 DOOR, OPS CHECKED GOOD. 2L72 4F RTA16WE 20040128001972004012800197NM 2004 1 28 DHL200342535 120031205A5320651986311 STIFFENER BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPON REMOVAL LT NLG TRUNNION THE VERTICAL STIFFENERS SUPPORT FWD & AFT (2 EA) FOUND CRACKED NDT CONFIRMED. DRILLED UP NEW PARTS P/N 65-19863-11 PO3348189 & P/N 65-19863-9 PO3348189 USING EXISTING FASTENER HOLES IAW B727 SRM 51-30-05 & 51-30-06. ALODINE, PRIMED AND PAINTED PARTS IAW B727 SRM 51-10-02 AND INSTALLED VERTICAL STIFFENERS IAW B727 SRM 51-30-02. 2L73 4F A3WE 20040128002012004012800201NM 2004 1 28 SWA2004F00002 120031031A5744654792327 SPAR BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE WBL CRACKED D SWAAO OTHER O OTHER NRNOT REPORTED 1 NM01379SW 26584 SPAR CRACKED. 2L72 4F4 FRTA16WE E2GL 20040129000232004012900023NM 2004 1 29 AWXA200400010 120031204A575369743235 CHANNEL BOEING737 73733A 1384673NM TE FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON NR 3 FLAP TRACK FAIRING SPRING DOOR ANCHOR BRACKET (CHANNEL) WBL 197 LT. MAINTENANCE REMOVED CRACKED NR 3 FLAP TRACK FAIRING SPRING DOOR CHANNEL AT WBL 197 LT; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, PG 1-45. 2L72 4F RTA16WE 20040309001582004030900158WP 2004 3 9 GTIA031055 120031112A5730 PANEL DOUG DC9 DC981 3022081WP RT WING CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT WING PANEL 1242C HAS CORROSION 3 PLACES. FABRICATED NEW WING PANEL EA 5730-0311. (M) 2L72 4F A6WE 20040309001662004030900166 2004 3 9 GTIA031070 420031230A2565D29982107 SLIDE DOUG DC9 DC983 3022083WP R1 DOOR TORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 LGA - R1 DOOR ESCAPE SLIDE RIPPED ALONG GIRT BAR. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE. (M) 2L72 4F RTA6WE 20040308001932004030800193NM 2004 3 8 ASAA0310676 120031222A53206567140509 FLOOR SUPPORT BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOOR SUPPORT AT FUSELAGE STATION 660, RIGHT BUTTOCK LINE 48, RIGHT BUTTOCK LINE 52 CORRODED. REPAIRED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20040308001972004030800197NM 2004 3 8 ASAA0310609 120031231A531565549101 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 847, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 61 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040309001652004030900165WP 2004 3 9 GTIA031066 120031227A3260833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23833NK 49449 FLL - NOSE GEAR RED LIGHT STAYS ON DURING FLIGHT STARTED IN PATTERN FOR LANDING LEFT AND RIGHT GEAR LIGHTS GO OUT WHEN THROTTLE GOES FORWARD. JACKED A/C NOSE AND PERFORMED OPS CHECK ON GEAR SWING, COULD NOT DUPLICATE MALFUNCTION. REMOVED AND REPLACED NOSE GEAR UP PROX SENSOR. CHECKED AIR GAP WITH GEAR UP. WITHIN LIMITS AT .065. NO FAULTS NOTED ON GEAR RETRACTION. (M) 2L72 4F RTA6WE 20040316000352004031600035WP 2004 3 16 ASAA0380291 120030404A532199366405 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOORBOARD LOWER SURFACE CORNER IS CRACKED. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20040316000152004031600015NM 2004 3 16 ASAA0370018 120031024A5321146A940121 STRAP BOEING737 737790 13844CNNM FLOOR PANEL CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01617AS 30542 OAK - DURING C-CHECK, FOUND FLOOR PANEL SUPPORT STRAP IS CORRODED AT FS 887. REPLACED STRAP PER MM 51-40-02. (M) 2L72 4F RTA16WE 20040316000932004031600093WP 2004 3 16 ASAA0380356 120030418A5310592600383 SUPPORT BEAM DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND MID CARGO BAY BARRIER DOOR SUPPORT BEAM IS CRACKED. INSTALLED DOUBLER ON BEAM PER SRM 51-10-3. (M) 2L72 4F RTA6WE 20040316001022004031600102WP 2004 3 16 ASAA0380307 120030411A53205932506113 STRAP DOUG DC9 DC983 3022083WP SIDEWALL SUPPORTCRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, FORWARD CARGO BAY LEFT SIDEWALL SUPPORT STRAP CRACKED. REPLACED SUPPORT PER SRM 53-01. (M) 2L72 4F RTA6WE 20040316001032004031600103WP 2004 3 16 ASAA0380309 120030411A5321995782821 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, E/E FLOOR PANEL IS CORRODED AT FS 160-218. REPLACED SUPPORT PER SRM 53-01 AND 51-30-2. (M) 2L72 4F RTA6WE 20040316001062004031600106WP 2004 3 16 ASAA0380310 120030411A53305936004 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND LOWER FUSELAGE IS DENTED AT FS 294 AT LONGERON 29L. INSTALLED DOUBLER PER SRM 53-04, 51-30-5, AND 51-30-2. (M) 2L72 4F RTA6WE 20040316000252004031600025WP 2004 3 16 ASAA0380285 120030404A5320993653429 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT EXFOLIATED AT FS 200. REPLACED SUPPORT PER SRM 51-10-3 AND 10-4. (M) 2L72 4F A6WE 20040316000682004031600068WP 2004 3 16 GTIA031075 120031219A3397 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND EMERGENCY LIGHTS FAIL OPS CHECK. FOUND CONNECTOR P1-1161 DISCONNECTED. CONNECTED PLUG. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20040316001042004031600104WP 2004 3 16 ASAA0380314 120030414A53409911842115 ATTACH BRACKET DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND TRIM AND LOAD FEEL CENTERING SPRING ACTUATOR ATTACH BRACKET IS CRACKED AT FS 1485. REPLACED BRACKET PER SRM 51-10-3 AND 10-4. (M) 2L72 4F RTA6WE 20040316000312004031600031NM 2004 3 16 ASAA0340332 120031006A33978100022608 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01769AS 25103 DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 25 INOPERATIVE. RECONNECTED WIRE AND OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040304001492004030400149WP 2004 3 4 ASAA0380831 120031215A3397 WIRE DOUG DC9 DC983 3022083WP LIGHT MODULE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 LAX - PREFLIGHT CHECK, ROW 4-5 EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001512004030400151NM 2004 3 4 ASAA0340338 120031106A33508100022608 WIRE BOEING737 737490 1384715NM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01799AS 29270 PDX - DURING MAINTENANCE CHECK, FOUND FORWARD EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. RECONNECTED WIRE. LIGHT THEN OPERATED NORMALLY. (M) 2L72 4F RTA16WE 20040304001622004030400162NM 2004 3 4 ASAA0340364 120031221A3397 CONNECTOR BOEING737 7374Q8 138447QNM EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 ANC - DURING LINE CHECK, FOUND NEAR ROW 13 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040304001592004030400159NM 2004 3 4 ASAA0340365 120031222A3397 CONNECTOR BOEING737 7374Q8 138447QNM EMERGNECY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01754AS 25095 YVR - DURING LINE CHECK FOUND NEAR ROW 14-16 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040308000492004030800049WP 2004 3 8 03FDEA00434 120030411A3097 WIRE DOUG DC10 DC1010 3022110WP NR 2 PYLON DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 COMPLY WITH EA 8-7160-69657, NUMBER 2 ENGINE COWL-ENGINE DRAIN HEATER WIRING RESTORATION. COMPLIED WITH EA 8-7161-69657. ADDED WIRES PER EA 8-7160-69657 NUMBER 2 ENGINE COWL, ENGINE HEATER WIRING RESTORATION. 2L73 4F A22WE 20040308001422004030800142NM 2004 3 8 ASAA0310232 120030326A5311 FRAME BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CHORD AT BS 675, RIGHT BUTTOCK LINE 45 CORRODED. REPAIRED CHORD PER EA. (M) 2L72 4F RTA16WE 20040308001612004030800161NM 2004 3 8 ASAA03100687 120031231A5320654581922 WEB BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REPAIRED WEB PER SRM AND EA. (M) 2L72 4F A16WE 20040308001462004030800146NM 2004 3 8 ASAA0310229 120030326A532065C320674 SPLICE PLATE BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SPLICE PLATE AT BS 661, WING STATION 71R GOUGED. REMOVED AND REPLACED SPLICE PLATE PER SRM. (M) 2L72 4F RTA16WE 20040308001962004030800196NM 2004 3 8 ASAA0310683 120031222A53156567140140 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-663, LEFT BUTTOCK LINE 24 CORRODED. REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040308001432004030800143NM 2004 3 8 ASAA0310227 120030326A532065524571 WEB BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND BULKHEAD FLOOR WEB AT BS 1016-1040, BUTTOCK LINE 0 RIGHT BUTTOCK LINE 40 CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20040309001502004030900150WP 2004 3 9 GTIA031053 120031225A3260833703 DOWNLOCK SENSOR DOUG DC9 DC982 3022082WP NLG FAILED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23804NK 49104 DTW - FLT 417 - FOUND NOSE GEAR DOWN LIGHT FAILED TO COME ON FOR 3 MINUTES AFTER GEAR EXTENSION. T/S NOSE GEAR DOWN LIGHT. REMOVED AND REPLACED NOSE GEAR DOWN LOCK SENSOR AND NOSE GEAR POSITION INTLK LIGHT SWITCH. JACKED AND SWUNG NOSE GEAR, NO DEFECTS NOTED. (M) 2L72 4F A6WE 20040308001922004030800192NM 2004 3 8 ASAA0310681 120031222A5311 FRAME BOEING737 7372Q8C 138448SNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FRAME AT FUSELAGE STATION 500, STRINGER 25L DENTED. REMOVED DAMAGED AREA AND REPAIRED FRAME PER SRM. (M) 2L72 4F A16WE 20040316000062004031600006WP 2004 3 16 ASAA0380354 120030418A5310S92600383 SUPPORT BEAM DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 DURING 15K CHECK, FOUND MID CARGO BAY BARRIER DOOR SUPPORT BEAM CRACKED ON INBOARD SIDE. INSTALLED DOUBLERS ON BEAM PER SRM 52-10. (M) 2L72 4F RTA6WE 20040316000162004031600016NM 2004 3 16 ASAA0370017 120031022A5320BAC1496377 ANGLE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01617AS 30542 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR Z-ANGLE. REPLACED WITH NEW 'Z' ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040316000262004031600026WP 2004 3 16 ASAA0380286 120030404A53129930873107 PRESSURE PANEL DOUG DC9 DC982 3022082WP MLG WW CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND OVERHEAD PRESSURE WEB CRACKED IN RIGHT MLG WHEEL WELL AT FS 995. CUT OUT DAMAGED SECTION AND REPLACED WITH DOUBLER PER SRM 53-04. (M) 2L72 4F A6WE 20040316000362004031600036WP 2004 3 16 ASAA0380292 120030404A5321993654711 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOORBOARD INSERTS MISSING AT FS 150-200. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20040129000282004012900028EU 2004 1 29 MALA030580 120031227A3260 CONTACTOR SAAB SF340 340B 7860101EU MLG INDICATOR DIRTY A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15441XJ 340B441 DURING FLIGHT 3145, RT MAIN GEAR LIGHT BULB INTERMITTENT, HAD TO CYCLE GEAR TWICE TO GET RT MLG LIGHT (GREEN) TO COME ON. MAINTENANCE CLEANED CONTACTS FOR INDICATOR. RELAMPED, OPS CHECK GOOD. 2L72 4T RTA52EU 20040129000702004012900070EA 2004 1 29 SWIA200312742 120031231A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07915SW2346 2346 7615 EN ROUTE FLAPS FAIL CAUTION MESSAGE. REPLACED FECU. OPS CHECK GOOD. 2L72 4F RTA21EA 20040129001482004012900148NM 2004 1 29 DHL200374256 120031203A5522 SKIN BOEING727 727225 1384077NM ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, RT ELEVATOR HAS TWO DINGS IN UPPER SKIN AT 30 INCHES FROM I/B EDGE, AND AT 30 INCHES O/B OF TAB CUTOUT. DENTS FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-20-1 FIG 1. REMOVED 2 EA DAMAGED AREAS DIM .250 DIA AND FABBED REPAIR DOUBLERS FROM 2024-T3 .032 PO9912070 DIM 6 X 3.5 INCH AND 45.5 X 3.875 INCH IAW B727 SRM 55-20-3 FIG 4. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 & INSTALLED IAW B727 SRM 55-20-3 FIG 4. CALCULATED ELEVATOR MOVEMENT TO BE 124.25 AND WITHIN THE .20_+_20 LIMITS IAE B727 SRM 51-80-7. 2L73 4F A3WE 20040130000252004013000025NM 2004 1 30 SWAA032804 120031223A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN FLOOR ACTIVATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29725SW 27857 EEPLS INOP AT FWD END. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20040130000642004013000064WP 2004 1 30 UPS04841698 120030106A5310 SHEAR TIE DOUG DC8 DC871F 302199DWP AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, STA 1766 AFT SIDE SHEAR TIE IS CRACKED AT LOWER END BETWEEN LONGERON 9L AND 10L. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B. 2L74 4F RT4A25 20040130000682004013000068EU 2004 1 30 04007307 120030107A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27307UE 41021 DURING INSPECTION A SECTION OF EMERGENCY LIGHTING WAS FOUND INOPERATIVE. THE BATTERY AND POWER SUPPLY WERE FOUND TO BE THE CAUSE OF THE FAULT AND WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040130000802004013000080NM 2004 1 30 DHL2003742556 120031203A5522 SKIN BOEING727 727225 1384077NM RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, RT ELEVATOR HAS TWO DINGS IN UPPER SKIN AT 30 INCHES FROM I/B EDGE, AND AT 30 INCHES O/B OF TAB CUTOUT. AT EACH DENT FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-20-1 FIG 1. REMOVED 2 DAMAGED AREAS DIM .250 DIA AND FABBED REPAIR DOUBLERS FROM 2024-T3 .032 PO 9912070 DIM 6 X 3.5 INCH AND 4.5 X 3.875 INCH IAW B727 SRM 55-20-3 FIG 4. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 & INSTALLED IAW B727 SRM 55-20-3 FIG 4. CALCULATED ELEVATOR MOVEMENT TO BE 124.25 AND WITHIN THE .20_+_20 LIMITS IAE B727 SRM 51-80-7. 2L73 4F A3WE 20040130001032004013000103NM 2004 1 30 DHL200374274 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742 21290 DURING C-CHECK, FUSELAGE EXTERIOR BS 620 STR 10R LAP SEAM VERIFIED REPAIRS DONE FOR STRUCTURAL REPAIRS MANUAL COMPLIANCE. EVALUATED REPAIR AND FOUND IT TO BE NON-COMPLIANT IAW 727 SRM 53-30-3 FIG 24. REMOVED PREVIOUS REPAIR AND FABBED NEW STRUCTURAL FILLER FROM 2024-T3 .063 PO 90024 DIM12.25 X 5.75 INCH AND DOUBLER FROM 2024-T3 .071 PO 90024 DIM10.25 X 9.25 INCH IAW 727 SRM 53-30-3 FIG 24. PARTS TREATED AND PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 53-30-3 FIG 24. 2L73 4F A3WE 20040128001382004012800138NM 2004 1 28 QXEA200301594 120031226A3040SYLZ50970 CONTROLLER DHAV DHC8 DHC8201 2809001NM ZONE 200 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09368PH318 512 PSC FLIGHT 2239 EN ROUTE FROM ALW TO SEA, CAPTAIN SIDE WINDOW HOT LIGHT ILLUMINATED, DIVERTED TO PSC. REPLACED TEMPERATURE CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040128001462004012800146EU 2004 1 28 MALA030573 120031214A5347 MOUNT SAAB SF340 340B 7860101EU LAVATORY CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15403XJ 340B403 DURING 4K INSPECTION IN LCQ, FWD LAV AFT I/B MOUNT HAS EVIDENCE OF CORROSION. MAINTENANCE REMOVED CORRODED LAV MOUNT, FABRICATED NEW MOUNT AND INSTALLED, IAW MESABA EO S25063, REV 0 DATED 19 DEC 2003. A/C RELEASE DATE 12/24/03. 2L72 4T RTA52EU 20040128002072004012800207WP 2004 1 28 UPS04841682 120031229A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:C3 RT WING L/E UPPER RIB IS CRACKED AT XFS 841. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040128002102004012800210WP 2004 1 28 UPS04841685 120031229A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LT WING L/E UPPER RIBS ARE CRACKED AT XFS 747.5, XFS 766.25, XFS 797.5. STOPDDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATED CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040129000072004012900007EA 2004 1 29 COMA0360578 120031226A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01815CA9256 7397 FLIGHT 5039 HYDRAULIC NR 2 LOW PRESSURE CAUTION. REPLACED THE RT ENGINE HYDRAULIC PUMP. 2L72 4F RTA21EA 20040129000382004012900038EU 2004 1 29 MALA030596 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 12D & 12F FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 12D, 12F IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040129000812004012900081NM 2004 1 29 DHL200342541 120031203A5320 WEB BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, STA 870 BELOW RT 70.5 FITTING, WEB IS CRACKED ON FWD SIDE. REMOVED AT STA 870 R/T 70.5 FITTING WEB ON FWD SIDE IAW B727 SRM 51-30-2, FABRICATED NEW WEB DIMENSIONS 12 X 6 INCH USING 7075-T6 .050 PO90096 IAW B727 SRM 51-10-2 FIG 3. ALODINED AND PRIMED NEW WEB IAW B727 SRM 51-10-2 AND INSTALLED NEW WEB IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040129002032004012900203NM 2004 1 29 F3LA200300190 120031231A5330 SKIN BOEING737 73736N 1384408NM FUSELAGE DENTED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED CREASED DENT IN EXTERNAL FUSELAGE SKIN AT STA 368, 4 IN BELOW STR 18R. REPAIRED PER SRM 53-00-01 FIG 202. 2L72 4F RTA16WE 20040130000272004013000027 2004 1 30 SWAA032820 420031228A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. READJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040130000632004013000063WP 2004 1 30 UPS04841696 120031229A573036412561 DOUBLER DOUG DC8 DC871F 302199DWP LEFT WING LE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LT WING L/E INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN XFS 622.75 TO XFS 610, LOWER INTERNAL DOUBLER AT PANEL OPENING. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641256 AND SRM 51-1-21. 2L74 4F RT4A25 20040130001072004013000107NM 2004 1 30 DHL200374278 120031203A5330 SKIN BOEING727 727225 1384077NM FUSELAGE CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSELAGE DOUBLER BETWEEN STA 720C- 720D LBL 6 STR 28L IS CHAFED BY RAM AIR DUCT. REMOVED OLD DOUBLER REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR FROM MAT 2024-T3 .125 PO 9912571 DIM 12.5 X 8.875 INCH IAW B727 SRM 53-30-2 FIG 3. TREATED AND PRIMED DOUBLER REPAIR IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040130001082004013000108EU 2004 1 30 MALA030607 120031229A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4Y/2Y INSPECTION IN LCQ, FS 640-686 LEFT I/B SEAT TRACK HAS CORROSION. MX REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060 DATED 3 NOV 2003 REV II. A/C RELEASE DATE 01/09/04. REFER TO 1196389 FOR ADDITIONAL DETAIL. 2L72 4T RTA52EU 20040130002032004013000203WP 2004 1 30 ABXA040013 120031208A5313 LONGERON DOUG DC8 DC861 3021952WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 FORWARD CARGO STA 300 TO 320, LONGERON 32 LEFT, ATTACH ANGLE HAD CORROSION. REMOVED CORROSION AND REPAIRED LONGERON IAW REA D853-48497MR AND DC-8 SRM 53-2-0. 2L74 4F 4A25 20040130002082004013000208WP 2004 1 30 ABXA040014 120031124A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 R2 AFT SERVICE DOOR, UPPER AFT CORNER HAD CRACK INDICATION. REPAIRED CRACKED AREA, INSTALLED REPAIR DOUBLERS IAW DC-8 SRM 53-2-0 AND REA D853-48479MR. 2L74 4F 4A25 20040130002112004013000211WP 2004 1 30 ABXA040004 120031203A531397549273 LONGERON DOUG DC8 DC861 3021952WP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 AFT CARGO AT STA 1180, LONGERON 26 LEFT, LONGERON HAD CORROSION. REMOVED CORROSION, CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPAIR ANGLES AND WEB SPLICE, ALODINED, AND PRIMED IAW DC-8 SRM 51-1-8, 53-2-0, 53-2-2, 51-1-21, 51-1-20D, AND REA D853-48485MR. 2L74 4F 4A25 20040129000952004012900095WP 2004 1 29 0400029935 120031227A5315 FLOORBEAM DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011332U 47404 DURING M-CHECK FOUND CORROSION ON FLOORBEAM WEB AT BS 996 RBL 50. REPAIRED PER EA 99-197352. 2L72 4F A6WE 20040129001042004012900104NM 2004 1 29 DHL2003742540 120031124A5744 MOUNT BOEING727 727225 1384077NM LE FLAP ACTUATORCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 5 KRUEGER FLAP ACT MOUNT IS CRACKED INBD 2 PLACES, OTBD 1 PLACE. REMOVED NR 5 L/E FLAP ACT SUPPORT BRACKETS IAW B727 SRM 51-30-02, FABRICATED PER SAMPLE I/B & O/B SUPPORT BRACKETS 7075-T6, .063 PO900226 (6 X 8 INCH) IAW B727 SRM 57-20-02 FIG 1. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-02, INSTALLED BOTH I/B & O/B SUPPORT BRACKETS IAW B727 SRM 51-30-02, OP/LEAK CHECK GOOD IAW B727 MM 27-81-00. 2L73 4F A3WE 20040129001432004012900143NM 2004 1 29 MWEA040004 120031219A5321995782663 FLOORBOARD DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CORROSION FOUND ON UPPER SKIN OF A FLOORBOARD UNDER THE FIRST OFFICERS CHAIR. REMOVED AND REPLACED FLOORBOARD. 2L72 4F RTA6WE 20040130000292004013000029NM 2004 1 30 SWAA032822 120031228A575465C26686 SKIN BOEING737 7373H4 1384600NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C2 CHECK, FOUND NR 3 L/E SLAT LOWER T/E SKIN CRACKED AT FASTENER'S ROW. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20040130000352004013000035NM 2004 1 30 SWAA032828 120031228A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING PREFLIGHT CK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040130002162004013000216WP 2004 1 30 ABXA040018 120031223A53115911448503 FRAME DOUG DC9 DC932 3022066WP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 FUSELAGE FRAME HAD LEVEL 2 CORROSION AT LONGERON 30, STA 813. REPAIRED AREA IAW DC-9 SRM 53-03. 2L72 4F A6WE 20040130002462004013000246EA 2004 1 30 SWIA200312760 120031128A5415 RIB CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 LT PYLON FS 605 RIB CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIB IAW CRJ SRM 51-40-11. P/N: 601-37004-85. 2L72 4F RTA21EA 20040130000322004013000032NM 2004 1 30 SWAA032825 120031228A33501000679 LIGHT BOEING737 7372T4 1384492NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20040130000782004013000078EA 2004 1 30 04006678 120030106A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27678BR 7653 DURING AIRCRAFT OPERATION THE CREW REPORTED A FLAP CONTROL SYSTEM FAILURE AT ZERO DEGREES. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040130000982004013000098NM 2004 1 30 DHL2003753501 120031229A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, FUSELAGE EXTERIOR SKIN 23R BS 440 DENTED (THIS IS A PREVIOUSLY MARKED DOT). DENT AT FUSELAGE EXTERIOR SKIN 23R BS 440 FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. REMOVED CREW 02 BOTTLE AND BRACKET IAW B-727 SRM MM 12-15-11. REMOVED FASTENERS B-727 SRM 51-30-2. CUT OUT DAMAGED 3.25 X 1.75 B-727 SRM 53-30-3. FABRICATED DOUBLER MAT USED 2024 T3 .050 PO 900471 DIM 10.5 X 7.25 INCH IAW B-727 SRM 53-30-3, FILLER AND TWO SHIM MATERIAL USED 2024 T3 .050 PO 900471 DIM FILLER 3.25 X 1.75 INCH SHIM 5 X 1.25 INCH AND 3.25 INCH X 1.125 INCH IAW B-727 SRM 53-30-3. TREATED , ALODINED, AND PRIMED SRM 51-10-2. INSTALLED DOUBLER AND FILLER AND TWO REPAIR IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040202001372004020200137NM 2004 2 2 UPS04541742 120031231A5347144N50802 INTERCOSTAL BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE: C, CORROSION ON INTERCOSTAL BS 900 RBL 24 - 45 WL 208. INTERCOSTAL FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW DWG 144N5081 & SRM 51-40-02. 2L72 4F RTA2NM 20040130001122004013000112SO 2004 1 30 MASA200300495 120031215A3350 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW07855MJ3290 145614 SUPP ASH 2710, PHL. AFT EMERGENCY LIGHTING FLOOR PROXIMITY LIGHTING STRIP WIRE BROKEN. MX PLACED ON MEL. 12/15/2003 MX REPLACED STRIP. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040130001702004013000170NM 2004 1 30 DHL2003752500 120030106A5315 STRAP BOEING727 727223 1384074NM FLOORBEAM CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, CABIN FLOORBEAM SUPPORT STRAP CRACKED AT BS 328 0 (SEEN FROM BELOW). CABIN FLOORBEAM SUPPORT STRAP AT BS 328 BL 0 CRACKED IN HALF OUT OF LIMITS IAW B-727 SRM 53-10-1. FABRICATED REPAIR STRAP FROM 7075-T6 .050 SIZE 2.5 X 8 INCH PO 900489 IAW B-727 SRM 53-10-2 FIG 7 AND 51-40-3 FIG 6. TREATED, PRIMED PART AND AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR IAW B-727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040130002242004013000224NM 2004 1 30 AWXA200400036 120031217A5315141N5112 FLOORBEAM BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM THAT EXTENDS UNDER R-1 DOOR THRESHOLD DRAIN PLATE BS 365, RBL 45 TO RBL 62. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM BS 365, RBL 45 TO RBL 62; FABRICATED A NEW REPLACEMENT SECTION OF CHORD, 2 EACH REPAIR ANGLES & STRAPS; INSTALLED REPAIR PARTS IAW B757 SRM 53-00-51 FIG 203, SHTS 1-5. 2L72 4F RTA2NM 20040130002332004013000233EU 2004 1 30 MALA040106 120031229A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, FS 294 RT I/B FWD SEAT TRACK HAS CORROSION. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. REFER NR 1195871 FOR ADDITIONAL INFO. A/C RELEASE DATE 1/6/04. 2L72 4T RTA52EU 20040130002372004013000237EU 2004 1 30 MALA040103 120031226A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, FS 686 RT WL 112 HAS BENT FLANGE. STOP DRILLED CRACK, FABRICATED AND INSTALLED FRAME DOUBLER REPAIR IAW MESABA EO S53152. A/C RELEASE DATE 01/6/04. REFER TO NR 1195871 FOR ADDITIONAL INFO. 2L72 4T RTA52EU 20040203000142004020300014 2004 2 3 ASAA0380588 420030912A25653961896501 LANYARD DOUG DC9 DC983 3022083WP R1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040203000172004020300017WP 2004 2 3 ASAA0380576 120030902A532099115554U16 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 OAK - DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT AFT END OF RT TIE DOWN AT FS 769-788. REPLACED INTERCOSTAL IAW SRM 51-10. (M) 2L72 4F A6WE 20040203000302004020300030WP 2004 2 3 ASAA0380562 120030824A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000322004020300032NM 2004 2 3 ASAA0380564 120030826A3350 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-16. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040203000382004020300038WP 2004 2 3 ASAA0380543 120030727A33501001191 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01974AS1527 1527 53450 ANC - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000542004020300054WP 2004 2 3 ASAA0380632 120031011A335060030451 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. SPLICED IN NEW CONNECTOR WIRE AT ROW 1. ALSO, REPLACED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040203000592004020300059NM 2004 2 3 ASAA0310161 120030320A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 663-727, BUTTOCK LINE 0 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040203000612004020300061NM 2004 2 3 ASAA0310159 120030320A5347655496922 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 727B-947, RIGHT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040203000632004020300063WP 2004 2 3 ASAA03805635 120031013A33506011779 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS2376611055 49103 SEA LINE CHECK, FOUND TWO OVERWING EMERGENCY EXIT LIGHTS FAILED TO OPERATE UPON CHECK. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F A6WE 20040203000712004020300071WP 2004 2 3 ASAA0380762 120031121A53305924802509 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FUSELAGE SKIN DENTED AT STATION 233. INSTALLED DOUBLER PER SRM 53-04, 51-10-3, AND 51-30-5. (M) 2L72 4F RTA6WE 20040203000722004020300072WP 2004 2 3 ASAA0380546 120030729A3397 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 YVR PREFLIGHT CHECK, FOUND FIRST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040130002292004013000229NM 2004 1 30 AWXA200400037 120031217A5320140N05043 FLOOR SUPPORT BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR ATTACH ANGLE BS 440, LBL 64. MAINTENANCE REMOVED CORRODED FLOOR ATTACH ANGLE FROM BS 430 TO BS 450, LBL 64; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 140N0504; INSTALLED REPAIR PART IAW B757 SRM 51-40-02, PG 1 PARA D. 2L72 4F RTA2NM 20040130002412004013000241SO 2004 1 30 SWIA200312755 120031227A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MISSING A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07579SW 120347 EXIT ROW 6 EXIT LIGHT MISSING. REMOVED AND REPLACED EXIT ROW LIGHT WITH A NEW ASSEMBLY IAW 33-00-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20040202001102004020200110EU 2004 2 2 04015327 120030115A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27327UE 41080 DURING INSPECTION THE FOWARD EMERGENCY TRACK LIGHTING WAS FOUND TO BE DIM. THE BATTERY PACK WAS FOUND TO BE DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040202003142004020200314NM 2004 2 2 AWXA200400059 120031227A53207075T6040 WEB BOEING757 7572G7 1384963NM THRESHOLD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .5625 INCH CRACK WAS FOUND ON R-1 DOOR THRESHOLD WEB AT BS 350, RBL 64, STR 17 RT. MAINTENANCE CUT OUT CRACKED AREA OF R-1 DOOR THRESHOLD WEB AT BS 350, RBL 64, STR 17 RT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B757 SRM 51-70-13, FIG 1. 2L72 4F RTA2NM 20040203000072004020300007 2004 2 3 ASAA0380570 420030831A2565D2998282107 LANYARD DOUG DC9 DC983 3022083WP SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 SAN PREFLIGHT CHECK, FOUND FORWARD PAX L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040203000502004020300050NM 2004 2 3 ASAA0310225 120030326A33508821004 BATTERY PACK BOEING737 737210C 1384459NM EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 AFTER RECONFIGURATION, FOUND FLOOR TRACK LIGHTS ON SEAT PALLET 8-13 WOULD NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK, THEN LIGHTS OPERATED NORMAL. (M) 2L72 4F A16WE 20040202001532004020200153WP 2004 2 2 UPS04841750 120031203A531537734421 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, FLOORBEAM IS CORRODED BEYOND LIMITS AT STATION 822 AT LBL 24 UPPER CAP. REMOVED, FABRICATED AND REPLACED FLOORBEAM IAW DWG 3773442 AND SRM 51-3-0, 51-1-20D. 2L74 4F RT4A25 20040203000682004020300068WP 2004 2 3 ASAA0380594 120030921A33970105603 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 SEA PREFLIGHT CHECK, FOUND ONE EMERGENCY FLOOR TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED WIRING. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203000832004020300083 2004 2 3 ASAA0380554 420030813A25653961896501 LANYARD DOUG DC9 DC982 3022082WP L1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01953AS 49386 PDX PREFLIGHT CHECK, FOUND FORWARD PAX L-1 DOOR EMERGENCY SLIDE LANYARD WAS DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20040203000902004020300090WP 2004 2 3 ASAA0380793 120031119A53219936544501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEFECTIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DEBONDED AT FS 160-200. REPLACED FLOORBOARD IAW SRM 53-05. (M) 2L72 4F RTA6WE 20040203001122004020300112EU 2004 2 3 03FDEA02345 120031022A2821 FILTER AIRBUS310 A310 EU FUEL SYSTEM CLOGGED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25423FE 281 ON CLIMBOUT HAD ENG 1 FUEL FILTER CLOG LIGHT ON APPROXIMATELY 100 N1 OUT AT AROUND 90 N1. REPLACED FUEL FILTER PER A310-200 MM 73-12-03 PG 2. LEAK CHECKED NORMAL. RAN ENGINE AT 100 PERCENT N1, NO CLOG LIGHT AT THIS TIME, OK TO CONTINUE. 2L72 4F RTA35EU 20040203003232004020300323EA 2004 2 3 MASA200300468 120031129A3230750006000D SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG UNSERVICEABLE A MASALA ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW0777286 7286 ASH 6146 LAS-SBA, DIVERTED TO LAX FOR A NOSE GEAR THAT WOULD NOT EXTEND. CREW TRIED TO CYCLE GEAR TWICE WITH THE SAME RESULT BEFORE DIVERTING TO LAX. ON APPROACH INTO LAX THE CREW CYCLED GEAR AGAIN AND THE GEAR EXTENDED WITHOUT FAULT. A/C FERRIED TO PHX FOR REPAIR. 2L72 4F RTA21EA 20040203003252004020300325EA 2004 2 3 MASA200300471 120031201A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA T/O CONFIG FALSE INDICATIONA MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775984 7489 ASH 2716 CLT-CMH, ABORTED T/O DUE TO TAKEOFF CONFIG WARNING FOLLOWED BY GND/FLT SPOILER MESSAGE AND CONFIG TRIM MESSAGE. MX PERFORMED AN OPS CHECK OF BOTH SYSTEMS AND FOUND NO DEFECTS. A/C DEPARTED WITHOUT FURTHER PROBLEM. NO PARTS USED. 2L72 4F RTA21EA 20040316000442004031600044EU 2004 3 16 SIMA200402004 120031231A53117253814417 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21901AE 340B401 ABI - DURING AN MBV INSPECTION, THE FRAME AT STA 686.888 WAS FOUND TO BE DENTED ON THE RIGHT SIDE THREE INCHES ABOVE THE FLOOR. REMOVED DAMAGED FRAME SECTION. INSTALLED NEW FRAME IAW SAAB SRM, 72LKS 3079, REV 42, 51-40-21, 51-40-40 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040316000952004031600095WP 2004 3 16 ASAA0380297 120030408A532039446771 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND SPLICE IS CORRODED AT LONGERON 28L BETWEEN FS 1174 AND 1187 IN AFT CARGO BAY. REPLACED SPLICE PER SRM 51-30-5 AND 10-4. (M) 2L72 4F RTA6WE 20040316001072004031600107WP 2004 3 16 ASAA0380312 120030414A53405920838 ATTACH BRACKET DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, E/E ATTACH ANGLE BRACKET IS CRACKED AT AFT SIDE OF TERMINAL END OF LONGERON 7R AT FS 1463. REPLACED BRACKET PER SRM 51-10-2 AND 30-5. (M) 2L72 4F RTA6WE 20040323000172004032300017EU 2004 3 23 BAQA092536 120031215A2422PC251123E INVERTER BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME108 7243 INVERTER LIGHT WILL NOT EXTINGUISH. REPLACED WITH SERVICABLE ASSET UNIT. 02/06/2004 1G72 3U3 U H13EU E5NE 20040323000192004032300019EU 2004 3 23 BAQA092570 120031229A670010545371 ROD END BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE FLT CONTROLS WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1360 7243 MECHANIC SCRAPPED CORE AT SITE. EXCESSIVE PLAY ON UNITS. REPLACED WITH SERVICABLE UNITS. 02/09/2004 1G72 3U3 U H13EU E5NE 20040323000342004032300034NE 2004 3 23 BAQA091670 220031129A732145033501 ECU UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE NR 1 ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH1074 0179 WARRANTY. NR 1 ENGINE WON'T START. UNIT WAS INSTALLED AT A/CTT 16.6. HARDCARDS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/17/2004 1G72 3U3 UO H88EU E42NE 20040323000352004032300035EU 2004 3 23 BAQA092754 120031003A291108233901102 ACCUMULATOR AEROSPAS365 AS365N2 8680815EU HYD SYSTEM LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME7126 6417 HYDRAULIC ACCUMULATOR UNIT LEAKING. REPLACED WITH SERVICABLE UNIT. 02/17/2004 1G72 3U RTH10EU 20040324000032004032400003NM 2004 3 24 ASAA0340340 120031114A5330 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01755AS 25096 GYR - DURING SI CHECK, FOUND DOUBLER AT STATION 907 IS CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040401000122004040100012NM 2004 4 1 AALA20031099 120031002A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21178AA 32398 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN FORWARD COACH SECTION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401000212004040100021WP 2004 4 1 ASAA0380401 120030421A575359304941 VANE DOUG DC9 DC982 3022082WP TE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP, INBOARD VANE BONDED REPAIR HAS DELAMINATED LOWER SURFACE. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040401001422004040100142EU 2004 4 1 TRB2004F00003 120031229A3397 CONNECTOR AEROSPATR72 ATR72212 8680945EU CABIN LIGHTS BURNED A TRBAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO21399AT 399 DURING ENGINE START A ZAPPING NOISE WAS HEARD, LIGHTS FLASHED, RELAYS CLACKED FOLLOWED BY WHITE/BLUE SMOKE IN COCKPIT, ODOR OF BURNING INSULATION. GPU DC CONNECTOR FOUND BURNED. GPU DC CONNECTOR REPLACED. OPERATIONAL CHECK OF ELECTRICAL SYSTEM CHECKED PROPERLY. 2H72 4T RTA53EU 20040401001732004040100173EU 2004 4 1 RO32004F00000 120031208A2810 FUEL CELL BRAERODH125 HS125700A 4230170EU FUSELAGE CHAFED B RO3RK NONE O OTHER ININSP/MAINT 1 CE03949CE82210 NA0343 DURING 48 MO. G INSPECTION, REQUIREMENTS TO REMOVE THE DORSAL FUEL TANK REVEALED SEVERE CHAFING ON THE AFT LOWER TANK SKIN. CHAFING WAS FOUND TO BE CAUSED BY A SEAL RETAINER FLANGE MOUNTED TO THE VERTICAL STABILIZER. AFTER REPAIRS WERE ACCOMPLISHED TO THE TANK, THE SERRATED TANK MOUNT BRACKETS, LOCATED ON THE VERTICAL STABILIZER WERE ADJUSTED TO OBTAIN ACCEPTABLE CLEARANCE BETWEEN THE SKIN AND SEAL RETAINER SO THAT ANY FUTURE CHAFING PROBLEM WOULD BE ELIMINATED. 2L72 4F A3EU 20040407000382004040700038NM 2004 4 7 TSAA0357211 120031119A57306552125 SKIN BOEING737 737230 1384401NM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 BLENDED OUT THE CORROSION, VERIFIED FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. DRILLED AND SPOTFACE FASTENER HOLE. COLD WORKED FASTENER HOLE. ALODINED AND TWO COATS BMS 10-79 TYPE III PRIMER TO BLEND AND SPOT FACE AREA. INSTALLED 1/32 INCHE OVERSIZE PROTRUDING TENSION HEAD HI-LOCKS. REPAIR COMPLETED IAW ECO 3390. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040407000402004040700040NM 2004 4 7 TSAA0353217 120031119A53306547950 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE SKIN, BONDED DOUBLER, AND BEARSTRAP, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED THE REPAIR PARTS AS SHOWN IN 737 SRM 53-30-3, FIGURE 46. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS, AFT CARGO DOOR CUTOUT FORWARD LOWER CORNER P/N 6547950, BS 807. REPAIR COMPLETED IAW ECO 3398. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040407000362004040700036NM 2004 4 7 TSAA0353209 120031111A57206545460 VENT BOEING737 737230 1384401NM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. FABRICATED A .020 INCH EXTERNAL DOUBLER FROM 7075-T6. ALODINED AND ONE COAT BMS 10-11, TYPE I PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. BOND THE EXTERNAL DOUBLER OVER THE BLEND AREA, WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 3387. (M) 2L72 4F RTA16WE 20040316000372004031600037WP 2004 3 16 ASAA0380293 120030404A571099363055 ANGLE DOUG DC9 DC982 3022082WP LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND LEFT WING LEADING EDGE FRAME TIE IS CRACKED AT UPPER AFT END. REPLACED ANGLE PER SRM 51-10-2. (M) 2L72 4F A6WE 20040316000382004031600038NM 2004 3 16 ASAA0310547 120031012A33508821004 BATTERY PACK BOEING737 737290C 138448VNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 JNU - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING AT SEAT PALLET 9 WOULD NOT EXTINGUISH. REPLACED BATTERY PACK, THEN FLOOR TRACK LIGHTS TESTED NORMAL. (M) 2L72 4F A16WE 20040316000642004031600064WP 2004 3 16 GTIA031072 120031117A5310 RECEPTACLE DOUG DC9 DC981 3022081WP EMERGENCY EXIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT AFT EMERGENCY EXIT DOOR JAMB AFT LOWER LOCK PIN RECEPTACLE CRACKED. REMOVED CRACKED RECEPTABLE. INSTALLED RECEPTACLE. (M) 2L72 4F A6WE 20040316000812004031600081WP 2004 3 16 ASAA0380282 120030403A52805930583193 DOOR DOUG DC9 DC983 3022083WP MLG CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND LEFT MLG DOOR CRACKED AT OUTBOARD CORNER. REPLACED EXISTING CORNER DOUBLER PER SRM 52-04. (M) 2L72 4F RTA6WE 20040316000842004031600084NM 2004 3 16 ASAA0380348 120030416A3397 WIRE GULTON DOUG MD80 MD83 3023681NM EMERGENCY LIGHT DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01979AS 53471 SEA PREFLIGHT CHECK, FOUND FIRST CLASS EMERGENCY TRACK LIGHTING INOPERATIVE. REPAIRED DAMGED WIRE AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040316000052004031600005WP 2004 3 16 ASAA0380317 120030414A53405936071 ATTACH ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND 15K CHECK, ATTACH ANGLE IS CORRODED BETWEEN FS 1212 AND 1222 OUTBOARD OF LONGERON 30 IN AFT CARGO BAY. REPLACED ATTACH ANGLE PER SRM 51-10-3 AND 4. (M) 2L72 4F RTA6WE 20040316000092004031600009WP 2004 3 16 ASAA0380284 120030403A53205930544133 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23947AS 53020 OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 256. REPLACED SUPPORT PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040316000332004031600033NM 2004 3 16 ASAA0310545 120031005A3350883200312 TRANSMITTER BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 SEA - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 8-10 AND 14-16 INOPERATIVE. REPLACED BATTERY PACK (P/N 8821004) AT ROW 14 AND TRANSMITTER (P/N 883200312) AT ROW 11, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040316000392004031600039NM 2004 3 16 ASAA0340331 120030922A33978100022608 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01765AS 25102 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT MID CABIN INOPERATIVE. RECONNECTED WIRE AND OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040316000672004031600067WP 2004 3 16 GTIA031074 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND FLOOR PANEL STATION 207-299, CORNERS DELAMINTATED, EDGE SEAL BROKEN OUT. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040316000862004031600086 2004 3 16 ASAA0380303 420030408A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 SEA PREFLIGHT CHECK, FOUND FORWARD RIGHT SERVICE (R1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040316000102004031600010WP 2004 3 16 ASAA0380283 120030403A528059305832 DOOR DOUG DC9 DC983 3022083WP MLG CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND RIGHT MLG DOOR AFT OUTBOARD CORNER CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05. (M) 2L72 4F RTA6WE 20040316000082004031600008WP 2004 3 16 ASAA0380346 120030418A54105930649507 DOOR DOUG DC9 DC983 3022083WP LT NACELLE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, LEFT ENGINE NACELLE CRACKED ON UPPER DOOR. REPLACED DAMAGED SECTION ARE REPAINTED PER SRM 51-10 AND EA 5410-0054. (M) 2L72 4F RTA6WE 20040316000112004031600011WP 2004 3 16 ASAA0380296 120030408A5321993061237 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND FLOOR WEB CRACK AT FS 1250 UNDER SEAT 32 F/D. STOP DRILLED CRACK AND INSTALLED DOUBLER AT RIGHT CUSP MEMBRANE WEB. (M) 2L72 4F RTA6WE 20040316000202004031600020NM 2004 3 16 ASAA0370014 120031002A5610141A48108 WINDOW BOEING737 737790 13844CNNM COCKPIT JAMMED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01613AS 30163 SEA - DURING PREFLIGHT, THE FIRST OFFICERS SLIDING WINDOW WAS JAMMED SHUT. TIGHTENED AFT ROLLER FOOT MOUNT. SLIDING WINDOW OPERATES NORMALLY. (M) 2L72 4F RTA16WE 20040407000682004040700068EA 2004 4 7 A6WA200340208 120031231A27604916405 COMPUTER CNDAIRCL600 CL6002B19 1900309EA SPOILERS FAILED A A6WAO OTHER J WARNING INDICATION LDLANDING 1 GL31436AW 7734 YELLOW 'FLIGHT SPOILER FAULT' AND SPOILER CAS MESSAGES, WHITE CAS MISCOMPARE AND OUTBOARD GROUND SPOILER FAULT MESSAGES. REMOVED AND REPLACED NR 1 SECU COMPUTER. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040407000762004040700076EU 2004 4 7 2004F00094 120031002A5321 FLOORBOARD AIRBUS320 A320233 3930329EU CABIN PUNCTURED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND AFT CABIN FLOORBOARD NR 261DF HAS MULTIPLE PUNCTURES. REPAIRED AFT CABIN FLOORBOARD PANEL NR 261DF. (M) 2L72 4F RTA28NM 20040412001792004041200179WP 2004 4 12 ASAA0380727 120031111A532199365491 INSERT DOUG DC9 DC983 3022083WP FLOORBOARD CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CRACKED INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05 AND 51-10-4. (M) 2L72 4F RTA6WE 20040412000012004041200001WP 2004 4 12 ASAA0380729 120031111A532199365531 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN FLOOR DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 200-256. BOND-REPAIRED EDGE PER SRM 51-90-0. (M) 2L72 4F RTA6WE 20040413000412004041300041NM 2004 4 13 ASAA024017A 120030322A532065479574 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 767-787. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040413000462004041300046NM 2004 4 13 ASAA024015R 120030319A531165C32395 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND DENT ON FRAME AT BS 727F, RBL 22 AND WL 158. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040413000022004041300002NM 2004 4 13 ASAA024018A 120030323A5320654795119 TRIM PANEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND AFT CARGO BAY CORROSION ON FLOOR TRIM PIECE AT STATION 794, RBL 17 AND WL 157. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040413000032004041300003NM 2004 4 13 ASAA024018B 120030323A5320654957323 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND LEFT SKATE ANGLES FOR RAM AIR PLENUM CRACKED AT FORWARD END. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040413000442004041300044NM 2004 4 13 ASAA024015F 120030319A531165C32395 FRAME BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND GOUGE ON FRAME AT BS 807, RBL 4 AND WL 152. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040415000132004041500013GL 2004 4 15 ERAA093705 220030819A7320252464430NH FCU BOLKMS105 BO105A EU ALLSN 250C 250C20B 03013GL ENGINE OUT OF ADJUST A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH S675 FUEL CONTROL IDLES BELOW 59 PERCENT AND WILL NOT ADJUST UP. MAKING VALVE FUEL FLOW ON HOT SIDE, IDLE FOUND ADJUSTABLE, CUTOFF SHAFT LEAKING. A REPAIRED AND TESTED IAW MFG OHM FORM 15-602E. 1G72 3U3 U H3EU E4CE 20040415000212004041500021GL 2004 4 15 ERAA093718 220031016A7320252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED A ERAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 AL03125EH8974 S562 TORQUE SPLIT OF 16 PERCENT. HEAVY DROOPING, HIGH HYSTERISIS. THROTTLE SHAFT BRAKING WORN, INTERNAL DRIVE BEARINGS TOUGH/DRY. REPAIRED AND TESTED IAW MFG OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20040415000902004041500090WP 2004 4 15 ASAA0380740 120031114A5330593666717 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND AFT CARGO COMPARTMENT STATION 1212, 28L UNDER LONGERON SPLICE CORRODED. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20040413000062004041300006NM 2004 4 13 ASAA024017D 120030322A532069434561 STRAP BOEING737 7374Q8 138447QNM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON STRAP UNDER SUB THRESHOLD FRAME AT BS 840-860. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040413000432004041300043NM 2004 4 13 ASAA024015C 120030322A532069165004 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CRACKED INTERCOSTAL AT BS 747-767, RBL 20 AND WL 156. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040415001682004041500168NM 2004 4 15 ASAA024014T 120030318A532069704221 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND FORWARD ENTRY DOOR LOWER AFT SUPPORT ANGLE CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040316000832004031600083WP 2004 3 16 ASAA0380300 120030408A53306AL4VX SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND OUTER FUSELAGE DENTED FROM FS 275-294 AT LONGERON 29 LOCATION. CUT OUT DENTED AREA. INSTALLED DOUBLER AND SKIN PLUG PER SRM 53-04. (M) 2L72 4F RTA6WE 20040316000992004031600099WP 2004 3 16 ASAA0380360 120030418A53205419084 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CRACKED IN FORWARD PASSENGER COMPARTMENT NEAR FLIGHT ATTENDANT SEAT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040316001052004031600105WP 2004 3 16 ASAA0380358 120030418A272059141395 LINK DOUG DC9 DC983 3022083WP RUDDER LIMITER CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, RUDDER THROW LIMITER LINK IS CORRODED. REPLACED LINK PER MM 27-20-06. (M) 2L72 4F RTA6WE 20040323000162004032300016EU 2004 3 23 BAQA092535 120031124A28221176415103 PUMP BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE BOOSTER PUMP INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1767 7243 WARRANTY. FUEL PUMP GROWLING. REPLACED WITH SERVICABLE UNIT FROM CLEV. STOCK. 02/06/2004 1G72 3U3 U H13EU E5NE 20040323000232004032300023EU 2004 3 23 BAQA092582 120031219A6210L621M1010054 BLADE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR CONTAMINATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME3288 0009 WATER IN BLADE. REPLACEMENT FOR BLADE NOT RECEIVED YET. BEING REPLACED WITH SERVICABLE UNIT. 02/09/2004 1G72 3U3 UO H88EU E42NE 20040324000122004032400012WP 2004 3 24 ASAA0380707 120031103A53119919604501 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FRAME IS CORRODED AT FS 1250. REPLACED DAMAGED FRAME SECTION PER SRM 53-03 AND 51-10-2. (M) 2L72 4F RTA6WE 20040324000152004032400015WP 2004 3 24 ASAA0380712 120031103A532199365841 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND PASSENGER FLOORBOARD IS CORRODED AT FS 256. REPLACED FLOOR PANEL PER SRM 53-05 AND 51-10-4. (M) 2L72 4F RTA6WE 20040401000182004040100018NM 2004 4 1 AALA20031116 120031006A3350 BATTERY BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21652AA 24610 ATL - FOUND EMERGENCY ESCAPE FLASHLIGHT INOPERATIVE AT THE AFT FLIGHT ATTENDANT LOCATION. REPLACED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040407000472004040700047NM 2004 4 7 TSAA0353207 120031119A521065C27257 DOOR BOEING737 737230 1384401NM MAIN PAX CRACKED A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ACCOMPLISHED FASTENER HOLE INSPECTION ON HOLES COVERED BY REPAIR. UTILIZED REPAIR PARTS FROM KIT PER FIGURE 1. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED APPROPRIATE REPAIR PER BOEING REPAIR DRAWING. REPAIR COMPLETED IAW BOEING DRAWING AND ECO 1896R1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040407000392004040700039NM 2004 4 7 TSAA0353215 120031125A53136546566 STRINGER BOEING737 737230 1384401NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 CUT OUT AND REMOVED DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES IAW TABLE 1. ALODINE AND APPLIED ONE LAYER OF BMS 10-11, TYPE 1 PRIMER. INSTALLED REPAIR PARTS AND MADE A FAYING SURFACE SEAL PER SRM 53-10-03, FIGURE 1. REPAIR COMPLETED IAW ECO 3394. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040407000742004040700074EA 2004 4 7 A6WA200340206 120031222A2910601R7528639 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM CHAFED A A6WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL31422AW 7341 HYDRAULIC LOW PRESSURE CAS MESSAGE COMPLIED WITH QRH AIR RETURN TO DEN OPERATE NR 1 EDP APPROXIMATELY 45 SECONDS BEFORE DISCONNECT. FOUND NR 1 HYD HIGH PRESSURE INBOUND FLEX LINE RUPTURED AND NR 1 HYD CASE DRAIN LINE CHAFED, CHAFE CAUSED BY LOWER FAIRLEAD WEAR. REPLACED CASE DRAIN LINE AND HIGH PRESSURE FLEX LINE PER AMM. (M) 2L72 4F RTA21EA 20040412001772004041200177WP 2004 4 12 ASAA0380725 120031111A532199365471 INSERT DOUG DC9 DC983 3022083WP FLOORBOARD CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-180. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000112004041500011EU 2004 4 15 ERAA093692 120031204A6320 BEVEL GEAR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL TRANSMISSION DETERIORATED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03298EH5685 1315 TRANSMISSION MAKING METAL. LT INPUT PINION AND BEVEL GEAR BREAKING DOWN, LT INPUT SEAL LEAKING. REMOVED AND SCRAPPED LT PINION AND BEVEL GEAR. INSTALLED SERVICEABLE LT INPUT PINION AND BEVEL GEAR, CLEANED AND INSPECTED ALL CENTER CASE AND LOWER CASE PARTS. ADJUSTED DISTANCE AND BACKLASH AS REQUIRED. REASSEMBLED IAW REM 103. REPLACED LT AND RT INPUT SEAL, COMPLIED WITH LT AND RT FREEWHEEL INSPECTION IAW REM 103. 1G72 3U3 U H3EU E4CE 20040415000142004041500014SW 2004 4 15 ERAA093707 120030910A6210412015300101 BLADE BELL 412 412 1182202SW MAIN ROTOR PIN HOLE A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03169EH8005 33064 DURING INSPECTION FOUND PIN HOLDS IN LEADING EDGE BEYOND LIMITS. SENT FOR REPAIR, INSPECTED PERFORMED 2500 HOUR INSPECTIONS IAW MFG 412 MM CHAPTER 5; REPLACED IB AND OB SPLICE COVERS IAW MFG 412 CR AND O PAGE 86B; TRIMMED IB ABRASION STRIP TANG IAW MFG 204-099-223 VOLUME XVII SECTION 2; REPLACED OB ABRASION STRIP IAW DAL-260; REPAIRED SKIN LOWER SURFACE AT STA 100 AND STA118 TO STA 161 AND AT TIP AND ON UPPER SURFACE AT STA 213 TO STA 214 AND STA 110 TO 127 AND STA 156 TO STA 161 IAW 204-099-223 VOLUME XVII SECTION 3 REV L. APPENDIX B SECTION 1.4.1. REPLACED TIP CAP IAW 412-62-10-800, DAL-683 AND 204-099-233 VOLUME XVII REV L; REPLACED ROOT EROS. 1G72 4U H4SW 20040415000162004041500016NE 2004 4 15 ERAA093709 120031104A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE CRACKED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03 ABRASION STRIP CRACKED AND DEBONDED ON UPPER SURFACE AS INDICATED C-CHANNEL DEBONDED AS INDICATED. ACTION TAKEN: SENT FOR REPAIR. INSPECTED IAW SA 4047-76-5 REV 11; REPLACED ABRASION STRIP IAW RS-005N-III. MODIFIED EXTERNAL DOUBLERS IAW RS-017-1; INSTALLED STAINLESS STEEL TIP COVER IAW RS-017-II. REPLACED BOTH FORWARD INTERNAL DOUBLERS AND REBOND C CHANNEL IAW DRWG. NR 76150-09043 SPEC. 38023-15000; REFINISHED IAW DRWG NR 76150-09043; STATIC BALANCE IAW RS-005N-VI. 1G72 3U H1NE 20040203003322004020300332EA 2004 2 3 MASA200300496 120031215A2720601R27065K1 DAMPENER CNDAIRCL600 CL6002B19 1900309EA INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0775998 7336 ASH 2837 PHL, FLUTTER DAMPENER STATUS MESSAGE. A/C RETURNED TO FIELD. MX REPLACED THE FLUTTER DAMPNERS. OP CHECKS GOOD. 2L72 4F RTA21EA 20040203000272004020300027NM 2004 2 3 ASAA0310168 120030320A53436545845523 FITTING BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NOSE LANDING GEAR ATTACH FITTING AT BODY STATION 294.5, LT BUTTOCK LINE 3, RT BUTTOCK LINE 3 CORRODED. REMOVED AND REPLACED FITTING IAW SRM. (M) 2L72 4F A16WE 20040203000942004020300094WP 2004 2 3 ABXA040036 120031229A2497051306D23392 WIRE DOUG DC8 DC863F 302198FWP GENERATOR BURNED A ABXAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 GL23816AX 46093 NR 3 GENERATOR UNPARALLED LIGHT ILLUMINATED IN FLIGHT, NO VOLTS, NO FREQS. RESET, NO VOLTS, NO FREQS, DISCONNECTED. REPLACED NR 3 ENGINE GENERATOR IAW 24-20-01-4-0002. DURING OPS CHECK, NOTED SPARKS COMING FROM THE TOP OF ENGINE. FOUND T1, T2, AND T3 WIRES SHORTED AT AFT OF THE PYLON CONNECTOR BOX. REPLACED WIRES IN NR 3 ENGINE PYLON (GENERATOR FEEDER CABLES) IAW DC8 MM 24-20-13 AND AVBORNE W/O 24003. ENGINE RUN OPS CHECKED GOOD IAW DC8 MM 24-10-00 AND 71-00-00. 2L74 4F 4A25 20040204000232004020400023WP 2004 2 4 0301969762 120031022A27805919526508 DUCT DOUG DC9 DC941 302207NWP LT AND RT DAMAGED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01762NW 47395 UPON SLAT EXTENSION DURING APPROACH, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED TO THE RIGHT. AS THE AIRCRAFT SLOWED TO BELOW 190 KTS, THE CREW HEARD A SLIGHT BANG AND THE DISAGREEMENT LIGHT EXTINGUISHED. NO MENTION OF COM PROCEDURES AND FLIGHT LANDED WITHOUT FURTHER INCIDENT AT MSP. MAINTENANCE WAS NOT ABLE TO DUPLICATE THE DISCREPANCY AND LUBRICATED BOTH TEE DUCTS. THE TEE DUCTS WERE REPLACED FIVE CYCLES LATER AS REQUIRED. 2L72 4F A6WE 20040204000302004020400030NM 2004 2 4 S03J27069 120030814A27509000040822 CONTROL UNIT BOEING747 747400 NM GE CF6 CF680C2* GL TE FLAPS FAILED W SAJFC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 WP03 30759 B18701 ABORT TAKEOFF AT GRD SPEED 45 KNOTS DUE TO (CONFIG FLAP) MSG APPEARED. CHECKED, FOUND RT OUTBOARD FLAP POSITION TRANSMITTER INTERMITTENT FAILURE. REPLACED RT O/B FLAP POSITION TRANSMITTER AND FLAP OPERATION TEST NORMAL. TSN/TSC OF REMOVED RVDT IS ONLY 230FH. REMOVED RVDT WAS SEND TO MFG FOR INVESTIGATION. MFG SHOP FINDING REVEAL THAT ACCURACY FAILED DUE TO A HANG-UP. THE SHIMMING INSIDE OF RVDT WAS INCORRECT ALLOWING THE TOP GEAR TO HANG-UP ON FIXED GEAR ASSEMBLY. SINCE THE PRODUCTION FAULT OF REMOVED RVDT WAS FOUND BY VENDOR AND NO SIMILAR SQUAWK HAS OCCURRED AFTER THE REMOVAL OF DEFECTIVE RVDT, THE ISOLATION CASE IS DETERMINED. 2L74 4F4 FRTA20WE E23EA 20040204000322004020400032EU 2004 2 4 03FDEA01740 120031015A2121CG7G011 COOLING FAN AIRBUS300 A300B4605R 3930308EU GE CF6 CF680 30025NE ZONE 100 FAILED A FDEAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO25655FE 742 ON BLOCKOUT BETWEEN STARTING NR 1 AND NR 2 ENGINES SMOKE STARTED COMING IN TO THE COCKPIT FROM THE EQUIPMENT BAY. PERFORMED VISUAL INSPECTION OF AVIONICS COMPARTMENT, CHECKED ALL BOXES FOR EVIDENCE OF ODOR, REMOVED RELAY PANEL COVERS LOOKING FOR EVIDENCE OF DAMAGE AND LOOKED AT ALL VISABLE WIRING IN AVIONICS COMPARTMENT WITH NO VISIBLE DEFECTS NOTED. FOUND COOLING FAN FILTER VERY DIRTY/BLOCKED AND SMELLED OF SMOKE. REPLACED COOLING FAN FILTER IAW MM 21-21-16-4. ORDERED AVIOINCS COOLING FAN AND SMOKE DETECTORS AS PRECAUTIONARY. REMOVED AND REPLACED AVIONICS COOLING FAN REF MM 21-21-11-4 OPS. 2L72 4F4 FRTA35EU E13NE 20040204000332004020400033NM 2004 2 4 03FDEA01582 120030918A5311 FRAME BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20935 AFT LAV SERVICE PAN AREA CORRODED, INCLUDING LOWER ATTACH ANGLE, STRINGER 22L AND 23L AT TERMINAL FITTING AND FS 1166 FRAME FWD AND AFT FACE BETWEEN STR. 20L AND 24L. REMOVED AND REPLACED FRAME AND ATTACH ANGLE IAW B727 SRM 51-30-2 AND 51-40-2. REFERENCE SNRM N01408 W/O 00023584. 2L73 4F RTA3WE 20040204000372004020400037NM 2004 2 4 AWXA200301256 120030929A5350654657715 SKIN BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE TAILCONE ASSY DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MINOR REPAIR - DURING C-17 CHECK FOUND TOP CENTER AREA OF TAIL CONE DISBONDED, 18 INCHES-22 INCHES FROM FORWARD EDGE. MAINTENANCE CUTOUT DISBONDED AREA OF TOP CENTER TAIL CONE, 18 INCH-22 INCHES FROM FORWARD EDGE AND PERFORMED A BOND REPAIR IAW B737-300 SRM 51-70-07, PG. 35, 50, AND 58, FIG. 13. 2L72 4F4 FRTA16WE E2GL 20040204000562004020400056SO 2004 2 4 RAIA00310261 120031015A282123061825 FILTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUEL SYSTEM CONTAMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03818HK 145059 5687-STL- MESSAGE: NR 2 FUEL IMPENDING BYPASS. MAINTENANCE REMOVED AND REPLACED NR 2 FUEL FILTER. 2L72 4T4 FRTT00011ATTE6CH 20040204000612004020400061NM 2004 2 4 DHL2003745021 120031017A3260 CONNECTOR BOEING727 727224 1384076NM PWA JT8 JT8D* NE MLG DOOR LOCK LOOSE A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 UPON GEAR RETRACTION - RED DOOR LIGHT REMAINED ILLUMINATED AND S/O'S AUXILIARY PANEL HAD RIGHT GEAR DOOR LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE IAW AOM. RED DOOR LIGHT WENT OUT WITH GEAR HANDLE UP. CLEANED AND RESET DOOR LOCK SWITCH CONNECTOR, OPS CHECKED NORMAL IAW M/M 32-62-0. 2L73 4F4 F A3WE E2EA 20040203003222004020300322EA 2004 2 3 MASA200300466 120031128A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0777181 7181 ON TAKEOFF ROLL A/C CAME OUT OF TAKEOFF CONFIG, ABORTED T/O. MX RESET SYSTEM, OPS CHECKED OK. 2L72 4F RTA21EA 20040204000712004020400071 2004 2 4 55097AMWA 420031010A341606603062008 ALTIMETER BEECH 1900 1900D 1154162CE COCKPIT MALFUNCTIONED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07131ZV UE131 AFTER TAKE OFF FROM FMN TO ABQ CAPT'S ALTIMETER FLAGGED. AIRCRAFT RETURNED TO FMN WITH NO FURTHER INCIDENTS. 2L72 4T RTA24CE 20040204001472004020400147NM 2004 2 4 EIA2003140 120031020A5530 WEB BOEING747 747212B 1384886NM VERTICAL STAB DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 VERTICAL STAB RT HANDSIDE ACCESS PANEL 324DR AFT WEB AND GUSSET DAMAGED. REMOVED 2 EA. GUSSETS, FABRICATED 2 EA. GUSSETS, SPLICE PLATE, FILLERS (2EA) AND WEB AND INSTALLED IAW ECRA 482-55-183-2 2L74 4F A20WE 20040204002022004020400202EA 2004 2 4 SWIA200312576 120031101A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RUDDER TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07460SW 7803 RUDDER TRIM IS INOPERATIVE, SWITCH WILL TRIM NOSE RT BUT WILL NOT TRIM NOSE LT. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL WITH SERVICEABLE UNIT IAW MM 27-12-10. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040204002052004020400205CE 2004 2 4 GLBA2003142 120031101A3097 WIRE BEECH 1900 1900D 1154162CE TRANSDUCER LOOSE A GLBAD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 NM0397UX UE97 STALL HEAT ANN ILLUM, RESECURED WIRE H91B16 ON TRANSDUCER. 2L72 4T RTA24CE 20040204002072004020400207CE 2004 2 4 GLBA2003144 120031101A324413600LA902A3 BEARING BEECH 1900 1900D 1154162CE WHEEL ASSY FAILED A GLBAO OTHER O OTHER NRNOT REPORTED 1 NM03220GL46 8916 UE220 NR 4 MLG WHEEL ASSEMBLY BEARING SPUN, REMOVED AND REPLACED WHEELS AND MLG STRUT ASSY. 2L72 4T RTA24CE 20040204002092004020400209CE 2004 2 4 00120 120031106A3260 UPLOCK SWITCH LEAR 24 24E 5170316CE GE CJ610 CJ6101 30006NE MLG DIRTY E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05330TW 330 AIRCRAFT DEPARTED YIP FOR RWI SHORTLY AFTER TAKEOFF LT UNSAFE GEAR LIGHT ILLUMINATED, CREW CYCLED GEAR SEVERAL TIMES WHEN GEAR WAS FULLY EXTENDED GEAR LIGHT WOULD GO OUT. RETURN TO DEPARTURE AIRPORT, MAINTENANCE CLEANED AND LUBED LT MAIN GEAR UPLOCK SWITCH AND OPS CHECKED NORMAL. 2L72 4J4 J A10CE 1E16 20040204002112004020400211EU 2004 2 4 034691 120031112A3000 BLEED VALVE SAAB SF340 SF340A 7850100EU ANTI ICE SYS FAILED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1743SZ 340A043 FLIGHT NR 8960 FROM PIT TO CLE. IN ROUTE, AIRCREW RECEIVED THE LT AIR VALVE LIGHT, LIGHT WAS ON AND STEADY. AIRCREW RETURNED TO PIT. WHEN MAINT. GOT TO THE A/C THEY FOUND THE LT ANTI-ICE START BLEED VALVE WAS BAD. REMOVED AND REPLACED VALVE A/C RETURNED TO SERVICE WITH NO FURTHER INCIDENT. 2L72 4T RTA52EU 20040204002132004020400213NM 2004 2 4 CALA0300638 120031024A5310 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714324 23375 MAINTENANCE DISCOVERED HEAVY CORROSION TO THE UPPER SURFACE OF THE HORIZONTAL LEG AND FORWARD SURFACE OF THE VERTICAL LEG ON THE LOWER OUTBOARD FRAME AT BULKHEAD STA 227.8. THE CORROSION WAS CENTERED AT BL 0.0 AND RAN FROM LBL 10 TO RBL 10. 2L72 4F RTA16WE 20040204002142004020400214SO 2004 2 4 GLBA2003146 120031110A610078249046 CONTROL UNIT EMB 120 EMB120ER 3260203SO PROPELLER DAMAGED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0396ZK 13191 120096 RT PROP OVERSPEED, REMOVED AND REPLACED RT PROP TRANSFER TUBE, OVERSPEED GOV PN 8210-160 SN 2252121B HR 9002 10529, PCU OVERSPEED GOV PUMP PN 8210-286 SN 13326287 HR 1493 1567 2L72 4T RTA31SO 20040204002202004020400220EU 2004 2 4 03313303 120031109A2730 SWITCH JETAIRJETSTMJETSTM4101 1500501EU ELEVATOR OUT OF ADJUST A VTZAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 EA27303UE 41015 DURING TAKEOFF CREW REPORTED A CONTROL DISCONNECT WARNING LIGHT. FLIGHT CREW REJECTED TAKEOFF AND PERFORMED QRH PROCEDURES. IT WAS DETERMINED THAT THE FLIGHT CONTROLS WERE NOT DISCONNECTED AND THE CAPTION LIGHT WAS INDICATING A FALSE WARNING. DURING FOLLOWUP MAINTENANCE THE ELEVATOR DISCONNECT WAS READJUSTED WHICH RESOLVED THE FALSE WARNING INDICATION. 2L72 4T RTA41NM 20040204002232004020400223NM 2004 2 4 DHL2003750007 120031112A2910BACH8C08NN0290 LINE BOEING727 7272M7 138407SNM HYD SYSTEM FAILED A DHLAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01750DH 21951 DURING TAXI OUT NR 2 B PUMP LOW PRESSURE LIGHT FLICKERED ON AND OFF. B SYSTEM QUANTITY DECREASED FROM FULL TO 1.5 GAL. NR 2 LOW PRESSURE LIGHT ILLUMINATED STEADY AND NR 1 LOW PRESSURE LIGHT BEGAN FLICKERING ON AND OFF WITH CORRESPONDING FLUCTUATION OF (B) SYSTEM PRESSURE. (B) SYSTEM OVER HEAT LIGHT ILLUMINATED AND TURNED BOTH PUMPS OFF OVER HEAT LIGHT EXTINGUISHED. REMOVED AND REPLACED TWO HYDRAULIC LINES FOR NR 2 B PUMP. OPS AND LEAK CHECKED NORMAL IAW M/M 20-10-12. P/N: BACH8CO8NN0290 AND P/N: BACH30AU06R0280. 2L73 4F A3WE 20040205000252004020500025NM 2004 2 5 EIA2003162 120031021A5313 STRINGER BOEING747 747132 1384882NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FS 1820 RT SIDE STR. 14 FRAME DAMAGE AND BENT STRINGER. REMOVED DAMAGE SECTION OF STRINGER AND REPLACED FRAME IAW SRM 51-30-02, 53-10-23 AND 53-10-03. 2L74 4F A20WE 20040205000332004020500033NM 2004 2 5 EIA2003152 120031024A5311 FRAME BOEING747 747132 1384882NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 NOSE SECTION STR 40 AND 41 FS 330 RT REMOVED TO FOM STA 340 FRAME REWORK. FABBED AND INSTALLED STR 40 AND 41 REPAIR AT STA. 330-340 RT IAW SRM 53-10-03 FIG 3 AND 51-30-02. 2L74 4F A20WE 20040205000362004020500036NM 2004 2 5 UIA9209 120031117A5311 FRAME DOUG MD90 MD9030 3023690NM FUSELAGE CORRODED Z K NONE O OTHER ININSP/MAINT 1 TW0017921 53554 PFM C04 CHK FOUND CORROSION ON FUSELAGE FRAME LOWER TEE CHORD AT STA Y-1437 L29R-L26R, CUT THE CORROSION PORTION OF T-CHRD. TRIM OUT THE INTERCOSTAL FORWARD SIDE, MAKE THE REPAIR PARTS AND INSTALL FASTENERS. 2L72 4F RTA6WE 20040205000512004020500051EA 2004 2 5 ASOA03676 120031223A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURNG A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINT R & R THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD IAW SRM 51-42-20. (M) 2L72 4F RTA21EA 20040205000642004020500064EU 2004 2 5 ASOA03666 120031221A24308260121 CONTROL UNIT AEROSPATR72 ATR72 EU NR 1 GENERATOR INOPERATIVE A ASOAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION APAPPROACH 1 SO11642AS 395 FLT 4193 - DURING VISUAL APPROACH INTO MYR FROM ATL, AT APPROX 1,800 FT THE CREW RECEIVED FAULT INDICATIONS INCLUDING DC NR 1 BUSS OFF AND LOSS OF THE DC NR 1 GENERATOR, INCLUDING AN INTERMITTENT FAILURE OF DC NR 2. THE CREW ALSO LOST COMMUNICATIONS 1 AND THE INTERPHONE. CABIN PRESSURE MADE RAPID FLUCTUATIONS ALONG WITH OTHER SYSTEMS FAILING INTERMITTENTLY. QRH PROCEDURES WERE COMPLIED WITH AN AN EMERGENCY DECLARED. THE AIRCRAFT LANDED SAFELY IN MYR. MAINTENANCE REMOVED AND REPLACED THE NR 1 GENERATOR, NR 1 GENERATOR CONTROL UNIT AND THE DC POWER BUSS CONTROL UNIT. OPS CHECKS DURING ENGINE RUN AND CROSS STARTS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040205000752004020500075EA 2004 2 5 ASOA03660 120031218A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA LT OVERWING INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11879AS 7600 FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE LT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EXTERIOR OVEWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040204000262004020400026NM 2004 2 4 HNAA0300079 120031203A531385320056 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07914HA 53 DURING C CHECK, FOUND CORROSION ON STR31 SEVERE ENOUGH TO WARRANT REMOVAL AND REPLACEMENT FROM X 182 TO F/SPAR X387. IAW EO8-53-0-30-1055 2H72 4T RTA13NM 20040204000522004020400052WP 2004 2 4 UPS03841386 120030923A534037540252 SUPPORT FITTING DOUG DC8 DC873F 302199FWP FWD LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, TORQUE BOX VERTICLE LEG SUPPORT FITTING IS CRACKED AT STA. 340 LONG. 27R. REMOVED AND REPLACED FITTING IAW DWG 3754025, AND SRM. 51-1-20D 2L74 4F RT4A25 20040204000972004020400097NM 2004 2 4 AWXA200301277 120031003A53476546815 SEAT TRACK BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK FROM BS 827 TO BS 867, LBL 45. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SEAT TRACK FROM BS 807 TO BS 867, LBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK, 2 EACH SPLICES, AND A RADIUS FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-52, FIG. 101, AND SRM 53-00-52, FIG. 204. 2L72 4F4 FRTA16WE E2GL 20040204001072004020400107NM 2004 2 4 AWXA200301287 120031002A5312651758349 BULKHEAD BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A .2500 INCH CRACK WAS FOUND ON BS 178 BULKHEAD VERTICAL WEB EMANATING FROM FORWARD INSULATION HOLE AT RBL 17.1, WL 183. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD VERTICAL WEB AT RBL 17.1, WL 183; FABRICATED A NEW REPLACEMENT VERTICAL WEB PER DWG 65-17583; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 12, PG. 1. 2L72 4F4 FRTA16WE E2GL 20040204001082004020400108NM 2004 2 4 AWXA200301288 120030930A575365C2630924 ANGLE BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE RT WING TE FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A .2500 INCH CRACK WAS FOUND ON RT UPPER WING TRAILING EDGE SUPPORT ANGLE ON NR 2 FLAP TRACK OUTBOARD, WBL 204. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE AT WBL 204; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1. 2L72 4F4 FRTA16WE E2GL 20040204001192004020400119EU 2004 2 4 MALA030473 120031018A3020 PRESSURE SWITCH BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE ANTI ICE SYS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15531XJ E2365 DURING FLIGHT NR 3466, ENGINE ANTI ICE NR 1 FAILS AT CLIMB AND FULL POWER SETTINGS. IT WORKS IN CRUISE AND DESCENT. AIR RETURN DUE TO ICING CONDITIONS TO DTW. MAINTENANCE REPLACED LOW PRESS SWITCH ALL CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20040204001822004020400182NM 2004 2 4 PCAA0311134 120031031A2121 FAN DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE COCKPIT FAILED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13827EX 390 CREW REPORTED A BURNING ODOR ABOVE CAPTAINS FLIGHT INSTRUMENTS AND STRONGEST JUST BELOW GLARE SHIELD. MAINTENANCE WAS ADVISED AND FOUND NR 1 ADVISORY FAN TO BE AT FAULT, ASSOCIATED CIRCUIT BREAKER WAS PULLED AND MEL ISSUED, AIRCRAFT THEN RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040204002182004020400218WP 2004 2 4 UPS03841557 120031028A53403755822501N FITTING DOUG DC8 DC873F 302199FWP LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2 BATHTUB FITTING IS CRACKED AT STATION 270 BETWEEN LONG. 35L AND 36. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822 AND SRM. 53-2-0 FIG. 2D 2L74 4F RT4A25 20040205000902004020500090NM 2004 2 5 HALA0301033 120031112A49203802981 APU BOEING767 767300 1385204NM APU BAY FAILED A HALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP13590HA3425 33467 ETOPS SIGNIFICANT SYSTEM, MAINT ENTRY, APU AUTO SHUTDOWN AT THE GATE. BITE CHECK APU ECU FOUND OIL HIGH TEMP FLAG CAME ON. TROUBLESHOOT FURTHER AND FOUND APU OIL COOLING FAN DRIVE SYSTEM NOT TURNING AND GEAR TEETH DAMAGE. REMOVED AND REPLACED APU ASSY IAW HAL M266-767 UP TO STEP 50. COMPLETED HAL M266-767, 767 APU CHANGE. 2L72 4F RTA1NM 20040205001092004020500109NE 2004 2 5 NACA20030122 220031125A8530356993 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL03438721151 1151 533294 P34767 NR 4 ENGINE SHUT DOWN DUE TO EXCESSIVE VIBRATION. REPLACED NR 4 ENGINE, NR 2 CYLINDER. OPS CHECKED GOOD. 2L74 4R4 R A781 5E8 20040205001142004020500114CE 2004 2 5 BSY2003F00028 120030909A5210 LINKAGE BEECH 58 58 1152740CE CONT O520 IO520* 17032SO HARTZLHCJ3Y PHCJ3YF2 GL PAX DOOR HANDLE OUT OF ADJUST E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL07297AT TH1349 299269R ED4135A CABIN DOOR CAME OPEN IN FLIGHT, RETURNED TO (CLE). ADJUSTED LINKAGE AT DOOR HANDLE. OPS CHECKED GOOD. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20040205001242004020500124WP 2004 2 5 G60A073 120031128A26123023117 FIRE WARNING DOUG DC10 DC1030F 3023504WP COCKPIT FALSE INDICATIONA G6OAFJA ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27612GC 47840 DURING CLIMB PASSING FL240 MASTER WARNING LIGHT AND FWD CARGO FIRE LIGHT ILLUMINATED. 2L73 4F RTA22WE 20040205001292004020500129NM 2004 2 5 C1HA200392009 120031126A5320 SUPPORT BOEING727 727212 138407GNM PWA JT8 JT8D* NE FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 WEB SUPPORT AT BS 312 BETWEEN RBL10 / 60 (IN DOG HOUSE AREA) IS EXFOLIATED AT IB WEB. 2L73 4F4 F A3WE E2EA 20040205001312004020500131CE 2004 2 5 GLBA20030507 120031201A31503PB11 SWITCH BEECH 1900 1900D 1154162CE COCKPIT MALFUNCTIONED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03255GL UE255 ALL WARNING ANNUNCIATORS ILLUMINATED, CLEANED PRESS TO TEST SWITCH PN 3PB1. OPS CK GOOD. 2L72 4T RTA24CE 20040205001322004020500132NM 2004 2 5 DHL2003721012 120031129A3350 CONNECTOR BOEING727 727228 1384083NM EMERGENCY LIGHTSDIRTY A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01721DH 19545 EMERGENCY EXIT LIGHTS ABOVE COCKPIT ENTRY DOOR DO NOT COME ON. CLEANED CONNECTION AND OPS CHECKED GOOD IAW B-M/M 33-50-101. 2L73 4F RTA3WE 20040205001332004020500133NM 2004 2 5 DHL2003745026 120031129A3260 WARNING SWITCH BOEING727 727224 1384076NM RT MLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER T/O, GEAR LEVER WAS MOVED FROM UP TO OFF, THE RED DOOR LIGHT AND THE AMBER RT GEAR DOOR ILLUMINATED. PERFORMED ABNORMAL, LANDING GEAR OR DOOR WILL STAY UP WITH THE GEAR LEVER IN OFF. CONTINUED FLIGHT WITH GEAR LEVER IN UP POSITION. ALL DOOR LIGHTS EXTINGUISHED. DEFERRED IAW MEL 32-1 CAT. (C) ITEM. DUE DATE 12-09-03. DMI NR 14873. PLACARD INSTALLED. REF: DMI NR 14873, AFTER T/O GEAR LEVER WAS MOVED FROM UP TO OFF THE RED DOOR LIGHT AND AMBER RT GEAR DOOR LIGHT ILLUMINATED. FLEW WITH GEAR HANDLE UP. ADJUSTED AND OPS CHECKED GOOD RIGHT LANDING GEAR DOOR WARNING SWITCH IAW B-727 MM 32-62-11. THIS CLEARS DMI NR 14873. PLACARDS REMOVED. 2L73 4F A3WE 20040206000032004020600003SW 2004 2 6 SDR11290376 120031128A7603C810242 CONTROL CABLE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCB3T HCB3TN5 GL ZONE 400 CHAFED E D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW17228AM33082166 TC300 P54062 BVA7662 DURING TAKE OFF PREP, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE POWER LEVER CABLE HAD BROKEN INSIDE THE CABLE HOUSING IN THE ENGINE COMPARTMENT. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20040206000092004020600009CE 2004 2 6 GLBA20030508 120031202A361012991003315 TUBE BEECH 1900 1900D 1154162CE BLEED AIR FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03195GL UE195 LT BLEED AIR FAILED, REMOVED AND REPLACED BLEED TUBE PN 129-910033-15. 2L72 4T RTA24CE 20040206000272004020600027SO 2004 2 6 SIMA200333802 120031204A2797 CONNECTOR EMB 135 EMB135LR 3260305SO TE FLAPS LOOSE A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21731BE 145356 BOS - FLT 4592 - FLAP FAIL/SPS ADVANCED FLAPS REMAINED AT ZERO REGARDLESS OF FLAP SELECTOR POSITION. RESECURED CONNECTOR ON FLAP VELOCITY SENSOR PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040206000292004020600029SO 2004 2 6 SIMA200334409 120031118A532014522178005 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE 145301 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALL NEW SILL IAW EMB STATMENT IC2003-145/0818 AND 3829. (M) 2L72 4F RTT00011AT 20040206000312004020600031SO 2004 2 6 SIMA200335202 120031218A2510147161100 SEAT EMB 135 EMB135KL 3260302SO COCKPIT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 LAX - FLT 3161 - CAPTAIN REPORTED THE PILOTS SEAT WOULD NOT LOCK IN PLACE. MAINTENANCE REMOVED AND REPLACED THE PILOTS SEAT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040206000752004020600075WP 2004 2 6 DHL2004806504 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 4 FLOOR TRACK PLUG LUG WORN AT STA 780.000. REMOVED PLUG WITH WORN LUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 4 FLOOR TRACK IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000862004020600086WP 2004 2 6 DHL2004806511 120031229A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 3 FLOOR TRACK LUG WORN STA 867.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3 PG 17 FIG 6D. INSTALLED SCREW IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000962004020600096WP 2004 2 6 DHL2004806518 120030104A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING OUTBOARD L/E FORMER UPPER PART CRACKED 0.500, STA XFS 772.500. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9,10. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10 SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040204001102004020400110NM 2004 2 4 QXEA200301302 120031018A243011521062 GENERATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09404QX560 4046 SEA-ON FLIGHT NUMBER 2273, NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED IN FLIGHT, RAN EMERGENCY CHECKLIST AND CYCLED NR 1 DC GENERATOR CONTROL SWITCH WITH NO CHANGE TO CAUTION LIGHT. ALL CIRCUIT BREAKERS ARE IN. REMOVED AND REPLACED NR 1 DC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040204001182004020400118CE 2004 2 4 DXTA200300144 120031021A3240M8353678024 RELAY CESSNA500 560CESSNA 2076750CE MLG BRAKE FAILED E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07330QS 5600329 AFTER SELECTING GEAR DOWN, POWER BRAKE LOW PRESS, ANTI SKID INOP ANNUNICATORS CAME ON, NO BRAKE PRESS EITHER SIDE. GO AROUND, ON SECOND APPROACH BOTH LIGHTS REMAINED ON FOR 5 SECONDS THEN EXTINGUISHED. BOTH PILOTS HAD POSITIVE BRAKE PRESSURE, NORMAL LANDING WAS ACCOMPLISHED. BACK UP AIR BRAKING NOT USED, ALSO NOTICED BRAKE HYD PUMP VERY NOISY. - JACKED A/C TO TROUBLESHOOT AND FOUND NORMAL TRANSITION OF BRAKE OPER GEAR UP/ DOWN NO DUP OF PILOT SQUAWK. BRAKE PRESSURE PUMP OPER SOUND NORMAL. INSPECTED SYS COMPONENTS FOUND SKID CONTROL RELAY KN002 SOAKED WITH SKYDROL REPLACED RELAY OPERATIONAL CHECK OF GEAR TRANSITION/ BRAKE SYS ENERGIZING SYS DETERMINED SATISFACTORY WORK PERFORMED WITH REFERENCE TO MFG 560 MM. 2L72 4F RTA22CE 20040204001562004020400156NM 2004 2 4 EIA2003127 120031020A5340 SKIN BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 RT FUS SEC 48 EXT. SKIN HAS CORROSION LOCATED BETWEEN STA. 2436-2460 STR.23R-25R. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-165-2. 2L74 4F A20WE 20040204001592004020400159NE 2004 2 4 EIA2003146 220031025A7261 O-RING BOEING747 747212B 1384886NM PWA JT8 JT8D7 52053NE G/B CHIP DETECT LEAKING A EIAAO OTHER S AFFECT SYSTEMS DEDESCENT 1 NM09482EV 20713 NR 1 ENGINE OIL QUANTITY DECREASED TO 1 GALLON AND NR 1 ENGINE OIL PRESSURE LIGHT CAME ON, SHUT DOWN NR 1 ENGINE, NR 1 ENGINE OIL PRESSURE AT 34 PSI. REPLACED ANGLE GEARBOX CHIP DETECTOR O-RINGS, PERFORMED LEAK CHECK NO OIL LOSS ON ENGINE RUN, SERVICE ENGINE OIL TO FULL IAW MM 79-11-00. 2L74 4F4 F A20WE E2EA 20040204001662004020400166EA 2004 2 4 SWIA200312535 120031021A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07441SW603 603 7602 FLAPS FAIL MESSAGE ON CLIMBOUT. CONTINUED TO SLC. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040204001722004020400172WP 2004 2 4 0301981224 120031001A5315 FLOORBEAM DOUG DC10 DC1030 3023501WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01224NW 46581 DURING M CHECK, FOUND CRACK ON FLOORBEAM AT BS 475 RBL 38. REPAIRED IAW EA 12-152773. 2L73 4F A22WE 20040205000032004020500003NE 2004 2 5 012071 220031117A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE ROTOL R389 R3894123F25 NE LEFT MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17340SZ 340A004 351 DRG550089 11/17/03 1715 (UTC) FLIGHT 4645 PIT-SDF. CREW REPORTED AN UNCOMMANDED POWER INCREASE OF THE LT ENGINE DURING CLIMB OUT. CREW REPORTED A RISE IN TQ AND ITT. CREW THEN FOLLOWED QRH, ENTERED TORQUE MOTOR LOCKOUT. ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO PIT WITHOUT INCIDENT. 2L72 4T4 TRTA52EU E8NE 6 CP30NE 20040205000892004020500089EU 2004 2 5 34931 120031123A6120 WARNING LIGHT SAAB SF340 SF340A 7850100EU AUTOCOARSEN ILLUMINATED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL1743SZ 340A043 FLIGHT NR 4555 FROM FWA TO PIT. ON TAKE-OFF AIRCREW NOTICED THAT THE AUTOCOARSEN LIGHT FAILED TO ILLUMINATE (ARM). AIRCREW ABORTED TAKE-OFF AND RETURNED TO THE GATE. 2L72 4T RTA52EU 20040205001002004020500100SW 2004 2 5 EH12003F00000 120031114A6710406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C* GL M/R PITCH LINK UNSERVICEABLE B EH1RO OTHER O OTHER NRNOT REPORTED 1 EA13175P 2108 53316 UPPER BEARING IN ASSEMBLY BECAME UNSTAKED/LOOSE AND WAS FREE TO MOVE IN/OUT OF BEARING HOUSING. CAUSED BY NORMAL OPS. 1G71 3U3 UO H2SW E4CE 20040206000162004020600016EU 2004 2 6 SIMA200334401 120031210A2120 ODOR SAAB SF340 340B 7860101EU CABIN DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21261AE 340B261 BFL - FLT 3012 - DURING FLIGHT, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. CREW DECLARED AN EMERGENCY. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. CAPTAIN REPORTED TO MAINTENANCE THAT NO SMOKE WAS PRESENT ONLY AN ELECTRICAL ODOR. SOME OF THE CABIN LIGHTS WERE PUT ON MEL AT THIS TIME AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040206000362004020600036EU 2004 2 6 USAASA03143 120031228A3350321431 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19182UW 1536 LAX - THE L-E EMERGENCY DOOR EMERGENCY POWER SUPPLY UNIT DOES NOT TEST DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY AT THE L3 POSITION. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040206000382004020600038WP 2004 2 6 ASAA0380826 120031212A533059530501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 360. RECONTOURED/COLD-WORKED SKIN. INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040206000562004020600056WP 2004 2 6 ASAA0380801 120031122A532199365841 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DUIRNG 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 1193-1250. REPLACED FLOORBOARD PER SRM 53-04. (M) 2L72 4F RTA6WE 20040206000742004020600074NM 2004 2 6 C8GA20030029 120031210A27406524917142 ACCESSORY UNIT BOEING727 727200 138407ENM STAB TRIM DEFECTIVE A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15713AA3006 22469 DURING CLIMB OUT, A/C EXPERIENCED RUNAWAY STAB TRIM. TRIM SWITCHES WERE POSITIONED TO CUT OFF, THIS DISENGAGED PITCH CTRL PADDLE SWITCH TO AUTOPILOT. AC JERKED NOSE UP, BEGAN EXCESSIVE CLIMB OF RATE AT WHICH TIME AUTOPILOT WAS DISENGAGED. AOM CHECKLIST, MN STAB TRIM WAS RE-ESTABLISHED, DECLARED EMERGENCY. AC AIR TURN BACK, LANDING WAS MADE USING MN ELECTRIC TRIM WITHOUT INCIDENT. INSPECTED STAB TRIM CONTROLS, FOUND CRUISE TRIM MOTOR CONTINUING IN MOTION. CYCLED CRUISE TRIM SWITCH, MANUAL WHEEL THROUGH SEVERAL TIMES FULL NOSE UP AND DOWN AND SYS OPS CHECK NORMAL. CLEANED TRIM SWITCHES, INSPECTED RELAYS, RESECURED LOOSE TERMINAL NR 14 ON R-27 CTRL RELAY. OPS SYS CHECKS WELL. AC RETURNED TO SERVICE. (K) 2L73 4F RTA3WE 20040204002282004020400228WP 2004 2 4 WRLA200328 120031118A3350BR964411 LIGHT DOUG DC10 DC1030 3023501WP ROW 21J INOPERATIVE A WRLAK NONE L NO TEST ININSP/MAINT 1 SO1114075 46922 EMERGENCY ISLE LIGHT INOPERATIVE AT 21J. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOOD 2L73 4F A22WE 20040205000172004020500017 2004 2 5 03321306 420031117A22107010680938 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP AUTOPILOT INTERMITTENT A VTZAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA27306UE 41020 DURING FLIGHT CREW REPORTED THE AUTOPILOT SYSTEM DISENGAGING EVERY 8 MINUTES. THE FAULT WAS VERIFIED AND THE AUTOPILOT COMPUTER WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T3 TRTA41NM E2WE 20040205000222004020500022NM 2004 2 5 EIA2003159 120031021A5730 SKIN BOEING747 747132 1384882NM WING CNTR SECT CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FS 1050 LBL 119 CORROSION ON UPPER WING CENTER SECTION SKIN AT BUTT JOINT BLEND OUT OF LIMITS. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR ECRA 479-57-177-2 2L74 4F A20WE 20040205001122004020500112 2004 2 5 GLBA2003160 420031128A34141303800057 INDICATOR BEECH 1900 1900D 1154162CE AIRSPEED SLOW A GLBAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 NM03247GL UE247 FO'S AIRSPEED IND SLOW, TURNED PITOT HEAT ON FOR LONGER PERIOD OPS CK GOOD PN 130-380005-7 2L72 4T RTA24CE 20040205001422004020500142CE 2004 2 5 WVE2003F00021 120031112A5720232507913 SUPPORT BRACKET LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE LT WING CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09235FX 153 WHILE INSTALLING LT WING AILERON CABLES, THE LT FLAP ACTUATOR UPPER AND LOWER SUPPORT BRACKETS WERE FOUND TO BE CRACKED. THESE BRACKETS ARE UNDER ACCESS PANEL 540EB WHICH IS NOT REQUIRED TO BE REMOVED FOR 1200 HOUR INSPECTION. REMOVE PANELS 540EB ON LT WING AND 640EB ON RT WING FOR INSPECTION OF BRACKETS EVERY 1200 HOUR INSPECTION. 2L72 4F4 FRTA10CE E35NE 20040206000042004020600004WP 2004 2 6 MEX2003519 120031114A2910S1168 SWITCH DOUG DC9 DC987 3022087WP HYDRAULIC SYS MALFUNCTIONED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23803ML 49726 DURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN THE SWITCH S1-168, SUCH SWITCH WAS BEHEADED. THE SWITCH WAS REPLACED AND THE HYDRAULIC SYSTEM WAS TESTED IAW MM 29-30-03. DURING OVERNIGHT SERVICE, THE SYSTEM WAS CHECKED BY LEAKAGES, ALL OK. 2L72 4F RTA6WE 20040206000532004020600053WP 2004 2 6 ASAA0380768 120031121A531099360749 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - FOUND SHEAR TIE CORRODED AT FS 655. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 51-10-2, 04, AND 53-03. (M) 2L72 4F RTA6WE 20040206000552004020600055WP 2004 2 6 ASAA0380760 120031122A534759305471 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 DRUING 15K CHECK, FOUND SEAT TRACK GOUGED. REPLACED TRACK PER SRM. (M) 2L72 4F RTA6WE 20040206000592004020600059WP 2004 2 6 ASAA0380806 120031123A532199365471 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD CORRODED FS 180-200. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040206000632004020600063WP 2004 2 6 ASAA0380825 120031212A533059114011 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS CRACKED AT LEFT AFT NLG DOOR CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-05. (M) 2L72 4F RTA6WE 20040206000672004020600067WP 2004 2 6 ASAA0380808 120031123A53209923666503 WEB DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OKC - DURING C-CHECK, FOUND FLOOR CUSP WEB IS GOUGED AT FS 180. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F RTA6WE 20040206000692004020600069WP 2004 2 6 ASAA0380750 120031118A531159624501 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND STATION 1079 FRAME HAS PITTING CORROSION. INSTALLED REPAIR STRAP PER SRM. (M) 2L72 4F RTA6WE 20040206000712004020600071WP 2004 2 6 ASAA0380752 120031118A53105936038501 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CORROSION ON CARGO DOOR BEAM REPAIR DOUBLER. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR DOUBLER AND TRIPLER PER EA 5310-02278. (M) 2L72 4F RTA6WE 20040205001232004020500123SO 2004 2 5 C2XA03CL195 120031130A2120 ODOR EMB 135 EMB135LR 3260305SO COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2714516 145323 CLE FLIGHT NR 2460 THE CREW REPORTED A STRONG FUEL ODOR AFTER THE APU WAS STARTED.THE CREW REPORTED THE ODOR DID GO AWAY EVENTUALLY. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU. NO DEFECTS WERE FOUND. 2L72 4F RTT00011AT 20040205001432004020500143CE 2004 2 5 CMR2003F00000 120031117A271012606481 ROD CESSNA206 206H 2073301CE LYC O540 IO540* 41532EA AILERON BROKEN B CMRRA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL2535561507 20608166 IMMEDIATELY AFTER TAKE OFF, THE PILOT NOTICED MINIMAL REACTION FROM AILERON CONTROL INPUTS. PILOT LANDED SAFELY. INVESTIGATION REVEALED LT AILERON DISCONNECTED FROM CONTROL ROD. FOUND THAT CONTROL ROD HAD BROKEN IN THREADED AREA JUST FORWARD OF AILERON CONTROL ROD END JAM NUT. IT APPEARS THAT BREAK WAS DUE TO SEIZURE OF ROD END. POSSIBLY DUE TO LACK OF LUBE. ALSO PLAY A PART, IT APPEARS ROD END ATTACH SCREW WAS OVER TORQUED SEIZING ROD END BEARING SO THAT IT COULD NOT ROTATE AROUND ATTACH SCREW. INSURE ON ALL INSPECTIONS THAT AILERON CONTROL ROD HAS FREEDOM OF MOVEMENT AND IS PROPERLY LUBRICATED. 1H71 3O3 ORTA4CE 1E4 20040206001152004020600115WP 2004 2 6 DHL2004806503 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 7 TRACK PLUG LUG WORN AT STA 275.000. REMOVED PLUG WITH WORN LUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 7 TRACK AT STA 275.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040210000012004021000001NM 2004 2 10 F3LA200300154 120031129A2701 YOKE BOEING737 7373M8 1384615NM COCKPIT FROZEN A F3LAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM03303FL 25039 ON FINAL APPROACH, FLIGHT CREW REPORTED YOKE FROZE UP IN TURN (ROLL ONLY). INSPECTED CASE DRAIN FILTERS IAW MM 29-15-91, AND FOUND NO DISCREPANCIES. REMOVED AND REINSTALLED NR 2 ENG. CASE DRAIN PLUG TO INSPECT IAW MM 29-15-00 AND FOUND NO DISCREPANCIES. VISUALLY INSPECTED LT AND RT AILERON CABLES FROM MAIN WHEEL WELL OB AND FOUND NO DISCREPANCIES. COMPLIED WITH FLIGHT CONTROL MOVEMENT WORK CARD, FOUND NO DISCREPANCIES. PERFORMED AILERON INTERNAL LEAK CHECK PROCEDURE IAW MM AND FOUND NO DISCREPANCIES. PERFORMED OPERATIONAL CHECK FLIGHT. NO DISCREPANCIES OR ABNORMALITIES NOTED. 2L72 4F RTA16WE 20040210000022004021000002 2004 2 10 KBM2003F00094 420031123A34225050010902 GYRO SNIAS 350 AS350BA 8680817EU COCKPIT MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P739 2347 DIRECTIONAL GYRO WILL NOT HOLD HEADING. INSTALLED O/H DIRECTIONAL GYRO. 1G71 3U NCH9EU 20040210000032004021000003NE 2004 2 10 KBM2003F00095 220031107A75329550158260 BLEED VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 BLEED VALVE WILL NOT OPEN/ CLOSE CORRECTLY. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040210000062004021000006NE 2004 2 10 MDR03021 120031120A65206535807053046 HOUSING SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE T/R GEARBOX CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09173AC 89 64015 THE TGB CENTER HOUSING WAS FOUND CRACKED WHILE INSTALLED ON AIRCRAFT. IT WAS REMOVED PREMATURELY, HAVING TSO 89.0 HOURS. THE SHOP DETECTED THE CRACK VISUALLY. THE CRACK BEGAN AT THE SECOND ROSAN STUD, CLOCKWISE FROM THE ROSAN SEAT PAD LOCATED 34 DEGREES FROM CENTERLINE OF INPUT BORE. THE CRACK EXTENDS RADIALLY THROUGH 3/8-16 NC TAPPED BORE THROUGH WEB STOPPING AFTER TRAVELING APPROXIMATELY 3.750 INCHES. 2G72 4U4 U H4EA E15EA 20040210000092004021000009WP 2004 2 10 UPS03841580 120031115A534037558412 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, BATHTUB FITTING IS CRACKED AT STATION 1230 BETWEEN LONG. 33R-34R. REMOVED AND REPLACED FITTING IAW DWG. 3755841 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040210000132004021000013WP 2004 2 10 UPS03841584 120031122A5320 WEB DOUG DC8 DC871F 302199DWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C1 COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS STATION -67 TO -80 AT RBL 20. REMOVED FINGER DOUBLER,CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND FINGER DOUBLER IAW DWG. 8930026 AND SRM. 51-1-21. 2L74 4F RT4A25 20040210000162004021000016WP 2004 2 10 UPS03841589 120031113A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STATION 1500 BETWEEN LONGERON 29L TO 31L. CUTOUT CORRODED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM.53-2-1 FIG. 7. 2L74 4F RT4A25 20040415000222004041500022GL 2004 4 15 ERAA093719 220031021A7320252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED A ERAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 AL03294EH8057 S675 SLOW TO RESPOND TO TORQUE SETTINGS. HAS 8-10 PERCENT TORQUE SPLITS ALL THE TIME. FOUND DROOPING, OVERSPEEDS EARLY, THROTTLE SHAFT STIFF, 3 INTERNAL BEARINGS ROUGH/DRY. REPAIRED AND TESTED IAW MFG OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20040415000732004041500073WP 2004 4 15 ASAA0380742 120031114A531359365631 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CORROSION ON AND AROUND FASTENERS ON LONGERON 30, STATION 807 AFT TO TERMINATION AT FORWARD SPAR OF FUEL TANK. REPAIRED PER SRM, ASA EA 5310-02266, AND AAR EA 10108. (M) 2L72 4F RTA6WE 20040415000752004041500075WP 2004 4 15 ASAA0380744 120031114A53119912243241 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND AFT CARGO COMPARTMENT STATION 1309 AT LONGERON 30 FRAME CORRODED. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20040415000962004041500096WP 2004 4 15 ASAA0380739 120031114A5311995301630 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FRAME AT FS 1437 TOP AFT SIDE CRACKED AT FASTENER HOLE RIGHT SIDE OF LONGERON 1. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20040415000172004041500017NE 2004 4 15 ERAA093710 120031006A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR DAMAGED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03575EH 760366 POLYURETHANE STRIP ERODED BOTH BLADES, TRAILING EDGE TAB DAMAGED. EROSION NEAR TIP. SENT FOR REPAIR. X RAYED ULTRASONIC INSPECTED IAW QATI 3016 AND 3098, PERFORMED ALL SCHEDULED INSPECTIONS UOP TO AND INCLUDING 1500 HR INSP IAW COMPOSITE MATERIALS MANUAL 4047-76-5 TABLE 2-2 AND MM 4047-76-2, 65-21-00 AND 65-21-01, INSPECTED ELLIPTICAL PLUG FOR DEBONDING IAW AD 94-14-20; COMPLIED WITH ASB 76-65-43 AND 76-65-46; REPLACED SPAR PLUG IAW RS-0221-II; REPAIRED TRAILING EDGE DAMAGE ON PADDLE A IAW RS-018M-IV; REPAIRED GOUGE IN PITCH HORN BUSHING AREA ON BOTH PADDLES IAW OR176100-018 PART VI; REPLACED BOTH PRIMARY POLYURETHANE STRIPS IAW RS-018M-1; REPLACED. 1G72 3U H1NE 20040415000192004041500019GL 2004 4 15 ERAA093715 220031128A7200 GEAR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL ENGINE MAKING METAL B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03130EH16429 558 CAE832700 ENGINE MAKING METAL. FOUND SPALLING ON PINION AND TORQUE METER GEAR. INSTALLED NEW PINION AND TORQUE METER GEAR. 1G72 3U3 U H3EU E4CE 20040416000212004041600021WP 2004 4 16 ASAA0380735 120031111A532199566541 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1079-1155. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040416000232004041600023WP 2004 4 16 ASAA0380737 120031111A533059360021 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 725. INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040419000172004041900017WP 2004 4 19 ASAA0380837 120031222A532049150671 BRACKET DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND CORNER BRACKET AT LEFT AFT SIDE OF APU OPENING IS CRACKED. INSTALLED DOUBLER ON BRACKET PER SRM 53-20-01. (M) 2L72 4F RTA6WE 20040419000182004041900018WP 2004 4 19 ASAA0380836 120031222A531259101300387 BULKHEAD DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND AFT PRESSURE BULKHEAD TEE IS GOUGED ON FORWARD SIDE. SPLICED IN NEW TEE SECTION PER EA 5310-02288. (M) 2L72 4F RTA6WE 20040419000202004041900020WP 2004 4 19 ASAA0380844 120031220A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND FLOOR CUSP MEMBRANE CRACKED AT FS 160. REPLACED RETAINER PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040419000252004041900025WP 2004 4 19 ASAA0380782 120031119A53209955763U11 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FORWARD PAX DOOR FRAME, INTERCOSTAL HAS .25 INCH CRACK IN RADIUS JUST AFT OF SEAL MECHANISM ADJUSTEMENT LINK. REPALCED INTERCOSTAL PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040415001402004041500140NM 2004 4 15 ASAA024014M 120030318A531065C32352 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500F BETWEEN STRINGER 26 AND 27 RT. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040419000112004041900011WP 2004 4 19 ASAA0380835 120031219A25003961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 SEA - PREFLIGHT CHECK, FOUND FORWARD AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040504000582004050400058NM 2004 5 4 ASAA2004BBB 120030323A5320BAC1496377 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IS CORRODED AT STATION 727-767, RBL 25, AND WL 158. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040210000212004021000021WP 2004 2 10 UPS03841595 120031116A534037537571N FITTING DOUG DC8 DC871F 302199DWP LOWER FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, EXTERIOR FUSELAGE LOWER CENTER SECTION FRAME TO KEELBEAM FITTING IS CRACKED AT STATION 702 RT SIDE OF CENTERLINE. REMOVED AND REPLACED FITTING IAW DWG. 3753757 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040210000372004021000037WP 2004 2 10 UPS03841615 120031118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STA 1726 LONG. 14L IS CRACKED. REMOVED DAMAGED SECTION OF LONGERON STATION 1716 TO 1736, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION AND STRAPS I.A.W. SRM. 53-2-2 FIG. 10 2L74 4F RT4A25 20040210000542004021000054NM 2004 2 10 ASAA02401AA 120030317A5410 STRUCTURE BOEING737 7374Q8 138447QNM RT PYLON CHAFED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01785AS 27628 PAE - DURING C-CHECK, FOUND WEB OUTBOARD OF RIGHT PYLON IN AFT FLAP WELL IS CHAFED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040210000592004021000059WP 2004 2 10 ASAA0380779 120031119A53205936071501 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CORROSION ON INTERCOSTAL AT LONGERON 29L FROM STATION 617-636. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20040210000682004021000068WP 2004 2 10 ASAA0380771 120031119A53305910228210 SKIN DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND AFT FUSELAGE SKIN BETWEEN STATION 1437 AND 1463 GOUGED. REPAIRED IAW SRM. (M) 2L72 4F RTA6WE 20040210000752004021000075NM 2004 2 10 TSAA0429001 120031230A291010602030153 LINE BOEING737 7372Y5 1384554NM HYD SYSTEM FAILED A TSAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13810AL 24031 FLT 240 - HNL-OGG - ON GEAR RETRACTION 'A' SYSTEM HYDRAULIC ANNUNCIATOR LIGHT CAME ON. SYSTEM QUANTITY AT 1.5 GALLONS. RETURNED TO HNL. FOUND RIGHT MAIN GEAR UPLOCK ACTUATOR FLEX-LINE RUPTURED. REMOVED AND REPLACED FLEX-LINE. LEAK CHECK OK. SERVICED HYDRAULIC FLUID AS REQUIRED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4U RTA16WE 20040210000832004021000083EU 2004 2 10 USAA030313 120031201A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED, 1 INCH BY 1 INCH AREA, 0 RBL 17.75 AT FRAME 68. DEFECTIVE PART REPLACED IDENTICAL PART PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20040210001082004021000108EU 2004 2 10 USAA030309 120031124A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED, .125 INCH AREA, LBL 17.75 FRAME 57.3 PLUS 10 INCHES. DAMAGED SECTION REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210001102004021000110EU 2004 2 10 USAA030308 120031124A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .150 SQUARE INCH AREA, LBL 17.75 FRAME 57.4. DAMAGED SECTION REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210000052004021000005EA 2004 2 10 COMA0360522 120031127A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01443CA 7539 FLIGHT 5006 DURING APPROACH TO YUL RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES FLAP POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A,B,C, AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20040210000072004021000007NE 2004 2 10 MDR03029 120031120A65206535807053043 HOUSING SKRSKYS64 S64F 8142610NE PWA JFTD12JFTD12A4A 52047NE T/R GEARBOX CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09223AC 64086 TGB CTR HSG FOUND CRACKED WHILE INSTALLED ON AC. IT WAS REMOVED PREMATURELY HAVING A TSO OF 974.7 HR. VISUALLY DETECTED INDIC IN OB WEB OF LT MOUNTING LUG. HSG WAS LOCALLY FPI INSPECTED TO VERIFY. NO IND WAS NOTED. AREA WAS STRIPPED, LIGHTLY ABRADED WITH SCOTCH-BRITE AND ETCHED. AREA WAS ALSO LOCALLY HEATED IN LT LUG AREA TO OPERATING TEMP AND FPI INSPECTED. AT THIS TIME, INDICATION WAS DETECTED. AS HOUSING COOLED TO ROOM TEMP, INDICATION WAS LESS NOTICEABLE. AT ROOM TEMP, INDICATION WAS VIRTUALLY NON-EXISTENT. CRACK LOCATION BEGINS AT RADIUS IN IB SIDE OF OB WEB OF LT MOUNTING PAD EXTENDING OUTWARDS, WRAPPING AROUND WEB ENDING AT BOSS FOR INPUT HSG BORE. CRACK LENGTH IS APPROX 2.0 INCHES. 2G72 4U4 U H6EA E15EA 20040210000142004021000014WP 2004 2 10 UPS03841585 120031121A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STA. 1050-1130 AT LONGERON 31L. REMOVED,FABRICATED AND REPLACED FINGER DOUBLER IAW SRM. 53-4-1 FIG. 17 AND SRM. 51-1-20D,51-1-21. 2L74 4F RT4A25 20040210000992004021000099EU 2004 2 10 USAA030289 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .250 SQUARE INCH, FRAME 62 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040211000052004021100005WP 2004 2 11 GTIA031043 120031209A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND CABIN CENTER FLOORBOARD STATION 270 IS SPONGY. REMOVED CABIN CENTER FLOORBOARD. FABRICATED NEW CABIN CENTER FLOORBOARD. INSTALLED FS 270 FLOORBOARD. (M) 2L72 4F RTA6WE 20040211000082004021100008WP 2004 2 11 AMTA200301455 120031026A5230 WEB LKHEED1011 1011385115 5265015WP CARGO DOOR DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 193B1230 FOUND C2 DOOR WEB STRUCTURE DAMAGED. REPLACED WEB IAW SRM 51-40-01. (M) 2L73 4F A23WE 20040211000122004021100012NM 2004 2 11 USAA030317 120031125A5414 SKIN BOEING737 7374B7 1384702NM NR 2 NACELLE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 PIT - FOUND SKIN CRACKED 1 INCH, NR 2 ENGINE PYLON PANEL 5727R. INSTALLED DOUBLER PER TR 54-30-07. (M) 2L72 4F RTA16WE 20040211000392004021100039EA 2004 2 11 ASOA03692 120031229A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE FORWARD FLOORBEAM ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLOORBEAM ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040210000782004021000078EA 2004 2 10 A6WA200340203 120031227A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FALSE INDICATIONA A6WAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL31431AW 7256 CARGO SMOKE WARNING, FIRE BOTTLES BLOWN, WHILE AIRCRAFT ON GROUND WITH CARGO AND PASSENGER DOOR OPENED. INSPECTED CARGO COMPARTMENT, NO HEAT OR SMOKE DAMAGE. COMPLIED WITH MAINTENANCE ACTION TASK 26-15-00-040-801. DEACTIVATED BOTH CARGO SMOKE DETECTORS. REMOVED AND REPLACED RIGHT FIREX BOTTLE, P/N 34600037-1, S/N OFF 14773F1, REMOVED AND REPLACED LEFT FIREX BOTTLES, P/N 36500018-3, S/N OFF 45875D1. (M) 2L72 4F RTA21EA 20040210000902004021000090EU 2004 2 10 USAA030303 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .125 INCH AREA, FRAME 60 PLUS 10 INCHES LBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210001032004021000103EU 2004 2 10 USAA030288 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .250 SQUARE INCH AREA, FS 62 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210001142004021000114EU 2004 2 10 USAA030276 120031202A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 2 INCH AREA, RBL 17.75 6 INCH FORWARD OF FRAME 49. INSTALLED NEW SECTION OF SEAT TRACK PER EA 95004. (M) 2L72 4F RTA46NM 20040210001172004021000117WP 2004 2 10 ASAA0380754 120031118A532199365491 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - FOUND 15K CHECK, FOUND FLOORBOARD INSERTS PULLED THROUGH. REPLACED WITH FLOORBOARD FABRICATED IAW SRM. (M) 2L72 4F RTA6WE 20040211000272004021100027NM 2004 2 11 USAA030321 120031230A5310 DOOR FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU50706 23701 PIT - FOUND DOOR FRAME SKIN CRACKED .5 INCH LONG, FORWARD SERVICE DOOR FRAME CRACK AT DOOR STOP NR 4. DOUBLER INSTALLED AT DOOR STOP NR 4 PER TR 52-10-11. (M) 2L72 4F RTA16WE 20040211001372004021100137CE 2004 2 11 IPMA854F 120031218A321112430097 TRUNNION CESSNA210 T210N 2073456CE CONT O520 TSIO520* 17040SO NLG FAILED E IPMAO OTHER O OTHER NRNOT REPORTED 1 WP119371Y9429 21064490 NOSE GEAR COLLAPSED DURING LANDING ROLLOUT. DETERMINED TO BE CAUSED BY FAILURE OF THE UPPER TRUNNION ASSY (NR 12430097) THE DRAG BRACE FAILED AT THE COLLAR AROUND THE STRUT TUBE. INDICATIONS OF INTERGRANULAR CORROSION ARE APPARENT AND PROBABLY CAUSED BY AN UNDETECTED CRACK. THIS AC IS SUBJECT TO DAILY TOWING. DETAILED INSPECTIONS INCLUDING PENETRANT INSPECTIONS OF THIS CASTING ARE RECOMMENDED. ADDITIONALLY MORE DETAILED INSPECTION OF THIS AREA IS RECOMMENDED FOR PREFLIGHT. (K) 1H71 3O3 O 3A21 E8CE 20040212000052004021200005GL 2004 2 12 UPS03641622 220031202A7320 HMU BOEING767 767300 1385204NM GE CF6 CF6* 30020GL RT ENGINE MALFUNCTIONED A IPXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO01328UP 27754 704762 RT ENGINE ROLLED BACK TO IDLE AND WOULD NOT RESPOND TO THRUST LEVER MOVEMENT. DIVERSION TO STL REPLACED HMU, EEC, AND CONTROL ALT. OPS , LEAK , POWER TESTS NORMAL. 2L72 4F4 FRTA1NM E23EA 20040212000082004021200008WP 2004 2 12 UPS03841625 120031117A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, MAIN CABIN STATION 1360 INTERCOSTAL IS CRACKED AT LONG. 10L CUTOUT DAMAGE,FABRICATED AND INSTALLED ANGLE REPAIR I.A.W. SRM. 53-2-0 FIG. 1B 2L74 4F RT4A25 20040212000142004021200014CE 2004 2 12 AMWA83 120031114A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0710675 UE10675 WHILE PERFORMING AND INSPECTION IN THE VERT. STAB., THE RIB FLANGES AT CANTED STAB STA 54.026 WERE FOUND CRACKED IN FOUR PLACES ON THE LEFT AND TWO PLACES ON THE RIGHT. REPAIRED CRACKS TO RIB FLANGE IAW BMM P/N 114-590021-9, 51-70-03 2L72 4T RTA24CE 20040212000222004021200022SO 2004 2 12 AK02003F00000 120031105A7810Q26 DUCT MAULE MT7235MT7235 5470209SO LYC O540 IO540W1A5 41532NE LT EXHAUST BROKEN C AK0MO OTHER O OTHER NRNOT REPORTED 1 AL03138CP100 100 18072C L2808848A DURING AN ANNUAL INSPECTION THE ALTERNATE AIR INTAKE DUCT WAS FOUND BROKEN OFF OF THE LEFT EXHAUST MUFFLER AT THE WELD. THE DUCT AND HOSE WAS FOUND CHAFING AGAINST THE ENGINE MOUNT TUBULAR STRUCTURE. THIS FAILURE WAS CAUSED BY AN INADEQUATE MEANS OF SUPPORTING THE WEIGHT OF THE DUCT AND HOSE WHEN ASSEMBLED. 1H71 3O3 ONC3A23 1E4 20040212000322004021200032SO 2004 2 12 TRK2003F00000 120031119A3230592669 SEQUENCE VALVE PIPER PA46 PA46350P 7104602SO LYC O540 TIO540* 41532EA NOSE GEAR LEAKING B TRKRO OTHER O OTHER NRNOT REPORTED 1 SO15548C 117 4636322 OWNER NOTICE HYDRAULIC FLUID ON GROUND BY NOSE WHEEL. INSPECTION FOUND NOSE GEAR SEQUENCE VALVE TO BE LEAKING FROM SHAFT. OWNER STATED THAT THIS VALVE HAS BEEN REPLACED TWICE BEFORE. THREE FAILURES OF SAME PN IN 117 HOURS WOULD INDICATE FAULTY DESIGN OR INEFFECTIVE QUALITY CONTROL. (K) 1L71 3O3 ORTA25SO E14EA 20040211000092004021100009NM 2004 2 11 USAASB04004 120030103A5230 SEAL BOEING737 7373B7 1384580NM FWD CARGO DOOR FAILED A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19518AU56132 23704 DURING CLIMB-OUT FROM PHL, EN ROUTE TO ORD AT FL270, CRWE HEARD A LOUD BANG AND A BURST OF AIR. NO MASTER CAUTION WARNING OR DOOR WARNING LIGHTS ILLUMINATED. THE AUTO PRESSURZATION SYSTEM HAD FAILED AND WAS PLACED IN STANDBY. IN STANDBY, THE CABIN ALTITUDE BEGAN TO COME DOWN SLOWLY. OUTFLOW VALVE WAS NOTED TO BE CLOSED. NO CABIN OXYGEN MASKS WERE DEPLOYED. FLT REACHED 10,000 FT AND DIVERTED TO PIT. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MAINTENANCE FOUND FORWARD CARGO DOOR LOWER SEAL, WHICH HAD BEEN PREVIOUSLY REPLACED, ROLLED OUT OF THE TRACK OF THE DOOR. REMOVED AND REPLACED THE FORWARD CARGO DOOR ASSEMBLY PER JOB CARD. OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20040212000032004021200003CE 2004 2 12 56207 120031116A8000312301901 LINE BEECH 1900 1900D 1154162CE P-3 BROKEN A AMWAO OTHER O OTHER CRCRUISE 1 CE075YV UE5 DURING CRUISE FLIGHT RT ENGINE QUIT. CREW RETURNED TO ABQ AND LANDED WITHOUT ANY INCIDENTS. PASSENGERS DEPLANED AT PRECAUTION WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED P-3 BROKEN LINE. CHANGE IT TO P-3 FILTER. P/N 3123019-01. 2L72 4T RTA24CE 20040212000472004021200047NE 2004 2 12 NACA20030125 220031207A8530 VALVE SEAT DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 CYLINDER POWER LOSS A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA1066 1066 A701WTXB 45529 P34011 NR 3 ENGINE SHUT DOWN DUE TO LOSS OF BMEP, AND LOW COMPRESSION. REPLACED NR 3 ENGINE , NR 2 CYLINDER. (STUCK VALVE SEAT). CHECKED GOOD. 2L74 4R4 R A781 5E8 20040212000692004021200069NE 2004 2 12 MDR03037 120031120A65206535807053043 HOUSING SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE T/R GEARBOX CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09194AC6488 1770 64017 THE TGB CENTER HOUSING WAS FOUND CRACKED WHILE INSTALLED ON THE AIRCRAFT. IT WAS REMOVED PREMATURELY ON SEPTEMBER 3, 2000. THE SHOP DETECTED THE CRACK VISUALLY. THE CRACK BEGAN AT THE SECOND ROSAN STUD CLOCKWISE FROM THE ROSAN SEAT PAD LOCATED 34 DEGREES FROM CENTERLINE OF INPUT BORE. THE CRACK EXTENDED RADIALLY THROUGH 3/8-16 NC TAPPED BORE ABOUT 3/4 OF AN INCH THROUGH THE WEB. PROBABLE CAUSE IS UNKNOWN AT THIS TIME. 2G72 4U4 U H4EA E15EA 20040212001142004021200114SW 2004 2 12 SDRO200306 120030918A6310206040270009 FREEWHEEL UNIT BELL 206 206L3 1182108SW MAIN ROTOR FAILED E IBUAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 WP07791CA 545 51455 DURING GROUND RUN PRIOR TO FLIGHT, TRANSMISSION CHIP LIGHT ILLUMINATED. AIRCRAFT WAS SHUT DOWN. ON INSPECTION, MECHANIC FOUND A SLIVER ON FREE WHEELING UNIT CHIP PLUG. CLEANED CHIP PLUGS AND PERFORMED MAINTENANCE REQUIREMENTS STATED IN MM. AIRCRAFT APPROVE FOR RETURN TO SERVICE. 1G71 3U H2SW 20040212001312004021200131NM 2004 2 12 DHL2003742512 120031121A5311 FRAME BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER LOBE INTERIOR FRAME HAS DENT STA 500 ABOVE 17 RT. CUT OUT DAMAGED AREA UPPER LOBE INTERIOR FRAME HAS DENT STA 500 ABOVE 17RT AND FABRICATED NEW ANGLE WITH MATERIAL 7075 T6 .071 PO 9912917 DIMENSION 8 X 4 X 1 INCH IAW B727 SRM 53-10-4 FIG 2. ALODINE AND PRIME IAW B-727 SRM 51-10-2. INSTALLED ANGLE IAW B-727 SRM 53-10-3 FIG 2. 2L73 4F A3WE 20040212001332004021200133NM 2004 2 12 DHL2003742515 120031124A5754 SKIN BOEING727 727225 1384077NM NR 5 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 5 SLAT OUTBOARD HOOK CUTOUT IN UPPER L/E SKIN AFT OUTBOARD CORNER IS CRACKED. REMOVED PAINT AT AFFECTED AREA IAW MM 51-20-1 AND STOP DRILLED CRACK IAW SRM 51-10-1 HFEC VERIFIED STOP DRILL IAW B-727 NDT MM PT 6 51-00-00 FIG 23. FABRICATED PLATE DOUBLER REPAIR FROM MAT 301-1/2 HD .025 PO 9912398 DIM 7.125 X 5.25 INCH AND FILLER STRAP FROM MAT 301-1/2 HD .032 PO 9912398 AND BACKING STRAP FROM MAT 2024 T3 .063 PO 900355 DIM 3 X 2 INCH IAW B-727 SRM 57-30-4 FIG 9. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED PLATE DOUBLER REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 20040212001802004021200180NM 2004 2 12 AWXA200301591 120031205A575465C26601179 SKIN BOEING737 73733A 1384673NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. 16, PG. 67-69. 2L72 4F RTA16WE 20040212001972004021200197NM 2004 2 12 HNAA0300081 120031210A2731 JACKSCREW DHAV DHC8 DHC8201 2809001NM ELEVATOR TRIM CONTAMINATED A HNAAO OTHER F FLT CONT AFFECTED DEDESCENT 1 EA07998HA 509 DURING DESCENT, ELEVATOR TRIM WOULD NOT GO NOSE DOWN. INSPECTED ELEVATOR CONTROL CABLES AND LINKAGE UNDER FLIGHT DECK FLOOR AND APU BAY, NO DEFECTS NOTED. INSPECTED ELEVATOR TRIM ACTUATOR JACKSCREWS AND CHAIN FOUND CONTAMINATED WITH WATER, CLEANED, LUBED. OPS CHECKED GOOD. 2H72 4T RTA13NM 20040213000142004021300014CE 2004 2 13 364031 120031226A5310 DOOR FRAME BEECH 1900 1900D 1154162CE FUSELAGE WORN A NSVAK NONE O OTHER ININSP/MAINT 1 EA27136MJ UE36 WORN NOTCH IN CARGO DOOR FRAME LOWER EDGE MID SPAN, REMOVED DAMAGED AREA AND INSTALLED AN INSERTION REPAIR WITH SPLIT DOUBLER ON UNDERSIDE TO SUPPORT THE RIB IAW SRM SKIN DAMAGE ( NON PRESSURIZED AREA). 2L72 4T RTA24CE 20040213000292004021300029EA 2004 2 13 SWIA200312722 120031124A2710 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 RT AILERON CONTROL HAS (UNUSUAL FEELING), CLICKING NOISE. (DISCOVERED DURING C-CHECK INSPECTION) SERVICE LETTER NR RJ-SL-27-045 COMPLIED WITH IAW CRJ AMM 27-11-05-420-001 PARAGRAPH 11. 2L72 4F4 FRTA21EA E15NE 20040213000312004021300031NM 2004 2 13 CALA0300724 120031230A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 772, RBL 3 AND RBL 7. REPAIRED FLOOR SUPPORTS IAW ECRA 5320-01603. 2L72 4F RTA16WE 20040213000342004021300034CE 2004 2 13 WVE2003F00028 120031217A323324170161 ACTUATOR LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE UPLATCH/LOCK CORRODED B WVERK NONE O OTHER ININSP/MAINT 1 EA09247FX 187 DURING 1200 HOUR INSPECTION, THE EMERGENCY LANDING GEAR UPLATCH/LOCK ACTUATORS WERE REMOVED FOR A DETAIL INSPECTION. THE LT ACTUATOR WAS FOUND TO CONTAIN CORROSION (RUST) INSIDE OF THE SPRING/HYDRAULIC CYLINDER. MOISTURE INTRUSION AND NO HYDRAULIC FLUID FLOW. MFG EVALUATE. 2L72 4F4 FRTA10CE E35NE 20040212000122004021200012WP 2004 2 12 UPS03841630 120031117A53403717780519 FITTING DOUG DC8 DC871F 302199DWP FWD. LOWER CARGOCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C1 A-PIT RT CARGO TRACK SUPPORT FITTING IS CRACKED AT STATION 100 AT LONG. 34R REMOVED,FABRICATED AND REPLACED FITTING IAW 8110-3 APPROVED DATED 11/24/03 SAA SK 718-027 DATED11/21/03,UPS ENGINEERING FILE NUMBER DC8- 53-20379 DATED 11/25/03 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040212000842004021200084NE 2004 2 12 MDR03030 120030924A6320643520516101 PLATE SKRSKYS64 S64F 8142610NE M/R GEARBOX CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09178AC3549 2392 A6162 64097 DURING THE MAGNETIC PARTICLE INSPECTION OF THE 2ND STAGE PLANETARY PLATE, A CRACK WAS DETECTED. THE CRACK IS LOCATED IN THE .125 INCH R. FROM THERE, IT TRAVELS TOWARDS THE SPLINE AT A 45 DEGREE ANGLE. THEN IT TRAVELS DOWN THE DRIVE SIDE TOOTH FILLET OF THE SPLINE ABOUT .7500 OF AND INCH. THIS PLATE HAS ACCUMULATED 2392.9 EAC HOURS. THE OVERALL LENGTH OF THE CRACK IS APPROXIMATELY 1.25 INCH. THIS PN PLATE IS NO LONGER BEING MANUFACTURED AND HAS BEEN REPLACED BY AN IMPROVED DESIGN. 2G72 4U H6EA 20040212000872004021200087NM 2004 2 12 03FDEA02166 120031211A5531 STRINGER BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 VERTICAL FIN STR 8L AT FIN STA 133 IS CRACKED ** SD ** COMING 2L73 4F RTA3WE 20040212000882004021200088SW 2004 2 12 JIKA20030004 120031210A53112722104046 FRAME SWRNGNSA227 SA227AC 8780603SW FUSELAGE CRACKED E JIKAK NONE O OTHER ININSP/MAINT 1 WP01421MA AC634 CRACKS FOUND ON LT AND RT SIDES OF FUSELAGE FRAME, DURING LETTER CHECK E AT FS 407.271. 2L72 4T RTA8SW 20040212001302004021200130NM 2004 2 12 DHL2003742511 120031121A5311 FRAME BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER LOBE INTERIOR BS 520 FRAME HAS DENT ABOVE 17 RT. CUT OUT DAMAGED AREA DIM 1.5 X 1 INCH AND FABBED REPAIR ANGLE FROM 7075 T6 .071 PO 9912917 DIM 9 X 5 X 1 INCH IAW B-727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 1. PART TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20040213000032004021300003EU 2004 2 13 AWXA200301607 120031227A561006283 WINDSHIELD AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE ZONE 200 DELAMINATED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28668AW6179 1764 AIR TURN BACK, AFTER TAKEOFF, EN ROUTE FOR SLC THE FIRST OFFICERS WINDSHIELD DELAMINATED, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM 56-11-11. VENDOR DID NOT PERFORM FAILURE ANALYSIS OF WINDSHIELD, BELIEVES DAMAGE WAS CAUSED BY WATER INGRESSION. 2L72 4F4 FRTA28NM E311NE 20040213000092004021300009EU 2004 2 13 010901 120031229A2430 GENERATOR SAAB SF340 SF340A 7850100EU RIGHT MALFUNCTIONED A UHLAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS HJGELECT. POWER LOSS-50 PC WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 GL1719XS 340A019 RT GENERATOR VOLTAGE LOW (22 VOLTS) RETURN TO PIT. AIRCRAFT TAKEN OUT OF SERVICE 12-29-2003. 2L72 4T RTA52EU 20040217000092004021700009EU 2004 2 17 2004F00060 120030915A5240D5348012220100 PLATE AIRBUS320 A320233 3930329EU R2 DOOR WORN A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND R2 DOOR CAM PLATE FOR DOOR HANDLE BACK MECHANISM ROLLER HAD WEAR MARKS. REMOVED AND REPLACED FITTING ON R2 DOOR, DOOR HANDLE BACK MECHANISM. (M) 2L72 4F RTA28NM 20040217000732004021700073NM 2004 2 17 TZR2004F00001 120030729A3210400053501 TORQUE LINK PIPER PA60 PA60601 7106010NM LYC O540 IO540S1A5 41532EA RT MLG BROKEN E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05600TE6973 610146077 TORQUE LINK ATTACH POINT ON THE RT STRUT BROKE AT LANDING. THIS ALLOWED THE RT MLG TIRE TO ROTATE AND PULL THE AIRCRAFT OFF THE RUNWAY. THE RESULTING SIDE LOAD ON THE MLG CAUSED THE OVER CENTER LINK , AND THE STRUT CYLINDER, TO BREAK. ALSO, BOTH RT SIDE MLG DOOR WERE DAMAGED ALONG WITH THE RT FLAP. THE CUFF FOR ATTACHING THE TORQUE LINKS TO THE STRUT IS INSTALLED BY THE SWEAT METHOD. THE CUFF WAS BROKEN AT ATTACH POINT FOR THE SCISSORS LINK FOR SOME TIME AND NOT NOTICED DUE TO COVERAGE OF PAINT. IT TOOK A FEW LANDINGS FOR THE SWEAT ATTACHMENT TO BREAK LOOSE. DEBONDING WAS EVIDENT BY DISCOLOR OF SWEAT SEALED AREA ON CUFF AND STRUT. INSP RECOMMENDED TO TORQUE LINK ATTACH POINT ON THE STRUT. 1M72 3O3 ORTA17WE 1E4 20040217000752004021700075 2004 2 17 KBM2004F00004 420031028A23120690102443 RADIO BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL VHF SYSTEM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 1833 2513 CONSTANT STATIC HEARD THRU PILOT HEADSET THRU VHF WITH ACCESSORIES ON. NO STATIC WITH ACCESSORIES OFF. REMOVED AND REPLACED WITH SERVICEABLE RADIO. (K) 1G71 3U3 U H2SW E4CE 20040217000762004021700076EU 2004 2 17 KBM2004F00006 120031104A6720350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV2202 3296 PITCH LINK WORN BEYOND LIMITS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20040217001082004021700108NM 2004 2 17 NACA20030130 120031228A5753 BEARING BOEING727 72723 1384004NM RT FLAP SEIZED A NACAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AL03992AJ 19428 DISCREPANCY: OB FLAPS WOULD NOT RETRACT PAST 4 DEGREES. REPLACED RT OB FLAPS, OB AND IB CARRIAGE TOGGLE DUE TO SEIZED BEARINGS. CHECKED GOOD. 2L73 4F A3WE 20040212000402004021200040NM 2004 2 12 COOSDR030161 120031201A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23395AJ 21100 MAIN CARGO CABIN, BS 1110, FLOORBEAM, LOWER CHORD CORRODED. 2L73 4F4 FRTA3WE E2EA 20040212000892004021200089SW 2004 2 12 JIKA20030005 120031210A53112722109017 FRAME SWRNGNSA227 SA227AC 8780603SW FUSELAGE CRACKED E JIKAK NONE O OTHER ININSP/MAINT 1 WP01421MA25031 AC634 CRACKS FOUND ON LT AND RT SIDES OF FUSELAGE FRAME, P/N 27-22109-017, DURING LETTER CHECK E AT FS 422.271. 2L72 4T RTA8SW 20040212001522004021200152EA 2004 2 12 COMA0360559 120031217A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 GENERATOR LACK OF LUBE A COMAC ABORTED TAKEOFF JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01868CA 7427 NR 2 IDG CAUTION MESSAGE AND GEN 2 CAUTION. SERVICED THE IDG OIL RESERVOIR, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20040213000172004021300017NM 2004 2 13 2003UALA00977 120031218A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROW 5 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29527UA 24995 EMERGENCY AISLE LIGHT AT ROW 5 INOPERATIVE. RELAMPED. 2L72 4F4 FRTA2NM E17NE 20040213000242004021300024NE 2004 2 13 CNMA200300010 220031228A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE NR3 FLAMED OUT A CNMAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW0749082 47927 NR 3 ENGINE FLAMED OUT AT TOP OF DECENT WITH THROTTLES AT IDLE. ACCOMPLISHED CHECKLIST IAW COM. 2L73 4F4 F A22WE E23EA 20040217001862004021700186EU 2004 2 17 U30A200300039 120031226A2150 A/C PACK AIRBUS320 A320212 3930322EU CONTAMINATED A U30AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA17265AV 427 AFTER LANDING, DURING TURNOFF FROM RUNWAY, CREW NOTED LIGHT SMOKE IN COCKPIT AND CABIN WITH NO DISTINCT ODOR OR ANY ECAM MESSAGE OR ABNORMAL INDICATION, EXCEPT ALL BRAKE TEMP SENSORS ON WHEEL PAGE SHOWED AMBER(XX). MAINT INSP AC AND FOUND WATER ON BELLY OF AC AROUND AIR COND PACK INLETS AND NR 2 ENG. FLIGHT CREW NOTED WATER PUDDLE ON TURN OFF WITH THRUST REVERSERS ACTIVATED. MAINT RAN AIR COND PACKS AND NO SMOKE OR ODOR NOTED THROUGHOUT AC. SUSPECT WATER INGESTION INTO AIR CONDITIONING PACK SYS AND RESULTING MIST/VAPOR ENTERED AC. PERFORMED BSCU (BRAKE STEERING CONTROL UNIT) TEST IAW AMM 32-46-00 AND BRAKE TEMP INDICATIONS ARE NORMAL. VISUALLY INSPECTED BSCU WITH NO DEFECTS NOTED. AC RETURNED TO SERVICE. 2L72 4F RTA28NM 20040217001922004021700192CE 2004 2 17 DXTA200300139 120031016A2910NAS16126 O-RING CESSNA750 750 2076810CE HYD SYSTEM LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07939QS1260 7500193 LT HYDRAULIC QUANTITY DROPPED TO ZERO 10 MINUTES AFTER TAKE-OFF. (A) SYSTEM UNLOADED, GEAR BLOW DOWN AND EMERGENCY BRAKE SYSTEMS ACTUATED. ACCOMPLISHED AIR TURN BACK TO CMH. - FOUND PLUG O-RING ON HYDRAULIC MANIFOLD LEAKING. REMOVED AND REPLACED O-RING, LEAK CHECKED GOOD. BLED HYDRAULIC SYSTEM IAW CE750 MM CHAPTER 12-10-15, SERVICED BOTH HYDRAULIC RESERVOIRS IAW CE750 MM 12-10-15. 2L72 4J RTT00007WI 20040218000062004021800006NM 2004 2 18 AWX2004F00000 120031202A278269358611 SPRING BOEING BOEING737 737277 1384570NM SLAT ACTUATOR WORN A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28189AW 1886 22656 EN ROUTE FROM PHX TO ABQ FLIGHT CREW REPORTED RT WING NR 5 SLAT HANGING DOWN APPROXIMATELY 5 INCHES, AIRCRAFT RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED NR 5 LEADING EDGE SLAT ACTUATOR PER AWA TASK CARD R3M27020, OPERATIONAL AND LEAK CHECK WAS GOOD. FUNCTIONAL TEST OF LEADING EDGE SLAT ACTUATOR S/N 1886 CONFIRMED FAILURE OF UNIT FOR NOT RETRACTING IN THE INTERMEDIATE POSITION. DISASSEMBLY OF UNIT REVEALED ALL O-RING & BACK UP SEALS WORN BEYOND LIMITS, SPRING SEAT GOUGED & SCRATCHED, AND SPRING NR 9, FIG. 1102 FAILED TEST. REPLACED ALL DEFECTIVE PARTS AND BENCH CHECKED UNIT IAW CMM 27-80-11, REV. 49. 2L72 4F RTA16WE 20040218000112004021800011CE 2004 2 18 GLBA20030522 120031230A5270 SWITCH BEECH 1900 1900D 1154162CE CARGO DOOR OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03202UX UE202 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, ADJUSTED DOOR AJAR SWITCH OPS CK GOOD 2L72 4T RTA24CE 20040218000072004021800007CE 2004 2 18 GLBA20030516 120031221A5270 SWITCH BEECH 1900 1900D 1154162CE CARGO DOOR DIRTY A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM0396UX UE96 CARGO DOOR ANNUNCIATOR LIGHT CAME ON IN FLIGHT, CLEANED CARGO DOOR WARNING SWITCHES & ADJUSTED CARGO DOOR AJAR SWITCH OPS CK GOOD 2L72 4T RTA24CE 20040301000642004030100064WP 2004 3 1 U2R2004F00000 120031029A5711 SPAR CAP DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE RT WING CRACKED A U2RBK NONE O OTHER ININSP/MAINT 1 GL23921R 67301 46145 DURING REPETIVE COMPLIANCE WITH AD AND SB, DETECTED 2 CRACKS AT RT WING FRONT SPAR LOWER CAP, REPAIRED IAW SB. REMAINING HOLES STRESS COINED TO CONDITION 1, OPTION 2. 2L74 4F4 F 4A25 1E8 20040301001102004030100110EU 2004 3 1 RYN2004F00011 120031019A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 ABOVE STRINGER 34 IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 JUST ABOVE 34L IN FORWARD CARGO COMPARTMENT. 2L72 4F4 FRTA28NM E311NE 20040301001782004030100178WP 2004 3 1 GTIA031047 120031220A2810 BLADDER DOUG DC9 DC983 3022083WP FUEL CELL LEAKING A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23832NK 49618 FLT 982 - DEN - UPON ARRIVAL, FOUND FUEL LEAK AFT OF MAIN WHEEL. REMOVED AND REPLACED AFT AUX BLADDER. LEAK CHECK GOOD. INSPECTED INSTALLATION OF AFT AUX TANK BLADDER AND FUEL DRAIN SHROUDS. NO LEAKS NOTED. (M) 2L72 4F RTA6WE 20040301001802004030100180NM 2004 3 1 ASAA0240174 120030322A5320655384422 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 727 PLUS 12 TO 867. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040301001812004030100181NM 2004 3 1 ASAA0340335 120031024A53205893543129 GUSSET BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01780AS 25112 JNU - DURING WINDSHIELD CHANGE DISCOVERED .75 INCH CRACK IN WINDSHIELD CUT OUT UPPER LEFT CORNER. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040227001012004022700101CE 2004 2 27 BTA2004F00000 120031216A2510551900922 SEAT CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE COCKPIT CRACKED B BTAAO OTHER O OTHER NRNOT REPORTED 1 GL23204CF 5500238 UPPER CHAIR BASE ASSY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. 1L72 4F4 F A22CE E1NE 20040301000142004030100014 2004 3 1 KBM2004F00011 420031009A34215040017901 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ATTITUDE INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH265 2337 PILOT REPORTS ATTITUDE INDICATOR WILL NOT HOLD HEADING AFTER APPROXIMATELY 20 MINUTES OF OPERATION. REMOVED AND REPLACED WITH OVERHAULED UNIT. (K) 1G71 3U3 UNCH9EU E19EU 20040301000382004030100038EA 2004 3 1 ASO2004F00000 120030802A5210A601R383705 CABLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPORTED THAT THREE ATTEMPTS WERE MADE BEFORE THE MAIN PASSENGER DOOR WOULD OPEN. MAINTENANCE REMOVED AND REPLACED THE MAIN PASSENGER DOOR WHEEL CABLE ON THE LT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT, OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040227000412004022700041NM 2004 2 27 ASAA0340350 120031208A531165C323946 FRAME BOEING737 7374Q8 138447QNM FS 601 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01756AS 25097 GYR - DURING SI CHECK, FOUND CRACKED FRAME CHORD AFT SIDE AT STATION 601 RBL 65 WL 203. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040301000512004030100051EU 2004 3 1 KBT2004F00001 120031212A6720350A33214501 CONTROL ROD SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED A KBTRK NONE O OTHER ININSP/MAINT 1 NM07352SL4099 2798 9338 DURING COMPLIANCE WITH AD, INSPECTED BOTH CONTROL RODS. FOUND BOTH BUSHINGS IN ELASTOMERIC BEARING CRACKED THROUGH TO BOTH ENDS. BOTH CONTROL RODS REJECTED FROM FURTHER SERVICE. INSTALLED NEW CONTROL RODS. NO RECORD OF REPLACEMENT IN AC LOGBOOK. THIS PUTS THE CONTROLS RODS AT PLUS 1528 HOURS TIME IN SERVICE. 1G71 3U3 U H9EU E19EU 20040416000202004041600020WP 2004 4 16 ASAA0380734 120031111A532199365582515 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AND BROKEN FASTENERS AT FS 1134-1174. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415001102004041500110WP 2004 4 15 ASAA0380811 120031126A57305930577501 SKIN DOUG DC9 DC983 3022083WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE CRACKED. INSTALLED DOUBLER AND FILLER PER SRM 57-06 AND 51-10-3. (M) 2L72 4F RTA6WE 20040419000822004041900082WP 2004 4 19 ASAA0380814 120031126A53219936688503 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 808-823. BOND-REPAIRED PER SRM 51-70-3. (M) 2L72 4F RTA6WE 20040419000832004041900083WP 2004 4 19 ASAA0380747 120031114A5720993758411 BRACKET DOUG DC9 DC983 3022083WP RT WING BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE AT APPROX XRS 100 CABLE BRACKET BROKEN. REPAIRED PER ASA EA 5740-01365 AND AAR EA 10105. (M) 2L72 4F RTA6WE 20040520002322004052000232EU 2004 5 20 2004F00117 120030909A5321 FLOOR PANEL AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION AND BARE METAL ON SEVERAL NUT PLATES AND CLIP NUTS AND THEIR UPPER AND LOWER MOUNTING SURFACE IN FORWARD CARGO COMPARTMENT BETWEEN RIGHT FRAME 28 TO FRAME 34, RIGHT STRINGER R-S 34 TO CENTER B/L. FABRICATE, ALODINED, PRIMED, APPLIED TOPCOAT AND INSTALLED INTERCOSTAL BETWEEN FRAME 28 TO FRAME 34, STRINGER 34R. (M) 2L72 4F RTA28NM 20040525000342004052500034EU 2004 5 25 2004F00124 120030916A5315D5437220925300 FLOORBEAM AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBEAM AT FRAME 20 AT RBL 12. REMOVED AND REPLACED FLOORBEAM AND SPLICE AT FRAME 20, RBL 12. (M) 2L72 4F RTA28NM 20040525000372004052500037EU 2004 5 25 2004F00127 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 62 AND 63 ABOVE STRINGER 37L IN AFT CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 62 AND 63 ABOVE STRINGER 37L. (M) 2L72 4F RTA28NM 20040525000432004052500043EU 2004 5 25 2004F00133 120030916A5320D5397470400300 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND 5 DAMAGED AREAS ON FLOORBOARD SUPPORT AT FRAME 59 BETWEEN STRINGER 42R AND 43L IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 59 ON RIGHT SIDE. (M) 2L72 4F RTA28NM 20040525000442004052500044EU 2004 5 25 2004F00134 120030916A5320D5347217220390 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT RIGHT STRINGER 38 BETWEEN FRAME 58 AND 59 ON AFT LOWER CARGO BAY FLOOR. REMOVED AND REPLACED FLOOR SUPPORT FRAME BETWEEN FRAME 58 AND 59. (M) 2L72 4F RTA28NM 20040525000492004052500049EU 2004 5 25 2004F00139 120030916A5340D534702682100 FITTING AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FITTING AT FRAME 59 AND STRINGER 41R IN AFT CARGO BAY. FITTING AT FRAME 59, RIGHT STRINGER 41 OF FLOOR STRUCTURE REMOVED AND REPLACED. (M) 2L72 4F RTA28NM 20040525000412004052500041EU 2004 5 25 2004F00131 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT FRAME 58 BETWEEN STRINGER 38R AND 40R IN AFT LOWER CARGO COMPARTMENT. REMOVED FLOORBOARD SUPPORT, FABRICATED AND INSTALLED NEW FLOORBOARD SUPPORT AT FRAME 58 BETWEEN STRINGER 38R AND 40R. (M) 2L72 4F RTA28NM 20040525000482004052500048EU 2004 5 25 2004F00138 120030917A5320D5348004320401 SILL AIRBUS320 A320233 3930329EU PAX DOOR CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION AT L2 DOOR INBOARD OF AFT GIRT BAR ATTACH PLATE AT FRAME 68 AND LBL 50. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITTING, DRAINS AND ANGLE AT FRAME 67, LEFT LOWER, UNDER SILL. (M) 2L72 4F RTA28NM 20040525000452004052500045EU 2004 5 25 2004F00135 120030917A5321 FLOORBOARD AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 221FF. REMOVED SURFACE CORROSION FROM FLOORBOARD 221FF. MATERIAL LOSS FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED. (M) 2L72 4F RTA28NM 20040525000512004052500051EU 2004 5 25 2004F00141 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 38L IN AFT CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 38L. (M) 2L72 4F RTA28NM 20040601001192004060100119WP 2004 6 1 04FDEA01497 120031201A5512ALC74391 SKIN PANEL DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25560FE 46938 HORIZ STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF NRC N1102) 2L73 4F4 FRTA22WE E23EA 20040303000372004030300037SW 2004 3 3 ERAA092654 120031026A7920209062502101 BLOWER BELL 412 412 1182202SW OIL COOLER DAMAGED B ERAAK NONE O OTHER ININSP/MAINT 1 AL03164EH9823 33004 OIL COOLER BLOWER DUE 1500 HR OVERHAUL. NO DEFECTS NOTED. DURING NDT CHECK NOTED ON BLADE OF IMPELLER AND RIM OF CASING ASSY. DISASSEMBLED, CLEANED AND VISUALLY INSPECTED ALL PARTS. C/W NDT OF REQUIRED PARTS. OVERHAULED IAW ERA CAMP PROGRAM AND BHT 412-CR&O CHAPTER 79. REASSEMBLED IAW 412-CR AND O CH 79 INSTALLING NEW CASING ASSY, NEW IMPELLER, 2 EA NEW BEARINGS, DECAL, ORING GASKET. TT 9823.3 1G72 4U H4SW 20040303000472004030300047 2004 3 3 BAQA090476 420030129A3453453102503 RECEIVER BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101* NE LORAN SYS INOPERATIVE B BAQAK NONE O OTHER ININSP/MAINT 1 EA0339188 7011 LOANER - RETURN OF LOANER UNIT S/N 43011 FROM LOANER PO 2-021974-05 REPLACED WITH UNIT BACK FROM REPAIR. 1G72 3U3 U H13EU E5NE 20040304000432004030400043SO 2004 3 4 TZR2004F00004 220031205A8530 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520U 17040SO MCAULY3AF32C3AF32C* GL NR 2 BURNED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05401TE4202 1102 4010180 515604 THE NR 2 CYLINDER FAILED. AT DISASSEMBLY THE NR 2 CYLINDER WAS FOUND TO HAVE BURNED, THE BURNING OF THIS CYLINDER CAUSED A LOSS OF OIL. THE RESULTING LOSS OF OIL CAUSED THE BEARING TO RUB WITHOUT OIL AND EVENTUAL FAILURE. WHEN IT FAILED, IT MADE A HOLE IN THE CASE ABOVE THE CYLINDER. THE CYLINDER WAS AN OVERHAULED CYLINDER. IT IS RECOMMENDED THAT CYLINDER USED ON TURBO CHARGED ENGINES BE REPLACED WITH NEW AT EACH ENGINE OVERHAUL. 1L72 3O3 O A7CE E8CE 5 CP22EA 20040304001442004030400144WP 2004 3 4 ASAA0380834 120031217A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01947AS 53020 SEA PREFLIGHT CHECK, FRONT EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001532004030400153WP 2004 3 4 ASAA0380848 120031230A3397 CONNECTOR DOUG DC9 DC983 3022083WP LIGHT MODULE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01974AS 53450 SMF PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM FORWARD GALLEY TO ROW 2. RECONNECTED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040329000362004032900036NM 2004 3 29 ASAA0340325 120030725A531565C3394823 FLOORBEAM BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND FLOORBEAM AT STATION 947 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040401000272004040100027WP 2004 4 1 ASAA0380412 120030425A5310593639517 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING C-CHECK, FOUND LEFT MLG DOOR JAMB DOUBLER IS CRACKED. REPLACED PREVIOUSLY INSTALLED DOUBLER PER SRM 51-10-3 AND 53-01. (M) 2L72 4F RTA6WE 20040401000352004040100035WP 2004 4 1 ASAA0380405 120030421A5347 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND AFT CARGO TRACKS BETWEEN L27R AND L28R ARE CORRODED. INSTALLED REPAIR DOUBLER PER SRM. (M) 2L72 4F A6WE 20040401000412004040100041NM 2004 4 1 AALA20031192 120031030A3350 CONTROL MODULE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, FOUND ALL KNEE LEVEL AND FLOOR LEVEL EMERGENCY EXIT MARKERS INOPERATIVE. REPLACED CONTROL MODULES AND BATTERY PACKS FOR EQUIPMENT M10798, M10799, M10800 AND M10801 EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401000482004040100048NM 2004 4 1 AMTA200400125 120030920A5330 SKIN BOEING757 75733N 1384931NM FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11559TZ 32593 REPAIRED FUSELAGE SKIN FS 199 TO FS 297, S20R TO BL 0. COMPLIED WITH ERA 757-53R-5305. PERMENANT SKIN REPAIR COMPLETE. (M) 2L72 4F RTA2NM 20040401000342004040100034WP 2004 4 1 ASAA0380404 120030421A5542 SKIN DOUG DC9 DC982 3022082WP RUDDER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RUDDER HAS DENT ON LEFT SIDE. REMOVED DAMAGE AND HOT BONDED .012 7075-T6 REPAIR DOUBELR TO RUDDER PER SRM. (M) 2L72 4F A6WE 20040401000372004040100037WP 2004 4 1 ASAA0380408 120030421A531327779223 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURNG 30K CHECK, FOUND LONGERON 28L CORRODED IN FORWARD CARGO BAY AT FS 231. REPLACED DAMAGED SECTION PER SRM 53-02. (M) 2L72 4F A6WE 20040401000472004040100047EU 2004 4 1 USAA030326 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED 5.5 INCH AREA, AT RBL 17.75 AT FRAME 70 PLUS 10 INCHES. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040401000712004040100071NM 2004 4 1 AALA20031138 120031010A3397 PIN BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 MIA - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT ROW 18. REPAIRED ELECTRICAL PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401001412004040100141EU 2004 4 1 TRB2004F00001 120031225A770056785538012 INDICATOR AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE ITT ERRATIC A TRBACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO21319AM21366 319 121108 DURING TAKEOFF THE RT ENGINE ITT WENT TO 765 DEGREES. CREW ABORTED THE TAKEOFF AND RETURNED TO BLOCK. REMOVED AND REPLACED THE ITT INDICATOR FOR THE RT ENGINE. 2H72 4T4 TRTA53EU E20NE 20040607000552004060700055WP 2004 6 7 04FDEA01615 120031113A5712ARB70602 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568049 47803 WINGS - RIGHT RIB XORS 372 UPPER CAPS CRACKED. TRIMMED OUT CRACKED PORTION AND SPLICE REPAIRED IAW FEDEX EA 8- 5710-72233 (REF FEDEX NRC N0895 AND N0944). 2L73 4F A22WE 20040607000562004060700056WP 2004 6 7 04FDEA01616 120031113A5511 SPAR CAP DOUG DC10 DC1010 3022110WP HORIAZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568049 47803 HORIZONTAL STABILIZER - RIGHT LOWER FRONT SPAR CAP CORROSION. SPAR CAP SECTION REPLACEMENT IAW FEDEX EO 8-5510-7-4302 (REF FEDEX NRC N1075). 2L73 4F A22WE 20040607000542004060700054WP 2004 6 7 04FDEA01614 120031113A5712ARB70601 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568049 47803 WINGS - LEFT RIB XORS 372 UPPER CAPS CRACKED. TRIMMED OUT CRACKED PORTION AND SPLICE REPAIRED IAW FEDEX EA 8- 5710-72233 (REF FEDEX NRC N0895 AND N0944). 2L73 4F A22WE 20031215001362003121500136WP 2003 12 15 AALA20031059 120030923A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21290AA 49302 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE IN THE FLIGHT DECK AND THE FIRST CLASS GALLEY. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001412003121500141WP 2003 12 15 AALA20031090 120030930A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21433AA 49451 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 31. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031215001432003121500143WP 2003 12 15 AALA20031128 120031009A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21423AA 49335 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN THE AFT TAILCONE. REPLACED ELECTRICAL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001622003121500162WP 2003 12 15 AALA20031125 120031002A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW213515 49892 IAD - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN THE FIRST CLASS SECTION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001732003121500173WP 2003 12 15 AALA20031213 120031104A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21496AA 49734 TPA - DURING OVERNIGHT MAINTENANCE, FOUND E LIGHT INOPERATIVE IN FIRST CLASS. INSTALLED NEW BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001762003121500176WP 2003 12 15 AALA20031198 120031102A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21224AA 49174 PHX - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD ENTRY CEILING LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD ENTRY CEILING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001982003121500198EU 2003 12 15 USAA030256 120031029A5320D53112828201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND FLOOR SUPPORT CORRODED 1.8 INCH LENGTH BY 1.5 INCH WIDE, MAX DEPTH .075 INCH, FLOOR SUPPORT FRAME 16, -Y45. CORROSION LEVEL 2, TASK NR JA220-53500. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11 AND 51-72-11. (M) 2L72 4F RTA28NM 20031215002012003121500201EU 2003 12 15 USAA030261 120031102A5320D5361042100000 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND PLATE ASSEMBLY CORRODED 25.4 CM BY 5.1 AREA, FRAME 24, PLUS 29-39. CORROSION LEVEL 2, TASK NR JA-900-09000-018. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. (M) 2L72 4F RTA28NM 20031216000062003121600006NM 2003 12 16 QXEA200301443 120031119A5210 STOP FITTING DHAV DHC8 DHC8202 2809007NM PAX DOOR LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09363PH 520 SEA- ON FLIGHT 2015 MAIN CABIN DOOR IS HARD TO OPEN. CLEANED AND LUBED MAIN CABIN DOOR STOPS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031216000122003121600012NM 2003 12 16 QXEA200301450 120031105A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- FLOOR NUTPLATE HAS CORROSION AT STATION X223.00, LEFT OF YL29.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-40-11 AND RD 8-53-7637. 2H72 4T RTA13NM 20031216000402003121600040NM 2003 12 16 SWAA032557 120031119A3350PL2230LH00 STRIP BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29422WN 29826 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK STRIP CRACKED AT ROW 4 ABC. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM. 2L72 4F RTA16WE 20031216000752003121600075NM 2003 12 16 SWAA032571 120031120A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 45. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031216000782003121600078NM 2003 12 16 SWAA032574 120031121A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED 1/4D CHECK, FOUND A .75 LONG CRACK AT BS 665 BEADED WEB, LBL 32. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040506000692004050600069CE 2004 5 6 AFB2004F00000 120031012A2916511700712 SIGHT TUBE CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO HYD RESERVOIR DAMAGED E AFBAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO17404PJ200 402C0513 PILOT REPORTED SHORT DURATION SMOKE IN COCKPIT. RETURNED TO ORIGINATION POINT AND MADE A NORMAL LANDING. AIRCRAFT WAS TURNED OVER TO MAINTENANCE AND IT WAS DETERMINED THAT HYDRAULIC RESERVOIR SIGHT TUBE HAD FAILED AND RESERVOIR PARTIALLY DEPLETED. CAUSE OF FAILURE APPEARS TO EXCESSIVE HEAT DAMAGE. CAUSE OF DAMAGE IS UNDER INVESTIGATION. PRESENTLY UNDER WAY. 1L72 3O3 O A7CE E8CE 20040517000572004051700057EA 2004 5 17 COMA0460311 120031201A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA WING BOX AREA CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01954CA 7100 PRESSURE FLOOR SKIN CRACKED IN WING BOX AREA. REPAIRED IAW REO 601R-53-41-102. 2L72 4F RTA21EA 20040520002212004052000221EU 2004 5 20 2004F00111 120030912A5321 FLOOR PANEL AIRBUS320 A320233 3930329EU AFT CARGO BAY CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSON ON FLOOR PANEL NR 152BF IN AFT CARGO COMPARTMENT. FABRICATED, PRIMED AND INSTALLED AFT CARGO FLOOR PANEL NR 152BF. (M) 2L72 4F RTA28NM 20040520002302004052000230NM 2004 5 20 2004F00115 120031224A27821U109592 ACTUATOR BOEING727 727230 1384080NM NR 7 LE SLAT FAULTY A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07302FV 21442 AFTER TAKEOFF FROM ELP, DURING SLAT RETRACTION, NR 7 LEADING EDGE SLAT REMAINED EXTENDED WITH SLAT HANDLE AT 0 DEGREES. AMBER LEADING EDGE SLAT LIGHT WAS ILLUMINATED AND NR 7 INDICATED EXTENDED ON FLIGHT ENGINEERS LEADING EDGE PANEL. AIRCRAFT RETURNED TO ELP AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 7 SLAT ACTUATOR. OPS CHECK NORMAL. (M) 2L73 4F A3WE 20040525000322004052500032EU 2004 5 25 2004F00122 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CRACK ON FLOORBOARD SUPPORT AT FRAME 56 AND STRINGER 42R IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 56 AND STRINGER 42R. (M) 2L72 4F RTA28NM 20040525000332004052500033EU 2004 5 25 2004F00123 120030917A5321 PAN AIRBUS320 A320233 3930329EU AFT LAVATORY CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M) 2L72 4F RTA28NM 20040525000352004052500035EU 2004 5 25 2004F00125 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 49 AND FRAME 50 ABOVE STRINGER 43L IN AFT CARGO BAY. INSTALLED NEW FLOORBAORD SUPPORT BETWEEN FRAME 49 AND 50 ABOVE STRINGER 43L IN AFT CARGO BAY. (M) 2L72 4F RTA28NM 20040525000472004052500047EU 2004 5 25 2004F00137 120030917A5321 FLOORBOARD AIRBUS320 A320233 3930329EU MAIN CABIN CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 222FF. REPAIRED MAIN CABIN FLOORBOARD NR 222FF. (M) 2L72 4F RTA28NM 20031216000252003121600025EA 2003 12 16 MASA200300455 120031117A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 OKC - EXTERNAL EMERGENCY EGRESS LIGHT NEAR SERVICE DOOR INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4F RTA21EA 20031216000282003121600028NM 2003 12 16 SWAA032598 120031125A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND BS 360 STRINGER SPLICE CRACKED AT STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20031216000352003121600035NM 2003 12 16 SWAA032551 120031119A256065C16820 CLIP BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE GIRT BAR RESTRAIN CLIP LOOSE. SECURED CLIP PER MM. 2L72 4F RTA16WE 20031216000412003121600041NM 2003 12 16 SWAA032558 120031118A53126545819 PRESSURE PANEL BOEING737 7375H4 138449DNM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED PM CHECK, FOUND A 3.5 LONG CRACK AT NLG W/W SIDE WEB, BS 258. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20031216000442003121600044NM 2003 12 16 SWAA032530 120031117A53206550781 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND FLOOR WEB CRACKED AT BS 188 TO BS 196 LT SIDE, WL 207. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20031216000672003121600067NM 2003 12 16 SWAA032562 120031120A335065C34691 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20031216000732003121600073NM 2003 12 16 SWAA032569 120031121A532065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 663, STR 10L AND 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20031216000872003121600087NM 2003 12 16 SWAA032583 120031122A3350S283W6032 POWER SUPPLY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED PM CHECK, FOUND L1 AND R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED RT EMERGENCY LIGHT POWER SUPPLY PER MM. 2L72 4F RTA16WE 20031217000072003121700007NM 2003 12 17 DHL2003747012 120031121A7331 POWER SUPPLY BOEING727 727224 1384076NM FUEL FLOW MALFUNCTIONED A DHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01747DH 22253 IN CRUISE FLIGHT ALL THREE FUEL FLOW GAUGES WENT TO ZERO, S/O ADVISED THAT 28 VDC AND 115 AC FUEL FLOW CIRCUIT BREAKERS HAD POPPED. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY IAW M/M 73-31-12, OPS CHECKED NORMAL IAW JET RUN-UP HANDBOOK 5.2 AND M/M 73-31-0. 2L73 4F A3WE 20031211001552003121100155WP 2003 12 11 AALA20031406 120031209A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21412AA 49323 DTW FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031212000032003121200003 2003 12 12 03313655 420031109A22136229815704 CIRCUIT BOARD CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS FAULTY A VTZAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA27655BR 7457 DURING FINAL APPROACH THE CREW REPORTED RECEIVING AUTOPILOT PITCH TRIM MESSAGES. FLIGHT LANDED UNEVENTFULLY. FAULT WAS TROUBLESHOT TO THE NR 2 FCC CARD AND UNIT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031212000052003121200005 2003 12 12 03313626 420031109A34178220372154 ADC CNDAIRCL600 CL6002B19 1900309EA NR 2 FAULTY A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27626BR 7225 DURING TAKEOFF CREW REPORTED THE FIRST OFFICERS MULTI FUNCTION AND PRIMARY FLIGHT DISPLAYS WERE FLICKERING CAUSING A LOSS OF ALL FLIGHT DISPLAY INFORMATION. THE FAULT WAS TROUBLESHOT BACK TO THE NR 2 ADC UNIT AND UNIT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031212000362003121200036SO 2003 12 12 C2XA03SH450 120031112A532014525681607 ANGLE EMB 145 EMB145ER 3260211SO CABIN WARPED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE CARGO DOOR CUTOUT FRAME 66 ANGLE WAS FOUND TO BE WARPED OUT OF CONFIGURATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031212000422003121200042NM 2003 12 12 CALA0300642 120031114A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 727D + 8, LBL 2. THE GOUGED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2L72 4F RTA16WE 20031215000192003121500019NM 2003 12 15 QXEA200301434 120031113A5345 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007NM FUSELAGE BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX- SUPPORT BRACKET FOR LOWER ENGINE FIRE BOTTLE DISCHARGE INDICATOR LINE BROKEN AND CHAFING FUSELAGE. REPAIRED IAW HORIZON AIR EA 2-53-513. 2H72 4T RTA13NM 20031215000292003121500029 2003 12 15 SWAA032506 420031113A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 L2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20031215000422003121500042NM 2003 12 15 03FDEA01917 120031114A5311 FRAME BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 FOUND CRACK ON FRAME TOOLING HOLE BS 1050 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1050, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3. 2L73 4F RTA3WE 20031215000522003121500052NM 2003 12 15 2003UALA00833 120031104A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29107UA 26900 EMERGENCY SLIDE LIGHT AT DOOR 4R INOP. DOOR SLIDE LIGHT ASSEMBLY REPLACED. 2L74 4F4 FRTA20WE E24NE 20031215000672003121500067NM 2003 12 15 AWXA200301447 120031104A552365C2579715 TRIM TAB BOEING737 7373G7 1384595NM RT ELEVATOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND ON RT ELEVATOR TRIM TAB IN UPPER CORNER AT INBOARD ATTACH POINT. MAINTENANCE PERFORMED BOND REPAIR ON RT ELEVATOR TRIM TAB IN UPPER CORNER AT INBOARD ATTACH POINT IAW B737-300 SRM 51-70-17 FIG 8 PG 2, REPAIR 10. 2L72 4F RTA16WE 20031215000752003121500075 2003 12 15 304AW0002 420031114A2211 CONNECTOR BOEING737 7373G7 1384595NM AUTOPILOT SYS DIRTY A PIDAK NONE J WARNING INDICATION NRNOT REPORTED 1 SO05304AW 24011 SPEED TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. PLACED ON MEL 22-10. CLEANED AND RESECURED CANNON PLUG ON FCC PER MM 22-11-33. PERFORMED BITE TEST PER MM 22-11-01. TEST PASSED. CLEARED MEL. 2L72 4F RTA16WE 20031215000842003121500084NM 2003 12 15 P5CA0300990 120031118A2751INDICATOR INDICATOR BOEING747 747283B 1384867NM COCKPIT DEFECTIVE A P5CAD RETURN TO BLOCK N FALSE WARNING ININSP/MAINT 1 WP23921FT 21575 OUTBOARD T/E FLAPS LEFT SIDE STOPPED AT 4 DEGREES, RT SIDE STOPPED AT 10 DEG. REPLACED FLAP POS INDICATOR, OPS CHECK OK PER MM 27-58-00. 2L74 4F A20WE 20031215000852003121500085WP 2003 12 15 03FDEA01953 120031119A3250 CABLE DOUG DC10 DC1010 3022110WP NLG BROKEN A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25390FE 46624 AT LIFTOFF AFTER GEAR RETRACTION TOWER INFORMED CREW, NOSE GEAR WAS DOWN. RECEIVED A RED NOSE GEAR LIGHT AND ELECTED TO EXTEND GEAR, NORMAL GEAR INDICATION (3 GREEN). DURING TAXI FELT SLIGHT RIGHT PULL BUT NO OTHER ABNORMALITIES. AFTER LANDING FOUND RIGHT STEERING CABLE BROKEN. REMOVED AND REPLACED BOTH LEFT AND RIGHT LOWER STEERING CABLES AND RIGGED PER DC-10 M/M 32-51-00-2. PERFORMED GEAR RETRACTION OF NOSE GEAR ASSY, GEAR RETRACTED NORMAL. OK FOR SERVICE. 2L73 4F A22WE 20031216000032003121600003NM 2003 12 16 AWXA200301474 120031102A57126549353 RIB BOEING737 737277 1384570NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 LCQ - MAJOR REPAIR - DURING C-14 CHECK .5 INCH CRACK WAS FOUND IN LT WING LEADING EDGE RIB, INBOARD OF NR 1 ENGINE AT L/E STA 222.7. MAINTENANCE REMOVED CRACKED LT WING LEADING EDGE RIB AT L/E STA 222.7; FABRICATED A NEW REPLACEMENT RIB PER DWG 65-49353; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PARA 9B. 2L72 4F RTA16WE 20031216000322003121600032NM 2003 12 16 SWAA032602 120031125A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C4 CHECK, FOUND 5 EA FUSELAGE SKIN CRACKS AT BS 727E+6, STR 18L, BS 931, STR 21L, BS 919, STR 24L, BS 727E+14, STR 19L, AND BS 931, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031216001012003121600101SO 2003 12 16 C2XA03IA108 120031125A3040163500112 HEATER EMB 145 EMB145LR 3260212SO WINDSHIELD ARCED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27149072016 2016 145468 FLIGHT 2019 - CREW REPORTED THAT THE FIRST OFFICER'S WINDSHIELD HEATER WAS SPARKING IN FLIGHT. THE WINDSHIELD HEAT WAS DEACTIVATED UNDER MEL 30-42-02 AND THE AIRCRAFT RELEASED TO SERVICE. AFTER FLIGHT 2842 ON 11/25/2003, MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD, OPERATIONALLY CHECKED THE WINDSHIELD HEATING SYSTEM AND REMOVED THE WINDSHIELD HEATING SYSTEM FROM MEL. 2L72 4T RTT00011AT 20031217000112003121700011WP 2003 12 17 CALA0300654 120031120A5730 SKIN DOUG DC9 DC982 3022082WP RT WING CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND RT WING LOWER T/E SKIN CORRODED AT REAR SPAR STA XRS 399-477. A SKIN DOUBLER WAS INSTALLED IAW ECRA 5731-01037. 2L72 4F A6WE 20031217000132003121700013NM 2003 12 17 CALA0300656 120031120A5420 STRAP BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND A 6 INCH CRACK IN O/B STRAP ON NR 1 PYLON AT STA 363.5. INSTALLED SPLICE STRAPS IAW ECRA 5421-01002. 2L72 4F RTA16WE 20031217000372003121700037WP 2003 12 17 DHL2003805506 120030731A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT OUTER WING OTBOARD L/E LOWER PART SHOWS FRAME CRACKED (1.000) STA XFS 841.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031217000492003121700049WP 2003 12 17 DHL2003805527 120030818A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING OTBD STUB WING FRAME ANGLE DOUBLER CRACKED 2.000 AT STA XW 454.000. REMOVED ANGLE DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (7075-0.071) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. FOR REMOVAL AND INSTALLATION OF RIGHT OTBD STUB WING SEE N/R 2030. 2L74 4F RT4A25 20031217000512003121700051WP 2003 12 17 DHL2003805539 120030729A5720 SPLICE DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD L/E SPLICE PLATE UPPER PART CRACKED 14.000, STA XFS 710.000. REMOVED CRACKED SPLICE PLATE IAW SRM 51-1-21. FABRICATED SPLICE PLATE (7075-T6 0.090) IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 18. CLEANED, TREATED AND PRIMED AREA AND SPLICE PLATE IAW SRM 51-1-8B. INSTALLED SPLICE PLATE IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031217000532003121700053WP 2003 12 17 DHL2003805547 120030728A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OUTBD L/E FRAME 0.500 CRACKED STA XFS 747.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO NR 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031217000572003121700057WP 2003 12 17 DHL2003805578 120030823A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LWR AFT CARGO COMPT FWD DOOR PLATING SHOW INTERIM REPAIR BETWEEN STA 1200.000 AND 1260.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS THE EXISTING SEGMENT AND SPLICE REPAIR. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGMENT (7075-T6 AL0.050) AND A DOUBLER SPLICE (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT AND DOUBLER SPLICE. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED THE NEW SKIN SEGMENT AND DOUBLER SPLICE ON FWD DOOR PLATING OF LWR AFT CARGO COMPT (BETWEEN STA 1200.000 - 1260.000) USING NEW FASTENERS IAW DHL-EDT66-9 AND DHL-DWGT66-R09, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, AND SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031217000682003121700068WP 2003 12 17 DHL2003805584 120030824A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING HAS CORROSION AROUND STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) AND A FILLER (7075-T6 AL0.050). CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR DOUBLER AND FILLER ON RIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING (AROUND STA XFS 710.000) USING NEW FASTENERS. SEE N/R 0119 FOR INBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031217001012003121700101SO 2003 12 17 C2XA03CL190 120031122A3260 WARNING LIGHT EMB 145 EMB145LR 3260212SO MLG ILLUMINATED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2716987 145261 CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AIR/GROUND OPERATIONAL CHECKS ALONG WITH LANDING GEAR OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20031217001092003121700109NE 2003 12 17 2003UALA00847 220031111A7261 CAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE OIL DRAIN INSTALLED A UALAA UNSCHED LANDING WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29587UA 26713 RETURNED TO FIELD DUE TO SMOKE IN THE CABIN. A YELLOW PROTECTIVE CAP WAS LT ON THE DEOILER OVERBOARD BREATHER TUBE AFTER ENGINE INSTALLATION. AT ENGINE START, THE EXISTENCE OF THE CAP ALLOWED THE INTERNAL OIL PRESSURE TO BUILD UP SUFFICIENTLY TO UNSEAT SEVERAL OF THE BEARING CARBON SEALS RESULTING IN A LARGE OIL LOSS (> 7QTS.). AFTER REMOVING THE CAP & PERFORMING SEVERAL ENGINE RUNS, THE AIRCRAFT WAS CLEARED FOR SERVICE. SMOKE IN THE CABIN OCCURRED SHORTLY AFTER TAKEOFF. AC RETURNED TO FIELD AND ENGINE REMOVED. UPON DISASSEMBLY LARGE AMOUNTS OF OIL WERE STILL FOUND IN HPC DRUM CAVITIES AND SEALS LEAKED. ALL SEALS REPLACED. 2L72 4F4 FRTA2NM E17NE 20040415001172004041500117NM 2004 4 15 ASAA024014K 120030318A531165C32395 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 727F, RBL 9.5 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040419000162004041900016WP 2004 4 19 ASAA0380838 120031222A53305911429151 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CUT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND DRAIN TRAP OUTER SKIN AT FS 1338 IS CUT FOR MAINTENANCE ACCESS. INSTALLED SKIN PANEL SPLICE PER EA 5310-02288. (M) 2L72 4F RTA6WE 20040511000072004051100007EU 2004 5 11 ERAA094449 120031023A642010531714 ROTOR HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR WORN A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03298EH10895 TAIL ROTOR ASSY WILL NOT BALANCE, PLAY IN FEATHERING BEARINGS. BOTH TAIL ROTOR BLADES ERODED ON HEADING EDGE, GRIP BUSHINGS WORN. ACTION TAKEN: DISASSEMBLED, CLEANED AND INSPECTED PARTS. INSTALLED NEW INNER SLEEVE BUSHINGS, NEW GRIP BUSHINGS, SEALS, SERVICEABLE BLADES, NEW NUTS AND WASHERS. REASSEMBLED AND BALANCED IAW BO-105 M;M CHAPTER 33 & 107 AND REM 301. C/W TABLE 101-10-1 SUPPLEMENTARY INSPECTION 300 HOUR AND 2400 HR INSPECTION. C/W BY AEC. 1G72 3U H3EU 20031216000762003121600076NM 2003 12 16 SWAA032572 120031120A53106647978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 967 RT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031216000832003121600083NM 2003 12 16 SWAA032579 120031120A53306545800 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031211001402003121100140WP 2003 12 11 AALA20031388 120031205A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21411AA 49322 DFW FORWARD RIGHT OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD RIGHT OVERWING EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001432003121100143WP 2003 12 11 AALA20031361 120031201A2450 CONTROL UNIT DOUG DC9 DC983 3022083WP ELECTRICAL SYS FAULTY A AALAO OTHER O OTHER CRCRUISE 1 SW21965TW 53615 PDX T1010/01 EN ROUTE PDX-DFW RIGHT HAND BUS FAULT AND POPPING CIRCUIT BREAKERS. RETURNED PDX AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED AIRCRAFT BUS CONTROL UNIT AND R2-36 RELAY SYSTEM PER MM 24-20-08-4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031211001662003121100166WP 2003 12 11 AALA20030910 120030826A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP A/C BAY DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031211001742003121100174EA 2003 12 11 ASOA03537 120031025A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FAULTY A ASOAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11886AS 7531 DURING CLIMB OUT FROM ATL-GSO, THE CREW RECEIVED A CARGO SMOKE MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW RELEASED BOTH FIRE BOTTLES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. UPON LANDING THE FIRE DEPARTMENT INSPECTED THE AIRCRAFT WITH NO EVIDENCE OF FIRE NOTED. MAINTENANCE REMOVED AND REPLACED THE AFT AND FORWARD CARGO SMOKE DETECTORS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031211001902003121100190EU 2003 12 11 USAA030253 120031031A5320D5347219020500 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND ATTACHMENT HOLES WITH CORROSION 1.1 INCH LONG BY .60 WIDE AND .067 INCH DEEP, FRAME 64-66 -Y 1114 FLOOR SUPPORT. (M) 2L72 4F RTA28NM 20031212000502003121200050NM 2003 12 12 03FDEA01906 120031112A5320 ATTACH ANGLE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 WHILE WORKING NRC N01585 FOUND CORROSION AT STA 950 10 RBL 11 TO 50 WL 148, RT MLG BANANA FAIRING ATTACH ANGLE. CORROSION AT BS 950 10, RBL 11 TO 50, WL 148 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED REPAIR ANGLES AND FILLERS AND INSTALLED FOR RT MLG BANANA FAIRING ATTACH ANGLE IAW SRM 51-40-4, 51-30-2. 2L73 4F RTA3WE 20031212001192003121200119NM 2003 12 12 SWAA032502 120031112A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND BS 188 FUSELAGE FRAME CRACKED AT WL 207, LT SIDE. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20031212001312003121200131NM 2003 12 12 AWXA200301437 120031105A5311651758243 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN FRAME WEB AT FASTENER HOLE AT BS 178, LBL 17.1, WL 203 TO WL 208. MAINTENANCE CUT OUT DAMAGE IN FRAME WEB AT BS 178, LBL 17.1, WL 203 TO WL 208; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND SPLICE; INSTALLED REPAIR PARTS IAW SRM 53-10-08 PG 288K-288X, FIG 212. 2L72 4F RTA16WE 20031215000362003121500036NM 2003 12 15 SWAA032513 120031113A5315BAC1505 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FLOORBEAMS CORRODED AT BS 727D+4, RBL 3, AND BS 772, RBL 8. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20031215001022003121500102EA 2003 12 15 QXEA200301438 120031115A3234533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09606QX2731 295 10023 BOI- ON FLIGHT 2547 AIRCRAFT RETURNED TO FIELD DUE TO GEAR DISAGREE WARNING LIGHT AFTER TAKEOFF. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031215001192003121500119WP 2003 12 15 AALA20030971 120030907A33508039001 CHARGER DOUG DC9 DC982 3022082WP TAIL CONE INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21492AA 49730 BNA - FLT 1422 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE IN AFT TAIL CONE. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001252003121500125WP 2003 12 15 AALA20030958 120030903A33508039001 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21597AA 53287 SAN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT OVERWING LOCATION. REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031215001632003121500163WP 2003 12 15 AALA20031199 120031102A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21224AA 49174 PHX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT SIGNS OVER FORWARD OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EXIT SIGNS OVER FORWARD OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001972003121500197EU 2003 12 15 USAA030259 120031102A5320D5361042200000 STRAP AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND STRAP CORROSION 5.08 CM BY .221 CM, FLOOR PANEL NR 222 EK STATION 808, +Y32. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. CORROSION LEVEL 2, TASK NR JA-900-09000-019. (M) 2L72 4F RTA28NM 20031216000272003121600027NM 2003 12 16 SWAA032597 120031125A14306938825 BOLT BOEING737 7372T4 1384492NM T/E FLAP LOOSE A SWAAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 SW29722WN 22698 NOTABLE ACFT ROLL TO THE RIGHT AFTER T/E FLAPS ARE POSITIONED AT 15 UNITS. FOUND RT OUTBD T/E FLAP CARRIAGE BEARING SUPPORT BOLTS LOOSE. TORQUED BOLTS PER MM. OPS CK GOOD. 2L72 4F A16WE 20031216000502003121600050NM 2003 12 16 SWAA032536 120031117A3350BR2013 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 EEPLS LOOSE AT MID CABIN. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20031216000742003121600074NM 2003 12 16 SWAA032570 120031120A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031217000292003121700029WP 2003 12 17 DHL2003805502 120030807A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT WING CTR L/E FORMER 0.250 CRACKED, STA XFS 291.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON RIGHT WING CTR L/E FORMER, STA 291.500 IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031217000452003121700045WP 2003 12 17 DHL2003805512 120030725A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 MAIN CARGO COMPT NR 6 CARGO TRACK PLUG WORN AT STA 250.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 6 SEAT TRACK, STA 250.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031217000772003121700077NM 2003 12 17 CALA0300666 120030716A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND FLOOR SUPPORT IN RT LAV AREA CORRODED AT STA 986.5-1006, RBL 42. A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031217000822003121700082NM 2003 12 17 CALA0300671 120030716A5320 SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND CROSS SUPPORT IN AFT LAV AREA CORRODED BETWEEN STA 1006 AND 1016, RBL 16. A CROSS SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031217000832003121700083WP 2003 12 17 IXXA0300079O 120031122A7722 PMC DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM562BFR 13802EU NR 2 OUT OF LIMITS A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11828BX814321294 45993 692264 DURING CRUISE NR 2 ENGINE EGT INCREASED FROM 730 DEGREES APPROXIMATELY TO 830 DEGREES. CREW REDUCED POWER TO IDLE AND EGT STABILIZED AT 640 DEGREES. PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED AND CREW LANDED IN KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED EGT HARNESS AND NO DEFECTS WERE NOTED. MAINTENANCE RAN ENGINES AND FOUND PMC DROP CHECK OUT OF LIMITS. ADJUSTED POWER TRIM AND OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20031217000852003121700085WP 2003 12 17 0302091232 120031109A5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01232NW 46961 DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT FROM BS 824-828 LBL 27.5 TO RBL 27.5. REPAIRED PER EA 12-196596. 2L73 4F A22WE 20031217000912003121700091NM 2003 12 17 AWXA200301486 120031107A53136545800122 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT FROM BS 305 TO BS 324. MAINTENANCE REMOVED DAMAGED STRINGER 28 RT FROM BS 294 TO BS 323; FABRICATED 2 EACH REPAIR ANGLES AND A CHANNEL; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-00-03 FIG 201, SHEETS 1-7. 2L72 4F RTA16WE 20031217001042003121700104WP 2003 12 17 IXXA0300080O 120031125A5270 WARNING SYSTEM DOUG DC8 DC871F 302199DWP MLG DOOR CORRODED A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11830BX753172076 45973 AFTER TAKEOFF FROM KTOL LANDING GEAR DOORS LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE ABNORMAL CHECK LIST COMPLIED WITH AND DOORS LIGHT REMAINED ON. CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEAR DOOR WARNING LIGHT SYSTEM AND FOUND CORROSION. MAINTENANCE CLEANED, RESECURED AND TESTED GEAR DOOR WARNING SYSTEM ON GROUND. OPERATIONAL CHECK GOOD ON GROUND PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040420001982004042000198NE 2004 4 20 ERAA092658 120030613A63217665009803105 MOTOR SKRSKYS76 S76A 8143006NE ROTOR BRAKE INOPERATIVE A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 9396 ROTOR BRAKE LIGHT WOULD NOT EXTINGUISH. SENT TO HELICOPTER SUPPORT FOR REPAIR. THE MOTOR ARMATURE HAS BEEN SENT TO OUTSIDE SERVICE FOR REWIND. MOTOR REASSEMBLY WILL INCLUDE A REPLACEMENT BRUSH AND PLATE ASSY. THE POWER PACK REC'D A THOROUGH FLUSHING AND CLEANING TO REMOVE CONTAMINANTS. THE PUMP CARTRIDGE WAS FLUSHED AS WELL. REASSEMBLY AND TESTING ARE TO BE PERFORMED IAW CRANE HYDRO AIRE MANUAL. 1G72 3U H1NE 20040420002012004042000201EU 2004 4 20 ERAA093696 120031211A3212D24762101 FLOAT BOLKMS105 BO105A EU MLG LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 FLOAT BAG IS LEAKING. FLOAT WAS REPAIRED AND C/W INSPECTION. TESTED SERVICEABLE FLOAT IAW 25-60-95. 1G72 3U H3EU 20040511000092004051100009EU 2004 5 11 ERAA094451 120031116A6520 SHAFT BOLKMS105 BO105S 5626006EU GEARBOX SCORED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03124EH6135 1359 S559 TAILROTOR SHAFTS SCORED. SENT FOR REPAIR. SHAFT BEYOND LIMITS. SCRAPPED IAW BO-105 MM CHAPTER 33 FIG 33-12 ACTION TAKEN: REMOVED AND SCRAPPED TAIL ROTOR SHAFT 5/1454. INSTALLED NEW SHAFT 5/2185 IAW BO-105 MM CHAPTER 33 PARA 33-22. REAMED BUSHINGS AS REQUIRED, PRO-SEALED AS REQUIRED. 1G72 3U H3EU 20040401001622004040100162SO 2004 4 1 GSB2004F00000 120031205A27106276600 ROD END PIPER PA32 PA32300 7103212SO LYC O540 TIO540* 41532EA AILERON WORN E GSBAO OTHER O OTHER NRNOT REPORTED 1 AL03107TA 327540099 DURING 100 HR INSPECTION, THE FORWARD AILERON ROD ENDS REQUIRED REPLACEMENT. AFTER REMOVAL OF AILERON ROD ASSY. THE FORWARD ROD END. THEREADED SHANK WAS FOUND TO BE BROKEN IN HALF IN THE AREA WHERE A ROLL PIN IS INSTALLED INSTEAD OF A JAM NUT. WHICH THE AFT ROD END HAS. BOTH LT AND RT AILERON PUSH ROD ASSY WERE IN THIS CONDITION. AT THE FORWARD RODEND. NO REFERENCE FOR THIS ROLL PIN INSTALLATION. REVISE THIS ASSEMBLY TO INCLUDE A FORWARD JAM NUT. 1L71 3O3 O A3SO E14EA 20040304001542004030400154NM 2004 3 4 ASAA0340347 120031201A3397 CONNECTOR BOEING737 7374Q8 138447QNM EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01764AS 25101 SEA - DURING SERVICE CHECK, FOUND SECTION 1 NEAR ROW 1 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040308001402004030800140NM 2004 3 8 ASAA0310234 120030326A53207075T6125 WEB BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND WEB AT BS 360, LEFT BUTTOCK LINE 50 CORRODED. REPAIRED WEB PER SRM. (M) 2L72 4F RTA16WE 20040308001502004030800150NM 2004 3 8 ASAA0310242 120030327A7110 FRAME BOEING737 737298C 1384490NM NR 1 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 152.25 CHAFED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040308001582004030800158NM 2004 3 8 ASAA0310689 120031231A5330654580030 SKIN BOEING737 7372Q8C 138448SNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 350, STRINGER 24L DENTED. REPAIRED SKIN PANEL PER SRM. (M) 2L72 4F A16WE 20040308001602004030800160NM 2004 3 8 ASAA0310688 120031231A5315 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, BUTTOCK LINE 0 CORRODED. REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040308001622004030800162WP 2004 3 8 ASAA0380717 120031110A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 SEA PREFLIGHT CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS ILLUMINATED DURING EXTERIOR CHECK. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040308001632004030800163NM 2004 3 8 ASAA0310555 120031021A3350883200312 RECEIVER BOEING737 737290C 138448VNM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 9 INOPERATIVE. REPLACED REMOTE ASSEMBLY RECEIVER, THEN FLOOR TRACK LIGHTS TESTED NORMAL. (M) 2L72 4F A16WE 20040308001672004030800167NM 2004 3 8 ASAA0310247 120030327A7110 FRAME BOEING737 737298C 1384490NM NR 1 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 125.25 CHAFED. REMOVED FRAME AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040304001572004030400157EU 2004 3 4 AALA20031243 120031108A2150 BOOT AIRBUS300 A300B4605R 3930308EU RIGHT PACK CUT A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2177080 626 JFK - FLT 619 - EN ROUTE JFK-SDQ, CABIN UNABLE TO MAINTAIN PRESSURIZATION IN AUTO AND MANUAL MODE. RETURNED JFK AND LANDED WITHOUT INCIDENT. RIGHT PACK FOUND WITH RUBBER BOOT CUT BY CLAMP AND LEAKING. REPLACED BOOT AND CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20040308001482004030800148NM 2004 3 8 ASAA0310244 120030327A7110 FRAME BOEING737 737298C 1384490NM NR 1 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 115.25 CHAFED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040308001852004030800185NM 2004 3 8 ASAA0310682 120031222A5310654581511 SHEAR TIE BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND DAMAGED SHEAR TIE AT FUSELAGE STATION 340, STRINGER 26R-27R. REPLACED SHEAR TIE PER SRM. (M) 2L72 4F A16WE 20040308002002004030800200NM 2004 3 8 ASAA0310674 120031219A335086210144 BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - EXIT IDENTIFIER WAS FOUND INOPERATIVE. REPLACED BATTERY PACK. THEN EXIT IDENTIFIER OPERATED NORMAL. (M) 2L72 4F A16WE 20040308001352004030800135NM 2004 3 8 ASAA0310246 120030327A71107076T6040 FRAME BOEING737 737298C 1384490NM NR 2 COWLING TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 110.25-115.25 TORN. REMOVED FRAME AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040308001512004030800151NM 2004 3 8 ASAA0310240 120030327A7110 SKIN BOEING737 737298C 1384490NM NR 2 COWLING DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL SKIN AT NACELLE STATION 110.60-117.60 DENTED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040308001982004030800198NM 2004 3 8 ASAA0310679 120031222A5347655496912 SEAT TRACK BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 683-727, RIGHT BUTTOCK LINE 60 CORRODED. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040309001372004030900137NM 2004 3 9 ASAA0310560 120031025A335086210144 BATTERY BOEING737 7372X6C 1384552NM SMOKE BARRIER DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - FOUND EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M) 2L72 4F RTA16WE 20040309001642004030900164WP 2004 3 9 GTIA031064 120031107A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND EXTERNAL REPAIR AT FS 375, FS 460 DOES NOT HAVE SUFFICIENT FASTENERS INSTALLED. REPAIR EXTENDS INTO FIVE FRAME BAYS AND REQUIRES REPLACEMENT. REMOVED EXTERNAL REPAIR DOUBLER. CUT OUT SIZE (84.5 BY 14 INCHES). FABRICATED NEW SKIN 4 STRAPS, TWO 9 DOUBLERS, TWELVE 5 DOUBLERS. INSTALLED ALL REPAIR PARTS AND SKIN. (M) 2L72 4F RTA6WE 20040308001952004030800195NM 2004 3 8 ASAA0310678 120031222A53156546817501 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 294, LEFT BUTTOCK LINE 11 CORRODED. REPLACED DAMAGED SECTION OF FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040309001492004030900149 2004 3 9 GTIA031052 420031228A2565 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 SJU - FLT 770 - L2 SLIDE PACK FELL OFF OF DOOR. REINSTALLED L2 SLIDE PACK. (M) 2L72 4F A6WE 20040309001522004030900152WP 2004 3 9 GTIA031062 120031112A335092745681 RELAY DOUG DC9 DC981 3022081WP COCKPIT FAILED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23818NK 48018 FTW - WHEN EMERGENCY DC BUS FEED C/B IS PULLED THE CAPTAINS, F/O'S, LEFT PEDESTAL AND CENTER INSTRUMENT PANEL LEFT FLOODLIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED R2-22 RELAY. (M) 2L72 4F A6WE 20040309001552004030900155WP 2004 3 9 GTIA031054 120031116A5313 STRINGER DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN STATION 1315 STRINGER 18L CORRODED. FORMED NEW ANGLE REPAIR. INSTALLED ANGLE DOUBLER. REPAIR ACCOMPLISHED EA 5310-0325. REMOVED FITTING. DRILLED UP NEW FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20040309001672004030900167NE 2004 3 9 GTIA031067 220031229A7310 SEAL DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE NR 2 ENGINE DAMAGED A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23806NK 48051 NR 2 ENGINE FUEL LEAK. INSTALLED SEAL ON LINE GOING FROM PYLON TO NR 2 FUEL BRIDLE LINE. PERFORM LEAK AND OPERATIONAL CHECK OF FUEL DISTRIBUTION FUEL BRIDLE. (M) 2L72 4F4 F A6WE E2EA 20040309001802004030900180NM 2004 3 9 ASAA0310644 120031217A335086210144 BATTERY BOEING737 7372X6C 1384552NM SMOKE BARRIER DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 ANC - DURING INSPECTION, FOUND THE EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHT TESTED NORMAL. (M) 2L72 4F RTA16WE 20040316000122004031600012WP 2004 3 16 ASAA0380298 120030408A5320993061295 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 1293 ON RIGHT SIDE, OUTBOARD OF OUTBOARD TRACK. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-05. (M) 2L72 4F RTA6WE 20040316000192004031600019NM 2004 3 16 ASAA0370013 120030314A3397 WIRE BOEING737 737790 13844CNNM EMERGENCY LIGHT BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01644AS 30795 DURING A MAINTENANCE CHECK, A BROKEN WIRE WAS FOUND IN THE FORWARD CABIN EMERGENCY TRACK LIGHTS. REPLACED AN EMERGENCY TRACK LIGHT ASSEMBLY. THE TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA16WE 20040316000212004031600021WP 2004 3 16 ASAA0380361 120030418A5510993780429 FAIRING DOUG DC9 DC983 3022083WP HORIZONTAL STAB CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND LEFT HORIZONTAL STAB FAIRING CRACKED AT ATTACH POINT. INSTALLED DOUBLER PER EA 5520-01156 AND SRM'S 51-10-3 AND 55-03. (M) 2L72 4F RTA6WE 20040316000282004031600028WP 2004 3 16 ASAA0380288 120030404A5710993758814 SHEAR TIE DOUG DC9 DC982 3022082WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2, AND 30-5. (M) 2L72 4F A6WE 20040316000322004031600032NM 2004 3 16 ASAA0310543 120031003A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 SEA - DURING RECON INSPECTION, FOUND BATTERY PACKS AT SEAT PALLETS 5-12 AND 8-9 INOPERATIVE. REPLACED BATTERY PACKS, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040316000852004031600085 2004 3 16 ASAA0380304 420030408A25653961896501 LANYARD DOUG DC9 DC983 3022083WP L1 DOOR DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01977AS 53453 LAX - PREFLIGHT CHECK, FOUND FORWARD LEFT PASSENGER L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040316000872004031600087WP 2004 3 16 ASAA0380278 120030402A53403936668507 FITTING DOUG DC9 DC983 3022083WP FLOOR SUPPORT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT FITTING BETWEEN PANELS C1 AND C2 IS CRACKED. REPLACED FITTING PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040316000892004031600089WP 2004 3 16 ASAA0380281 120030403A5320993061295 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FUSELAGE MEMBRANE WEB CRACKED IN TWO PLACES AT FS 1293. STOP DRILLED AND INSTALLED DOUBELR EPR SRM 53-05. (M) 2L72 4F RTA6WE 20040316000402004031600040NM 2004 3 16 ASAA0310530 120030928A335086210144 BATTERY BOEING737 7372X6C 1384552NM EMERGENCY SIGN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - FOUND EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M) 2L72 4F RTA16WE 20031212001082003121200108NM 2003 12 12 SWAA032442 120031105A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 13R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031212001102003121200110NM 2003 12 12 SWAA032444 120031105A531565C25723 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND 2 EA CHORDS CRACKED AT BS 616, LBL AND RBL 60, WL 200. REPAIRED CHORDS PER BFG ER. 2L72 4F RTA16WE 20031212001122003121200112 2003 12 12 SWAA032446 420031105A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20031212001372003121200137WP 2003 12 12 AALA20030935 120030902A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21405A 49316 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE IN THE AFT CABIN RIGHT SIDE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001472003121200147WP 2003 12 12 AALA20030927 120030830A3397 WIRE DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21513AA 49890 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE ON AFT OF WING IN CABIN. LOOSE WIRE FOUND AND REPOSITIONED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001492003121200149WP 2003 12 12 GTIA030854 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 22 INCH - 50 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031212001562003121200156WP 2003 12 12 GTIA030858 120030930A5314 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND RIGHT SIDE MLG FORWARD DOOR JAMB FRAME ATTACHED KEEL BEAM CRACKED AT DOUBLER. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED NEW REPAIR DOUBLERS. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20031212001582003121200158WP 2003 12 12 GTIA030856 120030831A5755 SKIN DOUG DC9 DC982 3022082WP LT SPOILER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND LEFT WING INBOARD FLIGHT SPOILER UPPER SURFACE DELAMINATED. REMOVED LEFT WING INBOARD FLIGHT SPOILER. REPAIRED LEFT WING INBOARD FLIGHT SPOILER UPPER SURFACE. INSTALLED LEFT WING INBOARD FLIGHT SPOILER. (M) 2L72 4F A6WE 20031212001612003121200161WP 2003 12 12 AALA20030956 120030904A3350020172004 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT ROW 19D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001622003121200162WP 2003 12 12 AALA20030955 120030904A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS WERE INOPERATIVE IN THE AFT CABIN AND TAILCONE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001642003121200164WP 2003 12 12 AALA20031206 120031102A3350AAP3274A CHARGER DOUG DC9 DC983 3022083WP COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21964TW 53614 DFW - DURING OVERNIGHT MAINTENANCE, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY B5-23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031212001702003121200170WP 2003 12 12 AALA20030916 120030831A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217538A 49992 MIA - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY LIGHTS WERE INOPERATIVE ON LEFT AND RIGHT SIDES. REPLACED BATTERY PACK B5-105. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215000052003121500005NM 2003 12 15 AWXA200301441 120031106A532069770803 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MINOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN FLOOR SUPPORT ATTACH BRACKET (CHANNEL) IN RADIUS OF OUTSIDE SUPPORT BS 986, RBL 21.5, WL 207.8. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT CHANNEL BS 986, RBL 21.5, INSTALLED A NEW REPLACEMENT CHANNEL IAW SRM 51-40-02 PG 1, 45, FIG 12. 2L72 4F RTA16WE 20031215000102003121500010NM 2003 12 15 QXEA200301421 120031112A245011521486 CONTACTOR BOMBDRDHC8 DHC8401 1390041NM ELECTRICAL SYS FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09546DS5095 49 4017 SEA- ON FLIGHT 2323 NR 2 AC GENERATOR CAUTION ILLUMINATED ON APPROACH, IT WOULD NO RESET PER CHECKLIST. REMOVED NAD REPLACED AC CONTACTOR BOX. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000182003121500018NM 2003 12 15 QXEA200301433 120031115A5542 SKIN DHAV DHC8 DHC8202 2809007NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX- A 2.25 INCH LONG CRACK IN SKIN OF FORE RUDDER NEAR TOP AFT CORNER. REPAIRED IAW DHC-8 RD 8-55-335. 2H72 4T RTA13NM 20031215000202003121500020NM 2003 12 15 SWAA032519 120031114A5551BACB30 PIN BOEING737 7377H4 1384404NM HORIZ STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED 5Y CHECK, FOUND BOTH LT HORIZONTAL STAB REAR SPAR ATTACH PIN CORRODED. REMOVED AND REPLACED ATTACH PINS PER SWA EA AND MM. 2L72 4F RTA16WE 20031215000272003121500027NM 2003 12 15 SWAA032526 120031116A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED A2 CHECK, FOUND 2 LONG CRACK AT FUSELAGE SKIN, BS 727E, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031215000322003121500032NM 2003 12 15 SWAA032509 120031113A53206551698 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20031215000452003121500045NM 2003 12 15 2003UALA00796 120031022A339758781 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29312UA 23673 EEL LIGHTS INOP IN AFT CABIN FROM ROWS 15 - 21. REPLACED FEEDER CABLE FROM ROWS 15-21. 2L72 4F4 FRTA16WE E2GL 20031215000562003121500056NM 2003 12 15 2003UALA00837 120031024A5754114N300358 WEDGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29527UA 24995 T/E WEDGE DELAMINATED, SLAT NR 6. MAJOR REPAIR ACCOMPLISHED. REPLACED WITH NEW T/E WEDGE. 2L72 4F4 FRTA2NM E17NE 20031211000262003121100026 2003 12 11 C8GA20030026 420031021A3417HG480B13 ADC BOEING727 7272A1 138407FNM E/E BAY FAULTY A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15287SC4374 21345 FLT 738 FROM TOL TO SLW. SHORTLY AFTER TAKEOFF, THE CAPTAIN'S ALTIMETER AND THE ALTITUDE ALERTER FLAGGED AND THE AUTOPILOT WOULD NOT ENGAGE. THE CREW TRIED CYCLING THE CIRCUIT BREAKER FOR THE AIR DATA COMPUTER BUT IT WOULD GO OFF AGAIN AFTER ONE SECOND. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT AIR TURNBACK TO TOL AND LANDED WITHOUT INCIDENT. UPON LANDING IN TOLEDO, THE NR 1 AIR DATA COMPUTER WAS REPLACED AND PITOT STATIC SYSTEM LEAK CHECK IAW B727 MM 34-12-0 AND 34-11-0. AIRCRAFT RETURN TO SERVICE. 2L73 4F A3WE 20031211000362003121100036NM 2003 12 11 QXEA200301395 120031108A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM09406QX 4048 SEA- ON FLIGHT NUMBER 2338, RETURNED TO FIELD DUE TO FUSELAGE DOOR WARNING LIGHT CAME ON ON ROTATION. FOUND AFT CARGO DOOR HANDLE NOT STOWED. OPENED/CLOSED CARGO DOOR SEVERAL TIMES AND INSPECTED HANDLE LATCH. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031211000402003121100040EA 2003 12 11 QXEA200301407 120031021A5753 VANE CNDAIRCL600 CL6002C10 1390015EA T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 CKB- LEFT AFT OUTBOARD FLAP VANE ASSEMBLY HAS A CHAFE .003 INCH DEEP AND .250 INCH LONG APPROXIMATELY 2 INCHES FROM OUTBOARD EDGE. REPAIRED IAW WVAC EO 601R-57-4319A AND HORIZON AIR EO R-57-50. 2L72 4F RTA21EA 20031211000702003121100070WP 2003 12 11 UPS03841563 120031022A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN STATION 220-260 LONG 29R-35L. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 9755878 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20031211000942003121100094EU 2003 12 11 03FDEA01884 120031106A3230D221270005 DAMPER AIRBUS310 A310 EU RT MLG LOW A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25423FE 281 LANDING GEAR LEVER WOULD NOT RETRACT ON SYS 2 SWITCHED TO SYS 1, STILL WOULD NOT RETRACT. THREE GREEN DOWN WITH 3 RED UNLK. FOUND RIGHT SIDE PITCH DAMPER INDICATION, RESET PIN & RESERVICED PITCH DAMPER WITH NITROGEN TO 1700 PSI. FOUND THE SYSTEM AT 1000 PSI. ALSO PERFORMED A BITE CHECK ON PROX BOX & ALL SYSTEMS ARE GOOD. A/C OK FOR SERVICE. ALL SERVICING PERFORMED PER M/M 12-12-3 2-0 SECTION 9. 2L72 4F RTA35EU 20031211001692003121100169WP 2003 12 11 AALA20030923 120030829A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21276AA 49273 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE ON LEFT SERVICE DOOR AND LEFT FORWARD DOOR. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031211001892003121100189EU 2003 12 11 USAA030254 120031031A5320D53112782200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT CORRODED 2.5 INCHES IN LENGTH, BY 1 INCH WIDE, MAX DEPTH .50 INCH, BETWEEN FRAME 14-21, RBL 48 LONGITUDINAL BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. (M) 2L72 4F RTA28NM 20031215000612003121500061NE 2003 12 15 COMA0360499 220031115A72605018T49P01 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE LEAKING A COMAEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO01712CA 7244 FLIGHT 5803 RT ENGINE LOST OIL PRESSURE IFSD. REPLACED THE RT ACCESSORY GEAR BOX OIL SEALS. 2L72 4F4 FRTA21EA E15NE 20031215000632003121500063EA 2003 12 15 COMA0360500 120031116A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01954CA 7100 FLIGHT 5044 FLAPS FAIL WARNING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031215000952003121500095NM 2003 12 15 MWEA030445 120031120A5320991156921 INTERCOSTAL DOUG MD88 MD88 3023688NM FUSELAGE GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 STATION 200-207 INTERCOSTAL AT LONGERON 10 RIGHT HAS SEVERAL GOUGES. FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F RTA6WE 20031215001102003121500110WP 2003 12 15 AALA20030960 120030904A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21495AA 49733 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE COMMON TO BATTERY PACK B5-104. REPLACED PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001212003121500121WP 2003 12 15 AALA20030970 120030908A33500211720004 SOCKET DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21456AA 49561 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 22D. REPLACED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001442003121500144WP 2003 12 15 AALA20031092 120031001A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21465A 49595 DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 20 THROUGH 25. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001492003121500149WP 2003 12 15 AALA20031195 120031030A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21241AA 49254 DEN - DURING OVERNIGHT MAINTENANCE, FOUND CEILING LIGHTS AT CLASS DIVIDER STATION 386 INOPERATIVE. REPLACED BATTERY PACK B5-100. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001522003121500152WP 2003 12 15 AALA20031124 120031003A33503015643 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21274AA 49271 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 4E. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001542003121500154WP 2003 12 15 AALA20031190 120031030A3397 WIRE HARNESS DOUG DC9 DC982 3022082WP CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21214AA 49162 DFW - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REPLACED SEAT 15D EMERGENCY LIGHT PIGTAIL HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001742003121500174EU 2003 12 15 ASOA03528 120031021A33507012210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11633AS 344 DURING AN 'A' CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031215001792003121500179EA 2003 12 15 ASOA03539 120031025A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031215001872003121500187NM 2003 12 15 AALA20031170 120030423A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 LAX - MAINTENANCE OBSERVED EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 2 THROUGH 13. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031215002002003121500200EU 2003 12 15 USAA030262 120031101A5320D534711240100 PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND TRANSITIONAL WITH CORROSION 1.25 INCHES WIDE BY 1 INCH LONG BY .030 INCH DEEP, RT OUTBOARD FRAME 69, OUTBOARD OF -Y114 TRANSITION PANEL/SHEAR WEB. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. (M) 2L72 4F RTA28NM 20031216000112003121600011NM 2003 12 16 QXEA200301449 120031105A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- AIRCRAFT SKIN UNDER LOWER VHF ANTENNA IS CORRODED. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16, 51-00-06, 51-00-04, RD 8-53-7635 AND HORIZON AIR EA 2-53-505. 2H72 4T RTA13NM 20031216000382003121600038 2003 12 16 SWAA032554 420031119A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031216000422003121600042 2003 12 16 SWAA032528 420031117A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031216000642003121600064NM 2003 12 16 SWAA032559 120031120A52106545871 DOOR FRAME BOEING737 7372H4 138448CNM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 L2 DOOR FRAME CRACKED AT FWD LOWER END. REMOVED AND REPLACED L2 DOOR PER MM. 2L72 4F A16WE 20040511000142004051100014GL 2004 5 11 ERAA094463 220031206A7320 BYPASS VALVE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL FUEL CONTROL STUCK A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03125EH10220 333673 S562 ENGINE WILL NOT START UNLESS BOOST PUMPS ARE OUT. BYPASS VALVE SEEMS TO BE STUCK OPEN. ACTION TAKEN: SENT TO MFG AND OVERHAUED IAW MFG OHM FORM 15-602E. 1G72 3U3 U H3EU E4CE 20040512001122004051200112SW 2004 5 12 ERAA094443 120030917A6230412040366105 MAST BELL 412 412 1182202SW MAIN ROTOR MAKING METAL A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03419EH16434 TRANSMISSION MAKING METAL ACTION TAKEN: DISASSEMBLED, CLEANED AND VISUALLY INSPECTED ALL PARTS AND BEARINGS FOR METAL CONTAMINATION. INSPECTED AND REASSEMBLED IAW 412 CR AND O CHAPTER 63, T.B. 412-96-137 AND T.B. 412-98-150 INSTALLING NEW MAST POLE, NEW BEARING RETENTION NUT, NEW LOWER RACE, NEW NUT, NEW SEAL AND O RING AND NEW WEAR SLEEVE. COMPLIED WITH T.B.412-96-137 AND T.B. 412-98-150. 1G72 4U H4SW 20040514001212004051400121NE 2004 5 14 3103 220031007A7200 ENGINE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 1 FIRE W EF ENGINE SHUTDOWN ACTIVATE FIRE EXT. AJ FLAME/FIRE WARNING INDICATION APAPPROACH 1 SO23VPBNH 261 FIRE ALARM NR 1 ENGINE ON FINAL APPROACH. AFTER LANDING, SMOKE DETECTED FIRE BOTTLES WERE DISCHARGED. ENGINE REPLACED. 2H72 4T4 TRTA53EU E20NE 20040419000812004041900081WP 2004 4 19 ASAA0380815 120031126A53115913595501 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURNG 15K CHECK, FOUND FRAME CHAFED AT FS 1418. REMOVED DAMAGE. INSTALLED ANGLE, PLATE, AND FILLER PER SRM 53-03 AND 51-10-3. (M) 2L72 4F RTA6WE 20040614001602004061400160NM 2004 6 14 RYN2004F00020 120030430A2612 WARNING LIGHT BOEING737 7374Y0 1384705NM PWA JT8 JT8D9 52048NE APU FIRE ILLUMINATED A RYNAFC ACTIVATE FIRE EXT. ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE07254RY 21451 APU FIRE WARNING LIGHT AND BELL CAME ON AFTER TAKE-OFF FROM LAS. DISCHARGED APU FIRE BOTTLE. PERFORMED EMERGENCY ACTION ITEMS IAW QUICK REFERENCE HANDBOOK. AIRCRAFT LANDED WITHOUT INCIDENT IN LAS APU AND APU FIRE EXTINGUISHER, DEFERRED. AIRCRAFT REMOVED FROM OUR CERTIFICATE ON 5/1/03. 2L72 4F4 FRTA16WE E2EA 20040614001902004061400190NM 2004 6 14 RYN2004F00026 120030807A322065404674 ACTUATOR BOEING727 72721 1384003NM PWA JT8 JT8D* NE NLG LOCK SPLIT A RYNAO OTHER J WARNING INDICATION CLCLIMB 1 CE07356QS 19258 AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. GREEN LIGHT ON, RED L DOOR LIGHT OUT, AND HYDRAULIC PRESSURE NORMAL. AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR. OPERATIONAL CHECK OF THE LANDING GEAR NORMAL. 2L73 4F4 F A3WE E2EA 20040614001942004061400194CE 2004 6 14 GUU2004F00009 120030110A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO171753414965 UE141 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040614001952004061400195CE 2004 6 14 GUU2004F00012 120030321A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178153814227 UE199 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040614001992004061400199CE 2004 6 14 GUU2004F00010 120030114A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178153515244 UE147 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040614002362004061400236SW 2004 6 14 JJWA0053223 120031203A6320MS172224 LOCKWASHER BELL 206 206B 1181511SW ALLSN 250C 250C* GL M/R TRANSMISSIONDEFECTIVE E JJWAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO1725PM 2868 1839 TRANSMISSION CHIP LIGHT CAME ON ON LANDING. FOUND TANG FROM ACCESSORY DRIVE LOCK WASHER ON CHIP DETECTOR. VERIFIED ON TRANSMISSION DISASSEMBLY. ALL TRANSMISSION BEARINGS REPLACED 1/9/1998 . OTHER WASHER TANG NOT IN NUT SLOT AND BENT SUGGESTING IMPROPER INSTALLATION. UNFORTUNATELY FOUND SUN GEAR 206-040-122-3 AND SHAFT 206-040-003 SPLINE AREAS WORN EXCESSIVE CAUSING MINOR REPAIR TO BECOME EXPENSIVE. SUN GEAR ONE UPPER TOOTH HARDNESS COATING CHIPPED OFF, NO DAMAGE TO PLANETARY OR ANY OTHER COMPONENTS, NO METAL FLAKES ON OIL FILTER OR IN GEAR CASE. 1G71 3U3 U H2SW E4CE 20040614003382004061400338EA 2004 6 14 COMA0460314 120031106A5330601R3114627 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01949CA 7080 PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102. 2L72 4F RTA21EA 20040614002522004061400252NM 2004 6 14 RYN2004F00023 120030903A2611 SMOKE DETECTOR BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE CARGO BAY FALSE ACTIVATIONA RYNAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE077644U 20038 AC DEPARTED, ENROUTE, MAIN CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED. AC DIVERTED WITHOUT INCIDENT. INSPECTED AC FOR EVIDENCE OF BURNED WIRES AND FLUIDS. NO EVIDENCE FOUND. INSPECTED CARGO SMOKE DETECTORS AND PERFORMED FUNCTIONAL TEST OF CARGO SMOKE DETECTION SYS. SYSTEM OPERATIONAL CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040614002582004061400258NM 2004 6 14 RYN2004F00021 120030712A27821U109592 ACTUATOR BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE RT WING SLAT LEAKING A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE077639U 19912 AFTER TAKEOFF, DURING ASCENT TO FLIGHT LEVEL 24.0 NR 7 FLAP LED AND YELLOW LIGHTS STAYED ILLUMINATED DURING FLAP RETRACTION. IMPLEMENTED PROCEDURES IAW MM FOR TROUBLESHOOTING. MANUAL STATED TO PROCEED WITH FLIGHT IF LIGHT EXTINGUISHED. LIGHTS EXTINGUISHED. UPON REACHING FLIGHT LEVEL 24.0 SPEED .80 MACH LIGHTS FOR NR 7 SLAT LED AND YELLOW LIGHTS ILLUMINATED ON FO BACK PANEL. THE AIRCRAFT ROLLED SLIGHTLY TO THE RT. PILOT SLOWED AC TO 230 KNOTS AND DESCENDED TO FLIGHT LEVEL 17.0 AND RETURNED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NR 7 SLAT ACTUATOR IAW MM. 2L73 4F4 F A3WE E2EA 20040924000722004092400072NE 2004 9 24 2004F00361 220031126A753239854221 BLEED VALVE BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE NR 1 ENGINE INOPERATIVE A PCSAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO17994AJ 20942 CREW REPORTED, NR 1 ENGINE BLEED AIR VALVE TRIP LIGHT ON DURING FLIGHT AND VALVE STATED CLOSED AFTER ACCOMPLISHING THE ALTERNATE PROCEDURE FROM AOM. AIRCRAFT RETURNED TO KMIA WITHOUT FURTHER INCIDENT. MAINTENACNE REMOVED AND REPLACED THE NR 1 ENGINE BLEED SHUTOFF VALVE IAW MM 36-10-01. OPS CHECKED ACCOMPLISHED IAW AMERIJET FORM B-41. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2L73 4F4 FRTA3WE E2EA 20031216000682003121600068NM 2003 12 16 SWAA032564 120031120A3350BR2013 STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 8. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20031216000692003121600069NM 2003 12 16 SWAA032565 120031120A27316959227 LINKAGE BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED SERVICE CHECK, RT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEV TAB NR 1 HINGE ATTACH HARWARE, AND TAB LOCKOUT MECHANISM LINKAGE PER MM. 2L72 4F RTA16WE 20031216000942003121600094SO 2003 12 16 C2XA03SH493 120031213A532014524119007 SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE MAIN PASSENGER DOOR SILL SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE MAIN PASSENGER DOOR SILL SUPPORT IAW EMB 145 IPC 53-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031217000022003121700002WP 2003 12 17 0302069994 120031114A2120 ODOR DOUG DC9 DC931 3022065WP CABIN DETECTED A NWAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL018979E 47328 AFTER TAKEOFF, THERE WAS A SMOKE ODOR IN THE AIRCRAFT AND THE SMOKE DETECTORS WERE SOUNDING. FLIGHT CREW DECLARED AN EMERGENCY, RETURNED TO DTW, AND LANDED WITHOUT FURTHER INCIDENT. FIRE RESCUE MET AND INSPECTED THE AIRCRAFT BUT FOUND NO EVIDENCE OF FIRE. MAINTENANCE REMOVED EXCESS OIL FROM BOTH ENGINES AND THE APU AND REPLACED BOTH COALESCER BAGS. NO EVIDENCE OF OIL OR DEBRIS IN THE SADDLE DUCT CAPS. RUN-UP OF ENGINE TO 1.7 EPR WITH PACKS AT FULL HOT FOR 10 MINUTES. NO SMOKE OR SMELL REMAINING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20031217000052003121700005EA 2003 12 17 MASA200300456 120031117A33503540S1202 RHEOSTAT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 EMERGENCY EXIT LIGHTING CONTROL INOP WITH FLIGHT ATTENDANTS SWITCH. MX REPLACED BROKEN TERMINAL LUG. 2L72 4F RTA21EA 20031217000062003121700006EA 2003 12 17 MASA200300457 120031117A3350BD50017003 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW0737218 7218 PILOT REPORTED THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR HAD LOOSE LENS. MX REPLACED THE LENS. 2L72 4F RTA21EA 20031211001312003121100131NM 2003 12 11 AALA20031336 120031127A2560 BATTERY PACK BOEING757 757223 1384957NM FLASHLIGHT DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21672AA 25337 SFO AFT RIGHT HAND INBOARD ATTENDANT EMERGENCY FLASHLIGHT LED INOPERATIVE. REPLACED BATTERY PACK FOR AFT RIGHT HAND INBOARD ATTENDANT EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031211001492003121100149WP 2003 12 11 AALA20031275 120031116A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21598AA 53288 STL SEAT 15 LEFT INSEAT EMERGENCY LIGHT INOPERATIVE. REPLACED ROW 15 OVERHEAD EMERGENCY LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031211001732003121100173EU 2003 12 11 USAA030248 120031031A5320D5347209000200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND FLOOR SUPPORT CORRODED 2.2 INCH LONG BY 2.0 INCHES WIDE BY .041 INCH DEEP, LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAME 65 AND FRAME 66. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-40-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20031212000042003121200004EU 2003 12 12 03316307 120031112A5610 SEAL JETAIRJETSTMJETSTM4101 1500501EU COCKPIT LEAKING A VTZABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27307UE 41021 DURING CLIMB ON FLIGHT 7799 FROM JFK FLIGHT CREW IN RAINY CONDITIONS CREW NOTED A SMOKE SMELL AND THE EHSI SCREEN WENT BLANK. EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. FAULT WAS TRACED BACK TO A LEAKING DV WINDOW CAUSING EHSI DISPLAY UNIT TO FAIL. THE WINDOW SEAL WAS CLEANED AND REINSTALLED AND THE EHSI DISPLAY UNIT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031212000322003121200032NM 2003 12 12 SWAA032428 120031103A531165C25722 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND INNER CHORD CRACKED AT BS 616, WL 208, LBL 62.5. REPAIRED CHORD PER SWA T1-153-18. 2L72 4F RTA16WE 20031212000382003121200038EU 2003 12 12 YENA200337 120031114A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN FAILED A YENAK NONE J WARNING INDICATION ININSP/MAINT 1 EA15526JB8982 1546 ON WEEKLY CHECK EPSU INTERMITTENT LOAD AFT -L- MSG ON FWD FLAP. REMOVED AND REPLACED AFT -L- EPSU AMM REF 33-51-38-000-001. 2L72 4F RTA28NM 20031212000452003121200045 2003 12 12 SWAA032500 420031112A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031212000462003121200046NE 2003 12 12 MWEA030443 220031113A7421CH347601 IGNITER BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LT ENGINE FAILED A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31909ME 55173 13374 RIGHT AND LEFT ENGINE WOULD NOT START. REMOVED AND REPLACED RIGHT AND LEFT IGNITER PLUGS. 2L72 4F4 FTRA6WE E00061EN 20031212000702003121200070EA 2003 12 12 MASA200300433 120031030A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT FALSE INDICATIONA MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0717275 7175 ASH FLT 3339 DEN-ABQ. PILOT RETURNED TO FIELD FOR PAX DOOR WARNING MESSAGE IN FLIGHT. MX COULD NOT DUPLICATE. OP CHECKS GOOD. 2L72 4F RTA21EA 20031212001712003121200171EA 2003 12 12 COMA0360525 120031202A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 FUSELAGE SKIN FS 600 BETWEEN STRINGERS 21L TO 22L HAS GOUGE APPROX .004 INCH DEEP. REPAIRED BY REMOVING DAMAGE, PERFORMING EDDY CURRENT INSPECTION, FABRICATING EXTERNAL REPAIR DOUBLER AND INSTALLING IAW CRJ 200 SRM 53-00-31 REPAIR NR 1. 2L72 4F RTA21EA 20031215000072003121500007NM 2003 12 15 AWXA200301443 120031106A532066235743 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN TIE CLIP AT BS 706, STR 11 LT. MAINTENANCE REMOVED AND REPLACED CRACKED TIE CLIP AT BS 706, STR 11 LT IAW SRM 51-40-02, PG 1, 38 & 55 FIG 8, 12 & 14. 2L72 4F RTA16WE 20031215000532003121500053NM 2003 12 15 2003UALA00834 120031104A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 DOOR 1R EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSEMBLY. 2L74 4F4 FRTA20WE E24NE 20031215000682003121500068EA 2003 12 15 03272629 120030929A2910601R752863 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A VTZAO OTHER K FLUID LOSS APAPPROACH 1 EA27629BR 7251 DURING FINAL NR 1 HYDRAULIC SYSTEM LOST ALL FLUID. AIRCRAFT LANDED SAFELY AND PASSENGERS DEPLANED NORMALLY. THE NR 1 HYDRAULIC PRESSURE SERVICE LINE HAD A HOLE IN IT AND WAS REPLACED. A SATISFACTORY LEAK CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031215001122003121500112WP 2003 12 15 AALA20030993 120030911A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21225AA 49175 SAT - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTING INOPERATIVE AT THE FORWARD GALLEY AND FLIGHT DECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001132003121500113WP 2003 12 15 AALA20030992 120030911A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21236AA 49251 DEN - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTING INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001262003121500126WP 2003 12 15 AALA20030957 120030905A3397 WIRE DOUG DC9 DC982 3022082WP CABIN PULLED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21223AA 49173 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT SEAT 29D. REATTACHED PULLED WIRES FROM CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001292003121500129WP 2003 12 15 AALA20030961 120030904A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP TAILCONE DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21466AA 49596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE IN THE TAILCONE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001372003121500137WP 2003 12 15 AALA20031121 120031003A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21274AA 49271 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT TAILCONE. SECURED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001892003121500189WP 2003 12 15 AALA20031208 120031102A3350AAP3274A CHARGER DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21964TW 53614 DFW - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD RIGHT AND LEFT OVERWING DOOR EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031215001932003121500193EU 2003 12 15 USAA030264 120031031A5320D2557206222800 FITTING AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 CARGO TIE DOWN FOUND WITH 1 INCH IN DIAMETER OF LIGHT SURFACE CORROSION, FRAME 29 BL 0. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-72-11. CORROSION LEVEL 2, TASK NR JA-135-53500. (M) 2L72 4F RTA28NM 20031216000052003121600005NM 2003 12 16 AWXA200301476 120031105A71106573771 FRAME BOEING737 737277 1384570NM NR 1 COWLING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 LCQ - MINOR REPAIR - DURING C-14 CHECK .75 INCH CRACK WAS FOUND IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7 AT PREVIOUS CUTOUT. MAINTENANCE CUTOUT CRACK IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-200 SRM 51-40-03, FIG 001. 2L72 4F RTA16WE 20031216000142003121600014NM 2003 12 16 QXEA200301452 120031104A1430 RIVET DHAV DHC8 DHC8202 2809007NM RUDDER LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- FORE RUDDER LOWER CLOSING RIB HAS LOOSE RIVET AT FORWARD RIGHT HAND SIDE. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20031216000342003121600034 2003 12 16 SWAA032550 420031119A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2/R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED SLIDES PER MM. 2L72 4F A16WE 20031216000432003121600043NM 2003 12 16 SWAA032529 120031117A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND BS 188 LT FUSELAGE FRAME CRACKED AT WL 207. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031216000972003121600097SO 2003 12 16 C2XA03SH491 120031211A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031217000082003121700008NM 2003 12 17 03323428 120031119A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27428FJ 3193 DURING INSPECTION THE FORWARD SECTION OF THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPY WAS IDENTIFIED AS THE SOURCE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031217000092003121700009NM 2003 12 17 CALA0300652 120031120A5340 ATTACH ANGLE BOEING737 737524 1384721NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711651 28912 INSPECTION FOUND A GOUGE ON VERTICAL ATTACH ANGLE ON RT SIDE OF VERTICAL STRAP AT STA 1121. A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013. 2L72 4F RTA16WE 20031217000232003121700023EA 2003 12 17 COMA0360507 120031118A2730DL2428M4 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LT ELEVATOR MALFUNCTIONED A COMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01975CA8855 7150 ELEVATOR CONTROLS STIFF. REPLACED THE LEFT ELEVATOR PITCH FEEL ACTUATOR. 2L72 4F RTA21EA 20031217000302003121700030WP 2003 12 17 DHL2003805600 120030905A573056538362 PANEL DOUG DC8 DC873F 302199FWP RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT CTR WING LOWER PART PANEL NR 721 INTERNAL SKIN DELAMINATED AT STA 730.000. REMOVED AND REPLACED NR 721 PANEL ON RIGHT CTR WING, STA 730.000. FOR REMOVAL SEE JC 8-10-30-003, FOR INSTALLATION SEE JC 8-90-30-003. 2L74 4F RT4A25 20031217000332003121700033WP 2003 12 17 DHL2003805598 120030903A5280 BRACKET DOUG DC8 DC873F 302199FWP MLG DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 N/R LT MLG MID DOOR LWR BRACKET WITH CRACK IN IT. REMOVED AND REPLACED BRACKET TO LEFT MLG MID DOOR IAW SRM 32-12-1 PG 401. REFER TO JC 8-32-20-007 FOR OPS CHECK. 2L74 4F RT4A25 20031217000362003121700036WP 2003 12 17 DHL2003805510 120030804A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 MAIN CARGO COMPT NR 7 CARGO TRACK LUG WORN (STA 289.000 - 329.000). TRIMMED OUT DAMAGED CARGO TRACK SECTION IAW SRM 53-2-3 PG 49-50. FABRICATED SPLICES (7075-T6 AL0.100, 0.125, 0.160) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CARGO TRACK AND SPLICE IAW SRM 53-2-3 PG 49-50. 2L74 4F RT4A25 20031217000432003121700043WP 2003 12 17 DHL2003805508 120030803A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FRAME 1.000 CRACKED, STA XFS 429.000 (LWR SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS (2024-T3 0.040) 92024-T3 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031217000472003121700047WP 2003 12 17 DHL2003805588 120030828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT WING EXTENDED L/E INBD VANE FWD PLATING ELONGATED HOLES AT STA XS 247.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER EXTERNAL DOUBLER (7075-T6 AL0.071), AN INTERNAL DOUBLER (7075-T6AL0.050) AND A FILLER (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED THE EXTERNAL REPAIR DOUBLER INTERIOR SURFACE AND INTERNAL DOUBLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED REPAIR EXTERNAL DOUBLER, INTERNAL DOUBLER AND FILLER ON RIGHT WING EXTENDED L/E INBD VANE FWD PLATING (AT STA XS 247.000) USING NEW FASTENERS. FOR LEAK CHECK SEE JC 8-36-00-003. 2L74 4F RT4A25 20031217000552003121700055WP 2003 12 17 DHL2003805576 120030825A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING OTBD FLAP UPPER SKIN SHOWS INTERIM REPAIR AROUND XF 345.000 TO STA XF 354.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN SEGMENT (2024-T3 AL0.063) AND A SPLICE STRAP (7075-T6 AL0.063) IAW DHL-EDT66-5 AND DHL-DWGT66-R05. CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT INTERIOR SURFACE AND THE SPLICE STRAP IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED THE NEW SKIN SEGMENT AND THE SPLICE STRAP ON LEFT WING OTBD FLAP UPPER SKIN (AROUND STA XF 345.000 TO XF 354.500) USING NEW FASTENERS. 2L74 4F RT4A25 20031217000742003121700074WP 2003 12 17 DHL2003807541 120031019A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING CENTER L/E UPPER SKIN CORRODED STA XFS 310.250 - XFS 335.250 XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED (4EA) FILLERS (7075-T6AL 0.063), AND DOUBLER (7075-T6AL 0.071) IAW ASTAR ED EDU21-9 AND DWG U21-R09. CLEANED, TREATED AND PRIMED AREA, FILLERS AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLERS AND DOUBLER WITH NEW FASTENER IAW ASTAR ED EDU21-9, DWG U21-R09, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031217000952003121700095NM 2003 12 17 CALA0300672 120031121A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 INSPECTION FOUND A 2 INCH CRACK IN RIGHT KEELBEAM AT STA 727. A NEW KEELBEAM SECTION WAS SPLICED IN IAW ECRA 5311-01176. 2L72 4F RTA16WE 20031217001122003121700112NM 2003 12 17 2003UALA00850 120031112A5753 HINGE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE TE FLAPS CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29673UA 29241 LT WING INBOARD T/E FLAP EXTERNAL CENTER HINGE CRACKED ON INBD SIDE. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE PER SRM 57-53-02, FIG 201 AND REINSTALLED FITTING PER MM 27-51-06. 2L72 4F4 FRTA1NM E24NE 20040419000212004041900021WP 2004 4 19 ASAA0380841 120031221A532199365811 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01975AS 53451 OKC - DURING C-CHECK, FOUND FLOORBOARD PANEL TORN AND DELAMINATED AT FS 313-389. REMOVED DAMAGED AREA AND REPAIRED WITH FIBERGLASS OVERLAP PER SRM 51-90-0. (M) 2L72 4F RTA6WE 20040419000222004041900022WP 2004 4 19 ASAA0380556 120030718A4940 STARTER DOUG DC9 DC982 3022082WP APU FAILED A ASAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM01935AS 49236 PDX - NOTICED SMOKE COMING FROM APU COMPARTMENT. OPENED COMPARTMENT LEFT DOOR AND OBSERVED FLAMES. ACTIVATED BOTH NR 1 AND NR 2 FIRE BOTTLES. SUBMITTERS STATES, THERE WAS DEFINITELY SMOKE, BUT WHETHER THERE WERE ACTUALLY FLAMES IS SOMEWHAT PROBLEMATIC. ENGINEERING SUGGESTS THAT THERE WAS PROBABLY ONLY SMOKE, AND THAT IT WAS DUE TO VAPORIZATION OF THE COIL AND ARMATURE COATINGS, NOT TO FIRE. SUBSEQUENT SHOP INVESTIGATION/REPAIR REVEALED THAT ALL DAMAGE WAS WITHIN THE APU STARTER MOTOR. THE ELECTRICAL LEADS TO THE STARTER WERE NOT DAMAGED, AS WAS FIRST SUSPECTED. THE STARTER MOTOR WAS REPAIRED BY REPLACING THE COIL AND ARMATURE, AND THE UNIT RETURN TO SEVICEABLE SPARES. (M) 2L72 4F A6WE 20040316000432004031600043NM 2004 3 16 ASAA0340333 120031013A3350S283TO143 BATTERY PACK BOEING737 7374Q8 138447QNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01756AS 25097 RNO - DURING MAINTENANCE CHECK, FOUND 2 EMERGENCY FLOOR TRACK SECTIONS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACKS OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040324000052004032400005NM 2004 3 24 ASAA0340339 120031117A55128602684 SKIN BOEING737 737490 1384715NM LT HORIZ STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01793AS 28888 OAK - DURING C-CHECK, FOUND LEFT HORIZONTAL STAB LE INBOARD SIDE DENTED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040324000162004032400016WP 2004 3 24 ASAA0380713 120031103A53219932816502 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD IS CRACKED AT FS 820-920. REPLACED FLOOR PANEL PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040324000252004032400025WP 2004 3 24 ASAA0380722 120031111A532199365445 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FORWARD LAVATORY FLOORBOARD EDGE DELAMINATED. REPAIRED SECTION WITH FIBERGLASS PER MM 25-41-13. (M) 2L72 4F RTA6WE 20040401000022004040100002 2004 4 1 AALA20031184 420031025A312043410312001 SOCKET BOEING757 757223 1384957NM INSTRUMENT PANELDAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21689AA 25731 ORD - FLT 417 - FOUND RIGHT ENGINE OVERHEAT LIGHT INTERMITTENT. REPLACED LIGHT CAPSULE AND SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040401000222004040100022WP 2004 4 1 ASAA0380275 120030324A33501001101 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR WAS INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040407000662004040700066EU 2004 4 7 2004F00089 120031002A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND AFT CABIN FLOOR SUPPORT HAS CORROSION AT STATION 3850 AND RBL 32. REMOVED LIGHT CORROSION AT NUT PLATE AT STATION 3850 AND RBL 32. FOUND TO BE WITHIN LIMITS. TREATED, PRIMED AND TOPCOAT APPLIED. (M) 2L72 4F RTA28NM 20040412000022004041200002WP 2004 4 12 ASAA0380730 120031111A532199366394 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS WORN V-FLANGES AND U-CHANNELS AT FS 970-1003. REPLACED DAMAGED/WORN PARTS PER SRM 53-24-0, 51-30-8, AND 51-10-4. (M) 2L72 4F RTA6WE 20040412000122004041200012WP 2004 4 12 ASAA0380732 120031111A532199365821 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1130. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040413000042004041300004NM 2004 4 13 ASAA024018C 120030323A531065C32396 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727B LBL 4 - RBL 4 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040412001612004041200161 2004 4 12 KBM2004F00021 420031228A342210302201 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 DIRECTIONAL GYRO WILL NOT POWER UP. REMOVED AND REPLACED GYRO. 1G71 3U3 U H9EU E19EU 20040413000402004041300040NM 2004 4 13 ASAA024015B 120030319A53116546550 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 807, LBL 5 TO RBL 5 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040412001752004041200175WP 2004 4 12 ASAA0380715 120031103A532199365833 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD IS PUNCTURED AT FS 1034-1060. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040413000472004041300047NM 2004 4 13 ASAA024016P 120030322A531065479576 BEAM BOEING737 7374Q8 138447QNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK,FOUND CORROSION ON AFT CARGO DOOR SUB THRESHOLD BEAM AT BS 794-847. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040412001432004041200143NM 2004 4 12 AALA2003100A 120030914A3397 CONNECTOR BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21696AN 26976 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTING INOPERATIVE AT SEAT 19D. RESEATED THE LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040512000982004051200098NE 2004 5 12 UIA9216 220030805A7200 BEARING DOUG MD90 MD9030 3023690NM IAE V2525 V2525D5 NE ENGINE MAKING METAL Z EA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 TW00179268428 53567 V20085 IN FLT, LT ENG OIL STRAINER CLOG MESSAGE SHOW ON EOAP AND OIL PRESSURE DROP TO (0) FAST, FLT CREW SHUTDOWN THE ENG MANUALLY, A/C DIVERTED ON BKI. METAL CHIP WAS FOUND ON MASTER MCD AND NR 1, 2, 3 BEARING COMPARTMENT DAMAGE. THE AIRCRAFT REPLACED THE NR 1 ENG AND FERRIED BACK. THE DAMAGE SENT IAE PFM COMPONENT INVESTIGATION . 2L72 4F4 FRTA6WE A40NE 20040622001462004062200146CE 2004 6 22 AMWA117 120031030A53131014200875 STRINGER CLIP BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE23 WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, STRINGER 13R WAS FOUND TO HAVE A CRACKED CLIP. 2L72 4T RTA24CE 20040622001452004062200145CE 2004 6 22 AMWA115 120031030A5730114430002200 PLATE BEECH 1900 1900D 1154162CE FUSELAGE CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE23 WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE RIGHT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFE. 2L72 4T RTA24CE 20040629000572004062900057WP 2004 6 29 04FDEA01659 120030503A5730ARB0983 DOUBLER DOUG DC10 DC1010 3022110WP WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25570FE 47829 BASIC WING STRUCTURE LEFT AND RIGHT LOWER DOUBLERS P/N ARB0983-1 AND -2 CORROSION. CORROSION REMOVAL AND DOUBLER INSTALLATION IAW FEDEX EA 8-5710- 70160. 2L73 4F A22WE 20040420001272004042000127EU 2004 4 20 ERAA094064 120030815A6320SKCP24563 DRIVE SHAFT BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL MAIN ROTOR DAMAGED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03149EH5337 S705 DRIVE SHAFT DAMAGED ; SLIPPAGE MARKS IAW MBB MM CHAPTER 11 SECTION 11-55 B DRIVESHAFT WAS INSPECTED, DISASSEMBLED, STRIPPED, REPAIRED AND RE MPI. RE COATED AND REBUILT USING NEW HARDWARE, BALANCED, INSPECTED. 1G72 3U3 U H3EU E4CE 20040422001362004042200136NM 2004 4 22 USA2004F00020 120030704A527081020401 SWITCH BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE APU DOOR OUT OF ADJUST A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19632AU 27810 ENROUTE, WITH THE LEFT GENERATOR ON MEL FOR RT GENERATOR NOT PICKING UP THE LT GENERATOR LOAD, AND APU OPERATING, THE APU PERFORMED AN AUTO SHUTDOWN. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT GCU, AND SUBSEQUENTLY (06JUL03), REPLACED THE STANDBY POWER MODULE AND RT GENERATOR BUS TIE BREAKER. A BITE WAS PERFORMED ON THE APU WITH NO FAULTS FOUND. MAINTENANCE CLEANTED AND ADJUSTED THE APU DOOR LIMIT SWITCH. 2L72 4F4 FRTA2NM A12EU 20040423000312004042300031CE 2004 4 23 CWQ2004F00003 120030812A2910662710034 LINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE LT WHEEL WELL CHAFED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05632QS2663 5605132 REPORT 110840, INSPECTED WHEEL WELL AREAS LT AND RT, FOUND THE LT WHEEL WELL LINES TO BE OK AT THIS TIME. RT WHEEL WELL BRAKE LINE ASSY , PN 6627100-34 AND THE FLAP RETRACT LINE ASSY PN 6627000-68, TO BE CHAFED BEYOND ALLOWABLE LIMITS STATED IN MM. REMOVED AND REPLACED BOTH LINES WITH NEW AND PERFORMED OPS AND LEAK CHECKS 2L72 4F4 FRTA22CE E00059EN 20040426001862004042600186NE 2004 4 26 DLM88040257 220030323A732176960612 FCU DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE MALFUNCTIONED A DALAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27997DL37816 F2470 53364 718224 NR 2 ENGINE ROLLED BACK DURING LEVEL OFF AT 8000 FT. ENGINE SHUTDOWN PER CHECKLIST. MTC IN PROGRESS. REPLACED NR 2 ENGINE FCU, PWR AND FUEL CUTOFF TELE-FLEX PUSH/PULL CABLES. 2L72 4F4 FRTA6WE E9NE 20040427000482004042700048SW 2004 4 27 SDR11280376 120031128A7603C810242 CONTROL CABLE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCB3T HCB3TN5 GL POWER LEVER CHAFED E BRYAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW17228AM33082166 TC300 P54062 BVA7662 DURINE TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE POWER LEVER CABLE HAD BROKEN INSIDE THE CABLE HOUSING IN THE ENGINE COMPARTMENT. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20040708001672004070800167CE 2004 7 8 ENHA200320805 120030904A2750262228112 BELLCRANK CESSNA208 208B 2073701CE TE FLAP DAMAGED E ENHAK NONE O OTHER ININSP/MAINT 1 AL031276P 208B0852 FLAP BELLCRANK P/N 2622281-12, S/N 898 TCSN 997. INSPECTION FOUND MISSING WELDS AT MATING PORTIONS OF THE ASSEMBLY. BELLCRANK COULD BE SUBJECT TO CATASTROPHIC FAILURE. INSPECTION PROMPTED BY AL FSDO LETTER DATED 8/15/03. SUBJECT BELLCRANK REPLACED WITH P/N 2622311-7 OF NEW DESIGN. 1H71 3T A37CE 20040713000112004071300011NM 2004 7 13 AMTA200301531 120031229A335020121 BATTERY BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11523AT 30232 EGRESS FLOOR LIGHTS BETWEEN ROW 5 TO ROW 9 INOPERATIVE. REMOVED AND REPLACED NR 731 BATTERY PACK AND POWR SUPPLY EGRESS LIGHTS, OP'S CHECK NORMAL. (M) 2L72 4F RTA2NM 20040713000652004071300065NM 2004 7 13 TSAA00453009 120031118A53306545849 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED TAPERED FILLERS AND PLATES FROM 2024-T3 CLAD. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGUR 24. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 83. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713000692004071300069NM 2004 7 13 TSAA0451005 120031120A53206546558 STRINGER SPLICE BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713000672004071300067NM 2004 7 13 TSAA0453012 120031111A53306552873 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED FILLER, DOUBLER, AND TRIPLER FROM 2024-T3 PER TABLE I. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 34. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 123. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040415000092004041500009GL 2004 4 15 ERAA093690 220030911A7530400T63G04 ACTUATOR SKRSKYS61 S61N 8142104NE GE CT58 CT58* 30011GL STATOR VANE LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03561EH 61471 STATOR VANE ACTUATOR IS LEAKING. OLD STYLE PISTON RINGS WERE BROKEN, U CUP SEAL DAMAGED. COMPLIED WITH SB-75-0025. DISASSEMBLED, CLEANED, INSPECTED, REASSEMBLED, AND TESTED UNIT. 2G72 4U4 U 1H15 1E3 20040415001132004041500113NM 2004 4 15 ASAA024014X 120030318A532065C30424 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FASTENER HOLES AT BS 947.5, LBL 20 - RBL 20 AND 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040419000192004041900019WP 2004 4 19 ASAA0380845 120031220A53305911401 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND FUSELAGE SKIN DENT AT FS 207 AND 218. INSTALLED SKIN DOUBLERS PER SRM 53-10-4. (M) 2L72 4F RTA6WE 20040415000152004041500015NE 2004 4 15 ERAA093708 120031104A62107615009043050 CAP SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE M/R BLADE CRACKED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03575EH2841 760366 LEADING EDGE ABRASION STRIP AND UPPER OUTER DOUBLER CRACKED. C-CHANNEL DEBONDED AND DAMAGED AS INDICATED. SENT TO FOR REPAIR. INSPECTED IAW SA4047-76-5 REV11; REPLACED ABRASION STRIP IAW RS-005N-III, MODIFIED EXTERNAL DOUBLERS IAW RS-017. INSTALLED STAINLESS STEEL TIP COVER IAW RS-017-II; REPLACED BOTH FORWARD INTERNAL DOUBLERS AND REBOND C CHANNEL IAW DRWG NR 76150-09043 SPEC 38023-15000; REFINISHED IAW DRWG NO 76150-09043; STATIC BALANCE IAW RS-05N-VI. 1G72 3U3 U H1NE E19EU 20040419000672004041900067EU 2004 4 19 USAABA03005 120030207A3350 LIGHT AIRBUS330 A330323 3930335EU ESCAPE SLIDE INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19674UW 0342 CLT - DURING THE ANNUAL SLIDE INFLATION CHECK, THE R-2 DOOR SLIDE DIRECTIONAL GUIDANCE LIGHTS DID NOT ILLUMINATE WHEN THE SLIDE WAS DEPLOYED. INVESTIGATION IN PROGRESS. THE SHOP CONFIRMED THAT THE SLIDE LIGHTS WORKED PROPERLY. NO OTHER DEFINITIVE REASON WAS FOUND TO DETERMINE THE CAUSE OF THE LIGHT FAILURE. IN SUBSEQUENT SLIDE DEPLOYMENTS, THIS ANOMALY HAS NOT REOCCURRED. (M) 2L72 4F RTA46NM 20040419000792004041900079WP 2004 4 19 ASAA0380812 120031126A53119912243241 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FRAME CORRODED AT FS 1309. REMOVED DAMAGED SECTION. INSTALLED ANGLE, PLATE, AND SPLICES PER SRM 53-03. (M) 2L72 4F RTA6WE 20040429000712004042900071EU 2004 4 29 BAQA089807 120031010A521011724282101 CATCHER BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE LT DOOR FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 SCRAPPED ON SITE SCRAPPED ON SITE IAW MECHANIC AND REPLACED WITH SERVICABLE PART. 1G72 3U3 U H13EU E5NE 20040504000572004050400057NM 2004 5 4 ASAA2004AAA 120030323A5100654795715 STRAP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON STRAP AT BS 794, RBL 20 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040505001182004050500118WP 2004 5 5 LDI2004F00001 220031020A72618968075 GEAR SHAFT BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP OIL PUMP SHEARED E LDIAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW05903EH 605 P42014C OIL PUMP SHAFT SHEARED THUS UNCOUPLING THE FUEL PUMP FROM THE ENGINES GEARBOX. THE CRACK THAT CAUSED THE EVENTUAL SHEARING OF THE GEARSHAFT APPARENTLY ORIGINATED AT A SLOT FOR THE LOCKING KEY THAT WAS MACHINED DURING A PAST REWORK (MODIFICATION) THAT HAD BEEN DONE TO THE PUMP. (SW05200400286) 2L72 4T4 TRTA21EU E4WE 20040504000592004050400059NM 2004 5 4 ASAA204CCC 120030322A532065479599 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON INNERCOSTAL AT BS 787-794. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040519000302004051900030NM 2004 5 19 583CC0002 120030926A3397 TERMINAL BOEING737 737291 138448WNM EMERGENCY LIGHT LOOSE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05583CC 21069 FWD EMERGENCY EXIT LIGHT IN CABIN CEILING AND IN COCKPIT CEILING INOP. FOUND LOOSE TERMINAL POINT AND REPAIRED PER SWPM 20-10-13. OPS CHECKS GOOD PER MM 33-51-02. 2L72 4F A16WE 20040520002622004052000262EU 2004 5 20 2004F00118 120030912A5321 FLOOR PANEL AIRBUS320 A320233 3930329EU AFT CARGO BAY CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND DAMAGE ON UPPER SKIN AND CORROSION ON FLOOR PANEL NR 151BF IN AFT CARGO BAY. FABRICATED AND INSTALLED NEW AFT CARGO COMPARTMENT, FLOOR PANEL NR 151BF. (M) 2L72 4F RTA28NM 20040520002222004052000222EU 2004 5 20 2004F00112 120030915A5310 STRUCTURE AIRBUS320 A320233 3930329EU CABIN FLOOR CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOOR STRUCTURE AT FRAME 69 PLUS 3 INCHES TO 69 PLUS 10 INCHES AND LBL 50 IN CABIN. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT FRAME 69 PLUS 3 INCHES TO FRAME 69 PLUS 10 INCHES, LBL 50. (M) 2L72 4F RTA28NM 20040525000402004052500040EU 2004 5 25 2004F00130 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 59 ABOVE STRINGER 40L IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT CHANNEL AT FRAME 59 ABOVE STRINGER 40L. (M) 2L72 4F RTA28NM 20040525000382004052500038EU 2004 5 25 2004F00128 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R. (M) 2L72 4F RTA28NM 20040930001012004093000101WP 2004 9 30 WX0400002 120030108A3350 BATTERY DOUG DC9 DC987 3022087WP EMERGENCY LIGHT DISCHARGED A WXOAO OTHER L NO TEST TXTAXI/GRND HDL 1 WP19948MA 49778 UPON RETURN TO LAS FROM COS, THE CREW REPORTED THAT THE EMERGENCY LIGHTING HAD DEAD BATTERIES. MAINTENANCE REMOVED THE DEAD BATTERIES AND INSTALLED RECHARGED BATTERIES. THE SYSTEM, OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20040629000562004062900056WP 2004 6 29 04FDEA01658 120030613A5753ARC0157501 HINGE BRACKET DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25384FE 46617 LEFT INBOARD FLAP OUTBOARD HINGE BRACKET P/N ARC0157-501 GOUGED UPPER HOLE. BUSHING REPAIRED IAW FEDEX EA 8-5710-70157. 2L73 4F A22WE 20040420001372004042000137NE 2004 4 20 ERAA094067 120031222A6320S613564038002 BLOWER SKRSKYS61 S61N 8142104NE GE CT58 CT58* 30011GL OIL COOLER WORN A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03563EH 61808 FAN RUBBING, WORN BEARINGS. SLIGHT FREE FLOAT OF BEARINGS OBSERVED, SIGNS OF RUBBING INDICATED IN A 1INCH PORTION OF OUTER HOUSING. PULLEY TO BE VERIFIED FOR ALIGNMENT UPON INSTALLATION ON AIRCRAFT. BEARINGS REPLACED WITH NEW. L GAP ADDRESSED WITH APPROPRIATE SHIMMING. OUTER HOUSING DRESSED OUT WHERE FAN HAS CONTACTED. 2G72 4U4 U 1H15 1E3 20040420002002004042000200EU 2004 4 20 ERAA093694 120031224A3212D24762101 FLOAT VALVE BOLKMS105 BO105A EU MLG CHAFED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 FORWARD COMPARTMENT LEAKING AROUND TOPPING OFF VALVE CHAFED AREA NEAR FORWARD COVER ATTACHMENT. REPLACED 3 EA TOP OFF VALVES PATCHED 3 PIN HOLES AND 1 CHAFED AREA. TESTED IAW 25-60-95 C/W 6 & 18 MONTH FLOAT INSPECTION. 1G72 3U H3EU 20040423000442004042300044WP 2004 4 23 AALA20030828 120030802A2914314195 PUMP DOUG DC9 DC982 3022082WP RT ENGINE FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21577AA 53154 DFW - FLT 389 - DFW-ABQ - EN ROUTE RT HYD PRESSURE LIGHT ILLUMINATED AND RIGHT HYD PRESSURE INDICATOR WENT TO ZERO. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040429000702004042900070EU 2004 4 29 BAQA089806 120031010A52101172428111 CATCHER BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE LT DOOR FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 CATCHER LT SCRAPPED ON SITE IAW MECHANIC AND REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H13EU E5NE 20040713000592004071300059NM 2004 7 13 TSAA0451014 120031212A531165C33722 FRAME BOEING737 737230 1384401NM BULKHEAD CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 DISCOVERED CRACK AT BS 727 OUTBOARD CHORD. REMOVED FASTENERS AS REQUIRED COMMON TO BS 727 OUTER CHORD FROM S-27 UP TO S-18. TRIM END OF VERTICAL STIFFENER TO PROVIDE CLEARANCE FOR CHORD SPLICE COMPONENTS. LAID OUT LOCATION FOR CUTTING CHORD. USED REMOVED SECTION OF CHORD FOR TEMPLATE. REPLACED RIGHT UPPER CHORD SECTION. APPLIED CHEMICAL FILM TREATMENT AND ONE COAT BMS 10-11, TYPE 1 PRIMER TO ALL BARE SURFACES. REPAIR COMPLETED IAW ECO 1785 R5 WITH DEVIATION O. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713000712004071300071NM 2004 7 13 TSAA0453010 120031118A53306552873 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED TAPERED FILLERS AND PLATES FROM 2024-T3 CLAD, PER TABLE 1. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 24. REPAIR COMPLETED IAW SRM 53-30-03, PATE 86A. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713001622004071300162 2004 7 13 MEX2003563 420031225A34214067241860 DISPLAY DOUG DC9 DC987 3022087WP VSI FAILED A ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW231075T 49724 FLT 563 - MEX-TAP - CAPTAIN REPORTED THE DURING FLIGHT RIGHT IVSI WAS OCCASIONALLY OUT OF SERVICE. AIRCRAFT WAS SENT TO THE HANGAR AND THE RIGHT IVSI AND BREAKER J-16 WERE REPLACED IAW MM 34-14-00 AND 20-25-00 RESPECTIVELY, ALL CORRECT. (M) 2L72 4F RTA6WE 20040713000732004071300073NM 2004 7 13 TSAA0451006 120031120A53136546567 STRINGER BOEING737 737230 1384401NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE PER TABLE 1. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. INSTALLED REPAIR PARTS AND MADE A FAYING SEAL WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 51-10-1 AND SRM 53-10-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713001242004071300124NM 2004 7 13 UIEA200300050 120030816A542069B941204 FITTING BOEING747 747271C 1384869NM NR 1 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 DURING C-CHECK, AT AMS NR 1 PYLON OUTBOARD SPRING BEAM SHEAR TRANSFER FITTINGS FOUND CRACKED DUE TO CONTACT WITH SPRING BEAM. CONTRACT RESULTED FROM MIS-LOCATION OF FITTINGS. SUBJECT FITTING WERE TRIMMED TO REMOVE CRACK & DAMAGE, NDT INSPECTED, & RESTORED PER DRAWING. FITTINGS. CRACK FOUND ON FITTING .47 INCH LONG. ACCOMPLISH A VISUAL INSP NR 4 PYLON. PROBLEM DID NOT OCCUR AT PYLON NR 4. DAMAGE FOUND ON FITTING 69B94120-3. DAMAGED AREA WAS TRIMMED. THE REPAIRS ARE STRUCTURALLY ACCEPTABLE AND SUFFICIENT CLEARANCE IS PROVIDED. CONDUCT A DETAIL VISUAL INSPECTION OF THE FITTING & INSTALLATION EVERY 6 MONTHS TO CONFORM NO FURTHER CRACKING OR DAMAGE TO THE FITTINGS. REPLACE THE FITTING WITHIN 18 MONTHS. (M)2L74 4F A20WE 20040713001462004071300146 2004 7 13 AMTA200400001 420031231A2565 SLIDE BOEING757 75723N 1384973NM PAX DOOR MALFUNCTIONED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 FOUND DOORS 4L, 2R SLIDE WILL NOT ARM. OPENED AND CLOSED DOOR, SLIDE ARMED AS REQUIRED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20040713001592004071300159NE 2004 7 13 MEX2003564 220031226A7200 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE BIRD INGESTION A ASMFC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SW23751RA 49779 AIRCRAFT RETURNED TO GATE, AIRCRAFT WAS STRUCK BY BIRDS, AND THE CAPTAIN REPORTED THAT THE RIGHT ENGINE LIGHT OF 'STRAINER FILTER CLOGGING' CAME ON. AT GATE, AIRCRAFT WAS VISUALLY INSPECTED FOR DAMAGES IN NLG, SLATS, FLAPS, ENGINES. STABILIZER AND RADOME, ALL CORRECT. BOTH NLG BEAM LIGHTS WERE REPLACED IAW MM 33-41-00, THE ENGINE CHIPS DETECTORS AND THE ENGINE PARAMETERS WERE VERIFIED IAW MM 77-00-00, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20040802000552004080200055NM 2004 8 2 ASAA0340359 120031213A52106551269501 SEAL DEPRESSOR BOEING737 7374Q8 138447QNM R1 DOOR CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01772AS 25105 GYR - DURING C-CHECK, FOUND CRACK IN UPPER SEAL DEPRESSOR OF R1 DOOR. REPAIR IAW SRM. (M) 2L72 4F RTA16WE 20040802000562004080200056NM 2004 8 2 ASAA0340360 120031213A7830 STRUCTURE BOEING737 7374Q8 138447QNM THRUST REVERSER GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01772AS 25105 GYR - DURING C-CHECK, FOUND NR 2 ENGINE THRUST REVERSER OUTBOARD HALF INNER CHORD GOUGED AT 6 AND 12 O'CLOCK POSITION. REPAIR IAW SRM. (M) 2L72 4F RTA16WE 20040607000522004060700052WP 2004 6 7 04FDEA01612 120031201A5512 SKIN PANEL DOUG DC10 DC1010 3022110WP HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25560FE 46938 HORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANELS CRACKED. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-70174 (REF FEDEX NRC N1048) PANELS REPLACED: ALC7204-1, ALC7205-1, ALC7207-1, ALC7208-1. 2L73 4F A22WE 20040607000572004060700057WP 2004 6 7 04FDEA01617 120031113A5511ALC70082 SPAR CAP DOUG DC10 DC1010 3022110WP HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568049 47803 HORIZONTAL STABILIZER - RIGHT UPPER AFT SPAR CAP CRACK. SPAR CAP SECTION REPLACEMENT IAW FEDEX EA 8-5510-72235 (REF FEDEX NRC N0828). 2L73 4F A22WE 20040614002572004061400257NM 2004 6 14 RYN2004F00024 120030903A5753 FLAP BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE LT & RT WINGS MALADJUSTMENT A RYNAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 CE077644U 20038 AFTER TAKEOFF, ACCELRATED TO 300 KNOTS. CREW EXPERIENCED MODERATE VIBRATION. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. ADJUSTED LT AND RT AFT FLAPS. REMOVED AND REPLACED AILERON HINGE SUPPORT FITTING. 2L73 4F4 F A3WE E2EA 20040614001332004061400133CE 2004 6 14 GUU2004F00013 120030928A55201016200121 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO176954915746 UE194 AT SCHEDULED ROUTINE MAINTENANCE, RT IB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT IB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040420001362004042000136GL 2004 4 20 ERAA094066 220031202A72106894171 GEARBOX BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MAKING METAL A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03423EH10786 S543 GEARBOX MAKING METAL. METAL FROM PINION GEAR AND TORQUE METER GEAR. INSTALLED NEW PINION GEAR AND TORQUE METER GEAR. 1G72 3U3 U H3EU E4CE 20040511000352004051100035WP 2004 5 11 UPS03840165 120030211A3220 LANDING GEAR DOUG DC8 DC871F 302199DWP NOSE COLLAPSED A IPXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01797UP 45897 NOSE LANDING GEAR COLLAPSED AFTER ENGINE SHUT DOWN, APPROX. 4 FT FRO M BLOCK. AIRCRAFT SOLD IN "AS IS" CONDITION 2L74 4F RT4A25 20040511000082004051100008EU 2004 5 11 ERAA094450 120031214A642010531714 ROTOR HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR DEBONDED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03293EH127 559 BEARING DEBONDING CAUSING BINDING. OB BUSHING ON INNER SLEEVE HAD SLIPPED. GRIP BUSHINGS WORN. ACTION TAKEN: C/W PRE INSPECTION AND FOUND INNER SLEEVE BUSHING NOT SEATED. DISASSEMBLED AS FAR AS NECESSARY FOR REPAIR, CLEANED AND VISUALLY INSPECTED PARTS. REASSEMBLED TAIL ROTOR WITH NEW SEALS 2 EA SERVICEABLE BLADES AND STATIC BALANCED. REPAIRED IAW REM 301AND BO105 MM CHAPTER 34 AND 107. 1G72 3U H3EU 20040422002362004042200236CE 2004 4 22 CWQ2004F00004 120030828A2810652610013 LINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE FUEL VENT MISMANUFACTURED B CWQRK NONE W INADEQUATE Q C ININSP/MAINT 1 GL05352QS 5600352 DURING ROUTINE MAINT, A FUEL LEAK WAS BEING WORKED IN RT WING AREA FORWARD OF MLG. DURING INSTALLATION OF PLUMBING WHICH WAS REMOVED FOR ACCESS A LINE WAS DAMAGED. PART WAS ORDERED AND RECEIVED BEFORE INSTALLATION LINES WERE COMPARED THE CORRECT PART NR WAS ON LINE ASSY, BUT THE LINE HAD THE CONNECTIONS SWAPPED (FLARED B-NUT AND WIGGINS CLAMP FITTING), MFG PULLED BUILD UP PRINT AND AGREED THAT THE LINE WAS BUILT INCORRECT. 2L72 4F4 FRTA22CE E25EA 20040423000452004042300045 2004 4 23 AALA20031067 420030925A2565 SLIDE DOUG DC9 DC982 3022082WP TAIL CONE DEFECTIVE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21462AA 49592 DFW - FLT 1128 - AIRCRAFT GROUND INTERRUPTED WITH SMOKE IN THE CABIN. EMERGENCY EVACUATION WAS EXECUTED BY DEPLOYING SLIDES. ALL PERSONS EVACUATED SAFELY. TAIL CONE SLIDE FAILED TO DEPLOY PROPERLY. SKYDROL NOTED DRIPPING UNDER AIRCRAFT. REPLACED TAIL SLIDE S/N A5189 OFF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040927000192004092700019NM 2004 9 27 372PA0075 120030909A5320 ANGLE BOEING737 737306 13844BGNM RAD INLET CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 DRAG ANGLE CRACKED ABOVE LEFT RAM AIR INLET. REPLACED ANGLE PER EA 53-235. 2L72 4F RTA16NE 20040927000992004092700099 2004 9 27 2004F00363 420031122A2300ACP2788AB04 CONTROL PANEL AIRBUS320 A320233 3930329EU COCKPIT INOPERATIVE A RJEFA UNSCHED LANDING O OTHER CLCLIMB 1 SO23981LR 558 FLT TA525 - SAL-DFW, DURING CLIMB, CAPTAIN AUDIO CONTROL PANEL WENT INOPERATIVE, AFFECTING AUDIO PLUS SELECTION OF THE SYSTEM. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, PERSONNEL REPLACED AND TESTED OF THE ACP PANEL NR 1 PER AMM 23-51-12. RESULTS WERE SATISFACTORY AND AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040930001102004093000110WP 2004 9 30 WX0400003 120030118A7900 FILTER DOUG DC9 DC983 3022083WP LT ENGINE OIL CLOGGED A WXOAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP19862GA 49556 ON DEPARTURE FROM STL, AT APPROXIMATELY 80 KNOTS DURING TAKEOFF, THE LEFT ENGINE OIL STRAINER CLOGGING ANNUNCIATOR ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED BACK TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE MAIN OIL STRAINER. THE SYSTEM LEAK CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20040930001272004093000127EU 2004 9 30 A6WA200360067 120031209A5753 STRUCTURE BAG BAE146BAE146200A 1500266EU TE FLAP DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. BUSHING LOCALLY MANUFACTURED AT AAO AND CAD PLATED IAW BAE FAX BARA/AVR/6605/03-DC. BUSHING INSTALLED IAW FLAP EO EO2/021/657. (M) 2H74 4F RTA49EU 20040628002022004062800202WP 2004 6 28 04FDEA01636 120031027A5510ALC72071 SKIN PANEL DOUG MD10 MD1010F 3022112WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25394FE 46628 HORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANEL CRACKED. PANELS REPLACEMENT PER SB 55-16. 2L73 4F RTA22WE 20040629000542004062900054WP 2004 6 29 04FDEA01656 120031008A5512 SKIN PANEL DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25370FE 46608 HORIZONTAL STABILIZER CONSTANT SECTION AND OUTBOARD SKIN PANELS CRACKED. P/N ALC7442-1, ALC7206-1, ALC7208-1. PANELS REPLACEMENT/REPAIR PER SB 55-16 IAW FEDEX EA 8-5510-72225. 2L73 4F A22WE 20040713000722004071300072NM 2004 7 13 TSAA0453011 120031111A53306545849 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED DOUBLER AND FILLER FROM .063 INCH, 2024-T3. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 33. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 119. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713000762004071300076NM 2004 7 13 TSAA0457016 120031220A57116545321 SPAR BOEING737 737230 1384401NM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 DISCOVERED CORROSION AT WBL 349 AND 503 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED ARE PER SRM 57-30-1, FIGURE 1A AND 1B INSTRUCTIONS. FABRICATED AN .020 INCH THICK EXTERNAL REPAIR DOUBLER FROM 7075-T6 SHEET. CLEAN AND TREATED ALL EXPOSED SURFACES. BONDED THE EXTERNAL DOUBLER OVER THE BLEND AREA, WITH BMS 5-95 SEALANT. INSTALLED AND SECURED THE EXTERNAL DOUBLER IN PLACE USING THE EXISTING FASTENERS WITH THE BLEND OUT AREA. INSPECTED REWORKED AREA ENSURING CORROSION AND CRACK FREE. APPLIED TOP COAT FINISHES TO REPAIR AREA. FILLET/TAPERED SEAL AROUND EDGES. REPAIR COMPLETED IAW ECO 3403. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713000962004071300096NM 2004 7 13 USAASB03224 120031231A335020121 POWER SUPPLY BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 PIT - MAINTENANCE REPORTED THE INTERIOR EMERGENCY LIGHTS INOPERATIVE. S/D - MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040713001572004071300157SO 2004 7 13 2004F00160 120031220A53474046711144 SEAT TRACK GULSTMGV GULFSTREAMGV3980116SO FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23661GA 561 FOUND THE LEFT CABIN SEAT TRACK HAD SUSTAINED CORROSION DUE TO WATER INTRUSION FROM THE LEFT NR 6 EMERGENCY CABIN WINDOW. REMOVED CORROSION AND BLENDED THE EFFECTIVE AREA OF THE SEAT TRACK. TREATED BARE METAL AND APPLIED PRIMER PER GULFSTREAM ENGINEERING DISPOSITION RFA NR 16478 DATED DECEMEBER 22, 2003. THIS IS A TEMP REPAIR AND IS GOOD FOR A PERIOD NOT TO EXCEED 30 DAYS AT WHICH TIME A PERMENATE REPAIR MUST BE INCORPORATED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA12EA 20040713001632004071300163NE 2004 7 13 MEX2003558 220031221A7230 BLADE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED A ASMFA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW23214AM 49585 AIRCRAFT AIR TURN BACK, DURING CLIMB THE RIGHT ENGINE STALLED. AT PLATFORM, IT WAS DETECTED DAMAGES IN FOUR C1 BLADES AND IN 2 C2 BLADES. INSPECTOR AND TECHNICAL PERSONNEL WERE SENT TO EVALUATE THE DAMAGES AND START THE CORRECTIVE ACTIONS. ENGINE WAS REPLACED. (M) 2L72 4F4 FRTA6WE E9NE 20040713000662004071300066NM 2004 7 13 TSAA0457017 120031203A57306546419 SKIN BOEING737 737230 1384401NM LEADING EDGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 REMOVED CORROSION FROM RIGHT FIXED LEADING EDGE AT WBL 375. TRIMMED OUT DAMAGED AREA. FABRICATED A FILLER AND DOUBLER PER TABLE 1. ALODIZED ALL TRIMMED EDGES AND BARE SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 57-40-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713001142004071300114NM 2004 7 13 TSAA0451004 120031118A53206546541 STRINGER SPLICE BOEING737 737230 1384401NM FUSELAGE DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USNG HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040722000082004072200008EU 2004 7 22 USAA040282 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK DAMAGED .175 SQUARE INCH AT RBL 17.75 FS 67. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040802000982004080200098NE 2004 8 2 C7WA200300050 220031224A726142D107A2 BYPASS SWITCH BOEING737 737231 1384079NM PWA JT8 JT8D NE NR 2 ENGINE INOPERATIVE A C7WAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO1724343 21630 NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT CRUISE. A PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED. INSPECTED NR 2 ENGINE INLET AND EXHAUST NO DEFECTS NOTED. CHECKED MAIN OIL SCREEN FOR DEBRIS, NONE FOUND. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH AND FILTER BYPASS SWITCH. ENGINE RUN AND OPS CHECK GOOD. (M) 2L72 4F4 FRTA16WE E2EA 20040802001562004080200156SW 2004 8 2 2004F00205 120031120A5230 DOOR SWRNGNSA227 SA227AC 8780603SW CARGO BAY STIFF A BSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0560NE AC760B FLT 2587 - HLN - THE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB AT 10,000 FT, CREW RETURNED TO STATION. SUSPECT DOOR CLOSING PROCEDURES WITH FULL BAGGAGE AREA CAUSING A DOOR HARD TO CLOSE, DOOR CLICKCLACK RIGGING/LUBRICATION, OR SWITH RIGGING. MAINTENANCE PERFORMED VISUAL INSPECTION, FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO THE MX BASE ON A SPECIAL FLIGHT PERMIT. THE LOWER AFT CLICKCLACK WAS ADJUSTED, AN THE SYSTEM OPS CHECKED GOOD. AFTER TAXI AND GROUND OPS CHECK, THE CARGO DOOR WARNING LIGHT CAME BACK ON. IT WAS DETERMINED THAT THE DOOR HANDLE MICROSWITCH ALSO NEEDED TO BE ADJUSTED. SYSTEM OPS CHECKED GOOD ON THE GROUND OPS CHECK. OPS CHECK FLIGHT WAS COMPLETED, SYSTEM OPS CHECKED GOOD. (M) 2L72 4T RTA8SW 20040809000382004080900038NM 2004 8 9 USAA030270 120031114A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU59971 22204 CLT - FOUND SKIN CRACKED 2 INCHES LONG, UPPER FORWARD CORNER OF L1 DOOR CUTOUT. REMOVED CRACK AREA AND INSTALLED TRIPLE DOUBLER AND SHIM PER EA 94810. (M) 2L72 4F RTA2NM 20030925000682003092500068CE 2003 9 25 2003F00578 120030602A2130 REGULATOR LEAR 35 31A 5170531CE CABIN PRESSURE DAMAGED A GTIAO OTHER O OTHER CLCLIMB 1 GL23712EJ 231 INADVERTENT ACTIVATION OF EMERGENCY AIR FLOW AT 9000 FT. TROUBLESHOOTING, INSPECTION OF PRESSURIZATION SYSTEM COMPONENTS, GROUND AND SUBSEQUENT FLIGHT PRESSURIZATION CHECKS PROVED NO NOTED DEFECTS. DURING OPERATIONAL CHECK/TESTS, FOUND PRESSURE REGULATORS FOR PRESSURIZATION AND TEMPERATURE CONTRL TO BE MARGINAL IN OPERATIONAL PRESSURE. REMOVED AND REPLACED BOTH LEFT AND RIGHT SERVO AIR PRESSURE REGULATORS IAW LEAR 31 MM 21-30-08, PAGE 201. FUNCTIONALLY CHECKED BOTH REGULATORS INDIVIDUALLY TO ENSURE THEY REGULATE AT 15 SPI. SATISFACTORILY COMPLETED AN OPERATIONAL CHECK OF PRESSURIZATION SYSTEM IAW LEAR 31 MM 21-30-00 PAGE 209. (M) 2L72 4F RTA10CE 20030925000712003092500071WP 2003 9 25 AALA20030895 120030824A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21467AA 49597 DURING OVERNIGHT MAINTENANCE, EXTERIOR EMREGENCY LIGHTS, LEFT AND RIGHT, INOPERATIVE. REPLACED BATTERY IN AFT CARGO COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERAITON. (M) 2L72 4F A6WE 20030925000782003092500078WP 2003 9 25 AALA20030437 120030214A5315 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW219615W 53562 FOUND FLOORBEAM FROM LBL 43 TO LBL 24, FLOOR SUPPORT CORRED FS 1155. FABRICATED NEW SUPPORT WITH EXTRUSION CRN4018034. TREATED PART AND INSTALLED PER SRM 51-10-35, 51-80-1. (M) 2L72 4F RTA6WE 20030925000862003092500086NE 2003 9 25 A6WA200340128 220030829A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 FAILED A O OTHER MXJOVER TEMP ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 GL31440AW 7766 UPON TAKEOFF NOTED NR 1 ENGINE ITT AT 900. DURING CLIMB NOTED ITT AT 858-874. AT FL280 HEARD THUMP AND NR 1 ENGINE SPOOLED DOWN. SECURED PER QRH AND COMPLIED WITH SINGLE ENGINE OPERATIONS. REMOVED AND REPLACED NR 1 ENGINE. SHOP REPORT REMARKS, REPLACED NR 3 BEARING AND FAN DRIVE SHAFT. TESTED ENGINE PER SEI - 756. (M) 2L72 4F4 FRTA21EA E15NE 20040802001152004080200115EU 2004 8 2 2004F00227 120030913A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE BENT A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND FLOOR PANEL SUPPORT FOR FLOOR PANEL 232WF IS BENT. FORMED FLOOR PANEL SUPPORT AT FLOOR PANEL NR 232WF BACK TO ORIGINAL CONTOUR. (M) 2L72 4F RTA28NM 20040803000052004080300005EU 2004 8 3 USAA040284A 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED APPROXIMATELY .2 SQUARE INCHES, FS 65 PLUS 10 INCHES RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040802000962004080200096NM 2004 8 2 C7WA200300051 120031219A1420 CONNECTOR BOEING727 7272M7 138407SNM OVERHEAT SYS LOOSE A C7WAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO17742RW 21952 FLIGHT RETURN, AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT. CLEANED AND RESEATED CONNECTOR AT LOWER AFT BODY OVERHEAT SENSING ELEMENT, OPS CHECK NORMAL IAW MM 20-60-01 AND 26-14-0. (M) 2L73 4F A3WE 20040809000592004080900059NE 2004 8 9 2004F00171 220031118A7230311856301 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GUUAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO1987552 UE216 114455 DURING TAKEOFF, LOUD BANG OCCURRED ON LEFT ENGINE. ABORTED TAKEOFF. DEMATED POEWR SECIOTN FROM GAS GENERTOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF. REPLACED LEFT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. CONFIRMED 2ND STAGE PT BLADE FAILURE. SUBSTANTIAL DAMAGE OCCURRED. FULL OVERHAUL OF POWRE SECTION REQUIRED. (M) 2L72 4T4 TRTA24CE E26NE 20040813000942004081300094 2004 8 13 2004UALA00725 420031025A2565 O-RING AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE SLIDE BOTTLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29835UA 1426 LOW BOTTLE PRESSURE. BOTTLE TO VALVE O-RING DETERIORATED. REPLACED CYLINDER ASSY. 2L72 4F4 FRTA28NM E40NE 20030925000322003092500032NM 2003 9 25 USAA030154 120030819A5330654576599 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US 23315 PIT - FOUND SKIN PANEL CRACKED 10 INCHES AND SEVERAL .25 INCH THROUGH .5 INCH LONG CRACKS AND DISBONDED, LAPJOIJNT S-10L BS 360-540 ALONG 15 FT SECTION OF FUSELAGE SKIN. INSTALLED THREE NEW SKIN PANELS .080 INCH PER EA 76610A. (M) 2L72 4F RTA16WE 20030925000362003092500036NM 2003 9 25 USAA030169 120030727A3230657376121 SUPPORT BOEING737 737301 1384611NM NLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US 23557 FOUND UPPER SUPPORT CORRODED .004 INCH TOP AND BOTTOM TOTAL OF .008 INCH, NLG UPPER SUPPORT. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20030925000592003092500059NM 2003 9 25 USAA030162 120030820A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US 23559 FOUND SKIN CRACKED 1 INCH, AFT OF 727A .5 INCH BELOW S23R. INSTALLED DOUBLER AND TRIPLER PER EA 94615. (M) 2L72 4F RTA16WE 20030925000672003092500067SO 2003 9 25 2003F00577 120030629A34110856TK3 PITOT HEAD GULSTMGV GULFSTREAMGV3980116SO PITOT/STATIC SYSDAMAGED A UG8AO OTHER P NO WARNING INDICATION CRCRUISE 1 GL23920DC 534 DURING THE SCHEDULED FLIGHT BETWEEN STUTTGART AND BASEL, THE FLT CREW NOTED THE ALTIMETERS HAVE AN OUT OF TOLERANCE 'SPLIT' BETWEEN THE NR 1 AND NR 2 SYSTEMS. THE NR 1 PITOT/STATIC PROBES WERE DAMAGED, CAUSING INACCURATE READINGS IN THE NR 1 SYSTEM. THE UPPER LT AND LOWER RT PITOT/STATIC PROBES WERE CHANGED PER CHAPTER 34 OF THE GV MM. THE SYSTEM WAS CHECKED FOR ACCURACY PER THE GV MM AND FOUND TO BE WITHIN TOLERANCE. ALL RVSM MAINTENANCE WAS PERFORMED PER THE AAR RVSM MX PROGRAM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA12EA 20030925000772003092500077NE 2003 9 25 GTIA030623 220030809A7230 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 726971 ON PREFLIGHT INSPECTION, FOUND FOD DAMAGE TO THE NR 2 ENGINE C-1 BLADES. REMOVED AND REPLACED NR 2 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20030925000802003092500080NM 2003 9 25 AALA20030890 120030822A2597 CONNECTOR BOEING757 757223 1384957NM ESCAPE SLIDE INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21199AN 32393 LT EMERGENCY SLIDE LEFT AFT OF WING AT STATION 1388 INOPERATIVE. FOUND PIN CONNECTOR D5526 PUSHED BACK. REPOSITIONED PIN BACK INTO CONNECTOR AND LOCKED EMERGENCY SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000822003092500082WP 2003 9 25 GTIA030626 120030731A5280 SKIN DOUG DC9 DC983 3022083WP MLG DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 THERE IS A 1.5 INCH CRACK ON SKIN ON LEFT ON NOSE GEAR DOOR HINGE. MANUFACTURED AND INSTALLED SKIN AND REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20030925000852003092500085WP 2003 9 25 GTIA030555 120030617A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FOUND MID PIT STATION 636-655 STRINGER 30-29L CORROSION AT FASTENERS. REMOVED LONGERON 30 FROM STATION 588 TO 665. FABRICATED NEW LONGERON SECTION. INSTALLED NEW LONGERON. (M) 2L72 4F A6WE 20030925001072003092500107NM 2003 9 25 P5CA0300931 120030827A2821408851 VALVE BOEING747 7472D3B 1384805NM NR 4 FUEL TANK MALFUNCTIONED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23505MC 21251 NR 4 MAIN FUEL TANK - REFILL VALVE WILL NOT SHUT OFF. REMOVED AND REPLACED NR 4 MAIN FUEL TANK REFILL VALVE IAW AMM 28-21-13. 2L74 4F RTA20WE 20030926000012003092600001NM 2003 9 26 PCAA0309109 120030912A326083220079107 COVER DHAV DHC8 DHC8102 2809003NM NLG PROX SWITCH CRACKED A PCAAO OTHER J WARNING INDICATION LDLANDING 1 EA13811AW 201 CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT EXTEND & THE RED UNSAFE LIGHT HAD ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE ALTERNATE EXTENSION DID WORK. THE CHECKLIST WAS COMPLETED WITH GEAR LOCKED AND PINNED. MAINTENANCE INSTALLED A NEW UPPER PROXIMITY SWITCH COVER. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030925000902003092500090NM 2003 9 25 03FDEA01412 120030901A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING I/B FLAP O/B HINGE (AIRCRAFT SIDE) I/B FACE OF I/B PIVOT BEARING BORE FOUND CORRODED. LT WING I/B FLAP O/B HINGE (A/C SIDE) I/B FACE OF I/B PIVOT BEARING BORE (LUG SURFACE) CORROSION REMOVED AND REPLACED AS PER EA 1-5750-72644. 2L73 4F RTA22WE 20030925000952003092500095 2003 9 25 DXTA200300115 420030910A2210 AUTOPILOT SYS CESSNA500 560CESSNA 2076750CE COCKPIT MALFUNCTIONED E DXTAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL07312QS 5600312 AIRCRAFT EXPERIENCED UNCOMMANDED RIGHT RUDDER INPUT DURING CRUISE WITH AUTOPILOT ON, ALSO DEVELOPED NOTICEABLE PITCH ROLL WITH AUTO PILOT ON. PERFORMED NJA OPERATIONAL CHECK FLIGHT AND COULD NOT DUPLICATE DISCREPANCY, NO FURTHER ACTION REQUIRED. 2L72 4F RTA22CE 20030926000112003092600011EU 2003 9 26 UPS03141147 120030825A3510 OXYGEN MASK AIRBUSA300 A300F4622R 3930360EU COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01127UP 0812 CAPTAINS OXYGEN MASK INOPERATIVE. REMOVED AND REPLACED CAPTAINS OXYGEN MASK STOWAGE BOX IAW MM 35-12-51-4. 2L72 4F RTA35EU 20030926000212003092600021GL 2003 9 26 00067669 320030827A6114D65312 HUB ARACFTSPORT ARROWSPORT1 0840102CE CONT O360 TSIO360* 17025SO HARTZLHCC2Y HCC2YF1 GL PROPELLER CORRODED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 LB17B CORRISION ON PROPELLER HUB. 1Q71 3R3 O ATC115 E9CE 5 CP920 20030926000312003092600031CE 2003 9 26 DXTA200300105 120030827A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG INTERMITTENT E DXTAO OTHER O OTHER LDLANDING 1 GL07398QS 5600522 BRAKE PEDALS FEEL SOFT DURING USE, BRAKES GRAB AND RELEASE INTERMITTENTLY DURING LANDING DECELERATION. JACKED A/C INSPECTED BRAKES AND ENGAGEMENT OF ANTI-SKID, NO DEFECTS NOTED, BLEED BRAKES ALL WORK PERFORMED IAW CE-560 MM CHAPTER 32-40. 2L72 4F RTA22CE 20030926000382003092600038EU 2003 9 26 0301623248 120030805A5347 SEAT TRACK AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01348NW 410 DURING L CHECK FOUND CORROSION ON SEAT TRACKS Y-765 AND Y-1292 BETWEEN FRAMES 16-24. REPAIRED IAW EA 32-195649. 2L72 4F RTA28NM 20030926000442003092600044NE 2003 9 26 AMTA200301051 220030813A7323FFG022AC GOVERNOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE ENGINE INOPERATIVE A AMTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL11523AT184777596 30232 31671 LT ENGINE WOULD NOT REACH TO EPR WITH EEC AND ENG LIMITER ON. ENG PARAMETERS NORM FOR LOW EPR TO WITH EE C AND ENG LIMITER OFF NOT CHECKED. REMOVED AND REPLACED NR 1 ENG FFG IAW MM. REF DIS 7100-482 AND -483 FOR LEAK CHECK AND POWER PLANT ADJUSTMENT TEST. 2L72 4F4 FRTA2NM E12EU 20030926000502003092600050NM 2003 9 26 MWEA030333 120030827A5330593602229 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FUSELAGE SKIN AT STATION 1107 BETWEEN LONGERON 28 AND 29 LEFT REQUIRE'S REPAIR TO THE OPEN HOLE DUE TO REMOVAL OF THE AIRPHONES ANTENNA. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. 2L72 4F RTA6WE 20030926000582003092600058EA 2003 9 26 COMA0360386 120030824A2420 ADG CNDAIRCL600 CL6002B19 1900309EA ELECTRICAL MALFUNCTIONED A COMAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO01477CA 7670 ADG AUTO DEPLOYED DURING FLIGHT. RESTOWED ADG - NO DEFECTS FOUND. 2L72 4F RTA21EA 20030924000312003092400031NM 2003 9 24 DL777030744 120030810A21214100945A FAN BOEING777 777232 1385232NM RECIRCULATION FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27860DA 29951 RECIRC FAN STATUS MESSAGE IN FLIGHT WITH ELEC ODOR IN FWD BUSINESS SECTION AND SLIGHT VISUAL. NO ODOR IN COCKPIT. DISSIPATED IN 1-2 MINUTES. REPLACE RECIRC FAN. SYSTEM OPS CK NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2L72 4F RTT00001SE 20030924000332003092400033NE 2003 9 24 DL76L030746 220030812A7261 CARBON SEAL BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE LEAKING A DALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 SO27199DN50344 28456 724148 ON TAKEOFF ACRID ODOR IN CABIN. SMOKE DETECTORS WENT OFF. FOUND OIL IN INLET OF NR 2 ENGINE. CARBON SEAL REPLACEMENT IN PROGRESS. 2L72 4F4 FRTA1NM E24NE 20030925000102003092500010EU 2003 9 25 AALA20030845 120030810A3260E0065Z01W01B RELAY AIRBUS300 A300B4605R 3930308EU NLG FAILED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2170074 517 DURING DEPARTURE UNABLE TO RETRACT LANDING GEAR. AIRCRAFT RETURNED JFK AND LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR TARGETS AND REPLACED RELAYS AT 141GB AND 96GB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030925000562003092500056NM 2003 9 25 USAA030159 120030731A5320 ATTACH ANGLE BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US40913 23987 FOUND ATTACH ANGLE CRACKED .5 INCH, BS 328 LBBL 45 CABIN FLOOR. MANUFACTURED NEW ANGLE AND INSTALLED PER DWG NR BAC-65-45812 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20030925000572003092500057NM 2003 9 25 USAA030160 120030818A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU49839 23856 FOUND SKIN CRACKED 2 INCHES, STATION 727E AT S24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20030925000642003092500064SO 2003 9 25 2003F00576 120030509A32401159SCL5043 KEY GULSTMGV GULFSTREAMGV3980116SO BRAKE ROTOR SHEARED A UG8AK NONE O OTHER ININSP/MAINT 1 GL235101 550 WHILE TOWING THE AIRCRAFT INTO THE HANGAR TO DTW IT WAS DISCOVERED THAT SEVERAL BRAKE ROTOR DRIVE KEYS ON BOTH LT OUTBOARD AND LT INBOARD BRAKES WERE SHEARED OFF. FURTHERMORE, UPON EXAMINATION BOTH OF THE RT BRAKES HAD SEVERAL CRACKED DRIVE KEYS. THIS IS A KNOWN PROBLEM WITH THE GV BRAKES AND IS UNDER INVESTIGATION BY BOTH GULFSTREAM AND THE BRAKE MANUFACTURE. REPLACED ALL FOUR AIRCRAFT BRAKES AND BOTH LEFT INBOARD AND OUTBOARD WHEEL ASSEMBLIES. BLED BRAKES AND PERFORMED OPERATIONAL CHRCKS IAW AIRCRAFT MM. ALL CHECKS WERE GOOD AND THE AIRCRAFT WS RETURNED TO SERVICE. (M) 2L72 4F RTA12EA 20040630000242004063000024CE 2004 6 30 W322004F00000 120031222A270105131683 YOKE CESSNA210 2105 2073404CE CONT O470 IO470* 17026SO PILOT SIDE CRACKED E W32AL ABORTED APPROACH F FLT CONT AFFECTED LDLANDING 1 WP078298Z 2050298 PILOT REPORTED THAT DURING LANDING FLARE, THE YOKE SNAPPED RESULTING IN A GO AROUND. AFTER INITIAL INSPECTION, YOKE WAS FOUND CRACKED COMPLETELY THROUGH ON UPPER LEFT HAND CORNER. YOKE MATERIAL APPEARS TO MANUFACTURED FROM PLASTIC, SUGGEST REMOVAL OF ALL PLASTIC YOKES FROM SERVICE AND REPLACE WITH THOSE MADE FROM ALUMINUM. 1H71 3O3 O 3A21 E1CE 20040630001832004063000183 2004 6 30 GLBA2003122 420030822A34526229352003 CONTROLLER BEECH 1900 1900D 1154162CE TRANSPONDER FAILED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 NM03208GL UE208 TRANSPONDER CONTROL WENT BLANK. REMOVED TRANSPONDER CONTROL P/N 622-9352-003, RE-SEATED IT, OPS CHECK GOOD. 2L72 4T RTA24CE 20040728001322004072800132CE 2004 7 28 2004F00207 120031006A56101143840206 WINDSHIELD BEECH 1900 1900C 1154161CE COCKPIT CRACKED A FFSAO OTHER O OTHER APAPPROACH 1 AL01575A 8778 UC83 CO-PILOT OUTER WINDSHIELD PANE CRACKED. CRACKS OCCURRED DURING THE APPROACH PHASE OF THE FLIGHT AT ABOUT 3,000 FEET MSL WITH MINIMAL CAIBN DIFFERENTIAL PRESSURE. WINDSHIELD HEAT WAS ON AND WORKING AT THE TIME. OUTSIDE AIR TEMPERATURE WAS WITHIN A COUPLE OF DEGREES OF FREEZING. (M) 2L72 4T RTA24CE 20040802000872004080200087EU 2004 8 2 2004F00210 120031221A5101 STRUCTURE AIRBUS320 A320233 3930329EU AIRFRAME VIBRATION A SOKFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO23981LR 558 DURING CLIMB, IT WAS EXPERIENCED A STRONG VIBRATION IN ALL PHASES OF FLIGHT ABOVE 300 KNOTS. THE AIRCRAFT WAS DEVIATED FROM ITS NORMAL FLIGHT SCHEDULE TO SAL STATION FOR MAINTENANCE. THE AIRCRAFT REMAINS ON GROUND AT SAL STATION FOR MAINTENANCE. (M) 2L72 4F RTA28NM 20040802001282004080200128NE 2004 8 2 2004F00217 220031118A7250311856301 TURBINE BLADES BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GUUAC ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 SO198153615235 UE152 114332 FLT 9236 - EYQ/TPA - AFTER CLEARANCE FOR TAKEOFF, LEFT ENGINE FAILED. ENGIEN IMMEDIATELY SECURED. ABORTED TAKEOFF. AIRCRAFT RETURNED TO THE GATE. DEMATED POEWR SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. CONFIRMED 2ND STAGE POWER TURBINE BLADE FAILURE. SUBSTANTIAL DAMAGE OCCURRED. ONLY 'STUBS' REMAIN. FULL OVERHAUL OF POWER SECTION REQUIRED. (M) 2L72 4T4 TRTA24CE E26NE 20040802001182004080200118NM 2004 8 2 2004F00229 120031231A1420BACC45FT14A7S CONNECTOR BOEING727 727233 138408ANM LE FLAP INOPERATIVE A PCSAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO17994AJ 20942 FLT 835 - KMIA-MTPP - CREW REPORTED, AFTER TAKEOFF ALL LEADING EDGES DEVICES REMAINED EXTENDED, FORWARD AND AFT GREEN LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED KMIA WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED L/E FLAP BYPASS VALVE CONNECTOR IAW STANDARD PRACTICES MANUAL 20-11-02, OPERATIONS CHECK GOOD IAW MM 57-81-0. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040802001162004080200116EU 2004 8 2 2004F00228 120030926A5320 INTERCOSTAL AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND INTERCOSTAL LOCATED BETWEEN FRAME 50 AND 51 RBL 27 AT AFT CARGO COMPARTMENT IS CORRODED AT FORWARD END. (M) 2L72 4F RTA28NM 20040809000392004080900039NM 2004 8 9 USAA030271 120031114A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU59971 22204 CLT - FOUND SKIN CRACKED 1 INCH, BS 1315 BETWEEN S 27 R AND S 28 R. WEB ASSEMBLY COMPLETED AND TRANS ANGLE INSTALLED PER SRM 51-10-00, 51-40-03, 51-70-11 AND EA 94804. (M) 2L72 4F RTA2NM 20040712001032004071200103SO 2004 7 12 C2XA03IA106 120031124A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727523 145389 FLIGHT 2833 - DURING PREFLIGHT INSPECTION THE FLIGHT CREW REPORTED THAT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040713000682004071300068NM 2004 7 13 TSAA0453008 120031116A53306546547 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED REPAIR DOUBLER. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 PER FIGURE 1. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 2B. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713000702004071300070NM 2004 7 13 TSAA0453003 120031217A53306552874 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 TRIMMED OUT THE SKIN CRACK. VERIFIED HFEC CUTOUT AND ROTARY PROBE INSPECTION OF LAP SPLICE FASTENER HOLES. FABRICATED AND INSTALLED STRUCTURAL FILLERS, A DOUBLER, AND TEARSTRAP PER FIGURE 48. ALODINED AND PRIMED ALL REPAIR PARTS AND BARE SURFACES. APPLIED CORROSION INHIBITING COMPOUND. ASSEMBLED REPAIR PARTS WITH BMS 5-59 SEALANT ON ALL MATING SURFACES PRIOR TO FASTENER INSTALLATION. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, DETAIL XII. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040712000062004071200006SO 2004 7 12 C2XA03CL193 120031129A3260 WARNING LIGHT EMB 145 EMB145LR 3260212SO MLG ILLUMINATED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2715983 145239 BNA FLIGHT 2831, THE CREW REPORTED THE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. ALSO RECEIVED A LANDING GEAR/LEVER DISAGREE WARNING ON THE EICAS. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040713000752004071300075NM 2004 7 13 TSAA0453002 120031224A53306546549 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13807AL 23443 FOUND AN INCH AND A HALF AND A TWO INCH FUSELAGE CRACK AT BS 767 AND BS 792, ON STRINGER 18L. TRIMMED OUT CRACKS AND VERIFIED CUTOUTS USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED STRUCTURAL AND TAPERED FILLERS, DOUBLER, AND TRIPLER FROM CLAD 2024 T3. CLEANED AND TREATED ALL EXPOSED SURFACES. REPAIR COMPLETED IAW SRM 53-30-3 FIGUR 48. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040713000892004071300089NM 2004 7 13 S2YA03037 120031218A2422PC2512A INVERTER DORNERDO32 DO328300 NM NR 2 FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13351SK 3108 MKE-BNA - FLT 2056 - DURING FLIGHT, THE CAPTAIN NOTED THE NR 2 INVERTER FAIL MESSAGE FOLLOWED BY SEVERAL AC BUSS FAILURES. THE PILOT CONSULTED MAINTENANCE. MAINTENANCE INSTRUCTED THE PILOT TO SHUT THE NR 2 INVERTER OFF AND CONTINUE WITH THE FLIGHT. THE PILOT MADE AN AIR-TURN-BACK TO MKE. UPON ARRIVAL IN MKE MAINTENANCE MEL'D THE NR 2 INVERTER ALLOWING THE A/C TO PROCEED WITH THE FIGHT. MAINTENANCE SWAPPED THEINVERTERS FOR TROUBLE SHOOTING BUT COULD NOT DUPLICATE THE DISCREPANCY. THE NR 1 INVERTER FAILED AND WAS MEL'D UNTIL LATER 12/22/2003 WHEN IT WAS REPLACED. MAINTENANCE RETURNED THE A/C TO SERVICE WITH NO FURTHER DEFECTS. (M) 2H72 4T RTA55NM 20040713000972004071300097NE 2004 7 13 S2YA03035 220031202A7230 COMPRESSOR DORNERDO32 DO328300 NM PWA 306 PW306B NE RT ENGINE STALLED A S2YAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL13359SK 3202 PCECD0159 WHILE TAXIING OUT FOR FLIGHT 2419, ATW-MKE, THE CREW NOTED A LOUD NOISE SOUNDING LIKES BRAKES. DETERMINED THT THE RIGHT ENGINES COMPRESSOR WAS STALLING WHEN THE POWER WAS ADVANCED. MAINTENANCE TROUBLESHOT THE SYSTEM AND REPLACE MOST OF THE BLEED SYSTEM COMPONENTS BUT THE COMPRESS STILL STALLED WHEN ADVANCING POWER. MAINTENANCE BORESCOPED THE ENGINE AND DEEMED IT SAFE FOR A FERRY FLIGHT BACK TO MKE. THE ENGINE WAS CHANGED TO CORRECT THE PROBLEM. (M) 2H72 4T4 FRTA55NM E35NE 20030926000122003092600012NM 2003 9 26 UPS03241144 120030826A3350 BATTERY BOEING727 727173C 1384059NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 EMERGENCY EXIT LIGHT OVERHEAD FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BATTERIES FORWARD ENTRY EMERGENCY EXIT LIGHT ASSY. CHECKS NORMAL. 2L73 4F A3WE 20030926000652003092600065NM 2003 9 26 AWXA200300996 120030817A53126516300190 BULKHEAD BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF WEB AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-11 PG 1, FIG 11. 2L72 4F RTA16WE 20030926000672003092600067NM 2003 9 26 AWXA200300998 120030815A53116546596122 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 MCN - MAJOR REPAIR - DURING C-16 CHECK A .625 INCH CRACK WAS FOUND IN RADIUS OF BS 727B FRAME AT STR 25 LT. MAINTENANCE CUTOUT DAMAGE ON BS 727B FRAME AT STR 25 LT; FABRICATED A RADIUS FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-11 PG 1, FIG 11. 2L72 4F RTA16WE 20030926000722003092600072NM 2003 9 26 PCAA0308102 120030827A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHTSBROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13847EX 333 DURING ROUTINE MAINTENANCE, VISIT ROW 8 WAS FOUND TO HAVE 2 EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. A BROKEN WIRE WAS FOUND AND REPAIRED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030926000752003092600075NM 2003 9 26 03FDEA01389 120030826A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 FWD CARGO BAY, DENTS IN FRAME, BS 520, AT STR 23L TO STR 25L. REMOVED FRAME SECTION, BS 520, STR 21-25, INSTALLED NEW FRAME SECTION BETWEEN SPLICES. ALL WORK DONE PER SRM 51-30-2, SRM 51-30-5, SRM 51-10-2 & MM 51-20-151-7 PG 1. 2L73 4F RTA3WE 20030926000782003092600078NM 2003 9 26 UPS03441106 120030720A5740 SUPPORT BOEING747 747123 1384873NM ACTUATOR MOUNT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, LT WING NR 9 VC FLAP I/B ARM O/B ROTARY ACTUATOR SUPPORT RIB ACTUATOR MOUNTING SCREW HOLE NR 1 AND NR 4 FOUND SCRATCH MARK (LOOKING O/B AND COUNT FROM TOP CW). SCREW HOLE NR 4 CORROSION REMOVED IAW SRM 57-20-03, SCREW HOLE NR 1 REPAIRED IAW RS R57-41-35047 AND EO B747-5740-19059-A. REPEAT INSP REQ AT EVERY C-CHECK INTERVAL, NOT TO EXCEED 18 MONTHS IAW EO B747-5740-19059-A. 2L74 4F A20WE 20030926000862003092600086EA 2003 9 26 COMA0360393 120030823A531160036030 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01719CA11799 7253 CRACK NOTED AT FLANGE RADIUS OF LT FRAME AT FS 718. REPARIED IAW SB 601R-53-055 PART B IAW EA NR 10-5320-00242. 2L72 4F RTA21EA 20030926000882003092600088CE 2003 9 26 RJ14001 120030819A3260MS245471 POSITION SWITCH BEECH MU300 400BEECH CE MLG FAILED E ERYAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07599JL8628 RJ14 GEAR WARNING SOUNDED DURING GEAR RETRACTION SHORTLY AFTER TAKE-OFF. 2H72 4F RTA16SW 20030926001022003092600102NM 2003 9 26 03FDEA01385 120030826A5320 SUPPORT FITTING BOEING727 727200 138407ENM BULKHEAD CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CORROSION ATTACH FITTING ON BS 228 BULKHEAD, AFT SIDE, LBL 10, 6 INCHES BELOW UPPER PRESSURE DECK IS CORRODED ON UPPER SIDE. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-5 & 51-30-2. 2L73 4F RTA3WE 20030926001072003092600107EU 2003 9 26 255033 120030901A3150004WS00 WARNING SYSTEM SAAB SF340 340B 7860101EU AIR CONDITIONINGACTIVATED A NSVAD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27299CJ 340B299 ON TAKEOFF WHEN GEAR SLECTED UP SHE GETS A CHIME WHEN THE AIR CONDITIONING CAUTION LIGHT ILLUMINATES WITH T/O INHIBIT SELECTED. REMOVED AND REPLACED (WEU) WARNING ELECTRONICS UNIT OPS CHECKED GOOD. 2L72 4T RTA52EU 20030926001122003092600112NM 2003 9 26 2003UALA00645 120030821A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 MAIN CABIN AT BS 987 TO 995 AT RBL 48 CREASE BEAM WEB CORRODED. MAJOR REPAIR ACCOMPLISHED, INSTALLED SILL. 2L72 4F4 FRTA16WE E2GL 20030926001312003092600131NE 2003 9 26 UPS03441156 220030830A7200 ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 4 FLAMED OUT A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO01676UP 20101 AT 1330Z INTO FLIGHT NR 4 ENG FLAMED OUT. COMPLY WITHIN FLIGHT ENGINE FAILURE/SHUTDOWN CK LIST. TRIED INFLIGHT START CK LIST AS THE ENG INDICATION WAS NORMAL WITH EXCEPTION OF NR 4 OIL TEMP BEING AROUND 100 DEG. REMOVED AND REPLACED MAIN FILTER, INSPECTED PIR, PTT2 AND PT2 LINES FOR LEAKS AND SECURITY. VERIFIED FUEL PUMP PRESSURE (700 LBS) FUEL FLOW AT START NORMAL, ENGINE A/I OPS NORMAL MM 71-00-46, 71-00-42. RAN NR 4 ENGINE TO 1.51 EPR 18.8 F/F, 95 PERCENT N1 818 EGT, NO DEFECTS. 2L74 4F4 F A20WE E20EA 20030926001402003092600140EU 2003 9 26 141191 120030901A3097 WIRE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE INTAKE HEAT BROKEN A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17149SZ 340A149 353 DURING FLIGHT THE RT AIR VALVE WARNING LIGHT ILLUMINATED. CREW FOLLOWED QRH AND REDUCED POWER BELOW 92 PERCENT, AND THE LIGHT STAYED ILLUMINATED. THE CREW RETURNED TO PIT A/C WAS TAKEN OUT OF SERVICE AT 2235 (LT). PIT MX T/S RT INTAKE HEAT SYSTEM AND FOUND A WIRE TO BE BROKEN ON THE RT INTAKE HEAT SWITCH. PIT MX REPAIRED WIRE, AND PERFORMED OPERATIONEL TEST OF THE RT INTAKE HEAT SYSTEM. OPERATIONAL TEST SATIFACTORY NO FAULTS NOTED. A/C RETURNED TO SERVICE AT 0040 9-2-03. 2L72 4T4 TRTA52EU E8NE6 20030926001412003092600141NM 2003 9 26 QXEA200300955 120030807A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 INOPERATIVE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09408QX 4050 AFT AIRSTAIRS WILL NOT DEPLOY. COMPLIED WITH HORIZON AIR EO 6-52-202A. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030929000022003092900002NM 2003 9 29 0301666303 120030829A3350 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01663US 23818 DURING LINE CHECK, FOUND ZONE 'B' LEFT AND ZONE 'E' RT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM THE DOOR TO ROW 12. REPAIRED ELECTRICAL CONNECTIONS LIGHT ASSEMBLIES. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030929000122003092900012NM 2003 9 29 AWXA200301012 120030813A533065458493 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 0.090 INCH CRACK WAS FOUND ON R-2 DOOR EXTERNAL SKIN AT CORNER OF UPPER HINGE CUTOUT. MAINTENANCE TRIMMED OUT CRACK ON R-2 DOOR EXTERNAL SKIN AT CORNER OF UPPER HINGE CUTOUT IAW B737-200 SRM 52-00-2 PG 3, FIG 1 & 6, SHEETS 3 & 6. 2L72 4F RTA16WE 20030929000212003092900021NM 2003 9 29 03FDEA01400 120030829A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 SIX PREVIOUSLY PLUGGED HOLES IN SKIN AT BS 400 BETWEEN STR 14 - 15 LT ADJACENT TO EXISTING FASTENERS. BS 400 SKIN AREA BETWEEN STR 14-15 LT WITH PLUGGED HOLES WAS REPAIRED PER FED EX EA 7-5330-70501. 2L73 4F RTA3WE 20030929000232003092900023NM 2003 9 29 03FDEA01411 120030903A5753 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500, CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP VANE STOP NOSE RIB SUPPORT ISLAND CRACKED. 2L73 4F RTA22WE 20030929000292003092900029NM 2003 9 29 03FDEA01421 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING I/B FLAP VANE I/B TEE FITTING I/B FACE AND O/B FACE FOUND WITH SURFACE CORROSION. SURFACE CORROSION ON RT WING, I/B FLAP VANE, I/B TEE FITTING, I/B & O/B FACE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL 2 AND FOUND WITHIN LIMITS. 2L73 4F RTA22WE 20040818001392004081800139EU 2004 8 18 KBM2004F00132 120030904A78100292808740 STRAP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE EXHAUST SUPPORT CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 EXHAUST SUPPORT STRAP HEAT SHRINK CRACKED. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040917000662004091700066NM 2004 9 17 2004F00331 120031220A3397 WIRE BOEING757 757236 1384971NM L2 DOOR EMER WORN A P9RAO OTHER L NO TEST CRCRUISE 1 SO11521NA 25592 FOUND EMERGENCY LIGHTS ON AT R2 AND L2 DOORS, ONLY DURING TURBULENCE. OVER L2 DOOR, FOUND TWO WIRES INSULATION WORN AWAY MAKING CONTACT. REPAIRED WIRING IAW SWPM 20-00-00. OPS CHECKED OK. (M) 2L72 4F RTA2NM 20040917000642004091700064NM 2004 9 17 TSAA0353219 120031102A57306545407 SKIN BOEING737 737282 13844ATNM LT WING CORRODED A TSAAO OTHER O OTHER NRNOT REPORTED 1 WP13824AL 23045 FOUND LT UPPER WING SURFACE CORRODED BETWEEN FRONT & REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 6 AS NR 1 - 19 AT LOCATIONS, NR 1, 2, & 3 AT WBL 227, NR 4 AT WLB 228, NR 5 AT WBL 254, NR 6 AT WBL 264, NR 7 AT WBL 268, NR 8 AT WBL 234, NR 9 AT WBL 236, NR 10 AT WBL 309.5, NR 11 AT WBL 555, NR 13 AT WBL 355, NR 18 AT WBL 580, AND NR 19 AT REAR SPAR WS 571. REMOVED CORROSION, FLAT PEEN, ALODINED, & SEALED. R & R FASTENERS WITHIN BLEND OUT AREA PER SRM. NR 12 AT WBL 555 FABRICATED & INSTALLED AN INTERNAL STRAP. NR 14, 15, 16 & 17 AT OVERWING REFUELING PORT WS 442 FABRICATED & INSTALLED REPAIR STRAPS AND FILLERS IAW SRM. REPAIRS COMPLETED IAW ECO 3400. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040721000342004072100034EU 2004 7 21 2004F00181 120031002A5320D5347048600000 INTERCOSTAL AIRBUS320 A320233 3930329EU CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUNDINTERCOSTAL AT FORWARD CARGO COMPARTMENT BETWEEN FRAME 51 AND 52 RBL 27 HAS SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL AT AFT CARGO COMPARTMENT BETWEEN FRAME 51 AND FRAME 52, RBL 27. (M) 2L72 4F RTA28NM 20040721000362004072100036EU 2004 7 21 USAASA03125 120031025A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW 1040 THE SEAT MOUNTED EMERGENCY LIGHT ON SEAT 4C WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT IN THE FORWARD CABIN. OPERAITONAL CHECKS OK. (M) 2L72 4F RTA28NM 20040722000142004072200014SW 2004 7 22 2004F00193 120031120A26121734361450 CONNECTOR SWRNGNSA227 SA227AC 8780603SW NR 2 FIRE LOOP LOOSE A BSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM05158MC AC726B NR 2 ENGINE FIRE WARNING LIGHT CAME ON DURING CLIMB, CREW DECLARED AN EMERGENCY AND RETURNED TO STATION. SUSPECT INDICATION PROBLEM. FOUND FIRE DETECTOR MOUNTED UNDER THE OIL COOLER AT THE FIRE WALL WITH A LOOSE CENTER CONNECTOR, ALLOWING THE CERAMIC CENTER TO SHIFT AND GO TO GROUND. TIGHTENED CENTER CONNECTOR AND INSTALLED SECOND NUT AS A SAFETY. SYSTEM OPS CHECKED GOOD. (M) 2L72 4T RTA8SW 20040825002642004082500264NM 2004 8 25 2004F00244 120031115A275165DT11005139 INDICATOR BOEING727 727233 138408ANM TE FLAPS DEFECTIVE A PCSAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO17495AJ 20937 FLT 855 - KMIA-MTPP - AFTER TAKEOFF, PILOT REPORTED ASYMMETRIC OUTBOARD FLAP LOCKS OUT. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OUTBOARD FLAP POSITION INDICATOR DEFECTIVE. REMOVED AND REPLACED OUTBOARD FLAP POSITION INDICATOR IAW MM 27-51-0, OPS CHECK OK. INSPECTED FLAPS POSITION TRANSMITTER CABLES AND PULLEYS, LUBRICATED CABLES AND PULLEYS, IAW MM 27-51-0. AIRCRAFT RETURNED BACK TO SERVICE. (M) 2L73 4F RTA3WE 20040902001602004090200160NM 2004 9 2 2004F00263 120031203A1420 CONNECTOR BOEING737 7373K2 13844BANM START VALVE LOOSE A FX7AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO19550FA 23411 DURING TAXI-OUT, NR 1 START VALVE OPEN LIGHT ILLUMINATED, RETUREND TO GATE. REMOVED CLEANED AND RE-TIGHTENED THE NR 1 ENGINE START VALVE CONNECTOR PER MM 80-10. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS. (M) 2L72 4F RTA16WE 20040902001622004090200162NE 2004 9 2 MEX2003571 220031229A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RIGHT OVERSPEED A ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23169PL 53175 FLT 460 - GDL-LAX - AIRCRAFT RETURNED, DUE TO DURING TAKEOFF, WITH ATS OUT OF SERVICE, THE RIGHT ENGINE N1 REACHED AN OVERSPEED OF 105.1 PERCENT. CAPTAIN PERFORMED PROCEDURE DURING DESCENT AND THE EPR'S REACHED 2 LASTING 2 MINUTES, AFTER THAT ALL PARAMETERS WITHIN LIMITS. AT GDL STATION, THE RIGHT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-01 AND 71-00-02, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20040902001902004090200190NE 2004 9 2 2004F00264 220031106A7261714810 VALVE BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE NR 3 ENGINE LEAKING A PCSAEA ENGINE SHUTDOWN UNSCHED LANDING XFJENGINE FLAMEOUT FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO17495AJ 20937 DURING CLIMB-OUT, F/E REPORTED NR 3 ENG FIRE WARNING LIGHT ILLUMINATED. CAPTAIN FOLLOWED EMERGENCY PROCEDURES. A/C DIVERTED TO KMIA & LANDED WITHOUT FURTHER INCIDENT. MX OPENED COWLING & FOUND EVIDENCE OF FLASH FIRE. FOUND STARTER WITH INTERNAL FAILURE, INSPECTED P/D VALVE & FOUND A LOOSE B-NUT WITH EVIDENCE OF FUEL LEAK, CLEANED GEN FEEDER WIRES NO DEFECT NOTED, INSPECTED INLET & TURBINE SECTION, NO DAMAGE FOUND. R & R STARTER, P/D VALVE, START VALVE, CSD INLINE SCREEN FILTER MOUNTING BOLTS & GEN FEEDER WIRE PER MM, & SWPM 20-10-11. REMOVED MAIN OIL FILTER & FOUND NO DEFECTS. R & R DISCHARGED LT FIRE BOTTLE IAW MM 26. RAN ALL ENGS IAW P/W MM 72-00, NO DEFECT NOTED. A/C RETURNED BACK TO SERVICE. (M) 2L73 4F4 FRTA3WE E2EA 20040910000562004091000056NM 2004 9 10 2004F00271 120031222A1420 CONNECTOR BOEING727 727276 138408RNM PWA JT8 JT8D15 52051NE BYPASS LIGHT DIRTY A FX7AEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19908PG 20951 ENGINE NR 1 OIL FILTER LIGHT ILLUMINATED IN CLIMB, FOLLOWED PROCEDURES AND SHUTDOWN ENGINE DUMPED FUEL AND RETURNED TO TSJU WITHOUT INCIDENT. CLEANED CONNECTOR ON OIL FILTER BYPASS LIGHT SWITCH CHECKED AND CLEANED OIL FILTER RAN ENGINE IAW 79-33-0. ENGINE CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE WITHOUT INCIDENT. (M) 2L73 4F4 FRTA3WE E2EA 20030926000042003092600004EU 2003 9 26 S9H2003F00003 120030714A2910704A33690004 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE HYD SYS FAILED E S9HAO OTHER O OTHER NRNOT REPORTED 1 WP19356NT83 2280 DURING A CHECK RIDE, THE AIR CONDITIONING SYSTEM FAILED. ISOLATION OF THE SYSTEM WAS CONDUCTED. ON THE RETURN FLIGHT BACK TO BASE, SHORTLY THEREAFTER THE HYDRAULIC SYSTEM FAILED. AIRCRAFT PERFORMED RECOMMENDED PROCEDURES AND UPON INSPECTION OF THE SYSTEM IT WAS CONFIRMED THAT THE AIR CONDITIONING BELT AND THE HYDRAULIC BELTS FAILED. BELTS WERE REPLACED. 1G71 3U3 UNCH9EU E19EU 20030926000102003092600010NM 2003 9 26 QXEA200301029 120030820A5711 SPAR DHAV DHC8 DHC8202 2809007NM ZONE 600 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 GOUGE IN RADIUS OF RIGHT HAND FORWARD SPAR TOP FLANGE TO SKIN JOINT FROM YW286.5 TO YW297.5. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-57-1675. 2H72 4T RTA13NM 20030926000372003092600037NM 2003 9 26 03FDEA01386 120030826A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 STA 720A STR 24L SKIN HAS A DENT. REMOVED DAMAGED SKIN AT 720A, STR 24L AND REPAIRED. WORK DONE IAW BOEING 727 SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20030926000392003092600039EU 2003 9 26 A1U2003F00001 120030801A530211730102 STRUCTURE BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE TAILBOOM CRACKED E A1UAK NONE O OTHER ININSP/MAINT 1 CE03211SL12150 7201 45618 WHILE PERFORMING A DAILY INSP, MECHANIC FOUND A .5000 INCH CRACK EXTENDING PAST THE LEADING EDGE FAIRING FOR THE HORIZONTAL STABILIZER, THE CRACK WAS IN THE TAILBOOM OF THE AIRCRAFT, AFTER REMOVING THE FAIRING FOR FURTHER INSPECTION, IT WAS DETERMNED THAT CRACK WAS 1.5 INCHES LONG EXTENDING UPWARDS FROM THE LEADING EDGE OF THE HOLE PROVIDE FOR THE HORIZONTAL STABILIZER, IN THE LEFT HAD SIDE OF THE TAILBOOM. TAILBOOM WAS REMOVED FROM AC AND SENT FOR REPAIR, A SERVICEABLE TAILBOOM WAS INSTALLED AND THE AC WAS RETURNED TO SERVICE ON 8/2/03. THIS AREA OF TAILBOOM IS PRONE TO CRACKS, PILOTS AND MECHANICS SHOULD PAY CLOSE ATTENTION TO THIS AREA ON PREFLIGHT AND DAILY INSPECTIONS. 1G72 3U3 U H13EU E5NE10 20030926000412003092600041NE 2003 9 26 ABXA030342 220030827A7200 FAN BOEING767 767281 1385109NM GE CF6 CF680A 30025NE RT ENGINE VIBRATION A ABXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL23786AX 23019 580168 RT ENGINE FAN VIBRATION INDICATIONS WERE HIGH. BETWEEN 2.5 AND 3.5, FL 390, M .80. ACCOMPANIED BY AIRFRAME/ENGINE VIBRATION. SETTLED BACK TO 1.5 THEN BACK TO 3.0. THIS CONTINUED FOR APPROXIMATELY 30 MINUTES THEN WENT AWAY. PERFORMED FIM 71-05-00-60, NO DEFECTS NOTED. PERFORMED AMM 71-00-00-5, TEST NR 7, ENGINE VIBRATION WITHIN LIMITS. ENGINE WITHIN LIMITS IAW AMM 71-00-00-2, PARA. J. 2L72 4F4 FRTA1NM E13NE 20030926000462003092600046 2003 9 26 00106 420030825A34188198022 TRANSDUCER LEAR 25 25 5170506CE AOA MALFUNCTIONED E HAEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW05147TW 023 PILOT REPORTED AT V1 NOSE OF AIRCRAFT OSCILATED UP AND DOWN, ABORTED TAKEOFF. AIRCRAFT WENT INTO OVERRUN AREA, NO DAMAGE TO AIRCRAFT OR AIRPORT. TAXIED BACK TO RAMP. MAINTENANCE INSPECTED NOSE STRUT AND HORIZONTAL STAB AND ELEVATOR CONTROL SYSTEM, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. UPDATE WITH FURTHER INFO FROM NEXT FLIGHT. AFTER DEPARTURE STICK SHAKER AND STICK PUSHER BEGAN OPERATING, STALL WARNING WAS TURNED OFF AND AIRCRAFT RETURNED TO ELP. NR 2 AOA TRANSDUCER WAS REPLACED, GROUND OPS CK GOOD. NO FURTHER PROBLEMS NEXT FLIGHT. 2L72 4J A10CE 20030926000542003092600054EA 2003 9 26 COMA0360382 120030821A80108989308 START VALVE CNDAIRCL600 CL6002B19 1900309EA RT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01952CA9434 7092 FLIGHT 5868 RT ENGINE STARTER ENGAGED DURING FLIGHT 3 TIMES. REPLACED THE AIR START VALVE. 2L72 4F RTA21EA 20030923000822003092300082WP 2003 9 23 DHL2003604775 120030525A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 UPPER EXTERNAL FUSE SKIN CORRODED AT STA 1050.000 BETWEEN L-2R - L-2L. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED ARE IAW SRM 51-1-8B. FABRICATED FINGER DOUBLERS (02 EA) (7075-T6 AL0.050) AND DOUBLER (7075-T6 AL0.090) IAW EODHL-030553. CLEANED, TREATED AND PRIMED FINGER DOUBLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FINGER DOUBLERS AND DOUBLER WITH NEW FASTENERS IAW EODHL-030553, ED-3307, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000902003092300090WP 2003 9 23 DHL2003604697 120030615A5320 TEE FITTING DOUG DC8 DC873F 302199FWP PRESSURE BLKHD CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT AFT PRESSURE BULKHEAD TEE FITTING CRACKED 2.500 APPROX BETWEEN L-7 AND L-8R STA 1766.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 9, SRM 51-1-1. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED REPAIR ANGLE (7075-T6 0.125) IAW SRM 53-2-5 FIG 9. HEAT TREATED REPAIR ANGLE IAW SRM 51-1-1 PG 11-13. PERFORMED LIQUID PENETRANT INSPECTION TO REPAIR ANGLE IAW DC8 NDT SPM PART 08-00-02106. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER WITH NEW FASTENERS IAW SRM 53-2-5 FIG 9 SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923001352003092300135NM 2003 9 23 234TR0011 120030821A33506013211 BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05234TR 23004 RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW MM 33-51-31. OPS CHECKS GOOD. 2L72 4F RTA16WE 20030923001652003092300165NM 2003 9 23 AALA20030459 120030414A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21921AN 29522 DURING OVERNIGHT MAINTENANCE, FOUND GALLEY EMERGENCY EXIT LIGHT DAMAGED. REPLACED GALLEY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030924000922003092400092NM 2003 9 24 AWXA200300984 120030816A532069353521 STRINGER CLIP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON TOP LEG OF STRINGER CLIP 22 RT, FORWARD SIDE OF BS 787. MAINTENANCE REMOVED CRACKED STRINGER CLIP 22 RT, BS 787; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, STEP 4B-4E, FIG. 3, 4, & 7. 2L72 4F RTA16WE 20030924001222003092400122WP 2003 9 24 AALA20030835 120030804A2432100105901 CHARGER DOUG DC9 DC982 3022082WP BATTERY FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21461AA 49566 EN ROUTE AIRCRAFT EXPERIENCE BATTERY CHARGER FAULT LIGHT. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030924001342003092400134EU 2003 9 24 AALA20030726 120030707A3233D226550002 ACTUATOR AIRBUS300 A300B4605R 3930308EU LT MLG MALFUNCTIONED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2159081 639 EN ROUTE MIA-SDQ, AFTER TAKEOFF, LANDING GEAR DID NOT RETRACT. RETURNED TO MIA WITHOUT FURTHER INCIDENT. REPLACED LEFT LANDING GEAR PITCH TRIM ACTUATOR. ACCOMPLISHED LANDING GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030926000432003092600043EU 2003 9 26 L2S2003F00000 120030723A6730 SERVO BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE TAIL ROTOR FAILED E L2SAO OTHER O OTHER NRNOT REPORTED 1 CE07911KS 7042 SERVO FAILED. INPUT PILOT VALVE INTERMITTENT. OPS INTERNALLY. CAUSED TAIL ROTOR CONTROL HARDER TO PUSH RIGHT THAN LEFT. SLIGHT BINDING IN TAIL ROTOR CONTROL. 1G72 3U3 U H13EU E5NE 20030926000642003092600064NM 2003 9 26 AWXA200300995 120030827A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 5 LT BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28182AW 22649 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030926000662003092600066NM 2003 9 26 AWXA200300997 120030817A53126516300191 BULKHEAD BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF WEB AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-11 PG 1, FIG 11. 2L72 4F RTA16WE 20030926000702003092600070NM 2003 9 26 C1HA200396017 120030828A3260 ACCESSORY UNIT BOEING727 7272J4 1384006NM MLG MALFUNCTIONED A C1HAO OTHER N FALSE WARNING CLCLIMB 1 GL15696CA 22574 ON GEAR RETRACTION AT STL, RED NOSE GEAR LIGHT REMAINED ILLUMINATED. CYCLED GEAR HANDLE UP - LIGHT REMAINED ON (CONT) ON ARRIVAL AT LAS. RED LIGHT EXTINGUSHIED WITH GEAR EXTENTION. RED NOSE GEAR LIGHT FLICKERED ON & OFF DURING TAXI INSPECTED NOSE GEAR WIRING HARNESS AND CONNECTIONS NO DESCREPANCIES NOTED. COULD NOT DUPLICATE RED NOSE GEAR LIGHT INDICATION. REMOVED, CLEANED, INSPECTED LANDING GEAR ACCESSORY UNIT ALL APPEARS OK. REFFM/M 32-61-71. 2L73 4F RTA3WE 20030926000732003092600073NM 2003 9 26 03FDEA01398 120030828A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CORROSION AT NUT PLATES BS 351 TO 341, LBL 18 TO RBL 18, W/L 152. REMOVED CORROSION ON T-CHORD AT VARIOUS LOCATIONS 1 X 1 X .077 INCH FROM ORIGINAL THICKNESS OF .097 INCH AT BS 341-351, LBL 18, RBL 18, WL 152 AND IS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND INSTALLED NEW CHORD AT BS 340, LBL 18 - RBL 18, WL 152 IAW SRM 51-30-2. 2L73 4F RTA3WE 20030926000892003092600089WP 2003 9 26 EIA2003110 120030826A33501001191 LIGHT DOUG DC9 DC933F 302207AWP CABIN WEAK A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09944F 47194 PORTABLE EMERGENCY EXIT LIGHT JUST INSIDE OF L-1 DOOR INOPERATIVE. REMOVED AND REPLACED PORTABLE EXIT LIGHT IAW DC9 MM 20-50-0 OPS CHECKED GOOD. 2L72 4F A6WE 20030926000952003092600095NM 2003 9 26 P5CA0300932 120030816A575365B02093202 PANEL BOEING747 747200 1384847NM TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 RT WING INBOARD TRAILING EDGE FLAP MID- FLAP PANEL DELAMINATED. REPAIRED BY BOUNDING NEW SKIN. 2L74 4F RTA20WE 20030926000972003092600097NM 2003 9 26 P5CA0300933 120030831A29133508806 PUMP BOEING747 7472U3B 1384846NM HYD SYS LEAKING A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23922FT 22768 LOSS HYD FLUID NR 4 SYS. NR 4 EDP REMOVED AND DEACTIVATED INSTALLED DEACTIVATION KIT IAW MEL 29-01-A TRASFERRED TO DMI 31340. 2L74 4F RTA20WE 20030926001002003092600100CE 2003 9 26 DXTA200300107 120030901A2750 CONTROL UNIT CESSNA750 750 2076810CE TE FLAPS INOPERATIVE E DXTAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 GL07929QS 7500129 AMBER (FLAPS FAIL) CAS MESSAGE ILLUMINATED IN FLIGHT WOULD NOT RESET. FLAPS WOULD NOT EXTEND, SLATS OPERATED NORMALLY, DIVERTED INTO JFK AND LANDED SAFELY. 2L72 4J RTT00007WI 20030926001102003092600110NM 2003 9 26 2003UALA00643 120030822A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 CREASE & PUNCTURE EXTERNAL FUSELAGE STA 463 TO STA 440 STR 16L &17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20030926001162003092600116EU 2003 9 26 A6WA200360031 120030803A2400MS2207310 CIRCUIT BREAKER BAC 146 146200A 1500266EU OVERHEAD PANEL INOPERATIVE A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL31292UE E2087 SMELLED ELECTRICAL SMOKE, SAW SPARKS FROM APU/ENGINE START PANEL, APPEARED TO BE START AND CONTINUOUS (A) CENTRAL C/B AND ALL IGNITION (A) AND CONTINUOUS IGNITION (A) 2 AND 3, PULLED C/B`S SPARKS STOPPED. PULLED CONTINUOUS IGNITION (A) 1 AND 4 C/BS. REMOVED AND REPLACED CIRCUIT BREAKERS E27 (L SCREEN HEAT (A)) AND E29 (MANUAL TEMP CONTROL). REMOVED AND REPLACED WIRES 133C AND FE44. GENERATED ADDITIONAL WORK CARDS IN WORK ORDER 52491 FOR OPS CHECKS. 2H74 4F A49EU 20030926001212003092600121NM 2003 9 26 DHL2003741008 120030829A52701EN161RB1 SWITCH BOEING727 7272Q9 138448MNM DOOR WARNING MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01741DH 21931 RIGHT GEAR DOOR OPENED WHEN GEAR HANDLE MOVED TO THE OFF POSITION. CYCLED HANDLE UP-OFF. DOOR REMAINED CLOSED ON SECOND ATTEMPT. REMOVED AND REPLACED LANDING GEAR DOOR WARNING SWITCH RT GEAR DOOR IAW M/M 32-62-11. SWITCH P/N: 1EN161RB1 TESTED IAW M/M 32-62-11. PERFORMED LANDING GEAR SWING IAW M/M 32-32-00. SYSTEM CHECKED GOOD AT THIS TIME. OK TO CONTINUE. 2L73 4F RTA3WE 20030926001282003092600128NM 2003 9 26 UPS03241153 120030815A5753 RIB BOEING727 72725C 138400HNM RT WING TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 INSPECTION TYPE: C, RT WING L/E CAVITY SUSPECT CRACK ON RIB ABOVE NR 5 L/E FLAP ACTUATOR ON INVESTIGATION T-SECTION FOUND CRACKED & CORRODED. REPLACED T-SECTION IAW SRM 51-30-02 & DRAWING NR 656268. 2L73 4F A3WE 20030926001422003092600142NM 2003 9 26 AWXA200301003 120030830A2560P2070001214 FLASHLIGHT BOEING737 7373S3 1384711NM ZONE 900 - LAVATINOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28313AW 23712 FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030926001432003092600143NM 2003 9 26 AWXA200301004 120030831A3397BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 3 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030926001452003092600145NM 2003 9 26 AWXA200301006 120030901A7312320115 VALVE BOEING737 737277 1384570NM NR 1 ENGINE BINDING A AWXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP28183AW359091031 22650 EN ROUTE FROM ONT TO PHX AT CRUISE RECEIVED HIGH OIL TEMPERATURE LIGHT, FOLLOWED QUICK REFERENCE HANDBOOK AND SHUTDOWN THE NO. 1 ENGINE, LANDED AT PHX WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE FUEL HEAT VALVE STUCK IN THE OPEN POSITION, REMOVED AND REPLACED FUEL HEAT DEICING AIR VALVE IAW BMM 73-14-11, PG. 401, OPERATIONAL CHECK WAS GOOD. WIND-MILLING DETERMINED TO BE LESS THAN 30 MINUTES, INSPECTED CHIP DETECTORS, NO DEFECTS NOTE, REMOVED AND REPLACED OIL FILTER AND CHANGED OIL. 2L72 4F RTA16WE 20030926001502003092600150WP 2003 9 26 ABXA030344 120030821A57535919217501 FITTING DOUG DC9 DC932 3022066WP TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 FLAP HINGE STUDS AT FLAP FITTING STA. 267 HEAVILY CORRODED. REPLACED FLAP HINGE IAW DC-9 MM 57-40-01-2-0001. 2L72 4F A6WE 20030929000062003092900006EA 2003 9 29 COMA0360398 120030829A2750860D10018AB FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01986CA15969 7174 FLT 5804 FLAPS FAIL MESSAGE DURING FLIGHT. REPLACED THE FECU. 2L72 4F RTA21EA 20030929000072003092900007EA 2003 9 29 COMA0360401 120030901A3241TC6019355 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS DAMAGED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01976CA17265 7151 ANTI-SKID OUTBOARD CAUTION MESSAGE DURING T/O. REPLACED THE OUTBOARD WHEEL SPEED TRANSDUCER. 2L72 4F RTA21EA 20030929000102003092900010NM 2003 9 29 AWXA200301010 120030813A5320654583470 STRAP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .5 INCH CRACK WAS FOUND ON FLOOR STRUCTURE TIE STRAP AT BS 342, LBL 1. MAINTENANCE REMOVED CRACKED TIE STRAP AT BS 342, LBL 1; FABRICATED A NEW REPLACEMENT TIE STRAP AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-09 PG 1, FIG 4. 2L72 4F RTA16WE 20030929000152003092900015EA 2003 9 29 COMA0370027 120030829A3230492301 SLEEVE CNDAIRCL600 CL6002C10 1390015EA RT MLG T LINK BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA2019 10069 RT MLG LOWER TORQUE LINK ASSY HAS BROKEN LOCKING SLEEVE. REMOVED BROKEN SLEEVE AND INSTALLED A SERVICEABLE ONE. 2L72 4F RTA21EA 20030929000302003092900030NM 2003 9 29 03FDEA01422 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING I/B FLAP VANE I/B TEE FITTING MID BORE FOUND WITH CORROSION. CORROSION ON RT WING, I/B FLAP VANE, I/B TEE FITTING, MID BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL 2 AND FOUND WITHIN LIMITS. 2L73 4F RTA22WE 20030929000322003092900032NM 2003 9 29 03FDEA01437 120030904A3610 CLAMP BOEING727 727200 138407ENM ZONE 400 LOOSE A FDEAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25207FE 22929 WHILE DEPARTING LAS, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED FOR (TEMP 37C) APPROX 15 SECONDS DURING INTIAL TAKE-OFF/ CLIMBOUT AT 180 KTS PRIOR TO FLAP RETRACTION, THEN EXTINGUISHED. SYSTEM TESTED OK REFERRED TO QRH AND CONTINUED. FOUND CLAMPS ON ENGINE BLEED VALVE LEAKING. REMOVED AND REPLACED CLAMPS IN REFERENCE TO B727-200 AMM 36-10-001-4. LEAK CHECK GOOD. 2L73 4F RTA3WE 20030929000332003092900033NM 2003 9 29 03FDEA01432 120030902A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING O/B FLAP O/B HINGE (A/C SIDE) I/B ACTUATOR ATTACH BORE FOUND CORRODED. 2L73 4F RTA22WE 20030929000362003092900036NM 2003 9 29 03FDEA01428 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RIGHT WING I/B FLAP VANE O/B TEE FITTING AFT BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG AFT BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490. 2L73 4F RTA22WE 20030929000372003092900037NM 2003 9 29 03FDEA01426 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RIGHT WING I/B FLAP VANE O/B TEE FITTING FWD BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG FWD BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490. 2L73 4F RTA22WE 20030929000402003092900040NE 2003 9 29 03FDEA01401 220030901A7210 PACKING BOEING727 727200 138407ENM PWA JT8 JT8D NE NR 1 ENGINE LEAKING A FDEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO25240FE 20978 700168 AFTER T/O NR 1 ENG EPR LOW WITH A HI FF AT FL200 NR 1 ENG THROTTLE LEVER 3 INCHES FWD OF NR 2 & 3 THROTTLE LEVERS W/ ALL EPR'S MATCHING & NR 1 FF GAUGE 3000 LBS/HR MORE THAN NR 2 & 3 FF GAUGES. ALL ENG INST IN GREEN. CL THRU FL230, NR 1 EPR INDIC 0 & NR 1 FF GAUGE IND 0 LBS/HR. ALSO NR 1 EGT GAUGE COOLING DOWN & N1 & N2 GAUGE LOW. PUSHED NR 1 THROTTLE LEVER FWD W/ NO ENG RESPONSE. FAILURE CHECKLIST COMPLETED. INSPECTED NR 1 ENG FOUND FUEL LINE FROM P&D VALVE TO FUEL OIL COOLER LEAKING. R & R PACKING AT P&D VALVE. RUN ENG IAW 727 JRH-OPS & LEAK CHKS GOOD. GND RUN ALL ENG'S ALL THROTTLE & ENG PARAMETERS MATCH. INSPECTED NR 1 ENG MAIN OIL FILTERS IAW 72-00-00 FOR ENG WINDMILLING, FOUND NO CONTAMINATION. 2L73 4F4 FRTA3WE E2EA 20040818001472004081800147EU 2004 8 18 KBM2004F00133 120031101A78100292808740 STRAP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE EXHAUST WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 ENGINE EXHAUST STRAP BRACKET WORN. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040721000332004072100033WP 2004 7 21 AALA20030836 120030803A3220SS093200147001 BUNGEE CYLINDER DOUG DC9 DC982 3022082WP NLG FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21251AA 49270 REPLACED NOSE GEAR BUNGEE CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040719001932004071900193EA 2004 7 19 A6WA20030190 120031210A53206013600130 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 FOUND RIGHT FS 640 BETWEEN STRINGER 9 AND STRINGER 12 ON AFT SIDE OF FRAME CRACKED AT SKIN DOUBLER. RIGHT REINFORCEMENT ANGLE REPLACED WHILE INCORPORATING SB 601R-53-061 REV E. (M) 2L72 4F RTA21EA 20040721001612004072100161 2004 7 21 HALA0400035 420031231A830037900912 GEARBOX BOEING717 717200 1383700NM NR 1 ENGINE FAILED A HALAK NONE O OTHER ININSP/MAINT 1 WP13476HA 55118 DEBRIS FOUND IN NR 1 ENGINE AGB SCAVENGE FILTER, METAL AND FIBERS, REF HAL M129 MCD AND AGB SCAVENGER FILTER INSPECTION (M1-79-03) TELCON W/J. SNOOK FOUND COPPER COLORED DEBRIS, FERROUS, GEARBOX CHANGE REQUIRED. REMOVED NR 1 ENGINE GEARBOX PER MM 72-61-00 STEPS 1 TO 6.12-31-03/6414 INSTALLED NR 1 ENGINE GEARBOX PER MM 72-61-00 WORKED SUBTASK 72-61-00-480-002 UP TO TIEM 8/4835 CONT INSTALLED FROM 5(G) TO 9(B)3. COMPLT AGB INSTALLED PER AMM 72-61-00-4. (M) 2L72 4F TRA6WE 20040713000992004071300099EU 2004 7 13 AALA20031253 120031111A335060030451 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211421K 11404 ORD - DURING OVERNIGHT MAINTENANCE, FOUND OVERHEAD EMERGENCY LIGHTS AT ROW 12 INOPERATIVE. RESEATED BATTERY PACK FOR OVERHEAD EMEGENCY LIGHTS AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20040713001272004071300127EU 2004 7 13 AALA20031175 120031022A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 JFK - MAINTENANCE OBSERVED EMERGENCY EXIT LIGHTING INOPERATIVE AT THE RIGHT SIDE OF ZONE A. REPLACED BATTEYR PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20040713001472004071300147NE 2004 7 13 HALA0301140 220031205A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 MAKING METAL A HALAK NONE O OTHER ININSP/MAINT 1 WP13485HA 55130 13301 LARGE AMOUNTS OF METAL FUZZ ON CHIP DETECTOR FOUND, NR 2 ENGINE. REMOVED NR 2 ENGINE PER HAL M144-717, 717 ENGINE REMOVAL. (M) 2L72 4F4 FTRA6WE E00061EN 20040713001642004071300164NM 2004 7 13 MEX2003568 120031227A492038003681 APU DOUG MD88 MD88 3023688NM APU BAY SMOKE A ASMFK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW23158PL 49761 FLT 422 - MEX-MIA - DUIRNG TRANSIT CHECK, WHEN THE GROUND POWER UNIT WAS CONNECTED, SMOKE WAS DETECTED IN THE PASSENGER CABIN. BOTH A/C SYSTEM WERE TESTED BUT SMOKE CONTINUED. THE WATER SEPARATORS WERE REPLACED AND SYSTEM WAS TESTED IAW MM 21-20-02, ALL CORRECT. DURING OVERNIGHT SERVICE, IN MEX STATION THE APU WAS VERIFIED DETECTING INTERNAL DAMAGES AND AN INTERNAL OIL LEAKAGE. THE APU WAS REPLACED AND SYSTEM TESTED IAW MM 49-00. (M) 2L72 4F RTA6WE 20040713000982004071300098NM 2004 7 13 TSAA0451013 120031129A49106546579 STRINGER BOEING737 737230 1384401NM APU BAY CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 APU INLET LONGERON STIFFENER, TORQUE BOX, EXFOLIATED. CUT AND REMOVED DAMAGED PORTION OF FORMED STRUCTURE. FABRICATED REPAIR PARTS FROM MATERIALS SPECIFIED IN TABLE 1. APPLIED ONE COAT OF BMS 10-11, TYPE 1 PRIMER, AND INSTALLED REPAIR PARTS WET WITH FASTENERS, MAKING A FAYING SURFACE SEAL WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 51-40-1, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040713001002004071300100EU 2004 7 13 AALA20031254 120031111A335060030451 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211421K 11404 ORD - DURING OVERNIGHT MAINTENANCE, FOUND TWO RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK FOR RIGHT OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20040713001262004071300126EU 2004 7 13 AALA20031255 120031111A335060030451 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211421K 11404 ORD - DURING OVERNIGHT MAINTENANCE, FOUND AISLE OVERHEAD EMERGENCY LIGHT AT ROW 17 INOPERATIVE. RESEATED BATTERY PACK FOR AISLE OVERHEAD EMERGENCY LGIHT AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20040713001402004071300140WP 2004 7 13 AMTA200301535 120031229A2530724105A OVEN LKHEED1011 10113853 5265020WP GALLEY MALFUNCTIONED A AMTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11163AT 1229 OVEN NR 3 AFT OUTBOARD BY L4 DOOR HAS A ELECTRICAL ODOR AND SMOKE COMING FROM ALL AROUND IT. SMOKE/ELECTRICAL FILLED THE HOLE AFT GALLEY KILLED OVEN POWER AT F/E PANEL. OPENED ALL C/B'S ON ALL AFT OVENS. REMOVED AND REPLACED NR 3 AFT GALLEY RCCB FEEDER NR 3 IAW MM 24-50-02, OPS CHECKS GOOD. REMOVED AND REPLACED OVEN NR 3 IAW MM 25-31-05. OPS CHECKS GOOD OK FOR SERVICE. (M) 2L73 4F A23WE 20040720001282004072000128SO 2004 7 20 C2XA03CL220 120030116A3230MS277891A SWITCH EMB 145 EMB145LR 3260212SO MLG EMER INTERMITTENT A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2713988 145265 CLE FLIGHT 2301 THE CREW REPORTED THE NOSE GEAR DOORS STAYED OPEN AFTER GEAR RETRACTION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR EMERGENCY EXTENSION OVERRIDE SWITCH. WIRE SPLICE SP1750 WAS ALSO REPAIRED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20040721000322004072100032NE 2004 7 21 AALA20030832 220030804A7261 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 1 LEAKING A AALAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW21424AA 49336 725375 EN ROUTE SHUT DOWN NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. AIRCRAFT DIVERTED TO AMA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030925000992003092500099EU 2003 9 25 DXTA200300121 120030919A2170 COALESCER BAG BRAERO1000 BAE1251000A 1500104EU PWA 305 PW305B 52128NE CABIN COOLING CONTAMINATED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07503QS 259003 PCE30525 ON CLIMB OUT AT 15,000 FT BROUGHT THRUST LEVERS TO IDLE AND CABIN BEGAN FILLING WITH SMOKE. REPLACED WATER SEPARATOR SOCK, AND LOWERED NR 2 ENG OIL PRESS IAW HAWKER 1000 M/M, CHAPTER 71-00-00 AND CHAPTER 21-50-15. AIR CONDITIONING SYSTEM FUNCTIONAL CHECKED GOOD. 2L72 4F4 FRTA3EU E35NE 20030926000682003092600068CE 2003 9 26 0021 120030828A57511005241201 SPROCKET BEECH 200 B200 1152922CE AILERON DEFECTIVE E CIEAK NONE O OTHER ININSP/MAINT 1 NM03203LG6275 BB926 DURING COMPLIANCE, THE AILERON SPROCKET WAS FOUND TO HAVE A POSSIBLE DEFECT. DOING A VISUAL INSPECTION BETWEEN THE TWO GEARS OF THE AILERON SPROCKET, ON THE LARGE GEAR NEAR THE SHAFT AREA, IT APPEARS THE WELDING MAY NOT HAVE BEEN COMPLETED IN A SMALL AREA, APPROXIMATELY .2500 INCH LONG, OR A CORROSION PIT HAS STARTED. THE DEFECT LOOKS LIKE A CORROSION TYPE OF PIT. THERE WAS NO VISUAL EVIDENCE OF A CRACK. NO NDT WAS PERFORMED ON THE UNIT AT THIS TIME. UNIT WAS CHANGED AS A PRECAUTION. 1L72 4T A24CE 20030926000792003092600079WP 2003 9 26 UPS03841149 120030828A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECKS OK AT THIS TIME. 2L74 4F RT4A25 20030926000802003092600080WP 2003 9 26 UPS03841150 120030828A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:N/A EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CK GOOD. 2L74 4F RT4A25 20030926000812003092600081EA 2003 9 26 COMA0360390 120030825A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01489CA1475 7755 GEAR DISAGREE WARNING, HYDRAULIC QUANTITY LESS THAN 5 PERCENT, REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20030926000942003092600094EU 2003 9 26 XNOA01151 120030829A2930 WARNING LIGHT AIRBUS300 A300B4203 3930306EU GREEN HYD SYS ILLUMINATED A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23372PC 196 ON TAXI OUT GREEN SYSTEM HYDRAULIC TEMP HI LIGHT CAME ON. PERFORMED INTERNAL LEAKAGE CHECK IAW A300 MM 27-00-00. OPS CHECK GOOD. 2L72 4F RTA35EU 20030926000962003092600096NM 2003 9 26 P5CA0300934 120030831A801174017913 STARTER BOEING747 747236B 1384804NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23924FT 21730 702225 ON START UP NR 4 ENG STARTER FAILED. REMOVED AND REPLACED 4 ENG STARTER IAW MM 80-11-01 OPS CK GOOD. 2L74 4F4 F A20WE E3NE 20030926001202003092600120EA 2003 9 26 A6WA200340115 120030730A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 GENERATOR LACK OF LUBE A A6WAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 GL31429AW 7711 GENERATOR 2 FAILED UPON APPLICATION OF TAKEOFF POWER. SERVICED IDG OIL AS REQUIRED, OPS CHECK GOOD. 2L72 4F RTA21EA 20030926001222003092600122EU 2003 9 26 DHL2003366005 120030826A733445D51 PRESSURE SWITCH AIRBUS300 A300B4203 3930306EU FUEL SYSTEM INOPERATIVE A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01366DH 249 ENGINE NR 1 FUEL FILTER CLOG LIGHT ILLUMINATED ON APPROACH. ABNORMAL PROCEDURE PERFORMED, LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW M/M 73-34-11. AFTER INSPECTION OF FUEL FILTER IAW M/M 73-12-03 IN WHICH NO CONTAMINATION FOUND. RAN ENGINE IAW JRH, SYSTEM OPS CHECKED GOOD. 2L72 4F RTA35EU 20030926001242003092600124EA 2003 9 26 A6WA200340117 120030804A3610 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA BLEED AIR DUCT ILLUMINATED A O OTHER O OTHER NRNOT REPORTED 1 GL31417AW 7610 LEFT 14TH STAGE BLEED AIR DUCT WARNING INFLIGHT COMPLIED WITH QRH MESSAGE WENT OUT AND THEN CAME BACK 10 MINUTES. WITH ENGINE SHUTDOWN MESSAGE PERSISTED ON GROUND. REMOVED AND REPLACED LT PYLON SENSING ELEMENT A59WK IAW AMM 36-21-04. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030926001292003092600129NM 2003 9 26 UPS03241154 120030812A5340 FITTING BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 INSPECTION TYPE: C, LT BS 740 FITTING CRACKED BEYOND LIMITS. LT BS 740 FITTING REPLACED IAW UPS EO B727-5310-7477-C. 2L73 4F A3WE 20030926001342003092600134WP 2003 9 26 DHL2003801089 120030902A5230 SEAL DOUG DC8 DC873F 302199FWP CARGO DOOR LEAKING A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01801DH 46033 CABIN PRESSURIZATION SYSTEM WILL NOT HOLD CABIN PRESSURE BELOW 10,000 UNLESS BOTH FLOW SWITCHES ARE IN THE MID POSITION OR HIGHER. CABIN ALTITUDE HORN ACTUATED AND THE EMERGENCY PROCEDURES WERE ACCOMPLISHED.INSPECTED AND CLEANED MAIN DOOR SEAL AND INFLATION HOLES. CHECKED GOOD AT THIS TIME IAW DC-8 M/M 52-36-8. 2L74 4F RT4A25 20030926001352003092600135EU 2003 9 26 UG82003F00001 120030120A5522 SKIN BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP ELEVATOR CORRODED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL2348FB 257129 WHILE PERFORMING INSPECTION ON THE ELEVATORS, FOUND CORROSION ON THE UPPER AND THE LOWER LEADING EDGE SKIN SURFACES OF THE LT ELEVATOR. THE CORROSION WAS CONCENTRATED WHERE THE SKIN IS FASTENED TO THE ELEVATOR FRONT BEAM. AFTER REMOVING THE CORROSION AND BLENDING THE AREA, FOUND THAT TWO SIGNIFICANT AREAS WHERE THE CORROSION WENT BEYOND THE LIMITS OF THE SRM. DETERIORATION OVER TIME. 2L72 4F4 F A3EU E6WE 20030926001532003092600153WP 2003 9 26 ARWA20030808 120030823A5230 RETAINER DOUG DC8 DC863 302198AWP CARGO DOOR SEAL DAMAGED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19345JW 46042 MALFUNCTION OF PRESSURIZATION SYSTEM; CABIN CLIMB AT 2000 FT, A MIN UNABLE TO CONTROL. ADJUSTED SEAL RETAINER ON MAIN CARGO DOOR AT FORWARD LOWER AREA IAW MM 52-30-8. OPERATIONAL CHECK SYSTEM NORMAL IAW NASI FLOW CONTROL SYSTEM STC ST466CH. 2L74 4F 4A25 20030926001592003092600159NM 2003 9 26 CALA0300504 120030829A5310 DOOR FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A 7.5 INCH CRACK IN FORWARD BAGGAGE BIN WEB AT FORWARD LOWER DOOR JAMB, STA 440. A NEW SECTION OF WEB WAS INSTALLED IAW SRM 51-70-13. 2L72 4F RTA16WE 20030926001602003092600160NM 2003 9 26 CALA0300505 120030829A5321 FLOOR PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A 1 INCH AND .5000 INCH CRACK IN AFT BAGGAGE BIN FLOOR PANEL 1536X AT STA 794.5-807. A DOUBLER WAS INSTALLED AT EACH CRACK LOCATION IAW SRM 53-30-53. 2L72 4F RTA16WE 20030926001622003092600162NM 2003 9 26 CALA0300507 120030830A5320 BRACKET BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A .2500 INCH CRACK IN VHF RIGHT FORWARD SUPPORT AFT CARGO COMPARTMENT BRACKET AT STA 727D. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030929000092003092900009NM 2003 9 29 AWXA200301009 120030902A2613355604310 ELEMENT BOEING737 7373G7 1384595NM RT ENGINE DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28157AW 23779 AFTER TAKEOFF AT PHX EN ROUTE FOR TUS RT WING TO BODY LIGHT ILLUMINATED CONTINUOUSLY, FOLLOWED QRH PROCEDURES AND TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE STRUT DETECTOR ELEMENT (M488) IAW BMM 26-18-11 PG 401. RAN ENGINE, APU AND RT AIR CONDITIONING PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030929000142003092900014NM 2003 9 29 ABXA030345 120030903A2120 DUCT BOEING767 767281 1385109NM GE CF6 CF680A 30025NE AIR CONDITIONER OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 44 23146 MAINTENANCE COULD NOT OPEN R-2 WINDOW. FOUND WINDOW BINDING ON LOWER AC DUCT. ADJUSTED AND SECURED AC DUCT. WINDOW OPENED NORMALLY. 2L72 4F4 FRTA1NM E13NE 20030929000192003092900019NM 2003 9 29 751PA0022 120030903A3397 WIRE BOEING757 757200 1384950NM EMERGENCY LIGHT BROKEN A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 RED EMERGENCY FLOOR LIGHT BY L1 DOOR INOP. REPAIRED BROKEN WIRE AND REPLACED LENSE. OPS CHECKS OK. 2L72 4F RTA2NM 20030929000222003092900022NM 2003 9 29 03FDEA01410 120030902A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING I/B FLAP I/B DRIVE ARM ATTACHMENT BORE (FLAP SIDE) CORRODED. 2L73 4F RTA22WE 20030929000422003092900042NM 2003 9 29 03FDEA01402 120030902A3240 LINE DOUG MD11 MD11 3023602NM BRAKE LEAKING A FDEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO25582FE 48420 AT BLOCK IN NUMBER 5 BRAKE LINE BROKE AND HYD FLUID SPRAYED ONTO HOT BRAKE CAUSING A FLAME WHICH QUICKLY WENT OUT. MEL 31AUG03 19:05 LCK R ACN RELEASED FOR SERVICE PER MEL/CDL: 32-43-02 CATEGORY: C EXPIRATION: 10SEP03 "MEL 32-43-02: NR 5 BRAKE HYD LINE INOP. INSPECTED BRAKE AND TIRE, NO DAMAGE FOUND. A/C OK FOR SERVICE. FACT 01SEP03 01:01 JFK R REPLACED LINE AS PER SMP. LEAK CHECKED OK, BLEED NR 5 BRAKE AS PER MM 32-40-00-6. 2L73 4F RTA22WE 20030929000432003092900043NM 2003 9 29 03FDEA01403 120030903A2610 WARNING LIGHT BOEING727 727200 138407ENM COCKPIT FALSE ACTIVATIONA FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25478FE 21395 BOTH FIRE WARNING MASTER LIGHTS ON FORWARD GLARESHIELD ILLUMINATED TWICE FOR ABOUT 1 SECOND EACH TIME DURING CRUISE AT F270. MOMENTARY BELL WITH EACH ILLUMINATION. NO OTHER WARNINGS AND ALL ENGINE INSTRUMENTS NORMAL. FIRE TEST IN BOTH LOOPS OK BOTH INFIGHT AND ON GROUND. PERFORMED FIRE WARNING DETECTOR SYSTEM TEST PER MM 26-11-000-05. OPS CK NORMAL. ALSO INSPECTED E&E COMPARTMENT FOR SECURITY OF ENG FIRE PROTECTION CONTROLLER. FOUND OK. NO HISTORY FOR LAST 90 DAYS. OK FOR SERVICE. 2L73 4F RTA3WE 20040818000302004081800030EA 2004 8 18 A6WA200340057 120030419A21331037708 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31415AW 7593 EXPERIENCED RAPID DECOMPRESSION AT FL310, COMMENCED EMERGENCY DESCENT, WERE UNABLE TO REGAIN CONTROL OF PRESSURIZATION IN MANUAL MODE, DROPPED ALL PASSENGER OXYGEN MASKS. DEPLETED OXYGEN SUPPLY, CABIN ALTITUDE RWP. REMOVED AND REPLACED OUTFLOW VALVE. SHOP FINDINGS, FAULT NOT CONFIRMED BUT FAILED VISUAL, REJECTED FOR OVERSPRAY, CONTAMINATED DIAPHRAGM. REPLACED RETAINER, VALVE ASSEMBLY, DIAPHRAGM ASSY, FILTER AND GASKET. (M) 2L72 4F RTA21EA 20040802001272004080200127NE 2004 8 2 2004F00216 220030908A7250311856301 TURBINE BLADES BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GUUAE ENGINE SHUTDOWN E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO194954315385 UE181 114453 DURING LEFT ENGINE START AT APPROXIMATELY 30 PERCENT N1, A GRINDING NOISE WAS HEARD AND STRANGE VIBRATION FELT IN LEFT PROP LEVER. SHUT DOWN ENGINE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES FAILED. POWER SECTION HAS INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. CONFIRMED 2ND STAGE POWER TURBINE BLADE FAILURE. SUBSTANTIAL DAMAGE OCCURRED. FULL OVERHAUL OF POEWR SECTION REQUIRED. (M) 2L72 4T4 TRTA24CE E26NE 20040811000922004081100092NM 2004 8 11 DLM88040702 120031129A531059360381 BEAM DOUG MD88 MD88 3023688NM C2 DOOR FRAME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27939DL 49812 CORROSION ON C2 LOWER JAMB BEAM REPAIRED C2 LOWER DOOR JAMB BEAM PER SRM 53-05 FIG 63. TREATED AND PAINTED AREA PER DELTA SRM 51-10-30. 2L72 4F RTA6WE 20040813000832004081300083 2004 8 13 2004UALA00721 420031224A2565 O-RING BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BOTTLE FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29508UA 24744 LOW BOTTLE PRESSURE. BOTTLE TO VALVE O-RING WAS DETERIORATED. REPLACED CYLINDER ASSY. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. 2L72 4F4 FRTA2NM E17NE 20040813000962004081300096 2004 8 13 2004UALA00727 420031202A2565 INDICATOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE SLIDE BOTTLE DEFECTIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29941UA 26676 LOW BOTTLE PRESSURE. CAUSE WAS DEFECTIVE GAUGE. CORRECTIVE ACTION TAKEN WAS SLIDE BOTTLE REPLACED WITH NEWLY OVERHAULED BOTTLE AND ULTRASONIC LEAK DETECTION IMPLEMENTED FOR BOTTLE INSPECTION. 2L72 4F4 FRTA16WE E2GL 20040917000612004091700061NM 2004 9 17 2004F00327 120031229A3350CA72720CR BATTERY BOEING737 737231 1384079NM VENTRAL STAIRWAYINOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1154344 21631 FOUND EMERGENCY LIGHT OVER VENTRAL STAIRWAY INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY IAW BMM 33-50-00. (M) 2L72 4F RTA16WE 20040930001112004093000111WP 2004 9 30 WX0300027 120031204A56105912290506 WINDSHIELD DOUG DC9 DC983 3022083WP COCKPIT CRACKED A WXOAA UNSCHED LANDING O OTHER CLCLIMB 1 WP19891GA 49423 EN ROUTE FROM LAS TO DSM, THE FO'S WINDSHIELD CRACKED AFTER TAKEOFF. THE FLIGHT RETURNED TO LAS AND PERFORMED AN OVERWEIGHT LANDING. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD AND PERFORMED AN OVERWEIGHT LANDING INSPECTION. NO DISCREPANCIES WERE NOTED. A PRESSURE TEST AND OPS CHECK OF THE WINDSHIELD HEAT WERE ALSO PERFORMED WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20040719002522004071900252NE 2004 7 19 WRLA200329 220030919A7261815189 SCREEN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 3 ENG OIL FAILED A WRLAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA27275WA 48631 FOUND ENGINE NR 3 OIL TEMPERATURE HIGH ILLUMINATED IN FLIGHT. ENGINE WAS SHUTDOWN WHEN TEMPERATURE REACH 177 DEGREES. OIL TEMPERATURE HIGH ILLUMINATED FOR 4 MINUTES. AS PER 72-00-04 PAGE 610 TABLE 606, NO MAINTENANCE REQUIRED. REPLACED NR 3 MAIN OIL SCREEN, PRECAUTION. REMOVED AND REPLACED MAIN OIL SCREEN. (M) 2L73 4F4 FRTA22WE E24NE 20040722000152004072200015SW 2004 7 22 2004F00194 120030328A5230 DOOR FRCHLDSA227 SA227DC 3377521SW CARGO BAY OUT OF RIG A BSAAO OTHER J WARNING INDICATION CRCRUISE 1 NM051119K DC830B BIL - FLT 6014 - CARGO DOOR WARNING LIGHT CAME ON WHEN CABIN ALTITUDE WAS ADJUSTED DOWN TOWARD THE END OF CRUISE. CREW DESCENDED AND LANDED DESTINATION AIRPORT. CARGO DOOR CLOSING PROCEDURES, SWITCH RIGGING OR LATCH RIGGING. ADJUSTED BOTTOM FORWARD CLICKCLACK PER MM. DOOR OPS CHECK GOOD. (M) 2L72 4T RTA18SW 20040825002682004082500268EA 2004 8 25 2004F00248 120031219A274084898001 SENSOR CNDAIRCL600 CL6002C10 1390015EA HORIZONAL STAB MALFUNCTIONED A FDKAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW07505MJ1519 10070 FRL 6931 - FAT-PHX - THE AIRCRAFT HAD A STAB/MACH TRIM CAUTION MSG INFLIGHT IN CRUISE CONFIG. THE CREW CALLED INTO MAKE MAINTENANCE CONTROL AND DISPATCH AWARE OF THE PROBLEM. THE AIRCRAFT LANDED W/O ANY FURTHER PROBLEMS AND MX CONTROL GROUNDED THE AIRCRAFT UNTIL THE PROBLEM IS FIXED. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER POSITION SENSOR AND RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4F RTA21EA 20040825002632004082500263NE 2004 8 25 2004F00243 220031027A7261 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE NR 3 MALFUNCTIONED A PCSAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO17794AJ 21243 FLT 813 - KMIA-TBPB - AFTER DEPARTURE FORM KMIA, NR 3 OIL PRESSURE INDICATED ABOVE ARC LINE, AND THEN OIL TEMP BEGAN CLIMBING AND WENT ABOVE ARC LINE. SHUT OFF NR 3 ENGINE AS PER PROCEDURES. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 3 ENGINE OIL OVER SERVICED. DRAINED OIL SYSTEM AND REMOVED OIL FILTER. INSPECTED FILTER AND FOUND NO CONTAMINATION. REPLENISHED OIL TANK WITH 19 QTS PER MM 12-13-1 AND 79-00 PAGE 301. RAN ENGINE AT TAKEOFF POWER FOR FIVE MINUTES. OIL TEMP STAYED 85 DEGREES OIL PRESSURE AT 55 PSI. ALSO, RAN ENGINE AT DIFFERENT POWER SETTINGS OIL PARAMETERS WITHIN LIMITS. CHECKED OPERATIONAL OF FUEL HEAT VALVE AT 1.4 EPR. VALVE OPERATION NORMAL 2L73 4F4 F A3WE E2EA 20040902001432004090200143SO 2004 9 2 2004F00254 120031015A24204111810 ALTERNATOR PIPER PA32 PA32260 7103206SO ENGINE FAILED A XP6AO OTHER O OTHER NRNOT REPORTED 1 SO331061Q 327200015 WHILE EN ROUTE ILM-JQF, FLIGHT 'RACE CITY' HAD AN ALTERNATOR FAILURE. THE PILOT DIVERTED TO FAY. A MECHANIC WAS DISPTACHED. ON INSPECTION IT WAS FOUND THAT THE ALTERNATOR ITSELF FAILED. A NEW ALTERNATOR WAS INSTALLED, THE ENGINE GROUND RAN, NEW ALTERNATOR SOLVED PROBLEM, SYSTEM SHOWED A CHARGE AT 14.5 V. AIRCRAFT RETURNED TO SERVICE. (M) 1L71 3O A3SO 20040902001612004090200161NM 2004 9 2 MEX2003575 120031230A2420696233B CSD DOUG MD80 MD83 3023681NM LT ENGINE FAILED A ASMFA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW23831LF 53050 FLT 610 - CUN-ATL - AIRCRAFT RETURNED AFTER APPROXIMATELY 30 MINUTES, DU TO THAT THE LEFT CONSTANT SPPED DRIVE REACHED THE HIGH TEMPERATURE RANGE AND THE RT GENERATOR WAS PREVIOUSLY DEFERRED BY MEL CAT B. CAPTAIN DISENGAGED THE CSD AND PERFORMED THE ABNORMAL PROCEDURE. AT PLATFORM, THE SYSTEM WAS TESTED. THE RT GENERATOR AND GCU AND THE LT CSD, GENERATOR AND HEAT EXCHANGER WERE REPLACED AND SYSTEM WAS TESTED IAW MM 24-10-01, 24-10-03, 24-20-01 AND 24-20-07, ALL CORRECT. (M) 2L72 4F RT 20040902001402004090200140NM 2004 9 2 2004F00251 120031220A3397 WIRE BOEING757 757231 1384950NM EMERGENCY LIGHT DAMAGED A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11708TW 28480 EMERGENCY LIGHTS FORWARD FLOOR LIGHT STRIPS INOPERATIVE. REPAIRED WIRING AT SEAT ROW 5 IAW BMM. OPS CHECKED GOOD. (M) 2L72 4F RTA2NM 20040902001422004090200142EU 2004 9 2 2004F00253 120030301A2932501310000 TRANSDUCER AIRBUS320 A320233 3930329EU HYD PRESSURE INOPERATIVE A SOKFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO23462TA 1334 SJO - FLT 640 - DURING CLIMB, THE CAPTAIN REPORTED THAT NR 2 ENGINE HYD PUMP FAILED. THE AIRCRAFT RETURNED TO SJO STATION. AT SJO, NR 2 ENGINE HYDRAULIC PUMP WAS REMOVED AND REPLACED IAW AMM 29-13-31, BUT IT WAS FOUND THE HYDRAULIC PRESSURE TRANSDUCER INOPERATIVE P/N 50-1-31-00-00. DUE LACK OF PARTS WAS INCLUDED AS WCC 2003-58116, DD SHEET 16/2003, ITEM 3, MEL REF 29-30-04, ITEM 4B. PERFORMED OVERWEIGHT LANDING INSPECTION PROCEDURE IAW A/C TSM 05-50-00-810-802 FOUND OK, AND THE AIRCRAFT RETUEND TO SERVICE. (M) 2L72 4F RTA28NM 20040913001032004091300103CE 2004 9 13 JEM2004F00007 120030828A551145A21146005 RIB BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01400FT2961 RK101 DURING A SCHEDULED INSPECTION OF THE HORIZ STAB ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE RIB AS WELL THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND INSERTING INTO THE HORIZ STABILIZER DRAIN HOLES NEAR THE SIDE ROLLER SUPPORT BRACKETS. THE RIB CRACK WAS NOT FOUND UNTIL THE ROLLER BRACKET WAS COMPLETELY REMOVED. THE FOLLOWING PARTS WERE CHANGED DUE TO CRACKS: RIB PN 45A21146005, BRACKETS PN 45A21086004, AND 45A21085004. ACTT:2961. 2H72 4F4 FRTA16SW E25EA 20040913001482004091300148NM 2004 9 13 0704004 120030907A5315 FLOORBEAM BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 ANGLE CRACKED RBL 24 AT FLOORBEAM. 2L72 4F4 F A16WE E2EA 20040913000022004091300002NM 2004 9 13 2004F00291 120031224A3610BACC10DU450 CLAMP BOEING727 727233 138408ANM NR 3 ENGINE LOOSE A PCSAJA DUMP FUEL UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO17994AJ 20942 FLT 829 - TTPP-SYCJ, FLIGHT CREW REPORTED, OVERHEAT ENGINE STRUT 3 ILLUMINATED AFTER TAKEOFF, JETTISONED FUEL, 9000 LBS. FLIGHT CREW DIVERTED AIRCRAFT BACK TO TTPP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING AND INSPECTION REVEALED AN PNEUMATIC LEAK. THE PNEUMATIC LEAK WAS A RESULT OF A LOOSE CLAMP AT THE NR 3 ENGINE 13TH STAGE DUCT. MAINTENACE REPOSTIONED AND TIGHTENED THE 13TH STAGE DUCT CLAMP. MAINTENANCE RAN ENGINE FOR FIVE MINUTES AT 1.4 SETTING. OPS CHECKED NORMAL, NO LEAKS NOTED AND LIGHT REMAINED OFF AT GROUND POWER RUN IAW 70-00-0. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20050202000582005020200058NM 2005 2 2 0704019 120031006A575365ND719023 ACCESS PANEL BOEING737 737230C 1384472NM LT WING TE FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW9992 9992 20257 LT WING TE MID FLAP ACCESS PANEL CRACKED AT WBL 127. 2L72 4F A16WE 20050202001142005020200114NM 2005 2 2 0704016 120030914A5511 RIB BOEING737 737230C 1384472NM HORIZONTAL STAB CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 RIB CRACKED RT HORIZ STAB LE STA 109. 2L72 4F A16WE 20050202000592005020200059NM 2005 2 2 0704013 120031010A531265C3785247 BULKHEAD BOEING737 737230C 1384472NM FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 NUMEROUS CRACKS AT FWD PRESSURE BULKHEAD BS 178. 2L72 4F A16WE 20050202000532005020200053NM 2005 2 2 0704003 120030907A5320 ANGLE BOEING737 737230C 1384472NM FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 ANGLE CRACKED AT BS 727B LBL 24 FLOORBEAM. 2L72 4F A16WE 20050208001722005020800172NM 2005 2 8 DLM90050062 120030126A3244 TIRE DOUG MD90 MD9030 3023690NM NR 1 MLG FAILED A DALAO OTHER C F.O.D. LDLANDING 1 SO27903DA 53383 UPON ARRIVAL INTO SLC TOWER INFORMED CAPTAIN THERE WAS SMOKE FROM NR 1 GEAR. FOUND NR 2 AND NR 3 TIRES BLOWN. LEFT AFT INBOARD FLAP DAMAGED. REPLACED NR 2 AND NR 3 MAIN WHEEL ASSEMBLIES. AFT FLAP REPAIRED. NO DAMAGE FOUND IN NR 1 ENGINE. 2L72 4F RTA6WE 20050222001062005022200106EU 2005 2 22 HAEA00115 120030930A7110 COWLING AMD FALC20FALCON 2720302EU RT NACELLE DEPARTED E HAEAO OTHER D INFLIGHT SEPARATION DEDESCENT 1 SW05165TW1294412944 65 PILOT REPORTED, UPON POST FLIGHT INSPECTION RT LOWER OUTBOARD ENGINE COWLING GONE. WILL UPDATE AFTER MAINTENANCE. COWLINGS REPLACED AND AIRCRAFT MOVED TO BASE FOR ENGINE INSPECTION. COWLING LOST IN FLIGHT. 2L72 4F A7EU 20050223001122005022300112EU 2005 2 23 ERAA097529 120030813A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM SHORTED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03130EH 558 GUIDE ASSY IS SHORTED, HAS BROKEN SOCKET. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 REM 405. 1G72 3U H3EU 20050222002182005022200218 2005 2 22 ERAA097080 420030326A25624530190 ELT BOLKMS105 BO105A EU CABIN CRACKED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH2054 S675 SUB ASSEMBLY, TOP COVER CRACKED. REPLACE BATTERY, SUB ASSEMBLY, TOP COVER. TESTED IAW ARTEX PROCEDURES 4128,4129,4130. 1G72 3U H3EU 20041108000812004110800081SO 2004 11 8 RAIA00409006 120030910A5270 WARNING SWITCH EMB 145 EMB145LR 3260212SO CARGO DOOR OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03839HK 14500829 STL - MAIN CARGO DOOR WARNING LIGHT CAME ON IN FLIGHT. MAINTENANCE DEFERRED MAIN CARGO DOOR WARNING SYSTEM PER MEL. CLEARED DMI. ADJUSTED BAGGAGE DOOR WARNING SWITCHES. 2L72 4T RTT00011AT 20040910000642004091000064WP 2004 9 10 2004F00290 220031211A732039423091 SHUTOFF VALVE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33110UG 01514WP LT ENGINE FAILED A FJTAO OTHER J WARNING INDICATION APAPPROACH 1 SO03862JX 862 CREW REPORTED ON REPOSITION FLIGHT FROM MIV TO ACY, WHILE BEING VECTORED TO APPROACH IN HEAVY TURBULENCE AND RAIN THE LEFT ENGINE EXPERIENCED A LOSS OF POWER. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. UPON INVESTIGATION MAINTENANCE PERSONNEL REPLACED THE ENGINE FUEL SHUTOFF VALVE, ENGINE GROUND RUNS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 20040913000962004091300096CE 2004 9 13 CWQ2004F00011 120031107A5753 BOLT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE FLAP ACTUATOR BROKEN B CWQRK NONE O OTHER ININSP/MAINT 1 GL05372QS3887 537 5600372 DURING PHASE 1-4 INSP, FOUND RT FLAP ACTUATOR TO HAVE THE CYLINDER TO ATTACH BASE BOLT HEAD SHEARED OFF. THE HEAD OF THE BOLT WAS STILL ATTACHED TO THE SAFTEY WIRE (THE ACTUATOR WAS NOT LEAKING AND STILL WORKING). IT APPEARS THAT THE BOLT HAD BEEN BROKEN FOR A WHILE, DUE TO THE DIRT AND GRIME AROUND AREA. THIS IS NOT THE FIRST TIME WE HAVE SEEN THIS ON THE FLAP ACTUATOR, AT LEAST TWO OTHERS THAT WE HAVE FOUND. 2L72 4F4 FRTA22CE E25EA 20041229002062004122900206 2004 12 29 2004UALA01178 420031201A2565 ASPIRATOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE ESCAPE SLIDE CRUSHED A UALAK NONE O OTHER ININSP/MAINT 1 WP29195UA 26899 BOTH ASPIRATORS WERE CRUSHED DURING THE PACKING PROCEDURE OF THE PREVIOUS OVERHAUL. ASPIRATOR DAMAGE LIKELY CAUSED BY EXCESSIVE PRESSURE APPLIED DURING THE PREVIOUS PACKING PROCESS. NO INDICATIONS OF SHIPPING DAMAGE. BOTH ASPIRATORS WERE REPLACED. 2L74 4F4 FRTA20WE E24NE 20050330000512005033000051 2005 3 30 KBM2005F00029 420031227A34225050031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT MALFUNCTIONED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19966SH 3787 DG, FLAG REMAINS OFF, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050202001112005020200111NM 2005 2 2 0704002 120030914A5320 INTERCOSTAL BOEING737 737230C 1384472NM FUSELAGE CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 INTERCOSTAL CORRODED BETWEEN BS727A-727B AT S25L-26L. 2L72 4F A16WE 20050202001122005020200112NM 2005 2 2 0704005 120030914A5320 FLOOR SUPPORT BOEING737 737230C 1384472NM FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 FLOOR SUPPORT ANGLE CRACKED BS 947.5 RBL16. 2L72 4F A16WE 20050202001172005020200117NM 2005 2 2 0704023 120031009A5753657994910 CARRIAGE BOEING737 737230C 1384472NM TE FLAP CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 RT OUTBD FLAP OUTBD CARRIAGE SPINDLE CORROSION AROUND BOLT HOLE. 2L72 4F A16WE 20050202000552005020200055NM 2005 2 2 0704012 120030929A5320 INTERCOSTAL BOEING737 737230C 1384472NM FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 INTERCOSTAL CRACKED BS 178-188 AT WL 195 L/R. 2L72 4F A16WE 20050202001132005020200113NM 2005 2 2 0704009 120031003A5315 SPLICE PLATE BOEING737 737230C 1384472NM FLOORBEAM CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 SPLICE PLATE CRACKED BS 540 AT S21L-S22L. 2L72 4F A16WE 20050222000252005022200025EU 2005 2 22 HAEA00114 120030922A5210 LATCH AMD FALC20FALCONE 2720305EU CABIN DOOR LEAKING E HAEAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW05285TW 285 PILOT REPORTED SEMI- RAPID DECOMPRESSION AT FL290 SIMULTANEOUSLY WITH DOOR LIGHT, AFTER RAPID DESCENT WAS INITIATED TO 10,000FT, AFTER APPROX 7 OR 8 MINUTES THE CABIN BEGAN PRESSURIZING. AIRCRAFT WAS DIVERTED TO ADS FOR MAINTENANCE. WILL UPDATE REPORT AFTER MAINTENANCE. RIGGED DOOR LATCH AND SWITCHES ON CARGO DOOR IAW AVDOOR MANUAL. 2L72 4F A7EU 20050222001172005022200117SW 2005 2 22 AC2A096515 120030926A33501000553 HOUSING BELL 430 430 1182150SW LIGHT BROKEN B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CH 49037 HOUSING IS BROKEN. LIGHT ASSEMBLY WILL NOT TEST. THE CHARGER IS INOPERATIVE. REPLACED ASSEMBLY. UNIT IS NOT ECONOMICALLY FEASIBLE TO REPAIR. 1G72 3U RTH9SW 20050222001982005022200198 2005 2 22 ERAA096635 420030801A2562ELT1106 BATTERY BELL 412 412 1182202SW ELT INOPERATIVE B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH 33004 ELT GOES OFF CONSTANTLY, BATTERY HAS BEEN DISCONNECTED. SENT TO ARTEX FOR REPAIR. COULD NOT DUPLICATE, CHECKED MOUNTING ANGLE, SHOULD BE HORIZONTAL. REPLACED BATTERY, EXPIRED. TESTED IAW ARTEX PROCEDURES, REPLACED BATTERY PACK. 1G72 4U H4SW 20050223001192005022300119EU 2005 2 23 ERAA097536 120031230A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM INOPERATIVE E ERAAK NONE O OTHER NRNOT REPORTED 1 AL03124EH S559 GUIDE ASSY INOPERABLE ACTION TAKEN: DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, POTTED AND TESTED. INSPETED AND REPAIRED IAW MBB BO105 REM 405. 1G72 3U H3EU 20040913001442004091300144NM 2004 9 13 0704006 120030907A5320 FLOOR SUPPORT BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70582 20257 FLOOR SUPPORT ANGLE CORRODED BS 947.5 LBL33. 2L72 4F4 F A16WE E2EA 20040913001462004091300146NM 2004 9 13 0704024 120030929A5753655224714 ATTACH FITTING BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE TE FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 RT IB FLAP IB TORQUE TUBE ATTACH FITTING CRACKED. 2L72 4F4 F A16WE E2EA 20040722000182004072200018SW 2004 7 22 2004F00196 120030317A3232 PLUNGER FRCHLDSA227 SA227DC 3377521SW ACTUATOR STUCK A BSAAO OTHER J WARNING INDICATION CRCRUISE 1 NM05853LS DC853B FLT 6016 - MSO - CARGO DOOR WARNING LIGHT CAME ON DURING CRUISE AT FL210. CREW FOLLOWED CHECKLIST PROCEDURES, WHEN PRESSURIZATION WAS 0 PSID, THE CARGO DOOR LIGHT WENT OUT. CARGO DOOR CLOSING PROCEDURES, MICROSWITCH RIGGING OR LATCH RIGGING. FOUND ONE CARGO DOOR WARNING ACTUATOR STICKING. CLEANED AND LUBED ALL CARGO DOOR WARNING SWITCH ACTUATOR PLUNGERS AND CLICK CLACKS. DOOR OPS CHECK GOOD. (M) 2L72 4T RTA18SW 20040930001332004093000133NE 2004 9 30 2004F00384 220031214A731437820112 PUMP BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE NR 1 ENGINE FUELFAILED A FX7AJA DUMP FUEL UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO1979749 22451 DURING INITIAL CLIMB ENGINE NR 1 FAILED, FLAMED OUT, DUMPED FUEL AND RETURNED TO KMIA WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER MM 73-11-01. OPS CHECK GOOD, A/C RETURNED TO SERVICE NO FURTHER INCIDENTS. (M) 2L73 4F4 F A3WE E2EA 20040721000442004072100044NE 2004 7 21 AALA20030827 220030802A732076960612 FUEL CONTROL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT ENGINE FAILED A AALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW21262AA 49290 EWR - FLT 1005 - LGA-TPA - DURING CLIMB-OUT AT ABOUT 16,000 FEET RIGHT ENGINE SHUT DOWN WITH NO INDICATION OF VIBRATION OR DAMAGE. AIRCRAFT DIVERTED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20040825002652004082500265NM 2004 8 25 2004F00245 120031117A7500593764 VALVE BOEING727 727233 138408ANM NR 3 ENGINE FAILED A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17495AJ 20937 FLT 811 - KMIA-TBPB, DURING LEVEL CRUISE, NR 3 ENGINE BEGAN TO SURGE AND ALL ENGINE INDICATORS FLUCTUATED. NR 3 ENGINE WAS SHUTDOWN FOR PRECAUTIONS. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTEANCNE REMOVED AND REPLACED NR 3 ENGINE PRBC VALVE IAW B727 MM 75-31-11. OPS CHECKED GOOD IAW PWA MM 73-00. PERFORMED ENGINE RUN PER AMJ FORM B-41 AND PWA MM 71-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040825002622004082500262EU 2004 8 25 2004F00242 120031002A5320 INTERCOSTAL AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, OFUND AFT CARGO COMPARTMENT FLOOR INTERCOSTAL CORRODED AT FRAME 54 AND RBL 17. REMOVED CORROSION FROM INTERCOSTAL AT FRAME 54, RBL 17. NO MEASUREABLE MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M) 2L72 4F RTA28NM 20040830001972004083000197EU 2004 8 30 00108 120030902A21300000 SWITCH AMD FALC20FALCON 2720302EU COCKPIT ACTIVE E HAEAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW05158TW1106311063 158 PILOT REPORTED THAT THE AIRCRAFT LOST CABIN PRESSURE AND REQUESTED EMERGENCY DECENT, AFTER DECENT THE CREW NOTED THAT THE DUMP VALVE WAS IN DUMP POSTION, RESET SWITCH TO NORMAL POSTION AND CABIN BEGAN PRESSURIZE. NO MAINTENANCE REQUIRED.(CLOSED) 2L72 4F A7EU 20040902001452004090200145NM 2004 9 2 C7WA200300049 120031114A7710M3902932260 PIN BOEING727 7272J7 138400ENM CONNECTOR BROKEN A C7WAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO17128NA 20879 REJECTED TAKEOFF, NR 3 EPR UNRELIABLE AT TAKEOFF POWER READS LOW. SEEMS TO READ NORMAL AT CRUISE POWER. FOUND WIRE NOT CONNECTED TO PIN NR 3 AT EPR GAUGE CANNON PLUG. INSTALLED NEW PIN AND RECONNECTED WIRE IAW WIRING STANDARD PRACTICE CH 20 EPR READS NORMAL IAW MM 77-11-00. (M) 2L73 4F A3WE 20040902001512004090200151WP 2004 9 2 2004F00257 220031211A732039423091 SHUTOFF VALVE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LT ENGINE MALFUNCTIONED A FJTAO OTHER J WARNING INDICATION APAPPROACH 1 SO03862JX 862 CREW REPORTED ON REPOSITION FLIGHT FROM MIV TO ACY, WHILE BEING VECTORED TO APPROACH IN HEAVY TURBULENCE AND RAIN, THE LEFT ENGINE EXPERIENCED A LOSS OF POWER. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. UPON INVESTIGATION MAINTENANCE PERSONNEL REPLACED THE ENGINE FUEL SHUTOFF VALVE, ENGINE GROUND RUNS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 20040902001572004090200157NM 2004 9 2 2004F00260 120031212A5297W34200820 WIRE BOEING727 7272J0 138407ENM AFT AIRSTAIR BROKEN A P9RAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11910PG 22606 DEPARTING SJU, ON TAKEOFF ROLL, AFT AIRSTAIR LIGHT CAME ON. EXITED RUNWAY AND CYCLED AIRSTAIRS AND THE LIGHT EXTINGUISHED. CONTACTED DISPATCH FOR NEW RELEASE AND PROCEEDED NORMALLY. DURING FLIGHT TO SFB, LIGHT ON AFT AIRSTAIR BEGAN FLICKERING AND THEN REMAINED ON. UPON LANDING, VISUALLY CHECKED AIRSTAIR AND PROCEEDED TO GATE. REPAIRED BROKEN WIRE AT AFT AIRSTAIR SWITCH. SYSTEM CHECKED NORMAL IAW BMM 52-62. (M) 2L73 4F RTA3WE 20040902001982004090200198NM 2004 9 2 MEX2003573 120031230A7603 THROTTLE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE LACK OF LUBE A ASMFD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 SW23945AS 49643 P725488D AIRCRAFT RETURNED TO PLATFORM, DUE TO SLOW ACCELERATION IN THE RIGHT ENGINE. THE WATER SUMP WAS DRAINED AND THE THROTTLE CHAMBER WAS LUBRICATED IAW MM 73-20-03. AT OVERNIGHT SERVICE IN MEX, PERFORMED A TRIM TO BOTH ENGINES AND AN ACCELERTION TEST IAW MM 71-00-00, PARAMETERS WITHIN LIMITS. (M) 2L72 4F4 FRT E9NE 20040902001582004090200158NM 2004 9 2 2004F00261 120031213A527069209852 UPLOCK SENSOR BOEING727 727200 138407ENM AFT AIRSTAIR OUT OF ADJUST A P9RAO OTHER N FALSE WARNING CRCRUISE 1 SO11910PG 22606 SFB-SYR - AMBER AFT AIRSTAIR DOOR WARNING LIGHT ON FLIGHT ENGINEERS PANEL ILLUMINATED. CONTINUED FLIGHT WITHOUT INCIDENT. ADJUSTED AFT AIRSTAIR UPLOCK SWITCH PER B727 MM 52-62-01. ACCOMPLISHED TESTE OF AIRSTAIRS IAW B727 MM 52-62-01. TESTED NORMAL. (M) 2L73 4F RTA3WE 20040907000012004090700001 2004 9 7 SWAA032760 420031218A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29073SW 22673 INADVERTANT DEPLOYMENT OF L2 DOOR EVACUATION SLIDE BY CLEANING CREW. REMOVED AND REPLACED L2 DOOR EVACUATION SLIDE PER MM. 2L72 4F A16WE 20040916000022004091600002NE 2004 9 16 Y2PA03015 220030708A7230 STUD AMD FALC20FALCON 2720302EU GE CF700 CF7002D 30010NE ENG COMPRESS SHEARED A Y2PAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL23827AA 298 245U419 NR 1 ENG FLAMED-OUT AT 32,000 FT, AIRSPEED 64 CLEAR NO TURBULENCE, -20 DEGREES CELSIUS, NR 1 EPR AND NR 1 FUEL FLOW ERRATIC DURING CLIMB. CREW DESCENDED TO FL300 & RESTARTED. RE-LIGHT OK, BUT FAN SPEED FLUCT 80-30 PERCENT. PERFORMED PRECAUTION SHUTDOWN. A/C DIVERTED & LANDED WITHOUT FURTHER INCIDENT. POST INSPECT OF ENG FOR FOD, NONE FOUND. NR 1 ENG INSPECTED IAW GE MM & AIRLINES GMM, NO DEFECTS. ENGINE RUN PERFORMED, NO DEFECTS OTHER THAN FAN SPEED IND PROBLEM. A/C RETURNED TO MX BASE FOR EVAL. EVAL ON PYLON, GAVE NO IND OF CAUSE OF FLAMEOUT. ROTATING COMPRESSOR DETERMINED 1 OR MORE COMPRESSOR STUDS MAY HAVE SHEARED DUE TO NOISE HEARD DURING ROTATION. ENG REMOVED FOR TEARDOWN & FURTHER EVAL. (M) 2L72 4F4 F A7EU E7EA 20040917000132004091700013 2004 9 17 WX0300025 420031228A256529982113 SLIDE DOUG DC9 DC983 3022083WP PAX DOOR DEPLOYED A WXOAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 WP19862GA 49556 IN PREPARATION FOR DEPARTURE FROM CZM, THE CAPT GAVE THE OK TO CLOSE DOORS. DOORS CLOSED AND THE SLIDES ARMED AND THE CAPTAIN WAS NOTIFIED ACCORDINGLY. AS THE LEAD FLIGHT ATTENDANT WAS PREPARING TO DO THE SAFETY BRIEFING, THE COCKPIT DOOR OPENED AND THE FIRST OFFICER EXITED THE FLIGHT DECK. INFORMED THE LEAD FLIGHT ATTENDANT THAT THERE WAS A PROBLEM WITH THE L1 DOOR. BEFORE THE LEAD FLIGHT ATTENDANT COULD REMIND THE FIRST OFFICER THAT THE DOOR WAS ARMED, HE OPENED THE DOOR. THE EMERGENCY SLIDE DEPLOYED. CONTRACT MX REPLACED THE SLIDE IAW AMM 25-62-00. RII WAS PERFORMED BY AN ALLEGIANT RII AUTHORIZED MECH WHO WAS TRANSPORTED TO CZM WITH THE REPLACEMENT SLIDE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20040930001322004093000132EU 2004 9 30 2004F00383 120031002A5320 INTERCOSTAL AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, OFUND AFT CARGO FLOOR INTERCOSTAL IS CORRODED AT FRAME 56 AND RBL 22-24. REMOVED CORROSION FROM INTERCOSAL AT FRAME 56, RBL 22-24. NO MEASUREABLE MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M) 2L72 4F RTA28NM 20041108001172004110800117CE 2004 11 8 05272003 120030527A55316231270 RIB CESSNA650 650 2076802CE VERTICAL STAB CRACKED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23384CW 6500144 WHILE INVESTIGATING A SUSPECTED WATER LEAK IN THE BAGGAGE COMPARTMENT MAINTENANCE DISCOVERED AN APPROXIMATELY 2.5 CRACK IN THE RIGHT LOWER VERT STAB LEADING EDGE SKIN P/N 6231276 AT APPROXIMATELY WL 160. AFTER REMOVING SKIN FOR REPLACEMENT IT WAS DISCOVERED THAT RIB P/N 6231270-28 HAD AN APPROX 2.5 CRACK IN THE SAME LOCATION AS THE OVERLYING SKIN. AFTER REMOVAL OF THE RIB, IT WAS DISCOVERED THAT THE 2 MOST FORWARD FASTENER HOLES ON THE RIGHT FLANGE OF THE RIB WERE NOT DRILLED AS THEY WERE ON THE OPPOSITE FLANGE OF THE RIB. IT IS SUSPECTED THAT DUE TO THE LACK OF THESE TWO FASTENERS THE RIB FLANGE WAS SUBJECT TO IMPROPER STRESS DISTRIBUTION CAUSING A DEFECT IN THE OVERLYING SKIN. THIS HAS OCCURRED ON 2 OTHER2L72 4F A9NM 20041108001202004110800120CE 2004 11 8 6262003 120030626A3246GYS186C21 BOLT BEECH MU300 400A 1155402CE WHEEL FAILED E DJFAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA23418CW RK18 AIRCRAFT HAD (L) MAIN TIRE FAILURE APPROXIMATELY 1000 FT INTO TAKEOFF ROLL. AIRCRAFT STOPPED SAFELY WITH NO INJURIES. FURTHER INVESTIGATION RESULTED IN FINDINGS OF FOUR (4) WHEEL BOLTS WERE LOOSE AND ONE (1) BOLT SHEARED. THIS IS THE FIFTH (5TH) OCCURANCE OF TRHIS TYPE IN THE PRECEEDING SIXTH (60) DAYS. THE BOLT P/N IS GYS186-C21, THE NUT P/N IS GYN186. 2H72 4F RTA16SW 20050816000802005081600080NM 2005 8 16 SWAA032400 120031030A53116546500 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND 5 EA FUSELAGE FRAMES CRACKED AT STR 9R, BS 747, BS 767, BS 807, BS 827 AND BS 907. REPAIRED FRAMES PER BFG ER. 2L72 4F RTA16WE 20050817000022005081700002NE 2005 8 17 MZZA0300001 220030330A7200 ENGINE BOEING737 737823 13844BZNM CFMINTCFM56 CFM567B26US NE NR 1 FAILED A MZZAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP1314235 28947 874299 THE NR 1 ENGINE FAILED DURING STABLE CRUISE AT FL 380 WHILE ENROUTE. THE HIGHEST EGT OBSERVED WAS 890 DEGREES AND N1 WENT TO 24 PERCENT. THE AIRCRAFT WAS DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. THE ENGINE FAILURE WAS REPORTED TO BE AN UNCOMMANDED SHUTDOWN. INITIAL ENGINE EXAMINATION FOUND MANY BLADES MISSING FROM FAN AND TURBINE WHEEL. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFO PENDING INVESTIGATION. (K) 2L72 4F4 FRTA16WE E00055EN 20050816002152005081600215NM 2005 8 16 MZZA0300005 120031214A5210 SKIN BOEING737 737823 13844BZNM L1 DOOR DENTED A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314240 28952 INSPECTION FOUND L-1 ENTRY DOOR REPAIR AT UPPER AFT CORNER BENT ON AFT EDGE. REMOVED EXISTING REPAIR AND REINSTALLED EXTERNAL DOUBLER IAW ECRA. (K) 2L72 4F RTA16WE 20051110000572005111000057NE 2005 11 10 0075156 320030520A61117725367 BEARING HAMSTD AEROSPATR72 ATR72 EU HAMSTD14SF 14SF* NE PROP BLADE CORRODED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 854971 854971 CORROSION ON BEARING BLADE PIN. 2H72 4T RT 6 CP7NE 20060104000982006010400098CE 2006 1 4 57174 120031218A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT TORQUE FAILED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07144ZV1604116041 UE144 AFTER TAXING OUT FROM GATE. CREW NOTED LT TORQUE INDICATOR WENT TO ZERO ON INITIAL SPOOL UP FOR TAKEOFF. CREW THEN RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE INDICATOR. 2L72 4T4 TRTA24CE E26NE 20060731000202006073100020WP 2006 7 31 IXXA060504S 120030122A5230 STRUCTURE DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND AFT PIT BASKET DOOR ATTACHMENT HOLE CRACKED. REMOVED DAMAGE, FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER AND FILLER, IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060731000552006073100055WP 2006 7 31 IXXA060506S 120030122A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE OUT BOARD SKIN SPLICE REPAIR, OUTER SKIN CRACKED. REMOVED EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 57-2-1, 51-1-8, 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20060731000192006073100019WP 2006 7 31 IXXA060503S 120030122A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK FOUND A SEAT TRACK GOUGED AT STATION 275 RBL 45.5. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS.IAW DC8 SRM 53-2-3, 51-1-8, AND 53-2-3. 2L74 4F RT4A25 20060801000172006080100017WP 2006 8 1 IXXA060512S 120030121A5210 FITTING DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND FITTING CRACKED ON INSIDE OF L1 DOOR UPPER AFT EDGE, BACK SIDE OF DOOR STOP. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1-21D. 2L74 4F RT4A25 20060801000282006080100028WP 2006 8 1 IXXA060515S 120030121A5720 WEB DOUG DC8 DC871F 302199DWP ZONE 500 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND LEFT MAIN LANDING GREA STRUT CUTOUT AFT VERTICAL WEB GOUGED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-21, 51-1-8, AND DOUGLAS DRAWING 5651221. 2L74 4F RT4A25 20060801000382006080100038WP 2006 8 1 IXXA060522S 120030914A7830 HINGE DOUG DC8 DC871F 302199DWP NR 2 ENG T/R ELONGATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND THE NR 2 ENGINE INBOARD THRUST REVERSER, FORWARD HINGE HAS AN ELONGATED HOLE. THE HOLE WAS REAMED TO ROUND AND TRUE, MANUFACTURED BUSHING AND INSTALLED TO RESTORE HINGE TO ORIGINAL DIMENSIONS IAW TIMCO REPAIR ENGINEERING ORDER, REO-G09483. 2L74 4F RT4A25 20060801000432006080100043WP 2006 8 1 IXXA060525S 120030917A5314 KEELBEAM DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND KEEL BEAM ATTACH ANGLE CRACKED AT HINGE FASTENER HOLE. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW ANGLE. IAW DC8 SRM 51-1-20D, 51-1-8, AND DOUGLAS DRAWING 5616306. 2L74 4F RT4A25 20060801000462006080100046WP 2006 8 1 IXXA060527S 120030912A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND INTERCOSTAL A HOLE IN THE RADIUS AT STATION 1390 ABOVE LONGERON 28 LEFT. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-21A, 51-1-21D, 51-1-8, AND DOUGLAS DRAWING 5750771. 2L74 4F RT4A25 20041108001402004110800140NE 2004 11 8 DJFA200300003 220031018A73206047T74P13 FUEL CONTROL CNDAIRCL600 CL6001A11 1900302EA GE CF34 CF343A 30015NE NR 2 ENGINE MALFUNCTIONED E DJFABA EMER. DESCENT UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA23602CW 3002 350102 AT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESENDED AND AT FLIGHT LEVEL 100 FT, WAS ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FURTHER PROBLEMS. 2L72 4F4 FRTA21EA E15NE 20050321000532005032100053WP 2005 3 21 IXXA0500019O 120030315A32004771392501 PIN DOUG DC8 DC873F 302199FWP MLG BROKEN A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11603AL942772366 46003 AFTER TAKEOFF WHEN GEAR WAS RAISED THE DOORS NOT LATCHED LIGHT, GEAR NOT LATCHED LIGHT AND SECONDARY RIGHT DOOR LIGHT STAYED ILLUMINATED. RECYCLED LANDING GEAR. GEAR DOWN INDICATIONS NORMAL RIGHT GEAR SEEMED TO INDICATE DOWN VERY QUICKLY. GEAR WAS RAISED WITH SAME INDICATIONS AS BEFORE. FLIGHT WAS CONTINUED USING GEAR EXTENED PROCEDURES. CREW LANDED AIRCRAFT AT HKJK WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT MAIN LANDING GEAR AND FOUND RETRACT PIN BROKEN. REMOVED AND REPLACED PIN PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050817000012005081700001NM 2005 8 17 MZZA0300002 120030417A5241 GUST LOCK BOEING737 737823 13844BZNM L2 DOOR BROKEN A MZZAK NONE O OTHER ININSP/MAINT 1 WP1335236 28801 THE L-2 DOOR HOLD OPEN LOCK (GUST LOCK) WAS FOUND BROKEN DURING CATERING. THE L-2 DOOR DOWEL PIN AND SPRING ASSEMBLY WERE REPLACED. (K) 2L72 4F RTA16WE 20050817000032005081700003NM 2005 8 17 MZZA0300003 120031027A5330 SKIN BOEING737 737823 13844BZNM STA 380 DENTED A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314240 28952 INSPECTION FOUND A DENT IN FUSELAGE SKIN NEAR L-1 DOOR, BELOW EMERGENCY LIGHT AT STA 380, S17L. THE SKIN WAS REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20050816000792005081600079NM 2005 8 16 SWAA031919 120030827A53306545766 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS, BS 500C+14 STR 10L, BS 500+13, STR 10R, BS 384, STR 10L, AND BS 500D+10, STR 12R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050816000832005081600083NM 2005 8 16 SWAA032556 120031119A53226546550 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE BILGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND 5 EA FUSELAGE BILGE AREA SHEAR TIES CORRODED AT BS 500B, LBL2, BS 807, LBL4 TO RBL 4, BS 767, LBL 7 TO RBL 25, BS 787, RBL 15 TO RBL 25 AND BS 727C, LBL 7 TO LBL 15. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001232005081600123NM 2005 8 16 SWAA032812 120031224A53116546500 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAMES AT STR 9L, BS 747, 787, 827, 907 AND STR 9R, BS 787, 827, 847, 887. REPAIRED FRAMES PER BFG ER. 2L72 4F RTA16WE 20051212000902005121200090CE 2005 12 12 AMWA54255 120030910A6120 PROPELLER BEECH 1900 1900D 1154162CE UNKNOWN A AMWAO OTHER J WARNING INDICATION DEDESCENT 1 CE07140ZV UE140 MAINTENANCE RECEIVED A CALL FROM CREW STATING PROP WOULD NOT GO INTO GROUND DURING FLIGHT. MAINTENANCE INSPECTED IT AND COULD NOT DUPLICATE THE PROBLEM ON GROUND. AIRCRAFT WAS FERRIED TO DUBOIS, PENNSYLVANIA AND WAS INSPECTED BY MAINTENANCE THERE AWAITING FOR TEST FLIGHT. OPERATED AIRCRAFT ON GROUND. OPS CHECK NORMAL. 2L72 4T RTA24CE 20060313001042006031300104SO 2006 3 13 LR7A03106 120031121A5100 REPAIR LKHEED382 382G 526414USO FS 528-577 NONE A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC3213 NOTED LMLG WHEEL WELL BULKHEAD WEB PREVIOUS REPAIR IN WEB AREA OF FS 528 - 577, WL 142 - 150, LBL 62. SCHEDULE REPLACEMENT TO ELIMINATE REPAIR. REPLACED WEB FS 528 - 577 IAW SRM SMP 583 51-60 & 51-70. 2H74 4T A1SO 20060313001942006031300194SO 2006 3 13 LR7A03097 120031121A5100LS5112 FLOORBEAM LKHEED382 382G 526414USO FS 737E-817E SCHEDULED MAINT A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND RT CENTER FUSELAGE FS 737E-817E CHINE ANGLE WITH NUMEROUS REPAIRS, RBL 61, WL 142. REPLACED CHINE ANGLE FS 737E-817E IAW SRM SMP 583 51-60 & 51-70. 2H74 4T A1SO 20060801002432006080100243WP 2006 8 1 IXXA060486S 120030124A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CRACKED AT STATION XW291. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW DC8 SRM 51-1-8, 51-2-1, 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20060801002442006080100244WP 2006 8 1 IXXA060487S 120030123A532056119433 ANGLE DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND ANGLE CORRODED AT STATION FS 70 LONGERON 32 LEFT. REMOVED DAMAGE, FABRICATED, REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, 51-2-0, AND 53-2-5. 2L74 4F RT4A25 20060802000732006080200073WP 2006 8 2 IXXA060492S 120030124A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK FOUND RIGHT AFT SERVICE DOOR CUTOUT UPPER AFT CORNER CRACKED AT FASTENER HOLE. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS WITH NEW FASTENERS IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20050427000282005042700028EU 2005 4 27 KBM2005F00032 120031230A2435 SHAFT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE STARTER GEN SHEARED E KBMAK NONE O OTHER ININSP/MAINT 1 WP1937SH 3171 6242 2300 STARTER GEN, SHEARED SHAFT, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20060731000162006073100016WP 2006 7 31 IXXA060475S 120030209A5753 PLATE DOUG DC8 DC871F 302199DWP ZONE 500 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK FOUND LEFT WING NUMBER FOUR FLAP VANE HAVE AN ELONGATED HOLE. REMOVED DAMAGED PLATE, FABRICATED NEW PLATE, LOCATED DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW PLATE IAW DOUGLAS DRAWING 5655752, DC8 SRM 51-1-8, 51-1-20D, AND 51-1-3. 2L74 4F RT4A25 20050202001162005020200116NM 2005 2 2 0704021 120031010A575365671565 FLAP TRACK BOEING737 737230C 1384472NM LT WING CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 LT WING OB FLAP OUTBD TRACK AFT ATTACH BOLT HOLE CORRODED. 2L72 4F A16WE 20050202000562005020200056NM 2005 2 2 0704022 120031007A575165464542 SKIN BOEING737 737230C 1384472NM RT WING AILERON DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 RT WING AILERON DELAMINATED AT WBL 481 2L72 4F A16WE 20050202001102005020200110NM 2005 2 2 0704014 120031006A5542UNK PANEL BOEING737 737230C 1384472NM RUDDER CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 RUDDER PANEL CORRODED STA 86-59, STA 121-64. 2L72 4F A16WE 20040913001422004091300142NM 2004 9 13 0704001 120030907A5320 SUPPORT ANGLE BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 SUPPORT ANGLE CRACKED BS 727+4 BETWEEN S23R-S24R. 2L72 4F4 F A16WE E2EA 20040913001452004091300145NM 2004 9 13 0704020 120030923A575365799499 GIMBAL JOINT BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE LT FLAP CARRIER CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 LT WING IB FLAP OB CARRIER GIMABL CRACKED. 2L72 4F4 F A16WE E2EA 20040913001472004091300147NM 2004 9 13 0704008 120030913A5320 ANGLE BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 ANGLE CRACKED AT BS 251.6 LBL 29. 2L72 4F4 F A16WE E2EA 20050607000102005060700010EA 2005 6 7 QXEA200500883 120030503A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE, LOWER SKIN PANEL ROCK CHIP DAMAGE STATION 310.00 TO 333.00 BETWEEN STRINGER 25R AND 25L. REPAIRED IAW CRJ-700 SRM 51-26-00-001-001-A01, 51-12-00-001-001-A01, 51-25-16-001-001-A01. 2L72 4F RTA21EA 20041026001802004102600180SO 2004 10 26 FPI2004F00004 220030701A7414 HOUSING CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO MAGNETO BROKEN E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO152667S1370 01010020 21061347 IMPULSE COUPLING FAILED CAUSING MAGNETO TO SEPARATE FROM ENGINE. 1H71 3O3 O 3A21 E5CE 20050222002542005022200254EU 2005 2 22 ERAA097109 120030624A2842VT044 TRANSMITTER BOLKMS105 BO105S 5626006EU FUEL QUANTITY WARPED E ERAAO OTHER N FALSE WARNING NRNOT REPORTED 1 AL03128EH 572 FLANGE WARPED, COMPLIED WITH PROPER TORQUE SPECIFICATIONS. REPLACED CASE ASSEMBLY AND TESTED. 1G72 3U H3EU 20041108001392004110800139CE 2004 11 8 DJFA200300008 120031217A3260 UPLOCK SWITCH BEECH MU300 400BEECH CE MLG FROZEN E DJFAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA23792TA RK264 AFTER TAKEOFF PILOTS WERE NOT ABLE TO GET THE GEAR UP AND LOCK. AFTER SEVERAL ATTEMPTS RETURNED TO THE DEPARTURE AIRPORT. MAINTENANCE FOUND ICE BUILT UP AROUND THE UPLOCK SWITCH. 2H72 4F RTA16SW 20050816001202005081600120NM 2005 8 16 SWAA032563 120031120A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C2 CHECK, FOUND 8 EA FUSELAGE SKIN CRACKS AT BS 487, STR 26L, AT BS 803, STR 20L, AT BS 970, STR 24L, AT BS 910, STR 23R, AT BS 759, STR 18R, AT BS 933, STR 23R, AT BS 685, STR 10R, AND AT BS 580, STR 10L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050427003632005042700363EA 2005 4 27 QXEA200500625 120030327A5310 STOP FITTING CNDAIRCL600 CL6002C10 1390015EA FUSELAGE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE, RIGHTHAND GALLEY SERVICE DOOR, DOOR STOP FITTING PAD WORN. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-25-00-001-001-A01, SRM 53-21-23-101-002-A01 AND CRJ700 AMM 52-00-00-790-801. 2L72 4F RTA21EA 20050816001252005081600125NM 2005 8 16 SWAA032829 120031228A53306545770 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED PM CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 500+2, STR 10R, BS 500B, STR 10R, AND BS 787, STR 19L. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001242005081600124NM 2005 8 16 SWAA032815 120031224A53116546500 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT STR 9L, BS 400 AND 480, AND STR 9R, BS 400 AND 480. REPAIRED DAMAGED AREA PER BFG ER. 2L72 4F RTA16WE 20051108000132005110800013NM 2005 11 8 XNOA01124 120030531A3240 BRAKE ASSY BOEING727 727200 138407ENM MLG UNKNOWN A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL2376753 21249 AFTER RELEASING BRAKES; ON POWER OUT OF MCO HEARD LOUD POP AND WHEN APPLYING PRESSURE TO BRAKES FELT VIBRATION COMING FROM MLG AREA. JACKED EACH MLG, INSPECTED EACH BRAKE & CYCLED NUMEROUS TIMES. NO DEFECTS NOTED. SERVICED ALL BRAKE LOCKOUTS. BRAKES CHECKED GOOD AS PER B727 MM 32-40-0. 2L73 4F RTA3WE 20060801000022006080100002WP 2006 8 1 IXXA060511S 120030122A5753 COVER DOUG DC8 DC871F 302199DWP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE FLAP SPRING COVER WORN AT STATION 255. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-3-0, DOUGLAS DRAWING NUMBER 5719443, AND TIMCO RE[AIR ENGINEERING ORDER REO-G09016 DATED 01/31/2003. 2L74 4F RT4A25 20060801000302006080100030WP 2006 8 1 IXXA060517S 120031017A5740 BRACKET DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE DUCTING BRACKET CRACKED. REMOVED BRACKET, WELDED BRACKET AND REINSTALLED BRACKET IAW DC8 MM 20-16-0. 2L74 4F RT4A25 20060801000412006080100041WP 2006 8 1 IXXA060524S 120030922A5740 ATTACH BRACKET DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE OUTBOARD END ATTACH FASTENER HOLES CRACKED. REMOVED DAMAGED HOLES. FABRICATED REPAIR DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW DOUBLER AND FILLER IAW TIMCO REPAIR ENGINEERING ORDER REO-G09488. 2L74 4F RT4A25 20060801000662006080100066WP 2006 8 1 IXXA060532S 120030911A572056110212527 SHIM DOUG DC8 DC871F 302199DWP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE SUPPORT SHIMS CORRODED AT STATION XIS59.492. REMOVED DAMAGED SHIMS. FABRICATED NEW SHIMS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SHIMS IAW DC8 SRM 51-1-8, 51-5-4, 51-3-0, TIMCO REPAIR ENGENEERING ORDER REO-G09465. 2L74 4F RT4A25 20060801000712006080100071WP 2006 8 1 IXXA060536S 120030910A7830 CHANNEL DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND NR 3 ENGINE THRUST REVERSER FIXED STRUCTURE AFT TWELVE O-CLOCK SEAL CHANNEL CRACKED. FABRICATED NEW SEAL CHANNEL, LOCATED, DRILLED, TRIMMED, AND INSTALLED NEW SEAL CHANNEL REPAIR PARTS IAW TIMCO REPAIR ENGINEERING ORDER, REO G-09505. 2L74 4F RT4A25 20060801000802006080100080WP 2006 8 1 IXXA060542S 120030916A5753 WEB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INTERNAL WEB CRACKED AT INBOARD LEADING EDGE AT STATION XF1. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 57-20-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060801001012006080100101WP 2006 8 1 IXXA060552S 120030910A57535701110502 VANE DOUG DC8 DC871F 302199DWP ZONE 600 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP NUMBER SIX VANE DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND BONDED NEW OUTER SKIN, OUTER DOUBLER AND INNER FILLER IAW TPS 1001 REV E AND DOUGLAS DRAWING 5701110 2L74 4F RT4A25 20060801001112006080100111WP 2006 8 1 IXXA060561S 120031003A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 MISREPAIRED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FIRST OFFICER FORWARD OUTBOARD SEAT TRACK HAS IMPROPER REPAIR. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-351-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060801001362006080100136WP 2006 8 1 IXXA060579S 120031009A5210 SKIN DOUG DC8 DC871F 302199DWP ZONE 800 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND DOOR L-1, UPPER AFT SKIN GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 52-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060801001392006080100139WP 2006 8 1 IXXA060582S 120030911A5320 WEB DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND WEB CRACKED AT STATION 1280 LONGERON 27 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060731000182006073100018WP 2006 7 31 IXXA060502S 120030123A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND SEAT TRACK WORN AND GOUGED AT STATION 240 BL-0. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS, IAW,DC8 SRM 53-2-3, AND 51-1-8. 2L74 4F RT4A25 20060801000972006080100097WP 2006 8 1 IXXA060549S 120030910A575336523062 HINGE FITTING DOUG DC8 DC871F 302199DWP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP EXHAUST GATE OUTBOARD HINGE FITTING HAS WORN BUSHING HOLES. WORN HOLES WERE OVERSIZED, BUSHINGS WERE MANUFACTURED AND INSTALLED, HOLES WERE FINAL SIZED TO MANUFACTURES ORIGINAL DIMENSIONS IAW DC8 SRM 51-1-21, 51-9-0, 51-3-0, TIMCO REPAIR ENGINEERING ORDER REO-G09472 DATED 09/18/2003. 2L74 4F RT4A25 20060801001182006080100118WP 2006 8 1 IXXA060568S 120030909A5320 SUPPORT CHANNEL DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND CRACKED FLOOR SUPPORT CHANNEL AT STATION 360, LONGERON 33 LEFT. REMOVED CRACKED FLOOR SUPPORT CHANNEL. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PART IAW DC8 SRM 51-1-21, 51-1-8, AND DOUGLAS DRAWING 3758633. 2L74 4F RT4A25 20060801001632006080100163WP 2006 8 1 IXXA060482S 120030127A5753 PLATE DOUG DC8 DC871F 302199DWP ZONE 500 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND THE LEFT NR 4 FLAP VANE CENTER OUTBOARD FLAP ATTACH PLATE GOUGED. REMOVED DAMAGED PLATE, FABRICATED NEW PLATE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED NEW PLATE IAW DOUGLAS DRAWING 565-37552 DC8 SRM 51-3-0, AND 51-1-8. 2L74 4F RT4A25 20060801002502006080100250WP 2006 8 1 IXXA060491S 120030123A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND AFT PASSENGER DOOR CUTOUT UPPER AFT CORNER CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060801000482006080100048WP 2006 8 1 IXXA060528S 120030912A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND A CRACKED INTERCOSTAL AT STATION 1160 LONGERON 27 RIGHT. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-20D, 51-1-8, AND DOUGLAS DRAWING 9573259. 2L74 4F RT4A25 20060801000652006080100065WP 2006 8 1 IXXA060531S 120030911A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FORWARD SERVICE DOOR CUTOUT UPPER FORWARD CORNER CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20060801000672006080100067WP 2006 8 1 IXXA060533S 120030910A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FRAME GOUGED AT STATION 1684 LONGERON 21 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-21, 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20060801000702006080100070WP 2006 8 1 IXXA060535S 120030910A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "F" GOUGED AT STATION 830. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION AND SPLICES, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW DC8 SRM 51-1-8, AND 53-2-3 2L74 4F RT4A25 20060801001162006080100116WP 2006 8 1 IXXA060566S 120031022A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND NUMBER "3" SEAT TRACK HAS BROKEN SCALLOPS AT STATION 70. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0. 2L74 4F RT4A25 20060801001302006080100130WP 2006 8 1 IXXA060573S 120030908A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 SCRATCHED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SCRATCHED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-1, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060801001332006080100133WP 2006 8 1 IXXA060576S 120030910A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "G" WORN AT STATION 670. REMOVED WORN SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0. 2L74 4F RT4A25 20060801001412006080100141WP 2006 8 1 IXXA060584S 120030912A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND INTERCOSTAL CRACKED AT STATION 1100 AT LONGERON 27 RIGHT. REMOVED DAMAGED INTERCOSTAL, FABRICATED ANGLE REPAIR, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 51-1-8, 53-4-0, AND 51-1-21. 2L74 4F RT4A25 20060801001422006080100142WP 2006 8 1 IXXA060585S 120030922A5320 CUSP WEB DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND CUSP WEB CRACKED AT STATION FS 670. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, 53-2-0, 53-4-1, AND 51-1-8. 2L74 4F RT4A25 20060801001462006080100146WP 2006 8 1 IXXA060589S 120030910A5753 FLAP TRACK DOUG DC8 DC871F 302199DWP ZONE 500 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LEFT OUTBOARD FLAP VANE MOUNT TRACK WORN AT HINGE NUMBER FIVE. REMOVED DAMAGED TRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 51-3-2, 57-50-2, AND 51-1-8. 2L74 4F RT4A25 20060801001082006080100108WP 2006 8 1 IXXA060558S 120030909A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND AFT PASSENGER DOOR, L-2, CUT-OUT LOWER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, AND 51-1-20D. 2L74 4F RT4A25 20060801001582006080100158WP 2006 8 1 IXXA060478S 120030129A5730 PANEL DOUG DC8 DC871F 302199DWP ZONE 500 CHAFED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND LEFT WING UPPER TRAILING EDGE PANEL AFT OF TRUNNION PANEL CHAFED ON INBOARD UPPER SKIN. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER. IAW 57-2-0, 57-2-1, 57-3-1, 51-1-22, 57-2-21 AND 51-1-8. 2L74 4F RT4A25 20060801002422006080100242WP 2006 8 1 IXXA060485S 120030125A5753 PLATE DOUG DC8 DC871F 302199DWP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP BOILER PLATE KNIFE EDGED AT STATION 410. REMOVED DAMAGED BOILER PLATE, FABRICATED REPAIR PARTS, LOCATED, DRILED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DOUGLAS DRAWINGS 5719443, 5719445, DC8 SRM 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060801000342006080100034WP 2006 8 1 IXXA060520S 120031006A5510 FAIRING DOUG DC8 DC871F 302199DWP ZONE 300 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER RUB FAIRING GOUGED ON UPPER END OF LOWER FAIRING. REMOVED FAIRING, REPAIRED AND REINSTALLED FAIRING PER ALL APPROVED DATA. 2L74 4F RT4A25 20060801001292006080100129WP 2006 8 1 IXXA060572S 120030909A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "E" GOUGED AT STATION 150. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 51-1-21, 53-2-3, AND 51-3-0. 2L74 4F RT4A25 20060313001262006031300126SO 2006 3 13 LR7A03047 120030609A53103483143 CROSS TIE LKHEED382 382G 526414USO FS 737 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 4606 DURING CARGO LOADING OPERATIONS FS 737, WL 256 CROSS TIE ASSY DAMAGED BY CARGO IMPACT. CROSS TIE ASSY CRACKED APPROX 3.0 IN AT RBL 61 ATTACH AND 12.0 IN AT LBL 61 ATTACH. TWO EACH CROSS TIE BRACES SEVERED AT UPPER FRAME ATTACH APPROX LBL AND RBL 45, WL 280. AIRCRAFT FERRIED UNPRESSURIZED TO ANC FOR REPAIR. AT ANC REPLACED CROSS TIE ASSY, BRACES AND END FITTINGS (PRECAUTIONARY) IAW SMP SRM 583 51-10 PG 4 AND 51-70. 2H74 4T A1SO 20060313001922006031300192SO 2006 3 13 LR7A03084 120031121A5315370499 FLOORBEAM LKHEED382 382G 526414USO FS 517-597 MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION CARRY OVER NR 0220 DUE FOR ACCOMPLISHMENT - LT CHINE CAP MISDRILLED HOLES FS 557, LBL, 61, WL 146. REPLACED LT CHINE CAP FS 517- 597 IAW SRM SMP 583 51-60 & 51-70. 2H74 4T A1SO 20060731000172006073100017WP 2006 7 31 IXXA060501S 120030123A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND SEAT TRACK GOUGED AT STATION 250 BL-0. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS, IAW DC8 SRM 53-2-3, AND 53-2-3. 2L74 4F RT4A25 20060731000542006073100054WP 2006 7 31 IXXA060505S 120030122A5320 WEB DOUG DC8 DC871F 302199DWP ZONE 200 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND LEFT AFT PASSENGER DOOR CUTOUT JAMB WEB HAS IMPACT DAMAGE. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DOUGLAS DRAWIMG 9751069, TIMCO REPAIR ENGENEERING ORDER REO-G09028 DATED 02/07/2003, DC8 SRM 51-1-8, 51-1-21, 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20060801000362006080100036WP 2006 8 1 IXXA060521S 120030924A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 459994 DURING ROUTINE C CHECK FOUND INTERCOSTAL CORRODED FROM STATION 1000 TO 1020 AT LONGERON 35 RIGHT. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D, AND DOUGLAS DRAWING 779929. 2L74 4F RT4A25 20060801000442006080100044WP 2006 8 1 IXXA060526S 120030916A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LONGERON 11 RIGHT CRACKED AT STATION FS 1660. REMOVED CRACKED LONGERON. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW LONGERON, IAW DC8 SRM 51-1-21, 51-1-8, 51-1-20D, AND DOUGLAS DRAWING 3773512. 2L74 4F RT4A25 20060801000012006080100001WP 2006 8 1 IXXA060510S 120030122A5320 WEB DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION FS 1165, LONGERON 35 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 1-1-8, 53-2-0, 51-1-21, 51-3-0, AND DOUGLAS DRAWING NUMBER 5750195. 2L74 4F RT4A25 20060801000722006080100072WP 2006 8 1 IXXA060537S 120030908A53205778293T0023 CLOSEOUT PANEL DOUG DC8 DC871F 302199DWP ZONE 100 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LEFT AFT PRESSURE BULKHEAD CLOSEOUT PANEL DELAMINATED. REMOVED DAMAGED PANEL. FABRICATED NEW CLOSEOUT PANEL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW CLOSEOUT PANEL IAW TIMCO REPAIR ENGINEERING ORDER REO-G09509. 2L74 4F RT4A25 20060801000772006080100077WP 2006 8 1 IXXA060540S 120030909A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX8682 2840 45994 DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION 245 BETWEEN LONGERONS 34 LEFT AND 35 LEFT. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-21,51-1-8, AND TIMCO REPAIR ENGINEERING ORDER REO-G9471. 2L74 4F RT4A25 20060801001002006080100100WP 2006 8 1 IXXA060551S 120030910A5753570152502 VANE DOUG DC8 DC871F 302199DWP ZONE 600 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RT OUTBOARD FLAP VANE DELAMINATED BETWEEN INBOARD AND CENTER HINGE. REPLACED FLAP VANE IAW DC8 SRM 27-51-14. 2L74 4F RT4A25 20060801001282006080100128WP 2006 8 1 IXXA060571S 120030919A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 100 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK NUMBER TWO GOUGED AT STATION 150. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK. IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0. 2L74 4F RT4A25 20060801001492006080100149WP 2006 8 1 IXXA060592S 120030906A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND CAPTAINS LEFT FORWARD SEAT TRACK WORN. REMOVED WORN SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 51-1-21, AND 51-3-0. 2L74 4F RT4A25 20060801001502006080100150WP 2006 8 1 IXXA060593S 120030910A5753 HINGE DOUG DC8 DC871F 302199DWP ZONE 500 CHAFED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LEFT INBOARD FLAP INBOARD HINGE FITTING OUTBOARD HINGE HALF CHAFED AT STATION XW3. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, AND DC8 SB 27-279. 2L74 4F RT4A25 20060801001612006080100161WP 2006 8 1 IXXA060481S 120030127A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND INTERCOSTAL CRACKED FROM STATION 1140 TO STATION 1160, AT LONGERON 33 LEFT. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060801001672006080100167WP 2006 8 1 IXXA060484S 120030126A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND A CRACKED FRAME AT STATION 280 LONGERON 29 RIGHT. REMOVED DAMAGED FRAME, FABRICATED NEW FRAME, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FRAME IAW DOUGLAS DRAWING 9779487, DC8 SRM 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060731000562006073100056WP 2006 7 31 IXXA060507S 120030122A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND RIGHT WING LOWER LEADING EDGE OUTBOARD OF PANEL 522A EXISTING REPAIR CRACKED. REMOVED EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 57-2-1, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060801000692006080100069WP 2006 8 1 IXXA060534S 120030910A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "F" GOUGED AT STATION 860. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED SEAT TRACK SECTION, AND SPLICES, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK SECTION, AND SPLICES IAW DC8 SRM 51-1-8, AND 53-2-3. 2L74 4F RT4A25 20060801000962006080100096WP 2006 8 1 IXXA060548S 120030910A5753 RUB STRIP DOUG DC8 DC871F 302199DWP TE FLAPS WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP EXHAUST GATE, OUTBOARD RUB STRIP WORN. REMOVED WORN RUB STRIP. FABRICATED NEW RUB STRIP, LOCATED, DRILLED, TRIMMED, AND INSTALLED NEW RUB STRIP IAW DC8 SRM 51-1-21, TIMCO REPAIR ENGINEERING ORDER REO-G094569 DATED 09/18/2003, AND DOUGLAS DRAWING 5652302. 2L74 4F RT4A25 20060801001102006080100110WP 2006 8 1 IXXA060560S 120030909A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND AFT SERVICE DOOR, R-2, CUT-OUT UPPER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D. 2L74 4F RT4A25 20060801001592006080100159WP 2006 8 1 IXXA060479S 120030128A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND LONGERON 11 RIGHT CRACKED AT AFT SERVICE DOOR JAMB UPPER AFT CORNER. FABRICATED NEW LONGERON AND NEW SPLICES, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED NEW LONGERON AND SPLICES IAW DOUGLAS DRAWING 3773512, DC8 SRM 51-1-24, 51-1-21, 51-1-20D, 51-3-0, AND 51-1-21A. 2L74 4F RT4A25 20060801000742006080100074WP 2006 8 1 IXXA060538S 120030909A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "D" TANG BROKEN AT STATION 150. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 53-2-3, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060801001092006080100109WP 2006 8 1 IXXA060559S 120030909A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND AFT SERVICE DOOR, R-2, CUT-OUT LOWER FORWARD CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D. 2L74 4F RT4A25 20060801001192006080100119WP 2006 8 1 IXXA060569S 120030928A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND A CRACKED INTERCOSTAL FROM STATION 1640 TO 1660 AT LONGERON 10 RIGHT. REMOVED CRACKED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-21, 51-1-8,51-3-0, AND DOUGLAS DRAWING 5772656. 2L74 4F RT4A25 20060801001512006080100151WP 2006 8 1 IXXA060594S 120030910A5753 HINGE DOUG DC8 DC871F 302199DWP ZONE 600 CHAFED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INBOARD HINGE FITTING OUTBOARD HINGE HALF CHAFED AT STATION XW3. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, AND DC8 SB 27-279. 2L74 4F RT4A25 20060801001652006080100165WP 2006 8 1 IXXA060483S 120030126A5713 STRINGER DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND THE CENTER WING LOWER STRINGER 76 LEFT CORRODED AT STATION XCW50.0. REMOVED CORROSION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW TIMCO REPAIR ENGINEERING ORDER REO-G09014 DATED 1/31/2003. 2L74 4F RT4A25 20060801000982006080100098WP 2006 8 1 IXXA060550S 120030910A5753 RUB STRIP DOUG DC8 DC871F 302199DWP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP EXHAUST GATE CUT-OUT FORWARD UPPER RUB STRIP WORN. REMOVED WORN RUB STRIP. FABRICATED NEW RUB STRIP, LOCATED, DRILLED, TRIMMED, AND INSTALLED NEW RUB STRIP IAW DC8 SRM 51-1-21, DOUGLAS DRAWING 5643970. 2L74 4F RT4A25 20060802001132006080200113WP 2006 8 2 IXXA060500S 120030123A5340 FITTING DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND A CRACKED END FITTING FROM STATION 1767 TO 1772 AT LONGERON 10 LEFT. REMOVED CRACKED END FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D, 51-1-21, 21-3-0, AND 51-1-24. 2L74 4F RT4A25 20060815001222006081500122WP 2006 8 15 IXXA060497S 120030123A5320 ANGLE DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUITNE C CHECK FOUND RIGHT HAND ELEVATOR DRAIN PAN INSIDE OF TAIL CONE CRACKED. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE. IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060815001232006081500123NM 2006 8 15 USAASB03174 120030928A2751 INDICATION SYS BOEING737 7373B7 1384580NM TE FLAPS MALFUNCTIONED A USAAL ABORTED APPROACH N FALSE WARNING DEDESCENT 1 EA19521AU 23856 CLT - FLT 1095 - DURING DESCENT INTO CLT FROM DFW, AT APPROXIMATELY 1,700 FEET, CREW ENCOUNTERED A SPLIT FLAP INDICATION. CREW BROKE OFF APPROACH, DECLARED AN EMERGENCY AND WENT THROUGH CORRECTIVE PROCEDURES. FLIGHT LANDED WITHOUT INCIDENT. BOTH FLAPS AT LANDING WERE AT 2 UNITS. MAINTENANCE COULD NOT DUPLICATE FLAP INDICATION PROBLEM PER MM 27-58-01. OPERATED FLAPS SEVERAL TIMES WITH NO FAULTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20070406001752007040600175NM 2007 4 6 AT0700023 120030930A5311 FRAME BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15949AT 55003 RIGHT HAND FUSELAGE FRAME DAMAGED AT STA 58.750. REPLACED FUSELAGE FRAME AT STA 58.75 PER DWG 9911502 AND B717 SRM 51-41-01 (RT SIDE). 2L72 4F TRA6WE 20070417002882007041700288NM 2007 4 17 AT0700025 120030318A5310 DOOR FRAME BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15957AT 55019 FWD CARGO DOOR JAMB DAMAGE. INSTALLED DOUBLER REPAIR ON FWD CARGO DOOR PAN AFT CORNER IAW BEACOM CQTCRL-03-00134H DATED MARCH 18, 2003 AND RES 03-0265. MATERIAL USED 2024-0 .063. HEAT TREATED TO 2024-T3, 5.5" X 5.5". 2L72 4F TRA6WE 20060801001352006080100135WP 2006 8 1 IXXA060578S 120030911A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FORWARD SERVICE DOOR, R-1, CUT-OUT LOWER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D. 2L74 4F RT4A25 20060801001522006080100152WP 2006 8 1 IXXA060595S 120030910A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 SEPARATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LEFT OUTBOARD FLAP UPPER SURFACE NUMBER THREE WEDGE FORWARD LEFT CORNER SEPARATED. INJECTED ADHESIVE, AND BONDED AREA IAW DC8 SRM 51-1-9. 2L74 4F RT4A25 20060802000742006080200074WP 2006 8 2 IXXA060493S 120030124A5240 STRUCTURE DOUG DC8 DC871F 302199DWP SERVICE DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND RIGHT AFT SERVICE DOOR AFT CORNER CRACKED, EXTENDING PAST STOP DRILL AT LIGHTNING HOLE. REMOVED DAMAGE, FABRICATED, REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 52-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060516000882006051600088SO 2006 5 16 RAIA00604046 120030429A3030CS500060D4A RELAY EMB 145 EMB145LR 3260212SO COCKPIT OVERHEATED A RAIAA UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 CE03811HK 145256 FLT 5546 AUS TO STL - FIRE AND SMOKE IN CABIN COMING FROM RT RELAY SUPPORT AREA AFT OF FO'S SEAT. FO PUT OUT FIRE WITH COCKPIT FIRE EXTINGUISHER AND AIRCRAFT MADE UNEVENTFUL UNPLANNED LANDING AT SGF. REPORTED TO NTSB. FAA INVESTIGATED. MAINTENANCE REMOVED AND REPLACED OVERHEATED RELAY K0057 AND ASSOCIATED RELAYS DAMAGED BY THE FIRE, AND PREPARED THE AIRCRAFT FOR FERRY TO STL TO COMPLETE REPAIRS. THE OVERHEATING OF THE PITOT HEAT RELAY RESULTED IN THE BURNING OF THE WINDOW SILL DRAIN HOSE. THE UNSAFE CONDITION IDENTIFIED IN AD 2006-04-02. THE AD HAD NOT YET BEEN ACCOMPLISHED ON N811HK. 2L72 4T RTT00011AT 20070503002302007050300230NM 2007 5 3 AT0700030 120031022A5313 STRINGER BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15992AT 55136 A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. STRINGER AND SLICED DAMAGED. INSTALLED REPAIR ON STRINGER SECTION AND SPLICE. 2L72 4F TRA6WE 20030606000612003060600061 2003 6 6 CEVA005 420030520A2562L84 BATTERY ACR BEACON SWOLLEN B CEVAO OTHER OO OTHER OTHER ININSP/MAINT 1 GL03 L763757 DURING THE YEARLY INSPECTION OF THE LIFE VEST, THE WATER ACTIVATER BATTERY FOR THE LOCATING LIGHT HAD SWOLLEN AND STARTED TO CRACK OPEN. 20030617001432003061700143GL 2003 6 17 ERAA087100 220030520A7200 ENGINE ALLSN 250C 250C20B 03013GL MAKING METAL E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01 14386 CAE833288 ENGINE MAKING METAL. FOUND TURBINE 3 U E4CE 20030318000552003031800055NE 2003 3 18 2003F00102 220030123A7310500013401 MANIFOLD PWA JT8 JT8D217A 52053NE FUEL DIST FRACTURED B O OTHER O OTHER NRNOT REPORTED 1 GL23 696406 LEFT HAND SECONDARY FUEL MANIFOLD FRACTURED 4 F E9NE 20030606000622003060600062 2003 6 6 CEVA006 420030520A2562L84 BATTERY KSE35L8 BEACON SWOLLEN B CEVAK NONE O OTHER ININSP/MAINT 1 GL03 14132 DURING THE YEARLY INSPECTION OF THE LIFE VEST, THE WATER ACTIVATER BATTERY FOR THE LOCATING LIGHT HAD SWOLLEN AND STARTED TO CRACK OPEN. 20030212000522003021200052NE 2003 2 12 CA030114003 320030103A6114E3932 HUB HARTZLHCE4A HCE4A3I NE PROPELLER FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)PROPELLER HUB FAILED. NEW HUB INSTALLED. NEW BEARINGS INSTALLED AS PER SB 61-258. 5 CP10NE 20030908002382003090800238 2003 9 8 MALA030345 420030723A2210 AUTOPILOT SYS COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL15076XJ INFLIGHT ON FLIGHT NR 3114, AT 15000 FT AN ELEV MISTRIM NOTICED, DISCONNECTED AUTOPILOT TO RETRIM AND FOUND MAIN ELEVATOR PITCH TRIM HAD FAILED, STANDBY WORKS NORMALLY. AIR RETURN TO MSP. MAINTENANCE COMPLETED OPERATIONAL TEST OF ELEVATOR TRIM SYSTEM PER SAAB AMM 27-32-30. ALSO AUTO PILOT SYSTEM, COULD NOT DUPLICATE TRIM FAULT. NO HISTORY AND OPS CHECK GOOD AT THIS TIME. 20030818000702003081800070SW 2003 8 18 HEEA088586 120030711A6220412310400101 ROD BEARING BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D3631 33076 MAIN ROTOR ROD BEARING WORN. SHOP REPAIR. 1G72 4U H4SW 20030819000862003081900086 2003 8 19 SWIA200312174 420030705A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07591SW4329 4329 7079 INTERMITTENT UNCOMMANDED RIGHT RUDDER INPUTS IN CLIMB, CRUISE, WITH OR WITHOUT AP ON. MUST HOLD + 5 DEGREES RIGHT RUDDER FOR COORDINATED FLIGHT. REMOVED AND REPLACED NR 1 YAW DAMPER ACTUATOR IAW CL600 MM 22-22-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20030331001092003033100109EU 2003 3 31 DHL2003363002 120030326A3242C200601004 BRAKE AIRBUS300 A300B4203 3930306EU MLG FAILED A DHLAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO01363DH 85 AFTER T/O & NORMAL GEAR RETRACTION, HOT BRAKE LIGHT ILLUMINATED. (200 DEG AND CLIMBING) FELT VIBRATION DURING EXTENSION. FOUND NR 2 TIRE BLOWN. R & R NR 1 TIRE ASSY IAW 12-37-32 (MATED TIRE). R & R NR 2 MAIN WHEEL ASSY IAW M/M 12-37-32. PERFORMED OPS CHECK OF ANTI-SKID SYSTEM IAW M/M 32-42-72. OPS CHECKED GOOD. REPLACED FAN DEBRIS GUARD AND BRAKE FAN OPS CHECKED GOOD IAW M/M 32-48-11. OK FOR SERVICE. 2L72 4F RTA35EU 20030820001832003082000183EA 2003 8 20 COMA0360351 120030805A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01963CA 7127 FLIGHT 5488 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030821002562003082100256WP 2003 8 21 GTIA030596 120030716A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN FLOORBOARD CORRODED, BROKEN INSERTS, EDGES BROKEN, FS 1271-1338. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030403000472003040300047NM 2003 4 3 AMTA200300306 120030304A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 EPW WHITE LIGHT, THREE EACH, AT ROWS 30 AND 31 INOPERATIVE. REF ITEM 4 THIS PAGE 558241 FOR ADDITIONAL INFORMATION, ONCE WIRE FOR 32D WAS RECONNECTED WHITE EPL LIGHTS AT 30 AND 31 CHECK GOOD. (M) 2L72 4F RTA2NM 20030407000102003040700010WP 2003 4 7 ASAA0380063 120030109A53209936534 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 180-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 FOUND DURING 30K CHECK, FALSE TRACK CORRODED AT FLOORBOARD FASTENER HOLES AT FS 180-200. REPLACED FALSE TRACK PER SRM 51-10-4 AND 51-30-1. (M) 2L72 4F RTA6WE 20030404000822003040400082NM 2003 4 4 DL767030221 120030307A335020131A BATTERY BOEING767 767232 1385132NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27109DL 22221 ON LAYOVER FOUND EMERGENCY LIGHTS AT EXTERIOR L2 AND OVERWING SLIDE INOP ON LT SIDE. REPLACED BATTERY PACK AND CHARGER PER M/M. OPS CHECK OK. 2L72 4F RTA1NM 20030414000852003041400085EU 2003 4 14 CA030304004 120030301A2400NSA9311901 MOUNT AIRBUS330 A330322 3930325EU PWA 4168 PW4168 NE FUSE BURNED W O OTHER M OVER TEMP NRNOT REPORTED 1 CA (CAN) A/C ARRIVED YVR WITH APU INOP. INSPECTION OF THE 5000VE PANEL REVEALED THAT THE FUSE F/N 6KA1 WAS INFACT BLOWN. CLOSER INSPECTION ALSO FOUND THAT ONE STUD BOLT OF THE MOUNT P/N NSA931190-1 THAT THE FUSE SITS ON WAS HEAVILY DAMAGED BY EXTREME HEAT. NUT ON STUD FOUND TO BE FUSED TO THREAD AND WASHER MELTED TO NUT. BUSS BAR F9259000720000 WAS ALSO FOUND TO HAVE DAMAGE WITH SEVERE PITTING AND MELTED MATERIAL ON IT. 2L72 4F4 FRTA46NM E36NE 20030415000722003041500072EU 2003 4 15 CA030327008 120030324A3250SD3730311XA HOSE STBROSSD3 SD360 8100606EU PWA PT6 PT6A65AR 52043NE NLG STEERING LEAKING W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION LDLANDING 1 CA (CAN) ON LANDING ROLLOUT BOTH STEERING AND NORMAL BRAKES WERE LOST. BOTH HYDRAULIC CAUTION LIGHTS CAME ON.THE AIRCRAFT WAS MANEUVERED OFF THE RUNWAY USING DIFFERENTIAL POWER AND EMERGENCY BRAKES AND THEN B OUGHT TO A STOP AND SHUT DOWN. THE AIRCRAFT WAS TOWED TO THE HANGAR WHERE MAINTENANCE PERSONNEL FOUND A NOSE WHEEL STEERING HYDRAULIC LINE LEAKING IN THE NOSE GEAR WELL. FLUID WAS ESCAPING BETWEEN THEFLEXIBLE BRAIDED HOSE AND THE SWAGED FITTING. THE HOSE WAS REPLACED AND ALL OTHER HOSES IN THE VICI NITY WERE INSPECTED FOR DEFECTS. 2H72 4T4 T A41EU E4EA 20030416001572003041600157NM 2003 4 16 DLM88030296 120030328A3260 BULB DOUG MD88 MD88 3023688NM MLG INDICATOR BURNED OUT A DALAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO27915DE 53420 GO-AROUND INITIATED AFTER FAILURE OF RT MLG GREEN DN LIGHT FAILURE. POM PROCEDURE FOLLOWED. CHANGED BULBS, DN INDICATION NORMAL. BOTH BULBS WERE BAD. BULBS REPLACED. CHECKED PROX BOX. SENSORS OK. 2L72 4F RTA6WE 20030417000922003041700092EA 2003 4 17 QXEA0300229 220030203A7200 SHROUD BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PCEFA0060 PDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE. NP SHROUD HAD HOLES IN IT. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE SENT TO PRATT AND WHITNEY FOR EVALUATION. 2H72 4T4 TRTA13NM E00062EN 20030424000612003042400061SO 2003 4 24 LD22003F00000 120030306A32421159SC15043 BRAKE ASSY GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE MLG CRACKED B LD2RO OTHER O OTHER NRNOT REPORTED 1 GL1523M 579 11261 CRACKS WERE FOUND IN THE NR ROTOR DRIVE CLIPS. A NEW BRAKE UNIT WAS INSTALLED. MFG ARE WORKING ON NEW DESIGNS TO CORRECT THESE PROBLEMS. 2L72 4F4 FRTA12EA E00057EN 20030430002052003043000205NM 2003 4 30 VNAA0304012 120030416A5270 PROXIMITY SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MAIN DOOR FAILED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07458PS 3068 DURING TAKEOFF, THE CREW RECEIVED A MAIN DOOR PROXI SWITCH FAIL INDICATION AND ABORTED TAKEOFF. OUTSTATION MAINTENANCE INSPECTED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00 AND FOUND CODES A06 AND S33 AND CLEANED THE MAIN DOOR PROXI SWITCH WHICH DID NOT CORRECT THE DEFICIENCY. THE AIRCRAFT WAS THEN SCHEDULED TO FERRY TO DAY. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030502000482003050200048WP 2003 5 2 ASAA0380148 120030222A53205926017501 SUPPORT FITTING DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO BAY BARRIER DOOR AFT NET SUPPORT FITTING IS CRACKED. REPLACED SUPPORT FITTING PER SRM 51-10-4 AND 51-30-1. (M) 2L72 4F A6WE 20030505000992003050500099NM 2003 5 5 PCA0300844 120030410A5347 SEAT TRACK BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 MAIN DECK SEAT TRACK FLANGE - LEVEL 1 CORROSION S1800 LBL 67.01. REPAIR PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20030506001072003050600107EA 2003 5 6 COMA0360214 120030423A2450V5643 RELAY CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A COMAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01488CA 7730 FLIGHT 5896 ACCESS BUS CAUTION MESSAGE. REPLACED THE SENSE RELAY KIXD. 2L72 4F RTA21EA 20030506001272003050600127EU 2003 5 6 AWXA200300421 120030329A5320D5311219820005 FITTING AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF L-1 DOORWAY LOWER OUTBOARD SILL ATTACH FITTING FR 18, STR 24 LT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED L-1 DOORWAY LOWER OUTBOARD SILL ATTACH FITTING FR 18, STR 24 LT; FABRICATED A NEW REPLACEMENT ATTACH FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-9. 2L72 4F RTA28NM 20030508000982003050800098EA 2003 5 8 QXEA0300534 120030423A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 PDX-DENT IN FUSELAGE AT STATION 349.00 MID FUSELAGE JUST AFT OF MAIN CABIN DOOR CUTOUT. REPAIRED IAW CRJ-700 SRM 53-00-01, SRM 51-12-00 AND SRM 51-25-16. HORIZON AIR EA R53-95, R53-94 AND EO 670-53-21-035. 2L72 4F RTA21EA 20030515000462003051500046SO 2003 5 15 SWIA200311919 120030428A5753 FLAP TRACK EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT WING WORN A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07214SW 120280 FLAP DISAGREEMENT AFTER TAKEOFF. OUTBOARD PAIR WOULD NOT RETRACT TO LESS THAN 10 DEGREES, OTHER PAIRS RETRACTED PROPERLY. APPLIED QRH PROCEDURE 3 TIMES, FAILED ALL 3 TIMES. FLAPS EXTENDED TO 25 DEGREES PROPERLY FOR LANDING, THEN RETRACTED PROPERLY TO 0 DEGREES AFTER LANDING. REMOVED AND REPLACED RIGHT OUTBOARD FLAPS OUTBOARD MOVEABLE TRACK AND ROLLERS. OPS CHECK GOOD IAW MM 27-50-02. 2L72 4T4 TRTA31SO E20NE 20070503002342007050300234NM 2007 5 3 AT0700052 120031022A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15992AT 55136 A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. SKIN FROM BS 171 TO BS203 DAMAGED. INSTALLED FUSELAGE SKIN REPAIR FROM BS 171 TO BS 203 STR 20R TO 23R, MATERIAL USED 2024 T3 .063 - 32 1/2 X 13 1/4, PER B717-SRM 53-00-01 REPAIR 6. 2L72 4F TRA6WE 20030320000692003032000069NE 2003 3 20 2003F00137 220030308A7200 BRACKET PWA JT8 JT8D219 52053NE FAN DUCT BROKEN B K NONE O OTHER ININSP/MAINT 1 GL09 718055 DURING TROUBLESHOOTING OF SUSPECTED OIL LEAK, FOUND HIDDEN DAMAGE. INSPECTION REVEALED DIFFUSER INNER FAN DUCT BRACKETS BROKEN. A SECTION OF THE BROKEN BRACKET WORKED ITS WAY BETWEEN THE DIFFUSER CASE AND SECONDARY FUEL MANIFOLD RESULTING IN FUEL MANIFOLD HOLE FROM CHAFING. 4 F E9NE 20030813001292003081300129WP 2003 8 13 AALA20030668 120030618A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21227AA 49177 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS ABOVE ROWS 8-11 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT BATTEYR CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030818000282003081800028SW 2003 8 18 HEEA088465 120030709A2434214175150105 STARTER GEN BELL 214 214ST 1182106SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 STARTER GENERATOR KICKS OFF LINE. 2G72 4U H10SW 20030820000802003082000080NM 2003 8 20 03FDEA00919 120030617A5754ARC0503504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING- O/B FLAP O/B HINGE I/B ACTUATOR BORE FOUND CORROSION. SNRM N0588 - RIGHT WING- O/B FLAP O/B HINGE I/B ACTUATOR BORE REPAIRED AS PER FEDEX EA 1-5750-69373, TITLE: WINGS- TRAILING EDGE FLAP- OUTBOARD TRAILING EDGE FLAP- SUPPORT BRACKETS- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030403000672003040300067NM 2003 4 3 AWXA200300329 120030324A5320654860713 WEB BOEING737 7373G7 1384595NM WING-BODY FAIRINCRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING LOWER STRUCTURE WEB, BS 530. MAINTENANCE CUTOUT DAMAGED SECTION OF R/H WING TO BODY FAIRING LOWER STRUCTURE WEB AT BS 530; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, FIG. 1, PG. 1-3. 2L72 4F RTA16WE 20030821001702003082100170NM 2003 8 21 03FDEA01032 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 FRAME DENTED BS 520 STR 24L. INSPECTED DENTS AT BS 520, STR 24L. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, FIG 1, DETAIL II, NOTE [S]. CUT OUT AND REPAIRED DAMAGE PER SRM 51-40-3, FIG 1. 2L73 4F RTA3WE 20030401001622003040100162WP 2003 4 1 DHL2003804771 120030310A57525642831504 TAB DOUG DC8 DC873F 302199FWP RT AILERON DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 REMOVAL/INSTALLATION OF RT AILERON CONTROL TAB DUE TO DELAMINATION ON LOWER SKIN. R & R RT AILERON CONTROL TAB IAW 27-11-4 PG. 201 -205 REFER TO N/R 0607 FOR OPS CHECK 2L74 4F RT4A25 20030408000292003040800029SO 2003 4 8 SIMA200302703 120030127A335078811 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21719AE 145276 BOS - FLT 9300 - CREW REPORTED AN EMERGENCY FLOOR LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 LIGHT STRIP IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030408000862003040800086NM 2003 4 8 03FDEA00395 120030407A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 N00566 CORROSION TASK NR C53-111-01(3) CORROSION ON STR 29 LT (KEELBEAM) 2L73 4F RTA3WE 20030410000882003041000088 2003 4 10 SWAA030660 420030322A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030415000812003041500081EA 2003 4 15 CA030328007 220030314A8530 PISTON PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT ENGINE MELTED W A UNSCHED LANDING EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 CA (CAN) DURING FLIGHT THE PILOT NOTICED AN OIL LEAK COMING FROM THE RT ENGINE. INVESTIGATION FOR THE CAUSE REVEALED THAT CYLINDER NR 5 HAD NO COMPRESSION. ONCE THE ENGINE WAS REMOVED, WE NOTICED THAT THE PISTON MELTED AND HAD BROKEN SEGMENTS. WE REPLACED THE CYLINDER, PERFORMED A GROUND RUN AND EVERYTHING SEEMED NORMAL. 1L72 3O3 O A20SO E14EA 20030410001152003041000115SO 2003 4 10 SIMA200300802 120030104A5313 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21654AE 145437 ABI - DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, REV 20) 53-24-02, AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030416000262003041600026NM 2003 4 16 UPS03440005 120030108A3350 BATTERY PACK BOEING747 747200 1384847NM EMERGENCY SIGN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: PFLT, EMERGENCY EXIT SIGN ABOVE ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK. 2L74 4F RTA20WE 20030416001932003041600193NM 2003 4 16 AALA20030287 120030305A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21369AA 25196 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25H INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR UNDER SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20060801000822006080100082WP 2006 8 1 IXXA060543S 120030906A5754 ANGLE DOUG DC8 DC871F 302199DWP ZONE 600 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND THREE FASTENER HEADS SHEARED ON THE RIGHT WING CENTER LEADING EDGE BOTTOM AFT OF THE END OF INBOARD SLAT. REMOVED DAMAGED ANGLE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS IAW DC8 SRM 51-1-8, 51-1-21, AND DOUGLAS DRAWING 5769891. 2L74 4F RT4A25 20060801001122006080100112WP 2006 8 1 IXXA060562S 120030922A5712 RIB DOUG DC8 DC871 302199AWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE LOWER SURFACE RIB CRACKED AT STATION 341. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 51-1-8, 51-3-0, AND 57-3-3. 2L74 4F 4A25 20060802000752006080200075WP 2006 8 2 IXXA060494S 120030123A5240 INTERCOSTAL DOUG DC8 DC871F 302199DWP SERVICE DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C-CHECK, FOUND RIGHT AFT SERVICE DOOR MID INTERCOSTAL CRACKED. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-20, 51-1-8, 51-1-21, AND DOUGLAS DRAWING 5772639. 2L74 4F RT4A25 20060802000762006080200076WP 2006 8 2 IXXA060495S 120030123A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 100 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C-CHECK, FOUND SEAT TRACK "B" GOUGED AT STATION FS 400. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-3, AND 51-1-8. 2L74 4F RT4A25 20060802001082006080200108WP 2006 8 2 IXXA060496S 120030123A5310 DOUBLER DOUG DC8 DC871F 302199DWP ZONE 100 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND FORWARD LOWER AIR CONDITIONER ACCESS DOOR INTERNAL DOUBLER REQUIRES REPLACEMENT DUE TO MANY PREVIOUS REPAIRS. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, DOUGLAS DRAWING 5613836, AND TIMCO REPAIR ENGINEERING ORDER REO-G09011 DATED 1/28/2003. 2L74 4F RT4A25 20060328002032006032800203SO 2006 3 28 MASA200300519 120031228A2700 UNKNOWN EMB 145 EMB145LR 3260212SO UNKNOWN A MASAH DEACTIVATE SYST/CIRCUITS P NO WARNING INDICATION DEDESCENT 1 SW07860MJ 145773 ASH 2609 - PITCH OSCILLATIONS IN YOKE AT 200KIAS DURING DESCENT WITH AP ENGAGED. FLAPS UP, GEARUP. PERFORMED GVI OF FLIGHT CONTROL SYSTEMS AND CHECKED CABLE TENSION. ALL CHECKED GOOD. MX COULD NOT DUPLICATE. NO PARTS USED. 2L72 4T RTT00011AT 20070309000032007030900003NE 2007 3 9 DJFA2006372 220031018A73216047T74P13 FUEL CONTROL CNDAIRCL600 CL6001A11 1900302EA GE CF34 CF343A 30015NE NR 2 ENGINE UNKNOWN E DJFAB EMER. DESCENT X ENGINE FLAMEOUT CRCRUISE 1 EA23602CW 3002 350102 AT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESCENDED AND AT FLIGHT LEVEL 100 FT THEY WERE ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FURTHER PROBLEMS. 2L72 4F4 FRTA21EA E15NE 20070406001732007040600173NM 2007 4 6 AT0700021 120030930A5330591140047 SKIN BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15949AT 55003 RIGHT HAND FUSELAGE SKIN DAMAGED STA 37 TO STA 110. INSTALLED NEW SKIN PANEL FROM STA 37 TO STA 110, BETWEEN L18R AND L27R AS PER DWG 5911400 AND B717 SRM 51-40-2. 2L72 4F TRA6WE 20070412001302007041200130NM 2007 4 12 AT0700047 120030930A5330 SKIN BOEING717 717200 1383700NM BS 256 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15947AT 55010 FUSELAGE DENT FWD OF STATION 256 ABOVE STR 18 L. D=2.0 X .075. FOUND TO BE WITHIN LIMITS PER B717 SRM 53-00-01 CONDITION 2. REQS REPETITIVE INSP AT C-CHECK INTERVALS. INSTALLED SKIN REPAIR AT FUSELAGE AT FWD OF STA 256 ABOVE STR 18L IAW AND B717 SRM 53-00-01 FIG 201. MATERIAL USED 2024 T3 .050, 35.5 X 14 INCH FOR FINGER, 2024 T3.025 FOR DOUBLER AND 2024 T3 .050, 35.5 X 4 INCH. 2L72 4F TRA6WE 20070412001242007041200124NM 2007 4 12 AT0700028 120030502A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15944AT 55007 AIRCRAFT STRUCK BY BAG CART ON AIRCRAFT RIGHT AFT OF RIGHT ENGINE ON EMP. INSTALLED FLUSH SKIN REPAIR AT FRAMES 1059 AND 1076 BETWEEN LONGERON 24L AND 24R IAW SRM 53-00-01 FIG 201 AND SRM 51-70-11 FIG 201. MATERIAL USED 7075-T6 .040 MFG LOT 26911, 7075-T6 .050 MFG LOT 708-411 AND 6AL4V .32 LOT NO PQ0LXF61, HEAT TREATED TO 7075-T6 PER GENERAL PROCESS SPECIFICATION 98PS.247PS-01. 2L72 4F TRA6WE 20070702001912007070200191NM 2007 7 2 ZZDA031119180 120031119A2150 CHECK VALVE BOEING717 717200 1383700NM CABIN AIR MALFUNCTIONED A ZZDAO OTHER O OTHER CRCRUISE 1 SO15949AT 55003 RIGHT PAC FLO DISAGREE, AMBER PACK ALERT. AFT CABIN TEMP GOT HOT, ESPECIALLY IN AFT LAV, PACK SHUT DOWN. TEMP COOLED, INSULATION BLOWN AROUND BACK OF AIRCRAFT. REMOVED AND REPLACED COND AIR CHECK VALVE ASSY, OPS LEAK CHECK GOOD. REF TO 21-22. 2L72 4F TRA6WE 20030429001472003042900147NE 2003 4 29 CA030306006 220030225A7200 ENGINE PWA PT6 PT6A67D NE FAILED W O OTHER O OTHER NRNOT REPORTED 1 CA 13226 (CAN) ENGINE WAS REMOVED AFTER A SUSPECTED NR 3 BEARING FAILURE AND OIL CONTAMINATION (METAL IN OIL). REPLACED THE CT DISK & PT DISKS AND TO OVERHAUL BOTH THE GG-PS 0090 & THE POWER SECTION. THIS FINAL REPORT COVERS THE FINDINGS ON THEPOWER SECTION - PS0095, A SEPARATE FINAL REPORT IS BEING ISSUED FOR THE GG SECTION(PS0090)-PT6A-2002-018.IT IS CLEAR NR 3 BEARING SUFFERED FROM ONE OR TWO ROLLERS BECOMING JAMMED IN THE CAGE WHICH SUBS EQUE3NTLY SKIDDED ON THE INNER AND OUTER RACES WEARING THEMSELVES & THE RACEWAYS & GENERATING METAL PARTICLES. THESE WERE GATHERED BY THE SCAVANGE OIL AND PICKED UP IN THE CHIP DETECTOR AND SCAVENGE STRAINERS. 4 T E26NE 20040105000742004010500074EA 2004 1 5 RAG2003F00000 220031023A8520559E SCREW LYC R680 R68013 41540EA MASTER ROD BROKEN B RAQRO OTHER O OTHER NRNOT REPORTED 1 SW15 12642 SB NR 126, 41.146 HAD NOT BEEN COMPLIED WITH. KNUCKLE PINS BACKED OUT OF THE MASTER ROD, HIT THE CRANKSHAFT AND CAUSED A CATASTROPHIC ENGINE FAILURE. CRANKSHAFT SEIZED AND BROKE JUST AFT OF THE PROPELLER. PROPELLER DEPARTED THE AIRCRAFT AND PILOT WAS FORCED TO MAKE AN EMERGENCY LANDING IN A PLOWED FIELD. (SW15200402816) 3 R E202 20030214000132003021400013NE 2003 2 14 2003F00099 320030116A61117756722 PIN HAMSTD 14SF15 HAMSTD14SF 14SF15 NE BLADE PIN MISINSTALLED B NQ3RK NONE W INADEQUATE Q C ININSP/MAINT 1 NM01 6620 86242315 AFTER REMOVING THE BLADE PIN SETSCREW THE BLADE PIN WAS SO LOOSE THAT IT COULD BE REMOVED BY HAND. THE ID OF THE SLEEVE BUSHING IS OVAL AND MATERIAL IS PUSHED TO BOTTOM OF BORE. THIS IS THE FIRST TIME WE HAVE SEEN THIS SINCE THE REQUIREMENT FOR THE BLADE PIN RETENTION TEST WAS INTRODUCED. THE BUSHING SLEEVE IS PRESS INTO THE BLADE AND THEN THE BLADE PIN IS PRESS INTO THE BUSHING SLEEVE AND THE ASSEMBLE SHOULD WITHSTAND A 200 INCH-POUNDS PULL TEST. 6 CP7NE 20030815000402003081500040 2003 8 15 HEEA088608 420030728A34427007700614 DISPLAY BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 SCREEN FADES OUT. FOCUS IS NOT SHARP, INSTENSITY IS DIM. 1G72 4U H4SW 20030819000572003081900057CE 2003 8 19 DXTA200300060 120030706A2120 ODOR CESSNA500 560CESSNA 2076750CE CABIN DETECTED E DXTAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 GL07333QS 5600333 ACM PRODUCING OILY ODOR AS TEMPATURE SET TO WARMER TEMPERATURE. PERFORMED OPS CHECK OF ACM AT VARIOUS POWER SETTINGS, THRU FULL TEMPERATURE RANGE IN BOTH AUTO AND MANUAL MODES AND SELECTING DIFFERENT BLEED AIR SOURCES. ACM APPEARS TO FUNCTION NORMAL, COULD NOT DUPLICATE OILY ODOR. 2L72 4F RTA22CE 20030820000862003082000086NM 2003 8 20 03FDEA00834 120030526A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LT WING - OUTBOARD TRAILING EDGE FLAP, AFT INBOARD FLAP-HINGE FITTING FOUND PIVOT BEARING, INBOARD HOLE BUSHING LOOSE, WORN (FLAP SIDE). REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69347 - WINGS - LT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030328000742003032800074NM 2003 3 28 CH1A200381009 120030323A3350 COVER BOEING727 7272S7 138407ZNM EMERGENCY LIGHT MISSING A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 EMERGENCY EXIT LIGHT IN OVERWING EXIT IS MISSING COVER A/C LEFT 2L73 4F A3WE 20030821001222003082100122NM 2003 8 21 03FDEA00873 120030522A5753ARC70531 SUPPORT DOUG MD11 MD11 3023602NM T/E FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LEFT WING - OUTBOARD TRAILING EDGE FLAP VANE FOUND NR 1 VANE TRACK SUPPORT FWD MOST MOUNT HOLE BORE SURFACE CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-71713 - WINGS - LEFT OUTBOARD FLAP VANE - NR 1 VANE TO TRACK SUPPORT CORRODED. 2L73 4F RTA22WE 20030328000932003032800093CE 2003 3 28 CWQ2003F00002 120030122A21206512072101 DUCT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA SCOOP MISOVERHAULED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05309QS 5600509 DURING INSPECTION, LOOKED INTO DORSAL NACA SCOOPS,MATERIAL MISSING FROM AIR VANES PN 6512072-11, 6512072-12 LOCATED IN TRANS DUCT MISSING MATERIAL LOCATION WAS A CONCERN BECAUSE ITS ONLY ROUTE WAS TO END UP IN VENT J-BOX (AIR MIXING BOX) WHERE IT WOULD HAVE PASSED CABIN PRESS, FRESH AIR CHECK VALVE (POSSIBLY WEDGING VALVE OPEN) THIS WOULD HAVE NOT ALLOWED A/C TO HOLD PRESS. 1ST PIECE WAS FOUND WEDGED IN CHECKVALVE (VALVE COULD NOT SEAL) 2ND PIECE WAS FOUND PAST OVERHEAD BLOWER WEDGED IN DUCT WORK (NO DAMAGE TO BLOWER CAGE). LOCATED BROKEN PARTS REMOVED, REPLACED BROKEN PARTS WITH NEW. CLOSED UP CABIN INTERIOR AND DUCT WORK. REASSEMBLED TAILCONE DUCTING. CHECKVALVE WAS SERVICEABLE REINSTALLED. 2L72 4F4 FRTA22CE E25EA 20030404000332003040400033NM 2003 4 4 03FDEA00377 120030402A5597 WIRE HARNESS DOUG MD11 MD11 3023602NM ZONE 300 BURNED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 HORIZONTAL STABILIZER CENTER SECTION TOP- WIRE BUNDLE AT THE RT INBOARD SIDE, INSIDE THE AFT FUSELAGE COMPT, FOUND BURNED AND DAMAGED DURING FSC RETURN-TO-SERVICE TEST. 2L73 4F RTA22WE 20030402000292003040200029NM 2003 4 2 2003UALA00236 120030302A2780755299B ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLATS WORN A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29571UA3530035300 26681 WHILE PLACING FLAPS IN UP POSITION, LEADING EDGE SLAT DISAGREE INDICATION CAME ON. INHIBITED SLAT MOVEMENT DUE TO FAULTED NR 11 LEADING EDGE SLAT ACTUATOR. REMOVED AND REPLACED THE SUBJECT LEADING EDGE SLAT ACTUATOR WITH NEW SERVICEABLE ACTUATOR 2L72 4F4 FRTA2NM E17NE 20030410000252003041000025NM 2003 4 10 SWAA030602 120030316A575465C2660389 DOUBLER BOEING737 7373L9 1384470NM L/E SLAT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 A 4 X 6 INCH PREVIOUS REPAIR MISSING AT NR 3 L/E SLAT UPPER SURFACE. REMOVED AND REPLACED NR 3 L/E SLAT PER MM. 2L72 4F RTA16WE 20030415000032003041500003SW 2003 4 15 CA030220001 120030214A5620205903100 WINDOW BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA PAX CABIN MISSING W O OTHER D INFLIGHT SEPARATION DEDESCENT 1 CA (CAN) HELI SKIING: HELICOPTER WAS UP IN AN ALPINE LANDING PAD. THE PASSENGERS HAVE BEEN ON LOADED FROM THEHELICOPTER. THE HELICOPTER SKIING GUIDE ON THE RIGHT SIDE OF THE HELICOPTER GAVE THE SIGNAL TO TAKE OFF. THE HELICOPTER TOOK OFF AND DESCENDED DOWN THE HILL. ENROUTE DESCENT A LOUD NOISE OCCURRED AND THE LOSS OF THE POP OUT WINDOW OCCURRED. THE PILOT LANDED AT THE HANGAR. 1G71 4U4 U H4SW E22EA 20030407000792003040700079EU 2003 4 7 SIMA200306202 120030225A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY DIRTY A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21374AE 340B374 DFW - FLT 3533 - CREW REPORTED THE AVIONICS SMOKE DETECTOR LIGHT ILLUMINATED FOR 30 SECONDS IN FLIGHT THEN WENT OUT. AIRCRAFT WAS RETURNED TO DFW. MAINTENANCE FOUND THE AVIONICS SMOKE DETECTOR DIRTY. DETECTOR WAS CLEANED AND AN OPERATIONAL CHECK COMPLIED WITH. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030416002542003041600254SO 2003 4 16 C2XA03SH095 120030408A531514526437001 BUTT STRAP EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 DURING C CHECK LAVORATORY'S FLOORBEAMS UPPER SURFACE WHERE FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED BUTTSTRAPS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030417001722003041700172NM 2003 4 17 UPS03440164 120030212A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: SPV, AFT CARGO BAY, STR 34L CRACKED AT BS 1660 (1 INCH) & BS 1720 (0.875 INCH) AT FRAME ATTACH AREA. STRINGER 34L AT BS 1660 & 1720 REPAIRED IAW SRM 53-10-03 FIG 2. 2L74 4F A20WE 20030422000962003042200096SO 2003 4 22 SIMA200307103 120030216A532014522461011 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW215100 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION GALLEY AFT DIAMOND HAS CORROSION. REMOVED AND INSTALLED NEW GALLEY AFT DIAMOND IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M) 2L72 4F RTT00011AT 20030424001542003042400154SO 2003 4 24 ZLW2003F00000 120030304A53151159B2047827 FLOORBEAM GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU FUSELAGE CRACKED E ZLWAO OTHER O OTHER NRNOT REPORTED 1 SW15622RR11488 12 DURING A ROUTINE CABIN BELOW FLOOR INSPECTION, IT WAS FOUND THAT THE AFT FLOORBEAM SECONDARY SUPPORT WAS CRACKED. A NEW PART IS AVAILABLE FROM MFG AND WILL BE INSTALLED PRIOR TO FURTHER FLIGHT. 2L72 4F4 FRTA12EA E2EU 20030423001952003042300195WP 2003 4 23 UPS03840291 120030315A3397 CIRCUIT BREAKER DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS 7.5 A C/B BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT C/B WITH NEW C/B. REF WDM 33-50-01, OPS CHECKS GOOD. 2L74 4F RT4A25 20030425000012003042500001WP 2003 4 25 UPS03840378 120030322A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, A/C ACCESSORY COMP BETWEEN STA 55 TO 70 BETWEEN LONG 35L TO 35R FRAME 55 IS CORRODED. REMOVED DAMAGED FRAME SECTION FROM L35R-L27L. FAB REPAIR ANGLES AND FRAME SECT IAW DC8 SRM 53-2-0. HEAT TREAT ANGLES & FRAME SECTION IAW TPS 1003 REV A. ALODINED & PRIMED REPAIR ANGLES AND FRAME SECTION IAW DC8 S RM 51-1-8. INSTALLED REPAIR ANGLES AND FRAME SECTION IAW DC8 SRM 53- 2-0 FIG 2 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20030515001222003051500122 2003 5 15 AWXA200300526 420030512A3414 CIRCUIT BREAKER BOEING737 7373G7 1384595NM MASTER DIM TRIPPED A AWXAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 WP28158AW 23780 AIR TURNBACK - AFTER TAKEOFF FROM LAS EN ROUTE FOR DEN EXPERIENCED SPEED LIMIT / MACH TRIM AUTO SLAT FAIL, THERE WERE NO INDICATIONS, NO RECALL, AND NO LIGHT WHEN LIGHT WAS TESTED. TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE MASTER DIM CIRCUIT BREAKER POPPED BEHIND FIRST OFFICERS SEAT. RESET CIRCUIT BREAKER, ALL LIGHTS AND INDICATIONS OPERATED NORMALLY. 2L72 4F RTA16WE 20030530001022003053000102EA 2003 5 30 CA030505007 120030505A5534C6TP103927 SPAR DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING CHANGE OVER TO FLOATS, CRACKS WERE OBSERVED UNDER THE FORWARD ATTACHMENT POINT. NEW SPAR MANUFACTURED. NO PARTS AVAILABLE FROM MANUFACTURE. 1H72 3T4 TRTA9EA E4EA 6 CP15EA 20030529000022003052900002NM 2003 5 29 2003F00324 120030119A2611CM376AS15 BULB DHAV DHC8 DHC8103 1386005NM SMOKE DETECTOR MALFUNCTIONED A KPVAO OTHER N FALSE WARNING APAPPROACH 1 WP13808WP 026 INTERMITTENT SMOKE WARNING LIGHT. NO OTHER INDICATIONS OF SMOKE OR FUMES. LIGHT COMES ON FOR 1-2 SECONDS THEN OUT. TROUBLESHOT SYSTEM AND DEFERRED PER MEL 26-8-1. DEACTIVATED NR 1 SMOKE DETECT SYSTEM AND SECURED. PLACARD INSTALLED. OPNE 2/19/03 CAT C DUE 3/1/2003. CLEAR MEL 26-8-1. REMOVED NR 1 SMOKE DETECTOR BY REMOVING 6 SCREWS AND CONNECTOR PLUG. REMOVED AND REPLACED BULB IN BEACON LAMP ASSY WITHIN THE SMOKE DETECTOR ASSY IAW PYROTECTOR INC COMPONENT MM 26-10-21 PAGE 7. REINSTALLED NR 1 SMOKE DETECTOR BY REINSTALLING 6 SCREWS AND CONNECTOR PLUG. OPS CHECK GOOD IAW DHC-8 MM 26-12-00. RESET CIRCUIT BREAKER AND REMOVED PLACARDS. 2H72 4T RTA13NM 20030602001072003060200107NM 2003 6 2 SWAA031175 120030524A3350BR2013 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 EEPLS SECTION LOOSE NEAR GALLEY. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030605000112003060500011NM 2003 6 5 AUS20030436 120030423A29127592113101 FILTER BOEING737 7377BX 13844D2NM GE CFM56 CFM567B24 NE HYD SYSTEM CONTAMINATED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) HYDRAULIC SYSTEM PRESSURISATION MODULE FILTER CONTAMINATED WITH WATER. 2L72 4F4 FRTA16WE E00055EN 20030605000692003060500069 2003 6 5 MEX2003154 420030503A22103927141 VALVE DOUG MD80 MD83 3023681NM LEFT FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23491SH 49150 DURING COCKPIT CHECK THE CAPTIAN FOUND PROBLEMS WITH (AUTO LAND) BUTTON AND LEFT PRESSURE REGULATOR VALVE. THE BUTTON WAS DEFERRED BY MEL CATEGORY C AD THE VALVE WAS REPLACED IAW MM. 2L72 4F RT 20030609000882003060900088EA 2003 6 9 QXEA0300641 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED ON STRINGER 11R, 4 INCHES FORWARD OF FS 893. REPAIRED IAW SRM 51-25-16. PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030611001662003061100166EA 2003 6 11 SWIA200312008 120030526A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07597SW 7293 BOTTOM PAX DOOR LIGHT INOP. REMOVED AND REPLACED BOTTOM (LOWER) PASSENGER DOOR BOARDING LIGHT IAW MM 33-23-04. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030611001322003061100132EA 2003 6 11 ASOA03201 120030513A2710272955 LINK CNDAIRCL600 CL6002B19 1900309EA AILERONS WORN A ASOAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 SO11829AS 7232 FLT 4690 - DURING CLIMB-OUT FROM ATL-YUL, AT APPROXIMATELY 5,000 FEET THE CREW NOTICED A CYCLICAL VIBRATION IN THE AIRFRAME WITH THE AIRCRAFT VIBRATING ABOUT 45 TO 60 SECONDS EACH TIME, FOR ABOUT 1 TO 2 SECONDS, WHICH WAS VERY DEEP IN FREQUENCY. WHILE THE CREW WAS COMPLYING WITH QRH PROCEDURES SHORTLY AFTER DISENGAGING THE AUTOPILOT AT APPROXIMATELY 17,000 FEET, THE AIRCRAFT ROLLED VIOLENTLY TO THE RIGHT AND WITHIN 15 TO 30 SECONDS IT ROLLED AGAIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CHA, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD POWER CONTROL UNIT OUTPUT LINKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030523000562003052300056NM 2003 5 23 SWAA031117 120030519A53206547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 868, RT SIDE AND BS 727B, LT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030527000872003052700087WP 2003 5 27 AALA20030314 120030315A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217537A 49991 DURING OVERNIGHT MAINTENANCE, AFT ZONE SEAT MOUNTED EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030617002332003061700233 2003 6 17 BAQA086809 420030605A221111788292 COMPUTER BOLKMS117 BK117A1 5626010EU SPAS WILL NOT TEST H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME406 7243 SPAS COMPUTER WILL NOT TEST. REPLACED WITH REPAIRED, SERVICEABLE UNIT. 1G72 3U H13EU 20030618001762003061800176SW 2003 6 18 HEEA087514 120030613A6230206033554101 LINK BELL 206 206L3 1182108SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 LINK ELASTOMER SEPERATED. REPLACED. 1G71 3U H2SW 20030521001822003052100182WP 2003 5 21 DHL2003804877 120030210A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING L/E UPPER SKIN CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030103, ED-3213. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON LT WING L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EODHL 030103, ED-3213. FABRICATED A REPAIR DOUBLER (7075T6AL 0.063), FILLER (7075T6AL-0.050) IAW EODHL 030103, ED-3213. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER AT LT WING L/E UPPER SKIN WITH NEW FASTENERS IAW EODHL 030103, ED-3213 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030522000862003052200086WP 2003 5 22 GTIA030300 120030501A3210 BOLT DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE RT MAIN GEAR MISSING A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23816NK 49140 RIGHT MAIN GEAR UNSAFE LIGHT CAME ON IN FLIGHT. FOUND BOLT MISSING FROM TARGET ALIGNMENT. RE-SECURED AND OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20030416001712003041600171NM 2003 4 16 DL76P030316 120030401A3350 CHARGER BOEING767 767332 1382001NM EMERGENCY LIGHTSINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27143DA 25991 POWER CHARGER FUSE BAD AT FWD 2A FLOOR PANEL. REPLACED WITH GOOD CHARGER DAL PART 333780100, S/N 44099, REPLACED WITH S/N 51658.E344. 2L72 4F RTA1NM 20030424001332003042400133WP 2003 4 24 UPS03840356 120030324A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 EMERGENCY LIGHTS BATTERY LOW (LIGHTS WILL NOT STAY ON) 5 SEC MAX. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-00. 2L74 4F RT4A25 20030429000302003042900030NM 2003 4 29 P5CA0300807 120030206A5730 SKIN BOEING747 747283B 1384867NM RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RIGHT WING L/E LWR SURFACE STA 1380-1385 FOUND CORROSION IN LWR SURFACE. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH DOUBLERS PER SRM 57-30-03 FIG -9. 2L74 4F A20WE 20030501001542003050100154WP 2003 5 1 ASAA0380126 120030209A5320S000925 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OAK - DURING C-CHECK, FOUND AFT CARGO BAY CIRCUMFERENTIAL FLOORBOARD SUPPORT CRACKED. CUTOUT DAMATED AREA AND INSTALLED DOUBLER AT FS 1079, L27L-L28L PER SRM 53-01, 51-10-4, AND 51-30-2. (M) 2L72 4F RTA6WE 20030506000272003050600027NM 2003 5 6 03FDEA00526 120030418A5753 FAIRING BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT WING NR 8 FLAP TRACK MOVABLE FAIRING EXTERNAL SKIN CRACKED AT FORWARD INBOARD EDGE. REPAIRED FAIRING IAW BOEING 727-200 SRM 57-20-04. 2L73 4F RTA3WE 20030506001262003050600126NM 2003 5 6 DHL2003746007 120030422A2612106087712 FIRE DETECTOR BOEING727 727224 1384076NM NR 1 ENGINE MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01746DH 22252 NR 1 ENGINE FIRE DETECTION SYSTEM-A UNABLE TO TEST. NR 1 ENGINE OVERHEAT AND FIRE DETECTION SYSTEM-A DEFERRED PER MEL 26-6 CAT-C. DMI 12653 PLACARD INSTALLED. REF DMI 12653 1 ENGINE FIRE DETECTION SYSTEM-A UNABLE TO TEST. REMOVED AND REPLACED FIRE DETECTION POWER UNIT SYSTEM, OPS CHECKED BAD PER GMM 26-11-1. DMI 12653 REMAINS OPEN. REINSTALLED ORIGINAL POWER UNIT. REF DMI 12653 NR 1 ENGINE FIRE DETECTION SYSTEM-A UNABLE TO TEST. REMOVED AND REPLACED NR 1 ENGINE FIRE WALL SENSOR RESPONDER WITH SERVICEABLE UNIT. OPS CHECKED GOOD IAW M/M 26-11-31. THIS CLEARS DMI 12653. 2L73 4F A3WE 20030513001872003051300187SO 2003 5 13 SWIA200311896 120030421A323012043270501 RELAY EMB 120 EMB120ER 3260203SO MLG MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07187SW2011 2011 120037 DURING FLIGHT, RIGHT MAIN ''A'' GREEN LIGHT ILLUMINATED. GEAR WOULD NOT EXTEND - ALL THREE GEAR RED LIGHTS ILLUMINATED EXCEPT RIGHT ''A'' RED WITH HANDLE DOWN. AFTER 5 MINUTES THE PROBLEM FIXED ITSELF AND THE GEAR LOWERED NORMALLY. REPLACED LANDING GEAR RELAY BOX IAW 32-31-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20030513002452003051300245EA 2003 5 13 A6WA200340059 120030411A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 THE LEFT CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621, LBL 36, WL 73. REMOVED CRACKED SECTION OF ANGLE AND INSTALLED REPAIR ANGLES IAW BOMBARDIER INC REO 601R-53-61-117 REV B. (M) 2L72 4F RTA21EA 20030515000142003051500014SO 2003 5 15 SWIA200311937 120030504A2150 A/C PACK EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AIR CONDITIONINGOVERHEATED A SWIAO OTHER MBJOVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 NM07290SW 120317 LAV SMOKE DETECTOR ALARM SOUNDS CONTINUOUSLY. PACKS APPEAR TO HAVE BEEN OVERHEATED. COOLED DOWN PACKS. NO VISIBLE SMOKE IN CABIN, BUT COULD SMELL PACKS BEFORE COOLING DOWN. LAV SMOKE DETECTOR CHECKED GOOD AFTER CABIN CLEARED OF PACK ODOR. CHECKED A/C PACK GROUND COOLING FAN AND RAN PACKS. PACKS CHECKED NORMAL. FOUND APU TO BE DEFECTIVE AND PUTTING OIL INTO BLEED LINES. REMOVED AND REPLACED APU IAW EMB120 MM 49-00-02. 2L72 4T4 TRTA31SO E20NE 20030604001102003060400110NM 2003 6 4 UPS03440525 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 760 LT STR 15L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35 AT BS 760 BETWEEN STR 14L TO 17L. 2L74 4F A20WE 20030604002112003060400211WP 2003 6 4 UPS03840630 120030416A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE MISREPAIRED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, MAIN CARGO DOOR OPENING AFT LOWER CORNER STA. 270 HAS A STAINLESS STEEL DOUBLER THAT DOES NOT COMPLY IAW DC8-5330-12800-D LONG. 20L-21L APPROX. REMOVED EXISTING REPAIR,NDT VERIFIED NO CRACKS AROUND EXISTING CUTOUT,FABRICATED DOUBLERS AND FILLER I.A.W SRO8530027 2L74 4F RT4A25 20030520001202003052000120NM 2003 5 20 USAABB03066 120030427A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU 22198 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROW 1 INOPERATIVE. MAINTENANCE REPLACD THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030609000282003060900028SO 2003 6 9 C2XA03TY075 120030521A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713903 145479 DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND 51-21-04,05, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION 2L72 4T RTT00011AT 20030521000252003052100025WP 2003 5 21 DHL2003804891 120030208A57205769933184 VANE DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT OUTBOARD SLOT VANE AT STA XOLDI6.224 HOLES ELONGATED (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030105,ED-3210. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030105, ED-3210. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075-T6-0.071) AND A FILLER (7075-T6-0.063) IAW EODHL-30105, ED-3210. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER AT RT OUTBOARD SLOT VANE STA XOLDI6.224 WITH NEW FASTENERS IAW EODHL-30105, ED-3210 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000962003052100096WP 2003 5 21 DHL2003801035 120030409A5730 SKIN DOUG DC8 DC873F 302199FWP LT STUB WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT INBOARD STUB WING LWR SURFACE DOUBLER WITH 0.500 INCH CRACK IN STA XFS 260.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1A PG 3 FIG 1. REMOVED DAMAGED DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075-T6 AL0.080) IAW SRM 57-2-1A PG 3 FIG 1. CLEANED, TREATED AND PRIMED DOUBLER INNER SIDE IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-1A PG 3 FIG 1, SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030530000072003053000007SW 2003 5 30 HEEA086669 120030522A2822205060606003 PUMP BELL 412 412 1182202SW FUEL BOOST NOISY E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW032261D 33076 FUEL BOOST PUMP IS EXCESSIVELY NOISY. 1G72 4U H4SW 20030630000602003063000060SW 2003 6 30 ALGA087760 120030625A6520407340032101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL TRANSMISSION FAILED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03687AL A388 53366 TAIL ROTOR TRANSMISSION REMOVED FOR METAL IN OIL, FOUND BEARING BREAKING DOWN. SUBMITTED BY: PRESTON BARZARE 1G71 3U3 UO H2SW E1GL 20030625000552003062500055NM 2003 6 25 03FDEA00750 120030513A5753NRC6066 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING, O/B FLAP I/B HINGE (FLAP HINGE SIDE) FWD ATTACHING POINT, O/B AFT BOLT HOLE CORRODED. SNRM N1126 - LT WING- O/B FLAP I/B HINGE (FLAP HINGE SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE REPAIR CARRIED OUT IAW E.A. 1-5750-68413 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030702000302003070200030NM 2003 7 2 TSAA0333113 120030503A3350 BATTERY PACK BOEING737 7372M6C 1384708NM PAX CABIN INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030701000222003070100022SW 2003 7 1 HEEA087876 120030614A291070061H000V112A LINE BELL 407 407 1182206SW HYD DIST CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 HYD LINE HAS DEVELOPMENT OF CORROSION UNDER SLEEVE DUE TO DISSIMILAR METALS USED DURING MANUFACTURE PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030707000782003070700078NM 2003 7 7 DL738030595 120030628A5210 DOOR BOEING737 737832 13844CFNM PAX OUT OF ADJUST A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27393DA 30377 AFT ENTRY DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL BELOW 75 KTS. C/A: ADJUSTED DOOR IAW TASK 52-13-820-802. 2L72 4F RTA16WE 20030630000492003063000049SW 2003 6 30 HEEA087832 120030614A5410206064819006 DOOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL INTAKE COWL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 INTAKE COWLING DOOR IS CORRODED AND CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030707000572003070700057NM 2003 7 7 AALA20030634 120030602A2434 GENERATOR BOEING767 767323 1385205NM LEFT ENGINE FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21363AA 24044 LEVEL AT 310 LT GEN DRIVE LIGHT FLICKERED AND THEN CAME ON STEADY. ROAR HEARD AND VIBRATION FLET. DISCONNECTED THE IDG AND RETURNED TO SCL. PLACARDED INOPERATIVE LEFT ENGINE IDG PER MEL 24-1 AUTH 6-49DC-A, ENTERED IN MIC SHEET AND MPM 24-1 ACCOMPLISHED SERVICING LT/RT AND APU IDGS, CHECKED HISTORY NONE FOUND. REPLACED LEFT ENGINE IDG AS PER AMM 24-11-01-4. RUNUP LEFT ENGINE AND CHECKED IDG FOUND TO BE OK. NO VIBRATION ON LEFT ENGINE DURING POWER RUNUP PER AMM. CLEARED MEL AND MIC. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA1NM 20030707001402003070700140EU 2003 7 7 DHL2003364010 120030610A2610 CONNECTOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE CFD CONTROLLER DIRTY A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 IN PREFLIGHT CHECK MANIFOLD FAULT DETECT LOOPS BOTH IN (B) ILLUMINATED APU AND NR 2 ENGINE MANIFOLD FAULT LIGHTS. DEFERRED IAW MEL 36-12-03 REF. DMI NR 13215 IN PREFLIGHT CHECK, MANIFOLD FAULT DETECT LOOPS BOTH IN B ILLUMINATED APU AND NR 2 ENGINE MANIFOLD FAULT LIGHTS. CLEANED CONNECTOR TO CFD CONTROLLER. SYSTEM TEST GOOD IAW MM 26-16-00. THIS CLEARS DMI NR 13215. MAINTENANCE CONTROL NOTIFIED. 2L72 4F4 FRTA35EU E23EA 20030709000932003070900093SO 2003 7 9 GLBA2003080 120030609A3030M610619017 RELAY EMB 120 EMB120ER 3260203SO PITOT HEAT FAILED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 NM03299UX 120299 NR 2 PITOT/ STATIC HEAT FAIL. REMOVED AND REPLACED RELAY, OPS CHECKED GOOD. 2L72 4T RTA31SO 20030710001112003071000111SO 2003 7 10 C2XA03SH192 120030618A5315 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030714000662003071400066NM 2003 7 14 SWAA031368 120030616A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 5L. REPAIRED BULKHEAD PER SRM. 2L72 4F RTA16WE 20030108000642003010800064WP 2003 1 8 NACA20030067 120030103A7160 PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE A NACAE ENGINE SHUTDOWN M OVER TEMP TXTAXI/GRND HDL 1 AL0399330 NK510186 43576 NK510186 DISCREPANCY: #4 ENGINE SHUT DOWN DUE TO CARBURETOR HEAT APPROACHING RED LINE AFTER GOING INTO REVERSE.CORRECTIVE ACTION: INSPECTED CARBURETOR INTAKE FOR FOREIGN OBJECTS, NONE FOUND. INSPECTED AIR DOOR FOR SECURITY, FOUND SECURE. RAN ENGINE TO 30" AND A REVERSE CHECK, ALL PARAMETERS FOUND OK. SUSPECT ICING CONDITION WAS THE FAULT. 2L74 4R4 R A781 5E8 20030204000362003020400036NM 2003 2 4 SWAA030227 120030129A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 2L AND STR 3R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030207001272003020700127NM 2003 2 7 ZW0A0301502 120030202A3397 WIRE DOUG MD80 MD83 3023681NM CABIN LOOSE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139412W 53187 THE EGRESS FLOOR LIGHTING WAS INOPERATIVE FROM CABIN ROW 26 TO 30. SECURED LOOSE WIRE CONNECTION AT ROW 30. 2L72 4F RT 20030429002272003042900227NM 2003 4 29 SWAA030781 120030407A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C2 CHECK, FOUND RT OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20030429000802003042900080NM 2003 4 29 P5CA0300825 120030410A5414 ACCESS PANEL BOEING747 747283B 1384867NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 NR 3 PYLON STRUT ACCESS PANEL 453FL CUTOUT CRACKED. REPAIRED PER SRM 54-34-03 FIG 2.3. 2L74 4F A20WE 20030502001242003050200124SO 2003 5 2 SWIA200311878 120030414A3320 BALLAST EMB 120 EMB120ER 3260203SO LAVATORY BURNED OUT A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 NM07565SW 120340 THERE WAS AN ODOR OF SMOKE IN THE CARGO AREA AND IN THE AFT CABIN. THE SMOKE DETECTOR IN THE LAVATORY WENT OFF WHILE BOARDING PASSENGERS. INVESTIGATED AFT CABIN, FOUND LIGHT IN LAVATORY BALLAST BURNED OUT AND RELEASED SMOKE INTO AFT CABIN AND LAV. REPLACED BALLAST OF LAV LIGHT, OPS CHECK GOOD. 2L72 4T RTA31SO 20030502002202003050200220NM 2003 5 2 EIA2003058 120030414A5414 SKIN BOEING747 747212B 1384886NM NR 1 PYLON CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FRETTING CORROSION AT FWD EDGE OF NR 1 PYLON O/B SAILPLANE DOOR CUTOUT. TRIMMED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 486-54-017-2. 2L74 4F A20WE 20030505002592003050500259NM 2003 5 5 03FDEA00530 120030418A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT HAND FUSELAGE STA 277 FORWARD TOILET SERVICE PANEL LOWER SKIN HAS A DENT. REPAIRED IAW FED EX EA 7-5330-69463. 2L73 4F RTA3WE 20030506001242003050600124NM 2003 5 6 PCA0300852 120030411A5230 TORQUE TUBE BOEING747 747249F 1384849NM LWR DOOR DEFORMED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 THE 5 L DOOR BODY TORQUE TUBE LWR HINGE HALF FITTING DEFORMED. REMOVED AND REPLACED 51-30-02. 2L74 4F A20WE 20030505001192003050500119NM 2003 5 5 AWXA200300403 120030421A3350321430 BATTERY AIRBUSA319 A319132 3930340NM ZONE 242 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28805AW 1049 PHX - EEL - FLIGHT CREW REPORTED THE RT OVERWING EMERGENCY EXIT LIGHT WAS FLASHING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030506001352003050600135WP 2003 5 6 GTIA030181 120030302A5320 SUPPORT ANGLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 160 TO 168 LBL FLOOR SUPPORT CORRODED. DRILL UP NEW ANGEL SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030507000402003050700040EU 2003 5 7 AUS20030339 220030317A7200CFM563C1 ENGINE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU NR 2 FAILED W O OTHER EXJVIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 2 ENGINE FAILED. DURING CLIMB A LOUD THUD WAS HEARD AND A PASSENGER REPORTED A LARGE FIREBALL. ENGINE INDICATIONS WERE NORMAL. 2L72 4F4 FRTA16WE E21EU 20030513001432003051300143NM 2003 5 13 CH1A200395040 120030414A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON CABIN FLOOR SUPPORT AT LBL 12 BS 1050 TO BS 1070 2L73 4F A3WE 20030529000162003052900016EU 2003 5 29 AALA20030426 120030406A3397 WIRE FOKKERF28 F28MK0100 4990807EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW211472B 11514 DURING OVERNIGHT MAINTENANCE, WHILE REMOVING LEFT OVERWING EMERGENCY EXIT LIGHT AT WIRE BROKE OFF OF PIN. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030604000982003060400098NM 2003 6 4 UPS03440513 120030412A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2182 - 2186, STR 14L STRINGER END FOUND CRACK. STRINGER REPLACED AS PER SRM 51-10-01 . 2L74 4F A20WE 20030604001492003060400149NM 2003 6 4 UPS03440569 120030410A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FWD CARGO COMPT - STA 540 STR 46R TO 47R FRAME SHEAR TIE FOUND CRACKED. FWD CARGO COMPT BS 540 STR 46R - 47R FRAME SHEAR TIE REPLACED AS PER SRM 51-10-01 P.8 2L74 4F A20WE 20030604000382003060400038SO 2003 6 4 SIMA200312717 120030428A532014522459003 RAMP EMB 135 EMB135KL 3260302SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21807AE 145506 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV NSPECTION GALLEY RAMP CORRODED AT FRAME 20. REMOVED AND INSTALLED NEW GALLEY RAMP IAW EMB 140 SRM 51-40-02, 51-20-07. (M) 2L72 4F RTT00011AT 20030604000102003060400010NM 2003 6 4 AALA20030495 120030424A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21774AN 29581 DURING OVERNIGHT MAINTENANCE, FORWARD LT FORWARD FACING LOWER EMERGENCY EXIT PATH LIGHT ON THE G3 GALLEY WALL INOPERATIVE. REPLACED FORWARD LEFT FORWARD FACING LOWER EMERGENCY EXIT PATH LIGHT ON THE G3 GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030210000532003021000053EA 2003 2 10 QXEA0300036 120030111A2612 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA FIRE DETECTION MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09615QX 10065 MFR- FIRE SYSTEM FAULT STATUS MESSAGE. INTERROGATED MDC, FOUND NO FAULTS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030214000432003021400043NM 2003 2 14 P5CA0300748 120030127A5312NONE BULKHEAD BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND FWD PRESSURE BULKHEAD OF F/S 140, 12:20 O'CLOCK. DAMAGED AREA TRIMMED OUT. REINFORCED AREA W/ STRAP & DOUBLER PER SRM 54-40-03, FIG. 2. 2L74 4F A20WE 20030218000102003021800010NM 2003 2 18 03FDEA00103 120030203A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D* NE BULKHEAD CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 N00723 CORROSION A/C BAY, STA 740, RBL 12 WL 140, CORROSION AT LOWER FRAME ANGLE OF BULKHEAD. INSTALLED NEW SPLICE DOUBLER IAW SRM AND EA. 2L73 4F4 FRTA3WE E2EA 20030220000092003022000009CE 2003 2 20 FPI2003F00004 120030204A323398820152 ACTUATOR CESSNA210 210N 2073453CE CONT O520 IO520* 17032SO MLG CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO155307A16173 21063360 INSPECTED ACTUATORS FOR CRACKS. FOUND CRACKS, REMOVED FROM SERVICE. 1H71 3O3 O 3A21 E5CE 20030221000682003022100068NM 2003 2 21 AWXA200300088 120030129A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 6 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030121000062003012100006NM 2003 1 21 SWAA030083 120030114A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT FUSELAGE SKIN, BS 899, STRINGER 25L AND BS 765, STRINGER 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030227000112003022700011SW 2003 2 27 HEEA084368 120030211A5610407540137 SLIDE CHANNEL BELL 407 407 1182206SW WINDOW CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 WINDOW SLIDE CHANNEL CRACKED. SCRAPPED. 1G71 3U O H2SW 20030228001152003022800115WP 2003 2 28 MWEA030115 120030227A532199365853 FLOORBOARD DOUG DC9 DC981 3022081WP STA 522 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOORBOARD BETWEEN SEAT TRACKS #1 AND #2 AT STATION 522 IS DENTED. -- FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F A6WE 20030306000482003030600048SW 2003 3 6 HEEA084763 120030221A3212412050013111 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 EMERGENCY FLOAT LEAKING. 1G72 4U H4SW 20030307000192003030700019NM 2003 3 7 SWAA030498 120030305A53156546804 BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D CHECK, FOUND BS 987 FLOORBEAM UPPER CHORD CORRODED BETWEEN LBL 15 AND RBL 41, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20030307001332003030700133WP 2003 3 7 AALA20030106 120030124A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21562AA 49344 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 1-19 DIM. REPLACED FORWARD AND MID EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030310000602003031000060SW 2003 3 10 HEEA084964 120030227A6220412010216105 BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 MAIN ROTOR HEAD BEARING WORN. REPAIRED. 1G72 4U H4SW 20030313001842003031300184WP 2003 3 13 AALA20030143 120030131A5320 STRUCTURE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21563AA 49345 TUL - FOUND WHALE BONE IS CRACKED AT FASTENER HOLE TOWARDS OUTBOARD END .5 INCH. INSTALLED DOUBLER PER AARD 53-10-00-12. (M) 2L72 4F RTA6WE 20030313002232003031300223NM 2003 3 13 QXEA0300197 120030127A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING, NR 4 FLAP TRACK, INBOARD SIDE LOAD TRACK IS PITTED. REPAIRED IAW HORIZON AIR EA 2-57-220. 2H72 4T RTA13NM 20030314000642003031400064NM 2003 3 14 CALA0300030 120030210A3350 FUSE BOEING737 7373T0 1384582NM POWER PACK BLOWN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0976354 23592 THE EMERGENCY EXIT AISLE LIGHTS AT ROW 12 - 20 WERE FOUND INOPERATIVE DURING SERVICE CHECK. MAINTENANCE FOUND REAR EMERGENCY LIGHT POWER PACK FUSES BLOWN. THE FUSES WERE REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. 2L72 4F RTA16WE 20030122002642003012200264SW 2003 1 22 HEEA083574 120030113A6420 BEARING BELL 412 412 1182202SW T/ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D6487 A927 33076 TAIL ROTOR HEAD FEATHERING BEARINGS WORN. REPAIRED. 1G72 4U H4SW 20030317001232003031700123WP 2003 3 17 03FDEA00282 120030307A78309007M63G15 BLOCKER DOOR DOUG DC10 DC1010 3022110WP THRUST REVERSER DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 DURING A ROUTINE INSPECTION OF THE NR 1 INBOARD THRUST REVERSER W/C NR 78C3501, IT WAS FOUND THAT BLOCKER DOOR NR 6, THE DRIVE LINK ATTACH FITTING HAD DISBONDED. REMOVED AND REPLACED BROKEN BLOCKER DOOR NR 6 I/B T/R IAW M/M 78-32-06-2, OP'S CHECK GOOD. 2L73 4F A22WE 20030319000602003031900060NM 2003 3 19 HALA0300010 120030110A5730 SKIN BOEING717 717200 1383700NM RT WING DAMAGED A HALAK NONE O OTHER ININSP/MAINT 1 WP13476HA 55118 HNL - FOUND DAMAGE TO RIGHT WING INBOARD SPOILER INBOARD AND OUTBOARD FITTING AND UPPER WING SKIN PANEL, REF SB 717-57A0013. PARTS TO BE REPLACED AND SKIN TO BE REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. (M) 2L72 4F TRA6WE 20030731001462003073100146WP 2003 7 31 GTIA030507 120030623A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND CORROSION ON L1 DOOR WEB, STATION 200 LOWER FORWARD CORNER LBL 54. REMOVED APPROX 8 INCHES FROM LOWER L1 DOOR WEB. FABRICATED L1 DOOR REPAIR. INSTALL REPAIR ON L1 DOOR WEB. (M) 2L72 4F A6WE 20030418000462003041800046EU 2003 4 18 MALA030159 120030218A3260 UPLOCK SENSOR BAC 146 AVRO146RJ85A1500097EU RT MLG DIRTY A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15513XJ E2329 DURING GEAR RETRACTION ON FLIGHT 3460, GEAR UNSAFE LIGHT ILLUMINATED, WOULD NOT EXTINGUISH. AIR RETURN TO DTW. RT MAIN GEAR UNSAFE INDICATION ILLUMINATED AFTER GEAR RETRACTION, CYCLED UNDER DIRECTION OF DTW MX. RT MAIN UNSAFE EXTINGUISHED. LT MAIN GEAR ILLUMINATED, CYCLED 5 TIMES UNDER DIRECTION OF MX LIGHT REMAINED ILLUMINATED. MAINTENANCE FOUND ICE AND SNOW SLUDGE ON MLG UPLOCKS, THAWED, CLEANED, AND LUBED UPLOCKS. PERFORMED OPS CHECK IAW AVRO AMM 32-30-00 501. DID SEVERAL GEAR SWINGS. NO DEFECTS NOTED AT THIS TIME. 2H74 4F RTA49EU 20030421001892003042100189NM 2003 4 21 USAABB03044 120030318A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 6, 9, 18 23 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030418000082003041800008EA 2003 4 18 QXEA0300274 120030214A26109847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09603QX 10011 PDX-FIRE DETECTOR CHIMNEY IN FORWARD CARGO COMPARTMENT DAMAGED. REMOVED AND REPLACED FORWARD CARGO COMPARTMENT FIRE DETECTOR CHIMNEY ENCLOSURE. SECURED WITH 8 SCREWS AND WASHERS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030422001042003042200104SO 2003 4 22 SIMA200307008 120030307A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 ABI - DURING A IMBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 33 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PEFORMED AN NDT INSPECTION. FABRICATED A DOUBLER, REPAIR DONE IAW EMB SRM (SRM EMB 145/1141 REV 20) CHAPTERS 53-21-10 FIG 208 AND EMB REPAIR STATEMENT IC2003-145/0771. (M) 2L72 4F RTT00011AT 20030422000052003042200005NM 2003 4 22 USAASB03033 120030302A27512061141 INDICATOR BOEING737 737301 1384611NM TE FLAPS FAILED A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19585US42713 23930 CLT - FLT 953 - ON APPROACH TO CLT FROM BOS, CREW REPORTED THAT WHEN FLAPS WERE EXTENDED TO 10 UNITS, THE RIGHT TRAILING EDGE FLAP STOPPED AT 6 UNITS. CREW EXTENDED GEAR AND ATTEMPTED TO MOVE THE FLAPS TO 15 UNITS BUT FLAPS WOULD NOT MOVE. CREW DISCONTINUED APPROACH AND BEGAN ACCOMPLISHING 'TRAILING EDGE ASYMMETRICAL FLAPS' PROCEDURE. WHILE ACCOMPLISHING PROCEDURE, THE RIGHT TRAILING EDGE FLAP MOVED TO 10 UNITS. FLAPS THEN EXTENDED TO 15 UNITS. AIRCRAFT LANDED NORMALLY WITH 30 UNITS OF FLAPS. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-41 DUE TO A RIGHT FLAP INDICATION POINTER STICKING. PERFORMED SATISFACTORY FLAP ASYMMETRY SYSTEM TEST. OPERATION2L72 4F RTA16WE 20030327001632003032700163SO 2003 3 27 C2XA03SH033 120030301A531014529610003 STOP EMB 145 EMB145ER 3260211SO CARGO DOORFRAME CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV- DURING C-CHECK THE FOWARD EXTERNAL FRAME ON CARGO DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030716000672003071600067EU 2003 7 16 2003F00423 120030413A5610SPSA320911 WINDOW AIRBUS320 A320233 3930329EU COCKPIT CRACKED A RJEFO OTHER O OTHER DEDESCENT 1 SO23483TA 1509 DURING DESCENT, THE PILOTS REPORT THAT L3 WINDOW WAS CRACK DURING DESCENT PROCEDURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. AT BZE STATION WINDOW-MIXED CHECK WAS PERFORMED ACCORDING TO AMM 56-11-22 AND FOUND IT WITHIN LIMITS. AT THE SAME TIME PRESSURIZATION WAS PERFORMED ACCORDING TO AMM 05-53-00. THE AIRCRAFT RETURNED TO SAL STATION WITHOUT ANY INCIDENT. AT EL SALVADOR STATION, THE FIXED WINDOW NR 3 LT WAS REMOVED AND REPLACED ACCORDING TO AMM 56-11-12-401. PERFORMED OPERATIONAL TEST OF THE ANTI-ICE AND DEFOGGING SYSTEM OF THE FIXED WINDOW AS PER REF. TASK 30-42-00-710. ALL THE CHECKS WERE PERFORMED WITH NORMAL RESULT. THE AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 20030805000592003080500059SO 2003 8 5 SIMA200319707 120030710A5330 SKIN EMB 135 EMB135LR 3260305SO FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21711PH 145235 AIRCRAFT ARRIVED FOR PERMANENT REPAIR OF TDMI NR 71153018B, REPAIR OF BLENDED GOUGE BETWEEN STATION 66-67 AND BETWEEN STRINGERS 15-16R. PERFORMED EDDY CURRENT INSPECTION A POSITIVE CRACK INDICATION AS DETECTED. PERFORMED A CUTOUT OF THE DAMAGED AREA. AN ADDITIONAL NDT INSPECTIN WITH NO CRACK INDICATION NOTED. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, EMB SRM 145-1142 REV 22, CHAPTER 53-31-01. (M) 2L72 4F RTT00011AT 20030422001592003042200159NM 2003 4 22 PCAA0303054 120030311A3350 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13816EX 329 DURING ROUTINE MAINTENANCE VISIT RIGHT FORWARD FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. BATTERY PACK AT POSITION NR 200 WAS REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030722000822003072200082EU 2003 7 22 MALA030335 120030620A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15526XJ E2351 DURING C-CHECK INSPECTION IN CVG, NR 4 SEAT RAIL CORRODED BEYOND LIMITS. FLOORBEAM AT FRAME 20-18. MAINTENANCE REPLACED SEAT TRACK NR 4 IAW EO NR A53026, REMOVED AND REINSTALLED ELEVATOR G-WEIGHT AND RIG CHECKED ELEVATOR CIRCUIT. SEE CONTINUATION CARD DETAIL. REFER 409 NR 127852 FOR DETAIL. A/C RELEASE DATE 7/1/2003. 2H74 4F RTA49EU 20030722001212003072200121NM 2003 7 22 AWXA200300738 120030618A53126516300 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-13 CHECK 3 EACH 1 INCH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT LBL 5, WL 200.5 - 201, WL 197.75 - 198.5, AND LBL 6.25, WL 200.3 - 201. MAINTENANCE STOP DRILLED CRACKS AT LBL 5, WL 200.5 - 201, WL 197.75 - 198.5, AND LBL 6.25, WL 200.3 - 201; PERFORMED HFEC INSPECTION OF STOP DRILL HOLES TO VERIFY CRACKS ARE CONTAINED; FABRICATED REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08 FIG 210. 2L72 4F RTA16WE 20030723000842003072300084NM 2003 7 23 AWXA200300664 120030519A5315654681143 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 LCQ - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND AT FASTENERS ON FLOORBEAM AT BS 986.5, LBL 25. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF UPPER TEE AT BS 986.5, LBL 25; FABRICATED A NEW REPLACEMENT SECTION OF UPPER TEE, 2 EACH SUPPORT ANGLES, AND 2 EACH REPAIR STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51 PG 207-211 FIG 202. 2L72 4F RTA16WE 20030724000192003072400019NM 2003 7 24 AWXA200300682 120030514A5313655292833 STRINGER BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 RT LOWER LOBE AT BS 907. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AND TRIMMED AWAY CORROSION ON STRINGER 27 RT, BS 907; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-45895-3 AND A FILLER; AND INSTALLED REPAIR PARTS IAW AWA ER 15-5361-03155-SS3. 2L72 4F RTA16WE 20030827000892003082700089SO 2003 8 27 C2XA03SH238 120030730A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 SHV- DURING C CHECK THE CENTER OMEGA BEAM IN GALLEY WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030828000252003082800025NE 2003 8 28 00098 220030611A7200 ENGINE LEAR 24 24B 5170306CE GE CJ610 CJ6106 30006NE RIGHT FLAMED OUT E HAEAB EMER. DESCENT X ENGINE FLAMEOUT CLCLIMB 1 SW05233TW PILOT REPORTED RT ENGINE FLAMED-OUT CLIMBING THRU FL410 FOR FL430. DESCENDED AND RELIGHT NORMAL, CLIMB BACK TO FL410 FOR REMAINDER OF LEG. UPDATE AFTER MAINTENANCE. AIRCRAFT RESTRICTED TO FL410. 2L72 4J4 J A10CE 1E16 20030828001882003082800188NM 2003 8 28 CALA0300459 120030810A5514 ATTACH ANGLE BOEING737 7373T0 1384582NM HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND A 6 INCH CRACK IN ATTACH ANGLE ON HORIZONTAL STABILIZER CENTER SECTION AT UPPER BEAM. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030728000262003072800026NM 2003 7 28 SWAA031572 120030716A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM CORRODED AT BS 1011. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20030729000372003072900037NM 2003 7 29 ZW0A0305801 120030309A3350BPS73 BATTERY PACK BOEING757 757231 1384950NM CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13722TW 29385 THE FIRST CLASS CABIN EGRESS FLOOR LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND CABLE PN 6664-9. 2L72 4F RTA2NM 20030729000642003072900064NM 2003 7 29 QXEA200300808 120030709A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09349PH10006145 486 PDX- AFT INTERIOR CEILING EMERGENCY LIGHT INOPERATIVE AND AFT RIGHT HAND EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030807000712003080700071NM 2003 8 7 AWXA200300842 120030725A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 PHX - MAJOR REPAIR - DURING INSPECTION A 4 INCH CRACK WAS FOUND ON SKIN AT BS 947, STR 24 LT. MAINTENANCE REMOVED DAMAGED AND FABRICATED A REPAIR DOUBLER OUT 2024-T3.074. PLACED ON MON, PERMANENT REPAIR REQUIRED NO LATER THAN 20,000 CYCLES. 2L72 4F RTA16WE 20030903001832003090300183WP 2003 9 3 AALA20030783 120030719A215079137451161 LINE DOUG DC9 DC982 3022082WP A/C BAY DAMAGED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21483A 49676 FLT 1719 - DFW-SEA - ON CLIMB-OUT AIRCRAFT HAD THE SMELL OF A PAK OVERHEAT FOLLOWED BY SMOKE IN THE CABIN. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FURTHER INVESTIGATION REVEALED A HOLE IN LEFT PACK HEAT EXCHANGER WATER SPRAY LINE. REMOED AND REPLACED LINE. PACK BURN ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904000322003090400032EA 2003 9 4 SWIA200312272 120030814A2742DL2428M4 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB FAILED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07720SW161 161 7297 PITCH FEEL CB POP OUT IN FLIGHT CH NR 1. REMOVED AND REPLACED NR 1 ACTUATOR-LINEAR IAW MM 27-31-23. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030908002552003090800255 2003 9 8 52767AMWA01 420030720A6122 GOVERNOR BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE RT ENGINE MALFUNCTIONED A AMWAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE07144ZV UE144 DURING TAKEOFF ON FLIGHT 5578 FROM READING PENNSYLVANIA TO PITTSBURGH, THE POWER ADDED TO THE RIGHT ENGINE WOULD NOT DEVELOPE MORE THAN 1000 FT LBS TORQUE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BLEED VALVE AND THE PROP GOVERNOR. STILL AWAITING MORE INFORMATION TO COME. 2L72 4T RTA24CE 5 CP10NE 20030821002452003082100245NM 2003 8 21 2003UALA00472 120030605A2611 WARNING SYSTEM AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29813UA 858 RETURNED TO FIELD DUE TO SMOKE INDICATION IN THE AVIONICS COMPARTMENT. *SUPPLEMENTAL DATA UPDATE* ACCOMPLISHED AIRBUS TSM TASK 21-26-00-810-813, VISUAL CHECK OF AVIONICS COMPARTMENT, TESTS OF AEVC & FWC 1 & 2. NO DEFECTS OR DISCREPANCIES NOTED. NO FURTHER FAULTING REPORTED. 2L72 4F4 FRTA28NM E40NE 20030910001462003091000146WP 2003 9 10 AALA20030876 120030515A53205936660171 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21964TW 53614 MCI - FOUND CORROSION ON CARGO FLOOR SUPPORT STATION 1155 TO 1212, 7 INCHES RBL TOP SIDE AND BOTTOM SIDE. REPLACED WITH NEW MPN 5936660-171, RIVETS WERE INSTALLED PER SRM 51-30-02. (M) 2L72 4F RTA6WE 20030910001592003091000159NE 2003 9 10 ASOA03362 220030807A72606078T58P01 SNAP RING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE MISSING A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO11851AS 7360 FLT 9331 - DURNG APPROACH INTO ATL FROM MCN, THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE. THE OIL PRESSURE WAS AT 25 PSI AND CONTINUED TO DECREASE. THE CREW COMPLIED WITH QRH PROCEDURES AND SHUTDOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSTALLED A MISSING RIGHT ENGINE CRANK PAD SNAP RING, AND REMOVED AND REPLACED THE RIGHT ENGINE OIL TRANSDUCER (P/N 601509199). OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20030911001732003091100173WP 2003 9 11 DHL2003873604 120030704A532036169452 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT FITTING ATTACHED TO FRAME CRACKED 3.000 STA.822.500 L21 TO L22L. PERFORMED MAJOR REPAIR IAW ATM NR P0201433, DWG NR 3616945. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW DWG NR 3616945 PERFORMED EDDY CURRENT INSPECTION IAW NDT SPM PAR 08-00-02/06. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030929000312003092900031NM 2003 9 29 03FDEA01423 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RIGHT WING I/B FLAP VANE I/B TEE FITTING FWD BORE FOUND CORRODED. CORROSION ON RT WING, I/B FLAP VANE I/B TEE FTG FWD BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL 2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490. 2L73 4F RTA22WE 20030926001272003092600127EU 2003 9 26 UPS03141152 120030826A5753 SKIN AIRBUSA300 A300F4622R 3930360EU LT WING TE FLAP GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01138UP 0821 INSPECTION TYPE: C1, LT WING INBD FLAP TOP SURFACE IS GOUGED OUTBOARD END, BLENDED AREA IAW A300 SRM 57-50-00. ORIGINAL THICKNESS OF .032 REMAINING MATERIAL .025 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE IAW A300 SRM 51-50-00 INSTALLED REPAIR DOUBLER IAW A300 SRM 51-21-00 & 51-40-40. 2L72 4F RTA35EU 20031002000662003100200066NM 2003 10 2 DHL2003720008 120030830A2611327 LAMP BOEING727 727228 1384083NM SMOKE DETECTOR INOPERATIVE A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01720DH 19544 RT NR 5 SMOKE DETECTOR INOPERATIVE. ITEM PLACED ON DMI LIST IAW MEL 26-14-1. CONTROL NR 14005 PLACARD INSTALLED. DMI NR 14005 NR 5 RIGHT SMOKE DETECTOR INOPERATIVE. RELAMPED OPS CHECKED GOOD IAW 26-17-1. THIS CLEARS DMI NR 14005. PLACARD REMOVED. 2L73 4F RTA3WE 20031006000322003100600032NM 2003 10 6 AWXA200301058 120030815A5320BAC1496364 ANGLE BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FORWARD CARGO COMPARTMENT LT TRANSITION ANGLE BETWEEN BS 380 AND BS 480. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ANGLE BETWEEN BS 380 AND BS 480; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-200 SRM 51-30--02, PG. 1, FIG. 2 & 3. 2L72 4F RTA16WE 20031007001082003100700108NM 2003 10 7 SWAA032006 120030908A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 EMERGENCY FLASHLIGHT IN FWD CABIN NOT CHARGING. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20031006001662003100600166NM 2003 10 6 SWAA031969 120030831A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 13R AND STR 14R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031021001342003102100134NM 2003 10 21 AALA20031010 120030916A3350P4010051112 CONTROL MODULE BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21697AN 26977 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS UNABLE TO BE TURNED OFF IN THE FIRST CLASS CABIN. REPLACED CONTROL MODULE AND BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002432003102100243WP 2003 10 21 GTIA030694 120030901A5330 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND FORWARD PIT STATION 465-484 STRINGER 29L-30 ANTENNA MOUNT CORRODED. AFTER FURTHER INVESTIGATION FOUND DOUBLER TO BE CRACKED. FABRICATED NEW ANTENNA DOUBLER. INSTALLED ANTENNA DOUBLER. (M) 2L72 4F A6WE 20030908003412003090800341NM 2003 9 8 SWAA031925 120030828A5315BAC1505 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT LONGITUDINAL FLOORBEAM CORRODED AT BS 860, LBL 8. REPAIRED BEAM PER SRM AND SWA EA. 2L72 4F RTA16WE 20030909000912003090900091SO 2003 9 9 SWIA200312313 120030822A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE T/E FLAP FAILED A SWIAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM07188SW7199 1798 120039 FLAP DISAGREEMENT ON OUTBOARD PAIR WHEN FLAPS 45 DEGREES SELECTED. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW EMB MM 27-50-00. OPS AND LEAK CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031027001332003102700133SO 2003 10 27 RAIA00309248 120030925A2997F0049 FUSE EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL HYD PUMP BLOWN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03815HK 145048 LEFT ELECTRICAL HYD PUMP FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED FUSE. 2L72 4T4 FRTT00011ATTE6CH 20031021002252003102100225NM 2003 10 21 QXEA200301168 120030916A61204122006002 PUMP DHAV DHC8 DHC8202 2809007NM ZONE 400 MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH9609 9609 530 ALTERNATE FEATHER PUMP DOES NOT COME ON DURING TEST ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 AUX FEATHER PUMP. 2H72 4T RTA13NM 20031027000612003102700061NM 2003 10 27 UPS03441261 120030908A531065B04410 DOOR FRAME BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, L4 DOOR FWD CUT-OUT REVEAL UPPER CRACKED.BS1664 S-17 & S-18 M/D- L4 DOOR FWD CUT-OUT REVEAL REPAIRED AS PER RS R-53-62-35069 AND UPS ENGINEERING FILE NO 747-53-20153 2L74 4F4 F A20WE E20EA 20031118000692003111800069NM 2003 11 18 DHL2003749515 120030925A5730 SKIN BOEING727 727200 138407ENM WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK, WING CENTER SECTION LOWER SKIN CORRODED ABOVE RT PRIMARY HEAT EXCHANGER. REMOVED CORROSION IAW B-727 SRM 51-10-6 WITH A MAT LOSS OF .057 AREAS FOUND TO BE OUT OF LIMITS IAW B-727 SRM 57-30-1 FIG 4 TABLE I FIG 5, PARA 2 FABBED DOUBLER FROM 2024 T3 .080 PO 900103 DIM 16.25 X 14.5 INCH AND TRIPLER FROM SAME MATERIAL DIM 14.375 X 13.5 INCH IAW B-727 SRM 57-30-3 FIG 8, 9 & 10. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 57-30-3 FIG 8, 9 & 10. REMOVED AND RE-INSTALLED RT PRIMARY HEAT EXCHANGER IAW B-727 MM 21-55-21. OP'S AND LEAKED CHECK GOOD IAW B-727 MM 21-00 AND FUEL LEAK CHECK GOOD IAW B-727 MM 28-11-0. 2L73 4F RTA3WE 20040114000452004011400045NM 2004 1 14 DLM88030959 120031027A2910 HYDRAULIC LINE DOUG MD88 MD88 3023688NM NR 2 ENGINE LEAKING A DALAK NONE K FLUID LOSS CRCRUISE 1 SO27959DL 49978 LOST RIGHT HYD SYSTEM IN FLIGHT. REPLACED RIGHT ENGINE PRESSURE FLEX LINE FOR LEAKING. 2L72 4F RTA6WE 20030604002182003060400218EU 2003 6 4 BAQA086323 120030502A25203100 SEAT UROCOPEC135 EC135T1 5620026EU CABIN CRUSHED W BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01136MH182 0161 SEATS CRUSHED. NEEDS REPAIRED. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030605001472003060500147EA 2003 6 5 SWIA200311973 120030512A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07442SW2767 1286 7609 THIRD CENTER CEILING AND BOTH CENTER EXTERIOR EXIT EGRESS LIGHTS INOP. REPLACED NR 3 EMERGENCY BATTERY. OPS CHECK GOOD. 2L72 4F RTA21EA 20030609001212003060900121WP 2003 6 9 ABXA030148 120030502A53203917285501 FITTING DOUG DC9 DC932 3022066WP LT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 DURING A LINE MAINTENANCE VISIT, FOUND THE LT WW SLANT PANEL ATTACH FITTING CRACKED 1.75 INCH LONG. REPLACED ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 20030609001322003060900132EU 2003 6 9 MALA030279 120030504A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15525XJ E2350 DURING C-CHECK INSPECTION IN CVG, CRACK AND CORROSION ON FLOOR BEAM 18, BETWEEN SEAT TRACK 3 & 4. MAINTENANCE REPAIRED FRAME 18 IAW EO A53116. REF 409 118195 FOR DETAIL. A/C RELEASE DATE 5/21/03. 2H74 4F RTA49EU 20030520000042003052000004SW 2003 5 20 CA030401006 120030321A6230204010433001 BEARING BELL BELL 412 412 1182202SW SWASHPLATE LOOSE W O OTHER O OTHER NRNOT REPORTED 1 CA RE670 (CAN) DURING UNSCHEDULED MAINTENANCE TO CORRECT MECHANICAL DAMAGE TO THE OUTER RING, PLAY WAS DETECTED IN THE GIMBAL RING AREA. FURTHER INVESTIGATION REVEALED LOOSENESS IN THE BEARING & LINER ASSEMBLY (4 EACH). ON DISASSEMBLY IT WAS FOUND THE BEARINGS P/N MS27640-5 WERE LOOSE AND SPINNING IN THE LINERS P/N 204-010-433-003. BEARINGS HAD BEENN INSTALLED IN LINERS WITH GREEN PRIMER. NEW BEARING & LINER ASSEMBLY INSTALLED AND SWASHPLATE RETURNED TO SERVICE. 1G72 4U H4SW 20030609001522003060900152SO 2003 6 9 C2XA03SH156 120030525A531014521721009 BUTTSTRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030613001142003061300114NM 2003 6 13 SWAA031255 120030604A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030617000162003061700016NM 2003 6 17 AUS20030480 120030505A2797D11822 WIRE BOEING737 737724 13844BYNM GE CFM56 CFM567B24 NE TE FLAP CONTROL CHAFED W O OTHER F FLT CONT AFFECTED TOTAKEOFF 1 AUS (AUS) FLAP WIRING CHAFED IN AREA BETWEEN CONNECTOR D11822 PINS 6 AND 7AND CONNECTOR D11824 PINS 1 AND 2. 2L72 4F4 FRTA16WE E00055EN 20030617001582003061700158NM 2003 6 17 QXEA200300716 120030601A5512 SKIN BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FRONT SPAR AND Y605D-73.00. REPAIRED IAW Q400 SRM 51-21-10, PAGES 204-205 AND SRM 51-25-10, PAGES 201-205. 2H72 4T RTA13NM 20030617002362003061700236EA 2003 6 17 QXEA200300697 120030605A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA RT WING BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - RIGHT HAND WING TRAILING EDGE HAS TWO LOOSE RIVETS NEXT TO INBOARD FLIGHT SPOILER AND TWO RIVETS BROKEN OFF ON LOWER SIDE OF FLIGHT SPOILERS. REPAIRED IAW HORIZON AIR EA R-57-37 AND WVAC EO 601R-57-4086. 2L72 4F RTA21EA 20030521001932003052100193EU 2003 5 21 AWXA200300544 120030508A5210FE174004 DAMPER AIRBUS320 A320231 3930325EU PAX DOOR SHEARED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW42273 064 MCN - EES - DURING C-04 CHECK THE R-1 DOOR DAMPER CYLINDER KNURLED KNOB WAS FOUND SHEARED. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR DAMPER CYLINDER IAW AMM TASK 52-11-14-000-001, 52-11-14-400-001, AND 52-11-14-04 FIG 401 & 402, SHT 1. 2L72 4F RTA28NM 20030520000812003052000081EU 2003 5 20 2003F00260 120030404A3260327 BULB STBROSSD3 SD330 8100602EU MLG INDICATOR BURNED OUT A DATAO OTHER N FALSE WARNING DEDESCENT 1 GL1358DD SH3008 ON APPROACH TO SDF, THE LANDING GEAR WAS PUT DOWN, HOWEVER, ONLY THE LT AND NOSE GEAR INDICATED IT WAS DOWN. THE CREW DECIDED TO GO AROUND AND CHECK THE PROBLEM. AFTER THE PROBLEM WAS CHECKED THE CREW DECIDED FOR THE RIGHT MLG WAS DOWN AND THE LIGHT BULB WAS NOT ILLUMINATED. THE CREW WAS STILL CONCERNED AND DECLARED AN EMERGENCY FOR SAFETY REASONS. THE AIRCRAFT WAS LANDED SAFELY AND WITHOUT INCIDENT. AN ACC MECHANIC VERIFIED THE RIGHT MLG LIGHT BULB WAS BURNED OUT. THE LIGHT BULB WAS REMOVED AND REPLACED AND OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED BACK TO SERVICE. (M) 2H72 4T A41EU 20030521000832003052100083WP 2003 5 21 DHL2003804912 120030121A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 M/C COMPT CTR TRACK LUGS WORN FROM STA 1670.000 - STA 1710.000. REMOVED DAMAGED AREA FROM CTR TRACK IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SECTION AND REINSTALLED SPLICES IAW SRM 53-2-3 PG 49-50 AND 51-3-0 PG 1. 2L74 4F RT4A25 20030527000402003052700040NM 2003 5 27 2003UALA00397 120030326A5754114W413016 WEDGE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 12 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29792UA 26934 T/E WEDGE DELAMINATED. REMOVED, REPAIRED AND REINSTALLED WEDGE, NR 12 SLAT. 2L72 4F4 FRTT0001SE E46NE 20030530000602003053000060NM 2003 5 30 AMTA200300589 120030501A2500 CONNECTOR BOEING757 75728A 1384976NM EMERGENCY LIGHT LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11513AT 32449 EMERGENCY ESCAPE PATH LIGHTING OUT FROM ROW 1 THROUGH ROW 5. RESEATED LOOSE CONNECTORS AT ROW 5 LIGHT ASSEMBLY, OPS CHECKS GOOD PER AMM 33-51-00. (M) 2L72 4F RTA2NM 20040212000462004021200046CE 2004 2 12 N382003F00003 120031114A212066001983 CONTROL VALVE LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP FLOW CONTROL INTERMITTENT E N38AA UNSCHED LANDING O OTHER CLCLIMB 1 EA05825LJ 496 CREW REPORTED NO CABIN AIR AFTER TAKE-OFF FROM TEB. AIRCRAFT RETURNED TO ABE BELOW 10,000 FOR SWAP OUT WITH ANOTHER. AIRCRAFT GROUND RUN BY MAINTENANCE PERSONNEL AND OPERATED THROUGH NORMAL AND EMERGENCY MODES. IT WAS DETERMINED THAT FLOW CONTROL VALVE WAS INTERMITTENT. FLOW CONTROL VALVE IS TO BE CHANGED. 2L72 4F4 F A10CE E6WE 20040212000982004021200098NM 2004 2 12 200300286 120031211A5753113T13691 ATTACH FITTING BOEING767 767383 1385214NM TE FLAP BROKEN B AAIAK NONE O OTHER ININSP/MAINT 1 WP07TFATT 24358 LEFT WING OUTBOARD T/E FLAP, OUTBOARD FLAP TRACK SUPPORT ATTACH FITTING BROKEN OFF AT REAR WING SPAR. 2L72 4F RTA1NM 20031118000262003111800026NM 2003 11 18 AWXA200301141 120030907A53206546585 STIFFENER BOEING737 7373Q8 1384670NM TORQUE BOX WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK FOUND THE RT APU TORQUE BOX SUPPORT STIFFENER WORN AT BS 1124. MAINTENANCE CUT OUT DAMAGED SECTION OF SUPPORT STIFFENER AT BS 1124; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, PG 1-6, FIG 1. 2L72 4F RTA16WE 20031119000672003111900067EA 2003 11 19 COMA0360453 120031007A53116013600129 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01963CA17437 7127 640 FRAM DOUBLER CRACKED, REMOVED AND REPLACED LT 640 FRAME DOUBLER IAW CRJ SRM 51-21-06, 51-42-20 AND 51-42-21. 2L72 4F RTA21EA 20031119001232003111900123NM 2003 11 19 2003UALA00752 120031006A5753 SKIN BOEING777 777222 1385219NM PWA 4052 PW4052 52119NE LT TE FLAP DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29224UA 30225 LT WING AFT FLAP TRAILING EDGE HAS 6 INCH SPANWISE BY 4 INCH CHORDWISE DELAMINATION 4 FT INBD FROM OTBD EDGE OF FLAP. THE ABOVE NOTED DELAM CONDITION WAS DISCOVERED WITH RELATIVELY LOW FLIGHT-HOURS AND FLIGHT-CYCLES. THE DELAM WAS DUE TO AERODYNAMIC LOADING DURING FLIGHT, ESPECIALLY DURING LANDING WHEN THE FLAP IS POSITIONED MORE DIRECTLY INTO THE AIRSTREAM, AND THUS IS SUBJECT TO MORE AIRLOADS. THE DELAMINATION WAS REPAIRED. 2L72 4F4 FRTT0001SE E24NE 20031107001452003110700145WP 2003 11 7 GTIA030737 120030923A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND MAIN CABIN STATION 465 TO STATION 541 RBL 44 INCHES FLOORBOARD HAS CRACKED/DAMAGED ON EDGE. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20040112001492004011200149EU 2004 1 12 MALA030560 120031218A7931 GAUGE SAAB SF340 SF340A 7850100EU COCKPIT FAULTY A MALAO OTHER N FALSE WARNING LDLANDING 1 GL15106XJ 340A106 AFTER TOUCHDOWN ON FLIGHT 2960, LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED WHEN REVERSE WAS SELECTED. MAINTENANCE REPLACED PRESSURE TRANSMIT AND PRESSURE GAUGE. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040113001222004011300122EU 2004 1 13 BAQA091481 120031210A7722304534402 THERMOCOUPLE AGUSTAA109 A109E 0260119EU ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109UP1130 11061 WARRANTY ENGINE PCE-BC0133. THERMCOUPLE ASSEMBLY INOPERATIVE. 12/10/03 1G72 3U RTH7EU 20040113000792004011300079EU 2004 1 13 ERAA091809 120031014A3212D24762101 FLOAT BOLKMS105 BO105S 5626006EU MLG LEAKING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03292EH517 562 INLET VALVE ATV NR 2 BULKHEAD IS LEAKING. SENT FOR REPAIR IAW OHSS 100-1 AND C/W INSPECTION IAW 25-60-05. 1G72 3U H3EU 20031120000592003112000059NM 2003 11 20 QXEA200301248 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 5 SEAT TRACK CHANNEL HAS LITE PITTING AT STATION X486.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20031121000762003112100076NM 2003 11 21 03FDEA01947 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 RIGHT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER BOLT HOLE I/B FLANGE SIDE CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, I/B HINGE FITTING LOWER BOLT HOLE I/B FLANGED SIDE CORROSION. R & R AS PER FEDEX EA 1-5740-74250. WINGS - LEFT & RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040114002242004011400224EA 2004 1 14 03360708 120031230A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27708BR 7575 DURING INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNED OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031218000322003121800032SO 2003 12 18 SWIA200312627 120031121A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07207SW6149 6149 120266 EMERGENCY LIGHTS ROW 1-4 INOP. REPLACED BATTERY PACK. OP CHECK OK. 2L72 4T RTA31SO 20031218001722003121800172WP 2003 12 18 CALA0300692 120031205A5320991186021N ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 SKIN FORMER AT STA 1451 UNDER LEFT VERTICAL ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED FORMER PER SRM 51-10-1. 2L72 4F A6WE 20031219001052003121900105NM 2003 12 19 2003UALA00935 120031204A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAO OTHER L NO TEST NRNOT REPORTED 1 WP29107UA 26900 EEL LIGHT AT AFT END OF SEAT 5A IS INOPERATIVE. INSTALLED NEW EEL LIGHT & CHECKED OK. 2L74 4F4 FRTA20WE E24NE 20030620000692003062000069NM 2003 6 20 USAA030081 120030522A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US49058 23316 PIT - FOUND SKIN CRACKED .75 INCH LONG, SKIN AFT SERVICE DOOR LOEWR HINGE CUTOUT STATION 947.5, STRINGER 14R. DOUBLE AND TRIPLER INSTALLED AND PAINTED PER SRM 53-60-01. (M) 2L72 4F RTA16WE 20030619000542003061900054 2003 6 19 HEEA087203 420030609A3120CK726424 CLOCK BELL 206 206L3 1182108SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 CLOCK INTERMITTENTLY STOPS. REPAIRED. 1G71 3U H2SW 20030625000322003062500032NM 2003 6 25 AWXA200300562 120030509A5340415N40019 FITTING BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON 3 EACH GALLEY SUPPORT FITTINGS ON AFT SHEAR DECK AT BS 1681 LT, BS 1681R/H, AND BS 1715 LT. MAINTENANCE REMOVED AND REPLACED 3 EACH GALLEY SUPPORT FITTINGS ON AFT SHEAR DECK AT BS 1681 LT, BS 1681 RT, AND BS 1715 LT IAW B757-200 SRM 51-40-02, PG. 12. 2L72 4F RTA2NM 20030626000022003062600002NM 2003 6 26 03FDEA00512 120030418A5320 SUPPORT BOEING727 727200 138407ENM BS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 AFT CARGO WALL SUPPORT LEFT AT STA 950E HAS NUMEROUS AREAS OF CORROSION. FABRICATED WALL SUPPORT IAW BOEING 727-200 SRM 51-20-1. 2L73 4F RTA3WE 20030709000582003070900058WP 2003 7 9 GTIA030420 120030513A5320 SUPPORT DOUG DC9 DC981 3022081WP NLG WW SHEARED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND NOSE WHEEL WELL, STATION 38-43 RBL 16, FOUR SHEARED RIVETS AT OUTBOARD LOWER END OF BULKHEAD SUPPORT. REMOVED BULKHEAD SUPPORT. ON FURTHER INSPECTION FOUND BULKHEAD SUPPORT CRACKED. LOCATED AND DRILLED HOLES ON NEW SUPPORT. INSTALLED SUPPORT BULKHEAD STRUCTURE. (M) 2L72 4F A6WE 20030710000172003071000017NM 2003 7 10 TSAA0333147 120030607A33508610062 BATTERY PACK BOEING737 73725A 1384481NM PAX CABIN INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 REPLACED AFT ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030710000422003071000042NM 2003 7 10 USAABB03088 120030608A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGNECY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU 27124 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 6, 13, 18 AND 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030709000942003070900094SO 2003 7 9 C2XA03CL107 120030609A3350 CONNECTOR EMB 135 EMB135LR 3260305SO EMERGENCY SIGN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716525 145403 CLE FLIGHT 2026 THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR ON THE EMERGENCY LIGHT NR 2 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030710000242003071000024EU 2003 7 10 ASOA03235 120030527A5320S53970816333 BRACKET AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11535AS 464 DURING HANGAR MAINTENANCE, THE RIGHT UPPER BANANA SEAL FAIRING SUPPORT BRACKETS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT UPPER BANANA SEAL FAIRING SUPPORT BRACKETS IAW SRM 53-91-42. (M) 2H72 4T RTA53EU 20030710001532003071000153WP 2003 7 10 MWEA030249 120030620A531199124535 FRAME DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 LOWER CARGO COMPARTMENT FRAME FORMER AT STATION 427 BETWEEN LONGERONS 28 & 28 LEFT HAS AN OVERSIZED HOLE FOR THE SKIN ATTACHING FASTENER. FABRICATED AND INSTALLED NEW FORMER. 2L72 4F A6WE 20030714000752003071400075 2003 7 14 SWAA031390 420030621A25656557463 FITTING BOEING737 7373G7 1384595NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FWD AND AFT GIRT BAR ATTACH FITTINGS CORRODED. REMOVED AND REPLACED ATTACH FITTINGS PER SRM. 2L72 4F RTA16WE 20030710000432003071000043 2003 7 10 USAASA03049 420030521A2565D5211044000600 GIRT BAR AIRBUS320 A320214 3930316EU L1 DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW 1061 BOS - DURING INSPECTION, THE L1 GIRT BAR WAS FOUND TO HAVE IMPROPER CLEARANCE WITH THE DOUBLER/STOP. MAINTENANCE REPLACED THE GIRT BAR. THE INSTALLATION WAS INSPECTED AND FOUND SERVICEABLE. (M) 2L72 4F RTA28NM 20030715000142003071500014NM 2003 7 15 2003F00399 120030313A5320 CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720C, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720C STRINGER 5R. (M) 2L73 4F A3WE 20030715000172003071500017NM 2003 7 15 2003F00401 120030314A5730 PANEL BOEING727 727222 1384073NM RT WING CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON RIGHT WING, OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD ATTACH BRACKET. FABRICATED BRACKET. TREATED, PRIMED AND INSTALLED BRACKET ON RIGHT WING OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD. (M) 2L73 4F A3WE 20030127000852003012700085SW 2003 1 27 HEEA083654 120030114A282070079H100F210 HOSE BELL 407 407 1182206SW FUEL DIST CUT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 FUEL HOSE ASSY CUT IN COVERING, INTO THE BRAID. 1G71 3U O H2SW 20030128000652003012800065SW 2003 1 28 HEEA083819 120030116A6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03742PH3291 53461 MAIN ROTOR SWASHPLATE HAS GREASE IN BOOT. REPAIRED. 1G71 3U O H2SW 20031229000672003122900067NM 2003 12 29 03FDEA02181 120031212A5753ARC0503 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT O/B FLAP, FOUND O/B HINGE FITTING I/B EDGE WITH CHIPPED MARK. COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040105000072004010500007NM 2004 1 5 DL738030998 120031110A2120 ODOR BOEING737 737832 13844CFNM COCKPIT DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO2737700 29631 IN DESCENT MUSTY ODOR LIKE DIRTY SOCKS EMINATED FROM AIR CONDITIONING SYSTEM SYSTEM. ODOR NOTICED IN FLIGHT DECK-NOT NOTICED IN CABIN. INSPECTED PACK BAYS AND RAN PACK ALL SETTINGS, NO ODORS OR DEFECTS NOTED. 2L72 4F RTA16WE 20040105000732004010500073NM 2004 1 5 03FDEA02209 120031217A5754ARB2850505 FITTING DOUG MD11 MD11 3023602NM L/E SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, FOUND NR 16 SLAT TRACK, INBOARD FITTING CRACKED, APPROX 0.250 INCH IN LENGTH. NR 16 SLAT TRACK, INBOARD FITTING REMOVED AND REPLACED NEW RIB FITTING ARB2850-505 AS PER SRM 51-33-01 VOL. II AND OPERATION CHECK CARRIED OUT AS PER AMM 27-80-30. 2L73 4F RTA22WE 20031229001582003122900158EA 2003 12 29 SWIA200312663 120031205A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 625 RIGHT INTERCOSTAL STRINGER 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20031009000542003100900054NM 2003 10 9 03FDEA01697 120031003A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 FWD CARGO SIDE FRAME DENTED STA 700 LBL 50 WL 166 FWD CARGO FRAME DENTED AT STA 700, LBL 50, WL 166 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE FRAME PER SRM 51-40-3. ALSO REPAIRED PER FED EX EA 7-5310-55031. 2L73 4F RTA3WE 20040108000652004010800065SO 2004 1 8 DYV2003F00002 220030929A8500GTSIO520L ENGINE CESSNA421 421C 2076016CE CONT O520 TSIO520* 17040SO LEFT FAILED E DYVAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM07911EA 1590 421C0870 608678 SHORTLY AFTER TAKEOFF, THE PILOT EXPERIENCED AN UNEXPLAINED GRADUAL LOSS OF POWER ON THE LT ENGINE. AFTER FEATHERING THE LT PROP, THE PILOT MADE A SAFE, ON AIRPORT LANDING. UPON INITIAL INSPECTION AFTER LANDING, THE ENGINE WAS FOUND SEIZED AND UNABLE TO ROTATE THE PROPELLER. NO OTHER INDICATIONS FOR ENGINE FAILURE COULD BE FOUND AT THIS TIME. THIS ENGINE HAD 12 HOURS TO GO TO NORMAL TBO. (OPEN) 1L72 3O3 O A7CE E8CE 20031202000312003120200031NM 2003 12 2 ASAA0310504 120030603A5311BAC14902807 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 887, STRINGER 24L-25L CORRODED. REMOVED DAMAGED SECTION OF FRAME AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031202000522003120200052NM 2003 12 2 USAASB03190 120031017A335020121 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 FOUND L1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER. (M) 2L72 4F RTA16WE 20031203000242003120300024NM 2003 12 3 GAIA03123ST 120031023A53117075T6 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND CABIN FRAME DENTED BS 540 STRINGER 17 RT. REF FASI N/R NR 61417, CUT OUT DAMAGE, INSTALLED DOUBLER REPAIR 8 INCH BY 5 INCH PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20040114002232004011400223EA 2004 1 14 03364701 120031230A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27701BR 7448 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNED OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040115000782004011500078NM 2004 1 15 03FDEA02336 120031230A5321 FLOOR PANEL DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK FLOOR PANEL 231BF FOUND TOP SURFACE DAMAGE. CABIN COMPARTMENT FLOOR PANEL 231BF REMOVED AND REPLACED AS PER AMM 53-21-04-4. 2L73 4F RTA22WE 20040121000412004012100041NM 2004 1 21 03FDEA02298 120031226A5350AKC754146 STIFFENER DOUG MD11 MD11 3023602NM ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 TAILCONE RT FWD MOST EDGE TOP STIFFENER FOUND CHAFED. TAILCONE RT FWD MOST EDGE TOP CHAFED DOUBLER REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II. 2L73 4F RTA22WE 20031208000932003120800093NM 2003 12 8 QXEA200301325 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 LEFT OUTBOARD TRACK NR 2 TOP INBOARD EDGE GOUGED/NICKED, APPROXIMATELY X469.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2H72 4T RTA13NM 20031209000402003120900040SO 2003 12 9 SWIA200312547 120031028A3230 PLUNGER EMB 120 EMB120ER 3260203SO SEQUENCE VALVE DAMAGED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07564SW 120339 DURING GEAR RETRACTION, LEFT MAIN LANDING GEAR WOULD NOT RETRACT. CYCLED LANDING GEAR 6-7 TIMES WITH SAME RESULT. RETURNED TO AIRPORT WITH NO FURTHER PROBLEM. REPLACED LEFT OUTBOARD MLG DOOR BEARING AND ADJUSTED LEFT OUTBOARD SEQUENCE VALVE PLUNGER IAW MM 32-32-04. OPS CHECK GOOD. 2L72 4T RTA31SO 20031209001212003120900121NM 2003 12 9 AWXA200301335 120031030A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 SEA - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANTS STATION WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040129000402004012900040EU 2004 1 29 MALA030598 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 13D & 13F FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 13D, 13F IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20031014000492003101400049NM 2003 10 14 SWAA032185 120030930A2612894481 FIRE LOOP BOEING737 7373H4 1384600NM APU BAY FAULTY A SWAAFB ACTIVATE FIRE EXT. EMER. DESCENT N FALSE WARNING CRCRUISE 1 SW29341SW 24091 DECLARED EMERGENCY, APU FIRE WARNING LIGHT ILLUMINATED, DISCHARGED BOTTLE. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE. REMOVED AND REPLACED FWD APU FIRE DETECTOR LOOP PER MM. 2L72 4F RTA16WE 20031211001872003121100187WP 2003 12 11 2003F00643 120030809A53109921166112 DOOR FRAME DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 FOUND C-CHECK SERVICE, UPPER CARGO DOOR, FRAME INBOARD FLANGE CRACKED, STA Y = 392.062 BETWEEN LONGERONS 13 LEFT AND 14 LEFT. THE DAMAGED PART WAS REPAIRED. (M) 2L72 4F A6WE 20030916000752003091600075WP 2003 9 16 GTIA030640 120030805A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND CABIN FLOOR PANEL 'HAT' CHANNEL CRACKED AT END FS 1174-1250. STOP DRILLED CRACK. FORMED HAT CHANNEL DOUBLER. INSTALLED FASTENERS. (M) 2L72 4F RTA6WE 20030919001602003091900160 2003 9 19 375PA0019 420030816A22104084042911 COUPLER BOEING737 73739A 138447PNM YAW DAMPER INOPERATIVE A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05375PA 23812 YAW DAMPER INOPERATIVE. RELEASED ON MEL 22-3-1. 8/16/2003: REPLACED YAW DAMPER COUPLER IAW MM22-12-32 PG.401 AND ACCOMPLISHED OPS. TEST, SELF TEST, SERVO TEST AND RUDDER PRESSURE REDUCER TEST. ALL OK. 2L72 4F RTA16WE 20030916001042003091600104EU 2003 9 16 ASOA03396 120030823A3210S3238006120100 SUPPORT BRACKET AEROSPATR72 ATR72212 8680945EU MLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11535AS 464 DURING HANGAR MAINTENANCE IN MCN, THE LEFT MLG UPLOCK SUPPORT BRACKET ON THE TOP SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT MLG UPLOCK SUPPORT BRACKET ON THE TOP SIDE IAW SRM 51-00. (M) 2H72 4T RTA53EU 20030918000992003091800099WP 2003 9 18 IXXA0300054O 120030805A3260 UPLOCK SWITCH DOUG DC8 DC873F 302199FWP MLG MALFUNCTIONED A IXXAO OTHER N FALSE WARNING CLCLIMB 1 SW11605AL92464441 46106 ENROUTE FROM KLAX TO KTOL LANDING GEAR UPLATCH CHECK FAILED. CREW CYCLED GEAR UNTIL GOOD CHECK ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT IN KTOL. MAINTENANCE INSPECTED SYSTEM CLEANED AND LUBRICATED RT MLG UPLATCH SYSTEM AND ASSOCIATED COMPONENTS. GEAR OPERATIONAL CHECK GOOD. ALL WORK COMPLETED PER APPLICABLE MANUALS AND AIRCRAFT RETURNED TO SERVICE 2L74 4F RT4A25 20030922000452003092200045EU 2003 9 22 RAIA00308211 120030813A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03560HK 41076 EMERGENCY ESCAPE PATH LIGHTING INOP. SECURED CONNECTOR TO PATH LIGHT STRIP 2L72 4T RTA41NM 20030924000512003092400051NM 2003 9 24 DL738030765 120030817A3350 BULB BOEING737 737832 13844CFNM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO273738B 30382 DURING OVERNIGHT INSPECTION MTC FOUND EMERGENCY LIGHT INOPERATIVE ABOVE SEAT 7C. MTC REPLACED BULB AND EMERGENCY LIGHT ABOVE 7C TESTS NORMAL. 2L72 4F RTA16WE 20030924000952003092400095NM 2003 9 24 AWXA200300987 120030815A53106516300191 BEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1/8 INCH CRACK WAS FOUND ON BEAM WEB AT INSULATION MOUNT HOLE BS 184, RBL 17.1, WL 178. MAINTENANCE CUTOUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 184, RBL 17.1, WL 178, AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACK EXISTS; FABRICATED A - 3 DOUBLER & -5 WEB; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-10-11, PG. 1, FIG. 011. 2L72 4F RTA16WE 20030925000212003092500021 2003 9 25 AALA20030761 420030709A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21638AA 24596 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001012003092400101NM 2003 9 24 03FDEA01284 120030807A5753ARC198413 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING O/B FLAP I/B HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTACHMENT I/B & O/B BORE HOLES FOUND CORROSION. LT WING O/B FLAP I/B HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTACHMENT I/B & O/B HOLES BORE REPAIRED AS PER FEDEX EA 1-5750-63120, 2L73 4F RTA22WE 20040130000232004013000023 2004 1 30 SWAA032818 420031226A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20040205000072004020500007NM 2004 2 5 P5CA0300988 120031115A2823MA11A11731 ACTUATOR BOEING747 747236B 1384804NM PWA JT9 JT9D7Q 52054NE FUEL SHUTOFF FAILED A P5CAD RETURN TO BLOCK YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 WP23924FT 21730 702031 NR 3 ENGINE FAILED TO START. REACHED 40 PERCENT, THEN APPEARED TO FLAME OUT. REPLACED FUEL SOV ACTUATOR. 2L74 4F4 F A20WE E3NE 20040217001432004021700143CE 2004 2 17 J4P2004F00001 120031009A2810 FUEL TANK CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C93 GL RT< WING CORRODED E J4PAK NONE O OTHER ININSP/MAINT 1 SO134837A 414A0101 R519028 941291 DURING ANNUAL INSPECTION, IT WAS DISCOVERED TO HAVE SURFACE CORROSION AT THE LT AND RT WING UNDERNEATH COMING FROM THE FUEL TANK AREA. LOCATION WAS IMMEDIATELY AFT OF THE FWD SPAR. THE PATCH IS LOCATED AT WS 119.29 AND ENDS AT WS 133.29 AND EXTENDS FROM THE FWD SPAR AFT 12 INCHES. THE CORROSION ON THE ORIGINAL SKIN WAS COMPLETELY CUT OUT BY REMOVING AT 5 INCH X 6 INCH AREA AT BOTH WING TANKS IN THE IDENTICAL SAME AREA. THIS WAS NOTICED BY THE RIPPLE OF PAINT CAUSED BY THE SURFACE CORROSION UNDERNEATH WITH JUST A SMALL AMOUNT OF PAINT MISSING THE SIZE OF A DIME. THIS AREA IS WHERE WATER WOULD ACCUMULATE NEXT TO A CHANNEL INSIDE THE TANK WHERE NO SUMP DRAIN IS LOCATED. (SO13200400166) 1L72 3O3 O A7CE E8CE 5 CP22EA 20030520001542003052000154NM 2003 5 20 2003F00282 120030121A5313 STRINGER BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND FLOOR STRINGER CRACKED AT STATION 950D, ABOVE STRINGER 29R. STOPPED DRILL FOR CRACK TERMINATION. FABRICATED ANGLE REPAIR. TREATED, PRIMED AND INSTALLED AT FUSELAGE STATION 950D, STRINGER 29R. (M) 2L73 4F A3WE 20030609001352003060900135NM 2003 6 9 AWXA200300580 120030502A5320146N5246U7 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK CORROSION WAS FOUND ON L/H CABIN FLOOR SUPPORT UNDER CUSP PANEL BS 1640 TO 1661. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT FROM BS 1640 TO 1661; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B 757-200 SRM 51-40-02, PG. 7. 2L72 4F RTA2NM 20030611000222003061100022WP 2003 6 11 GTIA030322 120030416A5412 FIRE SEAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE NR 2 ENGINE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 NR ENGINE APRON UPPER 6TH FROM FORWARD FIRE SEAL CRACKED. REMOVED CRACKED FIRE SEAL. FABRICATED NEW FIRE SEAL. INSTALL NEW FIRE SEAL. 2L72 4F4 F A6WE E2EA 20030613000782003061300078SO 2003 6 13 C2XA03SH174 120030608A532014525422001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 SHV-DURING C-CHECK THE LEFT HAND SILL AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030617002222003061700222NM 2003 6 17 QXEA200300734 120030613A1430 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM STRESS PANEL BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX- STRESS PANEL 622AT HAS SPINNING SCREW AND NUTPLATE AT FORWARD OUTBOARD HOLE. REPAIRED IAW DHC-8 Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030617002552003061700255NM 2003 6 17 QXEA200300679 120030606A2910DSC252B40124 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007NM NLG BROKEN A QXEAO OTHER K FLUID LOSS UKUNKNOWN 1 NM09361PH 516 SEA-ON FLIGHT NUMBER 2065, AFTER GEAR EXTENSION, NR 2 HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. NR 2 ENGINE HYDRAULIC PUMP AND NR 2 RUDDER HYDRAULIC CAUTION LIGHTS ILLUMINATED. FOUND BROKEN WIRE FOR NOSE GEAR EXTENSION LINE. INSTALLED NEW NOSE GEAR EXTENSION LINE FOR DRAG STRUT ACTUATOR. LEAK CHECK GOOD SERVICE NR 2 HYDRAULIC SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030618000862003061800086NM 2003 6 18 SWAA031299 120030610A53126517582 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED D-CHECK, FOUND UPPER CHORD CRACKED AT BS 178, WL 233, LBL 25. REMOVED AND REPLACED UPPER CHORD PER SRM. 2L72 4F RTA16WE 20030618000912003061800091NM 2003 6 18 SWAA031277 120030606A57536546434 SKIN BOEING737 737301 1384611NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C2 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM 2L72 4F RTA16WE 20030527000472003052700047NM 2003 5 27 DLM88030333 120030403A2133 SELECTOR KNOB DOUG MD88 MD88 3023688NM COCKPIT JAMMED A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27912DE 49997 AFTER TAKEOFF AUTO PRESS INOP LIGHT INOP ILLUM, WENT TO MANUAL PRESS AND COULD NOT CLOSE OUTFLOW VALVE. OUTFLOW VALVE WOULD OPEN, BUT NOT CLOSE. AIR TURNBACK AIRCRAFT RETURNED TO LGA. FOUND AUTOPILOT SELECTOR KNOB JAMMED IN OUTFLOW VALVE CONTROL WHEEL IN PEDESTAL. REMOVED KNOB OUTFLOW VALVE, OPS NML IN MANUAL. RESET NR 1 AND NR 2 AUTO PRESS CONTROLLERS. AUTO NOW OPS NML. INSPECTED OUTFLOW VALVE FOUND NML. 2L72 4F RTA6WE 20030521001832003052100183WP 2003 5 21 DHL2003604514 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD L/E FORMER AT STA XFS 741.250 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030522001292003052200129NM 2003 5 22 SWAA031131 120030519A53206545813 DOOR FRAME BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT BS 332.1, STR 8R. REPAIRED DOOR FRAME PER SWA EA. 2L72 4F A16WE 20030528000932003052800093SW 2003 5 28 AC2A086464 120030518A21505861653 TURBINE BELL 430 430 1182150SW A/C PACK ROUGH E AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CT2657 49089 COOLING TURBINE IS ROUGH. COOLING TURBINE FAILED. REPLACED TURBINE WITH SERVICABLE TURBINE. 1G72 3U RTH9SW 20030618001062003061800106 2003 6 18 HEEA087495 420030612A2561PHI10090 LIFE VEST BELL 407 407 1182206SW CABIN LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 LIFE VEST LEAKING. REPLACED. 1G71 3U O H2SW 20030625000512003062500051EU 2003 6 25 03FDEA00816 120030527A5410 SPAR AIRBUS300 A300B4605R 3930308EU PYLON DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 COMPLY WITH E.A.6-5455-70907 PYLON- REPAIR OF FWD FAIRING UPPER SPAR ANGLE 9333M29P112A. FACT 27MAY03 11:32 BFM U WORK COMPLIED WITH IAW/E.A. 6-5455-70907, PYLON-REPAIR OF FWD FAIRING UPPER SPAR ANGLE 9333M29P112A.IAW/51-70-40-FIG 201. 2L72 4F RTA35EU 20030714000802003071400080NM 2003 7 14 SWAA031415 120030624A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 11 AND 13. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030630000922003063000092SW 2003 6 30 HEEA087854 120030610A6510407040303119 SHAFT BELL 407 407 1182206SW BLOWER DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 TAIL ROTOR BLOWER SHAFT HAS A FORWARD BEARING BAD. REPLACED BEARING 407-340-339-101, S/N ZV14022 AND ZV14951 DUE TO ROUGH. REPAIRED. 1G71 3U O H2SW 20030711000532003071100053EU 2003 7 11 MALA030317 120030617A5753 SPAR SAAB SF340 340B 7860101EU TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 DURING 4K INSPECTION IN CWA, RT FLAP REAR SPAR CRACKED AT WS 142. MAINTENANCE COMPLETED REPAIR ON REAR SPAR IAW EO S57007. REF NR 179683 FOR INFORMATION. A/C RELEASE DATE IS 6/19/03. 2L72 4T RTA52EU 20030714001172003071400117NM 2003 7 14 CALA0300350 120030701A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED AT STA 937. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030714001292003071400129NE 2003 7 14 C1HA200394012 220030628A7530658385 BLEED VALVE BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 2 ENGINE FAILED A C1HAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION LDLANDING 1 GL15294AS 22146 NR 2 ENGINE COMPRESSOR STALL ON FINAL AS POWER ADDED. ON GROUND COMPRESSOR STALL WHILE TAXIING. 2L73 4F4 F A3WE E2EA 20030716000332003071600033NM 2003 7 16 USAABB03100 120030621A3350873203193 MODULE BOEING757 7572B7 1384964NM EMERGENCY LIGHT WEAK A USAAK NONE O OTHER ININSP/MAINT 1 EA19631AU 27809 FOUND THE FORWARD EMERGENCY AISLE LIGHT MODULE BATTERY WEAK. MAINTENANCE REPLACED THE MODULE. (M) 2L72 4F RTA2NM 20030710001292003071000129EU 2003 7 10 03169320 120030618A3350 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DAMAGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27320UE 41043 DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE FROM SEAT ROWS 1 TO 4. MAINTENANCE PERSONNEL REPAIRED THE WIRING FOR THE EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030716000042003071600004SO 2003 7 16 SIMA200314801 120030522A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21810AE 145525 ABI - DURING AN IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND 18 INCH BY 2 INCH EXTERNAL ANGLE, 10 INCH BY 2 INCH FILLER, 8 INCH BY 1 INCH PLATE AND 6 INCH BY 1 INCH SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142, REV 21, CHAPTER 53-21-10 FIG 201 SHEET 1. (M) 2L72 4F RTT00011AT 20030717000982003071700098NM 2003 7 17 TSAA0333125 120030524A335086210066 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 REPLACED FORWARD ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030717000202003071700020SW 2003 7 17 HEEA087997 120030627A6720407001026101 TUBE BELL 407 407 1182206SW TAIL ROTOR DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 TAIL ROTOR CONTROL TUBE BEARING DEFECTIVE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030110000522003011000052WP 2003 1 10 MWEA030030 120030110A533059101413 SKIN DOUG DC9 DC981 3022081WP CARGO DOOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 FORWARD CARGO DOOR OUTER SKIN IS DAMAGED ON THE LOWER EDGE NEAR THE CENTER OF THE DOOR. -- FABRICATED AND INSTALLED NEW DOUBLER AND SHIMS. 2L72 4F A6WE 20030127001032003012700103EA 2003 1 27 COMA0360048 120030123A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER SW AFFECT SYSTEMS INADEQUATE Q C ININSP/MAINT 1 SO01975CA 7150 FLIGHT 5530 EMERGENCY FLOOR LIGHTS AT WING EXITS ARE INOP.FOUND LIGHTS DISCONNECTED - RECONNECTED WIRING AT EXIT LIGHTS. 2L72 4F RTA21EA 20030127002062003012700206SW 2003 1 27 HEEA083698 120030115A2820206064263101 LINE BELL 407 407 1182206SW FUEL SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 FUEL LINE FERRELS FROZEN DUE TO CORROSION. 1G71 3U O H2SW 20030127002642003012700264SW 2003 1 27 HEEA083739 120030115A2897 CONNECTOR BELL 407 407 1182206SW FUEL BYPASS LITEDAMAGED E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03501PH 53401 "B" PIN LOOSE CAUSING FUEL FILTER LIGHT IN COCKPIT TO ILLUMINATE ON CAUTION PANEL. 1G71 3U O H2SW 20030128001822003012800182SW 2003 1 28 HEEA083881 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030204000552003020400055NM 2003 2 4 SWAA030205 120030127A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030128002532003012800253SW 2003 1 28 HEEA083900 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH NHFS5642 53400 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030129000122003012900012SW 2003 1 29 HEEA083922 120030117A6720407001732101 BELLCRANK BELL 407 407 1182206SW T/R CONTROL WORN E O OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 TAIL ROTOR CONTROL BELLCRANK HAS A WORN BEARING. 1G71 3U O H2SW 20030131001792003013100179NM 2003 1 31 UPS03240127 120030108A5753 FLAP TRACK BOEING727 72722C 138400FNM NO.2 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C+SI NO.2 FLAP TRACK HAS CORROSION IN BORE OF HOLE.D. NO.2 FLAP TRACK REPAIRED IAW SMRO EO 2003-003-002 2L73 4F A3WE 20030205000562003020500056CE 2003 2 5 NSVA200300004 120030204A5200 CABLE BEECH 1900 1900D 1154162CE A NSVAK NONE S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA27243CJ UE43 Airstair door would not open. Maintenance found one door support cable "jamed" on the forward edge between the door and structure. Maintenance dislodged cable, performed multiple operational check of door with no defects noted. 2L72 4T RTA24CE 20030212000462003021200046 2003 2 12 C2XA03BT030 420030211A2300 CONNECTOR EMB 145 EMB145ER 3260211SO COCKPIT AREA FAULTY A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2715941 145035 CVG/EWR---CO2547, CREW REPORTED "SMOKE COMING OUT PA PHONE BEHIND CAPTAINS HEAD." CVG MAINTENANCE TROUBLESHOT PROBLEM TO FORWARD PA UNIT. DISABLED PA SYSTEM, PULLED PA AND INTERPHONE CIRCUIT BREAKERS AND FORWARD PA CANNON PLUG CONNECTOR. AIRCRAFT MAINTENANCE FERRIED TO EWR. EWR MAINTENANCE REPOSITIONED CIRCUIT BREAKERS INTO NORMAL POSITION IAW EMB145 AMM #20-13-06. REMOVED AND REPLACED FLIGHT ATTENDENTS FORWARD HANDSET IAW EMB145 AMM #23-31-03. FOUND TWO WIRES TO BE BROKEN AND CANNON PLUG P8300 TO BE BAD. REMOVED AND REPLACED CANNON PLUG IAW EMB145 AMM #20-50-00, AND REPAIRED BROKEN WIRES IAW EMB145 MM #20-21-00. OPS.CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030218002522003021800252NM 2003 2 18 SWAA030249 120030130A335007912 COVER BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 EEPLS COVER DAMAGED AT ROW NR 16. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20030220000252003022000025NM 2003 2 20 03FDEA00121 120030213A5210 ROLLER BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE PAX DOOR FAILED A FDEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO25480FE 21462 DURING CLIMBOUT HEARD (LOUD) BANG AS IF SOMEONE HIT AIRCRAFT WITH HAMMER. SOUND OCCURRED AGAIN ABOUT 2 MINUTES LATER (BANG) WERE SO VIOLENT IT COULD BE FELT THROUGH SEATS. AFTER LANDING FOUND UPPER AFT ROLLER CAM ASSEMBLY ON FORWARD ENTRY DOOR BROKEN. BOTTOM ROLLER ALSO BROKEN. ** S/D ** COMING 2L73 4F4 F A3WE E2EA 20030220000712003022000071NM 2003 2 20 VNAA0301030 120030127A3243 MASTER CYLINDER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT LACK OF LUBE A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07429JS 3043 THE CAPTAINS LEFT HAND BRAKE WAS NOT WORKING. MAINTENANCE INSPECTED AND SERVICED THE CAPTAINS MASTER CYLINDER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030221000332003022100033EA 2003 2 21 QXEA0300143 120030114A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 CKB- TWENTY OVERSIZED HOLES AT STRINGER 12 THREW BULKHEAD. REPAIRED IAW HORIZON AIR EO 601R-53-3778 AND EA R-53-69. 2L72 4F RTA21EA 20030224000232003022400023 2003 2 24 BAQA084095 420030206A23124004512 ANTENNA BOLKMS117 BK117A1 5626010EU CORRODED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01136AE 7234 ANTENNA HAS CORROSION. HOUSING IS SPLIT. 1G72 3U H13EU 20030224000722003022400072GL 2003 2 24 HEEA084192 220030213A74219550175400 IGNITER AEROSPAS355 AS355* EU ALLSN 250C 250C* GL ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 ENGINE RT SIDE IGNITER WORN. 1G72 3U3 U H11EU E4CE 20030625001062003062500106NM 2003 6 25 F3LA200300088 120030225A5320 INTERCOSTAL BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT/INTERCOSTAL (WEB STRAP)FROM STA. 1006 BACK, LBL 2, CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB STRAP AND GALLEY BRACKET FROM STA. 1006 TO STA. 1031, LBL 2, PER SRM 51-30-02 AND BOEING DRAWING 65-46812. 2L72 4U RTA16WE 20030226000202003022600020SW 2003 2 26 HEEA084313 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH 53435 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030303000112003030300011EA 2003 3 3 03059630 120030228A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA WORN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING PREFLIGHT INSPECTION THE EMERGENCY TRACK LIGHTING BETWEEN ROWS 2-5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE TRACK LIGHTING CONNNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030304000272003030400027SO 2003 3 4 C2XA03CL061 120030301A3350GE1317 LAMP EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2716981 145208 TYS FLIGHT#2089 THE CREW REPORTED THE EXIT SIGN BY THE GALLEY DOOR WAS INOPERATIVE.MAINTENANCE REPLACED THE LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030204002202003020400220NM 2003 2 4 SWAA030169 120030123A335010126211 LIGHT BOEING737 7373K2 13844BANM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29340LV 23738 FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030625001132003062500113WP 2003 6 25 MWEA030059 120030208A57205910066513 FILLET DOUG DC9 DC932 3022066WP LT WING CRACKED A MWEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL31401ME 47133 CREW REPORTED LEFT SIDE WING AREA VIBRATION WITH FLAPS UP AND GEAR RETRACTED. FOUND FILLET CRACKS AND RIGHT ACM DUCT SUPPORT BRACKET BOLTS BROKE. REPAIRED FILLET PER SRM 53-01 AND WELDED REPAIR DUCT MOUNT FLANGES. 2L72 4F A6WE 20030214000572003021400057WP 2003 2 14 ASAA0380041 120030105A532159366031 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL IS CORRODED. REPLACED PANEL IS SRM 51-10-4. (M) 2L72 4F RTA6WE 20030216000022003021600002SO 2003 2 16 RAIA00302031 120030202A30207821008 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03811HK5385 5385 145256 5310-ITH- RIGHT ENGINE ANTI- ICE FAIL MESSAGE. MAINTENANCE DEFERRED PER MEL 30-21-01-1. CLEARED DMI BY REMOVING AND REPLACING THE #2 ENGINE OVERPRESSURE SWITCH. 2L72 4T RTT00011AT 20030219001142003021900114NM 2003 2 19 SWAA030340 120030212A33506556633 LIGHT BOEING737 7372H4 138448CNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED EXIT LIGHT PER MM. 2L72 4F A16WE 20030220000132003022000013EU 2003 2 20 0302051 120030205A77125035T27G04 TORQUE SENSOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE ZONE 400 COKED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE03146SD3572035720 146 514 DRG725688 AFTER TAKE-OFF, ON CLIMB, THE CREW NOTICED A +/- 40 PERCENT TORQUE SURGE ON THE LT ENGINE TORQUE GAUGE. ALONG WITH THE TORQUE INDICATION THEY FELT THE SURGE OF THE LT ENGINE. THE CREW DID NOT NOTICE ANY OTHER ABNORMAL ENGINE INDICATIONS. AIRCRAFT RETURNED TO PIT, AIRCRAFT TAKEN OUT OF SERVICE IN PIT AT 1801(LT). PIT MECHANIC REMOVED AND REPLACED LT ENGINE TORQUE SENSOR, AND PCU. PERFORMED OPERATIONAL CHECK OF SYSTEM. AIRCRAFT RETURNED TO SERVICE 2-7-03. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030220000192003022000019EA 2003 2 20 03044660 120030213A2560P4010021 BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FLASHLIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27660BR 7519 CAPTAINS EMERGENCY FLASHLIGHT DIM. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK PERFORMED AND AIRCRAFT WAS RELEASED BY MAINTENANCE PERSONNEL FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030220000222003022000022NM 2003 2 20 03FDEA00075 120030123A5511ALC81312 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 COMPLY WITH EA 1-5510-67532, HORIZONTAL STABILIZER, RT SPAR CAP, REPLACEMENT IAW SR DRAWING REPLACES EA 1-5510-64246 PART 3 AND IS TERMINATING ACTION. HORIZONTAL STABLIZER, RT SPAR CAP REMOVED AND REPLACED IAW EA 1-5510-67532. HORIZONTAL STABILIZER, RT SPAR CAP REPLACEMENT IAW SR DRAWING SR11550010. 2L73 4F RTA22WE 20030220000752003022000075CE 2003 2 20 GLBA2003018 120030219A79001241014 TRANSMITTER BEECH 1900 1900C 1154161CE A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03101UE2619 UC101 HIGH OIL PRESS RT ENG, R&R LH OIL PRESS TRANSMITTER OPS CKE LEAK CKE GOOD 2L72 4T RTA24CE 20030220001842003022000184WP 2003 2 20 ARWA20030204 120030213A249750137002 RELAY DOUG DC8 DC863F 302198FWP BUSS TIE DAMAGED A ARWAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO19784AL 46135 NR 2 GENERATOR UNPARALLEL AND LOST NR 2 BUS POWER FAIL LIGHT. FOUND FZ-1 FUSE BLOWN ON GENERATOR CONTROL UNIT (GCU) NR 2 FOR BUS TIE CONTROL. REMOVED AND REPLACED GCU NR BUS TIE RELAY IAW MM 24-20-5 AND 24-20-1; WIRING CHECK ACCOMPLISHED AS PER W/D 24-1-2 NO TROUBLE FOUND. GENERATOR 2 OPERATIONAL NORMAL IAW MM 24-20-0. 2L74 4F 4A25 20030224000152003022400015SW 2003 2 24 ALGA084142 120030220A6520214040009109 GEARBOX BELL 214 214ST 1182106SW TAIL ROTOR WORN H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01390AL3642 28198 TAIL ROTOR GEARBOX MOUNT HOLE ELONGATED AND WORN AT CONTACT POINT. 2G72 4U H10SW 20030226000272003022600027NM 2003 2 26 DHL2003780003 120030226A3350 BATTERY BOEING727 727223 1384074NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01780DH 22006 1) BOTH EMERGENCY EXIT LIGHTS INOPERATIVE.2) REMOVED AND REPLACED BATTERIES, OPS CHECKED NORMAL IAW M/M 33-50-71. 2L73 4F A3WE 20030228000352003022800035SW 2003 2 28 HEEA084448 120030213A6330206031564003 BEARING BELL 206 206B3 1181506SW LINK MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322751 CT2876 3627 MAIN ROTOR TRANSMISSION MOUNT LINK HAS WORN BEARINGS. REPLACED 4, 206031564003 BUSHINGS DUE TO CORROSION AND BEARING 206031590003 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030228000422003022800042NM 2003 2 28 CALA0300074 120030206A5320 CREASE BEAM BOEING737 737524 1384721NM STA 360-380 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914639 28900 THE FUSELAGE SKIN WAS FOUND DENTED COMMON TO THE CREASE BEAM BETWEEN STA 360 TO STA 380. FURTHER INSPECTION FOUND THE CREASE BEAM OUTBOARD CHORD AND SHEAR WEB DAMAGED. THE SKIN DENT WAS WITHIN SRM LIMITS. THE DAMAGE WAS REPAIRED IAW ECRA 5310-04100. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 24 MONTHS 0R 3000 CYCLES, WHICHEVER COMES FIRST. 2L72 4F RTA16WE 20030313001722003031300172WP 2003 3 13 AALA20030128 120030131A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21450AA 49476 TUL - FOUND FUSELAGE SKIN CRACKED AT APPROX 1437 BETWEEN LONGERON L3R AND L4R AT 4 RIVET HEADS. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLERS PER SRM 53-01-00 FIG 4 SHEET NR 3 ON FUSELAGE SKIN BETWEEN L3R AND L4R. (M) 2L72 4F A6WE 20030306000132003030600013SW 2003 3 6 HEEA084726 120030217A3246AB412050016102 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 MLG SKID SHOE WORN. REPAIRED. 1G72 4U H4SW 20030306000992003030600099SW 2003 3 6 HEEA084806 120030221A6220412010100193FM BEARING BELL 412 412 1182202SW M/R HEAD SPINDLEDEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 SPINDLE BEARING UNBONDED FROM SPINDLE. REPAIRED. 1G72 4U H4SW 20030308000082003030800008EU 2003 3 8 RAIA00302056 120030226A2730C850176 PROBE JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03562HK7542 41078 5407-RIC- RIGHT STALL WARNING ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RIGHT AOA VANE. OPS CK OK. 2L72 4T RTA41NM 20030313001272003031300127NM 2003 3 13 0300476642 120030225A5330 SKIN BOEING747 747212B 1384886NM CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01642NW 21942 During "L" check found corrosion on #3 door forward upper door surround skin. Repaired per EA 66-193805. 2L74 4F A20WE 20030121000612003012100061 2003 1 21 HEEA083263 420030108A3421206075607103 GYRO BELL 206 206L3 1182108SW ATTITUDE IND MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F ATTITUDE GYRO WILL NOT CAGE. REPAIRED. 1G71 3U H2SW 20030122001172003012200117NM 2003 1 22 DL72S030039 120030109A3350900542 RACK BOEING727 727225A 1384077NM CABIN UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO278890Z 21859 ON PREFLIGHT EMERGENCY EXIT LIGHTS WOULD NOT ILLUM. DURING STDBY POWER CHECK. WHEN TURNED ON EMERG EXIT LIGHTS CAME ON MOMENTARILLY THEN WENT OUT. COCKPIT EMERG LIGHT NEVER CAME ON. REPLACED BATTERIES FOR TRACK LIGHTING AT L1 AND R1 DOORS COCKPIT EMERGENCY LIGHTS. REPLACED RACK ASSEMBLY FOR EMERG LIGHT PACK AT LT OVERWING EXIT SIGN, CKS OK. 2L73 4F RTA3WE 20030319000082003031900008WP 2003 3 19 GTIA030009 120030111A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CABIN FLOOR PANEL, AFT AUX TANK, FORWARD CENTER HAS SOFT/DETERIORATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030320001042003032000104NM 2003 3 20 2003UALA00095 120030126A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29353UA 24321 STATION 787 FRAME CRACKED AT STRINGER 9R SUPPORT RAIL CLIP ATTACH FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030327000652003032700065NM 2003 3 27 C1HA200388003 120030216A3260 BULB BOEING727 7272S7 138407ZNM MLG INDICATOR BURNED OUT A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15688CA 22344 "NOSE GEAR" GREEN LIGHTS-LEFT SIDE BURNED OUT. R & R LAMP ON NOSE GEAR GREEN IND OPS NORMAL. 2L73 4F A3WE 20030303001962003030300196WP 2003 3 3 DHL2003804541 120030205A53003754473501N FITTING DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF. N/R 1308 AFT CARGO COMPT.- FITTING CRACKED @ STA 1320 , L31L (MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW 53-1-0 PG 1 AND BOEING FAX SEU-LIM-03-0002H DATED JAN 20TH , 2003 REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, CLEANED , TREATED AND PRIMED AREA IAW SRM51-1-8B, INSTALLED NEW FITTING ON AFT CARGO COMPARTMENT @ STA 1320 , L31L IAW SRM 51-1-20D PG. 9 2L74 4F RT4A25 20030327001742003032700174SO 2003 3 27 C2XA03SH059 120030323A5310 BEAM EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAITENANCE REMOVED DAMAGE SECTION AND REPAIRED AFFECTED BEAM IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327001962003032700196CE 2003 3 27 CA030211009 120030121A3297 WIRE BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA MLG LOOSE W A UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CA (CAN) UPON ROTATION AND RETURN TO BASE, CREW SELECTED MLG UP. MLG RETRACTED TO APPROXIMATELY HALF WAY UP & WAS INOPERATIVE IN EITHER UP OR DOWN SELECTION. CREW EXTENDED MLG MANUALLY DOWN UNTIL AND RETURNED TO BASE. A/C LANDED WITHOUT INCIDENT AND MLG INSPECTED PRIOR TO TOWING. A/C AND WAS FOUND TO BE DOWN AND LOCKED. A/C WAS PLACED ON JACKS AND EMERGENCY EXTENSION SYSTEM DISENGAGED. MAINT PERFORMED MLG RETRACTION TEST AND FOUND SYSTEM OPERATIONAL. ON SECOND RETRACTION TEST, SYSTEM FAILURE WAS DUPLICATED. LANDING GEAR MOTOR WAS REPLACED, TESTS CARRIED OUT. MLG SYSTEM FOUND TO BE INOPERATIVE ON AN INTERMITTENT BASIS. INVEST REVEALED A LOOSE WIRE CONNECTION ON EMERGENCY MLG EXTENSION HANDLE SAFETY LOCK-OUT 1L72 3T4 T A14CE E4EA 20030722000262003072200026NM 2003 7 22 2003F00454 120030125A5553 FITTING BOEING727 727222 1384073NM VERTICAL STAB CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND VERTICAL STAB AT FIN STATION 316, HORIZONTAL STAB HINGE FITTING BEARING HOLE, RIGHT SIDE HAS CORROSION ON INSIDE DIAMETER. REWORKED VERTICAL STAB HORIZONTAL STAB HINGE FITTING BEARING HOLE AT RIGHT SIDE AND INSTALLED NEW BEARING. (M) 2L73 4F A3WE 20030424000302003042400030WP 2003 4 24 ZW0A0303206 120030317A33508039001 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13984TW 53634 THE EGRESS LIGHTS WERE INOPERATIVE FROM SEAT ROW 28 AFT. REPLACED THE POWER SUPPLY. CHECK-C 12-17-02 STL. 2L72 4F RTA6WE 20030424000452003042400045NM 2003 4 24 QXEA0300320 120030226A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - AFT BAGGAGE DOOR CUTOUT, UPPER, AFT CORNER, FUSELAGE SKIN IS CHAFED. REPAIRED IAW DHC-8 400 SRM 51-25-10 AND SRM 51-25-15. 2H72 4T RTA13NM 20030313002072003031300207NM 2003 3 13 AALA20030175 120030207A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21383AN 26995 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030116002092003011600209SW 2003 1 16 HEEA083124 120030108A6220206010361001 PITCH LINK BELL 206 206B3 1181506SW M/R HEAD CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032753F 2729 MAIN ROTOR PITCH CONTROL LINK HAS EXCESSIVE CORROSION ON AREA OF FORK MOUNT POINTS. SCRAPPED. 1G71 3U H2SW 20030327000912003032700091SO 2003 3 27 C2XA03BT012 120030120A5610163500112 WINDSHIELD EMB 145 EMB145ER 3260211SO COCKPIT CRACKED A C2XAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW2714933 145018 BWI---CO2476, CREW REPORTED FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT AIRCRAFT DIVERTED TO BWI. AIRCRAFT LANDED UNEVENTFULLY. EWR MAINTENANCE WORKING WINDSHIELD CHANGE AT THIS TIME. 2L72 4F RTT00011AT 20030121000752003012100075WP 2003 1 21 DHL2003802001 120030121A2611 LAMP DOUG DC8 DC873 302199CWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01802DH 46076 1) #4 SMOKE DETECTOR WILL NOT TEST.2) PLACED #4 SMOKE DETECTOR ON DMI #11684 MEL 26-6-1.3) REF. DMI #11684, #4 SMOKE DETECTOR WILL NOT TEST.4) RELAMPED SMOKE DETECTOR. OPS CHECKED GOOD PER M/M 26-10-1. THIS CLEARS DMI #11684. PLACARD REMOVED. 2L74 4F RT4A25 20030121002042003012100204SW 2003 1 21 HEEA083348 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW033107N 51512 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030314000702003031400070NM 2003 3 14 CALA0300052 120030217A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FS 663 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND A 2.75 INCH CRACK IN RT WHEEL WELL PRESSURE DECK AT FS 663, RBL 35. REPAIRED IAW SRM 53-60-51, PAGE 213-231. 2L72 4F RTA16WE 20030314002382003031400238NM 2003 3 14 CALA0300117 120030204A5330 SKIN BOEING737 737524 1384721NM STA 450 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0937615 27328 INSPECTION FOUND FORWARD CARGO DOOR CUTOUT SKIN CORRODED ON INNER SIDE JUST BELOW LOWER AFT DOOR STOP, STA 450, STRINGER 22R.. THE CORRODED SECTION WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5331-01121. 2L72 4F RTA16WE 20030317000782003031700078NM 2003 3 17 03FDEA00238 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 34L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030318000112003031800011SW 2003 3 18 BAQA084116 120030212A6330222031605109 FLEXURE BELL 222 222U 1182140SW GEARBOX DELAMINATED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01219HM4464 47573 DELAMINATION OF FLEXURE. REPLACED WITH SERVICEABLE UNITS. 1G72 3U H9SW 20030318001032003031800103NM 2003 3 18 F3LA200300100 120030228A5330 STRAP BOEING737 7373Q8 1384670NM STA. 789 - 792 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT CARGO STRAP CORRODED AND CRACKED FROM STA. 789 TO STA. 792, STR. 21-R TO 24-R. FABRICATED DOUBLER PER SRM 51-70-13, FIG. 1. 2L72 4F RTA16WE 20030303001922003030300192WP 2003 3 3 DHL2003804537 120030219A53007075 SKIN DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF N/R 2660; iterim repair on fwd lwr. corner of the aft pax entry door ref srm53-2-0 pgs. 125/126 fig. 18 sheet 2m (major repair) corr: performed major repair iaw srm53-2-0 fig 18 , removed interim repair from aft pax entry door fwd. lwr. corner iaw srm51-1-21 pg. 1 , cleaned , treated , and primed area iaw srm51-1-8b, fabricated filler(7075-t6al .125) + doubler (7075t6al .090) tripler(7075t6.125 iaw srm53-2-0 fig 18 cleaned , treated and primed iaw srm51-1-8b, installed filler, doubler and triplerwith conicle washers iaw srm53-2-0 fig 18 , srm51-1-21 pg 1 ,.srm51-1-20d pg 9 , srm51-1-26 pg.1 srm51-1-15 pg.1 2L74 4F RT4A25 20030324000072003032400007WP 2003 3 24 03FDEA00341 120030319A2910AJK7016505 LINE DOUG DC10 DC1030 3023501WP HYD SYSTEM FAULTY A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25321FE 47836 AFTER APPROX 3 HRS OF FLT WHILE CRUISING AT FL 330 NO 1 HYD SYSTEM QTY SLOWLY DECREASED FROM 6.0 GALS TO 2.8 GALS AND STILL SLOWLY DECREASING. TURNED OFF #1 HYD PUMPS C/W RED TABS. TURNED PUMPS ON FOR LANDING, CONFIGURATION TO FLAP 35 EXTENSION NOTED 2.3 GALS ON FINAL APPROACH. REPLACED HYD LINE ASSY PER M.M.20-10-01-2, TYPE 2 REPAIR. SERVICED #1 HYD SYSTEM AND OP'S AND LEAK CHECKED NO LEAKS NOTED A/C OK FOR SERVICE. 2L73 4F A22WE 20030326000082003032600008SO 2003 3 26 AUS20030095 120030131A2823 SELECTOR MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL FUEL SYSTEM RESTRICTED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL SELECTOR RESTRICTED. THE AIRCRAFT DID NOT COMPLY WITH THETCDS IN THAT THE FUEL SELECTOR PLACARD DID NOT CONTAIN A "BOTH" POSITION. FURTHER INVESTIGATION REVEALED THAT TWO STOPS FABRICATED USING TWO MS27039-1-12 SCREWS, TEN AN960-10 WASHERS, TWO AN960-10L WASHERS AND TWO MS20356-10 NUTS WERE POSITIONED IN SUCH A MANNER THAT THE "BOTH" POSITION COULD NOT BE SELECTED. TO SELECT FROM LT TO RT AND VISA VERSA REQUIRED GOING THROUGH THE "OFF" POSITION. MAULE WAS CONTACTED AND CONFIRMED THAT THIS CONFIGURATION WAS NOT AUTHORISED BY THEM. 1H71 3O3 ONC3A23 E286 5 CP920 20030714001472003071400147EU 2003 7 14 HEEA088084 120030618A6320350A37107412 UNIBALL AEROSPAS355 AS355* EU TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 M857 3004 TRANSMISSION HAS EXCESSIVE WEAR ON UNIBALL. REPLACED. 1G72 3U H11EU 20030421001202003042100120NM 2003 4 21 QXEA0300316 120030303A36207506593 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09379PH 530 SEA ON FLIGHT 2247- ON APPROACH NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. FOLLOWED CHECKLIST. LIGHT EXTINGUISHED FIVE MINUTES AFTER TURNING OFF NR 2 BLEED. REMOVED AND REPLACED NR 2 BLEED AIR OVER-TEMPERTURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030422000832003042200083SO 2003 4 22 SIMA200308903 120030222A531014522459003 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION CENTER BEAM RAMP IS CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM IAW EMB 135 SRM 51-40-02, 51-40-06 AND 51-20-03. (M) 2L72 4F RTT00011AT 20030422001212003042200121NE 2003 4 22 USAABB03032 220030304A7261 OIL SYSTEM BOEING757 7572B7 1384964NM RROYCERB211 RB211535* NE LT ENGINE OVERSERVICED A USAAC ABORTED TAKEOFF WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA19629AU 27807 MCO - FLT 606 - ON TAKEOFF ROLL, AT TAKEOFF POWER, OIL ODOR WAS NOTED IN THE CABIN. MAINTENANCE FOUND THE LEFT ENGINE OIL OVERSERVICED AND SERVICED TO THE PROPER LEVEL. (M) 2L72 4F4 FRTA2NM E12EU 20040223001892004022300189WP 2004 2 23 ABXA040027 120031230A5311591359577 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 CRACKED FRAME AT LONGERON 2 RT, STA. 1076. REPLACED SECTION OF FRAME BETWEEN 3 LT AND 3 RT IAW SRM 51-30-5. 2L72 4F A6WE 20030825001302003082500130SO 2003 8 25 C2XA03TY139 120030824A551014520736004 HOUSING EMB 145 EMB145 3260210SO HORIZ STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL SATB SPHERICAL BEARING HOUSING WAS FOUND TO BE WORN AND PITTED. MAINTENANCE ACCOMPLISHED A BLEND-OUT AND REAM REPAIR IAW E.C. 5510-01062 AND EMB M.M. 51-50-01. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030724000512003072400051NM 2003 7 24 SWAA031437 120030629A552065C2638416M SKIN BOEING737 7373H4 1384600NM RT ELEVATOR TAB DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB DELAMINATED AT NR 3 HINGE. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20030728000512003072800051NM 2003 7 28 SWAA031608 120030719A32503839001007 METERING VALVE BOEING737 7377H4 1384404NM NLG STEERING INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 NOSE GEAR STEERING INOP. REMOVED AND REPLACED STEERING METERING VALVE PER MM. 2L72 4F RTA16WE 20030728000692003072800069NM 2003 7 28 SWAA031528 120030712A33506104781 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030806000912003080600091SO 2003 8 6 C2XA03CL125 120030718A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714562 145611 DURING ROUTINE MAINTENANCE THE RT AND LT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030904000462003090400046EA 2003 9 4 SWIA200312331 120030817A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED ANGLE IAW CRJ REO 601R-53-61-117 REV. ''A''. ANGLE P/N: 601R-53-61-117-1 2L72 4F RTA21EA 20030905002012003090500201NM 2003 9 5 USAA030145 120030806A5330654576656 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48389 23319 PIT - FOND SKIN CRACKED 3 INCHES, RIGHT SIDE STATION 520 STRINGER 12 RT. INSTLALED EXTERNAL DOUBLER, TEMPORARY REPAIR PER EA 76766 PER SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20030814000252003081400025 2003 8 14 SWAA031696 420030730A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT SERVICE DOORDISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030814001562003081400156WP 2003 8 14 GTIA030574 120030702A5340 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND CABIN FS 1309 FRAME TO FLOORBEAM ATTACH FITTING CORRODED AND FAST CORRODED STRINGER 18R. REMOVED OLD FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20030821001832003082100183NM 2003 8 21 03FDEA01270 120030812A2612 FIRE WARNING DOUG MD11 MD11 3023602NM CARGO BAY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25588FE 48490 LOWER AFT CARGO FIRE MASTER WARNING AND ALERT CAME ON DURING CRUISE AT FLT 390 DIVERTED IN DEN MEL 12AUG03 DEN ACN RELEASED FOR SERVICE PER MEL CDL 3A 26-22-01- 02 CATEGORY 3A B EXPIRATION 3A 15AUG03 AFTER DOWN LOAD 2 C INSPECTED AREA FOR SMOKE AND 2 FOR FIRE FOUND NONE. NO FREIGHT ON 2F 2C EMPTY CANS UP LOADED. DEFERRED PER MEL 26-22-01-02. PER FAULT ISOLATION MANUAL 26-14-00 2C. PERFORMED RTS OF AMSC 2C, NO FAULTS NOTED. PERFORMED LIGHTS AND MANUAL TEST FUNCTION PER 26-14-03-00 2CSTEP 2. SYSTEM OK. AFTER MAINTENANCE PERFORMED 2C RED FIRE BOTTLE 231 PER MM CHP 26-22-01-4 PERFORMED TESTS PER MM CHP 26-22-01-5. SYSTEM CKS OK USED TESTER DZZ7703-501B 2FN 4831 MEL ISC 2FW 2FC IS OK FOR FLT. 2L73 4F RTA22WE 20030826001462003082600146NM 2003 8 26 MEX2003316 120030703A2424947F9453 GCU DOUG MD88 MD88 3023688NM ENGINE FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL 53175 FLT 6581 - MEX-CUN - AIRCRAFT RETURNED TO GATE, AC CROSS TIE NO TEST. DURING REVISION WAS DETECTED ACTR LIGHT AND APU PWR AVAIL LIGHTS ON. THE GCU AND BCU WERE REPLACED IAW MM 24-20-04/08 AND ENGINES AND GENERATION SYSTEM WERE TESTED, ALL CORRECT. (M) 2L72 4F RTA6WE 20030731000552003073100055 2003 7 31 QXEA200300770 420030623A2312EVR716110350A TRANSCEIVER BOMBDRDHC8 DHC8401 1390041NM VHF COMM MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09409QX3313 4051 PDX- ON FLIGHT 2315 FROM SEA, DIVERTED TO PDX DUE TO COM 1 STUCK ON 121.7. AIRCRAFT LANDED WITHOUR INCIDENT. REMOVED AND REPLACED NR 1 VHF COMM TRANSCIEVER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030916000302003091600030NM 2003 9 16 03FDEA00981 120030624A5712ARC41251 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT WING - O/B T/E FLAP ASSY FOUND NR 2 TRACK STOP ISLAND RIB CRACKED AT BARREL NUT MOUNT AREA. REMOVED AND REPLACED RIB AT LT WING OUTBD TRAILING EDGE FLAP IAW SRM 51-31-01 VOL. II AND EA 1-5750-71834 - WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR. 2L73 4F RTA22WE 20030916000842003091600084WP 2003 9 16 GTIA030662 120030821A7830 DOOR DOUG DC9 DC983 3022083WP THRUST REVERSER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 THRUST REVERSER S/N 1741, UPPER CLAMSHELL DOOR OUTBOARD TRAILING EDGE DELAMINATED. REPAIRED CLAMSHELL DOOR. (M) 2L72 4F RTA6WE 20030930001152003093000115NM 2003 9 30 03FDEA01485 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG O/B SIDE SURFACE CORRODED. 2L73 4F RTA22WE 20030908001612003090800161EA 2003 9 8 SWIA200312236 120030802A2910 DRAIN LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A SWIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM07499SW 7398 AFTER T/O AT APPROX 22,000 FT, TOTAL LOSS OF HYDRAULIC PRESSURE & FLUID NR 1. RETURNED TO SLC WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NR 1 HYDRAULIC CASE DRAIN LINE. OPS AND LEAK CHECK GOOD. P/N: 601-75238-5 2L72 4F RTA21EA 20031001000312003100100031NM 2003 10 1 UPS03241214 120030910A3350 BATTERY BOEING727 727108C 1384039NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: ASV, EMERGENCY EXIT LIGHTS INOPERATIVE IN COCKPIT AND FORWARD ENTRY REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY. OPS CKS GOOD. 2L73 4F A3WE 20031003000702003100300070SO 2003 10 3 C2XA03SH331 120030914A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031006001902003100600190NM 2003 10 6 03FDEA01661 120031001A5230 FRAME BOEING727 727200 138407ENM MAIN CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 MAIN CARGO DOOR AFT SIDE FRAME GOUGED 12 INCHES FROM LOWER CORNER. REPAIRED GOUGED MAIN CARGO DOOR FRAME AFT SIDE 12 INCHES FROM LOWER CORNER IAW FED EX EA 7-5230-70516 2L73 4F RTA3WE 20031027000292003102700029EU 2003 10 27 AWXA200301105 120030913A5320D53480043202 SILL AIRBUS320 A320232 3930326EU L2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL Y1732, FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORROSION ON L-2 DOOR SILL Y1732, FR 66; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW A320 SRM 53-41-14, PG 207-213, FIG 201. 2L72 4F RTA28NM 20030910000292003091000029WP 2003 9 10 DHL2003604536 120030430A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING INBOARD L/E FORMER CRACKED (0.250) STA XFS 703.750. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031028000762003102800076CE 2003 10 28 AMWA58 120030920A2612 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LEFT FIRE A AMWAO OTHER A FLAME/FIRE NRNOT REPORTED 1 CE07139ZV UE139 FIRE STARTED IN LEFT ENGINE. FIRE WAS EXTINGUISHED BY MOTORING OF ENGINE. 2L72 4T3 TRTA24CE E2NE 20031119000092003111900009NM 2003 11 19 03283403 120031010A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27403FJ 3149 DURING THE EMERGENCY LIGHTING POWER SUPPLY WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE 5LK POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031029001052003102900105EU 2003 10 29 MALA030437 120030928A30202351A000 VALVE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE ANTI ICE SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15512XJ E2326 DURING FLIGHT NR 3528,NR 4 ENG INTAKE LO PRESS ILLUMINATES WITH ENG ANTI ICE SELECTED ON AT HIGH POWER LOW PRESS EXTINGUISHES WHEN POWER IS REDUCED. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED VALVE P/N 2351A000 S/N ON 922300-7 S/N OFF 760380-3 PERFORMED GN RUNS ALL CK'S GOOD IAW AVRO AMM. 2H74 4F4 FRTA49EU E6NE 20031110001732003111000173 2003 11 10 UPS03541448 420031019A34174040800912 ADC BOEING757 75724APF 1384969NM E/E BAY MALFUNCTIONED A IPXAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO01454UP 25475 INSPECTION TYPE:N/A F/O'S AIRSPEED DIFFERS BY 20KTS IN FLIGHT, ALTERNATE ADC SELECTED CURES ADC INDICATION PROBLEM. RT ADC SEEMS INACCURATE ASSOCIATED MACH TRIM AND RUDDER RATIO EICAS MSGS DISPLAYED. ELEVATOR ASYMMETRY MSG DISPLAYED INFLIGHT AND MILD PITCH VIBRATION FELT IN FLIGHT CONTROLS WHILE CONFIGURING TO LAND. T/S SYSTEM AND REPLACED RIGHT ADC ACCOMPLISHED MCDP TEST 30 NO FAULTS NOTED. ACCOMPLISHED ELEVATOR FREEPLAY CHECK PER MM. CABLE AND RIG TENSION CHECK OK PER MM 27-31-00-5. 2L72 4F RTA2NM 20030919000272003091900027NE 2003 9 19 NACA20030106 220030809A7421URHB32E SPARK PLUG DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 4 ENGINE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F480 480 533265 33553 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING AT CRUISE POWER, AUTO RICH. REPLACED NR 6 CYLINDER SPARK PLUGS. CHECKED GOOD. 2L74 4R4 R A781 5E8 20031014000082003101400008 2003 10 14 BAQA089048 420030909A34161042011968E ENCODER BOLKMS117 BK117A1 5626010EU ALTIMETER MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1097 7243 BAROMETER SET DEFECTIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030321000732003032100073NM 2003 3 21 2003UALA00214 120030223A5754114W412013 SIGNAL COND UNIT BOEING777 777222 1385219NM NR 2 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 TRAILING EDGE WEDGE, NR 2 SLAT, DELAMINATED. REMOVED, REPAIRED AND REINSTALLED WEDGE. 2L72 4F RTT0001SE 20030801001062003080100106EA 2003 8 1 COMA0360329 120030718A2710 AILERON CNDAIRCL600 CL6002B19 1900309EA WING BINDING A COMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01712CA 7244 FLIGHT 5378 CREW REPORTED "AILERONS BINDING". COULD NOT DUPLICATE - NO AILERON BINDING NOTED - C/W COMAIR EO 27-075 FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20040223001312004022300131WP 2004 2 23 IXXA0300086O 120031224A3260 DOWNLOCK SWITCH DOUG DC8 DC862 3021970WP MLG BROKEN A IXXAO OTHER J WARNING INDICATION LDLANDING 1 SW11728PL851892727 45918 WHEN GEAR WAS EXTENED THE LT GEAR LIGHT DID NOT ILLUMINATE. AFTER CYCLING GEAR ALL THREE GEAR LIGHTS WERE NORMAL. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR DOWN LOCK INDICATION SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20030825000852003082500085NM 2003 8 25 CALA0300437 120030805A5345 MOUNT BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND RT AFT LAV AFT WALL MOUNT PADS CORRODED AT STA 947.5. THE MOUNT PADS WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030828001192003082800119WP 2003 8 28 MWEA030293 120030728A5313591140125 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 ELECTRICAL/ELECTRONICS COMPARTMENT LONGERON 25 LEFT IS CRACKED AT STATION 160. FABRICATED AND INSTALLED NEW LONGERON. 2L72 4F A6WE 20030829001752003082900175NM 2003 8 29 SWAA031812 120030812A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, BELOW STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030903000112003090300011NM 2003 9 3 SCNA03005 120030714A3350 LIGHT BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15806SY 28215 EMERGENCY LIGHT AT SEAT 6C INOP. RELAMPED EMERGENCY LIGHT. OPS CHECKED GOOD 2L72 4F RTA16WE 20030806000422003080600042NM 2003 8 6 AWXA200300824 120030709A5414D54530052200 SKIN AIRBUSA319 A319132 3930340NM NR 1 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 DURING C-04 CHECK CORROSION WAS FOUND ON AFT LOWER INNER SKIN OF THE NR 1 PYLON AFT FIXED FAIRING. MAINTENANCE CUT OUT DAMAGED AREA OF NR 1 PYLON AFT FIXED FAIRING SKIN BETWEEN RIBS 11-16A; FABRICATED A NEW REPLACEMENT SECTION OF SKIN; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG A20-A25. 2L72 4F RTA28NM 20030813002042003081300204NM 2003 8 13 SWAA031652 120030722A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030724000982003072400098NM 2003 7 24 AWXA200300756 120030628A7732 ENGINE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B1US GL NR 1 MALFUNCTIONED A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28305AW344206090 24012 727205 AT CRUISE, NOTICEABLE NR 1 ENG VIBE, VIBE DISAPPEARS AS THROTTLE REDUCED CLOSE TO IDLE, DECLARED EMERGENCY, LANDED. MX PERFORMED A/C VIBE MONITOR CHECK IAW T/C F2A77001, & PERFORMED POWER ASSURANCE CHECK PER T/C F5M71003, BOTH GOOD. SHOOK AILERONS, FLAPS, ELEVATORS, & AC PACK DOORS, NO DEFECTS NOTED. PERFORMED TEST FLT. DURING CLIMB NR 1 COMPRESS STALLED. MX FOUND 6TH STAGE COMPRESS WITH 4 BLADE TIPS MISSING & SEVERAL BLADES BENT. R & R NR 1 ENG, OPS CHECK GOOD. FOUND WEAR IN THE HPC ROTOR, AFT STATOR, COMBUSTION CASE &COMBUSTOR, BUT THIS DID NOT CAUSE STALL. STALL CAUSED BY FOD DAMAGE TO STAGES 6 THRU 9 OF HPC ROTOR. FOD DAMAGE ALSO NOTED TO VANES IN STAGES 4 & 5 OF HPC FWD STATOR, & STAGES 6 & 7. 2L72 4F4 FRTA16WE E2GL 20030728001132003072800113NM 2003 7 28 SWAA031550 120030712A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 907, STR 4R AND STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030822001722003082200172NM 2003 8 22 UPS03441102 120030723A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C FWD CARGO COMPT - RT STA 958-STA 960 STRINGER 44 FOUND CORROSION CRACKED. FORWARD CARGO COMPT - RT STA 950 - STA 970 S44 STRINGER REPAIRED IAW SRM 53-10-03 FIG.1. 2L74 4F A20WE 20030911000972003091100097WP 2003 9 11 DHL2003873506 120030611A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OUTBD L/E FORMER CRACKED 0.250 AT STA XFS 566.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9,10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911000992003091100099WP 2003 9 11 DHL2003873520 120030617A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING CENTER LE UPPER PLATING CORRODED AT XS.478.897 XW. 408.343. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12, FIG 4. REMOVED CORROSION FROM CENTER LE UPPER PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. REMOVED CORRODED PLATING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW PLATING IAW SRM 57-3-30 PG 12, FIG 4. CLEANED, TREATED AND PRIMED NEW PLATING INNER PART IAW SRM 51-1-8B. INSTALLED PLATING ON CENTER L/E, XW.408.000 - XFS.526.000 IAW SRM 51-1-21 PG 1. SRM 51-1-20A PG 9, SRM 51-1-15 PG 1. FOR REMOVAL AND INSTALLATION OF CENTER L/E SEE N/R 0903. 2L74 4F RT4A25 20030911002272003091100227NM 2003 9 11 DHL2003752004 120030821A3260 WARNING SYSTEM BOEING727 727223 1384074NM COCKPIT MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01752DH 22466 UPON DEPARTURE, WHEN RETRACTING GEAR (RED) LIGHT ON FORWARD PANEL REMAINED ILLUMINATED. OPS CHECKED OK IAW B727 M/M 32-61-81. NO DEFECTS NOTED. 2L73 4F A3WE 20031119000212003111900021NE 2003 11 19 00117 220031008A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05237TW 24237 PILOT REPORTED LT ENGINE FLAMED OUT WHILE CLIMBING TO FL410 IN CONTINOUS LIGHT TO MODERATE TURBULANCE, NO EMERGENCY WAS DECLARED, RELIGHT NORMAL AT FL250, CLIMB TO FL390 FOR REMAINDER OF TRIP, INSPECTION OF ENGINE CONDUCTED AT THE COMPLETION OF TRIP NO FOD OR LEAKS. 2L72 4J4 J A10CE 1E16 20031120000342003112000034NM 2003 11 20 AWXA200301243 120030925A554165C259713 RIB BOEING737 737301 1384611NM RUDDER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BRACKET BELOW UPPER RUDDER HINGE, AT RDR STA 196. MAINTENANCE REMOVED CRACKED BRACKET BELOW UPPER RUDDER HINGE AT RDR STA 196; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 65C25971; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20040106002012004010600201WP 2004 1 6 GTIA030979 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND FLOOR PANEL AFT ENTRY DOOR, EDGE SEAL DETERIORATING. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040109000162004010900016SO 2004 1 9 N6P2003F00001 220031105A8530 CYLINDER CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO ENGINE CRACKED D N6PAO OTHER O OTHER NRNOT REPORTED 1 EA13340AB191 340A0471 224033R CYLINDER NR 1 CRACKED IN THE HEAD AREA NEAR THE EXHAUST SIDE OF THE HEAD. NR 6 CYLINDER IS SUBJECT TO A SB. NR 03-7. THIS CALLS FOR REPLACEMENT OF CERTAIN CYLINDERS MANUFACTURED BETWEEN 9/1/2002 AND 4/21/2003. THIS CYLINDER IS NOT SUBJECT TO THAT BULLENTIN DUE TO ITS INSTALLED POSITION BUT THIS SUBMITTER RECOMMENDS THAT ALL ECI CYLINDERS BE INSPECTED FOR CRACKS AT 50 HOUR INTERVALS UNTIL REACHING 500 HOURS. A COMPRESSION CHECK WITH A SOAP SOLUTION APPLIED TO THE SUSPECT AREA WILL SHOW A DEFECT. 1L72 3O3 O 3A25 E8CE 20040113001572004011300157EU 2004 1 13 BAQA089451 120031113A6497117954021 WIRE BOLKMS117 BK117B1 5626012EU ROTOR TACH DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME6501 7235 ROTOR TACH INTERMITTENT NR 1 TRANS PRESSURE. REPLACED WITH SERVICEABLE UNIT. 11/24/03 1G72 3U H13EU 20040114001212004011400121NM 2004 1 14 DL757031055 120031125A3610149N7314116 DUCT BOEING757 757232 1384965NM A/C BAY BURST A DALAO OTHER O OTHER CRCRUISE 1 SO27634DL 23615 BLEED AIR Y-DUCT IN RT A/C BAY BURST CAUSING PNEUMATIC AIR ACCESS DOOR TO BE RIPPED FROM ITS HINGES DEPARTING ACFT. REPLACED DUCT AND DOOR. 2L72 4F RTA2NM 20031124001562003112400156NM 2003 11 24 QXEA200301307 120031019A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE CABIN DISCHARGED A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09359PH13050 514 PDX-ON FLIGHT NUMBER 2388, A PORTION OF EMERGENCY FLOOR LIGHTING IS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY AT PS-2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031217001902003121700190SO 2003 12 17 SWIA200312609 120031113A3350 LIGHT EMB 120 EMB120ER 3260203SO LT OVERWING SHORTED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07187SW 120037 EMERGENCY EXIT LIGHTS AT 6A AND 6C OVERWING EXIT AND THE MIDDLE CEILING LIGHT AS WELL AS FOUR OR FIVE FLOOR LEVEL LIGHTS DO NOT ILLUMINATE OR JUST BARELY LIGHT UP. FOUND SHORT AT LEFT OVERWING EMERGENCY EXIT FLOOD LIGHT. RECONNECTED, REPOSITIONED TERMINALS AND REPLACED INSULATION BOOT. OPS CHECK GOOD. 2L72 4T RTA31SO 20031218000112003121800011NM 2003 12 18 MWEA030454 120031125A534599365347 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 J-CHANNEL FROM STATION 160-200 IS CORRODED AROUND FASTENER HOLE JUST INBOARD OF PAX DOOR. FABRICATED AND INSTALLED J-CHANNEL. 2L72 4F RTA6WE 20031217001592003121700159NM 2003 12 17 AWXA200301532 120031205A5320654962156 SUPPORT BOEING737 737301 1384611NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON THE AFT CARGO DOOR UP LATCH HOOK CATCH SUPPORT ON CEILING AT BS 847. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO DOOR UP LATCH HOOK CATCH SUPPORT IAW B737-300 SRM 51-40-02, FIG 8 &12, PG 1 & 45. 2L72 4F RTA16WE 20031222000162003122200016EA 2003 12 22 SWIA200312645 120031129A2751601R930303 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07953SW 7813 CREW REPORTS LEFT FLAP INDICATES 15 DEGREES INTERMITTENTLY IN FLIGHT. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER ASSEMBLY IAW CRJ MM 27-55-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20031224000022003122400002WP 2003 12 24 GTIA030835 120031006A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND FORWARD CABIN FLOOR PANEL STATION 160-200 CENTER HAS SEVERAL INSERTS BROKEN OUT/CORRODED AND SOFT/MUSHEY. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20031224000112003122400011WP 2003 12 24 GTIA030803 120030907A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND SEAT TRACKS LEFT STA 826 TO 1307 BARE METAL, NICKS LIGHT CORROSION, ALL THREE TRACKS. REMVOED OUTBOARD SEAT TRACK STA 826-1307 LOCATED AND DRILLED OUTBOARD SEAT TRACK AND LOCATED AND DRILLED SPLICES INSTALLED OUTBOARD SEAT TRACK AND SPLICES. REMOVED INBOARD SEAT TRACK STATION 797-1307 LOCATED AND DRILLED INBOARD SEAT TRACK AND LOCATED AND DRILLED SPLICES. INSTALLED INBOARD SEAT TRACK AND SPLICES. (M) 2L72 4F A6WE 20031223001292003122300129EU 2003 12 23 MALA030542 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 10B FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 10B IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031014001432003101400143NM 2003 10 14 SWAA032064 120030916A57536546435339 SKIN BOEING737 7373H4 1384600NM OUTBD TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C1 CHECK, FOUND LT OUTBD T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED LT OUTBD T/E FLAP PER MM. 2L72 4F RTA16WE 20031021001032003102100103SO 2003 10 21 SIMA200325301 120030901A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-02 FIG 201. (M) 2L72 4F RTT00011AT 20040114001642004011400164NM 2004 1 14 03FDEA02016 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT O/B FLAP, O/B HINGE ACTUATOR HOLE NR 2 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031124000572003112400057NM 2003 11 24 03FDEA01903 120031111A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORRODED KEEL BEAM STR 29L, O/B FLANGE BS 950D - 1004. CORROSION ON KEEL BEAM STR 29L O/B FLANGE BS 950D-1004 REPAIRED PER EA 7-5310- 55109 & SR 27-53-023A. 2L73 4F RTA3WE 20031126000382003112600038WP 2003 11 26 DHL2003805569 120030730A534774529527 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 MAIN CARGO COMPT NR 1 SEAT TRACK LUG WORN AT STA 327.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17-18. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, 18, 19. 2L74 4F RT4A25 20031203001232003120300123NM 2003 12 3 USAA030229 120031111A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU48203 23595 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY 4 INCH AREA BEYOND LIMITS, BS 1016 AFT LAV FLOOR AREA T-CAP TOP SURFACE. INSTALLED REPAIR T-CAPS PER TYP REP 53-20-10 REV A. (M) 2L72 4F RTA16WE 20031204000532003120400053WP 2003 12 4 AALA20031054 120030922A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21419AA 49331 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 18 THROUGH 22. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040121000822004012100082EA 2004 1 21 ASOA03610 120031201A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040122000422004012200042NM 2004 1 22 ASAA040122C 120030324A521065C36251 SKIN BOEING737 737490 1384715NM PAX DOOR DENTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01703AS 28893 DURING C-CHECK, FOUND DENT ON AFT DOOR SKIN. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030918000262003091800026NM 2003 9 18 2003F00566 120030505A5311 FRAME BOEING737 7372L9 1384497NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO27464AT 21278 DURING C-CHECK INSPECTION, A CRACK WAS FOUND AT THE 0 BBL FUSELAGE FRAME AT BS 663. THE CRACK EXTENDS THROUGH THE UPPER CHORD AND THROUGH THE WEB. THE REPAIRS HAVE BEEN ACCOMPLISHED ON NON ROUTINE 031284, USING SB KIT 65C34537-1. RELATED TO THIS REPAIR IS A SUSPECTED PRESSURIZATION LEAK NOTED AT BS 663.75 ON NON ROUTINE 031167. THE REPAIR OF THE 0 BBL WILL ENSURE THAT THE PRESSURIZATION LEAK IS REPAIRED AS IT IS IN THE SAME AREA. (M) 2L72 4F RTA16WE 20030923000592003092300059WP 2003 9 23 DHL2003604703 120030527A534037504972N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT ACCESSORY COMPT FITTING AT STA 660.000 WITH 7.000 CRACK IN IT BETWEEN L-35R AND L-36. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-3-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040128002082004012800208WP 2004 1 28 UPS04841683 120031230A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:C3 RT WING L/E UPPER RIB IS CRACKED AT XFS 448. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040130002102004013000210WP 2004 1 30 ABXA040005 120031128A5313 LONGERON DOUG DC8 DC861 3021952WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 AFT CARGO AT STA 1200 - 122 AND LONGERON 28 LEFT HAD CORROSION. REMOVED CORROSION, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 51-1-8, 51-1-20D AND REA D853-48483MR. 2L74 4F 4A25 20040204000422004020400042EU 2004 2 4 AWXA200301261 120031010A5411D5453003220000 RIB AIRBUS320 A320231 3930325EU NR 2 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-03 CHECK 2 EACH 1 INCH CRACKS WERE FOUND ON LOWER END OF RIB NR 14, ON NR 2 PYLON AT AFT FIXED FAIRING. MAINTENANCE REMOVED NR 14 RIB AT AFT FIXED FAIRING, NR 2 PYLON; RECEIVED A NEW REPLACEMENT RIB; INSTALLED NEW RIB IAW 54-54-11, PG. 4, FIG. 1. 2L72 4F RTA28NM 20040210000362004021000036WP 2004 2 10 UPS03841614 120031016A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE:C3 (C) PIT DOOR OUT LOWER SIDE WEB CORRODED NR 3 AND NR 6 (T) BOLT FITTING CORRODED. REMOVED (2) LATCHES. REMOVED CORROSION IAW DC8 SRM 51-1-8. AREA WITHIN LIMTS IAW DC8 SRM 53-2-0. PRIMED LONGERON AND INSTALLED FITTINGS IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20040211000282004021100028NM 2004 2 11 USAA030320 120031229A5310 DOOR FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU50706 23701 PIT - FOUND DOOR FRAME CRACKED 1 INCH, LOWER AFT FORWARD SERVICE DOOR CORNERS. INSTALLED DOUBLER PER EA 77600. (M) 2L72 4F RTA16WE 20040217000462004021700046NM 2004 2 17 2004F00072 120030930A5230MS20001167200 HINGE BOEING727 727222 1384073NM CARGO DOOR CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 SW077640U 19913 AT B-CHECK, FOUND AFT SECTION OF MAIN CARGO DOOR HINGE CRACKED AT AFT END AIRFRAME SIDE. REMOVED CRACKED SECTION OF MAIN CARGO DOOR HINGE. FABRICATE, TREAT, PRIME AND INSTALLED NEW HINGE SEGMENT. MAIN CARGO DOOR OPERATIONAL CHECKED NORMAL. (M) 2L73 4F A3WE 20031212001132003121200113NM 2003 12 12 SWAA032447 120031105A53136551698 STRINGER BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 26R CORRODED BETWEEN BS 747 AND BS 760. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20031217000722003121700072WP 2003 12 17 DHL2003807528 120031022A571437552222 FITTING DOUG DC8 DC873F 302199FWP CENTER WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MAIN CARGO COMPT CENTER WING FITTING CRACKED 1.500 AT STA 760.000 LBL-24. REMOVED AND REPLACED CRACKED FITTING ON MAIN CARGO COMPT CENTER WING, STA 760.000, LBL-24 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040316000272004031600027WP 2004 3 16 ASAA0380287 120030404A5710993758814 SHEAR TIE DOUG DC9 DC982 3022082WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2, AND 30-5. (M) 2L72 4F A6WE 20030814001192003081400119NM 2003 8 14 UPS03M40945 120030603A5347S49291477075T6 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 INSPECTION TYPE:C CORROSION ON SEAT TRACK AT STA 755-840 RBL 27.5. CORROSION ON TRACK AT STA 755-840 RBL 27.5 BLEND OUT AS PER SRM 51-21-0 1V2R33 ORI THK:0.090 INCH & REMOVED 0.060 INCH FOUND EXCEEDED LIMIT AS PER SRM 53-70-00V1R33. SEAT TRACK RBL 27.5 STA 869 TRIMMED & SMOOTHED AS PER SRM 53-70-00V1R33. NEW SEAT TRACK FROM STA 745-869 INSTALLED AS PER SRM 51-31-01V1R3. 2L73 4F RTA22WE 20030818000122003081800012NE 2003 8 18 HEEA088421 120030722A7600NYLC504482 MOTOR SKRSKYS76 S76A 8143006NE BEEP SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 TORQUE SPLIT, DEAD SPOT BEEPING FROM 60 TO 90 PERCENT. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030819002122003081900212NM 2003 8 19 UPS03241009 120030710A5320 ANGLE BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, SURFACE CORROSION ON ANGLE IN LT MLG WHEEL WELL AT BS 935 FWD OF 940 FITTING AT STR 19. REMOVED ANGLE IAW SRM 51-30-02. ANGLE FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01. FABRICATED ANGLE IAW DRAWING 65-22419 & SRM 51-20-01 & 51-40-3. INSTALLED ANGLE IAW 51-30-03. 2L73 4F A3WE 20030820000412003082000041NM 2003 8 20 03FDEA01140 120030723A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT I/B FLAP (FLAP SIDE) - O/B HINGE I/B PIVOT HOLE AND LUG INNER SURFACE CORRODED. RT I/B FLAP (FLAP SIDE)- O/B HINGE I/B PIVOT HOLE AND LUG INNER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69257 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBD FLAP HINGE BRACKET ASSY REPAIR. 2L73 4F RTA22WE 20030820000812003082000081NM 2003 8 20 03FDEA01266 120030719A5310 FLANGE BOEING727 727100 1384036NM E/E BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25103FE 19199 E AND E COMPT STA 420 STR 26R CRACKED AT LWR FLANGE AND BENT AT STA 422. REPAIRED CRACKED STRINGER IAW BOEING 727-100 SRM 53-10-3 2L73 4F RTA3WE 20030820001162003082000116NM 2003 8 20 UPS03M40989 120030722A3350 BATTERY DOUG MD11 MD11F 3023600NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP EMERGENCY LIGHT BATTERY LOW TEST FAIL. FOUND EMERGENCY PWR SELECTOR IN OFF SELECTED ARM OPS CK NORMAL IAW 33/51/01 & FIM 33/51/02. 2L73 4F RTA22WE 20030401000252003040100025EA 2003 4 1 ASOA03045 120030206A3350BM10006002 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11832AS 7243 DURING A GROUND INSPECTION IN DFW, THE LEFT FORWARD UPPER EXTERIOR EMRGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD UPPER EXTERIOR EMERGENCY LIGHT. OPERTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030821001522003082100152WP 2003 8 21 03FDEA01235 120030810A3411 STATIC PORT DOUG DC10 DC1030 3023501WP PITOT/STATIC SYSSEPARATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 NAVIGATION - ENLARGED GAP BETWEEN ALT STATIC PORT AND FUSE SKIN BY 3A 39017C RPT BY3A 39017 FACT 09AUG03 6 3A20 BFM RD COMPLIED WITH EA 8-3411-72250 NAVIGATION - ENLARGED GAP BETWEEN ALT STATIC PORT AND FUSE SKIN 40 MAE 0D 0 ARII. 2L73 4F A22WE 20030404001572003040400157NM 2003 4 4 SWAA030544 120030308A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED (9 EA) IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030416000022003041600002EA 2003 4 16 SWIA200311663 120030101A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07430SW 7523 FLOOR EMERGENCY LIGHTING STRIPS 5, 6, 7 & 8 ARE DIM. FOUND MOISTURE UNDER COVER STRIP. DRIED OUT MOISTURE. OPS CHECK GOOD PER 33-51-01. 2L72 4F RTA21EA 20030417000542003041700054SO 2003 4 17 LR7A03005 120030124A53303629591R SKIN LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 489 4698 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB0502 FOUND RT FUSELAGE FS 737 TO 770 SKIN PANEL CREASED AND OIL CANNING WL 170 - 220. REPLACED SKIN PANEL FS 737 TO 770 IAW DWG 362959 AND 372496. NR 0026. 2H74 4T A1SO 20030417001092003041700109NM 2003 4 17 PCAA0302037 120030207A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT LOOSE A PCAAO OTHER O OTHER NRNOT REPORTED 1 EA13842EX 341 PIT-FLIGHT 3716 CREW REPORTED EMERGENCY LIGHTS FLICKERED ON AND OFF IN FLIGHT. MAINTENANCE FOUND A WIRE STICKING UP FROM LIGHT STRIP. WIRE WAS RESECURED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030423000292003042300029NM 2003 4 23 MEX2003128 120030409A32404062575 TRANSDUCER DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE BRAKES FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23168PL1046010460 53174 AIRCRAFT REJECTED TAKEOFF, MAIN WHEEL LIGHT WAS ON. AT PLATFORM WHEELS WERE CHECKED FOR FREE DRAFT AND THE FOUR ANTI-ICE TRANSDUCER WERE CHECKED, DETECTING ONE PIN BENT OF TRANSDUCER WHEEL NUMBER 2 PIN WAS STRAIGHTEN. DURING OVERNIGHT SERVICE TRANSDUCER NUMBERS 2 AND 4 WERE REPLACED IAW MM AND WIRING CONNECTOR OF TRANSDUCER NR 4 WAS REPAIRED IAW MM, MAIN GEAR BRAKE NR 2 WAS REPLACED AND ANTI SKID WAS TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030925000252003092500025NM 2003 9 25 AALA20030854 120030814A3350 LIGHT BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21688AA 25730 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT SEAT 16D BROKEN. REPLACED EMERGENCY EXIT SEAT LIGHT AT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925000692003092500069WP 2003 9 25 AALA20030900 120030822A2131 CONTROLLER DOUG DC9 DC982 3022082WP CABIN PRESSURE MALFUNCTIONED A AALAO OTHER O OTHER NRNOT REPORTED 1 SW2170524 49916 EN ROUTE MIA-LGA, AT 29,000 FT PACK FLOW GAUGES WENT TO ZERO AND AIRCRAFT LOST ALL PRESSURIZATION. ALL MASK DEPLOYED. AIRCRAFT REMOVED FROM SERVICE AND FERRIED TO DFW. INSPECTED DUCTS IN TAIL COMPARTMENT AND WHEEL WELL. PERFORMED BITE OF CONTROLLERS. UNABLE TO DUPLICATE PROBLEM ON GROUND. REPLACED NR 1 CONTROLLRE AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030908002042003090800204EA 2003 9 8 SWIA200312290 120030719A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-51 2L72 4F RTA21EA 20030909001342003090900134CE 2003 9 9 S2YA03021 120030606A5270 SWITCH BEECH 1900 1900D 1154162CE PAX DOOR OUT OF ADJUST A S2YAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL13145SK UE145 DURING FLIGHT 1070, THE CABIN DOOR ANNUNCIATOR ILLUMINATED AT 2 POUNDS OF DIFFERENTIAL PRESSURE. THE CREW DID AN AIR TURNBACK. THE SYSTEM WAS PUT ON MEL AND THE AIRCRAFT RETURNED TO SERVICE. ON 06/09 MECHANIC CLEARED THE MEL BY ADJUSTING THE LOWER SILL SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. 2L72 4T RTA24CE 20031003000122003100300012NM 2003 10 3 AALA20030922 120030830A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 EMERGENCY LIGHTS INOPERATIVE ON SEATS 31B AND 32B. SECURED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031023000462003102300046EU 2003 10 23 AWXA200301094 120030914A5321D5367175404400 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK FOUND FLOOR PANEL 261NF DELAMINATED. MAINTENANCE REMOVED FLOOR PANEL 261NF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG D536-71754; INSTALLED NEW PANEL IAW A320 SRM 53-02-00, PG. 231. 2L72 4F RTA28NM 20031027000412003102700041NM 2003 10 27 CALA0300560 120030926A335020131A BATTERY PACK BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717309 23360 THE INTERIOR EMERGENCY AISLE LIGHTS AT ROWS 14R, 16L, 19L, 21R, AND 23L WERE FOUND INOPERATIVE. REPLACED BATTERY PACKS AT M1135 AND M1136 POWER SUPPLIES IAW MM 33-51-51, PARAGRAPH 3, PAGES 203-206. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA16WE E2GL 20031027001252003102700125NM 2003 10 27 QXEA200301186 120030924A5220 ESCAPE HATCH DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 ESCAPE HATCH SKIN IS SCRATCHED TO METAL ONE INCH LONG. REPAIRED IAW DHC-8 SRM 52-00-16, 51-00-06 AND 51-20-26. 2H72 4T4 TRTA13NM E20NE 20031028001582003102800158NM 2003 10 28 ASAA0340093 120030228A531065C25228 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION AT BASE OF THE SHEAR TIE AT BS 727B LBL 2 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000162003102900016EU 2003 10 29 ASOA03473 120031002A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11640AS 405 DURING A GROUND INSEPCTION IN MGM, THE EXTERNAL EMERGENCY LIGHTS BY THE PASSENGER AND SERVICE DOORS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERNAL EMERGENCY LIGHT LAMPS BY THE PASSENGER AND SERVICE DOORS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031119000832003111900083NM 2003 11 19 QXEA200301266 120031012A5210 DOOR DHAV DHC8 DHC8202 2809007NM ZONE 800 OUT OF ADJUST A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09369PH 513 ON FLIGHT 2034 MAIN CABIN DOOR OUTSIDE HANDLE SLIGHTLY RECESSED BEHIND TAB, DIFFICULT TO OPEN. OPENS FINE FROM INSIDE. SHIMMED MAIN CABIN DOOR HANDLE BUMPER STOP. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031121000112003112100011NM 2003 11 21 SWAA032461 120031106A53146545866 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND CORROSION ON KEEL BEAM INBD FLANGE AT B 500D + 18. REPAIRED PER EO. 2L72 4F RTA16WE 20040204001812004020400181NM 2004 2 4 PCAA0311133 120031030A3350 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EMERGENCY LIGHT DISCONNECTED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13812EX 312 DURING ROUTINE MAINTENANCE CHECK IT WAS FOUND THAT ROW 8 FLOOR PATH EMERGENCY LIGHT WAS INOP. MAINTENANCE FOUND WIRES DISCONNECTED AT ASSOCIATED SPLICE. A NEW SPLICE WAS USED AND SYSTEM OPERATIONAL CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20030910000092003091000009NE 2003 9 10 BAQA088155 220030721A732045033501 CONTROL BOX UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE NR 1 ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME840 132 ELECTRICAL MASTER BOX WILL NOT LET NR 1 ENGINE START. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H88EU E19EU 20031031000132003103100013SO 2003 10 31 HYI2003F00017 220030911A7320642702A10 FMU CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO RT ENGINE FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE0169SC 1 402C0041 828546 RT ENGINE FAILED TO SHUT OFF IN IDLE CUT OFF. REMOVED AND REPLACED FUEL METERING UNIT AND RELEASED AIRCRAFT BACK TO SERVICE. 1L72 3O3 O A7CE E8CE 20030425000492003042500049NM 2003 4 25 UPS03440398 120030302A534065B820113 BRACKET BOEING747 747200 1384847NM LT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, LT MLG WW - BS 1241 LBL 1 TO 8 HORIZONTAL BRACKET FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT. BRACKET REPLACED AS PER SRM 51-10-01 PAGE 8 TOTALLY 2 EA (P/N: 65B82011-3 AND 69B11570-1). 2L74 4F RTA20WE 20030429002222003042900222NM 2003 4 29 SWAA030806 120030406A53136551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20030501002072003050100207EA 2003 5 1 ASOA03118 120030319A4930M259882904 O-RING CNDAIRCL600 CL6002B19 1900309EA APU FUEL SYS LEAKING A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11915EV 7754 FLT 4772 - DURING CRUISE FROM MOB-DFW, AT APPROXIMATELY 31,000 FT, A STRONG FUEL ODOR OCCURRED IN THE COCKPIT. THE CREW INITIATED DESCENT OT 24,000 FEET AND SELECTED THE LEFT PACK OFF WHICH ELIMINATED THE FUEL ODOR. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED AN O-RING AT THE FUEL FLOW ELBOW ON THE AUXILIARY POWER UNIT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030505000862003050500086NM 2003 5 5 373PA0013 120030415A3350 LIGHT BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 EMERGENCY LIGHT INOP RT AFT OF WING TO BODY FAIRING. RELAMPED EMERGENCY LIGHT, OPS CHECK OK. 2L72 4F RTA16WE 20030506001982003050600198 2003 5 6 ASAA0380265 420030317A2565D29984103 SLIDE DOUG DC9 DC983 3022083WP PAX DOOR FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS6240 53019 OAK - FOUND DURING 15K CHECK, AFT PASSENGER DOOR EMERGENCY SLIDE FAILED LIGHT CHECK. REPLACED EMERGENCY SLIDE PER TASK CARD 24655000. (M) 2L72 4F RTA6WE 20030506002052003050600205WP 2003 5 6 ASAA0380253 120030307A534799578551 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FIRST OFFICER UPPER SEAT TRACKS WORN. REPLACED SEAT TRACKS PER SRM. (M) 2L72 4F A6WE 20030508001152003050800115NM 2003 5 8 HOC2003F00013 120030429A5315 FLOORBEAM BOEING727 727231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON LOWER FLANGE. COMMON TO FLOORBEAM STRAP AND INTERCOSTAL. STA 1130, LBL24. 2L73 4F4 F A3WE E2EA 20030509000862003050900086SW 2003 5 9 FTU2003F00009 120030424A3213AN386428 PIN GULSTM690TP 695A 7630519SW GARRTTTPE331TPE331* 01514WP MGL STRUT SCORED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE057812 96089 DURING A NORMAL PERIODIC INSPECTION IT WAS DISCOVERED THAT THE TAPERED PINS WHICH RETAIN THE MLG HOUSING SUPPORT PINS HAD INCORRECT HARDWARE (PLAIN WASHERS UNDER THE NUT, INSTEAD OF SPECIAL AN975-5 WASHERS) SECURING THE TAPERED PINS IN PLACE. FURTHER INVESTIGATION REVEALED THE TAPERED PINS IN PLACE. FURTHER INVESTIGATION REVEALED THE TAPERED PIN SIDES WERE DAMAGED FROM IMPROPER INSTALLATION AND THE TAPERED HOLES WERE FOUND NOT TO BE REAMED DEEP ENOUGH FOR CORRECT INSTALLATION. NO OTHER DAMAGE WAS FOUND. NEW PINS WERE INSTALLED AND HOLES REAMED TO THE CORRECT DEPTH AND PINS SECURED USING CORRECT HARDWARE. 1H72 4T3 T 2A4 E2WE 20030514000292003051400029EU 2003 5 14 AALA20030258 120030301A3397 WIRE FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211411G 11369 DFW - DURING OVERNIGHT MAINTENANCE, NR 1 OVERHEAD 6 VOLT CENTER AISLE EMERGENCY SPOT LIGHTING INOPERATIVE. REPAIRED NR 1 OVERHEAD 6 VOLT CENTER AISLE EMERGENCY SPOT LIGHTING WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030513002012003051300201EA 2003 5 13 QXEA0300478 120030404A5340 FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 AT FS 1126 STRINGER 11 RIGHT SIDE AT FITTING MM670-36545-002 EXISTING HOLES NR 5AD NEEDS STEPPED UP TO NR 6AD. REPAIRED IAW HORIZON AIR EA 601R-53-3912 AND EA R-53-84. 2L72 4F RTA21EA 20030605000872003060500087EU 2003 6 5 GXP2003F00000 120030505A3260 UPLOCK SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE MLG DIRTY E GXPAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL23174GA 27 AIRCRAFT RETURNED TO AIRPORT, AFTER TAKEOFF LANDING GEAR DOOR WILL NOT CLOSE AFTER GEARS WERE RETRACTED. CLEANED ALL LANDING GEAR UPLOCK SWITCHES, 3G SWITCH AND RESEATED 6G RELAY. OPS CHECKED LANDING GEAR WITH HYD MULE. NO DEFECTS NOTED OPS CHECKED GOOD. 2L72 4F4 F A7EU E7EA 20030605001372003060500137CE 2003 6 5 BLI2003F00002 120030331A3246 WHEEL CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO MLG CRACKED E BLIAO OTHER O OTHER NRNOT REPORTED 1 GL236387X 402B1350 DURING INSPECTION, FOUND MAIN LANDING GEAR WHEEL CRACKED. REPLACED WHEEL ASSEMBLY WITH NEW. 1L72 3O3 O A7CE E8CE 20030521001032003052100103WP 2003 5 21 DHL2003801048 120030414A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING ELONGATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 410.250 AND XOLDI 6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED DOUBLER INNER PART IAW SRM 51-1-8B. PERFORMED NEW HOLES (COUNTERSINK) ON DOUBLER WITH PROPER MEASURE IAW SRM 51-1-22 PG 1. INSTALLED DOUBLER ON CTR L/E UPPER SKIN WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030609001952003060900195EA 2003 6 9 CA030521001 220030515A7414M3100 RIVET SLICK 4372 ZLIN 242 Z242L 9970204EU LYC O360 AEIO360A1B6 41514EA IMPULSE COUPLINGLOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 100 HR INSPECTION, AND DUE TO PREVIOUS IMPULSE COUPLING FAILURES, THE LT MAGNETO IS REMOVED AND THE IMPULSE COUPLING IS INSPECTED EVERY 100 HOURS. THIS IMPULSE COUPLING HAD A LOOSE RIVET ON ONE OF THE LATCHING PAWLS AND THE POSSIBILITY OF THE RIVET SHEARING AND THE PAWL COMING OFF WAS VERY HARD. THE PAWL CAME OFF THE ENGINE WOULD HAVE SUSTAINED SIGNIFICANT DAMAGE. THE INSPECTIONS ON THE IMPULSE COUPLINGS WILL CONTINUE. 1L71 3O3 O0 A76EU 1E10 20030617001252003061700125GL 2003 6 17 HEEA087463 220030612A74216899084 IGNITER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 IGNITER WORN. REPLACED IGNITER. 1G71 3U3 UO H2SW E1GL 20030515001882003051500188NM 2003 5 15 AWXA200300513 120030414A5313655162823 STRINGER BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH AREA OF EXFOLIATION CORROSION WAS FOUND ON STRINGER 25 RT, AT BS 978 WATER TANK COMPARTMENT. MAINTENANCE CUT OUT CORROSION ON STRINGER 25 RT AT BS 978; FABRICATED A REPAIR SPLICE (HAT CHANNEL); INSTALLED REPAIR PART IAW B737-200 SRM 53-10-9 FIG 1. 2L72 4F RTA16WE 20030527001032003052700103NM 2003 5 27 C7WA200200040 120030304A5210507945114 PAN BOEING727 727225 1384077NM L1 DOOR CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO178887Z 21856 L1 DOOR VERY HARD TO CLOSE. DURING INSPECTION OF DOOR FOUND CRACKS IN DOOR PAN AROND UPPER AND LOWER TORQUE TUBES. REMOVED AND REPLACED FORWARD ENTRANCE DOOR. (M) 2L73 4F A3WE 20030523001132003052300113NM 2003 5 23 2003UALA00421 120030513A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29333UA 24228 EXTERNAL FUSELAGE SKIN DAMAGED AT STA 1050 ALONG CENTERLINE 36 INCHES FWD OF APU ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND SKIN DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030619000072003061900007SW 2003 6 19 HEEA087178 120030609A6320206040270101 SUPPORT BELL 206 206L3 1182108SW GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW036251X 51552 AFT GEARBOX SUPPORT LEAKING. REPAIRED. 1G71 3U H2SW 20030620000912003062000091NM 2003 6 20 USAA030063 120030516A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US46845 23232 FOUND SKIN CRACKED TWO PLACES .180 INCH, FORWARD SERVICE DOOR AFT FRAME WL 240 AND WL 250 CUTOUTS. ROUTED CRACKS OUT OF CUTOUT AT WL 250 AND 240 PER EA 74896. (M) 2L72 4F RTA16WE 20030624000622003062400062NM 2003 6 24 CALA0300305 120030610A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND AFT BAGGAGE BIN DOOR SKIN DENTED AT CENTER AREA 38 INCHES FROM BOTTOM AND FORWARD 22 INCHES FROM AFT WITH A DEPTH OF 0.128 INCH, 3.5 INCH WIDTH, AND 6 INCHES IN LENGTH. THE DENTED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030702000412003070200041WP 2003 7 2 GTIA030388 120030514A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND AFT ACCY COMPARTMENT CANTED FRAME CRACKED AT FS 1485 18 INCHES RBL. FABRICATED 7 DOUBLER AND 25 DOUBLER FRAME. INSTALLED 7 DOUBLER AND 25 FRAME. (M) 2L72 4F A6WE 20030718000412003071800041NM 2003 7 18 USAASB03089 120030622A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19529AU 24411 CLT - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND ERPLACED TEH BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030707001912003070700191WP 2003 7 7 UPS03840823 120030521A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, STATION 1781 LONG. 17R AND END FITTING ARE CRACKED, REMOVED LONGERON AND ENDFITTING, FABRICATED LONGERON AND REPLACED END FITTING IAW DWG. 4772397 AND 5649327,AND SRM. 51-1-21,51-1-20D. 2L74 4F RT4A25 20030709000972003070900097NM 2003 7 9 C1HA200397012 120030606A2900 HYDRAULIC SYSTEM BOEING727 727270 138408PNM A-SYSTEM LEAKING A C1HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15697CA 23052 AFTER 1 HR IN FLIGHT SYSTEM A-HYDRAULIC QUANTITY STARTED TO DECREASE, QUANTITY FELL TO 2.3 GALLONS. 2L73 4F RTA3WE 20030709001142003070900114SO 2003 7 9 C2XA03SH185 120030613A531313500400019 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK STRINGER 19R WAS FOUND GOUGED ON THE EXTERIOR BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709000262003070900026WP 2003 7 9 AALA20030556 120030512A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21420AA 49332 DURING OVERNIGHT MAINTENANCE, TAILCONE SIDEWALL EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE IN TAILCONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030714001042003071400104EA 2003 7 14 HNAA030030 120030623A612078249047 CONTROL UNIT DHAV DHC8 DHC8311 1386006EA PROPELLER LEAKING A HNAAA UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 EA07804SA144678314 375 DURING FLIGHT THE F/A REPORTED A FLUID LEAK FROM THE NR 1 NACELLE. AIRCRAFT RETURNED TO THE DEPARTURE FIELD. CREW REPORTED THERE WAS NO LOSS OF OIL PRESSURE OR ASSOCIATED CAUTION LIGHTS. FOUND NR 1 PROP CONTROL UNIT LEAKING. REPLACED PCU. 2H72 4T RTA13NM 20030717000402003071700040SW 2003 7 17 HEEA088015 120030620A7120407064105102 LEG ASSY BELL 407 407 1182206SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 ENGINE MOUNT LEG ASSY HAS A HOLE WALLED OUT OF LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030108000132003010800013WP 2003 1 8 MWEA03006 120030108A531359360531 SPLICE DOUG DC9 DC981 3022081WP STA 593 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 LONGERON 30 AT STATION 593 IS CORRODED AROUND FASTENER HOLES THAT GO THROUGH THE SKIN. -- REMOVED CORROSION AND INSTALLED SPLICE. 2L72 4F A6WE 20031103000992003110300099EU 2003 11 3 AWXA200301123 120030930A3350321452 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 263 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28631AW44220 077 PHX - EEL - DURING INSPECTION, OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED, CODES COM AFT LT AND INT LOAD AFT LT WERE REPORTED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031106002092003110600209 2003 11 6 GTIA030715 420030927A2565 LANYARD DOUG MD80 MD83 3023681NM L1 SLIDE PACK DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 LGA - FLT 381 - L1 DOOR SLIDE PACK LANYARD IS NOT ATTACHED. RE-INSTALLED L1 DOOR SLIDE PACK LANYARD. NO DEFECTS NOTED. (M) 2L72 4F RT 20031107001222003110700122SO 2003 11 7 SIMA200327907 120030930A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 ABI - DURING AN MBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. REMOVED CORROSION BY CREATING A CUTOUT IN THE FLANGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 22, 53-22-10, FIG 201 SHEET 2 AND CPM 51-21-06. (M) 2L72 4F RTT00011AT 20030730000482003073000048WP 2003 7 30 ABXA030251 120030211A5200 MOUNT DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 LOWER LATCH HOOK MOUNT HOLE AT STA 256.5 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR. 2L74 4F 4A25 20030911002352003091100235WP 2003 9 11 DHL2003604562 120030527A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 VERTICAL STAB L/E FORMER INNER SECTION CRACKED 0.500 AT STA ZFS 104.750 LT SIDE. STOP DRILLED CRACK AT ZFS 104.750 AND FABRICATED REINFORCEMENT IAW SRM 55-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND REINFORCEMENT IAW SRM 51-1-8B. INSTALLED REINFORCEMENT IAW SRM 51-1-20D PAGE 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000712003091200071WP 2003 9 12 DHL2003604792 120030430A5347S2772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT NR 4 TRACK LUGS WORN AT SEVERAL SPOTS STA 950.000-610.000. REMOVED NR 4 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED SPLICES IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040112000642004011200064NM 2004 1 12 TSAA0253260 120031218A53106546526 WINDOW FRAME BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INCH INSIDE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF MBS 10-79 TYPE III, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AI. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040109000042004010900004GL 2004 1 9 W592003F00001 320031021A6114B4776 BUSHING HARTZL BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO HARTZLHCC3Y PHCC3YF1 GL PROPELLER HUB SHIFTED B W59RK NONE O OTHER ININSP/MAINT 1 WP075599P2700 1360 EE17720 CE1344 825760R EE1772A AFTER TAKEOFF, THE PILOT DID NOT REDUCE RPM. DURING REMOVAL OF THE PROPELLER, THE REAR HUB BORE REPAIR BUSHING PN B-4776 WAS FOUND DISLOCATED FROM HUB IN THE CRANKSHAFT. THE LOSS OF THIS BUSHING CAUSED THE PROP HUB TO BECOME FILLED WITH OIL AND RESULTED IN AN INABILITY TO CHANGE PITCH DUE TO A HYDRAULIC LOCK. THE LOCKTITE ADHESIVE USED TO BOND THE BUSHING APPEARS TO HAVE FAILED AND THERE IS NO PROVISION FOR A MECHANICAL LOCKING RING. THIS BUSHING IS REQUIRED TO BE REMOVED AND REPLACED AT OVERHAUL, HOWEVER DUE TO THE INSTALLATION IT IS DIFFICULT TO DETERMINE IT BUSHING IS INSTALLED. RECOMMEND HUB BE STAMPED IN SOME MANNER TO INDICATE THIS REPAIR HAS BEEN PERFORMED.(K) 1L71 3O3 O 3A15 E5CE 5 CP25EA 20031120000032003112000003SO 2003 11 20 SWIA200312488 120030904A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07218SW 120287 FRAME 13 ON LEFT SIDE FLOOR PROP DOUBLER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT FLOOR PROP SUPPORT CLIP AT FRAME 13 PER SRM 51-40-02. 2L72 4T RTA31SO 20031121000632003112100063NM 2003 11 21 03FDEA01921 120031026A5753ARC2518502 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD LUG OUTBOARD SURFACE FOUND CORRODED. CORROSION AT RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT POINT OUTBOARD LUG SURFACE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73338. WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - INBOARD FLAP OUTBOARD HINGE STRAP FABRICATION DIFFERENCES. 2L73 4F RTA22WE 20040113001012004011300101EU 2004 1 13 BAQA091135 120031124A28201176417203 FUEL TANK BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03955ME6563 7243 FUEL TANK LEAKING. REPLACED WITH SERVICEABLE UNIT. 11/25/03 1G72 3U3 U H13EU E5NE 20040113001332004011300133NM 2004 1 13 03FDEA02254 120031226A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP O/B FWD HINGE SIDE SUPPORT MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75210. WINGS, TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040113002062004011300206SO 2004 1 13 C2XA03SH518 120031230A532014524131009 BRACKET EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 DURING C CHECK THE MAIN DOOR THRESHOLD FORWARD AND AFT U-BRACKETS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BRACKETS IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040113002312004011300231NM 2004 1 13 QXEA200301583 120031227A2910 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE HYD SYSTEM CONTAMINATED A QXEAO OTHER JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 NM09357PH 504 GEAR SELECTED UP, INDICATED RETRACTED BUT NOSE GEAR LIGHT SHOWED GEAR DOORS OPEN. MODERATE NOISE AND VIBRATION FELT. MASTER CAUTION NR 2 ENGINE HYDRAULIC PUMP ILLUMINATED SHORTLY THERE AFTER. NR 2 HYDRAULIC PUMP SHOWED ZERO PSI AFTER 5 MINUTES, NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT EXTINGUISHED AND PRESSURE INDICATED NORMAL. UPON SELECTING GEAR DOWN, GEAR EXTENDED NORMALLY AND GEAR DOOR LIGHT INDICATED NORMAL. BLED NR 2 HYDRAULIC SYSTEM AND RUDDER ACTUATORS AND NR 2 RESERVOIR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040114001692004011400169 2004 1 14 MALA030554 420031215A3418861CAR VANE SAAB SF340 340B 7860101EU STALL WARNING MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15430XJ 340B430 DURING FLIGHT, RT STALL FAIL LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REPLACED THE AOA VANE PN 861CAR SN OFF 01177 SN ON 01105,IAW SF3 AMM 27-35-05 OPS CHECKS GOOD STALL WARNING /IDENT SYS IAW SF3AMM 27-35-00-5 OPS CHECKS GOOD. 2L72 4T RTA52EU 20040115000192004011500019NM 2004 1 15 03FDEA02034 120031203A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 1 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040115000302004011500030NE 2004 1 15 SW07200300009 220030822A72504120T01P02 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE DAMAGED G FDKAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW07506MJ1206 10073 GEE965258 MAINTENANCE PERSONNEL PERFORMED A BOROSCOPE AND FOUND THE 2ND STAGE HIGH PRESSURE TURBINE BLADES DAMAGED. 2L72 4F4 FRTA21EA EOOO63EN 20031216000952003121600095SO 2003 12 16 C2XA03SH490 120031211A532014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031215001922003121500192EU 2003 12 15 USAA030265 120031031A5320D2557206222800 FITTING AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND TIE DOWN LUG WITH 1 INCH IN DIAMETER CORROSION, FRAME 25, RBL 24. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-72-11. CORROSION LEVEL 2, TASK NR JA-131-53500. (M) 2L72 4F RTA28NM 20031219001232003121900123NM 2003 12 19 03FDEA02068 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORRODED. OUTBOARD FLAP INBD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031223001782003122300178EA 2003 12 23 A6WA200340185 120031201A5710 BUSHING CNDAIRCL600 CL6002B19 1900309EA WING LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31423AW 7636 FOUND LT MLG AFT WING SPAR BUSHING MIGRATED .052 INCH. REMOVED MIGRATED BUSHING ON LEFT MLG, AND INSTALLED FIRST OVERSIZE BUSHING, P/N 601R-57-21-003-21 IAW REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20031229001202003122900120NM 2003 12 29 SWAA032726 120031214A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D-CHECK, FOUND CORROSION BS 294, RBL 33 TO 53, FLOORBEAM. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031231001102003123100110NM 2003 12 31 TSAA0351029 120030115A53126554893 PRESSURE PANEL BOEING737 7372T4 1384492NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 FABRICATED NEW PRESSURE WEB REPAIR DOUBLER. ALODINED AND PRIMED ALL BARE ALUMINUM. FAY SURFACE SEAL INSTALLED REPAIR DOUBLER WITH BMS 5-95 AND FASTENERS IDENTIFIED. APPLIED CORROSION INHIBITING COMPOUND TO THE INTERNAL SURFACES. REPAIR COMPLETED IAW ECO 3328, PART 1 AND V. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031007001262003100700126WP 2003 10 7 MWEA030374 120030916A533059102285 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 LEFT. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER. 2L72 4F A6WE 20031014001292003101400129 2003 10 14 SWAA032163 420030926A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29400WN 27891 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040108001362004010800136EU 2004 1 8 KBM2003F00068 120031019A3213350A41107620 LEAF SPRING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE MLG DEFECTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 LT AND RT LANDING GEAR SPRING BLADES DEFLECT LESS THAN 85MM. REPLACED WITH NEW LANDING GEAR SPRING BLADES.(K) 1G71 3U3 UNCH9EU E19EU 20040108001562004010800156NE 2004 1 8 Z1R2003F00006 120031028A1430SS5305L4G08 SCREW SKRSKYS76 S76C 8143008NE BLADE TIP CAP CRACKED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF714 760523 ONE SCREW CRACKED NR 1 BOTTOM POSITION LEADING EDGES. 1G72 3U NCH1NE 20031124001492003112400149NM 2003 11 24 CALA0300603 120031018A532065479573 WEB BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 AFT CARGO PIT CORROSION AROUND FASTENERS AT DOOR THRESHOLD WEB. REMOVED AND REPLACED WEB IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031202000632003120200063NM 2003 12 2 USAABB03193 120031017A33509221009 BATTERY BOEING757 757225 1384959NM EXIT SIGN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU 22198 MIA - FOUND R1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031124001602003112400160NM 2003 11 24 QXEA200301284 120031008A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-LT INBOARD TRACK NR 5 BOTTOM OF TRACK CHAFED FROM X445 TO X455 AND X507 TO X515. REPAIRED IAW RD8-53-1339. 2H72 4T4 TRTA13NM E20NE 20040311000292004031100029NM 2004 3 11 ASAA0310133 120030310A53306545800742 SKIN PANEL BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SKIN PANEL AT BS 328, RIGHT BUTTOCK LINE 65 CRACKED. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR PER EA. (M) 2L72 4F A16WE 20040122000972004012200097EU 2004 1 22 ASOA03626 120031204A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT 73WL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040122001412004012200141WP 2004 1 22 800LL112403 220031123A72007315R1H ENGINE RAYTHNDH125 HAWKER800 7450004CE GARRTTTFE731TFE7315R 01518WP NR 1 VIBRATION A AOQAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 EA11800LL7112 3764 258079 VIBRATION FELT DURING FLT FROM REAR OF AC. ALL ENG INDICATIONS NORMAL. PASSING AC REPORTED WITNESSING SPARKS FROM REAR OF RT SIDE OF AC. UPON INITIAL INSP, METAL DEBRIS WAS NOTED IN LT ENGINE TAIL PIPE AREA. ENG MFG AND REPAIR FACILITY WERE CONTACTED FOR FURTHER INSP. BOROSCOPE INSPECTION REVEALED POSSIBLE 4TH STAGE LP COMPRESSOR ROTOR OR STATOR FAILURE. ENGINE REMOVED FOR DISASSEMBLY, INSP AND REPAIR. CREW BRIEFED ON A POSSIBLE SINGLE ENG APPROACH AND REQUESTED AIRPORT FIRE RESCUE. APPROX 10 NM OUT, VIBRATION WAS FELT ALTHOUGH ALL ENG INDICATIONS CONTINUED TO REMAIN NORMAL. AC LANDED UNDER ALL ENGINE POWER, NO FURTHER VIBRATIONS DURING LANDING, ROLL OUT OR TAXI. (EA11200402104) 2L72 4F4 FRTA3EU E6WE 20031209002152003120900215NE 2003 12 9 SWIA200312565 220031030A7200PW118B ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RIGHT MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07188SW8158 8158 120039 IN FLIGHT, RT OIL PRESSURE DROPPED TO 40 PSID. ON 20 MILE FINAL OIL PRESSURE WENT TO 0. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY PER EMB 120 MM 71-00-00 AND RII 72-301. RAN ENGINE. OPS AND LEAKS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20031009000512003100900051NM 2003 10 9 03FDEA01643 120030926A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON FUSELAGE INNER SKIN BETWEEN STR S26-R AND S27-R, STA 720E TO 720F, UNDER STRINGER S27-R. REPAIRED IAW EA 7-5330-55027. 2L73 4F RTA3WE 20030918000802003091800080NE 2003 9 18 A6WA200340114 220030728A7200 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NR 1 ENG VIBRA FAILED A O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 GL31422AW 7341 DURING TAKE-OFF POWER APPLICATION RECEIVED VIBE INDICATION NR 1 ENGINE AT 88.1 PERCENT N1 IN PROGRESS. REPLACED VIBRATION TRANSDUCER WIRE HARNESS ON LEFT ENGINE, OPS CHECK GOOD. RAN LT ENGINE TO 90 PERCENT N1 NO N2 VIBRATION INDICATION NOTED. (M) 2L72 4F4 FRTA21EA E15NE 20030915000372003091500037EU 2003 9 15 BAQA089105 120030911A240045033500 MASTER BOX UROCOPEC135 EC135T1 5620026EU MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME 132 FAULT LED'S 2-1-F. GENERATOR WILL NOT COME ONLINE. VARIOUS BUSSES DROP OFFLINE. TEST WAS DONE USING THE BUILT IN TEST BUTTON ON THE BOX. IT DID NOT PASS AND WAS IMMEDIATELY REMOVED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030923001252003092300125WP 2003 9 23 DHL2003604756 120030724A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 TWO INTERIM REPAIRS ON LT AFT LWR CORNER OF MAIN CARGO DOOR STA 270.000 BETWEEN L-20L AND L-22L. REMOVED FASTENERS AND INTERIM REPAIR. TRIMMED OUT DAMAGED AREA IAW EODHL-030584 ED-3486. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED (1) DOUBLER (7075-T6 AL0.080) AND (2) FILLERS (7075-T6 AL0.071) AND (2) FINGERS DOUBLERS (7075-T6 AL0.050) IAW EODHL-030584, ED-3486. CLEANED, TREATED AND PRIMED AREA AND DOUBLER AND FILLERS AND FINGER DOUBLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FINGER DOUBLERS AND FILLER WITH NEW FASTENERS IAW EODHL-030584, ED-3486, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040128001062004012800106 2004 1 28 SWIA200312700 420031212A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07581SW4518 4518 120349 RIGHT STALL STICK PULLER ACTIVATES WHEN A/C IS POWERED UP ON SAFETY CHECK. REMOVED AND REPLACED STALL WARNING COMPUTER WITH A SERVICEABLE UNIT IAW 27-00-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20040203000102004020300010WP 2004 2 3 ASAA0380583 120030910A278099375199 CONTROL CABLE DOUG DC9 DC983 3022083WP NR 4 SLAT WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01973AS 53449 OAK LINE CHECK, FOUND LT NR 4 SLAT CABLE FOUND TO BE WEARING INTO WING LEADING EDGE. REPLACED LEADING EDGE STRUCTURE IAW EA 5740-01361. (M) 2L72 4F RTA6WE 20040203000222004020300022WP 2004 2 3 ASAA0380595 120030923A53479936534139 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC - DURING 15K CHECK, FOUND SEAT TRACK IS CORRODED FROM FS 1098 TO 1193. REPLACED TRACK IAW SRM 51-30-1, 10-2, 10-4, AND 10-3. (M) 2L72 4F RTA6WE 20040206000472004020600047SO 2004 2 6 SIMA200335702 120031219A27503634501003 GEARBOX EMB 145 EMB145LR 3260212SO TE FLAPS BINDING A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21628AE 145124 LBB - FLT 3573 - ON APPROACH CREW RECEIVED FLAP FAIL MSG WITH ASSOCIATED FLAP JAM ON CMC. TROUBLESHOT SYSTEM AND FOUND THE LEFT OUTBAORD ANGLE DRIVE WHEN PUT IN A VERY COLD FREEZING STATE WOULD BIND UP. REPLACED ANGLE DRIVE GEAR BOX. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040210000262004021000026WP 2004 2 10 UPS03841602 120031014A53305758874 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, FUSELAGE DENTED FS 160, BETWEEN LONGERON 25-26 LT, BLEND OUT GOUGE IAW DC8 SRM 53-2-0, ORIG THICKNESS .071 IAW DC8 SRM 53 -4-1, REMOVED .020, REMAINING .051 FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, RMVD DAMAGED AREA IAW DC8 SRM 53-24-0 & 53-4-1, FABBED AND LOCATED HOLES IAW DC8 SRM 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20040213000352004021300035NE 2004 2 13 HNAA0300090 320031229A6110SFA13M1ROA BLADE DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF7 NE PROPELLER BURNED A HNAAH DEACTIVATE SYST/CIRCUITS M OVER TEMP CRCRUISE 1 EA07938HA374033593 152 900802 WITH PROP HEAT ON NR 2 PROP STARTED GLOWING ORANGE CEASED WITH PROP HEAT OFF REMOVED AND REPLACED NR 2 BLADE AND BLADE RETAINING RING OPS AND LEAK CK GOOD IAW W/C 61-10-07R. 2H72 4T RTA13NM 6 CP7NE 20031211001222003121100122NM 2003 12 11 AALA20031330 120031125A33500201720003 LIGHT DOUG MD80 MD83 3023681NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219413T 53188 DTW FRONT ENTRY EMERGENCY EXIT LIGHT UPPER LOCK BROKEN. REPLACED FRONT ENTRY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20030127002172003012700217SW 2003 1 27 HEEA083706 120030115A5320206064902035S CHANNEL BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 FUSELAGE CHANNEL CRACKED. SCRAPPED. 1G71 3U O H2SW 20030129000882003012900088SW 2003 1 29 HEEA083988 120030117A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20030207000142003020700014NM 2003 2 7 DLM88030041 120030108A5312 BULKHEAD DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27949DL 49880 DURING HMV-2, TOOLING DAMAGE WAS FOUND ON THE VERTICAL FLANGE OF PN 5910130387 AFT PRESSURE BULKHEAD TEE CAP AT STA 1338 BETWEEN L-29L TO L-29R, AND ON PN 5910130285 PRESSURE BULHHEAD WEB. THE TEE CAP WAS SPICED PER MD80 SRM 53-03, FIG 37. THE WEB WAS REPAIRED PER MD80 SRM 53-05, FIG 116. A TITANIUM DOUBLER WAS USED TO REPAIR THE SKIN THAT WAS CUT OUT FOR ACCESS. 2L72 4F RTA6WE 20030218002282003021800228NM 2003 2 18 SWAA030293 120030206A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM MID CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAMS CRACKED (2 EA) AT BS 662, WL 206 AND RBL 25 AND BS 727A + 18, WL 208 AND RBL 27. REPAIRED FLOORBEAMS PER SRM. 2L72 4F RTA16WE 20030219001712003021900171WP 2003 2 19 MWEA030084 120030217A53129915558230 ANGLE DOUG DC9 DC981 3022081WP STATION Z48 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LOWER ANGLE SUPPORT FOR AFT PRESSURE BULKHEAD FORMER IS DAMAGED RIGHT OUTBOARD FORWARD SIDE. -- REMOVED AND REPLACED ANGLE. 2L72 4F A6WE 20030221000812003022100081NM 2003 2 21 AWXA200300175 120030127A5313146N5417 STRINGER BOEING757 7572S7 1384962NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 1/2" CRACK WAS FOUND ONN AFT CARGO COMPARTMENT FLOOR BOARD STRINGER L/H SIDE OF CENTER LINE, BS 1475. MAINTENANCE REMOVED DAMAGED ARM OF SUPPORT STRINGER BS 1475; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030224000562003022400056NE 2003 2 24 HEEA084177 120030212A2421 SHAFT SKRSKYS76 S76A 8143006NE AC GENERATOR SHEARED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 1464 760060 AC GENERATOR SHAFT SHEARED. 1G72 3U H1NE 20030116000442003011600044SW 2003 1 16 HEEA083003 120030106A7797DPUK0414 WIRE HARNESS BELL 206 206L4 1182110SW INTELASTART COMPFAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F 52038 FAULT LIGHT WOULD NOT COME ON. TROUBLESHOT WIRING IN AIRCRAFT, FOUND WIRE THAT GOES TO FAULT LIGHT (WHT). SOLDER SPLICED INCORRECTLY - FUSE WIRE WAS SOLDERED TO WHT WIRE OF OAT PROBE INSTEAD OF FAULT LT WIRE. 1G71 3U NCH2SW 20030116002622003011600262NM 2003 1 16 ABXA030021 120030106A5320451T2504 PANEL BOEING767 767281 1385109NM FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE BETWEEN STA 577 - 610, LBL - RBL 15, CORRODED SHEAR PANEL. CORRODED SHEAR PANEL REMOVED, NEW SHEAR PANEL INSTALLED IAW SRM 51-40-02. 2L72 4F RTA1NM 20030117000122003011700012SW 2003 1 17 HEEA083157 120030108A6220 BEARING BELL 206 206B3 1181506SW LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V A1910314 3605 MAIN ROTOR LINK ASSY HAS A WORN BEARING. REPAIRED. 1G71 3U H2SW 20030117000212003011700021SW 2003 1 17 HEEA083161 120030108A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 TRANSMISSION RESTRAINT WORN. 1G71 3U H2SW 20030121000382003012100038SW 2003 1 21 HEEA083230 120030108A2810206064633103 FUEL CELL BELL 206 206L3 1182108SW FUSELAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038590X 51494 AIR BUBBLES IN BETWEEN MATERIAL AT AREA AROUND THE PUMP OPENING OF THE CELL. 1G71 3U H2SW 20030121001122003012100112SW 2003 1 21 HEEA083295 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MISINSTALLED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW036251X 51552 SHOULDER STRAP IS INSTALLED ON REEL BACKWARDS. FLAT SIDE OF ADJUSTMENT BUCKLES ARE NOT TOWARD CHEST WHEN WORN BY PILOT. REEL CAN ONLY BE INSTALLED ONE WAY. 1G71 3U H2SW 20030305000702003030500070EU 2003 3 5 HEEA084653 120030212A6720 BEARING BOLKMS105 BO105S 5626006EU BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 TAIL ROTOR BELLCRANK HAS WORN BEARINGS. REPLACED BEARING 2828P AND EN2015BN06E DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030225000382003022500038SW 2003 2 25 HEEA084257 120030120A3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW FLOAT BOTTLE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 204 53188 EMERGENCY FLOAT BOTTLE SOLENOID VALVE THERMAL RELIEF BLEW. 1G71 3U O H2SW 20030324000412003032400041NE 2003 3 24 74451 320030313A61107826761 BEARING RACE HAMSTD EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROP BLADE CRACKED B EY2RK NONE O OTHER UKUNKNOWN 1 GL03 856553 CRACK IN RACE 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20030324001102003032400110WP 2003 3 24 MWEA030140 120030324A531359114471 DOUBLER DOUG DC9 DC981 3022081WP STA 237 LONG 15 GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 STATION 237 FRAME ABOVE LONGERON 15 RIGHT IS GOUGED. -- FABRICATED,LOCATED,DRILLED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030307000382003030700038 2003 3 7 SWAA030453 420030227A2565D31354 SLIDE BOEING737 7377H4 1384404NM ALL CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED C1 CHECK, FOUND ALL CABIN DOOR EMERGENCY EVAC SLIDE ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030311000432003031100043SW 2003 3 11 HEEA085059 120030228A3212OHSS2061001 COVER BELL 206 206L3 1182108SW EMERGENCY FLOAT DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 FLOAT COVER IS TORN AND DETERIORATED. 1G71 3U H2SW 20030313001442003031300144EA 2003 3 13 OEZ2003F00000 120030212A5510C6TP101929 HINGE BRACKET DHAV DHC6 DHC6 2802606EA PWA PT6 PT6A11 52043NE HORIZONTAL STAB BROKEN A OEZAK NONE O OTHER ININSP/MAINT 1 WP19227SA45922 517 DURING SCHEDULED INSPECTION MAINTENANCE PERSONNEL FOUND RIGHT ELEVATOR OUTBOARD HINGE PLATE LOOSE WITH RIVETS (WORKING) AT ATTACHMENT TO OUTBOARD STABILIZER RIB. UPON DISASSEMBLY FOR REPAIR. HINGE PLATE BRACKET WAS FOUND CRACKED AND BROKEN AWAY FROM FORWARD EXTENSION APPROXIMATELY 5 INCHES FROM AFT END OF BRACKET. OVERSIZE CHERRYMAX RIVETS HAVE PREVIOUSLY BEEN INSTALLED IN THIS AREA ATTACHMENT TO RIB. 1H72 3T3 TRTA9EA E4EA 20030314000152003031400015NM 2003 3 14 ANCF200300011 120030304A2131 CONTROLLER BOEING757 757200 1384950NM CABIN PRESSURE INOPERATIVE W ANCFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23262CT 26246 EICAS MSG "CABIN AUTO INOP" AND "CABIN ALT AUTO 1&2" DISPLAYED. UNABLE TO CONTROL OUTFLOW VALVE USING MANUAL MODE. AT FL 230 THE CABIN ALTITUD LIGHT COMES ON AND THE CREW MADE A RAPID DESCENT TO FL 100. FIGHT RETURNED TO NEW YORK. AC MOTOR NR 2 WAS REPLACED IAW AMM 21-31-05/401 AND NR 2 SYSTEM TEST WAS PERFORMED IAW AMM 21-31-00/501 WITH NORMAL RESULTS. AUTOMATIC SYSTEM #1 WAS DIFFERED UNDER MEL 21-31-1 CAT "C". 2L72 4F RTA2NM 20030314000502003031400050WP 2003 3 14 ABXA030094 120030203A531599581863 FLOORBEAM DOUG DC9 DC931 3022065WP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 FLOORBEAM SEVERLY CORRODED AT AFT LOWER CARGO DOOR HOLD-OPEN HOOK, FS 937, RIGHT BUTT LINE 12. REPAIRED FLOORBEAM IAW DC-9 SSRM K07411. 2L72 4F A6WE 20030315000012003031500001EU 2003 3 15 DHL2003367501 120030225A7830 FLANGE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 517321 Item Ref.N/R:36725:#2 O/B rev. upper side has internal metal structure broken. Corrective action:Cut out damaged area,fabricated repair IAW Timco REO-GO9095. Alodined an primed IAW A300 SRM 51-30-30. 2L72 4F4 FRTA35EU E23EA 20030318002152003031800215SO 2003 3 18 C2XA03IA031 120030307A33501317 LAMP EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715941 145035 During postflight inspection the mid cabin emergency exit light would not illuminate. Maintenance removed and replaced the exit light bulb. The system tested good and the aircraft was returned to service. 2L72 4F RTT00011AT 20030319001132003031900113NM 2003 3 19 UIEA200300005 120030122A5730 SKIN BOEING747 747243B 1384830NM WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15516MC 22507 DURING CURRENT C-CHECK AT SIA, FOUND BS 1241 L/S KICK FITTING AT BOLT HOLE NR 11 CRACKED IN WING SKIN ONLY. REAMED HOLE TO 1.169 INCH. NO CRACK INDICATION. FINAL REAMED HOLE TO 1.284 INCH IN WING SKIN AND CHORD. REAMED STRINGER SPLICE FITTING TO 1.126 INCH. FABRICATED INDIVIDUAL BUSHINGS FOR WING SKIN, RIB CHORD AND STRINGER FITTING. FABRICATED FILLER BLOCK TO TRAP WING SKIN BUSHING. INSTALLED BUSHINGS AND FILLER BLOCK IAW SB 747-57A2314 REV 1. REPETITIVE INSPECTION REQUIRED AT 8000 CYCLES OR 25000 HOURS WHICH EVER OCCURS FIRST. (M) 2L74 4F A20WE 20030320001792003032000179 2003 3 20 SWAA030597 420030316A25656557463 FITTING BOEING737 7377H4 1384404NM FWD ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29411WN 29821 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING LOOSE. SECURED FITTING PER MM. 2L72 4F RTA16WE 20030422001412003042200141NM 2003 4 22 UPS03240264 120030217A5330 SKIN BOEING727 727108C 1384039NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, AREA OF LIGHT SURFACE CORROSION ON SKIN ABOVE ENG NR 2 PYLON RT SIDE AT BS 1363 AT RT COWL HINGE LINE. FASTENERS REMOVED FROM SKIN & GUTTER IAW SRM 51-30-02. NEW PANEL MADE IAW SRM 54-10-2 & 51-10-1. NEW PANEL ALODINED & PRIMED IAW SRM 51-10-2. RAIN GUTTER INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20030801000722003080100072EU 2003 8 1 ASOA03290 120030611A5320 FLOOR SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DUIRNG A C-CHECK IN BNA, FLOORBOARD SUPPORT AT FRAMES 36, 38 AND 39 FROM THE LEF TO THE RIGHT SIDE WRE FOND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOORBOARD SUPPORT AT FRAMES 36, 38 AND 39 FROM THE LEFT TO THE RIGHT SIDE IAW ASA EO 72-53-0140. (M) 2H72 4T RT 20030826000572003082600057CE 2003 8 26 5300051803 120030518A7110665210042 COWLING CESSNA560 560XL 2076702CE RT ENGINE CRACKED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07613GY347 5605300 RIGHT ENGINE COWL CRACK FORMING FROM OIL SERVICE DOOR. 2L72 4F RTA22CE 20030826000812003082600081 2003 8 26 YENA200316 420030720A2330 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 EA15522JB 1464 FLIGHT ATTENDANT REPORTED BURNING SMELL NEAR ROW 18. TURNED TV'S OFF. SMELL DISAPPEARED. INSPECTED SEBS AT ROW 17, 18, 19 ABC. ALL OPS CHK NORMAL. NO SMELL OF BURNING. ALL SCREENS OPERATING NORMAL IAW LTV MM 23-39-00. 2L72 4F RTA28NM 20030828000332003082800033WP 2003 8 28 NACA20030089 120030529A5330 SKIN DOUG DC6 DC6 3021702WP FUSELAGE CRACKED A NACAK NONE O OTHER ININSP/MAINT 1 AL032907F 44636 RIGHT FUSELAGE HAS LAP SEAM CORROSION AND CRACK COMING OUT OF RIVET HOLE AT STA R170 LONGERON 20. INSTALLED DOUBLER PER NAC DRAWING NAC011 SCENARIO 1. 2L74 4R A781 20030828001752003082800175NM 2003 8 28 SWAA031870 120030819A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 737 AT STR 18L AND BS 930 AT STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030902001322003090200132WP 2003 9 2 03FDEA01049 120030705A3260 BULB DOUG DC10 DC1030 3023501WP MLG INDICATOR BURNED OUT A FDEAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO25323FE 47811 UPON LOWERING LANDING GEAR, RECEIVED NO GREEN INDICATION ON EITHER F/O'S PANEL OR S/O PANEL. COMPLETED GO AROUND. TESTED LIGHTS, NO TEST ON GREEN LIGHTS. REPLACED BULBS ON F/O'S PANEL. WORKED. FACT 05JUL03 11:30 DTW ? FOUND BULBS BURNT OUT ON F/O'S AND S/O PANEL. RELAMPED IAW SMP LIGHTS OPS CHECKS GOOD. 2L73 4F A22WE 20030829001282003082900128NM 2003 8 29 SWAA031856 120030818A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 10, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728000342003072800034NM 2003 7 28 SWAA031594 120030718A5752113A72003 TAB BOEING737 7377H4 1384404NM LT AILERON CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SCHEDULED C2 CHECK, FOUND LT AILERON TAB CRACKED ON OUTBD L/E. REMOVED AND REPLACED LT AILERON TAB PER MM. 2L72 4F RTA16WE 20030903000972003090300097WP 2003 9 3 MEX2003352 120030810A801138334221 STARTER DOUG DC9 DC983 3022083WP LT ENGINE LEAKING A ASMFD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SW23838AM 49397 FLT 192 - MTY-TIJ - AIRCRAFT RETURNED TO PLATFORM, DURING LEFT ENGINE STARTER, N2 TURN 6 PERCENT N1 TURN 1 PERCENT ONLY AND WITH STRONG NOISE LOW LEFT ACCELERATOR. DURING OPEN COWLING WAS DETECTED ENGINE AIR TURBINE WITH LEAK. THE ENGINE AIR TURBINE WAS REPLACED IAW MM 80-1-01, ENGINES WERE STARTED, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030903000142003090300014 2003 9 3 XNOA01139 420030715A3421 GYRO BOEING727 727227 1384078NM NR 2 COMPASS INOPERATIVE A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL2379754 21363 NR 2 COMPASS SYSTEM INOPERATIVE. COMPASS CARD STAYED FROZEN. REMOVED AND REPLACED THE NR 2 DIRECTIONAL GYRO. PERFORMED CHECK OF THE NR 2 COMPASS SYSTEM. OPS CHECKS IAW MM 34-21-00. 2L73 4F A3WE 20030903001492003090300149NM 2003 9 3 VNAA0308009 120030817A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07458PS 3068 THE CREW REPORTED RECEIVING A LAV SMOKE CAS MESSAGE, THERE WAS NO SMOKE. MAINTENANCE AND THE CREW DEFERRED THE LAV SMOKE DETECTOR WITH 26-3 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030903001722003090300172EU 2003 9 3 2003F00544 120030529A5210350A2500500003 DOOR SNIAS 350 AS350BA 8680817EU PAX DOOR OPEN A HXSAA UNSCHED LANDING O OTHER CLCLIMB 1 AL056180T 1149 DEPARTING JUNEAU ABOUT 5 MINUTES OUT, AND THE LEFT MAIN CABIN DOOR WAS NOTICED AJAR. AIRCRAFT RETURNED TO BASE AND PILOT REPORTED THAT THE BOTTOM AND MIDDLE PINS WERE GOOD BUT THAT THE UPPER LATCH WAS NOT ENGATED. INSTRUCTED ATTENDANTS ON PROPER DOOR LATCHING AND ALSO HAD THE MECHANICS REWORK THE LATCH PLATE TO ALLOW BETTER LOCKING. (M) 1G71 3U NCH9EU 20030905000322003090500032SO 2003 9 5 C2XA03CL158 120030903A3350110049 CHARGER EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713965 145125 DURING ROUTINE MAINTENANCE THE LEFT HAND EMERGENCY LIGHT FORWARD OF THE WING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030904001272003090400127NE 2003 9 4 DL76L030612 220030703A7261 SEAL BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE LEAKING A DALAD RETURN TO BLOCK KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27195DN 28452 727654 AFTER ENG START FLT ATTDS REPORTED FUMES AND ODOR IN THE CABIN. PILOTS NOTICED SMELL AFTER COCKPIT DOOR WAS OPENED. JFK MAINT FOUND OIL LEAK LT ENGINE NR 1 BEARING SEAL AREA. FOUND OIL DRIPPING IN THE NR 1 INLET. REPLACED NR 1 BEARING SEAL SEAT AND CARBON SEAL ASSY. PER DAJIC M522. RAN ENG PER PFHB NO DEFECTS NOTED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F4 FRTA1NM E24NE 20030821001402003082100140EU 2003 8 21 03FDEA00887 120030616A5512 SKIN AIRBUS300 A300B4605R 3930308EU HORIZ STAB DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE11023 742 ON WALKAROUND UPON A/C ARRIVAL FOUND DENT ON LT HORIZONTAL STABILIZER LEADING EDGE LOWER SURFACE. THIS WILL BE C/W IN C-CHECK. FOUND DENT TO BE IN V-SHAPE 4 X 3 X .0265 INCH DEEP. LOCATION IS 5FT FROM WING TIP, APPROX STA 750 LOWER LEADING EDGE. C/W EA 6-5510-60101 PART 1, PART 2 TO BE C/W AT OR BEFORE NEXT C-CHECK. FACT 16JUN03 15:54 CWF U REPAIRED LEADING EDGE PER EA 6-5510-60101 PT 2. 2L72 4F RTA35EU 20030822000832003082200083NM 2003 8 22 03FDEA01105 120030717A2612 FIRE WARNING BOEING727 727200 138407ENM COCKPIT MALFUNCTIONED A FDEAK NONE N FALSE WARNING CLCLIMB 1 SO25498FE 20867 AT 900FT ON CLIMBOUT, FIRE WARNING BELL SOUNDED AND ENGINE FIRE WARNING LIGHTS ON INSTRUMENT PANEL ILLUMINATED FOR 2 SECONDS. NO OTHER INDICATIONS AND ALL OTHER SYSTEMS OPERATED NORMALLY. PERFORMED ENGINE FIRE WARNING TEST. TESTED GOOD. COULD NOT DUPLICATE. OK FOR SERVICE. 2L73 4F RTA3WE 20030730000332003073000033WP 2003 7 30 ABXA030273 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME AT STA 157. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-24 AND 51-1-21. 2L74 4F 4A25 20030827000492003082700049SW 2003 8 27 HEE2003F00000 120030202A7920209062010001 VALVE BELL 412 412 1182202SW PWA PT6 PT6* 52043EA ENGINE OIL LEAKING A HEERO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032149S 36002 VALVE, LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 4U3 T H4SW E2NE 20040301001282004030100128WP 2004 3 1 U2R2004F00001 120031029A1430 FASTENER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE L2 DOOR MISMANUFACTURED I U2RBK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23921R 46145 REPAIRED L2 DOOR AT LOWER FORWARD CORNER FS1620 IAW MM. 2L74 4F4 F 4A25 1E8 20031211001082003121100108WP 2003 12 11 AALA20031396 120031207A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21501AA 49738 RDU FORWARD AUXILIARY EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD AUXILIARY EXIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031212000862003121200086NM 2003 12 12 SWAA032403 120031031A34110856AE18 PROBE BOEING737 7373Q8 1384670NM PITOT/STATIC SYSOVERHEATED A SWAABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29687SW 23388 DECLARED EMERGENCY, STRONG BURNING ODOR DETECTED IN COCKPIT, FOLLOWED BY SMALL AMOUNT OF SMOKE COMING FROM F/O'S AFT RIGHT SIDE PANEL. FOUND F/O'S AUX PITOT PROBE ASSY BURNING STATIC LINE. REMOVED AND REPLACED PITOT PROBE AND STATIC LINE PER MM. 2L72 4F RTA16WE 20031215000602003121500060EA 2003 12 15 COMA0360497 120031114A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA RT ENGINE MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01981CA 7163 FLIGHT 5076 - RIGHT T/R REVERSE UNLOCKED CAUTION MESSAGE. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040304001382004030400138WP 2004 3 4 ASAA0380702 120031030A33970105606 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01947AS 53020 SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 21. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20031217000322003121700032WP 2003 12 17 DHL2003805601 120030829A533057103672 PANEL DOUG DC8 DC873F 302199FWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT AFT ADF SENSE ANTENNA PANEL INTERNAL SKIN DELAMINATED, STA 980.000. REMOVED AND INSTALLED RIGHT AFT ADF SENSE FOR OPS CHECK SEE JC BE1E34026. 2L74 4F RT4A25 20040415001362004041500136NM 2004 4 15 ASAA024014L 120030318A531165C32395 FRAME BOEING737 7374Q8 138447QNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 727F, RBL 17 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040802001072004080200107EU 2004 8 2 2004F00213 120031221A2730 ROD END AIRBUS320 A320233 3930329EU ELEVATORS LOOSE A RJEFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO23981LR 558 BZE - FLT 410 - DURING CLIMB FLIGHT, EXPERIENCED A STRONG VIBRATION IN ALL PHASES OF FLIGHT ABOVE 300 KNOTS. THE AIRCRAFT WAS RETURNED TO SAL STATION FOR MX. AT EL SALVADOR STATION, THE ELEVATORS FREE PLAY WERE INSPECTED PER AMM 27-34-00, AND FOUND A PLAY ON A ROD END ON THE GREEN SYSTEM SERVO ACTUATOR OF THE LEFT ELEVATOR AND A PLAY ON THE ROD END OF THE BLUE SYSTEM SERVO ACTUATOR OF THE RIGHT ELEVATOR. BOTH SERVO ACTUATOR ROD ENDS WERE REPLACED AND RIGGED PER AMM 27-34-00. A FLIGHT TEST WAS PERFORMED AND NORMAL RESULTS WERE FOUND. AIRCRAFT TO NORMAL OPERATIONS. (M) 2L72 4F RTA28NM 20030925000652003092500065WP 2003 9 25 AALA20030898 120030823A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21286AA 49298 DURING OVERNIGHT MAINTENANCE, INTERIOR CEILING EMERGENCY ESCAPE PATH LIGHTING ROWS 27 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK AT B5 107. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20050816002172005081600217NM 2005 8 16 MZZA0300004 120030910A5711 SPAR BOEING737 737823 13844BZNM LT WING CORRODED A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314250 28957 INSPECTION FOUND HEAVY INTERGRANULAR CORROSION AT THE LT WING NR 1 FORWARD PUMP BONDING STRAP (FRONT SPAR WEB). FRONT SPAR WEB WAS REPAIRED IAW ECRA. RESISTANCE CHECK WAS GOOD IAW MM. (K) 2L72 4F RTA16WE 20030115001902003011500190GL 2003 1 15 ERAA082942 220030106A72606894171 GEARBOX ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01 6769 TORQUE FLUCTUATIONS. FOUND LOOSE PLUG ON AFT SLIDE OF COMPRESSOR STUD, HIDDEN DAMAGE FOUND WORN BUSHINGS ON OIL PUMP BODY AND WORN JOURNALS ON OIL PUMP SPUR GEAR. INSTALLED SERVICEABLE GEAR BOX HOUSING, NEW OIL PUMP SPUR GEAR AND PUMP BODY, OVERHAULED GEARBOX. 3 U E4CE 20030815000322003081500032 2003 8 15 HEEA088517 420030804A2312 HEADSET BELL 206 206L3 1182108SW COCKPIT NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610C 51425 DAYTIME/NIGHTTIME SENSOR CAUSES A BUZZ IN THE HEADSETS. IN SHOP REPAIR. 1G71 3U H2SW 20030819001392003081900139EU 2003 8 19 03220302 120030808A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27302UE 41013 DURING MAINTENANCE INSPECTION THE AFT SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE AFT EMERGENCY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030819001752003081900175NM 2003 8 19 SWAA031738 120030804A521090100722 SNUBBER BOEING737 7373K2 13844BANM FWD ENTRY DOOR FAULTY A SWAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SW29340LV 23738 AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AND REPLACED FWD ENTRY DOOR SNUBBER AND ADJUSTED DOOR PER MM. 2L72 4F RTA16WE 20030818000512003081800051 2003 8 18 BAQA088265 420030812A3421060001301 GYRO UROCOPEC135 EC135T1 5620026EU COCKPIT PRECESSES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118WS49 0089 GYRO PRECESSING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030819002342003081900234NM 2003 8 19 CALA0300372 120030709A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711641 28902 INSPECTION FOUND A .25 INCH CRACK IN INTERCOSTAL AT STA 344-360, RBL 3. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030820001282003082000128 2003 8 20 234TR0005 420030719A3421258733511 GYRO BOEING737 737228 13844AGNM COCKPIT MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 NR 1 VERTICAL GYRO SHOWS 3.5-4 DEGREES PITCH UP. REPLACED VERTICAL GYRO PER MM 34-21-21. 2L72 4F RTA16WE 20030820001522003082000152NM 2003 8 20 QXEA200300921 120030719A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- RIGHT HAND INBOARD NR 7 SEAT TRACK DRIP TRAY IS GOUGED AT STATION X312.350. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20030401000202003040100020WP 2003 4 1 AALA20030221 120030223A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21437AA 49455 DURING OVERNIGHT MAINTENANCE, WALL MOUNTED EMERGENCY EXIT LIGHT ACROSS FROM FORWARD LAVATORY IN AISLE INOPERATIVE. REPLACED WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030625001182003062500118NM 2003 6 25 DHL2003743006 120030401A2612 BRACKET BOEING727 727225 1384077NM NR 1 FIRE LOOP BROKEN A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 AFTER PRE-DEPARTURE CHECK FOUND NR 1 FIRE WARNING GROUND FAULT TEST LIGHT INOPERATIVE. DEFERRED PER MEL 26-9 CAT-C DMI 12419. REF DMI 12419; NR 1 FIRE WARNING GROUND FAULT TEST LIGHT INOPERATIVE. FOUND BROKEN BRACKET ON B-FLANGE, REPLACED, RE-SECURED FIRE LOOP, OPS CHECKED NORMAL IAW M/M 26-11-01 & 26-11-12. THIS CLEARS DMI 12419, PLACARD REMOVED. 2L73 4F A3WE 20030822000682003082200068EU 2003 8 22 2003UALA00450 120030524A2133VFT300B00 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE MALFUNCTIONED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29481UA 1559 AVIONICS VENT FAULT ECAM MESSAGE ILLUMINATED. FOUND SKIN AIR OUTLET VALVE MALFUNCTIONING AS REPORTED BY CFDS AND REPLACED SAME. 2L72 4F4 FRTA28NM E40NE 20030410001862003041000186NM 2003 4 10 DHL2003741513 120030323A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK FOUND BS 460 RT CIRCUMFERENTIAL DENTED 4 INCHES ABOVE FLOOR. CUT OUT DAMAGED AREA AS PER B-727 SRM 53-10-2. FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2. INSTALLED DOUBLER AS PER B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030423001292003042300129CE 2003 4 23 DXTA200300006 120030312A2120 SMOKE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE COCKPIT DETECTED E DXTAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07383QS 5600483 DURING GROUND OPERATION WITH GPU PLUGGED IN AND AVIONICS SYSTEM ON, ODOR AND SMOKE FILLED CABIN. SMOKE CAME FROM THE COCKPIT. 2L72 4F4 FRTA22CE E25EA 20030424001192003042400119NM 2003 4 24 UPS03440342 120030304A5310 STRAP BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, CRACKS FOUND AT BS 2231 RT INBOARD ATTACHED STRAP, THE CRACKS RUNNING FWD AND AFT DIRECTION OF ONE EACH FASTENER HOLE AND CRACKED THROUGH THICKNESS. M/D - RIGHT BS 2231 STR 24-25 REVEAL PANEL STRAP REPAIRED AS PER SRM 53-10-04 FIG 115. 2L74 4F RTA20WE 20030423001962003042300196NM 2003 4 23 QXEA0300364 120030317A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR LACK OF LUBE A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09402QX 4032 PDX ON FLIGHT 2309- AFT CARGO DOOR UNSAFE IN FLIGHT. AIRCRAFT RETURNED TO FIELD. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND AFT CARGO DOOR HANDLE OUT OF LOCKED POSITION. CLEANED AND LUBED HANDLE SHAFT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030428001602003042800160NM 2003 4 28 ZW0A0304001 120030408A3350 POWER SUPPLY DOUG MD80 MD83 3023681NM EMERGENCY LIGHTSINOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139414W 53189 THE EGRESS LIGHTS WERE INOPERATIVE BETWEEN ROWS 3 AND 4, AND BETWEEN ROWS 7 TO 13. RESEATED LAMP AT ROW 3-4 AND RESEATED BATTERY IN POWER SUPPLY B5-206 FOR ROWS 7 TO 13. CHECK-C 11-6-02 STL. 2L72 4F RT 20030428001872003042800187SO 2003 4 28 RAIA00303091 120030328A3320BR90002 BALLAST EMB 145 EMB145 3260210SO CABIN FAILED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03802HK 145066 PIT- CREW REPORTED ELECTICAL ODOR IN CABIN. MAINTENANCE FOUND DEFECTIVE LIGHT BALLAST AND REPLACED BALLAST, OPS CHECK OK. 2L72 4F RTT00011AT 20030429001342003042900134NM 2003 4 29 AUS20030285 120030212A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER SPLICE ON STRINGER 27L LOCATED AT BS 680 CONTAINED LEVEL2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030430000972003043000097NM 2003 4 30 USAASB03045 120030325A3260MS253831 SWITCH BOEING737 7374B7 1384702NM MLG FAILED A USAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 EA19426US 24548 EWR - FLT 540 - UPON APPROACH INTO EWR, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS WHILE EXTENDING LANDING GEAR. CREW RECYCLED THE LANDING GEAR WITH SAME RESULTS. CAPTAIN ACCOMPLISHED GO-AROUND AND PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES. RESULTS WERE THE SAME AGAIN. FIRST OFFICER THEN PUSHED FORCIBLY ON GEAR HANDLE AND RED LIGHTS EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AS EMERGENCY TRUCKS FOLLOWED AIRCRAFT TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER POSITION SWITCH S78 PER MM 32-61-11. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030430001702003043000170NM 2003 4 30 SWAA030864 120030416A53206551698 SPLICE BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030430001842003043000184NM 2003 4 30 SWAA030895 120030421A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030501000952003050100095WP 2003 5 1 GTIA030217 120030219A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND CORRODED WEB LONGERON 18L BETWEEN STATION 1079 AND 1098 UPPER CEILING AFT CARGO PIT. REMOVED DAMAGED WEB FROM STATION 1055 TO 1098. FOUND MORE CORROSION AT STATION 1022. OBTAINED MEMBRANE (WEB) FROM STOCK ROOM, LOCATED AND DRILLED MEMBRANE. INSTALLED NEW WEB. (M) 2L72 4F RTA6WE 20030505000932003050500093NM 2003 5 5 03FDEA00483 120030417A5414 SKIN BOEING727 727200 138407ENM NR 1 NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 1 ENGINE UPPER NACELLE FORWARD UPPER CORNER SKIN SEPARATED. REMOVED AND REPLACED REPAIR DOUBLER IAW BOEING 727 SRM 51-30-2. 2L73 4F RTA3WE 20030506000702003050600070NM 2003 5 6 03FDEA00574 120030422A5320 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION ON STR CLIP BS 870 STR 27L. 2L73 4F RTA3WE 20030506002062003050600206WP 2003 5 6 ASAA0380231 120030307A5320996535218 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CENTER FLOOR PANEL SUPPORT CORROSOIN. REPLACED SUPPORT PER SRM. (M) 2L72 4F A6WE 20030509000102003050900010WP 2003 5 9 GTIA030239 120030311A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND AFT PIT FS 1250 FRAME CORROSION. CUT OUT DAMAGE, FABRICATED 5, 9 AND 35 ANGLES AND 13 PLATES AND INSTALLED 5, 9, AND 35 ANGLES AND 13 PLATES. (M) 2L72 4F RTA6WE 20030514002092003051400209NM 2003 5 14 03FDEA00720 120030430A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING: O/B FLAP I/B HINGE ATTACHMENT TO FLAP LOWER AFT HOLE (2 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP. 2L73 4F RTA22WE 20030515000762003051500076EU 2003 5 15 DXTA200300024 120030430A3260 SWITCH BRAERO1000 HAWKER1000 7450005EU NLG LACK OF LUBE E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07549QS 259049 WHEN GEAR WAS SELECTED DOWN NO INTRANSIT LIGHTS OR GEARDOWN LIGHT ON FOR NOSE GEAR. INDICATOR PIN SHOWED GEAR DOWN AND LOCKED. GREEN LIGHT CAME ON ONE OR TWO MINUTES LATER. FOUND NLG LEG LOCK, CHANGE OVER AND STRUT LOCK SWITCHES STICKY, LUBED SWITCHES. 2L72 4F RTA3EU 20030514001672003051400167NM 2003 5 14 P5CA0300861 120030412A541281103 BULKHEAD BOEING747 747249F 1384849NM NR 1 PYLON GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 NR 1 PYLON BULKHEAD NAC STA 222 AFT FACE DOUBLER AT WL 174 ON LT SIDE OF THE WEB PER REF 1. REPAIRED PER SRM 54-14-03. PAO - SIN 03-0014M, PAO - SIN 03-00015F. 2L74 4F A20WE 20030515001462003051500146EU 2003 5 15 AWXA200300531 120030427A5320D53070011 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT Y254, FR 16 TO FR 20. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR SUPPORT Y254, FR 16 TO FR 20; FABRICATED 4 EACH REPAIR ANGLES, AND A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 211-212, FIG 202. 2L72 4F RTA28NM 20030520000512003052000051SO 2003 5 20 SIMA200311310 120030326A532014521725013 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, FORWARD SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030522000762003052200076SO 2003 5 22 C2XA03TY057 120030517A531514521699003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE DIGITAL PLATE WAS FOUND CORRODED AT FR20 & 22. MAINTENANCE REMOVED AND REPLACED THE LEFT TOP CAP DIGITAL IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030520001302003052000130EU 2003 5 20 ASOA03189 120030421A5320 SILL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN BNA, THE RIGHT SILL PLATE FROM FRAME 39 TO 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SILL PLATE FROM FRAME 39 TO 41 IAW SRM 51-25-01 AND SRM 51-25-03. (M) 2H72 4T RTA53EU 20030612001502003061200150WP 2003 6 12 UPS03840739 120030505A5510 CAP DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, LT HORZ STAB INBOARD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. REMOVED LT HORZ STAB INBOARD BOX T-CAP, REC'D NEW FITTING LOCATED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030523001292003052300129NM 2003 5 23 DHL2003748008 120030517A5710 ANGLE BOEING727 727225 1384077NM SLAT ACT SUPPORTCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 DURING DROP IN MAINTENANCE DISCREPANCY AS FOLLOWS, UPON REMOVAL OF DOUBLERS FOR SB 727-57-0130 FOUND THE OUTBOARD NR 8 SLAT ACTUATOR MOUNT ANGLE TO BE CRACKED. REMOVED NR 8 SLAT ACTUATOR CRACKED O/B MOUNT ANGLE IAW B-727 SRM 51-30-2. FABRICATED NEW ANGLE FROM 7075 T-6 .063 INCH PO 9912495, DIMENSIONS 11 X 4 INCH IAW B-727 S/B 727-57-0130. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED O/B NR 8 SLAT ACTUATOR ANGLE IAW B-727 SRM 51-30-2 AND S/B 727-57-0130. 2L73 4F A3WE 20030624000272003062400027NM 2003 6 24 HNAA0300028 120030603A246025ET1TF SWITCH DHAV DHC8 DHC8102 2809003NM ZONE 200 SHORTED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA07942HA37357 163 DURING NR 1 ENGINE START THE FLIGHT/TAXI SWITCH POPPED TO THE FLIGHT POSTION, FOLLOWED BY A DC BUS FAULT AND SMOKE COMING FROM THE FLIGHT TAXI SWITCH. REPLACED THE FLIGHT TAXI SWITCH. 2H72 4T RTA13NM 20030909001832003090900183EU 2003 9 9 BAQA088685 120030815A77141179405303 INDICATOR BOLKMS117 BK117A1 5626010EU TRIPLE TACH RATCHETING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03967LS2558 7067 ENGINE TRIPLE TACH NR 1 AND 2 NEEDLES RATCHET. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030910001872003091000187SO 2003 9 10 SIMA200320805 120030722A5330 SKIN EMB 135 EMB135LR 3260305SO FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 ABI - DURING AN IMBV INSPECTOIN, SEVEN GOUGES WERE FOUND JUST AFT OF FRAME 24 AND BELOW STRINGER 18L. COMPLETELY REMOVED DAMATE BY PERFORMING A CUTOUT. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMBL 145 SRM, SRM 145/1142 REV 22, 53-22-01, CPM 51-21-05 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030912001592003091200159EU 2003 9 12 AWXA200300911 120030803A5320D5397470600600 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 MCN - MINOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT CENTER PROFILE AT FR 56, BETWEEN STR 42 LT AND STR 41 RT. MAINTENANCE REMOVED CORRODED CENTER PROFILE AT FR 56, BETWEEN STR 42 LT & STR 41 RT; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW SRM 51-42-11, PG 21-22, FIG 8, PG 8-11, FIG 2, AND PG 12, FIG 3. 2L72 4F RTA28NM 20030929001252003092900125WP 2003 9 29 03FDEA01458 120030907A7830 SUPPORT DOUG MD10 MD1010F WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR. COMPLIED WITH E.A.8-7830-72283. EXHAUST-THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR. 2L73 4F RTA22WE 20031001000792003100100079NM 2003 10 1 2003UALA00717 120030925A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29369UA 24538 FWD LOWER FRAME OF THE FWD RT DOOR CUT-OUT HAS A PIECE MISSING. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031002001112003100200111NM 2003 10 2 QXEA200301096 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 2 SEAT TRACK IS CORRODED BELOW 2 RT LUGS AFT OF STATION X445. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031003000232003100300023NM 2003 10 3 AALA20030966 120030906A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21697AN 26977 EMERGENCY EXIT LIGHT INOPERATIVE IN THE FIRST CLASS CABIN. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031022000712003102200071SO 2003 10 22 C2XA03TY165 120030922A532014524119007 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713995 145295 DURING A SCHEDULED 2C INSPECTION THE PAX DOOR THRESHOLD WAS FOUND WITH CORROSION. MAINT. REMOVED AND REPLACED THE PAX DOOR THRESHOLD. CLEANED CORROSION UNDER DOOR SEAL RESTORED THE TOPCOAT AND TREATED THE ALUMINUM SURFACE IAW EMB 145 SRM 51-14-02;CPM 51-21-04'05'06 AND EMB 145 AMM 20-10-01. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T4 FRTT00011ATTE6CH 20030909002042003090900204WP 2003 9 9 ABXA030335 120030806A552339180341 ATTACH FITTING DOUG DC9 DC941 302207NWP ELEVATOR TAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 RIGHT ELEVATOR GEARED TAB ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20031023000492003102300049SO 2003 10 23 SWIA200312439 120030920A27503472001001 FCU EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07569SW7434 3419 120344 UPON FLAP RETRACTION AFTER TAKEOFF, FLAPS HAD DISAGREEMENT. IB WOULD NOT RETRACT INITIALLY. AFTER APPROXIMATELY 1 MIN, IB FLAPS RETRACTED. AFTER LANDING, FLAPS WOULD NOT RETRACT BEYOND 5-10 DEGREES WITH DISAGREEMENT ALL FLAPS. REMOVED AND REPLACED FCU IAW EMB MM 27-50-06. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031028001562003102800156NM 2003 10 28 GAIA03086 120030910A5311 FRAME BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE FUSELAGE DENTED E GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 380 HAS A DENT IN THE RADIUS BELOW STRINGER 6LT. REF FASI N/R 53129, CUT OUT DAMAGE 4.75 BY 1.25, DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-4 FIG 1. (M) 2L73 4F4 F A3WE E2EA 20040212000632004021200063SO 2004 2 12 421C120803 220031205A8520GTSIO520L1B CRANKCASE CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO ENGINE CRACKED B JBZRK NONE O OTHER ININSP/MAINT 1 WP27321FL 1031 421C0207 292488 AT ROUTINE 50 HOUR OIL CHANGE, MAINTENANCE PERSONNEL NOTICED OIL RT ENGINE CYLINDER BASE. VISUAL INSPECTION INDICATED CRACK BETWEEN NR 1 AND NR 3 CYLINDERS IN CRANKCASE WEB STRUCTURE. 1L72 3O3 O A7CE E7CE 20040212000772004021200077NM 2004 2 12 DHL2003782015 120031209A5230 PLATE BOEING727 727227 1384078NM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 FWD LWR CARGO DOOR THRESHOLD PLATE HAS 2 CRACKS. PREVIOUS WELD 1 CRACK TRANSVERSE 1 CRACK 1 INCH LONG. REPAIRED CRACK IAW BAC 5975 SPECS. REF. 8130-3 TRACKING NR AW152 COPY ATTACHED. RE-INSTALLED THRESHOLD IAW B727 M/M 20-80-1. 2L73 4F A3WE 20031030001082003103000108NM 2003 10 30 03FDEA01548 120030916A5320A5A7114507 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CTR CARGO PIT - POSSIBLE CRACK AT STA 5-115 STRINGER SPLICE 46L FLOOR AREA. CTR CARGO STA 5-115 S46L STRINGER CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG N5A6774 AND SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20031103001472003110300147NM 2003 11 3 03FDEA01778 120031009A5753ARC0503 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP O/B HINGE BRACKET (WING SIDE) - O/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION AND CMM 57-44-09 2L73 4F RTA22WE 20031112000602003111200060NM 2003 11 12 CALA0300625 120031107A5347 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND SEAT TRACK CORRODED AT STA 277-294, RBL 43. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031112000532003111200053 2003 11 12 SWIA200312583 420031030A2215 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07586SW 120354 CONTROL COLUMN BINDING WHEN PERFORMING FLIGHT CONTROL CHECK. REMOVED AND REPLACED PRIMARY ELEVATOR SERVO REF EMB 120 MM 27-00-03. OPS CHECKS GOOD. P/N: 5734002, S/N OFF: 10584. 2L72 4T RTA31SO 20031119000872003111900087NM 2003 11 19 AWXA200301207 120031012A3397BMS13311122 WIRE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE EMERGENCY LIGHT WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 DURING INSPECTION THE OVER WING EMERGENCY EXIT AISLE SIGN WAS FOUND INOPERATIVE ON ONE SIDE. MAINTENANCE RE-PINNED THE BACK SHELL CONNECTOR ON OVER WING EMERGENCY EXIT AISLE SIGN, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2EA 20031107001152003110700115NM 2003 11 7 ASAA0310436 120030512A5320BAC1509100146 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 859, RIGHT BUTTOCK LINE 8 CORRODED. CUT OUT DAMAGE AND REPAIRED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20031106002232003110600223NM 2003 11 6 ASAA0310458 120030515A523065C8073525 DOOR FRAME BOEING737 737290C 138448VNM CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE AFT CARGO DOOR FRAME AT FUSELAGE STATION 836, LEFT BUTTOCK LINE 60 CRACKED. REPLACED DAMAGED DOOR FRAME SECTION PER SRM. (M) 2L72 4F A16WE 20031110002042003111000204NM 2003 11 10 SWAA032230 120031008A531465458661030 KEELBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM CORRODED AT BS 500D + 10, STR 28R. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20031118000202003111800020EU 2003 11 18 MALA030444 120030926A49904501690A APU BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE APU BAY ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15532XJ E2366 DURING FLIGHT 3526, F/A COMPLAINED OF GAS ODORS COMING FROM CABIN. MAINTENANCE COMPLETED PACK BURN AND VERIFIED CONTAMINATION COMING FROM APU AIR SYSTEM DEFERRED APU PER MEL 49-00-1 (C) TRANSFERRED TO DMR MXC NOTIFIED 6425. MAINTENANCE REPLACED APU P/N 4501690A, S/N SPE977509 IAW APU GANGE JOB CARD REF JOB CARD AND 409, 172209 FOR DETAILS. REMOVED FROM DMR MXC NOTIFIED. 2H74 4F4 FRTA49EU E6NE 20040108001592004010800159CE 2004 1 8 CNQ2003F00002 120030929A2161IE4510 CONTROLLER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL CABIN TEMP SHORTED E CNQRO OTHER O OTHER DEDESCENT 1 CE07900QS2171 7500123 WHILE DESCENDING THROUGH FL330, THE COCKPIT TEMPERATURE CIRCUIT BREAKER TRIPPED. COCKPIT DISPLAY UNITS NR 1 AND NR 2 WENT INOPERATIVE. UPON FURTHER DESCENT, COCKPIT DISPLAY UNITS NR 4 AND NR 5 WENT INOPERATIVE. ALL DISPLAY UNITS WORKED OK AFTER COOLING OFF. REPLACED TEMPERATURE CONTROLLER, SYSTEM OPERATIONALLY CHECKED GOOD. 2L72 4J4 FRTT00007WITE6CH 20031120001242003112000124EU 2003 11 20 YENA200334 120031107A77206A5878 WIRE HARNESS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE EGT SHORTED A YENAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA15521JB10526 1452 10943 TAKEOFF ABORTED DUE TO NR 1 ENG OVERHEAT ECAM, ABOUT 90 KT. PERFORMED TSM TASK 77-00-00-810-817. EIS(DMC1) REPORT SHOWED NR ENG 1 OVERTEMP. CHECKED REPORTS 4, 6, 10 ON AIDS. NO OVERTEMP NOTED. PERFORMED VISUAL INSP OF EGT JUNCTION BOX ON NR 1 ENG, NO DEFECTS NOTED. PERFORMED VGV INSP & LUB AS PER 75-32-42. NO DEFECTS NOTED. PERFORMED TEST NR 11 HIGH POWER ASSURANCE TEST IAW AMM71-00-00-710- 013-A. TEST GOOD. NO FAULTS ON GROUND. AS PER MCC REQUEST PRECAUTIONARY REMOVED & REPLACED NR 1 ENG EIU & OPS OK PER MM 73-25-34. ON 11/9/03 PER JB ENGINEERING & AIRBUS REMOVED & REPLACED NR 1 ENG JUNCTION BOX & EGT HARNESS, TROUBLESHOOTING FOUND EGT HARNESS GROUND FROM B-CHANNEL BROKEN. 2L72 4F4 FRTA28NM E40NE 20031216000862003121600086NM 2003 12 16 SWAA032582 120031122A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 727E, STR 24R AND STR 23L. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20031217001242003121700124WP 2003 12 17 ABXA030468 120031125A531099115414 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 SHEAR TIE CRACKED AT FS 718 LONGERON 5 RIGHT. INSTALLED NEW SECTION OF SHEAR TIE IAW DC-9 SRM 53-03. 2L72 4F A6WE 20031218000912003121800091NM 2003 12 18 2003UALA00879 120031119A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29534UA 25129 FUSELAGE SKIN BETWEEN STA 595-625 AND STR 15L TO STR 18L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031222001082003122200108NM 2003 12 22 USAASB03201 120031113A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19437US 24559 MAINTENANCE REPORTED THE EMERGENCY LIGHTS INOPERATIVE AT THE FORWARD LEFT OVERWING EMERGENCY HATCH AND SEAT. MAINTENANCE REMOVED AND REPLACED THE M1479 BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031223000802003122300080EA 2003 12 23 COMA0360543 120031210A53206008610411 FITTING CNDAIRCL600 CL6002B19 1900309EA PROX SENSOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 NLG DOOR OPERATING MECHANISM BASE AFT SIDE IS CRACKED AT CUTOUT HOLE FOR PROX SENSOR PS17GA. REMOVED AND REPLACED NLG DOOR OPERATING MECHANISM ASSY P/N 600-86101-1001 IAW CRJ 200 AMM 32-32-15-400-801. 2L72 4F RTA21EA 20031231001112003123100111NM 2003 12 31 TSAA0329180 120031115A2910AE2464163E0192 HOSE BOEING737 7372T4 1384492NM "A" HYD SYSTEM FAILED A TSAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13807AL 23443 AFTER GEAR RETRACTION LOST ENTIRE 'A'SYSTEM HYD QTY. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PRESSURE RETURN HOSE ASSEMBLY. (M) 2L72 4F A16WE 20030623000082003062300008EA 2003 6 23 ASOA03217 120030517A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTION OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 4 A/C. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030630000392003063000039EU 2003 6 30 AWXA200300615 120030502A5320D5397470700000 PROFILE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, RBL 686 MM. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, RBL 686 MM; FABRICATED 2 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-05341-03142-TB5. 2L72 4F RTA28NM 20030630000662003063000066SW 2003 6 30 ALGA087782 120030626A8011214060056109 STARTER BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE ENGINE FAILED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03391AL 28103 STARTER WILL NOT ENGAGE. REQUEST WARRANTY REPAIR. DMR 719714 RO33252 2G72 4U4 U H10SW E8NE 20030714001162003071400116NM 2003 7 14 CALA0300349 120030701A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND STRINGER 26R CORRODED AT STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 5-40-2. 2L72 4F RTA16WE 20030716000482003071600048NM 2003 7 16 GAIA03018OP 120030611A2120 ODOR BOEING727 727251 138408HNM COCKPIT DETECTED A GAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07252US 19971 DURING FLIGHT AND TAXI IN, CREW NOTICED A UNIDENTIFIABLE ODOR IN THE COCKPIT. FUEL LEAKS WERE REPAIRED AT LT WING TO BODY BOLT AND AT BOTH LT AND RT FORWARD TRUNNION FITTINGS. REMOVED AND REPLACED BOTH WATER SEPARATOR SOCKS. INSPECTED ENTIRE AIRCRAFT, RAN ENGINES, AND PRESSURIZED AIRCRAFT TO 5 PSI DIFFERENTIAL PRESSURE. NO SMOKE FUMES OR ODD ODORS DETECTED BY GROUND CREW OR FIRE DEPARTMENT EQUIPMENT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030716000522003071600052WP 2003 7 16 GTIA030459 120030514A575259100472 TAB DOUG DC9 DC981 3022081WP RT AILERON DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND RT WING AILERON CONTROL TAB HAS NUMEROUS DENTS ON UPPER SIDE. ON REMOVAL OF PAINT, CORROSION WAS LOCATED ON THE RT TAB LOWER SKIN IN SEVERAL AREAS AS MARKED. REPLACED RT AILERON CONTROL TAB. (M) 2L72 4F A6WE 20030114000882003011400088NM 2003 1 14 CALA0300007 120030112A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 540 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917321 23372 INSPECTION FOUND A 1" CRACK IN RADIUS OF FLOORBEAM ON AFT SIDE OF STA 540 UNDER EXPANSION JOINT AT R/H I/B SEAT TRACK. REPAIRED IAW ECRA 5320-01406. 2L72 4F RTA16WE 20030106001542003010600154NE 2003 1 6 HEEA082805 120030102A63217665009803105 POWERPACK SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROTOR BRAKE POWER PACK CYCLES ON AND OFF EVERY 3 SECONDS WHEN HARD BRAKE PRESSURE ON. 1G72 3U H1NE 20030128001922003012800192NM 2003 1 28 QXEA0300126 120030125A326035138507002 CONTROL UNIT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAK NONE O OTHER UKUNKNOWN 1 NM09410QX1751 4053 PDX-ON FLIGHT NUMBER 2335, AFTER GEAR RETRACTION, GREEN NOSE GEAR DOWN INDICATOR REMAINED ILLUMINATED. ALTERNATE GEAR POSITION INDICATOR INDICATED NOSE GEAR WAS RETRACTED. REMOVED AND REPLACED ADVISORY CONTROL UNIT. OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030129000312003012900031SW 2003 1 29 HEEA083944 120030117A6420407012101111 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR OUT OF BALANCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH4901 53378 UNABLE TO BALANCE TAIL ROTOR HEAD BELOW .65 IPS WITH THE RADS GEAR. REPAIRED. 1G71 3U O H2SW 20030131001692003013100169NM 2003 1 31 UPS03240105 120030106A5510 BRACKET BOEING727 72722C 138400FNM HOR STAB R/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 19094 INSPECTION TYPE:C+SI R/H HOR-STAB,REAR SPAR,T-BRACKET ON REAR SPAR AT ELEV.RIB ST.66.50 I S CRACKED. BRACKET REMOVED IAW SRM 51-30-2 AND DRG.NO.65-16876. NEW BRACKET FITTED IAW SRM 51-30-2 AND DRG. NO.65-16876. 2L73 4F A3WE 20030207000922003020700092NM 2003 2 7 03FDEA00031 120030115A2497 LEAD BOEING727 727200 138407ENM PWA JT8 JT8D* NE GENERATOR SYS OUT OF POSITION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 STRINGER 20L CHAFED BY GENERATOR LEAD, BS 374, AT LT END OF E1 RACK. REPAIRED STR 20L BS 360-390 IAW SRM. 2L73 4F4 FRTA3WE E2EA 20030218000702003021800070NM 2003 2 18 AALA20030016 120030103A3350 TERMINAL BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT FORWARD OF M-2 LAV INOPERATIVE. REPLACED BROKEN TERMINAL AT EMERGENCY EXIT CEILING LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030218000872003021800087NM 2003 2 18 AMTA200300152 120030128A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 R2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. CHANGE BATTERY PACK IAW 33-51-07-902-003-001. (M) 2L72 4F RTA2NM 20030224001502003022400150NM 2003 2 24 AWXA200300202 120030213A531165465588 FRAME BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON AFT SIDE OF THE AFT CABIN FRAME BS 907, BETWEEN STR 1 & 2 R/H. MAINTENANCE CUTOUT CRACKED AREA OF AFT CABIN FRAME BS 907; FABRICATED A REPAIR CHANNEL AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG. 1, PG. 1-6. 2L72 4F RTA16WE 20030225000422003022500042SW 2003 2 25 HEEA084261 120030120A3230407073854101 TUBE BELL 407 407 1182206SW MLG HYD SYS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 MLG HYD SYSTEM LINE HAS CORROSION. 1G71 3U O H2SW 20030303000452003030300045 2003 3 3 HEEA084503 420030214A2340A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 INTERPHONE BOX PRODUCING STATIC WHEN TRANSMITTING. IN SHOP REPAIR. 1G72 4U H4SW 20030307000612003030700061 2003 3 7 SWAA030409 420030221A25656557463 FITTING BOEING737 7373H4 1384600NM AFT ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTING LOOSE. SECURED GIRT BAR FITTING PER MM. 2L72 4F RTA16WE 20030310000472003031000047EU 2003 3 10 DHL2003366003 120030307A5270 ACTUATOR AIRBUS300 A300B4203 3930306EU A DHLAO OTHER O OTHER CRCRUISE 1 SO01366DH 249 1) IN CRUISE FLIGHT, CARGO DOOR LIGHT AND THE NOT LATCHED LIGHT ILLUMINATED AS WELL AS THE CARGO SWITCH FAULT LIGHT. NO SINGLE STROKE CHIME OR MWP DISPLAY INDICATED.2) REMOVED AND REPLACED LINEAR ACTUATOR. OPS CHECKED GOOD IAW M/M SUPPLEMENTAL 52-36-11. RII REQUIRED. 2L72 4F RTA35EU 20030311000822003031100082EA 2003 3 11 COMA0360134 120030308A5610NP1393222 WINDOW CNDAIRCL600 CL6002B19 1900309EA R/H CRACKED A COMAO OTHER O OTHER DEDESCENT 1 SO01983CA13433 7169 FLIGHT 5774 COPILOTS SIDE WINDOW CRACKED.REPLACED WINDOW. 2L72 4F RTA21EA 20030117001282003011700128SW 2003 1 17 HEEA083204 120030108A7712206062627003 TACH GENERATOR BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 N1 INDICATOR WENT TO ZERO IN FLIGHT. 1G71 3U H2SW 20030121001542003012100154SW 2003 1 21 HEEA083314 120030109A716023033400 AIR FILTER BELL 206 206L3 1182108SW PC AIR CLOGGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 AIR FILTER CLOGGED. SCRAPPED. 1G71 3U H2SW 20030317000312003031700031NM 2003 3 17 03FDEA00165 120030224A5310 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION FWD CARGO BAY ON SKIN STA 640 STR 28L TO 28R WL 149. CORROSION FWD CARGO BAY ON SKIN STA 640, STR 28L TO 28R, WL 149, FOUND TO BE OUT OF LIMITS. REPAIRED AREA PER SRM 53-30-1, 53-30-3, 51-30-2. 2L73 4F RTA3WE 20030319000292003031900029WP 2003 3 19 GTIA030054 120030208A3260 WARNING LIGHT DOUG DC9 DC982 3022082WP RT MLG ILLUMINATED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23823NK 48020 FLT 787 - RIGHT MAIN GEAR LIGHT REMAINED ON AFTER RETRACTION, PER QRH RECYCLED GEAR/UNSAFE LIGHT WENT OUT. INSPECTED PROX SENSOR AND ASSOCIATED MECH. NO DEFECTS NOTED. ACP PROXIMITY BOX SENSOR CHECK. ALL OPS NORMAL, REF UP AND LATCH SENSOR. (M) 2L72 4F A6WE 20030319000952003031900095NM 2003 3 19 TSAA0329025 120030207A29135718607 PUMP BOEING737 737230 1384401NM B HYD SYS INOPERATIVE A C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13818AL 22117 DURING TAKEOFF AT 100 KNOTS, THE NR 2 HYDRAULIC SYSTEM 'B' PUMP LIGHT CAME ON STEADY WITH NO OTHER ABNORMAL INDICATIONS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. THE HYDRAULIC PUMP WAS PUT ON MEL AS INOPERABLE AND THE AIRCRAFT COMPLETED THE SCHEDULED FLIGHT DAY. REPLACED THE NR 2 HYDRAULIC SYSTEM 'B' PUMP. OPS CHECK WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030325000092003032500009EU 2003 3 25 2003F00156 120030131A5753 STRUCTURE BRAERODH125 HS125700A 4230170EU TE FLAP CRACKED A UG8AK NONE O OTHER ININSP/MAINT 1 GL2348FB 257129 KPTK - FOUND RIGHT FLAP HAS A CRACK ON THE UPPER SURFACE AT RIB NR 20. REPAIRED CRACK IAW STRUCTURE REPAIR MANUAL, 57-50-22, PAGE 204, FIGURE 203. FLAP WAS RETURNED TO SERVICE. (M) 2L72 4F A3EU 20030326001022003032600102NM 2003 3 26 2003UALA00306 120030320A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29363UA 24532 STATION 335 AND 328, AT STR 21R, FUSELAGE SKIN IS DENTED AND CREASED. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED FUSELAGE DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030320001842003032000184NM 2003 3 20 AWXA200300295 120030301A5320694146006 STIFFENER BOEING737 737277 1384570NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW0 0 22647 LCQ - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON VERTICAL STIFFENER AT FORWARD BULKHEAD, AFT CARGO COMPARTMENT BILGE, BS 727, RBL 6. MAINTENANCE REMOVED CRACKED STIFFENER AT FORWARD BULKHEAD, AFT CARGO COMPARTMENT, BS 727, RBL 6; FABRICATED A NEW REPLACEMENT VERTICAL STIFFENER; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-5, PG. 6-10. 2L72 4F RTA16WE 20030324001122003032400112EU 2003 3 24 AWXA200300100 120030202A5270 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU CARGO DOOR DIRTY A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28619AW 527 LAS - AIR TURN BACK - FLT 0728 - AFTER TAKEOFF FROM LAS EN ROUTE FOR ORD IN GUSTY WIND CONDITIONS THE AFT CARGO DOOR LIGHT ILLUMINATED, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED AND CLEANED THE AFT CARGO DOOR LOCKING MECHANISM UNDER PANEL 826AR, CLEANED AFT CARGO DOOR PROXIMITY SENSOR AND TARGET, AND CHECKED SENSOR GAP, GAP WAS GOOD IAW AMM 52-32-00-501. 2L72 4F RTA28NM 20030325000582003032500058EU 2003 3 25 AWXA200300220 120030301A2450NSA837901B TERMINAL BLOCK AIRBUS320 A320232 3930326EU ZONE 900 - LAVATARCED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28640AW 448 CRACKLING SOUND AND SPARKS WERE SEEN COMING FROM BEHIND AFT GALLEY OVEN ALONG WITH A SMALL AMOUNT OF SMOKE. AFT GALLEY FEEDER "A" CIRCUIT BREAKER WAS FOUND POPPED IN COCKPIT. MAINTENANCE FOUND TERMINALS LOOSE AT BLOCK TERMINAL (7200VT), TERMINALS 2, 3, & 4, WERE FOUND BURNED. REPLACED TERMINALS 2, 3, & 4 IAW AMM 20-48-11, OPERATIONAL CHECK OF AFT GALLEY OVENS WAS GOOD. 2L72 4F RTA28NM 20040105000662004010500066NM 2004 1 5 2003UALA00946 120031210A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 TWO EACH SKIN DENTS WITHIN 22 INCHES OF E&E BAY DOOR, ONE BETWEEN STATION 303 & STATION 325 (STR35L). MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 51-00-01. 2L72 4F4 FRTA1NM E24NE 20031231000152003123100015NM 2003 12 31 TSAA0321195 120031202A2150 SENSOR BOEING737 73776N 13844CHNM COOLING FAN DIRTY A TSAAO OTHER J WARNING INDICATION CRCRUISE 1 WP13742AL 30830 DURING CRUISE, EQUIPMENT FAIL LIGHT ILLUMINATED, EQUIPMENT COOLING EXHAUST FAN INOPERATIVE IN NORMAL AND ALTERNATE POSITION. RETURNED TO SNA. DEFERRED EQUIPMENT COOLING FAN IAW MEL 21-27-3, AIRCRAFT RETURNED TO SERVICE. CLEANED EQUIPMENT COOLING EXHAUST FAN SENSOR SYSTEM IAW MM 21-27-03, SYSTEM OPS CHECK GOOD. MEL CLEARED, PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030917000222003091700022GL 2003 9 17 WI52003F00000 220030627A720054861 DIFFUSER CESSNA525 525 2076601CE WILINTFJ44 FJ441A GL ENGINE RUPTURED B WI5RO OTHER O OTHER NRNOT REPORTED 1 GL23111AM 5250113 UPON ENGINE DISSASSEMBLY THE DIFFUSER WAS FOUND TO EXHIBIT A SEPARATION OF THE AXIAL WELD OF THE PRESSURE CASE. THE FAILURE WAS INITIATED AS A FATIGUE CRACK WHICH RUPTURED AFTER REACHING A 3.00 INCH CRITICAL LENGTH. CAUSE IS ATTRIBUTED TO LOCAL MATERIAL THINNING IN THE WELD HEAT AFFECTED ZONE. TO ADD AN ANNEAL CYCLE AND TO REDUCE THE ALLOWABLE WELD MISMATCH IN THIS AREA. 1L72 4F4 FRTA1WI E3GL 20030917000492003091700049NE 2003 9 17 GUU2003F00007 220030620A72503044700 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GUUAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO1769547133655127 UE189 PS114408 DURING TAKEOFF JUST AFTER BRAKE RELEASE, AN EXPLOSION WAS HEARD IN THE LT ENGINE. ABORTED TAKEOFF. REMOVED LEFT ENGINE. DETERMINED POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFT ENGINE. ROUTED FAILED ENGINE FOR FURTHER ANALYSIS AND REPAIR. VENDOR DETERMINED TO BE 2ND STAGE POWER TURBINE BLADE FAILURE WITH SUBSTANTIAL DAMAGE TO HOT SECTION. 2L72 4T4 TRTA24CE E26NE 20030918000152003091800015NM 2003 9 18 03FDEA01514 120030911A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 N1550 CRACKED STRINGER CLIP, BS 720, STR. 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720, STR. 5R PER SRM 51-30-02. 2L73 4F RTA3WE 20030918000332003091800033NM 2003 9 18 GAIA03027SP 120030719A5311 FRAME BOEING727 7272J0 138407ENM BS 600 DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 600 HAS A DENT INTO THE RADIUS AT STRINGER 16R. CUT OUT DAMAGED AREA OF FRAME. FABRICATED NEW SECTION OF FRAME, MAT USED 7075-T6 .050 P/O NR 991420 DIM 12 INCH BY 5 INCH, AND FILLER MAT USED 7075-T6 .050 P/O NR 991420 DIM 2.5 INCH BY 1.5 INCH IAW SRM 51-40-3. INSTALLED IAW SRM 51-40-3. (M) 2L73 4F RTA3WE 20031009000652003100900065EA 2003 10 9 SWIA200312389 120030910A5297 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR INOPERATIVE A SWIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07908SW 7540 IN FLIGHT, RECEIVED GEAR DISAGREEMENT WARNING MSG, AND GEAR ICONS ON EDI. COMPLIED WITH QRH. DIVERTED TO TUL. REMOVED AND REPLACED CARGO DOOR WIRE HARNESS IAW CRJ MM 32-61-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20031010000072003101000007NM 2003 10 10 USAABB03156 120030905A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20040105000582004010500058NM 2004 1 5 QXEA200301565 120031212A73345905588 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM NR 2 ENGINE FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09350PH 488 SEA- ON FLIGHT 2154 NR 2 ENGINE FUEL PRESSURE CAUTION LIGHT ILLUMINATED, DESCENDING THROUGH 22,000 FEET. CHECKLIST DIRECTED US TO TURN AUX PUMP ON AND THE LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 2 ENGINE NR 2 FUEL PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040105001392004010500139NM 2004 1 5 SWAA032757 120031217A53206547978 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND CREASE BEAM SPLICE CORRODED AT BS 290, RBL 53. REMOVED AND REPLACED CREASE BEAM SPLICE SECTION PER SRM. 2L72 4F RTA16WE 20040311000142004031100014NM 2004 3 11 ASAA0310111 120030306A53206573746 FLOOR SUPPORT BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 1006-1016, BUTTOCK LINE 0 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20040114001122004011400112NM 2004 1 14 DL75K031047 120031123A2560P4010021SM BATTERY BOEING757 757232 1384965NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO276710E 30482 ONE EMERGENCY FLASHLIGHT INOP AT 1L. REPLACED BATTERY. 2L72 4F RTA2NM 20040121000462004012100046CE 2004 1 21 RU3A03017 120031027A282035C15G FLOAT LEAR 60 60LEAR 5170707CE FUEL VENT DAMAGED A RU3AO OTHER K FLUID LOSS CRCRUISE 1 SW1555 013 FUEL LEAK IN FLT AND ON GROUND AFTER LANDING, RT WING, LOWER SURFACE, 500 LBS FUEL LOST. REPLACED FAULTY FUEL VENT FLOAT ASSEMBLY. (M) 2L72 4F RTA10CE 20031204000222003120400022 2003 12 4 GTIA030869 420031029A2565 CABLE DOUG DC9 DC982 3022082WP GIRT BAR DETACHED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND R1 DOOR COVER RELEASE CABLE NOT ATTACHED TO GIRT BAR. ATTACHED CABLE TO GIRT BAR. (M) 2L72 4F A6WE 20031205000302003120500030NM 2003 12 5 DL73S030920 120031012A276165445616 ACTUATOR BOEING737 737247 138448DNM NR 3 SPOILER LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27377DL 23604 LOST A-SYSTEM HYD PRESSURE AND QTY WHILE PASSING THROUGH 18,500. FOUND NR 3 SPOILER ACTUATOR LEAKING. REPLACED SAME. 2L72 4F A16WE 20030326000652003032600065NE 2003 3 26 CA030205002 220030125A7230 COMPRESSOR BOEING767 767333 1385301NM PWA 4060 PW4060 52119NE ENGINE STALLED W A UNSCHED LANDING YE ENGINE STOPPAGE VIBRATION/BUFFET CRCRUISE 1 CA (CAN) DURING FLIGHT YYZ/LHR, ACFT DIVERTED TO YUL, DUE TO LT. ENGINE COMPRESSOR STALL. ENGINE SHUT DOWN. RESTARTED BUT HIGH VIBRATION, AND RISING EGT. SO ENGINE SHUT DOWN AGAIN.ACFT REMOVED FROM SERVICE TO CARRY OUT BOROSCOPE AND INVESTIGATION. 2L72 4F4 FRTA1NM E24NE 20030716000432003071600043SO 2003 7 16 SIMA200316001 120030605A2612902081 MODULE EMB 135 EMB135LR 3260305SO FIRE DETECTION INOPERATIVE A SIMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21738NR 145401 DURING FLIGHT CREW RECEIVED AN E2 FIRE WARNING. ENGINE WAS SHUTDOWN AND LIGHT EXTINGUISHED. AIRCRAFT WAS DIVERTED TO ALB. AFTER LANDING CREW RECEIVED ANOTHER FIRE WARNING. FIRE BOTTLE WAS FIRED AND AN EMERGENCY EVACUATIO AS DONE ON THE TAXIWAY. MAINTEANCE INSPECTED ENGINE FOR BLEED LEAKS AND INSPECTED FIRE LOOPS WITH NO DEFECTS FOUND, THE RIGHT ENGINE FIRE CONTROL BOX WAS REMOVED AND REPLACED IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. THE FIRE BOTTLE WAS ALSO REPLACED. (M) 2L72 4F RTT00011AT 20030721001222003072100122NM 2003 7 21 SWAA031486 120030702A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 12R AND 13R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030718000312003071800031GL 2003 7 18 UIEA200300023 220030615A7200 BLADE BOEING747 74747UF 1384949NM GE CF6 CF680C GL NR 1 ENGINE DAMAGED A UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15412MC 29255 706122 REJECTED TAKEOFF, RUNWAY ABORT, ON TAKEOFF 2 LOUD BANGS/SHAKES AT 100 KIAS. EICAS MESSAG 'BRAKE TEMP'. TAKEOFF ABORTED AT APPROXIMATELY 100 KIAS. BRAKE TEMP EXCEEDED 900 DEGREES, PER FIRE DEPARTMENT. EXTINGUISHER AGENT SPRAYED ON LT MLG DUE TO BRAKE FIRE. APPRXIMATELY 24 MILLION FOOT LBS OF BRAKE ENERGY. ENGINE BOROSCOPED AND FOUND 5TH & 6TH STAGE HPC DAMAGE ON NR 1 ENG BEYOND MM LIMITS. RAN NR 1 ENGINE IAW ATLAS AIR JC A71710/GTI AND AMM 71-00-02. LEAK AND OPS CHECK GOOD. ALL MLG TIRES REMAINED INFLATED. PERFORMED HIGH ENERGY STOP INSP IAW AMM 05-51-10. NO HEAT DAMAGE NOTED TO THE LANDING GEAR. BRAKES NR 1, NR 2 AND NR 5 REPLACED DUE TO HIGH TEMP IAW AMM 32-41-15. ALL LEAK AND OPS CHECKS GOOD. (M)2L74 4F4 FRT1384945 E23EA 20030422000732003042200073SW 2003 4 22 2003F00234 120030109A5270 SWITCH FRCHLDSA227 SA227DC 3377521SW CARGO DOOR DIRTY A BSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM05453LA DC852B SEA - FLT 6006 - CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHT CAME ON DURING CLIMB AT 9,000 FEET. CREW RETUREND TO STATION. DOOR CLOSING PROCEDURES OR DOOR HARD TO CLOSE. CLEANED AND LUBED CARGO DOOR CLICK CLACKS AND SWITCHES. DOOR CYCLED MULTIPLE TIMES WITH NO DEFECTS NOTED. TEST FLIGHT WAS THEN COMPLETED WITH NO DEFECTS NOTED. (M) 2L72 4T RTA18SW 20040223000382004022300038NE 2004 2 23 RAIA00312328 220031229A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RIGHT SHUTDOWN A RAIAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 CE03564HK 41081 75111 5500-BMI- RT ENGINE UNCOMMANDED SHUTDOWN ON TAKE OFF. MAINTENANCE PERFORMED ENGINE GROUND RUN AND COULD NOT DUPLICATE PROBLEM. 2L72 4T4 TRTA41NM E18NE 20040223000792004022300079EU 2004 2 23 001031 120030107A2770 GUST LOCK SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE RUDDER INOPERATIVE A UHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL17149SZ 340A149 470 DRG129985 ON 01/07/03, APPROX 1140(UTC), AIRCRAFT RETURNED TO GATE WHEN THE RUDDER GUST LOCK WOULD NOT DISENGAGE. THE CREW STATED THAT WHEN THE GUST LOCK WAS RELEASED, THE GUST LOCK WOULD ILLUMINATE ON THE CWP FOLLOWED BY THE RUDDER GUST LOCK CIRCUIT BREAKER TO OPEN (POP). 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040226000012004022600001WP 2004 2 26 ASAA0380377 120030421A5753591004131 VANE CAP DOUG DC9 DC982 3022082WP LT ENG COWL CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT OUTBOARD FLAP NR 3 VANE CAP CRACKED ON UPPER SURFACE. REPLACED VANE CAP PER SRM 51-30-1 AND 2. (M) 2L72 4F A6WE 20030828001092003082800109NM 2003 8 28 MWEA030320 120030821A5311991151465 FRAME DOUG MD88 MD88 3023688NM FUSELAGE CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FUSELAGE FRAME AT STATION 148 IS CHAFED JUST AFT OF FIRST OFFICER'S ESCAPE ROPE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030829000572003082900057WP 2003 8 29 DHL2003801083 120030710A3231 MECHANISM DOUG DC8 DC873F 302199FWP RT GEAR DOOR LACK OF LUBE A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01801DH 46033 AFTER LANDING GEAR RETRACTION, DOOR NOT LATCHED AND RIGHT DOOR UNSAFE LIGHT ILLUMINATED 3 TIMES AND THEN EXTINGUISHED. VISUALLY INSPECTED RIGHT GEAR DOOR UP LATCH MECHANISM, NO DEFECTS NOTED. LUBED MECHANISM, PERFORMED TEST OF UP LATCH AS PER M/M 32-31-4, CHECKED GOOD EACH TIME. 2L74 4F RT4A25 20030729000292003072900029EA 2003 7 29 03196632 120030715A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27632BR 7268 DURING MAINTENANCE INSPECTION, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030806000792003080600079EU 2003 8 6 AWXA200300806 120030628A5411D5463046220100 PROFILE AIRBUS320 A320231 3930325EU ZONE 480 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON INBOARD UPPER ANGLE (PROFILE) AT ATTACH SCREW HOLE JUST AFT OF RIB 7 ON THE NR 2 PYLON. MAINTENANCE CUT OUT CRACKED AREA OF ANGLE JUST AFT OF RIB 7 ON THE NR 2 PYLON; FABRICATED A REPAIR SPLICE AND FILLER; INSTALLED REPAIR PART IAW A320 SRM 54-52-12 PG 215-217, & 220, FIG 203. 2L72 4F RTA28NM 20030828001682003082800168NM 2003 8 28 USAABB03122 120030725A4960 CONNECTOR BOEING757 757225 1384959NM APU BAY LOOSE A USAAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA19603AU 22198 CLT - FLT 1892 - EN ROUTE SXM TO CLT, CREW RECEIVED AN EICAS MESSAGE, LT GEN DRIVE DISCONNECTED. LT GEN DRIVE LIGHT ALSO ILLUM. THEN ON APPR TO CLT, APU GENERATOR KICKED OFFLINE AND WOULD NOT RESET. FLT LANDED AT CLT WITHOUT INCIDENT. MX ACCOM TROUBLESHOOTING PER FIM 24-20-00 AND FOUND LT IDG FILTER INDICATOR POPPED. CHECKED OIL FILTER. NO DEFECTS NOTED. INSTALLED NEW FILTER AND RESET INDICATOR. OPERATIONAL TEST NORMAL. AS FOR THE APU, MX FOUND THE APU MAIN CONTROL CONNECTOR NOT SECURED. INSPECTED AND SECURED CONNECTOR. TESTED NORMAL PER 24-20-00. FOUND APU PNEUMATIC FLEX DUCT AND CLAMP LEAKING. REPLACED DUCT ASSEMBLY, P/N 14J81-2, AND TIGHTENED CLAMP. OPERATIONAL TEST AND LEAK CHECK NORMAL. (M) 2L72 4F RTA2NM 20030903000982003090300098WP 2003 9 3 MEX2003285 120030703A2612892809040001 AMPLIFIER DOUG DC9 DC983 3022083WP NR 2 FAULTY A ASMFK NONE N FALSE WARNING ININSP/MAINT 1 SW23583MD 49659 DURING TRANSIT CHECK DETECTED THAT DURING TEST ENGINE FIRE ALARM SYSTEM NR 2 NOT CANCELL AURA WARNING. DURING REVISION BREAKER AND AMPLIFIER A2-6 WERE WITH DAMAGES. THE FIRE ENGINE NR 2 AMPLIFIER WAS SWAPPED WITH APU AMPLIFIER IAW MM 26-10-01, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030903002262003090300226NM 2003 9 3 QXEA200300974 120030814A2120 ODOR BOMBDRDHC8 DHC8401 1390041NM CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09407QX 4049 SEA- ON FLIGHT 2363 STRONG ELECTRICAL BURNING SMELL. RAN NR 1 AND NR 2 ENGINES BLEED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031208000642003120800064EA 2003 12 8 03297625 120031024A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING INSPECTION A DENT WITH A HOLE WAS DISCOVERED AT FS 621.00 RBL 9.00. 2L72 4F RTA21EA 20040121000512004012100051WP 2004 1 21 ASAA0380819 120031203A5210 SKIN DOUG DC9 DC983 3022083WP PAX DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 PREFLT CHECK, FORWARD PAX DOOR SKIN IS DENTED CAUSING DOOR TO BE HARD TO OPEN. REPAIRED DENT PER SRM 52-05 AND 51-10-03. DOOR THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040122000992004012200099EA 2004 1 22 ASOA03644 120031212A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11905EV 7632 DURING A HANGAR INSPECTION IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122001252004012200125WP 2004 1 22 GTIA030957 120031129A3260 PROXIMITY SENSOR DOUG DC9 DC981 3022081WP MLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23811NK 48017 FLL - FLT 268 - AFTER TAKEOFF, RIGHT MAIN GEAR RED LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON WTIH GEAR HANDLE UP-FOLLOWED QRH PROCEDURE AFTER WHICH GEAR LIGHTS INDICATED NORMAL, CONTINUED TO ACY. BITE CHECK OF PSEU SENSORS SHOWS NO FAULTS AT THIS TIME. CHECKED GEAR DOOR AND GEAR UP AND DOOR LATCH PROX SENSORS FOR CORRECT ADJUSTMENT AND SECURITY. CLEANED CONNECTORS ON BOTH SENSORS. CLEANED SENSOR AND TARGET AREA, PERFORMED STANDARD ELECTICAL T/S OF SENSORS PER ACCEPTED PCTS. NO DEFECTS NOTED AT THIS TIME. (M) 2L72 4F A6WE 20040127002122004012700212WP 2004 1 27 ASAA0380785 120031119A5753 ATTACH FITTING DOUG DC9 DC983 3022083WP TE FLAPS GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - FOUND DURING 15K CHECK, RIGHT WING FLEX JOINT OUTBOARD FLAP ATTACHMENT FITTING GOUGED ON EDGE. REPAIRED IAW EA. (M) 2L72 4F RTA6WE 20031014001022003101400102NM 2003 10 14 SWAA032141 120030922A2751656385112 MOTOR BOEING737 7373A4 1384585NM FLAP DRIVE FAULTY A SWAAB EMER. DESCENT FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 SW29675AA 23253 DECLARED EMERGENCY, T/E FLAPS WOULD NOT EXTEND PASS 1 PERCENT. REMOVED AND REPLACED FLAP DRIVE MOTOR (HYD AND ELECT) AND FLAP DRIVE UNIT PER MM. 2L72 4F RTA16WE 20031020003022003102000302NE 2003 10 20 2003UALA00728 220031001A7230 COMPRESSOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 ENGINE STALLED A UALAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS UKUNKNOWN 1 WP29656UA 25394 CANCELLED DUE TO NR 2 ENGINE COMPRESSOR STALL AT FL210. ENGINE SURGED ABOVE 1.25 EPR AND WAS REMOVED. SURGE CHECKS SHOWED NO IRREGULARITIES AND ENGINE PASSED TEST-21. PILOT REPORT STATED THAT AIRCRAFT HAD WAKE TURBULENCE DURING CLIMB. 2L72 4F4 FRTA1NM E24NE 20031212000062003121200006NM 2003 12 12 S03853091 120031105A5312 BULKHEAD BOEING737 737800* NM CFMINTCFM56 CFM567B26US NE FUSELAGE CANNING W SAJFO OTHER O OTHER TXTAXI/GRND HDL 1 WP03 30173 B-18612 THE DATUM A/C HAD AN OIL CAN CONDITION ON BS 1016 PRESSURE BULKHEAD. THE OIL CAN CONDITION WAS REPAIRED USING THE 738 SRM 53-80-08 REPAIR ON 4 NOV 10/02. THE ABOVE REPAIR BOEING CONSIDER IT WAS STRUCTURALLY ACCEPTABLE AS A TEMPORARY REPAIR, FOR A PERIOD OF 24 MONTHS FROM THE TIME OF INSTALL AND BOEING PROVIDED A PERMANENT REPAIR PLAN BY CHI-TPE-03-00157H FOR THE SUBJECT OIL CAN. CHI HAS ISSUED EO 738-53-00-0019 AND INCORPORATED FOR THE SUBJECT ITEM AS A PERMANENT REPAIR AND GOT APPROVAL DATA 8110-3 FORM. PER EO 738-53-00-0019 REPAIR. 2L72 4F4 FRTA16WE E00055EN 20030919001212003091900121EU 2003 9 19 XNOA01143 120030818A2611 WARNING LIGHT AIRBUS300 A300B4203 3930306EU CARGO SMOKE FALSE INDICATIONA XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23372PC 196 LOOP A MID 1 MAIN CARGO COMPT SMOKE DETECTOR LIGHT CAME ON DURING TAXI. RERACKED SMOKE DETECTOR BOX AND RETESTED MID 1 LOOPS A AND B. OPS CHECK NORMAL. LOOP LIGHT STAYS OUT. 2L72 4F RTA35EU 20030923000162003092300016EU 2003 9 23 AWXA200300969 120030821A3230508010250952018 SEAL AIRBUS320 A320232 3930326EU SELECTOR VALVE TORN A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28664AW 1621 DURING CLIMB OUT OF LAS EN ROUTE FOR BWI RECEIVED ECAM WARNING FOR GREEN HYD SYS LOW PRESSURE. TURNED OFF GREEN HYDRAULIC PUMP AND TURNED ON POWER TRANSFER UNIT, THEN RECEIVED ECAM MESSAGE FOR LOW GREEN HYDRAULIC QUANTITY WHICH WAS FOLLOWED BY A YELLOW HYDRAULIC OVERHEAT MESSAGE. TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED GREEN HYDRAULIC PUMP CASE DRAIN FILTER FOR CONTAMINATION, FILTER WAS CLEAN. PRESSURIZED HYDRAULIC SYSTEM AND FOUND FLUID LEAKING FROM LANDING GEAR DOOR SELECTOR VALVE (41GA). REMOVED VALVE AND FOUND THE SEAL DAMAGED WHERE VALVE MOUNTS TO MANIFOLD, REPLACED 4 EACH SEALS AND REINSTALLED SELECTOR VALVE IAW AMM 32-31-34-400-001, LEAK AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030924000682003092400068EU 2003 9 24 197050103 120030501A24345243212137 DRIVE SHAFT PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE NR 2 GEN SHEARED E S4WAO OTHER J WARNING INDICATION CRCRUISE 1 WP07613NA3756 197 NR 2 GENERATOR DROPPED OFF LINE. AFTER TROUBLESHOOTING PROBLEM, FOUND NR 2 GENERATOR DRIVE SHAFT SHEARED. 1L71 3T4 TRTA78EU E26NE 20030925000312003092500031NM 2003 9 25 USAA030153 120030819A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US 23315 PIT - FOUND SKIN CRACKED 2.4 INCH, AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER SRM 53-60-01 FIG 207. (M) 2L72 4F RTA16WE 20040206000702004020600070WP 2004 2 6 ASAA0380751 120031118A533059360047 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND SKIN CORROSION. INSTALLED REPAIR DOUBLER PER SRM. (M) 2L72 4F RTA6WE 20040210000952004021000095EU 2004 2 10 USAA030291 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED 2 SQUARE INCHES, FRAME 60 PLUS 10 INCHES RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040210001022004021000102EU 2004 2 10 USAA030273 120031202A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED 1 SQUARE INCH BY .25 INCH DEEP, FRAME 44 SEAT TRACK LBL 17.75. REPLACED 71 INCH SECTION OF SEAT TRACK WITH SPLICE JOINT PER SRM 53-31-15 FIG 201 AND EA 94997. (M) 2L72 4F RTA46NM 20030904001132003090400113EA 2003 9 4 QXEA200301037 120030825A2140GG43120223 SPRAYER CNDAIRCL600 CL6002C10 1390015EA A/C SYSTEM MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09602QX 10010 PDX- ON FLIGHT 2520 SLIGHT BURNT OIL SMELL WHEN TURNING UP HEAT FROM AIR CONDITIONING PACKS. REMOVED AND REPLACED COCKPIT RAM AIR WATER SPRAYER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030903001872003090300187WP 2003 9 3 AALA20030732 120030709A3350 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21471AA 49601 DFW - EMERGENCY LIGHT IN CEILING AT ROWS 8, 9, 10, 11 ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030904001222003090400122EA 2003 9 4 COMA0360395 120030830A783022850100234 THRUST PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE THRUST REVERSER BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01716CA 7250 807248 RIGHT THRUST REVERSER SPRING BOX ASSEMBLY AT 4 O'CLOCK POSITION WAS FOUND BROKEN. REMOVED BROKEN SPRING BOX ASSEMBLY AND INSTALLED A SERVICEABLE ONE. 2L72 4F4 FRTA21EA E15NE 20030904001832003090400183WP 2003 9 4 AALA20030724 120030705A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21439AA 49457 DFW - FORWARD GALLEY CEILING EMERGENCY LIGHT DIM. REMOVED AND REPLACED BATTERY PACK R5-23 IN FORWARD DROP DOWN CEILING PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030813000852003081300085NM 2003 8 13 2003UALA00484 120030608A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29663UA 27160 LEFT MOST FWD EMERGENCY EEL STRIP INOPERATIVE. SECURED EEL STRIP, OPS CHECK OK. 2L72 4F4 FRTA1NM E24NE 20030821000262003082100026NM 2003 8 21 03FDEA00963 120030622A5510ALC8100 BARREL NUT DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STAB LEFT UPPER AFT PLANK BARREL NUT BORE NR 31L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LEFT HORIZONTAL STAB UPPER AFT PLANK BARREL NUT NR 31L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030822001582003082200158NM 2003 8 22 UPS03441114 120030717A5312141U11075 PRESSURE PANEL BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C NLG W/W BOX STRUCTURE LT BS 300 VERTICAL BEAM WEB FOUND APPROX .125 INCH CRACK AT LOWER STAND OFF HOLE BETWEEN 1ST AND 2ND STIFFENER CLIP (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20030825001782003082500178NM 2003 8 25 03FDEA01252 120030810A2613 CONTROL PANEL BOEING727 727200 138407ENM COCKPIT MALFUNCTIONED A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 SO25208FE 22930 IN CRZ FLT LOWER AFT BODY OVERHEAT LIGHT CAME ON BLINKING AT VARIOUS RATES. ACCOMPLISHED QRH L.A.B. OVERHEAT CHECKLIST TO INCLUDE CLOSING NR 3 ENG. BLEED. BLINKING SLOWED THEN STOPPED. SYSTEM TESTED GOOD. CONTINUED IN CRUISE WITH NR 3 BLEED CLOSED. R7R OVERHEAT DETECTION PANEL 69-67178-1, WITH CANNED SERVICABLE UNIT FROM A/C 210FE. S/N'S OFF D00176 ON D00172. REMOVED AND REPLACED OVERHEAT DETECTION ACC. UNIT M113 WITH CANNED SERVICABLE UNIT FROM A/C 210FE. SUSPECT BAD LOWER AFT BODY HEAT LITE ASSY. STOPPED. REMOVED AND REPLACED UNITS ABOVE FOR PRECAUTION. SRL 670502 TAG 901161 ON MFG 65-24920-1 SRL 040 TAG 901151 2L73 4F RTA3WE 20030826000422003082600042NM 2003 8 26 03FDEA01194 120030730A5720ANB7445 SHIM DOUG MD11 MD11 3023602NM LT WING OUT OF POSITION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT WING ROOT- UPPER SURFACE STRINGER NR 3 SHIM FOUND MIGRATED 0.7 INCH DOWN. PREVIOUS RECORD IS 0.5 INCH. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION. 2L73 4F RTA22WE 20030826001502003082600150SO 2003 8 26 SIMA200321006 120030724A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21713AE 145249 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT A 16 INCH BY 21 INCH SECTION OF DAMAGED FORWARD DIGITAL. PREPARED A SECTION OF DIGITAL MATERIAL. FABRICATED SHIM AND TWO DOUBLERS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/1158 AND EMBRAER 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-10 FIG 203. (M) 2L72 4F RTT00011AT 20030827001112003082700111NM 2003 8 27 CALA0300415 120030725A555369720396 BUSHING BOEING737 737524 1384721NM VERTICAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT RT I/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED IAW SOPM 20-50-03. 2L72 4F RTA16WE 20030910002052003091000205EU 2003 9 10 MALA030386 120030820A3040HC921H0467000 PRINTED CKT BOAR BAC 146 AVRO146RJ85A1500097EU COCKPIT FAULTY A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15532XJ E2366 STRONG BURNING ODOR NOTED IN COCKPIT AND FIRST CLASS SECTION. MAINTENANCE UPON INSPECTION FOUND PCB FOR WINDSHIELD DEICE CONTROL 1HL23 TO BE BURNED. REMOVED AND REPLACED PCB AS REQURIED PN HC921H0467-000. PERFORMED OPS CHECKS ALL GOOD AT THIS TIME. INSPECTED, CLEANED SURROUNDING AREA AND WIRING NO DEFECT NOTED ALL CHECKS GOOD. 2H74 4F RTA49EU 20030911000212003091100021NM 2003 9 11 2003UALA00542 120030707A2780 STRUCTURE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29518UA 24871 AIRCRAFT EXPERIENCED LEADING EDGE SLAT PROBLEM. THE NR 6 SLAT TRAILING EDGE WEDGE BROKE APART. A SECTION OF THE TRAILING EDGE WEDGE SEPARATED FROM THE SLAT. THE SUSPECT CAUSE OF DAMAGE WAS CORROSION OF THE ALUMINUM HONEYCOMB IN THE TRAILING EDGE WEDGE DUE TO MOISTURE INGRESSION. INTENSIFIED INSPECTIONS WILL DETECT DELAMINATIONS PRIOR TO SEPARATON FAILURES. 2L72 4F4 FRTA2NM E17NE 20030911001212003091100121WP 2003 9 11 DHL2003873572 120030706A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FUSELAGE NOSE SECTION EXTERNAL AC POWER RECEPTECALE COMPARTMENT SKIN CRACKED 0.250 AROUND STA -39.000 BETWEEN L-31R AND L-33R. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030632, ED-3440. PERFORMED NDT INSPECTION IAW DC8 SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL REPAIR DOUBLER AND A FILLER. CLEANED, TREATED AND PRIMED THE REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER ON EXTERNAL AC POWER RECEPTACLE COMPARTMENT SKIN (AROUND STA.-39.000 BETWEEN L-31R AND L-33R) USING NEW FASTENERS. 2L74 4F RT4A25 20030929000582003092900058CE 2003 9 29 ENHA200320806 120030904A2750262228112 BELLCRANK CESSNA208 208B 2073701CE TE FLAP FAILED E ENHAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03454SF 208B0797 FLAP BELLCRANK INSPECTION FOUND MISSING WELDS AT MATING PORTIONS OF THE ASSEMBLY. BELLCRANK COULD BE SUBJECT TO CATASTROPHIC FAILURE. INSPECTION PROMPTED BY AL FSDO LETTER DATED 8/15/03. SUBJECT BELLCRANK REPLACED WITH P/N 2622311-7 OF NEW DESIGN. 1H71 3T A37CE 20030729000182003072900018EA 2003 7 29 03198653 120030717A2611 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA SMOKE DETECTOR CONTAMINATED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27653BR 7438 DURING CLIMB THE CREW REPORTED SMOKE IN THE CABIN. CREW DID NOT DECLARE EMERGENCY FLIGHT LANDED WITHOUT INCIDENT. PASSENGERS DEPLANED THROUGH NORMAL DOOR. MAINTENANCE PERSONNEL CLEANED AND RECONECTED THE LAV SMOKE DETECTOR CANNON PLUG. IT WAS DETERMINED SMOKE WAS CAUSED BY RESIDUAL OIL FROM PREVIOUS APU OIL LEAK. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030729001192003072900119EA 2003 7 29 SWIA200312192 120030712A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07431SW 7536 FLIGHT SPOILERS FAULT MESSAGE. INSTALLED SERVICEABLE INBOARD AND OUTBOARD FLIGHT SPOILER PCU'S ON LEFT FLIGHT SPOILER IAW CRJ MM 27-62-01. OPS AND LEAK CHECKS GOOD. OB - PN OFF/ON 27000-7 SN OFF 5147. IB-PN OFF/ON 27000-7 SN OFF 3313. 2L72 4F4 FRTA21EA E15NE 20030929000702003092900070NM 2003 9 29 QXEA200301055 120030831A33501161361 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 RT FORWARD EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS TEST. REMOVED AND REPLACED RIGHT FORWARD EMERGENCY EXIT DOOR BETA LIGHT. 2H72 4T RTA13NM 20030930000752003093000075NM 2003 9 30 AUC2003F00000 120030730A3244 TIRE LKHEEDP3A P3A 5260103NM ALLSN T56 T56A10 03004GL MLG FAILED B AUCRO OTHER O OTHER NRNOT REPORTED 1 WP25927AU14 151369 WHEEL ASSEMBLY WITH RECAPPED TIRES INSTALLED ON AIRCRAFT. THESE TIRES INSTALLED FOR A TOTAL OF 7 DAYS AND OPERATED FOR A TOTAL OF 14 FLIGHT HOURS. UPON TAKEOFF, ONE OF THE NOSE WHEELS LOST THE CENTER PORTION OF THE TIRE TREAD. THE FLIGHT CREW EXPERIENCED A VIBRATION ON TAKEOFF AND ELECTED TO RETURN TO BASE, MADE A SAFE LANDING. THE PAIR OF TIRES WERE CHANGED, INSPECTED THE AIRCRAFT AND NO DAMAGE WAS FOUND. WHEN THE TIRES RETURN TO MAINTENANCE, BOTH TIRES WERE CHECKED FOR PROPER INFLATION, NO LOSE OF PRESSURE FOUND. 2L74 4T4 TRTA32NM E282 20031001000102003100100010NM 2003 10 1 QXEA200301078 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 11 SEAT TRACK HAS CORROSION BELOW THREE SEAT RAIL LUGS BETWEEN 9 AND 11 INCHES AFT OF STATION X445. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031002000072003100200007NM 2003 10 2 USAA030171 120030821A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU48878 23228 FOUND SKIN CRACKED 1 INCH, AFT OF FS 727D BELOW S23R. INSTALLED DOUBLER PER EA 94615. (M) 2L72 4F RTA16WE 20030908002612003090800261CE 2003 9 8 AMWA23 120030818A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07178YV UE178 WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20030908002712003090800271 2003 9 8 SWIA200312362 420030821A3497 WIRE EMB 120 EMB120ER 3260203SO STALL WARNING BROKEN A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07284YV 120284 FIRST OFFICER STALL TEST HAS A PUSHER BUT NO SHAKER. REPAIRED BROKEN WIRE TO F/O'S SHAKER. OPS CHECK GOOD. 2L72 4T RTA31SO 20031003000872003100300087CE 2003 10 3 GLBA2003131 120030914A2750 FLAP BEECH 1900 1900D 1154162CE WINGS INOPERATIVE A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03245GL UE245 FLAPS WOULD NOT RETRACT AFTER T/O, ADJUSTED LT SPLIT FLAP SWITCH OPS CK GOOD. 2L72 4T RTA24CE 20031006001542003100600154 2003 10 6 SWAA032020 420030909A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031007000932003100700093NM 2003 10 7 SWAA031991 120030904A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767 + 3, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031006000052003100600005EA 2003 10 6 COMA0360409 120030911A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01471CA 7655 FLIGHT 5720 CONFIG SPOILERS MESSAGE DURING T/O. DEFERRED MAINTENANCE PER MEL ON RT INBOARD FLIGHT SPOILER PCU. 2L72 4F RTA21EA 20031022000262003102200026EU 2003 10 22 AWXA200301076 120030920A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU SEAT ROW 9 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE AT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031103000282003110300028NM 2003 11 3 DL73S030885 120030929A3320A313101 SWITCH BOEING737 737232 1384475NM FWD F/A PANEL BROKEN A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27304DL 23076 ELECTRICAL SMELL COMING FROM FWD FLIGHT ATTENDANT INTERPHONECOMM PANEL. FOUND CABIN SIDEWALL LIGHT SWITCH AT FWD F/A PANEL BROKEN AND SHORTING. REPLACED SWITCH, CHECKS OK. 2L72 4F RTA16WE 20031103000532003110300053NM 2003 11 3 03FDEA01604 120030921A5753ARC050213 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 SNRM N0453: LT OB FLAP IB HINGE (A/C SIDE); IB AND OB UPPER ACTUATOR ATTACH LUG FOUND CORRODED AT BORES AND SPOT FACES. SNRM N0453 : LT OUTBD FLAP IB HINGE (A/C SIDE) IB AND OB UPPER ACTUATOR ATTACH LUG FOUND CORRODED AT BORES AND SPOT FACES CORRODED AREA REPAIR CARRIED OUT IAW EA NR 1-5750-71757 : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. LT OB FLAP IB HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040324000082004032400008WP 2004 3 24 ASAA0380714 120031103A53219936639501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD IS DELAMINATED AT FS 887-947. REPLACED FLOOR PANEL PER SRM 53-24. (M) 2L72 4F RTA6WE 20040407000422004040700042NM 2004 4 7 TSAA0353206 120031115A53306520722 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ENLARGED TRIM BY .040 INCH INSURANCE CUT. HFEC INSPECTED ALL FASTENER HOLES. FABRICATED A .071 INCH STRUCTURAL FILLER, .063 INCH INNER PLATE, .063 INCH PLATE, .125 OUTER PLATE AND .0180 INCH THICK FILLER FROM 2024-T3 CLAD SHEET AS SHOWN IN FIGURE 1. ALODINED AND TWO COATS BMS 10-79, TYPE III PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES OF THE REPAIR. REPAIR COMPLETED IAW ECO 3396. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040614002002004061400200NM 2004 6 14 RYN2004F00027 120030916A291065178213 MODULE BOEING727 727222 1384073NM PWA JT9 JT9D* NE A-HYD SYSTEM FAILED A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE077640U 19913 AFTER TAKEOFF, RETRACTED FLAPS AND RECEIVED AN A-HYDRAULIC LOW PRESSURE INDICATION AT FLIGHT ENGINEER PANEL AND PILOTS FWD PANEL. FOLLOWED HYDRAULIC LOSS PROCEDURES. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYDRAULIC MOD PACK. OPERATIONAL CHECK NORMAL. 2L73 4F4 F A3WE E20EA 20040713001702004071300170NM 2004 7 13 MEX2003559 120031223A7830S148 SWITCH DOUG MD88 MD88 3023688NM NR 1 ENGINE FAILED A ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23158PL 49761 FLT 222 - MEX-CUU - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE THAT THE AMBER LIGHT OF 'RT REVERSE UNLOCK' AND THE BLUE LIGHT OF 'LT REVERSE UNLOCK' CAME ON. AT GATE, BOTH REVERSE AND MICROSWITCH MECHANISM WERE LUBRICATED, TESTS OK. DURING OVERNIGHT SERVICE AT MEX STATION THE LEFT REVERSE MICROSWITCH S1-48 WAS REPLACED, THE CIRCUIT WAS VERIFIED AND THE SYSTEM WAS TESTED IAW WDM 78-31-00. (M) 2L72 4F RTA6WE 20040913001412004091300141 2004 9 13 0704015 420030916A2360610R9A STATIC WICK BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE HORIZONTAL STAB CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 STATIC WICK BASE CORRODED ON RT HORIZ STAB. 2L72 4F4 F A16WE E2EA 20030819000332003081900033NM 2003 8 19 AMTA200300933 120030714A2613 WARNING LIGHT BOEING757 75733N 1384931NM LT STRUT FALSE ACTIVATIONA AMTAK NONE N FALSE WARNING ININSP/MAINT 1 GL11557TZ 32591 LT STRUT OVERHEAT DET 1, STATUS MSG ILLUMINATED. PERFORMED BITE CHECK PER FIM 26-12-00 FIG 103. VISUALLY INSPECTED NR 1 ENGINE PYLON AREA, NO DEFECTS FOUND. RAN ENGINES 15 MINS, NO OVERHEAT DETECTED. (M) 2L72 4F RTA2NM 20030819000262003081900026WP 2003 8 19 AALA20030646 120030516A5347597663503 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21965TW 53615 FOUND AFT CARGO, LEFT TIE DOWN TRACK CORRODED FROM STATION 1220-1309. REMOVED AND REPLACD TRACK. (M) 2L72 4F RTA6WE 20030401001232003040100123WP 2003 4 1 DHL2003804515 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER LOWER PART WITH 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030403000972003040300097NE 2003 4 3 DJFA200300001 220030105A7200 BEARING BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE NR 1 ENGINE FAILED E DJFAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA23731TA RK273 PCEJA0316 AIRCRAFT IN CRUISE AT 410 FT LOST OIL PRESSURE ON NR 1 ENGINE AND ENGINE SHUTDOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT DESCENDED AND LANDED AT SRQ. PRELIMINARY REPORT INDICATES BEARING FAILURE. 2H72 4F4 FRTA16SW E25EA 20030407000202003040700020WP 2003 4 7 ASAA0380075 120030113A5230593607017 PLATE DOUG DC9 DC983 3022083WP CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, MID CARGO BAY DOOR LOWER SCUFF PLATE IS CRACKED. CUT OUT AND REPLACED DAMAGED AREA PER SRM 53-01. (M) 2L72 4F RTA6WE 20030408000432003040800043NM 2003 4 8 USAA030019 120030214A5330 SKIN BOEING737 7373B7 1384580NM FS 727D CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US49657 22959 CLT - FOUND UNSCHEDULED MAINTENANCE, SKIN CRACKED 2.15 INCH, STATION 727D PLUS 19 INCHES ABOVE S23R. INSTALLED DOUBLER AND TRIPLER PER EA 87064. (M) 2L72 4F RTA16WE 20030630000012003063000001EA 2003 6 30 COMA0370018 120030614A7830M12883 RELAY CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01368CA 10075 FLIGHT 5743 LEFT THRUST REVERSER UNSAFE MESSAGE DURING FLIGHT. REPLACED RELAYS K27 AND K29. 2L72 4F RTA21EA 20030416000222003041600022SO 2003 4 16 SWIA200311681 120030107A27523430001001 ACTUATOR EMB 120 EMB120ER 3260203SO LT TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07270YV6988 6988 120270 RIGHT AFTER STARTING BOTH ENGINES, THE LEFT INBOARD FLAP EXTENDED ALL THE WAY DOWN. THE FLAP LIGHT ON MAP AND FLAP ASYMMETRY LIGHT ILLUMINATED. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20030416003722003041600372WP 2003 4 16 UPS03840020 120030107A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C-2 SEAT TRACK -D- FROM STA 1020 TO 1060 CORRODED ON UNDERSIDE AT CLIP NUTS. REMOVED DAMAGED TRACK, REPLACED WITH NEW TRACK AND UPS SPLICES. 2L74 4F RT4A25 20030417000972003041700097NE 2003 4 17 QXEA0300230 220030203A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX2576 10022 GEE965289 NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO BLADES MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THE MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20040212001232004021200123NE 2004 2 12 KBM2003F00110 220031130A73200164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19115SH147 3141 ENGINE FUEL CONTROL UNIT P2 AIR CAVITY IS LEAKING FUEL. INSTALLED SERVICEABLE FUEL CONTROL UNIT. 1G71 3U3 U H9EU E19EU 20031105000402003110500040WP 2003 11 5 ABXA030402 120031009A5320D0489841 WEB DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 CUSP WEB CRACKED AT RIGHT BUTT LINE 54 BETWEEN FS 945 - 965. REPAIRED CRACK IAW DC-9 53-01. 2L72 4F A6WE 20031106000462003110600046SO 2003 11 6 C2XA03SH403 120031022A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714542 145547 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED AT FRAME 52. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20030917000562003091700056CE 2003 9 17 DXTA200300111 120030910A3230 TORQUE LINK CESSNA750 750 2076810CE MLG WORN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07986QS 7500086 AFTER TAKE OFF FROM SWF FOR PHL, LANGING GEAR WOULD NOT RETRACT, ACCOMPLISHED AIT TURN BACK TO SWF. - INSPECTED GEAR & FOUND THE NOSE GEAR TORQUE LINK CAM BOLT HOLE ELONGATED & WORN. REPLACE NOSE GEAR TORQUE LINK CAM WITH NEW PER THE CE 750 MM CHAPTER 32-20-02, PERFORMED GEAR RETRACTION OPS CHECKED GOOD. 2L72 4J RTT00007WI 20031009000712003100900071EA 2003 10 9 03259631 120030916A33501317 BULB CNDAIRCL600 CL600* EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27631BR 7261 DURING INSPECTION THE FIRST OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGEMCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031007000362003100700036 2003 10 7 AALA20030810 420030714A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21676AN 29426 TUL - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRINGS NEEDED REPLACING. REPLACED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031119000622003111900062WP 2003 11 19 0301919754 120031010A2170 HOSE DOUG DC9 DC941 302207NWP LT WATER SEP SEPARATED A NWAAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL01754NW 47178 ON DEPARTURE CLIMBOUT AT 13,000 FT, CREW HEARD A MUFFLED BOOM AND CABIN STARTED TO CLIMB AT 2000 FPM. FLIGHT CREW WAS UNABLE TO CONTROL CABIN PRESSURIZATION IN AUTO OR MANUAL. MASKS DID NOT DEPLOY AND COM PROCEDURES WERE COMPLIED WITH. FLIGHT DIVERTED TO DTW AND LANDED UNEVENTFULLY. MAINTENANCE FOUND A DUCT HOSE JUST AFT OF THE LEFT WATER SEPARATOR BLOWN OFF. THE HOSE AND CLAMP WERE RE-ATTACHED AND LEAK CHECKED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20031120001232003112000123NM 2003 11 20 AWXA200301449 120031111A532065548627 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK 2 EACH 1 INCH CRACKS WERE FOUND IN INTERCOSTAL BETWEEN BS 1016 TO BS 1040, BL 0 TO RBL 15, WL 208.1. MAINTENANCE REMOVED CRACKED INTERCOSTAL BETWEEN BS 1016 TO BS 1040, BL 0 TO RBL 15; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-54862; INSTALLED REPAIR PART IAW SRM 51-40-02 FIG 3, 8 & 12. 2L72 4F RTA16WE 20031121000222003112100022 2003 11 21 03315311 420031111A3420172934001 RELAY JETAIRJETSTMJETSTM4101 1500501EU AUTOPILOT INOPERATIVE A VTZAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA27311UE 41029 DURING APPROACH CREW REPORTED THE AUTOPILOT PORPOSING TOWARDS THE END OF THE APPROACH. FLIGHT LANDED UNEVENTFULLY. THE FAULT WAS TRACED TO THE AHRU 1FC8 RELAY AND IT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031124000732003112400073NM 2003 11 24 CALA0300647 120031114A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND STRAP BROKEN ON BOTTOM OF BEAMS AT STA 312-328, RBL 42. THE STRAP WAS REPAIRED IAW SRM 53-10-51. 2L72 4F RTA16WE 20040113002272004011300227NM 2004 1 13 QXEA200301488 120031124A5210 FITTING DHAV DHC8 DHC8202 2809007NM PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- FITTING IS CRACKED ON CORNER OF MAIN CABIN DOOR. REPAIRED IAW DHC-8 SRM 51-00-06, 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20040114000352004011400035NM 2004 1 14 DL757030947 120031021A5330146N351111 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27659DL 24421 THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED BETWEEN FS 1380 & 1400 AND BETWEEN STRINGERS 28R & 30. THE DAMAGE WAS REMOVED WITH A 5.5 X 2.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385731-14, REV A. 2L72 4F RTA2NM 20031124000972003112400097WP 2003 11 24 DHL2003805503 120030813A57205769857U614 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E ZEE-PAN CRACKED 8.000 AT STA XS.520.000. REMOVED CRACKED ZEE-PAN FITTING IAW SRM 51-1-20 PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE-PAN FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040114002062004011400206WP 2004 1 14 MWEA030429 120031023A552299184807 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE RT ELEVATOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 RIGHT ELEVATOR HAS DAMAGE TO OUTBOARD TRAILING EDGE 1INCH X .5 INCH. INSTALLED EXTERNAL DOUBLER. 2L72 4F4 F A6WE E2EA 20031215001612003121500161WP 2003 12 15 AALA20031122 120031003A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21274AA 49271 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE OVERWING EXIT. INSTALLED WIRE AT BATTERY PACK B5-105. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001052003121500105NM 2003 12 15 AWXA200301467 120031105A5311651758268 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD VERTICAL FRAME WEB AT LBL 17.1, WL 183. MAINTENANCE CUT OUT CRACK IN WEB AT LBL 17.1, WL 183 AND PERFORMED A HFEC INSPECTION; FABRICATED A NEW SECTION OF WEB FILLER AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG 212, PG 288K-288X. 2L72 4F RTA16WE 20031217000802003121700080NM 2003 12 17 CALA0300669 120030717A5210 BEAM BOEING737 7373T0 1384582NM L-1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND A CRACK AT LOWER FORWARD CORNER OF LOWER BEAM OF L-1 DOOR. A DOUBLER WAS INSTALLED IAW SRM 52-10-02. 2L72 4F RTA16WE 20031218001572003121800157NM 2003 12 18 QXEA200301512 120031203A5210 STOP DHAV DHC8 DHC8202 2809007NM ZONE 800 LACK OF LUBE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09354PH 498 MAIN CABIN DOOR IS DIFFICULT TO OPEN. CLEANED AND LUBED DOOR STOP LUGS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031231000442003123100044EU 2003 12 31 ASOA03563 120031103A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11634AS 370 DURING HANGAR MAINTENANCE IN MCN, THE PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040105001312004010500131NM 2004 1 5 SWAA032771 120031218A3350610779 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29745SW 29491 RIGHT SIDE OVER WING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER SRM. 2L72 4F RTA16WE 20040106001052004010600105NM 2004 1 6 CALA0300713 120031218A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 616, LBL 65.5, WL 200. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20040105000722004010500072NM 2004 1 5 03FDEA02210 120031217A5320AJC73461 FITTING DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 AFT BODY BULKHEAD STA Y=2163 FWD FACE 1 OFF FITTING AT 6 O’CLOCK POSITION LT SIDE ABOVE THE TAILCONE LT HINGE POINT FOUND CRACK. AFT BODY BULKHEAD STA Y=2163 FWD FACE 1 OFF FITTING REMOVED AND REPLACED AS PER DRAWING AJC 7262 AND SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20031202001402003120200140EU 2003 12 2 ASOA03509 120030927A5320 SUPPORT ANGLE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING A C-CHECK IN BNA, THE SUPPORT ANGLE AT FS 39 AND SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ANGLE AT FS 39 AND SERVICE DOOR THRESHOLD IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20031202001662003120200166NM 2003 12 2 ASAA03100252 120030327A531165549581 FRAME BOEING737 737298C 1384490NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 DURING D-CHECK, FOUND FRAME AT BS 500B, STRINGER 23L CHAFED AND DENTED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031203001202003120300120EA 2003 12 3 A6WA200340132 120030815A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 FOUND STRINGER 14 OBLIQUE ANGLE P/N 601-35012-51 IS CRACKED APPROXIMATELY 2 INCHES. REMOVED AND REPLACED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M) 2L72 4F RTA21EA 20031204001272003120400127SO 2003 12 4 C2XA03SD001 120031016A3260805701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO MLG UNSERVICEABLE A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2718557 145596 LANDING GEAR WOULD NOT RETRACT. LG FAIL AIR/GRD FAIL IC 1-2 INOP CAUTION MESSAGES DISPLAYED. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED LT WEIGHT ON WHEELS PROXIMITY SENSOR, ADJUSTED RT AND LT MLG PROXIMITY SENSORS, AND C/W LANDING GEAR FUNCTIONAL CHECKS. WORK ACCOMPLISHED IAW EMB AMM II 32-63-01, 32-36-05. AIRCRAFT RELEASED. 2L72 4T RTT00011AT 20031204001422003120400142EA 2003 12 4 03289687 120031016A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27687BR 7720 DURING INSPECTION ALL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY BATTERY PACKS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040122000772004012200077WP 2004 1 22 GTIA0300964 120031107A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND FLOOR PANEL LEFT STATION 200-237, BLUE WATER STAIN, HAT CHANNEL DELAMINATING FROM PANEL DOME NUT BROKEN OFF. REBONDED HAT CHANNEL. (M) 2L72 4F RTA6WE 20040127001692004012700169NM 2004 1 27 ASAA0310189 120030321A5230658436020A FITTING BOEING737 737298C 1384490NM CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO DOOR SUPPORT FITTING AT BS 360, WATERLINE 298 GOUGED AND CHAFED. REMOVED AND REPLACED FITTING PER SRM. (M) 2L72 4F RTA16WE 20031204000572003120400057WP 2003 12 4 GTIA030847 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT CORROSION AT FS 160-200 51 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20031209001302003120900130NM 2003 12 9 QXEA200301343 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 RIGHT INBOARD TRACK NR 9 SEAT ATTACH AREA CORROSION AND BARE METAL BOTTOM APPROXIMATELY X541.00. REPAIRED IAW DASH 8-2 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030425000992003042500099NM 2003 4 25 P5CA0300784 120030320A3241421877 CONTROL UNIT BOEING747 7472D3B 1384805NM ANTI SKID SYS INOPERATIVE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23505MC 21251 ON PUSHBACK RT WING FRONT ANTI-SKID LIGHT ILLUMINATED. DE-ACTIVATED NR 14 BRAKE & DEFERRED ITEM. ONE DEFECTIVE CHANNEL WITHIN CONTROL UNIT. 2L74 4F RTA20WE 20030429000062003042900006NM 2003 4 29 P5CA0300792 120030203A5315 FLOORBEAM BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 STA 1800 LBL / RBL -5 / WL 2008 CORROSION ON THE FLOORBEAM UPPER CHORD. ACCOMPLISHED WORK PER SRM 51-40-03 FIG -3. 2L74 4F A20WE 20030430001622003043000162NM 2003 4 30 SWAA030873 120030419A53306545768 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS ( 3 EA ) AT STR 4R, BS 331 TO BS 358, BS 259 TO BS 268 & BS 290 TO BS 319. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030429002102003042900210NM 2003 4 29 VNAA0304004 120030410A3397 HARNESS DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL07463PS 3087 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 9A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 45LK ELECTRICAL HARNESS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030430002462003043000246WP 2003 4 30 MWEA030166 120030414A574059305031 BUSHING DOUG DC9 DC981 3022081WP LT WING DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 FOUR HI-LOKS REQUIRED REMOVAL IN THE LEFT WING FUEL TANK APPROXIMATELY XCW 67 AND XCW 69 DUE TO FUEL LEAKS. FABRICATED AND INSTALLED BUSHINGS. 2L72 4F A6WE 20030501001162003050100116WP 2003 5 1 ASAA0380097 120030122A5320993061269 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OAK - DURING C-CHECK, FOUND CABIN FLOOR MEMBRANE (WEB) CORRODED ON UNDERSIDE AT FS 1136-1174. CUT OUT CORRODED SECTION AND INSTALLED DOUBLER PER SRM 53-01, 51-30-2, AND 51-10-33. (M) 2L72 4F RTA6WE 20030501001782003050100178NM 2003 5 1 ASAA0310055 120030301A57546546419503 SKIN BOEING737 737298C 1384490NM RT WING LE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DUIRNG D-CHECK, FOUND RIGHT WING LEADING EDGE SKIN AT WING STATION 493.89 GOUGED. REPAIRED SKIN PANEL PER SRM. (M) 2L72 4F RTA16WE 20030501001062003050100106NM 2003 5 1 ASAA0310043 120030225A78306573771 RIB BOEING737 737210C 1384459NM THRUST REVERSER CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 1 ENGINE OUTBOARD TAILPIPE COWL RIB AT THRUST REVERSER STATION 123.47, WING STATION 191L CHAFED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F A16WE 20030502002722003050200272NM 2003 5 2 SWAA030851 120030416A53146545409 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL 33. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20030505001422003050500142NM 2003 5 5 03FDEA00629 120030428A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FUSELAGE OUTER SKIN AT FASTENER HOLE BS 700 BL 0 WL 148.5. 2L73 4F RTA3WE 20030508000212003050800021NM 2003 5 8 DLM88030343 120030407A5330591140213 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27905DL 49536 DURING HMV-3, FOUND ADDITIONAL DAMAGE AT L-1 DOOR HOLD-OPEN HOOK CUTOUT. INCREASED CUTOUT IN FUSELAGE SKIN TO 3.75 IN. (FWD-AFT) BY 2.90 IN. (UP-DOWN) MAX. INSTALLED REPAIR DOUBLERS PER ER/A 378453-14 REV. A. 2L72 4F RTA6WE 20030508000372003050800037WP 2003 5 8 0300871244 120030429A3320 LIGHT DOUG DC10 DC1030 3023501WP CABIN INOPERATIVE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01244NW 48316 ENROUTE TO MSP CABIN B CENTER SECTION ROWS 10-20 CDE AUDIO AND READING LIGHTS WERE INOP. A BURNING ELECTRICAL ODOR WAS NOTED. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. REPLACED SEAT 18 CDE SEB. OPERATIONAL CHECK GOOD. 2L73 4F A22WE 20030508001022003050800102SO 2003 5 8 C2XA03IA046 120030501A335074441 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716911 145446 EWR- ON POSTFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR FAILED TO ILLUMINATE. EWR- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030508000502003050800050SO 2003 5 8 C2XA03SH123 120030502A532014524131005 BRACKET EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 SHV DURING C CHECK CORROSION WAS FOUND UNDER THE MAIN DOOR'S THRESHOLD BETWEEN FRAMES 15 AND 18. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED THRESHOLD SUPPORT ANGLES IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030509001162003050900116EU 2003 5 9 BAQA085960 120030414A243245043003 BATTERY UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE MASTER FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03554ME1123 0154 BATTERY FAILED SELF TEST. AIRCRAFT WILL NOT CRANK. (BATTERY DISCONNECT). NO HARD CARD AVAILABLE. OLD 8130 ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H88EU E34NE 20030509001722003050900172NM 2003 5 9 USAA030037 120030404A5753 SKIN BOEING737 7374B7 1384702NM TE FLAP CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US38422 24548 FOUND FLAP SKIN CHAFED 6 INCHES LONG, LEFT OUTBOARD MID FLAP, INBOARD END NOSE CAP. CUT OUT DAMAGE AND INSTALLED DOUBLER PE SRM 57-53-01 FIG 208. (M) 2L72 4F RTA16WE 20030514001322003051400132NM 2003 5 14 SWAA031018 120030507A53116546569 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 927, RBL 4 TO LBL 4. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030514001942003051400194NM 2003 5 14 03FDEA00702 120030507A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING - O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT, I/B LUG I/B FACE FOUND CORRODED. RT WING- O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG I/B FACE CORROSION AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68414 WINGS- RIGHT O/B FLAP- O/B HINGE AFT SUPPORT CORROSION. 2L73 4F RTA22WE 20030602000882003060200088NM 2003 6 2 DLM88030489 120030524A3260 PROXIMITY SENSOR DOUG MD88 MD88 3023688NM NLG FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27959DL 49978 NOSE GEAR UNSAFE ON T/O. NOSE GEAR EXTENDED NORMALLY UPON RETURN. REPLACED NOSE GEAR LOCK PROX SENSOR. 2L72 4F RTA6WE 20030604000492003060400049WP 2003 6 4 UPS03840459 120030420A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, APPROX. STA 700, LONG 35 RT, SHEAR TIE (FRAME ANGLE) UNDER STRESS PN L IS CORRODED AND CRACKED REMOVED DAMAGED SECTION OF SHEAR TIE IAW DC8 SRM 51-1-20D, FABBED NE W SECTION IAW DWG 9753780, LOCATED AND DRILLED UP NEW SECTION IAW D WG 9753780 ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED ON AIRCRAFT IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20030604001742003060400174NM 2003 6 4 UPS03440594 120030415A575365B078752 RIB BOEING747 747121 1384871NM NR 19 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT WING - NR 19 VC FLAP O/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 6 ( VIEW FROM I/B ). BOLT HOLE CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO 747-5740-18687-A. 2L74 4F A20WE 20030612001972003061200197EA 2003 6 12 SWIA200311991 120030507A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW 7555 FS 280 RIGHT FLOORBEAM RBL 9.0 ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. 2L72 4F4 FRTA21EA E15NE 20030613000152003061300015NM 2003 6 13 ABXA030184 120030316A4997 WIRE BOEING767 767281 1385109NM APU DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 APU GENERATOR FEEDER WIRE DAMAGE, CAUSED SHORT CIRCUIT TO GROUND, RESULTING ARCHING TO WIRE AND CLAMP AT STA 1788 RIGHT. REPLACED THE FEEDER WIRE FROM THE NEARBY SPLICE TO APU SHROUD CONNECTOR D 4016J, AND CLAMP. OPS CHECKED GOOD IAW B767 MM. 2L72 4F RTA1NM 20030613001522003061300152NM 2003 6 13 SWAA031233 120030602A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED PM CHECK, FOUND STRINGER TIE CLIP CORRODED AT BS 967, STR 27L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20030617002172003061700217SW 2003 6 17 HEEA087313 120030611A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 SEALANT MISSING FROM ROOT END. CORROSION AT WEIGHT POCKET, HOLE ALONG TIP ABOVE BLADE TIE DOWN BRACKET. SERIAL NUMBERS REMOVED ARE A2029, A2041, A2060 AND A2061. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030617002382003061700238NM 2003 6 17 QXEA200300599 120030430A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT SUPOPRT FLANGE FOR 261FT IS CHAFED. REPAIRED IAW DHC-8 Q400 RD 8/4-53-451. 2H72 4T RTA13NM 20030520000532003052000053SO 2003 5 20 SIMA200311309 120030402A532014522461003 GUSSET EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 ABI - THIS A LEVEL TWO FINDING FOUND DURNG AN IMBV INSPECTION, RIGHT OMEGA BEAM 1/2 DIAMOND GUSSET AT FRAME 23 CORRODED. REMOVED AND INSTALLED RIGHT FLOORBEAM GUSSET AT FRAME 23 IAW EMB 145 SRM 51-20-01/03, 51-40-02/04/06. (M) 2L72 4T RTT00011AT 20030522000232003052200023NM 2003 5 22 2003UALA00415 120030503A5313 STRINGER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29815UA 867 AFT OF DOOR 2L AT THE FLOOR LINE THERE IS STRINGER & SKIN DAMAGE. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER AND INSTALLED DOUBLER REPAIR ON SKIN. 2L72 4F4 FRTA28NM E40NE 20030529000072003052900007EU 2003 5 29 AALA20030404 120030403A3350 PIN AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2140064 507 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 1R DOOR FORWARD HORIZONTAL ASSEMBLY INOPERATIVE. RESEATED PIN ON EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030527000202003052700020NM 2003 5 27 VNAA0305009 120030514A3350501122803 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07462PS180851696 3084 THE CREW REPORTED THAT THE AFT EMERGENCY BATTERY WAS INOP. MAINTENANCE INSPECTED AND REPLACED THE AFT POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031210000152003121000015NM 2003 12 10 SWAA032614 120031127A53116546569 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, ABOVE STR 14L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030919000692003091900069 2003 9 19 U30A200300028 420030805A2211C12850AB02 COMPUTER AIRBUS320 A320214 3930316EU ZONE 210 INOPERATIVE A U30AO OTHER J WARNING INDICATION DEDESCENT 1 EA17264AV2055 2055 1867 DURING DESCENT ON FLT 581 ATL-CUN, NR 1 FCU (FLIGHT CONTROL UNIT) WENT INOP.UNIT WAS DEFERRED PER MEL 22-81-01 ON GND IN CUN. IN ORD ON 5 AUG 03, REPLACED FCU IAW AMM 22-81-12-401 AND ALL SYSTEM CHECKS PERFORMED GOOD. AIRCRAFT RETUNED TO SERVICE. NOTE REVISED "DIFFICULTY DATE" ON AUGUST 12,2003; DATE WAS 05/05/2003, SHOULD READ 08/05/2005. 2L72 4F RTA28NM 20030916000992003091600099EA 2003 9 16 ASOA03380 120030817A5320MM67080500001 BRACKET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11701EV 10020 DURING AN A-CHECK IN BTR, THE LT BLEED AIR DUCT SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT BLEED AIR DUCT SUPPORT BRACKET IAW ASA EO 700-36-0003B. (M) 2L72 4F RTA21EA 20030924000272003092400027NM 2003 9 24 DL764030735 120030809A2751 WARNING LIGHT BOEING767 767432ER 1385134NM TE FLAPS ILLUMINATED A DALAO OTHER J WARNING INDICATION LDLANDING 1 SO27834MH 29707 WHEN EXTENDING FLAPS FROM 15 TO 20 TE FLAP DISAGREE MESSAGE ILLUMINATED. FLAPS IND 20 BUT MSG WOULD NOT GO AWAY WHEN QRH PROCEDURE ACCOMPLISHED LANDED WITH 20 FLAPS. CHECKED FLAP OPERATION IAW FIM 27-51-00 FIG 105 NO ACTUATORS WERE TRIPPED, SYSTEM OPS NORMAL. 2L72 4F RTA1NM 20030922001272003092200127NM 2003 9 22 QXEA200300992 120030811A3213 STRUT DHAV DHC8 DHC8202 2809007NM ZONE 700 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 RT HAND MAIN LANDING GEAR SHOCK STRUT AXLE IS GOUGED ON OUTBOARD AXLE. REPAIRED IAW DHC-8 RD 8-32-498 AND SRM 51-20-36. 2H72 4T RTA13NM 20040127002022004012700202WP 2004 1 27 ASAA0380668 120031015A53305924802 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND DENT IN SKIN ABOVE LAV SERVICE DOOR. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040128000552004012800055NM 2004 1 28 AWXA200301616 120031208A53156545812 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND IN 5 PLACE ON UPPER SURFACE OF FLOORBEAM AT BS 328, BETWEEN RBL 18 AND RBL 50. MAINTENANCE CUT OUT AND REMOVED DAMAGED SECTION OF FLOORBEAM AT BS 328, BETWEEN RBL 18 AND RBL 50; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM AND 2 EACH REPAIR ANGLES & STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51 FIG 201, PG 201-205. 2L72 4F RTA16WE 20040204000212004020400021EU 2004 2 4 202201 120031022A7997 WIRE SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE OIL PRESS XDUCERDAMAGED A UHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL17123XS 123XS FLIGHT NR 4585 FROM PIT TO IPT. A/C WAS FLYING TO IPT WHEN AIRCREW NOTICE RT PROP OIL PRESSURE GAUGE WOULD FLUCTUATE INTERMITTENTLY FROM 80 TO 5 PSI. MAINTENANCE REPAIRED INSULATION ON WIRE TO PROP OIL PRESSURE TRANSDUCER. GROUND RAN A/C AND RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 20031212000342003121200034SO 2003 12 12 C2XA03BT105 120031112A3350110049 BATTERY EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717928 145007 GSP---CO2600, CREW, DURING PREFLIGHT, NOTED EMERGENCY AISLE PATH LIGHTS AT ROW 7-12 ARE INOPERATIVE. CLT MAINTENANCE WENT TO GSP AND REMOVED AND REPLACED THE EMERGENCY BATTERY SUPPLY CHARGER ASSEMBLY, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031215001152003121500115WP 2003 12 15 AALA20030988 120030910A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2116545 53027 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROWS 29 THROUGH 31. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040316000072004031600007WP 2004 3 16 ASAA0380355 120030418A5500S9205563 FAIRING DOUG DC9 DC983 3022083WP STABILIZER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND RIGHT STABILIZER OUTBOARD LOWER HINGE FAIRING IS BENT AND CRACKED. REPLACED FAIRING PER SRM 51-30-1. (M) 2L72 4F RTA6WE 20031216000242003121600024EA 2003 12 16 MASA200300454 120031116A33502058381 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW0747239 7239 DEN-OKC, DURING PRE-FLT THE REAR HALF OF THE EMERGENCY FLOOR TRACK LIGHTING WAS INOP. MX REPAIRED A CONNECTOR. OP CHECKS GOOD. 2L72 4F RTA21EA 20031217000402003121700040WP 2003 12 17 DHL2003802519 120031106A5730 SKIN DOUG DC8 DC873 302199CWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING CTR L/E UPPER SKIN CORRODED, STA XFS 330.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG 38. FABRICATED FILLER (7075-T6 0.063) AND DOUBLER (7075-T6 0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030925000742003092500074CE 2003 9 25 2003F00580 120030824A5300 PANEL LEAR 25 25B 5170511CE NOSE DEPARTED A CEDAA UNSCHED LANDING WD INADEQUATE Q C INFLIGHT SEPARATION CLCLIMB 1 SW058005Y 121 AIRCRAFT LOST NOSE PANEL ON TAKEOFF DURNG A PART 91 FLIGHT AIRCRAFT RETURNED TO BASE. UPON RECOVERY INSPECTION, FOUND THAT NOSE PANEL WAS LEFT UNFASTENED BY MAINTENANCE PERSONEL. (M) 2L72 4J A10CE 20030925000762003092500076NE 2003 9 25 GTIA030613 220030804A7200 ACOUSTIC LINER DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE ENGINE MISSING A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 NR 1 ENGINE 14 SD INCHES OF ACOUSTIC LINER MISSING AFT OF NR 4 BEARING STRUT. PLACED ON CARRYOVER NR 0107964-1 AND NR 0120963-3 IS CONTAINED WITHIN 0120964-1. INSPECTED AND FOUND AIRWORTHY FOR FLIGHT. (M) 2L72 4F4 FRT E9NE 20030618002072003061800207GL 2003 6 18 HEEA086994 220030603A753223007827 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED W HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 ANTI ICE LIGHT ILLUMINATED IN FLIGHT. REPLACED. 1G71 3U3 UO H2SW E1GL 20030623000122003062300012NM 2003 6 23 AMTA200300656 120030516A3350 STRIP BOEING737 73783N 13844HINM CABIN DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11321TZ 28249 THE FLOOR EGRESS IN FRONT OF THE AFT LEFT LAV IS DISCOLORED. REMOVED AND REPLACED DAMAGED SECTION OF PHOTOLUMINESCENT STRIP REF MM 33-51-15-2. (M) 2L72 4F RTA16WE 20030702000282003070200028NM 2003 7 2 TSAA0353111 120030423A53156545834 FLOORBEAM BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 FOUND CORROSION ON UPPER FLOORBEAM AT BS 344 BLENDED OUT 1 INCH BY 1 INCH AREA IN TWO PLACES. CUTOUT DAMAGED AREA. FABRICATED NEW FLOORBEAM SECTION PER TABLE II, DETAIL I. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-10-9, FIGURE 5. (M) 2L72 4F RTA16WE 20030708000802003070800080NM 2003 7 8 AWXA200300651 120030517A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 7, WL 198.5-199.5. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW SRM 53-10-08, PG. 284. 2L72 4F RTA16WE 20030709000102003070900010WP 2003 7 9 AALA20030578 120030518A335060030451 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21569AA 49351 DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED AFT LAVATORY EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030710001182003071000118SO 2003 7 10 C2XA03BT067 120030615A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714916 145415 DURING ROUTINE INSPECTION, MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT AND THE COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULBS IAW EMB145 MM 33-50-05 AND 33-50-10. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030711000812003071100081EA 2003 7 11 COMA0360287 120030614A2721601R5122623 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA INST PANEL MALFUNCTIONED A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01451CA 7562 RUDDER TRIM WENT TO FULL NOSE LEFT WITH NO CREW COMMAND. REPLACED THE RUDDER TRIM CONTROL PANEL. 2L72 4F RTA21EA 20030114000422003011400042NM 2003 1 14 SWAA030035 120030106A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND LT AND RT FUSELAGE FRAMES CRACKED (2 EA) AT BS 188, WL 207 AND WL 208. REMOVED AND REPLACED FRAMES PER SRM. 2L72 4F RTA16WE 20030127000342003012700034 2003 1 27 HEEA083610 420030114A2312064105430 TRANSCEIVER BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 TRANSCEIVER DOES NOT RECEIVE. 1G71 3U O H2SW 20030129000532003012900053SW 2003 1 29 HEEA083966 120030117A5610407030115123 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 RT WINDSHIELD CRAZED. 1G71 3U O H2SW 20030204000662003020400066NM 2003 2 4 SWAA030191 120030125A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS 504 AND BS 500D + 8. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030211000072003021100007EA 2003 2 11 03030660 120030130A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DISCHARGED A VTZAD RETURN TO BLOCK L NO TEST ININSP/MAINT 1 EA27660BR 7519 DURING MAINTENANCE INSPECTION, FLOOR EMERGENCY TRACK LIGHTING IN ROWS 1-8 WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY LIGHT BATTERY, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED. 2L72 4F4 FRTA21EA E15NE 20030410002552003041000255NM 2003 4 10 F3LA200300039 120030128A5320 INTERCOSTAL BOEING737 7373M8 1384615NM FUSELAGE BENT A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL IN AFT CARGO COMPARTMENT BETWEEN STA 747 AND 767, ABOVE STR 25-R, BENT. FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 51-46-02 AND 51-10-02. FABRICATED REPLACEMENT INTERCOSTAL PER DRAWING 69-16500. INSTALLED PER SRM 51-40-02 AND BOEING DRAWING 69-16500. 2L72 4F RTA16WE 20030213001112003021300111WP 2003 2 13 2003F00079 120030105A2560P4010021 BATTERY LKHEED1011 10113851 5265010WP FLASHLIGHT DISCHARGED G K NONE L NO TEST ININSP/MAINT 1 GL11186AT 193C1074 EMERGENCY FLASHLIGHT, BEHIND SEAT 15D, BATTERY IS DEAD. REMOVED AND REPLACED FLASHLIGHT BATTERY. 2L73 4F A23WE 20030218002712003021800271NM 2003 2 18 AWXA200300157 120030217A3350BMS13311122 WIRE BOEING737 737277 1384570NM -N/A- DISTORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW0 0 22649 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROW 7 L/H WAS FOUND DAMAGED. MAINTENANCE REPLACED LIGHT ASSEMBLY COVER AND REPAIRED WIRING AT SEAT 7C. OPERATIONAL CHECK OF THE LIGHT ASSEMBLY WAS GOOD. 2L72 4F RTA16WE 20030303001272003030300127SW 2003 3 3 HEEA084551 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03223477537 36005 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS EROSION HOLE THROUGH THE STRIP. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030304000392003030400039SW 2003 3 4 HEEA084573 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T12737 33112 MAIN ROTOR BLADE LOWER TRAILING EDGE FRETTING PAD UNBONDED. 1G72 4U H4SW 20030306000282003030600028 2003 3 6 HEEA084741 420030217A2340 SWITCH BELL 412 412 1182202SW INTERPHONE BOX INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 8811175 33076 FM NR 1 AUDIO SWITCH IS INOPERATIVE. FOUND S2, S4, S5, S8, S9 MONITOR SWITCHES BAD. ALSO REPLACED BOTH KNOBS, BENCH CHECK GOOD. 1G72 4U H4SW 20030306000862003030600086SW 2003 3 6 HEEA084795 120030221A6730212076005111 SERVO BELL 412 412 1182202SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033893N 33010 MAIN ROTOR SERVO LEAKS FROM PILOT VALVES. 1G72 4U H4SW 20030312000542003031200054EA 2003 3 12 COMA0360141 120030310A27409960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA CONTROL COLUMN MALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01471CA 7655 FLIGHT 5417 STAB TRIM CAUTION AND MACH TRIM MESSAGE.REPLACED THE PITCH TRIM DISCONNECT SWITCH. 2L72 4F RTA21EA 20030317000902003031700090NM 2003 3 17 03FDEA00251 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 10R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030320000132003032000013NM 2003 3 20 USAABB03010 120030111A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19633AU 27811 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 23. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030320000432003032000043NM 2003 3 20 USAASB03011 120030120A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHTSDAMAGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19512AU 23595 ORD - MAINTENANCE REPORTED THE CABIN EMERGENCY LIGHT AT SEAT 14C INOPERATIVE. MAINTENANCE REPAIRED WIRE SPLICE BENEATH SEAT 14C. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030320000662003032000066NM 2003 3 20 03FDEA00333 120030313A5347 CARGO TRACK DOUG MD11 MD11 3023602NM CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 MAIN DECK CARGO BAY DOORWAY FLOOR CARGO TRACK AT LT SIDE STA 635, 8.5 INCHES FOUND CRACKED. 2L73 4F RTA22WE 20030320001382003032000138 2003 3 20 2003UALA00129 420030201A2565 GIRT BAR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ESCAPE SLIDE INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29934UA 26662 GIRT BAR AT DOOR 2L WILL NOT STAY ENGAGED DURING TAKEOFF AND LANDING. REPLACED SLIDE. SLIDE AND GIRT BAR HAVE BEEN EXAMINED BY THE SHOP. NO DEFECTS FOUND. 2L72 4F4 FRTA16WE E2GL 20030327000852003032700085SO 2003 3 27 C2XA02SH189 120030204A531014521700007 BEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713913 145438 DURING C-CHECK LT OMEGA BEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001122003032700112SO 2003 3 27 C2XA03CL032 120030207A32307455501 CONTROL UNIT EMB 135 EMB135LR 3260305SO MLG FAILED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2727523 145389 CLE FLIGHT 2117 THE CREW REPORTED THE LANDING GEAR SELECT LEVER REQUIRED THE DOWNLOCK RELEASE BUTTON TO BE PRESSED TO RETRACT THE GEAR. MAINTENANCE REPLACED THE LANDING GEAR SELECT LEVER CONTROL ASSEMBLY. ALSO REPLACED RELAYS KOO24, KOO25, AND KO453. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030324001302003032400130 2003 3 24 COMA0360163 420030320A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01818CA 7408 FLIGHT 5399 STALL FAIL CAUTION MESSAGE AFTER T/O.RESET STALL PROTECTION COMPUTER - OPERATIONAL. 2L72 4F RTA21EA 20030721001402003072100140NM 2003 7 21 751PA0017 120030630A3350 BULB BOEING757 757200 1384950NM EMERGENCY LIGHT BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 EXTERIOR EMERGENCY LIGHTS INOP AT L1 AND R1 DOORS. REPLACED BULB IN L1 EXTERIOR EMERGENCY LIGHT AND CLEANED CONTACTS FOR R1 EXTERIOR EMERGENCY LIGHT. OPS CHECKED OK. 2L72 4F RTA2NM 20030421001822003042100182NE 2003 4 21 MEX2003064 220030309A7261 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE NR 2 LACK OF LUBE A ASMFED ENGINE SHUTDOWN RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 SW231003Y 48068 FLT 940 - MEX-MTY, AIRCRAFT RETURNED TO PLATFORM, DURING TAXIING THE LOW QUANTITY OIL LIGHT OF ENGINE NR 2 TURNED ON. THE OIL LEVEL WAS VERIFIED BEING NECESSARY TO ADD 7 QUARTS. THE ENGINE MAIN OIL FILTER WAS INSPECTED IAW MM 79-20-06, ALL CORRECT FOR SERVICE. (M) 2L72 4F4 F A6WE E2EA 20030730001352003073000135EA 2003 7 30 SIMA200317602 120030623A3234533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA HYD BAY FAILED A SIMAO OTHER O OTHER APAPPROACH 1 SW21501BG 10017 DFW - FLT 3850 - DURING APPROACH CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND. FOLLOWED QRH PROCEDURES AND GEAR EXTENDED. AIRCRAFT LANDED WITH NO FURTHER INCIDENT REPORTED. NOSE WHEEL STEERING SYSTEM WAS INOPERATIVE UPON LANDING. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE IAW CRJ MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030801000702003080100070WP 2003 8 1 GTIA030529 120030615A5320 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - AFT PIT STATION 1117 STRINGER 30-29L FRAME SUPPORT CORRODED. FABRICATED ANGLE REPAIR. INSTALLED REPAIR ANGLE. (M) 2L72 4F A6WE 20030801000762003080100076EU 2003 8 1 2003F00490 120030516A3610 PRECOOLER AIRBUS320 A320233 3930329EU NR 1 ENGINE DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 1 ENGINE INTAKE PRECOOLER, ON BOTH SIDES OF THRUST REVERSER C-DUCT DELAMINATED. REPAIRED PRECOOLER IAW SRM 54-02-00. (M) 2L72 4F RTA28NM 20030825001252003082500125SO 2003 8 25 C2XA03IA082 120030809A335066367 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714945 145049 IAH - FLIGHT 2573 - THE FORWARD SECTION OF EMERGENCY PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030827000412003082700041CE 2003 8 27 8564188 120030619A29101013880175 FITTING BEECH 1900 1900D 1154162CE LT MLG LEAKING A JJBAO OTHER K FLUID LOSS LDLANDING 1 EA01856CA4602 66 UE405 LANDING GEAR WOULD NOT EXTEND ELECTRICALLY. LANDING GEAR WAS EXTENDED USING HAND PUMP. UPON INSPECTION, MAINTENANCE DISCOVERED FLUID LEAKING FROM THE SWAGE FITTING ON THE LT MAIN LANDING GEAR RETRACT ACTUATOR HOSE. SUSPECT CAUSE WAS FLEX FATIGUE. MAINTENANCE PROGRAM MODIFICATIONS ARE UNDER CONSIDERATION. 2L72 4T RTA24CE 20030828000212003082800021GL 2003 8 28 65686 320030321A6111L104DSZ BLADE BCRAFTHB HONEYBEEHB 1110102WP PWA PT6 PT6* 52043EA MCAULY5JFR365JFR36C1003 GL PROPELLER CORRODED B EY2RK NONE O OTHER UKUNKNOWN 1 GL03 920485 CORROSION ON BLADE. 1H71 3O3 T 4A11 E2NE 6 CP15NE 20030829000092003082900009WP 2003 8 29 ARWA20030510 120030527A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR LOWER SURFACE RIVET PLUNGED, STATION 540, BY L-36. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, TRIMMED OUT DAMAGED AREA AND FABRICATED PARTS IAW AVITAS ENGINEERING REPAIR ORDER AROW-031RO-4, PAGE 1 & 2, DATED 05/01/03 AND REPAIR SKETCH AIPSAC-N784AL-04/03, REV IR, SHEET A.1 TO A.5, DATED 05/01/03. TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW REPAIR ORDER AROW-031RO-4, PAGE 1 TO 2 AND REPAIR SKETCH AIPSAC-N784AL-04/03, REV IR. ISSUED FAA FORM 8110-3. 2L74 4F 4A25 20030722000892003072200089NM 2003 7 22 SWAA031442 120030630A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947.5 AT STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030723000072003072300007WP 2003 7 23 MEX2003249 120030625A215020495054 TURBINE DOUG DC9 DC987 3022087WP CABIN COOLING FAILED A ASMFO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW231075T 49724 AIRCRAFT ARRIVED WITH CAPTAIN REPORT 'DEFICIENT AIR CONDITIONING'. DURING REVISION THE LEFT TURBINE COOLING WAS DAMAGED. REPORT WAS DEFERRED IAW MEL 21-1, LEFT AIR CONDITION OUT SERVICE. DURING OVERNIGHT SERVICE THE LEFT TURBINE COOLING WAS REPLACED IAW MM 21-51-01, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030724001272003072400127NM 2003 7 24 DL757030575 120030620A5330146N351112 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL DENTS NEAR STRINGER 28L BETWEEN FS 1454 & 1466. THE DAMAGES WERE REMOVED WITH A SINGLE 6.8 X 3.4 INCH SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385095-14, REV A. 2L72 4F RTA2NM 20030731000062003073100006NM 2003 7 31 QXEA200300903 120030719A5720 MOUNT BRACKET DHAV DHC8 DHC8202 2809007NM WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- NUTPLATE MOUNT BRACKET FOR LEADING EDGE 611AR LOWER OUTBOARD NEXT TO NACELLE ON SPAR IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20030806000462003080600046SO 2003 8 6 C2XA03TY093 120030723A534714532606011 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713990 145277 DURING A SCHEDULED INSPECTION THE LW1, CABIN SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145-AMM-53-01-06. 2L72 4T RTT00011AT 20030903002532003090300253SO 2003 9 3 C2XA03SH313 120030901A532014521725013 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030729000262003072900026EA 2003 7 29 03204634 120030723A7931 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT FALSE INDICATIONA VTZAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27634BR11787 7287 872450 DURING CRUISE THE CREW REPORTED A LOW OIL PRESSURE INDICATION ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK OF THE RT ENGINE OIL SYSTEM AND A SATISFACTORY MAINTENANCE ACCEPTANCE FLIGHT WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030729000962003072900096EU 2003 7 29 2003F00476 120030516A5350 FAIRING AIRBUS320 A320233 3930329EU FUSELAGE DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND BELLY FAIRING 197CB DELAMINATED. REPAIRED FAIRING IAW SRM S3-45-12 PAGE 220, FIGURE 205. (M) 2L72 4F RTA28NM 20030825000082003082500008NM 2003 8 25 UPS03240955 120030708A2910 CHECK VALVE BOEING727 72722C 138400FNM HYD SYSTEM LEAKING A IPXAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01941UP 19196 INSPECTION TYPE: N/A SMOKE IN COCKPIT - ATB. A/C LANDED WITHOUT INCIDENT. T/S IN PROGRESS. REMOVED AND REPLACED THE A SYS AIR PRESSURE REGULATOR IAW MM 2912. FOUND EVIDENCE OF HYD FLUID IN THE RES AIR PRESS CHECK VALVE ASSY. REMOVED AND REPLACED ALL 3 CHECK VALVES PERFORMED LK CHECK AND RAN ALL 3 ENGINES APPROX 10 MINS 2 PACKS ON NO DEFECTS FOUND. 2L73 4F A3WE 20030821002902003082100290EU 2003 8 21 200315 120030715A335010335140004 BATTERY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A YENAK NONE O OTHER DEDESCENT 1 EA15565JB221 2031 EMERGENCY EXIT SIGNS AT AFT INOP. REMOVED AND REPLACED BATTERY IN EPSU FIN NR 13W PER AMM 33-51-38, OPS. CHECK OK. 2L72 4F RTA28NM 20030826000222003082600022NM 2003 8 26 03FDEA01369 120030806A5744ARC0503504 HINGE BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR INBOARD AND OUTBOARD HOLE FOUND CORROSION. RT WING OUTBD FLAP OUTBD HINGE BRACKET (WING SIDE) ACTUATOR INBOARD AND OUTBOARD HOLE REPAIR CARRIED OUT AS PER EA 1-5740-71796 WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030826000502003082600050NM 2003 8 26 03FDEA01217 120030806A5753 SUPPORT DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LEFT OUTBOARD FLAP NOSE RIB SUPPORT ISLAND FOUND 01 CRACK AT OUTBOARD SIDE, APPROX .1875 INCH LONG. LT OUTBD FLAP NOSE RIB DAMAGED SUPPORT ISLAND CARRIED OUT REPAIR IAW FEDEX EA 1-5750-63119, TITLE- WINGS- TRAILING EDGE FLAPS- OUTBOARD TRAILING EDGE FLAP- SECONDARY UP STOP- REPAIR. 2L73 4F RTA22WE 20030912000022003091200002EU 2003 9 12 MALA030370 120030806A7722 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE RT ENGINE MALFUNCTIONED A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL1527XJ 340A027 DURING TAKEOFF ON FLIGHT 2966, IN MODERATE RAIN THE RT ITT REACHED 914, AT LIGHTOFF AND AT 400 FT THE ITT DROPPED TO 905. CREW PROCEEDED TO DO THE AFTER TAKEOFF CHECK DURING CTOT REDUCTION AND NOTICED THE RH OVERTEMP LIGHT ON THE RH ENGINE. THE ITT DIGITAL PORTION JUST PAST THE 1000 MARK. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED ENGINE IAW TASK CARD 7100-301 INCLUDING WORK PACKAGE DATED 8/7/03. MAINTENANCE GROUND RAN A/C, ITT INDICATOR PEGGED OUT AT MAX INTERMITTANTLY DURING PROCEDURE, MAINTENANCE REPLACE ITT INDICATOR PN OFF/ON 523347, SN/OFF 6757, SN/ON 6013, OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20030908002402003090800240EU 2003 9 8 MALA030352 120030726A5270 WARNING SYSTEM SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15436XJ 340B436 AFTER TAKEOFF ON FLIGHT NR 3153, CARGO WARNING LIGHT ILLUMINATED. FOLLOWED QRH, RETURNED TO MEM. PILOT REPORTED SMALL SPIKES IN PRESSURIZATION DIFFERENTIAL. AIR RETURN TO MEM. MAINTENANCE RAN A/C ON GROUND, PERFORMED MANUAL PRESSURIZATION CHECKS, NO SPIKES OR CARGO DOOR OPEN INDICATIONS NOTED DURING 15 MINUTES GROUND RUN. OP CHECK OF PRESSURIZATION GOOD INSPECTION OF CARGO DOOR AND SEAL FOR CONDITION AND SECURITY, GOOD. SUSPECT DEBRIS IN CARGO DOOR AREA. COULD NOT DUPLICATE. 2L72 4T RTA52EU 20030909002312003090900231NE 2003 9 9 ABXA030341 220030821A7520 VALVE BOEING767 767281 1385109NM GE CF6 CF680A 30025NE NR 1 ENGINE MALFUNCTIONED A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23789AX 23022 580247 DURING CLIMBOUT AT 20,000 FEET, RECEIVED FIRE WARNING BELL, EICAS MSG AND FIRE LIGHT IN HANDLE. WHEN POWER REDUCED TO IDLE ALL INDICATION OF FIRE CEASED. OVERWEIGHT LANDING SINK RATE LESS THAN 260 FPM WITH LOW SINK RATE. REPLACED BOTH AFT LOOPS IAW B767 MM. REPLACED NR 1 ENGINE CORE COMPARTMENT COOLING VALVE, REPLACED COMPRESSOR CONTROL ALTITUDE SENSOR AND GASKET ON T3 COMPRESSOR OUTLET TEMP SENSOR. RESEALED HTP RECOUP DUCT. MEG AND POWER CHECKED SYSTEM WIRING. DURING MAINTENANCE BORESCOPE FOUND DAMAGE UNRELATED TO THE FIRE WARNING PROBLEM. DAMAGE TO THE NR 1 NOZZLE GUIDE VANE WHICH WAS OUT OF MM LIMITS. REPLACED NR 1 ENGINE. DURING FCF ON 08-27-03, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA1NM E13NE 20031014001072003101400107NM 2003 10 14 SWAA032136 120030923A3350BR2013 LIGHT BOEING737 7373H4 1384600NM AFT CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20031021003002003102100300WP 2003 10 21 ABXA030363 120030918A2497 WIRE DOUG DC9 DC941 302207NWP GLARESHIELD BROKEN A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23972AX 47631 INTERMITTENT ODOR OF BURNING INSULATION UNDER THE GLARESHIELD ON FIRST OFFICER'S SIDE. FOUND BROKEN WIRE ON FIRST OFFICERS CLEARVIEW WINDOW ANTI-FOG WIRING. SUSPECT WIRE MAY HAVE BEEN ARCING CAUSING THE SMELL. REPAIRED BROKEN WIRE. FIRST OFFICER'S CLEARVIEW WINDOW ANTI-FOG OPERATIONAL CHECK GOOD. 2L72 4F A6WE 20031121000062003112100006CE 2003 11 21 AMWA76 120031104A5260129400035131 RISER BEECH 1900 1900D 1154162CE AIRSTAIR DOOR CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127YV 127ZV WHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE AIRSTAIR DOOR AFT STEP RISER WAS FOUND TO BE CRACKED. 2L72 4T RTA24CE 20031029001242003102900124EU 2003 10 29 KBM2003F00019 120030821A6720350A33214500 LINK SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR LOOSE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 TAIL ROTOR PITCH CHANGE LINK BEARING HAS EXCESSIVE PLAY. REPLACED WITH SERVICEABLE PC LINK. 1G71 3U3 UNCH9EU E19EU 20031105000722003110500072NM 2003 11 5 SWAA032287 120031019A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 771, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20031106001372003110600137NM 2003 11 6 SWAA032274 120031016A53116516301 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND LBL 30. REMOVED AND REPLACED FRAME PER SRM. 2L72 4F RTA16WE 20030911001882003091100188WP 2003 9 11 AALA20030336 120030303A5320 SILL DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND MID CARGO LOWER SILL PLATE HAS SKIN DAMAGE, FS 674. REPAIRED FUSELAGE PER ESO 80559 DATED 2/28/2003. (M) 2L72 4F A6WE 20040112002362004011200236 2004 1 12 AALA20031409 420031209A3422 GYRO DOUG DC9 DC982 3022082WP COCKPIT FAILED A AALAO OTHER O OTHER CRCRUISE 1 SW21476AA 49651 DFW T1052/09 EN ROUTE IAH-DFW ALL PRIMARY FLIGHT INSTRUMENTS INOPERATIVE. NR 2 GYRO IN 30 DEGREES TURN CONTINUED TO ROTATE AT ONE POINT NR 1, NR 2 AND STANDBY ALL SHOWED HEADINGS THAT WERE 30 DEGREES MINIMUM APART. LANDED DFW WITHOUT INCIDENT. REPLACED NUMBER 1 AND 2 DIRECTIONAL GYROS AND CAPTAINS RADIO DIRECTION MAGNETIC INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031120000162003112000016NM 2003 11 20 AWXA200301225 120030922A5320656731147 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 993, RBL 44, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT AT BS 993, RBL 24 TO RBL 44, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-67311; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 16. 2L72 4F RTA16WE 20040114000642004011400064NM 2004 1 14 03FDEA01965 120031121A5753ARC0154 HINGE FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT INBOARD FLAP FOUND OUTBOARD HINGE FITTING PIVOT HOLE FLANGE LOCATION WITH SURFACE CORROSION AS MARKED. LT I/B FLAP O/B HINGE FITTING PIVOT HOLE FLANGE LOCATION SURFACE CORROSION REPAIRED AS PER FEDEX EA 1-5740-74253, WING - LT & RT I/B TRAILING EDGE FLAP- O/B HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20031215001512003121500151WP 2003 12 15 AALA20031191 120031029A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21449AA 49475 SAT - DURING OVERNIGHT MAINTENANCE FOUND FORWARD CABIN GALLEY AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD OVERHEAD EMERGENCY LIGHT BATTERY CHARGER AND BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031218000172003121800017EU 2003 12 18 MALA030510 120031124A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING C-CHECK INSPECTION IN LCQ, TIMCO FOUND CORROSION AT LT STA 294, AT BUTTLINE 19 LT SIDE SEAT TRACK ON FLOORBOARD FLANGE. TIMCO MAINTENANCE REPAIRED SEAT TRACK IAW MESABA AIRLINES EO A53060 BY REPLACING SEAT TRACK AT STA 294 LBL 19. REFER TO CONTINUATION CARD 048531 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20031219000402003121900040NM 2003 12 19 F3LA200300157 120031205A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 996, BL 0. REMOVED OLD INTERCOSTAL FROM STA 986.5 TO STA 1006, BL 0. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA B3-53R-10242 AND SRM 51-40-02. 2L72 4F RTA16WE 20031217001312003121700131NM 2003 12 17 SWAA032713 120031211A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN HAS CRACK AT 727D STRINGER 23R. REPAIRED CRACK PER SRM. 2L72 4F RTA16WE 20031222001022003122200102WP 2003 12 22 AALA20031076 120030928A7100 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 BIRD INGESTION A AALAA UNSCHED LANDING C F.O.D. CRCRUISE 1 SW21432AA 49350 EN ROUTE, AIRCRAFT ENGINE INGESTED BIRD INTO THE NR 2 ENGINE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT OVERWEIGHT INSPECTION PERFORMED. REPLACED THE NR 2 ENGINE. LEAK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20031222001382003122200138EA 2003 12 22 COMA0360539 120031207A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01917CA 7017 FLIGHT 5184 CABIN DOOR WARNING - AIRCRAFT WOULD NOT PRESSURIZE. CLEANED AND LUBED DOOR LATCH, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20031223000162003122300016NM 2003 12 23 SWAA032658 120031203A335065C27093 LIGHT BOEING737 7372T4 1384492NM ROW 3 INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C1 CHECK, FOUND AISLE OVERHEAD EMERGENCY LIGHT INOP AT ROW 3. RELAMPED PER MM. 2L72 4F A16WE 20031229001062003122900106NM 2003 12 29 AWXA200301550 120031202A5320672036 BEAM BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-04 CHECK 2 EACH CRACKS WERE FOUND COMING FROM INSULATION PIN HOLE ON VERTICAL BEAM WEB IN FORWARD E & E COMPARTMENT BS 179.5, RBL 5.7, WL 173.25. MAINTENANCE CUT OUT CRACKED AREA OF VERTICAL BEAM WEB BS 179.5, RBL 5.7, WL 173.25; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG 228, FIG 212. 2L72 4F RTA16WE 20031229000922003122900092NM 2003 12 29 DHL2003742510 120031120A5311 FRAME BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CABIN CRACK FRAME STA 380 ATTACH TO TOP OF R1 DOOR FRAME. REMOVED FASTENERS FOR ACCESS AS REQUIRED FOR REPAIR IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA DIMENSION 2 INCH X 1 INCH IAW B-727 SRM 53-10-4 FIG 1. FABRICATED REPAIR MAT USED 7075 T6 .063 PO 900226 DIM 6 INCH X 2 INCH AND FILLER MAT USED 7075 T6 .050 PO 90096 DIM 2 INCH X 1 INCH IAW B-727 SRM 53-10-4 FIG 1. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. 2L73 4F A3WE 20040105000422004010500042EA 2004 1 5 SWIA200312681 120031207A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM ACT FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07906SW2703 2703 7510 STAB TRIM CH 2 WILL NOT TEST AND DISCONNECTS WHEN STAB TRIM SWITCH IS EXERCISED. INSTALLED SERVICEABLE MCU AND HORIZONTAL STAB TRIM ACTUATOR IAW 27-42-01, REF RII CARD 27-415. HSTA P/N: 8396-3, S/N OFF: 278, OPS CHECKS GOOD. 2L72 4F RTA21EA 20040108000542004010800054NM 2004 1 8 IU62003F00037 120030917A291365447821 HOUSING BOEING737 737* NM ISOLATION VALVE CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 62254 1106 HOUSING IS CRACKED ON THE BACKSIDE OF PORT 2. METAL FATIGUE OVER TIME. REPLACE HOUSING ASSY. 2L72 4F RTA16WE 20040109000682004010900068NE 2004 1 9 2004F00006 220031005A7397 WIRE STBROSSD3 SD360 8100606EU PWA PT6 PT6A60A 52043NE TRANSMITTER BROKEN A PIVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13711MP SH3698 ABORTED TAKEOFF DUE TO LT ENGINE NO FUEL FLOW INDICATION. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED, FOUND BROKEN WIRE AT FUEL FLOW TRANSMITTER. WIRE WAS REPAIRED AND AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 T A41EU E4EA 20031202001242003120200124EA 2003 12 2 A6WA200340150 120031020A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31456ZW 7849 FLAP FAIL CAS MESSAGE AFTER TAKEOFF. COMPLIED WITH QRH, FLAPS AT ZERO. AIR RETURN, REMOVED AND REPLACED RIGHT BRAKE POSITION SENSING UNIT IAW MM 27-51-10. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040121000572004012100057EA 2004 1 21 ASOA03598 120031122A5210601R380742 ANCHOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11906EV 7642 DURING A C-CHECK IN MCN, THE FORWARD AND AFT ANCHOR MOUNTS ON THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT ANCHOR MOUNTS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040115001282004011500128NM 2004 1 15 03FDEA02106 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCKBOLT COLLAR CRACKED. GAIN ACCESS FROM PANEL 363PL. LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM51-33-01 VOL 2 2L73 4F RTA22WE 20031205000142003120500014EA 2003 12 5 CTO13098 120031023A282285816 PUMP DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA FUEL TRANSFER FAILED Z A UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 SW99VPCTO5100 5100 773 DURING CRUISE NR 1 FWD ELEC FUEL BOOST PUMP LOW PRESS WARNING LIGHT ILLUM. PULLED C/B. WITHIN MIN, PUMP NR 1 FWD PUMP FAILURE, NR 1 AFT ELEC FUEL BOOST PUMP LOW PRESS WARNING LIGHT ILLUM. PULLED C/B & RETURNED. UPON RESET OF C/B'S, SMOKE OBSERVED COMING FROM WIRING ACCESS OPENING ON AFT PUMP. BOTH PUMPS REMOVED & REPLACED. LEAK CHECKS C/O. TEARDOWN INDICATES FUSING OF COMMUTATOR INSIDE PUMP. ALSO INDICATES THAT CONDITION OF PUMP IS TYPICAL OF THIS P/N PUMP. OVERHAULER INDICATED MOST P/N 85816 UNITS SMELL BURNED & COMMUTATOR REPLACED DUE TO MELTING/FUSING. APPROX 6 PUMPS THIS STYLE FAILED WITHIN PAST 12 MO. TEARDOWN REPORTS ALL SIMILAR. SOME UNITS LASTED NO LONGER THAN 400 HRS FROM OVERHAUL. 1H72 3T4 TRTA9EA E4EA 20031208001192003120800119NM 2003 12 8 AWXA200301317 120031008A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM AT NUT PLATE HOLES BS 773, RBL 8. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF FLOORBEAM BS 773, RBL 8; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 PG 1 FIG 201. 2L72 4F RTA16WE 20031204000982003120400098WP 2003 12 4 UPS03841409 120030911A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT FUSE INTERIOR L17 RT END FITTING CRACKED BETWEEN FS 1766-FS 1772. REMOVED L17 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20031209001462003120900146NM 2003 12 9 QXEA200301361 120031023A3222 STRUT DHAV DHC8 DHC8202 2809007NM ZONE 700 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 NOSE LANDING GEAR STRUT IS CHAFED AT FORWARD EDGE EIGHT INCHES BELOW PROX SENSOR. REPAIRED DHC-8 RD 8-32-289. 2H72 4T RTA13NM 20031210000102003121000010NM 2003 12 10 03FDEA02124 120031128A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031210001012003121000101NM 2003 12 10 DHL2003741012 120031126A5753 STRUCTURE BOEING727 7272Q9 138448MNM T/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LT WING INBOARD AFT FLAP HAS 3 INCH CRACK AT L/E. REMOVED AND REPLACED AFT FLAP ASSEMBLY IAW B727-200 M/M CHAPTER 27-51-02. OPS CHECK REQUIRED. PERFORMED OPS CHECK IAW B727-200 M/M CHAPTER 27-51-02. OPS CHECKED GOOD. 2L73 4F RTA3WE 20031014000052003101400005EU 2003 10 14 BAQA089600 120031006A28221176415103 PUMP BOLKMS117 BK117A1 5626010EU FUEL BOOST MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 PRIME PUMP NOT SUPPLYING ENOUGH PRESSURE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031021000802003102100080SO 2003 10 21 SIMA200324608 120030814A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFE BLENDING AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ONE REPAIR ANGLE, TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2633, IC2003-145/2718A AND STANDARD EMB SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030924000542003092400054NM 2003 9 24 DLM88030769 120030815A3350 WIRE DOUG MD88 MD88 3023688NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27933DL 49720 ON INSPECTION, FOUND EMERGENCY PATH LIGHTING INOPERATIVE FROM ROWS 31-38 FOUND BROKEN WIRES AT ROW 36. REPAIRED WIRING AND LIGHTS NOW OPERATE NORMALLY. 2L72 4F RTA6WE 20040128000482004012800048WP 2004 1 28 MWEA030498 120031227A2410696233B CSD DOUG DC9 DC982 3022082WP LEFT CONTAMINATED A MWEAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL31809ME 48071 LEFT CONSTANT SPEED DRIVE OIL PRESSURE LOW ANNUNCIATOR ILLUMINATED. FOUND MAGNETIC CHIP DETECTOR CONTAMINATED WITH METAL AND BRASS SHAVINGS. REMOVED AND REPLACED LEFT CONSTANT SPEED DRIVE. 2L72 4F A6WE 20040130000622004013000062WP 2004 1 30 UPS04841695 120031230A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LONGERON 33R CORRODED AT STA 1480. CUT OUT CORRODED SECTION OF LONGERON 33R FROM STA 1470 TO 1490. FABRICATED AND INSTALLED REPLACEMENT SECTION PER SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040130000882004013000088NM 2004 1 30 DHL2003742567 120031125A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 5 SEAT TRACK AT BS 760-850 IS DAMAGED. REMOVED SEAT TRACK AT BS 760-850 FOR REPAIR IS OUT OF LIMITS IAW B727 SRM 51-30-2 AND 51-10-1 FIG 3, FABRICATED NEW SEAT TRACK AS PER SAMPLE IAW B727 SRM 51-10-1 DIM 95 INCHES USED BAC-1520-841 PO 323569 IAW B727 SRM 51-10-2, INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040205000132004020500013WP 2004 2 5 IXXA0300075O 120031115A2120 ODOR DOUG DC8 DC871 302199AWP GE CFM56 CFM56* 13802NE CABIN DETECTED A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW11829BX8687137 45994 DURING CRUISE AN ELECTRICAL ODOR WAS IN THE CEILING AREA OF THE FLT STATION DOOR AND COURIER COMPARTMENT. CREW TURNED OFF THE CIRCUIT BREAKER LIGHT SWITCH ON THE F/E PANEL AND ODOR DECREASED. MAINTENANCE RAN COCKPIT AND COURIOUR LIGHTING FOR 3 HOURS ON GROUND AT SJC. THEY INSPECTED BALLAST POSITIONED IN OVERHEAD ABOVE COCKPIT ENTRY DOOR, INSPECTED B61 BALLAST THAT OPERATES CIRCUIT BREAKER LIGHTS. NO DEFECTS NOTED. SYSTEM CHECKED NORMAL IAW ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 E2GL 20040217000172004021700017EU 2004 2 17 ASOA03681 120031201A5320 SILL AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE RIGHT SIDE WALL SILL PLATE BETWEEN FS 39-41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE WALL SILL PLATE BETWEEN FS 39-41 IAW SRM 51-25-02. (M) 2H72 4T RT 20040217000862004021700086NE 2004 2 17 NACA20030128 220031227A7421 SPARK PLUG PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 9 CYLINDER FOULED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL0343872203 203 234905 533294 P32204 NR 3 ENGINE SHUT DOWN DUE TO DOUBLE SHORTED SECONDARY NR 9 CYLINDER. REPLACED NR 3 ENGINE, NR 9 CYLINDER FRONT AND REAR SPARK PLUGS. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040301001042004030100104EU 2004 3 1 RYN2004F00005 120031019A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 34 AT STRINGER 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT FROM FRAME 31 TO 34, STRINGER 34L IN FORWARD PIT. 2L72 4F4 FRTA28NM E40NE 20040329000282004032900028NM 2004 3 29 USAASB03223 120031226A212065C280023 DUCT BOEING737 7373B7 1384580NM CABIN PRESSURE RUPTURED A USAAO OTHER J WARNING INDICATION CRCRUISE 1 EA19374US 22953 FLT DEPARTED WITH LT PACK ON MEL 21-1A. EN ROUTE AT FL250, RT PACK UNABLE TO HOLD CABIN PRESSURE AS CABIN PRESSURE WENT TO 10,000 FT. CREW DESCENDED TO FL200 BUT CABIN PRESSURE WOULD NOT COME DOWN UNTIL 16,000 FT. FLT CONTINUED ON & LANDED WITHOUT FURTHER INCIDENT. MAINT R/R LT MIX MANIFOLD DUCT FOUND RUPTURED. HOOKED UP DISCONNECTED COCKPIT SUPPLY DUCT. REPLACED OVERHEAD PANEL DUE TO LIMITED CONTROL IN AUTO & MANUAL. REPLACED LT AIR CON ANTICIPATOR & DUCT LIMITER DUE TO PACK TRIP WHEN PACK SELECTED IN AUTO OR MANUAL. REPLACED RT AIR CON MIX VALVE DUE TO NOT TRAVELING TO FULL RANGE IN AUTO MODE. OPERATIONAL TEST & HULL LEAK RATE NORMAL. CLEARED MEL 21-1A FOR LT PACK. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20031212001442003121200144WP 2003 12 12 AALA20030952 120030903A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21234AA 49181 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT SEAT ROWS 27 THROUGH 31. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040622001442004062200144CE 2004 6 22 AMWA114 120031030A531311443007335 STRINGER BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE23 WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, SKIN UNDER STRINGER 10R WAS FOUND CRACKED. 2L72 4T RTA24CE 20030926001552003092600155WP 2003 9 26 ARWA20030807 120030821A5310 DOOR FRAME DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45688 DURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT SERVICE DOOR JAMB, AFT TOP CORNER WITH CRACK OF 1.125 INCH. REPAIRED THE AFT SERVICE DOOR JAMB AFT TOP CORNER IAW SRM 53-2-0 FIG 16, SHEETS 4, 5, 6, 7 & 8 TEMPORARY REVISION 53-156, DATED 12/20/02. (EA 1021, DATED 08/21/03). 2L74 4F 4A25 20060801001402006080100140WP 2006 8 1 IXXA060583S 120030912A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND INTERCOSTAL CORRODED FROM STATION 1380 TO STATION 1390 AT LONGERON 33 LEFT. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-8, 53-4-0, AND 51-1-21. 2L74 4F RT4A25 20030819001692003081900169CE 2003 8 19 DXTA200300042 120030605A323081902 MANIFOLD CESSNA750 750 2076810CE MLG CONTROL FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07964QS 7500164 LANDING GEAR WOULD NOT RETRACK UPON RETRACTION, LT GEAR C/B POPPED, RESET ONCE TRIED ONE TIME, GEAR WOULD NOT RETRACT. USED GEAR BLOW DOWN BOTTLE TO ENSURE DOWN AND LOCKED. REMOVED AND REPLACED LANDING GEAR CONTROL MANIFOLD IAW 750 M/M 32-30-02, OPS AND LEAK CHECK GOOD. 2L72 4J RTT00007WI 20030820000262003082000026NM 2003 8 20 03FDEA01176 120030728A5320A5A7116503 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 CENTER CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 45L SPLICE FITTING FOUND CRACK. CENTER CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 45L SPLICE FITTING REMOVED & REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20030818000962003081800096SW 2003 8 18 ALGA088202 120030724A6200406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03497AL520 53172 MAIN ROTOR UNIVERSAL ROUGH, WORN AND BINDING. BEARING ASSY. REPLACED BY FIELD MAINT. 1G71 3U O H2SW 20030328000532003032800053NM 2003 3 28 C8GA20030005 120030227A32601061226211 DOWNLOCK BOEING727 727223 1384074NM MLG DEFECTIVE A C8GAO OTHER J WARNING INDICATION APAPPROACH 1 SO15708AA 22465 FLIGHT 705 FROM KMSP TO KTOL. ON APPROACH INTO TOLEDO, THE LEFT HAND MAIN GEAR INDICATED UNSAFE RED LIGHT ON. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST A-06-4. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE LEFT HAND GEAR DOWNLOCK CARD IN THE LANDING GEAR ACCESSORY UNIT WAS REPLACED. OPERATIONAL CHECKS WERE ACCOMPLISHED IAW MM 32-09-121 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030331001012003033100101NE 2003 3 31 CH1A200381010 220030327A7200 ENGINE BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 STALLED A C1HAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 GL15681CA 22020 ON TAKEOFF ROLL NR 2 ENGINE COMPRESSOR STALLED NR 2 EPR DROPPED TO 1.2 AUTO PACK TRIP SYSTEM ACTIVATED 2L73 4F4 F A3WE E2EA 20030401000602003040100060WP 2003 4 1 CA030225001 220030221A7314307085063 PUMP LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP FUEL FAILED W C ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 CA 10877 (CAN) AIRCRAFT WAS AT 70 KNOTS ON TAKE-OFF ROLL WHEN LT ENGINE FLAMED OUT. CREW REJECTED TAKE OFF. TROUBLESHOOTING FOUND LT ENGINE DRIVEN PUMP AT 30 PSI. AMM STATE MINIMUM 300 PSI. PUMP REPLACED. AIRCRAFT RETURN TO SERVICE. 2L72 4F4 F A10CE E6WE 20030821002512003082100251NM 2003 8 21 03FDEA01352 120030821A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CORROSION ON CHORDS IN NLG BAY AT B/S 284, LBL 18 INSIDE TORQUE BOX O/B OF STRUT DOOR FWD HINGE. REMOVED AND REPLACED LT CHORD AT B.S. 284, LBL 18 PER SRM 51-30-02. PERFORMED FUNCTIONAL TEST OF NLG PER M/M 32-22-001-5. FUNCTIONAL TEST GOOD. 2L73 4F RTA3WE 20030821002702003082100270EU 2003 8 21 2003F00517 120030809A36106774E010000 REGULATOR AIRBUS320 A320233 3930329EU NR 1 ENGINE STUCK A RJEFA UNSCHED LANDING O OTHER CRCRUISE 1 SO23462TA 1334 SAL - FLT 581 - DURING CRUISE, ENGINE NR 1 BLEED VALVE REMAINS CLOSED AND THE ENGINE NR 2 PRECOOLER REACHED THE LIMITS IN A SINGLE BLEED OPERATION. THE AIRCRAFT WAS DEVIATED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAL, TECHS REPLACED THE PRESSURE REGULATOR BLEED VALVE ON ENGINE NR 1 PER AMM 36-11-52, ON ENGINE NR 2 THE FAN AIR VALVE CONTROL THERMOSTAT (P/N 342B030000, WAS REPLACED PER AMM 36-11-43. AN ENGINE RUN UP WAS PERFORMED PER AMM 71-00-00. BLEED SYSTEM WAS OPERATIONG NORMALLY. ALSO, A TEST FLIGHT WAS PERFORMED PER AMM 71-00-00. BLEED SYSTEM WAS OPERATING NORMALLY. ALSO, A TEST FLIGHT WAS PERFORMED. ALL RESULTS WERE SATISFACTORY AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20030403000682003040300068NM 2003 4 3 AWXA200300330 120030321A532065353654 ANGLE BOEING737 7373G7 1384595NM INTERCOSTAL CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 DURING C-17 CHECK A 5/16 INCH CRACK WAS FOUND AT FASTENER HOLE ON CABIN AREA INTERCOSTAL UPPER SUPPORT ANGLE, BS 500D TO BS 520, BL 0. MAINTENANCE REMOVED INTERCOSTAL UPPER SUPPORT ANGLE, BS 500D TO BS 520, BL 0; FABRICATED A NEW REPLACEMENT UPPER SUPPORT ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG. 10, 11, & 35, FIG. 8. 2L72 4F RTA16WE 20030409000032003040900003WP 2003 4 9 03FDEA00400 120030408A5350 INTERCOSTAL DOUG DC10 DC1030 3023501WP TAILCONE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25320FE 47835 N 132 TAILCONE LT MAINT PLATFORM WEB IS CRACKED BETWEEN 2EA ACTUATOR ROD/STIFFNERS/ SUPPORT ANGLES PARALLER TO MAINT PLATFORM AT NON-SKID AREA. CLOSING ACTION ON 04/07/03. REMOVED CRACKED DOUBLER AND INTERCOSTAL IAW SRM 51-35-01. FABRICATED REPAIR DOUBLER IAW DC-10 SRM 53-52-01,53-00-01. FABRICATED NEW INTERCOSTAL ON M.A.E. TRAVELER T2/325492. INSTALLED NEW REPAIR DOUBLER AND INTERCOSTAL IAW DC-10 SRM 51-35-01. 2L73 4F A22WE 20030411000042003041100004NM 2003 4 11 SWAA030719 120030329A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND BS 1016 BULKHEAD CRACKED (5 EA) AT THE 12, 1 AND 3 O`CLOCK POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA AND SRM. 2L72 4F RTA16WE 20030410002322003041000232EU 2003 4 10 BAQA085816 120030325A6330L633M2010101 MOUNT UROCOPEC135 EC135T1 5620026EU LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03511ME237 0143 LEAKING. PIN NOT STICKING OUT UNDER A LOAD. REPLACED WITH SERVICEABLE UNIT 1G72 3U H88EU 20030416002292003041600229NM 2003 4 16 SWAA030776 120030407A27509004212 SENSOR BOEING737 7377H4 1384404NM RT WING TE FLAPSFAULTY A SWAAL ABORTED APPROACH PF NO WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SW29738CB 27870 DECLARED EMERGENCY, DURING APPROACH T/E FLAPS STOPPED AT POSITION 2. REMOVED AND REPLACED NR 6 T/E FLAP SKEW SENSOR PER MM. 2L72 4F RTA16WE 20030417001402003041700140NM 2003 4 17 ZW0A0301805 120030205A3350 POWER SUPPLY DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139420D 49824 THE EMERGENCY OVERHEAD LIGHTS WERE INOPERATIVE AT THE L2 DOOR, FWD AND AFT OF L2 DOOR IN AISLE, MID SECTION OF AIRCRAFT APPROXIMATELY 8 ROWS OF EGRESS LIGHTS, AND AFT MOST EGRESS RED LIGHT ADJACENT TO LAVS. REPLACED POWER SUPPLY PN 60-0304-51LB FOR L2 DOOR AND ADJACENT AISLE, BATTERIES RECHARGED FOR MID CABIN EGRESS LIGHTS, AND REPLACED MODULE PN 010-5606-004 FOR RED LIGHT ADJACENT TO AFT LAVS. CHECK-C 11-6-02 STL. 2L72 4F RT 20030424001562003042400156NM 2003 4 24 QXEA0300403 120030325A2910 LINE BOMBDRDHC8 DHC8401 1390041NM ZONE 700 LEAKING A QXEAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM09401QX 4031 SEA ON FLIGHT 2293- AT GEAR EXTENSION DOOR WOULD NOT CLOSE. NR 2 HYDRUALIC QUANTITY SHOWED VERY LOW, NEAR ZERO. CREW EXECUTED A MISSED APPROACH AND PERFORMED ALTERNATE GEAR EXTENSION. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR RIGHT HAND RETRACT ACTUATOR DOWNLOCK UPPER FLEX LINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424001872003042400187CE 2003 4 24 I5WA933J 120030213A575365251252 SKIN CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE TE FLAP DAMAGED E I5WAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SO0592ME S5500044 ON 2/10/2003, AIRCRAFT WAS AT CRUISE ALTITUDE (FL350). THE CREW HEARD A LOUD BANG NEAR THE AFT BAGGAGE AREA. THE AIRCRAFT THEN BEGAN TO VIBRATE. THE SIC WALKED TO THE REAR OF THE AIRCRAFT AND NOTICED DAMAGE TO THE RIGHT OUTBOARD FLAP. THE SIC THEN INFORMED THE PIC AND THEY REQUESTED A RETURN. THE AIRCRAFT DEMONSTRATED GOOD CONTROLLABILITY ABOUT ALL AXIS. THE CREW DECIDED TO LAND WITH FLAPS 7 DEGREES (LESS VIBRATION). AN EMERGENCY WAS NOT DECLARED. AFTER LANDING, IT WAS DETERMINED THAT THE OUTBOARD FLAP TO BE DAMAGED ON THE UPPER AND LOWER SURFACES. A 12 INCH X 12 INCH PIECE WAS MISSING ON THE LOWER SURFACE OF THE FLAP. 1L72 4F4 FRTA22CE E1NE 20030429001142003042900114EU 2003 4 29 RAIA00304102 120030404A3234F96GA0102 LEVER AEROSPATR72 ATR72202 8680940EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03723TE2467111846 283 SBN- LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER, OPS CHECK OK. 2H72 4T RTA53EU 20030430001902003043000190NM 2003 4 30 SWAA030936 120030427A3350BR9442 LIGHT BOEING737 7373H4 1384600NM FWD ENTRY INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 FWD ENTRY EMERGENCY EXIT LIGHT NEXT TO F/A SEAT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030501000122003050100012EA 2003 5 1 ASOA03099 120030310A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11860AS 7433 FLT 4711 - DURING A GROUND INSPECTION IN DFW, THE RIGHT OVERWING EMERGENCY EXIT AND THE FORWARD CEILING EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030502001822003050200182EU 2003 5 2 AWXA200300408 120030331A5311D53370303206 FRAME AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A .1875 INCH CRACK WAS FOUND AT THE FORTH FASTENER HOLE DOWN ON FRAME 41, BETWEEN STR 14-15 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME 41 BETWEEN STR 14-15 LT; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA EO 53-14-20. 2L72 4F RTA28NM 20030506002242003050600224WP 2003 5 6 ASAA0380197 120030303A57535910042509 STRUCTURE DOUG DC9 DC982 3022082WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND LEFT FLAP MID VANE OUTBOARD UPPER TRAILING EDGE CHAFED. REPAIRED CHAFED AREA PER SRM 51-70-2. (M) 2L72 4F A6WE 20030508000812003050800081NE 2003 5 8 COMA0360229 220030504A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE LOW A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01719CA 7253 807408 FLIGHT 5533 RT ENGINE OIL PRESSURE WARNING. SERVICED RT ENGINE WITH 4.75 QTS OF OIL. 2L72 4F4 FRTA21EA E15NE 20030926000902003092600090EA 2003 9 26 ACE082503 220030825A73208061328A FUEL CONTROL BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA NR 2 ENGINE FAULTY E YADAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL03112AX5327 UC45 PCE97546 NR 2 ENGINE STARTED TO SURGE AND THEN LOST POWER - PILOTS SECURED THE ENGINE AND MADE AN UNEVENTFUL LANDING AT THE AIRPORT OF ORIGIN. REPLACED FCU. 2L72 4T4 TRTA24CE E4EA 20030820000242003082000024NM 2003 8 20 03FDEA01005 120030625A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RT WING INBOARD FLAP AFT HINGE INBOARD PIVOT LUG BORE FOUND CORROSION. RT WING INBOARD FLAP AFT HINGE INBOARD PIVOT LUG BORE CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69360 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBOARD FLAP HINGE BRACKET ASSEMBLY REPAIR. 2L73 4F RTA22WE 20030820002062003082000206EU 2003 8 20 ASOA03325 120030710A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FS 36/39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FS 36/39 IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20030820002372003082000237NM 2003 8 20 USAASB03118 120030720A3350210310005 FUSE BOEING737 7373B7 1384580NM EMERGENCY LIGHT BLOWN A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU 23704 MAINTENANCE REPORTED THE LEFT OVERWING HATCH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE IN POWER SUPPLY M1134 AND A BAD PLUG ON THE EMERGENCY SIGN. REPLACED FUSE AND PLUG. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030821000672003082100067NM 2003 8 21 03FDEA00916 120030618A5753ARC199113 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE FOUND CORROSION. LEFT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE REPAIRED AS PER FEDEX EA 1-5750-69372, TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821001322003082100132EU 2003 8 21 03FDEA00891 120030616A7830491B1220000019 BLOWOUT DOOR AIRBUS300 A300B4605R 3930308EU THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 EXHAUST- THRUST REV - BLOWOUT DOOR SKIN REPAIR. FACT 16JUN03 05:39 BFM R COMPLIED WITH EA 6-7832-70933 PT1 EXHAUST- THRUST REV - BLOWOUT DOOR SKIN REPAIR AT BFM/MAE. 2L72 4F RTA35EU 20030407000012003040700001WP 2003 4 7 ASA0380065 120030109A532199365997 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 FOUND DURING 30K CHECK, FORWARD CARGO BAY FLOOR PANEL IS PUNCTURED AND FS 330-370. REPLACED SECTION OF FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030401000692003040100069NE 2003 4 1 CA030228012 220030220A8530116733 CYLINDER DOUG DC3 DC3CS1C3G 3021458WP PWA R1830 R183092 52020NE EXHAUST CRACKED W O OTHER K FLUID LOSS DEDESCENT 1 CA (CAN) DURING DESCENT INTO YAM WITH POWER BACK, OIL WAS NOTED ON RT NACELLE AREA. UPON LANDING UNEVENTFULLY, THE NR 1 CYLINDER WAS FOUND CRACKED. THE CYLINDER WAS REPLACED WITH AN OVERHAUL UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4R4 R A669 5E4 20030404000152003040400015NM 2003 4 4 CALA0300162 120030401A5312 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND TWO 0.1 INCH CRACKS AT RIVET HOLES IN AFT PRESSURE BULKHEAD BETWEEN S6L AND S7L AT BS 1016. REPAIRED IAW SRM 53-80-08, FIGURE 202 AND 207. 2L72 4F RTA16WE 20030411000152003041100015NM 2003 4 11 SWAA030754 120030404A33506040681 BATTERY BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030414000362003041400036NM 2003 4 14 MEX2003052 120030301A3150 SWITCH DOUG MD80 MD83 3023681NM TAIL CONE OUT OF POSITION W ASMFA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23945AS 49643 AIRCRAFT RETURNED TO PLATFORM DUE TO ROTATION TAIL CONE LIGHT ILLUMINATED. DURING CHECK WAS DETECTED SWITCH OUT OF ITS POSITION. MECHANISM WAS CHECKED AND TAIL CONE LIGHT TURNED OFF. TEST WAS PERFORMED IAW MM. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM, ALL CORRECT. 2L72 4F RT 20030410001562003041000156NM 2003 4 10 SWAA030710 120030329A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 799, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030414001162003041400116EA 2003 4 14 CA030305007 120030219A5510C2TP57 SPAR DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE LT STAB ATTACH CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) REMOVED STABILIZER P/N C2-TP-1A AND LT AND RT ATTACH BRACKETS P/N C2-TP-159 AND -160 FOR INSPECTION AS PER AD CF-91-42 AND SB 2/47. - FOUND CRACK IN SPAR ABOVE LT BRACKET ATTACH POINT. 1H71 3R3 R A806 5E1 20030416003982003041600398NM 2003 4 16 P5CA0300721 120030112A541565B913141 FITTING BOEING747 7472U3B 1384846NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 FIVE CRACKS TOTAL FOUND NR 3 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1.5 INCH & (1) .75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX .5 INCH & (2) .125 INCH EA RADIALLY. CRACKED BATHTUB FITTING REPLACED AS PER SB 747-54-2113-R2. 2L74 4F RTA20WE 20030416002632003041600263NM 2003 4 16 QXEA0300434 120030402A323382910016009 ACTUATOR DHAV DHC8 DHC8202 2809007NM ZONE 700 FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09353PH1302313023 496 ON FLIGHT 2029 AFTER GEAR EXTENSION ON APPROACH NOSE GEAR UNSAFE (RED) LIGHT ON AND NO GREEN OR AMBER LIGHT ILLUMINATED. RETRACTED GEAR AND EXTENDED AGAIN WITH THE SAME RESULT. NOSE GEAR EXTENDED AFTER ALTERNATE GEAR EXTENSION METHOD ONE. REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513001732003051300173NM 2003 5 13 2003UALA00381 120030415A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 FUSELAGE SKIN DENT 15 INCHES BELOW AND 18 INCHES AFT OF FWD LAV SERVICE PANEL. MANUFACTURED AND INSTALLED REPAIR STRAP AND DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030530001242003053000124NM 2003 5 30 2003F00354 120030425A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM NR 1 WILL NOT TEST A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13806WP 357 HNL - NR 1 SMOKE DETECTOR INOPERATIVE DURING TEST MODE. REMOVED 4 SCREW AND 2 BOLTS, REMOVED SMOKE DETECTOR AND CANNON PLUG. INSTALLED NEW SMOKE DETECTOR WITH 4 SCREWS AND 2 BOLTS AND SECURED CANNON PLUG WITH SAFETY WIRE. OPS CHECK GOOD AIW DHC-8 MM CHAPTER 26-12-00 PAGE 201. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030610000772003061000077NM 2003 6 10 DLM88030418 120030504A3246 BEARING DOUG MD88 MD88 3023688NM NLG WHEEL NOISY A DALAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO27902DE 53379 LOUD NOISE IS COMING FROM THE NOSE WHEEL AREA. FOUND LT NOSE WHEEL BEARING FAILED. REPLACED WHEEL ASSY 2L72 4F RTA6WE 20030613000532003061300053NM 2003 6 13 0301086302 120030603A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK FOUND RIGHT FLOOR PATH EMERGENCY LIGHTS INOP IN A & 1/B ZONES. RECONNECTED AND SECURED WIRING. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030523000872003052300087NM 2003 5 23 QXEA0300547 120030508A2710 AILERON DHAV DHC8 DHC8202 2809007NM ZONE 100 OUT OF ADJUST A QXEAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM09357PH 504 LWS-ON FLIGHT NUMBER 2710, CREW NOTICED CONTROLS WERE HEAVY. ADJUSTED AILERON CABLE TENSION AND SPOILER SYSTEM. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030527000282003052700028NM 2003 5 27 DL733030322 120030401A5330655298812 SKIN BOEING737 737347 1384647NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 A DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STA 1000 AND 1016 AND BETWEEN STRINGERS 13L AND 14L THE DENT IS CUT OUT AND EXTERNAL DOUBLER AND FILLER ARE INSTALLED SIMILAR TO B737-200 SRM 53-30-3, FIG 48 BUT IN ACCORDANCE WITH ER/A 384711-14. 2L72 4F RTA16WE 20030528000272003052800027GL 2003 5 28 ALGA086421 220030515A723023051123 MOUNT CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30S 03013GL COMPRESSOR MISMANUFACTURED E ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01PARTO CAE890773S FOUND MOUNT PAD MEASURING BELOW MIN. LIMITS. 1Q71 3R3 U 2A6 E1GL 20030617002872003061700287WP 2003 6 17 GTIA030339 120030409A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FTW - AFT LOWER CARGO, LOWER DOOR JAMB CUTOUT CORROSION AT DOUBLER REPAIR, ATTACH TO O/B BEAM. REMOVED DOOR JAMB BEAM STATION 1114 TO 1249. LOCATED AND DRILLED NEW JAMB BEAM STATION 1114 TO STATION 1249. INSTALLED NEW JAMB BEAM. (M) 2L72 4F A6WE 20030618001992003061800199SW 2003 6 18 HEEA087368 120030611A5210407070620143 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 CREW DOOR PANEL CRACKED. 1G71 3U O H2SW 20030619000352003061900035GL 2003 6 19 HEEA087189 220030609A753223007827 VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 ANTI ICE SYSTEM INTERMITTENT. SCRAPPED. 1G71 3U3 U H2SW E1GL 20030619000862003061900086SW 2003 6 19 HEEA087224 120030609A2420SM20ACD200A21 RELAY BELL 206 206L3 1182108SW GENERATOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 WHEN GEN. SWITCH IS TURNED ON IT TOOK 2 TO 3 MINUTES TO COME ON. ALSO GEN DROPPED OFF LINE IN FLIGHT. 1G71 3U H2SW 20030620000132003062000013SW 2003 6 20 HEEA086940 120030603A3212206050247132 COVER BELL 407 407 1182206SW FLOAT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 FLOAT COVER CRACKED AND HAS HOLES. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030707001042003070700104WP 2003 7 7 UPS03840857 120030616A571098874279 STIFFENER DOUG DC8 DC873F 302199FWP LEFT WING TE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LEFT WING TE. VERTICLE STIFFNER IS CRACKED TWO PLACES AT XW 11.5 REMOVED,FABRICATED AND REPLACED STIFFNER I.A.W. DWG. 9887427 AND SRM 51-1-20D. 2L74 4F RT4A25 20030714001612003071400161EU 2003 7 14 I05R088094 120030625A671041800847100 ACTUATOR UROCOPEC135 EC135P1 8680990EU FLIGHT CONTROLS VIBRATES E I05RO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 WP05552BA 190 AIRCRAFT HAD A VERTICAL VIBRATION. REPLACED PART. 1G72 3U O H88EU 20030716000152003071600015NM 2003 7 16 GAIA03019OP 120030619A56105717623097 WINDOW BOEING727 727224 1384076NM COCKPIT MALFUNCTIONED A GAIAK NONE O OTHER ININSP/MAINT 1 SW0769740 20668 DURING ROUTINE MAINTENANCE AT IAG, IT WAS DISCOVERED THAT THE CAPTAINS SLIDING WINDOW WOULD NOT CLOSE. ADJUSTED CAPTAINS SLIDING WINDOW PER 727 AMM CH 56-12-11. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030424001922003042400192SO 2003 4 24 SWIA200311843 120030323A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07560SW6939 6939 120334 EMERGENCY LIGHTS DO NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY IAW EMB 120 MM 33-50-1. 2L72 4T RTA31SO 20030425000032003042500003WP 2003 4 25 UPS03840381 120030315A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, R2 UPPER AFT DOOR JAMB CORNER CRACK NOTED AT LONG 11R EXTENDING FROM FASTENER HOLE. CUT OUT CRACKED AREA, FAB & INSTALLED SKIN FILLER -19 -21 DOUBLERS IAW DC8 SRM 53-2-0 FIG 16. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2L74 4F RT4A25 20030428001772003042800177CE 2003 4 28 GLBA2003045 120030408A2810 FUEL CAP BEECH 1900 1900D 1154162CE LOOSE A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03208GL UE208 LEFT INBOARD FUEL CAP LOOSE. SECURED FUEL CAP. 2L72 4T RTA24CE 20030429001392003042900139NM 2003 4 29 AUS20030293 120030212A5311 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FRAME FORMER LOCATED AT BS 1090 BETWEEN STRINGER 28R AND STRINGER29R CONTAINED LEVEL 2 CORROSION ON AFT FACE. FOUND DURING CPCPINSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030502000632003050200063WP 2003 5 2 ASAA0380175 120030301A532199365997 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND MID CARGO BAY FLOOR PANEL IS GOUGED IN SEVERAL PLACES ALONG EDGE. REPLACED PANEL PER SRM 51-10-2 AND 10-4. (M) 2L72 4F A6WE 20030506000942003050600094WP 2003 5 6 MWEA030184 120030428A5530591214160 ANGLE DOUG DC9 DC981 3022081WP VERTICAL STAB CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 RIGHT VERTICAL STABILIZER ATTACH ANGLE IS CRACKED IN RADIUS AT FRAME STATION 1437. FABRICATED AND INSTALLED ANGLE AND INSTALLED FILLER AND WASHERS. 2L72 4F A6WE 20030508000882003050800088NM 2003 5 8 AWXA200300474 120030410A5315654541025 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 4 1/2 INCH CRACK WAS FOUND ON LONGITUDINAL FLOOR BEAM RBL 45.5, RUNNING FROM BS 673 TO BS 677, INBOARD SIDE AT ATTACHMENT TO WHEEL WELL CEILING. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED; FABRICATED AN EXTRUSION; INSTALLED REPAIR PART IAW DWG 691A0066, AND AWA E.R. 15-5702-03121-ES1. 2L72 4F RTA16WE 20030507001402003050700140SW 2003 5 7 CA030421005 120030131A5313205030619 LONGERON BELL 204 204B 1181404SW LYC T53 T5311B 41549NE DOOR FRAME CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 17000 (CAN) MODIFICATION OF THE DOOR ASSEMBLY WAS COMPLETED PRIOR IAW BHT. TB204-79-11. THE CRACKED PIECES WERE REPLACED WITH NEW PIECES AND REINSTALLED IAW TB 204-79-11. 1G71 4U4 U H1SW E1EA 20030513001922003051300192SO 2003 5 13 CHQU4603 120030406A3610NM1024200200 CLAMP EMB 145 EMB145LR 3260212SO PYLON PRECOOLER LEAKING A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11279SK 145379 LAV SMOKE WARNING (AURAL, VISUAL, EICAS) ON CLIMB OUT OF IND. RETURNED TO IND. EMERGENCY DECLARED AND MADE UNEVENTFUL LANDING. FIRE DEPT MET WITH AIRCRAFT. NO EVIDENCE OF SMOKE. UPON INSPECTION FOUND 2 CLAMPS LEAKING IN PYLON BY PRECOOLER. REMOVED AND REPLACED BOTH CLANPS IAW MM 36-11-04. OPS CHECK GOOD DURING GROUND RUN. 2L72 4T RTT00011AT 20030513000052003051300005CE 2003 5 13 L35SDR0301 120030509A212166082672 MOTOR LEAR 35 35A 5170602CE COCKPIT BLOWER BURNED OUT E CVGAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO01442DM 35A405 DURING APPROACH INTO CVG, CREW EXPERIENCED SMOKE AND ELECTRICAL FUMES IN THE CABIN WHICH SEEMED TO ORIGINATE IN VICINITY OF BAGGAGE COMPARTMENT. FOUND COCKPIT BLOWER MOTOR BURNED OUT. NO FIRE OR FIRE DAMAGE. AICRAFT LANDED WITHOUT FURTHER INCIDENT. 2L72 4F A10CE 20030528000482003052800048EU 2003 5 28 BAQA086407 120030514A79311176131203 PRESSURE SWITCH BOLKMS117 BK117A1 5626010EU OIL SYSTEM INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME4142 7243 PRESSURE SWITCH INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030529000542003052900054NE 2003 5 29 HEEA086509 120030521A32462071A900 WHEEL SKRSKYS76 S76A 8143006NE MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322342 760096 MLG WHEEL WORN. REPLACED 4 EACH BOLTS GY185-28 DUE TO MECH DAMAGE AND 4 EACH NUTS GYN185 DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030602001122003060200112NM 2003 6 2 SWAA031180 120030527A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (4 EA) BS 616 AT STR 5R, BS 727 AT STR 7L, BS 727C AT STR 4R AND BS 727E AT STR 5L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030514001732003051400173 2003 5 14 250TR0010 420030421A2211 COMPUTER BOEING737 7372K5 138448XNM AUTOPILOT MALFUNCTIONED A PIDAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO05250TR 22597 B-AUTO PILOT CREATES JERKING OF ELEVATORS WHILE AIRCRAFT BANKED; OK WITH -A- AUTO PILOT. SWAPPED FCC'S FOR FURTHER TROUBLESHOOTING. 2L72 4F RTA16WE 20030606000332003060600033WP 2003 6 6 ABXA030143 120030513A2760 SWITCH DOUG DC8 DC863 302198AWP HYD SPOILER BROKEN A ABXAO OTHER O OTHER CRCRUISE 1 GL23818AX 46075 IN FLIGHT, WITH LANDING GEAR UP, SPOILER PUMP RAN AND PRESSURE INDICATED 3000 PSI. PUMP TURN OFF WITH SWITCH OFF. FOUND CABLE FOR LANDING INPUT FLIGHT SPOILER HYDRAULIC PUMP LIMIT SWITCH BROKEN. REPLACED CABLE IAW REA D827-47-355. COMPLIED WITH SPOILER ADJ/TEST, REF. WORK PACK 60172912. CABLE RUN S-23. 2L74 4F 4A25 20030609000542003060900054NM 2003 6 9 DHL2003746008 120030520A7711 INDICATOR BOEING727 727224 1384076NM EPR INOPERATIVE A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01746DH 22252 AFTER CLEARED FOR TAKEOFF NR 1 EPR GAGE DID NOT RESPOND TO THRUST LEVER MOVEMENT ALL OTHER INDICATIONS ARE NORMAL. NR 1 ENGINE EPR SYSTEM INOPERATIVE PER MEL 77-1-1 CAT. "A". DMI 13006 C/W SPECIAL REQUIREMENTS PER 77-1. AIRCRAFT OK FOR SERVICE. REF. DMI 13006 NR 1 ENGINE EPR INOPERATIVE. RAN NR 1 AND 2 ENGINE COULD NOT DUPLICATE IAW DHL B727 M/M 77-11-0. SWAPPED NR 1 AND 2 EPR INDICATORS BOTH OPS CHECKED GOOD ON ENGINE RUN UP. 2L73 4F A3WE 20030605001162003060500116NM 2003 6 5 UPS03240694 120030514A33501000679 LIGHT BOEING727 72721C 138400MNM CABIN INTERMITTENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 MAIN ENTRY DOOR EMERG LT INTERMITTENT. R/R LT ASSY & BATTERIES. OPS CK OK IAW MM 33-50-67. LT ASSY P/N ON/OFF 10-0067-9/10-0067-7. S/N ON/OFF S106/7432. 2L73 4F A3WE 20030610000182003061000018 2003 6 10 2003UALA00437 420030516A3418350E018301919 COMPUTER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE STALL WARNING MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29837UA 1474 FLIGHT DIVERTED DUE TO STALL WARNING AND MASTER CAUTION LIGHTS. SUPPLEMENTAL DATA UPDATE THE SPURIOUS STALL WARNING WAS CAUSED BY A FAULTY FLIGHT WARNING COMPUTER (FWC) AND WAS CORRECTED BY REPLACING NR 1 FWC. 2L72 4F4 FRTA28NM E40NE 20030609001532003060900153SO 2003 6 9 C2XA03SH 120030525A532014524131005 SUPPORT EMB 145 EMB145LR 3260212SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 DURING C-CHECK THE FORWARD PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030611000942003061100094 2003 6 11 HEEA086702 420030522A34447021450601 DISPLAY BELL 412 412 1182202SW RADAR SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 RADAR SCREEN TURNS BLUE WHEN SWITCHING MODES. SENT TO MFG FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030617003142003061700314 2003 6 17 SWAA031268 420030606A2565D31354 SLIDE BOEING737 737* NM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29799SW 28209 AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030523000572003052300057NM 2003 5 23 SWAA031118 120030519A335065C27093 LIGHT BOEING737 7373Y0 1384671NM FWD ENTRY DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030527000842003052700084WP 2003 5 27 AALA20030412 120030404A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS FROM ROW 28-29 INOPERATIVE. ADJUSTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030528000302003052800030NE 2003 5 28 BAQA086368 220030508A7310430167601 MANIFOLD BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ENGINE FUEL MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01932CJ31 7024 HIGH TOT AND ERRATIC STARTS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030529000632003052900063 2003 5 29 HEEA086650 420030521A34427007700614 DISPLAY BELL 412 412 1182202SW TCAS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 TCAS SCREEN IS BLUE AFTER IT GETS WARM. 1G72 4U H4SW 20030623000162003062300016NM 2003 6 23 USAABB03081 120030525A33508731002511REV15 SIGN BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 CLT - FOUND EXIT IDENTIFIER AT L4 DOOR INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER. (M) 2L72 4F RTA2NM 20030623000212003062300021NM 2003 6 23 USAA030055 120030529A5300 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU58358 22201 FOUND INTERCOSTAL CHANNEL AT STATION 396 RBL 59, WITH 1 INCH AREA OF CORROSION. FABRICATED PART FROM EXTRUSION PER BOEING DWG 14IN5161 AND SRM 51-10-0. CORROSION LEVEL 1, TASK NR C53-221 AND 222 -02, 03. (M) 2L72 4F RTA2NM 20030623001012003062300101NM 2003 6 23 USAASB03067 120030516A2420UA5385512 OIL COOLER BOEING737 7373B7 1384580NM CSD LEAKING A USAAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19529AU 24411 CLT - FLT 1050 - AFTER TAKEOFF FROM CLT, EN ROUTE TO BNA, CREW REPORTED THE LOW OIL PRESSURE LIGHT FOR THE NR 2 ENGINE CSD ILLUMINATED. THE NR 1 ENGINE CSD WAS ALREADY ON MEL. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE CSD, P/N 735511A, AND AIR/OIL COOLER. CLEARED MEL ON NR 1 ENGINE CSD BY REPLACING THE CSD, P/N 735511A. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030624000712003062400071NM 2003 6 24 0301096719 120030609A5412 FRAME BOEING747 747251F 1384898NM NR 1 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01619US 21321 DURING H-CHECK CRACKS WERE FOUND ON FORWARD FRAME WEB OF NR 1 PYLON REAR ENGINE MOUNT BULKHEAD. REPAIRED PER EA 67-165068. 2L74 4F A20WE 20030707001272003070700127NM 2003 7 7 CALA0300327 120030621A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 2 INCH CRACK IN INTERIOR SKIN OF FORWARD CARGO DOOR LOCATED OVER HANDLE AREA. A DOUBLER WAS INSTALLED IAW ECRA 5232-01031. 2L72 4F RTA16WE 20030709000382003070900038WP 2003 7 9 AALA20030504 120030427A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21292AA 49304 DURING OVERNIGHT MAINTENANCE, AFT TAIL COMPARTMENT WALKWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPINNED AFT TAIL COMPARTMENT WALKWAY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030708001122003070800112WP 2003 7 8 GTIA030429 120030519A5300 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND DENT AT FS 360 BETWEEN LONGERONS 19 AND 20R. DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED 1 DOUBLER. INSTALLED 1 DOUBLER REPAIR. (M) 2L72 4F A6WE 20030710001052003071000105SO 2003 7 10 C2XA03IA064 120030529A3350MS3476L106S CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711547 145563 DURING PREFLIGHT THE CREW NOTED THAT THE TWO AFT EMERGENCY LIGHTS WERE INOP. MTY- MAINTENANCE INSPECTED THE AIRCRAFT. THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE RECONNECTED THE CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711001162003071100116NM 2003 7 11 DHL2003720007 120030627A5311 FRAME BOEING727 727228 1384083NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01720DH 19544 DURING PRE-DEPARTURE CHECK, FOUND CORROSION ON LT BS 950 MAIN FRAME, WL 189, LWBL 70.5, AS VIEWED FROM LT WHEEL WELL. TRANSFERRED TO LOG PAGE 348951 ITEM 1M DUE TO FERRY FLIGHT IAW DHL GMM 2.12. REF LOG PAGE 341424 ITEM 8M REMOVE CORROSION AT LT STA 950 FRAME. BLENDED CORROSION AT LT BS 950 WL 191.0 - 186.5 LWBL 70.5 BLEND OUT LENGTH = 4.5 INCHES LONG, 2.0 INCHES WIDE, AND DEPTH .045 IAW B727 SRM 53-10-1. DURING PRE-DEPARTURE CHECK, FOUND CORROSION ON LT BS 950 MAIN FRAME WL 189 LWB L.70.5 AS VIEWED FROM LT WHEEL WELL. REMOVED CORROSION ON LT BS 950 MAIN FRAME WL 189 L.70.5, IAW B-727-SRM 51-10-6, MATERIAL LOSS .045, FOUND TO BE WITH IN LIMITS IAW B727 SRM 53-10-1 FIG 1. 2L73 4F RTA3WE 20030714000742003071400074NM 2003 7 14 SWAA031389 120030622A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED 1/D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BETWEEN STR 27L AND STR 27R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030710000042003071000004NM 2003 7 10 KPVA200324 120030608A33506104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13807WP 023 EMERGENCY EXIT FLOOR PATH LIGHTS ALL OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLIES 3352-PSI AND 3352-PS2. OPS CHECK GOOD IAW DHC 8 MM 33-51-00 PAGE 202. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030717000592003071700059 2003 7 17 HEEA088052 420030625A2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 TRANSMIT STATIC AND NOISE. FOUND TRANSMIT MODULATION DISTORTED. REALIGNED TRANSMITTER. REPAIRED. ADJUSTED C/N SQUELCH AND CARRIER SQUELCH. BENCH CHECK GOOD. 1G72 4U H4SW 20030103000692003010300069EU 2003 1 3 RAIA00301004 120030102A33503012000 POWERPACK AEROSPATR72 ATR72202 8680940EU INOPERATIVE A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03723TE1713516936 283 MX-STL- EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER PACK, OPS CK OK. 2H72 4T RTA53EU 20030127000542003012700054 2003 1 27 HEEA083632 420030114A342150400179015 INDICATOR BELL 407 407 1182206SW ADI MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 ADI WOULD NOT PULL POWER FLAG - UNRELIABLE. REPAIRED. 1G71 3U O H2SW 20030128000122003012800012GL 2003 1 28 HEEA083764 220030115A742123060816 LEAD BELL 407 407 1182206SW ALLSN 250C 250C* GL IGNITER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 IGNITER FAILED TO START. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128001492003012800149SW 2003 1 28 HEEA083870 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030129000092003012900009SW 2003 1 29 HEEA083919 120030117A6220407001528101 BELLCRANK BELL 407 407 1182206SW M/R HEAD DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 MAIN ROTOR HEAD BELLCRANK RUBBER IS DEBONDED. 1G71 3U O H2SW 20030327001842003032700184SO 2003 3 27 C2XA03TY020 120030203A213192185A010100 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716561 145610 TYS FLIGHT 2466 WAS CLIMBING AFTER TAKEOFF WHEN THE AUTO-MANUAL PRESSURE CONTROLLER WAS GIVING FLUCTATIONS AND THE CONTROLLER WOULD'NT ADJUST. THE PILOT BROUGHT THE A/C BACK TO TYS. MAINTENANCE REMOVED AND REPLACED THE DIGITAL CONTROLLER IAW EMB 145 MM 21-31-01 AND OPS CHECK WAS GOOD IAW EMB 145 MM 21-31-00. A/C RELEASED TO SERVICE. 2L72 4T RTT00011AT 20030213000182003021300018EU 2003 2 13 CA030123011 120030122A5610NF20216526 WINDSHIELD BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) DURING TAXI FOR DEPARTURE , F/O'S WINDSCREEN 'A' PANEL HAD MULTIPLE CRACKS . (AIRPORT TEMPERATURE BELOW 0 DEG C) INSPECTION FOUND OUTER GLASS PLY SHATTERED , CENTER STRUCTURAL PLYS AND INNNER GLASS PLY NOT EFFECTED. WINDSHIELD REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2H74 4F4 F A49EU E6NE 20030213000952003021300095EA 2003 2 13 COMA0360092 120030207A5610NP1393211 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA L/H CRACKED A COMABA EMER. DESCENT UNSCHED LANDING O OTHER CLCLIMB 1 SO01966CA15994 7132 FLIGHT 5803 PILOTS WINDSHIELD CRACKED.REPLACED WINDSHIELD. 2L72 4F RTA21EA 20030717000562003071700056SW 2003 7 17 HEEA088049 120030607A6220206011132113A GRIP BELL 206 206L1 1182107SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0345RP 101 A349 45521 GRIP RETAINER SPINNING IN RETAINER BORE DUE TO THE LACK OF ENOUGH PROSEAL WHEN RETAINER WAS INSTALLED AT BHT. 1G71 3U H2SW 20030718000132003071800013WP 2003 7 18 AMTA200300774 120030609A2612 CONNECTOR LKHEED1011 10113853 5265020WP NR 2 FIRE LOOP DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 NR 2 ENGINE FIRE DETECTION LOOP FLICKERS. REMOVED AND REPLACED CONNECTOR P720 OF WDM 26-11-02 IAW WDM 20-08-01. OPS CHECK GOOD. (M) 2L73 4F A23WE 20030707001662003070700166NM 2003 7 7 AWXA200300633 120030513A5754 SKIN BOEING737 737277 1384570NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW12397 111 22645 DURING C-15 CHECK THE NR 3 SLAT INBOARD END UPPER SKIN WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 3 SLAT IAW AWA T/C R3M27002. 2L72 4F RTA16WE 20030711000012003071100001WP 2003 7 11 DHL2003806007 120030605A33505708458503 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01806DH 46002 EMERGENCY EXIT LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY UNIT. OPS CHECKED GOOD IAW M/M 33-50-1. 2L74 4F RT4A25 20030711000152003071100015CE 2003 7 11 GLBA2003089 120030619A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAO OTHER O OTHER NRNOT REPORTED 1 NM03211GL UE211 CRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED SKIN IAW BEECH SRM. 2L72 4T RTA24CE 20030110000392003011000039EA 2003 1 10 03003621 120030103A335064643 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DEFECTIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27621BR 7186 DURING PREFLIGHT INSPECTION, EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED NR 2 EMERGENCY TRACK LIGHTING ELECTRICAL CABLE. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE 2L72 4F4 FRTA21EA E15NE 20030204000182003020400018EU 2003 2 4 QH52003F00000 120030122A3246AHA52339 WHEEL BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE731* 01518WP MLG CRACKED B QH5RK NONE O OTHER ININSP/MAINT 1 NM07833JP 258044 CRACK LOCATED ON BEADSEAT OF MLG WHEEL. 2L72 4F4 FRTA3EU E6WE 20030205001382003020500138SO 2003 2 5 C2XA03IA013 120030203A2610M8373110271 SWITCH EMB 145 EMB145LR 3260212SO COCKPIT DEFECTIVE A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2722909 145459 IAH- FLIGHT 2087, DURING FLIGHT THE BAGGAGE SMOKE MASTER & EICAS WARNING IN FLIGHT. CHECKED VISUALLY AND THERE WAS NO INDICATION OF SMOKE OR FIRE, SO BOTTLES WERE NOT DISCHARGED. IAH- MAINTENANCE REMOVED AND REPLACED THE BAGGAGE SMOKE DETECTOR TEST SWITCH, POSITION S7265, VERIFIED NORMAL OPERATION, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030206001512003020600151EA 2003 2 6 COMA0390002 120030202A2750766389G COMPUTER CNDAIRCL600 CL6002C10 1390015EA AVIONICS MALFUNCTIONED A COMAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO01368CA182 10075 FLIGHT 5899 FLAPS FAIL CAUTION MESSAGE.REPLACED THE SFECU 2L72 4F RTA21EA 20030213000982003021300098EA 2003 2 13 COMA0360095 120030208A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01927CA 7031 FLIGHT 5822 FLAPS FAILEDRESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030305000292003030500029NM 2003 3 5 C1HA200396001 120030105A3260 WARNING LIGHT BOEING727 727* NM MLG DOOR ILLUMINATED A C1HAO OTHER N FALSE WARNING CLCLIMB 1 GL15696CA 22574 AFTER GEAR RETRACTION, THE FWD DOOR LIGHT AND F/E'S RT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFORMED COM PROCEDURE 2.32.29 AND BOTH LIGHTS EXTINGUISHED. INSTALLED 3 PINS LANDING GEAR AND CYCLED FOR 2 TIMES, DOORS LANDING GEAR LIGHTS WORKING GOOD IAW MM 32-12-01 SEC 6-A82H. 2L73 4F RTA3WE 20030228000482003022800048SW 2003 2 28 HEEA084451 120030213A6320357950110932 SHAFT BELL 206 206L3 1182108SW OIL PUMP LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW034282Z BH367 51499 MAIN ROTOR GEARBOX OIL PUMP IS LEAKING. REPLACED SHAFT 357950110932 DUE TO SPLINES WORN BEYOND LIMITS. REPAIRED. 1G71 3U H2SW 20030228000802003022800080WP 2003 2 28 ASAA0380004 120030103A5320593666737 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, INTERCOSTAL GOUGED AT FS 1322-1338. REPLACED INTERCOSTAL PER SRM 51-10-2, 51-10-4, 51-30-2 AND DAC DWG 5936667. (M) 2L72 4F RTA6WE 20030303000142003030300014EA 2003 3 3 03062647BR 120030303A3350 BULB CNDAIRCL600 CL6002B19 1900309EA BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27647BR 7399 DURING PREFLIGHT INSPECTION CREW NOTICED THE L/H OVERWING EMERGENCY LAMP INOPERATIVEMAINTENANCE PERSONNEL REMOVED AND REPLACED OVERWING EMERGENCY LAMP. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030313000822003031300082GL 2003 3 13 EOO2003F00000 220030224A7323369A7701 BRACKET HUGHES369 369D 4470706WP ALLSN 250C 250C20 03013GL GOVERNOR CRACKED B EOORO OTHER O OTHER NRNOT REPORTED 1 AL0390431 1100833D FOUND GOVERNOR BELLCRANK BRACKET CRACKED. (SOR 300199 DATED 02/24/2003) A LEAK WAS SPOTTED COMING FROM UNDER THE GOV. BELCRANK BRACKET 369A7701. PART WAS REMOVED AND SUBSEQUENT INSPECTION REVEALED IT WAS CRACKED NEAR ONE OF THE BOLT HOLES. REPLACED UNIT. 1G71 3U3 U H3WE E4CE 20030314001912003031400191EU 2003 3 14 00081 120030226A3210 LANDING GEAR AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE MAINS INOPERATIVE E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05204TW 204 PILOT REPORTED GEAR WOULD NOT COME UP AFTER TAKE-OFF FROM, RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. WILL UPDATE AFTER MAINTENANCE. 2L72 4F4 F A7EU E7EA 20030122000932003012200093EU 2003 1 22 HEEA083485 120030107A6420 BEARING BOLKMS105 BO105S 5626006EU T/R PITCH LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 TAIL ROTOR PITCH LINK BEARINGS WORN. REPLACED BEARINGS. 1G72 3U H3EU 20030319000092003031900009SO 2003 3 19 C2XA03BT041 120030317A3260852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO A C2XAK NONE E VIBRATION/BUFFET CLCLIMB 1 SW2712996 145296 EWR AFTER T/O WITH THE GEAR UP INDICATION ON EICAS THERE WAS LOUD WIND NOISE AND VIBRATION COMING FROM NOSE GEAR AREA. ALL DOORS CLOSED ON MFD. WENT AWAY AFTER 10 MINS. DURING CLIMB. HYD PUMPS AND PRESSURE WERE NORMAL AT ALL TIMES. REMOVED AND REPLACED NLG DOOR SEQUENCE PROXIMITY SENSOR IAW EMB145AMM 32-63-03. SWUNG NLG. OPS CHECK GOOD IAW EMBAMM 32-30-00. 2L72 4T RTT00011AT 20030320001132003032000113NM 2003 3 20 2003UALA00104 120030124A5321 PRESSURE PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FLOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29567UA 26673 AFT CABIN PRESSURE DECK WEB, STA 1681 - RBL 50 TO 52, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED DECK WITH FILLER AND DOUBLER. 2L72 4F4 FRTA2NM E17NE 20030729001122003072900112 2003 7 29 USAABB03093 420030615A22106224717004 CONTROL PANEL BOEING767 767201 1385125NM COCKPIT FAILED A USAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 EA19650US33861 23902 PHL - FLT 98 - AT FL330, WITH CENTER COMMAND SELECTED, THE AUTOPILOT DISCONNECTED WITH THE ASSOCIATED LIGHTS AND WARNING. A STRONG ACRID SMELL WAS NOTED COMING FROM THE MODE CONTROL PANEL (MCP). THE AUTOPILOT WAS SWITCHED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE MCP AND THE FLIGHT CONTROL COMPUTER. (M) 2L72 4F RTA1NM 20030417001742003041700174WP 2003 4 17 UPS03840166 120030210A5610 WINDOW DOUG DC8 DC871F 302199DWP COCKPIT STUCK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:PFLT CAPT'S SLIDE WINDOW WILL NOT OPEN. CYCLE LOCK AND OPS, CHECK NORMAL. 2L74 4F RT4A25 20030421000462003042100046NE 2003 4 21 SWIA200311807 220030225A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 1 MALFUNCTIONED A SWIAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 NM07499SW4884 4884 7398 807597 ENTERING DOWNWIND AT SLC, 11,000 FT, LEFT ENGINE FAILED. RED OIL LOW PRESS WARNING AND YELLOW CAUTION MESSAGES. BELIEVE THE FUEL FLOW WENT TO ZERO. REMOVED AND REPLACED THE LEFT ENGINE WITH A SERVICEABLE UNIT. OPS AND LEAK CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20030423001122003042300112NM 2003 4 23 F3LA200300083 120030220A5320 CHANNEL BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN SCREW HOLES OF FWD LAVATORY AFT BULKHEAD ATTACH ANGLE, HAT SECTION, STA. 312, LBL 12 TO LBL 42. REMOVED HAT SECTION PER SRM 51-30-2. FABRICATED AND INSTALLED NEW HAT SECTION PER SRM 51-10-1, SRM 51-30-2 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030327001772003032700177SO 2003 3 27 C2XA03TY002 120030109A531514526437001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 DURING A SCHEDULED 2C INSPECTION THE RT LAV FLOORBEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RT LAV FLOORBEAM, PRIMED AND PAINTED IAW EMB 135/145 SRM 51-40-02, CPM 51-21-05,06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030805000202003080500020NM 2003 8 5 03FDEA00749 120030507A5753ARC2512503 HINGE BRACKET DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- IB FLAP OB HINGE (FLAP SIDE) LWR ATTACHING PIVOT OB LUG HOLE FOUND CORRODED. LT WING- I/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE. REPAIR CARRIED OUT IAW EA 1-5750-68410 WINGS-LEFT INBOARD TRAILING EDGE FLAP- HINGE BRACKET CORRODED. 2L73 4F4 FRTA22WE E13NE 20030423000942003042300094WP 2003 4 23 ZW0A0304301 120030413A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13917TW 49366 THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 14 TO 16, AND THE EMERGENCY EXIT SIGNS WERE INOPERATIVE ABOVE BOTH FWD OVERWING EXIT DOORS. RESEATED LIGHT STRIP CONNECTOR AT ROW 14 FOR THE EGRESS LIGHTS, AND RESEATED THE BATTERIES IN THE POWER SUPPLY FOR THE EXIT SIGNS. CHECK-C 7-8-02 STL. 2L72 4F A6WE 20030722000532003072200053NM 2003 7 22 DHL2003784001 120030708A3350 BATTERY BOEING727 727227 1384078NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01767AT 22001 COCKPIT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING STANDBY POWER CHECK. REPLACED LIGHT BATTERIES, OPS GOOD IAW M/M 33-50-71. 2L73 4F A3WE 20030723000372003072300037EU 2003 7 23 USAASA03072 120030627A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19104UW 0863 THE EMERGENCY LIGHTS SYSTEM TEST FAILED. MAINTENANCE REPLACED THE FORWARD AND AFT POWER SUPPLY UNITS, 10WL AND 13WL. (M) 2L72 4F RTA28NM 20030827001442003082700144NM 2003 8 27 2003UALA00537 120030703A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 LT MAIN DECK FLOOR, SEAT TRACK CORRODED BEYOND LIMITS BETWEEN BS 764-776, LBL 56-LBL 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION SPLICE. 2L72 4F4 FRTA1NM E24NE 20030828001232003082800123 2003 8 28 MWEA030302 420030802A34201428300001 GYRO DOUG DC9 DC981 3022081WP COCKPIT INOPERATIVE A MWEAD RETURN TO BLOCK I FLT. ATTITUDE INST. TXTAXI/GRND HDL 1 GL31805ME 48031 CAPTAIN'S ADI STUCK AT 20 DEGREES RIGHT TURN. REMOVED AND REPLACED MULTIDIRECTIONAL GYRO. 2L72 4F A6WE 20030214000212003021400021EU 2003 2 14 2003UALA00043 120030111A3397 WIRE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE POWER SUPPLY CHAFED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29434UA 592 FLIGHT DIVERTED DUE TO ELECTRICAL ODOR IN THE REAR CABIN. REPLACED 9A READING LIGHT POWER SUPPLY, FOUND ARCING WHEN WIRES MOVED. SHOP FINDINGS, FOUND WIRE LEADS CHAFED IN POWER SUPPLY. 2L72 4F4 FRTA28NM E40NE 20030214000552003021400055WP 2003 2 14 ASAA0380036 120030105A531043912261 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, DOOR FRAME CHANNEL CRACKED IN FORWARD CABIN AREA. REPAIRED CHANNEL PER SRM 51-70-5. (M) 2L72 4F RTA6WE 20030221000632003022100063EU 2003 2 21 AWXA200300083 120030107A5350D5323022620000 PLATE AIRBUS320 A320232 3930326EU RT WING FAIRING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CLOSING PLATE FRAME 34. MAINTENANCE REMOVED CRACKED RT WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 8-22, FIG. 2, PG. 10, FIG. 3, PG. 12, FIG. 4, AND SRM 51-44-11, PG. 6, TABLES 3. 2L72 4F RTA28NM 20030224000822003022400082 2003 2 24 HEEA084203 420030213A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 NR 2 YAW ACTUATOR DOES NOT DEFLECT NEEDLE. TO BE SENT TO VENDOR. 1G72 3U H1NE 20030224001422003022400142NM 2003 2 24 AWXA200300193 120030216A5320146N5416 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON NUT PLATES OF FLOOR SUPPORT BS 1330, RBL 11. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED AREA ON FLOOR SUPPORT BS 1330, RBL 11; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-2, & 4-6. 2L72 4F RTA2NM 20030228000342003022800034SW 2003 2 28 HEEA084447 120030213A6330206031564003 BUSHING BELL 206 206L3 1182108SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TRANSMISSION MOUNT LINK HAS WORN BUSHINGS. REPLACED 4, 206031564003 BUSHINGS DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030305000482003030500048 2003 3 5 HEEA084630 420030214A3455066104701 TRANSCEIVER BELL 412 412 1182202SW ADF INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 ADF TRANSCEIVER INOPERATIVE NO AUDIO. FOUND UNIT -15 VOLTS MISSING. FOUND POWER SUPPLY TRANSISTOR Q105, IC I101 AND RESISTOR R104 ALL BAD. REPLACED PARTS. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306001242003030600124WP 2003 3 6 CALA0300096 120030306A5210 SKIN DOUG DC9 DC981 3022081WP MAIN CAB DR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND A 1/4" CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AT LOWER FORWARD CORNER. A REPAIR WAS INSTALLED IAW SRM 52-05. 2L72 4F A6WE 20030307000212003030700021NM 2003 3 7 SWAA030500 120030305A335030131A BATTERY BOEING737 7372T4 1384492NM CABIN WEAK A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030307001252003030700125WP 2003 3 7 AALA20030097 120030120A5320 STRUCTURE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21583AA 53160 TUL - FOUND CORROSION REMOVAL BEYOND MANUAL LIMITS, CONDITION IV. INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3. (M) 2L72 4F A6WE 20030310000922003031000092 2003 3 10 HEEA084997 420030227A34578143902240B GPS BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 INDICATED GPS FAILED. SENT TO ASM FREEFLIGHT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030311001032003031100103NM 2003 3 11 377PA0010 120030309A3350 LIGHT BOEING737 7373L9 1384470NM CABIN CONTAMINATED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05377PA 23718 SECTION 1 & 2 EMERGENCY PATH LIGHTING INOP. REPLACED WET SEGMENTS OF LIGHT STRIP. OPS CHK OK PER MM 33-29-00 2L72 4F RTA16WE 20030313001932003031300193WP 2003 3 13 AALA20030158 120030128A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21274AA 49271 TUL - FOUND CORROSION ON LONGERON 30 AT STATION 1322. REMOVED AND REPLACED LONGERON 30 FROM STATION 1297 TO STATION 1335 PER SRM 51-30-02. (M) 2L72 4F A6WE 20030117001682003011700168NM 2003 1 17 AWXA200300047 120030103A5320BAC1509100146 FLOOR SUPPORT BOEING737 7373G7 138447JNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 LCQ - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND UNDER NUTPLATE ON AFT CARGO COMPARTMENT FLOOR SUPPORT "L" ANGLE BS 771, RBL 8. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; CUTOUT DAMAGED PORTION OF FLOOR SUPPORT; FABRICATED REPAIR ANGLES PER B737-300 SRM 53-00-53, PG. 201-203; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG. 201-203, FIG. 201. 2L72 4F RTA16WE 20030121000022003012100002NM 2003 1 21 SWAA030079 120030114A522065C35463 PLATE BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 LT EMERGENCY OVERWING EXIT DOOR HANDLE COVER PLATE BROKEN. REPAIRED COVER PLATE. 2L72 4F RTA16WE 20030121000342003012100034SW 2003 1 21 HEEA083226 120030108A7160206064213207 SCREEN BELL 206 206L3 1182108SW ENGINE INTAKE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 ENGINE INTAKE SCREEN ASSY HAS CORROSION. REPAIRED. 1G71 3U H2SW 20030121000802003012100080SW 2003 1 21 HEEA083274 120030108A7714206076373001 TACH GENERATOR BELL 206 206L3 1182108SW ENGINE MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW033108E 51498 TACH GENERATOR LOW RPM WARNING HORN COMES ON DURING START. 1G71 3U H2SW 20030314001012003031400101NM 2003 3 14 SWAA030509 120030306A53126516300 WEB BOEING737 7373H4 1384600NM NOSE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 196, RBL 5, AND WL 199, LBL 5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20030122000082003012200008SW 2003 1 22 HEEA083395 120030109A79218543909 OIL COOLER BELL 206 206L3 1182108SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 ENGINE OIL COOLER PRODUCING HIGH ENGINE OIL PRESSURE. 1G71 3U H2SW 20030123000122003012300012NM 2003 1 23 2003UALA00026 120030106A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29355UA 24361 CREASE BEAM WEB BELOW FORWARD GALLEY DOOR STA 297 - STA 327 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001722003032000172NM 2003 3 20 SWAA030619 120030317A552065C25727 SKIN BOEING737 7375H4 138449DNM LH HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED C3 CHECK, FOUND LH HORIZ STAB CRACKED ON LOWER SKIN FWD OF AFT SPAR RIVET LINE AT STA 135. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030321000862003032100086EU 2003 3 21 2003UALA00229 120030228A3610D3617006300200 DUCT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CROSSBLEED DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29415UA 475 LEFT WING LEAK ECAM DISPLAYED. FOUND LEFT HAND CROSSBLEED DUCT DAMAGED AT HIGH PRESSURE GROUND CONNECTION. REPLACED DUCT. 2L72 4F4 FRTA28NM E40NE 20030731001212003073100121NM 2003 7 31 QXEA200300779 120030628A291082970010459 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007NM HYD SYSTEM CRACKED A QXEAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 NM09351PH 490 EUG- DURING TAXI LOST ALL HYDRAULIC FLUID ON NR 2 SIDE. FOUND HYDRAULIC LINE CRACKED. REPLACED LINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030326000692003032600069EA 2003 3 26 CA030206002 120030204A2730MS1410412P BEARING CNDAIRCL215 CL2156B11415 EA PWA PW120 PW123 NE ELEVATOR SEIZED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) A BINDING NOISE WAS HEARD DURING INSPECTION WHEN ELEVATOR WAS MOVED BY HAND WITH THE CONTROL SYSTEM IN MANUAL MODE. INVESTIGATION SHOWED BEARING PN MS14104-12P TO BE SEIZED AND THE INNER RACE TO BE TURNING ON PIN PN 215T92638.BOTH TUBE ASSEMBLIES 215T92643-2 AND -3 WERE FOUND TO HAVE THIS CONDITION. ASSEMBLIES WERE REVOVED FROM THE AIRCRAFT AND RETURN TO THE MANUFACTURE FOR REPAIR. 2H72 4T4 TRTA14EA E20NE 20030327001002003032700100SO 2003 3 27 C2XA03CL007 120030107A2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY MALFUNCTIONED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714998 145302 MCI FLIGHT 2248 THE CREW REPORTED A LAV SMOKE WARNING ON TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. NO SMOKE WAS NOTED. MAINTENANCE INSPECTED THE SMOKE DETECTION SYSTEM AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030421000312003042100031NM 2003 4 21 VNAA0302020 120030223A2150 A/C PACK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07328JS 3030 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND PACK OVERHEAT CAS MESSAGE AND ABORTED TAKEOFF. THE SYSTEM RESET ITSELF AND FLIGHT 4021 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4021 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030422000802003042200080SO 2003 4 22 SIMA200307904 120030222A532014522460013 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING A IMBV INSPECTION CENTER BEAM GUSSETT IS CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 135 SRM 51-40-02, 51-20-03 AND 51-40-06. (M) 2L72 4F RTT00011AT 20030716000742003071600074SO 2003 7 16 SIMA200313208 120030508A5330 SKIN EMB 135 EMB135KL 3260302SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21830AE 145615 AIRCRAFT HAS LIGHTNING DAMAGE APPROX 1.5 INCH FORWARD OF FRAME 62A BETWEEN STRINGERS 21L AND 21R. REPAIRED DAMAGE IAW EMB SRM 53-31-06. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030423001822003042300182NM 2003 4 23 VNAA0303017 120030314A2150 A/C PACK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RIGHT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07459PS 3070 DURING TAKEOFF, THE RIGHT HAND PACK FAILED AND THE CREW ABORTED TAKEOFF. THE CREW THEN RESET THE SYSTEM AND WERE CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4019 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030828000122003082800012WP 2003 8 28 ARWA20030314 120030315A5320 ANGLE DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND, AFT LOWER CARGO COMPARTMENT STA 1280, FLOOR PANEL ANGLES (02 EACH) CRACKED. REMOVED ANGLES IAW DC8 SRM 51-1-21, FABRICATED NEW ANGLES IAW DC8 SRM 51-1-4, PRIMED NEW ANGLES IAW DC8 SRM 51-1-8 AND INSTALLED NEW ANGLES IAW DC8 SRM 51-1-21. 2L74 4F 4A25 20040210000702004021000070WP 2004 2 10 ASAA0380773 120031119A5330591022813 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND UPPER FUSELAGE SKIN DENTED AT FS 1437 BETWEEN 2R AND 3R. REPAIRED IAW SRM. (M) 2L72 4F RTA6WE 20040217001112004021700111NM 2004 2 17 DHL200374260 120031125A5754 MOUNT BRACKET BOEING727 727225 1384077NM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING "C" CHECK, NR 2 SLAT IB TRACK UPPER MOUNT IB (L) ANGLE IS CRACKED; CA: REMOVED DAMAGED ANGLE AND FABRICATED NEW FROM BAC1505-100617 PO NR 900411 DIM. 9.2500 X 1.2500 IAW SAMPLE IAW 727 SRM57-10-2 FIG.3 NEW ANGLE TREATED AND PRIMED IAW 727 SRM51-10-2,INSTALLED IAW 727 SRM51-30-2.LEAK CHECK GOOD IAW B727 MM27-81-00. 2L73 4F A3WE 20031211000892003121100089EU 2003 12 11 03FDEA01892 120031107A5270ABS030901 LIMIT SWITCH AIRBUS310 A310 EU ACCESS DOOR FAULTY A FDEAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SO25401FE 191 ON TAKEOFF OUT OF DTW LOWER ACCESS DOOR AMBER LIGHT- FOLLOWED ECAM RETURNED TO LAND DTW NO EMERGENCY DECLARED. AT BLOCK IN FOUND ACCESS DOORS CLOSED AND LOCKED. RELEASED LOCKS ON BOTH DOORS FOUND PRESSURE HOLDING DOORS IN CLOSED POSITION. CREW REPORT NO PRESSURE ALERT. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-30-03 CATEGORY: C EXPIRATION: 17NOV03 "MEL 52-30-03: FWD & AFT LOWER ACCESS DOORS CLOSED & LOCKED INDICATION ON ECAM, DOOR PAGE - INOP. FWD & AFT LOWER ACCESS DOORS VISUALLY CHECKED CLOSED & LOCKED. REMOVED AND REPLACED AFT LOWER ACCESS DOOR LIMIT SWITCH IAW M/M CH 52-71-11-4. OPS CHECK OK CLEARS MEL. 2L72 4F RTA35EU 20040505000302004050500030EU 2004 5 5 USA2004F00031 120030715A2120 ODOR AIRBUSA321 A321211 3930370EU GE CFM56 CFM56* 13802NE CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19180US 1525 ENROUTE, DURING DESCENT, THE CABIN CREW IN THE AFT CABIN NOTIFIED THE FLIGHT CREW OF AN ELECTRICAL SMOKE ODOR. SHORTLY AFTERWARDS, THE COCKPIT CREW NOTICED THE SAME ODOR. THE COCKPIT CREW FOLLOWED CHECKLIST PROCEDURES AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN BOTH PACKS WITH BLEED SOURCE FORM BOTH ENGINES AND THE APU. POWERED THE CABIN, GALLEY’S, AND LAVATORIES WITH AC POWER. CHECKED THE AVIONICS COOLING SYSTEM. NO FAULTS WERE FOUND. OK FOR SERVICE. 2L72 4F4 FRTA28NM E2GL 20040520000712004052000071EA 2004 5 20 MASA200400213 120030420A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGNECY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0787353 7353 ASH 6087. PHX. THE CREW REPORTED SEVERAL AFT FLOOR EMERGENCY PROX LIGHT STRIPS INOPERATIVE. MECHANIC REPLACED THE STRIPS. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031216000482003121600048NM 2003 12 16 SWAA032534 120031117A3350101114 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29751SW 29803 DURING SCHEDULED MS CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20031211001592003121100159NM 2003 12 11 AALA20031281 120031116A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21756AM 30264 DFW FORWARD LEFT HAND GALLEY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD LEFT HAND GALLEY EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031215001032003121500103EA 2003 12 15 QXEA200301439 120031116A5610601R3303310 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A QXEAO OTHER O OTHER DEDESCENT 1 NM09606QX 10023 SEA- ON FLIGHT 2452 FIRST OFFICER'S SIDE WINDSHIELD SHATTERED JUST AS DESCENT WAS STARTED AT 41,000 FEET. REMOVED AND REPLACED FIRST OFFICER'S RIGHT HAND SIDE WINDOW. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030925000872003092500087WP 2003 9 25 GTIA030627 120030726A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND FIBERGLASS FLOOR SUPPORT STATION 160-218 AT RT DOOR IS CRACKED AND DAMAGED. REMOVED CRACKED FIBERGLASS FLOOR SUPPORT. REPAIRED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20030926000172003092600017SO 2003 9 26 F2P2003F00000 120030821A2822RG9080J4A PUMP PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA RT ENGINE INOPERATIVE E F2PAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SO17684JJ 317952194 L61468A PILOT REPORTED ROUGH RUNNING RT ENGINE IN FLIGHT WITH HIGH PRESSURE BOOST PUMP SELECTED ON. PILOT STATED (WITH BOOST PUMP ON ENGINE WANTED TO QUITE RUNNING. WHEN PUMP OFF ENGINE RAN NORMALLY. TROUBLESHOT FOUND THAT WITH DECK REFERENCE LINE REMOVED FROM PUMP AND BOOST PUMP ON FUEL STREAMED FROM PUMP AT DECK REFERENCE FITTING. PART OF AD 91-08-07 ADDRESSED THIS PROBLEM. RECOMMEND A LEAK CHECK ON THESE PUMPS AT 100 HOUR INSPECTION. 1L72 3O3 O A20SO E14EA 20040917000602004091700060NE 2004 9 17 2004F00326 220030924A7200 ENGINE LEAR 25 25B 5170511CE GE CJ610 CJ6101 30006NE FLAMED OUT A POSAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA0367HB 189 ON A TEST FLIGHT AFTER ENGINE INSTALL. ENGINE BEING TESTED FLAMED OUT AT 42,500 FT. AT A LOWER ALTITUDE OF 23,000 FT ENGINE RESTARTED AND RAN WITH NO FURTHER TROUBLE AND NO INDICATIONS OF ENGINE PROBLEMS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST STAGE TURBINE SHROUDS. ADJUSTED 1ST STAGE AIR NOZZLE. AIRCRAFT FLIGHT TESTED AT 45,000 FEET SATISFACTORY FOR RETURN TO SERVICE. (M) 2L72 4J4 J A10CE 1E16 20041014000752004101400075NM 2004 10 14 MASA200300472 120031202A3230574205A VALVE DHAV DHC8 DHC8202 2809007NM LANDING GEAR LEAKING A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07455YV6149 455 DURING APPROACH TO PHX, THE LANDING GEAR DID NOT EXTEND NORMALLY. CREW FOLLOWED CFM AND EXTENDED GEAR WITH ALTERNATE RELEASE. 2H72 4T RTA13NM 20030813000992003081300099EA 2003 8 13 SWIA200312103 120030608A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AIR DISTRIBUTIONCONTAMINATED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07411SW 7067 AFTER STARTING THE APU AND BRINGING ON BOTH PACKS, GOT SMOKE INTO THE FLIGHT DECK AND THE CABIN. SMOKE WAS COMING FROM THE AIR CONDITIONING SYSTEM. ALSO GOT A SMOKE CAUTION MESSAGE. REMOVED AND REPLACED BOTH RIGHT AND LEFT ACM WATER SEPARATOR SOCKS WITH SERVICEABLE UNITS IAW MM 21-51-13. CHECKS GOOD AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20030813001652003081300165NM 2003 8 13 SWAA031675 120030725A55516551524 ATTACH FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND HORIZ STAB ATTACH FITTING FWD AND AFT SPAR LUGS CORRODED AT RT SIDE. REPAIRED ATTACH FITTING PER SRM. 2L72 4F RTA16WE 20030819000122003081900012WP 2003 8 19 AALA20030776 120030716A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21456AA 49561 DURING OVERNIGHT MAINTENANCE, FORWARD TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030725000262003072500026SO 2003 7 25 RAIA00305136 120030508A2120 SMOKE EMB 145 EMB145 3260210SO CABIN DETECTED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE03806HK 145112 SMOKE IN CABIN DURING LANDING. MAINTENANCE PERFORMED FAULT ISOLATION CHECK NO SMOKE OR SMOKE ODOR WAS DETECTED. 2L72 4F RTT00011AT 20030729000222003072900022EU 2003 7 29 03200331 120030719A33502058393 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN DETERIORATED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27331UE 41099 DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LAMPS AND CONNECTOR. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4T RTA41NM 20030729000702003072900070NM 2003 7 29 QXEA200300831 120030714A5420 BRACKET BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - NACELLE BRACKET CRACKED - UPPER SIDE OF LEFT NACELLE BELOW WING UPPER SHROUD TIE. REPAIRED IAW DHC-8-400 SRM 51-40-10-330-801. 2H72 4T4 TRTA13NM E00062EN 20030806001232003080600123SO 2003 8 6 C2XA03CL122 120030708A32348271013 LEVER EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2718982 145223 CREW REPORTED THAT LANDING GEAR LEVER WILL NOT GO UP WITHOUT OVERRIDE BUTTON. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER. OPERATIONAL CHECKS GOOD. 2L72 4T RTT00011AT 20030829001412003082900141NM 2003 8 29 SWAA031835 120030815A531565C645372 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 714, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030829001692003082900169NM 2003 8 29 SWAA031786 120030807A5314656212518 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED SPECIAL VISIT, FOUND KEEL BEAM CORRODED AT BS 727 + 3, STR 27R. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20030813000382003081300038EU 2003 8 13 RAIA00306155 120030602A3244ANH1890 TIRE AEROSPATR72 ATR72202 8680940EU MLG VIBRATES A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03722TE 220 RT MLG HAD STRANGE VIBRATION, STOPPED WHEN GEAR IN WELL. FELT VIBRATION AGAIN ON LANDING ROLL OUT. MAINTENANCE REMOVED AND REPLACED NR 3 AND 4 MLG WHEEL AND TIRES. 2H72 4T RTA53EU 20030812000782003081200078SW 2003 8 12 HEEA088623 120030806A2800206063601101 LINE BELL 206 206L3 1182108SW FUEL SYSTEM LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 LEAKING AT FLEX LINE. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20030822000692003082200069EU 2003 8 22 2003UALA00515 120030621A2120 ODOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GALLEY DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29419UA 487 FLIGHT DIVERTED DUE TO REPORTS OF BURNING SMELL IN AFT GALLEY AREA. BURNED GUM WAS FOUND ON HOT PLATE. CLEANED HOT PLATE. 2L72 4F4 FRTA28NM E40NE 20030826001382003082600138 2003 8 26 USAASA03084 420030731A2565 SLIDE AIRBUSA319 A319112 3930323EU AFT ENTRY DOOR DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19725UW 1135 CLT - THE RIGHT SIDE AFT ENTRY DOOR SLIDE COVER WOULD NOT REMAIN INSTALLED. MAINTENANCE REPLACED THE RIGHT SIDE AFT ENTRY DOOR ESCAPE SLIDE, THEN INSTALLED COVER. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030822001812003082200181WP 2003 8 22 UPS03841085 120030812A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:ASV EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, EMERGENCY LIGHTS OPS CHECK NORMAL. 2L74 4F RT4A25 20030911000372003091100037EA 2003 9 11 SWIA200312318 120030802A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07912SW 7595 FS 484 RT INTERCOSTAL OB FLANGE RBL 36 CRACKED. (DISCOVERED DURING C-CHECK)INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. ''A''. 2L72 4F4 FRTA21EA E15NE 20030929001002003092900100 2003 9 29 MALA030400 420030903A3420 COMPUTER SAAB SF340 340B 7860101EU ARHS FAILED A MALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL15363PX 340B260 EFIS WENT BLANK ON TAKEOFF. LEFT SIDE ARHS FAILURE AFTER ROTATION. REPLACED NR 1 AHRS COMPUTER. 2L72 4T RTA52EU 20030730001322003073000132 2003 7 30 MEX2003226 420030614A3425 INDICATOR DOUG DC9 DC987 3022087WP COCKPIT FAILED A ASMFB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW231075T 49724 MEX-SLC - FLT 486 - AIRCRAFT PERFORMED UNSCHEDULED LANDING, DURING CRUISE EFIS NR 2 FAILED AFFECTING VOR NR 2 AND ADI NR 1 AND DURING APPROACH BOTH TEMP OIL INDICATION CAME ON. BREAKER AHSRS 2 WAS RESET, EDP WAS TESTED AND ADDITIONALLY TEMP OIL SENSOR WERE CLEANED IAW MM 34-21-00, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030916000892003091600089WP 2003 9 16 GTIA030657 120030826A7160801407 INLET GUIDE VANE DOUG DC9 DC982 3022082WP ENGINE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 ENGINE 2-217A ESN 708450 INLET GUIDE VANE HAS ROOT AND INNER SHROUD WELD TO SHROUD CRACKED. REMOVED AND REPLACED IGV CASE. (M) 2L72 4F A6WE 20030819000132003081900013NM 2003 8 19 USAA030110 120030708A5210 SKIN BOEING737 737401 1384701NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 INTERIOR DOOR SKIN CRACKED .5 INCH LONG, 3RD DOOR STOP ADJUSTMENT SCREW FROM BOTTOM AT AFT SIDE MED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EA 76156, SRM 51-40-03, 52-10-01, 51-70-13. (M) 2L72 4F RTA16WE 20030818000742003081800074SW 2003 8 18 HEEA088601 120030806A5230206513211 ACTUATOR BELL 206 206L3 1182108SW CARGO DOOR WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 CARGO DOOR ACTUATOR WEAK. REPLACED PART. 1G71 3U H2SW 20030819000632003081900063SO 2003 8 19 SWIA200312121 120030522A5412 FIREWALL EMB 120 EMB120ER 3260203SO LEFT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 LEFT NACELLE FIREWALL HAS SMALL CRACK. FOUND DURING C-CHECK INSPECTION. REPAIR APPLIED TO AREA MENTIONED IAW SRM 120 51-10-02. 2L72 4T RTA31SO 20030331000312003033100031WP 2003 3 31 AALA20030038 120030112A2822 SCREW DOUG DC9 DC983 3022083WP BOOST PUMP LOOSE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2176202 53292 EN ROUTE LGB-DFW, AT 24,000 FEET SMALL FUEL LEAK NOTICED. NO DISCREPANCY IN FUEL BURN OR IMBALANCE. CLIMBED TO 33,000 FEET AND LEAK INCREASED TO A STEADY STREAM. DECLARED EMERGENCY, DIVERTED TO ELP AND LANDED WITHOUT INCIDENT. RETORQUED BOOST FUEL PANEL SCREWS TO BOOST PUMP. PANEL UNDER HEATER BLANKET. LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000892003033100089SO 2003 3 31 C2XA03SH066 120030329A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, REPAIR DOUBLER ON TEE REINFORCEMENT ON STRINGER 19 LT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030403000392003040300039NM 2003 4 3 AMTA200300254 120030222A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 FOUND ROW 1-4 BULLNOSE EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 DOOR BATTERY PACK IAW AMM 33-51-07, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030821000142003082100014WP 2003 8 21 ASOA03307 120030713A5210601R317035 CAM DOUG DC9 DC982 3022082WP PAX DOOR OUT OF RIG A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829US 49429 FLT 4140 - DURING GROUND INSPECTION IN DFW, THE MAIN PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE AND DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE RIGGED THE MAIN PASSENGER DOOR UPPER CAM MECHANISM. OPERATIONAL AND WARNING CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F A6WE 20030821002212003082100221SO 2003 8 21 RAIA00307185 120030705A3610S2D230 O-RING EMB 145 EMB145ER 3260211SO BLEED AIR SYS DAMAGED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03808HK 145157 5304-STL- NR 1 BLEED LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE O-RING AT LEFT SIDE BAGGAGE COMPARTMENT. 2L72 4F RTT00011AT 20030821000102003082100010EU 2003 8 21 USAABA03026 120030723A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19677UW 0380 FOUND L1 AND L3 DOOR EPSU BATTERY CAPACITY CHECK FAILED. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20030822000452003082200045NM 2003 8 22 UPS03241068 120030716A5755652162225 SUPPORT FITTING BOEING727 72725C 138400HNM SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C NR 11 SPOILER SUPPORT FITTING IS CRACKED. FITTING REPLACED IAW UPS EO B727-5750-5182. 2L73 4F A3WE 20030401001022003040100102NM 2003 4 1 DHL2003780004 120030327A3350 BATTERY BOEING727 727223 1384074NM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01780DH 22006 BOTH EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES, OPS CHECKED NORMAL IAW M/M 33-50-71. 2L73 4F A3WE 20030404001702003040400170NM 2003 4 4 SWAA030566 120030313A561058935733 WINDOW BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE M OVER TEMP CRCRUISE 1 SW29618WN 28034 DURING FLIGHT CAPTAINS L4 WINDOW SHATTERED. REMOVED AND REPLACED CAPTAINS L4 WINDOW PER MM. 2L72 4F RTA16WE 20030407000372003040700037WP 2003 4 7 GTIA030022 120030116A7120K22199SA31 ISOLATION MOUNT DOUG DC9 DC983 3022083WP ENGINE OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 DTW - FOUND FORWARD LOWER ISOLATION MOUNT ALIGNMENT MARKS MISMATCHED. REMOVED AND REPLACED FORWARD LOWER ISOLATER MOUNT IAW MD80 MM 71-20-02. (M) 2L72 4F RTA6WE 20030407000852003040700085SO 2003 4 7 SIMA200306405 120030128A532113500469401 FLOORBOARD EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 ABI - A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION GALLEY FLOORBOARD EXTENSION CORRODED. REMOVED AND INSTALLED SERVICEABLE EXTENSION IAW EMB 134 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030401001742003040100174NE 2003 4 1 DHL2003805002 220030126A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 1 MALFUNCTIONED A DHLAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO01805DH 46125 693488 NR 1 ENGINE DID NOT SPOOL 240,100, LESS THAN 60 KTS, 3C, 16 FOOT, NORMAL. FOR INFORMATION ONLY PER GMM CHAP 8 SEC 8 PAGE 3. 2L74 4F4 FRT4A25 E2GL 20030828001892003082800189NM 2003 8 28 CALA0300460 120030808A2612 FIRE LOOP BOEING737 7373T0 1384582NM APU DAMAGED A CALAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2760312 23363 THE APU FIRE LIGHT ILLUMINATED DURING CLIMBOUT OF DEN. THE FIRE HANDLE WAS PULLED AND THE FIRE BOTTLE WAS DISCHARGED. THE LIGHT WENT OUT, BUT ILLUMINATED AGAIN WITH THE FIRE BELL SOUNDED. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU COMPARTMENT AND APU, AND FOUND NO EVIDENCE OF FIRE. THE FORWARD SIDE OF BULKHEAD IN TAIL COMPARTMENT WAS ALSO INSPECTED WITH NO DISCREPANCIES FOUND. THE ENGINE FIRE CONTROL MODULE WAS REMOVED AND REPLACED. THE APU LOWER FIRE DETECTION LOOP WAS ALSO REPLACED DUE TO A DAMAGED LOOP. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED IAW MM 26-22-11, PAGE 401-406. AN OPERATIONAL CHECK OF THE APU FIRE PROTECTION SYSTEM WAS GOOD. 2L72 4F RTA16WE 20030807000882003080700088NM 2003 8 7 EIA2003104 120030725A5415 SKIN BOEING747 747212B 1384886NM NR 4 PYLON TORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 NR 4 PYLON I/B SKIN TORN OUT AFT OF AFT ENGINE MOUNT. DAMAGED AREA REPAIRED PER ECRA 485-54-138-2, REV A. 2L74 4F A20WE 20030806000752003080600075EU 2003 8 6 03216303 120030804A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27303UE 41015 DURING MAINTENANCE INSPECTION THE LT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULBS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030806001382003080600138SO 2003 8 6 C2XA03SH249 120030801A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030813001912003081300191NM 2003 8 13 SWAA031559 120030714A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 2, JUST BELOW STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030807001002003080700100NM 2003 8 7 EIA2003097 120030724A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 FUSELAGE SKIN CRACKED AT BATHTUB FITTING FWD FASTENER HOLE STA 1000 AT STR 38L. REMOVED DAMAGE, NDT AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 53-30-03 FIG 60. 2L74 4F A20WE 20030903001212003090300121 2003 9 3 2003F00531 420030730A3460 BLOCK CESSNA750 750 2076810CE FLT MANAGEMENT DEFECTIVE A O2GAO OTHER J WARNING INDICATION LDLANDING 1 NE03610GR 7500163 ON ROLL OUT, CREW GOT AN FGC A/B FAIL AMGER EICAS MESSAGE. CHECKED ASSOCIATED WIRING AND CONNECTORS. REPLACED BOTH TERMINATING RESISTOR BLOCK. TEST FLEW A/C OPERATIONAL CHECK GOOD. (M) 2L72 4J RTT00007WI 20030902000672003090200067CE 2003 9 2 00100 120030625A3260 UPLOCK SWITCH LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE MLG INOPERATIVE E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05324TW 24D324 PILOT REPORTED GEAR WOULD NOT RETRACT AFTER DEPARTING YIP, CREW RETURNED TO YIP WITH GEAR DOWN AND LOCKED INDICATION. MAINTENANCE CLEANED LUBED AND ADJUSTED ALL UPLOCK SWITCHES IAW LEAR M/M AIRCRAFT RETURNED TO SERVICE. 2L72 4J4 J A10CE 1E16 20030903000642003090300064 2003 9 3 HYI2003F00008 420030527A3197CM358950 MASTER SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LT SWITCH PANEL INOPERATIVE E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01514NC940 402C0514 AVIONICS MASTER SWITCH INOPERATIVE. MAINTENANCE REPLACED SWITCH AND RETURNED THE AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20030904000992003090400099EA 2003 9 4 QXEA200301019 120030822A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX- FORWARD CARGO BAY CHIMNEY AT DOOR AREA IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030812000732003081200073 2003 8 12 HEEA088590 420030801A34578143902240B GPS BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH2303 33150 GPS CAUSES CIRCUIT BREAKER TO POP. SHOP REPAIR. 1G72 4U H4SW 20030814001052003081400105SO 2003 8 14 RAIA00306161 120030609A3230 LANDING GEAR EMB 145 EMB145LR 3260212SO MAINS MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03817HK 145058 LANDING GEAR WILL NOT RETRACT. MAINTENANCE PERFORMED LANDING GEAR EXTENSION AND RETRACTION CHECK. NO DEFECTS NOTED, OPS OK. 2L72 4T RTT00011AT 20030815000242003081500024SW 2003 8 15 HEEA088531 120030730A6320 BEARING BELL 206 206L3 1182108SW LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X LK8664 51412 MAIN ROTOR HEAD LINK ASSY HAS WORN BEARINGS. IN SHOP REPAIR. 1G71 3U H2SW 20030728000682003072800068NM 2003 7 28 SWAA031527 120030711A33506104781 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED PM CHECK, FOUND BOTH LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030916000222003091600022GL 2003 9 16 EVAS092016 220030811A7320 HMU BOEING747 74745E 1384947NM GE CF6 CF680C2* GL ENGINE FAILED W QOCFD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 WP0316403 27141 DURING PUSHBACK, ENGINE FAILED TO START. CHECK SYSTEM, FOUND NO POWER TO ENGINE,TRY TO REPLACE HMU ON HELP,KEEP TROUBLESHOOTING FOUND THE FIRE HANDLE SWITCH OPERATION WAS NOT WELL,REPLACED THE SWITCH AND SYSTEM OPERATION CHECK NORMAL. 2L74 4F4 FRTA20WE E23EA 20031002000502003100200050WP 2003 10 2 UPS03841206 120030827A53405758571502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, FLOOR SUPPORT FITTING IS CRACKED AT STA. 120 LONG. 33R REMOVED AND REPLACED FITTING IAW DWG. 5758571,AND SRM. 51-1-20D. 2L74 4F RT4A25 20030909000502003090900050EA 2003 9 9 SWIA200312326 120030808A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 AFT EQUIPMENT COMPARTMENT DOOR CUTOUT FS 700 RT ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW 51-40-11. P/N: 601-35013-12 2L72 4F RTA21EA 20030908002532003090800253EA 2003 9 8 SWIA200312344 120030829A27604916406 ECU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07923SW 7664 FLT SPLRS FAULT STATUS MESSAGE INTERMITTENT. REMOVED AND REPLACED SECU. OPS CHECK GOOD IAW CRJ MM 27-00-00. S/N OFF: 01548. 2L72 4F4 FRTA21EA E15NE 20030930000872003093000087WP 2003 9 30 ABXA030357 120030818A533059114123 SKIN DOUG DC9 DC932F 3022067WP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 CORROSION BETWEEN LONGERON 26 RIGHT AND SKIN, BETWEEN STA 794 AND 813. REPAIRED AREA IAW DC-9 SRM 53-04. 2L72 4F A6WE 20031006000922003100600092NM 2003 10 6 HNAA0300047 120030903A33506013211X BATTERY DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DISCHARGED A HNAAO OTHER L NO TEST NRNOT REPORTED 1 EA07908HA22466182 015 RED FLOOR EMERGENCY LIGHTS 1 AND 2 INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY 3352-PS2, OPS CHECK GOOD. 2H72 4T RTA13NM 20031020002212003102000221NM 2003 10 20 UPS03241336 120030924A532065C3320226 SUPPORT FITTING BOEING727 72751C 1384015NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 INSPECTION TYPE:SP RIGHT FUSELAGE TO WING SUPPORT FITTING IS CRACKED AT STA 760.95 AT RBL 70.5. REMOVED AND REPLACED FITTING IAW DWG 65C33202 AND SRM 51-30-02. 2L73 4F A3WE 20031031000202003103100020EA 2003 10 31 03270626 120030928A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27626BR 7225 CREW REPORTED BURNING ODOR DURING UNLOADING OF PASSENGERS FROM LIGHTING NEAR ROWS 8C AND 8D. 2L72 4F RTA21EA 20031103000812003110300081SW 2003 11 3 ALG2003F00073 120030315A5312206064902125 FIREWALL BELL 407 407 1182206SW FUSELAGE CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03409AL1501 53494 DAILY. FIREWALL HAD 1.5 INCH CRACK ON FIREWALL LT LWR CORNER OF COMBUSTION CAN DEPRESSION. THICKER FIREWALL. 1G71 3U O H2SW 20031027000792003102700079NM 2003 10 27 QXEA200301181 120030924A4930 APU BOMBDRDHC8 DHC8401 1390041NM ZONE 100 LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 FUEL LEAKING FROM APU DRAIN. REPAIRED IAW Q400 TASK 49-30-01-400-801. 2H72 4T RTA13NM 20031110000682003111000068EU 2003 11 10 AWXA200301371 120031106A5210FE240221001 DIAPHRAGM AIRBUS320 A320231 3930325EU R-1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SNA - EES - DURING 8-DAY INSPECTION THE R-1 DOOR ASSIST BOTTLE WAS FOUND AT 0 PSI, THE DOOR SLIDE WAS NOT DEPLOYED. MAINTENANCE REMOVED AND REPLACED R-1 DOOR ASSIST BOTTLE DIAPHRAGM IAW 52-10-00, OPERATIONAL AND LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20031120000952003112000095 2003 11 20 COE2003F00003 420031003A3197 WIRE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE INSTRUMENT PANELBURNED E COEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM13779FX 208B0276 19152 AFTER TAKEOFF FROM LMT, PILOT NOTICED SMOKE COMING FROM AVIONICS VENT ON GLARE SHIELD. ELECTRICAL ODOR ACCOMPANIED SMOKE. OXYGEN MASK WAS NOT USED. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE VISUALLY INSPECTED WIRING BEHIND INSTRUMENT PANEL, CIRCUIT BREAKERS AND RAN ELECTRICAL SYSTEMS. COULD NOT DUPLICATE. A/C WAS RETURNED TO SERVICE. FURTHER INVESTIGATION IN PDX REVEALED SHORTED WIRE IN RADAR ALTIMETER WIRE BUNDLE. WIRE HAS BEEN REPAIRED AND A/C RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 20040128000672004012800067EA 2004 1 28 QXEA200301588 120031227A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX- FORWARD CARGO COMPARTMENT CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20040212001742004021200174NM 2004 2 12 AWXA200301585 120031204A5340650163312 ATTACH ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND ON FRAME ATTACH ANGLE AT BS 294.5, STR 13 LT MAINTENANCE REMOVED CRACKED FRAME ATTACH ANGLE AT BS 294.5, STR 13 LT; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 65-1633; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 8, 12, AND 14, PG. 1, 4, 45, AND 64. 2L72 4F RTA16WE 20040401000282004040100028WP 2004 4 1 ASAA0380400 120030421A55235910413511 SKIN DOUG DC9 DC982 3022082WP CONTROL TAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND LEFT ELEVATOR CONTROL TAB HAS SHARP DENT ON LOWER SURFACE INBOARD SIDE. REPAIRED PER SRM. (M) 2L72 4F A6WE 20031105000802003110500080NM 2003 11 5 03FDEA01831 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG BORE FOUND CORROSION. 2L73 4F RTA22WE 20031107001052003110700105NM 2003 11 7 AALA20031098 120030925A2421GEN5103 IDG BOEING767 767323 1385205NM RT ENGINE FAILED A AALAK NONE J WARNING INDICATION CRCRUISE 1 SW21395AN 29432 FIVE HOURS INTO FLIGHT RIGHT GENERATOR TRIPPED AND RIGHT FIELD OFF LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE IDG PER MM. OPS AND LEAK CHECK OK. (M) 2L72 4F RTA1NM 20031118000492003111800049EU 2003 11 18 AWXA200301164 120030824A5321D5367180500200 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON FLOOR PANEL 261 FF. MAINTENANCE REMOVED DAMAGED PORTION OF FLOOR PANEL; CLEANED AND PREPARED SURFACE; APPLIED FIBERGLASS BOND REPAIR IAW A320 SRM 53-02-00 PG 208-211 FIG 203. 2L72 4F RTA28NM 20031118001062003111800106NM 2003 11 18 AWXA200301182 120030912A5321146N575024 FLOOR PANEL BOEING757 7572S7 1384962NM CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL P-6 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 146N5750, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1. 2L72 4F RTA2NM 20040112000192004011200019WP 2004 1 12 GTIA031016 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND LT COCKPIT FLOOR PANEL 4415A, NON SKID WORN OFF, CRACKED, CHAFING/SURFACE CORRODED. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLERS. (M) 2L72 4F A6WE 20031124001182003112400118WP 2003 11 24 DHL2003807527 120031024A5320 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MLG W/W CEILING L-ANGLE SPLICE ANGLE CRACKED 0.500, STA 857.000 RBL 46. REMOVED CRACKED SPLICE ANGLE IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED NEW SPLICE ANGLE IAW SRM 53-2-0. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SPLICE ANGLE IAW SRM 51-1-20D, SRM 51-1-21. 2L74 4F RT4A25 20031124001342003112400134NM 2003 11 24 USAA030202 120030924A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US 23312 PIT - FOUND SKIN CRACKED 4.5 INCH HORIZONTALLY, BS 727E STRINGER 24 LT. INSTALLED TEMPORARY REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20031125000342003112500034WP 2003 11 25 DHL2003805570 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER 0.250 CRACKED, STA XFS 316.500. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RIGHT WING CTR L/E, STA XFS 316.500 IAW SRM 57-2-0 PG 9-10, IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040115001052004011500105NM 2004 1 15 UPS03541389 120031011A2930211C223296 PRESSURE SWITCH BOEING757 75724APF 1384969NM RROYCERB211 RB211* 54555NE HYD SYSTEM MALFUNCTIONED A IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01467UP 25483 INSPECTION TYPE:N/A C HYD SYS PRESS EICAS MESSAGE IN FLIGHT. SYS PRESS LIGHT ON OVERHEAD P PANEL ILLUMINATED. PERFORMED TEST OF CENTER HYD SYS IAW B-757 FIM 29-11-00. OPS CHECK NORMAL. COULD NOT DUPLICATE FAILURE. CTR SYS CASE DRAIN MODULE SYS PRESS SWITCH REMOVED AND REPLACED ON L/P 875624 ITEM 3. 2L72 4F4 FRTA2NM A12EU 20031219000722003121900072EU 2003 12 19 AWXA200301514 120031206A2782830A000002 ACTUATOR AIRBUS320 A320231 3930325EU SLAT MALFUNCTIONED A AWXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP28633AW44834 082 ON APPROACH INTO DTW EN ROUTE FROM LAS THE LEADING EDGE SLAT SYSTEM LOCKED OUT AT POSITION 1 WHEN SELECTED, TRAILING EDGE FLAPS OPERATED NORMALLY. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND LT WING SLAT WING TIP BRAKE INDICATOR POPPED, RESET INDICATOR AND CYCLED SLATS SEVERAL TIMES, ALL OPERATIONS WERE NORMAL. A FOLLOW-UP WAS WRITTEN TO REPLACE THE LT WING OUTBOARD LEADING EDGE SLAT ACTUATOR AS A PRECAUTIONARY MEASURE. ON 12/07/2003 MAINTENANCE REPLACED THE LT WING NR 5 SLAT ACTUATOR IAW AMM 27-84-49, PG 401; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031219000122003121900012NM 2003 12 19 DHL2003747013 120031104A5210 SLEEVE BOEING727 727224 1384076NM PAX DOOR HANDLE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 OUTSIDE MAIN ENTRY DOOR HANDLE WOULD NOT ENGAGE. SPRING ACTION FINE. REMOVED AND REPLACED MAIN ENTRY DOOR HANDLE MECHANICAL SLEEVE PER B-727 M/M 52-11-01. OPS CHECKED GOOD PER B-727 M/M 52-11-01 PAGE 501. 2L73 4F A3WE 20031219000842003121900084NM 2003 12 19 2003UALA00912 120031126A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29193UA 26890 AFT PIT FRAME UPPER TEE CHORD AT STA 1740 HAS 2 DENTS ON THE HORIZONTAL FLANGE AT RBL 47 AND 51. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS REPAIRED PER MAE EA 47-5365-13-A1057. 2L74 4F4 FRTA20WE E24NE 20040105000802004010500080WP 2004 1 5 AALA20031442 120031218A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21218AA 49168 AUS EMERGENCY CEILING LIGHTS OVER SEATS 28DEF THROUGH 31DEF INOPERATIVE. REPLACED EMERGENCY CEILING LIGHT BATTERY PACK IN OVERHEAD BIN AT SEAT 28DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031229001052003122900105NM 2003 12 29 AWXA200301549 120031125A532050826162 INTERCOSTAL BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-04 CHECK A 5 INCH CRACK WAS FOUND ON INTERCOSTAL AT BS 303, STR 3 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 303, STR 3 LT AND FOUND ATTACH STRAP CRACKED, REMOVED CRACKED ATTACH STRAP; ORDERED AND RECEIVED A NEW REPLACEMENT INTERCOSTAL, AND FABRICATED A NEW REPLACEMENT ATTACH STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG 1, FIG 101. 2L72 4F RTA16WE 20040106001242004010600124NM 2004 1 6 DHL2003742532 120031125A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 5 SEAT TRACK AT BS 760 IS DAMAGED. REMOVED SEAT TRACK AT BS 760 TO 850 FOR REPAIR IS OUT OF LIMITS IAW B-727 SRM 51-30-2 AND 51-10-1 FIG 3. FABRICATED NEW SEAT TRACK AS PER SAMPLE IAW B-727 SRM 51-10-1. DIMENSION IS 95 INCHES MAT USED BAC-1520-841 PO 323569 IAW B-727 SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040106001882004010600188NM 2004 1 6 AALA20031200 120031101A3350S283T0143 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY SEAT AISLE LIGHTS AT 3B, 4B, 5B, AND 6B INOPERATIVE. REPLACED PACK AT M735. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040122000832004012200083NM 2004 1 22 USAASA03217 120031218A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU 23381 PIT - MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT CONNECTOR BEHIND LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031209000502003120900050NM 2003 12 9 P5CA0300971 120031028A532065B8325310 SUPPORT BOEING747 747283B 1384867NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LBG - WING TO BODY FLAP TORQUE TUBE - LOWER GANG SEAL - SUPPORT BLOCK CORRODED - LEVEL ONE. REPLACED SUPPORT BLOCK PER SRM 51-10-01. 2L74 4F A20WE 20031204001252003120400125NM 2003 12 4 AWXA200301266 120031008A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM BS 773, LBL 3. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT DAMAGED SECTION OF FLOORBEAM BS 773, LBL 3; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG 201. 2L72 4F RTA16WE 20030919000342003091900034 2003 9 19 U30A200300033 420030811A2213 COMPUTER AIRBUS320 A320212 3930322EU FLT AUGMENTATIONMALFUNCTIONED A U30AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA17265AV 427 AFTER PUSHBACK FOR FLT 326 IN BWI, CREW RECEIVED ECAM MESSAGE FOR AUTO FLT YAW DAMPER FAULT, AFTER ENGINE START. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET THE NR 2 FAC (FLIGHT AUGMENTATION COMPUTER) IAW CAATS TASK 22-63-00-810-815. SYSTEM OPS CK'D OK. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA28NM 20030923000232003092300023WP 2003 9 23 DHL2003604585 120030609A5711 FRAME DOUG DC8 DC873F 302199FWP CENTER WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT. WING CENTER L/E FORMER CRACKED 3.000 AT STA. XOLDI 6.225. STOP DRILLED CRACK AT STA. XOLDI 6.225 AND FABRICATED REINFORCEMENT ANGLE (301 0.250H 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE WITH NEW FASTENERS IAW SRM 51-1-20D PG.9, SRM 51-3-0 PG.1 2L74 4F RT4A25 20030924001072003092400107NM 2003 9 24 03FDEA01279 120030806A5753ARC1984 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) INBOARD AND OUTBOARD PIVOT HOLES CORRODED AT BORES AND SPOT FACES. RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) INBOARD AND OUTBOARD PIVOT HOLES CORRODED AT BORES AND SPOT FACES REPAIRED AS PER FEDEX EA 1-5750-63181. 2L73 4F RTA22WE 20040128001922004012800192NM 2004 1 28 P5CA0401017 120031223A523065B073296 PUSHROD BOEING747 7472U3B 1384846NM CARGO DOOR BROKEN A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23922FT 22768 SIDE CARGO DOOR FAILS TO OPEN. FOUND PUSH ROD BROKEN HOOK ACTUATOR FWD SIDE. REMOVED AND REPLACED ROD AS PER MM 52-32-00, OPS CHECK, OPERATION CHECK NORMAL. 2L74 4F RTA20WE 20040202001312004020200131NM 2004 2 2 AALA20040071 120031204A28205343T0054 VALVE BOEING777 777223 1385213NM RT FUEL TANK INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21772AN 29580 DURING CRUISE DECREASED FUEL NOTED LT MAIN TANK, QTY LT TANK STABILIZED 63,300 LBS. RT MAIN TANK INCREASED 64,500 LBS TO 66,900 LBS WHILE CONTINUING TO USE CENTER TANK FUEL PROBES 18, 19, 20 LT MAIN TANK INDICATED LOWER HEIGHT PROBES 18, 19, 20 RT MAIN TANK. CALCULATED & TOTALIZER FUEL AGREEMENT WITHIN 300 LBS. FUEL IMBALANCE MESSAGE EICAS SHOWED 3900 LB IMBALANCE PRIOR TO CENTER TANK EMPTY & BEFORE INITIATING FUEL IMBALANCE PROCEDURE. CENTER TANK PUMPS TURNED OFF, 1500 LBS, CENTER PUMPS OFF & FUEL IN BOTH MAIN TANKS ABOVE 29000 LBS. FUEL CENTER TANK EMPTIED & FUEL IMBALANCE CEASED TO EXIST. REPLACED PROBES 18, 19, 20 RT MAIN FUEL TANK & RT FLOAT. OPERATED FUEL SCAVENGE VALVES, SYS GRD CHECKED NORM. 2L72 4F RTT00001SE 20040203000462004020300046WP 2004 2 3 ASAA0380568 120030828A531359366679 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 DURING C-CHECK, FOUND LONGERON 28R CORRODED THROUGH AFT OF FS 1287. REPLACED DAMGED SECTION FROM FS 1287-1309. SPLICED IAW EA 53-10-02243. (M) 2L72 4F A6WE 20040204000672004020400067NM 2004 2 4 03287405 120031014A2760 SPOILER DORNERDO32 DO328300 NM LANDING DEPLOYED A VTZAO OTHER F FLT CONT AFFECTED LDLANDING 1 EA27405FJ 3155 DURING LANDING THE GROUND SPOILERS DEPLOYED PRIOR TO TOUCH DOWN. MANTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK OF SPOILER SYSTEM AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040217000082004021700008EU 2004 2 17 2004F00059 120030915A5220D5227908520200 FITTING AIRBUS320 A320233 3930329EU EMERGENCY EXIT GOUGED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND GOUGES ON THE LATCHES OF THE LOWER FITTING OF THE RT FORWARD EMERGENCY EXIT DOOR. REMOVED AND REPLACED LOWER LATCH FITTINGS ON RT FORWARD EMERGENCY EXIT DOOR. (M) 2L72 4F RTA28NM 20031211000522003121100052NM 2003 12 11 AWXA200301404 120031013A5320435N163239 SUPPORT BRACKET BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM SUPPORT BRACKET BS 1310, RBL 14. MAINTENANCE REMOVED CORRODED FLOORBEAM SUPPORT BRACKET BS 1310, RBL 14; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 7A. 2L72 4F RTA2NM 20031212000132003121200013 2003 12 12 SWAA032434 420031104A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 L2 DOOR EVACUATION SLIDE OUT OF ADJUST. READJUSTED SLIDE ASSY PER MM. 2L72 4F A16WE 20040323000012004032300001 2004 3 23 ERAA092665 420031208A2562 G SWITCH SNIAS AS332 AS332C 8680808EU TMECA MAKILAMAKILA1A 60040EU ELT STICKS B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03171EH627 68128 2058 G SWITCH STICKS, REPLACED G SWITCH AND TESTED ELT IAW ARTEX PROCEDURES (4090, 1401. 4091) REINSTALLED BATTERY PACK ELT MEETS ALL SPECIFICATIONS. 2G72 4U4 U H4EU E12NE 20031216000392003121600039NM 2003 12 16 SWAA032555 120031119A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 500, STR 10L AND BS 500B, STR 15L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030410000672003041000067NM 2003 4 10 SWAA030646 120030320A33506556633 LIGHT BOEING737 7373T5 1384608NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030404000572003040400057NM 2003 4 4 DL757030206 120030302A521080330033 RESERVOIR BOEING757 757232 1384965NM L-1 DOOR UNSERVICEABLE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27650DL 24390 AIRCRAFT ARRIVED AT GATE A 24. FLIGHT ATTENDANT FAILED TO DISARM L-1 ENTRANCE DOOR. DOOR ASSIST BOTTLE FIRED. SLIDE DID NOT DEPLOY. REPLACED ASSIST BOTTLE, DOOR OPERATION NORMAL. 2L72 4F RTA2NM 20030408000572003040800057NM 2003 4 8 0300706301 120030406A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01661US 23719 DURING LINE CHECK FOUND LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 22-31. RECONNECTED WIRES AND OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030410002052003041000205WP 2003 4 10 GTIA030154 120030312A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 237 TO STA 218 HAS CORROSION ON MEMBRANE WEB LT SIDE WASTE DISPOSAL DRAIN MOUNT. FAB DOUBLER. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA6WE E2EA 20030414001302003041400130EA 2003 4 14 CA030311005 220030305A7322269A4897901 CONTROL CABLE SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA FUEL CONTROL STIFF W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) FUEL CONTROL CABLE STIFF TO OPERATE. REPLACED CONTROL WITH NEW PART. 1G71 3U3 O0 4H12 1E10 20030414001082003041400108NM 2003 4 14 CA030304003 120030226A2121732591A COOLING FAN BOEING767 767383 1385214NM GE CF6 CF680C2B6F 30025NE COCKPIT FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) SMOKE IN COCKPIT . STOPPED AFTER 20 SECS. AFTER LANDING IN ANC STATUS MSG. 'FWD EQ EXH FAN' AND C/B H21 LWR EQUIP PANEL 'FWD EXH EQUIP COOL FAN ' TRIPPED.FWD EQUIPMENT COOLING FAN REPLACED AS PER AMM 2L72 4F4 FRTA1NM E13NE 20030416000722003041600072EA 2003 4 16 SWIA200311861 120030329A3260 PIN CNDAIRCL600 CL6002B19 1900309EA RT MLG CONNECTORBENT A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07418SW 7446 GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOLLOWED AND COMPLETED QRH PROCEDURE, RETURNED TO HELENA. FOUND PUSHED PIN ON RIGHT GEAR SIDE STAY ACTUATOR CONNECTOR (P110 PIN-E). RE-SECURED PIN. SWUNG GEAR. OPS CHECK GOOD. 2L72 4F RTA21EA 20030416003852003041600385EU 2003 4 16 UHLA0301091 120030109A7931IPTE1191000200 TRANSMITTER SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE ROTOL R389 R3894123F26 NE LT ENGINE OIL CONTAMINATED A UHLAO OTHER J WARNING INDICATION CRCRUISE 1 GL17148SD 340A148 132 DRG189389 DURING FLIGHT 4501 FROM PIT TO LEX, LT ENGINE OIL PRESS LIGHT ILLUMINATED INFLIGHT AND LT PROP PSI FLUCTUATING BETWEEN 0 - 100 PSI. REMOVED AND CLEANED CANNON PLUG ON OIL PRESSURE TRANSMITTER IAW SAAB AMM 73-00-00, OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 6 CP30NE 20030424001682003042400168SO 2003 4 24 LR7A03023 120030313A5311 FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND FS 814 RING SEGMENT WEB CRACKED AT LBL 67, WL 150. REPAIRED IAW SRM SMP 583 51-140-17. NR 2158. 2H74 4T A1SO 20030428001592003042800159EU 2003 4 28 03098319 120030408A3350126243 SIGN JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BROKEN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27319UE 41042 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD CABIN EMERGENCY EXIT SIGN WAS BROKEN. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030425000532003042500053CE 2003 4 25 NSVA200300022 120030321A2120 SMOKE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA CABIN DETECTED A NSVAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27129CJ UC129 AFTER NR 2 ENG START AND TAXI OUT OF GATE CREW NOTICED THE APPEARANCE OF SMOKE IN THE COCKPIT AND IN CABIN. AIRCRAFT RETURNED TO GATE AND MAINTENANCE DISPATCHED. MAINTENANCE INSPECTED RT GENERATOR AND FOUND RESIDUAL OIL. CLEANED OIL AS REQUIRED. PERFORMED VISUAL INSPECTION OF RT ENG COMPARTMENT AND OIL LINES. CLEANED ALL RESIDUAL OIL IN RT ENG COMPARTMENT. CHECKED OIL CONNECTIONS AND FOUND SCAVANGE SCREEN OIL FITTING AT ACCESSORY CASE NEEDED TO BE TIGHTENED. PERFORMED INSPECTION AND OPERATIONAL CHECK OF CABIN VENT BLOWERS. NO DEFECTS NOTED. RAN NR 2 ENG AND ALL SYS CHECK GOOD. RAN NR 1 AND NR 2 ENG WITH NO DEFECTS. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. NO OTHER REPORTS AS OF THIS DATE.2L72 4T4 TRTA24CE E4EA 20030428000312003042800031WP 2003 4 28 GTIA030176 120030306A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 PAX CABIN CENTER FLOOR PANEL STA 946 TO STA 1003 CRACKED/ DAMAGED SEVERAL INSERTS BROKEN OUT. DRILL AND LOCATE. 2L72 4F4 FRTA6WE E2EA 20030430002592003043000259 2003 4 30 SWAA030820 420030410A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING FASTENERS LOOSE. SECURED ATTACH FITTING PER MM. 2L72 4F RTA16WE 20030501001762003050100176NM 2003 5 1 ASAA0310021 120030221A5320BAC1509100146 FLOOR SUPPORT BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT STATION 767-807, STRINGER 26R CORRODED. REPAIRED FLOOR SUPPORT PER SRM. (M) 2L72 4F RTA16WE 20030505000172003050500017NM 2003 5 5 DHL2003741540 120030325A5510 STRUCTURE BOEING727 727200 138407ENM VERTICAL FIN CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, EMPENNAGE INT'R STRUCTURE VERTICAL FIN HAS CRACK AT STR 8L FIN STA 133.8 AT THRU BOLT ATTACH ANGLE TO CHORD ANGLE. CUT OUT DAMAGED AREA DIM 7.75 INCH AND FABRICATED FILLER AND 2 EACH REPAIR ANGLES FROM BAC 1517-1367 PO 3077124 FILLER DIM 7.75 INCH EACH ANGLES DIM 20 INCHES LONG AND RADIUS FILLER FROM BAC 15-12-3398. PO 9912746 DIM 20 X 1 INCH ALL IAW B-727 SRM 55-30-4 FIG 1 AND 55-30-2 FIG 2. PART TREATED WITH ALODINE, PRIMED IAW B-727 SRM 51-10-2. INSTALLED STR REPAIR AT 8L FIN STA 133.8 IAW B-727 SRM 55-30-4 FIG 1 AND 55-30-2 FIG 2. 2L73 4F RTA3WE 20030506000382003050600038WP 2003 5 6 03FDEA00656 120030429A2910 LINE DOUG DC10 DC1010 3022110WP LEFT WING SLAT DAMAGED A FDEAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO25385FE 46619 SYSTEM 1 HYD QUANTITY DROPPED BELOW 1 GALLON. NR 1 HYD PRESSURE AND TEMP REMAINED FINE. COMPLETED ACTIONS PER QRH. EVIDENCE OF HYD LEAK AT WINGROOT ON LT WING. MX TO BEGIN T/S. FOUND LEAK ON LEFT WING L/E SLAT PIPING (ITEM 720) REF 27-82-24-02 FIG 2 AT BEND. REMOVED 9 IN PIECE OF PIPING AND REPLACED NEW SECTION PER MM 20-10-01-2, LEAK CHECK GOOD. SERVICED SYS 1 HYD SYS PER 12-13-02-3, OK FOR RETURN TO SERVICE. 2L73 4F A22WE 20030505001922003050500192NM 2003 5 5 EIA2003071 120030418A5230 FITTING BOEING747 747273C 1384896NM CARGO DOOR CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 NR 4R NOSE CARGO DOOR LATCH FITTING ON NR 4 BOLT HOLE LOCATION IS CHAFED. REAMED HOLE NR 4 FROM .530 TO .5605 PER EO 53-747-1633-01 REV-C , FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED. 2L74 4F A20WE 20030507000412003050700041NM 2003 5 7 AUS20030340 120030310A242151608003 GCU LUCAS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE AC GENERATOR FAILED W O OTHER H ELECT. POWER LOSS-50 PC CLCLIMB 1 AUS 96048 (AUS) NR 1 AC GENERATOR CONTROL UNIT (GCU) FAILED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030507001992003050700199WP 2003 5 7 CH1A200395022 120030411A5315 FLOORBEAM DOUG DC7 DC7C 3021806WP FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295 45465 FLOORBEAM AT BS420 CORRODED BETWEEN RBL 12 & RBL 22. 2L74 4R 4A10 20030508000452003050800045NM 2003 5 8 03FDEA00674 120030503A3610132712 HOSE BOEING727 727200 138407ENM NR 3 PYLON LEAKING A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25222FE 20933 APPROX 5 MIN AFTER TAKEOFF PASSING THROUGH 1000 FT, ENG. 3 STRUT LT ILLUMINATED. LT EXTINGUISHED ON ITS OWN BEFORE ANY QRH ITEMS WERE ACCOMPLISHED. FOLLOWED QRH TESTED SYSTEM-GOOD AND MONITORED. PARAMETERS: A/C WEIGHT 180.0 TAT +12 EPR 1.90,1.95,1.90 N1 95%. REMOVED NR 3 STRUT LOWER PANELS AND INSPECTED DETECTOR LOOP CKD GOOD. RAN ENGINE AND FOUND A PNEUMATIC FLEX LINE LEAKING WITH TELL TAILS HEADING TOWARDS HEAT DETECTOR. THIS WAS A REPEAT ITEM, NO ANOMALY HERE ! R & R T/R FLEX LINE PER SMP. RAN #3 ENGINE PER JRH NO MORE LEAKS FOUND. 2L73 4F RTA3WE 20030509000072003050900007WP 2003 5 9 GTIA030244 120030402A2611CGAB140001 SMOKE DETECTOR DOUG DC9 DC982 3022082WP CARGO BAY MALFUNCTIONED A GTIAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23812NK 48021 CARGO FIRE DETECTION FORWARD 'B' FAIL LIGHT AND ANNUNCIATOR PANEL SMOKE DETECTOR LOOP LIGHT ILLUMINATED. REMOVED AND REPLACED CARGO COMPARTMENT SMOKE DETECTOR. (M) 2L72 4F A6WE 20030509000452003050900045SO 2003 5 9 SIMA200309603 120030402A5510KSC270720V HOUSING EMB 145 EMB145LR 3260212SO BEARING WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 ABI - DURING A IMBV INSPECTION, THE HORIZONTAL STABILIZER LEFT AND RIGHT SPHERICAL BEARING HOUSING WORN BEYOND LIMITS. REMOVED THE EXISTING BEARING FROM THE HOUSING. REAMED THE LEFT AND RIGHT HOUSING TO 2.2834 INCH. TREATED THE REWORK HOUSING AND INSTALLED FOUR FIRST OVERSIZED BUSHINGS. REPAIR DONE IAW EMB SERVICE BULLETIN 145-55-0021, FIGURE 2. (M) 2L72 4T RTT00011AT 20030513002822003051300282WP 2003 5 13 AALA20030214 120030205A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21574AA 53151 FOUND CORROSION ON CUSP WEB ABOVE MID-CARGO DOOR CUTOUT STATION 677-690. CUT OUT CORRODED SECTION OF CUSP WEB AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. (M) 2L72 4F A6WE 20030522001192003052200119 2003 5 22 MALA030270 420030518A34206226342022 DISPLAY SAAB SF340 SF340A 7850100EU COCKPIT FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15115XJ 340A115 DURING FLIGHT 2993 CAPT EHSI/EFIS DISPLAY WENT BLANK. CREW REPORTED ELECTRICAL ODOR SHORTLY AFTER SCREEN WENT BLANK. QRH/ C/B PULLED. MAINTENANCE REMOVED AND REPLACED LT EHSI AND ALL CHECKS GOOD IAW SF340 MM CHAP 34. P/N 622-6342-022, S/N ON 5068. 2L72 4T RTA52EU 20030609000252003060900025SO 2003 6 9 C2XA03TY072 120030520A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 DURING A SCHEDULED INSPECTION THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030609000722003060900072EA 2003 6 9 QXEA0300624 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS295, 2 INCHES BELOW STRINGER 18R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030515000782003051500078SO 2003 5 15 C2XA03CL094 120030427A3350744437 SIGN EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2715932 145015 CLE FLIGHT 2300 THE CREW REPORTED THE EMERGENCY EXIT SIGN AT 12A WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030612000302003061200030WP 2003 6 12 0301059865 120030523A27805919526508 DUCT DOUG DC9 DC951 3022051WP LEFT LACK OF LUBE A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01774NC 47776 ON DESCENT FOR LANDING WHEN SLATS WERE SELECTED TO EXTEND THE SLAT DISAGREE LIGHT REMAINED ON AND THE AIRCRAFT ROLLED RIGHT. CREW APPLIED COM PROCEDURES AND ACCOMPLISHED A FLAP ONLY LANDING INTO VPS. MAINTENANCE LUBRICATED THE LEFT T-DUCT AND PERFORMED AN OPERATIONAL CHECK WITH NO OTHER PROBLEMS FOUND. AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F RTA6WE 20030617000372003061700037SO 2003 6 17 AUS20030489 120030505A71605491602 ELBOW PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL ENG AIR INTAKE UNSERVICEABLE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INDUCTION ELBOW UNSERVICEABLE DUE TO AD/PA31/43. 1L72 3O3 O A20SO E14EA 5 CP33EA 20030617002912003061700291SW 2003 6 17 HEEA087034 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH2220 53386 MAIN ROTOR UNIVERAL WORN. 1G71 3U O H2SW 20030618000302003061800030NM 2003 6 18 SWAA031324 120030614A33501000679 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29080SW 22675 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20030523000182003052300018CE 2003 5 23 2003F00299 120030411A2131 CONTROLLER LEAR 60 60LEAR 5170707CE CABIN PRESSURE MALFUNCTIONED A UG8AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23699DA 237 CABIN PRESSURE CONTROLLER MALFUNCTIONING IN AUTO MODE. AIRCRAFT ABORTED ITS TAKEOFF. FAILURE OF THE PRESSURIZATION SYSTEM TO OPERATE IN AUTO MODE. REPLCED FLOW CONTROL VALVE. REPLACED LEFT EMERGENCY PRESSURIZATION VALVE. REPLACED CABIN PRESSURIZATION CONTROLLER. SYSTEM OPERATIONAL TEST PER LEARJET MM. THIS CLEARED DMI LOG M0410-1. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA10CE 20030530000112003053000011SW 2003 5 30 HEEA086672 120030522A2844209062003001 SWITCH BELL 412 412 1182202SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0321498 36003 LIGHT FLICKERS ON INTERMITTENTLY. SCRAPPED SWITCH. 1G72 4U H4SW 20030618001242003061800124NE 2003 6 18 HEEA087134 120030610A5510 PANEL SKRSKYS76 S76A 8143006NE HORIZONTAL STAB DELAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 FIBERGLASS CLOSE OUT BEHIND FITTING ASSEMBLY DELAMINATED FROM SPAR. REPAIRED. 1G72 3U H1NE 20030623000142003062300014SO 2003 6 23 ASOA03218 120030517A339703091022 CONNECTOR EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11267AS 120198 DURING A GROUND INSPECTION IN DFW, THE AFT SECTION OF THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTION IN THE AFT SECTION EMERGENCY LIGHTING AND RE-SECURED THE CONNECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030630000202003063000020EU 2003 6 30 U30A200300015 120030508A2897MB926T12F4S CONNECTOR AIRBUS320 A320212 3930322EU NR 2 FUEL PUMP ARCED A U30AK NONE J WARNING INDICATION ININSP/MAINT 1 EA17265AV 427 DURING MAINTENANCE INSPECTION, DURING ENGINE RUN, AN ECAM MESSAGE FOR THE RT FUEL TANK PUMP NR 2, LOW PRESSURE. FURTHER TROUBLESHOOTING REVEALED ELECTRICAL ARCING AT THE RT WING FUEL PUMP WIRE HARNESS CONNECTOR. RELATED CIRCUIT BREAKER DID NOT TRIP. REPLACED FUEL PUMP IAW AMM. REPLACED FUEL PUMP CONNECTOR. INSPECTED ALL REMAINING WING (RT & LT) AND CENTER SECTION FUEL PUMPS & WIRING WITH NO OTHER DEFECTS NOTED. RELACED CIRCUIT BREAKER FOR PRECAUTIONARY REASONS. OPERATIONALLY CHECKED THE FUEL PUMP SYSTEM IAW AMM, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030630000812003063000081SW 2003 6 30 HEEA087843 120030618A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 MAIN ROTOR UNIVERSAL WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030707000622003070700062NM 2003 7 7 2003UALA00521 120030626A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 MAIN CABIN AT STATION 1065, LBL 11, SEAT TRACK WORN. 2L72 4F4 FRTA1NM E24NE 20030716001092003071600109 2003 7 16 HEEA088037 420030707A3421102005901 INDICATOR SKRSKYS76 S76A 8143006NE ATTITUDE PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 ATTITUDE INDICATOR PRECESSES. SHOP REPAIR. 1G72 3U H1NE 20030630000542003063000054 2003 6 30 ALGA087723 420030624A830023071896 GEARSHAFT BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0360WJ 704 CAG70698 45276 CAE860696 FOUND SPALLING ON GEAR TEETH. REMOVED AND REPLACED DUE TO SPALLING ON GEAR TEETH FROM POSSIBLE IMPROPER MESHING OF GEAR TEETH. 1G71 3U3 U H2SW E1GL 20030708000402003070800040WP 2003 7 8 UPS03840901 120030602A5313 LONGERON DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3B 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3, AFT PIT BETWEEN STA 1260 AND STA 1280 STR 36 CRACKED REMOVED CRACKED LONG 36 FS 1270-1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 36 FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0. 2L74 4F4 FRT4A25 1E8 20030702000182003070200018NM 2003 7 2 AMTA200300756 120030516A3230 LINK BOEING737 73783N 13844HINM NLG GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11317TZ 28246 NLG LOWER TORSION LINK LEFT SIDE OF LOWER FACE GOUGED 3.25 INCH FROM CENTER OF APEX LUGS. REPAIRED TORSION LINK IAW ER/A 737-32R-5180. (M) 2L72 4F RTA16WE 20030707001482003070700148NM 2003 7 7 DHL2003752003 120030625A5250 DOOR BOEING727 727223 1384074NM COCKPIT LOOSE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01752DH 22466 COCKPIT DOOR KNOB AND LOCK ARE LOOSE. IT IS DIFFICULT TO OPEN AND CLOSE DOOR. RE-SECURED DOOR LATCH. OPS CHECKED OK IAW MM 52-50-1. 2L73 4F A3WE 20030702000372003070200037CE 2003 7 2 2003F00390 120030528A2161 CONTROLLER LEAR 35 31A 5170531CE CABIN TEMP MALFUNCTIONED A GTIAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL23712EJ 231 INADVERTENT ACTIVATION OF EMERGENCY AIR FLOW AT 9000 FT. TROUBLESHOOTING, INSPECTION OF PRESSURIZATION SYSTEM COMPONENTS, GROUND AND SUBSEQUENT FLIGHT PRESSURIZATION CHECKS PROVED NO NOTED DEFECTS. DURING OPERATIONAL CHECK/TESTS, FOUND PRESSURE REGULATORS FOR PRESSURIZATION AND TEMPERATURE CONTROL TO BE MARGINAL IN OPERATIONAL PRESSURE. REMOVED AND REPLACED BOTH LEFT AND RIGHT SERVO AIR PRESSUR REGULATORS IAW LEAR 31 MM 21-30-08, PAGE 201. FUNCTIONALLY CHECKED BOTH REGULATORS INDIVIDUALLY TO ENSURE THEY REGULATE AT 15 PSI. SATISFACTORILY COMPLETED AN OPERATIONAL CHECK OF PRESSURIZATION SYSTEM IAW LEAR 31 MM 21-30-00, PAGE 209. (M) 2L72 4F RTA10CE 20030709000432003070900043WP 2003 7 9 AALA20030512 120030430A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21216AA 49167 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 12D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT PIGTAIL AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030714000102003071400010EA 2003 7 14 COMA0360304 120030626A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DEFECTIVE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01986CA12262 7174 FLIGHT 5584 DURING DESCENT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY. REPLACED RIGHT BRAKE POSITION SENSING UNIT. 2L72 4F RTA21EA 20030128000432003012800043SW 2003 1 28 HEEA083797 120030115A7120 BEARING BELL 407 407 1182206SW REAR MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 14880 53159 REAR ENGINE MOUNT HAS A WORN SPHERICAL BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128000582003012800058SW 2003 1 28 HEEA083812 120030116A6210406010120101 BOLT BELL 407 407 1182206SW M/R BLADE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 MAIN ROTOR BLADE BOLTS HAVE CORROSION BEYOND LIMITS. 1G71 3U O H2SW 20030128001162003012800116 2003 1 28 159PL0026 420030127A22102588812901 COMPUTER BOEING737 737242 1384477NM ROLL CHANNEL MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05159PL 21186 ROLL CHANNEL AUTO PILOT WILL NOT ENGAGE. REMOVED AND REPLACED ROLL CHANNEL COMPUTER PER MM 22-11-161. 2L72 4F A16WE 20030128002272003012800227NM 2003 1 28 AWXA200300039 120030113A532069152241 STRAP BOEING737 7373Y0 1384671NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK THE FORWARD CARGO COMPARTMENT DOOR OPENING FORWARD TORQUE BOX COVER (REVEAL STRAP) WAS FOUND TORN AND CHAFED ON EDGE BS 440, STR 19R TO 24R. MAINTENANCE BLENDED TORN AND CHAFED OF FORWARD CARGO COMPARTMENT DOOR OPENING FORWARD TORQUE BOX COVER AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED TORQUE BOX COVER; FABRICATED A NEW REPLACEMENT TORQUE BOX COVER PER DWG 69-15224; AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 3 & 4. 2L72 4F RTA16WE 20030129001282003012900128EU 2003 1 29 HEEA084001 120030113A2822D107318D1 PUMP BOLKMS105 BO105S 5626006EU FUEL BOOST INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 FUEL BOOST PUMP INOPERATIVE. 1G72 3U H3EU 20030205000372003020500037NM 2003 2 5 SROM200300004 120030107A532065207269 SUPPORT BOEING737 737205 1384456NM FUSELAGE DAMAGED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA322481310 23466 DURING C CHECK INSPECTION FOUND MECHANICL DAMAGE ON FLOOR TO SIDEWALL SUPPERT AT BS 480 IN FWD CARGO BAY. REMOVED DAMAGED PART, DRILLED NEW PART, INSTALLED HARDWARE & INSTALLED PART PER SRM 51-30-2. MINOR REPAIR. 2L72 4F RTA16WE 20030206001852003020600185NE 2003 2 6 SWAA030272 220030204A7320658385 VALVE BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAULTY A SWAAK NONE R PARTIAL RPM/PWR LOSS UKUNKNOWN 1 SW29086SW 22827 THE NR 1 ENGINE COMPRESSOR STALLS WHEN THROTTLE ADVANCED. REMOVED AND REPLACED NR 1 ENG START CHECK VALVE AND PRESS RATIO BLEED CONTROL PER MM. 2L72 4F4 F A16WE E2EA 20030214001102003021400110WP 2003 2 14 ASAA0380058 120030105A5320993061237N WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 1174-1250. REPLACED CUSP WEB PER SRM 51-30-2 AND 51-30-5. (M) 2L72 4F RTA6WE 20030216000052003021600005EU 2003 2 16 RAIA00302038 120030204A3200C245890002 UPLOCK AEROSPATR72 ATR72202 8680940EU INTERMITTENT A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03723TE2090318337 283 5552-STL- LANDING GEAR HANDLE WILL NOT GO TO THE RETRACT POSITION. MAINTENANCE REMOVED AND REPLACED THE L/H MLG UP-LOCK BOX. 2H72 4T RTA53EU 20030314000302003031400030WP 2003 3 14 03FDEA00108 120030204A5730 SKIN DOUG DC10 DC1030 3023501WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25318FE 46837 LEFT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108, LT WING PANEL, AT STATION XIS 168.66 TO XORS 130.40, STRINGER 7L AND 19L, AREAS A-THRU -I IN ACCORDANCE WITH SRM CHAPT 51 AND SRM 57-10-00 IN COMPLIANCE WITH EA 8-5710-67584. REF SNRM N238, N332, AND 775. 2L73 4F A22WE 20030220001092003022000109EA 2003 2 20 QXEA0300104 120030119A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09601QX 10009 SUP LAX ON FLIGHT 2550- FIRE SYSTEM FAULT STATUS MESSAGE. PERFORMED FIRE DETECTION SYSTEM TEST PER CRJ AMM 26-10-00 PAGE 501-504. NO FAULTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030224001092003022400109SW 2003 2 24 HEEA084224 120030120A2510407070620149 PANEL BELL 407 407 1182206SW SEAT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 SEAT PANEL CRACKED. 1G71 3U O H2SW 20030227000042003022700004SW 2003 2 27 HEEA084361 120030211A6710407375038101 PANEL BELL 407 407 1182206SW COLLECTIVE STICKDAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 LIGHTED PANEL ON COLLECTIVE STICK CHIPPED ALONG LOWER EDGE. 1G71 3U O H2SW 20030228000242003022800024NM 2003 2 28 SWAA030384 120030217A53206547978 BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 867 & BS 897, WL 208. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030912001202003091200120NM 2003 9 12 AWXA200300887 120030725A53156546592 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 770, RBL 5. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF AFT CARGO COMPARTMENT FLOORBEAM AT BS 770, RBL 5; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-53, FIG 201, PG 1. 2L72 4F RTA16WE 20030929000852003092900085NM 2003 9 29 DHL2003745019 120030904A3213 STRUT BOEING727 727224 1384076NM NLG DISCHARGED A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01745DH 20665 AFTER SMOOTH LANDING AND DURING MINIMAL BRAKING ROLLOUT, NOSE STRUT FELT TO BOTTOM OUT AND FORWARD ENTRY DOOR LIGHT ILLUMINATED. AIRCRAFT STOPPED AND DOOR CHECKED BY S/O. HANDLE NOT FULLY DOWN AND LOCKED. SERVICED NOSE STRUT AS REQUIRED IAW B727 M/M 12-15-24. NO LEAKS NOTED. ADJUSTED ENTRY DOOR FOR SOFT UNLATCHING IAW B727 M/M 52-11-01. NO DEFECTS NOTED. 2L73 4F A3WE 20031002001412003100200141NM 2003 10 2 CALA0300525 120030911A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND LIGHT CORROSION ON O/B FLANGE OF LEFT KEELBEAM FROM BS 663-727. INSTALLED REPAIR IAW ECRA 5311-01167. 2L72 4F RTA16WE 20031003000482003100300048NM 2003 10 3 AWXA200301053 120030827A5343656717218 FITTING BOEING737 737277 1384570NM STAB FITTING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK CORROSION WAS FOUND ON RT MAIN LANDING GEAR BEAM INBOARD STABILIZER FITTING AT TRAILING EDGE OF WING. MAINTENANCE REMOVED AND REPLACED CORRODED STABILIZER FITTING IAW AMM 57-01-000-4, PG. 1-2. 2L72 4F RTA16WE 20031006001572003100600157NM 2003 10 6 SWAA031960 120030901A2560P2070001 FLASHLIGHT BOEING737 7373Q8 1384670NM FWD CABIN WEAK A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 EMERGENCY FLASHLIGHT IN FWD CABIN WEAK. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20031006001072003100600107NM 2003 10 6 2003UALA00675 120030909A5311 FRAME AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29816UA 871 AFT PIT FRAME 54L DAMAGED AT STR 38L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA28NM E40NE 20031014001542003101400154NM 2003 10 14 SWAA032073 120030917A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED C2 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20031021002892003102100289NM 2003 10 21 CALA0300547 120030921A5320 ANGLE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND ZEE ANGLE CORRODED AROUND FASTENER AT L-2 DOOR, STA 947-986. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20031023000262003102300026NM 2003 10 23 UPS03441248 120030907A532065B38600140 CLIP BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C M/D, BS 840 STR 6L FRAME ATT TIE CLIP CRACKED. M/D BS 840 STR 6L FRAME ATT TIE CLIP REPLACED IAW SRM 51-10-01 P.8. 2L74 4F4 F A20WE E20EA 20030908003242003090800324NM 2003 9 8 SWAA031902 120030825A2560PH22300L STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 EEPLS PHOTOLUMINICENT STRIP LOOSE AT MID CABIN. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20030910000562003091000056SW 2003 9 10 HEEA088923 120030822A6710214010434001 BEARING BELL 214 214ST 1182106SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 WHEN BEARING GREASED, BLACK GREASE COMES OUT. 2G72 4U H10SW 20031027001422003102700142WP 2003 10 27 0301819613 120030903A5320 DOUBLER DOUG DC9 DC932 3022066WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47438 DURING L-CHECK FOUND CRACK IN EXISTING REPAIR DOUBLER ON AFT CARGO DOOR JAMB AT BS 897. REPAIRED PER EA 96-195991. 2L72 4F A6WE 20031028000362003102800036EA 2003 10 28 03266688 120030923A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27688BR 7723 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20040114000362004011400036NM 2004 1 14 DL733030948 120031024A3350 FUSE BOEING737 737347 1384647NM BATTERY RACK BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27305WA 23346 EMERGENCY LIGHT AT SEAT 27DEF INOP. REPLACED 5 AMP FUSE ON BATTERY RACK. 2L72 4F RTA16WE 20040115001702004011500170NM 2004 1 15 03FDEA02163 120031211A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 BS 720 STR 6 LT STRINGER CLIP IS CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 720, STR 6L IAW SRM 51-30-02. 2L73 4F RTA3WE 20030228001262003022800126 2003 2 28 HEEA084473 420030214A2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 TRANSMISSION SOUNDS SCRATCHY AT RECEIVING STATIONS. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030306001232003030600123NE 2003 3 6 HEEA084876 120030227A77140177555240 TACH GENERATOR SKRSKYS76 S76A 8143006NE NR 1 MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 NR 1 OVERSPEED GOVERNOR LIGHT OFF AND ENGINE WILL NOT MOTOR. 1G72 3U H1NE 20030307001162003030700116EU 2003 3 7 AALA20030043 120030110A3350 CONNECTOR FOKKERF28 F28MK0100 4990807EU CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW211411G 11369 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT IN FIRST CLASS INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030307001862003030700186WP 2003 3 7 AALA20030075 120030118A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21496AA 49734 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM 20D AFT, EXITS AND SEATS, ARE INTERMITTENT. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030121000452003012100045SW 2003 1 21 HEEA083241 120030108A2510 CLIP BELL 206 206L3 1182108SW SEAT BACK BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 SEAT BACK HAS A BROKEN CLIP. REPAIRED. 1G71 3U H2SW 20030318000962003031800096NM 2003 3 18 2003UALA00264 120030311A5315 CAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE ERODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 CABIN STA 1640, RBL 57" FLOORBEAM TOP CAP HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. PERFORMED SINGLE FLANGE BLENDOUT REPAIR. 2L72 4F4 FRTA2NM E17NE 20030123000292003012300029NM 2003 1 23 2003UALA00048 120030111A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 CABIN FLOOR BEAM UPPER CHORD HAS INTERGRANULAR CORROSION BODY STATION 310, RBL 40-45. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM UPPER CAP. 2L72 4F4 FRTA2NM E17NE 20030324000312003032400031WP 2003 3 24 CALA0300140 120030323A5210 SKIN DOUG DC9 DC982 3022082WP L-I DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0915820 49480 INSPECTION FOUND A 1/2" CRACK IN L-1 DOOR SKIN AT AFT LOWER CORNER. A REPAIR WAS INSTALLED IAW SRM 52-05, PAGE 223. 2L72 4F A6WE 20030331000592003033100059WP 2003 3 31 ARWA20030302 120030311A3241 WIRE DOUG DC8 DC863F 302198FWP ANTI SKID SYS DAMAGED A ARWAO OTHER N FALSE WARNING APAPPROACH 1 SO19441J 45988 ON FINAL ANTI-SKID LIGHT STAYED ON WITH LFI INDICATION. CHECKED ANTI-SKID WIRING IAW W/D 32-3-0. FOUND BROKEN WIRE GOING TO LT IN-BOUND VALVE, REPAIRED WIRE IN ACCORDANCE WITH MM 20-50-1, OPERATIONAL CHECKED ANTI-SKID SYSTEM IAW MM 32-43-0. OPERATIONAL CHECKED NORMAL. ANTI-SKID SYSTEM CHECKED NORMAL IAW MM 32-43-0. 2L74 4F 4A25 20030418000022003041800002NM 2003 4 18 P5CA0300766 120030208A2613533T301181 CIRCUIT CARD BOEING747 747400 NM FIRE WARNING FAULTY A P5CAO OTHER J WARNING INDICATION LDLANDING 1 WP23496MC 29257 ON LANDING ROLL EICAS MSG APPEARED -APU FIRE LOOP A-, -APU FIRE LOOP B- AND APU BOTTLE LOW-. NO INTERIOR OR EXTERIOR INDICATIONS OF FIRE. DE-ACTIVATED APU PER AMM 49-11-00-042-064 AND DEFERRED PER DDPG 49-11-01. 2L74 4F RTA20WE 20030421000172003042100017WP 2003 4 21 ZW0A0302301 120030218A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13950U 49230 DURING CHECK-C MAINT FOUND CORROSION ON CABIN SEAT TRACK AT STA 1150 TO 1164, LBL 22. REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION PER SRM 53-05, FIG 4F, FROM STA 1150 TO 1230. 2L72 4F A6WE 20030417002062003041700206WP 2003 4 17 ZW0A0302103 120030211A5310 BEAM DOUG DC9 DC982 3022082WP SERVICE DOORWAY CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13950U 49230 DURING CHECK-C, THE FWD SERVICE DOOR LOWER BEAM WAS CRACKED AT FWD END IN RADIUS. ALSO A SMALL CLIP WAS CRACKED INSIDE LIGHTENING HOLE AT UPPER AFT CORNER. REPLACED CLIP AND REPLACED LOWER BEAM PER SPM 6-70-01. 2L72 4F A6WE 20030327001972003032700197CE 2003 3 27 CA030211010 120030121A27801003840403 MOTOR BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA TE FLAP FAILED W H DEACTIVATE SYST/CIRCUITS BF SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN) AFTER LANDING, FLIGHT CREW RETRACTED WING FLAPS AND TAXIED TO APRON. UPON DEPARTING THE AIRCRAFT, AN ODOR WAS DETECTED IN CABIN AROUND WING FLAP MOTOR POSITION AND FLAP SYSTEM CIRCUIT BREAKER WAS POPPED. ALL OTHER SYSTEMS WERE OPERATING NORMAL DURING GROUND CHECKS. AIRCRAFT RETURNED TO BASE WITH THE WING FLAP SYSTEM DISABLED, AND A FLAPLESS LANDING WAS CARRIED OUT. THE FLAP MOTOR/GEARBOX WAS INSPECTED AND FOUND TO BE INOPERATIVE, WITH AN ACCOMPANYING BURNT ODOUR. THE FLAP MOTOR/GEARBOX WAS REPLACED WITH AN OH UNIT PN 100-524073-1 AND FLAP RIGGING CHECKS CARRIED OUT. SYSTEMGROUND-CHECKED AND FOUND TO BE OPERATIONAL. 1L72 3T4 T A14CE E4EA 20030722000472003072200047 2003 7 22 SWAA031505 420030708A2565 INDICATOR BOEING737 7372H4 138448CNM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29071SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030729000872003072900087NM 2003 7 29 QXEA200300752 120030618A5540 STRUCTURE DHAV DHC8 DHC8202 2809007NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX- FORE RUDDER CRACKED AT LOWER LEFT HAND SIDE OF PREVIOUS REPAIR. REPAIRED IAW DHC-8 SRM 55-40-28. 2H72 4T RTA13NM 20030826001392003082600139NM 2003 8 26 UIEA200300041 120030731A2750 SPINDLE BOEING747 74747UF 1384949NM T/E FLAP LACK OF LUBE A UIEAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 EA15408MC 29261 ON APPROACH WHEN LANDING FLAPS 30 SELECTED, EICAS MESSAGE 'FLAPS DRIVE'. INBOARD T/E NORMAL, OUTBOARD T/E AT FLAPS 25. GO AROUND EXECUTED AND NNP ACCOMPLISHED. ON SUBSEQUENT APPROACH MESSAGE 'FLAPS DRIVE'. AFTER LANDING WHEN FLAPS RETRACTED EICAS MESSAGE 'FLAPS DRIVE' AND OUTBOARD T/E FLAPS REMAINED AT FLAPS 25. FOUND C/B FROM ELECTRIC OPERATION POPPED. RESET C/B AND ALSO FOUND ALL FLAP TRACK SPINDLE ASSEMBLIES, INBOARD AND OUTBOARD FLAPS, VERY DRY. GREASED ALL 8 SPINDLES ACC MM 27-51-00. CHECKED OPERATION AND FOUND NORMAL. (M) 2L74 4F RT1384945 20030723000432003072300043NM 2003 7 23 TSAA0353133 120030506A5315 FLOORBEAM BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 FOUND CORROSION DISCOVERED AT BS 312 FLOORBEAM UPPER TEE. CUTOUT DAMAGED SECTION OF STRINGER. FABRIATED NEW CHORD SECTION AND SPLICE ANGLE. DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-9, FIGURE 5. (M) 2L72 4F RTA16WE 20030805001152003080500115NE 2003 8 5 ALGA088095 120030714A6320E6893673 GEAR SKRSKYS76 S76A 8143006NE GEARBOX INOPERATIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03705AL219 760267 T/M GEAR REMOVED FOR INSPECTION IAW SBT-076 REMOVED AND REPLACED T/M GEAR. 1G72 3U H1NE 20030805001182003080500118EU 2003 8 5 BAQA088273 120030730A3340 RELAY BOLKMS117 BK117A3 5626015EU SEARCH LIGHT INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911BK132 7099 LAMP RELAY INTERMITTENT. EXTEND AND RETRACT MOTOR ROUGH. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030806000972003080600097SO 2003 8 6 C2XA03TY110 120030801A534714532605009 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK RW 5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030807000202003080700020WP 2003 8 7 WX030007 120030714A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WXOAK NONE O OTHER ININSP/MAINT 1 WP17860GA 49786 DURING ACCOMPLISHMENT OF A SERVICE CHECK IN FAT, MAINTENANCE FOUND EMERGENCY TRACK FLOOR LIGHTS INOPERATIVE FROM ROW 30 TO ROW 34 AND EMERGENCY FLOOR TRACK LIGHT COVER AT AFT EXIT ROW TO BE UNSECURE. THE CONNECTOR AT ROW 34 WAS RECONNECTED AND THE UNSECURED COVER SECURED OPERATIONAL CHECK WAS PERFORMED. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20030905001722003090500172NM 2003 9 5 USAABB03134 120030814A2780 SLAT BOEING767 767201 1385125NM WINGS MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19645US 23897 PIT - FLT 740 - ON CLIMB-OUT FROM PIT, AT 3,500 FEET, CREW RECEIVED A LEADING EDGE SLAT DISAGREE EICAS MESSAGE AND A LEADING EDGE LIGHT WITH FLAP HANDLE AT ZERO POSITION. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT PIT. ON FLAP EXTENSION, CREW REPORTED AN UNUSUAL BINDING NOISE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS MAINTENANCE FERRIED FROM PIT TO PHL. FLIGHT CREW REPORTED NO FAULTS WITH LEADING EDGE SLATS DISAGREEMENT. MAINTENANCE PERFORMED FIM PROCEDURES 27-51-00/101-104 AND 27-81-00/101-104. NO FAULTS DETECTED. ALSO, PERFORMED VISUAL INSPECTION OF LEADING EDGE SLATS AND CYCLED SLATS/FLAPS NUMEROUS TIMES. ALL CHECKS NORMAL. (M) 2L72 4F RTA1NM 20030905001822003090500182EU 2003 9 5 ASOA03369 120030813A5210 DOUBLER AEROSPATR72 ATR72 EU PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 FLT 4285 - DURING A HANGAR INSPECTION IN MCN, THE FORWARD PASSENGER DOOR FIRST STOP DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW SRM 51-24-06. THIS MRR WILL REMAIN OPEN PENDING THE PERMANENT REPAIR, TO BE COMPLIED WITH AT THE NEXT A-CHECK. (M) 2H72 4T RT 20030805001012003080500101EU 2003 8 5 ASOA03272 120030622A2120 SMOKE AEROSPATR72 ATR72 EU CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11641AS 387 FLT 4308 - DURING FINAL APPROACH FROM ATL-PFN, THE FLIGHT ATTENDANT SMELLED AND OBSERVED SMOKE IN THE AFT CABIN SECTION. THE AIRCRAFT LANDED SAFELY IN PFN. MAINTENANCE GROUND RAN THE ENGINES OPERATING ALL RELATED SYSTEMS, BUT COULD NOT DUPLICATE THE SMOKE OR SMELL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030812000562003081200056SW 2003 8 12 HEEA088490 120030422A6710212001035101 FORCE GRADIENT BELL 412 412 1182202SW FLT CONTROLS ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 FORCE GRADIENT BEARING ROUGH; STICKING; CANNON PLUG CORRODED. REPAIRED. 1G72 4U H4SW 20030814001412003081400141NM 2003 8 14 AALA20030441 120030410A3350 NUT BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21683A 25340 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. ADJUSTED EMERGENCY EXIT LIGHT WING NUT ON ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030725000312003072500031NE 2003 7 25 RAIA00305144 220030519A7320 LINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE P3 UNSECURE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03551HK 41040 76094 ENGINE NR 1 UNCOMMENTED SHUT DOWN. MAINTENANCE SECURED P3 LINE AND OPS CK OK. 2L72 4T4 TRTA41NM E18NE 20030729000112003072900011EA 2003 7 29 03184662 120030703A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27662BR 7526 DURING MAINTENANCE INSPECTION, THE SECOND TO AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030825000932003082500093EA 2003 8 25 COMA0360358 120030809A3234750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01920CA3192 7022 FLIGHT 5520 GEAR DISAGREE WARNING, RT MLG INDICATED INTRANSIT. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20030910001822003091000182SO 2003 9 10 SIMA200322504 120030807A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21819AE 145566 ABI - DURING AN MBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF DAMAGED OMEGA BEAM. FABRICATED A REPAIR ANGLE, FILLER, SHIMS, REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-22-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20040204001042004020400104NM 2004 2 4 AWXA200301284 120031002A532069353521 STRINGER CLIP BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A .1250 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN AFT CARGO COMPARTMENT AT BS 727B, STR 23 LT. MAINTENANCE REMOVED AND REPLACED CRACKED STRINGER TIE CLIP AT BS 727B, STR 23 LT IAW DWG 69-46596. 2L72 4F4 FRTA16WE E2GL 20040204001242004020400124EU 2004 2 4 MALA030472 120031016A27208377M7 ACTUATOR SAAB SF340 SF340A 7850100EU RUDDER LIMITER FAILED A MALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL1599XJ 340A099 DURING FLIGHT NR 2790 RUDDER LIMITER OVER RIDE C/B TRIPPING INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RUDDER LIMITER OVERIDE ACTUATOR IAW SF340 MM 27-21-60 PN OFF 8618M2 SN/OFF 106374A PN/ON 8377M7 SN/ON M169 ALL OPS CHECKS GOOD. 2L72 4T RTA52EU 20031103000232003110300023NM 2003 11 3 DL733030877 120030925A5330654576660 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312WA 23598 FUSELAGE/SKIN/STA 500D - STA 520/STR 12R - REPAIR OF CRACK. THE CRACK IS CUT OUT OF THE FUSELAGE SKIN AND AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER ARE INSTALLED IN ACCORDANCE WITH ER/A 381822-14 REV C. 2L72 4F RTA16WE 20040212001682004021200168NM 2004 2 12 2003UALA00970 120031218A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE STRINGER CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STA 460 STRINGER 14R HAS A CRACKED SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20031117000622003111700062NM 2003 11 17 C1HA200385009 120031004A3350 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT DISCHARGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 EMERGENCY EXIT LIGHT OVER AFT AIRSTAIRS DOOR OUT. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT OVER AFT AIRSTAIRS DOOR AS REQ'D, OPS NORMAL. 2L73 4F A3WE 20031105000282003110500028NM 2003 11 5 AWXA200301353 120031013A5320146N5399 WEB BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FORMER WEB BS 1420, LBL 2. MAINTENANCE REMOVED DAMAGED FORMER WEB FROM BS 1420, LBL 2; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 1, PARA B1-A. 2L72 4F RTA2NM 20040108001052004010800105 2004 1 8 KBM2003F00055 420031012A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE VHF SYSTEM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 VHF RADIO DROPS PILOTS VOICE OUT DURING LONG TRANSMISSIONS. INSTALLED SERVICEABLE VHF RADIO. 1G71 3U3 UNCH9EU E19EU 20040113000012004011300001SW 2004 1 13 ALGA091602 120031219A6220407010105101 STUD BELL 407 407 1182206SW M/R HEAD CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03497AL A224 53172 FOUND 8 EA. STUDS CRACKED AT BASE OF THREAD SHANK IN RADIUS. 1G71 3U O H2SW 20040311000422004031100042NM 2004 3 11 ASAA0310145 120030316A53206519603507 ANGLE BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND ANGLE AT BS 344-380, RIGHT BUTTOCK LINE 62 CRACKED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040114000772004011400077NM 2004 1 14 DLM88030992 120031109A3260329202570 SWITCH DOUG MD88 MD88 3023688NM NLG DEFECTIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27932DL 49719 AFTER T/O WHEN GEAR HANDLE WAS RAISED THE NOSE GEAR RED UNSAFE MSG ILLUMINATED. REPLACED S1-412 INTERLOCK SWITCH. 2L72 4F RTA6WE 20031216000812003121600081NM 2003 12 16 SWAA032577 120031121A3350PL2230LH00 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 17, 23, 16, 14, 2, AND 1. REMOVED AND REPLACED TRACK COVERS PER MM. 2L72 4F RTA16WE 20031217000602003121700060WP 2003 12 17 DHL2003807505 120031007A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING CTR L/E UPPER FORMER 0.250 CRACK AT STA XFS 297.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RIGHT WING CENTER L/E UPPER FORMER STA XFS 297.750 IAW SRM 57-2-0 PG 9, 10 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031217001912003121700191SO 2003 12 17 SWIA200312610 120031118A5753 BRACKET EMB 120 EMB120ER 3260203SO FLAP ACTUATOR FAILED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07189SW 120048 FLAP CONTROL FAULT ON EXTENSION OF FLAPS 25. REMOVED AND REPLACED FORWARD ACTUATOR BRACKET FOR LEFT ACTUATOR. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031218000012003121800001SO 2003 12 18 CHQA0000430 120031116A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11833 145687 DURING SCHEDULED OPERATIONAL CHECK, THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB P/N 1317 IAW AMM 33-50-09. OPS CHECK GOOD. 2L72 4T RTT00011AT 20031219000512003121900051NM 2003 12 19 375PA0022 120031207A3350S417N5091 LIGHT BOEING737 73739A 138447PNM CABIN INOPERATIVE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY MISSING AT ROW 16 AREA. INSTALLED EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY PER MM 33-51-81. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20040105001622004010500162CE 2004 1 5 AMWA94 120031216A143050420066380 RIVET BEECH 1900 1900D 1154162CE FUSELAGE SHEARED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE WINDOW FINGER DOUBLER WAS FOUND TO HAVE ONE SHEARED RIVET. 2L72 4T RTA24CE 20031009000502003100900050NM 2003 10 9 03FDEA01648 120030926A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON STRINGER AT BS 720F 18, STR 27R. CUT OUT DAMAGED STR B/S 720F 9 FABRICATED AND INSTALLED STR 27R. REPAIRED IAW SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20031009000582003100900058WP 2003 10 9 DHL2003807014 120030913A28305252541 ACTUATOR DOUG DC8 DC873F 302199FWP FUEL DUMP FAILED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01807DH 45990 ELECTRIC FUEL DUMP NOT WORKING. DEFERRED ELECTRIC FUEL DUMP AS PER MEL 28-9-1. ASSIGNED DMI #14138. COLLARED CIRCUIT BREAKER AND PLACARDED PANEL. REF. DMI #14138 - ELECTRIC FUEL DUMP NOT WORKING. REMOVED AND REPLACED FUEL DUMP ACTUATOR PER M/M 28-30-2. OPS CHECKED GOOD. THIS CLEARS DMI 14138. 2L74 4F RT4A25 20031125001442003112500144NM 2003 11 25 ASAA0340122 120030310A532065C33896145 WEB BOEING737 737490 1384715NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 PAE - DURING C-CHECK, FOUND LEFT MLG LOWER CUT OUT WEB CHAFED BEYOND LIMITS. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031126000452003112600045 2003 11 26 03315675 420031111A31606229810016 DISPLAY CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A VTZAO OTHER O OTHER CRCRUISE 1 EA27675BR 7635 DURING FLIGHT CREW REPORTED THE NR 2 MULTI FUNCTION DISPLAY FAILED. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. THE DISPLAY UNIT WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031126000762003112600076SO 2003 11 26 C2XA03SH454 120031112A531014525480003 DOOR FRAME EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031208000322003120800032NE 2003 12 8 2003UALA00846 220031107A72301663M24P01 BLADE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ENGINE INLET OUT OF TRIM A UALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP29916UA 25383 726277 LANDED DSM UNDER AMBER ALERT DUE TO A NR 1 ENGINE VIBRATION. ACCOMPLISHED VIBRATION TROUBLESHOOTING ON THE NR 1 ENGINE AND FOUND NO DISCREPANCIES. TO ENSURE THE ENGINE WAS WITHIN ACCEPTABLE VIBRATION LIMITS AN ENGINE TRIM BALANCE WAS ACCOMPLISHED ON THE NR 1 ENGINE BY TEST CELL PERSONNEL. 2L72 4F4 FRTA16WE E2GL 20031208000492003120800049NM 2003 12 8 VNAA0310006 120031007A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07423JS164561263 3032 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 9 AND 10 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031208001372003120800137NM 2003 12 8 2003UALA00786 120031020A5310 WINDOW FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 FLIGHT DECK 3L WINDOW FRAME HAS CORROSION ON LWR SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED WINDOW SILL. 2L74 4F4 FRTA20WE E24NE 20031208001392003120800139EU 2003 12 8 2003UALA00789 120031022A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29429UA 539 ROWS 2AB, 11ABC, 21ABC, 22ABC, 25ABC EELS ARE INOPERATIVE. REPLACED EEL LIGHTS. CHECKS OKAY. 2L72 4F4 FRTA28NM E40NE 20040122001362004012200136NE 2004 1 22 WRLA200323 220031123A7261 ENGINE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 3 MALFUNCTIONED A WRLAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 SO11278WA 48746 733779 ENGINE 3 OIL PRESSURE LOW LEVEL 2 ALERT. TEMPERATURE AND QUANTITY STABLE. ENGINE SHUTDOWN IAW PROCEDURE. REPLACED NR 3 ENGINE IAW PAPER WORK CARD 0104 COMPLIED WITH PREFLIGHT HANDBOOK MM 71-00-01. REPLACED ENGINE. (M) 2L73 4F4 FRTA22WE E24NE 20040128000882004012800088NM 2004 1 28 AWXA200301634 120031203A575465C266032 SKIN BOEING737 737301 1384611NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK THE RIGHT WING NR 4 SLAT WAS FOUND DELAMINATED AT INBOARD LOWER TRAILING EDGE. MAINTENANCE CUT OUT DELAMINATED SECTION OF SKIN AT INBOARD LOWER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TO SLAT SKIN IAW B737-300 SRM 51-70-10, FIG 5 & 16, PG 8, 31, 41, 43-44, & 67-69. 2L72 4F RTA16WE 20031015000112003101500011NM 2003 10 15 USAASB03167 120030916A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US 24862 MAINTENANCE REPORTED THE INTERIOR EMERGENCY LIGHTS AT SEAT ROW 12 THROUGH 19 AND THE EXTERIOR EMERGENCY LIGHTS AT THE AFT LEFT WING-TO-BODY FAIRING AND THE AFT RIGHT OVERWING EXIT ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POSITION NR 5. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20031020001312003102000131SO 2003 10 20 RAIA00309253 120030908A7897 WIRE HARNESS EMB 145 EMB145 3260210SO NR 1 T/R DEFECTIVE A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03805HK 145096 52366-PIT- ENG NR 1 T/R DISAGREE. MAINTENANCE PLACED NR 1 T/R ON DEFERRAL PER MEL. SUBSEQUENTLY CLEARED DMI BY REPAIRING T/R ELECTRICAL HARNESS. 2L72 4F RTT00011AT 20031209002482003120900248NM 2003 12 9 UPS03241529 120031014A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, SUSPECT CRACK AT NR 3 RT COCKPIT WINDOW CUTOUT AFT LWR CORNER. REPAIR CARRIED OUT IAW SRM 51-30-02, 53-30-03, 51-10-02 & 51-20-04. 2L73 4F A3WE 20030909001512003090900151NE 2003 9 9 BAQA088895 220030828A74129550177760 EXCITER AGUSTAA109 A109E 0260119EU TMECA ARRIUSARRIUS2K1 NE ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037YL 739 11502 IGNITOR BOX FAILED OPERATIONAL CHECK. 1 CHANNEL FAILED TO FIRE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 URTH7EU E34NE 20030912000922003091200092NM 2003 9 12 AWXA200300860 120030712A5320654659221 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL BS 859, LBL 8. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL FROM BS 857 TO BS 860; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG 201-203, FIG 201. 2L72 4F RTA16WE 20030910001222003091000122CE 2003 9 10 DXTA200300069 120030720A3230 DOWNLOCK SWITCH CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RT MLG INOPERATIVE E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07933QS 7500133 RIGHT MAIN LANDING GEAR INDICATION REMAINED GREEN AFTER GEAR WAS RETRACTED, USED EMERGENCY BLOW DOWN GEAR. LANDING WAS UNEVENTFUL. DETERMINED THE RIGHT GEAR ACTUATOR DOWNLOCK SWITCH WAS FAULTY, REMOVED AND REPLACED WITH NEW SWITCH, PERFORMED GEAR OPERATIONAL CHECKS AND RESETTING BLOWDOWN SYSTEM, WORK DONE IAW 750 MAINTENANCE MANUAL CHAPTER 32-30-04. 2L72 4J4 FRTT00007WITE6CH 20031002000012003100200001SO 2003 10 2 2003F00589 120030914A3411 PROBE GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE PITOT STATIC WORN A UG8AO OTHER O OTHER CLCLIMB 1 GL23910DC 544 CREW REPORTED ON CLIMB THROUGH 29,000 FT, 'ALT' COMPARISON MONITOR ILLUMINATED. CREW FOUND THE NR 1 MADC IN ERROR. NR 3 SELECTED, AND CLIMB CONTINUED TO FL400. 'ALT' COMPARISON LIGHT ILLUMINATED AGAIN, & NONE OF MADC'S AGREED. ON DESCENT, ALL MADC'S AGAIN AGREED TO FL80. APPARENT CAUSE WAS ERRODED PITOT/STATIC PROBES. A/C WAS THOROUGHLY INSPECTED PHYSICALLY & ELECTRONICALLY PER GULFSTREAM V MM & ONLY DEFECT DISCOVERED WAS UPPER LT & RT PITOT/STATIC PROBES WERE ERRODED & CAUSING REPORTED ERRORS. PROBES (P/N 0856TK3 AND 0856TK4) WERE REPLACED PER THE GV MM & AAC GV CAMP DOCUMENT & ALL MADC SYSTEMS PERFORMED TO SPECIFICATIONS. A/C WAS RETURNED TOS ERVICE & RETURNED TO HOME BASE WITHOUT INCIDENT. (M) 2L72 4F4 FRTA12EA E00057EN 20031015000202003101500020EA 2003 10 15 ASOA03436 120030912A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP AT THE ATTACH POINT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000532003101500053EA 2003 10 15 ASOA03454 120030902A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE FORWARD LONG SEAT TRACKS AT LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD LONG SEAT TRACKS AT LBL 9 AND RBL 9 IAW WITH SRM 51-00. (M) 2L72 4F RTA21EA 20031022001312003102200131NM 2003 10 22 2003UALA00686 120030912A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN MALFUNCTIONED A UALAO OTHER O OTHER TXTAXI/GRND HDL 1 WP29213UA 30219 EMERGENCY EXIT LIGHTS ON AND OFF DURING TAXI. CHECKED AND CYCLED COCKPIT, DOOR 1, DOOR 4 SWITCHES. 2L72 4F4 FRTT0001SE E46NE 20031023000792003102300079NM 2003 10 23 P5CA0300953 120030922A272160130011 ACTUATOR BOEING747 7472U3B 1384846NM PWA JT9 JT9D* NE RUDDER DEFECTIVE A P5CAO OTHER J WARNING INDICATION CLCLIMB 1 WP23923FT 22769 RUDDER RATIO LIGHT CAME ON AFTER FLAPS UP. REPLACED LOWER RUDDER RATIO CHANGER ACTUATOR IAW MM 27-21-12 2L74 4F4 FRTA20WE E20EA 20031022000212003102200021EU 2003 10 22 AWXA200301071 120030909A5320D53112087204 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y254 FLOOR SUPPORT AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT CORRODED AREA OF FLANGE ON Y254 FLOOR SUPPORT AT FR 20; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 220-225 FIG 204. 2L72 4F RTA28NM 20031120000452003112000045 2003 11 20 SWIA200312493 420031005A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07221SW7952 7952 120290 CAPTAIN'S FLIGHT DIRECTOR COMMAND BARS ERRATIC IN ROLL DURING TURNS. BARS JERK +/- 3 DEGREES IN ROLL DURING TURNS. COMMAND BARS ARE STABLE IN STRAIGHT FLIGHT. REPLACED CAPT'S AUTOPILOT COMPUTER APC-65B. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20031120000642003112000064NM 2003 11 20 QXEA200301253 120030929A5344 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 6 SEAT TRACK TOP FLANGE IS GOUGED 4 INCHES FORWARD OF STATION X545.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-784. 2H72 4T RTA13NM 20040203003312004020300331EA 2004 2 3 MASA200300490 120031214A495038004883 APU CNDAIRCL600 CL6002B19 1900309EA AFT SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW0717337145012786 7337 ASH 6499 BFL-PHX, DURING APPROACH WHEN APU BLEEDS SWITCHED ON, SMOKE AND FUMES IN THE COCKPIT. CAPT DECLARED AN EMERGENCY. WHEN APU BLEEDS WERE SWITCHED OFF, SMOKE AND FUMES DISSIPATED. MX CHECKED APU AND BLEED SYSTEM. DEFERRED APU AND CONTINUES OPS 12/18/2003. MX REPLACED THE APU, OP CHECKS GOOD. 2L72 4F RTA21EA 20040212000962004021200096NM 2004 2 12 EIA2003166 120031205A5311 FRAME BOEING747 747212B 1384886NM PWA JT9 JT9D* NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 AIRCRAFT NOSE W/W TUNNEL RT SIDE BS 300 3 EA HOLES CRACKED IN THE FRAME SEGMENT ABOVE STR. 40, 41, AND 42 RT. REMOVED DAMAGE, NDT AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 53-10-04 FIG 94 DETAIL III AND ECRA 485-53-168-2 2L74 4F4 F A20WE E20EA 20040212001052004021200105NM 2004 2 12 F3LA200300175 120031211A5340 MOUNT BRACKET BOEING737 73736E 138443ANM GIRT BAR CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON GIRT BAR MOUNT AT STA. 344, LBL 60. REPLACED GIRT BAR MOUNT BRACKET SRM 51-36-01 AND 51-40-02. 2L72 4F RTA16WE 20031105000192003110500019SO 2003 11 5 C2XA03SH421 120031028A335020131A BATTERY EMB 145 EMB145 3260210SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 SHV-DURING C-CHECK THE NR 2 EMERGENCY LIGHT BATTERY WAS FOUND TO HAVE NO OUTPUT. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031106000502003110600050SO 2003 11 6 C2XA03IA103 120031022A28102810051103 VALVE EMB 145 EMB145XR 3260214SO NR 1 LEAKING A C2XAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW2711119 145677 PSP - PILOT REPORTED THAT THE LEFT WING WAS LOSING FUEL DURING CLIMB. THE AIRCRAFT RETURNED TO PSP AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 VENT VALVE. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20031106000522003110600052NM 2003 11 6 03FDEA01813 120031022A5744 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE FITTING (WING SIDE), ACTUATOR ATTACHMENT LUG INBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20031107000252003110700025NM 2003 11 7 HNAA0300065 120031105A533085330033 SKIN DHAV DHC8 DHC8102 2809003NM FUSELAGE DAMAGED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07930HA 126 MAJOR REPAIR; REPAIR FOR AFT LOWER FUSELAGE SKIN DAMAGE. 2H72 4T RTA13NM 20030915000772003091500077EU 2003 9 15 BAQA088916 120030902A28221176415103 PUMP BOLKMS117 BK117A3 5626015EU FUEL BOOST INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA033918883 7011 BOOST PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20040108001432004010800143EU 2004 1 8 KBM2003F00077 120031021A6320FDT4194 BAR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE M GEARBOX WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH5629 3141 MGB REAR BAR, FOUND EXCESSIVE PLAY. REMOVED AND REPLACED WITH NEW.(K) 1G71 3U3 U H9EU E19EU 20040112000772004011200077NM 2004 1 12 AWXA200301567 120031220A3397BMS13311122 WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28175AW 23634 DEN - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 12-14 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 14 LT, OPERATIONAL CHECK OF EEL SYSTEM WAS GOOD. 2L72 4F RTA16WE 20040113000562004011300056 2004 1 13 BAQA091161 420031119A3422206075606103 GYRO BOLKMS117 BK117A1 5626010EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03136AE4691 7234 OFF FLAG WILL NOT GO OFF. DG INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20040114000562004011400056NM 2004 1 14 DL73S030972 120031028A3260106122615 PROXIMITY SWITCH BOEING737 737232 1384475NM LT MLG FAILED A DALAO OTHER N FALSE WARNING CLCLIMB 1 SO27322DL 23094 ATB LANDING MAIN RED LIGHT ON WITH GEAR RETRACTED. FOUND LEFT MAIN GEAR UPLOCK PROX SWITCH BAD S-72. REMOVED SAME, INSTALLED NEW PROX SENSOR AND ADJUSTED. CHECK GOOD ON GEAR SWING. 2L72 4F RTA16WE 20031216000292003121600029NM 2003 12 16 SWAA032599 120031125A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 43, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031216000822003121600082NM 2003 12 16 SWAA032578 120031122A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 EEPLS INOP AT FWD AND MID CABIN AREAS. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20031218000702003121800070NM 2003 12 18 C1HA200395071 120031201A3350 BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 OVERHEAD EMERGENCY LIGHT INOP AT ROW 4. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 727 MM 33-50-22, ALL OPS NORMAL. 2L73 4F A3WE 20031222000302003122200030NM 2003 12 22 QXEA200301530 120031207A5413 STRINGER DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 LEFT HAND NACELLE - OUTBOARD LOWER STRINGER ON FINGERNAIL DECK CRACKED AT FORWARD END. REPAIRED IAW DHC-8-200 SRM 651-40-11. 2H72 4T RTA13NM 20031222000982003122200098NM 2003 12 22 USAA030230 120031111A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 FOUND INTERCOSTAL CORRODED 2 INCHES BY 15 INCHES, CABIN FLOOR INTERCOSTAL AT LBL 24.75, BS 324-345. DEFECTIVE PART REPLACED WITH IDENTICAL PAR IAW 757 AMM SRM 51-10-2. CORROSION LEVEL 2, TASK NR C53-221-02. (M) 2L72 4F RTA2NM 20031222001252003122200125WP 2003 12 22 AMTA200301414 120031121A3350 POWER SUPPLY LKHEED1011 10113853 5265020WP EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EMERGENCY EGRESS PATH LIGHT AT FORWARD GALLEY FLOOR INOPERATIVE. POWER SUPPLY STRIP DISCONNECTED BETWEEN STRIPS. RECONNECTED AND SECURED. OPS CHECK GOOD. (M) 2L73 4F A23WE 20031223000112003122300011EA 2003 12 23 03343691 120031209A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27691BR 7740 DURING INPSECTION THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOR INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031217000762003121700076WP 2003 12 17 DHL2003809006 120031122A5210 LATCH DOUG DC8 DC873F 302199FWP PAX DOOR OUT OF ADJUST A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01604AL 46047 FLIGHT DECK DOOR WILL NOT LATCH CLOSED PROPERLY AND JAMS IN CLOSED POSITION. ADJUSTED UPPER LATCH AND OPS CHECKED PER MSI M/M 52-10-0. ALL CHECKS GOOD. 2L74 4F RT4A25 20030926001582003092600158NM 2003 9 26 CALA0300503 120030829A5720 SUPPORT BOEING737 7373T0 1384582NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A .5000 INCH CRACK IN RT WING UPPER MOST I/B T/E PANEL SUPPORT. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040902001552004090200155WP 2004 9 2 MEX2003574 120031230A2797 WIRE HARNESS DOUG DC9 DC987 3022087WP RUDDER PROX SW DAMAGED A ASMFD RETURN TO BLOCK HP ELECT. POWER LOSS-50 PC NO WARNING INDICATION TXTAXI/GRND HDL 1 SW23205AM 49405 FLT 605 - DFW-MEX - AIRCRAFT RETURNED TO PLATFORM, DURING THE TAXI THE LIGHT OF 'RUDDER TRAVEL UNRESTRICTED' DID NOT COME ON. THE SYSTEM WAS REVISED AND THE WIRE BUNDLE OF THE PROXIMITY SENSOR D1-33 WAS FOUND WITH DAMAGES. THE WIRE BUNDLE WAS REPAIRED IAW MM 20-20, STANDARD PRACTICES, AND THE SYSTEM WAS TESTED IAW MM 27-33-00 AND 27-20-06, ALL CORRECT. (M) 2L72 4F RTA6WE 20050427000292005042700029EU 2005 4 27 KBM2005F00034 120031120A6310350A35109120 COUPLING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TRANSMISSION FATIGUED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19966SH862 3787 BELT SLIPPAGE OVERTEMP. POSSIBLE METAL FATIGUE. (K) 1G71 3U3 U H9EU E19EU 20060328002022006032800202SO 2006 3 28 MASA200300518 120031228A2731 TRIM SYSTEM EMB 145 EMB145LR 3260212SO MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07846MJ 145507 ASH NR 2811, IND PITCH TRIM MAIN AND BACK-UP MSGS WITH ACCOMPANYING PITCH TRIM INOP. CAPT DECLARED AN EMERGENCY AND RETURNED TO FIELD. MX RESET PITCH TRIM SYSTEM. SYSTEM OP CHECKS GOOD. PER DQA NTSB DID NOT REQUIRE MX TO PULL FDR AND CVR. RETURNED A/C TO SERVICE. NO PARTS USED. 2L72 4T RTT00011AT 20030814000032003081400003 2003 8 14 SWAA031715 420030801A25656557463 CLIP BOEING737 7372H4 138448CNM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACHMENT CLIPS LOOSE. SECURED ATTACHMENT CLIPS PER MM. 2L72 4F A16WE 20030819000902003081900090 2003 8 19 SWAA031742 420030803A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030819001742003081900174NM 2003 8 19 SWAA031737 120030804A33501000679 LIGHT BOEING737 7372H4 138448CNM AFT ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F A16WE 20030404001632003040400163NM 2003 4 4 SWAA030553 120030310A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW NR 2 & ROW 23. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030407000992003040700099NM 2003 4 7 TSAA0353011 120030130A53136546554 STRINGER BOEING737 7372M6C 1384708NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 TRIMMED OUT DAMAGE STRINGER SECTION. FABRICATED A .090 INCH THICK J AND U-CHANNEL FROM 7075-T6. ALODINED AND APPLIED TWO COATS PRIMER TO ALL BARE ALUMINUM. INSTALLED REPAIR PARTS USING FASTENERS IDENTIFIED IN FIGURE 2. SEALED FAYING SURFACE WITH BMS 5-95 SEALANT. APPLIED CORROSION INHIBITING COMPOUND TO REPAIR AREA. VERIFIED 8110-3 RECEIVED. REPAIR SPLICE COMPLETED IAW ECO 2599, FIGURE 2. (M) 2L72 4F RTA16WE 20030404001862003040400186NM 2003 4 4 SWAA030598 120030317A3350604222 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29713SW 27847 DURING SCHEDULED RON, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT & FWD CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030416002652003041600265NM 2003 4 16 CALA0300184 120030408A5330 SKIN BOEING777 777224 1385225NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0978008 29478 INSPECTION FOUND FUSELAGE SKIN DENTED AT FORWARD LT SIDE THREE FEET FORWARD OF L-2 DOOR AT BS 678, STRINGER 27L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 4. A DIP WAS INITIATED TO REINSPECT THE REPAIR AT 30,000 FLIGHT CYCLES WITH INTERVALS OF 16,000 FLIGHT CYCLES. 2L72 4F RTT00001SE 20030417000962003041700096EA 2003 4 17 SWIA200311757 120030130A301020035008067 CONTROL UNIT CNDAIRCL600 CL600* EA BLEED AIR MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07453SW 7743 ANTI-ICE DUCT WARNING OCCURRED ABOUT FL260. PERFORMED QRH PROCEDURE AND MESSAGE CONTINUED INTERMITTENTLY. RETURNED TO DFW. MESSAGE WENT OUT PRIOR TO LANDING. REMOVED AND REPLACED NR 15 SENSOR IAW MM 36-21-07. REMOVED AND REPLACED LEFT BLEED CONTROL UNIT IAW MM 30-12-19. OPS CHECK GOOD. P/N OFF/ON 20-035008-067, S/N OFF A2286, S/N ON A1754. 2L72 4F RTA21EA 20030423001322003042300132EU 2003 4 23 MALA030196 120030312A3260 PROXIMITY SENSOR BAC 146 AVRO146RJ85A1500097EU MLG UPLOCK FAILED A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15505XJ E2313 DURING GEAR SELECTED UP ON FLIGHT 3411, LT GEAR UNSAFE LIGHT AND INTRANSIT LIGHT WOULD NOT EXTINGUISH ON RETRACTION. AIR RETURN TO MEM. MAINTENANCE REPLACED LT MAIN GEAR DOOR UPLOCK ACTUATOR PROXIMITY SWITCH. OPS CHECK GOOD IAW AMM 32-60-17. PN ON/OFF 8-018-01, SN/OFF 6940, SN/ON A53404. 2H74 4F RTA49EU 20030425001132003042500113NM 2003 4 25 DLM11030228 120030308A5241520201842 SOLENOID DOUG MD11 MD11 3023602NM L2 DOOR INOPERATIVE A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27806DE 48477 L2 DOOR SMELLS LIKE ELECTRICAL BURNING AND WILL NOT OPERATE ELECTRICALLY. REPLACED LOCK/RELEASE SOLENOID PER M/M. OPS GOOD. NO MORE BURNING SMELL. 2L73 4F RTA22WE 20031222000472003122200047WP 2003 12 22 03334331 220031130A7200310349016 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTFE731TFE731* 01518WP RIGHT FAILED A VTZAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA27331UE 41099 P76112C DURING CRUISE EN ROUTE TO DAY CREW RECIEVED RT ENGINE OIL CONTAMINATION LIGHT. THE CREW WAS ACCOMPLISHING THE QRH WHEN THE ENGINE FLAMED OUT DIVERTED TO PIT. CREW DECLARED EMERGENCY AND FLIGHT LANDED UNEVENTFULLY. THE ENGINE WAS DECLARED INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PEFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T4 FRTA41NM E6WE 20040105000032004010500003NM 2004 1 5 DL764030993 120031109A2780114T642126 TARGET BOEING767 767432ER 1385134NM NR 9 SLAT FALSE INDICATIONA DALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO27830MH 29701 BETWEEN FLAPS 25 AND THIRTY WITH GEAR DOWN GOT LOW AIRSPEED EICAS AND L/E SLAT ASYM EICAS. RAN QRH PROCEDURE LANDED WITH FLAPS 25. PRONOUNCED PORPOISING IN THE FLARE DURING MANUAL LANDING. BIT PSEU. FAULTED 303 SENSOR I/B NR 9 L/E SLAT. REMOVED PANEL 62 TO ACCESS S303. FOUND BOLT AT 303 SENSOR TARGET BROKEN. REPLACED BOLT AND INSTALLED TARGET PER MM. CYCLED SLATS SEVERAL TIMES CKS NORMAL. NO MSGS ON PSEU. REINSTALLED PANEL 621JB. CHECKED OPERATION OF FLIGHT CONTROLS. FOUND ALL TO OPERATE NORMAL. 2L72 4F RTA1NM 20040106000072004010600007WP 2004 1 6 DHL2003802568 120031202A5754 DOOR DOUG DC8 DC873 302199CWP L/E SLOT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING OTBD SLOT UPPER DOOR CRACKED 3.000. REMOVED AND REPLACED UPPER DOOR ON RIGHT WING OTBD SLOT IAW MM 27-80-2 PG 201-203, SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR 1456. 2L74 4F RT4A25 20031010000502003101000050NM 2003 10 10 03FDEA01567 120030918A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON FLOORBEAM AT BS 1050, LBL 35, WL 208. **SD** COMING 2L73 4F RTA3WE 20031014000862003101400086NM 2003 10 14 SWAA032216 120031004A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 500C + 8, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040108000622004010800062SO 2004 1 8 HLF2003F00001 220031006A8520 CRANKCASE CESSNA421 421C 2076016CE CONT O520 GTSIO520* 17032SO ENGINE CRACKED B HLFRO OTHER O OTHER NRNOT REPORTED 1 SW17148MA 421C0078 292492R CRACKED CRANKCASE AT NR 7 STUD, BETWEEN CYLINDERS NR 1 AND NR 3. CRACK IS ON CRITICAL AREA AND EXCEEDS THE MAX ALLOWED IAW SBM 90-17. PROBABLE CAUSE: OVERTORQUED NUT OR DEFECTIVE CRANKCASE. REPORTED TO MFG. 1L72 3O3 O A7CE E7CE 20031202001622003120200162NM 2003 12 2 AALA20031152 120031007A2421GEMT513 IDG BOEING767 767323 1385205NM RIGHT MALFUNCTIONED A AALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TOTAKEOFF 1 SW21349AN 33088 RIGHT GENERATOR DRIVE, RIGHT GEN OFF, BOTH LIGHT ILLUMINATED. DISCONNECTED RIGHT IDG AS PER PROCEDURE. REMOVED AND REPLACED IDG PER M/M 24-11-01 EMP 509163. RT IDG OPS CHECKED GOOD EMP 108099. REMOVED MEL 10-129DC-C AND CLEARED MIS SHEET. (M) 2L72 4F RTA1NM 20040121000832004012100083EA 2004 1 21 ASOA03609 120031129A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING A GROUND INSPECTION IN MYR, THE PASSENGER DOOR BOTTOM STEP CONNECTION TO THE RETRACTION ROD WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121001112004012100111NM 2004 1 21 03FDEA02344 120031229A5750ARC76691 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING I/B FLAP O/B HINGE (WING SIDE) FAIRING SUPPORT BRACKET (TOP OF ACTUATOR) FOUND CRACKED. REMOVED & INSTALLED NEW BRACKET AS PER CMM 20-50-02. 2L73 4F RTA22WE 20031014002082003101400208EU 2003 10 14 BAQA086810 120031007A6330L633M2010105 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135QC39 0281 TRANSMISSION MOUNT SHOWING BAD INDICATION ON PLUNGER WHEN INSTALLED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031009000462003100900046SO 2003 10 9 SIMA200318102 120030628A335020131A BATTERY PACK EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21831AE 145616 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT BETWEEN SEAT 7A AND 11A WILL NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031010000202003101000020NM 2003 10 10 USAASB03145 120030822A2750679402 PRIORITY VALVE BOEING737 7373B7 1384580NM TE FLAPS FAILED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19519AU47147 23705 ON CLIMB-OUT FROM TPA, EN ROUTE TO PIT, CAPTAIN REPORTED VIA ACARS THE FLAPS WOULD NOT RETRACT FROM THE FLAPS ONE POSITION TO THE FLAP UP POSITION. FLAPS WOULD NOT RETRACT OR EXTEND. DUE TO WEATHER AT TPA AND THE FACT THE CAPTAIN WAS COMFORTABLE, IT WS DECIDED TO PROCEED NORTH TO CLT. FLIGHT DIVERTED TO CLT AND COMPLETED A FLAPS FIFTEEN LANDING WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP PRIORITY VALVE AND THE FLOW LIMITER VALVE, P/N 6114-6, PER MM 27-81-71. OPS CHECK AND LEAK CHECK GOOD. FLAPS AND SLATS CHECK GOOD. (M) 2L72 4F RTA16WE 20030917000762003091700076EU 2003 9 17 ALGA089089 120030910A6510C651A2001101 DISC PACK UROCOPEC120 EC120B 8680987EU T/R DRIVESHAFT CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL55 1263 FOUND ONE CRACKED LAMINATE ON TAIL ROTOR DISC PACK. REMOVED AND REPLACED. 1G72 3U NCR0001RD 20030919001352003091900135EU 2003 9 19 9075062703 120030615A21210500846 BLOWER MOTOR SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE A/C CONDENSOR INOPERATIVE E S4WAK NONE L NO TEST ININSP/MAINT 1 WP07350R 1395 9015 9667 AIR CONDITIONING CONDENSOR BLOWER MOTOR INOPERATIVE. 1G71 3U3 U H9EU E00054EN 20030915001112003091500111NM 2003 9 15 S03453045 120030625A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE CORRODED W SAJFO OTHER O OTHER NRNOT REPORTED 1 WP03 29219 FUSELAGE BELLY SKIN CORROSION BETWEEN BS 741 AND BS 760, S-47L, S-47R REPAIRED IAW EO 744-53-00-0007 2L74 4F4 FRTA20WE E24NE 20030922001062003092200106 2003 9 22 BAQA088834 420030827A221041800478034 ACTUATOR AEROSPAS365 AS365N2 8680815EU YAW STUCK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME309 6417 TAIL ROTOR KICK AND GALVA METER STICKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20040127002282004012700228WP 2004 1 27 ASAA0380685 120031015A534795301157 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND SEAT TRACK CORRODED AT FS 200-240. REMOVED DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-05. (M) 2L72 4F RTA6WE 20040127001982004012700198NM 2004 1 27 ASAA0310218 120030325A5320693741318 FITTING BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO PIT FLOOR FITTING AT BS 490, STRINGER 27R CORRODED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040130001232004013000123WP 2004 1 30 UPS04841704 120031231A53403754041501 FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, A-PIT DOOR STOP BACK-UP FITTING CRACKED AT STA 320 L27L. REMOVED AND REPLACED FITTING REF DC8 SRM 51-1-20D AND SRM 51-3-0. 2L74 4F RT4A25 20040203000332004020300033NM 2004 2 3 ASAA0310167 120030320A53476554969 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 697-616, LT BUTTOCK LINE 45, RT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040205000272004020500027NM 2004 2 5 EIA2003148 120031105A5330 SKIN BOEING747 747132 1384882NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FUSELAGE STATION 2742 WL310 RT SIDE EXISTING REPAIR CORRODED. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-30-02 PAGE 1-3. TRIMMED DAMAGE SKIN FROM STA 2731-2742 WL 305-315 IAW SRM 53-30-03 PAGE 2A-2R. FABRICATED NEW EXTERNAL DOUBLER AND FILLER IAW SRM53-30-03 PAGE 2A-2R. ALODINED PARTS IAW SRM 51-10-02 PAGE 6-7. PRIMED PARTS BSOPM 20-41-02 PAGE 7-9 AND INSTALLED REPAIR SRM 53-30-03 PAGE 2A-2R. 2L74 4F A20WE 20040206000022004020600002SW 2004 2 6 11290376 120031128A7603C810242 CONTROL CABLE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCB3T HCB3TN5 GL ZONE 400 CHAFED E D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW17228AM33082166 TC300 P54062 BVA7662 DURINE TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE POWER LEVER CABLE HAD BROKEN INSIDE THE CABLE HOUSING IN THE ENGINE COMPARTMENT. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20040212000492004021200049NE 2004 2 12 NAFA20030003 220031205A8500 ENGINE DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 2 OVERSPEED I N32BE ENGINE SHUTDOWN RK PARTIAL RPM/PWR LOSS FLUID LOSS CRCRUISE 1 AL017780B1867 1867 45372 P36927 NR 2 ENGINE RUNNING ROUGH AND LOOSING OIL. ENGINE/PROP OVERSPEED 3500 RPM. REPLACED NR 2 ENGINE. 2L74 4R4 R 6A3 5E8 20040213000152004021300015NM 2004 2 13 2003UALA00870 120031118A2120 ODOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE ROW 3 & 6 DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29838UA 1477 FLIGHT DIVERTED DUE TO ELECTRICAL ODOR IN CABIN BETWEEN ROWS 3 AND 6. VENT BLOWER AND EXTRACT FANS RUNNING NORMAL, CHECKED RECIRCULATION FANS, BOTH PACKS OPERATING NORMAL. CHECKED CABIN LIGHTING AND PASSENGER ENTERTAINMENT SYSTEM, NO DEFECTS FOUND. 2L72 4F4 FRTA28NM E40NE 20040308001392004030800139NM 2004 3 8 ASAA0310235 120030326A53116545817519 FRAME BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SUB FRAME AT BS 354, STRINGER 64L CORRODED. REMOVED AND REPLACED SUB FRAME PER SRM. (M) 2L72 4F RTA16WE 20031211000582003121100058NM 2003 12 11 C1HA200394039 120031108A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 344 - 480 LBL 45.5 HAS LIGHT CORROSION AND WORN AREAS. 2L73 4F A3WE 20040415001142004041500114NM 2004 4 15 ASAA024015J 120030318A532065C2730892 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON SIDEWALL SUPPORT AT BS 727G BL 23. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040525000502004052500050EU 2004 5 25 2004F00140 120030909A5311 FRAME AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON LEFT SIDE OF FRAME BETWEEN FRAME 24 AND 35 AT STRINGER 34L TO CENTER BUTT LINE. FABRICATED AND INSTALLED FLOOR SUPPORTS FRAME BETWEEN FRAME 24 TO FRAME 34 AT STRINGER 34L. (M) 2L72 4F RTA28NM 20040713001612004071300161WP 2004 7 13 MEX2003562 120031225A2913AS66411LS666 PUMP DOUG DC9 DC987 3022087WP HYD PRESS FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23751RA241636333 49779 FLT 136 - MEX-AGU - AIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINE STARTING HYDRAULIC PRESSURE DROPPED TO ZERO. HYDRAULIC PRESSURE PUMP WAS REPLACED IAW MM 29-10-05, ALL CORRECT. (M0 2L72 4F RTA6WE 20030924000712003092400071NM 2003 9 24 2003UALA00628 120030815A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 BS 616 RT FRAME TO STAB BEAM CRACKED BELOW FLOOR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030428001262003042800126WP 2003 4 28 ZW0A0303903 120030402A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13925TW 49357 THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 598, LONGERON 25R TO 26R. REPAIRED PER SRM 53-04, FIG 12C, AND AREA NUMBER 1 ON ARA 18438A. CHECK-C 8-15-02 STL. 2L72 4F A6WE 20030428001352003042800135NM 2003 4 28 DHL2003745010 120030405A3231 SWITCH BOEING727 727224 1384076NM MLG DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01745DH 20665 RIGHT MAIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. ABNORMAL PROCEDURE COMPLETED. LIGHT EXTINGUISHED. PLACED RT MAIN DOOR ANNUNCIATOR ON MEL 32-1. DMI 12479 AIRCRAFT OK FOR SERVICE. REF DMI 12479 RIGHT MAIN DOOR ANUNNCIATOR INOPERATIVE. FOUND RIGHT GEAR DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SAME IAW M/M 32-62-11. OPS NORMAL ON GROUND. THIS CLEARS DMI 12479. 2L73 4F A3WE 20030430001212003043000121NM 2003 4 30 03FDEA00203 120030301A3260 UPLOCK SWITCH BOEING727 727200 138407ENM ZONE 700 MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25265FE 21671 RED NOSE GEAR LIGHT ILLUMINATED INFLIGHT WITH GEAR HANDLE OFF. FOLLOWED RED TAB PROCEDURE WHICH DIRECTED RAISING GEAR HANDLE. LIGHT STAYED ON INDICATING AN UPLOCK OR GEAR SENSOR FAILURE. ALSO - NOSE GEAR "GREEN" LIGHT FLICKERED/DIM DURING THIS MALFUNCTION. TROUBLESHOT NLG WARNING LIGHT TO UP AND LOCK GEAR SWITCH PER FEDEX MM 32-64- 01,32-64-02. R/R NOSE GEAR UP AND LOCK SWITCH PER FED EX MM 32-61-071-4 AND FUNCT CHECKED GOOD PER FED EX MM 32-32-000-5 AND 32-61-71-4. REF N00025 DATE 03-01-03 RII Q/C206 2L73 4F RTA3WE 20030502001322003050200132NM 2003 5 2 DHL2003741526 120030324A5720 ANGLE BOEING727 727200 138407ENM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, RT WING, LWR I/B LEADING EDGE, INSIDE ACCESS PANEL CAVITY 6401 UPPER O/B, L/E WEB TO L/E SKIN ATTACH ANGLE HAS 2 INCH CRACK. REMOVED FASTENERS RT LOWER I/B, L/E INSIDE ACCESS PANEL UPPER O/B L/E WEB TO L/E SKIN ANGLE IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA, DIMENSIONS 17.5 X 2.5. FABRICATED ANGLE REPAIR, DIMENSIONS 17.5 X 2.5 AND SPLICE REPAIR DIMENSIONS, 9.5 X 2.5 INCH. MATERIAL USED 2024 T-3 .080 PO 123 IAW B-727 SRM 57-20-2 FIG 1. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-40-3 FIG 2 51-30-2. 2L73 4F RTA3WE 20030501000202003050100020WP 2003 5 1 AALA20030273 120030220A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 TUL - FOUND PIT IN FUSELAGE SKIN AFT OF FORWARD DOOR STATION 427 LONGERON 25R. CUT OUT DAMAGE (OUTER SKIN) INSTALLED FILLER AND DOUBLER PER SRM 53-05 FIG 82. (M) 2L72 4F RTA6WE 20030502002592003050200259NE 2003 5 2 2003UALA00281 220030316A72306A5994 RUB STRIP AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COMPRESSOR DEBONDED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29818UA 12047 882 V10057 DIVERTED DUE TO NR 1 ENGINE COMPRESSOR STALL. COMPRESSOR STALL CAUSED BY HIGH PRESSURE COMPRESSOR (HPC) 6TH STAGE (C6) BLADE DAMAGE WHICH WAS IN TURN CAUSED BY HPC C6 RUBSTRIP COATING DISBONDING. SERVICE BULLETIN 72-0369 IS IN PLACE TO UPGRADE COATING TO AVOID DISBOND. THIS SERVICE BULLETIN IS ACTIVELY ACCOMPLISHED AT ENGINE SHOP VISIT. 2L72 4F4 FRTA28NM E40NE 20030505002662003050500266EU 2003 5 5 03109330 120030419A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030506002432003050600243WP 2003 5 6 ASAA0380163 120030228A53203936668507N BRACKET DOUG DC9 DC982 3022082WP FLOOR SUPPORT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOORBEAM STIFFENER BRACKET IS CRACKED AT CUSP LINE AT FS 503. REPLACED STIFFENER, ANGLE, PER SRM 51-10-4 AND 30-5. (M) 2L72 4F A6WE 20030506000562003050600056WP 2003 5 6 UPS03840462 120030403A5230 LONGERON DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C3 R2 DOOR LONGERON 11R IS CRACK AT UPPER AFT DOOR JAMB CORNER. REMOVED LONGERON IAW DC8 SRM 51-1-21 & 51-1-20D. REMOVED & REINSTALLED GILLINER & INSULATION IAW DC8 SRM 51-3-0. REC'D LOCATED & DRILLED NEW LONGERON IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030506001932003050600193WP 2003 5 6 ASAA0380226 120030307A532199365993 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND MID CARGO FLOORBOARD PUNCTURED AND CORRODED AT FASTENER HOLES. REPLACED FLOOR PANEL PER SRM. (M) 2L72 4F A6WE 20030509000472003050900047WP 2003 5 9 GTIA030252 120030312A7830 STRUCTURE DOUG DC9 DC983 3022083WP THRUST REVERSER DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 NR 1 ENGINE THRUST REVERSER INNER CORE HAS HEAT DAMAGE AND IS COMING OUT OF ACCOUSTIC. REPAIRED DAMAGED CORE ON W/O 67 11-N-67. (M) 2L72 4F RTA6WE 20030509000612003050900061NM 2003 5 9 HOC2003F00004 120030420A5320652427650 TIE BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON TENSION TIE FITTING AND SPLICE ANGLE AT STA 1183, STR 17R. 2L72 4F4 FRTA16WE E2EA 20030513000302003051300030NM 2003 5 13 HNAA0300021 120030502A2900 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE MALFUNCTIONED A HNAAO OTHER J WARNING INDICATION LDLANDING 1 EA07906HA 9 AFTER LANDING WHEN NR 1 PROP WAS FEATHERED, CREW REPORTED LOSING NOSE WHEEL STEERING AND THE NORMAL BEAKES. CREW USED PARK BRAKE TO STOP AIRCRAFT. CREW OBSERVED MAIN AND STANDBY HYDRAULIC PRESSURE AT LESS THAN 1800 PSI FOLLOWED BY NR 1 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATING. AFTER 10 SECONDS ALL INDICATIONS RETURNED TO NORMAL. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. 2H72 4T RTA13NM 20030513002062003051300206NM 2003 5 13 QXEA0300482 120030410A5410 BRACE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 FORWARD STABILIZER BRACE ASSEMBLY IS GOUGED IN TWO LOCATIONS ON LEFT HAND NACELLE. REPAIRED IAW Q400 AMM 32-11-16-400-801, PAGE 411, PARAGRAPH 4A. 2H72 4T RTA13NM 20030513002132003051300213NM 2003 5 13 DXTA200300011 120030415A2613610002 WARNING LIGHT AMD FALC50FALCON2000 2730170NM LT MLG WW INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL07236QS 136 LEFT HAND WHEELWELL OVERHEAT WARNING LIGHT CAME ON DURING DESCENT. 2K73 4F RTA50NM 20030514000842003051400084NM 2003 5 14 SWAA030985 120030502A532065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT STR 10R, BS 597 & BS 578. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030604000802003060400080NM 2003 6 4 UPS03440494 120030410A5314 SUPPORT BRACKET BOEING747 747121 1384871NM KEEL BEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 KEEL BEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1203 LBL 9. SUPPORT BRACKET REPLACED AS PER SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCHES . EXCEED SRM LIMIT. 2L74 4F A20WE 20030604001302003060400130NM 2003 6 4 UPS03440550 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2080, BET S25-26L FRAME WEB FOUND CRACK. M/DECK BS 2080 BETWEEN STR 25L - 26L FRAME REPAIRED AS PER SRM 53-10-04 FIG 39. 2L74 4F A20WE 20030514001122003051400112NM 2003 5 14 SWAA031023 120030507A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND 1.75 INCH LONG FUSELAGE SKIN CRACK, BETWEEN BS 768 & BS 778, STRINGER 20R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030609001552003060900155SO 2003 6 9 C2XA03SH159 120030525A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV- DURING C-CHECK THE CENTER FLOORBEAM BETWEEN FRAMES 16 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030521001072003052100107WP 2003 5 21 DHL2003804878 120030130A57535655433401 COVER DOUG DC8 DC873F 302199FWP TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING JOINT FLAP COVER LOWER SKIN DELAMINATED. REMOVED AND REPLACED LT JOINT FLAP COVER IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030520000362003052000036NE 2003 5 20 SIMA200309002 220030326A73216071T20P16 CONTROL UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE INOPERATIVE A SIMAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SW21903AE 340B282 DURING DESCENT AT 9000 MSL RT ENGINE HAD MINOR TORQUE ROLLBACK WITH NO IGNITION LIGHT. 1 MINUTE LATER RIGHT TORQU WENT OT 118 PERCENT AND RIGHT ITT WENT TO 1000C WITH OVERTEMP LIGHT ILLUMINATED A STRON VIBRATION WAS FELT ON RIGHT SIDE OF AIRCRAFT. RIGHT ENGINE WAS SHUTDOWN. MAINTENANCE DOWNLOADED DFDR AND CONFIRMED NO OPERATIONAL LIMITS WERE EXCEEDED. THE DECU (DIGITAL ELECTRONIC CONTROL UNIT) WAS REMOVED AND REPLACED IAW SAAB MM. OPERATIONAL CHECK WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20030611000712003061100071NE 2003 6 11 HEEA086556 120030522A28206531703006110 VALVE SKRSKYS76 S76A 8143006NE FUEL SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 ENGINE FAILS TO START AFTER SITTING IDLE FOR A WHILE. REPLACED WITH SERVICEABLE VALVE. 1G72 3U H1NE 20030613000132003061300013EU 2003 6 13 MALA030286 120030529A7600 RELAY SAAB SF340 340B 7860101EU ENG CONTROLS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15445XJ 340B445 DURING FLIGHT 2938, F1 STOP OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION MCX NOTIFIED UPON LANDING F1 STOP LIGHT ILLUMINATED NORMALLY AND F1 STOP FUNCTION APPEARS TO OPERATE NORMALLY. TRIGGER REQUIRED TO PULL POWER LEVERS BELOW F1. AIR RETURN TO MEM DUE TO FLIGHT IDLE STOPS LIGHT ON. MAINTENANCE REMOVED AND REPLACED RELAY 80KA AND 20GA, PERFORMED OPS CHECK OF F1 STOP FUNCTION AND INDICATION IAW MAL TASK CARD 761501, ALL SYSTEMS CHECKS NORMAL AT THIS TIME. 2L72 4T RTA52EU 20030612000052003061200005EA 2003 6 12 SWIA200312013 120030526A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA LT SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07445SW 7651 FLT SPOILER AND O/B GROUND SPOILER STATUS MESSAGES ILLUMINATED. REMOVED AND REPLACED LEFT SECU. MESSAGES NO LONGER DISPLAYED. OPS CHECK GOOD AT THIS TIME. S/N OFF 01600. 2L72 4F RTA21EA 20030612001412003061200141WP 2003 6 12 UPS03840730 120030503A5340 ANGLE DOUG DC8 DC873F 302199FWP KEELBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, CRACK IN ANGLE ATTACHING TO KEELBEAM AT STA 902 BETWEEN MLG DOORS. REMOVED AND REPLACED FITTING (P/N 4775262-501) IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20030613000912003061300091EA 2003 6 13 COMA0360258 120030603A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONAL STAB MALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO01965CA149142129 7131 FLIGHT 5843 STAB TRIM, MACH TRIM AND AUTO PILOT NOSE DOWN CAUTION MESSAGE. REPLACED THE HSTA. 2L72 4F RTA21EA 20030623000372003062300037WP 2003 6 23 GTIA030344 120030507A5540 BRACKET DOUG DC9 DC982 3022082WP RUDDER CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 VERTICAL STAB RUDDER HINGE UPPER 'V' BRACKET ASSEMBLY HAS CORROSION STATION ZR 133. REMOVED VERTICAL STABILIZER RUDDER HINGE UPPER 'V' BRACKET. INSTALLED BRACKET ASSEMBLY. (M) 2L72 4F A6WE 20030619000792003061900079SW 2003 6 19 HEEA087414 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030707001582003070700158NM 2003 7 7 AWXA200300721 120030620A2913 PUMP BOEING737 737277 1384570NM HYDRAULIC SYS FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28184AW 22651 ON DEPARTURE, LOST A-SYSTEM HYDRAULIC PRESSURE, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. AIRCRAFT TOWED BACK TO GATE. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED, REMOVED AND REPLACED PUMP. A-SYSTEM HYDRAULICS FLUSHED, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN OF ENGINE DRIVEN HYDRAULIC PUMP S/N 183862 CONFIRMED FAILURE OF UNIT. THRUST BEARING FAILED ON INTERNAL DRIVE SHAFT CAUSING DAMAGE TO THE CYLINDER BLOCK BEARING. PISTON SHOES WERE ALSO FOUND WORN BEYOND LIMITS. REPLACED O-RINGS, BACK-UP SEALS, BEARINGS, PISTON SHOE ASSEMBLIES, STROKING PISTON, INTERNAL & EXTERNAL DRIVE SHAFT, THRUST BEARING RETAINER, ROTATING GROUP ASSEMBLY, AND CYLINDER BLOCK. UNIT WAS BENCH TESTED IAW CMM 2L72 4F RTA16WE 20030708001012003070800101EU 2003 7 8 AWXA200300703 120030610A5320D532302270100 ANGLE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK A 2 INCH CRACK WAS FOUND ON ANGLE AFT R 34, STR 31 RT. MAINTENANCE REMOVED CRACKED ANGLE AT FR 34, STR 31 RT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-44-11, PG. 11,16, AND 20. 2L72 4F RTA28NM 20030709000462003070900046WP 2003 7 9 GTIA030442 120030521A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLOOR PANEL OUTBOARD G-2 STIFFENERS CHAFING AND DEBONDED. REPAIRED FLOOR PANEL. (M) 2L72 4F A6WE 20030710001492003071000149NM 2003 7 10 DHL2003783011 120030617A251001801631 SEAT BELT BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01766AT 21999 UNABLE TO UNLOCK SECOND OFFICERS SHOULDER HARNESS FROM RETRACTED POSITION. REMOVED AND REPLACED S/O SHOULDER HARNESS BELT REEL IAW M/M 25-10-0. OPS CHECKED GOOD. 2L73 4F A3WE 20030108000122003010800012WP 2003 1 8 MWEA030005 120030107A53305910228214 SKIN DOUG DC9 DC981 3022081WP STA 1485 GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 DEEP GOUGE ON INNER SKIN JUST AFT OF FRAME STATION 1485, RIGHT SIDE BELOW SMALL CATWALK STEP SUPPORT PANEL. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20030108000362003010800036EA 2003 1 8 COMA0360004 120030103A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS DEDESCENT 1 SO01446CA 7546 FLIGHT 5114 FLAPS FAIL CAUTION MESSAGE.COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20030114002582003011400258EA 2003 1 14 COMA0360026 120030113A5240 ACCESS DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING EW VIBRATION/BUFFET INADEQUATE Q C CLCLIMB 1 SO01962CA 7123 FLIGHT 9485 LOUD HOWLING NOISE FROM FRONT OF AIRCRAFT.GROUND POWER CONTROL PANEL OPENED DURING FLIGHT - CLOSED DOOR - NO DAMAGE NOTED. 2L72 4F RTA21EA 20030115001082003011500108NM 2003 1 15 03FDEA00008 120030108A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION UNDER EDGE OF RIGHT RAM AIR DOOR ACTUATOR PANEL. CORROSION OUT OF LIMITS, REPAIRED IAW EA 7-5330-68147. 2L73 4F4 FRTA3WE E2EA 20030203002392003020300239NM 2003 2 3 QXEA0300216 120030131A243051608003 GCU DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAK NONE O OTHER UKUNKNOWN 1 NM09364PH2359 524 PDX-ON FLIGHT NUMBER 2059,#1 DC GENERATOR CAUTION AS WELL AS #1 AC GENERATOR LIGHTS ILLUMINATED. UNABLE TO SET PER CHECKLIST. REMOVED AND REPLACED #1 AC GENERATOR CONTROL UNIT AND #1 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030204002142003020400214NM 2003 2 4 SWAA030160 120030122A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND 7 EA STRINGER CLIPS CRACKED, BS 559, STR 10RL, BS 597, STR 7R, BS 907, STR 7R, BS 706, STR 7R, BS 616, STR 5L, BS 727D, STR 1, AND BS 400, STR 4L. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20030206001342003020600134EA 2003 2 6 COMA0360073 120030131A324017300110 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA R/H MLG DEFECTIVE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01918CA 7018 FLIGHT 5767 INBD ANTI SKID INOP CAUTION MESSAGE.REPLACED ANTI-SKID WIRE HARNESS. 2L72 4F RTA21EA 20030212000192003021200019SO 2003 2 12 AUS20030006 120030105A49306515259004 LINE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE APU FUEL LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 1995 P189 (AUS) APU FUEL LINE LOCATED BETWEEN THE FCU AND FUEL SHUTOFF VALVE FITTED BACK TO FRONT AND LEAKING FROM UNIONS. PIPE WAS ALSO FOULING ON THE APU CASING. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20030212000882003021200088NM 2003 2 12 CALA0300039 120030211A5311 FRAME BOEING737 7373Q8 1384670NM STA 1121 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914384 26313 INSPECTION FOUND INNER FORMED FRAME CHORD DENTED AT STA 1121, RBL 28, WL 292. REPAIRED IAW SRM 51-70-11, FIGURE 1. 2L72 4F RTA16WE 20030625000732003062500073NM 2003 6 25 F3LA200300047 120030129A5320 PANEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON LT SUPPORT ZEE IN AFT CARGO COMPARTMENT. FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. REMOVED Z-TRANSITION PANEL FROM STA 727 TO 9L47, LBL 21. FABRICATED AND INSTALLED REPLACEMENT PANEL PER SRM 53-60-53, FIG 204, SOPM 20-41-02, SRM 53-60-53 AND SRM 51-40-02. 2L72 4F RTA16WE 20030219000592003021900059NM 2003 2 19 RYN2003F00002 120030103A5320AE727104211 SPLICE BOEING727 727222 1384073NM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077638U 19911 AT B CHECK, CRACK FOUND AT FUSELAGE INTERIOR FLOOR SPLICE PLATE TO LOWER SILL BEAM, BS 640. 2L73 4F4 F A3WE E2EA 20030219000712003021900071NM 2003 2 19 SWAA030250 120030202A335020131A BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030220000422003022000042WP 2003 2 20 ABXA030043 120030113A532099578453 INTERCOSTAL DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23977AX 47513 LEVEL I CORROSION BETWEEN FS 218 - 200 AT FLOOR SUPPORT INTERCOSTAL, JUST INBOARD FROM 29 RT LONGERON. REPLACED INTERCOSTAL IAW DC-9 SRM. 2L72 4F A6WE 20030221000182003022100018NM 2003 2 21 AWXA200300065 120030105A5754 STRUCTURE BOEING737 737300 1384610NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C-14 CHECK THE NR 5 SLAT OUTBOARD WEDGE WAS FOUND DELAMINATED. MAINTENANCE REPAIRED DAMAGE TO HONEYCOMB OF NR 5 SLAT OUTBOARD WEDGE IAW B737-300 SRM 51-70-10, REP. 22, FIG. 31, PG. 88F-88H. 2L72 4F RTA16WE 20030221000702003022100070NM 2003 2 21 QXEA0300291 120030209A321083210001071 TIRE DHAV DHC8 DHC8202 2809007NM ZONE 700 BLOWN A QXEAO OTHER O OTHER LDLANDING 1 NM09369PH29 29 513 SEA - FLIGHT 2067 - UPON LANDING THE NUMBER 3 AND 4 TIRES BLEW. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH WHEEL ASSEMBLIES, BOTH BRAKES ASSEMBLIES AND RELATED HOSES. THE RIGHT HAND WHEEL SPEED GENERATOR AND CONDUIT WERE ALSO REPLACED. OPERATIONAL AND LEAK CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030228000102003022800010NM 2003 2 28 SWAA030432 120030226A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030305000442003030500044 2003 3 5 HEEA084626 420030214A3434066104400 RECEIVER BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 RECEIVER FAILED OUTER MARKER LIGHT INOPERATIVE. CLEANED EXCESSIVE CORROSION. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000352003030600035SW 2003 3 6 HEEA084748 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 STEP WILL NOT EXTEND. REPAIRED ACTUATOR. 1G72 4U H4SW 20030306001032003030600103SW 2003 3 6 HEEA084810 120030221A2510412070820101 SEATBACK CUSHION BELL 412 412 1182202SW CREW SEAT WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 SEAT BACK HAS A WEAK CUSHION. REPAIRED. 1G72 4U H4SW 20030310000302003031000030SW 2003 3 10 HEEA084939 120030227A7120212061108003 BEARING BELL 412 412 1182202SW BIPOD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 BIPOD BEARINGS WORN. REPAIRED. 1G72 4U H4SW 20030313001032003031300103CE 2003 3 13 BJG2003F00000 120030113A531012114224 DOUBLER CESSNA210 210F 2073418CE CONT O520 IO520* 17032SO FUSELAGE CRACKED A BJGAO OTHER O OTHER NRNOT REPORTED 1 EA236450N 21058801 FOUND DURING ANNUAL INSPECTION. THIS DOUBLER IS AFT OF MAIN GEAR LEG AS STA68.33. PART OF LANDING GEAR SUPPORT STRUCTURE. 1H71 3O3 O 3A21 E5CE 20030313001662003031300166NM 2003 3 13 AALA20030121 120030129A2130 SWITCH BOEING767 767223 1385123NM A/C BAY DEFECTIVE A AALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW21335AA 22333 DEN - FLT 1835 - EN ROUTE ORD-SFO, DURING CRUISE AT 35,000 FEET, RIGHT PACK INOPERATIVE LIGHT ILLUMINATED AND THE PACK QUIT OPERATING. AS THE LEFT PACK WAS PLACARDED INOPERATIVE, CREW DECLARE AN EMERGENCY AND DESCENDED TO 10,000 FEET. PASSING 12,000 FEET CREW SUCCESSFULLY RESET THE RIGHT PACK, BUT IT FAILED ONLY A FEW MINUTES LATER. CABIN ALTITUDE NEVER WENT ABOVE 9,000 FEET. ANOTHER RESET ON THE RIGHT PACK WAS ATTEMPTED AT 10,000 FEET. THE PACK DID RESET, BUT FAILED AGAIN SEVERAL MINUTES LATER. LANDED DEN WITHOUT FURTHER INCIDENT. REPLACED COMPRESSOR OVERHEAT SWITCH, AND FLOW CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030121000072003012100007NM 2003 1 21 SWAA030084 120030114A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT/RT ELEVS WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29748SW 29800 DURING SCHEDULED C4 CHECK, BOTH LT/RT ELEVATOR TABS FAILED FREEPLAY CHECKS. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB NR 1 HINGE BUSHINGS PER MM. 2L72 4F RTA16WE 20030121001272003012100127 2003 1 21 GLBA2003001 420030109A3418 COMPUTER BEECH 1900 1900D 1154162CE STALL WARNING MALFUNCTIONED A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03240GL UE240 STALL WARNING HORN WENT OFF AT 60 KTS ON T/O ROLL. CALIBRATED STALL WARNING COMPUTER, TEST FLIGHT SATISFACTORY. 2L72 4T RTA24CE 20030121001312003012100131GL 2003 1 21 HEEA083303 220030109A753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 BLEED VALVE PRODUCING HIGH TOT. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 U H2SW E1GL 20030314002172003031400217EA 2003 3 14 03048674 120030217A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT EMER LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27674BR 7601 RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. DEFFERED MX AWAITING FURTHER INFORMATION. 2L72 4F4 FRTA21EA E15NE 20030317000862003031700086NM 2003 3 17 03FDEA00247 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 6R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030319000412003031900041WP 2003 3 19 GTIA030066 120030206A5321 FLOORBOARD DOUG DC9 DC981 3022081WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOORBOARD R1 ENTRY DETERIORATED. FABRICATED NEW R1 ENTRY FLOORBOARD. (M) 2L72 4F A6WE 20030320000122003032000012NM 2003 3 20 USAABB03009 120030112A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 9 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030320001352003032000135NM 2003 3 20 2003UALA00126 120030131A5313 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 SHEAR WEB CRACKED AT STRINGER 17L BETWEEN STATION 188 AND 196.5. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20030320001492003032000149NM 2003 3 20 2003UALA00143 120030205A5313 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29567UA 26673 MID CABIN BS 612 CREASE BEAM LEFT SIDE, TOOLING DAMAGE ON BOTTOM OF HORIZONTAL FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED 2 EACH UPPER AND LOWER REPAIR ANGLES. 2L72 4F4 FRTA2NM E17NE 20030122002652003012200265NM 2003 1 22 UPS03440040 120030107A5310 CLIP BOEING747 747259B 1384804NM BS 2200 STG 25R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C M/D - BS 2200 STRINGER S25R TIE CLIP FOUND CRACK. BS 2200 STRINGER 25R TIE CLIP REPLACED AS PER SRM 51-10-01 P.8. 2L74 4F RTA20WE 20030327000402003032700040NM 2003 3 27 AWXA200300312 120030228A5320146N524027 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON SUPPORT ANGLE ON UNDER SIDE OF SHEAR DECK AT BS 1715, RBL 35-40. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT BS 1715, RBL 35-40; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 146N5240-27. 2L72 4F RTA2NM 20030731000422003073100042NM 2003 7 31 QXEA200300862 120030719A243611521084 GCU BOMBDRDHC8 DHC8401 1390041NM NR 1 FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09412QX1158 1158 4059 SEA- ON FLIGHT 2315 NR 1 DC GENERATOR CAUTION IN FLIGHT. GENERATOR RESET PER CHECKLIST WITH NO FURTHER PROBLEMS. REMOVED AND REPLACED NR 1 DC GCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000482003073100048NM 2003 7 31 QXEA200300880 120030721A2611302133 CONNECTOR DHAV DHC8 DHC8202 2809007NM SMOKE DETECTOR DISCONNECTED A QXEAO OTHER L NO TEST UKUNKNOWN 1 NM09358PH 506 PSC-ON FLIGHT NUMBER 2105, NR 1 TEST BAGGAGE SMOKE WARNING WILL NOT TEST. FOUND CANNON PLUG DISCONNECTED. RECONNECTED CANNON PLUG. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731000842003073100084EA 2003 7 31 QXEA200300813 120030706A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA RT WING POPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX - RIGHT HAND WING UPPER TRAILING EDGE BOTTOM SIDE HAS TWO POPPED RIVET HEADS AT APPROXIMATELY WS199. REPAIRED IAW CRJ 700 SRM 51-25-01. AND SRM 51-42-06. 2L72 4F RTA21EA 20030303000722003030300072NE 2003 3 3 HEEA084514 220030214A732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 TROUBLESHOOTING. FOUND GOVERNOR BREAK LOW AND UNIT HANGING. SPLIT UNIT AND INSPECTED INTERIOR AND FOUND FLYWEIGHTS STICKING SLIGHTLY. CLEANED FLYWEIGHT PINS AND RETESTED. UNIT TESTED OK. 1G72 4U4 U H4SW E22EA 20030303001182003030300118SW 2003 3 3 HEEA084536 120030214A2841393008047 INDICATOR BELL 412 412 1182202SW FUEL QTY ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 FUEL QTY INDICATION ERRATIC; WILL NOT RETURN TO SAME POSITION ON TEST. 1G72 4U H4SW 20030326000442003032600044NM 2003 3 26 AUS20030195 120030105A282260989761 PUMP BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL BOOST FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 3 MAIN FUEL TANK FORWARD BOOST PUMP FAILED RESISTANCE CHECK.FOUND DURING COMPLIANCE WITH AD/B747/173. 2L74 4F4 FRTA20WE E30NE 20030327001242003032700124SO 2003 3 27 C2XA03CL058 120030228A335066367 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717521 145378 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP AT ROW 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AISLE PATH EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030418000772003041800077NM 2003 4 18 QXEA0300287 120030213A5410 SUPPORT DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - NR 2 ENGINE OUTBOARD SUPPORT STRUT IS CHAFED ON INBOARD SIDE AFT OF FORWARD END. REPAIRED IAW HORIZON AIR EA 2-54-166. 2H72 4T RTA13NM 20030421000392003042100039NM 2003 4 21 UPS03440242 120030129A5330 SKIN BOEING747 747200 1384847NM FUSELAGE BULGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C M/D, BS 2360 BULKHEAD SKIN TO Y-RING FOUND BULGED UP AT STR 51L. BULKHEAD SKIN REPAIRED AS PER RS NR R53-83-34972 AND FX SKIN REPAIRED AT BS 2360 - 2370 BETWEEN S46L TO S46R AS PER SRM 53-10-04 FIG 5 DETAIL V, REF EO B747-5310-18355-A. TRIMMED AREA 1.5 X 10 INCH AT STR 50L AREA. 2L74 4F RTA20WE 20030418000532003041800053WP 2003 4 18 UPS03840191 120030210A574037048412 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD SIDE AT XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D. 2L74 4F RT4A25 20030421001082003042100108NE 2003 4 21 DL76L030197 220030225A7230PW40603 BLADE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE DENTED A DALAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SO27196DN25123 28453 727707 DURING T/O AT 110 KNTS BIRD INGESTION INTO NR 2 ENGINE WITH ENGINE SURGE DETECTED. ENGINE INDICATIONS NORMAL. REPORTED BY CREW 1 HR INTO FLT, NR 1 ENG GEN FAILED. A/C DIVERTED TO LGW. FOUND BIRD DEBRIS IN ENG 1, FAN BLADE DAMAGED OUT OF LIMITS. BOROSCOPE INSPECTION COMPLETED WITH NO FAULTS. FOUND DAMAGE TO FAN EXIT VANE. FAN BLADE TO BE REPLACED/ERA ISSUED FOR REPAIR TO VANE. IDG REPLACED. BIRD STRIKE INSPECTION COMPLETED. 2L72 4F4 FRTA1NM E24NE 20030723000912003072300091NM 2003 7 23 AWXA200300638 120030514A53156546540547 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS ON FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50. MAINTENANCE REMOVED DAMAGED FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50; FABRICATED A NEW REPLACEMENT ANGLE AND STRAP; INSTALLED REPAIR PARTS IAW SB 737-53-1061, AND ER 15-5300-03142-TB1. 2L72 4F RTA16WE 20030828001292003082800129 2003 8 28 MWEA030305 420030807A23125224088203 TRANSCEIVER DOUG DC9 DC932 3022066WP COCKPIT INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31501ME 47132 UNABLE TO TRANSMIT ON NUMBER ONE COMMUNICATION. REMOVED AND REPLACED NUMBER ONE COMMUNICATION TRANCEIVER. 2L72 4F A6WE 20030828001742003082800174NM 2003 8 28 SWAA031869 120030818A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND BOTH LEFTH AND RIGHT STUB FRAMES CRACKED AT BS 188, WL 207. REMOVED AND REPLACED STUB FRAMES PER SRM. 2L72 4F RTA16WE 20030728000122003072800012NM 2003 7 28 SWAA031631 120030720A531069353656 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED (2 EA) AT BS 360 BETWEEN STR 14R AND STR 15R, BS 400 BETWEEN STR 13L AND STR 14L. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20030728000962003072800096NM 2003 7 28 SWAA031617 120030718A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030729000032003072900003EA 2003 7 29 03202653 120030721A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27653BR 7438 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED AN INVERTER AND POWER SUPPLY CABLE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20030801001262003080100126 2003 8 1 MWEA030274 420030710A34574058001 WARNING SYSTEM DOUG DC9 DC981 3022081WP COCKPIT FALSE INDICATIONA MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31803ME 48029 THE DEAD RECKONING LIGHT CAME ON BOTH MULTIFUCTIONAL CONTROL DISPLAY UNIT. PERFORMED ADJUSTMENT TEST CHECKED OK PERFORMED RETURN TO SERVICE BITE TEST, CHECKED OK. 2L72 4F A6WE 20030903001152003090300115NM 2003 9 3 KPVA200332 120030725A33506104781 BATTERY DHAV DHC8 DHC8103 1386005NM CABIN DISCHARGED A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13808WP 026 HNL - LEFT AFT EGRESS AND OVERHEAD EMERGENCY LGIHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT. BATTERY AT 3351 P&3, LEFT PSU PANEL ROW NR 3, IAW DHC-8 MM CHM CHAP 33-50-67 STEP 8 PAGE 504. OPS CHECK GOOD IAW DHC-8 MM CHAP 33051-00 PAGE 201-202. (M) 2H72 4T RTA13NM 20030904001182003090400118EA 2003 9 4 COMA0360326 120030716A2760 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE COCKPIT ACTIVATED A COMAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO01496CA 7791 FLIGHT 5845 TAKEOFF ABORTED DUE TO YAWING TO RIGHT AND CONFIG SPOILER MESSAGE. COULD NOT DUPLICATE. NO FAULT CODES IN SECU, FUNCTIONAL CHECK WAS NORMAL. HIGH SPEED TAXI, NO YAWING OR FAULTS. 2L72 4F4 FRTA21EA E15NE 20030904001452003090400145WP 2003 9 4 DHL2003873603 120030709A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 AFT LOWER CARGO COMPT L-27R CORRODED AT STA 1290.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 11. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-2 FIG 11. FABRICATED FILLER AND DOUBLER ANGLE IAW SRM 53-2-2 FIG 11. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 53-2-2 FIG 11, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030812000842003081200084EU 2003 8 12 HEEA088645 120030727A772156375600010 INDICATOR AEROSPAS355 AS355* EU COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH 3248 LT MOUNTING NUTS INSIDE INDICATOR SPIN WITH SCREWS. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030826001592003082600159 2003 8 26 WX030011 420030727A2565 COVER DOUG DC9 DC983 3022083WP SERVICE DOOR OUT OF POSITION A WXOAK NONE O OTHER TXTAXI/GRND HDL 1 WP17860GA 49786 DURING A TURN IN LAS, CREW REPORTED THAT THE FORWARD SERVICE DOOR SLIDE PACK COVER CAME OFF. CONTRACT MAINTENANCE WAS CALLED OUT. THE SLIDE PACK COVER WAS RE-SECURED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20030825000742003082500074NM 2003 8 25 0301456309 120030802A3320 LIGHT BOEING747 747451 1384940NM CABIN SMOKE A NWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL01669US 24224 DURING FLIGHT, THE SMELL OF SMOKE WAS NOTICED FROM THE FOUR AREA LIGHTS OVER THE 2R JUMPSEAT. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. RELAMPED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030910002022003091000202EU 2003 9 10 MALA030367 120030802A243423080031 GENERATOR SAAB SF340 340B 7860101EU LT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15421XJ 340B421 DURING FLIGHT NR 2984, LEFT DC GEN ILLUMINATED WOULD NOT RESET. QRH COMPLETED ALL ENGINE INDICATIONS NORMAL. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED LT DC GEN PN 23080-031 SN/ON 97379 SN/OFF 3974 OPS CHECKS GOOD. IAW JC 243103. 2L72 4T RTA52EU 20030916001272003091600127WP 2003 9 16 AALA20030683 120030623A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21490AA 49683 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAIL COMPARTMENT VERY DIM. CLEANED EMERGENCY EXIT LIGHT BATTTERIES FOR TAIL COMPARTMENT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030929001132003092900113NM 2003 9 29 QXEA200301061 120030904A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09365PH 526 FLOOR PROXIMITY EMERGENCY LIGHTING IS NOT WORKING PROPERLY. REMOVED AND REPLACED FLOOR TRACK LIGHTS AT ROW 5-7. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930000232003093000023NM 2003 9 30 03FDEA01467 120030909A2613 SWITCH BOEING727 727200 138407ENM ZONE 400 FALSE INDICATIONA FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 SO25463FE 22551 ENGINE NR 3 OVERHEAT LIGHT ILLUMINATED ON CLIMB OUT REFRENCED JRH AND CLOSED THE RIGHT WING ANTI-ICE SWITCH. LIGHT WENT OUT AND STAYED OUT FOR REMAINDER OF FLIGHT. CHECKED DUCTS AND CLAMPS ON NR 3 ENGINE OPS CHECK SYSTEM USING APU POWER IAW SMP. COULD NOT DUPLICATE PROBLEM. 2L73 4F RTA3WE 20030910000182003091000018WP 2003 9 10 DHL2003604549 120030523A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBD FLAP UPPER PLATING SHOWS INTERIM REPAIR, XW 104.000 - XW 122.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED UPPER PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED NEW UPPER PLATING IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. CLEANED, TREATED AND PRIMED AREA AND UPPER PLATING INNER PART IAW SRM 51-1-8B. INSTALLED NEW UPPER PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031006000672003100600067CE 2003 10 6 AMWA41 120030907A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127ZV UE127 RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-37 LT SIDE (1EA CRACK ON THIS RIB) 2L72 4T RTA24CE 20031002001702003100200170SO 2003 10 2 WS92003F00000 220030815A8530AEC631397 CYLINDER HEAD CESSNA414 414A 2075907CE CONT O520 TSIO520N 17040SO ENGINE SEPARATED B WS9RA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 NM09415ST235 414A0467 R228062R AIRCRAFT DEPARTED, PILOT EXPERIENCES ROUGH RUNNING RIGHT ENGINE, AND LOSS OF POWER. PILOT LANDED, AND UPON INSPECTION BY COMPANY MECHANIC DISCOVERED NR 6 CYLINDER CRACKED ALL THE WAY AROUND CYLINDER HEAD BETWEEN THE 9TH AND 10TH COOLING FIN. CYLINDER WAS REPLACED AND BROUGHT BACK WITH NO OTHER APPARENT PROBLEMS. ON THE 19 OF AUG, RECEIVED A LETTER FROM A/C MFG COMPANY WITH A SB AND ECI SB. UPON INSPECTION OF THE LEFT ENGINE, FOUND NR 6 CYLINDER EFFECTED BY SB`S BUT NOT CRACKED. 1L72 3O3 O A7CE E8CE 20031014001832003101400183NM 2003 10 14 SWAA032095 120030919A53306550570 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031020002152003102000215WP 2003 10 20 UPS03841363 120030919A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 772.500. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20031020002292003102000229WP 2003 10 20 UPS03841341 120030923A53203755822505 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 340 BETWEEN LONG 27L-28L. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20031020002942003102000294NM 2003 10 20 2003UALA00723 120030928A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29369UA 24538 CABIN FLOORBEAM AT STA 294.4 HAS CORROSION FROM RBL 24 TO RBL45. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPLACEMENT WITH ANGLE SPLICE. 2L72 4F4 FRTA16WE E2GL 20031030000462003103000046NM 2003 10 30 UPS03441304 120030905A571265B078345 RIB BOEING747 747121 1384871NM NR 4 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 4 V/C FLAP I/B LINKAGE O/B SUPPORT RIB FOUND CORROSION CRACKED. RIB ASSY REPAIRED IAW SRM 51-10-01 PG 8. 2L74 4F A20WE 20031027001112003102700111NM 2003 10 27 ASAA02402PP 120030407A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND SHEAR TIE CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001702003102800170EU 2003 10 28 USAASA03117 120030922A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19700UW 0885 DCA - THE EMERGENCY LIGHTS FAILED THE SELF TEST. MAINTENANCE REPLACED THE LEFT MIDDLE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031118000432003111800043EU 2003 11 18 AWXA200301158 120031007A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 242 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28631AW 077 LAS - EEL - FLIGHT CREW REPORTED THE RT OVERWING EMERGENCY EXIT SIGN WAS NOT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040204001262004020400126NM 2004 2 4 EIA2003122 120031003A5320 WEB BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 AFT CARGO COMPT, BS 1480 TO BS 1490 BETWEEN LBL 0 TO LBL 45.5, UPPER SURFACE OF THE WEB IS CORRODED. FABRICATED THE FOLLOWING REPAIR PARTS, (1) EA, WEB P/N 482-53-2-2, (1) EA DOUBLER P/N 482-53-188-2-3, (1) EA DOUBLER P/N 482-53-188-2-4, AND INSTALLED IAW ECRA NR 482-53-188-2, PAGES 1-4, ITEMS 1-15. 2L74 4F A20WE 20040204001712004020400171EA 2004 2 4 COMA0360474 120031026A712060135006 BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE SUPPORT CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01814CA9034 7387 CRACK ON UPPER ENGINE SUPPORT BEAM. REPAIRED IAW 601R-53-61-345. 2L72 4F RTA21EA 20040212001022004021200102WP 2004 2 12 CALA0300708 120031211A5754 SKIN DOUG DC9 DC982 3022082WP NR 1 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716806 49260 INSPECTION FOUND A 3 INCH CRACK IN NR 1 SLAT INTERIOR SKIN BETWEEN NR 4 AND NR 5 SLAT TRACKS OF LT WING, STA XFS 167. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5752-01134, PART 1, STEP 13. 2L72 4F A6WE 20031103001352003110300135EA 2003 11 3 SWIA200312475 120031002A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 280 LT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-57 2L72 4F4 FRTA21EA E15NE 20031106002162003110600216NM 2003 11 6 ASAA0310463 120030515A5310654659526 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE SHEAR TIE AT FUSELAGE STATION 727A, RIGHT BUTTOCK LINE 8 CORRODED. REPLACED SHEAR TIE PER SRM. (M) 2L72 4F A16WE 20031117000912003111700091NE 2003 11 17 ALG2003F00096 120030626A3110 WARNING LIGHT SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL CAUTION PANEL FALSE INDICATIONE ALGAK NONE L NO TEST ININSP/MAINT 1 SW03703AL 052 760266 PRIOR TO TAKE OFF, DURING THE FLOAT SYSTEM TEST, WHEN THE TEST SWITCH WAS PLACED IN THE TEST POSITION ALL CAUTION LIGHTS ILLUMINATED. (SAME AS PRESSING CAUTION PANEL TEST SWITCH). THE PILOT ALERTED MAINTENANCE, THE MECHANIC REMOVED AND REPLACED THE CAUTION PANEL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20031120000942003112000094WP 2003 11 20 MEX2003459 120031003A32465930594547 WHEEL DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE MLG STUCK W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW231003Y7888 48068 AIRCRAFT RETURN TO PLATFORM DUE TO TAXING VIBRATION WS FELT ON THE BRAKES AND THE AIRCRAFT STOPS BY ITSELF. DURING REVISION WAS DETECTED THE BRAKE NUMBER THREE TIED. BRAKE ASSEMBLY AND TIRE NUMBER 3 WAS REPLACED IAW MM 32-42-01 AND 32-40-01. 2L72 4F4 F A6WE E2EA 20040112001842004011200184EU 2004 1 12 03FDEA02236 120031223A2840SIC50545 COMPUTER AIRBUS310 A310 EU FUEL SYSTEM FAULTY A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25415FE 349 LEFT INNER TANK QUANTITY WENT TO ZERO READING IN LESS THAN A MINUTE. AFTER THE FQI CHAN SUPPLY 1 AND 2 C/B'S WERE RESET IAW QRH FUEL LEAK PROCEDURE ECAM SHOWED XX'S IN LT INNER AND TOTAL. FUEL QUANTITY READING RETURNED PASSING 12,700 FT. ON THE DESCENT. REMOVED AND REPLACED FQIC (15QT) IN REF TO A310 AMM 28-42-38-4. PERFORMED FQIC FUNCTIONAL TEST AND OPS CHECK IN REF TO A310 AMM 28-42-38-5. ALL FQIC SYSTEMS CHECK GOOD AT THIS TIME. 2L72 4F RTA35EU 20040112001902004011200190SO 2004 1 12 C2XA03BT120 120031222A323221180100009 ACTUATOR EMB 145 EMB145 3260210SO NLG LEAKING A C2XAK NONE O OTHER APAPPROACH 1 SW27149591223712237 145091 CREW REPORTED, THUMPING NOISE HEARD ON DESCENT AND APPROACH. ALMOST SEEMS THAT NOSE GEAR DOOR WAS CYCLING. MAINTENANCE TROUBLESHOT AND FOUND A LEAKING ACTUATOR AT NOSE LANDING GEAR DOOR NR 2. REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATOR IAW EMB145 AMM 32-33-03, OPS CHECKED GOOD. ALSO, FOUND CORROSION ON THE NOSE LANDING GEAR WOW PROXIMITY SWITCH. REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH (PART NUMBER: 80-057-01 SERIAL NUMBER: 1374) IAW EMB145 AMM 32-63-02, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040112002522004011200252WP 2004 1 12 AALA20031430 120031214A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21447AA 49473 DFW OVERWING EXIT DOOR EMERGENCY EXIT SIGN LIGHTS INOPERATIVE AT AFT LT AND RT ABOVE THE DOORS. REPLACED THE B5-10 BATTERY PACK ASSEMBLY ABOVE THE DOORS AT AFT LT AND RT OVERWING EXIT DOOR EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20040112002412004011200241WP 2004 1 12 AALA20040002 120031231A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21598AA 53288 SAT EMERGENCY LIGHTS FROM ROWS 21 THROUGH 31 INOPERATIVE. REPLACED CENTER AFT BATTERY MODULE AND BATTERY FOR EMERGENCY LIGHTS FROM ROWS 21 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA6WE 20040114000012004011400001GL 2004 1 14 DXTA200300152 220031104A7200 ENGINE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LEFT FLAMED OUT E DXTAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 GL07936QS 7500036 CAE330079 DURING TAKE-OFF LT ENGINE CHIP DETECTOR AMBER CAS MESSAGE CAME ON. ABORTED TAKE-OFF. REMOVED AND REPLACED LEFT HAND ENGINE IAW CESSNA 750 MAINTENANCE MANUAL CHAPTER 71-00-03. 2L72 4J4 FRTT00007WITE6CH 20040114000052004011400005 2004 1 14 DHL2003362013 420031115A2297 WIRE AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE TORQUE LIMITER BROKEN A DHLAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01362DH 84 IN CLIMB THRU 15,000 FT, NR 1 PITCH TRIM DISENGAGED, NR 1 PITCH TRIM ENGAGED, WITH NO PITCH TRIM FUNCTION. AFTER PITCH TRIM DISENGAGE, HARMONIC VIBE DURING LEVEL FLT AT 17,000 FT, VIBE CEASED WITH POWER REDUCTION. CLIMB THRU FL180, REPETITIVE LOUD NOISE OCCURRED. RETURN TO JFK. ENG PARAMETERS NORM THRU ALL FLT REGIMES. NO ABNORM ROLL TEND NOTED. YOKE VIBE FELT FROM 1ST INSTANCE OF A/C VIBE. FOUND 2 BROKEN WIRES AT PITCH TRIM TORQUE LIMITER. REPAIRED IAW ESPM. TORQUE LIMITER ALSO FOUND TO HAVE 1 BAD SWITCH. R&R LIMITER. NR 1 PITCH TRIM OPS CKD NORM. INSPECTED UPPER SURFACE OF RT STAB, FOUND PANEL MISSING FASTENERS. INSTALLED FASTENERS IAW MM. A/C INSPECTED & FOUND SAFE OPERATING CONDITION FOR ACCEPTANCE FLT. 2L72 4F4 FRTA35EU E23EA 20040114000242004011400024EA 2004 1 14 SWIA200312588 120031112A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 FS 280 RIGHT FLOORBOARD RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11 & RII 53-401. 2L72 4F4 FRTA21EA E15NE 20031125000302003112500030WP 2003 11 25 DHL2003805534 120030804A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 FWD SERVICE DOOR JAMB AFT LWR CORNER CRACKED 0.600 BETWEEN STA 185.000 AND STA 190.000, L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 14 SHEET 2 PG 85-86. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 14 SHEET 2 PG 85-86. FABRICATED FILLER AND DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 14 SHEET 2 PG 85-86. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER AND TRIPLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 14 SHEET 2 PG 85-86, SRM 51-1-21 PG 1 SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031124001072003112400107WP 2003 11 24 DHL2003805556 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS.410.250 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, 2. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS 2 EA IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10 SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, 2. 2L74 4F RT4A25 20040114001952004011400195SO 2004 1 14 MASA200300418 120031017A2560RE1013104 MEDICAL KIT EMB 145 EMB145LR 3260212SO CABIN OPEN A MASAK NONE O OTHER UKUNKNOWN 1 SW07855MJ2856 145614 DURING PREFLIGHT CREW FOUND EMERGENCY MEDICAL KIT OPENED. MECHANIC REINSPECTED AND RESEALED KIT. 2L72 4T RTT00011AT 20031215001352003121500135WP 2003 12 15 AALA20031166 120031026A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21249AA 49269 BOS - DURING OVERNIGHT MAINTENANCE, FOUND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031218000202003121800020NM 2003 12 18 QXEA200301475 120031123A2910 HYDRAULIC SYSTEM BOMBDRDHC8 DHC8401 1390041NM NR 2 SYSTEM CONTAMINATED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09413QX 4060 ON FLIGHT NUMBER 2351, LT DOOR UNSAFE & GEAR HANDLE LIGHT REMAINED ON FOR 10 SECONDS AFTER GEAR RETRACTION & THEN CYCLED ON/OFF 4 TIMES IN 5 SECOND INTERVALS. FOUND LARGE QUANTITYS OF AIR, NR 2 HYDRAULIC SYSTEM. PERFORMED FULL BLEED. RAISED & LOWERED A/C. PERFORMED OPERATIONAL TEST OF PRIMARY EXTENSION & RETRACTION SYSTEM. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031222000652003122200065WP 2003 12 22 ASAA0380614 120031007A53219936537503 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, FLIGHT DECK HAS CORRODED FLOORBOARD INSERTS AT FS 150-160. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031222000792003122200079WP 2003 12 22 MEX2003540 120031128A2913AS66411LS666 PUMP DOUG DC9 DC983 3022083WP HYD SYSTEM FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23838AM 49397 AIRCRAFT RETURNED TO GATE DUE TO THE LT ENGINE HYDRAULIC PUMP DID NOT SHUTOFF IN THE 'OFF' SWITCH POSITION. THE HYDRAULIC PUMP WAS REPLACED AND THE SYSTEM WAS TESTED IAW MM 29-10-01. (M) 2L72 4F RTA6WE 20031219001292003121900129NM 2003 12 19 03FDEA02110 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031223001352003122300135EU 2003 12 23 MALA030537 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 8B FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 8B IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031231000122003123100012NM 2003 12 31 TSAA0253249 120030917A531565C345371 FLOORBEAM BOEING737 737282 13844ATNM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13824AL 23045 REMOVED EXISTING FASTENERS, STIFFENERS, ANGLE AND A SECTION OF THE WEB. REMOVED AND DISCARDED REINFORCING ANGLE, DOUBLER AND A SECTION OF THE WEB. DRILL AND COLD WORKED THE HOLES IN THE CHORD. INSTALLED SPLICE ANGLE AND STIFFENERS WITH FASTENERS SHOWN IN SECTION A-A. INSTALLED THE ANGLE, REINFORCING ANGLE, FILLER DOUBLER, SPLICE PLATES AND THE WEB WITH FASTENERS FROM THE KIT. APPLIED ALODINE, BMS 10-11 TYPE 1 PRIMER AND TYPE 11 ENAMEL TO ANY BARE SURFACE. COMPLETED REPAIR IAW ECO 2223, FIGURES 4 AND 9. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040105001402004010500140NM 2004 1 5 SWAA032758 120031217A53306546881 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1025, BETWEEN STR 16L AND STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040106002192004010600219WP 2004 1 6 GTIA030992 120031119A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - PILOT SEAT FLOOR PANEL, RUB STRIPS DELAMINATED, CENTER HAT, CHANNEL DELAMINATED, RUB STRIPS MISSING, CRACK IN PANEL, CONE CRACKED, CONE SEAL MISSING, CORRODED, AND NO NON-SKID. FABRICATED NEW SEAT FLOOR PANEL. (M) 2L72 4F RTA6WE 20031010000902003101000090SW 2003 10 10 BAQA089486 120030922A2435 BRUSHES BELL 222 222U 1182140SW LYC LTS101LTS101* NE STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03223HX927 24683 47511 BRUSHES WORN. 1000 HOUR OVERHAUL DUE SOON. THIS IS 2 OF 2 TO BE RETURNED. REPLACED WITH SERVICEABLE UNIT. 9/29/03 1G72 3U3 U H9SW E5NE 20040112000102004011200010NM 2004 1 12 USAABB03224 120031215A3350 CONNECTOR BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 FOUND FLOOR EMERGENCY LIGHTS AT THE OVERWING CROSS AISLE AND ROW 17 THROUGH 23 INOPERATIVE. MAINTENANCE SECURED LOOSE CONNECTIONS. (M) 2L72 4F RTA1NM 20040311000202004031100020NM 2004 3 11 ASAA0310257 120030327A53206546583 FLANGE BOEING737 737298C 1384490NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLANGE AT BS 1040-1064, STRINGER 22L CHAFED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031203000662003120300066EU 2003 12 3 A6WA200360056 120031015A5330 SKIN BAC 146 146200A 1500266EU FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31183US E2043 LT FUSELAGE DENTS MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830004. (M) 2H74 4F A49EU 20031203001722003120300172WP 2003 12 3 GTIA030884 120031017A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP CABIN CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR WEB CORRODED UNDER GALLEY DRAIN PAN STATION 158 RBL - 44 INCHES. (M) 2L72 4F A6WE 20040123000662004012300066EU 2004 1 23 KBM2003F00091 120031108A5210852G10 SEAL SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE LT DOOR TORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 RUBBER PROFILE SEAL, LT DOOR SEAL RIPPED AND TORN. REPLACED WITH NEW. 1G71 3U3 UNCH9EU E19EU 20040122000582004012200058SO 2004 1 22 SIMA200332706 120031123A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 MAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR. CONNECTOR WAS RECONNECTED AND AN OPS CHECK WAS COMPLIED WITH AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040127001782004012700178WP 2004 1 27 ASAA0380651 120031015A53219936692501 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS CORRODED INSERTS AT FS 1117-1174. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20031208000302003120800030NM 2003 12 8 03FDEA01908 120031108A5712ARB2850506 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT WING LEADING EDGE NR 16 SLAT TRACK INBOARD WEB SUSPECT CRACK. RT WING L/E EDGE NR 16 SLAT TRACK I/B CRACKED RIB REMOVED & REPLACED AS PER SRM 51- 33-01 VOL 2. 2L73 4F RTA22WE 20031204001462003120400146WP 2003 12 4 03FDEA01761 120031016A2140 SENSOR DOUG DC10 DC1010 3022110WP CARGO TEMP MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25367FE 46605 CARGO BAY TEMP AFT WAS PEGGED AT 170 DEG. RETURNED FLIGHT TO LAX. REMOVED AND REPLACED CARGO COMPARTMENT TEMP SENSOR (TRANSMITTER) PER MM 21-41-01-2, OP'S CK'D GOOD. 2L73 4F A22WE 20031208001752003120800175SO 2003 12 8 C2XA03CL184 120031029A32347455501 CONTROL LEVER EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2716911 145446 THE CREW REPORTED DURING CLIMBOUT THE GEAR WOULD NOT RETRACT. THE CREW RECYCLED THE GEAR AND THE GEAR RETRACTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20031208001042003120800104 2003 12 8 IXXA0300065O 420031025A23005220535004 SUPPRESSOR DOUG DC8 DC871F 302199DWP RADIO FAULTY A IXXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW11822BX87363355 45813 DURING CRUISE FROM RJTY TO VTBU CREW NOTED NR 2 HF INOP WHEN KEYING MIC TO TUNE RADIO. TONE WAS FUZZY. CREW RETURNED AIRCRAFT TO RJTY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT TO FAULTY LIGHTNING ARRESTOR AND FAULTY TRANSMIT COAX. MAINTENANCE REPAIRED COAX AND REPLACED LIGHTING ARRESTOR PER ALL APPLICABLE MANUALS. OPERATIONAL CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20031209001502003120900150NM 2003 12 9 QXEA200301366 120031027A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX- REPLACE SEAT TRACK NR 8 DUE TO CORROSION DAMAGE. REPAIRED IAW DHC-8 RD 8-53-4473. 2H72 4T RTA13NM 20031210000752003121000075WP 2003 12 10 AALA20031319 120031124A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217539A 49993 RDU VENTRAL STAIRS SIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR VENTRAL STAIRS SIDE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210001742003121000174NM 2003 12 10 CALA0300608 120031019A253099259890001 OVEN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FWD GALLEY MALFUNCTIONED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0916310 23361 SMOKE IN FLIGHT DECK. REMOVED AND REPLACED OVEN. 2L72 4F4 FRTA16WE E2GL 20030919000532003091900053 2003 9 19 GLBA2003118 420030811A3442 CONNECTOR BEECH 1900 1900D 1154162CE WX RADAR SYS LOOSE A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03208GL UE208 WX RADAR DOES NOT TILT, SECURED LOOSE CONNECTOR ON ANTENNA. 2L72 4T RTA24CE 20030919000882003091900088NM 2003 9 19 372PA0034 120030812A339758781 WIRE HARNESS BOEING737 737306 13844BGNM EMERGENCY LIGHT DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 LOW LEVEL EMERGENCY LIGHTING (AFT SECTION) INOPERATIVE. REPLACED AFT EMERGENCY HARNESS. OPS CHECKS GOOD IAW MM33-50-0. 2L72 4F RTA16NE 20030918001082003091800108NM 2003 9 18 PCAA0308094 120030806A2120 ODOR DHAV DHC8 DHC8102 2809003NM CABIN DETECTED A PCAAO OTHER O OTHER NRNOT REPORTED 1 EA13807EX 292 CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN AREA. MAINTENANCE INSPECTED AREA AND REPORTED NO ODOR WITH THE OVERHEAD LIGHT OFF. MEL 33-02 WAS ISSUED. AIRCRAFT RETURNED TO SERVICE. DURING NEXT OVERNIGHT MAINTENANCE VISIT ALL LAMPS AND FIXTURES FOR OVERHEAD LIGHTING WERE INSPECTED, AND NO DEFECTS WERE FOUND. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030922001142003092200114CE 2003 9 22 DXTA200300087 120030817A3260 BULB CESSNA500 560CESSNA 2076750CE MLG INDICATOR BURNED OUT E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07343QS 5600444 RT MAIN LANDING GEAR LIGHT NOT ILLUMINATED WHEN GEAR CONTROL SELECTED DOWN ON APPROACH TO PHX, EMERGENCY GEAR EXTENSION SYSTEM ACTIVATED. TROUBLESHOT SYSTEM FOUND RT MLG INDICATOR BULB NOT ILLUMINATING. REMOVED AND REPLACED BULB, RETRACTED AND EXTENDED LANDING GEAR SEVERAL TIMES. PURGED LANDING GEAR HYDRAULIC SYSTEM, SERVICED NITROGEN BOTTLE AND HYDRAULIC RESERVOIR, ALL WORK DONE IAW 560 MM CHAPTER 32-30-00. 2L72 4F RTA22CE 20060801001072006080100107WP 2006 8 1 IXXA060557S 120030909A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND AFT PASSENGER DOOR, L-2, CUT-OUT UPPER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D. 2L74 4F RT4A25 20030401001512003040100151WP 2003 4 1 DHL2003804661 120030212A5210 SKIN DOUG DC8 DC873F 302199FWP PAX DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FWD PASSENGER DOOR INTERIM REPAIR AT AFT LWR JAMB CORNER STA. 55.00 LT PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 15 REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG. 1 CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG , FABRICATED FILLER & DOUBLER (7075 T6 0.63) & TRIPLER (7075T6 .080) IAW SRM53-2-0 FIG 15 . CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B. ISTALLED FILLER , DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG. 15 , SRM 51-1-21 PG. 1 , SRM 51-1-20D PG. 9 , SRM51-1-15 PG 1 2L74 4F RT4A25 20030821000792003082100079NM 2003 8 21 03FDEA00934 120030620A5510ALC8100 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT HORIZONTAL STAB UPPER AFT PLANK 28L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS. LEFT HORIZONTAL STAB UPPER AFT PLANK NR 28L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030331001162003033100116NM 2003 3 31 DHL2003704508 120030203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH FUSELAGE FRAME AT STA 520 IS DENTED BETWEEN STR 16-R AND 17-R. ROUTED CRACK AREA APPROX 730 X 1.210. FABRICATED REPAIR DOUBLER FROM 7075-T6 .063. TREATED AND PRIMED AND INSTALLED PER SRM 51-40-1 FIG 1. 2L73 4F RTA3WE 20030328000482003032800048SO 2003 3 28 C2XA03TY039 120030326A531114525422001 FRAME EMB 145 EMB145ER 3260211SO LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 DURING A SCHEDULED INSPECTION THE LAVATORY L/H FLOOR SIDEWALL FRAME AT STRINGER 15 LT WAS FOUND TO BE CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE SIDEWALL FRAME IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030402000192003040200019NM 2003 4 2 03FDEA00358 120030304A5740ARC050213 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING OUTBOARD FLAP INBOARD HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLE AND LUG CORRODED. WINGS- LEFT O/B FLAP- I/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED HOLE REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1-5740-68588. 2L73 4F RTA22WE 20030425000212003042500021NM 2003 4 25 KPVA200310 120030225A2560 BATTERY DHAV DHC8 DHC8103 1386005NM LIGHT INOPERATIVE A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13805WP67 63436 353 COCKPIT PORTABLE EMERGENCY LIGHT BATTERY WEAK. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT. OPERATIONAL CHECK OF SYSTEM GOOD. WORK IAW MM. 2H72 4T RTA13NM 20030428000892003042800089EU 2003 4 28 MALA030223 120030403A3030QR50V SENSOR SAAB SF340 340B 7860101EU PITOT HEAT FAILED A MALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15446XJ 340B446 DURING TAXI OF FLIGHT 3148, ELECTRICAL ODOR NOTED IN CABIN BY F/A AND PASSENGERS FOUR ROWS BACK. MAINTENANCE FOUND WIRE HG-7-2002 CHAFED AND CURRENT SENSOR TO LT PITOT HEATER BURNED. REPLACED CURRENT SENSOR (P/N ON/OFF QR50V), PERFORMED TEMP REPAIR OF WIRE HG-7-2002, FOR FERRY FLIGHT. PERFORMED OPS CHECKS OF LT PITOT HEAT. OPS CHECK GOOD. INSPECTED REMAINDER OF A/C, FOUND SAFE FOR FERRY FLIGHT ABR-MSP. 2L72 4T RTA52EU 20030428001232003042800123WP 2003 4 28 ZW0A0303801 120030404A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139619V 53566 THE EGRESS LIGHT WAS INOPERATIVE AT ROW 12, 13, 21 AND ROWS 27 TO 30. REPLACED THE LAMP (P/N 7732) AT ROW 12, 13, AND 21. RECONNECTED LOOSE CONNECTOR AT ROW 31 FOR ROW 27 TO 30. CHECK-C 10-30-02 STL. 2L72 4F RTA6WE 20030425000802003042500080NM 2003 4 25 QXEA0300387 120030320A5420 DEFLECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - OIL COOLER AIR DEFLECTOR RIGHT HAND FORWARD LIP IS CHAFING ON LOWER COWL. REPAIRED IAW Q-400 NDT MANUAL 51-00-01-250-801, HORIZON AIR EA 6-71-81 AND RD 8/4-71-046. 2H72 4T RTA13NM 20030429001252003042900125NM 2003 4 29 PCAA0304066 120030410A3320 LIGHT DHAV DHC8 DHC8102 2809003NM CABIN SMOKE A PCAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA13844EX 339 PIT-ERI FLIGHT 3989 CREW REPORTED A SMOKE ODOR IN THE CABIN, SMOKE WAS SEEN AT SEAT 1AC PASSENGER SERVICE UNIT. SMOKE EXTINGUISHED WHEN LIGHTS WERE TURNED OFF. EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED ALL CABIN LIGHTING. PROBLEM WAS ISOLATED TO LIGHT AT SEAT 2AC. FLUORESCENT TUBE WAS REMOVED. POWER WAS REAPPLIED, NO DEFECTS WERE NOTED. MEL 33-02 WAS ISSUED. AIRCRAFT WAS RETURNED TO SERVICE. ON 12 APRIL 2003 A NEW FLUORESCENT TUBE WAS INSTALLED AT SEAT 2AC. NO SMOKE OR OTHER DEFECTS WERE NOTED AFTER TESTING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030501002052003050100205NM 2003 5 1 ASAA0310038 120030225A532065319601 PAD BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, STANSION PAD AT BS 807, RIGHT BUTTOCK LINE 60 CORRODED. REMOVED AND REPLACED STANSION PAD PER SRM. (M) 2L72 4F RTA16WE 20030505001572003050500157EA 2003 5 5 COMA0360192 120030415A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01959CA17188 7116 FLIGHT 5907 LANDING GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030506002022003050600202WP 2003 5 6 ASAA0380141 120030222A535059360461 FILLET DOUG DC9 DC983 3022083WP WING TO BODY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OAK - DUIRNG C-CHECK, FOUND CORROSION ON LEFT WING-TO-BODY FAIRING FILLET PANEL 2108. INSTALLED DOUBLER AT FS 1079-1098 PER SRM 53-04. (M) 2L72 4F RTA6WE 20030507001202003050700120CE 2003 5 7 CA030417010 120030407A21211013841761 BEARING BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL BLOWER FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CA 21337 (CAN) DURING DESCENT THE CREW NOTICED AN ELECTRICAL SMOKE ODOR IN THE CABIN WITH NO VISIBLE SIGNS OF SMOKE, THE CREW ACTIONED THE EMERGENCY CHECKLIST AND LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE FORWARD BLOWER ASSEMBLY WAS A LITTLE NOISY AND AFTER APPROXIMATELY ONE HOUR OF OPERATION IT WOULD START TO SLOW DOWN AND MAKING SEVERE UNUSUAL NOISES (SOUNDS LIKE A BAD BEARING). THE BLOWER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A24CE E4EA 5 CSTC 20031211001882003121100188WP 2003 12 11 2003F00644 120030907A5210591412155 PAN DOUG DC9 DC915F 3022037WP ENTRY DOOR CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 DURING 4C CHECK SERVICE, FOUND FORWARD ENTRY DOOR, UPPER AFT PAN SEGMENT CRACKED. THE DAMAGED PART WAS REPLACED BY A NEW ONE. (M) 2L72 4F A6WE 20031212000092003121200009NM 2003 12 12 SWAA032478 120031107A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED (3 EA) AT LBL 1, WL 187, RBL 1, WL 187, AND RBL 5, WL 213. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20030919001012003091900101EU 2003 9 19 PH92003F00001 120030723A6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU TAIL ROTOR CRACKED E PH9AO OTHER O OTHER NRNOT REPORTED 1 NM05170PA2760 2637 TAIL ROTOR BLADE HAS 4000 HOURS TBR(SLL). UNIT FAILED AT 2760.0 TTSN. MASSIVE SPAR CRACK ON LAMINATED SPAR. UNIT RETURNED TO MFG. 1G71 3U H9EU 20030922000882003092200088 2003 9 22 CNMA200300003 420030818A2300 MULTIPLEXER DOUG DC10 DC1030 3023501WP AUDIO SMOKE A CNMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07540AX 46595 SMOKE REPORTED BY CABIN CREW RT SIDE AT R-3 AFTER TAKE-OFF. 2L73 4F A22WE 20030923001482003092300148NM 2003 9 23 03FDEA01414 120030901A5753ARC70571 SUPPORT FITTING DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING- O/B FLAP VANE SUPPORT FITTING NR 5 FROM I/B ATTACH HOLE FOUND CORRODED. CORROSION ON LT WING, O/B FLAP VANE SUPPORT FITTING NR 5 FROM I/B ATTACH HOLE REMOVED AND REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-73298. 2L73 4F RTA22WE 20040128000592004012800059NM 2004 1 28 03360401 120031226A3350321430 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27401FJ 3145 DURING INSPECTION THE EMERGENCY FLOOR LIGHTING FROM ROWS 4 TO 8 WAS FOUND INOPERATIVE. THE BATTERY WAS FOUND DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040130000762004013000076NM 2004 1 30 DHL2003742545 120031208A5751 RIB BOEING727 727225 1384077NM LT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, LT WING O/B AILERON INTERNAL RIB CRACKED (11TH) FROM O/B. REMOVED AILERON INTERNAL RIB CRACKED 11TH FROM O/B IAW B727 SRM 51-30-2. FABRICATED NEW RIB 11TH FROM MAT 7075-T6 .025 PO 9912281 DIM14.125 X 5.5 INCH IAW B727 SRM 57-20-2 FIG 8. TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED NEW WEB 11TH, IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040204000152004020400015NM 2004 2 4 C1HA200394047 120031128A3350 BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 EXTERIOR EMERGENCY LIGHT ON C2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR C2 DOOR LIGHT OPS NORMAL IAW 727 MM 33-50-22. 2L73 4F A3WE 20040205000312004020500031NM 2004 2 5 C8GA20030027 120031119A7933 WIRE BOEING727 727223 1384074NM PWA JT8 JT8D15A 52051NE OIL TEMP BULB BROKEN A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO15715AA 22470 700782 FLT 800 FROM KMIA TO MMUN. AFTER TAKE-OFF CLIMBING THROUGH 1,000 FT AGL, THE NR 3 ENGINE OIL TEMPERATURE BEGAN TO FLUCTUATE BETWEEN 100 DEGREES AND OFF SCALE HIGH. AT APPROXIMATELY 15,000 FT, THE NR 3 ENGINE STAYED OFF SCALE HIGH. REFERENCE AOM CHECKLIST FOLLOWED BY NR 3 ENGINE IN-FLIGHT SHUTDOWN AS PRECAUTIONARY, ADVISED ATC AND DECLARED EMERGENCY. AIRCRAFT AIR TURN BACK TO KMIA AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND A BROKEN WIRE/PIN AT THE NR 3 ENGINE OIL TEMP BULB CONNECTOR. REPAIRED AND REPINNED BROKEN WIRE AT CONNECTOR, PERFORMED ENGINE RUN AND SYSTEM CHECK GOOD IAW MM 79-32-0 AND 20-11-1. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040205000802004020500080NE 2004 2 5 ASOA03697 220031231A7261AS3209153 O-RING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE OIL FILTER BROKEN A ASOAO OTHER J WARNING INDICATION DEDESCENT 1 SO11533AS 460 FLT 4313 - DURING DESCENT INTO ATL FROM MGM, THE CREW RECEIVED A LOW OIL PRESSURE ALARM ON THE LEFT ENGINE. QRH PROCEDURES WERE COMPLIED WITH. THE CREW SHUTDOWN THE LEFT ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED A BROKEN O-RING ON THE OIL FILTER TO THE LEFT ENGINE. THE OIL FILTER WAS ALSO REMOVED AND REPLACED. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20040206000812004020600081WP 2004 2 6 DHL2004806509 120031229A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 2 FLOOR TRACK PLUG LUGS WORN STA 1130.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040210000422004021000042NM 2004 2 10 PCAA0311145 120031130A6120 BETA SWITCH DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF* NE LOCK OUT MALFUNCTIONED A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13824EX 387 121178 001505 AFTER TAKEOFF, NR 1 PROP CYCLED FROM 1200 TO 800 RPM, COULD NOT BE CONTROLLED UNTIL ENGINE WAS SHUTDOWN AND FEATHERED. AFTER RETURN TO FIELD, MAINTENANCE READ THE FDR, NO OVERTORQUE FOUND. THE ENGINE AND PROP CONTROL LINKAGES WERE INSPECTED, NO DEFECTS FOUND. NO ABNORMAL PARAMETERS NOTED ON GROUND RUN, THE BETA LOCKOUT SYSTEM WAS DETERMINED TO HAVE CAUSED THE PROP RPM FLUCTUATION. BETA LOCKOUT MEL WAS COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20040316001012004031600101WP 2004 3 16 ASAA0380306 120030411A53205936603501 TRANSITION PANEL DOUG DC9 DC983 3022083WP CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, AFT CARGO BAY TRANSITION PANEL IS CORRODED. REPLACED PANEL PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20031217000662003121700066WP 2003 12 17 DHL2003805592 120030729A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E UPPER SKIN CORRODED AT XFS 423.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS ON RIGHT WING CTR L/E, XFS 423.000 IAW SRM 57-2-1 FIG 38, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. FOR REMOVAL/REINSTALLATION OF CTR L/E SEE NR 0211. 2L74 4F RT4A25 20040401000462004040100046WP 2004 4 1 ASAA0380399 120030421A5347 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FORWARD FLIGHT ATTENDANT SEAT INBOARD FLOOR ATTACH ANGLE CORRODED. REPAIRED PER SRM. (M) 2L72 4F A6WE 20030819001772003081900177EA 2003 8 19 03222632 120030810A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING MAINTENANCE INSPECTION THE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OVERHEAD EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030402000532003040200053NM 2003 4 2 2003UALA00330 120030326A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 847, STR 9R, FRAME WEB IS CRACKED AT FASTENER HOLE MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT, DOUBLER INSTALLED 2L72 4F4 FRTA16WE E2GL 20030404001342003040400134 2003 4 4 SWAA030410 420030221A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED A1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F A16WE 20030410000372003041000037WP 2003 4 10 GTIA030088 120030210A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND WEB STATION 200-218 RBL 26 LBL 26 HAS CORROSION. FABRICATED WEB PANEL. (M) 2L72 4F A6WE 20030410001322003041000132NM 2003 4 10 SWAA030681 120030324A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 767, RBL 8 TO LBL 12. REPAIRED FLOORBEAM PER SWA RA. 2L72 4F RTA16WE 20030416003942003041600394 2003 4 16 SWIA200311700 420030112A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA NR 1 AHRS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07591SW 7079 PHX: YAW DAMPER ONE WON'T ENGAGE. POWERED DOWN A/C AND DID NOT CLEAR PROBLEM. FERRIED TO SLC. SLC: CAPTAIN'S AHRS FAILURE. RED FD, ATT & MAG MESSAGE ON PFD. RED MAG MESSAGE ON MFD. REMOVED AND REPLACED NR 1 AHRS PER CRJ MM 34-21-01. OPS CHECK GOOD. FCC DIAGNOSTICS AND MDC INDICATE NR 1 AHRS OPS CHECK GOOD. NO FAULTS NOTED. 2L72 4F RTA21EA 20030417000562003041700056EU 2003 4 17 MALA030133 120030126A3020 DUCT SAAB SF340 340B 7860101EU RT INTAKE HEAT DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15433XJ 340B433 DURING FLIGHT NR 3319 RT INTAKE HEAT FAILED. RT INTAKE HEAT ANNUNCIATOR ILLUMINATED REPEATILY WHILE INFLIGHT. CYCLED ON AND OFF EVERY 20 SECONDS. QRH COMPLETED. NO ABNORMAL ENGINE INDICATIONS WERE NOTED. AIR RETURN TO DTW DUE TO WEATHER. MAINTENANCE REMOVED AND REPLACED ENGINE UPPER DUCT ASSEMBLY IAW TASKCARD 7160-302. OPS CHECK OF RT INTAKE HEAT SYSTEM IAW MM IS GOOD. 2L72 4T RTA52EU 20030425000732003042500073NE 2003 4 25 MALA030217 220030331A7530216035040 ACTUATOR BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE BLEED BAND MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15530XJ E2364 DURING FLIGHT 3489, NR 2 ENGINE LOW POWER, HIGH EGT. AIR RETURN TO MSP. NR 2 ENGINE ONLY PRODUCE APPROX 91 - 92 PERCENT N1, BUT EGT WENT OVER 600 C. OTHER ENGINE STAYED AT APPROXIMATELY 95 PERCENT, N1 AND EGT WAS CLOSER TO 500 C. A 70 DEGREE DIFFERENCE. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED BAND ACTUATOR P/N 2-160-350-40, SN/OFF 97B009, SN/ON XRC13-98 IAW 72-00-34, BOROESCOPED HOT SECTION 1ST STAGE NOZZLE AND NO DAMAGE NOTED. PERFORMED POWER ASSURANCE CHECK IAW 7100-501, ALL CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20030428001152003042800115NM 2003 4 28 EIA2003053 120030324A5310 SHEAR TIE BOEING747 747273C 1384896NM PWA JT9 JT9D* NE FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 SEVERAL RIVET HEADS POPPED AT SKIN B.S. 680-700, STRINGER 41 RIGHT TO 42 RIGHT. SKIN REPAIR ACCOMPLISHED IAW SRM 53-30-03 FIGURE 1 SHEET 4-7 PAGES 2D, 2E, 2F, AND 2G. SHEAR TIE REPLACED WITH NEW IAW SRM 51-30-02 PAGES 21-32. 2L74 4F4 F A20WE E20EA 20030429001072003042900107SO 2003 4 29 C2XA03SH104 120030413A531014526437001 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV - DURING C-CHECK, THE RIGHT HAND BUTT STRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030429001782003042900178NM 2003 4 29 CA030404008 120030220A2761659603 ISOLATION VALVE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE SPOILERS INOPERATIVE W O OTHER J WARNING INDICATION APAPPROACH 1 CA 1961115727 (CAN) A/C WAS ON APPROACH WHEN NR 2 HYDR ISO VALVE CAUTION LIGHT ILLUMINATED, A/C LANDED WITHOUT INCIDENT. A/C WAS BROUGHT BACK TO HANGAR, NR 2 HYD SYS WAS TOPPED UP AND GEAR SWINGS WERE CARRIED OUT WITH NO LEAKS NOTED. ONCE FLIGHT/TAXI MODE SWITCH WAS PUT INTO FLIGHT MODE GROUND SPOILERS TRIED TO DEPLOY, FLIGHT SPOILER VALVE IN NR 2 WHEEL WELL WAS FOUND LEAKING. AFTER REMOVAL, DISCOVERED THAT THREE OF FOUR RETAINING BOLTS ON ADAPTER PLATE ON SHUTTLE VALVE WERE SHEARED OFF. PROBLEM IS CAUSED BY POUNDING OF SHUTTLE VALVE WHEN THREE THOUSAND POUNDS OF HYD PRESS IS APPLIED TOO IT, WE HAVE BEEN REPLACING RETAINING BOLTS ON STEERING MANIFOLD AND TORQUE BOLTS ACCORDING TO MFG SB 8-32-52. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030505000332003050500033NM 2003 5 5 2003UALA00374 120030410A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 RT FUSELAGE FRAME CRACKED AT BS 360 SKIN ATTACH FLANGE BELOW STRINGER 14R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW REPAIR FLANGE. 2L72 4F4 FRTA16WE E2GL 20030506000962003050600096NM 2003 5 6 CALA0300217 120030425A3350D71702030 CHARGER BOEING737 737824 13844BZNM CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 THE EMERGENCY EXIT LIGHTS ABOVE L-1 DOOR, COCKPIT AND FORWARD CENTER AISLE ILLUMINATES WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. THE BATTERY CHARGER AT LEFT FORWARD POSITION (M1675) WAS REMOVED AND REPLACED IAW MM 33-51-06-960-806. OPERATION OF THE EMERGENCY EXIT LIGHTS CHECKED GOOD. 2L72 4F RTA16WE 20030506001712003050600171WP 2003 5 6 ASAA0380248 120030307A531359360281 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND AFT CARGO AREA LONGERON 30 CORRODED ON UNDERSIDE OF FLANGE. REPAIRED LONGERON 30 PER SRM. (M) 2L72 4F A6WE 20030505001302003050500130NM 2003 5 5 03FDEA00488 120030417A2510 PANEL BOEING727 727200 138407ENM PEDAL COVER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 THE COVER PANEL OVER THE CAPTAINS RT RUDDER PEDAL IS CRACKED. REPAIRED COVER PANEL IAW BOEING CMM 25-00-67. 2L73 4F RTA3WE 20030508000492003050800049NM 2003 5 8 DL738030349 120030410A302032156183 VALVE BOEING737 737832 13844CFNM ANTI ICE FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27375DA 29623 AT START OF T/O ROLL ANTI ICE LIGHT INUNCIATOR ILLUMINATED. POWER WAS RETURNED TO IDLE AND LIGHT WENT OUT. T/O ROLL WAS STOPED AT 40KTS. REPLACED LEFT AND RIGHT ENGINE COWL ANTI ICE VALVES. LEAK CHECKS OK. 2L72 4F RTA16WE 20030508000232003050800023NE 2003 5 8 DL764030345 220030408A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680C2B2 30025NE NR 1 FAILED A DALAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO27829MH7402 7402 29700 706151 ON TAKEOFF ROLL, BETWEEN 30 AND 50 KTS, POWER STABILIZED AT ALTENATE 60, HEARD LOUD BANG AND CONTINUOUS RUMBLE. TAKEOFF ABORTED. ENGINE INSTRUMENTS LOOKED NORMAL. PASSENGERS REPORTED SEEING FLASH OF FLAME ON THE LEFT SIDE OF THE AIRCRAFT. FOUND METAL IN TAIL PIPE. NR 1 ENG REPLACED PER TRANS 14T1 2L72 4F4 FRTA1NM E13NE 20030509000872003050900087SW 2003 5 9 FTU2003F00010 120030424A52305305293 ARM GULSTM690TP 695A 7630519SW GARRTTTPE331TPE331* 01514WP CARGO DOOR CRACKED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE057812 96089 DURING A NORMAL PERIODIC INSPECTION, WHILE INSPECTING UNDER THE BAGGAGE COMPARTMENT FLOOR, THE ELEVATOR BOB WEIGHTS ARE BOLTED TO CRACKS WERE FOUND AROUND THE BOLT HOLES. ITS OUR OPINION THAT THE AREA WHERE THE WEIGHTS ARE BOLTED TO SHOULD BE A THICKER MATERIAL. PARTS WERE REPLACED WITH A NEW ASSEMBLY AND INSTALLED WITH NO PROBLEMS. 1H72 4T3 T 2A4 E2WE 20030513001142003051300114NM 2003 5 13 QXEA0300451 120030408A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM MLG OUT OF ADJUST A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09405QX 4047 ON CLIMBOUT WITH GEAR HANDLE UP, GEAR MOMENTARILY BEGAN TO EXTEND (AMBER UNSAFE LIGHT ILLUMINATED) AND THEN RETRACTED AGAIN. PROBLEM REPEATED NUMEROUS TIMES. GEAR EXTENDED NORMALLY FOR LANDING BUT, LEFT GEAR DOOR LIGHT IS ON. ADJUSTED RIGHT & LEFT HAND MAIN LANDING GEAR PROX SENSORS AND DOOR SENSORS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513002162003051300216CE 2003 5 13 GLBA2003053 120030423A7933MS280341 BULB BEECH 1900 1900D 1154162CE OIL TEMP ERRATIC A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03192GL UE192 LT OIL TEMP ERRATIC, R & R LT OIL TEMP BULB OPS CHECK GOOD 2L72 4T RTA24CE 20030530001092003053000109EA 2003 5 30 CA030507002 120030505A291082970010477 LINE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE HYD SYSTEM LEAKING W O OTHER K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) CREW REPORTED 'TAXIING IN, NR 2 HYD PRESSURE DROPPED TO ZERO.' MAINTENANCE FOUND NR 2 SYSTEM ENGINE DRIVEN PUMP PRESSURE TUBE ASSY TO MANIFOLD CHAFED AND PINHOLE LEAK IN MIDDLE OF LINE. LINE REPLACED AFTT 26193:36 HRS. AF CYCLES: 38398. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030528000092003052800009SW 2003 5 28 HEEA086735 120030522A792137010200004 OIL COOLER BOLKMS105 BO105CB* SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03205UC S668 OIL COOLER MALFUNCTIONED, BOTH ENGINE OIL TEMPS RUNNING TOO HIGH. TO BE SENT TO VENDOR. 1G72 4U H3EU 20030606000362003060600036NM 2003 6 6 CW12003F00002 120030501A3020F2MA724601300A1 PIPE AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE NACELLE ANTI-ICECRACKED B CW1RO OTHER O OTHER NRNOT REPORTED 1 EA11790M 4894 19 WHILE PERFORMING A ROUTINE ENGINE INSPECTION, A BLEED AIR TAP FOR NACELLE ANTI-ICE PRESSURE SWITCHES WAS FOUND TO BE CRACKED AT THE WELD LOCATION. PROBABLE CAUSE WAS VIBRATION. THIS COULD BE PREVENTED BY INSTALLING SUPPORT BRACKET AND NOTING SPECIFIC AREA FOR INSPECTION DURING ENGINE INSPECTIONS. 2K73 4F4 FRTA50NM E44NE 20030609000482003060900048NM 2003 6 9 CALA0300262 120030521A5311 FRAME BOEING757 757224 1384958NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714120 27562 INSPECTION FOUND IMPACT DAMAGE TO FRAME AT BS 1520, STRINGER 26L. THE FRAME WAS REPAIRED IAW ECRA 5310-04348. 2L72 4F RTA2NM 20030520001232003052000123NM 2003 5 20 AALA20030351 120030327A2420GEN5103 IDG BOEING767 767323 1385205NM RT ENGINE FAILED A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21389AA 27449 BLINKING GEN DRIVE LIGHT FOLLOWED BY A STEADY RT GEN DRIVE EICAS MESSAGE, DISCONNECTED RIGHT IDG. PLACARDED RIGHT IDG INOPERATIVE PER MEL REF 24-1 AUTH. CHECKED AND FILLED TO LEVEL IDG OIL LEVELS ALSO CHECKED APU OIL LEVEL FOUND NORMAL ENTERED IN MIC SHEET DEF RED 24-1 AUTH NR 3-129DC-A. REPLACED RIGHT ENG IDG OPS AND LEAK CHECK NORMAL. REMOVED PLAC, CLD MIC SHEET, RAN ENGINE CK IDG LOAD CK OK. (M) 2L72 4F RTA1NM 20030521001702003052100170NM 2003 5 21 SWAA031090 120030514A53206517583 STIFFENER BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL STIFFENER WEB CRACKED AT BS 180, WL 177 & LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SRM. 2L72 4F RTA16WE 20030612000342003061200034SO 2003 6 12 SWIA200312026 120030525A3231 SEQUENCE VALVE EMB 120 EMB120ER 3260203SO MLG DOOR LACK OF LUBE A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07566SW 120341 LEFT MAIN GEAR REQUIRED THREE ATTEMPTS BEFORE RETRACTING. IT APPEARED THAT THE INBOARD GEAR DOOR WAS NOT OPENING. CYCLED LANDING GEAR NUMEROUS TIMES WITHOUT DEFECT. CLEANED AND LUBRICATED SEQUENCE VALVE AND PLUNGERS ON ALL GEAR. OPS CHECK GOOD. 2L72 4T RTA31SO 20030612001262003061200126NM 2003 6 12 UPS03440772 120030521A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, DURING RAP ACCOMPLISH, ITEM N521UP-46-26 CLASSIFY AS CATEGORY -D- REPAIR. SKIN REPAIRED AT BS 2030-2045 STR 44R - 45R AREA AS PER SRM 53-30-03 FIG 1. 2L74 4F RTA20WE 20030613000212003061300021NM 2003 6 13 UPS03440784 120030516A5310 DOOR FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - R2 PAX DOOR FOUND AFT FRAME LOWER CORNER CRACKED AS MARKED. LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 8. 2L74 4F RTA20WE 20030613001432003061300143NM 2003 6 13 SWAA031224 120030603A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BS 500C AND BS 500D. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030513000702003051300070SO 2003 5 13 RAIA00304120 120030424A3260D3899 CONNECTOR EMB 145 EMB145LR 3260212SO MLG UPLOCK LOOSE A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03810HK 145231 RT MAIN GEAR WOULD NOT SHOW UP AND LOCKED AFTER RETRACTION. MAINTENANCE REMOVED AND REPLACED NR 2 MLG UPLOCK PROXIMITY SWITCH CONNECTOR. OPS CK OK. 2L72 4T RTT00011AT 20030514000122003051400012EA 2003 5 14 ASOA03145 120030402A5610NP1393225 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A ASOAB EMER. DESCENT O OTHER DEDESCENT 1 SO11716EV 10084 DURING DESCENT INTO ATL FROM PHF, AT APPROXIMATELY 30,000 FT, THE CAPTAIN'S SIDE WINDOW CRACKED. THE CREW COMPLIED WITH QRH PROCEDURES, REDUCED AIR SPEED AND DESCENDED TO 10,000 FT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S SIDE WINDOW. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514001002003051400100NM 2003 5 14 SWAA031001 120030505A53146545866 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C2 CHECK, FOUND 1 INCH LONG CRACK AT KEELBEAM CENTER PANEL, BS 685, STRINGER 28L. REPAIRED KEEL BEAM PANEL PER SRM. 2L72 4F RTA16WE 20030515000082003051500008EU 2003 5 15 03125324 120030505A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27324UE 41017 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL CLEANED AND SECURED THE CONNECTOR FOR THE FORWARD LIGHTING SECTION. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030604001832003060400183NM 2003 6 4 UPS03440603 120030409A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, AFT CARGO DOOR CUTOUT FWD UPPER CORNER FOUND ONE EACH HOLE CRACK AT SKIN AT SEVEN O'CLOCK POSITION 0.040 INCHES IN LENGTH AS MARKED. AFT CARGO DOOR CUTOUT FWD UPPER CORNER REPAIRED AS PER SRM 53-30-03 FIG 62. CAT B REPAIR REQUIRES REPEAT INSPECTION THRESHOLD AT 15,000 CYCLES AFTER REPAIR INSTALLATION AND REPEAT AT 3,000 CYC INTEVAL PER SRM. 2L74 4F A20WE 20030605000512003060500051NM 2003 6 5 AMTA200300664 120030518A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 AFT C-ZONE 3 LAST EGRESS LIGHTS OUT. INSTALLED NEW LIGHT ASSEMBLY AT ROW 30 DEF, OPS NORMAL ALL THREE LIGHTS, OPS NORMAL. (M) 2L72 4F RTA2NM 20030520000012003052000001NE 2003 5 20 CA030331004 220030325A7261 LINE BOEING737 737275 1384485NM PWA JT8 JT8D9A 52048NE ENGINE LEAKING W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) ON DEPARTURE, OIL QUANTITY ON NR 2 ENGINE AT OR NEAR ZERO AS THEY PASSED THROUGH 300 FT. CREW ELECTED TO CONTINUE FLT & MONITOR. PASSING THROUGH 22,000 FT. OIL PRESSURE STARTED TO FLUCTUATE, CREW IMMEDIATELY CONDUCTED ENG SHUTDOWN CHECKLIST. A/C RETURNED UNDER ABNORMAL LANDING CONFIG & LANDED WITHOUT INCIDENT. MAINT INSPECTION REVEALED NR 2 NACELLE FILLED WITH OIL. MAINT FOUND LEAK AT UPPER BANJO FITTING ON TOP LT SIDE OF GEAR CASE. SOLID LINE THAT RUNS FROM BANJO FITTING TO VENT SIDE OF OIL FILTER BYPASS SWITCH. AS A REPAIR ELECTED TO ACCOMPLISH BOEING SB:737-79-1004 (RELOCATION OF ENGINE OIL FILTER BYPASS SWITCH). A/C GROUND RUNS ACCOMPLISHED WITH NO LEAKS TO REPORT. A/C RETURNED TO SERVICE WITH NO2L72 4F4 F A16WE E2EA 20030521000032003052100003WP 2003 5 21 DHL2003801061 120030405A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING-CTR L/E FORMER CRACKED 0.500, STA XFS. 360.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE AND NEW FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030611000752003061100075NE 2003 6 11 HEEA086560 120030522A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR ERODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03223429030 760096 FIBERGLASS ERODED UNDER THE PRIMARY RUBBER. SENT COMPOSITES FOR INSPECTION. 1G72 3U H1NE 20030612000572003061200057SO 2003 6 12 SWIA200312031 120030527A2752 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07214SW 120280 FLAPS WILL NOT RETRACT FULLY. OUTBOARD FLAPS REMAIN AT ABOUT 10 DEGREES. RETURNED TO SLC. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE PART IAW MM 27-50-09. OPS AND LEAK CHECK GOOD. 2L72 4T RTA31SO 20030617002632003061700263NM 2003 6 17 QXEA200300604 120030430A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - FORWARD SUPPORT FLANGE FOR 262HT IS CHAFED. REPAIRED IAW DHC-8 400 RD 8/4-53-451. 2H72 4T RTA13NM 20030617001832003061700183NM 2003 6 17 QXEA200300590 120030430A7110 CHANNEL BOMBDRDHC8 DHC8401 1390041NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - NR 2 LOWER COWL BOTH VERTICAL CHANNELS FOR BYPASS DOOR MOUNTING CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030521001402003052100140WP 2003 5 21 DHL2003801047 120030404A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 AFT ACCESSORY COMPT- INTERCOSTAL 0.500 INCH CRACKED (STA 1680.00 - STA 1700.000, RBL 20.000). STOP DRILLED CRACK BETWEEN STA 1680.000 AND STA 1700.000, RBL 20.000 IAW SRM 53-2-0 FIG 1B. FABRICATED REINFORCEMENT (2024-T3 0.050) IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ON INTERCOSTAL (AFT ACCY COMPT) IAW SRM 53-2-0 FIG 1B AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001692003052100169NM 2003 5 21 SWAA031089 120030514A53126516300 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, LBL 5.7, WL 183 & WL 213. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20030520000762003052000076NM 2003 5 20 HALA0300230 120030414A7700112E9321G2 CONTROL UNIT BOEING717 717200 1383700NM OVERSPEED PROTECMALFUNCTIONED A HALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP13480HA 55125 RIGHT ENIGNE SYSTEM FAIL LIGHT CAME ON. PERFORMED WIRING CHECK PER FIM 73-21. ALL OK. REMOVED AND REPLACED NR 2 INDEPENDANT OVERSPEED PROTECTOR (IOP) PER MM 73-21-11. CHECK OK. RTS CHECKED OK. OK FOR SERVICE. (M) 2L72 4F TRA6WE 20030522001042003052200104NM 2003 5 22 DHL2003748007 120030517A5710 BRACKET BOEING727 727225 1384077NM SLAT ACTUATOR CRACKED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01748DH 22440 DURING DROP IN MAINTENANCE DISCREPANCY AS FOLLOWS, UPON REMOVAL OF DOUBLERS FOR SB 727-57-0130, FOUND BOTH NR 1 SLAT ACTUATOR MOUNT ANGLES TO BE CRACKED. REMOVED NR 1 SLAT ACTUATOR ANGLES IAW B-727 51-30-2. FAB NEW ANGLES FROM 7075 T-6 .063 INCH PO 9912495 11 X 4 IAW S/B B 727-727-57-0130. TREATED AND PRIMED ANGLES IAW B-727 SRM 51-10-2. INSTALL ACTUATOR ANGLES IAW B-727 SRM 51-30-2 AND S/B 727-57-0130. 2L73 4F A3WE 20030523000232003052300023EA 2003 5 23 QXEA0300551 120030508A2420766277A CONTROLLER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09610QX3442 1744 10033 PDX- ON FLIGHT 2437 IDG1 CAUTION MESSAGE AND DISCONNECT IAW EMERGENCY PROCEDURE. REMOVED AND REPLACED O/SSPG3 CONTROLLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030618000292003061800029NM 2003 6 18 SWAA031323 120030613A335020121 BATTERY BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED RON, FOUND RT FWD CABIN OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030523000982003052300098WP 2003 5 23 MWEA030220 120030519A5320993053823 DOUBLER DOUG DC9 DC982 3022082WP SUBFLOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 SUBFLOOR HAS CRACK LOCATED JUST AFT OF FRAME STATION 275 AND RIGHT CUSP. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030528001052003052800105SW 2003 5 28 ALGA086487 120030522A6230412010453105 SUPPORT BELL 412 412 1182202SW SWASHPLATE WORN E ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01XATAM2164 RE736 33169 SWASHPLATE SUPPORT LUG BORES WORN BEYOUND MAX. DIMENSIONS. 1G72 4U H4SW 20030529000442003052900044SW 2003 5 29 HEEA086635 120030521A6230 BEARING BELL 412 412 1182202SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 MAIN ROTOR LINK HAS WORN BEARINGS. REPLACED 4 EACH BEARINGS 412310400107 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030529000592003052900059SW 2003 5 29 HEEA086646 120030521A3213412321104 CROSSTUBE BELL 412 412 1182202SW MLG DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347169 36005 CROSSTUBE CENTER PIVOT SUPPORT UNBONDED. 1G72 4U H4SW 20030618000882003061800088 2003 6 18 SWAA031301 420030609A256565C19901 CABLE BOEING737 7373H4 1384600NM EVAC SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030623000432003062300043WP 2003 6 23 GTIA030352 120030510A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND DENT AT FS 40 RIGHT FUSELAGE NOSE LANDING GEAR CUT OUT. FABRICATED INTERNAL DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20030702000532003070200053EU 2003 7 2 USAASA03050 120030524A3350321430 BATTERY AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19716UW 1055 THE EMERGENCY POWER SUPPLY UNIT IN THE OVERWING POSITION FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY PACK IN THE RIGHT OVERWING POSITION. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030721000062003072100006NM 2003 7 21 AUS20030562 120030610A324630038812 WHEEL BFGOODRICH 313061M BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE MLG DISINTEGRATED W K NONE O OTHER ININSP/MAINT 1 AUS 3442A447 (AUS) NR 3 MAIN WHEEL ASSEMBLY INBOARD HUB DISINTEGRATED IN AREA AROUND THE INBOARD BEARING HUB. BRAKE ASSEMBLY DAMAGED. 2L73 4F4 FRTA3WE E2EA 20030127000302003012700030 2003 1 27 HEEA083606 420030114A345713824120234 GPS BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 GPS RECEIVER BUTTONS NOT ENGAGING WHEN PUSHED IN. SENT TO SHOP FOR REPAIR. 1G71 3U H2SW 20030127000652003012700065 2003 1 27 HEEA083643 420030114A34225050031904 GYRO BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 DIRCTIONAL GYRO FLAG WOULD NOT RETRACT. REPAIRED. 1G71 3U O H2SW 20030127002052003012700205SW 2003 1 27 HEEA083697 120030115A7160206064213207 SCREEN BELL 407 407 1182206SW ENGINE INTAKE BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 ENGINE INTAKE SCREEN ASSY BROKEN. 1G71 3U O H2SW 20030128001802003012800180WP 2003 1 28 ZW0A0301001 120030121A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139403W 53139 DEPLETED BATTERIES IN EMERGENCY LIGHTING. REPLACED BATTERIES AND CHECKS MADE PER MM33-59-00. 2L72 4F RTA6WE 20030128002692003012800269EA 2003 1 28 COMA0360051 120030123A2750853D10018 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA R/H WING UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01443CA3129 7539 FLIGHT 5194 FLAPS FAIL MESSAGE DURING APPROACH.COULD NOT DUPLICATE; REPLACED ALL 4 R/H WING FLAP ACTUATORS FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20030129000572003012900057SW 2003 1 29 HEEA083970 120030117A6510407040302101 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03612PH 53199 TAIL ROTOR DRIVE SHAFT REPLACED DUE TO BLACK GREASE COMING FROM BEARING. 1G71 3U O H2SW 20030204000872003020400087NM 2003 2 4 SWAA030146 120030121A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND BS 639 FRAME CRACKED AT WL 208, LT AND RT SIDES. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030204002482003020400248NE 2003 2 4 VNAA0301012 320030111A6140 WARNING SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A PROP SPEED WARNING CAS MESSAGE AND ABORTED TAKEOFF. THE CREW THEN TAXIED OFF THE RUNWAY AND CALLED MAINTENANCE CONTROL. THE CREW WAS INSTRUCTED TO TRY AND DUPLICATE THE PROBLEM PERFORMING ENGINE RUNS BUT THE PROBLEM DID NOT REOCCUR AND NO OTHER DISCREPANCIES WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030210000802003021000080NM 2003 2 10 QXEA0300043 120030112A2120 SMOKE DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09367PH 511 SEA-ON FLIGHT NUMBER 2056, PASSENGER AND FLIGHT ATTENDANT REPORTED MOMENTARY BLUE HAZE IN CABIN, ALSO OILY FUMES, DURING DESCENT 14,000 TO 10,000. POWER LEVERS AT FLIGHT IDLE TO 30 PERCENT. CHECKED ENGINE OIL SERVICING, CHECKED NORMAL. GROUND RAN ENGINES AT VARIOUS POWER SETTINGS. NO BLUE HAZE OR OIL SMELL IN COCKPIT OR CABIN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030212000242003021200024WP 2003 2 12 AUS20030024 120030114A571151762561 SPAR CAP DOUG DC4 C54E 3021530WP RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT OUTER WING PANEL UPPER SPAR CAP CORRODED BETWEEN WS 585 AND WS 613. 2L74 4R A762 20030220001032003022000103EU 2003 2 20 QXEA0300097 120030111A5720 CHANNEL FOKKERF28 F28MK4000 4990810EU LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09497US 11173 PDX- LEFT HAND WING LOWER STATION 2230 RIB 'U' CHANNEL HAS EXFOLIATION CORROSION ON THE INTERIOR INBOARD RADIUS AT STRINGER 2.14 APPROXIMATELY .35 INCHES LONG. REPAIRED IAW FOKKER SRM 57-01-01. 2L72 4F RTA20EU 20030221000152003022100015NE 2003 2 21 QXEA0300129 220030128A72504124T3P03 TURBINE BLADES GE CF348C1 CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX GEE965281 10031 965281 PDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT 1 BLADES 2/3 MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION OF THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030224000132003022400013SW 2003 2 24 ALGA084139 120030220A6240407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH DEFECTIVE H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01582363 53069 NR AND NP ERRATIC. THE NR NEEDLE GOES TO ZERO ON GROUND RUN. REPLACED DUAL TACH INDICATOR. 1G71 3U O H2SW 20030116001732003011600173SO 2003 1 16 C2XA02SH168 120030103A532014529150001 CROSSBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV- DURING C-CHECK FLOORBOARD ANGLE CROSS BEAM JUST AFT OF FRAME 23 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-04-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030117000472003011700047SW 2003 1 17 HEEA083168 120030108A6320206033518007 STOP BELL 206 206L3 1182108SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 MAIN ROTOR GEARBOX STOP HAS A RUBBER BUMPER WORN OUT. 1G71 3U H2SW 20030117001732003011700173EA 2003 1 17 SWIA200311698 120030109A3020601970977 ANTI-ICE VALVE CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07411SW 7067 RIGHT COWL ANTI-ICE CAUTION MESSAGE WITH RIGHT COWL SWITCH IN THE ON POSITION AIRBORNE. RAN QRH PROCEDURE, NOT EFFECTIVE. RETURNED TO ELP. REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE IAW MM 30-22-01. OPS CHECK GOOD. S/N OFF: 2173. 2L72 4F RTA21EA 20030121001972003012100197SW 2003 1 21 HEEA083341 120030109A243230135002 BATTERY BELL 206 206B3 1181506SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032268V 3605 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030304001022003030400102 2003 3 4 HEEA084604 420030214A3442MI585200 TRANSCEIVER BELL 412 412 1182202SW WX RADAR SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 WEATHER RADAR RT INOPERATIVE. REPLACED F202 FUSE, REPAIRED, BENCH CHECK GOOD. 1G72 4U H4SW 20030305000812003030500081EU 2003 3 5 HEEA084664 120030213A2435150SG122Q STARTER GEN AEROSPAS355 AS355* EU ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH718 3248 AIRCRAFT WOULD NOT START, STARTER WOULD NOT TURN. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H11EU 20030225000392003022500039SW 2003 2 25 HEEA084258 120030120A3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW FLOAT BOTTLE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 163 53398 EMERGENCY FLOAT BOTTLE WILL NOT SERVICE UP FROM EMPTY. LEAKS PASS SEAT ON SOLENOID VALVE. 1G71 3U O H2SW 20030226000352003022600035SW 2003 2 26 HEEA084324 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 FUEL CELL PRESSURE SWITCH STICKING. 1G71 3U O H2SW 20030226000702003022600070SW 2003 2 26 HEEA084357 120030211A2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL QTY SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 SIGNAL COND UNIT INDICATING 100 LBS MORE ON FUEL GAUGE. 1G71 3U O H2SW 20030325000662003032500066NM 2003 3 25 AWXA200300229 120030217A551265C274941 SKIN BOEING737 7373S3 1384711NM HORIZONTAL STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-11 CHECK A 2 INCH CRACK WAS FOUND ON L/H HORIZONTAL STABILIZER LOWER SKIN AT FORWARD OF INBOARD BALANCE PANEL, APPROXIMATELY 1 1/2 INCHES FORWARD OF REAR SPAR. MAINTENANCE STOP DRILLED CRACK ON LT HORIZONTAL STABILIZER LOWER SKIN AT FORWARD OF INBOARD BALANCE PANEL; PERFORMED HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA E.R. 03-5513-03062-TB2A. 2L72 4F RTA16WE 20030313000682003031300068NM 2003 3 13 03FDEA00192 120030303A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION (C53-224-011) ON TOP OF UPPER LOBE FLOORBEAM AT BS 620, RBL 3, TO RBL 23. CORROSION AT BS 620, WL 208, RBL 3 TO RBL 23 DETERMINED TO BE OUT OF LIMITS IAW B727, SRM 53-10-1 FIG 4. REMOVED UPPER CHORD OF BEAM FROM LBL 32 TO RBL 36.5. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. ALL WORK ACCOMPLISHED IAW B727 SRM 53-10-1, 53-10-8, 51-10-2 & 51-20-4. 2L73 4F4 F A3WE E2EA 20030313000772003031300077EU 2003 3 13 132634 120030226A2751 WARNING SYSTEM SAAB SF340 SF340A 7850100EU COCKPIT ACTIVATED A UHLAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL17340SZ 340A004 DURING FLT 4476 TTN-BED WX CONDITIONS CLEAR AND RUNWAY DRY, THE FLAP CAUTION LIGHT ILLUMINATED IN FLIGHT. PILOT ALSO REPORTED THE FLAP POSITION NEEDLES ON INDICATOR WERE NOT SYNC'D AND HAD AN UNCOMMANDED MOVEMENT OF THE FLAPS. 2L72 4T RTA52EU 20030121003412003012100341NM 2003 1 21 HNAA0300003 120030117A272082700544001 CABLE DHAV DHC8 DHC8201 2809001NM LOOSE A HNAAO OTHER O OTHER CRCRUISE 1 EA07988HA1748317483 426 RUDDER OSCILATES BACK AND FORTH +/- 10 DEGREESE BELOW 160 KNOTS. NORMAL ABOVE 160 KNOTS. FOUND RUDDER CONTROLL CABLES AFT OF STATION YX396 AT HALF OF REQURIED TENSION. TIGHTENED CABLE TO PROPER TENSION AND PERFORMED RUDDER RIGGING. EVALUATION FLIGHT SATISFACTORY. 2H72 4T RTA13NM 20030318000642003031800064WP 2003 3 18 AALA20030187 120030210A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21491AA 49684 TUL - FOUND .25 INCH CRACK IN FUSELAGE SKIN AT RIVET HEAD. INSTALLED EXTERNAL DOUBLER PER SRM 53-01. (M) 2L72 4F A6WE 20030319000972003031900097NM 2003 3 19 TSAA0333013 120030124A33509221009 BATTERY PACK BOEING737 737230 1384401NM PAX CABIN DISCHARGED A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13821AL 23155 REPLACED LEFT AFT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030731000812003073100081NM 2003 7 31 QXEA200300797 120030619A7110 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - NR 2 LOWER COWL AFT CONE SUPPORT BRACKET CRACKED. REPAIED IAW RD 8/4-71-016 AND RD 8/4-71-053. 2H72 4T RTA13NM 20030801000092003080100009WP 2003 8 1 GTIA030530 120030612A5730 PANEL DOUG DC9 DC982 3022082WP LT WING DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND LEFT WING UPPER FORWARD TRAP PANEL PAINT CRACK THROUGH OUT TOP COAT AND VISABLE TO COMPOSITE MATERIAL. FOUND LEFT WING UPPER FORWARD TRAP PANEL DELAMINATED. REPAIRED TWO DELAMINATES ON LEFT WING UPPER TRAP PANEL. (M) 2L72 4F A6WE 20030326000942003032600094NM 2003 3 26 2003UALA00297 120030318A5320 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 STRINGER CLIP AT STRINGER 8R STATION 597 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP REPLACED. 2L72 4F4 FRTA16WE E2GL 20030325000242003032500024NM 2003 3 25 AWXA200300139 120030213A3310 LIGHT BOEING737 737277 1384570NM COCKPIT SHORTED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP28180AW 22647 SMOKE IN COCKPIT - FLT 0227 - DURING TAXI TO GATE IN PHX THE GLARE SHIELD FLUORESCENT LIGHTS BEGAN TO SMOKE, SHUT LIGHTS OFF SMOKE DISSIPATED. MAINTENANCE PERFORMED VISUAL INSPECTION OF ALL COCKPIT AND INSTRUMENT LIGHTING AND FOUND WIRE INSULATION BURNED, AND TOUCHING FLUORESCENT LIGHTS AT CENTER AND LEFT COCKPIT. TRIMMED INSULATION, AND REPOSITIONED WIRES AWAY FROM LAMPS. 2L72 4F RTA16WE 20030805000022003080500002NM 2003 8 5 ANCF200300016 120030528A3211NAS6404U50 BOLT DOUG MD80 MD83 3023681NM MLG BROKEN W ANCFO OTHER J WARNING INDICATION DEDESCENT 1 SO23583AN 53183 PILOT REPORT: DURING APPROACH WHEN LOWERING LANDING GEAR, IT SHOWS 3 GREEN LIGHTS BUT GEAR DOOR OPEN LIGHT REMAINS ON. ABNORMAL LIST WAS PERFORMED BUT LIGHT REMAINS ON. AIRCRAFT LANDED WITH LANDING GEAR DOORS OPEN. DURING INSPECTION ON GROUND WAS FOUND IN BOTH MAIN GEAR INBOARD DOOR BUMPERS SKID WORN AND LT MAIN GEAR INBOARD DOOR STRUCTURE OUTER SKIN WITH SEVERAL CRACKS. LT OUTER BOLT IN ROD-MAIN LANDING GEAR FOLLOW-UP SYSTEM DRIVE WAS FOUND BROKEN, IT WAS REPLACED IAW AMM 32-30-00. LT MAIN GEAR INBOARD DOOR STRUCTURE OUTER SKIN CRACKS WERE REPAIRED IAW SRM AND BUMPERS SKID WERE REPLACED IAW AMM. IT WAS PERFORMED EXTENSION AND RETRACTION TEST IAW AMM 32-30-00 PAG 201. IT WAS SATISFACTORY. 2L72 4F RT 20030722000702003072200070NM 2003 7 22 SWAA031459 120030701A335065C34691 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 15 ABC. SECURED BULLNOSE LIGHT PER MM. 2L72 4F RTA16WE 20030723000752003072300075NM 2003 7 23 AWXA200300792 120030617A53156553844 FLOORBEAM BOEING737 7373G7 138447JNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - MAJOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND AT 8 PLACES ON FLOOR SUPPORT IN AFT CARGO COMPARTMENT BS 773. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT BS 773; FABRICATED 5 EACH REPAIR ANGLES FROM 7075-0.071, AND 4 EACH REPAIR ANGLES FROM 7075-0.080; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-53 PG 106. 2L72 4F RTA16WE 20030722000252003072200025NM 2003 7 22 2003F00453 120030125A5553 FITTING BOEING727 727222 1384073NM VERTICAL STAB CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND VERTICAL STAB AT FIN STATION 316, HORIZONTAL STAB HINGE FITTING BEARING HOLE, LT SIDE, HAS CORROSION ON INSIDE DIAMETER. REWORK VERTICAL STAB, HORIZONTAL STAB HINGE FITTING BEARING HOLE AT LEFT SIDE AND INSTALLED NEW BEARING. (M) 2L73 4F A3WE 20030724000652003072400065NM 2003 7 24 AWXA200300774 120030701A575465C26686 SKIN BOEING737 7373G7 1384595NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-13 CHECK 19.5 INCH AREA OF THE NR 5 SLAT WAS FOUND DELAMINATED BETWEEN WS 234 AND WS 249. MAINTENANCE CUTOUT THE DAMAGED AREA OF NR 5 SLAT BETWEEN WS 234 AND WS 249; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR IAW B737-300 SRM 51-70-10 PG 22, FIG 31. 2L72 4F RTA16WE 20030826001292003082600129EU 2003 8 26 03FDEA00998 120030629A5320A53812906200 FITTING AIRBUS300 A300F4605R 3930327EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 MDIS 658 53-10 0006643 25JUN03 BFM CLOSE R FABRICATE NEW FITTING PER EA NR 6-5310-70963 AND INSTALL AFTER FABRICATION. 29JUN03 01:33 BFM R COMPLIED WITH FUSELAGE-MAINFRAME-MATERIAL SUB FOR FITTING P/N A538-12906-200 EA NR 6-5310-70963 AND FED-EX NON ROUTINE N00377_AT MAE CLOSED ON 06/29/2003. 2L72 4F RTA35EU 20030902001112003090200111NM 2003 9 2 NACA20030090 120030702A2611100064901 SMOKE DETECTOR BOEING727 727100 1384036NM FALSE INDICATIONA NACAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 AL03992AJ 19428 LOWER COMPARTMENT FIRE WARNING CAME ON DURING TAXI. REPLACED AFT BELLY FORWARD SMOKE DETECTOR. 2L73 4F RTA3WE 20030902001932003090200193NM 2003 9 2 PCAA0307082 120030712A2910DSC252C60200 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM LEAKING A PCAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA13839EX 226 CREW REPORTED LOSS OF NR 2 HYDRAULIC CONTENTS AFTER TAKE OFF. HYDRAULIC ISOLATION VALVE LIGHT ILLUMINATED. EMERGENCY WAS DECLARED, AND AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A HYDRAULIC FLEX LINE AT THE NOSE GEAR DRAG STRUT ACTUATOR. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030828001842003082800184NM 2003 8 28 CALA0300494 120030825A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT BS 947-986, LBL 48. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030728001222003072800122NE 2003 7 28 MTNA20033 220030708A7320500104118001 ACTUATOR FOKKERF27 F27MK500 4990629EU RROYCEDART DART5527R 54513NE FUEL SYSTEM STUCK A MTNAA UNSCHED LANDING O OTHER CLCLIMB 1 SO33726FE 3740 10683 AFTER TAKEOFF FROM MEM EN ROUTE TO MLU. THE FLIGHT CREW FOUND THE RIGHT FUEL TRIMMER WOULD NOT ADJUST. IT WAS STUCK AT 81 PERCENT. THE CREW DECLARED AN EMERGENCY DUE TO THE NEED TO MAKE A OVERWEIGHT LANDING. THE CREW LANDED THE AIRCRAFT WITH A SMOOTH LANDING WITHOUT INCIDENT IN MEM. MAINTENANCE PERFORMED A OVERWEIGHT LANDING INSPECTION IAW THE FOKKER MAINTENANCE MANUAL CH 05-50-02. NO PROBLEMS WERE FOUND ON THE INSPECTION. 2H72 4T4 T A817 E297 20030812000132003081200013GL 2003 8 12 HEEA088417 220030801A74219550175400 IGNITER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 IGNITER PRODUCING A SLOW START. TO BE SENT TO VENDOR. 1G72 3U3 U H1NE E1GL 20030813000312003081300031SW 2003 8 13 HEEA088575 120030729A6220 BEARING BELL 412 412 1182202SW PENDULUM ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L SC35 33006 PENDULUM ASSY HAS ROUGHNESS IN BEARINGS. SHOP REPAIR. 1G72 4U H4SW 20030814000392003081400039EU 2003 8 14 2003UALA00550 120030710A2611 SMOKE DETECTOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO BAY MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29418UA 485 FLIGHT DIVERTED DUE TO CARGO PIT SMOKE INDICATION. REPLACED FAILED SDCU (SMOKE DETECTOR CONTROL UNIT) 2L72 4F4 FRTA28NM E40NE 20030904001762003090400176WP 2003 9 4 AALA20030563 120030513A213121171803 CONTROLLER DOUG DC9 DC982 3022082WP CABIN PRESSURE FAILED A AALAG O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 SW21427AA 49339 BOS - FLT 1120 - EN ROUTE STL-BOS - DURING CLIMBOUT AT 29,500 FT, A LARGE POP WAS HEARD FOLLOWED BY THE CABIN PRESSURE RAPIDLY CLIMBING. THE STANDBY AND TRANSFER LOCK OUT LIGHTS WERE ILLUM ON THE PRESSURIZATION PNL. O2 MASKS WERE DEPLOYED WITH THE COCKPIT SWITCH AS THE CABIN RAPIDLY ROSE THROUGH 6,000 FT. CONTINUED TO BOS AT 10,000 FT AFTER PAX ACTIVATED THEIR O2. LANDED BOS WITHOUT INCIDENT. REPLACED NR2 PRESSURE CONTROLLER AND OUTFLOW VALVE ACTUATOR. ACCOM BITE OF BOTH PRESSURE CONTROLLRS BOTH PASSED. REPLACED ALL O2 GENERATORS EXCEPT ROWS 10 DEF THROUGHT 31 DEF. CREW O2 SERVICED TO FULL. A/C RELEASED FOR MX FERRY TO DFW FOR 02 GENERATOR REPLACEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030903002752003090300275SO 2003 9 3 C2XA03SH292 120030827A532014521721005 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 14 AND 17 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905001052003090500105SO 2003 9 5 C2XA03CL151 120030823A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2748901 145501 DURING ROUTINE MAINTENANCE THE AFT 3 EMERGENCY AISLE PATH LIGNT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED REAR INVERTER OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20030905002172003090500217SO 2003 9 5 C2XA03SH285 120030821A532014525422001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE LEFT HAND SILL AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030521000692003052100069WP 2003 5 21 MWEA030202 120030507A5754592253435 SKIN DOUG DC9 DC981 3022081WP LT WING SLAT DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LEFT WING SLAT NR 4 LEADING EDGE APPROXIMATELY STATION XOS 467-468 HAS TWO DENTS APPROXIMATELY 1 INCH APART. FABRICATED AND INSTALLED REPAIR PART, INSTALLED UPPER SKIN FILLER, FABRICATED AND INSTALLED SPLICE DOUBLER, REMOVED AND REPLACED FASTENERS AND NR 10 BUSHINGS. INSTALLED NR 4 SLAT AND ANTI-ICE DUCTS. PERFORMED ADJUSTMENT TEST. 2L72 4F A6WE 20030624000932003062400093NM 2003 6 24 DL764030467 120030516A2120 ODOR BOEING767 767424ER 1385270NM LAVATORY DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27838MH 29711 AFTER LANDING BURNING ODOR FROM 4 R LAV VENT. INSPECTED LAV AREA NO ODOR OR TROUBLE FOUND. 2L72 4F RTA1NM 20030714000652003071400065NM 2003 7 14 SWAA031367 120030618A5520BACB28AKMO7 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED C3 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER MM. 2L72 4F RTA16WE 20030716000262003071600026NM 2003 7 16 2003F00418 120030313A5320 STRINGER CLIP BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STAITON 540, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 540 STRINGER 5R. (M) 2L73 4F A3WE 20030716000632003071600063SO 2003 7 16 SIMA200316006 120030529A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21809AE 145521 DURING AN MBV INSPECTION, FOUND STRINGER 19L CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-24-01 FIGURE 201. (M) 2L72 4F RTT00011AT 20030630000772003063000077SW 2003 6 30 HEEA087839 120030609A5343400052007103 BEAM BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 MLG BEAM HAS CORROSION AT MOUNT BOLT IN EXCESS OF CLEAN UP LIMITS PER FAX FROM BELL. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030708000182003070800018NE 2003 7 8 03173702 220030622A72006089T11G01 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RIGHT FAILED A VTZAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA27702BR5099 7462 DURING CRUISE, CREW HEARD A LOUD NOISE AND THEN EXPERIENCED A SLIGHT YAW. ITT READINGS ON THE RT ENGINE ROSE TO OVER 900; CREW FOLLOWED QRH AND SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY IN. MANITENANCE PERSONNEL REMOVED AND REPLACED THE RT ENGINE. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030711001182003071100118WP 2003 7 11 MWEA030256 120030627A53475936594525 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 SPOTS OF LITE CORROSION ON MID-PIT RIGHT SIDE TIE DOWN RAIL FROM FRAME STATION 541 - 636. BLENDED CORROSION, REPLACED ENTIRE SECTION OF TIE DOWN RAIL, FABRICATED AND INSTALLED SPLICE. 2L72 4F A6WE 20030714000872003071400087NM 2003 7 14 SWAA031345 120030614A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR 8R AND STR 9R, BS 480 AND BS 847. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030204002682003020400268 2003 2 4 C2XA03CL025 420030203A34607014300901SWMOD CDU EMB 145 EMB145LR 3260212SO COCKPIT FAILED A C2XAK NONE J WARNING INDICATION CRCRUISE 1 SW2716911 145446 PHL FLIGHT#2062 THE CREW REPORTED #1 CDU/FMS FAILED IN FLIGHT.AFTER LANDING A STRONG BURNING/SMOKE ODOR IN COCKPIT AND CABIN WAS NOTICED.MAINTENANCE REPLACED THE #1 CDU AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030213000472003021300047GL 2003 2 13 CA030204017 220030202A720023001846 TUBE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE CONTAMINATED W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) THE AIRCRAFT WAS ON A TRAINING FLIGHT. NR 1 ENGINE WAS IN THE FLIGHT IDLE POSITION. WHEN IT WAS BROUGHT BACK TO THE FLY POSITION IT BEGAN TO SURGE ANYTIME THE ENGINE TORQUE WAS ABOVE 40 PERCENT. THE ENGINE WAS TRIMMED TO 40 PERCENT TORQUE AND RETURNED TO YVR WITHOUT FURTHER INCIDENT. THE FLARE ON THE TUBE WAS INSPECTED FOR CRACKS AND NONE WERE FOUND. THERE WAS A CARBON LIKE BUILD UP ON THE FITTING THE TUBE ATTACHES TO. WHEN CONNECTED TO SHOP AIR THE TUBE WAS FOUND TO BE LEAKING. WITH THE BUILD UP REMOVED THERE WAS NO LEAK. THE AIRCRAFT WAS GROUND RUN AND THEN TEST FLOWN AND ON FAULT FOUND AND SO RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20030218000342003021800034NM 2003 2 18 AWXA200300012 120030104A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28151AW 23219 FLIGHT CREW REPORTED THAT THE AFT RT EMERGENCY FLASHLIGHT DOES NOT HAVE FLASHING RED LIGHT. MAINTENANCE REMOVED AND REPLACED THE AFT RT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030218001822003021800182NM 2003 2 18 QXEA0300174 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 1 SEAT TRACK HAS SCRATCHES AT STATION 370-375. REPAIRED IAW RD 8-53-1342, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218001962003021800196NM 2003 2 18 SWAA030349 120030211A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT RADIUS OF EQUIPTMENT COOLING EXHAUST PORT, BS 378.5 AND LBL 2.8. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030219001332003021900133NM 2003 2 19 HALA0300009 120030111A2710E14931MOD3 CONTROL UNIT BOEING717 717200 1383700NM AILERON MALFUNCTIONED A HALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP13482HA 55127 OGG - EXPERIENCED AIRCRAFT CONTROL PROBLEMS IN ROLL AXIS PASSING 10,000 FEET QUICK 'JERK' AND AIRCRAFT MADE AN ABRUPT ROLL TO THE LEFT. SECURITY AND OPERATIONAL CHECKED FLIGHT CONTROL SYSTEM CHECK OK. REPLACED AILERON CONTROL UNIT PER MM. REPLACED TRIM PANEL PER MM TASK 27-11-01-720-801. (M) 2L72 4F TRA6WE 20030220000572003022000057WP 2003 2 20 ABXA030058 120030124A3231 ROLLER DOUG DC8 DC861 3021952WP MLG DOOR OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23849AX 45891 GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RT DOOR INDICATED NOT LATCHED ON FLIGHT ENGINEERS PANEL. CYCLED GEAR ONCE AND ALL CHECKED GOOD. SHIMMED RT MLG DOOR UPLATCH ROLLER IAW DC-8 MM 32-31-04. PULL CHECK OF RT MLG DOOR IAW DC-8 MM 32-31-04. PERFORMED GEAR SWING IAW DC-8 MM 32-60-0. NO DEFECTS NOTED. 2L74 4F 4A25 20030116001752003011600175SO 2003 1 16 C2XA02SH171 120030104A531313500400013 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715912 145439 SHV - DURING C-CHECK T REINFORCEMENT AT STRINGER 19L WAS FOUND CHAFFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030221000222003022100022NM 2003 2 21 QXEA0300130 120030128A2434 GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE MALFUNCTIONED A QXEAK NONE J WARNING INDICATION UKUNKNOWN 1 NM09345PH 476 SEA-ON FLIGHT NUMBER 2022 - NR 1 DC GENERATOR MASTER CAUTION CAME ON. RAN CHECKLIST, GENERATOR RESET FOR LESS THAN ONE MINUTE. TESTED NR 1 DC GENERATOR. OPERATED NR 1 DC GENERATOR WITH LOTS OF DC CONSUMERS. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030224000342003022400034NE 2003 2 24 HEEA084155 120030211A75007650007903102 SHUTOFF VALVE SKRSKYS76 S76A 8143006NE BLEED AIR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 BLEED AIR SHUTOFF VALVE INOPERATIVE. 1G72 3U H1NE 20030226000242003022600024EA 2003 2 26 03057654 120030226A33502013A BATTERY CNDAIRCL600 CL6002B19 1900309EA UNSERVICEABLE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27645BR 7383 Interior emergency light inoperative. Maintenance personnel removed and replaced battery pack. Operational check good. Aircraft released for continued service. 2L72 4F RTA21EA 20030226000612003022600061WP 2003 2 26 MWEA030112 120030225A326051319 THROTTLE SWITCH DOUG DC9 DC932 3022066WP DEFECTIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31401ME 47133 GEAR WARNING HORN SOUNDED. -- REMOVED AND REPLACED ON SWITCH UNIT AND INSTALLED LEFT THROTTLE SWITCH. 2L72 4F A6WE 20030227001302003022700130SW 2003 2 27 HEEA084436 120030213A6710206010470101 BEARING BELL 206 206L1 1182107SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0327766 RE1715 45312 CYCLIC CONTROL BELLCRANK HAS PLAY IN THE PIVOT BEARING. REPLACED BEARING DUE TO BEING WORN. REPAIRED. 1G71 3U H2SW 20030304000932003030400093NM 2003 3 4 DL76L030175 120030222A5610141T480014 WINDOW BOEING767 767332 1382001NM COCKPIT DAMAGED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27182DN TX2762R 25987 AT CRUISE AND NEAR MSP, CREW SMELLED AN ELECTRICAL ODOR. WENT TO STBY ON EQPT COOLING AND SHUTTING OFF GASPER AND RECIRC FANS. SMELL STARTED TO GO AWAY AND THEN CAME BACK FORA SPLIT SECOND AND THEN WENT AWAY AGAIN. SEEMED TO COME OUT FROM THE VENTS. MADE A PRECAUTIONARY LANDING INTO MSP. MTC IN PROGRESS REPLACING R1 WINDOW DUE TO TERMINAL BLOCK ATBOTTOM FOUND LOOSE AND ARCING. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030307000972003030700097NE 2003 3 7 HEEA084898 120030227A32127625101101105 FLOAT SKRSKYS76 S76A 8143006NE NLG FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 NLG EMERGENCY FLOAT DOES NOT HOLD PRESSURE. 1G72 3U H1NE 20030311001062003031100106WP 2003 3 11 MWEA030130 120030307A3030851AH PITOT TUBE DOUG DC9 DC981 3022081WP COCKPIT DEFECTIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31805ME 48031 FIRST OFFICER'S PITOT STALL HEAT OFF ANNUNCIATOR ON AND NO AMP DRAW, ICE BULIKING UP ON PITOT TUBE. -- REMOVED AND REPLACED PITOT TUBE. 2L72 4F A6WE 20030121000192003012100019NM 2003 1 21 SWAA030062 120030110A575465C26602 SLAT BOEING737 7373Y0 1384671NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED BC3 CHECK, FOUND NR 5 L/E SLAT CRACKED AT RIVETS ON LOWER SURFACE. REPAIRED SLAT PER SWA EA. 2L72 4F RTA16WE 20030314002142003031400214NM 2003 3 14 03010 120030309A7100 ENGINE BOEING747 7472B4B 138481BNM PWA JT9 JT9D7J 52054NE NR 3 VIBRATION A KCSAJC DUMP FUEL ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL23713CK 21099 689470 DURING T/O ROLL NR 3 ENGINE HAD VIBRATION AND LOUD NOISE. AIRBORNE VISUAL INSPECTION REVEALED DAMAGE TO ENGINE. DUMPED FUEL AND RETURNED TO BASE. 2L74 4F4 FRTA20WE E20EA 20030314002042003031400204 2003 3 14 0300396308 420030303A2330 CONTROL BOX BOEING747 747451 1384940NM SEAT 79A SHORTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01668US 24223 ENROUTE TO HNL AN OVERHEATED PLASTIC ODOR WAS DETECTED ABOUT 45 MINUTES BEFORE SEAT 79AB PVS FAILED. REPLACED UEB, SEB AND CONSOLE. 2L74 4F RTA20WE 20030317001052003031700105NM 2003 3 17 03FDEA00265 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 25R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030320000572003032000057NM 2003 3 20 USAASB03028 120030217A3260189929 CIRCUIT CARD BOEING737 7373B7 1384580NM RT MLG FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19390US 23312 ATL - FLT 520 - AFTER TAKEOFF FROM ATL, EN ROUTE TO PIT, CREW REPORTED THE RIGHT MLG RED LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE OFF PAND UP POSITION. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR AND CONNECTOR PLUG PINS ALSO, REMOVED AND REPLACED THE RT MAIN LANDING GEAR UP AND LOCK LOGIC CARD M982 AS PRECAUTIONARY. SYSTEM OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030825001222003082500122EU 2003 8 25 AWXA200300811 120030719A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28665AW30665308 1644 LAS - EEL - DURING EMERGENCY LIGHT TEST THE SYSTEM INDICATED OK, BUT FAILED TO ILLUMINATE THE EMERGENCY ESCAPE PATH LIGHTS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL TEST WAS GOOD IAW AMM 33-51-00. 2L72 4F4 FRTA28NM E311NE 20030730000412003073000041WP 2003 7 30 ABXA030284 120030715A3260 PIN DOUG DC9 DC941 302207NWP LANDING GEAR BENT A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23951AX 47616 AFTER TAKEOFF, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER INITIAL RETRACTION. THERE WAS NO ASSOCIATED YAW OR NOISE. AFTER RECYCLING GEAR, ALL INDICATIONS WERE NROMAL. FOUND PIN A BENT ON R5-1150. STRAIGHTENED PIN. OPS CHECKED GOOD IAW DC-9 AMM 32-60-00. 2L72 4F A6WE 20030827000382003082700038CE 2003 8 27 51492 120030610A2612 CONNECTOR BEECH 1900 1900D 1154162CE ENGINE LOOSE A AMWAA UNSCHED LANDING O OTHER CRCRUISE 1 CE07138YV UE138 THE AIRCRAFT WAS RUNNING A FIRE LOOP TEST. DURING FLIGHT, THE LEFT FIRE LOOP FAILED THE TEST. THE AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE TIGHTENED THE CANNON PLUG ON AFT FIREWALL. THEN, MAINTENANCE SYSTEM CHECKED IT AND IT WAS FINE. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030910001782003091000178EU 2003 9 10 SIMA200322305 120030801A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21375AE 340B375 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSIATED THE APPLICATION OF A REPAIR DOUBLER TO THE UPPER FUSELAGE SKIN 2.1 INCHES AFT OF FRAME STATION 560 AND BETWEEN STRINGERS 1503 AND 1504. REMOVED DENT BY CREATING A CUTOUT. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB STATEMENT 340SDS005824 PARA 1.3.4 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20030911001372003091100137WP 2003 9 11 DHL2003873595 120030704A53204612650 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FWD ACCY COMPT FITTING CORRODED AT STA 8.000 - 16.000, L33L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED FITTING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8. INSTALLED NEW FITTING IN FWD ACCY COMPT, STA 8.000 - 16.000, L33L IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-3-1 PG 4. 2L74 4F RT4A25 20030912001642003091200164NM 2003 9 12 AWXA200300916 120030812A261310621871 ACCESSORY UNIT BOEING737 7373G7 1384595NM OVERHEAT SYS MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28309AW12257 24711 PHX - AIR TURN BACK - FLT 0297 - ON CLIMB OUT OF PHX EN ROUTE FOR SJC THE RT WING TO BODY OVERHEAT LIGHT ILLUMINATED. TURNED BACK TO PHX, LIGHT REMAINED ILLUMINATED UNTIL AFTER LANDING. MAINTENANCE PERFORMED ENGINE RUN AT CLIMB POWER, FENWAL DIGITAL BOX 44 OVERHEAT CONDITION (AFT BAG PIT AREA) WAS DUPLICATED WITHIN 3 MINUTES OF RUN. REMOVED AND REPLACED COMPARTMENT OVERHEAT ACCESSORY UNIT IAW BMM 26-10-02, PG. 401. REACCOMPLISHED ENGINE RUN AT CLIMB POWER FOR 10 MINUTES, NO FAULTS NOTED. SDR WILL BE SUBMITTED UPON RECEIPT OF VENDOR TEARDOWN REPORT. 2L72 4F RTA16WE 20030929000882003092900088NM 2003 9 29 UPS03241168 120030812A2910 SHUTOFF VALVE BOEING727 72725C 138400HNM NR 2 ENGINE DEFECTIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 INSPECTION TYPE: C, DURING TEST OF ENG NR 2 HYD SHUTOFF VALVE FAILED TO OPERATE CORRECTLY. TROUBLESHOOTING CARRIED OUT IAW WDM 29-11-01 AND ENG NR 2, SYS A HYD SHUT OFF VALVE FOUND TO BE DEFECTIVE. INSTALLED REPLACEMENT HYD SHUT OFF VALVE IAW MM 29-11-21 REF NRC 681341 FOR CANNON PLUG INST & TEST. LEAK CHECK CARRIED OUT IAW MM 29-11-21 STEP 5. NO LEAKS FOUND AND REMAINING STEPS COMPLETED IAW MM 29-11-21. 2L73 4F A3WE 20030930000612003093000061 2003 9 30 P5CA0300935 420030902A34131QF2364A CONNECTOR BOEING747 747200 1384847NM COCKPIT FAILED A P5CAD RETURN TO BLOCK I FLT. ATTITUDE INST. TXTAXI/GRND HDL 1 WP23524UP 21446 ON PUSH BACK, CAPT'S ALT FAILED TO STAND - BY WOULD NOT RESET. REMOVED AND REPLACED, CAPT'S ALT NR 1 CADC, STATIC CONNECTOR TO CAPT'S ALT AND LEAK CKD IAW MM 34-13-04, 34-12-01, 34-11-00 2L74 4F RTA20WE 20031001000962003100100096NE 2003 10 1 AMTA200301127 220030903A7200 ENGINE LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE NR 2 VIBRATION A AMTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL11163AT 1229 NR 2 ENGINE INDICATES HIGH VIBS ON BOTH CHANNELS, VIBS ARE LOW SIDE AND FOLLOW THE THROTTLES. ENGINE VIBE ON TAKEOFF WERE 2.3 ON B-CHANNEL AND 2.4 ON A-CHANNEL. DURING CLIMB, VIBE DECREASED TO APPROX 1.5 BOTH CHANNEL. PERFORMED TRIM BALANCE PER M11-72-52. OK FOR SERVICE. AVM SURVEY NORMAL. TRIM RUN .6 LOW. (M) 2L73 4F4 F A23WE A12EU 20031001000022003100100002NM 2003 10 1 0301726313 120030908A3350 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01673US 30268 DURING LINE CHECK, FOUND ZONE (D) RT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED ELECTRICAL PLUGS AT 52JHK. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031002000292003100200029EU 2003 10 2 A6WA200360038 120030910A5753 STRUCTURE BAC 146 146200A 1500266EU LT WING TE FLAP DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 DAMAGED BUSHING BORES AT LT WING FLAP STRUCTURE AT TRACK 2. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060005. (M) 2H74 4F A49EU 20031002001462003100200146NM 2003 10 2 03FDEA01471 120030909A5710 RIB BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CRACK INDICATION NOTED AT BS 760 WL 208 RBL 70.5 IN THE FWD UPPER HOLE COMMON TO THE RIB CHORD UPPER VERTICAL FLANGE IN THE RIB CHORD LAYER AT THE 12 O'CLOCK POSITION. REPAIRED PER EA 7-5710-54691 AND EO 7-5710-7-2308 I PT 3. 2L73 4F RTA3WE 20031001000542003100100054NM 2003 10 1 CALA0300569 120030930A5320 ANGLE BOEING737 737524 1384721NM R-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716647 28908 INSPECTION FOUND UPPER SURFACE OF R-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031007001102003100700110EA 2003 10 7 03242679 120030830A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 DURING MAINTENANCE INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OVERWING EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031008000402003100800040NM 2003 10 8 VNAA0309003 120030905A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07423JS183361028 3032 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 TO 7 WERE INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030122002082003012200208SW 2003 1 22 HEEA083553 120030113A771232447066 CONTROL UNIT BELL 412 412 1182202SW TORQUE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 NR 2 ENGINE TORQUE WENT 30 PERCENT LOW, N2 AND ITT ALSO DECREASED. MAINTENANCE REPLACED TORQUE CONTROL UNIT. 1G72 4U H4SW 20030327001582003032700158SO 2003 3 27 C2XA03SH004 120030218A531514522460013 BUTT STRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK, BUTTSTRAP ON THE CENTER FLOORBEAM BETWEEN FRAMES 18 TO 23 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030303001342003030300134SW 2003 3 3 HEEA084558 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T10414 33112 MAIN ROTOR BLADE UPPER AFT FRETTING PAD UNBONDED AND UPPER SKIN HAS AREA AROUND PREVIOUS REPAIR CRACKED. 1G72 4U H4SW 20030418001082003041800108NM 2003 4 18 F3LA200300065 120030218A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA 344, LBL 60 - RBL 14. REMOVED DAMAGE ON WEB BETWEEN STA 332 AND STA 344 AFT OF R-1 DOOR PER SRM 51-40-2, PAGES 1-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-02, PAGES 1-3, AND SOPM 20-41-02. 2L72 4U RTA16WE 20040224000722004022400072WP 2004 2 24 GKZR200479902 120031104A53435750092506 SUPPORT FITTING DOUG DC8 DC862 3021970WP MLG CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11799AL 45922 RIGHT MLG SUPPORT FITTING CRACKED AT TOP ATTACH POINT. REMOVED AND REPLACED RIGHT MLG SUPPORT FITTING (TRAP) IAW DC-8 SRM 51-1-20 & 51-1-21. BORED RIGHT MLG SUPPORT FITTING PER DOUGLAS BLUE PRINT 5611440. 2L74 4F 4A25 20030828000432003082800043NM 2003 8 28 XNOA01130 120030529A3232 ACTUATOR BOEING727 727227 1384078NM RT MLG DOOR MALFUNCTIONED A XN0AO OTHER J WARNING INDICATION CLCLIMB 1 GL23793A 20774 AFTER T/O KBWI, WHEN GEAR HANDLE PLACED TO OFF POSITION RED DOOR LIGHT ILLUMINATED ALONG WITH ASSOC AMBER R GEAR DOOR LIGHT ON F/E PANEL. ENA ABNORMAL CHECKLIST PERFORMED. RED DOOR LIGHT EXTINGUISHED. REMOVED AND REPLACED RT MLG DOOR ACTUATOR PER B727 MM 32-32-81. OPS CHECK, LEAK CHECK NORMAL PER B727 MM 32-32-00. CHECKS GOOD ON GROUND. 2L73 4F A3WE 20030723001032003072300103NM 2003 7 23 DL733030498 120030529A5753 SPAR BOEING737 737347 1384647NM LT WING TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312WA 23598 NR 2 INBOARD MID FLAP FRONT SPAR ASSEMBLY WAS FOUND DAMAGED. A REPLACEMENT WEB SECTION AND SPLICE DOUBLER WAS INSTALLED PER ER/A 423065-14. 2L72 4F RTA16WE 20030724000022003072400002NM 2003 7 24 DLM88030518 120030605A32405952247503 DEFLECTOR DOUG MD88 MD88 3023688NM NLG WORN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27930DL 49717 NOSE GEAR WOULD NOT RETRACT AFTER T/O. REPLACED LT NOSE LANDING GEAR SPRAY DEFLECTOR. 2L72 4F RTA6WE 20030724000862003072400086NM 2003 7 24 SWAA031428 120030626A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, ABOVE STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030903000202003090300020NM 2003 9 3 03FDEA01094 120030711A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 CORROSION ON FLOOR SUPPORT BS 344, LBL 45, WL 208. CORROSION ON FLOORBEAM BS 344, LBL 45, WL 208. REPAIRED FLOORBEAM IAW SRM 53-10- 1, 51-10-1, 51-30-2 & 53-10-8. 2L73 4F4 FRTA3WE E2EA 20030903002442003090300244EA 2003 9 3 03236638 120030824A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27638BR 7311 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING IN ROWS 2-5 WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE ROW 2-5 EMERGENCY ESCAPE PATH LIGHTING STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030904001052003090400105NM 2003 9 4 QXEA200301043 120030820A5720 BRACKET DHAV DHC8 DHC8202 2809007NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- RIGHT HAND UPPER BRACKET AT RIGHT HAND WING STATION YW139.00 IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20030813001302003081300130WP 2003 8 13 AALA20030710 120030702A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21491AA 49684 DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. REPLACED AFT EMERGENCY EXIT LIGHT SOCKET AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030724000012003072400001NM 2003 7 24 DL73K030517 120030604A5330 SKIN BOEING737 737232 1384475NM KEELBEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 FS 661 - 727, KEEL BEAM SKIN PANEL FABRICATION: DURING INSPECTIONS PER EO 3-58542-3, THE SUBJECT PANEL WAS FOUND CRACKED. BAC SB 737-53-1104 PROVIDES REPAIR INSTRUCTIONS TO REFABRICATE THE PANEL, HOWEVER ER/A 385214-14 WAS ISSUED TO CUT AN ACCESS HOLE IN THE MOUNTING COVER BETWEEN THE HYDRAULIC PUMP AND RESERVOIR IN ORDER TO INSTALL SOLID FASTENERS IN ALL SKIN PANEL LOCATIONS. 2L72 4F RTA16WE 20030911001082003091100108NM 2003 9 11 03FDEA01179 120030728A5512ALC8103502 SKIN DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RH HOR STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 27 RIGHT HAND SIDE. 2L73 4F4 FRTA22WE E13NE 20030910000742003091000074EU 2003 9 10 DHL2003366004 120030803A5250 DOOR AIRBUS300 A300B4203 3930306EU COCKPIT MALFUNCTIONED A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01366DH 249 THE COCKPIT DOOR DOES NOT GO INTO THE LOCKED POSITION. PERFORMED FUNCTIONAL TEST OF COCKPIT DOOR AS PER NASI M/M 52-10-00 PAGE 603. DOOR OPS NORMAL. 2L72 4F RTA35EU 20030930000992003093000099NM 2003 9 30 QXEA200301110 120030907A521085210276101 BUSHING DHAV DHC8 DHC8202 2809007NM ZONE 800 MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09346PH 477 ON FLIGHT 2122 MAIN CABIN DOOR ONLY OPENS HALFWAY. REMOVED AND REPLACED THREADED STRUT BUSHING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030930000982003093000098NM 2003 9 30 QXEA200301109 120030904A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 FAILED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09411QX 4055 AFT AIRSTAIRS WILL NOT DEPLOY. TESTED POST MOD AIRSTAIR ASSEMBLY, TESTS GOOD. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031002000702003100200070SO 2003 10 2 C2XA03TY147 120030910A532014524131005 BRACKET EMB 135 EMB135ER 3260203SO THRESHOLD CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULE INSPECTION THE MAIN PASSENGER DOOR THRESHOLD BRACKETS WERE FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD BRACKETS IAW EMB SRM 51-40/02, 51-30-02 AND CPM 51-21-04,05 AND 06. THE REPAIR WAS FOUND TO SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031001001152003100100115NM 2003 10 1 USAA030188 120030907A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US50934 22959 FOUND SKIN CRACKED 1.5 INCHES, LT FUSELAGE STRINGER 22L AT STATION 727E. INSTALLED DOUBLER PER SRM 51-00-01. (M) 2L72 4F RTA16WE 20030909001272003090900127NE 2003 9 9 MALA030349 220030724A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT MALFUNCTIONED A MALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL15451XJ 340B451 INFLIGHT ON 2726, CREW REPORTED LT ENGINE CWP OIL PSI WENT TO 30 PSI. LIGHT ILLUMINATED. OBSERVED OIL PRESSURE (LT ENGINE ZERO, BELOW 30 PSI). RAN QRH- SHUTDOWN LT ENGINE. REST OF FLIGHT UNEVENTFUL/NO UNUSUAL ENGINE OPERATION ISSUES OBSERVED. MAINTENANCE TRANSFERRED TO 409 CARD NR 181763 LT ENGINE WAS REPLACED WITH SERVICEABLE ENGINE. REF WORK PACKAGE DATED 7/24/03 FOR COMPLETE DETAILS LT ENGINE IS SERVICEABLE. SHUTDOWN ENGINE. 2L72 4T4 TRTA52EU E8NE 20031002001602003100200160 2003 10 2 SWIA200312380 420030906A22106229945003 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07464SW 7827 AUTOPILOT FAILED INFLIGHT WITH YD2 FD2 STATUS MESSAGES DISPLAYED ON ED2. QRH PROC'S FOLLOWED, BUT NO HELP. RETURNED TO DFW. REMOVED AND REPLACED IAPS 2A POWER SUPPLY IAW CL600 MM 22-12-02. OPS CHECKS GOOD. 2L72 4F RTA21EA 20031020000502003102000050EU 2003 10 20 RAIA00310257 120031008A5270 SWITCH JETAIRJETSTMJETSTM4101 1500501EU REFUEL DOOR OUT OF ADJUST A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03569HK 41088 5476-STL- REFUEL DOOR OPEN WARNING INDICATION. MAINTENANCE ADJUSTED FUEL DOOR WARNING MICRO SWITCH. 2L72 4T RTA41NM 20031020001112003102000111EA 2003 10 20 03274689 120031001A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA LAVATORY DETECTED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA27689BR 7737 DURING APPROACH CREW NOTED A SULFUR ODOR IN COCKPIT & CABIN. F/A NOTED THE PRESENCE OF SMOKE IN LAVATORY AND USED HALON EXTINGUISHER TO REMEMDY SITUATION. EMERGENCY WAS NOT DECLARED, FLT LANDED WITHOUT INCIDENT. FIRE EXTINGUISHER WAS REPLACED AND AIRCRAFT RELEASED FOR CONTINUED SERVICE. AN OPERATIONAL CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM HAS BEEN REQUESTED TO ENSURE PROPER OPERATION OF SMOKE DECTECTION SYSTEM AS A PRECAUTIONATY MEASURE. MAINTENANCE PERSONNEL PERFORMED A SATISFACTORY OPERATIONAL CHECK OF LAV SMOKE AND FIRE DETECTION SYSTEM WITH NO DEFECTS NOTED. IT HAS BEEN NOTED A PASSENGER WAS POSSIBLY SMOKING IN THE LAVATORY. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031020003102003102000310NM 2003 10 20 2003UALA00701 120030919A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29180UA 25224 STA 2090 STRINGER 34R, VENT FOR LAV TANKS HAS CORROSION COMMON TO INTERIOR SKIN. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED. 2L74 4F4 FRTA20WE E24NE 20031021002422003102100242SO 2003 10 21 C2XA03SH338 120030921A532014521725013 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE RT SILL AT FRAME 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031027001192003102700119EU 2003 10 27 PA03003AA 120030120A5522S25TE4136 SKIN BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP RT ELEVATOR CORRODED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL2348FB DHB259 257129 WHILE PERFORMING INSPECTION ON THE ELEVATORS, FOUND CORROSION ON HT UPPER AND THE LOWER LEADING EDGE SKIN SURFACES OF THE RT ELEVATOR. THE CORROSION WAS CONCENTRATED WHERE THE SKIN IS FASTENED TO THE ELEVATOR FRONT BEAM. AFTER REMOVING THE CORROSION AND BLENDING THE AREA FOUND THAT TWO SIGNIFICANT AREAS WHERE THE CORROSION WENT BEYOND THE LIMITS OF THE SRM. 2L72 4F4 F A3EU E6WE 20031028000442003102800044SO 2003 10 28 SWIA200312457 120030923A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07567SW7754 7754 120342 FORWARD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PACK IAW EMB MM 33-50-02. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031028000802003102800080NM 2003 10 28 2003UALA00745 120031005A2751 SWITCH BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FLAP PROXIMITY FAILED A UALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP29341UA 24245 UNABLE TO SELECT NOSE DOWN ELEVATOR TRIM FROM BOTH YOKES. MAINTENANCE TECHNICIANS DUPLICATED THE PROBLEM ON GROUND. THE PROBLEM WAS TRACED TO A FAULTY FLAPS UP SWITCH (S245). THE SWITCH WAS REPLACED. OPERATIONAL CHECKS WERE PERFORMED SATISFACTORILY. 2L72 4F4 FRTA16WE E2GL 20031028001182003102800118NM 2003 10 28 AALA20030991 120030911A3350P4010049 BATTERY BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21632AA 24590 DFW - TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 9D THROUGH 14D. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924000052003092400005NM 2003 9 24 03FDEA01384 120030825A36101897403 PRECOOLER DOUG MD11 MD11 3023602NM BLEED AIR FAILED A FDEAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SO25578FE4824 4824 48458 MOMENTARY INDICATION OF NR 2 BLEED MANF FAILURE. (RED LIGHT ON OVERHEAD AND RED LINE ON NR 2 BLEED MANF SYNOPTIC). ASC DEPRESSURIZED NR 2 MANF. QRH PROCEDURES ACCOMPLISHED. PHONE PATCH W/MEM GOC ADVISED TO CONTINUE TO NANDI. PERFORMED DECAY CHECK AND DECAY CHECK FAILED PER JRH. OPENED ENGINE PER MM REF 71-10-00-2 AND INSPECTED FOR BLOWN DUCTS AND LEAKS. NO DISCREPANCIES NOTED. PER MFC FAULT OPENED PRECOOLER AREA AND FOUND PRECOOLER LEAKING. REMOVED AND REPLACED PRECOOLER PER MM REF 36-13-01-2-2.OPS AND LEAK CHECK GOOD. PERFORMED DECAY CHECK AGAIN PER JRH AND DECAY PASSED.CLOSED ENG & PATIO PER MM REF 71-10-00-2-1. DUE TO AIR TURN BACK. 2L73 4F RTA22WE 20040128000352004012800035SO 2004 1 28 C2XA03CL215 120031228A2560P4010030 BATTERY EMB 145 EMB145 3260210SO FLASHLIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713969 145141 DURING ROUTINE MAINTENANCE THE CAPTAINS EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040128001042004012800104SO 2004 1 28 SWIA200312698 120031212A5713 STRINGER EMB 120 EMB120ER 3260203SO WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07207SW 120266 STRINGER NR 8 AT RIB 5 CRACKED. DISCOVERED DURING A CHECK INSPECTION. REPAIRED STRINGER IAW EMB SRM 57-20-03 AND GST 3176/02. 2L72 4T RTA31SO 20040206000332004020600033SO 2004 2 6 SIMA200334407 120031115A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE 145301 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL AS FOUND CORRODED BELOW SRM LIMITS. CUT OUT CORRODED SECTION OF THE FORWARD DIGITAL. MADE REPLACEMENT STRAP, FABRICATED SHIM, TWO DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 23, CHAPTER 53-21-10 FIGURE 203. (M) 2L72 4F RTT00011AT 20040206000572004020600057WP 2004 2 6 ASAA0380673 120031026A5230591014167 FLANGE DOUG DC9 DC982 3022082WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND AFT CARGO BAY DOOR IS CHAFED ON FLANGE AT AFT STOPS. INSTALLED DOUBLER PER EA 5230-01205. (M) 2L72 4F A6WE 20031210001982003121000198NM 2003 12 10 03FDEA01875 120031105A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 N01453 CORROSION WHILE WORKING N01449 FOUND CORROSION ON TOP SURFACE OF UPPER CHORD OF FLOORBEAM BS 1070, RBL 23, WL 208 ** SD ** COMING 2L73 4F RTA3WE 20040309001562004030900156WP 2004 3 9 GTIA031058 120031113A2752 FITTING DOUG DC9 DC981 3022081WP T/E FLAP CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND LEFT WING INBOARD FLAP INBOARD STRUCTURE FLAP ACTUATOR FITTING CRACKED. LOCATED AND DRILLED LEFT WING INBOARD FLAP ACTUATOR FITTING. INSTALLED LEFT WING INBOARD ACTUATOR FITTING. (M) 2L72 4F A6WE 20030926000242003092600024NE 2003 9 26 AWXA200300970 220030821A7200 ENGINE AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 2 MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28814AW 1281 ON TAKEOFF ROLL AT ORD EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE INSPECTED ENGINE INLET AREA, NO DAMAGE NOTED. PERFORMED FULL AUTHORITY DIGITAL ENGINE CONTROL TEST ON THE NR 2 ENGINE PER TSM 75-30-00-810-846, ALL TESTS WERE GOOD. PERFORMED HIGH POWER ASSURANCE TEST IAW AMM 71-00-00-710-013-A, ALL ENGINE PARAMETERS ARE WITHIN LIMITS, NO FAULTS OR WANINGS ON PFR OR ECAM. COULD NOT DUPLICATE PROBLEM. 2L72 4F4 FRTA28NM E40NE 20060801001142006080100114WP 2006 8 1 IXXA060564S 120030924A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND INTERCOSTAL CORRODED BETWEEN STATION 980, AND 1000 AT LONGERON 35 RIGHT. REMOVED CORROSION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, 51-30-30, 53-2-0, AND DOUGLAS DRAWING 5779959. 2L74 4F RT4A25 20030617000302003061700030NE 2003 6 17 CA030528008 220030512A73233240070 LEVER PWA JT15 JT15D4 52112NE GOVERNOR SEPARATED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) OPERATOR REPORTED LOST OF POWER TO SUB-IDLE IN FLT. DURING DISMANTLING OF THEFCU (FUEL CONTROL UNIT), THE GOVERNOR LEVER ASSEMBLY P/N 3240070 WAS FOUND WITH THE WEIGHT SEPARATED FROM THE LEVER. THE LEVER SHOWED SINGS OF HEAVY PIT CORROSION, WHICH HAD BEEN REMOVED. AS PER THE ATTACHED REPORT, THE MOST PROBABLE CAUSE IS THE ASSEMBLY WAS PASSIVATED IN NITRIC ACID TO PREVENT RUSTING IN THE FUTURE. WHAT THE REPAIR SHOP DID NOT KNOW WAS THAT THE TUNGSTEN CARBIDE WEI GHT IS BRAZED ONTO THE LEVER WITH A SILVER ALLOW WHICH IS SOLUBLE IN NITRIC ACID. IT WAS ONLY A MATTER OF TIME BEFORE THE WEIGHT AND LEVER WOULD COME APART. 4 F E1NE 20030813001232003081300123NM 2003 8 13 USAA030119 120030717A5315 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND FLOORBEAM CRACKED APPROX 1 INCH, BS 328 RBL 10.0. DOUBLER INSTALLED PER EA 76205. (M) 2L72 4F RTA16WE 20030820002462003082000246NM 2003 8 20 USAASB03111 120030715A3210 LANDING GEAR BOEING737 7374B7 1384702NM MALFUNCTIONED A USAAL ABORTED APPROACH O OTHER APAPPROACH 1 EA19444US 24862 ON APPROACH INTO EWR, FROM PIT, CREW EN COUNTERED A MALFUNCTIONING LEFT MAIN LANDING GEAR INDICATION LIGHT. CREW EXECUTED A GO-AROUND, RECYCLED THE LANDING GEAR AND WAS ABLE TO GET THE INDICATION LIGHT WORKING DURING A HOLD NEAR THE FIELD. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. AN EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED LANDING GEAR LIGHTS TEST AND PUSHED-TO-TEST. INSPECTED LANDING GEAR PROXIMITY SWITCHES. ALL CHECKS NORMAL. (M) 2L72 4F RTA16WE 20030401000782003040100078NM 2003 4 1 DHL2003741504 120030323A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C CHECK, FUSELAGE INTERIOR BS 480 AND LWR SILL BEAM. ( CARGO DOOR) FRAME ATTACH TO FUSELAGE CRACKED FWD. AND AFT. ALSO MISSING (8 EACH). 2L73 4F RTA3WE 20030408000172003040800017WP 2003 4 8 ASAA0380104 120030124A3350 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01965AS 53079 SJC - PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN FIRST CLASS WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030410000732003041000073WP 2003 4 10 GTIA030102 120030210A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND MAIN CABIN FS 1297 STRINGER 18R WEB CRACKED. STOP DRILLED CRACKS, TWO. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20030415000302003041500030SO 2003 4 15 CA030318005 220030311A8530655238 BOSS BEECH 58 58 1152740CE CONT O550 IO550C SO INTAKE TUBE CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) INTAKE TUBE DRAIN BOSS WELD FOUND CRACKED. 1L72 3O3 O 3A16 E3SO 20030416000482003041600048 2003 4 16 MALA030235 420030412A23505020011003 CONTROL PANEL SAAB SF340 340B 7860101EU FIRST OFF AUDIO INOPERATIVE A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15362PX 340B258 DURING FLIGHT 3169, AFTER TAKEOFF THE F/O'S AUDIO CONTROL PANEL BECAME INOP. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED F/O'S ACP P/N 502-0011-003, SN/ON 0287, SN/OFF 0159. ALL CHECKS GOOD IAW SF340 MM CHAP 23. 2L72 4T RTA52EU 20030416001852003041600185NM 2003 4 16 AALA20030251 120030227A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21772AN 29580 ORD - EMERGENCY LIGHT ACROSS FROM L1 DOOR IS BROKE. REPLACED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030424000552003042400055NM 2003 4 24 QXEA0300330 120030304A5320 MOUNT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - NR 2 COMM ANTENNA MOUNTING STRUCTURE BRACKET CRACKED AT STRINGER 32S AND STATION X77.5. REPAIRED IAW HORIZON AIR EA 6-53-162A. 2H72 4T RTA13NM 20030423001972003042300197SO 2003 4 23 RAIA00303068 120030310A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DETACHED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03817HK 145058 STL- EMERGENCY PATH LIGHTS INOP AT 10A AND 11A. MAINTENANCE RE-SECURED WIRE IN FLOOR STRIP, OPS CHECK OK. 2L72 4T RTT00011AT 20030428000772003042800077SO 2003 4 28 C2XA03SH085 120030407A531014521721009 BUTT STRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV-DURING C CHECK THE FORWARD DIGITAL BUTT STRAP BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 (REPAIR 4). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030428000352003042800035NM 2003 4 28 P5CA030078 120030403A7933 CONNECTOR BOEING747 74746NF 13848BTNM ENG OIL TEMP DAMAGED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23453PA 30811 706263 NR 2 ENG OIL PRESSURE VARIED FROM 100-160 ON TAXI OUT. OPENED NR 2 ENG, CHECKED CONNECTION AT OIL PRESSURE TRANSMITTER AND FOUND PUSHED BACK PIN. RESEATED OPS CHECKED NORMAL ON ENG RUN. 2L74 4F RTA20WE 20030430002382003043000238NM 2003 4 30 AWXA200300365 120030413A2560P2070001214 FLASHLIGHT BOEING737 7373G7 1384595NM ZONE 900 - LAVATINOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28308AW 24710 FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030501001852003050100185NM 2003 5 1 ASAA0310089 120030305A57306546419501 SKIN BOEING737 737298C 1384490NM RT WING LE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND RIGHT WING LEADING EDGE SKIN AT WING STATION 497-536 CHAFED. REMOVED DAMAGED SECTION OF SKIN AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20030501000992003050100099WP 2003 5 1 GTIA030230 120030312A5321 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND PASSENGER CABIN CENTER FLOOR PANEL STATION 541-579 HAS SOFT/DETERIORATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030502001282003050200128EA 2003 5 2 03104627 120030414A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT ALL OF THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LIGHTING SYSTEM BATTERIES. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030502002312003050200231EA 2003 5 2 QXEA0300447 120030408A2612473971 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 INOPERATIVE A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09615QX1167 10065 PDX- ON FLIGHT NUMBER 2434, FIRE SYSTEM STATUS MESSAGE CAME ON IN FLIGHT, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED LOWER FIRE DETECTOR RAIL. OPERATIONAL TEST CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030502002662003050200266NM 2003 5 2 03FDEA00439 120030414A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 EXTERIOR SKIN OIL CANNED BS 1139 BETWEEN STR 23 AND 24 RT OIL CANNED EXTERIOR SKIN BS 1139 BETWEEN STR 23 AND 24 RT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REMOVED DAMAGE IN AN AREA OF 3.6 X 4.4 INCH, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3. 2L73 4F RTA3WE 20030505001412003050500141NM 2003 5 5 03FDEA00630 120030428A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-111-01) ON STRINGER BS 660 STR 28R . 2L73 4F RTA3WE 20030508001332003050800133EA 2003 5 8 03118664 120030428A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27664BR 7528 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISVOCEVERED AS EMERGENCY EXIT SIGN AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030509001142003050900114EU 2003 5 9 BAQA086248 120030423A6220365A3118100451 STARFLEX AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR DEBONDED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365KY164 6529 MAIN ROTOR DEBONDING OF STAR ARM BUSHING. 1G72 3U3 U H10EU E19EU 20030513002142003051300214WP 2003 5 13 ABXA030137 120030416A33505708458503 BATTERY DOUG DC8 DC863F 302198FWP CABIN DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX176 46113 MAINTENANCE FOUND EMERGENCY LIGHT VERY WEAK IN TEST. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM. 2L74 4F 4A25 20030514000642003051400064NM 2003 5 14 SWAA030963 120030430A53116546529 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B BELOW STR 20L. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20030530000382003053000038SW 2003 5 30 HEEA086683 120030522A3213212321103 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 CROSSTUBE CORRODED AT LOWER SADDLE MOUNT SUPPORTS TO A DEPTH OF .012 BEFORE TOTAL CLEAN UP. 1G72 4U H4SW 20030602001292003060200129NM 2003 6 2 SWAA031167 120030523A53126517582 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED (2 EA) AT LBL 17.1, BS 179 AT WL 227 AND BS 183 AT WL 231. REPAIRED VERTICAL BEAM WEB PER SRM. 2L72 4F A16WE 20030604000592003060400059WP 2003 6 4 UPS03840474 120030331A531037504972N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, FWD ACCESSORY COMPARTMENT AT STA 660 & L36 FRAME AND FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW FITTING P N# 3750497-2N-5N TAG 477912 LOCATED & DRILLED HOLES IAW DC8 SRM 51-1 -24 INSTALLED FITTING IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20030606000652003060600065NM 2003 6 6 03FDEA00612 120030421A5753ARB74131 SKIN DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING UPPER SURFACE ABOVE WING TRAILING EDGE SPAR STA XORS 1090 FOUND BULGED. WINGS - OUTER WING/REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIRED AS PER FEDEX EA 1-5720-69230. 2L73 4F RTA22WE 20030610000212003061000021NM 2003 6 10 2003UALA00442 120030520A5210 BOTTLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE PAX DOOR DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 DOOR 1R ASST BOTTLE FOUND WITH NO PRESSURE. BOTTLE PRESSURE EVACUATED DUE TO RUPTURED BURST DISC ON ASSIST BOTTLE. DOOR ASSIST BOTTLE REPLACED. NO ADDITIONAL DISCREPANCIES NOTED AND NO HISTORY THAT COULD HAVE RESULTED IN EMERGENCY OPERATION OF DOOR. 2L72 4F4 FRTA2NM E17NE 20030613000092003061300009EA 2003 6 13 SWIA200312062 120030421A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 FS 235 FUSELAGE SKIN LBL 6.0 NLG CUTOUT CRACKED. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-3-11-048 REV B. 2L72 4F RTA21EA 20030613000522003061300052NM 2003 6 13 CALA0300284 120030605A5320 STIFFENER BOEING737 7373T0 1384582NM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND STIFFENERS ON FORWARD SIDE OF AFT PRESSURE BULKHEAD CORRODED AT STA 1016 BETWEEN S28L AND S28R. THE STIFFENERS WERE REPAIRED IAW BOEING DRAWING 65C28106 AND SRM 51-10-02. 2L72 4F RTA16WE 20030617000282003061700028CE 2003 6 17 CA030603002 120030511A3211 BUSHING BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE TORQUE KNEE SEPARATED W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA (CAN) DURING LANDING IN HEAVY CROSSWIND, INITIAL RUNWAY CONTACT & SUBSEQUENT "BOUNCE" PROVIDED ENOUGH TORQUE TO ALLOW UPPER TORQUE KNEE LINK BUSHING TO BE PULLED THROUGH BY ATTACH BOLT, WHICH ALLOWED LOWER GEAR ASSEMBLY TO ROTATE 180 DEGREES. LANDING CONTINUED WITHOUT INCIDENT. UPPER TORQUE KNEE WAS REPLACED & AIRCRAFT RETURNED TO SERVICE. IT IS UNCERTAIN BUT THERE IS A POSSIBILITY THAT ARRANGEMENT OF TORQUE KNEE STACK, WASHER ARRANGEMENT, WAS NOT AS SPECIFIED IN MM. IF SO, ADDITIONAL TORQUE PRESENTED DURING CROSSWIND LANDING ALLOWED BOLT TO PASS THROUGH A WASHER AND DRAW BUSHING OUT ALLOWING TWO KNEES TO SEPARATE. A FLEET CHECK REVEALED NO OTHER AIRCRAFT WITH ANY INDICATION OF AN INCORRECT STACK. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030617000632003061700063EA 2003 6 17 QXEA200300704 120030611A4920WE38007703 APU CNDAIRCL600 CL6002C10 1390015EA APU BAY MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09610QX 10033 PDX- 'SUP'ON FLIGHT 2527 DURING APPROACH LAVATORY SMOKE DETECTOR ACTIVATED SHORTLY AFTER BLEED SYSTEM CHANGED OVER TO APU AIR. NO SMOKE NOTED. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030617000652003061700065NM 2003 6 17 QXEA200300667 120030530A32605352011 PANEL DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09363PH3057 520 YYJ-ON FLIGHT NUMBER 2073, AFTER TAKEOFF AND RETRACTING LANDING GEAR. NOSE LANDING GEAR GREEN LIGHT REILLUMINATED, PER EMERGENCY CHECKLIST. CYCLED GEAR OPERATION NORMAL. NOSE LANDING GEAR EXTINGUSHED. REMOVED AND REPLACED LANDING GEAR SELECTOR PANEL. FUNCTIONAL TEST LANDING GEAR EXTENSION AND RETRACTION SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030617001472003061700147NE 2003 6 17 ERAA087102 120030520A62107615009100053 BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01576EH5855 760212 M/R BLADE SEPARATION BETWEEN TIP RIB AND BLADE ASSY. INSPECTED, PERFORMED X RAY, ULTRASONIC INSPECTIONS PER QATI3048-3016, SS8806 & 6095, PERFORMED ALL INSPECTIONS UP TO AND INCLUDING 900 HOUR INSPECTIONS CMPLIED WITH AD 84-10-02, ASB 76-65-18C &N ASB 76-65-57. REPLACED SHIMS PER SA4047-76-5 PROCEDURE NO 9 REV 9 REPLACED 4 ROOT END THROUGH BUSHINGS PER RS-004N-VII; REPLACED STIFFNERS PER RS-003C; REPAIRED VOID ON UPPER SURFACE AT TIP PER PROCEDURE NR 18-1PLY; REPLACED NICKEL STRIP PER RS-007J-I; INJECTED SHEATH VOID AT TIP PER SA4047-76-5 PROCEDURE 2; REINSTALLED TIP CAP SN A175-03746; REFINISHED PAINT WITH HIGH VIS SCHEME 02 PER S76 SRM SA4047-76-5 DRWG 76150-09000 AND 76150-09100; STATIC BALANCED PER CTI-DAL-1G72 3U H1NE 20030613000402003061300040EA 2003 6 13 SWIA200311996 120030514A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07433SW 7550 FLOORBEAM ATTACH ANGLES AT FS 280 LBL 9 ARE CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11 PAR 4, 51-42-20, 51-42-06 & RII53-401. 2L72 4F4 FRTA21EA E15NE 20031027001132003102700113NM 2003 10 27 ASAA02402RR 120030407A532069353622 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT BS 867. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031030000372003103000037NM 2003 10 30 UPS03441295 120030906A5712 RIB BOEING747 747121 1384871NM NR 8 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 8 V/C FLAP I/B LINKAGE I/B RIB NR 4 AND NR 5 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 4 AND NR 5 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000062003103000006WP 2003 10 30 MWEA030400 120031001A78304330003ADL THRUST REVERSER DOUG DC9 DC932 3022066WP ENGINE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31209ME 47730 LIGHT CORROSION ON OUTER FACE OF LEFT DRIVE ARM, TOP BUCKET IN FLANGE RADIUS. REMOVED AND REPLACED THRUST REVERSER. 2L72 4F A6WE 20031103000032003110300003NM 2003 11 3 DL733030855 120030917A5415311A11112 BEAM BOEING737 737347 1384647NM NR 1 PYLON CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312WA 23598 CORROSION WAS FOUND IN THE AFT LUG BORE OF THE NR 1 PYLON CROWN BEAM FITTING AT NAC STA 257.25. THE BORE WAS OVERSIZED TO REMOVE THE CORROSION, HFEC INSPECTED, AND STEEL REPAIR BUSHINGS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385679-14. 2L72 4F RTA16WE 20031106001492003110600149NM 2003 11 6 QXEA200301384 120031102A2421 GENERATOR BOMBDRDHC8 DHC8401 1390041NM NR 2 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09546DS 4017 PDX- NR 2 AC GENERATOR OCCASIONALLY ILLUMINATES. RESETS OKAY PER ABNORMAL CHECKLIST. FOUND FAULTS 2A AND 26. CLEARED FAULTS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031112000132003111200013NM 2003 11 12 03FDEA01857 120031103A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 FWD LWR CARGO FRAME IS DENTED AT STA 560 STR 24 LT. REMOVED DAMAGE AREA AT FRAME IN AREA 1 X 2, AT BS 560, STR 24 LT. FABRICATE THE DOUBLER MADE FROM 7075-T6 0.063, AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3. 2L73 4F RTA3WE 20040112001012004011200101SO 2004 1 12 C2XA03SH511 120031223A531514522460015 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV- DURING C-CHECK THE CABIN FLOOR STRUCTURE AFT DIGITAL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT DIGITAL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040114001522004011400152CE 2004 1 14 DXTA200300169 120031123A324199122813 BOWL CESSNA560 560XL 2076702CE ANTI SKID SYS CRACKED E DXTAO OTHER JS WARNING INDICATION AFFECT SYSTEMS LDLANDING 1 GL07610QS 5605210 LOW BRAKE PRESSURE AND ANTISKID INOPERATIVE LIGHTS ILLUMINATED, FOLLOWED BY BRAKE FAILURE. USED EMERGENCY BRAKE TO STOP AIRCRAFT. TROUBLESHOT CRACKED ANTI-SKIP PUMP FILTER BOW, CHANGED FILTER BOWL, O RING ALONG WITH FILTER, ALSO AS PRECAUTION REPLACED PUMP ALONG WITH DISTURBED O-RINGS. SERVICED NITROGEN AND BLEED BRAKE SYSTEM, LEAK & OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE I.A.W CESSNA 560XL M/M CHAPTER 32-42-00. 2L72 4F RTA22CE 20040115001042004011500104NM 2004 1 15 03FDEA02081 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLAR CRACKED. RT CENTER SECTION OF NR 1 BANJO FITTING (AJC7051-505) FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY. 2L73 4F RTA22WE 20031217001652003121700165WP 2003 12 17 DHL2003803016 120031213A2120 DUCT DOUG DC8 DC873 302199CWP ACM LOOSE A DHLAJA DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01803DH 46123 IMMEDIATELY AFTER GEAR RETRACTION THERE WAS A CONTINUOUS VIBRATION / SHUDDER AND LOUD NOISE IN THE NOSE AREA. NOISE AND SHUDDER STOPPED AT 500 FEET WHEN PACK WAS TURNED OFF FOR LANDING. RE-SECURED LOOSE ACM DUCT RT EXPANSION SIDE PER DACO M/M 21-55-1. ALSO RE-SECURED LT PACK CURTAIN SNAPS THAT WERE OFF. PACKS CHECKED SERVICEABLE PER DACO M/M 21-55-00. 2L74 4F RT4A25 20031223000332003122300033NM 2003 12 23 SWAA032636 120031129A3350PL22300LH00 LIGHT BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C4 CHECK, FOUND EELPS TRACK STRIPS WORN. REMOVED AND REPLACED EELPS TRACK STRIPS PER MM. 2L72 4F RTA16WE 20031231000222003123100022NM 2003 12 31 TSAA0334042 120030305A3411 PITOT TUBE BOEING737 7372S2C 138448GNM PITOT STATIC SYSOBSTRUCTED A TSAAO OTHER C F.O.D. CLCLIMB 1 WP13806AL 21927 FIRST OFFICERS AIRSPEED INDICATOR FAILED IN FLIGHT. THE AIRCRAFT RETURNED TO HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED FOD FROM THE FIRST OFFICER'S PITOT TUBE. THE PITOT/STATIC SYSTEM WAS TESTED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231000812003123100081WP 2003 12 31 GTIA030935 120031029A7830 EXHAUST DUCT DOUG DC9 DC983 3022083WP THRUST REVERSER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND LEFT ENGINE T/R ACCOUSTIC EXHAUST DUCT DELAMINATED IN SEVERAL AREAS. REPAIRED DAMAGED AREA. (M) 2L72 4F RTA6WE 20031231001062003123100106NM 2003 12 31 TSAA0353045 120030301A53116546525 FRAME BOEING737 737282C 13844AUNM FUSLEAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13826AL 23051 TRIMMED OUT BODY FRAME AND REMOVED DAMAGED PART OF FRAME. FABRICATED REPAIR CHANNELS AND FILLER PER TABLE 1 FROM .063 INCH THICK 7075-T6 CLAD. ALODINED AND PRIMED REPAIR PART. INSTALLED THE REPAIR PARTS MAKING A FRAYING SEAL WITH BMS 5-95 SEALANT IAW SRM 53-10-4, FIGURE 6. (M) 2L72 4F RTA16WE 20031231000232003123100023NE 2003 12 31 TSAA0373191R1 220031122A7320442124 HMU BOEING737 73776N 13844CHNM CFMINTCFM567CFM567B22 13802NE NR 1 ENGINE MALFUNCTIONED A TSAAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 WP13745AL 29904 874870 40NM EAST OF FIXED POINT FANTO, NR 1 ENGINE FAILED. ATTEMPTED IN FIGHT ENGINE RESTART SUCCESSFULLY, BUT ENGINE REMAINED AT IDLE AND OIL TEMPERATURE ROSE RAPIDLY WHEN THRUST LEVER WAS ADVANCED. REMOVED AND REPLACED HYDRO-MECHANICAL METERING UNIT AND ENGINE DRIVEN FUEL PUMP. LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTA16WE E00055EN 20040108000762004010800076NE 2004 1 8 UIEA200300058 220031004A7200CF650E2 ENGINE BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE NR 2 SHUTDOWN A UIEAA UNSCHED LANDING RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 EA15537MC 22403 517568 INFLIGHT ENGINE SHUTDOWN IN CRUISE NR 2 ENGINE N1 SPOOLED DOWN FROM 102 PERCENT TO 55 PERCENT. ALL OTHER INDICATIONS NORMAL. ENGINE WOULD NOT RESPOND TO THRUST LEVER MOVEMENT. ENGINE SHUTDOWN AS PRECAUTION AT 07:55 UTC. C/A: FOUND DEBRIS IN EXHAUST. BOROSCOPED HPC/LPC IAW FIM 71-00-42 PAGE 105 ITEM 2. ALL ROTOR BLADES DAMAGED FROM HPC STAGE NR1 THRU NR 2 NIL DAMAGE FOUND. REMOVED AND REPLACED NR 2 ENGINE IAW MM 71-00-02 AND FORM 01-AA-45. SN ON 530257.(K) 2L74 4F4 F A20WE E23EA 20040106001622004010600162 2004 1 6 03348672 420031214A22116229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS FAULTY A VTZAK NONE F FLT CONT AFFECTED DEDESCENT 1 EA27672BR 7594 DURING DESCENT THE CREW REPORTED THE AIRCRAFT ROLLING TO THE RIGHT 2 TO 3 DEGREES PER SECOND. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. THE FAULT WAS FOUND TO BE FLIGHT CONTROL COMPUTERS AND THEY WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040114002182004011400218NM 2004 1 14 MWEA030491 120031215A57535930496508 SKIN DOUG MD88 MD88 3023688NM FLAP VANE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RT OUTBOARD FLAP, INBOARD FIX VANE HAS MINOR DAMAGE ON LEADING EDGE ON INBOARD END. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20031125000482003112500048WP 2003 11 25 DHL2003807558 120031022A53204772359U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SEAT TRACK SUPPORT FITTING CRACKED 0.500, STA 620.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031126000192003112600019EA 2003 11 26 QXEA200301400 120031106A2120 DUCT CNDAIRCL600 CL6002C10 1390015EA A/C BAY CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX-RIGHT HAND AIR CYCLE MACHINE EXHAUST DUCT LOUVER CRACKED. REPAIRED IAW CRJ SRM 51-42-06 AND SRM 51-42-21. 2L72 4F RTA21EA 20031203001802003120300180WP 2003 12 3 AALA20031100 120031003A33500211720004 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21489AA 49682 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 8D. REPLACED LIGHT SOCKET SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040120000322004012000032NM 2004 1 20 03FDEA02293 120031229A5744ARC198413 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, OB FLAP IB HINGE ACTUATOR OB MOUNT IB AND OB SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR 2L73 4F4 FRTA22WE E13NE 20040121000482004012100048EA 2004 1 21 ASOA03591 120031119A532060034017595 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT AT FS 280 LBL 9.0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT AT FS 280.0, LBL 9.0 IAW ASA EO 600-53-0123. (M) 2L72 4F RTA21EA 20040123000362004012300036NM 2004 1 23 MEX2003526 120031118A56105887275505 WINDSHIELD DOUG MD88 MD88 3023688NM COCKPIT FAILED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW23160PL 49763 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MZT DUE TO THE CENTER WINDSHIELD BEING BROKEN AT FLIGHT LEVEL 35,000. THE CENTER WINDSHIELD, THE WINDSHIELD TEMPERATURE CONTROLLER AND THE TRANSFORMER T1-50 WERE REPLACED AND TESTS WERE PERFORMED IAW MM 56-10-01 AND 30-11-00, ALL OK. 2L72 4F RTA6WE 20031204000212003120400021WP 2003 12 4 GTIA030870 120030928A5730 PANEL DOUG DC9 DC982 3022082WP RT WING DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND RIGHT WING BOTTOM TRAILING EDGE TRAP PANEL JUST FORWARD OF RT MLG DELAMINATED. REMOVED RIGHT WING BOTTOM TRAP PANEL. REPAIRED RT WING BOTTOM TE TRAP PANEL INSTALLED RIGHT BOTTOM TE TRAP PANEL. (M) 2L72 4F A6WE 20031204001902003120400190WP 2003 12 4 MWEA030426 120031021A5321993659915 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 MID CARGO COMPARTMENT CENTER FLOORBOARD STATION 598-636 IS DETERIORATED ALONG AFT EDGE. FABRICATED AND INSTALLED FLOORBOARD. 2L72 4F A6WE 20031209000732003120900073NM 2003 12 9 SWAA032373 120031027A53116546539 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 639, LBL 63, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20031209002662003120900266NM 2003 12 9 AWXA200301366 120031021A5320654681282 WEB BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD END OF LT SHEAR WEB AT BS 995.5, LBL 43.5, AND EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT OUTBOARD SHEAR WEB, BS 1002, LBL 40. MAINTENANCE REMOVED DAMAGED SHEAR WEB FROM BS 995.5 TO BS 1014, LBL 43.5 TO LBL 48; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, FIG 2, 3 & 11. 2L72 4F RTA16WE 20031211000032003121100003EA 2003 12 11 COMA0370047 120031104A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA2240 10079 FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20030916001482003091600148WP 2003 9 16 ARWA20030509 120030527A5330 DOUBLER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT STATION 1620, BETWEEN L-26R AND L-31R INNER SKIN WITH SEVERAL SPOTS OF CORROSION. REPAIRED FUSELAGE INNER DOUBLER AT FS 1620, BETWEEN L-25R AND L-31R IAW MFG ENGINEERING REPAIR ORDER AROW-031RO-3, PAGE 1 TO 2, DATED 05/01/03 AND REPAIR DRAWING NUMBER AISAC-N784AL-03/03, SHEETS A-1 TO A-5, DATED 05/01/03, REVISION IR. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. 2L74 4F4 F 4A25 1E8 20030617001912003061700191SW 2003 6 17 HEEA087474 120030612A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 FLOAT BOTTLE DISCHARGED THROUGH FUSIBLE PLUG. 1G71 3U O H2SW 20030528000392003052800039 2003 5 28 HEEA086593 420030521A2330 CIRCUIT BOARD BELL 412 412 1182202SW PA AMPLIFIER CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 099 36005 PA AMP HAS CORROSION. FOUND CORROSION ON PC BOARD. UNIT WORKS INTERMITTENTLY, CONNECTOR P2 AND PINS BAD, UNIT COVER BAD. CLEANED CORROSION ON PC BOARD, REPLACED CONNECTOR P2, PINS AND UNIT COVER. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030529000012003052900001SO 2003 5 29 2003F00323 120030328A56101159SCB51023 WINDSHIELD GULSTMG1159 GIV 3980115SO COCKPIT CRACKED A IMJAO OTHER O OTHER NRNOT REPORTED 1 EA25440TC 1115 CO-PILOTS WINDSHIELD OUTER PANE CRACKED IN CRUISE, AT FL39 AND MACH .82. (M) 2L72 4F RTA12EA 20030623000802003062300080WP 2003 6 23 MEX2003190 120030523A212039613011 VALVE DOUG DC9 DC982 3022082WP FLOW CONTROL MALFUNCTIONED A ASMFO OTHER J WARNING INDICATION DEDESCENT 1 SW23505MD 49149 HMO - FLT 104 - GDL - DURING DESCENT, INDICATION STARTED TO CLIMB AND LOW FLOW LIGHT TURNED ON WITH PRESURIZATION VALVE CLOSED, ENGINE ACCELERATED TO 1.5 EPR AND A/C INDICATED PRESSURE OF 12 PSI. SYSTEM WAS CHECKED FOR LEAKAGES AND BOTH CONTROLLERS PRESSURE TRANSFER RELAY WERE TESTED, ALL CORRECT. LEFT REGULATOR PRESSURE VALVE AND FLOW CONTROL VALVE WERE REPLACED IAW MM 21-31-1/2 AND MM 21-32-3, ALL CORRECT. (M) 2L72 4F A6WE 20030625000362003062500036NM 2003 6 25 AWXA200300590 120030505A5320146N5246U6 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR SUPPORT AT RBL 70, B/S 1660-1680. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR SUPPORT RBL 70, BS 1660-1680; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 7-8. 2L72 4F RTA2NM 20030708000332003070800033WP 2003 7 8 UPS03840892 120030617A5754 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RIGHT WING LE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LEADING EDGE INBOARD END OF OUTBBOARD. SLOT HAS SCREWS PULLING THRU SKIN AT XFS XOLDI 6.225. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM. 57-2-0 FIG. 2A 2L74 4F4 FRT4A25 E2GL 20030710000572003071000057NM 2003 7 10 DHL2003749006 120030521A2613D201W3 SWITCH BOEING727 7272J0 138407ENM OVERHEAT SYS MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01749DH 22013 ON PRE-DEPARTURE CHECK LOWER AFT BODY OVERHEAT WOULD NOT TEST. TRANSFERRED TO DMI CONTROL 13029 PER MEL 26-10-2. PLACARD INSTALLED. SPECIAL PROCEDURES 26-10-2 COMPLIED WITH TO VERIFY SYSTEM OPERATION. REF DMI 13029 ON PRE-DEPARTURE CHECK LOWER AFT BODY OVERHEAT WOULD NOT TEST. REPLACED TEST SWITCH ON LOWER AFT BODY OVERHEAT PANEL. OPS CHECKED GOOD IAW B727 M/M 26-14-0. THIS CLEARS DMI 13029. 2L73 4F RTA3WE 20030710000612003071000061WP 2003 7 10 DHL2003806008 120030606A33505708458503 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01806DH 46002 DURING PREFLIGHT EMERGENCY LIGHTS DID NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PER M/M 33-50-0. OPS CHECKED GOOD. 2L74 4F RT4A25 20030716000752003071600075SO 2003 7 16 SIMA200313906 120030514A5315145225381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21808AE 145519 DURING AN MBV INSPECTION, THE LT FLOORBEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGE SECTION OF THE LEFT OMEGA BEAM, CLEANED, AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-21-10 FIG 202, SHEET 2 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030114001362003011400136NM 2003 1 14 SWAA030040 120030108A256061020 BATTERY BOEING737 7372H4 138448CNM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29085SW 22826 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F A16WE 20030115001242003011500124NM 2003 1 15 PCAA0301015 120030114A6120V319 SWITCH DHAV DHC8 DHC8102 2809003NM COCKPIT INTERMITTENT A PCAAK NONE S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA13843EX 335 BOS-FLIGHT#3852. CREW REPORTED AIRCRAFT ACCELERATES WHEN REVERSE IS SELECTED. MAINTENANCE VERIFIED BETA BACKUP SYSTEM IS ENGAGING, AND REPLACED BETA BACKUP POWER LEVER SWITCH 6141-S3. AFTER TAXIING AIRCRAFT, OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030127000612003012700061 2003 1 27 HEEA083639 420030114A34225050010902 GYRO BELL 407 407 1182206SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 GYRO PRECESSES 15 DEGREES OFF COURSE IN FLIGHT. MUST BE RESET CONSTANTLY. REPAIRED. 1G71 3U O H2SW 20030127001162003012700116SW 2003 1 27 HEEA083666 120030115A6710206001396001 SHAFT BELL 407 407 1182206SW CYCLIC STICK DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 CYCLIC STICK SHAFT ASSY FINE THREADS ROLLED/WORN. 1G71 3U O H2SW 20030129000672003012900067SW 2003 1 29 HEEA083981 120030117A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 ENGINE BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030201000032003020100003SO 2003 2 1 C2XA02SH186 120030201A532014522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727523 145389 SHV DURING C CHECK SUPPORT RAMP ON CENTER OMEGA FLOOR BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT RAMP IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030204002062003020400206 2003 2 4 SWAA030135 420030120A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER UKUNKNOWN 1 SW29648SW 27718 L1 DOOR ESCAPE SLIDE PARTIALLY FELL OUT OF CONTAINER. REINSTALLED THE L1 ESCAPE SLIDE PER MM. 2L72 4F RTA16WE 20030218002172003021800217NM 2003 2 18 SWAA030312 120030207A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8R AND STR 9R, AT BS'S 440, 480, 727D, 767, 827 AND 867. 2L72 4F RTA16WE 20030219000952003021900095NM 2003 2 19 SWAA030311E 120030207A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030221000422003022100042NM 2003 2 21 QXEA0300153 120030122A7110 DOOR DHAV DHC8 DHC8202 2809007NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 2 COWL DOOR 424AR IS CRACKED BY DATA PLACARD AT PREVIOUS WELD. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20030224001372003022400137NM 2003 2 24 AWXA200300188 120030127A5320146N52465 SUPPORT BOEING757 7572S7 1384962NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON THRESHOLD SUPPORT BS 1640 TO BS 1680, LBL 60. MAINTENANCE REMOVED DAMAGED THRESHOLD SUPPORT BS 1661 TO BS 1680, LBL 60; FABRICATED A REPLACEMENT THRESHOLD SUPPORT; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-05, PG. 1-2. 2L72 4F RTA2NM 20030225000872003022500087SW 2003 2 25 HEEA084301 120030211A6321407340302101 CALIPER BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 ROTOR BRAKE CALIPER WORN AND WEAK. 1G71 3U O H2SW 20030306000022003030600002 2003 3 6 HEEA084714 420030217A3454 KNOB BELL 412 412EP 1182205SW CONTROL UNIT LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03412PH 2173 36140 LOOSE KNOB. FOUND PHOTOCELL LENS AND 25K PULL KNOB BAD. ALSO FOUND OUTER KNOB SET SCREWS LOOSE AND OUTER KNOB SHAFT RETAINING RING CAME OFF. REPLACED PHOTOCELL LENS AND 25K PULL KNOB. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030310000342003031000034SW 2003 3 10 HEEA084943 120030227A7120 BEARING BELL 412 412 1182202SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ENGINE MOUNT BEARINGS WORN. REPAIRED. 1G72 4U H4SW 20030121002372003012100237 2003 1 21 HEEA083358 420030109A34424000038001 CONTROL UNIT BELL 206 206B3 1181506SW WX RADAR SYS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 PINS BROKEN ON HEAD. FOUND SEVERAL PINS ON REAR CONNECTOR BENT. STRAIGHTENED PINS AND BENCH CHECK GOOD. 1G71 3U H2SW 20030121002592003012100259NM 2003 1 21 PCAA0301003 120030101A3350 SOCKET DHAV DHC8 DHC8102 2809003NM CABIN DEFECTIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13840EX 327 DURING ROUTINE MAINTENANCE VISIT EMERGENCY PATH LIGHTING FORWARD MOST LIGHT FOUND INOPERATIVE. LIGHT SOCKET WAS REPLACED ON THE EMERGENCY PATH LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030314001832003031400183SO 2003 3 14 000242 120030120A4920 APU EMB 145 EMB145 3260210SO APU BAY CONTAMINATED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL11280 SMOKE IN COCKPIT.FOUND APU INLET FILLED WITH DEICE FLUID. CLEANED APU INLET AND COMPARTMENT AND STARTED APU. WHEN PACK 1 SELECTED, SMELLED DEICE FLUID IN COCKPIT. RAN BOTH PACKS WITH APU TO CLEAR OUT DEICE FLUID. APU AND PACKS NOW OPERATE WITHOUT SMOKE OR SMELL OF SMOKE OR DEICE FLUID IN COCKPIT OR CABIN/ 2L72 4F RTT00011AT 20030318001342003031800134NM 2003 3 18 GAIA03006OP 120030212A3260651781915 MOUNT BOEING727 727223 1384074NM LT MLG U/L ACT BROKEN A GAIAO OTHER N FALSE WARNING APAPPROACH 1 SW076831 20184 FLT 743 - MEM-TOL - DURING LANDING APPROACH TO TOL, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION, THE LEFT MLG RED UNSFAFE LIGHT ILLUMINATED. THE CREW RAN THE MANUAL EXTENTION CHECKLIST TO EXTEND THE GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THAT THE LT MLG UPLOCK ACTUATOR UPPER MOUNT WAS BROKEN. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT WAS FERRIED TO CYYZ FOR GEAR SWING. LANDING GEAR RETRACTION CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030320000512003032000051NM 2003 3 20 USAASB03021 120030207A2750 CONNECTOR BOEING737 7373B7 1384580NM TE FLAPS CONTAMINATED A USAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA19529AU 24411 ORD - FLT 1227 - EN ROUTE, CREW REPORTED TE FLAPS LOCKED OUT AT 10 UNITS AND AT 15 UNITS DURING FLT. FLAPS UNLOCKED AFTER TOUCHDOWN AT ORD. ONCE ON GROUND, CREW CYCLED FLAPS AND THEN LOCKED OUT AT 20 UNITS AND AT 25 UNITS. MAINTENANCE WAS UNABLE TO DUPLICATE PROBLEM. FOUND CONNECTORS D229 AND D275 TO BOTH FLAP POSITION TRANSMITTERS WET WITH DEICE FLUID. CLEANED BOTH CONNECTORS AND ACCOMPLISHED SATISFACTORY FUNCTIONAL CHECK OF FLAP POSITION INDICATION SYSTEMS. ALSO, REMOVED AND REPLACED FLAP POSITION INDICATOR (P/N 2061-14-1) AS PRECAUTIONARY. (M) 2L72 4F RTA16WE 20030122001532003012200153NM 2003 1 22 DL757030059 120030114A79107T0908 OIL CAP BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE LOOSE A DALAK NONE K FLUID LOSS CLCLIMB 1 SO27692DL 29724 727277 RT ENG OIL TEMP IN AMBER RANGE, 168 DEGREES ON CLIMBOUT FROM ATL. RT OIL PUMP LOW EICAS MSG. FOUND OIL TANK CAP POPPED OFF, FOUND LOCKING TAB VERY LOOSE, POPS OFF WITH MINIMAL PRESSURE. RETORQUED ADJUSTMENT SECURING NUT ON CAP LOCKING TAB ASSY AND REPLACED O-RING. CAP REINSTALLED, SECURE AND TIGHT. 2L72 4F4 FRTA2NM E17NE 20030324000562003032400056WP 2003 3 24 ABXA030115 120030311A528056489321 DOOR DOUG DC8 DC861 3021952WP MLG MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 LEFT MAIN LANDING GEAR LOWER COVER PANEL (FOR STRUT) MISSING ON BPO WALK AROUND. INSTALLED NEW LEFT MAIN LANDING GEAR CENTER DOOR IAW DC-8 MM. 2L74 4F 4A25 20030327001542003032700154SO 2003 3 27 C2XA03IA028 120030316A3222 STRUT EMB 145 EMB145 3260210SO NLG UNDERSERVICED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149597752 7752 145091 FLT 2825 - DURING CLIMB THE CREW NOTICED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED AND LANDED AT IAH WITHOUT FURTHER INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. THE AIRCRAFT WAS RETURNED TO SERVICE AND THE DISCREPANCY REOCCURED ON FLIGHT 2810. MAINTENANCE INSPECTED AND FOUND THE NOSE LANDING GEAR STRUT TO REQUIRE SERVICING. THE NOSE LANDING GEAR STRUT WAS SERVICED, THE AIRCRAFT SUCESSFULLY TEST FLOWN, AND THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030417000912003041700091EU 2003 4 17 MALA030140 120030203A2913 PUMP SAAB SF340 SF340A 7850100EU HYD SYSTEM MALFUNCTIONED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL1599XJ 340A099 DURING FLIGHT 3396, HYDRAULIC ACCUMULATOR PRESSURE WENT TO ZERO AND THE HYDRAULIC PUMP DID NOT RUN IN AUTO. CREW DECLARED AN EMERGENCY AND LOWERED THE GEAR USING EMERGENCY EXTENSION METHOD (EXPLOSIVE BOLTS). CREW BLEW BOLTS TO DROP GEAR AND AIRCRAFT LANDED WITHOUT INCIDENT. 2L72 4T RTA52EU 20030417001842003041700184SO 2003 4 17 SWIA200311775 120030207A27503075001017 CONTROL UNIT EMB 120 EMB120RT 3260202SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07593SW4846 1783 120191 ON TAKEOFF THE ANALOG FLAP INDICATOR BOUNCED BACK AND FORTH BETWEEN 0-15 DEGREES, SETTING OFF THE TAKEOFF AURAL WARNING SYSTEM. ALSO, EACH TIME IT WENT TO 0 DEGREES, RECEIVED FLAP AND ADVANCED SWS WARNINGS ON THE MAP. OPERATED FLAPS SEVERAL TIMES, COULD NOT DUPLICATE. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB120 MM 25-50-06 FOR TROUBLESHOOTING. OPS CHECK GOOD. 2L72 4T RTA31SO 20030421000992003042100099NM 2003 4 21 DLM88030163 120030219A2420976J2528 GENERATOR DOUG MD88 MD88 3023688NM NR 1 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO27923DL 49705 UNK AFTER TAKEOFF AT 1000 FT AGL LEFT ENG GENERATOR TRIPPED OFF AND GOT X-TIE LOCKOUT MESSAGE. RT ENG DID NOT PICK UP BUS. RESET LT GENERATOR AND REPOWERED BUS. APU WAS STARTED BUT NOT PUT ON LINE. LANDED WITH X-TIE LOCKOUT MESSAGE. RESET RELAY, SERVICED CSD, RAN ENGINE. 2L72 4F RTA6WE 20030423000602003042300060 2003 4 23 BAQA085102 420030306A3421109290 GYRO BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101750B1 41560NE COCKPIT DISCONNECTED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03300CP2430 7249 RATE GYRO LIGHT ILLUMINATED IN FLIGHT AND DECOUPLED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE10 20040225000502004022500050CE 2004 2 25 BSY2004F00002 120030313A32606838 BULB LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP MLG INDICATOR INOPERATIVE E BSYAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL0727TT 0122 P74105 NO NOSE GEAR DOWN AND LOCK LIGHT. REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2L72 4F4 F A10CE E6WE 20040226000222004022600022NM 2004 2 26 ASAA0370006 120030409A5320146A9401 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01607AS 29751 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE. REPLACED FLOOR SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20030903000072003090300007WP 2003 9 3 DHL2003804006 120030712A535057536043 RADOME DOUG DC8 DC873F 302199FWP FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH3033 3033 46124 RADOME HAS A 12 INCH CREASE LOWER LEFT SIDE. REMOVED AND REPLACED RADOME ASSY IAW DC-8 M/M 53-50-1. OPS CHECKS GOOD. 2L74 4F RT4A25 20030805000032003080500003WP 2003 8 5 03FDEA00740 120030516A2740 PIVOT ASSY DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL RT HORIZ STAB SEIZED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 HORIZ STAB CONSTANT SECTION BEARINGS - SUSPECTS R/H PIVOT BEARING IS FROZEN. PIVOT BEARING SHAFT HEAD MOVED INTO SUPPORT RETAINER. PREFORMED PIVOT BOLT LUBRICATION PER W/C 27C2116, FUNCTIONED ENTIRE HORIZONTAL STAB TO FULL ANUG AS WELL AS FULL A N D PER W/C27C4602. NO BINDING OR POPPING NOISE NOTED. 5/16/03. 2L73 4F4 F A22WE E23EA 20030903001602003090300160EU 2003 9 3 WRNA200300012 120030722A3230C230056 DAMPENER AIRBUS300 A300B4203 3930306EU RT MLG LACK OF LUBE A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05820SC 154 UNABLE TO RETRACT LANDING GEAR ON SYSTEM 1 OR 2. RETURNED TO AIRPORT, NO FUEL DUMPED, LANDING NORMAL. AIRCRAFT RETURNED TO GATE. FOUND RT MLG PITCH DAMPNER INDICATOR POPPED. SERVICED DAMPNER IAW MM 12-12-32. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20030904000632003090400063 2003 9 4 SWIA200312303 420030824A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07215SW113103507 120281 FO AUTOPILOT FLIGHT DIRECTOR NOSE DOWN 10 DEGREES. AUTOPILOT FAIL AND TRIM FAIL MASTER WARN ON MAP ASSOC WITH RED TRIM AND AP LIGHTS ALSO GREEN VS AND AMBER DIS. REMOVED AND REPLACED NR 2 APC 65B IAW 22-10-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030904000282003090400028SO 2003 9 4 C2XA03SH274 120030817A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV DURING C CHECK THE APU FIREWALL WAS FOUND CRACKED AT THE RIGHT HAND APU SUPPORT. MAINTENACE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001122003080600112SO 2003 8 6 C2XA03SH256 120030803A532014521725013 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 SHV- DURING C-CHECK, THE FORWARD SERVICE DOOR SILL BETWEEN FRAMES 18 AND 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030812000322003081200032 2003 8 12 HEEA088396 420030801A34214020550904 INDICATOR SKRSKYS76 S76A 8143006NE COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 ADI ERRATIC, INTERMITTENTLY PRECESSES IN FLIGHT. SHOP REPAIR. 1G72 3U H1NE 20030813000682003081300068EA 2003 8 13 SWIA200312080 120030608A5210 CAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07947SW 7786 MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. PAX DOOR LOCK PAWL STOPPING AGAINST LATCH-CAM TORQUE TUBE. ADJUSTED CONTROL ROD END ON LOCK PAWL IAW MM 52-11-15. OPS CHECKS GOOD AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20030814000942003081400094NM 2003 8 14 2003UALA00584 120030722A3230 CONNECTOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE MCI LOOSE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29819UA 893 V10065 DVTD TO MCI DUE TO LGCIU 1 FAULT ON ECAM / ELECT CONNECTOR LOOSE ON SENSOR. REPLACED THE LGCIU. 2L72 4F4 FRTA28NM E40NE 20030814001272003081400127NM 2003 8 14 2003UALA00575 120030720A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29663UA 27160 MAIN CABIN BETWEEN BS 785.9 AND BS 814, LBL 55, SEAT TRACK CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE SECTION. 2L72 4F4 FRTA1NM E24NE 20030815000102003081500010WP 2003 8 15 GTIA030572 120030630A5320 WEB DOUG DC9 DC982 3022082WP SUBFLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND FLIGHT COMPARTMENT CORRODED SUBFLOOR AT FS 133-148 29 INCHES TO 48 INCHES RBL. REMOVED WEB. FABRICATED NEW SUB FLOOR. INSTALLED NEW WEB. (M) 2L72 4F A6WE 20030822000402003082200040NM 2003 8 22 03FDEA01317 120030806A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RIGHT OUTBOARD FLAP OUTBOARD HINGE 28 2FC SIDE 29 OUTBOARD UPPER ATTACH HOLE WORN AT FWD SIDE OF BORE. RT WING OUTBOARD FLAP, OUTBD HINGE ( A/C SIDE ) OUTBD UPPER ATTACH HOLE BORE REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030910001032003091000103NM 2003 9 10 MWEA030356 120030902A532039120751 FITTING DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FRAME TO FLOOR FITTING IS CORRODED AT FRAME STATION 1060. REMOVED CORROSION 2L72 4F RTA6WE 20030730001262003073000126EU 2003 7 30 2003F00489 120030516A7830 COUPLING AIRBUS320 A320233 3930329EU THRUST REVERSER DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 1 ENGINE LEFT THRUST REVERSER COUPLING OUTER SKIN C-DUCT DELAMINATED AND MISSING MATERIAL. REPAIRED 'C' DUCT IAW SRM V2500, REPAIR NR 4, REV 31. (M) 2L72 4F RTA28NM 20030915000632003091500063GL 2003 9 15 ALGA089023 220030905A725023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE GALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO N1 COUPLING FOUND TO HAVE SPLINES GALLED ON INSPECTION. RETURNED PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20030908003132003090800313NM 2003 9 8 SWAA031891 120030822A3350311500 LENS BOEING737 737317 138447PNM EXTERIOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C2 CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20031002000692003100200069NM 2003 10 2 AWXA200301035 120030909A2781BCREF2609 LIGHT BOEING737 7373G7 1384595NM FLAP INDICATOR BROKEN A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28154AW 23776 ON TAKEOFF ROLL AT PHX EN ROUTE FOR OMA THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED ON AND OFF TWICE AT APPROXIMATELY 70 KTS, REJECTED TAKEOFF. MEL 27-4, COND. 1 L/E FLAP TRANSIT LIGHT INOP WAS ISSUED. UPON ARRIVAL BACK IN PHX, MAINTENANCE INSPECTED THE L/E FLAPS AND SLATS, NO DISCREPANCIES WERE NOTED. INSPECTED THE KORRY LIGHT ASSEMBLY AND FOUND THE LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED L/E FLAP TRANSIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031003000342003100300034NM 2003 10 3 AALA20030798 120030725A2497 WIRE BOEING757 757223 1384957NM LT GENERATOR LOOSE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21630AA 24588 LEFT GENERATOR FAILED IN FLIGHT. AIRCRAFT RETURNED ANC AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT GENERATOR GROUND WIRE LOOSE AT IDG TERMINAL BLOCK. RE-TORQUED WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000582003100300058SO 2003 10 3 C2XA03SH321 120030913A532014522480003 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE CARGO DOOR LOWER SILL BETWEEN FRAMES 65 AND 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031006000512003100600051 2003 10 6 UO22003F00003 420030909A3416804710 ALTIMETER AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP COCKPIT FAILED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19707CX 135 REMOVED UNIT FROM AIRCRAFT DUE TO UNIT LEAKING AND SHIPPED TO INSTRUMENT SERVICES, INC. FOR REPAIR. REINSTALLED UNIT AFTER REPAIR AND UNIT FAILED LEAK TEST. REMOVED UNIT AND WILL SENT UNIT BACK REPAIR STATION. 2L72 4F4 F A33EU E6WE 20031006000432003100600043NM 2003 10 6 PCAA0309110 120030907A3397BVO330012150 SOCKET DHAV DHC8 DHC8102 2809003NM SEAT 7DF BURNED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13810EX 308 CREW REPORTED THAT THE OVERHEAD LIGHT AT SEAT 7D WAS GLOWING, SPARKING, AND SMOKING. MAINTENANCE REMOVED BULB AT SEAT 7D, AND ISSUED A DEFERRAL. ON 15 SEPTEMBER 2003 MAINTENANCE INSPECTED WIRING AND SOCKETS AT 7DF AND 9EF. SOCKET AT POSITION 7DF WAS FOUND TO BE BURNED AND UNSERVICABLE. SOCKET WAS REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031006000422003100600042NM 2003 10 6 QXEA200301127 120030912A2810 O-RING DHAV DHC8 DHC8202 2809007NM ZONE 400 LEAKING A QXEAK NONE K FLUID LOSS ININSP/MAINT 1 NM09348PH 484 FUEL DRIPPING FORWARD OF SPR DOOR. REMOVED MASTER REFUEL/DEFUEL VALVE AND INSTALLED NEW O-RINGS. RE-INSTALLED VALVE. 2H72 4T RTA13NM 20030910000582003091000058WP 2003 9 10 DHL2003604550 120030508A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 INTERIM REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP BETWEEN XF 309.000 AND XF 333.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 4. REMOVED LOWER SKIN OF LT OUTBOARD FLAP WITH INTERIM REPAIR (XF 309.000 - XF 333.000) IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN AND FILLER IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 4. CLEANED, TREATED AND PRIMED AREA AND FILLER AND NEW SKIN IAW SRM 51-1-8B. INSTALLED FILLER AND NEW SKIN IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031027001072003102700107NM 2003 10 27 ASAA02402NN 120030331A5311 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND CORRODED FRAME AT BS 500. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001542003102800154NM 2003 10 28 GAIA03090 120030910A5311 FRAME BOEING727 727223 1384074NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 600 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53133, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F A3WE 20031028001652003102800165NM 2003 10 28 ASAA0340100 120030301A531065C25230 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE BS 727E RBL 11 AND EL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031027000752003102700075NE 2003 10 27 MALA030425 220030912A7530 BLEED BAND BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE ENGINE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15532XJ E2366 DURING CLIMBOUT ON FLIGHT 3673, EGT WENT TO 643 FOR A VERY SHORT TIME. POWER WAS REDUCED BACK TO IDLE, ALL OTHER ENGINE PARAMETERS WERE NORMAL. RETURNED TO MSP. MAINTENANCE REPLACED BLEED BAND PER LF 507 MM 72-00-34. BORESCOPED ENG AND PERFORMED ENG RUNS, ALL CHECKS GOOD REF 409 CARD 195072 FOR FURTHER DETAILS. 2H74 4F4 FRTA49EU E6NE 20031028001462003102800146EA 2003 10 28 ASOA03491 120031006A5240 SEAL CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE SERVICE DOOR SEAL PLATE WAS FOUND TO BE CORRODED BEYOND LIMTIS. MAINTENANCE IS REMOVING AND REPLACING THE SERVICE DOOR SEAL PLATE IAW ASA EO 600-53-0052A. (M) 2L72 4F RTA21EA 20031119001142003111900114NM 2003 11 19 2003UALA00742 120031005A2150 A/C PACK BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ODOR A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29796UA 26931 RANCID ODOR COMING AIR CONDITIONER. SMOKE OR FUMES IN CABIN. APU WAS REPLACED AND SHOP DISASSEMBLED GEARBOX AND LOAD COMPRESSOR. ENGINEERING FOUND INDICATIONS THAT THE LOAD COMPRESSOR FRONT CARBON SEAL TO BE THE ROOT CAUSE FOR ODOR IN CABIN. THE LOAD COMPRESSOR CARBON SEAL HOUSING WAS FOUND BULGED AND WITH HEAT DAMAGE TO INNER LIP SEAL RESULTING IN COKING ON SEAL ROTOR. CARBON SEAL, SEAL ROTOR, BEARING, AND BACK SCHROUD REPLACED. 2L72 4F4 FRTT0001SE E46NE 20031121000192003112100019NM 2003 11 21 SWAA032482 120031109A32116516300 FITTING BOEING737 7373G7 1384595NM LT/RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG FWD WALKING BEAM HANGER FITTINGS CORRODED. REPAIRED FITTINGS PER SWA EA. 2L72 4F RTA16WE 20040329000052004032900005EU 2004 3 29 USAASA03139 120031220A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19730US12396 1182 TPA - LEFT FORWARD EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHT TEST. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031030000622003103000062WP 2003 10 30 UPS03841306 120030919A53403779978U1 FITTING DOUG DC8 DC873F 302199FWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STA 834 FRAME TO LONGERON FITTING IS CRACKED AT LONG 14R. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D. 2L74 4F RT4A25 20031103000822003110300082SW 2003 11 3 ALG2003F00074 120030331A5320206031329103S FITTING BELL 206 206L1 1182107SW FUSELAGE CRACKED E ALGAK NONE O OTHER ININSP/MAINT 1 SW032759N 45271 ON A DAILY, FITTING WAS CRACKED. 1G71 3U H2SW 20031112000012003111200001NM 2003 11 12 2003UALA00810 120031027A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29374UA 24639 STA 597 STR 7R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20031107001482003110700148WP 2003 11 7 GTIA030740 120030923A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND MAIN CABIN STATION 1079 TO STATION 1117 FLOOR PANEL CRACKED/DAMAGED AT CORNER. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20031009000782003100900078EA 2003 10 9 SWIA200312400 120030912A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS484 RT INTERCOSTAL OUTBOARD FLG, RBL36 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV ''A''. 2L72 4F RTA21EA 20031010000182003101000018NM 2003 10 10 USAABB03161 120030906A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 DIM. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20040113001212004011300121EA 2004 1 13 03359637 120031225A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27637BR 7308 DURING INSPECTION THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031125000972003112500097NM 2003 11 25 AALA20031288 120031117A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21790AN 30251 DFW BUSINESS CLASS SEATS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR BUSINESS CLASS SEATS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031219001282003121900128NM 2003 12 19 03FDEA02109 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE CORRODED. LT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031218001272003121800127EU 2003 12 18 MALA030519 120031121A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING E-CHECK INSPECTION. CABIN AFT FRAME STA 6586 WL 75 THRU 87 GOUGED. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER REPAIR IAW AND MESABA EO S53152. REFER TO 409 NR 1206073 FOR DETAIL. A/C RELEASE DATE IS 12/2/03. REFER TO 409 NR 1206073 FOR ADDITION INFO. 2L72 4T RTA52EU 20031219001182003121900118NM 2003 12 19 03FDEA02063 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73352, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031223000382003122300038NM 2003 12 23 SWAA032641 120031130A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 202, RBL 5 AND LBL 5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031223001042003122300104EA 2003 12 23 SWIA200312657 120031031A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07594SW 7285 PULLEY INTERCOSTAL ANGLE CRACK AT STA 484 RBL 27 O/B. REPAIRED INTERCOSTAL ANGLE IAW CRJ REO 601R-53-41-059 REV A & RII 53-401 ON RBL 27.0. P/N: 601R31171-9. 2L72 4F RTA21EA 20031229000082003122900008WP 2003 12 29 ABXA030471 120031202A5310J06011940 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23960AX 47762 SHEAR TIE FS 1056 LONGERON 14 RT CRACKED. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20031231001352003123100135SO 2003 12 31 C2XA03TY210 120031218A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714543 145553 DURING A SCHEDULED 1C INSPECTION THE LT FLOORBEAM WAS CORRODED. MAINT. REMOVED THE CARBON FIBER AT FR 20 AND FAB A NEW PART TO THE FLOORBEAM. ALODINED, PRIMED AND PAINTED AND REINSTALLED IAW SRM 53-21-10; CPM 51-21-04-05-06 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040106000062004010600006WP 2004 1 6 DHL2003802555 120031201A5754 SKIN DOUG DC8 DC873 302199CWP L/E SLOT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LT OUTER WING CENTER EXTENDED L/E SLOT LWR PLATING ELONGATED HOLES AROUND STA XFS 526.000 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA IAW ED EDU38-2 AND DWG U38-R02. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06,10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER, AND A FILLER IAW ED EDU38-2 AND DWG U38-R02. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B, APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED THE REPAIR PARTS ON CTR EXTENDED L/E USING NEW FASTENERS IAW ED EDU38-2 AND DWG U38-R02, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031014000342003101400034SO 2003 10 14 ENHA2003004 220030820A8530 PUSHROD TUBE CESSNA207 T207A 2073614CE CONT O520 IO520F 17032SO NR 6 CYLINDER CRACKED B ENHRO OTHER O OTHER NRNOT REPORTED 1 AL0348CF 323 20700366 814874R NR 6 CYLINDER EXHAUST PUSHROD TUBE HOUSING CRACKED, PUSHROD BENT. SUSPECT STUCK VALVE. 1H71 3O3 O A16CE E5CE 20031010000362003101000036EU 2003 10 10 USAABA03031 120030910A3350321430 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 0370 EPSU BATTERIES FAILED THE CAPACITY CHECK AT 12WL, 13WL AND 16WL. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20031124001442003112400144EA 2003 11 24 03289644 120031016A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27644BR 7379 DURING INSPECTION THE NR 2 EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031125001142003112500114SW 2003 11 25 2003F00617 120030910A2613 WARNING SYSTEM FRCHLDSA227 SA227DC 3377521SW COCKPIT MALFUNCTIONED A BSAAO OTHER N FALSE WARNING CRCRUISE 1 NM05854LS DC854B TIL - FLT 6014 - LT WING OVERHEAT LIGHT CAME ON DURING CRUISE, CREW TURNED OFF BLEED AND GENERATOR, LIGHT WENT OUT AFTER 2 MIN, 55 SEC. CREW LANDED AT DESTINATION STATION WITHOUT INCIDENT. DESTINATION STATION WAS THE CLOSEST AIRPORT AT THIS TIME. NO FAULT WAS FOUND. AS A NOTE, IF THE BLEED AIR HEAT IS LT ON HI IN MANUAL MODE, CABIN TEMP LIMITER IS RUNNING ON A DIFFERENT SENSOR AT A HIGHER SETTING, HIGH ENOUGH TO SET OFF THE WING OVERHEAT SENSOR. AWAITING FURTHER INPUT FROM THE CREW. INSPECTED LT WING AREA COVERED BY OVERHEAT SENSORS, GEN WIRING, AND BLEED LINES. NO DEFECTS WERE FOUND. PERFORMED OPERATIONAL CHECK, SYS OPS CHECK GOOD. NO FURTHER DEFECTS NOTED WITH THIS SYS IN THIS AIRCRAFT. (M) 2L72 4T RTA18SW 20031202001122003120200112SO 2003 12 2 SIMA200329704 120031020A532014522178005 SILL EMB 145 EMB145 3260210SO GALLEY SERV DOORCORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED SERVICE CENTER DOOR SILL. INSTALLED NEW SILL IAW EMB SRM, SRM EMB 145-1142 REV 23, CHAPTERS 51-40-02, 04, 05, 06, 07, 51-20-01 AND 51-20-03. (M) 2L72 4F RTT00011AT 20031204001012003120400101WP 2003 12 4 UPS03841412 120030911A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C3 AFT FUSE INTERIOR L17LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED CRACKED LONGERON END FITTING AND INSTALLED NEW FITTING IAW UPS DC8 SRM, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20031204001392003120400139WP 2003 12 4 ARWA20031001 120031014A27505751152503 LINK DOUG DC8 DC863F 302198FWP TE FLAP BROKEN A ARWAO OTHER O OTHER APAPPROACH 1 SO19784AL 46135 ON APPROACH, WHEN SELECTING FLAPS 23 DEGREES AIRCRAFT ROLLED TO THE LEFT WITH SPLIT FLAP INDICATION, ON POST FLIGHT FOUND RT INBOARD FLAP BRACKET BROKEN. RECORD FOR 27-268. REMOVED AND REPLACED RT INBOARD FLAP IAW MM 27-51-4. OPERATIONAL CHECK NORMAL IAW 27-50-0. 2L74 4F 4A25 20040122000622004012200062NM 2004 1 22 USAASB03218 120031219A21337110033 OUTFLOW VALVE BOEING737 7373B7 1384580NM CABIN PRESSURE FAILED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19522AU 23857 EN ROUTE FROM PIT TO IND, AT FL200, THE CABIN ALTITUDE WARNING HORN SOUNDED WITH NO AUTO FAIL LIGHT. CREW DESCENDED FLIGHT TO 12,000 FEET AND USED MANUAL AC TO CLOSE OUTFLOW VALVE BUT COULD NOT OPEN IT. CREW HAD TO USE MANUAL DC TO OPEN OUTFLOW VALVE. FLIGHT CONTINUED ONTO IND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFT OUTFLOW VALVE PER MM 21-31-11-400. OPS CHECK GOOD PER MM 21-31-00-1201. (M) 2L72 4F RTA16WE 20031208001252003120800125SO 2003 12 8 RAIA00310263 120031018A3260 CONNECTOR EMB 145 EMB145LR 3260212SO MLG LOOSE A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03816HK 145055 LANDING GEAR DISAGREE MESSAGE. MAINTENANCE SECURED LOOSE CONNECTOR ON RIGHT MLG UPLOCK BOX. 2L72 4T RTT00011AT 20031209001002003120900100NM 2003 12 9 SWAA032320 120031021A55116547985 RIB BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER RIB CHORD CRACKED AT STA 120.3. REPAIRED RIB ASSY PER SRM. 2L72 4F RTA16WE 20031204001792003120400179SO 2003 12 4 C2XA03TY183 120031020A531514521713003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING A SCHEDULED INSPECTION THE LEFT HAND FLOORBEAM AT FRAME 18 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031209001672003120900167NE 2003 12 9 CX7A194J0352 220030713A73206071T20P17 CONTROL UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE MALFUNCTIONED A CX7AA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL03307CE 340B204 ERRATIC RIGHT ENGINE TORQUE FLUCTUATIONS AS WELL AS ENG PSI FLUCTUATIONS. RAN ERRATIC ENGINE CHECKLIST, ENGINE SHUTDOWN AND OEI OPERATION. 2L72 4T4 TRTA52EU E8NE 20031210001622003121000162WP 2003 12 10 AALA20031381 120031203A3234 SWITCH DOUG DC9 DC982 3022082WP NLG FAILED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21236AA 49251 DFW T9602/03 EN ROUTE MSY-DFW NOSE GEAR DID NOT RETRACT. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE SWITCH AND RESERVICED NOSE GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20030919000702003091900070CE 2003 9 19 2003F00518 120030812A278050000083 CONTROL CABLE CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO LE FLAPS BROKEN E O OTHER F FLT CONT AFFECTED APAPPROACH 1 GL27402SS 402B0562 WHILE ON APPROACH AND EXTENDING FULL FLAP POSITION, THE PILOT HEARD A LOUD BANG AND THE AIRPLANE BEGAN TO ROLL LEFT. HE THEN RETRACTED THE FLAPS AND MADE AND UNEVENTFUL LANDING. 1L72 3O3 O A7CE E8CE 20030916000502003091600050CE 2003 9 16 52776 120030720A243523078019 STARTER GEN BEECH 1900 1900D 1154162CE ENGINE FAILED A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07237YV615 615 UE237 ON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RIGHT GENERATOR WOULD NOT STAY ON LINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED GENERATOR, GCU AND REPAIRED A WIRE ON THE GENERATOR. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20030919001422003091900142EA 2003 9 19 COMA0360373 120030817A291673021 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 2 OVERTEMP A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01712CA 7244 FLIGHT 9457 NR 2 HYDRAULIC SYSTEM HIGH TEMP CAUTION. REPLACED THE NR 2 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20030917001182003091700118CE 2003 9 17 ENHA200362C1 120030729A554012604187 BAR CESSNA207 207A 2073604CE CONT O520 IO520* 17032SO RUDDER CRACKED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL032162C 20700575 PILOTS FORWARD RUDDER BAR CRACKED AT LEFT RUDDER PEDAL POST. 1H71 3O3 O A16CE E5CE 20030922000542003092200054EU 2003 9 22 BRM2003F00000 120030805A73301178978301 SENSOR BOLKMS105 BO105LSA3 5626020EU FUEL PUMP FAILED E BRMAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 NM07315LS 767 2033 FORWARD TRANSFER PUMP ANNUNCIATOR LIGHT CAME ON. A PRECAUTIONARY LANDING WAS MADE. THE SYSTEM WAS CHECKED OUT AND IT WAS DETERMINED THAT THE DETECTOR, FUEL PUMP FAIL SENSING UNIT PN 117-89783-01 WAS THE CAUSE OF THE PROBLEM AND IT WAS REPLACED. 1G72 3U H3AU 20030923000202003092300020SO 2003 9 23 RAIA00308218 120030821A315080069925 WARNING SYSTEM EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03814HK6284 145046 TAKE OFF TRIM WARNING. MAINTENANCE REMOVED AND REPLACED AURAL WARNING UNIT. 2L72 4T RTT00011AT 20040128001202004012800120EA 2004 1 28 SWIA200312712 120031224A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07432SW4531 4531 7548 SPOILERONS FAULT STATUS ON TAKEOFF FROM COS, LEFT OUTBOARD SPOILERON SHOWS WHITE BOX. REMOVED AND REPLACED PCU IAW CRJ AMM 27-62-01. OPS CHECK GOOD, NO LEAKS NOTED. 2L72 4F RTA21EA 20040212000792004021200079NE 2004 2 12 MDR03024 120030812A5302642066345101 FITTING SKRSKYS64 S64F 8142610NE PWA JFTD12JFTD12A4A 52047NE T/R GEARBOX CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09179AC8212 64091 UPON POST-FLIGHT INSPECTION, FIELD MAINTENANCE PERSONNEL DISCOVERED THE LOWER FITTING TGB, PN 6420-66345-101, CRACKED AT THE AFT LOWER LEFT-HAND CORNER. THE CRACK IS APPROXIAMTELY .5000 INCH IN LENGTH AND TRAVELS THROUGH THE THICK WEB AND TURNS TOWARDS THE LOWER LEFT-HAND BARREL NUT RECESS OF THE TAIL GEARBOX FITTING (UPPER). CAUSE: UNKNOWN 2G72 4U4 U H6EA E15EA 20031015000372003101500037EA 2003 10 15 ASOA03420 120030907A2710600911777 CONTROL QUADRANT CNDAIRCL600 CL6002B19 1900309EA AILERONS DIRTY A ASOAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 SO11842AS 7304 DURING CLIMB-OUT FROM DFW-MOB, THE CREW EXPERIENCED THE AILERONS SHOWING SIGNS OF BINDING WHEN INITIATING LEFT TURNS. WITH SUFFICIENT INPUT THE AILERON POPPED FREE AND THE AIRCRAFT JERKED LEFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE INSPECTED THE LEFT AND RIGHT AILERON QUADRANTS INCLUDING THE LEFT AND RIGHT AILERON PULLEYS IN THE BRAKE AND POSITION SENSOR UNTI AREA. THE LEFT AND RIGHT AILERON QUADRANTS WERE FOUND TO BE SOILED AND GRITTY ON BOTH SIDES. MAINTENANCE CLEANED BOTH THE AILERON QUADRANTS AND PULLEYS IAW SERVICE LETTER NR RJ-SL-27-080. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031022000092003102200009NM 2003 10 22 F3LA200300139 120030920A5347 MOUNT BOEING737 73736E 138443ANM GE CFM56 CFM56* 13802NE LAVATORY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED LAVATORY MOUNT AT STA. 947.5, RBL 25, CORRODED. REPLACED MOUNT IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20030909001532003090900153NE 2003 9 9 S2YA03016 220030428A753202ND362033 BLEED VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE RT ENGINE INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13354SK4546 3126 DURING FLIGHT 2022, A CAS MESSAGE ILLUMINATED FOR RT ENGINE ANTI-ICE FAIL. THE CREW PERFORMED AN AIR TURNBACK. MECHANIC REPLACED THE BLEED AIR SHUTOFF VALVE AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DEFECTS. 2H72 4T4 FRTA55NM E35NE 20030909001572003090900157EU 2003 9 9 BAQA087756 120030625A26129560129980 FIRE DETECTOR AEROSPSA365 SA365N 8680669EU ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 6425 ENGINE COVERED UNDER WARRANTY. INOPERATIVE FIRE LIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20031027000822003102700082NM 2003 10 27 PCAA0310122 120031011A7603 SWITCH DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE COCKPIT DIRTY A PCAAEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER TOTAKEOFF 1 EA13980HA27325347 376 120988 SYR-FLIGHT NR 3629. CREW REPORTED THAT THE NR 2 ENGINE POWER UPTRIM PARTIALLY ACTIVATED DURING TAKEOFF. CREW EXPERIENCED REPEATED NR 2 ENGINE SURGING. ENGINE WAS SHUT DOWN, AND AIRCRAFT RETURNED TO SYR, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE POWER LEVER SWITCHES FOR THE PROPELLER AUTOFEATHER SYSTEM. OPERATIONAL CHECK DURING GROUND RUN OF AIRCRAFT WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031028000592003102800059SO 2003 10 28 C2XA03SH354 120030930A530014525480003 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 DURING C CHECK THE CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031028001052003102800105 2003 10 28 KBM2003F00002 420030823A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE VHF SYS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 RADIO REPORTED TO BE GARBLED. REPLACED WITH SERVICEABLE RADIO. 1G71 3U3 UNCH9EU E19EU 20031029000322003102900032NM 2003 10 29 USAABB03178 120030926A33501000679 LIGHT BOEING767 767201 1385125NM COCKPIT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 SNN - FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA1NM 20031110002032003111000203NM 2003 11 10 SWAA032229 120031005A53306545768 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031119001052003111900105NM 2003 11 19 CALA0300592 120031013A5754 SKIN BOEING737 7373T0 1384582NM NR 3 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 2 INCH CRACK IN LT WING NR 3 SLAT PANEL LOWER SKIN. A DOUBLER WAS INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20031119001352003111900135NM 2003 11 19 2003UALA00767 120031009A5730 ACCESS PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LT WING DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29369UA 24538 LEFT WING INBOARD FLAP LOWER ACCESS PANEL 8407L DAMAGED AT ATTACH HOLE COUNTERSINK. MAJOR REPAIR ACCOMPLISHED. REPLACED PANEL. 2L72 4F4 FRTA16WE E2GL 20040115001532004011500153NM 2004 1 15 03FDEA02154 120031209A5310 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 BS 720B STR 9 RT STR CLIP IS CRACKED. REMOVED CRACKED STR CLIP AT BS 720B STR 9 RT PER SRM 51-30-2. LOCATED, DRILLED, AND INSTALLED NEW STRINGER PER SRM 51-30-5, 51-30-6 AND 51-30-2. 2L73 4F RTA3WE 20040210001212004021000121WP 2004 2 10 ASAA0380758 120031118A532199365821 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FLOORBOARD MISSING INSERTS. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M) 2L72 4F RTA6WE 20031030001102003103000110NM 2003 10 30 03FDEA01553 120030916A5320A5A7114505 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 POSSIBLE CRACK AT STA 1541 STR SPLICE 44R. CTR CARGO STA 1541 STRINGER 44R CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20031110000462003111000046SO 2003 11 10 RAIA00310275 120031028A3020C1460092 ANTI-ICE VALVE EMB 145 EMB145 3260210SO NR 1 ENGINE DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03820HK11042 145064 5723-CID- ENGINE NR 1 AIR INLET ANTI-ICE INDICATION. MAINTENANCE DEFERRED NR 1 ENGINE ANTI-ICE VALVE PER MEL 30-21-01. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 ENGINE ANTI-ICE VALVE. 2L72 4F RTT00011AT 20040113000252004011300025NE 2004 1 13 HEEA087806 120030623A243229490001 BATTERY SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE MASTER OVERHEATED E HEEAK NONE O OTHER NRNOT REPORTED 1 SW03763P 760166 HOT LIGHT ILLUMINATED. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E19EU 20040113001902004011300190WP 2004 1 13 AALA20031188 120031028A2913314195 PUMP DOUG DC9 DC983 3022083WP LT ENGINE INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW219681B 53631 STL - FLT 1055 - EN ROUTE STL-SFO - ON CLIMB-OUT LEFT ENGINE HYDRAUILC PRESSURE LOW. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031120000392003112000039NM 2003 11 20 AWXA200301248 120030921A55116547993504 RIB BOEING737 737301 1384611NM HORIZONTAL STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON THE 8TH RIB FROM OUTBOARD END ON RT HORIZONTAL STABILIZER LEADING EDGE. MAINTENANCE CUT OUT CRACK ON RIB RT HORIZONTAL STABILIZER LEADING EDGE; FABRICATED A REPAIR ANGLE PER DWG 65-47993; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11, PG 1-6 FIG 1. 2L72 4F RTA16WE 20031121000732003112100073NE 2003 11 21 UPS03841568 220031118A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 1 FLAMED OUT A IPXAEA ENGINE SHUTDOWN UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO01894UP 46094 ENGINE NR 1 FLAMED OUT AT 30,000 FT DUE TO FUEL STARVATION. DID INFLIGHT ENGINE RESTART. ENGINE WINDMILLED FOR ABOUT 2 MINUTES. OK FOR SERVICE IAW AMM 71-00-00-5 PARAGRAPH 6B ABNORMAL OPERATION. NO DEFECTS NOTED. 2L74 4F4 FRT4A25 E2GL 20031124000612003112400061NM 2003 11 24 QXEA200301457 120031104A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 NR 5 SEAT TRACK HAS A CHAFE ON THE INBOARD FACE OF THE RIGHT HAND LUG .5 INCH AFT OF FORWARD END OF TRACK. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-507. 2H72 4T RTA13NM 20031223000422003122300042NM 2003 12 23 SWAA032663 120031204A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SPECIAL VISIT FOUND SHEAR TIE CRACKED BETWEEN STR L 13 AND L 14, BS 787. REPAIRED DAMAGE PER SRM. 2L72 4F RTA16WE 20031009000492003100900049SO 2003 10 9 SIMA20030808 120030724A335066368 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21733KR 145368 DURING OVERNIGHT MAINTENANCE, THE FLOOR PROXIMITY EMERGENCY LIGHTING AT SEAT 10A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHTS TRIPS IAW EMB MM. OPS CHECK WAS GOOD AND AIRCARFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040106001612004010600161EU 2004 1 6 03351320 120031217A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27320UE 41043 DURING INSPECTION THE RT AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031126001222003112600122NM 2003 11 26 ASAA0310441 120030512A78106547966506 SUPPORT ANGLE BOEING737 737290C 138448VNM NR 1 ENGINE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND NR 1 ENGINE TAILPIPE FAIRING AT THRUST REVERSER STATION 98.60 CHAFED. REPLACED ANGLE PER SRM. (M) 2L72 4F A16WE 20040311000262004031100026NM 2004 3 11 ASAA0310118 120030307A7110657377420 FRAME BOEING737 737298C 1384490NM NR 2 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 99 CHAFED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20031126000482003112600048EU 2003 11 26 MALA030488 120031103A302044730501 CONTROL MODULE SAAB SF340 340B 7860101EU DE-ICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15413XJ 340B413 AFTER TAKEOFF OF FLIGHT 2924, RIGHT INTAKE LIGHT ILLUMINATED. LIGHT ILLUMINATED 2-3 SECONDS AFTER SWITCH WAS TURNED ON. QRH COMPLETE, AIR RETURN TO DTW. MAINTENANCE REMOVED & REPLACED DE-ICE CONTROL MODULE P/N ON OFF 44730-501, S/N ON L248470, S/N OFF A00342. RAN AC FOR APPROX 15 MIN, ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20031202000532003120200053NM 2003 12 2 USAASB03189 120031016A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY SIGN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US 23988 FOUND R2 DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE M1136 POWER SUPPLY ASSEMBLY, CHARGER. (M) 2L72 4F RTA16WE 20031202001022003120200102EA 2003 12 2 ASOA03520 120031019A5320601R3501153 SEAL PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE CARGO DOOR SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DORO SEAL PLATE IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20031203000172003120300017NM 2003 12 3 GAIA03122ST 120031024A53117075T6 FRAME BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND AMIN CABIN FRAME DENTED BS 520 AT STRINGER 17 RT. REF FASI N/R NR 61416, CUT OUT DAMAGE 2.5 INCH BY 1.5 INCH INSTALLED DOUBLER REPAIR PER SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20031203001102003120300110EA 2003 12 3 ASOA03554 120031101A33506100928 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11707EV 10057 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121000522004012100052WP 2004 1 21 ASAA0380820 120031203A52105910081137 DOOR DOUG DC9 DC983 3022083WP PAX DOOR OUT OF RIG A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS53026 53024 SEA PREFLIGHT CHECK, FORWARD PAX DOOR DIFFICULT TO OPEN. RERIGGED DOOR. DOOR THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20031204000012003120400001WP 2003 12 4 GTIA030892 120030925A5755 SPOILER PANEL DOUG DC9 DC982 3022082WP LT WING DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND LEFT WING INBOARD FLIGHT SPOILER DELAMINATED AT REPAIR. REMOVED DAMAGED AREA. CUT CORE AND REPLACED LOWER SKIN IN DAMAGED AREA. (M) 2L72 4F A6WE 20031204001062003120400106WP 2003 12 4 UPS03841424 120030918A5310575036519 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AT FUSELAGE STA 700 (APPROX) INSIDE STRESS PANEL AREA, SHEAR TIE ON LT SIDE CRACKED. FABRICATED SHEAR TIE FROM MAT 7075-0.071 AND HEAT TREATED TO T-6 IAW DAC DWG 5750365 & TPS 1003 REV A FOR HEAT TREAT. LOCATED, DRILLED, AND DEBURRED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20031204000732003120400073SO 2003 12 4 C2XA03SH390 120031017A531014522226003 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 DURING C-CHECK THE CENTER BUTTSTRAP AT FR 59-60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031208000842003120800084SO 2003 12 8 C2XA03BT102 120031024A335066364 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715932 145015 CREW REPORTED, EMERGENCY AISLE PATH FLOOR LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY AISLE PATH FLOOR LIGHT STRIP IAW EMB145 MM 33-50-00. OPS CHECKED EMERGENCY LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031209000642003120900064NM 2003 12 9 SWAA032364 120031026A53306545890 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031210000192003121000019 2003 12 10 MWEA030473 420031203A3100MDISIS22 INDICATOR BOEING717 717200 1383700NM COCKPIT MALFUNCTIONED A MWEAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 GL31907ME 55171 INTEGRATED STANDBY INSTRUMENT SYSTEM INDICATOR TURNED WHITE AND WENT BLANK. COMPLIED WITH FIM 34-11-806 AND REVIEWED 30 DAY HISTORY WITH NO SIMILAR ENTRIES FOUND, SYSTEM OPERATIONS CHECK OK. 2L72 4F TRA6WE 20031210001022003121000102NM 2003 12 10 03FDEA01992 120031128A5712 RIB DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING LEADING EDGE SLAT TRACK NR 16 INBOARD SUPPORT RIB SUSPECT CRACK. LT WING LEADING EDGE SLAT TRACK NR 16 INBOARD SUPPORT RIB REMOVED AS PER SRM 51-31-01 VOL II AND NEW RIB INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040126000452004012600045NE 2004 1 26 ERAA091800 220030813A7320252464430N FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE LEAKING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03423EH15150 FUEL CONTROL LEAKING AT MAX FUEL FLOW ADJUSTMENT. DRIVESHAFT AND GOVERNOR WEIGHS QUITE OLD. OVERHAULED IAW MFG OHM FORM 15-602E. CEB'S 1357R1, 136719, 1382R1 AND SIL 26 EMBODIED. 1G72 4U4 U H4SW E22EA 20040122001102004012200110WP 2004 1 22 GTIA030970 120031118A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND CABIN STATION 1117 LBL 10 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040129000342004012900034EU 2004 1 29 MALA030579 120031227A5220 DOOR BAC 146 AVRO146RJ85A1500097EU EMERGENCY UNSECURE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15524XJ E2349 DURING FLIGHT 3687, F/A REPORTED THE RT FWD EMERGENCY EXIT DOOR UNARMED ITSELF INFLIGHT. UNABLE TO RE-ARM. MAINTENANCE INSPECTED NORMAL DOOR OPERATION NOTED, DOOR EVAC SLIDE ARMING OPERATED NORMAL SUSPECT AIRSTREAM DISARMED A PARTIAL CLOSED OUTSIDE DOOR HANDLE. NO PRESSURIZATION PROBLEMS INDICATED NO DOOR WARNING INDICATION. OPS CHECKS GOOD AT THIS TIME. 2H74 4F RTA49EU 20030916001182003091600118EU 2003 9 16 AALA20020438 120030404A2910A290114200066Y MANIFOLD AIRBUS300 A300B4605R 3930308EU MLG LEAKING A AALAO OTHER K FLUID LOSS CRCRUISE 1 SW217062A 474 EN ROUTE MIA-SJU, LOST GREEN HYDRAULIC QUANTITY SYSTEM. PERFORMED IN FLIGHT MANUAL GEAR EXTENSION. LANDED SJU WITHOUT FURTHER INCIDENT. REPLACED GREEN SYSTEM HYDRAULIC MANIFOLD ASSEMBLY. SERVICED GREEN HYDRAULIC SYSTEM. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20031210002012003121000201NM 2003 12 10 03FDEA01743 120031015A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE53392 20935 STA 1163 FLOORBEAM REPAIR NOT IAW STANDARD REWORK DRAWING. REWORKED FLOORBEAM REPAIR STA 1163 IAW EA 7-5310-55026 2L73 4F RTA3WE 20031210002142003121000214WP 2003 12 10 UPS03841546 120031023A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 1750 LONGERON 15R IS CRACKED. REMOVED DAMAGED SECTION BETWEEN STATION 1720 TO 1760,FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10 2L74 4F RT4A25 20031211000492003121100049WP 2003 12 11 ARWA20031101 120031109A324226014122 BRAKE ASSY DOUG DC8 DC863F 302198FWP MLG DAMAGED A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19784AL 46135 AIRCRAFT DOES NOT TAXI UNDER IT'S OWN POWER. FOUND NR 6 BRAKE ASSEMBLY DAMAGED. REMOVED AND REPLACED BRAKE ASSEMBLY IAW DC8 MM 32-42-1 AND MAIN WHEEL ASSEMBLY IAW MM 32-40-1. OPERATIONAL CHECK NORMAL. 2L74 4F 4A25 20031212001002003121200100NM 2003 12 12 SWAA032395 120031030A3350101114 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29712SW 27846 EMERGENCY EXIT LIGHT LENS MISSING NEXT TO R2 DOOR. SECURED LIGHT ASSY PER MX NOTE. 2L72 4F RTA16WE 20031215000932003121500093NM 2003 12 15 DHL2003745025 120031120A3240 BRAKE BOEING727 727224 1384076NM MLG CONTAMINATED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01745DH 20665 BRAKES ARE WEAK AND CAN BE APPLIED TO THE MECHANICAL STOPS. INSPECTED ACCUMULATOR FOR PROPER PRE-CHARGE, FOUND OK PER BMM 12-15. BLED BRAKES IAW B727 M/M 32-41-12 & 12-15-01. BRAKES OPERATE NORMALLY DURING RAMP TAXI CHECK. 2L73 4F A3WE 20030813001152003081300115WP 2003 8 13 GTIA030564 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND FORWARD CABIN STATION 200 RBL 44 TO 23 INCHES FLOOR SUPPORT CORRODED. FABRICATED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030815000772003081500077SW 2003 8 15 HEEA088455 120030520A6520206040402105 GEARBOX BELL 206 206L3 1182108SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108PH21489 51334 TAIL ROTOR GEARBOX HAS CORROSION ON INSIDE DIAMETER OF OUTPUT SHAFT; BINDING. REPLACED OUTPUT SHAFT 206-040-439-001, S/N A-FS6642 DUE TO EXCESSIVE CORROSION; CONTROL TUBE 206-011-724-109 DUE TO EXCESSIVE CORROSION. REPAIRED. 1G71 3U H2SW 20030820001392003082000139NM 2003 8 20 CALA0300405 120030724A532065C161216 BRACKET BOEING737 737524 1384721NM GIRT BAR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND L-1 DOOR GIRT BAR AFT LATCH ATTACH BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02. 2L72 4F RTA16WE 20030819000292003081900029NM 2003 8 19 AALA20030604 120030519A5730 SKIN BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21368AA 25195 FOUND CORROSION ON WING CTR SECTION, UPPER SKIN STATION 955 BETWEEN BL0 AND LBL 10 MINIMUM THICKNESS AFTER BLEND ON AFT EDGE O.144 INCHES. REMOVED FASTENERS IN AFFECTED AREA AND REMOVED CORROSION, PERFORMED EDDY CURRENT INSPECTION. REWORKED AREA WITH FLAP PEEN AND FINISHED PER SRM 51-20-01. REINSTALLED FASTENERS AND APPLIED FUEL BARRIER. (M) 2L72 4F RTA1NM 20030328000612003032800061NM 2003 3 28 CALA0300105 120030307A335020121 CHARGER BOEING757 757224 1384958NM CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW0918112 27302 INSPECTION FOUND EMERGENCY LIGHTS AT SEATS 12-16 INOPERATIVE. THE EMERGENCY LIGHT BATTERY CHARGER WAS REPLACED AND THE LIGHTS TESTED GOOD. 2L72 4F RTA2NM 20030820000282003082000028NM 2003 8 20 03FDEA00794 120030522A5753NRC6753503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 SNRM N1069 : LT WING FOUND LT OUTBOARD FLAP, INBOARD AFT HINGE FITTING TO FLAP LOWER AFT, FWD MOST HOLE QTY 01 EACH WITH SUSPECTED CRACK. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATISFACTORY. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP. 2L73 4F RTA22WE 20030401000552003040100055EA 2003 4 1 CA030221005 120030217A5610NP1393213 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE COCKPIT BROKEN W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 11696 (CAN) WHILE TAXIING, CAPTAINS WINDSHIELD SHATTERED. TEMP -26, THIS WAS THE ORIGINAL WINDSHIELD. WINDSHIELD TOTAL TIME 11,696 2L72 4F4 FRTA21EA E15NE 20030408000722003040800072NM 2003 4 8 03FDEA00371 120030402A3260 UPLOCK SWITCH BOEING727 727200 138407ENM NLG INOPERATIVE A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25265FE 21671 FLIGHT TEST. AIR BORNE WITH GEAR UP AND LDG GEAR HANDLE IN OFF POSITION, RED NOSE GEAR LIGHT COMES ON BRIGHT, AND GREEN NOSE GEAR LT COMES ON DIM. NO OTHER GEAR OR DOOR LIGHTS ON. NO LIGHTS ON S/O PANEL. LOG BOOK ENTRY REQ. UPON TROUBLESHOOTING NLG FOUND LOCK & POSITION SWITCH TO BE INOP. REMOVED AND REPLACED NLG LOCK & POSITION SWITCH IAW FED-EX M/M 32-61-071-4. PERFORMED OPERATIONAL TEST IAW FED-EX M/M 32-33-000-5. CHECKED OUT GOOD. SWITCH ROBBED FROM A/C N266FE. 2L73 4F RTA3WE 20030404000222003040400022NM 2003 4 4 DHL2003742008 120030402A2611 SMOKE DETECTOR BOEING727 727225 1384077NM CARGO BAY MALFUNCTIONED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01742DH 21290 "CARGO SMOKE" WARNING LIGHT ILLUMINATED DURING CLIMBOUT. COMPLETED EMERGENCY CHECKLIST AND RETURNED TO MIA. REMOVED AND REPLACED NR 2 SMOKE DETECTOR PER B727 M/M 26 PAGE 23. OPS CHECKED NORMAL. NO DEFECTS NOTED. 2L73 4F A3WE 20030401001422003040100142WP 2003 4 1 DHL2003804551 120030213A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 "C" CARGO DOOR LWR EXTERIOR SKIN WITH 2EACH INTERIM REPAIRS ON IT. (FS 1200.000-1260.000 PERFORMED MAJOR REPAIR IAW EO DHL 030111 , ED-3218. REMOVED FASTNERS IAW 51-1-21 PG. 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030111, ED-3218. FABRICATED A REPAIR SKIN SEGMENT (7075T6AL.050) AND A DOUBLER SPLICE (7075T6AL.063)IAW EO DHL 030111 , ED-3218. CLEANED , TREATED , AND PRIMED IAW SRM51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW IAW SRM51-1-15 PG 1 . INSTALLED NEW SKIN IAW EO DHL 030111 , ED-3218. INSTALLED NEW FASTNERS IAW SRM51-1-21 PG. 1 SEE N/R 0244 FOR "C" CARGO DOOR REMOVAL & INSTALLATION. 2L74 4F RT4A25 20030403001062003040300106NM 2003 4 3 DL72S030222 120030305A5312 BULKHEAD BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27523DA 21583 INSPECTION OF THE FS 1183 BULKHEAD AFT ENTRY DOOR FRAME AT RBL 17.8 PER AD 99-18-05 REVEALED A CRACKED FASTENER HOLE AT WL 273. THE CRACKED HOLE WAS OVERSIZED TO REMOVE ALL CRACK INDICATIONS AND AN ADDITIONAL OVERSIZING INSURANCE CUT WAS MADE. AN OVERSIZE FASTENER WAS INSTALLED TO FILL THE LARGER HOLE. THE WORK WAS ACCOMPLISHED PER ER/A 384658-14AD. 2L73 4F A3WE 20030404001512003040400151NM 2003 4 4 SWAA030532 120030310A33506556633 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EXIT EMERGENCY LIGHT INOP. RELAMPED PER MM. 2L72 4F A16WE 20030415001022003041500102EU 2003 4 15 CA030403001 120030402A2910AE7060322 HOSE AIRBUS310 A310300 3930305EU MLG DAMAGED W O OTHER K FLUID LOSS CRCRUISE 1 CA (CAN) AIRCRAFT LOST GREEN HYDRAULIC FLUID DURING FLIGHT . DURING TROUBLE SHOOTING , THE RT MLG TRUCK POSITION ACTUATOR FLEX HOSE WAS FOUND PERFORATED UNDER THE BRADED SURFACE . THE HOSE ASSY WAS REPLACED AND THE SYSTEM WAS TESTED SERVICEABLE. 2L72 4F RTA35EU 20030424000812003042400081NM 2003 4 24 XNOA01109 120030325A2752 FLAP BOEING727 727227 1384078NM WINGS MALFUNCTIONED A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23793A 20774 AFTER T/O FROM DAY, OUTBOARD FLAPS WOULD NOT RETRACT PAST 5 DEGREES. ALL APPLICABLE ENA EMERG/ABNORMAL PROCEDURES COMPLETED. AIRCRAFT RETURNED TO DAY. INSPECTED FLAP SYSTEM. NO DEFECTS NOTED. RESET SYSTEM. OPS CHECK SYSTEM SEVERAL TIMES. OPS CHECK GOOD IAW 727 MM 27-52-0. 2L73 4F A3WE 20030917000642003091700064SW 2003 9 17 ALGA089067 120030909A6510407340340103 DISC PACK BELL 407 407 1182206SW T/R DRIVESHAFT BROKEN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03647AL186 53357 2EA. DISC. BROKEN IN ASSY. REMOVED AND REPLACED, BY FIELD MAINT. 1G71 3U O H2SW 20030923000722003092300072WP 2003 9 23 DHL2003604734 120030615A5730 PLATE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT INNER WING L/E AUX TANK UPPER PLATING SHOW HOLES FOR DOUBLER REMOVAL. PERFORMED MAJOR REPAIR IAW EODHL-030577, ED-3426. REMOVED ALL EVIDENCE OF CORROSION FROM REPAIRED AREA IAW SRM 51-1-8 PG 17-18. PLUGGED EXISTING HOLES WITH RIVETS IAW EODHL-030577, ED-3426. FOR LEAK CHECK SEE N/R 3824. 2L74 4F RT4A25 20030923001232003092300123WP 2003 9 23 DHL2003604660 120030528A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR LE UPPER PLATING HAS CORROSION AND INTERIM REPAIR FROM STA XFS 341.500 TO XW 257.000). REMOVED INTERIM REPAIR AND FASTENERS. REMOVED CORROSION ON LT WING CTR L/E UPPER PLATING. FOUND OUT OF LIMITS. TRIMMED OUT THE CORROSION SKIN AREA IAW EO DHL 030560, ED 3388. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER (7075-T6AL 0.071), TWO FILLERS (7075-T5AL 0.063) IAW EO DHL 030560, ED 3388. CLEANED TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE AND FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLER AND FILLERS ON LT WING CTR LE UPPER FLARING STA XFS 341.500 TO XW 257.000 USING NEW FASTENERS IAW EO DHL 030560, ED 3388 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923001612003092300161NM 2003 9 23 AALA20030822 120030729A2420 FILTER BOEING767 767323 1385205NM IDG CLOGGED A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW21361AA 24042 ON DEPARTURE CLIMB-OUT, THE GENERATOR LIGHT FLICKERED WITH ACCOMPANIED EICAS MSG RT GENERATOR DRIVE, DISCONNECTED RIGHT GENERATOR. CHECKED RT IDG AND FOUND OIL OVER FILLED AND DIFF PRESS POP OUT. REPLACED OIL IDG PRESS FILTER AND SERVICED IDG IAW MM 12 RUN UP PERFORMED ALL INDICATIONS ARE NORMAL OK FOR SERVICE. NO DEBRIS FOUND. (M) 2L72 4F RTA1NM 20040127001452004012700145NM 2004 1 27 ASAA0310190 120030321A5751654652014 FITTING BOEING737 737298C 1384490NM AILERON CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND RIGHT AILERON NR 1 HINGE FITTING AT WING STATION 517.757 CRACKED. REMOVED DAMAGE, FORMED, FABRICATED ADN INSTALLED REPAIR ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040205001032004020500103CE 2004 2 5 FPI2003F00013 120031107A7921654585 OIL COOLER CESSNA210 T210N 2073456CE CONT O550 IO550* SO ENGINE CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO152145U370 21064776 821012R BOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION. 1H71 3O3 O 3A21 E3SO 20040210000442004021000044CE 2004 2 10 DXTA200300170 120031121A3222 LANDING GEAR CESSNA560 560XL 2076702CE NOSE MALFUNCTIONED E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07632QS 5605132 DURING APPROACH TO HXD FOUND NOSE LANDING GEAR WOULD NOT COME DOWN, DIVERTED TO SAV. AIRCRAFT LANDED WITH NLG PARTIALLY EXTENDED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040211000072004021100007WP 2004 2 11 AMTA200301459 120031204A3350 CONNECTOR LKHEED1011 10113853 5265020WP EMERGENCY LIGHT LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 FOUND EMERGENCY PATH LIGHT AT AFT GALLEY FLOOR INOPERATIVE. CLEANED AND RESECURED PATH LIGHT CONNECTION AT AFT GALLEY FLOOR. OPS CHECK GOOD, REF MM 33-50-01. (M) 2L73 4F A23WE 20040212001182004021200118NM 2004 2 12 UIA9213 120031213A2910AN81510D COUPLER DHAV DHC8 DHC8301 1386003NM HYD SYSTEM BROKEN Z O OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 TW0015221 325 NR 1 ENG HYD PUMP CAUTION LIGHT ILLUMINATED AFTER LANDING. CHECK FOUND PRESSURE MANIFOLD UNION NR 10 (B) NUT BROKEN. REPLACED A PRESSURE MANIFOLD UNION NR 10 AND GROUND ENG RUNUP CHK NML. NO HYD LEAK . 2H72 4T RTA13NM 20040301000062004030100006GL 2004 3 1 ALG2004F00001 220031111A7310 B-NUT CESSNASTC STC206C 1182107CE ALLSN 250C 250C28 03013GL FUEL CONTROL LOOSE A ALGAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03211EL 45251 CAE860764 IN FLIGHT SMELLED SLIGHT ODOR OF FUEL. ON POST FLIGHT SAW DRIPS OF FUEL ON LINES AROUND FUEL CONTROL. MAINTENANCE FOUND B-NUT ON FUEL CONTROL INLET FROM PUMP SEEPING. LOOSENED NUT, CLEANED FITTING AND RETORQUED NUT. LEAKED CHECKED WITH BOOST PUMPS AND GROUND RAN AIRCRAFT FOR APPROX. 15 MINUTES NO OTHER SEEPS DETECTED. 1H71 3O3 UNTA4CE E1GL 20040304001462004030400146NM 2004 3 4 ASAA0340336 120031027A33978100022608 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01754AS 25095 SEA - DURING RON CHECK, FOUND ROW 14 TO ROW 17 EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LOOSE WIRES, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040308001992004030800199NM 2004 3 8 ASAA0310597 120031031A33508621004 BATTERY PACK BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 14-15 WILL NOT EXTINGUISH. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040416000222004041600022WP 2004 4 16 ASAA0380736 120031111A53305924802517 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN DENTED FORWARD OF NR 1 WINDOW. REMOVED EXISTING DOUBLER. INSTALLED NEW SKIN DOUBLER, FINER DOUBLER AND STRAPS PER SRM 53-04, 51-10-3, AND 51-30-2. (M) 2L72 4F RTA6WE 20030925000792003092500079NM 2003 9 25 AALA20030891 120030820A3610CON5114 SHUTOFF VALVE BOEING767 767323 1385205NM RT ENGINE LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21382AN 25451 RT ENGINE HPSOV EICAS MSG APPEARED IN FLIGHT, COMPLIED WITH QRH PROCEDURE. PLACARDED RT ENGINE HI STAGE HPSOV INOPERATIVE PER MEL. VALVE SECURED CLOSED PER MPM 36-02. ENT IN MIC SHEET AUTH 8 463DC. SECURED LOOSE SENSE LINES AT HP CONTROLLER CLEANED AND LUBED POSITION SWITCHES PERFORMED OPERATIONAL CHECK FOND NORMAL RESTORED TO NORMAL CONFIGURATION. (M) 2L72 4F RTA1NM 20071001000152007100100015SO 2007 10 1 C2XA07IA212 120030922A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27125633160 3160 145612 IAH - DURING A-CHECK INSPECTION THE AISLE PATH LIGHTING FROM SEAT 8A TO 12A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030818000192003081800019 2003 8 18 HEEA088375 420030714A34168503S20LW INDICATOR SKRSKYS76 S76A 8143006NE ALTIMETER READS HIGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 ALTIMETER INDICATOR READS 150 FT HIGH. 1G72 3U H1NE 20030819000242003081900024NE 2003 8 19 AMTA200300928 220030714A7310 FITTING BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LT ENG FUEL LEAKING A AMTAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11522AT 29330 31604 FUEL LEAK, LT ENGINE. ENGINE SHUTDOWN FOR ONE HOUR AND FOUR MINUTES. OIL PRESSURE POSITIVE. RESECURED HIGH PRESSURE FUEL LINE FITTING. LEAK CHECK AND TEST RUN OK, ALL INDICATIONS NORMAL. (M) 2L72 4F4 FRTA2NM E12EU 20030819000612003081900061SO 2003 8 19 SWIA200312108 120030618A5753 ROLLER EMB 120 EMB120ER 3260203SO TE FLAP BINDING A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07186SW 120034 OUTBOARD FLAP DISAGREEMENT DURING FLAP RETRACTION. RESET BY SLOWING TO APPROX 140 AND RESETTING LEVER. FOUND RIGHT OUTBOARD FLAP LOWER MOVEABLE CHANNEL MISSING ROLLER AND FLAP WAS BINDING. INSTALLED NEW ROLLER AND SUPPORT BRACKET IAW MM 57-52-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030819000852003081900085NM 2003 8 19 751PA0018 120030703A3350 FLASHLIGHT BOEING757 757200 1384950NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 EMERGENCY FLASHLIGHT AT L3 DOOR INOP. REPLACED FLASHLIGHT ASSEMBLY. 2L72 4F RTA2NM 20030819000842003081900084 2003 8 19 SWIA200312218 420030725A3418501125904 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA STICK PUSHER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07447SW 7677 STALL FAIL CAUTION MESSAGE DISPLAYED. REMOVED AND REPLACED STICK-PUSHER ACTUATOR IAW MM 27-35-00. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030331001002003033100100 2003 3 31 CALA0300149 420030327A25655262100 ACTUATOR BOEING767 767224 1385170NM SLIDE INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW097615110116 30430 THE FORWARD AND AFT DOOR ACTUATORS FOR THE RT SIDE OFF-WING SLIDE DOOR WERE FOUND EXPENDED. THE DOOR ACTUATORS WERE REMOVED AND REPLACED IAW MM 25-65-10. 2L72 4F RTA1NM 20030401000122003040100012NM 2003 4 1 250TR0009 120030326A33501000679 LIGHT BOEING737 7372K5 138448XNM CABIN MALFUNCTIONED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 EMERGENCY EXIT LIGHT COMES ON WHEN POWER IS SWITCHED OFF AND EMERGENCY EXIT SWITCH IS IN OFF POSITION. REPLACED RT FWD EMERGENCY EXIT LIGHT ASSY AND OPS CHECK PER MM 33-51-11. 2L72 4F RTA16WE 20030401000142003040100014WP 2003 4 1 AALA20030001 120030103A3350 LIGHT DOUG DC9 DC982 3022082WP EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21293AA 49305 DURING OVERNIGHT MAINTENANCE, RT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RT EXTERIOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000222003040100022WP 2003 4 1 AALA20030236 120030224A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170401 49312 DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT AISLE SEAT LIGHT AT SEAT 26D INOPERATIVE. PLUGGED EMERGENCY EXIT LIGHT WIRE IN TO RECEPTACLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030821002462003082100246WP 2003 8 21 03FDEA01335 120030818A5350AKC70111 HINGE DOUG DC10 DC1010 3022110WP TAILCONE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 DOORS - SERVICE - TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC7011-1. COMPLY WITH EA 8-5240-72249 REV NR POS ENT BY: 402783. FACT 18AUG03 23:02 BFM R COMPLIED WITH EA 8-5240-72249 DOORS - SERVICE- TAIL CONE- PATIO DOOR HINGE REPAIR P/N AKC 7011-1 AT MAE. 2L73 4F A22WE 20030822000202003082200020 2003 8 22 03FDEA01040 420030704A3140 COMPUTER DOUG DC10 DC1030 3023501WP E/E BAY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25316FE 48314 AFTER TAKEOFF AT 1000 FEET AGL HAD RED MANIFOLD FAIL NR 2, RTB IN ACCORDANCE WITH QRH. RESET MANIFOLD FAILURE DETECTION LOOP NR 2 CIRCUIT BREAKER. PER SMP. PERFORMED AIR TEST, PASSES PER MM 36-23-01-5. RAN NR 2 ENGINE OP'S CHECK NORMAL 181623 PER JRH. REMOVED AND REPLACED NR 1 AVIONICS INTERFACE UNIT PRECAUTIONARY PER MM 31-43-02-4. PERFORMED AIR PREFLIGHT TEST SYSTEM CHECKS NORMAL JRH INTERIOR CHECK. 2L73 4F A22WE 20030404000042003040400004WP 2003 4 4 ABXA030121 120030403A5610 LOCK DOUG DC9 DC933F 302207AWP WINDOW BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING PRE "D" CHECK, MAINTENANCE FOUND THAT THE FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND THE UPPER LOCK BAR BROKEN. REMOVED AND REPLACED THE UPPER LOCK BAR AND ADJUSTED IAW DC-9 MM 56-10-03-5. OPS CHECKED GOOD. 2L72 4F A6WE 20030407000522003040700052NM 2003 4 7 MEX2003016 120030129A3150 WARNING SYSTEM BOEING757 7572Q8 1384972NM COCKPIT MALFUNCTIONED A ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23805AM 26272 FLT 600 - MEX-ALT - AIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, MESSAGE EICAS STATUS MAIN BATTERY CHARGE. RESET PROCEDURE WAS PERFORMED AND MESSAGES WAS ERASED, BUT WHEN BATTERY AND BARS WERE DISCONNECTED MESSAGES EICAS STATUS LEFT AND RIGHT CONTROL VALVE APPEARS, IT WS NOT POSSIBLE RESET AND ENGINES WERE SHUTDOWN. RESET PROCEDURE WAS PERFORMED AND MESSAGES WERE ERASED. ENGINES STARTED IAW MM 24-31-00, ALL CORRECTED. (M) 2L72 4F RTA2NM 20030410000982003041000098NM 2003 4 10 SWAA030670 120030321A533065C27257 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER AFT CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030416001322003041600132NM 2003 4 16 DL76S030270 120030323A2560MV10 MEGAPHONE BOEING767 767332 1382001NM F/C CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27128DL 24078 FIRST CLASS MEGAPHONE INOP. REPLACED FIRST CLASS MEGAPHONE. 2L72 4F RTA1NM 20030425000142003042500014 2003 4 25 MALA030210 420030327A3414 INDICATOR SAAB SF340 340B 7860101EU AIRSPEED FROZEN A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15360PX 340B220 DURING CLIMBOUT ON FLIGHT 2790, F/O'S AIRSPEED INDICATOR FROZE AT 260 KNOTS. AIR RETURN TO MSP. MAINTENANCE DRAINED AND PURGED NR 2 PITOT SYSTEM WITH DRY NITROGEN. NR 2 PITOT SYSTEM OPS CHECK GOOD AND LEAK CHECKS GOOD IAW SF340 M/M CHAP 34. 2L72 4T RTA52EU 20030424001242003042400124WP 2003 4 24 UPS03840346 120030324A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01. 2L74 4F RT4A25 20030428001702003042800170WP 2003 4 28 03FDEA00409 120030408A5420 ANGLE DOUG DC10 DC1030 3023501WP NR 3 PYLON BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25317FE 46835 NR 3 PYLON TOP PANEL 487 RT, RT SIDE NUT PLATE L-ANGLE BROKEN. REMOVED BROKEN ANGLE IAW SRM 51-31-01. REMOVED DOUBLER IAW SRM 51-31-01. FABBED NEW DOUBLER IAW DPS 4.710, TREATED AND PRIMED DOUBLER IAW SRM 51-21-01. DRILLED UP NEW ANGLE T2/325729 IAW SRM 51-31-01. TREATED AND PRIMED NEW ANGLE IAW SRM 51-21-01. INSTALLED ANGLE AND DOUBLER IAW SRM 51-31-01. 2L73 4F A22WE 20030429000602003042900060SO 2003 4 29 SWIA200311866 120030330A3350 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSBLOWN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07284YV 120284 EMERGENCY LIGHTS AT ROW 6 DOOR, AND FLOOR LIGHTS BETWEEN ROW 3 AND 6, FOUND INOPERATIVE DURING F/A PREFLIGHT CHECKS. REPLACED ROW 6 EMERGENCY LIGHTS FUSE. OPS CHECK GOOD. 2L72 4T RTA31SO 20030501001812003050100181NM 2003 5 1 ASAA0310067 120030301A532065596582 DOUBLER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AFT AIRSTAIR INTERCOSTAL DOUBLER AT BS 947-967, LEFT BUTTOCK LINE 51.5 CORRODED. REMOVED AND REPLACED DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20030502000332003050200033WP 2003 5 2 ASAA0380138 120030215A5321993654715 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, CABIN FLOOR PANEL TO HAVE 16 CORRODED INSERTS FROM FS 160-180. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030501001382003050100138NM 2003 5 1 ASAA0310045 120030226A575465C26272 SKIN PANEL BOEING737 737210C 1384459NM LT WING LE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND LEFT WING LEADING EDGE SKIN PANEL AT WS 329 CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PER EA. (M) 2L72 4F A16WE 20030505002392003050500239NM 2003 5 5 03FDEA00544 120030418A5320 PANEL BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FORWARD CARGO FORWARD BULKHEAD UPPER LEFT PANEL STA 480 HAS A HOLE. INSTALLED DOUBLER AND 1 EA FILLER IAW BOEING 727-200 SRM 53-10-9. 2L73 4F RTA3WE 20030506000432003050600043EA 2003 5 6 COMA0360204 120030418A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A COMAC ABORTED TAKEOFF JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 SO01976CA16159 7151 FLIGHT 5748 STAB TRIM CAUTION MESSAGE. REPLACED THE HSTCU. 2L72 4F RTA21EA 20030508000392003050800039NM 2003 5 8 CH1A200395034 120030411A5320 FLOOR SUPPORT BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON FLOOR SUPPORT AROUND FASTENER HOLES AT R2 DOOR SILL AREA RBL 62 F-S 1040 TO F-S 1070 2L73 4F A3WE 20030530001232003053000123NM 2003 5 30 2003F00353 120030427A2611 WARNING LIGHT DHAV DHC8 DHC8103 1386005NM CARGO SMOKE ILLUMINATED A KPVAO OTHER N FALSE WARNING APAPPROACH 1 WP13808WP 026 BAGGAGE SMOKE WARNING IN FLIGHT. FLIGHT ATTENDANT CHECKED BAGGAGE COMPARTMENT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. COMPLIED WITH WALK AROUND INSPECTION AND HAVE DETERMINED THIS AIRCRAFT TO BE IN SAFE CONDITION FOR A FERRY FLIGHT FROM MKK TO HNL ONLY IAW GMM CHAPTER 4 PAGE 4.7 TO 4.10. RE-LAMPED NR 2 BAGGAGE SMOKE DETECTOR IAW 8 CMM 26-10-21 SECTION 60 PATE 7. OPS CHECK GOOD IAW 8 MM 26-12-00 PAGE 201 SECTION A. NO DEFECTS FOUND. (M) 2H72 4T RTA13NM 20030602000422003060200042CE 2003 6 2 CA030423006 120030423A55110432001646 RIB CESSNA150 150L 2071826CE CONT O200 O200A 17020SO HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 11809 (CAN) LEADING EDGE RIB ASSEMBLIES ARE VERY DIFFICULT TO SEE.THE USE OF A MIRROR THROUGH THE HORIZONTAL SPAR AND RIB LIGHTNING HOLES IS THE ONLY WAY TO SEE THE CRACKS ALONG THE TABS.WE BELIEVE THE RIBS ARE CRACKING DUE TO IMPROPER GROUND HANDLING.THE PRACTICE OF PUSHING THE AIRCRAFTS TAIL DOWN BY ITS SPAR IN ORDER TO ROTATE THE AIRCRAFT IN POSITION MAY BE DAMAGING THESE RIBS. BOTH RIBS WERE REPLACED WITH NEW.THE TAIL SURFACES WERE REMOVED AND RE-INSTALLED. 1H71 3O3 O 3A19 E252 20030514000132003051400013NM 2003 5 14 AALA20030358 120030323A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21681AA 25338 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE FLOOR LIGHT INOPERATIVE. REPLACED WIRE FROM SIDEWALL TO EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030520000832003052000083NM 2003 5 20 AMTA200300492 120030410A3350 COVER LKHEED1011 1011 N/A-SDRNM EMERGENCY LIGHT MISSING A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11195AT 193C1041 EGRESS TRACK MISSING COVER PLATES AT SEATS 4 ABC, 5ABC, 4HJK, AND 12HJK. INSTALLED COVER PLATES AS REQUIRED. (M) 2L73 4F RTA23WE 20030515000712003051500071SO 2003 5 15 SWIA200311925 120030429A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07393SW4712 4712 120330 EMERGENCY EXIT LIGHTS OPERATE INTERMITTENTLY FROM F/A STATION AND FLIGHT DECK. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY IAW 33-50-00. OPS CHECK OK. 2L72 4T RTA31SO 20030606001002003060600100EU 2003 6 6 CX7A194J0344 120030513A2731NAS620417D BOLT SAAB SF340 340B 7860101EU SEIZED A CX7AO OTHER J WARNING INDICATION CRCRUISE 1 GL03312CE 340B334 BOLT SEIZED AND PRODUCE PITCH TRIM LIGHT ILLUMINATED IN FLIGHT. 2L72 4T RTA52EU 20030521000482003052100048WP 2003 5 21 DHL2003804902 120030125A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 366.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON LT WING CTR L/E FORMER UPPER PART AT XFS 366.500 WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521000582003052100058WP 2003 5 21 DHL2003801005 120030425A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 FWD SERVICE DOOR JAMB WITH 2.000 INCH CRACK IN AFT LWR CORNER STA 180.000 L-20R- L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG SR08530021, SRM 53-2-0 FIG 14. CUT OUT DAMAGED AREA IAW DWG DACCO SR08530021, SRM 53-2-0 FIG 14. FABRICATED FILLER, DOUBLER (7075-T6 0.063) AND TRIPLER (7075-T6 0.080) IAW DWG DACCO SR08530021, SRM 53-2-0 FIG 14. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER, DOUBLER AND TRIPLER WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, DWG DACCO SR08530021, SRM 53-2-0 FIG 14, SRM 51-1-21 PG 1 AND SRM 51-1-21A PG 1-4. 2L74 4F RT4A25 20030521001082003052100108WP 2003 5 21 DHL2003801027 120030419A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 LT WING OUTBOARD STUB WING FORMER CRACKED, STA XS 520.168. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (7075-T6 0.090) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030522000712003052200071SO 2003 5 22 C2XA03TY065 120030517A541214547494403 FIREWALL EMB 145 EMB145LR 3260212SO NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED A DOUBLER AND INSTALLED IAW EC5330-01250. THE REPAIR IS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2L72 4T RTT00011AT 20030521000322003052100032WP 2003 5 21 DHL2003604526 120030502A5310 GUSSET DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT - GUSSET CRACKED 0.250 AT STA 1347.000, L-7R. REMOVED CRACKED GUSSET IAW SRM 51-1-21 PG 2. FABRICATED NEW GUSSET (7075-T6 AL0.071) IAW SRM 53-2-0 PG 2. CLEANED, TREATED AND PRIMED AREA AND NEW GUSSET IAW SRM 51-1-8B. INSTALLED NEW GUSSET IAW SRM 53-2-0 PG 2, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030612000642003061200064EA 2003 6 12 SWIA200312038 120030526A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07588SW 7069 FLAPS EXTENDED 41 DEGREES DURING APPROACH. AFTER LANDING THE FLAPS OSCILLATED BETWEEN 45 AND 42 DEGREES. OPERATED AND INSPECTED FLAP PANELS & ACTUATORS. INTERROGATED FECU & FCC DIAGNOSTIC SYSTEMS. FOUND TO BE OPERATING NORMALLY ON THE GROUND. OPS CHECKS GOOD AT THIS TIME IAW CL600 MM 27-51-06. 2L72 4F RTA21EA 20030617001822003061700182NM 2003 6 17 QXEA200300589 120030505A5210 HINGE FITTING BOMBDRDHC8 DHC8401 1390041NM PAX DOOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - AFT PASSENGER DOOR, MAIN HINGE, BOTTOM FUSELAGE ATTACH POINT, BOTTOM LUG HAS CHAFE. REPAIRED IAW HORIZON AIR EA 6-52-288. 2H72 4T RTA13NM 20030618000072003061800007SW 2003 6 18 HEEA087485 120030612A6240M835362028M RELAY BELL 407 407 1182206SW ROTOR HORN MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03724PH 53327 RELAY CAUSING DEGRADE LIGHT. 1G71 3U O H2SW 20030523000312003052300031NM 2003 5 23 AWXA200300572 120030416A531165479602 FRAME BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON BS 847 FRAME LOWER STIFFENER STRAP RBL 19-25, WL 160. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED -12 INNER FRAME CHORD STRAP; FABRICATED A -1 REPAIR ANGLE, -2 TAPERED FILLER, AND 1 EACH FRAME & STRINGER CLIP; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-03134-ES1. 2L72 4F RTA16WE 20030522001202003052200120EU 2003 5 22 MALA030269 120030517A2197 WIRE SAAB SF340 340B 7860101EU DAMAGED A MALAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL15413XJ 340B413 DURING TAKEOFF ON FLIGHT 2927, LT DUCT TEMP WAS UNCONTROLABLE. AIR TURNBACK TO DTW. LT DUCT OVERTEMP INFLIGHT. LEFT BLEED AUTO CLOSED, NO CONTROL OF DUCT TEMP IN OR OUT OF MANUAL OR AUTO. MAINTENANCE FOUND DAMAGED GROUNG WIRE FROM PIN C TO GROUND STUD 323VN SEE 409 # 155904 FOR DETAIL. 2L72 4T RTA52EU 20030523000992003052300099NM 2003 5 23 QXEA0300558 120030512A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX-FOUR DENTS IN RIGHT HAND FUSELAGE BS 298.000 TO BS 290.000 BETWEEN STRINGER 18 AND 17. REPAIRED IAW HORIZON AIR EA 6-53-253. 2H72 4T RTA13NM 20030528000692003052800069SW 2003 5 28 AC2A086462 120030513A5210NAS5623R7A CAM FOLLOWER BELL 430 430 1182150SW PAX DOOR BROKEN E AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CM1302 49090 CAM FOLLOWER IS BROKEN. BEARINGS BECOME CORRODED AND THE OUTER RACE SEPARATES FROM THE INNER RACE. DAMAGE WAS FOUND ON THE LEADING EDGE OF ONE TAIL ROTOR BLADE ON THIS AIRCRAFT, THE PREVIOUS DAY. IT IS SUSPECTED THAT THE BEARING OUTER RACE BECAME DISCONNECTED AND STRUCK THE TAIL ROTOR BLADE. TAIL ROTOR BLADE WAS REMOVED FROM SERVICE DUE TO DAMAGE. REPLACED LOWER CAM FOLLOWER ON RT PASSENGER DOOR, AND UPPER CAM FOLLOWER ON L/H PASSENGER DOOR. 1G72 3U RTH9SW 20030620000842003062000084EU 2003 6 20 USAASA03039 120030513A3350321430 BATTERY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19103US 0861 DURING EMERGENCY LIGHTS TEST, RECEIVED 'EPSU INT LOAD EMER R' FAULT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACK AT THE RIGHT EMERGENCY EXIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030702000082003070200008CE 2003 7 2 2003F00389 120030525A2697 WIRE BEECH 1900 1900D 1154162CE FIRE BOTTLE UNSECURE A GUUAO OTHER J WARNING INDICATION CRCRUISE 1 SO1781556 UE239 DURING FLIGHT, LT FIRE BOTTLE DISCHARGE LIGHT CAME ON AND OFF. SECURED GROUND WIRE AT SQUIB. OPERATIONAL CHECK GOOD. (M0 2L72 4T RTA24CE 20030708000342003070800034WP 2003 7 8 UPS03840894 120030617A5720975329424 ANGLE DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LEADING EDGE ABOVE NR 3 PYLON, RIB TO WEB ATTACH ANGLE IS CRACKED AT LOWER END AT XS 256.339 APPROX. REMOVED ATTACH ANGLE, FABRICATED AND REPLACED ANGLE IAW DWG. 9753294, AND SRM. 51-1-20D 2L74 4F4 FRT4A25 E2GL 20031212000022003121200002EA 2003 12 12 03311663 120031107A2910 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM TRIPPED A VTZAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 EA27663BR 7527 DURING TAXI CREW REPORTED HYDRAULIC SYSTEM 2B AND 3B CIRCUIT BREAKERS TRIPPED WHEN FLAPS WERE SELECTED. MAINTENANCE PERFORMED OPERATIONAL CHECK AND RESET CIRCUIT BREAKERS NO DEFECTS WERE FOUND. 2L72 4F RTA21EA 20031211000212003121100021WP 2003 12 11 ABXA030425 120031026A5311 FRAME DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 FORWARD CARGO BILGE AREA HAD CRACK ON FRAME FS 240, LONG 34 RIGHT - LONG 35 RIGHT. CUT OUT DAMAGE AND FABRICATED REPAIR ANGLE AND FILLER IAW DC-8 SRM STD5310-02. ALODINED AND PRIMED ANGLE AND FILLER IAW DC-8 SRM 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC-8 SRM 51-1-20D. ALL WORK COMPLIED WITH IAW ABX REA D853-48062MR. 2L74 4F 4A25 20030922000342003092200034GL 2003 9 22 RAIA00307200 220030727A7532 BLEED VALVE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE INOPERATIVE A RAIAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 CE03811HK 145256 LT ENGINE ITT OVERTEMP INDICATION. MAINTENANCE CLEANED NR 1 COMPRESSOR BLEED VALVE, NO ADDITIONAL WORK REQUIRED. 2L72 4T4 FRTT00011ATTE6CH 20030924001212003092400121EA 2003 9 24 BSY2003F00022 220030722A8500 ENGINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RIGHT MALFUNCTIONED E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0735871 318052123 L861761A RT ENGINE WILL NOT DEVELOP MORE THAN 1600 RPM. HAD MAINTENANCE CHECK AND RUN ENGINE COULD NOT DUPLICATE PROBLEM. 1L72 3O3 O A20SO E14EA 20030924001332003092400133 2003 9 24 AALA20030754 420030710A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21610AA 24486 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, EIGHT GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED EIGHT GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040205000672004020500067NE 2004 2 5 ASOA03663 220031219A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11848AS 7339 FLT 4637 - DURING CLIMB-OUT FROM BTR-DFW, THE CREW NOTICED A STRANGE OILY ODOR IN THE AIRCRAFT WHEN SWITCHING THE PACKS FROM THE APU TO THE TENTH STATE BLEEDS. THE ODOR BEGAN TO DISSIPATE WHEN THE BLEEDS WERE SWITCHED BACK TO THE APU. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040212002032004021200203CE 2004 2 12 GLBA20030519 120031226A561010138402517 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT CRACKED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03220GL4039 UE220 CAPT WINDSHIELD CRACKED RETURN TO AIRPORT, REMOVED AND REPLACED WINDSHIELD PN 101-384025-17. 2L72 4T RTA24CE 20031215000542003121500054NM 2003 12 15 2003UALA00835 120031104A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29373UA 24638 STA 344 STR 11R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20030926001062003092600106NE 2003 9 26 NACA20030111 220030830A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 18 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 AL03993301853 1853 43576 P33821 NR 4 ENGINE SHUT DOWN DUE TO BACKFIRING. REPLACED NR 4 ENGINE, NR 18 CYLINDER DUE TO CRACKED HEAD. OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20060801000952006080100095WP 2006 8 1 IXXA060547S 120030907A5720 SPACER DOUG DC8 DC871F 302199DWP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE AT STATION XFS 422-750 SPACER CORRODED. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PART IAW REPAIR ENGINEERING ORDER REO-G09480. 2L74 4F RT4A25 20060801001472006080100147WP 2006 8 1 IXXA060590S 120030910A57535652287502 VANE DOUG DC8 DC871F 302199DWP ZONE 600 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INBOARD VANE DELAMINATED NEAR INBOARD END. REMOVED VANE. REPAIRED VANE. REINSTALLED VANE PER ALL APPROVED DATA. 2L74 4F RT4A25 20060801000792006080100079WP 2006 8 1 IXXA060541S 120030909A5310 MOUNT DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND ANTENNA MOUNT CORRODED AT STATION FS410, LONGERON 36. ANTENNA NOT IN USE, REMOVED MOUNT IAW TIMCO REPAIR ENGINEERING ORDER REO-G09474. 2L74 4F RT4A25 20030814000352003081400035NM 2003 8 14 UPS03241071 120030710A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, SKIN CRACKS FROM FASTENER HOLES BS 255 (AFT OF NR 3 RT WINDOW CUTOUT) BETWEEN S-10R AND S-9R. REPAIR CARRIED OUT IAW SRM 53-30-03, FIGURE 29. 2L73 4F A3WE 20030815000542003081500054SW 2003 8 15 HEEA088499 120030714A243230703001 BATTERY BELL 412 412 1182202SW MASTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 BATTERY DEAD. REPAIRED. 1G72 4U H4SW 20030818000372003081800037SW 2003 8 18 HEEA088486 120030722A6320206040184001 PUMP BELL 206 206B3 1181506SW M/R OIL SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032275Y 3626 MAIN ROTOR GEARBOX OIL PUMP LEAKING. REPAIRED. 1G71 3U H2SW 20030630000822003063000082SW 2003 6 30 HEEA087844 120030615A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03741PH 53457 MAIN ROTOR BLADE LEADING EDGE CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030710000062003071000006SO 2003 7 10 ASOA03245 120030531A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11639AS 120283 FLT 4894 - DURING A GROUND INSPECTION IN DFW, THE FORWARD AND OVERHEAD EMERGENCY LIGHTS DIMMED OUT AFTER APPROXIMATELY TWO SECONDS WHILE THE REMAINING LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030716000452003071600045NM 2003 7 16 TSAA0333115 120030511A335086210151 BATTERY PACK BOEING737 737209 13844AENM PAX CABIN DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 REPLACED AFT ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030109000732003010900073NM 2003 1 9 MWEA030020 120030109A5310991015194 DOUBLER DOUG MD88 MD88 3023688NM STA 826-845 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RIGHT CUSP MEMBRANE HAS CORROSION BETWEEN STATION 826-845. -- FABRICATED AND INSTALLED DOUBLER.REMOVED AND REPLACED GRILL AND INSTALLED SIDE WALL PANEL. 2L72 4F RTA6WE 20030113001482003011300148 2003 1 13 730PA0002 420030107A2220 COMPUTER BOEING737 7373L9 1384470NM A PIDAK NONE J WARNING INDICATION UKUNKNOWN 1 SO05730PA 27924 On landing checklist "speed trim fail light" illuminated when recall was pressed. Performed BITE test of DFCS system per MM 22-03-10, Function check normal. 2L72 4F RTA16WE 20030127002462003012700246WP 2003 1 27 MWEA030002 120030107A575459394001 SLAT TRACK DOUG DC9 DC981 3022081WP L/E SLAT DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 LEFT HAND WING THE "O" SLAT INBOARD IDLER TRACK HAS A QUARTER INCH DIAMETER ATTACH HOLE THAT IS ELONGATED. FABRICATED AND INSTALLED BUSHINGS. 2L72 4F A6WE 20030131001672003013100167NM 2003 1 31 UPS03240103 120030107A5310 SHEAR TIE BOEING727 72722C 138400FNM BS 320 BL20R/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI FLOOR BEAM SHEAR TIE CRACKED AT BS 320 APPROX AND BL 20 R/H FLOOR BEAM SHEAR TIE REPAIRED AT BS 320 AND BL 20 R/H IAW SRM 53-10- 3 FIGURE 6 2L73 4F A3WE 20030203002302003020300230EU 2003 2 3 DHL2003364002 120030201A2610 FIRE DETECTOR AIRBUS300 A300B4203 3930306EU A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01364DH 141 1) ENGINE #2 LOOP "A" LIGHT ILLUMINATED. "ENGINE OR APU LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURE COMPLETED."2) TRANSFERRED TO DEFERRAL PER MEL 26-12-01-1. ASSIGNED DMI #11836. PLACARDS INSTALLED. "B" LOOP OPS NORMAL.3) ENGINE #2 LOOP "A" LIGHT ILLUMINATED. ENGINE OR APU LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURE COMPETED.4) TROUBLESHOOT TO #2 ENGINE DUAL CONTROL FIRE DETECTOR UNIT. REMOVED AND REPLACED UNIT AS PER M/M 26-12-11. GROUND TEST NORMAL. THIS CLEARS DMI #11836. 2L72 4F RTA35EU 20030204000142003020400014SO 2003 2 4 NCL2003F00000 120030110A57127847504 RIB PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360KB 17025SO WING CRACKED B NCLRK NONE O OTHER ININSP/MAINT 1 NE012900S7676 347970344 315100 THE LT AND RT FORWARD TRUNNION FITTING ASSEMBLIES WERE REMOVED TO REPLACE THE BEARINGS. WHILE THE FITTINGS WERE REMOVED THE TECH NOTICED THAT BOTH LT AND RT RIBS WERE CRACKED AT THE FORWARD OUTBOARD FLANGES OF THE RIBS. THIS FLANGE IS UNDER THE TRUNNION FITTING ASSEMBLY AND CANNOT BE SEEN WITHOUT REMOVAL. 1L72 3O3 O A7SO E9CE 20030204000192003020400019EU 2003 2 4 R142003F00000 120030113A5753 STRUCTURE HWKSLYDH125 DH125400A 4230140EU RROYCEVIPER VIPER* EU LT TE FLAP FAILED B R14RK NONE O OTHER ININSP/MAINT 1 EA17284DB13678 NA715 LT FLAP FAILURE 41 INCHES OUTBOARD OF INBOARD END. FLAP WAS IAW SB. WHICH STRENGTHENS FLAP FOR LANDING IN HEAVY WATER/ SLUSH CONDITIONS. AIRCRAFT ARRIVED WITH HEAVY PRECIP PRIOR TO LANDING. 2L72 4J4 J A3EU E3EU 20030204002222003020400222NM 2003 2 4 SWAA030179 120030125A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29708SW 27842 SMALL SECTION OF EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030210001102003021000110NM 2003 2 10 QXEA0300058 120030107A5755 SKIN BOMBDRDHC8 DHC8401 1390041NM LT SPOILER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX-OUTBOARD TRAILING EDGE OF OUTBOARD SPOILER AND LEFT HAND WING IS CHAFED ON LOWER SKIN. REPAIRED IAW DHC-84 SRM 51-21-10, SRM 51-14-00 AND SRM 51-25-05. 2H72 4T RTA13NM 20030219000922003021900092NM 2003 2 19 SWAA030311B 120030207A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030225000072003022500007SO 2003 2 25 C2XA03SH023 120030225A530014523186001 BEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-21-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SEVICE. 2L72 4F RTT00011AT 20030226000342003022600034SW 2003 2 26 HEEA084323 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 LEFT TRANSFER LIGHT STAYS ON. REPLACED FUEL CELL PRESSURE SWITCH. 1G71 3U O H2SW 20030303002062003030300206NM 2003 3 3 CALA0300084 120030302A5320 ANGLE BOEING737 7373T0 1384582NM STA 1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 INSPECTION FOUND CORROSION ON UPPER SURFACE OF ANGLE AT NUTPLATES, STA 1006, LBL 10. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030308000012003030800001EU 2003 3 8 RAIA00302046 120030212A2741C850176 SENSOR JETAIRJETSTMJETSTM4101 1500501EU SHORTED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03563HK14070 41079 5395-BWI- LEFT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE AOA SENSOR, OPS CK OK. 2L72 4T RTA41NM 20030310001262003031000126NM 2003 3 10 UPS03240262 120030218A2710 AILERON BOEING727 727108C 1384039NM O/B R/H CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI CORROSION ON O/B R/H AILERON HINGES 2, 3 & 4 ON INVESTIGATION OF HINGE ASSYS, HINGES FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 57-50-11. INSTALLED REPLACEMENT AILERON IAW MM 27-10-14. REF. NRC 632179 FOR AILERON RIGGING & OUSTANDING STEP S 2L73 4F A3WE 20030313001622003031300162EU 2003 3 13 AALA20030116 120030125A2841 CONNECTOR AIRBUS300 A300B4605R 3930308EU LT WING CONTAMINATED A AALAE ENGINE SHUTDOWN N FALSE WARNING NRNOT REPORTED 1 SW2150051 459 JFK - FLT 1270 - EN ROUTE SJU-EWR, LEFT ENGINE WAS SHUTDOWN FOR APPROXIMATELY 10 MINUTES DUE TO LEFT WING OUTER TANK INDICATION SHOWING FUEL QUANTITY GOING UP AND DOWN. LANDED JFK WITHOUT INCIDENT. AFTER AIRCRAFT LANDED INSPECTED LEFT WING WITH NO FUEL LEAKS BEING NOTED. CLEARED AND CLEANED COMPENSATOR HARNESS CONNECTOR OF ALL CONTAMINATES AND PERFORMED CAPACITANCE AND RESISTANCE CHECK OF LEFT WING OUTER TANK. ALL CHECKS WITHIN LIMITS. SUMPED LEFT WING OUTER TANK AS REQUIRED. ACCOMPLISHED INSPECTION OF LEFT WING TANKS. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030121000782003012100078SW 2003 1 21 HEEA083273 120030108A7714 SPLINE ADAPTER BELL 206 206L3 1182108SW TACH GENERATOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 TACH GENERATOR HAS A WORN DRIVE SPLINE. 1G71 3U H2SW 20030314001732003031400173NM 2003 3 14 USAABB03034 120030306A335086210066 BATTERY BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE ROWS 1,4,6,9 DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS, 1,4, 6 AND 9, INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2L72 4F4 FRTA2NM A12EU 20030122002122003012200212NM 2003 1 22 DL76G030025 120030105A2740285T0015116 MODULE BOEING767 767332 1382001NM STABILIZER FAULTY A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO271609 30574 UNSCHED STAB TRIM, EICAS CAUTION ON TAKEOFF ROLL. TAKEOFF ABORTED. T/S PER FIM ON UNSCH STAB TRIM EICAS MSG. LT SAM FAULTED `STCM` REPLACED LT SAM PER M/M. LT STAB TRIM OPS NORMAL. 2L72 4F RTA1NM 20030321000472003032100047NM 2003 3 21 CALA0300127 120030320A5520 FITTING BOEING737 737524 1384721NM R/H ELEVATOR WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2716617 27330 INSPECTION FOUND THE R/H ELEVATOR O/B HINGE FITTING WORN. THE HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-51-02 AND 51-40-02. 2L72 4F RTA16WE 20030303001372003030300137SW 2003 3 3 HEEA084561 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032234713458 36005 MAIN ROTOR BLADE HAS A HOLE IN TOP SKIN AT STA 93 WITH MULTIPLE BRANCHES. 1G72 4U H4SW 20030327001682003032700168SO 2003 3 27 C2XA03SH049 120030310A531014522226003 BUTT STRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C-CHECK CENTER BUTTSTRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 59 TO 61. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030417001202003041700120EA 2003 4 17 QXEA0300239 120030205A2820 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 ILLUMINATED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09615QX 10065 SEA-ON FLIGHT NUMBER 2504, LT TRANSFER SHUT OFF VALVE CAUTION MESSAGE IN FLIGHT. USED ABNORMAL CHECKLIST. AFTER 5-10 MINUTES, CAUTION MESSAGE DISAPPEARED. MDC, LT TRANSFER VALVE COMMAND DISAGREE. COMPLIED WITH FIM TASK. NO DEFECTS NOTED. COMPLIED WITH LRU TEST OF VALVES/PUMPS. SELF TEST PASSED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030421000802003042100080NM 2003 4 21 DL777030085 120030122A4900 CHARGER BOEING777 777232 1385232NM APU ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27861DA 29952 F/A AT 4R REPORTS SMOKE IN CABIN FROM AROUND SEATS 53 - 56. REPLACED APU BATTERY AND CHARGER. AC ALSO HAD STATUS MSG FOR BATTERY AND CHARGER. INSPECTED FOR DAMAGE, NONE FOUND. 2L72 4F RTT00001SE 20030422000482003042200048EU 2003 4 22 USAASA03017 120030218A3350NSA934324075 CIRCUIT BREAKER AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19729US 1170 PIT - THE EMERGENCY LIGHTING CIRCUIT BREAKER WAS FOUND OPEN. MAINTENANCE REPLACED THE EMERGENCY LIGHTING CIRCUIT BREAKER. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20040224000522004022400052WP 2004 2 24 ASAA0380277 120030329A33500105603 LIGHT DOUG DC9 DC983 3022083WP AFT CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01958AS 53024 SEA - DURING PREFLIGHT CHECK, NOT ALL EMERGENCY TRACK LIGHTING ILLUMINATED UPON TEST. REPAIRED DAMATED WIRING IN FORWARD CABIN. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030826001222003082600122EU 2003 8 26 03FDEA00987 120030627A7830 ANGLE AIRBUS300 A300F4605R 3930327EU THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 COMPLY WITH E.A NR 6-7832-70958 EXHAUST-TR ASSY-REPAIR OF FORMED ZEE ON CORE COWL, INNER SURFACE. FACT 27JUN03 12:16 BFM R WORK COMPLIED ON EA 6-7832-70958 EXHAUST-TR ASSY REPAIR OF FORMED ZEE ON CORE COWL INNER SURFACE. 2L72 4F RTA35EU 20030828000662003082800066NE 2003 8 28 P5CA03000915 220030817A73217800001 FUEL CONTROL BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE OVERHEATED A P5CAK NONE R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23923FT 22769 702370 ON DESCENT INTO HKG AT FL 360 NR 3 ENG FUEL TEMP WENT OFF SCALE HOT AND NR 3 ENG STALLED OUT. CORRECTIVE ACTION TAKEN: REPLACED NR 3 ENG FUEL CNTRL IAW AMM 73-21-01 LEAK CK OK PERFORMED TEST NR 9 FUEL CONTROL TRIM OK IAW 71-00-00 PG 580. 2L74 4F4 FRTA20WE E3NE 20030902000392003090200039EA 2003 9 2 TA12003F00000 120030506A7500601800332B COUPLING CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE BLEED AIR IMPROPER PART B TA1RO OTHER O OTHER NRNOT REPORTED 1 SW05417CL4844 5107 WHILE COMPLYING WITH SB A601-0556 (SPECIAL CHECK/ REWORK WING ANTI-ICING SYSTEM) FOUND THAT THE RIGHT WING HAD THE WRONG BLEED AIR COUPLING WITH THE PROPER PART NUMBER STAMPED ON IT. IT APPEARS THIS PART WAS MADE FOR THE LEFT WING WITH THE RIGHT WING MARKING. 2L72 4F4 FRTA21EA E15NE 20030724001182003072400118NM 2003 7 24 AWXA200300674 120030506A532065176856 STRAP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK .1875 INCH CRACK WAS FOUND ON STRAP AT L-1 DOOR CUTOUT, BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED STRAP AT L-1 DOOR CUTOUT, BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-17685; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 10 & 11. 2L72 4F RTA16WE 20030729000732003072900073NM 2003 7 29 QXEA200300740 120030615A5270 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09408QX 4050 SEA-ON FLIGHT NUMBER 2308, FUSELAGE DOORS WARNING LIGHT ILLUMINATED INFLIGHT. MFD PAGE INDICATED SERVICE DOOR NOT SECURED, DOOR FOUND TO BE SECURE VISUALLY BY FLIGHT ATTENDANT. INTERGATED PSEU, FORWARD AFT SERVICE DOOR LOCK UNREASONABLY FAR IN FAULT HISTORY. CYCLED AFT SERVICE DOOR. PRESSURIZED A/C TO 5.5 PSID.AFT SERVICE DOOR LOCK OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030806000702003080600070NM 2003 8 6 AWXA200300854 120030713A5315654581094 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK .25 INCH CRACK WAS FOUND ON UPPER SURFACE OF FLOORBEAM BS 312, RBL 11, WL 208. MAINTENANCE CUT OUT DAMAGE ON UPPER SURFACE OF FLOORBEAM BS 312, RBL 11; FABRICATED A NEW SECTION OF FLOORBEAM, A FILLER, AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, PG 224-228, FIG 206. 2L72 4F RTA16WE 20030807000512003080700051EA 2003 8 7 COMA0360341 120030728A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01455CA 7592 FLT 5055 EMERGENCY FLOOR PATH LIGHTING, FORWARD SECTION IS INOP. REPLACED FLEXIBLE LAMP. 2L72 4F RTA21EA 20030903000722003090300072EU 2003 9 3 187801 120030518A2613 CONNECTOR SAAB SF340 SF340A 7850100EU EXH PIPE HOT SYSDIRTY A UHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL17108CQ 340A108 AIRCRAFT 108CQ FROM HGR-PIT FLT 4535 ABORTED TAKE OFF DUE TO RIGHT TAIL PIPE HOT LIGHT. PIT MAINTENANCE DISPATCHED TO AIRCRAFT. MAINTENANCE CLEANED CONNECTORS ON TAIL PIPE HOT SYSTEM, GROUND RAN AIRCRAFT, OPS CHECK IAW 26-12-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE AND COMPLETED FLT 4535 HGR-PIT. 2L72 4T RTA52EU 20030903000632003090300063 2003 9 3 HYI2003F00007 420030622A3197CM358950 MASTER SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LT SWITCH PANEL INOPERATIVE E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE0126156813 402C0112 AVIONICS MASTER SWITCH, INOPERATIVE. MAINTENANCE REPLACED SWITCH AND RETURNED THE AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20030905001832003090500183EA 2003 9 5 ASOA03370 120030814A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 FLT 4232 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY FLOOR LIGHTS AT ROWS 2-5 AND WAS UNABLE TO FIND ANY DEFECTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030905001882003090500188NM 2003 9 5 USAA030137 120030809A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US48147 23935 PIT - FOUND SKIN CRAKED 3 INCHES, STATION 727E PLUS 2 INCHES S24R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20030806000362003080600036EU 2003 8 6 AWXA200300872 120030803A7540342B030000 THERMOSTAT AIRBUS320 A320232 3930326EU NR 2 ENGINE DEFECTIVE A AWXAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING JSGWARNING INDICATION AFFECT SYSTEMS MULTIPLE FAILURE CLCLIMB 1 WP28658AW14239 1110 AFTER TAKEOFF RECEIVED NR 1 & NR 2 ENGINE BLEED CLASS MESSAGES. BOTH BLEED VALVES CLOSED & TEMP AT 320 C, CYCLED SWITCHES WITH NO SUCCESS. TURNED APU BLEED ON & BOTH ENG BLEEDS RETURNED TO NORMAL. RETURNED BOTH ENG BLEEDS TO SERVICE & 2 MIN LATER BOTH ENG BLEEDS FAULTED AGAIN. CYCLED BLEED CIRCUIT BREAKERS PER MX CONTROL & CAPT EMERGENCY AUTHORITY & BOTH BLEEDS RETURNED TO NORMAL. AFTER TURNBACK OBSERVED HOT ODOR, TURNED BOTH BLEEDS OFF, LANDED WITHOUT EVENT. MX PERFORMED A FUNCTIONAL CHECK OF FAN AIR VALVES, CHECK WAS GOOD. REMOVED & REPLACED NR 1 & NR 2 ENG TEMP CONTROL THERMOSTATS. OPS AND LEAK CHECKS GOOD. BLEED MONITORING COMPUTERS 1 & 2 BOTH CHECKED GOOD ON CENTRALIZED FAULT DISPLAY SYS. 2L72 4F RTA28NM 20030807000052003080700005NM 2003 8 7 USAASB03106 120030712A29136507506 PUMP BOEING737 737301 1384611NM NR 2 ENGINE HYD LEAKING A USAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA19558AU 23512 ON DESCENT INTO PIT, FROM DFW, CAPTAIN REPORTED A LOSS OF 'B' HYDRAULIC SYSTEM PRESSURE ALONG WITH FLUID LOSS TO ONE-QUARTER. CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE FOND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED PUMP PER MM 29-15-12. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030807000672003080700067EU 2003 8 7 03216311 120030804A3350 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27311UE 41029 DURING MAINTENANCE INSPECTION THE RT AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030813001462003081300146NM 2003 8 13 SWAA031759 120030805A53146545866 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500C, WL146 AND LBL 6. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20030821002682003082100268WP 2003 8 21 GTIA030586 120030628A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND AFT PIT CORRODED FLOOR WEB AROUND DOME NUT AT FS 1174-1193 LONGERON 18L. FABRICATED REPAIR PARTS FILLER AND DOUBLER. INSTALLED DOUBLER AND FILLER. PRIOR TO STEP 6 PAGE 1 REMOVED DAMAGED AREA OF WEB. (M) 2L72 4F A6WE 20030910001232003091000123NM 2003 9 10 MWEA030339 120030827A5320993653519 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FLOOR SUPPORT EXTRUSION HAS BEEN NOTCHED OUT IN 7 AREAS ALONG OUTBOARD EDGE STATION 200-256 LOCATED 12 INCHES LEFT OF AIRCRAFT CENTER LINE. 2L72 4F RTA6WE 20030912001742003091200174WP 2003 9 12 AALA20030866 120030815A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21454AA 49559 RDU - FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030731000222003073100022EA 2003 7 31 QXEA200300856 120030716A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT FALSE INDICATIONA QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX 10045 LAX- ON FLIGHT 2545 FIRE SYSTEM FAULT STATUS MESSAGE. INTERROGATED MDC, FOUND NO FAULTS. COMPLIED WITH FIRE TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030916000452003091600045WP 2003 9 16 GTIA030052 120030208A3260 PROXIMITY SENSOR DOUG DC9 DC941 302207NWP MLG MALFUNCTIONED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23131NK 47605 LEFT GEAR UNSAFE LIGHT NEVER CAME ON EXTENTION. GROUND TESTS OK IAW MM 32-60-0. REMOVED AND REPLACED LEFT GEAR UP-LOCK PROXIMITY SENSOR AS PRECAUTIONARY. 2L72 4F A6WE 20030916000862003091600086WP 2003 9 16 GTIA030664 120030813A5542 SKIN DOUG DC9 DC983 3022083WP RUDDER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FTW - FOUND RUDDER LEFT SIDE LOWER DELAMINATED ON EDGE AND LEFT SIDE FAIRING PAINT CRACK VISABLE TO MATERIAL. REPAIRED DAMGED AREA. REPLACED FLAME SPRAY. (M) 2L72 4F RTA6WE 20030916000952003091600095EU 2003 9 16 ASOA03386 120030725A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING A C-CHECK IN BNA, THE AFT RIGHT SEAT TRACK FROM FS 36-39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT SEAT TRACK FROM FS 36-39 IAW SRM 51-25-04. (M) 2H72 4T RT 20030908001512003090800151 2003 9 8 SWIA200312226 420030729A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07292UX 120292 ON LEVEL OUT AFTER CLIMB YOKE SHOOK FORWARD QUICKLY WITH SINGLE CHIME ALERT AND NO OTHER INDICATIONS. REPEATED ON DESCENT INITIATION. BOTH TIMES AP ON. CHECKED SYSTEM. FOUND NO FAULTS WITH AOA NR 1 OR AOA NR 2 OR SIDE SLIP. ALL SYSTEM TEST POINTS CHECK GOOD. REMOVED AND REPLACED THE STALL WARNING COMPUTER AS A PRECAUTION IAW MM 27-34-03. SYSTEM OPS CHECKS GOOD WITH NO FAULTS FOUND. 2L72 4T4 TRTA31SO E20NE 20031003000352003100300035EU 2003 10 3 AALA20030473 120030419A3397 WIRE FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211426A 11411 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 11D INOPERATIVE. REPAIRED EMEGENCY EXIT FLOOR PATH LIGHT WIRE AT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031007000692003100700069NM 2003 10 7 SWAA031983 120030904A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM FWD CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 EMERGENCY FLASHLIGHT INOP IN FWD CABIN. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20031021002672003102100267NM 2003 10 21 03FDEA01578 120030918A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 STRINGER CLIP 8R CRACKED AT BS 720D. REMOVED AND REPLACED CLIP IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20031022001422003102200142EU 2003 10 22 AWXA200301084 120030907A5347D5311278220200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CORROSION WAS FOUND ON THE FORWARD OUTBOARD END OF THE RT OUTBOARD SEAT TRACK AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SEAT TRACK FROM FS 6053 TO FS 9766, Y1292; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 23-28, 39-41, FIG. 39-41. 2L72 4F RTA28NM 20031028001632003102800163NM 2003 10 28 GAIA03105 120030910A5311 FRAME BOEING727 727223 1384074NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 1010 HAS A DENT ABOVE STRINGER 25R. REF FASI N/R 53289 CUT OUT DAMAGE, 7 INCHES BY 3.5 INCHES DOUBLER REPAIR PER B727 SRM 51-40-3, FIGURE 1 AND 53-10-2 FIGURE 5. (M) 2L73 4F A3WE 20031110000402003111000040EA 2003 11 10 COMA0360487 120031105A3350 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01716CA 7250 FLIGHT 5238 SECTION OF FLOOR EMERGENCY LIGHTING AFT OF ROW 8 IS INOPERATIVE. REPLACED FAILED FLOOR EMERGENCY POWER STRIP. 2L72 4F RTA21EA 20031110001802003111000180 2003 11 10 SWAA032251 420031014A2565D63551101 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29428WN 29844 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20040212000172004021200017CE 2004 2 12 AMWA86 120031126A553110164000021 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07138YV UE138 DURING THE D-6 INSPECTION THERE WERE TWO CRACKS FOUND AT THE LOWER RT SIDE VERTICAL RIB ON JOGGLE THROUGH RIVET HOLE. REPAIRED CRACKS IAW BMM. P/N 101-640000-21, 54.026 2L72 4T RTA24CE 20040212001582004021200158NM 2004 2 12 F3LA200300181 120031219A5310 SHEAR TIE BOEING737 73736N 1384408NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED SHEARTIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 27R AND 28R. REPAIRED IAW SRM 53-00-07. 2L72 4F RTA16WE 20031106002362003110600236WP 2003 11 6 GTIA030727 120030921A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND PASSENGER CABIN DELAMINATED PANEL STATION 1250 CENTER TO STATION 1310. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030918000052003091800005NM 2003 9 18 03FDEA01504 120030911A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON FLOORBEAM LOWER CHORD UNDER NUTCLIP. REPAIRED IAW SRM 53-10-8. 2L73 4F RTA3WE 20031124000442003112400044NM 2003 11 24 03FDEA01931 120031110A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE NR 1 INBOARD CORRODED. LT WING I/B FLAP, O/B HINGE PIVOT HOLE NR 1 I/B CORROSION R & R AS PER FEDEX EA 1-5750-74248. WINGS - LEFT I/B TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20040112001622004011200162WP 2004 1 12 AALA20031242 120031107A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21481AA 49656 DFW - DURING OVERNIGHT MAINTENANCE FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED TAILCONE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040113000502004011300050EU 2004 1 13 BAQA090689 120031112A21211260720 BLOWER UROCOPEC135 EC135P1 8680990EU EVAPORATOR INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH1771 0069 EVAPORATOR BLOWER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20040113002092004011300209SO 2004 1 13 C2XA03IA118 120031222A33501317 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711547 145563 DURING SCHEDULED MAINTENANCE THE LT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP AND OPERATIONALLY TESTED THE LIGHTING SYSTEM. 2L72 4T RTT00011AT 20040311000382004031100038NM 2004 3 11 ASAA0310143 120030316A531065621003 CREASE BEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CREASE BEAM AT BS 351.2, STRINGER 18L CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20031217002152003121700215NM 2003 12 17 PCAA0311143 120031121A335061047811 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13804EX 227 MAINTENANCE NOTICED UPON OPERATIONAL CHECK THAT 1 FORWARD EMERGENCY LIGHT AND 2 RIGHT HAND AFT SIDEWALL EMERGENCY LIGHTS WERE INOPERABLE. MAINTENANCE THEN REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES AT POSITIONS NR 1, 2, 3, 5. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031218001642003121800164NM 2003 12 18 MWEA030464 120031203A5320993658045 INTERCOSTAL DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 THE INTERCOSTAL BETWEEN FLOORBEAMS AT STATION 1287-1309 AT AIRCRAFT CENTERLINE HAS TWO EACH CRACKS ADJACENT TO SCREW HOLES. FABRICATED AND INSTALLED REPAIR DOUBLERS. 2L72 4F RTA6WE 20031218001612003121800161SO 2003 12 18 C2XA03SH482 120031204A532014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031222000772003122200077WP 2003 12 22 2003F00651 120030813A532049157411 FITTING DOUG DC9 DC915F 3022037WP SERVICE DOOR CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 FOUND 4C CHECK SERVICE, FOUND FORWARD SERVICE DOOR HOLD OPEN HOOK PAN, FITTING CRACKED. FITTIG WAS REPLACED. (M) 2L72 4F A6WE 20031222000812003122200081SO 2003 12 22 SIMA200332701 120031120A5347 SEAT TRACK EMB 135 EMB135LR 3260305SO COCKPIT LACK OF LUBE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 RDU - FLT 4852 - PILOT REPORTED AN UNCOMMANDED SEAT MOVEMENT. MAINTENANCE CLEANED AND LUBRICATED THE SEAT TRACK AND RAILS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031223001862003122300186WP 2003 12 23 GTIA030827 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200, 36 INCHES RBL. REMOVED CABIN FLOOR SUPPORT. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031231001002003123100100NM 2003 12 31 TSAA0357063 120030410A572069406121 LEG ASSY BOEING737 737209 13844AENM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 REMOVED CORROSION DAMAGE BY BLENDING TO A 20 TO 1 RATION. PERFORMED 10X VISUAL AND HFEC INSPECTON TO VERIFY CRACK AND CORROSION FREE. FABRICATED A TAPERED SHIM FROM 2024-T3. FLAT PEENED SURFACE. APPLIED ALODINE AND TWO COATS OF BMS 10-11, TYPE I PRIMER TO BLENDOUT LOCATION. WET INSTALLED 1/32 OVERSIZED HI-LOCKS PROTRUDING HEADS WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 2948. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040106000662004010600066SO 2004 1 6 SWIA200312693 120031212A32331959500007 ACTUATOR EMB 120 EMB120ER 3260203SO RT MLG FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07289YV8886 8886 120289 RIGHT MAIN GEAR WOULD NOT RETRACT. FULL GEAR EXTENSION OK. RETURNED TO LAX. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR WITH SERVICEABLE IAW MM 32-11-00. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030425000842003042500084NM 2003 4 25 QXEA0300391 120030319A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND FUSELAGE SKIN GOUGED AT X799.0 - X801.0, RIGHT HAND STRINGER 23. REPAIRED IAW RD 8/4-53-468 AND HORIZON AIR EA 6-53-222. 2H72 4T RTA13NM 20030428000012003042800001NM 2003 4 28 DLM88030243 120030315A2910AS153080254 LINE DOUG MD88 MD88 3023688NM RT TAIL COMPT LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27912DE 49997 RT HYD PRESSURE AND QTY WENT TO ZERO FOLLOWING LANDING GEAR EXTENSION. REPLACED LEAKING FLEX LINE FWD OUTBOARD ON RT ENGINE HYD FILTER MODULE. 2L72 4F RTA6WE 20030428001002003042800100NM 2003 4 28 VNAA0303027 120030324A3350 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT DISCONNECTED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07434JS 3051 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTS AT ROWS 4-6 WERE INOPERTIVE. MAINTENANCE RESECURED LIGHT STRIP CONNECTION AND PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00 AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030429000192003042900019NM 2003 4 29 P5CA0300817 120030126A5320 FLOOR SUPPORT BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LWR LOBE AFT CRG CRACK ON BRACKET AT FLOOR TRACK SUPPORT RBL-25 BETWEEN STA 1900-1920. CRACKED BRACKET REMOVED, NEW BRACKET FABRICATED PER SRM 53-11-25, ANODIZE PER SRM 51-10-02, FASTENERS INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 20030502000192003050200019SO 2003 5 2 SIMA200309020 120030314A531014522461011 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, RIGHT BEAM FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE RIGHT BEAM FORWARD GUSSET IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030502001292003050200129EA 2003 5 2 03104655 120030414A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 DURING MAINTENANCE INSPECTION, THE AFT CEILING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030502000272003050200027NM 2003 5 2 AMTA200300399 120030327A2420 GENERATOR BOEING757 75733N 1384931NM LEFT FAILED A AMTAO OTHER J WARNING INDICATION DEDESCENT 1 GL11551TZ 32585 LEFT GEN CONT OFF LIGHT ILLUMINATED. TRIED ONE RESET, NO HELP. APU POWERED BUSS OK. NO OTHER INDICATIONS. (M) 2L72 4F RTA2NM 20030505001132003050500113NM 2003 5 5 AWXA200300431 120030402A5753113N3500 SKIN BOEING757 757225 1384959NM TE FLAPS CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - FLIGHT CONTROL - DURING C-08 CHECK THE LT OUTBOARD FLAP INBOARD LEADING EDGE SKIN WAS FOUND CHAFING ON THE WING TRAILING EDGE AT WS 309 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF LT OUTBOARD FLAP INBOARD LEADING EDGE SKIN AND PERFORMED SKIN REPAIR IAW B757-200 SRM 57-53-01 PG 210-213 FIG 203. 2L72 4F RTA2NM 20030506002142003050600214NM 2003 5 6 ASAA0310016 120030216A5320655383911 STRIP BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING SCHEDULED D-CHECK, FOUND TRANSITION STRIP AT BODY STATION 847-927, STRINGER 25L CORRODED. REMOVED AND REPLACED TRANSITION STRIP PER SRM. (M) 2L72 4F RTA16WE 20030509001492003050900149NM 2003 5 9 AMTA200300418 120030328A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 FOUND ROW 35 AND BACK EGRESS LIGHTS INOPERATIVE. INSTALLED NEW LIGHT ASSEMBLY AT ROW 35, AS REQUIRED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030513000682003051300068NM 2003 5 13 CALA0300240 120030511A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714307 23358 INSPECTION FOUND A CRACK IN THE AFT CARGO DOOR INNER SKIN. THE SKIN WAS REPAIRED IAW ECRA 5232-01027. 2L72 4F RTA16WE 20030513000552003051300055NE 2003 5 13 ASOA03127 220030323A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT MALFUNCTIONED A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO11836AS 7263 DURING CLIMB-OUT AT APPROXIMATELY 6,500 FT THE CREW RECEIVED A RED FLAG ON THE LT INTERSTAGE TURBINE TEMPERATURE GAUGE OF APPROXIMATELY 886 DEGREES. THE CREW REDUCED POWER SLIGHTLY ON THE LT ENGINE WITH THE TEMPERATURE RETURNING TO NORMAL, THEN INCREASED POWER SLIGHTLY AND THE RED FLAG RE-OCCURRED INCLUDING A SLIGHT VIBRATION. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20030514000752003051400075NM 2003 5 14 SWAA030941 120030428A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 1006 & BS 1016, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030513001902003051300190NM 2003 5 13 QXEA0300473 120030421A5260 BUSHING BOMBDRDHC8 DHC8401 1390041NM HAND RAIL DAMAGED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09403QX 4037 ON FLIGHT 2328 MAIN CABIN DOOR WILL NOT OPEN OR CLOSE. REMOVED AND REPLACED MAIN CABIN DOOR HANDRAIL ASSEMBLY BUSHINGS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030528000372003052800037EU 2003 5 28 ERAA086447 120030425A62101051410110 BOLT BOLKMS105 BO105CBS 5626008EU ROTOR BLADE WORN E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01129EH 580 PRIMARY BLADE BOLTS ARE WORN. BOTTOM COVER CRACKED THROUGH BOLT THREADS BROKEN. DISSEMBLED AND CLEANED. PERFORMED VISUAL & NDT INSPECTIONS. SCRAPPED BOTTOM COVER & THROUGH BOLT. RETURNED SERVICEABLE PARTS TO STOCK. INSPECTED IAW BO-105 MM CH 12. 1G72 3U NCH3EU 20030602001342003060200134NM 2003 6 2 SWAA031145 120030522A3350100031 LIGHT BOEING737 7373K2 13844BANM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 FWD ENTRY EMERGENCY EXIT SIDE LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030605000412003060500041NM 2003 6 5 AMTA200300682 120030520A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 EGRESS FLOOR LIGHTING AT SEAT ROW 1ABC WILL NOT ILLUMINATE. RECONNECTED WIRES TO LIGHT ASSEMBLY, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030606000732003060600073NM 2003 6 6 03FDEA00776 120030513A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LEFT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT, O/B CTR BOLT, HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F4 FRTA22WE E13NE 20030609001042003060900104SO 2003 6 9 C2XA03SH146 120030523A532014525422001 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE LT HAND SILL AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030515001852003051500185EU 2003 5 15 AWXA200300508 120030507A3250 CONTROL UNIT AIRBUS320 A320232 3930326EU NLG STEERING MALFUNCTIONED A AWXAO OTHER J WARNING INDICATION APAPPROACH 1 WP28619AW 527 ON APPROACH, RECEIVED BRAKE STEERING CONTROL UNIT FAULT CHANNEL NR 1. AFTER CLEARING RUNWAY BSCU NR 2 FAULTED WITH LOSS OF NORMAL BRAKES, NOSE WHEEL STEERING, AND ANTI-SKID. MX TAXIED ACFT & DUPLICATED FAULTS AND LOSS OF BRAKES & STEERING. INSPECTED BSCU AND CENTRAL FAULT DISPLAY INTERFACE UNIT RACK CONNECTORS; PERFORMED CONTINUITY & INTEGRITY CHECK OF WIRING FROM CFDIU (1TW) PINS AA/8F, 8G, TO TERMINAL BLOCK. ALL CHECKS GOOD. REPLACED CFDIU IAW AMM 31-32-34-000-001 AND REPLACED BSCU IAW T/C R2A32301. TAXIED ACFT TWICE WITH NO FAULTS NOTED. PART NAME; BSCU, MFG; MESSIER, P/N; C202163382D32, S/N; 005122, TT; 7850, TC; 3086. 2L72 4F RTA28NM 20030514001452003051400145NM 2003 5 14 SWAA031045 120030509A53306545774 SKIN BOEING737 7373A4 1384585NM FUSDELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 823, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030610000452003061000045WP 2003 6 10 ABXA030158 120030402A532059242741 BRACKET DOUG DC9 DC932 3022066WP LT MGL WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 LEFT LATERAL CONTROL MIXER BRACKET CRACKED. REPLACED LEFT LATERAL CONTROL MIXER IAW DC-9 MM. 2L72 4F A6WE 20030610001162003061000116SW 2003 6 10 HEEA087013 120030604A6230406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH964 53114 WORN BUSHINGS. REPLACED 4 EACH BUSHINGS 406-310-406-101 DUE TO WORN. REPAIRED. 1G71 3U O H2SW 20030611000282003061100028WP 2003 6 11 GTIA030317 120030415A5320 FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT PIT STA 1007 1 FITTING SUPPORT END CARGO TRACK ATTACH TO INTERCOASTAL RIGHT SIDE IS CRACKED. REMOVED CRACKED FITTING. HOLES LOCATED AND DRILLED ON NEW FITTING. INSTALLED NEW FITTING. 2L72 4F4 F A6WE E2EA 20030612000252003061200025WP 2003 6 12 0301049995 120030526A2780 SLAT DOUG DC9 DC931 3022065WP WING MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL018978E 47327 AIRCRAFT EXPERIENCED A ROLL WHEN THE SLATS WERE INITIALLY EXTENDED. COM PROCEDURES COMPLIED WITH AND WHEN THE CIRCUIT BREAKER FOR THE SLAT EXTEND RELAY WAS PULLED AND RESET PER THOSE PROCEDURES THE BLUE SLAT EXTEND LIGHT ILLUMINATED. LANDING WAS WITHOUT FURTHER INCIDENT AT MKE. MAINTENANCE INSPECTED THE SLAT OPERATING SYSTEM BUT FOUND NO PROBLEMS AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. ALL TESTS RESULTS WERE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030613000562003061300056EU 2003 6 13 UPS03140802 120030605A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EVACUATION SLIDEINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 EVACUATION SLIDE WARNING LIGHT INOP. RESET POWER TO ADJUST POWER AND TESTED LIGHT IAW AMM 5273-11-4. THIS CLEARS M260785 - PLACARD REMOVED. 2L72 4F RTA35EU 20030612001712003061200171EA 2003 6 12 SWIA200312044 120030530A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07932SW1379 1379 7714 STAB CH 1 INOP STATUS MESSAGE ON TAXI OUT. CH 1 WOULD NOT RE-ENGAGE. RETURNED TO GATE. STAB CH 2 FAIL DURING TROUBLESHOOTING HSTCU BITE CODE MOTOR 2 FAIL DISPLAYED. CHANNEL 2 FAIL WOULD NOT RESET, REMAINED DISPLAYED. REMOVED AND REPLACED MCU & HSTCA IAW CRJ MM 27-40-00. P/N: 7062-3, S/N OFF: 1004, S/N ON: 804. 2L72 4F RTA21EA 20030521000612003052100061WP 2003 5 21 DHL2003804881 120030202A5753 SKIN DOUG DC8 DC873F 302199FWP LT TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT OUTBOARD FLAP UPPER SKIN SURFACE WITH 1.000 INCH CRACK BETWEEN STA XF 213.000 AND XF 169.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-5 PG 3-6. CUT OUT DAMAGED SKIN IAW SRM 57-2-5 PG 3-6. FABRICATED FILLER (2024-T3 0.020) AND SPLICE (2024-T3 0.063) AND NEW SKIN (2024-T3 0.063) IAW SRM 57-2-5 PG 3-6. CLEANED, TREATED AND PRIMED FILLER AND SPLICE AND NEW SKIN INNER SURFACE IAW SRM 51-1-8B. INSTALLED FILLER AND SPLICE AND NEW SKIN IAW SRM 57-2-5 PG 3-6, SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030522000952003052200095NM 2003 5 22 SWAA031067 120030512A53116546546 FRAME BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727, WL 148 & RBL 4. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20030523000432003052300043NE 2003 5 23 DLM88030399 220030429A7261 OIL SYSTEM DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE LOW A DALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO27912DL25959 49543 726916 PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL QUANTITY WINDMILL TIME 15 MIN, MINIMUM OIL PRESSURE 8 PSI. MAX OIL TEMP 162 FOR LESS THEN 5 MIN. REPLACED NR 1 ENGINE ASSY. 2L72 4F4 FRTA6WE E9NE 20040106001402004010600140EA 2004 1 6 COMA0360558 120031214A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01988CA 7204 FLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031014001352003101400135NM 2003 10 14 SWAA032157 120030925A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 378.5, LBL 2.9 AND LBL 2.8 AT EQUIPTMENT COOLING EXHAUST PORT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030915000352003091500035EU 2003 9 15 BAQA089103 120030911A6330L633M2010105 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135QC17 0281 GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030916000722003091600072CE 2003 9 16 BSY2003F00016 120030602A3297 WIRE BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO SQUAT SWITCH BROKEN E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL07696BD TH352 299492R GEAR WOULD NOT RETRACT, FOUND BROKEN WIRE IN LEFT WHEEL WELL COMING OFF SQUAT SWITCH, REPAIRED WIRE, OPS CHECK GOOD. 1L72 3O3 O 3A16 E5CE 20040115000092004011500009NM 2004 1 15 03FDEA02024 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 1 I/B WITH WORN CHROME PLATING AT HOLE. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031203001372003120300137EU 2003 12 3 A6WA200360064 120031029A2497S3200ANC6 WIRE BAC 146 146200A 1500266EU FWD CARGO BAY BURNED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 APU GENERATOR INOPERATIVE. DURING MAINTENANCE CORRECTIVE ACTION FOUND 3 APU GENERATOR WIRES IN FORWARD CARGO BAY CEILING BURNED AND EVIDENCE OF ARCHING ON CARGO LINER. MAINTENANCE REPLACED THE 3 PHASE APU GENERATOR WIRES AND CRIMP SLEEVES, PER BAE MM 24-00-00, FROM FWD BREAK TO APU CONTACTOR. (M) 2H74 4F A49EU 20031203000562003120300056NM 2003 12 3 GAIA03145ST 120031024A53302024T3 SKIN BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENT AT BS 312 BELOW STRINGER 21 RT. REF FASI N/R NR 61825, CUT OUT DAMAGE, INSTALLED FLUSH REPAIR PER B727 SRM 53030-3 PAGE 10 AND 11. (M) 2L73 4F RTA3WE 20031205000462003120500046NM 2003 12 5 DLM88030936 120031019A8000 STARTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE SEIZED A DALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SO27997DL 53364 718224 ON ENG START WOULD NOT ACCELERATE ENGINE PAST 16 PERCENT AND A TAILPIPE FIRE ENSUED. REPLACED SEIZED STARTER. 2L72 4F4 FRTA6WE E9NE 20040121000232004012100023NM 2004 1 21 03FDEA02324 120031229A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 CORROSION ON STRINGER 28L AND SPLICE AT BS 676 FWD CARGO BAY. CORROSION FOUND TO BE OUT OF LIMITS ON STRINGER, STRINGER SPLICE, SKIN AND SHEAR TIE. REPAIRED DAMAGED STRINGER AND STRINGER SPLICE PER SRM 53-10-2, 53-10-3. REPAIRED SKIN PER SRM 53-30-3 AND REPLACED SHEAR TIE PER SRM 53-10-2 AND 51-20-2 AT BS 676-685, STR 28 LT. 2L73 4F RTA3WE 20040122001072004012200107EA 2004 1 22 ASOA03636 120031207A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11827AS 7212 FLT 4306 - DURING TAKEOFF FROM ATL-CLT, THE CREW SELECTED THE GEAR HANDLE UP, BUT THE NOSE GEAR DID NTO RETRACT. QRH PROCEDURES WERE COMPLIED WITH, AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE ADJUSTED THE NOSE DOOR PROXIMITY SENSOR SWITCH ON THE RIGHT SIDE AND ALSO CLEANED THE NR 2 DOWN LOCK SWITCH CANNON PLUG ON THE NOSE DOOR IN ADDITION TO CYCLING THE GEAR TWENTY TIMES WITHOUT ANY DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040126000532004012600053 2004 1 26 HEEA087800 420030612A3457N0010001 CONTROL UNIT SKRSKYS76 S76A 8143006NE GPS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K 760082 MENU BUTTON IS INTERMITTENT. 1G72 3U H1NE 20040122001172004012200117EA 2004 1 22 ASOA03654 120031216A5210601R3181273 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11901EV 7616 FLT 4520 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR PRESSURE VALVE CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OF FOR SERVICE. (M) 2L72 4F RTA21EA 20031208001092003120800109NM 2003 12 8 AWXA200301307 120031006A555365538344 FITTING BOEING737 7373G7 1384595NM VERTICAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK THE VERTICAL STABILIZER RT AFT ATTACH DRAG FITTING AT THE FORWARD FUSELAGE LUG WAS FOUND PITTED. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STABILIZER RT AFT ATTACH DRAG FITTING IAW B737-300 SRM 51-40-02 PG 38 FIG 8 & 12. 2L72 4F RTA16WE 20031208000702003120800070EU 2003 12 8 AWXA200301291 120031008A5414D5453005200203 SKIN AIRBUS320 A320231 3930325EU ZONE 470 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-03 CHECK FOUND THE NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN PITTED. MAINTENANCE REMOVED PITTED NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW SECTION OF SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8 PG 8-12. 2L72 4F RTA28NM 20031210000222003121000022NM 2003 12 10 CALA0300682 120031202A5514697203928 BUSHING BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916649 28910 CORROSION ON FORWARD UPPER HORIZONTAL STAB CENTER SECTION LUG AFT CLEVIS ON AFT FACE AT BUSHING. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10. 2L72 4F RTA16WE 20030618001202003061800120NE 2003 6 18 HEEA087133 120030610A67307610408015103 PIN SKRSKYS76 S76C 8143008NE ROTOR SERVO LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 EXPANDABLE PIN FOUND LOOSE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20030618001542003061800154SW 2003 6 18 HEEA087503 120030612A6320PHI407111 SEAL BELL 407 407 1182206SW TRANSMISSION LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03499PH 53400 OIL SEEPING FROM TRANSMISSION INPUT SEAL. REPLACED. 1G71 3U O H2SW 20030528000152003052800015EU 2003 5 28 ERAA086438 120030424A6420 BUSHING BOLKMS105 BO105S 5626006EU T/R HEAD WORN E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01 37651 52114 WORN INNER SLEEVE BUSHINGS. BLADE SKIN ERRODED, INNER SLEEVE STEEL BUSHINGS SCRAP, 1 CRACKED, GRIP TEFLON BUSHINGS SCRAP, ROTTEN SEALS. COMPLETELY DISASSEMBLED FOR INSPECTION. COMPLIED WITH VISUAL & NDT INSPECTIONS REPLACED INNER SLEEVE BUSHINGS, GRIP TEFLON BUSHINGS, SEALS & 1 SPACER. PRIMED & PAINTED AS REQUIRED. COMPLIED WITH 1200 HR & 2400 HR / 6 YEAR INSPECTIONS ON TAILROTOR. 300 HR & 2400 HR BLADE INSPECTIONS COMPLIED WITH BY AEC. ASSEMBLED SEALS & 2 SERVICEABLE BLADES & STATIC BALANCED. INSPECGTED REPAIRED IAW BO-105 REM 301, MM 33 & 34 MM 101 & 107 TT 3765.1 TSI -0- 1G72 3U H3EU 20030623000882003062300088WP 2003 6 23 GTIA030407 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLOOR SUPPORT STATION 190 RBL 9-43 HAS LT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030623000612003062300061NM 2003 6 23 2003F00376 120030319A3246 WHEEL DHAV DHC8 DHC8103 1386005NM MLG WORN A IAHAK NONE O OTHER ININSP/MAINT 1 WP13805WP 353 NR 4 MLG WHEEL ASSEMBLY WORN. REMOVED AND REPLACED NR 4 MAIN WHEEL ASSEMBLY IAW DHC8MM 32-41-11 PAGE 201-205. COMPLIED WITH MM INSPECTION AND NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030624000972003062400097NM 2003 6 24 DL76G030471 120030517A3397 WIRE BOEING767 7673P6 1385105NM EMERGENCY LIGHT CHAFED A DALAO OTHER O OTHER NRNOT REPORTED 1 SO27153DL 24985 FOUND CHAFED WIRE AT SEAT 10A. REPAIRED WIRE. AND REPLACED FUSE. OPS CHECK OK. 2L72 4F RTA1NM 20030707001452003070700145WP 2003 7 7 UPS03840870 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RT WING LE. UPPER RIB IS CRACKED AT XFS 297. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030718000252003071800025WP 2003 7 18 GTIA030474 120030519A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND RIGHT CO-PILOT CONTROL COLUMN FLOOR PANEL CRACKED. REMOVED DAMAGED FLOOR PANEL. LOCATED AND DRILLED NEW FLOOR PANEL. INSTALLED NEW FLOOR PANEL SKIN. (M) 2L72 4F A6WE 20030714001102003071400110EU 2003 7 14 MALA030325 120030625A5320 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430XJ 340B430 A/C WEATHER-VANED DUE TO HIGH WINDS CAUSING SHEETMETAL DAMAGE BETWEEN STA 622-677. MAINTENANCE REPLACED FUSELAGE SKIN BETWEEN STA 622-668. ALSO COMPLETED REPAIR BETWEEN STA 668-710, BETWEEN SL1524- SL1624. ALL WORK PERFORMED IAW EO S53164. REFER TO LOG SHEET 1183788 FOR DETAIL. 2L72 4T RTA52EU 20030710000782003071000078NM 2003 7 10 DHL2003726009 120030611A7922515197 TEE FITTING BOEING727 727228 1384083NM NR 3 ENGINE LEAKING A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01726DH 20409 ON CLIMBOUT, NR 3 ENGINE OIL QUANTITY DECREASING RAPIDLY. WHEN OIL PSI WENT BELOW 40 PSI, PERFORMED IN FLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURES. FOUND PLUG ON NR 3 ENGINE OIL COOLER SUPPLY T-FITTING PARTIALLY INSTALLED/THREADS IN FITTING WERE STRIPPED. REMOVED & REPLACED T-FITTING AND ALL ASSOCIATED O-RINGS, PER P&W M/M 79-22-1. OPS & LEAK CHECK GOOD. SERVICED ENGINE OIL. 2L73 4F RTA3WE 20030714001432003071400143EU 2003 7 14 CCHA087897 120030701A6340L634M20C1001 TRANSDUCER UROCOPEC135 EC135T1 5620026EU M/R GEARBOX DEFECTIVE B CCHAO OTHER O OTHER NRNOT REPORTED 1 SW19911CK1372 0138 MAIN ROTOR GEARBXO HAS INTERMITTANT GUAGE FLUCUATIONS. 1G72 3U H88EU 20030204002802003020400280NM 2003 2 4 F3LA200300012 120030117A5320 INTERCOSTAL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED TWO CORRODED FASTENERS, INCLUDING NUT CLIPS, ON INTERCOSTAL BETWEEN STA 294.5 AND 312, LBL 11. REPLACED INTERCOSTAL PER SRM 51-40-2. 2L72 4F RTA16WE 20030127000092003012700009 2003 1 27 HEEA083585 420030114A3421504001790116 GYRO BELL 412 412 1182202SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 HORIZON GYRO PRECESSES. SHOP REPAIR. 1G72 4U H4SW 20030127001122003012700112NE 2003 1 27 DHL2003362006 220030124A7310 FUEL FILTER AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE A DHLAKO NONE OTHER O OTHER CLCLIMB 1 SO01362DH 84 517788 1) ENGINE #1 FUEL CLOG LIGHT ILLUMINATED AFTER T/O AT T/O THRUST SETTING. LIGHT EXTINGUISHED AFTER INITIAL POWER REDUCTION. DURING CRUISE LIGHT ILLUMINATED AGAIN RAN ABNORMAL PROCEDURES.2) REMOVED AND REPLACED #1 ENGINE FUEL FILTER. GROUND RAN ENGINE OPS CHECKED GOOD IAW 73-12-03. 2L72 4F4 FRTA35EU E23EA 20030127002772003012700277GL 2003 1 27 HEEA083753 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH 53461 CAUSING LOW POWER. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030820001892003082000189NM 2003 8 20 UPS03441058 120030718A5320 WEB BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, M/D - BS 360 - 380 STR 26R RBL 98 - 104 SUPPORT WEB CRACKED. SUPPORT WEB REPAIRED AS PER SRM 51-40-02. 2L74 4F A20WE 20030819000502003081900050EU 2003 8 19 RAIA00306168 120030619A3297 CONNECTOR AEROSPATR72 ATR72202 8680940EU MLG DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03723TE 283 LANDING WEAR WILL NOT RETRACT. MAINTENANCE REPAIRED RECESSED PIN AT MFC CONNECTOR. TEST FLIGHT PERFORMED AND LANDING GEAR PERFORMED WITHOUT DEFECT. 2H72 4T RTA53EU 20030331001342003033100134NM 2003 3 31 DHL2003740515 120030203A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH AFT CARGO COMPT AFT PIT FLOORBEAM AT RBL 15 IS CRACKED AT NUT PLATE STA 950E. REMOVED FASTENERS PER SRM 51-30-2. FABRICATED DOUBLER ANGLES (2024-T3 .050) PER SRM 51-40-3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 51-30-2. 2L73 4F RTA3WE 20030331001272003033100127NM 2003 3 31 DHL2003740507 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FWD CARGO FRAME HAS 3 DENTS INTO THE RADIUS AT BS 680 STR 23 & 24R. REMOVED FASTENERS FOR ACCSESS PER SRM 51-30-2. FABRICATED REPAIR DOUBLER USING .063 7075-T6 PER SR 53-10-2 FIG 11. TREATED, PRIMED AND INSTALLED PER SRM 51-40-3. 2L73 4F RTA3WE 20030408001412003040800141NM 2003 4 8 AWXA200300347 120030312A575465C206602217 STRUCTURE BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE NR 2 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 YVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OUTBOARD TRAILING EDGE OF THE NR 2 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 SLAT IAW BMM 27-81-21, PG. 401-419. 2L72 4F4 FRTA16WE E2GL 20030414000262003041400026NM 2003 4 14 SWAA030732 120030402A53106551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20030410002232003041000223 2003 4 10 DL76K030080 420030121A2565 SLIDE BOEING767 767332 1382001NM OVERWING EXIT DEPLOYED A DALAK NONE O OTHER ININSP/MAINT 1 SO27171DZ 29690 LEFT OVERWING SLIDE DEPLOYED ON ITS OWN DAMAGING SLIDE DOOR. REPLACED SLIDE, DOOR AND INFLATION CYLINDER. 2L72 4F RTA1NM 20030416000122003041600012NM 2003 4 16 UPS03439999 120030104A3350 BATTERY BOEING747 747123 1384873NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01675UP 20390 DURING PREFLT INSPECTION 2 EMERGENCY LIGHTS ARE OUT ABOVE UPPER DECK EMERGENCY EXIT DOOR. REMOVED AND REPLACED BATTERY POWER UNIT (X327) PER WDM 33-51-01 & OPERATION CHECKED GOOD. 2L74 4F A20WE 20030417001592003041700159EU 2003 4 17 MALA030149 120030210A2497 WIRE SAAB SF340 340B 7860101EU LT GENERATOR DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15414XJ 340B414 DURING FLIGHT 3184, LT A/C GEN FAILED IN FLIGHT. AIR RETURN TO DTW. MAINTENANCE FOUND SHORTS TO GROUND ON WIRES FOR PHASE B & C (APPROXIMATELY 2 MEG). REPAIRED DAMAGED WIRES NEAR C/B IN LT NACELLE PER SAAB W/M. ALL CHECKS GOOD, IAW SF-340 MM CHAP 30. 2L72 4T RTA52EU 20030423001722003042300172NM 2003 4 23 F3LA200300098 120030228A5551 ATTACH FITTING BOEING737 7373Q8 1384670NM HORIZONTAL STAB CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED CORROSION ON OUTER SURFACE OF LT. HORIZONTAL STABILIZER FRONT SPAR LOWER ATTACH LUG. REWORKED FRONTIER SPAR LOWER ATTACH LUG PER CMM 55-10-06. PERFORMED HFEC PER D637239, PART 6, 51-00-00, FIG. 23, NO CRACKS FOUND. FABRICATED AND INSTALLED BUSHING PER CMM 55-10-06, SOPM 20-10-03, MM 55-10-06, SOPM 20-50-03, AND MM 27-41-12. 2L72 4F RTA16WE 20030425000172003042500017NM 2003 4 25 HALA0300071 120030221A2430G095 IDG BOEING767 767300 1385204NM RT GENERATOR FAILED A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13585HA 24257 ATB-ETOPS SIGNIFICANT SYSTEM - RT GEN DRIVE EICAS MSG DISPLAYED GEN DRIVE LT ILLUMINATED STEADY GEN DRIVE WAS DISCONNECTED. A/C RETURNED TO LAX, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED NR 2 IDG IAW HAL 767-3-405001. REPLACED IDG AND GCU, LEAK CHECK AND OPERATIONAL CHECK NORMAL IAW CARD NOL 767-3-405001. 2L72 4F RTA1NM 20030425000402003042500040EU 2003 4 25 RAIA00303086 120030327A28213035681 FILTER AEROSPATR42 ATR42300 8680920EU FUEL SYSTEM CLOGGED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03423TE 119 STL- ENGINE NR 1 FUEL CLOG WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP FILTER, LEAK AND OPS CHECK OK. 2H72 4T RTA53EU 20030428000632003042800063WP 2003 4 28 MWEA030159 120030403A2697 WIRE DOUG DC9 DC932 3022066WP ENGINE CHAFED A MWEAO OTHER N FALSE WARNING APAPPROACH 1 GL31401ME 47133 LT ENGINE FIRE HANDLE LIGHT ILLUMINATED DURING APPROACH. REPAIRED CHAFED WIRE. 2L72 4F A6WE 20030428000122003042800012WP 2003 4 28 ZW0A0303605 120030330A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139407R 49400 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 27 TO 30. RESEATED THE BATTERIES IN THE BATTERY PACK AT ROW 29. CHECK-C 3-17-03 STL. 2L72 4F RTA6WE 20030429000522003042900052EA 2003 4 29 03101622 120030411A3350 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHT AT THE LOWER LEFT SIDE OF THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED A LOOSE WIRE CONNECTOR BEHIND THE GALLEY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20031210000762003121000076WP 2003 12 10 AALA20031320 120031123A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21576AA 53153 DFW EMERGENCY LIGHTS AT SEATS 20D AND 2D INOPERATIVE. RESECURED CONNECTOR FOR SEATS 20D AND 2D EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20030918000362003091800036NM 2003 9 18 GAIA03025SP 120030719A5313 STRINGER BOEING727 727* NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FORWARD STATION 720C, STRINGER 15L IS CRACKED AFT OF WING LIGHT. CUT OUT CRACK FROM STRINGER 15L, IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 5.2 INCH BY 3.2 INCH, TWO FILLERS .100 7075-T6 5.2 BY .8 IAW SRM 53-10-3 FIG 5, INSTALLED PARTS IAW SRM 51-10-3 FIG 5. (M) 2L73 4F RTA3WE 20030919000292003091900029WP 2003 9 19 0301549931 120030809A291037723745503 FLEX LINE DOUG DC9 DC931 3022065WP HYD SYSTEM LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL0190S 47244 UPON GEAR EXTENSION FOR LANDING, THE RT HYDRAULIC SYS FLUID QUANTITY WENT TO ZERO. LANDING GEAR LOCKED DOWN AND SAFE WITH NO FURTHER PROBLEMS. AUXILIARY HYD PUMP WAS SHUT OFF AFTER LANDING. NO MENTION OF COM COMPLIANCE OR OF OTHER HYDRAULIC SYSTEM INDICATIONS LIKE PRESSURE OR TEMPERATURE. MAINTENANCE FOUND A FAILED FLEX LINE AT THE AUXILIARY PUMP AND A LEAKING RUDDER POWER SHUTOFF VALVE. REPLACED BOTH AND THE AUXILIARY PUMP AND ASSOCIATED FILTERS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030924000172003092400017NM 2003 9 24 DLM88030724 120030805A335060030451 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27959DL 49978 ON LAYOVER CHECK FOUND RT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES AND POWER SUPPLY. 2L72 4F RTA6WE 20030923000112003092300011NM 2003 9 23 QXEA200301010 120030820A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FALSE INDICATIONA QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09365PH11185 526 MASTER WARNING AND SMOKE LIGHT ILLUMINATED AND EXTINGUSHED FOUR TIMES ON APPROACH. INTERMITTANT INDICATION. NO SIGN OF ACTUAL SMOKE. REMOVED AND REPLACED NR 1 BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030925000382003092500038NM 2003 9 25 USAA030163 120030716A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US 24552 FOUND FRAME CRACKED 1 INCH LONG, FS 601, LEFT SIDE BELOW CABIN FLOOR, THROUGH 2 FASTENERS. DAMAGE CUT OUT, FILLER AND DOUBLER INSTALLED PER EA 76450. (M) 2L72 4F RTA16WE 20040127002232004012700223WP 2004 1 27 ASAA0380658 120031015A5321936639501 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FLOORBOARD DELAMINATED. REPLACED FLOORBOARD. (M) 2L72 4F A6WE 20040128001352004012800135NM 2004 1 28 QXEA200301595 120031229A3150 WARNING HORN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FALSE ACTIVATIONA QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09402QX 4032 SEA- ON FLIGHT 2394 ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING HORN SOUNDED ON TAKEOFF AS POWER LEVERS WERE PUT FORWARD OF FLIGHT IDLE. PERFORMED TAKEOFF WARNING SYSTEM TEST IAW MM 31-52-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203000082004020300008WP 2004 2 3 ASAA0380573 120030902A531159365971 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 OAK - DURING C-CHECK, FOUND CORRODED AT FS 1231 BETWEEN LONGERON 28L AND 28R. REPLACED FRAME. (M) 2L72 4F A6WE 20040203000862004020300086WP 2004 2 3 ASAA0380797 120031119A573099375841 DOUBLER DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND LT WING LEADING EDGE SPLICE DOUBLER IS CRACKED AT STATION 120. INSTALLED SPLICE DOUBLER IAW SRM 51-30-2. (M) 2L72 4F RTA6WE 20040205000402004020500040NM 2004 2 5 MEX2003514 120031110A2915122253600 RELIEF VALVE DOUG MD80 MD83 3023681NM RT HYD SYSTEM FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23EIBTY1225112251 49667 AIRCRAFT RETURNED TO PLATFORM DUE TO RT HYD HIGH TEMPERATURE INDICATION. AIRCRAFT WAS TAKEN TO THE MAINTENANCE HANGAR AND DURING OVERNIGHT SERVICE AT MEX. THE HYD RELIEF VALVE AND THE TEMPERATURE SENSOR WERE REPLACED IAW MM 29-10-12, TESTS WERE PERFORMED IAW MM 29-30-03, ALL OK. 2L72 4F RT 20040210000552004021000055NM 2004 2 10 ASAA02401AB 120030317A575369353463 FLAP TRACK BOEING737 7374Q8 138447QNM LT WING WORN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01785AS 27628 PAE - DURING C-CHECK, FOUND LEFT OUTBOARD FOR FLAP TRACKS ARE WORN INBOARD TRACK. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031215000962003121500096NM 2003 12 15 MWEA030446 120031120A5347593054768 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 NR 4 SEAT TRACK HAS CORROSION IN SEVERAL PLACES FROM STATION 200 - 256. FABRICATED AND INSTALLED SEAT TRACK SECTION. 2L72 4F RTA6WE 20040309001542004030900154WP 2004 3 9 GTIA031051 120031225A3350 SIGN DOUG DC9 DC981 3022081WP CABIN OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23805NK 48058 LGA - FOUND AFT GALLEY G-4 GALLEY EMERGENCY FLOOR EXIT SIGN MISSING. FOUND AND REINSTALLED G-4 EMERGENCY EXIT SIGN. (M) 2L72 4F A6WE 20040316000962004031600096WP 2004 3 16 ASAA0380299 120030408A5320993061285 MEMBRANE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 1322, OUTBOARD OF OUTBOARD SEAT TRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F RTA6WE 20030128000862003012800086EA 2003 1 28 03025708 120030125A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE J WARNING INDICATION ININSP/MAINT 1 EA27708BR L/H EMERGENCY LIGHT INOP. RELAMPED LIGHT, OP'S CK'D GOOD 2L72 4F RTA21EA 20030625001212003062500121NM 2003 6 25 AWXA200300030 120030111A2121731376 FAN BOEING757 7572S7 1384962NM ZONE 821 OVERHEATED A AWXAH DEACTIVATE SYST/CIRCUITS O OTHER NRNOT REPORTED 1 WP28902AW45355 23322 BURNING SMELL - EN ROUTE OBSERVED A STRONG ELECTRICAL ODOR IN FLT DECK WITH EXCESSIVE HEAT, UNABLE TO LOCATE SOURCE, NO C/B POPPED. MX DISCOVERED EQUIPMENT COOLING FAN NR 2 CIRCUIT BREAKER POPPED. COLLARED CIRCUIT BREAKER AND PLACED ON MEL 21-58-3, COND 1, ONE FWD EQUIPMENT COOLING FAN INOP. MX REMOVED AND REPLACED EQUIPMENT COOLING FAN IAW BMM 21-58-06, AND FORWARD EQUIPMENT EXHAUST SMOKE DETECTOR (TS164) IAW BMM 21-58-19-201; OPS CHECKS GOOD. *S/D* VENDOR TEARDOWN OF EQUIPMENT COOLING FAN (AXIAL FLOW) S/N 0706 CONFIRMED FAILURE OF UNIT. TEARDOWN REVEALED THE MOTOR BEARING WAS SHATTERED & FAN CONTACTED CASE HOUSING. UNIT REPAIRED & TESTED IAW OHM 21-58-15. NO PART REPLACED, INFO SUPPLIED BY VENDOR. 2L72 4F RTA2NM 20030206001602003020600160EA 2003 2 6 A6WA200340020 120030118A3620 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31406AW 7402 14TH DUCT WARNING MESSAGE IN FLIGHT, COMPLIED WITH QRH MESSAGE CAME BACK TWICE MOMENTARILY. AFTER LANDING P/L IDLE MESSAGE CAME BACK STAYED ON GROUND RAN A/C AT VARIOUS POWER SETTINGS. RAN ALL SYSTEMS ASSOCIATED WITH 14TH STAGE BLEED, NO FAULTS NOTED. PER MAINTENANCE CONTROL SWAPPED LOOP CONTROL UNITS. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030207001022003020700102WP 2003 2 7 03FDEA00057 120030120A324160001893C1A VALVE DOUG MD10 MD1010F WP GE CF6 CF6* 30020GL ANTI-SKID SYS FAILED A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25566FE 46989 WHEN LOWERING THE GEAR FOR LANDING GEAR WAS DOWN AND LOCKED. WE HAD ANTI-SKID FAIL WARNING ON CONFIG PAGE. WENT AROUND RECYCLED GEAR DID NOT GET THE WARNING THE SECOND TIME. ALSO TRIED RECYCLING ANTI SKID SWITCH WITH GEAR DOWN DID NOT PUT THE WARNING LIGHT OUT. REMOVED AND REPLACED UPPER (C) ANTI-SKID VALVE ON LT MLG IAW AMM. OPS CHECK IAW 32-45-00-2 PARA 2A/B. AIRCRAFT OK FOR CONTINUED SERVICE. 2L73 4F4 FRTA22WE E23EA 20030219000052003021900005CE 2003 2 19 DYVA0002 120030129A2120 SMOKE CESSNA421 421C 2076016CE CABIN DETECTED A DYVAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07215MP 421C1231 DURING FLIGHT, SHORTLY AFTER HEATER WAS ACTIVATED, AN ODOR WAS OBSERVED IN AFT CABIN, FOLLOWED BY SMOKE. HEATER WAS TURNED OFF AND THE AIRCRAFT RETURNED TO BASE WITH NO INCIDENT. HEATING SYSTEM WAS INSPECTED INCLUDING A HEATER PRESSURE DECAY TEST. THE SYSTEM WAS FOUND TO HAVE NO DEFECTS AND HEATER CANISTER COMBUSTION CHAMBER PASSED THE MANUFACTURES DECAY TEST. A NEW HEAT DUCT WAS RECENTLY INSTALLED AND MAY HAVE HAD SOME MANUFACTURING OR STORAGE RESIDUE THAT EMMITED THE ODOR AND SMOKE. THE HEATING SYSTEM WAS OPERATED ON THE GROUND FOR SEVERAL MINUTES WITH NO ODOR OR SMOKE OBSERVED. CONTINUED OPERATION DURING FLIGHT AFTER RETURN TO SERVICE ALSO REVEALED NO ODOR, SMOKE, OR ABNORMAL FUNCTION. 1L72 3O A7CE 20030219000832003021900083NM 2003 2 19 SWAA030294 120030206A52306545871 DOOR FRAME BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER BEAM CRACKED AT NR 2 STOP FITTING. REMOVED AND REPLACED LOWER BEAM WEB PER SRM. 2L72 4F RTA16WE 20030116000652003011600065SW 2003 1 16 HEEA083024 120030106A6220 BUSHING BELL 206 206L3 1182108SW DRIVE LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 MAIN ROTOR HEAD HAS WORN BUSHINGS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116001052003011600105 2003 1 16 HEEA083057 420030107A34570110005400 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341791 51465 GPS MENU BUTTON INOPERATIVE. 1G71 3U H2SW 20030116001112003011600111 2003 1 16 HEEA083061 420030107A2312064101900 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 TRANSCEIVER SELECTOR KNOB BENT AND WOULD NOT MOVE. 1G71 3U H2SW 20030224000032003022400003SW 2003 2 24 ALGA084091 120030205A6410406016100119 BLADE BELL 407 407 1182206SW TAIL ROTOR PEELING H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01408AL24 53491 FOUND PAINT PEELING FROM NEW TAIL ROTOR BLADES. TIME SINCE NEW ON BLADES IS 23.7 HOURS. 1G71 3U O H2SW 20030227001082003022700108 2003 2 27 HEEA084414 420030212A344280510800001 CONTROL BOX BELL 214 214ST 1182106SW WX RADAR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 SKYWATCH DATA BOX SHOWS TAC FAIL CONSTANTLY. 2G72 4U H10SW 20030228000152003022800015NM 2003 2 28 SWAA030393 120030219A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030307000282003030700028NM 2003 3 7 SWAA030476 120030303A57126545444 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D CHECK, FOUND RT WING UPPER RIB CHORD CRACKED AT WS 114, STR 2. REPAIRED RIB PER BFG ER. 2L72 4F RTA16WE 20030310001252003031000125SW 2003 3 10 HEEA085025 120030228A6220206011118001 SEAL BELL 206 206L1 1182107SW M/R HEAD CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032133X6371 HB156 45634 MAIN ROTOR HEAD WHITE GRIP SEAL SLINGING GREASE. REPLACED SEAL DUE TO CORROSION. REPAIRED. 1G71 3U H2SW 20030310001562003031000156NM 2003 3 10 EIA2003024 120030227A5300UNK STRAP BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Lap repairs from STA 1960-2180 at Stringer 19L requires additional strap. CORECTIVE ACTION: Installed external strap per ECRA 481-53-169-2 Rev A 2L74 4F A20WE 20030429001942003042900194NM 2003 4 29 CA030409017 120030403A5330 SKIN BOEING737 7372Q9 138448MNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5754854795 (CAN) 1.7500 FT CRACK FOUND ON EXTERIOR FUSELAGE AT FS 767 AT STRINGER S-18R. CRACK REPAIRED I.A.W. SRM 53-30-3 FIG.1 TIMES -57548:02CYCLES -54795 2L72 4F4 F A16WE E2EA 20030502000972003050200097EU 2003 5 2 AWXA200300383 120030329A5310D5438002009701 SHEAR TIE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A CRACK WAS FOUND ON SHEAR WEB AFT SIDE OF FR 68, AND OUTBOARD OF Y-1292 RT. MAINTENANCE REMOVED CRACKED SHEAR WEB AFT SIDE OF FR 68, Y1292 RT. FABRICATED A NEW REPLACEMENT SHEAR WEB. INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-A24. 2L72 4F RTA28NM 20030505000032003050500003NM 2003 5 5 03FDEA00444 120030415A5330 TRIPLER BOEING727 727200 138407ENM FUSELAGE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 COMPLY WITH EA 7-5330-68778; TRIPLER SURROUNDING MAIN CARGO DOOR HAS WEAR, REWORK AS INSTRUCTED. FACT 15APR03 10:55 BFM R, COMPLIED WITH EA 7-5330-68778 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR, P/N 53FX1301-9/-7 (AD 2002-16-19). 2L73 4F RTA3WE 20030505000092003050500009EU 2003 5 5 XNOA01116 120030419A2761 BELLCRANK AIRBUS300 A300B4203 3930306EU SPOILER ACTUATORSTUCK A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23373PC 218 AFTER T/O PROGRESSIVELY INCREASING RT AILERON (RIGHT WING DOWN) REQUIRED TO KEEP AIRCRAFT FLYING WINGS LEVEL. FCPI SHOWED LEFT SPOILER DEFLECTED APPROX 12 DEGREES. ON GROUND LEFT O/B SPOILER WAS DEFLECTED FULL UP (ACTUAL POSITION). INSPECTED & FOUND LEFT INBOARD FLIGHT SPOILER ACTUATOR BELLCRANK ASSY STICKING AS A RESULT OF DIRT & GRIME. CLEANED & LUBED BELL CRANK ASSY. SPOILER SYS, OPS CHECK GOOD IAW A300 MM 27-10-00. 2L72 4F RTA35EU 20030506000362003050600036NM 2003 5 6 DHL2003741549 120030324A552165C3082523 SPAR BOEING727 727200 138407ENM LT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK, LT ELEVATOR NR 3 TAB HINGE LOOSE, INDICATION OF CRACK. REMOVED DAMAGED SPAR AND INSTALLED NEW P/N 65C30825-23 PO 307748 PER S/B 727-55-0089 R1. OP'S CHECK GOOD IAW M/M 27-30-00. 2L73 4F RTA3WE 20030506000812003050600081NM 2003 5 6 03FDEA00583 120030423A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FRAME BS 720C, LBL 10, WL 149. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20030513002222003051300222WP 2003 5 13 ZW0A0304502 120030419A33500105601003PA57 COVER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT MISSING A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13966TW 53616 DURING OVERNIGHT INEPECT EMERGENCY LITE COVER AT 3E MISSING. REPLACED EMERGENCY LITE COVER AT 3E. PERF OPS CHECK PER MM 33-53-00. CHECK-C 6-07-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030513002322003051300232EU 2003 5 13 CX7A194J39 120030422A3230 LANDING GEAR SAAB SF340 340B 7860101EU MAINS INOPERATIVE A CX7AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL03307CE 340B204 GEAR WOULD NOT RETRACT-PUMP OPERATING CONTINUOUSLY. 2L72 4T RTA52EU 20030509001742003050900174NM 2003 5 9 USAABB03056 120030405A2612 FIRE DETECTOR BOEING767 7672B7 1385107NM CARGO BAY MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19656US 26847 CREW RECEIVED THE EICAS MESSAGE 'CARGO BTL 2' AND THE BOTTLE DISCHARGED LIGHT. A FLIGHT ATTENDANT REPORTED THAT THE AFT GALLEY FLOOR WAS WARM, WHICH WAS VERIFIED BY ONE OF THE PILOTS. FLIGHT DIVERTED TO YQX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AFT CARGO COMPARTMENT AND EQUIPMENT AREA. NO EVIDENCE OF EXCESSIVE HEAT WAS FOUND. THE SQUIB TEST AND FIRE/OVERHEAT WARNING TESTS WERE PERFORMED WITH NO FAULTS FOUND. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L72 4F RTA1NM 20030514001132003051400113NM 2003 5 14 SWAA031024 120030508A335007912 WIRE BOEING737 7373H4 1384600NM EMERGENCY LIGHT EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 EEPLS WIRES EXPOSED AT ROW 11. REMOVED AND REPLACED EEPLS TRACK COVER PER MM. 2L72 4F RTA16WE 20030604000342003060400034SO 2003 6 4 SIMA200312707 120030416A531014522461011 GUSSET EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, THE DIAMOND GUSSET AND RIGHT HAT BEAM AT FRAME 20 HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET ON RIGHT HAT BEAM IAW EMB 135 SRM 51-20-03, 51-40-02/06. (M) 2L72 4F RTT00011AT 20030606000272003060600027WP 2003 6 6 03FDEA00729 120030513A2780NRB62241 SKIN DOUG DC10 DC1030 3023501WP LE SLAT CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25316FE 48314 COMPLY WITH E.A. 8-5722-70371, WINGS - REPAIR OF MINOR DAMAGE TO LEADING EDGE SLAT SKIN. ACT 07MAY03 06:26 BFM R COMPLIED WITH E/A 8-5755-70371 AT MAE/BFM. 2L73 4F A22WE 20030521001462003052100146WP 2003 5 21 DHL2003801012 120030418A5730576954589 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT OUTER WING OUTBOARD L/E OUTER PLATING CORRODED AT STA XW 761.000. PERFORMED MAJOR REPAIR IAW EO DHL 030404, ED 3254. REMOVED CORROSION FROM LT WING OUTBOARD L/E OUTER PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED AREA IAW EO DHL 030404, ED 3254. FABRICATED FILLER (7075-T6 0.050) AND DOUBLER (7075-T6 0.063) IAW EO DHL 030404, ED 3254. CLEANED, TREATED AND PRIMED INNER SIDE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EO DHL 03404 ED 3254, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030609000112003060900011SO 2003 6 9 SWIA200311978 120030513A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07301YV6935 6935 120301 CONTROL FAULT RECEIVED ON OUTBOARD FLAPS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW 27-50-09. 2L72 4T RTA31SO 20030612000722003061200072NM 2003 6 12 UPS03440715 120030519A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D CROWN - S4R STRINGER CORRODED FROM BS 1311 TO 1319. CORROSION BLEND OUT 0.030 X .5 X 2 INCH EXCEED SRM LIMIT. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. 2L74 4F RTA20WE 20030610000902003061000090NM 2003 6 10 DLM88030433 120030506A335060030451 CHARGER DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27902DE 53379 EMERGENCY LIGHTS OUT AT ROW 17 THRU ROW 23. REPLACED BATTERY CHARGER 2L72 4F RTA6WE 20030520001182003052000118 2003 5 20 WRLA200308 420030415A2565 BOTTLE DOUG MD11 MD11 3023602NM ESCAPE SLIDE DISCHARGED A WRLAK NONE O OTHER ININSP/MAINT 1 EA27278WA 48746 PRIOR TO SLIDE RAFT DEPLOYMENT EGAT ADVISED THAT THE BOTTLE PRESSURE OF THE SLIDE RAFT INDICATED ZERO. THE PRESS TO TEST SYSTEM INDICATED NORMAL. THE SLIDE RAFT WAS DEPLOYED TO VERIFY PROPER DEPLOYMENT. THE SLIDE DEPLOYED BUT FAILED TO INFLATE. THE PRESS TO TEST SWITCH WAS INSPECTED AND FOUND TO BE WIRED INCORRECTLY. THE SLIDE RAFT ASSEMBLY WAS REPLACED IAW MM 25-61-1. REPLACED SLIDE RAFT ASSEMBLY. (M) 2L73 4F RTA22WE 20030527000232003052700023NM 2003 5 27 DHL2003747505 120030513A5311 FRAME BOEING727 727224 1384076NM CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR FRAME AT BS 600 DENT AND CRACK BETWEEN STR 16R/17R. CUT OUT DAMAGED AREA ON FRAME DIM 1 X .75 INCH AND FABRICATED ONE DOUBLER REPAIR DIMENSIONS 9 X 7 INCHES USING 7075-T6 .063 PO 92123380 IAW B-727 SRM 51-40-3. ALODINED AND PRIMED DOUBLER IAW B-727 SRM 51-10-2. INSTALLED REPAIR AT FRAME BS 600 IAW B-727 SRM 51-40-3. 2L73 4F A3WE 20030617001362003061700136NM 2003 6 17 QXEA200300722 120030602A7110 BRACKET BOMBDRDHC8 DHC8401 1390041NM COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - TOP "L" ATTACH BRACKET CRACKED AT FORWARD TWO RIVETS, FOR CENTER WEB SUPPORT, AFT CONE TO UPPER DECK. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030618001982003061800198SW 2003 6 18 HEEA087367 120030611A5210407070620143 PANEL BELL 407 407 1182206SW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 CREW DOOR PANEL CRACKED BEYOND REPAIR. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030528000792003052800079EA 2003 5 28 2003F00301 120030404A3222601R85002 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG UNDERSERVICED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0747239 7239 AFTER TAKEOFF, AIRCREW REPORTED GEAR DISAGREE AND NOSE GEAR DOR OPEN. CREW SELECTED GEAR DOWN AND GOT THREE GREEN DOWN AND LOCKED. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING AT THIS TIME. MAINTENANCE SERVICED STRUT. OPS CHECKS GOOD ON DROP CHECK. (M) 2L72 4F RTA21EA 20030618002182003061800218SW 2003 6 18 HEEA087171 120030609A6330206033509003 BEARING BELL 206 206L3 1182108SW RESTRAINT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X LK0424 51552 TRANSMISSION RESTRAINT WORN BEARINGS. REPLACED BEARINGS (2 EA) DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030619000192003061900019SW 2003 6 19 HEEA087182 120030609A7714206076373001 TACH GENERATOR BELL 206 206L3 1182108SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 CAUSING NR SPIKES TO THE INTELLISTART SYSTEM. 1G71 3U H2SW 20030624000682003062400068SO 2003 6 24 LR7A03048 120030613A53433883941 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 578 4590 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB3201 FOUND LT FS 517 MLG BEAM OUTER CAP CRACKED AT WL 215, LBL 62. REPLACED OUTER CAP IAW DWG 388394 AND SRM SMP 583 51-70. NR 0014. 2H74 4T A1SO 20030625001302003062500130EU 2003 6 25 03100316 120030410A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE L/H FWD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED THE LAMP IN THE LIGHT SOCKET. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030709000162003070900016WP 2003 7 9 AALA20030595 120030522A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21473AA 49648 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS FROM 1-19 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORAML OPERATION. (M) 2L72 4F A6WE 20030709000232003070900023WP 2003 7 9 AALA20030526 120030502A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21402A 49313 DURING OVERNIGHT, MAINTENANCE FORWARD EMERGENCY EXIT LIGHTS COMMON TO EMERGENCY EXIT LIGHT BATTERY PACK B5 23 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030710000712003071000071NM 2003 7 10 DHL2003746500 120030603A5311 FRAME BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 DURING C-CHECK DISCREPANCY AS FOLLOWS, IN FWD CARGO FRAME BS 660 HAS A DENT INTO THE RADIUS AT STR 25R. CUT OUT DAMAGED AREA OF FRAME AT BS 660 AT STR 25 R DIMENSIONS 1 INCH X 4.5 INCH AND FABRICATED ONE DOUBLER DIMENSIONS 3.5 INCH X 19 INCHES USING .063 7075-T6 PO 9912495 IAW B-727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. ALODINED AND PRIMED DOUBLER IAW B-727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B-727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20030109000772003010900077SO 2003 1 9 C2XA03BT005 120030106A2530 COFFEEMAKER EMB 135 EMB135LR 3260305SO FAULTY A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2712528 145504 CLE---CO2162, CREW REPORTED, " STRONG BURNING SMELL IN GALLEY WITH AND WITHOUT GALLEY POWER ON." INSPECTED AND REPLACED HOT JUG AS REQUIRED. (OPS.CHECKED NO BURNING SMELL NOTED, AIRCRAFT RETURNED TO SERVICE.) 2L72 4F RTT00011AT 20030109001292003010900129NM 2003 1 9 S03J30001 120030101A3000 WINDSHIELD BOEING747 747400 NM GE CF6 CF680C2* GL 1L WINDSHIELD OVERHEATED W SAJFO OTHER O OTHER CRCRUISE 1 WP03 30760 B-18702During flight from SIN to TPE, LH windshield was noticed smoke and scorching smell.The abnormality disappeared after switched off LH window heat functionC/A:1. Check found LH windshield lower bus bar terminal have poor contact, accordingly, the terminal was replaced.2. After replaced the terminal,the window heat function test normal IAW AMM 30-41-00.3. EON will be issued for one time inspection on 747-400 fleet. 4. Submmit the Service Difficulty Report to Boeing for investigation, and request Boeing to provide preventive action. 2L74 4F4 FRTA20WE E23EA 20030311000472003031100047 2003 3 11 HEEA085062 420030228A2561PHI10090 LIFE VEST BELL 206 206L3 1182108SW CABIN WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036748D 51106 LIFE VEST FAILED 3 MONTH INSPECTION (WOULD NOT HOLD AIR). SHOP REPAIR. 1G71 3U H2SW 20030313001542003031300154SO 2003 3 13 WVBA2003001 120030221A8120LW12778 WASTEGATE VALVE PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA TURBOCHARGER LEAKING E WVBAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 AL014082T 318152089 RL74168A AIRCRAFT ENROUTE, MANIFOLD PRESSURE AND OIL PRESSURE STARTED DECENDING. AIRCRAFT LANDED. MECHANICS FOUND WASTEGATE LEAKING OIL FROM DRAIN. WASTEGATE REPLACED, TESTED ON RUNUP, WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 1L72 3O3 O A20SO E14EA 20030313001802003031300180WP 2003 3 13 AALA20030138 120030204A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21588AA 53251 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET STATION 1380 1 INCH ABOVE LEFT PYLON. INSTALLED DOUBLER PER 53-01-00, AARD 53-30-00-02. (M) 2L72 4F RTA6WE 20030121001752003012100175GL 2003 1 21 HEEA083326 220030109A7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE FLUCTUATES E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW036251X8657 51552 GOVERNOR PRODUCING TORQUE AND TOT FLUCTUATES. UNABLE TO VERIFY DIFFICULTY REPORTED. NO DISCREPANICES NOTED. 1G71 3U3 U H2SW E1GL 20030121002452003012100245SW 2003 1 21 HEEA083363 120030109A6300 BEARING BELL 206 206L3 1182108SW CRADLE ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 MAIN ROTOR DRIVE, CRADLE ASSY BEARING WORN. SCRAPPED. 1G71 3U H2SW 20030122000292003012200029SW 2003 1 22 HEEA083416 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038590X452 51494 MAIN BATTERY WEAK. 1G71 3U H2SW 20030318000332003031800033SW 2003 3 18 ERAA085157 120030218A3212D24921119 FLOAT BELL 412 412 1182202SW MLG DAMAGED H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01422EH1095 33068 FWD CELL OF FLOAT BAG HAS 2 HOLES IN IT. PINHOLES WERE PATCHED IAW OHSS 100-1 AND BAG WAS TESTED IAW 412-SI-2. 1G72 4U H4SW 20030418001492003041800149 2003 4 18 MALA030167 420030222A34206226190113 COMPUTER SAAB SF340 340B 7860101EU AHRS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15457XJ 340B457 DURING FLIGHT NR 2996, CAPT AND F/O'S HEADING OFF 10 DEGREES. YELLOW HEADING ON EHSI ON ABOUT EVERY 2 MINUTES. HDG SLAVE RESETS TO ABOUT 5 DEGREE DIFFERENCE. F/O'S HDG MATCHES MAG COMPASS, CAPTS HDG DRIFTS TO ABOUT +9 DEGREES. AIR RETURN TO DTW. MAINTENANCE REPLACED NR 1 AHRS COMPUTER P/N 622-6190-113, SN/OFF 3045, SN/ON 279. NR 1 AHRS OPS CHECKS GOOD IAW SF340, MM CHAP 34. 2L72 4T RTA52EU 20030422000322003042200032EA 2003 4 22 ASOA03082 120030226A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 FLT 4771 - DUIRNG A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 14 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 14. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030422001622003042200162NM 2003 4 22 UPS03240274 120030221A5320 STIFFENER BOEING727 727108C 1384039NM NLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C+SI, VERT STIFFENER HAS INTERGRANULAR CORROSION AT BS 343 APPROX AT NLG CUTOUT LT VERT WEB. INSTALLED NEW STIFFENER IAW SRM 51-30-02. 2L73 4F A3WE 20030730000122003073000012WP 2003 7 30 ABXA030215 120030528A5415591326238 ATTACH ANGLE DOUG DC9 DC941 302207NWP NR 2 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 NR 2 ENGINE LOWER PYLON ATTACH ANGLE WAS CRACKED AT STA 1030. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20030805000662003080500066NM 2003 8 5 AALA20030661 120030614A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139356 24037 DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 32H INOPERATIVE. RECONNECTED SEAT MOUNTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030903000092003090300009NM 2003 9 3 SCNA03003 120030714A3350 LAMP BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15806SY 28215 EXTERIOR EMERGENCY OVERWING EXIT LIGHT BEHIND THE AFT LT OVERWING DOOR INOPERATIVE. RELAMPED THE EMERGENCY LIGHT, OPS CHECKED GOOD. 2L72 4F RTA16WE 20030902001392003090200139WP 2003 9 2 DHL2003807013 120030708A3097 WIRE DOUG DC8 DC873F 302199FWP WINDSHIELD SHORTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01807DH 45990 HEAVY STATIC BUILDUP ON CENTER WINDSHIELD PANEL CAUSED LARGE SPARK. CENTER WINDSHIELD BEGINS TO SMOKE AND THE CIRCUIT BREAKER POPPED. FOUND CENTER WINDSHIELD (PUCK) SENSOR WIRES MAKING CONTACT WITH RETAIN SPRING, REPAIRED WIRE, SYSTEM REQUIRES FURTHER TROUBLESHOOTING. DEFERRED SYSTEM IAW MEL 30.5 CAT. (C) DMI NR 13464 ASSIGNED. REF. DMI NR 13464 HEAVY STATIC BUILD UP ON CENTER WINDSHIELD PANEL CAUSED LARGE SPARK. REF. LOG PAGE 322177 ITEM NR 1. SYSTEM CHECKED GOOD IAW AMM 30-40-0. PLACARD REMOVED. THIS CLEARS DMI NR 13464. 2L74 4F RT4A25 20030904000432003090400043EA 2003 9 4 SWIA200312280 120030719A532060034017723 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 280 PILOT'S BULKHEAD LT VERTICAL ANGLE LBL 12 CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ REO 601R-53-11-034 REV ''A''. P/N: 600-34017-723 2L72 4F RTA21EA 20030904001692003090400169WP 2003 9 4 DHL2003873559 120030628A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING CTR L/E PLATING CORRODED AT XFS 354.000 UPPER PART (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORRSION ON CTR L/E PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 44. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 57-2-1 FIG 44. CLEANED, TREATED AND PRIMED DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED NEW DOUBLER ON CTR L/E STA XFS 354.00 (UPPER PART) WITH NEW FASTENTERS IAW SRM 57-2-1 FIG 44, SRM 51-1-21 PG 1, 51-1-20D PG 9. FOR REMOVAL AND REINSTALLATION OF CTR L/E SEE N/R 0824. 2L74 4F RT4A25 20030730000582003073000058WP 2003 7 30 ABXA030302 120030617A533059114333 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 CRACK IN SKIN .25 INCH IN LENGTH FROM RIVET HOLE BETWEEN LONGERON 12 LEFT AND LONGERON 13 LEFT AT STA 1114. REPAIRED DAMAGED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030825000312003082500031WP 2003 8 25 UPS03840957 120030708A33505708454503 BATTERY PACK DOUG DC8 DC871F 302199DWP COCKPIT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOPERATIVE. ROBBED EMERGENCY LIGHT BATTERY PACK FROM A/C 708 SN D69 P/N 5708454-503. OPS CKS GOOD 2L74 4F RT4A25 20030827001612003082700161NE 2003 8 27 2003UALA00617 220030812A7532 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ENGINE BLEED SYSFAILED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29452UA 955 ABORTED TAKEOFF DUE TO NR 1 ENGINE N2 OVERSPEED AND EGT AMBER. DUE TO 2.5 BLEED ACTUATOR MALFUNCTION THE BLEED VALVE FAILED IN OPEN POSITON RESULTING IN HIGH EGT. DEN MAINTENANCE REPLACED THE 2.5 BLEED ACTUATOR AND LUBRICATED THE 2.5 BLEED VALVE ACTUATING MECHANISM. N2 WAS 100.1 FOR 1 SEC AND THAT WAS WITHIN JRH ACCEPTABLE LIMITS. 2L72 4F4 FRTA28NM E40NE 20030910001942003091000194NM 2003 9 10 USAASB03133 120030808A2613659401 CONTROL MODULE BOEING737 7373B7 1384580NM E/E BAY FAULTY A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19520AU 23706 ORF - FLT 636 - EN ROUTE FROM CLT-PVD, AT FL330, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW REDUCED THE NR 1 ENGINE THROTTLE TO IDLE AND THE LIGHT EXTINGUISHED. CREW DECLARED AN EMERGENCY AND DIVERTED TO ORF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE M279 FIRE/OVERHEAT CONTROL MODULE PER MM 26-10-01. PERFORMED FAULT ISOLATION PER MM 26-11-00-1. NO FAULTS NOTED. RAN ENGINE FOR 15 MINUTES AT POWER SETTING. NO FAULTS NOTED. (M) 2L72 4F RTA16WE 20030929000672003092900067EU 2003 9 29 AWXA200301017 220030903A7200 ENGINE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU NR 1 SURGES A AWXAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 WP28308AW 24710 724432 AFTER TAKEOFF FROM SJC EN ROUTE FOR PHX THE NR 1 ENGINE BEGAN TO SURGE (N1) BETWEEN 85 TO 90 PERCENT AT HIGH POWER LOADS DURING CLIMB AND STRAIGHT AND LEVEL FLIGHT. TURNED BACK TO SJC AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT PER BMM 71-00-42, RAN ENGINES TO TAKEOFF POWER 92.6 PERCENT, ACCELERATION AND DECELERATION WAS SMOOTH, AND ALL PARAMETERS WERE STABLE AND NORMAL. ENGINE RUN ACCOMPLISHED WITH POWER MANAGEMENT CONTROL (PMC) ON AND OFF, NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E21EU 20030929001202003092900120EU 2003 9 29 RAIA00309235 120030904A7930 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU RT ENG OIL ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03567HK 41085 RIGHT OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE INSPECTED FOUND FUZZ ON PICK-UP. TOOK SOAP SAMPLE. ACFT RETURNED TO SERVICE. 2L72 4T RTA41NM 20030908001812003090800181EA 2003 9 8 SWIA200312262 120030815A27604916406 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07918SW1865 1865 7645 PILOT REPORTS L SPOILER FAULT ON INBOUND FLIGHT. REPLACED NR 1 SECU. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20031003000442003100300044NM 2003 10 3 AWXA200301048 120030815A575465C2619129 DOOR BOEING737 737277 1384570NM NR 5 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .3125 INCH CRACK WAS FOUND ON NR 5 SLAT ACTUATOR CLOSE OUT DOOR. MAINTENANCE REMOVED CLOSE OUT DOOR ON NR 5 SLAT AT WBL 435; FABRICATED A NEW REPLACEMENT CLOSE OUT DOOR PER DWG 65C26191; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 1. 2L72 4F RTA16WE 20031007001172003100700117GL 2003 10 7 DXTA200300116 220030915A7532 BLEED VALVE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RT ENGINE MALFUNCTIONED E DXTAEC ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07938QS 7500183 CAE330384 UPON CLEARED FOR TAKEOFF, ADVANCED THROTTLES AND THE RED CAS MESSAGE, ENGINE FAIL R APPEARED. ENGINE AUTO SHUTDOWN. EXCEEDS PAGE SHOWED IT WAS TRIGGERED BY R ITT 1020 DEGREES COMPARED TO LEFT ITT OF 644 DEGREES. BORESCOPED COMBUSTION SECTION & TURBINE ASSEMBLIES PER RR AE3007C MM CHAPTER 72-40-00 & 72-50-00, NO DEFECTS NOTED. REPLACED START BLEED CONTROL VALVE WITH NEW REF ROLLS ROYCE SB AE3007C-75-021. GROUND RAN ENGINE, OPS CHECKED GOOD. 2L72 4J4 FRTT00007WITE6CH 20031007000722003100700072 2003 10 7 SWAA031946 420030830A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD SVC DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20031008000392003100800039NM 2003 10 8 HOC2003F00026 120030826A5330 SKIN BOEING727 727224 1384076NM FUSELAGE CORRODED B HOCRK NONE O OTHER ININSP/MAINT 1 WP0779749 22451 DURING C CHECK, CORROSION WAS NOTED ON FUSELAGE INTERIOR SKIN AT STA 660-680 RBL-1. 2L73 4F A3WE 20031020002882003102000288NM 2003 10 20 2003UALA00652 120030827A2421764939A IDG BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE LT & RT ENGINES CONTAMINATED A UALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 WP29789UA 26935 LT & RT GENERATOR FAILED IN FLIGHT DURING CRUISE. RT GENERATOR DRIVE LIGHT ILLUMINATED & RT GENERATOR MANUALLY DISCONNECTED. THEN LT GENERATOR FAILED. GENERATOR OIL SYSTEM FLUSHED & BOTH GENERATORS REPLACED. LEFT & RIGHT BACKUP GENERATOR OIL SYSTEM FLUSHED & SERVICED TO CORRECT LEVEL. MAINTENANCE REPORTED WATER COMING OUT OF LT IDG FILL LINE. WATER CONTAMINATION FOUND IN BOTH IDGS. 2L72 4F4 FRTT0001SE E46NE 20031027000572003102700057EA 2003 10 27 COMA0360430 120030925A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01821CA 7420 FLIGHT 5836 DURING DECENT INTO YUL RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3,(A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F4 FRTA21EA E15NE 20040129001872004012900187 2004 1 29 AALA20040034 420031119A25655A33073 SLIDE BOEING737 737823 13844BZNM GALLEY DOOR WILL NOT TEST A AALAK NONE L NO TEST ININSP/MAINT 1 SW21905AN 29507 MCI RIGHT HAND FORWARD GALLEY DOOR EVACUATION CHUTE SLIDE AT FORWARD STATION 340 RIGHT FAILED OPERATIONAL TEST. DOOR WOULD NOT FULLY OPEN WITH GIRT BAR INSTALLED. FOUND GIRT BAR RETAINER SNAGGED ON SLIDE PACK FABRIC NOT ALLOWING DOOR TO OPEN. REPLACED WITH A SERVICABLE CHUTE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040204001732004020400173CE 2004 2 4 55265 120031015A3210 LANDING GEAR BEECH 1900 1900D 1154162CE MAINS FAILED A AMWAO OTHER J WARNING INDICATION DEDESCENT 1 CE07173YV UE173 UPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND. IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN) CREW GOT THREE DOWN AND LOCKED IND AHD SAFETY WITH NO FURTHER INCIDENTS. 2L72 4T RTA24CE 20040212000722004021200072NM 2004 2 12 HNAA0300080 120031205A323183231014003 CONTROL ROD DHAV DHC8 DHC8201 2809001NM MLG DOOR BROKEN A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07985HA 479 LT AFT GEAR DOOR DID NOT CLOSE AFTER GEAR RETRACTION. 2H72 4T RTA13NM 20031105000242003110500024SO 2003 11 5 C2XA03SH418 120031028A2560A114000002 LIGHT EMB 145 EMB145LR 3260212SO FLASHLIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711539 145536 SHV-DURING C-CHECK THE FORWARD EMERGENCY FLASHLIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT LAMP IAW DME CORPORATION VCMM 25-60-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031106002392003110600239WP 2003 11 6 GTIA030720 120030828A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND LEFT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES SEVERAL AREAS FROM FS 1050-1136. FOUND LEFT OUTBOARD SEAT TRACK FS 1050-1136 OUT OF LIMITS. REMOVED LEFT OUTBOARD SEAT TRACK. LOCATED AND DRILLED NEW TRACK. INSTALLED NEW TRACK. (M) 2L72 4F A6WE 20031110001122003111000112EA 2003 11 10 SWIA200312539 120031018A27604916405 ECU CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07915SW 7615 FLIGHT SPOILERS STATUS MESSAGE ON TAXI OUT. REMOVED AND REPLACED NR 2 SECU PER AMM 27-61-05. OPS CHECK GOOD. P/N OFF: 49-164-05, S/N OFF: 01430. 2L72 4F RTA21EA 20031112001062003111200106NM 2003 11 12 AWXA200301384 120031107A2497NOTPROVIDED WIRE BOEING757 757225 1384959NM ELECTRICAL SYS ARCED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP28914AW 22208 LAS - FIRE - WHILE TROUBLESHOOTING STATIC INVERTER PROBLEM, WIRE BUNDLE W0060 ARCHED BURNING THRU MULTIPLE WIRES AT CLAMP JUST INBOARD OF P6-1 DOOR HINGE. MAINTENANCE REPAIRED DAMAGED WIRES IN WIRE BUNDLE W0060 JUST INSIDE OF P6-1 DOOR HINGE IAW SPM 20-00-13 & 20-10-13. PERFORMED VOLTAGE CHECK FROM CIRCUIT BREAKER TO CONNECTOR ON ALL REPLACED WIRES, AND COMPLETED PARKING BRAKE OPERATIONAL CHECK IAW T/C F4M32603, ALTERNATE GEAR EXTENSION IAW T/C F1B32601, DC TIE RELAY CONTROL UNIT CHECK IAW T/C F1B24601, AND IRS BITE TEST IAW T/C A1B34610, ALL CHECKS WERE GOOD. 2L72 4F RTA2NM 20031112000812003111200081NM 2003 11 12 C1HA200394030 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK AT BS 480 - 580 RBL 45 HAS BARE METAL AND CORROSION. 2L73 4F A3WE 20040106002122004010600212NM 2004 1 6 SWAA032685 120031209A531065478509 WINDOW FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 CYXX - DURING SPECIAL VISIT CRACK INDICATION AT WINDOW 12 BS 530. REMOVED AND REPLACED WINDOW FRAME PER MM. (M) 2L72 4F RTA16WE 20040112001462004011200146WP 2004 1 12 ZIAA03005 120031103A57308005481 PANEL LKHEED188 188A 5262602WP WING CORRODED A K NONE O OTHER ININSP/MAINT 1 GL23346HA 188A1043 YIP - PLANK NR 3 JUST AFT OF 2-3 PLANK SEAM CORROSION BETWEEN RISERS AT BL61R, CENTER DRY BAY, LOWER SURFACE. REMOVED CORROSION AND TREATED AREA. REPAIRED PER LOCKHEED S/B 678 DWG 841795. (M) 2L74 4T RT4A22 20040112002272004011200227NM 2004 1 12 SWAA032801 120031222A53106547978 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED SPECIAL VISIT, FOUND CREASE BEAM CORRODED, BS 500 TO BS 500A, LT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20031120000082003112000008NM 2003 11 20 QXEA200301235 120031002A5310 CROSSBEAM DHAV DHC8 DHC8202 2809007NM ZONE 100 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FORWARD RIGHT HAND EMERGENCY EXIT UPPER FORWARD CROSSBEAM HAS STEP WEAR. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-52-349. 2H72 4T RTA13NM 20040113001192004011300119NM 2004 1 13 F3LA200300188 120031219A5753 FLAP TRACK BOEING737 73736N 1384408NM T/E FLAP CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NR 7 OTBD FLAP TRACK ASSY. REMOVED EXISTING BUSHINGS TO EXPOSE ALL SURFACES TO INSPECTION. INSPECTED FLAP TRACK PER OHM 57-53-15. MACHINED THE HOLE FORWARD OF BUSHING NR 60 PER SOPM 20-10-01 AND SOPM 20-10-02 TO REMOVE CORROSION. PERFORMED ALL POST MACHINING REQUIREMENTS PER SOPM 20-10-02. PERFORMED MAGNETIC PARTICLE INSPECTION OF TRACK PER SOPM 20-20-01. SHOT AND/OR FLAP PEENED THE REWORKED BORE PER SOPM 20-10-03. STYLUS CADMIUM PLATED THE BORE PER SOPM 20-42-10. REFINISHED PER OHN 57-53-15. 2L72 4F RTA16WE 20031216000472003121600047NM 2003 12 16 SWAA032533 120031117A5311963820 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SPECIAL VISIT, FOUND .75 LONG CRACK AT VERTICAL CHORD, BS 178, WL 184. REPAIRED VERTICAL CHORD PER SRM. 2L72 4F RTA16WE 20031217001322003121700132NM 2003 12 17 SWAA032714 120031211A53216546568 FLOOR PANEL BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB CRACKED AT BS 986.5 AND BS 1016, RBL 41. REPAIRED FLOORWEB PER SRM. 2L72 4F RTA16WE 20031229000772003122900077NM 2003 12 29 03FDEA02198 120031215A3260 POSITION SWITCH BOEING727 727100 1384036NM NLG DOOR INOPERATIVE A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25187FE 19079 NLG DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. COMPLIED WITH QRH PROCEDURE. LIGHT REMAINED ON. CONFIRMED PROBLEM. NLG DOOR LIGHT ON ALL THE TIME. TROUBLESHOOT USING 727WDM 32-62-01. FOUND LT NLG DOOR POSITION SWITCH INOP. REPLACED LT NLG POSTION SWITCH PER 727-100 MM 32-62-001-4. ADJUSTED AND OPS CHECKED PER 727-100 MM 32-62-001-5. OPS CHECK GOOD. 2L73 4F RTA3WE 20031229001802003122900180SO 2003 12 29 SWIA200312675 120031116A5410 BRACKET EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07227SW 120304 RT HYD LOWER PACK BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT HYD LOWER PACK BRACKET WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00. 2L72 4T RTA31SO 20031009000612003100900061EA 2003 10 9 03258662 120030915A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27662BR 7523 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A SECTION OF THE EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20040114002252004011400225EA 2004 1 14 03333665 120031129A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAULTY A VTZAO OTHER N FALSE WARNING UKUNKNOWN 1 EA27665BR 7534 DURING AIRCRAFT OPERATION, A LAVATORY SMOKE INDICATION WAS REPORTED BY THE FLIGHT CREW. THE SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040311000242004031100024NM 2004 3 11 ASAA0310121 120030307A7110 FRAME BOEING737 737298C 1384490NM NR 2 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 113 CHAFED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20031126001002003112600100SO 2003 11 26 C2XA03SH464 120031119A531514521713005 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031203001152003120300115EA 2003 12 3 A6WA200340159 120031107A2613 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU FALSE INDICATIONA A6WAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL31432AW P672 7257 ABORTED TAKEOFF AT 100 KNOTS DUE TO APU WARNING (HI-TEMP) TEMP 999 DEGREES FOLLOWED BY AMBER CAS MESSAGE APU OIL PRESSURE. NORMAL BRAKING APPLIED. INSPECTED APU, NO VISUAL SIGNS ON APU FIRE. INSPECTED TAILPIPE, NO EVIDENCE OF APU DAMAGE, COMPLIED WITH RTO INSPECTION IAW 05-51-27, NO DEFECTS MEL'D APU. (M) 2L72 4F RTA21EA 20040122000032004012200003NM 2004 1 22 03FDEA02300 120031226A5350AKC786840 BRACKET DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT TAILCONE UPPER DOOR FWD MOST TRIANGULAR VERTICAL BRACKET FOUND CHAFED. REMOVED DAMAGED BRACKET AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW STIFFENER AS PER DRAWING AKC 7868. INSTALLED NEW STIFFENER AT RT TAILCONE UPPER DOOR FWD MOST AS PER SRM 51-31-01 VOL. II. 2L73 4F4 FRTA22WE E13NE 20040123000502004012300050CE 2004 1 23 HYI2003F00021 120031105A272051152604 TORQUE TUBE CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO RUDDER PEDAL FAILED E HYIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NE01763EA 402C0497 ON TAKE OFF ROLL, RIGHT RUDDER PEDAL FAILED. MECHANIC FOUND RUDDER PEDAL TORQUE TUBE FAILED AT POST WELD. REMOVED AND REPLACED TORQUE TUBE AND RETURNED AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20031209001182003120900118WP 2003 12 9 DHL2003873015 120031030A323357155835501 CYLINDER DOUG DC8 DC873F 302199FWP LT MLG DOOR DAMAGED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01873SJ 46091 AFTER GEAR RETRACTION DEPARTURE DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, COULD NOT GET THE LIGHT TO GO OUT. DEFERRED PER MEL 32-16-2 DMI 14603 PLACARD INSTALLED CAT-A. REFERENCE DMI NR 14603 AFTER GEAR RETRACTION DOOR LATCHED LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL PROCEDURE COULD NOT GET THE LIGHT TO GO OUT. REMOVED AND REPLACED LEFT-HAND MAIN GEAR DOOR ACTUATING ASSEMBLY IAW DC8 M/M 32-32-7. THIS CLEARS DMI 14603. 2L74 4F RT4A25 20031208001512003120800151NM 2003 12 8 QXEA200301348 120031024A6120 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 FALSE ACTIVATIONA QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09358PH 506 AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED FUNCTION TEST OF POWER LEVER LIMIT SWITCHES, AUTO FEATHER ARMING INITIATES WITHIN TEST CHART OF DHC AMM 61-26-00, FIGURE 501. NO FAULTS FOUND. NO PARTS REPLACED, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031210000902003121000090EA 2003 12 10 COMA0360514 120031129A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01967CA 7134 FLIGHT 5148 PRIOR TO GRR APPROACH RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20031014000432003101400043NM 2003 10 14 QXEA200301145 120030916A5310 DOOR FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 RT AFT SERVICE DOOR APERTURE IS NICKED ON FORWARD SIDE 13.5 INCH DOWN FROM TOP. REPAIRED IAW Q400 SRM 51-14-00 AND 51-25-15. 2H72 4T RTA13NM 20030918000232003091800023NM 2003 9 18 GAIA03024SP 120030719A5313 STRINGER BOEING727 7272J0 138407ENM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND AT MAIN CABIN FORWARD STATION 720B, STRINGER 15L IS CRACKED. CUT OUT CRACK FROM STRINGER 15L, IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 4.7 INCH BY 3.2 INCH, TWO FILLRES .100 7075-T6 4.7 BY 8 IAW SRM 53-10-3 FIG 5, INSTALLED PARTS IAW SRM 51-10-3 FIG 5. (M) 2L73 4F RTA3WE 20030919001542003091900154EU 2003 9 19 AWXA200300934 120030805A5315D53472188204 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND AT AFT ENDS OF AFT CABIN FLOORBEAM Y1162, FR 68 TO FR 69. MAINTENANCE REMOVED FLOORBEAM FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 29-30. 2L72 4F RTA28NM 20030922000752003092200075NM 2003 9 22 AWXA200300952 120030805A5315D53112761200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y765 AT FR 16. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM Y765 AT FR 16; FABRICATED A NEW SECTION OF BEAM AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-15, PG. 208, 211-212, FIG. 202. 2L72 4F RTA28NM 20030923000582003092300058WP 2003 9 23 DHL2003604646 120030509A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT HORIZONTAL STAB INTERIM REPAIR ON INBD L/E XFS 178.750. PERFORMED MAJOR REPAIR IAW EODHL-030504, ED-3275. REMOVED FASTENERS, EXISTING INTERIM REPAIR AND FILLER IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030504, ED-3275. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) AND A FILLER (7075-T6 0.050) IAW EODHL-030504, ED-3275. CLEANED, TREATED AND PRIMED DOUBLER INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER AND FILLER ON RT HORZ STAB INBD L/E, STA XFS 178.750 USING NEW FASTENERS IAW EODHL-030504, ED-3275 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030124000882003012400088NM 2003 1 24 UPS03440059 120030103A5310 FITTING BOEING747 747259B 1384804NM RH BS 1480 B/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C RH BS 1480 B/H NO.17 HOLE CRACK AT OUTER CHORD SPLICE FITTING RUNNING O/B AND I/B APPROX 3/16" AND 0.040" RESPECTIVELY. REFER G ATTACH SKETCH FOR DETAILS. DEFECTIVE HOLE REWORKED AS PER RS 53-43-34957 ISSUE B AND EO B747-5310-18127-A. 2L74 4F RTA20WE 20030128000022003012800002SW 2003 1 28 ALGA084010 120030120A6320407040037101 GEAR SHAFT BELL 407 407 1182206SW TRANSMISSION SCORED H ALGAK NONE O OTHER ININSP/MAINT 1 FS01697AL2457 A388 53374 ON DISSASSEMBLY FOUND 30 BOLTS ON GEAR SHAFT LOOSE, MATING SURFACE FRETTED BEYOUND LIMITS IN CR&O MANUAL. THIS WAS THE FIRST TIME UNIT WAS DISSASSEMBLED SINCE NEW. REMOVED AND REPLACED GEAR SHAFT. 1G71 3U O H2SW 20030129001802003012900180NM 2003 1 29 UPS03240096 120030106A5310 BRACKET BOEING727 72722C 138400FNM BS 610 S28L/H CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI BODY FAIRING SUPPORT ANGLE BRAKCET CORRODED UNDER ANCHOR NUT AT BS 6 10 S28 L/H BRAKCET REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-1 FIG. 7 & SRM 53-50-1 FIG 1. INSTALLED IAW SRM 51-30-02 2L73 4F A3WE 20030203000222003020300022NM 2003 2 3 CA030113007 120030113A276185710558001 BRACKET DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LT SPOILER ACT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 35181 (CAN) DURING HEAVY MAINTENANCE CHECKS IN YHZ, THE LT, OUTBOARD SPOILER ACTUATOR BRACKET WAS FOUND CRACKED DURING FUNCTIONAL CHECKS. THIS BRACKET WAS REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030206001532003020600153WP 2003 2 6 ZW0A0301301 120030129A3350 CONNECTOR DOUG DC9 DC983 3022083WP CABIN LOOSE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13966TW 53616 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 26 TO 29. FOUND ELECTRICAL CONNECTOR AT ROW 29 WAS LOOSE. TIGHTENED CONNECTOR. 2L72 4F RTA6WE 20030214000172003021400017NM 2003 2 14 2003FA0000143 120030127A2910200496 HOUSING BOEING737 737* NM FLOW REGULATOR ERODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 FLOW REGULATOR ORIFICE IS ERODED. 2L72 4F RTA16WE 20030220000352003022000035NM 2003 2 20 03FDEA00131 120030214A5313 STRINGER BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 CORROSION ON STRINGER 27 RT, B/S 686 ** SD ** COMING. 2L73 4F RTA3WE 20030224000222003022400022EU 2003 2 24 BAQA084085 120030205A7714117902111 INDICATOR BOLKMSBK117 BK117C1 5626025EU TRIPLE TACH STICKING H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01117NC1549 7517 TRIPLE TACH NR NEEDLE STICKS. 1G72 3U NCH13EU 20030114002092003011400209NM 2003 1 14 VNAA0301004 120030105A5270 WARNING SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07461PS 3075 DURING FLIGHT, THE CREW RECEIVED A 9A EMERGENCY EXIT DOOR OPEN IN FLIGHT INDICATION BUT WAS VERIFIED TO BE CLOSED. UPON LANDING AT CVG, OUTSTATION INSPECTED, CLEANED, AND RESEATED THE DOOR THEN PRESSURIZED THE AIRCRAFT WITH THE CREW WHICH CHECKED GOOD. AFTER OPERATIONAL CHECKS WERE PERFORMED THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030116000372003011600037SW 2003 1 16 HEEA082996 120030106A7740DPUA0101 COMPUTER BELL 206 206L4 1182110SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0362127 52023 COMPUTER HAS FAULT LIGHT WIRE WAS SHORTED TO GROUND ON FACTORY HARNESS. 1G71 3U NCH2SW 20030121001822003012100182GL 2003 1 21 HEEA083330 220030109A732125490926 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03310778050 51520 N2 WOULD NOT STAY AT SET RPM. FOUND N1 RESET GUIDE AND ROD ASSY WORN. REPAIRED FUEL CONTROL. 1G71 3U3 U H2SW E1GL 20030225000762003022500076EA 2003 2 25 SWIA200311793 120030219A2711 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NA AILERON TRIM POPPED A SWIAC ABORTED TAKEOFF JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07437SW 7564 ABORTED TAKEOFF IN SJC FOR AILERON TRIM WARNING. AILERON TRIM CB POPPED, RESET CB. OPERATED SYSTEM THROUGH SEVERAL TIMES. AILERON TRIM OPS CHECK GOOD AT THIS TIME IAW CRJ MM 27-11-00. 2L72 4F4 FRTA21EA E15NE 20030324000042003032400004NM 2003 3 24 03FDEA00338 120030319A2611 WARNING SYSTEM BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE APU FALSE ACTIVATIONA FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25242FE 21178 DESCENDING THROUGH 10,000 FT, APU FIRE LIGHT CAME ON. PULLED FIRE HANDLE AND LIGHT WENT OUT. 2L73 4F4 FRTA3WE E2EA 20030307000392003030700039 2003 3 7 SWAA030454 420030227A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030307001622003030700162NE 2003 3 7 HEEA084906 120030228A32977655202010105 HARNESS SKRSKYS76 S76A 8143006NE EMERGENCY FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 SHEATH BROKEN FROM FLOAT INFLATION. SCRAPPED. 1G72 3U H1NE 20030311000192003031100019SW 2003 3 11 HEEA085040 120030228A3212206073848117 BOTTLE BELL 206 206L3 1182108SW EMERGENCY FLOAT CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671 51301 EMERGENCY FLOAT BOTTLE HAS CORROSION ON NECK AND VALVE. IN SHOP FOR REPAIR. 1G71 3U H2SW 20030122000332003012200033SW 2003 1 22 HEEA083420 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038587X412 51464 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000652003012200065 2003 1 22 HEEA083453 420030109A2300N0010001 CONTROL UNIT BELL 206 206L1 1182107SW COMMS SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032764F 45279 COMMS SYSTEM CONTROL UNIT WILL NOT POWER UP. 1G71 3U H2SW 20030318000162003031800016GL 2003 3 18 BAQA085088 220030304A7323252466715H GOVERNOR AEROSPAS355 AS355F 8680806EU ALLSN 250C 250C20 03013GL ENGINE INOPERATIVE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS019UC 310 5500 GOVERNOR WILL NOT GOVERN, INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H11EU E4CE 20030318001012003031800101EA 2003 3 18 COMA0360148 120030313A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01916CA2070710 7014 FLIGHT 5943 GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030321000632003032100063NM 2003 3 21 2003UALA00195 120030217A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29196UA 28715 DOOR 2R EMERGENCY EXIT BUSTLE LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2L74 4F4 FRTA20WE E24NE 20030321000672003032100067NM 2003 3 21 2003UALA00206 120030216A5754114W41508 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLAT NR 10 DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 DELAMINATED TRAILING EDGE WEDGE SKIN (SLAT NR 10). REPAIRED TRAILING EDGE WEDGE, SLAT NR 10. 2L72 4F4 FRTT0001SE E46NE 20030417000672003041700067NM 2003 4 17 UPS03240115 120030115A5320 WEB BOEING727 72722C 138400FNM LT STAIRWELL CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, LT STAIRWELL HORIZONTAL WEB IS CHAFED UNDERNEATH LT & RT AIRCON. FLOW CONTROL & SOV'S. REPAIR CARRIED OUT IAW SRM 51-40-02. 2L73 4F A3WE 20030422000452003042200045NE 2003 4 22 ASOA03111 220030315A7597MS2275941229 WIRE EMB 120 EMB120RT 3260202SO GE CT7TP CT79B 30030NE SENSOR LOOSE A ASOAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO11264AS 120165 FLT 4320 - DURING DESCENT INTO MCN FROM ATL, THE CREW RECEIVED A LT DUCT LEAK MESSAGE. THE CRE COMPLIED WITH QRH PROCEDURES AND SHUT DOWN THE LT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT LANDED SAFELY IN MCN. MAINTENANCE RE-ATTACHED A LOOSE SENSOR WIRE UNDER PANEL 191. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T4 TRTA31SO E8NE 20030422000692003042200069SO 2003 4 22 SIMA200305401 120030220A335066364 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21617AE 145093 XNA - FLT 3854 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTING AT EMERGENCY EXIT ROW WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED FLOOR PATH LIGHT STRIP NR 7 IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030801000732003080100073EU 2003 8 1 ASOA03289 120030611A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN BNA, THE LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 15/16 IAW ASA EO 72-53-0140. (M) 2H72 4T RT 20030806000542003080600054SO 2003 8 6 C2XA03SH223 120030717A33507287580505 LIGHT EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 DURING C-CHECK, THE NUMBER 5 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030422000742003042200074NM 2003 4 22 USAA030020 120030226A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19573US48509 23560 CLT - FOND SKIN CRACKED 2 INCHES, 2.5 INCHES AFT OF 727D 23R. INSTALLED DOUBLER PER TR 53-60-03. (M) 2L72 4F RTA16WE 20030723000122003072300012WP 2003 7 23 GTIA030496 120030611A5310 BEAM DOUG DC9 DC982 3022082WP CARGO DOORWAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - MID PIT INBOARD DOOR BEAM CORRODED. REMOVED DOOR BEAM. HOLES LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. (M) 2L72 4F A6WE 20030722001302003072200130NM 2003 7 22 AWXA200300656 120030523A53306545765 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 RT, BS 431. MAINTENANCE CUTOUT CRACKED SKIN AT STR 4 RT, BETWEEN BS 428 AND BS 432; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH DOUBLERS, 2 EACH FILLERS, 2 EACH INTERNAL DOUBLERS AND A TAPERED FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 PG 355 FIG 228. 2L72 4F RTA16WE 20030827000162003082700016NM 2003 8 27 03FDEA00954 120030623A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 N00461 SHEAR TIE CRACKED BS 560 ABOVE STR 18L. ** S/D ** COMING 2L73 4F RTA3WE 20030828000682003082800068NM 2003 8 28 DL757030619 120030707A3350S283T0143 POWER SUPPLY BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27660DL 24422 ON L/O CHECK FOUND EMERGENCY LIGHT ON SEAT 3B INOPERATIVE. REPLACED SEAT HARNESS AND POWER SUPPLY 2L72 4F RTA2NM 20030828001402003082800140EA 2003 8 28 ASOA03352 120030803A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 DURING A C-CHECK IN MCN, THE CARGO DOOR ENTRANCE SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR ENTRANCE SEAL PLATE IAW SRM 51-00. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030828001962003082800196NM 2003 8 28 CALA0300449 120030805A5330 SKIN BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712116 27558 INSPECTION FOUND AFT LOWER LT GTE AIRFONE ANTENNA MOUNT SKIN CORRODED AT STA 1500-1520, STRINGERS 28L TO 29L. THE SKIN WAS REPAIRED IAW ECRA 5330-03274. 2L72 4F RTA2NM 20030728000882003072800088NE 2003 7 28 SWAA031642 220030722A7230808931 BLADE BOEING737 7372H4 138448CNM PWA JT8 JT8D15 52051NE NR 2 ENGINE BENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 707419 ON POST FLT WALK AROUND NOTICED DEVIATION IN NR 2 ENGINE FAN BLADE. DEVIATION IS 1.25 LONG AND .375 OFF OF STRAIGHT AND LEVEL. REMOVED AND REPLACED C1 FAN ASSY PER MM. 2L72 4F4 F A16WE E2EA 20030728001382003072800138EU 2003 7 28 03FDEA01122 120030721A5311A5377263620801 FRAME AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25659FE 757 TEMPORARY REPAIR ON FRAME20A. PERMANENT REPAIR INSTALLED IAW EA 6-5310-60187 A AND DWG SR30-53-001. 2L72 4F4 FRTA35EU E13NE 20030729000242003072900024EA 2003 7 29 03195663 120030714A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27663BR 7527 DURING OVERNIGHT MAINTENANCE THE RT OVERWING EMERGENCY EXIT LIGHT WAS DISCOVERED INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED THE OVERWING EMERGENCY LAMP. A SATISFACTORY OPERTIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030729000562003072900056NM 2003 7 29 QXEA200300844 120030716A32607002537 CONTROL BOX DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE LANDING GEAR FAILED A QXEAO OTHER N FALSE WARNING DEDESCENT 1 NM09352PH* 7351 494 PUW- ON FLIGHT 2020 WHEN SELECTING GEAR DOWN, GOT NO LEFT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT. CYCLED GEAR HANDLE A SECOND TIME WITH SAME RESULTS. CONFIRMED GEAR DOWN INDICATION VIA ALTERNATE GEAR LIGHTS IN FLOOR. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ADVISORY LIGHT CONTROL BOX. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030729000672003072900067NM 2003 7 29 QXEA200300826 120030714A5320 FLANGE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - FORWARD FLANGE ON PANEL 262AT CHAFED. REPAIRED IAW RD 8/4-53-521. 2H72 4T4 TRTA13NM E00062EN 20030807001192003080700119 2003 8 7 BAQA087116 420030723A3442066311400 INDICATOR BOLKMS117 BK117A3 5626015EU WX RADAR SYS MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LC 7027 ERRONEOUS DISPLAY OF STORMS ON CLEAR DAY. RMA#: 49821 REPLACED WITH ANOTHER SERVICEABLE RENTAL UNIT WHILE OURS IS BEING REPAIRED. 1G72 3U H13EU 20030813000452003081300045NM 2003 8 13 2003UALA00459 120030602A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 MAIN CABIN FLOORBEAM AT BS 852-871 LBL 33 CORRODED. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR. 2L72 4F4 FRTA1NM E24NE 20030806001682003080600168NE 2003 8 6 AWXA200300869 220030802A75321777MK2 BLEED VALVE AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE NR 2 ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP28661AW18465679 1284 ON TAKEOFF AT PHX EN ROUTE FOR BOS OVER TEMP OCCURRED ON THE NR 2 ENG, REJECTED T/O AT 100 KTS. MAINT COMPLIED WITH STEP 4C OF AMM FORCE CK OF VSV MECH, FORCE REQUIRED LESS THAN 350 INCH POUNDS. R & R NR 2 ENG MASTER BLEED VALVE ACT, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL CHECK OF MASTER BLEED VALVE ACT, GOOD, BUT RIG TEST REVEALED PISTON VELOCITIES WERE OUT OF LIMITS. UNIT WAS DISASSEMBLED & INLET FILTER, TORQUE MOTOR FILTERS, & CONTROL SERVO VALVE PISTON FOUND LACQUERED TO LEVEL 2. UNIT CLEANED, TESTED AND RE-CERTIFIED IAW CMM. 2L72 4F4 FRTA28NM E311NE 20030904000552003090400055EA 2003 9 4 SWIA200312321 120030808A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 FS 280 LT FLOORBEAM ATTACH ANGLE LBL 9 IB AND OB CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R-31113-57 2L72 4F4 FRTA21EA E15NE 20030814001622003081400162NM 2003 8 14 AALA20030448 120030412A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21690AA 25696 DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHT AT 16D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000212003081500021SW 2003 8 15 HEEA088528 120030730A6320 BEARING BELL 206 206L3 1182108SW LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X LK8664 51412 LINK ASSY WORN BEARINGS. IN SHOP REPAIR. 1G71 3U H2SW 20031212000962003121200096NM 2003 12 12 SWAA032413 120031101A53106546555 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND 2 EA FUSELAGE FRAME SHEAR TIES CORRODED AT BS 847, RBL 3, WL 149, AND BS 767, RBL 7, WL 149. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20031215000882003121500088NM 2003 12 15 03FDEA01957 120031119A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB LEFT UPPER CENTER PLANK NR 26L BARREL NUT BORE FITTING FOUND CORROSION ON BEARING SIDEWALL SURFACES BEYOND EO 1-5510-7-5000 LIMITATIONS. NEW 26L FITTING FABRICATED AS PER DWG ALC8107 AND EA 1-5510-74245, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. DAMAGED 26L FITTING ON HOR STAB LT UPPER CENTRE PLANK 26L REMOVED & REPLACED AS PER SRM 51-33--01 VOL2. 2L73 4F RTA22WE 20040614002012004061400201CE 2004 6 14 GUU2004F00011 120030328A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO173853715833 UE158 AT SCHEDULED ROUTINE MAINTNANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20030925000332003092500033NM 2003 9 25 USAA030155 120030819A5343BACB30Y10K4X BEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 SW21340US 23237 FOUND BEAM CRACKED 2 INCHES, WEB OF NLG ACTUATOR ATTACH BEAM, STATION 235 NLG WHEEL WELL. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-10-14 AND BOEING DWG J65-45819. (M) 2L72 4F RTA16WE 20060801001372006080100137WP 2006 8 1 IXXA060580S 120030911A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "F" GOUGED FROM STATION 1390 TO STATION 1455. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0. 2L74 4F RT4A25 20030813000352003081300035SW 2003 8 13 HEEA088580 120030728A6230 BEARING BELL 412 412 1182202SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH A2208 33150 MAIN ROTOR LINK BEARINGS WORN. SHOP REPAIR. 1G72 4U H4SW 20030814000582003081400058WP 2003 8 14 0301369156 120030721A5330 SKIN DOUG DC9 DC914 3022034WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018915E 45832 DURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 LBL 18 TO LBL 19. REPAIRED PER EA 91-195861. 2L72 4F A6WE 20030818000942003081800094NE 2003 8 18 HEEA088433 220030718A75329550164960 BLEED VALVE AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1D1 NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE 2777 9728 BLEED VALVE CLOSING AT TOO HIGH AN INDICATED NG RPM. 1G72 3U3 U H11EU E19EU 20030820001142003082000114NM 2003 8 20 UPS03640991 120030719A335020131A BATTERY PACK BOEING767 76734AF 1385212NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01304UP 27242 EMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS WHEN SELECTED TO ON. REPLACED BATTERY, OPS GOOD. 2L72 4F RTA1NM 20030331000112003033100011EU 2003 3 31 03X03038751 120030310A27201379013E401 ARM BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RUDDER CRACKED A O3XAK NONE O OTHER ININSP/MAINT 1 SO03875AE19935400 875 DURING A SCHEDULED INSPECTION THE RUDDER QUADRANT DRIVE ASSEMBLY WAS FOUND CRACKED AT THE RUDDER FEEL SPRING ATTACH ARM. THE FEEL SPRING ATTACH ARM IS ATTACHED IN TWO SECTIONS TO THE RUDDER QUADRANT, ONE SECTION WAS CRACKED ALL THE WAY THROUGH. IF THE ATTACH FEEL CONTROL ARM CONTINUED TO CRACK THE REMAINING WAY THROUGH, THIS CONDITON COULD CAUSE LOSS OF YAW CONTROL. 2L72 4T4 TRTA56EU E4WE 20030402000232003040200023NM 2003 4 2 03091405 120030401A3350 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27405FJ 3155 DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY EXIT SIGN LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REPLACED LIGHTS IN THE EMERGENCY EXIT SIGNS, AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUTED SERVICE 2H72 4T RTA55NM 20030821001042003082100104NM 2003 8 21 03FDEA01184 120030731A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 NOSE WHEEL WELL GOUGE AROUND PANEL OPENING 3124, BS 237 LT. BLENDED GOUGE TO NEW SKIN AT BS 237. FOUND TO BE OUT OF LIMITS IAW 53-10-1. DAMAGE WILL BE REPAIRED ON CARD N00468. 2L73 4F RTA3WE 20030822000562003082200056NM 2003 8 22 03FDEA01170 120030726A5320A5A7114519 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 CTR CARGO RT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING FOUND CRACK. CTR CARGO RT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20030403000992003040300099NE 2003 4 3 DL72S030110 220030129A7200 WARNING LIGHT BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE ILLUMINATED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27523DA63607 21583 700319 NR 1 ENG OIL FILTER BYPASS LIGHT PER POM SHUT ENGINE DOWN. CLEANED CONNECTOR FOR MASTER DIM AND TEST MODULE AND PERFORMED ENGINE WINDMILL INSP PER M/M. 2L73 4F4 F A3WE E2EA 20030328000472003032800047SO 2003 3 28 C2XA03TY036 120030322A521014522460015 GUSSET EMB 145 EMB145ER 3260211SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 TYS DURING A SCHEDULED 3-C INSPECTION, CORROSION WAS FOUND ON THE TOP CAP INSIDE THE PAX DOOR. MAINT R & R THE GUSSET IAW EMB 135/145 SRM 51-40-02.ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030404000302003040400030NM 2003 4 4 DL73K030161 120030215A5730654549517 SKIN BOEING737 737232 1384475NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27307DL 23079 THE UPPER SKIN OF THE LT WING WAS FOUND WITH A 2.5 INCH CRACK AT WBL 170 RUNNING FWD FROM THE AFT EDGE OF THE SKIN NEAR THE REAR SPAR. THE CRACK WAS REMOVED WITH A 3 INCH BY 2 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH 2 ALUMINUM REPAIR DOUBLERS PER ER/A 384594-14, REV A. 2L72 4F RTA16WE 20030408000512003040800051WP 2003 4 8 WRLA200228 120030203A36109787344 VALVE DOUG DC10 DC1030 3023501WP PNEUMATIC SYS FAILED A WRLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA27352WL 47838 NR 1 PNEUMATIC TEMP HIGH LIGHT. PNEUMATIC TEMP EXCEEDED RED LINE. PNEUMATIC TEMP CONTINUED TO RISE TOWARD RED LINE. DUMPED 40,000 LBS OF FUEL TO REACH MAXIMUM LANDING WEIGHT. RETURNED TO DEPARTURE STATION FOR REPAIRS, NR 3 SYSTEM PNEUMATIC FAN AIR VALVE WAS ON DMI. REMOVED FAN AIR VALVE AND REPLACED PERFORMED ENGINE RUN TO CLIMB POWER FOR 25 MINUTES THREE TIMES. OPERATIONAL CHECK GOOD ON THE GROUND. REPLACED FAN AIR VALVE. (M) 2L73 4F A22WE 20030408000952003040800095NM 2003 4 8 2003UALA00314 120030303A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 AFT PIT BULK DOOR INTERIOR WEB DOUBLER ON LWR FRAME IS GOUGED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20030421002032003042100203NM 2003 4 21 AMTA200300244 120030221A3350 LIGHT BOEING737 73783N 13844HINM CABIN LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11318TZ 28247 FLOOR LIGHTING BY FORWARD ENTRY IS UNSECURE. SECURED FORWARD SECTION OF FLOOR LIGHTING, OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030424001212003042400121NM 2003 4 24 UPS03440344 120030306A5711 SPAR BOEING747 747200 1384847NM LT WING MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, LT WING MLGWW BS 1241 LBL 'O' PRESSURE BULKHEAD REAR SPAR ATT T-CHORD FOUND SURFACE CORROSION. T-CHORD REPLACED AS PER SRM 51-10-01 PG 8. (DEPTH 0.060 INCH, WIDTH 1 INCH, LENGTH 1 INCH). 2L74 4F RTA20WE 20030428000822003042800082CE 2003 4 28 GLBA2003043 120030404A3610 TUBE BEECH 1900 1900D 1154162CE LT WING DISCONNECTED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03257GL UE257 LEFT BLEED AIR FAIL ANNUC ILLUM. RECONNECTED EVA TUBING ON LEFT WING. 2L72 4T RTA24CE 20030429001802003042900180EU 2003 4 29 CA030407004 120030404A5250 SOLENOID BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU ROTOL R4304 R2124304 EU COCKPIT DOOR INOPERATIVE W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) ENROUTE CREW OBSERVED STRONG ELECTRICAL OVERHEAT ODOR ON FLIGHT DECK AND VISIBLE SMOKE. THE SECURITY DOOR LATCH ASSY WAS DETERMINED TO BE THE SOURCE. THE FLIGHT CONTINUED HOWEVER THE DOOR IS MECHANICAL LOCK ONLY WITH POWER REMOVED FROM THE CIRCUIT. 2L72 3T4 T A24EU A196 6 CP899 20030501000822003050100082WP 2003 5 1 GTIA030229 120030312A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND PASSENGER CABIN STATION 1003 TO STATION 1079 CENTER FLOOR PANEL HAS SOFT/MUSHEY, DETERIORATED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030505000712003050500071SO 2003 5 5 C2XA03SH113 120030422A531514530627001 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030505000412003050500041NM 2003 5 5 SWAA030836 120030410A253041610019 COFFEEMAKER BOEING737 7373H4 1384600NM AFT GALLEY OVERHEATED A SWAAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW29397SW 27691 DURING APPROACH, F/A SMELLED BURING ODOR IN AFT GALLEY. FOUND NR 1 COFFEEMAKER CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED NR 1 COFFEEMAKER PER MM. 2L72 4F RTA16WE 20030506001632003050600163WP 2003 5 6 ASAA0380221 120030307A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FRAME FLANGE HAS TOOL DAMAGE AT FASTENER HOLES. REPLACED DAMAGED FRAME PER SRM. (M) 2L72 4F A6WE 20030508000932003050800093NM 2003 5 8 2003UALA00407 120030501A5230 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CARGO DOOR PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29655UA 25393 FOUND 3/8 INCH HOLE IN BULK CARGO PIT DOOR 25 INCHES FROM TOP OF DOOR AND 1-3/4 INCHES FROM AFT SIDE OF DOOR. DOUBLER INSTALLED. 2L72 4F4 FRTA1NM E24NE 20030513001652003051300165EA 2003 5 13 QXEA0300468 120030413A5320 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 INTERCOSTAL IMMEDIATELY FORWARD OF REAR PRESSURE BULKHEAD CRACKED AT RIGHT HAND HYDRUALIC PRESSURE LINE FEED THROUGH. REPAIRED IAW HORIZON AIR EO R-29-07. 2L72 4F RTA21EA 20030514000172003051400017EU 2003 5 14 A6WA200360015 120030423A5754 SKIN BAC 146 146200A 1500266EU WING LE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 CRACKED IN HALF ABOVE PYLON NR 2 LEADING EDGE FIXED STRUCTURE. REMOVED AND REPLACED DOUBLER, P/N HC572H1080-001. 2 INCH CRACK TO NUTPLATE. PIECE INTACT, BUT CRACKED ALL THE WAY THROUGH. CAUSE OF DAMAGE, NORMAL FATIGUE. (M) 2H74 4F A49EU 20030604000052003060400005SO 2003 6 4 SIMA200311805 120030423A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 DURING AN IMBV INSPECTION, THE LT FLOORBEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED SECTION ON THE LEFT FLOORBEAM. CLEANED, AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-21-10 FIG 201, SHEET 1 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030609000412003060900041NM 2003 6 9 C1HA200396011 120030520A5347 SEAT TRACK BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 PITTING CORROSION AND GOUGING ON NR 4 SEAT TRACK AT RBL 44 BETWEEN BS 690 & 740 2L73 4F RTA3WE 20030613001062003061300106NM 2003 6 13 SWAA031247 120030605A3350AD20131A BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED PM CHECK, FOUND COCKPIT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030523000692003052300069NM 2003 5 23 SWAA031101 120030516A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030619000382003061900038SW 2003 6 19 HEEA087382 120030611A5320407070620312 PANEL BELL 407 407 1182206SW COCKPIT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030620000242003062000024SW 2003 6 20 HEEA086946 120030603A3212206050247137 COVER BELL 407 407 1182206SW FLOAT ASSY TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 FLOAT COVER ASSY TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030707000372003070700037NM 2003 7 7 AALA20030548 120030509A33501000679 LIGHT BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21307AA 22313 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BATTERY WILL NOT TAKE A CHARGE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030630000692003063000069EU 2003 6 30 ALGA087750 120030624A6220 PLATE UROCOPEC120 EC120B 8680987EU SCISSOR DRIVE WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03515AL91 MAP84 1165 MAIN ROTOR HEAD SCISSOR DRIVE ASSY FOUND TO HAVE A WEAR PLATE DEBONDED. REMOVED AND REPLACED. 1G72 3U NCR0001RD 20030708000082003070800008NM 2003 7 8 DL76L030602 120030701A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271200K 28457 FLIGHT ATTENDANT REPORTED A SLIGHT BURNING PLASTIC ODOR AROUND ROW 24 ON THE COPILOTS SIDE. IT WENT AWAY IN 2 MIN. NO OTHER INDICATIONS. INSPECTED ALL AREAS AND UNABLE TO DUPLICATE, INSPECTED ALL AREA AND UNABLE TO DUPLICATE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2L72 4F RTA1NM 20030702000222003070200022NM 2003 7 2 USAASB03077 120030610A335030043229 LIGHT BOEING737 737301 1384611NM ESCAPE SLIDE INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 MAINTENANCE FOUND THE MAIN ENTRY DOOR EXTERIOR ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERAITONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030710000362003071000036EU 2003 7 10 SIMA200314702 120030523A2910AE7064588 HOSE SAAB SF340 340B 7860101EU HYD SYS LEAKING A SIMAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21338SB 340B338 DURING CLIMB-OUT OF SBA, CREW RECEIVED A HYDRAULIC WARNING ON THE CWP. HYDRAULIC PUMP WAS SELECTED OFF DUE TO HYDRAULIC QUANTITY GOING DOWN. CREW DECLARED AN EMERGENCY AND CONTINUED TO LAX AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE FORWARD HYDRAULIC HOSE ON THE EXTENSION ACTUATOR LEAKING. BOTH FORWARD AND AFT HOSES WERE REPLACED IAW SAAB MM. OPERATIONAL AND LEAK CHECK WAS GOOD AND AIRCRAT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030710000682003071000068NM 2003 7 10 DHL2003750002 120030606A5610 WINDOW BOEING727 7272M7 138407SNM COCKPIT CRACKED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01750DH 21951 CAPTAINS L1 WINDOW CRACKED. REMOVED AND REPLACED CAPTAIN'S L-1 WINDOW IAW B727 M/M 56-11-11 AND B727 WDM 30-41-11. TESTED L-1 WINDOW HEAT SYSTEM IAW B727 M/M 30-41-01. OPS CHECKED NORMAL. 2L73 4F A3WE 20030717000142003071700014SW 2003 7 17 HEEA087991 120030702A5610407030115125A WINDSHIELD BELL 407 407 1182206SW COCKPIT MISMARKED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 WRONG IDENTIFICATION ON WINDOW--RT; IT IS LT. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 3U O H2SW 20030114000372003011400037NM 2003 1 14 SWAA030025 120030106A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 4 HINGE ATTACH POINTS PER MM. 2L72 4F RTA16WE 20030115001122003011500112EU 2003 1 15 BAQA082881 120030107A6410365A12002002 BLADE AEROSPSA365 SA365N 8680669EU TAIL ROTOR DAMAGED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM504 6396 TAIL ROTOR BLADE HAS EXCESSIVE PLAY IN SPOOL. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030116000902003011600090NE 2003 1 16 HEEA083048 220030107A732122007762 VALVE BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE FUEL CONTROL STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 FUEL CONTROL VALVE IS STUCK IN THE NORMAL MODE. 1G72 3U3 U H9SW E5NE 20030730000552003073000055NM 2003 7 30 P5CA0300888 120030613A29315048320 INDICATOR BOEING747 747249F 1384849NM HYD SYSTEM FAULTY A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23920FT 22237 NR 3 HYD SYS PRESSURE 2100 MAX. CONFIRMED INDICATOR AT FAULT, TRANSFERRED TO DMI 30942 (29-9). 2L74 4F A20WE 20030731000092003073100009NM 2003 7 31 QXEA200300908 120030719A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- RIGHT HAND OUTBOARD NR 11 SEAT TRACK HAS A GOUGE IN CENTER OF TRACK AT STATION X440.500. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-16, 51-20-36 AND RD 8-53-1342. 2H72 4T RTA13NM 20030911001662003091100166 2003 9 11 250TR0022 420030803A2210 GYRO BOEING737 7372K5 138448XNM 1 & 2 VERTICALS MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05250TR 22597 B CHANNEL AUTO PILOT JERKS EXCESSIVELY IN RIGHT AND LEFT TURNS. PLACED B CHANNEL AUTO PILOT ON MEL 22-1. 8/15/2003: REPLACED NR 1 AND 3 VERTICAL GYROS PER MM34-22-1. AUTO PILOT BITE TEST NORMAL PER MM22-11-01. 2L72 4F RTA16WE 20030826000062003082600006WP 2003 8 26 03FDEA01355 120030821A5753ARC1984 HINGE BRACKET DOUG DC10 DC1010 3022110WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 COMPLY WITH EA 8-5750-72256- WINGS- RIGHT OUTBOARD FLAP INBOARD HINGE ASSY-ARC 1984--PIVOT BORE REWORK ENT BY: 39014C RPT BY: 39010C FACT 21AUG03 15:11 BFM R COMPLIED WITH EA 8-5750-72256 ENT BY: 497191 RPT BY: 497191. 2L73 4F A22WE 20030826000202003082600020NM 2003 8 26 03FDEA01366 120030807A5744ARC0503503 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING OUTBOARD FLAP OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR HOLE FOUND CORROSION. LT WING OUTBD FLAP OUTBD HINGE BRACKET (WING SIDE) ACTUATOR HOLE REPAIR CARRIED AS PER FEDEX EA 1-5740-71796, WINGS- LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030826000242003082600024NM 2003 8 26 03FDEA01370 120030806A5744ARC0503504 HINGE BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE BRACKET (WING SIDE) BARREL HOLE FOUND CORROSION. RT WING OUTBD FLAP OUTBD HINGE BRACKET (WING SIDE) BARREL HOLE REPAIRED CARRIED OUT AS PER FEDEX EA 1-5740-71796, TITLE - WINGS - LT AND RT O/B FLAP - O/B HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030822001442003082200144NM 2003 8 22 C1HA200381019 120030806A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON SEAT TRACK LBL 45 BETWEEN FS 1010 AND 1110. 2L73 4F A3WE 20030910000982003091000098WP 2003 9 10 UPS03841016 120030731A5230 SEAL DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01868UP 45968 LOST PRESSURIZATION IN FLIGHT - CABIN ALTITUDE CLIMBED AT A RAPID RATE 2L74 4F RT4A25 20030910001692003091000169SO 2003 9 10 SIMA200321001 120030725A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142, REV 22, CHAPTERS 51-40-02, 51-40-06, 51-20-03. (M) 2L72 4F RTT00011AT 20030911000782003091100078WP 2003 9 11 DHL2003873516 120030617A5511 FRAME DOUG DC8 DC873F 302199FWP HORIZ STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT HORIZ STAB L/E INNER FORMER HAS 0.500 CRACK IN UPPER AND LOWER PART (XFS. 53.750). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED REINFORCING ANGLES IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLES IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030912001232003091200123NM 2003 9 12 AWXA200300890 120030728A53206935366 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .625 INCH CRACK WAS FOUND ON FLOOR SUPPORT UPPER WEB BS 540, LBL 24. MAINTENANCE REMOVED CRACKED WEB AT BS 540, LBL 24; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-01, PG 1. 2L72 4F RTA16WE 20030930000202003093000020NM 2003 9 30 03FDEA01453 120030906A5270 WARNING LIGHT BOEING727 727200 138407ENM AIRSTAIR DOOR ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25209FE 22931 DURING CLIMBOUT AT FL180, LIGHT CHOP, AFT AIRSTAIR AMBER LIGHT ILLUMINATED, AND REMAINED ON, COMPLIED WITH QRH. INSPECTED AFT AIRSTAIR WARNING INDICATION AND STAIR POSITION MICROSWITCHES IAW M/M 52-62-001-6-1, A (11). NO DEFECTS FOUND. FLIGHT CREW REPORTED NO PROBLEMS LAST 3 LEGS. CLEANED SWITCHES AND OPS CHECKED OK.. 2L73 4F RTA3WE 20031002000232003100200023 2003 10 2 GTIA030679 420030914A2565 SLIDE DOUG DC9 DC983 3022083WP CABIN DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 REAR L-2 SLIDE FELL OFF DOOR. RE-INSTALLED L-2 SLIDE ON DOOR. (M) 2L72 4F RTA6WE 20031007000422003100700042EA 2003 10 7 ASOA03402 120030816A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FIRST SEAT TRACKS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT FIRST SEAT TRACKS IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20031021000412003102100041 2003 10 21 GTIA030713 420030924A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 LGA - FLT 705 - SLIDE PACK FELL OFF L-1. FORWARD ENTRY DOOR SLIDE PACK FELL OFF WHEN OPENING DOOR AT ARRIVAL GATE. GIRT BAR LATCH ON THE FLOOR IS VERY DIRTY AND STICKY. REINSTALLED L1 DOOR SLIDE AND CHECKED GIRT BAR LATCHES FOR OPERATION, OPS NORMAL. (M) 2L72 4F A6WE 20031022000622003102200062NM 2003 10 22 QXEA200301163 120030917A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 TWO NICKS 2 INCHES APART OUTBOARD OF RIGHT STRINGER 32, 3 INCHES FORWARD OF X1.0 LOWER FUSELAGE EXTERIOR. REPAIRED IAW Q400 SRM 51-26-10, 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801 AND RD 8/4-53-505. 2H72 4T4 TRTA13NM E00062EN 20030123000782003012300078NM 2003 1 23 QXEA0300114 120030122A30804100S00501 VALVE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09404QX2778 2778 4046 SEA- DEICE PRESSURE CAUTION LIGHT ILLUMINATED, RAN CHECKLIST. PSI ON GUAGE HELD STEADY. REMOVED AND REPLACED LEFT OUTBOARD WING DUAL DISTRIBUTION VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030127002362003012700236SW 2003 1 27 HEEA083720 120030115A6730206076062105 SERVO BELL 407 407 1182206SW ROTOR SERVO LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03719PH2390 53266 ROTOR SERVO HAS A STATIC LEAK. 1G71 3U O H2SW 20030130000012003013000001NE 2003 1 30 ANCF200300001 220030112A7200 ENGINE BOEING767 767259 1385136NM PWA JT9 JT9D7R4D 52054NE LEFT STALLED W ANCFO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 SO23985AN 24618 LT ENGINE STALLED DURING DESCENT OUT AT 390 TO 380. ALL LT ENGINE PARAMETERS FLUCTUATED DURING STALL. CARRY OUT T/S IAW FIM 71-05-00. PAGE 105, WITHOUT FINDING DAMAGES OR FAULTS . CARRY OUT WATER TRAP IAW MM 73-21-04. PAGE 601 WITHOUT EVIDENCE OF WATER. TESTS WERE PERFORMED WITH SATISFACTORY RESULTS 2L72 4F4 FRTA1NM E3NE 20030131001042003013100104CE 2003 1 31 CA030107001 120030105A5520115610010125 SPLINE ADAPTER BEECH BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 17916 123A156B (CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS WERE FOUND CRACKED AT SEVERAL LOCATIONS, THIS IS THE 6TH SDR REGARDING THESE SPLINES AND A TOTAL OF 9 SPLINES FOUND CRACKED. THE ELEVATORS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. WE ARE CURRENTLY CONDUCTING A FLEET INSPECTION. 1L72 3T4 T A14CE E4EA 20030131001462003013100146SO 2003 1 31 C2XA03BT022 120030128A4900 APU EMB 145 EMB145LR 3260212SO TAILCONE ODOR A C2XAO OTHER O OTHER APAPPROACH 1 SW2729906 145472 EWR---CO2521, CREW REPORTED, "STRONG SMELL OF FUEL WHEN APU START IN FLIGHT". MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE APU IAW EMB145 AMM #49-10-00. NO FAULTS NOTED. VISUALLY INSPECTED APU IAW EMB145 AMM #49-02-00. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030206001502003020600150WP 2003 2 6 ZW0A0301201 120030128A2497 WIRE HARNESS DOUG DC9 DC982 3022082WP APU GENERATOR BURNED A ZW0AD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE13958U 49703 FLIGHT RETURNED FROM TAXI REPORTING AN ELECTRICAL ODOR. FOUND APU GENERATOR FEEDER CABLE WITH A TERMINAL BURNED AT S3-23. THE CABLE WAS TAPED, APU DEACTIVATED, AND AIRCRAFT OPERATED DIRECTLY TO A MAJOR BASE FOR REPLACEMENT OF THE CABLE. 2L72 4F A6WE 20030207001592003020700159EA 2003 2 7 COMA0360082 120030206A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO01798CA 7348 FLIGHT 5771 T/O ABORTED FOR SPOILER CAUTION MESSAGE.COULD NOT DUPLICATE. SPOILER OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA21EA 20030208000032003020800003GL 2003 2 8 RAIA00301020 220030121A7200AE3007A ENGINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FIRE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03804HK9877 145082 310130 5250-MSN-RIGHT ENGINE WILL NOT START. DURING MAINTENANCE THE ENGINE WAS DAMAGED BY FIRE, WAS REMOVED, AND REPLACED ENGINE. 2L72 4F4 FRTT00011ATTE6CH 20030213000332003021300033GL 2003 2 13 CA030130001 220030130A8500 ENGINE EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NACELLE FIRE W F ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 CA (CAN) TRANS STATE EMBRAER 145ER HAD ON GROUND ENGINE FIRE (NO PAX). AFTER DRY ROTOR, MECHANICS NOTED ENGINE FIRE. WHILE TROUBLESHOOTING THE ENGINE DUE TO INABILITY TO START. FUEL SPRAY NOZZLES HAD JUST BEEN CHANGED, FIRE BOTTLES DISCHARGED AND FIRE DEPT CALL TO EXTINGUISH. ENGINE CURRENTLY AT RRC TO DETERMINE CAUSE OF FIRE. 2L72 4F4 FRTT00011ATTE6CH 20030214000662003021400066WP 2003 2 14 ABXA030007 120030104A2497 WIRE DOUG DC9 DC932 3022066WP PWA JT8 JT8D NE FUSELAGE BURNED A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23983AX 47257 DURING MAINTENANCE, NOTED 3 WIRES CONNECTED TO APU FEEDERS BEHIND GENERATOR CONTROL RACK WERE BURNED. REPLACED WIRES FROM S30-12 BURNDY BLOCK TO STA. 160 LEFT IAW REA D924-46054. WAS MISWIRED AT S30-12 WAS INSTALLED IN TERMINAL 26 INSTEAD OF 25. OPS CHECKED GOOD. WIRED IAW DC-9 WD 24-21-03, EA 24300008, AND SB DC9-24A072. 2L72 4F4 F A6WE E2EA 20030217000082003021700008NM 2003 2 17 UPS03440176 120030206A5330 SKIN BOEING747 747200 1384847NM BS 1935-1945 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C DURING PATCH N522UP-46-08 BTN BS 1935-1945 STR 43L-45L REMOVED SHORT EDGE MARGIN FOUND BTN FASTENER & CUT OUT ABOUT 0.280" REPAIR AGAIN REQUIRED. FX - BS 1935-1945 STR 43L-45L SKIN REPAIRED AS PER SRM 53-30-03 FIG.1. 2L74 4F RTA20WE 20030218002322003021800232NM 2003 2 18 SWAA030262 120030203A53156545410 BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727A, RBL 43, WL 208. REPAIRED BEAM PER BFG ER. 2L72 4F RTA16WE 20030219001452003021900145NM 2003 2 19 USAA030009 120030115A5512 SKIN BOEING737 737401 1384701NM HORIZ STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US39486 23988 PIT - FOUND DURING MAINTENANCE, LOWER SKIN CRACKED 1.5 INCH, RIGHT HORIZ STAB LOWER SKIN AFT OF SPAR CHORD STATION 125. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TR 55-10-07. (M) 2L72 4F RTA16WE 20030220000632003022000063WP 2003 2 20 ABXA030064 120030206A3260 SOCKET DOUG DC9 DC941 302207NWP MLG INDICATOR WORN A ABXAO OTHER P NO WARNING INDICATION DEDESCENT 1 GL23979AX 47492 ON GEAR EXTENSION INTO PIE, GEAR DOOR OPEN LIGHT NEVER ILLUMINATED. BULB CHECKED GOOD. GEAR RECYCLED. ON NEXT EXTENSION IT DID NOT COME ON BUT ONLY FOR 1 SECOND, NOT THE NORMAL 30 SECONDS. VERIFIED, FOUND GEAR DOOR OPEN LAMP WORN WHICH CAUSED AN INTERMITTENT PROBLEM. OPS CHECKED GOOD IAW DC-9 AMM 32-60-00-0. 2L72 4F A6WE 20030221000282003022100028NM 2003 2 21 QXEA0300136 120030111A5420 SUPPORT BOMBDRDHC8 DHC8401 1390041NM NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- SUPPORT FLANGE FOR PANELS 262HT, 262FT AND 262AT FORWARD EDGES ARE CHAFED. REPAIRED IAW DHC-8 400 SRM 51-21-10 AND HORIZON AIR EA 6-53-174. 2H72 4T RTA13NM 20030224001212003022400121EA 2003 2 24 COMA0360113 120030222A28427686571 CAPACITOR CNDAIRCL600 CL6002B19 1900309EA #6 MALFUNCTIONED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01709CA 7238 FLIGHT 5022 FUEL QUANTITY INDICATION IS ERRATIC.REPLACED THE #6 FUEL QUANTITY PROBE. 2L72 4F RTA21EA 20030225000472003022500047SW 2003 2 25 HEEA084267 120030129A5522 SKIN BELL 214 214ST 1182106SW ELEVATOR ERODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806803 A200 28140 EROSION OF SKIN UNDER PAINT. SOMETHING MUST HAVE BEEN SPLASHED ON IT BEFORE PRIMED AT BELL CAUSING EROSION. THE ERODED AREA IS 18 X 20 INCHES. BLASTED PAINT TO BE ABLE TO EVALUATE THE ELEVATOR. 2G72 4U H10SW 20030226000172003022600017NM 2003 2 26 0300295642 120030224A4990 HONEYWELL BOEING757 757251 1384970NM A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01542US 26489 During climb three lavatory smoke alarms sounded. Flight attendants reported strong electrical smell. Flight crew returned aircraft to departure airport. Maintenance found oil dripping from the left pack outlet duct. Oil in the packs is residual from APU removed previous day. Maintenance replaced numerous oil contaminated pac/air conditioning components and performed pack burnout procedure. 2L72 4F RTA2NM 20030306000342003030600034SW 2003 3 6 HEEA084747 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 RT PASSENGER STEP WILL NOT EXTEND. REPAIRED ACTUATOR. 1G72 4U H4SW 20030307001672003030700167NM 2003 3 7 AWXA200300230 120030305A3350606171 SOCKET BOEING737 7373G7 1384595NM SEAT ROW 8 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW0 0 23779 DFW - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED DAMAGED LIGHT SOCKET ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030310000932003031000093 2003 3 10 HEEA084998 420030227A34578143902240B GPS BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 GPS UNABLE TO ACQUIRE DATA. CLEANED DATA CARD READER CONTACTS. REPAIRED. 1G72 4U H4SW 20030117001602003011700160SW 2003 1 17 HEEA083214 120030108A6710206062721113 ACTUATOR BELL 206 206B3 1181506SW MAIN ROTOR STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 ACTUATOR KEEPS STICKING. 1G71 3U H2SW 20030317000402003031700040NM 2003 3 17 03FDEA00175 120030225A5311 FRAME BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE CARGO BAY LWR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION FORWARD CARGO BAY ON LOWER FRAME AT STA 660, STR 28L TO 28R. 2L73 4F4 F A3WE E2EA 20030319000672003031900067NM 2003 3 19 KPVA20037 120030218A3350 BATTERY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT DISCHARGED A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13807WP1860 023 HNL - EMERGENCY LIGHT POWER SUPPLY BATTERY LOW LOCATED AT STATION PS3. REMOVED AND REPLACED AFFECTED POWER SUPPLY. OPERATIONAL CHECK OF SYSTEM GOOD. WORK IAW DHC-8 MM 33-51-00, PAGES 201-202. (M) 2H72 4T RTA13NM 20030123000202003012300020NM 2003 1 23 2003UALA00036 120030108A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 CABIN FRAME STATION 400 FRAME WEB CRACKED AT FASTENER HOLE JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030327000542003032700054NM 2003 3 27 C1HA200382003 120030221A2612 FIRE LOOP BOEING727 7272S7 138407ZNM NR 2 ENGINE SHORTED A C1HAO OTHER J WARNING INDICATION CRCRUISE 1 GL15682CA 22019 NR 1 ENGINE FIRE WARNING GROUND FAULT DECTOR LIGHT ILLUMINATED DURING FLIGHT. PERFORMED FIRE WARNING TEST PROCEDURES COM 2.26.3 TESTED NORMAL REPOSITIONED FIRE LOOP GROUND TESTS NORMAL. PER MM 26-11-01 2L73 4F A3WE 20030321000572003032100057EA 2003 3 21 COMA0360157 120030318A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO01920CA 7022 FLIGHT 5873 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030728001312003072800131WP 2003 7 28 AMTA200300864 120030701A5321 FLOOR PANEL LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND C1 CARGO PIT CRACK IN FLOOR PANEL AT FS 679 DAMAGE IS 7 INCHES RT OF CENTER LINE 1.5 INCHES LONG. PERFORMED INTERIM REPAIR PER ERA L10-53T-2549 REV B. 2L73 4F A23WE 20030801000532003080100053WP 2003 8 1 GTIA030515 120030623A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FORWARD CABIN STATION 160 TO STATION 200 LBL 54 INCHES CORRODED AT THE FLOOR SUPPORT. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030731000262003073100026NM 2003 7 31 QXEA200300915 120030728A33506138001 BATTERY PACK BOMBDRDHC8 DHC8401 1390041NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09409QX3411 1503 4051 SEA- AFT EMERGENCY EXIT SIGN WILL NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TURNED ON. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030303001932003030300193WP 2003 3 3 DHL2003804538 120030128A5712 DOUBLER DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF. N/R: 1473 - LH WING CTR. L/E INNER DOUBLER UPPER PART WITH4.000 CRACK IN IT (STA XFS416.5000-429.000)CORR: REMOVED FASTNERS IAW SRM 51-1-21- PG. 1 REMOVED INNER DOUBLER IAW SRM51-1-21-PG 1 FABRICATED NEW INNER DOUBLER ( 7075T6AL.080) IAW SRM57-2-0 FIG 2 , CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B , INSTALLED NEW INNER DOUBLER AND FASTNERS IAW 51-1-21 PG. 1 2L74 4F RT4A25 20030325000172003032500017NM 2003 3 25 AWXA200300127 120030127A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK 2 EACH CRACKS A 4" AND 2" WERE FOUND ON CHORD AND WEB OF CABIN CENTER SECTION FLOOR BEAM AT BS 663, BL "0". MAINTENANCE CUTOUT DAMAGE ON FLOORBEAM BS 663 BL "0"; FABRICATED 2 EACH FILLERS, STRAPS, SPLICE ANGLES, AND SPLICE PLATES, 1 EACH WEB AND ANGLE EXTRUSION; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5702-03038-TB2. 2L72 4F4 FRTA16WE E2GL 20040325000782004032500078SW 2004 3 25 AC2A093328 120030726A6240430340002101 CHIP DETECTOR BELL 430 430 1182150SW TRANSMISSION SHORTED E AC2AO OTHER N FALSE WARNING NRNOT REPORTED 1 SO07430CM 49090 CHIP DETECTOR CIRCUIT-SHORTED. DETECTOR CAUSES PLANETARY LIGHT TO STAY ILLUMINATED. REPLACED PART. 1G72 3U RTH9SW 20030417000452003041700045EA 2003 4 17 SWIA200311739 120030114A5270 SWITCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR STICKING A SWIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM07413SW 7102 CREW REPORTED PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE AT 25,000 FT. LUBRICATED AND CLEANED OUTER HANDLE SWITCH. OPERATIONAL CHECK IS OK. 2L72 4F RTA21EA 20030717000282003071700028SW 2003 7 17 HEEA088005 120030627A6330KWDB623 BEARING BELL 407 407 1182206SW SPRING ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH3912 LK1562 53400 MAIN ROTOR SPRING ASSY HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000512003071700051 2003 7 17 HEEA088027 420030627A34570110050400 GPS BELL 206 206L4 1182110SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F 52038 GPS NOT DISPLAYING AIR TRAFFIC. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U NCH2SW 20030722000382003072200038NM 2003 7 22 2003F00466 120030124A5320 SUPPORT ANGLE BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CRACK ON SUPPORT ANGLE, FUSELAGE BODY FAIRING, STATION 720, STRINGER 29L. REPAIRED SUPPORT ANGLE BELOW FUSELAGE BODY FAIRING AT INBOARD END, STATION 720 STRINGER 29L. (M) 2L73 4F A3WE 20030722001352003072200135NM 2003 7 22 SWAA031472 120030705A2781655280773 MODULE BOEING737 7373L9 1384470NM LE FLAP/SLAT FAULTY A SWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW29657SW 23331 ABORTED TAKEOFF, WARNING HORN SOUNDED ASSOCIATED WITH L/E INDICATOR LIGHTS. REMOVED AND REPLACED L/E FLAP/SLAT POSITION IND MODULE PER MM. 2L72 4F RTA16WE 20030424000012003042400001NE 2003 4 24 P5CA0300782 220030316A7421CH31843 IGNITER BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 4 ENGINE DEFECTIVE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23505MC 21251 517529 RETURN TO BLOCKS DUE TO NR 4 ENG FAILED TO START. REPLACED BOTH IGNITER PLUGS TESTED OK. DEFECTED IGNITER PLUG NR 2 POS NR 1 SYS PREV DEFERRED. 2L74 4F4 FRTA20WE E23EA 20030827000462003082700046SW 2003 8 27 ALG2003F00063 120030503A78104606AC CLAMP BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL ENGINE BROKEN A ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW03167H 2968 CAE831002 DURING LANDING THE PILOT SMELLED A DISTINCT ODOR, UPON LANDING FOUND ONE OF THE EXHAUST STACKS ON THE SIDE OF THE ENGINE COWLING. THE MECHANIC REMOVED AND REPLACED THE BROKEN CLAMP AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 20030828000362003082800036WP 2003 8 28 PNSA030601 220030615A7320 LIMITER SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE FAULTY A PNSAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL0341NE AC741B P44691 DURING TAKEOFF ROLL RT ENGINE AUTOMATIC TEMP LIMITER SYSTEM CAME ON BYPASSING FUEL WITH AN ASSOCIATED DROP IN TORQUE. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PROBLEM, DEFERRED TEMP LIMITER SYSTEM PER MEL AND SECURED CIRCUIT BREAKER FOR SYSTEM. AIRCRAFT WAS DISPATCHED PER MEL WITH NO OTHER PROBLEMS NOTED. MAINTENANCE HAS SCHEDULED AIRCRAFT FOR FURTHER TROUBLESHOOTING, SINCE THIS SYSTEM HAS FAILED INTERMITTANTLY IN THE LAST TWO WEEKS. 2L72 4T4 TRTA8SW E4WE 20030902000532003090200053EA 2003 9 2 I8P2003F00000 220030107A8520LW13212 ROD BEARING MOONEYM20 M20J 5870219SW LYC O360 IO360A3B6 41514EA ENGINE DELAMINATED E I8PAO OTHER O OTHER NRNOT REPORTED 1 WP07201DD641 240102 DURING ROUTINE OIL CHANGE METAL FOUND IN OIL FILTER. METAL FOUND TO BE BEARING MATERIAL COMING FROM CONNECTING ROD BEARING PREMATURE FAILURE. BEARING MATERIAL IS DELAMINATING. CONNECTING ROD BEARING MANUFACTURE DATES ARE (ML-KS 2-9A AND 3-99) MANUFACTURING DEFECT/PROBLEM KNOWN TO MFG. CRANKSHAFT GRIND REQUIRED TO CORRECT JOURNAL HEAT DEFECTS. (WPO1200303672) 1L71 3O3 O 2A3 1E10 20030725000142003072500014NE 2003 7 25 DL757030588 220030626A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 SHUTDOWN A DALAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO276702 9523 30188 728761 AT FLT LVL 370, PILOT HAD THE RT ENG OIL PRESSURE BOXED IN RED, ENGINE WAS SHUTTING ITSELF DOWN. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20030725000292003072500029EU 2003 7 25 RAIA00305142 120030514A3150 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03567HK 41085 RECEIVED TAKEOFF CONFIGURATION WARNING ON TAKEOFF. MAINTENANCE OPERATIONAL CHECKED TAKEOFF CONFIGURATION WARNING WITH NO DEFECTS NOTED. 2L72 4T RTA41NM 20030801000252003080100025WP 2003 8 1 GTIA030537 120030628A5320 CLIP DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND FORWARD PIT STRINGER 21L INTERCOSTAL CLIP CRACKED AT FS 237. REMOVED INNER COSTAL CLIP. FABRICATED NEW CLIP. INSTALLED INNER COSTAL CLIP. (M) 2L72 4F A6WE 20030903001262003090300126NE 2003 9 3 UIEA200300033 220030711A73218062899 MEC BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 1 ENGINE MALFUNCTIONED A UIEAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA15509MC 21221 RMS/FRU - REJECTED TAKEOFF, ON TAKEOFF ROLL, NR 1 ENGINE WOULD PRODUCE ONLY 108.0 N1 WITH FIREWALL THRUST. 113.0 N1 WAS THE DESIRED POWER SETTING. ABORTED TAKEOFF AT 80 KTS, NR 1 N1 APPEARED TO SPIN UP SLOWER THAN THE REST. ALL OTHER ENGINES APPEARED NORMAL. REMOVED AND REPLACED NR 1 ENGINE MEC PER MM 73-21-01. OP AND LEAK CHECKS OK. OK FOR SERVICE. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER MM 73-11-01. OPS AND LEAK CHECKS OK. OK FOR SERVICE. FUEL PUMP P/N 9039M45P14. (M) 2L74 4F4 F A20WE E23EA 20030904000242003090400024SO 2003 9 4 C2XA03IA090 120030902A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712567 145623 DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY FLOOR LIGHTS FAILED TO ILLUMINATE DURING TEST. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030904001912003090400191WP 2003 9 4 AALA20030722 120030704A3397 WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21505AA 49799 DFW - EXIT IDENTIFIER BETWEEN 1ST CLASS AND FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EXIT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905000062003090500006SO 2003 9 5 LR7A03053 120030725A5320 DOUBLER LKHEED382 382G 526414USO FUSELAGE DEFORMED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND RMLG WHEEL WELL FS 598-610 CHINE ANGLE REPAIR DOUBLER DEFORMED AND BUCKLED AT RBL 61, WL 143. REPAIRED CHINE ANGLE AND REPLACED DOUBLER IAW SRM SMP 583 53-40-27. NR 2016. 2H74 4T A1SO 20030905000452003090500045SO 2003 9 5 C2XA03BT077 120030805A2611FAU751A4 PANEL EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAO OTHER N FALSE WARNING CRCRUISE 1 SW2713990 145277 EWR CO2879, CREW REPORTED, LAV SMOKE WARNING DURING FLIGHT WITH ASSOCIATED SMOKE ALARM. PERFORMED QRH. NO VISIBLE SIGN OF SMOKE OR FIRE. FLIGHT CONTINUED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTION PANEL IN GALLEY IAW EMB145 AMM 26-14-02. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030812000072003081200007NE 2003 8 12 HEEA088407 120030710A52107620710009062 HANDLE SKRSKYS76 S76C 8143008NE CREW DOOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 EXTERIOR DOOR HANDLE BROKEN. TO BE SENT TO VENDOR. 1G72 3U NCH1NE 20030822000782003082200078EU 2003 8 22 03FDEA01079 120030709A5330 SKIN AIRBUS300 A300B4605R 3930308EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 GOUGE IN SKIN APPROX 0.020 DEEP AFT OF TOILET SERVICE DOOR CUTOUT (L=.875 X W=.125) BETWEEN LT FR12 & LT FR12A. CUT OUT GOUGED AREA AND REPAIRED SKIN WITH FILLER AND 3 X 7 INCH DOUBLER IAW AIRBUS A300-600 SRM 53-12-12 FIG 202. 2L72 4F RTA35EU 20030825001122003082500112EA 2003 8 25 03231702 120030819A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27702BR 7462 DURING MAINTENANCE INSPECTION THE NR 3 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030826000872003082600087 2003 8 26 YENA200310 420030615A23303042865102 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15550JB 1891 ACAR REPORT A BURNING SMELL MID CABIN. TURNED LTV OFF; F/A REPORTS SMELL DISAPPEARED. AT JFK LTV TROUBLESHOT, UNABLE TO FAULT. AS PRECAUTIONARY, REPLACED SEB AT SEAT 8 ABC. LTV OPS GOOD. 2L72 4F RTA28NM 20030729001002003072900100EU 2003 7 29 2003F00480 120030516A5350 FAIRING AIRBUS320 A320233 3930329EU FUSELAGE DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND RIGHT BELLY FAIRING 197GB, DELAMINATED. REPAIRED BELLY FAIRING 197GB IAW SRM S3-4S-12, PAGE 220 FIG 205. (M) 2L72 4F RTA28NM 20030930000132003093000013NM 2003 9 30 QXEA200301066 120030903A2810 CHECK VALVE DHAV DHC8 DHC8202 2809007NM ZONE 400 LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09374PH 528 ON FLIGHT 2058 ONE DRIP PER SECOND COMING FROM SPR AREA. FUEL MADE 12 INCH PUDDLE IN 10 MINUTES TIME. FOUND CHECK VALVE OFF CENTER ON SPR. REPOSITIONED CHECK VALVE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030926000082003092600008NM 2003 9 26 QXEA200301027 120030820A5730 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 500 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 SEVEN INCH SCRATCH ON TOP SIDE OF LEFT HAND WING 6 INCHES AFT OF FORWARD SPAR STATION YW207. REPAIRED IAW DHC-8 SRM 51-20-11, 51-00-06, 51-00-02 AND 51-00-04. 2H72 4T RTA13NM 20030909002132003090900213EU 2003 9 9 BAQA088357 120030807A771456337118010 INDICATOR AEROSPAS365 AS365N2 8680815EU NG INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME435 6417 NG INDICATOR INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030909001632003090900163SW 2003 9 9 HEEA088907 120030829A2841412375001105 INDICATOR CLARK 1000 1000CLARK 2230102SW FUEL QTY READS LOW B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO RT FUEL INDICATOR READING 100 POUNDS LOW. 1Q71 3R 2A6 20030909002822003090900282NM 2003 9 9 QXEA200300951 120030805A2910 B-NUT DHAV DHC8 DHC8202 2809007NM HYD SYSTEM LOOSE A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09345PH 476 PDX- ON TAXI NR 2 HYRDAULIC SYSTEM DEPLETED TO ZERO QUANTITY. FOUND HYDRAULIC UNIT TO PTU LEAKING AT B-NUT. RETIGHTENED AND GROUND RAN ENGINES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031003000262003100300026EU 2003 10 3 AALA20030974 120030908A3350P4010049 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211455K 11467 FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROWS 4 AND 5. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031007000572003100700057NM 2003 10 7 03FDEA01616 120030924A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION BS 950F FLOORBEAM LWR CHORD NUTPLATE HOLES LBL 45 - RBL 45 WL 200. REPAIRED IAW SRM 53-10-8 2L73 4F4 FRTA3WE E2EA 20031015000142003101500014EU 2003 10 15 USAA030181 120030902A5210 SKIN AIRBUSA319 A319112 3930323EU DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19742US 1275 FOUND SKIN AND SEAL RETAINER WITH 1 INCH CRACK WITH DENT AND 5 INCH CRACK ONSEAL RETAINER, AFT LOWER CORNER OF MED L-1 EXT DOOR SKIN. SECTION OF DOOR SEAL RETAINER REPLACED AND SKIN DOUBLER INSTALLED PER SRM 52-10-00. (M) 2L72 4F RTA28NM 20031021000632003102100063NM 2003 10 21 HALA0300787 120030921A28225006003C HOUSING BOEING767 76733A 1385209NM BOOST PUMP DAMAGED A HALAK NONE O OTHER ININSP/MAINT 1 WP13583HA 25531 PAE - LEFT WING MAIN TANK BOOST PUMP HOUSING HAS ARCING DAMAGE. REPAIR IN WORK. (M) 2L72 4F RTA1NM 20031022000362003102200036 2003 10 22 P5CA0300945 420030922A344220704090101 ANTENNA BOEING747 747200 1384847NM NR 1 & 2 RADAR DEFECTIVE A P5CAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 WP23524UP 21446 NR 1 AND NR 2 RADAR SYS. WILL NOT PAINT WEATHER ENROUTE. TESTS OK. REMOVED AND REPLACED RADAR CONTROL PANEL AND RADAR ANTENNA IAW MM 34-43-03. OPS CHECK NORMAL. 2L74 4F RTA20WE 20031022001112003102200111EA 2003 10 22 COMA0360419 120030912A3610 CLAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE 14TH STAGE DUCT OUT OF POSITION A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01914CA 7012 FLIGHT 9488 LEFT 14TH STAGE DUCT MESSAGE DURING T/O. REPOSITIONED 14TH STAGE SOV CLAMP. 2L72 4F4 FRTA21EA E15NE 20031022001442003102200144EA 2003 10 22 SWIA200312429 120030922A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ESCAPE HATCH CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. DISCOVERED DURING C-CHECK INSPECTION. CREW ESCAPE HATCH OUTER HANDLE REPLACED, REF. CMM 52-22-03. PN: H3419-33 2L72 4F4 FRTA21EA E15NE 20031027001392003102700139NM 2003 10 27 03FDEA01634 120030902A5753ARC2518501 STRAP DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING INBOARD FLAP OUTBOARD HINGE PIVOT LUG FACE (FLAP SIDE) FOUND CORRODED. LT WING I/B FLAP O/B HINGE PIVOT (O/B LUG O/B FACE) STRAP P/N ARC2518-501. REMOVED AND REPLACED WITH NEW STRAP IAW EA 1-5750-72646, TITLE : WINGS - TRAILING EDGE DEVICES - LT INBOARD FLAP OUTBOARD AFT HINGE PIVOT BORE CORROSION AND EA EA 1-5750-72650 2L73 4F RTA22WE 20031029001012003102900101EU 2003 10 29 YENA200326 120030927A4997 CONNECTOR AIRBUS320 A320232 3930326EU RAM AIR TURBINE DAMAGED A YENAK NONE O OTHER ININSP/MAINT 1 EA15553JB 1896 RAM AIR TURBINE AUTO-DEPLOY OPERATIONAL CHECK FAILED IAW JB WORK CARD 292000-05-1. FOUND PIN 7 ON 2224VC PUSHED IN, PULLED AND RECONNECTED. OPS CHECK GOOD. REFERENCE AIRCRFT WIRING MM 24-24-04 PAGE 1. 2L72 4F RTA28NM 20031029000572003102900057NM 2003 10 29 ASAA0240218 120030401A532014963777075T6 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND SIDE WALL FLOOR CHANNEL CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000942003102900094NE 2003 10 29 KBM2003F00009 220030711A75329550164960 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 BLEED VALVE FLAG SHOWING, SUSPECTED BLEED VALVE WILL NOT CLOSE. REMOVED AND REPLACED WITH SERVICEABLE BLEED VALVE.(K) 1G71 3U3 U H9EU E19EU 20031120000102003112000010EU 2003 11 20 AWXA200301219 120031013A3397E0052R8B3APNE CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 15 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CANNON PLUG AT BULKHEAD SEAT ROW 15 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040129001442004012900144NM 2004 1 29 MWEA040005 120031219A53209936534177 STRUCTURE DOUG MD88 MD88 3023688NM SUB FLOOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 SUBFLOOR IS CORRODED APPROXIMATELY FUSELAGE STATION 180 LEFT SIDE NEAR PASSENGER DOOR PAN. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F RTA6WE 20040204000822004020400082NM 2004 2 4 AWXA200301273 120031002A5320654585546 ANGLE BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR CREASE BEAM LOWER SUPPORT ANGLE BS 964, RBL 48. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SUPPORT ANGLE BS 964, RBL 48; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1, FIG. 3 AND 4. 2L72 4F4 FRTA16WE E2GL 20040212000582004021200058EU 2004 2 12 KBM2003F00100 120031105A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR TORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH1235 3141 TAIL ROTOR HUB HINGE LAMINATED BEARING TORN AND RIPPED. REPLAED WITH NEW BEARINGS. 1G71 3U3 U H9EU E19EU 20031103001202003110300120EU 2003 11 3 AWXA200301117 120030926A5720D574435584000 ANGLE AIRBUS320 A320232 3930326EU LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK THE LEFT WING LEADING EDGE SUB SPAR TO RIB ANLE WAS FOUND CRACKED NEAR NR 3 UPSTOP PAD AT LT RIB 15 STA. 8268 . MAINTENANCE REMOVED,FORMED,AND INTALLED LEFT WING LEADING EDGE SUB SPAR TO RIB ANGLE IAW A320 SRM 51-42-11 PAGES 22 FIG 8, A27, FIG 62. ADDITIONAL REFERENCES FOR COMPLETION INCLUDE 51-26-11 FIG 1-5 PAGS 1-13 AND 51-41-11 PAGS 8-12 FIG 2 AND 3 PG A24 PROCEDURE D. UTILIZING AIRBUS DRAWING NR D57443558 AND AWA E.R. 26-5128-02218-SS1 REPAIR WAS ACCOMPLISHED AS REQUIRED. 2L72 4F RTA28NM 20031105000932003110500093NM 2003 11 5 QXEA200301371 120031022A5720 STIFFENER DHAV DHC8 DHC8202 2809007NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX- PANEL 524AT HAS CHAFED STIFFENER, SECOND STIFFENER FROM OUTBOARD END FORWARD SIDE OF LEFT HAND WING. REPAIRED IAW DHC-8 RD 8-57-1568. 2H72 4T RTA13NM 20031103001112003110300111NM 2003 11 3 AWXA200301135 120030904A53106546532 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND FLOOR SUPPORT SHEAR TIE AT BS 500, LBL 1. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGE FROM BS 500 FROM BL 0 TO LBL 5; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07, PG. 232, FIG. 210. 2L72 4F RTA16WE 20031106000962003110600096NM 2003 11 6 AWXA200301343 120031021A5320694147371 INTERCOSTAL BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MINOR REPAIR - DURING C-21 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 480, LBL 24. MAINTENANCE REMOVED INTERCOSTAL FROM BS 460 TO BS 480, LBL 24; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-41473; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, FIG 11, PG 2-3. 2L72 4F RTA16WE 20031112001322003111200132EU 2003 11 12 BAQA090130 120031017A2150510286C GEARBOX UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE A/C PACK FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH1548 0069 90 DEGREE GEARBOX HAS NO OUTPUT. UNIT LASTED ONLY 244.4 HOURS SINCE INSTALLED. REPLACED WITH SERVICEABLE UNIT. UNIT SENT DIRECTLY FROM ORLANDO, FL TO METRO AVIATION. 1G72 3U3 UO H88EU E42NE 20031120000282003112000028NM 2003 11 20 AWXA200301237 120030922A532065524578 PAN BOEING737 737301 1384611NM LAVATORY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT LAVATORY SUBFLOOR PAN REPAIR DOUBLER BS 1020, RBL 15, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED RT AFT LAVATORY SUBFLOOR PAN AT BS 1020, RBL 15, WL 208; FABRICATED A NEW REPLACEMENT PAN; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, STEP 4 & 5 AND PG 42, FIG 10. 2L72 4F RTA16WE 20040112001272004011200127EU 2004 1 12 2004F00029 120030803A2435150SG122Q GENERATOR SNIAS 350 AS350B3 8680954EU ENGINE INTERMITTENT A S4WAK NONE O OTHER ININSP/MAINT 1 WP07820NA 3602 STARTER GEN IS OPERATING INTERMITTENTLY DURING START CYCLE. SUSPECT BRUSHES OR 'DEAD' SPOT ON COMMUTATOR. REPLACED WITH SERVICEABLE PART AND OPS CHECK OK. (M) 1G71 3U H9EU 20040112001982004011200198NM 2004 1 12 2003UALA00956 120031211A335060243 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29329UA 24149 EEL LIGHT INOP FROM SEAT ROW 15 TO 21. RELAMPED, TESTED GOOD. 2L72 4F4 FRTA16WE E2GL 20040415000722004041500072WP 2004 4 15 ASAA0380741 120031114A2540MD08050711 STRUCTURE DOUG DC9 DC983 3022083WP LAVATORY CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CRACKS IN TRASH SHOOT ABOVE BOX IN RIGHT AFT LAV TRASH VANITY. REPAIRED PER SRM, ASA EA 2540-01113, AND AAR EA 10099. (M) 2L72 4F RTA6WE 20031125001362003112500136NM 2003 11 25 ASAA0310155 120030318A7830 DOOR BOEING737 737210C 1384459NM THRUST REVERSER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 2 ENGINE DEFLECTOR DOOR SKIN AT THRUST REVERSER STATION 200.70 CRACKED. REMOVED DAMAGED AREA AND REPAIRED SKIN PER OHM. (M) 2L72 4F A16WE 20031222000502003122200050WP 2003 12 22 GTIA030949 120031107A5320 STRUCTURE DOUG DC9 DC983 3022083WP SUB FLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND CABIN STATION 218 LBL 45 SUB-FLOOR CORRODED AT FLOOR SUPPORT. REMOVED DAMAGED AREA. FABRICATED REPAIR FILLER AND DOUBLER. INSTALLED REPAIR. (M) 2L72 4F RTA6WE 20031222001032003122200103NM 2003 12 22 AMTA200301375 120031107A5210 STATIC LINE BOEING757 75723N 1384973NM DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11524AT 30233 1L DOOR SLIDE ARM LEVER WILL NOT MOVE ALL THE WAY TO THE DISARMED POSITION. FOUND STATIC LINE JAMMED UNDER GIRT BAR. INSTALLED STATIC IAW MM 25-66-10-2, SLIDE OPS CHECK OK. (M) 2L72 4F RTA2NM 20031229000802003122900080NM 2003 12 29 DHL2003742500 120031122A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSELAGE SKIN TWO DENTS STA 430 BETWEEN STR 2R AND STR 3R. MEASURE DENT AND FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGE AREA DIM 4 INCH X 1.375 INCH AND FABRICATED ONE DOUBLER DIM 14 INCH X 9.5 INCH USING 2024 T-3 .050 PO 900226 IAW B-727 SRM 53-30-3 FIG 1. ALODINED AND PRIMED DOUBLER IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040106000012004010600001WP 2004 1 6 DHL2003802578 120031211A27105715841506 MECHANISM DOUG DC8 DC873 302199CWP RT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING INBD AILERON MANUAL REVERSION MECHANISM CRACKED. REMOVED AND REPLACED MANUAL REVERSION MECHANISM AT RIGHT WING INBD AILERON IAW MM 27-11-8 PG 401-404. PERFORMED ADJUSTMENT TEST, GOOD IAW MM 27-10-0 PAGES 510 THRU 515. SEE NR 1456 FOR OPS CHECK. 2L74 4F RT4A25 20031014001692003101400169NM 2003 10 14 SWAA032085 120030918A53136551698 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26R CORRODED AT BS 1011 TO BS 1015. REPAIRED STRINGER PER SRM. 2L72 4F A16WE 20031124001402003112400140EU 2003 11 24 03296317 120031023A7931 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP COCKPIT ACTIVATED A VTZAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA27317UE 41031 DURING TAKEOFF CREW RECEIVED A LT ENGINE LOW OIL PRESSURE WARNING. CREW PERFORMED IN FLIGHT SHUT DOWN AND DECLARED EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT. 2L72 4T3 TRTA41NM E2WE 20031202000812003120200081NM 2003 12 2 USAA030220 120031028A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US43197 23876 FOUND SKIN CRACKED 1.5 INCH, FS 744 JUST ABOVE S25R. DOUBLER INSTALLED PER SRM 53-00-01 FIG 231. (M) 2L72 4F RTA16WE 20031203000472003120300047EA 2003 12 3 2003F00638 120030913A7830 ISOLATION VALVE CNDAIRCL600 CL6002D24 EA THRUST REVERSER DEFECTIVE A FDKACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW07903FJ893 15003 ABORTED TAKEOFF DUE RIGHT REVERSER UNSAFE CAUTION MESSAGE. OPS CHECK GOOD. VALVE ISOLATION CONTROL P/N TY214810A. (M) 2L72 4F RTA21EA 20031204000112003120400011WP 2003 12 4 GTIA030879 120031002A5754 CAP DOUG DC9 DC982 3022082WP RT WING SLAT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP IS CRACKED. REMOVED END CAP. LOCATED AND DRILLED NEW PART. INSTALLED NEW END CAP. (M) 2L72 4F A6WE 20031204000682003120400068EA 2003 12 4 03284638 120031011A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 DURING INSPECTION THE OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB AS WELL AS REPAIRED A WIRE TO THE LIGHT ASSEMBLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031205000612003120500061 2003 12 5 SWIA200312520 420031010A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA STALL WARNING DISCONNECTED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07454SW 7749 CAPTAIN'S STICK SHAKER NOT WORKING, BOTH WIRES ARE PULLED FROM UNIT ON CAPTAIN'S COLUMN. REINSTALLED PINS ONTO CAPT'S STICK SHAKER PER MM 20-00-00. OPS CHECK GOOD PER MM 27-00-00. 2L72 4F RTA21EA 20031208000202003120800020SO 2003 12 8 C2XA03TY198 120031202A532014521725013 SILL EMB 135 EMB135ER 3260203SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727506 145206 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB SRM 51-40-02 AND CPM 51-21-05/06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031209001822003120900182NM 2003 12 9 UPS03441500 120031009A5730 PANEL BOEING747 747200 1384847NM RT WING DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, RT WING I/B FIXED T/E PANEL UPPER SURFACE ONE LOCATION FOUND DEBONDED AS RED MARKED AT WBL 237 APPROX. RT WING I/B FIXED T/E PANEL UPPER SURFACE REPAIRED AS PER SRM 57-30-04 FIG 7. PERFORM REINSPECT AT EACH A-CHECK AS PER UPS EO B747-5720-19453 AND REPLACE PANEL BY NEXT C-CHECK OR LATER THAN 18 MONTHS AS PER UPS EO B747-5720-19453. 2L74 4F RTA20WE 20031209002552003120900255NM 2003 12 9 UPS03441522 120031017A1430BACB30US8K31 FASTENER BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, RT BS 1480 BULKHEAD - ONE EACH FASTENER NR 5 WAS CRACKED AT EXTENSION FITTING AREA RUNNING AFT APPROX 0.040 INCH LONG. REF RS R53-43-35093 & EO B747-5310-19423A RT BS 1480 BULKHEAD SPLICE EXTENSION FTG NR 5 HOLE OVERSIZED TO 0.625 INCH & HFEC CONFIRMED NO CRACK REPAIR BUSHING FABRICATED AND INSTALLED NR 5 BOLT REPLACED THE HOLE DIAMETER EDGE/END MARGIN REF RS TABLE 1. THE BS 1480 BULKHEAD SPLICE HOLES 1 TO 26 REQUIRED REPEAT INSPECTION EVERY 6000 FLT CYCS PER SB747-53A2390. 2L74 4F A20WE 20030919000942003091900094NM 2003 9 19 2003F00574 120030813A49206981934 IMPELLER HONEYWELL 85129H BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE APU BROKEN B E ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 WP0714653 P100646 28914 P100646 BROKEN BLADE FROM SECOND STAGE IMPELLER THAT POSSIBLY EXITED TURBINE PLENUM. 2L72 4F4 FRTA16WE E2GL 20030923001642003092300164NM 2003 9 23 AALA20030414 120030406A3350 SOCKET BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21971AN 29547 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT 11D LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SOCKET AT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030924001302003092400130EU 2003 9 24 AALA20030006 120030105A2750 SCREW AIRBUS300 A300B4605R 3930308EU FLAP/SLAT HANDLEDAMAGED A AALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SW2133069 512 LEADING EDGE SLATS WOULD NOT MOVE INTO SELECTED RETRACT POSITION OR 30/40 POSITION. CAPTAIN DECLARED AN EMERGENCY AND AIRCRAFT RETURNED TO SJU WITHOUT INCIDENT. REPLACED FLAP/SLAT HANDLE SCREW. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20040128000472004012800047 2004 1 28 UPS03141669 420031223A2565 CONNECTOR AIRBUS300 A300B4622R 3930312EU EVAC SLIDE LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01147UP P1548 INSPECTION TYPE: PFLT, DURING STATIC WARNING TEST RED LIGHT DID NOT ILLUMINATE, TOW WAS HEARD. *SUPPLEMENTAL* RESEATED C/P ON THE AUTONOMOUS STANDBY POWER SUPPLY UNIT. OPS CHECKS GOOD PER MM 52-73-00. THIS CLEARS M273081. REFERENCE LP 141511. 2L72 4F RTA35EU 20040129000422004012900042EU 2004 1 29 MALA030600 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 12D & 14F FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAMES 14D, 14F IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040128001512004012800151NM 2004 1 28 QXEA200301600 120031215A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 CRACK IN RIGHT FIRE WALL ON RIVET SIDE OF NACELLE ABOVE FIRE LOOP BRACKET ON OUTBOARD NACELLE. REPAIRED IAW DHC-8 RD 8-54-806, RD 8-54-109 AND RD 8-54-800. 2H72 4T RTA13NM 20040203000362004020300036NM 2004 2 3 ASAA0310206 120030322A54106961970 RETAINER BOEING737 737210C 1384459NM NR 1 NACELLE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND NR 1 ENGINE SEAL RETAINER AT NACELLE STATION 173 CRACKED. REMOVED AND REPLACED RETAINER IAW SRM. (M) 2L72 4F A16WE 20030923000772003092300077WP 2003 9 23 DHL2003604682 120030604A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP PAX DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT AFT PASSENGER DOOR JAMB AFT UPPER CORNER HAS INTERIM REPAIR. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 18 SHEET 3 TR 53-135, DWG SR 08530021, DWG 5750776. FABRICATED FILLER (7075-T6 AL0.080) AND (02 EA) DOUBLERS (7075-T6 AL0.90) (7075-T6 0.125) IAW SRM 53-2-0 FIG 18 SHEET 3 TR 53-135, DWG SR08530021, DWG 5750776. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLERS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 18 SHEET 3 TR 53-135, DWG SR 08530021, DWG 5750776, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040127002172004012700217WP 2004 1 27 ASAA0380602 120031003A33500105603 LIGHT DOUG DC9 DC982 3022082WP FWD CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 4. SPLICED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040130002322004013000232EU 2004 1 30 MALA040105 120031229A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, FS 294 LT I/B FWD SEAT TRACK HAS CORROSION. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. REFER TO NR 1195871 FOR ADDITIONAL INFO. A/C RELEASE DATE 01/06/2004. 2L72 4T RTA52EU 20040202003132004020200313NM 2004 2 2 AWXA200400058 120031205A575465C2660399SP WEDGE BOEING737 73733A 1384673NM NR 3 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN DELAMINATED. MAINTENANCE CUT OUT DELAMINATED AREA NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN; CLEANED AND PREPARED AREA; FABRICATED REPAIR DOUBLERS; INSTALLED BOND REPAIR IAW B737-300 SRM 51-70-10, FIG 16, PG 67-69. 2L72 4F RTA16WE 20040206000422004020600042WP 2004 2 6 ASAA0380829 120031216A53305913421 SKIN DOUG DC9 DC983 3022083WP FUSELAGE BULGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND SKIN BULGED JUST AFT OF RIGHT NLG DOOR. REPLACED SKIN PER DAC DWG 5913421. (M) 2L72 4F RTA6WE 20040209000152004020900015NM 2004 2 9 DHL2003753511 120031229A571265173103OR4 RIB BOEING727 727223 1384074NM NR 7 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, NR 7 SLAT AT ACTUATOR ATTACH MOUNT INBOARD/OUTBOARD SIDES RIB AND PREVIOUS CRACKED SLAT STA 292. REMOVED NR 7 SLAT IAW B-727 M/M 27-81-11. REMOVED INT ACCESS PANELS AND RIBS (2) AT NR 7 SLAT IAW B-727 SRM 51-30-2. DRILLED NEW HOLES AT RIBS IAW B-727 SRM 51-30-5. INSTALLED NEW RIBS P/N 65-17310-3 AND 65-17310-4 PO 3421124 AND 342176 IAW B-727 SRM 51-30-2. REINSTALLED NR 7 SLAT IAW B-727 M/M 27-81-11. OP'S CHECK GOOD IAW B-727 M/M 27-81-0. 2L73 4F A3WE 20040210000912004021000091EU 2004 2 10 USAA030302 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .140 SQUARE INCH AREA, FRAME 64 LBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040212000302004021200030CE 2004 2 12 56653 120031201A32341013841377 HANDLE BEECH 1900 1900D 1154162CE MLG STUCK A AMWAO OTHER F FLT CONT AFFECTED LDLANDING 1 CE07173YV UE173 WHEN LANDING GEAR WAS PLACED IN DOWN POSITION LANDING GEAR FAILED TO EXTEND GEAR MANUALLY PUMPED DOWN IND THREE GREENS ACFT LANDED WITH NO FURTHER INCIDENT...CAUSE OF PROBLEM WAS CONTROL, LANDING GEAR HANDLE. WE HAVE RR LDG GEAR SELECTOR HANDLE. P/N 1013841377 S/N 1449A 2L72 4T RTA24CE 20040212000562004021200056EU 2004 2 12 KBM2003F00098 120031105A6220126892P BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ROD END WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 UPPER AND LOWER BEARING HAS DAMAGE, WORN AND HAS EXCESSIVE PLAY ON BEARING. REPLACED WITH 3 NEW ROD END BEARINGS. 1G71 3U3 U H9EU E19EU 20031209002572003120900257WP 2003 12 9 UPS03841524 120031022A5714 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, CENTER WING TANK UPPER REAR SPAR CAP SPLICE/ANGLE REPAIR FILLER SPACER IS CORRODED BEYOND LIMITS AT RBL 43 AT STA 857. REMOVED, FABRICATED AND REPLACED SPLICE IAW SRM 53-2-5 FIG 12. 2L74 4F RT4A25 20031211001972003121100197EU 2003 12 11 USAA030247 120031031A5320D5347209000200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT CORRODED 1.0 INCH LONG BY .70 INCH WIDE, BY .045 INCH DEEP, FRAME 66 OUTBOARD OF FLOOR CTR LEFT OF CTR LINE LAV AREA. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040316000662004031600066WP 2004 3 16 GTIA031073 120031117A5321 CHANNEL DOUG DC9 DC981 3022081WP FLOOR PANEL CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND LT OUTBOARD FLOOR PANEL STATION 945 HAT CHANNEL CRACKED. REPAIRED CRACKED AREAS. (M) 2L72 4F A6WE 20031217000462003121700046WP 2003 12 17 DHL2003802525 120031114A53204611067N FITTING DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 FWD ACCY COMPT FITTING CORRODED, STA 70.000, L-24R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031217000812003121700081NM 2003 12 17 CALA0300670 120030718A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND FLOOR SUPPORT CORRODED ON LOWER SIDE OF FLOOR SUPPORT AT STA 967-986, LBL 17. 2L72 4F RTA16WE 20060801001312006080100131WP 2006 8 1 IXXA060574S 120030909A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "B" TANG BROKEN AT STATION 240. REMOVED DAMAGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0. 2L74 4F RT4A25 20030821000452003082100045NM 2003 8 21 03FDEA01022 120030627A5754ARC015428 HINGE DOUG MD11 MD11 3023602NM LE FLAP CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT WING INBOARD FLAP OUTBOARD FWD HINGE PIVOT LUG BORE AT INBOARD LOWER SIDE FOUND CHIPPED OFF. RIGHT WING INBOARD FLAP OUTBOARD FWD HINGE PIVOT LUG BORE AT INBOARD LOWER SIDE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69363 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030404000022003040400002NM 2003 4 4 372PA0019 120030401A3350 LIGHT BOEING737 737306 13844BGNM CABIN CONTAMINATED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. CLEANED ALL LIGHT RECEPTICALS AND DRIED WATER OUT OF TRACKS AS REQUIRED. OPS CHECK NORMAL. 2L72 4F RTA16NE 20030407000362003040700036WP 2003 4 7 GTIA021398 120030125A3397 WIRE DOUG DC9 DC982 3022082WP TAIL BAY DAMAGED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT, DO NOT COME ON WITH EMERGENCY POWER. FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT NOT CONNECTED. SPLICED WIRING FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT. (M) 2L72 4F A6WE 20030408001332003040800133NM 2003 4 8 AWXA200300339 120030324A5320693816717 INTERCOSTAL BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND ON INTERCOSTAL AT FASTENER HOLE OF LT RAM AIR INLET BS 530. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 530; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-38167; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10 & 11. 2L72 4F4 FRTA16WE E2GL 20030410001912003041000191 2003 4 10 DL76G030119 420030201A2565333780100 POWER SUPPLY BOEING767 767324 1385203NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27394DL 27394 ON PDC FOUND LEFT OVERWING SLIDE SQUIB NOT ILLUMINATING WITH TEST SWITCH 1. RT SPOILER SQUIB LIGHT WILL NOT ILLUMINATE WITH TEST SWITCH 2. INSTALLED NEW BATTERY POWER SUPPLY AND BATTERY M962. ALL SQUIB TESTS NOW OK. 2L72 4F RTA1NM 20030409000252003040900025 2003 4 9 MEX2003049 420030228A3130 RECORDER DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FLT DATA INOPERATIVE W ASMFD RETURN TO BLOCK O OTHER NRNOT REPORTED 1 SW23505MD 49149 AIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN DISCONTINUE ENGINE NR 1 STARTING, FOR FIRE DURING STARTING OF ENGINE NR 2, WITH INDICATION AT CABIN. ENGINES WERE INSPECTED AND TESTED IAW MM, ALL CORRECT. IAW MAINTENANCE CONVENIENCE FLIGHT DATA RECORDER WAS REPLACED. DURING OVERNIGHT SERVICE DENGINE NR 2 WAS INSPECTED AND FDR WAS READ, ALL CORRECT. 2L72 4F4 F A6WE E2EA 20030414001232003041400123NE 2003 4 14 CA030306007 220030221A7261LR47000A SHAFT BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE OIL PUMP SHEARED W A UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 CA (CAN) IFSD AND DIVERSION, LOSS OF LT OIL PRESSURE DATA FOLLOWED BY INDICATION OF 0 PSI. 3-MIN LATER COMPRESSOR STALL ON LT ENGINE WITH COMPLETE SHUTDOWN. PRELIMINARY FINDING, RRD REPORTED OIL PUMP FAILURE AND SUSPECT OVERSERVICING. OIL TANK WAS FOUND TO BE AT FULL LEVEL, MECHANIC REPORTED BEING NORMAL BUT ALSO SAID IT WAS 2 GAL (WHICH WOULD BE TOO HIGH). N2 SYSTEM SEIZED, FAN AND N1 WAS FREE TO ROTATE BUT MINOR SCRAPING NOISE HEARD. OIL PUMP REMOVED AND FOUND TO HAVE A SHEARED SHAFT, AT THE SHEAR NECK. 2L72 4F4 FTRA6WE E00061EN 20030416002842003041600284WP 2003 4 16 AALA20030297 120030309A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21271AA 49293 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS FROM 8D-11D INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR SEATS 8D-11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030423001002003042300100CE 2003 4 23 GLBA2003008 120030117A3233 CAP BEECH 1900 1900D 1154162CE NLG ACTUATOR BROKEN A GLBAK NONE O OTHER ININSP/MAINT 1 NM03204GL15564 508 UE204 NOSE GEAR ACTUATOR CAP BROKE. REMOVED AND REPLACED NOSE GEAR. 2L72 4T RTA24CE 20030423001922003042300192NM 2003 4 23 UPS03240296 120030306A5260 STRUCTURE BOEING727 72725C 138400HNM AIRSTAIRS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 INSPECTION TYPE: C&SI, AIRSTAIRS; A CRACK IS EXTENDING FROM BENEATH REPAIR AT LIGHTENING HOLE ON RT SIDE OF AIRSTAIRS AT STEP 10 AND ONE RIVET IN THE REPAIR IS NOT SECURE. REPAIR PLATE FITTED AS PER SRM 51-40-2. RIVETED AS PER SRM 51-30-2, TREATED PER SRM 57-10-2. STOP CRACK HOLES DRILLED AS PER SRM 51-10-1. HFEC CARRIED OUT AROUND STOP DRILLED HOLES IAW B727 NDTM 51-00-00. CRACK CONTAINED BY STOP DRILLS. 2L73 4F A3WE 20030424001802003042400180SO 2003 4 24 LR7A03035 120030313A53433884829 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5323 FOUND FS 577 LT MLG BEAM ASSY CRACKED AT LBL 64, WL 240. PREVIOUS REPAIRS AT WL 225 & 245. BEAM ASSY REPLACED IAW SRM SMP 583 51-60 & 51-70 AND DWG 388482. NR 2316. 2H74 4T A1SO 20030430002132003043000213NM 2003 4 30 VNAA0304014 120030416A24208160121 GENERATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RIGHT FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07427JS4571 219 3039 DURING CLIMBOUT, THE LEFT HAND GENERATOR FAILED AND THE CREW THEN RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND STARTER GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030501001492003050100149 2003 5 1 ASAA0380116 420030202A256539A61896501 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01954AS 49387 SEA/SJD - DURING PREFLIGHT CHECK AT BOTH STATIONS, FOUND AFT LEFT (L2) SERVICE DOOR GIRT-TO-SLIDE COVER LANYARD DISCONNECTED. REATTACHED LANYARD. (M) 2L72 4F A6WE 20030502000152003050200015NM 2003 5 2 AMTA200300372 120030319A3350 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 AFT THREE EMERGENCY FLOOR LIGHTS OUT IN ZONE C. RECONNECTED WIRING PER SWP 20-00-00 TEST GOOD. (M) 2L72 4F RTA2NM 20030505001142003050500114EU 2003 5 5 00088 120030423A5230 LATCH AMD FALC20FALCON 2720302EU CARGO DOOR OUT OF ADJUST E HAEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW05158TW 158 PILOT REPORTED AFTER REACHING FL330 -DOOR- UNSAFE ILLUMINATED, DIVERTED TO ADS FOR MAINTENANCE. MAINTENANCE ADJUSTED TOP FWD DOOR LATCH PER MAINTENANCE MANUAL AND OPS CHECK GOOD. 2L72 4F A7EU 20030505001052003050500105NM 2003 5 5 03FDEA00208 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 4L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030506001822003050600182WP 2003 5 6 ASAA0380255 120030307A531199115055 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FRAME AT FS 83.5 CRACKED AT RBL 9. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM. (M) 2L72 4F A6WE 20030507002032003050700203NM 2003 5 7 CH1A200395016 120030410A5320 CHANNEL BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON HAT CHANNEL SECTION BS 1070 AT LBL 55. 2L73 4F A3WE 20030508000262003050800026CE 2003 5 8 CXU2003F00000 120030327A323112810331 ACCUMULATOR CESSNA210 210M 2073450CE CONT O520 IO520* 17032SO MLG FAILED E CXUAO OTHER O OTHER NRNOT REPORTED 1 CE07965B 21061580 END PLUG IN HYDRAULIC ACCUULATOR DEPARTED RELEASING HYDRAULIC FLUID AND PRESSURE. AIRCRAFT TACH READS 3679.2. 1H71 3O3 O 3A21 E5CE 20030506001402003050600140WP 2003 5 6 GTIA030191 120030221A5320 BRACKET DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 MAIN CABIN UNDER FLOOR AT STA 905, RT FLOORBEAM TO FUSELAGE ATTACH BRACKET CRACKED. LOCATED AND DRILLED NEW FLOORBEAM TO FUSELAGE ATTACH BRACKET. INSTALLED NEW ATTACH BRACKET. 2L72 4F4 FRTA6WE E2EA 20030508000612003050800061NE 2003 5 8 COMA0360226 220030503A72614138T09P01 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE ACCY GEARBOX LEAKING A COMAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01408CA 7440 FLIGHT 5854 RT ENGINE LOW OIL PRESSURE WARNING. REPLACED THE ACCESSORY GEAR BOX DRIVE CARBON SEALS. 2L72 4F4 FRTA21EA E15NE 20030509000462003050900046NM 2003 5 9 USAASB03043 120030319A3260MS253831 SWITCH BOEING737 737301 1384611NM MLG FAILED A USAAO OTHER O OTHER APAPPROACH 1 EA19334US 23231 UPON APPROACH INTO PWM, WITH GEAR HANDLE DOWN, CREW RECEIVED A RED NOSE LANDING GEAR UNSAFE LIGHT ALONG WITH ALL THREE GREEN GEAR DOWN AND LOCKED LIGHTS. CREW DECLARED AN EMERGENCY AND MANUALLY LOWERED THE NOSE LANDING GEAR. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE ACCOMPLISHED LANDING GEAR POSITION AND WARNING SYSTEM TROUBLESHOOTING PER MM 32-61-00 AND WD 32-64-01. REMOVED AND REPLACED LANDING GEAR LEVER POSITION SWITCH S78 PER MM 32-61-11. ALSO, REMOVED AND REPLACED NOSE GEAR LATCHING RELAY R374 (P/N BR20AXH5V3) AND PRINTED CIRCUIT CARD M983 (P/N 65-58250-29), AS PRECAUTIONARY, PER MM. JACKED AND OPERATIONALLY CHECKED NOSE LANDING GEAR RETRACTION AND EXTENSION SYSTEMS. 2L72 4F RTA16WE 20030509001612003050900161 2003 5 9 AMTA200300336 420030308A3417 PITOT HEAD BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE DAMAGED A AMTAO OTHER N FALSE WARNING CLCLIMB 1 GL11554TZ 32588 31817 CLIMBING OUT OF FL 210 AT -14 TAT, RT ENGINE STARTING SURGING BADLY. POWER LEVER RETARDED, RT EEC SELECTED OFF AND OPS NORMAL` REST OF FLIGHT WITH BOTH EEC'S OFF PER MEL. INSPECTED NR 2 ENGINE PER AMM 77-11-04-06 FOUND BROKEN PITOT HEAD REPAIRED PITOT HEAD AS NEEDED IAW ERA NR 757-72T-4666. (M) 2L72 4F4 FRTA2NM E12EU 20030527001182003052700118NM 2003 5 27 COOSDR030016 120030501A57536521634 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE RT WING TE FLAP DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG 20725 RIGHT WING, INBOARD AFT FLAP, PN 65-21634-75, SN BN-8001 WITH DELAMINATION. 2L73 4F4 FRTA3WE E2EA 20030602001542003060200154NE 2003 6 2 VNAA0305017 220030526A7532 BLEED VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT ENGINE FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07459PS 3070 DURING CLIMB OUT FROM PIT, THE CREW REPORTED THE RIGHT HAND HIGH PRESSURE BLEED VALVE FAILED AND THEN HAD A POWER LEVER SPLIT AND RETURNED TO PIT. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE THEN TRIMMED THE RIGHT HAND ENGINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00 OPERATIONAL CHECKS WERE PERFORMED AND NO DEFECTS WERE NOTED. THE HIGH PRESSURE BLEED VALVE WAS THEN PLACED ON THE MEL LIST UNDER 36-1 C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030604001592003060400159NM 2003 6 4 UPS03440579 120030412A575365B106261 RIB BOEING747 747121 1384871NM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 4 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1, 2, 4, 5, 7 & 8 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030604000872003060400087NM 2003 6 4 UPS03440501 120030408A5310 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 FWD CARGO - BELL FRAME FOUND CRACK AT STA 660, STR 38L AREA AS MARKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20030604001372003060400137NM 2003 6 4 UPS03440557 120030411A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 2220 RT STRINGER 26R FRAME FOUND CRACKED. M/D BS 2220 RT FRAME REPAIRED AT BETWEEN STR 24R TO 34R AS PER SRM 53-10-04 FIG.100 & BOEING MSG UPS-HKF-03-00059H /61F FOR DETAIL. 2L74 4F A20WE 20030520001432003052000143SW 2003 5 20 ALGA086418 120030515A6320406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01477AL1737 53203 EXCESSIVE AXIAL PLAY. 1G71 3U O H2SW 20030612000562003061200056SO 2003 6 12 C2XA03IA054 120030527A3210 LANDING GEAR EMB 145 EMB145LR 3260212SO MAIN MALFUNCTIONED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2719554 145587 IAH - FLT 2857 - PILOT REPORTED THAT THE UPON CLIMBOUT FROM STL THE GEAR HANDLE HAD TO BE CYCLED TWICE TO GET THE LANDING GEAR TO RETRACT. THE AIRCRAFT CONTINUED ON TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR AND FOUND THE LANDING GEAR SYSTEM TO BE OPERATING NORMALLY. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030613000032003061300003EA 2003 6 13 SWIA200312056 120030531A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07441SW 7602 OVER MEM AT FL 410 TEMP -60C DEGREES F/O WINDSHIELD CRACKED. F/O SIDE WINDOW CRACKED AT 11,000. FOLLOWED QRH FOR CRACKED WINDSHIELD AND CONTINUED TO KNOXVILLE. REMOVED AND REPLACED RIGHT WINDSHIELD AND RIGHT SIDE WINDOW IAW CRJ MM 56-11-01. P/N OFF: 601R33033-14 S/N OFF: 01214H4750 P/N ON: NP-139321-10 S/N ON: 01296R1711, P/N OFF: 601R33033-12 S/N OFF: 0199H3356, P/N ON: NP-139322-6 S/N ON: 03133H3843. 2L72 4F4 FRTA21EA E15NE 20030612000202003061200020SO 2003 6 12 C2XA03SH164 120030529A3260852701 SQUAT SWITCH EMB 145 EMB145ER 3260211SO MLG FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING TEST FLIGHT 3160 A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. PILOT USED DOWNLOCK RELEASE BUTTON TO RAISE AND LOWER GEAR. THE AIRCRAFT COMPLETED FLIGHT WITH NO OTHER INCIDENTS. MAINTENANCE ADJUSTED LEFT HAND MAIN LANDING GEAR WOW SWITCH IAW EMB 145 AMM 32-63-05. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030520001402003052000140NM 2003 5 20 UIEA200300015 120030326A3610 CLAMP BOEING747 747228F 1384895NM BLEED AIR LOOSE A UIEAJEA DUMP FUEL ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA15536MC 21576 NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED & FIRE BELL ACTIVATED DURING CLIMB THROUGH 3000 FT. NR 1 ENGINE NACELLE TEMP INDICATES 'F' FOR BOTH 'A' AND 'B' LOOPS. ENG FIRE CHECKLIST ACCOMPLISHED. 80,000 KGS OF FUEL DUMPED. AFTER PULLING FIRE HANDLE LIGHT WENT OUT IMMEDIATELY. FIRE BOTTLE WAS NOT DISCHARGED. NR 1 ENGINE TEMP LOOPS STILL IN THE 'F' RANGE. A/C ARRIVED WITH NR 1 ENGINE T/R DEPLOYED. EXTERNAL CHECKS, NO SIGN ON O/H OR DAMAGE. T/R STOWED AND FUNCTION CHECKED USING PNEUMATICS FROM APU SAT. ENGINE DUCT SEPARATION/RUPTURE INSPECTION ACTIONED IAW MM 5-51-86. PNEUMATIC TEST ACTIONED IAW MM 71-00-00. PNEUMATIC LEAK FOUND AT CLAMP DOWN STREAM OF HIGH STAGE BLEED VALVE & BEFORE PRV. CLAMP TAPPED2L74 4F A20WE 20030618002092003061800209SW 2003 6 18 HEEA087371 120030611A5210407070620151 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 CREW DOOR PANEL CRACKED. 1G71 3U O H2SW 20030620000502003062000050EU 2003 6 20 ASOA03227 120030520A5320S53970716357 BRACKET AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT UPPER AND LOWER ATTACHMENT BRACKETS FOR THE BANANA SEAL PANEL WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT UPPER AND LOWER ATTACHMENT BRACKETS FOR THE BANANA SEAL PANEL IAW SRM 53-91-42. (M) 2H72 4T RTA53EU 20030620000752003062000075NM 2003 6 20 USAA030071 120030529A5320 STRINGER CLIP BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 FOUND CLIP CRACKED 1 INCH, STRINGER CLIP 11R STATION 360. INSTALLED FABRICATED CLIP PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20030623000252003062300025NM 2003 6 23 USAA030053 120030515A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 FOUND SKIN AND KEEL BEAMS CORRODED 1 INCH BY .5 INCH AREA, STATION 727, L STRINGER 27 AND RT STRINGER 28 KEEL BEAMS. REPLACED LEFT AND RIGHT BEAMS SPLICED AT STATION 540 RETAINING FORWARD SECTIONS OF KEEL BEAMS PER TYPICAL REPAIR 53-60-09. CORROSION LEVEL 1. (M) 2L72 4F RTA16WE 20030707001532003070700153EU 2003 7 7 03FDEA00991 120030627A5414 PANEL AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE NR 1 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 NR 1 ENGINE PYLON PRE-COOLER PANEL, CRACK REPAIR. FACT 27JUN03 03:15 BFM R COMPLIED WITH E.A. 6-5452-70948 NACELLES/PYLONS. NR 1 ENGINE PYLON PRE-COOLER PANEL PANEL CRACK REPAIR. 2L72 4F4 FRTA35EU E13NE 20030708000812003070800081NM 2003 7 8 UPS03440880 120030623A3350 LIGHT BOEING747 747256B 1384865NM PWA JT9 JT9D* NE CABIN BURNED OUT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01528UP 24071 INSPECTION TYPE: PFLT, ENTRY DOOR, AFT EMERGENCY LIGHT OUT. RELAMPED, OPS CHECK GOOD. 2L74 4F4 FRTA20WE E20EA 20030707001762003070700176EU 2003 7 7 03167318 120030616A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMGERGENCY LIGHTBURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27318UE 41041 DURING MAINTENANCE INSPECTION, THE LT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030709001122003070900112SO 2003 7 9 C2XA03SH182 120030613A521014533395001 SKIN EMB 145 EMB145LR 3260212SO PAX DOOR DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK PASSANGER DOOR WAS FOUND TO HAVE TWO DENTS ON OUTER SKIN AFT OF HANDLE. MAINTENANCE REMOVED DAMAGE AND REPAIRED SKIN SECTION AFFECTED IAW EMB 145 SRM 52-10-00. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709000732003070900073EA 2003 7 9 03153638 120030602A5240601R313613 SEAL CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR LEAKING A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27638BR 7692 DURING CRUISE, THE CREW REPORTED A LOUD WHISTLING NOISE FROM THE RT FRONT OF THE AIRCRAFT. THE FLIGHT DIVERTED TO ORF AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE SERVICE DOOR SEAL. PRESSURIZATION AND OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030710000962003071000096SO 2003 7 10 C2A03SH178 120030612A532014524131001 CHANNEL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK U-CHANNEL WAS FOUND TO HAVE CORROSION UNDER MAIN DOOR THRESHOLD. MAINTENANCE REMOVED AND REPLACED AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030106001642003010600164NE 2003 1 6 HEEA082815 120030102A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 ROTOR BRAKE CYCLES CONTINUOUSLY. 1G72 3U H1NE 20030127001242003012700124SW 2003 1 27 HEEA083670 120030115A3212206050247131 COVER BELL 407 407 1182206SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 EMERGENCY FLOAT COVER TORN. 1G71 3U O H2SW 20030908002032003090800203EA 2003 9 8 SWIA200312289 120030719A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 CARGO DOOR COAMING FS 580 CRACKED. DISCOVERED DURING C-CHECK, REPLACED COAMING IAW CRJ SRM 51-40-11. P/N: 600-35160-11 2L72 4F RTA21EA 20031028000112003102800011WP 2003 10 28 0301839852 120030925A213110256861 CONTROLLER DOUG DC9 DC951 3022051WP PWA JT8 JT8D9 52048NE CABIN PRESSURE MALFUNCTIONED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01761NC 47709 AT FL330, THE RED CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FT & REGAINED CONTROL OF CABIN PRESSURIZATION IN MANUAL MODE. FLT CONTINUED & LANDED WITHOUT INCIDENT AT MSY WHERE MAINTENANCE MEL'D THE AUTOMATIC PRESSURE CONTROLLER. AFTER THE AIRCRAFT ARRIVED BACK AT DTW, MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. NO MENTION OF BITE BEING PERFORMED OR NOT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E2EA 20031029000742003102900074NM 2003 10 29 ASAA0340071 120030227A53206940710 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 727A 727B LBL 2 WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031119000272003111900027EA 2003 11 19 WVE2003F00014 120030908A5340MM67080500001 BRACKET CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE LT BLEED DUCT CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09610QX 10033 LEFT BLEED AIR DUCT SUPPORT BRACKET PN MM67080500001 AT FRAME STA 1108, LEFT BUTT LINE 27, WATER LINE 99.91 IS CRACKED APPROX 2 INCHES. PROBABLE CAUSE: STRESS. 2L72 4F4 FRTA21EA E15NE 20031120000702003112000070NM 2003 11 20 QXEA200301258 120030930A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 AIRCRAFT SKIN IS GOUGED AT X780, Z171 AND Y15R. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16, 51-20-26 AND RD 8-53-4941. 2H72 4T RTA13NM 20031030000252003103000025NM 2003 10 30 UPS03441283 120030905A5712 RIB BOEING747 747121 1384871NM NR 20 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING - NR 20 V/C FLAP I/B LINKAGE O/B RIB NR 2, NR 3 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2, NR 3 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTION. 2L74 4F A20WE 20031117000352003111700035EA 2003 11 17 QXEA200301217 120031005A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 SLIGHT DENT WITH CHERRY-MAX RIVET IN CENTER AT AFT MIDSECTION 4 INCHES FROM EDGE OF MAIN CABIN DOOR. REPAIRED IAW EA R-52-124. 2L72 4F RTA21EA 20031112000872003111200087SW 2003 11 12 BAQA090477 120031031A2435 BRUSHES BELL 206 206L3 1182108SW STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03206CJ628 98257 51579 STARTER GEN HAS BRUSHES WORN. REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20031118000672003111800067NM 2003 11 18 03FDEA01691 120031002A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON OB FLANGE OF S28-R KEELBEAM, STA 720E TO 720F. REPAIRED PER E.A. 7-5310-55007. 2L73 4F RTA3WE 20031106002142003110600214NM 2003 11 6 ASAA0310475 120030519A5313 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND STRINGER 20R AT FUSELAGE STATION 767 CORRODED. REPAIRED STRINGER PER SRM. (M) 2L72 4F A16WE 20031106001522003110600152SO 2003 11 6 C2XA03TY172 120031005A521012021065001 SKIN EMB 145 EMB145LR 3260212SO PAX DOOR DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712540 145537 DURING A SCHEDULED INSPECTION THE PASSENGER ENTRY DOOR EXTERIOR SKIN WAS FOUND TO BE DENTED JUST AFT OF THE RELEASE HANDLE. MAINTENANCE RECONTOURED THE SKIN AND PERFORMED A NDT ON THE AFFECTED AREA WITH NO DISCREPANCIES NOTED, ALL WORK ACCOMPLISHED IAW EMB IC NR 2003-145/3275 AND CPM 51-21-04,05. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20031105000532003110500053 2003 11 5 SWAA032306 420031020A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031110001492003111000149EU 2003 11 10 AWXA200301348 120031104A5230 HANDLE AIRBUS320 A320231 3930325EU CARGO DOOR UNSECURE A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28633AW 082 SEA - ABORTED TAKEOFF - FLT 0749 - DURING TAKEOFF AT SEA EN ROUTE FOR PHX AFTER TAKEOFF THRUST APPLIED RECEIVED AFT CARGO DOOR OPEN INDICATION ON ECAM, REJECTED TAKEOFF AT LOW SPEED AND RETURNED TO GATE. MAINTENANCE FOUND AFT CARGO DOOR HANDLE EXTENDED, RESECURED HANDLE AND ALL INDICATIONS RETURNED TO NORMAL. 2L72 4F RTA28NM 20040109000012004010900001SO 2004 1 9 IRJC2003001 120030807A27311708800 DRUM PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA ELEVATOR TRIM UNSERVICEABLE E IRJCK NONE O OTHER ININSP/MAINT 1 AL01820FS 317952185 PREFLIGHT AND OPS CHECK OF TRIM SYSTEM NORMAL. 30 MINUTES INTO FLIGHT, PILOT NOTICED LIMITED RANGE IN ELEVATOR TRIM. PERFORMANCE DEGRADED AND TRIM JAMMED, MANUAL AND ELECTRIC. INSPECTION REVEALED WEAR ON THE JACKSCREW AND DRUM THREADS. PARTS WERE REPLACED AS REQUIRED. TOTAL TIME ON PART UNKNOWN BUT IS SUSPECTED TO BE CONSIDERABLE. RECOMMEND A SPECIAL INSPECTION TO INCLUDE DISASSEMBLY, INSPECTION, AND REPLACEMENT AS REQUIRED OF TRIM DRIVE MECHANISM PARTS AT EACH 1000 HOURS TIME IN SERVICE. 1L72 3O3 O A20SO E14EA 20040112000672004011200067NM 2004 1 12 DHL2003747014 120031219A2560 DOOR BOEING727 727224 1384076NM COCKPIT UNSECURE A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01747DH 22253 CAPTAIN'S SIDE ESCAPE ROPE DOOR WON'T CLOSE. RE-SECURED DOOR AS REQUIRED; OPS CHECKED NORMAL. 2L73 4F A3WE 20031124000082003112400008EA 2003 11 24 SWIA200312595 120031110A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TRIM SWITCH LOOSE A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07591SW 7079 CAPTAIN'S TRIM SWITCH WILL NOT TRIM DOWN. SOLDERED WIRE ON TRIM SWITCH. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20031121000882003112100088NM 2003 11 21 AWXA200301422 120031030A5320651768538 WEB BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK 2 EACH CRACKS WERE FOUND ON SHEAR WEB AT BS 344, AFT OF L-1 DOOR. MAINTENANCE REMOVED DAMAGED SHEAR WEB BS 344; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-200 SRM 51-20-02, FIG 7. 2L72 4F RTA16WE 20031217000872003121700087WP 2003 12 17 ABXA030447 120031106A552099184809 STRUCTURE DOUG DC9 DC932 3022066WP LT ELEVATOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 LEFT ELEVATOR OUTBOARD OF GEARED TAB HAD LEVEL II CORROSION WITH DISHED RIVETS AND BULGING SKIN. REPLACED LEFT ELEVATOR ON NON ROUTINE 0518, IAW DC-9 MM. 2L72 4F A6WE 20031218000232003121800023NM 2003 12 18 DHL2003780013 120031125A3240 BRAKE BOEING727 727223 1384074NM RIGHT STUCK A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01780DH 22006 RT BRAKE IS HYPER SENSITIVE, SUSPECT RT BRAKE PRESSING, RT BRAKE STUCK ON TAXI. MAINTENANCE TOWED A/C TO BLOCKS. PERFORMED OPS CHECK OF BRAKES AND BRAKES OPS CHECK GOOD. NO DEFECTS NOTED IAW M/M 32-41-00 AND JRH 9.1 FOR TAXI CHECK. 2L73 4F A3WE 20031229000902003122900090NM 2003 12 29 DHL2003742509 120031123A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CORROSION ON BS 360 FLOORBEAM UPPER CHORD SPLICE LBL 20, WL 208. REMOVED DAMAGED PARTS AND FABBED NEW T-SPLICE FROM BAC 1505-100617 PO 90041 DIM 12 INCHES LONG AND 2 EACH SPLICE ANGLES FROM BAC 1505-29222 PO 9912219 DIM 12 INCHES AND 8.5 INCHES LONG IAW B-727 SRM 53-10-8 FIG 1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-10-8 FIG 1. 2L73 4F A3WE 20031229001522003122900152 2003 12 29 03348307 420031214A31607003110901 DISPLAY JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA27307UE 41021 DURING OPERATION OF THE AIRCRAFT CREW REPORTED A SMOKE ODOR IN THE FLIGHT COMPARTMENT. THE SOURCE OF THE ODOR WAS FOUND TO BE THE FIRST OFFICERS LOWER ELECTRONIC DISPLAY UNIT. THE UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031223001382003122300138CE 2003 12 23 DXTA200300187 120031115A2710666000161 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07699QS 5605199 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20040106000402004010600040WP 2004 1 6 DHL2003802577 120031203A5751 HINGE FITTING DOUG DC8 DC873 302199CWP LT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 NR 4 LT AILERON HINGE FITTING CRACK. REMOVED AND REPLACED NR 4 LT AILERON HINGE FITTING IAW MM 20-16-0 PG 208. 2L74 4F RT4A25 20040105000692004010500069NM 2004 1 5 2003UALA00949 120031212A5230 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29121UA 29167 AFT CARGO DOOR BOTTOM EDGE DENTED APPROX SIZE OF DENT IS 2.00 IN (L) BY 6.00 IN (W) BY 0.150 IN DEPTH. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER & FILLER REPAIR ON EXTERNAL SKIN. 2L74 4F4 FRTA20WE E24NE 20040106001962004010600196WP 2004 1 6 GTIA030984 120031117A5320 SPLICE DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN STATION 1338 STRINGER 18L WEB CORRODED TOP AND BOTTOM. REMOVED SPLICE. FABRICATED NEW SPLICE. INSTALLED NEW SPLICE. (M) 2L72 4F A6WE 20040106002282004010600228WP 2004 1 6 GTIA031038 120031212A3260833703 SENSOR DOUG DC9 DC982 3022082WP NLG DEFECTIVE A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23804NK 49104 DEN - FLT 980 - NOSE GEAR UNSAFE LIGHT DID NOT EXTINGUISH DURING GEAR EXTENSION. WENT AROUND, FOLLOWED QRH-LANDED NORMALLY LIGHT EXTINGUISHED DURING QRH PROCEDURE AFTER RE-CYCLING GEAR. REMOVED AND REPLACED UNSAFE SENSOR. (M) 2L72 4F A6WE 20040109000602004010900060WP 2004 1 9 AALA20031252 120031111A33501001191 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219616 53563 DURING OVERNIGHT MAINTENANCE, FOUND FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031125001742003112500174NM 2003 11 25 SWAA032471 120031109A25606547654 PANEL BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 CAPT'S EMERGENCY ESCAPE ROPE DOOR WOULD NOT OPEN. TEMP REPAIRED TRIM PANEL PER MX NOTE. 2L72 4F RTA16WE 20031202001182003120200118SO 2003 12 2 SIMA200330202 120031029A27503631001005 FCU EMB 135 EMB135KL 3260302SO AVIONIC BAY FAILED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21830AE 145615 DURING FLIGHT CREW REPORTED A FLAPS FAIL MESSAGE ON EICAS AND FLAPS STUCK IN THE FIVE DEGREE POSITION. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040121000402004012100040NM 2004 1 21 03FDEA02306 120031227A5744ARC74801 FITTING DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING INBOARD FLAP VANE INBOARD SUPPORT FITTING INBOARD & OUTBOARD MOUNT HOLES WORN. COMPLIED WITH FEDEX EA 1-5750-75205. TRAILING EDGE AND TRAILING EDGE DEVICES. LT AND RT INBOARD. FLAP VANE ATTACH FITTINGS REWORK. 2L73 4F RTA22WE 20030128000552003012800055SW 2003 1 28 HEEA083809 120030116A30402314M2218 ARM BELL 407 407 1182206SW WINDSHIELD WIPERCORRODED E O OTHER O OTHER NRNOT REPORTED 1 SW03 WINDSHIELD WIPER ARM HAS CORROSION. 1G71 3U O H2SW 20030128002452003012800245SW 2003 1 28 HEEA083893 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030204000132003020400013CE 2003 2 4 MGO2003F00000 120030103A1430 RIVET BEECH 36 A36 1151604CE CONT O550 IO550* SO RUDDER MISSING B MGORK NONE O OTHER ININSP/MAINT 1 CE091072F791 E3002 DURING ANNUAL INSPECTION OF AIRCRAFT. FOUND MISSING RIVETS FROM THE RUDDER UPPER HINGE REINFORCEMENT BRACKET. 2 EACH RIVETS APPEAR TO HAVE BEEN MISSING SINCE DATE OF MFG. 1L71 3O3 O 3A15 E3SO 20030206001392003020600139EA 2003 2 6 COMA0360078 120030201A2750855D1007 BPSU CNDAIRCL600 CL6002B19 1900309EA R/H UNRELIABLE A COMAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 SO01912CA11480 7011 FLIGHT 9499 FLAPS FAILED CAUTION MESSAGE.REPLACED THE R/H BPSU. 2L72 4F RTA21EA 20030207001332003020700133NM 2003 2 7 QXEA0300004 120030102A2530JA010001 COFFEEMAKER DHAV DHC8 DHC8202 2809007NM GALLEY MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09350PH 488 SEA ON FLIGHT 2170- BURNING SMELL EXPERIENCED IN GALLEY IN THE COFFEE WARMER AREA. REMOVED AND REPLACED NR 1 AND 2 COFFEE JUGS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030212000892003021200089NM 2003 2 12 CALA0300040 120030211A5320 WEB BOEING737 7373Q8 1384670NM STA 1119-1125 PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914384 26313 INSPECTION FOUND THREE PUNCTURES IN HORIZONTAL BEAM WEB AT STA 1119-1125, LBL 18, WL 264. THE PUNCTURES WERE REPAIRED IAW SRM 51-70-13, FIGURE 1 AND 51-40-02, FIGURE 3. 2L72 4F RTA16WE 20030214000812003021400081WP 2003 2 14 ASAA0380053 120030105A5753593591929 RUB STRIP DOUG DC9 DC983 3022083WP T/E FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT WING FLAP FLEX JOINT UPPER PANEL CHAFE STRIPS WORN. REPLACED RUB STRIP PER SRM 51-10-2 AND 51-10-4. (M) 2L72 4F RTA6WE 20030214001032003021400103NE 2003 2 14 0302061 220030206A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE MALFUNCTIONED A UHLAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 NE03146SD 146SD 1835 PILOT REPORTS, DEPARTED PIT CLIMBING 1000 FT-2000 FT, HAD ERRATIC TORQUE INDICATOR 80-90 PERCENT, ITT STAYED SAME, NG FLUCUATED 2-3 PERCENT , PROP RPM 1270-1150. LEVEL FLIGHT AT 3000 FT, PULLED PL TO 50 PERCENT, NO ERRATIC INDICATIONS. ADVANCED PL ERRATIC INDICATIONS CONTINUED, SHUT DOWN ENGINE. TIME FROM SHUT DOWN TO LANDING WAS REPORTED APPROX 7 MINS. 2L72 4T4 TRTA52EU E8NE6 20030220000532003022000053NM 2003 2 20 ABXA030053 120030131A335020131A BATTERY BOEING767 767281 1385109NM CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23768AX 22786 EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERY ASSEMBLY IAW B767 MM. OPS CHECKED GOOD. 2L72 4F RTA1NM 20030116002682003011600268NM 2003 1 16 ABXA030031 120030106A335020131A BATTERY PACK BOEING767 767200 1385120NM GE CF6 CF680 30025NE CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23775AX 22790 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED SPARE BATTERY PACK FOR EMERGENCY LIGHTS. OPS CHECKED GOOD IAW MM. 2L72 4F4 FRTA1NM E13NE 20030117000542003011700054SW 2003 1 17 HEEA083173 120030108A6330 BUSHING BELL 206 206L3 1182108SW MOUNT ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 MAIN ROTOR TRANSMISSION MOUNT BUSHINGS WORN. REPAIRED. 1G71 3U H2SW 20030117001042003011700104NM 2003 1 17 UPS03440015 120030106A5210 BEAM BOEING747 747259B 1384804NM NO.2R DR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C NO.2R DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED & INSTALLED AS PER SRM 52-10-02 FIG.10. 2L74 4F RTA20WE 20030221000612003022100061NM 2003 2 21 QXEA0300185 120030126A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 8 SEAT TRACK HAS SCRATCHES AT STATION 474-486. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030224000502003022400050NE 2003 2 24 HEEA084171 120030212A62107615009100049A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH11657 760224 MAIN ROTOR BLADE TITANIUM LEADING EDGE HAS A COMPLETE CHORDWISE CRACK WITH SEPARATION BEYOND LIMITS. 1G72 3U H1NE 20030227000662003022700066CE 2003 2 27 NSVA200300014 120030226A5200 DOOR BEECH 1900 1900D 1154162CE A NSVAK NONE O OTHER UKUNKNOWN 1 EA27240CJ UE40 LGA: Passenger door sticking. MX lubricated exterior release switch on door with LPS Type 1. 2L72 4T RTA24CE 20030228000332003022800033EA 2003 2 28 COMA0360124 120030226A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01403CA 7428 FLIGHT 5715 FLAPS FAIL CAUTON MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2L72 4F RTA21EA 20030303001332003030300133SW 2003 3 3 HEEA084557 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 6343 33113 MAIN ROTOR BLADE EROSION SHIELD ON LOWER SIDE HAS SOME SEPARATION AND LIFTING. 1G72 4U H4SW 20030306000232003030600023 2003 3 6 HEEA084736 420030217A2340 SWITCH BELL 412 412 1182202SW INTERPHONE BOX DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 8008790 33076 NR 1 FM WILL NOT SHUT OFF. FOUND SWITCHES S5, S7, S8, S9, VOLUME AND SELECTOR KNOB AND VOLUME CONTROL R72 BAD. ALSO SWITCH S1 NOISY. REPLACED SWITCHES, VOLUME CONTROL AND VOLUME AND SELECTOR KNOBS AND CLEANED SWITCH S1. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030307001932003030700193 2003 3 7 HEEA084910 420030228A3457N0002000 GPS SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 GPS SYSTEM WON'T ACKNOWLEDGE ARM. 1G72 3U H1NE 20030310000232003031000023SW 2003 3 10 HEEA084932 120030227A6520204040604005 COUPLING BELL 412 412 1182202SW T/R GEARBOX CORRODED E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03107X 8061 A105 33113 TAIL ROTOR GEARBOX LEAKING OIL. REPAIRED. REPLACED OUTER COUPLING DUE TO PITTING. 1G72 4U H4SW 20030310000722003031000072SW 2003 3 10 HEEA084976 120030227A6710 BEARING BELL 412 412 1182202SW UNIVERSAL WORN E O OTHER O OTHER NRNOT REPORTED 1 SW037128R SW478 36007 COLLECTIVE UNIVERSAL HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030310001462003031000146WP 2003 3 10 EIA2003048 120030305A2700UNK PUSHROD TUBE DOUG DC9 DC933F 302207AWP A EIAAK NONE O OTHER ININSP/MAINT 1 NM09944F 47194 INTEERCONNECT TUBE BETWEEN PILOT AND COPILOT HAS SEVERE GOUGHING ON LEFT UPPER SIDE' RH UPPER SIDE SLIGHTLY GOUGED DUE TO BOLT LENGTH OF CENTER PEDESTAL AND PANEL INSTILLATIONREPAIRED AS PER ECRA 944-27-161-2 INTERCONNECT TORQUE TUBE REQUIRED SPLICE. CUT TORQUE TUBE PER bwn SRO 9278001 USING DOUGLAS PROVIDED CUTTER FROM 5327-288 KIT1, SHR1 REV A OF DWG SRO 927-8001 INSTALLED REPAIR SPLICE SLEEVE AS PER SRO 9278001 2L72 4F A6WE 20030313001902003031300190WP 2003 3 13 AALA20030153 120030204A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21286AA 49298 DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 13D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT PIGTAIL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030121001332003012100133GL 2003 1 21 HEEA083304 220030109A753223005366 BLEED VALVE BELL 206 206L1 1182107SW ALLSN 250C 250C28 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032759U 45272 LOUD BANG FROM COMPRESSOR ON TAKEOFF FOLLOWED BY 4 MORE BANGS. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 U H2SW E1GL 20030122001162003012200116NM 2003 1 22 375PA0009 120030114A3350 WIRE BOEING737 737317 138447PNM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 Several emergency exit lights out. Repaired wiring on lights per WDM Chpt. 20. Ops chk OK. 2L72 4F RTA16WE 20030314001812003031400181SO 2003 3 14 000239 120030124A3310 CIRCUIT BREAKER EMB 145 EMB145 3260210SO READING LIGHT BURNED A CHQAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL11263 COCKPIT READING LIGHT CIRCUIT BREAKER POPPED WITH SMOKE/ODOR IN COCKPIT. DISASSEMBLED AND INSPECTED CAPTAINS AND F/OS READING LIGHT. FOUND NO SIGNS OF HOT SPOTS OR SHORTS. 2L72 4F RTT00011AT 20030319000152003031900015 2003 3 19 GTIA030017 420030126A2565 SLIDE DOUG DC9 DC982 3022082WP PAX DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FLT 1108- LAS - L-1 DOOR SLIDE PACK FELL OFF DOOR. REINSTALLED SLIDE PACK ASSEMBLY PER MD 80 MM 25-62-00. (M) 2L72 4F A6WE 20030319000232003031900023WP 2003 3 19 GTIA030044 120030205A2420696233B CSD DOUG DC9 DC982 3022082WP NR 2 FAILED A GTIAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL23823NK 48020 FLT 779 - LGA - IN CRUISE AT 35,000 FEET NEAR WILMINGTON NC, LOST ALL ELECTRICAL POWER. SELECTED EMERGENCY POWER DECLARED EMERGENCY, BEGAN DIVERSION TO MYR. PERFORMED QRH PROCEDURES GOT LEFT GENERATOR ON LINE, HAD X-TIE LOCKOUT. LANDED SUCCESSFULLY IN MYR. PRIOR TO LOSS OF ELECTRICAL, HEARD AND FELT LOW RUMBLE AND VIBRATION IN A/C. ALL ENGINE GEN VOLTS AND FREQS NORMAL. ALL ENGINE INDICATIONS NORMAL. NEVER ABLE TO GET RT GENERATOR ON LINE. REMOVED AND REPLACED NR 2 CSD IAW MD 80 MM 24-10-01 SERVICED CSD AND CAVITY OPS AND LEAK CHECK GOOD. (M) 2L72 4F A6WE 20030326000712003032600071EU 2003 3 26 CA030207003 120030205A3297 WIRE PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL MLG BROKEN W L ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CA (CAN) ON APPROACH, LANDING GEAR WAS SELECTED DOWN AND CREW REPORTED NO GREEN LIGHT SHOWING LT MLG WAS DOWN AND LOCKED. UPON CONSULTATION WITH MAINT, DECIDED TO FLY BACK TO BASE. GEAR WAS CYCLED TWICE IN ATTEMPTS TO OBTAIN THE DOWN AND LOCKED LIGHT, CREW COULD VISUALLY SEE GEAR DOOR WAS DOWN. A FLY BY WAS CARRIED OUT THAT CONFIRMED GEA R APPEARED TO BE DOWN, BUT AS A PRECAUTIONARY MEASURE THEY CONTINUED TO BURN OFF THEIR FUEL. AIRCRAFT LANDED SAFELY AND WAS TOWED OFF RUNWAY AFTER THE ACTUATOR WAS LOCKED EXTERNALLY BY MAINTENANCE. UPON INSPECTION A BROKEN WIRE WAS FOUND IN THE CONNECTOR PLUG THAT ATTACHES TO THE ACTUATOR. WIRE WAS REPAIRED, GEAR SWINGS CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030324001062003032400106 2003 3 24 AWXA200300098 420030131A344146657602 COMPUTER AIRBUS320 A320232 3930326EU ADIRU FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28647AW 3419 762 PHX - AIR TURN BACK - FLT 0014 - AFTER TAKEOFF FROM PHX EN ROUTE TO JFK, MAXIMUM OPERATING LIMIT SPEED (VMO/MMO) ALERT WOULD SOUND AND REMAIN ON IN ACCESS OF 240 KNOTS, AND EXTINGUISH AT 230 KNOTS. NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) DISPLAYED ERRONEOUS VMO INDICATION ON PRIMARY FLIGHT DISPLAY. TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED NR 1 ADIRU IAW AWA T/C R2A34304, OPERATIONAL CHECK IS GOOD. VENDOR BENCH TEST OF ADIRU S/N 3419 CONFIRMED FAILURE OF UNIT. REPLACED AIR DATA RESOLVER PCB ASSEMBLY, CALIBRATED AND TESTED IAW CMM TP1011 REV 22. 2L72 4F RTA28NM 20030417001022003041700102WP 2003 4 17 UPS03840134 120030202A3233 ROD DOUG DC8 DC871F 302199DWP RT MLG ACTUATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 RT MAIN LANDING GEAR RETRACT ACTUATOR HAS CORROSION ON ROD END, JAM NUT & LOCK TAB WASHER ROD END CONDITION UNKNOWN. REPAIR PER EO DC8-3230-3958-D PARTS ON ORDER, ACTUATOR AND ROD END ASSY. REMOVED AND REPLACED MLG ACTUATOR IAW MM 32-32-02. 2L74 4F RT4A25 20030421000162003042100016EA 2003 4 21 QXEA0300304 120030225A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09604QX 10019 PDX ON FLIGHT 2490- FORWARD CARGO CHIMNEY IS DAMAGED. REMOVED AND REPLACED OVERHEAD CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030417001752003041700175WP 2003 4 17 ZW0A0302001 120030211A335060030451LB BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13984TW 53634 THE EGRESS LIGHT WAS INOPERATIVE AT THE FWD EMERGENCY EXIT AND 5 ROWS FORWARD. REPLACED THE BATTERY PACK AT ROW 16. CHECK-C 12-17-02 STL. 2L72 4F RTA6WE 20030421000852003042100085NM 2003 4 21 DL76S030111 120030127A5753 SKIN BOEING767 767332 1382001NM RT WING TE FLAP DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27116DL 23275 RIGHT INBOARD AFT FLAP DISBONDED. REPAIRED PER ER/A 418200-14. 2L72 4F RTA1NM 20030327001332003032700133SO 2003 3 27 C2XA03CL071 120030317A3230355022002MOD2 CONTROL UNIT EMB 145 EMB145ER 3260211SO COCKPIT FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716944 145045 ROC FLIGHT 2160 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT ON CLIMBOUT. THE AIRCRAFT RETURNED TO ROC AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030721000132003072100013 2003 7 21 AUS20030569 420030606A34601762000101 FMC BOEING737 737* NM GE CFM56 CFM56* 13802NE COCKPIT FAULTY W O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 AUS (AUS) BOTH FLIGHT MANAGEMENT COMPUTERS (FMC) FAILED. INVESTIGATION ANDTESTING COULD FIND NO FAULT. 2L72 4F4 FRTA16WE E2GL 20030722000032003072200003NM 2003 7 22 2003F00431 120030307A5330 SKIN BOEING727 727222 1384073NM FUSELAGE LIGHTNING STRIKEA RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND LIGHTNING STRIKE AT FUSE CROWN, BS 718 STRINGER 3R. DRILLED OUT LIGHTNING STRIKE ON FUSELAGE CROWN, BS 718, STRINGER 3R, AND INSTALLED FASTENER. (M) 2L73 4F A3WE 20030422001102003042200110SO 2003 4 22 SIMA200305010 120030130A534714530659011 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 ABI - DURING IMBV INSPECTION A LEVEL 2 FINDING FOUND, LEFT LOWER FORWARD NR 1 SEAT TRACK CORRODED AROUND HARDWARE. REMOVED AND INSTALLED LEFT LOWER NR 1 SEAT TRACK IAW EMB 145 SRM 53-01-06. (M) 2L72 4T RTT00011AT 20030423001882003042300188NM 2003 4 23 VNAA0303009 120030307A5220 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY EXIT FAILED A VNAAO OTHER O OTHER CRCRUISE 1 GL07433JS 3047 EN ROUTE, THE EMERGENCY DOOR WARNING LIGHT WAS DISPLAYED. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO RIC. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND ADJUSTED THE PROXI SENSOR AND THE DOOR LOCK SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030321000112003032100011NM 2003 3 21 2003UALA00164 120030211A5313 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29954UA 26739 CABIN RT CREASE BEAM WEB CORRODED BETWEEN BODY STATION 727B AND BODY STATION 727C. MAJOR REPAIR ACCOMPLISHED. REPLACED RT CREASE BEAM WEB. 2L72 4F4 FRTA16WE E2GL 20030827000852003082700085SO 2003 8 27 C2XA03CL143 120030807A335078241 INVERTER EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717524 145399 CLE FLIGHT NR 2138 THE CREW REPORTED THE FRONT EMERGENCY LIGHT DID NOT ILLIMINATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030827001322003082700132NM 2003 8 27 CALA0300427 120030730A5347 SEAT TRACK BOEING777 777224 1385225NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776010 29480 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1513, RBL 74. THE SEAT TRACK WAS REPIARED IAW SRM 53-00-52, REPAIR 3. 2L72 4F RTT00001SE 20030827001712003082700171SO 2003 8 27 C2XA03SH303 120030827A532014521700003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE RAMP ANGLE ON THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 18 AND 19 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030828001352003082800135NM 2003 8 28 MEX2003283 120030711A2997 WIRE DOUG MD88 MD88 3023688NM HYD SYSTEM DAMAGED A ASMFO OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SW23160PL 49763 FLT 109 - TIJ-MEX - AIRCRAFT ARRIVED WITH CAPTAIN REPORT 'BREAKER S-27 OF LEFT HYDRAULIC ENGINE PUMP WAS OUT OF SERVICE'. DURING REVISION WAS DETECTED WIRING OF LAMP BETWEEN BACK CABIN AND RESTROOMS GROUNDED. THE WIRING WAS REPAIRED IAW WDM 29-11-02, ALL TESTS CORRECT. DURING OVERNIGHT SERVICE LINES AD3D18 OF PLUG RE-1223 PIN K, F948A18 OF PLUG R5-1223 PIN M AND 2J3D18 OF PLUG R5-1224 PIN R WERE COVERED WITH THERFIT IAW WDM 29-11-02, 30-31-01 AND 74-11-00, ALL CORRECT. (M) 2L72 4F RTA6WE 20030723001292003072300129NM 2003 7 23 AWXA200300692 120030612A33503114981 REFLECTOR BOEING737 7373Y0 1384671NM BS INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING INSPECTION THE EMERGENCY EXIT LIGHT ON LT SIDE OF FUSELAGE, AFT OF WING TRAILING EDGE WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SOCKET ON EMERGENCY EXIT LIGHT, LT SIDE OF FUSELAGE, AFT OF WING TRAILING EDGE. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031204000872003120400087WP 2003 12 4 UPS03841397 120030908A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, R2 AFT SERVICE DOOR HAS CRACK INDICATION AT UPPER AFT CUTOUT CRACKED AREA IAW DC8 SRM 53-2-0 FIG 16, TR 53-130 & TR53-156 PERFORMED HFEC IAW MD NDT SPM 06-10-01.001 NO CRACKS NOTED. REMOVED INTERCOSTAL ABOVE R2 DOOR, 2 EA CLIPS, TOP AFT DOOR STOP FITTING. OPENED R2 DOOR TORQUE BOX WEB. FABBED DOUBLERS AND TRIPLERS AND REPAIRED DOOR FRAME RE-ASSEMBLED FRAME IAW DC8 SRM 53-2-0 FIG 16, TR53-130, TR53-156. 2L74 4F RT4A25 20031208000602003120800060EU 2003 12 8 03FDEA01797 120031024A5720A5381131920095 ANGLE AIRBUS310 A310203 3930313EU ZONE 100 MISREPAIRED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25442FE 353 LEFT WING RIB NR 40 HAS 24 EA EXISTING HOLES THAT IS ( 2-AND) OVERSIZE IN FRAME 40. PICKUP ANGLE C/T FUEL TANK EO6-5310-7-5003 WORK INSTRUCTION - DRILL HOLES TO THE (1ST) OVERSIZE. COMPLIED WITH WORK CARD (EA6-5310-7-5003 02 PT3) , EA6-5310-73418, EA6-5310-73418A, EA6-5310-73418B AND NRC (SOOO24) AT CWF. BY DRILLING ALL FASTENER HOLES AND PICKUP ANGLE TO CORRECT SIZE AND INSTALLING ON A/C, AND INSTALLING ALL NEW FASTENERS IAW ENGINEER FASTENER CALLOUT SHEET REVISION (C). 2L72 4F RTA35EU 20031209000852003120900085 2003 12 9 SWAA032351 420031025A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031208000852003120800085SO 2003 12 8 C2XA03CL177 120031023A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715932 145015 CLE FLIGHT 2163 THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. 2L72 4F RTT00011AT 20031210000542003121000054SO 2003 12 10 C2XA03SH473 120031123A532014522178005 THRESHOLD EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040123000652004012300065NE 2004 1 23 MDR03022 120030728A6210641520201049 BLADE SKRSKYS64 S64E 8142604NE MAIN ROTOR CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09CGJZK13637 64003 THE BLADE WAS REMOVED FROM THE AIRCRAFT FOR BIM INDICATION. A 10-DAY LEAK CHECK WAS PERFORMED AND A LEAK WAS FOUND IN A CRACK IN NR 18 POCKET. AFTER THE POCKET WAS REMOVED AND ADHESIVE WAS CHEMICALLY REMOVED, THE CRACK WAS FOUND 168.75 INCHES FROM THE ROOT END AND 9.50 INCHES FROM THE LEADING EDGE ON THE BOTTOM SIDE OF THE BLADE. THE CRACK IS APPROXIMATELY 3 INCHES LONG AND WRAPS AROUND THE TRAILING EDGE RADIUS TO THE BACK WALL OF THE SPAR. CAUSE: UNKNOWN 2G72 4U H4EA 20040127001562004012700156NM 2004 1 27 ASAA0310201 120030321A53306545771 DOUBLER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND DOUBLER AT BS 727, STRINGER 19R CORRODED. REMOVED AND REPLACED DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20040127001732004012700173NM 2004 1 27 ASAA0310223 120030325A5313BAC15032731 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND BLADE SEAL ANGLE AT BS 616-639, STRINGER 2 RT CORRODED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031211001042003121100104CE 2003 12 11 AMWA68 120031024A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07174YV UE174 6 CRACKS ON THIS RIB. 3 ON LT AND 3 ON RT SIDES AT STRINGER TO RIB INTERSECTION. CRACKS LOCATED AT FIRST RIVET HOLE. LT STRINGER P/N 101-640000-37, 101-640000-39, 101-640000-45. RT STRINGER P/N 101-640000-38,101-640000-46, 101-640000-42 2L72 4T RTA24CE 20030923001932003092300193WP 2003 9 23 AALA20030852 120030813A3350P2010031303 LIGHT DOUG DC9 DC982 3022082WP AFT STAIRS BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW217532A 49924 DURING OVERNIGHT MAINTENANCE, AFT STAIR AFT WALL EMERGENCY EXIT LIGHT BROKEN. REPLACED EMERGENCY EXIT AFT STAIR AFT WALL LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040130000302004013000030NM 2004 1 30 SWAA032823 120031228A53106545410 BEAM BOEING737 7373A4 1384585NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRECKED AT BS 663, BL 0, WL 208. REPAIRED BEAM PER BFG ER. 2L72 4F RTA16WE 20040203000762004020300076NM 2004 2 3 ASAA0310526 120030909A33508821004 BATTERY PACK BOEING737 737210C 1384459NM ROW 11 DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 ANC - FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 11. REPLACED REMOTE ASSEMBLY RECEIVER P/N 88-3-2003-1-2, AND BATTERY PACK, THEN LIGHTS OPERATED NORMAL. (M) 2L72 4F A16WE 20040204000432004020400043NM 2004 2 4 S03253067 120030814A5330 SKIN BOEING747 747200 1384847NM PWA JT9 JT9D7R4G2 52054NE FUSELAGE CRACKED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 22299 FUSELAGE SKIN CRACK BETWEEN FASTENER HOLES AT BS 2060,STRINGER-26R. REPAIR IAW SRM 53-30-03,FIGURE1. SUBMIT THE CRACKED SKIN TO MFG FOR ANALYSIS. 2L74 4F4 FRTA20WE E3NE 20040210000492004021000049NM 2004 2 10 QXEA200301493 120031120A5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- FLOOR SUPPORT ANGLE IS CORRODED ABOVE FORWARD END OF MAIN CABIN DOOR LAYSHAFT. REPAIRED IAW DHC-8 SRM 51-20-11. 2H72 4T RTA13NM 20031215000042003121500004NM 2003 12 15 AWXA200301440 120031104A5320564797322 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MINOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN SHEAR WEB BETWEEN BS 616 AND BS 618, RBL 63.5, WL 208. MAINTENANCE REMOVED CRACKED SHEAR WEB BETWEEN BS 616 AND BS 618, RBL 63.5; INSTALLED A NEW REPLACEMENT SHEAR WEB IAW SRM 51-40-02 PG 1, 26, 29 & 32 FIG 3-4 & 6-7. 2L72 4F RTA16WE 20030902001522003090200152EA 2003 9 2 SWIA200312164 120030630A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07929SW25 25 7703 STAB TRIM CHANNEL 1 FAILED TO ENGAGE AFTER AIRCRAFT POWER UP. REPLACED HSTCU COMPUTER. OPS CHECK GOOD IAW RJ MM 27-41-01 2L72 4F RTA21EA 20030904001142003090400114EA 2003 9 4 QXEA200300964 120030809A5520 ELEVATOR CNDAIRCL600 CL6002C10 1390015EA RIGHT LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 PDX- LIGHTNING STRIKE DAMAGE TO RIGHT HAND ELEVATOR. REPAIRED IAW HORIZON AIR EA R-27-81B AND REO 670-55-21-004. 2L72 4F RTA21EA 20030904002072003090400207EA 2003 9 4 SWIA200312182 120030711A3350365271 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07405SW 7029 EMERGENCY EXIT LIGHT NEXT TO PAX DOOR INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT ASSY. OPS CHECK GOOD. P/N: 36527-1 2L72 4F RTA21EA 20030812000622003081200062 2003 8 12 HEEA088518 420030713A3455066104701 TRANSCEIVER BELL 412 412 1182202SW ADF INTERFERENCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 ADF TRANSCEIVER RECEIVES WITH EXCESSIVE STATIC. IN SHOP REPAIR. 1G72 4U H4SW 20030813001762003081300176 2003 8 13 SWAA031686 420030728A2565D31354 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030825001162003082500116NM 2003 8 25 ABXA030194 120030610A5414311T14002 PANEL BOEING767 767281 1385109NM NR 1 NACELLE GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23796AX 23146 DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 1 ENGINE STRUT RIGHT SKIN PANEL NEAR AN ACCESS DOOR CUTOUT. MAXIMUM DEPTH OF BLEND OUT REQUIRED TO COMPLETELY REMOVE DAMAGE WAS 0.035 INCH. REPAIRED AREA IAW REA B654-46243MR. 2L72 4F RTA1NM 20030909002502003090900250WP 2003 9 9 AMTA200300833 120030626A5313 STRINGER LKHEED1011 10113853 5265020WP FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 IMPROPER STRINGER REPAIR FOUND. REMOVED REPAIR AND INSTALLED STRINGER SECTION IAW SRM 51-40-01. (M) 2L73 4F A23WE 20030911000012003091100001NM 2003 9 11 UPS03541075 120030806A2910 HYDRAULIC SYSTEM BOEING757 75724APF 1384969NM RIGHT OVERSERVICED A IPXAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01447UP 27736 INSPECTION TYPE:N/A RIGHT PACK EMITS STRONG ODOR. LT PACK WAS TURNED OFF AROUND 2000 FT ON CLIMB OUT. ODOR STARTED AND PACKS WERE SWITCHED TO LT PACK ON AND RIGHT PACK OFF. AT CRUISE, LT PACK WAS TURNED OFF AND RT PACK ON . ODOR STARTED AGAIN AND RT TURNED OFF AND LT PACK ON FOR REMAINDER OF FLIGHT. LOWERED RIGHT SYSTEM HYD RESERVOIR DUE TO OVERSERVICE OF SYSTEM. THIS CLEARS DEF M264268 FOR RIGHT PACK SKYDROL ODOR - NO LONGER EXISTS. RE FERENCE LOG PAGE 043621 2L72 4F RTA2NM 20030911001972003091100197WP 2003 9 11 AALA20030436 120030228A5320 SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW219615W 53562 MCI - AFT LOWER SUPPORT BETWEEN MLG WHEEL WELL CRACKED, LEFT SIDE, FS 977. REPLACED CRACKED PART WITH NEW PART CPN NR 4057240. INSTALLED PER SRM 51-30-2, SRM 51-30-5, TREATED PART PER SRM 51-10-3. (M) 2L72 4F RTA6WE 20030910001082003091000108WP 2003 9 10 MWEA030364 120030907A5330592081423 DOUBLER DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 CORROSION FOUND ON COVER PLATE AND ON FUSELAGE. REMOVED AND REPLACED REPAIR DOUBLER. 2L72 4F A6WE 20030911002472003091100247WP 2003 9 11 DHL2003604604 120030527A5754 VANE DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING EXTENDED LE OB VANE HAS SEVERAL ELONGATED HOLES AND INTERIM REPAIR AT STA XOLDO 67. REMOVED FASTENERS. REMOVED THE EXISTING INTERIM REPAIR IAW EO DHL 030558, ED-3351. CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL REPAIR DOUBLER AN INTERNAL DOUBLER AND A FILLER IAW EO DHL 030558, ED-3351. CLEANED TREATED & PRIMED THE REPAIR DOUBLER INTERIOR SURFACE INTERNAL DOUBLER & FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED EXTERNAL DOUBLER, INTERNAL DOUBLER, FILLER ON RT WING EXTENDED L/E OTBD VANE, STA XOLDO 67.000, USING NEW FASTENERS. 2L74 4F RT4A25 20030912000012003091200001NM 2003 9 12 03FDEA01296 120030813A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 EMPENNAGE- HORIZONTAL STABILIZER BARREL NUT HOLE 36R CORROSION BEYOND A LIMIT. EMPENNAGE- HORIZONTAL STABILIZER BARREL NUT HOLE 36R REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71801 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030926000572003092600057EA 2003 9 26 COMA0360385 120030824A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAC ABORTED TAKEOFF JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 SO01914CA7698 7012 FLIGHT 5188 FLIGHT SPOILERS CAUTION MESSAGE DURING TAKE OFF. REPLACED THE NR 2 SECU. 2L72 4F RTA21EA 20030926000822003092600082NM 2003 9 26 AWXA200300999 120030828A2432279202 CHARGER BOEING737 73733A 1384673NM BATTERY FAULTY A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28166AW53972 23627 ON CLIMB OUT OF PHX EN ROUTE FOR SFO FLIGHT ATTENDANTS DETECTED AN ODOR IN CABIN LIKE BURNING HAIR, TURNED BACK TO PHX. MAINTENANCE T/S AND FOUND D2936 BATTERY PROTECTION CIRCUIT OPEN, REPAIRED CONNECTION AND REMOVED AND REPLACED MAIN BATTERY AND BATTERY CHARGER IAW BMM, T/C A1B24004, T/C A2A24001. BURNING ODOR WAS A RESULT OF THE BATTERY OVERHEATING.VENDOR FUNCTIONAL TEST OF BATTERY CHARGER CONFIRMED FAILURE OF UNIT FOR FAILING OHM OUTPUT TEST. FOUND DIODES CR1 AND CR6 DEFECTIVE. REMOVED AND REPLACED DIODES CR1 (P/N 1N1184A) AND CR6 (P/N 1N1184RA). TESTED UNIT AND RETURNED TO SERVICE. 2L72 4F RTA16WE 20030926001262003092600126WP 2003 9 26 DHL2003802011 120030830A5280 DOOR DOUG DC8 DC873 302199CWP RT MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH 46076 RIGHT MAIN GEAR DOOR HAS CRACK PROPAGATING FROM RIVET B.S. 860 12 INCHES FROM OUTBOARD RADIUS. CRACK .5 INCHES LONG. STOPPED DRILLED CRACK. INSTALLED A DOUBLER REPAIR IAW SRM 52-2-3. 2L74 4F RT4A25 20031002000242003100200024WP 2003 10 2 GTIA030672 120030827A5340 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND AFT PIT CORRODED ANGLE AT FS 1155 4 INCHES RBL AND 1 CORRODED FASTENER AT FS 1145, SHORT FRAME, 4 INCHES RBL. AFTER FURTHER INSPECTION DISCOVERED FLOOR SUPPORT STATION 1148 4 INCHES RBL CRACKED. REMOVED FLOOR SUPPORT RECEIVED NEW FLOOR SUPPORT FITTING. INSTALLED NEW SUPPORT FITTING. (M) 2L72 4F A6WE 20031002001722003100200172NM 2003 10 2 252TR0010 120030912A7930 WARNING LIGHT BOEING737 737228 13844AGNM ENGINE OIL ILLUMINATED A PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05252TR 23001 OIL FILTER BYPASS LIGHT NR 2 ILLUMINATED ON GROUND IN TAKE OFF PRIOR TO 80KTS. CHECKED MAIN ENGINE OIL SCREEN, NO CONTAMINATION FOUND. RAN AND LEAK CHECKED OK PER MM 79-35-0. 2L72 4F RTA16WE 20030909000432003090900043SO 2003 9 9 C2XA03BT084 120030827A49304951960 HOUSING EMB 145 EMB145XR SO APU LEAKING A C2XAK NONE K FLUID LOSS UKUNKNOWN 1 SW2711107 654 EWR LOG BOOK SQUAWK MASSIVE FUEL LEAK. LOCATED LEAK ON APU FILTER. RED BYPASS BUTTON WAS LEAKING WHEN PUMP PRESSURE APPLIED. REMOVED AND REPLACED APU FILTER HOUSING. OPS AND LEAK CHECK GOOD IAW EMB145 MM 49-31-07. 2L72 4F RT 20030908002862003090800286NM 2003 9 8 SWAA031935 120030828A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSLEAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 639 RT SIDE. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031007000082003100700008 2003 10 7 GTIA030686 420030921A256529985107 SLIDE DOUG DC9 DC983 3022083WP PAX DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FOUND L-2 DOOR SLIDE PACK FELL FROM DOOR. REMOVED AND REPLACED L-2 SLIDE PACK. (M) 2L72 4F RTA6WE 20031014001212003101400121NM 2003 10 14 SWAA032171 120030927A3350BR9442 LIGHT BOEING737 7373H4 1384600NM FWD CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT DAMAGED AND LOOSE NEXT TO FWD F/A 'S SEAT. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20031020001762003102000176NM 2003 10 20 DL75A030811 120030904A2422100201021000 INVERTER BOEING757 757212 1384951NM E/E BAY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27751AT 23125 STANDBY INVERTER INOP. REPLACED STANDBY INVERTER. 2L72 4F RTA2NM 20031021001992003102100199WP 2003 10 21 GTIA030705 120030910A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND PAX CABIN LEFT SIDE AFT OF DOOR JAMB FS 207 LONGERON 11L SKIN WEB EAR IS CRACKED. REMOVED DAMAGED PART OF THE SKIN WEB. FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. (M) 2L72 4F A6WE 20031022000162003102200016EU 2003 10 22 AWXA200301066 120030921A2917C60AA0062 PRESSURE SWITCH AIRBUS320 A320232 3930326EU HYD SYSTEM FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28647AW21917 762 ON CLIMBOUT OF PHX EN ROUTE FOR SNA RECEIVED ECAM GREEN HYDRAULIC PUMP LOW PRESSURE INDICATION, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED GREEN HYDRAULIC SYSTEM ENGINE PUMP LOW PRESSURE SWITCH IAW AMM 29-11-17-04, AND GREEN RESERVOIR LOW LEVEL SWITCH IAW AMM 29-11-41-04. INSPECTED GREEN HYDRAULIC PUMP CASE DRAIN FILTER FOR DEBRIS, NONE FOUND. PERFORMED ENGINE RUN, SYSTEM LEAK AND OPERATIONAL CHECK WAS GOOD. FUNCTIONAL CHECK OF LOW LEVEL SWITCH FAILED LEAKAGE & INSULATION TESTS. TEARDOWN REVEALED DRIP STICK WIRING HAD SKYDROL SATURATION DAMAGE THAT WAS CAUSE OF FAULT. REPLACED DRIP STICK. UNIT MODIFIED & REPAIRED IAW CMM. 2L72 4F RTA28NM 20031023000142003102300014NE 2003 10 23 QEM2003F00000 220030918A72501767M32P03 TURBINE WHEEL GE BOEING777 777* UTILUSENM GE GE90 GE9090B NE LPT DAMAGED B QEMYO OTHER O OTHER NRNOT REPORTED 1 EA35 20549 P900230 900230 LPT BLADE LIBERATION, QTY 1 AT DISK SLOT NR 24. DISK POST SHOWS EVIDENCE OF HEAT EXPOSURE. BLADE RETENTION DOVETAIL HAS YIELDED ALLOWING BLADE LIBERATION. BLADE PLATFORM RECOVERED AND NO VISIBLE DAMAGE TO DOVETAIL. NO VISIBLE DAMAGE TO DOVETAIL. PARTS (DISK AND BLADES) RETURNED FOR FURTHER ELEVATION. 2L72 4F4 FRTT00001SEE00049EN 20031023000652003102300065SO 2003 10 23 C2XA03SH349 120030924A531514522461011 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 DURING C CHECK MAINTENANCE FOUND THE RT FLOORBEAM DOUBLER TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED PART IAW WITH EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031028000182003102800018NM 2003 10 28 UPS03441271 120030904A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT STA 2638 STR 8-9 SKIN CRACKED (ABOVE I/B ELEV). SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A. 2L74 4F A20WE 20031028001132003102800113EA 2003 10 28 ASOA03483 120031004A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 IAW ASA EO 600-53-0122. (M) 2L72 4F RTA21EA 20031028000942003102800094NM 2003 10 28 ASAA0240GGG 120030403A53116546533 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND FORWARD CARGO BAY FRAME CORRODED AT BS 500. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040210001072004021000107EU 2004 2 10 USAA030310 120031124A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED, FRAME 57.2 PLUS 10 INCHES LBL 17.75. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040205000472004020500047WP 2004 2 5 ASAA0380763 120031121A532099305383 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CUSP WEB IS CORRODED AT FS 505. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-10-3, 53-14-2, 53-01, 51-70-4, ET AL. (M) 2L72 4F RTA6WE 20040205001252004020500125NM 2004 2 5 HNAA0300073 120031126A2761A44700009 ACTUATOR DHAV DHC8 DHC8102 2809003NM SPOILERS FAILED A HNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA07936HA 145 LOST NR 1 HYDRAULIC, QUANTITY WHEN FIGHT/TAXI SWITCH SELECTED TO FLIGHT. REMOVED AND REPLACED INBOARD ROLL SPOILER ACTUATOR. 2H72 4T RTA13NM 20040205001402004020500140SW 2004 2 5 21200003 120031128A7603C810242 CONTROL CABLE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCB3T HCB3TN5 GL ZONE 400 CHAFED E D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW17228AM33082166 TC300 P54062 BVA7662 DURING TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWER LEVER CABLE HAD BROKEN INSIDE THE CABLE HOUSING IN THE ENGINE COMPARTMENT. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20040329000352004032900035WP 2004 3 29 ASAA0380387 120030421A5310993657813 SHEAR TIE DOUG DC9 DC982 3022082WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND SHEAR TIE AT FRAME 712 BETWEEN L30 AND L29. REPLACED SHEAR TIE PER SRM. (M) 2L72 4F A6WE 20040308001472004030800147NM 2004 3 8 ASAA0310228 120030326A5313655292843 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 19L AT BS 757 CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20031216000892003121600089EA 2003 12 16 03331664 120031127A2540AE0405A02 FAN CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAILED A VTZAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 EA27664BR 7528 DURING APPROACH TO FSD ON FLT NR 7654, CREW RECEIVED A LAVATORY TOILET SMOKE MESSAGE. CREW VERIFIED NO VISIBLE SMOKE IN THE LAVATORY. THE CREW COMPLETED THE ORH AND FLIGHT LANDED WITHOUT INCIDENT. THE LAVATORY FAN WAS IDENTIFIED AS THE CAUSE OF THE SMOKE AND DEFERRED UNTIL AIRCRAFT RETURNED TO ORD FOR MAINTENANCE. THE LAVATORY SMOKE FAN WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE LAVATORY FAN WAS ACCOMPLISHED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031217000162003121700016NM 2003 12 17 CALA0300659 120031121A5542 SKIN BOEING737 7373T0 1384582NM RUDDER LIGHTNING STRIKEA CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON RUDDER T/E APPROXIMATELY 30 INCHES BELOW STATIC WICK. REPAIRED IAW ECRA 5540-01171. 2L72 4F RTA16WE 20040427000532004042700053SW 2004 4 27 ERAA093706 120031001A6320412040123101 QUILL ASSY BELL 412 412 1182202SW TRANSMISSION WORN A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 4959 913 QUILL ASSY HAS VERTICAL PLAY IN SHAFT. SPACER SET DAMAGED FROM APPARENT BEARING ROTATION IN LINER OF SLEEVE. DISASSEMBLED, CLEANED AND VISUALLY INSPECTED ALL PARTS. CHECKED SHIMMING AND REASSEMBLED, TORQUED AND SAFTIED IAW BHT 412-CR, 0 CHAPTER 63 INSTALLING NEW SPACER SET, REPAIRED A SLEEVE ASSY AND ALL NEW O RINGS TSO 912-7. 1G72 4U H4SW 20040902001492004090200149CE 2004 9 2 2004F00256 120031218A323012430097 TRUNNION CESSNA210 T210N 2073456CE NLG CRACKED A IPMAO OTHER O OTHER LDLANDING 1 WP119371Y 21064490 NOSE GEAR COLLAPSED DURING LANDING ROLLOUT. DETERMINED TO BE CAUSED BY FAILURE OF THE UPPER TRUNNION ASSY NR 1243009-7. THE DRAG BRACE FAILED AT THE COLLAR AROUND THE STRUT TUBE. INDICATIONS OF INTERGRANULAR CORROSION ARE APPARENT AND PROBABLY CAUSED BY AN UNDETECTED CRACK. THIS AIRCRAFT IS SUBJECT TO DAILY TOWING. DETAILED INSPECTIONS INCLUDING PENETRANT INSPECTIONS OF THIS CASTING ARE RECOMMENDED. ADDITIONALLY MORE DETAILED INSPECTION OF THIS AREA IS RECOMMENDED FOR PREFLIGHT. (M) 1H71 3O 3A21 20050223001032005022300103EU 2005 2 23 ERAA097520 120030824A641010531980 BLADE BOLKMS105 BO105S 5626006EU TAIL ROTOR DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03152EH3657 S701 BLADE SENT TO AEC FOR REPAIR. REPLACED LEADING EDGE, REFINISHED BLADE, REPLACED ROOT TAPE. 1G72 3U H3EU 20030818000752003081800075 2003 8 18 HEEA088607 420030728A34427021450601 COMPUTER BELL 412 412 1182202SW RADAR SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 COMPUTER CAUSES INDICATOR TO LOSE FOCUS AND FADE AFTER 30 MINUTES. 1G72 4U H4SW 20030819000712003081900071EA 2003 8 19 COMA0370024 120030807A3240 THERMOCOUPLE CNDAIRCL600 CL6002C10 1390015EA BRAKE OVERHEAT CONTAMINATED A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01376CA 10092 BRAKE OVERHEAT WARNING, LEFT INBOARD BRAKE INDICATED 20. CLEANED CONTAMINATION FROM BTMS WIRING CONNECTOR. 2L72 4F RTA21EA 20030328000052003032800005NE 2003 3 28 CA030212009 120030207A62106117020201067 BLADE SKRSKYS61 S61N 8142104NE GE CT58 CT581402 30011NE MAIN ROTOR CRACKED W BA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) INBOUND FROM RIG, 'BIM' LIGHT ILLUMINATED. EMERGENCY CHECKLIST C/W. AIRCRAFT DIVERTED TO SABLE ISLAND FOR PRECAUTIONARY LANDING. COMM CENTRE ADVISED.POST S/D CHECK CONFIRMED PRESSURE BELOW LIMITS. 2G72 4U4 U 1H15 1E3 20030401001682003040100168WP 2003 4 1 DHL2003804778 120030214A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FWD ACCESSORY BAY FRAME CRACKED 1.00 INCH, STA. 55.000 L23R. PERFORMED MAJOR REPAIR IAW 53-2-0 PG. 20/21 FIG. 2 (SHEET 2)., REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 , SRM51-1-20D PG 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 PG. 20/21 SHEET 2 . FABRICATED NEW FRAME SEGMENT & SLICES IAW SRM53-2-0 PG. 20/21 FIG. 2 SHEET 2. HEAT TREATED IAW SRM 51-1-1 PG. 1-17 , SRM51-1-4, PG.1-3, DPS1-05.3, CLEANED , TREATED AND PRIMED IAW SRM53-2-0 PG.20/21 SHEET 2 , SRM51-1-21 PG. 1 , SRM51-1-20D PG. 9 FOR PNUE. DUCT R/R AND LEAK CK. SEE N/R 1834 2L74 4F RT4A25 20030820002082003082000208EA 2003 8 20 ASOA03315 120030716A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY CEILING LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMPS IN THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000922003040100092NM 2003 4 1 DHL2003747003 120030129A2612 FIRE DETECTOR BOEING727 727224 1384076NM NR 1 ILLUMINATED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01747DH 22253 FIRE PROTECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED, NR 1. PLACED ON MEL 26-9-1 DMI 11789. PLACARDS INSTALLED. REF DMI NR 11789 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. OPS CHECK NR 1 ENG FIRE DETECTOR, NO DEFECTS NOTED PER MM 26-11-001. THIS CLEARS DMI 11789. 2L73 4F A3WE 20030410002022003041000202WP 2003 4 10 GTIA030152 120030312A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DETERIORATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO STA 160 LBL 8 INCHES TO 44 INCHES (40X36) HAS SOFT/MUSHEY DETERIORATED AND INSERTS CORR. FABBED NEW CABIN FLOORBOARD STA 200-160 LBL 8 LBL 44. 2L72 4F4 FRTA6WE E2EA 20030414000332003041400033WP 2003 4 14 MEX2003074 120030314A2910 LINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE HYD SYSTEM LEAKING W ASMFO OTHER K FLUID LOSS NRNOT REPORTED 1 SW23803ML 49726 DURING OVERNIGHT SERVICE, A BLADE ON T4 (TURBINE STAGE) WAS DETECTED WITH DAMAGE. ENGINE WAS REPLACED IAW MM AND TESTS IAW MM, ALL CORRECT. DURING REVERSE TEST, A HYDRAULIC FLUID LEAK WAS DETECTED AND HYDRAULIC LINES WERE REPLACED. 2L72 4F4 FRTA6WE E2EA 20030408001002003040800100NM 2003 4 8 2003UALA00353 120030329A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 AFT PIT STA 1174 AND RBL 9, FRAME T-CAP CORRODED MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP WITH SPLICED SECTION 2L72 4F4 FRTA1NM E24NE 20030424001352003042400135EU 2003 4 24 MALA030207 120030324A3210 CONNECTOR SAAB SF340 340B 7860101EU MLG LOOSE A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15421XJ 340B421 DURING GEAR DOWN SELECTION ON FLIGHT 3240, LT MAIN GREEN LIGHT DID NOT ILLUMINATE. INTRANSIT LIGHT OPERATED NORMALLY, ATTEMPTED TO RECYCLE AND MANUALLY EXTEND GEAR STILL DID NOT GET LIGHT. EXECUTED NORMAL LANDING AND PINNED GEAR. MAINTENANCE FOUND CONNECTOR IN LT WHEEL WELL LOOSE. CLEANED AND RECONNECTED CONNECTOR. INDICATIONS CHECK GOOD. REPLACED EXPLOSIVE BOLTS P/N 117510-1 SN/OFF LT 1913, SN/ON 2891, RT SN/OFF 1914, SN/ON 2901 PER 32-34-15-2, PERFORMED GEAR CYCLES (FUNCTIONAL CHECKS PER 32-30-00 CHECKS GOOD.) 2L72 4T RTA52EU 20030424000542003042400054NM 2003 4 24 QXEA0300329 120030304A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - RIGHT HAND AFT FUSELAGE SKIN NICKED AFT OF SERVICE DOOR, FORWARD OF X704 AT STRINGER 19. REPAIRED IAW DHC-84 SRM 51-25-15, STEP 5, PARAGRAPH 3. 2H72 4T RTA13NM 20030430002002003043000200NM 2003 4 30 SWAA030926 120030425A57536546434 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT INBOARD AFT T/E FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED LT INBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030502000922003050200092SO 2003 5 2 C2XA03BT051 120030414A21302014AB MODULE EMB 145 EMB145 3260210SO COCKPIT FAULTY A C2XAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW2727962 145110 EWR---CO2306, CREW REPORTED AUTO PRESSURIZATION FAILURE IN FLIGHT. AFTER DUMPING QRH AND TAXIING TO MAINTENANCE COULD NOT GET PRESSURIZATION TO STABILIZE IN MANUAL MODE. MAINTENANCE REMOVED AND REPLACED CABIN PRESS ACQUISION MODULE (CPAM) IAW EMB145 MM 21-32-01. OPS CHECKED AND LEAK CHECKED GOOD IAW EMB145 MM 21-31-01 AND 34-13-00. AUTO AND MANUAL MODES OF PRESSURIZATION OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030502002002003050200200NM 2003 5 2 AWXA200300418 120030402A5320146N852238 WEB BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK INTERGRANULAR CORROSION WAS FOUND WEB AT STR 27 RT, BS 1340 TO BS 1360. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED LOWER SILL FORWARD WEB AT STR 27 RT, BS 1340 TO BS 1360; FABRICATED A NEW REPLACEMENT WEB, A REPAIR ANGLE AND SHIMS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-6 FIG 2. 2L72 4F RTA2NM 20030502002232003050200223NM 2003 5 2 EIA2003061 120030416A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE WORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 RIGHT FUSELAGE SKIN FS 2521-2598 WORN AT INTERFACE OF VERT STAB SEAL. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PARTS PER EO 53-747-1670-02 REV-A AND ECRA 471-53-218-2. 2L74 4F A20WE 20030502001172003050200117SO 2003 5 2 SWIA200311871 120030410A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07268UE5844 1432 120207 FLAP CONTROL FAULT IN CRUISE. ONE SEGMENT NAC FLASHING, REST OK. FLAP CONTROL FAULT WHEN 25 DEGREES OF FLAPS SELECTED AT APPROXIMATELY 15 DEGREES OF FLAPS, REMAINDER OK. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB120 MM 27-50-06. OPS CHECK GOOD. 2L72 4T RTA31SO 20030505000302003050500030NM 2003 5 5 2003UALA00364 120030407A3350 BATTERY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHTSBURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29670UA 29240 EMERGENCY LIGHTS INOP FROM SEAT 35 AB TO 41 AB. REPLACED EMERGENCY LIGHT BATTERY. 2L72 4F4 FRTA1NM E24NE 20030507000182003050700018EU 2003 5 7 AUS20030324 120030317A5753D5757126420101 DOUBLER AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE TE FLAP CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT OUTBOARD FLAP LOWER SURFACE EXTERNAL DOUBLER CONTAINED LEVEL 2 CORROSION LOCATED AT THE NO4 FLAP TRACK POSITION. FOUND DURING INSPECTION IAW J9-IA57-0869. 2L72 4F4 FRTA46NM E29NE 20030514001572003051400157EU 2003 5 14 RAIA00304114 120030415A3350 WIRE AEROSPATR42 ATR42300 8680920EU EMERGENCY LIGHT BROKEN A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03421TE 102 EMERGENCY EXIT LIGHT OUT AT BOTTOM OF PAX STAIRS. REPAIRED BROKEN WIRE AT TOP STEP. OPS CHECK GOOD. 2H72 4T RTA53EU 20030523001372003052300137WP 2003 5 23 DHL2003604513 120030428A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR L/E FORMER WITH 0.500 INCH CRACK STA XS 478.897. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AT XS 478.897 IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030602000202003060200020NM 2003 6 2 USAA030045 120030428A5313 STRINGER BOEING737 737401 1384701NM FS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US40460 23885 PIT - FOUND STRINGER CRACKED .5 INCH, HAT CHANNEL STRINGER AT STATION 380 S2R. COMPLETED REPAIR SPLICES, SECTION AND SHEAR CLIP PER SRM 53-00-03. (M) 2L72 4F RTA16WE 20030602000672003060200067CE 2003 6 2 CA030424006 120030408A323211238002221 ACTUATOR BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE NLG LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING A POST FLIGHT WALK AROUND, THE PILOT NOTICED HYDRAULIC FLUID LEAKING FROM THE NOSE GEAR ACTUATOR P/N 112-280022-21. THE FLUID WAS COMING FROM ABOVE THE RETAINER. THE ACTUATOR WAS REPLACED WITH A OVERHAULED UNIT. DURING THE RIGGING PROCESS THE POSITION WARNING LIGHTS WERE MALFUNCTIONING. THE DOWN AND LOCK INDICATION WOULD GO OUT BEFORE THE SWITCH WAS DEACTIVATED. DURING THE EXTEND CYCLE THE DOWN AND LOCK INDICATION WOULD ILLUMINATE BEFORE THE GEAR DOORS OPENED. THE CAUSE OF THE MALFUNCTION WAS THE CONNECTOR ON THE ACTUATOR WAS IMPROPERLY WIRED. 1L72 4T4 T A24CE E4EA 20030604001622003060400162NM 2003 6 4 UPS03440582 120030412A575365B078691 RIB BOEING747 747121 1384871NM NR 6 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 6 VC FLAP I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2 & 3 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030520000722003052000072 2003 5 20 GTIA030274 420030422A2565 SLIDE DOUG DC9 DC941 302207NWP CABIN DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23130NK 47604 PBI - FLT 330 - LEFT SIDE PACK FELL OFF. REINSTALLED SLIDE/COVER. (M) 2L72 4F A6WE 20030605000542003060500054WP 2003 6 5 UPS03840659 120030508A5753 SKIN DOUG DC8 DC873F 302199FWP TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 45936 RT INBD FLAP INBD WEB CRACKED. REMOVED ONE AREA OF CRACKED SKIN. D. RIEKE. 75838 5-8-03. REMOVED WEB. FABRICATED NEW WEB FROM 2024-T3 .040" PER SAMPLE. STARTED DRILLING NEW WEB. J. DUNLAP 26402 05-09-03. INSTALLED NEW WEB AND STIFFNERS IAW EO DC-8 5750-18733. 2L74 4F RT4A25 20030609001242003060900124WP 2003 6 9 ABXA030153 120030515A575259100512 STRUCTURE DOUG DC9 DC931 3022065WP RT AILERON TAB DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING A WATCH ITEM INSPECTION, FOUND THE RIGHT AILERON TRIM TAB LOWER SURFACE DELAMINATED 10.6 SQ INCHES AND BEYOND LIMITS IAW DC-9 SRM 51-50-3, PARA 2. REPLACED RIGHT AILERON TRIM TAB IAW DC-9 MM 27-10-05-2-0001. 2L72 4F A6WE 20030521001422003052100142EU 2003 5 21 DHL2003368003 120030508A3230 SEQUENCE VALVE AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01368DH 207 UPON GEAR RETRACTION, LT GEAR UNSAFE AND DOOR LIGHT REMAIN ILLUMINATED LT GEAR DOWN LIGHT ILLUMINATED INTERMITTENTLY ON BOTH PANELS. UNSAFE GEAR ABNORMAL PROCEDURE COMPLETED CONTINUED FLIGHT GEAR DOWN. REMOVED AND REPLACED LT DOOR SEQUENCE VALVE PER M/M 32-21-37 & LT GEAR UPLATCH ASSEMBLY PER M/M 32-31-44. OPS CHECKED GOOD ON GEAR RETRACTION TEST AND LEAK CHECKED GOOD. 2L72 4F RTA35EU 20030618000422003061800042NM 2003 6 18 SWAA031334 120030615A2560P2070001 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 AFT CABIN EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030527000922003052700092WP 2003 5 27 AALA20030387 120030330A3397 CONTACTOR DOUG DC9 DC982 3022082WP EMER BATTERY INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. CLEANED BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030529000772003052900077NE 2003 5 29 HEEA086519 120030521A62307610408020047 SCISSORS SKRSKYS76 S76A 8143006NE MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 WORN BEARINGS. REPLACED WASHER MS200002C12 DUE TO WORN; BEARING (4 EA) SB5200-103 DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030619000292003061900029SW 2003 6 19 HEEA087378 120030611A5210407070620158 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 CREW DOOR PANEL CRACKED. 1G71 3U O H2SW 20030620000282003062000028SW 2003 6 20 HEEA086950 120030603A3211 CUSHION BELL 407 407 1182206SW STRAP ASSY CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03417PH 53038 FOUND CUSHION UNBONDING, DETECTED CORROSION UNDER CUSHION. UNABLE TO DETECT CORROSION WHILE STRAP WAS INSTALLED ON AIRCRAFT, STRAP CORRODED DUE TO IMPROPER PROTECTION DURING THE MANUFACTURING PROCESS. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030623000702003062300070CE 2003 6 23 2003F00380 120030430A712012991004717 TRUSS BEECH 1900 1900D 1154162CE ENGINE CHAFED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1916540 UE172 AT SCHEDULED ROUTINE MAINTENANCE, CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON INBOARD SIDE. PERFORMED TRUSS REPAIR TO CHAFED AREA IAW FAA APPROVED DATA CONTAINED IN REPORT NR 030430, DERT 510305-CE. (M) 2L72 4T RTA24CE 20030623000912003062300091 2003 6 23 GTIA030415 420030605A2565 SLIDE DOUG DC9 DC982 3022082WP PAX DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 DTW - FLT 461 - L1 SLIDE FELL OFF NOW IN SPIRIT PLUS. INSTALLED L1 SLIDE. (M) 2L72 4F A6WE 20030710001382003071000138EU 2003 7 10 MALA030307 120030604A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4K INSPECTION IN CWA, RT FUSELAGE DENT AT STA 318. MAINTENANCE COMPLETED REPAIR IAW EO 53159. REF 409 NR 179562 FOR DETAIL. A/C RELEASE DATE 6/6/03. 2L72 4T RTA52EU 20030711000952003071100095EA 2003 7 11 COMA0360292 120030624A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01969CA17104 7141 FLIGHT 5647 GEAR DISAGREE WARNING AFTER T/O. REPLACED HYDRAULIC RESERVOIR NR 3. 2L72 4F RTA21EA 20040211000572004021100057NE 2004 2 11 2003UALA00962 220031214A7320 LINE BOEING777 777222 1385219NM PWA PW4077PW4077 NE EEC CONTAMINATED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29781UA 26945 222008 ON CLIMB TO FL410 FROM FL370 ENGINES MAXED OUT. PWR REQ 1.47 LEFT ENG TOPPED OUT. RIGHT 1.430 WITH RT THROTTLE AT STOP AND LT ENG THROTTLE ABOUT 1 & 1 AND A HALF INCHES BEHIND. THRUST SHORT FALL WAS CAUSED BY AN AMBIENT PRESSURE (PAMB) SENSOR ERROR TO THE EEC. THE ERROR WAS DETERMINED NOT TO BE INTERNAL TO THE EEC UNIT ITSELF. REMOVED EEC WAS TESTED BY HAMILTON-SUNDSTRAND, AND PASSED ALL INCOMING FUNCTIONAL CHECKS. A LOOSE PAMB B-NUT WAS TIGHTENED ON 12/17/03. ON 12/18/03, WHEN THE EEC WAS REPLACED, APPROXIMATELY A TEASPOON OF WATER WAS DRAINED OUT OF THE PAMB LINE. IT IS BELIEVED THAT THE COMBINATION OF THE LOOSE NUT, ALONG WITH WATER CONTAMINATION, CAUSED THE PAMB ERROR. 2L72 4F4 FRTT0001SE E46NE 20031105000042003110500004NM 2003 11 5 NACA20030118 120031021A5270 TERMINAL BOEING727 72723 1384004NM PWA JT8 JT8D* NE DOOR WARNING SYSBROKEN A NACAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL03992AJ 19428 CARGO DOOR UNLOCKED LIGHT ILLUMINATED DURING TAKEOFF ROLL. REPLACED BROKEN TERMINAL RING AND REATTACHED TO NR 3 LATCH WARNING SWITCH. 2L73 4F4 F A3WE E2EA 20031112000332003111200033NM 2003 11 12 03FDEA01719 120031008A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING OB FLAP IB HINGE (FLAP SIDE) BRACKET- OB HINGE LUG AND HOLE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B HINGE LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, WINGS- LEFT AND RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20030912001792003091200179NM 2003 9 12 AALA20030888 120030822A3350 CONNECTOR BOEING777 777223 1385213NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21765AN 32879 BOS - FOUND ROW 44 EMERGENCY PATH LIGHT IS OUT. RECONNECTED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20040109000342004010900034EA 2004 1 9 CHI2003F00000 120030604A6220114R21551 BAR BOEING234 234 1385049EA LYC AL5512AL5512 41581NE ROTOR HEAD CRACKED B CHIRO OTHER O OTHER NRNOT REPORTED 1 NM09239CH3898 MJ006 DURING NORMAL ROTOR HEAD MAINTENANCE, THE TWO REPORTED TIE BARS WERE FOUND WITH NUMEROUS DEFECTS. THE DEFECTS CONSISTED OF SEVERAL CRACKED PLATES AT THE TIE BAR PINHOLE. THE TWO TIE BARS WERE SENT TO THE MANUFACTURER FOR EVALUATION AND AFTER DISASSEMBLY, ADDITIONAL DEFECTS WERE DISCOVERED. A ROTOR OVERSPEED MAY HAVE BEEN THE CAUSE OF THESE DEFECTS. HOWEVER, DURING THE LIFE OF THESE TWO TIE BARS, NO ROTOR OVERSPEEDS WERE REPORTED. THE MANUFACTURER CURRENTLY HAS THIS MATTER UNDER INVESTIGATION. (CHI2711) 2G72 4U4 U H9EA E4NE 20031118000382003111800038EU 2003 11 18 AWXA200301153 120030924A5320D534711240100 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE OUTBOARD RT AFT SHEAR PLATE AT Y1292, FORWARD OF FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT Y1292, FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG A24-A27, 8-12, & 21-22, FIG 61 & 62, 2, 3, & 8. 2L72 4F RTA28NM 20031118000812003111800081SW 2003 11 18 BDJ2003F00001 120030929A57115146R SPAR BBAVIA7 7AC 2110102SW CONT A65 A65* 17003SO WING CRACKED E BDJAO OTHER O OTHER NRNOT REPORTED 1 GL272205E4437 7AC5776 OWNER REQUESTED AN INSPECTION IAW AD2000-25-02R1 WOOD SPAR INSPECTION. INSPECTION REVEALED THAT ALL INSPECTION HOLES HAD NOT BEEN ADDED IAW SL406 REV. A. UPPER FRONT SPAR HOLES WERE CUT AND CONVERED WITH DUCT TAPE, RT FRONT SPAR HAD OPEN CRACK AT BUTT EXTENDING INTO SPAR PLATE ATTACHING BOLT HOLE. SPAR DELAMINATING THE FULL LENGTH AT SEVERAL PLAES ON BOTH SIDES. NAILS MISSING OUT OF SEVERAL RIBS. LAST SPAR INSPECTION IAW AD HAD BEEN COMPLETED AUT 1/03. LAST RECOVERED AND SPAR VARNISH DATED NOV 1977. 1H71 3O3 O A759 E205 20031217000442003121700044WP 2003 12 17 DHL2003805511 120030726A534774529527 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 MAIN CARGO COMPT NR 7 CARGO TRACK LUG WORN AT STA 228.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031223001372003122300137WP 2003 12 23 UPS03841648 120031210A32507649739552 LINE DOUG DC8 DC871F 302199DWP NLG STEERING FAILED A IPXAO OTHER GK MULTIPLE FAILURE FLUID LOSS TXTAXI/GRND HDL 1 SO01750UP 45950 INSPECTION TYPE:N/A, A/C TAXIED OUT CARGO RAMP NOSE WHEEL STEERING NOT EFFECTING AND WAS STIFF. LOSS OF ALL HYDRAULICS. ACP NLG LINE REPLACED PER STANDARD PRACT CH 20-10-01. 2L74 4F RT4A25 20031224000102003122400010WP 2003 12 24 GTIA030805 120031008A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND FORWARD CABIN STA 200 TO 256 LBL 14 TO 21 FLOOR PANEL HAS CRACKED/DAMAGED AT CORNERS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20031223000042003122300004NM 2003 12 23 AWXA200301522 120031209A3350900835A BATTERY BOEING737 737277 1384570NM EMERGENCY LIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28187AW 22654 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHT SYSTEM THE EMERGENCY EXIT SIGN ABOVE THE R-2 FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK ABOVE THE R-2 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030918000532003091800053NM 2003 9 18 DL76G030708 120030731A2820AV311 ACTUATOR BOEING767 7673P6 1385105NM XFEED VALVE INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271501P 24983 FUEL CROSSFEED VALVE WOULD NOT OPEN IN FLIGHT. VALVE ACTUATOR REPLACED 2L72 4F RTA1NM 20031009001172003100900117SW 2003 10 9 505091703 120030917A2910 B-NUT SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL HYD SYSTEM LOOSE E STZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03505FS AC591B ENROUTE TO DESTINATION, AIRPORT CREW NOTICED THE ILLUMINATION OF THE LOW HYDRALIC PRESSURE ANNUNCIATORS FOLLOWED BY A DECREASE IN HYDRAULIC SYSTEM PRESSURE ON THE PRESSURE GAUGE. CREW RETURNED TO THE DEPARTURE AIRPORT AND PERFORMED MANUAL GEAR EXTENSION AND LANDED WITHOUT INCIDENT. FURTHER INVESTIGATION BY MAINTENANCE FOUND THE HYD SYSTEM RETURN LINE B-NUT AFT OF THE NR 2 FIREWALL LOOSE. MAINT. CHANGED BOTH HYD PUMPS AND SYSTEM FILTERS AND RETORQUED B-NUT. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20031125000032003112500003WP 2003 11 25 DHL2003807557 120031027A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA 1575.000 - STA 1594.000. REMOVED DAMAGED TRACK SECTION IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED DAMAGED AREA AND NEW TRACK SECTION IAW SRM 51-1-8B. INSTALLED NEW TRACK SECTION IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031125000842003112500084WP 2003 11 25 DHL2003805533 120030807A5753 PLATE DOUG DC8 DC873F 302199FWP T/E FLAP NICKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING INBD FLAP PLATING UPPER PART WITH 0.500 NICK AT XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2, FIG 1. PERFORMED BLEND OUT ON PLATING FOUND OUT OF LIMITS (DEPTH 0.042, DIA 0.500) IAW SRM 57-2-0 PG 14. REMOVED NICK PLATING IAW SRM 51-1-21 PG 1. FABRICATED PLATING IAW SRM 57-7-1 PG 2, FIG 1. CLEANED, TREATED AND PRIMED INTERNAL PART IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030716000132003071600013EU 2003 7 16 2003F00408 120030628A2900 COVER AIRBUS320 A320233 3930329EU HYD VALVE BROKEN A RJEFO OTHER O OTHER TXTAXI/GRND HDL 1 SO23981LR 558 DURING TAXIING PROCESS OF FLIGHT, THE 'THS' CONFIGURATION WENT ALL DOWN AND THE AIRCRAFT COULDN'T DEPART FROM LAX STATION. THE AIRCRAFT REMAINED ON GROUND FOR MAINTENANCE. TECHNICIANS CHECKED THE 'THS' MECHANISM PER AMM 27-44-00 AND FOUND ONE OF THE PLASTIC COVERS OF THE HYDRAULIC VALVE BLOCKS BROKEN, BOTH PLASTIC COVERS WERE REPLACED AS PER AMM 27-44-00. TEST OF THE 'THS' ACTUATOR ELECTRICAL CONTROL AND THE ELAC 1 AND 2 AND SEC 1 WAS PERFORMED PER AMM 27-96-00. TESTS RESULTS WERE SATISFACTORY AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20030716001122003071600112NE 2003 7 16 HEEA088042 120030706A24207655009005104 GCU SKRSKYS76 S76A 8143006NE AC GENERATOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 GCU INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030116001922003011600192 2003 1 16 HEEA083103 420030108A345713824120234 RECEIVER BELL 206 206L3 1182108SW GPS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331821 51076 GPS INTERMITTENTLY RECYCLES ON-OFF-ON. FOUND UNIT WOULD NOT PASS GPS TEST. 1G71 3U H2SW 20030127000432003012700043 2003 1 27 HEEA083620 420030114A345713824120234 GPS BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 GPS RECEIVER LOSES POWER WHEN CHECKING NAV FLAG. 1G71 3U O H2SW 20030130000832003013000083NM 2003 1 30 P5CA0300738 120030123A5411NONE FRAME BOEING747 7472U3B 1384846NM #4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CRACK, APPROX. 1", FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FRAME ON HORIZONTAL FLANGE, STARTING FROM TOP EDGE. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3. 2L74 4F RTA20WE 20030203002322003020300232EA 2003 2 3 COMA0360063 120030130A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER O OTHER APAPPROACH 1 SO01811CA 7380 FLIGHT 5890 GEAR DISAGREE WARNING FOR 10 SEC.COULD NOT DUPLICATE. LANDING GEAR RETRACT AND EXTEND CHECKS WERE NORMAL. 2L72 4F RTA21EA 20030204000952003020400095NM 2003 2 4 SWAA030112 120030117A531365C27314 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 400 BETWEEN STR 13R AND STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030204001142003020400114CE 2003 2 4 UG8AG0243 120030113A2720 CONTROL MODULE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RUDDER MALFUNCTIONED E UG8AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL235112 7500010 SHORTLY AFTER TAKEOFF THE (RUDDER LIMIT FAIL) CAS MESSAGE ILLUMINATED. PERFORMED RUDDER CONTROL LIMITER TEST IAW MM. NO FAULTS DURING 3 HOURS OF TESTING. RESET RUDDER LIMIT CONTROL MODULE NK123. PERFORMED OPERATIONAL CHECK FLIGHT. NO PROBLEMS WERE ENCOUNTERED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4J4 FRTT00007WITE6CH 20030207001052003020700105NM 2003 2 7 03FDEA00062 120030122A5347 SEAT TRACK BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION ON SEAT TRACK OUTBOARD FLANGE BS 720D - 720D+10 LBL 25 WL 208. REMOVED AND REPLACED NEW SEAT TRACK IAW SRM 51-30-2. 2L73 4F4 FRTA3WE E2EA 20030212000382003021200038NM 2003 2 12 CA030106004 120030103A2797 CONNECTOR BOEING737 7372T5 1384474NM PWA JT8 JT8D17 52049NE STAB TRIM MOTOR BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA (CAN) ON OVERNIGHT CHECK OF AUTO PILOT STAB TRIM, C/B FOUND TRIPPED AND UNABLE TO RESET. SMOKE NOTED IN STAB COMPARTMENT AND UPON INVESTIGATION FOUND CONNECTOR AND 3 INCHES OF ASSOCIATED WIRING DAMAGED ATA/P STAB TRIM MOTOR CONNECTION. WIRING REPAIRED, CONNECTOR AND STAB TRIM MOTOR REPLACED. STAB TRIM OPERATION CHECKED SERVICABLE. 2L72 4F4 FRTA16WE E2EA 20030213000712003021300071NM 2003 2 13 0300146302 120030128A2120 ODOR BOEING747 747451 1384940NM GALLEY DETECTED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL01662US 23720 DURING DESCENT, A BURNING ODOR EMITTED IN THE FORWARD PART OF THE GALLEY BY THE NR 4 DOOR. TURNED OFF GALLEY LIGHTS AND PULLED GALLEY CIRCUIT BREAKERS. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. INSPECTED AND OPERATIONALLY CHECKED THE GALLEY EQUIPMENT WITH NO FAULTS FOUND. 2L74 4F RTA20WE 20030220001882003022000188NM 2003 2 20 AWXA200300163 120030131A534065B578393 FITTING BOEING737 73733A 1384673NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW0 0 23634 LCQ - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT LAVATORY AREA FLOOR BOARD ATTACH HOLE BS 986, RBL 20. MAINTENANCE REMOVED AND REPLACED ATTACH FITTING AT BS 986, RBL 20 IAW B737-300 SRM 51-40-02, PG. 6-9. 2L72 4F RTA16WE 20030224000062003022400006SW 2003 2 24 ALGA084107 120030210A3246214052053101 SKID BELL 214 214ST 1182106SW MLG MISMANUFACTURED H ALGAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 FS01391AL 28103 PART TT: NEW: FWD AND AFT SKID TUBE INSERTS WILL NOT ALIGN FOR ATTACHMENT- MISMANUFACTURED. 2G72 4U H10SW 20030226000062003022600006SW 2003 2 26 ERAA084680 120030110A3150209075325109 LIGHT BELL 412 412 1182202SW COCKPIT INTERMITTENT H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01418EH1234 CAUTION LIGHT FLICKERS WHEN TESTED WITH TEST SWITCH ON PANEL. 1G72 4U H4SW 20030227000092003022700009SW 2003 2 27 HEEA084367 120030211A5620407540010 WINDOW BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 WINDOW CRACKED. SCRAPPED. 1G71 3U O H2SW 20030311000552003031100055EU 2003 3 11 HEEA085069 120030227A6720 BEARING BOLKMS105 BO105S 5626006EU CONTROL ROD ASSYWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 CONTROL ROD ASSY HAS WORN BEARINGS. REPAIRED. 1G72 3U H3EU 20030325000012003032500001NM 2003 3 25 0303002 120030308A53306545800584 SKIN BOEING737 737230C 1384472NM FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW69627 20257 ONE CRACK EMINATING FROM RIVET HOLE IN SKIN PANEL APPROXIMATELY 0.125 INCH IN LENGTH AT BS 258 BETWEEN S-19L AND S-20L. REPLACED SKIN PANEL FROM BS223 TO BS259.5 S-19L TO S-24L PER BOEING MESSAGE CGG-ADS-03-00005H. FAA FORM 8110-3 ISSUED. 2L72 4F A16WE 20030121000082003012100008NM 2003 1 21 SWAA030069 120030113A2560PH22300L STRIP BOEING737 7377H4 1384404NM CABIN FLOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29714CB 27848 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 ABC. SECURED STRIP PER MM. 2L72 4F RTA16WE 20030121000492003012100049SW 2003 1 21 HEEA083251 120030108A2560206072841115 SEAT BELT BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 SEAT BELT HARD TO ADJUST LAP BELT PORTION. REPAIRED. 1G71 3U H2SW 20030320001242003032000124NM 2003 3 20 2003UALA00114 120030128A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHT SHORTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29677UA 30029 SEAT 20 THROUGH 23 EEL LIGHTS WERE INOPERATIVE. FOUND MID-GALLEY EEL LIGHT ASSEMBLY SHORTING OUT THE SEAT EEL LIGHTS. REPLACED MID-GALLEY EEL ASSEMBLY. 2L72 4F4 FRTA1NM E24NE 20030122000532003012200053SW 2003 1 22 HEEA083441 120030109A3212D24972113 FLOAT BELL 206 206B3 1181506SW EMERGENCY FLOAT LEAKING E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032268V 3605 EMERGENCY FLOAT BAG FAILED 10 YEAR INSPECTION AND LEAKED. 1G71 3U H2SW 20030320000832003032000083NM 2003 3 20 2003UALA00058 120030115A3244 TIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE MLG FAILED A UALAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 WP29121UA 29167 AIRCRAFT BLEW 2 TIRES ON LT MLG ON TAKEOFF. CAUSE OF TIRE FAILURE UNKNOWN, PRESUMED TO BE DUE TO FOD. TIRES 3F,AND 4F REPLACED FOR FAILURE, 3F AND 3R REPLACED DUE TO SUBSEQUENT DAMAGE. LBG INBOARD STRUT DOOR REPLACED DUE TO BEING BENT. 2L74 4F4 FRTA20WE E24NE 20030321000932003032100093NM 2003 3 21 2003UALA00239 120030228A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29648UA 25285 EEL PATH LIGHT STRIP AT RH MID-GALLEY IS INOP. REPAIRED DAMAGED SECTION. 2L72 4F4 FRTA1NM E24NE 20030303001862003030300186SW 2003 3 3 HEEA084568 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 14335 33113 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES ERODED THROUGH. 1G72 4U H4SW 20030326000722003032600072NM 2003 3 26 CA030207004 120030207A5330 SKIN BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A C CHECK AT KELOWNA FLIGHTCRAFT A QUARTER INCH CRACK WAS FOUND AT BS 827. ALSO FURTHER INVESTIGATION FOUND A 5 INCH CRACK WAS DETECTED,COMMON TO THE LOWER SKIN JUST BELOW THE STR 4R OUTER SKIN LAP JOINT BETWEEN BS 827 & BS 837. BOTH CRACKS WERE REPAIRED PER SRM 53-30-03 FIG 48, DETAIL XIII. TIME-57134.7CYCLES-54518. 2L72 4F4 F A16WE E2EA 20030418001322003041800132EA 2003 4 18 SWIA200311788 120030216A5280 LATCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG DOOR UNSECURE A SWIAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM07917SW 7641 AFTER TAKEOFF HEARD A LOUD WHISTLE COMING FROM THE OUTSIDE. ALSO RECEIVED A STALL FAIL CAUTION MESSAGE FOR A FEW SECONDS, THEN IT CLEARED ITSELF. WITH INCREASED SPEED, THE NOISE GOT LOUDER AND FELT SLIGHT VIBRATION. RETURNED TO DEN FOR LANDING. FOUND THE FORWARD NOSE DOOR SERVICE PANEL HAD FORWARD LATCH UNSECURED. RESECURED LATCH, INSPECTED FOR DAMAGE. NO DAMAGE FOUND. 2L72 4F4 FRTA21EA E15NE 20030421000402003042100040NM 2003 4 21 UPS03440244 120030128A5314 ANGLE BOEING747 747200 1384847NM RT KEELBEAM BOX CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C FX, KEEL BEAM BOX INTERIOR LOWER FRAME RT SIDE FOUND HEAVY CORROSION AT STA 1460 TO STA 1470 RBL 6 TO RBL 9. REPAIRED ANGLE FABRICATED AS PER HX RS R53-49-34970 AND EA 747-53-20123. BLEND OUT 0.146 X 2.4 X 3 INCH. 2L74 4F RTA20WE 20030421000872003042100087NM 2003 4 21 DLM11030121 120030202A3240 FITTING DOUG MD11 MD11 3023602NM BRAKE ASSY CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27803DE 48474 FOUND DURING D1 LTR CHECK- P/N ABH7269-509 FITTING CRACKED THRU FASTENER HOLES. REPLACED WITH A -521 FITTING. THIS IS THE LT SIDE FITTING FOR THE BRAKE PEDAL TORQUE TUBE ASSY REF NR297. 2L73 4F RTA22WE 20030422000222003042200022WP 2003 4 22 MEX2003062 120030308A496012955211 THERMOSTAT DOUG DC9 DC932 3022066WP APU FAILED A ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW231003P 48150 FLT 248 - MEX-GDL - DURING PUSH BACK, THE APU SHUT OFF ON RAMP. THE AIRCRAFT RETURNED TO POSITION. THE PNEUMATIC LOAD CONTROL THERMOSTAT WAS REPLACED IAW MM 49-52-1, TESTS CORRECT. (M) 2L72 4F A6WE 20030422000652003042200065SO 2003 4 22 SIMA200307003 120030306A532014525480003 SILL EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED THE CENTER SILL AND INSTALL NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 20 CHAPTERS 51-40-02, 51-20-03, AND 51-40-06. (M) 2L72 4T RTT00011AT 20040223001842004022300184WP 2004 2 23 UPS04841714 120031230A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LONGERON 34R IS CRACKED BETWEEN STATION 1270-1290. REMOVED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20030723000862003072300086NE 2003 7 23 VNAA0307001 220030709A7397 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EEC FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07424JS 3033 THE CREW RECEIVED AN INDICATION THAT THE LEFT HAND PROP WAS ONLY PRODUCING 36 NP. THE FLIGHT THEN RETURNED TO EVV. OUTSTATION MAINTENANCE INSPECTED AND CLEANED THE FEATHER SOLENOID AND ENGINE CONTROL UNIT CONNECTOR AND CYCLED THE I-2 CIRCUIT BREAKER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030801000242003080100024WP 2003 8 1 2003F00507 120030609A2560P2070003001 FLASHLIGHT DOUG DC9 DC931 3022065WP CABIN CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO35933JK 48159 FORWARD CABIN UPPER EMERGENCY FLASHLIGHT LED DIM, INTERNAL FAILURE OF LED. NO FLASH. REMOVED AND REPLACED EMERGENCY FLASHLIGHT IAW DC9 MM 25-60-00. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 20030903000652003090300065EU 2003 9 3 U30A200300021 120030716A2611PAI283000 SMOKE DETECTOR AIRBUS320 A320212 3930322EU GE CFM56 CFM56* 13802NE ZONE 262 FAULTY A U30AK NONE N FALSE WARNING ININSP/MAINT 1 EA17265AV 427 AFTER FLT 319 CUN-BWI, DURING "DAILY CHECK", ECAM MESSAGE SHOWED SMOKE DETECTOR IN LAV D WAS FAULTED. REMOVED AND REPLACED LAV D SMOKE DETECTOR IAW AMM 27-17-15-401. OPS CK'D IAW AMM 26-17-00-710-001 WITH NO FAULTS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E2GL 20030806000722003080600072SO 2003 8 6 C2XA03SH231 120030726A541014576057621 STIFFENER EMB 145 EMB145LR 3260212SO NACELLE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK THE LEFT HAND UPPER COWLING INTERNAL STIFFENER WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030821000162003082100016NM 2003 8 21 WRLA200316 120030716A29136506606 PUMP DOUG MD11 MD11 3023602NM NR 1 ENG HYD CRACKED A WRLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA27272WA 48437 HYDRAULIC 1 SYSTEM FAILED IN FLIGHT. AIRCRAFT DESTINATION WAS CHANGED FROM BGR TO ATL FOR REPAIRS. REMOVED AND REPLACED LEFT AND RIGHT HYDRAULIC PUMPS RAN ENGINES FOUND NO LEAKS. REMOVED AND REPLACED FILTER PER MM. REPLACE ENGINE DRIVEN HYDRAULIC PUMPS. (M) 2L73 4F RTA22WE 20030825001772003082500177NM 2003 8 25 03FDEA01211 120030729A5753ARC70561 TEE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 SNRM N1007 - RT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND WITH CORROSION IN HOLE. SNRM N1007 - RT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED IAW EA 1-5750-71878, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RT OUTBOARD FLAP NR 2, 3, 4 AND 5 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20030826000352003082600035NM 2003 8 26 03FDEA01342 120030819A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CHORD AT BS 1352 IS CHAFED ALONG ENTIRE CIRCUMFERENCE AND RUB STRIPS ARE MISSING. FOUND FLANGE ON 1352 CHORD TO BE OUT OF LIMITS. REMOVED DAMAGED CHORD, DRILLED UP AND INSTALLED NEW 1352 CHORD IAW SRM 53-10-1, 51-30-2, 51-30-5. 2L73 4F RTA3WE 20030911001932003091100193WP 2003 9 11 AALA20030343 120030228A5310 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND STATION 1437 FRAME, AFT SHEAR TIE CRACKED AT FASTENER. REMOVED AND REPLACED SHEAR TIE AT STATION 1473 PER SRM 51-10-01. (M) 2L72 4F A6WE 20030915000992003091500099SW 2003 9 15 BAQA085129 120030905A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW GEARBOX MOUNT DELAMINATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03206CJ 51579 GEARBOX MOUNT RESTRAINT IS DELAMINATED BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20031001000232003100100023NM 2003 10 1 QXEA200301084 120030827A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PANEL CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CORRODED NUTPLATE ON BOTTOM SIDE OF AFT FLOOR SUPPORT FOR PANEL 144AZ AT STATION Y21L. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-11, 51-20-16 AND 51-40-00. 2H72 4T RTA13NM 20030929001362003092900136 2003 9 29 252TR0009 420030906A34132587335111 GYRO BOEING737 737228 13844AGNM COCKPIT INOPERATIVE A PIDAO OTHER O OTHER CRCRUISE 1 SO05252TR 23001 AUTO PILOT "B" CHANNEL JERKS IN TURNS. REPLACED NR 2 VERTICAL GYRO IAW MM 34-20-0. PERFORMED OPERATIONAL TEST; TEST NORMAL. 2L72 4F RTA16WE 20030908003362003090800336NM 2003 9 8 SWAA031912 120030826A2612 FIRE WARNING BOEING737 7373H4 1384600NM CARGO BAY FALSE ACTIVATIONA SWAAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29630WN 27705 DECLARED EMERGENCY, DIVERSION, AFT CARGO FIRE WARNING LIGHT ILLUMINATED, BOTTLES FIRED. REMOVED AND REPLACED BOTH SUPRESSION BOTTLES, CORE FILTERS, SCU, CCU AND ALL AFT CARGO SMOKE DETECTORS PER MM. SYSTEM TEST GOOD WITH NO EVIDENCE OF A FIRE. 2L72 4F RTA16WE 20030909001552003090900155 2003 9 9 BAQA088906 420030829A3421 PHOTO CELL BEECH 100 100BEECH 1152916CE HSI INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03777GS6 79080302 B241 PHOTO CELL NOT WORKING ON HSI. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20031003000392003100300039NM 2003 10 3 AWXA200301043 120030811A5414657377339 SKIN BOEING737 737277 1384570NM LT NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON NR 2 ENGINE LT FORWARD COWL INNER SKIN UNDER UPPER FORWARD SAFETY LATCH. MAINTENANCE CUTOUT CRACKED SKIN ON NR 2 ENGINE LT FORWARD COWL INNER SKIN NAC STA 120 RT; FABRICATED A DOUBLER, SHIM AND FILLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 54-10-3, PG. 3-4, FIG. 2. 2L72 4F RTA16WE 20031203000632003120300063NM 2003 12 3 AALA20031181 120031016A5330146T3261 SKIN BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21374AA 25201 FOUND FUSELAGE SKIN ON INNER SIDE HAD CORROSION BLEND BEYOND SRM LIMITS. BLEND OUT CORROSION PER ATTACHED SKETCH. DYE CHECK TO ENSURE CRACK FREE. ROTO PEEN BLENDED AREA. REFINISH THE BLENDED AREA PER SRM. FILL BLENDED AREA WITH BMS 5-95. SHIM AS REQUIRED TO REINSTALL THE DRAIN BRACKETS TO THEIR PREVIOUS LOCATIONS PER MRB 767-2528. (M) 2L72 4F RTA1NM 20031203001522003120300152WP 2003 12 3 AALA20031000 120030912A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21461AA 49566 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS OBSERVED TO BE INOPERATIVE IN THE FORWARD CABIN. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040116000142004011600014NM 2004 1 16 03FDEA02191 120031215A5710ARC74821 FITTING DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING - INBOARD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES, FOUND 3 THAT EXCEED LIMITS. LT WING - INBD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-75176, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT INBD. FLAP VANE ATTACH FITTINGS REWORK. 2L73 4F RTA22WE 20040123000072004012300007WP 2004 1 23 ASAA0380704 120031104A56104616968501 ROD DOUG DC9 DC983 3022083WP CLEARVIEW WINDOWOUT OF POSITION A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 LAX PREFLIGHT CHECK, LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPOSITIONED ACTUATING ROD GUIDE PIN. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20031208000042003120800004NM 2003 12 8 QXEA200301276 120031015A7710 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 400 FAILED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09350PH 488 DURING FLIGHT 2084 FROM SEA TO CLM AIRCRAFT RETURNED TO FIELD DUE TO SHORTLY AFTER TAKEOFF NR 2 ENGINE SURGED AND CREW SHUT ENGINE DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED BETA BACK-UP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031208001632003120800163NM 2003 12 8 AWXA200301325 120031006A553465537448 CHANNEL BOEING737 7373G7 1384595NM VERTICAL STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MINOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON FUSELAGE ANGLE JUST AFT OF RT VERTICAL STABILIZER ATTACH FITTING BS 1093. MAINTENANCE REMOVED 2 EACH CRACKED ANGLES JUST AFT OF RT VERTICAL STABILIZER ATTACH FITTING BS 1093; FABRICATED 2 EACH NEW REPLACEMENT ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12 SHEET 2. 2L72 4F RTA16WE 20031209000062003120900006WP 2003 12 9 UPS03841471 120031022A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN STATION 400 TO 450 AT LONG 31R. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5773863 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20031208001012003120800101NM 2003 12 8 QXEA200301335 120031009A5310 DOOR FRAME DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - WEB CHAFED ABOVE BAG DOOR CUTOUT AT FRAME X580.5. REPAIRED IAW RD 8-53-5461. 2H72 4T RTA13NM 20031210001482003121000148EU 2003 12 10 AALA20031364 120031201A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2133069 512 JFK SEAT MOUNTED EMERGENCY LIGHT AT 15G INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 15G. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA35EU 20031211000432003121100043EU 2003 12 11 XNOA1165 120031111A2731 WHEEL AIRBUS300 A300B4203 3930306EU COCKPIT OUT OF ADJUST A XN0AD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL23373PC 218 PILOT AND COPILOTS TRIM INDICATOR ELEVATOR POSITION READS CAPT 1 DEGREE NOSE UP & F/O 3 DEGREES NOSE UP. REPOSITIONED CAPT'S PITCH TRIM INDICATION WHEEL, VISUALLY VERIFIED INDICATION. ALL INDICATIONS NORMAL. WORK ACCOMPLISHED IAW A300 MM 27-41-00 & 22-23-00. 2L72 4F RTA35EU 20030919000432003091900043NM 2003 9 19 IU62003F00027 120030613A2913624022 ADAPTER BOEING737 737* NM HYD PUMP ERODED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 2664 MX602570 HYDRAULIC PUMP ADAPTER BLOCK, EROSION/ WEAR AROUND STROKING PISTON PORT STATIC SEAL SURFACE. SOFT MATERIAL OR TOO HARD OF A SEAL. IMPROVE SCALING SURFACE OR INSTALL A DIFFERENT SEAL. (NR 178228) 2L72 4F RTA16WE 20030919000762003091900076WP 2003 9 19 IXXA0300055O 120030812A1430 SCREW DOUG DC8 DC871F 302199DWP NLG WW PANEL MISSING A IXXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW11828BX81077939 45993 AFTER TAKE OFF FROM KPHL TO KTOL AND DURING GEAR RETRACTION CREW EXPERIENCED A NOISE AND VIBRATION COMING FROM THE NOSE GEAR AREA. THE GEAR WAS LEFT DOWN FOR THE REMAINDER OF FLT AND MADE AN UNEVENTFUL LANDING IN KTOL. MAINTENANCE FOUND SCREWS MISSING FROM RIGHT AFT PANEL IN NOSE WHEEL WELL. MAINTENANCE REPLACED SCREWS IAW ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE 2L74 4F RT4A25 20030923001822003092300182EU 2003 9 23 AALA20030844 120030809A3233125505 ACTUATOR FOKKERF28 F28MK0100 4990807EU NLG INOPERATIVE A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW211463A 11483 DURING FLIGHT NOSE GEAR DOOR LOCK INDICATOR KEPT SWITCHING ON AND OFF AGAIN. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED NLG DOOR UPLOCK ACTUATOR. ADJUSTED NR 2 SENSOR TARGET. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2L72 4F RT 20030923000642003092300064WP 2003 9 23 DHL2003604713 120030602A534037540322N FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT FITTING CRACKED AT STA 1170.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040122000862004012200086EA 2004 1 22 A6WA200340195 120031221A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE SCRATCHED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 LEFT SIDE FUSELAGE SKIN SCRATCHES FS 280 TO FS 295, STRINGER 25L TO STRINGER 26L. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SECTION OF SKIN, COMPLYING WITH HFEC TO ENSURE CRACK EXIST AND INSTALLING A NON-FLUSH PATCH IAW CRJ SRM 53-00-31 REPAIR NR 1 REO 601R-53-21-410 REV A. (M) 2L72 4F RTA21EA 20040128002002004012800200NM 2004 1 28 SWA2004F00001 120031031A5744654792328 SPAR BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE WING CRACKED D SWAAO OTHER O OTHER NRNOT REPORTED 1 NM01379SW 26585 CRACKED AT O/B AFT FLAP TRACK LOWER ATTACH HOLES. 2L72 4F4 FRTA16WE E2GL 20031015000292003101500029EA 2003 10 15 ASOA03430 120030910A5300 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE FLOORBEAM VERTICAL ANGLES AT FS 484, LBL AND RBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOORBEAM VERTICAL ANGLES AT FS 484, LBL AND RBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20031021002582003102100258NM 2003 10 21 03FDEA01597 120030920A5270 DOOR BOEING727 727200 138407ENM ZONE 700 FALSE INDICATIONA FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25240FE 20978 RED GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION AND HANDLE PLACED IN OFF POSITION. LIGHT EXTINGUISHED WHEN GEAR HANDLE PLACED IN UP POSITION. COMPLIED WITH ALL APPLICABLE CHECK LIST. PUT IN GEAR PINS, CYCLED GEAR DOORS, ALL INDICATIONS NORMAL, REF PER MM 32-12-000- 0. REMOVED GEAR PINS. 2L73 4F RTA3WE 20031021002792003102100279NM 2003 10 21 CALA0300537 120030919A5730 SKIN BOEING757 757224 1384958NM RROYCERB211 RB211* 54555NE LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717128 27567 INSPECTION FOUND AN 8 INCHES CRACK IN LT WING FIXED LEADING EDGE SKIN AT OSS 421-471. THE SKIN WAS REPAIRED IAW ECRA 5721-01010, REV. D. 2L72 4F4 FRTA2NM A12EU 20031021002232003102100223SO 2003 10 21 SIMA200325306 120030902A531514522460013 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21717AE 145272 ABI - DURING AN IMBV INSPECTION, THE GALLEY FLOOR CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER BEAM AND INSTALLED NEW BEAM. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, 51-40-02, AND 51-40-04 AND CPM 51-21-04. (M) 2L72 4F RTT00011AT 20031022001592003102200159SO 2003 10 22 C2XA03SH346 120030924A542014576631622 STIFFENER EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL NR 2 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED ALONG THE ENTIRE RADIUS. MAINTENANCE REMOVED THE DAMAGED AFT STIFFENER AND REPLACED IT WITH A NEW AFT STIFFENER IAW WITH EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031023000342003102300034NM 2003 10 23 UPS03441258 120030907A53107075T60063IN SHEAR TIE BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C AFT CARGO COMPT- BELOW FLOOR SUPPORT FRAME LOWER SHEAR TIE PLATE FOUND CRACKED AT STA 1880 LT SIDE STRG 45L. SHEAR TIE REPAIRED IAW SRM 53-10-04 FIG 41 AT AFT CARGO COMPT STA 1880 BETWEEN S45L. 2L74 4F4 F A20WE E20EA 20031029000662003102900066 2003 10 29 ASAA0380544 420030728A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 PREFLIGHT CHECK, FORWARD PAX ENTRY L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20031027000692003102700069CE 2003 10 27 8544318 120030827A2720 BOLT RAYTHN BEECH 1900 1900D 1154162CE CONTROL HORN LOOSE A JJBAK NONE O OTHER ININSP/MAINT 1 EA01854CA4920 672 UE399 DURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE. 2L72 4T RTA24CE 20031027001032003102700103NM 2003 10 27 ASAA02402JJ 120030412A53306545775 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND GOUGE ON FUSELAGE SKIN. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20031022001362003102200136NM 2003 10 22 2003UALA00694 120030918A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 DENTED FUSLAGE SKIN AT BS 311 BELOW STR 18R REQUIRES REPAIR. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031118000622003111800062NM 2003 11 18 QXEA200301223 120031006A3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 300 INTERMITTENT A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09347PH 480 ON FLIGHT 2209 DURING CLIMBOUT AFTER ROTATION, LEFT STALL CAUTION LIGHT ILLUMINATED BRIEFLY THEN EXITING. SEVERAL MINUTES LATER LEFT STALL CAUTION LIGHT ILLUMINATED A SECOND TIME AND WENT OUT. FLIGHT VMC. PERFORMED FUNCTIONAL TEST OF LEFT HAND STALL WARNING IAW DHC-8 MM TASK 27-33-00-720-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031120001272003112000127NM 2003 11 20 AWXA200301452 120031104A531069353509 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT SHEAR TIE AT BS 500, STR 28 LT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 500, STR 28 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PART IAW SRM 51-40-02 PG 2-4, 26 & 38 FIG 3 & 38. 2L72 4F RTA16WE 20040204000112004020400011SO 2004 2 4 C2XA03CL194 120031129A2120 SMOKE EMB 145 EMB145 3260210SO COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2713968 145138 CLE) FLIGHT NR 3230, THE CREW REPORTED THE COCKPIT AND CABIN FILLED WITH SMOKE ON DESCENT INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 1 AND NR 2 BLEED AIR SYSTEM,THE NR 1 AND NR 2 ENGINES AND APU. NO DEFECTS WERE FOUND. MAINTENANCE SUSPECT GLYCOL ODOR. 2L72 4F RTT00011AT 20040212000642004021200064NM 2004 2 12 690A120903MT 220031209A72008957202 ENGINE GULSTM690TP 690A 0141722SW GARRTTTPE331TPE3315251K NM SEIZED B JBZRO OTHER O OTHER TXTAXI/GRND HDL 1 WP27677WA3604 143 11243 P06472 AFTER SHUTDOWN THE PROPELLER WAS BEING TURNED THROUGH BY HAND WHICH IS STANDARD PROCEDURE FOR TPE331-5'S. THE PILOT NOTICED A RUBBING NOISE AND THE PROP BECAME HARDER TO TURN. LATER THE PROP COULD NOT BE TURNED. 1H72 3T4 T 2A4 E2WE 20031103001252003110300125NM 2003 11 3 03FDEA01734 120031008A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG SURFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031107001192003110700119NM 2003 11 7 ASAA0310487 120030526A5330654576939 SKIN PANEL BOEING737 737290C 138448VNM FUSELAGE BULGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 520, STRINGER 27L-28L BULGING. REMOVED DAMAGED AREA AND REPAIRED SKIN PANEL PER EA. (M) 2L72 4F A16WE 20030918000562003091800056NM 2003 9 18 DL76L030712 120030801A5753 WEDGE BOEING767 767332 1382001NM LT WING TE FLAP DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27178DN 25143 LT WING INBOARD AFT FLAP TE WEDGE DISBONDED. REPAIRED PER ER/A 423265-14 2L72 4F RTA1NM 20030918000702003091800070NM 2003 9 18 NACA20030101 120030801A2611 WARNING LIGHT BOEING727 727100 1384036NM MLG FIRE MALFUNCTIONED A NACAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AL03930FT 19387 AFTER TAKE-OFF THE WHEEL WELL FIRE WARNING ILLUMINATED AND BELL SOUNDED. BOTH EXTINGUISHED UPON GEAR EXTENSION. CREW REPORTED HEAVY BRAKING AT PAEN. INSPECTED WHEEL WELL AND LOOPS. NO EVIDENCE OF FIRE NOTED. OPERATED WHEEL WELL FIRE WARNING TEST MULTIPLE TIMES WITH NO DEFECTS. 2L73 4F RTA3WE 20030918001432003091800143EA 2003 9 18 2003F00521 220030805A855077852 OIL FILTER PIPER PA32 PA32300 7103212SO LYC O540 IO540K1G5 41532EA HARTZLHCC2Y HCC2YK1 GL ENGINE CRACKED A O OTHER O OTHER NRNOT REPORTED 1 AL05666EB42 42 327940115 RL1694248A CH36382B CRACK FOUND IN OIL FILTER ASSY CAUSING OIL LEAK ON NEWLY OVERHAULED ENGINE WITH ONLY 42.3 HOURS. 1L71 3O3 O A3SO 1E4 5 CP920 20030919000042003091900004GL 2003 9 19 00656686 320030321A6111L104DSZ BLADE BCRAFTHB HONEYBEEHB 1110102WP PWA PT6 PT6* 52043EA MCAULY5JFR365JFR36C1003 GL PROPELLER CORRODED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 920485 PROPELLER BLADE HAS CORROSION ON BLADE 1H71 3O3 T 4A11 E2NE 6 CP15NE 20031010000562003101000056NM 2003 10 10 03FDEA01561 120030918A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 N00560 2 DENTS IN 3.5 INCHES AREA, ON FWD CARGO FRAME BS 560 AT STR 24L. **SD** COMING 2L73 4F RTA3WE 20031009000682003100900068EA 2003 10 9 SWIA200312392 120030906A2760 PCU CNDAIRCL600 CL6002B19 1900309EA LT OB SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07459SW1246 1246 MAL6299 7782 SPOILERON FAILS DURING TAKEOFF AND LANDING ROLL (STATUS MESSAGE). REMOVED AND REPLACED LEFT OUTBOARD SPOILER PCU IAW 27-62-01. OPS AND LEAK CHECKS GOOD. 2L72 4F RTA21EA 20040112002682004011200268EU 2004 1 12 AALA20031464 120031222A3350P4010049 POWER SUPPLY AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2190070 513 AFT COACH AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY FOR AFT COACH AREA EMERGENCY LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2L72 4F RTA35EU 20040114000672004011400067NM 2004 1 14 DLM88030982 120031106A3350D339101295 BATTERY PACK DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27934DL 49721 COCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED FWD BATTERY AND BATTERY PACK ASSY B5-23 PER M/M, CHECK'S OK. 2L72 4F RTA6WE 20031124000802003112400080WP 2003 11 24 DHL2003807535 120031024A572036169622 CLIP DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NR 4 MAIN TANK INTERNAL PART CLIP CRACKED AT STA XRS 172.000, S-73 (REF ACCESS DOOR 505D). REMOVED AND REPLACED CRACKED CLIP ON NR 4 MAIN TANK INTERNAL PART STA XRS 172.000 S-73 (ACCESS DOOR 505D) IAW SRM 51-1-20D. FOR LEAK CHECK SEE NR 1482. 2L74 4F RT4A25 20031126000492003112600049NM 2003 11 26 03FDEA01980 120031125A2782 CONNECTOR BOEING727 727200 138407ENM L/E SLAT CONTAMINATED A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25284FE 22621 AFTER INITIAL TAKEOFF ON FLAP RETRACTION GOING FROM FLAPS 2 TO FLAPS 0. NR 4 LED SLAT WOULD NOT RETRACT. RETURNED TO PHL, HAD TO GO TO FLAPS 5 TO GET GREEN LIGHT AND NORMAL POSITION. FOUND MOISTURE IN NR 4 LEADING EDGE SLAT ACTUATOR CONNECTOR. CLEANED SAME. OPS CK'S OK. NUMEROUS CYCLES PER M/M 27-82-011-4. AIRCRAFT OK FOR FURTHER SERVICE. 2L73 4F RTA3WE 20040311000492004031100049NM 2004 3 11 ASAA0310128 120030310A53156554913502 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 947, LEFT BUTTOCK LINE 44, RIGHT BUTTOCK LINE 54 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20031215001902003121500190WP 2003 12 15 AALA20031196 120031030A3350P401005111 MODULE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21241AA 49254 DEN - DURING OVERNIGHT MAINTENANCE FOUND ESCAPE PATH EXIT LIGHT AT RIGHT AFT OVERWING DOOR INOPERATIVE. REPLACED LOWER BATTERY MODULE AT STATION 900. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031219001722003121900172EA 2003 12 19 QXEA200301520 120031208A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 PDX- CHIMNEY AT FORWARD ENRTY WAY TO BAGGAGE COMPARTMENT HAS DAMAGED WEBBING. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20031219001812003121900181EU 2003 12 19 MALA030525 120031208A5240 DOOR SAAB SF340 340B 7860101EU LAV SERVICE OPEN A MALAA UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CRCRUISE 1 GL15414XJ 340B414 DURING FLIGHT 2917, AIRFRAME VIBRATION FELT ABOVE 190 KNOTS. AIR RETURN TO DTW FOR INSPECTION. MAINTENANCE FOUND LAVATORY SERVICING DOOR PANEL OPEN, RESECURED. PERFORMED VISUAL INSPECTION OF EXTERIOR OF A/C FOR DISCREPANCIES, NONE NOTED. ALL CHECKS GOOD. 2L72 4T RTA52EU 20031231000872003123100087WP 2003 12 31 GTIA030927 120031110A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND CABIN FLOORBOARD AT FS 200-260 CORRODED INSERTS MARKED. DAMAGE FORWARD EDGE SEALER. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040106001532004010600153NM 2004 1 6 DHL2003780014 120031217A5270 SWITCH BOEING727 727223 1384074NM PAX DOOR OUT OF ADJUST A DHLAK NONE N FALSE WARNING LDLANDING 1 SO01780DH 22006 FORWARD ENTRY LIGHT ILLUMINATED AFTER LANDING. LANDING WAS SMOOTH. ADJUSTED DOOR UNLATCH SWITCH IAW BMM CHAPTER 52-11-01, OPS CHECKED GOOD ON GROUND. 2L73 4F A3WE 20040106000612004010600061SO 2004 1 6 SWIA200312688 120031211A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO T/E FLAP FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07301YV5 5 120301 NACELLE FLAP DISAGREEMENT. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW 27-50-08. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031015000612003101500061NM 2003 10 15 USAASB03155 120030827A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US 23315 CLT - MAINTENANCE REPORTED THE CABIN OVERHEAD BIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT BATTERY PACKS. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040105001662004010500166CE 2004 1 5 AMWA106 120031216A1430 FASTENER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 105 WERE FOUND TO HAVE EVIDENCE OF CORROSION. 2L72 4T RTA24CE 20040109000302004010900030NE 2004 1 9 MEX2003493 220031016A7200 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE LEFT OUT OF TRIM W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23216AM 49586 CAPTAIN REPORTED THAT AFTER ENGINES STARTING READINGS IN LT ENGINE WERE OUT OF LIMITS N2 AND EGT`S RISE TO 480. TECHNICAL PERSONNEL PERFORMED TRIM TO LT ENGINE AND IT WAS TESTED IAW MM 73-2-01, BEING PARAMETERS BETWEEN THEIR OPERATIONAL LIMITS.(K) 2L72 4F4 FRTA6WE E2EA 20040121000102004012100010NM 2004 1 21 03FDEA02263 120031226A5710ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING O/B FLAP I/B HINGE FITTING O/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031126000282003112600028EU 2003 11 26 MALA030498 120031028A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE BENT A MALAK NONE O OTHER ININSP/MAINT 1 GL15434XJ 340B434 DURING 4K INSPECTION IN LCQ, RIGHT FRAME STA 686 RBL 32 WL 72 FRAME BENT. VENDOR FABRICATED AND INSTALLED L-ANGLE FRAME REPAIR IAW MESABA EO 553152 DATED 02 MAY 03. A/C RELEASE DATE 11/18/03. 2L72 4T RTA52EU 20031202001312003120200131EA 2003 12 2 ASOA03512 120031015A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO OPEN FROM THE OUTSIDE. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031204001182003120400118WP 2003 12 4 UPS03841436 120030930A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C3 FLOORBEAM UPPER FWD FLANGE CORRODED FS 1300 LBL 12. REMOVED CORR FROM UPPER & LOWER SURFACE OF FLOORBEAM FLANGE, OUT OF LIMITS IAW DC8 SRM 51-1-8 & 53-2-0; FABBED RPR ANGLE AND STRAP IAW DC8 SRM TR 53-124. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE AND STRAP IAW DC8 SRM TR 53-124. 2L74 4F RT4A25 20040123000402004012300040CE 2004 1 23 CGO2003F00009 120031017A29101225802571 LINE BEECH 2000 2000 1152000CE PWA PT6 PT6* 52043EA HYD SYSTEM CRACKED B CGORK NONE K FLUID LOSS ININSP/MAINT 1 GL038158X1807 NC42 DURING SCHEDULED INSPECTION NOTED HYDRAULIC FLUID LEAK FROM HYDRAULIC LINE CONNECTING POWER BRAKE SYSTEM FILTER ASSY. TO SYSTEM ACCUMULATOR. FURTHER INVESTIGATION REVEALED TUBING TO BE CRACKED NEXT TO B NUT FITTING. POSSIBLE CAUSES MAY INCLUDE TUBING MISALIGNMENT OR OVERTORQUING OF B-NUT AT SOME POINT, RESULTING IN FATIGUE CRACKING. TECH NEEDS TO FOLLOW PROCEDURES IN MM WHEN REINSTALLING TUBING AND HOSE CONNECTIONS. 1L72 4T3 TRTA38ACE E2NE 20031208000222003120800022NM 2003 12 8 03FDEA01962 120031121A5754 STRUCTURE DOUG MD11 MD11 3023602NM NR 5 SLAT CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT OUTBOARD FLAP FOUND VANE TO TRACK ATTACHMENT NR 5 WITH SLOT CORRODED AS MARKED. RT OUTBOARD FLAP VANE TO TRACK ATTACHMENT NR 5 CORROSION REPAIRED AS PER FEDEX EA 1-5750-74257, WING RT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20031209000162003120900016 2003 12 9 PCAA0310132 420031027A3442071013190030 TRANSCEIVER DHAV DHC8 DHC8102 2809003NM WX RADAR SYSTEM FAILED A PCAAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 EA13824EX254 387 WHILE IN CRUISE FLIGHT AIRCRAFT 824EX, FLIGHT 3648 FROM BUFFALO NEW YORK TO BRADLEY, CT. THE WEATHER RADAR FAILED, CAUSING THE FLIGHT TO BE DIVERTED. MAINTENANCE REMOVED AND REPLACED THE RADAR RECEIVER TRANSMITTER AND OPERATIONAL CHECKS WERE GOOD ON THE GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031210000552003121000055NM 2003 12 10 03FDEA02091 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 ATTACHED HORIZONTAL WEB FOUND WITH 03 EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 ATTACHED HORIZONTAL WEB 3 CRACKED LOCKBOLT COLLARS REMOVED AND REPLACED AS PER SRM 51-32-01 VOL. II AND SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20031211000452003121100045NM 2003 12 11 P5CA0300981 120031109A3260 CONNECTOR BOEING747 747200 1384847NM E/E BAY DAMAGED A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23524UP 21446 CAPT'S GLIDE SLOPE IND OSCILLATES DURING APPROACH. REPAIRED RACK CONNECTOR AT ALT GEAR LOGIC MODULE PER MM 32-61-05, OPERATIONAL CHECK OK PER MM 34-31-00. 2L74 4F RTA20WE 20030923000532003092300053WP 2003 9 23 DHL2003604726 120030615A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD ACCY COMPT FRAME CRACKED 1.500, STA 55.000, L-24R . TRIMMED OUT CRACKED FRAME SEGMENT IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FRAME SEGMENT (7075-T6 AL0.071) AND SPLICE ANGLES (02 EA) (7075-T6 AL0.071) IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. PERFORMED HEAT TREATMENT TO FRAME SEGMENT AND NEW SPLICE ANGLES IAW SRM 51-1-1, DPS 7.00-1. CLEANED, TREATED AND PRIMED FRAME SEGMENT AND NEW SPLICE ANGLES IAW SRM 51-1-8B. INSTALLED FRAME SEGMENT AND SPLICE ANGLES WITH NEW FASTENERS IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040129000672004012900067EA 2004 1 29 SWIA200312739 120031230A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07951SW 7795 WHEN DEPLOYING FLIGHT SPOILERS SHARP LT ROLLING MOMENT AND THEN LEVELED OUT. WHEN RETRACTING SPOILERS, ALSO A MOMENTARY SHARP ROLLING MOMENT. NO FAULTS FOUND. CYCLED SPOILERS MANY TIMES IAW MM 27-61-00. COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA21EA 20040203000742004020300074WP 2004 2 3 ASAA0380558 120030819A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 RNO LINE CHECK, FOUND PORTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040205000532004020500053EA 2004 2 5 ASOA03673 120031225A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA AIR DISTRIBUTIONDIRTY A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11827AS 7212 FLT 4529 - DURING CLIMB-OUT FROM ATL-MGM, THE CREW NOTICED A BURNING ODOR COMING FROM THE LEFT PACK. THE ODOR BEGAN TO DECREASE WITH THE POWER SET TO IDLE DURING DESCENT. THE AIRCRAFT LANDED SAFELY IN MGM. MAINTENANCE REMOVED AND REPLACED THE LEFT COALESCER BAG AND CLEANED OIL OUT OF THE AIR CYCLE MACHINE CANISTER. OPS CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040301000822004030100082WP 2004 3 1 DKE2004F00000 120030516A2611 BATTERY DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE SMOKE DETECTOR MALFUNCTIONED A DKEBO OTHER N FALSE WARNING NRNOT REPORTED 1 SO15112PS 0750 47013 ATC WAS NOTIFIED OF A FIRE WARNING LIGHT ACTIVATION. FLIGHT DIVERTED TO NEAREST SUITABLE AIRPORT. CARGO SMOKE DETECTION LIGHT IN THE FORWARD BAGGAGE COMPARTMENT ILLUMINATED WHILE ENROUTE. THE ONLY ITEMS IN THE COMPARTMENT WAS A FLY AWAY KIT. THE FLIGHT MANUAL WAS CONSULTED AND EMERGENCY PROCEDURES FOLLOWED. FLIGHT WAS MET BY THE FIRE DEPARTMENT UPON LANDING. ALL CARGO COMPARTMENTS WERE CHECKED BY THE CREW AND THE FIRE DEPARTMENT AND NO SIGNS OF FIRE OR SMOKE WERE DETECTED. ALL ITEMS WERE REMOVED FROM BOTH CARGO BAYS. (SO15200324766) 2L72 4F4 F A6WE E2EA 20031212000532003121200053SO 2003 12 12 CHQA000428 120031105A3350 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260 145128 DURING TEST OF EMERGENCY EVACUATION LIGHTS, FLOOR EMERGENCY LIGHTING FROM 402 12 BACK DID NOT ILLUMINATE. RESECURED EMERGENCY LIGHT CONNECTION IAW EMB 145 PRACTICES. 2L72 4T RTT00011AT 20031215000162003121500016NM 2003 12 15 QXEA200301430 120031115A5330 ICE SHIELD BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX- TWO DENTS FOUND ON LEFT HAND FUSELAGE LOCATED AT ICE SHIELD EDGE ABOVE WINDOW AND OTHER IS 5 INCHES FORWARD OF FIRST DENT. REPAIRED IAW HORIZON AIR EA 6-53-315. 2H72 4T RTA13NM 20031215000572003121500057NM 2003 12 15 2003UALA00840 120031106A5753 HINGE FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE T/E FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29656UA 25394 RIGHT WING INBOARD FLAP AT CENTER HINGE FITTING IS CRACKED BROKEN. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING PER SRM 51-40-2 AND 57-53-02, FIG 201. 2L72 4F4 FRTA1NM E24NE 20040401001532004040100153CE 2004 4 1 WIW2004F00000 120030912A322026430181 PIN CESSNA208 208 2073702CE PWA PT6 PT6A11 52043NE NLG STRUT SEPARATED B WIWRO OTHER O OTHER NRNOT REPORTED 1 WP07208JW 20800166 NOSE LANDING GEAR STRUT WAS RESEALED 5/1/01 SO FAILURE OCCURED AFTER THAT TIME. AIRCRAFT WAS HAVING RECURING SHIMMY PROBLEMS WHICH LED TO THE STRUT DISASSEMBLY FOR INSPECTION. DURING INSPECTION THE LOWER PLUG WAS FOUND SEPARATED FROM METERING PIN ASSEMBLY CAUSING THE DAMPENING EFFECT OF THE STRUT TO BE LOST. CONDITION OCCURED DURING NORMAL OPERATION. UNKNOWN PROBABLE CAUSE AND NO RECOMMENDATIONS TO PREVENT RECURRENCE. 1H71 3T3 TNTA37CE E4EA 20040308001322004030800132NM 2004 3 8 ASAA0310245 120030327A71102024T3040 SKIN BOEING737 737298C 1384490NM NR 1 COWLING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - FOUND DURING D-CHECK, NR 1 ENGINE COWL SKIN AT NACELLE STATION 108.60-117.60 GOUGED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040316000922004031600092WP 2004 3 16 ASAA0380316 120030414A53209936534107 SHIM DOUG DC9 DC983 3022083WP DOOR SILL CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, PASSENGER L1 DOOR SILL DRAIN SHIM CORRODED. REPLACED SHIM PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040520002462004052000246SO 2004 5 20 ZIAA04059 120031208A53208122591 FLOOR SUPPORT LKHEED188 188C 5262604SO FUSLEAGE CORRODED A ZIAAK NONE O OTHER ININSP/MAINT 1 GL23286F 1146 YIP - FOUND RIGHT WING CENTER SECTION RBL 40 AT NR 1 PLANK UPPER SURFACE CORROSION AT FLOOR SUPPORT BRACKET. REMOVED CORROSION AND TREATED AREA PER L-188 SRM 51-2-14. MATERIAL REMOVED IS PAST NEGLIGIBLE LIMITS. REPAIRED AREA PER L-188 SRM 57-2-1, PAGE 19. REMOVED AND REPLACED CORRODED FLOOR SUPPORT BRACKET. (M) 2L74 4T 4A22 20031216000882003121600088EU 2003 12 16 03335317 120031201A33503022471 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27317UE 41031 DURING INSPECTION THE RT AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031212001142003121200114NM 2003 12 12 SWAA032448 120031105A53156540804 FLOORBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040510000372004051000037SO 2004 5 10 A8O2004F00000 120031214A28201159P201061 LINE GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY50614 54519EU FUEL SYSTEM LEAKING E A8OAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO1141AV 61 FUEL SYSTEM/FUEL DUMP SYSTEM AFFECTS FUEL FLOW OR LEAKAGE DURING FLIGHT. EMERGENCY ACTION TAKEN DURING FLIGHT DUE TO A COMPONENT OR SYSTEM MALFUNCTION. UPON ROTATION, THE LEFT FUEL FILTER LIGHT CAME ON. THE CREW ACTED FOLLOWING THE EMERGENCY PROCEDURE, DECLARED AN EMERGENCY AND LANDED. WHEN THE AC TAXIED TO TERMINAL, LINE PERSONNEL ALERTED THE CREW TO A SUBSTANTIAL LEAK COMING FROM THE CENTERLINE OF THE AC. ALERTED ON-CALL MAINTENANCE. UPON INVESTIGATION FOUND THE LT ENGINE FUEL LINE RUPTURED. DETERMINED BY APPLYING PRESSURE TO FUEL SYSTEM. THIS WAS NOT VISIBLE TO NAKED EYE. DUE TO STAINLESS BRADED COVERING ON THE LINE. ORDERED NEW LINE FROME MFG. RECEIVED NEW LINE, INSTALLED, LEAK CHECK GOOD. 2L72 4F4 FRTA12EA E2EU 20031215000342003121500034NM 2003 12 15 SWAA032511 120031113A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, BETWEEN STRINGERS 24L AND 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031211001672003121100167EA 2003 12 11 ASOA03536 120031025A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A ASOAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO11828AS 7213 FLT 4600 - DURING APPROACH INTO YOW FROM ATL, THE CREW SELECTED THE FLAPS TO TWENTY DEGREES AND AT ELEVEN DEGREES RECEIVED A FLAPS FAIL CAUTION MESSAGE, WITH THE FLAPS REMAINING AT ELEVEN DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE FLAPS WERE SELECTED TO EIGHT DEGREES AND THE AIRCRAFT LANDED SAFELY IN YOW. LOCAL MAINTENANCE INSPECTED AND RESET THE FLAPS IAW AD 98-20-01. ASA MAINTENANCE REMOVED AND REPLACED THE FLAPS POWER DRIVE UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031217000692003121700069WP 2003 12 17 DHL2003802502 120031107A5711 FRAME DOUG DC8 DC873 302199CWP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LT WING L/E FRAME CRACKED 0.500 STA XFS 772.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031217001112003121700111NE 2003 12 17 2003UALA00849 220031111A7230 BLADE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COMPRESSOR FAILED A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29815UA 867 CREW REPORTED LOUD BANG ON T/O ROLL AT APPROXIMATELY 40 KNOTS. TAKEOFF ABORTED. ENGINE WAS REMOVED FOR TEARDOWN AND INVESTIGATION, WHICH REVEALED A HIGH COMPRESSOR BLADE FRACTURE WITH SIGNS OF FOREIGN OBJECT DAMAGE (FOD) AT FRACTURE INITIATION SITE. THIS FRACTURE IN TURN LED TO COMPRESSOR FAILURE WHICH INITIATED AN ENGINE SURGE. THIS ENGINE FAILURE HAS BEEN ATTRIBUTED TO FOD. 2L72 4F4 FRTA28NM E40NE 20040419000052004041900005WP 2004 4 19 ASAA0380842 120031222A5320991195337 SUPPORT ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND AIRSTAIR LEFT SUPPORT ANGLE ABOVE TORQUE TUBE IS CRACKED. REPLACED SUPPORT ANGLE. (M) 2L72 4F RTA6WE 20040713000932004071300093EU 2004 7 13 AALA20031219 120031105A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2180057 465 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS AT DOOR 2R AND RIGHT FIRST CLASS SEAT LIGHTS INOPERATIVE. REPLACED DOOR 2R AND RIGHT FIRST CLASS SEAT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20050223000952005022300095 2005 2 23 ERAA097509 420030109A3440 RESISTOR SKRSKYS61 S61N 8142104NE RADAR INDICATOR OVERHEATED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03563EH 1575 61808 UNIT SMOKED UPON INSTALLATION. UNIT WORKED GOOD. FOUND TWO OVERHEATED RESISTORS. REPLACED DAMAGED RESISTORS AND TESTED. . 2G72 4U 1H15 20030813001942003081300194NM 2003 8 13 SWAA031562 120030715A57546573714 SKIN BOEING737 7373H4 1384600NM NR 6 L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/2D CHECK, FOUND NR 6 L/E SLAT CRACKED IN LOWER SKIN OUTBD EDGE. REMOVED AND REPLACED NR 6 L/E SLAT PER MM. 2L72 4F RTA16WE 20030815000412003081500041SW 2003 8 15 HEEA088618 120030218A243230703001 BATTERY BELL 412 412 1182202SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 MASTER BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030820000462003082000046NM 2003 8 20 03FDEA01135 120030723A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT O/B FLAP (FLAP SIDE) - I/B HINGE BRACKET I/B ACTUATOR ATTACHMENT HOLE FOUND CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE BRACKET I/B ACTUATOR ATTACHMENT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030820000732003082000073NM 2003 8 20 03FDEA01117 120030719A2916 RESERVOIR DOUG MD11 MD11 3023602NM HYD SYSTEM LEAKING A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25607FE 48547 DURING CRUISE, HYD 3 ELEV OFF LEVEL 1 LIGHT CAME ON AT 4.4 GAL, INDICATING THE 3-2 NRMP INOP. ONE HOUR LATER THE HYD 3 OFF LEVEL 1 ALERT LIGHT AT 2.5 GAL, CAME ON. TWO HOURS LATER THE HYD 3 FAIL LEVEL 2 ALERT LIGHT CAME ON AT 1.0 GAL. RESET ALT GEAR EXTENSION HANDLE REF MM 32-32-00-5, FOUND RELIEF VALVE ON NR 3 RESERVOIR LEAKING EVEN WHEN HYD RESEVOIR WAS DEPRESSURISED. THE RESERVOIR WAS DRAINED OF REMAINING FLUID AND RELIEF VALVE WAS CLEANED AND REINSTALLED. THE ENGINES WERE RUN REF JRH ALL TEMPERTURES AND PRESSURES WERE NORMAL 42 DEG CELSIUS, INSPECTED RELIEF VALVE AND NO LEAK WAS NOTED. ALL THE FLIGHT CONTROLS WERE OPERATED, NO FURTHER LEAKS NOTED. AC OK FOR SERVICE. 2L73 4F RTA22WE 20030820001722003082000172NM 2003 8 20 CALA0300382 120030712A5743 SUPPORT ANGLE BOEING737 7373T0 1384582NM LT MLG GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND LT MLG STAB LINK SUPPORT ANGLES GOUGED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030821000772003082100077NM 2003 8 21 03FDEA00863 120030606A5210 SKIN BOEING727 727200 138407ENM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25487FE 21490 FWD ENTRY DOOR FWD UPPER CORNER OF DOOR SKIN IS CRACKED JUST BELOW UPPER GATE. REPAIRED FWD ENTRY DOOR, AFT UPPER CORNER OF DOOR SKIN, IAW SRM 52-00-2, 52-00-3, FIG 4. 2L73 4F RTA3WE 20030821000892003082100089NM 2003 8 21 03FDEA00806 120030523A5753ARC198414 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP - HINGE AFT FITTING FOUND INBOARD ACTUATOR BORE WITH MINOR CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69255 - WINGS - RIGHT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030328000282003032800028EU 2003 3 28 03FDEA00353 120030328A5530A5357000800600 PANEL AIRBUS310 A310 EU VERTICAL STAB DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 VERTICAL STAB. LE PANEL 321AL DELAMINATED 2L72 4F RTA35EU 20030401000632003040100063EA 2003 4 1 CA030225008 120030215A3230 DRAG BRACE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG CRACKED W O OTHER E VIBRATION/BUFFET LDLANDING 1 CA (CAN) THE AIRCRAFT LANDED NORMALLY AND SHORTLY AFTER, THE NLG TOUCH DOWN, THE CREW REPORTED AN IMPACT FOLLOWED BY A NOISE AND THE NLG COLLAPSED. THE NLG COLLAPSE DUE TO THE DRAG BRACE CRACKED. THE CREW MENTIONNED ALSO A PROBABLE IMPACT WITH A SNOW BANK FOR SEVERAL REASONS: RUNWAY SNOW CONTAMINATION INCONSISTENT (CLEAR , 4 FT AND SNOW BANKS) SIDE OF THE RUNWAY CLEAR FROM SNOW- SNOW GSE ACTIVITY AT A RUNWAY TEE INTERSECTION (JUST AFTER THE LANDING AREA) THE NLG COLLAPSE DUE TO THE DRAG BRACE CRACK. 2L72 4F4 FRTA21EA E15NE 20030401000642003040100064NE 2003 4 1 CA030226001 220030224A7230 COMPRESSOR BOEING767 767375 1385217NM GE CF6 CF680C2B6F 30025NE LT ENGINE STALLED W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CA (CAN) REJECTED TAKE OFF AFTER COMPRESSOR STALL ON THE LT ENGINE AND RISE IN TEMP AT 155 KNOTS, ALL 8 TIRES WENT FLAT (FUSES BLOWED OUT). 2L72 4F4 FRTA1NM E13NE 20030401000662003040100066SW 2003 4 1 CA030227002 120030226A3230A882DL RELAY SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCE4N HCE4N3 NE RT MLG WW BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 32888 (CAN) UPON INSPECTION IN THE RT WHEEL WELL RELAY WAS FOUND DETACHED FROM MOUNTING PLATE AND THE RIVETS ATTACHING THE MOUNTING PLATE TO THE RELAY WERE FOUND SHEARED. THE RELAY AFTER DETACHING FROM THE MOUNTING PLATE WAS FOUND RESTING ON A BANK OF RELAYS LOCATED BELOW IT. NO SUBSEQUENT DAMAGE WAS FOUND DUE TO RELAY FAILURE. RELAY WAS REPLACED. 2L72 4T4 TRTA8SW E4WE 5 CP10NE 20030403001082003040300108NM 2003 4 3 DL72S030268 120030322A335010604503 RELAY BOEING727 727225A 1384077NM EMERGENCY LIGHT FAILED A DALAO OTHER L NO TEST NRNOT REPORTED 1 SO278890Z 21859 EMERGENCY EXIT/FLOOR TRACK LIGHTING ILLUMINATED INFLIGHT MOMENTARILY AND VERY SPARADICALLY. ALL ELECTRICAL INDICATIONS NORMAL. FOUND EMERGENCY LIGHTS NOW COME ON IN ARM POS WITH ANY POWERSOURCE T/S PER WDM. REPLACED CHARGER CONTROL RELAY-R70. EMERGENCY LIGHTS NOW OPERATE NORMALLY. 2L73 4F RTA3WE 20030410000362003041000036NM 2003 4 10 SWAA030612 120030317A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030415000622003041500062NM 2003 4 15 CA030326004 120030323A792128E997 OIL COOLER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 2 ENGINE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA 24650 (CAN) NR 2 ENGINE OIL COOLER FOUND LEAKING FROM COOLING FINS. OIL COOLER REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030424000922003042400092NM 2003 4 24 F3LA200300110 120030228A5320 CHANNEL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED CHANNELS IN FWD CARGO COMPARTMENT CRACKED AT STA. 540, WL 208, BETWEEN LBL 24.5 AND RBL 24.5. FABRICATED AND REPLACED FLOOR SUPPORT PER SRM 51-30-01, FIG. 3, SRM 51-10-02, PARA. 12, SRM 51-20-02, SRM 51-40-02 AND 51-20-01 2L72 4F RTA16WE 20030424001622003042400162SO 2003 4 24 LR7A03017 120030313A5320 BEAM LKHEED382 382G 526414USO FUSELAGE CHAFED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5324 FOUND RT MLG WHEEL WELL SUPPORT ANGLE TO VERTICAL BEAM ATTACH CHAFED AND WORN AT FS 577, RBL 65, WL 236. REPAIRED IAW LAC MEA 382-53-03-011. NR 2084. 2H74 4T A1SO 20030424001972003042400197EA 2003 4 24 SWIA200311848 120030323A2721 SWITCH CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07917SW 7641 RUDDER TRIM KNOB LOOSE - WILL NOT OPERATE RUDDER TRIM. TIGHTENED SWITCH AND RESOLDERED CONNECTIONS. OPS CHECK GOOD OF SWITCH PER CRJ MM 27-22-00. 2L72 4F RTA21EA 20030424002082003042400208WP 2003 4 24 UPS03840368 120030312A5310 FITTING DOUG DC8 DC873F 302199FWP EMPENNAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, EMPENNAGE L10 LT END FITTING CRACKED FROM 1768-1773. PERFORMED HFEC IAW NDT SPM 06-10-01, .001 CRACK FOUND ON FITTING. REMOVED OLD FITTING TO FOM. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030425001152003042500115NM 2003 4 25 DLM90030236 120030312A3231 DOOR DOUG MD90 MD9030 3023690NM NLG OPEN A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27904DA 53384 AIRCRAFT HAD AN AIR TURNBACK. UPON GEAR RETRACTION, NOSE GEAR MADE A LOUD NOISE AND CONTINUED TO SPIN. NO GEAR OR GEAR DOOR LIGHTS. GEAR ALSO VIBRATED. ONCE AT GATE MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR OPEN. RESECURED NOSE GEAR DOOR. 2L72 4F RTA6WE 20030430001712003043000171NM 2003 4 30 SWAA030863 120030416A335065C34691 LIGHT BOEING737 7373G7 1384595NM EXIT SIGN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROW NR 2 DEF, ROW NR 9 DEF, ROW NR 11 ABC, ROW NR 14 ABC & ROW NR 18 ABC. SECURED OVERHEAD BIN BULLNOSE EMERGENCY EXITS LIGHTS PER MM. 2L72 4F RTA16WE 20030430002152003043000215NM 2003 4 30 VNAA0304022 120030423A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07430JS1357872 3044 THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY LIGHTS WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030502001872003050200187NM 2003 5 2 AWXA200300413 120030408A5313146N3110184 STRINGER BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 29 LT AT BS 1418 AND 1438, IN AFT CARGO COMPARTMENT. MAINTENANCE REMOVED AIRCRAFT SKIN FROM BS 1400 TO 1460, STR 26 LT TO STR 29 RT; BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED STRINGER 29 LT FROM BS 1410 TO 1455; FABRICATED A NEW SECTION OF REPLACEMENT STRINGER; INSTALLED REPAIR PART AND REMOVED SKIN IAW 757-200 SRM 51-40-02 PG 4-5, 7-8, 11, & 31-32. 2L72 4F RTA2NM 20030505001492003050500149NM 2003 5 5 03FDEA00493 120030417A2612473925 CONTROL UNIT BOEING727 727100 1384036NM CARGO FIRE DETECFAILED A FDEAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO25189FE 19082 DURING TAXI INTO IND, LWR AFT CARGO SMOKE ALARM ACTIVATED WITH AFT SMOKE LIGHT AND ARMED LIGHT. PERFORMED CHECKLIST ITEMS, INCLUDING DISCHARGE OF BOTH BOTTLES. NO OTHER INDICATIONS OF SMOKE OR FIRE; SYS TEST INDICATES FAULT IN AFT SYSTEM. REMOVED AND REPLACED LWR AFT CARGO COMP CEU IAW 26-16-012-2. SYSTEM NOW OPERATES NORMAL. 2L73 4F RTA3WE 20030505001882003050500188NM 2003 5 5 03FDEA00500 120030417A5753 FAIRING BOEING727 727200 138407ENM TE FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT OUTBOARD MIDFLAP INBOARD JACKSCREW FAIRING HAS A LOOSE SKIN AND DOUBLER ON SIDE. *S/D* RE-ATTACHED LOOSE DOUBLER WITH 2 EA RIVETS THAT WHERE LOOSE IAW BOEING SRM 51-30-02. 2L73 4F RTA3WE 20030506000322003050600032SO 2003 5 6 SWIA200311884 120030412A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07236SW5971 5971 120312 EMERGENCY LIGHTS EXIT LIGHT ARE INOP ABOVE 5C AND 5A. REMOVED AND REPLACED NR 2 MID EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20030507000502003050700050CE 2003 5 7 AUS20030349 120030322A532050420066175 DOUBLER BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE FUSELAGE WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) DOUBLER WORN THROUGH BY LT WINDSHIELD DEMIST DUCT. 1L72 4T4 T A24CE E4EA 6 C3PNE 20030507000732003050700073CE 2003 5 7 AUS20030365 120030326A534715142142 SEAT TRACK CESSNA337 337 2075702CE CONT O360 IO360C 17025SO MCAULY2AF34CD2AF34C306 GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SEAT TRACK CRACKED IN TWO PLACES. ON REMOVAL OF THE SEAT TRACK ANOTHER CRACK WAS FOUND AT THE CUTOUT FOR THE REMOVAL OF THESECOND ROW OF SEATS. 1H72 3O3 O A6CE E1CE 5 CP5EA 20030509001572003050900157WP 2003 5 9 AMTA200300474 120030407A52101281T10033 ACTUATOR LKHEED1011 1011385115 5265015WP PAX DOOR FAILED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 193B1230 FOUND L1 DOOR FAILS TO CLOSE ELECTRICALLY. REMOVED AND REPLACED L1 DOOR ACTUATOR IAW MM 52-12-01, OPS NORMAL IAW MM 52-12-00. (M) 2L73 4F A23WE 20030513001252003051300125WP 2003 5 13 UPS03840662 120030413A5753565228163 SKIN DOUG DC8 DC873F 302199FWP LT WING TE FLAP GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, LT WING IB. FLAP OB. LOWER SKIN IS GOUGED BEYOND LIMITS APPROX 25 INCHES AFT OF LE. BETWEEN XW101 TO XW 115. REMOVED, FABRICATED AND REPLACED SKIN IAW DWG 5652281,AND SRM. 51-1-21,51-3-0 2L74 4F RT4A25 20030513002992003051300299EU 2003 5 13 ASOA03182 120030425A33507012210 BULB AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11633AS 344 DURING AN 'A' CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030514000432003051400043NM 2003 5 14 PCAA0304071 120030405A33506104789 BATTERY DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DISCHARGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13839EX 226 DCA- FLIGHT 182, CREW REPORTED NUMEROUS FLOOR PROXIMITY EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030515000382003051500038EA 2003 5 15 SWIA200311907 120030303A5411 RIB CNDAIRCL600 CL6002B19 1900309EA RT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 RIGHT PYLON RIB AT FS 605 IS CRACKED AT LOWER FLANGE NEAR OUTBOARD END. FOUND DURING C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-20. P/N 601-37004-86. 2L72 4F RTA21EA 20030515001272003051500127NM 2003 5 15 AWXA200300536 120030423A5320654659210 FLOOR SUPPORT BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT UNDER FLANGE IN AFT CARGO COMPARTMENT BS 859, RBL 3. MAINTENANCE CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR SUPPORT BS 859, RBL 3; FABRICATED A CHANNEL FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW SRM 53-00-53 PG 201-202, FIG 201. 2L72 4F RTA16WE 20030530000252003053000025SW 2003 5 30 HEEA086679 120030522A7120 BEARING BELL 412 412 1182202SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 ENGINE MOUNT HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20030602000972003060200097NM 2003 6 2 SWAA031189 120030527A3350PH22300L LIGHT BOEING737 7375H4 138449DNM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINSCENT STRIP WORN AND CHIPPED IN SEVERAL AREAS. REMOVED AND REPLACED WORN AREAS OF EEPLS STRIP. 2L72 4F RTA16WE 20030604001202003060400120NM 2003 6 4 UPS03440535 120030413A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, SEAT TRACK FOUND CORROSION AT BS 480 - 485 RBL 65. SEAT TRACK REPAIRED AT U/D BS 480 - 530 RBL 65 AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.045 X 1 X 8 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030605000012003060500001SW 2003 6 5 AUS20030426 120030413A291027810321040 LINE SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UA 01514WP HYD SYSTEM CRACKED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS 13479 (AUS) NUMEROUS HYDRAULIC PIPE UNIONS LOOSE. FLAP DOWN HYDRAULIC PIPE CRACKED AT WS 66.5. PIPE UNIONS LOOSE IN THE FOLLOWING AREAS:-1. HYDRAULIC BLEED AIR PIPE UNION AT WS 66.5 LT 2. BYPASS LINE UNION AT WS 81.1 LH3. FLAP UP AND DOWN PIPE UNIONS AT WS 66.5 AND WS 81.1LOSS OF HYDRAULIC FLUID. 2L72 4T4 TRTA5SW E4WE 20030609000192003060900019WP 2003 6 9 ARWA20030214 120030215A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198968U 46069 DURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 400 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 400 IAW STC SA1063SO AND SA1377SO. 2L74 4F 4A25 20030520001482003052000148NM 2003 5 20 2003F00276 120030120A5313 STRINGER BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND STRINGER 9R, FUSELAGE STATION 950C HAS CRACKED STRINGER. FABRICATED, TREATED, PRIMED AND INSTALLED FLANGE AT FUSELAGE STATION 950, STRINGER 9R. (M) 2L73 4F A3WE 20030521001592003052100159WP 2003 5 21 DHL2003604504 120030428A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR L/E FORMER WITH 0.500 INCH CRACK STA XS 491.193. STOP DRILLED AND FABRICATED DOUBLER ANGLE (2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON LT WING CTR L/E FORMER (XS 491.193) IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030523000062003052300006 2003 5 23 2003F00290 420030501A3420HG2010AC03 INDICATOR CESSNA750 750 2076810CE AHRS MALFUNCTIONED A UG8AO OTHER O OTHER NRNOT REPORTED 1 GL235113 7500013 ATTITUDE AND HEADING STUCK IN THE TEST MODE. NR 1 AHRS HAD FAILED. REPLCED NR 1 AHRS AND OPERATION WAS NORMAL. (M) 2L72 4J RTT00007WI 20030619000122003061900012SW 2003 6 19 AC2A086762 120030522A291070012H000Y264 LINE BELL 430 430 1182150SW HYDRAULIC SYS FAILED E AC2AE ENGINE SHUTDOWN K FLUID LOSS NRNOT REPORTED 1 SO07430CT 49089 NR 1 HYDRAULIC SYSTEM PRESSURE LINE FAILURE. REMOVED AND REPLACED LINE , PUMP, FILTERS. 1G72 3U RTH9SW 20030701000122003070100012SW 2003 7 1 HEEA087866 120030617A3411407075035101 STATIC LINE BELL 407 407 1182206SW STATIC/PITOT CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03491PH 53386 STATIC LINE HAS DEVELOPMENT OF CORROSION DUE TO TREATMENT USED DURING MANUFACTURE PROCESS. REPLACED TUBE. 1G71 3U O H2SW 20030707000152003070700015NM 2003 7 7 AUS20030452 120030428A324226123121 BRAKE BOEING737 737832 13844CFNM GE CFM56 CFM56* 13802NE NR 2 FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 MAIN BRAKE FAILED. INSPECTION FOUND SMALL METAL CHIPS AROUND BRAKE AND IN WHEEL HUB. 2L72 4F4 FRTA16WE E2GL 20030707001352003070700135NM 2003 7 7 AWXA200300708 120030618A5210FE12710004 SHEAR PIN AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE PAX DOOR DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28818AW 1375 DURING 8-DAY CHECK FOUND THE R-1 DOOR ASSIST BOTTLE WOULD NOT HOLD PRESSURE. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR DAMPER CYLINDER SHEAR PIN AND PUNCTURE DISK IAW 52-11-14-401, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20030709000792003070900079NM 2003 7 9 377PA0017 120030605A5330 SKIN BOEING737 7373L9 1384470NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05377PA 23718 FUSELAGE SKIN CRACKED AT AFT SIDE OF E&E EQUIPMENT FAN OUTLET. REPAIRED PER SB 737-53-1117. 2L72 4F RTA16WE 20030710000622003071000062NM 2003 7 10 DHL2003721004 120030604A3350 BATTERY PACK BOEING727 727228 1384083NM EMERGENCY LIGHT LOOSE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01721DH 19545 EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR BURNED OUT. RESEATED BATTERY PACK, OPS GOOD IAW M/M 33-50-01. 2L73 4F RTA3WE 20030714000332003071400033NM 2003 7 14 SWAA031405 120030623A3397BR2013 WIRE BOEING737 7375H4 138449DNM EMERGENCY LIGHT DISCONNECTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP INOP. RECONNECTED EEPLS WIRES PER MM. 2L72 4F RTA16WE 20030716000252003071600025NM 2003 7 16 2003F00417 120030314A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 680, STRINGER 23R/24R. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATION 680 STRINGER 23R THROUGH 24R. (M) 2L73 4F A3WE 20030106001292003010600129SW 2003 1 6 ALGA082773 120030102A6420406312100101 BEARING BELL 407 407 1182206SW T/R HEAD WORN H ALGAK NONE O OTHER ININSP/MAINT 1 FS01577AL80 53247 DURING COMPLIANCE OF ASB, FOUND TAIL ROTOR HEAD BEARINGS HAD EXCESSIVE AXIAL PLAY. 1G71 3U O H2SW 20030314000252003031400025NM 2003 3 14 03FDEA00045 120030114A5712ARB2850506 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING NR 16 SLAT TRACK INBOARD STRUCTURAL RIB CRACKED (CRACK LENGTH APPROX 0.5 INCHES). RT WING NR 16 TRACK I/B STRUCTURAL CRACK RIB REMOVED AND NEW RIB INSTALLED AS PER SRM 51-31-01 VOL 2. RIB FABRICATED AS PER DWG ARB 2850. 2L73 4F RTA22WE 20030129000032003012900003SW 2003 1 29 HEEA083912 120030117A6710 BEARING BELL 407 407 1182206SW IDLER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 IDLER PIVOT BEARING WORN. 1G71 3U O H2SW 20030204001122003020400112NM 2003 2 4 SWAA030091 120030114A53306545771 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACK BETWEEN BS 727D AND 727E AT STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030218000182003021800018EU 2003 2 18 03FDEA00113 120030206A2612 WARNING LIGHT AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE CABIN FALSE INDICATIONA FDEAF ACTIVATE FIRE EXT. J WARNING INDICATION APAPPROACH 1 SO25676FE 790 AFT AND BULK SMOKE LIGHT CAME ON DURING LANDING APPROACH AT 1000 FT AGL. FIRED AGENT 1. LIGHT WENT OUT AFTER A SHORT DELAY. FIRE PERSONNEL REPORTED NO EXTERIOR INDICATION OF SMOKE OR FIRE AFTER LANDING. FIRST OFFICER REPORTED MUSTY ODOR PRIOR TO DONNING OXYGEN MASK. AIRCRAFT RELEASED FOR SERVICE IAW MEL/CDL: 26-16-02-B FACT 06FEB03 12:46 REPLACED NR 1 LOWER DECK FIRE EXT BOTTLE. M/M REF. 26-23-11-4-02. ALL CHECKS OK. 2L72 4F4 FRTA35EU E13NE 20030220001822003022000182WP 2003 2 20 ARWA20030202 120030207A324142241 CONTROL BOX DOUG DC8 DC863F 302198FWP ANTI SKID SYS FAILED A ARWAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO19784AL 46135 ANTI-SKID INOPERATIVE. REMOVED AND REPLACED CONTROL BOX IN ACCORDANCE WITH MM 32-43-6. OPERATIONAL CHECKED GOOD IAW MM 33-43-0. 2L74 4F 4A25 20030221000862003022100086NM 2003 2 21 AWXA200300181 120030127A5313140N200216 SHEAR TIE BOEING757 7572S7 1384962NM ZONE 100 - FUSELCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON STRINGER SHEAR TIE AT B.S. 879 BETWEEN STR 28 L/H AND STR 28 R/H. MAINTENANCE REMOVED CORRODED SHEAR TIE B.S. 879; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-01, PG. 3. 2L72 4F RTA2NM 20030224000612003022400061NE 2003 2 24 HEEA084182 220030212A74219550175400 IGNITER SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 IGNITER WORN. 1G72 3U3 U H1NE E19EU 20030304000772003030400077NM 2003 3 4 DL757030095 120030124A5330143N33203 SKIN BOEING757 757232 1384965NM FS 628, S-17L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 FUSELAGE / SKIN / FS 628 / STRG. 16L-18L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH TWO DENTS NEAR FS 628 BETWEEN STRINGERS 16L & 18L. THE DENTS WERE NEAR AND EXISTING SKIN REPAIR DOUBLER FOR A SMALL DAMAGE CUTOUT. THE EXISTING REPAIR WAS REMOVED AND UNDERLYING SKIN INSPECTED. THE DENTS WERE REMOVED WITH CUTOUTS. ALL THREE CUTOUT AREAS WERE REPAIRED WITH A SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 384333-14, REV A. 2L72 4F RTA2NM 20030225000602003022500060SW 2003 2 25 HEEA084282 120030211A6710206001053005 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 FLT CONTROL BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS. REPAIRED. 1G71 3U H2SW 20030227000482003022700048 2003 2 27 HEEA084378 420030211A2350AMS44 KNOB BELL 407 407 1182206SW AUDIO CONTROL STRIPPED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 INTERMITTENTLY PILOT UNABLE TO TRANSMIT TO PASSENGERS. FOUND METAL SHAVINGS INSIDE UNIT, BOTH RX KNOBS AND ICS KNOB BAD. REPLACED AND CLEANED METAL SHAVINGS FROM INSIDE UNIT. BENCH CHECK GOOD. 1G71 3U O H2SW 20030227000972003022700097SW 2003 2 27 HEEA084403 120030212A2140S9276EC5 LINE BELL 407 407 1182206SW HEATER LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03404PH 53188 LINE LEAKING THROUGH WALL. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030228000942003022800094SW 2003 2 28 HEEA084458 120030213A6730206076031023 SERVO BELL 206 206B3 1181506SW FLT CONTROLS LEAKING E O OTHER K FLUID LOSS NRNOT REPORTED 1 SW032275Y17641 3626 CYCLIC AND COLLECTIVE SERVO ACTUATOR IS LEAKING FROM THE EXCLUDER SEALS. IN SHOP FOR REPAIR. 1G71 3U H2SW 20030321001142003032100114NE 2003 3 21 2003UALA00258 220030310A73217791005 FUEL CONTROL BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 WP29546UA8511 8511 25367 717996 NUMBER 1 ENGINE N1 OVERSPEED OF 103 PERCENT FOR 40 SECONDS. N1 PASSED 100.5 REDLINE FOR 42 SECONDS AND REACHED A MAXIMUM OF 103.0. NO OTHER EXCEEDENCES OCCURRED. INITIAL PROGNOSIS IS A MECHANICAL FAULT IN THE FUEL CONTROL UNIT. 2L72 4F4 FRTA2NM E17NE 20030324000772003032400077CE 2003 3 24 AMWA15 120030225A5711 SPAR BEECH 1900 1900D 1154162CE WING CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 UPON A ROUTINE INSPECTION MAINTENANCE DISCOVERED THE RIGHT SPAR CHAFED ON THE FORWARD SIDE. ALSO THE RT WING MAIN SPAR CHAFED BY FUEL PRESSURE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED OUT THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030324001192003032400119NM 2003 3 24 AWXA200300109 120030130A531069730641 CREASE BEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 YVR - MAJOR REPAIR - DURING C-14 CHECK CORROSION WAS FOUND ON CREASE BEAM WEB ON CABIN FLOOR BS 500A-500B, STR 17 L/H. MAINTENANCE REMOVED CORRODED CREASE BEAM WEB BS 500A-500B, STR 17 L/H; FABRICATED A NEW REPLACEMENT CREASE BEAM WEB; INSTALLED REPAIR PART IAW DWG 69-73064. 2L72 4F RTA16WE 20030306000582003030600058SW 2003 3 6 HEEA084773 120030221A3212412050017133 COVER BELL 412 412 1182202SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 EMERGENCY FLOAT COVER IS WORN. 1G72 4U H4SW 20030306000842003030600084NM 2003 3 6 DHL2003753002 120030305A2510 BUCKLE BOEING727 727223 1384074NM A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01753DH 22468 1) FIRST OBSERVER'S SHOULDER HARNESS CAME LOOSE FROM BUCKLE.2) INSTALLED BUCKLE ON FIRST OBSERVER'S SHOULDER HARNESS. OPS CHECKED NORMAL. 2L73 4F A3WE 20030307000672003030700067NM 2003 3 7 SWAA030419 120030221A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 DURING SCHEDULED C4 CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER MM. 2L72 4F RTA16WE 20030310000502003031000050NE 2003 3 10 HEEA084954 220030227A732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TORQUE SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S5273 36002 TORQUE SPLITS AND OSCILLATIONS. FOUND LEAKAGE. POLISHED AND RESET SERVO VALVES AND LEVER. TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030314000722003031400072WP 2003 3 14 CALA0300062 120030221A5347 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0972822 49482 INSPECTION FOUND RT TIEDOWN RAIL CORRODED AT STA 522 - 636. A NEW TIEDOWN RAIL WAS INSTALLED IAW ECRA 5321-01134. 2L72 4F A6WE 20030314001062003031400106EA 2003 3 14 A6WA200340029 120030204A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 2 LEAKING A A6WAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31405AW 7362 F/A REPORTED SMOKE IN CABIN. NOTICED TEMPERATURE RISING. PACK NR 2 SELECTED MANUALLY. REDUCED TEMP PACK, ODOR AND SMOKE SUBSIDED. GROUND RAN A/C NR 1 AND NR 2 PACKS. OPS NORMAL. NR 2 PACK SHOWS EVIDENCE OF OIL LEAKAGE. PLACED PACK ON MEL. 2L72 4F4 FRTA21EA E15NE 20030327000562003032700056NM 2003 3 27 C1HA200383002 120030224A2612 FIRE LOOP BOEING727 7272S7 138407ZNM NR 1 ENGINE SHORTED A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15683CA 22490 NR 1 ENGINE FIRE DETECTOR GROUND CIRCUIT LIGHT FLICKERED OCCATIONALLY DURING CRUISE. PREFLT CK OK. INSPECTED NR 1 ENGINE FIRE LOOP, COWLING & CLAMPS ADJUSTED FROM POTENTIAL GROUND SPOTS. TESTED SYS. CHECKS OK. 2L73 4F A3WE 20030319001262003031900126NM 2003 3 19 CH1A200338008 120030309A2751 ACTUATOR CABLE BOEING727 7272S7 138407ZNM A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15681CA 22020 On climb out of CUN outboard flaps indicated asymmetry at 5 degrees. Performed emergency check list dumped 20,000 lbs of fuel to land at 160,000 lbs 2L73 4F A3WE 20030320001462003032000146NM 2003 3 20 2003UALA00139 120030203A5320 FLOOR SUPPORT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 CABIN FLOOR SUPPORT AT STATION 335 RBL 52 TO 60, STRINGER 17R HAD EXCESSIVE CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW VENDOR T -ANGLE SUPPORT. 2L72 4F4 FRTA16WE E2GL 20030321000242003032100024NE 2003 3 21 NACA20030079 220030319A732239138418 CARBURETOR PWA CB3 DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE #3 POWER LOSS A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03438721163 1163 P32204 44665 P32204 DISCREPANCY: #3 ENGINE SHUT DOWN DUE TO HIGH FUEL FLOW AND LOW BMEP.CORRECTIVE ACTION: REPLACED CARBURETOR AND FUEL FEED VALVE. 2L74 4R4 R 6A3 5E8 20030728000972003072800097NM 2003 7 28 SWAA031618 120030721A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20030418000202003041800020 2003 4 18 MWEA030105 420030215A34318220761101 RECEIVER DOUG DC9 DC932 3022066WP E&E BAY INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31209ME 47730 FIRST OFFICER NR 2 NAV FAILED, VOR, GS, AND LOC FLAGS SHOWING. REMOVED AND REPLACED VOR/ILS RECEIVER. 2L72 4F A6WE 20030421001712003042100171NM 2003 4 21 USAABB03022 120030215A213121173886 CONTROLLER BOEING757 757225 1384959NM CABIN PRESSURE FAILED A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19605AU52440 22201 BWI - FLT 691 - CLIMBING OUT OF BWI, AT APPROXIMATELY 17,000 FEET, THE LEFT ENGIEN BLEED LIGHT ILLUMINATED. CABIN ALTITUDE BEGAN TO INCREASE. THE OXYGEN MASKS DEPLOYED, AND THE CREW PERFORMED A DESCENT. FLIGHT RETURNED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE DEDICATED GENERATOR AND THE NR 2 PRESSURE CONTROLLER. (M) 2L72 4F RTA2NM 20030421001792003042100179WP 2003 4 21 GTIA030134 120030130A5320 PAN DOUG DC9 DC981 3022081WP E/E BAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - E/E COMPARTMENT HAS CORROSION AT FORWARD AND AFT DOOR PAN. REMOVED E/E COMPARTMENT DOOR PAN. RECEIVED NEW DOOR PAN. COMPLETED INSTALLATION OF NEW DOOR PAN. (M) 2L72 4F A6WE 20030421000022003042100002NM 2003 4 21 UPS03440229 120030204A5711 FITTING BOEING747 747200 1384847NM WING REAR SPAR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, LT WING REAR SPAR KICK FITTING AREA, CORROSION FOUND ON HOLE-D AT TERMINAL FITTING. D-HOLE REWORK AS PER EO B747-5710-18343A AND RS 57-12-34973. 2L74 4F RTA20WE 20030801000332003080100033WP 2003 8 1 2003F00508 120030709A3350OL3071BPEGPL LIGHT DOUG DC9 DC931 3022065WP CABIN INTERMITTENT A A4JAK NONE O OTHER ININSP/MAINT 1 SO35934LK 48157 DURING B-CHECK PIE MAINTENANCE, FOUND AFT RED EMERGENCY EGRESS LIGHT ON FLOOR INTERMITTENT. RELAMPED AFT RED FLOOR EGRESS LIGHT IAW MM 33-53-0, CHECKS NORMAL. (M) 2L72 4F A6WE 20030807000282003080700028NM 2003 8 7 USAABB03110 120030711A33509221009 BATTERY BOEING757 7572B7 1384964NM R3 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 FOUND EXIT IDENTIFIER AT R3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20040223000252004022300025NE 2004 2 23 WVE2004F00000 220031215A72616047T63P04 CARBON SEAL CNDAIRCL604 CL604 1900301EA GE CF34 CF343B1 NE RT ENGINE LEAKING B WVERK NONE K FLUID LOSS ININSP/MAINT 1 EA09316FX STA3313B DURING 400/800/12 MO INSPECTION THE RT ENGINE NR 1 CARBON SEAL WAS FOUND TO BE LEAKING OIL EXCESSIVELY. THE NR 1 CARBON SEAL WAS CHANGED THREE TIMES PREVIOUSLY: AT 1/22/00 TT: 1274:44 TC: 663, AT 8/3/00 TT: 1902:37 TC:953: AND 1/25/02 TT: 3448:35 TC: 1805. NOTE: THE LEFT ENGINE WITH THE SAME TIMES AND CYCLES AT RT, THE NR 1 CARBON SEAL HAS NOT BEEN CHANGED. 2L72 4F4 FRTA21EA E15NE 20040225001762004022500176NM 2004 2 25 DLM90031145 120031227A33506011779 BATTERY DOUG MD90 MD9030 3023690NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27901DA 53381 DURING L/O FOUND 2R & 1L EXTERIOR LIGHTS INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHTS BATTERY AND BATTERY RACK (B5-125). CHECKS GOOD. 2L72 4F RTA6WE 20030721001302003072100130NM 2003 7 21 SWAA031494 120030707A53126545819139 PRESSURE PANEL BOEING737 7375H4 138449DNM NLG W/W CRACKED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29512SW 24189 (AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. FOUND WEB CRACKED IN NLG W/W AT BS 259, WL 174. REPAIRED NLG W/W WEB PER SWA EA. 2L72 4F RTA16WE 20030722001362003072200136NM 2003 7 22 SWAA031427 120030626A53306545767 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 495, ABOVE STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040227000472004022700047NM 2004 2 27 ASAA0340363 120031219A5347655384425 CARGO TRACK BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01713AS 30161 OAK - DURING C-CHECK, FOUND AFT CARGO LEFT CARGO TRACK IS DAMAGE BEYOND LIMITS. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030829001462003082900146 2003 8 29 SWAA031840 420030816A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030829001342003082900134NM 2003 8 29 SWAA031862 120030819A53306545785 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SPECIAL VISIT, FOUND WINDOW CUTOUT FWD UPPER CORNER CRACKED AT RT WINDOW NR 11. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030722000162003072200016NM 2003 7 22 2003F00444 120030307A5330 SKIN BOEING727 727222 1384073NM FUSELAGE LIGHTNING STRIKEA RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND LIGHTNING STRIKE AT FUSE CROWN, BS 747 STRINGER 2. DRILLED OUT LIGHTNING STRIKE AT FUSELAGE CROWN BS 747, STRINGER 2 AND INSTALLED FASTENER. (M) 2L73 4F A3WE 20030723000452003072300045NM 2003 7 23 TSAA0353135 120030505A5320 WEB BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 CORROSION DISCOVERED BETWEEN FSS 540 AND 552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED PORTION OF THE WEB. FABRICATED NEW WEB SECTION, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-6, FIGURE 1. (M) 2L72 4F RTA16WE 20030728000162003072800016 2003 7 28 VNAA0307008 420030724A3445 WARNING SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL07328JS 3030 ON APPROACH TO PHL AT 6000 FEET AND 20 MILES WEST THE FLIGHT CREW RECEIVED A TCAS RA. THE FLIGHT CREW INIATED A DESCENT TO 5400 FEET WHERE THE TCAS RA ALERT CLEARED. ATC WAS CONTACTED AND THE FLIGHT CREW WAS ADVISED THAT THERE WAS NO TRAFFIC IN THE AREA. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030807000662003080700066SO 2003 8 7 C2XA03CL135 120030804A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714952 145067 DURING ROUTINE MAINTENANCE THE EMERGENCY CEILING LIGHT WAS FOUND INOPERATIVE AT ROW 17. MAINTENANCE REPLACED EMERGENCY CEILING LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030902001372003090200137NM 2003 9 2 03FDEA00909 120030616A5753ARC0503503 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LT W O/B FLAP O/B HINGE ACTUATOR I/B BORE FOUND CORROSION. WORK CARRIED OUT IAW EA 1-5740-71722, WINGS- LEFT O/B FLAP- O/B HINGE BRACKET ASSEMBLY FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030905001252003090500125NM 2003 9 5 DL76K030646 120030714A3350BPS73 CHARGER BOEING767 767332 1382001NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27171DZ 29690 EMERGENCY LIGHTS INOP ON F/C SEATS. REPLACED BATTERY CHARGER FOR F/C EMERGENCY LIGHTS. ETOPS CATEGORY 'X': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2L72 4F RTA1NM 20030905002122003090500212SO 2003 9 5 C2XA03TY129 120030818A534714532606011 SEAT TRACK EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LW1. MAINTENANCE REMOVED AND REPLACED THE TRACK IAW EMB MM 53-01-06, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030825000552003082500055WP 2003 8 25 UPS03841126 120030819A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. R&R EMERGENCY LGT BATT PACK. OPS CK NORMAL 2L74 4F RT4A25 20030728001162003072800116NM 2003 7 28 SWAA031540 120030712A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040128001572004012800157EA 2004 1 28 SWIA200312730 120031226A335020131A POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY SIGN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07955SW6467 6467 7817 AFT FACING AISLE OVERWING EXIT SIGN DOES NOT ILLUMINATE DURING EMERGENCY EXIT LIGHT TEST. REPLACED NR 3 BATTERY PACK. OPS CHECK GOOD. 2L72 4F RTA21EA 20040129001302004012900130NE 2004 1 29 COMA0460009 220031230A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FLUCTUATES A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01528CA 7841 FLIGHT 5732 N1 AND N2 AND F/F FLUCTUATING. COULD NOT DUPLCIATE. GROUND RUNS WERE NORMAL AND SATISFACTORY. 2L72 4F4 FRTA21EA E15NE 20040203000672004020300067WP 2004 2 3 ASAA0380585 120030911A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01937AS149642877 49364 SEA LINE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE, BATTERY PACK DISCHARGED. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040206000662004020600066WP 2004 2 6 ASAA0380807 120031123A53305924802509 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OKC - DURING C-CHECK FOUND DAMAGED, DENTED, AT FS 229-245. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND STRAPS PER SRM 53-04. (M) 2L72 4F RTA6WE 20040206000832004020600083WP 2004 2 6 DHL2004806500 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 6 FLOOR TRACK PLUG LUG WORN AT STA 210.000. REMOVED PLUG WITH WORN LUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 6 FLOOR TRACK AT STA 210.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040205001362004020500136GL 2004 2 5 P5CA0300998 220031125A73212718326 SOLENOID VALVE BOEING747 74747UF 1384949NM GE CF6 CF6* 30020GL HMU MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23496MC 29257 704916 RETURNED TO BLOCKS. ENG. NR 3 FAILED TO START DUE TO 0 FUEL FLOW (NO EICAS MESS.) REPLACED NR 3 ENG. HMU FUEL SOLENOID VALVE. OPS CHECK OK IAW MM 73-21-00. 2L74 4F4 FRT1384945 E23EA 20040213000022004021300002WP 2004 2 13 MEX2003547 120031208A3213 STRUT DOUG DC9 DC987 3022087WP RT MLG LEAKING W ASMFO OTHER K FLUID LOSS NRNOT REPORTED 1 SW23754RA 49641 DURING THE AIRCRAFT DISPATCH AT GDL STATION, THE TECHNICAL PERSONNEL SAW A LITTLE LEAK IN THE STRUT OF THE RT MLG. AT STATION , PERFORMED A VERIFICATION OF THIS LEAK. THE STRUT SEALS WERE CHANGED AND THE MLG WAS TESTED IAW MM, ALL CORRECT. 2L72 4F RTA6WE 20031211001052003121100105CE 2003 12 11 55039 120031008A3411 PITOT TUBE BEECH 1900 1900D 1154162CE PITOT/STATIC SYSDEFECTIVE A AMWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE07161YV UE161 DURING TAKE OFF ROLL FO AIRSPEED INDICATOR FAILED TO RESPOND. TAKE OFF WAS ABORTED AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED FO'S PITOT TUBE AIRSPEED IND P/N1293640797 S/N593D95 2L72 4T RTA24CE 20031212000692003121200069EA 2003 12 12 MASA200300431 120031024A32440276140 TIRE CNDAIRCL600 CL6002B19 1900309EA NLG BLOWN A MASAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW0777260 77260 ASH FLT 6016 FAT. DURING TAKEOFF BOTH NOSE TIRES BLEW. TIRE DEBRIS DAMAGE TO AFT NOSE GEAR DOOR AND POSSIBLE TIRE DEBRIS INGESTED INTO BOTH ENGINES. TWO DENTS NOTED ON UNDERSIDE OF FUSELAGE AT FS 260 AFT OF NOSE WHEEL WELL. FURTHER INSPECTION AND INVESTIGATION UNDERWAY AT THIS TIME. 2L72 4F RTA21EA 20040309001792004030900179NM 2004 3 9 ASAA0310643 120031211A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - FOUND EMERGENCY FLOOR TRACK LIGHTS ON SEAT PALLET 9-5 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20031215001992003121500199EU 2003 12 15 USAA030263 120031103A5320D53480043005 SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND SUPPORT WITH 5.2 CM BY 2.5 CM WITH CORROSION OVER 50 PERCENT MATERIAL LOSS, FRAME 66, -Y 130. CORROSION LEVEL 2, TASK NR JA 260-53500-014. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. (M) 2L72 4F RTA28NM 20031217000342003121700034WP 2003 12 17 DHL2003805599 120030829A53305656352506 PANEL DOUG DC8 DC873F 302199FWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT LOWER FUSELAGE PANEL NR 736 EXTERNAL SKIN DELAMINATED, STA 1040.000 - STA 1060.000. REMOVED AND INSTALLED RT LOWER PANEL NR 736 (STA 1040.000 - 1060.000) IAW MM 53-50-3. 2L74 4F RT4A25 20030815000832003081500083NE 2003 8 15 HEEA088411 120030728A63217665009803103 BRAKE SKRSKYS76 S76A 8143006NE ROTOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 ROTOR BRAKE CONTINUOUSLY CYCLES. SHOP REPAIR. 1G72 3U H1NE 20030819001242003081900124NM 2003 8 19 UPS03M40999 120030723A3350 POWER SUPPLY DOUG MD11 MD11F 3023600NM EMERGENCY LIGHT FAILED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01250UP EMERGENCY POWER TEST FAIL. POWERED DOWN A/C, REPOWERED, PERFORMED RTS OF EPCU. TEST PASSED & EMERGENCY POWER TEST PASSED. 2L73 4F RTA22WE 20030819000532003081900053SO 2003 8 19 RAIA00306171 120030622A3350 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCONNECTED A RAIAO OTHER N FALSE WARNING ININSP/MAINT 1 CE03801HK 145053 FLOOR EMERGENCY LIGHTS OUT AT SEAT 12A. RE-SECURED CONNECTOR AT FLOOR LIGHT STRIP. 2L72 4F RTT00011AT 20030912000882003091200088NM 2003 9 12 AWXA200300836 120030713A3350E0052R8B3APNE CONNECTOR AIRBUSA319 A319132 3930340NM CABIN DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 12 LT WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 12 LT IAW ESPM 20-48-21, PG 12-16, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030827000902003082700090SO 2003 8 27 C2XA03CL117 120030702A3350110049 CHARGER EMB 135 EMB135LR 3260305SO CABIN FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715527 145413 DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTS WERE DIM. MAINTENANCE REPLACED THE NR 2 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031001000502003100100050WP 2003 10 1 UPS03841195 120030813A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, MAIN CABIN FS 1620 FLOORBEAM UPPER FLANGE IS CORRODED AT LBL 40. REMOVED CORROSION IAW DC8 SRM 51-1-8. MATERIAL REMAINING .034 ORIG MATERIAL .125 FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR ANGLE AND FILLER IAW DC8 SRM TR 53-124 AND 53-2-0 FIG 1B. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE AND FILLER IA W DC8 SRM TR 53-124 AND 53-2-0 FIG 1B. 2L74 4F RT4A25 20031006000112003100600011EU 2003 10 6 MALA030407 120030905A3230HP848430621 CONTROL VALVE SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL15453XJ 340B453 DURING DESCENT ON FLIGHT 3199, ON GEAR DOWN SELECTION IN TRANSIT LIGHT ON GOOD PRESSURE AND VOLUME. NO GREEN LIGHTS HYDRAULIC PUMP STILL ON GO AROUND DURING QRH NOTICED LANDING GEAR CONTROL C/B POPPED RESET PER MAINTENANCE GEAR SELECTED DOWN NORMAL LANDING. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE PN HP848430-621 SN/ON 1119, SN/OFF 0011 IAW SAAB AMM 32-31-15-4 ALL CHECKS GOOD REFER 409 195532 FOR DETAIL. 2L72 4T RTA52EU 20031006000752003100600075CE 2003 10 6 54215 120030908A3260327 BULB BEECH 1900 1900D 1154162CE ANNUNCIATOR INOPERATIVE A AMWAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 CE07166YV UE166 UPON INITIATING GEAR DOWN CREW NOTICED THAT THE NOSE GEAR ANNUNCIATOR DIDN'T ILLUM. CREW PERFORMED AND NOTIFIED TOWER MANUAL GEAR EXT PROCEDURE WAS INITIATED AFTER COMPLETION OF CHECK LIST. IT WAS NOTED GEAR DOWN ANNUNCIATOR STILL DIDN'T ILLUM. SPARE BULB WAS PLACED IN THE NOSE GEAR. BOTH ANNUNCIATOR BULBS ILLUMINATED. A FLY BY THE TOWER WAS CONDUCTED TO CONFIRM THAT GEAR APPEARED TO BE DOWN AS A PRECAUTION. CAPT ORDERED ARFF EQUIP BE POSITIONED NEXT TO RUNWAY. LANDING WAS MADE WITH NO FURTHER INCIDENTS. CHANGED LIGHT BULBS. THIS DOES NOT REQUIRE A TEARDOWN REPORT. 2L72 4T RTA24CE 20031008000092003100800009NM 2003 10 8 03253429 120030910A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27429FJ 3194 DURING MAINTENANCE INSPECTION THE EMERGENCY POWER SUPPLY WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20031008000452003100800045NM 2003 10 8 VNAA0309005 120030808A24001060003 BPCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BUSS POWER FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07424JS179602380 3033 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL AND DISPLAYS 3, 4, AND 5 FAILED AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE BUSS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031021000722003102100072SO 2003 10 21 SIMA200326506 120030916A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21720AE 145279 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFED BY BLENDING AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ON REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2849 AND STANDARD EMB SRM/CPM PRACTICES. (M) 2L72 4F RTT00011AT 20030908001742003090800174EA 2003 9 8 SWIA200312244 120030624A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 BAGGAGE COMPARTMENT SEAT TRACKS LBL 9.0 & RBL 9.0 BETWEEN FS 559 + 80 AND 559 + 96 CORRODED. DISCOVERED DURING C-CHECK, SEAT TRACKS REPLACED IAW CRJ AMM 20-21-00. P/N: 601R38779-13 2L72 4F RTA21EA 20030910000372003091000037SW 2003 9 10 HEEA088217 120030715A7332206075676111 INDICATOR BELL 206 206L3 1182108SW FUEL PRESSURE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FUEL PRESSURE INDICATOR NOT INDICATING CORRECTLY. 1G71 3U H2SW 20031027000562003102700056NM 2003 10 27 0301786625 120030924A3350 POWER SUPPLY BOEING747 747251B 1384892NM EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01625US 21707 DURING LINE CHECK, FOUND ZONE-E FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040416000022004041600002NM 2004 4 16 ASAA0240AAA 120030323A523065479577 WEB BOEING737 7374Q8 138447QNM CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON WEB INSIDE AFT CARGO DOOR AT BS 847, RBL 21 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040115001762004011500176NM 2004 1 15 UIEA200300064 120031115A2410 CSD BOEING747 747243B 1384830NM NR 1 MALFUNCTIONED A UIEAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 EA15540MC 22508 NR 1 GENERATOR FIELD TRIPPED CAUSING NR 2 GENERATOR TO TRIP ALSO. CHECKED EACH GENERATOR FREQUENCY AND VOLTS NR 2 OK. RETURNED TO NORMAL OPERATION WITH NR 3. NR 1 FREQUENCY WAS OVER 8000 THEN TRIPPED AGAIN. NR 1 CSD DISCONNECTED BY CHECKLIST PROCEDURES. REMOVED AND REPLACED NR 1 CSD IAW MM 24-11-01. OPERATION CHECK NORMAL NO LEAKS FOUND IAW MM 24-20-00. REMOVED AND REPLACED NR 1 GCU OPERATION CHECK NORMAL IAW MM 24-20-00. REMOVED AND REPLACED NR 2 GCU OPERATION CHECK NORMAL IAW MM 24-20-00. (M) 2L74 4F A20WE 20031031000802003103100080NM 2003 10 31 DLM88030846 120030916A3260 UPLOCK DOUG MD88 MD88 3023688NM RIGHT MLG BROKEN A DALAL ABORTED APPROACH O OTHER APAPPROACH 1 SO27949DL 49880 GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. EXECUTED A GO AROUND AND COMPLIED WITH POM PROCEDURES TO UNEVENTFUL LANDING. FOUND MAIN LANDING GEAR LATCH FOLLOW UP MECHANISM ATTACH BOLT BROKEN REF IPC 32-30-00-12A ITEM 126. REPLACED BOLT AND CYCLED DOORS SEVERAL TIMES. GEAR DOOR OPERATION IS NOW NORMAL. 2L72 4F RTA6WE 20031103000572003110300057NM 2003 11 3 03FDEA01687 120031002A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 STRINGER CLIP CRACKED AT BS 950E STRINGER 4 LT. REMOVED AND REPLACED STRINGER CLIP AT BS 950E STRINGE 4LH IAW SRM 51-30-2 AND SRM 51-30-5. 2L73 4F RTA3WE 20030821000322003082100032NM 2003 8 21 03FDEA00910 120030616A5753ARC0503503 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING O/B FLAP O/B HINGE ACTUATOR O/B BORE FOUND CORROSION. LEFT WING O/B FLAP O/B HINGE O/B ACTUATOR BORE REPAIRED AS PER FEDEX EA 1-5740-71722, TITLE: WINGS- LEFT O/B FLAP- O/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030820000542003082000054NM 2003 8 20 03FDEA01166 120030725A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT WING O/B FLAP (FLAP SIDE) O/B HINGE I/B AND O/B PIVOT HOLES BUSHING FOUND LOOSE. LEFT O/B FLAP (FLAP SIDE) O/B HINGE I/B AND O/B PIVOT HOLES REPAIRED AS PER FEDEX EA 1-5750-69278 - WINGS TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030408000402003040800040EU 2003 4 8 SIMA200305009 120030112A5330ALCLAD2024T42 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21371AE 340B371 ABI - DURING AN IMBV INSPECTION, THE FRAME AT STATION 640 WAS FOUND TO BE DENTED ON THE RIGHT SIDE 16 INCHES ABOVE THE FLOOR. RECONTOURED DAMAGED AREA. PERFORMED AND EDDY CURRENT INSPECTION. NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER ANGLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS005026 PARA 11 AND STANDARD SRM (72LKS 3079 REV 41) PRACTICES. (M) 2L72 4T RTA52EU 20030407000942003040700094SO 2003 4 7 SIMA200306415 120030215A532014521725001 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21704PG 145174 ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION LT FLOOR SILL CORRODED BETWEEN FRAMES 18-23. INSTALLED SERVICEABLE LEFT FLOOR SILL IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030408000132003040800013WP 2003 4 8 ASAA0380087 120030114A52505936715505 SKIN DOUG DC9 DC983 3022083WP BARRIER DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND C-CHECK, AFT CARGO BAY BARRIER DOOR INTERNAL SKIN IS CRACKED 1.25 INCH. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20030404001642003040400164NM 2003 4 4 SWAA030554 120030311A531265458197 BULKHEAD BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) IN NLG W/W AT BS 246 & WL 168.5 RT. REPAIRED WEB PER SWA EA. 2L72 4F A16WE 20030408001282003040800128NM 2003 4 8 AMTA200300226 120030214A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 FOUND EMERGENCY LIGHT ABOVE SEAT NR 2 ABC, AT THE CURVE EDGE OF STOWAGE BIN, OUT. (M) 2L72 4F RTA2NM 20030416003122003041600312EU 2003 4 16 AALA20030306 120030310A2910 O-RING FOKKERF28 F28MK0100 4990807EU HYD SYSTEM DAMAGED A AALAK NONE K FLUID LOSS CRCRUISE 1 SW211426A 11411 DTW - FLT 1461 - EN ROUTE DCA-ORD, EXPERIENCED LOSS OF NR 1 HYDRAULIC SYSTEM FLUID IN FLIGHT. COMPLIED WITH ALL RELEVANT EMERGENCY PROCEDURES. GEAR WAS EXTENDED USING ALTERNATE LANDING GEAR CONTROL. LANDED DTW WITHOUT INCIDENT. REPLACED O-RING ON NR 1 HYDRAULIC PUMP FOR NR 2 ENGINE PRESSURE LINE. BAD O-RING. PERFORMED OPERATIONAL AND LEAK CHECK. OPERATIONS AND LEAK CHECK GOOD. RESERVICED NR 1 HYDRAULIC SYSTEM. PERFORMED MAIN LANDING GEAR SELECTOR VALVE RESET PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030416001602003041600160 2003 4 16 HNAA0300018 420030323A23001010531AB2K ANTENNA DHAV DHC8 DHC8311 1386006EA COMMS BROKEN A HNAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA07337EN21756 284 CREW REPORTED VIBRATION DURING CLIMBOUT, WITH INCREASING INTENSITY. AIRCRAFT RETURNED TO FIELD. FOUND PORTION OF LOWER COMM ANTENNA MISSING. REPLACED ANTENNA. 2H72 4T RTA13NM 20030416001662003041600166NM 2003 4 16 SWAA030769 120030403A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C4 CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 10R, BS 727E AND BS 727D. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2L72 4F RTA16WE 20030416000172003041600017SO 2003 4 16 SWIA200311675 120030103A2797 CONNECTOR EMB 120 EMB120ER 3260203SO LEFT OB FLAP WORN A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07214SW 120280 FLAPS WOULD NOT RETRACT, DISAGREEMENT WITH THE OUTBOARD PAIRS, WOULD NOT CORRECT. FOUND LEFT OUTBOARD FLAP CONNECTOR TO HAVE FLUID INSIDE AND WORN BACKSHELL. REPLACED CANNON PLUG AND BACKSHELL. APPLIED SUPER CORR-B TO CANNON PLUG AND CONNECTORS. OPS CHECK OF FLAP SYSTEM GOOD IAW 20-50-00 AND 27-50-00. 2L72 4T RTA31SO 20030417001042003041700104WP 2003 4 17 MWEA030056 120030205A52805930583153 ANGLE DOUG DC9 DC981 3022081WP RT MLG DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 RT MLG DOOR NR 1 FRAME TO INTERCOSTAL ATTACH T-ANGLE CRACKED IN THREE PLACES, LOCATED JUST OUTBOARD AFT OF ACTUATOR ATTACH FITTINGS. FABRICATED AND INSTALLED T-ANGLE, COMPLETED ALL REPAIRS AND CLOSED SKIN. 2L72 4F A6WE 20030417001682003041700168NE 2003 4 17 QXEA0300248 220030206A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX641 10026 GEE965266 NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030417001922003041700192NM 2003 4 17 P5CA0300756 120030130A5320 CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND UPPER DECK WALL ON CLIP 500 & 520 RT SIDE. STRAINER 8, 9, 10, 10A, 11 & 12. FABRICATED NEW CLIP PER SRM 57-40-03, 51-30-02 & 51-10-01. 2L74 4F A20WE 20030424001462003042400146NM 2003 4 24 QXEA0300374 120030313A5320 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - TOP WING TO FUSELAGE AFT APERTURE FOR PANEL 261LT IS CHAFED. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20031112000242003111200024SO 2003 11 12 C2XA03SH446 120031112A711014576599003 STRUCTURE EMB 145 EMB145LR 3260212SO LT COWLING DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV-DURING C-CHECK THE LEFT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE DENTED. MAINTENANCE REFORMED THE DENTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031118000562003111800056EU 2003 11 18 AWXA200301171 120031006A5321D5367320400000 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL 151AF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL; FABRICATED A NEW REPLACEMENT PANEL IAW A320 SRM 53-02-00, PG 231-234. 2L72 4F RTA28NM 20031106000582003110600058NM 2003 11 6 03FDEA01818 120031023A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD PIVOT LUG BORE FOUND CORRODED. 2L73 4F RTA22WE 20031106000652003110600065NM 2003 11 6 SWAA032295 120031018A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 15L, BS 374 AND BS 378. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031106001362003110600136NM 2003 11 6 SWAA032273 120031016A53136545877 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 360, STR 4L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20031107001662003110700166NM 2003 11 7 AALA20031044 120030921A33500202365001 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21761AJ 31478 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT CLOSET L1. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20031107000212003110700021WP 2003 11 7 MWEA030439 120031103A551159361162 SPAR DOUG DC9 DC981 3022081WP HORIZ STAB GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 HORIZONTAL STABILIZER CENTER BOX AREA, RIGHT OUTBOARD AFT SPAR SECTION HAS GOUGE MARKS ON AFT SIDE IN CENTER POSITION. BLENDED AREA. 2L72 4F A6WE 20031107001322003110700132SO 2003 11 7 SIMA200328201 120031005A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A. (M) 2L72 4F RTT00011AT 20040106002162004010600216NM 2004 1 6 SWAA032692 120031208A53116546522 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 PAE - DURING SCHEDULED D-CHECK, FOUND CORROSION ON AFT CARGO COMP FRAME BS 847 RBL 4 TO LBL 4, WL 154. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031120001192003112000119NM 2003 11 20 SWAA032457 120031106A53116546543 BELTFRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED OUTER BELTFRAME CHORD BS 639 STR 17. REPLACED CHORD PER EA. 2L72 4F RTA16WE 20040114001232004011400123NM 2004 1 14 DL75K031057 120031125A2560P2070003001 FLASHLIGHT BOEING757 757232 1384965NM CABIN INOPERATIVE A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO276714Q 30485 EMERGENCY FLASHLIGHT AT THE L2 POSITION INOP. REPLACED SAME. 2L72 4F RTA2NM 20040115001122004011500112NM 2004 1 15 DL73S031095 120031216A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 FOUND ON W-2 LETTER CK, CORROSION ON FORMER STA 967 AT SKIN ATTACH ANGLE BETWEEN STR 27 LEFT AND 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11. 2L72 4F RTA16WE 20031217002032003121700203NM 2003 12 17 AWXA200301497 120031106A532065C3267714 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF LT AFT LAVATORY SUB FLOOR STRAP BETWEEN BS 1017 AND BS 1028, LBL 3, WL 208. MAINTENANCE REMOVED CORRODED SUB FLOOR SHEAR WEB BETWEEN BS 1017 AND BS 1028, LBL 3, WL 208; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51, FIG 101. 2L72 4F RTA16WE 20031223001312003122300131EU 2003 12 23 MALA030544 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION IN LAKE CITY, FL - TIMCO FOUND SEAT 5B, 5F FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 5B, 5F IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031223001992003122300199WP 2003 12 23 GTIA030813 120031006A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND RIGHT SIDE LOWER FORWARD EXIT SIGN INOPERATIVE. FOUND WIRING DISCONNECTED. RECONNECTED WIRING. (M) 2L72 4F A6WE 20031224000402003122400040 2003 12 24 ASAA0380636 420031012A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01965AS 53079 LINE CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20031229000962003122900096NM 2003 12 29 AWXA200301540 120031209A532069451462 BRACKET BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN BRACKET FOR JUNCTION BOX J10 AT BS 380. MAINTENANCE REMOVED BRACKET FOR JUNCTION BOX J10 AT BS 380; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 69-45146; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 6 & 45, FIG 8 & 12. 2L72 4F RTA16WE 20031007000652003100700065NM 2003 10 7 SWAA031979 120030902A26126558234 FIRE LOOP BOEING737 7372H4 138448CNM NR 2 ENGINE FAULTY A SWAAO OTHER N FALSE WARNING CRCRUISE 1 SW29083SW 22732 NR 2 ENGINE FIRE WARNING, AFTER TESTING WARNING DISAPPEARED AND REAPPEARED SEVERAL TIMES, DID NOT SHUT ENGINE DOWN. FOUND UPPER LOOP M336 HIGH IN RESISTANCE, REMOVED AND REPLACED UPPER LOOP PER MM. 2L72 4F A16WE 20040121000732004012100073EA 2004 1 21 ASOA03620 120031202A53206013501251 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11907EV 7648 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 621-625, NEAR STRINGER 14L WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INTERCOSTAL AT FS 621-625, NEAR STRINGER 14L IAW SRM 51-40. (M) 2L72 4F RTA21EA 20031204000432003120400043WP 2003 12 4 AALA20031052 120030922A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21455AA 49560 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 19 THROUGH 21. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204001732003120400173NM 2003 12 4 QXEA200301294 120031017A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09357PH3191 364 504 FORWARD SECTION OF FLOOR TRACK LIGHTING IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PS1 & PS4. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031209001432003120900143EA 2003 12 9 QXEA200301317 120031001A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 DENT IN SIDE OF FUSELAGE BELOW PILOTS WINDOW. REPAIRED IAW REO 670-53-11-015. 2L72 4F RTA21EA 20031210000062003121000006NM 2003 12 10 03FDEA02078 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AJC7052-501 AFT FACE FLANGE 05EA CRACK LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II. 2L73 4F RTA22WE 20031210000402003121000040WP 2003 12 10 03FDEA01975 120031121A5511 SPAR CAP DOUG DC10 DC1010 3022110WP HORIZ STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 NR S 15 COMPLY WITH EA8-5510-73851. STABILIZER HORIZONTAL ELONGATED HOLE IN HORIZONTAL STAB UPPER REAR SPAR CAP AD 52-22-10. COMPLIED WITH EA8-5510-73851. 2L73 4F A22WE 20040128001902004012800190CE 2004 1 28 0401 120031229A2612 WARNING LIGHT LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP RT ENG FIRE LOOPFALSE INDICATIONE BSYAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL0727BL 163 P74333 RIGHT ENGINE INDICATED A FIRE, SHUT DOWN RIGHT ENGINE AND FIRED BOTH FIRE BOTTLES. HAD MAINT. TROUBLESHOOT SYSTEM, DISCONNECED ALL THREE LOOPS, ALL CHECKED OUT GOOD. RECONNECTED SYSTEM CHECKED OUT NORMAL. RETURNED TO SERVICE. 2L72 4F4 F A10CE E6WE 20030917000292003091700029WP 2003 9 17 03FDEA01152 120030725A5754ARB1617 STRUCTURE DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 NR S-16 COMPLY WITH E.A.8-5750-70983. WINGS LEADING EDGE SLAT-NO-S SLAT TRAILING EDGE CRACK REPAIR. CLOSING ACTION ON 07/22/03 COMPLIED WITH E.A.8-5750-70983. 2L73 4F A22WE 20030919000642003091900064NE 2003 9 19 HALA0300648 220030722A7320 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE NR 2 ENGINE MALFUNCTIONED A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13481HA 55126 RT ENGINE FADAC ALTN WILL NOT RESET. REPLACED NR 2 EEC IAW MM 73-21-01. RETURN TO SERVICE TEST OK. GROUND RUN OK. 2L72 4F4 FTRA6WE E00057EN 20030919001442003091900144 2003 9 19 29040311031 420030311A34215040017901 GYRO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP074027Q3196 2904 9456 DIRECTIONAL GYRO INOPERATIVE. 1G71 3U3 U H9EU E00054EN 20030917001092003091700109NM 2003 9 17 AMTA200301065 120030817A3240215871 BRAKE BOEING737 73783N 13844HINM WHEEL ASSY MALFUNCTIONED A AMTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL11327TZ 32613 SUSPECT DRAGGING BRAKE, RETURN TO GATE. REMOVED AND REPLACED NR 3 MAIN BRAKE ASSEMBLY IAW MM 32-41-41, OPS AND LEAK CHECK NORMAL. (M) 2L72 4F RTA16WE 20030923000862003092300086WP 2003 9 23 DHL2003604740 120030608A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT CARGO COMPT FRAME ANGLE DOUBLER CORRODED AT STA 1040.000 L-33R - L-34R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION ON FRAME ANGLE DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. TRIMMED OUT CORRODED AREA IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6 AL0.063) AND ANGLE DOUBLERS (02 EA) (301 0.250H 0.040) IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED FILLER IAW SRM 51-1-8B. INSTALLED FILLER AND ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 53-2-0 FIG 2, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030924001092003092400109NM 2003 9 24 C1HA200395066 120030825A3350MISC062 BATTERY BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 STA. 950 EMERGENCY CABIN AREA LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY CABIN BATTERY ASSEMBLY PER M/M 33-50-21. 2L73 4F A3WE 20030929000202003092900020NM 2003 9 29 03FDEA01399 120030829A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CORROSION ON BS 1130 FLOORBEAM UPPER CHORD AROUND HOLES AND UNDER NUT PLATES, LBL 48, WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOORBEAM AT BS 1130, LBL 48, WL 208 FWD UPPER FLANGE PER SRM 53-10-8. 2L73 4F RTA3WE 20040902001562004090200156WP 2004 9 2 MEX2003572 120031229A2910 COUPLER DOUG DC9 DC987 3022087WP HYD SYSTEM LEAKING A ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW231075T 49724 FLT 143 - PVR-MEX - DURING TRANSIT CHECK, OBSERVED HYDRAULIC LEAKAGE COMING FROM THE MLG COMPARTMENT. THE LT HYDRAULIC SYSTEM,WITH LOW LEVEL, WAS PRESSURIZED, OBSERVING AN HYDRUALIC LEAKAGE IN A CONNECTING COUPLE OF THE POWER TRANSFER SHUTOFF VALVE. THE COUPLE WAS TIGHTENED AND SYSTEM TESTED IAW MM 29-10-08. NO LEAKAGE WAS PRESENT, ALL CORRECT. (M) 2L72 4F RTA6WE 20030815000162003081500016SW 2003 8 15 HEEA088611 120030716A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW GEARBOX DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FOUND BUSHING STICKING OUT FARTHER THEN UNITS SURFACE. 1G71 3U H2SW 20030819000162003081900016NM 2003 8 19 USAA030098 120030701A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US40808 23986 PIT - FOUND ENTRY DOOR CUTOUT CRACKED .25 INCH, STATION 947, STRINGER 11L, LEFT AFT ENTRY DOOR CUTOUT. INSTALLED DOUBLER PER SRM 53-60-01. (M) 2L72 4F RTA16WE 20030820000502003082000050NM 2003 8 20 03FDEA00924 120030618A5753ARC0503503 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LT WING O/B FLAP O/B HINGE O/B LOWER BORE FOUND CORROSION. LT WING O/B FLAP O/B HINGE O/B LOWER BORE REPAIRED AS PER FEDEX EA 1-5750- 69373, OUTBOARD TRAILING EDGE FLAP - SUPPORT BRACKETS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821000082003082100008NM 2003 8 21 USAASB03121 120030726A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU 23551 PILOT REPORTED THE RIGHT OVERHEAD EMERGENCY EXIT SIGN, THE LEFT OVERWING EXIT SIGN, THE LEFT SIDEWALL EXIT SIGN AT ROW 10 AISLE EXIT AND THE EMERGENCY LIGHTS AT ROW 14 DEF GRAB RAIL LIGHTS INTERMITTENTLY ILLUMINATE WITH EMERGENCY LIGHTS ARMED AND EXTINGUISH FIVE SECONDS AFTER EMERGENCY LIGHTS ARE ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/ 2013-1A. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030403001072003040300107NM 2003 4 3 DL72S030232 120030309A33501000677 SWITCH BOEING727 727225A 1384077NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO278890Z 21859 L1 DOOR EMERGENCY LIGHT DOES NOT TURN WITH EMERGENCY LIGHT SWITCH. LIGHTS GO DIM WITH PACK ON SWITCH. REPLACED POWER SUPPLY. 2L73 4F RTA3WE 20030401001162003040100116WP 2003 4 1 DHL2003804507 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART HAS A 1 INCH CRACK AT STA XFS 772.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024 T3 AL 0.032) PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030407000432003040700043WP 2003 4 7 GTIA030030 120030115A5510 DOUBLER DOUG DC9 DC983 3022083WP ELEVATOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND RIGHT ELEVATOR STATION 1417 DOUBLER BENT CRACKED. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTLALED NEW DOUBLER. (M) 2L72 4F RTA6WE 20030414000182003041400018NM 2003 4 14 SWAA030746 120030402A53306552988 SKIN BOEING737 7373G7 1384595NM AFT FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030416001692003041600169EA 2003 4 16 COMA0360182 120030402A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HYD SYS WEAK A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01457CA3072 7612 FLIGHT 5710 GEAR DISAGREE WARNING, NOSE LANDING GEAR DID NOT EXTEND. REPLACED HYDRAULIC PUMP 3A. 2L72 4F4 FRTA21EA E15NE 20030417000732003041700073SO 2003 4 17 SWIA200311747 120030126A492038003761 APU EMB 120 EMB120ER 3260203SO SMOKE A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 NM07221SW 120290 APU BLEED CAUSES LAVATORY SMOKE DETECTOR TO GO OFF. REMOVED AND REPLACED APU IAW EMB 120 MM 49-00-02. S/N OFF P-456. 2L72 4T RTA31SO 20030417001532003041700153SO 2003 4 17 SWIA200311765 120030128A7712 INDICATOR EMB 120 EMB120ER 3260203SO RT ENGINE MALFUNCTIONED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07186SW 120034 ON DEPARTURE FROM SLC, WHEN CLIMB POWER WAS SET 84 PERCENT TORQUE THE RIGHT TORQUE GUAGE FLUCTUATED, BOTH ANALOG AND DIGITAL. ALL OTHER ENGINE PARAMETER STAYED STABILIZED. FLUCTUATIONS WERE FROM 84 PERCENT TO APPROXIMATELY 50 PERCENT. REMOVED AND REPLACED RIGHT TORQUE INDICATOR PICK UP PROBE IAW P&W MM 72-01-60 AND EMB MM 77-11-02. OPS CHECK GOOD ON ENGINE GROUND RUN. P/N 3116947-01. 2L72 4T RTA31SO 20030425000902003042500090NM 2003 4 25 QXEA0300397 120030316A5420 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND LOWER COWL LOWER ANGLE IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030430001202003043000120WP 2003 4 30 03FDEA00600 120030424A5710 HINGE DOUG DC10 DC1030 3023501WP WINGS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR S 31 C/W E.A.8-5740-68783-L/H I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION .COMPLIED WITH E.A.8-5740-68783. ON 04/18/03. 2L73 4F A22WE 20030502002332003050200233NM 2003 5 2 DHL2003783001 120030415A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF ADJUST A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01766AT 21999 NR 3 FIRE DETECTOR INOPERATIVE LIGHT ILLUMINATED INDICATING A SHORT IN THE RESPECTIVE ENGINE'S FIRE DETECTION CIRCUITRY. INSPECTED LOOP AND ADJUSTED SLIGHTLY IAW BMM CHAPTER 26-11-01, OPS CHECKED GOOD ON GROUND. 2L73 4F A3WE 20030506001892003050600189WP 2003 5 6 ASAA0380216 120030307A53209930538U67 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FORWARD CARGO AREA LEFT CUSP WEB CRACKED. REPLACED CUSP WEB PER SRM. (M) 2L72 4F A6WE 20030506002012003050600201WP 2003 5 6 ASAA0380131 120030213A5311991960563 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01964AS 53078 OAK - DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF CIRCUMFERENCE FRAME IN AFT CARGO BAY COMPARTMENT AT FS 1271 BETWEEN L28 AND R28 LONGERONS. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 5303, 51-10-3, 51-10-3B, 51-30-2, AND 50-30-5. (M) 2L72 4F RTA6WE 20030509000052003050900005CE 2003 5 9 MGF2003F00000 120030310A32305141001225 TRUNNION CESSNA310 310R 2074245CE CONT O520 IO520* 17032SO MLG INOPERATIVE B MGFRO OTHER O OTHER NRNOT REPORTED 1 EA236096C5064 310R1263 DURING SCHEDULED INSPECTION REMOVED BOTH MAIN LANDING GEAR TRUNNIONS TO INSPECT ATTACH PINS AND BEARINGS. FOUND EXCESSIVE UP AND DOWN MOVEMENT OF PINS IN TRUNNIONS. (FOR AND AFT MOVEMENT WAS SATISFACTORY). TRUNNIONS WERE BUSHED AND NEW PINS INSTALLED IAW MFG. 1L72 3O3 O 3A10 E5CE 20030513002652003051300265NM 2003 5 13 2003F00253 120030410A3610 DUCT BOEING727 727225 1384077NM NR 1 ENGINE LEAKING A MYWAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO19804MA 22435 ON TAKEOFF FROM CAE, AFTER GEAR RETRACTION NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ABNORMAL CHECKLIST PROCEDURES AND ENGINE SHUTDOWN PROCEDURES. DECLARED AN EMERGENCY WITH ATC AND AIRCRAFT CLEARED TO SAV FOR LANDING. LANDED AT SAV WITHOUT INCIDENT. FOUND SEVERAL LEAKING DUCTS ADJACENT TO OVERHEAT LOOP. REPOSITIONED CLAMPS AND NO LEAKS NOTED. RAN ENGINE AT TAKEOFF POWER FOR 5 MINUTES. SYSTEM OPS CHECKS NORMAL IAW MM 36-12-01. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030513000082003051300008EA 2003 5 13 QXEA030542 120030508A26109847101501 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX3364 22 10005 THE FORWARD, CENTER, AND AFT SECTIONS OF THE SMOKE DETECTOR CHIMNEY ARE DAMAGED. MAINTENANCE REPLACED THE DAMAGED SECTIONS AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513002472003051300247EA 2003 5 13 ASOA03155 120030410A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 DURING A C-CHECK IN MCN, THE LOWER METAL TRIM PANEL NUT PLATE ANGLE AT THE SERVICE DOOR ENTRANCE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING THE LOWER METAL PANEL NUT PLATE ANGLE AT THE SERVICE DOOR ENTRANCE IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030530000902003053000090CE 2003 5 30 050601 120030511A2720130380033 TRANSDUCER BEECH 1900 1900D 1154162CE RUDDER BOOST FAILED A AMWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE073YV 2665 2665 UE3 FROM FARMINGTON NEW MEXICO TO ALBURQUERQUE NEW MEXICO ON FLIGHT 704, DURING TAKEOFF THE RUDDER FELT CROOKED AND STIFF ACCORDING TO THE CREW. ABORTED TAKEOFF AND RETURNED TO THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE CHANGED THE LEFT HAND ENGINE RUDDER BOOST TRANSDUCER. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20030610000662003061000066NM 2003 6 10 DLM88030407 120030501A2612 FIRE WARNING DOUG MD88 MD88 3023688NM COCKPIT FALSE ACTIVATIONA DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27955DL 49886 ON PUSHBACK FROM CVG GOT OAP..CARGO FIRE..LIGHT WITH NO OTHER FIRE INDICATIONS. REPLACED OAP PANEL PER M/M. OP CHECKS OK 2L72 4F RTA6WE 20030520000652003052000065NM 2003 5 20 AMTA200300526 120030418A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11525AT 30548 RED TRACK LIGHT AT LAST ROW INOPERATIVE. REPLACED EMERGENCY TRACK LIGHT ASSEMBLY, CHECKS GOOD. REF MM 33-51-11. (M) 2L72 4F RTA2NM 20030521000512003052100051EU 2003 5 21 MALA030254 120030430A5755 STRUCTURE BAC 146 AVRO146RJ85A1500097EU RT LIFT SPOILER DAMAGED A MALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL15504XJ E2311 DURING FLIGHT 3636, SLIGHT CONTROL FLUTTER FELT AT 275 KNOTS. FLUTTER IS FELT IN THE FLIGHT CONTROLS AT AIRSPEED OF 275 KNOTS IN CLIMB AND CRUISE WITH AUTO PILOT ENGAGED. MAINTENANCE FOUND TRAILING EDGE OF RT LIFT SPOILER TO BE SLIGHTLY RAISED. RE-CONTOURED EDGE CHECKS GOOD IAW CHECKS IN AMM 27-61-14. 2H74 4F RTA49EU 20030521000902003052100090WP 2003 5 21 DHL2003801071 120030512A53303654299401 FILLET DOUG DC8 DC873F 302199FWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 LT LWR FILLET 724 AT STA 779.000 INTERNAL SKIN DELAMINATED. REMOVED AND REPLACED LT LWR FILLET 724 AT STA 779.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030522000782003052200078SO 2003 5 22 C2XA03SH138 120030518A531014525480003 BEAM EMB 145 EMB145ER 3260211SO BAGGAGE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV DURING C-CHECK THE LOWER BAGGAGE DOOR CUTOUT BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 53-31-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030611000852003061100085SW 2003 6 11 HEEA086693 120030522A6220412010216105 BEARING BELL 412 412 1182202SW MAIN ROTOR ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L7157 33023 BEARING ROUGH. SHOP REPAIR. 1G72 4U H4SW 20030610000802003061000080NM 2003 6 10 DLM88030421 120030502A27813953485501 SENSOR DOUG MD88 MD88 3023688NM NR 1 SLAT MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27934DL 49721 UPON SLAT RETRACTION DISAGREEMENT LIGHT ILLUMINATED WITH FLAP HANDLE IN THE FULL UP POSITION.NO ASSYMETRY. FOUND C31 SENSOR PLUNGER AND SPRINGS WORN.REPLACED SAME. SYSTEM CKS OK 2L72 4F RTA6WE 20030613000602003061300060NM 2003 6 13 UPS03440794 120030516A5320 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - STA 580, STR 23R ATTACH TIE CLIP FOUND CORROSION REVEALED. M/D BS 580 S23R ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8 DUE TO CORROSION 1 X 0.5 X 0.020 INCH MAT'L REMAIN OUT OF SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F RTA20WE 20030613000982003061300098NM 2003 6 13 UPS03440811 120030515A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D - LT FRAME SHEAR TIE CRACKED (BS 520) AT S9L. U/D BS 520 LT FRAME AT S9L REPAIRED AS PER HX RS R53-12-35024 AND UPS EO B747-5310-18844-A. 2L74 4F RTA20WE 20030523000672003052300067NM 2003 5 23 SWAA031099 120030516A53306545890 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030527001072003052700107NM 2003 5 27 2003F00317 120030218A3233BACH30AT080310 LINE BOEING727 7272F9 138407DNM RT MLG ACTUATOR DEFECTIVE A PCSAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO17199AJ 21426 FLT 825 - SVD-GND - CREW REPORTED, ON APPROACH LOST OF SYSTEM 'A' HYDRAULICS. CAPTAIN ELECTED TO DIVERT FROM SVD TO GND. AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE FOUND MLG ACTUATOR HOSE LEAKING. A TEMPORARY FLEX LINE WAS INSTALLED IN PLACE OF THE DEFECTIVE HYDRAULIC LINE. THE HYDRAULIC SYSTEM WAS SERVICED. CYCLED FLIGHT CONTROLS AND LANDING GEAR SEVERAL TIMES. CHECKED NR 1 AND NR 2 ENGINE HYDRAULIC PUMPS. OPS AND LEAK CHECK GOOD. SERVICE SYSTEM IAW 12-12-0. TRANSFERRED TEMPORARY REPLACEMENT ON DMI# 12508 IAW GMM 4-21-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20030618000702003061800070NM 2003 6 18 SWAA031311 120030610A52306547952 SKIN BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT CORNER OF HANDLE SPRING FLIP DOOR. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030618000412003061800041NM 2003 6 18 SWAA031333 120030613A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM LT LOWER CHORD CORRODED AT BS 540. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20030619000422003061900042SW 2003 6 19 HEEA087192 120030609A2435209060221001 STARTER GEN BELL 412 412 1182202SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 STARTER GEN CONTINUES TO RUN. 1G72 4U H4SW 20030619001002003061900100SW 2003 6 19 HEEA087424 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030630000142003063000014CE 2003 6 30 2003F00331 120030529A321108411111 SCREW CESSNA310 310Q 2074242CE CONT O470 IO470V 17026SO MCAULY3AF32C3AF32C87 GL ADJUSTMENT BROKEN A O OTHER O OTHER LDLANDING 1 SW01589DM 310Q1048 171303R 881400 ON LANDING ROLLOUT AT 30 KNOTS, THE RIGHT MAIN LANDING GEAR COLLAPSED CAUSING RIGHT PROP TO STRIKE THE GROUND. THE ADJUSTMENT SCREW PN 0841111-1 BROKE. A SPAS PN QUERY SHOWED NO OTHER ACCIDENTS OR INCIDENTS. 1L72 3O3 O 3A10 3E1 5 CP22EA 20030630000462003063000046SW 2003 6 30 HEEA087829 120030618A28221C2710 CARTRIDGE BELL 407 407 1182206SW ALLSN 250C 250C47B GL BOOST PUMP FAILED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03406PH 53198 LEFT BOOST LIGHT ILLUMINATED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030624000062003062400006EU 2003 6 24 A6WA200360028 120030513A2150 A/C PACK BAC 146 146200A 1500266EU SMOKE A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31606AW E2033 PACKS EMITTING SMOKE INTO CABIN MAINTENANCE REMOVED AND REPLACED APU, PERFORMED PACK BURNOUT IAW AWAC SUPP 96.31. (M) 2H74 4F A49EU 20030707000932003070700093NM 2003 7 7 DLM88030599 120030630A499036280 APU DOUG MD88 MD88 3023688NM AFT LEAKING A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27970DL12084 43173 WITH CONDITIONED AIR AND PACKS POWERED BY START CART FUMES ENTERED CABIN. TURNED OFF PACKS FUMES DISSIPATED. AFTER TAKEOFF, CABIN WAS KEPT COOL AND FUMES DISSIPATED TOTALLY. IN CRUISE WHEN TEMP SELECTED ABOVE 60 DEG FUMES NOTICED AGAIN. PERFORMED OPNS 5088,5089 CABIN SMOKE/ODER T/S AND DUCT BURNOUT. NO CABIN FUMES NOW NOTED 2L72 4F RTA6WE 20030702000262003070200026EA 2003 7 2 A6WA200340030 120030219A3010 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA RT ENGINE FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31409AW 7447 RIGHT COWL ANTI-ICE CASS RECEIVED INFLIGHT, COMPLIED WITH QRH PROCEDURES, MESSAGE REMAINS. REMOVED AND REPLACED RIGHT ENGINE PRESSURE RELIEF SHUTOFF VALVE. (M) 2L72 4F RTA21EA 20030707001712003070700171NM 2003 7 7 AWXA200300744 120030627A3350ABS0374B HOUSING AIRBUSA319 A319132 3930340NM RT OVERWING EXITDEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28820AW 1397 EMERGENCY LIGHT FLASHING ON AND OFF AT RT OVERWING EXIT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT HOUSING AT THE RT OVERWING EXIT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030709000742003070900074WP 2003 7 9 MWEA030239 120030604A522049144121 FITTING DOUG DC9 DC932 3022066WP OVERWING EXIT LOOSE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31502ME 48132 CREW REPORTED AFT LEFT OVERWING EXIT DOOR MAKING NOISE AND APPEARS TO BE LOOSE. ADJUSTED LATCH BAR. 2L72 4F A6WE 20030429001952003042900195NM 2003 4 29 CA030409018 120030403A5330 SKIN BOEING737 7372Q9 138448MNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 2.5 FT CRACK FOUND ON EXTERIOR FUSELAGE AT FS 733 AT STRINGER S-17R. CRACK REPAIRED I.A.W. SRM 53-30-3 FIG.25. TIMES - 57548:02 CYCLES- 54795 2L72 4F4 F A16WE E2EA 20030430001352003043000135NM 2003 4 30 SWAA030914 120030424A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT BS 725 @ STR 23R & BS 884 @ STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030430001502003043000150NM 2003 4 30 SWAA030885 120030421A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030501001002003050100100EU 2003 5 1 USAA030027 120030311A5320 STRUCTURE AIRBUSA321 A321211 3930370EU DOOR MOD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19166US 1436 PIT - FOUND DOOR MOD CORNER CRACKED, FORWARD OF FS 50 STRINGER 37R, AFT CARGO BIN. INSTALLED DOUBLER PER EA 76006. (M) 2L72 4F RTA28NM 20030502000942003050200094SO 2003 5 2 C2XA03TY047 120030415A531313500473002 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE BENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715527 145413 TYS, DURING A SCHEDULED INSPECTION A TEMPORARY REPAIR BETWEEN FRAMES 24 AND 25 AT STRINGER 12R, WAS MADE PERMANENT. REMOVED THE OLD REPAIR STRINGER 12R, CUT OUT A SECTION OF FR 24 AND INSTALLED A FRAME SPLICE, DOUBLER AND STRINGER IAW SRM 53-00-04, 53-22-01, 51-21-04 AND 05. THE REPAIR WAS SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030501002002003050100200NM 2003 5 1 ASAA0310033 120030225A53206541986503 PAD BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, STANSION PAD AT BS 559, RIGHT BUTTOCK LINE 50 CORRODED. REMOVED AND REPLACED STANSION PAD PER SRM. (M) 2L72 4F RTA16WE 20030505001692003050500169NM 2003 5 5 SWAA030841 120030415A33506104789 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED A1 CHECK, FOUND BOTH FWD ENTRY & FWD SVC DOOR THRESHOLD EMERGENCY EXIT LIGHTS STAY ILLUMINATED WHEN SW IS IN OFF POSITION. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030505002022003050500202NM 2003 5 5 UPS03M40435 120030315A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT RBL 8.5 BETWEEN STA 1273-1289 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK STA 1273-1289 RBL 8.5 & FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I REV 32 & 51-21-01 VOL II REV 32. NEW SEAT TRACK REWORKED & HOLES PICK OUT AS PER SRM 53-70-00 VOL I REV 32, SEAT TRACK PROTECTED PER SRM 51-21-01 REV 32 VOL II & NEW SEAT TRACK INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 1273-1289 RBL 8.5. 2L73 4F RTA22WE 20030505002342003050500234WP 2003 5 5 UPS03840450 120030412A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C1 LT FUSELAGE SKIN IS DENTED AT STA 300 AT LONG 20L. REWORKED DENT, FOUND WITHIN LIMITS, NDT VERIFIED A .375 INCH CRACK AT DENTED AREA. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AROUND CUTOUT. FABRICATED AND INSTALLED DOUBLER FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030506001252003050600125NM 2003 5 6 P5CA0300853 120030412A5310 DOOR FRAME BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 THE 5 L DOOR LWR FWD FRAME CUTOUT CRACKED. REPAIR PER SRM 51-30-02. 2L74 4F A20WE 20030506001562003050600156NM 2003 5 6 IU62003F00005 120030505A2760654494710 HOUSING BOEING BOEING737 737* NM ACTUATOR CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 557143394 0881 HOUSING IS CRACKED AT THE MIDDLE SHOULDER OPPOSITE MOUNTING LUG. METAL FATIGUE, CYCLING PROBABLE CAUSE. UTILIZE THE UPGRADED HOUSING ASSEMBLY. 2L72 4F RTA16WE 20030507001242003050700124EU 2003 5 7 AUS20030391 120030403A5753D5754008120000 FLAP TRACK AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE TE FLAPS CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING NR 2 FLAP TRACK AFT SPIGOT AND BUSH CONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTION IAW J9-IA57-0400 (R2). 2L72 4F4 FRTA46NM E29NE 20030508000202003050800020NE 2003 5 8 DL777030342 220030407A7200 ENGINE BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 1 FAILED A DALAA UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27866DA11957 051188 29738 051188 ATB-NR 1 ENGINE VIBRATES N2 5.0 AND COMPRESSOR STALL. METAL FOUND IN TAILPIPE ON ARRIVAL IN MAN. 2L72 4F4 FRTT00001SEE00050EN 20030514000592003051400059NM 2003 5 14 SWAA030958 120030429A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20030528000222003052800022SW 2003 5 28 HEEA086588 120030507A5302204030769006S BULKHEAD BELL 412 412 1182202SW TAILBOOM MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 BULKHEAD IS 3/16 INCH TOO WIDE ON FORWARD END AT FLANGE RADIUS. 1G72 4U H4SW 20030714000522003071400052NM 2003 7 14 SWAA031377 120030621A33506104781 HOUSING BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT HOUSING PER MM. 2L72 4F RTA16WE 20030716001202003071600120SW 2003 7 16 HEEA087976 120030622A6210214015300107 BLADE BELL 214 214ST 1182106SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03598066388 28140 THE SKIN AT THE ROOT END IS UNBONDED AND SKIN AT THE TIP END NEXT TO THE TIP SHOE IS UNBONDED. TRIM TAB UNBONDED. FRETTING PAD HAS SOME SEPERATION. 2G72 4U H10SW 20030116000962003011600096 2003 1 16 HEEA083051 420030107A34427021450601 COMPUTER BELL 214 214ST 1182106SW WX RADAR SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 WX RADAR COMPUTER FAILED IN FLIGHT. 2G72 4U H10SW 20030124001012003012400101EA 2003 1 24 COMA0360041 120030122A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01443CA 7539 FLIGHT 5617 FLAPS FAIL CAUTION MESSAGE FLAPS FAILED AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2L72 4F RTA21EA 20030129000432003012900043SW 2003 1 29 HEEA083956 120030117A3246407012203 SKID BELL 407 407 1182206SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 LT MLG SKID IS CORRODED. 1G71 3U O H2SW 20030129001002003012900100SW 2003 1 29 HEEA083993 120030117A7810 WASHER BELL 407 407 1182206SW EXHAUST DUCT DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 EXHAUST DUCT BUFFER WASHER UNBONDED. 1G71 3U O H2SW 20030131000532003013100053EU 2003 1 31 CA030106003 120030104A3230D31AB4431 ISOLATION VALVE AIRBUS330 A330342 EU RROYCERB211 RB211TRENT77 NE MLG FAILED W O OTHER J WARNING INDICATION DEDESCENT 1 CA (CAN) LANDING GEAR DID NOT LOWER ON APPROACH. CREW RECYCLED TWICE WITH NO SUCCESS.ALTERNATE EXTENSION (FREE FALL) CARRIED OUT AND UNEVENTFUL LANDING ACCOMPLISHED. L/G ISOLATION SAFETY VALVE REPLACED AS PER AMM 32-31-17 AND OPERATION CHECK CARRIED OUT AS PER AMM 32-31-00. LANDING GEAR EXTENSION / RETRACTION SYSTEM CHECKED SERVICEABLE. 1L72 4F4 FRTA46NM E39NE 20030131001422003013100142NM 2003 1 31 PCAA0301027 120030130A6123V319 SWITCH DHAV DHC8 DHC8102 2809003NM COCKPIT STUCK A PCAAK NONE S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA13846EX 326 PIT-FLIGHT#3989. CREW REPORTED #1 GROUND RANGE LIGHT CYCLES WITH POWER LEVER IN DISC. MAINTENANCE REPLACED POWER LEVER SWITCH 6141 S3 AND SWITCH 6121 S11 FOUND TO BE OUT OF ADJUSTMENT. REMOVED AND REPLACED SWITCHES IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 76-10-13. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030209000012003020900001NM 2003 2 9 ANCF200300006 120030206A2911NAS16128 PACKING BOEING767 76733A 1385209NM BROKEN W ANCFD RETURN TO BLOCK K FLUID LOSS CRCRUISE 1 SO23535AW 25535 L HYD QTY DECREASE TO 0.06 WITH EDP PRESSURIZED AND ACMP OFF; HYD QTY CONTINUED DECREASING. AIRCRAFT RETURNED TO BOGOTA.CORRECTIVE ACTION:LH DIFFERENTIAL PRESSURE INDICATOR WAS FOUND WITH LEAK. DIFFERENTIAL PRESSURE INDICATOR WAS REMOVED AND BOTH PACKINGS WERE REPLACED IAW AMM 29-11-15 PAGE 401 AND AMM 20-10-19 PAGE 401. LH HYD SYSTEM WAS REFILLED IAW AMM:12-12-01PAGE 301. ENG RUN UP LEAK CHECK WAS PERFORMED WITHOUT DUPLICATING FAULT. 2L72 4F RTA1NM 20030213000422003021300042 2003 2 13 CA030204001 420030202A3197693733595 CONTROL PANEL BOEING737 737275 1384485NM PWA JT8 JT8D17 52049NE COCKPIT SMOKE W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) AT 33000 FT, SMOKE WAS NOTICE COMING FROM THE OVERHEAD COCKPIT FUEL PANEL P5-2. PUMPS SELECTED OFF. DECLARED AN EMERGENCY LANDING. REPLACED PANEL. 2L72 4F4 F A16WE E2EA 20030218002442003021800244NM 2003 2 18 SWAA030240 120030130A335007912 COVER BOEING737 7377H4 1384404NM FWD CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29713SW 27847 EEPLS COVER MISSING IN FWD CABIN. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20030220000082003022000008CE 2003 2 20 FPI2003F00003 120030204A323398820152 ACTUATOR CESSNA210 210N 2073453CE CONT O520 IO520* 17032SO MLG CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO155307A16173 21063360 INSPECTED ACTUATORS FOR CRACKS. FOUND CRACKS, REMOVED FROM SERVICE. 1H71 3O3 O 3A21 E5CE 20030227000682003022700068 2003 2 27 HEEA084382 420030211A2312CI196 ANTENNA BELL 407 407 1182206SW VHF COMMS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 VHF ANTENNA WEAK TRANSMITTING. ANTENNA BASE PLATE CORRODED. SCRAPPED. 1G71 3U O H2SW 20030306001202003030600120SW 2003 3 6 HEEA084822 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 MAIN ROTOR HEAD HAS A WORN ROD BEARING. REPAIRED. 1G72 4U H4SW 20030307000582003030700058NM 2003 3 7 SWAA030446 120030226A533065458197 WEB BOEING737 7373H4 1384600NM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND RT NLG W/W WEB CRACKED AT BS 246, WL 168.5. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20030308000052003030800005CE 2003 3 8 RAIA00302051 120030214A32005004VC CONNECTOR CESSNA206 U206G 2073356CE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03723 U20606714 5521-MLI - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE DEFERRED IAW MEL 32-31-03. SUBSEQUENTLY REPLACING CONNECTOR 5004VC AND WIRES, OPS CK OK. 1H71 3O A4CE 20030310001442003031000144NM 2003 3 10 EIA2003043 120030228A5300UNK STRINGER BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 LAP @ STA 2280 to 2340, RIGHT SIDE, STRINGER 12, HAS CORROSION LIFTING SEALANT. CORRECTIVE ACTION: REPAIRED STRINGER 12, FAB'D DOUBLER, PRIMED AND SEALED PER B747 SRM 53-30-03, FIG 18, & 53-30-02, FIG 2. REST OF LAP PER EO 53-747-1047-90 Rev B. 2L74 4F A20WE 20030121002032003012100203SW 2003 1 21 HEEA083347 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW034180F MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030320001432003032000143NM 2003 3 20 2003UALA00136 120030202A7603 THROTTLE CABLE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 1 ENGINE BINDING A UALACD ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 WP29619UA 21879 NR 1 ENGINE THROTTLE CABLE BINDING. LEFT THROTTLE LEVER WILL NOT PROCEED PAST IDLE. NO THROTTLE RESPONSE AT 20 KTS. PUSH-PULL CABLE FOUND BINDING. CABLE WAS REPLACED. DELAY 2:48. PULL CHECK AND INSPECTION DONE AT C-CHK. NO KNOWN PREVIOUS INCIDENTS. 2L72 4F4 FRTA1NM E3NE 20030122001512003012200151NM 2003 1 22 DL757030042 120030109A3240EM91795 VALVE BOEING757 757232 1384965NM RT MLG WW FAILED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27619DL 22909 ON TAXI OUT, PARKING BRAKE LIGHT AND ANTISKID LIGHTS ILLUMINATED SIMULTANEOUSLY AND WOULD NOT RECYCLE. REPLACED PARKING BRAKE VALVE V41 PER M/M. 2L72 4F RTA2NM 20030731000822003073100082NM 2003 7 31 QXEA200300803 120030624A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - DAMAGE AT STATION X3.0 AT STRINGER 31 ON LOWER FUSELAGE EXTERNAL SKIN. REPAIRED IAW RD 8/4-53-578. 2H72 4T RTA13NM 20030729001462003072900146WP 2003 7 29 ABXA030294 120030624A522059131951 PAN DOUG DC9 DC932 3022066WP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 RIGHT FORWARD EMERGENCY OVERWING EXIT DOOR PAN WAS CRACKED AT LOWER FORWARD FITTING. REPAIRED FITTING IAW DC-9 SSRM K07390, 51-30-2, AND 51-30-5. 2L72 4F A6WE 20030321001082003032100108NE 2003 3 21 2003UALA00253 220030307A7261 SWITCH BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29533UA 25073 726711 A/C RECEIVED NR 1 ENGINE OIL FILTER BYPASS MESSAGE. DELTA PRESSURE SWITCH AND OIL FILTER REPLACED. 2L72 4F4 FRTA2NM E17NE 20030324000342003032400034NM 2003 3 24 DHL2003749003 120030322A3350 BATTERY PACK BOEING727 727200 138407ENM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01749DH 22013 1) COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE.2) REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECKED GOOD. DONE IAW B-727 M/M 33-50-111. 2L73 4F RTA3WE 20030325000732003032500073NM 2003 3 25 AWXA200300239 120030310A7830 PROXIMITY SENSOR BOEING737 7373G7 1384595NM THRUST REVERSER DAMAGED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28150AW 23218 DURING TAKEOFF ROLL AT LAS EN ROUTE FOR OAK THE MASTER CAUTION LIGHT ILLUMINATED FOLLOWED BY NO. ENGINE AFT BOOST PUMP LIGHT, REJECTED TAKEOFF AT APPROXIMATELY 110 KTS. MAINTENANCE PERFORMED HIGH POWER ENGINE RUN, COULD NOT DUPLICATE THE NR1 ENGINE BOOST PUMP LIGHT. FOUND THE NR 2 ENGINE THRUST REVERSER LIGHT ILLUMINATED ON THE OVERHEAD PANEL. ISSUED DPI MEL 78-1 COND. 3, "NR 2 ENGINE T/R INOP". 03/11/2003 MAINTENANCE FOUND NR 2 ENGINE THRUST REVERSER INBOARD PROXIMITY SENSOR WAS BEING STRUCK BY THE TARGET. REMOVED AND REPLACED PROXIMITY SENSOR IAW BMM 78-34-03-04. NO HELP, PROBLEM STILL EXISTS. 2L72 4F RTA16WE 20030422001192003042200119NM 2003 4 22 USAASB03038 120030311A21337110033 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN PRESSURE MALFUNCTIONED A USAAB EMER. DESCENT O OTHER CRCRUISE 1 EA19577US 23742 PHL - FLT 1897 - EN ROUTE FROM DFW-PHL, AT FL370, THE CABIN ALTITUDE EXCEEDED 10,000 FEET. CABIN WAS CLIMBING AT 100 FEET PER MINUTE. CAPTAIN DECLARED AN EMERGENCY AND DESCENDED TO FL240, WHERE CABIN PRESSURE WAS MAINTAINED IN STANDBY MODE. FLIGHT CONTINUED ONTO PHL AND LANDED WITHOUT FURTHER INCIDENT. OXYGEN MASKS WERE DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE FORWARD OUTFLOW VALVE (P/N 32-2684-007) AND THE AFT OUTFLOW VALVE PER MM 21-43-11 AND 21-31-11. OPERAITONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20030423001492003042300149WP 2003 4 23 ZW0A0303009 120030306A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 AT STA 160 THE FRAME WAS DAMAGED AT LONGERON 19R TO 22R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20040223001572004022300157NM 2004 2 23 QV12004F00000 120031225A2570 HUMIDIFIER BOEING737 737* NM GE CFM56 CFM56* 13802NE CABIN MALFUNCTIONED W QV1YA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA33737GG 29136 874583 DURING TEST FLT, FOLLOWING MAINTENANCE INPUT. SMOKE REPORTED IN CABIN AT 31000 FT. AIRCRAFT RETURNED TO AIRPORT. ON INVESTIGATION, CABIN HUMIDIFIER CONTROL CIRCUIT BREAKER C9124 ON AUX POWER DISTRIBUTION PANEL P9101 FOUND TRIPPED. CABIN HUMIDIFIER SYSTEM DEACTIVATED FURTHER INVESTIGATION TO BE CARRIED OUT WHEN AIRCRAFT IS AVAILABLE. TEST FLIGHT REPEATED, NO FURTHER SMOKE REPORTED. NOTE: HUMIDIFIER IS NON-ESSENTIAL EQUIPMENT. 2L72 4F4 FRTA16WE E2GL 20040223001782004022300178WP 2004 2 23 ABXA040012 120031127A5311 FRAME DOUG DC8 DC861 3021952WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 A/C ACCESS COMPARTMENT AT FS 56, BETWEEN LONGERON 35 LT AND 35 RT, FRAME LOWER FLANGE WAS CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND REA D853-48484MR. 2L74 4F 4A25 20030829000032003082900003CE 2003 8 29 52034AMWA2 120030628A32301013880083 VALVE BEECH 1900 1900D 1154162CE LANDING GEAR FAILED A AMWAO OTHER O OTHER APAPPROACH 1 CE07126YV UE126 DURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3 GREEN) INDICATIONS. LANDED NORMALLY WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED ON THE TAXI WAY AND THE AIRCRAFT WAS TOWED TO THE HANGAR. MAINTENANCE REPLACED THE LANDING GEAR SERVICE VALVE AND LT UPLOCK SWITCH. THE PART HOURS WILL BE AVAILABLE AT A LATER DATE. REFER TO SDR 52034. 2L72 4T RTA24CE 20030902001812003090200181NM 2003 9 2 03FDEA01084 120030710A533053FX130179 TRIPLER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE MAIN CARGO DOOR WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25284FE 22621 MDIS 284 53-30 0005339 07JUL03 BFM CLOSER COMPLY WITH EA 7-5330-70973 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR,P/N 53FX1301-7/-9 (AD 2002-16-19). FACT 10JUL03 10:28 BFM R COMPLIED WITH E.A. NR 7-5330-70973 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR, P/N 53FX1301-7/-9 (AD2002-16-19). 2L73 4F4 FRTA3WE E2EA 20030728001062003072800106NM 2003 7 28 SWAA031623 120030722A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030729000302003072900030EA 2003 7 29 03203660 120030722A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27660BR 7519 DURING MAINTENANCE INSPECTION THE FORWARD SECTIONS OF THE EMERGENCY TRACK LIGHTING WERE FOUND INOPERATIVE MAINTENANCE PERSONNEL CLEANED AND RESECURED THE CONNECTORS ON THE FORWARD SECTIONS OF THE EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030806001222003080600122SO 2003 8 6 C2XA03TY100 120030725A531114522898605 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE BENT A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713929 145009 ON GROUND WITH GUSTLOCK ENGAGED, AIRCRAFT EXPERIENCED WINDS GUSTING 54+KTS. GUSTLOCK DISENGAGED. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE FRAME JUST FORWARD OF THE GUSTLOCK ASSY IN THE FORWARD FUSELAGE UNDER THE COCKPIT CENTER PEDESTAL BENT. MAINTENANCE REMOVED AND REPLACED THE FRAME IAW EMB-135/145 SRM 51-40-02. TEST FLIGHTED GOOD. AIRCRAFT RELEASED TO SERVICE. 2L72 4F RTT00011AT 20030902001262003090200126NM 2003 9 2 AWXA200300780 120030607A53306545770140 SKIN BOEING737 7373Y0 1384671NM ZONE 200 - FUSELDENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK, DENTS FOUND ON CROWN SKIN FROM BS 540 TO BS 727 STR 4 RT TO STR 10 RT. MAINTENANCE REMOVED AND REPLACED CROWN SKIN FROM BS 540-727 STR 4 RT TO STR 10 RT IAW SRM 51-40-02 PG. 38 FIG. 8 AND AWA E.R. 03-5100-01187-JS1C. 2L72 4F RTA16WE 20030903002422003090300242EA 2003 9 3 03238624 120030826A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27624BR 7211 DURING MAINTENANCE INSPECTION THE 3RD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030904000762003090400076EA 2003 9 4 QXEA200300938 120030716A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA PAX DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 PDX- PASSENGER MAIN CABIN DOOR EXTERIOR SKIN HAS THREE GOUGES ON UPPER AFT CORNER EDGE OF DOOR. REPAIRED IAW CRJ SRM 51-20-06, 51-21-11, 51-25-01 AND AMM TASK 51-26-00-100-801-A01. 2L72 4F RTA21EA 20030904000222003090400022EU 2003 9 4 AWXA200300801 120030713A2930114079017 SELECTOR VALVE AIRBUS320 A320232 3930326EU MLG BYPASSING A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28658AW1406114057 1110 EN ROUTE, CREW OBSERVED A GREEN HYD SYS OVERHEAT MESSAGE ON ECAM & PROCEEDED WITH ECAM ACTIONS. FLT RETURNED TO PHX WHERE MX PERFORMED A GREEN HYD SYS INTERNAL LEAKAGE TEST IAW TSM 29-00-00-280-001. MAINT DISCOVERED MLG SELECTOR VALVE BYPASSING HEAVILY & PROCEEDED TO REMOVE & REPLACE MLG SELECTOR VALVE & MLG DOOR SELECTOR VALVE IAW AMM 32-31-34, AMM 32-31-12 & AMM 32-31-00. LEAK & OPERATIONAL TESTS GOOD. VENDORS PRE-TEST OF MLG SELECTOR VALVE CONFIRMED FAILURE OF UNIT FOR EXTERNAL LEAKAGE, RESEALED UNIT PER CMM 32-31-34, VENDORS PRE-TEST OF MLGDOOR SELECTOR VALVE P/N 114079016, S/N CWDD-DH 48-99 ALSO CONFIRMED FAILURE OF UNIT FOR INTERNAL LEAKAGE. UNIT REPAIRED IAW CMM 32-31-34 BY REPLACING 2 EACH PISTON SEA2L72 4F RTA28NM 20030812000462003081200046 2003 8 12 HEEA088418 420030730A2350A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 INTERMITTENT TRANSMIT. SHOP REPAIR. 1G72 3U H1NE 20030814000432003081400043NM 2003 8 14 SWAA031772 120030807A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030813001572003081300157NM 2003 8 13 SWAA031667 120030725A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030911000172003091100017NM 2003 9 11 03FDEA01311 120030808A5753ARC0502403 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING - O/B T/E FLAP, I/B FWD HINGE FITTING FOUND HYD ACTUATOR'S INBOARD MOUNT HOLE SPOT FACES WITH SURFACE CORROSION. LT WING O/B FLAP, I/B FWD HINGE FITTING HYD ACTUATOR INBOARD MOUNT HOLE SPOT FACES SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030728000332003072800033 2003 7 28 SWAA031593 420030718A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030930000292003093000029NM 2003 9 30 03FDEA01461 120030908A5753652165120 ATTACH FITTING BOEING727 727200 138407ENM FLAP TRACK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25233FE62581 21327 NR 5 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED AT BORE COMMON TO THE TRUNNION STUD. CLEANED AREA AND REINSPECTED AREA IAW BOEING SOPM 20-30-03. NO CORROSION NOTED AFTER CLEANING. 2L73 4F RTA3WE 20030929000012003092900001NM 2003 9 29 PCAA0308103 120030829A32345352011 HANDLE DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A PCAAO OTHER J WARNING INDICATION LDLANDING 1 EA13846EX36405 326 CREW REPORTED THAT DURING APPROACH, WHEN SELECTING GEAR HANDLE DOWN GEAR DID NOT EXTEND. MANUAL EXTENSION WAS PERFORMED AND EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE GEAR HANDLE AND USED A HYDRAULIC MULE FOR OPERATIONAL CHECK. OPERATIONAL CHECK OF EXTENSION AND RETRACTION SYSTEMS WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030528000952003052800095NE 2003 5 28 BAQA086476 220030521A7323430121205 GOVERNOR BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE ENGINE MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911WS4 7068 ENGINE TORQUE MATCHING BELOW 40 PERCENT BEYOND MANUFACTURE SPECS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030602000982003060200098NM 2003 6 2 SWAA031190 120030527A335065C34697 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 21 DEF. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030606000282003060600028NM 2003 6 6 03FDEA00730 120030514A322065348784 PIN BOEING727 727200 138407ENM ZONE 700 VIBRATES A FDEAO OTHER E VIBRATION/BUFFET LDLANDING 1 SO25268FE 21674 AFTER LANDING, LESS THAN 80 KNOTS, NOSE WHEEL BEGAN SEVERE VIBRATIONS. SHUT DOWN ON THE RUNWAY. REPLACED NOSE GEAR LINK PIN. OP CHECKS NORMAL PER B727-200 MM 32-21-021-6. OK FOR SERVICE. 2L73 4F RTA3WE 20030514002212003051400221NM 2003 5 14 03FDEA00639 120030426A5753ARC41251 RIB DOUG MD11 MD11 3023602NM LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT OUTBOARD FLAP ASSY LEADING EDGE, NOSE RIB SUPPORT ISLAND WITH CRACK. LT OUTBOARD FLAP ASSEMBLY LEADING EDGE, NOSE RIB SUPPORT ISLAND REMOVED AND REPLACED AS PER SRM 5-31-01 VOL. II. 2L73 4F RTA22WE 20030609000832003060900083EA 2003 6 9 QXEA0300636 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 8R, 7 INCHES AFT OF FS645. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-03 PG 1-8. 2L72 4F RTA21EA 20030611000812003061100081NE 2003 6 11 HEEA086566 120030522A32437625001101102 MASTER CYLINDER SKRSKYS76 S76A 8143006NE BRAKE SYS LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW031546G 760076 PILOT LEFT BRAKE MASTER CYLINDER LEAKING. IN SHOP REPAIR. 1G72 3U H1NE 20030611001342003061100134EA 2003 6 11 ASOA03199 120030507A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE NR 3 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030612001942003061200194EA 2003 6 12 COMA0360251 120030531A5270601R386455 PLUNGER CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR BENT A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01819CA 7415 FLIGHT 5452 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED BENT PRESSURE VENT VALVE PLUNGER. 2L72 4F RTA21EA 20030612001792003061200179SO 2003 6 12 C2XA03TY083 120030602A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO GALLEY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM PLATE I/A/W-EMB-135/145-SRM-53-21-10 AND CMP-53-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030612001092003061200109NM 2003 6 12 UPS03240747 120030523A5330 SHEAR TIE BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, 2 SUSPECT CRACKS AT SHEAR STRAPS AT LBBL 20 BETWEEN BS 294 & BS 328 2 REPAIRS. FABRICATED NEW SHEAR TIES IAW SRM 51-20-1. REPAIRED SHEAR TIES IAW SRM 51-40-3. INSTALLED NEW SHEAR TIES IAW SRM 51-30-2. 2L73 4F A3WE 20030617001622003061700162SW 2003 6 17 HEEA087301 120030611A6300407010206103 BEARING BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH4449 53327 MAIN ROTORO DRIVE ROD END BEARINGS WORN. 1G71 3U O H2SW 20030522000912003052200091WP 2003 5 22 MWEA030210 120030513A273090G623 PRESSURE SWITCH DOUG DC9 DC915 3022036WP COCKPIT INOPERATIVE A MWEAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 GL31300ME 45718 COULD NOT GET ELEVATOR POWER ON LIGHT TO COME ON. REMOVED AND REPLACED ELEVATOR PRESSURE SWITCH, AND REPAIRED BROKEN WIRES. 2L72 4F A6WE 20030520000992003052000099NM 2003 5 20 USAASB03055 120030410A3260 WARNING LIGHT BOEING737 737401 1384701NM NLG MALFUNCTIONED A USAAO OTHER N FALSE WARNING APAPPROACH 1 EA19417US 23984 ON GEAR EXTENSION INTO PHL, CREW RECEIVED A RED NOSE GEAR UNSAFE LIGHT WITH NO GREEN GEAR INDICATION LIGHTS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND FOUND A CIRCUIT BREAKER FOR THE AIR GROUND SENSOR HAD TO BE RESET. CREW RESET CIRCUIT BREAKER AN RECEIVED NORMAL GEAR INDICATION OF THREE GREEN GEAR LIGHTS AND NO RED GEAR UNSAFE LIGHTS. FLIGHTS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND OPERATIONAL CHECK PER MM 32-61-00-5-001. GEAR INDICATION CHECKS GOOD IN UP AND DOWN POSITION. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030618001492003061800149EA 2003 6 18 COMA0360273 120030611A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01427CA 7460 FLIGHT 5258 CABIN DOOR WARNING MESSAGE. FOUND DOOR HANDLE MECHANISM ALL GUMMED UP. CLEANED AND LUBED DOOR MECHANISM. 2L72 4F RTA21EA 20030618002102003061800210EU 2003 6 18 HEEA087524 120030610A2121AM7031 MOTOR AEROSPAS355 AS355* EU BLOWER FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03732AE 2873 AC CONDENSOR BLOWER MOTOR BLEW 25 AMP CIRCUIT BREAKER AND 50 AMP FUSE. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030929000082003092900008EA 2003 9 29 COMA0360400 120030901A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01999CA 7230 RT REVERSE UNLOCK MESSAGE AFTER T/O. DEFERRED MAINT. ON T/R SYSTEM IAW MEL. 2L72 4F RTA21EA 20030905002142003090500214SO 2003 9 5 C2XA03SH282 120030821A531514526437001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE RIGHT HAND OMEGA BEAM BETWEEN FRAMES 58 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030909000332003090900033SO 2003 9 9 C2XA03CL161 120030906A52207137021504 SHROUD EMB 145 EMB145ER 3260211SO EMERGENCY EXIT LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714925 145004 WHILE PERFORMING A 1A INSPECTION MAINTENANCE REPORTED THAT THE RIGHT HAND EMERGENCY EXIT WOULD NOT OPEN IT WAS BLOCKED AT THE TOP BY A SIDEWALL PANEL. MAINTENANCE RESECURED SIDEWALL PANEL AND ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031002001152003100200115NM 2003 10 2 QXEA200301100 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 3 SEAT TRACK BOTTOM OF CHANNEL HAS A CHAFE .3750 INCH FROM AFT END. REPAIRED IAW DHC-8 RD 8-53-3644 AND SRM 51-00-06. 2H72 4T RTA13NM 20031027000012003102700001NM 2003 10 27 QXEA200301175 120030921A5711 SPAR CAP DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 RIGHT WING LOWER SPAR CAP IS CHAFED WHERE INBOARD END OF 611AR CONTACTS LOWER SPAR CAP. REPAIRED IAW DHC-8 SRM 51-00-06, 51-40-11, 51-20-16, 51-20-36 AND RD 8-57-811. 2H72 4T4 TRTA13NM E20NE 20031027000402003102700040NM 2003 10 27 CALA0300559 120030925A5320 STRAP BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND STRESS WEB UPPER STRAP CORRODED AT STA 1028, RBL 18. THE CORRODED STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031103000082003110300008NM 2003 11 3 DLM88030860 120030921A3610 DUCT DOUG MD88 MD88 3023688NM PNEUMATIC SYS SEPARATED A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27998DL 53370 LOUD NOISE AND VIBRATION IN FLOOR FROM AFT F/A SEAT ON BACK, STARTED WHEN POWER APPLIED DURING T/O RUN. SLIGHTLY MORE NOTICEABLE ON C/P SIDE DURING FLIGHT NOISE AND VIBRATION WOULD INCREASE AS POWER INCREASE AND DECREASE AS THROTTLE RETARDED. FOUND PNEUMATIC DUCT SEPARATED. REPAIRED SAME. 2L72 4F RTA6WE 20040113001922004011300192GL 2004 1 13 RAIA00312303 320031205A6112B4018316 BOOT JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR B5JFR36C1101GL LT PROPELLER FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03555HK 41072 TRI- LEFT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED LEFT PROP NR 3 DEICE BOOT. 2L72 4T RTA41NM 5 CP15WE 20040129001092004012900109NM 2004 1 29 DHL2003742552 120031125A5744 ANGLE BOEING727 727225 1384077NM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 2 SLAT INBOARD TRACK UPPER MOUNT INBOARD L-ANGLE SUPPORT IS CRACKED. REMOVED DAMAGED ANGLE AND FABBED NEW FROM BAC 1505-100617 PO900411 DIM 9.25 X 1.25 X 1 INCH AS PER SAMPLE IAW 727 SRM 57-10-2 FIG 2. NEW ANGLE TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-302. LEAK CHECK GOOD IAW B-727 MM 27-81-00. 2L73 4F A3WE 20040204001582004020400158NM 2004 2 4 EIA2003132 120031020A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 VERTICAL STAB TO FUSELAGE. AREA LT SIDE BELOW RUDDER BETWEEN STA. 2521 AND 2598 HAS A GOUGE IN FUS. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2. 2L74 4F A20WE 20031112000472003111200047CE 2003 11 12 DXTA200300142 120031019A793299124641 TRANSMITTER CESSNA560 560XL 2076702CE PWA 545 PW545A NE NR 2 ENGINE MALFUNCTIONED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07612QS592 5605312 PCEDB0570 AS TAKE OFF POWER WAS APPLIED, THE RIGHT ENGINE OIL PRESSURE DROPPED TO ZERO THEN BEGAN TO JUMP BETWEEN NORMAL LEVELS AND ZERO. NO OTHER LOW OIL PRESSURE INDICATIONS WERE NOTED. TAKE OFF ABORTED. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER WITH NEW TRANSMITTER IAW CESSNA-560XL MM CHAPTER 79-31-01. OPS CHECK AND LEAK CHECK GOOD. 2L72 4F4 FRTA22CE E00059EN 20031117000562003111700056EA 2003 11 17 COMA0360444 120031004A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA FLAPS ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01446CA 7546 FLIGHT 5160 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20031103000422003110300042NM 2003 11 3 DL738030900 120031004A2930202190101 TRANSMITTER BOEING737 737832 13844CFNM HYD SYSTEM MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27376DA 29624 ON T/O A/C CONTROLS FELT VERY HEAVY EVEN WHEN PROPERLY TRIMMED NOT BINDING. OBSERVED HYD SYS A QTY DROP TO 73 PERCENT. NO CHANGE IN CONTROLS STILL HEAVY ON APPROACH AND LANDING IN CVG. GEAR DOWN QTY A RECOVERED. INSPD FLT CONTROLS. NO ACTUATORS BYPASSING. CKD A-SYS RESERVOIR CKS OK. FLUID FULL. REPLACED A-SYS HYD QTY XMITTER PER M/M 29-33-12 401, LEAK CKS OPS, CHECKS OK. 2L72 4F RTA16WE 20030917001352003091700135NM 2003 9 17 DL757030698 120030726A2530 COFFEEMAKER BOEING757 757232 1384965NM GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27621DL 22911 LIGHT ELECTRICAL ODOR AT 2L DOOR AND GALLEY AREA F/A'S PULLED COFFEE AND OVEN C/B'S AND ODOR DISSIPATED//INSPECTED GALLEY AND SURROUNDING AREA FOR SOURCE RESET C/B'S RAN GALLEY EQUIPMENT NO DESCREPANCIES FOUND 2L72 4F RTA2NM 20031124001112003112400111WP 2003 11 24 DHL2003805546 120030731A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING OTBD L/E FORMER 0.500 CRACKED, STA XFS 747.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. FOR REMOVAL AND REINSTALLATION OF OTBD L/E SEE N/R 0345. 2L74 4F RT4A25 20031125000452003112500045WP 2003 11 25 DHL2003805524 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 484.000 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20040114002192004011400219NM 2004 1 14 MWEA030483 120031215A52305910141105 STRUCTURE DOUG MD88 MD88 3023688NM CARGO DOOR DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 MID CARGO DOOR HAS A DENT BETWEEN BEAMS 4 AND 5 (FROM BOTTOM OF DOOR) 11 INCHES FRONT EDGE OF DOOR. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20040115000562004011500056NM 2004 1 15 DLM88031082 120031213A3350RPS1B POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27916DL 49591 ON L/O CHECK FOUND AFT SERIES OF EMERGENCY LIGHTS INOP. REPLACED BATTERY POWER SUPPLY. 2L72 4F RTA6WE 20031216000092003121600009NM 2003 12 16 QXEA200301447 120031106A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- NR 9 SEAT TRACK REQUIRES REPLACEMENT DUE TO DAMAGE THAT IS OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD'S 8-53-784 AND 8-53-4472. 2H72 4T RTA13NM 20031217000042003121700004EA 2003 12 17 MASA200300408 120031014A3350 BATTERY CNDAIRCL600 CL6002C10 1390015EA E/E BAY DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07512MJ 10109 DEN EMERGENCY EXIT LIGHTS INOPERATIVE DURING TEST. BATTERIES WERE CHARGED WITH A/C POWER. OP CHECKS GOOD. 2L72 4F RTA21EA 20031217001932003121700193EU 2003 12 17 MALA030507 120031120A7930 CHIP DETECTOR SAAB SF340 340B 7860101EU LT ENGINE CONTAMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15408XJ 340B408 DURING FLT, CREW REPORTED INFLIGHT LT CHIP DECTECTOR LIGHT ON STEADY. AIR RETURN TO MSP. MAINTENANCE INSPECTED, COMPLETED TASK CARDS 7910-303 AND 791107, MATERIAL FOUND ON CHIP DETECTOR WAS OF THE ALLOWABLE CATEGORY. CLEANED AND REINSTALLED CHIP DET, OPS AND LEAK CHECK GOOD. 2L72 4T RTA52EU 20031217001552003121700155CE 2003 12 17 DXTA200300199 120031215A3246 TIRE CESSNA750 750 2076810CE MLG FAILED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07982QS 7500182 ON LANDING AT TXKF BOTH MAIN TIRES BLEW DAMAGING HARDWARE ON STRUT, GEAR DOOR AND FLAP TRACK FAIRINGS. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20031222000492003122200049EA 2003 12 22 03336643 120031202A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27643BR 7363 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031222000922003122200092NM 2003 12 22 USAASB03199 120031108A3397 WIRE BOEING737 737401 1384701NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US 23992 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEATS 10ABC AND 11ABC INOPERATIVE. MAINTENANCE REPAIRED WIRE AT LIGHT ON SEAT 11ABC. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20031224000392003122400039 2003 12 24 ASAA0380604 420031007A25653961896501 LANYARD DOUG MD80 MD83 3023681NM ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01979AS 53471 PREFLIGHT CHECK, FORWARD PASSENGER L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RT 20031229000462003122900046NM 2003 12 29 AALA20031420 120031213A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21787AL 30010 LT EMERGENCY LIGHT ON CLOSET JAMB TORN OUT AT DOOR 1L. REPLACED EMERGENCY LIGHT ASSEMBLY ON CLOSET JAMB AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031231001092003123100109NM 2003 12 31 TSAA0351030 120030115A53206554893 WEB BOEING737 7372T4 1384492NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 TRIMMED RIGHT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO RBL 70. FABRICATED NEW PRESSURE WEB SECTION, STIFFENERS AND FILLERS. SHOT PEENED, ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS. INSTALLED REPAIR PARTS PER FIGURE 3. REPAIR COMPLETED IAW ECO 3328, PART II AND V. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040106001452004010600145EA 2004 1 6 COMA0370057 120031213A33102LA00691307 LIGHT CNDAIRCL600 CL6002C10 1390015EA COCKPIT DEFECTIVE A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01625CA 10113 FLIGHT 5523 SMOKE IN COCKPIT COPILOTS SIDE. REPLACED THE COPILOT FLOOD LIGHT ASSY. 2L72 4F RTA21EA 20040105001472004010500147WP 2004 1 5 ABXA030477 120031216A335060030451 POWER SUPPLY DOUG DC9 DC941 302207NWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23955AX1698 47619 FOUND COCKPIT EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK POWER SUPPLY IAW DC9 MM 33-53-02-4-0001. OPS CHECK GOOD. 2L72 4F A6WE 20040106001322004010600132NM 2004 1 6 DHL2003754022 120031217A324226011825 BRAKE BOEING727 727223 1384074NM NR 3 & 4 FAILED A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01754DH 22008 RIGHT SIDE BRAKES SHATTERING AND GRABBING. TAXIED AIRCRAFT FOR TROUBLESHOOTING, FOUND RIGHT-HAND SIDE NOISE SOUNDING LIKE METAL GRINDING. REMOVED AND REPLACED NR 3 & 4 BRAKE ASSEMBLIES AS PER 32-41-32. NO DEFECTS NOTED. OPS CHECKED GOOD. 2L73 4F A3WE 20040106001952004010600195WP 2004 1 6 GTIA030994 120031031A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FTW - FOUND NOSE GEAR RIGHT SIDE AFT DOOR JAMB HAS DENTED/DAMAGED STATION 110. REMOVED DAMAGED FRAME. INSTALLED FRAME. (M) 2L72 4F A6WE 20031021000292003102100029EU 2003 10 21 USAASA03096 120030819A2810 FUEL SYS AIRBUS320 A320214 3930316EU LEFT MALFUNCTIONED A USAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 EA19112US 1134 NAS - FLT 978 - EN ROUTE AUA-CLT, WHILE AT FL350, CREW RECEIVED ECAM MESSAGE 'AUTO FEED FAULT'. THE QRH PROCEDUES WERE APPLIED, BUT FUEL CONTINUED TO RAPIDLY MIGRATE FROM THE LEFT INNER FUEL TANK TO THE CENTER FUEL TANK, CAUSING A LATERAL IMBALANCE OF APPROXIMATELY 2,700 LBS. CREW COULD NOT GET FUEL IN CENTER TANK TO FEED FOR USE. FLIGHT DIVERTED TO NAS AND LANDED WITHOUT FURTHER INCIDENT. (M) 2L72 4F RTA28NM 20040109000332004010900033NM 2004 1 9 MEX2003469 120031006A3411 PITOT LINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE PITOT STATIC SYSOBSTRUCTED W ASMFC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SW23946AS 49658 AIRCRAFT SUSPENDED TAKEOFF AT 120 KTS, BECAUSE OF 40 KT DIFFERENCE BETWEEN IAS/MACH SPEED INDICATORS. LT INDICATED 80 KTS AND RT INDICATED 120 KTS. CADCS WERE TESTED FOUND ALL CORRECT. DURING PITOT TUBES REVISION WAS DETECTED A BEE IN THE CAPTAIN PITOT TUBE. LINES WERE BLOWING WITH AIR AND OPERATIONAL TEST WERE PERFORMED IAW MM34-11-00. ADDITIONALLY, HIGH ENERGY STOP CONDITIONS INSPECTION WAS PERFORMED IAW MM 05-57-00, ALL CORRECT.(K) 2L72 4F4 FRT E2EA 20031203000972003120300097EA 2003 12 3 SIMA200325101 120030906A29109752661 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA AFT EQUIP BAY CRACKED A SIMAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW21507AE 10059 CREW REPORTED HYDRAULIC SYSTEM NR 2 ZERO PERCENT QUANTITY AND ZERO PRESSURE. RAMP REPORTED A LARGE QUANTITY OF FLUID UNDER AFT FUSELAGE. MAINTENANCE FOUND THE NR 2 HYDRAULIC SHUTOFF VALVE LEAKING DUE TO THE VALVE BODY SPLIT. MAINTENANCE REMOVED AND REPLACED THE SHUTOFF VALVE IAW CRJ MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20031203001622003120300162WP 2003 12 3 AALA20031019 120030917A3350 LIGHT DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21513AA 49890 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE FORWARD LAVATORY EXIT LOCATION. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204001862003120400186EU 2003 12 4 MALA030469 120030929A5753 PIN BAC 146 AVRO146RJ85A1500097EU FLAP TRACK CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, FOUND LEFT FLAP POSITION TRACK NR 2 AFT LINK FORWARD AND AFT PINS CORRODED. MAINTENANCE REPLACED PINS IAW EO AD020307. REFER 189957 FOR ADDITIONAL INFORMATION. 2H74 4F RTA49EU 20040126000022004012600002EU 2004 1 26 BAQA091747 120031212A6320L633M2001106 MOUNT UROCOPEC135 EC135P1 8680990EU MAIN ROTOR G/B COLLAPSED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03577LF539 0140 ARIS MOUNT COLLAPSED. PART REPLACED WITH SERVICABLE UNIT. 01/06/2004 1G72 3U O H88EU 20031208001572003120800157WP 2003 12 8 IXXA0300066O 120031026A7797CFM5621C WIRE HARNESS DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C1 13802NE NR 3 ENGINE FAULTY A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11822BX87364356 45813 693308 CREW DID AIR RETURN TO RJTY FOR AN ERRATIC EGT ON NR 3. EGT FLUCUATES BETWEEN +/- 30 DEGREES. CREW SHUTDOWN ENGINE AND OIL PRESSURE WAS ZERO PSI. CREW THEN RETURNED THE AIRCRAFT TO RJTY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT NR 3 ENGINE EGT SYSTEM AND FOUND BAD CFM 56-2C1 EGT HARNESS. MAINTENANCE THEN REMOVED AND REPLACED HARNESS PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20030919001242003091900124EU 2003 9 19 3602062403 120030624A6730SC5083 SERVO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE MAIN ROTOR LEAKING E S4WAK NONE O OTHER ININSP/MAINT 1 WP07820NA694 3602 22342 LT LATERAL SERVO LEAKING BEYOND LIMITS. 1G71 3U3 U H9EU E00054EN 20030919001332003091900133 2003 9 19 3602011703 420030117A2310CDM1550 RADIO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP07350R 968 9075 9667 AUX FM INOPERATIVE. 1G71 3U3 U H9EU E00054EN 20030924001322003092400132 2003 9 24 AALA20030752 420030703A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21690AN 29590 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001372003092400137NM 2003 9 24 AALA20030487 120030419A7830 WARNING LIGHT BOEING757 757223 1384957NM THRUST REVERSER ILLUMINATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21690AA 25696 LEFT THRUST REVERSER AMBER LIGHT CAME ON DURING CLIMB-OUT AT FL170. (M) 2L72 4F RTA2NM 20040129001032004012900103NM 2004 1 29 DHL2003742539 120031124A5744 MOUNT BRACKET BOEING727 727225 1384077NM LE FLAP ACTUATORCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 6 KRUEGER FLAP INBD ACT MOUNT CRACKED 2 EA PLACES. REMOVED SUPPORT BRACKETS IAW B727 SRM 51-30-02, FABRICATED AT 2 EA SUPPORT BRACKETS, 7075-T6 .063 PO 900226 PER SAMPLE DIM 3.5 X 7 INCHES IAW B727 SRM 57-20-02. ALODINED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED SUPPORTS IAW B727 SRM 51-30-02, OPS CHECK GOOD IAW B727 MM 27-81-00. 2L73 4F A3WE 20040204001702004020400170NM 2004 2 4 MWEA030436 120031028A2760V3601 THROTTLE SWITCH DOUG MD88 MD88 3023688NM SPOILER INOPERATIVE A MWEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL31601ME 49762 SPOILER ANNUNCIATION ILLUMINATED WHEN CROSSWIND, CORRECTION WAS APPLIED WITH ALIERON. REMOVED AND REPLACED THROTTLE POSITION SWITCH. 2L72 4F RTA6WE 20040217000392004021700039EU 2004 2 17 2004F00065 120030926A5340D5347026920000 FITTING AIRBUS320 A320233 3930329EU FLOOR SUPPORT CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56 BL 0 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT FITTING AT FRAME 56, BL 0 IN AFT CARGO PIT. (M) 2L72 4F RTA28NM 20031211001372003121100137EU 2003 12 11 AALA20031342 120031128A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW213075A 606 MIA EMERGENCY EXIT LIGHTS AT DOOR 3L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT DOOR 3L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20030923001632003092300163WP 2003 9 23 AALA20030791 120030724A3350 WIRE HARNESS DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21443AA 49469 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT SEAT 11D INOPERATIVE. FOUND BREAK IN WIRE HARNESS ON SEAT. REMOVED AND REPLACED HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030926000492003092600049NE 2003 9 26 00107 220030827A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05888TW 292 249SC104A PILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL400 TO FL410 NORMAL RESTART PERFORMED AND RETURN TO FL410 FOR REMAINDER OF FLIGHT WITH NO FURTHER PROBLEM, ENGINE INSPECTED IAW MM AT YIP BASE REPLACED T2 LINE AND OPS CHECKED GOOD. 2L72 4J4 J A10CE 1E16 20040128001722004012800172EU 2004 1 28 AWXA200400007 120031222A5414D54530052200 SKIN AIRBUS320 A320231 3930325EU NR 2 ENG PYLON ERODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 MCN - MINOR REPAIR - DURING C-02 CHECK THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN WAS FOUND ERODED. MAINTENANCE REMOVED ERODED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-12, & 22. 2L72 4F RTA28NM 20040205001412004020500141EA 2004 2 5 WVE2003F00020 120031116A5754 PANEL CNDAIRCL600 CL6002C10 1390015EA LE SLAT MISRIGGED B WVERO OTHER W INADEQUATE Q C NRNOT REPORTED 1 EA09613QX 10045 LT WING LEADING EDGE PANEL 531AL AFT OUTBOARD SIDE IS CHAFED .3750 INCH LONG, .3750 INCH WIDE, .003 INCH DEEP. MISRIG OF LEADING EDGE SLAT CAUSING CONTACT ON UNDERLYING PANEL. RECOMMENDATION: BLEND CHAFED AREA TO SMOOTH THE SURFACE, PERFORM EDDY CURRENT TO ENSURE THAT NO CRACKS EXIST, ALODINE, PRIME, PAINT TO MATCH SURROUNDING STRUCTURE AND ENSURE THE SLAT IS PROPERLY RIGGED TO PREVENT FURTHER DAMAGE IAW EA R-57-51 AND EO 601R-57-4361 DATED 11/04/03. 2L72 4F RTA21EA 20040205001442004020500144EU 2004 2 5 U30A200300038 120031130A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT DISCHARGED A U30AK NONE L NO TEST TXTAXI/GRND HDL 1 EA17261AV 1615 AFTER LANDING ON FLT 206 PIT-CUN IN CUN, THE EMERGENCY EXIT SIGN OVERWING LT SIDE OF CABIN WAS INOPERATIVE. MAINTENANCE RESET AND TESTED THE EMERGENCY LIGHTS IAW AMM 33-73-06-740-005 AND LIGHTS TESTED OK. AIRCRAFT RETURNED TO SERVICE. UPON RETURN TO EWR AFTER, FURTHER TROUBLESHOOTING INDICATED A FAULT ON THE LT OVERWING EMERGENCY EXIT SIGN. REPLACED THE EPSU (EMERGENCY POWER SUPPLY UNIT) AND CHECKED NORMAL I/A/W AMM 33-51-00-710-001. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040210000282004021000028WP 2004 2 10 UPS03841604 120031016A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, AIR CONDITIONING ACCY COMPARTMENT AT STA 46 RBL 44. FLOORBEAM MISSING TWO FASTENERS. UPON INSP OF MISSING FAST FOUND FLOORBEAM TO BE CORRODED, REMOVED CORRODED IAW DC8 SRM 51-1-8 OUT OF LIMITS IAW DC8 SRM 53-2-0, REMOVED FLOORBOARD AN D 2 EA FLOOR SUPPORT ANGLES. FABBED TEE CAP REPAIR ANGLE IAW TR 53-152 AND FLR SUPPORT ANGLE IAW DAC DWG 4774654. ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20D, 51-3-0, AND TR 53-152 FIG 1H. 2L74 4F RT4A25 20040212000092004021200009WP 2004 2 12 UPS03841626 120031121A534037558452N FITTING DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C1, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 1200 LONG.36 TO 35R. REMOVED AND REPLACED FITTING IAW DWG. 3755845 AND SRM. 53-2-0 FIG. 2D. 2L74 4F RT4A25 20040213000322004021300032NM 2004 2 13 CALA0300725 120031231A3350D71702030 CHARGER BOEING737 737724 13844BYNM EMERGENCY LIGHTSINOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2716713 28784 EMERGENCY AISLE LIGHTS WERE FOUND INOPERATIVE AT STA 790. MAINTENANCE FOUND BATTERY CHARGER M1673 AT FAULT. THE BATTERY CHARGER WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20040212000852004021200085NE 2004 2 12 CNMA200300008 220031210A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE NR 1 OVERTEMP A CNMAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW0759083 47926 ON INITIAL CLIMBOUT NR 1 ENGINE OIL TEMP CLIMBED TO AND EXCEEDED LIMITS. (PEGGED OUT) SHUT DOWN ENGINE. 2L73 4F4 F A22WE E23EA 20031215000152003121500015NM 2003 12 15 QXEA200301429 120031116A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8401 1390041NM ENGINE MALFUNCTIONED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09400QX 4030 SEA- ON FLIGHT 2336 AIRCRAFT FAILED INITIAL AUTO FEATHER TEST. COMPLIED WITH TEST OF AUTO FEATHER AND UPTRIM SYSTEMS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040324000142004032400014NM 2004 3 24 ASAA0340341 120031114A533065C323657 SKIN BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01755AS 25096 GYR - DURING SI CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 793. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040407000712004040700071NM 2004 4 7 TSAA0353218 120031102A57306545407 SKIN BOEING737 737282 13844ATNM RT WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13824AL 23045 FOUND RIGHT UPPER WING SURFACE CORROSION BETWEEN THE FRONT AND REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 5 AS NR 1 TO NR 15 AT THE FOLLOWING LOCATIONS, NR 1 AT WBL 92.5, NR 2, 3, 4, 5 AND 6 BETWEEN WBL 198.6 AND WBL 227.0, NR 7 AND 8 AT WBL 157, NR 9 AND 10 BETWEEN WS 442 AND WS 453, NR 11, 12 AND 13 AT WS 505, NR 14 AT WS 472, NR 15 AT WBL 227. REMOVED CORROSION, FLAT PEEN, ALODINED AND SEALED. REMOVED AND REPLACED FASTENERS WITHIN BLEND OUT AREA PER SRM 57-30-1. REPAIR COMPLETED IAW ECO 3399. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040520002692004052000269EU 2004 5 20 2004F00120 120030917A5315 FLOORBEAM AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION AT R2 DOOR FLOORBEAM 8 INCHES INBOARD OF DOOR CUT OUT FROM FRAMES 66 TO 68 RBL 50. REPAIRED CORRODED AREA AT R2 DOOR FLOORBEAM, 8 INCHES INBOARD OF DOOR CUTOUT FROM FRAMES 66 TO 68, RBL 50. (M) 2L72 4F RTA28NM 20030819001372003081900137NM 2003 8 19 CALA0300359 120030627A5512 SKIN BOEING737 737524 1384721NM HORIZONTAL STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714660 28921 MAINTENANCE REMOVED AN INTERIM REPAIR ON THE RT HORIZONTAL STABILIZER AT THE LEADING EDGE. THE DENT WAS NEAR A RIB AT LEADING EDGE STATION 184.66. THE FINAL TRIM OUT WAS 3.5 INCHES BY 4.5 INCHES. A PERMANENT REPAIR WAS PERFORMED BY INSTALLING A FLUSH REPAIR AT THE RIB. 2L72 4F RTA16WE 20030819001452003081900145EA 2003 8 19 SWIA200312151 120030625A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 280 RBL 12 VERTICAL ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ REO 601R-53-11-034 REV A. 2L72 4F4 FRTA21EA E15NE 20030819000582003081900058CE 2003 8 19 DXTA200300036 120030524A2613 FIRE LOOP CESSNA560 560XL 2076702CE PWA 545 PW545A NE LT ENGINE MISROUTED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07690QS 5605090 PCEDB0185 DURING FLIGHT 120124-1 FROM MIA TO CHS DIVERTED TO MCO DUE TO LT ENGINE FIRE LIGHT CAME ON AT FL240. REDUCED POWER TO HALF THROTTLE AND LIGHT EXTINGUISHED, NO EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED LT ENG COWLS AND RAN FOR LEAK CHECK. NO LEAKS NOTED. FOUND FIRE DETECT LOOP ROUTED UNDER EXHAUST VENT HOLE, REROUTED FIRE LOOP. PERFORMED LOOP CONTINUITY RESISTANCE CHECK IAW CE-560XL M/M CHAP 26-11-00 CHECKS GOOD. GROUND RAN LT ENG, NO LEAKS NOTED AT 100 PERCENT. 2L72 4F4 FRTA22CE E00059EN 20030819002222003081900222CE 2003 8 19 DXTA200300054 120030627A32226794070AND6794 STRUT CESSNA750 750 2076810CE NLG CONTAMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07912QS4145 7500012 GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH RECYCLED ONCE AND IT STILL DID NOT GO OUT. FOUND PARTICLES IN NLG STRUT FLUID. REMOVED AND REPLACED UPPER & LOWER NLG BARREL ASSY. LANDING GEAR FUNCTIONAL TEST NORMAL, WORK IAW CE-750 MM CHAPTER 32-20-02. 2L72 4J RTT00007WI 20030820001242003082000124NM 2003 8 20 QXEA200300933 120030730A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09411QX 4055 ON FLIGHT 2267 AFT PASSENGER STAIRS WILL NOT DEPLOY. EXTENDED AND RETRACTED AFT PASSENGER STAIRS SEVERAL TIMES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030820001902003082000190EA 2003 8 20 COMA0360348 120030806A3260 TARGET CNDAIRCL600 CL6002B19 1900309EA MLG LOOSE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01912CA23918 7011 DURING FLIGHT 5620A, GEAR DISAGREE WARNING MESSAGE APPEARED IN FLIGHT. AIRCRAFT PERFORMED UNSCHEDULED LANDING AT CKB AND LEFT MLG UPLOCK SENSOR TARGET CLEARANCE WAS ADJUSTED IAW CRJ 200 AMM 32-32-00-820-002. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20030328000982003032800098EU 2003 3 28 CX7A194J30 120030203A26131734362450 SENSOR SAAB SF340 340B 7860101EU RT TAILPIPE CONTAMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03300CE 340B184 RT TAILPIPE HOT OCCURRED ON TAKEOFF AT APPROX 150 FEET AGL. DID AIR RETURN. 2L72 4T RTA52EU 20030331000352003033100035WP 2003 3 31 AALA20030045 120030112A212160529042 FAN DOUG DC9 DC982 3022082WP ACM BAY FAILED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21454AA 49559 EN ROUTE DEN-DFW, ON TAKEOFF ROLL, HEAR A FAN TYPE NOISE SIMILAR TO INSTRUMENT COOLING FAN CYCLING ON/OFF SEVERAL TIMES. PAST V1 HAD BLAST OF AIR AND SAW SMOKE (GRAY) IN COCKPIT WITH PACK FLOW OFF. TURNED LEFT PACK OFF, SMOKE STOPPED IMMEDIATELY. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. INSPECTED COCKPIT, CABIN AND TAIL SECTION OF AIRCRAFT. NO SMOKE OR ODOR DETECTED. REPLACED LT PACK HEAT EXCHANGER COOLING FAN. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030402000592003040200059NM 2003 4 2 2003UALA00336 120030307A5754114W41113 SKIN BOEING777 777222 1385219NM NR 1 SLAT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29785UA 26954 NR 1 SLAT, OTBD LOWER L/E SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACK REPAIRED W/EXTERNAL DOUBLER. 2L72 4F RTT0001SE 20030820001602003082000160NM 2003 8 20 2003UALA00572 120030717A7722 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE ILLUMINATED A UALAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP29347UA 24251 AIRCRAFT ABORTED TAKEOFF AT 90 KNOTS DUE TO NR 2 ENGINE RED EGT LIGHT ON. EGT EXCEEDANCE CHECK PERFORMED, POWER MANAGMENT CONTROL (PMC) SYSTEM CHECKED . ALL RESISTANCE CHECKS OK, EXCEPT FOR T12 TEMP SENSOR. T12 SENSOR WAS REPLACED. PLA VOLTAGE ON PMC WITHIN LIMITS. CONFIRMED NO EGT EXCEEDANCE AND NO EGT INDICATION FAULTS WERE FOUND. 2L72 4F4 FRTA16WE E2GL 20030821001122003082100112NM 2003 8 21 03FDEA00881 120030616A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 CORROSION (C53-113-01) STA 660, LBL 4 - RBL 4 ON FRAME SHEAR TIE. 2L73 4F RTA3WE 20030403000902003040300090EA 2003 4 3 COMA0360171 120030330A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01984CA14949 7171 FLIGHT 5132 EMERGENCY FLOOR PATH LIGHTING ROWS 1 THRU 5 IS INOP. REPLACED THE NR 1 EMERGENCY BATTERY. 2L72 4F RTA21EA 20030331000402003033100040WP 2003 3 31 AALA20030089 120030121A28223980001 PUMP DOUG DC9 DC982 3022082WP FUEL BOOST FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21467AA 49597 EN ROUTE AUS-ORD DURING CRUISE, WAS UNABLE TO BURN FUEL OUT OF CENTER TANK. RAN APPROPRIATE CHECKLIST TO NO AVAIL. AIR INTERRUPTED AND LANDED DFW WITHOUT INCIDENT. REPLACED CENTER AFT FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000352003040100035SO 2003 4 1 ASOA03055 120030212A531012022788017011 WINDOW POST EMB 120 EMB120RT 3260202SO FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11280AS 120231 DURING A HANGAR CHECK IN TXK, THE LT DIRECT VISUAL WINDOW POST SKIN AT THE LOWER TRAILING EDGE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-53-0119A. (M) 2L72 4T RTA31SO 20030404000692003040400069NM 2003 4 4 DL757030288 120030324A5330146N34002 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27612DL 22819 THE FUSELAGE SKIN WAS FOUND WITH CORROSION AT FS 1610 BETWEEN STRINGERS 28L & 29R. THE UNDERLYING STRINGERS ALSO HAD AREAS OF CORROSION. THE STRINGERS WERE REPAIRED WITH CHANNEL SECTIONS PER THE SRM. THE SKIN DAMAGE WAS REMOVED WITH A 10 X 4 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384582-14, REV A. 2L72 4F RTA2NM 20030414000222003041400022 2003 4 14 SWAA030725 420030330A2565D31354 SLIDE BOEING737 7373G7 1384595NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030416001762003041600176NM 2003 4 16 AALA20030231 120030223A3350233T32101033 CONTROL PANEL BOEING767 767223 1385123NM COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21329AA 22329 LAX - DURING OVERNIGHT MAINTENANCE, COCKPIT OVERHEAD EMERGENCY UNARMED LIGHT INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHT PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416003432003041600343 2003 4 16 SWIA200311693 420030103A34206226190204 INDICATOR EMB 120 EMB120ER 3260203SO ATTITUDE MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07188SW5806 2638 120039 CAPTAIN'S ATTITUDE INDICATOR INDICATED APPROX 15 DEGREES BANK TO THE LT WITH WINGS LEVEL. ATTITUDE RESET HAD NO EFFECT. ATTITUDE DISPLAY WAS ILLUMINATED ON THE MAP. RETURNED OT SLC. REMOVED AND REPLACED NR 1 AH85 IAW 34-25-00. COMPLIED WITH OPS CHECK AS REQUIRED. OPS CHECK GOOD. 2L72 4T RTA31SO 20030424000912003042400091NM 2003 4 24 F3LA200300109 120030228A5320 ANGLE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED INTERCOSTAL UPPER ANGLE IN FWD CARGO COMPARTMENT CRACKED FROM STA. 380 TO STA. 400, BL O, WL 208. FABRICATED AND REPLACED ANGLE PER SRM 51-10-2 AND 51-40-2. 2L72 4F RTA16WE 20030428000172003042800017CE 2003 4 28 IBUA121E 120030319A2916511700712 RESERVOIR CESSNA421 421C 2076016CE CONT O520 GTSIO520* 17032SO HYD SYSTEM LEAKING E IBUAK NONE K FLUID LOSS ININSP/MAINT 1 WP0784GE 421C1401 DURING INSPECTION OF AIRCRAFT, FOUND SIGHT TUBE ON HYDRAULIC RESERVOIR TO BE LEAKING, REPLACED WITH NEW. AFTER A FEW DAYS THE AIRCRAFT WAS STILL IN INSPECTION AND SAW THAT IT WAS CRACKED AGAIN SO WE INSTALLED AND OTHER SIGHT TUBE. ON THE LAST DAY OF INSPECTION SAW IT WAS CRACKED AGAIN SO INSTALLED ANOTHER NEW SIGHT TUBE ABOUT 4 DAYS LATER AFTER THE AIRCRAFT WAS IN SERVICE. FOUND THAT THE SIGHT TUBE WAS LEAKING AGAIN, REPLACED WITH NEW AGAIN. 1L72 3O3 O A7CE E7CE 20030428001172003042800117SO 2003 4 28 C2XA03CL086 120030404A335066367 LIGHT EMB 145 EMB145ER 3260211SO ALLSN AE3007AE3007C GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714945 145049 DURING ROUTINE MAINTAINENCE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE AT ROW/SEATS 6. MAINTENANCE INSPECTED AND REPLACED EMERGENCY LIGHT FLOOR STRIP. OPERATIONAL CHECKS GOOD 2L72 4F4 FRTT00011ATTE6CH 20030505002382003050500238NM 2003 5 5 AWXA200300388 120030413A2560P2070001214 FLASHLIGHT BOEING737 73733A 1384673NM ZONE 900 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - EMERGENCY EQUIPMENT - DURING C-17 CHECK THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030507000232003050700023WP 2003 5 7 CA030408003 120030404A6410369D21640501 BLADE HUGHES369 369D 4470706WP TAIL ROTOR DEBONDED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE DOING A DAILY INSPECTION ON THE TAIL ROTOR BLADES IT WAS NOTICED THAT THE LEADING EDGE WAS DEBONDING ON THE TRAILING EDGE OF THE LEADING EDGE ABRASION STRIP. THE LOCATION IS ABOUT 8 INCHES FROM THE TIP OF THE BLADE AND THE TOTAL LENGTH OF THE DELAM IS 4.5 INCHES. THE BLADE WAS REPLACED IMMEDIATELY WITH A SERVICEABLE BLADE. THIS IS THE NEW STYLE TAIL ROTOR BLADE WITH THE FULL LENGTH ABRASION STRIP. THE OTHER BLADE WAS INSPECTED AND NO DEFECTS WERE FOUND. 1G71 3U H3WE 20030513000902003051300090NM 2003 5 13 UPS03240672 120030424A5310 SUPPORT BOEING727 72722C 138400FNM RAM AIR DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, RT RAM AIR INTAKE DOOR SUPPORT BRACKET FOUND CRACKED AT BS 600 S25R. DOOR SUPPORT BRACKET FABRICATED IAW SRM 51-20-1 FIG 7, NEW BRACKET RE-PROTECTED IAW SRM 51-10-02 NEW DOOR SUPPORT AND FASTENERS RE-INSTALLED IAW SRM 51-30-02 2L73 4F A3WE 20030514001722003051400172NM 2003 5 14 P5CA0300871 120030425A30402314M1161 BLADE BOEING747 7472U3B 1384846NM WINDSHIELD WIPERBROKEN A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23923FT 22769 CAPT'S WIPER BLADE BROKE OFF DURING TAXI. INSP ARM AND DEFERRED ITEM PER DDPG - WAS LATER REPLACED IN PIK. BLADE SHEARED OFF ARM. 2L74 4F RTA20WE 20030604000782003060400078NM 2003 6 4 UPS03440492 120030413A5320 STRUCTURE BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 M/D - HAT SECTION FWD FLANGE CORROSION. CORRODED HAT SECTION REPLACED AS PER SRM 51-10-01 PAGE 8. CORROSION BLEND OUT 0.030 X 1 X 1 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030515001712003051500171EU 2003 5 15 AWXA200300489 120030425A5210 INDICATOR AIRBUS320 A320231 3930325EU DOOR BOTTLE FALSE INDICATIONA AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW43092 054 MCN - EES - DURING C-03 CHECK THE L-2 DOOR ASSIST CYLINDER GAUGE READ 400 PSI WITH ZERO PRESSURE IN CYLINDER. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW AMM TASK 52-13-14-000-001, AND TASK 52-13-14-400-001. 2L72 4F RTA28NM 20030520000592003052000059NM 2003 5 20 AMTA200300508 120030415A2612 FIRE LOOP BOEING757 75733N 1384931NM RT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11556TZ 32590 EICAS STATUS MSG RT ENGINE FIRE LP 2 DISPLAYED. OPS CHECKED FIRE LOOP SYSTEM PER MM 26-11-00-5. OPS CHECK NORMAL. NO EICAS MESSAGE PRESENT. OK FOR CONT SERVICE. (M) 2L72 4F RTA2NM 20030515000222003051500022EA 2003 5 15 SWIA200311943 120030331A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 VERTICAL ANGLE AT FS 280 AT LBL 12.0 BETWEEN WL 79.5 AND 69.1 IS CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-11-034 REV A. 2L72 4F RTA21EA 20030605001282003060500128NM 2003 6 5 MEX2003116 120030404A7711LG80E1 COMPUTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE NR 2 EPR FAILED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL23158PL37749 49761 AIRCRAFT RETURNED TO PLATFORM DUE TO FAIL OF RIGHT ENGINE DIGITAL EPR INDICATING SYSTEM. AT PLATFORM, EPR TRANSMITTERS WERE INTERCHANGED BUT FAILURE CONTINUED. THEY WERE RETURNED TO THEIR ORIGINAL POSITION AND RIGHT TRANSMITTER WAS REPLACED IAW MM, RUNNING ENGINES TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E2EA 20030610000352003061000035EA 2003 6 10 03144692 120030524A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27692BR 7759 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030613000842003061300084 2003 6 13 MALA030298 420030608A3442 DISPLAY BAC 146 AVRO146RJ85A1500097EU WEATHER RADAR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15518XJ E2337 DURING FLIGHT 3409 EN ROUTE DTW-CHS, THE WEATHER RADAR FAILED R/T MESSAGE SHOWN ON SCREEN. AC DIVERTED TO CVG. MAINTENANCE REPLACED WEATHER RADAR RT/XT BOX WITH SERVICEABLE UNIT PN/OFF 2041217-0414, SN/OFF 7585, PN/ON 2041217-0414 SN/ON 7238 IAW AMM. 2H74 4F RTA49EU 20030522001212003052200121 2003 5 22 SWAA031123 420030520A2565D31354 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED AFT CABIN DOOR SLIDES PER MM. 2L72 4F A16WE 20030522000962003052200096NM 2003 5 22 SWAA031068 120030512A53116546546 FRAME BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727C, WL 148 RBL 5 TO LBL 5. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030523001232003052300123NM 2003 5 23 2003UALA00431 120030421A575465C26603191 WEDGE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 3 SLAT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 HAIL DAMAGE OCCURRED TO T/E WEDGE, NR 3 SLAT. REPAIRED T/E WEDGE, SLAT NR 3. 2L72 4F4 FRTA16WE E2GL 20030527000092003052700009WP 2003 5 27 DHL2003801058 120030407A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 441.561. STOP DRILLED CRACK AT STA XFS 441.561 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030617003052003061700305NM 2003 6 17 SWAA031261 120030606A57526546455 TAB BOEING737 7372T4 1384492NM AILERON DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND RT AILERON TAB DELAMINATED ON INBD T/E. REMOVED AND REPLACED RT AILERON TAB PER MM. 2L72 4F A16WE 20030528000752003052800075WP 2003 5 28 AALA20030451 120030411A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217512A 49806 DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS THROUGH FRONT OF COACH SECTION INOPERATIVE. SECURED OVERHEAD EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030527001082003052700108EA 2003 5 27 2003F00318 120030403A3222 PACKING CNDAIRCL600 CL6002B19 1900309EA NLG STRUT FAILED A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0747239 7239 RETURN TO FIELD WITH GEAR DISAGREE, NOSE GEAR DOOR OPEN, NOSE WHEEL STEERING INOPERATIVE MESSAGE. MAINTENANCE REPACKED NOSE STRUT. OP CHECKS GOOD. (M) 2L72 4F RTA21EA 20030619000492003061900049SW 2003 6 19 HEEA087199 120030609A771465023031 INDICATOR BELL 206 206B3 1181506SW DUAL TACH SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032275Y 3626 DUAL TACH INDICATOR NEEDLES SPLIT ON START UP. 1G71 3U H2SW 20030625000272003062500027WP 2003 6 25 MWEA030236 120030528A5230995766437 FRAME DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 MID CARGO DOOR LOWER FORWARD STOP FITTING ANGLE IS CRACKED. -- FABRICATED AND INSTALLED NEW FORMER. 2L72 4F A6WE 20030707000672003070700067NM 2003 7 7 2003UALA00494 120030613A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29198UA 28716 2 EA. DENTS TOP FLOORBEAM FORWARD PIT BS 720 RBL 12. MAJOR REPAIR ACCOMPLISHED. REPLACED TOP "T"CORD. 2L74 4F4 FRTA20WE E24NE 20030630000272003063000027 2003 6 30 03FDEA00824 420030529A34164045053914 ADC AIRBUS310 A310 EU NR 1 INOPERATIVE A FDEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO25413FE6527 6527 397 AFTER T/O F/O PFD AIRSPEED WAS SLOW TO RESPOND 80 ON CAPT SIDE 50 ON F/O'S SWITCHED TO ADC NR 1 ON F/O SIDE, AT 1000AGL GOT FLAP HIGH SPEED WARNING OVER- SPEED WARNING, SPEED OF A/C WAS 160 KTS IND. FACT 28MAY03 22:03 MEM R REMOVED AND REPLACED NR 2 ADC PER A310 MM 34-11-34 SYSTEM OPS CHECKS GOOD. 34-10/6446 PURGED SYS AND PUMP DOWN ACCOMPLISHED PREMATURE REMOVAL/INSTALLATION. 2L72 4F RTA35EU 20030711000972003071100097EA 2003 7 11 COMA0360295 120030625A3240158863 SOLENOID VALVE CNDAIRCL600 CL6002B19 1900309EA BRAKE SYSTEM MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01819CA188 7415 FLIGHT 5316 PARKING BRAKE CAUTION MESSAGE IN FLIGHT. REPLACED THE PARKING BRAKE SOLENOID VALVE 2L72 4F RTA21EA 20030714001442003071400144EU 2003 7 14 XG3R087905 120030601A6730350A33318000 TORSION BAR UROCOPEC120 EC120B 8680987EU TMECA ARRIELARRIEL2B NE FENESTRON CORRODED B XG3RO OTHER O OTHER NRNOT REPORTED 1 WP0526LB 485 M114 3514 23017 PREMATURE WEAR OF LAMINATED TORSION BARS. REPLACED LAMINATED TORSION BARS DUE TO WEAR LIMITS. 1G72 3U3 UNCR0001RD E00054EN 20030124000832003012400083NM 2003 1 24 UPS03240050 120030108A2730NA BRACKET BOEING727 72721C 138400MNM L/H ELEV. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE:C ON REMOVAL OF L/H ELEVATOR PCU BRACKET ON FRONT SPAR OF ELEVATOR FOU ND TO BE CRACKED POSITION SENSOR BRACKET ON L/H ELEV. FRONT SPAR REPLACED IAW MM 27-3 0-01 PG 410 STEP 4J 2L73 4F A3WE 20030128001202003012800120SW 2003 1 28 HEEA083860 120030116A6310406040316101 SPLINE ADAPTER BELL 407 407 1182206SW ENGINE TO GB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 ENGINE TO GEARBOX SPLINE ADAPTER HAS WORN SPLINES. 1G71 3U O H2SW 20030204000262003020400026NM 2003 2 4 SWAA030183 120030123A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030314000282003031400028NM 2003 3 14 03FDEA00089 120030130A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION ON FLOORBEAM UPPER FLANGE BS 720D LBL 25-45, WL 208. REMOVED CORROSION FROM FLOORBEAM UPPER FLANGE BS 720D LBL 25-45 WL 208. AREA REMOVED .4 INCH X 1 INCH .045 INCH, ORIGINAL THICKNESS .125 INCH FOUND OUT OF LIMITS PER SRM 53-10-1. CUT OUT, OUT OF LIMITS DAMAGED AREA, 1.5 INCH X 2.0 INCH AT LBL 35. FABRICATED REPAIR PARTS AND INSTALLED WORK DONE IAW SRM 53-10-8. 2L73 4F RTA3WE 20030214000182003021400018NM 2003 2 14 2003FA0000144 120030115A2730401606223 HOUSING BOEING737 737* NM FEEL COMPUTER CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 1448D CRACKED ON SYSTEM (B) SIDE OF HOUSING MOUNTING SURFACE FOR BELLOWS. 2L72 4F RTA16WE 20030225000152003022500015SW 2003 2 25 HEEA084234 120030120A5320407070620156 HEADLINER BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 HEADLINER CRACKED. 1G71 3U O H2SW 20030116001692003011600169SO 2003 1 16 C2XA02SH163 120030103A711014576631622 STRUCTURE EMB 145 EMB145LR 3260212SO NR 2 COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV- DURING C-CHECK NUMBER TWO LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFFED. MAINTENANCE REMOVED AND PLACED AFFECTED EDGE MEMBER IAW EMB SRM 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030304000122003030400012SW 2003 3 4 AC2A084868 120030224A6400222312718001 BEARING BELL 430 430 1182150SW TAIL ROTOR ROUGH H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CT 49089 TAIL ROTOR BEARING IS ROUGH. REPALCED BEARING. 1G72 3U RTH9SW 20030305000612003030500061 2003 3 5 HEEA084643 420030214A3454066107800 RECEIVER BELL 412 412 1182202SW VOR SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 VOR STAYS INVALID. REPAIRED BROKEN FOIL ON NAV RECEIVER BOARD. BENCH CHECK GOOD. 1G72 4U H4SW 20030228001272003022800127NM 2003 2 28 AWXA200300212 120030216A53226545834 INTERCOSTAL BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW0 0 24060 YVR - MAJOR REPAIR - DURING C-11 CHECK A 1/2" CRACK WAS FOUND ON LOWER WEB FLANGE (INTERCOSTAL) AT BS 360, BL 0. MAINTENANCE CUTOUT CRACKED AREA OF INTERCOSTAL AT BS 360, BL 0; FABRICATED A TAPERED SHIM AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG. 1, SHEETS 1-5. 2L72 4F RTA16WE 20030303000662003030300066NE 2003 3 3 HEEA084513 220030214A732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 FREE TURBINE GOVERNOR PRODUCING N1, ITT, N2 OSCILLATION AT FLAT PITCH AND FLIGHT. REPAIRED. 1G72 4U4 U H4SW E22EA 20030306000382003030600038SW 2003 3 6 HEEA084751 120030217A5260 BEARING BELL 412 412 1182202SW STEP ACTUATOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 STEP ACTUATOR HAS A BEARING WORN. REPAIRED. 1G72 4U H4SW 20030307000332003030700033 2003 3 7 SWAA030481 420030303A2565D31354 SLIDE BOEING737 7373A4 1384585NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE ASSY LOOSE. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030307001782003030700178NM 2003 3 7 AALA20030067 120030117A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21934AN 29531 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 10D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030311000242003031100024WP 2003 3 11 DHL2003807004 120030311A3260 SWITCH DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER J WARNING INDICATION CLCLIMB 1 SO01807DH 45990 1) AFTER GEAR RETRACTION WITH GEAR HANDLE UP, DOOR UNLATCHED LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY 20 SECONDS, THEN EXTINGUISHED. UPLATCH CHECK ACCOMPLISHED SATISFACTORY. RAN DOOR NOT LATCHED LIGHT ABNORMAL PROCEDURES, DOOR UNLATCHED LIGHT FUNCTIONED NORMALLY UPON RECYCLING GEAR.2) REMOVED AND REPLACED LEFT GEAR DOOR SWITCH PER 32-60-0. 2L74 4F RT4A25 20030314001022003031400102NM 2003 3 14 SWAA030510 120030306A3211654611324 PIN BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED C4 CHECK, FOUND RT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNION PIN PER MM. 2L72 4F RTA16WE 20030327000032003032700003EU 2003 3 27 AWXA200300265 120030313A3397ABS0374A24 TERMINAL AIRBUS320 A320231 3930325EU SEAT ROW 26 BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28644AW 317 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS INOPERATIVE. MAINTENANCE REPAIRED WALL PLUG CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030327001382003032700138SO 2003 3 27 C2XA03IA003 120030104A27503631001005 CONTROL UNIT EMB 145 EMB145LR 3260212SO TE FLAPS INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2716976 145171 IAH- DURING CRUISE THE CREW NOTED THAT THE FLAP FAIL MESSAGE APPEARED IN FLIGHT. THE CREW DID AN AIR RETURN AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030318000672003031800067NM 2003 3 18 AMTA200300142 120030126A33508100022608 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11526AT 30735 EGRESS TRACK LIGHTING BETWEEN SEATS 6 DEF- 9DEF INOPERATIVE. REMOVED AND REPLACED 5 LIGHT ASSEMBLIES AND 2 TRACK COVERS PER AMM TASK 33-51-11-403-049. LIGHTS OPERATIONALLY CHECKS NORMAL. (M) 2L72 4F RTA2NM 20030320001292003032000129NM 2003 3 20 2003UALA00120 120030131A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 STATION 188 RT FRAME CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030730000272003073000027NM 2003 7 30 P5CA0300900 120030716A32501U11715 ACTUATOR BOEING747 7472D3B 1384805NM NLG STEERING FAILED A P5CAR AUTOROTATION K FLUID LOSS TXTAXI/GRND HDL 1 WP23505MC 21251 RT INBND BODY GEAR STEERING ACTUATOR FAILED, CAUSING LOSS OF NR 1 HYDRO SYS. REMOVED AND REPLACED RT INBND BODY GEAR STEERING ACTUATOR. LEAK CK AND GROUND OPS NORMAL IAW MM 32-51-05, SERVIVED NR 1 HYD SYS IAW 72-00. 2L74 4F RTA20WE 20030418001402003041800140WP 2003 4 18 ZW0A0302702 120030222A2150 A/C PACK DOUG DC9 DC982 3022082WP AIR CONDITIONINGCONTAMINATED A ZW0AO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE13907TW 49165 AT GATE VISIBLE SMOKE AND SMOKE SMELL IN AFT OF AC AFTER TURNING ON PACKS DUE TO POSSIBLE DE-ICER FLUID CONTAMINATION. TURNED OFF PACKS AND REPLACED LT AND RT WATER SEPARATOR PER MM 21-20-02 MD9-49-16 AND MD9-49-04. CHECK-C STL 1-30-03. 2L72 4F A6WE 20030422000022003042200002CE 2003 4 22 2003F00226 120030227A2131 CONTROLLER LEAR 60 60LEAR 5170707CE CABIN PRESSURE MALFUNCTIONED A UG8AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23699DA 237 THE AIRCRAFT BEGAN ITS TAKEOFF ROLL, AT TAKEOFF POWER THE WHEELS BROKE GROUND AND THE PRESSURIZATION BEGAN TO DRIVE THE CABIN TO SEA LEVEL. THE CABIN BEGAN TO PRESSURIZE AT A RAPID RATE WITH BLEED AIR FORM THE ENGINES ON POWER UP. NO POSITIVE REASON WAS IDENTIFIED. THE AIRCRAFT RETURNED TO THE DEPARURE RAMP AND THE MX DEPARTMENT PERFORMED A CABIN PRESSURIZATION OPERATIONAL CHECK IAW THE LEAR 60 MX MANUAL, 21-30-00, PAGE 215. NO DEFECTS WERE NOTED, AND THE DISCREPANCY COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2L72 4F RTA10CE 20040329000272004032900027EU 2004 3 29 USAASA03140 120031222A2530112251 COFFEEMAKER AIRBUSA319 A319112 3930323EU GALLEY ODOR A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19727UW9173 1147 PHL - FLT 1068 - EN ROUTE IAH-PHL - A SLIGHT BURNING ODOR WAS NOTED IN THE AFT GALLEY NEAR THE CHILLERS. ALL ASSOCIATED CIRCUIT BREAKERS WERE PULLED, HOWEVER, THE ODOR REMAINED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AFT GALLEY RIGHT SIDE COFFEE MAKER DUE TO A BURNING ELECTRICAL ODOR. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030730001132003073000113WP 2003 7 30 AMTA200300903 120030621A5744 ATTACH FITTING LKHEED1011 10113853 5265020WP RT WING CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 RIGHT WING AFT SPAR OUTBOARD AILERON ATTACH FITTING CRACKED AT SECOND HINGE FROM OUTBOARD. REPLACED FITTING IAW SRM 51-10-01 AND ER/A L10-57R-5202. (M) 2L73 4F A23WE 20030422001582003042200158NM 2003 4 22 PCAA0303052 120030311A5610NP15790110 WINDSHIELD DHAV DHC8 DHC8102 2809003NM RIGHT FAILED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA13807EX23603 292 SYR-FLIGHT 3889 APPROXIMATELY 4 MINUTES PRIOR TO LANDING IN SYR, SMOKE STARTED TO APPEAR IN COCKPIT. SMOKE ORIGINATED FROM THE HEATING ELEMENT OF THE RIGHT WINDSHIELD. WHILE TAXIING IN THE WINDSHIELD CRACKED. CREW REPORTED TO MAINTENANCE THAT THE RIGHT WINDSHIELD HEATING ELEMENT OVERHEATED CAUSING FUMES IN THE COCKPIT & RIGHT WINDSHIELD WAS CRACKED. MAINTENANCE REPLACED THE WINDSHIELD, WINDSHIELD HEAT CONTROLLER, RELAY 3041-K10, AND TERMINAL END L2. AIRCRAFT GROUND RAN, AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030723001242003072300124EU 2003 7 23 AWXA200300621 120030529A2560P4010021 BATTERY AIRBUS320 A320232 3930326EU LAV FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28648AW 770 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE FORWARD GALLEY WAS NOT BLINKING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030825000912003082500091WP 2003 8 25 03FDEA01242 120030810A5753ARC2179 RIB DOUG DC10 DC1030 3023501WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 WINGS- RT OUTBD FLAP- INBD CLOSURE RIB DAMAGED HOLE REPAIR 2C P 2FN ARCV 2179 ENT BY 3A 39014C RPT BY 3A 39014C0D. FACT 08AUG03 04 3A34 BFM COMPLIED WITH EA 8-5750-72242 WINGS- RT 2FB FLAP-INBD CLOSURE RIB DAMAGED HOLE REPAIR 2C P 2FN AARC 2179 40 MAE ENT BY3 A 39014C RPT BY 3A 39014C. 2L73 4F A22WE 20030828000822003082800082NM 2003 8 28 DL757030675 120030719A5310143N831215 DOOR FRAME BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27655DL 24395 L2 DOOR AFT OPENING FRAME AT STA 729 WAS BLENDED BELOW SRM LIMITS TO REMOVE CORROSION. REPAIR IAW ER/A 385354-14 2L72 4F RTA2NM 20030828001532003082800153NM 2003 8 28 USAASB03128 120030804A21317638104 CONTROLLER BOEING737 7373B7 1384580NM CABIN PRESSURE MALFUNCTIONED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19375US 22954 CMH - FLT 1295 - EN ROUTE FROM PIT TO DFW, AT FL350, THE CABIN PRESSURIZATION BEGAN TO CLIMB. CREW FOLLOWED QUICK REF HANDBOOK PROCEDURES AND NOTED THAT THE CABIN PRESSURIZATION COULD ONLY BE MAINTAINED IN MANUAL PRESSURIZATION MODE, AS AUTO AND STANDBY MODES FAILED. DECISSION WAS MADE TO DIVERT TO CMH. AN EMERGENCY WAS DECLARED AND THE CABIN WAS PREPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CMH. OXYGEN MASKS WERE NOT DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE SELECTOR PANEL (P/N 71002-5) AND THE CABIN PRESSURE CONTROLLER. OPS CHECK GOOD PER MM 21-31-00. (M) 2L72 4F RTA16WE 20030829000522003082900052WP 2003 8 29 DHL2003873542 120030630A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZ STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 INTERIM REPAIR ON RT HORIZONTAL STABILIZER OTBD L/E XFS.210.000 - XFS.222.500. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4, PG 17. CLEANED, TREATED AND PRIMED DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED DOUBLER ON RT HORIZONTAL STABILIZER OTBD L/E, XFS.210.000 - XFS.222.500 IAW SRM 55-2-1 FIG 4, PG 17, SRM 51-1-15 PG 1, SRM 51-1-21 PG 1. FOR REMOVAL AND REINSTALLATION SEE JC BX3455072. 2L74 4F RT4A25 20030902001852003090200185NM 2003 9 2 03FDEA00973 120030620A5512ALC8100 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 SNRM N0897 - LT HOR STAB UPPER FWD PLANK NR 8L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS. CORRECTIVE ACTION: SNRM N0897 - LT HOR STAB UPPER FWD PLANK NR 8L BORE REPAIR CARRIED OUT IAW EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20031212000472003121200047NM 2003 12 12 DHL2003740006 120031107A2120 ODOR BOEING727 7272Q9 138448MNM CABIN DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01740DH 21930 HOT SMELL COMING FROM AIR CONDITIONING PACK TEMPERATURE AND DUCT TEMPERATURE NORMAL. RAN ENGINES AND PACKS IAW JRH & M/M 21-20-01. NO DEFECTS NOTED. CAN NOT DUPLICATE, OK TO CONTINUE. 2L73 4F RTA3WE 20031211000812003121100081NM 2003 12 11 AWXA200301416 120031027A5320654659221 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR CHANNEL AT BS 860, LBL 13.80. MAINTENANCE REMOVED DAMAGE SECTION OF FLOOR CHANNEL AT BS 860, LBL 13.80; FABRICATED A NEW REPLACEMENT SECTION OF CHANNEL AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG 201. 2L72 4F RTA16WE 20040309001632004030900163WP 2004 3 9 GTIA031063 120031120A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND DENT AT FS 208 BETWEEN LONGERONS 17L AND 18L, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. REMOVED DAMAGED SKIN. SKIN CUTOUT (13 INCHES BY 40 INCHES). FABRICATED NEW SECTION OF SKIN, DOUBLER AND FINGER DOUBLER. FABRICATED 7 STRAP AND 23 DOUBLER. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20040316000172004031600017NM 2004 3 16 ASAA0370016 120031022A5347146A75012 CARGO TRACK BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01617AS 30542 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR TIE DOWN TRACK. SPLICE IN NEW SECTION PER SRM. (M) 2L72 4F RTA16WE 20040412001782004041200178WP 2004 4 12 ASAA0380726 120031111A532199365451 INSERT DOUG DC9 DC983 3022083WP FLOORBOARD CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415001112004041500111WP 2004 4 15 ASAA0380748 120031114A53115913595501 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND AFT ACCESSORY TAIL FRAME CHAFFED AT STATION 1418, STRINGER 20R CHAFFED. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20031216000912003121600091EA 2003 12 16 03333683 120031130A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27683BR 7692 DURING FINAL ON FLIGHT INTO YUL CREW REPORTED A LAVATORY SMOKE MESSAGE. FLIGHT LANDED UNEVENTFULLY. THE LAVATORY SMOKE DETECTION SYSTEM WAS FUNCTIONALLY CHECKED AND NO FAULTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030926001252003092600125NE 2003 9 26 A1U2003F00002 220030621A7261B4443A CHIP DETECTOR BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101750B1 41560NE NR 2 ENGINE CONTAMINATED E A1UAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03880SL 7130 45007 WHILE IN CRUISE FLIGHT, ENGINE NR 2 CHIP LIGHT ILLUMINATED, CHIP PLUSE SYSTEM WAS ACTIVATED THREE TIMES, EACH TIME THE LIGHT REILLUMINATED. INFORMED COMPANY DISPATCH OF SITUATION, THEY INFORMED MAINTENANCE. INITIATED PRECAUTIONARY LANDING PROCEDURES, CONTACTED PARKS DOWNTOWN TOWER (CPS) AND REQUESTED LANDING CLEARANCE. PREFORMED NORMAL APPROACH AND LANDING TO A TAXIWAY, SHUTDOWN AIRCRAFT, AND WAITED FOR MAINT TO ARRIVE. MECH INSPECT CHIP PLUGS, FOUND ONE HAIR LIKE PIECE OF METAL ON SCAVENGE PLUG, DRAINED OIL AND FILTERS INSPECTED FOR METAL, NONE FOUND. PERFORMED 20 MINUTE PENALTY RUN, REINSPECTED PLUGS, OIL AND FILTERS NO METAL FOUND. REINSTALLED PLUGS AND FILTERS, SERVICED OIL RETURNED AC TO SERVICE. 1G72 3U3 UNCH13EU E5NE10 20060313001932006031300193SO 2006 3 13 LR7A03096 120031121A5315LS5112 FLOORBEAM LKHEED382 382G 526414USO FS 737E-817E SCHEDULED MAINT A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND LT CENTER FUSELAGE FS 737E-817E CHINE ANGLE WITH NUMEROUS REPAIRS, LBL 61, WL 142. REPLACED CHINE ANGLE FS 737E-817E IAW SRM SMP 583 51-60 & 51-70. 2H74 4T A1SO 20030813001802003081300180NM 2003 8 13 SWAA031690 120030729A53306546529 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030819000212003081900021NM 2003 8 19 USAA030109 120030621A5210 SKIN BOEING737 737301 1384611NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 PIT - FOUND DOOR SKIN CRACKED .5 INCH LONG, MED INTERIOR EDGE OF INNER SKIN, 4TH STOP PAD SCREW HOLE. DOUBLER INSTALLED PER EA 76491. (M) 2L72 4F RTA16WE 20030819001582003081900158NM 2003 8 19 2003UALA00594 120030728A2751 WARNING LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE TE FLAPS ILLUMINATED A UALAO OTHER J WARNING INDICATION APAPPROACH 1 WP29948UA 26691 FLIGHT CREW HAD ASYMMETRICAL FLAP INDICATION ON APPROACH. MADE NORMAL LANDING. CHECK OF THE FLAP INDICATION SYSTEM ON THE GROUND WAS ACCOMPLISHED AND NO DEFECTS WERE NOTED. THE FLAP POSITION INDICATOR (N54) WAS REPLACED AS A PRECAUTION. SYSTEM HAS FUNCTIONED PROPERLY SINCE INDICATOR REPLACEMENT. UPON INTERNAL INSPECTION OF THE INDICATOR, IT WAS FOUND THAT AN INTERNAL NUT, SPACER AND WASHER CAME LOOSE AND CAUSED A DISTORTION IN THE MAIN SHAFT RUNNING THE LENGTH OF THE INDICATOR. 2L72 4F4 FRTA16WE E2GL 20030820001072003082000107NM 2003 8 20 UPS03240970 120030708A29101111588311 CHECK VALVE BOEING727 72722C 138400FNM HYD SYSTEM CONTAMINATED A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01941UP 19196 INSPECTION TYPE:N/A AT APPROX 3000 FT CREW NOTICED SMOKE IN COCKPIT DID AN AIR TURNBACK TO DEC. REMOVED AND REPLACED THE A-SYSTEM AIR PRESUURE REGULATOR IAW M/M 2912. FOUND EVIDENCE OF HYDRAULIC FLUID IN RES AIR PRESSURE CHECK VALVE ASSY RNR ALL 3 CHECK VALVES PERFORMED LEAK CK RAN ALL ENGINES WITH 2 PACKS, NO FAULTS NOTED RNR WATER SEPARATOR BAGS PRECAUTIONARY. 2L73 4F A3WE 20030819001972003081900197SO 2003 8 19 SWIA200312208 120030723A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07301YV 120301 FLOOR LEVEL EMERGENCY LIGHT BURNED OUT. INSTALLED BULB. OPS CHECK GOOD. 2L72 4T RTA31SO 20030402000422003040200042NM 2003 4 2 2003UALA00319 120030325A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 CABIN BODY FRAME STRINGER CLIP IS CRACKED AT BS 639, STR 4RT. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20030724001052003072400105NM 2003 7 24 DL738030565 120030621A3350D71702030 POWER SUPPLY BOEING737 737832 13844CFNM ROW 17 INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO273768 29630 ROWS 16, 17 AND 18 EMERGENCY LIGHTS INOP. FOUND PWR SUPPLY M1695 INOP. REPLACED PWR SUPPLY. EMERGENCY LIGHTS CHECK GOOD. 2L72 4F RTA16WE 20030807000922003080700092NE 2003 8 7 HNAA0300036 220030729A7321324485318 FUEL CONTROL DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE ZONE 400 MALFUNCTIONED A HNAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 EA07337EN225113183 284 123218 ON CLIMBOUT, NR 1 ENGINE TORQUE DROPPED TO 45 PERCENT. REPLACED MFC. 2H72 4T4 TRTA13NM E20NE 20030903000772003090300077 2003 9 3 MALA030342 420030712A3410 CONNECTOR BAC 146 AVRO146RJ85A1500097EU INSTRUMENT PANELDISCONNECTED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15533XJ E2367 AFTER TAKEOFF, PRESSURIZATION ON MWS. ADC-1 ON PRESS PANEL, FTC LIGHT, FLEX TRIM LT AND YO LIGHT WINDSHEAR MAP LIGHT. AIR RETURN TO MEM. FOUND CONNECTIONS AG AND CH OF INTRUMENT PANEL DISCONNECT 211-20-00 TO BE LOOSE WITH ASSOCIATED DAMAGE TO LOCKING DEVICES. RESECURED AND PERFORMED TEMP REPAIR. INITIATED PWI FOR PERMANENT REPAIR WITH 150 FLIGHT HOURS. MAINTENANCE REPAIRED AND REPLACED JACKSCREWS ON CONNECTORS 211-20-00 PAG, PBH, PCH,PDH IAW AVRO MM CHAP 20. OPS CHECKS OF ASSOCIATED SYSTEMS GOOD. 2H74 4F RTA49EU 20030903001442003090300144WP 2003 9 3 GTIA030615 120030728A3397 WIRE DOUG DC9 DC982 3022082WP CABIN SHORTED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND OVERWING EMERGENCY EXIT SIGNS ARE INOPERATIVE. TROUBLESHOOT OVERWING EMERGENCY EXIT SIGNS AND FOUND SHORTED WIRES TO THE EXIT LIGHTS. REPAIRED SHORTED WIRING. (M) 2L72 4F A6WE 20030904000742003090400074NM 2003 9 4 QXEA200301048 120030901A26113023143 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09360PH2036910351 515 SEA- ON FLIGHT 2176 RETURNED TO FIELD DUE TO, AFTER DEPARTURE RECIEVED AN INTERMITTENT SMOKE WARNING INDICATION. REMOVED AND REPLACED AFT BAGGAGE COMPARTMENT SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903001692003090300169WP 2003 9 3 AALA20030698 120030627A2612 CONNECTOR DOUG DC9 DC982 3022082WP FIRE LOOPS LOOSE A AALAO OTHER N FALSE WARNING DEDESCENT 1 SW2173444 49470 MEX - FLT 1111 - EN ROUTE DFW-MEX, DURING DESCENT FIRE DETECTOR LOOP LIGHT ON ANNUNCIATOR PANEL FLASHED ON AND OFF, ALSO MASTER CAUTION LIGHT FLASHING. LOOP LIGHTS ON OVERHEAD PANEL DID NOT ILLUMINATED. LANDED MEX WITHOUT INCIDENT. TIGHTENED CONNECTIONS AT LOOP DETECTORS ON BOTH ENGINES. RE-RACKED MASTER WARNING AND CAUTION CONTROLLER, RAN UP ENGINES AT DIFFERENT POWER SETTINGS UNABLE TO DUPLICATE, PERFORMED FIRE AND LOOP FUNCTIONAL TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030903001962003090300196EU 2003 9 3 AALA20030800 120030725A21331037223 OUTFLOW VALVE FOKKERF28 F28MK0100 4990807EU CABIN PRESSURE FAULTY A AALAK NONE O OTHER CLCLIMB 1 SW211435D 11425 FLT 1599 - DURING CLIMB, AIRCRAFT UNABLE TO PRESSURIZE. AIRCRAFT DIVERTED AND LANDED IAD WITHOUT INCIDENT. REMOVED AND REPLACED BOTH OUTFLOW VALVES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030825000722003082500072NM 2003 8 25 0301466305 120030803A3397 WIRE BOEING747 747451 1384940NM CABIN DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01665US 23820 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AFT OF DOOR 1R. REPAIRED WIRE. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030826001622003082600162WP 2003 8 26 MEX2003295 120030718A274295901 ACTUATOR DOUG DC9 DC983 3022083WP HORIZ STAB FAILED A ASMFA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW23838AM 49397 FLT 113 - TIJ-GDL - AIRTURN BACK DUE TO RIGHT CONTROL STABILIZER DID NOT OPERATE AND LEFT CONTROL STABILIZER WORKED INTERMITTENTLY. DURING REVSION THE SW S10-19 WAS DETECTED WITH OCCASIONAL FAIL. THE S10-19 AND BRAKE OVERRIDE SW S10-20 WERE REPLACED IAW MM 27-40-02/07. THE STABILIZER AND ELEVATORS WERE CHECKED FOR CONDITION, ALL CORRECT. THE PRIMARY AND ALT LONGITUDINAL TRIM ACTUATOR AND LONGITUDINAL TRIM GEARBOX WERE REPLACED IAW MM 27-40-01, ALL TEST CORRECT. (M) 2L72 4F RTA6WE 20030826001732003082600173SO 2003 8 26 SWIA200312133 120030620A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07583SW 120351 EMERGENCY EXIT OVERHEAD LIGHT INOP. REPLACED BULB FOR RIGHT EMERGENCY LIGHT EXIT OVERHEAD. OPS CHECK GOOD. 2L72 4T RTA31SO 20030911000132003091100013EU 2003 9 11 DXTA200300090 120030815A3297 WIRE BRAERO1000 BAE1251000 1500287EU MLG BROKEN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07514QS NA1005 AFTER TAKE-OFF COULD NOT RETRACT LANDING GEAR, ACCOMPLISHED AIR TURN BACK TO TPA AND LANDED OVERWEIGHT. - REPAIRED BROKEN WIRE AT KAPIS BY INSTALLING SPLICE P/N D436-36, OPS CHECKED GOOD I/A/W HAWKER 1000 MM CHAPTER 32-30-00. C/W PRESSURIZE CHECK ON GROUND OPS CHECKED, LEAK CHECKED GOOD IAW HAWKER 1000 MM CHAPTER 21-30-00. 2L72 4F RTA3EU 20030910002142003091000214EU 2003 9 10 MALA030360 120030704A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING C-CHECK INSPECTION IN CVG, NR 4 SEAT RAIL FROM FRAME 18 TO FRAME 20A IS CORRODED. MAINTENANCE REPAIRED IAW EO NR A53026. REFER TO 409 NR 128126, TASK CARD NR 0893A FOR DETAIL. A/C RELEASE DATE 7/25/03 2H74 4F RTA49EU 20030911002072003091100207WP 2003 9 11 AALA20030328 120030310A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21567AM 53293 TUL - FOUND HOLE IN CUSP AT STATION 1060 LEFT. CUT OUT DAMAGED SECTION, INSTALL DOUBLER PER AARD 53-00-00-02. (M) 2L72 4F RTA6WE 20030929001422003092900142EU 2003 9 29 XNOA01153 120030906A2700 CONTROL CABLE AIRBUS300 A300B4203 3930306EU FLT CONTROLS LACK OF LUBE A XN0AC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 GL23473AS 203 FLIGHT CONTROLS LOCKED TO LEFT ON TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KTS. INSPECTED AIL CABLES AND TENSION REG. LUBED TENSION REG. OPS CHECK NORMAL IAW A300 MM 27-11-00. INSP. AIL HYD ACT. SYS IAW A300 MM 27-14-00. NO DEFECTS NOTED. 2L72 4F RTA35EU 20030930000842003093000084WP 2003 9 30 ABXA030347 120030814A5320991015517 STRUCTURE DOUG DC9 DC932F 3022067WP LT WHEEL WELL CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 LEFT WHEEL WELL STA 712, BUTT LINE 53 RETAINER CORRODED AND RIVETS POPPED. REPLACED RETAINER FROM FS 699 AND 756 LEFT BUTT LINE 30 TO LEFT BUTT LINE 56 IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20030328000582003032800058NM 2003 3 28 CALA0300094 120030221A5320 STRUCTURE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912313 23364 MAINTENANCE FOUND THE AFT CARGO DOOR LOWER BEAM TEE CHORD CRACKED. TWO CRACKS WERE EMANATING FROM A RIVET HOLE. THE CRACKS WERE 0.4 INCH LONG AND 0.8 INCH LONG. THE AREA WAS REPAIRED IAW ECRA 5230-01715. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS. 2L72 4F RTA16WE 20030820002202003082000220EA 2003 8 20 ASOA03342 120030725A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA DOOR SEAL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11861AS 7445 DURING A C-CHECK IN MCN, THE CARGO DOOR CUT OUT LOWER SEAL PLATE WAS FOND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT LOWER SEAL PLATE IAW SRM 51-00. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030820000372003082000037NM 2003 8 20 03FDEA01066 120030625A5730APB74411 SKIN PANEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 MAIN DECK - BETWEEN BS 1215-1235, LEFT XCW 75-115, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK. 2L73 4F RTA22WE 20030821001112003082100111NM 2003 8 21 03FDEA01017 120030627A5753ARC0503504 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE FOUND CORROSION. RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5740-71734 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030403001192003040300119NM 2003 4 3 DL733030129 120030205A5610 WIRE BOEING737 737347 1384647NM COCKPIT ARCED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27303WA 23183 CO-PILOTS FRONT WINDSHIELD POWER WIRE IN UPPER RT CORNER ARCED. C/BS PULLED TO REMOVE POWER. REPLACED TERMINAL END AND HARDWARE. REPAIRED SAME. 2L72 4F RTA16WE 20030407000062003040700006NM 2003 4 7 ASAA0310006 120030111A335086210144 BATTERY BOEING737 7372X6C 1384552NM SMOKE BARRIER DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - EMERGENCY EXIT LIGHTS AT ROW 16 AND SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AT SMOKE BARRIER AND BATTERY PACK (P/N 86-2-1004) AT ROW 16, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20030401001782003040100178WP 2003 4 1 DHL2003807003 120030311A3260 CONNECTOR DOUG DC8 DC873F 302199FWP MLG DOOR DISCONNECTED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01807DH 45990 DURING UPLATCH CHECK "DOORS NOT LATCHED" LIGHT ILLUMINATED, CYCLED GEAR 4 TIMES. LIGHT WENT OUT. ABNORMAL PROCEDURE COMPLETE. DEFERRED PER DHL MEL REF. 32-14 CONTROL 12234. PLACARD INSTALLED. CAT. "A" EXPIRES TWO FLIGHT DAYS 13 MAR 03. REF. DMI 12234: DURING UPLATCH CHECK "DOORS NOT LATCHED" LIGHT ILLUMINATED. CYCLED GEAR 4 TIMES LIGHT WENT OUT. ABNORMAL PROCEDURE COMPLETED. FOUND LT GEAR WARNING SWITCH LOOSE. RESECURED LT GEAR DOOR SWITCH CONNECTOR PLUG PER 32-60-0. DMI 12234 CLEARED. 2L74 4F RT4A25 20030401000802003040100080NM 2003 4 1 DHL2003745002 120030121A3260 SWITCH BOEING727 727224 1384076NM MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER DEPARTURE IN STL WHEN GEAR HANDLE WAS MOVED FROM UP TO OFF RT GEAR DOOR ON ANNUNCIATOR PANEL ILLUMINATED, AND DOOR LIGHT ON PILOTS PANEL ILLUMINATED. GEAR HANDLE THEN MOVED BACK TO UP AND LIGHTS EXTINGUISHED. GEAR HANDLE REPOSITIONED BACK TO OFF AND NO GEAR LIGHT ILLUMINATED. ADJUSTED RIGHT GEAR DOOR INDICATION LIGHT SWITCH. SYSTEM OPS CHECKED GOOD IAW B727 M/M 32-12-1. 2L73 4F A3WE 20030410001482003041000148NM 2003 4 10 SWAA030702 120030328A531196380 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, WL 207 AND LBL 26. REMOVED AND REPLACED LT SIDE CHORD PER SWA ACO AND SRM. 2L72 4F RTA16WE 20030416001302003041600130SO 2003 4 16 C2XA03BT048 120030403A2621M835362024M RELAY EMB 145 EMB145ER 3260211SO ALLSN AE3007AE3007C GL FIRE BOTTLE INOPERATIVE A C2XAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW2714940 145033 CO2573, CREW REPORTED THAT (E1/E2 FIRE EXTINGUISHER BOTTLE A IS INOPERATIVE). MAINTENANCE REMOVED AND REPLACED THE PRESSURE RELAY FOR ENGINE FIRE BOTTLE (A). OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030416001802003041600180NM 2003 4 16 AALA20030243 120030224A3397 WIRE BOEING767 767223 1385123NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21308AA 22314 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEATS 20B-29B, LEFT OVERWING HATCH, LOWER AFT AND FLOOR FLOOR LIGHT, AND LEFT SIDE OF MID GALLEY INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE ON SEAT 26A OUTBOARD LOWER SIDE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030416001862003041600186NM 2003 4 16 AWXA200300357 120030409A3397ABS0374A24 WIRE AIRBUSA319 A319132 3930340NM SEAT ROW 18 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28806AW 1056 DURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR BROKEN AT SEAT ROW 18 LT. MAINTENANCE REPAIRED WIRING ON THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 18 LT. 2L72 4F RTA28NM 20030417001372003041700137WP 2003 4 17 UPS03840152 120030130A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, EXTERNAL FUSELAGE SKIN IS CRACKED AND CORRODED AT FASTENER HOLE AT STA 445 LONG 31L. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030424000512003042400051NM 2003 4 24 QXEA0300326 120030227A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261CT, AFT EDGE, AT FIRST FIVE CAMLOC HOLES FROM OUTBOARD EDGE. BLENDED DAMAGED AREA. 2H72 4T RTA13NM 20030430000372003043000037EA 2003 4 30 COMA0360216 120030424A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01729CA 7265 FLIGHT 5825 AVIONICS BAY DOOR CAUTION MESSAGE. DEFERRED MAINTENANCE ON DOOR WARNING SYSTEM PER MEL. 2L72 4F RTA21EA 20031002001002003100200100SO 2003 10 2 C2XA03TY155 120030910A533014520553001 SKIN EMB 135 EMB135ER 3260203SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION 2 DENTS WHERE FOUND AFT OF THE PAX DOOR BETWEEN FRAMES 19 AND 20, ABOVE STR 12L. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A FILLER AND DOUBLER, ALIDINED, INSTALLED THE PATCH, PRIMED AND PAINTED. I/A/W-EMB-135/145-SRM-53-21-01, CMP-51-21-04, 05 AND 06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4F RTT00011AT 20031006000452003100600045NE 2003 10 6 KC82003F00003 220030820A7230CF7002D FAN AMD FALCONFALCON20 2730103EU GE CF700 CF7002D 30010NE COMPRESSOR DAMAGED E KC8AA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23192CK216101793 192 245274 SHORTLY AFTER TAKE OFF THE RT ENGINE ROLLED BACK CLIMBING THROUGH 3000 FT. FOUND RT ENGINE WITH COMPRESSOR FOD. REPLACED RT ENGINE WITH SERVICEABLE ENGINE. 2L72 4F4 FRTA7EU E7EA 20031014002052003101400205 2003 10 14 BAQA089586 420031008A221041800847000 ACTUATOR UROCOPEC135 EC135P1 8680990EU YAW FAULTY B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME3985 0009 YAW ACTUATOR SAS FAULT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20031020003052003102000305NM 2003 10 20 2003UALA00731 120031002A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29116UA 26908 AFT PIT STA 1540 RBL 47 FLOORBEAM T-CHORD DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR ANGLE. INSTALLED NESTED REPAIR USING SHIMS & FILLERS AS REQUIRED. 2L74 4F4 FRTA20WE E24NE 20030908003062003090800306 2003 9 8 SWAA031884 420030822A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030908001562003090800156EA 2003 9 8 SWIA200312231 120030806A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07441SW 7602 STAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW CRJ MM 27-42-05. STAB TRIM SYSTEM OPS CHECKS GOOD IAW 27-41-00. S/N OFF: 880 2L72 4F RTA21EA 20031028001162003102800116 2003 10 28 AALA20030676 420030621A2300503214 CONTROL PANEL BOEING757 757223 1384957NM AUDIO SELECT BURNED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21681AA 25338 IAH - FLT 315 - EN ROUTE DFW-CUN, CAPTAINS AUDIO SELECTOR PANEL HAD SMOKE COMING OUT. ISOLATED LEFT BUS SMOKE STOPPED. LANDED IAH WITHOUT FURTHER INCIDENT. REPLACED LEFT AUDION SELECT PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040115001892004011500189NM 2004 1 15 03FDEA02268 120031226A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT WING - O/B FLAP I/B HINGE ACTUATOR O/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031030000442003103000044NM 2003 10 30 UPS03441302 120030905A5712 RIB BOEING747 747121 1384871NM NR 1 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 1 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 5 ROTARY ACTUATOR MOUNTING HOLES FOUND FITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 5 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031030000712003103000071NM 2003 10 30 0301856634 120030927A2530 SWITCH BOEING747 747227B 1384888NM AFT GALLEY BURNED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01634US 22234 DURING FLIGHT, THE CIRCUIT BREAKER FOR THE NR 1 HOTPLATE IN THE AFT GALLEY POPPED AFTER SPARKS, ALONG WITH A STRONG ELECTRICAL SMOKE ODOR EMITTING FROM THE HOTPLATE. CREW PULLED ALL CIRCUIT BREAKERS FOR THE NR 1 COFFEEMAKER AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE HOTPLATE SWITCH. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20031113000182003111300018EU 2003 11 13 BAQA090554 120031030A2435 BRUSHES BOLKMS117 BK117B2 5626013EU STARTER GEN ARCED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA031174U137 715 7146 STARTER GENERATOR BRUSHES STARTED ARCING AFTER ONLY 119.6 HOURS OF USE. . REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20031105000362003110500036SO 2003 11 5 C2XA03SH413 120031025A531514521700007 FLOORBEAM EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV-DURING C-CHECK THE LT CENTER OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 22-23 AND FRAME 24-25. MAINTENANCE REMOVED DAMAGED AREAS AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040113001532004011300153NM 2004 1 13 AWXA200301606 120031207A532065C10592158 PLATE BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MINOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND UPPER SURFACE OF SUPPORT FILLER PLATE AT BS 951, RBL 47. MAINTENANCE REMOVED CORRODED FILLER PLATE AT BS 951, RBL 47; FABRICATED A NEW REPLACEMENT FILLER PLATE PER DWG 65C10592; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031124000512003112400051EU 2003 11 24 03FDEA01913 120031111A3020224W9915501 CONNECTOR AIRBUS300 A300F4605R 3930327EU ANTI ICE VALVE LOOSE A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25659FE 757 DURING CLIMB NR 1 ENG ANTI-ICE FAULT LIGHT ON / ECAM IND FAULT. DEPART ICING WX IN 30 SEC, SHUT OFF ENG A/I, FAULT LIGHT OUT. A/I VALVE DEACT'D, LOCKED OPEN FOR TROUBLESHOOTING. OPENED ENG FAN & REV COWLS FOR T/S. CW HARNESS SHAKE TEST AT CONNECTOR DV220, FOUND INTERMITTENT FAULT LIGHT WITH ECAM WARN. VALVE UNLOCKED, CTRL & WARNING C/B FOR NR 1 ENGINE A/I VALVE OPENED. REMOVED CONNECTOR DV220 FROM A/I VALVE. REMOVED BACK SHELL ON CONNECTOR, WIRE NR 6 INTO PLUG SHORTED BY SHAKING WIRE. BACKSHELL NOT SECURED TO CP DV220. CONNECTOR NOT SECURED TO A/I VALVE. REMOVED AND REPLACED NR 1 ENG CORE HARNESS. REF: A300-600 MM 71-52-01-4. CW ADJ/TEST OF NR 1 ENG A/I VALVE, OPS CK OK. 2L72 4F RTA35EU 20040113002552004011300255SO 2004 1 13 C2XA03TY219 120031226A532014529495003 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE LEFT SILL AT STR 16L AND FR 59 AND 61. MAINT REMOVED AND REPLACED THE LEFT FLOOR SILL AT THE DAMAGE AREA IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030502001802003050200180NM 2003 5 2 AWXA200300375 120030415A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW 23219 PHX - MAJOR REPAIR - DURING INSPECTION A 1.875 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 763, STR 19 RT. MAINTENANCE PERFORMED TEMPORARY REPAIR BY CUTTING OUT DAMAGED AREA OF SKIN; FABRICATING A REPAIR PLATE; INSTALLING REPAIR PART AND BLIND RIVET REPAIR IAW B737-300 SRM 53-00-01 PG 204-206 FIG 202. REPAIR TO BE REINSPECTED EVERY 2500 FLIGHT HOURS, PERMANENT REPAIR TO BE ACCOMPLISHED WITH 20,000 FLIGHT HOURS. 2L72 4F RTA16WE 20030502001902003050200190NM 2003 5 2 03FDEA00454 120030416A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION (C53-113-01-2) ON INNER SKIN SURFACE BS 950F+1 TO 8 LBL-16. BLENDED SKIN OUT OF LIMITS PER SRM 53-30-1. SKIN REPAIR TO BE ACCOMPLISHED ON NR00317 FUSELAGE 5093. 2L73 4F RTA3WE 20030502000752003050200075WP 2003 5 2 ASAA0380187 120030302A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, FRAME SEVERLY WORN AT FS 636. INSTALLED FILLER, ANGLE, AND PLATE ON FRAME PER SRM 53-03. (M) 2L72 4F A6WE 20030505002002003050500200NM 2003 5 5 UPS03M40433 120030315A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT LBL 8.5 BETWEEN STA 1268-1275 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK LBL 8.5 AT STA 1268-1275 & FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK REWORKED & HOLES PICK OUT AS PER SRM 53-70-00 VOL I REV 32, PROTCTED AS PER SRM 51-21-01 REV 32 VOL II & NEW SEAT TRACK INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 1268-1275 LBL 8.5. 2L73 4F RTA22WE 20030506001612003050600161WP 2003 5 6 ASAA0380238 120030307A5330595358328 PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT FUSELGAE AFT PANEL NR 2207 IS CRACKED AT THE FORWARD END. REPAIRED PANEL WITH BONDED FIBERGLASS OVERLAY PER SRM. (M) 2L72 4F A6WE 20030507000072003050700007EA 2003 5 7 CA030406002 120030402A5610NP1393225 WINDOW CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) CREW REPORTED THAT CAPTAINS SIDE WINDOW CRACKED AT 30,000 FT. FOLLOWING THE WINDOW REPLACEMENT, THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20030509000792003050900079EA 2003 5 9 RU32003F00003 120030430A493038826081 HOUSING CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE APU FUEL FILTER CRACKED E RU3AO OTHER O OTHER NRNOT REPORTED 1 SW1587 777 5190 APU FUEL FILTER HOUSING ATTACHMENT FLANGES CRACKED. THIS IS THE FIFTH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, THREE ON N86 AND TWO ON N87. AFTER INVESTIGATION IT WAS CONCLUDED THAT THE FUEL FILTER HOUSING FAILURES ARE THE RESULT OF FUEL CONTROL UNIT OVERPRESSURE CAUSED BY THE MALFUNCTION OF AN INTERNAL ULTIMATE RELIEF VALVE. 2L72 4F4 FRTA21EA E15NE 20030513002812003051300281EA 2003 5 13 ASOA03137 120030330A4930MS29513218 O-RING CNDAIRCL600 CL6002B19 1900309EA APU FUEL LINE LEAKING A ASOAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11842AS 7304 DURING CRUISE A STRONG FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN JAN. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNITS FUEL FEED LINE O-RINGS, ([P/N'S MS29513-218, MS29513-222, MS29513-015). OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030528000442003052800044EU 2003 5 28 BAQA085879 120030401A651010513221 BEARING BOLKMS117 BK117B1 5626012EU DRIVE LINK DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME1661 7243 EXCESS BEARING PLAY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030604001472003060400147NM 2003 6 4 UPS03440567 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 620 LT STRINGER 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.35. 2L74 4F A20WE 20030530000852003053000085NM 2003 5 30 DL76G030477 120030519A1430UNKNOWN NUT BOEING767 7673P6 1385105NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO271501P 24983 INSPECTION OF THE BARREL NUTS FOR THE VERTICAL STABILIZER TO FUSELAGE ATTACHMENT REVEALED CRACKED SEALANT AT ONE NUT LOCATION ON THE LT SIDE AT FS 1654. SINCE THIS IS INDICATIVE OF A POSSIBLE POOR TORQUE CONDITION, THE NUT AND BOLT WERE REPLACED PER ER/A 385082-14AD. 2L72 4F RTA1NM 20030520000192003052000019NM 2003 5 20 AMTA200300562 120030427A3350 LIGHT BOEING757 75723N 1384973NM ROW 32 INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11524AT 30233 ONE FLOOR PATH LIGHT (WHITE) AT SEAT ROW 32 INOPERATIVE. RESECURED WIRE, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030521001722003052100172NM 2003 5 21 SWAA031055 120030511A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030609001752003060900175CE 2003 6 9 CA030501002 120030501A555107123022 SUPPORT CESSNA185 A185E 2072818CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL HORIZONTAL STAB CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING ROUTINE SCHEDULED MAINTENANCE, IT WAS DISCOVERED THAT THE RT AFT HORIZONTAL STABILIZER SUPPORT BRACKET WAS CRACKED. NEW PART 0712302-2 WAS INSTALLED USING CESSNA SERVICE MANUAL D2000-9-13. 1H71 3O3 O 3A24 E5CE 5 CP3EA 20030612001122003061200112NM 2003 6 12 UPS03240750 120030516A5310 STOP BOEING727 727185C 138406NNM PAX DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, AFT NR 1 DOOR STOP ON FWD DOOR HAS A SUSPECT CRACK. HFEC INSP CARRIED OUT ON AFT NR 1 DOOR STOP ON FWD DOOR IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. AFT NR 1 DOOR STOP FITTING REPAIRED IAW EO B727-5230-0032-N APPX C REFERENCE NRC 674885. 2L73 4F A3WE 20030523001062003052300106NM 2003 5 23 QXEA0300614 120030517A5210 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- EIGHT DENTS ON MAIN CABIN DOOR SHELL 6.5 INCHES FROM FORWARD EDGE OF DOOR AND 7 INCHES FROM BOTTOM EDGE. REPAIRED IAW HORIZON AIR EA 6-52-293. 2H72 4T RTA13NM 20030619000622003061900062SW 2003 6 19 HEEA087403 120030611A6510407340339101 BEARING BELL 407 407 1182206SW T/R DRIVE ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 TAIL ROTOR DRIVE BEARING ROUGH. 1G71 3U O H2SW 20030624000332003062400033NM 2003 6 24 CALA0300315 120030616A3397 WIRE BOEING737 737724 13844BYNM EMERGENCY LIGHT CHAFED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713718 28937 INSPECTION FOUND THE EMERGENCY LIGHTING CHARGER C/B POPED. EMERGENCY EXIT LIGHT, OVERHEAD LIGHTS, AND SEAT PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND WIRES CHAFING AT ROW 19 AIRCRAFT LEFT, O/B OF OVERHEAD BIN SUPPORT AND SIDEWALL. REPAIRED WIRING IAW MM 20-10-00 AND 33-51-11 AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20030707000792003070700079NM 2003 7 7 DHL2003754009 120030528A326065602113 CONTROL BOX BOEING727 727223 1384074NM MLG INOPERATIVE A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01754DH 22008 AFTER LANDING GEAR LEVER SELECTED DOWN ALL THREE GREEN GEAR LIGHTS ILLUMINATED, AND ALL THREE RED GEAR LIGHTS, AND AMBER TAIL SKID LIGHTS ILLUMINATED. REPLACED LANDING ACCESS CONTROL BOX IAW M/M 32-09-111. CLEANED AND OPS CHECKED GEAR HANDLE S/W INDICATIONS OPS CHECKED NORMAL. 2L73 4F A3WE 20030718000082003071800008NM 2003 7 18 TSAA0353123 120030505A53306573742 SKIN BOEING737 73725A 1384481NM FUSELAGE DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DENT LOCATED AT BS 396 BETWEEN STRINGER 24 AND 25R. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED A NEW STRINGER REPAIR SECTION. ALODINE, PRIMED, AND INSTALLED REPAR PART IAW FASTENERS FROM TABLE 1 MAKING A FAYING SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. (M) 2L72 4F RTA16WE 20030718000452003071800045WP 2003 7 18 AMTA200300744 120030427A5753 SKIN LKHEED1011 10113853 5265020WP TE FLAPS GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11164AT 1238 FOUND 1R FLAP UPPER SKIN GOUGED AT INBOARD EDGE 27 INCHES FROM AFT EDGE. REPAIRED SKIN IAW SRM 51-50-01. (M) 2L73 4F A23WE 20030707001442003070700144WP 2003 7 7 UPS03840869 120030617A5753 SPAR DOUG DC8 DC873F 302199FWP LT FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LT IB FLAP INSIDE AT REAR SPAR ON FLAP AT XCW 64 WEB IS CRACKED IN CORNER. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATE CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001932003070700193WP 2003 7 7 UPS03840825 120030519A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, R-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM. 53-2-0 FIG. 14 STA. 418 AT LONG. 21R. REMOVED EXISTING REPAIR,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER IAW SRM. 53-2-0 FIG. 14 2L74 4F RT4A25 20030710000452003071000045WP 2003 7 10 DHL2003805010 120030528A2611 LAMP DOUG DC8 DC873F 302199FWP SMOKE DETECTOR BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01805DH 46125 NR 3 SMOKE DETECTOR WON'T TEST. REMOVED AND REPLACED NR 5 SMOKE DETECTOR TEST LAMP AS NEEDED PER SMM 26-15-00. 2L74 4F RT4A25 20030714000532003071400053NM 2003 7 14 SWAA031378 120030621A57106545445 SHEAR TIE BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED D CHECK, FOUND RT WING SHEAR TIE CRACKED AT STA 135.5 LOWER REAR SPAR. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030717000102003071700010SW 2003 7 17 HEEA087987 120030701A2810AF11C9 VALVE BELL 412 412 1182202SW SUMP LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 SUMP VALVE LEAKING. REPLACED. 1G72 4U H4SW 20030127002302003012700230SW 2003 1 27 HEEA083716 120030115A2913206076030111 PUMP BELL 407 407 1182206SW HYD SYSTEM NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 HYD PUMP MAKES NOISE ON LET DOWN. 1G71 3U O H2SW 20030128001152003012800115SW 2003 1 28 HEEA083856 120030116A6520406040072105 SPLINE ADAPTER BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 TAIL ROTOR ADAPTER HAS WORN SPLINES. 1G71 3U O H2SW 20030128001842003012800184WP 2003 1 28 ZW0A0301103 120030116A5230 DOOR FRAME DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT FORWARD CARGO DOOR FORWARD SIDE AT SECOND DOOR STOP FROM BOTTOM PIN AREA CRACKED. INSTALLED DOUBLER REPAIR PER SRM 52-05 PAGE 291. 2L72 4F A6WE 20030204001062003020400106NM 2003 2 4 SWAA030102 120030116A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR LOWER FWD FUSELAGE SKIN CUT OUT CRACKED .750 INCHES LONG. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20030206000382003020600038NM 2003 2 6 0300186718 120030128A5311 WEB BOEING747 747251F 1384898NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 During "L" check found crack in frame web at BS 360 at S23 and S24. Repaired per EA 67-165034. 2L74 4F A20WE 20030217000122003021700012NM 2003 2 17 AWXA200300145 120030206A53136948948501 CHANNEL BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON OUTBOARD EDGE OF STRINGER 28 R/H AT BS 364, BELOW FLOW CONTROL VALVE. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS ON STRINGER END CLIP, STR 28 R/H, BS 364; REMOVED DAMAGED STRINGER END CLIP; FABRICATED A NEW REPLACEMENT STRINGER END CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3-4, 26, 29, & 38, FIG. 3, 4, & 8. 2L72 4F RTA16WE 20030116001992003011600199SW 2003 1 16 HEEA083114 120030108A771420AG44 TACH GENERATOR BELL 206 206L3 1182108SW ENGINE FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 AFTER FIRST START OF DAY, TURBINE NEEDLE (N2) FLUCTUATED AND WENT TO ZERO. REPAIRED. 1G71 3U H2SW 20030117000022003011700002SW 2003 1 17 HEEA083147 120030108A6720 BEARING BELL 206 206L3 1182108SW T/R CONTROL ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 TAIL ROTOR HEAD CONTROL ROD WORN BEARING. SCRAPPED. 1G71 3U H2SW 20030117000912003011700091NM 2003 1 17 2003UALA00014 120030105A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 847 FRAME CRACKED AT RIVET HOLE S9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030224000462003022400046 2003 2 24 HEEA084167 420030212A34427021450601 INDICATOR SKRSKYS76 S76A 8143006NE WX RADAR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 WEATHER RADAR INOPERATIVE. 1G72 3U H1NE 20030226000562003022600056SW 2003 2 26 HEEA084345 120030211A6340407375005101 INDICATOR BELL 407 407 1182206SW GEARBOX OIL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 GEARBOX OIL PRESSURE DROPPED TO ZERO DURING ENGINE COOL DOWN. 1G71 3U O H2SW 20030311000722003031100072EU 2003 3 11 AWXA200300247 120030301A5320D53480020295 WEB AIRBUS320 A320231 3930325EU DOORWAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK A CRACK WAS FOUND ON HORIZONTAL WEB AFT SIDE OF L-2 DOOR AT FR 68+8, LBL49. MAINTENANCE REMOVED DAMAGED HORIZONTAL WEB AT FR 68+8, LBL49; FABRICATED A REPLACEMENT WEB PER DWG D53480020; INSTALLED REPAIR PART IAW A320 SRM 51-31-00, PG. 22, TABLE 4, AND SRM 51-21-11 PG. 5 & 7. 2L72 4F RTA28NM 20030313000892003031300089 2003 3 13 2003F00140 420030313A3418521410329 PITOT LINE CESSNA402 402C 207590RCE PITOT STATIC MELTED G O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW01635MA 402C0634 WHILE ENROUTE FROM PHX TO ABQ TE CAPTAINS AIRSPEED INDICATOR WENT TO ZERO AND THE CABIN FILLED WITH SMOKE. THE CAPTAINS AIRSPEED PITOT LINE WAS POSITIONED TOO CLOSE TO THE HEATER VENT NEAR THE RUDDER PEDALS. THE LINE WAS REMOVED, REPLACED AND REPOSITIONED, PN 5214103-29. 1L72 3O A7CE 20030317000242003031700024NM 2003 3 17 03FDEA00157 120030221A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLOORBEAM UPR FLANGE BS 1110, RBL 57 TO LBL 57, WL 208. 2L73 4F4 F A3WE E2EA 20030317000572003031700057NM 2003 3 17 SWAA030576 120030311A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 500D, STR 13R & BS 520, STR'S 12R & 12L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030122002002003012200200GL 2003 1 22 HEEA083548 220030114A7200686404602 CLIP BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 CAE847043 ENGINE OUTER CLIP RUSTED. SCRAPPED. 1G71 3U3 UO H2SW E1GL 20030123000322003012300032NM 2003 1 23 2003UALA00053 120030114A5320 FLOOR SUPPORT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 CABIN FLOOR SUPPORT ANGLE CRACK STATION 380-400 AT RBL 0. MAJOR REPAIR ACCOMPLISHED. REPLACED CRACKED ANGLE. 2L72 4F4 FRTA16WE E2GL 20030123000542003012300054WP 2003 1 23 CALA0300017 120030121A5311 FRAME DOUG DC9 DC982 3022082WP STA 1463 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0969826 49486 INSPECTION FOUND A 1" CRACK IN CANTED FRAME AT STA 1463, L3L-L3R. THE CRACKED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-00 AND 51-30-05. 2L72 4F A6WE 20030327000162003032700016EU 2003 3 27 AWXA200300283 120030301A5315D5347209001000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM FR 66 - FR 69, Y1292. MAINTENANCE REMOVED CORRODED FLOORBEAM FROM FR 64 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 5-20, & 39-41, SRM 51-44-11, PG. 11-12, TABLES 11 & 12, SRM 51-46-11, PG. 1, SRM 51-21-11, PG. 5-6. 2L72 4F RTA28NM 20030327001512003032700151SO 2003 3 27 C2XA03IA021 120030214A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713990 145277 DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY FLOOR LIGHTING FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE BATTERY PACK, PERFORMED A OPERATIONAL CHECK AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030327001792003032700179SO 2003 3 27 C2XA03TY010 120030118A531314521725001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 DURING A SCHEDULED INSPECTION A STRINGER WAS FOUND CHAFED ON THE INBOARD SIDE OF 19L. MAINTENANCE REMOVED CHAFED AREA, FABRICATED SHIMS AND DOUBLERS, REINSTALLED, RESTORED FINISH IAW-EMB-135/145-SRM-53-24-02, CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030324001212003032400121NM 2003 3 24 AWXA200300110 120030128A5523654645514 STRUCTURE BOEING737 7373G7 1384595NM ELEVATOR TAB DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW14841 24009 YVR - FLIGHT CONTROL REPAIR - DURING C-14 CHECK THE RT AILERON BALANCE TAB WAS FOUND DELAMINATED AT THE OUTBOARD TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED THE RT AILERON BALANCE TAB IAW T/C R3M27014. 2L72 4F RTA16WE 20030418000432003041800043WP 2003 4 18 MWEA030074 120030217A5320593643621 CLIP DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LONGERON 10 AND IT'S CLIP IS DAMAGED FORWARD AREA OF AFT PRESSURE BULKHEAD RIGHT SIDE. REMOVED SHOVEL CLIP AND FOUND LONGERON 10 NOT TO BE DAMAGED INSTALLED CLIP. 2L72 4F A6WE 20030327001312003032700131SO 2003 3 27 C2XA03CL068 120030313A335066366 LIGHT EMB 135 EMB135ER 3260203SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715509 145238 DURING ROUTINE MAINTENANCE THE FIRST ALL WHITE EMERGENCY AISLE PATH LIGHTING STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030423000082003042300008NM 2003 4 23 AUS20030295 120030212A5311 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME LOCATED AT BS1130 CONTAINED LEVEL 2 CORROSION ON LOWER FLANGE IN AREA BETWEEN STRINGER 28L AND 29L. FOUND DURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423001372003042300137 2003 4 23 P5CA0300774 420030309A3431 DISPLAY BOEING747 74746NF 13848BTNM VOR INOPERATIVE A P5CAO OTHER O OTHER DEDESCENT 1 WP23453PA 30811 CENTER AUTO PILOT ON THE ILS DIDN'T CAPTURE LOCALIZER / GLIDE SLOPE. FOUND CMC MESSAGE VOR - RIGHT DISPLAYED. GROUND TEST CARRIED OUT PER 34-51-00. NO FAULTS NOTED. 2L74 4F RTA20WE 20040223000742004022300074SO 2004 2 23 SWIA200312747 120031214A5411 FRAME EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07229SW 120305 RT NACELLE FRAME CRACKED AFT CENTER JUST BELOW JET PIPE. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT INSTALLED AT AFFECTED RT NACELLE AREA IAW EMB120 SRM 51-40-02. 2L72 4T RTA31SO 20040225001612004022500161NM 2004 2 25 DL73S031129 120031223A5330 SKIN BOEING737 737232 1384475NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 DAMAGED FASTENER HOLES WERE REPORTED DURING PERMANENT REPAIR ACCOMPLISHMENT TO THE R2 DOOR UPPER HINGE CUTOUT. AREA WAS REWORKED/REPAIRED PER ERA 360517-14, REV A. 2L72 4F RTA16WE 20030827001632003082700163EU 2003 8 27 MALA030354 120030727A2750 FLAP BAC 146 AVRO146RJ85A1500097EU WING MALFUNCTIONED A MALAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 GL15519XJ E2344 DURING FLIGHT NR 3565, FLAP FAULT AND INOP WARNING. FLIGHT DID A GO AROUND, THEN LANDED WITH FLAPS AT 18 DEGREES. MAINTENANCE PERFORMED FLAP FAULT RESET. ALL CHECKS GOOD. RAN FLAPS FROM 0-35 SEVERAL TIMES. NO FAULTS NOTED. 2H74 4F RTA49EU 20030829001602003082900160NM 2003 8 29 SWAA031825 120030814A335010126211 LENS BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN AT FWD F/A'S SEAT. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030723000382003072300038EU 2003 7 23 USAASA0373 120030629A3350321430 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19164UW 1425 AIRCRAFT FAILED THE EMERGENCY LIGHT SYSTEM TEST, WITH A 'EPSU AFT L' MESSAGE. MAINTENANCE REPLACED BATTERIES FOR THE AFT LEFT EMERGENCY POWER SUPPLY UNIT (13WL). OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030806000832003080600083SO 2003 8 6 C2XA03SH228 120030718A532014525480005 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 145477 SHV- DURING C-CHECK, THE BAGGAGE DOOR LOWER CUTOUT SILL BETWEEN FRAMES 66 AND 67 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030807000392003080700039NE 2003 8 7 C1HA200392004 220030804A73217436025 FUEL CONTROL BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE NR 2 ENGINE MALFUNCTIONED A C1HAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15292AS 21458 ON TAKEOFF ROLL, NR 2 ENGINE EGT PEAKED AT 650 DEG, THEN HEATED TO 670 FOR 5 SECONDS. ABORTED TAKEOFF, FULL POWER USED FOR T/O. REMOVED AND REPLACED NR 2 ENGINE FUEL CONTROL IAW P&W MM 73-21-01. 2L73 4F4 F A3WE E2EA 20030905000262003090500026SO 2003 9 5 LR7A03071 120030725A5714 WEB LKHEED382 382G 526414USO CENTER WING CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION NR 2109 ACCOMPLISHMENT FOUND RT CENTER WING AFT BEAM WEB CRACKED APPROX 2.0 INCHES AT CWS 22, WL 280. REPAIRED IAW SRM SMP 583 57-30-25 AND LAC MEA 382-57-03-054. NR 2143. 2H74 4T A1SO 20030814000682003081400068SO 2003 8 14 SWIA200312115 120030522A5413 STRINGER EMB 135 EMB135ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 LEFT NACELLE OUTBOARD STRINGER CRACKED AT RIVET HOLES. FOUND DURING C-CHECK INSPECTION. APPLIED DOUBLER TO CRACKED AREA IAW SRM120 51-10-02. 2L72 4F RTT00011AT 20030723000302003072300030NM 2003 7 23 USAA030100 120030620A5310146N83261 CREASE BEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU 22201 FOUND CREASE BEAM/CHORD CORRODED 10 INCHES BY 1 INCH AREA, STATION 1319-1369.9 LEFT SIDE. REPLACED CREASE BEAM AND ANGLE PER EA 85570. (M) 2L72 4F RTA2NM 20030728001012003072800101 2003 7 28 SWAA031584 420030718A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030729000482003072900048NM 2003 7 29 ZW0A0305705 120030703A256069B148553 SPRING BOEING757 7572Q8 1384972NM GIRT BAR BROKEN A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13712TW 27624 AN EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRING WAS BROKEN AND REPLACED AT THE L1 AND R1 DOORS. 2L72 4F RTA2NM 20030820002302003082000230NM 2003 8 20 USAASB03099 120030703A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19429US 24551 MAINTENANCE REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY EXIT LIGHT AT SEAT ROW 11, LEFT SIDE, ALONG WITH THE FLOOR PATH EMERGENCY LIGHTS FROM SEAT ROWS 7 THROUGH 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, P/N 2013-1A, AND CHARGER ASSEMBLY AT STATION 598, RIGHT SIDE. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20030912001432003091200143NM 2003 9 12 AWXA200300901 120030725A53206546592 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 770, BL 0. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF FLOOR SUPPORT BS 770, BL 0; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-70-53, FIG 201, PG 1. 2L72 4F RTA16WE 20030930000462003093000046NM 2003 9 30 2003UALA00665 120030904A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 EXTERNAL FUSELAGE SKIN DENTED AT BODY STA 1780 ADJACENT TO STRINGER 34R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED EXTERNAL DOUBLER & FILLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20030930001282003093000128NM 2003 9 30 F3LA200300127 120030904A5320 WEB BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLES ON WEB AT STA 787 TO STA 794.3. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-10-2. 2L72 4F RTA16WE 20030929000792003092900079NM 2003 9 29 03FDEA01448 120030901A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING I/B FLAP O/B HINGE (FLAP SIDE) LOWER I/B BORE FOUND CORRODED. 2L73 4F RTA22WE 20031001000692003100100069NM 2003 10 1 2003UALA00707 120030921A5230 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29305UA 23666 FWD CARGO PIT DOOR EXTERNAL SKIN, AFT LOWER QUADRANT-HAS NUMEROUS DENTS. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030908002502003090800250NM 2003 9 8 VNAA0308017 120030826A7931 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE DIRTY A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07457PS 3048 EN ROUTE, THE CREW RECEIVED A LEFT HAND PROP LOW OIL PRESSURE INDICATION AND RETURNED TO TYS. MAINTENANCE INSPECTED AND SERVICED THE LEFT HAND OIL AND CLEANED THE CANNON PLUG ON THE LOW PRESSURE SWITCH THEN PERFORMED GROUND RUNS WITH THE CREW IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031006000592003100600059CE 2003 10 6 AMWA33 120030907A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07182YV UE182 RIB CRACKED AT CSS 69.184 AT STRG P/N 101-640000-46 RT AND STRG P/N 101-640000-45 LT SIDE (2EA CRACK AT THIS RIB). 2L72 4T RTA24CE 20031014000682003101400068NM 2003 10 14 SWAA032206 120031003A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 6, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031022000962003102200096NE 2003 10 22 UO22003F00004 220030911A723030724631 BLADE AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE73131C 01518NE COMPRESSOR FAILED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19517CW10092 17 P76154 FAN BLADE MIDSPAN DAMPER FAILED CAUSING DAMAGE TO ENGINE INLET AND BY-PASS STATOR. 2L73 4F4 F A46EU E6WE 20031023000762003102300076NM 2003 10 23 F3LA200300145 120030924A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT LBL 16, BETWEEN STA 967 AND 947.5, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10-2, 51-40-02, 53-60-51 AND 51-20-01. 2L72 4F RTA16WE 20031120000852003112000085EU 2003 11 20 MALA030454 120031005A5311 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN CWA, FRAME 258 TOP PROFILE HAS CORROSION. MAINTENANCE CUT OUT DAMAGE, FABRICATED REPAIR, INSTALLED NEW FWD ANGLE IAW SRM 51 AND EO NR 53102. REF LOG PAGE NR 195722 FOR DETAIL. A/C RELEASE DATE 10/12/2003. 2L72 4T4 TRTA52EU E8NE 20030613001502003061300150NM 2003 6 13 SWAA031231 120030602A5313BAC1498 STRINGER BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 179, STR 17L. REPAIRED STRINGER PER SRM. 2L72 4F A16WE 20030613001582003061300158NM 2003 6 13 SWAA031217 120030601A57546546430 SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED C4 CHECK, FOUND LT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBD FOREFLAP PER MM. 2L72 4F RTA16WE 20030618000922003061800092NM 2003 6 18 SWAA031278 120030609A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030528000762003052800076WP 2003 5 28 AALA20030428 120030409A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21455AA 49560 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 16D INOPERATIVE. REPLACED EMERENCY EXIT LIGHT ASSEMBLY AT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030618000852003061800085SW 2003 6 18 HEEA087345 120030611A6510407040330105 SHAFT BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH3063 53378 BEARING MOUNT AREA HAS DAMAGE. 1G71 3U O H2SW 20030618001752003061800175SW 2003 6 18 HEEA087513 120030612A3212206050247135 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 FLOAT COVER TORN. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030630000332003063000033NM 2003 6 30 AWXA200300608 120030514A5315654654023 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A 2 INCH CRACK WAS FOUND ON TRANSVERSE FLOORBEAM WEB OUTBOARD OF LBL 45.50, BS 639. MAINTENANCE REMOVED DAMAGED ON WEB AT LBL 45.50, BS 639; FABRICATED REPAIR DOUBLERS AND A STRAP PER SB 737-53-1061 R4; INSTALLED REPAIR PARTS IAW E.R. 15-5300-03142-TB1. 2L72 4F RTA16WE 20030623001172003062300117EA 2003 6 23 A6WA200340079 120030528A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR SEAL DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 PASSENGER DOOR SEAL STRIKER AT FS 310 IS DAMAGED MIDWAY TOP TO BOTTOM. REPAIRED DAMAGED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-52-11-008 REV B. (M) 2L72 4F RTA21EA 20030625000352003062500035NM 2003 6 25 AWXA200300589 120030503A5320146N52421 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SUPPORT AT B/S 1640, BL 0. MAINTENANCE FOUND CORROSION WAS ON EXISTING REPAIR; REMOVED CORRODED REPAIR PART AT BS 1640, BL 0; FABRICATED A LEACH CHANNEL PER DWG 146N5242-1, AND A NEW REPLACEMENT FLOOR SUPPORT PER DWG 146N5230; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-20-01, PG. 10. 2L72 4F RTA2NM 20030708000892003070800089WP 2003 7 8 UPS03840925 120030618A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, EXTERIOR FUSELAGE FRAME TO SKIN SHEAR TIE IS BROKEN,STATION 702 BETWEEN LONG. 33L TO 35L. REMOVED DAMAGED SHEAR TIE SECTION, FABRICATED AND REPLACED SHEARTIE SECTION IAW DWG. 5750365 AND SRM. 53-2-0 FIG. 2 2L74 4F4 FRT4A25 E2GL 20030710000152003071000015NM 2003 7 10 TSAA0333145 120030609A33509221009 BATTERY PACK BOEING737 7372S2C 138448GNM PAX CABIN INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13806AL 21927 REPLACED AFT CARGO BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030710001092003071000109SO 2003 7 10 C2XA03SH190 120030618A532014521721005 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK THE LT HAND BUTTSTRAP BETWEEN FRAMES 14 AND 17 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01074. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116001582003011600158NM 2003 1 16 2003F00085 120030106A2560 RETAINER BOEING737 73783N 13844HINM L1 DOOR DEFECTIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11310TZ 28243 GIRT BAR RETAINER DEFECTIVE AT L1 DOOR. ADJUSTED GIRT BAR RETAINER HOOKS, OK FOR SERVICE. 2L72 4F RTA16WE 20030127002312003012700231SO 2003 1 27 C2XA03BT015 120030126A3350 LIGHT EMB 145 EMB145ER 3260211SO INTERMITTENT A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2714945 145049 BDL---CO2578, CREW REPORTED, "EMERGENCY AISLE PATH LIGHTING INTERMITTENT". MAINTENANCE PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM IAW EMB145 AMM #33-50-00. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030128001732003012800173SW 2003 1 28 HEEA083879 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20040114000742004011400074NM 2004 1 14 DL757030991 120031108A3260841602 PSEU BOEING757 757232 1384965NM E/E BAY FAULTY A DALAA UNSCHED LANDING FGJFLT CONT AFFECTED MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO27610DL 22817 DIVERSION TO PHX - APPARENT GROUND PROX SYS ERROR-AT CRUISE ALT GOT F/O PITOT- RT AUX PITOT- TAT - A/T DISC - PROBE HEAT CAUTIONS. LEFT GREEN SIDE OF NOSE AND RIGHT MAIN GEAR LIGHTS ILLUMINATED. STATUS MSGS GROUND PROX SYS - LANDING GEAR MONITOR - NOSE A/G DISAGREE - AIR GROUND DISAGREE - CABIN TEMP HARD TO CONTROL TOO. FLT CREW GAVE AMT VERBAL REPORT OF FULL SPOILER DEPLOYMENT ON APPROACH RESULTING IN CONTROL DIFFICULTIES. CREW SUBSEQUENTLY STOWED SPOILERS. FOUND CARD 5 BAD IN PSEU. REPLACED PSEU. PERFORMED SUCCESSFUL TEST OF PSEU. 2L72 4F RTA2NM 20040127001712004012700171NM 2004 1 27 ASAA0310199 120030321A534765549057 FLOORBEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOORBEAM AT BS 420, BUTTOCK LINE 0, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031030000832003103000083NM 2003 10 30 QXEA200301198 120030925A5340 CLIP DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FRAME CLIP IS DAMAGED AT INBOARD END BEHIND SEAT TRACK AT FRAME 270.500 FORWARD SIDE OF NR 1 SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20031031000162003103100016WP 2003 10 31 ABXA030371 120030930A3260 UPLOCK DOUG DC9 DC931 3022065WP PWA JT8 JT8D* NE MLG OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CRCRUISE 1 GL23908AX 47008 CYCLED MAIN LANDING GEAR AT 210 KNOTS, 3000 FT, CLEAN UPON RETRACT. RIGHT MAIN LANDING GEAR UNSAFE LIGHT STAYED ON. ADJUSTED RIGHT MAIN LANDING GEAR DOOR UPLATCH IAW DC-9 MM AND WORK ACCOMPLISHED ON W.O. NR 2003908. OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20031028001452003102800145NM 2003 10 28 GAIA03099 120030910A5310 BEAM BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND BS 1183 VERTICAL BEAM CRACKED LBL 36 INCHES WL 250. REF FASI N/R 53249, INSTALLED REPAIR PER S/B 727-53-0192 REV 2. (M) 2L73 4F A3WE 20031105000302003110500030EU 2003 11 5 AWXA200301296 120031008A5414D54530052200201 SKIN AIRBUS320 A320231 3930325EU NR 1 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 MCN - MAJOR REPAIR - DURING C-03 CHECK THE NR 1 PYLON AFT FIXED FAIRING OUTBOARD SKIN WAS FOUND PITTED. MAINTENANCE REMOVED PITTED NR 1 PYLON AFT FIXED FAIRING OUTBOARD SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-12, & 22, FIG 2, 3, & 8. 2L72 4F RTA28NM 20031105000872003110500087NM 2003 11 5 2003UALA00794 120031027A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29181UA 25278 LIGHTNING STRIKE DAMAGE AT STA 134.75 AND STR 45R. MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20031106001772003110600177NM 2003 11 6 03FDEA01827 120031029A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION WHILE WORKING N01449 FOUND CORROSION ON TOP SURFACE OF UPPER CHORD OF FLOORBEAM BS 1070 RBL 23 WL 208. 2L73 4F RTA3WE 20031106002052003110600205NM 2003 11 6 2003F00596 120030928A2560SG9634 STRIP BOEING727 727200 138407ENM AFT GALLEY OUT OF POSITION A P9RAK NONE O OTHER ININSP/MAINT 1 SO11910PG 22606 FLOOR EMERGENCY GLOW STRIP DISPLACED IN AFT GALLEY. INSTALLED DISPLACED PHOTO LUMINESCENT TRACK SEGMENT PER SAFTGLO MM 33-60-13. (M) 2L73 4F RTA3WE 20031103000962003110300096WP 2003 11 3 ABXA030384 120031001A57433755769 BUSHING DOUG DC8 DC861 3021952WP RT MLG CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 RIGHT MAIN LANDING GEAR ATTACH FITTING (TRUNION) HAD BROWN GREASE EMITTING FROM LUGS AT FORWARD AND AFT ATTACH POINTS. REMOVED RIGHT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45, DC-8 SRM 51-1-8. REINSTALLED RIGHT MAIN LANDING GEAR IAW DC-8 MM 32-11-01, 32-32-10, 32-32-02, 32-11-03, 32-11-04, 32-43-02, AND 32-41-01. OPS CHECKED GOOD IAW DC-8 MM 32-30-0, 32-43-00, AND 32-32-02. LUBRICATED RIGHT MAIN LANDING GEAR IAW DC-8 MM 12-81-01. LEAK CHECKED GOOD IAW DC-8 MM 29-10-00-6. RIGHT MAIN LANDING GEAR STRUT SERVICE COMPLIED WITH ON JOB CARD 8761002, AND IAW DC-8 MM. 2L74 4F 4A25 20031110001622003111000162NM 2003 11 10 SWAA032264 120031015A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 4R CRACKED AT BS 619. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030915000912003091500091SW 2003 9 15 BAQA088959 120030903A2435 BRUSHES BELL 222 222U 1182140SW STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03223HX752 14523 47511 STARTER GEN BRUSHES WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H9SW 20030916001322003091600132WP 2003 9 16 GTIA030637 120030727A5321 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND LEFT AFT LAV INBOARD ASSEMBLY FLOOR PANEL IS DAMAGED AND DISBONDED UPPER AND LOWER SURFACE. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040112000382004011200038NM 2004 1 12 AALA20031450 120031219A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21907AN 29509 BOS EMERGENCY LIGHTS AT ROWS 7DEF THROUGH 10DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7DEF THROUGH 10DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040112001172004011200117WP 2004 1 12 AALA20031230 120031106A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 DEN - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD RIGHT AND LEFT UPPER DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD RIGHT AND LEFT UPPER DOOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112001892004011200189NM 2004 1 12 AWXA200301255 120031009A531256175823 BULKHEAD BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND AT FASTENER HOLE ON BS 178 BULKHEAD VERTICAL WEB AT RBL 17.1, WL 234. MAINTENANCE CUTOUT CRACK ON VERTICAL WEB AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SECTION OF VERTICAL WEB; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG. 288K-288V, FIG. 212. 2L72 4F4 FRTA16WE E2GL 20031117000402003111700040CE 2003 11 17 54885 120031002A7712 INDICATOR BEECH 1900 1900D 1154162CE RT ENG TORQUE FLUCTUATES A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07143YV UE143 DURING TAKE OFF RIGHT TORQUE WENT TO ZERO. TAKE OFF WAS ABORTED AND AIRCRAFT RETURNED TO MAINT. REMOVED AND REAPLCED GAUGE.P/N 114-3800-653 S/N 132. 2L72 4T RTA24CE 20040113001042004011300104EU 2004 1 13 BAQA091402 120031127A243523081057 STARTER GEN UROCOPEC135 EC135T1 5620026EU ENGINE INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME1667 0143 STARTER GENERATOR IS PRODUCING INTERMITTENT STARTS. REPLACED WITH SERVICEABLE UNIT. 12/8/03 1G72 3U H88EU 20031216000622003121600062NM 2003 12 16 SWAA032548 120031118A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 727E, STR 20L AND BS 727E+13, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031219001652003121900165NM 2003 12 19 QXEA200301502 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 2 SEAT TRACK HAS LITE SURFACE CORROSION ON TOP OF RAILS AND BOTTOM OF CHANNEL FROM 2 TO 6 INCHES FORWARD OF STATION X488. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20031219000192003121900019EA 2003 12 19 COMA0360529 120031202A5312601R5341057 POST CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 THE RIGHT BULKHEAD POST AT FS 559, RBL 9, WL 50 HAS A CRACKED FLANGE. REMOVED PORTION OF CRACKED FLANGE, FABRICATED AND INSTALLED A REPAIR ANGLE IAW REO 601R-53-41-057. 2L72 4F RTA21EA 20031222000092003122200009SO 2003 12 22 C2XA03BT115 120031207A213122250N030201 CONTROLLER EMB 135 EMB135LR 3260305SO CABIN PRESSURE FAULTY A C2XAO OTHER S AFFECT SYSTEMS DEDESCENT 1 SW27155276845 6845 145413 CREW REPORTED, AUTO PRESSURIZATION FAILED DURING DESCENT. AIRCRAFT WAS RELEASED IAW MEL 21-31-03/1 CONTROL NUMBER 037305. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER IAW EMB135 AMM 21-31-01. OPS CHECKED GOOD. REMOVED FROM MEL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031223000922003122300092NM 2003 12 23 SWAA032703 120031210A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND CRACK IN STRINGER 7L BS 1012. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20031219000782003121900078NM 2003 12 19 P5CA0301004 120031205A3260 DOWNLOCK SWITCH BOEING747 747236B 1384804NM NLG SHORTED A P5CAD RETURN TO BLOCK J WARNING INDICATION ININSP/MAINT 1 WP23924FT 21730 AFTER PUSHBACK AUTO SPOILER LT CAME ON FOUND PRIM & CONT C/B POPPED. A/C RETURNED TO BLOCKS. TRANSFERRED TO DMI 31904 PER MEL 32-11A FOUND NOSE GEAR PRIMARY DOWNLOCK SWITCH S206 SHORTED. 2L74 4F A20WE 20031229000492003122900049NM 2003 12 29 AALA20031417 120031211A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21791AN 30254 ALL SEAT MOUNTED EMERGENCY LIGHTS IN AFT COACH INOPERATIVE. REPLACED BATTERY PACK FOR ALL SEAT MOUNTED EMERGENCY LIGHTS IN AFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20031231000702003123100070EA 2003 12 31 ASOA03573 120031108A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 FLT 4415 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPS CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040105001222004010500122NM 2004 1 5 SWAA032761 120031217A32601899 SENSOR BOEING737 7373H4 1384600NM NLG FAULTY A SWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW29374SW 26582 INFLIGHT AT CRUISE RED NOSE GEAR LIGHT ILLUMINATED, WENT OUT ON ITS OWN. ON SHORT FINAL AFTER GOOD 3 GREEN, GREEN LIGHT OUT RED LIGHT ON, LANDING GEAR WARNING HORN, GO AROUND RECONFIGURED, THIS TIME NOSE GEAR GREEN. REMOVED AND REPLACED LOCK SENSOR PER MM. 2L72 4F RTA16WE 20031010000262003101000026NM 2003 10 10 USAABB03166 120030911A33509221009 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031014001442003101400144NM 2003 10 14 SWAA032063 120030915A57536546435278 SKIN BOEING737 7373H4 1384600NM OUTBD T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C1 CHECK, FOUND RT OUTBD T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED RT OUTBD T/E FLAP PER MM. 2L72 4F RTA16WE 20031124001412003112400141EA 2003 11 24 03294633 120031021A3350 TERMINAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DIRTY A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27633BR 7274 DURING INSPECTION THE EMERGENCY TRACK LIGHTING AFT OF THE EMERGENCY EXIT ROW WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE WIRE TERMINALS AT THE CONNECTION. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031126000072003112600007SO 2003 11 26 RAIA00311289 120031120A3230 LANDING GEAR EMB 145 EMB145LR 3260212SO NLG & MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03810HK 145231 5253-PIT- LANDING GEAR WILL NOT RETRACT. MAINTENANCE PERFORMED NUMEROUS LANDING GEAR RETRACTION CYCLES. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20031126000692003112600069NM 2003 11 26 AWXA200301479 120031123A3350BR964411 LIGHT BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20031126001152003112600115NM 2003 11 26 ASAA0310448 120030515A575365495053 SKIN BOEING737 737290C 138448VNM TE FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND RIGHT WING FORE FLAP SKIN AT WING STATION 417 WORN. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031202000372003120200037NM 2003 12 2 ASAA0340088 120030228A53206547690 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON TOP FO FLOOR TO SIDEWALL SUPPORT BS 727 LBL 21. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031202000732003120200073NM 2003 12 2 USAABB03188 120031014A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 9, 12 AND 33 LOW ON POWER. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031202001042003120200104EU 2003 12 2 ASOA03519 120031018A5343S53975102204 SUPPORT BRACKET AEROSPATR72 ATR72212 8680945EU MLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11532AS 458 DURNG AN A-CHECK IN MCN, THE LEFT MAIN LANDING GEAR AFT UPSTOP SUPPORT BRACKET ON THE TOP SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR AFT UPSTOP SUPPORT BRACKET IAW SRM 51-00. (M) 2H72 4T RTA53EU 20031204000342003120400034 2003 12 4 AALA20030996 420030909A25655A33073 SLIDE BOEING737 737823 13844BZNM R1 DOOR FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21902AN 29504 TECHNICIAN OBSERVED EMERGENCY ESCAPE SLIDE FAILED TO DEPLOY PROPERLY. SLIDE WAS TIED IN A KNOT AFTER INFLATION. BOTTLE PRESSURE WAS GOOD, EVERYTHING ELSE APPEARED TO BE NORMAL. REPLACED SLIDE PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20031204001502003120400150NM 2003 12 4 03FDEA01768 120031020A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 FLOOR SUPPORT AT STA 635 LT =47.5 CRACKED. 2L73 4F RTA22WE 20031211000682003121100068WP 2003 12 11 UPS03841561 120031024A52309754003505 DOUBLER DOUG DC8 DC873F 302199FWP CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 A PIT DOOR INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN STATION 260-320 AND LONG 28R TO LONG 36. REMOVED AND REPLACED DOUBLER IAW DWG 9754003 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20031015000322003101500032EA 2003 10 15 ASOA03429 120030910A55006002112318 ANGLE CNDAIRCL600 CL6002B19 1900309EA TAIL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE VERTICAL STABILIZER RIGHT VISOR PANEL ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STABILIZER RIGHT VISOR PANEL ANGLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030916000152003091600015NM 2003 9 16 S03453043 120030603A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJFO OTHER O OTHER NRNOT REPORTED 1 WP03 29219 FUSELAGE SKIN IMPACT DAMAGE AT BS 200, BETWEEN S-43L AND S-44L. REPAIRE PER EO 744-53-00-0006 R1 2L74 4F4 FRTA20WE E24NE 20030916000162003091600016NM 2003 9 16 MEX2003236 120030618A29109216797 PACKING BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED W ASMFO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW23803AM 26268 AIRCRAFT ARRIVED WITH CAPTAIN REPORT WITH 1 QUART OF OIL IN ENGINE NR 2. DURING REVISION WAS DETECTED LEAK IN RIGHT HYDRAULIC PUMP. THE RIGHT HYDRAULIC PUMP PACKING WAS REPLACED IAW MM. DURING OVERNIGHT SERVICE RIGHT HYDRAULIC PUMP WAS REPLACED IAW 29-11-40, ALL TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20030923001302003092300130CE 2003 9 23 DXTA200300101 120030823A3234 CONTROL HANDLE CESSNA560 560XL 2076702CE MLG DEFECTIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07651QS 5605251 AFTER TAKEOFF THE GEAR WOULD NOT RETRACT, NO UNLOCK LIGHT OR ANY FLICKERING OF THE 3 GREEN LIGHTS, ACCOMPLISHED AIR TURN BACK TO SJC. - FOUND LANDING GEAR CONTROL HANDLE DEFECTIVE, REMOVED DEFECTIVE LANDING GEAR CONTROL HANDLE AND INSTALLED NEW UNIT IAW MFG 560XL MM CHAPTER 32-30, SYSTEM OPS CHECKED GOOD. 2L72 4F RTA22CE 20040217000132004021700013EU 2004 2 17 ASOA03691 120031228A3397E0053R10B6SNF CONNECTOR AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING AN 'A' CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE CLEANED THE PASSENGER DOOR EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031210001112003121000111 2003 12 10 AWXA200301504 420031129A344146502003030312 IRU AIRBUSA319 A319132 3930340NM E/E BAY FAULTY A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28827AW 1547 LAX - ABORTED TAKEOFF - FLT 0408 - ON TAKEOFF ROLL AT LAX EN ROUTE FOR BOS THE CAPTAINS AIRSPEED INDICATOR SHOWED 40 KTS AT THE 80 KTS CROSS CHECK. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST OF ADIRU S/N 3248 CONFIRMED FAILURE OF UNIT. REPLACED 2 EACH VIBRATION ISOLATORS AND ISOLATOR COVER (P/N 465301-01). INCORPORATED SERVICE BULLETIN SB 101-34-57 PER CEO 3412-01020, REPAIR PERFORMED IAW CMM TP1011, REV. 23. 2L72 4F RTA28NM 20030203002372003020300237EU 2003 2 3 WRNA200300002 120030131A5230 DOOR AIRBUS300 A300B4203 3930306EU A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05821SC 211 After Departure bulk cargo door illuminated in flight. A/C returned to field, landing normal, no fuel was dumped.Corrective Action: Cycled aft bulk door I/A/W MM 52-34-00. Door indication op's checked normal. Door was verified to be closed and locked. Aircraft returned to service. 2L72 4F RTA35EU 20030204001782003020400178NM 2003 2 4 SWAA030105 120030116A3350BR2013 CAP BOEING737 7372H4 138448CNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C2 CHECK, FOUND EEPLS, AFT TRACK END CAP MISSING. INSTALLED NEW EEPLS TRACK END CAP PER M/M. 2L72 4F A16WE 20030204001952003020400195NM 2003 2 4 SWAA030125 120030119A3350610478 BATTERY PACK BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED A1 CHECK, FOUND THE OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT LIGHT BATTERY PACK PER MM. 2L72 4F A16WE 20030213000262003021300026NM 2003 2 13 CA030127006 120030117A551165174331 RIB BOEING BOEING727 727171C 1384057NM PWA JT8 JT8D7A 52053NE HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 32312 (CAN) DURING INSPECTION OF THE HORIZONTAL STABILIZER TRAILING EDGE RIBS, IN ACCORDANCE WITH AD 2002-12-13 AND BOEING SB 727-55A0091 A CRACK WAS FOUND ON THE UPPER OUTBOARD FLANGE OF THE FITTING AT ELEVATOR STATION 66.50 RT. THE CRACK WAS REPORTED TO BOEING SERVICE ENGINEERING AND THEY PROVIDED A REPAIR SCHEME, EKO-YEG-03-00006H, WHICH WAS INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. THE REPAIR IS LISTED AS TEMPORARY AND WILL BE CHANGED WITHIN 12 MONTHS WITH PERIODIC NDT AT 90 DAY INTERVALS UNTIL FITTING REPLACEMENT. 2L73 4F4 F A3WE E2EA 20030213000842003021300084WP 2003 2 13 03FDEA0043 120030116A5310AEA70971 BEAM DOUG DC10 DC1030F 3023504WP GE CF6 CF680 30025NE RT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25306FE43440 48287 TEE CAP AEA 7097-1, STA.1521 WAS FOUND CORRODED AT RT STA.-80.125 WHERE VERTICLE BEAM A0024-2 ATTACHES. THE BEAM ATTCHMENT TO THE TEE CAP CREATES A (V) WHERE WATER CAN PUDDLE. AWAITING APPROVED REPAIR FROM BOEING 2L73 4F4 FRTA22WE E13NE 20030224000572003022400057NE 2003 2 24 HEEA084178 120030212A24217655009005109 GENERATOR SKRSKYS76 S76A 8143006NE AC SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 AC GENERATOR FALLS OFF LINE IN FLIGHT. 1G72 3U H1NE 20030227000012003022700001SO 2003 2 27 C2XA03SH031 120030227A530014521721005 STRAP EMB 145 EMB145LR 3260212SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV-DURING C CHECK A SPLICE ANGLE ON THE CENTER BEAM TO BUTTSTRAP BETWEEN FRAMES 14 AND 16 WAS FOUND CRACKED. MAINTENANCE PERFORMED AN ANGLE SPLICE REPAIR TO AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030304000152003030400015SW 2003 3 4 AC2A084871 120030225A5330 SKIN BELL 430 430 1182150SW FUSELAGE CHAFED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT 49089 CABIN ROOF RT SIDE, HAD CHAFED SPOT FROM COWLING THROUGH HONEYCOMB PANEL STATION 210, WL 87. THE COWLING WAS POORLY FITTED TO THE AIRCRAFT, DURING THE MANUFACTURING PROCESS. THE CABIN ROOF HAD TO BE PATCHED AND THE BOTTOM EDGE OF COWLING HAD TO BE TRIMMED. 1G72 3U RTH9SW 20030304001052003030400105NM 2003 3 4 HNAA0300011 120030304A291082910010111 HYDRAULIC LINE DHAV DHC8 DHC8201 2809001NM NOSE GEAR WELL BURST A HNAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA07987HA1806818068 425 Lost number 2 hydraulic quantity in flight. Replaced nose gear up line. 2H72 4T RTA13NM 20030305000712003030500071EU 2003 3 5 HEEA084654 120030212A6720 BEARING BOLKMS105 BO105S 5626006EU BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038199J S826 BELLCRANK ASSY WORN BEARINGS. REPLACED BEARING 2828P AND EN2015BN06E DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030307000992003030700099 2003 3 7 HEEA084900 420030228A34427021450601 COMPUTER SKRSKYS76 S76A 8143006NE WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 WEATHER RADAR SYSTEM COMPUTER INTERMITTENTLY SHUTS DOWN AFTER TEN MINUTES. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030310000832003031000083 2003 3 10 HEEA084987 420030227A34427021450601 COMPUTER BELL 412 412 1182202SW WX RADAR SYSTEM FAILED E O OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 WEATHER RADAR SYSTEM UNIT DISPLAYS FAIL MESSAGE. 1G72 4U H4SW 20030310000872003031000087 2003 3 10 HEEA084991 420030227A344580511400003 CONTROL UNIT BELL 412 412 1182202SW COLLISION AVOID INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 AIR COLLISION AVOIDANCE CONTROL UNIT DATA DISPLAYED ON WEATHER RADAR INTERMITTENTLY CHANGES COLOR. 1G72 4U H4SW 20030310001472003031000147NM 2003 3 10 EIA2003014 120030222A5300UNK BELTFRAME BOEING747 747132 1384882NM A EIAAO OTHER O OTHER ININSP/MAINT 1 NM09481EV 19896 Frame Cracked STA 340 1" below Sringer 16 left. CORRECTIVE ACTION: Repaired per ECR # 481-53-175-2 2L74 4F A20WE 20030311000332003031100033 2003 3 11 HEEA085050 420030228A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038592X 51508 ADI UNRELIABLE AND PRECESSES. SHOP REPAIR. 1G71 3U H2SW 20030311001082003031100108WP 2003 3 11 ABXA030107 120030305A278039202772 BRACKET DOUG DC9 DC941 302207NWP RIGHT WING BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 SLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, #1 AND #2 SLAT PULLEY BRACKETS BROKEN, AND 3 EACH LEADING EDGE RIBS (FORMERS) DAMAGED. THE RIGHT #2 SLAT DRIVE TRACK CABLE PULLEY BRACKET (P/N 3920277-2) WAS BROKEN IN HALF AT BOTH FEET AND CORRODED AT A SMALL CORNER OF THE BROKEN SURFACE. REPLACED PULLEY BRACKET IAW DC-9 MM 20-17-2-001. 2L72 4F A6WE 20030117000242003011700024SW 2003 1 17 HEEA083163 120030108A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 TRANSMISSION RESTRAINT WORN. REPAIRED. 1G71 3U H2SW 20030120000162003012000016EA 2003 1 20 COMA0360034 120030116A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01409CA 7441 FLIGHT 5118 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL. 2L72 4F RTA21EA 20030121000092003012100009NM 2003 1 21 SWAA030070 120030111A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 639, RBL 65, WL 208. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20030121000722003012100072NM 2003 1 21 PCAA0301018 120030119A3231DSC1822 RELAY DHAV DHC8 DHC8102 2809003NM CLOSET INTERMITTENT A PCAAK NONE S AFFECT SYSTEMS APAPPROACH 1 EA13814EX 318 PHL-FLIGHT#3907. CREW REPORTED ALL GEAR DOORS CYCLED OPEN AND CLOSED 4 TIMES AFTER GEAR WAS SELECTED DOWN AND LOCKED. MAINTENANCE OPERATIONALLY CHECKED PROXIMITY SENSOR ELECTRONICS UNIT(PSEU), OPERATIONAL CHECKED GOOD. AIRCRAFT GROUND RAN, AND DOORS CYCLED. PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. PIT-FLIGHT#3891. CREW REPORTED GEAR DOORS CYCLED OPEN AND CLOSED SEVERAL TIMES WHILE ON APPROACH. MAINTENANCE REPLACED RELAYS 3261-K8 AND 3261-K9. GEAR SWUNG SEVERAL TIMES, WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030314001352003031400135WP 2003 3 14 GTIA030112 120030211A5313 LONGERON DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FS 370 CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 MAIN CABIN FS 370, STR 16, CRACKED. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED LONGERON SECTION AND SPLICE. INSTALLED LONGERON AND SPLICES. 2L72 4F4 F A6WE E2EA 20030314001472003031400147SO 2003 3 14 O2G2003F00004 120030213A53105E2510211943 DOUBLER GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU LOWER FUSELAGE CORRODED E O2GAO OTHER O OTHER NRNOT REPORTED 1 NE03524MM4605 85 CORROSION PRESENT ON DOUBLERS FORWARD OF BATTERY BOX AND AFT OF BAGGAGE DOOR. REPAIR REQUIRED PULLING BACK SKIN FROM STRINGER 19 TO STRINGER 11 AND FORWARD TO THE FAIRINGS BELOW THE BAGGAGE DOOR AND SPLICING NEW DOUBLER INTO PLACE. 2L72 4F4 FRTA12EA E2EU 20030314001852003031400185SO 2003 3 14 000244 120030220A3240 BRAKE ASSY EMB 145 EMB145 3260210SO MLG OVERHEATED A CHQAD RETURN TO BLOCK MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL11370 RT INBOARD MLG BRAKE ASSY. SHOWED HIGH TEMP INDICATIONS ON MFD AND NOTICED SMOKE COMING FROM RT INBOARD BRAKE ASSY. R&R'D RT INBOARD BRAKE 2L72 4F RTT00011AT 20030317001212003031700121NM 2003 3 17 03FDEA00280 120030306A2612 WARNING LIGHT BOEING727 727200 138407ENM NR 2 ENG FIRE ILLUMINATED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25210FE 22932 FIRE WARNING BELL SOUNDED AND GLARE SHIELD FIRE WARNING LIGHT ILLUMINATED MOMENTARILY WHILE ADDING POWER IN A CLIMB FROM FL 290, ABOUT 1.7 EPR, HAPPENED AGAIN 10 MIN LATER AT FL 310, ABOUT 2.0 EPR, TO QUICK TO DETERMINE WHICH ENGINE. 2L73 4F RTA3WE 20030318001192003031800119NM 2003 3 18 F3LA200300102 120030228A5320 CHANNEL BOEING737 7373Q8 1384670NM STA. 727 CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT CHANNEL CRACKED AT STA. 727, RBL 4. FABRICATED AND REPLACED CHANNEL PER 51-20-02, 51-30-01, FIG. 3, 51-10-02, FIG. 7, AND 51-20-01. 2L72 4F RTA16WE 20030320000722003032000072NM 2003 3 20 2003F00149 120030319A492038007021 APU BOEING737 737724 13844BYNM APU BAY FLAMED OUT B CALAO OTHER O OTHER NRNOT REPORTED 1 WP28237076984 6984 28768 APU REMOVED FROM AIRCRAFT WHEN APPARENT THERMAL DAMAGE WAS NOTED AT TAIL SECTION OF AIRCRAFT. UPON RECEIPT OF APU AT HONEYWELL REPAIR STATION THE APU WAS EVALUATED IN A TEST CELL. FLAMES OUT THE TAILPIPE WERE NOTED DURING TEST CELL OPERATION OF THE APU. CURRENTLY ROOT CAUSE ANALYSIS IS BEING PERFORMED TO DETERMINE THE FAILRE MODE OF THE APU. 2L72 4F RTA16WE 20030121003222003012100322 2003 1 21 HEEA083373 420030109A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 ADI INOPERATIVE, FLAG WILL PULL BUT GYRO WILL NOT WIND UP. REPAIRED. 1G71 3U H2SW 20030122000132003012200013SW 2003 1 22 HEEA083400 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 536 MAIN BATTERY WEAK. 1G71 3U H2SW 20030327000202003032700020NM 2003 3 27 AWXA200300288 120030303A5311651630087 FRAME BOEING737 737277 1384570NM 178 BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD SIDE FRAME WL 207, RBL 24, JUST ABOVE FLIGHT COMPARTMENT FLOOR. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD SIDE FRAME AT WL 207, RBL 24; FABRICATED A NEW REPLACEMENT FRAME; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-30-2, PG. 1. 2L72 4F RTA16WE 20030418000512003041800051WP 2003 4 18 UPS03840186 120030203A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, STA 1760 LONG 25L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED SPLICES IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040225001582004022500158NM 2004 2 25 DL73S031126 120031223A5340 CLEVIS BOEING737 737232 1384475NM AFT FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 CORROSION DAMAGE FOUND WHICH EXCEEDED LIMITS COVERED IN 03-085220-03. CORROSION WAS FOUND IN THE NR 6 AND NR 12 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND REWORKED PER ERA 386007-14. 2L72 4F RTA16WE 20040226000392004022600039NM 2004 2 26 ASAA0310685 120031224A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 9 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20030827000432003082700043SO 2003 8 27 J792003F00002 220030606A8510641250 SEAL BEECH 58 58 1152740CE CONT O550 IO550C SO ENGINE LEAKING A J79RK NONE K FLUID LOSS ININSP/MAINT 1 GL1395KM 497 TH1315 810485R DURING ANNUAL 100 HOUR INSPECTION, FOUND RIGHT ENGINE CRANKSHAFT SEAL LEAKING. REPLACED WITH NEW PN 641250. LEAK CHECK, OK. SUSPECT LEAK CAUSED BY WEAK SEALANT AND TSMOH. 1L72 3O3 O 3A16 E3SO 20030829000842003082900084 2003 8 29 P5CA0300927 420030825A25657A14124 SLIDE BOEING747 74747UF 1384949NM CABIN FAILED A P5CAK NONE L NO TEST ININSP/MAINT 1 WP23496MC 29257 RIGHT UPPER DECK SLIDE ASSY FAILED TO DEPLOY DURING MC CHECK. NEW SLIDE INSTALLED. 2L74 4F RT1384945 20030829002002003082900200NM 2003 8 29 USAA030129 120030731A5314 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 PIT - FOUND RIGHT KEEL BEAM FORWARD OF STATION 520, WITH CORROSION 1 INCH BY 6 INCHES. CORROSION LEVEL 1, TASK NR C53-20-01. REPLACED KEEL BEAM SECTION FROM STATION 540-500 PER TYPICAL REPAIR MANUAL 53-60-09. (M) 2L72 4F RTA16WE 20030731001282003073100128NM 2003 7 31 QXEA200300828 120030714A5320 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - VARIOUS CHAFING UNDER PANELS 262AT, 262FT ANFD 262HT ON FORWARD SIDE OF THE FUSELAGE. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030805000672003080500067 2003 8 5 ASOA03255 420030606A34426229302003 ANTENNA CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11856AS 7404 DURING CLIMB-OUT FROM VPS-DFW, THE RADAR BECAME UNSTABLE PAINTING RED AT ALL RANGES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO VPS, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR ANTENNA. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030807000812003080700081SO 2003 8 7 C2XA03SH246 120030731A532014521725401 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, THE SERVICE DOOR FOWARD SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-05. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030812000272003081200027NE 2003 8 12 HEEA088386 220030727A73200164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X3910 760050 5056 FUEL CONTROL PRODUCING TORQUE SPLITS. TO BE SENT TO VENDOR. 1G72 3U3 U H1NE E19EU 20030904001242003090400124 2003 9 4 DL757030609 420030702A2340285T002420 CONTROL PANEL BOEING757 757232 1384965NM COCKPIT MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27670DN 25331 GROUND CALL C/B POPPED WHEN GROUND CALL WAS USED TWICE IN A ROW. ALSO HAD ELECTRICAL SMELL WHEN C/B POPPED. FOUND CREW CALL PNL EMITTING ELECTRICAL SMELL. REPLACED CREW CALL PANEL NOW CKS NML. 2L72 4F RTA2NM 20030905001272003090500127NM 2003 9 5 DL73G030647 120030712A5311651630087 FRAME BOEING737 7373L9 1384470NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27232DZ 24220 FUSELAGE BULKHEAD FS 178 SIDE CHORD WL 207 : CRACK REPAIR, THE LT SIDE CHORD OF THE FS 178 BULKHEAD WAS FOUND WITH A 1 INCH CRACK AT WL 207. THE CRACK IS TYPICAL OF BAC S/B 737-53 -1173 AND AD 2000-05-29. THE CRACKED SECTION OF CHORD WAS REMOVED AND A NEW SECTION INSTALLED PER THE REQUIREMENTS OF THE S/B AND PER ER/A 385358-14AD. 2L72 4F RTA16WE 20030805000862003080500086EA 2003 8 5 ASOA03299 120030701A53116013600121 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE FRAME SECTOR AT FS 640 BELOW STRINGER 9 ON THE LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME SECTOR AT FS 640 BELOW STRINGER 9 ON THE LT SIDE IAW ASA EO 600-53-0075. (M) 2L72 4F RTA21EA 20030821002222003082100222SO 2003 8 21 RAIA00306178 120030621A361014531128402 LINE EMB 145 EMB145 3260210SO BLEED AIR SYS CRACKED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK 145068 5722-STL- AFTER TAKEOFF WHEN CHANGING FROM T/O TO CLIMB ON POWER PANEL THE RIGHT ENGINE ITT WENT INTO THE RED. MAINTENANCE REMOVED AND REPLACED CRACKED BLEED LINE FROM RT BLEED SYS. 2L72 4F RTT00011AT 20030826001362003082600136NM 2003 8 26 MEX2003272 120030707A2520 ARM DOUG MD88 MD88 3023688NM CABIN LOOSE A ASMFK NONE O OTHER ININSP/MAINT 1 SW23162PL 49765 FLT 423 - MIA-MEX - DURING CHECK, DETECTED A LOOSE ARM REST. ARM REST WAS SECURED IAW MM 20-30-01, ALL CORRECT. (M) 2L72 4F RTA6WE 20030827001572003082700157NM 2003 8 27 2003UALA00607 120030801A2913 PUMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HYD SYSTEM LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29347UA 24251 AIRCRAFT MADE A LANDING UNDER AMBER ALERT DUE TO HYDRAULIC FLUID LEAKAGE. INSPECTION REVEALED THAT THE B SYSTEM ENGINE DRIVEN HYDRAULIC PUMP WAS LEAKING FROM THE SPLINED INPUT SHAFT. THE PUMP WAS REPLACED AND THE SYSTEM WAS TESTED WITH NO LEAKS NOTED. INTERNAL INSPECTION OF THE PUMP REVEALED THAT IT HAD OVERHEATED IN SERVICE, DAMAGED INTERNAL COMPONENTS. SUBSEQUENT INSPECTION OF THE AIRCRAFT ENGINE DRIVEN PUMP CASE DRAIN FILTERS DISCOVERED THAT THE FILTER ELEMENTS WERE CLOGGED, PREVENTING ADEQUATE FLOW OF HYDRAULIC FLUID THROUGH THE PUMP CASE. 2L72 4F4 FRTA16WE E2GL 20030910000712003091000071 2003 9 10 DHL2003604790 420030818A3444 WARNING SYSTEM DOUG DC8 DC873F 302199FWP GPWS FAULTY A DHLAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01604AL89636 46047 GPWS FAIL LIGHT ILLUMINATED. REPLACED GPWS MK II WITH GPWS/WS MKVII AND OPS CHECKED GOOD IAW J/C EA34450002-001-D. 2L74 4F RT4A25 20030911000062003091100006NM 2003 9 11 03FDEA01250 120030811A5510 BARREL NUT DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 EMPENNAGE LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 36 FOUND CORRODED BEYOND LIMIT. EMPENNAGE LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 36L REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71801 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030910000392003091000039 2003 9 10 HEEA088221 420030723A2200 TARSYN BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 NR 2 HELIPILOT FAILED IN FLIGHT, THE COPILOT ATTITUDE INDICATOR FAILED AND THE CIRCUIT BREAKER POPPED. SMELLED BURNING WIRE. MAINTENANCE FOUND WIRING TO COPILOT TARSYN UNIT CHAFED IN THE AVIONICS COMPARTMENT WHERE THE TARSYN UNIT MOUNTS. REPLACED TARSYN UNIT AND REPAIRED WIRING. 1G72 4U H4SW 20030926001232003092600123EA 2003 9 26 A6WA200340116 120030803A3610 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ENGINE BLEED ILLUMINATED A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31417AW 7610 RECEIVED LT 14TH STAGE DUCT MESSAGE, COMPLIED WITH QRH. MESSAGE CLEARED WITH THRUST LEVER RETARDED. INSPECTED LEFT 14TH STAGE DUCT BLEED AIR SYSTEM IAW MM 36-12-04. NO FAULTS FOUND. RAN ENGINES TO POWER, NO FAULTS NOTED. OK FOR SERVICE. 2L72 4F RTA21EA 20030905001942003090500194NM 2003 9 5 USAA030147 120030501A1430 NUT PLATE BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 PIT - FOUND NUTPLATE CORRODED .75 INCH BY 1 INCH AREA, FS 727A-727B 21 LT. INSTALLED DOUBLER PER SRM 53-00-3. CORROSION LEVEL 1, TASK NR C53-107-01. (M) 2L72 4F RTA16WE 20030908001482003090800148EA 2003 9 8 SWIA200312216 120030723A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07430SW2964 2964 7523 'STAB CHANNEL 2 HSTA' CIRCUIT BREAKER KEEPS POPPING. REMOVED AND REPLACED MOTOR CONTROL UNIT PER CRJ MM 27-42-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20030909001482003090900148 2003 9 9 BAQA088785 420030819A3442066311400 INDICATOR BOLKMS117 BK117B1 5626012EU RADAR INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G118 7179 INDICATOR INTERMITTENTLY COMES ON WHEN IT IS IN THE STANDBY POSITION. THIS PART ONLY LASTED 118.0 HOURS AND WAS PURCHASED IN JUNE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031003000302003100300030EU 2003 10 3 AALA20030536 120030506A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211434A 11419 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN FORWARD CLOSETS OF FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING FORWARD OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031006001482003100600148NM 2003 10 6 SWAA032014 120030909A3230 LANDING GEAR BOEING737 7373H4 1384600NM MAINS MALFUNCTIONED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29391SW 27378 AIR TURNBACK, NLG WOULD NOT RETRACT, RED UNSAFE ILLUMINATED. RECYCLED GEAR, SAME INDICATION. C/W NLG EXTENSION AND RETRACTION TEST PER MM, NO DEFECTS NOTED. REMOVED AND REPLACED M1214 AND M1215 CIRCUIT CARDS PER MM FOR COMPANY CONV. 2L72 4F RTA16WE 20031021002952003102100295NM 2003 10 21 QXEA200301148 120030911A5210 STOP BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX- MAIN CABIN DOOR AFT STOP FITTING IS CHAFED. SECOND STOP DOWN FROM TOP. REPAIRED IAW Q400 SRM 51-21-10, 51-25-10 2H72 4T4 TRTA13NM E00062EN 20031023000362003102300036WP 2003 10 23 UPS03841251 120030923A3150 CONTROL PANEL DOUG DC8 DC873F 302199FWP COCKPIT SMOKE A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01811UP 46089 SMOKE IN FLIGHT DECK, ATB SMOKE COMING FROM BEHIND F/E PANEL. REMOVED 2 FUSES AND SMOKE DISSIPATED. FOUND 2 WIRES BROKEN OF P1-509 OF TI-19 REPAIRED AND REINSTALLED WIRES L120A20 & L94A-20. ALSO T/S PROBLEM TO DEFECTIVE TRANSFORMER TI-37. 2L74 4F RT4A25 20031027000272003102700027EU 2003 10 27 AWXA200301103 120030913A5315D5347218920000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON Y1292 FLOORBEAM FR 68-69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y1292 FLOORBEAM FROM FR 68 TO FR 69; RECEIVED NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PARTS IAW A320 SRM 51-49-00, PG. 5-6, TABLE 1. 2L72 4F RTA28NM 20030910000592003091000059WP 2003 9 10 DHL2003604534 120030430A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING OUTBOARD L/E FORMER CRACKED (0.250) STA XFS 747.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031027001052003102700105NM 2003 10 27 ASAA02401LL 120030329A532069736891 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND STRINGER CLIP CORRODED AT BS 787. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031030000352003103000035NM 2003 10 30 UPS03441293 120030905A5712 RIB BOEING747 747121 1384871NM NR 8 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LEFT WING NR 8 V/C FLAP I/B LINKAGE O/B RIB NR 3, NR 5 AND NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 3, NR 5 AND NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031022001262003102200126EA 2003 10 22 COMA0360422 120030922A339764645 POWER CABLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT DEFECTIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01914CA 7012 FLIGHT 5700 FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 2C, 3C, 4C AND 5C ARE INOPERATIVE. REPLACED FLOOR PROXIMITY EMERGENCY POWER STRIP. 2L72 4F4 FRTA21EA E15NE 20031112000072003111200007NM 2003 11 12 2003UALA00816 120031028A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 STA 616 STR 7L SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20031106001402003110600140SO 2003 11 6 SWIA200312529 120031023A492038003761 APU EMB 120 EMB120ER 3260203SO APU BAY LEAKING A SWIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07189SW8022 6525 120048 ON THE GROUND WITH APU ON RIGHT AND LEFT PACK IN LOW CABIN FILLS WITH SMOKE, CAUSES THE FIRE/SMOKE DETECTOR TO SOUND IN THE LAV. FOUND APU LEAKING OIL INTO BLEED AIR. REMOVED AND REPLACED APU WITH SERVICEABLE UNIT IAW MM 49-00-02. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030917000752003091700075EU 2003 9 17 BAQA089028 120030902A2822P94C16602 PUMP AEROSPAS355 AS355F1 8680810EU FUEL BOOST418008NOISY B BAQAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA03911KY1746 5101 BOOST PUMP MAKING EXTREMELY LOUD NOISES. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030918000932003091800093NM 2003 9 18 PCAA0308092 120030728A2731 CONTROL CABLE DHAV DHC8 DHC8102 2809003NM ELEVATOR TRIM OUT OF RIG A PCAAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 EA13804EX 227 CREW REPORT THAT ELEV TRIM APPEARS TO BE OUT OF RIG. MAINT CHECKED RIGGING OF ELEV TRIM AND SPRING TAB SYSTEM IAW MM. ALL TENSIONS AND REQUIRMENTS WERE WITHIN LIMITS. ELEV JACKSCREW ACT WERE LUBED. TEST FLT WAS OK. AC WAS RETNED TO SERVICE. FLT NR 3736. CREW REPORTED THAT AC APPEARS TO HAVE SOME TYPE OF TRIM OR ELEV PROBLEM, AS AC OVERROTATES ON TAKEOFF WITH TRIM SET IN NORMAL POSITION. AT 1600 FEET WILL NOT GO ABOVE 181 KTS WITH NORMAL CRUISE POWER SET. TEMP -1 DEG C. MAINT CHECKED TRAVELS ON ELEV, ELEV TRIM TAB, ELEV SPRING TABS. LT AND RT ELEV SPRING TABS WERE REPLACED AND ATTACH FITTINGS WERE LUB. SPRING TABS WERE RIGGED IAW MM. VISUAL AND OPS CHECKS WERE GOOD. TEST FLT WAS OK. AC RETURNED TO SERVICE. 2H72 4T RTA13NM 20031009000902003100900090SO 2003 10 9 SWIA200312412 120030913A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCONNECTED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07214SW 120280 FORWARD EMERGENCY LIGHT (INOPERATIVE). RECONNECTED BOTH POWER LEADS AT FORWARD (EXIT) SIGN. OPS CHECK GOOD. 2L72 4T RTA31SO 20031120000322003112000032NM 2003 11 20 AWXA200301241 120030922A531065C807351 CREASE BEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT CREASE BEAM UPPER SURFACE OF BOTTOM LEG BS 940-993, RBL 52, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED RT AFT CREASE BEAM BS 940-993, RBL 52 TO RBL 54, WL 208; INSTALLED A NEW REPLACEMENT CREASE BEAM IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031121000462003112100046NM 2003 11 21 SWAA032518 120031114A5554175A12057 FITTING BOEING737 7377H4 1384404NM RUDDER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED 5Y CHECK, FOUND RUDDER FITTING RIG PIN BOSS CRACKED AT BASE ON STAB RIB, STA 56.480. REPAIRED BOSS PER SWA EA. 2L72 4F RTA16WE 20040112002012004011200201NM 2004 1 12 2003UALA00959 120031215A5730 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT WING DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29171UA 24322 LEFT WING INBOARD L/E HAS 4 EACH INTERIM REPAIR DOUBLERS INSTALLED AT L/E STATIONS 330, 415, & 543. MAJOR REPAIR ACCOMPLISHED. PERMANENT FLUSH REPAIRS WERE ACP PER SRM 57-41-01. 2L74 4F4 FRTA20WE E24NE 20031124001192003112400119WP 2003 11 24 DHL2003802512 120031113A532047585141N FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 1.000, STA 1180 L-33R. REMOVED CRACK FITTING AT STA 1180.000, L-33R IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING AND FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125001292003112500129NM 2003 11 25 ASAA0310153 120030318A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 727B-947, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040115000502004011500050NM 2004 1 15 DL767031053 120031124A5512185T20031 SKIN BOEING767 767232 1385132NM HORIZ STAB GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27102DA 22214 DENT/GOUGE FOUND ON LOWER SURFACE OF LT HORIZONTAL STAB, FORWARD TORQUE BOX, INBD SKIN PANEL. DENT WAS DUE TO GROUND DAMAGE. REPAIRED PER ERA 423716-14. 2L72 4F RTA1NM 20031215001082003121500108NM 2003 12 15 AWXA200301470 120031106A53156546812815 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON SHIM AND UPPER SURFACE OF FLOORBEAM BS 1000.5, LBL 4, WL 208. MAINTENANCE REMOVED CORRODED SHIM AND FLOORBEAM FROM BS 986.50 TO BS 1006, LBL 4 TO LBL 18.32; FABRICATED A NEW REPLACEMENT SHIM AND FLOORBEAM PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12 & 13. 2L72 4F RTA16WE 20031216000662003121600066 2003 12 16 SWAA032561 420031120A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031222000182003122200018EA 2003 12 22 SWIA200312647 120031201A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07423SW5633 5633 7456 PULLING INTO GATE IN SLC THERE WAS A HOT BURNING ODOR FOLLOWED BY SMOKE COMING OUT OF GASPERS, FOLLOWED BY APU AUTO SHUTDOWN. REMOVED AND REPLACED APU WITH A SERVICEABLE UNIT PER CRJ MM 49-10-00. OPS AND LEAK CHECK GOOD. P/N: 3800488-3, S/N OFF: P-745, S/N ON: P184C. 2L72 4F RTA21EA 20031223000152003122300015NM 2003 12 23 SWAA032657 120031202A3350OL3071BPL5GPL LAMP BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW 16. RELAMPED PER MM. 2L72 4F A16WE 20031212001202003121200120NM 2003 12 12 SWAA032504 120031112A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 312, BL 0 TO LBL 17, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20031215001532003121500153WP 2003 12 15 AALA20031066 120030924A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21437AA 49455 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE ON THE PASSENGER SEATS. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030924000472003092400047 2003 9 24 DL75K030761 420030816A2564D806627 LIFE RAFT BOEING757 757232 1384965NM CABIN DEPLOYED A DALAK NONE O OTHER ININSP/MAINT 1 SO2767171 30839 DURING L/O SERVICE FOUND FORWARD 10 MAN LIFE RAFT PARTIALLY INFLATED IN STOW POSITION REPLACED SAME. 2L72 4F RTA2NM 20060801001052006080100105WP 2006 8 1 IXXA060556S 120030908A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK FOUND EXTERNAL FUSELAGE SKIN DENTED AT STATION FS 1350 LONGERON 29 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 51-1-0, 53-2-0, 53-2-1, 51-1-8, AND 51-1-11. 2L74 4F RT4A25 20060327001072006032700107SO 2006 3 27 MASA200300508 120031223A3020EETH503B PROBE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL TAT INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07840MJ 145429 CAE311759 ASH NR 2609 SDF-DCA - ABORTED TAKEOFF DUE TO A TAT HEAT NR 1 CAUTION MSG. MX REPLACED THE TAT PROBE. OP CHECKS GOOD. 2L72 4T4 FRTT00011ATTE6CH 20030813001372003081300137NM 2003 8 13 SWAA031750 120030806A3350BR2013 LIGHT BOEING737 7377H4 1384404NM FWD CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 EEPLS LOOSE IN FWD CABIN. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030815000782003081500078SW 2003 8 15 HEEA088480 120030519A6300 BEARING BELL 412 412 1182202SW M/R SUPPORT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 BEARING WORN. REPLACED ( 2 EACH) SUPPORT 204-001-330-005 DUE TO CORROSION; BEARING MS27646-45 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030818000562003081800056 2003 8 18 HEEA088521 420030724A2312066107800 RECEIVER BELL 412 412 1182202SW VHF NAV WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036559Z 36019 MARKER BEACON WILL NOT TEST. IN SHOP REPAIR. 1G72 4U H4SW 20030403000772003040300077NM 2003 4 3 CALA0300150 120030328A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND PASSENGER CABIN FLOORBEAM CORRODED AT BS 294.5, LBL 20 TO RBL 23. THE UPPER FLOORBEAM WAS REPLACED IAW SRM 53-10-51, FIGURE 205. 2L72 4F RTA16WE 20030403001202003040300120NM 2003 4 3 DL733030142 120030210A3350 LIGHT BOEING737 737347 1384647NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27312WA 23598 EMERGENCY EXIT LIGHTING INOP AT ROW 22 AND 25. REPLACED LIGHT SOCKET AT ROW 22 AND REATTACHED WIRES AT ROW 25. BOTH EMERGENCY EXIT LIGHTS NOW CHECK NORMAL. 2L72 4F RTA16WE 20030403001312003040300131NM 2003 4 3 DL738030136 120030209A4920 APU BOEING737 737832 13844CFNM APU BAY CONTAMINATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO273741S5232 P5846 30487 P5846 ON THE GROUND AT GATE IN MSP, DEICING FLUID WAS APPLIED TO TAIL SECTION WITHOUT PRIOR COORDINATION WITH FLIGHT CREW. SMOKE FILLED COCKPIT, STARTED TO FLOW INTO CABIN. PAX EVAC THROUGH 1L DOOR. SMOKE REM PROC FOLLOWED. DEICE FLUID INJESTED INTO APU INLET, CAUSED FUMES IN CABIN. RAN PACKS AT GATE AND CLEARED CABIN. ALL CHECKS NORMAL, AC OK FOR SERVICE. 2L72 4F RTA16WE 20030402000432003040200043NM 2003 4 2 2003UALA00320 120030324A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY DOOR BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29774UA 26936 EMERGENCY DOOR LIGHT AT DOOR 4R IS INOP RELAMPED 2L72 4F4 FRTT0001SE E46NE 20030404000212003040400021NM 2003 4 4 DHL2003742007 120030401A2611 BULB BOEING727 727225 1384077NM SMOKE TEST BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01742DH 21290 NR 2 SMOKE DETECTOR WILL NOT TEST. RELAMPED, OPS CHECKED OK IAW M/M 26-10-0. 2L73 4F A3WE 20030410002342003041000234EU 2003 4 10 BAQA085824 120030327A6330L633M2010103A003MOUNT UROCOPEC135 EC135T1 5620026EU TRANSMISSION LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03511ME255 0143 AIRCRAFT VIBRATION. MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030408001042003040800104EA 2003 4 8 03097667 120030407A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27667BR 7535 DURING MAINTENANCE INSPECTION, THE FWD EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030416002352003041600235NM 2003 4 16 CALA0300172 120030405A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 1INCH CRACK IN FLOOR SUPPORT AT STA 312-328, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E2GL 20030417000122003041700012EU 2003 4 17 MALA030117 120030121A3350 LIGHT BAC 146 AVRO146RJ85A1500097EU CABIN LOOSE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15501XJ E2208 EMERGENCY TRACK LIGHTING IN FORWARD CABIN TRACK COMING APART. MAINTENANCE RESECURED TRACK LIGHTING. ALL CHECKS GOOD. 2H74 4F RTA49EU 20030425000242003042500024EA 2003 4 25 SWIA200311853 120030324A2740 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07591SW 7079 AFTER LIFT OFF STAB TRIM CH 1 AND 2 FAILED AND MACH TRIM FAILED. UNABLE TO RESET IN FLIGHT. ABLE TO RESET AFTER LANDING. RETURNED TO PHX. PERFORMED ADJ/TEST OF HORIZONTAL STABILIZER CONTROL SYSTEM PER CANADAIR REGIONAL JET MM REF 27-41-00. NO DISCREPANCIES NOTED AT THIS TIME. 2L72 4F RTA21EA 20030428000472003042800047NM 2003 4 28 OZIA200341001 120030117A5320001A534C4061338 FLOOR SUPPORT DORNERDO32 DO328300 NM PWA 306 PW306B NE FUSELAGE CORRODED A OZIAK NONE O OTHER ININSP/MAINT 1 CE05410Z 7126 3125 FORWARD SIDE OF LAVATORY FLOOR SUPPORT (FRAME 35) CORRODED. 2H72 4T4 FRTA55NM E35NE 20030428001692003042800169WP 2003 4 28 03FDEA00410 120030408A5410 FRAME DOUG DC10 DC1030 3023501WP RT PYLON GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25317FE 46835 RIGHT PYLON UPPER PANEL 487EL, INNER FRAME GOUGED AND PREVIOUS REPAIR AND L/E CRACKED. CLOSING ACTION ON 04/07/03. REMOVED FRAME IAW SRM 51-35-01. FAB NEW FRAME WITH TRAVEER T2/324411. INSTALLED NEW FRAME IAW SRM 51-31-01 AND SRM 51-31-01. 2L73 4F A22WE 20030429000132003042900013NM 2003 4 29 P5CA0300800 120030129A5310 STRUCTURE BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 UPPER LOBE DECK CRACK ON F/S 520 RT BETWEEN STR 7 TO 10A. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH SEGMENT AND SPLICE STRAP. 2L74 4F A20WE 20030430000252003043000025NM 2003 4 30 AWXA200300444 120030414A532065524577 PAN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON DRIP PAN ASSEMBLY AT BS 1016, RBL 8. MAINTENANCE STOP DRILLED CRACK AT BS 1016, RBL 8; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 51-40-2, FIG. 1. 2L72 4F RTA16WE 20030429002182003042900218WP 2003 4 29 03FDEA00436 120030307A5743 FITTING DOUG DC10 DC1010 3022110WP MLG DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 COMPLY WITH EA 8-5740-68748 WINGS-MLG ATTACH FITTING OVERSIZED HOLE REPAIR FACT 13MAR03 18:11 COMPLIED WITH EA 8-5740-68748 WING -MLG ATTACH FITTING OVERSIZED HOLE REPAIR (RIGHT SIDE) BUSHING FABBED ON MAE TRAVELER T2/31970. INSTALLED BUSHING IAW SRM 57-20-00 & EA 8-5740-68748 AT MAE/BFM. 2L73 4F A22WE 20030502000022003050200002EA 2003 5 2 ASOA03121 120030320A5210CC670386011 DOOR CNDAIRCL600 CL6002C10 1390015EA FUSELAGE STUCK A ASOAK NONE O OTHER ININSP/MAINT 1 SO11707EV 10057 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND TO BE STUCK CLOSED. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR SEVERAL TIMES BUT COULD NOT DUPLICATE THE PROBLEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030502001492003050200149 2003 5 2 372PA0022 420030411A2230735SUE912 COMPUTER BOEING737 737306 13844BGNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05372PA 23546 AUTO THROTTLE WILL NOT ARM. DEFERRED PER MEL 22-4. 4/15/2003: REMOVED AND REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-10 AND PERFORMED BITE AND INTERFACE TEST. TEST NORMAL. 2L72 4F RTA16NE 20030502002512003050200251NM 2003 5 2 03FDEA00588 120030421A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK CRACKED AT STA 635 LBL 8.5 BETWEEN FLOOR PANELS 233FF AND 233EF. CABIN STA 635 TO STA 655 LBL 8.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG.1, VOL.1. 2L73 4F RTA22WE 20030502001502003050200150WP 2003 5 2 GTIA030144 120030220A5310 SHEAR TIE DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 AFT CARGO FS 1250 SHEAR TIE CRACKED STR 28R. REMOVED CRACKED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED REPAIR PARTS. 2L72 4F4 FRTA6WE E2EA 20030506000162003050600016NE 2003 5 6 MALA030242 220030422A7261 CHIP DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE CONTAMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15445XJ 340B445 LT CHIP DETECT LIGHT CAME ON INTERMITTENTLY AFTER DEPARTURE ON FLIGHT 2798. ABOUT 5 MINUTES INTO FLIGHT, LIGHT CAME ON STEADY. ALL ENGINE PARAMETERS FOR LT ENGINE REMAINED NORMAL. AIR RETURN TO DTW. MAINTENANCE INSPECTED LT ENGINE CHIP DETECTOR FOUND SMALL PARTICLE OF CARBON. CLEANED DETECTOR AND RAN ENGINE FOR SEVERAL MINUTES. ALL CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW SF340 AMM AND GE CT7MM. 2L72 4T4 TRTA52EU E8NE 20030505002522003050500252NM 2003 5 5 CALA0300205 120030421A3350252005 FUSE BOEING737 737524 1384721NM BATTERY PACK BLOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2717620 27333 INSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE AT ROW 1AB TO 3AB. THE BATTERY PACK FUSE WAS FOUND AT FAULT. THE FUSE WAS REPLACED AND OPERATION OF THE EMERGENCY AISLE PATH LIGHTS CHECKED GOOD. 2L72 4F RTA16WE 20030507000292003050700029NM 2003 5 7 AUS20030332 120030315A7830 BLOCKER DOOR BOEING747 747438 NM RROYCERB211 RB211* 54555NE THRUST REVERSER DAMAGED W O OTHER E VIBRATION/BUFFET LDLANDING 1 AUS (AUS) NR 2 ENGINE THRUST REVERSER DAMAGED. INSPECTION FOUND THREE BLOCKER DOORS AT THE 8 O'CLOCK AND 9 O'CLOCK POSITIONS DAMAGED OR MISSING AND THE SHROUD ON THE PIPE CLUSTER AT THE 6 O'CLOCK POSITION MISSING. 2L74 4F4 FRTA20WE A12EU 20030508001302003050800130NM 2003 5 8 UPS03440625 120030413A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C M/D - SEAT TRACK O/B FLANGE LOWER SURFACE CORROSION. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 16. CORROSION BLEND OUT 0.050 X 1 X 1.5 INCH. EXCEED SRM LIMIT. 2L74 4F A20WE 20030509001202003050900120EU 2003 5 9 I05R086280 120030425A5320L262M1805205 BRACKET UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE FIRE BOTTLE CRACKED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05551BA880 188 SUPPORT FOUND CRACKED DURING INSPECTION. REPLACED SUPPORT WITH NEW. 1G72 3U3 UO H88EU E42NE 20030513000542003051300054EA 2003 5 13 ASOA03128 120030323A3397487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGNECY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 FLT 4753 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE EMERGENCY FLOOR LIGHTS FROM ROW 8 TO THE BACK OF THE CBIN WERE INOPERATIVE. MAINTENANCE RESECURED FLOOR LIGHT STRIP CONNECTORS AT ROW 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514002262003051400226WP 2003 5 14 03FDEA00726 120030512A5310 DOOR FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 NR 200 RT PATIO DOOR NR 10 FRAME CRACKED AS MARKED. STOPPED DRILL CRACK IAW MD-10 SRM 53-30-00. FAB ANGLE REPAIR IAW MAE TRAVLER T2/333232. LOCATED AND DRILLED ANGLE IAW MD-10 SRM 53-30-00, INSTALLED ANGLE REPAIR IAW SRM 51-31-01, 51-33-01. 2L73 4F A22WE 20030604001082003060400108NM 2003 6 4 UPS03440523 120030412A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 1570 - 1580, STR 16L STRINGER END AREA FOUND CRACK. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20030602001302003060200130NM 2003 6 2 SWAA031168 120030524A53126516300 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AT RBL 10.5. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F A16WE 20030605000902003060500090NM 2003 6 5 UPS03240684 120030410A5350 FRAME BOEING727 72722C 138400FNM W/B FAIRING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, BODY FAIRING NR 3430, HAS CORRODED FRAME AFT OF GND. COOLING FAN DOOR CUT OUT. FRAME REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06 OUT OF LIMITS IAW SRM 51-10-01. NEW FRAME FABRICATED IAW SRM 51-20- 1 FIG 7. NEW FRAME INSTALLED IAW SRM 51-30-2 2L73 4F A3WE 20030609001462003060900146SO 2003 6 9 SWIA200312003 120030514A3260 UPLOCK SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE MLG MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07209SW 120269 UPON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. SYSTEM A & B SHOWED DISAGREEMENT, WITH THE EXCEPTION OF SYSTEM A, LEFT MAIN GEAR. RAN QRH, NO RESULTS, CYCLED GEAR, NO RESULTS, PULLED & RESET LANDING GEAR CB, GEAR RETRACTED.REMOVED AND REPLACED ''A'' UPLOCK PROX SENSOR ON LEFT MAIN GEAR IAW MM 32-61-01. OPERATIONAL CHECK OF GEAR SWING, GOOD. 2L72 4T4 TRTA31SO E20NE 20030515000492003051500049WP 2003 5 15 ZW0A0304702 120030508A3350408822101 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139402W 53138 THE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 9-4-02 STL. 2L72 4F RTA6WE 20030515001102003051500110NM 2003 5 15 CH1A200395052 120030425A5313 STRINGER BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 STRINGER 30 AND SURROUNDING STRUCTURE IS CORRODED AT BS 1148. 2L73 4F A3WE 20030611001082003061100108EU 2003 6 11 HEEA086712 120030521A642010531821 BEARING BOLKMS105 BO105S 5626006EU CONTROL ROD ASSYWORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 CONTROL ROD HAS WORN BEARINGS. REPLACED 2 EACH 116488P BEARINGS DUE TO WORN; 2 EACH 11-3943P BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030617000522003061700052CE 2003 6 17 CA030529002 120030522A5610 WINDSHIELD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA COCKPIT FRACTURED W B EMER. DESCENT O OTHER CRCRUISE 1 CA (CAN) IN CRUISE AT 24,000 FT ALTITUDE WITH 5.8 PSI PRESSURIZATION AND CLEAR CONDITIONS (OAT -25C) AND THE WINDSHIELD HEAT ON, THE LT WINDSHIELD SUDDENLY CRACKED. THE INNER PLY IN ITS TOTALITY FRACTURED IN MINI PARTICLE 1/4 INCH DIAMETER. NO PRES SURIZATION WAS LOST. EMERGENCY DESCENT WAS CARRIED OUT TO NEAREST AIRPORT WITH AN UNEVENTFUL LANDING. 1L72 4T4 T A24CE E4EA 20030617003342003061700334SW 2003 6 17 HEEA087045 120030604A6220406312103101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR LINK WORN. 1G71 3U O H2SW 20030521001442003052100144EU 2003 5 21 MALA030260 120030504A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING C1 INSPECTION IN CWA, RT CARGO FRAME AT STA 649 HAS SEVERAL HOLES IN FLANGE FROM SL1608-1620. MAINTENANCE COMPLETED REPAIR IAW EO 53152. A/C RELEASE DATE 5/6/03. 2L72 4T RTA52EU 20030523000052003052300005NM 2003 5 23 2003F00289 120030119A5320 SUPPORT BOEING727 727222 1384073NM FUSELAGE CORRODED A UG8AO OTHER O OTHER NRNOT REPORTED 1 CE077643U 20037 AT C-CHECK, FOUND CORROSION IN E/E BAY, FUSELAGE STATION 328, RBL 50, FLOOR SUPPORT. REMOVED CORROSION AT FUSELAGE STATOIN 328 RBL 50 PER B727 SRM 51-10-06. FOUND TO BE OUT OF LIMITS. FABRICATE FILLER AND TWO ANGLES PER B727 SRM 53-10-8. TREATED AND PRIMED, AND INSTALLED PARTS. (M) 2L73 4F A3WE 20030620000562003062000056EA 2003 6 20 ASOA03228 120030520A3230750006000 VALVE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11849AS 7347 DURING APPROACH INTO ATL FROM LFT, A GEAR DISAGREEMENT WARNING MESSAGE WAS RECEIVED. THE CREW COMPLIED WITH QRH PROCEDURES, PERFORMED A GO AROUND AND CYCLED THE GEARS. THREE GREEN LIGHTS WERE RECEIVED INDICATING THE LANDING GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR SELECTOR VALVE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030620000082003062000008SW 2003 6 20 HEEA086935 120030603A3220206020110103 STRUCTURE BELL 407 407 1182206SW TAIL SKID BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 TAIL SKID ASSY BROKEN. TO BE SENT TO MFG. 1G71 3U O H2SW 20030702000132003070200013NE 2003 7 2 TSAA0377105 220030616A7250 LINE BOEING737 737230 1384401NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE LEAKING A TSAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP13820AL 22138 DURING TAKEOFF ROLL, UNABLE TO ACHIEVE TAKEOFF POWER ON ENGINE NR 2, FIREWALL ONLY GAVE 1.86 EPR. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND A LEAK IN THE TURBINE EXHAUST LINE, REPLACED THE PT7 TUBE ASSY IAW MM 77-00. LEAK CHECK OF LINE OK. JETCAL ACCOMPLISHED IAW FORM M-215. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTA16WE E2EA 20030718000022003071800002EU 2003 7 18 USAASA03062 120030611A3350 BATTERY PACK AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAO OTHER O OTHER CLCLIMB 1 EA19182UW 1536 EN ROUTE MCO-PHL, THE FLOOR LEVEL EMERGENCY LIGHTING AND EXT SIGN LIGHTING TURNED ON AND OFF EVERY 15 SECONDS IN FLIGHT. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT (11WL) AND A BATTERY PACK. (M) 2L72 4F RTA28NM 20030714001062003071400106CE 2003 7 14 GLBA2003097 120030630A760011438903921 ACTUATOR BEECH 1900 1900D 1154162CE RT ENGINE MALFUNCTIONED A GLBAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 NM03208GL14482 UE208 RIGHT ENG WILL NOT MAKE T/O POWER. REMOVED AND REPLACED RT ENG ACTUATOR. 2L72 4T RTA24CE 20030717000552003071700055SW 2003 7 17 HEEA088031 120030613A7931301755S CONNECTOR BELL 222 222U 1182140SW NR 2 ENGINE LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 NR 2 ENGINE OIL PRESSURE DROPPED TO ZERO IN FLIGHT. MAINTENANCE FOUND A PIN BACKED OUT OF CONNECTOR TO OIL PRESSURE TRANSMITTER. 1G72 3U H9SW 20030707001252003070700125NM 2003 7 7 CALA0300337 120030626A521065554786 GATE BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE L2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717644 28905 INSPECTION FOUND A 0.33 INCH CRACK IN LOWER GATE OF L-2 DOOR. THE CRACK WAS LOCATED AT AFT CORNER FROM AFT MOST RIVET TOWARDS HINGE. INSTALLED HINGE AND SEALED RETAINERS ON NEW GATE IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20030709000512003070900051WP 2003 7 9 GTIA030437 120030515A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP COCKPIT DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FLIGHT COMPARTMENT OBSERVER SEAT FLOOR PANEL DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20030710001212003071000121EU 2003 7 10 03168305 120030617A3397FU248 FUSE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT FAILED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27305UE 41019 DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FUSE AND REPAIRED WIRING TO AFT EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030710001172003071000117WP 2003 7 10 MWEA030246 120030618A5310SRO95200089 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 MID CARGO DOOR JAMB HAS SEVERAL SPOTS OF LITE CORROSION AROUND FASTENER HOLES ON DOUBLER BETWEEN STATION 645-685. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030113000932003011300093NM 2003 1 13 QXEA0300039 120030110A33506138001 BATTERY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX542 4055 PDX-EMERGENCY EXIT SIGN JUST AFT OF RIGHT HAND FORWARD EMERGENCY EXIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK HOUSING AT POSITION TWO AND BOTH EMERGENCY BATTERIES, ALSO FOUND CONNECTOR TO EMERGENCY EXIT SIGN DISCONNECTED, RECONNECTED CONNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030103000672003010300067SO 2003 1 3 RAIA00301002 120030102A324221582 BRAKE ASSY EMB 145 EMB145 3260210SO DRAGGING A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03801HK6074 416 145053 5282-PIT- LEFT BRAKE FELT LIKE IT WAS DRAGGING WITH INCREASING LEFT OUT-BOARD TEMPERATURE RISING. MAINTENANCE REMOVED AND REPLACED THE LEFT OUT-BOARD BRAKE, LK AND OPS CK OK. 2L72 4F RTT00011AT 20030128000222003012800022SW 2003 1 28 HEEA083774 120030115A7714 BEARING BELL 407 407 1182206SW PMA FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 FADEC FAULT IN FLIGHT. FOUND PMA SHAFT SHEARED DUE TO FAILED BEARING IN PMA. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030129000472003012900047SW 2003 1 29 HEEA083960 120030117A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 MAIN ROTOR BLADE HAS SEPARATION ON BOTTOM OF BLADE. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030203000752003020300075SW 2003 2 3 AC2A084073 120030128A6321222080060001 CYLINDER BELL 430 430 1182150SW ROTOR BRAKE DEFECTIVE H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CM981 49090 ROTOR BRAKE CYLINDER WEAK AT TIMES. REPLACED ROTOR BRAKE CYLINDER. 1G72 3U RTH9SW 20031229001602003122900160EA 2003 12 29 SWIA200312665 120031205A7120 BEAM CNDAIRCL600 CL6002B19 1900309EA RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 ENGINE SUPPORT BEAM LOWER WEB RIGHT SIDE RBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'', RII 53-401. 2L72 4F RTA21EA 20031223001492003122300149CE 2003 12 23 DXTA200300185 120031123A2710666000162 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07692QS 5605092 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20040106001512004010600151NM 2004 1 6 UPS03241668 120031218A3350 LIGHT BOEING727 727108C 1384039NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:PFLT CABIN DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED CABIN DOOR, EMERGENCY EXIT LIGHT OPS CHECKS NORMAL AT THIS TIME PER MM 33-50. 2L73 4F A3WE 20040105000412004010500041EA 2004 1 5 QXEA200301563 120031215A3620GG670800053 SENSOR CNDAIRCL600 CL6002C10 1390015EA BLEED AIR SYS MALFUNCTIONED A QXEAO OTHER N FALSE WARNING DEDESCENT 1 NM09601QX2531 2531 10009 PDX- ON FLIGHT 2520 RIGHT PACK CAUTION MESSAGE DURING DESCENT. SHUT OFF PACK PER ABNORMAL CHECKLIST AND CAUTION MESSAGE WENT AWAY. REMOVED AND REPLACED RIGHT BLEED TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031021001482003102100148NM 2003 10 21 AALA20030565 120030513A3397 WIRE BOEING757 757223 1384957NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21194AA 32388 LAX - DURING OVERNIGHT MAINTENANCE, OVERHEAD BIN BULKNOSE TRIM EMERGENCY EXIT LIGHTS AT 20DEF AND 24DEF INOPERATIVE. REPAIRED OVERHEAD BIN BULKNOSE TRIM EMERGENCY EXIT LIGHTS WIRES AT 24DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040112000122004011200012EU 2004 1 12 USAASB03206 220031123A7200 ENGINE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 1 FAILED A USAAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA19385US 22958 720671 CLIMBING THROUGH 16,000 FT OUT OF BOS, EN ROUTE TO DCA, THE NR 1 ENGINE EXPERIENCED A LOUD BANG. THE AIRCRAFT STARTED TRACKING TO THE LT. CREW DETERMINED NO THRUST WAS BEING PRODUCED FROM THE NR 1 ENGINE, SO THEY FOLLOWED CHECKLIST AND SHUTDOWN THE NR 1 ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO PVD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THE NR 1 ENGINE SUSTAINED A HOT SECTION FAILURE AS METAL WAS FOUND IN THE TAILPIPE. REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY PER JOB CARD J371-00-01. OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F4 FRTA16WE E21EU 20031202000062003120200006NM 2003 12 2 ASAA0310465 120030515A53206545800 ANGLE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND ANGLE AT FUSELAGE STATION 348-360, STRINGER 27R CORRODED. REPLACED ANGLE PER EA. (M) 2L72 4F A16WE 20031204000412003120400041WP 2003 12 4 AALA20031081 120030927A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21470AA 49600 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 18 THROUGH 20. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040123000492004012300049EU 2004 1 23 KBM2003F00109 120031130A6730123668P BALL JOINT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE FWD AFT SERVO WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 FOUND FORWARD AFT SERVO LOWER BEARING WORN. REPLACE WITH NEW BEARING. 1G71 3U3 UNCH9EU E19EU 20040121000372004012100037NM 2004 1 21 03FDEA02310 120031227A5753ARC74821 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING INBOARD FLAP VANE OUTBOARD SUPPORT FITTING INBD & OUTBOARD MOUNT HOLES WORN. COMPLIED WITH FEDEX EA 1-5750-75206 TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT INBOARD. FLAP VANE ATTACH FITTING REWORK. 2L73 4F RTA22WE 20031209002732003120900273NM 2003 12 9 03FDEA01886 120031107A5310 FAILSAFE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CRACKED FAILSAFE CHORD, BS 804 AT STR 14L. 2L73 4F RTA3WE 20031209001192003120900119NM 2003 12 9 QXEA200301358 120031030A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM ZONE 800 NOT CLOSED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09406QX 4048 ON FLIGHT 2384 DURING CLIMBOUT OF SEA, FUSELAGE DOOR WARNING ILLUMINATED, SHOWING AFT BAGGAGE DOOR UNSECURE. RETURNED TO SEA WITH NORMAL PRESSURIZATION ON LANDING. FOUND AFT BAGGAGE DOOR HANDLE OPEN. CLOSED AFT BAGGAGE DOOR HANDLE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031210001232003121000123EU 2003 12 10 QXEA200301486 320031201A6140 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM ROTOL R408 CR4086123F17EU COCKPIT MALFUNCTIONED A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09400QX 4030 GEG- ON FLIGHT 2359 DURING AUTOFEATHER TEST, NR 1 ENGINE SHOWED FAILED MESSAGE. POWER DOWN AND BACK UP. PERFORMED AUTOFEATHER TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP17BO 20030919001222003091900122EU 2003 9 19 XNOA01144 120030818A2611 FILTER AIRBUS300 A300B4203 3930306EU SMOKE DETECTOR CLOGGED A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23372PC 196 LOOP A MID 1 MAIN DECK COMPT. SMOKE DET. LIGHT CAME ON DURING TAXI (REPEAT). FOUND FILTER SCREEN TO MID 1 MAIN DECK SMOKE DETECTOR CLOGGED. CLEANED SCREEN. SMOKE DETECTOR SYST. TESTS NORMAL IAW MM 26-19-00. 2L72 4F RTA35EU 20040128001082004012800108SO 2004 1 28 SWIA200312702 120031209A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM07190SW4084 4084 120050 ON DESCENT INTO SGU- LOW SPEED ALARM WENT OFF AND WOULD NOT STOP DESPITE NO ICING CONDITIONS AND ONLY STANDARD ICE ON. LANDED IN SGU WITHOUT INCIDENT AND WHEN THE ALARM STOPPED, THE SMOKE STOPPED. REMOVED AND REPLACED FLAP SELECTOR PANEL IAW MM 27-50-01. S/N OFF: 120131, OPS CHECK GOOD IAW MM 27-50-00. REPLACED LOW SPEED ALARM PANEL IAW MM 30-90-01. LOW SPEED ALARM OPS CHECK GOOD IAW MM 30-90-00. P/N: 120-64199-001, S/N ON: 1209998612, S/N OFF: 1209994742. 2L72 4T RTA31SO 20031212000302003121200030NM 2003 12 12 SWAA032426 120031103A3350101114 LENS BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 RT OVERWING EXIT EMERGENCY EXIT LIGHT LENS LOOSE. REINSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20031219000442003121900044 2003 12 19 SWAA032604 420031126A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031219000692003121900069NM 2003 12 19 CALA0300703 120031208A2560ACREM1A MEGAPHONE BOEING737 737724 13844BYNM EMERGENCY EQUIP INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2754711 28782 THE FORWARD CABIN MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-64-00. 2L72 4F RTA16WE 20031219001352003121900135NM 2003 12 19 03FDEA02116 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001492003121900149NM 2003 12 19 03FDEA02134 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNT BOLT HOLE SPOT FACE CORRODED. 2L73 4F RTA22WE 20031222000322003122200032NM 2003 12 22 F3LA200300163 120031205A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 328, RBL 49. REMOVED SECTION OF FLOORBEAM AND INSTALLED NEW UPPER CAP END REPAIR AND SPLICES PER EA 03-531-10225. 2L72 4F RTA16WE 20031222001142003122200114EU 2003 12 22 A6WA200360051 120031004A5330 SKIN BAG BAE146BAE146200A 1500266EU FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 FOUND DENTS FORWARD OF CARGO DOOR. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX CAX 1683-6810007. (M) 2H74 4F RTA49EU 20031229001282003122900128EA 2003 12 29 MASA200300480 120031207A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777286 7286 CREW REPORTED ORANGE SECTION OF FLOOR STRIP LIGHTS INOP. MX REPLACED POWER SUPPLY. 2L72 4F RTA21EA 20040105000262004010500026NM 2004 1 5 AALA20031439 120031216A3350 SPRING BOEING767 767223 1385123NM LIGHT GUARD MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21323AA 22324 SPRING FELL OFF OF OVERHEAD EMERGENCY LIGHT SWITCH GUARD. REPLACED OVERHEAD PANEL FOR THE EMERGENCY LIGHT SWITCH GUARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20030917001372003091700137NM 2003 9 17 DL767030701 120030729A2742251T43101 ACTUATOR BOEING767 767232 1385132NM HORIZONTAL STAB BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27105DA 22217 DURING A LUBE VISIT (1T188), AN AMT FOUND THE LOWER ICE SCRAPER RING FROM THE STAB TRIM ACTUATOR BALL NUT BENT AND OUT OF PLACE. IT WAS FOUND AT THE BOTTOM OF THE BALLSCREW. THE ACTUATOR PART NUMBER IS 251T4310-1. THE PART NUMBER OF THE SCRAPER IS B18834-7R. REPLACED SAME 2L72 4F RTA1NM 20030918001462003091800146WP 2003 9 18 03FDEA01207 120030803A5320AZZ74653 TRACK DOUG DC10 DC1030 3023501WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 N 462 CROSSTRACK ASSY CRACKED AT STA 969 LBL 27-47 MCD. REPLACED CROSSTRACK ASSY AND INSTALLED IAW W/C 25C5510-01 @ MAE. 2L73 4F A22WE 20040106001212004010600121CE 2004 1 6 DXTA200300201 120031216A2710666000161TO64 CONTROL CABLE CESSNA560 560XL 2076702CE AILERON FRAYED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07621QS 5605280 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED AGAINST WING ACCESS COVE ASSEMBLY, FOUND ALL FOUR CABLES FRAYED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031124000132003112400013EA 2003 11 24 SWIA200312600 120031116A27507455001 LEVER CNDAIRCL600 CL6002B19 1900309EA FLAP CONTROL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07407SW3044 3037 7034 AFTER LANDING, WHEN SELECTING FLAPS FROM 45 DEGREES TO 30 DEGREES, FLAPS STAYED AT 30 DEGREES AND ECI SHOWED A FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED FLAP CONTROL LEVER IAW MM 27-51-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20031202001492003120200149NM 2003 12 2 MEX2003502 120031023A2913AS66411LS666 PUMP DOUG MD88 MD88 3023688NM HYD SYSTEM FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23162PL 49765 AIRCRAFT RETURNED TO BLOCK, AFTER ENGINES START WITH LEFT HYDRAULIC PRESSURE PUMP ON HIGH INDICATED PRESSURE WAS ON 1100 WITH LEFT HYDRAULIC PRESSURE IN LOW. LEFT HYDRAULIC PRESSURE PUMP WAS REPLACED IAW MM 29-10-06, TESTS CORRECT. DURING OVERNIGHT SERVICE LEFT HYDRAULIC PRESSURE PUMP WAS TESTED IAW MM 29-10-06, ALL CORRECT. (M) 2L72 4F RTA6WE 20040114001772004011400177SO 2004 1 14 MASA200300413 120031016A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07841MJ 145448 ASH NR 2666. PIT AFT CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MECHANIC REPLACED LIGHT. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040114001882004011400188SO 2004 1 14 MASA200300444 120031108A2560P2070009120 MOUNT EMB 145 EMB145LR 3260212SO FLASHLIGHT BROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW07828MJ 145218 ASH NR 2690 CLT. CREW REPORTED FORWARD EMERGENCY FLASHLIGHT CRADLE BROKEN. MECHANIC REPLACED ASSEMBLY. 2L72 4T RTT00011AT 20030218001982003021800198NM 2003 2 18 SWAA030335 120030211A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) ABOVE STR 4R, AT BS 747, BS 755, BS 767 AND BS 775. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030219001312003021900131NM 2003 2 19 SWAA030356 120030213A3397 WIRE BOEING737 7373H4 1384600NM COCKPIT BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND COCKPIT OVERHEAD EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE L-4 TO M1219 MODULE PER MM. 2L72 4F RTA16WE 20030116000072003011600007GL 2003 1 16 ERAA082949 220030106A7321 FILTER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL FUEL CONTROL CLOGGED H ERAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 FS01 9273 328017 FUEL CONTROL FLAMED OUT ENGINE AT IDLE. NO FUEL FLOW FROM NOZZLE OUTLET FUEL CIRCUIT FOUND CONTAMINATED. INLET FILTER PLUGGED. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-602E. 1G72 3U3 U H3EU E4CE 20030116002752003011600275SW 2003 1 16 HEEA083136 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 MAIN ROTOR FLAP RESTRAINT STICKING IN DOWN POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030117000062003011700006SW 2003 1 17 HEEA083151 120030108A5302206020113163 STABILIZER BELL 206 206L3 1182108SW TAIL BOOM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 TAIL BOOM FIN ASSY HAS CORROSION. 1G71 3U H2SW 20030221000482003022100048NM 2003 2 21 AWXA200300075 120030125A3350BR964411 LIGHT BOEING757 7572S7 1384962NM SEAT ROW 25 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28904AW 23566 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 25 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 25 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030224000682003022400068EU 2003 2 24 HEEA084189 120030213A71000292217030 DISTRIBUTOR AEROSPAS355 AS355* EU FUEL SYSTEM CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03971AE 3230 CARBON BUILD UP IN FUEL DISTRIBUTOR CAUSING ENGINE NOT TO START DUE TO COMPRESSOR WOULD NOT TURN. 1G72 3U H11EU 20030625001022003062500102NM 2003 6 25 SQ7A242003 120030224A7312320115 VALVE BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE INOPERATIVE A SQ7AE ENGINE SHUTDOWN O OTHER CRCRUISE 1 SO01282US 21161 700126 AT CURISE NR 1 ENGINE FUEL HEAT VALVE STUCK OPEN, ACCOMPLISHED ABNORMAL PROCEDURE 1-314-3, OIL TEMP REMIANED IN YELLOW BAND, ACCOMPLISHED ABNORMAL PROCEDURE 1-314-4, SHUT DOWN #1 ENGINE AS PERCAUTION. ADVISED ATC LANDING CVG UNEVENTFUL. 2L73 4F4 F A3WE E2EA 20030226000452003022600045SW 2003 2 26 HEEA084334 120030211A7722407375001105 INDICATOR BELL 407 407 1182206SW MGT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 MGT INDICATOR GOES TO ZERO IN FLIGHT. 1G71 3U O H2SW 20030227000272003022700027 2003 2 27 HEEA084371 420030211A344280510800001 CONTROL BOX BELL 407 407 1182206SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 CONTROL BOX DATA FAIL DISPLAYED ON INDICATOR. 1G71 3U O H2SW 20030227001182003022700118SW 2003 2 27 HEEA084424 120030212A6310222044006109A COUPLING BELL 230 230 1182149SW MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RC2482 23037 COUPLING LEAKING GREASE. REPLACED OUTER COUPLING DUE TO PITTING IN RETAINER GROOVE. REPAIRED. 1G72 3U NCH9SW 20030228000932003022800093SW 2003 2 28 HEEA084457 120030213A6340206075681105 INDICATOR BELL 206 206L3 1182108SW DUAL TACH MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 DUAL TACH INDICATOR NEEDLE HANGS UP. 1G71 3U H2SW 20030305000522003030500052 2003 3 5 HEEA084636 420030214A3452066107100 TRANSPONDER BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 TRANSPONDER CAUSES TCAS TO DISPLAY ITSELF (NO SUPPRESSION PULSE). CLEANED CORROSION FROM UNIT. REPLACED WASHER AND 3 INSULATORS. BENCH CHECK GOOD. 1G72 4U H4SW 20030121002072003012100207SW 2003 1 21 HEEA083351 120030109A243232007001 BATTERY BELL 206 206L1 1182107SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03406EH 45183 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030316000042003031600004EU 2003 3 16 RAIA00303061 120030304A30607826874 BRUSH BLOCK AEROSPATR42 ATR42300 8680920EU WORN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03426TE 228 5639-STL- RIGHT PROPELLER ANTI-ICE FAILED. MAINTENANCE REMOVED AND REPLACED RIGHT PROPELLER BRUSH BLOCK, OPS CK OK. 2H72 4T RTA53EU 20030317001392003031700139NM 2003 3 17 03FDEA00303 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 660, BETWEEN STR 24L AND 25L. 2L73 4F RTA3WE 20030318001132003031800113NM 2003 3 18 BJNA030213 120030214A5320CORRODED SPLICE BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A STRINGER SPLICE LOCATED ON STRINGER 22 LEFT AT STATION 727-727A. REMOVED THE CORRODED STRINGER SPLICE, FABRICATE AND INSTALLED REPLACEMENT PARTS IAW BOEING SRM 51-20-1 FIGURE 7, PATE 18 AND 51-30-2 FIGURE 11, PAGE 39. (M) 2L72 4F RTA16WE 20030321000042003032100004NM 2003 3 21 SWAA030625 120030318A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 10R. REPAIRED SKIN PER SWA RA. 2L72 4F RTA16WE 20030327000282003032700028NE 2003 3 27 AWXA200300300 220030322A7200 ENGINE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 2 OUT OF TRIM A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28182AW 22649 ON TAKEOFF AT PHX EN ROUTE FOR ONT WHEN SELECTING TAKEOFF POWER, TAKEOFF POWER WAS SET TO 2.11 EPR AND THE NR 2 ENGINE ONLY CAME UP TO 1.59 EPR. FURTHER ADVANCEMENT OF THROTTLE DID NOT VARY 1.99 EPR , REJECTED TAKEOFF. MAINTENANCE PERFORMED ENGINE TRIM RUNS PER AMM 71-00, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2EA 20030324001022003032400102NM 2003 3 24 AWXA200300093 120030128A533065757783 SKIN BOEING737 737300 1384610NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK A 3/4 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 867, BETWEEN STR 18-19 RT. MAINTENANCE CUTOUT DAMAGED SECTION OF FUSELAGE SKIN AT BS 867, BETWEEN STR 18-19 RT AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5361-03030-ES1. 2L72 4F RTA16WE 20030625001372003062500137NM 2003 6 25 03FDEA00348 120030325A5753ARC41251 FITTING DOUG MD11 MD11 3023602NM O/B FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 LT OB FLAP TRACK FITTING IS CRACKED AT THE UP STOP MOUNT BARREL NUT HOLE. REPAIRED PER EA 1-5750-67543. THIS EA REMOVES THE 3D0011 BARREL NUT ASSY. AND NAS578-8B RETAINER AND INSTALLS A ZERO CLEARANCE FIT PLUG IN PLACE OF THE REMOVED PARTS AND PROVIDES FOR REPETITIVE INSPECTIONS UNTIL REPLACED WITH A NEW PART WHEN AVAILABLE FROM BOEING.. 2L73 4F RTA22WE 20030326000872003032600087NM 2003 3 26 2003UALA00287 120030314A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT CABIN FUSELAGE FRAME AT BS 1360, HOLE 3.5 INCHES TO THE RIGHT OF STRINGER 1. AFT SIDE OF FRAME HAS TOOLING MARK OR MISDRILLED SURROUNDING AREA OF HOLE. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR DONE ON AREA. 2L72 4F4 FRTA2NM E17NE 20030418000252003041800025NM 2003 4 18 VNAA0302010 120030211A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PASSENGER DOOR FAILED A VNAAO OTHER N FALSE WARNING CLCLIMB 1 GL07463PS 3087 THE CREW RECEIVED A MAIN CABIN OPEN LIGHT ON THE RED WARNING PANEL AND RETURNED TO PIT. MAINTENANCE INSPECTED AND ADJUSTED THE OTHER THE CENTER PROXY SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421000682003042100068SO 2003 4 21 SWIA200311817 120030228A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07566SW 120341 CENTER EMERGENCY LIGHTS DO NOT TURN ON. FOUND BROKEN WIRE ON EMERGENCY LIGHT FLOOR TRACK. REPAIRED BROKEN WIRE IAW EMB120 WM 20-00-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030721001372003072100137NM 2003 7 21 SWAA031450 120030630A5520BACB28AKM07 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C4 CHECK, SWA SI 11138-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER MM. 2L72 4F RTA16WE 20030422000042003042200004EU 2003 4 22 USAABA03004 120030223A3350321440 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 PHL - FOUND THE R2 AND R3 DOOR EPSU'S FAULTING. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20030422000532003042200053EA 2003 4 22 ASOA03103 120030311A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA FAILED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11880AS 7606 FLT 4400 - DURING DESCENT INTO HSV FROM DFW AT APPROX 10,500 FEET AND 260 KIAS, AN EXTREMELY POWERFUL ODOR OF JET FUEL OCCURRED IN THE COCKPIT AND CABIN AFTER THE AUXILIARY POWER UNIT WAS STARTED. THE CREW SHUT THE AUXILIARY POWER UNIT DOWN LEAVING THE BLEEDS ON THE ENGINE. THE AIRCRAFT LANDED SAFELY IN HSV. MAINTENANCE DEFERRED THE AUXILIARY POWER UNIT IAW MEL NR 49-10-01, PENDING THE APPROPRIATE REPAIRS. MAINTENANCE CLEARED THIS DEFERRAL BY REMOVING AND REPLACING THE AUXILIARY POWER UNIT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030731000852003073100085NM 2003 7 31 QXEA200300821 120030711A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - PANEL 261LT FLANGES CHAFED VARIOUS AREAS AROUND CIRCUMFERENCE ON PANEL. REPAIRED IAW Q400 RD 8/4-53-521, PAGE 4, STEP 5 AND RD 8/4-53-521, STEP 9. 2H72 4T RTA13NM 20030801000202003080100020WP 2003 8 1 GTIA030550 120030629A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND AFT PIT FLOORBEAM INTERCOSTAL CRACKED IN NUTPLATE HOLES 0 BL AT FS 1287-1309. REMOVED INTERCOSTAL UPPER REPAIR. FABRICATED UPPER REPAIR. INSTALLED UPPER INTERCOSTAL REPAIR. (M) 2L72 4F A6WE 20030829000242003082900024NM 2003 8 29 CALA0300482 120030822A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT AT STA 380-400, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030829000222003082900022NM 2003 8 29 CALA0300450 120030807A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND LT CABIN FLOOR Z-ANGLE CORRODED AT STA 947.5 TO 1006. THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030903000592003090300059WP 2003 9 3 DHL2003801084 120030713A2611302314 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP CARGO DECK INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01801DH 46033 ON PREFLIGHT NR 10 MAIN CARGO DECK SMOKE DETECTOR WOULD NOT TEST. TRANSFERRED TO DMI NR 13532 IAW MEL 26-6 CAT. "C" PLACARDS INSTALLED. REF. DMI NR 13532 ON PREFLIGHT NR 10 MAIN CARGO DECK SMOKE DETECTOR WOULD NOT TEST. REPLACED NR 10 SMOKE DETECTOR UNIT IAW M/M 26-10-00. THIS CLEARS DMI NR 13532 NR 10 SMOKE DETECTOR TESTS OK IAW M/M 26-10-00. 2L74 4F RT4A25 20030903001612003090300161EA 2003 9 3 SWIA200312213 120030722A2910 O-RING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HYD SYSTEM WORN A SWIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM07591SW 7079 AFTER DEPARTURE HYD 2 LOW PRESS CAUTION MSG FLUID QUANTITY INDICATED ZERO. RETURNED FOR LANDING AT SLC. FOUND PLUG ON NR 2 FILTER MANIFOLD LEAKING. REMOVED AND REPLACED O-RING ON PLUG. NO LEAKS NOTED AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20030904001592003090400159WP 2003 9 4 DHL2003873587 120030705A5320 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE MISSING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT (2) NR 1 TRACK SPLICES MISSING STA 985-995. FABRICATED SPLICES IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED SPLICES (2) ON MAIN CARGO COMPT NR 1 TRACK STA 985-STA 995 IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030807000412003080700041EA 2003 8 7 03211641 120030730A324450105711 TIRE CNDAIRCL600 CL6002B19 1900309EA MLG SEPARATED A VTZAO OTHER O OTHER TOTAKEOFF 1 EA27641BR 7349 IMMEDIATELY UPON TAKEOFF CREW NOTED MINOR VIBRATIONS, UPON GEAR RETRACTION VIBRATIONS DISCONTINUED, ALL INDICATIONS NORMAL. APPROX 45-50 MIN INTO FLIGHT ATC NOTIFIED CREW OF TIRE & OTHER DEBRIS ON RUNWAY. NO ABNORMAL INDICATIONS NOTED BY CREW & FLIGHT CONTINUED TO DESTINATION. UPON ARRIVAL TO DESTINATION, CREW DECLARED AN EMERGENCY & FLIGHT LANDED UNEVENTFULLY. UPON INSPECTION AFTER LANDING TIRE TREAD SEPARATION ON MLG CONFIRMED, ADDITIONAL DAMAGE TO LANDING GEAR DOOR, FLAPS & MINOR FOD DAMAGE TO ENG FOUND. AIRCRAFT GROUNDED AWAITING REPAIR AT THIS TIME. MX PERSONNEL REMOVED AND REPLACED TIRE. AIRCRAFT IS CURRENTLY GROUNDED PENDING ADDITIONAL REPAIRS FOR ANCILLARY DAMAGE TO FLAPS, GEAR DOOR, AND ENGINE. 2L72 4F RTA21EA 20030813000512003081300051NM 2003 8 13 2003UALA00465 120030604A5313 STRINGER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE MISREPAIRED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 STATION 1361 TO 1379, STRINGER 34R, STRINGER SECTION AND SPLICE DO NOT HAVE REQUIRED EDGE DISTANCE BETWEEN REPAIR SPLICES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER & SPLICE REPAIRS. 2L72 4F4 FRTA1NM E3NE 20030821000542003082100054NM 2003 8 21 03FDEA01052 120030702A5753 BUSHING DOUG MD11 MD11 3023602NM TE FLAP HINGE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING OUTBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BUSHING FOUND LOOSE. LEFT WING OUTBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BUSHING REPLACED IAW FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030825000202003082500020WP 2003 8 25 UPS03841095 120030724A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA. -12 AT LONG. 27R. CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. E.O. DC8-5330-4732-D 2L74 4F RT4A25 20030822000772003082200077NM 2003 8 22 UPS03241014 120030731A2612160117302 BATTERY BOEING727 72725C 138400HNM CARGO BAY DISCHARGED A IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01932UP 19856 INSPECTION TYPE:N/A FIRE BELL SOUNDED ON CLIMB, LOWER CARGO LIGHT ON INSPECTED, FOUND TO BE INDICATION INOP DUE TO LOW BATTERY. DEFERRED PER MEL. 2L73 4F A3WE 20030910001392003091000139NM 2003 9 10 MWEA030349 120030827A5320593054497 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CORROSION FOUND ON FLOOR SUPPORT AT STATION 1250 BETWEEN SEAT TRACK 32&3 THIRD HOLE FORM OUTBOARD END. 2L72 4F RTA6WE 20030911000282003091100028CE 2003 9 11 DXTA200300099 120030822A3230 VALVE CESSNA750 750 2076810CE MLG STUCK E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07996QS 7500196 UPON APPROACH TO LNK, WITH GEAR HANDLE SELECTED DOWN MAIN GEARS EXTENDED, NO GREEN NOSE GEAR INDICATION. COMPLIED WITH CE-750 CHECKLIST AFTER TOWER FLY BY-VISUALLY CONFIRMED DOWN, USED BLOW DOWN SYSTEM AS PER CHECKLIST, LANDING UNEVENTFUL. TROUBLESHOT AND FOUND RETRACT PRESSURE RELEASE VALVE STUCK. RESEAT VALVE AND ACTUATED 50 TIMES L AND R NO FUTHER STICKING OR BINDING. PERFORMED 15 NORMAL GEAR CYCLES AND 5 EMERGENCY EXTENSIONS ARE GOOD RESULTS. SERVICED RESERVIOR TO FULL AND GEAR BOTTLE TO 2000 PSI REF 650 MM CHAPTER 12-11, PERFORMED 3 MORE NORMAL GEAR CYCLES BLED SYSTEM ALL CHECKS GOOD. 2L72 4J RTT00007WI 20030911001072003091100107WP 2003 9 11 DHL2003873529 120030621A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING IB FLAP AFT LOWER PLATING HAS DENTS AND ELONGATED HOLES AT STA XW.104.000 - XW.115.000. PERFORMED MAJOR REPAIR IAW EODHL-030603, ED-3421. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL, AND INNER BONDED STRAP IAW EODHL-030603, ED-3421. CLEANED, TREATED AND PRIMED NEW SKIN PANEL AND INNER STRAP IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW SKIN PANEL AND INNER BONDED STRAP ON LT WING IB FLAP AFT LOWER PLATING STA XW.104.000 - XW.115.000 USING NEW FASTENERS IAW EODHL-030603, ED-3421 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910001472003091000147NM 2003 9 10 MEX2003383 120030822A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE LIGHTNING STRIKEA ASMFK NONE O OTHER ININSP/MAINT 1 SW23160PL 49763 FLT 173 - TIJ-MEX - DURING TRANSIT CHECK, DETECTED LIGHTNING IMPACT AT FUSELAGE RIGHT SIDE. DURING LIGHTNING INSPECTION, DETECTED DAMAGES WITHIN LIMITS FROM STATION Y-110 TO 250 AND FROM LONGERONS 19 TO 22. THREE NON ROUTINE CARDS WERE ISSUED TO ATTEND THE DAMAGES TO BE ATTENDED IN THE NEXT AIRCRAFT A-CHECK. THE NON ROUTINE AREA ASSOCIATED TO SMALL DAMAGES AT FUSELAGE, .125 INCH DAMAGES AT LEFT ELEVATOR GEAR TAB TRAILING EDGE, .1875 INCH DIAMETER HOLES AT UPPER AND LOWER SURFACE OF LEFT AILERON. (M) 2L72 4F RTA6WE 20030912000602003091200060WP 2003 9 12 DHL2003604704 120030607A53204611067501N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD CARGO COMPT END FITTING CORRODED, STA 70.000, L-27R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21 SRM 51-1-21 PG 1. REMOVED CORROSION FROM END FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG 2P. REMOVED END FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030929001352003092900135NM 2003 9 29 CALA0300515 120030905A5230 SKIN BOEING737 737524 1384721NM C-2 DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717627 27531 INSPECTION FOUND THE C-2 DOOR SKIN DENTED ABOVE AND AFT OF DOOR HANDLE. THE SKIN WAS REPAIRED IAW SRM 52-00-01, FIGURE 203. 2L72 4F RTA16WE 20030905002312003090500231SO 2003 9 5 C2XA03TY126 120030811A534714532606009 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION SEAT TRACK LW6 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030908002762003090800276 2003 9 8 SWIA200312374 420030903A341845150340 VANE CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07408SW 7055 STALL FAIL MSG APPEARS JUST A FEW SECONDS AFTER TAKEOFF. REMOVED AND REPLACED LEFT AOA IAW MM 22-35-05. OPS CHECKS GOOD. P/N ON 45150340, SN OFF 229. 2L72 4F RTA21EA 20031014001342003101400134NM 2003 10 14 SWAA032158 120030926A53306545800 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, BETWEEN STR 19L AND STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20031021002362003102100236SO 2003 10 21 RAIA00309243 120030917A3260 PROXIMITY SENSOR EMB 145 EMB145 3260210SO MLG FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03807HK 145119 AIR GROUND FAIL INDICATION AFTER TAKE OFF. MAINTENANCE ADJUSTED NR 2 MAIN FWD PROX SENSOR AND OPS CK OK. 2L72 4F RTT00011AT 20031027001012003102700101NM 2003 10 27 ASAA02402HH 120030412A5330655053141 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND EXTERNAL POWER RECEPTACLE INTERNAL DOUBLER CRACKED ON LOWER EDGE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031118001162003111800116NM 2003 11 18 AWXA200301192 120030912A5313146N5417 STRINGER BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FLOOR STRINGER IN AFT CARGO COMPARTMENT BS 1280 TO BS 1360, LBL 18 TO RBL 20. MAINTENANCE CUTOUT CORRODED AREAS OF FLOOR STRINGER BS 1280 TO BS 1360, LBL 18 TO RBL 20; FABRICATED REPAIR PLATES AND FILLERS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG. 1, FIG. 1. 2L72 4F4 FRTA2NM A12EU 20031119001472003111900147EA 2003 11 19 SWIA200312483 120031002A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07591SW40 40 7079 STAB TRIM & MACH TRIM FAILED INFLIGHT GOING THROUGH APPROX 17,000. RETURNED TO SLC. REMOVED AND REPLACED HSTCU. OPS CHECK GOOD. 2L72 4F RTA21EA 20040204000272004020400027NM 2004 2 4 2003UALA00775 120031015A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 FORWARD PIT FRAME STA 740 APPROX. RBL 51 HAS DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR. 2L74 4F4 FRTA20WE E24NE 20040204001302004020400130NM 2004 2 4 EIA2003114 120030726A2611FR2121 SMOKE DETECTOR BOEING747 747132 1384882NM CARGO BAY MALFUNCTIONED A EIAAO OTHER N FALSE WARNING CRCRUISE 1 NM09481EV 19896 NR 4 MAIN CARGO SMOKE DETECTOR WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALL FIVE (5) TIMES AN EXAMINATION OF UPPER DECK DISCLOSED NO FIRE. CORRECTIVE ACTION, REMOVED AND REPLACED SMOKE DETECTOR IAW MM 747-26-14-02. 2L74 4F A20WE 20040329000482004032900048NM 2004 3 29 ASAA0340326 120030725A5320 ANGLE BOEING737 7374S3 1384711NM FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND SUPPORT FRAME ANGLES AT STATION 1016 HAVE WORN GROOVES FROM RUDDER CABLES. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20030910000362003091000036WP 2003 9 10 ABXA030325 120030730A532099115717 INTERCOSTAL DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 INTERCOSTAL CRACKED AT FORWARD CONDUIT HOLE, STA 155, 43 INCHES UP FROM FLOOR RIGHT SIDE. REPAIRED AREA IAW DC-9 SRM 53, 51-30-2 AND 51-30-5. 2L72 4F A6WE 20031030000042003103000004CE 2003 10 30 I122003F00001 120030922A1430MS20426AD3 RIVET LEAR 35 35A 5170602CE WINGTIP TANK FAILED B I12RO OTHER O OTHER NRNOT REPORTED 1 EA23498JR7603 498 RIVETS UNDERNEATH WING TIP TANK ACCESS PANEL FAILED. THESE MS426AD3 RIVETS SECURE SEALED NUTPLATES THAT HOLD THE ACCESS PANEL ATTACHMENT SCREWS. DURING THE MANUFACTURING PROCESS, THESE RIVETS WERE SHAVED FLUSH WITH THE ACCESS PANEL RECESS ON THE TIP TANK AND SOME WERE SHAVED TO THE POINT WHERE THE IDENTIFYING MARK ON THE RIVET (DIMPLE) IS GONE. CORROSION WAS FOUND UNDER THE FAILED NUTPLATES AS WELL. DEFECT FOUND ON SCHEDULED INSPECTION. INSPECT FOR FAILED FASTENERS AND REPAIR AS REQUIRED (WITHIN 25 FLIGHT HOURS). LOSS OF CONTROL OF AIRCRAFT POSSIBLE DUE TO FUEL LOSS AND/OR DRAG FROM LOOSE PANEL. 2L72 4F A10CE 20031112000112003111200011NM 2003 11 12 2003UALA00819 120031029A5313 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT PIT WEB ON AFT SIDE OF STA 1540, AND AT STR 29R AND 29L HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20031117001042003111700104WP 2003 11 17 MWEA030410 120031007A5320991015421 SPLICE DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSLEAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 SPLICE PLATE BETWEEN CUSP AND FLOORBEAM AT STATION 1338 LONGERON 18 LEFT HAS LIGHT CORROSION ON TOP SURFACE. FABRICATED AND INSTALLED NEW SPLICE. 2L72 4F4 F A6WE E2EA 20040112002712004011200271WP 2004 1 12 AALA20031472 120031225A3350 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219406W CENTER SECTION OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER SECTION EMERGENCY LIGHT BATTERY CHARGER AND BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031118000592003111800059EU 2003 11 18 AWXA200301174 120031006A5321D5367202200000 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL 151LF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL; FABRICATED A NEW REPLACEMENT PANEL IAW A320 SRM 53-02-00 PG 231-234. 2L72 4F RTA28NM 20040112001232004011200123WP 2004 1 12 GTIA031006 120031115A5520 HORN DOUG DC9 DC981 3022081WP RT ELEVATOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT ELEVATOR BALANCE HORN CORRODED AROUND ATTACHED STRUCTURE INSIDE. REMOVED RIGHT ELEVATOR BALANCE HORN. INSTALLED NEW BALANCE HORN. (M) 2L72 4F A6WE 20040115000042004011500004NM 2004 1 15 03FDEA02019 120031203A5753ARC1991 FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 4 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031218000962003121800096NM 2003 12 18 2003UALA00531 120030701A5270 PROXIMITY SENSOR BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CARGO DOOR DIRTY A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29603UA 21864 UNSCHEDULED LANDING DUE TO FWD CARGO DOOR EICAS. CHECKED DOOR LOCKED AND CLOSED PROXIMITY SENSORS FOR PROPER GAPS. ALL CHECK WITHIN LIMITS. SHOOK OUT PROX SENSOR WIRING WHILE ACCOMPLISHING TARGET NEAR/FAR TESTS. CHECKED WITH AIRCRAFT PRESSURIZED. UNABLE TO DUPLICATE. CLEANED PROX SENSORS AND TARGETS. 2L72 4F4 FRTA1NM E3NE 20031219000982003121900098NM 2003 12 19 2003UALA00927 120031125A2121 FAN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 WP29122UA 29168 SMOKE & ELECTRICAL BURNING ODOR IN CABIN. THE LOWER RT RECIRCULATION FAN MOTOR BEARINGS FAILED.THE RECIRCULATION FAN WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 20031223001522003122300152SO 2003 12 23 C2XA03IA111 120031207A33503025103 LIGHT EMB 145 EMB145XR SO RT OVERWING INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714116 145672 PILOT REPORTED THAT THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM. 2L72 4F RT 20031229000402003122900040SO 2003 12 29 LR7A03105 120031121A5320LS309982 PLATE LKHEED382 382G 526414USO FUSELAGE GOUGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND FLOOR END SCUFF PLATE GOUGED AT FS 817E, WL 146, LBL 60 - RBL 60. REPLACED SCUFF PLATE IAW SMP 583 51-60 & 51-70. NR 2243. 2H74 4T A1SO 20040105000302004010500030EA 2004 1 5 03363634 120031229A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27634BR 7287 DURING INSPECTION THE RT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040105000852004010500085CE 2004 1 5 BSY2003F00029 120030912A323399100023 MOTOR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C* GL MLG GEARBOX MALFUNCTIONED E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0728NT 310R0243 811735R 001943 LANDING GEAR SELECTED DOWN, NOTHING HAPPENED. HAND CRANKED GEAR DOWN LANDED, NO PROBLEM. MAINTENANCE CYCLED GEAR MANY TIMES, COULD NOT DUPLICATE. CHANGED LANDING GEAR MOTOR AS PRECAUTIONARY MEASURE, OPS CHECKS GOOD. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20040105000602004010500060NM 2004 1 5 2003UALA00940 120031206A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29598UA 28751 FOUND SMALL DENT AFT OF DOOR 3 RIGHT, ABOUT 20 INCHES AFT OF DOOR 3 RIGHT OUTSIDE EMERGENCY LIGHT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040105001802004010500180NM 2004 1 5 AWXA200301624 120031207A573065C26271 SKIN BOEING737 737301 1384611NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MINOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN AT NR 2 SLAT OUTBOARD AUXILIARY TRACK CUTOUT WS 346 TO WS 349. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16 PG 27, REPAIR 11. 2L72 4F RTA16WE 20040106000772004010600077SO 2004 1 6 C2XA03SH503 120031218A532014521725001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAME 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040114001272004011400127NM 2004 1 14 DL764031061 120031128A3350 CONTACTOR BOEING767 767432ER 1385134NM COCKPIT DIRTY A DALAK NONE O OTHER ININSP/MAINT 1 SO27844MH 29717 EMERGENCY LIGHT OVER COCKPIT DOOR WILL NOT SHUT OFF. REMOVED LIGHT ASSY, CLEANED CONTACTS AND SWITCH. OPS NORMAL. 2L72 4F RTA1NM 20031124001132003112400113WP 2003 11 24 DHL2003805560 120030806A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS.641.250 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000902003112500090WP 2003 11 25 DHL2003805582 120030804A5754 PLATE DOUG DC8 DC873F 302199FWP L/E SLOT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT INNER WING EXTENDED L/E SLOT UPPER PLATING CORRODED, STA XFS 207.000 AND XFS 220.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT CORRODED AREA IAW SRM 57-2-1 FIG 38. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20031203001162003120300116EU 2003 12 3 A6WA200360033 120030831A3222HC323L0015002 SPRING BAG BAE146BAE146200A 1500266EU NLG BAY BROKEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31292UE E2087 NLG RIGHT WHEEL BRAKE, SPRING BROKEN. MAINTENANCE REMOVED AND REPLACED BROKENS SPRING GUIDE TUBE, SPRING AND REPAIRED DAMAGE TO THE CEILING OVER NLG BAY. (M) 2H74 4F RTA49EU 20040126000312004012600031 2004 1 26 HEEA087797 420030614A2350A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 INTERPHONE BOX HAS BACKGROUND NOISE FROM FM RADIO. SHOP REPAIR. 1G72 3U H1NE 20040121000382004012100038NM 2004 1 21 03FDEA02309 120031227A5744ARC74901 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING INBOARD FLAP VANE OUTBD TEE FITTING MOUNT HOLES 03 EA WORN. COMPLIED WITH FEDEX EA 1-5750-75215, TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBOARD FLAP VANE ATTACH FITTING REWORK. 2L73 4F RTA22WE 20031203001492003120300149WP 2003 12 3 AMTA200301265 120030808A5330 SKIN LKHEED1011 10113851 5265010WP FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND FUSELAGE SKIN DENTED FORWARD OF LAV SERVICE DOOR. REPAIRED FUSELAGE SKIN IAW SRM 53-31-00, FIG 802. (M) 2L73 4F A23WE 20031208000142003120800014EA 2003 12 8 SWIA200312512 120031021A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 484 LT INTERCOSTAL OB FLANGE LBL 36 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ RE 601R-53-41-059 REV ''A'' & RII 53-401. 2L72 4F RTA21EA 20031209001122003120900112NM 2003 12 9 VNAA0310016 120031022A5210 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR FAILED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07442JS 3060 DURING FLIGHT, THE CREW RECEIVED A PASSENGER OPEN INDICATION IN FLIGHT AND RETURNED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE PASSENGER DOOR ROD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031209002602003120900260NM 2003 12 9 AWXA200301361 120031013A5315146N5416 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1320, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1215 TO BS 1320, LBL 2; FABRICATED A REPLACEMENT FLOORBEAM AND SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1. 2L72 4F RTA2NM 20031210001852003121000185NM 2003 12 10 CALA0300637 120031024A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714324 23375 MAINTENANCE DISCOVERED AN IMPROPERLY INSTALLED REPAIR TO THE AFT CARGO DOOR INNER SKIN AT AN UPPER LIGHTENING HOLE. A SMALL CRACK WAS ALSO DISCOVERED AT THE LIGHTENING HOLE AFT OF THE IMPROPER REPAIR. THE AREAS WERE REPAIRED IAW ECRA 5232-01039. 2L72 4F RTA16WE 20031020001422003102000142EU 2003 10 20 MALA030442 120030930A7603 POWER LEVER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COCKPIT OUT OF RIG A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15403XJ 340B403 DURING CLIMBOUT ON FLIGHT 2987, LT ENGINE WAS FIREWALLED FROM 17000 TO CRUISE ALTITUDE 22000. RAN APPROX 5 - 6 PERCENT LESS THAN CHARTED TORQUE. ITT WAS APPROXIMATELY 830-840. AIR RETURN TO MSP AS PER MXC, AND DISPATCH UNABLE TO MAKE CHARTED TORQUE POWER LEVER SPLIT NOTED AT MOST SETTING LEFT PL 3/4 AHEAD OF RIGHT PL. MAINTENANCE FOUND LT ENGINE OUT OF RIG. RERIGGED LT ENGINE PER SAAB AMM 76-10-00. PERFORMED GROUND RUN, FOUND NO POWER LEVER SPLIT. PERFORMED GPA, FOUND MARGIN TO BE ACCEPTABLE. 2L72 4T4 TRTA52EU E8NE 20031021000332003102100033NM 2003 10 21 USAABB03144 120030822A3510 OXYGEN SYSTEM BOEING767 767201 1385125NM COCKPIT LEAKING A USAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA19648US 23900 SNN - FL49 - EN ROUTE CDG TO PHL, CREW NOTED ON EICAS THE CREW OXYGEN PRESSURE HAD FALLEN TO 50. FLIGHT DIVERTED TO SNN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN SNN CONFIRMED THAT THE FIRST OFFICERS MASK/REGULATOR/BOX ASSEMBLY WAS LEAKING. THE UNIT WAS SWAPPED WITH THE 2ND OBSERVER'S UNIT, THE 2ND POSITION OXYGEN LINE CAPPED AND THE OXYGEN SYSTEM SERVICED. THE FLIGHT CONTINUED TO PHL. MAINTENANCE AT PHL REPLACED UNIT. (M) 2L72 4F RTA1NM 20030919000802003091900080CE 2003 9 19 DXTA200300072 120030721A2130 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NR 2 LEAKING E DXTAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07333QS7102 5600333 OILY ODOR ON TAKEOFF AND DESCENT AND AT ALTITUDE OF 15,000 FT. PERFORMED ENGINE BORESCOPE AND FOUND EVIDENCE OF ENGINE OIL IN GAS GENERATOR CASE AREA, REMOVED NR 2 ENGINE AS PRECAUTIONARY. 2L72 4F4 FRTA22CE E25EA 20030922000402003092200040EU 2003 9 22 RAIA00308206 120030801A3260EO276ANOP016 SWITCH AEROSPATR42 ATR42300 8680920EU PARKING BRAKE DEFECTIVE A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03426TE 228 PARKING BRAKE LIGHT ILLUMINATED ON TAXI. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE SWITCH. 2H72 4T RTA53EU 20030924000652003092400065NM 2003 9 24 DL757030781 120030824A3397 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT LOOSE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27672DL 25977 SEAT 1C, 5C, 25C 31C EMERGENCY LIGHTS INOPERATIVE. FOUND LOOSE CONNECTIONS. RESECURED WIRES OPS CK NML 2L72 4F RTA2NM 20040122000452004012200045EA 2004 1 22 ASOA03619 120031202A5260601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11907EV 7648 DURING A C-CHECK IN MCN, THE TOP AND BOTTOM PASSENGER DOOR STEPS WERE FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP AND BOTTOM PASSENGER DOOR STEPS. (M) 2L72 4F RTA21EA 20040122001022004012200102EU 2004 1 22 ASOA03602 120031124A2750 VALVE AEROSPATR72 ATR72212 8680945EU TE FLAPS FAILED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11634AS 370 FLT 4874 - DURING APPROACH INTO TYS FROM ATL, THE CREW RECEIVED A FLAPS UNLOCK MESSAGE. IN COMPLIANCE WITH THE PILOT'S OPERATING HANDBOOK, THEY COMPLETED A GO AROUND AND PERFORMED A ZERO FLAPS LANDING. DUE TO WEATHER CONDITIONS, AS A PRECAUTION THE CREW REQUESTED EMERGENCY VEHICLES BE ON STAND-BY. THE AIRCRAFT LANDED SAFELY IN TYS. MAINTENANCE REMOVED AND REPLACED THE FLAP VALVE BLOCK, FLAP ACTUATORS AND TWO OF THE FLAP ACTUATOR HOSES ON THE LEFT OUTBOARD SIDE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040115001742004011500174 2004 1 15 USAASB03211 420031205A2215AR6460M2 SERVO BOEING737 737301 1384611NM AUTOPILOT SYS FAILED A USAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 EA19355US 23558 DURING FLIGHT, EN ROUTE, THE STABILIZER OUT OF TRIM LIGHT ILLUMINATED. THE AUTOPILOT WOULD NOT TRIM. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT SERVO MOTOR. OPS CHECK AND BITE TEST NORMAL. (M) 2L72 4F RTA16WE 20031204001612003120400161EU 2003 12 4 MALA030460 120030925A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, NR 4 SEAT RAIL CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED IAW EO A53026. A/C RELEASE DATE 10/12/03. REFER TO 409 189909 FOR ADDITIONAL DETAIL. 2H74 4F RTA49EU 20031208001522003120800152 2003 12 8 QXEA200301353 420031025A34180856VK9 PITOT HEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 OBSTRUCTED A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09614QX96 10049 FLIGHT 2452 ABORTED TAKEOFF DUE TO LARGE A/S SPLIT, FIRST OFFICERS A/S INDICATED APPROXIMATELY 80 KTS, CAPTAINS INDICATED APPROXIMATLEY 50 KTS. ALSO INDICATED MASTER CAUTION WITH/EFIS COMPUTER MON AND MACH MESSAGES. FOUND OBSTRUCTION IN PILOTS PITOT TUBE. REPLACED PILOTS PITOT STATIC HEAD. PERFORMED P/S LEAK TEST OF PILOTS SYSTEM ALL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031209002192003120900219NM 2003 12 9 CALA0300615 120031101A5347 GALLEY TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 INSPECTION FOUND FLOOR SUPPORT UNDER GALLEY MOUNT CORRODED AT STA 277-290, RBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-02. 2L72 4F RTA16WE 20040128000962004012800096NM 2004 1 28 AWXA200301642 120031203A572065C2670127 ANGLE BOEING737 73733A 1384673NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND ON LT WING LEADING EDGE BRACKET (Z-ANGLE) INSIDE PANEL 5748, WS 191. MAINTENANCE REMOVED CRACKED Z-ANGLE WS 191, UPON REMOVAL OF ANGLE FOUND LOWER SKIN CRACKED. REMOVED CRACKED SECTION OF SKIN; FABRICATED A NEW REPLACEMENT ANGLE AND NEW SECTION OF SKIN PER DWG 65C26701; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, FIG 3, 6, 7, & 8, PG 1, 28, 32, 36, & 38. 2L72 4F RTA16WE 20031014000822003101400082NM 2003 10 14 SWAA032220 120031002A7920717000 HOUSING BOEING737 7372H4 138448CNM NR 2 ENGINE LEAKING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 NR 2 ENGINE MAIN OIL FILTER HOUSING LEAKING. REMOVED AND REPLACED NR 2 ENGINE GEAR BOX PER MM. 2L72 4F A16WE 20031016000062003101600006EU 2003 10 16 N382003F00011 120030928A5320 SUPPORT BRACKET ISRAEL1124 1124 4500102EU GARRTTTFE731TFE731* 01518WP NLG WW BROKEN B N38RO OTHER O OTHER NRNOT REPORTED 1 EA05163WC8227 217 WHILE ON VECTORS FOR A VISUAL RIGHT DOWNWIND TO RUNWAY 01 AT KMKC WE SELECTED GEAR DOWN. NO NOSE GEAR DOWN LIGHT AND GEAR IN TRANS LIGHT STAYED ON. THE GEAR WAS CYCLED ABOUT FOUR TIMES WITH NO CHANGE. WE FOLLOWED THE PROCEDURES OF THE 1124 CHECKLIST AND COULD NOT GET A NOSE GEAR DOWN LIGHT. WE STAYED IN CONTACT WITH KMCK TOWER THE ENTIRE TIME AND REQUESTED A LOW APPROACH. THE NOSE GEAR WAS REPORTED VISUALLY DOWN BY A PERSON ON THE GROUND. ALL GROUND CRASH FIRE RESCUE PERSONNEL WERE CALLED AND A NORMAL LANDING WAS MADE. THE AIRCRAFT WAS TOWED FROM THE RUNWAY. 2M72 4F4 F A2SW E6WE 20031209002432003120900243NM 2003 12 9 UPS03241517 120031010A5312 PANEL BOEING727 72731C 1384011NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, DURING PRESSURE LEAKAGE CHECK IN NLG WW A 3 INCH CRACK WAS FOUND ON RT CEILING. DAMAGED PART OF WEB CUTOUT REMOVED IAW SRM 51-40-2. DE-RIVETED IAW SRM 51-30-02. HFEC INSPECTION CARRIED OUT AROUND CUTOUT IN NWW ON RT CEILING IAW B727 NDTM PT 6 51-00-00 RESULT NDF. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1. 2L73 4F A3WE 20031212000672003121200067EA 2003 12 12 MASA200300426 120031025A7603 CONTROL QUADRANT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE OBSTRUCTED A MASAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SW077733110316 7331 872550 ASH 7331 DEN. AIRCRAFT ABORTED TAKEOFF DUE TO NR 2 ENG W/N PRODUCE T/O THRUST. MX REMOVED FOD FROM THROTTLE QUADRANT AREA. OP CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031211001382003121100138WP 2003 12 11 AALA20031386 120031205A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 DFW EMERGENCY AISLE LIGHT AT SEAT 20D INOPERATIVE. REPLACED BOTH SOCKETS FOR EMERGENCY AISLE LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20030919000962003091900096CE 2003 9 19 GLBA2003121 120030814A7722 TRIM SWITCH BEECH 1900 1900D 1154162CE NR 2 ENGINE OUT OF ADJUST A GLBAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 NM0396UX UE96 NR 2 ENG EXCEDED ITT TAKE OFF LIMITS 3392 ON TORQUE, READJUSTED TRIM STICK OHMS TO PROPER ADJUSTMENT. 2L72 4T RTA24CE 20030922000182003092200018NM 2003 9 22 QXEA200300982 120030816A5410 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 NR 2 ENGINE LOWER NACELLE UPPER DECK SUPPORT ANGLE IS CRACKED. REPAIRED IAW Q400 RD 8/4-71-016. 2H72 4T RTA13NM 20030915000972003091500097GL 2003 9 15 BAQA088977 220030828A732323007506 GOVERNOR AGUSTAA109 A109A2 0260120EU ALLSN 250C 250C20B 03013GL PT ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA031PJ 976 7262 PT GOVERNOR HAS ERRATIC OPERATION. BEYOND ECONOMICAL REPAIR FOR TIME CONTINUED OPERATION. REQUIRES OVERHAUL OR REPLACEMENT WITH NEW CONFIGURATION GOVERNOR PER CED-1391. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H7EU E4CE 20030916001592003091600159NE 2003 9 16 JYD2003F00000 120030304A5320642066345404EAC FITTING SKRSKYS64 S64E 8142604NE PYLON CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09CGESG4051 64065 CRACK FROM RIVET HOLE BOTTOM LEFT CORNER TO OUTER EDGE OF FITTING. CRACK LENGTH APPROXIMATELY .5000 INCH. THIS IS ONE OF FOUR EARS THAT ATTACH TO THE PYLON LONGERONS. THIS PART OF THE ASSEMBLY THAT THE TAIL ROTOR GEARBOX ATTACHES TO. CAUSE UNKNOWN AT THIS TIME. 2G72 4U H4EA 20030919000742003091900074NM 2003 9 19 751PA0021 120030812A3350 LAMP BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 RT 1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED R1 DOOR EXTERIOR LIGHT. OPS CHECKS OK. 2L72 4F RTA2NM 20040128000302004012800030NM 2004 1 28 03FDEA02224 120031221A5753ARC2518501 STRAP DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING, INBD FLAP OUTBD HINGE (FLAP SIDE), OUTBD STRAP, PIVOT POINT SPOT FACE CORRODED. LEFT WING - INBD FLAP OUTBD HINGE (FLAP SIDE), OUTBD STRAP REMOVED AND REPLACED WITH NEW AS PER SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20040206000602004020600060WP 2004 2 6 ASAA0380675 120031026A5230591014167 FLANGE DOUG DC9 DC982 3022082WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND AFT CARGO BAY DOOR IS CHAFED ON FLANGE AT FORWARD STOPS. INSTALLED DOUBLERS PER EA 5230-01205. (M) 2L72 4F A6WE 20040211000202004021100020NM 2004 2 11 USAA030319 120031219A5330 SKIN PANEL BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US49845 23232 PIT - FOUND SKIN PANEL CRACKED 2 INCHES, STATION 720 KEEL BEAM. INSTALLED DOUBLER PER EA 77147 AND SRM 53-10. (M) 2L72 4F RTA16WE 20040218000362004021800036NM 2004 2 18 UPS04441734 120031231A5340 STRINGER CLIP BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, MAIN DECK - BS 2340, S44R STRINGER CLIP FOUND CRACK. STRINGER CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20040401000292004040100029WP 2004 4 1 ASAA0380410 120030421A5312995821213 BULKHEAD DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT MLG WHEEL WELL AFT PRESSURE BULKHEAD IS GOUGED AT FS 1003. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-70-4. (M) 2L72 4F A6WE 20031217001022003121700102NM 2003 12 17 03FDEA01889 120031107A5230 SKIN BOEING727 727100 1384036NM CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 LWR AFT CARGO DOOR SKIN, SKIN DAMAGED ALONG FWD EDGE AT NR 2 STOP FITTING FROM TOP. *S/D* INSPECTED LWR AFT CARGO DOOR SKIN ALONG WD EDGE, DAMAGE WAS 1 X 16 X .25 INCH FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, ALODINED, PRIMED, INSTALLED AND PAINTED IAW SRM 52-00-3, 51-30-2, 51-10-2, 51-10-1, 51-30- 5, 51-20-1, 51-30-2. 2L73 4F RTA3WE 20040902001722004090200172NM 2004 9 2 UIEA200300051 120030816A541069B941203 FITTING BOEING747 747271C 1384869NM NR 1 PYLON DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 DURING C-CHECK, NR 1 PYLON OB SPRING BEAM SHEAR TRANSFER FITTINGS FOUND DAMAGED DUE TO CONTACT WITH SPRING BEAM. CONTRACT RESULTED FROM MISLOCATION OF FITTINGS. SUBJECT FITTINGS WERE TRIMMED TO REMOVED DAMAGE, NDT INSPECTED, & RESTORED PER DRAWING. FITTINGS OTHERWISE MET DRAWING REQUIREMENTS. CRACK FOUND ON FITTING 69B941204, .47 INCH LONG. ACCOMPLISH A VISUAL INSP NR 4 PYLON. PROBLEM DID NOT OCCUR AT PYLON NR 4. DAMAGE FOUND FITTING 69B94120-3. DAMAGE TRIMMED. REPAIRS STRUCTURALLY ACCEPTABLE & SUFFICIENT CLEARANCE PROVIDED. CONDUCT A DETAIL VISUAL INSPECTION OF FITTING & INSTALLATION EVERY 6 MONTHS TO CONFIRM NO OTHER FURTHER CRACKING OR DAMAGE TO THE FITTING, REPLACE FITTING WITHIN 18 MONTHS. (M) 2L74 4F A20WE 20060801000942006080100094WP 2006 8 1 IXXA060546S 120030907A5520 FAIRING DOUG DC8 DC871F 302199DWP ZONE 300 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR UPPER TRAILING EDGE ATTACHMENT FAIRING HAS A HOLE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 55-3-0, 55-2-0, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060801001342006080100134WP 2006 8 1 IXXA060577S 120030911A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "B" TANG BROKEN AT STATION 260. REMOVED DAMAGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0. 2L74 4F RT4A25 20030819000362003081900036WP 2003 8 19 AALA20030691 120030624A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21420AA 49332 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT STAIRWAY INOPERATIVE. REPAIRED AFT STAIRWAY EMERGENCY EXIT LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030820000332003082000033NM 2003 8 20 03FDEA01169 120030728A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED- OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 27 RIGHT HAND SIDE. 2L73 4F RTA22WE 20030820000872003082000087EU 2003 8 20 03FDEA00868 120030610A3297 WIRE AIRBUS300 A300B4605R 3930308EU MLG BROKEN A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25651FE 728 AFTER GEAR RETRACTION, GOT LANDING GEAR RETRACT INOP ON ECAM. DURING RETRACTION NEVER GOT RED UPLOCK LIGHT IN NOSE INDICATOR LIGHT. TRIED POSITION INDICATION SYSTEM 2, SAME WARNING ON ECAM. AFTER RETRACTION ALL GEAR LIGHTS EXTINGUISHED. REPEAT WRITE-UP. T/S FOUND BROKEN WIRES ON 39GBA C/P FACT 11JUN03 18:28 FLL R FOUND BROKEN WIRE TO PIN 'E' AT C/P 39GBA (NLG UPLOCK SYS1 MICROSWITCH). REMOVED AND REPLACED C/P IAW SWP'S. C/W NOSE GEAR TEST (SWING) IAW AMMSUPP 32-31-00-5 PAR 6. ALL NOSE GEAR & DOOR INDICATIONS CHK NORMAL. 2L72 4F RTA35EU 20030819001502003081900150NM 2003 8 19 2003UALA00507 120030617A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29789UA 26935 RIGHT UPPER FUSELAGE DENTED AT STA 605 STRINGER 6R TO 7R. 2L72 4F4 FRTT0001SE E46NE 20030401000172003040100017WP 2003 4 1 AALA20030031 120030107A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21266AA 49291 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROW 7-11 INOPERATIVE. RESEATED CEILING EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401001292003040100129WP 2003 4 1 DHL2003804521 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 622.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030822000522003082200052NM 2003 8 22 2003UALA00565 120030716A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE PUNCTURED A UALAK NONE O OTHER UKUNKNOWN 1 WP29663UA 27160 AFT PIT FRAME HAS 3 INCH PUNCTURE STA 1351, STR 24R TO 25R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20030402000622003040200062NM 2003 4 2 2003UALA00339 120030304A5754114W423011 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 3 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 3 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED 2L72 4F4 FRTT0001SE E46NE 20030408001062003040800106NE 2003 4 8 2003F00213 220030211A7230M31104 COMPRESSOR WHEEL GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE LT ENGINE OUT OF BALANCE A UG8AO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL235102 551 11211 DURING CLIMB, OUT OF KDTW, THE LEFT ENGINE AMBER 'VIBRATION EXCEEDANCE' CAS MESSAGE WAS RECEIVED. POWER ON THE LT ENGINE WAS REDUCED, IAW THE AFM, AND THE MESSAGE EXTINGUISHED. THERE FORE, THE TRIP CONTINUED TO DESTINATION AND AACI MX PROVIDER AT KDTW WAS CONTACTED. LEFT ENGINE FAN BALANCE WEIGHT WAS REINSTALLED IN THE INCORRECT POSITION AFTER NDT INSPECTION OF FAN HUB. ENGINE VIBRATION EXCEEDANCE INSPECTIONS HAVE BEEN COMPLETED PER THE BR710 MAINTENANCE MANUAL CHAPTER 71-00-00. FUEL TUBE NR 20 HAS BEEN REPLACED PER THESE INSTRUCTIONS. NO DISCREPANCIES NOTED DURING THESE REQUIRED INSPECTIONS. THE LT ENGINE FAN WAS BALANCED PER THE TRIM BALANCE PROCEDURES IN THE BR710 MAINTENANCE MANUAL CHAPTER 71-00-00 2L72 4F4 FRTA12EA E00057EN 20030410001832003041000183EU 2003 4 10 FG32003F00000 120030301A2121M3348A1 MOTOR SAAB SF340 SF340A 7850100EU ON FAN INOPERATIVE B FG3RO OTHER O OTHER NRNOT REPORTED 1 WP05 5098 WHEN FAN WAS TESTED, IT FAILED THE MINIMUM RPM REQUIREMENTS. WHEN IT WAS DISASSEMBLED, IT WAS DISCOVERED THAT THIS OVERHAULED UNIT HAS NOT BEEN OVERHAULED IAW DAE OVERHAUL MANUAL. THE ARMATURE IS NOT OF DAE DESIGN. ONE LEAD OF THE ARMATURE IS BURNED, THE COMMUTATOR IS SCORED, AND THE IMPELLER SHOWS SIGNS OF RUBBING. DAE OVERHAUL MANUAL DOES NOT ALLOW FOR THE REWINDING OF THE ARMATURE OR THE REPLACEMENT OF PARTS OTHER THAN LISTED. 2L72 4T RTA52EU 20030414000032003041400003 2003 4 14 SWAA030760 420030404A2565D31354 SLIDE BOEING737 7373Q8 1384670NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030416000732003041600073WP 2003 4 16 ZW0A0303501 120030326A3350408822101 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139677W 53627 THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 10-05-02 STL. 2L72 4F RTA6WE 20030416003292003041600329EA 2003 4 16 SWIA200311730 120030102A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW 7518 FS 625 STR 14L LT INTERCOSTAL ANGLE FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 & 51-42-06. P/N: 601-35012-51. 2L72 4F RTA21EA 20030416003522003041600352 2003 4 16 SWIA200311688 420030104A22108220287401 MODULE CNDAIRCL600 CL6002B19 1900309EA LIGHTNING PROTECMALFUNCTIONED A SWIAO OTHER EF VIBRATION/BUFFET FLT CONT AFFECTED CRCRUISE 1 NM07589SW2969 2969 7079 AT FL310 AND .74 MACH, EXPERIENCED RUDDER FLUTTER. ADDED RIGHT RUDDER TRIM, AIRCRAFT WAS THEN OUT OF TRIM BUT FLUTTER WENT AWAY. REPLACED BOTH LIGHTNING WIRE PROTECTION MODULES IAW 22-12-0B. OPS CHECK GOOD. P/N 2: 822-0332-401, S/N OFF: 216. 2L72 4F RTA21EA 20030417000602003041700060EU 2003 4 17 MALA030135 120030126A5320 SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING E-CHECK IN CWA, RBL 11 FRAME SUPPORT BETWEEN STA 272-288 HAS CORROSION. MAINTENANCE REPLACED FRAME. RELEASE DATE 1/28/03. REF 409 175562 FOR DETAIL. 2L72 4T RTA52EU 20030425000682003042500068CE 2003 4 25 WVE2003F00006 120030310A243530728692 SPLINE ADAPTER LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312B WP STARTER GEN WORN B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09407FX2203 090 DURING 600 HOUR INSPECTION OF THE STARTER/GENERATOR SPLINE ADAPTOR IT WAS FOUND TO BE WORN ON OUTSIDE SPLINE. 2L72 4F4 FRTT00008WIE6WE 20030428001542003042800154WP 2003 4 28 DHL2003803006 120030408A5347 SEAT TRACK DOUG DC8 DC873 302199CWP COCKPIT DIRTY A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01803DH 46123 F/E'S SEAT DIFFICULT TO SLIDE FORE AND AFT. LOCKING MECHANISM DOES NOT SEEM TO BE DISENGAGING FULLY. CLEANED SEAT TRACK, LUBED TRACK AND MECHANICAL HANDLE SEAT, OPS OK M/M 25-11-6. 2L74 4F RT4A25 20030428000812003042800081EA 2003 4 28 JBXA03003 120030407A3260 SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG DOOR MALFUNCTIONED A JBXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO05592 AIR RETURN FLIGHT 5132, NLG DOOR OPEN MESSAGE ON AFTER GEAR RETRACTION ON TAKEOFF. AIRCRAFT RETURNED TO GATE, MAINTENANCE FOUND DOOR CONTROL SWITCH IN OPEN POSITION. INSPECTED AND OPERATED DOOR SEVERAL TIMES USING SWITCH, OPS CHECK GOOD. NO DEFECTS NOTED IAW AMM 32-20-00. 2L72 4F RTA21EA 20030429002062003042900206NM 2003 4 29 CALA0300194 120030407A5522 SKIN BOEING737 737524 1384721NM ELEVATOR PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0918622 27526 THE UPPER SURFACE SKIN PANEL OF THE RT ELEVATOR SUFFERED SMALL PUNCTURE DAMAGE AT APPROXIMATELY ELEVATOR STATION 105.1 WHILE AIRCRAFT WAS IN 1/4D CHECK AT HOU. THE DAMAGE WAS THROUGH ALL PLIES, BUT THERE WAS NO CORE DAMAGE. THE PUNCTURE WAS APPROXIMATELY 4.2 INCHES FORWARD OF THE ELEVATOR'S TRAILING EDGE. THE SKIN WAS REPAIRED IAW ECRA 5520-01323. 2L72 4F RTA16WE 20030501000402003050100040WP 2003 5 1 AALA20030197 120030203A5310 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21588AA 53251 TUL - FOUND BOTH LEFT AND RIGHT SHEAR TIE DOUBLERS ON AFT SIDE OF FRAME 1451 CRACKED BELOW VERTICAL STAB ATTACH ANGLES. REPLACED SHEAR TIE DOUBLERS WITH NEW PARTS. REMOVED AND REPLACED PER SRM 53-01-00. (M) 2L72 4F RTA6WE 20030430000032003043000003NM 2003 4 30 QXEA0300495 120030411A5350 FAIRING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - WING TO FUSELAGE FAIRING, PANEL 262HT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030430002532003043000253 2003 4 30 SWAA030814 420030413A2565 GIRT BAR BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29734SA 27866 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030502001942003050200194EA 2003 5 2 A6WA200340047 120030206A2420761341A ADG CNDAIRCL600 CL6002B19 1900309EA ELETRICAL INOPERATIVE A A6WAO OTHER L NO TEST NRNOT REPORTED 1 GL31413AW2896 7585 MAINTENANCE CHECK FLIGHT REQUIRED FOR INFLIGHT DEPLOYMENT OF ADG. ADG TEST FLIGHT UNSATISFACTORY. REMOVED AND REPLACED GCU (S/N OFF: 0570, S/N ON: 0212). OPERATIONAL CHECK OF GCU GOOD. ADG TEST FLIGHT GOOD. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, PASSED INCOMING ATP TEST WITH NO ERRORS. 2L72 4F RTA21EA 20030505001262003050500126NM 2003 5 5 03FDEA00213 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 9L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030507000252003050700025EU 2003 5 7 CA030409001 120030407A2913 BELT SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE HYD PUMP CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON ROUTINE INSPECTION, AME FOUND HYDRAULIC PUMP BELT TO BE CRACKED AND STARTING TO DELAMINATE (1/8INCH DELAMINATED) AT LAP JOINT. BELT REPLACED PRIOR TO FURTHER FLIGHT. IT WAS NOTED THAT THE BELT WAS 'VERY TIGHT' WHEN STRETCHED TO REQUIRED VALUE ON INSTALLATION. 1G71 3U3 U H9EU E19EU 20030508000672003050800067NE 2003 5 8 CH1A200393008 220030413A7230 COMPRESSOR BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A C1HAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL15293AS 21348 FL310 NR 2 ENGINE COMPRESSOR STALLED DUE TO MOMENTARY FUEL STARVATION. THRUST LEVER IDLE, FUEL FLOW RESTORED TO NORMAL ALL OTHER INDICATIONS NORMAL RETURNED TO CRUISE 2L73 4F4 F A3WE E2EA 20030513000402003051300040EA 2003 5 13 SWIA200311948 120030331A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FS 589 AND 605 FLOOR TRANSVERSE BEAMS LEFT SIDE ATTACH ANGLES CRACKED. FOUND DURING C CHECK INSPECTION. AFT ANGLE AT FS 605 REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. FORWARD ANGLE AT FS 589 REPLACED IAW CRJ SRM 51-40-11, 51-40-06, 51-42-21, AND 51-23-00. 2L72 4F RTA21EA 20030513001612003051300161NM 2003 5 13 QXEA0300463 120030413A521085217008101 SEAL BOMBDRDHC8 DHC8401 1390041NM PAX DOOR FAILED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09409QX 4051 SEA- AFT PASSENGER DOOR WILL NOT OPEN. REMOVED AND REPLACED AFT PASSENGER DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030514000482003051400048NM 2003 5 14 SWAA030971 120030429A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED AND LIGHT LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS AND SECURED LIGHT PER MM. 2L72 4F RTA16WE 20030514000582003051400058 2003 5 14 SWAA030957 420030430A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20031124000202003112400020NE 2003 11 24 038463 220031120A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT MALFUNCTIONED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 487 DURING TAKEOFF ROLL CREW NOTICED THAT LT ENGINE OIL PRESSURE AND TEMPERATURE BOTH INDICATED ZERO. CREW ABORTED T/O AND RETURNED TO GATE IN ERI. A/C TAKEN OUT OF SERVICE 11-20-03 AT 0835 (LT). 2L72 4T4 TRTA52EU E8NE6 20030602001672003060200167EA 2003 6 2 A6WA200340065 120030506A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT ARE CRACKED. REMOVED AND REPLACED OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT SIDES IAW CRJ SRM 51-42-06. (M) 2L72 4F RTA21EA 20030604000682003060400068WP 2003 6 4 UPS03840484 120030415A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C1 REMOVE L-2 DOOR LOWER FWD. CORNER DOUBLER AND REPAIR PER SRM. 53-2-0 FIG. 18 CUTOUT DOES NOT CONFORM,STA. 1620 LONG. 20L. REMOVED EXISTING REPAIR,CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM.53-2-0 FIG. 18. 2L74 4F RT4A25 20030606000982003060600098NM 2003 6 6 PCAA0305075 120030517A531285310056 PRESSURE PANEL DHAV DHC8 DHC8102 2809003NM WHEEL WELL CRACKED A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13831EX 160 SYR-LGA FLIGHT 3994. CREW REPORTED GEAR WOULD NOT RETRACT NORMALLY. LT AND RT AMBER DOOR ADVISORY LIGHTS ILLUMINATED AND RED DOOR ADVISORY LIGHT ILLUMINATED WHEN GEAR SELECTED UP. AIRCRAFT DIVERTED TO BGM. MAINTENANCE INSPECTED AIRCRAFT AND FOUND STRUCTURAL DAMAGE TO NOSE GEARWELL UPPER DECK BY UPLOCK TRIPPING ARM. DAMAGE WAS REPAIRED IN ACCORDANCE WITH DEHAVILLAND DASH 8 REPAIR DRAWING RD8-53-039. GEAR OPERATED AFTER REPAIR INSTALLED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030609000162003060900016EA 2003 6 9 SWIA200311984 120030518A3230 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA LT MLG MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07941SW 7750 GEAR DOWN DISAGREE ON APPROACH TO EUG. TOWER REPORTED THE LEFT MAIN GEAR APPEARED TO BE IN THE UP POSITION. PERFORMED GEAR DOWN DISAGREE IN QRH. THE WARNING WENT AWAY AND THE LEFT MAIN INDICATED DOWN AND GREEN. REPLACED MAIN LANDING GEAR PRIORITY VALVE IAW MM 32-32-15. LANDING GEAR FUNCTIONS CHECK GOOD. NO LEAKS. 2L72 4F RTA21EA 20030515001932003051500193NE 2003 5 15 AWXA200300518 220030507A75101726256 VALVE BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE NR 2 ENGINE OPEN A AWXAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 WP28312AW463411178 24060 STL - DIVERSION - FLT 0126 - EN ROUTE FROM PHX TO MKE, NR 2 ENGINE COWL ANTI-ICE VALVE FAILED TO OPEN, DUE TO ICING CONDITIONS DIVERTED TO STL. MAINTENANCE AT STL COMPLIED WITH MEL PROCEDURE 30-3, COND 4, OPENING OF THE NR 2 ENGINE COWL ANTI-ICE VALVE. WHEN AIRCRAFT ARRIVED IN PHX, MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE COWL ANTI-ICE VALVE IAW BMM 30-21-11 PG 401-404, OPERATIONAL CHECK WAS GOOD. VENDOR BENCH TEST OF ENGINE COWL ANTI-ICE VALVE S/N 1547AB CONFIRMED FAILURE OF UNIT. VALVE WAS FOUND TO STICK IN THE CLOSED POSITION, REGULATOR VALVE STICKS IN MID POSITION 0 PSI TO 790 PSI AFTER BEING MANUALLY CYCLED, AND FAILED BONDING TEST. REPLACED PISTON SEALS, O-RINGS, AND BEARINGS PER CMM 30-21-01. 2L72 4F4 FRTA16WE E2GL 20030520001382003052000138WP 2003 5 20 WX030001 120030313A7711 LINE DOUG DC9 DC987 3022087WP PT2 OBSTRUCTED A O OTHER F FLT CONT AFFECTED TOTAKEOFF 1 WP17945MA 49725 ON TAKEOFF FROM IFP CREW OBSERVED LT ENG EPR WAS 1/2 PERCENT LOWER THAN RT ENGINE. RT ENG WAS ADJUSTED TO MATCH LT ENG. ON CLIMB-OUT CREW OBSERVED THAT AS ALTITUDE INCREASED DIFFERENCE BETWEEN LT & RT ENG EPR ALSO INCREASED. WHEN CREW ATTEMPTED TO MATCH EPR'S AIRCRAFT YAWED. FLT WAS THEN DIVERTED TO LAS. EMERGENCY MAINTENANCE WAS CALLED OUT TO TROUBLESHOOT. IT WAS DETERMINED THAT THERE WAS AN EPR INDICATION PROBLEM. LT ENG EPR WAS DEFERRED UNDER MEL 77-1 & FLIGHT RESUMED WITH NO FURTHER PROBLEMS. THROUBLESHOOTING REVEALED RT ENGINE EPR INDICATING HIGH & NOT LT ENGINE INDICATING LOW. MAINT FOUND AN OBSTRUCITON IN PT2 LINE. OBSTRUCTION WAS CLEARED & DEFERRAL CLOSED. NO FURTHER PROBLEMS HAVE BEEN RECOR2L72 4F RTA6WE 20030610001062003061000106GL 2003 6 10 HEEA087001 220030604A753223073353 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH15277 53393 BLEED VALVE PRODUCING TOT HIGH IN FLIGHT. REPAIRED. 1G71 3U3 UO H2SW E4CE 20030612000822003061200082WP 2003 6 12 UPS03840705 120030521A534036431121 FITTING DOUG DC8 DC871F 302199DWP SUBFLOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, LT SIDE STA 800 ON SUBFLOOR AFT OF FLOORBEAM AT LBL 60 THERE IS A CRACKED SUPPORT FITTING. REMOVED AND REPLACED FITTING IAW DWG 3643112 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612000972003061200097NM 2003 6 12 CALA0300272 120030530A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND FLOORBEAM T-CAP CORRODED ON TOP SIDE AND BOTTOM SIDE AT FS 986.5, LBL 25. THE FLOORBEAM WAS REPAIRED BY SPLICING IN A NEW SECTION IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030617000712003061700071EU 2003 6 17 AUS20030497 120030511A71101159P11505 COWLING FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY65015 54557NE NR 1 ENGINE BIRD STRIKE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BIRDSTRIKE ON LT SIDE OF FUSELAGE NOSE CONE. INSPECTION FOUND NR 1 ENGINE INTAKE AUCOUSTIC LINER LOWER PANEL DELAMINATED. SOME SHREDDED STRANDS OF THE LINER WERE FOUND ON THE FAN BLADES ANDTHE BYPASS DUCT. A BORESCOPE INSPECTION OF ALL STAGES OF THECOMPRESSOR AND TURBINE REVEALED NIL DEFECTS. 2L72 4F4 FRT E25NE 20030522000372003052200037NM 2003 5 22 0300866314 120030502A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT LOOSE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01674US 30269 DURING LINE CHECK FOUND RIGHT FLOOR PATH EMERGENCY LIGHTS INOP FROM ROWS 51-65. RESECURED WIRES, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040127002482004012700248SW 2004 1 27 AC2A092332 120031120A7810230063301101 EXHAUST STACK BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE ENGINE CRACKED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH 49037 844192 EXHAUST STACK IS CRACKED. REPLACED EXHAUST STACK 1G72 3U3 URTH9SW E1GL 20030523000862003052300086EA 2003 5 23 QXEA0300541 120030509A2430TRU3502 TRU CNDAIRCL600 CL6002C10 1390015EA ZONE 200 BURNED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09612QX 10042 SEA-STRONG ELECTRICAL SMELL EMITTING AROUND NOSE AREA. TRANSFORMER RECTIFIER UNIT 2 BURNED INTERNALLY. REMOVED AND REPLACED TRANSFORMER RECTIFIER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030523001182003052300118NM 2003 5 23 CALA0300250 120030514A2697 WIRE HARNESS BOEING737 737724 13844BYNM LT ENGINE WORN A CALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2754711 28782 THE FIRE FAULT LIGHT ILLUMINATED WHILE EN ROUTE FROM GCM TO IAH. THE AIRCRAFT WAS DIVERTED TO CUN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. TROUBLESHOOTING FOUND THE LEFT ENGINE CORE FIRE LOOP HARNESS WORN. THE CORE LOOP HARNESS WAS REPLACED IAW MM 26-11-02. IN ADDITION, THE ENGINE FIRE DETECTION UNIT AND FIRE CONTROL PANEL WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20030527000532003052700053NM 2003 5 27 CALA0300249 120030515A5320 STRIP BOEING737 737524 1384721NM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2746625 27529 INSPECTION FOUND A .25 INCH CRACK AT O/B CORNER OF RT WHEEL WELL FORWARD FAIRING AFT ATTACH STRIP. AN ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030528000162003052800016SW 2003 5 28 HEEA086581 120030422A6710214001347005 ACTUATOR BELL 412 412 1182202SW FLIGHT CONTROLS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 ROTARY ACTUATOR CAUSING BINDING IN CYCLIC FORE AND AFT CONTROLS. 1G72 4U H4SW 20030623000302003062300030EU 2003 6 23 USAASA03040 120030513A25972131631 WIRE AIRBUSA319 A319112 3930323EU CARGO BAY INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19743UW 1277 THE LEFT SIDE SLIDE CYLINDER ASSEMBLY WIRE PAW WAS FOUND BROKEN DURING C-CHECK INSPECTION. MAINTENANCE REPLACED THE LEFT SIDE SLIDE CYLINDER ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030624000042003062400004WP 2003 6 24 GTIA030374 120030512A3397 WIRE DOUG DC9 DC981 3022081WP EMERGENCY LIGHT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND EMERGENCY LIGHTS INOPERATIVE, ROW 1, 20, 29 AND 31. REPAIRED WIRES. (M) 2L72 4F A6WE 20030624000782003062400078SO 2003 6 24 SWIA200312074 120030605A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS FAILED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07293SW7147 7147 120320 ON DEPARTURE WITH FLAPS SET 15, RECEIVED CONTROL FAULT WARNING. RESET AS PER QRH. FLAPS OPERATED NORMALLY. REMOVED AND REPLACED ANNUNCIATOR IAW MM 27-50-05. OPS CHECKS GOOD. NO FAULTS FOUND. 2L72 4T RTA31SO 20030619000062003061900006SW 2003 6 19 HEEA087177 120030609A6330 GARLOCK SEAL BELL 206 206L3 1182108SW AFT SUPPORT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 GARLOCK SEAL LEAKING. REPAIRED. 1G71 3U H2SW 20030630000582003063000058NE 2003 6 30 ALGA087757 120030625A6520SB8207102 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL T/R GEARBOX LEAKING B ALGAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03717AL A12600090 760221 TAIL ROTOR GEARBOX INPUT SEAL LEAKED WHEN RUN-UP ON TEST STAND. 1G72 3U3 U H1NE E1GL 20030625000582003062500058 2003 6 25 03FDEA00779 420030520A2565 SLIDE AIRBUS300 A300B4605R 3930308EU DOORS FAILED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25657FE 748 WHILE PERFORMING W/C E65210-7-5000 PT 1 OPERATIONAL CHECK OF DOOR L1- DOOR SLIDE LACES FAILED. REMOVED AND REPLACED LT CREW/PAX ENTRY DOOR EMERGENCY EVACUATION SLIDE IAW A300600. 2L72 4F RTA35EU 20030718000222003071800022WP 2003 7 18 GTIA030472 120030512A5310 BEAM DOUG DC9 DC981 3022081WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 AFT PIT DOOR BEAM CORRODED. FORMED NEW DOUBLER. INSTALLED NEW REPAIR. (M) 2L72 4F A6WE 20030708000552003070800055EA 2003 7 8 SWIA200312092 120030605A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA ANGLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 625 STR 14L LT INTERCOSTAL ANGLE CRACKED. (DISCOVERED DURING C-CHECK) REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 600-35012-51 2L72 4F RTA21EA 20030717000212003071700021SW 2003 7 17 HEEA087998 120030622A6710407001523101 IDLER ASSY BELL 407 407 1182206SW M/R CONTROL RATCHETING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR CONTROL IDLER ASSY HAS BEARINGS RATCHETY. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030127000392003012700039 2003 1 27 HEEA083616 420030114A2562110324 ANTENNA BELL 407 407 1182206SW ELT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 ELT ANTENNA WHIP BROKEN. SCRAPPED. 1G71 3U O H2SW 20030204000582003020400058NM 2003 2 4 SWAA030170 120030123A32306558206 SENSOR BOEING737 7373H4 1384600NM RT MLG W/W OUT OF ADJUST A SWAAD RETURN TO BLOCK S AFFECT SYSTEMS CLCLIMB 1 SW29614SW 28033 AIR TURNBACK, LANDING GEAR LEVER WOULD NOT GO UP PAST THE OFF POSITION. TAKEOFF WARNING HORN SOUNDED. MX FERRY TO MDW, AND ADJUSTED GROUND SHIFT AIR SENSOR CABLE ASSY PER MM. 2L72 4F RTA16WE 20030204000732003020400073NM 2003 2 4 SWAA030156 120030121A53306552988 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29081SW 22730 DURING SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED, BS 943, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030206001472003020600147NM 2003 2 6 03FDEA00027 120030115A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION ON LOWER FLOORBEAM CHORD, AROUND NUTPLATES, STA 1130 0 BL, RBL 48, WL 200. REPAIRED FLOORBEAM BS 113 WL 200 IAW EA 7-5310-68165. 2L73 4F4 FRTA3WE E2EA 20030314000272003031400027NM 2003 3 14 03FDEA00080 120030127A5510ALC81072 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT HORIZONTAL STAB NR 26 BARREL NUT HOLE FOUND FITTING WITH CRACK. COMPLIED WITH FEDEX EA 1-5510-67565, STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE 26 RT FITTING FABRICATION. 2L73 4F RTA22WE 20030212000202003021200020NE 2003 2 12 AUS20030016 320030106A6114660714259 HUB SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R390 R3904123F27 NE PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1173 (AUS) PROPELLER HUB CRACKED IN AREA ADJACENT TO THE MOUNTING BOLT HOLE NEXT TO NR 2 BLADE. FOUND DURING NDT INSPECTION. 2L72 4T4 TRTA52EU E8NE 6 CP31NE 20030116000882003011600088SW 2003 1 16 HEEA083047 120030107A6320212040149001 GEAR BELL 212 212 1181420SW M/R GEARBOX WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736D 31135 MAIN ROTOR GEARBOX GEAR HAS WORN WHERE SEAL RIDES. 1G71 4U H4SW 20030221000312003022100031EA 2003 2 21 QXEA0300139 120030119A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 CKB- CRACK INDICATED ON PRESSURE BULKHEAD AT STATION 1098.20 ON RIGHT HAND SIDE. REPAIRED IAW CRJ SRM 51-20-06, 51-21-16, 51-23-00, 51-42-21 AND REO 670-53-61-034. 2L72 4F RTA21EA 20030224000282003022400028NM 2003 2 24 F3LA200300075 120030219A5315 FLOORBEAM BOEING737 7372Y5 1384554NM STA. 312 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA. 312, LBL 13 TO RBL 10. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. FABRICATED AND INSTALLED NEW CAP PER SRM 53-10-1. 2L72 4U RTA16WE 20030228000232003022800023NM 2003 2 28 SWAA030383 120030217A53306552988 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED, BS 1013, BETWEEN STRINGERS 21L & 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030303000672003030300067NM 2003 3 3 SWAA030402 120030219A52406545871132 GUSSET BOEING737 7373G7 1384595NM SERVICE DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR INTERNAL GUSSET CRACKED AT AFT DOOR HINGE. REMOVED AND REPLACED FWD SVC DOOR PER MM. 2L72 4F RTA16WE 20030303000982003030300098SW 2003 3 3 HEEA084524 120030214A243230703001 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 MAIN BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030305000092003030500009 2003 3 5 HEEA084614 420030214A2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 VHF TRANSCEIVER HAS SCRATCHY SIDETONE. REPLACED Q109 AND Q110 TRANSISTORS AND Q110 TRANSISTOR SOCKET. REPAIRED. ALIGNED TRANSMITTER AND ADJUSTED CARRIER SQUELCH. REMOVED LIGHT CORROSION FROM UNIT. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000442003030600044SW 2003 3 6 HEEA084758 120030218A3210407030112103 FITTING BELL 407 407 1182206SW MLG CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 FITTING CHAFED FROM LANDING GEAR SHIFTING OVER. REPLACED FITTING. 1G71 3U O H2SW 20030311000292003031100029GL 2003 3 11 HEEA085046 220030228A724023030910 COMBUSTION LINER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 COMBUSTION CASE HAS STRIPPED THREADS IN IGNITER BOSS. REPAIRED. 1G71 3U3 U H2SW E1GL 20030313001192003031300119SO 2003 3 13 FQA2003F00002 120030213A5320620860023 CHANNEL PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA FUSELAGE CRACKED B FQARK NONE O OTHER ININSP/MAINT 1 WP07918PA3154 2843307 L3716136A DURING A HARD LANDING INSPECTION, A MECHANIC NOTED THE AFT STIFFENING CHANNEL, PN 62086-003 CRACKED ON THE LEFT, LOWER, SKIN NEAR THE WING ROOT. THE CRACK APPEARS OLD. THE LEFT WING FORWARD STIFFENING CHANNEL WAS NOT DAMAGED. 1L71 3O3 O 2A13 E286 20030313001762003031300176EU 2003 3 13 AALA20030131 120030131A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211404D 11355 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN FLIGHT ATTENDANT PANEL FLOOR PATH TEST LIGHT ASSEMBLY WILL NOT STAY ENGAGED. REPLACED AFT CABIN FLIGHT ATTENDANT PANEL FLOOR PATH TEST LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030121001892003012100189SW 2003 1 21 HEEA083336 120030109A243230135002 BATTERY BELL 206 206B3 1181506SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032268V 3605 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121002612003012100261NM 2003 1 21 PCAA0301005 120030104A3297 WIRE DHAV DHC8 DHC8102 2809003NM COCKPIT LOOSE A PCAAL ABORTED APPROACH O OTHER APAPPROACH 1 EA13841EX 249 BUF-LGA FLIGHT 3779 CREW REPORTED WHILE ON FINAL APPROACH FOR LANDING, GEAR WOULD NOT EXTEND. EMERGENCY DECLARED, AIRCRAFT PERFORMED GO-AROUND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE, AND BLED HYDRAULIC SYSTEM. LEAK CHECK GOOD. A LOOSE WIRE WAS FOUND ON LANDING GEAR INHIBIT SWITCH IN COCKPIT. CONNECTION FOR WIRE TIGHTENED ON SWITCH AND SWITCH TIGHTENED IN PLACE. GEAR CYCLED SEVERAL TIMES UP AND DOWN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030318000212003031800021 2003 3 18 BAQA085096 420030306A3421C17027AA01 INDICATOR UROCOPEC135 EC135T1 5620026EU ATTITUDE OUT OF TOLERANCEH BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01575ME1618 0157 ADU 3000 FAILS FAR 91-411 CHECK. ALTITUDE OUT OF LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030319001032003031900103NM 2003 3 19 UPS03240305 120030217A5720 PANEL BOEING727 727108C 1384039NM #10 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI DELAM ON R/H WING TE PANEL UPPER FWD OF NO 10 SPOILER PANEL REPAIRED IAW SRM 51-40-5 2L73 4F A3WE 20030320001602003032000160NM 2003 3 20 2003UALA00153 120030206A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29952UA 26699 CABIN FLOOR INTERCOSTAL UPPER FLANGE CRACKED AT FASTENER HOLES, STA 927-947 AT CENTERLINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20030122001732003012200173 2003 1 22 HEEA083541 420030113A2300N0001553 ANTENNA SKRSKYS76 S76A 8143006NE COMMS SYSTEM CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 OUTERLINK TRANSMIT ANTENNA FULL OF WATER AND DOES NOT TRANSMIT. REPLACED ANTENNA. 1G72 3U H1NE 20030416002742003041600274NM 2003 4 16 QXEA0300441 120030410A3260301450201 SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09404QX 4046 LANDING GEAR WILL NOT RETRACT. REMOVED AND REPLACED NOSE WHEEL CONTROL PROXIMITY SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417001422003041700142NM 2003 4 17 QXEA0300243 120030202A5210 HANDLE DHAV DHC8 DHC8202 2809007NM ZONE 800 LACK OF LUBE A QXEAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 NM09369PH 513 PDX ON FLIGHT 2283- MAIN CABIN EXIT DOOR HANDLE IS HARD TO OPEN. CLEANED AND LUBED SEAL AND STOPS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030418001392003041800139NM 2003 4 18 QXEA0300297 120030221A523085237600001 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DAMAGED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09405QX3531 4047 PDX - FLIGHT 2307 - THE AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE AFT CARGO DOOR WARNING ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE HANDLE AND LATCH ASSEMBLY. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421000562003042100056WP 2003 4 21 MWEA030120 120030228A8010 WARNING LIGHT DOUG DC9 DC932 3022066WP START VALVE ILLUMINATED A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31216ME 47740 RT START ENGINE VALVE ANNUNCIATOR STAYED ON. VERIFIED VALVE CLOSED, LIGHT IN COCKPIT OUT, COULD NOT DULPICATE AT THIS TIME. 2L72 4F A6WE 20030421001122003042100112EU 2003 4 21 MALA030186 120030303A3260 UPLOCK SWITCH SAAB SF340 SF340A 7850100EU MLG FROZEN A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL1527XJ 340A027 DURING FLIGHT 3329, GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH WHEN GEAR SELECTED UP POSITION HYDRAULIC PUMP SEEMS TO WORK NORMALLY. MAINTENANCE FOUND LT MAIN GEAR UPLOCK SWITCH FROZEN. CLEANED SWITCH, CYCLED LANDING GEAR 5 TIMES IAW SAAB AMM 32-30-00. ALL CHECKS GOOD. 2L72 4T RTA52EU 20030718000472003071800047NM 2003 7 18 AUS20030544 120030408A5311 FRAME BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAMES CRACKED AT PSU ATTACHMENT POINTS. A TOTAL OF ELEVEN FRAMES CRACKED ON LT SIDE AND SEVEN FRAMES ON THE RT SIDE. FOUND DURING EDDY CURRENT INSPECTION IAW EI 737-53-61R1. 2L72 4F4 FRTA16WE E21EU 20030423000252003042300025EU 2003 4 23 AUS20030306 120030305A324434X10751612 TIRE FOKKERF27 F27MK50 EU PWA PWA120PW125B NE MLG PUNCTURED W O OTHER O OTHER LDLANDING 1 AUS (AUS) MAIN LANDING GEAR TIRE FLAT. SUSPECT TIRE HAD BEEN PUNCTURED DURING TAKEOFF. 2H72 4T4 TRTA817 E20NE 20030423001022003042300102EU 2003 4 23 U30A200300003 120030129A5210 SEAL AIRBUS320 A320212 3930322EU PAX DOOR BOTTLE DAMAGED A U30AK NONE O OTHER ININSP/MAINT 1 EA17265AV 427 DURING WEEKLY INSPECTION AFTER FLT 315 IN BWI, THE R2 CREW PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. REPLACED SEAL P/N FE240-221-001 AND ASSOCIATED PACKINGS I/A W AMM 52-10-000-610. SERVICED TO CORRECT PRESSURE I/A/W AMM 52-10-00-614-001. 2L72 4F RTA28NM 20030424000412003042400041NM 2003 4 24 QXEA0300343 120030308A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261LT, AFT FLANGE BETWEEN CAMLOCK HOLES 1-5. REPAIRED IAW HORIZON AIR EA 6-57-122 AND RD 8/4-57-144. 2H72 4T RTA13NM 20040225000912004022500091GL 2004 2 25 HEEA092085 220031210A73210164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL NR 2 ENGINE FAILED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322342 760096 NR 2 ENGINE HAD HIGH SIDE GOVERNOR FAILURE. MAINTENANCE REPLACED THE FUEL CONTROL UNIT. 1G72 3U3 U H1NE E1GL 20030828000702003082800070NM 2003 8 28 DL777030635 120030712A3610 CONTROLLER BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 2 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27877DA5345 051361 29739 051361 ENROUTE, BLEED OFF LT ENG EICAS MSG ILLUMINATED, REPLACED THE LEFT HIGH PRESSURE FAN AIR CONTROLLER AND THE LEFT MANIFOLD DUAL TEMP SENSOR (M36004). RAN THE ENGINE AT HIGH POWER ALL CHECKS WERE NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK. 2L72 4F4 FRTT00001SEE00050EN 20030829001112003082900111NM 2003 8 29 SWAA031879 120030820A335010126011 LIGHT BOEING737 7373Y0 1384671NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030722001112003072200111NM 2003 7 22 AWXA200300726 120030509A575465C26603102 SKIN BOEING737 7373G7 1384595NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-13 CHECK 6 EACH CRACKS WERE FOUND BETWEEN FASTENERS ON NR 4 LEADING EDGE SLAT LOWER SKIN AT SLAT ACTUATOR. MAINTENANCE CUT OUT CRACKED AREA OF LOWER SLAT SKIN; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 PG 216-219. 2L72 4F RTA16WE 20030813000612003081300061NM 2003 8 13 UPS03440833 120030519A5315 FLOORBEAM BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, BULK CARGO STA 2040 LBL 60 - RBL 60 FLOORBEAM STRAP FOUND CORRODED AT UPPER AND LOWER SURFACE. DEFECT TRANSVERSE FLOORBEAM REMOVED AND SERVICABLE FLOORBEAM REPLACED PER SRM 51-10-01 PG 8, CORROSION BLEND OUT (0.020 INCH X 1 X 4 INCH). 2L74 4F RTA20WE 20030723000162003072300016WP 2003 7 23 GTIA030486 120030627A7920 LINE DOUG DC9 DC982 3022082WP ENGINE OIL LEAKING A GTIAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23801NK 48048 RT ENGINE WAS LOSING OIL PRESSURE AND QUANTITY. FOLLOWED QRH PROCEDURES SHUT DOWN ENGINE. OIL PRESSURE AT SHUTDOWN 30 PSI OIL TEMP AT SHUTDOWN 135 DEGREES, OIL QTY AT SHUTDOWN 5 QUARTS, OIL PRESSURE WINDMILLING 2 PSI, OIL QUANTITY WINDMILLING 4 QUARTS. FOUND CRACKED FLARE AT OIL LINE FROM OIL BYPASS SWITCH. REPAIRED THIS. MOTORIZED ENGINE WITH REMAINING OIL QUANTITY AND ACHIEVED 30 PSI, ALSO REMOVED OIL FILTER NO CONTAMINENTS FOUND AND REPLACED WITH NEW FILER, SERVICED ENGINE OIL TO FULL QUANTITY AND RAN ENGINE. NO LEAKS AND ALL PARAMETERS NORMAL INDICATIONS. (M) 2L72 4F A6WE 20030825000342003082500034WP 2003 8 25 UPS03840969 120030709A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP CARGO BAY DEFECTIVE A IPXAK NONE N FALSE WARNING NRNOT REPORTED 1 SO01814UP 46090 INSPECTION TYPE:N/A CARGO SMOKE WARNING INDI FOR POS NR 6, NO EMERGENCY DECLARED, NO ODOR OR VISUAL SMOKE. REMOVED AND REPLACED NR 6 SMOKE DETECTOR. OPS CHECK NORMAL. 2L74 4F RT4A25 20030910000542003091000054WP 2003 9 10 DHL2003604540 120030428A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING OUTBOARD L/E UPPER SKIN SHOWS INTERIM REPAIR, XFS 766.250 - XFS 778.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED AREA AND INNER PART OF DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-1 PG 38, SRM 51-1-20D, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910001262003091000126 2003 9 10 GLBA2003108 420030719A3418 STALL WARNING EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM0396ZK 120096 STALL WARNING SOUNDS CONTINUOUSLY, R&R AURAL WARNING UNIT OPS CK GOOD 2L72 4T RTA31SO 20030911000432003091100043NM 2003 9 11 DHL2003741005 120030718A2611 SMOKE WARNING BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE COCKPIT FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING APAPPROACH 1 SO01741DH 21931 CARGO SMOKE LIGHT ILLUMINATED ON FINAL APPROACH. PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE OK FOR SERVICE. CARGO LIGHT IS NOT ILLUMINATED. 2L73 4F4 FRTA3WE E2EA 20030911001412003091100141WP 2003 9 11 DHL2003873611 120030704A5313S1616757 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FUSELAGE TAIL SECTION INTERIOR L17R CRACKED 2.000 AT STA 1771-000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030910001622003091000162EU 2003 9 10 ASOA03359 120030807A5260S5217640802000 STEP AEROSPATR72 ATR72 EU PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING AN A-CHECK IN MCN, THE SECOND AND THIRD PASSENGER DOOR STEPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE SECOND AND THIRD PASSENGER DOOR STEPS IAW SRM 51-12-00. (M) 2H72 4T RT 20030912001532003091200153NM 2003 9 12 AWXA200300906 120030725A53206546592 PANEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MINOR REPAIR - DURING C-17 CHECK A 2.2 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT TRANSITION PANEL AT BS 787-813. MAINTENANCE REMOVED DAMAGED SECTION OF TRANSITION PANEL AT BS 787-813; FABRICATED A NEW REPLACEMENT SECTION OF TRANSITION PANEL PER DWG 69-43477; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-15, FIG 101, DETAIL 10. 2L72 4F RTA16WE 20030929000802003092900080NM 2003 9 29 03FDEA01443 120030830A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING O/B FLAP O/B HINGE (FLAP SIDE) LOWER ATTACHMENT BORE FOUND CORRODED. 2L73 4F RTA22WE 20031001000152003100100015WP 2003 10 1 ARWA20030905 120030906A5420 ANGLE DOUG DC8 DC861 3021952WP SPAR CAP CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1929UA 46159 DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON STUB WING BELOW LT SPAR CAP (Z) ANGLE WITH CRACK. 2L74 4F 4A25 20031001001012003100100101WP 2003 10 1 AMTA200301100 120030813A5313 LONGERON LKHEED1011 10113851 5265010WP FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND LONGERON 30 CORRODED AT APPROX FS 1808 JUST FWD OF APB FRAME. REPAIRED STRINGER IAW SRM 53-13-00 SEE PARTAIL ACCOMPLISHED AND ATTACHED M12A. (M) 2L73 4F A23WE 20031007000122003100700012NM 2003 10 7 AALA20030700 120030628A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21621AM 24579 DURNIG OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 27D INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 27D. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031003000652003100300065SO 2003 10 3 C2XA03SH328 120030913A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE CENTER FLOORBEAM BETWEEN FRAMES 18 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031015000382003101500038EU 2003 10 15 ASOA03446 120030905A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING A C-CHECK IN BNA, THE RT SEAT TRACK AT FS 39 TO FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACK AT FS 39 TO FS 40 IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20031023000572003102300057SO 2003 10 23 SWIA200312447 120030923A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RUDDER MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07224SW8889 8889 120294 ON CLIMBOUT RIGHT RUDDER PEDDLE FROZE. RAN QRH, TURNED OFF BLUE SYSTEM AND REGAINED CONTROL. REPLACED UPPER RUDDER ACTUATOR IAW 27-22-02. LEAK AND OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031022000562003102200056NM 2003 10 22 QXEA200301157 120030916A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 LOWER FUSLEAGE SKIN IS SCRATCHED AT LEFT HAND STRINGER 27, 6 INCH AFT OF X38.4. REPAIRED IAW Q400 SRM 51-26-10, 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801 AND RD 8/4-53-666. 2H72 4T4 TRTA13NM E00062EN 20031027000072003102700007WP 2003 10 27 MWEA030393 120030925A53133924810510 LONGERON DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31209ME 47730 WHILE REPLACING DOME NUTS FOR FUSELAGE FILET PANEL, FOUND SUSPECT CRACK ON AFT END OF LONGERON 26 RT FRAME STATION 604. FABRICATED AND INSTALLED FITTING. 2L72 4F4 F A6WE E2EA 20031028000642003102800064NM 2003 10 28 VNAA0309013 120030921A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07430JS2034 588 3044 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 9 AND 10 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040210000192004021000019WP 2004 2 10 UPS03841593 120031118A53403779762U601 FITTING DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 680 LONG. 5L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG.3779762 AND SRM. 51-1-20D. 2L74 4F RT4A25 20031030000022003103000002EU 2003 10 30 KBM2003F00032 120030908A5540 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE RUDDER WORN E KBMAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 WP19230SH 2337 HIGH FREQ VIBRATION IN PEDALS. INSPECTED FOUND TROS BEARING, NR 1,2,3,5 HAS EXCESSIVE PLAY. REPLACED WITH NEW PN 704A33-698-027, FA3819, PN 593404 REPLACED WITH NEW, PN 704A33-698-027 BEARING, FA 3819 RUBBER, PN 593404 BEARING (K) 1G71 3U3 UNCH9EU E19EU 20031029000422003102900042NM 2003 10 29 ASAA0310431 120030512A5320BAC1509100146 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 859, STRINGER 3L CORRODED. REPLACED SUPPORT ANGLES PER SRM. (M) 2L72 4F A16WE 20031106002412003110600241WP 2003 11 6 GTIA030396 120030508A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND FLOOR WEB CORRODED AT BOTTOM OF L2 DOOR STATION 1136-1174 (2) Z-ANGLE BRACKETS CORRODED TWO EACH. CUT OUT FLOOR WEB. FABRICATED FILLER AND DOUBLER. INSTALLED DOUBLER REPAIR AND FILLER. (M) 2L72 4F A6WE 20031117000732003111700073SW 2003 11 17 ALG2003F00086 120030830A2435200SGL111Q STARTER GEN BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031078N 45389 CAE860266 COMING TO A HOVER FOR TAKE OFF. N2 DROOPED TO 94 PERCENT AT 50 PERCENT TORQUE AND STAYED THERE FOR 15 SECONDS. ABLE TO RECOVER BY BEEPING. BEFORE HOVER, N2 WAS STABILIZED AT 100 PERCENT. MAINTENANCE REPLACED STARTER GENERATOR. 1G71 3U3 U H2SW E1GL 20040112000892004011200089NM 2004 1 12 AWXA200301579 120031208A53206517684638 INTERCOSTAL BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR FORWARD INTERCOSTAL AT BS 294.5, STR 12 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT L-1 DOOR BS 294.5, STR 12 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 8, 12 & 14. 2L72 4F RTA16WE 20040112001042004011200104SO 2004 1 12 C2XA03CL207 120031221A335020131A BATTERY EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHTS FROM ROW 8 TO 12 WERE DIM. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031119000492003111900049NM 2003 11 19 CALA0300582 120031010A5210 STOP FITTING BOEING737 7373T0 1384582NM L-1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR UPPER AFT STOP FITTING. THE STOP FITTING WAS REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20031118000952003111800095CE 2003 11 18 55032 120031007A2820 LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA P3 SUPPLY LOOSE A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CE07190YV UE190 ODOR OF FUMES FROM COCKPIT. TIGHTENED RT ENG P3 SUPPLY LINE B NUT. OPS CK NORMAL. NO FUMES NOTED 2L72 4T3 TRTA24CE E2NE 20040113001762004011300176EU 2004 1 13 MALA030569 120031221A243523080031 STARTER GEN SAAB SF340 340B 7860101EU RIGHT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15360PX 340B220 DURING FLIGHT 2745, RIGHT GENERATOR FALLING OFF LINE AND NOT RESETTING. AIR RETURN TO MSP. MAINTENANCE REPLACED RIGHT DC STARTER/GENERATOR P/N 23080-031, S/N ON 6931, S/N OFF 4515. 2L72 4T RTA52EU 20040114000092004011400009NM 2004 1 14 03FDEA01927 120031117A5510ALC81072 FITTING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STABILIZER RT UPPER CENTER PLANK NR 26R BARREL NUT BORE FOUND CORROSION ON BOTTOM AND SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. NEW 26R FITTING FABRICATED AS PER DWG ALC8107 AND EA 1-5510-74245, HORIZONTAL STABILIZER BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. DAMAGED 26R FITTING ON HOR STAB RH UPPER CENTRE PLANK 26R REMOVED & REPLACED AS PER SRM 51-33--01 VOL2. 2L73 4F4 FRTA22WE E13NE 20031218000682003121800068SO 2003 12 18 C2XA03TY200 120031202A574014569009407 FITTING EMB 135 EMB135ER 3260203SO LT AILERON WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717507 145215 DURING A SCHEDULED INSPECTION THE LEFT HAND AILERON PCA INBOARD ATTACH FITTING FLANGE HOLE WAS WORN OUT OF ROUND. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND AILERON PCA ATTACH FITTING IAW EC 5750-01177 AND CPM 51-21-05/06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031217001172003121700117NM 2003 12 17 2003UALA00856 120031107A5740113W70036 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE ACTUATOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 AILERON ACTUATOR FITTINGS CRACKED. REPLACED ACTUATOR FITTINGS. 2L72 4F4 FRTT0001SE E46NE 20031219001382003121900138NM 2003 12 19 03FDEA02119 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031223000612003122300061NM 2003 12 23 ABXA030461 120031210A2150 ACM BOEING767 767231 1385131NM AIR CONDITIONER CONTAMINATED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL23709AX 22572 AIR CONDITIONING SYSTEM HAD A STRONG GLUE TYPE ODOR, ESPECIALLY DURING DESCENT. ODOR WAS THERE WITH APU OR ENGINES SUPPLYING AIR. FOUND ODOR TO BE AN OIL TYPE ODOR FROM ACM'S. PERFORMED STEPS TO REMOVE OIL CONTAMINATION FROM AIR CONDITIONING SYSTEM IAW B767 21-00-21-2. NO ODOR DETECTED AFTER PURGING SYSTEM. 2L72 4F RTA1NM 20031223000932003122300093NM 2003 12 23 SWAA032704 120031210A575365C26602 WEDGE BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND NR 5 T/E FLAP WEDGE OUTBOARD END DELAMINATED. REPAIRED WEDGE PER SRM. 2L72 4F RTA16WE 20031224000142003122400014EU 2003 12 24 USAASA03129 120031114A3222D23592000 SHOCK ABSORBER AIRBUSA319 A319112 3930323EU NLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19700UW 0885 AFTER TAKEOFF, THE NOSE LANDING GEAR WOULD NOT RETRACT. CREW RECEIVED ECAM MESSAGES 'SHOCK ABSORBER FAULT' AND 'SYS DISAGREE'. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR SHOCK ABSORBER. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031229001652003122900165NM 2003 12 29 03FDEA02206 120031217A2810 SKIN BOEING727 727200 138407ENM FUEL TANK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION WHILE WORKING FLOOR CLOSE FOUND CORROSION ON CENTER TANK SKIN BS 825 LBL 10. 2L73 4F RTA3WE 20031231000052003123100005EA 2003 12 31 ASOA03564 120031103A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11926EV 7843 DURING TAKEOFF, AT APPROX 1,000 FEET AFTER SELECTING THE FLAPS FROM EIGHT DEGREES TO ZERO DEGREES THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW REQUESTED EMERGENCY EQUIPMENT STANDBY AS A PRECAUTION AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT BRAKE AND POSITION SENSOR UNIT, AND ALSO PREFORMED OPS CHECK OF THE FLAPS SYSTEM FOR APPROX FIFTEEN MINUTES WITH NORMAL RESULTS. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031010000802003101000080NM 2003 10 10 0301776310 120030917A3320 LIGHT BOEING747 747451 1384940NM CABIN ODOR A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01670US 24225 DURING FLIGHT, AN ELECTRICAL BURNING ODOR EMITTED IN THE AREA OF 4B. THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPOSITIONED AND SECURED THE SLEEP LIGHT ABOVE DOOR 1L THAT WAS COMING IN CONTACT WITH THE PLASTIC SURROUND. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031014000362003101400036EU 2003 10 14 MALA030379 120030819A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15366PX 340B267 DURING 4K INSPECTION IN CWA, LT CENTER FWD SEAT TRACK ASSEMBLY HAS CORROSION OUT OF LIMITS. MAINTENANCE REPAIRED DAMAGED SECTION OF SEAT TRACK IAW EO NR S53060 LBL 18.5 AT STA 297 TO STA 329. A/C RELEASE DATE IS 8/11/03. REFER TO 409 NR 192875 FOR DETAIL. 2L72 4T RTA52EU 20031010000972003101000097EU 2003 10 10 BAQA089523 120030930A243245043006 BATTERY UROCOPEC135 EC135T1 5620026EU MASTER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03485AE15 0273 ENGINE WILL NOT START ON BATTERY POWER. BOX WILL NOT TEST. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031126000772003112600077SO 2003 11 26 C2XA03SH428 120031104A532014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK, THE CENTER BUTTSTRAP WAS FOUND TO CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-24-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031203000572003120300057NM 2003 12 3 GAIA03144ST 120031024A5347BAC1520841 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK LBL 45.5 CORRODED BS 760 TO 850. REF FASI N/R NR 61760, REPLACED SEAT TRACK BS 760 TO 850 LBL 45.5 PER B727 SRM 53-10-5 FIG 7 AND 53-10-2 FIG 7. (M) 2L73 4F RTA3WE 20031203000762003120300076EA 2003 12 3 2003F00621 120031004A7830MS244236 ISOLATION VALVE CNDAIRCL600 CL6002D24 EA THRUST REVERSER MALFUNCTIONED A FDKAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07904FJ 15006 CREW ABORTED TAKEOFF DUE TO RIGHT REVERSER UNSAFE CAUTION MESSAGE. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 ENGINE T/R ISOLATION VALVE. (M) 2L72 4F RTA21EA 20040122000792004012200079WP 2004 1 22 GTIA030962 120031109A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND CABIN STATON 160-200 LBL 54 FLOOR SUPPORT GOUGED AND CORRODED AT AFT EDGE. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20031204000912003120400091WP 2003 12 4 UPS03841402 120030909A532037558411 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT PIT AT STA 1220 STR 34R INSIDE TORQUE BOX AREA FITTING CRACKED. REMOVED FITTING CRACKED IAW DC8 SRM 51-1-20D, REC'D NEW Z-FITTING AND 2 EA PLATES P/N 3755841-1, P/N 3755841-3, P/N 3755841-5. LOCATED, DRILLED, AND TRIMMING IAW DC8 SRM 53-2-0, AND 51-1-20D. INSTALLED Z-FITTING AND PLATES IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20031205000452003120500045GL 2003 12 5 DL764030935 220031018A7320731003363 HYDROMECH UNIT BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 1 ENGINE FAILED A DALAO OTHER J WARNING INDICATION DEDESCENT 1 SO27844MH 29717 706431 ON DESCENT L ENGINE CONTROL MSG DISPLAYED. T/S PER FIM 73-21-00 FIG 112 AND 71 PIMU MESSAGES PAGE 27. FOUND CODE 155 - 23 A/B. REMOVED HMU PER AMM. REPLACE LT ENGINE MNU AS PER MM RAN ENG AT IDLE NO MSG. NO LEAKS F/O RAN ENG PER PFHB. 2L72 4F4 FRTA1NM E23EA 20031208000532003120800053NM 2003 12 8 03FDEA01787 120031021A5230 HINGE BOEING727 727200 138407ENM CARGO DOOR CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-5230-73214 DOORS - MAIN CARGO - WEAR/CHAFING ON 2 EACH LOBES OF MCD HINGE ASSY. COMPLIED WITH EA 7-5230-73214 DOORS - MAIN CARGO - WEAR/CHAFING ON 2 EACH LOBES OF MCD HINGE ASSY. 2L73 4F RTA3WE 20031210000142003121000014NM 2003 12 10 SWAA032613 120031128A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 EMERGENCY LIGHTS ILLUMINATED. REMOVED AND REPLACED LT AFT CABIN EMERGENCY LIGHT BASE PER MM. 2L72 4F RTA16WE 20031015000342003101500034EA 2003 10 15 ASOA03412 120030903A3350BF10044004 SIGN CNDAIRCL600 CL6002B19 1900309EA CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT SIGN AT ROW 1 A/B WAS FOUND MISSING. MAINTENANCE INSTALLED AN EMERGENCY EXIT SIGN AT ROW 1 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040129000022004012900002EA 2004 1 29 COMA036573 120031213A5320601R35031211 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01809CA 7366 LEFT HAND 621 FLOOR SUPPORT ANGLE CRACKED. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-117. 2L72 4F RTA21EA 20040130000392004013000039NM 2004 1 30 SWAA032833 120031229A53126545819 PRESSURE PANEL BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND NLG W/W LT SIDEWALL CRACKED BELOW ACCESS PANEL AT BS 247. REPAIRED WEB PER SWA EA. 2L72 4F A16WE 20040203003372004020300337EA 2004 2 3 MASA200300511 120031224A5210 DOOR CNDAIRCL600 CL6002D24 1390016EA MAIN PAX STUCK A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07907MJ 15007 ASH 6223 AUS-PHX, THE AIRCRAFT ARRIVED IN PHX AND THE F/A COULD NOT OPEN THE DOOR FROM THE INSIDE, SO GROUND SERVICE PERSONNEL OPENED IT FROM THE OUTSIDE. LAST FLT OF THE NIGHT, SO AIRCRAFT WENT TO MX AND WILL BE WORKED WITH OVERNIGHT MX. MX COULD NOT DUPLICATE. OP CHECKS GOOD. 2L72 4F RTA21EA 20040212000662004021200066CE 2004 2 12 V9B2003F00004 120031124A2612 WARNING LIGHT LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE7313 01518WP RT ENGINE FIRE ILLUMINATED E V9BAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05120LJ 120 PILOT REPORTED MASTER WARNING LIGHT TO RT ENGINE FIRE LIGHT CAME ON AFTER TAKE-OFF. THE POWER WAS REDUCED AS OUTLINED IN THE AFM BUT THE FIRE LIGHT DID NOT GO OUT. THE FIRE EXTINGUISHER WAS FIRED AND THE PILOT RETURNED TO THE AIRPORT. 2L72 4F4 F A10CE E6WE 20031211001122003121100112EU 2003 12 11 AALA20031296 120031118A3020 ANTI-ICE VALVE FOKKERF28 F28MK0100 4990807EU NR 2 ENGINE FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW211409B 11367 STL EN ROUTE MDW-DFW NUMBER 2 ENGINE ANTI ICE FAULT LIGHT ON. LANDED STL WITHOUT INCIDENT. OPENED NUMBER 2 ENGINE ANTI ICE ACCESS AND FOUND VALVE NOT FULLY OPENED. REPOSITIONED NUMBER 2 ENGINE ANTI ICE VALVE TO FULL OPEN POSITION AND PINNED OPEN PER MEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20031211001462003121100146WP 2003 12 11 AALA20031272 120031115A335060030451 BATTERY DOUG DC9 DC982 3022082WP TAIL CONE DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21580AA 53157 DFW TAIL CONE ILLUMINATION EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY FOR TAIL CONE ILLUMINATION EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001482003121100148WP 2003 12 11 AALA20031274 120031116A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21598AA 53288 STL ROW 16 INSEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED ROW 16 INSEAT EMERGENCY LIGHTS BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20031215001482003121500148WP 2003 12 15 AALA20031209 120031103A3350 CONNECTOR DOUG DC9 DC983 3022083WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219621A 53592 DFW - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD OVERHEAD EMERGENCY AISLE LIGHT INOPERATIVE ON AFT AISLE GANGWAY. REPAIRED QUICK DISCONNECT ASSEMBLY FOR FORWARD OVERHEAD EMERGENCY AISLE LIGHT IN AFT AISLE GANGWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20040308001642004030800164NM 2004 3 8 ASAA0380697 120031025A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 SAN PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FLASH INTERMITTENTLY IN 1ST CLASS CABIN. REPLACED BATTERY PACK ABOVE SEAT 2E. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040316000412004031600041NM 2004 3 16 ASAA0310546 120031010A33508821004 BATTERY PACK BOEING737 7372Q8C 138448SNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 SEA - DURING SCHEDULED MAINTENANCE INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING AT SEAT PALLETS 1-11, 3-3 AND 9-2 INOPERATIVE. REPLACED BATTERY PACKS, THEN FLOOR TRACK LIGHTS TESTED NORMAL. (M) 2L72 4F A16WE 20030814000542003081400054NM 2003 8 14 UPS03M40953 120030604A5754 RIB DOUG MD11 MD11F 3023600NM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 INSPECTION TYPE:C, RT NR 08 SLAT FOUND NR 16 SLAT TRACK AT X0598.0 WITH I/B SUPPORT RIB CRACKED AS MARKED. CRACKED SUPPORT RIB RT NR 08 SLAT XOS98.0 REMOVED IAW SRM 51-35-01V2.R 33. INSTALLED NEW SUPPORT RIB PER SRM 51-35-01 & 51-33-01 V2.R33. 2L73 4F RTA22WE 20030814000782003081400078EA 2003 8 14 SWIA200312190 120030604A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 ANGLE AT FS 621 TO 625 AT STR 15S IS CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 PARA 4. P/N: 601-35012-41. 2L72 4F RTA21EA 20030819000972003081900097NM 2003 8 19 UPS03M41051 120030806A5610 WINDOW DOUG MD11 MD11F 3023600NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP CAPTAIN'S FORWARD WINDOW WILL NOT CLOSE. REPOSITIONED TRIM SLIDING CLEAR VIEW WINDOW AND AFT POST IAW MD11 M/M 56-12-01 STEP 3E9. WINDOW CLOSES NORMALLY NOW WITH NO PROBLEM NOTED. 2L73 4F RTA22WE 20030819002292003081900229NM 2003 8 19 CALA0300369 120030708A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717644 28905 INSPECTION FOUND FORWARD ENTRY AREA INTERCOSTAL CRACKED AT STA 344-360, BL 0. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-00. 2L72 4F RTA16WE 20030401000272003040100027EU 2003 4 1 ASOA03047 120030207A33507012210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11636AS 375 DURING A GROUND INSPECTION IN VPS, THE FORWARD EMERGENCY EXIT LAMPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXT LIGHT LAMPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030401000952003040100095NM 2003 4 1 DHL2003751005 120030205A2120 ODOR BOEING727 727264 138408MNM CABIN DETECTED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01751DH 22982 AFTER CLOSING MCD ON TAXI OUT IN MCI, AN ACRID ODOR BECOMES PRESENT IN COCKPIT, AFTER TURNING ON PACKS, ODOR REMAINS FOR 5-10 MINUTES. RETIGHTENED GROUND INTERCONNECT LINES, RAN PACKS FOR 30 MINUTES, NO ODOR DETECTED, OPS CHECKED NORMAL IAW M/M 21-21-0 & 20-80-01. 2L73 4F A3WE 20030403000272003040300027NM 2003 4 3 03FDEA00361 120030401A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION ON FLOORBEAM BS 1070 RBL 1 RBL 44, WL 201 AT FASTENER HOLES. REMOVED CORROSION ON LOWER FLOORBEAM BS 1070 RBL 1-44 AT FASTENER HOLES. ORIGINAL THICKNESS .130 REMOVED .010 MAX MATERIAL IN A 1 X 1 AREA RBL 1-RBL 26 & RBL 31-44 IN LIMITS PER SRM 53-10-1. REMOVED CORROSION ON BS 1070 FLOORBEAM RBL 27-30. ORIGINAL THICKNESS .130 REMOVED .053 MAX IN A 1.25 X 2.25 AREA OUT OF LIMITS PER SRM5 3-10-1. REMOVED DAMAGE RBL 27-31. FABRICATED AND DRILLED UP REPAIR PARTS. INSTALLED REPAIR PARTS AND FASTENERS WET WITH SEALANT ALL WORK ACCOMPLISHED IAW 727 SRM 51-10-8, FIG 8 AND 51-10-2. 2L73 4F RTA3WE 20030821001622003082100162NM 2003 8 21 03FDEA01026 120030701A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE AT FLAP SIDE INBOARD PIVOT LUG BORE OUTER SURFACE FOUND CORRODED. LEFT WING OUTBOARD FLAP INBOARD AFT HINGE AT FLAP SIDE INBOARD PIVOT LUG BORE OUTER SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-69352. 2L73 4F RTA22WE 20030404001472003040400147NM 2003 4 4 SWAA030502 120030305A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP ABOVE AFT SERVICE DOOR. REMOVED AND REPLACED BATTERY PACK AND LIGHT ASSY PER MM. 2L72 4F A16WE 20030410001792003041000179NM 2003 4 10 DHL2003741511 120030326A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, BS 521 - 530 LT BL 45 SEAT TRACK ARE GOUGED AT LOCK EARS. REMOVED DAMAGED SEAT TRACK AT BS 480-540 LBL 45 IAW B-727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK AND INSTALLED IAW B-727 SRM 53-10-5 FIG 7. 2L73 4F RTA3WE 20030416001042003041600104NM 2003 4 16 SWAA030783 120030408A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 887 AND BS 907, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030424002152003042400215WP 2003 4 24 UPS03840376 120030327A2611 SMOKE DETECTOR DOUG DC8 DC871F 302199DWP NR 3 INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01706UP 46056 NR 3 SMOKE DETECTOR DOES NOT TEST. RELAMPED, OPS CHECK GOOD. 2L74 4F RT4A25 20030428001632003042800163EA 2003 4 28 03098705 120030408A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 DURING MAINTENANCE INSPECTION, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030429000202003042900020NM 2003 4 29 P5CA0300799 120030130A5410 WEB BOEING747 747283B 1384867NM NR 1 NACELLE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 689169 NR 1 ENG LT C-DUCT LWR VERTICAL WEB CRACKED AND DELAMINATED. REPAIRED DUCT AS PER SRM 54-05-009. 2L74 4F A20WE 20030430002522003043000252NM 2003 4 30 SWAA030813 120030413A575465C26602 SKIN BOEING737 7373L9 1384470NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT OUTBOARD UPPER T/E WEDGE DELAMINATED. REPAIRED NR 5 L/E SLAT PER SRM. 2L72 4F RTA16WE 20030502001222003050200122 2003 5 2 SWIA200311876 420030412A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STICK SHAKER DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07910SW 7566 STICK SHAKER DOES NOT OPERATE CORRECTLY DURING TEST. REPAIRED WIRE TO LEFT STICK SHAKER. OPS CHECKED NORMAL. 2L72 4F4 FRTA21EA E15NE 20030505001322003050500132NM 2003 5 5 DHL2003741533 120030323A5343 BEAM BOEING727 727200 138407ENM MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, RT MLG BEAM OUTBOARD TO REAR SPAR SUPPORT FITTING IS CRACKED UPPER INBOARD CORNER OF THE CUTOUT. ROUND OUT REMOVAL AREA TO A .375 INCH RADIUS AND BLENDED OUT UPPER AND LOWER AREA OF DAMAGE WITH .3888 INCH DEPTH REMOVAL OF CRACK MATERIAL IAW S/B 727-57-167. HEFC INSP BLEND OUT PER B-727 NDT PT6 51-00-00 FIG 4. NO CRACK REMAINING, REMOVED AN ADDITIONAL .030 INCH OF MATERIAL TO ENSURE REMOVAL OF UNDETECTABLE REMAIN OF CRACK END IAW S/B 727-57-167. BARE METAL TREATED AND PRIMED IAW B-727 SRM 51-10-2. NOTE: AT APPROXIMATELY EVERY C-CHECK DO A CLOSE VISUAL AND EDDY CURRENT INSPECTION FOR FURTHER CRACKING IN THE CRACK REMOVAL AREA OF FITTING, SPAR WEB, AND FWD SUPPORT FITTIN2L73 4F RTA3WE 20030505001942003050500194SO 2003 5 5 C2XA03IA040 120030421A27613605401003 ACTUATOR EMB 145 EMB145LR 3260212SO SPEED BRAKE LEAKING A C2XAO OTHER K FLUID LOSS DEDESCENT 1 SW2713914 145430 IAH- FLIGHT 2751, THE CREW DECLARED EMERGENCY INTO IAH DUE TO NR 2 HYDRAULIC LOW QUANTITY AND LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 2 SPEED BRAKE ACTUATOR, SERVICED THE HYDRAULIC SYSTEM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030505001212003050500121EU 2003 5 5 AWXA200300405 120030404A5347D5311278220200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF RT INBOARD CABIN SEAT TRACK AT FORWARD END OF FR 20. MAINTENANCE REMOVED CORRODED RT INBOARD CABIN SEAT TRACK AT FORWARD END OF FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 28-30, 32, 39, & 41, FIG 12, 13, & 18. 2L72 4F RTA28NM 20030506002562003050600256WP 2003 5 6 AUS20030442 220030428A723031071521 IMPELLER SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UHR WP COMPRESSOR DAMAGED W O OTHER EC VIBRATION/BUFFET F.O.D. LDLANDING 1 AUS (AUS) LH ENGINE IMPELLER BLADES DAMAGED BY BIRDSTRIKE. 2L72 4T4 TRTA5SW E4WE 20030508001522003050800152NM 2003 5 8 QXEA0300514 120030418A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PANEL 261FT HAS CHAFE DAMAGE ON LOWER SURFACE. REPAIRED IAW RD 8/4-53-521, PAGES 4-5. 2H72 4T RTA13NM 20030507001622003050700162NE 2003 5 7 GTIA030139 220030312A7230798821002 BLADE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NR 1 ENGINE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23815NK 49415 NR 1 ENGINE 1 EA C1 BLADE HAS .2500 IN/ SQ CHIP OUT 2 INCHES FROM PLATFORM OF BLADE, 1 EA C1 BLADE HAS .3750 FLAT ON L/E 2 INCHES FROM PLATFORM OF BLADE. REMOVED AND REPLACED 4 EA BLADES FROM NR 1 ENGINE IAW MM. 2L72 4F4 FRTA6WE E2EA 20030513000862003051300086NM 2003 5 13 UPS03240667 120030411A5320 ANGLE BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, SURFACE CORROSION ON ANGLE AT LWR END OF BS 950 FITTING LT AT STR. 22 LT IN LT MLG WHEEL WELL. REPAIR CARRIED OUT IAW SMRO EO 2003025009. 2L73 4F A3WE 20030514001382003051400138NM 2003 5 14 SWAA031038 120030508A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 3, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030515000062003051500006EU 2003 5 15 03125316 120030505A3350S34C12ST6S0S0 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FORWARD LIGHTING TRACK SECTION. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030513001852003051300185EA 2003 5 13 SWIA200311894 120030402A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07587SW4060 4060 7062 STAB TRIM MACH WOULD NOT MOVE DURING FFOD. THEY WOULD ALSO AUTO DISENGAGE. REMOVED AND REPLACED HSTA AND MCU IAW CRJ MM 27-42-01 AND 27-42-05. 2L72 4F RTA21EA 20030513002982003051300298NM 2003 5 13 AALA20030223 120030222A3397 CONNECTOR BOEING737 737823 13844BZNM EMER LITE BATTERDISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21931AN 30079 DURING OVERNIGHT MIANTENANCE, EMERGENCY EXIT ILGHTS ON BOTH SIDES OF AISLE BETWEEN END OF FIRST CLASS AND FRONT OF COACH INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030602001492003060200149 2003 6 2 SWAA031137 420030520A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PERE MM. 2L72 4F RTA16WE 20030520000572003052000057NM 2003 5 20 AMTA200300511 120030416A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11527AT 30886 FORWARD (RED) EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD EGRESS LIGHT ASSY IAW MM 33-51-11-3. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030520001332003052000133NM 2003 5 20 2003F00266 120030124A5510 BEARING BOEING727 727222 1384073NM HORIZONTAL STABCRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CRACK ON VERTICAL STAB, RIGHT HORIZONTAL STAB HINGE BEARING. REMOVED AND REPLACED VERTICAL STAB, RIGHT HORIZ STABILIZER HINGE BEARING. (M) 2L73 4F A3WE 20030521000822003052100082WP 2003 5 21 DHL2003804910 120030127A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 460.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AND NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030520001522003052000152NM 2003 5 20 2003F00280 120030122A5315 FLOORBEAM BOEING727 727222 1384073NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CORROSION ON TOP OF BEAM IN CABIN FLOOR AREA AT STATION 950, RBL 30 TO RBL 42. REMOVED CORROSION. MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED DAMAGED AREA. TREATED AND PRIMED AREA. (M) 2L73 4F A3WE 20030609000462003060900046 2003 6 9 CALA0300260 420030521A2565D31393110 SLIDE BOEING757 757224 1384958NM RT OVERWING LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW271412015343 27562 THE RT OVERWING SLIDE PACK WAS FOUND UNLACED AT TOP DURING SYSTEM CHECK. THE SLIDE PACK WAS REPLACED IAW MM 25-65-00. 2L72 4F RTA2NM 20030610001212003061000121SW 2003 6 10 HEEA087018 120030604A6230406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH877 53038 DISSIMILAR METAL CORROSION DUE TO STAINLESS STEEL BUSHING IN ALUMINUM CASTING. TO BE SENT TO BELL FOR CREDIT. 1G71 3U O H2SW 20030611000082003061100008NE 2003 6 11 DTH2003F00001 220030512A73143029309001 PUMP DORNERDO32 DO328300 NM PWA 306 PW306B NE NR 2 ENG FUEL FAILED E DTHAO OTHER O OTHER NRNOT REPORTED 1 GL25328GT565 3183 PCECD0156 UPON INVESTIGATING A DUAL ENG, NO START. (FUEL CONTAMINATION PROBABLE CAUSE) PULLED ENGINE FUEL FILTERS AND FOUND NON METALLIC SHAVINGS IN THE RIGHT ENGINE FUEL FILTER. FOUND SHAVINGS TO BE COMING FROM FUEL PUMP ON HMV. FUEL PUMP HAD F.O.D. IN SIDE AT THE ENTRANCE OF THE IMPELLER. AFTER FURTHER INVESTIGATION, FOUND THAT THE FUEL PUMP HAD AN IMPELLER WHERE THE FUEL LINE CAME INTO WAS GOEN. TECH ON SITE TOOK PICTURES. SENT FULE FILTER AND FUEL PUMP OFF RIGHT ENGINE TO BE ANALIZED. 2H72 4T4 FRTA55NM E35NE 20030611001542003061100154NM 2003 6 11 P5CA0300881 120030524A242021B73D CONTROL UNIT BOEING747 747236B 1384804NM NR 1 ENGINE INOPERATIVE A P5CAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 WP23924FT 21730 RTB, NR 1 ENG GENERATOR FIELD LT NR 4 ADP INOP. NR 2 GENERATOR ALREADY ON DEFERRAL, 1-2ND RTB NR 3 GEN INOP. SWAPPED NR 1 & NR 2 GCU (NR 2 GEN DEFERRED) OPS NORMAL. CLEANED & RESEATED CONNECTORS FOR NR 4 ADP S/O VALVE, ADP OPS NORMAL 2ND RTB NR 3 ENG GENERATOR OPS CHECKED NORMAL ON ENG RUN. SWAPPED GLU'S FROM NR 2 GENERATOR (ON DEFERRAL) NR 1 GEN OPS NORMAL. NO FURTHER DISCREPENCIES. 2L74 4F A20WE 20030617000772003061700077EA 2003 6 17 QXEA200300659 120030523A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 CKB - RIGHT HAND PRESSURE BULKHEAD WEB BBL34-41 STRINGER 8-9 CRACKED. REPAIRED IAW CRJ 700 AMM 21-31-00-910-801-401 AND REO 670-53-61-034. 2L72 4F RTA21EA 20030523000542003052300054NM 2003 5 23 SWAA031115 120030517A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030527000142003052700014WP 2003 5 27 DHL2003801041 120030410A5751 STRUCTURE DOUG DC8 DC873F 302199FWP LT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING- LT AILERON T/E CRACKED 0.500 INCH BETWEEN STA XA 715.000 AND XA 780.000. REMOVED AILERON T/E (CRACKED) IAW SRM 51-1-21A PG 3-4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW T/E (2024-T3 AL0.020) IAW SRM 57-8-1 PG 8. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. INSTALLED NEW T/E IAW SRM 57-8-1 PG 8 AND SRM 51-1-21A PG 3-4. 2L74 4F RT4A25 20030527000432003052700043NM 2003 5 27 DL738030329 120030403A25307200775000 OVEN BOEING737 737832 13844CFNM AFT GALLEY SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO273767 30821 AFTER TAKEOFF AIRCRAFT FILLED WITH BURNING ODOR NR 1 OVEN IN AFT GALLEY WAS EXTREMELY HOT EVEN THOUGH OVEN WAS NOT IN USE PULLED C/B AND IT SLOWLY COOLED OFF AFTER 30-40 MIN. REPLACED OVEN. 2L72 4F RTA16WE 20030619000512003061900051SW 2003 6 19 HEEA087201 120030609A2420A700ZC7 RELAY BELL 206 206B3 1181506SW GEN RCR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 GENERATOR WILL NOT COME ON LINE. 1G71 3U H2SW 20030620000782003062000078NM 2003 6 20 USAA030075 120030515A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US50342 23311 FOUND SKIN CRACKED APPROXIMATELY 1 INCH, S23R BETWEEN FRAME 727D AND 727E. INSTALLED DOUBLER PER EA 87231. (M) 2L72 4F RTA16WE 20030623000392003062300039WP 2003 6 23 GTIA030346 120030508A5530 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 INTERNAL ANGLES ON DORSAL FITTINGS CRACKED BOTH SIDES, STATION 1437. REMOVED LEFT AND RIGHT INTERNAL ANGLES. LOCATED AND DRILLED NEW INNER ANGLE ON LEFT DORSAL FIN. INSTALLED LEFT AND RIGHT INNER ANGLES. (M) 2L72 4F A6WE 20030619000882003061900088 2003 6 19 HEEA086927 420030529A345713824120234 RECEIVER BELL 407 407 1182206SW GPS STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 PUSH BUTTONS STICKING. CLEANED ALL BUTTONS AND REPLACED CALC AND APT/VOR SWITCHES. REPAIRED. ALSO REPLACED BAD LENS AND SELECTOR KNOB. BENCH CHECK GOOD. 1G71 3U O H2SW 20030716000642003071600064NM 2003 7 16 2003F00421 120030313A2120 DUCT BOEING727 727222 1384073NM FS CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON HEATING AND AIR CONDITIONING DUCT AT BS 720E/D, STRINGER 12/13. STOP DRILLED CRACKS. FABRICATED DOUBLER. ALODINED, PRIMED AND INSTALLED DOUBLER AT FUSELAGE HEATING AND AIR CONDITIONING DUCT, RIGHT SIDE OF CABIN, BETWEEN STATION 720E AND 720D, AND STRINGER 12 AND 13. (M) 2L73 4F A3WE 20030709000562003070900056 2003 7 9 AALA20030614 420030523A3420FRD7705 INDICATOR BOEING767 767323 1385205NM COCKPIT FAILED A AALAO OTHER O OTHER CLCLIMB 1 SW21366AA 25193 FIRST OFFICERS HSI NAV DISPLAY INOPERATIVE. WHEN AIRCRAFT POWER SWITCHED TO APU DISPLAY CAME BACK ON. RE-RACKED FIRST OFFICERS HSI, OPS CHECK NORMAL. (M) 2L72 4F RTA1NM 20030710000892003071000089NM 2003 7 10 DHL2003746506 120030602A5710 ANGLE BOEING727 727224 1384076NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 DURING C-CHECK, N/R 54144 RT WING LEADING EDGE L-ANGLE IS CRACKED JUST INBOARD OF NR 4 KRUEGER FLAP AT L/E STA 130.7. NR 4 L/E FLAP REMOVED AND REINSTALLED ON NR 54306. REMOVED FASTENERS AND SUB-STRUCTURE FOR ACCESS IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED SECTION OF ANGLE AND FABBED NEW FROM 2024 T3 .040 PO 314696 DIM 10.5 INCH AND REPAIR ANGLE SAME MATERIAL DIM 9 INCHES IAW B-727 SRM 51-40-3 FIG 1 AND 57-20-2 FIG 1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 51-40-3 FIG 1. REINSTALLED SUB-STRUCTURE IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20030127000222003012700022 2003 1 27 HEEA083598 420030114A3442MI585200 INDICATOR BELL 412 412 1182202SW RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 RADAR DROPS OFF LINE AND THE TEST PATTERN TURNS BLUE. SHOP REPAIR. 1G72 4U H4SW 20030127002342003012700234SW 2003 1 27 HEEA083719 120030115A6730206076062107 SERVO BELL 407 407 1182206SW CYCLIC LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03498PH3602 53399 CYCLIC SERVO LEAKING. 1G71 3U O H2SW 20030131001782003013100178NM 2003 1 31 UPS03240125 120030110A5755 FITTING BOEING727 72722C 138400FNM #3 SPOILER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI ON #3 SPOILER ACTUATING QUADRANT DISCONNECTION #3 SPOILLER SUPPORT F ITTING FOUND TO BE CORRODED BEYOND THE LIMITS REPLACED FITTING IAW DRAWING 65-21622-22 & MM 20-10-05 2L73 4F A3WE 20030204000902003020400090NM 2003 2 4 SWAA030149 120030121A575365C3570328 FLAP BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBD T/E FORE FLAP LOWER SURFACE CRACKED. REMOVED AND REPLACED FLAP ASSY PER MM 2L72 4F RTA16WE 20030204002282003020400228NM 2003 2 4 SWAA030193 120030125A3350071701100 BATTERY BOEING737 7377AD 1384502NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29798SW 28436 DURING SCHEDULED RON, FOUND FWD RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030207000752003020700075NM 2003 2 7 DHL2003746001 120030206A2611 SMOKE DETECTOR BOEING727 727224 1384076NM A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01746DH 22252 1) LOWER CARGO FIRE DETECTOR.2) FOUND CODE A14836. REMOVED AND REPLACED SMOKE DETECTOR IAW B727 M/M SUPPLEMENTAL 26-16-01. TESTED IAW B727 M/M 26-16-00. OPS CHECKED NORMAL. 2L73 4F A3WE 20030212000942003021200094NM 2003 2 12 AWXA200300119 120030206A531369353521 TIE CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 4 L/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 4 L/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 38, FIG. 8, AND SRM 51-40-05, PG. 1-4, FIG. 1-2, PG. 7, FIG. 4. 2L72 4F RTA16WE 20030218002002003021800200NM 2003 2 18 SWAA030337 120030211A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 396, STR 12R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030218002682003021800268NE 2003 2 18 ALG2003F00023 120030118A77149550177380 SENSOR SKRSKYS76 S76A 8143006NE TMECA ARRIUSARRIUS1A NE NR 1 ENGINE MALFUNCTIONED E ALGAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW03521AL16799 760132 15550TEC DURING TAKE OFF, TWO MINUTES AFTER TAKEOFF FROM BASE, NR 1 ENGINE OVERSPEED CAUTION LIGHT FLICKERED REPEATEDLY (BRIGHT NOT DIM). AIRCRAFT WAS RETURNED TO BASE. UPON LANDING THE MECHANIC REMOVED AND REPLACED THE NR 1 ENGINE SPEED SENSOR. AIRCRAFT WAS FUNCTION CHECKED AND RETURNED TO SERVICE. 1G72 3U3 U H1NE E34NE 20030220000882003022000088WP 2003 2 20 ABXA030078 120030207A57535914872503 FITTING DOUG DC9 DC932 3022066WP LT TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23928AX 47392 LEFT FLAP INBOARD HINGE, INTERNAL HINGE ATTACH FITTING WAS CRACKED ON THE OUTBOARD AFT CORNER. REMOVED AND REPLACED FLAP IAW DC-9 MM 27-51-01-4-0201. 2L72 4F A6WE 20030224001402003022400140NM 2003 2 24 AWXA200300191 120030130A53137075T6071 STRAP BOEING757 7572S7 1384962NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON BEEF-UP STRAP INSIDE STRINGER 29 L/H, BS 1434, AFT CARGO COMPARTMENT. MAINTENANCE REMOVED CORRODED STRAP INSIDE STRINGER 29 L/H, BS 1434; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 7-8. 2L72 4F RTA2NM 20030224001482003022400148NM 2003 2 24 AWXA200300200 120030203A53305079451 SKIN BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 3/16" CRACK WAS FOUND ON THE UPPER EDGE OF EXTERNAL SKIN AT UPPER HINGE CUTOUT OF L-1 DOOR, BS 318, STR 10 L/H; CONFIRMED BY HFEC INSPECTION. MAINTENANCE CUTOUT CRACK ON UPPER EDGE OF EXTERNAL SKIN AT UPPER HINGE CUTOUT OF L-1 DOOR; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 52-00-01, FIG. 203, PG. 205-206. 2L72 4F RTA16WE 20030225000802003022500080NM 2003 2 25 QXEA0300298 120030221A3260471515 HARNESS BOMBDRDHC8 DHC8401 1390041NM ZONE 700 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM09409QX2425 177 4051 GEG - FLIGHT 2353 - AFTER DEPARTURE, THE LANDING GEAR WOULD NOT RETRACT WITH THE HANDLE IN THE UP POSITION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE #2 WOW PROXIMITY HARNESS. THE HARNESS/SYSTEM WAS RIGGED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030226000442003022600044SW 2003 2 26 HEEA084333 120030211A7722407375001105 INDICATOR BELL 407 407 1182206SW MGT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 MGT INDICATOR RANGE BAR FLASHES ON START UP. 1G71 3U O H2SW 20030304000582003030400058SW 2003 3 4 HEEA084589 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030307000112003030700011 2003 3 7 HEEA084881 420030227A3421102005901 INDICATOR SKRSKYS76 S76A 8143006NE ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 ATTITUDE INDICATOR WILL NOT CAGE. 1G72 3U H1NE 20030307000512003030700051NM 2003 3 7 SWAA030469 120030228A52106545871 DOOR FRAME BOEING737 7373T5 1384608NM FWD SVC DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT CUTOUT AT 3RD FROM TOP STOP PIN CASTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030310000622003031000062SW 2003 3 10 HEEA084966 120030227A6220412010216107 BEARING BELL 412 412 1182202SW PENDULUM ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MAIN ROTOR HEAD PENDULUM ASSY BEARING ROUGH. REPAIRED. 1G72 4U H4SW 20030310001592003031000159NM 2003 3 10 EIA2003016 120030227A5300UNK BELTFRAME BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Fwd. Cargo Pit, R/H structure frame at STA 540, RBL 60", has a crack as marked. CORRECTIVE ACTION: Repaired as per ECRA 481-53-167-2 2L74 4F A20WE 20030117001112003011700111SW 2003 1 17 HEEA083195 120030108A3210206052105013 STRAP BELL 206 206B3 1181506SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 MLG STRAP ASSY HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030117001322003011700132SW 2003 1 17 HEEA083206 120030108A6710206062721113 ACTUATOR BELL 206 206B3 1181506SW ROTOR CONTROL INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032275Y 3626 ACTUATOR HAS INTERMITTENT OPERATION. 1G71 3U H2SW 20030121000172003012100017 2003 1 21 SWAA030059 420030110A2565D31354 SLIDE BOEING737 7377H4 1384404NM AFT SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29744SW 29490 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030314000732003031400073NM 2003 3 14 CALA0300072 120030118A5330 SKIN BOEING737 737524 1384721NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0946625 27529 MAINTENANCE DISCOVERED A CREASE TO THE FUSELAGE SKIN AT BS 807 BETWEEN S26R AND S27R DURING GROUND OPERATIONS IN CLE. WHEN THE CREASED AREA WAS CUT OUT THE UNDERLYING SHEAR TIE WAS FOUND DAMAGED AND WAS REPLACED. A PERMANENT FUSELAGE SKIN REPAIR WAS PERFORMED IAW ECRA 5330-03214. 2L72 4F RTA16WE 20030314001872003031400187CE 2003 3 14 00078 120030218A2612 FIRE LOOP LEAR 24 24D 5170311CE GE CJ610 CJ610* 30006NE LT ENGINE GROUNDED E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05299TW 24299 AIRCRFT DEPARTED YIP FOR IND, ENGINE FIRE WARNING LT ENGINE, ALL OTHER INDICATIONS NORMAL, RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE FOUND FIRELOOP GROUNDING OUT. ADJUSTED LOOP, OPS CHECK NORMAL. 2L72 4J4 J A10CE 1E16 20030314002362003031400236WP 2003 3 14 CALA0300115 120030313A335060030431LB BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW0933817 49371 INSPECTION FOUND BOTH THE R/H AND L/H EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2L72 4F A6WE 20030317000592003031700059NM 2003 3 17 03FDEA00189 120030228A5330 SKIN BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 LT AFT FUSELAGE SEC 48, SKIN HAS A CREASED DENT AT BS. 1349, WL 196 APPROX 8 O'CLOCK POS. LEFT AFT FUSE, SEC 48, SKIN CREASE DENT AT B.S 1349, WL 196, REMOVED DAMAGE, FOUND TO GO THROUGH BONDED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW E.A 7-5450-69416. 2L73 4F4 F A3WE E2EA 20030122002092003012200209 2003 1 22 HEEA083554 420030113A34570110050400 GPS BELL 206 206L4 1182110SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F 52038 GPS VERY SLOW TO ACQUIRE SIGNALS. 1G71 3U NCH2SW 20030122002702003012200270NM 2003 1 22 UPS03440047 120030103A5330 SKIN BOEING747 747259B 1384804NM BS 1480 FX SKIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C RH BS 1480 FX SKIN AT EXTENSION FTG AREA HOLE #12 TWO CRACKS FOUND THROUGH FOR DETAIL, PLS REF ATTACHED SKETCH. HOLE REWORKED AS PER RS R-53-43-34957 DUE EXCEEDED SB B747-53A2390 LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTIONS). 2L74 4F RTA20WE 20030729000942003072900094EU 2003 7 29 2003F00474 120030516A5350 FAIRING AIRBUS320 A320233 3930329EU FUSELAGE DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND BELLY FAIRING 192AB DELAMINATED. REPAIRED FAIRING IAW SRM 51-77-12 PAR 3B, FIGURE 3. (M) 2L72 4F RTA28NM 20030303001852003030300185SW 2003 3 3 HEEA084567 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L9053 33023 MAIN ROTOR BLADE HAS WATER IN THE CHORE NEAR THE MID SPAN TRIM TAB. 1G72 4U H4SW 20030417000282003041700028WP 2003 4 17 UPS03840078 120030116A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C-2, AFT PIT DOOR SLIDE AREA STA 1210 BETWEEN LONG 31R-32R END FITTING CORRODED. REMOVED EXISTING FITTINGS, LOCATED, DRILLED AND DEBURRED NEW FITTINGS P/N 3754930-1N, 5894282-501, & 5894282-502 IAW DC8 SRM 51-3-2 AND INSTALLED FITTINGS IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030326001132003032600113 2003 3 26 AMTA200300150 420030127A256580330034 BOTTLE BOEING757 75733N 1384931NM DOOR DISCHARGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11557TZ 32591 WHILE AT THE GATE, A PASSENGER ATTEMPTED TO OPEN L-2 DOOR WHILE ARMED. SLIDE DID NOT DEPLOY HOWEVER, IT APPEARS CO2 CHARGE DISCHARGED OR AIR BOTTLE FOR DOOR DISCHARGED. REMOVED AND REPLACED BOTTLE AS REQ'D REF MM 52-11-3 0-4. (M) 2L72 4F RTA2NM 20030721000032003072100003NM 2003 7 21 AUS20030559 120030411A531165465244 FRAME BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME BS 400 CRACKED. CRACK LENGTH 10.16MM (0.4IN). FUSELAGE FRAME BS440 CRACKED. CRACK LENGTH 12.7MM (0.5IN). FRAMES CRACKED AT FLANGE BEND RADIUS BETWEEN S-13R AND S-14R. FOUNDDURING EDDY CURRENT INSPECTION IAW EI 733-53-11 , BOEING NTM PART 6 51-00-00 FIG4 AND NDT TECHNIQUEE-18. 2L72 4F4 FRTA16WE E21EU 20030722001022003072200102NM 2003 7 22 SWAA031475 120030704A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INTERMITTENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 EMERGENCY EXIT LIGHTS ILLUMINATE IN ARMED POSITION, CAN ONLY BE EXTINGUISHED BY TURNING TO OFF POSITION. RESET EMERGENCY LIGHT CIRCUIT BREAKER AND OPS CK GOOD PER MM. 2L72 4F RTA16WE 20030723000772003072300077NM 2003 7 23 AWXA200300794 120030610A5320694754217 ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A .75 INCH CRACK WAS FOUND AT AFT END OF INBOARD UPPER ATTACH ANGLE IN LT FLAP WELL BS 711-727, WBL 71.24. MAINTENANCE REMOVED ATTACH ANGLE BS 711-727, WBL 71.24; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3-4, 10-11 & 16-19 FIG 12 & 13. 2L72 4F RTA16WE 20030723000882003072300088EU 2003 7 23 AWXA200300635 120030602A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU SEAT ROW 16 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 LAS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT CONNECTOR OF EMERGENCY ESCAPE PATH LIGHT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030723000972003072300097EU 2003 7 23 03190302 120030709A33501317 LAMP JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27302UE 41013 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FWD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030422001372003042200137EU 2003 4 22 RAIA00302054 120030224A3150 SWITCH JETAIRJETSTMJETSTM4101 1500501EU COCKPIT DIRTY A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03565HK 41082 STL- CONFIG WARNING LIGHT CAME ON DURING TAKEOFF. MAINTENANCE CLEANED SWITCH ON CONDITION LEVERS. OPS CHECK OK. 2L72 4T RTA41NM 20030422001612003042200161NM 2003 4 22 UPS03240272 120030218A2710 HINGE BOEING727 727108C 1384039NM AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C+SI, LT WING O/B AILERON BEARING HINGES (4 OFF) CORRODED. LEFT O/B AILERON REPLACED IAW MM 27-10-14. 2L73 4F A3WE 20030423001502003042300150WP 2003 4 23 ZW0A0303010 120030306A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 LONGERON 19R AT STA 160 TO 154 WAS DAMAGED. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030424000142003042400014NM 2003 4 24 QXEA0300379 120030318A1430 RIVET DHAV DHC8 DHC8202 2809007NM RT NACELLE SHEARED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX- RIGHT HAND NACELLE HAS FOUR SHEARED RIVETS ON VERTICAL STIFFENER EIGHT INCHES OUTBOARD OF MASTER REFUEL/DEFUEL VALVE AT TOP OF NACELLE. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040223000242004022300024CE 2004 2 23 JGV2004F00000 120031223A53204520008430001 BRACKET LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312 01518WP STARTER GEN BROKEN B JGVRO OTHER O OTHER NRNOT REPORTED 1 CE09745E 008 LT111159 AFTER ENGINE REINSTALLATION, DURING ENGINE START, NO ROTATION WAS OBSERVED ON THE LT ENGINE. FOUND STARTER/GENERATOR WIRE GROUNDING BRACKET NO LONGER ATTACHED TO THE FUSELAGE SKIN. THE BRACKET HAD OVERHEATED AND MELTED A HOLE IN THE FUSELAGE SKIN, APPROXIMATELY 1.8 INCH BY 2.25 INCH. SB 45-53-10 WAS COMPLIED WITH IN 9/3. THIS SB INSTALLS A NEW GROUNDING BRACKET AND IS SUPPOSED TO IMPROVED THE BOND FOR BETTER CONDUCTIVITY. OPERATOR INSPECTED OTHER 45`S IN THEIR FLEET AND FOUND EVIDENCE OF FASTENER OVERHEAT ON AT LEAST 1 AIRCRAFT. 2L72 4F4 FRTT00008WIE6WE 20030827000372003082700037CE 2003 8 27 MQK2003F00000 120030511A3233MS141025 BEARING BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112NE MLG ACTUATOR BINDING E MQKAO OTHER O OTHER NRNOT REPORTED 1 EA093113B RJ13 PCE100070 BEARING BINDING. MLG DOWNLOCK ACTUATOR. 2H72 4F4 FRTA16SW E25EA 20030828001772003082800177NM 2003 8 28 SWAA031872 120030819A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 500 PLUS 2 AT STR 15R AND BS 747 AT STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030828001802003082800180NM 2003 8 28 SWAA031850 120030818A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030902000872003090200087EA 2003 9 2 SWIA200312136 120030617A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA FORWARD CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07906SW 7510 EMERGENCY LIGHTING SYSTEM INOPERATIVE ROWS 1 THROUGH 5. EXIT SIGN FOR ROW 8 ALSO INOPERATIVE, LOWER, LEFT HAND SIDE. REPLACED LIGHT STRIP AT FORWARD CABIN. OPS CHECK GOOD. 2L72 4F RTA21EA 20030902001682003090200168CE 2003 9 2 PCP2003F00000 120030623A3230AN737TW7491 CLAMP BEECH 36 B36TC 1151609CE CONT O520 TSIO520UB 17040SO GEAR RELAY DAMAGED B PCPRO OTHER O OTHER NRNOT REPORTED 1 WP25842BE EA432 249061R OWNER REPORTED, UNABLE TO ACHIEVE GEAR DOWN AND LOCK ON APPROACH TO LANDING. GEARS WERE MANUALLY EXTENDED IAW POH EMERGENCY GEAR EXTENSION PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION BY TECH REVEALED A HEAT DUCT CLAMP (UNDER CO-PILOT SEAT) OF THE PN AN737TW7491 HAD BEEN PREVIOUSLY INSTALLED IN PLACE OF THE CORRECT PN AN737TW56-66 CLAMP. THE LARGER CLAMP, WHEN TIGHTENED LEFT A PIG-TAIL WHICH CAUGHT ON THE RIGHT INBOARD GEAR DOOR ROD/BELLCRANK ASSEMBLY, FORCING IT OFF OF THE DUCT AND FALLING ONTO THE LANDING GEAR RELAY PN SM50D7 ADJACENT TO THE DUCT. THE CLAMP SHORTED THE GEAR RELAY, RENDERING THE GEAR INOPERATIVE IN NORMAL MODE. 1L71 3O3 O 3A15 E8CE 20030904000472003090400047EA 2003 9 4 SWIA200312252 120030805A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07423SW 7456 AS WE ADDED POWER TO TAKEOFF, ALL GROUND SPOILERS DUMPED; THEN AS WE ADDED POWER TO CLEAR RUNWAY, THEY DUMPED AGAIN, AND ENDED WITH A SPOILERON STATUS MESSAGE. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW MM 27-62-01. OPS AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20030903002622003090300262SO 2003 9 3 C2XA03SH311 120030830A532014526437001 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE RIGHT HAND OMEGA BEAM BUTT STRAP BETWEEN FR 59-60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OMEGA BEAM BUTT STRAP IAW EMB 145 SRM 53-24-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030924000522003092400052NE 2003 9 24 DL757030767 220030818A7200PW2037RTC LINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE LOOSE A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27640DL48744 23994 716475 ON TAKEOFF ROLL LT ENGINE WAS RUNUP TO 1.12..WHEN THROTTLES ADVANCED TO TO POWER THE LT ENGINE EPR ROLLED BACK TO 1.06. FOUND P4.9 LINE LOOSE. TIGHTENED SAME 2L72 4F4 FRTA2NM E17NE 20040127002092004012700209WP 2004 1 27 ASAA0380663 120031015A53135911432103 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND AFT ACCY STATION 1437 LONGERON 2L CRACKED. REPAIRED PER SRM. (M) 2L72 4F A6WE 20040128000502004012800050NM 2004 1 28 AWXA200301611 120031206A5320651768470 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE L-1 DOOR INTERCOSTAL CHAFED AT LOWER HINGE CUTOUT BS 303.9, STR 13 LT. MAINTENANCE REMOVED INTERCOSTAL AT LOWER HINGE CUTOUT BS 303.9, STR 13 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1 & 38. 2L72 4F RTA16WE 20040129001112004012900111SO 2004 1 29 DHL200374247 120031204A5754 SKIN PIPER PA18 PA18150 7101828SO SLAT DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742 188146 DURING C-CHECK, LEFT HAND INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. CUT OUT UPPER SKIN DELAMINATION APPROX 1.7 INCH DIA & DOUBLER APPROX 4 X 4.75 INCH FROM 2024-T3 .016 PO900291. FURTHER EVALATION FOUND 1 PUNCTURE & 1 SHARP DENT ON LOWER SKIN, 2 EA DELAMINATED & DENTED AREAS ON LOWER SKIN. CUT OUT DAMAGED AREAS 3 EA APPROX 1 INCH DIA & 1 EA APPROX 1 X 5.5 INCH, FABRICATED 3 EA FILLERS APPROX 1 INCH DIA AND 1 EA 1 X 5.5 AND 4 EA DOUBLERS APPROX 4 INCH DIA. 4.25 X 8.5, 3.75 X 4 INCH & 3.5 X 3.5 INCH FROM 2024 T-3 .016 PO900291. CLEANED, PREPPED, TREATED, PRIMED AND SEALED AND BONDED RUBSTRIP. 1H71 3O 1A2 20040204002192004020400219WP 2004 2 4 UPS03841558 120031020A53409754022U504 FITTING DOUG DC8 DC873F 302199FWP LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 340 MAIN CARGO FLOORBEAM END FITTING IS CRACKED AT RT. SIDE RBL 67 APPROX. REMOVED AND REPLACED FITTING IAW DWG. 9754022 AND SRM. 51-1-20D 2L74 4F RT4A25 20040210000562004021000056CE 2004 2 10 GLBA2003075 120030604A2130 FILTER BEECH 1900 1900D 1154162CE PRESS CONTROLLERCLOGGED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03219GL UE219 FOUND PRESSURE CONTROLLER FILTER PLUGGED, ( CLEANED FILTER,PN 101-380018-3) OPS CHECK GOOD. 2L72 4T RTA24CE 20031212001722003121200172EA 2003 12 12 COMA0360526 120031202A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 FUSELAGE SKIN FS 585 TO 600 BETWEEN STRINGERS 21L TO 23L HAS SEVERAL DENTS. REPAIRED BY RE-CONTOURING DAMAGED AREAS, PERFORMING EDDY CURRENT INSPECTION, APPLIED PROTECTIVE TREATMENT AND APPLIED EXTERIOR FINISH TO MATCH CUSTOMER CONFIGURATION IAW WVAC EO 601R-53-4441. 2L72 4F RTA21EA 20040518000202004051800020WP 2004 5 18 GTIA040339 120030422A3260833605 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP RT MLG INOPERATIVE A GTIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL23801NK 48048 MYR - FLT 1582 - RIGHT MAIN LANDING GEAR INDICATION ON DEPARTURE. QRH ACCOMPLISHED AND LANDING GEAR RECYCLED GEAR DOOR OPEN LIGHT INTERMITTENTLY ON WITH NO VIBRATION NOTED. RIGHT MLG LIGHT EXTINGUISHED WHEN REACHING 10000 FT ON DESCENT. TROUBLESHOT SYSTEM, FOUND PROXIMITY SWITCH ELECTRONIC UNIT AT FAULT. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. PERFORMED OPS CHECK. NO FAULTS NOTED. (M) 2L72 4F A6WE 20031215001812003121500181EA 2003 12 15 ASOA03530 120031021A5210601R3807423 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR THE CRACK AND REPLACE DOOR CABLE FITTING WITHIN 100 FLIGHT HOURS PER REO 601R-11-420. (M) 2L72 4F RTA21EA 20030926000032003092600003EU 2003 9 26 S9H2003F00002 120030714A215045140003 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE AIR CONDITIONER FAILED E S9HAO OTHER O OTHER NRNOT REPORTED 1 WP19356NT327 2280 DURING A CHECK RIDE, THE AIRCONDITIONING SYSTEM FAILED. ISOLATION OF THE SYSTEM WAS CONDUCTED. AIRCRAFT PERFORMED RECOMMENDED PROCEDURES AND UPON INSPECTON OF THE SYSTEM IT WAS CONFIRMED THAT THE AIR CONDITIONING BELT HAD FAILED. BELT WAS REPLACED. 1G71 3U3 UNCH9EU E19EU 20040917000062004091700006WP 2004 9 17 WX0300026 120031230A3350 LIGHT DOUG DC9 DC987 3022087WP CABIN INOPERATIVE A WXOAK NONE L NO TEST ININSP/MAINT 1 WP19945MA 49725 DURING A ROUTINE SERVICE CHECK IN LAS, THREE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE EMERGENCY LIGHTS AS REQUIRED IAW AMM 33-53-00. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20050816000822005081600082NM 2005 8 16 SWAA032503 120031112A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND 13 EA STRINGER CLIPS CRACKED AT STR 10R, BS 480, BS 500, BS 500A, BS 500B, BS 500C, BS 520 AT STR 10L BS 480, BS 460, BS 500A, BS 500B, BS 500C AT STR 8R, BS 500D, BS 520. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20060801001172006080100117WP 2006 8 1 IXXA060567S 120030906A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND CAPTAINS RIGHT FORWARD SEAT TRACK WORN. REMOVED WORN SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-21, AND 51-3-0. 2L74 4F RT4A25 20030814000152003081400015NM 2003 8 14 SWAA031727 120030803A53116546569 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1091, WL 285 AND LBL 38. REMOVED AND REPLACED FUSELAGE FRAME SECTION PER SRM. 2L72 4F RTA16WE 20030819002362003081900236NM 2003 8 19 C1HA200381027 120030812A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON FLOORBEAM BS 440 LBL 21 TO RBL 15. 2L73 4F A3WE 20030820000562003082000056NM 2003 8 20 03FDEA01070 120030706A5510NLC6725 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT HORIZONTAL STABILIZER NR 13 BORE CORROSION EXCEEDED CONDITION 3. CORROSION ON RIGHT HORIZONTAL STABILIZER NR 13 BORE REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5510-71831 2L73 4F RTA22WE 20030820001772003082000177EA 2003 8 20 COMA0360363 120030809A2421755469E IDG CNDAIRCL600 CL6002B19 1900309EA RIGHT FAILED A COMAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01446CA4672 7546 FLIGHT 5711 NR 2 GENERATOR OFF WARNING DURING T/O. REPLACED THE RT GENERATOR. 2L72 4F RTA21EA 20030401000042003040100004EA 2003 4 1 03088628 120030329A3350 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27628BR 7240 DURING MAINTENANCE INSPECTION, THE CABIN DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030821000392003082100039NM 2003 8 21 03FDEA01012 120030625A5753ARC050311 FITTING DOUG MD11 MD11 3023602NM TE FLAP HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING - OUTBOARD T/E FLAP, OUTBOARD FWD HINGE FITTING FOUND INBOARD SIDE ARM, BARREL NUTS MOUNT HOLES WITH CORROSION (WING SIDE FITTING). LEFT WING - OUTBOARD T/E FLAP, OUTBOARD FWD HINGE FITTING INBOARD SIDE ARM BARREL NUTS MOUNT HOLES (WING SIDE FITTING) CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5750-69356 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP, OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030821001292003082100129EU 2003 8 21 03FDEA00893 120030616A5320A92449635720000 SUPPORT AIRBUS300 A300B4605R 3930308EU CARGO BAY BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 FWD CARGO ANT CABLE SUPPORTS ARE BENT AT FR 25 STR 45L. REMOVED AND REPLACED CABLE SUPPORTS IAW SRM 51-40-21. 2L72 4F RTA35EU 20030403000862003040300086WP 2003 4 3 CALA0300159 120030311A5230 SKIN DOUG DC9 DC982 3022082WP CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 MAINTENANCE FOUND A CREASE IN THE AFT UPPER CORNER OF THE OUTER SKIN OF THE AFT CARGO DOOR. THE CREASED AREA OF DOOR SKIN WAS REPAIRED IAW ECRA 5232-01023. A DIP WAS ISSUED TO PERFORM INSPECTION OF THE REPAIR IAW ECRA 5232-01023 BEGINNING AT OR BEFORE 45,815 CYCLES AND TO REPEAT THE INSPECTION AT INTERVALS NOT TO EXCEED 15,000 CYCLES. THE REPAIR IS PERMANENT WITH REPETITIVE INSPECTIONS. THERE IS NO TERMINATING ACTION. 2L72 4F A6WE 20030328000372003032800037SO 2003 3 28 C2XA03TY022 120030210A531014522460013 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE FWD-CENTER OMEGA BEAM TOP CAP WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030416002282003041600228WP 2003 4 16 AALA20030275 120030304A3222 SCHRADER VALVE DOUG DC9 DC982 3022082WP NLG LEAKING A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21574AA 53151 SEA - FLT 1760 - EN ROUTE SEA-DFW, AFTER TAKEOFF, LANDING NOSE GEAR DID NOT RETRACT. ALSO, HAD A STALL WARNING LIGHT ILLUMINATE. RETURNED AND LANDED SEA WITHOUT INCIDENT. REPLACED NOSE STRUT SCHRADER VALVE AND SERVICED NOSE STRUT. NO SIGN OF FLUID LEAKAGE FROM STRUT. ACCOMPLISHED NOSE GEAR SWING SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030425000322003042500032EU 2003 4 25 RAIA00303078 120030318A612031056244 PRESSURE SWITCH JETAIRJETSTMJETSTM4101 1500501EU BETA SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 CE03561HK3468 41077 STL- LEFT ENGINE GREEN BETA LIGHT WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NUMBER ONE ENGINE BETA PRESSURE SWITCH, LEAK AND OPS CHECK OK. 2L72 4T RTA41NM 20030428000592003042800059NM 2003 4 28 OZI2003F00004 120030117A531000153SB6018200 SILL DORNERDO32 DO328300 NM ZONE231 CORRODED A OZIAO OTHER O OTHER NRNOT REPORTED 1 SW07410Z 3125 BAGGAGE COMPARTMENT DOOR SILL CORRODED. 2H72 4T RTA55NM 20030428001482003042800148CE 2003 4 28 DXTA20030007 120030210A2497M22759 WIRE CESSNA500 560CESSNA 2076750CE MAIN ELECTRICAL CHAFED E DXTAO OTHER O OTHER ININSP/MAINT 1 GL07330QS7331 5600329 DURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY ADJACENT TO A SHROUDED FUEL CROSSFEED LINE, AND CABIN OUTFLOW VALVES. SHOULD A FIRE START, IT IS POSSIBLE THAT IT COULD GO UNNOTICED UNTIL THE CROSSFEED SHROUD AND LINE IS BREACHED. 2L72 4F RTA22CE 20030430000392003043000039EA 2003 4 30 COMA0370013 120030424A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA LANDING GEAR UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01355CA570 453 10067 FLIGHT 5320 LANDING GEAR DISAGREE WARNING. REPLACED THE GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20030501000522003050100052WP 2003 5 1 AALA20030025 120030103A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21456AA 49561 TUL - FOUND LONGERON NR 2 RIGHT CRACKED AT FLANGE OF FRAME, AFT SIDE OF FRAME, STATION 1418. INSTALLED NEW SECTION OF LONGERON NR 2 RIGHT SIDE, STATION 1418 PER AARD 53-30-00-02. (M) 2L72 4F A6WE 20030502002792003050200279NM 2003 5 2 SWAA030858 120030415A32136561740 STRUT BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG UPPER OUTER CYLINDER CORRODED. REMOVED AND REPLACED LT MLG UPPER OUTER CYLINDER PER MM. 2L72 4F RTA16WE 20030505002612003050500261NM 2003 5 5 03FDEA00532 120030418A5350 RADOME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RADOME FAILED MOISTURE CHECK. REMOVED AND REPLACED RADOME IAW FED EX M/M 53-15-000-04. 2L73 4F RTA3WE 20030506002162003050600216 2003 5 6 ASAA0380128 420030211A25653961896501 LANYARD DOUG DC9 DC983 3022083WP R1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 LAX - DURING PREFLIGHT CHECK, FOUND RIGHT FORWARD (R-1) SERVICE DOOR GIRT-TO-SLIDE COVER LANYARD DISCONNECTED. REATTACHED LANYARD. (M) 2L72 4F RTA6WE 20030507000782003050700078WP 2003 5 7 CA030414001 220030402A75326621000000073 BLEED VALVE LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312 01518WP COMPRESSOR FAILED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING INSPECTION LT BLEED VALVE FAILED OPS CHECK, REPLACED VALVE, OPS CHECKED SERVICEABLE. 2L72 4F4 FRTT00008WIE6WE 20030605000762003060500076EU 2003 6 5 PJY2003F00000 120030506A49304503501 LINE SUNDSTRANDAI BRAERODH125 BAE125800A 1500285EU APU FUEL CHAFED B PJYRO OTHER K FLUID LOSS NRNOT REPORTED 1 GL15160NW 897636 NA0436 FOUND FUEL LINE(TUBE ASSEMBLY SEE FIG 2 PART 10) ON APU CHAFED 99 PERCENT ALL THE WAY THROUGH THE SIDE WALL (STEEL LINE). AFTER PART WAS REMOVED, IT TOOK VERY LITTLE PRESSURE TO POKE A HOLE IN LINE. FOUND ON APU MAINT. CHECK. 2L72 4F RTA3EU 20030606000962003060600096NM 2003 6 6 COOSDR030023 120030501A5755 SKIN BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 2 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG TIC1693 20725 LT WING, SPOILER NR 2, PN 65-17347-48, SN TIC-1693, WITH DELAMINATION. 2L73 4F4 FRTA3WE E2EA 20030609000392003060900039NM 2003 6 9 C1HA200396006 120030520A5347 SEAT TRACK BOEING727 72722 1384002NM FUSELAGE GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 LT OTBD SEAT TRACK GOUGED BETWEEN BS 954 & 956 2L73 4F A3WE 20030606000242003060600024NM 2003 6 6 03FDEA00739 120030516A2613 WARNING LIGHT BOEING727 727200 138407ENM BODY OVERHEAT ILLUMINATED A FDEAO OTHER J WARNING INDICATION CRCRUISE 1 SO25269FE 21675 PASSING FL230, 330 KIAS, EPR 2.01/2.07/2.01, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. LEVELED OFF AT FL 260 AND PRIOR TO COMPLETING RED TABS , LOWER AFT BODY OVERHEAT LIGHT EXTINGGUISHED. RED TABS COMPLETED AND SYSTEM TEST GOOD. AT LEVEL OFF FL260 THROTTLES WERE REDUCED, SWITCH POSITION CARGO HEAT OUTFLOW-NORMAL, BLEED AIR 1/3 OPEN, BLEED 2 CLOSED, RIGHT AND LEFT PACK ON. INSPECTED PNUEMATIC DUCTING FOR LEAKS NONE NOTED AT THIS TIME REF. 26-14-001-2. 2L73 4F RTA3WE 20030515000742003051500074CE 2003 5 15 DXTA200300022 120030430A3220 LANDING GEAR CESSNA750 750 2076810CE NOSE VIBRATION E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07971QS 7500071 REJECTED TAKEOFF DUE TO SEVERE NOSE WHEEL SHIMMY. 2L72 4J RTT00007WI 20030610001262003061000126SW 2003 6 10 HEEA087023 120030604A6520406040400117FM DRIVE GEAR BELL 407 407 1182206SW T/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 CORROSION ON T/R HUB DRIVE SPLINES. 1G71 3U O H2SW 20030611000842003061100084NE 2003 6 11 HEEA086569 120030522A24217655009005105 GENERATOR SKRSKYS76 S76A 8143006NE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 GENERATOR INOPERATIVE. SENT FOR WARRANTY REPAIR. 1G72 3U H1NE 20030611001452003061100145EA 2003 6 11 2003F00366 120030413A7830TY214810A CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER FAILED A FDKAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07503MJ 10058 ASH - FLT 6950 - PHX-FAT, ABORTED TAKEOFF DUE TO RIGHT TR UNSAFE WARNING MESSAGE. MAINTENANCE REPLACED THE ISOLATION CONTROL VALVE. OPS CHECKED GOOD. (M) 2L72 4F RTA21EA 20030612001912003061200191WP 2003 6 12 EIA2003078 120030429A5311 FRAME DOUG DC9 DC915F 3022037WP BULKHEAD CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09915F 47061 FUSELAGE INTERIOR BS 642, RBL 8 UNDER THE FLOOR, UPPER FRAME OF THE FWD BULKHEAD OF THE AFT CARGO COMPARTMENT HAS SURFACE CORROSION. REMOVE AND REPLACE UPPER FRAME OF THE FWD BULKHEAD OF THE AFT CARGO COMPARMENT PER DC9 SRM 51-30-01, PG 1-10, 51-30-02 PG 1-8 & 51-30-05, PG 1-30. 2L72 4F A6WE 20030617002562003061700256EA 2003 6 17 QXEA200300677 120030606A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09604QX 10019 PDX- ON FLIGHT 2497 EMERGENCY LIGHTS CYCLED ON AT IRREGULAR INTERVALS, THEN OFF WITH SWITCH IN ARM POSITION DURING CLIMB AND DESCENT. REMOVED AND REPLACED ALL FOUR BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030515001832003051500183NM 2003 5 15 SWAA031077 120030511A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STRINGER 22R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030521000562003052100056EU 2003 5 21 DHL2003368004 120030517A3260 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU MLG DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01368DH 207 BOTH LEFT AND RIGHT MAIN WHEEL DOOR, RED UNSAFE AND GREEN LIGHTS ILLUMINATED AFTER NORMAL GEAR RETRACTION ON BOTH SYSTEMS. REMOVED AND REPLACED PROXIMITY DETECTOR MODULE UNIT IAW M/M 32-61-12. 2L72 4F RTA35EU 20030521000752003052100075WP 2003 5 21 DHL2003802007 120030517A2697 CONNECTOR DOUG DC8 DC873 302199CWP NR 3 FIRE LOOP DEFECTIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01802DH 46076 NR 3 FIRE DETECTOR LOOP-B SYSTEM FAILED TO TEST. TRANSFERRED TO DMI 12964 CAT-C IAW MEL 26-2-3, PLACARDS INSTALLED. REF DMI 12964 NR 3 FIRE DETECTOR LOOP-B SYSTEM FAILED TO TEST. REPLACED DEFECTIVE CONNECTOR AT FAN CASE RT PER DACO M/M 20-504. OPS CHECKED SERVICEABLE PER DACO M/M 26-10-1. DMI 12964 CLEARED. PLACARD REMOVED. 2L74 4F RT4A25 20030523000402003052300040NM 2003 5 23 DLM11030396 120030428A5210 HANDLE DOUG MD11 MD11 3023602NM DOOR ASSIST STUCK A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27808DE 48479 DOOR 1L WAS ACTUATED BY THE EXTERIOR EMERGENCY HANDLE, DOOR ASSIST BOTTLE BLEW AND HANDLE STUCK IN EMERGENCY POSITION. DOOR WOULD NOT OPEN OR CLOSE ELECTRICALLY. RESET HANDLE AND RESERVICED ASSIST BOTTLE, OPS NORMAL. 2L73 4F RTA22WE 20030523001302003052300130NM 2003 5 23 2003UALA00435 120030507A5754 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SLAT WEDGE DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29787UA 26939 T/E WEDGE LOWER SKIN DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED AND REINSTALLED T/E WEDGE, LT WING, SLAT NR 1. 2L72 4F4 FRTT0001SE E46NE 20030624000572003062400057NM 2003 6 24 CALA0300294 120030607A5347655384420 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND RIGHT CARGO TRACK CORRODED AT STA 944. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW TRACK AND SPLICE WERE INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20030624001002003062400100NM 2003 6 24 DL73S030476 120030519A53126546568515 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 WHILE ACCOMPLISHING INSPECTIONS OF THE AFT PRESSURE BULKHEAD IAW AD 99-08-23, 2 CRACKS WERE FOUND EMANATING FROM FASTENER HOLES IN THE BULKHEAD AT THE ATTACH AREA. THE CRACKED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM DOUBLER IAW SRM AND ER/A 385086-14AD. 2L72 4F RTA16WE 20030707001722003070700172 2003 7 7 VQM2003F00000 420030409A3197MS2721255 TERMINAL BLOCK BEECH 90 C90 1152913CE INSTRUMENT PANELBURNED E VQMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM03738R LJ517 PILOT REPORTED SMOKE IN THE CABIN COMING FROM CO-PILOT INSTRUMENT PANEL UPON INSPECTING FOUND PRIMARY WIRES TO BELLY TERMINAL BLOCK BELOW CENTER PEDESTAL WAS LOOSE DUE TO SECURING NUT ON BLOCK HAD BACKED OFF CAUSING WIRES TO GET HOT AND BURN INSULATION. REPLACED TERMINAL BLOCK AND FOUR WIRES, TWO WIRES WENT TO NR 1 BUSS AND TWO WIRES WENT TO MAX HEAT 150 AMP CIRCUIT BREAKER AT PILOTS FEET. PERFORMED STATISFACTORY GROUND RUS AND FUNCTION CHECKS OF ELECTRICAL SYSTEMS. PRIOR TO THIS INCIDENT PLANE HAD A PREVIOUS HISTORY OF THE GENERATORS NOT STAYING ON LINE OR IN PARALLEL. SWAPPED GENERATORS AND VOLTAGE REGULATORS FOR TROUBLESHOOTING AND CLEANED SHUNTS, HEAT SINKS AND DIODES IN WHEEL WELLS. 1L72 3T 3A20 20030710000812003071000081EU 2003 7 10 DHL2003366502 120030524A7830 DOOR AIRBUS300 A300B4203 3930306EU THRUST REVERSER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 NR 1 ENG THRUST REVERSER LOWER DOOR IS CRACKED. REMOVED AND REINSTALLED DOOR IAW A300 SRM 51-30-30. FABBED REPAIR DOUBLER IAW A300 SRM 51-40-00 USING 7075-T6 .050 PO 409830.2 IAW ESTM 1476-97. ALODINED AND PRIMED DOUBLER IAW A300 SRM 51-40-12. INSTALLED DOUBLER IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20030711000932003071100093 2003 7 11 ZW0A0305501 420030626A256561474129 SLIDE BOEING757 757231 1384950NM DISLODGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13711ZX 28481 AFTER CHECK-C AND DURING A MINI CABIN EVACUATION DEMONSTRATION THE ESCAPE SLIDE AT THE RIGHT SIDE NUMBER 2 DOOR DID NOT INFLATE BUT FELL TO THE FLOOR. THE GIRT BAR WAS WITH THE SLIDE. 2L72 4F RTA2NM 20030114000622003011400062NM 2003 1 14 SWAA030012 120030104A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030115001232003011500123NM 2003 1 15 03FDEA00018 120030112A56105893543110 WINDSHIELD BOEING727 727233 138408ANM COCKPIT CRACKED A FDEAO OTHER O OTHER CRCRUISE 1 SO25265FE 21671 F/O WINDSCREEN (R-1) CRACKED 50 MINUTES INTO FLIGHT AT FL310 302KIAS. REPLACED GLARESHIELD AND TRIM PANELS IAW MM. RESET ALL CIRCUIT BREAKERS ON P6 AND P18 PANELS. PERFORMED WINDOW HEAT CHECKS REFERENCE W 30-40/5278. PRIMARY HEAT SENSOR USED. VERIFIED TERMINAL NR 26 CONNECTED TO THE RIGHT SIDE AS PRESCRIBED IN MM 30-41-002-5. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20030127000192003012700019 2003 1 27 HEEA083595 420030114A3442MI5851352 INDICATOR BELL 412 412 1182202SW RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 RADAR HAS TEST PATTERN ON ANY SCALE ABOVE 4 MILES. SHOP REPAIR. 1G72 4U H4SW 20030128001772003012800177WP 2003 1 28 ZW0A0300810 120030113A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT IN THE FWD ENTRY FOUND CORROSION ON WEB, BELOW FLOOR AT STA 168 TO 200, LBL 54. CLEANED AREA OF CORROSION. CUT OUT AREA BEYOND LIMITS AND INSTALLED REPAIR PER SRM 53-01, PAGE 9. 2L72 4F A6WE 20030204002502003020400250NM 2003 2 4 VNAA0301014 120030113A26123280170 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07463PS2233 3087 THE CREW REPORTED THAT THE CARGO FIRE DETECT FAILED. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECT PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030212000812003021200081NM 2003 2 12 UPS03240159 120030127A5310 RIB BOEING727 72725C 138400HNM BS870 S9 TO S12 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C DURING EDDY CURRENT INSP.OF R/H BS870 FORGING 2 CRACKS WERE FOUND ON FWD INTEGRAL RIB AT S11. REF EO.B727-5310-3057 APPDX.D FOR PARTIAL REPLACEMENT OF TERMINAL F ITTING S9 TO S12 AND APPDX.C STEP 1. 2L73 4F A3WE 20030214000712003021400071EU 2003 2 14 QXEA0300254 120030212A33501012721 CARTRIDGE FOKKERF28 F28MK4000 4990810EU ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09492US 11159 PDX-EMERGENCY EGRESS LIGHTS AT ROWS 5, 6 AND 8 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY CARTRIDGE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20030218002352003021800235NM 2003 2 18 SWAA030265 120030203A532065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER CLIPS CRACKED, BS 616, STR 5L AND BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030220000312003022000031NM 2003 2 20 03FDEA00127 120030118A5753ARC050312 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE TE FLAPS LOOSE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25607FE 48547 RT WING OUTBOARD FLAP, OUTBOARD HINGE, ACTUATOR HINGE, INBOARD AND OUTBOARD BUSHING (AIRFRAME SIDE) LOOSE. REMOVED AND REPLACED OUTBOARD FLAP HINGE IAW EA. 1-5750-67564. 2L73 4F4 FRTA22WE E13NE 20030117000182003011700018SW 2003 1 17 HEEA083158 120030108A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 TRANSMISSION RESTRAINT IS WORN. REPAIRED. 1G71 3U H2SW 20030226000092003022600009SW 2003 2 26 HEEA084307 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 TAIL ROTOR DISC PACK BROKEN. 1G71 3U O H2SW 20030226000132003022600013SW 2003 2 26 HEEA084311 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030303001982003030300198WP 2003 3 3 DHL2003804543 120030207A27505701446501 VANE DOUG DOUG DC8 DC873F 302199FWP DELAMINATED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 ASI0020311 46124 ITEM REF. N/R: 0100 : LH WING REMOVAL AND INSTALLATION OF #3 FLAP VANE FOR DELAMINATION IN L/E (REF. N/R0097) CORR: R/R #3 FLAP VANE ON LH WING IAW M/M 27-51-14 PG. 201-203 FOR OPS CHECK SEE N/R0607 2L74 4F RT4A25 20030304000822003030400082NM 2003 3 4 DL757030116 120030128A5330143N33206 SKIN BOEING757 757232 1384965NM FS 439, S-17L GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27685DA 27588 FUSELAGE / SKIN / FS 428-440 / STRG. 17L-18L : DENT AND GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED BY GROUND EQUIPMENT JUST FWD AND JUST AFT OF THE FS 439 SKIN BUTT JOINT BETWEEN STRINGERS 17L & 18L. THE DAMAGE IN EACH SKIN WAS REMOVED WITH A CUTOUT. EACH SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384450-14, REV A. 2L72 4F RTA2NM 20030307000162003030700016NM 2003 3 7 375PA0012 120030306A3350BAC1522453714 STRIP BOEING737 737317 138447PNM A PIDAK NONE O OTHER UKUNKNOWN 1 SO05375PA 23812 3C emergency light strip broken. Removed & replaced track cover. Connected wires, Ops chk. OK per MM 33-51-00. 2L72 4F RTA16WE 20030311000142003031100014SW 2003 3 11 HEEA085035 120030228A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPENS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 51029 ACTUATOR WOULD NOT RESPOND TO DROOP COMPENSATION ADJUSTMENTS. 1G71 3U H2SW 20030314001162003031400116NM 2003 3 14 SWAA030560 120030312A53116546576 FRAME BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1138, ABOVE STR 12R. R&R FRAME PER SRM. 2L72 4F A16WE 20030317000442003031700044NM 2003 3 17 03FDEA00180 120030226A3210 SNUBBER BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE NLG WORN A FDEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25264FE 21626 SMELLED BURNING RUBBER AFTER LANDING GEAR RETRACTION AND SMELL FADED ABOUT 4000 AGL. CHECKED NOSE WHEEL SNUBBER FOR WEAR. SNUBBER PADS WITHIN LIMITS IAW MM 32-45-021-2. CHECKED ALL OTHER TIRES/WHEELS, RAN A/C PACKS, NO PROBLEMS OR SMELLS NOTED. 2L73 4F4 FRTA3WE E2EA 20030317001012003031700101NM 2003 3 17 DHL2003743004 120030315A2612 LAMP BOEING727 727225 1384077NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01743DH 22438 1) APU FIRE WARNING LIGHT IN LEFT-HAND WHEEL WELL WILL NOT ILLUMINATE DURING TEST. 2) RELAMPED APU FIRE WARNING LIGHT LEFT-HAND WHEEL WELL IAW M/M 33-10-51. SYSTEM OPS CHECKED GOOD IAW M/M 26-15-00. 2L73 4F A3WE 20030317001572003031700157EU 2003 3 17 DHL2003367508 120030227A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R 0029517:Main cabin floor seat tracks worn LT/side t STA.4551 between FR.73 an 73A Corrective action:Blended IAW A300 SRM 53-10-00,alodined IAW A300 SRM 51-40-12,primed IAW A300 SRM 51-40-12,painted IAW A300 SRM 51-40-12. Blended was found within limits IAW A300 SRM 53-10-00,orig. mat. thickness 0.138,mat. removed 0.002 2L72 4F RTA35EU 20030320001062003032000106NM 2003 3 20 2003UALA00097 120030126A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 STATION 767 FRAME CRACKED AT STRINGER 9L AT SUPPORT RAIL ATTACH FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030417000302003041700030EU 2003 4 17 MALA030123 120030123A3260 DOWNLOCK SWITCH SAAB SF340 340B 7860101EU MLG DIRTY A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15365PX 340B265 CREW ON FLIGHT 3110, REPORTED THE RT GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR IS SELECTED DOWN. MAINTENANCE CLEANED AND LUBED DOWNLOCK ACTUATOR SWITCH, PERFORMED GEAR SWINGS. ALL CHECKS GOOD IAW SF340 AMM CHAP 32-30-00-5. 2L72 4T RTA52EU 20030321000172003032100017NM 2003 3 21 2003UALA00174 120030211A5320 SUPPORT BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29211UA 30217 (U) CHANNEL SUPPORT IS CRACKED AT STA 246 AFT SIDE OF FLOORBEAM, UPPER OUTBOARD & INBOARD RADIUS. MAJOR REPAIR ACCOMPLISHED. REPLACED 'U' CHANNEL SUPPORT. 2L72 4F4 FRTT0001SE E46NE 20030807000772003080700077SO 2003 8 7 C2XA03CL127 120030725A335078241 INVERTER EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716525 145403 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN ON THE RIGHT WINDSCREEN DIDN'T ILLUMINATE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030827000312003082700031NM 2003 8 27 F3LA200300120 120030615A5270ABS030903 SWITCH AIRBUSA319 A319111 3930336NM REFUELING PANEL FAULTY A F3LAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03915FR 436 1851 ABORTED TAKEOFF DUE TO REFUELING PANEL INDICATION. PERFORMED BRAKE INSPECTION IAW AMM 05-51-16-06. NO DEFECTS NOTED. REPLACED REFUELING PANEL DOOR SWITCH 20QJ IAW AMM 52-42-18-820-050 AND SYSTEM CHECKED NORMAL. 2L72 4F RTA28NM 20030910001702003091000170SO 2003 9 10 SIMA200321004 120030723A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. APPLIED TREATMENT TO THE BARE METAL SURFACE. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW EMB REPAIR STATEMENT IC 2003-145/2467A DATED JULY 22, 2003. (M) 2L72 4F RTT00011AT 20030912001662003091200166EU 2003 9 12 AWXA200300918 120030804A5320D5347112420100 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND AT FASTENER HOLES OF FLOOR SUPPORT SHEAR PLATE FR 69+6, Y-45. MAINTENANCE REMOVED FLOOR SUPPORT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-12, & 21-22, FIG 2, 3, & 8 , AND SRM 51-46-11, PG 1-2, FIG 1. 2L72 4F RTA28NM 20030730000972003073000097SO 2003 7 30 SIMA200317604 120030621A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21712AE 145247 ABI - DURING AN IMBV INSPECTION, FOUND CORROSOIN ON THE EXISTING REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED EXISTING REPAIR. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND INSTALLED. REPAIR DONE IAW EMB 145, SRM 145/1142 REV 22, 53-21-10 PARA 2 FIG 201 SHEET 1, AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030915000392003091500039EU 2003 9 15 BAQA089174 120030915A2822130100 CARTRIDGE UROCOPEC135 EC135T1 5620026EU BOOST PUMP INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135QC17 0281 BOOST PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030915001002003091500100GL 2003 9 15 BAQA089111 220030912A73140319928670 PUMP AGUSTAA109 A109E 0260119EU ALLSN 250C 250C20F 03013GL FUEL SYSTEM LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03109DU839 11503 LEAKING FUEL FROM DRIVESHAFT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 URTH7EU E4CE 20030925000602003092500060NM 2003 9 25 USAA030165 120030704A5320 ANGLE BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US 23886 FOUND ZEE ANGLE CORRODED 2 INCHES BY 3 INCHES, AFT ENTRY DOOR ZEE ANGLE, STATION 907 TO 1006. REPLACED ZEE ANGLE PER SRM 51-10-02 AND BOEING REPAIR DWG NR 65-52878. CORROSION LEVEL 1, TASK NR C53-67-01. (M) 2L72 4F RTA16WE 20030929000682003092900068NM 2003 9 29 QXEA200301053 120030830A5512 SKIN BOMBDRDHC8 DHC8401 1390041NM HORIZONTAL STAB DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 DENT IN UNDERSIDE OF LT HORIZONTAL STABILIZER INBOARD OF LOGO LIGHT AT LT STABILIZER STATION XH19.903 - YH103.25. REPAIRED IAW Q400 RD 8/4-55-121 AND HORIZON AIR EA 6-55-50. 2H72 4T RTA13NM 20031001001332003100100133WP 2003 10 1 GTIA030674 120030906A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FOUND MAIN CABIN FS 1068 WEB CRACKED RBL 54. REMOVED DAMGE. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20031006000302003100600030NM 2003 10 6 AWXA200301056 120030913A77009974M82P03 ALTERNATOR BOEING737 737301 1384611NM NR 2 ENGINE FAULTY A AWXAC ABORTED TAKEOFF JS WARNING INDICATION AFFECT SYSTEMS TOTAKEOFF 1 WP28326AW338689360 23258 ON TAKEOFF ROLL AT DFW EN ROUTE FOR PHX NO. 2 ENGINE N2 INDICATOR HAD ERRATIC FLUCTUATION BETWEEN 30-40 PERCENT, REJECTED TAKEOFF BELOW 80 KTS. MAINTENANCE ISSUED MEL 77-3, COND. 2 (NR 2 ENG TACH GEN INOP). WHEN AIRCRAFT ARRIVED IN PHX MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE CONTROL ALTERNATOR SPEED SENSOR IAW BMM 73-21-08, PG. 401, ENGINE RUN OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST AND TEARDOWN OF STATOR ALTERNATOR S/N GJAG6485M WAS FO FAULT FOUND, UNIT TESTED IAW CMM 77-11-21, REV. 03. . 2L72 4F RTA16WE 20031001001222003100100122NM 2003 10 1 03FDEA01534 120030902A5320A5A70321 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CENTER CARGO PIT HAS A DAMAGED STRINGER SPLICE AT STA 1541, 48R AT TRANSVERSE AND LONGITUDINAL SPLICE. DAMAGED STRINGER SPLICE AT STA 1541 48R AT TRANSVERSE AND LONGITUDINAL SPLICE REPAIRED AS PER SRM 53-10-00 FIG 2 SHT 5 IAW EA 1-5310-72657 2L73 4F RTA22WE 20031007000062003100700006NM 2003 10 7 AALA20030688 120030616A5320111T1002 PLATE BOEING767 767223 1385123NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21329AA 22329 FOUND DURING INSPECTION CF, THE H11 BOLTS THROUGH THE SPLICE PLATE PER BOEING S/B 767-57 A0064, 'C' HOLE WAS FOUND TO BE CORRODED AND REQUIRED OVERSIZING. THE HOLE WAS COMMON TO THE HORIZONTAL FLANGES OF THE OUTBOARD WING SPAR CHORD. REAMED CORRODED 'C'C HOLE TO 0.781 INCH DIAMETER/HFEC INSPECTED 'C' HOLE, HOLE IS CORROSION AND CRACK FREE. INSTALLED A 2ND OVERSIZE, .75 INCH BOLT. SEALED THE FASTENER PER BOEING S/B 757-57A0064. (M) 2L72 4F RTA1NM 20031007000952003100700095NM 2003 10 7 SWAA031993 120030905A36101301009 BOOT BOEING737 7377H4 1384404NM BLEED AIR DUCT LEAKING A SWAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SW29706SW 27840 AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AND REPLACED PNEU BLEED AIR DUCT BOOT AT KEELBEAM AND THREE BODY DRAINS, TIGHTENED CLAMPS AND REMOVED AND REPLACED WATER SEPARATOR SEALS PER MM. 2L72 4F RTA16WE 20031020000782003102000078NM 2003 10 20 VNAA0310001 120031001A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CARGO DOOR LOOSE A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07437JS 3055 EN ROUTE, THE CREW RECEIVED A BAGGAGE DOOR OPEN INDICATION AND DIVERTED TO RDU. MAINTENANCE INSPECTED AND FOUND FASTENERS LOOSE ON THE SHOOT BOLT PROXI SENSOR AND SECURED THE FASTENERS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031027000192003102700019EA 2003 10 27 COMA0360429 120030924A335059465 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DEFECTIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01966CA 7132 FLIGHT 5498 DURING INSPECTION FOUND THE FLOOR PROXIMITY EMERGENCY LIGHTING INOPERATIVE AT ROWS 6,7, AND 8. REPLACED SECTION OF THE FLOOR EMERGENCY LIGHTING STRIP. 2L72 4F4 FRTA21EA E15NE 20031021002502003102100250SO 2003 10 21 C2XA03IA095 120030918A28302810051103 VALVE EMB 145 EMB145XR SO RIGHT WING INOPERATIVE A C2XAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW2713133 145712 AFTER TAKEOFF FUEL NOTICED BY THE TOWER. MAINTENANCE VISUALLY INSPECTED BOTH WINGS, NO LEAKS NOTED. FUEL VENTING FROM RT WING. MAINTENANCE REMOVED AND REPLACED THE RT WING VENT VALVE, REF 145XR MM 28-23-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20031031000012003103100001NM 2003 10 31 03FDEA01624 120030924A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 AFT CARGO BAY, FRAME DENTED BS 1110 STR 26R. DAMAGE ON FRAME AT BS 1110, STR 26R (DENT) FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 1110, STR 26R IAW SRM 51-40-3 AND EA 7-5310-54986. 2L73 4F RTA3WE 20031027001232003102700123NM 2003 10 27 QXEA200301184 120030924A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 PDX- NR 4 FLAP TRACK RT WING INBOARD SIDE LOAD ROLLER TRACK SURFACE IS PITTED. REPAIRED IAW HORIZON AIR EA 2-57-234. 2H72 4T RTA13NM 20031105000702003110500070 2003 11 5 SWAA032285 420031017A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031106002332003110600233NM 2003 11 6 ASAA0310461 120030515A5310HFAB53ST011 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE SHEAR TIE AT FUSELAGE STATION 987, STRINGER 25L-26L CORRODED. REPAIRED SHEAR TIE PER SRM. (M) 2L72 4F A16WE 20031107001492003110700149WP 2003 11 7 GTIA030739 120030923A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND MAIN CABIN STATION 1117 TO STATION 1174 RIGHT SIDE OUTBOARD FLOOR PANEL HAS BROKEN HALF/DAMAGE AT CORNER. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20031113000312003111300031EU 2003 11 13 BAQA090564 120031022A33406034743 POWER SUPPLY BOLKMS117 BK117B2 5626013EU STROBE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03296GL 7222 ZERO VOLTAGE COMING FROM 500 VOLTS PLUG. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030918000172003091800017NM 2003 9 18 03FDEA01516 120030911A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 N01548 CRACKED STRINGER, BS 720B 4 STR 15R. REMOVED DAMAGED PORTION OF STR 15R AT BS 720B 4 IAW SRM 53-10-3 FIG 5. HFEC INSPECTION ON PERPHERY OF CUTOUT NO CRACKS NOTED. FABRICATED ALODINED, PRIMED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3 FIG 5. 2L73 4F RTA3WE 20031007000392003100700039EA 2003 10 7 A6WA200340134 120030909A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A A6WAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 GL31432AW 7257 CARGO SMOKE MESSAGE INTERMITTENT DURING FLIGHT AT 20,000 FT COMPLIED WITH EMERGENCY ACTION CHECKLIST. REMOVED AND REPLACED NR 2 FIRE BOTTLE (REF BLK 2) SEE 116092/2 FOR MEL. FIRE DEPARTMENT FOUND NO EVIDENCE OF SMOKE OR FUMES. SMOKE DETECTION SYSTEM, OPS TEST GOOD AT THIS TIME. (M) 2L72 4F RTA21EA 20031008000192003100800019EA 2003 10 8 03257653 120030914A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27653BR 7438 DURING MAINTENANCE INSPECTION THE AFT EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTNANACE PERSONNEL RECONNECTED AFT EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031119000422003111900042EU 2003 11 19 AWXA200301205 120030924A5320D53913789200 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT CENTER PROFILE FR 31, AT FASTENER HOLES. MAINTENANCE REMOVED AND REPLACED CENTER PROFILE AT FR 31 IAW A320 SRM 51-42-11, PG. 21 AND 22, FIG. 8, AND PG. 7-10, AND 12, FIG. 2 & 3. 2L72 4F RTA28NM 20031119000852003111900085NM 2003 11 19 QXEA200301268 120031011A335010005511 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09374PH 528 ON FLIGHT 2199 EMERGENCY EXIT LIGHT BENEATH FLIGHT ATTENDENT'S COMMUNICATION PANEL IS INTERMITTENT. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031117000752003111700075NM 2003 11 17 DHL2003749508 120030920A5320 FLOOR SUPPORT BOEING727 7272J0 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C CHECK, PIT FLOOR SUPPORT FROM STA. (50 E TO STA. 990 LBL 14 HAS SEVERAL DENTS. REMOVED DAMAGED FLOOR SUPPORT FROM AFT. PIT STA. 950 E TO 990, LBL 14 I.A.W. B-727 SRM 51-30-2. DRILLED NEW FLOOR SUPPORT P.O. NR 328319, P/N BAC 1500-6199. 3) DIMENSION 5 INCHES, 10 INCHES IAW SAMPLE 51-20-1. 3) ALODINED AND PRIMED IAW B-727 SRM 51-10-2. 4) INSTALLED NEW FLOOR SUPPORT IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20031125000522003112500052WP 2003 11 25 DHL2003807547 120031028A5280 SKIN DOUG DC8 DC873F 302199FWP RT MLG DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT MLG DOOR LOWER PART INTERNAL SKIN CRACKED 0.500 AT STA 932.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER IAW SRM 52-2-0 FIG 4. PERFORMED HEAT TREATMENT TO DOUBLER IAW SRM 51-1-1 PG 17. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 52-2-0 FIG 4, SRM 51-1-21 PG 1. FOR OPS CHECK SEE JC 8-32-00-003. 2L74 4F RT4A25 20031218000592003121800059EU 2003 12 18 03329309 120031125A33502058403 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT WORN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27309UE 41022 DURING INSPECTION THE EMERGENCY LIGHT NEAR THE GALLEY WAS FOUND INOPERATIVE. THE CONNECTOR WAS FOUND TO BE WORN AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030321000302003032100030NM 2003 3 21 2003UALA00187 120030207A5754114W425011 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29766UA 26917 DELAMINATED TRAILING EDGE WEDGE. SLAT NR 5 BECAME DELAMINATED. REMOVED AND REINSTALLED T/E WEDGE. 2L72 4F4 FRTT0001SE E46NE 20030321000792003032100079NM 2003 3 21 2003UALA00220 120030224A5754114W414015 SKIN BOEING777 777222 1385219NM NR 4 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 TRAILING EDGE WEDGE, SLAT NR 4, DELAMINATED REPAIRED TRAILING EDGE WEDGE, SLAT NR 4. 2L72 4F RTT0001SE 20030731001022003073100102NM 2003 7 31 QXEA200300892 120030726A2760C1486561 TRANSDUCER BOMBDRDHC8 DHC8401 1390041NM SPOILER MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09411QX 4055 PDX- ON FLIGHT 2310 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. REMOVED AND REPLACED LEFT HAND INBOARD SPOILER LVDT. OPERATIONAL CHECKS GOOD. AIRCRAFT REUTNED TO SERVICE. 2H72 4T RTA13NM 20030805000092003080500009CE 2003 8 5 VIB2003F00000 120030523A3230 HOOK BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE RT MLG FAILED B VIB3O OTHER O OTHER NRNOT REPORTED 1 SO0374 FF9 J-HOOK OVER LANDING GEAR SELECTOR HANDLE IN COCKPIT RETRACTED WITH AIRCRAFT ON GROUND. LUBRICATED AND ACTUATED (J) HOOK AND RIGGED RIGHT MAIN LANDING GEAR SAFETY SWITCH, IAW MM. TIGHTENED B-NUT ON RT MAIN LANDING GEAR ACTUATOR AND SERVICE HYDRAULIC SYSTEM. OPERATIONAL AND LEAK CHECK SATISFACTORY. THE MAINTENANCE APPROVED, RETURNED TO SERVICE. (WO 13396) 2L72 4T4 T A24CE E4EA 20030828001502003082800150NM 2003 8 28 HALA0300697 120030806A5755 BRACKET BOEING717 717200 1383700NM RT SPOILER CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13483HA 55128 RIGHT OUTBOARD SPOILER BRACKET CRACKED. REPAIRS IN WORK. (M) 2L72 4F TRA6WE 20030723000252003072300025 2003 7 23 UIEA200300028 420030630A25657A14124 SLIDE BOEING747 74747UF 1384949NM PAX DOOR FAILED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15494MC 29255 DURING C-04 CHECK IN FRA, A TEST OF THE UPPER DECK RIGHT ESCAPE SLIDE WAS TO BE PERFORMED. DURING PREPARATION A NOTE WAS MADE TO A DEFECT WITH A PACKBOARD LOCKING PLATE & 4 RETAINING SCREWS BEING LOOSE & LOCKING PLATE BEING BENT & OUT OF POSITION. AS A PRECAUTION SLIDE INFLATION WAS PROHIBITED TO AVOID A/C DAMAGE. WHEN SLIDE WAS MANUALLY DEPLOYED THROUGHT DOOR, IT TWISTED AFT AND FAILED TO LOCATE ON THE HOOK. SLIDE FAILED TO DEPLOY CORRECTLY & REMOVED TO SHOP FOR INVEST. DURING INSTALL OF SLIDE A FAILURE MUST HAVE BEEN PRESENT OR OCCURRED. MECHANISM BENT & NOT POSSIBLE TO FULFILL ORIGINAL FUNCTION. 2L74 4F RT1384945 20030724000552003072400055EU 2003 7 24 AWXA200300762 120030616A5320D53370039201 STIFFENER AIRBUS320 A320231 3930325EU FLOOR SUPPORT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON LT OUTBOARD FLOOR SUPPORT SIDE RAIL STIFFENER (PROFILE) FR 37, Y-1732. MAINTENANCE REMOVED DAMAGED PROFILE FR 37, Y-1732; FABRICATED A NEW REPLACEMENT PROFILE PER DWG D53370039; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 26-30 & 35 FIG 10-12. 2L72 4F RTA28NM 20030806000682003080600068SO 2003 8 6 C2XA03TY098 120030727A53201452542200 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713990 145277 DURING A SCHEDULED 2C INSPECTION THE LT LAV SIDEWALL FLOOR SUPPORT HAD CORRODED NUT PLATED AND RIVETS FWD AND AFT. MAINTENANCE REMOVED AND REPLACED THE LT LAV FLOOR SUPPORT WITH ALL NEW HARDWARE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030807000352003080700035NM 2003 8 7 USAA030127 120030624A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US 24552 FOUND ZEE ANGLE CORRODED SEVERAL 1 INCH IN DIAMETER AREAS. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED WITH NEW Z-ANGLE PER SRM 51-20-01. (M) 2L72 4F RTA16WE 20030829000872003082900087NM 2003 8 29 P5CA0300909 120030808A793141806104 INDICATOR BOEING747 74746NF 13848BTNM OIL PRESSURE INOPERATIVE A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23450PA 30808 NR 4 ENG OIL PRESSURE INDICATION FAILED AFTER ENG START. RE-PINNED BRKN AND WIRE AT DT679 PIN A. ALSO REMOVED AND REPLACED INOP OIL TRANSMITTER. 2L74 4F RTA20WE 20030903001352003090300135WP 2003 9 3 2003F00538 120030405A5347 SEAT TRACK DOUG DC9 DC987 3022087WP FUSELAGE CORRODED A WXOAK NONE O OTHER ININSP/MAINT 1 WP17948MA 49778 FOUND CABIN FLOOR SEAT TRACK HAS CORROSION FS 200-223 LBL 22. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR MEMBER IAW DC9/MD80 SRM 51-10-3, 53-05 FIG 4B-1, 53-05 AND 53-05 FIG 4F. (M) 2L72 4F RTA6WE 20030904000052003090400005EA 2003 9 4 SWIA200312154 120030625A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAEG CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 605 LBL 42 TRANSVERSE BEAM ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601R35011-13 2L72 4F RTA21EA 20030904000072003090400007EA 2003 9 4 SWIA200312156 120030625A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52 2L72 4F RTA21EA 20030903001712003090300171EU 2003 9 3 2003F00543 120030707A3260 WARNING SYSTEM BRAERODH125 HS125700A 4230170EU LANDING GEAR MALFUNCTIONED A AOQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA11727TA NA0202 FOLLOWING TAKEOFF, MAIN GEAR RETRACTION RED UNSAFE LIGHT REMAINED ILLUMINATED. GEAR WAS RECYCLED AND ALL GREEN DOWN/LOCKED WAS INDICATED. AIRCRAFT RETURNED TO POINT OF DEPARTURE. AIRCRAFT RETURNED TO ISP FOR INSPECTION AND EVALUATION. NO DISCREPANCIES NOTED DURING FERRY FLIGHT. LANDING GEAR INSTALLATION, MICRO-SWITCHES AND SIDESTAYS INSPECTED AND ADJUSTMENTS CHECKED FOR PROPER RIGGING. ACCOMPLISHED SUCCESSFUL GEAR SYSTEM SWINGS AND FUNCTIONAL CHECKS. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A3EU 20030903001782003090300178 2003 9 3 AALA20030788 420030722A34426225132109 TRANSCEIVER BOEING767 767323 1385205NM WEATHER RADAR INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21357AA 24038 FLT 1539 - MIA-SFO - WEATHER RADAR INOPERATIVE. AIRCRAFT RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR TRANSCEIVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030806001392003080600139SO 2003 8 6 C2XA03SH213 120030702A532014590082003 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030814000592003081400059EA 2003 8 14 SWIA200312172 120030708A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07905SW6141 6141 7437 STAB CHANNEL 1 INOPERATIVE. CHANGED HSTCA & MCU IAW 27-41-00. P/N 7062-3 S/N OFF 926. 2L72 4F4 FRTA21EA E15NE 20030725000322003072500032SO 2003 7 25 RAIA00305146 120030520A243430086011 GENERATOR EMB 145 EMB145 3260210SO NR 4 INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03807HK4801 274 145119 GENERATOR NR 4 FELL OFF LINE. MAINTENANCE REMOVER AND REPLACED NR 4 GENERATOR. 2L72 4F RTT00011AT 20030728000012003072800001NM 2003 7 28 SWAA031628 120030719A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT 2 EA BULBS INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030723000032003072300003EU 2003 7 23 USAASA03074 120030701A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19766US 1378 DURING THE EMERGENCY LIGHTS TEST, RECEIVED 'L AFT EPSU' MESSAGE. MAINTENANCE REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT BATTERIES. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030729000022003072900002NM 2003 7 29 03189410 120030708A3350 LIGHT DORNERDO32 DO328300 NM CABIN MALFUNCTIONED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27410FJ 3165 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE BETWEEN SEAT ROWS 7 AND 8. MAINTENANCE PERSONNEL RESET THE FLOOR TRACK LIGHTING SWITCH. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030825000622003082500062NM 2003 8 25 UPS03241061 120030714A5312652286728 PRESSURE PANEL BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE:C NLG WHEEL WELL RT CEILING PRESSURE PANEL HAS A CRACK FROM OUTBOARD EDGE OF PANEL TO BOLT HOLE. PANEL REPAIRED IAW 2003-041-005. REFERENCE UPS ENGINEERING FILE NR 727-53-20125. 2L73 4F A3WE 20030826000122003082600012NM 2003 8 26 03FDEA01360 120030822A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 CORROSION (C53-113-01, 2) ON FRAME STA 970 BETWEEN STR 28L & 29L. CORROSION ON FRAME BS 970, STR 28L-29L WAS FOUND OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED FRAME SECTION AT SHEAR TIE SKIN ATTACHMENT, FABRICATED REPAIR PARTS, AND INSTALLED PER SRM 53-10-4. 2L73 4F RTA3WE 20030911000922003091100092WP 2003 9 11 DHL2003873530 120030621A5753 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING INBD FLAP LOWER FWD PLATING HAS INERIM REPAIR AT STA XW.86.50 TO XW.115.250. PERFORMED MAJOR REPAIR IAW EODHL-030602, ED-3428. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030602, ED-3428. FABRICATED A NEW SKIN SEGMENT, A SPLICE STRAP, AND A FILLER IAW EODHL-030602, ED-3428. CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT, SPLICE STRAP AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SEGMENT AND SPLICE STRAP AND FILLER ON LT WING INBD FLAP LWR PLATING, STA XW.86.50 - XW.115.250, USING NEW FASTENERS IAW EODHL-030602, ED-3428 AND SRM 51-1-21 PG1. 2L74 4F4 FRT4A25 E2GL 20030930000062003093000006NM 2003 9 30 AWXA200301025 120030906A2560P4010021 BATTERY BOEING737 7373G7 1384595NM ZONE 900 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28160AW 23782 EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031002000892003100200089NM 2003 10 2 C1HA200386005 120030908A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 CORROSION ON FLOORBEAM UPPER CHORD AT BS 312. 2L73 4F A3WE 20030909002762003090900276SO 2003 9 9 RAIA00307197 120030725A324038793500 SHUTOFF VALVE EMB 145 EMB145LR 3260212SO BRAKE SYSTEM DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03811HK8458 145256 5316-PIT- RIGHT OB BRAKE INOPERATIVE MESSAGE. MAINTENANCE REMOVED AND REPLACED RT OB BRAKE SHUTOFF VALVE. 2L72 4T RTT00011AT 20031015000662003101500066NM 2003 10 15 USAASB03143 120030822A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU 23551 MAINTENANCE REPORTED THE LEFT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031022000302003102200030NM 2003 10 22 C1HA200393012 120030922A3350 BATTERY BOEING727 727212 138407GNM EMERGENCY LIGHT DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15293AS 21348 AFT AIR STAIR EMERGENCY AREA ILLUMINATION LIGHT IS INOP.REMOVED AND REPLACED BATTERIES REF: 727 MM 33-50-61. OPS CHECK WAS GOOD. 2L73 4F A3WE 20031028000882003102800088NM 2003 10 28 2003UALA00772 120031010A2820 VALVE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CROSS FEED DEFECTIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29566UA 26670 FUEL IMBALANCE BETWEEN LT AND RT TANKS. THE CAUSE OF THE FUEL IMBALANCE CONDITION WAS DUE TO A DEFECTIVE CROSS-FEED VALVE BODY ASSY. SHOP FINDINGS REVEALED THAT THE SPLINE AND SEAL ON THE VALVE DISK WERE WORN OUT. THIS WAS THE FIRST TIME THE VALVE WAS REMOVED SINCE THE DELIVERY OF A/C IN AUG OF 1992. THIS PARTICULAR FAILURE MODE WILL SET UP A CONDITION WHERE BOTH THE LEFT AND RIGHT MAIN TANK PUMPS ARE FEEDING BOTH LEFT AND RIGHT ENGINES. THE STRONGER MAIN TANK PUMPS FROM EITHER THE LEFT OR RIGHT WILL OVERRIDE THE WEAKER SIDE THEREFORE ALLOWING A FUEL IMBALANCE TO OCCUR DURING THE FLIGHT. IN THIS CASE, THE STRONGER PUMPS WERE FROM THE LEFT AS EVIDENCED BY THE FUEL QUANTITY INDICATION. 2L72 4F4 FRTA2NM E17NE 20031121000082003112100008CE 2003 11 21 AMWA78 120031104A53101145140587 BRACKET BEECH 1900 1900D 1154162CE CARGO DOOR FRAMEWORN A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127YV UE127 WHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE CARGO DOOR UPPER FORWARD GAS SPRING ASSEMBLY BRACKET HAD WORKING RIVETS. 2L72 4T RTA24CE 20040212000532004021200053EU 2004 2 12 UO22003F00013 120031201A291522843773MI RELIEF VALVE AMD FALC20FALCON20F5 2730105EU HYD RESERVOIR LEAKING B UO2RA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL19600CD202 377 THE AIRCRAFT WAS CLIMBING TO 37,000 FT WHEN THE LOW HYDRAULIC RESERVOIR HEAD PRESSURE LIGHT COME ON. THE PILOT DESCENDED TO 20,000 FT IAW THE FLIGHT MANUAL. WE FOUND THAT THE NR 2 HYDRAULIC RESERVOIR OVER PRESSURE RELIEF VALVE WAS LEAKING. THE VALVE WAS PURCHASED FROM MFG ON 11-20-03, IT WAS A NEW PART. 2L72 4F RTA7EU 20031029001132003102900113EA 2003 10 29 QXEA200301193 120030928A2611 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE LAV SMOKE DET ACTIVATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09609QX 10031 ON FLIGHT 2529 AMOKE AFT LAVATORY WARNING ILLUMINATED ON TAKEOFF ROLL. SMOKE ALARM WAS GOING OFF AND THERE WAS A PRESENCE OF SOME SMOKE, ACCORDING TO THE FLIGHT ATTENDANT. REMOVED AND REPLACED NEW WIRES ON APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20031103000152003110300015 2003 11 3 DL757030867 420030916A2565580242024 CONTROL CABLE BOEING757 757232 1384965NM RT WING SLIDE SEIZED A DALAK NONE O OTHER ININSP/MAINT 1 SO27658DL 24420 RT OFF WING SLIDE MANUAL DEPLOYMENT CABLE FOUND SEIZED DURING OPN 6740, OFF WING SLIDE DEPLOYMENT SYSTEM TEST. CABLE 580-242-024 REPLACED ON NR 1170. AC UNDERGOING HMV-2 AT THE TIME OF DISCOVERY. 2L72 4F RTA2NM 20031103000632003110300063WP 2003 11 3 03FDEA01681 120031002A5270 SWITCH DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL A/C DOOR INOPERATIVE A FDEAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25374FE 46612 AIR CONDITIONING DOORS LIGHT ON S/O PANEL BEGAN FLICKERING INFLIGHT. FUEL WAS DUMPED AND LANDING ACCOMPLISHED AT SLC IAW RED TABS. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-04-04 CATEGORY: C EXPIRATION: 11OCT03, FACT 03OCT03 07:58 EWR R . REMOVED AND REPLACED ALL 3 DOOR SWITCHS IAW DC-10-10 MM 52-70-07-2. OPS CHECK GOOD. 2L73 4F4 F A22WE E23EA 20031106001572003110600157NM 2003 11 6 03FDEA01845 120031101A323269163395 SUPPORT FITTING BOEING727 727200 138407ENM NLG DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-3220-73848 LANDING GEAR - NLG - ELONGATED HOLES IN 69-16339-5 SUPPORT FITTING. COMPLIED WITH EA 7-3220-73848 LANDING GEAR - NLG - ELONGATED HOLES IN 69-16339-5 SUPPORT FITTING, AT MAE. 2L73 4F RTA3WE 20031112000272003111200027CE 2003 11 12 GLBA2003143 120031101A61201293640919 CIRCUIT BOARD BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA PROP CONTROL FAILED A GLBAO OTHER S AFFECT SYSTEMS LDLANDING 1 NM03255GL UE255 NR 2 PROP FEATHERED ON LANDING APPROACH, REMOVED AND REPLACED PCB. OPS CK GOOD. 2L72 4T3 TRTA24CE E2NE 20031112000722003111200072NM 2003 11 12 AWXA200301396 120031019A53306545769545 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A .5 INCH CRACK WAS FOUND ON PREVIOUS REPAIR AT FASTENER HOLE OF LOWER FUSELAGE SKIN BS 454, RBL 3. MAINTENANCE TRIMMED OUT DAMAGE ON PREVIOUS REPAIR AT FASTENER HOLE OF LOWER FUSELAGE SKIN BS 454, RBL 3; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, A STRINGER FILLER, 5 EACH STRUCTURAL FILLERS, A DOUBLERS, AND A TRIPLER; INSTALLED REPAIR PARTS IAW ER 15-5331-03311-ES1. 2L72 4F RTA16WE 20030730000672003073000067WP 2003 7 30 ABXA030258 120030312A5200 DOOR FRAME DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CENTER LATCH HOOK MOUNT HOLE AT STA 167.0 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46043MR. 2L74 4F 4A25 20030916000922003091600092EA 2003 9 16 REXA03002 120030530A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A REXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO258432A 7432 SMOKE AND FUMES IN COCKPIT AIR RETURN. PERFORMED HIGH POWER ENGINE RUNS CLEARED 10 AND 14 STAGE DUCTS, NO SMOKE NOTED INSPECTED ACMS AND ENGINES. NO DEFECTS, OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030916001152003091600115 2003 9 16 AALA20030874 420030818A2565 CONNECTOR DOUG DC9 DC982 3022082WP ESCAPE SLIDE LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW217536A 49990 SLIDE HANDLE EMERGENCY LIGHT INOPERATIVE. RESEATED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031117000302003111700030NM 2003 11 17 AWXA200301121 120031001A2913887673 PUMP AIRBUSA319 A319132 3930340NM NR 1 ENGINE HYD LEAKING A AWXAB EMER. DESCENT K FLUID LOSS CRCRUISE 1 WP28824AW 1490 EN ROUTE FROM IAD TO PHX FLIGHT CREW OBSERVED A LOSS OF THE GREEN SYSTEM HYDRAULICS, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE PLUG ON TOP THE NR 1 ENGINE DRIVEN PUMP LEAKING. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-51-04. OPERATIONAL CHECK GOOD. FUNCTIONAL TEST OF HYD EDP CONFIRMED FAILURE OF UNIT. SOLENOID WAS FOUND WORN BEYOND LIMITS, REPLACED SOLENOID AND PACKINGS. UNIT REPAIRED AND TESTED IAW CMM 29-11-34, REV. 4. 2L72 4F RTA28NM 20040112001242004011200124WP 2004 1 12 GTIA031028 120031107A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND CABIN STATION 160-200 LBL 7 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATE DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. PITTED CORROSION AND GOUGES FOUND UNDER FLOOR SUPPORT IN THE SKIN 160-200 LBL 7. CUTOUT CORRODED AREA 4 INCHES BY 52 INCHES ON FLOOR SUPPORT SKIN. FABRICATED NEW FLOOR SUPPORT STATION 160-200 LBL 7. INSTALL NEW FLOOR SUPPORT AT STATION 160-200 STR 7L. (M) 2L72 4F RTA6WE 20040112001502004011200150EU 2004 1 12 MALA030562 120031222A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15441XJ 340B441 EMERGENCY LIGHTS AT 13LN, 14LN, 26LN, 27LN, 34LN AND 35LN INOP. MAINTENANCE REPLACED POWER SUPPLY 23LN, P/N 3301-51, S/N ON 1422, S/N OFF 1323, OPS CHECKS GOOD IAW SAAB AMM 33-50-10. 2L72 4T RTA52EU 20040112002102004011200210SW 2004 1 12 HEEA087812 120030622A8011A1077V RELAY BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL STARTER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 STARTER RELAY STICKS CLOSED. TO BE SENT TO VENDOR. 1G71 3U3 U H2SW E1GL 20040113002372004011300237EA 2004 1 13 QXEA200301483 120031125A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX- LIGHTING STRIKE BURN MARK AT FUSELAGE STATION 169.00 ON THE MATING SURFACE FOR THE RADOME. REPAIRED IAW CRJ SRM 53-00-01 AND 51-20-06. 2L72 4F RTA21EA 20040115000212004011500021NM 2004 1 15 03FDEA02036 120031203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION ON FRAME SPLICE STA 500 RBL 26.5 WL 156. REMOVED CORROSION FWD CARGO ON FRAME SPLICE AT BS 500, RBL 26.5, WL 156 IN AREA OF 1 X1 X .020 INCH MAX REMOVED. FOUND TO BE OUT OF LIMITS. FABRICATED THE DOUBLER MADE FROM 7075-T6 0.071, AND INSTALLED THE REPAIR DOUBLER IAW SRM 51-40-3. 2L73 4F RTA3WE 20031216000612003121600061NM 2003 12 16 SWAA032547 120031118A53306550570 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C2 CHECK, FOUND .5 LONG FUSELAGE SKIN CRACK AT R2 DOOR UPPER FWD HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031217001002003121700100SO 2003 12 17 C2XA03CL189 120031118A33503025103 LIGHT EMB 135 EMB135LR 3260305SO EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715527 145413 CLE FLIGHT 2051 THE CREW REPORTED THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031218000812003121800081NM 2003 12 18 2003UALA00862 120031114A5315 FLOORBEAM BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29209UA 30215 STA 246 FLOORBEAM LBL 7.88 VERTICAL STIFFENER CRACKED. MAJOR REPAIR ACCOMPLISHED. STIFFENER REPLACED. 2L72 4F4 FRTT0001SE E46NE 20031218001312003121800131EU 2003 12 18 RAIA00311290 120031122A3297 WIRE AEROSPATR42 ATR42300 8680920EU RT UPLOCK SWITCHBROKEN A RAIAO OTHER O OTHER DEDESCENT 1 CE03426TE 228 ON DESCENT FOR LANDING RIGHT MLG CYCLED RAPIDLY UNTIL LANDING GEAR WAS EXTENDED. MAINTENANCE DEFERRED LANDING GEAR PER MEL 32-31-3. SUBSEQUENTLY CLEARED DMI - REPAIRED BROKEN WIRE TO RIGHT HAND MLG UPLOCK SWITCH. 2H72 4T RTA53EU 20031222000292003122200029NM 2003 12 22 QXEA200301529 120031207A5411 FRAME DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 FRAME CHAFED UNDER RIGHT HAND GRAVEL GUARD. REPAIRED IAW RD 8-54-1052. 2H72 4T RTA13NM 20031222001212003122200121EA 2003 12 22 ASOA03546 120031029A3350YAD4F RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT FAILED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11719EV 10099 DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS CYCLED ON THEN OFF IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE K135 SENSE RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031223000502003122300050NM 2003 12 23 SWAA032671 120031207A213340631997201AA OUTFLOW VALVE BOEING737 7373H4 1384600NM CABIN PRESSURE FAULTY A SWAAO OTHER S AFFECT SYSTEMS CLCLIMB 1 SW29615SW 27698 LOSS OF CABIN PRESSURE LEVEL AT FL290, CABIN PRESS REACHED FL220. UNCONTROLABLE IN MANUAL MODE. GOOD BLEED AIR PRESSURE DURING DEPRESSURIZATION. REMOVED AND REPLACED MAIN OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER PER MM. 2L72 4F RTA16WE 20031223001102003122300110NM 2003 12 23 QXEA200301545 120031208A5410 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX- LEFT HAND NACELLE AFT FINGERNAIL DECK IS CRACKED AT FINGERNAIL MOUNT HOLES. REPAIRED IAW Q400 RD 8/4-54-044. 2H72 4T RTA13NM 20031229001302003122900130EA 2003 12 29 MASA200300470 120031130A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER L NO TEST ININSP/MAINT 1 SW0737218 7218 FLT CXLD AND FERRIED TO PHX FOR AFT FLOOR PATH EMERGENCY LIGHTS INOP. MX REPLACED POWER PACK AND REPAIRED ASSY WIRING. 2L72 4F RTA21EA 20031231000502003123100050EA 2003 12 31 ASOA03578 120031114A3350BR9279106 CASE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11850AS 7355 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BASE AND LENS BY THE SERVICE DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031006000942003100600094CE 2003 10 6 DXTA200300106 120030828A2910 MANIFOLD CESSNA750 750 2076810CE HYD SYSTEM DAMAGED E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07931QS 7500064 DESCENDING THRU FL180 AN UNCOMMANDED EXTENSION OF GEAR WAS EXPERIENCED (GEAR DID NOT FULLY EXTEND) GOT UNLOCKED LIGHT THEN GEAR RETRACTED. - TROUBLESHOT AND FOUND HYDRAULIC MANIFOLD DOES NOT HOLD PRESSURE. REMOVED AND REPLACED LANDING GEAR HYDRAULIC MANIFOLD ASSEMBLY IAW CESSNA 750 MM CHAPTER 32-30-02, OPS CHECKED GOOD. 2L72 4J RTT00007WI 20040106001862004010600186NM 2004 1 6 AALA20030930 120030902A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 32AB. RECONNECTED LOOSE CONNECTOR AT SEAT 32AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040112000082004011200008EU 2004 1 12 USAABA03041 120031212A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 EPSU BATTERY AT R2 DOOR FAILED SELF TEST. MAINTENANCE REPLACED THE EPSU BATTERY AT R2 DOOR. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA46NM 20031124001472003112400147NM 2003 11 24 CALA0300601 120031009A532069353654 ANGLE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 FLOOR SUPPORT ANGLE CRACKED AT STA 380 - 400 BL-0. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031125000952003112500095NM 2003 11 25 QXEA200301412 120031108A5260 CHAIN BOMBDRDHC8 DHC8401 1390041NM AFT AIRSTAIRS BROKEN A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09410QX 4053 BOI- ON FLIGHT 2398 AFT AIRSTAIRS CANNOT BE RETRACTED. CHAINS ON SIDE OF STEPS ARE BROKEN. THIS SDR IS WAITING FOR FURTHER INFORMATION. 2H72 4T RTA13NM 20031126000052003112600005NM 2003 11 26 QXEA200301468 120031121A2843 CONNECTOR DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM DIRTY A QXEAO OTHER O OTHER CRCRUISE 1 NM09352PH 494 PSC- ON FLIGHT 2105 DURING CRUISE NR 2 FUEL TEMPERATURE GAUGE FLUCTUATED BETWEEN 60-80 DEGREES. TURNED THE AUXILIARY FUEL PUMP ON AS PER CHECKLIST WITH NO CHANGE. AFTER FIVE MINUTES THE GAUGE RETURNED TO NORMAL FOR THE REMAINDER OF THE FLIGHT. CLEANED FUEL TEMPERATURE TRANSMITTER ELECTRICAL CONNECTION. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031203001262003120300126EA 2003 12 3 A6WA200340129 120030902A2421755469D IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 FAILED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31422AW 7341 'IDG 1' AMGER CAS MESSAGE ON TAKEOFF ROLL, FOLLOWED BY 'GEN 1 OFF' AMBER CAS MESSAGE, CREW PERFORMED QRH AND ABORTED TAKEOFF. FOUND IDG NR 1 LOW OIL LEVEL, SERVICED IDG IAW AMM, GROUND RAN ENGINE, LEAK AND OPS CHECK GOOD. VOLTS AND FREQUENCY NORMAL, OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040114001662004011400166NM 2004 1 14 DLM90030977 120031102A3222 STRUT DOUG MD90 MD9030 3023690NM NLG LOW A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27904DA 53384 NOSE GEAR FAILED TO RETRACT ON T/O, 3 VGRN WITH GEAR HANDLE DOWN. SERVICED NOSE GEAR PER M/M 32-21-01-619-801, NOSE GEAR OPERATION CHECKS NORMAL. 2L72 4F RTA6WE 20040121000652004012100065NM 2004 1 21 USAASB03215 120031214A520010608211 DOOR SEAL BOEING737 7373B7 1384580NM FWD CARGO DOOR FAILED A USAAGA O2 MASK DEPLOYED UNSCHED LANDING O OTHER CRCRUISE 1 EA19518AU 23704 DURING CRUISE, EN ROUTE FROM IND-CLT AT FL290, A LOUD BANG WAS HEARD FROM THE FORWARD GALLEY AREA, FOLLOWED BY THE CABIN ALTITUDE CLIMBING UNCONTROLABLLY. CREW REPORTED THE OUTFLOW VALVE WAS IN THE FULL CLOSED POSITION. THE OXYGEN MASKS DEPLOYED AND BOTH TE PASSENGERS AND CREW DONNED THEIR MASKS. AN EMERGENCY DECLARED AS A/C DESCENDED TO 8,000 FT BEFORE CABIN ALTITUDE COULD BE BROUGHT UNDER CONTROL. FLT RETURNED TO FIELD AT IND AND LANDED WITHOUT FURTHER INCIDENT. MAINT FOUND FWD CARGO DOOR SEAL UNSEATED. REMOVED AND REPLACED THE FWD CARGO DOOR SEAL PER MM. LEAK CHECK GOOD. PERFORMED CABIN LEAK RATE CHECK PER MM. LEAK RATE WITHIN LIMITS. REMOVED AND REPLACED OXYGEN GENERATORS AND REPACKED MASKS. (M) 2L72 4F RTA16WE 20031209001482003120900148NM 2003 12 9 QXEA200301363 120031023A5510 FITTING DHAV DHC8 DHC8202 2809007NM ZONE 300 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 HORIZONTAL STABILIZER TO VERTICAL STABILIZER FORWARD ATTACH POINT LUG FITTINGS HAVE SCRATCH MARKS ON OUTBOARD FACES AT LEFT HAND AND RIGHT HAND POSITIONS. REPAIRED IAW DHC-8 RD 8-55-847. 2H72 4T RTA13NM 20031209002302003120900230EU 2003 12 9 MALA030481 120031028A61208210163 GOVERNOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE OVERSPEED FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15361PX 340B249 DURING FLIGHT 3319, RT PROP INDICATES 1240. RIGHT ENGINE PROP RPM 1240 W/ CONDITIONER LEVER MAX RIGHT AFTER +10. APPROX 10 MINUTES LATER DROPPED BELOW 1180. QRH ENGINE SHUTDOWN BELOW 1200 RPM ACCOMMPLISHED. T/M LOCKOUT DID NOT CHANGE. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RT PROP OVERSPEED GOVERNOR, P/N ON/OFF 8210-163, S/N ON 2162706 IAW SAAB MM CH 61 AND 72. PERFORMED ALL OPS CHECK GOOD AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20031210002092003121000209NM 2003 12 10 UPS03541382 120031010A33503025521 SOCKET BOEING757 75724APF 1384969NM CABIN DIRTY A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01473UP 28846 INSPECTION TYPE:ASV EXTERNAL EMERGENCY EXIT LIGHT UNDER THE FWD ENTRY DOOR IS INOP. CLEANED THE LAMPHOLDER SOCKET ON THE EXTERNAL EMERGENCY EXIT EGRESS LIGHT ASSY AS REQUIRED. OPS CHECKS GOOD IAW M/M 33-51-06-2. OK FOR SERVICE. 2L72 4F RTA2NM 20031014001942003101400194NM 2003 10 14 SWAA032103 120030922A7920BCREF2490 WARNING SYSTEM BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAULTY A SWAAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29332SW 23696 721339 IN FLT SHUTDOWN, AIR TURNBACK, DECLARED EMERGENCY, NR 2 ENG OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED NR 2 ENG OIL FILTER. NO DEFECTS FOUND. DEFERRED NR 2 ENG OIL FILTER WARN SYS PER MEL. LATER AT LAS, REMOVED AND REPLACED NR 2 ENG OIL FILTER AS PRECAUTIONARY. 2L72 4F4 FRTA16WE E2GL 20030919001002003091900100NM 2003 9 19 03FDEA01325 120030815A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 STRINGER HAS CORROSION, WHILE WORKING ON CARD NR N00150, FOUND CORROSION ON STRINGER 27R AT BS 1056. 2L73 4F RTA3WE 20040127001942004012700194NM 2004 1 27 ASAA0310211 120030325A531365458953 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 27L AT BS 908 CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER PER SRM. (M) 2L72 4F RTA16WE 20040128000212004012800021SO 2004 1 28 RAIA00312315 120031214A326016251 PROXIMITY SENSOR EMB 145 EMB145 3260210SO MLG DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03827HK STL- WINDSHIELD HEAT NR 2 FAIL, AIR GROUND FAIL, RUDDER NR 1 AND NR 2 FAIL. MAINTENANCE CLEANED CONNECTOR ON AIR GROUND PROXIMITY SENSOR. 2L72 4F RTT00011AT 20040130002092004013000209WP 2004 1 30 ABXA040007 120031203A5730 SKIN DOUG DC8 DC861 3021952WP LT WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 LEFT WING UPPER XRS 519 - 624 CORROSION AROUND FASTENER HEADS (24 EACH). REPAIRED AREA IAW REA D857-48493MR. 2L74 4F 4A25 20040203000402004020300040NM 2004 2 3 ASAA0310165 120030320A53206953063 ANGLE BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND MAIN CARGO DOOR ANGLE AT BS 480, LT BUTTOCK LINE 36 CRACKED. REMOVED AND REPLACED ANGLE IAW SRM. (M) 2L72 4F A16WE 20031218000692003121800069SO 2003 12 18 C2XA03SH478 120031202A531014522460015 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031219001532003121900153NM 2003 12 19 03FDEA02139 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09. 2L73 4F RTA22WE 20031222000462003122200046NM 2003 12 22 NACA20030126 120031209A2612182518003752 FIRE LOOP BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE OUT OF ADJUST A NACAO OTHER N FALSE WARNING CRCRUISE 1 AL03992AJ3 3 19428 649003 NR 3 ENGINE FIRE DETECTOR LIGHT ON IN FLIGHT. ADJUSTED NR 3 ENGINE FIRE LOOP AWAY FROM COWLING, LIGHT EXTINGUISHED. FIRE LOOP WAS REPLACED ON PREVIOUS LOG SHEET/FLIGHT. CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20031218001512003121800151NE 2003 12 18 DHL2003752006 220031129A7230 COMPRESSOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE NR 2 ENGINE STALLED A DHLACD ABORTED TAKEOFF RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO01752DH 22466 ENGINE NR 2 COMPRESSOR STALL WHEN ON POSITION RUNNING UP THE ENGINES AT 80 PERCENT, HIGH CROSSWIND COMPONENT. INSPECTED NR 2 ENGINE FAN, NO DEFECTS NOTED. ACCESS HATCH SECURED IAW M/M 71-00 PAGE 608. 2L73 4F4 F A3WE E2EA 20031224000242003122400024NM 2003 12 24 USAASB03203 120031121A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US 23992 BDL - MAINTENANCE REPORTED THE EMERGENCY ROW IDENTIFIER LIGHTS AT SEAT ROWS 10 AND 11, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY AT STATION 598. OPS TEST OF EMERGENCY LIGHTS GOOD. (M) 2L72 4F RTA16WE 20031224000332003122400033WP 2003 12 24 ASAA0380626 120031011A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS SEVERAL CORRODED INSERTS AND LARGE TORN AREA FROM FS 1155 TO 1250. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031229000422003122900042NM 2003 12 29 UPS03441658 120031214A3350 LAMP BOEING747 747SR46 1384816NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:N/A UPPER DECK CEILING RIGHT EMERGENCY LIGHT INOP. RELAMPED CEILING EMERGENCY LIGHT CHECKS GOOD. 2L74 4F RTA20WE 20040105000932004010500093WP 2004 1 5 DHL2003802548 120031125A57203645612U BRACKET DOUG DC8 DC873 302199CWP WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 NR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 21, 9 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040105001692004010500169CE 2004 1 5 AMWA96 120031216A534711443010653 SEAT TRACK BEECH 1900 1900D 1154162CE FUSELAGE DAMAGED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT AFT SEAT TRACK WAS FOUND TO BE DAMAGED. 2L72 4T RTA24CE 20040105000312004010500031NM 2004 1 5 033604201 120031226A32502318000002 CONTROL UNIT DORNERDO32 DO328300 NM NLG STEERING FAULTY A VTZAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27420FJ 3178 DURING TAXI THE CREW REPORTED AN UNCOMMANDED RIGHT STEERING INPUT ON THE NOSE WHEEL STEERING. THE NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040105001372004010500137NM 2004 1 5 SWAA032755 120031216A251065C27385 GLARE SHIELD BOEING737 737317 138447PNM COCKPIT MALFUNCTIONED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW29698SW 23176 SMOKE APPEARED IN FRONT OF CAPT'S INSTRUMENT PANEL FOR ABOUT 5 SECONDS. SMOKE AND ODOR DISSIPATED. COMPLIED WITH COCKPIT INSPECTION NO DEFECTS FOUND. REMOVED AND REPLACED GLARESHIELD ASSY, RADAR IND, FMC CDU, AND RADIO CONTROL PANELS PER MM. 2L72 4F RTA16WE 20040105001092004010500109WP 2004 1 5 DHL2003802535 120031120A53203758497U2 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 2.000, STA 1180.000 - STA 120.000, L-35R. REMOVED CRACKED FITTING FROM AFT CARGO COMPT (STA 1180.000-1200.000, L-35R) IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040311000312004031100031NM 2004 3 11 ASAA0310131 120030310A53206546812 FLOOR SUPPORT BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 944-1016, LEFT BUTTOCK LINE 6, LEFT BUTTOCK LINE 15 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20031125001632003112500163NM 2003 11 25 ASAA0310512 120030603A53156567140139 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-706, LEFT BUTTOCK LINE 25 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM AND EA. (M) 2L72 4F RTA16WE 20031203001302003120300130WP 2003 12 3 AMTA200301267 120030812A5320 WEB LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 C3 PIT WEB ABOVE STRINGER 29 IS CRACKED. REPAIRED WEB IAW SRM 53-23-00 AND 51-50-01, FIG 2. (M) 2L73 4F A23WE 20030923000362003092300036WP 2003 9 23 DHL2003604579 120030509A5720 INTERCOSTAL DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING T/E INTERCOSTAL WITH 2.000 CRACK IN IT AT STA. XRS.74.000. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 FIG.2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG.1. 2L74 4F RT4A25 20030925000052003092500005NM 2003 9 25 USAABB03132 120030813A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6, 9, 26 AND 33 WEAK. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20040130000312004013000031NM 2004 1 30 SWAA032824 120031228A335020131A BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20040202001382004020200138NM 2004 2 2 UPS04541743 120031231A5347BAC15202474 SEAT TRACK BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE: C, CORROSION ON SEAT TRACK AROUND FASTENER HOLE BS 544 LBL 45. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REPAIRED SEAT TRACK PER GOODRICH ER 04-1022. 2L72 4F RTA2NM 20040204001912004020400191NM 2004 2 4 03FDEA01880 120031105A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION FOUND ON FORWARD SIDE OF 970 FRAME AT STR 29 LT. OPEN 2L73 4F RTA3WE 20040210000762004021000076WP 2004 2 10 ASAA0380775 120031119A53135936053501 LONGERON DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CORROSION AROUND FASTENERS ON LONGERON 29L AT STATION 637. REPAIRED IAW EA. (M) 2L72 4F RTA6WE 20040213000122004021300012CE 2004 2 13 56696 120031202A521012951405925 LATCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA PAX DOOR BROKEN A AMWAO OTHER J WARNING INDICATION APAPPROACH 1 CE07126YV UE126 UPON ARRIVAL CREW HAD DOOR WARNING ANNUNCIATOR. IT WOULD NOT EXTUNGUISH. MAINT WAS CALLED AND FOUND LATCH CABLE BROKEN. CABIN DOOR INOPERATIVE CAMS ON AFT SIDE WILL NOT CLOSE. REMOVED AND REPLACED AFT DOOR LATCH CABLE. P/N 129-514059-25 2L72 4T3 TRTA24CE E2NE 20040213000082004021300008EU 2004 2 13 011271 120031223A6120 PANEL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE RT CTOT MALFUNCTIONED A UHLAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL17150CN 150 434 DRG49983 THE CREW ABORTED TAKEOFF WHEN THE CTOT ON THE RT SIDE ARMED AND THEN DISARMED. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20031212001572003121200157WP 2003 12 12 GTIA030857 120031015A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND DAMAGED LONGERON STATION FS 1271 L24L. REMOVED DAMAGED LONGERON AT L24L FS 1322-1271. FABRICATED NEW LONGERON. LOCATED AND DRILLED SPLICE. INSTALLED SPLICE AND LONGERON. (M) 2L72 4F A6WE 20030818000052003081800005 2003 8 18 HEEA088390 420030728A3434066104400 RECEIVER SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 FREQ LIGHT DOES NOT ILLUMINATE. IN SHOP REPAIR. 1G72 3U H1NE 20030819000182003081900018WP 2003 8 19 AALA20030654 120030611A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21208AA 49159 DURING OVERNIGHT MAINTENANCE, FORWARD RIGHT SERVICE DOOR EMRGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD RIGHT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030408000362003040800036EA 2003 4 8 SIMA200304103 120030209A3620 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A BA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21504AE 10044 HOU - FLT 3812 - CREW REPORTED A LEFT BLEED DUCT WARNING AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND RETURNED TO HOU WITH NO FURTHER INCIDENTS NOTED. BLEED SELECTED MESSAGE LATER WENT OUT. MAINTENANCE REMOVED AND REPLACED THE LEFT WING ANTI-ICE VALVE IAW CRJ MM. OP CHECK AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030410000972003041000097NM 2003 4 10 SWAA030669 120030323A2750285A12001 FSEU BOEING737 7377H4 1384404NM E/E BAY FAULTY A SWAAK NONE F FLT CONT AFFECTED NRNOT REPORTED 1 SW29416WN 32453 DURING FLAP EXTENSION AN ASYMMETRY DEVELOPED, LOWERED FLAPS WITH ALTERNATE SYSTEM & LANDED UNEVENTFULLY. REMOVED AND REPLACED FLAP/SLAT ELECT. UNIT, OPS CK'D GOOD PER MM. 2L72 4F RTA16WE 20030408000832003040800083WP 2003 4 8 03FDEA00392 120030405A5350 PIN DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE TAIL CONE LOOSE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25317FE 46835 TAILCONE LT SIDE MATING FLANGE UPPER ALIGNMENT PIN HOLE FOR THE PIN HAS EXCESSIVE PLAY. REMOVED FILLER AND PIN IAW SRM 51-31-01. FAB NEW FILLER IAW SRM 53-30-00 FIG 1, INSTALLED IAW SRM 51-31-01. 2L73 4F4 F A22WE E23EA 20030410000842003041000084NM 2003 4 10 SWAA030656 120030321A5310589358 WINDOW POST BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C3 CHECK, FOUND RT COCKPIT WINDOW C POST CRACKED. REPAIRED POST PER SRM. 2L72 4F RTA16WE 20040203003352004020300335EA 2004 2 3 MASA200300503 120031219A2700270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS OUT OF TOLERANCEA MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07772786805 6805 7278 ASH 6320 PHX-GJT, ABORTED T/O FOR SPOILER CONFIG WARNING MSG. MX REPLACED THE PCU. OP CHECKS GOOD. 2L72 4F RTA21EA 20040205000242004020500024NM 2004 2 5 EIA2003161 120031023A5740 FITTING BOEING747 747132 1384882NM WING SPAR CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 DURING WING REAR SPAR UPPER SPLICE FITTING INSPECTION, CRACKS WERE FOUND ON THE VERTICAL FLANGE OF THE SPLICE FITTING RT SIDE. REMOVED AND REPLACED WING REAR SPAR UPPER SPLICE FITTING PER EO 57-747-1011-90 REV A. 2L74 4F A20WE 20040206000392004020600039WP 2004 2 6 ASAA0380817 120031201A53109707970 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT FS 1257. REPLACED SHEAR TIE PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040204001542004020400154NM 2004 2 4 EIA2003143 120031020A5530 BEAM BOEING747 747212B 1384886NM VERTICAL STAB DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 VERTICAL STAB RT TRAILING EDGE BEAM FWD AND AFT WEBS DAMAGED, DO TO POWER PACK LOWER RUDDER INSTALLATION. INSTALLED FORWARD WEB DOUBLER AND 2 EA. FILLERS IAW MFG 747 SRM 51-30-02 AND ECRA 482-55-183-2 2L74 4F A20WE 20040212001192004021200119EU 2004 2 12 COE2003F00004 120031203A32118480180001 PIN FOKKERF27 F27MK600 4990706EU RROYCEDART DART532* EU ROTOL R4304 R1934304 EU MLG FAILED G COEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM02702FE 10350 1472514403 DRG5968 PILOT REPORTED, HAD TO RECYCLE LANDING GEAR C/B TO GET THE LANDING GEAR TO RETRACT (ALL GEAR). MAINTENANCE REPLACED PIN CONNECTING LANDING GEAR LOCK SOLENOID TO LOCKING PAWL. PERFORMED GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 T A817 E297 6 CP899 20040401000572004040100057WP 2004 4 1 2004F00087 120030119A2170 COALESCER BAG DOUG DC9 DC931 3022065WP AIR CON SYS CONTAMINATED A A4JAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO35935DS 48158 AFTER TURNING WEATHER RADAR ON, A STRONG ELECTRICAL ODOR FILLED THE COCKPIT. REMOVED AND REPLACED LEFT AND RIGHT PACK COALESCER BAGS IAW MM 21-20-2. OPERATIONAL CHECK GOOD. RAN PACKS NO ODOR NOTED. BOTH BAGS WERE SATURATED WITH MOISTURE, ODOR OF GLYCOL. REMOVED WEATHER RADAR INDICATOR, VISUALLY INSPECTED INDICATOR AND ASSOCIATED WIRING/CONNECTORS, NO APPARENT DAMAGE OR ODOR FOUND. REINSTALLED INDICATOR, OPERATIONAL CHECK GOOD IAW MM 34-41-0. (M) 2L72 4F A6WE 20040401000332004040100033WP 2004 4 1 ASAA0380409 120030421A53405936462 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND MID CARGO BAY LOWER DOOR JAMB FITTING IS CORRODED AT FS 636-644. REPLACED DAMAGED FITTING, SUPPORT PER SRM 51-10-2, 4, AND 5. (M) 2L72 4F A6WE 20040303000362004030300036EU 2004 3 3 ERAA092653 120031229A6420 BUSHING BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL TAIL ROTOR HEAD MISINSTALLED A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03152EH10760 214 S701 UNABLE TO ADJUST FOR PEDAL FORCE. TEFLON ON GRIP BUSHINGS FLAKING. COMPLY PREINSPECTION AND NOTED NO DEFECTS. DISASSEMBLED AS FAR AS NECESSARY FOR REPAIR. VISUALLY NOTED TEFLON FLAKING ON GRIP BUSHING. POSSIBLE CAUSE OF ABOVE DISCREPANCY. NO OTHER DISCREPANCIES FOUND. INSTALLED NEW GRIP BUSHINGS, AND SEALS, C/W SLIDING FRICTION FORCE TEST, AND BREAK AWAY FORCE TEST. REASSEMBLED WITH ORIGINAL HARDWARE, BLADES AND STATIC BALANCED. REPAIRED IAW REM 301, MM CHAPTER 33.34 AND 107 TT 10760.1 TSI 60.3. 1G72 3U3 U H3EU E4CE 20031211000122003121100012NM 2003 12 11 AWXA200301378 120031028A5320654583471 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK 2 EACH .75 INCH CRACKS WERE FOUND ON LOWER AFT SIDE OF TIE STRAP BS 328, RBL 45. MAINTENANCE CUT OUT DAMAGE ON TIE STRAP BS 310 TO BS 362, RBL 45; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1-4. 2L72 4F RTA16WE 20031211001802003121100180NM 2003 12 11 USAABB03200 120031027A3397W3634010422 WIRE BOEING757 7572B7 1384964NM CABIN PULLED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU 27123 CLT - THE AISLE EMERGENCY LIGHTS IN ROWS 25 THROUGH 33 REMAINED ILLUMINATED. MAINTENANCE FOUND WIRE W3634-0104-22 PULLED OUT FROM SM2. (M) 2L72 4F RTA2NM 20031211002002003121100200EU 2003 12 11 USAA030249 120031030A5347D5311278220201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT/SEAT TRACK CORRODED .750 BY .750 BY .056 DEEP, FRAME 20 RBL 28 CABIN FLOOR SUPPORT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. CORROSION LEVEL 2, TASK NR JA-220-53500-07. (M) 2L72 4F RTA28NM 20040520002312004052000231EU 2004 5 20 2004F00116 120030912A5321 FLOOR PANEL AIRBUS320 A320233 3930329EU AFT CARGO COMPT CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK FOUND EXFOLIATED CORROSION AT AFT CARGO COMPARTMENT FLOOR PANEL 151DF. FABRICATED AND INSTALLED FLOOR PANEL NR 151DF, AFT CARGO COMPARTMENT. (M) 2L72 4F RTA28NM 20040924000662004092400066CE 2004 9 24 2004F00360 120031227A3240 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A GUUAO OTHER O OTHER LDLANDING 1 SO1969547 UE189 FLT 9227 - NAS-FLL - AFTER LANDING, BRAKES ARE SPONGY AND LOSE PRESSURE WHILE TURNING AND STOPPING. BLED BRAKES. LEAK CHECK OK. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20060731000572006073100057WP 2006 7 31 IXXA060508S 120030122A5522 SKIN DOUG DC8 DC871F 302199DWP ZONE 300 BENT A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR UPPER SKIN IS BENT AT OUTBOARD HINGE CUTOUT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-8, 51-1-24, 51-1-21 AND DOUGLAS DRAWING J644400. 2L74 4F RT4A25 20060801001382006080100138WP 2006 8 1 IXXA060581S 120030912A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FRAME CRACKED AT STATION 1395 LONGERON 28 RIGHT. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, NAD DOUGLAS DRAWING 5616674. 2L74 4F RT4A25 20030819000772003081900077NM 2003 8 19 CALA0300392 120030715A5347 SEAT TRACK BOEING777 777224 1385225NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778009 29479 INSPECTION FOUND SEAT TRACK CROWN CORRODED AT BS 1513-1530, RBL 108. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 4, FIGURE 202. 2L72 4F RTT00001SE 20030328001062003032800106EU 2003 3 28 DHL2003362003 120030113A2612 CONNECTOR AIRBUS300 A300B4203 3930306EU NR2 FIRE LOOP LOOSE A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01362DH 84 ENGINE NR 2 LOOP A-LIGHT ILLUMINATED INTERMITTENTLY ON GROUND AFTER LANDING. CLEANED ALL A-LOOP CONNECTOR PLUGS ON FAN, CORE, AND PYLON ON NR 2 ENGINE. FOUND LOOP CLAMP ON LOOP UNFASTENED. REFASTEN CLAMP. OPS CHECKED GOOD IAW 26-12-00 PAGE 6. 2L72 4F RTA35EU 20030820002232003082000223NM 2003 8 20 USAABB03120 120030725A33503017681M SOCKET BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 SNN - FOUND EXTERIOR EMERGENCY LIGHT AT 2L DOOR INOPERATIVE. MAINTENANCE ADJUSTED THE LIGHT SOCKET ASSEMBLY. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA1NM 20030822000542003082200054NM 2003 8 22 03FDEA01246 120030803A5712ARB2850501 RIB DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING- SLAT TRACK 2316 INBOARD RIB FOUND CRACK 2C LENGTH OF CRACK APPROX 750 22. LT WING - SLAT TRACK NR 16 INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20030407000872003040700087SO 2003 4 7 SIMA200306407 120030227A532014521725615 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED ALL CORROSION BY BLENDING. FABRICATED A DOUBLER, REPAIR DONE IAW AEAI ETN NR EB-53-0321 AND STANDARD EMB SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030410000902003041000090NM 2003 4 10 SWAA030662 120030322A575465C26602223 SLAT BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT BOTH ENDS. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20030424001902003042400190WP 2003 4 24 MWEA030149 120030328A572059512614 NUT PLATE DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 CORROSION AROUND NUT PLATE AT STATION 1015 INSIDE RIGHT FLAP TRACK STRUCTURE SUPPORT/FAIRING SUPPORT. DRILLED UP AND INSTALLED SUPPORT. 2L72 4F A6WE 20030425000612003042500061SO 2003 4 25 SWIA200311858 120030330A3230 LANDING GEAR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LEFT MALFUNCTIONED A SWIAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM07196SW 120151 LEFT MAIN LANDING GEAR INDICATION REMAINS RED ON RETRACTION AND SEEMS TO HANG. MAINTENANCE SWUNG GEAR APPROXIMATELY 20 TIMES. NO DEFECTS NOTED. PERFORMED MAIN AND NOSE LANDING GEAR EXTENSION/RETRACTION HYDRAULIC CIRCUIT TEST AS PER 32-32-00. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030502002152003050200215EU 2003 5 2 AWXA200300398 120030405A5320D5311281820401 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT BEAM Y-254, AFT OF FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT BEAM Y-254 FROM FR 12 TO FR 21; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 28-33, 39, & 41, FIG 12, 13, & 18. 2L72 4F RTA28NM 20030505001872003050500187NM 2003 5 5 03FDEA00218 120030303A5510ALC8104 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 16L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030506002382003050600238WP 2003 5 6 ASAA0380267 120030317A534759366634521 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OAK - DURING 15K CHECK, FOUND AFT CARGO BAY LEFT TIEDOWN TRACK IS CORRODED AROUND SCREW HOLES FROM FS 1003 TO 1322. REPLACED TIEDOWN TRACK PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20030506001772003050600177WP 2003 5 6 ASAA0380245 120030307A52605910382 STEP DOUG DC9 DC982 3022082WP AIRSTAIR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, AFT ENTRY STAIRS HAVE CRACK ON LOWER STEP. BLENDED OUT CRACKS PER SRM. (M) 2L72 4F A6WE 20030506001292003050600129EU 2003 5 6 AWXA200300423 120030329A5315D5347209800600 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-919 AT FORWARD SIDE OF FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE WITHIN ALLOWABLE LIMITS PER AWA ER 26-5341-03105-SS1; TREATED, PRIMED AND TOP COATED BLENDED AREA IAW A320 SRM 51-21-11 PG 2-7. 2L72 4F RTA28NM 20030508001002003050800100EA 2003 5 8 QXEA0300536 120030424A5310 STRIKER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 PDX-FORWARD LOWER CORNER OF PASSENGER DOOR SEAL STRIKER ON FUSELAGE HAS A GOUGE AND CRACK IN METAL. REPAIRED IAW CRJ-700 SRM 51-42-06. 2L72 4F RTA21EA 20030513001032003051300103SO 2003 5 13 C2XA03TY051 120030504A532014525422 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 DURING A SCHEDULED INSPECTION THE LEFT HAND OUTBOARD AFT FLOOR SUPPORT FRAME UNDER THE LAVATORY SINK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LAVATORY FLOOR FRAME SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20031208000612003120800061EU 2003 12 8 03FDEA01798 120031024A5720A5381131920195 ANGLE AIRBUS310 A310203 3930313EU ZONE 100 MISMANUFACTURED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25442FE 353 RIGHT WING FRAME NR 40 HAS NUMEROUS HOLES DRILLED THRU FUSELAGE SKIN ONLY. THAT IS OUT OF ROUND/ELONGATED. ACCOMPLISHED WORK CARD EA6-5310-7-5003 02 PT4 AND EA6-5310-73419A AT CWF BY DRILLING FASTENER HOLES TO CORRECT SIZE AND INSTALLING PICKUP ANGLE TO ENGINEERS FASTENER INSTALLATION SHEET. 2L72 4F RTA35EU 20031208000952003120800095NM 2003 12 8 QXEA200301327 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - LEFT OUTBOARD TRACK NR 1 SEAT ATTACH AREA CORROSION UNDER INBOARD AND OUTBOARD LUGS, APPROXIMATELY X424.00. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20031209002632003120900263NM 2003 12 9 AWXA200301364 120031022A531565498835 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER AFT LEG AT BS 947 FROM RBL 5 TO LBL 53. MAINTENANCE CUT OUT DAMAGED FLOORBEAM UPPER AFT LEG AT BS 947 FROM RBL 5 TO LBL 53; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-09 PG 1-5 FIG 7. 2L72 4F RTA16WE 20030923000912003092300091WP 2003 9 23 DHL2003604701 120030621A5313 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD ACCY COMPT FRAME CRACKED 2.000, STA 55.000, L-24L. TRIMMED OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW FRAME SEGMENT (7075-T6 AL0.071) AND SPLICE ANGLE (02 EA) (7075-T6 AL0.071) IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. PERFORMED HEAT TREATMENT TO FRAME SEGMENT AND NEW SPLICE ANGLES IAW SRM 51-1-1, DPS 7.00-1. CLEANED, TREATED AND PRIMED FRAME SEGMENT AND NEW SPLICE ANGLES IAW SRM 51-1-8B. INSTALLED FRAME SEGMENT AND NEW SPLICE ANGLES WITH NEW FASTENERS IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040129000102004012900010EA 2004 1 29 COMA0360581 120031230A5524600230459 HINGE FITTING CNDAIRCL600 CL6002B19 1900309EA RT ELEVATOR CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO01956CA19994 7105 RIGHT ELEVATOR NR 1 HINGE POINT ON THE HORIZONTAL IS CHAFED. REPAIRED BY BLENDING CHAFED AREA SMOOTH, PERFORMED LIQUID PENETRANT INSPECTION, ROTO/FLAP PEEN REWORKED AREA IAW CNDAIR SRM 51-24-11, AND TREATED AREA WITH ALODINE, ALL WORK PERFORMED IAW WVAC EO 601R-55-4508. 2L72 4F RTA21EA 20040203000162004020300016WP 2004 2 3 ASAA0380575 120030902A531359360531 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 OAK - DURING C-CHECK, FOUND FASTENERS CORRODED ON LONGERON 30 FROM FS 598 TO 788. REPLACED LONGERON IAW EA 5310-02244. (M) 2L72 4F A6WE 20040211000412004021100041EA 2004 2 11 ASOA03695 120031230A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 DURING GROUND INSPECTION IN SHV, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040213000102004021300010 2004 2 13 57171 420031218A3422 GYRO BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA COCKPIT INOPERATIVE A AMWAA UNSCHED LANDING O OTHER CLCLIMB 1 CE07218YV UE218 SHORTLY AFTER DEPARTURE FROM PIT CREW NOTICED CAPT'S GYROSCOPIC DIRECTIONAL COMPASS SYSTEM WASN'T WORKING CORRECTLY. SO DECEIDED TO RETURN TO PIT. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. T/S REPAIRED PINS 5 AND 7 OF CONNECTOR J203 AT NR 1 FLUX DETECTOR. OPS CK GOOD. P/N FREESTOCK 2L72 4T3 TRTA24CE E4EA 20031211000062003121100006NM 2003 12 11 CALA0300623 120031104A3230273A28033 FITTING BOEING737 737724 13844BYNM LT MLG BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713720 28939 WHEN GEAR HANDLE WAS RAISED AFTER TAKEOFF FROM MSY THE LT MLG DID NOT RETRACT. THE FORWARD PANEL RED AND GREEN LT GEAR LIGHTS WERE ILLUMINATED. THE OVERHEAD PANEL SHOWED GREEN LT GEAR LIGHT ON. THE GEAR WAS CYCLED WITH THE SAME RESULT. GEAR DOWN INDICATIONS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO MSY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG FRANGIBLE FITTING BROKEN. NO OTHER DAMAGE WAS NOTED. THE FRANGIBLE FITTING AND NUT WERE REMOVED AND REPLACED. 2L72 4F RTA16WE 20040304001582004030400158NM 2004 3 4 ASAA0340356 120031210A3397 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01784AS 28199 PDX - DURING LINE CHECK, FOUND FLOOR TRACK IGHTING INOPERATIVE AT ROW 13-15. RECONNECTED WIRES, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040316000422004031600042NM 2004 3 16 ASAA0340334 120031012A33978100022608 WIRE BOEING737 737490 1384715NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01796AS 28891 PDX - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. RECONNECTED WIRE AND OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040412000032004041200003WP 2004 4 12 ASAA0380731 120031111A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS PUNCTURED AT FS 1118-1160. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040614001682004061400168CE 2004 6 14 GUU2004F00007 120031124A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178153317255 UE137 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040713001652004071300165NM 2004 7 13 MEX2003557 120031220A2100 WARNING HORN BOEING737 737* NM COCKPIT ACTIVATED A ASMFGA O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23XAAAM 33783 FLT 683 - ORD-MEX - AIRCRAFT AIR TURNED BACK, DUE TO LOSS OF PRESSURIZATION. AT 13,000 FEET SOUND THE ALARM WITHOUT WARNING VISUAL INDICATION. AT 14,000 FEET THE 'OVERHEAD' LIGHT CAME ON AND THE OXYGEN MASKS WERE DEPLOYED IN THE PASSENGER CABIN. ONCE IN THE PLATFORM A BITE TO BOTH CABIN PRESSURE CONTROLLERS WAS PERFORMED AND NO FAIL WAS CONFIRMED. OXYGEN GENERATORS WERE REPLACED WHERE NEED IT AND A HARD LANDING INSPECTON WAS PERFORMED IAW MM 35-22-11 AND 05-51-01 RESPECTVELY, NO DEFECTS WERE DETECTED. (M) 2L72 4F RTA16WE 20040902001922004090200192NE 2004 9 2 I5HA0324002 220031024A8530 CYLINDER CVAC 240 240* 2422601WP PWA R2800 R2800* 52026NE NR 16 FAILED A I5HAO OTHER RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CRCRUISE 1 GL2399380 249 P33621 EN ROUTE, PILOT NOTICED A DECREASE IN OIL QTY ON RT ENG. CONTINUED TO PIT. ELECTED TO KEEP RT ENG RUNNING. OIL QTY CONTINUED TO DECREASE. PILOT NOTICED MINOR TORQUE FLUCTUATION JUST PRIOR TO TOUCHDOWN. UPON TOUCHDOWN, NOTIFIED THAT THE RT ENG ON FIRE. E-HANDLED RT ENG & TAXIED TO CARGO APRON. PRELIMINARY INSP REVEALED A HOLE APPROX .075 INCH IN DIAMETER IN NR 16 CYLINDER. ENG BAY COVERED WITH OIL. TOP T/E OF RT FLAP BENEATH AUGMENTER TUBE HAD BURN DAMAGE. AUGMENTER FIRE CAUSED BY EXCESSIVE OIL ACCUMULATION IN BEAVER TAIL AREA DUE TO FAILURE OF NR 16 CYLINDER. FURTHER INSP REVEALED A CRACKED CONNECTING ROD ON NR 16 CYLINDER. ENG R & R. A/C WAS RETURNED TO SERVICE. (M) 2L72 4R4 R A793 5E8 20030514000912003051400091NM 2003 5 14 SWAA030992 120030504A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727D + 19 & BS 794, LT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20030515000122003051500012EA 2003 5 15 SWIA200311935 120030504A7830 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER DIRTY A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07943SW 7762 LEFT THRUST REVERSER DID NOT DEPLOY ON LANDING. CLEANED SCREWS, ACTUATOR AND CONNECTORS. PERFORMED OPERATIONAL CHECK ON LEFT THRUST REVERSER IAW MM 78-30-00. OPS CHECK GOOD AT THIS TIME. COULD NOT DUPLICATE ON GROUND. 2L72 4F RTA21EA 20030605001452003060500145EA 2003 6 5 SWIA200311971 120030509A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07926SW 7687 ''FLAPS FAIL'' MESSAGE DURING CRUISE (16,000' AT 320 KTS). HIGH SPEED CLACKER REMAINED ON UNTIL AIR SPEED WAS BELOW 250 KTS. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. PERFORMED RIGGING AND OPS CHECKS OF FLAP SYSTEM. NO DEFECTS NOTED AT ANY TIME. 2L72 4F RTA21EA 20030609000432003060900043NM 2003 6 9 C1HA200396008 120030520A5347 SEAT TRACK BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 PITTING CORROSION AND GOUGING ON NR 1 SEAT TRACK AT LBL 44 BETWEEN BS 380 & 480. 2L73 4F RTA3WE 20030609000322003060900032NM 2003 6 9 XNOA01119 120030520A3230 MECHANISM BOEING727 727227 1384078NM DOOR RELEASE STUCK A XN0AO OTHER J WARNING INDICATION CLCLIMB 1 GL2376753 21249 AFTER GEAR ROTATION MDT-WITH GEAR HANDLE PLACED TO OFF, RED DOOR LIGHT ILLUMINATED WITH AMBER. R-GEAR DOOR LIGHT ON FE'S PANEL. CYCLED GEAR PER ENA ABNORMAL CHECKLIST. BOTH LIGHTS EXTINGUISHED. FOUND MANUAL DOOR RELEASE QUADRANT & DOOR LOCK RELEASE STICKING TO OPEN POSITION WHEN GROUND RELEASE HANDLE STOWED. LUBE QUADRANTS & LOCK RELEASE. OPS CHECK GOOD. REF MM CH 32-12. 2L73 4F A3WE 20030609001442003060900144SO 2003 6 9 SWIA200312001 120030521A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07213SW 120277 EMERGENCY OVERHEAD LIGHT AT MAIN CABIN DOOR IS INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. 2L72 4T RTA31SO 20030520001222003052000122NM 2003 5 20 USAABB03064 120030427A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU 22198 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 6, 13, 18, 23, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030609001372003060900137NM 2003 6 9 AWXA200300582 120030504A5320BAC15172226 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 7. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 7; FABRICATED A NEW SECTION OF FLOOR SUPPORT STRINGER, AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030617003242003061700324NM 2003 6 17 SWAA031275 120030606A52406545871 DOOR FRAME BOEING737 7373H4 1384600NM SERVICE DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR CRACKED AT AFT LOWER CORNER OF UPPER HINGE CUTOUT. REPAIRED DOOR FRAME PER SRM. 2L72 4F RTA16WE 20030521000112003052100011WP 2003 5 21 DHL2003801015 120030503A57205769584501N DOOR DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LEFT WING OUTBOARD SLOT OUTBOARD DOOR CRACKED. REMOVED AND REPLACED OUTBOARD SLOT OUTBOARD DOOR AND TIGHTENED SRCEW OF LT WING IAW SRM 51-3-1 PG 2A. FOR OPS CHECK SEE N/R 0075. 2L74 4F RT4A25 20030521001732003052100173 2003 5 21 MWEA030200 420030505A34254055900906 SYMBOL GENERATOR DOUG DC9 DC982 3022082WP COCKPIT INOPERATIVE A MWEAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL31809ME 48071 FIRST OFFICER'S PRIMARY FLIGHT DISPLAY AND NAVIGATION DISPLAY UNIT WENT OUT. REMOVED AND REPLACED NR 2 SYMBOL GENERATOR. 2L72 4F A6WE 20030522000062003052200006 2003 5 22 372PA0029 420030511A3425 INDICATOR BOEING737 737306 13844BGNM FAILED A PIDAO OTHER O OTHER TOTAKEOFF 1 SO05372PA 23546 FLIGHT DIRECTORS BLANK ON TAKEOFF. TESTED ALL SYSTEMS PER MM 34-31-02. NO DEFECTS NOTED. 2L72 4F RTA16NE 20030521001212003052100121NM 2003 5 21 DHL2003781002 120030514A3350 LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01768AT 21996 EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE OVER MAIN ENTRY. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW B727 M/M 33-50-101. OPS CHECKED GOOD. 2L73 4F A3WE 20030618000672003061800067NM 2003 6 18 SWAA031308 120030611A2760V3L2228 SWITCH BOEING737 7372T4 1384492NM COCKPIT FAULTY A SWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW29702ML 22054 ABORTED TAKEOFF, TAKEOFF WARNING HORN ACTIVATED. REMOVED AND REPLACED SPEED BRAKE TAKEOFF WARNING SWITCH PER MM. 2L72 4F A16WE 20030523000882003052300088NM 2003 5 23 QXEA0300548 120030507A5210 HANDLE BOMBDRDHC8 DHC8401 1390041NM ZONE 800 LACK OF LUBE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09402QX 4032 SEA-ON FLIGHT NUMBER 2433, FLIGHT ATTENDANT REPORTS HIGH FORCE REQUIRED TO OPEN AFT PASSENGER DOOR. LUBED DOOR TRACKS AND HANDLE. DOOR OPERATES NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030522001112003052200111EU 2003 5 22 AWXA200300551 120030427A5315D5311141420000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM Y179 AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14 FIG 202, PG 211-212. 2L72 4F RTA28NM 20030527001292003052700129WP 2003 5 27 MEX2003156 120030504A215039271411 VALVE DOUG DC9 DC9* WP PWA JT8 JT8D NE LT A/C PACK FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23501AM6463 1507 49188 AIRCRAFT AIR TURNBACK, DURING CLIMB AT 8,000 FT THE (TAIL COP TEMP HI) COMES ON. IT WAS VERIFIED BY LEAKS AND THE ENGINE EXTINGUISHER WAS CHECKED ON HIGH TEMPERATURE DECAL. NO LEAKS WERE DETECTED. THE LT AIR CONDITIONING PACK WAS DEFERRED BY MEL. THE PRESSURE REGULATOR VALVE WAS REPLACED IAW MM. 2L72 4F4 F A6WE E2EA 20030623000282003062300028NM 2003 6 23 USAA030083 120030505A5330 BEAR STRAP BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50022 23514 FOUND BEAR STRAP CRACKED .1875 INCH, MED BEAR STRAP BS 304 UPPER AND LOEWR HINGE CUTOUT. INSTALLED DOUBLERS PER EA 76233. (M) 2L72 4F RTA16WE 20030620000202003062000020SW 2003 6 20 HEEA086942 120030603A3212206050247132 COVER BELL 407 407 1182206SW FLOAT MISSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 EMERGENCY FLOAT COVER MISSING AFT FLAP. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030624000602003062400060NM 2003 6 24 CALA0300303 120030610A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT STRAP CORRODED AT STA 727E, LBL 21. THE FLOOR SUPPORT STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030707000472003070700047WP 2003 7 7 AALA20030636 120030604A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21435AA 49453 DURING OVERNIGHT MAINTNANCE, EMERGENCY EXIT LIGHTS 3-19 AND EXIT DOOR INOPERATIVE. REPLACED TWO EMERGENCY EXIT LIGHT BATTERIES. SYTSEM GORND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030709000012003070900001WP 2003 7 9 GTIA030422 120030513A5312 PRESSURE PANEL DOUG DC9 DC981 3022081WP NLG WW CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 NOSE WHEEL WELL STATION 38 RBL 11, BULKHEAD SUPPORT WEB IS CRACKED. REMOVED CRACKED WEB. LOCATED AND DRILLED ON NEW WEB. INSTALLED WEB. (M) 2L72 4F A6WE 20030711000562003071100056NE 2003 7 11 MALA030319 220030621A7220CT75A2 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT MAKING METAL A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL1598XJ 340A098 DURING FLIGHT 3254, LT CHIP DETECTOR LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REPLACED LT ENGINE IAW JC 7100-301 PN ON/OFF CT7-5A2 SN/OFF GE-E367320 SN/ON GE-E367273 SEE 409 NR 167742 AND OWRK PACKAGE DATED 6/22/03 FOR ALL INFO. 2L72 4T4 TRTA52EU E8NE6 20030709000712003070900071CE 2003 7 9 GLBA2003073 120030602A3150 CONNECTOR BEECH 1900 1900D 1154162CE MASTER CAUTION LOOSE A GLBAO OTHER N FALSE WARNING CLCLIMB 1 NM03179GL UE179 MASTER CAUTION ANNUNCIATORS FLASHERS REPEATLY WITH NO MAP ASSOCIATION. RECONNECTED LOOSE CONNECTION AT PCBA318. 2L72 4T RTA24CE 20030714000242003071400024NM 2003 7 14 SWAA031396 120030622A3350BR2013 LIGHT BOEING737 7377H4 1384404NM FWD CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29744SW 29490 DURING SCHEDULED C3 CHECK, FOUND EEPLS SECTION CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS SECTION AT ROW NR 1 PER MM. 2L72 4F RTA16WE 20030716000592003071600059WP 2003 7 16 GTIA030466 120030505A5246 DOOR DOUG DC9 DC982 3022082WP FUEL SERVICE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 RT WING LEADING EDGE STATION XRS 240 REFUELING ACCESS DOOR CRACKED AND WORN ON INTERIOR. REMOVED REFUELING ACCESS DOOR. INSTALLED NEW FUEL DOOR. (M) 2L72 4F A6WE 20030716000812003071600081EA 2003 7 16 A6WA200340097 120030609A5753 VANE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 LT OUTBOARD FLAP HAS A DENT ON THE INBOARD SIDE OF THE FLAP VANE. REMOVED AND REPLACED DAMAGED LEFT OUTBOARD FLAP VANE P/N 601R14571-7 IAW 200 SRM 51-42-11, 51-23-00, 51-25-16, 51-42-21, AND WVAC EO 601R-57-4088. (M) 2L72 4F RTA21EA 20030203001972003020300197NM 2003 2 3 A6WA200330001 120030113A3260870004 PSEU DORNERDO32 DO328100 2996000NM E/E BAY FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31328MX 3071 IN FLIGHT YELLOW PROXIMITY SYSTEM FAIL, HYD QUANTITY FAIL ON EICAS SYSTEM PAGE, HYD PROXY SYSTEM FAIL, BYPASS FAIL, LOCK FAIL, LEV FAIL, AUX ATY FAIL AND NWS INOPERATIVE. REMOVED AND REPLACED PSEU. (M) 2H72 4T RTA45NM 20030205001402003020500140NM 2003 2 5 CALA0300005 120030106A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914335 23573 INSPECTION FOUND AN 8 INCH CRACK IN LT MAIN WHEEL WELL PRESSURE DECK WEB AT STA 664-675. THE AREA WAS REPAIRED IAW SRM 53-60-51. 2L72 4F RTA16WE 20030207001232003020700123NM 2003 2 7 03FDEA00099 120030203A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION ON SHEAR TIE AT BS 1166, LBL 2, WL 152, AFT CARGO BAY. 2L73 4F RTA3WE 20030214000612003021400061WP 2003 2 14 ASAA0380043 120030105A532199366007 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL HAS DAMAGED EDGE. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030219000622003021900062NM 2003 2 19 RYN2003F00005 120030109A5343 FITTING BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE LT & RT MLG CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077642U 19915 DURING B CHECK, LT AND RT MAIN GEAR BEAM FITTING SAFETY BOLT LUGS FOUND CRACKED. 2L73 4F4 F A3WE E2EA 20030219001472003021900147NM 2003 2 19 USAA030012 120030116A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU49188 23228 PIT - FOUND SKIN CORRODED 2 INCHES BY 4 INCHES, BELOW CABIN FLOOR STATION 1016 AT BL 0 AFT PRESSURE BULKHEAD, CORROSION LEVEL 2, TASK NR C53-107-02. REMOVED CORRODED SECTION, INSTALLED DOUBLERS AND SPLICE PER SRM 53-80-08 AND 51-40-02, EA 75070. (M) 2L72 4F RTA16WE 20030219001702003021900170WP 2003 2 19 MWEA030064 120030217A5313591143333 LONGERON DOUG DC9 DC981 3022081WP STA 1341 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LONGERON 11 AND IT'S SHOVEL CLIP IS DAMAGED RIGHT OF AFT PRESSURE BULKHEAD STATION 1341. -- REMOVED DAMAGED SECTION, LOCATED AND DRILLED AND INSTALLED NEW LONGERON AND NEW SHOVEL CLIP. 2L72 4F A6WE 20030116002462003011600246NM 2003 1 16 ZW0A0300503 120030109A3350 SOCKET DOUG MD80 MD83 3023681NM CABIN LOOSE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13951TW 53470 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW 19, 21, AND 29. SECURED THE LIGHT SOCKET AT ROW 29, AND REPLACED THE LIGHT MODULE AT ROW 19 AND 21. 2L72 4F RT 20030224001222003022400122EA 2003 2 24 COMA0360114 120030221A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA 3B DEFECTIVE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01937CA8731 1 7044 FLIGHT 5797 GEAR DISAGREE WARNING DURING EXTENSION.REPLACED THE 3B HYDRAULIC PUMP. 2L72 4F RTA21EA 20030304000372003030400037SW 2003 3 4 HEEA084571 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T11879 33112 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES DUE TO EROSION. 1G72 4U H4SW 20030307001592003030700159EA 2003 3 7 03047640 120030216A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27640BR 7340 EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED AFT EMERGENCY EXIT LAMP. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2L72 4F4 FRTA21EA E15NE 20030310000132003031000013 2003 3 10 HEEA084922 420030227A34571624811 ANTENNA BELL 412 412 1182202SW GPS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 GPS LOSES RAIM IN FLIGHT. SCRAPPED ANTENNA. 1G72 4U H4SW 20030311001112003031100111NM 2003 3 11 0300435512 120030204A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01512US 23200 DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED PER EA 55-193441. 2L72 4F RTA2NM 20030313000222003031300022SO 2003 3 13 C2XA03BT036 120030311A33501317 LIGHT EMB 145 EMB145 3260210SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2716961 145103 BTV---CO2943, DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND RIGHTHAND OVERWING EMERGENCY LIGHT TO BE INOPERATIVE.....REMOVED AND REPLACED RIGHTHAND OVERWING EMERGENCY LIGHT IAW EMB145 AMM #33-50-00. OPS.CHECKED GOOD. 2L72 4F RTT00011AT 20030313002342003031300234NM 2003 3 13 QXEA0300210 120030115A7110 FLANGE BOMBDRDHC8 DHC8401 1390041NM LT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 CKB- FLANGE IS CRACKED ON LEFT HAND LOWER COWL. REPAIRED IAW DHC-8 Q400 RD 8/4-71-016. 2H72 4T RTA13NM 20030314000692003031400069NM 2003 3 14 CALA0300050 120030216A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND H-STRAP CORRODED AT STA 1006, BL 0. THE H-STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030327000892003032700089SO 2003 3 27 C2XA03BT010 120030117A323023092900001 UPLOCK SWITCH EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2714925 145004 SYR---CO2576, CREW REPORTED, LANDING GEAR LEVER DISAGREEMENT AFTER TAKEOFF. LEFT MAIN GEAR WOULD NOT RETRACT. AIRCRAFT AIR RETURNED TO SYR AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDING GEAR UPLOCK BOX IAW 32-33-10. OPS CHECKED, RETRACTION TESTED, AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030314001712003031400171NM 2003 3 14 USAABB03030 120030304A335020131A BATTERY PACK BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE L3DOOR DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 FOUND EVACUATION LIGHT AT L3 DOOR, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. 2L72 4F4 FRTA2NM A12EU 20030314002012003031400201NM 2003 3 14 0300276306 120030220A3397 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK FOUND LEFT (B) ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED FLOOR EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030318001062003031800106EA 2003 3 18 ASOA03031 120030125A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A ASOAO OTHER O OTHER TXTAXI/GRND HDL 1 SO11848AS 7339 AFTER LANDING IN ATL AND DURING DEPLANING OF PASSENGERS AT THE GATE, THE CAPTAINS LEFT FRONT WINDSHIELD SHATTERED. THE WINDSHIELD HEAT HAD ALREADY BEEN TURNED OFF WHEN IT OCCURRED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS LEFT FRONT WINDSHIELD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030320000552003032000055NM 2003 3 20 USAASB03025 120030212A2910 MODULE BOEING737 7373B7 1384580NM B HYD SYS FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19374US 22953 PIT - FLT 553 - EN ROUTE FROM CLT TO CLE, DURING CRUISE, THE 'B' HYDRAULIC SYSTEM FLIGHT CONTROL LOW PRESSURE LIGHT ILLUMINATED. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE 'B' HYDRAULIC SYSTEM FLIGHT CONTROL MODULE PACKAGE PER MM 27-09-21. OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030320001392003032000139EU 2003 3 20 2003UALA00130 120030129A5311 FRAME AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29412UA 465 DAMAGED FRAME SECTIONS AT FRAME 60 ON STRINGER 40 LT & STRINGER 41 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAME. 2L72 4F4 FRTA28NM E40NE 20030325000952003032500095EU 2003 3 25 AWXA200300257 120030224A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 242 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW 099 DURING C-02 CHECK THE RT OVER WING EMERGENCY EXIT LIGHT AND RT OVER WING EXTERIOR EXIT LIGHT WERE FLICKERING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE RT EMERGENCY EXIT LIGHT BATTERY PACK IAW T/C R1C33301, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030326000312003032600031SO 2003 3 26 AUS20030130 120030108A3230 ROD END PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL MLG FAULTY W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) NOSE LANDING GEAR ACTUATOR DRAG LINK RODEND FAULTY. BUMPER STOP OUT OF ADJUSTMENT. 1L72 3O3 O A20SO E14EA 5 CP33EA 20040329000292004032900029EU 2004 3 29 USAASA03137 120031213A335032145510 PSU AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19183UW 1539 PHL - THE RIGHT MID CABIN EMERGENCY POWER SUPPLY UNIT FAULTS DURING TEST OF EMERGENCY LIGHT SYSTEM. MAINTENANCE REPLACED THE LEFT AND RIGHT EMERGENCY POWER SUPPLY UNITS. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030716000122003071600012NE 2003 7 16 2003F00407 220030627A7230 BLADE AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE COMPRESSOR BENT A RJEFEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO23464TA 1353 DURING CLIMB, TWO COMPRESSOR STALLS AND LOSS OF POWER ON ENGINE NR 1 WERE EXPERIENCED. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT WAS RETURNED TO SAL STATION. ON GROUND TECHNICIANS PERFORMED HPC BOROSCOPE INSPECTION PER AMM 72-00-00. THE 6TH WAS FOUND WITH BENT BLADES. THE ENGINE WAS REPLACED AND TESTED AS PER AMM 71-00-20. ALL TEST RESULTS WERE NORMAL AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F4 FRTA28NM E40NE 20030716001162003071600116NE 2003 7 16 HEEA088046 120030704A6540B538A3 CHIP DETECTOR SKRSKYS76 S76A 8143006NE GEARBOX BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 ELECTRICAL PINS BROKEN. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20030424000472003042400047NM 2003 4 24 QXEA0300322 120030227A5410 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CRACK IN SUPPORT BRACKET UPPER END OF RIGHT HAND COWL, ABOVE BYPASS DOOR INTAKE. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20040226000262004022600026NM 2004 2 26 ASAA0240163 120030322A5320654790U9 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 852. REPAIRED IAW SRM. M) 2L72 4F RTA16WE 20040301000422004030100042EA 2004 3 1 AJC2004F00000 120030923A3260840534 SQUAT SWITCH CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE RT MLG DEFECTIVE E AJCAO OTHER N FALSE WARNING CLCLIMB 1 EA2564YP 5077 AC DEPARTED, ENROUTE. DURING CLIMB OUT THE CREW ATTEMPTED TO RETRACT THE LANDING GEAR. THEY FOUND THAT ALL OF THE GEAR REMAINED IN THE DOWN AND LOCKED POSITION. AFTER CONSULTING THE ABNORMAL PROCEDURES MANUAL THE CREW ELECTED TO DIVERT TO HOME BASE. LANDING WAS UNEVENTFUL. CREW DID NOT DECLARE EMERGENCY. UPON INVESTIGATION IT WAS DETERMINED THAT NR 2 RT MLG WEIGHT ON WHEELS PROXIMITY SWITCH HAD FAILED. FAULTY SWITCH WAS REMOVED AND REPLACED. SATISFACTORY FUNCTIONAL AND OPERATIONAL CHECKS OF LANDING GEAR SYS WAS ACCOMPLISHED. NO FURTHER DEFECTS NOTED, AC RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030828000242003082800024NE 2003 8 28 00096 220030602A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT X ENGINE FLAMEOUT CLCLIMB 1 SW05324TW 24D324 251718 PILOT REPORTED LT ENGINE FLAMED-OUT WHILE CLIMBING FROM FL42.5 FOR FL430, DESCEND AND RELIGHT. WILL UPDATE AFTER MAINTENANCE. MAINTENANCE PERFORMED ENGINE INSPECTION AND GROUND RUNS IAW WITH GE M/M AIRCRAFT RETURNED TO SERVICE. 2L72 4J4 J A10CE 1E16 20030828000992003082800099WP 2003 8 28 MWEA030329 120030824A3610F17D87 PERISEAL DOUG DC9 DC981 3022081WP A/C BAY LEAKING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31814ME 48010 TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AND STAYED ON UNTIL QRH WAS USED. NO LEAKS OBVIOUS. CLEANED TAIL TEMP SENSOR DOORS AND PROBES. FURTHER MAINTENANCE REMOVED AND REPLACED LEAKING PERI SEALS ON LEFT PNEUMATIC DUCT AND PERFORMED ADJUSTMENT TEST OF THE LEFT AND RIGHT TAIL COMPARTMENT TEMPERATURE HIGH SENSORS. 2L72 4F A6WE 20030829000142003082900014NM 2003 8 29 CALA0300479 120030822A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20030722000502003072200050NM 2003 7 22 SWAA031508 120030709A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 372, STR 15L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030718000142003071800014NM 2003 7 18 AMTA200300790 120030617A3350 FUSE BOEING737 73783N 13844HINM EMERGENCY LIGHTSFAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11311TZ 32578 RIGHT OVERWING EXTERIOR EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FUSES. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030806001272003080600127NM 2003 8 6 AWXA200300826 120030711A5320654583471 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A 1 INCH CRACK WAS FOUND ON TIE STRAP AT BS 343, LBL 48, WL 200.5. MAINTENANCE STOP DRILLED CRACK ON TIE STRAP AT BS 343, LBL 48, WL 200.5; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 PG 213 & 219, FIG 204. 2L72 4F RTA16WE 20030807001152003080700115SW 2003 8 7 ALGA088163 120030721A6320E6893673 GEAR BELL 407 407 1182206SW ALLSN 250C 250C30S 03013GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03507AL723 CAG90759 53103 CAE890824S HEAVY SPALLING ON GEAR TEETH, DUE TO IMPROPER MESHING OF GEAR TEETH. REMOVED AND REPLACED. 1G71 3U3 UO H2SW E1GL 20030812000192003081200019NE 2003 8 12 HEEA088438 120030801A33407655002005104 SEARCH LIGHT SKRSKYS76 S76A 8143006NE EXTERIOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 SEARCH LIGHT WOULD NOT TURN OFF. 1G72 3U H1NE 20030829001632003082900163NM 2003 8 29 SWAA031828 120030813A32601061226 UPLOCK SENSOR BOEING737 7373K2 13844BANM RT MLG FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29340LV 23738 AIR TURNBACK, RT MLG UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP AND OFF. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20030902001142003090200114NM 2003 9 2 0301236306 120030704A3350 CONNECTOR BOEING747 747451 1384940NM BATTERY PACK INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21-35 HJK AND FROM DOOR 1L TO LAV DOOR 1L. RESEATED CONNECTOR PLUG AT BATTERY PACK AND RESPLICED WIRE. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030904001212003090400121EA 2003 9 4 COMA0360397 120030830A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01991CA13280 7216 FLIGHT 5188 GEAR DISAGREE WARNING. REPLACED HYDRAULIC PUMP 3A. 2L72 4F RTA21EA 20030904001872003090400187WP 2003 9 4 AALA20030719 120030704A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST UKUNKNOWN 1 SW21210AA 49161 DFW - OVERHEAD EMERGENCY LIGHT INOPERATIVE IN CABIN. RECONNECTED LOOSE CONNECTION AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030813001082003081300108WP 2003 8 13 GTIA030554 120030617A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD PIT STATION 450 TO 494 L30, LONGERON FLANGES CORRODED ON UPPER AND LOWER SURFACES. REMOVED 01 LONGERON 30 BETWEEN STATION 475 FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW LONGERON 30. INSTALLED NEW LONGERON 30. FABRICATED NEW LONGERON SPLICE FOR STATION 415 PER SPIRIT AIRLINES EA 5310-0317. INSTALLED NEW SPLICE. (M) 2L72 4F A6WE 20030728000822003072800082NE 2003 7 28 SWAA031596 220030718A72613352610040 OIL SYSTEM BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE NR 1 ENGINE CONTAMINATED A SWAAAB UNSCHED LANDING EMER. DESCENT JY WARNING INDICATION ENGINE STOPPAGE CRCRUISE 1 SW29659SW 23229 724426 IN FLIGHT SHUTDOWN, DECLARED EMERGENCY, NR 1 ENGINE OIL PRESS LIGHT ILLUMINATED, OIL QUANITY WAS AT ZERO. FOUND TORLON CHIPS IN LUB UNIT, CLEANED AND REINSTALLED PER MM. 2L72 4F4 FRTA16WE E2GL 20030729000802003072900080NM 2003 7 29 QXEA200300750 120030616A5410 STRUT DHAV DHC8 DHC8201 2809001NM NR 2 NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - CHAFING ON LOWER SUPPORT STRUT NR 2 ENGINE. REPAIRED IAW RD 8-54-036. 2H72 4T RTA13NM 20030825000042003082500004WP 2003 8 25 UPS03840940 120030616A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3 HFEC INSPECTION OF THE L-1 DOOR LOWER AFT CORNER DETECTED A CRACK APPROX. .750 INCHES SKIN, STATION 60 BETWEEN LONG. 20L-21L CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER I.A.W. SRM. 53-2-0 FIG. 15. 2L74 4F RT4A25 20030825000942003082500094NM 2003 8 25 CALA0300435 120030804A5720 BRACKET BOEING737 737524 1384721NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND A 6 INCH CRACK IN RT WING BRACKET UNDER PANEL 5849, WBL 198.6. THE BRACKET WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030825001442003082500144WP 2003 8 25 GTIA030607 120030709A5755 SUPPORT DOUG DC9 DC982 3022082WP LT SPOILER BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND LEFT INBOARD SPOILER TORSION BAR OUTBOARD SUPPORT BROKEN. REMOVED LEFT INBOARD SPOILER TORSION BAR OUTBOARD SUPPORT. INSTALLED NEW SUPPORT. (M) 2L72 4F A6WE 20030910001612003091000161EU 2003 9 10 ASOA03360 120030807A7110S5431212000200 COWLING AEROSPATR72 ATR72 EU RT ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING AN A-CHECK IN MCN, THE RIGHT ENGINE AFT OUTBOARD COWL BOTTOM CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ENGINE AFT OUTBOARD COWL BOTTOM CORNER IAW SRM 54-30-00. (M) 2H72 4T RT 20030926001492003092600149WP 2003 9 26 ABXA030343 120030820A53203913577501 INTERCOSTAL DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 CABIN FLOORBEAM INTERCOSTAL BETWEEN STA. 256 AND 275, BUTT LINE O, CRACKED FORWARD END. REPLACED INTERCOSTAL IAW DC-9 SSRM K05159. 2L72 4F A6WE 20031001000622003100100062NM 2003 10 1 03FDEA00450 120030415A5312 BULKHEAD BOEING727 727200 138407ENM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 CRACKS IN RIGHT WHEEL WELL, 870 BULKHEAD SKIN WEB. REPAIRED CRACK IAW FEDEX EA 7-5310-69465 2L73 4F RTA3WE 20031002001272003100200127NM 2003 10 2 AWXA200301038 120030813A53306545849158 SKIN BOEING737 737277 1384570NM PWA JT8 JT8D* NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON EXTERNAL FUSELAGE SKIN AT FASTENER HOLE OF R-2 DOOR CUTOUT AT FORWARD LOWER CORNER. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED AN INNER PLATE, OUTER PLATE, AND A FILLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-3, PG. 200-227, FIG. 46. 2L72 4F4 FRTA16WE E2EA 20030908002512003090800251EA 2003 9 8 SWIA200312342 120030825A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 AFT COMPARTMENT; FS 625.0; STR 14L HAS A CRACKED ATTACH ANGLE. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-42-06, 51-40-11 & 51-25-16. P/N: 601-35012-51 2L72 4F RTA21EA 20030908002692003090800269 2003 9 8 SWIA200312360 420030827A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07578SW4288 4288 120346 AUTOPILOT FAILS WHEN SELECTED TO F/O'S SIDE. TRIM FAIL & AUTOPILOT FAIL ON MAP & T, P, & E ON AUTO PILOT PANEL. ILLUMINATE WITH ASSOCIATED FAILURE. F/O'S FLIGHT DIRECTOR BARS AT TIMES ERACTIC WITH PITCH UP COMMANDS. REMOVED AND REPLACED AUTOPILOT COMPUTER IAW MM 22-10-02. OP CHECKS GOOD. P/N: 622-8315-402 S/N OFF: 2947 S/N ON: 1539. 2L72 4T RTA31SO 20030909002082003090900208 2003 9 9 BAQA088836 420030822A3416066305401 ALTIMETER BOLKMS117 BK117A3 5626015EU RADAR WILL NOT TEST B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03391813103 7003 RADAR ALTIMETER UNIT WILL NOT TEST. WHEN KNOB IS PUSHED TO SET FLAG, YOU CAN FEEL IT SLIPPING AND RATCHETING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030909002412003090900241WP 2003 9 9 ABXA030321 120030804A33505708458503 BATTERY PACK DOUG DC8 DC863 302198AWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23819AX 45927 DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY IAW DC8 MM 33-50-01. CHECKED GOOD. 2L74 4F 4A25 20031006001322003100600132NM 2003 10 6 SWAA032026 120030911A3350BR2013 LAMP BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND SEVERAL EEPLS LIGHTS INOP AND SEVERAL EEPLS LENS MISSING IN CABIN. RELAMPER LIGHTS AND INSTALLED LENSES PER MM. 2L72 4F A16WE 20031006001172003100600117NM 2003 10 6 HOC2003F00020 120030826A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0779749 22451 DURING A (C) CHECK, CORROSION WAS NOTED ON FUSELAGE SKIN INTERIOR AT STA 600-680, LBL85. 2L73 4F4 F A3WE E2EA 20031007000752003100700075NM 2003 10 7 SWAA031949 120030829A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031021002482003102100248WP 2003 10 21 GTIA030696 120030912A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND CABIN LONG 18L WEB CORRODED STATION 274. CUT OUT DAMAGED WEB AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20031022000652003102200065NM 2003 10 22 QXEA200301166 120030911A5410 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 LEFT LOWER COWL AFT CONE SUPPORT BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103. 2H72 4T4 TRTA13NM E00062EN 20031027001312003102700131EU 2003 10 27 RAIA00309246 120030921A2910EP2000106 LINE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM LEAKING A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03551HK 41040 5471-PIA- AFTER ARRIVAL AND PARKING AT STL LOST HYD PRESSURE. MAINTENANCE REMOVED AND REPLACED PRESSURE LINE IN RIGHT ENGINE BAY AREA. 2L72 4T RTA41NM 20031028001662003102800166NM 2003 10 28 ASAA0340073 120030227A53206573746 ANCHOR BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND AFT PIT FORWARD NET LEFT LOWER ANCHOR CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040127001992004012700199NM 2004 1 27 ASAA0380597 120030927A33500105603 LIGHT DOUG MD80 MD83 3023681NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01979AS 53471 SAN PREFLIGHT CHECK, FIRST 4 EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20031029001062003102900106NE 2003 10 29 MALA030439 220030925A7510216118218 BLEED BAND BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 4 ENGINE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15523XJ E2348 DURING FLIGHT NR 3447, AFTER DEPARTURE THE NR 4 ENGINE ITT WENT HIGH, AND OTHER PARAMETERS DROPPED OFF. AIR RETURN TO MEM. MAINTENANCE REPLACED NR 4 ENGINE BLEED BAND IAW ALLIED SIGNAL MM 72-00-34. PN/ON 2-161-182-18, SN/OFF UNREADABLE, SN/ON 032453712278. OPS CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20031107001282003110700128SO 2003 11 7 SIMA200327909 120031004A531514521713005 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 ABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 23. BLENDED THE CORRODED AREA OF THE HAT BEAM AND PERFORMED NDT INSPECTION. CLEANED, TREATED, AND APPLIED EPOXY PRIMER TO THE BLENDED AREA. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 22, CHAPTER 53-21-10 FIGURE 207. (M) 2L72 4F RTT00011AT 20031107001532003110700153NM 2003 11 7 AALA20031074 120030917A3397 WIRE BOEING767 767323 1385205NM CABIN BURNED A AALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW21372AA 25199 AFW - DURING ROUTINE MX CHECK, FOUND WIRE HARNESS TO CONNECTOR EPL POWER SUPPLY WIRES CHAFED AND BURNED. INSPECTED HARNESS FOUND PLUG MISWIRED JUMPER BETWEEN PIN 24-20 WAS ACTUALLY IN POSITION 24-21. THIS A/C FLEW IN LIKE THIS EPL SYSTEM OPS CHECKED GOOD UNDER THESE CONDITIONS. HOWEVER, 4 WIRES WERE BURNED DOWN TO CONDUCTOR. INSPECTED, REPAIRED AND SECURED WIRES PER WDM CHP 20 STANDARD PRACTICES. OPS CHECK EMERGENCY LIGHTING SYSTEM, CHECKED GOOD. INSTALLED JUMPER IN CORRECT LOCATION PER SDM 33-51-14. (M) 2L72 4F RTA1NM 20031110001172003111000117NM 2003 11 10 QXEA200301309 120031020A6120699018002 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM PROPELLER SYS MALFUNCTIONED A QXEAK NONE O OTHER CLCLIMB 1 NM09407QX838 4049 BOI - FLIGHT NR 2398 DURING CLIMB NR 2 PROP CHANGED FROM 850 TO 1020 UNCOMMANDED, POWER LEVERS IN RATING DETENT. CONDITION LEVERS AT 850 POWER AT MCL. AFTER RESETTING PROPS TO 850, -5 MINUTES LATER NR 2 PROP AGAIN WENT TO 1020. REPLACED PEC, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031110001612003111000161NM 2003 11 10 SWAA032263 120031015A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 460 AND BS 480. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031112001032003111200103NM 2003 11 12 AWXA200301382 120031109A521080330035 RESERVOIR BOEING757 757225 1384959NM R1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 PHX - EMERGENCY EVACUATION SYSTEM - DURING INSPECTION THE R-1 DOOR ASSIST BOTTLE PRESSURE LEAKED DOWN TO 2000 PSI. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR EMERGENCY POWER RESERVOIR IAW BMM 52-11-30 PG 401, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030731000252003073100025NM 2003 7 31 QXEA200300846 120030720A243611521086 GCU BOMBDRDHC8 DHC8401 1390041NM NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM09412QX 4059 SEA- ON FLIGHT 2344 NR 1 DC GENERATOR CAUTION LIGHT CAME ON AFTER TAKEOFF IN SUN AND AGAIN AFTER TAKEOFF IN BOI. ABNORMAL CHECKLIST WAS FOLLOWED ON BOTH OCCASIONS. LIGHT WENT OUT BOTH TIMES. REMOVED AND REPLACED DC GCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030911000192003091100019SO 2003 9 11 C2XA03BT083 120030822A2621 RELAY EMB 145 EMB145XR SO FIRE BOTTLE FAILED A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2714105 649 BAG EXTINGUISHER NOT ILLUMINATED DURING FIRE DETECT TEST. REMOVED AND REPLACED RELAY NR I01. OPS CHECK GOOD IAW EMB145 MM 26-23-00. 2L72 4F RT 20030911000622003091100062WP 2003 9 11 DHL2003873552 120030617A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING IB L/E FORMER CRACKED 0.250 AT XFS.566.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT XFS.566.000 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030915000692003091500069SW 2003 9 15 HEEA088965 120030826A243523046020 STARTER GEN BELL 212 212 1181420SW ENGINE FAILED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03278057340 31106 GENERATOR FAILED IN FLIGHT. AFTER SHUTDOWN NOTED LOUD GRINDING NOISE COMING FROM THE STARTER WHEN UNIT WAS MOTORED. REPLACED STARTER GENERATOR. TO BE SENT TO VENDOR FOR REPAIR. 1G71 4U H4SW 20030916001402003091600140GL 2003 9 16 BAQ2003F00001 220030625A72602306336970 SEAL AGUSTAA109 A109A2 0260120EU ALLSN 250C 250C20B 03013GL GEARBOX LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 NM011PJ 35 CAG37313 7262 CAE834460 AFTER 35 HOURS TIME IN SERVICE NR 1 ENG STARTED LEAKING (BEYOND LIMIT). FOUND BOTH FORWARD AND AFT SEALS HAD MISSING INTERSAL CIRCULAR SPRINGS. THIS GEARBOX WAS JUST OVERHAULED, W/O NR LW422398. ALSO FOUND 2ND GEARBOX IN INVENTORY SN: CAG37879, IN SAME CONDITION. 1G72 3U3 U H7EU E4CE 20031118000742003111800074 2003 11 18 CALA0300580 420031009A2565 CONNECTOR BOEING757 757224 1384958NM DISARM PANEL CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712125 28967 THE LT EMERGENCY ESCAPE SLIDE FAILED TEST 1. TROUBLESHOOTING PER FIM 25-65-00 FOUND CANNON PLUG D40828 AT LT EMERGENCY HATCH DISARM PANEL HAD LITE SURFACE CORROSION ON SEVERAL PINS. THE CONNECTOR WAS CLEANED AND RECONNECTED AND SYSTEM TESTED NORMAL. 2L72 4F RTA2NM 20040113000712004011300071EA 2004 1 13 03357689 120031223A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27689BR 7737 DURING INSPECTION THE LT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040115000012004011500001EU 2004 1 15 AWXA200301333 120031025A274247145133 ACTUATOR AIRBUS320 A320231 3930325EU THS BINDING A AWXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP28621AW 053 DURING C-03 CHECK VERIFICATION FLT AFTER T/O PILOTS OBSERVED AN ELAC 1 & 2 PITCH FAULT FOLLOWED BY A REPORT THAT STAB JAMMED & STAB TRIM WHEELS WERE HARD TO MOVE. MAINT R&R THS ACT IAW A320 AMM. LEAK AND OPERATIONAL TEST OF THE THS ELECTRICAL CONTROL GOOD IAW A320 AMM. FUNC TEST OF TRIMMABLE HORIZONTAL STAB ACT CONFIRMED FAILURE OF UNIT. FAILURE FOUND ON 2 PTA ELECTRIC MOTORS AS WELL AS OTHER FAULTS. DISASSEMBLY REVEALED UNIT LEAKING FROM COMMAND RVDT PACK, PTA PLUNGER, MOTOR SHAFT SEALS, & THRESHOLDS, A BACK SEAL FOUND MISSING AS WELL AS A SPRING ON PTA PLUNGER. ACCOMPLISHED SB 47145-27-04 & SB 47145-27-05 CHANGING MFG PN TO 47145133. UNIT CLEANED, INSPECTED, REPAIRED, RECALIBRATED, & RECERTIFIED IAW CMM. 2L72 4F RTA28NM 20031218001002003121800100NM 2003 12 18 2003UALA00888 120031123A5753 ATTACH FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT WING TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29645UA 25280 LT WING, INBOARD FLAP, AFT FLAP MID ATTACH FITTING IS CRACKED ON OUTBOARD AND INBOARD SIDES, T/E FLAP HINGE FITTING. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING PER SRM 57-53-02, FIG 201. 2L72 4F4 FRTA1NM E24NE 20031219000772003121900077SO 2003 12 19 C2XA03TY205 120031207A5514KSC357620V BEARING EMB 145 EMB145 3260210SO HORIZONTAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 DURING A SCHEDULED INSPECTION BOTH HORIZONTAL STABILIZER SPHERICAL BEARING WERE FOUND TO BE WORN BEYOND SERVICE LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPHERICAL BEARINGS IAW EMB MM 55-37-00 AND EC 5510-01070. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20040105000532004010500053EA 2004 1 5 SWIA200312683 120031209A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILERON MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07925SW2982 2982 7682 SPOILERON FAULT MESSAGE. RIGHT SPOILERON ILLUMINATED WHITE DURING TAXI. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW CRJ MM 27-61-05. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 SECU UNIT WITH SERVICEABLE UNIT. (SECU) P/N OFF: 49-164-6, S/N OFF: 01656, OPS CHECKS GOOD. 2L72 4F RTA21EA 20030918001242003091800124EU 2003 9 18 FBL2003F00000 120030708A5302109037160109 MOUNT BRACKET AGUSTAA109 A109E 0260119EU TAILBOOM DAMAGED B FBLRO OTHER O OTHER NRNOT REPORTED 1 SO171YU 223 11130 WHILE TROUBLESHOOTING A FAULTY ANTI-COLLISION LIGHT THE MAINTENANCE TECHNICION FOUND THE LOWER ANTI-COLLISION LIGHT MOUNT BRACKET LOOSE AND SMOKING AT THE TWO FORWARD SCREWS. THIS BRACKET PN 109-0371-60-109 IS MOUNTED ON THREE RUBBER SHOCKMOUNTS. A NEW MOUNT WAS ORDERED, AND IT WAS DETERMINED THAT THE COUNTER SUNK SCREW THREADS WERE BOTTOMING OUT IN THE SHOCKMOUNTS BEFORE PROPER CLAMP-UP OF THE MOUNT COULD BE ACHIEVED. HAD THIS CONDITION CONTINUED, THE MOUNT WOULD HAVE CHAFED THROUGH POSSIBLY ALLOWING THE ANTICOLLISION LIGHT TO DEPART THE AIRCRAFT. THIS CONDITION WAS ELIMINATED BY ADDING A NAS1149FN623P WASHER BETWEEN THE SHOCKMOUNT AND THE MOUNT BRACKET. 1G72 3U RTH7EU 20031010000492003101000049NM 2003 10 10 03FDEA01568 120030918A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CRACKED FRAME AT BS 380, 3 INCHES BELOW STR. 7R FWD UPPER END OF DOOR CUTOUT. ** SD ** COMING 2L73 4F RTA3WE 20031014000962003101400096NM 2003 10 14 SWAA032147 120030923A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727D AT STR 23L AND BS 941 AT STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031124000712003112400071NM 2003 11 24 CALA0300645 120031114A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND A 1 INCH CRACK IN FRAME INNER CHORD AT STA 616, WL 200, RT SIDE. THE INNER CHORD WAS REPAIRED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20031125000722003112500072WP 2003 11 25 DHL2003805603 120030818A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 FLIGHT COMPT CAPT'S LEFT AFT SEAT TRACK HOLES ELONGATED. FABRICATED STRAP IAW SRM 53-2- PG 3 OF 3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED STRAP ON FLIGHT COMPT CAPT'S LEFT AFT SEAT TRACK IAW SRM 53-2-3 PG 3 OF 3, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031202001212003120200121SO 2003 12 2 SIMA200330101 120031017A2120 ODOR EMB 135 EMB135KL 3260302SO CAIBN DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21827AE 145602 CREW REPORTED A BURNING INSULATION ODOR IN FLIGHT. AIRCRAFT WAS DIVERTED TO LIT AND LANDED WITH NO OTHER INCIDENT REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. BLEED SYSTEM WAS INSPECTED AND AN OPERATIONAL CHECK WAS COMPLIED WITH. NO ODOR WAS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040121000182004012100018NM 2004 1 21 03FDEA02274 120031226A5744ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT WING O/B FLAP O/B HINGE FITTING I/B MOUNT I/B AND O/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD. FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040116000072004011600007NE 2004 1 16 IXXA0300084O 220031209A7230 COMPRESSOR DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 3 ENGINE STALLED A IXXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW1141CX 756622196 46129 ON TAKE OFF FROM TAPA AT 115KTS NR 3 ENGINE COMPRESSOR STALLED AND POWER ROLLED BACK. CREW REJECTED TAKE OFF. 1 TIRE WAS FLAT AND THERMALED 3 MAIN ON RIGHT GEAR. MAINTENANCE INSPECTED NR 3 ENGINE FOR FOD/BIRD STRIKE PER ALL APPLICABLE MANUALS, AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20040122001392004012200139SO 2004 1 22 QRX2004F00002 120031029A783094HEN102RA SWITCH GULSTMGV GV 3980116SO RROYCEBR700 BR700710A110 NE THRUST REVERSER FAILED B QRXRO OTHER O OTHER NRNOT REPORTED 1 SW05130GV1170 630 SWITCH FAILED. FOUND THE SWITCH HOUSING FULL OF WATER. THIS SWITCH IS LOCATED ON THE TOP SIDE OF THE ENGINE NACELLE. IT APPEARS TO HAVE WATER MIGRATING THROUGH THE SWITCH PLUNGER INTO THE HOUSING. THIS COULD COME FROM BEING PARKED IN THE RAIN OR AIRCRAFT BEING WASHED. 2L72 4F4 FRTA12EA E00057EN 20031204000462003120400046WP 2003 12 4 GTIA030837 120031006A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FORWARD CABIN FLOORBOARD STATION 180 TO STATION 160 RBL 8 INCHES TO RBL 44 HAS SEVERAL INSERTS BROKEN OUT, CORRODED AND SOFT/MUSHEY. FABRICATED NEW FLOOR BOARD. (M) 2L72 4F A6WE 20031204000552003120400055NM 2003 12 4 GTIA030849 120031020A3350 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 MCO - ONE EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT ON PANEL AT LEFT SIDE OF WALKWAY. RELAMPED AND SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT ON PANEL. (M) 2L72 4F RT 20031209000572003120900057CE 2003 12 9 DXTA200300149 120031030A3260327 BULB CESSNA500 560CESSNA 2076750CE MLG INDICATOR BURNED OUT E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07377QS 5600377 UPON GEAR EXTENSION RIGHT MAIN AND NOSE GEAR INDICATED DOWN AND LOCKED, LEFT MAIN GEAR NO INDICATION, ALSO NO (RED) GEAR UNSAFE. EXECUTED EMERGENCY GEAR EXTENSION CHECKLIST, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED THE LT MAIN GEAR DOWN & LOCKED LIGHT BULB WITH A NEW UNIT. RESET LOCK AT HANDLES & CONTROL LEVER ON PNEUMATIC BOTTLE, RE-SERVICED PNEUMATIC BOTTLE. ACCOMPLISHED GEAR SWINGS, ALL WORK IAW THE CESSNA 560 MM CHAPTERS 33-00-00, 32-01-00 & 12-13-01. 2L72 4F RTA22CE 20031211000482003121100048NM 2003 12 11 C1HA200385012 120031107A3350 BATTERY PACK BOEING727 7272S7 138407ZNM CABIN DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15685CA 22492 OUTER EMERGENCY LIGHTS BY R2 & L2 DOORS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 33-50-51 IN 727 MM, ALL OPS CKS GOOD. 2L73 4F A3WE 20031211000762003121100076NM 2003 12 11 AWXA200301411 120031029A5320654529624 SPLICE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT TEE SPLICE AT BS 860. MAINTENANCE REMOVED AND REPLACED CORRODED TEE SPLICE AT BS 860 IAW B737-300 SRM 51-40-02, FIG 9 & 10. 2L72 4F RTA16WE 20031020000862003102000086NM 2003 10 20 VNAA0309015 120030924A3241 ANTI-SKID SYS DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG MALFUNCTIONED A VNAAO OTHER O OTHER TOTAKEOFF 1 GL07463PS 3087 THE CREW REPORTED THAT THE AIRCRAFT LEANED TO THE RIGHT ON THE TAKEOFF ROLL, THE ANTI-SKID SYSTEM FAILED, THE CREW THEN ABORTED TAKEOFF. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM AND THE ANTI-SKID SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. HIGH SPEED TAXI RUNS WERE THEN PERFORMED, ALL WITH NO DEFECIENCIES NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030915000832003091500083 2003 9 15 BAQA088880 420030830A34221303465209130004HSI BOLKMS117 BK117A3 5626015EU COCKPIT STUCK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911BK1787 7099 COMPASS CARD STICKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030916000202003091600020WP 2003 9 16 ANCF200300024 120030904A213139245431 CONTROLLER DOUG DC9 DC983 3022083WP AC PACK MALFUNCTIONED W ANCFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23190AN3980 3980 53190 AFTER T/O WITH PACKS ON, THE FLOW LIGHT WAS PRESENTED,THE LEFT PACK DROPPED TO ZERO AND THE RIGH PACK WAS SHOWING 20 PSI. THE LEFT PACK WAS NOT POSSIBLE TO RESTORE SO WE PROCEED TO PRESSURIZE MANUALLY,WHICH WAS ALSO IMPOSSIBLE.ON FINAL THE LT PACK WAS RESTORED. RT PACK FLOW CONTROL VALVE WAS REPLACED IAW AMM 21-31-02 IN LT PACK WAS REPLACED NEUMATIC PRESSURE REGULATING VALVE. PRESSURIZATION CHECK WAS ACCOMPLISHED IAW AMM 21-00-00 PAG 504. SATISFACTORY RESULTS. 2L72 4F RTA6WE 20030916000322003091600032NM 2003 9 16 03FDEA01074 120030627A5753ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT WING (WING SIDE) - OUTBOARD TRAILING EDGE FLAP, INBOARD HINGE FITTING FOUND HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORRODED. LT WING (WING SIDE) - OUTBOARD TRAILING EDGE FLAP, INBOARD HINGE FITTING HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW EA 1-5750-69355 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP, INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030918000582003091800058NM 2003 9 18 DLM88030714 120030801A2620269701055 FIRE BOTTLE DOUG MD88 MD88 3023688NM TAIL COMPT DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27919DL 49584 NR 2 FIRE BOTTLED DISCHARGED DURING T/S ENGINE RUN DUE TO AUG VALVE LEAK. REMOVED AND REPLACED LT ENGINE NR 2 AGENT BOTTLE. FOUND FLEX LINE FOR APU AGENT BAD. REPLACED SAME ALL WORK DONE PERM/M 2L72 4F RTA6WE 20040128000362004012800036NM 2004 1 28 DHL2003755012 120031226A3260 SWITCH BOEING727 727225 1384077NM MLG DOOR DIRTY A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01755DH 21857 RIGHT MAIN GEAR DOOR WILL NOT STAY UP WITH GEAR LEVER IN THE OFF POSITION. INSPECTED GEAR DOOR, DOOR MECHANISM, AND DOOR SWITCH. NO DISCREPANCIES. CLEANED DOOR SWITCH. OPERATED DOORS PER M/M 32-12-01, CHECKED GOOD. 2L73 4F A3WE 20040128000222004012800022SO 2004 1 28 RAIA00312317 120031215A2612 WARNING LIGHT EMB 145 EMB145 3260210SO APU FIRE DETECT MALFUNCTIONED A RAIAO OTHER N FALSE WARNING DEDESCENT 1 CE03821HK 145068 JAX- APU FIRE INDICATION DURING AIR START. MAINTENANCE INSPECTED APU, NO SIGN OF FIRE NOTED. 2L72 4F RTT00011AT 20040128001952004012800195NM 2004 1 28 P5CA0401020 120031227A7330 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 4 ENGINE ILLUMINATED A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23450PA 30808 706198 NR 4 ENG FUEL VALVE MESSAGE. TRANSFERRED TO DMI 32018 AND MEL 73-31-02 PER DDPG. 2L74 4F4 FRTA20WE E23EA 20040206000062004020600006 2004 2 6 MEX2003524 420031116A3417HG280D80 ADC DOUG DC9 DC987 3022087WP NR 1 FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23216AM46801 49586 AIRCRAFT RETURNED TO PLATFORM DUE TO A DIFFERENCE OF 6 KNOTS BETWEEN VELOCIMETERS. AT PLATFORM THE SYSTEM WAS CHECKED, CONFIRMING CADC NR 1 FAILURE. CADC NR 1 WAS REPLACED AND TESTED IAW MM 34-16-01. ADDITIONALLY BRAKE ASSEMBLY WAS CHECKED BY CONDITION, IAW MM 05-52-0 THE INSPECTION BY REJECTED TAKEOFF IS NOT NECESSARY. 2L72 4F RTA6WE 20040204000872004020400087NM 2004 2 4 QXEA200301286 120031011A5320 BRACKET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX- BRACKET FOR FORWARD DOOR STOP HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-36. 2H72 4T4 TRTA13NM E20NE 20040205000962004020500096NE 2004 2 5 CX7A194J0354 220031123A7261NAS61712 O-RING SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE OIL KINKED A CX7AE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 GL03302CE 340B193 785187 LEFT ENGINE OIL PRESSURE LOW BOTH GAUGE AND CWP INDICATIONS. 2L72 4T4 TRTA52EU E8NE 20040212000242004021200024SO 2004 2 12 AK02003F00001 120031105A7810 SHROUD MAULE MT7235MT7235 5470209SO LYC O540 IO540W1A5 41532NE RT EXHAUST CHAFED C AK0MK NONE O OTHER ININSP/MAINT 1 AL03138CP100 18072C L2808848A DURING AN ANNUAL INSPECTION THE RIGHT EXHAUST MUFFLER SHROUD WAS FOUND CONTACTING THE NR 3 CYLINDER INTAKE TUBE. IT APPEARS THAT DURING THE AIRCRAFT ASSEMBLY, THE EXHAUST MUFFLER SHROUD IS ATTACHED TO THE MUFFLER PRIOR TO INSTALLING ON THE ENGINE. DURING THE INSTALLATION, ADEQUATE CLEARANCE BETWEEN THE EXHAUST SHROUD AND INTAKE TUBE WAS NOT MAINTAINED CAUSING THE TWO PARTS TO BE PINCHED TOGETHER. THE SHROUD WAS IMPOSSIBLE TO REMOVE TO INSPECT THE MUFFLER WITHOUT REMOVING THE ENTIRE RIGHT EXHAUST ASSEMBLY. RECOMMENDATIONS FOR RECURRENCE ARE TO DESIGN A CLEARANCE CUTOUT IN THE EXHAUST SHROUD ASSEMBLY TO FACILITATE EASE OF REMOVAL AND PREVENT CONTACT WITH THE INTAKE TUBE. 1H71 3O3 ONC3A23 1E4 20040213000272004021300027SO 2004 2 13 SWIA200312720 120031227A275012064207615 HANDLE EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07237SW4533 4533 120314 FLAPS DO NOT RESPOND TO FLAP HANDLE. FLAP 15 SELECTED. FLAPS REMAIN UP. REMOVED FLAP HANDLE AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040217000062004021700006SO 2004 2 17 SIMA200402003 120030117A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21728AE7198 145328 THE LT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. CUT OUT DAMAGE SECTION OF LT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED EXTERNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 24, CHAPTER 53-21-10 FIG 201 SHEET 1. (M) 2L72 4F RTT00011AT 20030410001252003041000125SO 2003 4 10 SIMA200304802 120030213A27503632501003 MOTOR EMB 145 EMB145LR 3260212SO NR 2 FLAP DRIVE FAILED A SIMAO OTHER J WARNING INDICATION DEDESCENT 1 SW21623AE 145109 YOW - FLT 4098 - DURING DESCENT, CREW REPORTED A FLAP FAIL MESSAGE WITH FLAPS STUCK AT 1 DEGREE. CREW RESET PER AOM WITH NO HELP. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 FLAP DRIVE MOTOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030415001032003041500103GL 2003 4 15 CA030404001 220030331A72406870992J COMBUST CHAMBER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE CRACKED W O OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 CA (CAN) WHILE IN CRUISE FLIGHT THE PILOT NOTICED NR 2 ENGINE TOT WAS HIGHER THAN THAT OF NR 1 ENGINE. PILOT ATTEMPTED TO CARRY OUT A POWER CHECK ON NR 2 ENGINE BUT WAS UNABLE TO COMPLETE THE CHECK DUE TO TOT REACHING RED LINE.AIRCRAFT RETURNED TO BASE AND THE AME CARRIED OUT A VISUAL INSPECTION OF THE AIRCRAFT AND ENGINE. INSPECTION OF THE TURBINE AREA REVEALED A CRACK ACROSS THE REINFORCED AREA OF THE ARMPIT OF THE OUTER COMBUSTION CASE. THE OUTER COMBUSTION CASE WAS CHANGED AND THE A/C RETURNED TO SERVICE WITH NO FURTHER INCIDENT. 1G72 3U3 U H3EU E4CE 20030417001282003041700128NM 2003 4 17 UPS03240140 120030128A5320 FITTING BOEING727 72725C 138400HNM TAIL SKID CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, RT UPPER TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED RT UPPER TERMINAL FITTING IAW SRM 51-30-02. NEW FITTING INSTALLED IAW DRAWING 65-25992. 2L73 4F A3WE 20030424001552003042400155CE 2003 4 24 TIM2003F00000 120030303A5711991100471 SPAR CAP BEECH 99 C99 1154006CE PWA PT6 PT6A11 52043NE WING CORRODED E TIMAO OTHER O OTHER NRNOT REPORTED 1 NM07236AL17143 U236 DURING AN ANNUAL WING OUTBOARD UPPER AND LOWER MAIN SPAR CAP INSPECTION SEVERAL SMALL SPOTS WERE NOTICED. FURTHER INVESTIGATING REVEALED CONSIDERABLE CORROSION. 1L72 3T3 T A14CE E4EA 20030424002102003042400210WP 2003 4 24 UPS03840371 120030228A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, R1 LWR AFT DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED BETWEEN FASTENERS HOLES. CUT OUT DAMAGE IN SKIN IAW DC8 SRM 53-2-0. FAB FILLER DOUBLER AND TRIPLER IAW DC8 SRM TR 53-154. ALODINED AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 TR 53-154 AND DC8 SRM 53-2-0. 2L74 4F RT4A25 20030428000192003042800019WP 2003 4 28 MWEA030156 120030402A53305930485507 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RIGHT FUSELAGE SKIN AT A NUT PLATE HOLE STATION 1095 BELOW LONGERON 19 RIGHT HAS DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20030430000672003043000067NM 2003 4 30 USAASB03016 120030129A2750 WARNING LIGHT BOEING737 737401 1384701NM TE FLAPS ILLUMINATED A USAAO OTHER J WARNING INDICATION APAPPROACH 1 EA19425US 23992 ALB - FLT 1057 - ON APPROACH INTO ALB, FROM CLT, CREW RECEIVED A TWO DEGREE FLAP ASYMMETRY INDICATION. CREW DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ON TAXI TO THE GATE, THE FLAP PROBLEM CORRECTED ITSELF. MAINTENANCE OPERATED FLAPS THROUGH ENTIRE RANGE. INSPECTED JACKSCREW ASSEMBLIES, TRACK ASSEMBLIES AND ATTACHMENT POINTS. NO DISCREPANCIES NOTED. SYSTEM OPERATES NORMAL. (M) 2L72 4F RTA16WE 20030430001112003043000111NM 2003 4 30 CALA0300227 120030428A53146562125 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917306 23357 FORWARD BAG BIN CORROSION AT STRINGER 28R STATION 500D PLUS 17 IN. REPAIR ACCOMPLISHED PER EC/RA 5310-04345. 2L72 4F RTA16WE 20030502000532003050200053WP 2003 5 2 ASAA0380165 120030228A53202929169 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL SUPPORT IS CORRODED AROUND FASTENER HOLES AT FS 237. REPLACED SUPPORT PER SRM 51-10-2, 10-3, 10-4, AND 30-5. (M) 2L72 4F A6WE 20030502000592003050200059WP 2003 5 2 ASAA0380153 120030224A531199115057 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FRAME CRACKED IN FIVE PLACES AT FS 83. REPLACED FRAME PER SRM 51-10-4, 30-2, AND 30-5. (M) 2L72 4F A6WE 20030502002622003050200262NM 2003 5 2 DHL2003741550 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS 2 EACH DENTS AFT BS 400 BELOW STR 18L. CUT OUT DAMAGE AREA (2 EACH DENTS) 1 INCH DIA BS 400 BELOW STR 18L IAW B-727 SRM 53-30-3 FIG 13. FABRICATED REPAIR DOUBLER 3.80 DIA 2024 T-3 .050 PO 9912380 IAW B-727 SRM 53-30-3 FIG 13. FABRICATED REPAIR FILLER 1 INCH DIA 2024 T-3 .040 PO 9912380 IAW B-727 SRM 53-30-3 FIG 13. TREATED AND PRIMED DOUBLER AND FILLER IAW B-727 SRM 51-10-6. INSTALLED DOUBLER AND FILLER IAW B-727 SRM 53-30-3 FIG 13. 2L73 4F RTA3WE 20030505001082003050500108NM 2003 5 5 AWXA200300426 120030423A3397BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 18 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE SPLICE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030506000662003050600066NM 2003 5 6 03FDEA00644 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) UPPER ATTACHMENT FITTING TO WING REAR SPAR BORE HOLE (2 EACH) CORRODED. CORROSION ON LT WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) UPPER ATTACHMENT FITTING TO WING REAR SPAR BORE HOLES (2 EACH) REMOVED AND REPAIR CARRIED-OUT AS PER CMM 57-44-08, FIG. 401. 2L73 4F RTA22WE 20030509000522003050900052NM 2003 5 9 MP011603B 120030407A571165162337 SPAR BOEING727 72721 1384003NM PWA JT8 JT8D9 52048NE WING CORRODED B KQ7RO OTHER O OTHER NRNOT REPORTED 1 SW1730MP 38261 18998 DURING AD COMPLIANCE, A CLOSE VISUAL AND NDT HFEC INSP OF WING REAR SPAR, A CRACK AND CORROSION WAS FOUND IN THE HEEL OF THE INBOARD PORTION OF THE DETERMINED TO BE OUT OF LIMITS IAW MFG SRM. ENGINEERING WAS CONTACTED AND REPAIRS WERE DRAWN. A SECTION OF THE SPAR WAS REPLACED FROM WS 70.5 THROUGH WS 210 IAW ENGINEERING DRAWINGS, MFG SRM AND SB. THIS A/C IS EARLY MODEL WITH LOW HOURS WITH CORPORATE INTERIOR. AC HAS SPENT MOST OF ITS CORPORATE LIFE ON THE WEST COAST IN DAMP SALTY SEA AIR ENVIRONMENT. THERE WERE NO INDICATIONS OF HARD LANDINGS OR WING OVER LOADING. 2L73 4F4 F A3WE E2EA 20030509001102003050900110SW 2003 5 9 ALGA086245 120030423A6220406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL ROTOR HEAD WORN E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03627AL345 53284 FOUND BEARING WORN AND RATCHETING. BEARING REPLACED BY (FIELD) MAINT. 1G71 3U3 UO H2SW E1GL 20030513001102003051300110NM 2003 5 13 AWXA200300462 120030428A575465C267935 SKIN BOEING737 73733A 1384673NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-17 CHECK 3 EACH 2 INCH CRACKS WERE FOUND ON NR 3 SLAT SKIN AT FASTENER HOLES ABOVE OUTBOARD AUXILIARY TRACK (HFEC VERIFIED). MAINTENANCE CUTOUT CRACKED SECTION OF NO. 3 SLAT SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, PG. 216-219, FIG. 206. 2L72 4F RTA16WE 20030527000912003052700091WP 2003 5 27 AALA20030375 120030326A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21591AA 53254 ORD - FLT 1251 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AFT OF ROW 22 RIGHT SIDE INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT LEFT OVERWING SIDE MARKER LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030528001002003052800100SW 2003 5 28 HEEA086609 120030521A6720 BEARING BELL 212 212 1181420SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736D 31135 BELLCRANK HAS WORN BEARINGS. REPLACED BEARING DW-4 DUE TO WORN AND SLEEVE 120-015-4KA DUE TO WORN. REPAIRED. 1G71 4U H4SW 20030528000612003052800061EU 2003 5 28 BAQA086415 120030514A6210L621M1010054 BLADE UROCOPEC135 EC135T1 5620026EU MAIN ROTOR CONTAMINATED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01511ME1781 0143 SUSPECTED WATER IN BLADE. PART ONLY LASTED 131.3 HOURS FROM LAST REPAIR. 1G72 3U H88EU 20030604002232003060400223EU 2003 6 4 BAQA086305 120030430A6330L633M2010101 MOUNT UROCOPEC135 EC135P1 8680990EU GEARBOX LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 FS01577LF 0140 GEARBOX MOUNT LEAKING FLUID. PLUNGER RECESSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030609001072003060900107SO 2003 6 9 C2XA03SH149 120030523A531014522460015 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030514001102003051400110NM 2003 5 14 SWAA031011 120030506A53116546543 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED (12 EA) AT STRINGER 9L, BS 406, 827, 867, 901, 440, 480, 500, 747, 767, 887, 847 & 807. REPAIRED FRAMES PER BFG ER. 2L72 4F RTA16WE 20030520000712003052000071WP 2003 5 20 GTIA030242 120030223A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CABIN STATION 200 BL0 TO RBL 50, LB5 CORRODED ON WEB SURFACE. REMOVED DAMAGED WEB SECTION. FABRICATED NEW WEB SECTION. FABRICATE SPLICE DOUBLER. INSTALLED SPLICE WEB DOUBLER. INSTALLED NEW WEB SECTION. (M) 2L72 4F RTA6WE 20030521001232003052100123NM 2003 5 21 C1HA200395061 120030515A3350ADMISC062 BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 AFT AIRSTAIR EMERGENCY EXIT LIGHT IS INOP. 2L73 4F A3WE 20030609001622003060900162EU 2003 6 9 CA030405002 120030403A63204619310069 BEARING BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL OTPUT QUILL PEELING W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) OUTPUT QUILL TAPERED ROLLER BEARING INNER RACE PEELING. 1G72 3U3 U H3EU E4CE 20030606000082003060600008NM 2003 6 6 C8GA20030015 120030516A2613355484225 SENSOR BOEING727 7272A1 138407FNM OVERHEAT DEFECTIVE A C8GAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO15286SC 21601 FLT 707 FROM PHX TO TOL. THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. FOLLOWED ALL CCIA PROCEDURES AND THE LOWER BODY OVERHEAT LIGHT REMAIN ON. ADVISED CCIA FLIGHT FOLLOWING AND ATC IN PHX OF THE PROBLEM AND AIR TURN BACK TO PHX. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED SYSTEM AND REMOVED AND REPLACED THE FORWARD AFT BODY (KEELBEAM) OVERHEAT SENSOR IAW MM 26-10. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030612001652003061200165NE 2003 6 12 AT0300015 220030529A7200BR700715AL30 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LEFT FAILED A ZZDAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO15958AT 55020 LEFT HAND ENGINE, LOUD POP AT FL350. ENGINE WAS NOTICED TO BE SPOOLING DOWN AT IDLE OIL QUANTITY WAS AT 2 QUARTS, OIL PRESSURE -0- AND RED BOX. REMOVED AND REPLACED LEFT HAND ENGINE ASSY. 2L72 4F4 FTRA6WE E00061EN 20030522000562003052200056SO 2003 5 22 C2XA03TY062 120030517A5320145217525615 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE RIGHT AFT FLOOR SILL AT FR22-23 WAS FOUND CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE AFT SERVICE DOOR SILL IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2L72 4T RTT00011AT 20030522000462003052200046WP 2003 5 22 GTIA030307 120030420A5321 FLOORBOARD DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 PAX CABIN FLOORBOARD CRACKED/BROKEN AT FS 218-294 LEFT BETWEEN SEAT TRACKS 1 AND 2. REMOVED FLOORBOARD, DRILL AND LOCATE AND INSTALLED FLOORBOARD. 2L72 4F4 F A6WE E2EA 20030527001252003052700125WP 2003 5 27 GTIA030329 120030415A5320 BRACKET DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE CARGO TRACK CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT PIT STA 1155 TO STA 1117. 4 EA BRACKETS SUPPORT RIGHT CARGO TRACK CORRODED (ATTACH TO THE BEAM). FABRICATED 4 EA ANGLES. 2L72 4F4 F A6WE E2EA 20030620000152003062000015SW 2003 6 20 HEEA087234 120030610A243523081018 STARTER GEN BELL 206 206L3 1182108SW ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038594X 51531 STARTER GEN MAKES GRINDING NOISE. FOUND CLUTCH DISENGRATED. SHOP REPAIR. 1G71 3U H2SW 20030707000872003070700087NM 2003 7 7 371PA0025 120030625A339758782 POWER CABLE BOEING737 737306 13844BGNM EMERGENCY LIGHTSINOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING SYSTEM INOPERATIVE. REPLACED POWER CABLE ASSY AND FLEX LAMP. OPS CHECK NORMAL. 2L72 4F RTA16NE 20030714000272003071400027NM 2003 7 14 SWAA031399 120030623A53306562125 SKIN BOEING737 7372H4 138448CNM KEEL BEAM CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT LT KEEL BEAM, BS 727 PLUS 10. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030630000182003063000018NM 2003 6 30 AWXA200300603 120030513A532069374221 ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND ON CENTER SECTION ANGLE BS 663, LBL 60. MAINTENANCE REMOVED CRACKED ANGLE AT BS 663, LBL 60; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-37422; INSTALLED REPAIR PART IAW B737-200 SRM 51-10-2, PG. 8. 2L72 4F RTA16WE 20030710000372003071000037NM 2003 7 10 GTIA030450 120030608A542059306451 ACCOUSTIC LINER DOUG MD80 MD83 3023681NM NR 1 NACELLE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 DURING DAILY INSPECTION, FOUND NR 1 ENGINE ACCOUSTIC LINER DAMAGED. REMOVED/REPLACED NR 1 ENGINE NOSE COWL, NO DEFECTS NOTED. (M) 2L72 4F RT 20030709000422003070900042WP 2003 7 9 AALA20030514 120030430A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21422AA 49334 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM ROW 3-20 AND OVERWING INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHTS WIRES AT 19R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030710000522003071000052NM 2003 7 10 DHL2003721003 120030530A2150R101ARE5001FC RELAY BOEING727 727228 1384083NM LT & RT AC PACKSFAILED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01721DH 19545 ON GROUND WITH BOTH PACKS ON LT PACK TRIP AND OVERHEAT LIGHT ILLUMINATED. SMOKE ENTERED IN THE COCKPIT. DEFERRED PER MEL 21-5-4 CAT C TRANSFERRED TO DMI 13119. PLACARD INSTALLED. MAINTENANCE CONTROL WAS NOTIFIED. COMPLIED WITH SP 21-5. REF DMI 13119, BOTH PACKS ON LEFT PACK TRIPPED OVERHEAT. REPLACED LT RELAY R596 PER M/M 21-50. OPS NORMAL. THIS CLEARS DMI 13119. PLACARDS REMOVED. 2L73 4F RTA3WE 20030714000402003071400040NM 2003 7 14 SWAA031355 120030617A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030710001422003071000142NM 2003 7 10 EIA2003087 120030614A5753 FLAP TRACK BOEING747 747SR46 1384816NM TE FLAPS CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 NR 1 FLAP TRACK FWD I/B SIDE BOLTS HOLES 1, 3 & 4 ARE CORRODED AND SOME CAD PLATING MISSING. REWORKED NR 1 FLAP TRACK I/B HOLES 1, 3 AND 4 PER SB 747-57-2256 PAGES 1-52. 2L74 4F RTA20WE 20030128001762003012800176WP 2003 1 28 ZW0A0300809 120030113A2560 FITTING DOUG DC9 DC982 3022082WP CABIN CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT IN THE FWD CABIN AT THE FWD SERVICE DOOR WAY, FOUND SILL BRACKET (GIRT BAR FITTING) CORRODED AT STA 172, RBL 53. REMOVED AND REPLACED FITTING PER SPM 6-70-01. 2L72 4F A6WE 20030203001682003020300168EA 2003 2 3 EXO2003F00001 120030121A7830 MOUNT CNDAIRCL600 CL6001A11 1900302EA THRUST REVERSER CRACKED E EXOAK NONE O OTHER ININSP/MAINT 1 SO17678CG7063 B90036 1027 DURING INSPECTION OF THE RT THRUST REVERSER TRANSLATING SLEEVE. THE TOP JACKSCREW MOUNTING WAS FOUND CRACKED AROUND THE O-RING. 2L72 4F RTA21EA 20030207001612003020700161EA 2003 2 7 COMA0360085 120030205A5230H2912A SPRING CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR BROKEN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01958CA 7111 FLIGHT 5542 CARGO DOOR CAUTION MESSAGE.REPLACED THE DOOR HANDLE LATCH SPRING. 2L72 4F RTA21EA 20030214000732003021400073WP 2003 2 14 ASAA0380048 120030105A5230591014160 RETAINER DOUG DC9 DC983 3022083WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY DOOR LOWER SEAL RETAINER IS CHAFED AT FORWARD AND AFT CORNERS. REPLACED SEAL RETAINER PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20030218000212003021800021NM 2003 2 18 03FDEA00118 120030210A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION AROUND LOWER FLOORBEAM ANGLE NUT PLATE HOLES. BS 1070, LBL 41, RBL 51, WL 201. REPLACED BS 1070 FLOORBEAM LOWER ANGLE IAW EA 7-5310-68182. 2L73 4F4 FRTA3WE E2EA 20030220000892003022000089 2003 2 20 QXEA0300085 420030114A3444 WARNING SYSTEM DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09379PH 530 SEA ON FLIGHT 2251- GPWS CAUTION LIGHT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST. PERFORMED EGWPS TEST WITH NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040301000182004030100018EU 2004 3 1 KBM2004F00015 120031217A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE T/R HALF SHELL WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH1268 314 DURING POSTFLIGHT, FOUND TAIL ROTOR BLADE SHELL LAMINATED LEG IS WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW. (K) 1G71 3U3 U H9EU E19EU 20031211001842003121100184WP 2003 12 11 2003F00641 120030907A532039162172 FITTING DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 RIGHT MAIN WHEEL WELL Y STA 577, FITTING CRACKED. (M) 2L72 4F A6WE 20031212001782003121200178EA 2003 12 12 COMA0360519 120031124A3234555405 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01735CA3449 7267 FLIGHT 5578 LANDING GEAR DISAGREE WARNING, REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20040309001782004030900178NM 2004 3 9 ASAA0310673 120031218A335086210144 BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - EMERGENCY EXIT IDENTIFIER FOR THE RIGHT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK, THEN EXIT IDENTIFIER TESTED NORMAL. (M) 2L72 4F RTA16WE 20031211001752003121100175EA 2003 12 11 ASOA03534 120031024A27409960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11885AS 7521 DURING CLIMB-OUT FROM ATL-MTY, AFTER ROTATION THE CREW RECEIVED STABILIZER AND MACH TRIM WARNINGS. THE CREW COMPLIED WITH THE ABNORMAL CHECKLIST WITHOUT ANY EFFECTS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS STABILIZER DISCONNECT SWITCH AND THE HORIZONTAL STABILIZER TRIM CONTROL UNIT, P/N 7060-8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031212001052003121200105NM 2003 12 12 SWAA032401 120031030A53116516301 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 188, WL 207, LT AND RT SIDES. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20040423000432004042300043WP 2004 4 23 AALA20030830 120030803A324142807 CONTROL BOX DOUG DC9 DC983 3022083WP ANTI SKID MALFUNCTIONED A AALAO OTHER J WARNING INDICATION LDLANDING 1 SW21962TW 53612 ORD - FLT 2356 - DFW-ORD, ON LANDING ROLL BOTH RIGHT MAIN TIRES GRABBED AT SPEED OF ABOUT 89 KNOTS. ANTI-SKID FLASHED ON OVERHEAD PANEL. BOTH TIRES WENT FLAT. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20050223001182005022300118EU 2005 2 23 ERAA097535 120031230A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM INOPERATIVE E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03124EH S559 GUIDE ASSY IS INOPERABLE. FOUND BROKEN SOCKET AND SWITCHES. 2 SCREWS CORRODED. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SWITCHES, SCREWS AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 REM 405. 1G72 3U H3EU 20030813001972003081300197 2003 8 13 SWAA031645 420030724A2565D31354 INDICATOR BOEING737 7372T4 1384492NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED PM CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES PRESS INDICATOR OUT OF VIEW. REPOSITIONED AFT CABIN DOOR SLIDES PER MM 2L72 4F A16WE 20030815000312003081500031 2003 8 15 HEEA088515 420030721A3457N0002000 GPS BELL 214 214ST 1182106SW COCPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N 28106 GPS GIVES COMM FAILURE. 2G72 4U H10SW 20030818000632003081800063SW 2003 8 18 HEEA088552 120030724A7722212075067113 INDICATOR BELL 412 412 1182202SW ITT STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 STICKS WHEN ENGINE IS FIRST STARTED UNTIL ABOUT 45 PERCENT N1. SHOP REPAIR. 1G72 4U H4SW 20030819002202003081900220 2003 8 19 234TR0003 420030715A221013TX5315A SENSOR BOEING737 737228 13844AGNM AUTOPILOT MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 AUTO-PILOT A&B NEUTRAL SHIFT SENSOR OUT OF TOLERANCE PER ELEVATOR RIGGING BITE TEST. REMOVED, REPLACED, AND ADJUSTED NEUTRAL SHIFT SENSOR. OPS. CHECKS GOOD PER MM 22-11-122. 2L72 4F RTA16WE 20030820001482003082000148NM 2003 8 20 QXEA200300923 120030718A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 RIGHT HAND INBOARD NR 7 SEAT TRACK HAS LIGHT SURFACE CORROSION ON THE CENTER OF THE TRACK AT STATION 282.400. REPAIRED IAW DHC-8 SRM 51-40-11, 51-20-31 AND RD 8-53-4473. 2H72 4T RTA13NM 20030401000462003040100046SO 2003 4 1 C2XA03SH082 120030331A531014521725013 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK FOWARD SILL HAS CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND MADE A DOUBLER REPAIR ON AFFECTED SILL IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030401001582003040100158WP 2003 4 1 DHL2003804668 120030117A57005769584502 DOOR DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING L/E OUTBD. SLOT DOORS SHOW .5000 CRACKS ON THREE SECTIONS BETWEEN STA. 435.789 - XS520.168 REMOVED DAMAGED L/E SLOT DOORS IAW MM 27-80-2 PG. 201-203 PERFORMED NEW HOLESAND COUNTERSUNK IAW SRM 51-1-22 FIG. 476 . INSTALLED NEW SLOT DOORS ON THE THREE SECTIONS BETWEEN STA. XS 435.789 AND XS520.168 IAW MM. 2L74 4F RT4A25 20030821001002003082100100NM 2003 8 21 03FDEA01156 120030728A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 DAMAGED FASTENER HOLE ON FRAME AT BS 1070, LBL 22, WL 152. DAMAGED FASTENER HOLES ON FRAME AT BS 1070, LBL-22, WL-152 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGED MATERIAL AND REPAIRED IAW SRM5 1-40-3, FED- EX EA 7-5310-54913. 2L73 4F RTA3WE 20030328000352003032800035SO 2003 3 28 C2XA03CL078 120030326A2530500064001 COFFEEMAKER EMB 135 EMB135ER 3260203SO GALLEY SHORTED A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714505 145192 LGA FLIGHT 2827 THE CREW REPORTED A ELECTRICAL ODOR COMING FROM THE COFFEEMAKER. MAINTENANCE REPLACED THE NR 1 COFFEEMAKER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030404000122003040400012SO 2003 4 4 C2XA03BT047 120030403A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711535 145518 DURING ROUTINE INSPECTION ON OVERNIGHT, MAINTENANCE FOUND THE SERVICE DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LAMP AT SERVICE DOOR EMERGENCY LIGHT IAW EMB145 MM 33-50-10. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20030408001072003040800107CE 2003 4 8 2003F00214 120030211A76036715190 THROTTLE CESSNA750 750 2076810CE COCKPIT STUCK A UG8AO OTHER F FLT CONT AFFECTED LDLANDING 1 GL235113 7500013 AFTER LANDING AT CYYZ, THE RIGHT THROTTLE THRUST REVERSER LEVER WOULD NOT STOW. LEVER STUCK IN THE UP POSITION. ADJUSTED RIGHT THRUST REVERSER LEVER DETENT IAW CESSNA CITATION 750 MM. OPERATIONAL CHECK OF RIGHT THRUST REVERSER, THRUST REVERSER LEVER AND RIGHT THROTTLE WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030416000852003041600085NM 2003 4 16 SWAA030779 120030407A32106546113 TRUNION PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LEFT AND RIGHT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030416000042003041600004 2003 4 16 SWIA200311665 420030101A3415 WARNING SYSTEM EMB 120 EMB120ER 3260203SO COCKPIT FALSE ACTIVATIONA SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07207SW 120266 HIGH SPEED WARNING ON TAKEOFF AT 60 KIAS. ABORTED TAKEOFF. THIS HAPPENED TWICE. PERFORMED TEST PROCEDURES FOR BOTH AIRSPEED INDICATORS AND OVERSPEED WARNINGS. ALL READINGS CORRECT AND OPS CHECK GOOD PER 34-12-01. 2L72 4T RTA31SO 20030416001442003041600144NM 2003 4 16 PCAA0303062 120030331A5320853411420109 ANGLE DHAV DHC8 DHC8102 2809003NM NLGWW CRACKED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13809EX29292 302 DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING A INSPECTION TASK 5340/01 NOSE LANDING GEAR WELL RT ZEE MEMBER AT STATION X97, NOSE LANDING GEAR WELL TRUNNION RIGHT SIDEWALL WEB AND SIDEWALL ANGLE AT STATION X101 WERE FOUND TO BE CRACKED. CRACKS WERE REPAIRED IN ACCORDANCE WITH DEHAVILLAND DASH 8 REPAIR DRAWINGS RD8-53-764, RD8-53-458, AND RD8-53-3630. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424000732003042400073NM 2003 4 24 UPS03440334 120030308A5310 DOOR FRAME BOEING747 747200 1384847NM R5 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, R5 DOOR FWD LOWER CORNER CRACK FOUND AT VERTICAL RADIUS AS MARKED. LWR CORNER REPAIRED AS PER SRM 52-10-02 FIG 10. 2L74 4F RTA20WE 20030425000962003042500096NM 2003 4 25 KPVA200312 120030228A256010005511 LIGHT DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE COCKPIT INOPERATIVE A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13806WP4 357 COCKPIT PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT PORTABLE EMERGENCY LIGHT IAW MM. OPS CHECKED GOOD. 2H72 4T4 TRTA13NM E20NE 20030424000632003042400063NE 2003 4 24 NAFA20030001 220030321A7421AUBURN283 SPARK PLUG DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE ENGINE OVERHEATED I N32BEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL017780B379 379 45372 NK510771 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING. REPLACED NR 18 CYLINDER FRONT AND REAR SPARK PLUGS. 2L74 4R4 R 6A3 5E8 20030428001732003042800173WP 2003 4 28 03FDEA00402 120030408A5248 SEAL DOUG DC10 DC1030 3023501WP TAILCONE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 TAIL CONE AFT END OF LT PATIO DOOR, 13 INCH METAL CLOSEOUT SEAL IS WORN, UPPER TO LOWER SURFACE. CLOSING ACTION ON 04/07/03. REMOVED CLOSEOUT STRIP SEAL LWR AFT END OF LT PATIO DOOR IAW SRM 51-31-01. FAB NEW CLOSEOUT STRIP SEAL PER TRAVELER T2/325001. INSTALLED CLOSEOUT STRIP SEAL PER SRM 51-31-01. 2L73 4F A22WE 20030430000232003043000023NM 2003 4 30 AWXA200300446 120030414A5320654797321 WEB BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON LT HORIZONTAL SHEAR WEB JUST AFT OF BS 616, AT WL 207.5. MAINTENANCE FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 51-40-2, FIG. 1, PG. 1-3. 2L72 4F RTA16WE 20030430001752003043000175NM 2003 4 30 SWAA030904 120030421A2910AS118G0194CTR LINE BOEING737 7373G7 1384595NM HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29690SW 23783 AIR TURNBACK, DECLARED EMERGENCY. LOST B-SYSTEM HYDRAULIC FLUID CAUSING FAILURE OF B-SYSTEM. FOUND, HYD LINE LEAKING FROM ACOUSTIC FILTER TO PRESS B-MODULE. REMOVED AND REPLACED HYD LINE FROM ACOUSTIC FILTER TO PRESS B-MODULE PER MM. 2L72 4F RTA16WE 20030501002152003050100215NM 2003 5 1 2003F00244 120030212A3610652244143 MANIFOLD BOEING727 727222 1384073NM NR 2 ENGINE CRACKED A RYNAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE077638U 19911 DURING CLIMB-OUT AT KANSAS CITY, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND HORN SOUNDED. EMERGENCY CHECKLIST FOLLOWED. ENGINE WAS SHUTDOWN AND NR 1 FIRE BOTTLE DISCHARGED. AIRCRAFT RETURNED TO KANSAS CITY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 13 STAGE MANIFOLD IAW MM. (M) 2L73 4F A3WE 20030501000832003050100083SW 2003 5 1 2003F00236 120030102A5270 WARNING LIGHT FRCHLDSA227 SA227DC 3377521SW CARGO DOOR FALSE ACTIVATIONA BSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM05453LA DC852B FLT 1411 - OLM - CARGO DOOR LIGHT CAME ON DURING CLIMB. CREW RETURNED TO STATION. NO MECHANICAL PROBLEM WERE NOTED. DOOR WAS OPENED, SHUT AND RELATCHED. NO PROBLEM WAS NOTED. FLIGHT WAS CONTINUED WITH NO FURTHER PROBLEMS. (M) 2L72 4T RTA18SW 20030501001202003050100120WP 2003 5 1 ASAA0380099 120030123A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01977AS 53453 PDX - OVERHEAD EMERGENCY SPOT LIGHT FOUND INOPERATIVE AT ROW 8-12. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK, B5-101. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030501001712003050100171NM 2003 5 1 ASAA0310063 120030301A5320656739314 WEB BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AFT AIRSTAIR TORQUE BOX WEB AT BS 947-967, LEFT BUTTOCK LINE 50 CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM. (M) 2L72 4F RTA16WE 20030502002782003050200278NM 2003 5 2 SWAA030857 120030415A32106546113 PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030506001102003050600110EA 2003 5 6 03113624 120030423A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030502002482003050200248NM 2003 5 2 2003UALA00366 120030405A3310 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NAVIGATION PANELBURNED OUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29656UA 25394 BOTH RED NAV LIGHTS ON LEFT WING ARE OUT. CLEANED CONNECTOR, REPLACED BOTH NAV LIGHTS. 2L72 4F4 FRTA1NM E24NE 20030507001222003050700122EA 2003 5 7 CA030419001 120030307A29106017523843 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYDRAULIC SYS CHAFED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) AT FLIGHT LEVEL 33000, YELLOW CAS MESSAGE, HYD NR 2 LOW PSI ILLUMINATED.REF /A/ - IPC 29-11-00, ITEM35, P/N 601-75238-43, HYD PUMP PRESS SYS 2 TUBE ASSYREF /B/ - IPC 29-11-00, ITEM 215, P/N 601R75286-51, CASE DRAIN SYS 2 TUBE ASSYIT WAS FOUND BY THE MAINTENANCE, THAT TUBE ASSEMBLY REF /A/ AND /B/ HAD CHAFED TOGETHER AT THE 90 DEGREE BEND.IN ADDITION, IT WAS ALSO NOTED THAT THE BLOCK FAIRLEADS WERE WORN.TUBE ASSEMBLIES AND THE THREE SETS OF BLOCK FAIRLEADS WERE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20030508001322003050800132SO 2003 5 8 LR7A03043 120030428A3350PR2 LAMP LKHEED382 382G 526414USO EMERGENCY LIGHT INOPERATIVE A LR7AO OTHER O OTHER NRNOT REPORTED 1 AL03401LC 10 4606 FLIGHT CREW REPORTED CREW ENTRANCE EMERGENCY EXIT LIGHT INOP. REPLACED LAMP ASSEMBLY. OPS CKS GOOD IAW SMP 581 33-50. LP 11710, ITEM 4. 2H74 4T A1SO 20030509001642003050900164NM 2003 5 9 USAASB03047 120030401A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US 23987 TPA - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, AT THE FORWARD RIGHT CABIN, WILL NOT HOLD A CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030509000882003050900088EU 2003 5 9 A6WA200360023 120030425A5755 SKIN BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA AIR BRAKE DENTED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31290UE E2080 DENTS OUT OF LIMITS ON THE RT AIR BRAKE. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584-6900003. 2H74 4F4 F A49EU E6NE 20030513001582003051300158WP 2003 5 13 0300829955 120030418A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN PRESSURE MALFUNCTIONED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01922RW 47182 LOST CABIN PRESSURIZATION AT FL 310. CREW PERFORMED AN EMERGENCY DESCENT TO FL 190 WHERE THEY WERE ABLE TO REGAIN CONTROL OF CABIN PRESSURE WHEN "CROSSFEED VALVES" WHERE CLOSED. ANTI-ICE WAS FULL ON, CABIN ALTITUDE REACHED 11,000 FEET AND MASKS DID NOT DEPLOY. LANDING AT AUS WAS WITHOUT INCIDENT. MAINTENANCE CHECKED FOR VESSEL LEAKS AND PERFORMED BITE ON THE PRESSURE CONTROLLER, BOTH HAD NO TROUBLE FOUND. 2L72 4F A6WE 20030509000202003050900020EU 2003 5 9 A6WA200360005 120030410A7603251561 CABLE BAC 146 146300A 1500267EU UPPER PYLON UNSERVICEABLE A A6WAO OTHER O OTHER CRCRUISE 1 GL31616AW E3145 NR 2 THRUST LEVER WILL NOT MOVE BELOW CRUISE AT 31K (31,000 FEET), OK AFTER 14K (14,000 FEET). REMOVED AND REPLACED UPPER PYLON TELEFLEX CABLE. ON INSPECTION OF THE UNSERVICEABLE TELEFLEX CABLE. CONFIRMED THAT A CRIMP ALONG THE LENGTH OF THE CABLE CAUSED IT TO BIND, POSSIBLEY CAUSED DURING MAINTENANCE. NO OTHER ADVERSE CONDITIONS OR TRENDS NOTED. (M) 2H74 4F RTA49EU 20030513000452003051300045SO 2003 5 13 SWIA200311953 120030505A5220 SEAL EMB 120 EMB120ER 3260203SO EMERGENCY EXIT CONTAMINATED A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07236SW 120312 AIRCRAFT DID NOT PRESSURIZE ON TAKEOFF. TRIED BOTH AUTO AND MANUAL. RETURNED TO SLC. CLEANED DEBRIS FROM THE SEAL AROUND THE LEFT OVERWING EXIT. PRESSURIZED THE AIRCRAFT. BOTH AUTO AND MANUAL PRESSURE CHECKS GOOD. 2L72 4T RTA31SO 20030602000942003060200094NM 2003 6 2 SWAA031186 120030528A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 500C, STR 24R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030602001792003060200179NM 2003 6 2 AALA20030521 120030503A3350 SOCKET BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21755AN 30263 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 43C INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SOCKET T 43C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030605000572003060500057NE 2003 6 5 C8GA20030013 220030513A7321 FUEL CONTROL BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE NR 2 ENGINE OUT OF ADJUST A C8GAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO1589427 21365 666201 FLIGHT 717 FROM ELP TO STL. THE NR 2 ENGINE WOULD NOT ACHIEVE TAKE-OFF POWER. TAKE-OFF WAS STOPPED, AIRSPEED HAD NOT COME OFF "PEG" AT THE TIME TAKE-OFF WAS STOPPED AND ONLY MINIMAL BRAKES WERE USED. AIRCRAFT RETURNED TO BLOCKS WITHOUT INCIDENT. PERFORMED ENGINE RUN-UP TO TAKE-OFF POWER ON NR 2 ENGINE, ACCOMPLISHED FUEL CONTROL TRIM ADJUSTMENT IAW MM 71-00-30. OPERATIONAL CHECKS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20030605000092003060500009NM 2003 6 5 AUS20030434 120030424A29127592113101 FILTER BOEING737 73776N 13844CHNM GE CFM56 CFM56* 13802NE HYD SYSTEM FAULTY W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) HYDRAULIC RESERVOIR PRESSURE MODULE FILTER SUSPECT FAULTY. 2L72 4F4 FRTA16WE E2GL 20030606000672003060600067WP 2003 6 6 03FDEA00783 120030520A5753 VANE DOUG DC10 DC1010 3022110WP RT WING TE FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 RT O/B FLAP UPPER O/B UPPER SURFACE HAS TWO DEEP GOUGES. CLOSING ACTION OM 05/20/03. REMOVED AND REPLACED RT O/B FLAP VANE IAW M/M 27-50-03-2.OP'S CHECK TO BE ACCOMPLISHED ON W/C E-8-5750-7-5000 PT2. 2L73 4F A22WE 20030609000742003060900074EA 2003 6 9 QXEA0300626 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 15R, 3 INCHES AFT OF FS379. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030515000832003051500083NM 2003 5 15 C1HA200394009 120030509A2611 SMOKE DETECTOR BOEING727 727290 138408WNM CARGO BAY MALFUNCTIONED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15294AS 22146 AFT CARGO SMOKE DETECTOR LOOP-A FAULTS WHEN TESTED IN LOOP OR BOTH POSITIONS. 2L73 4F A3WE 20030520000162003052000016NM 2003 5 20 AMTA200300570 120030428A33508100022601 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 LIGHT INOPERATIVE ON EMERGENCY EGRESS TRACK AT SEAT 32C. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030515001192003051500119EA 2003 5 15 03118626 120030428A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27626BR 7225 DURING PREFLIGHT INSPECTION THE FLIGHT CREW DISCOVERED AN EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030609001822003060900182SO 2003 6 9 CA030501009 120030501A2750486597 DRIVE SHAFT PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA TE FLAP ASSY CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) RT FLAP FLEX CABLE WAS FOUND TO HAVE A CRACK ON THE SLINED SHAFT FROM THE PIN HOLE TO THE END OF THE DRIVE. THIS WAS DISCOVERED WHEN AD 82-27-13 WAS CARRIED OUT. REPLACED SHAFT DRIVE 1L72 3O3 O A20SO E14EA 20030617001072003061700107SW 2003 6 17 HEEA087289 120030611A6710 WASHER BELL 407 407 1182206SW ALLSN 250C 250C47B GL BELLCRANK DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH468 53209 BUFFER WASHER DISBONDED. TO BE SENT TO MFG. 1G71 3U3 UO H2SW E1GL 20030617001092003061700109EA 2003 6 17 QXEA200300732 120030610A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09610QX 10033 TUS- ON FLIGHT 2433 DURING FINAL AFTER GEAR SELECTED DOWN GOT SMOKE AFT LAVATORY WARNING MESSAGE. PERFORMED TEST OF LAVATORY SMOKE DETECTOR IAW 26-16-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030520000772003052000077GL 2003 5 20 UIEA200300021 120030430A21317757901 CONTROLLER BOEING747 747300 GL CABIN PRESSURE FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA1524837 24837 MIA/UIO - AIR TURNBACK, AFTER TAKEOFF, PRESSURIZATION INOPERATIVE. EXCESSIVE RATE OF CLIMB. WENT TO MANUAL. NO INDICATION OF FAILURE. NO RATE LIMIT LIGHT. FOUND BOTH OUTFLOW VALVES OPEN. UNABLE TO CONTROL PRESSURE MANUAL 'L' OR 'R'. NO FUEL DUMPED. REMOVED AND REPLACED THE PRESSURE CONTROLLER. SYSTEM OPS CHECK NORMAL IAW MM 21-31-02. (M) 2L74 4F RTA20WE 20030522000292003052200029WP 2003 5 22 GTIA030276 120030427A3260 UPLOCK DOUG DC9 DC981 3022081WP PWA JT8 JT8D NE MLG INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23818NK 48018 RED NOSE GEAR LIGHT ILLUMINATED BRIEFLY TWO TIMES APPROACHING SJU GEAR HANDLE WAS UP NO USUAL NOISE NOTED GEAR EXTENDED NORMALLY. PERFORMED BITE TEST ON PSEU OF NOSE GEAR UPLOCK, CLEANED SENSOR OF EXCESS GREASE, CHECKED CONNECTOR AND WIRING. OPS CHECK GOOD, NO FAULTS FOUND AT THIS TIME. 2L72 4F4 F A6WE E2EA 20030528000722003052800072WP 2003 5 28 AALA20030443 120030410A25601001191 FLASHLIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21294AA 49306 SEA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030618002122003061800212SW 2003 6 18 HEEA087165 120030609A3212206030104023 FITTING BELL 206 206L3 1182108SW MLG FLOAT CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 FITTING ASSY HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030620000862003062000086EU 2003 6 20 ASOA03221 120030502A5330 SKIN AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN BNA, THE CENTER BELLY SKIN BETWEEN FR 23D AND 24 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CORRODED CENTER BELLY SKIN BETWEEN FR 23D AND 24 BY FABRICATING AND INSTALLING A DOUBLER IAW SRM 51-21-42 AND SRM 53-00-00. (M) 2H72 4T RTA53EU 20030624000692003062400069WP 2003 6 24 AT0300017 120030612A3220 DOOR DOUG DC9 DC932 3022066WP NLG MALFUNCTIONED A ZZDAO OTHER O OTHER CLCLIMB 1 SO15836AT 47397 LOUD VIBRATION WHEN GEAR CAME UP. FOUND RT NLG DOOR HANGING DOWN. PERFORMED VISUAL INSPECTION OF DOORS AND HINGE AREA. NO DEFECTS NOTED. CLOSED NOSE GEAR DOORS PER STANDARD PRACTICES OUTLINED IN DC9 MM 32-00. DOORS REMAINED LOCKED NORMALLY. 2L72 4F A6WE 20030116000552003011600055GL 2003 1 16 HEEA083014 220030106A7230NAS1375A08SB062 DUCT BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL COMPRESSOR TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 ENGINE COMPRESSOR INDUCER BLEED DUCT TORN. SCRAPPED. 1G71 3U3 U H2SW E1GL 20030116000762003011600076SW 2003 1 16 HEEA083036 120030106A2430SM20ACD200A21 RELAY BELL 206 206L1 1182107SW DC SYSTEM STUCK E O OTHER O OTHER NRNOT REPORTED 1 SW035019F 45244 STUCK BATTERY RELAY. 1G71 3U H2SW 20030120000042003012000004 2003 1 20 249TR0012 420030113A22104038891916 COMPUTER BOEING737 7372K5 138448XNM A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 F/O's ADI & HSI will not self test in VOR or ILS. Removed & replaced FCCB computer. Ops checknormal per MM 34-31-0 and 22-11-01. Ops check good. 2L72 4F RTA16WE 20030120000072003012000007EU 2003 1 20 03019330 120030119A3350DM21 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27303UE 41015 During preflight inspection, the crew reported that the forward section of emergency floor track lighting was inoperative. Maintenance personnel installed a connector and pigtail for the forward emergency floor track lights. The aircraft was returned to service. 2L72 4T RTA41NM 20030304000322003030400032GL 2003 3 4 HE66084852 220030228A7413106149501 IGNITER BOX BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL NR 1 ENGINE DEFECTIVE H HEEAO OTHER O OTHER NRNOT REPORTED 1 FS01202LF 2014 CAE280089 NR 1 ENGINE WOULD NOT START, EXCITER BOX WAS NOT PUTTING OUT REPLACED 1G72 3U3 U H3AU E1GL 20030227000832003022700083 2003 2 27 HEEA084389 420030212A2300N0001552 ANTENNA BELL 407 407 1182206SW COMMUNICATIONS DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 WOULD NOT RECEIVE ANY SIGNAL. 1G71 3U O H2SW 20030228000992003022800099SW 2003 2 28 HEEA084461 120030213A243523081018 STARTER GEN BELL 206 206L1 1182107SW DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032764F 45279 STARTER GEN FAN HITTING SHROUD. IN SHOP FOR REPAIR. 1G71 3U H2SW 20030306001162003030600116EU 2003 3 6 03063330 120030304A33501317 LAMP JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 During maintenance it was discovered that the l/h fwd exterior emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the l/h aft exterior emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4T RTA41NM 20030307000872003030700087NE 2003 3 7 HEEA084888 120030227A261247320501 FIRE DETECTOR SKRSKYS76 S76A 8143006NE WILL NOT TEST E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03911MJ 760231 FIRE DETECTOR WILL NOT TEST PROPERLY. 1G72 3U H1NE 20030307001722003030700172NM 2003 3 7 AALA20030053 120030111A1430 NUT BOEING777 777223 1385213NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21779AN 29955 ORD - DURING OVERNIGHT MAINTENANCE, D3L EMERGENCY EXIT LIGHT INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT NUT AT D3L. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030313002292003031300229NM 2003 3 13 QXEA0300204 120030113A5712 RIB BOMBDRDHC8 DHC8401 1390041NM LT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 CKB- LEFT HAND WING CENTER LEADING EDGE FOUR CORNERS ARE CRACKED ON RIB. REPAIRED IAW HORIZON AIR EA 6-57-107. 2H72 4T RTA13NM 20030122000822003012200082 2003 1 22 HEEA083474 420030110A3452066107100 TRANSPONDER BELL 412 412 1182202SW ATC SYSTEM ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ATC TRANSMITS ERRATIC AND INTERROGATION PULSES WILL NOT NULL OUT. IN SHOP REPAIR. 1G72 4U H4SW 20030122001122003012200112NM 2003 1 22 DL72S030022 120030103A33501102833 LIGHT BOEING727 727225A 1384077NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO278891Z 21860 MID OVERHEAD EMERGENCY LIGHT INOP. REPLACED OVERHEAD LIGHT ASSY. 2L73 4F RTA3WE 20030327001142003032700114SO 2003 3 27 C2XA03CL035 120030208A26123601134480 FIRE DETECTOR EMB 135 EMB135ER 3260203SO NR 2 PYLON CHAFED A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2715509 145238 CLE FLIGHT 2116 THE CREW REPORTED A ENGINE NR 2 FIRE DETECT FAIL MESSAGE INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE PYLON FIRE DETECTOR ASSEMBLY. ALSO REPLACED THE NR 2 ENGINE FIRE CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030318000892003031800089WP 2003 3 18 ASAA0380026 120030104A575339195832 FITTING DOUG DC9 DC983 3022083WP RT WING TE FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP VANE NR 5 FITTING IS WORN. REPLACED FITTING PER CMM 27-50-02. (M) 2L72 4F RTA6WE 20030624000282003062400028WP 2003 6 24 EIA2003080 120030430A5310 DOOR FRAME DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09915F 47061 PER N5349, LT ENTRY DOOR JAMB AFT STOP 4, BS 200 CRACKED AT DOOR STOP HOLE. REMOVED DAMAGE, INSTALLED, FABRICATED DOUBLERS & FILLERS PER SRM 53-05, PGS 546, 551, 552. REPEAT INSPECTION PER W/C N5343 AT OR BEFORE 28,000 CYCLES. 2L72 4F A6WE 20030702000012003070200001NM 2003 7 2 AMTA200300772 120030613A3350 LENS BOEING737 73783N 13844HINM EMERGENCY LIGHT CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11313TZ 32580 EMERGENCY EXIT LENS FORWARD OF R1 DOR CRACKED. REPLACED LIGHT ASSEMBLY PER AMM 33-51-01, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030716001072003071600107 2003 7 16 HEEA088035 420030702A2312064102300 TRANSCEIVER SKRSKYS76 S76A 8143006NE VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 VHF TRANCEIVER HAS GARBLED TRANSMISSION. SHOP REPAIR. 1G72 3U H1NE 20030708000312003070800031WP 2003 7 8 IXXA0300045O 120030626A32223615977 MECHANISM DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE MLG BROKEN A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11828BX80986849 45993 AFTER TAKEOFF AND GEAR RETRACTION, CREW EXPERIENCED A VIBRATION AND NOISE COMING FROM NOSE GEAR AREA. THE CREW ELECTED TO RETURN BASE. MAINTENANCE FOUND GROUND SHIFT ARM BROKEN. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED GROUND SHIFT MECHANISM, THEY ALSO FOUND THE NOSE WHEEL STEERING OUT OF RIG. NOSE WHEEL STEERING WAS RIGGED, OPERATIONAL CHECK GOOD. ALL WORK PERFORMED IAW APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20030709000812003070900081EU 2003 7 9 MALA030288 120030529A243023080031 GENERATOR SAAB SF340 340B 7860101EU LEFT MALFUNCTIONED A MALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL15424XJ 340B424 DURING FLIGHT 3145, LEFT DC GEN FELL OFF LINE. AIR RETURN TO MSP. MAINTENANCE REPLACED LEFT GENERATOR P/N 23080-031, S/N OFF 7182, S/N ON 3406 IAW MAL JC 243103. 2L72 4T RTA52EU 20030401001752003040100175WP 2003 4 1 DHL2003806001 120030102A2497 CONTROL PANEL DOUG DC8 DC873F 302199FWP COCKPIT SPARKS A DHLAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01806DH 46002 ON THE TAXI WAY JUST PRIOR TO T/O A/C EXPERIENCED SPARKS AND SMOKE FROM OVERHEAD PANEL. EXECUTED EMERGENCY PROCEDURE AND RETURNED TO BLOCKS. 2L74 4F RT4A25 20030103000432003010300043SO 2003 1 3 C2XA03CL001 120030103A33501317 BULB EMB 135 EMB135LR 3260305SO CABIN BURNED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2724517 145332 DURING 3A INSPECTION THE AFT AISLE EMERGENCY LIGHT WAS NOT ILLUMINATING IN THE TEST MODE. MAINTENANCE REPLACED THE AFT AISLE EMERGENCY LIGHT,IT THEN TESTED GOOD. 2L72 4F RTT00011AT 20030127000982003012700098EA 2003 1 27 COMA0360043 120030126A53116003603332 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FS718 CRACKED A COMAO OTHER O OTHER ININSP/MAINT 1 SO01967CA16115 7134 RIGHT FS 718 DOUBLER CRACKED BETWEEN STRINGERS 10 AND 12.REPLACED DOUBLER I/A/W BOMBARDIER REO 601R-53-61-193A. 2L72 4F RTA21EA 20030129000512003012900051SW 2003 1 29 HEEA083964 120030117A5320407023800136A DOUBLER BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH 53278 FUSELAGE DOUBLER IS CRACKED. 1G71 3U O H2SW 20030218001892003021800189NM 2003 2 18 QXEA0300181 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 5 SEAT TRACK HAS SCRATCHES AT STATION 500-515. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030116000122003011600012 2003 1 16 HEEA082969 420030107A3416212070238003 INDICATOR SKRSKYS76 S76A 8143006NE ALTIMETER SLUGGISH E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03762P 760060 ALTIMETER INDICATOR IS SLUGGISH. IN SHOP REPAIR. 1G72 3U H1NE 20030116000452003011600045 2003 1 16 HEEA083004 420030106A3416D120P2T ANEROID BELL 206 206L3 1182108SW TCAS SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 TCAS FAILED ERROR CODE 020 BAROMETRIC ALTITUDE INPUT. 1G71 3U H2SW 20030224000652003022400065 2003 2 24 HEEA084186 420030212A2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 CAUSES BLEED OVER FROM AFT CABIN ICS TO PILOT AND COPILOT STATIONS. IN SHOP REPAIR. 1G72 3U H1NE 20030227000952003022700095 2003 2 27 HEEA084399 420030212A2340PM212302 SWITCH BELL 407 407 1182206SW CYCLIC STICK STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 ICS/RADIO SWITCH STICKS IN CLOSED POSITION. 1G71 3U O H2SW 20030304000512003030400051SW 2003 3 4 HEEA084582 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z2772 A2372 36019 MAIN ROTOR MAST LINK HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030307000772003030700077NM 2003 3 7 SWAA030491 120030304A5552183A1340 FITTING BOEING737 7377H4 1384404NM LT/RT ELEV WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 DURING SCHEDULED 5Y CHECK, FOUND EXCESSIVE PLAY AT BOTH LT AND RT ELEVATOR NR 4 ATTACH HINGE POINTS. REMOVED AND REPLACED BOTH NR 4 ELEV HINGE FITTINGS PER MM. 2L72 4F RTA16WE 20030310000352003031000035SW 2003 3 10 HEEA084944 120030227A7120212061117001 TUBE BELL 412 412 1182202SW ENGINE MOUNT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 TUBING OPENING IS TOO LARGE FOR BEARING DIAMETER. REPAIRED. 1G72 4U H4SW 20030311000672003031100067SW 2003 3 11 IO5R084696 120030224A31107886643 INDICATOR CLARK 1000 1000CLARK 2230102SW COCKPIT MALFUNCTIONED H IO5RO OTHER O OTHER NRNOT REPORTED 1 FS01120KJ125 1185 BACKLIGHTING INOP REMOVED AND REPLACED. 1Q71 3R 2A6 20030313000922003031300092EA 2003 3 13 A5O2003F00000 220030303A853060828 PISTON PIN PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA ENGINE WRONG PART B A5ORK NONE W INADEQUATE Q C ININSP/MAINT 1 SO091475X118 287525296 L4141127A DURING 100 HOUR INSP OF A/C, DISCOVERED NR 1 CYL COMPRESSION WAS READING 25/80 AND OIL FILTER CONTAINED AN EXCESS AMOUNT OF ALUMINUM SHAVINGS. NR 1 CYL WAS REMOVED FROM SERVICE TO INVESTIGATE REASON FOR LOW COMPRESSION AND EXCESS ALUMINUM IN THE FILTER. NR 1 CYL EXHAUST VALVE, GUIDE AND SEAT WERE ALL WORN BEYOND LIMITS. PISTON PIN PLUGS SHOWED SIGNS OF WEAR AND SCUFFING ON CYL WALLS. BOREASCOPE INSP OF OTHER 3 CYL SHOWED SIGNS OF SIMILAR SCUFFING. INVESTIGATION REVEALED PISTON PIN PLUG (PN 60828) WERE USED WITH CHROME CYLINDERS. MFG PARTS LISTS IDENTIFIES PISTON PIN PLUGS(PN 72198) TO BE USED WITH CHROME CYL. ASSY. PROB CAUSE: FAILURE OF O/H FACILITY TO USE AND FOLLOW MFG. PARTS AND O/H INSTRUCTIONS. 1L71 3O3 O 2A13 E274 20030120000132003012000013WP 2003 1 20 MWEA030039 120030120A522039146641 SEAL DOUG DC9 DC932 3022066WP OVERWING EXT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 LOWER SEAL ON LEFT FORWARD OVERWING EMERGENCY EXIT DOOR IS CORRODED. -- LOCATED AND INSTALLED NEW SEAL RETAINER. 2L72 4F A6WE 20030324000422003032400042NM 2003 3 24 751PA0011 120030119A3350 BULB BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05751PA 23928 BULB INOPERATIVE IN L3 EMERGENCY LIGHT. REMOVED AND REPLACED BULB. OPS CHECKED GOOD. 2L72 4F RTA2NM 20030314001402003031400140WP 2003 3 14 GTIA030117 120030227A3260 SENSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE MLG CONTAMINATED A GTIAO OTHER O OTHER CLCLIMB 1 GL23826NK 49391 LANDING GEAR RETRACTED NORMALLY THEN DURING CLIMB NOSE GEAR LITE ILLUMINATED. GEAR RECYCLED IAW QRH PROCEDURE. RED LIGHT WENT OUT. NOSE GEAR RED WARNING LIGHT ILLUMINATES OCCASIONALLY IN FLIGHT BELOW 210 KNOTS WHEN GEAR LIGHT DO NOT ILLUMINATE. FOUND LARGE GREASE DEBRIS ON NOSEGEAR UP POSITION SENSOR AND INTERLOCK SWITCH ROLLER. CLEANED DEBRIS AND NO FURTHER DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF NOSE GEAR UP LOCK SENSOR, FOUND OK, PERFORMED OPS CHECK. OPS CHECK OK AND OK FOR CONTINUED SERVICE. 2L72 4F4 FRTA6WE E2EA 20030314001762003031400176CE 2003 3 14 WVE2003F00003 120030120A27206622500001003 SENSOR LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP RUDDER FORCE INOPERATIVE B WVERO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA09427FX 163 DURING POWER UP BY FLIGHT CREW; THE FLIGHT CREW REPORTED RIGHT RUDDER FORCE EXISTS WITH AMBER LIGHT (RUDDER BOOST) ILLUMINATED, PEDAL FORCE STOPS WHEN LEFT RUDDER FORCE IS APPLIED. 2L72 4F4 FRTT00008WIE6WE 20030317001612003031700161CE 2003 3 17 048044 120030220A522012953008656 SKIN BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA EMERGENCY EXIT DELAMINATED A AMWAO OTHER O OTHER APAPPROACH 1 CE07133YV UE133 WHILE INBOUND FROM PONCA CITY, OKLAHOMA TO ENID OKLAHOMA ON FLIGHT 2501, SEAT 4F EMERGENCY EXIT OUTER SKIN PEELED OFF AND DEPARTED FROM THE AIRCRAFT WHILE INFLIGHT. THE CREW DECLARED AN EMERGENCY LANDING. THERE WAS NO FURTHER INCIDENT. MAINTENANCE FOUND HOLES IN VERTICAL FAIRING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT DOOR. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T3 TRTA24CE E2NE 20030317001662003031700166EU 2003 3 17 AWXA200300275 120030304A5315D53371090002 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-03 CHECK A 1 5/8 CRACK WAS FOUND ON CABIN FLOOR SUPPORT BEAM FR 47, Y 254. MAINTENANCE CUTOUT DAMAGED AREA OF CABIN FLOOR SUPPORT BEAM FR 47, Y 254; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW AWA E.R. 26-5330-03075-GFI. 2L72 4F RTA28NM 20030319000822003031900082 2003 3 19 RU3A03001 420030110A3400 MOTOR BEECH 300 300BEECH 1152930CE IRU BLOWER ROUGH A RU3AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2167 FF2 CREW NOTICED OFFENSIVE ODOR IN COCKPIT AND CABIN. NO SMOKE WAS PRESENT. CREW ABORTED FLIGHT. MECHANIC WAS SENT TO LOCATION, ENGINES WERE RAN AND ALL POWER ON AND COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO HOME STATION AND AVIONICS FOUND THAT THE IRU BLOWER MOTOR WAS EXTREMELY HOT. WHEN MOTOR WAS REMOVED AND SHAFT TURNED ROUGH AND COULD SEIZE. MOTOR WAS REPLACED AND NO FURTHER PROBLEMS WERE ENCOUNTERED. (M) 2L72 4T A24CE 20030327000812003032700081 2003 3 27 C1HA200397010 420030221A3442 TRANSCEIVER BOEING727 727270 138408PNM WX RADAR SYS FAILED A C1HAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15697CA 23052 ENROUTE, WX RADAR DID NOT PAINT WEATHER (DIVERSION) REPLACED RADAR R/T AND OPS CHECK GOOD PER MM 34-41-0 2L73 4F RTA3WE 20030327001102003032700110SO 2003 3 27 C2XA03CL027 120030203A5610163500112 WINDSHIELD EMB 145 EMB145ER 3260211SO COCKPIT FAILED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW2714930 145011 CLE FLIGHT 2067 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD SHATTERED IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030327001392003032700139SO 2003 3 27 C2XA03IA004 120030111A2131792185A010100 CONTROLLER EMB 145 EMB145 3260210SO CABIN PRESSURE INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2718114 145664 DURING CLIMBOUT THE CREW NOTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE. THE CREW DECLARED EMERGENCY, RETURNED TO IAH AND LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE DIGITAL CONTROLLER, PERFORMED A OPERATIONAL CHECK AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030325000222003032500022NM 2003 3 25 AWXA200300137 120030125A5315146N5111 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM FORWARD UPPER T CAP BS 1681.8, AT NUT CLIP ATTACH POINTS FROM CUSP TO CUSP. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED FLOORBEAM FROM BS 1660 TO BS 1681; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG 146N5111; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-20, PG. 10-12. 2L72 4F RTA2NM 20030324001202003032400120EU 2003 3 24 03082309 120030323A3350S34C12ST6S0S0 LIGHT JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27309UE 41022 During preflight inspection, the crew reported that the emergency floor track lighting from the main cabin door to seat row 3 was inoperative. Maintenance personnel removed and replaced the first and second emergency floor track light strips. An operational check was satisfactory and the aircraft was returned to service. 2L72 4T RTA41NM 20030418000012003041800001NM 2003 4 18 P5CA0300764 120030207A2150 A/C PACK BOEING747 74746NF 13848BTNM COCKPIT ODOR A P5CAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP23451PA 30809 DURING CRUISE OILY ODOR WAS NOTICED ON FLT DECK FOLLOWED BY LITE SMOKE FROM F/O'S AC VENT. AOM PROCEDURE COMPLIED WITH, A/C DESCENDED TO FL29 AS A PRECAUTION WITH CREW ON 02. SMOKE CLEARED FOLLOWING COMPLETION OF PROCEDURE WITH INTERMITTANT INCREASED ODOR. PERFORMED INSPECTION FOR OIL CONTAMINATIONS AS PER MM 21-00-01-802, NO OIL FOUND IN DUCTS PER PACK 1, 2, 3 PER MM 21-51-05 -201. NO LEAKS OR FURTHER ODOR WITH 3 PACKS RUNNING. 2L74 4F RTA20WE 20030416003862003041600386CE 2003 4 16 DXTA200300004 120030110A7830CX783600463 CIRCUIT BOARD CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL THRUST REVERSER FAILED E DXTAO OTHER O OTHER LDLANDING 1 GL07920QS413 7500120 UPON LANDING THE LT THRUST REVERSER DEPLOYED, BUT THE HANDLE WOULD NOT LET THRUST GO ABOVE IDLE. 2L72 4J4 FRTT00007WITE6CH 20030417001162003041700116NM 2003 4 17 QXEA0300232 120030131A5420 SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX-RIGHT HAND LOWER COWL AFT CENTER SUPPORT WEB LOWER ANGLE IS CRACKED. REPAIRED IAW RD8/4-71-016. 2H72 4T RTA13NM 20030421000532003042100053NM 2003 4 21 QXEA0300309 120030301A2612 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09358PH 506 RDM ON FLIGHT 2086- FAULT A ILLUMINATED ON NR 2 FIRE DETECTION. CYCLED CIRCUIT BREAKER NR 2 FIRE DETECTION H7. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030418000882003041800088NM 2003 4 18 F3LA200300059 120030201A5320 STRAP BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD DOOR FRAME RADIUS STRAP CORRODED AT STA 794.3, STR 25-R. FOUND CORROSION OUT OF LIMITS PER SRM 53-16-15, FIG 101. REPLACED RADIUS STRAP PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20030327000602003032700060NM 2003 3 27 C1HA200384002 120030219A2611 FIRE DETECTOR BOEING727 7272S7 138407ZNM CARGO BAY MALFUNCTIONED A C1HAO OTHER N FALSE WARNING DEDESCENT 1 GL15684CA 22491 DURING DESENT INTO DESTINATION (GGG) APPROX 60 MILES 20,000 FEET, THE CARGO SMOKE FIRE DETECTION SYSTEM FOR AFT CARGO COMPARTMENT SOUNDED BELL AND LIGHT ACTIVATED. A FEW SECONDS AFTER BELL WAS SILENCED ALL LIGHTS EXTINGUISHED . THIS REPEATED TWICE AN OUR APPROACH. VISUALLY INSPECTED AFT CARGO PIT SMOKE DETECTOR. NO DEFECTS NOTED. SYSTEM OPS CHECK NORMAL REF 26-15 OK FOR CONTINUED SERVICE. 2L73 4F A3WE 20030714001462003071400146EU 2003 7 14 HEEA088083 120030703A6720350A33214501 ROD AEROSPAS355 AS355* EU PITCH CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 MAIN ROTOR PITCH CONTROL ROD ELASTOMERIC BEARING RUBBER WORN. REPLACED. 1G72 3U H11EU 20030321000102003032100010SW 2003 3 21 2003F00150 120030319A2742DL5040M5 ACTUATOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP HORIZONTAL TRIM DEFECTIVE E O OTHER F FLT CONT AFFECTED CLCLIMB 1 GL27340AE 479 AC510 HORIZONTAL TRIM ACTUATOR WOULD NOT ACTUATE IN EITHER THE PILOT/CO-PILOT/AUX POSITION. FOUND ACTUATOR TO BE BAD. 2L72 4T3 TRTA8SW E2WE 20030321000692003032100069NM 2003 3 21 2003UALA00209 120030219A5754114W41101 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLAT NR 1 DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 TRAILING EDGE WEDGE, SLAT NR 1, DELAMINATED ON LOWER SURFACE. OUTBOARD END SEAL PLUG MISSING. REPAIRED TRAILING EDGE WEDGE. REPLACED OUTBOARD SEAL PLUG. 2L72 4F4 FRTT0001SE E46NE 20040226000112004022600011WP 2004 2 26 ASAA0380420 120030501A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 SEA - DURING PREFLIGHT CHECK FOUND EMERGENCY FLOOR TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. REPLACED SEGMENT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030828001132003082800113WP 2003 8 28 MWEA030273 120030710A36109267621 FLEX LINE DOUG DC9 DC932 3022066WP CABIN CRACKED A MWEABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL31207ME 47734 AT 35,000 FEET RED MASTER WARNING LIGHT ILLUMINATED ALONG WITH THE RED CABIN ANNUCIATOR, MASK DROPPED -- REPLACED COALESER BAG AND CLEANED BOTH WATER OUTLET SCEENS, ALSO PERFORMED A CABIN PRESSURIZATION CONTROL ADJUST, REMOVED AND REPLACED WATER SEPERATOR TEMPERTURE CONTROL VAVLE. REMOVED AND REPLACED CRACKED TUBE WITH TEMPORARY FLEX LINE, PLACED FLEX LINE ON CARRY OVER FOR REPLACEMENT AT LATER DATE. 2L72 4F A6WE 20030722001282003072200128NM 2003 7 22 AWXA200300653 120030324A53306545765 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-17 CHECK 6 EACH .0625 INCH CRACKS WERE FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 LT, BS 500D+4, BS 500D+13, BS 522, BS 523, BS 525, AND BS 527. MAINTENANCE CUT OUT CRACKED SKIN AT STR 4 LT BS 500D+4, BS 500D+13, AND FROM BS 518 TO BS 526; PERFORMED A HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH REPAIR DOUBLERS, 3 EACH FILLERS, AND 2 EACH INTERNAL DOUBLERS; INSTALLED REPAIR FROM BS 500D TO BS 530 IAW B737-300 SRM 51-40-02 PG 38 FIG 8 AND SRM 53-00-01 PG 362 FIG 228. 2L72 4F RTA16WE 20030806001022003080600102SO 2003 8 6 C2XA03SH218 120030711A541014576631621 STIFFENER EMB 145 EMB145LR 3260212SO NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 DURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001592003080600159NM 2003 8 6 AWXA200300831 120030709A5315D53472188202 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM Y1292 FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-44-11, PG 9, 13, 28-30, & 39-40, FIG 12. 2L72 4F RTA28NM 20030902001232003090200123NM 2003 9 2 PCAA0307080 120030705A33506104789 BATTERY PACK DHAV DHC8 DHC8102 2809003NM POSITION NR 3 DISCHARGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13851EX 343 DURING ROUTINE MAINTENANCE VISIT THE FORWARD AND THIRD LIGHT BACK ON CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. POSITION NUMBER 3 EMERGENCY LIGHT BATTERY WAS REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030812000772003081200077SW 2003 8 12 HEEA088617 120030728A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149819183 36003 STARTER GEN MAKING NOISE. 1G72 4U H4SW 20030813001792003081300179NM 2003 8 13 SWAA031689 120030728A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030728001212003072800121EA 2003 7 28 COMA0360309 120030702A7931 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE DIRTY A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01806CA 7359 FLIGHT 3046 RECEIVED A LEFT ENGINE OIL PRESSURE CAUTION DURING TAKEOFF, ABORTED AND RETURNED TO THE GATE. REMOVED, CLEANED AND REINSTALLED THE LEFT ENGINE OIL PRESSURE TRANSDUCER. 2L72 4F RTA21EA 20030822001522003082200152NM 2003 8 22 QXEA200300941 120030730A2497 WIRE DHAV DHC8 DHC8202 2809007NM ELECTRICAL SYS CHAFED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09359PH 514 SEA- ON FLIGHT 2038 BOTH LEFT AC BUS AND RIGHT AC BUS CAUTION LIGHTS ILLUMINATED WHEN PROPELLERS WERE SELECTED. SLIGHT ELECTRICAL SMOKE SMELL DETECTED. REPAIRED TWO CHAFED WIRES LEADING INTO AIRCRAFT EXTERNAL POWER RECEPTICAL WITH ENVIRONMENTAL SPLICES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030910000532003091000053SW 2003 9 10 HEEA088921 120030821A6220206011149105 YOKE BELL 206 206L3 1182108SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FOUND RETAINER SPINNING IN GRIP RETAINING BORE DUE TO INSUFFICIENT AMOUNT OF PROSEAL AT TIME OF GRIP ASSY. FURTHER CAUSING INADEQUATE AMOUNT OF LUBRICANT TO BEARING JOURNAL AND BEARING RESULTING IN YOKE BEARING JOURNAL FAILURE AND BEARING ROLLOVER. SENT TO BELL HELICOPTER TEXTRON FOR WARRANTY REPAIR. 1G71 3U H2SW 20031001000772003100100077NM 2003 10 1 2003UALA00715 120030924A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29369UA 24538 CABIN FLOORBEAM IS GOUGED AT STA 360 AND BL 0. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030909002352003090900235WP 2003 9 9 ABXA030315 120030716A5320J0602289 PAN DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 AREA BETWEEN AFT LOWER CARGO JAMB PAN AND FUSELAGE SKIN EXFOLIATED. LEVEL I BETWEEN FS 904 AND 917. SPLICED IN NEW SECTION OF PAN IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030909002462003090900246EA 2003 9 9 ASOA03376 120030816A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A C-CHECK IN MCN, THE FLOORBEAMS AT LEFT ADN RIGHT 9 AND 27 BETWEEN FS 280 AND FS 409 PLUS 5 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOORBEAMS AT LEFT AND RIGHT 9 AND 27 BETWEEN FS 280 AND FS 409 PLUS 5 IAW ASA EO 600-53-0052. (M) 2L72 4F RTA21EA 20031006000542003100600054NE 2003 10 6 MEX2003409 220030905A7230815331 BLADE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE COMPRESSOR FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23881LF 53051 DURING TRANSIT CHECK WAS DETECTED, LT ENGINE DAMAGED BY FOD WITH 1 BLADE OUT OF LIMITS IN THE FAN. THE COMPRESSOR BOROSCOPIC INSPECTION TO 6TH AND 7TH STAGE WAS PERFORMED AND THE BLADE SET FAN WAS REPLACED IAW MM, ALL CORRECT. 2L72 4F4 FRT E9NE 20031002000712003100200071SO 2003 10 2 C2XA03TY148 120030910A322011700C000001 CAM EMB 135 EMB135ER 3260203SO NLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27165027745 7745 145166 DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR STRUT MAIN HOUSING AND LOWER CAM WERE FOUND TO HAVE AREAS OF CORROSION AND PITTING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR LEG ASSEMBLY IAW EMB MM 32-20-01, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031003000382003100300038NM 2003 10 3 AALA20030652 120030610A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21673AN 29423 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SOCKET DAMAGED AT ROW 18DEF. REPLACED EMERGENCY EXIT LIGHT SOCKET AT 18DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031020002922003102000292EU 2003 10 20 2003UALA00721 120030926A2120 COFFEEMAKER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GALLEY FAILED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29431UA 571 RETURN TO FIELD DUE TO ELECTRICAL ODOR IN CABIN. REPLACED COFFEEMAKER M11 IN FORWARD GALLEY. 2L72 4F4 FRTA28NM E40NE 20031119000602003111900060NE 2003 11 19 P5CA0300963 220031012A7311 VALVE BOEING747 74746NF 13848BTNM GE CF6 CF680 30025NE NR 3 ENGINE INACTIVE A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23450PA 30808 706200 AT PUSHBACK, NR 3 ENGINE DID NOT START. NO FUEL FLOW. REF DMI 31578. REACTIVATED NR 3 ENG FUEL VALVE. EICAS MESSAGE GROUND. NR 3 ENG STARTS, GROUND STARTS NORMAL, IAWMM 71-00-00. DMI CLEARED, PLACARDS REMOVED. 2L74 4F4 FRTA20WE E13NE 20031121000172003112100017NM 2003 11 21 SWAA032467 120031106A53126545866 PRESSURE PANEL BOEING737 7377H4 1384404NM WHEEL WELL CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED 5Y CHECK, FOUND LT AND RT WHEEL WELL CUTOUT AFT WEB DOUBLERS CRACKED. REMOVED AND REPLACED WEBS PER SRM. 2L72 4F RTA16WE 20030910000242003091000024EU 2003 9 10 BAQA087890 120030717A2140JBS8803 HEATER UROCOPEC135 EC135T1 5620026EU CABIN MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME170 132 WILL NOT OPEN WHEN HEAT IS SELECTED. PART LASTED ONLY 170.4 HOURS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031103000332003110300033NM 2003 11 3 DL738030891 120030930A5330143A32128 SKIN BOEING737 737832 13844CFNM FUSELAGE PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27394DA 30562 THE FUSELAGE SKIN WAS PUNCTURED BY FOD NEAR FS 500D AND STRINGER 23L. THE DAMAGE WAS REMOVED WITH A 11 X 9 INCH SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087373-14, REV A. 2L72 4F RTA16WE 20031103000352003110300035NE 2003 11 3 DLM90030893 220031001A732021SN04372 SWITCH DOUG MD90 MD9030 3023690NM IAE V2500 V2500A1 NE NR 2 ENGINE UNSERVICEABLE A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27914DN 53394 200454 RIGHT FUEL PRESSURE LIGHT ILLUMINATED ON TAKEOFF ROLL. REPLACED FUEL FILTER AND PRESSURE SWITCH PER MAINT MANUAL. 2L72 4F4 FRTA6WE E311NE 20031103001372003110300137EA 2003 11 3 SWIA200312477 120031002A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 PAX DOOR OUTER HANDLE IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) OUTER HANDLE REMOVED AND REPLACED IAW CRJ AMM 52-11-03. P/N: 601R31763-1 2L72 4F4 FRTA21EA E15NE 20031106000822003110600082WP 2003 11 6 UPS03841510 120031025A532037540231N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 A-PIT DOOR CUTOUT FITTING CRACKED I/B OF NR 5 T-BOLT FITTING AT STA 320. REMOVED, REPLACED AND INSTALLED NEW T-BOLT FITTING ON A-PIT DOOR CUTOUT STA 320 IAW SRM 51-1-20D. 2L74 4F RT4A25 20031107000342003110700034EA 2003 11 7 03306657 120031102A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27657BR 7491 DURING INSPECTION THE OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. 2L72 4F RTA21EA 20031112000802003111200080SO 2003 11 12 C2XA03IA104 120031106A3040163500111 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT ARCED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27195543561 3561 145587 FLIGHT 2959, PILOT REPORTED THAT THE NR 1 WINDSHIELD WAS SPARKING ALONG THE SIDE DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED WINDSHIELD. 2L72 4T RTT00011AT 20030731000392003073100039NM 2003 7 31 QXEA200300785 120030701A30404100S02002 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09412QX3251 3251 4059 GEG- ON FLIGHT 2345 WINDSHIELD HOT CAUTION LIGHT ILLUMINATED IN CRUISE TWO MINUTES AFTER SELECTING. RAN CHECKLIST, SWITCHED TO WARM-UP. AFTER 5 MINUTES CAUTION LIGHT ILLUMINATED AGAIN. REMOVED AND REPLACED ANTIICE CONTROLLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030912001132003091200113NM 2003 9 12 AWXA200300880 120030725A53476553844 CARGO TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR TRACK AT BS 787-847, RBL 15. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT AFT CARGO COMPARTMENT FLOOR TRACK AT BS 787-847, RBL 15; FABRICATED 3 EACH "L" ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-53, FIG 101, PG 106. 2L72 4F RTA16WE 20030917001052003091700105EA 2003 9 17 ASOA03394 120030822A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY FRAMES FS 718, STRINGERS 10 TO 12 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT EQUIPMENT BAY FRAMES FS 718, STRIGNERS 10 TO 12 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20040108001022004010800102 2004 1 8 KBM2003F00052 420031010A34215040017901 GYRO SNIAS 350 AS350B1 8680811EU COCKPIT MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 265 2009 WILL NOT HOLD HORIZON IN FLIGHT. INSTALLED SERVICEABLE ATTITUDE GYRO. 1G71 3U H9EU 20040109000402004010900040WP 2004 1 9 WX0300021 120031102A3244 TIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NLG LOW E WXOAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 WP07861GA 49557 ON DEPARTURE, UPON APPLYING TAKEOFF POWER, THE AIRCRAFT STARTED TO ROLL DOWN THE RUNWAY NORMALLY. AT ABOUT 60 KNOTS THE NOSE WHEEL STARTED TO SHAKE UNCONTROLLABLY. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED BACK TO THE GATE. MAINT INSP THE NOSE WHEELS, GEAR AND TORQUE LINKS. NO DEFECT WAS NOTED. FURTHER INSP FOUND THAT BOTH NOSE TIRES WERE ABOUT 25 PSI LOW ON PRESSURE. THE TIRES WERE SERVICED WITH NITROGEN AND THE AIRCRAFT RELEASED TO SERVICE. THE CREW INIATED ANOTHER TAKEOFF. THE AC PERFORMED NORMALLY. THE FLIGHT CONTINUED TO LAS WHERE THE AC LANDED WITHOUT FURTHER INCIDENT.(K) 2L72 4F4 FRTA6WE E2EA 20031118000512003111800051EU 2003 11 18 AWXA200301166 120030923A5414D54530052200 SKIN AIRBUS320 A320232 3930326EU PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN AT LOWER AFT AREA. MAINTENANCE REMOVED NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-12 & 21-22, FIG 2, 3 & 8. 2L72 4F RTA28NM 20031119001212003111900121NM 2003 11 19 2003UALA00750 120031006A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 FUSELAGE SKIN DENTED AND CRACKED AT STA 1600 AND STR 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20031218000452003121800045EA 2003 12 18 03327688 120031123A2910 HYDRAULIC SYSTEM CNDAIRCL600 CL6002B19 1900309EA 1B SYSTEM OVERSERVICED A VTZAO OTHER WJ INADEQUATE Q C WARNING INDICATION APAPPROACH 1 EA27688BR 7723 DURING APPROACH AFTER FLAPS WERE SELECTED CREW RECEIVED A FLIGHT SPOILER AND INBOARD GROUND SPOILER FAULT. THE FAULT WAS FOUND TO BE DUE TO 1B HYDRAULIC SYSTEM BEING OVERSERVICED. THE 1B SYSTEM WAS DESERVICED TO THE PROPER LEVEL AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031218001692003121800169WP 2003 12 18 CALA0300689 120031204A5320993658049 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 AFT BAG BIN INTERCOSTAL FOR CABIN FLOORBEAM IS CRACKED AT STA 1041 CENTER LINE OF A/C. FABRICATED AND INSTALLED DOUBLER PER SRM 51-70-04 AND STOP DRILLED CRACK IN INTERCOSTAL. 2L72 4F A6WE 20031218001252003121800125EU 2003 12 18 MALA030512 120031106A5320 STRUCTURE BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15527XJ E2352 DURING C-CHECK INSPECTION, AFT CARGO DOOR CHAFED. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO A52034, DATED 24 NOV 2003. A/C RELEASE DATE 11/29/03. REFER TO 409 NR 197618 FOR FURTHER REFERENCE. 2H74 4F RTA49EU 20031223001192003122300119NE 2003 12 23 MALA030530 220031203A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT MALFUNCTIONED A MALAK NONE O OTHER NRNOT REPORTED 1 GL15110XJ 340A110 DURING FLIGHT 3009, LT ENGINE SHOWING GRADUAL LOSS IN ITT MARGIN. LT ENGINE PLACED ON DERIVITIVE POWER FOR CONTINUED SERVICE. CTOT AND ANTI SKID SYSTEMS MUST BE OPERATIVE. MAINTENANCE PROCEDURES COMPLIED WITH FOR DERIVATIVE POWER PROGRAM. CHAP 2, SECTION 2.1 ENTERED IN MDR AND MAINTENANCE CONTROL NOTIFIED. 2L72 4T4 TRTA52EU E8NE6 20031219001842003121900184NM 2003 12 19 MWEA030478 120031209A5320591359577 ANGLE DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 STATION 1418 FRAME IS CRACKED BELOW LONGERON ONE AT SUPPORT ATTACH FASTENER. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F RTA6WE 20031229000692003122900069NM 2003 12 29 03FDEA02183 120031214A5754 FAIRING DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING FIX LEADING EDGE FAIRING ADJACENT TO OUTBOARD END OF LEADING EDGE SLAT FOUND WORN AT 02 LOCATIONS. COMPLIED WITH FEDEX EA 1-5720-73368, OUTER WING FIXED LEADING EDGE SKIN. 2L73 4F RTA22WE 20031229000412003122900041EU 2003 12 29 UPS03141657 120031214A5210 SWITCH AIRBUSA300 A300F4622R 3930360EU PAX DOOR OUT OF ADJUST A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01148UP 831 IN CRUISE LEVEL FLIGHT FL 310 DOOR WARNING (SLIDE ACTIVATION WARNING ON ENTRY DOOR) CAME ON WITH NO ECAM ACTIVATION HANDLE WAS PUSHED DOWN AND WARNING STOPPED. FOUND PASS CREW DOOR LIMIT SWITCH (9WN) OUT OF ADJUSTMENT. ADJUSTED SWITCH MM REF 52-73-13 OPS/CK GOOD. 2L72 4F RTA35EU 20031231000932003123100093WP 2003 12 31 GTIA030937 120031106A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND MAIN CABIN FLOORBOARD STATION 446-522 HAS DAMAGED INSERTS. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20031006001472003100600147NM 2003 10 6 SWAA032013 120030909A53116516301 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED FRAME PER SRM. 2L72 4F RTA16WE 20031007000482003100700048NM 2003 10 7 AALA20030781 120030718A275118173810 TRANSMITTER BOEING737 737823 13844BZNM FLAP INDICATOR MALFUNCTIONED A AALAO OTHER F FLT CONT AFFECTED LDLANDING 1 SW21953AN 29539 DURING LANDING, FLAPS STUCK AT 2 DEGREES. NO EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACEC LEFT WING FLAP POSITION TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2L72 4F RTA16WE 20031009000082003100900008NM 2003 10 9 USAA030191 120030908A5300 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 FOUND SKIN CRACKED .125 INCH, UPPER HINGE CUTOUT OF AFT ENTRY DOOR OPENING. BLENDED DAMAGE PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040106001022004010600102NM 2004 1 6 CALA0300711 120031216A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716650 28911 INSPECTION FOUND L-2 DOORWAY Z-ANGLE CORRODED AT STA 967. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040106001302004010600130NE 2004 1 6 DHL2003807016 220031217A7310WF337017 FUEL FILTER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 4 ENGINE DIRTY A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01807DH 45990 693483 NR 4 FUEL BYPASS FILTER LIGHT ILLUMINATED, ON SHORT FINAL. RAN PROCEDURE AFTER LANDING, LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 4 ENGINE FUEL FILTER. GROUND RAN ENGINE, OPS CHECKED GOOD PER 73-10-2. P/N: WF337017. 2L74 4F4 FRT4A25 E2GL 20040108000892004010800089 2004 1 8 KBM2003F00039 420031004A3120102149 HOUR METER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT INACCURATE E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19350SH 2957 HOUR METER INACCURATE, RUNS LOW. REPLACED WITH NEW SERVICEABLE METER. 1G71 3U3 UNCH9EU E19EU 20031121000512003112100051NM 2003 11 21 SWAA032489 120031110A5754 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C4 CHECK, FOUND #6 L/E SLAT DELAMINATED AT MID SPAN AREA. REMOVED AND REPLACED SLAT ASSY PER MM. 2L72 4F RTA16WE 20040114001432004011400143NE 2004 1 14 DLM88031072 220031209A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 MALFUNCTIONED A DALAFC ACTIVATE FIRE EXT. ABORTED TAKEOFF RA PARTIAL RPM/PWR LOSS FLAME/FIRE TOTAKEOFF 1 SO27956DL24984 49887 725358 ABORT TAKEOFF 80 KIAS. NR 1 ENGINE POSSIBLE COMP STALL. TAILPIPE FIRE MAX EGT NOTED 770. BOTH BOTTLES FIRED. FIRE DEPT APPLIED HALON TO TAILPIPE. REPLACED ENGINE AND BOTTLES. 2L72 4F4 FRTA6WE E9NE 20040120000552004012000055NM 2004 1 20 03FDEA02230 120031223A5753ARC050214 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING. OB FLAP IB FWD HINGE ACTUATOR MOUNT IB LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75209, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031202001452003120200145NE 2003 12 2 AALA20030964 220030906A73201459M13P01 PMC AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 1 ENGINE FAILED A AALAO OTHER M OVER TEMP CRCRUISE 1 SW2134078 615 AIRCRAFT EN ROUTE AUA TO JFK, PASSING THROUGH FLIGHT LEVEL 210, EXPERIENCED SURGE IN THE NR 1 ENGINE. N1 GREATER THAN 125, EXHAUST GAS TEMPERATURE ABOUT 980 DEGREES. EMERGENCY DECLARED AND COMPLETED A LANDING WITHOUT INCIDENT. AIRCRAFT NOT OVERWEIGHT. REPLACED POWER MANAGEMENT CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA35EU E13NE 20031204000772003120400077NM 2003 12 4 HNAA0300055 120031014A7931APT761000100DW TRANSMITTER DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE NR 1 ENG OIL PREFALSE INDICATIONA HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07965HA 450 AG0042 ON CLIMBOUT NR 1 ENGINE OIL PRESS STARTED A GRADUAL CLIMB TO 80 PSI. WHEN ENGINE TORQUE WAS REDUCED TO 40 PERCENT OIL PRESS RETURNED TO NORMAL. INCREASING TORQUE WOULD CAUSE OIL PRESS TO INCREASE TO 95 PSI. WHEN TORQUE WAS REDUCED AGAIN TO 40 PERCENT OIL PRESS RETURNED TO NORMAL. AIRCRAFT RETURNED TO FIELD. REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER. 2H72 4T4 TRTA13NM E20NE 20031204000962003120400096WP 2003 12 4 UPS03841407 120030911A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L10 RT END FITTING CRACKED BETWEEN FS 1768-1772. REMOVED L10 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20031204001112003120400111WP 2003 12 4 UPS03841429 120030922A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, FLOORBEAM REPAIR ANGLE CORRODED FS 1680 LBL 20. REMOVED CORRODED REPAIR ANGLE IAW DC8 SRM 51-3-0. FABBED REPAIR ANGLE AND STRAP IAW DC8 53-2-0 & 53-2-04. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE, STEEL STRAP, SUPPORT ANGLE AND REINSTALLED FLOOR BOARD IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20031208001172003120800117NM 2003 12 8 AWXA200301315 120031001A532069353654 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND AT FASTENER HOLE ON MAIN CABIN FLOOR SUPPORT AT LBL 1, BS 500D TO BS 520. MAINTENANCE REMOVED DAMAGED UPPER CHORD AT LBL 1, BS 500D TO BS 520; FABRICATED A FILLER AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-30-51 FIG 202. 2L72 4F RTA16WE 20031208001352003120800135NM 2003 12 8 2003UALA00784 120031017A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 FWD PIT STA 720 FLOORBEAM T-CHORD AT RBL 10 APPROX IS DENTED ON THE HORIZONTAL FLANGE & EXTENDS INTO THE RADIUS OF THE FLANGE. MAJOR REPAIR ACCOMPLISHED. THE FLANGE WAS TRIMMED OUT AS MUCH AS POSSIBLE. ACP HFEC NDT INSP OF AREA FOR CRACKS, NONE FOUND. THIS REPAIR APPROVED BY BOEING-FAA 8110-3 ON MOBILE AEROSPACE ENGINEERING AUTHORIZATION 47-5325-13-A1038. 2L74 4F4 FRTA20WE E24NE 20031209000922003120900092 2003 12 9 SWAA032358 420031025A2565D31354 SLIDE BOEING737 7377H4 1384404NM R1/L2 DOORS LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 DURING SCHEDULED C3 CHECK, FOUND BOTH R1 AND L2 DOOR EVACUATION SLIDES OUT OF ADJUST. REINSTALLED SLIDES PER MM. 2L72 4F RTA16WE 20031210001902003121000190EU 2003 12 10 03FDEA01801 120031025A7830683L293G01 SKIN AIRBUS300 A300B4605R 3930308EU GE CF6 CF680 30025NE THRUST REVERSER GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25660FE 759 MDIS 660 78-30 0007125 22OCT03 BFM CLOSE R NR S 14 COMPLY WITH EA NR 6-7832-73847 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR. FACT 25OCT03 16:46 BFM U COMPLIED WITH EA NR 6-7832-73847 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR. CLOSED ON 10/25/03. 2L72 4F4 FRTA35EU E13NE 20031014001622003101400162NM 2003 10 14 SWAA032092 120030918A531065C22909 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, STR 28R TO STR 28L. REPAIRED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20031021000582003102100058EU 2003 10 21 A6WA200360041 120030929A5524HC551B0098000 BRACKET BAC 146 146200A 1500266EU LT ELEVATOR IMPROPER A A6WAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31606AW E2033 LEFT ELEVATOR NR 2 HINGE 'A' FRAME TOP MOUNTING BOLT HAS AN IMPROPER SAFETY BRACKET, POORLY MANUFACTURED. REPLACED WITH NWE PART NR HC551B0098-000. (M) 2H74 4F A49EU 20030922000142003092200014EU 2003 9 22 189111 120030819A6120 WARNING LIGHT SAAB SF340 SF340A 7850100EU AUTOCOARSEN ILLUMINATED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 FLIGHT 4493 FROM PIT TO CLE. AIRCREW WAS IN THE PROCESS OF TAKING OFF WHEN THEY RECEIVED THE INDICATION OF THE AUTOCOARSEN NOT ARMING. AIRCREW ABORTED TAKEOFF AND RETURN TO THE GATE WITHOUT INCIDENT. 2L72 4T RTA52EU 20030924000392003092400039NM 2003 9 24 DL757030752 120030814A3240 HANDLE BOEING757 757232 1384965NM PARK BRAKE UNSECURE A DALAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 SO27618DL 22908 FOR INFO ONLY ON T/O ROLL AT 20KTS RECEIVED T/O CONFIG WARNING. TAKEOFF WAS REJECTED. FOUND PARK BRAKE HANDLE NOT FULLY SEATED. EXERCISED HANDLE AND PARK BRAKE OP NORMAL. TEMPS READ 7 ZEROS AND 1 ONE. 2L72 4F RTA2NM 20030924000012003092400001EA 2003 9 24 QXEA200301017 120030823A2610 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 INTERMITTENT A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09615QX 10065 ON FLIGHT 2451 INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. PERFORMED FIRE SYSTEM TEST AND CHECKED ENGINE FIRE BOTTLES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040128000632004012800063NM 2004 1 28 QXEA200301581 120031226A243023088002B GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09345PH10981732 476 SEA- ON FLIGHT 2057 NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED UPON LANDING. WOULD NOT RESET PER CHECKLIST. REMOVED AND REPLACED NR 1 ENGINE STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060802001112006080200111WP 2006 8 2 IXXA060499S 120030123A5313 FITTING DOUG DC8 DC871F 302199DWP BS 1767-1770 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND A CRACKED END FITTING FROM STATION 1767 TO 1770 AT LONGERON 17 RIGHT. REMOVED CRACKED END FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D, 51-1-21, AND 51-3-0. 2L74 4F RT4A25 20030818000212003081800021SW 2003 8 18 HEEA088449 120030723A6410206016201131 BLADE CLARK 1000 1000CLARK 2230102SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03266P 707 TAIL ROTOR BLADE FRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE. 1Q71 3R 2A6 20030819000452003081900045WP 2003 8 19 AALA20030644 120030609A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21411AA 49322 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEATS 21 AND AFT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CHARGER CONNECTOR ABOVE ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030822000372003082200037WP 2003 8 22 03FDEA01220 120030807A5753 HINGE BRACKET DOUG DC10 DC1030 3023501WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 RIGHT I\B FLAP HINGE BRACKET LOWER O\B BOLT HOLE BORE PITTED. FACT 04AUG03 05:45 BFM R COMPLIED WITH EA 8-5740-70995 WINGS- LEFT I/B FLAP, HINGE ASSY ATTACH LUG REWORK AT MAE. 2L73 4F A22WE 20030404001582003040400158NM 2003 4 4 SWAA030546 120030309A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C2 CHECK, FOUND BOTH SEVERAL LAMPS INOP AT AFT CABIN DOOR EMERGENCY EXIT LIGHTS. RELAMPED BOTH EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20030407000462003040700046WP 2003 4 7 GTIA030034 120030117A5320 ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND MID PIT HAS CORROSION ON 2 ANGLE (FWD) STATION 655-598. REMOVED Z-ANGLE STATION 598-655. FORMED NEW ANGLE. INSTALLED NEW Z-ANGLE IN MID PIT FS 655-598. (M) 2L72 4F RTA6WE 20030416003272003041600327EA 2003 4 16 SWIA200311729 120030102A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW 7518 FS 280 LBL 9.0 FLOORBEAM I/B & O/B ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, AND 51-42-21. P/N: 601R3113-57. 2L72 4F RTA21EA 20030416001612003041600161NM 2003 4 16 AALA20030201 120030217A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21697AN 26977 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 12D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030424001312003042400131WP 2003 4 24 UPS03840354 120030313A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, AFT FUSELAGE SECTION APPROX STA 1500 AT LONG 25L TO 26L EXISTING DOUBLER HAS BLIND FASTENERS. REMOVED BLIND FASTENERS, FOUND SKIN BULGED AND DRILL STARTS OUT OF LIMITS AT STA 1505 AT LONG 26L. CUT OUT DAMAGED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, DOUBLER, FILLER, FINGER DOUBLERS AND INSTALLED LONGERON SPLICES IAW SRM 53-2-2 FIG 10 AND 53-2-1 FIG 7. 2L74 4F RT4A25 20030425000772003042500077NM 2003 4 25 MYW2003F00001 120030118A361039271611 REGULATOR VALVE BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE INOPERATIVE A MYWAO OTHER O OTHER NRNOT REPORTED 1 SO19804MA1 22435 700278 ON DEPARTURE, NR 1 ENGINE SUPPLY PRESSURE (DUCT PRESSURE) REACHED 95 PSI FOLLOWED BY STRUT OVERHEAT AND PACK TRIP. RETURN AIRCRAFT. AIRCRAFT PREPED FOR TWO ENGINE FERR. ACCOMPLISHED TWO ENGINE FERRY TO MIA IAW MM. REMOVED AND REPLACED 13 STAGE MODULATING REGULATOR VALVE IAW MM. OPS AND LEAK CHECK, OK. AIRCRAFT RETURNED TO REVENUE SERVICE. (SDR 03004, LOG PAGE 108353, 108354) 2L73 4F4 F A3WE E2EA 20030424000422003042400042NM 2003 4 24 QXEA0300344 120030305A5240 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - AFT SERVICE DOOR FORWARD CENTER GUIDE BRACKET IS GOUGED. REPAIRED IAW HORIZON AIR EA 6-52-248. 2H72 4T RTA13NM 20030425000812003042500081NM 2003 4 25 QXEA0300388 120030316A5420 CHANNEL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND LOWER COWL LEFT AND RIGHT CHANNELS CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030429000232003042900023NM 2003 4 29 PCA0300815 120030127A5320 INTERCOSTAL BOEING747 747283B 1384867NM FUSELAGE TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LWR LOBE AFT CARGO SEVERAL TEARS, CORROSION & DISTORTION ON INTERCOSTAL BETWEEN STA 1900-1920 & RBL 58-LBL 58. DAMAGED INTERCOSTAL REMOVED, NEW SECTION FABRICATED & SRM 53-11-25, PROTECTED AREA PER SRM 51-10-02, RIVETED PER SRM 51-30-02. 2L74 4F A20WE 20030430000312003043000031SO 2003 4 30 GLBA2003051 120030422A21301103P273 PRESSURE SWITCH EMB 120 EMB120ER 3260203SO CABIN PRESSURE FAILED A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03297UX 120297 SMOKE IN CABIN, R&R PRESS SWITCH ON P2S OPS CHECK GOOD 2L72 4T RTA31SO 20030430000322003043000032SO 2003 4 30 C2XA03CL096 120030421A33207287103507 MODULE EMB 145 EMB145ER 3260211SO CABIN FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2731131 145705 IAH FLIGHT 2106 THE CREW REPORTED A BURNING ODOR FROM THE CABIN LIGHT CONTROL MODULE. MAINTENANCE REPLACED THE CABIN LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030430000542003043000054NM 2003 4 30 2003UALA00383 120030415A27511812996 INDICATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FLAP POSITION INOPERATIVE A UALAO OTHER N FALSE WARNING APAPPROACH 1 WP29368UA 2899 24537 AIRCRAFT REPORTED ASYMMETRIC FLAP CONDITION AND LANDED UNDER AMBER ALERT WITH FLAP POSITION 1. GROUND TEST DETERMINED THAT FLAP SYSTEM WAS FUNCTIONING PROPERLY. THE FAILURE WAS ISOLATED TO THE INDICATOR IN THE FLAP POSITION INDICATION SYSTEM. THE INDICATOR WAS REPLACED AND AN OPERATIONAL CHECK VERIFIED PROPER SYSTEM OPERATION. DURING REPAIR OF INDICATOR IN SHOP, IT WAS FOUND THAT THE RIGHT BRUSH WAS WORN, RESULTING IN A BURNED SLIP RING AND POOR ELECTRICAL CONTACT. 2L72 4F4 FRTA16WE E2GL 20030430000682003043000068NM 2003 4 30 USAABB03052 120030322A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 6 AND 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030501001612003050100161NM 2003 5 1 ASAA0310041 120030225A5313 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 21L AT BS 1016 CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20030501000762003050100076WP 2003 5 1 GTIA030219 120030217A3260 CAP DOUG DC9 DC983 3022083WP MLG INDICATOR BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND LEFT LANDING GEAR LIGHT (GREEN) INTERMITTENT. TROUBLE SHOT SYSTEM, FOUND LEFT GEAR LIGHT CAP ASSEMBLY BROKEN. REMOVED LEFT GEAR LIGHT CAP ASSEMBLY. INSTALLED LEFT LANDING GEAR LIGHT CAP ASSEMBLY. (M) 2L72 4F RTA6WE 20030508000432003050800043NM 2003 5 8 03FDEA00676 120030504A53116516312145 FRAME BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 CORROSION ON FRAME 294, WL 148.5, LBL 18 ON NLG WHEEL WELL LBL BULKHEAD. REPAIRED NOSE LANDING GEAR WHEEL WELL BULKHEAD IN ACCORDANCE WITH FEDEX E.A. 7- 5310-69487. 2L73 4F RTA3WE 20030506002082003050600208WP 2003 5 6 ASAA0380233 120030307A53209936534111 CHANNEL DOUG DC9 DC982 3022082WP SUBFLOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT SUB FLOOR U-CHANNEL IS CRACKED. FABRICATED AND REPLACED U-CHANNEL PER SRM. (M) 2L72 4F A6WE 20030508001072003050800107NM 2003 5 8 DL76K030369 120030417A2781 TARGET BOEING767 767332 1382001NM SLAT BENT A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27178DZ 30596 SELECTED FLAPS UP AFTER T/O AND GOT LE SLAT ASSYMETRY EICAS MESSAGE AND LEADING EDGE AMBER LIGHT. WITH HANDLE IN UP POSITION THE INDICATOR NEEDLES. REMAINED BETWEEN UP AND 1 DEG. POSITIONS. PERFORMED BITE ON PSEU, LAST FLIGHT FAULT SHOWS TARGET OF SW 296 NR 10 RT OUTBD. FOUND TARGET BENT, CHECKED FOR DAMAGE OR OBSTRUCTIONS NONE FOUND. REPOSITIONED TARGET AND ADJUSTED CLEARANCE TO SWITCH. OPS CHECKD OK. 2L72 4F RTA1NM 20030513001552003051300155NM 2003 5 13 QXEA0300458 120030404A5410 DOOR BOMBDRDHC8 DHC8401 1390041NM RT NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 RIGHT HAND NACELLE REFUEL/DEFUEL DOOR CHAFED ON INSIDE AT LIGHT SWITCH. REPAIRED IAW HORIZON AIR EA 6-54-225. 2H72 4T RTA13NM 20030514001992003051400199WP 2003 5 14 03FDEA00694 120030508A5420 FAIRING DOUG DC10 DC1010 3022110WP NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 NR 1 PYLON AFT FAIRING O/B AFT SECTION CRACKED. NEW PART FAB ON TRAVELER T2/231892. INSTALLED IAW SRM 51-43-01. 2L73 4F A22WE 20030527000362003052700036WP 2003 5 27 DHL2003804875 120030123A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FUSE EXT - WEB LOWER PART CRACKED AT STA, 808.000 LBL 54.000. STOP DRILLED CRACK AT STA 808.000 LBL 54.000 IAW SRM 53-2-0, FABRICATED REINFORCEMENT (2024 T3 .040) IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ON FUS EXT WEB IAW SRM 53-2-0 FIG 1B, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030602000052003060200005SO 2003 6 2 SIMA200312715 120030421A532014521725615 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY AREA RIGHT AFT SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02/06, 51-20-03. (M) 2L72 4T RTT00011AT 20030602000912003060200091NM 2003 6 2 SWAA031142 120030521A55306546872 FITTING BOEING737 7373H4 1384600NM VERT STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR PRIMARY LUG AFT FACE CORRODED ON BOTH LT/RT SIDES. REPAIRED VERT STAB PER BFG ER. 2L72 4F RTA16WE 20030604001182003060400118NM 2003 6 4 UPS03440533 120030413A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 1394 S11L STRINGER CRACKED. BS 1385 - 1410 STR 11L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 5. 2L74 4F A20WE 20030515001212003051500121SO 2003 5 15 C2XA03SH121 120030502A532014524056003 BRACKET EMB 135 EMB135LR 3260305SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 SHV - DURING C-CHECK SUPPORT BRACKET AFT OF PAX DOOR SECOND FROM THE TOP WAS FOUND GOUGED BY FRAME 18. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030520000372003052000037SO 2003 5 20 SIMA200311307 120030402A532014529150009 STRUCTURE EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION CROSSMEMBER AT FRAME 23 CORRODED. REMOVED AND INSTALLED NEW CROSSMEMBER AT FRAME 23 IAW EMB 145 SRM 51-20-01/03, 51-40-02/04/06. (M) 2L72 4T RTT00011AT 20030416002052003041600205WP 2003 4 16 ABXA030131 120030410A3310 LIGHT DOUG DC9 DC931 3022065WP COCKPIT SMOKE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23948AX 47065 CAPTAIN'S MAP LIGHT BEGAN EMITTING ELECTRICAL SMOKE. MAP LIGHT CIRCUIT BREAKER TRIPPED. REPLACED CAPTAIN'S MAP LIGHT ASSEMBLY IAW DC-9 AMM 33-10-00. OPS CHECKED GOOD. PLACARD REMOVED. RESET CIRCUIT BREAKER. 2L72 4F A6WE 20030418000332003041800033NM 2003 4 18 ZW0A0302201 120030215A3350S283T0143 BATTERY PACK BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13719TW 28487 THE EGRESS LIGHTING IN CABIN SECTION-C WAS FLASHING ON AND OFF. REPLACED THE POWER SUPPLY. CHECK-C 7-7-02 MCI. 2L72 4F RTA2NM 20030421000442003042100044 2003 4 21 UPS03840246 420030227A2565 BOTTLE DOUG DC8 DC873F 302199FWP ESCAPE SLIDE DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 ESCAPE SLIDE AIR PRESSURE GAUGE IN THE RED. EMERGENCY ESCAPE SLIDE CYLINDER PRESSURE WITHIN SERVICEABLE LIMITS PER MM 25-60-01 TEMPERATURE COMPENSATION CHART. 2L74 4F RT4A25 20030418000152003041800015EU 2003 4 18 MALA030152 120030211A3000 VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ANTI ICE SYS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15421XJ 340B421 DURING CLIMBOUT OF FLIGHT 3169, ENGINE WAS SELECTED, AIR VALVE LIGHT ILLUMINATED AFTER 3-5 SECONDS QRH COMPLETED, VALVE RESET ITSELF. SECOND TIME ANTI-ICE SWITCHED ON. AIR VALVE ON AGAIN AND STAYED ON AFTER QRH COMPLETED. AIR RETURN TO DTW. MAINTENANCE REPLACED LT ENGINE ANTI-ICE VALVE, REPLACED LT ENGINE GREEN WIRING HARNESS, REPLACED LT ENGINE CHIP DETECTOR. PERFORMED REQUIRED OPS/LEAK CHECKS. ALL CHECKS GOOD. ALL REF GE MM. 2L72 4T4 TRTA52EU E8NE 20030418001132003041800113WP 2003 4 18 UPS03840212 120030128A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, L1 DOOR UPPER FWD CORNER CRACKED BY CUTOUT, MARKED. FOUND WITH NDT ON SKIN MAT ID -17 DOUBLER 7075-T6 .063 PO 3874552 -15 DOUBLER 7075-T6 .080 PO 3958421 FILLER 7075-T6 .050 PO 3924131 IAW DC8 SRM 53-2-0. FAB DOUBLER TRIPER IAW DC8 SRM 53-2-0 FIG 15. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER TRIPLER IAW DC8 SRM 53-2-0. 2L74 4F RT4A25 20030327001722003032700172SO 2003 3 27 C2XA03SH056 120030316A5310 THRESHOLD EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 DURING C-CHECK PASSENGER DOOR THRESHOLD U-SHAPE WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED U-SHAPE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030327000742003032700074NM 2003 3 27 C1HA200395007 120030220A3350 SWITCH BOEING727 727290 138408WNM EMERGENCY LIGHTSFAILED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15295AS 22147 EMERGENCY EXIT LIGHTS WILL NOT TURN ON FROM AFT ATTENDANTS PANEL. FOUND BAD SWITCH AT AFT ATTENDANTS PANEL ,REPLACED SWITCH PER MM CH 33 STANDARD PRACTICES 2L73 4F A3WE 20030801001092003080100109EA 2003 8 1 COMA0360334 120030727A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01936CA21743 7043 FOUND LOWER RIGHT WING PLANK CRACKED AT WS 148.019 DURING EO 57-014. PERFORMED TEMPORARY REPAIR AND DEFERRED PER REO 601R-57-21-138 2L72 4F RTA21EA 20030805000922003080500092EU 2003 8 5 ASOA03282 120030702A2120S3611200800263 VALVE AEROSPATR72 ATR72 EU ENGINE INOPERATIVE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11641AS 387 DURING DESCENT INTO ATL FROM VPS, SMOKE OCCURRED IN THE CABIN DURING OPERATION OF THE RT PACK. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE P2.5 TO P3 SWITCHING VALVE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030801000102003080100010WP 2003 8 1 GTIA030520 120030619A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FORWARD CABIN FLOOR SUPPORT STATION 200 RBL 6 TO LBL 22 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030422000792003042200079SO 2003 4 22 SIMA200307914 120030227A532014521725001 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, LEFT SILL HAS CORROSION BETWEEN FRAME 19 AND 20. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2L72 4T RTT00011AT 20040223001502004022300150SO 2004 2 23 XGN2004F00001 220031210A8520SA649520A3 CAMSHAFT BEECH 55 D55 1152730CE CONT O520 IO520C 17032SO ENGINE BROKEN E XGNAEA ENGINE SHUTDOWN UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 SW0569RP 3313 1213 TE766 561985 AIRCRAFT WAS ENROUTE, PIC NOTICED THE AIRCRAFT YAWING WAY TO THE RIGHT. THERE WAS NOT ANY LOSS OF OIL OR FUEL PRESSURE NOR ANY VIBRATION. THE PILOT SHUT THE ENGINE DOWN AND LANDED. THE OIL PAN WAS REMOVED AND FOUND THE CAMSHAFT WAS BROKEN. HAVE NO IDEA WHAT CAUSED THE FAILURE. (SW05200403504) 1L72 3O3 O 3A16 E5CE 20030723001062003072300106NM 2003 7 23 DL73K030501 120030601A29106546858236 TUBE BOEING737 737247 138448DNM HYD SYSTEM CRACKED A DALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO27382DL 23609 SLOW LEAK IN FLT RESULTED IN A-SYSTEM RESERVOIR GOING TO ZERO AND SUBSEQUENT LOW PRESSURE LIGHTS ILLUMINATED. FOUND NR 1 ENG TO PYLON PRESSURE LINE CRACKED AT BEND. REPLACED HYD LINE. RAN ENGINES/FLIGHT CONTROLS, NO FURTHER LEAKS NOTED. 2L72 4F A16WE 20030829000662003082900066EU 2003 8 29 40003 120030711A7830F900HD3100001A3 SKIN PANEL AMD FALC50FALCON900 2700160EU THRUST REVERSER GOUGED E ERYAK NONE O OTHER ININSP/MAINT 1 CE07369BG6145 040 DURING SCHEDULED MAINTENANCE EVENT, FOUND FURTHER GOUGING AND CHAFING PRESENT ON RT THRUST REVERSER DOOR SKIN. THE GOUGING, AT THIS TIME, IS CONSIDERED ACCEPTABLE, HOWEVER DASSAULT FALCON STRUCTURE ENGINEERING DEPARTMENT HAS RECOMMENDED THAT A PERIODIC VISUAL INSPECTION BE PERFORMED TO DETECT FURTHER DETERIORATION OF GOUGE CONDITION. REFERENCE DASSAULT FALCON STRUCTURES PROJECT 5544. 2L73 4F RTA46EU 20030728000752003072800075NM 2003 7 28 SWAA031549 120030714A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, JUST BELOW STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030520001142003052000114NM 2003 5 20 AALA20030397 120030401A3397 CONNECTOR BOEING777 777223 1385213NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21771AN 29579 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 43 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE CONNECTOR AT ROW 42. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20030609000582003060900058NM 2003 6 9 QXEA0300643 120030520A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM ZONE 400 MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09346PH 477 PDX ON FLIGHT 9850 TAKEOFF WAS ABORTED DUE TO AUTOFEATHER NOT ARMING. ARM LIGHT TESTED GOOD. REPEATEDLY ARMED/DISARMED AUTOFEATHER SYSTEM AND PERFORMED MULTIPULE AUTOFEATHER AND POWER UPTRIM TESTS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030609001502003060900150SO 2003 6 9 C2XA03SH154 120030525A532014524131011 SUPPORT EMB 145 EMB145ER 3260211SO THRESHOLD CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE AFT PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030613000192003061300019NM 2003 6 13 UPS03440782 120030516A5320 FLOOR SUPPORT BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - FLOOR SUPPORT FOUND CORROSION AT BS 2316 LBL 25-26. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8. CORROSION BLEND OUT 0.037 X 1 X 1 INCH. 2L74 4F RTA20WE 20030617002142003061700214SW 2003 6 17 HEEA087311 120030611A6420 BEARING BELL 407 407 1182206SW T/R HUB ASSY DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH2091 53386 53400 CLICKING SOUND FROM ELASTOMERIC BEARING. REPAIRED. 1G71 3U O H2SW 20030527000982003052700098EA 2003 5 27 2003F00308 120030306A2760270005 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERON INOPERATIVE A MASAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW0717156 7156 AIRCRAFT ABORTED TAKEOFF DUE OT TRIM CONFIGURATION WARNING. MAINTENANCE TROUBLESHOT AND REPLACED THE SPOILERON PCU. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20030620000432003062000043NM 2003 6 20 USAA030057 120030516A5315 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU 22201 FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCH, UPPER SURFACE FLOORBEAM UPPER CHORD BS 1320, RBL 35. FLOORBEAM UPPER CHORD REPAIR, UPPER CHORD REPLACEMENT LBL 54 - RBL 36 PER T/R 53-15-01. CORROSION LEVEL 1, TASK NR C53-251 AND 252-02. (M) 2L72 4F RTA2NM 20030620000512003062000051WP 2003 6 20 GTIA030400 120030511A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND MID PIT CARGO STATION 636 AND STATION 693 RIGHT SUPPORTS CORRODED. PRIOR TO STEP 11 REMOVED CORRODED ANGLES. INSTALLED NEW ANGLES. FABRICATED TWO SUPPORTS CHANNELS. (M) 2L72 4F A6WE 20030624000252003062400025NM 2003 6 24 HNAA0300026 120030529A2611PU90461S SMOKE DETECTOR DHAV DHC8 DHC8201 2809001NM LAVATORY MALFUNCTIONED A HNAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA07969HA9632 468 LAV SMOKE DETECTOR SOUNDED AT 1000 FEET IN FLIGHT. NO SMOKE WAS NOTED. REPLACED LAV SMOKE DETECTOR. 2H72 4T RTA13NM 20030619000782003061900078SW 2003 6 19 HEEA087413 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 TAIL ROTOR DISC PACK PLATES, WHEN TORQUED CAP BEYOND LIMITS. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030625000282003062500028 2003 6 25 G5S2003F00001 420030430A25657A14124 SLIDE BOEING747 747400 NM GE CF6 CF680 30025NE UPPER DECK DOOR INOPERATIVE E G5SAO OTHER O OTHER NRNOT REPORTED 1 SO09493MC 29254 INFLATABLE EVACUATION SYSTEM OF THE RIGHT UPPER DECK DOOR DOES NOT INFLATE PROPERLY. THE SLIDE WAS LIFTED AND HAS BEEN FALLEN OUT OF THE DOOR FRAME. SUDDENLY THE SLIDE STOPPED ROTATING AND STUCK. AFTER WAITING SEVERAL SECONDS THE MECHANIC OPENED THE VELCRO TAPES, WHICH CONNECT THE ASPIRATORS WITH THE GIRT. AFTER THIS, THE SLIDE TURNED TO THE END POSITION AND INFLATED PROPERLY. INVESTIGATION OV THE VIDEO RECORD HAS SHOW THT THE FORWARD RELEASE CABLE WAS TIGHT WHEN THE SLIDE STUCK. THE LAST RELEASE PIN WAS LAYING BENEATH THE GIRT. OPENING OF THE VELCRO TAPES INCREASED THE FORCE AND THE RELEASE CABLE GOT FREE. AFTER THIS MANUAL RELEASE, THE SLIDE INFLATED PROPERLY. 2L74 4F4 FRTA20WE E13NE 20030708000992003070800099NE 2003 7 8 070103 220030701A7532 BLEED VALVE LEAR 25 25B 5170511CE GE CJ610 CJ610* 30006NE NR 1 ENGINE OUT OF ADJUST E ESUAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 CE03425JL 127 240157A WHILE CLIMBING THROUGH FL40.5, NR 1 ENGINE FLAMEOUT. AIRCRAFT DESENDED TO FL290, THE ENGINE WAS RELIGHT AND AIRCRAFT CONTINUED TO SRQ AT FL240. MAINTENANCE DETERMINED THAT THE BLEED VALVES WERE OUT OF ADJUSTMENT. 2L72 4J4 J A10CE 1E16 20030711000042003071100004WP 2003 7 11 DHL2003804003 120030605A3350313 LIGHT DOUG DC8 DC873F 302199FWP CABIN BURNED OUT A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01804DH 46124 EMERGENCY LIGHTS ARMED LIGHT BURNED OUT. REPLACED ARMED LIGHT, OPS CHECKED GOOD PER DC8 M/M 33-50-2. 2L74 4F RT4A25 20030710000072003071000007NM 2003 7 10 KPVA200326 120030608A33506104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13807WP 023 FOUND LEFT AND RIGHT FORWARD EGRESS LIGHT OUT AND ONE FORWARD CEILING AISLE LIGHT EMERGENCY LIGHT OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLIES 3351-PS1 AND 3351-PS2. OPS CHECK GOOD IAW DHC 8 MM 33-51-00 PAGE 202. NO DEFECTS NOTED. (M) 2H72 4T RTA13NM 20030714001022003071400102NM 2003 7 14 CALA0300347 120030630A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND RT AFT LAV FORWARD WALL LOWER U-CHANNEL CORRODED AT STA 986.5 - 1006. THE U-CHANNEL WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030724000582003072400058NM 2003 7 24 AWXA200300713 120030618A2560P4010021 BATTERY BOEING737 7373S3 1384711NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28313AW 23712 EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030729000792003072900079NM 2003 7 29 QXEA200300749 120030616A5410 STRUT DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX-GOUGED UPPER SUPPORT STRUT AFT AREA OUTBOARD NR 2 ENGINE. REPAIRED IAW RD8-54-1811, RD8-54-036 AND HORIZON AIR EA 2-54-172. 2H72 4T RTA13NM 20030807000592003080700059SO 2003 8 7 C2XA03CL132 120030802A335066368 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2716944 145045 THE CREW REPORTED THE AFT SECTION OF THE AISLE PATH EMEREGENCY LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT LIGHT STRIP SECTION. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030814000162003081400016NM 2003 8 14 SWAA031728 120030803A32106545800219 FITTING BOEING737 7373H4 1384600NM LT AND RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG WALKING BEAM FITTINGS PER SWA SI AND MM. 2L72 4F RTA16WE 20030903000872003090300087EA 2003 9 3 A6WA200340120 120030815A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 FOUND FS 625 RIGHT UPPER OBLIQUE ANGLE, P/N 601-35012-52, AT STRINGER 14 IS CRACKED APPROX 2 INCHES. (M) 2L72 4F RTA21EA 20030812000932003081200093EU 2003 8 12 HEEA088633 120030720A3340 NUT BOLKMS117 BK117A1 5626010EU LANDING LIGHT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC 7152 KNURL NUT FOR WIRE HARNESS FROZEN AND HOUSING CRACKED. SHOP REPAIR. 1G72 3U H13EU 20030730001102003073000110SO 2003 7 30 SIMA200317402 120030619A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO E/E BAY MALFUNCTIONED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21625AE 145115 HOU - FLT 3926 - AFTER TAKEOFF CREW RECEIVED LANDING GEAR AIR/GROUND FAIL MESSAGE. AIRCRAFT RETURNED TO FIELD AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030826001532003082600153EU 2003 8 26 SIMA200321605 120030801A3230 CIRCUIT BREAKER SAAB SF340 340B 7860101EU LANDING GEAR TRIPPED A SIMAD RETURN TO BLOCK O OTHER CLCLIMB 1 SW21330AE 340B330 DFW - FLT 3311 - DURING DESCENT, THE CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND, CREW FOUND CB F7 POPPED. F7 WAS RESET AND LANDING GEAR THEN EXTENED NORMAL. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK AS COMPLIED WITH, NO DEFECTS NOTED. AIRCRAFT WAS THE RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030827000232003082700023NM 2003 8 27 03FDEA00906 120030618A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 N00367 950F FRAME DENTED BETWEEN S26L AND S25L. REPAIRED FRAME AT BS 950F BETWEEN STR 26L AND STR 25L IAW SRM 51-40-3 FIG 1, BS 950F FRAME DENT BETWEEN STR 25L AND STR 26L OUT OF LIMITS IAW SRM 53-10-1. 2L73 4F RTA3WE 20030911002462003091100246WP 2003 9 11 DHL2003604603 120030622A573056554331 FAIRING DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OTBD FAIRING ASSY WITH EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED OB FAIRING ASSY ON LT WING IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR 0531. 2L74 4F RT4A25 20031002000582003100200058WP 2003 10 2 UPS03841216 120030910A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 45914 INSPECTION TYPE: ASV, EMERGENCY EXIT LIGHT BATTERY, DEAD. REPLACED EMERGENCY LIGHT BATTERY PACK AND RELAY UNIT ASSY. OPS CK GOOD. 2L74 4F RT4A25 20031006000202003100600020EU 2003 10 6 MALA030410 120030812A5260 TRACK BAC 146 AVRO146RJ85A1500097EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK IN CVG, OB AIRSTAIR RAIL CORROSION. MAINTENANCE REMOVED AND REPAIRED CORROSION. REFER TO 409 NR 190255 FOR DETAIL. A/C RELEASE DATE 9/2/2003. 2H74 4F RTA49EU 20031003001032003100300103EA 2003 10 3 958851 120030915A32425003320 GRIP GOODYEARAERO FLEET 16B FINCH2 3480504EA BRAKE SLIPPED B K NONE O OTHER ININSP/MAINT 1 SW11678M JAN82648 226 BRAKE RETURN SPRING ASSY GRIPS & TUBE ASSY SLIPPED THEREFORE BRAKE PRESS PLATE DID NOT RETRACT CAUSING WHEEL TO DRAG. SLIPPAGE OCCURRED DURING TAXI TEST & ALSO DURING BRAKE BLEEDING PROCEDURES. ADDITIONAL S/N'S OF FAILED BRAKES: NOV99-1724,MAR00-1736,MAR00-1739, SEPT98-1630, DEC89-1241, NOV98-1641, MAR00-1737 1Q71 3R 2566 20031006001672003100600167NM 2003 10 6 SWAA031970 120030902A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, BS 807 BETWEEN STR 26R AND STR 27R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20031007000592003100700059NE 2003 10 7 AWXA200301061 220030915A7200 ENGINE AIRBUSA319 A319132 3930340NM IAE V2527 V2527A5 NE NR 2 MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28660AW 1234 ON TAKEOFF AT PHX EN ROUTE FOR BWI NR 2 ENGINE DID NOT PRODUCE FLEX TAKEOFF POWER, EPR ONLY REACHED 1.2, EPR OF 1.4 REQUIRED, REJECTED TAKEOFF AT 78 KTS. MAINTENANCE PERFORMED A HIGH POWER ASSURANCE TEST IAW T/C F5M71312, NO FAULTS WERE NOTED, NR 2 ENGINE EPR WELL ABOVE 1.2. 2L72 4F4 FRTA28NM E40NE 20031006001882003100600188NM 2003 10 6 03FDEA01678 120031001A532065453132 STRINGER CLIP BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CRACK IN STRINGER CLIP AT BS 950B, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950B, STRINGER 6 RT IAW SRM 51-30-2 & 51-30-5. 2L73 4F4 FRTA3WE E2EA 20030909001612003090900161SO 2003 9 9 SWIA200312308 120030822A2460 RELAY EMB 120 EMB120ER 3260203SO ELECTRICAL SYS OVERHEATED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07562SW 120336 JUST PRIOR TO ENGINE START, FLIGHT DECK BEGAN TO SMELL OF SOMETHING ELECTRICAL OVERHEATING. ISOLATED TO APU PANEL RT SIDE CONSOLE. FOUND APU FEEDER PROTECTION RELAY SHOWING SIGNS OF EXCESSIVE HEAT. REMOVED AND REPLACED FEEDER PROTECTION RELAY IAW W/M 20-10-00. OPS CHECK OK. 2L72 4T RTA31SO 20030910000022003091000002EU 2003 9 10 BAQA088806 120030821A143011213171216 BOLT BOLKMSBK117 BK117C1 5626025EU MISMANUFACTURED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG 7506 BOLTS JUST PURCHASED, BUT THE COTTER PINS HOLES ARE DRILLED WRONG, MAKING THE BOLTS UNUSEABLE. REQUEST WARRANTY CREDIT ON THESE BOLTS. 1G72 3U NCH13EU 20030910000682003091000068WP 2003 9 10 DHL2003604779 120030521A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT FRAME FLANGE WITH 2.000 CRACK, STA 1580.000, L-21L - L-20L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110, SRM 51-1-1. TRIMMED OUT DAMAGED FRAME AND FABRICATED NEW FRAME SEGMENT AND SPLICE ANGLES (02 EA) IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53 110. PERFORMED HEAT TREATMENT TO NEW FRAME SEGMENT AND SPLICE ANGLE IAW SRM 51-1-1 PG 11-13. CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT AND SPLICE ANGLES IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND SPLICE ANGLES WITH NEW FASTENERS IAW SRM 53-2-0 FIG 2, TR NR 53-125, TR NR 53-110, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031119000162003111900016WP 2003 11 19 UPS03841373 120031004A5531 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE VERTICLE STAB LECRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, VERTICLE STAB LE RT RIB IS CRACKED AT ZFS 68. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATED CRACK,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 55-2-0 FIG.2 2L74 4F4 FRT4A25 E2GL 20031119000632003111900063NM 2003 11 19 0301926307 120031012A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01667US 24222 DURING LINE CHECK, FOUND LT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 1-14. REPAIRED WIRING. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031030000962003103000096NM 2003 10 30 03FDEA01673 120031001A5320 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 STRINGER CLIP CRACKED AT BS 950D STRINGER 9 LT. ** SD ** COMING 2L73 4F RTA3WE 20031031000222003103100022CE 2003 10 31 ACE093003 120030930A2420 CSD BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA GOVERNOR FAILED E YADAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL03112AX UC45 97546 PILOT REPORTED NR 2 ENGINE TORQUE STARTED TO SURGE (1500 LBLS) AND WAS SHUT DOWN PER THE QRH. MAINTENANCE REPLACED THE NR 2 ENGINE CONSTANT SPEED GOVERNOR AND OVERSPEED GOVERNOR FOR TROUBLESHOOTING (THE REPORTED PROBLEM COULD NOT BE DUPLICATED ON THE GROUND). 2L72 4T4 TRTA24CE E4EA 20031031000542003103100054NM 2003 10 31 QXEA200301205 120030928A5230 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 800 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 PDX- DEEP SCRATCHES ON CARGO DOOR OUTER SKIN REPAIR STRAP ON THE UPPER PART OF DOOR. REPAIRED IAW DHC-8 SRM 51-40-11, 51-20-26 AND RD 8-52-029. 2H72 4T RTA13NM 20031031000072003103100007SO 2003 10 31 SWIA200312465 120030927A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07579SW6913 6913 120347 EMERGENCY LIGHTS WOULD NOT TEST CORRECTLY IN EKO FROM ROW 9 BACK WOULD NOT LIGHT UP. LET SYSTEM CHARGE 10 MIN AND THEY TESTED OK. FLOOR LEVEL EMERGENCY LIGHTS ON LAST THREE ROWS (9, 10, 11) INTERMITTENT. REMOVED AND REPLACED NR 3 ELBP IAW MM 33-50-02. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040212001422004021200142NM 2004 2 12 DHL2003742522 120031126A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CORROSION CABIN FLOORBEAM 1030 BLR 45 TO BLR 60. REMOVED CORROSION AT FLOORBEAM 1030 BLR 45 TO 60 IS OUT OF LIMITS. REMOVED FASTENERS FOR ACCESS AS REQUIRED FOR REPAIR. CUT OUT DAMAGE AREA DIMENSION IS 12 INCHES AS REQUIRED FOR REPAIR IAW B-727 SRM 53-10-8 FIG 1. FABRICATED UPPER CHORD MAT USED BAC 1505-100617 PO 900411 DIMENSION 12 INCHES, ONE SUPPORT ANGLE MAT USED BAC 1490-2631 PO 332363 DIMENSIONS 19 X 2.5 INCH AND OTHER SUPPORT ANGLE MAT USED BAC 1512-3396 PO 900412 DIM 23 X 1 INCH AND OTHER ENFORCEMENT STRAP MAT USED BAC 1512-3353 PO 217961 DIM 19 X 1 INCH. ALODINED AND PRIMED. INSTALLED REPAIR. 2L73 4F A3WE 20031112000392003111200039NM 2003 11 12 03FDEA01773 120031009A5753ARC0502505 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING O/B FLAP I/B HINGE (WING SIDE) - I/B LOWER ATTACHMENT TO REAR SPAR, HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031106001832003110600183NM 2003 11 6 03FDEA01862 120031103A5315652082753 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION BS 400 FLOORBEAM TOP CHORD CORRODED, LBL 6 TO LBL 10, WL 208. 2L73 4F RTA3WE 20031107000402003110700040SO 2003 11 7 C2XA03SH431 120031107A711014576057622 STIFFENER EMB 145 EMB145LR 3260212SO NR 2 COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031106002022003110600202EA 2003 11 6 ASOA03464 120030929A2730 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA ELEVATOR MALFUNCTIONED A ASOAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO11707EV 10057 DURING CLIMB-OUT FROM OAK-DFW, THE CREW RECEIVED A SPLIT ELEVATOR CAUTION LIGHT. AN EMERGENCY WAS DECLARED WITH EMERGENCY VEHICLES REQUESTED FOR STAND BY AS A PRECAUTION. THE AIRCRAFT RETURNED TO OAK AND LANDED SAFELY. MAINTENANCE RESET THE ELEVATOR CONTROL SYSTEM AND PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040202001792004020200179NM 2004 2 2 AWXA200400051 120031224A575465C2803619 ATTACH BRACKET BOEING737 7373B7 1384580NM SLAT ACTUATOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1.1875 INCH CRACK WAS FOUND ON LT WING LEADING EDGE NR 3 SLAT ACTUATOR DOOR FORWARD ATTACH BRACKET AT WBL 328. MAINTENANCE REMOVED CRACKED NR 3 SLAT ACTUATOR DOOR ATTACH BRACKET AT WBL 328; FABRICATED A NEW REPLACEMENT ATTACH BRACKET; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040205000492004020500049WP 2004 2 5 ASAA0380765 120031121A53209930538 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 FOUND DURING 15K CHECK, CUSP WEB IS CORRODED AT FS 1237. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 53-01 AND 51-10-3. (M) 2L72 4F RTA6WE 20040205000502004020500050EA 2004 2 5 ASOA03677 120031226A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE LT AND RT FLOOR SUPPORT ANGLES ON THE AFT BULKHEAD AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT REPAIRED THE LT AND RT FLOOR SUPPORT ANGLES ON THE AFT BULKHEAD AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040204001772004020400177EU 2004 2 4 C2010312003MT 120031028A76006877277 LINE ALLSN AGUSTAA109 A109 0260109EU ALLSN 250C 250C20B 03013GL AIR SENSE CHAFED B JBZRK NONE P NO WARNING INDICATION ININSP/MAINT 1 WP274999B300 300 7155 CAE831221 DURING DAILY INSPECTION THE P/C AIR SENSE LINE WAS FOUND TO BE DAMAGED BEYOND LIMITS. THE DAMAGE WAS CAUSED BY THE THREADED PORTION OF A SCREW RUBBING AGAINST THE LINE. THE SCREW ATTACHES TWO CLAMPS TOGETHER AS REQUIRED BY CEB 1198. THE CLAMPS (P/N 6749387-03 OR MS9825-03) FIT LOOSELY AND SLIDE CAUSING CONTACT. 1G72 3U3 U H7EU E4CE 20040212000352004021200035WP 2004 2 12 ZW0A0306501 120031207A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSLOOSE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13939AS 49657 THE EGRESS LIGHTS WERE INOPERATIVE BETWEEN CABIN ROWS 27 AND 30. SECURED LOOSE CONNECTOR AT ROW 30. CHECK-C 11-23-03 STL. --CLOSED--- 2L72 4F RTA6WE 20031211001342003121100134NM 2003 12 11 AALA20031339 120031128A3350 BATTERY PACK BOEING737 737823 13844BZNM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21971AN 29547 MIA ROWS 7 TO 11DEF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR ROWS 7 TO 11DEF EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20031215001072003121500107NM 2003 12 15 AWXA200301469 120031104A5414313A135515 SKIN BOEING737 7373G7 1384595NM RT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MINOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON RT PYLON SKIN ON INBOARD SIDE BELOW PANEL 5843R, NAC STA 332.12 - 345.28. MAINTENANCE REMOVED DAMAGED SKIN ON RT PYLON INBOARD SIDE BELOW PANEL 5843R; FABRICATED NEW SKIN PER DWG 313A1355; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, 6, 7, 8, 12, 13 & 14 PG 1, 26, 29, 32, 36, 38, 45 & 51-65. 2L72 4F RTA16WE 20031217000782003121700078NM 2003 12 17 CALA0300667 120030716A5320 SUPPORT BOEING737 7373T0 1384582NM RT AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND RIGHT AFT LAV WALL SUPPORT CORRODED. THE LAV WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-00. 2L72 4F RTA16WE 20040622001432004062200143CE 2004 6 22 AMWA116 120031030A1430114430002199 RIVET BEECH 1900 1900D 1154162CE FUSELAGE CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE23 WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE LEFT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFED. 2L72 4T RTA24CE 20030926001512003092600151NM 2003 9 26 SCNA03007 120030902A3350 LENS BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT MISSING A SCNAK NONE O OTHER ININSP/MAINT 1 GL15801SY 30332 FOUND LENS FOR EMERGENCY EXIT SIGN MISSING AFT SIDE OF L2 DOOR. INSTALLED A NEW LIGHT LENS ASSY OPS CHECKED EMERGENCY LIGHT SYSTEM, OPS CHECKED GOOD. 2L72 4F RTA16WE 20060801000332006080100033WP 2006 8 1 IXXA060519S 120031010A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LONGERON 15 LEFT CRACKED AT STATION 1748. REMOVED CRACKED LONGERON. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-20D, 51-1-8, 53-2-2, AND 51-3-1. 2L74 4F RT4A25 20030819002032003081900203EA 2003 8 19 03223631 120030811A2711 NUT CNDAIRCL600 CL6002B19 1900309EA AILERON CONTROL BINDING A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27631BR 7261 DURING CRUISE CREW REPORTED BINDING IN THE AILERON CONTROL SYSTEM. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTURE FIELD, FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL RETORQUED THE RT YOKE NUT ON THE AILERON CONTROL WHEEL. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030820001012003082000101NM 2003 8 20 UPS03241048 120030724A5330 FRAME BOEING727 72725C 138400HNM BS303 S10L-S9L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, DURING INSPECTION OF SKIN CHANGE AREA FRAME AT BS 303 FOUND DAMAGED BETWEEN S10L AND S9L. CLEANED UP DAMAGED AREA IAW SRM 51-40-4. FABRICATED REPAIR PART IAW SRM 51-40-4. INSTALLED REPAIR PART IAW SRM 51-40-4. 2L73 4F A3WE 20030401000582003040100058NM 2003 4 1 CA030224003 120030220A2612 FIRE LOOP BOEING737 737281 138448PNM PWA JT8 JT8D17 52049NE APU MALFUNCTIONED W FA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA 34247 (CAN) CREW REPORTED, AT CRUISING ALTITUDE, 20 MINUTES OUT OF YLW THEY EXPERIENCED A VIBRATION FOLLOWED BY AN APU FIRE WARNING. CREW SHUTDOWN APU WITH THE FIRE HANDLE AND APU FIRE BOTTLES WERE DISCHARGED. A/C COMPLETED AN (ABNORMAL LANDING CONFIGURATION) IN YLW WITH CFR ON STANDBY NO EMERGENCY WAS DECLARED. A/C LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION FOR EVIDENCE OF FIRE AND EXTERNAL INTEGRITY OF THE APU REVEALED NO SIGNS OF FIRE. THE APU AND APU FIRE SHUT OFF SYSTEM WAS PLACED ON MEL (49-1 AND 26-7-1). MAINTENANCE HAS SINCE REPLACED APU FIRE LOOP WARNING HARNESS AND PLAN TO REPLACE EGT WIRING PRIOR TO MEL EXPIRING 02 MAR.03. AIRCRAFT HAS RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2L72 4F4 F A16WE E2EA 20030821001592003082100159NM 2003 8 21 03FDEA01164 120030723A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT O/B FLAP (FLAP SIDE) I/B HINGE I/B AND O/B ACTUATOR HOLES CORRODED. RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE I/B AND O/B ACTUATOR HOLES REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030821001652003082100165NM 2003 8 21 03FDEA01029 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 FRAME DENTED BS 500 STR 24L. REPAIRED DENTED FRAME AT BS 500, STR 24L PER SRM 51-40-3. 2L73 4F RTA3WE 20030821002312003082100231EA 2003 8 21 COMA0360364 120030809A4990 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA APU DIRTY A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01446CA 7546 FLIGHT 5711 APU OIL PRESSURE CAUTION MESSAGE. CLEANED OIL PRESSURE SWITCH AND OPERATED APU WITH NO FAULTS. 2L72 4F RTA21EA 20030821002622003082100262NM 2003 8 21 USAASB03125 120030801A3350 SOCKET BOEING737 7373B7 1384580NM CABIN SHORTED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19515AU 23701 CLT - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. MAINTENANCE FOUND THE LIGHT SOCKET SHORTED. REMOVED AND REPLACED LIGHT SOCKET AT SEAT ROW 12 AND REPLACED BATTERY PACK, P/N 2013-1A, AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030822000902003082200090CE 2003 8 22 DXTA200300049 120030615A4920RE100XL APU CESSNA560 560XL 2076702CE APU BAY FAILED E DXTAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07605QS 5605321 DURING CLIMBOUT SMOKE WAS NOTICED IN THE COCKPIT AND CABIN. APU FAIL LIGHT ILLUMINATED AND APU SHUTDOWN. FOUND APU OIL QTY EMPTY, RESERVICED & OIL LEAKS INTO APU INLET. ALSO FOUND METAL ON MAGNETIC OIL PLUG. REMOVED AND REPLACED APU IAW CESSNA 560 MM & HONEYWELL RE100XL MM. 2L72 4F RTA22CE 20030403000962003040300096EU 2003 4 3 DHL2003367002 120030327A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01367DH 265 BATT. SMOKE LIGHT AND SMOKE LIGHT ON MWP ILLUMINATED. EMERGENCY CHECKLIST COMPLETED. RETURNED TO GSO. REMOVED AND REPLACED BATT. SMOKE DETECTOR, IAW A300 M/M 26-11-11. REMOVED AND REPLACED ELECTRIC SMOKE DETECTOR BOX IAW A300 M/M 26-11-11 & SMOKE DETECTOR SYSTEM OPS CHECKED GOOD IAW A300 M/M 26-11-00. 2L72 4F RTA35EU 20030625001242003062500124EU 2003 6 25 03FDEA00378 120030403A78307065M93G10 PANEL AIRBUS310 A310 EU THRUST REVERSER DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 1 ENGINE O/B T/R TRANSLATING COWL, LWR AFT LINER DELAMINATED. REMOVED AND REPLACED NR 2 ENGINE T/R TRANS COWL IAW MM 78-32-11-4-B. 2L72 4F RTA35EU 20030404000352003040400035EU 2003 4 4 03FDEA00380 120030403A5420 RIB AIRBUS310 A310 EU NR 1 PYLON DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 1 ENG PYLON HYD CASE DRAIN LINE HAS ELONGATED HOLE THRU FRAME AT RIB 20 AND HAS CHAFED THRU ADJACENT ANGLE. R & R STRAP, RIB AND DOUBLER PER IAW SRM 51-40-21 2L72 4F RTA35EU 20030416002602003041600260NM 2003 4 16 QXEA0300436 120030405A5420 STIFFENER BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 NR 2 ENGINE LOWER NACELLE LONGITUDINAL STIFFENER JUST TO THE RT OF THE ICE DOOR IS CRACKED ON THE AFT END. REPAIRED IAW RD8/4-71-016. 2H72 4T RTA13NM 20030424001072003042400107WP 2003 4 24 MWEA030146 120030326A53109912243227 SHEAR TIE DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 SHEAR CLIP IS CRACKED AT FRAME STATION 1309 ABOVE LONGERON 16 LEFT. LOCATED, DRILLED AND INSTALLED SHEAR CLIP. 2L72 4F A6WE 20030424001002003042400100EA 2003 4 24 SWIA200311841 120030320A3250 LINK CNDAIRCL600 CL6002B19 1900309EA NLG DISCONNECTED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07926SW 7687 AFTER TAKEOFF, WHEN THE GEAR WAS RETRACTED, RECEIVED NOSE DOOR, GEAR DISAGREE, WOW INPUT, AND NWS STRG MESSAGES. RETURNED COS. FOUND NR 1 AND NR 2 NOSE TIRES DEBRAIDED DUE TO NOSE LINK DISCONNECTED. INSTALLED SERVICEABLE NR 1 AND NR 2 NOSE TIRE ASSEMBLIES. INSPECTED NOSE LINK FOR DAMAGE. NONE NOTED. OPS CHECK GOOD. 2L72 4F RTA21EA 20030428001402003042800140NM 2003 4 28 CALA0300182 120030407A5753 SKIN BOEING737 7373T0 1384582NM NR 2 TE FLAP DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND NR 2 MID FLAP SKIN DENTED AT LEADING EDGE CENTER. REPAIRED IAW SRM 57-53-01. 2L72 4F RTA16WE 20030428001302003042800130WP 2003 4 28 ZW0A0303901 120030406A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139617R 53564 THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 20 TO 23. RESEATED THE BATTERIES IN THE BATTERY PACK. CHECK-C 9-11-02 STL. 2L72 4F RTA6WE 20030429000582003042900058WP 2003 4 29 EIA2003055 120030408A5210 CROSSBEAM DOUG DC9 DC915F 3022037WP PAX DOOR CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09916F 47044 L1 DOOR CROSSBEAM 2ND FROM TOP .5 INCH CRACK AT FWD END IN RADIUS. REPAIRED L1 DOOR CROSSBEAM, BLENDED EDGE AO PART REF DC9 SRM 53-01 FIG 1, STOPPED DRILLED CRACK PER DC9 SRM 52-05 FIG 3, HF EDDY CURRENT PER DOUGLAS SOP 51-06-07, NO CRACKS NOTED. 2L72 4F A6WE 20030429000022003042900002 2003 4 29 MWEA030164 420030409A31404081570906 DISPLAY BOEING717 717200 1383700NM COCKPIT FAILED A MWEAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL31903ME 55167 ON CLIMB TO FLIGHT LEVEL 310 THE AUTO-PILOT & THROTTLES WENT OFF FOLLOWED BY LOSS OF INDICATION ON THE ELECT, HYDRAULIC, AIR AND FUEL. REMOVED AND REPLACED VERSATILE INTEGRATED AVIONICS UNIT (VIA). 2L72 4F TRA6WE 20030429001022003042900102EU 2003 4 29 61841 120030411A243023080031 GENERATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT DEFECTIVE A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17138SD3344 1200 138 461 FLIGHT 4495 PIT-LEX, DURING FLIGHT THE CREW NOTICED THAT THE EMERGENCY POWER LIGHT WAS ILLUMINATED. THE CREW FOLLOWED THE QRH AND NOTICED THAT THE LT DC GENERATOR VOLTAGE WAS LOW. THE GENERATOR WAS SECURED, AND THE WARNING LIGHT WENT OUT. A/C 138 TURNED AROUND AND LANDED IN PIT. A/C TAKEN OUT OF SERVICE 4-11-03 AT 1232. PIT MX TROUBLESHOOTING PROBLEM. PIT MX REMOVED AND REPLACED THE LT DC GENERATOR. PERFORMED OPERATIONAL TEST OF DC GENERATION SYSTEM. OPS CHECKS GOOD AT THIS TIME. 2L72 4T4 TRTA52EU E8NE6 20030430001872003043000187NM 2003 4 30 SWAA030892 120030421A2560P2070001 FLASHLIGHT BOEING737 7373L9 1384470NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER MM. 2L72 4F RTA16WE 20030501000272003050100027EA 2003 5 1 ASOA03113 120030315A3350100865 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11860AS 7433 DURING A GROUND INSPECTION IN DFW, THE MID AND AFT CABIN EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY CHARGER AND BATTERY PACK (S/N 20131A). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030502000362003050200036WP 2003 5 2 ASAA0380143 120030222A52805930583217 DOOR DOUG DC9 DC982 3022082WP MLG CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, LEFT MLG DOOR AFT OUTBOARD CORNER WAS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05. (M) 2L72 4F A6WE 20030513000652003051300065NM 2003 5 13 CALA0300237 120030510A5320 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2746625 27529 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 380-400, BL 0. THE INTERCOSTAL WAS REMOVED NAD REPLACED IAW SRM 53-30-51. 2L72 4F RTA16WE 20030509000702003050900070CE 2003 5 9 JEM2003F00000 120030415A55003361001013 TRIM TAB BEECH 36 A36 1151604CE CONT O550 IO550* SO LT TRIM TAB HORNMISMANUFACTURED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01267EA E3466 2 EACH NR 4 RIVETS WHICH HELP HOLD TRIM TAB HORN TO TRIM TAB, WERE MISSING, AND HOLES HAD NOT BEEN DRILLED FOR RIVETS. 1L71 3O3 O 3A15 E3SO 20030514000282003051400028EA 2003 5 14 ASOA03131 120030327A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA ASOAO OTHER N FALSE WARNING CRCRUISE 1 SO11849AS 7347 DURING CRUISE FROM JAN-DFW - THE CREW RECEIVED A BRIEF 'SMOKE TOILET' AMBER CAUTION MESSAGE WHICH SUBSEQUENTLY CLEARED ITSELF. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514001522003051400152 2003 5 14 SWAA031052 420030508A256565C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE GIRT BAR AFT HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20030602001502003060200150 2003 6 2 SWAA031138 420030520A25656567380 LENS BOEING737 7373H4 1384600NM SLIDE INDICATOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW LENS MISSING. INSTALLED VIEWING WINDOW LENS PER MM. 2L72 4F RTA16WE 20030604001502003060400150NM 2003 6 4 UPS03440570 120030410A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C M/D - BS 2320 FRAME CRACKED AT STRINGER 26R AS MARKED. FRAME REPAIRED AS PER SRM 51-10-03 FIG.2 AT BS 2320 STR 24R TO STR 34R AREA. 2L74 4F A20WE 20030609000512003060900051EU 2003 6 9 MALA030272 120030517A7603610627023 CONTROL QUADRANT SAAB SF340 340B 7860101EU ENGINE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15367PX 340B271 AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP, THE F1 STOP OPEN LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE REPLACED CONTROL QUADRANT IAW TASK CARD 761002. ALL SYSTEM CHECKS NORMAL SEE CONTINUATION CARD 039947, 040855 FOR DETAILS. DISC NR 1 REMOVED ALL CENTER CONSOLE TO FACILITATE FO MX/CA NR 1 INSTALLED EVERYTHING IN CENTER CONSOLE AS REQUIRED. ALL CHECK GOOD. DISC NR 2 PANEL ON SIDE OF CENTER CONSOLE REMOVED AND INSTALLED PANELS. DISC NR 3 DURING ENGINE RUNS FOR QUADRANT CHANGE, AUTOCOURSEN, APR AND CTOT INOP. MX FOUND RELAY 44KA BAD, REPLACED RELAY ALL SYSTEMS CHECK NORMAL. PN 6106-27-023. 2L72 4T RTA52EU 20030610000282003061000028NM 2003 6 10 QXEA0300648 120030520A33506038443 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH248711308 504 NR 3 EMERGENCY BATTERY POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED NO.3 EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030611000502003061100050NM 2003 6 11 CA030428009 120030428A792128E997 OIL COOLER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 1 ENGINE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) NR 1 ENGINE LEAKING OIL FROM AREA OF OIL COOLER. OIL PRESENT ON NACELLE ALL THE WAY TO THE BACK OF THE NACELLE, AND ON GEAR LEG. NO OIL WAS PRESENT DURING WALKAROUND IN BWI. NR 1 ENGINE OIL COOLER REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030611000772003061100077NE 2003 6 11 HEEA086562 120030522A62107610608000050 DAMPER SKRSKYS76 S76C 8143008NE MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03505PH 760505 MAIN ROTOR DAMPER LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 3U NCH1NE 20030612001432003061200143WP 2003 6 12 UPS03840732 120030503A5330 SKIN PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, L1 DOOR JAMB LOWER AFT CORNER CRACKED 1 EA MARKED FOUND WITH NDT. REMOVED FLOORBOARD INBOARD OF L1 DOOR FOM, CUT OUT CRACK AND FABBED DOUBLERS AND FILLER IAW DC8 SRM 53-25-0 TR 53-128 TR 53-155. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-20D. INSTALLED FLOORBOARD IAW DC8 SRM 51-3-0, INSTALLED SEAL DEPRESSOR IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20030612001962003061200196EA 2003 6 12 COMA0360253 120030531A5270 SWITCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01819CA 7415 FLIGHT 5821 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED SWITCH S102MB. 2L72 4F RTA21EA 20030521000912003052100091WP 2003 5 21 DHL2003801028 120030422A57405769857614 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING CTR L\E ZEE PAN CRACKED 3.500, STA XS 520.168. REMOVED AND REPLACED DAMAGED ZEE PAN FITTING AT STA XS 520.168 (RT WING CTR L\E IAW 51-1-21 PG 1 AND SRM 51-1-20D PG 9 AND 21. 2L74 4F RT4A25 20030523000752003052300075NM 2003 5 23 QXEA0300539 120030502A5753 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - NR 3 FLAP TRACK FAIRING BRACKET IS CRACKED. REPAIRED IAW DHC-8 Q400 SRM 51-40-15, PAGE 206. 2H72 4T RTA13NM 20030527000712003052700071WP 2003 5 27 AALA20030353 120030320A3350 SOCKET DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21570AA 49352 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030617002602003061700260NM 2003 6 17 QXEA200300602 120030430A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - FORWARD SUPPORT FLANGE FOR 262AT IS CHAFED. REPAIRED IAW DHC-8 400 RD 8/4-53-451. 2H72 4T RTA13NM 20030617003172003061700317 2003 6 17 BAQA087062 420030611A34214021541791 INDICATOR BOLKMS117 BK117A1 5626010EU COCKPIT MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME415 7243 NR 1 AND NR 2 MISCOMPARE. INSTALLED SERVICEABLE UNIT. 1G72 3U H13EU 20030619000572003061900057 2003 6 19 HEEA087208 420030609A3442MI585202 PEDESTAL BELL 412 412 1182202SW ANTENNA MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 ANTENNA FAULT ERROR CODE. COULD NOT VERIFY COMPLAINT. FOUND TILT CABLE BROKEN AND NEGATOR SPRINGS BROKEN, REPLACED CABLE, REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030623000852003062300085EU 2003 6 23 USAABA03014 120030315A3350321430 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 THE 14WL EPSU FAILED THE CAP TEST. MAINTENANCE REPLACED THE EPSU BATTERY. (M) 2L72 4F RTA46NM 20030620000452003062000045WP 2003 6 20 GTIA030381 120030515A5320 STRUCTURE DOUG DC9 DC981 3022081WP SUBFLOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 SUBFLOOR CRACKED AND HOLE PUNCTURED STATION 199 RBL 50. CUT OUT DAMGAED SECTION OF WEB. FABRICATED NEW SECTION OF WEB AND DOUBLER. INSTALLED WEB AND DOUBLER. (M) 2L72 4F A6WE 20030718000152003071800015EU 2003 7 18 USAASA03070 120030626A3350321430 BATTERY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19107US 1052 RECEIVED A 'FWD L EPSU' FAULT MESSAGE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE FORWARD LT EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030630000612003063000061 2003 6 30 BAQA087780 420030626A3160066040211411 SYMBOL GENERATOR BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101750B1 41560NE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME450 7243 SYMBOL GENERATOR AMBER FAULT, "FUNCTION NOT IMPLEMENTED", ON POWER UP. RMA: 47048. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE10 20030708001032003070800103EU 2003 7 8 AWXA200300705 120030506A5315D5347217220100 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292 RT, FORWARD FO FR 67. MAINTENANCE REMOVED FLOORBEAM BETWEEN FR 66 AND FR 68, FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6 AND 7. 2L72 4F RTA28NM 20030711000132003071100013CE 2003 7 11 GLBA2003087 120030619A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03179GL UE179 CRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED CRACK IAW BEECH SRM. 2L72 4T RTA24CE 20030710000192003071000019EU 2003 7 10 ASOA03238 120030530A7712311649902 PROBE AEROSPATR72 ATR72212 8680945EU ENGINE TORQUE INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11531AS 454 DURING APPROACH INTO ATL FROM LEX, THE CREW RECEIVED A TORQUE FLUX INDICATION ON THE LT ENGINE EXCEEDING LIMITS FROM THIRTY PERCENT TO PAST THE RED LINE. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW REDUCED LT ENGINE SPEED TO FLIGHT IDLE AT APPROXIMATELY 1,000 FT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NR 2 TORQUE PROBE ON THE LEFT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030716000952003071600095EU 2003 7 16 BAQA085214 120030702A2820SC80342 SERVO AEROSPAS365 AS365N2 8680815EU PILOT VALVE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 PILOT VALVE IS JAMMING. JUST REPAIRED AND UNIT WAS JUST INSTALLED WHEN PROBLEM OCCURRED. 1G72 3U RTH10EU 20030114001332003011400133NM 2003 1 14 SWAA030037 120030107A1430 FASTENER BOEING737 7377H4 1384404NM ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29754SW 29849 DURING SCHEDULED BC3 CHECK, FOUND LOOSE FASTENER AT FWD ENTRY DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK. REMOVED AND REPLACED FASTENER PER SRM. 2L72 4F RTA16WE 20030110000632003011000063CE 2003 1 10 NSVA200300002 120030110A27301016100195 TORQUE TUBE RAYTHN BEECH 1900 1900C 1154161CE Zone 300 WORN A NSVAK NONE O OTHER ININSP/MAINT 1 EA271503198 98 UC103 On or about 12/20/2002 aircraft N51031 (ACTT 24504.0, ACTC 39671) was in for scheduled maintenance (# 6 Detail). Mechanics found that the LH elevator torque tube (crank)was worn where the rivets secure the inner and outer portion of the torque tube together. The unit was removed and replaced IAW applicable technical data. The operational check was good and the aircraft was returned to service. On or about 01/09/2003, approximately 98 flight hours later, the same elevator torque tube (crank) installed on N15031 in December was inspected and found to be unserviceable. The rivets securing the inner and outer portions of the torque tube were loose in the same manor as the torque tube assembly that was R&R in Decemb2L72 4T RTA24CE 20030128002502003012800250SW 2003 1 28 HEEA083897 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E O OTHER O OTHER NRNOT REPORTED 1 SW03722PH NHFS4371 53288 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030130001052003013000105NM 2003 1 30 DHL2003743003 120030129A3350 BATTERY PACK BOEING727 727225 1384077NM A DHLAKO NONE OTHER OL OTHER NO TEST NRNOT REPORTED 1 SO01743DH 22438 1) MAIN ENTRY DOOR EMERGENCY LIGHTS FOUND HANGING FROM HOLDER AND WILL NOT ILLUMINATE.2) REMOVED AND REPLACED BATTERY PACK, OPS CHECKED NORMAL, MM REF. 33-50-71. 2L73 4F A3WE 20030205000522003020500052NM 2003 2 5 SROM200300020 120030121A541017310441 FAIRING BOEING737 737205 1384456NM ZONE 400 PUNCTURED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 2 ENGINE OB TR ACTUATOR FAIRING PUNCTURED ABOVE THE LOWER AFT MOUNTING HOLE. REMOVED DAMAGE AREA, FABRICATED REPAIR PART AND INSTALLED PER SRM 54-30-1 AND 51-40-2. MINOR REPAIR 2L72 4F RTA16WE 20030213001002003021300100WP 2003 2 13 2003F00072 120030105A2560 CONNECTOR LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE EVAC HORN INOPERATIVE G AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EVAC HORN AT L1 DOOR DOES NOT SOUND DURING TEST. RESEATED CONNECTOR PLUG ON EVAC BOX AT L1 AS REQUIRED. 2L73 4F4 F A23WE A12EU 20030216000082003021600008SO 2003 2 16 RAIA00302042 120030210A3030CS500060DVW RELAY EMB 145 EMB145 3260210SO SHORTED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03807HK 145119 5250-MSN- SMOKE IN CABIN, PITOT 2 INOP WARNING. MAINTENANCE REMOVED K0054 RELAY FOR #2 PITOT HEAT SYS, OPS CK OK. 2L72 4F RTT00011AT 20030218002732003021800273SO 2003 2 18 CXA03SH002 120030218A530014521721005 GUSSET EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV-DURING C CHECK FOWARD FLOOR GUSSET WAS FOUND TO HAVE NUMEROUS AREAS OF CORROSION AND GOUGING. MAINTENANCE REMOVED DAMAGE AREAS AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 51-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030219000232003021900023 2003 2 19 ZDU2003F00000 420030201A2562300011 ELT CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA CABIN FAILED D ZDUSK NONE L NO TEST ININSP/MAINT 1 WP075173V445 172S9046 L3022051A DURING ROUTINE MECHANIC CHECK, ELT REMOTE SWITCH FOUND INOPERATIVE, FAILURE TRACED TO ELT ITSELF. ALL UNITS FAILED REMOTE TEST BETWEEN 400-600 HOURS. ALL OTHER ELT FUNCTIONS, NORMAL. 1H71 3O3 ONT3A12 1E10 20030220000562003022000056WP 2003 2 20 ABXA030057 120030127A323257155835001 ACTUATOR DOUG DC8 DC861 3021952WP RT MLG WW DEFECTIVE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23849AX343 45891 WHEN GEAR WAS RETRACTED AFTER TAKE-OFF, LANDING GEAR UNSAFE LIGHT REMAINED ON. RT MLG DOOR INDICATED NOT LATCHED. CYCLED GEAR PER ILN MAINTENANCE REQUEST. NO CHANGE IN PROBLEM. REPLACED RT MLG DOOR ACTUATOR IAW DC-8 MM 32-31-05. ADJUSTED FOLLOW-UP HITCH IAW DC-8 MM 32-31-05. OPS CHECKED GOOD. 2L74 4F 4A25 20030221000202003022100020NM 2003 2 21 AWXA200300068 120030105A5754 SKIN BOEING737 737300 1384610NM LE SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C-14 CHECK THE NR 2 SLAT INBOARD AND OUTBOARD WEDGES WERE FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 SLAT IAW BMM 27-81-21, PG. 401-419; OPERATIONAL TEST AND ADJUSTMENT COMPLIED WITH BMM 27-81-00, PG. 513-530. 2L72 4F RTA16WE 20030221000672003022100067NM 2003 2 21 AWXA200300086 120030128A3350900835A BATTERY BOEING737 737277 1384570NM SEAT ROW 11 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 FLIGHT CREW REPORTED THE OVER WING EMERGENCY EXIT ISLE LIGHTS COMES ON WITH EMERGENCY LIGHTING SWITCH IN OFF POSITION, AND LIGHTS GO OUT WHEN GROUND POWER IS APPLIED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK UNDER SEAT ROW 11 LT, OPERATIONAL CHECK IS GOOD. 2L72 4F RTA16WE 20030221000792003022100079NM 2003 2 21 AWXA200300173 120030127A5313146N5417 STRINGER BOEING757 7572S7 1384962NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW0 0 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 1/2" CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOOR BOARD STRINGER L/H SIDE OF CENTER LINE, BS 1475. MAINTENANCE REMOVED DAMAGED ARM OF SUPPORT STRINGER BS 1475; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030625000972003062500097NM 2003 6 25 F3LA200300077 120030219A5347 SEAT TRACK BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT NUTCLIP HOLES, RT. SIDE BETWEEN FLOORBEAM AT STA. 986.5 TO STA. 1016. REPLACED SEAT TRACK PER SRM 53-10-01, FIG. 3, SRM 51-30-02, MM 51-21-41 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030225000552003022500055SW 2003 2 25 HEEA084277 120030211A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T2 28101 MAIN BATTERY WEAK. 2G72 4U H10SW 20030304000742003030400074NM 2003 3 4 DLM88030083 120030122A5312991008893 BULKHEAD DOUG MD88 MD88 3023688NM FS 95 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27932DL 49719 FUSELAGE / BULKHEAD / NLG WHEEL WELL / RH SIDEWALL / FS 94 :WEB REPAIR THE WEB OF THE RH NOSE LANDING GEAR WHEEL WELL BULKHEAD WAS GOUGED BY A GEAR STEARING ACTUTATOR DURING A GROUND TUG OPERATION. THE GOUGE WAS REMOVED WITH A CUTOUT IN THE BULKHEAD WEB AND REPAIRED WITH AN ALUMINUM AND TITANIUM REPAIR DOUBLER PER ER/A 384387-14, REV A. 2L72 4F RTA6WE 20030115001022003011500102SW 2003 1 15 ALGA082954 120030113A5302206030446001F FITTING BELL 206 206B3 1181506SW TAILBOOM CRACKED H ALGAK NONE O OTHER ININSP/MAINT 1 FS011078Y15510 2924 FOUND TAILBOOM FITTING CRACKED COMPLETELY THROUGH WHERE LT AFT 90 DEGREES GEARBOX STUD ATTACHES. 1G71 3U H2SW 20030204002822003020400282NM 2003 2 4 F3LA200300014 120030118A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 294.5 CORRODED IN SEVERAL AREAS FROM BL 0 TO RT MOPSILL. DETERMINED CORROSION ON FLOORBEAM AT STA 294.5 FROM CENTER TO LBL 12 TO BE OUT OF LIMITS PER SRM 53-10-15. REPAIRED FLOORBEAM UPPER CHORD FROM LBL 22 TO RBL 59 PER SRM 53-10-51, FIG 205, SRM 51-40-2 AND SOPM 20-41-02. 2L72 4F RTA16WE 20030127001432003012700143SW 2003 1 27 HEEA083681 120030115A3212206050247137 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20030127002392003012700239SW 2003 1 27 HEEA083722 120030115A6310206340300107 DRIVE SHAFT BELL 407 407 1182206SW M/R GEARBOX CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 MAIN ROTOR DRIVE SHAFT FLEX FRAMES ARE CORRODED. 1G71 3U O H2SW 20030128000782003012800078SW 2003 1 28 HEEA083832 120030116A6230406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03741PH 53457 MAIN ROTOR SWASHPLATE LINK ASSY HAS CORROSION. 1G71 3U O H2SW 20030128002512003012800251SW 2003 1 28 HEEA083898 120030117A6720 BEARING BELL 407 407 1182206SW LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH NHFS4445 53288 TAIL ROTOR LINK BEARING WORN. 1G71 3U O H2SW 20030204002162003020400216NM 2003 2 4 SWAA030162 120030122A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 907, STR 10R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030207000202003020700020NM 2003 2 7 DLM88030061 120030114A3350RPS1 POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27910DL 49541 ON L/O INSPECTION, AFT EMERGENCY ISLE EXIT LIGHTS WILL NOT TEST. REPLACED POWER SUPPLY 2L72 4F RTA6WE 20030116000672003011600067SW 2003 1 16 HEEA083026 120030106A6520PHI2062003 SEAL BELL 206 206L3 1182108SW T/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0381671 51301 TAIL ROTOR GEARBOX SEAL LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030117000942003011700094NM 2003 1 17 2003UALA00020 120030107A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 887 FRAME CRACKED AT RIVET HOLE NEAR STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030117001402003011700140SW 2003 1 17 HEEA083210 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 ACTUATOR INOPERATIVE. 1G71 3U H2SW 20030304000442003030400044SW 2003 3 4 HEEA084578 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R A1917A2615 36007 MAIN ROTOR MAST LINK HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030307001292003030700129WP 2003 3 7 AALA20030101 120030120A5320 STRUCTURE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21598AA 53288 TUL - FOUND FS 1418 CRACKED AT 2R. INSTALLED DOUBLER PER 53-01-00 AND AARD 53-10-00-15. (M) 2L72 4F RTA6WE 20030307001432003030700143NM 2003 3 7 AALA20030123 120030130A33500201922001 LIGHT BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21328AA 22328 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030311000212003031100021SW 2003 3 11 HEEA085042 120030228A3246206323004 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N 51512 SKID TUBE HAS CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE TUBE. 1G71 3U H2SW 20030313001092003031300109CE 2003 3 13 DBC2003F00000 120030210A323311238002221 ACTUATOR BEECH 200 B200 1152922CE PWA PT6 PT6A6 52043EA NLG INOPERATIVE E DBCAO OTHER J WARNING INDICATION APAPPROACH 1 GL132618C325 BB1757 ACTURATOR, ON APPROACH, PILOT SELECTED GEAR DOWN. PILOT FELT NOSE GEAR TOOK LONGER THAN NORMAL TO REACH DOWN AND LOCKED POSITION. LANDING GEAR RETRACT TEST COMPLIED WITH. NOSE GEAR EXTEND TIME WAS FOUND TO BE OUT OF LIMITS IAW MM. NOSE GEAR ACTUATOR REPLACED (W/O 455347). LANDING GEAR RETRACT TEST OPERATIONS CHECKED NORMAL. 1L72 4T3 T A24CE E4EA 20030121000402003012100040SW 2003 1 21 HEEA083232 120030108A7603206064713103 POWER LEVER BELL 206 206L3 1182108SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 POWER LEVER WORN. SCRAPPED. 1G71 3U H2SW 20030122000422003012200042SW 2003 1 22 HEEA083429 120030109A3411AN58131 PITOT TUBE BELL 206 206L3 1182108SW PITOT STATIC SYSCRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 PITOT TUBE BENT AND CRACKED. SCRAPPED. 1G71 3U H2SW 20030314001432003031400143EA 2003 3 14 COMA0360143 120030311A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01916CA121451702 7014 FLIGHT 5130 NLG FAILED TO RETRACT WHEN GEAR SELECTED UP. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20030317000502003031700050NM 2003 3 17 03FDEA00186 120030225A5753 STRUCTURE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 FOUND LT WING OUTBOARD HINGE FLAP SIDE PIVOT HOLE CORRODED, AFTER REMOVAL OF BUSHINGS. 2L73 4F4 FRTA22WE E13NE 20030317000842003031700084NM 2003 3 17 03FDEA00245 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 3R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030318001022003031800102WP 2003 3 18 ASAA0380038 120030104A53209936632504 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, INTERCOSTAL IS CORRODED AT FS 541, 29R. CUT OUT AND REPLACED CORRODED SECTION WITH FILLER AND DOUBLER PER SRM 51-70-5. (M) 2L72 4F RTA6WE 20030319000022003031900002WP 2003 3 19 GTIA030002 120030111A3222 STRUT DOUG DC9 DC982 3022082WP NLG UNDERSERVICED A GTIAO OTHER O OTHER LDLANDING 1 GL23804NK 49104 DTW - FLT 1691 - AIRCRAFT OVERWEIGHT LANDING. NOSE GEAR DOORS DID NOT CLOSE, COMPLIED WITH QRH AIRCRAFT WEIGHT 137,000 LBS. INSPECTED NOSE GEAR, FOUND NOSE STRUT TO REQUIRE SERVICING. SERVICED NOSE STRUT, PERFORMED GEAR SWING. NO FAULTS NOTED AT THIS TIME. (M) 2L72 4F A6WE 20030327000382003032700038NM 2003 3 27 AWXA200300310 120030228A5320146N53236 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON SUPPORT ANGLE ON UNDER SIDE OF SHEAR DECK AT BS 1701-1720, RBL 60. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT BS 1701-1720, RBL 60; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 146N5323-6. 2L72 4F RTA2NM 20030324000152003032400015NM 2003 3 24 2003UALA00266 120030110A2730 BUSHING BOEING777 777222 1385219NM PWA PW4077PW4077 NE JACKSCREW CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29777UA 26916 HORIZONTAL STABILIZER JACKSCREW BUSHING FOUND TO BE DAMAGED/CRACKED. DURING SHOP INSPECTION, JACKSCREW BUSHING FOUND TO BE DAMAGED AND/OR CRACKED WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20030418000162003041800016EU 2003 4 18 MALA030154 120030213A3080 WARNING LIGHT SAAB SF340 340B 7860101EU DE-ICE SYSTEM ILLUMINATED A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15453XJ 340B453 ICE PROTECTION ON CWP ILLUMINATED WITH DE-ICE OVERTEMP ON OHP. LIGHTS GO OUT AT LOWER POWER SETTINGS. AIR RETURN TO MEM. MAINTENANCE COULD NOT DUPLICATE. 2L72 4T RTA52EU 20030418001202003041800120NE 2003 4 18 QXEA0300293 220030218A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX3454 10024 GEE965244 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR BLADES BROKEN. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2L72 4F4 FRTA21EA EOOO63EN 20030327001662003032700166SO 2003 3 27 C2XA03SH046 120030310A531014522226003 BUTT STRAP EMB 145 EMB145LR 3260212SO LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK CENTER BUTTSTRAP AT LAV WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030422001332003042200133 2003 4 22 SWIA200311823 420030227A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07449SW 7699 WINDSHEAR FAIL STATUS MESSAGE ILLUMINATES DURING FLIGHT. MESSAGE WENT CLEAR AFTER LANDING. FAULT HISTORY SHOWED FCC CARD FAULTS. REMOVED AND REPLACED FCC 4000 IN IAPS CARD CAGE IAW MM 22-12-14. PERFORMED OPS CHECK IAW MM 22-11-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20030423000192003042300019NM 2003 4 23 AUS20030302 120030212A5311 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME BS 950E CONTAINED LEVEL 2 CORROSION ON LOWER FLANGE IN AREA LOCATED BETWEEN STRINGER 28L AND STRINGER 29L. FOUNDDURING CPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030423001242003042300124WP 2003 4 23 UPS03840276 120030311A2611 BATTERY DOUG DC8 DC873F 302199FWP FIRE DETECTOR DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:N/A REF: M256103 P33 LOWER CARGO FIRE DET INOP. DETECTOR BATTERY AC1296 ZERO DH. REMOVED AND REPLACED BATTERIES PER MM 26-18-02. OP GOOD, DEFERRAL CLEARED. 2L74 4F RT4A25 20030321000262003032100026NM 2003 3 21 2003UALA00181 120030215A2934 SENSOR BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 1 HYD SYSTEM MALFUNCTIONED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP29603UA 21864 LEFT HYDRAULIC QUANTITY LIGHT ILLUMINATED. QUANTITY LEVEL .02. QUANTITY RETURNED TO NORMAL AFTER LANDING. REPLACED HYDRAULIC QUANTITY MONITORING UNIT. VENDOR SHOP FINDINGS IDENTIFIED LEFT CHANNEL INOP. 2L72 4F4 FRTA1NM E3NE 20030730001022003073000102SO 2003 7 30 SIMA200314804 120030515A532014521725013 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21646AE 145213 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOND TO BE CORRODED BELOW SRM LIMITS AROUND A FASTENER HOLE. BLENDED THE CORRODED AREA AND PERFORMED NON DESTRUCTIVE TESTING WITH NO CRACK INDICATIONS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 21) CHAPTER 51-40-02/06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE NR EM-53-036R1. (M) 2L72 4T RTT00011AT 20030731001182003073100118NM 2003 7 31 QXEA200300759 120030621A33506138001 BATTERY PACK BOMBDRDHC8 DHC8401 1390041NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09402QX811 4032 PDX-OVERHEAD EMERGENCY LIGHTS AT ROW 9, 13, 16, EXIT SIGN BEHIND SEAT 18D, AND EXIT SIGN IN AFT GALLEY FAIL TO ILLUMINATE WHEN SELECTED ON. REPLACED EMERGENCY POWER SUPPLY UNIT. REPLACED EMERGENCY LIGHT BATTERY LT3/RT3. OPERATIIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030731001262003073100126NM 2003 7 31 QXEA200300777 120030625A5230 DOUBLER BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX- AFT CARGO DOOR LOWER FORWARD CORNER INNER DOUBLER IS DAMAGED. REPAIRED IAW HORIZON AIR EA 6-52-297. 2H72 4T RTA13NM 20030828000852003082800085NM 2003 8 28 DLM88030682 120030721A2421 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE LT ENGINE DAMAGED A DALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SO27978DL29556 53259 178238 A C LOCKOUT WITH LT GEN INOP MESSAGE IN FLIGHT - FOUND GENERATOR WINDINGS COMING APART - REPLACED LT CSD AND GEN. 2L72 4F4 FRTA6WE E2EA 20030829002042003082900204WP 2003 8 29 GTIA030620 120030722A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND FORWARD CARGO FS 427 WEB CORRODED AND HAS DOUBLE DRILLED HOLES STRINGER 28R-24R. CUTOUT DAMAGED WEB. FABRICATED NEW WEB SECTION. FABRICATED REPAIR DOUBLER. INSTALLED NEW WEB SECTION AND REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20030828001792003082800179NM 2003 8 28 SWAA031849 120030817A57536546434369 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C1 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030721000042003072100004NM 2003 7 21 AUS20030560 120030606A2497 WIRE BOEING767 767* NM RROYCERB211 RB211524* NE ELECTRICAL POWERBURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 AUS (AUS) ELECTRICAL WIRING LOCATED IN THE MEC AT THE REAR OF THE E3 PANEL ARCED AND BURNED. CAUSED BY PANEL RETAINING SCREW CHAFING ON 115 VOLT AND 28 VOLT WIRING OF THE LEFT TRU. 2L72 4F4 FRTA1NM E12EU 20030722000102003072200010NM 2003 7 22 2003F00438 120030124A5514 HINGE PIN BOEING727 727222 1384073NM HORIZONTAL STABCORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND HORIZONTAL STAB, RIGHT INNER HINGE PIN, HAS CORROSION ON THREADED END. REMOVED AND ERPLACED RIGHT INNER HINGE PIN. (M) 2L73 4F A3WE 20030721001422003072100142NM 2003 7 21 DHL2003742011 120030708A3260 INDICATOR BOEING727 727225 1384077NM MLG MALFUNCTIONED A DHLAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01742DH 21290 UPON GEAR EXTENSION HAD 3 GREEN, 3 RED LIGHTS, AND DOOR LIGHTS. S/O PANEL HAD MAIN GEAR GREEN, AND TAIL SKID LIGHT ON. BELOW 500 FT GPWS ANNOUNCED TOO LOW GEAR, AFTER GO AROUND CYCLED GEAR, ALL INDICATIONS NORMAL AND LANDED. UPON TAXI IN LEFT GREEN GEAR LIGHT WENT OUT TEMPORARILY AND CAME BACK ON. OPS CHECKED GEAR SYSTEM PER M/M 32-71-01. ALL LIGHTS INDICATED NORMAL ON GROUND. MAINTENANCE CONTROL ADVISED. 2L73 4F A3WE 20030801000142003080100014WP 2003 8 1 GTIA030532 120030618A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD LAV INBOARD SECTION FLOOR PANEL DELAMINATED AND CORRODED AROUND EDGES. REPAIRED DELAMINATION. (M) 2L72 4F A6WE 20030806000982003080600098SO 2003 8 6 C2XA03TY112 120030801A534714530658009 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK RF5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20030812000182003081200018NE 2003 8 12 HEEA088437 120030724A6210 RIB SKRSKYS76 S76C 8143008NE M/R BLADE TIP DELAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH A08602519 760505 MAIN ROTOR BLADE TIP RIB DELAMINATION. 1G72 3U NCH1NE 20030829001432003082900143NM 2003 8 29 SWAA031837 120030815A335007912 COVER BOEING737 7372T4 1384492NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVERS MISSING AT ROW'S NR 7, NR 8 AND NR 21. INSTALLED COVERS PER MM. 2L72 4F A16WE 20030904001612003090400161WP 2003 9 4 DHL2003873597 120030701A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING CTR L/E OUTER PLATING SHOWS CORROSION AROUND XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS & EXSITING DOUBLER. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN SEGMENT. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER AND TWO FILLERS EACH IAW EODHL-030626, ED-3458. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE AND FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLER AND FILLERS ON LT WING CTR L/E OUTER PLATING (AROUND STA. XW.257.500) USING NEW FASTENERS IAW EODHL-030626, ED3458, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030813000972003081300097SO 2003 8 13 SWIA200312101 120030609A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT FAILED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07560SW7035 7035 120334 FLOOR LEVEL EMERGENCY LIGHT BULBS DO NOT ILLUMINATE AT ROWS 3, 4, 5. REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY. 2L72 4T RTA31SO 20030728000622003072800062 2003 7 28 SWAA031637 420030723A2565D31354 SLIDE BOEING737 7373G7 1384595NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030729000192003072900019EU 2003 7 29 03200333 120030719A3350OL3071BPEGPL LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27333UE 41101 DURING MAINTENANCE INSPECTION, 2 FWD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LAMPS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4T RTA41NM 20030826001212003082600121NM 2003 8 26 03FDEA00936 120030620A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25487FE 21490 N00389 CORROSION AFT CARGO BAY, STA 950C TO 950F STR 29L HAS CORROSION. REPAIRED LT KEEL BEAM STR 29L IAW FED EX E.A. 7-5310-54856. 2L73 4F RTA3WE 20030930000032003093000003NM 2003 9 30 QXEA200301063 120030906A2810 FLOW DIVIDER DHAV DHC8 DHC8202 2809007NM ZONE 400 LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09364PH 524 FUEL LEAK ON NR 2 ENGINE RIGHT BELOW FUEL FLOW DIVIDER. REPAIRED IAW DHC-8 SRM 71-00-02 AND 72-01-40. 2H72 4T RTA13NM 20031002000282003100200028NM 2003 10 2 AMTA200301147 120030908A335070036611 BALLAST BOEING737 73783N 13844HINM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11325TZ 32884 FOUND LEFT MIDDLE FORWARD WINDOW EXIT SIGN LIGHT, ABOVE THE OVERWING EXIT IS INOPERATIVE. REMOVED AND REPLACED LEFT FORWARD OVERWING EXIT LIGHT ASSEMBLY IAW MM 33-21-00-2. OK FOR SERVICE. (M) 2L72 4F RTA16WE 20031002000482003100200048WP 2003 10 2 UPS03841204 120030825A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE NICKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, DEEP NICKS ON FUSELAGE SKIN AT STATION 520 LONGERON 25R, BLENDED OUT NICKS, FOUND OUT OF LIMITS, NDT VERIFIED NO CRACKS AT BLENDOUT AREAS. FABRICATED AND INSTALLED REPAIR DOUBLERS AT B-PIT UPPER FORWARD DOOR CORNER I.A.W. SRM. 53-2-0 FIG. 20,53-2-0 FIG. 1F. 2L74 4F RT4A25 20031002001732003100200173NM 2003 10 2 375PA0020 120030912A335020131A BATTERY PACK BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 EMERGENCY LIGHTS INOPERATIVE AT FIRST 4 SEATS AND AT OVERWING SECTION. REPLACED BATTERY PACK AT RIGHT SIDE OF CABIN AND AT OVERHEAD COMPARTMENT. 2L72 4F RTA16WE 20030908002912003090800291NM 2003 9 8 SWAA031940 120030830A25606557463 BRACKET BOEING737 7373A4 1384585NM AFT ENTRY OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR WOULD NOT LOCK PROPERLY AT FLOOR BRACKETS. REPAIRED FLOOR BRACKETS PER SWA EA. 2L72 4F RTA16WE 20030909001702003090900170EU 2003 9 9 HE66088883 120030825A249745023501 CONTROL BOX UROCOPEC135 EC135T1 5620026EU NR 2 SYSTEM DEFECTIVE B HEEAH DEACTIVATE SYST/CIRCUITS S AFFECT SYSTEMS APAPPROACH 1 SW03135CR1068 0164 NR 2 MASTER ELECTRICAL BOX FAILED DURING LANDING, REPLACED 1G72 3U H88EU 20031003000142003100300014NE 2003 10 3 AALA20030942 220030902A7200 ENGINE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 2 FAILED A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW213075A 606 695219 AIRBUS REPORTED NR 2 ENGINE COMPRESSOR STALL, DECLARES AN EMERGENCY AND LANDS SAFELY. FOUND METAL IN TAILPIPE OF ENGINE. ENGINE CHANGED OUT AT SJU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA35EU E13NE 20031002001522003100200152EU 2003 10 2 03FDEA01519 120030911A5610NP1752331 WINDOW AIRBUS310 A310 EU COCKPIT CRACKED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25447FE 251 AFT EDGE OF CAPT'S SIDE VIEW WINDOW GLOWED WHITE HOT IN TWO SPOTS. THERE WAS A NOTICABLE BURNING ODOR AND A SMALL AMOUNT OF SMOKE. TURNED OFF WINDOW HEAT AND BURNING STOPPED. RETURNEDTO MEMPHIS. FOUND CRACK IN WINDOW. REMOVED AND REPLACED LEFT FIXED SIDE WINDOW IAW M/M 56-11-12-4 OPS CK IAW M/M 30-42-00-5 GOOD OK FOR SERVICE PER MTSI WRI 56-10-6335 ALSO REMOVED AND REPLACED CONTROLLER 19DG AND PROTECTION UNIT 87DG ALSO CK GOOD PREMATURE REMOVAL/INSTALLATION OFF MFG NP175233-1 POS LT SRL 94168H8065 TAG 928284 ON MFG NP175233-1 SRL 03037H5905 TAG 830268. 2L72 4F RTA35EU 20031003000472003100300047NM 2003 10 3 AWXA200301051 120030812A541065479681 ANGLE BOEING737 737277 1384570NM NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1 1/8 INCH CRACK WAS FOUND ON NR 1 ENGINE RT FORWARD COWL LOWER ZEE ANGLE AT RIB 7, NAC STA 151. MAINTENANCE CUTOUT CRACK ON RIB 7; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 54-40-03, FIG. 001. 2L72 4F RTA16WE 20031014000952003101400095NM 2003 10 14 SWAA032148 120030924A3350 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 EEPLS COVER BROKEN AT ROW NR 1. REMOVED AND REPLACED EEPLS LIGHT UNIT AT ROWS NR 1 AND NR 2 PER MM. 2L72 4F RTA16WE 20030306000112003030600011 2003 3 6 HEEA084724 420030217A2340AA21400 SIREN BELL 412 412 1182202SW CABIN INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 INTERNAL PA INOPERATIVE. 1G72 4U H4SW 20030306000432003030600043SW 2003 3 6 HEEA084757 120030218A3210400052015101 STRAP BELL 407 407 1182206SW MLG CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 STRAP CHAFED FROM LANDING GEAR SHIFTING OVER. REPLACED STRAP. 1G71 3U O H2SW 20030306001122003030600112SW 2003 3 6 HEEA084819 120030221A6220412310400101 ROD BEARING BELL 412 412 1182202SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 M/R HEAD HAS A WORN ROD BEARING. REPAIRED. 1G72 4U H4SW 20030116002132003011600213SW 2003 1 16 HEEA083126 120030108A6420 BEARING BELL 206 206L3 1182108SW PITCH LINK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 TAIL ROTOR HEAD PITCH CONTROL LINK HAS WORN BEARINGS. SCRAPPED. 1G71 3U H2SW 20030116002262003011600226SW 2003 1 16 HEEA083130 120030108A6220206011117003 RESTRAINT BELL 206 206B3 1181506SW FLAP STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03103PH 3000 MAIN ROTOR FLAP RESTRAINT STICKS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030121000822003012100082WP 2003 1 21 ABXA030035 120030113A33505708458503 BATTERY PACK DOUG DC8 DC863F 302198FWP CABIN DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX675 45927 EMERGENCY BATTERY CHARGER CIRCUIT BREAKER TRIPPED. REPLACED EMERGENCY LIGHTING BATTERY PACK ASSEMBLY IAW DC-8 MM 33-50-01-2. 2L74 4F 4A25 20030121001152003012100115SW 2003 1 21 HEEA083297 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 SEAT BELT WORN AND FRAYED. 1G71 3U H2SW 20030121001952003012100195SW 2003 1 21 HEEA083339 120030109A243230135002 BATTERY BELL 206 206B3 1181506SW MAIN MALFUNCTIONED E HEEAO OTHER M OVER TEMP NRNOT REPORTED 1 SW032753F 2729 BATTERY HAS HIGH TEMP ON STARTS. REPLACED BATTERY. 1G71 3U H2SW 20030121002472003012100247SW 2003 1 21 HEEA083364 120030109A78104606AC CLAMP BELL 206 206B3 1181506SW ENGINE EXHAUST CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 ENGINE EXAHAUST CLAMP CRACKED NEAR RIVETS. SCRAPPED. 1G71 3U H2SW 20030314001242003031400124CE 2003 3 14 CJP2003F00002 120030217A261237702810 CONTROL BOX CESSNA650 650 2076802CE GE CJ610 CJ6108 30006NE TAILCONE INTERMITTENT E CJPAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM03800GM 6500077 FLIGHT CREW EXPERIENCED INTERMITTENT RIGHT ENGINE FIRE WARNING. AIRCRAFT LANDED AT INTENDED DESTINATION. MAINTENANCE TROUBLESHOT ENGINE PYLON WIRING WHICH IS THE USUAL CAUSE OF INTERMITTENT FIRE WARNINGS, AND COULD NOT RESOLVE PROBLEM. TROUBLESHOOTING MOVED INTO THE AIRCRAFT TAIL CONE WHERE THE RIGHT ENGINE FIRE DETECT CONTROL UNIT WAS DETERMINED INOPERATIVE. THE CONTROL UNIT WAS SWAPPED WITH LEFT TO CONFIRMED. A REPLACEMENT FIRE DETECT CONTROL UNIT WAS INSTALLED. SYSTEM WOULD NOT TEST. DISCOVERED CHAFED WIRE TO FIRE DETECT CONTROL IN WIRE BUNDLE WHICH CAUSED A SHORT IN ORIGINAL CONTROL. REPAIRED WIRE, TEST OF FIRE WARNING SYSTEM WAS NORMAL. 2L72 4F4 J A9NM 1E16 20030314001502003031400150CE 2003 3 14 OIZ2003F00001 120030204A53501016200301 ANGLE BEECH 1900 1900C 1154161CE HORZ/VERT STAB CRACKED A OIZAO OTHER O OTHER NRNOT REPORTED 1 WP19381CR UB69 DURING THE ACCOMPLISHMENT OF AD, A SMALL CRACK WAS FOUND IN THE LEFT VERTICAL TO HORIZONTAL STABILIZER FAIRING ANGLE. THE CRACK WAS LOCATED IN THE APPROXIMATE CENTER OF THE ANGLE AND ALONG THE UPPER SECTION (HORIZONTAL STABILIZER SIDE) OF THE BEND RADIUS. THE CRACK WAS APPROXIMATELY ONE INCH LONG AND WAS INITIALLY NOTED AS A FINE BLACK LINE. THE AREA WAS CLEANED AND A DYE PENETRANT INSPECTION WAS PERFORMED TO CONFIRM CRACK. THE ANGLE WAS REPLACED WITH A NEW PART. 2L72 4T RTA24CE 20030314001992003031400199SO 2003 3 14 030011692 120030313A5620159SCC10317 WINDOW GULSTMG1159 G1159A 3970109SO CABIN CRACKED B Y3PRK NONE O OTHER ININSP/MAINT 1 SO35477SJ 477 LT NR 1 CABIN WINDOW OUTER PANE IS CRACKED. CRACK WAS FOUND DURING FUSELAGE EXTERNAL INSPECTION. 2L72 4F A12EA 20030317000152003031700015NM 2003 3 17 03FDEA00145 120030220A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 560, RBL 3 TO RBL 23. CORROSION ON TOP OF FLOORBEAM AT BS 560, RBL 3 TO 13, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, SEALED, AND INSTALLED REPAIR CHORD IAW SRM 51-30-2, 53-10-1, 53-10-8, 51-10-2. 2L73 4F RTA3WE 20030319000612003031900061NM 2003 3 19 HALA0300012 120030113A57515910044402 SKIN BOEING717 717200 1383700NM RT WING AILERON CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP13477HA2694 55122 HNL - LEVEL 2 CORROSION ON RIGHT AILERON UNDER THE 9957571-23 RUBSTRIP IS BETWEEN XA 374.00 AND XA 382.125. THE CORROSION AFFECTED THE 995757-34 DOUBLER AND 9957571-36 SKIN. THESE 2 PARTS HAD 100 PERCENT CORROSION PENETRATION. THE AILERON WAS REPLACED PER BOEING MM. (M) 2L72 4F TRA6WE 20030319000982003031900098NM 2003 3 19 TSAA0333018 120030131A33501000679 BATTERY PACK BOEING737 7372T4 1384492NM PAX CABIN INOPERATIVE A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13808AL 23445 REPLACED AFT PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031014001932003101400193NM 2003 10 14 SWAA032104 120030921A326065C28034 SENSOR BOEING737 7373Q8 1384670NM NLG FAULTY A SWAAO OTHER J WARNING INDICATION DEDESCENT 1 SW29317WN 24068 DURING GEAR RETRACTION, NLG UNSAFE WARN LIGHT ILLUMINATED, RECYCLED GEAR AND LIGHT DID NOT EXTINGUISHED. REMOVED AND REPLACED NLG UPLOCK AND DOWLOCK SENSORS S845 AND S846. OPS CK GOOD PER MM. 2L72 4F RTA16WE 20031020002752003102000275NM 2003 10 20 03269402 120030926A33508GH00567806 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27402FJ 3147 DURING INSPECTION THE LAVATORY EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031022000032003102200003NM 2003 10 22 MWEA030383 120030922A5321993653425 FLOOR SUPPORT DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 PASSENGER ENTRYWAY FLOOR SUPPORT CORRODED AT STATION 157-200 AND 6 INCHES LEFT OF AIRCRAFT CENTER LINE. FABRICATED AND INSTALLED NEW FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20031029000032003102900003NM 2003 10 29 ASAA0340102 120030301A531065C32395 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727F RBL 10 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040129001062004012900106NM 2004 1 29 DHL2003742542 120031121A5320 INTERCOSTAL BOEING727 727225 1384077NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, UPPER LOBE INTERIOR STIFFENER BUCKLED AT STA 360 STR 5 R. REMOVED UPPER LOBE INTERCOSTAL BS 360 STR 5 RT AS REQUIRED FOR FAB NEW IAW B727 SRM 51-30-02, FABRICATED NEW WEB INTERCOSTAL MAT IDENTIFICATION 7075-T6 .032 PO 991238 DIMENSIONS 19 X 5.5 INCHES IAW B727 SRM 53-10-2 FIG 3. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW INTERCOSTAL WEB AT STA 360 STR 5 R IAW B727 SRM 51-40-2. 2L73 4F A3WE 20030728000922003072800092NM 2003 7 28 SWAA031615 120030721A335057771 CAP BOEING737 7375H4 138449DNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2L72 4F RTA16WE 20030729000932003072900093NM 2003 7 29 2003F00473 120030703A532069436952 FITTING BOEING727 727225 1384077NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07810EA 22432 AT CORROSION REPAIR INPUT, FOUND FRAME FITTING, ANGLE, CORRODED AT BS 740, RBL 16. REMOVED CORRODED FITTING. REPAIRED, DRILLED AND INSTALLED 740 RIGHT BULKHEAD FITTING IAW B727 DWG 65-15940 AND SRM 51-30-2. (M) 2L73 4F A3WE 20031112000642003111200064NM 2003 11 12 CALA0300628 120031108A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L AT STA 504. REPAIRED IAW ECRA 5310-03262. 2L72 4F RTA16WE 20031112001142003111200114WP 2003 11 12 DHL2003809004 120031108A5250 DOOR DOUG DC8 DC873F 302199FWP COCKPIT OUT OF ADJUST A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01604AL 46047 COCKPIT ENTRY DOOR JAMS AND IS VERY HARD TO OPEN FROM THE GALLEY SIDE. ADJUSTED DOOR PER SMM AND M/M 51-10-0. 2L74 4F RT4A25 20031119001332003111900133NM 2003 11 19 2003UALA00765 120031008A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29799UA 26926 EMERGENCY EXIT LIGHTS DAMAGED. SECURED SEAT EMERGENCY EXIT LIGHT. 2L72 4F4 FRTT0001SE E46NE 20031120000192003112000019NM 2003 11 20 AWXA200301228 120030922A5320BACF3F020K023N6 FILLER BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FILLER PLATE AT BS 951, RBL 44, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FILLER PLATE AND FILLER AT BS 951, RBL 44, WL 208; FABRICATED A NEW REPLACEMENT FILLER PLATE AND FILLER PER DWG 65C10592; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20031120000372003112000037NM 2003 11 20 AWXA200301246 120030927A532069353262 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT INTERCOSTAL AT STR 25 RT, BETWEEN BS 747 AND BS 767. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CARGO COMPARTMENT INTERCOSTAL AT STR 25 RT, BETWEEN BS 747 AND BS 767; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040114000892004011400089NM 2004 1 14 03FDEA01990 120031126A1430ALC8131 BOLT DOUG MD11 MD11 3023602NM FAILSAFE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 UPON REMOVAL OF BOLT 36 LT FAILSAFE FOUND BOLT HOLE INNER SURFACE WITH 03 EA GOUGES. COMPLIED WITH FEDEX EA 1-5510-74261 STABILIZERS - HORIZONTAL STABILIZER 36L FAIL-SAFE BORE GAUGED 2L73 4F RTA22WE 20040114001862004011400186EA 2004 1 14 MASA200300506 120031222A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777195 7195 CREW REPORTED THE LOWER CABIN DOOR EMERGENCY LIGHTS INOPERATIVE. MECHANIC REPAIRED THE WIRING. OP CHECKS GOOD. NO PARTS USED 2L72 4F RTA21EA 20031217002052003121700205SO 2003 12 17 SWIA200312612 120031119A2701 SHAFT EMB 120 EMB120ER 3260203SO YOKE DAMAGED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07236SW 120312 TRIED TO MOVE YOKE TO THE LT AND IT WAS BOUND UP AND WOULD NOT GO TO THE LT. REPLACED BELLCRANK SHAFT IAW MM 31-30-10. OPS CHECK GOOD. 2L72 4T RTA31SO 20031218000052003121800005NE 2003 12 18 P5CA0300991 220031116A7200 ENGINE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 2 FAILED A P5CAO OTHER O OTHER CRCRUISE 1 WP23922FT 22768 702370 NR 2 ENGINE FAILED IN FLT LOUD RUMBLE FOLLOWED BY LOSS OF POWER HIGH EGT VIBRATION OIL LOSS. REPLACED NR 2 ENG PER MM 71-00-002. 2L74 4F4 FRTA20WE E3NE 20031218001192003121800119NM 2003 12 18 2003UALA00910 120031126A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29370UA 24539 FRAME CRACKED BS 616 RT STRINGER 17R. ALSO FRAME INNER CORD CRACKED BS 616 UNDER LT STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031222000622003122200062WP 2003 12 22 ASAA0380631 120031011A532199365841 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 DURING 15K C-CHECK, FOUND CABIN FLOOR PANEL HAS SEVERAL GOUGES BETWEEN FS 1117 AND 1174. REPLACED DAMAGED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20031219001032003121900103NM 2003 12 19 2003UALA00932 120031203A5330 SKIN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29839UA 1507 LARGE DENT APPROX 1 FT BY 1 FT UNDER LT STATIC PORT. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 53-00-11 & SRM 51-47-00. 2L72 4F4 FRTA28NM E40NE 20031231000862003123100086WP 2003 12 31 GTIA030915 120031101A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND FLOOR PANEL RIGHT OUTBOARD STATION 769-826 HAT CHANNEL END CRACKED THROUGH. CUT OUT DAMAGED PORTION OF HAT CHANNEL. FABRICATED NEW HAT CHANNEL. FABRICATED SPLICE. INSTALLED HAT CHANNEL AND SPLICE. (M) 2L72 4F RTA6WE 20031006000692003100600069CE 2003 10 6 AMWA43 120030902A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07176YV UE176 RIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 STRG P/N 101-640000-42 BOTH RT SIDE AND STRG P/N 101-640000-37 STRG P/N 101-640000-45 ON LT SIDE (4 EA TOTAL CRACKS ON THIS RIB) 2L72 4T RTA24CE 20031009000192003100900019SO 2003 10 9 SIMA200320501 120030724A3350744436 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21642AE 145193 OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RAI EXIT MARKER ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031007001212003100700121EA 2003 10 7 03246680 120030903A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27680BR 7679 DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED A SATISFACTORY OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031014000132003101400013EU 2003 10 14 BAQA089602 120031004A2842L284M30C1002 PROBE UROCOPEC135 EC135P1 8680990EU FUEL CELL MALFUNCTIONED B BAQAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA03911BG935 0015 SUPPLY TANK RED LOW WARNING LIGHT ON. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20031202001382003120200138NM 2003 12 2 GAIA03115SP 120031022A5320 ANGLE BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076831 20184 DURING B-CHECK AT DFW, FOUND CORROSION ON AN ANGLE IN THE FORWARD BAGGAGE BIN AT BS 540 BY STRINGER 26R. THE CORROSION WAS REMOVED AND THE ANGLE WAS REPAIRED PER THE B727 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031202001552003120200155SO 2003 12 2 SIMA200327202 120030927A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21614AE 145086 FORWARD TWO EMERGENCY FLOOR STRIP LIGHTS INOPERATIVE AND BOTH FORWARD OVERHEAD EXIT SIGNS INOPERATIVE. RAI BATTERY POWER SUPPLY AND NR 1 EMERGENCY BATTERY POWER SUPPLY OFF, P/N 20131A AND S/N 65143, EMERGENCY BATTERY P/N 110049, S/N 13617. (M) 2L72 4T RTT00011AT 20040121000592004012100059SO 2004 1 21 SIMA200334405 120031127A531112010732001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21616AE 145092 ABI - DURING AN MBV INSPECTION, FRAME 81 WAS FOUND GOUGED BELOW SRM LIMITS. BLENDED THE GOUGE AND PERFORMED NDT INSPECTION FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB STATEMENT IC2003-145/4017 DATED NOV 27, 2003. (M) 2L72 4T RTT00011AT 20040122000822004012200082SO 2004 1 22 SIMA200329702 120031023A33502013A POWER SUPPLY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT FAILED A SIMAO OTHER L NO TEST ININSP/MAINT 1 SW21821AE 145577 LAX - FLT 3160 - EMERGENCY LIGHTS CB POPPED WILL NOT RESET AND EXIT LIGHT FOR MAIN ENTRANCE DOOR WILL NOT GO OUT. RAI NR 1 EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20031204000052003120400005 2003 12 4 GTIA030864 420031024A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 DTW - FOUND L1 DOOR SLIDE PACK FELL OFF. INSTALLED L1 DOOR EVACUATION SLIDE. NO DISCERPANCIES NOTED. (M) 2L72 4F A6WE 20031203001242003120300124NM 2003 12 3 USAA030240 120031104A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US53237 22954 FOUND SKIN CRACKED 1.75 INCH, ABOVE STRINGER 20R AT STATION 762. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI AND XIX. (M) 2L72 4F RTA16WE 20030319001122003031900112NM 2003 3 19 UIEA200300003 120030122A541465B9405326 SKIN BOEING747 747243B 1384830NM NR 2 NACELLE WRINKLED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15516MC 22507 DURING CURRENT C-CHECK AT SIA, FOUND NR 2 PYLON R/S SKIN WRINKLED TWO PLACES FROM 1) NAC 286 TO 300 AT STR 5, 2) NAC 300 TO 316 AT STRINGER6. REPAIR AREA (1) CUTOUT EXISTING DAMAGE IN FLAT BAY AREAS ONLY. HFEC INSPECTED ALL OPEN HOLES, CUT EDGES AND ADJACENT STRUCTURE FOR CRACKS AND TEMPER LOSS. NO DAMAGE OR TEMPER LOSS FOUND. FABRICATED ADDITIONAL DOUBLER AND TRIPLER SPLICE PLATE. INSTALLED PER SRM STANDARD PRACTICES. (2) SKIN WRINKLE IS SMOOTH AND ROUND AND DOES NOT EXCEED .050 INCH DEEP. HFEC INSPECTED AREA AS ABOVE. NO DEFECTS OR TEMPER LOSS. NO REPAIR REQUIRED IN AREA 2 BUT IT MUST BE INSPECTED AT EVER 'C' CHECK NOT TO EXCEED 18 MONTHS, REF SRM 51-10-01 AND 54-31-03. (M) 2L74 4F A20WE 20030320000452003032000045NM 2003 3 20 USAASB03013 120030120A2133322684003 OUTFLOW VALVE BOEING737 7373B7 1384580NM FWD FUSELAGE FAILED A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19391US 23313 PIT - FLT 231 - ON CLIMB-OUT, AT FL330, CABIN ALTITUDE BEGAN A RAPID CLIMB AT 2,000 FT PER MINUTE. CREW ACCOMPLISHED AN EMERGENCY DESCENT AND REGAINED CONTROL, CABIN AT FL120 IN MANUAL PRESSURIZATION MODE. AT FL100, CABIN ALTITUDE NORMAL WHEN TRYING STANDBY PRESSURIZATION MODE. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. OXYGEN MASKS WERE NOT DEPLOYED. MAINT FOUND FWD OUTFLOW VALVE FAILED IN OPEN POSITION. R & R FWD OUTFLOW VALVE PER MM. REMOVED AND REPLACED P5-6 CABIN PRESSURE SELECTOR PANEL AND CABIN PRESSURE CONTROLLER AS PRECAUTIONARY. OP CHECK GOOD. ACCOMPLISHED HULL LEAK CHECK AND CONFIDENCE CHECK OF CABIN PRESSURE WITH SINGLE PACK OPERATION. SYSTEM CHECKS GOOD. NO HULL LEAKS NOTED. 2L72 4F RTA16WE 20030122000562003012200056 2003 1 22 HEEA083444 420030109A2300H1037 HEADSET BELL 206 206L3 1182108SW COMMS SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 SCREW STRIPPED THAT HOLDS MIC BOOM SECURE. REPLACED HEADSET. 1G71 3U H2SW 20030122000742003012200074SW 2003 1 22 HEEA083466 120030109A7712P155150GE1A SENSOR BELL 206 206L3 1182108SW TORQUE INDICATORUNRELIABLE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 TORQUE SENSOR GIVES UNRELIABLE INDICATIONS (SPIKES OVER 140 PERCENT). 1G71 3U H2SW 20030731001292003073100129NM 2003 7 31 QXEA200300833 120030707A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - H-STAB TO V-STAB FORWARD RIGHT HAND CONNECTION POINT SHIMS/SPACER IS EXTRUDING. REPAIRED IAW Q400 AMM 55-10-010, TASK 55-10-00-000-801 AND RD 8/4-55-094. 2H72 4T RTA13NM 20030303000952003030300095NE 2003 3 3 HEEA084523 220030214A75323043023 BLEED VALVE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 TROUBLESHOOTING BLEED VALVE FOR HIGH ITT. 1G72 4U4 U H4SW E22EA 20040329000472004032900047NM 2004 3 29 ASAA0340322 120030725A5320652333692 INTERCOSTAL BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT FS 947-967 CORRODED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030421001652003042100165WP 2003 4 21 WRLA200303 120030304A2821AC922F1740 FUEL FILTER DOUG DC10 DC1030 3023501WP NR 3 ENGINE DIRTY A WRLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27352WL 47838 ON TAKEOFF WITH N1 PASSING 60 PERCENT NR 3 ENGINE FUEL FILTER PRESSURE DROP LIGHT ILLUMINATED WITH MASTER CAUTION LIGHT ON. REJECTED TAKEOFF AT 80 KNOTS AT BANGOR MAINE. REMOVED AND REPLACED NR 3 FUEL FILTER. OPS CHECK OK ON ENGINE RUN. REPLACED FUEL FILTER ELEMENT. (M) 2L73 4F A22WE 20030418000222003041800022NM 2003 4 18 VNAA0302014 120030216A2611 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FIRE FALSE INDICATIONA VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07472PS 3008 THE CREW REPORTED A LAV FIRE LIGHT ON THE RED WARNING PANEL ILLUMINATED. THERE WAS NO FIRE. MAINTENANCE CONTROL WITH THE CREW THEN DEFERRED THE LAV FIRE EXTINGUISH SYSTEM WITH CODE 26-4 C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030722000812003072200081EU 2003 7 22 MALA030337 120030710A2611 WARNING LIGHT SAAB SF340 SF340A 7850100EU CARGO SMOKE ILLUMINATED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15119XJ 340A119 AVIONICS RACK SMOKE DETECTOR CAME ON INFLIGHT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. REFER TO LOG PAGE 111263 FOR DETAIL. 2L72 4T RTA52EU 20030724000052003072400005 2003 7 24 DLM88030521 420030606A3417HG280D80 ADC DOUG MD88 MD88 3023688NM COCKPIT FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27931DL 49718 CAPT LOST AIRSPEED INDICATOR AFTER AIRBORNE. FLT 1425 DIVERTED TO BOSTON FROM PVD. REPLACED NR 1 CADC PER MM. ALL CHECKS OK. 2L72 4F RTA6WE 20030421002042003042100204NM 2003 4 21 AMTA200300322 120030307A3350 LIGHT BOEING737 73783N 13844HINM CABIN CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11318TZ 28247 FLOOR PATH LIGHTING RIGHT SIDE AFT END CRACKED. REMOVED AND REPLACED PATH LIGHT IAW MM 33-51-15-2. 2L72 4F RTA16WE 20030423001982003042300198EU 2003 4 23 RAIA00303071 120030313A3150 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03565HK 41082 STL - RIGHT -IEC- FAULT INDICATION. MAINTENANCE INSPECTED AND CLEARED FAULT AND COULD NOT DUPLICATE THE FAULT INDICATION. 2L72 4T RTA41NM 20040224000162004022400016EA 2004 2 24 ASOA04011 120031230A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11839AS 7284 DURING TAKEOFF FROM, THE NOSE GEAR WOULD NOT RETRACT. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED, LANDING SAFELY. MAINTENANCE DISCOVERED THE NOSE GEAR S23 PROXIMITY SENSOR HITTING THE TARGET AND ADJUSTED THE SENSOR. MAINTENANCE ALSO PERFORMED FOUR GEAR SWINGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030826001012003082600101SO 2003 8 26 FFS2003F00018 120030507A323321150021 PISTON ROD PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA LT MLG ACTUATOR BROKEN A FFSAA UNSCHED LANDING O OTHER CLCLIMB 1 AL014301C WTC6115 318353001 (FL90965) THE PILOT TOOK OFF AT ANIAK AND RETRACTED THE LANDING GEAR. A LOUD BANG WAS HEARD, AND THE LEFT MAIN LANDING GEAR FELL OUT OF THE WHEEL WELL. THE LEFT MAIN LANDING GEAR ACTUATOR PISTON ROD HAD BROKEN AT THE EXTENSION END. THE PILOT EXTENDED THE LANDING GEAR AND LANDED SAFELY AT ANIAK. 1L72 3O3 O A20SO E14EA 20030827001792003082700179SO 2003 8 27 C2XA03TY136TY 120030820A254014525422001 SEAL EMB 145 EMB145LR 3260212SO LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED 2C INSPECTION THE LEFT SEAL IN LAV WAS FOUND CORRODED AROUNDN NUT PLATE. MAINT R&R A NEW LEFT LAV SEAL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030828000572003082800057NE 2003 8 28 P5CA0300910 220030811A7310 FILTER BOEING747 7472U3B 1384846NM PWA JT9 JT9D7 52054NE NR 3 ENGINE CONTAMINATED A P5CAK NONE R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23923FT 22769 702370 ON DECENT NR 3 ENG HAD STALLED CONDITION. AT FL 290 SHUT DOWN. ON SECOND RESTART WITH FUEL HEAT APPLIED OPERATION NORMAL. CORRECTIVE ACTION TAKEN: REMOVED FUEL FILTER. INSPECTED AND CLEANED WATER FROM FILTER. REINSTALLED FILTER PERFORMED AURAL CK OF FUEL HEAT SOLENOID CK OK ENG RUN UP OK. 2L74 4F4 FRTA20WE E20EA 20030829001172003082900117NM 2003 8 29 SWAA031805 120030811A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030903001652003090300165WP 2003 9 3 DHL2003803013 120030723A2560 ESCAPE ROPE DOUG DC8 DC873 302199CWP COCKPIT OUT OF ADJUST A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01803DH 46123 CAPTAIN'S ESCAPE ROPE ACCESS DOOR WILL NOT REMAIN SECURED AND OPENED FREQUENTLY. RE-POSITIONED AND SECURED AS REQUIRED. CAPTAIN'S ESCAPE ROPE ACCESS DOOR OK, REF M/M 25-60-2. 2L74 4F RT4A25 20030902001302003090200130NM 2003 9 2 03FDEA00900 120030612A5712ARC2850505 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 SNRM N0065 - LT WING L/E NR 16 SLAT TRACK I/B RIB FOUND CRACKED. LT WING L/E NR 16 SLAT TRACK I/B CRACKED RIB REMOVED AND NEW RIB INSTALLED IAW SRM 51-31-01 VOL.II. 2L73 4F RTA22WE 20030904000662003090400066EA 2003 9 4 SWIA200312306 120030821A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07437SW 7564 ''STAB TRIM'' AND ''MACH TRIM'' CAUTION MSGS AFTER TAKEOFF AND AFTER LANDING. REMOVED AND REPLACED CAPTAIN'S DISCONNECT SWITCH IAW CL6000 27-41-30. OPS CHECK GOOD. 2L72 4F RTA21EA 20030821002532003082100253NM 2003 8 21 03FDEA01349 120030820A2612346000293 FIRE LOOP DOUG MD11 MD11 3023602NM NR 2 ENGINE SHORTED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25588FE 48490 AT 1455Z, FL360,M.83.ENG NR 2 FIRE LIGHT CAME ON. INTERMITTENT AT FIRST IT BECAME STEADY AND ENG NR 2 WAS SHUTDOWN IAW CHECKLIST. NO OTHER ADVERSE INDICATIONS OBSERVED EXCEPT FIRE DETECT 2 FAIL LEVEL 1 ALERT. RTB WAS UNEVENTFUL, 1 FIRE BOTTLE WAS DISCHARGED. USING MEGGER FOUND UPPER LT B-LOOP AND LOWER TURBINE A-LOOP SHORTED TO GROUND. R AND I BOTH LOOP DETECTOR PER MM 26-11-03-4 FDCU NR 2 RTS TEST PASSED. R AND I ENG NR 2 SYS 1 FIRE BOTTLE AND TEST PER MM 26-21-01-4 TEST OK. RUN NR 2 ENG PER MD11 JRH ALL PARAMETERS AND INDICATIONS NML. PERFORMED NR 2 ENG DECAY CHK PER MD11 JRH TEST PASSED. OPEN AND CLOSED ENG COWLS AND PLATFORM PER MM 71-10-00. 2L73 4F RTA22WE 20030826001262003082600126WP 2003 8 26 03FDEA00983 120030627A5753 HINGE DOUG DC10 DC1030 3023501WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 S 16 COMPLY WITH EA 8-5740-70941.WINGS-RT INBD FLAP HINGE ATTACH LUG REWORK. COMPLIED WITH EA 8-5740-70941.WINGS-RT INBD FLAP HINGE ASSY ATTACH REWORK. 2L73 4F A22WE 20030826001432003082600143EU 2003 8 26 SIMA200320803 120030722A55127255150522 SKIN SAAB SF340 340B 7860101EU HORIZ STAB DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21375AE 340B375 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECCESSITATED THE REPLACEMENT OF THE RIGHT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS 3079, REV 41, 51-40-21, 22, 23, 40, 51-20-40, 41, 43. (M) 2L72 4T RTA52EU 20030825001092003082500109EA 2003 8 25 03229636 120030817A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27636BR 7307 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHTING STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030910000142003091000014WP 2003 9 10 DHL2003604569 120030606A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBD FLAP PLATING CRACKED 2.000 STA XW 125.000 - XW 128.000. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. CLEANTED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911000822003091100082WP 2003 9 11 DHL2003873539 120030627A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OUTBD L/E FORMER 0.250 AT STA XFS.728.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031001000892003100100089SW 2003 10 1 2003F00586 120030606A212039290811 CONTROL VALVE FRCHLDSA227 SA227DC 3377521SW AIR DISTRIBUTIONSTUCK A BSAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM05453LA DC852B WITH BLEEDS OFF, CREW WAS GETTING AIRFLOW INTO CABIN THAT SMELLED OF SMOKE. CREW FOLLOWED PROCEDURES AND LANDED AT THE NEXT STATION, WHICH WAS THE CLOSEST. IT WAS SUSPECTED THAT A FLOW CONTROL VALVE STUCK OPEN, THE ENVIRONMENTAL AIR DUCTING GOT HOT, WHICH CAUSED SMOKE. REPLACED THE FLOW CONTROL VALVE, SYSTEM OPS CHECKED GOOD. (M) 2L72 4T RTA18SW 20031001000282003100100028NM 2003 10 1 CALA0300518 120030909A5320 INTERCOSTAL BOEING777 777224 1385225NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778013 29861 INSPECTION FOUND FLOORBEAM FORWARD INTERCOSTALS CRACKED AT BS 246. THE CRACKS WERE LOCATED AT HOLES IN INTERCOSTAL AT LBL 26.06, LBL 7.88, AND RBL 25.09. THE CRACK LENGTHS WERE NOT IDENTIFIED. 2L72 4F RTT00001SE 20031001000982003100100098NM 2003 10 1 AMTA200301129 120030903A3260 INDICATOR BOEING757 75723N 1384973NM MLG INOPERATIVE A AMTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL11523AT 30232 RIGHT MAIN GEAR GREEN LIGHT INOPERATIVE. REPLACD RIGHT MLG LAMP ASSEMBLY PER CHAPTER 20 PART USED WAS CCN 3221420. (M) 2L72 4F RTA2NM 20030908003162003090800316 2003 9 8 SWAA031894 420030823A2565D31354 SLIDE BOEING737 7373Q8 1384670NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030905002192003090500219SO 2003 9 5 C2XA03XH268 120030812A533014520554001 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE SCORED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV-DURING C CHECK THE EXTERNAL SKIN SCORED NEAR FRAME 20 AT STRINGER 13L. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030908001932003090800193EA 2003 9 8 SWIA200312270 120030817A214068AA7594 HEATER CNDAIRCL600 CL6002B19 1900309EA GALLEY MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07592SW12 12 7279 THE NR 1 GALLEY HTR CAUSES A SMOKEY SMELL WHEN ON. CREW REPORTS THAT THERE IS A STRONG BURNT ELECTRICAL SMELL IN THE GALLEY OR FLIGHT DECK JUST AFTER PUSHBACK. REMOVED AND REPLACED NR 1 GALLEY HEATER IAW CRJ AMM 21-23-05. P/N: 2831-45 S/N OFF: 584. ALSO REMOVED AND REPLACED GALLEY VENTILATION FAN. SYSTEM OPS CHECK GOOD. NO TRACE OF ELECTRICAL BURNING SMELL. 2L72 4F RTA21EA 20030908002372003090800237EU 2003 9 8 MALA030344 120030720A7931230386402 COMPUTER BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE OIL SYSTEM FAULTY A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15507XJ E2316 DURING FLIGHT NR 3557, NR 1 ENGINE OIL LOW PRESSURE LIGHT CYCLING ALL OTHER INDICATION NORMAL. AIR RETURN TO MSP. MAINTENANCE REPLACED PROCESSOR PN/ON-OFF 2-303-864-02, SN/OFF 10130700411 SN/ON 020130700436 IAW AMM 77-40-01 OPS CHECKS GOOD MXC NR 4103 NOTIFIED. 2H74 4F4 FRTA49EU E6NE 20031009000132003100900013WP 2003 10 9 AALA20030986 120030910A33500211720004 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21259AA 49289 DURING OVERNIGHT MAINTENANCE, TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 14D. REPLACED SEAT MOUNTED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031028000962003102800096NM 2003 10 28 03FDEA01606 120030912A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OB FLAP IB HINGE (FLAP SIDE) FOUND CORROSION ON INBD AND OB PIVOT BORES AND SPOT FACES. RT OB FLAP IB HINGE (FLAP SIDE) IB AND OB PIVOT BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT IAW EA NR 1-5750-72686 WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES - RT OB FLAP / IB SUPPORT BRACKET, CORROSION REMOVAL AND REPAIR. 2L73 4F4 FRTA22WE E13NE 20031023000812003102300081NM 2003 10 23 P5CA0300955 120030922A76007270981 PUSH-PULL CABLE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 4 THROTTLE FAILED A P5CAO OTHER O OTHER CRCRUISE 1 WP23923FT 22769 702280 NR 4 ENGINE THROTTLE BINDED NR 4 ENG FUEL CONDITION MOTOR POPPED C/B. REPLACED ENGINE PUSH PULL CABLE IAW MM 76-11-07 OPS CK OK. REPAIRED WIRE IAW STANDARD PRACTICES 20-00-00. OPS CK OK IAW AMM 76-11-00 2L74 4F4 FRTA20WE E3NE 20031028001212003102800121SO 2003 10 28 SIMA200324606 120030814A531114522367001 FRAME EMB 135 EMB135LR 3260305SO FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 ABI - DURING AN IMBV INSPECTION, THE LOWER RIGHT SECTION OF FRAME 72 WAS FOUND TO BE CREASED AND DENTED. REMOVED THE DAMAGED LOWER SECTION OF FRAME 72. INSTALLED NEW FRAME IAW EMB SRM, SRM 145/1142 REV 22, 51-40-02 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031110001912003111000191NM 2003 11 10 SWAA032236 120031011A53306545766 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED 3.5 LONG AT BS 501D, STR 12R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040127001972004012700197NM 2004 1 27 ASAA0310216 120030325A49106550904276 FRAME BOEING737 737298C 1384490NM APU COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND APU COWLING FRAME AT BS 1104, BUTTOCK LINE 0 CHAFED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20031105000262003110500026NM 2003 11 5 AWXA200301351 120031013A5315BAC15172226 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON NUT PLATES LOWER SIDE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1304 TO BS 1312, LBL 2. MAINTENANCE REMOVED DAMAGED FLOORBEAM FROM BS 1215 TO BS 1320, LBL 2; FABRICATED A NEW REPLACEMENT FLOORBEAM AND SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 1-6. 2L72 4F RTA2NM 20031106001132003110600113NM 2003 11 6 QXEA200301381 120031029A3350 SWITCH DHAV DHC8 DHC8202 2809007NM CABIN CONTAMINATED A QXEAK NONE O OTHER CRCRUISE 1 NM09349PH 486 SEA- ON FLIGHT 2163 EXIT FLOOR TRACK EMERGENCY LIGHTS FLICKER ON AND OFF IN FLIGHT. FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH IS DAMP. CLEANED AND DRIED SWITCH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031107000242003110700024NM 2003 11 7 HNAA0300063 120031103A531185330566 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07930HA 126 MAJOR REPAIR; X467 FRAME SECTION REPLACEMENT. 2H72 4T RTA13NM 20031105000742003110500074NM 2003 11 5 03FDEA01837 120031030A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORRODED KEEL BEAM STR 29R, O/B FLANGE 950F-970. REMOVED CORROSION ON RT KEEL BEAM AT BS 950F TO BS 970. FABRICATED REPAIR STRAP. ALODINED, PRIMED REPAIR AND INSTALLED REPAIR WET WITH SEALANT AS PER FED EX SRM DRW SR 27-53-023 AND SRM 51-30-2, 53-10-1, 51-10-6. 2L73 4F RTA3WE 20031010000062003101000006NM 2003 10 10 USAABB03154 120030903A3350873100251REV15 LIGHT BOEING757 7572B7 1384964NM R2 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 CREW NOTED THE YELLOW AND GREEN LED'S FLASHING AT THE EXIT IDENTIFIER AT DOOR R3. AIRCRAFT FERRIED TO CLT. NO FAULTS FOUND WITH THE LIGHT AT R3. MAINTENANCE FOUND THE R2 EXIT IDENTIFIER INOPERATIVE AND REPLACED IT. (M) 2L72 4F RTA2NM 20031106001412003110600141SO 2003 11 6 SWIA200312530 120031023A3231 ROD END EMB 120 EMB120ER 3260203SO RT MLG DOOR OUT OF ADJUST A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07299SW 120329 RIGHT GEAR DOOR REMAINS OPEN AFTER GEAR SELECTOR UP. VISUALLY VERIFIED THAT GEAR WAS UP WITH DOORS OPEN. RED INTRANSIT LIGHT IS REMAINING ON. ADJUSTED ACTUATOR ROD END (LENGTHENED 1 TURN) PER32-32-10 AND ADJUSTED UPLOCK TARGET PER MM 32-61-01. OPS CHECKS GOOD. 2L72 4T RTA31SO 20031112000712003111200071NM 2003 11 12 ASAA02003A 120030316A541065C2630946 ANGLE BOEING737 7374Q8 138447QNM NR 2 ENG PYLON CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND NR 2 ENGINE PYLON CUTOUT FOR INBOARD FLAP UPPER ANGLE WORN 20 INCHES FROM FORWARD EDGE OF CUT OUT. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040108000952004010800095EU 2004 1 8 KBM2003F00045 120031005A6710126892P BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE M/R PITCH LINK WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 3 EACH LOWER ROD BEARINGS ON MAIN ROTOR PITCH CHANGE LINK ARE WORN BEYOND LIMITS. REMOVED AND REPLACED WITH 3 EACH NEW SERVICEABLE ROD END BEARINGS. 1G71 3U3 UNCH9EU E19EU 20040311000582004031100058NM 2004 3 11 ASAA0310106 120030306A5310654656411 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SHEAR TIE AT BS 1006, STRINGER 24R-25R CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. (M) 2L72 4F RTA16WE 20040113000662004011300066EA 2004 1 13 033286254 120031124A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING HEAVY CHECK INSPECTION THE FLOOR BEAM WAS FOUND CORRODED BETWEEN FS 333 AND FS 349, RBL 27. THE FLOORBEAM SECTION THAT WAS CORRODED WAS REPAIRED PER SRM INSTRUCTIONS. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040113000852004011300085NM 2004 1 13 AWXA200301597 120031203A5311651630087 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BS 178 BULKHEAD CHORD AT AFT CENTER OF RADIUS RBL 29, WL 207. MAINTENANCE REMOVED CRACKED CHORD AT RBL 29, WL 207; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 6, 7, 8, 12, & 14, PG 1, 26, 28, 32, 36, 38, 45, 49, & 55. 2L72 4F RTA16WE 20040114001262004011400126NM 2004 1 14 DLM88031060 120031128A3340 JAM-NUT DOUG MD88 MD88 3023688NM COCKPIT LOOSE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27974DL 53242 WHEN NOSE LIGHTS SWITCH TURNED OFF AFTER T/O, SPARKS FLEW FROM SWITCH UNIT. C/BS STAYED IN, BUT WERE PULLED BY CREW. FOUND JAM NUT LOOSE ON NOSE LIGHTS SWITCH CAUSING TERMINAL TO CONTACT METAL SUPPORT STRUCTURE. SECURED JAM NUT. CYCLED SWITCH SEVERAL TIMES, NO DEFECTS NOTED. 2L72 4F RTA6WE 20040115001142004011500114NM 2004 1 15 03FDEA02087 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 2 LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 3 BANJO FITTING AJC7053-503 AFT FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL2 & REPLACED AS PER SRM 51-33-01 VOL2 & SRM 51-38-01 VOL2. 2L73 4F RTA22WE 20031217001742003121700174NM 2003 12 17 SWAA032648 120031202A53136551698 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND STRINGER 25R CORRODED AT BS 903 TO 910. REMOVED AND REPLACED PER SRM. 2L72 4F RTA16WE 20031222000032003122200003WP 2003 12 22 ARWA20031203 120031207A2130 WARNING LIGHT DOUG DC8 DC862F 3021972WP COCKPIT ILLUMINATED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19791AL 46150 AFTER TAKEOFF OUT OF KMIA VENT DOOR WARNING LIGHT CAME ON & CABIN PRESS WAS UNABLE TO BE MAINTAINED. 2L74 4F 4A25 20031223000642003122300064NM 2003 12 23 03FDEA02168 120031211A5531 STRINGER BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 VERTICAL FIN STR 8L AT FIN STA 180 IS CRACKED. 2L73 4F RTA3WE 20031231000562003123100056WP 2003 12 31 GTIA030905 120031118A33501001191 LIGHT DOUG DC9 DC982 3022082WP CABIN WILL NOT TEST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 PORTABLE EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M) 2L72 4F A6WE 20031231001182003123100118WP 2003 12 31 GTIA030940 120031106A2510 SEAT DOUG DC9 DC983 3022083WP COCKPIT INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FIRST OFFICERS SEAT WILL NOT ADJUST UP DOWN AND BACK. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F RTA6WE 20031231000972003123100097NM 2003 12 31 TSAA0355033 120030114A551065499253 FITTING BOEING737 7372T4 1384492NM HORIZONTAL STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 THE LEFT HORIZONTAL STABILIZER CENTER CENTER SECTION REAR SPAR UPPER FITTING ASSEMBLY UPPER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW OVERSIZED BUSHING PER DRAWING. SHOT PEENED, REFINISHED THE LUG FACES, AND INSTALLED BUSHING. REPAIR COMPLETED IAW ECO 3330. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031231001072003123100107NM 2003 12 31 TSAA0353035 120030118A5311656212529 KEELBEAM BOEING737 7372T4 1384492NM FUSLEAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 TRIMMED OUT FUSELAGE SKIN BETWEEN KEEL BEAMS AND AFT OF BS 727. REMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM FROM BS 500 TO BS 727 PLUS 16. VISUALLY AND HFEC INSPECTED TRIMLINE AND AREA UNDER REPAIR FOR SIGNS OF CORROSION AND DISBONDING. FABRICATED AND INSTALLED THREE FILLERS, A DOUBLER AND TRIPLER. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS BMS 10-79, TYPE III PRIMER. REPAIR COMPLETED IAW ECO 3327, FIGURE 1. AIRCRAFT RETURNED TO SERVICE (M) 2L72 4F A16WE 20040109000572004010900057NM 2004 1 9 2004F00004 120031031A790056B17C BULB BOEING727 727200 138407ENM PWA JT8 JT8D17A 52049NE OIL TEMP BULB LOOSE A P9RAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO11910PG 22606 709501 ON CLIMB, NR 3 ENGINE OIL TEMP INCREASED INTO THE YELLOW BAND WHERE IT PROCEEDED TO FLUCTUATE BETWEEN THE YELLOW AND GREEN BAND. ON DESCENT, THE OIL TEMP INCREASED AND REMAINED INTO THE HIGH RANGE OF THE YELLOW BAND. INITIATED PRECAUTIONARY ENGINE SHUTDOWN. FOUND CONNECTOR PLUG ON NR 3 TEMP BULB LOOSE. REMOVED AND REPLACED NR 3 OIL TEMP BULB AND RESECURED CONNECTOR PLUG. IDLE RUN LEAK CHECK GOOD. HIGH POWER RUN CHECKED GOOD. NO FURTHER DEFECTS NOTED, NR 4 BEARING INDICATOR NORMAL. (M) 2L73 4F4 FRTA3WE E2EA 20040112002172004011200217NM 2004 1 12 2003UALA00966 120031218A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29541UA 25253 EXTERNAL SKIN FUSELAGE DOUBLER REPAIR INSTALLED AT STA 620 STR 8R AT HMV-2 ON 6-29-02 PER EVA IMC20373 REV B. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW DOUBLER REPAIR PER EVA IMC20373C. 2L72 4F4 FRTA2NM E17NE 20040109000612004010900061EA 2004 1 9 A6WA200340170 120031031A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31452AW 7835 FOUND FRAME AT FS 589 SKIN FLANGE BETWEEN STRINGERS 24L AND 25L IS DAMAGED AND FLANGE BETWEEN STRINGERS 25L AND 26L IS DAMAGED. REMOVED FLANGE, FABRICATED REPAIR FLANGES FROM 2024 T3 .050 INCH WVAC PO NR 29699/1, FABRICATED FILLER SHIMS FROM 2024 T3 .090 INCH WVAC PO NR 25026/1, AND INSTALLED REPAIR PARTS WET USING PR1422B 1/2 AND FASTENERS MS20426AD-S IAW CRJ200 SRM 53-00-51 REPAIR NR 2. (M) 2L72 4F RTA21EA 20040112002662004011200266WP 2004 1 12 AALA20031462 120031221A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21236AA 49251 EMERGENCY LIGHTS FROM ROWS 21-31 INOPERATIVE. REPLACED SOCKET IN ROW 30. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2L72 4F A6WE 20040114000572004011400057 2004 1 14 DL76L030973 420031030A23301301851100 MONITOR BOEING767 767332 1382001NM CABIN OVERHEATED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27191DN 28448 IFE SYS CONTROL PNL AREA AND OVERHEAD BINS AT ROW ONE EXHIBITED A BURNING ODOR DURING MID CLIMBOUT. ODOR DISSIPATED WITHIN A FEW MINUTES BUT F/A COULD NOT TURN SYS OFF. FOUND WALL MOUNTED VIDEO MONITOR AT SEATS 1A AND 1B AT FAULT MONITOR NIIS JFK. FWD TO MCO AND PLAC PER MEL 25-20-01J. DISCONNECTED AND STOWED CONNECTORS. SYSTEM SHUT DOWN WITH TIME LIMIT, NEEDS DPN 251711825. REPLACED WALL MOUNTED VIDEO MONITOR. OPS CHECK NORMAL. NO ODOR NOTED. REMOVED MCO AND PLACARD. 2L72 4F RTA1NM 20040114000922004011400092NM 2004 1 14 03FDEA01989 120031126A5730 SKIN DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT WING NR 1 SLAT TRACK CUT OUT I/B SKIN FOUND CRACKED DURING I/B SLAT RIGGING CHECK. RT WING NR 1 SLAT TRACK CUT OUT I/B SKIN CRACK REPAIRED AS PER SRM 57-10-00 FIG 15 VOL1. 2L73 4F RTA22WE 20040115000462004011500046CE 2004 1 15 AMWA56724 120031203A291011438800013 POWERPACK BEECH 1900 1900D 1154162CE HYD SYSTEM FAILED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0715YV UE15 AFTER TAKE OFF FROM PFN TO VPS. LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. PROBLEM WAS POWER PACK, HYDRAULIC. R&R'D POWER PACK/RPRD BROKEN WIRE OPS OK P/N 1143880001-3 S/N MX607544 2L72 4T RTA24CE 20031212001342003121200134WP 2003 12 12 AALA20031220 120031105A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219618A 53565 TPA - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD COACH OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN FORWARD COACH OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031218000352003121800035 2003 12 18 SWIA200312630 420031124A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07564SW7927 7927 120339 NEITHER CAPTAIN NOR F/O'S AUTOPILOT WILL CAPTURE AND FOLLOW THE COMMAND BARS, NOR WILL IT CAPTURE AN ALTITUDE. REMOVED AND REPLACED APP-65A AUTOPILOT CONTROL PANEL AND REPLACED ELEVATOR SERVO IAW EMB 120 MM 22-10-04. OPS CHECK GOOD. SERVO P/N: 622-5734-002, S/N OFF: 8426. 2L72 4T RTA31SO 20031218001552003121800155NM 2003 12 18 QXEA200301510 120031202A3230858601 PSEU DHAV DHC8 DHC8202 2809007NM ZONE 700 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09374PH 528 DURING CLIMBOUT THROUGH 9000 FT NOSE GEAR CYCLED DOWN AND UP. ALL INDICATIONS WERE NORMAL. GEAR INDICATIONS WERE UP AND LOCKED AS NORMAL PRIOR TO THE GEAR CYCLING. GEAR CAME DOWN AND LOCKED WITH THREE GREEN ON THE PANEL AND FLOOR. REMOVED AND REPLACED PSEU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040105000082004010500008NM 2004 1 5 DL757031000 120031111A2910 LINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE DAMAGED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27602DL 716590 22809 716590 RIGHT HYD QTY LOSS. FOUND PRESSURE LINE IN RT PYLON DAMAGED. REPLACED SAME. 2L72 4F4 FRTA2NM E17NE 20031010000332003101000033NM 2003 10 10 USAABB03142 120030818A2422111101020714 STATIC INVERTER BOEING757 7572B7 1384964NM A/C SYSTEM FAILED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19626AU31173 27303 EN ROUTE FROM LAS TO PHL, CREW RECEIVED AN EICAS MESSAGE FOR STANDBY INVERTER AND THE FILGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE CABIN. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CONFIRMED STATIC INVERTER WAS SOURCE OF ODOR IN THE CABIN. REMOVED AND REPLACED STATIC INVERTER PER MM 24-33-03. CLEARED EICAS STATUS MESSAGE. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20031020000622003102000062SO 2003 10 20 C2XA03SH380 120031011A711014576599604 STRUCTURE EMB 145 EMB145LR 3260212SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 SHV- DURING C-CHECK THE RIGHT TOP ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040311000222004031100022NM 2004 3 11 ASAA0310138 120030314A5320656210012 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND TORQUE BOX WEB ANGLE AT BS 351.2, STRINGER 18L CORRODED. REMOVED AND REPLACED WEB ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031202000902003120200090NM 2003 12 2 USAABB03198 120031026A335020131A BATTERY BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 FOUND FLOOR TRACK LIGHTING, LEFT SIDE, FROM OVERWING EXIT TO SEAT ROW 9 INOPERATIVE. MAINTENANCE LET THE BATTERIES CHARGE OVERNIGHT. SYSTEM CHECKED NORMAL. (M) 2L72 4F RTA1NM 20031204000202003120400020WP 2003 12 4 GTIA030872 120031020A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOORBEAM, IN MID PIT, CHAFING AND CORRODED. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20031208000352003120800035WP 2003 12 8 ARWA20031103 120031115A3213 AXLE DOUG DC8 DC863F 302198FWP MLG DAMAGED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19661AV 45969 RED DOOR NOT LATCHED, LIGHT WOULD NOT GO OUT AFTER MLG RETRACTION. RECYCLED PER ABNORMAL CHECKLIST, NO HELP. RED GEAR NOT LATCHED. LIGHT WOULD NOT GO OUT AFTER GEAR RETRACTION. RECYCLED PER ABNORMAL CHECK LIST, NO HELP. UPON INSPECTION OF MLG FOUND NR 7 WHEEL ASSY BACKED OF THE AXLE CAUSING DAMAGE TO NR 7 BRAKE ASSY. WHEEL & BRAKE REMOVAL ACCOMPLISHED, AXLE INSPECTED FOR DAMAGE & NO DISCREPANCIES FOUND. WHEEL RETAINING NUT WAS STILL SECURE TO AXLE. INSPECTION REVEALED A BEARING FAILURE WHICH CAUSE WHEEL TO MOVE OUT OF PLACE NOT ALLOWING GEAR CYCLE TO BE COMPLETED. AFTER NDT INSPECTION OF AXLE & REPLACEMENT OF BRAKE & WHEEL ASSY, A GEAR RETRACTION ACCOMPLISHED & FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE 2L74 4F 4A25 20031208000472003120800047NM 2003 12 8 VNAA0310008 120031009A5210 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR OUT OF ADJUST A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07434JS 3051 DURING CLIMBOUT, THE CREW RECEIVED A PASSENGER DOOR UNLOCK INDICATION AND RETURNED TO PHL. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE DOOR ROD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031209000252003120900025EA 2003 12 9 COMA0370045 120031029A5313MM67038108 STRINGER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA2508 10069 WHILE ACCOMPLISHING EO 55-009 THE INSTALLATION OF RAIN GUTTER ON STRINGERS 10L AND 10R AT WL 109-673 BETWEEN MID SPAR DATUM 43.750 PERCENT TO 55.625 PERCENT THE FASTENER HOLES WERE ELONGATED DURING THE DRILLING PROCESS. PERFORMED A MAJOR REPAIR BY REAMING HOLES TO REMOVE DAMAGE, FABRICATING AND INSTALLING FREEZE PLUGS IAW WVAC EO 601R-53-4345. 2L72 4F RTA21EA 20031209000932003120900093NM 2003 12 9 SWAA032313 120031018A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STR 11R CRACKED AT BS 777. REPAIRED STRINGER PER ERO. 2L72 4F RTA16WE 20031210001722003121000172NM 2003 12 10 CALA0300606 120031020A5320BAC1496377 PANEL BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914324 23375 AFT CARGO PIT LEFT TRANS PANEL CORRODED AROUND FASTENERS MARKED (STA 847 - 947). FABRICATED AND INSTALLED NEW TRANS PANEL IAW SRM 53-00-01. 2L72 4F4 FRTA16WE E2GL 20031210000732003121000073WP 2003 12 10 AALA20031317 120031123A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 DFW AFT VAULT DOOR OVERHEAD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT VAULT DOOR OVERHEAD CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210002122003121000212WP 2003 12 10 UPS03841544 120031021A532057585421N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 AC COMPARTMENT STATION 55 AT CEILING LT SIDE FLOORBEAM FITTING IS CRACKED AT LBL 48 APPROX. REMOVED AND REPLACED FITTING IAW DWG 5758542 AND SRM 51-1-20D, 51-1-21 2L74 4F RT4A25 20031015000052003101500005NM 2003 10 15 USAASB03169 120030917A335020131A BATTERY BOEING737 737301 1384611NM FWD/MID CABIN WEAK A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 23740 FOUND LT OVERWING AND FORWARD ENTRY EMERGENCY LIGHT BATTERIES WEAK. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA16WE 20030918000502003091800050NM 2003 9 18 DL73G030705 120030728A2197 WIRE BOEING737 73735B 13844BMNM OUTFLOW VALVE SHORTED A DALAO OTHER P NO WARNING INDICATION LDLANDING 1 SO27221DL 23970 UPON LANDING A ACRID ELECTRICAL ODOR NOTICED IN COCKPIT AND CABIN. REPAIRED SHORTED WIRE IN FWD CARGO COMPARTMENT AND REPLACED CABIN PRESSURE CONTROLLER 2L72 4F RTA16WE 20040127002312004012700231WP 2004 1 27 ASAA0380653 120031015A531139544231 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND CORROSION ON FRAME 1060. REPLACED FRAME CAP. (M) 2L72 4F A6WE 20040203003302004020300330EA 2004 2 3 MASA200300487 120031212A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAK NONE O OTHER ININSP/MAINT 1 SW0737228 7228 CREW REPORTED MAIN PAX DOOR HARD TO OPEN. MX CLEANED AND LUBED LATCHING MECHANISM. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20031216000792003121600079NM 2003 12 16 SWAA032575 120031121A53306552880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030925000622003092500062EA 2003 9 25 SIMA200321802 120030803A27605120011 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA LT WING SPOILER INOPERATIVE A SIMAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 SW21501BG 10017 DURING DESCENT, THE CREW REPORTED AN OUTBOARD SPOILERON AND AN OUTBOARD SPOILER CAUTION MESSAG ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE SPOILER ACTUATOR IAW CRJ MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030924000822003092400082EU 2003 9 24 223022703 120030227A30103D248526 TIMER PILATSPC12 PC1245 7090551EU DE ICE SYSTEM FAILED E S4WAO OTHER J WARNING INDICATION CRCRUISE 1 WP07317NA 223 WING DE-ICE CAWS LIGHT ILLUMINATED IN FLIGHT. 1L71 3T RTA78EU 20030815000982003081500098NE 2003 8 15 BAQA088340 220030806A7261430118501 PUMP BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE ENGINE OIL LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911WS4820 7068 OIL PUMP LEAKS FROM TOP AREA OF HOUSING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030820000762003082000076NM 2003 8 20 03FDEA01120 120030721A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 CORROSION ON SHEAR TIE AFT SIDE BS 1130, BETWEEN STR 29 AND 28 LT. REMOVED CORROSION ON SHEAR TIE AFT SIDE 2.20 X 1.80 X .007 INCH MAX, IAW SRM 51-10-6. ORIGINAL MATERIAL .050, OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR SHEAR TIE OF 7075 T6 .050 LOT 504450 PER SRM 51-10-3, SRM 51-20-1, SRM 51-30-5, ALODINED PER SRM 51-10-2 PAR 3 G. PRIMED, PAINTED AND INSTALLED IAW FED-EX MM 51-20-151-7 SEC 5-8 AND SRM 51-30-2 SEC 4. 2L73 4F RTA3WE 20030821002402003082100240WP 2003 8 21 0301409617 120030730A2120 DUCT DOUG DC9 DC932 3022066WP CABIN PRESSURE OUT OF POSITION A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01617NW 47235 THE CABIN ALTITUDE BEGAN TO CLIMB FOLLOWING A MUFFLED REPORT. AIRCRAFT WAS IN CRUISE AT FL330 WHEN MASTER WARNING ILLUMINATED AND PRESSURE LOSS BEGAN. CREW INITIATED AN EMERGENCY DESCENT TO FL100 WHEN CABIN PRESSURE GRADUALLY RECOVERED. FLIGHT CONTINUED TO A NORMAL SAFE LANDING AT MSP. MAINTENANCE FOUND A BLOWN DUCT OFF THE LEFT WATER SEPARATOR AND RESECURED IT. OPERATIONAL CHECKS WERE ALL GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20030822000592003082200059EA 2003 8 22 QXEA200300928 120030729A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09607QX 10024 STRONG BURNED ODOR IN AIRCRAFT WITH NR 2 PACKS ON. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030404001832003040400183NE 2003 4 4 SWAA030591 220030313A7200332A1000 ENGINE BOEING737 7373A4 1384585NM GE CFM56 CFM56* 13802NE NR 1 MALFUNCTIONED A SWAAK NONE E VIBRATION/BUFFET DEDESCENT 1 SW29680AA 23505 856436 DURING DESCENT,THRUST LEVERS RETARDED, HEARD LOUD BANGING NOISE FROM NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030410002242003041000224NM 2003 4 10 DL76K030124 120030201A2530 COFFEEMAKER BOEING767 767332 1382001NM GALLEY DIRTY A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27177DZ 29698 AFT GALLEY HAD ELECTRICAL TYPE SMELL ON RT SIDE OF GALLEY. CHECK AFT GALLEY FOR ANY IRREGULARITIES. THE UTILITY BUSSES WERE TURNED OFF. UTILITY BUSSES RESET BY CREW. OPERATION ALL AFT GALLEY OVENS, CHILLERS COFFEEMAKERS AND LIGHTS. FOUND COFFEEPOT WITH BURNT COFFEE IN BOTTOM OF POT. NO OTHER SMELLS OR TROUBLE FOUND. 2L72 4F RTA1NM 20030408001392003040800139NM 2003 4 8 AWXA200300345 120030314A53126516300302 FRAME BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 YVR - MAJOR REPAIR - DURING C-16 CHECK A .5000 INCH CRACK WAS FOUND ON LT AND RT SIDE FRAMES, BS 178 BULKHEAD, WL 207. MAINTENANCE CUTOUT DAMAGED SECTION OF RT SIDE FRAMES, BS 178, WL 207; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A SPLICE FRAME, SPLICE ANGLES, AND SPLICE PLATES; INSTALLED REPAIR PARTS IAW E.R. 03-5312-03093-TB2. MAINTENANCE REMOVED LT SIDE CHORD; FABRICATED A NEW REPLACEMENT SIDE FRAME PER DWG 65-16300; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3 & 6. 2L72 4F4 FRTA16WE E2GL 20030409000262003040900026NM 2003 4 9 MEX2003050 120030301A2497 RELAY DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE DC SYSTEM DAMAGED W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23160PL 49763 CAPTAIN REPORTED DC BUS OFF LIGHT TURN ON. FAIL WAS CAUSED BY A TEMPORARY ELECTRICITY FAILURE IN JET WAY. DURING CHECK, WAS DETECTED THE RELAY R2-21 DAMAGED. AFTER RELAY WAS COOLED DOWN, THE ELECTRIC SYSTEM WAS RESETED AND WITH APU POWER WAS PERFORMED A TEST AND DC BUS OFF LIGHT TURNED OFF. TEST WAS PERFORMED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030416002042003041600204NM 2003 4 16 SWAA030770 120030403A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 480 AT STR 16R, BS 520 AT STR 4L AND BS 727B AT STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030429000342003042900034NM 2003 4 29 03FDEA00415 120030409A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION (C53-111-01, 3) ON FRAME BS 950D WL 148 LBL 8-10. REPAIRED FRAME IAW SRM 53-10-4 FIG 15 AND EA 7-5310-69653. 2L73 4F RTA3WE 20030430002122003043000212NM 2003 4 30 VNAA0304010 120030415A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07471PS10606713 3007 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 9 WAS NOT WORKING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030502001012003050200101NM 2003 5 2 P5CA0300855 120030411A5311 FRAME BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FRAME CRACK 1700 13R. REPAIRED FRAME PER SRM 51-40-03 FIG 2. 2L74 4F A20WE 20030501000442003050100044WP 2003 5 1 AALA20030238 120030221A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21228AA 49178 TUL - FOUND THREE CRACKS EXTENDING FROM FASTENER HOLE IN FUSELAGE SKIN LT SIDE STATION 1380 BETWEEN LONGERONS 13L AND 14L. STOP DIRLLED CRACKS AND INSTALLED DOUBLER PER SRM 53-01-00 FIG 2 SHEET 3. (M) 2L72 4F A6WE 20030501001902003050100190NM 2003 5 1 ASAA0310058 120030301A5321654961612 FLOOR PANEL BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO PIT FLOOR PANEL ATTACH ANGLE AT BS 947, STRINGER 23L CORRODED. REMOVED AND REPLACED ATTACH ANGLE PER SRM. (M) 2L72 4F RTA16WE 20030501000932003050100093WP 2003 5 1 GTIA030210 120030308A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND CORROSION ON SKIN AROUND FORWARD AND AFT CABIN SAFETY RELIEF VALVES. MATERIAL LOSS OUT OF LIMITS AT AFT RING. DRILLED AND LOCATE HOLE NEW RING. INSTALLED NEW RING. (M) 2L72 4F RTA6WE 20030502000652003050200065WP 2003 5 2 ASAA0380177 120030301A532199365527 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL IS MISSING SEVERAL INSERTS REPLACED PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030505002272003050500227WP 2003 5 5 03FDEA00546 120030419A3697 WIRE DOUG DC10 DC1010 3022110WP NR 1 PNEUMATIC INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2568052 47806 WITH NR 1 PNEUMATIC SYSTEM DEFERRED UNDER 36-01-A NR 1 SYSTEM IS STILL PROVIDING AIR TO RUN A-PACK WITH ISOL VALVES CLOSED & PNEUMATIC NR 1 SELECTOR OFF. WHILE DESCENDING WITH ALL THROTTLES IDLE, THE NR 1 PNEUMATIC PRESSURE WAS 15 PSI. PUSHED NR 1THROTTLE UP & PSI WENT TO 45 PSI. FOUND BROKEN WIRE ON CONNECTOR. CHANGED BROKEN CONNECTOR IAW SMP CHAPTER 20 DC10AMM. 2L73 4F A22WE 20030508000712003050800071NE 2003 5 8 DL777030359 220030407A7200 ENGINE BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 1 FAILED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27866DA13978 29738 51188 LT ENGINE VIBRATION WENT TO 5.0 ON CLIMBOUT ACCOMPLISHED BY ENGINE SURGE STALL. RETURNED TO MAN NOTICEABLE AIRFRAME BUFFETING OPERATED ENG AT IDLE TO NO OTHER ABNORMAL INDICATIONS. REPLACED NBR 1 ENG PER ROUTINE CARD DECK 2L72 4F4 FRTT00001SEE00050EN 20030509000242003050900024WP 2003 5 9 GTIA030224 120030303A5320 WEB DOUG DC9 DC983 3022083WP SUB FLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND SUB FLOOR WEB CORRODED IN MAIN CABIN LBL 42 FS 164. REMOVED DAMAGED SUB FLOOR WEB SECTION. FABRICATED NEW WEB. INSTALLED NEW SUB FLOOR. (M) 2L72 4F RTA6WE 20030509000712003050900071NM 2003 5 9 HOC2003F00006 120030420A5315 FLOORBEAM BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON CABIN FLOORBEAM, STA 1110, BL-0. 2L72 4F4 FRTA16WE E2EA 20030513003032003051300303EA 2003 5 13 ASOA03165 120030416A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EXTERIOR BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 FLT 4693 - DUIRNG A GROUND INSPECTION IN ATL, THE MIDDLE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MIDDLE EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514001642003051400164NM 2003 5 14 P5CA0300863 120030412A5330 SKIN BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEVEL 1 CORROSION AROUND FASTENERS HOLES COMMON TO BS 2220 FRAME INNER CHORD AND WEB BETWEEN STR 40R AND STR 42R PER REF /B/. FRAME STRAP REPLACED PER BOEING TELEX. 2L74 4F A20WE 20030515000882003051500088SO 2003 5 15 C2XA03SH128 120030505A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713908 145465 SHV - DURING C-CHECK LEFT HAND FLOORBEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030609001582003060900158WP 2003 6 9 MWEA030229 120030522A3260833605 PROXIMITY SENSOR DOUG DC9 DC981 3022081WP NLG INOPERATIVE A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31807ME 48033 AFTER GEAR RETRACTION NOSE UNSAFE ILLUMINATED. -- REMOVED AND REPLACED PROXIMITY SENSING ELECTRONICS UNIT (PSEU). 2L72 4F A6WE 20030606000752003060600075NM 2003 6 6 03FDEA00774 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP O/B HINGE (FLAP SIDE) AFT ATTACHING POINT, AFT BOLT HOLE CORRODED. ** S/D ** COMING 2L73 4F RTA22WE 20030609000862003060900086EA 2003 6 9 QXEA0300639 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT STRINGER 9R, 5 INCHES AFT OF FS 797. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030514001062003051400106NM 2003 5 14 SWAA031007 120030505A33506527093 LIGHT BOEING737 7373H4 1384600NM FWD GALLEY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT BROKEN AT FWD GALLEY. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030612001992003061200199EA 2003 6 12 SWIA200311994 120030507A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW 7555 FLOORBEAM ANGLES AT STR 14 FS 625 ARE CRACKED BOTH SIDES. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F4 FRTA21EA E15NE 20030613000292003061300029NM 2003 6 13 CALA0300282 120030521A5314 STRUCTURE BOEING737 737524 1384721NM KEELBEAM WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2719621 27334 WEAR DAMAGE WAS FOUND AT THE UPPER SURFACE OF THE OUTBOARD FLANGE OF RT KEEL BEAM LOWER STRUCTURE JUST FORWARD OF STA 727 WHILE AIRCRAFT WAS IN MAINTENANCE CHECK AT HOU. THE WEAR WAS CAUSED BY THE FLOATING NUT PLATES ATTACHED TO THE OUTBOARD FLANGE OF THE LOWER STRUCTURE. THE NUT PLATES ARE USED TO ATTACH THE WHEEL WELL FAIRING. THE KEEL BEAM STRUCTURE OUTBOARD FLANGE WAS REPAIRED IAW ECRA 5311-01149. 2L72 4F RTA16WE 20030611000262003061100026WP 2003 6 11 GTIA030319 120030415A5340 FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT PIT LT FITTING SUPPORT LOWER DOOR JAMB, 2 EA CORRODED STA 1155, STA 1211. REMOVED 2EA LT FITTINGS. LOCATED AND DRILLED NEW FITTINGS. INSTALLED NEW FITTING. 2L72 4F4 F A6WE E2EA 20030521000742003052100074WP 2003 5 21 DHL2003805009 120030516A2611 LAMP DOUG DC8 DC873F 302199FWP SMOKE DETECTOR BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01805DH 46125 NR 4 SMOKE DETECTOR WILL NOT TEST. RE-LAMPED NR 4 SMOKE DETECTOR OPS CHECKED GOOD AS PER M/M 26-10-5. 2L74 4F RT4A25 20030522000262003052200026WP 2003 5 22 GTIA030281 120030428A7120K22199SA31 ISOLATOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NR 2 ENGINE INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23824NK 53015 NR 2 ENGINE LOWER ISOLATOR NEEDS REPLACED. REPLACED NR 2 ENGINE FORWARD LOWER ISOLATOR. 2L72 4F4 FRTA6WE E2EA 20030618001402003061800140SW 2003 6 18 HEEA087355 120030611A6710407070007101 COVER BELL 407 407 1182206SW M/R CONTROL CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR CONTROL COVER CRACKED. 1G71 3U O H2SW 20030528000462003052800046EU 2003 5 28 BAQA086299 120030430A6240L771M40C1003 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE TACH STUCK E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01135MH 0131 TRIPLE TACH ROTOR RPM NEEDLE STICKS. 1G72 3U H88EU 20030528000922003052800092EU 2003 5 28 BAQA086431 120030519A6220E1T302301 FREQ ADAPTER AEROSPAS365 AS365N2 8680815EU MAIN ROTOR CRACKED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS012XJ 1209 6089 FREQUENCY ADAPTER CRACKED BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030529000142003052900014NM 2003 5 29 AALA20030431 120030409A5320 FLOOR SUPPORT BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21621AM 24579 TUL - FOUND TOP OF FLOOR SUPPORT CORRODED CTR, FS 1660. REMOVED TOP OF FLOOR SUPPORT FROM STATION 1660 TO 1680 CENTER SUPPORT PER SRM 51-70. INSTALLED NEW SUPPORT. (M) 2L72 4F RTA2NM 20030529000462003052900046SW 2003 5 29 HEEA086637 120030521A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 8154 33134 AFT FRETTING PADS ON BOTH SURFACE SEPARATED, MID SPAN AND INBOARD TRIM TAB UNBONDED, EROSION SHIELD HAS SOME SEPARATION. SENT TO ROTOR BLADES, INC. FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030620000112003062000011SW 2003 6 20 HEEA086938 120030603A79218537651 OIL COOLER BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 FOUND COOLING FINS BENT. SENT TO MFG FOR INSPECTION AND REPAIR. 1G72 4U4 U H4SW E22EA 20030707000602003070700060NM 2003 7 7 2003UALA00479 120030605A5313 STRINGER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 BS 1361-1379 STRINGER SECTION REQUIRES REPLACEMENT IN ORDER TO MAINTAIN 20 INCH MINIMUM SPACING BETWEEN STRINGER SPLICE AT STATION 1337, STRINGER 34R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SECTION AND SPLICE. 2L72 4F4 FRTA1NM E3NE 20030701000162003070100016SW 2003 7 1 HEEA087870 120030116A6510 SEAL BELL 407 407 1182206SW BEARING TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH128 ZV17027 53327 TAIL ROTOR DRIVE BLOWER SHAFT BEARING, RUBBER SEAL TORN. REPLACED BEARING. 1G71 3U O H2SW 20030708000422003070800042WP 2003 7 8 UPS03840903 120030602A5210NPN SKIN DOUG DC8 DC873F 302199FWP DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3, L1 DOOR UPPER FORWARD CORNER SHOWS CRACK INDICATION WITH X-RAY INSPECTION. CUT OUT CRACK AND FABBED -15 DOUBLER, -17 DOUBLER, AND -19 FILLER IAW SRM 53-2-0 FIG 15 TR 53-155. ALODINED AND PRIMED IAW SRM 5 1-1-8. INSTALLED DOUBLERS AND FILLER IAW SRM 51-1-20D AND SRM 53-2-0 FIG 15 TR 53-155. DRILLED NEW SPLICE ANGLE PN 5597646-99 IAW SRM 51-1-24. INSTALLED ANGLE IAW SRM 51-1-21. 2L74 4F RT4A25 20030709000302003070900030WP 2003 7 9 AALA20030506 120030428A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21411AA 49322 DURING OVERNIGHT MAINTENANCE, ENTRY WAY EMERGENCY EXIT IGHT ACROSS FROM FIRST CLASS LAVATORY BROKEN. REPLACD ENTRY WAY EMEGENCY EXIT LIGHT ACROSS FROM FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030710001252003071000125NM 2003 7 10 AT0300018 120030617A3040CWC0107P TERMINAL BLOCK BOEING717 717200 1383700NM WINDOW HEAT BURNED A ZZDAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO15924AT 55080 AT 9000 FEET STRONG BURNING ODOR AND SMOKE (LIGHT) COMING FROM CAPTAIN'S WINDSHIELD. WHEN WINDSHIELD HEAT WAS SELECTED OFF, SMOKE DISSIPATED. ATL MAINTENANCE DISPATCHED, REMOVED AND REPLACED THE CAPTAIN'S LEFT WINDSHIELD, WINDOW HEAT CONTROL TERMINAL BLOCK, AND WINDOW HEAT CONTROLLER. 2L72 4F TRA6WE 20030711000572003071100057EU 2003 7 11 MALA030310 120030612A3230 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU MLG ILLUMINATED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15513XJ E2329 DURING APPROACH OF FLIGHT 3415, WHEN GEAR SELECTED DOWN, GEAR DID NOT EXTEND WHILE QRH TROUBLESHOOTING GEAR EXTENDED AND GREEN HI TEMP LIGHT ILLUMINATED. MAINTENANCE INSPECTED LANDING GEAR, OPERATED GREEN SYSTEM HYDRAULICS FOR 45 MINUTES. OPS CHECK GOOD. FOUND A/C SAFE FOR ONE TIME FLIGHT FROM XNA TO CVG FOR REPAIRS TO LANDING GEAR. NO OTHER INFORMATION AT THIS TIME. OPEN 2H74 4F RTA49EU 20030714001312003071400131NM 2003 7 14 C1HA200395064 120030630A3350900835A BATTERY PACK BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 RIGHT FWD OVERWING OUTSIDE EMERGENCY EXIT LIGHT INOP. 2L73 4F A3WE 20031203000102003120300010NM 2003 12 3 AALA20031109 120031006A33503015643 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21389AA 27449 DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROW 26B. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031203001122003120300112NM 2003 12 3 USAABB03209 120031107A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19621AU 27200 FOUND ONE FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20031204000652003120400065EA 2003 12 4 COMA0360458 120031013A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA HEAT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01716CA14409 7250 RT WINDSHIELD HEAT CAUTION MESSAGE. REPLACED THE HEAT CONTROLLER. 2L72 4F RTA21EA 20031204001952003120400195EA 2003 12 4 03292687 120031019A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27687BR 7720 DURING INSPECTION THE OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040122000932004012200093 2004 1 22 GTIA030959 420031128A2565D29985 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 ACY - DURING MAINTENANCE THE CLEANERS OPENED L2 DOOR AND DROPPED SLIDE PACK ON RAMP. REMOVED AND REPLACED L-2 SLIDE. (M) 2L72 4F A6WE 20031208000252003120800025NM 2003 12 8 03FDEA01890 120031107A5330 SKIN BOEING727 727100 1384036NM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 EXTERNAL SKIN BULGED AT BS 350 BETWEEN STR 25R AND 26R. INVESTIGATED BULGED SKIN BS 350, STR 25R & 26R. FOUND SKIN TO BE CORRODED BETWEEN SHIM AND SHEAR TIE. REMOVED OLD SHIM. FABRICATED NEW SHIM. ALODINED, PRIMED, AND INSTALLED. ALL PER SRM 51-30-2, MM 51-20-021-7 & MM 51-20-151-7. 2L73 4F RTA3WE 20031210001962003121000196NM 2003 12 10 03FDEA01872 120031105A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 N01482 CORROSION WHILE WORKING CARD NO N00939, FOUND CORROSION ON FLOORBEAM, STA 344 RBL 13-53 WL 208. ** SD ** COMING 2L73 4F RTA3WE 20030919000932003091900093EU 2003 9 19 MALA030372 120030806A2120 ODOR SAAB SF340 340B 7860101EU CABIN DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL15414XJ 340B414 FA AND PASSENGERS SMELLED BURING RUBBER IN CABIN ROW 6. MAINTENANCE RAN BOTH ENGINE HIGH AND LOW PSI BLEED WITH FULL AIR HOT AND COLD NO SMELLS NOTED SUSPECT LARGE A/C LANDING IN FRONT OF THIS CREATING RUBBER ODOR FROM TIRES WHICH THEN WERE INDUCED INTO AIR SYSTEM. NO FAULTS WITH ENGINE OR A/C SYSTEM OF ACM. 2L72 4T RTA52EU 20040126000502004012600050 2004 1 26 HEEA087798 420030614A2350A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 INTERPHONE BOX HAS BACKGROUND NOISE FROM FM RADIO. SHOP REPAIR. 1G72 3U H1NE 20040206000482004020600048SO 2004 2 6 SIMA200335704 120031221A4920 TURBINE WHEEL EMB 145 EMB145LR 3260212SO APU INOPERATIVE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21617AE SPE0219479 145093 APU FAILED INITIAL OBSERVATION WAS SMOKE IN CABIN AND COCKPIT. UPON FURTHER INVESTIGATION FOUND APU TURBINE WHEEL DAMAGED. APU THEN DEFERRED IAW MEL 49-1. MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040210001162004021000116WP 2004 2 10 ASAA0380753 120031118A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND FRAME CORROSION. INSTALLED REPAIR ANGLE AND STRAP PER EA 5310-02279. (M) 2L72 4F RTA6WE 20031212001112003121200111NM 2003 12 12 SWAA032445 120031105A3350BR2013 STRIP BOEING737 7373H4 1384600NM CABIN DETERIORATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP DETERIORATED AT LT AFT END. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20031211000412003121100041NM 2003 12 11 PCAA0311138 120031107A33506104781 BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13817EX 191 FLIGHT 3800, LAGUARDIA, DURING TEST CREW FOUND THAT TWO CEILING LIGHTS WERE INOP. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040316000942004031600094WP 2004 3 16 ASAA0380357 120030418A272059141389 CRANK ASSY DOUG DC9 DC983 3022083WP RUDDER LIMITER CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, RUDDER THROW LIMITER CRANK ASSY IS CORRODED. REPLACED CRANK ASSY PER MM 27-20-06. (M) 2L72 4F RTA6WE 20040413000492004041300049NM 2004 4 13 ASAA024016X 120030322A532065479577 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 860. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030925000612003092500061SO 2003 9 25 SIMA200323002 120030815A27503631001007 FCU EMB 135 EMB135KL 3260302SO AVIONIC BAY INOPERATIVE A SIMAO OTHER O OTHER DEDESCENT 1 SW21839AE 145653 DURING APPROACH, TEH CREW REPORTED THE FLAPS BECAME STUCK IN THE DOWN POSITION. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED IN CMH WITH NO FURTHER PROBLEMS NOTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030711000452003071100045WP 2003 7 11 DHL2003804004 120030620A2611327 LAMP DOUG DC8 DC873F 302199FWP SMOKE DETECTOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01804DH 46124 NR 12 SMOKE DETECTOR NOT TESTING. DEFERRED NR 12 SMOKE DETECTOR PER MEL 26-6-1 CAT C DMI 13315. REF DMI 13315 NR 12 SMOKE DETECTOR WON'T TEST. RELAMPED AND TESTED NR 12 SMOKE DETECTOR SYSTEM CHECKED GOOD PER M/M 26-10-6. THIS CLEARS DMI 13315. PLACARD REMOVED. 2L74 4F RT4A25 20030127001112003012700111 2003 1 27 HEEA083664 420030114A34578143802240D GPS BELL 407 407 1182206SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 GPS FACE PLATE KEEPS COMING OFF MAKING IT UNREADABLE. FOUND LENS BAD. REPLACED LENS, REPAIRED. BENCH CHECK GOOD. 1G71 3U O H2SW 20030128001122003012800112SW 2003 1 28 HEEA083854 120030116A3212406015043101 COVER BELL 407 407 1182206SW EMERGENCY FLOAT CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH2699 53378 EMERGENCY FLOAT COVER CORRODED BEYOND REPAIR. SCRAPPED. 1G71 3U O H2SW 20030128002332003012800233EU 2003 1 28 AWXA200300045 120030115A33501012881 LIGHT AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28621AW 053 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AND HARNESS AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030204001692003020400169EU 2003 2 4 2003F00106 120030203A291010545023 POWERPACK BOLKMS105 BO105S 5626006EU HYD SYSTEM MALFUNCTIONED E A UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW09557HH121001576 S557 IN CRUISE FLIGHT AT 800 FT AGL, THE HYDRAULIC PACK SWITCHED FROM SYSTEM NR 1 TO SYSTEM NR 2. THE COLLECTIVE BOTTOMED OUT ON THE LOWER STOP, PUTTING THE AIRCRAFT NOSE DOWN. THE AIRCRAFT IMMEDIATELY LOST 200 FEET OF ALTITUDE. PILOT REPORTED HYD BLOCK LIGHT ON FIRST, FOLLOWED BY HYD 1 AND HYD 2 LIGHTS FOR ABOUT 3 TO 4 SECONDS BEFORE BOTH EXTINGUISHED. HYD BLOCK REMAINED ILLUMINATED. LANDING AT NEARBY AIRPORT WAS NORMAL. HYDRAULIC PACK WAS REMOVED AND SENT TO MANUFACTURER FOR EVALUATION. 1G72 3U H3EU 20030206001832003020600183 2003 2 6 USAASA03003 420030110A2565 SLIDE AIRBUSA321 A321211 3930370EU L1 DOOR MALFUNCTIONED A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19186US 1701 BOS - RECEIVED 'EPSU EXT LOAD FWD L' MESSAGE DURING THE EMERGENCY LIGHT TEST. MAINTENANCE REPLACED THE L1 DOOR ESCAPE SLIDE. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030207001002003020700100NM 2003 2 7 03FDEA00055 120030120A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION IB-FLANGE ON SEAT TRACK NUT PLATE HOLE STA 514 LBL 25 WL 208. R&R SEAT TRACK PER SRM 51-30-2. 2L73 4F RTA3WE 20030220001142003022000114EA 2003 2 20 QXEA0300110 120030121A2421766277A IDG CNDAIRCL600 CL6002C10 1390015EA NR 2 ENGINE MALFUNCTIONED A QXEAK NONE J WARNING INDICATION UKUNKNOWN 1 NM09613QX1640 10045 PSP-ON FLIGHT NUMBER 2528, IDG NR 2 CAUTION MESSAGE. IDG DISCONNECTED PER EMERGENCY CHECKLIST. REMOVED AND REPLACED IDG. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030117000032003011700003SW 2003 1 17 HEEA083148 120030108A6720206011725001 BEARING BELL 206 206L3 1182108SW T/R CONTROL ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 TAIL ROTOR HEAD CONTROL ROD WORN BEARING. SCRAPPED. 1G71 3U H2SW 20030224000542003022400054NE 2003 2 24 HEEA084175 120030212A79317645001078119 TRANSMITTER SKRSKYS76 S76A 8143006NE OIL PRESSURE READS HIGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 NR 2 ENGINE OIL PRESSURE INDICATES ABOVE RED LINE ABOVE IDLE. FOUND PRESSURE TRANSMITTER INDICATING ABOVE 160 PSI WITH DEAD WEIGHT TESTER AT 130 PSI. SCRAPPED TRANSMITTER. 1G72 3U H1NE 20030224001082003022400108SW 2003 2 24 HEEA084223 120030120A5320407070620143 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030303000092003030300009 2003 3 3 HEEA084482 420030214A22102593996333 TARSYN BELL 412 412 1182202SW AUTO FLIGHT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 TARSYN COMPASS FLAG WON'T PULL UNTIL 10 MINUTES AFTER INVERTERS PUT ON. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030304000192003030400019SW 2003 3 4 ALGA084828 120030226A5260212075418105 ACTUATOR BELL 412 412EP 1182205SW STEP DEFECTIVE H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS015NBDZ 36278 STEP LINEAR ACTUATOR STUCK IN EXTEND POSITION. REQUEST WARRANTY REPAIR. 1G72 4U H4SW 20030307000242003030700024 2003 3 7 SWAA030470 420030303A2565D31354 SLIDE BOEING737 7372H4 138448CNM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 FWD SERVICE DOOR EVACUATION SLIDE ASSY LOOSE. ADJUSTED SLIDE ASSY PER MM. 2L72 4F A16WE 20030313000672003031300067NM 2003 3 13 03FDEA00190 120030228A3260 WARNING SYSTEM DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE COCKPIT MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25609FE 48549 AFTER TAKEOFF, GEAR RETRACTION RIGHT GEAR UNSAFE RED LIGHT ON PRIMARY PNL ABOVE GEAR HANDLE AND ON CONFIG SYNOPTIC PAGE. RED TABS ACCOMPLISHED, GEAR EXTENDED AND RIGHT GEAR INDICATION IMMEDIATELY WENT GREEN. RAISED GEAR AND ALL INDICATION. T/S FIM 32-30-03, PERFORMED BITE CHECK ON PSEU- LAST LEG NO FAULT NOTED. CARRIED BITE CHECK ON PSEU SYS AND TARGET CHECK, NO FAULTS NOTED. CARRIED OUT VISUAL INSPECTION ON RIGHT HAND MLG DOOR LATCH, PROX SENSORS, RETRACTION CYLINDER AND SELECTOR VALVE IAW MM 32-34-03-4 AND 32-31-20. 2L73 4F4 FRTA22WE E13NE 20030313001992003031300199EU 2003 3 13 AALA20030167 120030206A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211414D 11377 DFW - FOUND DURING OVERNIGHT MAINTENANCE, NR 5 EMERGENCY EXIT AISLE LIGHT INOPERATIVE. REPLACED NR 5 EMERGENCY EXIT AISLE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030121001992003012100199SW 2003 1 21 HEEA083343 120030109A771432005008 TACH GENERATOR BELL 206 206L3 1182108SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610Y 51419 TACH GEN NOT GENERATING. 1G71 3U H2SW 20030122001272003012200127NM 2003 1 22 DL73K030038 120030106A5315 FLOORBEAM BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 CORROSION DAMAGE ON STA 986.5 FLOORBEAM UPPER CHORD AT LBL 6 AND RBL 6. REPAIRED PER SRM DRD 53-20-1D FIG 803D, UPPER CHORD REPLACEMENT. 2L72 4F A16WE 20030317000092003031700009WP 2003 3 17 03FDEA00137 120030218A2450MS21919DG16 CLAMP DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 IN RT PICKLE BARREL AREA, UNDER PANEL 264GA, FOUND NR 2 GENERATOR FEEDER CABLE WIRE (NR 2X2B0B (AL)) CHAFING AGAINST WORN CLAMP. UPON FURTHER INSPECTION FOUND SMALL HOLE IN INSULATION AND WIRE STRANDS INSIDE, MELTED DOWN, LEAVING THE WIRE ALMOST HOLLOW AT THAT SECTION. C/A: SPLICED FEEDER 2X2B0B(AL) IAW E.A. 8-2450-63125. OK FOR SERVICE. 2L73 4F4 F A22WE E23EA 20030318000842003031800084WP 2003 3 18 ASAA0380021 120030104A5720592081530 BRACKET DOUG DC9 DC983 3022083WP RT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE PANEL 1248C BRACKET IS CHAFED. REPLACED CHAFED AREAS OF BRACKET PER SRM 51-10-2 AND 51-30-2. (M) 2L72 4F RTA6WE 20030319000782003031900078NE 2003 3 19 MEX2003036 220030214A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8* 52044NE RIGHT MALFUNCTIONED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23162PL 49765 FLT 428 - MEX-MIA - AIRCRAFT RETURNED TO GATE, DURING TAXI RIGHT GENERATOR WENT OUT OF LINE, RIGHT ENGINE DID NOT ENTRY GENERATOR, DURING REVISION OF ACCELERATE TO THE PARAMETERS ESTABLISHED IN LOW RPM'S WITH N2 AT 42 PERCENT RPM, INCREASING EGT. AIRCRAFT WAS SENT TO THE HANGAR, RIGHT ENGINE WAS REPLACED IAW MM 71-00-01, TESTS CORRECT. (M) 2L72 4F4 FRTA6WE E2EA 20030320001142003032000114NM 2003 3 20 2003UALA00106 120030128A7830286T0332 WIRE HARNESS BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE THRUST REVERSER CHAFED A UALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP29601UA 21862 707522 DURING TAKEOFF ROLL AT 110 KTS, AN AMBER LIGHT ENG NR 1 EICAS MESSAGE CAME ON. THE CAUSE WAS A CHAFED WIRE AT SWITCH S167. THIS IS THE ENGINE 1 RT REVERSER DEPLOY PROXIMITY SENSOR. THE WIRE WAS REPAIRED. WIRE HARNESS STAYS WITH THE REVERSER AND IS NOT CHANGED WITH THE ENGINE. 2L72 4F4 FRTA1NM E3NE 20030324001092003032400109WP 2003 3 24 MWEA030139 120030324A532199365355 DOUBLER DOUG DC9 DC981 3022081WP STA 207 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 SUBFLOOR HAS A SPOT OF LIGHT CORROSION AT STATION 207 APPROBIMATELY 6" RIGHT OF CENTER. -- FABRICATED AND INSTALLED NEW REPAIR DOUBLER. 2L72 4F A6WE 20030418000392003041800039WP 2003 4 18 MWEA030083 120030212A53204912515519 CLIP DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 CLIP FOR LONGERON 10 IS DAMAGED AFT OF AFT PRESSURE BULKHEAD STATION 1341 RIGHT. LOCATED, DRILLED AND INSTALLED NEW SHOVEL CLIP. 2L72 4F A6WE 20030417000502003041700050NM 2003 4 17 UPS03240094 120030117A5350 FRAME BOEING727 72722C 138400FNM FAIRING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, FAIRING 3429 HAS CORRODED FRAME SECTION ABOVE ACCESS PANEL 3420. CUTOUT CORRODED FRAME SECTION, REMOVED IAW SRM 51-30-2. NEW FRAME SECTION FABRICATED IAW SRM 51-20-1 FIG 7 AND SRM 53-50-1 FIG 2. NEW FRAME SECTION INSTALLED IAW SRM 51-30-2. 2L73 4F A3WE 20040329000442004032900044WP 2004 3 29 ASAA0380380 120030421A5320993653411 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 160. REPLACED DAMAGED SUPPORT PER SRM 51-10-3. (M) 2L72 4F A6WE 20030801000662003080100066WP 2003 8 1 GTIA030510 120030613A5330 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - MID PIT STATION 598-610 STRINGER 27L-30 ANTENNA CUTOUT CORRODED. REMOVED ANTENNA DOUBLER. LOCATED AND DRILLED NEW ANTENNA DOUBLER. INSTALLED ANTENNA DOUBLER. (M) 2L72 4F A6WE 20030827001422003082700142NM 2003 8 27 2003UALA00535 120030703A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 FLOORBEAM CORRODED AT STATION 830-873, LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION WITH ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030829000502003082900050WP 2003 8 29 DHL2003873522 120030617A534774529523 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT NR 2 TRACK PLUG LUG WORN AT STA 1312. REMOVED AND REPLACED PLUG ON MAIN CARGO COMPT NR 2 TRACK AT STA 1312 IAW SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20030723000512003072300051NM 2003 7 23 USAABB03109 120030706A33508731002511REV15 LIGHT BOEING757 7572B7 1384964NM L2 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND L2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030722000752003072200075EA 2003 7 22 COMA0360320 120030707A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01984CA9468 7171 FLIGHT 5118 EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY PACKS. 2L72 4F RTA21EA 20030904001412003090400141WP 2003 9 4 DHL2003873601 120030709A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING INBD EXTENDED L/E OUTER PLATING SHOWS CORROSION & ELONGATED HOLES AROUND STA XFS 710 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE CORRODED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA, FABRICATED A REPAIR DOUBLER A FILLER AND A TRIPLER. CLEANED, TREATED AND PRIMED DOUBLER AND TRIPLER INTERIOR SURFACE AND FILLER. APPLIED PRC SEALANT ON FAYING SURFACE AND FILLER. INSTALLED FILLER AND DOUBLER AND TRIPLER ON RT OUTER WING INBD EXTEDNED L/E OUTER PLATING (AROUND STA XFS 710.000) USING NEW FASTENERS. 2L74 4F RT4A25 20030814000192003081400019NM 2003 8 14 SWAA031731 120030802A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727D PLUS 2 AT STR 23L AND BS 943 AT STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030725000402003072500040SO 2003 7 25 RAIA00305138 120030511A33501317 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT INTERMITTENT A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03803HK 145077 EMERGENCY LIGHTS AT ZONE TWO INTERMITTENT. REMOVED AND REPLACED LIGHT BULB. 2L72 4F RTT00011AT 20030822000142003082200014NM 2003 8 22 03FDEA01346 120030811A5753 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LEFT WING I/B TRAILING EDGE FLAP ASSY HAS LEADING EDGE SIDE GUIDE ROLLER BRACKET ASSY WITH BOLT MOUNT HOLE; LOWER BUSHING LOOSE. LT WING I/B T/E FLAP ASSY HAS L/E SIDE GUIDE ROLLER BRACKET ASSY WITH BOLT MOUNT HOLE; LOWER BUSHING LOOSE REPAIRED AS PER FEDEX EA 1-5750-63188, TITLE- WINGS- LT INBOARD FLAP- REPAIR UP STOP BRACKET. 2L73 4F RTA22WE 20030827001552003082700155NM 2003 8 27 2003UALA00546 120030708A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 FLOOR BEAM TOP CAP CORRODED AT BS 266 RBL 76. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030827001592003082700159NM 2003 8 27 2003UALA00615 120030811A5270 WARNING SYSTEM AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29801UA 686 ECAM FWD CARGO DOOR AFTER TAKEOFF. ACCOMPLISHED OPERATIONAL CHECKS, NO FAULT MESSAGES INDICATED. 2L72 4F4 FRTA28NM E40NE 20030912000812003091200081NM 2003 9 12 AWXA200300818 120030709A5315D53111412200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y254, FR 20. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AREA OF FLOORBEAM Y254 AT FR 20; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-14, PG 203-206, FIG 201. 2L72 4F RTA28NM 20030910001012003091000101NM 2003 9 10 MWEA030354 120030902A5347593054769 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 NR 1 SEAT TRACK HAS CORROSION AT STATION 524. FABRICATED AND INSTALLED SEAT TRACK SECTION. 2L72 4F RTA6WE 20030929000982003092900098NE 2003 9 29 MALA030398 320030830A6140 SENSOR SAAB SF340 340B 7860101EU ROTOL R390 R3904123F27 NE PROP SPEED INOPERATIVE A MALAO OTHER O OTHER CLCLIMB 1 GL15428XJ 340B428 PROP INDICATOR WENT TO ZERO ON CLIMBOUT. PULLED AND RESET BREAKER. ON FINAL APPROACH INDICATOR WENT BACK TO WORKING. REPLACED PROP SPEED SENSOR. 2L72 4T RTA52EU 6 CP31NE 20030908003152003090800315NM 2003 9 8 SWAA031893 120030824A3350101114 LENS BOEING737 7373Q8 1384670NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030908002012003090800201EA 2003 9 8 SWIA200312287 120030719A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 LT LWR WING PLANK WS 148 CRACKED. DISCOVERED DURING C-CHECK, DAMAGED AREA REPAIRED IAW CRJ REO 601R-57-21-130 REV 'D' & 601R-57-21-131 REV 'NC'. 2L72 4F RTA21EA 20030909001692003090900169SO 2003 9 9 SWIA200312311 120030821A27223081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07576SW8373 8373 120345 ON CLIMBOUT NO RUDDER TRAVEL. RAN QRH, TURNED OFF BLUE SYSTEM, PROBLEM CEASED. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-21-00. OPS CHECKS AND LEAK CHECKS GOOD. 2L72 4T RTA31SO 20030909002252003090900225WP 2003 9 9 DHL2003604666 120030624A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT ELEVATOR LOWER OUTER SKIN CORRODED ON SEVERAL SPOTS FROM STA XE 246.000 TO STA XH 285.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030574, ED 3411. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EO DHL 030574, ED 3411. CLEANED, TREATED AND PRIMED NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON RT ELEVATOR LOWER OUTER SURFACE (STA XE 246.000 TO STA XH 285.000) USING NEW FASTENERS IAW EO DHL 030574, ED 3411, SRM 51-1-21 PG 1. SEE NR 4037 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20030909002512003090900251WP 2003 9 9 AMTA200301014 120030725A5330 SKIN LKHEED1011 10113853 5265020WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 FUSELAGE SKIN CRACKED 2 INCHES ABOVE L-1 DOOR UPPER AFT CUTOUT. REPAIRED SKIN IAW SRM 53-31-00. (M) 2L73 4F A23WE 20031006000222003100600022EU 2003 10 6 MALA030420 120030911A243051539007B GCU SAAB SF340 340B 7860101EU DC GENERATOR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15402XJ 340B402 DURING FLIGHT NR 3021, LT DC GEN FAILED INFLIGHT ZRH COMPLETED MX. NOTIFIED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LT DC GEN GCU PN 51539-007B SN/ON 98657 OFF/98114 IAW AMM 24-31-10-2 OPS CHECK GOOD- 2L72 4T RTA52EU 20031021000342003102100034WP 2003 10 21 GTIA030700 120030907A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FOUND CABIN FLOORBOARD RIGHT OUTBOARD 1212-1309 MISSING EDGE FILLER AND HAS SURFACE DELAMINATION. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20031021002742003102100274NM 2003 10 21 PCAA0309112 120030921A3397 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13831EX 160 DURING ROUTINE MAINTENANCE VISIT, AN EMERGENCY PATH LIGHT AT ROW 8 WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE SPLICED THE WIRE USING AN ENVIROMENTAL BUTT SPLICE. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031027000532003102700053NM 2003 10 27 03FDEA01619 120030924A5315BACB150529222 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON FLOORBEAM, UPR & LWR SURFACE AROUND FASTENER HOLES AND TOP, BS 344, LBL 45 TO RBL 13, WL 208. 2L73 4F4 FRTA3WE E2EA 20031028000332003102800033EA 2003 10 28 COMA0360436 120030926A2750860D10018AB CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE AVIONICS UNRELIABLE A COMAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 SO01969CA18755 7141 FLAPS FAIL MESSAGE WHEN TRANSFERRING POWER TO NR 2 GENERATOR. REPLACED THE FECU. 2L72 4F4 FRTA21EA E15NE 20031027000802003102700080WP 2003 10 27 DXTA200300132 220031002A7230 COMPRESSOR RAYTHNDH125 HAWKER800XP 7150012CE ALIDSGTFE731TFE7313AR WP NR 1 ENGINE DAMAGED E DXTAEA ENGINE SHUTDOWN UNSCHED LANDING EJRVIBRATION/BUFFET WARNING INDICATION PARTIAL RPM/PWR LOSS CRCRUISE 1 GL07892QS 258592 P107727 AT FLIGHT LEVER 370, NR 1 ENGINED EXPERIENCE A LOUD BANG WITH ITT SPIKING AT 1016 DEGREES WITH AIRFRAME VIBRATION. N1 AND N2 ROSE, ITT THEN FELL TO 450 DEGREES WITH N1 AND N2 DROPPING. SHUT DOWN ENGINE. TROUBLESHOT NR 1 ENGINE FOUND THE LOW PRESSURE COMPRESSOR DAMAGED, HARD TO ROTATE BY HAND. REMOVED NR 1 ENGINE AND INSTALLED A SERVICEABLE LOANER ENGINE IAW RAYTHEON HAWKER 800XP MM AND HONEYWELL TFE 731-5BR LMM CHAPTER 72-02-96. PERFORMED OPERATIONAL, FUNCTIONAL & LEAK CHECKS, ALL CHECKED GOOD. 2L72 4F4 FRTA3EU E6WE 20031029000692003102900069 2003 10 29 ASAA0380542 420030724A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 PREFLIGHT CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20031120001012003112000101NM 2003 11 20 03FDEA01706 120031007A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION (C53-111-01(3)) ON BS 1148 FLOORBEAM LOWER CHORD BL 0, WL 200. *S/D* CORROSION ON FLOORBEAM AT BS 1148 LOWER CHORD BL 0 WL 200 WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER FED EX EA 7-5310-55019. 2L73 4F RTA3WE 20040210000412004021000041WP 2004 2 10 UPS03841619 120031115A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, LONGERON 33L IS CORRODED BEYOND LIMITS, STATION 1240 TO 1270. REMOVED LONGERON SECTION BETWEEN STATION 1210 TO 1270,FABRICATED AND INSTALLED LONGERON AND STRAPS IAW SRM. 53-2-2 FIG. 10. 2L74 4F RT4A25 20030910000322003091000032WP 2003 9 10 DHL2003604570 120030527A52305616673U55 TRACK DOUG DC8 DC873F 302199FWP CARGO DOOR BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 D-BELLY DOOR FWD TRACK BROKEN, STA 1400.000. REMOVED BROKEN TRACK IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK IAW SRM 51-1-21 PG 1. SEE N/R 0530 FOR OPS CK. 2L74 4F RT4A25 20031030001012003103000101CE 2003 10 30 HYI2003F00015 120030827A28226462108AIR PUMP CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LEFT ENGINE FAILED E HYIAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NE012714M2303 402C0211 823301 ON CLIMB OUT, TOWER REPORTED SMOKE FROM LT ENGINE, CREW REPORTED LOSS OF POWER AFTER AUX BOOST PUMP WAS TURNED ON, ENGINE SHUT DOWN, RETURNED W/O INCIDENT. MECHANIC REMOVED AND REPLACED LT ENGINE DRIVEN FUEL PUMP. RETURNED AC TO SERVICE. 1L72 3O3 O A7CE E8CE 20031029001272003102900127EU 2003 10 29 KBM2003F00022 120030726A6520350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH762 1864 LAMINATE BEARINGS HAS MULTIPLE CUTS. REPLACED WITH NEW LAMINATE BEARING.(K) 1G71 3U3 UNCH9EU E19EU 20031103000112003110300011NM 2003 11 3 DL777030863 120030921A253072077500 OVEN BOEING777 777232 1385232NM FWD GALLEY DIRTY A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27862DA 29734 NR 2 OVEN IN FORWARD GALLEY EMITTED SMOKE AFTER HEATING UPON CLIMBOUT MUST BE CLEANED. FWD TO MCO/PLAC MEL 25-20-01H. 2L72 4F RTT00001SE 20031103000382003110300038NM 2003 11 3 DL73K030896 120031002A52306546921108 FRAME BOEING737 737232 1384475NM CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 THE LOWER FORWARD FRAME OF THE C1 DOOR HAD A TIME-LIMITED REPAIR PREVIOUSLY INSTALLED AND NEEDED PERMANENT REPAIR INSTRUCTIONS. PERMANENT REPAIR ISSUED VIA ERA 377407-14AD, REV A. 2L72 4F RTA16WE 20040108001352004010800135EU 2004 1 8 KBM2003F00067 120031017A6720355A27006020 SLEEVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 TAIL ROTOR CONTROL ROD SLEEVE IS WORN OUT. HOLE WAS ELONGATED. REPLACED WITH NEW SLEEVE.(K) 1G71 3U3 U H9EU E19EU 20031202000712003120200071EU 2003 12 2 USAABA03036 120031015A2161978B000001 CONTROLLER AIRBUS330 A330323 3930335EU CABIN TEMP FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19670UW 0315 EN ROUTE LGW-CLT, CREW COULD NOT CONTROL TEMPERATURE IN THE CABIN. THE FLIGHT TURNED BACK TO LGW, HOWEVER, THE CREW WAS ADVISED TO TURN BOTH HEAT SOURCES OFF. THIS ACTION EVENED OUT THE TEMPERATURE THROUGHOUT THE CABIN. FLIGHT THEN RESUMED ITS ROUTE TO CLT. FLIGHT DIVERTED TO PHL FOR FUEL. MAINTENANCE REPLACED THE AFT ZONE TEMPERATURE CONTROLLER. (M) 2L72 4F RTA46NM 20031203001852003120300185WP 2003 12 3 GTIA030894 120031107A3260833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP NLG WW MALFUNCTIONED A GTIAO OTHER O OTHER CRCRUISE 1 GL23826NK 49391 NOSE GEAR RED UNSAFE LIGHT COMES ON DURING CRUISE FLIGHT. FOUND NOSE GEAR LOCKED PROX SWITCH HAD HIGH RESISTANCE. REMOVED AND REPLACED PROX SWITCH. (M) 2L72 4F RTA6WE 20031209001602003120900160NM 2003 12 9 03FDEA01716 120031008A5753ARC2512504 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) BRACKET- I/B HINGE PIN HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-71761 - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20040127001872004012700187WP 2004 1 27 ASAA0380641 120031015A53305911410 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC - DURING 15K CHECK, FUSELAGE SKIN DENTED AT FS 327-350. INSTALLED CLASS 1 REPAIR PER SRM 53-04. (M) 2L72 4F RTA6WE 20040127002422004012700242WP 2004 1 27 ASAA03805629 120031009A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS41613430 49103 OKC - DURING 30K CHECK, FOUND LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE, FAILED TO OPERATE UPON CHECK. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040128000712004012800071SO 2004 1 28 C2XA03SH521 120031230A531514521713005 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV- DURING C-CHECK THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031008000152003100800015NM 2003 10 8 03FDEA01543 120030916A3260 INDICATOR BOEING727 727200 138407ENM MLG FALSE INDICATIONA FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25499FE 21018 ON DEPARTURE WHEN THE GEAR HANDLE WAS PUT UP THE GEAR CAME UP NORMAL THE RED GEAR DOOR LIGHT STAYED ON, GREEN GEAR LIGHTS OFF AND S/O PANEL ALL LIGHTS SHOWED NORMAL. CYCLE GEAR ONCE SAME INDICATION. PULLED GEAR INDICATION CB'S AND RECYCLED GEAR NORMAL INDICATION RECYCLE GEAR AGAIN AND NORMAL INDICATION AGAIN. DURING THE FLIGHT, A/C FLEW NORMAL AS IF GEAR AND DOORS WERE UP IVEN WHEN DOOR LIGHT REMAINED ON. 2L73 4F RTA3WE 20031212000872003121200087NM 2003 12 12 SWAA032404 120031101A335020121 HOUSING BOEING737 7373H4 1384600NM CABIN SHORTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED A1 CHECK, FOUND BOTH FWD EXTERIOR EMERGENCY EXIT LIGHT AND INTERIOR EXIT LIGHT NEXT TO FWD F/A'S SEAT INOP. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY HOUSING PER MM. 2L72 4F RTA16WE 20030925000422003092500042 2003 9 25 AALA20030766 420030709A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21604AA 27055 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING NEEDING REPLACED. REPLACE ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030923000102003092300010NM 2003 9 23 QXEA200301009 120030816A26214739511 FIRE BOTTLE BOMBDRDHC8 DHC8401 1390041NM ZONE 100 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09404QX4879 4046 UPON PUSHING POWER BUTTON TO START APU, CHECK FIRE DETECTION WARNING LIGHT CAME ON AND BTC LOW LIGHT ILLUMINATED. APU FIRE VALVE ALSO CYCLED OPEN AND CLOSED SEVERAL TIMES. REMOVED AND REPLACED APU FIRE BOTTLE. OPERATIONAL CHECK OF PRESSURE FOR NEW BOTTLE WORK GOOD AND CHECK OG FIRE DETECTION SYSTEM WORKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203000062004020300006NM 2004 2 3 ASAA0310177 120030320A54206547966507 ANGLE BOEING737 737298C 1384490NM NR 1 NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL ANGLE AT NACELLE STATON 94.60-104.60 CHAFED. REMOVED AND REPLACED ANGLE IAW SRM. (M) 2L72 4F RTA16WE 20040204000512004020400051WP 2004 2 4 UPS03841385 120030922A5311 FRAME DOUG DC8 DC873F 302199FWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STATION 1680 FRAME IS CRACKED AT FLOOR LEVEL APPROX. LONG. 21L. CUTOUT DAMAGE, FABRICATED AND INSTALLED FRAME SPLICES AND FRAME SEGMENT IAW SRM. 53-2-0 FIG. 2 2L74 4F RT4A25 20040205000212004020500021NM 2004 2 5 EIA2003158 120031021A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 UPPER DECK STA. 520 STR 1 LT HAS CORROSION NEAR LAP SEAM. REMOVED DAMAGED, FABBED AND INSTALLED NEW REPAIR IAW SRM 51-10-02, 53-30-03 AND 51-30-02. 2L74 4F A20WE 20040308001942004030800194NM 2004 3 8 ASAA0310677 120031222A534765549698 SEAT TRACK BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 807-947, RIGHT BUTTOCK LINE 24.75 CORRODED. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20030915000532003091500053SW 2003 9 15 ALGA088969 120030904A5610407546122 WINDSHIELD CLARK 1000 1000CLARK 2230102SW COCKPIT CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO UPON STOCKING OF PART,FOUND DAMAGE(CRACKED AREA) ON WINDOW EDGE. SENT PART TO VENDOR FOR WARRANTY CREDIT.SUBMITTED BY:PRESTON BARZARE 1Q71 3R 2A6 20031118000192003111800019EU 2003 11 18 MALA030446 120030929A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 DURING MAINTENANCE INSPECTION FOUND EMERGENCY BATTERY LT FWD LE22 TO BE LOW. MAINTENANCE REPLACED LT FWD EMERGENCY BATTERY PACK LE22, WITH SERVICEABLE UNIT P/N 61-2275-1, S/N ON 9811820, S/N OFF 9911211. ALL CHECKS GOOD ALL FROM RJ85 MM CHAPTER 33. 2H74 4F RTA49EU 20040113000362004011300036 2004 1 13 BAQA090611 420031106A3416C19269AA CONTROL UNIT UROCOPEC135 EC135T1 5620026EU ALTIMETER MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03554ME2122 0154 BARO ADJUST NOT WORKING AND PULLS IN AND OUT. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040112000792004011200079NM 2004 1 12 AWXA200301569 120031220A33503114981 REFLECTOR BOEING737 737277 1384570NM EXTERIOR DEFECTIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - EEL - DURING 4-DAY CHECK FOUND THE R-2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOPERATIVE, AFTER BULB REPLACEMENT LIGHT WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT REFLECTOR ASSEMBLY. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040113000902004011300090NM 2004 1 13 AWXA200301601 120031209A575465C2668627 SKIN BOEING737 737301 1384611NM L/E SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING -18 CHECK THE NR 2 SLAT INBOARD UPPER TRAILING EDGE WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED EXISTING REPAIR AND DELAMINATED SKIN ON NR 2 SLAT INBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG 16, PG 67-69. 2L72 4F RTA16WE 20040114001022004011400102NM 2004 1 14 03FDEA01986 120031126A5510ALC8103 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB RIGHT UPPER AFT PLANK NR 35R BARREL NUT BORE FOUND CORROSION EXCEEDED EO LIMITATION. HOR STAB RH UPPER AFT PLANK 35R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1- 5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR 1- 5510-7-5000. 2L73 4F RTA22WE 20031212000522003121200052WP 2003 12 12 UPS03841566 120031019A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 MAIN CABIN RT CUSP IS CORRODED BEYOND LIMITS AT STATION 260. REMOVED, FABRICATED AND REPLACED CUSP SECTION BETWEEN STA 210 TO 390 IAW SRM 53-2-5 FIG 15. 2L74 4F RT4A25 20031218000762003121800076NM 2003 12 18 AWXA200301511 120031202A21337110035 OUTFLOW VALVE BOEING737 737301 1384611NM ZONE 218 FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28325AW192858460 23260 EN ROUTE, AT CRUISE FL 24000. CABIN ALTITUDE KEPT CLIMBING AT 400 FPM UNTIL IT REACHED 10000 FT. DIVERTED TO LAS, NO MASKS DEPLOYED. MAINTENANCE PERFORMED PRESSURIZATION INTEGRITY CHECK, TEST FAILED. REMOVED AND REPLACED OUTFLOW VALVE IAW T/C R6A21001. ALSO FOUND LEAKING CLAMP AT APU SUPPLY DUCT PRESSURE BULKHEAD. RESECURED CLAMP AND RE-ACCOMPLISHED PRESSURIZATION INTEGRITY CHECK, CHECK WAS GOOD PER T/C F1B21006. VENDORS INCOMING TEST OF OUTFLOW VALVE S/N 96123798 CONFIRMED REASON FOR REMOVAL. DISASSEMBLY OF UNIT FOUND AC & DC ACTUATOR SWITCHES LEAKING & VARIABLE RESISTOR SPRINGS WORN. THE SWITCH CAMS HAD EVIDENCE OF DEEP WEAR AND MISCELLANEOUS BEARINGS WERE ROUGH & BINDING. UNIT WAS OVERHAULED IAW CM. 2L72 4F RTA16WE 20031218001702003121800170WP 2003 12 18 CALA0300690 120031204A533059114323 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 CRACK ON INNER SKIN FORWARD UPPER CORNER BY ROLLER ARM RIGHT MLG INNER DOOR. FABRICATED AND INSTALLED DOUBLER PER SRM 52-01 FIG 2. 2L72 4F A6WE 20031223000972003122300097NE 2003 12 23 VNAA0311009 220031125A7320 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE IBV VALVE CONTAMINATED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07463PS 3087 DURING FLIGHT, THE LT ENGINE TORQUE SHOWED 10 PERCENT AND THE FLIGHT RETURNED TO PIT. MAINTENANCE INSPECTED AND REMOVED DEBRIS FROM THE IBV CONNECTOR IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031223000402003122300040NM 2003 12 23 SWAA032661 120031204A57126545445 RIB BOEING737 7373A4 1384585NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND NR 3 SLAT LWR T/E SPAR CRACKED AT IB RIB OF ACTUATOR ATTACH POINT. REMOVED AND REPLACED NR 3 SLAT LWR T/E SPAR CORD PER SRM. 2L72 4F RTA16WE 20040106000372004010600037WP 2004 1 6 DHL2003802557 120031124A53204751820 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 742.250 RBL 20. REMOVED CRACKED FITTING FROM UPPER CARGO COMPT, STA 742.250 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201844, DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106000942004010600094SO 2004 1 6 C2XA03TY212 120031218A532014524131004 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS DURING A SCHEDULED 3C INSPECTION THE MAIN DOOR SILL WAS CORRODED AT THE NUT PLATES. MAINT REMOVED AND REPLACED THE MAIN DOOR SILL AND NUT PLATES. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031010000832003101000083EU 2003 10 10 BAQA089303 120030716A77129580113720 TRANSMITTER AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE TORQUE INDICATORREADS LOW B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 6425 TORQUE READS LOW. REPLACED WITH SERVICEABLE UNIT. 9/22/03 1G72 3U3 U H10EU E19EU 20040106001002004010600100NM 2004 1 6 DHL2003742529 120031120A5330 SKIN BOEING727 727225 1384077NM FUSELAGE LIGHTNING STRIKEA DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, LOWER FUSELAGE EXTERIOR BS 277 TO BS 178 AREAS SKIN DEEP BLEND OUTS BETWEEN STR 25R TO 26R. STRIPPED PAINT AND FOUND LIGHTNING STRIKES. DRILLED 6 EACH AREAS TO .250 AND INSTALLED FASTENERS IAW B-727 SRM 53-30-3 FIG 20. ONE EACH AREA FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED REPAIR FILLER IAW B-727 SRM 53-30-3 FIG 3. BARE METAL AND REPAIR PARTS. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED IAW B-727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20040109000082004010900008EU 2004 1 9 U022003F00000 120031027A27400210972700 MOTOR AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE731* 01518WP STAB TRIM FAILED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19519CW 19 AFTER 2 HOURS OF FLIGHT TIME THE NORMAL HORIZONTAL STABILIZER TRIM FAILS (EMERGENCY) TRIM WORKS. ON THE GROUND THE STABILIZER TRIM WORKS NORMALLY. THE STAB TRIM WOULD PASS ALL FUNCTIONAL TESTS. THE NORMAL MOTOR WAS CHECK AND FOUND TO HAVE FRICTION DISK BROKEN IN TOW PIECES. ONE OF THE TEFLON DISKS HAD SEPARATED FROM THE DISC BODY. TWO LOCATING PINS WERE OUT OF POSITION AND NO GREASE IN GREASE CUP. EVEN WITH ALL THESE PROBLEMS ALL FUNCTIONAL CHECKS WERE GOOD. EACH TIME THE AIRCRAFT WAS COLD SOAKED, THE NORMAL STAB TRIM MOTOR WOULD FAIL.(K) 2L73 4F4 F A46EU E6WE 20031125000082003112500008WP 2003 11 25 DHL2003805514 120030817A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING T/E UPPER SKIN SURFACE 0.500 CRACKED, STA XW 31.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-15 PG 1, SRM 51-1-21 PG 1, SRM 51-1-21A PG 1-4. 2L74 4F RT4A25 20031125000852003112500085WP 2003 11 25 DHL2003805536 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 816.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO NR 0249 FOR LEFT OUTER WING OTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031202000592003120200059 2003 12 2 USAABB03181 420031001A2565W460F1A RELAY BOEING767 767201 1385125NM SLIDE INDICATOR FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19646US 23898 DURING SQUIB TEST 1, THE EMERGENCY ESCAPE SLIDE INDICATOR LIGHT REMAINED EXTINGUISHED. MAINTENANCE REPLACED THE SQUIB TEST 1 RELAY, K838. (M) 2L72 4F RTA1NM 20031202001082003120200108EU 2003 12 2 ASOA03516 120031016A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11632AS 338 DURNG A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY FLOOD LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031205000262003120500026NM 2003 12 5 DL76K030913 120031009A33970201991008 WIRE HARNESS BOEING767 767332 1382001NM EMERGENCY LIGHT DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27175DZ 29696 FOUND SEATS 43F, 40B, 36B EMERGENCY PATH LIGHTS INOP. REPLACED WIRE HARNESS AT 43F, 40B, 36B. 2L72 4F RTA1NM 20031209001592003120900159NM 2003 12 9 03FDEA01781 120031007A5711ARB74132 SPAR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT WING - REAR SPAR UPPER SURFACE O/B OF O/B AILERON FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5710-74238 - WINGS, BASIC STRUCTURE - RIGHT REAR SPAR UPPER SURFACE CORROSION - XORS 1044.800. 2L73 4F RTA22WE 20031014000602003101400060NM 2003 10 14 SWAA032192 120031002A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) BS 360, STR 4R AND STR 10R. REMOVED AND REPLACED STR SPLICES PER SRM. 2L72 4F RTA16WE 20030919001202003091900120SO 2003 9 19 CHQA000417 120030817A2611 RMU EMB 145 EMB145 3260210SO NR 2 SMOKE A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL11280 NR 2 RMU SCREEN WENT BLANK AND SMOKE STARTED TO COME OUT OF IT. RR'D RMU. 2L72 4F RTT00011AT 20030915000902003091500090 2003 9 15 BAQA089074 420030909A22104008519913 COMPUTER BEECH 100 100BEECH 1152916CE AUTOFLIGHT SYS INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03777GS271 B241 COMPUTER INTERMITTENT. ERRATIC ROLL OPERATION. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20030919001562003091900156EU 2003 9 19 AWXA200300936 120030803A5320D53470476200 PROFILE AIRBUS320 A320232 3930326EU CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LT TRANSITION PROFILE BETWEEN FR 55-56. MAINTENANCE CUTOUT DAMAGE ON LT TRANSITION PROFILE BETWEEN FR 55-56; FABRICATED A REPAIR SPLICE AND FILLER; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5320-03154-SS1. 2L72 4F RTA28NM 20030922000942003092200094NM 2003 9 22 03FDEA01434 120030902A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - SEAT TRACK AT STA 1169 AND 1205, RBL 47 FOUND CROWN AREA DAMAGED. CORRECTIVE ACTION : SNRM N0375 : MAIN DECK - SEAT TRACK AT STA 1169 AND 1205 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL. 1. 2L73 4F RTA22WE 20030922000242003092200024NM 2003 9 22 2003UALA00621 120030812A5310 SHEAR TIE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA 29239 AFT CARGO PIT AT BS 1197+22 BETWEEN STR 39L-39R SHEAR TIE IS CORRODED. 2L72 4F4 FRTA1NM E24NE 20030923001732003092300173WP 2003 9 23 AALA20030796 120030726A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21568AA 49349 DURING OVERNIGHT MAINTENANCE, AFT STAIR SIDE WALL TAIL LIGHTS INOPERATIVE. SPLICED DAMAGED WIRE TO EMERGENCY STAIRWELL SIDE WALL TAIL LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20040128002062004012800206WP 2004 1 28 UPS04841681 120031229A5710 RIB DOUG DC8 DC871F 302199DWP LH WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XS 448.581. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040212000812004021200081NE 2004 2 12 MDR03026 120030812A64106516000025104 STRAP SKRSKYS64 S64E 8142604NE TAIL ROTOR BLADECRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09CGESG391 64V12401261 64065 THE STRAP IS CRACKED ON THE OUTBOARD SIDE OF THE BLADE, APPROXIMATELY 9.5 INCHES FROM THE TRAILING EDGE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROXIMATELY 2 INCHES. THE CRACK STARTS WHERE THE LEADING EDGE OF THE FAIRING, PN 65161-00011-042, (ON THE OUTBOARD SIDE) SLIDES BETWEEN THE STRAP, PN 65160-00025-104, AND THE CHANNEL ASSEMBLY, PN 65160-00029-081. CAUSE: UNKNOWN 2G72 4U H4EA 20040301000552004030100055CE 2004 3 1 CWQ2004F00002 120030513A2120651207212 VANE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA SCOOP CRACKED B CWQRK NONE O OTHER ININSP/MAINT 1 GL05394QS 5600394 DURING ROUTINE INSPECTION LOOKED INTO DORSAL NACA SCOOP AND SAW THE LOWER AIR VANE CRACKED AND MISSING 2 INCH PIECE OF VANE. GAINED ACCESS THROUGH BAGGAGE AREA, REMOVED BROKEN VANE AND LOCATED MISSING PART DOWN STREAM IN DUCT WORK (FRESH AIR) AFTER ACM AND BEFORE CHECK VALVE (REMOVED DEBRIS). CRACK APPEARED TO START FROM (V) CUT DUE TO NO RELIEF HOLE DRILLED AT INTERSECTION OF CUT OUT. INSTALLED NEW VANE AFTER IT WAS FIT AND RELIEF HOLE WAS DRILLED WITH LIBERAL AMOUNTS OF EA 9309 AND INSTALLED IAW MFG. REINSTALLED ITEMS, REMOVED FOR ACCESS AND CLOSED UP BAGGAGE AREA. 2L72 4F4 FRTA22CE E25EA 20031211000542003121100054NM 2003 12 11 AWXA200301406 120031104A3150 WARNING SYSTEM BOEING737 7373Q8 1384670NM COCKPIT ACTIVATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28327AW 23507 IND - ABORTED TAKEOFF - FLT 0182 - PREPARING FOR TAKEOFF AT IND EN ROUTE FOR PHX, AS THROTTLES WERE ADVANCED THE TAKEOFF WARNING CONFIGURATION HORN SOUNDED. REJECTED TAKEOFF AT APPROXIMATELY 20 KTS. TAXIED ON RUNWAY AND RESET FLIGHT CONTROLS, SUBSEQUENT TAKEOFF WAS NORMAL. 2L72 4F RTA16WE 20040316000042004031600004WP 2004 3 16 ASAA0380308 120030411A5320993653447 FLOOR SUPPORT DOUG DC9 DC983 3022083WP E/E BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 DURING 15K CHECK, E/E FLOOR SUPPORT IS CORRODED AT FS 180-190. REPLACED SUPPORT PER SRM 53-01 AND 51-30-2. (M) 2L72 4F RTA6WE 20040316000632004031600063WP 2004 3 16 GTIA031071 120031223A3350 LIGHT DOUG DC9 DC981 3022081WP TAIL COMPARTMENTDISCONNECTED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23818NK 48018 DTW - FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT NOT CONNECTED. CONNECTED TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT. (M) 2L72 4F A6WE 20040412001762004041200176WP 2004 4 12 ASAA0380716 120031103A532199366401 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 880-920. REPAIRED WITH FIBERGLASS OVERLAY PER SRM 51-70-3. (M) 2L72 4F RTA6WE 20031216000332003121600033NM 2003 12 16 SWAA032603 120031125A21307110025 CONTROL PANEL BOEING737 737301 1384611NM COCKPIT FAULTY A SWAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29659SW 23229 DIVERSION, CABIN ALTITUDE WARNING HORN SOUNDED, BOTH A/C PACKS SET IN HIGH AND NO HELP, OUTFLOW VALVE INDICATED FULL CLOSED. REMOVED AND REPLACED CABIN PRESS CONTROL PANEL AND RESEALED L1 DOOR HINGE AREAS PER MM. 2L72 4F RTA16WE 20031216000932003121600093SO 2003 12 16 C2XA03SH489 120031211A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 SHV-DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE CHAFED AT FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040512000692004051200069EU 2004 5 12 BAQA089812 120030910A2140L713M2053102 EJECTOR UROCOPEC135 EC135P1 8680990EU ENGINE WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH490 0179 EJECTOR WORN BEYOND LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 1G72 3U O H88EU 20030814000052003081400005 2003 8 14 SWAA031717 420030801A2565 INDICATOR BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030818000522003081800052EU 2003 8 18 BAQA087562 120030630A3340G83857 LANDING LIGHT BOLKMS117 BK117B1 5626012EU EXTERIOR MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE828 7219 LANDING LIGHT WILL NOT EXTEND OR RETRACT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030819000682003081900068EA 2003 8 19 SWIA200312126 120030616A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 625 RT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-52. 2L72 4F4 FRTA21EA E15NE 20030820000982003082000098CE 2003 8 20 DXTA200300070 120030720A3230 LANDING GEAR CESSNA500 560CESSNA 2076750CE LEFT MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07293QS 5600293 AFTER PUTTING GEAR HANDLE IN UP POSITION, GEAR UNSAFE LIGHT STAYED ILLUMINATED AND HYDRAULIC PRESSURE LIGHT CAME ON. PULLED GEAR CIRCUIT BREAKER AND LEFT MAIN GEAR FELL TO DOWN AND LOCKED POSITION. FOUND MLG ACTUATOR DEFFECTIVE, REMOVED AND REPLACED ACTUATOR IAW 560 MM CHAPTER 32-31-04. 2L72 4F RTA22CE 20030820000782003082000078WP 2003 8 20 03FDEA01159 120030728A5330NEA6013 SKIN DOUG DC10 DC1010 3022110WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 NR S 14 COMPLY WITH EA 8-5330-70980 FUSELAGE - PLATES AND SKIN - NEA6013 SKIN CRACK REPAIR AT STA 1154, LONGERON 38R. CLOSING ACTION ON 07/28/03 COMPLIED WITH EA 8-5330-70980. 2L73 4F A22WE 20030401001442003040100144WP 2003 4 1 DHL2003804553 120030203A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 "A" CARGO DOOR LOWER EXT. SKIN SHOWS WEAR (FS.280.000-340.000) PERFORMED MAJOR REPAIR IAW SRM52-1-0 PG. 1 , SRM51-9-0 FIG 68A, SRM 52-4-1 PG. 2 FIG. 1. REMOVED DAMAGED SKIN FROM "A" CARGO DOOR IAW SRM51-1-21 PG. 1 , SRM51-1-20D PG. 21. FABRICATED NEW SKIN (7075T6.050) IAW SRM 52-4-1 PG. 2 FIG 1 . CLEANED , TREATED AND PRIMED IAW SRM51-1-8B, INSTALLED NEW SKIN IAW SRM52-4-1 PG. 2 FIG.1 , SRM51-1-21 PG. 1 , SRM51-1-20D PG.9 , SRM51-1-15 PG. 1REFER TO N/R 0243 FOR "A" CARGO DOOR REMOVAL AND INSTALLATION. 2L74 4F RT4A25 20030821002492003082100249NM 2003 8 21 03FDEA01350 120030821A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 CORROSION (C53-113-01) ON FLOOR FUSELAGE SKIN STA 703 BL 0 WL 148. REPAIRED SKIN B.S 703, WL 148, BL 0, IAW SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20030821000112003082100011NM 2003 8 21 USAASB03113 120030718A4900 CSD BOEING737 7373B7 1384580NM NR 2 ENGINE DISCONNECTED A USAAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19527AU 23862 ON CLIMB-OUT FROM FLL, EN ROUTE TO DCA, CREW REPORTED THE NR 2 ENGINE GENERATOR TRIPPED OFF LIE AS THE NR 2 CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW STARTED APU AND PLACED THE APU GENERATOR ON LINE. AT FL240, THE APU SHUTDOWN WITH THE FAULT LIGHT AND THE LOW OIL PRESSURE LIGHTS ILLUMINATING. THE APU FAILED TO RESTART ON FIRST ATTEMPT AT FL250. CREW BEGAN DIVERSION PROCEDURES. AT FL140, THE APU STARTED ON SECOND ATTMEPT BUT CREW STILL ELECTED TO DIVERT TO MIA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE CSD TO BE INADVERTENTLY DISCONNECTED IN FLL. RECONNECTED NR 2 ENGINE CSD AND CHECKED OIL LEVEL. RAN ENGINE. OPERATIONAL CHECK NORMAL PER MM. THE APU WAS PLACED ON MEL.2L72 4F RTA16WE 20030410001002003041000100NM 2003 4 10 SWAA030672 120030322A32116582770 FITTING BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED A1 CHECK, FOUND BOTH LT & RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG WALKING BEAM FITTINGS PER MM. 2L72 4F RTA16WE 20030416002882003041600288WP 2003 4 16 AALA20030299 120030309A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114551 53033 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS ROW 23-26 INOPERATIVE. REATTACHED EMERGENCY EXIT LIGHT BATTERY AT SEAT 23-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030416001872003041600187NM 2003 4 16 AALA20030255 120030227A5330 SKIN BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21693AA 26973 TUL - FOUND LOWER FUSELAGE SKIN CORRODED AT SKIN SPLICE, STATION 1400 BETWEEN STRINGER 29L AND 29R. REMOVED CORRODED SECTION OF SKIN AND REPAIRED AREAS AFFECTED IAW ESO 90309 DATED 02/25/2003. REPAIR NR 26-536012-2570 AND REPAIR NR 26536012-257 DATED 02-27-03. (M) 2L72 4F RTA2NM 20030417001692003041700169NM 2003 4 17 UPS03240157 120030127A5320 FITTING BOEING727 72725C 138400HNM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, TO FACILITATE REPAIR TO BE 870 RT FITTING REMOVE FASTENERS X 20 BELOW PROPOSED CUT LINE AT S12 AND CARRY OUT NDT ON OPEN HOLES. FASTENERS REMOVED BELOW PROPOSED CUT LINE IAW SRM 51-30-02. FASTENER HOLE NDT INSP IAW NDTM H6 51-00-00 FIG 16 WITH NDF. FASTENER INSTALLATION IAW SMRO EO2003-005-003 + UPS EO B727-5310-182 54-A. 2L73 4F A3WE 20030424001642003042400164SO 2003 4 24 LR7A03019 120030313A5315 FLOORBEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC4911 FOUND LT FLOORBEAM CHINE ANGLE CRACKED AT FS 477, LBL 61, WL 140. REPAIR IAW SRM SMP 583 53-40-27. NR 2108. 2H74 4T A1SO 20030423002052003042300205NM 2003 4 23 UPS03240303 120030217A5312 PRESSURE PANEL BOEING727 727108C 1384039NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, SUSPECT CRACK AT AFT END OF BEAD IN RIGHT MLG CEILING AT BS 940 RBL 58 APPROX. REPAIRED IN CONJUNCTION WITH 940 FITTING REPLACEMENT REF NRC 631320. 2L73 4F A3WE 20030425000862003042500086NM 2003 4 25 QXEA0300393 120030320A2720 HINGE BOMBDRDHC8 DHC8401 1390041NM ZONE 300 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - FORE RUDDER UPPER MAIN HINGE WORN EXCESSIVELY OR MISSING PARTS. REPAIRED IAW DHC-8 400 SRM 51-22-40-340-801 AND HORIZON AIR EA 6-55-26. 2H72 4T RTA13NM 20030430001732003043000173NM 2003 4 30 SWAA030861 120030417A32106546113 PIN BOEING737 7373H4 1384600NM LT & RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 DURING SCHEDULED C3 CHECK, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM. 2L72 4F RTA16WE 20030502001712003050200171NM 2003 5 2 03FDEA00456 120030416A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION ON FLOORBEAM STA 1130 BETWEEN LBL 45 TO RBL 45 WL 200. 2L73 4F RTA3WE 20030502002542003050200254NM 2003 5 2 SWAA030848 120030415A53206547951 THRESHOLD BOEING737 7373H4 1384600NM FUSELAGE LEAKING A SWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW29339SW 24090 CABIN ALTITUDE ALERT HORN SOUNDED, EMERGENCY DESCENT TO 9,000 FT, NO MASKS WERE DEPLOYED. FOUND EXCESSIVE LEAK AT AFT CARGO DOOR THRESHOLD. REMOVED THRESHOLD, RESEALED & REINSTALLED PER MM. CONFIDENCE CHECK PASSED PER MM. 2L72 4F RTA16WE 20030505001392003050500139NM 2003 5 5 03FDEA00632 120030428A5312 BULKHEAD BOEING727 727200 138407ENM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT MLG WHEEL WELL STATION 870 BULKHEAD IS CRACKED AT RBL 56 W/L 185.5. REPAIRED IN ACCORDANCE WITH FEDEX EA 7-5310-69465. 2L73 4F RTA3WE 20030505001892003050500189NM 2003 5 5 EIA2003068 120030418A5230 STRUCTURE BOEING747 747273C 1384896NM CARGO DOOR LATCHCORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 NR 3R NOSE CARGO DOOR LATCH BOLT HOLE NR 3 HAS CORROSION. REAMED HOLE NR 3 FROM 0.621 TO 0.671 PER EO 53-747-1633-01 REV-C, FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED. 2L74 4F A20WE 20030506000772003050600077NM 2003 5 6 03FDEA00520 120030418A5230 PANEL BOEING727 727200 138407ENM DOOR LINER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CARGO DOOR LOWER PANEL DETERIORATED. *S/D* FABRICATED NEW PANEL IAW FED EX SRZ 25-005C. 2L73 4F RTA3WE 20030506000872003050600087WP 2003 5 6 MWEA030183 120030428A5230591014187 SKIN DOUG DC9 DC981 3022081WP CARGO DOOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 MID CARGO DOOR OUTER SKIN HAS A DAMAGED RIVET HOLE LOWER SIDE OF DOOR AT LOCATION OF INTERCOSTAL AREA. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20030506000502003050600050WP 2003 5 6 UPS03840454 120030415A5321 PRESSURE PANEL DOUG DC8 DC873F 302199FWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, LT NOSE WHEEL WELL TUNNEL, PRESSURE WEB IS CORRODED BEYOND LIMITS OUTBOARD OF HEAT EXCHANGER SUPPORT BRACKET AT STA -68 AT APPROX LBL 64. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, SPLICE, DOUBLERS, FINGER DOUBLERS IAW REPAIR DWG SRO8530026 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20030506001842003050600184WP 2003 5 6 ASAA0380228 120030307A5347002017001 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN SEAT TRACK CORROSION AT FASTENERS. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M) 2L72 4F A6WE 20030507001102003050700110SW 2003 5 7 AUS20030385 120030331A27202770001041 CONTROL CABLE SWRNGNSA227 SA227* SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL RUDDER WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT RUDDER CONTROL CABLE WORN BEYOND LIMITS. 2L72 4T4 TRTA5SW E4WE 6 CP61GL 20030513000162003051300016EU 2003 5 13 AALA20030277 120030304A3397 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114061 471 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28G INOPERATIVE. SECURED EMERGENCY EXIT LIGHT PLG AT SEAT 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030513001232003051300123NM 2003 5 13 UPS03240679 120030416A5347 SEAT TRACK BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C&SI, SEAT TRACK CRACKED AT O/B FLANGE, RBL 45.5 BETWEEN BS 780 - BS 804 REPLACED SEAT TRACK IAW DRAWING NR 65-41980 2L73 4F A3WE 20030530001212003053000121NM 2003 5 30 AMTA200300599 120030502A4920211734219 ECU BOEING757 75733N 1384931NM E/E BAY MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11551TZ 32585 APU WILL NOT START. REMOVED AND REPLACED ECU REF AMM 49-61-05-2. OPS GOOD. (M) 2L72 4F RTA2NM 20030602001772003060200177NM 2003 6 2 AALA20030543 120030506A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21797AN 30012 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON COAT CLOSET NEXT TO L1 DOOR BROKEN. REPLACED EMERGENCY EXIT LIGHT ON COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030604001352003060400135NM 2003 6 4 UPS03440555 120030410A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 AFT CARGO BELOW FLOOR SHEAR TIE FOUND CRACKED AT BS 1900 BETWEEN STR 44L AND STR 45L AS MARKED. SHEAR TIE REPAIRED AT BS 1900 BETWEEN STR 44L - 45L AS PER SRM 55-10-04 FIG.3A 2L74 4F A20WE 20030604001572003060400157NM 2003 6 4 UPS03440577 120030412A575365B106341 RIB BOEING747 747121 1384871NM NR 2 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 2 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1, 2, 3, 4, 5 AND 6 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO 747-5740-18687-A. 2L74 4F A20WE 20030610000162003061000016NM 2003 6 10 2003UALA00398 120030521A3397 WIRE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE EMERGENCY LIGHT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29615UA 21876 EMERGENCY EXIT LIGHTS FROM SEAT 26F AFT TO AFT GALLEY INOP. SUPPLEMENTAL DATA UPDATE SECURED LOOSE LEAD WIRE CONNECTORS AT EEL. 2L72 4F4 FRTA1NM E3NE 20030515001082003051500108NM 2003 5 15 CH1A200395050 120030425A5753 SKIN BOEING727 727290 138408WNM TE FLAP DELAMINATED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LEFT INBOARD FORE FLAP UPPER SURFACE (APPROX MID-WAY) DELAMINATED. 2L73 4F A3WE 20030610000942003061000094NM 2003 6 10 DL767030438 120030504A5753113T122625 SUPPORT FITTING BOEING767 767232 1385132NM LT WING TE FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27113DA 22225 THE ATTACH HOLE BORES FOR THE INBD FLAP, OUTBD SUPPORT FITTING ON THE LT WING WERE FOUND CORRODED WITH ADDITIONAL CORROSION ON THE FACES OF THE LUGS. THE HOLE BORES WERE OVERSIZED TO CLEAN UP THE CORROSION, HFEC INSPECTED, INSURANCE REAMED, AND ALUMINUM BUSHINGS INSTALLED. THE FACES WERE LIGHTLY SPOT FACED TO REMOVE THE CORROSION. THE REPAIR WAS ACCOMPLISHED PER ER/A 384974-14. 2L72 4F RTA1NM 20030612001692003061200169EA 2003 6 12 SWIA200312042 120030415A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA INTERCOSTAL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 625 RIGHT INTERCOSTAL ANGLE CRACKED STR 14R. REPLACED ANGLE IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20030613001052003061300105 2003 6 13 SWAA031245 420030605A2565D31591 INDICATOR BOEING737 7373H4 1384600NM SLIDE BOTTLE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030523001362003052300136WP 2003 5 23 DHL2003804887 120030206A57405769859164 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING L/E ZEE PAN CRACKED 2.000 INCHES AT STA XW 223.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED FITTING ZEE PAN CRACKED IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ZEE PAN ON RT WING L/E AT STA XW 223.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030528000142003052800014GL 2003 5 28 ERAA086436 220030424A72606894171 GEARBOX BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL ACCESSORY MAKING METAL E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01135EH13999 S675 GEARBOX MAKING METAL. 2 1/2 BEARING FAILED. OVERHAULED GEARBOX. COMPLIED WITH CEB A-1211 MAG PLUG INSP, CEB-A-1340 REMOVE PINION GEAR, CEB-A-1351, REPLACE OIL TUBE, CEB-1363 NEW DAMPER RING, CEB-A-1372 INSPECT DAMPER RING, AD 2001-24-12 PER CEB-A-1386. 1G72 3U3 UNCH3EU E4CE 20030618002062003061800206EU 2003 6 18 HEEA087523 120030610A6321AHA1121M0D1234 HEAD BOLKMS105 BO105S 5626006EU ROTOR BRAKE WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 BRAKE HEAD ASSY WEAK. REPLACED WITH SERVICEABLE ROTOR BRAKE. 1G72 3U H3EU 20030620000142003062000014SW 2003 6 20 HEEA087233 120030610A243523081018 STARTER GEN BELL 206 206L3 1182108SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 GENERATOR WILL NOT COME ON LINE. SHOP REPAIR. 1G71 3U H2SW 20030707001092003070700109WP 2003 7 7 UPS03840862 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE. UPPER RIB IS CRACKED AT XFS 822. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030707001952003070700195EU 2003 7 7 XNOA01125 120030603A2611 CONNECTOR AIRBUS300 A300B4203 3930306EU SMOKE DETECTOR DIRTY A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23224KW 073 ON TAXI OUT FLT DECK SMOKE LIGHT ILLUMINATED AND REMAINED ON. ACTION TAKEN: CLEANED CONNECTOR PLUG ON SMOKE DETECTOR AND RESET SET SYSTEM. OPS CHECK GOOD IAW A300 MM 26-14-00. 2L72 4F RTA35EU 20030709000602003070900060EU 2003 7 9 03149307 120030529A3350 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27307UE 41021 LT FWD EMERGENCY LIGHT OUT. REMOVED AND REPLACED LT FWD EMERGENCY LIGHT BULB. OPS CHECK GOOD. 2L72 4T RTA41NM 20030714000352003071400035NM 2003 7 14 SWAA031407 120030623A53306545765 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING CONNECTION CUTOUT, RT FWD FASTENER HOLE. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030714000552003071400055NM 2003 7 14 SWAA031380 120030619A53126545819 PRESSURE PANEL BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND BOTH LT AND RT NLG W/W WEBS CRACKED (2 EA) AT BS 246.0,WL 168.5. REPAIRED WEBS PER SWA EA. 2L72 4F A16WE 20030108000292003010800029WP 2003 1 8 MWEA030010 120030107A5520993780435 DOUBLER DOUG DC9 DC981 3022081WP OUTBD FAIRING CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 RIGHT ELEVATOR OUTBOARD FAIRING UPPER ATTACH STRIP IS CRACKED. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20030115001272003011500127EU 2003 1 15 BAQA082914 120030110A7712L771M20C1005 INDICATOR UROCOPEC135 EC135P1 8680990EU DUAL TORQUE MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01135ME1970 0009 DUAL TORQUE INDICATOR NR 1 NEEDLE DROPS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20030128002372003012800237SW 2003 1 28 HEEA083887 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030203002332003020300233EA 2003 2 3 COMA0360064 120030130A3350 BUSS CNDAIRCL600 CL6002B19 1900309EA A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01962CA 7123 FLIGHT 5785 ROW 1 EMERGENCY FLOOR LIGHTING IS INOP.CLEANED WATER CONTAMINATIN FROM LIGHT STRIP. 2L72 4F RTA21EA 20030204002132003020400213NM 2003 2 4 SWAA030159 120030122A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND 6 EA STRINGER CLIPS CRACKED, BS 500D, STR 19R AND 19L, BS 727A, STR 10L, BS 727B, STR 10L, BS 867, STR 9L, AND BS 727B, STR 13R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20030320001502003032000150NM 2003 3 20 2003UALA00144 120030204A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29675UA 29243 LT NOSE TUNNEL AT BS 246, LBL 40 VERTICAL STIFFENER - ATTACH ANGLE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH FABRICATION OF ANGLE AND DOUBLER, THEN INSTALLED. 2L72 4F4 FRTA1NM E24NE 20030219000812003021900081NE 2003 2 19 NACA20030077 220030130A8530356993 CYLINDER PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE #4 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 AL0399330475 475 28737 43576 28737 DISCREPANCY: #2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND OIL LOSS.CORRECTIVE ACTION: REPLACED #2 ENGINE #4 CYLINDER. 2L74 4R4 R A781 5E8 20030219001742003021900174EU 2003 2 19 AWXA200300161 120030205A5315D53911600203 ANGLE AIRBUS320 A320232 3930326EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW0 0 770 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON R/H FLOOR ATTACH ANGLE BETWEEN FR 33 - 34, FORWARD CARGO COMPARTMENT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR ATTACH ANGLE FR 33 - 34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2-8, PG. 1, 2, & 8 - 22. 2L72 4F RTA28NM 20030220000872003022000087NM 2003 2 20 DHL2003748001 120030220A3350 BATTERY BOEING727 727225 1384077NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01748DH 22440 1) NEITHER THE COCKPIT EMERGENCY EXIT OR THE ENTRYWAY EMERGENCY EXIT LIGHTS WORKED WITH THE SWITCH IN THE ON POSITION.2) REPLACED BATTERIES IN COCKPIT AND ENTRYWAY EXIT LIGHTS. OPS CHECKED GOOD IAW M/M 33-50-0. 2L73 4F A3WE 20030225000562003022500056 2003 2 25 HEEA084278 420030211A2312064101900 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032761N 45277 TRANSCEIVER INOPERATIVE. FOUND TRANSCEIVER WOULD NOT TURN ON. REPLACED BAD F101 FUSE. REPAIRED PROBLEM. FOUND DISPLAY WOULD NOT DIM PROPERLY. REPLACED BAD V501 PHOTOCELL AND ALSO BAD DISPLAY LENS. REPAIRED PROBLEM. ADJUSTED MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20030225000582003022500058SW 2003 2 25 HEEA084280 120030211A6710 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 MAIN ROTOR BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS 206001053005. REPAIRED. 1G71 3U H2SW 20030228000122003022800012NM 2003 2 28 SWAA030435 120030226A53116546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030303001262003030300126 2003 3 3 HEEA084545 420030214A342139563001 INDICATOR BELL 412 412 1182202SW ATTITUDE WILL NOT TEST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 ATTITUDE INDICATOR WON'T TEST. 1G72 4U H4SW 20030305000622003030500062 2003 3 5 HEEA084644 420030214A3454066107810 RECEIVER BELL 412 412EP 1182205SW VOR SYSTEM ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03412PH 36140 VOR SYSTEM YELLOW NEEDLE ERRATIC. SENT TO HONEYWELL, KANSAS FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20030305000872003030500087 2003 3 5 HEEA084670 420030213A34225040111920 GYRO AEROSPAS355 AS355* EU COCKPIT DAMAGED E HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03975AE 2777 PILOT HORIZON GYRO INDICATOR INSTRUMENT MAKE LOUD ROARING NOISE WHEN SELECTED ON. ALSO FEELS HOT WHEN RUNNING. SMELL OF SMOKE NOTED WHILE RUNNING HORIZON GYRO. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H11EU 20030306000532003030600053SW 2003 3 6 HEEA084768 120030221A3246412050015111 SKID BELL 412 412 1182202SW MLG CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 SKID TUBE HAS A SMALL CRACK AT FORWARD CUFF INBOARD. 1G72 4U H4SW 20030310000772003031000077 2003 3 10 HEEA084981 420030227A22157001484 ACTUATOR BELL 412 412 1182202SW YAW CONTROL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 YAW NEEDLE DEFLECTS FULL LEFT AND STAYS. 1G72 4U H4SW 20030314001042003031400104 2003 3 14 SWAA030512 420030306A256565C16820 GIRT BAR BOEING737 7377H4 1384404NM L2/R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29729SW 27861 BOTH AFT CABIN DOOR EVACUATION SLIDE GIRT BARS WOULD NOT GO IN BRACKETS. REMOVED AND REPLACED BOTH EVACUATION SLIDE ASSY'S PER MM. 2L72 4F RTA16WE 20030121003172003012100317WP 2003 1 21 MWEA030036 120030118A7600 LINE DOUG DC9 DC981 3022081WP ENGINE DISCONNECTED A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31804ME 48030 ON LEFT THROTTLE, SPLIT INCREASED WITH ALTITUDE TO ABOUT 1 1/2 KNOBS. -- RECONNECTED PRESSURE TOTAL 2 LINE. 2L72 4F A6WE 20030317000372003031700037NE 2003 3 17 03FDEA00172 220030222A7321 COMPRESSOR BOEING727 727277 138408SNM PWA JT8 JT8D NE ANTI-ICE SYSTEM STALLED A FDEAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SO25245FE 22016 UPON LEVELING AT FL310 WITH CRUISE POWER SET AND AFTER CLOSING ENGINE, ANTI-ICE COMPRESSOR STALLS. NR 2 ENGINE EPR DROPPED FROM 1.8 TO 1.2,EGT STARTING TO CLIMB, NR 2 THROTTLE TO IDLE. SLOWLY RESTORED NR 2 POWER AND CYCLED ENGINE ANTI-ICE BACK TO OFF, COMPRESSOR STALLS RE-OCCURRED, NR 2 THROTTLE BACK TO IDLE, OBSERVED 3 HARD COMPRESSOR STALLS, SHUTDOWN ENGINE IAW QRH. REMOVED AND REPLACED NR 2 ENGINE. 2L73 4F4 FRTA3WE E2EA 20030625001272003062500127NM 2003 6 25 03FDEA00290 120030303A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RTWING O/B FLAP I/B HINGE O/B LUG HOLE CORRODED. RIGHT O/B FLAP- I/B HINGE AFT SUPPORT BORE CORROSION REMOVED AND BUSHING REPAIRED AS PER FEDEX EA 1-5750-66818. 2L73 4F RTA22WE 20030318000082003031800008GL 2003 3 18 ALGA085104 220030306A73136899001E FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE DEFECTIVE H ALGAO OTHER O OTHER NRNOT REPORTED 1 FS01361AL15231 51212 ENGINE LOW MOANING/ BURBLING NOISE WITH N1 OSCILLATIONS AT FLIGHT IDLE. 1G71 3U3 U H2SW E1GL 20030326000032003032600003EA 2003 3 26 AUS20030085 220030128A7310UK DIAPHRAGM PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL PRESSURE REG FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL PRESSURE REGULATOR DIAPHRAGM SUSPECT FAULTY. 1L72 3O3 O A20SO E14EA 5 CP33EA 20030327000142003032700014NM 2003 3 27 AWXA200300281 120030317A3030851JB PROBE BOEING757 7572S7 1384962NM NR 1 ENGINE P1 FAULTY A AWXAO OTHER J WARNING INDICATION CLCLIMB 1 WP28901AW 23321 EN ROUTE FROM SJD TO PHX RECEIVED NR 1 ENGINE PROBE HEAT STATUS MESSAGE, DECLARED EMERGENCY AND LANDED WITHOUT EVENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE P1 PROBE, OPERATIONAL CHECK WAS GOOD IAW BMM 30-34-00. 2L72 4F RTA2NM 20030324000282003032400028WP 2003 3 24 0300571226 120030323A5712 SILL DOUG DC10 DC1030 3023501WP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01226NW 46583 During "M" check found crack in left wing upper leading edge sill at station XW 244 LHS. Repaired per EA 12-194275. 2L73 4F A22WE 20030325000282003032500028NM 2003 3 25 AWXA200300143 120030215A33501012623 LIGHT BOEING737 737277 1384570NM SEAT ROW 9 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND BROKEN AT SEAT ROW 9 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030418000572003041800057NM 2003 4 18 QXEA0300264 120030206A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - X730 Y1.5R SEAT TRACK TOP FLANGE IS GOUGED. REPAIRED IAW HORIZON AIR EA 6-53-193. 2H72 4T RTA13NM 20040223000092004022300009 2004 2 23 G6OA03073 420031230A3197S3663 TERMINAL BLOCK BELL 206 206B3 1181506SW GE CF6 CF650C2 30018NE INSTRUMENT PANELSHORTED A G6OAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27612 4200 MOMENTARY FLASH OF MASTER WARNING 3 SEPERATE TIMES 3RD TIME POSSIBLY ACCOMPANIED BY CARGO FIRE LIGHT ON PILOTS PANEL. 1G71 3U4 F H2SW E23EA 20030716000842003071600084WP 2003 7 16 GTIA030454 120030614A3260 CONNECTOR DOUG DC9 DC982 3022082WP PSEU LOOSE A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23820NK 49126 WITH GEAR UP, LANIDNG GEAR DOOR OPEN LIGHT WAS ON, THERE WERE NO GER UNSAFE LIGHTS ON LIGHT STAYED ON AN HR AND THEN EXTINGUISHED. IN CLIMB, THE LANDING GEAR DOOR OPEN LIGHT CAME ON WITHOUT A GEAR UNSAFE LIGHT. AFTER LEVELING OFF AT ALT, THE LIGHT EXTINGUISHED. GEAR DOOR OPEN LIGHT COMES ON ITNERMITTENTLY IN FLIGHT. GEAR DOOR OPEN LIGHT ILLUMINATES INTERMITTENTLY. FOUND LOOSE CONNECTOR FOR GEAR DOOR UP, SECURED CONNECTOR AND CYCLED GEAR DOOR SEVERAL TIMES, NO DEFECTS NOTED. T/S MLG DOOR INDICATOR DETERMINED THE TARGET TO SENSOR GAP OUT OF LIMITS ON BOTH GEAR DOORS, ADJUSTED GAP ON BOTH DOORS, OPS CHECK GOOD. REMOVED AND REPLACED PSEU OPS CHECK PASS. T/S PSEU, FAILED LEFT MAIN GEAR DOOR SENSOR R/R LEFT MA2L72 4F A6WE 20030321000312003032100031NM 2003 3 21 2003UALA00188 120030207A5754114W424012 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLAT NR 11 DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29766UA 26917 DELAMINATED TRAILING EDGE WEDGE SLAT, NR 11 BECAME DELAMINATED. REMOVED AND REINSTALLED TRAILING EDGE WEDGE. 2L72 4F4 FRTT0001SE E46NE 20030825000532003082500053WP 2003 8 25 UPS03841124 120030819A33505708403 BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT TEST. R&R EMERGENCY LIGHT BATTERY PACK. P/N ON AND OFF 5708403, S/N ON FLS/ST/7021, S/N OFF CAW250. 2L74 4F RT4A25 20030828000612003082800061NM 2003 8 28 P5CA0300919 120030819A575365B08422201 PANEL BOEING747 747200 1384847NM T/E FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 LT IB MID FLAP OF DELAMINATION AT OUT MID FLT PANEL. CORRECTIVE ACTION TAKEN: PANEL REPLACED SRM 51-10-01 AND 51-30-02. 2L74 4F RTA20WE 20030828001302003082800130WP 2003 8 28 MWEA030298 120030729A5310SRO95200089 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 AFT CARGO LOWER DOOR JAMB HAS LIGHT CORROSION ON REPAIR DOUBLER AROUND SCREW HOLES AT STATION 1162-1205. FABRICATED NINE SPACERS AND INSTALLED DOUBLER. 2L72 4F A6WE 20030829001482003082900148 2003 8 29 SWAA031842 420030816A2565D31354 SLIDE BOEING737 7377H4 1384404NM ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030723000272003072300027NM 2003 7 23 UIEA200300026 120030520A532165B38140606 FLOOR PANEL BOEING747 747228F 1384895NM FUSELAGE DELAMINATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15809MC 20887 DURING C-CEHCK AT SIN, FOUND FLOOR PANEL DELAMINATED AT FS 2040 TO STATION 2140, RIGHT SIDE RBL 33.00-75.00. REPAIR BOND A 2024-T3 REPAIR DOUBLER TO THE UNDERSIDE OF THE FLOOR PANEL, PER REF'A'. REPAIR PER REF 'A' IS TIME LIMITED. DER APPROVAL OF REF 'A' ENGINEERING INSTRUCTIONS FOR THE SUBJECT TIME LIMITED REPAIR. REPLACE FLOOR PANEL WITH A NEW PANEL, THAT IS EQUIVALENT TO THE PRODUCTION PANEL, WITHIN 90 DAYS. ISSUED MCI A130 TO CHANGE FLOOR PANEL. (M) 2L74 4F A20WE 20030722001312003072200131NM 2003 7 22 AWXA200300658 120030516A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 5.7, WL 212.5-213.5. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08 PG 286. 2L72 4F RTA16WE 20030801000292003080100029WP 2003 8 1 GTIA030552 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-196, 44 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030905000292003090500029SO 2003 9 5 LR7A03073 120030725A5312 PRESSURE PANEL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL FS 577 WEB CRACKED APPROX 1.75 INCHES AT LBL 61, WL 150. REPAIRED IAW SRM SMP 583 51-140-17. NR 2153. 2H74 4T A1SO 20030812000962003081200096EU 2003 8 12 HEEA088642 120030804A5302355A1305200303 SPAR AEROSPAS355 AS355* EU STABILIZER CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH3176 3352 STEEL OUTER SPAR STRAP IS PITTED AND CHAFED AND CENTER SKIN IS CRACKED. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030813000482003081300048NM 2003 8 13 2003UALA00462 120030531A3350 LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29536UA 25156 LEFT AFT OFF-WING EMERGENCY SLIDE LIGHT AFT OF AFT OVERWING EXIT HATCH INOPERATIVE. RELAMPED LIGHT. 2L72 4F4 FRTA2NM E17NE 20030814000662003081400066EA 2003 8 14 SWIA200312224 120030725A5346 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 REINFORCEMENT ANGLE AND FRAME ON LEFT SIDE OF FS 640.00 BETWEEN STR 9 AND STR 12 IS CRACKED NEAR TOP OF BOX BEAM. DISCOVERED DURING A CHECK INSPECTION. REPLACED LEFT QUARTER FRAME AT FS 640 WITH SERVICEABLE UNIT IAW SRM 51-42-06 AND 51-42-20. 2L72 4F RTA21EA 20030822000752003082200075EA 2003 8 22 QXEA200300935 120030730A7110 COWLING CNDAIRCL600 CL6002C10 1390015EA NR 1 ENGINE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX- UPPER CORE COWL HAS FOD DAMAGE AT 12 O'CLOCK POSITION OF NR 1 ENGINE. REPAIRED IAW HORIZON AIR EA R-54-33 AND REO 670-54-23-129. 2L72 4F RTA21EA 20030911002242003091100224WP 2003 9 11 DHL2003803014 120030818A33505708458503 BATTERY DOUG DC8 DC873 302199CWP CABIN DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01803DH 46123 EMERGENCY LIGHT BATTERY DRAINED. REPLACED IAW M/M 33-50-1. OPS CHECKED SERVICEABLE. 2L74 4F RT4A25 20030912001722003091200172EU 2003 9 12 AALA20030864 120030816A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211430D 11415 ORD - FORWARD HALF OF EMERGENCY LIGHTS IN CABIN DO NOT OPERATE DURING CHECK OF EMERGENCY LIGHTS. REPLACED FLOOR LIGHTING SECTION FROM FIRST CLASS TO COACH SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031001001122003100100112NM 2003 10 1 USAA030175 120030827A5553AMS4640 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US 23984 PIT FOUND FITTING CORRODED 1 INCH LONG INSIDE RADIUS BORE, VERT STAB AFT RT OUTBOARD LUG FWD CLEVIS BETWEEN CLEVIS AND T-FITTING. REMOVED AND REPLACED BUSHING/OVERSIZE PER EA 76801. (M) 2L72 4F RTA16WE 20031006001042003100600104NM 2003 10 6 2003UALA00672 120030909A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29372UA 24637 DENTED FUSELAGE SKIN AT BS 388-393, STR 5L TO STR 7L, 11 INCHES LONG AND 1 INCH WIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031003000862003100300086NE 2003 10 3 154691 220030912A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT FAILED A UHLAECD ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK JMXWARNING INDICATION OVER TEMP ENGINE FLAMEOUT TOTAKEOFF 1 GL1740SZ 40 GEE367488 DURING TAKE-OFF ROLL AT 60 PERCENT TQ CTOT WAS NOT ARMED. THE CREW HEARD A LOUD BANG, AND THE RT ENGINE TQ STARTED TO DROP AND THE RT ENGINE ITT SPIKED AND THE ENGINE OVERTEMP WARNING LIGHT ILLUMINATED. PAX AT SEAT 10F SAW FLAMES FROM TAILPIPE. THE CREW IMMEDIATELY SHUT DOWN THE ENGINE AND RETURNED TO THE GATE. A/C TAKEN OUT OF SERVICE AT 1445(LT). 2L72 4T4 TRTA52EU E8NE6 20031021002872003102100287NM 2003 10 21 CALA0300545 120030920A5311 FRAME BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND BELTFRAME CORRODED AT STA 500, S28R TO S28L. A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07. 2L72 4F4 FRTA16WE E2GL 20031023000612003102300061NE 2003 10 23 QXEA200301178 220030921A7310 MANIFOLD DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 400 MALFUNCTIONED A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09350PH 488 AG0052 SEA- ON FLIGHT 2246 DURING NR.1 ENGINE START RAMP AGENT REPORTED FLUID THAT SMELLED LIKE FUEL LEAKING FROM NR 1 ENGINE NACELLE DRAIN. FOUND NR 1 ENGINE DRAIN MANIFOLD FULL. DRAINED MANIFOLD AND RAN NR 1 ENGINE FOR 5 MINUTES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031028001682003102800168EA 2003 10 28 ASOA03471 120031001A5260601R3167013 STEP CNDAIRCL600 CL6002B19 1900309EA AIRSTAIR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11916AS 7757 FLT 4642 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEOP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. () 2L72 4F RTA21EA 20031029000712003102900071NM 2003 10 29 ASAA0340095 120030228A531065C25228 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE BS 727C RBL 9 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040114002032004011400203WP 2004 1 14 MWEA030500 120031231A53125910130 BULKHEAD DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31501ME 47132 LOWER LT VENTRAL DOOR CORNER WEB IS CRACKED. INSTALLED DOUBLERS TO BOTH LOWER DOOR CORNERS OF THE AFT PRESSURE BULKHEAD. 2L72 4F A6WE 20031030000782003103000078NM 2003 10 30 QXEA200301196 120030927A5320 WEB DHAV DHC8 DHC8202 2809007NM ZONE 200 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 LEFT FUSELAGE WEB BETWEEN FRAMES 370.8 AND 354.250 ARE BROKEN AT FORWARD INBOARD END. REPAIRED IAW DHC-8 SRM 51-40-11, RD 8-53-7556 AND HORIZON AIR EA 2-53-485. 2H72 4T RTA13NM 20031106001172003110600117NM 2003 11 6 03FDEA01860 120031103A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-111-01, 2) FWD CARGO COMPARTMENT SHEAR TIE ON AT SIDE OF BS 700 FRAME LBL 9 WL 148. 2L73 4F RTA3WE 20030731000442003073100044NM 2003 7 31 QXEA200300864 120030719A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM AFT AIRSTAIRS LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09402QX 4032 SEA- ON FLIGHT 2321 AFT AIRSTAIR DOOR WILL NOT OPEN. CLEANED AND LUBED AFT PASSENGER DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030915000442003091500044CE 2003 9 15 BAQA088852 120030826A33005102CW28 LIGHT BEECH 100 100BEECH 1152916CE CABIN MISMANUFACTURED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03777GS B241 POST LIGHTS HAVE FACTORY DEFECT. WILL SHORT OUT IF CHANGING LIGHT BULB. WE HAD TALKED TO NICK FISCHER. 1L72 3T A14CE 20040112002792004011200279WP 2004 1 12 AALA20031415 120031210A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21591AA 53254 ORD) OVERWING LOWER SIDE WALL EMERGENCY LIGHT AT ROW 2 INOPERATIVE. RESEATED BATTERY PACK FOR OVERWING LOWER SIDE WALL EMERGENCY LIGHT AT ROW 2. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA6WE 20031117000572003111700057EA 2003 11 17 COMA0360443 120031003A2613355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA BLEED SENSOR FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01716CA 7250 FLIGHT 5703 LT 14TH STAGE BLEED LEAK WARNING. REPLACED THE PYLON BLEED LEAK SENSE ELEMENT. 2L72 4F RTA21EA 20031118000632003111800063SO 2003 11 18 C2XA03SH378 120031009A542014576526008 STIFFENER EMB 145 EMB145LR 3260212SO LT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 DURING C-CHECK THE INBOARD STIFFENER OF THE LEFT ENGINE COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040114000602004011400060SO 2004 1 14 CHQA0000429 120031118A2741 CONTROLLER EMB 135 EMB135KL 3260302SO PITCH TRIM MALFUNCTIONED A CHQAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL11371 145535 ON DEPARTURE FROM DCA AT 8000 MSL RECEIVED THE PITCH TRIM 1-2 INOP ON THE EICAS. MAIN AND BACKUP TRIP CONFIRMED INOP BY TRIM SWITCHES. COMPLETED EMERGENCY CHECKLIST AND EMERGENCY WAS DECLARED INTO IAD. EMERGENCY EQUIPMENT WAS STANDING BY AND MADE UNEVENTFUL LANDING. NO FURTHER INFO AT THIS TIME. MAINTENANCE INVESTIGATED THE PROBLEM AND RESET PITCH TRIM SYSTEM 1 & 2 AND OPERATIONAL CHECK WAS SATIFACTORY PER AMM 27-40-00. 2L72 4F RTT00011AT 20040114000812004011400081NE 2004 1 14 ABXA030451 220031118A7230803723 ACOUSTIC LINER BOEING767 767231 1385131NM PWA JT9 JT9D7R4D 52054NE NR 2 ENGINE MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23708AX 22571 707546 NR 2 ENGINE REVERSER OUTBOARD SIDE INNER AREA HAD DAMAGE DUE TO LIBERATION OF A P/N 803723 ENGINE FAN EXIT CASE OUTBOARD ACOUSTIC LINER SEGMENT ASSEMBLY, WHICH RAN FROM THE 3 O'CLOCK TO THE 5 O'CLOCK POSITION, AFT FACING FORWARD. REPLACED NR 2 ENGINE OUTBOARD REVERSER IAW BMM 767 78-31-01-4. OPS CHECKED GOOD. 2L72 4F4 FRTA1NM E3NE 20040113001272004011300127CE 2004 1 13 BAQA088980 120031112A3233508202085 ACTUATOR BEECH 90 C90 1152913CE NLG FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0390LF 737 LJ852 NLG ACTUATOR FAILED END PLAY INSPECTION. REPLACED WITH SERVICEABLE UNIT. 12/10/03 1L72 3T 3A20 20031218001592003121800159SO 2003 12 18 C2XA03SH480 120031204A532014522460009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 SHV- DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031223000472003122300047NM 2003 12 23 SWAA032668 120031206A2750657327121 TUBE BOEING737 7373H4 1384600NM RT WING TE FLAP WORN A SWAAO OTHER O OTHER APAPPROACH 1 SW29360SW 26571 DURING T/E FLAP EXTENSION, LT T/E FLAP POSITION INDICATED 30, WHILE THE RT INDICATED 25. REMOVED AND REPLACED RT T/E FLAP TRANSMISSION TORQUE TUBE PER MM. 2L72 4F RTA16WE 20040106000602004010600060SO 2004 1 6 C2XA03CL201 120031217A335078241 INVERTER EMB 135 EMB135LR 3260305SO CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2728529 145512 CLE FLIGHT 2115 THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CABIN EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030919000412003091900041NM 2003 9 19 IU62003F00025 120030530A278165447526 HOUSING BOEING737 737* NM ACTUATOR CRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 4121CN SLAT ACTUATOR HOUSING CRACKED. ADD TO NDI REQUIREMENTS IN OHM. (NR 177789) 2L72 4F RTA16WE 20031008000432003100800043 2003 10 8 VNAA0309007 420030808A3417861EF1 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AOA FAILED A VNAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07434JS15588403 3051 THE CREW REPORTED RECEIVING A RIGHT HAND SHAKER ON SIDE CAS MESSAGE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE ANGLE OF ATTACK SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031124001572003112400157NM 2003 11 24 QXEA200301278 120031012A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX- LT HAND INBOARD SEAT TRACK NR 4 HAS DEEP PITTING CORROSION ON FLANGE AROUND RIVET HOLES BETWEEN STATION X195 AND X202. REPAIRED IAW RD8-53-1102, RD8-53-4473 AND SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20031202000252003120200025NM 2003 12 2 ASAA0310495 120030602A53306545767 SKIN PANEL BOEING737 7372X6C 1384552NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 378, WATERLINE 184.1L DENTED. CUT OUT DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20040123000082004012300008 2004 1 23 ASAA0380687 420031021A25653961896501 LANYARD DOUG MD80 MD83 3023681NM R1 DOOR DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01982AS 53473 PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RT 20031203000152003120300015NM 2003 12 3 GAIA03135ST 120031024A5330 SKIN BOEING727 727243 138408DNM FUSELAGE GOUGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN LAP SEAT GOUGED AT BS 720E STRINGER 19 RT. REF FASI N/R NR 61529, CUT OUT DAMAGE AND INSTALLED LAP SEAM REPAIR DOUBLER PER B727 SRM 53-30-3 FIG 14. (M) 2L73 4F RTA3WE 20031209001552003120900155NM 2003 12 9 QXEA200301373 120031026A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 REPLACE NR 4 SEAT TRACK DUE TO CORROSION DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-11, 51-30-26 AND RD'S 8-53-1102 AND 8-53-4473. 2H72 4T RTA13NM 20031208000062003120800006NM 2003 12 8 MWEA030471 120031203A53473952158503 GALLEY TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 AFT INBOARD G2 GALLEY MOUNT FITTINGS AT STATION 218 IS CORRODED. FABRICATED AND INSTALLED FITTINGS. 2L72 4F RTA6WE 20031209001512003120900151NM 2003 12 9 QXEA200301368 120031021A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 LEFT HAND OUTBOARD NR 1 SEAT TRACK ATTACH AREA HAS TOP CORROSION AT STATION X298.00. REPAIRED IAW DHC-8 RD 8-53-1342. 2H72 4T RTA13NM 20030922000772003092200077NM 2003 9 22 AWXA200300954 120030804A5320D53974972200 PROFILE AIRBUSA319 A319132 3930340NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 56, STR 39 LT - 39 R/H. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 56, STR 39 LT - 39 RT; FABRICATED A NEW REPLACEMENT PROFILE PER DWG 17-D53974972; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12, & 21-22, FIG. 3 & 8. 2L72 4F RTA28NM 20040122001432004012200143CE 2004 1 22 R142003F00002 120031030A324036800111 CALIPER CESSNA150 150L 2071826CE CONT O200 O200* 17020SO LT BRAKE CORRODED B R14RO OTHER O OTHER NRNOT REPORTED 1 EA17427JW 15073873 LEFT BRAKE CALIPER REMOVED AND INSPECTION OF PART FOUND CORROSION AND PITTING ON CALIPER PISTON WALLS. PISTON WAS BINDING WHEN MOVED. THE PISTON WOULD NOT MOVE FREELY WITNIN CALIPER HOUSING. INSTALLED NEW LEFT BRAKE CALIPER. 1H71 3O3 O 3A19 E252 20040127001762004012700176WP 2004 1 27 ASAA0380638 120031015A53305936004 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 769 TO 788 UNDER FAIRING RUB STRIP AND AROUND FASTENER HOLES. INSTALLED DOUBLER, FILLERS, ANGLE, SHIMS, TRIPLER, AND SPLICE PER EA 5330-01708. (M) 2L72 4F RTA6WE 20040129000502004012900050EU 2004 1 29 MALA030588 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 7D, 7E & 7F FRAMES CRACKED. ACCOMPLISHED WELD REAPAIRS ON SEAT FRAMES 7A, 7E & 7F IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040128001592004012800159EA 2004 1 28 SWIA200312732 120031225A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07961SW359 359 7857 STAB TRIM CH 2 FAILS FFOD CHECK. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL PER TASK CARD RII 27-415. OPS CHECK GOOD. P/N 7062-3, S/N ON 786, S/N OFF 1184. 2L72 4F RTA21EA 20040129000032004012900003EA 2004 1 29 COMA0360574 120031213A5320601R35031211 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01809CA 7366 RIGHT HAND 621 FLOOR SUPPORT ANGLE CRACKED. REPAIRED IN ACCORDANCE WTIH REO 601R-53-61-117 AND CRJ SRM 51-25-16. 2L72 4F RTA21EA 20040130002252004013000225NM 2004 1 30 AWXA200400038 120031224A5412311N5033 FITTING BOEING757 7572G7 1384963NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .0625 INCH CRACK WAS FOUND IN FORWARD SLEEVE BOLT HOLE OF NR 1 ENGINE PYLON RT MID BULKHEAD FITTING PPS 174.30. MAINTENANCE REAMED OUT HOLE; FABRICATED A BUSHING; INSTALLED REPAIR PART IAW AWA ER 19-5453-04006-SS1. 2L72 4F RTA2NM 20040206000052004020600005NM 2004 2 6 MEX2003522 120031115A7410103538754 IGNITER BOX DOUG MD80 MD83 3023681NM NR 1 ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23946AS2687 2687 49658 AIRCRAFT RETURNED TO PLATFORM DUE TO LT ENGINE IGNITION IN (OVER) AND (GROUND) POSITION IS OUT OF SERVICE. IGNITION BOX WAS REPLACED AND TESTS WERE PERFORMED IAW MM 74-10-01, ALL OK. 2L72 4F RT 20031212001682003121200168WP 2003 12 12 AALA20030919 120030831A3350 CONNECTOR DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21441AA 49460 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE ON CATWALK. SECURED LOOSE CONNECTOR ON FORWARD CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001382003121500138WP 2003 12 15 AALA20031088 120031001A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21253AA 49286 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031212001282003121200128NM 2003 12 12 AWXA200301434 120031027A5320655384420 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR CHANNEL BETWEEN BS 807 AND BS 814, RBL 13.80. MAINTENANCE REMOVED CORRODED FLOOR CHANNEL BETWEEN BS 727 AND BS 945, RBL 13.80; FABRICATED A NEW REPLACEMENT FLOOR CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 10, PG 1. 2L72 4F RTA16WE 20040525000392004052500039EU 2004 5 25 2004F00129 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FASTENER HOLE BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L. (M) 2L72 4F RTA28NM 20040601001182004060100118WP 2004 6 1 04FDEA01496 120031201A5512ALC74391 SKIN PANEL DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25560FE 46938 HORIZONTAL STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF FEDEX NRC N1102) *S/D COMING* 2L73 4F4 FRTA22WE E23EA 20030926000252003092600025NM 2003 9 26 DHL2003748500 120030820A5320 WEB BOEING727 727225 1384077NM CARGO FLOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 DURING C-CHECK AT PEMCO, AFT CARGO DOOR LOWER LOBE BULKHEAD STA 1183, APPROX BL 44, UPPER FLOOR WEB CRACKED IN 2 EACH PLACES. STOPPED DRILLED CRACK IAW B-727 SRM 51-10-01. REMOVED ACCESS COVER ON TOP OF FLOOR, FOUND CORROSION UNDER COVER, MATERIAL OUT OF LIMITS IAW B-727 SRM 51-10-6. CUT AND REMOVED DAMAGED AREA IAW B-727 SRM 51-10-01. MATERIAL ID FOR NEW DOUBLER AND FILLER 160 X 48 X 144 7075 T-6 PO 0230573. FABRICATED, DRILLED AND DEBURRED NEW DOUBLER AND FILLER IAW B-727 IAW B-727-SRM 51-30-8. ALODINED, PRIMED AND INSTALLED IAW B-727 SRM 51-30-2, 51-10-6. 2L73 4F A3WE 20030929000442003092900044NM 2003 9 29 03FDEA01404 120030903A32607500357 PANEL BOEING727 727100 1384036NM COCKPIT MALFUNCTIONED A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25136FE 19855 ON INITIAL GEAR EXTENTION, ALL RED GEAR DOOR LIGHTS OPERATED NORMALLY BUT ONLY GREEN MAIN GEAR LIGHTS ILLUMINATED (NO GREEN NOSE GEAR LIGHT). RECYCLED GEAR UP / DOWN, TWO MAIN INDICATED BRIGHT GREEN, NOSE INDICATED VERY DIM GREEN, CYCLED LIGHT TEST SWITCH AND NOSE GEAR THEN ILLUMINATED BRIGHT GREEN (ALL NORMAL). REMOVED & REPLACED L/G ANNUNCIATOR PANEL PER MM 32-61-001-64 NEEDS OPS CK REPLACED SW S96 PRECAUTIONARY, OPS CHECKED ANNUN PANEL PER MM 32-61-021-5, OK FOR SERVICE. 2L73 4F RTA3WE 20040903000122004090300012GL 2004 9 3 I5HA0358006 220031226A72616850819 PUMP CVAC 580 580 2422806WP ALLSN 501D 501D13 03004GL RT ENGINE OIL MALFUNCTIONED A I5HAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 GL23582P 475 WHILE EN ROUTE, RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WITH AN ASSOCIATED DROP IN REDUCTION GEARBOX OIL PRESSURE FROM APPROXIMATELY 150 PSI TO 100 PSI. NORMAL LIMITS ARE 130 PSI TO 250 PSI. CREW PERFORMED AN EMERGENCY IN FLT ENG SHUTDOWN USING THE E-HANDLE & PRECEEDED TO PIT & LANDED UNEVENTFULLY. REMOVED AND REPLACED RT REDUCTION GEARBOX OIL PUMP. PROPER FUNCTION OF THE PUMP HAS BEEN VERIFIED AT LOW SPEED GROUND IDLE BUT HAS NOT BEEN VERIFIED AT HIGH SPEED GROUND IDLE DUE TO AN UNRELATED ENGINE FAILURE AT THE TIME OF THE FUNCTIONAL CHECK OF THE PUMP. THE ENGINE IS TO BE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN UNTIL THE ENGINE HAS BEEN CHANGED AND RETURNED TO SERVICE. (M) 2L72 4T4 TRT E282 20030814001542003081400154NM 2003 8 14 AALA20030321 120030318A3350 WIRE HARNESS BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21184AN 29594 SFO - DURING OVERNIGHT MAINTENANCE, EMREGENCY EXIT LIGHTS FROM SEAT 9D-16D INOPERATIVE. ADJUSTED EMERGENCY EXIT LIGHT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030821000972003082100097WP 2003 8 21 03FDEA00819 120030527A5714 SKIN DOUG DC10 DC1010 3022110WP CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 MAIN CARGO-CORROSION FOUND AT STA 1371 LBL 85 AT REAR SPAR TOP OF FUEL TANK. WILL NEED TO HAVE FASTENERS REMOVED. ** S/D ** CLOSING ACTION: ACCOMPLISHED REPAIR - CENTER WING - UPPER SKIN CORROSION - PER EA 8-5710-69306. 2L73 4F A22WE 20030821001732003082100173NM 2003 8 21 03FDEA01035 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 FRAME DENTED BS 580 BETWEEN STR 23L TO STR 5L. CUT OUT DAMAGED AREA ON BS 580 FRAME, 2 AREAS BETWEEN STR 23L AND 25L, 1.4 X 1 AND 3.8 X 1 INCH. FABRICATED REPAIR DOUBLER. ALODINED, PRIMED AND INSTALLED PER FED EX SRM 51-40-3. 2L73 4F RTA3WE 20030821001842003082100184NM 2003 8 21 03FDEA01269 120030719A5330 SKIN BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25103FE 19199 L 2FH NLG 2F SKIN CRACKED AT STA 242 BELOW PANEL CUT OUT. 2L73 4F RTA3WE 20030410001372003041000137NM 2003 4 10 SWAA030691 120030327A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030416001752003041600175NM 2003 4 16 AALA20030228 120030223A25201301696101 PHONE BOEING777 777223 1385213NM CABIN SHORTED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21786AN 30250 LHR - FLT 122 - EN ROUTE JFK-LHR, SEAT 11B HANDSET BECAME STUCK IN HOLDER, ELECTRICAL BURNING HEAT FROM PASSENGER HANDSET BECAME EVIDENT. PASSENGER SEAT POWER WAS TURNED OFF. REPLACED HANDSET 11B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030428000912003042800091NE 2003 4 28 MALA030225 220030403A7261230304015 LABYRINTH SEAL BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 1 ENGINE LEAKING A MALAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL15535XJ E2371 AFTER TAKEOFF AND CHANGE OVER FROM APU AIR TO ENGINE AIR GOT HEAVY SMOKE IN FLT DECK, WHEN NR 1 PACK WAS SELECTED ON. SELECTED NR 1 PACK OFF, SMOKE DISSIPATED. RAN QRH, RETURNED FOR LANDING. ACFT TO BE FERRIED, FOR NR 1 ENGINE REPAIR/REPLACEMENT. MX INSPECTED PACK ASSY, FOUND OK. FOUND NR 1 ENGINE OIL LEVEL 2 QTS LOW. SERVICED OIL, RAN FOR 1/2 GR AT CRUISE POWER. CONSUMPTION AT 1/16 QT PER HOUR. SUSPECT NR 2 LAB SEAL LEAK. ACFT SAFE FOR NR 4 ENGINE FERRY FLIGHT. A/C TO BE FLOWN WITH NR 1 PACK OFF (CURRENTLY REMAINS DEFERRED) NR 1 ENGINE BLEED OFF UNLESS REQUIRED FOR AIRFRAME ANTI-ICE. REPLACED NR 1 ENGINE P/N 2-003-040-15, S/N OFF P07892, S/N ON P07723. REF WORK PKG DATED 4/3/03 FOR DETAILS. 2H74 4F4 FRTA49EU E6NE 20030501000772003050100077WP 2003 5 1 GTIA030220 120030218A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - AFT CARGO DOOR, EXTERNAL, HAS DENT AT MID SECTION. CUT OUT DAMAGED AFT CARGO DOOR. FABRICATE PLUG AND DOUBLER. INSTALLED PLUG AND DOUBLER. (M) 2L72 4F RTA6WE 20030501001222003050100122NM 2003 5 1 ASAA0310028 120030225A53306545774 SKIN PANEL BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN PANEL AT BODY STATION 872, STRINGER 23L-24L GOUGED. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20030501001682003050100168NM 2003 5 1 ASAA0310077 120030304A53306545800 SKIN PANEL BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN PANEL AT BS 340-350, STRINGER 21R-22R DENTED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20030502000072003050200007SO 2003 5 2 SIMA200309014 120030314A532014521725613 SILL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SERVICE DOOR FORWRAD SILL IAW EMB 135 SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030502002102003050200210NM 2003 5 2 AWXA200300393 120030419A3244 TIRE AIRBUSA319 A319132 3930340NM NLG DAMAGED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP28828AW 1552 SNA - ABORTED TAKEOFF - FLT 0250 - EN ROUTE FROM SNA TO PHX - AS AIRCRAFT STARTED TAKEOFF ROLL AT FROM EPR OF 1.05 THE THRUST CAME UPSLIGHTLY STAGGERED, AIRCRAFT STARTED TO DEVIATE FROM CENTER LINE, CAPTAIN TOOK CONTROL AND REJECTED TAKEOFF. NOSE TIRES WERE DAMAGED DUE TO SKID. MAINTENANCE REMOVED AND REPLACED THE LT AND RT NOSE TIRES IAW AWA T/C R4N32303. PERFORMED ACCELERATION CHECK IAW AMM 71-00-00-501 PG 2, ITEM 6. NO DEFECTS NOTED. 2L72 4F RTA28NM 20030505000592003050500059NM 2003 5 5 DHL2003741536 120030325A5510 STRUCTURE BOEING727 727200 138407ENM EMPENNAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, EMPENNAGE INT'R STRUCTURE VERTICAL FIN HAS CRACK AT STR 9L FIN STA 133.8 AT THRU BOLT ATTACH ANGLE TO CHORD ANGLE. CUT OUT DAMAGED AREA DIM 7.75 INCH AND FABRICATED FILLER AND 2 EACH REPAIR ANGLES FROM BAC1517-1367 PO 3077124 FILLER DIM 7.75 INCH AND 2 EACH ANGLES DIM 20 INCHES LONG AND 2 EACH RADIUS FILLER FROM BAC1512-3398 PO 912246 DIM 20 X 1 INCH ALL IAW B-727 SRM 55-30-4 FIG 1 AND 55-30-2 FIG 2. PART TREATED WITH ALODINE AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED STR REPAIR AT 9L FIN STA 133.8 IAW B-727 SRM 55-30-4 FIG 1 AND 55-30-2 FIG 2. 2L73 4F RTA3WE 20030505001542003050500154NM 2003 5 5 03FDEA00498 120030417A5720 COVER BOEING727 727200 138407ENM LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT WING INBOARD FORE FLAP UPPER SURFACE GOUGED UNDER NR 2 GROUND SPOILER. REMOVED AND REPLACED COVER PLATE IAW BOEING 727-200 SRM 51-30-02. 2L73 4F RTA3WE 20030505000132003050500013WP 2003 5 5 MWEA030174 120030411A26110462 SMOKE DETECTOR DOUG DC9 DC932 3022066WP RT LAVATORY DEFECTIVE A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31501ME 47132 RIGHT LAVATORY SMOKE ALARM WENT OFF DURING PUSHBACK. INSPECTED AFT ACCESSARY AND APU COMPARTMENT FOR EVIDENCE OF LEAKAGE, NONE FOUND. REMOVED AND REPLACED RIGHT SMOKE DETECTOR. 2L72 4F A6WE 20030506000122003050600012WP 2003 5 6 03FDEA00536 120030418A2750D425TB PULLEY DOUG DC10 DC1030 3023501WP RT WING BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 RT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. CLOSING ACTION ON 04/18/03. REPLACED RT INBOARD FLAP FOLLOW-UP CABLE O/B PULLEY BRACKET, PULLEY AND SHAFT IAW M/M 20-20-07-2 AT M/M 20-50-02-2. 2L73 4F A22WE 20030508001162003050800116NM 2003 5 8 HOC2003F00014 120030429A5320 SUPPORT BRACKET BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON DITCHING PANEL SUPPORT BRACKET AT STA1176-1183R. 2L72 4F4 FRTA16WE E2EA 20030514001222003051400122NM 2003 5 14 SWAA031033 120030508A3350100031 LIGHT BOEING737 7373K2 13844BANM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20030604000262003060400026SO 2003 6 4 SIMA200311102 120030416A2913YB203A PUMP EMB 135 EMB135LR 3260305SO HYD SYSTEM INOPERATIVE A SIMAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21704PG 145174 DURING CRUISE FLIGHT, THE CREW REPORTED LOSING THE NR 1 HYDRAULIC SYSTEM, QUANTITY AND SYSTEM. AN EMERGENCY AND AIRCRAFT WAS LANDED SAFELY WITH NO OTHER INCIDENTS REPORTED. GEAR DID GO DOWN AND LOCK SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 4 ENGINE DRIVEN HYDRAULIC PUMP IAW EMB MM. OPERATIONAL AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030604000572003060400057WP 2003 6 4 UPS03840472 120030331A53103750498 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, FWD ACCESSORY COMPARTMENT AT STA 660 & L36 FRAME SPLICE FITTING CRACKED. RECEIVED NEW FITTING PN 3750498 LOCATED AND DRILLED HOLES IAW DC8 S RM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20030604001402003060400140NM 2003 6 4 UPS03440560 120030411A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 1920, BETWEEN STR 13-14R, FRAME I/B CHORD EXTEND CRACK FOUND ON PREVIOUSLY REPAIR. FRAME REPAIRED AS PER SRM 51-40-03 FIG.1. 2L74 4F A20WE 20030602000582003060200058EA 2003 6 2 CA030425008 120030407A6220269A505085 BEARING SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA MAIN ROTOR FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BEARING INNER RACE TURNING ON PULLEY SHAFT. 1G71 3U3 O0 4H12 1E10 20060801001042006080100104WP 2006 8 1 IXXA060555S 120030911A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FORWARD SERVICE DOOR, R-1, CUT-OUT LOWER FORWARD CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D. 2L74 4F RT4A25 20030813000332003081300033SW 2003 8 13 HEEA088559 120030715A2560222320300105 SHOULDER BELT BELL 222 222U 1182140SW COCKPIT MISINSTALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 SHOULDER STRAP IS INSTALLED INTO THE INERTIA UPSIDE DOWN. IN ORDER FOR THIS SHOULDER STRAP TO BE CLIPPED TO THE LAP BELT, IT NEEDS TO BE ROTATED 180 DEGREES. THIS CAUSES THE SHOULDER BELT TO BE TWISTED OVER THE PASSENGER CHEST. TO BE SENT TO VENDOR. 1G72 3U H9SW 20030815000742003081500074 2003 8 15 HEEA088452 420030722A3422102005901 INDICATOR BELL 412 412 1182202SW ATTITUDE PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 ATTITUDE INDICATOR PRECESSES 15 DEGREES. 1G72 4U H4SW 20030819000442003081900044NM 2003 8 19 USAA030104 120030619A5347 CARGO TRACK BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 FOUND CARGO TRACK CORRODED .5 INCH BY 2 INCHES, AFT CARGO STATION 807 2 INCHES S-26R TIE DOWN TRACK. CARGO TRACK REPAIR PER SRM 53-10-53 FIG 202. (M) 2L72 4F RTA16WE 20030818000802003081800080SW 2003 8 18 HEEA088621 120030711A6720PHI41294 BEARING BELL 412 412 1182202SW TAIL ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 WORN BEARINGS. REPLACED LINK ASSY (2 EA) 212-010-711-003 DUE TO WORN BEARINGS; LINK ASSY (2 EA) 212-011-710-001 DUE TO WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030821000612003082100061EU 2003 8 21 03FDEA01202 120030803A7931VT0304S INDICATOR AIRBUS310 A310 EU PWA JT9 JT9D7 52054NE NR 1 ENG LOW OILFALSE INDICATIONA FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25452FE 313 715439 IN CRUISE NR 1 ENGINE LOW OIL PRESS (32) ON ECAM. NO CONFIRMING LOW OIL PRESS LIGHT. ENGINE OPERATED AT IDLE. A/C DIVERTED TO EDDF. NR 1 OIL QUANTITY DROPPED 3 QTS OIL, TEMP WAS 30 DEGREES HIGH. MOMENTARY DC ELEC ADVISORY NR 1 AMPS FLUCTUATING. REMOVED AND REPLACED NR 1 MAIN OIL FILTER AS PER MM 79-21-03-4. NO DECONTAMINATION FOUND. REMOVED AND REPLACED LOW OIL PRESSURE TRANSMITTER AS PER MM 79-33-11-4. PERFORMED HIGH POWER ENGINE RUN PER JRH. ALL PARAMETERS NORMAL. 2L72 4F4 FRTA35EU E20EA 20030402000352003040200035NM 2003 4 2 2003UALA00310 120030321A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 CABIN RT SIDE STA 616 FRAME CRACKED BELOW CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR 2L72 4F4 FRTA16WE E2GL 20030404000362003040400036NM 2003 4 4 DL73K030207 120030302A2410948F4585 CONTROLLER BOEING737 737247 138448DNM COCKPIT INOPERATIVE A DALAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO27378DL 23605 NR 1 CSD HIGH OIL TEMP LIGHT ILLUM CLIMBING THRU 15000 FT. DISCONNECTED CSD PER POM. STARTED APU AT 19000 FT THEN AT FL250 THE APU GEN DROPPED OFF LINE. DIVERTED TO MCO. FOUND CSD OVERSERVICED. SERVICED TO CORRECT LEVEL. CHECKS NORMAL ON ENGINE RUN. FWD TO MCO AND PLACARD DUE TO HISTORY. REPLACED APU GCU. APU GENERATOR OPN NORMAL. 2L72 4F A16WE 20030410001072003041000107NM 2003 4 10 SWAA030679 120030325A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29333SW 23697 FWD CABIN INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT AND BATTERY PER MM. 2L72 4F RTA16WE 20030416001112003041600111NM 2003 4 16 QXEA0300414 120030328A5753 DOUBLER BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - DOUBLER ON TOP SURFACE OF OUTBOARD FLAP HAS ADDITION CHAFE DAMAGE. REPAIRED IAW DHC-8 400 SRM 57-15-370-801 AND SRM 51-21-10-380-801. 2H72 4T RTA13NM 20030417001112003041700111EU 2003 4 17 MALA030142 120030118A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 DURING C-CHECK IN CVG, NR 3 SEAT TRACK SHOWS CORROSION BETWEEN FRAME 18 & 20A. MAINTENANCE REPAIRED DAMAGE IAW EO A53026. A/C RELEASE DATE 1/30/03. 2H74 4F RTA49EU 20030505000522003050500052EU 2003 5 5 MALA030237 120030414A2150A2042C PDU SAAB SF340 340B 7860101EU BUSS TIE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15449XJ 340B449 DURING FLIGHT 3367, BUS TIE LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REPLACED LT PDU P/N A2042C, S/N OFF C1-92296, S/N ON CL-93459, AND RELAY G5PC. OPS CHECK GOOD. 2L72 4T RTA52EU 20030505001802003050500180EA 2003 5 5 03109668 120030419A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27668BR 7544 DURING MAINTENANCE INSPECTION, THE RT AFT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030506001012003050600101NM 2003 5 6 CALA0300215 120030424A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914320 23371 INSPECTION FOUND A PUNCTURE IN FUSELAGE TAIL SECTION SKIN AT STA 1043, BL 0. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2L72 4F RTA16WE 20030506001042003050600104EU 2003 5 6 MALA030244 120030424A3350 LIGHT SAAB SF340 340B 7860101EU CABIN DISLODGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15443XJ 340B443 CREW REPORTED RT EMERGENCY EXIT LIGHT FELL OFF. MAINTENANCE INSTALLED NEW PLACARD. 2L72 4T RTA52EU 20040210001182004021000118WP 2004 2 10 ASAA0380755 120031118A532199365461 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - FOUND DURING 15K CHECK, FLOORBOARD EDGE DAMAGE. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M) 2L72 4F RTA6WE 20040210000152004021000015WP 2004 2 10 UPS03841588 120031115A53403755845U1 FITTING DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, BATHTUB FITTINGS ARE CORRODED BEYOND LIMITS BETWEEN LONG. 35L TO 35R AT STATION 1150. REMOVED AND REPLACED FITTINGS IAW DWG. 3755845 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040213000232004021300023GL 2004 2 13 03FDEA02244 220031224A7250 CASE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL TURBINE SPLIT A FDEAA UNSCHED LANDING BMJSMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION CLCLIMB 1 SO25566FE70437 46989 451350 DURING TO AT 300 FT, NR 3 EGT "X'ED" OUT. EAD SHOWED ENG NR 3 EXCEEDANCE. EGT X WENT AWAY AND SHOWED NORMAL EGT. EGT THEN SPIKED INTO THE RED SHOWING 1027 EGT. THROTTLE WAS RETARDED AND ALL INDICATIONS (N1, EGT, N2, AND FUEL FLOW) WERE NORMAL, NO OTHER INDICATIONS WERE ABNORMAL. RETURNED FOR LANDING. FOUND OPEN FROM PIN A LT SIDE JUNCTION AND PIN A OF RT SIDE JUNCTION, ALSO FOUND CRACKED HARDLINE AT BOTTOM OF ENGINE. FOUND LOWER TURBINE CASE SPLIT LINE STUD BROKEN AT THE SIX O`CLOCK POSITION. HARNESS IS ON THE ENG BUT NOT COMPLETELY INSTALLED. REPLACED BROKEN STUD, AND RESECURED THE AFT THERMOCOUPLE. RAN NR 3 ENGINE TO OPS CHECK NR 3 EGT SYSTEM. CHECKS NORMAL, 2L73 4F4 FRTA22WE E23EA 20040212001482004021200148NM 2004 2 12 EIA2003171 120031217A3350S135610A BATTERY PACK BOEING747 747273C 1384896NM EMERGENCY LIGHTSINOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 UPPER DECK EMERGENCY LIGHTS ABOVE STAIRS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED IAW B747 MM 33-51-00. 2L74 4F A20WE 20040217000032004021700003EA 2004 2 17 ASOA03678 120031227A5320601R31171917 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK, THE CLIPS AT FS 484, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANACE REMOVED AND REPLACED THE CLIPS AT FS 484, LBL 27 AND RBL 27 IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20031210001942003121000194NM 2003 12 10 03FDEA01744 120031015A5320 ATTACH ANGLE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE53392 20935 ATTACH ANGLE ABOVE AFT LAV SERVICE PAN CORRODED. REMOVED AND REPLACED IAW EA 7-5320-55012. 2L73 4F RTA3WE 20031210002082003121000208NM 2003 12 10 UPS03M41395 120031013A3213 AXLE DOUG MD11 MD11F 3023600NM LT MLG GOUGED A IPXAK NONE O OTHER TXTAXI/GRND HDL 1 SO01271UP INSPECTION TYPE:N/A NR 1 AXEL ON LEFT MLG GOUGED ***MRR FILED OPEN*** 2L73 4F RTA22WE 20040308001492004030800149NM 2004 3 8 ASAA0310243 120030327A7110 SKIN BOEING737 737298C 1384490NM NR 2 COWLING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL SKIN AT NACELLE STATION 112.60 GOUGED. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040416000242004041600024WP 2004 4 16 ASAA0380738 120031114A533059364341 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND INNER SKIN CORRODED AT FS 541-548 AND BETWEEN 30 AND 29L AT BODY DRAIN. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20040503002192004050300219WP 2004 5 3 AALA20030842 120030808A7920 OIL FILTER DOUG DC9 DC982 3022082WP RT ENGINE CLOGGED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217519A 49896 FLT 700 - DFW-LGA - AFTER TAKEOFF RIGHT OIL STRAINER CLOGGING LIGHT CAME ON WHILE CLIMBING THROUGH 17,000. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED FILTER AND FILTER CLOG PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040927000972004092700097SW 2004 9 27 2004F00362 120030818A56103600431B WINDSHIELD GULSTM690TP 690A 0141722SW COCKPIT CRACKED A O9IAO OTHER O OTHER CRCRUISE 1 NM09290PF 11290 PILOT WINDSHIELD CRACKED VERTICALLY IN LEFT LOWER CORNER TO UPPER LEFT CORNER DURING FLIGHT, OUTER PANE ONLY. AIRCRAFT WAS DESCENDING ON FINAL FROM 13,000 FEET. AIRCRAFT DID NOT DEPRESSURIZE AND LANDED WITHOUT INCIDENT. (M) 1H72 3T 2A4 20030926001632003092600163NM 2003 9 26 CALA0300508 120030828A21214100945A FAN BOEING777 777224 1385225NM AIR DISTRIBUTIONINOPERATIVE A CALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2778005 27581 THE (SMOKE CREW CABIN REST AREA), MASTER WARNING, AND SMOKE ALARMS CAME ON WHILE CLIMBING FROM FL 360 TO 380 WHILE ENROUTE TO EWR. THE WARNINGS WERE ACCOMPANIED BY AN ELECTRICAL ODOR AND EICAS STATUS MESSAGE (RECIRC FAN) CAME ON APPROXIMATELY 2 MINUTES AFTER THE ODOR WAS NOTICED. THE AIRCRAFT WAS DESCENDED TO FL 340 AND DURING THE DESCENT THE WARNINGS CEASED. THE ELECTRICAL ODOR ALSO DISSIPATED QUICKLY. THE FLIGHT CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE UPPER RECIRCULATION FAN B21153 FAILED. THE FAN WAS REMOVED AND REPLACED IAW MM 21-25-01-000-801. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTT00001SE 20040719001062004071900106NM 2004 7 19 USAA030267 120031113A5315 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU59971 22204 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 3 INCHES, FS 377.7 AND LBL 6.0 FORWARD FLANGE. INSTALLED ANGLES, BLENDED, PRIMED, PAINTED PER SRM 51-70-12, TR 53-15-02. CORROSION LEVEL 1. (M) 2L72 4F RTA2NM 20060731000582006073100058WP 2006 7 31 IXXA060509S 120030122A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 MISREPAIRED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FORWARD ENTRY DOOR CUTOUT LOWER AFT EXISTING REPAIR DOES NOT MEET THE INTENT OF AD 2000-20-08. REMOVED EXISTING DOUBLER. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060801000762006080100076WP 2006 8 1 IXXA060539S 120030909A5340 FITTING DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND A CORRODED FITTING UNDER NUT PLATE AT STATION 240 LONGEREON 33 RIGHT. REMOVED DAMAGED FITTING. MANUFACTURED NEW FITTING, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW TIMCO REPAIR ENGINEERING ORDER REO-G09501. 2L74 4F RT4A25 20030515001362003051500136NM 2003 5 15 AWXA200300480 120030424A531365516982 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND AT RIVET HOLES ON STRINGER 4 RT BS 908-909. MAINTENANCE REMOVED CRACKED STRINGER SPLICE ON STRINGER 4 RT BS 908-909; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3, 10-12, & 38. 2L72 4F RTA16WE 20030609001972003060900197 2003 6 9 HEEA086570 420030522A22157690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS CHATTERING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH3363 760505 AFCS ACTUATOR CHATTERS. 1G72 3U NCH1NE 20030611001052003061100105EU 2003 6 11 HEEA086709 120030521A6420116488P BEARING BOLKMS105 BO105S 5626006EU CONTROL ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037136H S833 CONTROL ROD HAS WORN BEARINGS. REPLACED 2 EACH 11-6488P BEARINGS DUE TO WORN; 2 EACH 11-3948P BEARINGS DUE TO WORN. REPAIRED. 1G72 3U H3EU 20030612000132003061200013EA 2003 6 12 SWIA200312021 120030417A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 ANGLES CRACKED AT FS 280, RBL 9, INBOARD AND OUTBOARD. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20030613001282003061300128 2003 6 13 SWAA031234 420030603A256565C19901 CABLE BOEING737 7372H4 138448CNM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20030617001262003061700126GL 2003 6 17 HEEA087464 220030612A74216899084 IGNITER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 IGNITER PRODUCING DELAYED LIGHT OFFS DUE TO WORN. REPLACED IGNITER. 1G71 3U3 UO H2SW E1GL 20030522001222003052200122 2003 5 22 SWAA031124 420030519A2565D31354 SLIDE BOEING737 7373Q8 1384670NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030527000442003052700044NM 2003 5 27 DL733030330 120030402A555365474011 FITTING BOEING737 737347 1384647NM VERTICAL STAB MISALIGNED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 VERTICAL STABILIZER REAR TERMINAL FITTING LUGS WERE DETERMINED TO HAVE UNDERGONE PREVIOUS REWORK WHICH LEFT THE LUG THICKNESS LESS THAN BLUEPRINT SPECIFICATIONS AT EACH OF THE FOUR LUGS. AREA INSPECTED AND NEW BUSHINGS WERE FABRICATED PER DAL ER/A 384672-14 TO COMPENSATE FOR THE REWORK. 2L72 4F RTA16WE 20030527000552003052700055WP 2003 5 27 DHL2003801057 120030408A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING CTR L/E UPPER SKIN HOLES ELONGATED BETWEEN XS 484.895 AND XS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12, FIG 4. REMOVED SKIN WITH HOLES ELONGATED IAW SRM 57-3-3 PG 12, FIG 4 AND SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6 AL0.063) IAW SRM 57-3-3 PG 12 FIG 4. CLEANED, TREATED AND PRIMED INNER PART IAW SRM 51-1-8B. INSTALLED NEW SKIN IAW SRM 57-3-3 PG 12 FIG 4 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030527000562003052700056WP 2003 5 27 AALA20030421 120030408A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217537A 49991 ORD - DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTS AT ROW 20 INOPERATIVE. REPLACED AFT EMERGENCY EXIT PATH LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030618000262003061800026SW 2003 6 18 HEEA087334 120030611A6510 COUPLING BELL 407 407 1182206SW T/R DRIVE SHAFT CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH4488 A1899 53393 SPLINE COUPLING HAS CORROSION ON SPLINES. REPLACED. 1G71 3U O H2SW 20030618000972003061800097NM 2003 6 18 SWAA031282 120030609A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030529000862003052900086SW 2003 5 29 HEEA086660 120030521A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T344 28101 BATTERY HAS WEAK VOLTAGE. 2G72 4U H10SW 20030623000542003062300054WP 2003 6 23 GTIA030342 120030506A5342 ANGLE DOUG DC9 DC982 3022082WP VERTICAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 RIGHT DORSAL FIN VERTICAL ATTACH ANGLE HAS CRACKING VERTICAL LEG. ALSO, DOUBLER ATTACHMENT IS OUT OF LIMITS. REMOVED RIGHT DORSAL FIN VERTICAL ATTACH ANGLE. REMOVED DOUBLER ATTACHMENT. FABRICATED NEW DOUBLER ATTACHMENT. FABRICATED NEW GUSSET. LOCATED AND DRILLED NEW OUTER DORSAL FIN ATTACH ANGLE. INSTALLED RIGHT DORSAL FIN OUTSIDE ATTACH ANGLE. INSTALLED NEW DOUBLER ATTACHMENT. INSTALLED GUSSET. (M) 2L72 4F A6WE 20030625000062003062500006EA 2003 6 25 03148661 120030528A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27661BR 7520 DURING MAINTENANCE INSPECTION, THE CABIN CEILING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030820001682003082000168NM 2003 8 20 CALA0300379 120030711A3230 SOLENOID BOEING737 737524 1384721NM MLG LEVER INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716642 28903 THE LANDING GEAR HANDLE WOULD NOT RAISE PAST THE OFF POSITION AFTER TAKEOFF FROM EWR. QRH PROCEDURES WERE FOLLOWED AND THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE LANDING GEAR LEVER LOCK CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET. THE GEAR WAS SWUNG SEVERAL TIMES, BUT THE FAILURE COULD NOT BE DUPLICATED. THE LANDING GEAR LEVER LOCK SOLENOID WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE GEAR WAS SWUNG SEVERAL TIMES AGAIN AND ALL OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20030820001932003082000193NM 2003 8 20 03226428 120030814A33502LA00672900 BALLAST DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27428FJ 3193 DURING MAINTENANCE INSPECTION THE AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE AFT EXTERIOR EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030819000402003081900040NM 2003 8 19 AALA20030606 120030520A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21368AA 25195 FLOORBEAM AT STATION 303 HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCH, BEYOND SRM LIMITS. COMPLETELY RMOVED CORROSION. APPLY ALODINE TO BLENDED AREA. APPLY PRIMER. FILL WITH SEALANT. (M) 2L72 4F RTA1NM 20030401000012003040100001EU 2003 4 1 00086 120030326A33109993 CONTROL PANEL AMD FALC20FALCONE 2720305EU COCKPIT FAILED E HAEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05285TW 285 PILOT REPORTED DURING CLIMB AT FL290 ELECTRICAL SMOKE IN COCKPIT REQUESTED RETURN TO DEPARTURE AIRPORT ADS, ISOLATED NR 1 ELECTRICAL SYSTEM AND SMOKE DECREASED, REMAINDER OF FLIGHT UNEVENTFUL. WILL UPDATE THIS REPORT AFTER MAINTENANCE. REMOVED AND REPLACED FAILURE WARNING PANEL. OPS CHECK GOOD. 2L72 4F A7EU 20030401001602003040100160WP 2003 4 1 DHL2003804767 120030212A573057695831N PANEL DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING L/E OUTBD SLOT UPPER DOOOR SHOWS FOUR .250 CRACKS BTWN STA XS484.895 AND XS520.168 CORR: R & R LT WING OUTBD SLOT UPPER DOOR BETWEEN XS484.895 AND XS520.168 IAW MM. 2L74 4F RT4A25 20030403000312003040300031NM 2003 4 3 03FDEA00373 120030401A3110 WARNING LIGHT BOEING727 727200 138407ENM WINDSHEAR ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25207FE 22929 DURING INITIAL CLIMB PASSING 800-1000 FT WE EXPERIENCED A RED WINDSHEAR WARNING AND AURAL WARNING. WE PERF THE EMERGENGY ESCAPE MANUVER AND IMMEDIATELY FIREWALL ALL THRUST LEVERS. WARNING LASTED 5 SECONDS. THRUST LEVERS WERE THEN RETARDED TO MAX POWER. #1 EPR READ 2.15 WITH MAX ON T.O.L.D CARD 1.94. WE DID HAVE DECREASING A/S INITIALLY. DIVERSION FLIGHT TIME WAS 31 MINUTES AT 14000 FEET PERF INLET AND EXHAUST INSPECTION. PERF ANALYTICAL ANALYSIS WORKSHEET ON ALL THREE ENGINES PER JRH FIREWALL AND OR EMERGENCY ESCAPE CHECK ON PAGE 6-38 AND 6-38A PREF BITE TEST OF GPWS PER 32- 52-000-1. NO FAULTS ANNUNCIATED C/W INSPECTION PROCEDURES PER E.A. 78-7100-69076. 2L73 4F RTA3WE 20030820001592003082000159NM 2003 8 20 2003UALA00570 120030715A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29392UA 24667 SKIN STA 500B ABOVE STRINGER 4 RT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030328001032003032800103CE 2003 3 28 DEBA391MT0103 120030124A304010138402522 WINDSHIELD BEECH 300 300BEECH 1152930CE COCKPIT CRACKED E DEBAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03391MT844 FA111 CO-PILOTS WINDSHIELD INNER PANE SHATTERED IN FLIGHT. WINDSHIELD HEAT WAS NOT TURNED ON AT THE TIME. 2L72 4T A24CE 20030401000422003040100042SO 2003 4 1 C2XA03CL080 120030328A33501317 LAMP EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714977 145175 DURING ROUTINE MAINTENANCE THE AISLE EMERGENCY LIGHT AT ROW 12 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT LAMP AT ROW 12.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030408000812003040800081WP 2003 4 8 03FDEA00389 120030405A5410 PYLON DOUG MD10 MD1010F WP GE CF6 CF66D 30020GL NR 1 DAMAGED A FDEAK NONE O OTHER LDLANDING 1 SO25393FE 46627 NR 1 ENGINE PYLON RIGHT SIDE CLOSE OUT ON LOWER WING BROKEN ABOVE PANEL 437ER. CLOSING ACTION ON 04/05/03. ON NR N00313. REMOVED CLOSE-OUT PANEL ROUTED TO FAB IAW SRM 51-31-01. T/R NR T2/322652 AND 1 PANEL ON T2/322695, LOCATED AND DRILLED IAW SRM 51-31-01,51-33-01. INSTALLED PANEL IAW SRM 51-35-01 AND 51-35-02 AND 51-33-01. 2L73 4F4 FRTA22WE E23EA 20030408001272003040800127 2003 4 8 AMTA200300224 420030216A2565D30170529 SLIDE LKHEED1011 1011385115 5265015WP PAX DOOR DEPLOYED A AMTAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL11198AT16055493 193B1111 L1 DOOR SLIDE INADVERTANTLY SEMI-DEPLOYED BY CONTRACT COMPANY. REMOVED AND REPLACED L1 DOOR SLIDE IAW MM 25-61-01A, OPS CHECK NORMAL. (M) 2L73 4F A23WE 20030415000192003041500019GL 2003 4 15 CA030314004 220030303A7250 BEARING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TURBINE ASSY FAILED W A UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 CA (CAN) ON TEST FLIGHT FOLLOWING SCHEDULED MAINTENANCE INSPECTION, ENGINE CHIP LIGHT ILLUMINATED. AIRCRAFT LANDED AND ENGINE WAS SHUTDOWN, N2 DECAYED RAPIDLY AT SHUTDONW. TURBINE WAS FOUND TO HAVE ROTATIONAL BINDING, SUSPECT NR 8 BEARING FAILURE. METAL CONTAMINATION CAUSED SCORING IN ENGINE SCAVENGE OIL PUMP. AFFECTED ENGINE PARTS SENT TO REPAIR FACILITY. 1G71 3U3 U H2SW E4CE 20030415000642003041500064NM 2003 4 15 CA030326006 120030326A3260 DOWNLOCK SENSOR BOMBDRDHC8 DHC8400 NM PWC 150 PW150A EA NLG FAILED W O OTHER N FALSE WARNING CLCLIMB 1 CA (CAN) AFTER GEAR RETRACTION DURING DEPARTURE THE NOSE GEAR UNSAFE ADVISORY LIGHT AND THE GEAR TRANSIT ADVISORY LIGHT REMAINED ILLUMINATED. AFTER NORMAL GEAR EXTENSION THE GREEN NOSE GEAR DOWN AND LOCKED ADVISORY LIGHT FAILED TO ILLUMINATE AND THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AN ALTERNATE GEAR EXTENSION WAS PERFORMED AND RESULTED IN THREE GREEN ADVISORY LIGHTS AT THE ALTERNATE DOWNLOCK VERIFICATION SYSTEM. AS A PREVENTIVE MEASURE THE COMMANDER DECIDED TO PREPARE THE AIRCRAFT FOR AN EMERGENCY LANDING ACCORDING TO OPERATOR'S PROCEDURES. NOSE GEAR DOWNLOCK SENSOR WIRING FOUND 'OPEN'. HARNESS ASSY REPLACED. 2H72 4T4 TRTA13NM E00062EN 20030414001252003041400125WP 2003 4 14 CA030307002 220030307A7230 ENGINE LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP VIBRATION W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 CA 15899 (CAN) PILOT REPORTED AIRFRAME VIBRATION WHEN POWER RETARDED DURING DESCENT (FROM 94 TO 88 PERCENT). ITT FLUCTUATING AS LOW AS 200 DEGREES. ENGINE N1 & N2 FLUCTUATES .5 TO 1.5 PERCENT DURING CRUISE WITH LOW BUZZING.UPON INSPECTION OF INLET, FOUND FOD DAMAGE ON 3 LP COMPRESSOR STATOR BLADE (2 BENT BLADE) REAR ACOUSTICLINER AROUND THE 12 O'CLOCK POSITION AND BLADE RUB STRIPE AROUND THE THE 10 O'CLOCK POSITION. 2L72 4F4 F A10CE E6WE 20030416002132003041600213WP 2003 4 16 AALA20030047 120030107A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21593AA 53256 TUL - FOUND LONGERON 2R IS CRACKED AFT OF STATION 1418 FRAME, CRACK IS APPROX .125 INCH LONG. REMOVED DAMAGED SECTION OF LONGERON, OBTAINED AND INSTALLED EXTRUSION PER AARD 53-30-00-2. (M) 2L72 4F RTA6WE 20030429002112003042900211NM 2003 4 29 VNAA0304002 120030406A3240 BRAKE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07426JS 3038 THE CREW REPORTED THAT THE CAPTAIN'S BRAKES HIT THE STOP WITHOUT ANY BRAKING ACTION TAKING PLACE. MAINTENANCE INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030429002192003042900219 2003 4 29 SWAA030803 420030410A2565 GAUGE BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 FWD SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030430002412003043000241NM 2003 4 30 AWXA200300368 120030326A5311654655138 FRAME BOEING737 7373G7 1384595NM FUSELAEG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK .25 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FRAME AT BS 807, BL 0. MAINTENANCE REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT FRAME AT BS 807, BL 0; FABRICATED A SHEAR TIE; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07, PG 219-221, FIG 207. 2L72 4F RTA16WE 20030501000052003050100005WP 2003 5 1 AALA20030233 120030130A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 TUL - FOUND CRACK IN FRAME AT STATION 1136 LONGERON 6R. INSTALLED DOUBLER ON FRAME STATION 1136 L6R PER AARD 53-10-00-30. (M) 2L72 4F A6WE 20030505002362003050500236 2003 5 5 AWXA200300386 420030416A256580330034 RESERVOIR BOEING757 7572S7 1384962NM ESCAPE SLIDE DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28906AW 23568 PHX - EES - FLT 0046 - L-2 DOOR EMERGENCY SLIDE PULLED FROM BONNET WITH GIRT STILL ATTACHED, ASSIST BOTTLE DISCHARGED AND SLIDE HANDLE FOUND ENGAGED. MAINTENANCE REINSTALLED L-2 DOOR SLIDE IAW BMM 25-66-01-404. REMOVED AND REPLACED DOOR ASSIST BOTTLE IAW BMM 52-11-30-4, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20030507001262003050700126WP 2003 5 7 AUS20030393 120030403A6410C0291 BLADE ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA TAIL ROTOR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL ROTOR BLADE LEADING EDGE CONTAINED SMALL HOLES. 1G71 3O3 O H11NM E295 20030514000342003051400034NM 2003 5 14 PCAA0304068 120030424A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DAMAGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13979HA 373 DURING ROUTINE MAINTENANCE VISIT FLOOR STRIP EMERGENCY LIGHT SYSTEMS LAST SEGMENT UNDER ROW 9 WOULD NOT ILLUMINATE. WIRE WAS REPAIRED REFERENCING ADVISORY CIRCULAR 43-13. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030530000812003053000081SO 2003 5 30 2003F00351 120030121A36101159SCC5661 LINE GULSTMGV GULFSTREAMGV3980116SO PNEUMATIC SYS CRACKED A UG8AO OTHER O OTHER ININSP/MAINT 1 GL23920DC 534 WHILE PERFORMING THE ELEVATOR HARD OVER PROTECTION TEST, FOUND THE ELEVATOR DISCONNECT HANDLE GUIDE FOR THE PNEUMATIC ASSIST TO BE CRACKED. THE ELEVATOR DISCONNECT HANDLE ASSY WAS REPLACED, APPROPRIATE OPERATIONAL CHECKS PERFORMED PER THE G-V MM AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA12EA 20030602000642003060200064NE 2003 6 2 CA030424003 220030416A72500292253350 TURBINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE 2ND STAGE DAMAGED W O OTHER O OTHER NRNOT REPORTED 1 CA 9290 (CAN) THE ENGINEERS WERE CARRYING OUT THE ALERT SERVICE BULLETIN A292-72-0263.SUBJECT: CHECK OF RELATIVE POSITION OF 2ND STAGE TURBINE BLADES.THIS CHECK OF THE POSITION OF 2ND STAGE TURBINE BLADES CAN BE CARRIED OUT BY TWO METHODS WITHOUT DISASSEMBLY AND WITH DISASSEMBLY.WE WERE USING METHOD 1 AND THE RELATIVE POSITION OF THE 2ND STAGE BLADES WERE OUT OF THE ALLOWABLE LIMITS. THE GAS GENERATOR WAS REMOVED AND SENT TO AN APPROVED REPAIR STATION. 1G71 3U3 U H9EU E19EU 20030604000312003060400031NM 2003 6 4 USAASB03057 120030430A33503114981 REFLECTOR BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19391US 23313 ATL - FOUND THE LEFT AFT FUSELAGE EMERGENCY EXIT LIGHT WITH A DEFECTIVE REFLECTOR. MAINTENANCE REPLACED THE REFLECTOR. (M) 2L72 4F RTA16WE 20030604002152003060400215 2003 6 4 BAQA086292 420030430A3444 SWITCH LEAR 35 35A 5170602CE RADAR INDICATOR INOPERATIVE W BAQAO OTHER O OTHER NRNOT REPORTED 1 FS0130DK 505 2296 345 STAB ON/OFF SWITCH INOPERATIVE. SPEX FILE NR 00118196. REPLACED WITH SERVICEABLE UNIT. 2L72 4F A10CE 20030610000652003061000065NM 2003 6 10 DL73S030404 120030429A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST BELOW STRINGER 18R AT FS 750. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737-200 SRM AND PER ER/A 384987-14. 2L72 4F A16WE 20030612000842003061200084WP 2003 6 12 UPS03840707 120030520A53405750540502N FITTING DOUG DC8 DC871F 302199DWP LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING IS CRACKED BETWEEN STA 660-680 LONG 11L. REMOVED AND REPLACED FITTING IAW DWG 5750540 AND SRM 51-1-20D. 2L74 4F RT4A25 20030611000372003061100037 2003 6 11 MEX2003168 420030509A3420 WARNING LIGHT DOUG DC9 DC987 3022087WP AHRS ILLUMINATED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23755RA 49727 AIRCRAFT CARRIED OUT AN UNSCHEDULED LANDING DUE TO FLIGHT DIRECTOR FAILURE DUE TO AHRS FAILURE MESSAGE ON EFIS DISPLAY. AHRS NR 2 BRAKERS WERE RESETED AND CONNECTORS WERE CLEANED IAW MM 34-20-00. BOTH FLIGHT GUIDANCE WERE TESTED IAW MM 22-01-05, ALL CORRECT. 2L72 4F RTA6WE 20030617001612003061700161CE 2003 6 17 2003F00373 120030425A2621 CONNECTOR BEECH 1900 1900D 1154162CE FIRE BOTTLE DIRTY A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1981556 UE239 FLT 9249 - MCO/MIA - DURING FLIGHT, LEFT AMBER FIRE DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. CONTINUED TO MIA AND LANDED WITHOUT INCIDENT. CLEANED CONNECTOR ON LEFT FIRE BOTTLE. OPERATIONAL CHECK GOOD. (M) 2L72 4T RTA24CE 20030506002262003050600226WP 2003 5 6 ASAA0380199 120030304A5320993653415 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, RIGHT FORWARD FLOOR PANEL SUPPORT CORRODED AT FS 200. REPLACED SUPPORT PER SRM 53-01. (M) 2L72 4F A6WE 20030505002152003050500215NM 2003 5 5 03FDEA00515 120030418A5240 LINER BOEING727 727200 138407ENM SERVICE DOOR DETERIORATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 RIGHT AFT SERVICE DOOR LINER DETERIORATED. 2L73 4F RTA3WE 20030509001702003050900170NM 2003 5 9 USAA030039 120030411A5311 FRAME BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU35259 27124 CLT - FOUND FRAME CRACKED 2 INCHES, LEFT PACK BAY, FRAME AT BS 900 LBL 0. INSTALLED FABRICATED REPAIR SPLICE DOUBLER PER EA 87134. (M) 2L72 4F RTA2NM 20030513000332003051300033NM 2003 5 13 03FDEA00712 120030430A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING, FOUND OUTBD FLAP, INBOARD MOST HINGE LOCATION FLAP SIDE MOUNT HOLES QTY. 5 EACH LOCATION WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69251 WINGS- OUTBOARD FLAP HINGE FIIRINGS OVERSIZE HOLES- REPAIR. 2L73 4F RTA22WE 20030508000732003050800073NM 2003 5 8 DL757030362 120030414A5330143N33206 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27699DL 29970 DENT CUTOUT REPAIRED THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS BETWEEN FS 600 & 630 AND BETWEEN STRINGERS 15L & 17L. THE DENTS WERE REMOVED WITH 2 SEPARATE CUTOUTS AND REPAIRED WITH A SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 384840-14, REV B. 2L72 4F RTA2NM 20030528000252003052800025EU 2003 5 28 HEEA086737 120030522A6240614764031 INDICATOR AEROSPAS355 AS355* EU NR FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 NTL NEEDLE FLUCTUATES IN FLIGHT WITHOUT CORRESPONDING N1 FLUCTUATION. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H11EU 20030602000442003060200044EA 2003 6 2 CA030514002 120030508A2710272955 LINK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON PCU WORN W B EMER. DESCENT F FLT CONT AFFECTED CLCLIMB 1 CA 13124 (CAN) AFTER T/O AT APPROX 4,000 FT CREW COMPLAINED ABOUT AN AIRFRAME HARMONIC VIBRATION. NO EICAS MSGS WERE POSTED & ENGINE VIBRATIONS AND PARAMETERS WERE NORMAL .AT 16,000 FT A/P DISCONNECTED, APPROX 10-20 SECONDS LATER A/C ROLLED TO THE RT, F/O BROUGHT THE A/C BACK TO NEUTRAL, WITH CONSIDERABLE FORCE.APPROX 10-20 SECONDS LATER A/C ROLLED TO RT AGAIN, F/O BROUGHT BACK TO NEUTRAL. THIS CYCLING CONTINUED APPROX EVERY 10-20 SECONDS. EMERGENCY WAS DECLARED TO LAND IN CHATTANOOGA. THE LANDING WAS UNEVENTFUL.PRIMARY INVESTIGATION REVEALED THAT ONE RIGHT AILERON PCU OUTPUT LINKS WAS WORN BEYOND LIMITS.THE INVESTIGATION IS CONTINUING.CVR AND DFDR DOWNLOAD HAVE BEEN REQUESTED. 2L72 4F4 FRTA21EA E15NE 20030604000612003060400061WP 2003 6 4 UPS03840476 120030402A53115597646 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C3 BS 55 L21L CUSP FRAME CRACKED APPROX 6 INCHES LONG. REMOVED FWD CORNER PAN AND FWD LOWER WEB FOR ACCESS FABBED NEW FRAME IAW DAC DWG 5597646. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTAL LED IAW DAC DWG 5597646, 51-1-21 AND 51-1-20D. REINSTALLED FWD LOWER WEB AND FWD LOWER CORNER PAN. 2L74 4F RT4A25 20030604002102003060400210WP 2003 6 4 UPS03840629 120030416A53405750540502N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, STA. 660 - 680 LONG. 11 LT SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 5750540,AND SRM. 51-1-20D 2L74 4F RT4A25 20030610000512003061000051WP 2003 6 10 ABXA030163 120030414A575399575802N SKIN DOUG DC9 DC931 3022065WP LT WING TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 BULGE IN FLAP SKIN AND CUPPED HEAD FASTENERS UPPER SURF AT INBOARD EXPANSION JOINT. REPLACED SKIN AND REINSTALLED INBOARD FLAP SECTION IAW DC-9 SRM. 2L72 4F A6WE 20030521000662003052100066WP 2003 5 21 DHL2003804898 120030211A5720 ANGLE DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING- CTR L/E TO STUB WING JOINT ANGLE CRACKED 0.500. REMOVED CRACKED JOINT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED JOINT ANGLE (7075-0-0.080) IAW SRM 57-2-0 PG 2. PERFORMED HEAT TREATMENT IAW SRM 51-1-4 PG 1-3, DPS 1-05.3, SRM 51-1-1 PG 1, 17. CLEANED, TREATED AND PRIMED ANGLE IAW SRM 51-1-8B. INSTALLED JOINT ANGLE IAW SRM 51-121 PG 1. 2L74 4F RT4A25 20030522001082003052200108NM 2003 5 22 CALA0300259 120030520A3230 CONTROL VALVE BOEING737 7373T0 1384582NM WHEEL WELL OUT OF ADJUST A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW2777303 23354 THE CREW RECEIVED 3 RED LIGHTS AND THREE GREEN LIGHTS WHEN GEAR WAS LOWERED ON APPROACH TO EWR. THE APPROACH WAS ABORTED AND THE CHECKLIST WAS ACCOMPLISHED. WHEN THE GEAR WAS LOWERED AGAIN NORMAL INDICATION WAS RECEIVED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE NOSE LANDING GEAR CONTROL VALVE OUT OF ADJUSTMENT. THE LANDING GEAR CONTROL VALVE WAS ADJUSTED IAW MM 32-31-00, PAGES 501-504. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20030617000352003061700035CE 2003 6 17 AUS20030487 120030502A712022510001 MOUNT CESSNA182 182Q 2072732CE CONT O470 O470* 17026SO MCAULY2A34C C2A34C204 GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT REAR ENGINE MOUNT FOOT CRACKED AT CORNER OF FOOT SUPPORT.CRACK LENGTH APPROXIMATELY 44.45MM (1.75IN). CRACK ALSO FOUND ALONGSIDE WELD OF FOOT. CRACK LENGTH APPROXIMATELY 50.8MM (2IN).FOUND DURING INSPECTION IAW AD/182/4A1. 1H71 3O3 ONT3A13 E273 5 CP3EA 20030527000022003052700002NM 2003 5 27 SWAA031096 120030514A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED FROM BS 390 TO BS 500C + 17, RT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20030528000402003052800040 2003 5 28 HEEA086594 420030521A3452071119208 CONTROL UNIT BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 DISPLAY IS INTERMITTENT. SCRAPPED UNIT. 1G72 4U H4SW 20030521001452003052100145NM 2003 5 21 DHL2003747502 120030513A5311 FRAME BOEING727 727224 1384076NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR AT BS 640 HAS GOUGE AREA BETWEEN STR 16R/17R. BLENDED DAMAGE AREA FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-40-3 FIG 1. MATERIAL LOSS 7075 T-6 .063 P/O 9912495 DIM 6 X 7 INCH. TREATED AND PRIMED AREA AND PART IAW SRM B-727 51-10-2 AND INSTALLED IAW B-727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20030618000742003061800074NE 2003 6 18 HEEA087131 120030610A632140004769R CALIPER SKRSKYS76 S76A 8143006NE ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 WORN PUCKS - SLOW TO RELEASE. SHOP REPAIR. 1G72 3U H1NE 20030618001612003061800161SW 2003 6 18 HEEA087508 120030612A6510407040303119 SHAFT BELL 407 407 1182206SW BLOWER ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 BLOWER SHAFT HAS A ROUGH BEARING. REPLACED. 1G71 3U O H2SW 20030527001262003052700126WP 2003 5 27 GTIA030332 120030503A5754 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE LT WING LE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23800NK 49144 LEFT WING LEADING EDGE PANEL, 1118C CORROSION AT FASTENER HOLES. FABRICATED DOUBLER. INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20030523000422003052300042NM 2003 5 23 DL76G030398 120030429A21216066223 FAN BOEING767 7673P6 1385105NM CABIN SMOKE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27155DL 25269 CREW REPORTS RT RECIRC FAN EICAS MSG WITH SMOKE ODOR. QRH PROCEDURES COMPLIED WITH ODOR DISSIPATED. REPLACED RT RECIRCULATION FAN. 2L72 4F RTA1NM 20030619000662003061900066 2003 6 19 HEEA087211 420030609A3442PHI0506001803 ANTENNA BELL 206 206B3 1181506SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 WEATHER RADAR ANTENNA WILL NOT RECEIVE. SCRAPPED. 1G71 3U H2SW 20030620000102003062000010SW 2003 6 20 HEEA086937 120030603A79218537651 OIL COOLER BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW036559Z 36019 OIL COOLER LEAKING. SENT TO MFG. FOR WARRANTY REPAIR. 1G72 4U4 U H4SW E22EA 20030619000992003061900099SW 2003 6 19 HEEA087423 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030620000592003062000059EA 2003 6 20 ASOA03231 120030524A3397M22759 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING HANGAR MAINTENANCE IN MCN, THE CENTER SECTION EMERGENCY FLOOR TRACK WIRES WREE FOUND TO BE BROKEN. MAINTENANCE REPAIRED THE CENTER SECTION EMERGENCY FLOOR TRACK WIRING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030624000092003062400009WP 2003 6 24 GTIA030376 120030511A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND CABIN RIGHT INBOARD SEAT TRACK CORRODED FS 692-886. REMOVED TRACK. DRILLED AND LOCATED NEW TRACK AND SPLICES. INSTALLED NEW TRACK. (M) 2L72 4F A6WE 20030623000012003062300001NM 2003 6 23 USAA030065 120030516A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19584US 23743 FOUND SKIN CRACKED .375 INCH LONG, AFT RIGHT SERVICE DOOR UPPER HINGE CUTOUT STATION 951. INSTALLED DOUBLER PER SRM 53-60-01. (M) 2L72 4F RTA16WE 20030625000382003062500038NM 2003 6 25 AWXA200300592 120030504A5315146N54568 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1470, RBL 13. MAINTENANCE FOUND CORROSION TO BE ON EXISTING REPAIR ANGLE; REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT LIMITS; REMOVED CORRODED REPAIR ANGLE AT BS 1470, RBL 13; FABRICATED A NEW REPLACEMENT REPAIR ANGLE; INSTALLED REPAIR PART IAW 51-40-02, PG. 11-12. 2L72 4F RTA2NM 20030702000242003070200024NM 2003 7 2 USAA030091 120030603A5320 WEB BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU58984 22199 PIT - FOUND WEB CRACKED 1 INCH, BS 620 AT DOOR STOP NR 6. DAMAGE CUT OUT, INSTALLED NEW WEB SECTION AND REPAIR DOUBLERS PER SRM 53-00-07 FIG 202 AND EA 87277. (M) 2L72 4F RTA2NM 20030709001292003070900129EA 2003 7 9 03166658 120030615A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030708000702003070800070NM 2003 7 8 AWXA200300641 120030603A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 14 LT INOPERATIVE A AWXAK NONE O OTHER NRNOT REPORTED 1 WP28157AW 23779 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 14 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030716000852003071600085 2003 7 16 USAASA03059 420030602A2565 SLIDE AIRBUS320 A320214 3930316EU PAX DOOR DESTROYED A USAAK NONE O OTHER ININSP/MAINT 1 EA19122US 1298 THE RT FORWARD SLIDE FELL APART WHEN COVER WAS REMOVED. MAINTENANCE REPLACED THE ESCAPE SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030115002172003011500217EA 2003 1 15 COMA0360029 120030114A490038004883 APU CNDAIRCL600 CL6002B19 1900309EA AFT UNWANTED A COMAO OTHER O OTHER LDLANDING 1 SO01941CA12702 7050 FLIGHT 5807 STRONG FUEL SMELL WHEN APU STARTED.REPLACED APU. 2L72 4F RTA21EA 20030127002522003012700252SW 2003 1 27 HEEA083729 120030115A3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 EMERGENCY FLOAT PRESSURE GAUGE GIVING INACCURATE INDICATIONS. 1G71 3U O H2SW 20030204001132003020400113NM 2003 2 4 SWAA030093 120030116A53306545766 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACK BS 430 STR 10R. REPAIRED SKIN PER SWA RA AND SRM. 2L72 4F A16WE 20030204002622003020400262NM 2003 2 4 2003UALA00116 120030123A5751 AILERON BOEING777 777222 1385219NM PWA PW4077PW4077 NE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29773UA 26929 IN DIRECT FLIGHT CONTROL YAW, AIRCRAFT ROLLED LEFT AND REQUIRED 2 UNITS RH YOKE TO LEVEL WINGS. WITH WINGS LEVEL USING RUDDER, LH OB AILERON TE IS UP. INSPECTION OF THE LEFT AILERON FOUND THE INBOARD ATTACH FITTING AT FRONT SPAR CRACKED ON THE INBOARD AND OUTBOARD SIDE. CORRECTIVE ACTION: LEFT INBOARD AILERON WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20030218000842003021800084NM 2003 2 18 AMTA200300140 120030125A3397 WIRE BOEING757 75723N 1384973NM CABIN LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11525AT 30548 EGRESS LIGHTS INOPERATIVE AT ROW 22 THROUGH 26. RESECURED LOOSE WIRING AT ROW 26, OPS CHECK GOOD. 2L72 4F RTA2NM 20030219000172003021900017EA 2003 2 19 COMA0360104 120030215A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01796CA 7338 FLIGHT 9801 GEAR DISAGREE WARNING AFTER T/O.SERVICED THE NLG SHOCK STRUT AND ADJUSTED THE NLG CENTERED PROXIMITY SWITCH. 2L72 4F RTA21EA 20030116000222003011600022NE 2003 1 16 HEEA082979 120030107A28207630702904101 CHECK VALVE SKRSKYS76 S76A 8143006NE FUEL DIST DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 NR 1 ENGINE WOULD NOT START ON FIRST START. DAMAGED FUEL DISTRIBUTION CHECK VALVE 1G72 3U H1NE 20030116001142003011600114 2003 1 16 HEEA083064 420030107A2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 VHF TRANSMITS WEAK. REPLACED R181 RESISTOR AND ADJUSTED TRANSMIT FREQUENCY. REPAIRED. ALSO REPLACED WEAK DISPLAY. ADJUSTED C/N SQUELCH, MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20030117000772003011700077SW 2003 1 17 HEEA083185 120030108A3212206050248109 FLOAT BELL 206 206B3 1181506SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 LT AFT FLOAT BAG LEAKING. 1G71 3U H2SW 20030117001622003011700162SW 2003 1 17 HEEA083216 120030108A2841206063653103 INDICATOR BELL 206 206L3 1182108SW FUEL QYT GLASS CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F FUEL QTY INDICATOR GLASS CRAZED. REPAIRED. 1G71 3U H2SW 20030224000202003022400020NE 2003 2 24 BAQA084069 220030131A7323430121204 GOVERNOR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101650B1 41560NE ENGINE MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS015405G2121 7179 ENGINE GOVERNOR PRODUCING SPLIT TORQUE. ENGINE LE 48177. 1G72 3U3 U H13EU E5NE 20030224000972003022400097SW 2003 2 24 HEEA084218 120030120A5320407070620137 PANEL BELL 407 407 1182206SW PAX DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 CREW/PAX DOOR INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030227001172003022700117SW 2003 2 27 HEEA084423 120030212A6510222044003101 HANGER ASSY BELL 222 222U 1182140SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 RUST ON ADAPTERS. REPLACED BEARING DUE TO SEAL DAMAGED. REPLACED HANGER DUE TO CORROSION. REPLACED SHAFT DUE TO CORROSION. REPAIRED. 1G72 3U H9SW 20030227001372003022700137NM 2003 2 27 AWXA200300210 120030226A3350ABS0374A24 CABLE AIRBUSA319 A319132 3930340NM SEAT ROW 12 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW0 0 924 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BROKEN CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H IAW ESPM 20-25-21; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030228000302003022800030SW 2003 2 28 HEEA084445 120030213A6220 BEARING BELL 206 206L3 1182108SW M/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 7102 AFS7397 51527 MAIN ROTOR HEAD FEATHERING BEARINGS WORN. REPAIRED. 1G71 3U H2SW 20030305000082003030500008 2003 3 5 HEEA084613 420030214A2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 VHF TRANSCEIVER BREAKS SQUELCH, POSSIBLE WATER DAMAGE. FOUND NO SIGNS OF WATER DAMAGE. FOUND RECEIVER AND TRANSMITTER WEAK AT 118 MHZ. ALIGNED RECEIVER. REPAIRED. REPLACED C531 CAPACITOR AND Q504 TRANSISTOR. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000562003030600056SW 2003 3 6 HEEA084771 120030221A3246412050016101 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 MLG SKID SHOE IS WORN. REPAIRED. 1G72 4U H4SW 20030306001022003030600102SW 2003 3 6 HEEA084809 120030221A2510412070819101 SEATBACK CUSHION BELL 412 412 1182202SW CREW SEAT TORN E O OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 CREW SEAT BACK CUSHION TORN. REPAIRED. 1G72 4U H4SW 20030307000312003030700031NM 2003 3 7 SWAA030479 120030303A53206547978 BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED, BS 867 TO BS 887, WL 208, LBL 65. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20030307002062003030700206EU 2003 3 7 RAIA00302044 120030210A561014156002410 WINDSHIELD JETAIRJETSTMJETSTM4101 1500501EU CRACKED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03559HK 41075 5594-STL- RIGHT INBOARD WINDSHIELD CRACKED. Maintenance removed and replaced the right inboard windscreen. 2L72 4T RTA41NM 20030312000552003031200055WP 2003 3 12 ABXA030112 120030225A530027779221 LONGERON DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23958AX 47760 LONGERON 17 RIGHT CRACKED AT STA. 389, APPROXIMATELY 1/4" LONG. INSTALLED NEW FABRICATED LONGERON (P/N 2777922-1) AND SPLICE (P/N 7637813-3) IAW DC-9 SRM 53-02. 2L72 4F A6WE 20030317000772003031700077NM 2003 3 17 03FDEA00237 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 33L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030318001082003031800108EA 2003 3 18 COMA0360151 120030313A3350013071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A COMAO OTHER O OTHER ININSP/MAINT 1 SO01451CA 7562 FLIGHT 5267 SERVICE DOOR EMERGENCY LIGHT IS INOP.REPLACED THE LIGHT BULB. 2L72 4F RTA21EA 20030320000352003032000035NM 2003 3 20 USAASB03001 120030102A56105893543110 WINDSHIELD BOEING737 7373B7 1384580NM COCKPIT CRACKED A USAAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19395US15123 23317 CLT - FLT 1641 - EN ROUTE FROM PHL-ATL, AT FL350, THE FIRST OFFICERS WINDSHIELD BEGAN ARCING, DELAMINATING AND CRACKING. CAPTAIN LOWERED CABIN PRESSURIZATION TO PREVENT WINDSHIELD FROM GIBING OUT, THEN THE PASSENGER OXYGEN MASKS DEPLOYED. CREW DECLARED AN EMERGENCY AND DIVERTED TO CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD AND THE WINDOW HEAT CONTROLLER (P/N 83000-05602). REPLACED OXYGEN GENERATORS AND CLEANED/REPACKED OXYGEN MASKS. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20030326000062003032600006SO 2003 3 26 AUS20030093 120030131A57202200E LIFT STRUT MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL WING OUT OF ADJUST W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING LIFT STRUTS (4OFF) PNO 2200E AND PNO 2201E OUT OF ADJUSTMENT RESULTING IN THE MAINPLANES NOT BEING SYMMETRICAL WITH THE FUSELAGE. LIFT STRUTS HAD BEEN FITTED ON 10 MAY 1996 IAW AD/ML-M7/2. 1H71 3O3 ONC3A23 E286 5 CP920 20030324000402003032400040CE 2003 3 24 4519702102003 120030210A7797 WIRE HARNESS LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312 01518WP LT ENGINE ITT FAULTY E J7SAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05432FX304 304 197 P116393 LT ENGINE ITT EXCEEDED LIMITS. REDUCED POWER AND ITT CONTINUED TO CLIMB. INDICATION EXCEEDED 1008 DEGREES. SHUT DOWN LEFT ENGINE AND MADE PRECAUTIONARY LANDING (EMERGENCY DECLARED). DEEC INTEROGATED BY MAINTENANCE AND NO ACTUAL OVERTEMP OCCURED. MAINTENANCE SUSPECTS FAULITY ITT HARNESS 2L72 4F4 FRTT00008WIE6WE 20030324001352003032400135EA 2003 3 24 COMA0370008 120030321A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA LANDING GEAR INOPERATIVE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS DEDESCENT 1 SO01369CA474 10079 FLIGHT 5429 GEAR DISAGREE WARNING, GEAR DID NOT EXTEND.REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20030325000642003032500064EU 2003 3 25 AWXA200300227 120030304A256011352000151 BATTERY AIRBUS320 A320231 3930325EU FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 FLIGHT CREW REPORTED EMERGENCY FLASHLIGHT AT CABIN ATTENDANT FOLD DOWN JUMP SEAT (AFT LAVATORY) RT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT AT CABIN ATTENDANT FOLD DOWN JUMP SEAT, OPERATIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20030418001212003041800121SO 2003 4 18 SWIA200311777 120030212A3297 WIRE HARNESS EMB 120 EMB120ER 3260203SO MLG SHORTED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07292SW 120319 UPON GEAR RETRACTION, GREEN AND RED -A- SYSTEM NOSE WHEEL LIGHTS STAY ILLUMINATED. FOUND A DOWN HARNESS TO BE GROUNDED OUT. REPLACED A DOWN HARNESS. PERFORMED GEAR OPERATIONAL SWINGS AND NOSE GEAR INDICATION OPS CHECK GOOD. 2L72 4T RTA31SO 20030530000392003053000039SW 2003 5 30 HEEA086684 120030522A2841393008047 INDICATOR BELL 412 412 1182202SW FUEL QTY MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 FUEL QUANTITY INDICATOR DROPS TO ZERO. 1G72 4U H4SW 20030630000152003063000015EU 2003 6 30 DHL2003365005 120030528A2611 SENSOR AIRBUS300 A300B4203 3930306EU CARGO SMOKE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01365DH 149 DURING A/C LOADING ON JFK RAMP SMOKE DETECTED AT NR 44L SENSOR IN MAIN CARGO AREA. RESET CIRCUIT BREAKER. OPERATED OK PER M/M 26-11-00. 2L72 4F RTA35EU 20030624001012003062400101NM 2003 6 24 DL73S030479 120030519A5553 ATTACH FITTING BOEING737 737232 1384475NM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 FUSELAGE ATTACH FITTINGS: VERTICAL STABILIZER CLEVIS LUGS - CORROSION. THE NR 11 CLEVIS LUG FWD FACE WAS FOUND GOUGED. THE DAMAGE WAS CLEANED UP USING A SPOTFACE, WITH A MIN REMAINING LUG THICKNESS OF 0.940 INCH IAW DAL ER/A 412535-14, INITIAL RELEASE. 2L72 4F RTA16WE 20030707001602003070700160NM 2003 7 7 AWXA200300723 120030608A53206546812186 FLOOR SUPPORT BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT AT BS 996-1004, LBL 11, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED CORRODED FLOOR SUPPORT BS 996-1004, LBL 11, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11. 2L72 4F RTA16WE 20030701000292003070100029EU 2003 7 1 HEEA087881 120030623A672010531821 CONTROL ROD BOLKMS105 BO105S 5626006EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 TAIL ROTOR CONTROL ROD PITCH LINK WORN. SHOP REPAIR. 1G72 3U H3EU 20030710000662003071000066WP 2003 7 10 DHL2003802008 120030606A7900 ENGINE DOUG DC8 DC873 302199CWP CFMINTCFM56 CFM562AFR 13802EU NR 3 ENGINE LEAKING A DHLAAEO UNSCHED LANDING ENGINE SHUTDOWN OTHER O OTHER CRCRUISE 1 SO01802DH 46076 LOSS OF OIL QUANTITY NR 3 ENGINE. PERFORMED ABNORMAL PROCEDURE, RESULTED IN IN-FLIGHT ENGINE SHUTDOWN AT 0620Z. OIL PRESS 6 PSI. OIL QUANTITY -0-. OIL TEMP 75 CELSIUS. REMOVED STARTER ON NR 3 ENGINE. FOUND SHAFT SHEARED AND DAMAGE TO TRANSFER GEARBOX (TGB). REMOVED AND REPLACED TRANSFER GEARBOX (TGB) AND ACCESSORY GEARBOX (AGB) AND INSTALLED NEW STARTER ON NR 3 ENGINE IAW W/0 56-2C1-ER-050623V01 AND CFM56-2 M/M. OPS AND LEAK CHECKED GOOD. 2L74 4F4 FRT4A25 E21EU 20030714000362003071400036NM 2003 7 14 SWAA031408 120030624A33506013211 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030716000392003071600039SO 2003 7 16 SIMA200316904 120030617A27503631001007 CONTROL UNIT EMB 135 EMB135KL 3260302SO AVIONIC BAY INOPERATIVE A SIMAB EMER. DESCENT O OTHER DEDESCENT 1 SW21840AE 145656 DURING DESCENT, CREW NOTED FLAP FAIL INDICATION WITH SPS ADVANCE CREW FOLLOWED AOM AND DECLARED AN EMERGENCY. DURING THE DESCENT INTO ORD THE FLAPS WERE STUCK AT ZERO. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030711000882003071100088WP 2003 7 11 MWEA030254 120030624A2720 RUDDER DOUG DC9 DC932 3022066WP EMPENNAGE INOPERATIVE A MWEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL31206ME 47791 RUDDER FULL RIGHT APPLIED WITH NO APPARENT EFFECT. ADJUSTED CABLE RUN AND SENSING SECTOR, PERFORMED ADJUSTMENT TEST. NO DEFECTS NOTED. (AIRCRAFT PARKED SINCE 6-23-03, CURRENTLY ON OPERATION CERTIFICATE, PLANNED RETIREMENT DATE UNDECIDED) 2L72 4F A6WE 20030114000652003011400065NM 2003 1 14 SWAA030015 120030104A57536546435278 FLAP BOEING737 7373Y0 1384671NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030116000702003011600070SW 2003 1 16 HEEA083030 120030106A6520PHI206L3957 PITCH LINK BELL 206 206L3 1182108SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 TAIL ROTOR PITCH LINK SHAFT CRACKED ON OUTBOARD SURFACE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030116001792003011600179SO 2003 1 16 C2XA02SH177 120030116A532014521721009 BUTT STRAP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712519 145366 SHV - DURING C-CHECK DIGITAL BUTT STRAP BETWEEN FRAMES 15 AND 14 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A SPLICE REPAIR IAW EMB 135 SRM 53-21-10 REPAIR NR 4. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030127000152003012700015SW 2003 1 27 HEEA083591 120030114A79218537653 OIL COOLER BELL 412 412 1182202SW ENGINE MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 METAL FOUND AT FWD CHIP PLUG. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030128000352003012800035SW 2003 1 28 HEEA083788 120030115A282123066697 FILTER BELL 407 407 1182206SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 FILTER BYPASS INDICATOR POPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128001622003012800162SW 2003 1 28 HEEA083876 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030421001872003042100187NM 2003 4 21 AMTA200300097 120030116A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 EGRESS LIGHT INOPERATIVE AT ROW 27. RECONNECTED WIRES AS REQUIRED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030421002052003042100205NM 2003 4 21 AMTA200300334 120030310A3350 LIGHT BOEING737 73783N 13844HINM LT OVERWING INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11308TZ 28244 LEFT AFT OVERWING EXIT WINDOW LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-21-00-2. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030722000362003072200036NM 2003 7 22 2003F00464 120030124A5514 BEARING BOEING727 727222 1384073NM HORIZONTAL STAB CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CRACK ON VERTICAL STAB, LEFT HORIZONTAL STAB HINGE BEARING. REMOVED AND REPLACED VERTICAL STAB, LEFT HORIZONTAL STAB HINGE BEARING. (M) 2L73 4F A3WE 20030424000042003042400004SO 2003 4 24 SWIA200311828 120030312A5753 BRACKET EMB 120 EMB120ER 3260203SO RIGHT TE FLAP CRACKED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07565SW 120340 FOUND CRACK IN INBOARD RIGHT FLAP ROLLER BRACKET. INSTALLED NEW BRACKET AND ROLLER ASSEMBLY IAW 54-20-00. ALL CHECKS OK. 2L72 4T RTA31SO 20030731000702003073100070EA 2003 7 31 QXEA200300858 120030717A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT INTERMITTENT A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09613QX 10045 BOI- FIRE SYSTEM FAULT STATUS MESSAGE APPEARS INTERMITTENTLY. COULD NOT DUPLICATE. NO PARTS REPLACED. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030731001162003073100116NM 2003 7 31 QXEA200300795 120030623A5320 MOUNT BRACKET BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - FORWARD LEFT AND RIGHT HAND VHF ANTENNA MOUNT BRACKETS CRACKED APPROXIMATELY X83.00. REPAIRED IAW HORIZON AIR EO 6-53-162A. 2H72 4T RTA13NM 20030825000112003082500011NM 2003 8 25 UPS03240965 120030605A5730 SKIN BOEING727 727185C 138406NNM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C SUSPECT CORROSION ON FIXED L-EDGE SKIN UPPER AFT SURFACE AT 2 LOCATIONS LE STA 345 AND 340 APPROX RT. REPAIR CARRIED OUT IAW SMRO EO 2003-038-007. UPS ENGINEERING FILE NO. 727-57-20106 2L73 4F A3WE 20030827000092003082700009NM 2003 8 27 03FDEA00839 120030523A5744ARC0503504 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0748: RT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP-HINGE FWD FITTING FOUND OUTBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0748: REPAIR CARRIED-OUT IAW CMM 57-44-09 AND EA 1-5740-71708 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030828000922003082800092NM 2003 8 28 DLM88030636 120030712A2424947F9453 GCU DOUG MD88 MD88 3023688NM E/E BAY FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27970DL 43173 AFTER TAKE OFF, HAD LEFT GENERATOR FAIL AND AC CROSSTIE LOCK OUT MSG. AIR RETURN TO PHX T/S LEFT GCU WITH GCU FAULT LIGHT REPLACED LEFT GCU. INSP LT GEN AND CURRENT TRANSFORMERS. ALL CKS GOOD. RAN AC CROSSTIE TEST. FAILED TEST. REPLACED LT GEN POWER RELAY. NOW CKS OK. 2L72 4F RTA6WE 20030828001662003082800166NM 2003 8 28 USAABB03130 120030811A3397 WIRE BOEING767 767201 1385125NM CABIN DAMAGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19646US 23898 PHL - FOUND LOW LEVEL EMERGENCY LIGHTS INOPERATIVE FROM ROW 10 TO THE OVERWING EXIT, LEFT SIDE. MAINTENANCE REPAIRED WIRING AT THE OVERWING EXIT. (M) 2L72 4F RTA1NM 20030724000892003072400089NM 2003 7 24 AWXA200300728 120030610A5320BAC1489273 ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF R-1 DOOR ATTACH ANGLE AT BS 280-314, RBL 55, WL 208.5. MAINTENANCE REMOVED R-1 DOOR SILL SUPPORT ANGLE AND DRIP PAN TO ACCESS CORRODED ANGLE; REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ATTACH ANGLE AT BS 280-314, RBL 55, WL 208.5; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART AND REINSTALLED DOOR SILL SUPPORT ANGLE & DRIP PAN IAW B737-300 SRM 51-40-02 PG 10-11 FIG 12. 2L72 4F RTA16WE 20030724000942003072400094NM 2003 7 24 DL76L030558 120030617A3350 FUSE BOEING767 767332 1382001NM CABIN BLOWN A DALAK NONE O OTHER ININSP/MAINT 1 SO27195DN 28452 SEATS 21 THRU 39 EMER LIGHTS RT SIDE INOP. FOUND FUSE BLOWN BATTERY PACK ASSY M9009. REPLACED FUSE. FOUND WIRING AT SEAT 31FG DAMAGED. REPAIRED WIRING SEATS 21 THRU 39 EMERGENCY LIGHTS, CHECK NORMAL. 2L72 4F RTA1NM 20030805000632003080500063SO 2003 8 5 ASOA03247 120030604A27503075001017 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS INOPERATIVE A ASOAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO11266AS 120188 DURING APPROACH FROM OKC-DFW, THE CREW RECEIVED A FLAP CONTROL FAULT THAT WOULD NOT RESET, WITH THE FLAPS AT ZERO DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND THE FIRE TRUCKS REQUESTED AS A PRECAUTION. THE AIRCRAFT LANDED AT DFW SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030806001202003080600120SO 2003 8 6 C2XA03SH208 120030701A531014522460013 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE CENTER BUTTSTRAP AT FRAME 18 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030806001332003080600133NM 2003 8 6 AWXA200300874 120030714A5310655287846 DOOR FRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C14 CHECK A PITTING CORROSION WAS FOUND UPPER SURFACE OF L-2 DOORWAY INNER STRUCTURE AT BS 987, LBL 53, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED INNER STRUCTURE AT LBL 53 FROM BS 917 TO BS 1016; FABRICATED A NEW REPLACEMENT INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8, PG 3-4, 11 & 38. 2L72 4F RTA16WE 20030807000752003080700075SO 2003 8 7 C2XA03SH237 120030728A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV- DURING C-CHECK, THE LT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030829000752003082900075NE 2003 8 29 NACA20030099 220030729A8500R2800 ENGINE DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 1 MALFUNCTIONED A NACAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 AL03993302131 2131 43576 P31669 NR 1 ENGINE LOSS OF OIL AND NO BMEP INDICATION. REPLACED NR 1 ENGINE ASSEMBLY. 2L74 4R4 R 6A3 5E8 20030903002762003090300276SO 2003 9 3 C2XA02SH294 120030827A532014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030903001852003090300185WP 2003 9 3 AALA20030709 120030702A2150 ACM DOUG DC9 DC982 3022082WP A/C BAY LACK OF LUBE A AALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW21496AA 49734 SAN - FLT 736 - EN ROUTE SAN-DFW, IMMEDIATELY AFTER TAKEOFF CABIN BEGAN TO FILL UP WITH A BLUE HAZE/SMOKE. RAN EMERGENCY PROCEDURES AND RETURNED TO SAN. SMOKE FINALLY BEGAN TO DISSIPATE JUST PRIOR TO LANDING. SERVICED ACMS TO PROPER LEVEL. ACCOMPLISHED PACK BURN PER MM. NO SMOKE IN CABIN DURING PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030807000682003080700068SO 2003 8 7 C2XA03BT075 120030724A2530 COFFEEMAKER EMB 145 EMB145 3260210SO GALLEY SMOKE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712142 145735 CREW REPORTED, FLIGHT ATTENDANT SMELLED ELECTRICAL SMOKE FROM GALLEY LIGHT CIRCUIT BREAKER. MAINTENANCE INSPECTED COFFEE POT(S) SOCKET AND GALLEY LIGHT ASSEMBLY, NO FAULT FOUND. OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030813000172003081300017SW 2003 8 13 HEEA088605 120030806A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 MAIN ROTOR BLADE CRACKED. SHOP REPAIR. 1G72 4U H4SW 20030729000502003072900050NM 2003 7 29 ZW0A0305707 120030702A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13718TW 28486 THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS WERE ADJUSTED ACCOUNT DEFORMED AT THE L1, R1, L2, R2, L4, AND R4 CABIN DOORS. 2L72 4F RTA2NM 20030730000012003073000001NM 2003 7 30 P5CA0300891 120030620A2810 FUEL SYS BOEING747 7472D3B 1384805NM SURGE TANK MALFUNCTIONED A P5CAR AUTOROTATION KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP23505MC 21251 REPORTED FUEL LEAK BY TOWER ON CLIMBOUT WITH SMELL OF FUEL IN UPPER CRG DECK. FOUND LT SURGE TANK WITH FUEL SUMPED SURGED TANK. FOUND VOLUMETRIC SYS INOP. OPENED DMI 28-20-1. MALFUNCTION OF VOLUMETRIC SYS. 2L74 4F RTA20WE 20030910001892003091000189NM 2003 9 10 HALA0300723 120030815A57555926060512 SUPPORT FITTING BOEING717 717200 1383700NM LT SPOILER CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13478HA3357 55123 HNL - LEFT OUTBOARD SPOILER ACTUATOR SUPPORT FITTING CRACKED. REPLACED SPOILER ACTUATOR SUPPORT FITTNG. (M) 2L72 4F TRA6WE 20030910001562003091000156EA 2003 9 10 A6WA200340122 120030819A2920AE7127631 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A A6WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31401AW 7280 HYD 2 LOW PRESS EICAS MESSAGE IN FLIGHT, HYD PAGE INDICATES 0 PERCENT QUANTITY, EDP NR 2 RAN FOR 45 MINUTES WITH ZERO QUANTITY, DIVERTED TO LNK. REPLACED NR 2 EDP AND EDP PSI LINE AT PYLON. CHECK HYD FILTER FOR METAL. NONE NOTED. BLEED SYSTEM. LEAK AND OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030930000092003093000009NM 2003 9 30 AWXA200301028 120030816A575365495091 FAIRING BOEING737 737277 1384570NM LT WING TE FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .7500 INCH CRACK WAS FOUND ON LT WING NR 1 FLAP TRACK MOVEABLE FAIRING AT UPPER LT AFT CORNER. MAINTENANCE PERFORMED A BOND REPAIR ON LT WING NR 1 FLAP TRACK MOVEABLE FAIRING AT UPPER LT AFT CORNER IAW B737-200 SRM 51-40-09, PG. 3, 8-9. 2L72 4F RTA16WE 20031002000812003100200081NM 2003 10 2 F3LA200300130 120030911A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA. 312 AND 328, LBL 12, CORRODED ON TOP. REPLACED INTERCOSTAL IAW SRM 51-10-02. 2L72 4F RTA16WE 20030908003442003090800344NM 2003 9 8 SWAA031928 120030828A55236959227 HINGE BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED C3 CHECK, (SI 11138-55), LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED NR 1 LT ELEVATOR TAB ATTACH HINGE BUSHING/HARDWARE PER MM. 2L72 4F RTA16WE 20030908003082003090800308NM 2003 9 8 SWAA031886 120030821A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 26L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031006000132003100600013EU 2003 10 6 MALA030409 120030811A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK IN CVG, AFT CARGO TOP FRAME AT GUIDE PIN CRACKED. MAINTENANCE REPAIRED IAW SRM 52-32-11 (201). A/C RELEASE DATE 9/2/03. REFER TO 409# 190216 FOR DETAIL. 2H74 4F RTA49EU 20031014001862003101400186NM 2003 10 14 SWAA032111 120030922A53306552988 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 LONG AT BS 933, STRINGER 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031020003132003102000313 2003 10 20 SWIA200312449 420030923A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAK NONE FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07578SW7416 7314 120346 AUTOPILOT DISCONNECTED IN FLIGHT (F/O SIDE) WITH RED E AND AP LIGHTS ON AP PANEL. REMOVED AND REPLACED ELEVATOR SERVO IAW EMB MM 22-10-05. OPS CHECK GOOD. 2L72 4T RTA31SO 20031020002102003102000210WP 2003 10 20 UPS03841361 120030924A5320375543U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 STATION 1204 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R TO 35R. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20031021000532003102100053WP 2003 10 21 GTIA030707 120030912A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FOUND SKIN DELAMINATED FLOOR BOARD MAIN CABIN RT INBOARD STATION 1193. FABRICATED FLOORBOARD. (M) 2L72 4F A6WE 20031021002562003102100256NM 2003 10 21 03FDEA01598 120030920A2913 PUMP DOUG MD11 MD11 3023602NM HYD SYSTEM FAILED A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25601FE 48401 HYDRAULIC 3 FAILURE DURING FLIGHT. REMOVED AND REPLACED UPPER AND LOWER ENG DRIVEN HYD PUMP ASSY AS PER MM 29- 11-20-4, FOR LEAK CHK AND OPS CHK. REMOVED AND REPLACED PER MOCC REQUEST FOR PRECAUTIONARY. 2L73 4F RTA22WE 20031022000132003102200013NM 2003 10 22 MWEA030388 120030922A53209936534 FLOOR SUPPORT DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 CABIN FLOOR SUPPORT IS CORRODED AT STATION 200, 9 INCHES RIGHT OF AIRCRAFT CENTER LINE TO END OF SEAT TRACK NR 5. FABRICATED AND INSTALLED CABIN FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20031027001172003102700117NM 2003 10 27 ASAA02402TT 120030331A53207075T6 WEB BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND AFT CARGO DOOR CUTOUT FORWARD LOWER CLOSE OUT WEB GOUGED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031119001392003111900139WP 2003 11 19 MWEA030419 120031014A531159360351 SKIN DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 AFT GALLEY DOOR JAMB, FORWARD SIDE, INNER LAYER OF SKIN IS EXFOLIATED BETWEEN LONGERON 16 LEFT AND 17 LEFT. FABRICATED AND INSTALLED REPAIR AND FILLER. 2L72 4F A6WE 20040114002142004011400214NM 2004 1 14 MWEA030488 120031215A551359304972 SKIN DOUG MD88 MD88 3023688NM HORIZ STAB TAB DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 RT HORIZONTAL STABILIZER ANTI-FLOAT TAB HAS LIGHT DAMAGE ON BOTTOM SIDE, 20 INCHES FROM OUTBOARD EDGE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20040128000022004012800002 2004 1 28 BAQA091600 420031223A3452066011410101 TRANSPONDER UROCOPEC135 EC135P1 8680990EU ATC` INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH248 0179 TRANSPONDER IS INOPERATIVE. ATC DOES NOT PICK UP AIRCRAFT. REPLACED WITH SERVICABLE UNIT. 01/23/2004 1G72 3U O H88EU 20040129001822004012900182NM 2004 1 29 DHL200374270 120031120A5310 DOOR FRAME BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD, CORNER AREA WITH DENTS. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABED NEW ONE FROM BAC 1503-100274 PO 3344880 DIM 42 INCHES & SPLICE ANGLE DIM 9 INCHES IAE B727 SRM 51-40-1 FIG 1. CUT OUT DAMAGED WEB & FABED NEW FROM 7075-T6 .071 DIM 31 X 4.25 INCH PO 900242 & 2 EA SPLICE DOUBLERS SAME MATL DIM 8.5 X 4.25 INCH IAW B727 SRM 53-10-2 FIG 3, 51-40-2 FIG 1. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2, AND INSTALLED IAW B727 SRM 51-40-2 FIG 1 & 51-40-4 FIG 1. 2L73 4F A3WE 20031103000012003110300001NM 2003 11 3 DL733030852 120030917A3397RPS1 WIRE HARNESS BOEING737 737347 1384647NM AFT OVERHEAD INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27302WA 23182 WHILE REPOSITIONING HARNESS AT SEAT ROW 27 PINS PULLED OUT OF HARNESS AND SHORTED POWER SUPPLY. REPLACED HARNESS AT SEAT ROW 27 AND POWER SUPPLY/BATTERY PER M/M. 2L72 4F RTA16WE 20031031000092003103100009SO 2003 10 31 SWIA200312467 120030927A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM0716731 120190 ON SHORT FINAL FLAP ASYMMETRY LEFT OUTBOARD 25 DEGREES, RIGHT OUTBOARD 15 DEGREES. REMOVED AND REPLACED FLAP CONTROL LEVER AND FLAP CONTROL UNIT. OPS CHECK GOOD ON GROUND. S/N OFF: 120197 2L72 4T4 TRTA31SO E20NE 20031106000812003110600081WP 2003 11 6 UPS03841509 120031025A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 CORROSION ON FUSELAGE LONGERON 35R AT STA 320-300. REMOVED, FABRICATED AND REPLACED LONGERON AT STA 250-320 IAW SRM 51-1-21, 53-2-2 FIG 10 AND 51-1-20D FIG 10. 2L74 4F RT4A25 20031105000512003110500051NM 2003 11 5 SWAA032304 120031020A3350101114 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 LT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LENS COVER PER MM. 2L72 4F RTA16WE 20040108000922004010800092EU 2004 1 8 KBM2003F00042 120031005A2912806966 FILTER ELEMENT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE HYD SYSTEM CLOGGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 HYDRAULIC FILTER ELEMENT PENDING BYPASS BUTTON POPPED. REPLACED HYDRAULIC FILTER WITH NEW.(K) 1G71 3U3 U H9EU E19EU 20031118000642003111800064NM 2003 11 18 HNAA0300053 120031007A533085330027 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07914HA 53 MAJOR REPAIR DENTS ON THE SIDE OF THE FUSELAGE. 2H72 4T RTA13NM 20031212000442003121200044 2003 12 12 SWAA032499 420031112A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031223000792003122300079CE 2003 12 23 DXTA200300179 120031207A2170 COALESCER BAG CESSNA560 560XL 2076702CE CABIN DIRTY E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07681QS 5605181 AFTER TAKEOFF FROM LNK, NOTICE BURNING ODOR IN COCKPIT WITH POWER AT OR ABOVE 70 PERCENT AND APU OFF, ACCOMPLISHED AIR TURNBACK TO LNK. INVESTIGATED AND FOUND WATER SOCK AREA CLEAN AND FREE OF ODOR PER CESSNA 560XL MM CHAPTER 21-50-00, SYSTEM OPS CHECKED OK. RAN AIRCRAFT ON GROUND AT DIFFERENT POWER SETTING AND COULD NOT DUPLICATE STRONG ACID ODOR. 2L72 4F RTA22CE 20031223001902003122300190WP 2003 12 23 GTIA030807 120031001A5320 CHANNEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND FORWARD CABIN PANEL RIGHT OUTBOARD STATION 256-313 CHANNEL CRACKED AT FORWARD AND AFT ENDS AND BENT. REMOVED DAMAGED CHANNEL. FABRICATED NEW CHANNEL. INSTALLED HAT CHANNEL. (M) 2L72 4F A6WE 20031229000982003122900098NM 2003 12 29 AWXA200301542 120031206A534069353521 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER CLIP BS 520, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 520, STR 14 LT; RECEIVED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 45 & 64, FIG 12 & 14. 2L72 4F RTA16WE 20031009000522003100900052NM 2003 10 9 03FDEA01700 120031003A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 FWD CARGO SIDE FRAME DENTED STA 680 RBL 30 WL 157. FWD CARGO SIDE FRAME DENTED STA 680, RBL 30, WL 157 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3. 2L73 4F RTA3WE 20031009001102003100900110SO 2003 10 9 C2XA03BT093 120030913A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712567 145623 CREW REPORTED THE EMERGENCY LIGHTS IN ROW NR 3 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW EMB145 33-50-04. 2L72 4T RTT00011AT 20040105001282004010500128NM 2004 1 5 SWAA032767 120031218A53116546564 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND FRAME CORRODED AT BS 986.5, RBL 46, WL 208. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040106001502004010600150 2004 1 6 UPS03141667 420031215A2565 SLIDE AIRBUS300 A300B4622R 3930312EU PAX DOOR MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0810 INSPECTION TYPE:N/A MAIN CABIN DOOR SLIDE INOPERABLE REF UPS03641656 VOIDED BECAUSE TAIL NUMBER SHLD HAD BEEN N137UP INSTEAD OF N320UP. INSTALLED DUAL ESCAPE SLIDE TO DOOR PER Z831 PER MM 25-61-21-4, CLEARS M272188. 2L72 4F RTA35EU 20031124001372003112400137NM 2003 11 24 AALA20031150 120031009A5347 SEAT TRACK BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21626AA 24584 TUL - FOUND CORROSION IN SEAT TRACK CHANNEL AND AROUND FASTENERS TRACK. REMOVED CORRODED SECTION OF NR 4 SEAT TRACK AND SPLICED IN NEW SECTION PER SRM 53-00-52-2 AND PER ESP 90309. (M) 2L72 4F RTA2NM 20031202000162003120200016WP 2003 12 2 GTIA030729 120030910A5730 SKIN PANEL DOUG DC9 DC982 3022082WP LT WING CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND CORROSION AND TOOL MARKS ON LE PANEL NR 1117C LEFT WING. TWO BLENDED AREAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20031203000532003120300053NM 2003 12 3 GAIA03157ST 120031024A5315 FLOORBEAM BOEING727 727243 138408DNM COCKPIT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURNG C-CHECK INSPECTION FOUND COCKPIT FLOORBEAM ANGLES CRACKED AT BS 258, ONE AT LBL 4, ONE AT LBL 8. REF FASI N/R NR 61888, REPLACED BOTH CRACKED ANGLES PER B727 SRM 53-10 2 FIG 1. (M) 2L73 4F RTA3WE 20040121000452004012100045NM 2004 1 21 USAASB03213 120031212A56105893543129 WINDSHIELD BOEING737 7373B7 1384580NM COCKPIT ARCED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19387US 22959 ON CLIMB-OUT FROM CLT, AT FL170, CREW NOTED A STRONG ACRID ODOR IN THE COCKPIT. NO ODOR WAS NOTED COMING FROM THE GASPER VENTS OR AIR CONDITIONING DUCTS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMEREGNCY WAS DECLARED. MAINTENANCE REMOVED AND ERPLACED THE CAPTAINS L1 WINDSHIELD PER JOB CARD DUE TO LOWER LT STUD ARCING. ALSO, R & R THE L1 WINDSHIELD HEAT CONTROL UNIT, P/N 231-2 PER MM 30-41-11. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040121000562004012100056NM 2004 1 21 BJNA031101 120031109A33506013211 BATTERY PACK BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A SCHEDULED MAINTENANCE CHECK THE EMERGENCY EXIT LIGHTS AT DOOR R-2, AND L2 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE R-2, AND L2 EMERGENCY BATTERY PACK IAW BOEING MM 33-51-01, LIGHTS NOW ILLUMINATE. (M) 2L72 4F RTA16WE 20040122001242004012200124EA 2004 1 22 ASOA03653 120031216A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11881AS 7496 FLT 4721 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP BRACKET WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040121000492004012100049EA 2004 1 21 ASOA03588 120031119A33501317 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11718EV 10095 DURING A GROUND INSPECTION IN DFW, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT AFT OVERWING EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031205000632003120500063EA 2003 12 5 SWIA200312522 120031015A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07587SW 7062 FLAPS HALFSPEED MESSAGE. REMOVED AND REPLACED THE PDU IAW MM 27-52-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20031209001402003120900140NM 2003 12 9 QXEA200301337 120031012A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 NR 8 SEAT TRACK HAS A NR 6 RIVET HOLE BLOWN OUT ON BOTTOM FORWARD END IN SPLICE AREA THIRD HOLE AFT. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-55-4722. 2H72 4T RTA13NM 20031210000422003121000042 2003 12 10 COMA0360509 420031118A2211 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01523CA 7821 FLIGHT 5184 IAPS DEGRADED RESET THE IAPS. 2L72 4F RTA21EA 20030916000762003091600076WP 2003 9 16 GTIA030644 120030810A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PEELING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FOUND CABIN FLOORBOARD CENTER STATION 468-541 HAS EDGE DAMAGE AND FLOORBOARD FACESIDE PEELING. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030923000482003092300048WP 2003 9 23 DHL2003604760 120030527A5310 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT ACCESSORY COMPT. CLIP ATTACHING FRAME TO SKIN AT STA. 660.000 L-22L WITH 1.500 CRACK IN IT. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG.21. FABRICATED NEW CLIP (STEEL 0.500 H0.050) IAW SRM 53-1-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-20D PG.9, SRM 51-1-14A. 2L74 4F RT4A25 20030923001072003092300107WP 2003 9 23 DHL2003604733 120030528A53403754918U1 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT. FITTING CRACKED 2.000 AT STA.1187.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, SRM 51-1-20D PG.9,21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG.9. 2L74 4F RT4A25 20040128001402004012800140NM 2004 1 28 AWXA200301644 120031230A3350BR964411 LIGHT BOEING757 7572S7 1384962NM SEAT ROW 14 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28906AW 23568 PHX - EEL - DURING A-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLE AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040129000292004012900029EU 2004 1 29 MALA030581 120031228A2540 LAVATORY SAAB SF340 340B 7860101EU CABIN CONTAMINATED A MALAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15421XJ 340B421 FLIGHT DECK AND CABIN HAD STRONG ODOR OF ALCOHOL. COMPLAINTS FROM PAX. POST INSPECTION MAINTENANCE FOUND NO BLUE FLUID IN LAV TANK, JUST 2 GALLONS OF CLEAR ALCOHOL. MAINTENANCE DRAINED AND FLUSHED. RAN A/C WITH BLEEDS SELECTED UNTIL ODOR DISSIPATED FROM A/C BELIEVED TO BE CLEANING SOLUTION. 2L72 4T RTA52EU 20040203000572004020300057NM 2004 2 3 ASAA0310163 120030320A53116546558503 FRAME BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 DURING C-CHECK, FOUND FRAME AT BS 907, STRINGER 18L-19L CRACKED. REMOVED AND REPLACED FRAME IAW SRM. (M) 2L72 4F A16WE 20040203000852004020300085 2004 2 3 ASAA0380565 420030826A2565D29982107 LANYARD DOUG DC9 DC982 3022082WP L1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01953AS 49386 SJC PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20040203000882004020300088WP 2004 2 3 ASAA0380587 120030912A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA LINE CHECK - FOUND EMERGENCY TRACK LIGHTS INOPERATIVE, BATTERY PACK DISCHARGED. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040205000182004020500018NM 2004 2 5 UIA9208 120031105A53119912246115 FRAME DOUG MD90 MD9030 3023690NM FUSELAGE CORRODED Z K NONE O OTHER ININSP/MAINT 1 TW0017919 53569 PERFORMED C04 CHECK, FOUND CORROSION ON FUSELAGE FRAME LOWER TEE CHORD AT STA Y=1437 L29R-L26R,CUT THE CORROSION PORTION OF T-CHORD. TRIM OUT THE INTERCOSTAL FORWARD SIDE, MAKE THE REPAIR PARTS AND INSTALL FASTENERS. 2L72 4F RTA6WE 20040204002342004020400234NE 2004 2 4 DHL2003765001 220031114A7200 ENGINE BOEING727 727264 138408MNM PWA JT8 JT8D17 52049NE STALLED A DHLAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO01765AT 23014 ON TAKE OFF, PRIOR TO REACHING TAKE OFF EPR HAD A SUSPECTED ENGINE COMPRESSOR STALL AND AN AUTO PACK TRIP EVENT. INSPECTED INLETS AND EXHAUSTS IAW M/M 05-21-10. NO DEFECTS NOTED. RUNWAY 33 BEING USED. WIND WAS AT 29 AT 26 KNOTS GUSTING TO 36. SUSPECT CROSS-WIND. AIRCRAFT OK FOR SERVICE. 2L73 4F4 F A3WE E2EA 20040205000542004020500054EU 2004 2 5 ASOA03671 120031225A3350 SWITCH AEROSPATR72 ATR72212 8680945EU COCKIT DIRTY A ASOAO OTHER O OTHER CRCRUISE 1 SO11634AS 370 FLT 4187 - DURING FILGHT FROM ATL-CSG, THE AFT ONE-THIRD PORTIONS OF EMERGENCY FLOOR LIGHTS ILLUMINATED UNCOMMANDED. AFTER THE CAPTAIN RESET THE FLT DECK, THE AFT FLT ATTENDANT STATION SWITCHES, AND RESET THE MFC'S THE LIGHTS WENT OUT. THE SYSTEM CHECKED NORMAL ON GROUND AFTER LANDING BY MX. IN FLT ON THE RETURN FLT FROM CSG TO ATL, THE AFT MOST SECTION OF FLOOR EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH. THE AIRCRAFT LANDED SAFELY IN ATL. MAINT RESET THE SYSTEM AND OPERATIONALLY CHECKED THE FLT ATTENDANT PANEL PUSH-BUTTON AND TOGGLE SWITCHES IN THE COCKPIT. THE DISCREPANCY WAS UNABLE TO BE DUPLICATED ON THE GROUND. (M) 2H72 4T RTA53EU 20040210000102004021000010WP 2004 2 10 UPS03841581 120031114A5312 BULKHEAD DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, AFT PRESSURE BULKHEAD IS CRACKED AT STATION 1766 AT LBL 36, 65 INCHES ABOVE FLOOR LEVEL. REMOVED EXISTING REPAIR DOUBLER,CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED FILLER AND REPLACEMENT DOUBLER I.A.W. DWG. SRO8530007,SRM 53-2-5 FIG. 14A. 2L74 4F RT4A25 20030129001132003012900113SW 2003 1 29 HEEA083997 120030117A5200407064807119 SUPPORT BELL 407 407 1182206SW ENG BAY DOOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 ENGINE BAY DOOR SUPPORT HAS HOLES FOR PIN ELONGATED. 1G71 3U O H2SW 20030131001562003013100156NM 2003 1 31 CA030108011 120030106A2612 WARNING SYSTEM BOEING737 737217 1384464NM PWA JT8 JT8D17 52049NE APU BAY ACTIVATED W F ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 CA (CAN) DURING CRUISE, THE APU FIRE DETECT LIGHT FLICKERED 3 TIMES. MAINTENANCE GROUND TESTED, NO FAULTS FOUND AND AIRCRAFT RELEASED FOR SERVICE.THE NEXT DAY THE APU FIRE DETECT LIGHT CAME ON BEFORE LANDING. AFTER LANDINGTHE APU FIRE LIGHT AND BELL CAME ON AND THE FLIGHT CREW PULLEDTHE FIRE HANDLE AND THE LIGHT STAYED ON. THE FIRE BOTTLE WAS DISCHARGED. NO IN DICATION OF FIRE. MAINTENANCE VERIFIED NO FIRE BUT THE APU COMPARTMENT WAS CONTAMINATED WITH DEICE GLYCOL. THE FIRE BOTTLE WAS REPLACED BUT NIL STOCK ON THE SQUIB SO THE APU WAS MEL'D AND THE AIRCRAFTRELEASED FOPR SERVICE. WILL UPDATE WITH ADDITIONAL INFO REGARDING THE DETECTION SYSTEM. 2L72 4F4 F A16WE E2EA 20030204001992003020400199NM 2003 2 4 SWAA030128 120030119A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 578 STR 11L, BS 663 STR 10R, BS 706 STR 10L, BS 727A STR 7R, BS 727B STR 8R, 767 STR 10L, BS 787 STR 10L AND STR 10R AND BS 807 STR 10L. REMOVED AND REPLACED CRACKED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030207001122003020700112NM 2003 2 7 03FDEA00072 120030122A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 MECHANICAL DAMAGE ON FLOORBEAM BS 990 RBL 37.5 WL 207. 2L73 4F RTA3WE 20030208000062003020800006 2003 2 8 RAIA00301024 420030124A341845150560 PROBE AEROSPATR42 ATR42300 8680920EU FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03426TE158333753 228 5589-STL- THE RIGHT ANGLE OF ATTACK C/B POPPED. MAINTENANCE REPLACED THE RIGHT ANGLE OF ATTACK PROBE, OPS CK OK. 2H72 4T RTA53EU 20030213000742003021300074NM 2003 2 13 03031407 120030131A2120 SMOKE DORNERDO32 DO328300 NM COCKPIT DETECTED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27407FJ 3157 AFTER TAKE OFF, CREW REPORTED HEAVY SMOKE IN COCKPIT. AN EMERGENCY WAS DECLARED WITH ATC AND AIRCRAFT RETURNED TO POINT OF DEPARTURE. AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE PERSONNEL INSPECTED AND ADJUSTED CROSSBLEED VALVE AND RAN ENGINES, NO SMOKE NOTED. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T RTA55NM 20030218002422003021800242NM 2003 2 18 SWAA030238 120030131A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 663, STR 10L AND STR 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM 2L72 4F RTA16WE 20030219000742003021900074NM 2003 2 19 SWAA030252 120030202A335020131A BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030220001112003022000111EA 2003 2 20 QXEA0300106 120030119A3010 LINE CNDAIRCL600 CL6002C10 1390015EA ANTI-ICE SYS RUPTURED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09614QX 10049 SUP SEA ON FLIGHT 2461- ABORTED TAKEOFF DUE TO WING ANTI-ICE FAULT MESSAGE. FOUND A LINE RUPTURED. REMOVED AND REPLACED LINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030221000242003022100024EA 2003 2 21 QXEA0300132 220030128A7230304865101 BLADE PWC PW150A BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA NR 2 ENGINE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX3516 PCEFA0007 4037 PCEFA0007 PDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE. LP COMPRESSOR ROTOR 1 BLADE CRACKED. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE SENT TO PRATT AND WHITNEY FOR EVALUATION. 2H72 4T4 TRTA13NM E00062EN 20030221000952003022100095SW 2003 2 21 AC2A084148 120030210A3213430036140105 CROSSTUBE BELL 430 430 1182150SW MLG CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT1068 49089 CROSSTUBE IS CORRODED. CROSSTUBE WAS REPLACED 1G72 3U RTH9SW 20030224000802003022400080NE 2003 2 24 HEEA084201 120030213A63207635109132102 PINION GEAR SKRSKYS76 S76A 8143006NE M/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322342970 A08100268 760096 MAIN ROTOR PINION GEAR HAS HEAVY FROSTING AND PITTING - GEAR WAS LOAD TESTED AND ACCEPTED PRIOR BY SIKORSKY PER SO # DF 624-0001 ON APRIL 18, 2001. TO BE SENT TO VENDOR. 1G72 3U H1NE 20030227001282003022700128SW 2003 2 27 HEEA084434 120030213A2435200SGL132Q STARTER GEN BELL 206 206L3 1182108SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03979BH2842 51403 STARTER GEN INOPERATIVE, NOT PRODUCING ANY D AND E VOLTAGE ON TEST STAND. 1G71 3U H2SW 20030228001122003022800112SW 2003 2 28 HEEA084467 120030213A3212OHSS2061001 COVER BELL 206 206L3 1182108SW EMERGENCY FLOAT DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 LT REAR, LT MID, RT REAR, RT MID FLOAT COVERS DETERIORATED. SCRAPPED. 1G71 3U H2SW 20030307000622003030700062 2003 3 7 SWAA030412 420030220A256565C19901 CABLE BOEING737 7373H4 1384600NM AFT SVC DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030630000262003063000026NM 2003 6 30 XNOA01122 120030528A3230 ACCESSORY UNIT BOEING727 727227 1384078NM MLG MALFUNCTIONED A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2376753 21249 AFTER GEAR RETRACTION ALL 3 RED GEAR UNSAFE LIGHTS REMAIN ILLUMINATED. GEAR POSITION INDICATOR INDICATED GEAR UP. ON GEAR RETRACTION TAIL SKID LIGHT REMAIN ILLUMINATED. FOM PROCEDURE INDICATED INSUFFICIANT FUEL FOR TRIP WITH TAIL SKID EXTENDED. RETURN TO FLL. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW B727 MM 32-09-121. PERFORMED GEAR SWING IAW B727 32-30-1. OPS CHECK NORMAL. 2L73 4F A3WE 20030707000332003070700033NM 2003 7 7 AALA20030573 120030516A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21351AA 24032 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 29 ABC INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT ASSEMBLY AT SEAT 29 ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030717000832003071700083SW 2003 7 17 HEEA088075 120030701A2432RG214 BATTERY BELL 214 214ST 1182106SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T386 28101 BATTERY WEAK. 2G72 4U H10SW 20030710000842003071000084EU 2003 7 10 DHL2003366505 120030523A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH 249 FWD CABIN FLOOR- FR 16 BL 61R SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK AT FR 16 BL 61 R IAW A300 SRM 51-40-11. ORIGINAL THICKNESS .200 REMOVED .027 AND .030 FOUND TO BE WITHIN LIMITS IAW A300 SRM 53-10-00. ALODINED AND PRIMED IAW A300 SRM 51-40-11. 2L72 4F RTA35EU 20030131001822003013100182WP 2003 1 31 MWEA030049 120030128A532059100911 DOUBLER DOUG DC9 DC982 3022082WP LEFT RADOME CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 LEFT RADOME HINGE CUT-OUT IS CRACKED AT PREVIOUS REPAIR. -- CUT-OUT DAMAGE, FABRICATED FILLER AND DOULBER AND INSTALLED. 2L72 4F A6WE 20030204000202003020400020SO 2003 2 4 R2J2003F00000 120030108A5540 STRUCTURE PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO RUDDER DAMAGED B R2JRK NONE O OTHER ININSP/MAINT 1 EA21113DK5533 347870151 DURING ANNUAL INSPECTION, FOUND RUDDER LOOSE AT ATTACHMENT. FITTING BOLT HOLES FOUND ELONGATED. AIRCRAFT ALREADY UPGRADED WITH MFG RUDDER FITTING KIT 7.64-100 (BIGGER BOLTS). THERE IS STILL A PROBLEM IN THIS AREA. SECOND AIRCRAFT FOUND WITH THIS PROBLEM. NEW FITTING INSTALLED. 1L72 3O3 O A7SO E9CE 20030204002742003020400274NM 2003 2 4 VNAA0301022 120030122A3240 METERING VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BRAKE SYS CONTAMINATED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07470PS 3006 THE CREW REPORTED THAT THE FIRST OFFICER'S BRAKES WERE NOT WORKING. MAINTENANCE INSPECTED AND BLED THE BRAKE METERING UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030205000492003020500049NM 2003 2 5 SROM200300016 120030116A5414657377482 SKIN BOEING737 737205 1384456NM ZONE 400 DENTED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 1 ENGINE IB NACELLE NR 2 LATCH CUTOUT DAMAGED. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 54-30-1, 51-40-2 & 51-10-2. MINOR REPAIR 2L72 4F RTA16WE 20030205000872003020500087NM 2003 2 5 DL76L030009 120030102A2530811150417 COFFEEMAKER BOEING767 767332 1382001NM FWD GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27188DN 27583 GALLEY 1R FWD OF DOOR COFFEEMAKER CB POPPED. BURNING ODOR. CONTINUED ON MCO. NO PARTS ATL. MEL 25-20-01D. 2L72 4F RTA1NM 20030207001532003020700153WP 2003 2 7 ZW0A0301702 120030206A33507732 LAMP DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13979TW 53629 THE EGRESS LIGHT AT THE RH OVERWING EXIT AND AT THE AFT GALLEY EXIT, WERE INOPERATIVE. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 10-11-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030625000842003062500084NM 2003 6 25 F3LA200300057 120030201A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 312 CORRODED FROM LBL 1 TO LBL 31. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-51, PARA 114, DETAIL XI. FABRICATED AND INSTALLED REPLACEMENT PART PER SRM 53-10-51 AND 51-40-02. 2L72 4F RTA16WE 20030219000522003021900052WP 2003 2 19 MWEA030102 120030217A5313591143361 LONGERON DOUG DC9 DC981 3022081WP LONG 12 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LONGERON 12 AND IT'S SHOVEL CLIP IS DAMAGED RIGHT OUTBOARD AFT OF AFT PRESSURE BULKHEAD. -- LOCATED AND DRILLED AND INSTALLED NEW SECTION OF LONGERON. 2L72 4F A6WE 20030219001502003021900150NM 2003 2 19 USAABB02011A 120030117A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19620AU 27199 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 17, 22, 26 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030115001172003011500117EU 2003 1 15 BAQA082898 120030108A6220 BEARING AEROSPSA365 SA365N 8680669EU STARFLEX SEPARATED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911UF1162 M1671 6338 MAIN ROTOR STARFLEX BEARING CAME OFF. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030116000272003011600027NE 2003 1 16 HEEA082984 220030107A74129550176020 GENERATOR SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE IGNITION SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 HIGH ENERGY GENERATOR POPS START CONTROL CIRCUIT BREAKER. 1G72 3U3 U H1NE E19EU 20030116001282003011600128 2003 1 16 HEEA083073 420030108A2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 NO TRANSMIT OR RECEIVE. REPLACED BROKEN C636 AND Q507. FOUND BAD R604 ON TRANSMITTER BOARD. REPLACED. CLEANED SLIGHT CORROSION ON MAIN BOARD. REPLACED Q602. REPLACED T603. 1G71 3U H2SW 20030116002672003011600267 2003 1 16 ABXA030028 420030108A2565416T200326 SLIDE BOEING767 767281 1385109NM L1 DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23790AX641 23140 MAIN ENTRY DOOR L1 SLIDE DAMAGED. INSTALLED MAIN ENTRY DOOR EMERGENCY SLIDE IAW MM. 2L72 4F RTA1NM 20030118000012003011800001SO 2003 1 18 C2XA02SH178 120030118A531214547494003 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2736915 145421 SHV-DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT TOP 2 RIVETS OF R/H VERTICAL REINFORCEMENT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030324000332003032400033NE 2003 3 24 NACA20030080 220030321A8530356996 CYLINDER PWA CB3 DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03993301755 1755 P31699 43576 P31669 DISCREPANCY: #1 ENGINE SHUT DOWN DUE TO RUNNING ROUGH.CORRECTIVE ACTION: REPLACED #11 CYLINDER. 2L74 4R4 R 6A3 5E8 20030306000922003030600092SW 2003 3 6 HEEA084800 120030221A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 STARTER GENERATOR WOULD NOT TURN OVER ENGINE. 1G72 4U H4SW 20030307000442003030700044NM 2003 3 7 SWAA030460 120030302A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 500A, BETWEEN STR 16R AND STR 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030310000202003031000020SW 2003 3 10 HEEA084929 120030227A6420 BEARING BELL 412 412 1182202SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH TR070197 33150 TAIL ROTOR HEAD HAS WORN FEATHERING BEARING. REPAIRED. 1G72 4U H4SW 20030310001652003031000165NM 2003 3 10 EIA2003032 120030228A5300UNK STRINGER BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Stringer 22L at BS 544 Corroded. CORRECTIVE ACTION: Repaired er ECRA 481-53-178-2. Removed corrosion per B747 SRM 51-10-02 2L74 4F A20WE 20030317000712003031700071EU 2003 3 17 03FDEA00231 120030305A5730 ACCESS PANEL AIRBUS310 A310 EU PWA JT9 JT9D* NE ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25448FE 260 LT WING, LOWER ACCESS CUTOUT FOR PANEL 550GB. TWO SCREW HOLES FOR PANEL HAVE DAMAGED EDGES. REMOVED ANCHOR NUTS TO ACCESS DAMAGED HOLES. REMOVED DAMAGED AREA AND REAMED HOLES TO 0.495 AND 0.467. ENSURED CLEANED HOLES ARE CRACK FREE BY HFEC IAW NTM 51-10-01. FABRICATED 2 BUSHINGS FROM 2024T3 AND FREEZE INSTALLED. REAMED BOTH HOLES TO FINAL DIA. OF 0.312 AND PROTECTED AFFECTED AREA IAW SRM A310 SRM 51-23-00. REINSTALLED ANCHOR NUTS. ALL WORK COMPLETED IAW RAS 0288/2003 AND EA 6-5710-68295 DATED 02-13-2003. 2L72 4F4 FRTA35EU E20EA 20030317000962003031700096NM 2003 3 17 03FDEA00257 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 17R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030122000172003012200017SW 2003 1 22 HEEA083404 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0353119467 51575 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000392003012200039 2003 1 22 HEEA083426 420030109A2340AA21400 AMPLIFIER BELL 206 206L1 1182107SW PA SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035745S 45491 PA AMPLIFIER SIREN INOPERATIVE. 1G71 3U H2SW 20030122002312003012200231SW 2003 1 22 HEEA083563 120030113A6210206015001107 BLADE BELL 206 206L3 1182108SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03129MR2929 51129 TIP CAP OF BLADE IS SEPARATED AT THE OUTBOARD END. 1G71 3U H2SW 20030327001162003032700116GL 2003 3 27 C2XA03CL043 220030217A720023070401 ENGINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 PYLON LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW27149605691 5691 145100 CAE311393 CLE FLIGHT 2067 THE CREW REPORTED A LAV SMOKE WARNING INFLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND A INTERNAL OIL LEAK ON THE NR 2 ENGINE. THE NR 2 ENGINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030317001162003031700116NM 2003 3 17 03FDEA00275 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 35R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030310000102003031000010 2003 3 10 HEEA084919 420030227A34211113034 INDICATOR BELL 412 412 1182202SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ATTITUDE INDICATOR ROLL WILL NOT ADJUST UNTIL 5 TO 10 MINUTES AFTER OPERATION. 1G72 4U H4SW 20030121000852003012100085SW 2003 1 21 HEEA083276 120030108A3213206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 CROSSTUBE HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030121001172003012100117SW 2003 1 21 HEEA083298 120030109A2560222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MISMANUFACTURED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 STRAPS ON SHOULDER HARNESS TOO SHORT. 1G71 3U H2SW 20030121001362003012100136WP 2003 1 21 ABXA030041 120030117A2133 OUTFLOW VALVE DOUG DC9 DC933F 302207AWP CABIN PRESSURE LACK OF LUBE A ABXAK NONE O OTHER CLCLIMB 1 GL23934AX 47462 AIRCRAFT WOULD NOT AUTO PRESSURIZE ON CLIMBOUT. MANUAL PRESSURIZATION ATTEMPTED, BUT OUTFLOW CONTROL WHEEL WOULD NOT MOVE. INSPECTED AND CLEANED OUTFLOW VALVE AS REQUIRED. NO DEFECTS NOTED. REMOVED CIRCUIT BREAKER COLLARS FROM CABIN PRESS CONTROL. OPS CHECKED GOOD. CLEANED VALVE AND LUBRICATED IAW DC-9 AMM 21-32-05 AND INSPECTED, OPS CHECKED IAW DC-9 AMM 21-32-00. 2L72 4F A6WE 20030730000312003073000031WP 2003 7 30 ABXA030268 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE STUB FRAME IN MAIN CARGO DOOR STA 223.5. REMOVED STUB FRAME, FABRICATED AND INSTALLED FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-3-0 AND 51-1-20D. 2L74 4F 4A25 20030722000492003072200049NM 2003 7 22 SWAA031507 120030709A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED TIE CLIP PER SRM. 2L72 4F RTA16WE 20030722000232003072200023NM 2003 7 22 2003F00451 120030120A5347 SEAT TRACK BOEING727 727222 1384073NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CORROSION ON SEAT TRACK AT STATION 1100, RBL 48. REPLACED SEAT TRACK AT FUSELAGE STATION 1070-1136, RBL 48. TREATED AND PRIMED. (M) 2L73 4F A3WE 20030722001242003072200124NM 2003 7 22 AWXA200300741 120030621A5414D54530052200 SKIN AIRBUSA319 A319132 3930340NM LT PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28820AW 1397 MCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 22-23. 2L72 4F RTA28NM 20030422001572003042200157SO 2003 4 22 LR7A03010 120030310A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2 4606 DURING THRU FLIGHT CHECK FOUND RAMP STA 8 SKIN DAMAGED BY CARGO RESTRAINT CHAIN AT FS 833, RBL 58 WL 178. REPAIRED SKIN IAW SRM SMP 583 51-140-12. LP 12124, PR 2. 2H74 4T A1SO 20030828000812003082800081NM 2003 8 28 DL777030671 120030719A24402550 RECEPTACLE BOEING777 777232 1385232NM EXTERNAL POWER ARCED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27863DA 29735 AFTER HOOKING UP EXTERNAL POWER, NOTICED ARCING COMING FROM RECEPTICLE. DISCONNECTED CORD FROM A/C. RECEPTACLE HAD BURNED. REPLACED EXTERNAL POWER RECEPTACLE IAW M/M. OPS CHECK GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F RTT00001SE 20030829000372003082900037NM 2003 8 29 CALA0300501 120030827A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616. A DOUBLER ANGLE WAS INSTALLED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20030725000172003072500017 2003 7 25 CHQA00412 420030529A3420 ODOR EMB 145 EMB145 3260210SO PFD DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL11834 AVIONIC BUTTON ON NR 2 PFD BLACK AND CHECK PFD2 ON EICAS SMOKE FOR UNDER PF D.FOUND PFD BURNED ODOR R&R FO'S PFD. 2L72 4F RTT00011AT 20030805001162003080500116SW 2003 8 5 ALGA088104 120030715A6320E6893673 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03587AL914 53248 CAE847158 REMOVED GEAR FOR EXCESSIVE SPALLING ON GEAR TEETH. 1G71 3U3 UO H2SW E1GL 20030904000612003090400061NE 2003 9 4 SWIA200312211 220030721A7261 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT ENGINE LEAKING A SWIAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 NM07597SW 7293 LEFT ENGINE OIL PRESSURE FLUCTUATING 27-32 LBS. AFTER 15 MINUTES (APPROX) PRESSURE DROPPED TO BELOW 25 PSI. ENGINE WAS SHUT DOWN. FOUND LEFT ENGINE STARTER CARBON SEAL LEAKING. INSTALLED SERVICEABLE CARBON SEAL AND SEAL RING. ALSO REPLACED IDG AND HYD PUMP CARBON SEALS AND SEAL RINGS. OPS AND LEAKS CHECKS GOOD. IAW GE SEI-756 SPECIAL PROCEDURE 63. P/N: 5018T49P01, 4018T16P04. 2L72 4F4 FRTA21EA E15NE 20030910001442003091000144NM 2003 9 10 MWEA030336 120030827A532159366931 FLOOR PANEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 AFT CABIN THE FILLER FLOOR PANEL LOCATED BETWEEN NR 2 AND NR 3 SEAT TRACK HAS CORROSION LOCATED BETWEEN STATION 1250-1309. FABRICATED AND INSTALLED FILLER FLOOR PANEL. 2L72 4F RTA6WE 20030318000022003031800002 2003 3 18 SWAA030581 420030315A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT SVC DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030318000472003031800047GL 2003 3 18 1503 220030225A7200 ENGINE BOEING767 767300 1385204NM GE CF6 CF680C2* GL NR 2 MALFUNCTIONED H EA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO21 30110 704955 DURING CRUISE NR 2 ENGINE STALLED, THRUST REDUCED TO IDLE. ENGINE STABALIZED. THRUST REAPPLIED, EGT RAPIDLY INCREASED AND ENGINE 2 WAS SHUT DOWN. 2L72 4F4 FRTA1NM E23EA 20030318001362003031800136NM 2003 3 18 GAIA03007OP 120030212A7932 INDICATOR BOEING727 727224 1384076NM NR 2 ENG OIL FALSE INDICATIONA GAIAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0779748 22450 FLT 879 - RNO-SJC - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE OIL QUANTITY ON NR 2 ENGINE WAS STEADILY DECREASING. THE CREW DECLARED AN EMERGENCY AND MADE A PRECAUTIONARY SHUT DOWN OF THE NR 2 ENGINE. DURING APPROACH THE OIL QUANTITY RETURNED TO NORMAL. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AT SJC. THE NR 2 ENGINE OIL FILTER WAS INSPECTED AND NO DEFECTS WERE NOTED. THE ENGINE AND OIL QUANTITY INDICATION OPS CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030326000332003032600033NM 2003 3 26 AUS20030134 120030209A2820 PUMP DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE FUEL SYSTEM FOD W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) FUEL SYSTEM EJECTOR PUMP FOD. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030418000812003041800081WP 2003 4 18 ZW0A0302402 120030219A3350 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139626F 53596 DURING OVERNIGHT LS CHECK EMERGENCLY LIGHTS IN AFT TAIL STAIRWAY INOP. INSTALLED BATTERIES IN POWER PACK B5-28 AND B5-27 LAMP 7732 1315. OPS CK NORMAL. CHECK-C 11-11-02 MCI. 2L72 4F RTA6WE 20030416004112003041600411EU 2003 4 16 XNOA01100 120030115A3240 BRAKE ASSY AIRBUS300 A300B4203 3930306EU NR 8 MALFUNCTIONED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23224KW 073 NUMBER 8 BRAKE WOULD NOT DISENGAGE WHILE ON TAXI WAY. REMOVED GREEN HYDRAULIC PRESS FROM NR 8 BRAKE. NR 8 BRAKE RELEASED. TRANS GREEN BRAKE SYSTEM TO DMI IAW ENA MEL 32-42-01. DMI 3049. PLACARDS INSTALLED. 2L72 4F RTA35EU 20030417000472003041700047CE 2003 4 17 DXTA200300001 120030123A783099144315 CIRCUIT BOARD CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL THRUST REVERSER FAILED E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07983QS3228 7500083 ON APPROACH TO GSO, (LT TR AUTOSTOW) AMBER CAS MESSAGE ILLUMINATED AND THROTTLE ROLLED BACK TO IDLE. 2L72 4J4 FRTT00007WITE6CH 20030327001482003032700148SO 2003 3 27 C2XA03IA018 120030209A3230355022002MOD3 CONTROL UNIT EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A C2XAO OTHER O OTHER CRCRUISE 1 SW2713913 145438 DURING FLIGHT THE CREW NOTED THAT THE AIR/GROUND FAIL MESSAGE ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB 145 AMM 32-32-01. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030731000932003073100093NM 2003 7 31 QXEA200300767 120030620A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - PATCH SKIN AT STATION X260, 11 INCHES BELOW BAGGAGE DOOR CUT-OUT. REPAIRED IAW RD 8/4-53-505, PAGE 3. 2H72 4T RTA13NM 20030801000832003080100083SO 2003 8 1 C2XA03IA073 120030716A323023092900001 UPLOCK EMB 145 EMB145 3260210SO NLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149591138011380 145091 IAH - FLIGHT 2368, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT FULLY RETRACT WITH A LANDING GEAR DISAGREE MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NOSE LANDING GEAR UP-LOCK BOX IAW EMB-145 M/M 32-33-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040223000682004022300068NM 2004 2 23 UPS04M41693 120031229A5730 SKIN DOUG MD11 MD11F 3023600NM RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01253UP INSPECTION TYPE: 1C, RT WING LOWER FIXED LE SKIN CRACKED AT NR 7 SLAT IB TRACK CUTOUT AT XOS 888. NDT VERIFIES CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-10-00 FIG.21. 2L73 4F RTA22WE 20030721001362003072100136NM 2003 7 21 SWAA031449 120030630A53206551698 SPLICE BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 8R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F A16WE 20030722000152003072200015NM 2003 7 22 2003F00443 120030307A5330 SKIN BOEING727 727222 1384073NM FUSELAGE LIGHTNING STRIKEA RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND LIGHTNING STRIKE AT FUSE CROWN, BS 720 STRINGER 3R. DRILLED OUT LIGHTNING STRIKE AT FUSELAGE CROWN BS 720A PLUS 11 INCHES, STRINGER 3 RIGHT, AND INSTALLED FASTENER. (M) 2L73 4F A3WE 20030721001292003072100129NM 2003 7 21 SWAA031493 120030706A5754654643099 SKIN BOEING737 7373TO 138447GNM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C4 CHECK, FOUND LT INBD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBD T/E FOREFLAP PER MM. 2L72 4F RTA16WE 20030724000352003072400035NM 2003 7 24 DL76G030535 120030610A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM EMERGENCY LIGHTSFAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO271604R 30180 ON LAYOVER FOUND RIGHT AFT 3 WING SLIDE EMERGENCY LIGHTS INOP. FOUND ALL 3 BULBS BAD ALONG WITH PWR SUPPLY M733. REPLACED BULBS AND PWR SUPPLY WITH BATTERY PACK. 2L72 4F RTA1NM 20040217000742004021700074EU 2004 2 17 KBM2004F00005 120031104A6720350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 TAIL ROTOR PITCH LINKS HAVE PLAY BEYOND LIMITS. REMOVE AND REPLACE PITCH LINKS. (K) 1G71 3U3 U H9EU E19EU 20040329001792004032900179NM 2004 3 29 2003UALA00869 120031117A2133202248010 ACTUATOR BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE OUTFLOW VALVE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29620UA37502972 21880 RETURNED TO FIELD DUE TO CABIN PRESSURE PROBLEMS. AUTO PRESS MODE FAILED. *S/D* THE OUTFLOW DOOR DC MOTOR WAS FOUND TO FAIL WHEN EXPOSED TO COLD SOAK NOT ALLOWING THE AC MOTOR TO OPERATE. 2L72 4F4 FRTA1NM E3NE 20040308001662004030800166NM 2004 3 8 ASAA0310248 120030327A7110 FRAME BOEING737 737298C 1384490NM NR 2 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 153 CHAFED. FABRICATED AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040316000972004031600097WP 2004 3 16 ASAA0380311 120030411A57201044415 SUPPORT BRACKET DOUG DC9 DC983 3022083WP RT FUEL LINE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, RIGHT FUEL TANK FUEL LINE SUPPORT BRACKET IS CRACKED ON OUTBOARD SIDE. REPLACED SUPPORT BRACKET PER SRM 51-30-1 AND 10-4. (M) 2L72 4F RTA6WE 20040728001422004072800142NM 2004 7 28 ASAA0340346 120031128A282361163 SHUTOFF VALVE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU ENGINE FUEL LEAKING A ASAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 NM01713AS15886 30161 860139 DURING CRUISE, NR 1 ENGINE EXPERIENCE ELECTRICAL POWER DISREPANCIES AND SUBSEQUENT FLAME OUT. AIRCRAFT DIVERTED TO EUG AND LANDED WITHOUT INCIDENT. SEA - WHILE PERFORMING ENGINE FUEL FEED LINES/COUPLING VACUUM TEST AS PER TECH SERVICE REQUEST AND IAW BOEING AMM 28-22-00. FOUND THE THERMAL RELIEF VALVE ON PORT ADAPTER ASSEMBLY ON ENGINE FUEL SHUTOFF VALVE LEAKING AIR. REMOVED AND REPLACED ENGINE FUEL SHUTOFF VALVE. OPS CHECKED GOOD. (M) 2L72 4F4 FRTA16WE E21EU 20030414001222003041400122NE 2003 4 14 CA030306005 220030225A7230 ENGINE PWA PT6 PT6A67D NE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 12514 (CAN) ENGINE WAS REMOVED FROM WING AFTER WHAT WAS SUSPECTED TO BE A NR 3 BEARING FAILURE AND OIL CONTAMINATION (METAL IN OIL). ENGINE WAS SENT TO ATI TO INVESTIGATE BOTH THE BEARING FAILURE AND THE OIL CONTAMINATION, TO REPLACE THE CT DISK & PT DISKS AND TO OVERHAUL BOTH GG-PS 0090 & POWER SECTION. THIS FINAL REPORT COVERS FINDINGS ONTHE GAS GENERATOR SECTION SEPARATE FINAL REPORT IS BEING ISSUED FOR POWER SECTION. DAMAGE THAT WAS FOUND IN GG SECTION IS NOT UNEXPECTED FOR AN ENGINE WHICH OPERATED FOR 12514.3 HOURS WITHOUT OVERHAUL AND 6154.3 SINCE LAST SHOP VISIT. THERE WAS NO EVIDENCE OF OIL FILTER BYPASS OR OF ANY DAMAGE RELATED TO METAL CONTAMINATION. 4 T E26NE 20030819000042003081900004EU 2003 8 19 ALGA088138 120030629A6730SC50911 SERVO UROCOPEC120 EC120B 8680987EU CYCLIC MALFUNCTIONED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03513AL 1261 CYCLIC SERVO HAS FEEDBACK FORWARD & AFT. TO RETURN CORE OWED. RETURNING P/N:SC5091-1 S/N:876 RO 15193 1G72 3U NCR0001RD 20030819001352003081900135NM 2003 8 19 CALA0300357 120030702A5347 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND THE LT I/B SEAT TRACK CORRODED BETWEEN BS 907 AND 947. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. 2L72 4F RTA16WE 20030328000442003032800044SO 2003 3 28 C2XA03TY030 120030226A531014525480003 SILL EMB 145 EMB145ER 3260211SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 DURING A SCHEDULED 3C INSPECTION THERE WAS EVIDENCE OF CORROSION UNDER THE CARGO DOOR SILL PROTECTIVE PLATE. MAINTENANCE DRILL OUT THE RIVETS IN SILL, REMOVED CORRODED PARTS, FAB NEW BRACKETS AND INSTALL ALONG WITH A NEW CARGO SILL IAW EMB 135/145 SRM 51-40-02; SRM 51-30-01 AND EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030820000952003082000095NM 2003 8 20 UPS03640986 120030719A3350 BATTERY BOEING767 76734AF 1385212NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01304UP 27242 EMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS WHEN SELECTED TO ON. REPLACED BATTERY, OPS GOOD. 2L72 4F RTA1NM 20030820000712003082000071NM 2003 8 20 03FDEA01115 120030718A5270 SWITCH DOUG MD11 MD11 3023602NM CARGO DOOR INTERMITTENT A FDEABJA EMER. DESCENT DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25588FE 48490 AT APPROX 500 FEET CARGO DOOR AFT -A- LEVEL TWO ILLUMINATED. DUMPED TO MAX LANDING WEIGHT. COMPLIED WITH QRH AND RETURNED TO SFS. NOTE: DOOR OPEN LIGHT ALSO ILLUMINATED. ENT BY: 317084 RPT BY: 096537 FACT 18JUL03 22:14 SFS R REMOVED AND REPLACED S1 -383 DOOR CLOSE SWITCH DUE FOUND INTERMITTENT OPERATION, AND S1-261 DOOR LOCK SWITCH FOR PRECAUTIONARY PER MD11 AMM 52-33-04. PERFORMED CARGO DOOR CHECK, OPENING AND CLOSING NORMAL. ENT BY: 363743 RPT BY: 363743. 2L73 4F RTA22WE 20030401000772003040100077NM 2003 4 1 DHL2003741503 120030323A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C CHECK, BS 500 RT CIRCUM. DENTED 4 INCH ABOVE FLOOR. CUT-OUT DAMAGED AREA DIM 1 1/2 INCH AS PER B-727 SRM 53-10-4 FIG. 2. 2L73 4F RTA3WE 20030410002222003041000222NM 2003 4 10 DL76G030309 120030331A33501317 LIGHT BOEING767 767332 1382001NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO271602 29694 ON L/O FOUND EMERGENCY EXIT LIGHT INOP AT 37FG OVERHEAD. RELAMPED, CHECKS OK. 2L72 4F RTA1NM 20030416002452003041600245SO 2003 4 16 C2XA03SH090 120030407A531014522226003 BUTT STRAP EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL LAVARATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV DURING C CHECK LAVARATORY CENTER BUTT STRAP WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030416003482003041600348EU 2003 4 16 KAI1 120030103A2121207640 MOTOR BRAERODH125 HS125700A 4230170EU FAN OVERHEATED E KKYAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NE03270KA2080 NA0307 AFTER START OF NR 2 ENG, SMOKE COMING FROM AFT CABIN AREA. CREW SHUT DOWN RT ENG, APU, EVACUATED PAX & TURNED OFF ELECTRICAL PW. INVESTIGATION REVEALED NO SOURCE OF SMOKE. DETERMINED SMOKE COMING FROM AFT BAGGAGE AREA RT BULKHEAD AREA, AND A BLOWN CB GROUND RECIRC FAN, INDICATED A POSSIBLE VENTURI FAN MOTOR FAILURE. INSPECTION OF VENTRI FAN REVEALED A HIGH HEAT AREA. FAILED COMPONENT ELECTRICALLY ISOLATED, ACFT FLOWN TO HOME BASE. AN AD 94-11-03 HAD BEEN ACCOMPLISHED ON ACFT WHEN IT FIRST CAME INTO EFFECTIVITY IAW ALERT S/B 21-A150. REINSPECTED WITHIN PAST 24 MO AS PART OF AN MFG`S FLEXIBLE MX SCHEDULE PROGRAM 48 MOS ITEM. UNIT REPLACED WITH THERMALLY PROTECTED PART, REPLACEMENT PER S/B 21-142-3514A. 2L72 4F A3EU 20030425000102003042500010WP 2003 4 25 UPS03840391 120030320A5310 FITTING DOUG DC8 DC873F 302199FWP C1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, C1 DOOR AFT TORQUE BOX FLOOR SUPPORT FITTING CRACKED AT TWO LOCATIONS. REMOVED SUPPORT FITTING. DRILLED AND INSTALLED NEW FITTING (P/N 97540 55-2). 2L74 4F RT4A25 20030429001812003042900181SW 2003 4 29 CA030407006 120030402A3246D26651 SADDLE BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL SKID TUBE CRACKED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) UPON PREFLIGHT INSPECTION, CRACK WAS DETECTED VISUALLY IN AFT OUTBOARD SADDLE OF LT SIDE TUBE. THE MANUFACTURER PUBLISHED SERVICE INSTRUCTION DRAWING NO.DSI 9150 DATED 99.04.01 TITLED (ADD 206 SADDLE SPACERS) TO PREVENT SADDLE CRACKING. THIS AIRCRAFT HAD COMPLIED WITH THIS SERVICE INSTRUCTION, CORRECT TORQUE WAS FOUND ON ALL FASTENERS. 1G71 3U3 U H2SW E4CE 20030430000822003043000082SO 2003 4 30 SIMA200308402 120030318A5310 WINDOW FRAME EMB 135 EMB135LR 3260305SO COCKPIT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 DURING AN IMBV INSPECTION, THE RIGHT WINDSHIELD LOWER BEAM OUTBOARD 8 SCREW HOLES WERE FOUND TO BE CORRODED. HOLES WERE REAMED TO REMOVED CORROSION. FIVE HOLES REQUIRED FURTHER REAMING AND REQUIRED BUSHINGS TO BE FABRICATED AND INSTALLED. ALL WORK WAS DONE IAW REPAIR STATEMENT IC2003-145/0899, GST-1578/02-B AND ETN EB-53-035. (M) 2L72 4F RTT00011AT 20030501001982003050100198NM 2003 5 1 ASAA0310053 120030301A5347BAC15201432 SEAT TRACK BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SEAT TRACK AT BS 787-867, LEFT BUTTOCK LINE 24 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20030505000622003050500062NM 2003 5 5 CALA0300208 120030406A5522 SKIN BOEING737 737524 1384721NM ELEVATOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2737615 27328 THE AIRCRAFT SUFFERED HAIL DAMAGE TO THE LT ELEVATOR UPPER SKIN PANEL AT APPROXIMATELY ELEVATOR STATION 110.49. THE HAIL IMPACT CAUSED A SMALL DENT APPROXIMATELY 4.5 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE CLEAN UP REQUIRED REMOVAL OF ALL PLIES. THE SKIN WAS REPAIRED IAW ECRA 5520-01329. 2L72 4F RTA16WE 20030505001182003050500118SO 2003 5 5 C2XA03SH111 120030421A531014522460013 BUTT STRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE CENTER BUTT STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030505001752003050500175NM 2003 5 5 SWAA030847 120030415A2612894093 FIRE LOOP BOEING737 7372H4 138448CNM PWA JT8 JT8D15 52051NE NR 1 ENGINE MALFUNCTIONED A SWAAEFBAENGINE SHUTDOWN ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29092SW 22964 687787 IN FLIGHT SHUTDOWN, DECLARED EMERGENCY. NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. NO SIGN OF ENGINE PROBLEMS INDICATED ON ENGINE INSTRUMENTS. BOTH FIRE BOTTLES EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE LOWER FIRE LOOP & FIRE DETECTION UNIT PER MM. 2L72 4F4 F A16WE E2EA 20030506000652003050600065NM 2003 5 6 03FDEA00646 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) FITTING BORE HOLE FOUND CORRODED. CORROSION ON LH WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) FITTING PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-08 FIG. 401. 2L73 4F RTA22WE 20030506002182003050600218WP 2003 5 6 ASAA0380201 120030304A53202929169 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, FORWARD FLOOR SUPPORT CORRODED AT FS 160-200. REPLACED SUPPORT PER SRM 53-01. (M) 2L72 4F A6WE 20030513000722003051300072SO 2003 5 13 RAIA00304122 120030427A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03817HK 145058 EMERGENCY EXCAPE PATH LIGHTING, ONE STRIP INOP. RESET POWER AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20030513000762003051300076 2003 5 13 RAIA00305126 420030501A31607003110901 DISPLAY AEROSPATR42 ATR42300 8680920EU COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03423TE132324276 119 FO'S EFIS TUBE WENT BLANK. MAINTENANCE REMOVED AND REPLACED THE FO'S EFIS TUBE, OPS CK OK. 2H72 4T RTA53EU 20030515000202003051500020EA 2003 5 15 SWIA200311941 120030331A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FOUND FS 280 BL 9.0 LEFT AND RIGHT FLOORBEAM ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 41-42-21 AND 51-23-00. 2L72 4F RTA21EA 20030627000022003062700002CE 2003 6 27 DXTA200300016 120030418A3230 LANDING GEAR CESSNA750 750 2076810CE MAIN FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07910QS 7500110 AFTER TAKE OFF GEAR WOULD NOT RETRACT. - SERVICED NOSE STRUT AND PERFORMED GEAR SWING, SYSTEM OPS CHECKED GOOD. 2L72 4J RTT00007WI 20030602000222003060200022NM 2003 6 2 USAA030047 120030502A5540 FLANGE BOEING737 737401 1384701NM RUDDER BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 FOUND HINGE COVER ATTACH FLANGE BROKEN OFF, LOWER RIGHT SIDE OF RUDDER 23 INCHES FROM BOTTOM. MANUFACTURED REPAIR STRAP AND FILLERS PER EA 76261. (M) 2L72 4F RTA16WE 20030604000502003060400050NM 2003 6 4 UPS03640465 120030425A5754 SKIN BOEING767 76734AF 1385212NM LT WING SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01304UP 27242 LT WING L/E CRACK IN FIBERGLASS SKIN ON SLAT CLOSURE PANEL. FOUND S MALL DENT WITH CRACKS LOWER LEADING EDGE OF LEFT WING NEAR FUSELAGE. TRIMED DAMAGE REA OUT PER SRM 51 70 AND EO B767 5750 15568-B (AS REF FOR GAP). 2L72 4F RTA1NM 20030929000922003092900092WP 2003 9 29 UPS03841161 120030825A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, 1 EA LIGHTNING STRIKE IS OUT OF LIMITS AT STA -95 4 INCHES ABOVE LONG 20L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030730000022003073000002WP 2003 7 30 ABXA030202 120030421A534057508683 ATTACH FITTING DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23843AX 46017 TAIL SKID UPPER ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20 AND 51-1-21. REMOVED AND REPLACED GILLINER IAW DC-8 SRM 51-1-21. 2L74 4F 4A25 20030915000942003091500094SW 2003 9 15 ALGA089087 120030910A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03457AL 53151 FOUND DISC CRACKED. REMOVED AND REPLACED. 1G71 3U O H2SW 20030929000252003092900025NM 2003 9 29 03FDEA01416 120030901A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING O/B FLAP VANE NR 4 FROM I/B, TEE FITTING FWD BORE FOUND CORRODED. 2L73 4F RTA22WE 20030930000962003093000096NM 2003 9 30 AWXA200301033 120030905A5320693535214 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK A .7500 INCH CRACK WAS FOUND ON STRINGER CLIP AT BS 597, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 597, STR 8 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20030905002162003090500216SO 2003 9 5 C2XA03TY130 120030818A534714532606003 SEAT TRACK EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LW3. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20031002001042003100200104EU 2003 10 2 DHL2003366006 120030911A5210 LINKAGE AIRBUS300 A300B4203 3930306EU PAX DOOR UNSECURE A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01366DH 249 MAIN ENTRY DOOR WILL NOT CLOSE. HANDLE STOPS HALFWAY DOWN. FOUND HORIZONTAL LINKAGE SHAFT NOT SECURED. SECURED SHAFT AS REQUIRED. REF. 52-11-11 IPC AS REQUIRED. DOOR OPERATES OKAY. 2L72 4F RTA35EU 20031008000602003100800060EA 2003 10 8 COMA0360414 120030912A3320 LIGHT CNDAIRCL600 CL6002B19 1900309EA LAVATORY ODOR A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01959CA 7116 F/A REPORTED BURNING ELECTRICAL ODOR IN LAVATORY. DEFERRED THE LAV LIGHTING SYSTEM PER MEL. 2L72 4F RTA21EA 20031016000052003101600005NM 2003 10 16 03FDEA01668 120031001A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 RT 930 FRAME CRACKED AT LWR SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 RT, PER SRM 53-10-4, EA 7-5310-55032. 2L73 4F4 FRTA3WE E2EA 20031020001562003102000156NM 2003 10 20 DLM88030785 120030826A2120R2279 RELAY DOUG MD88 MD88 3023688NM E/E BAY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27973DL 53241 F/A REPORTED HEAVY BURNING SMELL IN CABIN, SHORTLY AFTER SMELL ALSO IN COCKPIT. DIVERTED TO CVG. DISSIPATED AFTER 10-15 MINS. T/S PER OPN 5088 COMPLETED BLOCKS 1 THROUGH 6, NO TROUBLE FOUND. C/W OP 5088 AND 5089 DUCT BURNOUT, NO ODORS NOTED. ALSO DURING T/S FOUND CABIN RECIRC FAN INOP. REPLACED RELAY R2-279, OPS CHECKS GOOD. 2L72 4F RTA6WE 20031020002902003102000290NM 2003 10 20 2003UALA00650 120030826A2130AC4500052 SWITCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN PRESSURE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29657UA* 27112 FWD EQUIP OVERHEAT MSG DISPLAYED. THE CABIN PRESSSURIZATION CONTROL MODULE M17, ROTARY SWITCH FAILED. THE SWITCH WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20031021003022003102100302SO 2003 10 21 C2XA03CL168 120030920A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714942 145037 DURING ROUTINE MAINTENANCE THE CENTER FUSELAGE CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CENTER FUSELAGE CABIN EMERGENCY CEILING LIGHT INVERTER. OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS WERE GOOD. 2L72 4F RTT00011AT 20031022000602003102200060NM 2003 10 22 QXEA200301161 120030917A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 TWO NICKS .2500 INCH APART IN LOWER FUSELAGE SKIN BETWEEN LEFT STRINGERS 31 AND 32, 2 INCHES AFT OF X1.0. REPAIRED IAW Q400 SRM 51-26-10, 51-14-00, 51-00-02, 51-00-04, 51-25-05-370-801, RD 8/4-53-714 AND HORIZON AIR EA 6-53-296. 2H72 4T4 TRTA13NM E00062EN 20031028000262003102800026NM 2003 10 28 CALA0300567 120030928A256010775277 BATTERY BOEING777 777224 1385225NM FLASHLIGHT DISCHARGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777012 29860 INSPECTION FOUND THE FLIGHT ATTENDANT FLASHLIGHT NEAR L-4 DOOR DISCHARGED AND THE EMERGENCY USE ONLY SEAL WAS BROKEN. THE BATTERY, INSPECTION STICKER, AND EMERGENCY USE ONLY SEAL WAS REPLACED. 2L72 4F RTT00001SE 20031029000642003102900064NM 2003 10 29 ASAA0340068 120030227A5311654796039 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND DENTS ON RADIUS OF FRAME AT BS 847 RBL 21-22 WL 156. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031118000412003111800041NM 2003 11 18 AWXA200301156 120031007A33501012623 LIGHT BOEING737 7373G7 1384595NM FUSELAGE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING INSPECTION THE OVERWING EMERGENCY EXIT LIGHT IN CENTER CABIN WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT CENTER CABIN, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031110000962003111000096SO 2003 11 10 C2XA03SH427 120031104A532014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK, THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031120000472003112000047EA 2003 11 20 SWIA200312495 120031005A2752852D10011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07915SW3667 3667 7615 FLAPS FAIL MESSAGE WHEN SELECTED TO 45 DEGREES. FLAPS STOPPED AT 33 DEGREES. QRH COMPLIED. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR AND RIGHT INBOARD FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-53-01 AND 27-53-05. P/N OFF: 852D100-11, S/N OFF: 3220AB, P/N ON: 852D100-19, S/N ON: 3759. 2L72 4F4 FRTA21EA E15NE 20040212000552004021200055EU 2004 2 12 KBM2003F00097 120031105A6420350A27119123 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 NR 1 AND NR 4 PUSH PULL TUBE BEARING WORN. REMOVED AND REPLACED WITH NEW. 1G71 3U3 U H9EU E19EU 20031103001482003110300148NM 2003 11 3 03FDEA01724 120031008A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING OB FLAP OB HINGE FITTING (FLAP SIDE)- OB HINGE LUG HOLE AND SURFACE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE)- O/B HINGE LUG HOLE AND SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031106001942003110600194 2003 11 6 SWAA032258 420031015A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED RON, FOUND R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031112000932003111200093NM 2003 11 12 C1HA200394027 120031107A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 FLOORBEAM CORRODED BS 1110 RBL 12. 2L73 4F A3WE 20030918000892003091800089EU 2003 9 18 V9B2003F00003 120030620A27224AS5820500001 ACTUATOR ISRAELGALAXYGALAXY 4500307EU RUDDER TRIM INOPERATIVE E V9BAO OTHER O OTHER NRNOT REPORTED 1 SW0583EJ 2501 009 RUDDER TRIM WOULD NOT MOVE. FOUND LOWER TRIM ACTUATOR RECEIVING POWER BUT IT WOULD NOT MOVE. INSTALLED NEW LOWER ACT PN 4AS5830510-013 BUT COULD NOT TIME ACTUATORS TOGETHER, SO REPLACED THE UPPER ACTUATOR AND WAS ABLE TO RIG ACTUATOR TOGETHER. 2L72 4F RTA53NM 20030919000312003091900031NM 2003 9 19 730PA0005 120030808A3350 BULB BOEING737 7373L9 1384470NM EMERGENCY LIGHT BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05730PA 27924 EMERGENCY EXIT BULB BURNED OUT AT MAIN ENTRY DOOR, OVER HEAD BINS 2A, 3A, AND AFT RT. REPLACED BULBS. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20031006001592003100600159 2003 10 6 SWAA031962 420030831A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20031007000502003100700050 2003 10 7 AALA20030774 420030716A2565 GIRT BAR BOEING757 757223 1384957NM CABIN LACK OF LUBE A AALAK NONE O OTHER ININSP/MAINT 1 SW21612AA 24488 UPON ARRIVAL BOS L1 DOOR GIRT BAR WOULD NOT RELEASE. CLEANED AND LUBRICATED L1 DOOR GIRT BAR SLIDERS ON FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031006001962003100600196NM 2003 10 6 03FDEA01587 120030919A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) INBOARD AND OUTBOARD PIVOT HOLES CORRODED AT BORES AND SPOT FACES. RT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) INBOARD AND OUTBOARD PIVOT HOLES BORES AND SPOT FACES CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-72703. 2L73 4F RTA22WE 20031119000552003111900055WP 2003 11 19 CALA0300589 120031012A5330 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2792874 49122 INSPECTION FOUND INTERNAL DOUBLER FOR OUTFLOW VALVE CORRODED AT STA 1325 BETWEEN L21L AND L22L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-02. 2L72 4F A6WE 20031121000452003112100045NM 2003 11 21 SWAA032517 120031113A5610141A48103 CONTROLLER BOEING737 7377H4 1384404NM WINDSHIELD FAILED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29726SW 27858 L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 COCKPIT WINDOW AND HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20031124000552003112400055NM 2003 11 24 03FDEA01899 120031110A5280 HINGE BOEING727 727200 138407ENM MLG DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION ON FASTENERS ALONG UPPER LT GEAR BODY DOOR HINGE AREA ENTIRE LENGTH. *S/D* CORROSION ALONG UPPER LT GEAR BODY DOOR HINGE AREA ENTIRE LENGTH. ORIG THICKNESS .020. LOWEST READING .078, FOUND TO BE IN LIMITS IAW SRM 53-10-1. 2L73 4F RTA3WE 20030604000762003060400076NM 2003 6 4 UPS03440490 120030411A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 M/D - SEAT TRACK I/B FLANGE CORROSION. CUTOUT SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.050 X 1 X 1 INCH. EXCEED SRM LIMIT. 2L74 4F A20WE 20030605001362003060500136EU 2003 6 5 CA030319003 120030318A2435BOGUS BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE STARTER GEN SEIZED W A UNSCHED LANDING HE ELECT. POWER LOSS-50 PC VIBRATION/BUFFET CRCRUISE 1 CA 5970 (CAN) DRIVE END BEARING SEIZED DURING FLT, SPUN IN BEARING LINER. WORE OUTER DIAMETER OF BRG RACE DOWN TO POINT THAT ARMATURE BEGAN RUBBING ON STATOR. THIS WEAR CONTINUED UNTIL SUFFICIENT TORQUE BUILT UP TO SHEAR DRIVE SHAFT AT QUILL SECTION. TEARDOWN OF UNIT REVEALED THAT BRGS INSTALLED ARE BOGUS PARTS. CORRECT PART IS MADE BY THE OEM, APC, AND IS P/N 150SG1052B. BEARINGS FOUND WERE MARED 'JAF 6203RS JAPAN'. SEIZED BRG SHED ITS SEALS, EXPOSING BALLS. BOGUS BEARINGS HAVE TWO ROWS OF EIGHT BALLS, WHILE OEM PART HAS ONE ROW OF EIGHT BALLS. ACCORDING TO COMPONENT HISTORY CARD, UNIT WAS INSTALLED ON AN A/C WHEN IT WAS IMPORTED THE BEARINGS ARE BEING HELD IN QUARANTINE PENDING INSPECTION. 1G71 3U3 UNCH9EU E19EU 20030609001022003060900102SO 2003 6 9 C2XA03SH144 120030523A531014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030515001022003051500102NM 2003 5 15 03FDEA00615 120030423A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING FOUND INBOARD FLAP, OUTBOARD HINGE, INBOARD & OUTBOARD HOLE WITH CORROSION (FLAP SIDE PIVOT HOLE). CORROSION ON RT WING, INBOARD FLAP, OUTBOARD HINGE, INBOARD AND OUTBOARD HOLE REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5750-69224. 2L73 4F RTA22WE 20030520000212003052000021WP 2003 5 20 GTIA030266 120030409A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 180 FLOOR PANEL SOFT/MUSHEY CORRODED AT INSERTS. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20030520001022003052000102NM 2003 5 20 AALA20030345 120030318A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21388AA 27448 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 2F INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030612000922003061200092SO 2003 6 12 C2XA03IA056 120030529A3230355022022MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG INTERMITTENT A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2719554 145587 FLIGHT 2548, THE CREW NOTED INTERMITTENT LANDING GEAR LEVER DISAGREE IN FLIGHT. HANDLE IN THE UP POSITION ALL GEAR INDICATORS SHOW UP, BUT BOXED IN RED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, IAW ERJ 145 MM- 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030617002112003061700211NM 2003 6 17 QXEA200300720 120030604A5714 FLANGE BOMBDRDHC8 DHC8401 1390041NM WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - TRAILING WING BOX UPPER FLANGE HAS CHAFES FROM YW43L TO YW43R. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030521000522003052100052EU 2003 5 21 MALA030256 120030416A5753HC579L0884000 HINGE BAC 146 AVRO146RJ85A1500097EU TE FLAP CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 WHILE COMPLYING WITH FLAP EO AD020307 FOUND RT O/B HINGE AFT PIN HC579L0884-004 AND RT I/B FLAP HINGE PINS HC579L0884-000 AND HC579K0884-002 WITH CORROSION. MAINTENANCE REPLACED PINS FOR CORRECTIVE ACTION. 2H74 4F RTA49EU 20030522000542003052200054SO 2003 5 22 C2XA03TY067 120030517A532014522178005 CHANNEL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL CHANNEL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREA, FILLED WITH EPOXY RESIN, FABRICATED AND INSTALLED A DOUBLER IAW GST1927/02A AND CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030522000352003052200035WP 2003 5 22 GTIA030288 120030412A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 CABIN FLOORBOARD STA 1003-1079 DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20030618001132003061800113NM 2003 6 18 SWAA031290 120030609A575165C25911 AILERON BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED PM CHECK, FOUND LT AILERON DELAMINATED AT T/E. REMOVED AND REPLACED LEFT AILERON PER MM. 2L72 4F RTA16WE 20030523001452003052300145WP 2003 5 23 GTIA030310 120030408A5310 DOOR FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE LWR DOOR JAMB CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FORWARD CARGO LOWER DOOR JAMB CUTOUT CORRODED (DOOR PAN). FABRICATED -19, -21 REPAIR SPLICES. DRILLED AND LOCATED NEW PAN. INSTALLED DOOR JAMB PAN. INSTALLED FWD AND AFT REPAIR SPLICE. 2L72 4F4 F A6WE E2EA 20030527000522003052700052NM 2003 5 27 AWXA200300456 120030423A53156546812 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM BS 1006-1016, LBL 10. MAINTENANCE REMOVED FLOOR SUPPORT BEAM BS 1006-1016, LBL 10 AND UPON FURTHER EVALUATION DISCOVERED FILLER WAS CORRODED BEYOND LIMITS; FABRICATED A NEW FILLER; INSTALLED FILLER ON BEAM; AND REINSTALLED FLOOR SUPPORT BEAM IAW B737-300 SRM 51-30-01 PG 23. 2L72 4F RTA16WE 20030619000602003061900060SW 2003 6 19 HEEA087401 120030611A6510407340339101 BEARING BELL 407 407 1182206SW TAIL ROTOR TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 TAIL ROTOR BEARING HAS A TORN SEAL. 1G71 3U O H2SW 20031124000622003112400062NM 2003 11 24 C1HA200394045 120031114A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 959 - 1140 RBL 24 HAS BARE METAL AND CORROSION. 2L73 4F A3WE 20031117000832003111700083SW 2003 11 17 ALG2003F00090 120030822A6340B4678 CHIP DETECTOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TRANSMISSION MALFUNCTIONED E ALGAO OTHER N FALSE WARNING LDLANDING 1 SW03457AL 53151 CAE847197 DURING LANDING, TRANSMISSION LIGHT ILLUMINATED AS AIRCRAFT WAS LANDING ON EC 195, CHECKED CHIP PLUGS, FOUND NORMAL FUZZ C/W 30 MINUTE GROUND RUN, LEAK CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20031118000232003111800023NM 2003 11 18 AWXA200301138 120030904A5313BAC1498141 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 26 RT AT BS 500B+8. MAINTENANCE FOUND CORROSION DAMAGE BEYOND LIMITS WITH 100 PERCENT MATERIAL LOSS; CUT OUT A 14 INCH SECTION OF STRINGER 26 RT AT BS 500B+8; FABRICATED A HAT SECTION; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-03 PG 6 FIG 201. 2L72 4F RTA16WE 20040112001952004011200195EU 2004 1 12 2003UALA00954 120031213A5520 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT ELEVATOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29406UA 454 LEFT ELEVATOR MR55501-006 HAD 2 AREAS OF WATER INGRESS FOUND DURING ACP OF COA 40535. ONE ON THE UPPER SURFACE 2.3 BY 1.4 INCH, 154 INCHES FROM THE I/B EDGE, AND 3.5 INCHES FROM THE T/E. ONE ON THE LWR SURFACE 2.9 BY 1.9 INCH, 139 INCHES FROM THE I/B EDGE AND 3.5 INCHES FROM THE T/E. MAJOR REPAIR ACCOMPLISHED. REPAIRS ACP PER SRM 55-21-11 REP 5E, PG 226, FIG 205 SHEET 3. 2L72 4F4 FRTA28NM E40NE 20040113002462004011300246NM 2004 1 13 QXEA200301491 120031122A5420 BRACKET DHAV DHC8 DHC8202 2809007NM LT NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- LT NACELLE WHEEL WELL TOP OB GRAVEL GUARD BRACKET IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-40-11. 2H72 4T RTA13NM 20040114001542004011400154NM 2004 1 14 03FDEA02009 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM LT TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 N0304 LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 3 IB CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031124001032003112400103WP 2003 11 24 DHL2003805550 120030728A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 778.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO N/R 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20040311000282004031100028NM 2004 3 11 ASAA0310255 120030327A53306546882 SKIN PANEL BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN PANEL AT BS 1088, WATERLINE 220 GOUGED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040114001972004011400197NM 2004 1 14 MASA200300411 120031015A2910 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007NM HYD SYSTEM CRACKED A MASAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW07455YV 455 PHX-GJT A/C LOST HYD SYS 1 IN-FLIGHT. MECHANIC FOUND A CRACKED HYDRAULIC LINE IN THE WHEEL WELL. LINE REPLACED AND SYSTEM FLUSHED. A/C RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000062003121500006NM 2003 12 15 AWXA200301442 120031106A5320693535214 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND IN TIE CLIP AT BS 639, STR 4 RT. MAINTENANCE REMOVED CRACKED TIE CLIP AT BS 639, STR 4 RT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW SRM 51-40-02 PG 1, 38 & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031219001312003121900131NM 2003 12 19 03FDEA02112 120031128A5754 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. LT WING OUTBD FLAP INBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031219001632003121900163NM 2003 12 19 03FDEA02130 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. REMOVED AS PER EA 1-5750-73351, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031222000442003122200044EA 2003 12 22 COMA0360530 120031207A5311601R53055K2 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01721CA 7259 CRACK NOTED AT FS 718.00 RIGHT HAND DOUBLER BETWEEN STRINGER 10 - 12. REPAIRED PER EO 53-027 AND SERVICE BULLETIN 601R-53-055 PE. 2L72 4F RTA21EA 20031218000832003121800083NM 2003 12 18 2003UALA00866 120031118A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29197UA 26901 EMERGENCY EXIT LIGHTS, FLOOR LIGHT DAMAGED AT 17B. SECURED LIGHTS. 2L74 4F4 FRTA20WE E24NE 20031222001052003122200105NM 2003 12 22 USAA030222 120031104A5313 STRINGER BOEING737 7373B7 1384580NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48142 23319 FOUND STRINGER CORRODED 6 INCHES, STRINGER 27R BETWEEN STRINGER TIE BS 360 AND BS 366. CORROSION LEVEL 1, TASK NR C53-202-01. ACCOMPLISHED REPAIR IAW SRM 53-00-03 FIG 201, WITH MINOR DEVIATION GRANTED BY EA 77108. (M) 2L72 4F RTA16WE 20030623000662003062300066EA 2003 6 23 ASOA03213 120030517A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 280 ENTRY TO THE COCKPIT SECTION WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOORBEAM AT FS 280 ENTRY TO THE COCKPIT SECTION IAW ASA O600-53-0052. (M) 2L72 4F RTA21EA 20030630000302003063000030NM 2003 6 30 AWXA200300605 120030528A3350900835A BATTERY BOEING737 737277 1384570NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING 8-DAY CHECK THE EMERGENCY EXIT LIGHT ABOVE THE R-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT EMERGENCY EXIT LIGHT ABOVE THE R-2 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030714001552003071400155 2003 7 14 BAQA087928 420030707A3160 CONTROL PANEL BOLKMS117 BK117B2 5626013EU ANNUNCIATOR MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03296GL 0037 7222 ANNUNCIATOR PANEL INOPERATIVE. MASTER CAUTION WILL NOT EXTINGUISH UNLESS ALL 5 SEGMENTS ARE OUT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20030707000562003070700056WP 2003 7 7 AALA20030628 120030602A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21236AA 49251 FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 7D INOPERATIVE. REPLACED AFT EMERGENCY EXIT PATH LIGHT SOCKETS AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030711001152003071100115 2003 7 11 250TR0020 420030627A22104084042911 COUPLER BOEING737 7372K5 138448XNM YAW DAMPER FAILED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 YAW DAMPER INOPERATIVE. REPLACED YAW CAMPER COUPLER PER MM 22-12-01. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20030711000992003071100099EA 2003 7 11 COMA0360297 120030625A325016900107 ECU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01805CA1724 7354 FLIGHT 5506 NWS INOP CAUTION MESSAGE. REPLACED THE NWS ECU. 2L72 4F RTA21EA 20030711000862003071100086NM 2003 7 11 CALA0300335 120030625A323065448105 UPLOCK BOEING737 7373T0 1384582NM RT MLG INOPERATIVE A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW27173094737711790 23360 THE RT MLG FAILED TO EXTEND ON FIRST ATTEMPT WHILE ON APPROACH TO IAH. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE RT MLG RED WARNING LIGHT. A TOWER FLY-BY CONFIRMED THAT THE GEAR WAS NOT EXTENDED. THE LANDING GEAR WAS EXTENDED MANUALLY, CREW RECEIVED THREE GREEN GEAR INDICATION LIGHTS, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAILURE. THE RT MLG UPLOCK ACTUATOR AND RT MLG MODULAR PACKAGE WERE REPLACED IAW MM 32-32-44 AND 32-32-61 RESPECTIVELY. 2L72 4F RTA16WE 20030717000662003071700066SW 2003 7 17 HEEA088059 120030702A6320212040001141FM GEARBOX BELL 212 212 1181420SW MAIN ROTOR MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033131S14495 30953 MAIN ROTOR TRANSMISSION CHIP LIGHT ILLUMINATED. REPLACED WITH SERVICEABLE PART. 1G71 4U H4SW 20030115001072003011500107NM 2003 1 15 03FDEA00007 120030108A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 DENT IN FRAME, BS 950C STR 26L. REPAIR FRAME IAW SRM. 2L73 4F4 FRTA3WE E2EA 20030115001492003011500149EU 2003 1 15 ERAA082935 120030102A642010531714 ROTOR HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01130EH13185 558 TAIL ROTOR HAS WORN PITCH CHANGE BUSHINGS. BLADE PAINT IS ERODED, 2 RINGS WARPED, 1 SLEEVE CORRODED, HARDWARE CORRODED. ACTION TAKEN: DISASSEMBLED, CLEANED, & INSPECTED. REPLACED INNER SLEEVE BUSHINGS, GRIP TEFLON BUSHINGS, RINGS, GASKETS & 1 SPACER. COMPLIED WITH 1200 HR & 2400 HR / 6 YEAR INSPECTIONS ON TAIL ROTOR. 300 HR & 2400 HR BLADE INSPECTIONS DONE BY AEC. REASSEMBLED WITH NEW NUTS AND WASHERS, TORQUED & SAFETY WIRED AS REQUIRED. INSTALLED 2 SERVICEABLE BLADES AND STATIC BALANCED. INSPECTED AND A REPAIRED IAW BO-105 REM 301, MM CH 33,34, & 107. 1G72 3U H3EU 20030127000452003012700045 2003 1 27 HEEA083622 420030114A345713824120234 GPS BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 GPS RECEIVER MEMORY WILL NOT RETAIN WAYPOINTS. FOUND BATTERY VOLTAGE GOOD. REPLACED BUTTONS AND REPAINTED FACEPLATE. BENCH CHECK GOOD. 1G71 3U O H2SW 20030128002382003012800238SW 2003 1 28 HEEA083888 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030410002472003041000247NM 2003 4 10 F3LA200300029 120030125A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT SUPPORT CHANNEL CORRODED AT LBBL 8.10, STA. 772. FABRICATED AND INSTALLED REPAIR PART PER SRM 53-60-53, 53-00-53, FIG 202, AND SOPM 20-41-02. 2L72 4F RTA16WE 20030212000442003021200044SO 2003 2 12 C2XA03CL037 120030210A3243211118 SHUTTLE VALVE EMB 145 EMB145LR 3260212SO #4 BRAKE LEAKING A C2XAB EMER. DESCENT K FLUID LOSS CLCLIMB 1 SW2715912 145439 CLE FLIGHT#2968 THE CREW REPORTED A HYDRAULIC SYSTEM #1 FAIL IN FLIGHT.LOST HYDRAULIC FLUID ON THE #1 SYSTEM.THE CREW LANDED IN MSP WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 AND #4 BRAKE SHUTTLE VALVES.OPERATIONAL CHECKS WERE GOOD.P/N #1 VALVE 211-118 S/N 1479 2L72 4T RTT00011AT 20030213000832003021300083NM 2003 2 13 375PA0010 120030210A3350 BATTERY PACK BOEING737 737317 138447PNM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 Two sections of emergency floor lighting inop. Battery pack low Rt. side. After charging battery pack, Ops check normal. 2L72 4F RTA16WE 20030214000192003021400019NM 2003 2 14 2003FA0000146 120030107A2761654494710 HOUSING BOEING737 737 UTILSYSNM ACTUATOR CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 62208 3393 HOUSING CRACKED AROUND THE SHOULDER, ON THE INSIDE DIAMETER. 2L72 4F RTA16WE 20030214000692003021400069NE 2003 2 14 ABXA030027 220030109A72618D1467 PRESSURE SWITCH BOEING767 767231 1385131NM PWA JT8 JT8D* NE ENGINE OIL DEFECTIVE A ABXAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL23702AX1721 22566 709644 LT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. AFTER ENGINE SHUTDOWN, MESSAGE DISAPPEARED. NOTE: LT ENGINE SHUTDOWN, (0) OIL PRESSURE LAST 5 MINUTES OF FLT. REMOVED AND REPLACED THE NR 1 ENGINE MAIN OIL FILTER AND THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH IAW MM. LEAK AND OPS CHECKED GOOD. 2L72 4F4 FRTA1NM E2EA 20030218002062003021800206NM 2003 2 18 SWAA030327 120030209A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 500D + 3 AT STR 12R AND BS 773 AT STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030218002132003021800213NM 2003 2 18 SWAA030305 120030209A335015AT17 SWITCH BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED RON, FOUND EMERGENCY LIGHTS ILLUMINATING WHEN OVERHEAD SWITCH IS ARMED. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL SWITCH PER MM. 2L72 4F RTA16WE 20030220001202003022000120NM 2003 2 20 QXEA0300116 120030122A2120 ODOR BOMBDRDHC8 DHC8401 1390041NM CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09404QX 4046 SEA-BOTH FLIGHT ATTENDANTS REPORT HAZE AND SMELL IN CABIN AND BURNING EYES. APU ON CABIN DUCT AND FC DUCT TEMPERATURES BELOW 30 DEGREES. GROUND RAN APU FOR SEVERAL HOURS. CYCLED BLEED AIR UP AND DOWN SEVERAL TIMES. NO HAZE OR SMELL DETECTED. NO OTHER FAULTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030221000882003022100088NM 2003 2 21 CALA0300059 120030219A5320 SKIN BOEING737 737524 1384721NM STA 807 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0946625 27529 INSPECTION FOUND A 1.5" CRACK IN FUSELAGE SKIN BELOW AFT CARGO PIT THRESHOLD AT STA 807, S26R-S27R. THE SKIN WAS REPAIRED IAW ECRA 5330-03214. 2L72 4F RTA16WE 20030223000082003022300008SO 2003 2 23 C2XA03SH018 120030222A530014525994001 CROSSBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND AND CENTER FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030224001452003022400145NM 2003 2 24 AWXA200300196 120030216A5320146N5416 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON NUT PLATES OF FLOOR SUPPORT BS 1330, LBL 11. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED AREA ON FLOOR SUPPORT BS 1330, LBL 11; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-2, & 4-6. 2L72 4F RTA2NM 20030303000562003030300056SW 2003 3 3 HEEA084511 120030214A2910232A48T CHECK VALVE BELL 412 412 1182202SW HYD SYSTEM CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 HYDRAULIC SYSTEM CHECK VALVE IS CRACKED. SCRAPPED. 1G72 4U H4SW 20030304000612003030400061SW 2003 3 4 HEEA084592 120030214A6230412010406115 LINK BELL 412 412 1182202SW HUB AND SLEEVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z4058 36019 HUB AND SLEEVE ASSY HAS A WORN LINK. REPAIRED. 1G72 4U H4SW 20030313001692003031300169EU 2003 3 13 AALA20030125 120030130A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114077 612 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 6G INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 6G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030313002172003031300217NM 2003 3 13 QXEA0300191 120030121A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - SKIN PROTRUSION AT STATION 205.000 BETWEEN 30L AND 31L. REPAIRED IAW RD 8-53-2181. 2H72 4T RTA13NM 20030121003232003012100323 2003 1 21 HEEA083374 420030109A34215040017901 INDICATOR BELL 206 206L3 1182108SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 ATTITUDE INDICATOR WOULD NOT CAGE. REPAIRED. 1G71 3U H2SW 20030314001132003031400113NM 2003 3 14 SWAA030556 120030310A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 312 ABOVE STR 18R, BS 400 ABOVE STR 17L & BS 747 BELOW STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030317000942003031700094NM 2003 3 17 03FDEA00255 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 15R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030317001262003031700126NM 2003 3 17 03FDEA00286 120030307A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 DENTED FRAME BS 1030 LBL 28 WL 150. REPAIRED DENTED FRAME IAW EA 7-5310-69419. 2L73 4F RTA3WE 20030318000782003031800078NM 2003 3 18 AMTA200300206 120030130A5510 SHIM BOEING737 73783N 13844HINM HORIZONTAL STAB DISLODGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11314TZ 30640 HORIZONTAL STABILIZER LEFT AFT SPAR INBOARD END HAS MIGRATING SHIM. COMPLIED WITH ER/A 737-55N-5076 SECTION 1. (M) 2L72 4F RTA16WE 20030320001002003032000100NM 2003 3 20 2003UALA00091 120030122A5411 FRAME 1206802 BOEING777 777222 1385219NM NR 2 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29791UA 26933 NR 2 PYLON SAILTAIL FRAME WAS CRACKED AT C-CHECK. MAJOR REPAIR ACCOMPLISHED. FRAME REPLACED. 2L72 4F RTT0001SE 20030320001312003032000131NM 2003 3 20 2003UALA00122 120030131A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 FRAME AT BODY STATION 727E STRINGER 9L AT SUPPORT RAIL CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030320001572003032000157WP 2003 3 20 AT0300007 120030319A52205910233 TAIL CONE DOUG DC9 DC932 3022066WP TAIL CONE INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15831AT 47674 TAIL CONE DID NOT RELEASE FROM AIRCRAFT, STEP 12.1.4, EO09-5350-29-E1476 REV B. CORRECTIVE ACTION: REMOVED AND REPLACED TAIL CONE REF MM 53-50. DROP CHECK GOOD. 2L72 4F A6WE 20030324001052003032400105EU 2003 3 24 AWXA200300096 120030130A2910D2901010200200 PIPE AIRBUS320 A320231 3930325EU ZONE 420 LEAKING A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28646AW 271 LAS - EMERGENCY LANDING - EN ROUTE FROM DFW TO LAS ON DECENT THE GREEN HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND CHAFED HYDRAULIC RETURN LINE IN LT ENGINE PYLON, REPLACED HYDRAULIC LINE LT PYLON. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP DUE TO POSSIBLE CAVITATION IAW AMM 29-11-51, PG. 401-412. 2L72 4F RTA28NM 20030326000732003032600073EU 2003 3 26 CA030207006 220030207A8530913220 CYLINDER DIAMONDA20 DA20A1 2990000GL ROTAX 912 ROTAX912F3 EU HOFMANHOV352HOV352F NE ENGINE DAMAGED W A UNSCHED LANDING DERINFLIGHT SEPARATION VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 CA (CAN) WHILE ESTABLISHED IN CRUISE FLIGHT A LOUD BANG WAS HEARD FOLLOWED BY SUBSTANTIAL ENGINE VIBRATION AND POWER LOSS. THE OIL PRESSURE GAUGE READ 0 PSI. THROTTLE WAS REDUCED TO IDLE AND A FORCED LANDINGWAS CARRIED OUT.THE PROPELLER STOPPED ROTATING SHORTLY AFTER LANDING. A COMPRESSION CHECK INDICATED EXCESSIVELY LOW COMPRESSIONS IN CYLINDERS NR 1 AND 3. BOTH TOP AND BOTTOM SPARK PLUGS FROM THE NR 1 CYLINDER SHOWED SIGNS OF IMPACT DAMAGE. 1L71 3O3 ONTTA4CH E00051EN5 CTP5BO 20030717000492003071700049SW 2003 7 17 HEEA088025 120030623A7120NAS6606D12 BOLT BELL 407 407 1182206SW ENGINE MOUNT CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03491PH 53386 ENGINE MOUNT BOLT CORRODED DUE TO INADEQUATE PROTECTION DURING MFG PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030418001502003041800150EU 2003 4 18 MALA030169 120030223A3411 PITOT LINE SAAB SF340 340B 7860101EU CONTAMINATED A MALAO OTHER J WARNING INDICATION DEDESCENT 1 GL15411XJ 340B411 DURING DESCENT DECLARED EMERGENCY ALL THREE AIRSPEED INDICATORS WENT TO ZERO, CAME BACK AFTER 10 MIN. IN DESCENT IN ICING CONDITIONS, CAPT AIRSPEED INDICATOR, STANDBY AIRSPEED INDICATOR AND FL'S AIRSPEED ALL BLED OFF INDICATED AIR SPEED UNTIL PEGGED AT ZERO. ALSO LOST FLIGHT DIRETOR, AND HAD RED FD FLAG ON CAPT SIDE. THERE WERE NO OTHER INSTRUMENT MANFUNCTIONS AND NO ASSOCIATED WARNING LIGHTS OR CHIMES WENT OFF. MX FOUND WATER IN NR 1, 2 AND STANDBY PITOT LINES. DRAINED AND PURGED ALL THREE SYS WITH NITROGEN. RUDDER LIMITER LIGHT IS ASSOCIATED WITH STBY AND NR 1 BEING DIFFERENT AT TIME OF PROBLEM. F/O SYS OPS CHECK GOOD IAW SF340MM CHAP 34. NR 1, 23 AND STBY PITOT/STATIC SYS OPS AND LEAK CHECK GOOD. 2L72 4T RTA52EU 20030423002022003042300202SO 2003 4 23 ZKG2003F00001 220030224A8530646320 CYLINDER PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360EB 17025SO CRANKCASE SEPARATED B ZKGREA ENGINE SHUTDOWN UNSCHED LANDING RKJPARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION CRCRUISE 1 NE054516F1362 347670340 233770R IN CRUSE FLIGHT ENGINE LOST POWER, OIL PRESSURE WAS DECREASING, PILOT SHUT ENGINE DOWN AND LANDED WITH NO TROUBLE UPON INSPECTION, FOUND NR 2 CYLINDER OFF OF CASE WITH ALL 8 STUDS (HOLDDOWN) BROKEN, FOUND CONNECTING ROD CAP MISSING FROM CONNECTING ROD. CAP JAMMED IN CASE AND CONNECTING ROD ALSO JAMMED IN CASE. COULD NOT REMOVE CYLINDER FROM PISTON ASSEMBLY. 1L72 3O3 O A7SO E9CE 20030801000372003080100037WP 2003 8 1 GTIA030522 120030619A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FORWARD CABIN FLOOR SUPPORT LBL 6 STATION 168.75 TO 205 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED SUPPORT. (M) 2L72 4F A6WE 20040226000232004022600023NM 2004 2 26 ASAA0240165 120030322A532065479575 INTERCOSTAL BOEING737 7374Q8 138447QNM FS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CRACKED INTERCOSTAL AT BS 787-794. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030828000292003082800029WP 2003 8 28 IXXA0300044O 120030619A7920 LINE DOUG DC8 DC871F 302199DWP OIL SYSTEM CRACKED A IXXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW11825BX840741024 45978 DURING FLIGHT FROM KSJC TO KTOL, NR 2 OIL PRESSURE LIGHT ILLUMINATED WITH 20 PSI OIL PRESSURE, TEMP 72 DEGREE C AND OIL QUANTITY 3 QUARTS. SHUT DOWN NR 2 ENGINE. CREW LANDED IN TOL WITHOUT INCIDENT. MAINTENANCE FOUND LINE AFT OF OIL PRESSURE TRANSMITTER CRACKED AT FLARE. MAINTENANCE REMOVED AND REPLACED LINE IN ACCORDANCE WITH DOUGLAS AIRCRAFT DC-8 MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD ON GROUND. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030829000592003082900059WP 2003 8 29 DHL2003801086 120030714A2611302314 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP CABIN WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01801DH 46033 NR 11 SMOKE DETECTOR MAIN DECK INOPERATIVE. PLACED NR 11 MAIN DECK SMOKE DETECTOR ON DMI 13539 AS PER MEL 26-6-1. REF DMI 13539 MAIN DECK SMOKE DETECTOR WOULD NOT TEST. REMOVED AND REPLACED NR 11 SMOKE DETECTOR PER M/M 26-10-0. OPS CHECKED GOOD. THIS CLEARS DMI 13539. PLACARD REMOVED. 2L74 4F RT4A25 20030829001782003082900178NM 2003 8 29 SWAA031815 120030811A3350101073 LENS BOEING737 7375H4 138449DNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20030722000132003072200013NM 2003 7 22 2003F00441 120030312A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND INDICATION OF CRACK AT TERMINAL HOLE FITTING, BS 870. STOP DRILLED CRACK AT SECOND FASTENER ROW, SECOND FASTENER DOWN FROM STRINGER 9R ON BS 870 TERMINAL FITTING. FABRICATED AN EXTERNAL DOUBLER REPAIR. TREATED AND PRIMED DOUBLER AND AREA OF FUSELAGE SKIN AT STATION 870, COMMON TO RIGHT STATION 870, TERMINAL FITTING AT STRINGER 9. (M) 2L73 4F A3WE 20030723000022003072300002NM 2003 7 23 UIEA200300031 120030520A54147A1323111 SKIN BOEING747 747228F 1384895NM NR 2 PYLON DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15809MC 20887 DURING C-CHECK SERVICE IN SIAEC, NR 2 PYLON EXTERNAL SKIN FOUND WRINKLED AT INBOARD SIDE AREA OF PYLON VALVE FROM STATION 286 TO STATION 300, BETWEEN THE MID SPAR AND NR 5 STIFFENER. NDT AND CONDUCTIVITY CHECKS WERE ACCOMPLISHED AS PER CARDS A00043 AND A00044. PYLON EXTERNAL SKIN REPAIR CARRIED OUT AS PER TLS-SIN-03-063H, TLS-SIN-03-0053F, AND TLS-SIN-03-0002H. (M) 2L74 4F A20WE 20030725000222003072500022 2003 7 25 RAIA00305131 420030505A31607011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU NR 1 INOPERATIVE A RAIAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 CE03573HK8385 41092 SYMBOL GENERATOR NR 1 FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 SYMBOL GENERATOR. 2L72 4T RTA41NM 20030806001082003080600108SO 2003 8 6 C2XA03TY105 120030802A531514532628001 FLOORBEAM EMB 145 EMB145ER 3260211SO GALLEY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED 3C INSPECTION, THE LEFT HAND GALLEY FLOORBEAM WAS CORRODED AND PREVIOUS REPAIR WAS CORRODED. MAINTENANCE REMOVED THE OLD REPAIR, FAB FILLER AND ANGLE, ALODINED AND PRIMED NEW FAB PART. INSTALLED NEW PARTS IAW EMB 135/145 SRM 53-21-04, 05, 10 EMB 145 CPM 51-21-06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030903000702003090300070EU 2003 9 3 127461 120030716A3250 TILLER SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE NLG STEERING MALFUNCTIONED A UHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL17118SD 118 151 DRG936587 FLIGHT 4515 TTN-BED. DURING T/O ROLL AT ABOUT 60 KNOTS AFTER RELEASING THE NOSE STEER TILLER, THE A/C TURNED TO THE RIGHT. THE CREW CORRECTED WITH THE TILLER TO APPOX. 80 KNOTS. THE A/C AGAIN TURNED TO THE RIGHT AFTER RELEASING THE TILLER. THE CREW ABORTED THE TAKE-OFF AND RETURNED TO THE GATE. A/C TAKEN OUT OF SERVICE AT 1600(LT). TTN MX INSPECTED NOSE STEERING SYSTEM, DID NORMAL TAXI FUNCTION TEST,FOUND NO DEFECTS. A/C PERFORMED TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. A/C RETURNED TO SERVICE 7-16-03 AT 2120(LT) 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030904000542003090400054SO 2003 9 4 SWIA200312260 120030813A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM0715732 120195 CONTROL FAULT IN FLIGHT AND ON GROUND. ON GROUND: INBOARD'S FLASHING 5 BARS, INDICATOR SHOWING 8 DEGREES WITH FLAPS UP. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW 27-00-00. SN OFF 0279 2L72 4T RTA31SO 20030813000772003081300077NM 2003 8 13 UPS03440828 120030519A5314 BUSHING BOEING747 747200 1384847NM KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, A REPAIR BUSHING IS INSTALLED ON THE KEEL BEAM INTERIOR BATH TUB FITTING AT LT FWD BOLT HOLE & THE WALL THICKNESS OF THE BUSHING IS ONLY 0.020 INCH. REPAIR BUSHING REPLACED AS PER RS R53-49-35025 AND ENG'R/FILE NR 747 -53-20139. 2L74 4F RTA20WE 20030812000642003081200064SW 2003 8 12 HEEA088527 120030712A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW FLAP STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 FLAP ARM STICKS. IN SHOP REPAIR. 1G71 3U H2SW 20030725000242003072500024EU 2003 7 25 RAIO00305134 120030507A3397 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK 41040 EMERGENCY PATH LIGHTS INOP AT 2A. RECONNECT EMERGENCY PATH LIGHTING STRIP. 2L72 4T RTA41NM 20030725000422003072500042WP 2003 7 25 IXXA0300039O 120030530A3260 PROXIMITY SWITCH DOUG DC8 DC873F 302199FWP MLG LOOSE A IXXAO OTHER N FALSE WARNING CLCLIMB 1 SW11606AL896111364 46044 DURING TAKEOFF FROM KRFD TO KLRD SELECTED GEAR UP AND " DOORS NOT LATCHED" LIGHT REMAINED ILLUMINATED. ALT LIGHTS WERE OUT. TEST SWITCH SHOWED LEFT HAND DOOR AT FAULT. RAN CHECKLIST, CYCLED GEAR, BOTH THE ALTERNATE AND MAIN DOOR LIGHT WOULD NOT EXTINGISH. FLIGHT CONTINUED TO KLRD WITH AN UNEVENTFUL LANDING.MAINTENANCE FOUND LOOSE HARDWARE ON LEFT MAIN DOOR UPLATCH SWITCH. HARDWARE WAS RESECURED IN ACCORDANCE WITH DOUGLAS DC-8 MAINTENANCE MANUAL.OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20030729001182003072900118WP 2003 7 29 03FDEA01150 120030725A5720ARB21761 CLIP DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 LEFT WING LWR SPAR-TO-RIB FITTING IS CRACKED AT STA XORS 402 LWR SPAR S37. REMOVED CRACKED BUTTERFLY CLIP STA XORS 402 LWR SPAR S37 IAW SRM 51-33-01. INSTALLED NEW CLIP IAW SRM 51-33-01 SEALED IAW SRM 51-41-01. 2L73 4F A22WE 20030826001702003082600170SO 2003 8 26 SWIA200312113 120030617A3350 LAMP EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07189SW 120048 ROW 6A EMERGENCY LIGHT POD INOPERATIVE. RE-LAMPED ROW 6A EMERGENCY LIGHT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030909000252003090900025EA 2003 9 9 SWIA200312336 120030824A5220 SHAFT CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913SW 7597 CREW ESCAPE HATCH OUTER HANDLE HAS CORROSION ON INNER SHAFT. DISCOVERED DURING C-CHECK. CREW ESCAPE HATCH OUTER HANDLE REPLACED AS PER HARTWELL CMM 52-22-03. P/N: H3419-33 2L72 4F RTA21EA 20030910000062003091000006EU 2003 9 10 BAQA088677 120030731A6520AC67032 SERVO AEROSPAS355 AS355F2 8680812EU TAIL ROTOR LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03912KY3601 5500 TAIL ROTOR SERVO LEAKING AT SHAFT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20030911001762003091100176WP 2003 9 11 DHL2003873618 120030620A5347S2772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 MAIN CARGO COMPT NR 3 TRACK LUG WORN. (STA.1680.000 - 1695.000) CUT OUT NR 3 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED SPLICES IAW SRM 53-2-3 PG.49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030911002432003091100243WP 2003 9 11 DHL2003604599 120030527A5754 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING EXTENDED L/E INBD VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030563, ED-3312. REMOVED FASTENERS AND THE EXSISTING DOUBLER IAW SRM 51-1-21 PG 1. TRIMMED OUT THE ELONGATED HOLES SKIN AREA. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, A FILLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE FILLER AND INTERNAL DOUBLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER ON LT WING EXTENDED L/E INBD VANE, STA XS.247.000 USING NEW FASTENERS. 2L74 4F RT4A25 20030926000922003092600092NM 2003 9 26 03FDEA01379 120030808A5753ARC70551 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LT WING OUTBOARD FLAP VANE NR 3 FITTING FORWARD HOLE FOUND CORROSION. LT WING OUTBOARD FLAP VANE NR 3 FITTING FWD HOLE CARRIED OUT REPAIR AS IAW EA NR 1-5750-71792. 2L73 4F RTA22WE 20031001000252003100100025NM 2003 10 1 QXEA200301086 120030831A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 FIREWALL HAS A CRACK ALONG INBOARD SIDE OF EXHAUST APERATURE AT STATION YN12. REPAIRED IAW HORIZON AIR EA 2-54-180. 2H72 4T RTA13NM 20031001000672003100100067NM 2003 10 1 2003UALA00705 120030919A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29781UA 26945 AFT GALLEY EEL LIGHT RIGHT SIDE AT FLOOR INOP. REPLACED LIGHT ASSEMBLY. 2L72 4F4 FRTT0001SE E46NE 20030909001842003090900184NE 2003 9 9 ALGA088803 120030820A6320E6893672 PINION GEAR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL GEARBOX CORRODED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0331211705 CAG90801 760225 CAE890052S FOUND CORROSION AND RUST PITTING AT ROOT OF GEAR TEETH. REMOVED AND REPLACED. REQUEST WARRANTY CREDIT DUE TO LOW TIME. 1G72 3U3 U H1NE E1GL 20031003000012003100300001EU 2003 10 3 ASOA03426 120030908A33503011210 LIGHT AEROSPATR72 ATR72 EU FUSELAGE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SW21643AS2081 413 DURING A GROUND INSPECTION IN ATL, THE EMEGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031007000162003100700016NM 2003 10 7 AALA20030696 120030626A3350 LIGHT BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT STRIP FROM 4E-6E INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NROMAL OPERATION. (M) 2L72 4F RTA2NM 20031015000422003101500042EU 2003 10 15 ASOA03444 120030905A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING A C-CHECK IN BNA, THE LEFT AND RIGHT SEAT TRACKS AT FS 36 TO FS 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS AT FS 36 TO FS 39 IAW SRM 51-25-02. (M) 2H72 4T RTA53EU 20031020001592003102000159NM 2003 10 20 DL757030787 120030826A28226075504 PUMP BOEING757 757232 1384965NM FUEL SYSTEM FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27624DL2886028860 22914 DURING ROUTINE DISASSEMBLY OF A FAILED FUEL BOOST PUMP, SEVERE BEARING AND HOUSING WEAR WAS DISCOVERED, TO THE EXTENT THAT END CAP FAILURE WAS IMMINENT. ROTOR AND STATOR HAD CONTACTED EACH OTHER AND EVIDENCE OF HEAT WAS PRESENT. PUMP P/N 60-75504, S/N 048910657A. C/A NONE. PART WAS ALREADY REMOVED FROM AIRCRAFT AND IN REPAIR PROCESS. 2L72 4F RTA2NM 20031022001162003102200116NM 2003 10 22 JGV2003F00003 120030910A2810 FUEL TANK ISRAEL1125 1125 NM GARRTTATF3 ATF3* 29002WP CENTER WING LEAKING B JGVRO OTHER K FLUID LOSS NRNOT REPORTED 1 CE09500AJ 074 FUEL LEAKING INTO CABIN FROM CENTRAL TANK LOWER. INSUFFICIENT AMOUNT OF SEALANT APPLIED TO INTERIOR AND EXTERIOR PORTION OF FUEL TANK. LEAK FLOWED FORWARD AND AWAY FROM CABIN AREA DRAIN. FUEL FOUND UNDER FLOOR PANELS DURING INSPECTION. INSULATION ALSO SOAKED WITH FUEL. (CE09200304096) 2L72 4F4 FRTA16NM E7WE 20031023000832003102300083NM 2003 10 23 F3LA200300147 120030924A5347 MOUNT BOEING737 73736E 138443ANM GE CFM56 CFM56* 13802NE LAVATORY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED LAV MOUNT AT STA. 947.5, LBL 25, CORRODED. REPLACED LAV MOUNT IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031027000772003102700077 2003 10 27 MALA030427 420030906A34406228973001 ANTENNA BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE TCAS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15523XJ E2348 ON THE FIRST FLIGHT OF THE DAY OUTBOUND ON FLIGHT 3529 TCAS FAILED. AIR RETURN TO MSP. MAINTENANCE REMOVED & REPLACED LOWER TCAS ANT. P/N OFF/ON 622-8973-001. S/N OFF/7796. S/N ON 11P9T. TCAS OP CHECKS GOOD IAW RJ-85 M/M CHAP 34. REMOVED FROM DMR. MXC NOTIFIED. 2H74 4F4 FRTA49EU E6NE 20031030001162003103000116NM 2003 10 30 03FDEA01636 120030924A2920861555 PUMP DOUG MD11 MD11 3023602NM ZONE 100 BURNED A FDEAO OTHER A FLAME/FIRE NRNOT REPORTED 1 SO25603FE 48459 HYD AUXILIARY PUMP NR 2 ELECTRICAL CONNECTOR FOUND ELECTRICALLY SHORTED AND ARCING DAMAGED. AUX ELEC PUMP REMOVED AND REPLACED AS PER AMM 29-21-01. ELECTRICAL: REMOVED AND REPLACED B1-624 RCCB AS PER STANDARD WIRING PRACTICE. REMOVED AND REPLACED NR 2 HYD PUMP ELECT CONNECTOR AS PER STANDARD WIRING PRACTICE. NR 2 PUMP ELECT WIRING INSULATION CHECKED, FOUND SATISFACTORY. PUMP OPS CHECK CARRIED OUT AS PER MM 29-21-01-5, FOUND SATISFACTORY. 2L73 4F RTA22WE 20031030001112003103000111NM 2003 10 30 03FDEA01554 120030916A5320AFA77751 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 UPON REMOVAL OF TRANSVERSE SPLICE. FOUND CORROSION ON AFT STRINGER UNDER REMOVED SPLICE. CTR CARGO STA 1541 S48R STRINGER CORROSION REPAIRED AS PER SRM 53-00-01 FIG 3 VOL 1. 2L73 4F RTA22WE 20031103000502003110300050WP 2003 11 3 03FDEA01693 120031003A5753 BRACKET DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 RT IB FLAP TRACK MOUNT BRACKETS CORRODED ON FACES (3 OF 4 ). CLOSING ACTION ON 10/02/03.PN. N/R N01283. REMOVED CORRODED BRACKETS, FOUND WITHIN LIMITS IAW SRM 51-21-01, FAB NEW BUSHUINGS ON TRAVLER T2/370669 IAW EA8-5750-73196, INSTALLED NEW BUSHINGS IAW E.A.8-5750-73196. REWORKED AREAS ON N/R S00010. IAW E.A. 8-5750-73196. 2L73 4F A22WE 20031107000272003110700027NM 2003 11 7 QXEA200301391 120031030A2751 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM FLAP SYSTEM ACTIVATED A QXEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION APAPPROACH 1 NM09403QX 4037 SEA- ON FLIGHT NUMBER 2368, FLAP POWER CAUTION MESSAGE ILLUMINATED AFTER SELECTED FLAPS 15 DEGREES. ACCOMPLISHED EMERGENCY CHECKLIST AFTER LANDING AND PER CHECKLIST PULLED FLAP CONTROL CIRCUIT BREAKER. CAUTION LIGHT DISAPPEARED. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM. NO DEFECTS NOTED. CAUTION LIGHT DID NOT ILLUMINATE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031119000792003111900079WP 2003 11 19 MWEA030416 120031013A532099578283 THRESHOLD DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 FORWARD GALLEY DOOR THRESHOLD IS CORRODED AT STATION 160-200. -- FABRICATED AND INSTALLED FILLER AND PANEL. 2L72 4F A6WE 20040113001082004011300108 2004 1 13 BAQA091471 420031107A2220501113204 COMPUTER LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP MACH TRIM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 11343 092 MACH TRIM COMPUTER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 12/9/03 2L72 4F4 F A10CE E6WE 20040113001102004011300110EU 2004 1 13 BAQA091151 120031114A6210L621M1010054 BLADE UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE MAIN ROTOR WILL NOT BALANCEB BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME793 0144 MAIN ROTOR BLADE WILL NOT BALANCE. REPLACED WITH CANNED UNIT FROM A/C. 1G72 3U3 U H88EU E34NE 20040113002512004011300251NM 2004 1 13 QXEA200301498 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX- NR 5 SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL 9 INCHES FORWARD OF X510. REPAIRED IAW DHC-8 SRM 51-20-16, 51-00-06 AND RD 8-53-1339. 2H72 4T RTA13NM 20031218000792003121800079NM 2003 12 18 2003UALA00860 120031116A3350 COVER BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29561UA 26661 EMERGENCY EXIT LIGHTS SWITCH IN COCKPIT WON'T ARM SWITCH WHEN COVER IS CLOSED. REPLACED BROKEN SWITCH COVER. EMERGENCY LIGHTS TEST OK. 2L72 4F4 FRTA2NM E17NE 20031219000672003121900067WP 2003 12 19 CALA0300701 120031206A5311 BELTFRAME DOUG DC9 DC982 3022082WP STA CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716806 49260 INSPECTION FOUND CANTED BELTFRAME CRACKED AT L2L, 3L, 2R, AND 3R, STA 1416. THE CRACKS WERE .25 INCH TO 4 INCHES LONG. THE CANTED BELTFRAME SECTION FROM L15R TO L15L WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2L72 4F A6WE 20031229001502003122900150SO 2003 12 29 C2XA03CL199 120031216A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716919 145393 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 12B/C WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BULB AT ROW 12 B/C. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20031229000302003122900030SO 2003 12 29 LR7A03091 120031121A1430 FASTENER LKHEED382 382G 526414USO LOOSE A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND LOOSE FASTENERS FS 345E-245 FUSELAGE SKIN, LBL 30, WL 230-285. REPLACED 60 EA RIVETS IAW AC 43.13-1B AND SB 382-53-42. NR 2067. 2H74 4T A1SO 20031007000452003100700045EU 2003 10 7 2003F00594 120030808A7712G555674 TRANSDUCER BOLKMS117 BK117B2 5626013EU NR 2 ENGINE FAILED A A1URO OTHER N FALSE WARNING CLCLIMB 1 CE03550SL 7139 APPROXIMATELY 305 MINUTES AFTER TAKEOFF, NR 2 TORQUE INDICATOR FAILED. ALL OTHER INSTRUMENTS WERE INDICATING NORMAL. REMOVED AND REPLACED PRESSURE TRANSDUCER. OPERATION CHECKS GOOD. (M) 1G72 3U NCH13EU 20031014001092003101400109NM 2003 10 14 SWAA032134 120030922A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) STR 8R, BS 500 AND BS 500D. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031231001152003123100115NM 2003 12 31 TSAA0353037 120030209A53306546529 SKIN BOEING737 7372Y5 1384554NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13810AL 24031 NINE RIVETS ON STRINGER 16R SHOW SIGNS OF STRESS CRACKS EMANATING FROM THE FASTENER HOLES. REMOVED RIVETS, OVERSIZED HOLES BY 1/16, HFEC VERIFIED FASTENER HOLES CRACK FREE. FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS PER SRM 53-30-3, FIGURE 17. REPAIR COMPLETED IAW SRM AND ECO 3340. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4U RTA16WE 20040105000062004010500006NM 2004 1 5 DL757030997 120031111A2422S282T00410 STATIC INVERTER BOEING757 757232 1384965NM FWD E/E BAY SHORTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27692DL 29724 REPLACED STATIC INVERTER FOR SMOKING. 2L72 4F RTA2NM 20031204000392003120400039WP 2003 12 4 AALA20031086 120030929A33503015643 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21580AA 53157 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE FORWARD GALLEY LOCATION. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031203001692003120300169 2003 12 3 GTIA030896 420031107A2565 GIRT BAR DOUG DC9 DC982 3022082WP L1 SLIDE PACK DIRTY A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 ORD - FLT 1525A - L1 SLIDE PACK SLIPS OUT OF PLACE WHEN SLIDE IS DISARMED. DETERMINED GIRT BAR FALLING OUT OF LOCKS. CLEANED AND LUBED GIRT BAR LOCKS, OPS CHECK NORMAL. ALSO, ADJ GIRT BAR DISENGAGE HOLDER. (M) 2L72 4F A6WE 20031222001222003122200122WP 2003 12 22 GTIA030950 120031107A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND PAX CABIN CENTER FLOOR PANEL STATION 1309 TO 1338 HAS DAMAGES ON EDGE, SOFT, SEVERAL INSERTS BROKEN OUT. FABRICATED NEW CENTER FLOOR PANEL. (M) 2L72 4F RTA6WE 20031231000292003123100029NM 2003 12 31 TSAA0332193 120031202A323010613378 CONTROL CABLE BOEING737 737230 1384401NM RT MLG OUT OF ADJUST A TSAAO OTHER J WARNING INDICATION CLCLIMB 1 WP13818AL 22117 AFTER TAEKOFF, DURING CLIM THE LANDING GEAR CONTROL LEVER WOULD NOT MOVE UP AND SIMULTANEOUSLY THE TAKEOFF WARNING HORN SOUNDED WHEN THE FLAPS WERE RETRACTED. PERFORMED GROUND SPOILER INTERLOCK VALVE CONTROL CABLE ADJUSTMENT AND TEST IAW MM 27-62-51. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031015000652003101500065 2003 10 15 USAASB03147 420030823A22004051601932 CONTROL PANEL BOEING737 7374B7 1384702NM COCKPIT INOPERATIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19783AU 25022 THE MODE CONTROL PANEL BECAME INOPERATIVE. CREW WAS UNABLE TO ACTIVATE FLIGHT DIRECTORS. FLIGHT DIVERTED TO CAE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MODE CONTROL PANEL. FUNCTIONAL CHECK NORMAL PER MM. (M) 2L72 4F RTA16WE 20040106002302004010600230WP 2004 1 6 GTIA031036 120031029A5310 STOP FITTING DOUG DC9 DC983 3022083WP FUSELAGE OUT OF LIMITS A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - AFT CARGO DOOR JAMB SURROUNDING HAS 9 SET SCREWS CORRODED. DOOR STOP FITTING ON AFT SIDE OF AFT CARGO DOOR FRAME IS OUT OF LIMITS. INSTALLED NEW DOOR STOP FITTING. (M) 2L72 4F RTA6WE 20031126001202003112600120SO 2003 11 26 C2XA03BT100 120031022A2611 SMOKE DETECTOR EMB 145 EMB145XR SO CARGO BAY MALFUNCTIONED A C2XAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2711119 145677 CREW REPORTED AFTER TAKEOFF THROUGH 5000 FEET, BAGGAGE FIRE WARNING CAME ON, BLEW BOTH BOTTLES, AND AIR RETURNED TO DAY. MEL'D BAGGAGE COMPARTMENT AND CONTINUED FLIGHT TO EWR. EWR MAINTENANCE INSPECTED BAGGAGE COMPARTMENT FOR EVIDENCE OF SMOKE OR FIRE. NONE NOTED. PERFORMED TEST OF BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM, CHECKED GOOD. REMOVED AND REPLACED BOTH FIRE EXTINGUISHER BOTTLES (PART NUMBER: 33700027-1) IAW EMB145 MM 26-23-01. CLEARED MEL AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F RT 20031202000792003120200079NM 2003 12 2 USAA030214 120031017A5312 STIFFENER BOEING737 737301 1384611NM BULKHEAD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US48679 23937 FOUND RADIAL STIFFENER CORRODED 2 INCH BY 1 INCH AREA, AFT PRESS BULKHEAD STATION 1016 AT BL 0. INSTALLED SPLICE SECTION AND REPAIR DOUBLERS PER EO 5302V112 AND BOEING DWG 65C28106 AND EA 77188. (M) 2L72 4F RTA16WE 20031203001142003120300114EA 2003 12 3 ASOA03553 120031101A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11926EV 7843 DURING CLIMB-OUT, WHEN FLAPS WERE SELECTED TO ZERO DEGREES, THEY STAYED AT EIGHT DEGREES AND THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW LEVELED OFF THE AIRCRAFT AND MAINTAINED A SPEED OF 200 KNOTS WHILE COMPLYING WITH THE QRH. UPON NOTIFYING THE FLIGHT ATTENDANT AND PASSENGERS OF THE INTENT TO RETURN TO DFW, THE FLIGHT ATTENDANT REPORTED A BURNING SMELL IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT. OPERATIONAL AND GROUND TEST WERE NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040122000092004012200009EA 2004 1 22 SWIA200312729 120031224A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52 2L72 4F RTA21EA 20040126000432004012600043EU 2004 1 26 BAQA091233 120031121A6420105317261 LAMINATE STOP BOLKMS117 BK117A1 5626010EU TAIL ROTOR CORRODED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 TEFFLON WORN OUT, CORROSION. 1G72 3U H13EU 20031209002462003120900246NM 2003 12 9 UPS03241527 120031011A5340 FITTING BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, RT 930 FITTING HS SUSPECT CRACK AT AFT O/B FLANGE AT FLOOR LEVEL. REPAIR & REPLACEMENT OF BS 930 FITTING & ASSOCIATED STURCTURAL ITEMS CARRIED OUT IAW SMRO EO 2003-055-001 UPS ENGINEERING FILE 727-53-20 130. 2L73 4F A3WE 20030916001462003091600146WP 2003 9 16 ARWA20030507 120030527A5320 ANGLE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT AFT DOOR SUPPORT ANGLE WITH CRACK; STATION 1420. REMOVED ANGLE IAW DPS 3.67-27, FABRICATED NEW ANGLE IAW DPS 3.69-4, PRIMED NEW ANGLE IAW DC8 SRM 51- 1-8 AND INSTALLED ANGLE AIW DC8 SRM 51-1-21. 2L74 4F4 F 4A25 1E8 20030923000122003092300012EU 2003 9 23 0301593217 120030815A2433 TRU AIRBUS320 A320211 3930320EU NR 2 INOPERATIVE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01317US 197 WHILE AT CRUISE (LAX-MSP) RECEIVED TR2 (NR 2 TRANSFORMER RECTIFIER) FAULT MESSAGE AND NOTED ELECTRICAL BURNING ODOR WITH NO SMOKE VISIBLE. DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM. REPLACED NBR 2 TRANSFORMER RECTIFIER AND RELAY 7XX IAW AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040128001942004012800194NM 2004 1 28 P5CA0401019 120031225A3610 DUCT BOEING747 7472U3B 1384846NM CARGO BAY LEAKING A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23923FT 22769 BLEED AIR LEAK, APU SUPPLY DUCT AFT OF BULK CARGO COMPARTMENT. ITEM TRANSFERRED TO DMI 32017 AND MEL 49-01-01 PER DDPG. 2L74 4F RTA20WE 20040129000122004012900012EA 2004 1 29 MASA200300524 120031231A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 ASH FLT 6019 PHX-FAT, FLOOR EMERGENCY LIGHT INOP IN CABIN. MX RESECURED LIGHTS, OPS CHECK GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040130000282004013000028 2004 1 30 SWAA032821 420031228A256561621469 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031208000782003120800078NM 2003 12 8 SWAA032226 120031008A53206558280 ATTACH ANGLE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN ATTACH ANGLE CRACKED AT BS 360, BETWEEN STR 14R AND STR 15R. REPAIRED ATTACH ANGLE PER SRM. 2L72 4F RTA16WE 20031210001832003121000183NM 2003 12 10 CALA0300635 120031020A5542 SKIN BOEING737 7373T0 1384582NM RUDDER DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 THE RUDDER LT SIDE BONDED SKIN ASSEMBLY WAS FOUND DAMAGED AT APPROXIMATELY R STA 172. THE DAMAGE WAS REMOVED BY TAPER SANDING. A REPAIR WAS INSTALLED IAW ECRA 5540-01170. 2L72 4F RTA16WE 20030918000732003091800073EU 2003 9 18 U30A200300023 120030731A2611 SMOKE DETECTOR AIRBUS320 A320212 3930322EU CARGO BAY FAULTY A U30AK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 EA17265AV 427 ON FLT 300, BWI-CUN, DURING TAXI IN, ECAM MESSAGE FOR SMOKE LAV AND CARGO DETECTOR FAULTED. MAINTENANCE IN CUN RESET CIRCUIT BREAKER AND PERFORMED OPS CHECK IAW AMM 26-17-00-710-01 WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. UPON RETURN TO BWI, MAINTENANCE INSPECTED LAV"D" SMOKE DETECTOR DUCTING AND FOUND BLOCKAGE REMOVED BLOCKAGE FROM VACUUM RESTRICTOR AND VACUUM WAS RESTORED. OPS CHECKED OK. 2L72 4F RTA28NM 20030923001292003092300129EU 2003 9 23 189201 120030825A7600 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE COCKPIT ILLUMINATED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 407 DRG409890 ON 08/25/03, APPROX. 1143(UTC), FLT 4500, AIRCRAFT ABORTED TAKEOFF WHEN THE FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FIELD. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040127001842004012700184NM 2004 1 27 ASAA0310197 120030321A5313BAC1498162 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRINGER 19R AT BODY STATION 727B CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2L72 4F RTA16WE 20040128000572004012800057NM 2004 1 28 AWXA200301626 120031207A532065525471 PAN BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT LAVATORY MAIN DECK DRIP PAN AT BS 1018, LBL 14. MAINTENANCE REMOVED CORRODED LT AFT LAVATORY MAIN DECK DRIP PAN AT BS 1018, LBL 14; FABRICATED A NEW REPLACEMENT DRIP PAN PER DWG 65-52547; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12 & 101, PG 1 & 110. 2L72 4F RTA16WE 20040127002242004012700224WP 2004 1 27 ASAA0380643 120031015A5330593666751 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FUSELAGE SKIN IS CORRODED UNDER FRAME AT STATION 1287 AT 28R. REPLACED DAMAGED SECTION PER SRM 53-04. (M) 2L72 4F A6WE 20040129000442004012900044EU 2004 1 29 MALA030602 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEAT 15F FRAMES CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAME 15F IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF NR 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040205000382004020500038CE 2004 2 5 TIM2003F00002 120031105A57115012007H3 FITTING BEECH 99 B99 1154004CE PWA PT6 PT6* 52043EA RT MAIN SPAR CRACKED E TIMAO OTHER O OTHER NRNOT REPORTED 1 NM07950AA U159 FITTING FOUND TO BE CRACKED DURING STRUCTURAL INSPECTION. (CNTRL NR 82) 1L72 3T3 T A14CE E2NE 20040205001042004020500104 2004 2 5 UO22003F00011 420031119A830030602732 SHAFT LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312 01518WP PLANETARY GEAR UNSERVICEABLE B UO2RK NONE O OTHER ININSP/MAINT 1 GL19158PH2359 047 P111209 ENGINE WAS INSPECTED DUE TO BAD SOAP. DURING INSPECTION OF FAN GEARBOX AREA 1 EA PLANETARY GEARSHAFT WAS FOUND SHEARED THROUGH AT LARGE BEARING. NO OTHER PARTS WERE EFFECTED. 2L72 4F4 FRTT00008WIE6WE 20040210001252004021000125CE 2004 2 10 CED2003F00000 120031115A2821WF334761 FILTER LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE FUEL SYSTEM INOPERATIVE E CEDAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW05233CA 133 251397A ON NOV 20, 2003, THE AIRCRAFT EXPERIENCED LOW FUEL PRESSURE WARNING LIGHTS. UPON INVESTIGATION OF THE DISCREPANCY WE CHANGED THE FUEL FILTERS BECAUSE THE FELT SEAL HAD CONE UNGLUED AND CLOGGED THE FILTER. THE AIRCRAFT WAS IN FOR A INSPECTION OF THE 15 NOV 2003, AND THE FUEL FILTER WERE CHANGED DURING THIS INSPECTION. THE AIRCRAFT HAD ONLY FLOWN TWO LEGS OF A TRIP BEFORE THE PROBLEM OCCURRED. SPOKE WITH SEVERAL OTHER OPERATORS AND FOUND THAT THIS HAS OCCURRED TO TEM WHEN USING THIS SAME PN OR FILTER. 2L72 4J4 J A10CE 1E16 20040212000022004021200002 2004 2 12 56473 420031124A3418 WARNING HORN BEECH 1900 1900D 1154162CE STALL WARNING FALSE ACTIVATIONA AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07142YV UE142 STALL WARNING SOUNDED ON TAKE OFF ROLL. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. IAW HIGH SPEED TAXI CK/CND 2L72 4T RTA24CE 20040212001402004021200140NM 2004 2 12 DHL2003742520 120031121A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK DISCREPANCY AS FOLLOWS, NR 59977 FWD CARGO COMPARTMENT, CABIN SEAT TRACK AND SPLICE PARTS ARE CORRODED BETWEEN STA 680-700 RBL 24. REMOVED SPLICE OF SEAT TRACK BETWEEN STA 680 TO 700 RBL 24 IAW B-727 SRM 51-30-2. REMOVED LITE CORROSION OF SEAT TRACK BETWEEN STA 680 TO 700 RBL 24 WITH A MAT LOSS .002 INCH AREA FOUND TO BE WITHIN LIMITS IAW SRM 51-10-6 FIG 1. FABRICATED NEW SPLICE FROM MAT 7075-T6 .250 PO 9911344 DIM 6.75 X 2 INCH IAW B-727 SRM 53-10-5 FIG 1. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040217000612004021700061NM 2004 2 17 USAA030329 120031224A5320 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU 22205 CLT - FOUND ZEE ANGLE CORRODED, CABIN FLOOR LEVEL AT STATION 740, LBL 54. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-00. CORROSION LEVEL 1, TASK NR C53-231-02 AND C53-232-02. (M) 2L72 4F RTA2NM 20040401000172004040100017NM 2004 4 1 AALA20031172 120031021A33500201991020 LIGHT BOEING757 757223 1384957NM SEAT 29D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21183AN 29593 DFW - MAINTENANCE OBSERVED EMERGENCY LIGHTING INOPERATIVE AT SEAT 29D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030828000352003082800035CE 2003 8 28 NSVA20030027 120030620A2400 ELECTRICAL BOX BEECH 1900 1900D 1154162CE COCKPIT CONTAMINATED A NSVAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27191CJ UE19 SMOKE REPORTED COMING OUT OF CIRCUIT BREAKER PANEL RT SIDE. REMOVED PANEL AND FOUND WATER IN THE AREA. CLEANED OFF WATER AND INSPECTED AREA FOR SIGNS OF DAMAGE AND OVERHEATING, FOUND SATISFACTORY. 2L72 4T RTA24CE 20030829000942003082900094CE 2003 8 29 S2YA03006 120030209A3260 SQUAT SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A11 52043NE RIGHT DIRTY A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13831SK UE83 AFTER TAKEOFF OF FLIGHT 1007, THE GEAR INTRANSIT LIGHT ILLUMINATED WITH THE GEAR HANDLE UP AFTER, THE GEAR SHOULD HAVE RETRACTED. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT UPLOCK SWITCH. MECHANIC OPS CHECK THE SYSTEM FOUND NO DISCREPANCIES AND RETURN THE AIRCRAFT TO SERVICE. ON 2/11/03 AFTER TAKEOFF OF FLIGHT 1838, THE GEAR INTRANSIT LIGHT ILUMINATED WITH THE GEAR HANDLE UP AFTER THE GEAR SHOULD HAVE RETRACTED. THE CREW MADE AN AIR TURNBACK, MECHANIC INSPECTED THE AIRCRAFT AND CLEANED THE RIGH SQUAT SWITCH. MECHANIC OPS CHECK THE SYSTEM FOUND NO DISCREPANCIES AND RETURN THE AIRCRAFT TO SERVICE. 2L72 4T3 TRTA24CE E4EA 20030829001182003082900118NM 2003 8 29 SWAA031805A 120030811A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20030902000462003090200046SW 2003 9 2 ALG2003F00064 120030306A6720206001089001 TUBE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL T/R CONTROL DISCONNECTED A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03343AL 51372 CAE895020 DURING CONTROL FUNCTION CHECK ON RUN-UP TAIL ROTOR PEDALS FELT WEAK, PILOT SHUT THE AIRCRAFT DOWN AND NOTIFIED MAINTENANCE. THE MECHANIC FOUND TAIL ROTOR CONTROL TUBE IN THE BOX BEAM TO THE BELLCRANK IN HAT RACK AREA NOT CONNECTED, THE MECHANIC RECONNECTED THE CONTROL TUBE. 1G71 3U3 U H2SW E1GL 20030724000922003072400092EU 2003 7 24 AWXA200300731 120030623A2923693335 PUMP AIRBUS320 A320232 3930326EU ZONE 190 OVERHEATED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28605AW11175 543 ON CLIMBOUT, AT 11000 FEET RECEIVED ECAM BLUE HYDRAULIC SYSTEM OVERHEAT WARNING, TURNED BACK TO LAS. MAINTENANCE TROUBLESHOT SYSTEM PER TSM 29-12-00-810-806 AND IDENTIFIED THE BLUE ELECTRIC HYDRAULIC PUMP AS BAD. REMOVED AND REPLACED BLUE HYDRAULIC SYSTEM ELECTRIC PUMP IAW AMM 29-12-51-401, OPERATIONAL CHECK AND LEAK CHECK WERE GOOD. VENDOR TEARDOWN OF BLUE HYDRAULIC SYSTEM ELECTRIC PUMP S/N MX616661 CONFIRMED FAILURE OF UNIT. THE STATOR (P/N 973545), BEARING (P/N 732029), SPRING WASHER (P/N 849209), RETAINING RING (P/N 388180), CONNECTOR (P/N 681950), PACKINGS, SHIMS, AND SEALS WERE ALL FOUND WORN BEYOND LIMITS. REPLACED ALL WORN PARTS AND TESTED PUMP IAW CMM 29-21-20, REV. 4. 2L72 4F RTA28NM 20030813000342003081300034 2003 8 13 HEEA088565 420030731A34222594484 TRANSMITTER BELL 412 412 1182202SW TARSYN UNIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 FLUX VALVE CAUSES FUSE TO BLOW AT TARSYN UNIT. SHOP REPAIR. 1G72 4U H4SW 20030813002082003081300208NM 2003 8 13 SWAA031705 120030731A3350101073 LENS BOEING737 7372H4 138448CNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F A16WE 20030902001842003090200184NM 2003 9 2 03FDEA00968 120030621A5753ARC70561 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LT WING- O/B FLAP VANE NR 4 FITTING FORWARD HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-69380 - WINGS - TRAILING EDGE FLAPS - LEFT HAND OUTBOARD FLAP - VANE SUPPORTS - CORROSION REPAIR AND REFURBISHMENT. 2L73 4F RTA22WE 20030903002392003090300239EA 2003 9 3 03235650 120030823A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27650BR 7418 DURING MAINTENANCE INPSPECTION THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTIUED SERVICE 2L72 4F RTA21EA 20030904001402003090400140WP 2003 9 4 MWEA030264 120030623A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LIGHTNING STRIKE FOUND AT FRAME 49, 52, 57, 71, 86. REPAIRED SKIN. 2L72 4F A6WE 20030905000782003090500078SO 2003 9 5 C2XA03SH264 120030808A491012038509001 FRAME EMB 145 EMB145LR 3260212SO APU COWLING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 SHV DURING C CHECK THE APU COWLING FRAME CRACKED AND SKIN BENT AT 11 O'CLOCK. MAINTENANCE REPAIRED AFFECTED SECTION IAW EMB 145 IC2003-145/2629 AND EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030813000112003081300011NE 2003 8 13 HEEA088655 220030730A72100292104110 COUPLING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03854PH 3248 DURING 1500 HOUR ENGINE INSPECTION FOUND RETAINING RING P/N 9745008005 LOOSE IN MOUNT GROOVE IN COUPLING. REPLACED RING WITH NEW RING WITH NO CHANGE (RING SHOULD BE TIGHT WITHIN GROOVE WITH NO MOVEMENT). DETERMINED COUPLING TO BE WORN AT RING GROOVE. TO BE SENT TO VENDOR. 1G71 3U3 U H9EU E19EU 20030815000032003081500003NM 2003 8 15 AALA20030551 120030509A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21192AN 32386 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 24 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT PINS OF GRILL TO SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030825000822003082500082NM 2003 8 25 03FDEA01225 120030808A5315 FLOORBEAM BOEING727 7272S2F 1384O81NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 AFT CARGO BAY FLOORBEAM LWR FLANGE HAS CORROSION AT FASTENER HOLES WL 200 LBL 40 RBL 53. R/R FLOORBEAM. 2L73 4F A3WE 20030728000442003072800044NM 2003 7 28 SWAA031601 120030721A53146545866 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND KEELBEAM CORRODED BETWEEN BS 500D + 2 AND BS 500D + 6, WL 147 AND RBL 7. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20030909002662003090900266EU 2003 9 9 RAIA00308224 120030827A5270 SWITCH JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03554HK 41067 5506-STL- BAGGAGE DOOR WARNING LIGHT CAME ON. MAINTENANCE CLEANED MICRO SWITCH AND SECURED BAGGAGE DOOR HANDLE. 2L72 4T RTA41NM 20030926000852003092600085EA 2003 9 26 COMA0360392 120030826A3210 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01492CA 7763 AIRCRAFT PULLED SEVERELY TO LEFT DURING T/O. COULD NOT DUPLICATE. INSPECTED WHEELS, BRAKES AND NWS SYSTEM. NO DEFECTS FOUND 2L72 4F RTA21EA 20031001000032003100100003NM 2003 10 1 QXEA200301071 120030831A5720 ANGLE DHAV DHC8 DHC8202 2809007NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 LT WING VERTICAL CONNECTION ANGLE ON FORWARD SPAR AT NACELLE HAS TWO CRACKS IN RADIUS AT UPPER AND LOWER ENDS. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20031006000782003100600078CE 2003 10 6 AMWA51 120030903A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07132YV UE132 WHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLANGE AT CANTED STAB. STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE LT SIDE AT THE AFT STRG INTERSECTION AND ONE PLACE ON THE RT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH SRM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031003000662003100300066SO 2003 10 3 C2XA03TY162 120030913A532014522460015 GUSSET EMB 135 EMB135ER 3260203SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719503 145176 DURING A SCHEDULED 2C INSPECTION THE AFT GUSSET WAS FOUND CORRODED IN SEVERAL SPOTS. MAINT. R/R THE AFT GUSSET IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031008000612003100800061NM 2003 10 8 USAA030198 120030912A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US46240 23739 FOUND SKIN CRACKED 2 INCHES, FS 727D PLUS 4 INCHES AT STRINGER 23R. REPAIRED WITH .050 DOUBLER PER EA 94691. (M) 2L72 4F RTA16WE 20031020002062003102000206NE 2003 10 20 DLM90030819 220030907A7200 BEARING DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 1 ENGINE COKED A DALAK NONE A FLAME/FIRE TXTAXI/GRND HDL 1 SO27903DA1973912152 53383 020012 NUMBER ONE ENGINE HAD TAIL PIPE FIRE ON SHUT DOWN. NUMBER 1 ENGINE BEING CHANGED DUE TO EXCESSIVE COKING IN NUMBER 5 BEARING COMPARTMENT PER IAE. 2L72 4F4 FRTA6WE E40NE 20031022000552003102200055SO 2003 10 22 LR7A03078 120030922A53153556712R FITTING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FLOORBEAM CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 693 4590 DURING SCHEDULED B2 INSPECTION IAW JOB CARD HB5302 FOUND RT FS 477 FLOORBEAM END FITTING CRACKED AT RBL 60, WL 146. REPLACED FITTING IAW DWG 356245-19 AND SRM SMP 583 51-70. NR 0027. 2H74 4T4 T A1SO E282 20031022001032003102200103CE 2003 10 22 DXTA200300124 120030919A7603 BELLCRANK CESSNA560 560XL 2076702CE PWA 545 PW545A NE THROTTLE LINKAGEMISINSTALLED E DXTAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL07676QS 5605176 ON LANDING AT TEB, LT ENGINE FAILED UPON STOWING THRUST REVERSERS, TROUBLESHOT AND FOUND THE LEFT ENGINE WHEN POWER IS ABRUPLY REDUCED TO IDLE, ENGINE FAILED (THROTTLE WENT TO CUT-OFF) - FERRIED AIRCRAFT TO CMH FOR REPAIR, CONFIRMED DISCREPANCY TROUBLESHOT AND FOUND THROTTLE ARMS UNDER CREW SEATS INSTALLED BACKWARDS. THROTTLE ARMS WERE INSTALLED UNDER MFG SB 560XL-76-03R1 ON 09/17/03, REPOSITIONED THE THROTTLE ARMS AND RE-RIGGED BOTH ENGINES. WORK DONE IAW MFG 560XL MM CHAPTER 76-11-00 AND SB 560XL-76-03 R1, ENGINE OPS CHECKED GOOD. 2L72 4F4 FRTA22CE E00059EN 20030908003052003090800305 2003 9 8 SWAA031883 420030820A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F A16WE 20030909002862003090900286EA 2003 9 9 QXEA200300956 120030807A7830 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER MALFUNCTIONED A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09613QX 10045 BOI- ON FLIGHT 2547 ABORTED TAKEOFF DUE TO ON TAKEOFF ROLL AT ABOUT 90-100 KTS, THRUST REVERSER UNSAFE LIGHT CAME ON. IT WAS UNCLEAR WEATHER OR NOT IT WAS RIGHT OR LEFT. PERFORMED HI-SPEED TAXI WITH FLIGHT CREW, NO FAULTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030910000072003091000007EU 2003 9 10 BAQA088312 120030805A6340L771M40C1003 INDICATOR UROCOPEC135 EC135T1 5620026EU MAIN ROTOR INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03136MH45 0161 TRIPLE TACH ROTOR NEEDLE INOPERATIVE. ON START-UP AFTER TEST ROTOR NEEDLE CLICKS BACK PAST THE ZERO. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031027001092003102700109NM 2003 10 27 ASAA02401PP 120030329A5320654795576 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK FOUND FLOOR SUPPORT WEB IS CORRODED FROM BS 814-847. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031023000122003102300012NM 2003 10 23 03FDEA01497 120030903A5753ARC0502505 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING: O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR I/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5740-71779. WINGS - LEFT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031027000982003102700098NM 2003 10 27 ASAA02402FF 120030407A572065C2631176 STRUCTURE BOEING737 7374Q8 138447QNM RT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND RIGHT WING INBOARD EXHAUST FATE UPPER SURFACE CHAFED AT OUTBOARD FORWARD EDGE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031022001452003102200145EA 2003 10 22 SWIA200312430 120030922A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 FS 280 LT FLOORBEAM LBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INBOARD AND OUTBOARD ANGLES AT FS 280 LBL 9 FLOORBEAM REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-57 2L72 4F4 FRTA21EA E15NE 20031029000252003102900025NM 2003 10 29 ASAA0340081 120030227A532065479573 THRESHOLD BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON SUB THRESHOLD AT RBL 23 AND WL 155. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031118000332003111800033NM 2003 11 18 AWXA200301148 120030903A571065C2630924 ATTACH ANGLE BOEING737 7373Q8 1384670NM RT WING TE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-16 CHECK A .75 INCH CRACK WAS FOUND ON RT WING TRAILING EDGE UPPER PANEL INBOARD ATTACH ANGLE AT WBL 198.6. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT WBL 198.6; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA B-1-2. 2L72 4F RTA16WE 20031120000532003112000053NM 2003 11 20 QXEA200301241 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 1 SEAT TRACK HAS PITTING CORROSION AT STATION 348. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11, 20-21-21 AND RD 8-53-1339. 2H72 4T RTA13NM 20040113002082004011300208SO 2004 1 13 C2XA03TY191 120031106A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716999 145307 TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKS I/A/W EMB-145-SRM-53-32-13 AND EC5330-01287. 2L72 4T RTT00011AT 20040115000932004011500093NM 2004 1 15 03FDEA02073 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LOWER SECTION OF NR 2 BANJO FITTING (AJC7052- 501) AFT FACE FLANGE FOUND WITH 07 EA LOCK BOLT COLLARS CRACKED. RT LOWER SECTION OF NR 2 BANJO FITTING AJC7052-501 AFT FACE FLANGE 07EA CRACK LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. AND SRM 51-38-01 VOL. II. 2L73 4F RTA22WE 20040204000202004020400020WP 2004 2 4 NACA20030123 120031128A7932RS1143 SEAL DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 3 ENGINE WORN A NACAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 AL03993305664 5664 43576 NK510318 NR 3 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE. FOUND OIL FILLER CAP LEAKING AND TANK DOWN TO 8 GALLONS. REPLACED OIL FILLER CAP SEALS FOR SUSPECTED SIPHONING ACTION. OPS AND LEAK CHECK, GOOD. 2L74 4R4 R 6A3 5E8 20040204000982004020400098NM 2004 2 4 AWXA200301278 120031003A53476546815 SEAT TRACK BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON SEAT TRACK FROM BS 460 TO BS 480, RBL 25. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 460 TO BS 480, RBL 25; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 2 EACH RADIUS FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-52, FIG. 202, PG. 202-205. 2L72 4F4 FRTA16WE E2GL 20031030000872003103000087SO 2003 10 30 C2XA03SH364 120031002A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 DURING C-CHECK THE RIGHT CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031030000512003103000051NM 2003 10 30 UPS03441314 120030907A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D BS 360 S-14 LT FRAME CRACKED. MAIN DECK BS 360 STR 14 LT FRAME REPAIRED AS PER RS R53-12-35070 AND AS PER EO B747-5310-19268-A. 2L74 4F A20WE 20031119000032003111900003NM 2003 11 19 03280405 120031007A3350 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27405FJ 3155 DURING INSPECTION THE RT AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031106000832003110600083WP 2003 11 6 UPS03841514 120031022A5514SE085500094 FITTING DOUG DC8 DC873F 302199FWP HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 T-CHORD CRACKED, RT HORIZONTAL STAB INBOARD FRONT SPAR LOWER OUTBOARD CORNER AT XFS 60. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0 AND DWG 3701427. 2L74 4F RT4A25 20031106001012003110600101EA 2003 11 6 QXEA200301376 120031031A26119847101505 SCREEN CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX- FORWARD BAGGAGE BAY CENTER CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20031107000312003110700031EA 2003 11 7 QXEA200301394 120031104A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY FAILED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09615QX 10065 SEA- ON FLIGHT NUMBER 2478, FIRE SYSTEM FAULT STATUS MESSAGE APPEARED FOR 20 MINUTES AND THEN EXTINGUISHED. FOUND MDC MESSAGE AFT SMOKE DETECTOR 1 FAILED WIRING NO RESPONSE TO COMMAND IN FAULT HX. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031117000742003111700074NM 2003 11 17 DHL2003749507 120030920A5320 FLOOR SUPPORT BOEING727 7272J0 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK, AFT PIT FLOOR SUPPORT FROM STA 950E TO STA 990 HAS SEVERAL DENTS IN UPPER FLANGE LBL 10. REMOVED ANGLES SUPPORT AFT PIT STA 950E TO 990 LBL 10 IAW B-727 SRM 51-30-2. COLD WORKING AREA AND RETURNED TO ORIGINAL COUNTOUR. NO CRACK NOTED IAW B-727 SRM 51-10-2. INSTALLED ANGLE SUPPORT AFT PIT STA 950 E TO 990 LBL 10 IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20040401000422004040100042NM 2004 4 1 AALA20031139 120031013A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21641AA 24599 SFO - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT AFT PASSENGER DOOR. CLEANED AND TIGHTENED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031216000712003121600071NM 2003 12 16 SWAA032567 120031120A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 30, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040713000742004071300074NM 2004 7 13 TSAA0457015 120031220A57116545321 SPAR BOEING737 737230 1384401NM WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 DISCOVERED CORROSION AT WBL 245, 254, 336, AND 341 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED AREA PER SRM 57-30-1, FIGURES 1A AND 1B INSTRUCTIONS. REMOVED FASTENERS IN THE BLEND OUT AREA. INSTALLED HI-LOCKS WET WITH BMS 5-26 SEALANT IN TRANSITION FIT HOLES. CLEAN AND TREEATED ALL EXPOSED SURFACES, FILLED REMAINING VOIDS AND GAPS WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 3403. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030815000022003081500002NM 2003 8 15 AALA20030401 120030402A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21673AN 29423 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 13D INOPERATIVE. SECURED EMERGENCY EXIT LIGHT ASSEMBLY UNDER SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030819001232003081900123NM 2003 8 19 2003UALA00505 120030522A5754 WEDGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 5 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29546UA 25367 T/E WEDGE DELAMINATED, SLAT NR 5. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED AND REINSTALLED T/E WEDGE. 2L72 4F4 FRTA2NM E17NE 20030818000092003081800009NE 2003 8 18 HEEA088405 120030724A62107615009043054 TIP CAP SKRSKYS76 S76C 8143008NE M/R BLADE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 MAIN ROTOR BLADE TIP CAP CRACKED. TO BE SENT TO VENDOR. 1G72 3U NCH1NE 20030408000712003040800071NM 2003 4 8 03FDEA00368 120030401A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 B/S 600 FRAME DENT STR 23L. DENT IN FRAME AT BS 600 STR 23L FOUND TO BE OUT OF LIMITS. REPAIRED PER FED-EX EA 7-5310-54458. 2L73 4F RTA3WE 20030328000552003032800055NE 2003 3 28 C8GA20030008 220030320A7250 BEARING BOEING727 727225 1384077NM PWA JT8 JT8D9A 52048NE ENGINE FAILED A C8GAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15808EA 22439 666631 FLIGHT 723 FROM BOS TO ROC. ON CLIMB OUT, NR 3 ENGINE OIL QUANTITY DECREASED STEADILY TO APPROXIMATELY ONE GALLON. AIR TURNBACK TO BOSTON AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND SERVICE NR 3 ENGINE OILS. RAN ENGINE ON GROUND AND NO OIL LOSS OR LEAKS WERE NOTED ON GROUND IAW MM 79-31-0. AIRCRAFT RETURNED TO SERVICE. FLIGHT 723 FROM BOS TO ROC. ON CLIMB OUT, NR 3 ENGINE OIL QUANTITY DECREASED STEADILY. AIRCRAFT AIR TURNBACK TO BOSTON AND LANDED WITHOUT INCIDENT. RAN ENGINE PER MM 71-00-67 PAGE 211 AND NOTED EXCESSIVE OIL COMING FROM BREATHER. SUSPECT NR 5 BEARING CARBON SEAL BAD. PREPARED ENGINE FOR FERRY FLIGHT. 2L73 4F4 F A3WE E2EA 20030407000442003040700044WP 2003 4 7 GTIA030032 120030128A3260 PROXIMITY SWITCH DOUG DC9 DC981 3022081WP LT MLG DOOR LOOSE A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23805NK 48058 PBI - FLT 834 - GEAR DOOR OPEN LIGHT ILLUMINATED SHORTLY AFTER GEAR RETRACTION AFTER GEAR RETRACTION. PERFORMED QRH PROCEDURES. FOUND LEFT MAIN GEAR DOOR PROXIMITY SWITCH LOOSE. ADJUSTED AND TIGHTENED LEFT MAIN GEAR DOOR PROXIMITY SWITCH, OPS CHECK GOOD, NO DEFECTS NOTED. (M) 2L72 4F A6WE 20030416001482003041600148NM 2003 4 16 QXEA0300426 120030401A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FUSELAGE BELLY SCRATCHED SKIN FORWARD OF STATION X32.40 AND STRINGER 33. REPAIRED IAW RD 8/4-53-489. 2H72 4T RTA13NM 20030422001442003042200144NM 2003 4 22 UPS03640267 120030309A2612285N00286 FIRE DETECTOR BOEING767 76734AF 1385212NM MAIN CARGO FALSE INDICATIONA IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01324UP 27750 MAIN CARGO FIRE INDICATED, EICAS AND BELL ON T/O ROLL MOMENTARLY AT 80 KTS, THEN EXTINGUISHED. OCCURRED AFTER LANDING AND REMAINED ON BUT NO SMOKE OR FIRE PRESENT. FOUND SHRED OF SAFETY WIRE AROUND DIODE CR2 IN APU/CARGO FIRE CONT MODULE PNL AND REMOVED SAFETY WIRE SHRED. PRECAUTION REMOVED AND REPLACED AFOLTS CARD M2026 AND MAIN CARGO FIRE WARNING TEST OK PER MM 26-15-00. P/N OFF/ON 285N0028-36, S/N OFF D12060, S/N ON D10143. 2L72 4F RTA1NM 20030425000362003042500036EU 2003 4 25 RAIA00303082 120030321A793356774098010 INDICATOR AEROSPATR72 ATR72202 8680940EU LT ENG OIL TEMP INOPERATIVE A RAIAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 CE03722TE215911912 220 STL- LEFT HAND ENGINE OIL TEMPERATURE GAUGE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LEFT HAND OIL TEMPERATURE GAUGE, OPS CHECK OK. 2H72 4T RTA53EU 20030429000092003042900009NM 2003 4 29 P5CA0300790 120030216A5330 SKIN BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK ON BS 360 RIGHT B/T STR 8 TO 10. DAMAGED AREA TRIMMED OUT, REINFORCED WITH SEGMENT AND SPLICE PER SRM 53-10-01 FIG 10 & 51-10-02 & 51-30-02. 2L74 4F A20WE 20030501000862003050100086WP 2003 5 1 GTIA030200 120030217A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOND UPPER WEB LONGERON 18R MID PIT BETWEEN 541/560 CORRODED. CUT OUT WEB FROM STATION 503-605. FABRICATED NEW WEB REPAIR. INSTALLED WEB REPAIR. (M) 2L72 4F RTA6WE 20030501001482003050100148WP 2003 5 1 ASAA0380133 120030218A33500105603 LIGHT DOUG DC9 DC983 3022083WP FWD CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT FORWARD GALLEY. ALSO, THE TRACK COVER WAS MISSING. RECONNECTED WIRING CONNECTOR AND RESECURED COVER. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030506001852003050600185EA 2003 5 6 A6WA200340050 120030411A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 THE RIGHT CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621, ABL36, WL 73. REMOVED SECTION OF RIGHT CARGO FLOOR SUPPORT ANGLE FS 621. REPAIRED RIGHT FLOOR SUPPORT ANGLE IAW BOMBARDIER INC REO 601R-53-61-117 REV B. (M) 2L72 4F RTA21EA 20030506000482003050600048WP 2003 5 6 UPS03840452 120030416A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, FREON SYSTEM EXHAUST DOOR AFT LOWER CORNER STA 55 HAS A STAINLESS DOUBLER, DOES NOT COMPLY IAW EO DC8-5330-12800-D, AND IS CRACKED AT STA 52. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 13, NDT VERIFIED NO CRACKS AT CUTOUTS. 2L74 4F RT4A25 20030508000012003050800001NM 2003 5 8 P5CA0300873 120030422A361069B409671 DUCT BOEING747 747249F 1384849NM LT WING LEAKING A P5CAO OTHER K FLUID LOSS DEDESCENT 1 WP23920FT 22237 PILOT REPORTED BY PHONE PATCH THAT LT WING HAD A BLEED AIR LEAK. FOUND BLOWN DUCTS ON INSPECTION. REPLACED DUCTS AND REPAIRED WING TO BODY FAIRING PNL. (191KL) 2L74 4F A20WE 20030508000942003050800094EU 2003 5 8 AW6A200360021 120030425A5330 PANEL BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA FUSELAGE DENTED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31290UE E2080 DENTS OUT OF LIMITS ON THE LT WING PANEL BETWEEN RIB 14A AND 15. REPAIR REQUESTED FOR BAE SYSTEM REF. 2H74 4F4 F A49EU E6NE 20030509000012003050900001SO 2003 5 9 C2XA03CL099 120030506A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713936 145025 CLE FLIGHT 2268 THE CREW REPORTED EMERGENCY EXIT LIGHT WAS INOPERATIVE ON THE RIGHT SIDE BULKHEAD IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS.NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030509001402003050900140EU 2003 5 9 MALA030262 120030505A3040 CONTROLLER SAAB SF340 340B 7860101EU WINDSHIELD HEAT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15366PX 340B267 DURING FLIGHT 3082 LT FRONT WIND SHIELD LIGHT ILLUMINATED 3 TIMES IN 10 MINUTES. FOLLOWED QRH, COMES ON AGAIN. AIR RETURN TO MSP. MAINTENANCE COMPLETED 409 CARD 144349 REPLACED LT WINDSHIELD HEAT CONTROLLER. SEE CONTINUATION CARD 144349 FOR DETAILS. OPS CHECK GOOD. 2L72 4T RTA52EU 20030513000292003051300029CE 2003 5 13 A063SA 120030509A326041EN16 SQUAT SWITCH MTSBSIMU300 MU300 5780602CE LT MLG STRUT MISRIGGED E ERYAO OTHER N FALSE WARNING LDLANDING 1 CE07984SA6056 A063SA UPON LANDING, THRUST REVERSERS FAILED TO DEPLOY AND SPEED BRAKES FAILED TO EXTEND. WHEEL BRAKES INITIALLY WORKED, BUT FAILED DURING ROLLOUT. THE USE OF EMERGENCY BRAKES WERE REQUIRED. AS AIRCRAFT SLOWED, USE OF THRUST REVERSERS, SPEED BRAKES, AND WHEEL BRAKES BECAME EFFECTIVE. SYSTEMS WERE TROUBLESHOT AND FOUND IMPROPER SERVICING OF GEAR STRUTS, PREVENTING SQUAT SWITCH(ES) FROM ACTIVATING PROPERLY. SERVICED STRUTS IAW M/M AND SERVICED HYDRAULIC SYSTEM AND EMERGENCY BRAKE ACTIVATION SYSTEM. 2H72 4F RTA14SW 20030513002722003051300272EA 2003 5 13 ASOA03141 120030401A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIPS IN THE AFT CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT STRIP CONNECTORS IN THE AFT CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514001702003051400170NM 2003 5 14 P5CA0300865 120030411A5330 FRAME BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 BS 200-S13L-S14L FRAME WEB CRACK. REPAIRED PER SRM 53-10-04 FIG 93. 2L74 4F A20WE 20030605000962003060500096NM 2003 6 5 UPS03240692 120030416A5753 CARRIAGE BOEING727 72722C 138400FNM NR 6 TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, NR 6 FLAP CARRIAGE SPINDLE INTERNALLY CORRODED. NR 6 FLAP CARRIAGE REPLACED IAW OHM 57-58-02 & OHM 57-52-01 REF. TC C5 7-581-04-4D FOR INST. & DUAL 2L73 4F A3WE 20030606000102003060600010NE 2003 6 6 HCM2003F00000 220030430A732070BMF01000 FADEC UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE CONTROL INOPERATIVE E HCMAO OTHER O OTHER NRNOT REPORTED 1 WP1311QD 2017 TEN MINUTES INTO THE FIRST FLIGHT OF THE DAY, A SERIES OF WARNING GONGS WENT OFF IN THE PILOTS HEADSET FOLLOWED BY THE YELLOW (GOV) LIGHT, THE RED (GOV) LIGHT AND THE RED (TWX GRIP) LIGHT ALL BEING ILLUMINATED. THE RED (GOV) LIGHT FLICKERED AND EVENTUALLY WENT OUT. THE PILOT RETURNED TO THE HELIPORT. THE TWIST GRIP WOULD NOT RETARD THE ENGINE SPEED AND THE AIRCRAFT HAD TO BE SHUT DOWN FROM FLIGHT IDLE WITH THE SHUT OFF SWITCH. THIS INDICATES THE AIRCRAFT WAS FLOWN BACK IN THE FULL EMERGENCY (EBCAU) MODE. THE FADEC WAS CHANGED TO CORRECT THE PROBLEM. 1G72 3U3 U H9EU E19EU 20030606000152003060600015EU 2003 6 6 03FDEA00759 120030519A5410491B1220000003 DOOR AIRBUS300 A300F4605R 3930327EU T/R BLOWOUT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 NR 1 ENGINE RT T/R COWL BLOW OUT DOOR INTERIOR HAS TWO EACH CHAFED AREAS WHERE RETAINING CABLE HAS MADE CONTACT. REPAIRED DAMAGED AREAS BY BLENDING, ALODINING, AND FILLING AREA WITH HIGH TEMP SEALANT, AND APPLYING A COAT OF TEFLON PAINT IN THE REWORKED AREA. THEN ROTATED THE UPPER END OF THE CABLE TO PREVENT FURTHER DAMAGE AND WRAPPED THE CABLE WITH RUBBER STRIP. ALL WORK DONE PER E.A. 6-7800-69701. 2L72 4F RTA35EU 20030515001592003051500159NM 2003 5 15 SWAA031075 120030510A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED 7 INCH LONG AT BS 639 STRINGER 16L. REPAIRED FRAME PER ERO. 2L72 4F RTA16WE 20030515000362003051500036NM 2003 5 15 C1HA200381012 120030503A3150 WARNING HORN BOEING727 7272S7 138407ZNM COCKPIT ACTIVATED A C1HAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15681CA 22020 ON TAKEOFF, TAKEOFF WARNING HORN SOUNDED. 2L73 4F A3WE 20030610000062003061000006EU 2003 6 10 HEEA086725 120030522A6720 BEARING BOLKMS105 BO105S 5626006EU CONTROL ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 CONTROL ROD HAS WORN BEARINGS. IN SHOP REPAIR. 1G72 3U H3EU 20030612000402003061200040NM 2003 6 12 CALA0300269 120030528A5512 SKIN BOEING737 737524 1384721NM HORIZONTAL STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714639 28900 INSPECTION FOUND A DENT WITH GOUGE IN LT HORIZONTAL STABILIZER UPPER SPAR SKIN. THE DENT WAS LOCATED 51 INCHES O/B FROM I/B EDGE AND 3.5 INCHES AFT OF FORWARD SPAR. THE DENTED AREA WAS CUTOUT AND A DOUBLER WAS INSTALLED IAW SRM 55-10-01, FIGURE 207. 2L72 4F RTA16WE 20030617002652003061700265NM 2003 6 17 QXEA200300612 120030508A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - SHIMS BETWEEN FORWARD, RT HAND H-STAB TO V-STAB ATTACH POINT HAVE COMPLETELY EXTRUDED. REPAIRED IAW Q400 AMM TASK 55-10-00-400-801. 2H72 4T RTA13NM 20030617001952003061700195GL 2003 6 17 ERAA087104 220030521A7200250C20B ENGINE BOLKMS105 BO105A EU ALLSN 250C 250C20B 03013GL MAKING METAL E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01135EH14386 S675 ENGINE MAKING METAL. FOUND TURBINE MOUNT STUD ON LT SIDE OF GEARBOX LOOSE, MOVING. 1G72 3U3 U H3EU E4CE 20030521000442003052100044WP 2003 5 21 DHL2003804888 120030212A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING T/E UPPER SKIN SURFACE WITH 0.500 INCH CRACK STA XRS.285.000- 305.000. CUT OUT DAMAGED AREA IAW SRM 57-2-0 FIG 2. FABRICATED FILLER (2024-T3 0.032) AND DOUBLER (2024-T3 0.050) IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW SRM 57-2-0 FIG 2, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001122003052100112WP 2003 5 21 DHL2003801064 120030405A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS AT STA 318.000 WORN. REMOVED AND REPLACED NR 7 TRACK PLUG LUGS AT STA 318.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030618000502003061800050 2003 6 18 SWAA031317 420030611A2565D31354 SLIDE BOEING737 7373A4 1384585NM ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030527000502003052700050NM 2003 5 27 CALA0300247 120030514A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2710323 23374 INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-01. 2L72 4F RTA16WE 20030529000052003052900005EU 2003 5 29 AALA20030423 120030407A2560 FLASHLIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2125071 514 MIA - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030530000492003053000049NE 2003 5 30 HEEA086546 220030522A7397 CONNECTOR SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE VALVE ASSY DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 ENGINE VALVE CONNECTOR DAMAGED. REPLACED CONNECTOR V5032-135 DUE TO DAMAGED. REPAIRED. 1G72 3U3 U H1NE E19EU 20030624000652003062400065NM 2003 6 24 CALA0300308 120030611A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, RBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603. 2L72 4F RTA16WE 20030707001312003070700131NM 2003 7 7 DL757030506 120030601A5330146N31316 SKIN BOEING757 757232 1384965NM FS S-6R DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27633DL 23614 LIGHTNING DAMAGE, CUTOUT REPAIR. THE FUSELAGE SKIN WAS STRUCK BY LIGHTNING AT FS 1450 AND STRINGER 6R. THE DAMAGE WAS REMOVED WITH A 1.2 INCH CUTOUT IN THE CROWN SKIN. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 385187-14, REV A. 2L72 4F RTA2NM 20030707001222003070700122EU 2003 7 7 AWXA200300733 120030623A2910D2905310900001 LINE AIRBUS320 A320231 3930325EU AFT SPAR CHAFED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28625AW 064 ON DECENT, EN ROUTE RECEIVED ECAM MESSAGE GREEN HYDRAULIC SYSTEM LOW QUANTITY; DECLARED EMERGENCY, NO NOSE WHEEL STEERING, AIRCRAFT TOWED OFF RUNWAY. MAINTENANCE FOUND GREEN SYSTEM HYDRAULIC PRESSURE LINE CHAFED AND LEAKING IN LT WHEEL WELL ON AFT SPAR BETWEEN RIBS 2 AND 5. PERFORMED REPAIR IAW AMM 20-23-11, PG. 201, LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20030710000442003071000044 2003 7 10 USAASA03060 420030604A2565 GIRT BAR AIRBUSA319 A319112 3930323EU ESCAPE SLIDE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW 0896 THE FORWARD GALLEY SLIDE ARMING LEVER DOES NOT ARM SMOOTHLY, AND DOES NOT ALWAYS INDICATE ARMED. MAINTENANCE ADJUSTED THE FLAP ON THE GIRT BAR. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030709000632003070900063NM 2003 7 9 C1HA200393009 120030527A3350900835A BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 EMERGENCY EXIT LIGHT ON RIGHT AFT CARGO DOOR INOP. 2L73 4F A3WE 20030716000232003071600023NM 2003 7 16 2003F00415 120030313A5330 SKIN BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON OUTER SKIN OF CO-PILOT WINDOW POST AT BS 203. FABRICATE DOUBLER REPAIR. ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ON OUTER SKIN OF CO-PILOT WINDOW POST AT BS 203. (M) 2L73 4F A3WE 20030124000902003012400090NM 2003 1 24 UPS03440070 120030102A5310 BULKHEAD BOEING747 747259B 1384804NM LH WLG W/W CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C LH WLG W/W FWD BULKHEAD WEB UPPER AREA BS 1241 LBL 60-100 CORROSION REVEALED. CORROSION REMOVED AND C/OUT REPAIR AS PER RS R57-12-34959. DEPTH 0.038, WIDTH 1", LENGTH 2". 2L74 4F RTA20WE 20030127002232003012700223SW 2003 1 27 HEEA083710 120030115A6730206076062107 SERVO BELL 407 407 1182206SW CYCLIC WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH2390 53266 CYCLIC SERVO BEARING ON AFT END OF SERVO IS WORN. 1G71 3U O H2SW 20030127002572003012700257SW 2003 1 27 HEEA083732 120030115A6320214040806003 PRESSURE SWITCH BELL 407 407 1182206SW M/R GEARBOX MALFUNCTIONED E HEEAO OTHER N FALSE WARNING ININSP/MAINT 1 SW03742PH 53461 MAIN ROTOR GEARBOX PRESSURE SWITCH MALFUNCTIONED, LIGHT STAYS ON. 1G71 3U O H2SW 20030128000472003012800047GL 2003 1 28 HEEA083800 220030115A732023072725 HYDROMECH UNIT BELL 407 407 1182206SW ALLSN 250C 250C* GL FUEL CONTROL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 HMU WILL NOT KEEP MAIN ROTOR FROM DROOPING. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000972003012800097SW 2003 1 28 HEEA083844 120030116A6230 BUSHING BELL 407 407 1182206SW SWASHPLATE LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH4082 AFS1028 53393 MAIN ROTOR SWASHPLATE LINK BUSHINGS ARE WORN. 1G71 3U O H2SW 20030128001292003012800129SW 2003 1 28 HEEA083866 120030116A6310 HOUSING BELL 407 407 1182206SW FREEWHEEL UNIT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH A4865 53188 FREEWHEEL UNIT HAS A CRACK BETWEEN 2 BOLT HOLES ON HOUSING. REPLACED FREEWHEEL UNIT. 1G71 3U O H2SW 20030130000812003013000081NM 2003 1 30 P5CA0300736 120030123A5411NONE FRAME BOEING747 7472U3B 1384846NM #2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 5 CRACKS TOTAL FOUND #2 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST FWD FRAME. L/H: (1) 2" CRACK ON L/H SIDE FRAME, STARTING FROM TOP EDGE ON VERTICAL FLANGE. R/H: (3) 1/2" EA. CRACKS ON R/H SIDE, STARTING ON 1ST AFT FASTENER HOLE FROM TOP ON HORIZONTAL FLANGE & (1) 1/2" CRACK, STARTING FROM TOP EDGE RADIUS. L/H & R/H FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 811O-3. 2L74 4F RTA20WE 20030204000372003020400037NM 2003 2 4 SWAA030228 120030128A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT RADIUS OF EQUIPTMENT COOLING CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204000602003020400060NM 2003 2 4 SWAA030172 120030123A53106516301 FRAME BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND BS 188 FRAME CRACKED AT STR 17L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20030212000222003021200022WP 2003 2 12 AUS20030022 120030114A571151762561 SPAR DOUG DC4 C54E 3021530WP RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT OUTER WING UPPER SPAR CAP CORRODED AT WS 378. 2L74 4R A762 20030218001722003021800172NM 2003 2 18 QXEA0300164 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 4 SEAT TRACK HAS SCRATCHES AT STATION 285-295. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030220000472003022000047WP 2003 2 20 ABXA030048 120030127A2421976J2544 VOLT REGULATOR DOUG DC9 DC941 302207NWP APU BURNED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23990AX 47493 SMOKE IN UPPER CARGO COMPARTMENT AND COCKPIT. INSPECTED AND FOUND APU GENERATOR CONTROL PANEL AND APU VOLTAGE REGULATOR BURNED. INSPECTED WIRING FOR DAMAGE, NONE NOTED. INSPECTED AC BUS CONTROL FOR DAMAGE, NONE NOTED. INSPECTED FOR ANY CIRCUIT BREAKERS TRIPPED, NONE WERE TRIPPED. INSPECTED APU STARTER WIRES, TERMINALS AND APU GENERATOR WIRES, NO DAMAGE NOTED. REMOVED AND REPLACED APU VOLTAGE REGULATOR AND APU AC GEN CONTROL PANEL. APU GENERATOR AND VOLTAGE REGULATOR OPS CHECKED GOOD IAW DC-9 MM 24-20-02-5-0, ALSO CROSSTIE CHECKED GOOD FOR THE APU IAW DC-9 1 SERVICE CHECK. 2L72 4F A6WE 20030220000922003022000092EA 2003 2 20 QXEA0300087 120030115A2824P93A25602 CARTRIDGE CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAULTY A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09613QX1599 10045 PDX - FLIGHT 2495 - DURING CRUISE FLIGHT, THE LEFT FUEL TANK DECREASED IN FUEL QUANTITY 3 TIMES FASTER THAT THE FIGHT TANK. THE CREW ALSO RECEIVED A XFLOW PUMP CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE XFLOW PUMP CARTRIDGE. THE SYSTEM LEAK CHECKS AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030115002192003011500219WP 2003 1 15 ZW0A0300701 120030114A3350408822101 BATTERY DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13982TW 53632 BOTH COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 11-19-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030116000612003011600061 2003 1 16 HEEA083020 420030106A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMM SYSTEM WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 MIXER BOX HAS WEAK TRANSMISSIONS ON FIRST FLIGHT OF DAY. REPAIRED. 1G71 3U H2SW 20030117000552003011700055SW 2003 1 17 HEEA083174 120030108A6310206040270101 SUPPORT BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MAIN ROTOR SUPPORT LEAKING. REPAIRED. 1G71 3U H2SW 20030224000442003022400044 2003 2 24 HEEA084165 420030212A34427007700614 INDICATOR SKRSKYS76 S76A 8143006NE WX RADAR SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 WEATHER RADAR INDICATOR INOPERATIVE. 1G72 3U H1NE 20030225000362003022500036SW 2003 2 25 HEEA084255 120030120A5210407070620218 TRIM PANEL BELL 407 407 1182206SW DOOR INTERIOR CRACKED E O OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 PAX/CREW DOOR INTERIOR TRIM PANEL CRACKED. 1G71 3U O H2SW 20030226000282003022600028SW 2003 2 26 HEEA084318 120030211A2842407362005103 SWITCH BELL 407 407 1182206SW LOW FUEL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH 53435 FUEL LOW LEVEL LIGHT STAYS ON. REPLACED FUEL CELL, FUEL LOW SWITCH. 1G71 3U O H2SW 20030303000042003030300004 2003 3 3 HEEA084477 420030214A341613011001 ENCODER BELL 412 412 1182202SW ALTIMETER READS HIGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 ALTIMETER ENCODER READS 100 FT HIGH. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030305000202003030500020 2003 3 5 C1HA200382001 420030112A2565 SLIDE BOEING727 7272S7 138407ZNM L2 DOOR DISLODGED A C1HAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15682CA 22019 L2 DOOR SLIDE OUT OF CONTAINER. REINSTALLED L2 SLIDE IN CONTAINER IAW MM 26-60, OK FOR SERVICE. 2L73 4F A3WE 20030307001442003030700144NM 2003 3 7 AALA20030133 120030130A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21174AA 31308 MIA - DURING OVERNIGHT MAINTENANCE, R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030310000522003031000052NE 2003 3 10 HEEA084956 220030227A732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TORQUE OSCILLATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 TORQUE CONTROL UNIT CAUSES ENGINE OSCILLATIONS AND TORQUE ACCELERATIONS. COULD NOT DUPLICATE OSCILLATION. UNIT NEEDED MINOR TRIM ADJUSTMENTS. TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030313001462003031300146 2003 3 13 R2J2003F00002 420030108A2562 BATTERY MTSBSIMU2 MU2B40 5780440CE GARRTTTPE331TPE331* 01514WP ELT LEAKING B R2JRK NONE K FLUID LOSS ININSP/MAINT 1 EA21361MA 429SA WHILE CONDUCTING 91.207D, ELT SYSTEM INSPECTION NOTICED WET SPOT AT CORNER OF BATTERY PACK CARDBOARD. PACK HAD 1-2 MONTHS REMAINING ON LIFE LIMIT AND ELT WORKED PERFECTLY FURTHER INSPECTION REVEALED. 1 CELL IN BATTERY PACK LEAKY AND CORRODED. BATTERY VOLTS OK. NEW BATTERY PACK WAS INSTALLED AND ELT CHECKED IAW 91.207-OK. SUGGEST GOOD VISUAL INPUT AT YEARLY ELT SYSTEM CHECKS. (PTRS-EA212003B1136) 1H72 3T3 TRTA10SW E2WE 20030314000902003031400090NM 2003 3 14 SWAA030535 120030307A531365C27314 TIE CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STR TIE CLIP PER SRM. 2L72 4F RTA16WE 20030118000072003011800007SO 2003 1 18 C2XA03TY005 120030118A534014522459003 ANGLE EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 TYS, During a scheduled inspection corrosion was found on the center ramp angle between frames 19 and 20. Maintenance removed and replaced the center ramp angle, alodined, primed and painted. I/A/W-EMB-135/145-SRM-51-40-02. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2L72 4T RTT00011AT 20030121000622003012100062SW 2003 1 21 HEEA083264 120030108A7714206075682107 INDICATOR BELL 206 206L4 1182110SW ENGINE N1 INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 N1 GAUGE NEEDLE BOUNCES AROUND ON THE LOW END DURING START. 1G71 3U NCH2SW 20030317000662003031700066SO 2003 3 17 C2XA03BT039 120030314A3350 BATTERY PACK EMB 145 EMB145ER 3260211SO CABIN LOOSE A C2XAK NONE O OTHER TXTAXI/GRND HDL 1 SW2716944 145045 EWR ON PREFLT FOUND MAIN CABIN DOOR EMERGENCY LIGHTS INOP. RERACKED EMERGENCY BATTERY IAW EMB 145MM 33-50-04. OPS CHECK GOOD. 2L72 4F RTT00011AT 20030317001372003031700137NM 2003 3 17 03FDEA00301 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 600, BETWEN STR 24L AND 25L. 2L73 4F RTA3WE 20030318000032003031800003NM 2003 3 18 SWAA030583 120030315A53306545774 SLIDE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030122002742003012200274NM 2003 1 22 AWXA200300055 120030120A3350BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 19 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW0 0 22647 TUS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE DISCOVERED A WIRE PULLED FROM SPLICE UNDER SEAT, REPAIRED BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030123000142003012300014NM 2003 1 23 2003UALA00030 120030107A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29951UA 26696 STATION 178 BULKHEAD WEB CRACKED AT RBL 1 IN WL 188. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030418000712003041800071NM 2003 4 18 QXEA0300281 120030210A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - CHAFING DAMAGE ON PANEL 262AT. REPAIRED IAW HORIZON AIR EA 6-53-196. 2H72 4T RTA13NM 20030416003812003041600381NM 2003 4 16 P5CA0300718 120030109A541565B913141 FITTING BOEING747 7472U3B 1384846NM NR 1PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 TWO CRACKS FOUND AROUND INBOARD AND OUTBOARD FASTENER HOLES NR 1 PYLON REAR ENGINE MOUNT BULKHEAD BATHTUB FITTING. - I/B: (1) .75 INCH, (1) .125 INCH RADIALLY. O/B: (1) .75 INCH, (1) .5 INCH RADIALLY. CRACKED BATHTUB FITTING REPLACED AS PER S/B 747-54-2113 R2. 2L74 4F RTA20WE 20030421000592003042100059NM 2003 4 21 EIA2003045 120030302A3020322963010 VALVE BOEING747 747212B 1384886NM PWA JT9 JT9D7F 52054NE ANTI-ICE FAILED A EIAAJ DUMP FUEL S AFFECT SYSTEMS CRCRUISE 1 NM09486EV 20888 662133 NR 3 ENGINE ANTI-ICE VALVE INOPERATIVE. REPLACED NR 3 ENGINE ANTI-ICE VALVE, OPS AND LOCK CHECK, OK. IAW 30-21-03 AND 30-21-00. 2L74 4F4 F A20WE E20EA 20030422000212003042200021NE 2003 4 22 MEX2003060 220030304A73217696068 FUEL CONTROL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE ENGINE FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23505MD 49149 FLT 189 - TIJ-MEX - AIRCRAFT RETURNED TO PLATFORM, OSCILLATION IN ENGINE PARAMETERS. OIL FILTER, OIL MAIN FILTER AND CHIP DETECTOR WERE VERIFIED. N2 WAS ADJUSTED AT LOW LEVEL REMAIN AT 52 PERCENT AND THE REST OF PARAMETERS WERE OK. AN ENGINE VISUAL INSPECTION WAS PERFORMED AT MEX RON. THE FCU WAS REPLACED AND ENGINE TEST WAS PERFORMED IAW MM 71-00-00. (M) 2L72 4F4 F A6WE E9NE 20030801000362003080100036NM 2003 8 1 AMTA200300799 120030618A3397 WIRE BOEING757 75723N 1384973NM CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11528AT 30887 EMERGENCY EXIT FLOOR LIGHTS ROWS 15 THROUGH 21 INOPERATIVE. RECONNECTED WIRING AT ROW 15. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030801000512003080100051WP 2003 8 1 GTIA030500 120030626A5754 RIB DOUG DC9 DC982 3022082WP L/E SLAT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - RIGHT WING OUTBOARD SLAT EDGE SEAL TORN, FOUND CRACKED CASTING. REMOVED CASTING. LOCATED AND DRILLED NEW RIB. INSTALLED NEW RIB. (M) 2L72 4F A6WE 20030828001322003082800132WP 2003 8 28 MWEA030300 120030729A5322 ATTACH ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 AFT INBOARD NUTPLATE ATTACH ANGLE FOR G3 MOUNT HAS CORROSION. FABRICATED AND INSTALLED ANGLE. 2L72 4F A6WE 20030829001622003082900162NM 2003 8 29 SWAA031827 120030813A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 502 AT STR 10R AND BS 878 AT STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030806001352003080600135SO 2003 8 6 C2XA03TY120 120030805A534714530658005 SEAT TRACK EMB 145 EMB145ER 3260211SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED 3C INSPECTION, SEAT TRACK RF3 IS CORRODED. MAINTENANCE REMOVED DAMAGED SEAT TRACK, CLEANED AREA, REINSTALLED SEAT TRACK, APPLIED CIC AND PLACED ON DMI FOR 200 FLIGHT CYCLES (REF M-602, 596609). WORK WAS IAW EMB 1C2003-145/2602 AND 53-10-06. A/C WAS REL UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030903002272003090300227EA 2003 9 3 03209671 120030728A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27671BR 7572 DURING INSPECTION THE CREW REPORTED THE LAST ONE THIRD EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND COULD NOT DUPLICATE THE FAULT. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030903002382003090300238EU 2003 9 3 03238307 120030826A261251228532 FIRE LOOP JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE FAULTY A VTZAEFD ENGINE SHUTDOWN ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27307UE 41021 75059 DURING TAXI CREW RECEIVED A FIRE INDICATION ON THE LT ENGINE. THE ENGINE WAS SHUTDOWN AND THE FIRE EXTINGUISHING SYSTEM WAS ACTIVATED AS A PRECAUTION. CREW VISUALLY VERIFIED NO VISIBLE FIRE. FLIGHT RETURNED TO GATE UNEVENTFULLY PASSENGERS WERE DEPLANED AT GATE. MAINTENANCE PERSONNEL VERIFIED NO FIRE WAS PRESENT AND FOUND THE ENGINE FIRE WIRE WAS PROVIDING A FALSE FIRE INDICATION. THE FIRE WAS REMOVED AND REPLACED. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T4 TRTA41NM E18NE 20030904001472003090400147WP 2003 9 4 DHL2003873567 120030703A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT ELEVATOR LOWER SKIN INBD SECTION DEFLECTED FROM STA XAR.0.000 TO XE132.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030618, ED-3435. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030618, ED3435. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL IAW EODHL-030618, ED-3435. CLEANED, TREATED AND PRIMED THE NEW SKIN INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON RT ELEVATOR LOWER SKIN PANEL INBD SECTION USING NEW FASTENERS IAW EODHL-030618, ED-3435, SRM 51-1-21 PG 1. SEE N/R 2157 FOR REBALANCING. SEE J/C BX3455074 FOR RT ELEVATOR REMOVAL AND INSTALLATION. 2L74 4F RT4A25 20030903002482003090300248EA 2003 9 3 03233637 120030821A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27637BR 7308 DURING MAINTENANCE INSPECTION THE OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OVERHEAD ENERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030904000882003090400088NM 2003 9 4 QXEA200300994 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GROOVED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 12 SEAT TRACK HAS A GROOVE IN THE LOWER SURFACE AT STATION X545.00. REPAIRED IAW DHC-8 RD 8-53-3644. 2H72 4T RTA13NM 20030812000472003081200047NE 2003 8 12 HEEA088427 120030731A21217650007901103 BLOWER SKRSKYS76 S76A 8143006NE CABIN COOLING INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 BLOWER ASSY FOUND TO BE INOPERATIVE. 1G72 3U H1NE 20030807000032003080700003NM 2003 8 7 USAASB03101 120030704A4900 APU BOEING737 7374B7 1384702NM AFT FIRE A USAAFD ACTIVATE FIRE EXT. RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 EA19785AU 25024 AFTER PUSHBACK FROM THE GATE, CREW REPORTED THE APU GENERATOR DROPPED OFF LINE. GORUND CREW ALERTED PILOT THAT THERE WAS AN APU TAILPIPE FIRE. NO APU FIRE DETECTION WAS NOTED BUT CREW ARMED AND DISCHARGED THE APU FIRE BOTTLE. THE MSY FIRE DEPARTMENT WAS CALLED AS A PRECAUTION. FLIGHT RETURNED TO THE GATE. (M) 2L72 4F RTA16WE 20030813001392003081300139 2003 8 13 SWAA031752 420030805A2565D31354 GIRT BAR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20030728000502003072800050 2003 7 28 SWAA031607 420030720A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030728000652003072800065NM 2003 7 28 SWAA031537 120030713A53116516301 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND RT BS 188 CHORD CRACKED AT WL 207. REMOVED AND REPLACED CHORD PER SRM. 2L72 4F RTA16WE 20030724000522003072400052NM 2003 7 24 SWAA031438 120030629A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS BROKEN AT ROWS NR 1, NR 17 AND NR 19. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030911001252003091100125WP 2003 9 11 DHL2003873545 120030630A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING CTR L/E FORMER CRACKED 0.250 AT STA XS.478.897. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE IAW 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE USING NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030912001612003091200161NM 2003 9 12 AWXA200300913 120030804A5320D5320226C20000 BRACKET AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 MCN - MINOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON UPPER ATTACH BRACKET (CLOSING PLATE) UNDER LT FUSELAGE PANEL 191AT AT FR 34, BS 1438. MAINTENANCE REMOVED CRACKED CLOSING PLATE AT FR 34, BS 1438; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PARTS IAW A319 SRM 51-42-11. 2L72 4F RTA28NM 20030930000352003093000035NE 2003 9 30 2003UALA00640 220030821A72303053557170 BEARING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 4 FAILED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29346UA14633505 24250 722381 NUMBER 1 ENGINE HAD SEVERE COMPRESSOR STALLS PASSING ABOUT 23000 FT EGT STABILIZED AT 610 WITH THROTTLE AT IDLE. WHEN THROTTLE INCREASED STALLS RESUMED. COMPRESSOR STALL AND INTERNAL GRINDING NOISE ON ENGINE SHUT DOWN. CAUSE OF THE COMPRESSOR STALL WAS A FAILED NR 4 BEARING. ALTHOUGH IT'S NOT A FREQUENT OCCURRENCE NR 4 BEARINGS IS AN INDUSTRY KNOWN FAILURE MODE. CFMI HAS ISSUED VARIOUS SERVICE BULLETINS TO IMPROVE NR 4 BEARING RELIABILITY. UA HAS INCORPORATED ALL NR 4 BEARING IMPROVEMENTS ON THE CFM56 FLEET ON ATTRITION BASIS. SHOP HAS INCORPORATED BEST PRACTICES BEARING HANDLING PROCEDURE TO PREVENT NR 4 BEARINGS FROM FAILING. 2L72 4F4 FRTA16WE E2GL 20030929000622003092900062CE 2003 9 29 ENHA200320808 120030904A2750262228112 BELLCRANK CESSNA208 208B 2073701CE ZONE 600 INOPERATIVE E ENHAK NONE O OTHER ININSP/MAINT 1 AL031229C 208B0589 FLAP BELLCRANK INSPECTION OF BELLCRANK FOUND WELDS AT MATING PORTIONS OF ASSEMBLY. ASSEMBLY DETERMINED SERVICEABLE HOWEVER COMPANY OPTED TO REMOVE FROM AIRCRAFT AND INSTALL REPACEMENT BELLCRANK. INSPECTION PROMPTED BY AL FSDO LETTER DATED 8/15/03. SUBJECT BELLCRANK REPLACED WITH P/N 2622311-7 OF NEW DESIGN. 1H71 3T A37CE 20031001000052003100100005NM 2003 10 1 QXEA200301073 120030828A5414 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 RT NACELLE INBOARD INNER SKIN HAS A CRACK AT RIVET JUST AFT OF PANEL 425AL. REPAIRED IAW DHC-8 SRM 51-00-06, RD 8-54-1838 AND HORIZON AIR EA 2-54-179. 2H72 4T RTA13NM 20030930000922003093000092EU 2003 9 30 180401 120030909A3150 WARNING LIGHT SAAB SF340 SF340A 7850100EU COCKPIT ILLUMINATED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL17104CQ 340A104 FLT 4507 ON TAKEOFF FROM CRW TO PIT ON 9/9/03 EXPERIENCED A CONFIGURATION WARNING ON TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. SUSPECT CONDITION LEVER BACKED OFF DURING ROLL AND CAUSED WARNING. 2L72 4T RTA52EU 20030930001322003093000132NM 2003 9 30 F3LA200300129 120030909A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT STA 312. REPLACED FLOORBEAM T-CAP AND SPLICES AT STA 312, RBL 24 TO LBL 34, PER SRM 53-10-51, FIG 205, 51-40-02, 51-10-02 AND SOPM 20-41-02. 2L72 4F RTA16WE 20031003000072003100300007EU 2003 10 3 AALA20030642 120030608A3350 SWITCH FOKKERF28 F28MK0100 4990807EU COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211400H 11340 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH TEST LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED EMERGENCY EXIT FLOOR PATH TEST LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030909002202003090900220EU 2003 9 9 BAQA085826 120030819A6220L673M20A1005 ACTUATOR UROCOPEC135 EC135T1 5620026EU MAIN ROTOR LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME1950 0143 MAIN ROTOR ACTUATOR LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20031006000902003100600090WP 2003 10 6 0301749937 120030915A2780 DUCT DOUG DC9 DC931 3022065WP RT WING DAMAGED A NWAALA ABORTED APPROACH UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 GL01908H 47517 ON SLAT EXTENSION DURING APPROACH FOR LANDING AT PDX, THE SLAT DISAGREEMENT LIGHT ILLUMINATED, THE SLAT EXTEND LIGHT DID NOT ILLUMINATE, AND THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO THE RT. COM PROCEDURES WERE PERFORMED AND THE FLIGHT CREW DIVERTED TO BOS DUE TO THE LONGER RUNWAY AND MAINTENANCE AVAILABLE THERE. MAINTENANCE WAS UNABLE TO FIND ANY ABNORMALITIES OF THE SLAT SYSTEM. THE REPLACEMENT OF THE RIGHT 'T' DUCT HAS BEEN DEFERRED. 2L72 4F A6WE 20031006001692003100600169NM 2003 10 6 SWAA031972 120030902A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 747 AT STR 19R, BS 757 AT STR 19R AND BS 797 AT STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031021002662003102100266NM 2003 10 21 03FDEA01581 120030918A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON SHEAR TIE AFT SIDE OF FRAME BS 1150 BETWEEN STR 26L AND 27L. REPAIRED SHEAR TIE IAW SRM 53-10-1, 53-10-4. 2L73 4F RTA3WE 20031028001172003102800117NM 2003 10 28 AALA20030972 120030905A2612W20168 SWITCH BOEING737 737823 13844BZNM COCKPIT INOPERATIVE A AALAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21963AN 29543 IAH - FLT 927 - FIRE WARNING TEST FAILED. CAPTAINS FIRE WARNING BELL CUTOUT SWITCH WAS INOPERATIVE. REPLACED CAPTAINS FIRE WARNING SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20031028001262003102800126SO 2003 10 28 SIMA200323903 120030826A261147359713 SMOKE DETECTOR EMB 135 EMB135KL 3260302SO CARGO BAY INOPERATIVE A SIMAO OTHER J WARNING INDICATION CRCRUISE 1 SW21843AE 145680 FLT 3595 - CRP - CREW REPORTED DURING CRUISE FILGHT THE CARGO FIRE DETECTION LIGHT CAME ON CREW FOLLOWED AOM PROCEDURES AND FIRED THE CARGO FIRE BOTTLES. LIGHT EXTINGUISHED AFTER 60 SECONDS. AFTER AN INSPECTION SYSTEM WAS PUT ON MEL. S/D - MAINTENANCE REMOVED AND REPLACED TEH CARGO SMOKE DETECTORS IAW EMB MM. OPS CHECK AND AIRCRAFT WAS RETURNED TO SERVICE AFTER REPLACING THE CARGO FIRE BOTTLE. (M) 2L72 4F RTT00011AT 20031028000572003102800057EA 2003 10 28 QXEA200301191 120030928A26129847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE ZONE 200 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 FORWARD CARGO BAY CENTER FIRE DETECTION CHIMNEY IS TORN. REMOVED AND REPLACED CHIMNEY. 2L72 4F4 FRTA21EA E15NE 20040204000852004020400085NM 2004 2 4 AWXA200301276 120031002A532069434772 CHANNEL BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT SIDE PLATE CHANNEL BS 767-787, RBL 20. MAINTENANCE REMOVED CORRODED RT SIDE PLATE CHANNEL BS 767-787, RBL 20; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 69-43477; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1, FIG. 2. 2L72 4F4 FRTA16WE E2GL 20031029000182003102900018NM 2003 10 29 ASAA0340112 120030305A542065C2630923 ANGLE BOEING737 7374Q8 138447QNM NR 2 PYLON CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND NR 2 PYLON OUTBOARD ATTACK ANGLE CRACKED. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031028001822003102800182NM 2003 10 28 ASAA0340078 120030227A531165C22910 FRAME BOEING737 7374Q8 138447QNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 500D RBL 5 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031103001042003110300104NM 2003 11 3 AWXA200301128 120030905A5310693535214 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK A .6250 INCH CRACK WAS FOUND ON STRINGER TIE CLIP (SHEAR TIE) AT BS 632, STR 1 RT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 632, STR 1 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7. 2L72 4F RTA16WE 20031105000502003110500050NM 2003 11 5 SWAA032303 120031018A53306545877 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER CUT OUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031107001012003110700101EU 2003 11 7 03309307 120031105A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27307UE 41021 DURING INSPECTION THE EMERGENCY TRACK LIGHTING FROM ROW 6-8 WAS FOUND INOPERATIVE. THE EMERGENCY BATTERY PACK WAS REPLACED AND THE SYSTEM OPERATIONAL CHECKED GOOD. 2L72 4T RTA41NM 20031110000552003111000055SO 2003 11 10 C2XA03SH437 120031109A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV- DURING C-CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031113000262003111300026EU 2003 11 13 BAQA089940 120031014A2821 HOUSING AEROSPAS365 AS365N2 8680815EU FUEL FILTER CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 781838 6417 FUEL FILTER HOUSING IS STRIPPED AND CRACKED. FAXED SCRAP CERTIFICATION WITH MMIR. REPLACED WITH SERVICEABLE UNIT. 10/15/03 1G72 3U RTH10EU 20040112001282004011200128NE 2004 1 12 2004F00030 220030908A72503044700 TURBINE BLADES BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE DAMAGED A GUUAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 WP1749543 UE181 114453 FLT 9240 - FLL - DURING LEFT ENGINE START AT APPROXIMATELY 30 PERCENT N1, A GRINDING NOISE WAS HEARD AND STRANGE VIBRATION FELT IN LEFT PROP LEVER. SHUT DOWN ENGINE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES FAILED. POWER SECTION HAS INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODULE AND ROUTED FAILED UNTI FOR FURTHER ANALYSIS AND REPAIR. (M) 2L72 4T4 TRTA24CE E26NE 20031121000542003112100054NM 2003 11 21 SWAA032492 120031110A53156546804 FLOORBEAM BOEING737 737317 138447PNM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 FLOORBEAM CORRODED AT RBL 22. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20031124000412003112400041CE 2003 11 24 DXTA200300160 120031112A3230 LANDING GEAR CESSNA750 750 2076810CE MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07958QS 7500158 ON APPROACH AFTER GEAR EXTENDED, GOT THREE GREEN AND THEN RED UNSAFE LIGHT ILLUMINATED. BLEW GEAR DOWN BY PNEUMATIC BOTTLE. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20031126000042003112600004NM 2003 11 26 QXEA200301465 120031120A5210 DOOR SEAL BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DEFECTIVE A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09402QX 4032 YYC- ON FLIGHT 2329 AIRCRAFT RETURNED TO FIELD, LOST PRESSURIZATION AT 1500 FEET AFTER TAKEOFF. FLIGHT ATTENDANT NOTICED DAYLIGHT AROUND MAIN CABIN DOOR SEAL. RAN PRESSURIZATION FAIL CHECKLIST AND WERE UNABLE TO REGAIN PRESSURIZATION. REMOVED AND REPLACED FORWARD PASSENGER DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031126000552003112600055NM 2003 11 26 CALA0300660 120030715A5753 SKIN BOEING737 7373T0 1384582NM T/E FLAP DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND TWO DENTS ON BOTTOM I/B SURFACE OF LEFT AFT NR 2 T/E FLAP. REPAIRED PER SRM 57-53-02, 51-70-10. 2L72 4F RTA16WE 20031212000722003121200072WP 2003 12 12 03FDEA01918 120031116A3230 FUSE DOUG DC10 DC1030 3023501WP RT MLG WW TRIPPED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25304FE 46992 LANDING GEAR HANDLE WOULD NOT MOVE TO LANDING GEAR POSITION. RAN RED TABS AND THAT (DEPRESS THE HANDLE RELEASE BUTTON & RAISE - ENSURE NOSE GEAR STEER CENTERED) DID NOT HELP. RETURNED FOR NORMAL LANDING. FOUND THE MAIN GEAR TRIM INTERLOCK FUSE HAD TRIPPED IN THE RT MAIN GEAR W/W. BLED SYSTEM HYDRAULICS, RE-SET FUSE. PINNED ALL GEAR & PERFORMED A RETRACTION TEST. OPS CHECK WAS GOOD. SAFETIED FUSE. REF DC10-30 M/M 32-31-06-2 ENT BY: 157364 RPT BY: 157364. 2L73 4F A22WE 20031218000262003121800026SO 2003 12 18 C2XA03BT112 120031125A2611FDS765A2 SENSOR EMB 145 EMB145ER 3260211SO CARGO BAY FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2717928 145007 CREW REPORTED, MASTER WARNING AND LAVATORY SMOKE INDICATION ON EICAS. AIR RETURNED TO EWR, LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR SENSOR (PART NUMBER: FDS765A-2 SERIAL NUMBER: 203574) IAW EMB145 AMM 26-14-01. REMOVED AND REPLACED SMOKE DETECTOR PANEL FORWARD GALLEY (PART NUMBER: FAU751A-4 SERIAL NUMBER: 042797) IAW EMB145 AMM 26-14-02, RAN BOTH ENGINES TO TAKEOFF POWER FOR FIVE MINUTES OPS CHECKED GOOD, LAVATORY SMOKE DETECTION SYSTEM OPS CHECKED GOOD IAW EMB145 AMM 26-14-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031218000542003121800054EA 2003 12 18 03332658 120031128A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 DURING INSPECTION THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNED OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031223000232003122300023NM 2003 12 23 SWAA032626 120031130A5310141A880 WINDOW POST BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED 1/4D CHECK, FOUND RT COCKPIT WINDOW POST CRACKED AT UPPER INBD CORNER. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20031229000262003122900026NE 2003 12 29 COMA0360551 220031211A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT SMOKE A COMAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO01735CA20802 7267 807100 FLIGHT 5357 SMOKE TOILET MESSAGE. F/A REPORTED HAZE IN CABIN. REPLACED THE RT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040105000912004010500091WP 2004 1 5 DHL2003802547 120031114A5310 DOOR FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 EXTERNAL FUSELAGE FWD PASSENGER DOOR JAMB AFT LWR CORNER CRACKED 0.750 STA 55.000, L20 - L21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 15, SERVICE REWORK DWG SRO8530021, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 15, SERVICE REWORK DWG SRO8530021, DWG 5750776. FABRICATED FILLER DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 15, SERVICE REWORK DWG SRO8530021, DWG 5750776. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER AND TRIPLER AND AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER AND TRIPLER WITH NEW FASTENERS. 2L74 4F RT4A25 20040106000322004010600032WP 2004 1 6 DHL2003802561 120031124A532081763 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 798.000 RBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 798.000 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201844 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031231000652003123100065WP 2003 12 31 GTIA030913 120031105A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND CABIN FLOOR PANEL CENTER STATION 465-541 INSERTS BROKEN OUT. FABRICATED NEW CABIN FLOOR PANEL. (M) 2L72 4F RTA6WE 20030912001712003091200171WP 2003 9 12 AALA20030881 120030820A3397 WIRE DOUG DC9 DC983 3022083WP AFT AIRSTAIRS LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21974TW 53624 DFW - FOUND AFT STAIRWAY HAS ONE OVERHEAD EMERGENCY LIGHT INOPERATIVE. FOUND WIRES TO SOCKET ASSEMBLY OF LIGHT LOOSE. SECURED WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030919000442003091900044NM 2003 9 19 IU62003F00028 120030613A2761654494715 HOUSING BOEING737 737* NM SPOILER ACTUATORCRACKED B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 4768814210 6099 SPOILER ACTUATOR HOUSING CRACKED AROUND SHOULDER ON THE INSIDE DIAMETER OF THE HOUSING. OLD STYLE HOUSING IS SUSECPTIBLE TO CRACKING. REPLACE WITH NEW STEEL HOUSING. (NR 178260) 2L72 4F RTA16WE 20030731000282003073100028NM 2003 7 31 QXEA200300823 120030711A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - PANEL 261FT CHAFED AFT FLANGE. REPAIRED IAW Q400 RD 8/4-53-521, PAGE 8, STEP 9 AND RD 8/4-53-521, STEP 9. 2H72 4T RTA13NM 20040112000692004011200069NM 2004 1 12 DHL2003780016 120031220A5270C210211 SWITCH BOEING727 727223 1384074NM PAX DOOR FAULTY A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01780DH 22006 FORWARD ENTRY DOOR AMBER LIGHT ILLUMINATED DURING TAXI IN. REMOVED AND REPLACED FORWARD ENTRY DOOR SWITCH, OPS CHECKED GOOD IAW 52-11-01. P/N: C2-1021-1. 2L73 4F A3WE 20040108000712004010800071CE 2004 1 8 E812003F00001 120031006A3397L173C18 WIRE BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA LANDING LIGHT CHAFED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL03200ZT1804 BB1393 INVESTIAGATED COMPLAINT OF LT LANDING LIGHT NOT ILLUMINATING. FOUND LT LANDING LIGHT POWER SUPPLY WIRE L173C18 CHAFED THROUGH AND CORRODED AT APPROXIMATE HALFWAY POINT BETWEEN LANDING LIGHT AND NOSE WHEEL WELL CONNECTOR P509. CHECKS SHOWED VOLTAGE PRESENT AT TERMINAL, BUT UNABLE TO LIGHT LAMP. SUGGEST A MORE DETAILED INSPECTION OF LANDING GEAR WIRING BE CONDUCTED IN CONJUNCTION WITH LANDING GEAR 6 YEAR/ 8000 CYCLE INSPECTIONS. 1L72 4T3 T A24CE E2NE 20040108001162004010800116SO 2004 1 8 K5S2003F00000 120030925A32301025572 SEQUENCE VALVE PIPER PA46 PA46500TP 7104622SO PWA PT6 PT6* 52043EA NLG LEAKING B K5SRO OTHER O OTHER NRNOT REPORTED 1 NM0753369139 4697088 PILOT REPORTED HYDRAULIC LIGHT ON AFTER TAKE OFF. RETURNED AND FOUND NLG SEQUENCE VALVE LEAKING. REMOVED AND REPLACED VALVE. 1L71 3O3 TRTA25SO E2NE 20031118000852003111800085 2003 11 18 LA02003F00000 420030923A611314422B SPINNER PIPER PA18 PA18135 7101820SO LYC O290 O290* 41506EA MCAULY1A200 1A200* GL PROPELLER CRACKED E LAOAO OTHER O OTHER NRNOT REPORTED 1 AL051590P 183755 UG46004 SPINNER CONTACTS PROPELLER BLADES AT LEADING EDGE AND TRAILING EDGE OF BLADE CUTOUTS IN THE SPINNER. A GROOVE HAS BEEN WORN INTO THE PROPELLER BLADES, WITH THE WORST BEING .080 INCH DEEP AND .9 INCH LONG ON THE LEADING EDGE OF ONE BLADE. SPINNER AND BOTH SPINNER BACKPLATES WERE DESTROYED BY CRACKING CAUSED BY THE LACK OF MATERIAL THAT WAS WORN BY PROPELLER INTERFERENCE. DAMAGE OCCURRED DUE TO NORMAL OPERATIONS, WITH NO KNOWN STRIKE TO EITHER THE PROPELLER OR SPINNER ASSY. TO PREVENT RECURRENCE, A SPINNER ASSEMBLY NEEDS TO BE INSTALLED WITH EITHER LARGE ENOUGH BLADE CUTOUTS, OR EXTENDED BACKPLATES TO PREVENT INTERFERENCE WITH THE PROPELLER. DAMAGE WAS FOUND DURING AN NORMAL INSPECTION. 1H71 3O3 O 1A2 E229 5 NP874 20031118000732003111800073WP 2003 11 18 CALA0300579 120031008A5347 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714831 49491 INSPECTION FOUND FORWARD BAGGAGE BIN RT AFT CARGO TRACK CORRODED AT ATTACH SCREWS IN THREE PLACES FROM STA 465-503. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01. 2L72 4F A6WE 20040112001812004011200181EU 2004 1 12 I05R091299 120031017A5210677110123 LATCH SNIAS 350 AS350* EU TMECA ARRIELARRIEL2B NE DOOR HANDLE FAILED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 760 3560 DOOR SPRING FAILURE REMOVED DOOR INNER PANEL AND FOUND BROKEN SPRING AT THE LATCH ARM. REPLACED SPRING. 1G71 3U3 U H9EU E00054EN 20040113000872004011300087NM 2004 1 13 AWXA200301599 120031219A5320143N5140 INTERCOSTAL BOEING757 7572G7 1384963NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK A 2 INCH CRACK WAS FOUND ON CABIN FLOOR INTERCOSTAL BS 860-880, BL-0. MAINTENANCE REMOVED CRACKED INTERCOSTAL BS 860-880, BL-0; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51 FIG 204, PG 214-215. 2L72 4F RTA2NM 20031212001302003121200130NM 2003 12 12 AWXA200301436 120031105A5311651758267 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN FRAME WEB VERTICAL BEAM AT FASTENER HOLE AT BS 178, RBL 17.1, WL 183. MAINTENANCE CUT OUT DAMAGE IN FRAME WEB VERTICAL BEAM AT BS 178, RBL 17.1, WL 183; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A DOUBLER; INSTALLED REPAIR PARTS IAW SRM 53-10-08, PG 288K-288X, FIG 212. 2L72 4F RTA16WE 20031217001462003121700146EA 2003 12 17 COMA0370055 120031211A2721CC670511143 PANEL CNDAIRCL600 CL6002C10 1390015EA RUDDER TRIM MALFUNCTIONED A COMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO01368CA 10075 DURING TAKE OFF RUDDER TRIM MOVED 1 UNIT LT. REPLACED THE RUDDER TRIM SWITCH PANEL. 2L72 4F RTA21EA 20031223000882003122300088NM 2003 12 23 SWAA032699 120031210A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND STRINGER 15 L CRACKED AT BS 380 FRAME. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040105000322004010500032NM 2004 1 5 DL764031015 120031114A3350 CONNECTOR BOEING767 767432ER 1385134NM SEAT 48 F&G LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27833MH 29706 ON TRANSIT CHECK THE EMERGENCY LIGHTS AT ROWS 42 TO 47 F&G DID NOT TEST. RESEATED CONNECTOR AT SEAT 48 F&G, OPS CHECK GOOD. 2L72 4F RTA1NM 20031121000902003112100090NM 2003 11 21 03FDEA01942 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 LEFT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING BARREL NUT BOLT HOLE LOWER CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20031125000212003112500021WP 2003 11 25 DHL2003809553 120031101A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LOWER CTR FUSELAGE SKIN HAS OIL CAN, STA 857.000 - 879.000. REMOVED OIL CAN SKIN IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SKIN IAW SRM 53-2-0 PG 1, 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SKIN ON LOWER CTR FUSELAGE STA 857.000 - 879.000 L-36 WITH NEW FASTENERS IAW SRM 51-1-15 PG 1, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031124000752003112400075NM 2003 11 24 QXEA200301409 120031108A7600 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 400 OUT OF ADJUST A QXEAO OTHER R PARTIAL RPM/PWR LOSS APAPPROACH 1 NM09368PH 512 ON FLIGHT 2172 DURING APPROACH WHEN BRINGING CONDITION LEVERS TO 1050, POWER LEVERS FLIGHT IDLE NR 1 ENGINE SURGED FOR ABOUT 2 SECONDS. WHEN POWER LEVERS WERE ADVANCED AHEAD OF FLIGHT IDLE SURGE STOPPED. UPON INSPECTION FOUND NR 1 POWER LEVER BETA BACKUP SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031202000912003120200091EA 2003 12 2 ASOA03339 120030726A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 DURING A GROUND INSPECTION IN DFW, THE LEFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031203000672003120300067NM 2003 12 3 USAA030204 120030926A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 PIT - FOUND SKIN CRACKED .25 INCH, AFT SERVICE DOOR UPPER HINGE STATION 951. INSTALLED DOUBLER PER SRM 53-60-01 FIG 205. (M) 2L72 4F RTA16WE 20040122000462004012200046WP 2004 1 22 2004F00049 120030821A7603 THROTTLE DOUG DC9 DC931 3022065WP PWA JT8 JT8D NE LT ENGINE BINDING A A4JAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO35933JK 48159 667239 EN ROUTE TO FLL, LT ENGINE THROTTLE BEGAN BINDING. LT THROTTLE WOULD NOT RETARD BEYOND MIDWAY, APPROXIMATELY 1.4 EPR. ALL OTHER ENGINE PARAMETERS INDICATED NORMAL. PERFORMED EMERGENCY SINGLE ENGINE LANDING INTO FLL. (M) 2L72 4F4 F A6WE E2EA 20031203000162003120300016NM 2003 12 3 GAIA03121ST 120031024A57117075T6 STIFFENER BOEING727 727243 138408DNM RT WING SPAR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND RIGHT WING FRONT SPAR VERTICAL STIFFENER CRACKED AT WBL 90.5. REF FASI N/R NR 61293. INSTALLED DOUBLER REPAIR 7075-T6 .063 5.5 INCH BY 2.5 INCH IAW B727 SRM 57-10-2 AND 51-40-3 FIG 3. (M) 2L73 4F RTA3WE 20031204000592003120400059WP 2003 12 4 GTIA030842 120031006A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND FORWARD CABIN FLOORBOARD STATION 200 TO STATION 256 LBL 14.5 TO LBL 21 HAS SEVERAL INSERTS BROKEN OUT, CORRODED, SOFT/MUSHEY. FABRICATED NEW FLOOR BOARD. (M) 2L72 4F A6WE 20031205000392003120500039NM 2003 12 5 DLM88030929 120031016A2530 OVEN DOUG MD88 MD88 3023688NM AFT GALLEY ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27918DE 49959 F/A REPORTS BAD ODOR, LIKE BURNING OIL IN AFT LEFT CABIN AS A/C WAS CLIMBING THRU FL 280 TO FL 300. ODOR LASTED APPROX 2 TO 3 MINS AND DISSIPATED. ODOR DID NOT RETURN. REPLACED DIRTY OVEN. 2L72 4F RTA6WE 20031209002522003120900252NM 2003 12 9 UPS03241537 120031019A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, NLG WW BS 259 SUSPECT CRACKS AT RIVETS AT RT AFT PRESSURE PANEL FWD EDGE. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC CONFIRMS DEFECT FREE CUTOUT. REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1. 2L73 4F A3WE 20031205000552003120500055NM 2003 12 5 MWEA030434 120031022A2450 RELAY DOUG MD88 MD88 3023688NM APU DIRTY A MWEAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 GL31601ME 49762 ON ENGINE START, RIGHT ENGINE GENERATOR WOULD NOT PICK UP THE LOAD FROM THE APU GENERATOR ON SUBSEQUENT STARTS, RELAY TRANSFERRED NORMALLY. CLEANED CONTACTS ON RIGHT VOLTAGE REGULATOR, RAN RIGHT ENGINE, OPERATIONS CHECK. 2L72 4F RTA6WE 20031210000342003121000034WP 2003 12 10 AALA20031307 120031121A3397 WIRE DOUG DC9 DC982 3022082WP TAILCONE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21464AA 49594 DFW TAIL CONE EJECT HANDLE EMERGENCY ILLUMINATION LIGHT INOPERATIVE. REPAIRED TAIL CONE EJECT HANDLE EMERGENCY ILLUMINATION LIGHT WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031210001692003121000169NM 2003 12 10 CALA0300680 120031201A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716649 28910 INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 967-990. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20031014001722003101400172 2003 10 14 SWAA032082 420030918A256565C19901 CABLE BOEING737 7372H4 138448CNM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29080SW 22675 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVAC SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F A16WE 20031014000562003101400056 2003 10 14 SWAA032178 420031001A2565 INDICATOR BOEING737 7373Y0 1384671NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031010000632003101000063 2003 10 10 SWIA200312414 420030914A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER OI OTHER FLT. ATTITUDE INST. NRNOT REPORTED 1 NM07215SW4832 4832 120281 F/O'S FLIGHT DIRECTOR WILL NOT CAPTURE GLIDE SLOPE. REPLACED F/O'S AUTOPILOT COMPUTER. SYSTEM TESTS NORMALLY PER MM 22-11-00. 2L72 4T RTA31SO 20030923000522003092300052WP 2003 9 23 DHL2003604654 120030611A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT INNER WING CTR L/E LOWER PLATING SHOWS THREE INTERIM REPAIRS AND CORROSION AROUND STA XFS 304.000. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.071) AND TWO FILLERS (7075-T6 AL0.063 EACH ONE) IAW EODHL-030542, ED-3289. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER ON LT INNER WING CTR L/E LOWER PLATING AROUND STA XFS.304.000 WITH NEW FASTENERS IAW EODHL-030542, ED-3289, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030925000242003092500024EU 2003 9 25 ASOA03410 120030816A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11633AS 344 DURING A C-CHECK IN BNA, THE LEFT AND RIGHT SEAT TRACKS AT FRAMES 36 THROUGH 39, AND THE LEFT SEAT TRACK AT FRAMES 39 THROUGH 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS AT FRAMES 36 THROUGH 39, AND THE LEFT SEAT TRACK AT FRAMES 39 THROUGH 41 IAW SRM 51-25-00 AND 51-25-04. (M) 2H72 4T RTA53EU 20040407000732004040700073NE 2004 4 7 BJNA031201 220031217A7200 ENGINE BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE NR 1 FAILED A CF ABORTED TAKEOFF ACTIVATE FIRE EXT. MBJOVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 WP11233TM 23043 709303 ON TAKEOFF AT 80 KNOTS, NR 1 ENGINE FAILED. THE TOWER REPORTED THE ENGINE WAS ON FIRE, NO FIRE WARNING INDICATION. DISCHARGED THE FIRE BOTTLE. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. FAILURE CAUSE NOT DETERMINED, ENGINE PARTED OUT AND SOLD. 2L72 4F4 FRTA16WE E2EA 20031216000452003121600045NM 2003 12 16 SWAA032531 120031117A53106546559 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 927, LBL 4 TO RBL 4. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040713001582004071300158NM 2004 7 13 MEX2003560 120031223A29337586631 INDICATOR BOEING757 7572Q8 1384972NM NR 2 ENGINE LEAKING A ASMFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW23805AM 26272 FLT 494 - MEX-LAX - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING IN GDL AS CONSEQUENCE OF THE RIGHT QUANTITY INDICATION DECREASE TO .08 QUARTS. AT PLATFORM, THE HYDRAULIC SYSTEM WAS REPLENISHED TO DETECT THE LEAKAGE, THE DIFFERENTIAL PRESSURE INDICATOR WAS REPLACED AND SYSTEM TESTED IAW MM 29-11-17. DURING OVERNIGHT SERVICE IN MEX, THE HYDRAULIC LINES WERE REVISED IAW MM 29-11-17, ALL CORRECT. (M) 2L72 4F RTA2NM 20040713000922004071300092NM 2004 7 13 S2YA03036 120031209A21304068B000002 FLOW VALVE DORNERDO32 DO328300 NM CABIN PRESSURE INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13358SK5881 3188 FLT 2158 - MKE-IND, DURING TAKEOFF, THE CREW NOTED A RT PACK BLUE CASS MESSAGE FOLLOWED BY A BLEED SOV YELLOW CASS MESSAGE. THE ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE FLOW CONTROL VALVE, OPS CHECKED THE SYSTEM AND RETURNED THE A/C TO SERVICE. (M) 2H72 4T RTA55NM 20040802001572004080200157SW 2004 8 2 2004F00206 120031121A2910SS10127 PRESSURE SWITCH FRCHLDSA227 SA227DC 3377521SW HYD SYSTEM FAILED A BSAAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 NM05854LS DC854B FLT 2578 - MLS - FOUND LEFT HYDRAULIC LOW PRESS WARNIG LIGHT CAME ON WHEN FLAPS WERE LOWERED. HYDRAULIC PRESSURE REMAINED AT 2,000 PSI. CREW RETURNED TO MAIN BASE, ALTERNATE LANDING LOCATION, DUE TO REPORTED ICING CONDITIONS AND WEATHER AT DESTINATION STATION. HYDRAULIC PRESSURE SWITCH FAILURE. REPLACED LEFT HYDRAULIC PRESSURE LOW SWITCH. (M) 2L72 4T RTA18SW 20030925001032003092500103EU 2003 9 25 174062403 120030624A24205243212161 SHAFT PILATSPC12 PC1245 7090551EU NR 2 GENERATOR SHEARED E S4WAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 WP07562NA 174 NR 2 GENERATOR DRIVE SHAFT SHEARED. 1L71 3T RTA78EU 20040818001722004081800172EU 2004 8 18 KBM2004F00141 120030910A54100292808740 STRAP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HEAT SHIELD WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 ENGINE MO 5 HEAT SHIELD STRAP BRACKET HEAT SHRINK IS WORN. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20060801001532006080100153WP 2006 8 1 IXXA060596S 120030910A5753 WEB DOUG DC8 DC871F 302199DWP ZONE 600 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INBOARD LEADING EDGE WEB HAS TWO RIVETS IMPROPERLY INSTALLED, ONE HAS A DOUBLE DRILLED HOLE AT STATION XW3. REMOVED DAMAGED WEB, FABRICATED NEW WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW WEB. IAW DC8 SRM 51-3-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20030814000922003081400092WP 2003 8 14 UPS03841036 120030706A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, LONGERON 17R CRACKED AT STA 1770-1780 (INSIDE DOOR 60). REMOVED LONG 17RT TO FOM, FABBED NEW -35 SPLICE DOUBLER IAW DAC DWG 5 649327. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONG 17 RT IAW DAC DWG 5649327. 2L74 4F RT4A25 20030814001422003081400142WP 2003 8 14 GTIA030576 120030708A5320 STRUCTURE DOUG DC9 DC982 3022082WP SUB FLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND SUB FLOOR AT STATION 200 RBL 24 HAS CORROSION. CUT OUT DAMAGED SECTION OF SUB FLOOR. FABRICATED NEW SUB FLOOR SECTION AND DOUBLERS. INSTALLED SUB FLOOR AND DOUBLERS. (M) 2L72 4F A6WE 20030819001332003081900133NM 2003 8 19 UPS03640998 120030725A2780834503 PROXIMITY SENSOR BOEING767 767300 1385204NM L/E SLATS INOPERATIVE A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01324UP 27750 INSPECTION TYPE: ETOP, DIVERTED DUE TO EICAS MSG, L/E SLAT ASYM DISPLAYED, L/E LIGHT ILLUM WITH FLAP LEVER UP. EICAS MSG ILLUMINATED MULTIPLE TIMES. PSEU BITE TEST CARRIED OUT IAW FIM 32-09-03. OUTBOARD N010 PROX SENSOR 296 INDICATES INOP, PROX SENSOR REPLACED AND TESTED IAW AMM 27-88-01. 2L72 4F RTA1NM 20030819002042003081900204 2003 8 19 SWAA031775 420030809A2565 INDICATOR BOEING737 7377H4 1384404NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29782SA 0118A 29808 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030819001322003081900132NM 2003 8 19 UPS03440997 120030723A5532 SKIN BOEING747 747121 1384871NM VERTICAL STAB DAMAGED A IPXAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO01682UP 20349 ON WALKAROUND INSPECTION FOUND DAMAGE (FROM WING PANEL DEPARTING) ON VERTICAL FIN LT SIDE DAMAGE APPROX 24 X 15 INCHES. ACCOMPLISHED INTERIM REPAIR TO VERTICAL STABILIZER PER EO B747-5100-19 029. 2L74 4F A20WE 20030331001212003033100121NM 2003 3 31 DHL2003740501 120030203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FWD CARGO FRAME HAS 2 DENTS INTO THE RADIUS AT BS 700 STR 23 AT 24R. REMOVED FASTENERS FOR ACCESS PER SRM 51-30-2. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER (7075-T6 .063 PER SRM 53-10-2 FIG 11 AND 51-40-0 FIG 1. ALODINED AND PRIMED PER SRM 51-10-2 AND INSTALLED REPAIR PER SRM 51-40-3 PG 1. 2L73 4F RTA3WE 20030401000282003040100028EA 2003 4 1 ASOA03048 120030207A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11848AS 7339 DURING DESCENT INTO MLB FROM ATL, AS THE AUXILIARY POWER UNIT WAS POWERED UP EXTREME JET FUEL FUMES OCCURRED IN THE CABIN THROUGH THE ENVIROMENTAL CONTROL SYSTEM. THE CREW SHUT DOWN THE AUXILIARY POWER UNIT AND THE AIRCRAFT LANDED SAFELY IN MLB. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401001572003040100157WP 2003 4 1 DHL2003804667 120030204A5710576998592 VANE DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING L/E INBD. VANE SHOWS HOLES ELONGATED , XS247.000 PERFORMED MAJOR REPAIR IAW EO DHL 030104 , ED-3208. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 TRIMMED OUT DAMAGED SKIN SEGEMENT IAW EA DHL 030104, ED-3208 FABRICATED REPAIR DOUBLER. A FILLER 7075T6 AL 0/063 AND INTERNAL DOUBLER IAW EO DHL 030104 , ED-3208. CLEANED , TREATED AND PRIMED INTERIOR SURFACES IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG. 1 INSTALLED FILLER AND DOUBLERS IN RT WING L/E VANE WITH NEW FASTNERS IAW EO DHL 030104 , ED-3208, SRM51-1-21 PG 1. 2L74 4F RT4A25 20030822000172003082200017NM 2003 8 22 03FDEA00809 120030523A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP - HINGE AFT FITTING FOUND OUTBOARD ACTUATOR BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69255 - WINGS - RIGHT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030403001132003040300113NE 2003 4 3 DL72W030192 220030224A7314 PUMP BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 1 FUEL FAILED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27297WA 22534 700301 AIR TURNBACK, NR 1 ENGINE. REPLACED FUEL PUMP AND CONTROL. 2L73 4F4 F A3WE E2EA 20030404000372003040400037NM 2003 4 4 DL73K030274 120030323A3233654462514 ACTUATOR BOEING737 737247 138448DNM NLG BROKEN A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO27243WA 23517 ON APPROACH INTO MCO NOSE LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. OK ON SECOND ATTEMP AND LANDED WITH OUT INCIDENT. AMT FOUND LOCK ACTUATOR FAILED CAUSING 1 INCH DIAMETER HOLE IN FWD PRESS BULKHEAD NOSE WHEEL WELL. 2L72 4F A16WE 20030401001392003040100139NM 2003 4 1 DHL2003749004 120030401A2697 WIRE BOEING727 727200 138407ENM SWITCH BROKEN A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01749DH 22013 GLARESHIELD BELL CUTOUT SWITCH DOES NOT WORK. REPAIRED BROKEN WIRE ON CUTOUT SWITCH IAW M/M 20-11-0. CUTOUT SWITCH OPS CHECKED GOOD. 2L73 4F RTA3WE 20030410000682003041000068WP 2003 4 10 GTIA030100 120030213A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FORWARD CABIN STATION 200-260 RBL 24 TO 44 FLOORBOARD HAS CORROSION AT INSERTS/SOFT MUSHEY. FABRICATED PANEL. (M) 2L72 4F A6WE 20030415000412003041500041WP 2003 4 15 CA030320004 120030307A2910D2022 BRACKET ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA HYD SERVO CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) IN COMPLIANCE WITH SB 45 HYDRAULIC SERVO BRACKET D202-2 WAS REPLACED WITH D202-2 REV.F. THE BRACKET WAS FOUND TO BE CRACKED IN THE BEND RADIUS WHICH PROMPTED THE SB. 1G71 3O3 O H11NM E295 20030408001012003040800101NM 2003 4 8 2003UALA00354 120030401A3350 POWER SUPPLY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29361UA 24454 DURING PREFLIGHT INSPECTION, FLIGHT CREW REPORTED THAT SECTIONS OF EMERGENCY EXIT LIGHTING (EEL) WAS INOPERATIVE. SUPPLEMENTAL DATA UPDATE REPAIRED POWER STRIP, CHECKS NORMAL. 2L72 4F4 FRTA16WE E2GL 20030416001312003041600131SO 2003 4 16 C2XA03CL089 120030409A4930MS2877304 O-RING EMB 145 EMB145LR 3260212SO APU DEFECTIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW2713995 145295 CLE FLIGHT 2230 CREW REPORTED STRONG FUEL ODOR WITH NR 1 PACK BEING SUPPLIED BY APU BLEED. MAINTENANCE REMOVED AND REPLACED O-RING AND RETAINING RING ON FUEL SOLENOID. OPERATIONAL AND LEAK CHECKS GOOD. 2L72 4T RTT00011AT 20030417000322003041700032NE 2003 4 17 MALA030125 220030126A7230 ENGINE SAAB SF340 340B 7860101EU GE CT7TS CT72B 30030NE RIGHT STALLED A MALAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL15414XJ 340B414 DURING FLIGHT, RT ENGINE COMPRSSOR STALLED & OVERTEMPED. AIR RETURN TO INL. CREW REPORTED, GOING THRU 500 FT WHILE DIALING DOWN CTOT, RT ENGINE SUFFERED COMPRESSOR STALL. DUE TO COMPRESSOR STALL, ENGINE TEMP EXCEEDED 970 DEGREES FOR 31 SECONDS BEFORE STALL WAS CLEARED BY PULLING POWER LEVER BACK. STALL WAS SUFFICIENT TO CAUSE RT PROP TO AUTOCOARSEN. EVENT DISCUSS WITH GE SERVICE ENGINEER, DISCUSSION CENTERED AROUND INSPECTION FOR FERRY FLIGHT FOR ENGINE CHANGE, AND WHY THIS KEEPS OCCURING, THIRD COMPRESSOR STALL EVENT AT MESABA SINCE 12/7/02. GE IS INVESTIGATING. THE ONLY ADVICE GE CAN OFFER AT THIS TIME IS TO DO AN ECS ON TAKEOFF FOR FIRST FLIGHT OF DAY. 2L72 4T4 URTA52EU E8NE 20030425000382003042500038EU 2003 4 25 RAIA00303084 120030325A3230DHE1148 SQUAT SWITCH AEROSPATR72 ATR72202 8680940EU MLG FAILED A RAIAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 CE03722TE9 220 STL- LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR WEIGHT ON WHEEL SWITCH, OPS CK OK. 2H72 4T RTA53EU 20030430000282003043000028NM 2003 4 30 AWXA200300441 120030428A335032145410 BATTERY PACK AIRBUSA319 A319132 3930340NM ZONE 242 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28823AW7565 1463 PHX - EEL - DURING INSPECTION EMERGENCY LIGHT TEST FAILED ON CIDS. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY POWER SUPPLY UNITS (10WL-13WL) AND BATTERY PACKS, OPERATIONAL CHECK WAS GOOD IAW 33-51-38-401. PART NAME, EPSU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 3718, LOC; POS NR 1 (10WL) ZONE 221, TT; 7556, TC; 2895. PART NAME, EPSU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 3656, LOC; POS NR 2 (11WL) ZONE 241, TT; 7556, TC; 2895. PART NAME, EPSU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 3712, LOC; POS NR 4 (13WL) ZONE 263, TT; 7556, TC; 2895. 2L72 4F RTA28NM 20030429002202003042900220 2003 4 29 SWAA030804 420030409A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29420WN 29825 FWD SERVICE DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030505000142003050500014SO 2003 5 5 C2XA03TY048 120030415A531514521721005 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715527 145413 TYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE WAS FOUND CORRODED AFT OF THE COCKPIT STEP IN THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE CENTER FORWARD DIGITAL IAW EMB-145 SRM 53-21-10, 51-40-02, 51-21-04/05 AND 06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20030505002232003050500223NM 2003 5 5 03FDEA00550 120030421A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION FWD CARGO BAY 740 LWR CHORD RBL 12 WL 148.5 UPPER SURFACE AROUND FASTENERS. 2L73 4F RTA3WE 20030502002362003050200236WP 2003 5 2 ABXA030135 120030416A5610 WINDOW DOUG DC9 DC931 3022065WP COCKPIT MISALIGNED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 FIRST OFFICER'S WINDOW WOULD NOT OPEN. FOUND SCREW IN UPPER FORWARD CORNER OF FIRST OFFICER'S WINDOW TO BE TO LONG AND MIS-ALIGNED WINDOW TRACK. REPLACED WITH SHORTER SCREW. WINDOW OPS CHECKED GOOD IAW DC-9 MM 56. 2L72 4F A6WE 20030506000912003050600091NM 2003 5 6 PCA0300850 120030412A5330 SKIN BOEING747 747249F 1384849NM FUSELAGE PUNCTURED A P5CAO OTHER K FLUID LOSS ININSP/MAINT 1 WP23920FT 22237 FUSELAGE SKIN PUNCTURE BS 2598 BETWEEN S25R, S26R JACKING INCIDENT DURING C-CHECK AT SIN. 2L74 4F A20WE 20030508000662003050800066NM 2003 5 8 DL76G030355 120030413A2530811150417 COFFEEMAKER BOEING767 767332 1382001NM GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO271608 30573 AT DEPARTURE F/A INFORMED OF A SMOKE ODOR AT AFT RT GALLEY COFFEEMAKER AREA. REMOVED NR 1 AND NR 2 COFFEEMAKER AND FOUND WIRES OK. NOTICE AN ODOR AT NR 2 COFFEE MAKER. REPLACED NR 1 AND 2 COFFEEMAKERS IN AFT RT GALLEY. OPS OK. 2L72 4F RTA1NM 20030509000412003050900041SO 2003 5 9 SIMA200309605 120030402A531514525381003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE LEFT FLOORBEAM BETWEEN FRAMES 24 AND 25. REMOVED CORROSION BY PERFORMING A 4.5 INCH CUTOUT. FABRICATED A DOUBLER ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM 145/1142 REV 20, 53-21-10, AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030514000622003051400062NM 2003 5 14 SWAA030961 120030429A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20030513002092003051300209NM 2003 5 13 QXEA0300485 120030419A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 GOUGE IN FUSELAGE SKIN AT X71 AND STRINGER 29R. REPAIRED IAW HORIZON AIR EA 6-53-247 AND RD8/4-53-530. 2H72 4T RTA13NM 20030604000752003060400075NM 2003 6 4 UPS03440489 120030410A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 AFT CARGO BELOW FLOOR SHEAR TIE FOUND CRACKED AT BS 1880 BETWEEN STR 43L AND STR 44L AS MARKED. AFT CARGO BELOW FLOOR SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A AT BS 1880 BTN STR 43L AND STR 44L. 2L74 4F A20WE 20030609000172003060900017WP 2003 6 9 ARWA20030212 120030215A5315 FLOORBEAM DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO198968U 46069 DURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 360, STRINGER 21. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 360 IAW STC SA1063SO AND SA1377SO. 2L74 4F 4A25 20030604001812003060400181NM 2003 6 4 UPS03440601 120030410A5410 FRAME BOEING747 747121 1384871NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, NR 2 PYLON REAR ENGINE MOUNT BULKHEAD FORWARD FOUND CRACKED AT 7 O/C POSITION ( LOOKING FWD ). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD O/B FORWARD FRAME REPAIRED AS PER RS 54-53-35009 AND UPS REPAIR 747-54-20035 REPEAT DVI AND HFEC INSPECTIONS EVERY 1200 FLT CYC OR 18 MOUTHS WHICH EVER IS EARLIER . REF UPS IAW SB 747-54A2202. 2L74 4F A20WE 20030605000682003060500068NE 2003 6 5 MEX2002153 220030505A7320V3400283 SOLENOID DOUG MD80 MD83 3023681NM PWA JT8 JT8D217 52053NE NR 2 ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23946AS 49658 DURING ENGINE START THE (APPROACH IDLE FUSE) MESSAGE COMES ON, THE ENGINE NR 2 IS MORE ACCELERATED THAN ENGINE NR 1. THE RIGHT SOLENOIDE WAS REPLACED IAW MM, TEST CORRECT IAW MM. 2L72 4F4 FRT E9NE 20030610000472003061000047WP 2003 6 10 ABXA030157 120030325A5330591142551 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 CORRODED SKIN BULGING FS 950 - 960, APPROXIMATELY BETWEEN LONGERON 27 RIGHT - LONGERON 29 RIGHT. REPAIRED AREA IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030521002032003052100203NM 2003 5 21 SWAA031065 120030509A57536546430131 SKIN BOEING737 737317 138447PNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C4 CHECK, FOUND LEFT INBOARD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LEFT INBOARD T/E FORE FLAP PER MM. 2L72 4F RTA16WE 20030611001562003061100156SO 2003 6 11 C2XA03BT062 120030528A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2736915 145421 DURING ROUTINE INSPECTION MAINTENANCE FOUND SEAT 12BC PSU EMERGENCY LIGHT TO BE INOPERATIVE. RELAMPED EMERGENCY LIGHT ASSEMBLY AT 12BC PSU IAW AMM 33-50-07. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20030611001642003061100164 2003 6 11 SWIA200312006 420030521A22166225734002 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE ELEVATOR MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07292SW3001 3001 120319 CAPTAIN'S AND F/O'S YOKE TRIM SWITCHES FAIL TO MOVE TRIM WHEEL. TRIM FAIL APPEARS ON MAP AFTER THE YOKE TRIM SWITCHES ARE PUSHED. ALSO, TRIM ILLUMINATES ON AUTOPILOT PANEL. REPLACED ELEVATOR TRIM SERVO. OPS CHECK GOOD. UPDATE 5/24/03 FAILURE REPEATED. REPLACED TRIM SERVO RELAY K0463. BOTH AUTOPILOT TRIM SWITCHES OPS CHECK GOOD IAW MM 22-10-00. P/N M83536/6-022M. 2L72 4T4 TRTA31SO E20NE 20030612000322003061200032EA 2003 6 12 SWIA200312024 120030417A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 FS 621.0 LBL 42 LEFT FLOORBEAM ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117. 2L72 4F RTA21EA 20031125000672003112500067WP 2003 11 25 DHL2003807548 120031018A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 C-BELLY DOOR EXTERNAL SKIN LOWER PART BROKEN 1.000 X 0.375 AT STA 1200.000 L-31 L-32 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ASTAR ED EDU21-5, ASTAR DWG U21-R05. TRIMMED OUT DAMAGED SKIN SEGMENT AND REMOVED EXISTING SPLICE STRAP IAW ASTAR ED EDU21-5, ASTAR DWG U21-R05. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. FABRICATED NEW SKIN SEGMENT IAW ASTAR ED EDU21-5, ASTAR DWG U21-R05. CLEANED, TREATED AND PRIMED AREA, SPLICE STRAP AND NEW SKIN SEGMENT IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED SPLICE STRAP AND NEW SKIN SEGMENT WITH NEW FASTENERS IAW ASTAR ED EDU21-5, ASTAR DWG U21-R05, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031202000072003120200007NM 2003 12 2 ASAA0310453 120030515A575465464353 SKIN BOEING737 737290C 138448VNM LE FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND LEFT WING FORE FLAP LEADING EDGE SKIN AT WING STATION 417 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031202001502003120200150NM 2003 12 2 2003F00607 120030807A2421761574B IDG BOEING737 737800* NM NR 1 ENGINE INOPERATIVE A MYWAO OTHER J WARNING INDICATION CRCRUISE 1 SO19732MA 30618 DURNG CRUISE INBOUND TO SNN, NR 1 IDG LIGHT ILLUMINATED IN FILGHT. ALSO,NR 1 GENERATOR OFF BUS AND SOURCE OFF LIGHTS ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. TRANSFERRED TO DMI 3111. REMOVED AND REPLACED NR 1 IDG AT MIA IAW MM 24-11-11 OPS CHECK GOOD. ETOP VERIFICATION FLIGHT ACCOMPLISHED AND ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO ETOPS STATUS. (M) 2L72 4F RTA16WE 20031203001402003120300140EU 2003 12 3 A6WA200360046 120031006A5512 SKIN BAG BAE146BAE146200A 1500266EU HORIZONTAL STAB DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 DENTS ON THE LEFT AND RIGHT HORIZONTAL STAB MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS RED AMAX FAX 1683-6810002. (M) 2H74 4F RTA49EU 20031204000382003120400038WP 2003 12 4 GTIA030840 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 148-200 14 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031205000192003120500019NM 2003 12 5 DL75K030905 120031006A5754 WEDGE BOEING757 757232 1384965NM NR 8 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO276715C 30486 FOUND ON PSV-2 CK DENT ON NUMBER 8 SLAT T/E WEDGE. REPAIRED PER SRM 57-43-02D, SRM 51-70-10D AND OPERATION 1000. 2L72 4F RTA2NM 20031208001272003120800127EU 2003 12 8 RAIA00310265 120031019A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK 41040 EMERGENCY PATH LIGHTS FROM ROW 7 BACK INOP. RE-SECURED CONNECTOR AT ROW 7 FOR PATH LIGHTS. 2L72 4T RTA41NM 20031204000252003120400025WP 2003 12 4 GTIA030862 120031002A5310 BEAM DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND L1 DOOR FORWARD VERTICAL BEAM AND STRAP CRACKED/BENT. REMOVED T-ANGLE. REMOVED CRACKED STRAP. REMOVED FORWARD VERTICAL BEAM. FABRICATED REPLACEMENT VERTICAL BEAM AND STRAP. INSTALLED NEW VERTICAL BEAM, NEW STRAP AND T-ANGLE. (M) 2L72 4F A6WE 20031209000752003120900075NM 2003 12 9 SWAA032341 120031024A3350101114 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29407WN 29817 FWD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20031209001702003120900170WP 2003 12 9 ABXA030410 120031014A553199118216 RIB DOUG DC9 DC932 3022066WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB AT THE BOTTOM OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20031208000552003120800055NM 2003 12 8 03FDEA01791 120031022A53436517673 FITTING BOEING727 727200 138407ENM NLG CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-5310-73211 FUSELAGE - MAIN FRAME - NLG DRAG BRACE SUPPORT CHAFE REPAIR P/N 65-17673. COMPLIED WITH EA 7-5310-73211 FUSELAGE - MAIN FRAME - NLG DRAG BRACE SUPPORT CHAFE REPAIR P/N 65-17673, AT MAE. 2L73 4F RTA3WE 20031209000272003120900027EA 2003 12 9 COMA0360466 120031022A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA RIGHT UNLOCKED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01712CA 7244 FLIGHT 5141 RIGHT THRUST REVERSER UNLOCKED CAUTION DURING TAKEOFF. SECURED AND DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20031209000632003120900063NM 2003 12 9 SWAA032363 120031026A52406545871 FRAME BOEING737 737317 138447PNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 3 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031209001072003120900107NM 2003 12 9 SWAA032336 120031023A3350 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C1 CHECK, FOUND RT SIDE EMERGENCY EXIT SIDEWALL LIGHTS INOP. RELAMPED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20040123000372004012300037SW 2004 1 23 KBM2003F00081 120031108A6320206031509001 DRAG PIN BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL M/R GEARBOX LOOSE E KBMAK NONE O OTHER ININSP/MAINT 1 WP1973DP 2513 DURING POST FLIGHT, FOUND MAIN GEARBOX DRAG PIN BEARING SHOOK LOOSE. REMOVED AND REPLACED. 1G71 3U3 U H2SW E4CE 20040123000742004012300074NM 2004 1 23 AMTA200301175 120030915A3350516574 CHARGER LKHEED1011 1011 N/A-SDRNM RROYCERB211 RB21122* 54555NE EMERGENCY LIGHT INOPERATIVE A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11188AT 193C1078 L3 DOOR EXTERIOR EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED L3 DOOR EGRESS LIGHTING POWER PA CHECK IAW MM 33-51-03, OPS. CHECK NORMAL. 2L73 4F4 FRTA23WE A12EU 20031009000102003100900010NM 2003 10 9 USAABB03171 120030920A33509221009 BATTERY BOEING757 7572B7 1384964NM EXIT SIGN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 FOUND R2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031014001492003101400149NM 2003 10 14 SWAA032058 120030915A2560PH22300L STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 EEPLS PHOTOLUMINESCENT STRIP LOOSE IN CABIN. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20031014000162003101400016NM 2003 10 14 UPS03441236 120030917A5330 SKIN BOEING747 747SR46 1384816NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: SP, SKIN EXFOLIATED ON AFT BELLY SKIN AT STA 1964 STR 45L 3.5. CUT OUT CORRODED AREA PER SRM 53-30-03. REMOVED LITE SURFACE CORROSION ON INTERNAL TEAR STRAP, FOUND WITHIN LIMITS, NDT HFEC PER NDTSOM 06 10-01.001, NO CRACKS NOTED AT CUTOUT. FABBED DOUBLER AND FILLER FROM 2 024T3 .071, TREATED AND PRIMED PARTS, INSTALLED COUNTER SINK WASHERS, INSTALLED REPAIR PARTS PER SRM 53-30-03 FIG 47 SRM 51-30-02. 2L74 4F RTA20WE 20031021000492003102100049 2003 10 21 USAASA03107 420030830A2565C37103103 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19742US 1275 PHL - THE AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20031211000292003121100029WP 2003 12 11 ABXA030432 120031027A5342591214159 ATTACH ANGLE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 VERTICAL STABILIZER LEFT ATTACH ANGLE WAS CRACKED AT 99. REPLACED LEFT VERTICAL STABILIZER ATTACH ANGLE IAW DC-9 SRM 53-05. 2L72 4F A6WE 20031210000362003121000036WP 2003 12 10 AALA20031309 120031123A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21576AA 53153 DFW EMERGENCY LIGHTS AT SEAT 20D INOPERATIVE. RESECURED LOOSE CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20030922000322003092200032NM 2003 9 22 AWXA200300942 120030807A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319132 3930340NM AFT CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT CABIN FLOOR PANEL 261FF. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AND REPLACED FLOOR PANEL 261FF IAW A319 SRM 53-02-00, PG. 108, FIG. 104. 2L72 4F RTA28NM 20030922001282003092200128NM 2003 9 22 AWXA200300960 120030807A5321D53671800500500 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT CABIN FLOOR PANEL 262FF. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AND REPLACED AFT CABIN FLOOR PANEL 262FF IAW A319 SRM 53-02-00, PG. 108, FIG. 104. 2L72 4F RTA28NM 20030923000602003092300060WP 2003 9 23 DHL2003604656 120030521A5730 PLATE DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING OUTBD L/E UPPER PLATING CORRODED AT STA XW 761.000. PERFORMED MAJOR REPAIR IAW EODHL-030529, ED-3305. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) AND A FILLER (7075-T6 AL0.050) IAW EODHL-030529, ED-3305. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER ON RT OUTERWING OTBD L/E UPPER PLATING STA XW 761.000 USING NEW FASTENERS IAW EODHL-030529, ED3305 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000992003092300099WP 2003 9 23 DHL2003604670 120030704A574046495971N ATTACH FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING T/E INNER UPPER FITTING CRACKED 1.000 AT XRS.434.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON LT. WING T/E AT XRS. 434.000 IAW SRM 51-1-20D 2L74 4F RT4A25 20030924000092003092400009EU 2003 9 24 197021003 120030210A77129752115206 TRANSDUCER PILATSPC12 PC1245 7090551EU TORQUE INDICATORFAILED E S4WAO OTHER S AFFECT SYSTEMS LDLANDING 1 WP07613NA 197 TORQUE INDICATION SHOWS ZERO TORQUE AT IDLE. 1L71 3T RTA78EU 20030926000322003092600032NM 2003 9 26 03FDEA01396 120030828A5330 SKIN BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25119FE 19301 CORROSION AND WORKING FASTENERS ON FUSELAGE SKIN ABOVE MAIN CARGO DOOR CUTOUT APPROXIMATELY STA.500 TO 560 STR 1L TO 5L. AIRCRAFT REMOVED FROM SERVICE BY FEDEX. 2L73 4F RTA3WE 20040206000432004020600043WP 2004 2 6 ASAA0380830 120031216A53209958212305 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND INTERCOSTAL CORRODED AT FS 1003-1022. REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040211000182004021100018WP 2004 2 11 GTIA031041 120031113A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN METAL FLOOR PANEL HAS PULLED FASTENERS AND TORN/CRACKED EDGE AT FS 1007-1079 LEFT OUTBOARD PANEL. REMOVED FLOOR PANEL. FABRICATED REPLACEMENT PANEL. INSTALLED FLOOR PANEL. (M) 2L72 4F A6WE 20030924000382003092400038NM 2003 9 24 DL767030751 120030813A3350 FUSE BOEING767 767232 1385132NM EMERGENCY LIGHT BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27108DL 22220 EXTERNAL EMERGENCY LIGHTS AFT OF RT OVERWING EXIT INOP (2ND & 3RD) FOUND FUSE BLOWN IN EMERGENCY BATTERY CHARGER RECEPTACLE. REPLACED SAME. LIGHTS OPERATE NORMAL. 2L72 4F RTA1NM 20040129000532004012900053EU 2004 1 29 MALA030591 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 9B FRAME CRACKED. ACCOMPLISHED WELD REPAIRS ON SEAT FRAME 9B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040128001452004012800145NM 2004 1 28 QXEA200301598 120031229A5751 STRUCTURE DHAV DHC8 DHC8202 2809007NM AILERON DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH12058 513 PDX - A HOLE WAS FOUND IN THE JOINT OF THE TRAILING EDGE OF THE RIGHT AILERON, 2 INCHES FROM THE OUTBOARD TIP. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE IAW THE D-8 SRM, 200, 57-40-00. THE AILERON WAS BALANCED IAW SRM 57-60-71. 2H72 4T RTA13NM 20040130002452004013000245EA 2004 1 30 SWIA200312759 120031128A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 484 LT INTERCOSTAL O/B FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV A AND RII 53-401. 2L72 4F RTA21EA 20040203001282004020300128SO 2004 2 3 SWIA200312777 120031209A5311 FRAME EMB 120 EMB120ER 3260203SO HYD BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07221SW 120290 LEFT HYDRAULIC BAY CUTOUT AFT FRAME CRACKED OUT OF OUTBOARD CORNER. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT HYD BAY DOOR CUTOUT AFT FRAME WITH SERVICEABLE UNIT IAW SRM 54-20-09. 2L72 4T RTA31SO 20040204000392004020400039NM 2004 2 4 AWXA200301258 120031006A5350 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE TAILCONE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK 8 AREAS OF TAIL CONE SURFACE WERE FOUND DEBONDED. MAINTENANCE CUTOUT DAMAGE ON TAIL CONE SURFACE AT BS 1176 CENTERLINE, BS 1166.5, 6 INCHES RT OF CENTER, BS 1169 2.5 INCHES RT OF CENTER, BS 1163.5, 3 INCHES RT OF CENTER, BS 1165.5 11INCHES LT OF CENTER, BS 1173 3 INCHES RT OF CENTER, BS 1165 7 INCHES LT OF CENTER, AND BS 1196 AT CENTERLINE, PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-07, PG. 28, FIG. 9. 2L72 4F4 FRTA16WE E2GL 20040204000592004020400059EU 2004 2 4 025291 120031016A2731 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE STBY PITCH TRIM ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17104CQ 340A104 FLT 4571 IN ROUTE FROM PIT TO LYH EXPERIENCED A STBY PITCH TRIM LIGHT IN FLT, CAPTAIN RETURNED TO PIT. 2L72 4T4 TRTA52EU E8NE 20040205001222004020500122EA 2004 2 5 QXEA200301481 120031130A3020 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 400 FALSE INDICATIONA QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09600QX 10005 RT COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT WHEN RIGHT COWL ANTI-ICE IS SELECTED ON. SAT -38 DEGREES C. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST AND MESSAGE REMAINED ON. CLIMBED OUT OF ICING CONDITIONS. DURING DESCENT RT COWL ANTI-ICE OPERATED NORMALLY. GROUND RAN BOTH ENGINES AND CHECKED COWL ANTI-ICE SYSTEM IAW MM 30-20-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031215000012003121500001EA 2003 12 15 COMA0360464 120031022A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01924CA24145 7026 DURING COMPLIANCE OF TASK NR 002-53-160-610, 4 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL9.0 AND RBL 9.0. THE CRACKS RANGE FROM 2.5 INCH TO 3.1250 INCHES LENGTH. THE PRESSURE SKIN WAS REPAIRED IAW MFG REO NR 601R-53-41-102, REV B, DATED 6-8-2003, AND REO NR 601R-53-41-162, DATED 6-9-2003. OK FOR RETURN TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040316000342004031600034WP 2004 3 16 ASAA0380290 120030404A532199578243 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOORBOARD MISSING RIVETS AND IS DELAMINATED AT FS 200-237. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20040316000822004031600082 2004 3 16 ASAA0380318 420030411A25653961896501 LANYARD DOUG MD80 MD83 3023681NM L2 DOOR DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 SEA PREFLIGHT CHECK, FOUND LEFT AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RT 20031216000592003121600059NM 2003 12 16 SWAA032545 120031118A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED PM CHECK, FOUND 4 IN LONG FUSELAGE SKIN CRACK AT BS 807, STRINGER 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040420002022004042000202EU 2004 4 20 ERAA093697 120031224A3212D24762102 FLOAT BOLKMS105 BO105A EU MLG DAMAGED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 FORWARD GIRT SEPARATING FROM FLOAT BAG PATCH 3 PIN HOLES, TESTED, IAW 25-60-95. 1G72 3U H3EU 20060801001152006080100115WP 2006 8 1 IXXA060565S 120031027A5230 DOUBLER DOUG DC8 DC871F 302199DWP ZONE 800 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND "D" PIT DOOR INBOARD WEB DOUBLER CRACKED. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, AND 53-2-0. 2L74 4F RT4A25 20030814000092003081400009NM 2003 8 14 SWAA031721 120030801A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030814000712003081400071SO 2003 8 14 SWIA200312118 120030522A5411 SUPPORT EMB 120 EMB120ER 3260203SO RT MLG WW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 RT WHEEL WELL INBOARD SIDE VERTICAL SUPPORT CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED RIGHT WHEEL WELL BRACKET IAW 120 SRM 51-10-02. P/N: 120-22916-001 2L72 4T RTA31SO 20030818000322003081800032GL 2003 8 18 HEEA088384 220030804A73200164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 NR 1 START HARD TO MODULATE. TO BE SENT TO VENDOR. 1G72 3U3 U H1NE E1GL 20030819000072003081900007EU 2003 8 19 BAQA088149 120030716A7810117651121 TAILPIPE BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101750B1 41560NE ENGINE CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1077 7243 TAIL PIPE ASSY CRACKED AND INTERNAL CONE DEFORMED. REPLACED WITH SERVICEABLE UNIT. 7/24/03 1G72 3U3 U H13EU E5NE10 20030819002322003081900232NM 2003 8 19 CALA0300370 120030708A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME ANGLE AT STA 616 BELOW FLOOR LINE, WL 200. REPAIRED FRAME IAW ECRA 5311-01154. 2L72 4F RTA16WE 20030820001432003082000143WP 2003 8 20 UPS03840974 120030709A5220 FASTENER DOUG DC8 DC873F 302199FWP EMERGENCY DOOR LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 FASTENERS MISSING AND LOOSE BOTTOM EDGE OF LEFT FWD EMERGENCY DOOR. CW EO DC8-5220-18984-A INTERIM REPAIR DEFERRED PER EO FOR REPETITIVE INSP AND PERM REPAIR. 2L74 4F RT4A25 20030331000452003033100045WP 2003 3 31 AALA20030199 120030216A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21475AA 49650 DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS OVER SEATS 21-27 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401001102003040100110WP 2003 4 1 DHL2003804501 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 766.500. REMOVED FASTENERS PER SRC2 PG 1. STOP DRILLED CRACK PER SRM 57-20 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030402000672003040200067NM 2003 4 2 2003UALA00344 120030316A5754114W413016 WEDGE BOEING777 777222 1385219NM SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29206UA 30212 T/E WEDGE, SLAT ASSEMBLY, DELAMINATED. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE WAS REPAIRED. 2L72 4F RTT0001SE 20030404000662003040400066NE 2003 4 4 DL757030272 220030323A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO27695DA37506 29727 716569 RT ENGINE CSD QUIT, WENT THROUGH NORMAL DISCONNECT PROCEDURES, CSD DISCONNECTED OK. AFTER CSD DISCONNECTED GOT A RT ENGINE OIL FILTER LIGHT, OPENED UP THE QRH AND STARTED TO GO THROUGH THE PROCEDURE WHEN THE ENGINE SPOOLED DOWN ON ITS OWN. NEVER FINISHED THE PROCEDURES. DIVERTED INTO NAS. REPLACED RIGHT ENGINE. 2L72 4F4 FRTA2NM E17NE 20030411000062003041100006NM 2003 4 11 SWAA030740 120030403A335020131A BATTERY PACK BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20030414000052003041400005NM 2003 4 14 SWAA030762 120030405A531365C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) AT BS 747 AT STR 20L, BS 747 AT STR 22R, BS 867 AT STR 20R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030410000642003041000064WP 2003 4 10 GTIA030098 120030210A5340 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND MAIN CABIN FS 1022 STATION 181 T-FITTING CORRODED. REMOVED T-FITTING, LOCATED AND DRILLED NEW PART. INSTALLED FITTING. (M) 2L72 4F A6WE 20030416001652003041600165NM 2003 4 16 AALA20030208 120030218A3222CBE1028 STRUT BOEING757 757223 1384957NM NLG LOW A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21635AA 24593 ATL - FLT 1461 - EN ROUTE ATL-DFW, AFTER TAKEOFF, GEAR HANDLE BUT BOTH GEAR AND GEAR DOORS LIGHT REMAINED ILLUMINATED AND WARNING HORN ON. GEAR WAS PLACED DOWN AND RECEIVED THREE GREEN LIGHTS. RETURNED ATL AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BITE CHECK OF PSEU. SERVICED NOSE STRUT WITH AIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416003332003041600333WP 2003 4 16 UPS03840029 120030102A5315577327558 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE: C2, FLOORBEAM TO VERTICAL STIFFENER ATTACH ANGLE IS CRACKED AT STA 680 AT RBL 48. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275, AND SRM 51-1-20. 2L74 4F RT4A25 20030425000072003042500007WP 2003 4 25 UPS03840388 120030321A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, A/C COMPARTMENT AT FS 25 L23L FRAME IS CORRODED BEHIND WIRE BUNDLE. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE AND FAB REPAIR DOUBLER IAW UPS EO DC8310-11728/DWG DC8-53A-011. HEAT TREAT TO T6 IAW TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030613000502003061300050SO 2003 6 13 C2XA03IA059 120030603A2910A9140413 LINE EMB 145 EMB145LR 3260212SO HYD PUMP LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2715910 145455 BAN- FLIGHT 2623 (IAH-DAY), THE CREW NOTED THAT HYDRAULIC NR 1 LOW QTY MESSAGE APPEARED ON EICAS WITH HYDRAULIC LEAK. (NOTE: THE FLIGHT WAS DIVERTED TO BNA ). BNA- MAINTENANCE REMOVED AND REPLACED THE SUCTION AND PRESSURE HYDRAULIC LINES AT THE ENGINE DRIVEN PUMP, NR 1 ENGINE, SERVICED THE NR 1 HYDRAULIC SYSTEM, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030617001112003061700111SW 2003 6 17 HEEA087292 120030611A6710 BOLT BELL 407 407 1182206SW ALLSN 250C 250C47B GL BELLCRANK ELONGATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 LONG TUBE BOLT HOLE OUT OF ROUND. TO BE SENT TO MFG. 1G71 3U3 UO H2SW E1GL 20030617002202003061700220SW 2003 6 17 HEEA087476 120030612A32128226003 FUSIBLE PLUG BELL 407 407 1182206SW RT FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH 53435 RT FLOAT BOTTLE FUSIBLE PLUG LEAKING. 1G71 3U O H2SW 20030523001022003052300102EU 2003 5 23 AWXA200300546 120030428A5350 ANGLE AIRBUS320 A320231 3930325EU FAIRING SUPPORT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON ATTACH ANGLE AT FR 34 ON FAIRING SUPPORT STRUCTURE AT AFT UPPER EDGE OF PANEL 192AB. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE AT FR-34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW AWA ER 26-5323-03129-TB1. 2L72 4F RTA28NM 20030527000262003052700026NM 2003 5 27 DL733030320 120030331A53306545722188 SKIN BOEING737 737347 1384647NM FUSELAGE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 THE FUSELAGE SKIN WITH AN AREA OF WEAR BETWEEN FS 857 & 877 NEAR STRINGER 1. THE DAMAGE WAS BLENDED SMOOTH AND AN AREA CUTOUT. THE DAMAGE WAS REPAIRED WITH AN ALUMINUM EXTERNAL REPAIR DOUBLER PER ER/A 384701-14, REV A. 2L72 4F RTA16WE 20030527000972003052700097CE 2003 5 27 2003F00307 120030429A2760F78EC103M POTENTIOMETER CESSNA650 650 2076802CE SPEED BRAKE FAILED A UG8AO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL235117 6507064 WHILE PERFORMING PREFLIGHT CHECKLIST, THE CREW NOTICED THE AOA INDICATOR WAS INDICATION 'INOP' ANOTHER AIRCRAFT WAS UTILIZED FOR THE TRIP. THE RIGHT SPEED BRAKE POSITION SENSOR VOLTAGE WAS TOO HIGH. POSITION SENSOR VOLTAGE WAS ADJUSTED PER MM TO PROPER SPECS. OPERATION AS NORMAL. (M) 2L72 4F A9NM 20030527001112003052700111EA 2003 5 27 2003F00321 120030410A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A MASAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0737178 7178 FLT 6129 - MCI -PHX - DIVERTED TO ABQ DUE TO THE CARGO SMOKE INDICATOR. FIRE BOTTLE UTILIZED. MAINTENANCE MEL'D THE CARGO SMOKE BOTTLE IN ABQ. MAINTENANCE REPLACED FIRE BOTTLES. (M) 2L72 4F RTA21EA 20030618001122003061800112SW 2003 6 18 HEEA087498 120030612A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY OVERHEATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 BLOWER ASSY EMITTING BLACK GREASE. REPLACED. 1G71 3U O H2SW 20030619000582003061900058SW 2003 6 19 HEEA087399 120030611A6510407340339101 BEARING BELL 407 407 1182206SW COOLER BLOWER ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 FWD BEARING ROUGH ON OIL COOLER BLOWER SHAFT. 1G71 3U O H2SW 20030624000112003062400011WP 2003 6 24 GTIA030409 120030527A5315 FLOORBEAM DOUG DC9 DC981 3022081WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FS 655 CABIN FLOORBEAM BROKEN OFF AT RIVETS. DRILLED EXISTING HOLES. INSTALLED FLOOR PANEL SUPPORT. (M) 2L72 4F A6WE 20030625000082003062500008NE 2003 6 25 GLBA2003065 220030527A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE OUT OF ADJUST A GLBAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 NM03254GL UE254 LT PROP AND T/O POWER AT 1650 RPM RT FLUX BETWEEN 1650-1700, ADJUSTED LT / RT N2 MAX RPM 2L72 4T4 TRTA24CE E26NE 20030626000192003062600019NM 2003 6 26 2003UALA00369 120030408A5270 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE PAX DOOR ILLUMINATED A UALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP29307UA 23668 NA AIRCRAFT ABORTED TAKEOFF DUE TO DOOR 1L INDICATION LIGHT ON. CAUSE UNKNOWN. INSPECTED AND SECURED TARGET AND PLATE. DOOR INDICATION SYSTEM FUNCTIONED NORMALLY. 2L72 4F4 FRTA16WE E2GL 20030707000262003070700026WP 2003 7 7 AALA20030497 120030427A2120 DUCT DOUG DC9 DC982 3022082WP ACM BAY LEAKING A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217528A 49920 EN ROUTE, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED JUST AFTER TAKEOFF. STAYED ON FOR APPROXIMATELY 3-5 MINUTES CROSSFEED CLOSED, AIRFOIL ICE OFF, HP BLEED OFF. RETURNED AND LANDED TUL WITHOUT INCIDENT. REINSTALLED OUTBOARD FORWARD DUCT AIR CONDITIONING DUCT AND TORQUED CLAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707000582003070700058NM 2003 7 7 AALA20030621 120030530A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21790AN 30251 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT INTERIOR FORWARD LEFT G3 CLOSET INOPERATIVE. REPLACED EMERGENCY EXIT INTERIOR FORWARD LEFT G3 CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030707001892003070700189NM 2003 7 7 UPS03440841 120030519A5313 LONGERON BOEING747 747200 1384847NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 AFT CARGO STA 1696-1700 STR 48R CORROSION REVEALED. TIE CLIP AND HI-LOCKS REINSTALLED IAW SRM 51-30-02. CORROSION BLEND OUT (0.080 INCH X 1 INCH X 2 INCHES) AFT CARGO - BS 1690 - 1710 STR 48R REPAIRED IAW SRM 53-10-03 FIG 7. 2L74 4F RTA20WE 20030717000112003071700011 2003 7 17 HEEA087988 420030629A3442MI5852013 INDICATOR BELL 412 412 1182202SW WX RADAR SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 WEATHER RADAR INDICATOR INOPERATIVE. SHOP REPAIR. 1G72 4U H4SW 20040415001392004041500139NM 2004 4 15 ASAA0240148 120030318A53116546552 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 827, LBL 10 - RBL 4 AND WL 142. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030116001132003011600113 2003 1 16 HEEA083063 420030107A2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 FIRST DIGITS OF BOTH SIDES OF TRANSCEIVER DISPLAY MISSING. IN SHOP REPAIR. 1G71 3U H2SW 20030124000892003012400089NM 2003 1 24 UPS03440060 120030103A5310 FITTING BOEING747 747259B 1384804NM LH BS 1480 B/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C LH BS 1480 B/H NO.24 HOLE CRACK AT OUTER CHORD SPLICE FITTING RUNNING O/B APPROX 5/32". REFER ATTACH SKETCH FOR DETAILS. DEFECTIVE HOLE REWORKED AS PER RS-53-43-34957 ISSUE 'B' AND EO B747-5310-18127-A 2L74 4F RTA20WE 20030201000012003020100001SO 2003 2 1 C2XA02SH184 120030201A531313500400019 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713913 145438 SHV- DURING C CHECK EXTERNAL GOUGE WAS FOUND ON STRINGER T REINFORCEMENT AT FRAME 52 STRINGER 19R. MAINTENANCE REMOVED DAMAGE AND PERFORMED DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030204000272003020400027NM 2003 2 4 SWAA030184 120030123A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 15L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204001372003020400137CE 2003 2 4 VJ32003F00020 120030114A3610RA216CW PUMP BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO DRY AIR WORN B VJ3RK NONE O OTHER ININSP/MAINT 1 WP075540P CE1335 DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANES ARE WORN. 1L71 3O3 O 3A15 E5CE 20030210001572003021000157SO 2003 2 10 C2XA03BT029 120030208A5300 SKIN EMB 145 EMB145LR 3260212SO DENTED A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2716954 145072 BTV---CO2002, MAJOR REPAIR WAS PERFORMED AFT OF MAIN CABIN DOOR BETWEEN STRINGER 12L AND 13L AND FRAME 18 AND FRAME 20, HAD DENT (OUT OF LIMITS), DENT REPAIRED IAW EMB145 SRM #53-21-01. SEAL AND PAINTED IAW EMB145 SRM CHAPTER #51. PRESSURIZATION CHECK PERFORMED IAW EMB145 AMM #21-31-00. PRESSURIZATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030625001042003062500104NM 2003 6 25 F3LA200300085 120030220A5320 FLOOR SUPPORT BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO FLOOR SUPPORT CORRODED ON LOWER FLANGE AT STA. 859, RBL 8. INSTALLED REPAIR PER SRM 53-10-5 AND MM 51-21-99. 2L72 4U RTA16WE 20030227000852003022700085SW 2003 2 27 HEEA084392 120030212A6510 BEARING BELL 407 407 1182206SW T/R BLOWER ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH PHI0014 53003 TAIL ROTOR BLOWER DRIVE SHAFT FWD BEARING ROUGH. REPAIRED. 1G71 3U O H2SW 20030305000422003030500042 2003 3 5 HEEA084624 420030214A2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 VHF TRANSCEIVER RF CONNECTOR LOOSE. TIGHTENED CONNECTOR AND RESOLDERED LOOSE WIRE ON CONNECTOR. REPAIRED. REMOVED CORROSION FROM CHASSIS. REPLACED BAD TRANSISTOR INSULATORS ON Q108, Q109 AND Q110 TRANSISTORS. REPLACED BAD Q110 TRANSISTOR SOCKET, REPAIRED. ADJUSTED C/N SQUELCH, CARRIER SQUELCH, AND ALIGNED TRANSMITTER. BENCH CHECK GOOD. 1G72 4U H4SW 20030307000412003030700041 2003 3 7 SWAA030456 420030228A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030307001652003030700165NM 2003 3 7 250TR0007 120030202A71106560529 COWLING BOEING737 7372K5 138448XNM A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 #2 engine air inlet cowl has gouge at 1:30 position. Repaired damaged area per EA No. 54-045 dated 2/14/2003. 2L72 4F RTA16WE 20030313002332003031300233NM 2003 3 13 QXEA0300209 120030114A7110 FRAME BOMBDRDHC8 DHC8401 1390041NM RT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 CKB- FRAME AND ANGLE CRACKED AT RIGHT HAND LOWER COWLING. REPAIRED IAW DHC-8 Q400 RD 8/4-71-016. 2H72 4T RTA13NM 20030314002302003031400230EU 2003 3 14 03069302A 120030309A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27302UE 41013 DURING MAINTENANCE/INSPECTION MAINTENANCE PERSONNEL FOUND EXIT ROW 6 OVERHEAD EMERGENCY LIGHT INOPERATIVE.MAINTENANCE PERSONNEL INSPECTED, NO DEFECTS NOTED ON EXIT ROW (6A) EMERGENCY LIGHT. OPS CK'D OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA41NM 20030429000382003042900038WP 2003 4 29 ZW0A0304101 120030409A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DAMAGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139307R 49663 THE EMERGENCY LIGHTS WERE INOPERATIVE AT THE MOST FORWARD CABIN DOOR LEFT AND RIGHT SIDE, AND THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. RESEATED THE BATTERIES IN THE BATTERY PACK FOR THE EMERGENCY LIGHTS, AND RESEATED THE BATTERIES IN THE BATTERY PACK FOR THE EGRESS LIGHTS. CHECK-C 10-02-02 MCI. 2L72 4F RTA6WE 20030430000642003043000064NM 2003 4 30 USAA030030 120030321A5711 SPAR BOEING737 737301 1384611NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU 23512 PIT - FOUND LEFT REAR SPAR CRACKED .80 INCHES, 2ND FASTENER HOLE AT RSS 224.41. TEMP TIME LIMITED, DOUBLER INSTALLED PER EA 74944. (M) 2L72 4F RTA16WE 20030501000422003050100042WP 2003 5 1 AALA20030033 120030107A5310 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21492AA 49730 TUL - FOUND TWO .125 INCH CRACKS EXTENDING OUT FROM LOWER FASTENER IN SHEAR TIE STATION 1380, LONGERON 12L TO 13L, ABOVE LEFT PYLON. STOP DRILLED CRACKS. INSTALLED DOUBLER PER SRM 53-01-00. (M) 2L72 4F A6WE 20030501001942003050100194EU 2003 5 1 USAASA03027 120030324A3350321430 BATTERY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19119US 1268 CLT - THE AFT EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030430001382003043000138NM 2003 4 30 SWAA030911 120030423A5313FUSELAGE STRINGER BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1121, STR 3L. REPAIRED STR PER SRM. 2L72 4F RTA16WE 20030502001562003050200156NM 2003 5 2 03FDEA00474 120030417A5411 FRAME BOEING727 727200 138407ENM NR 3 NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE COWLING FRAME NR 5 HAS A HOLE AND CHAFING CONDITION. 2L73 4F RTA3WE 20030505001582003050500158EA 2003 5 5 03112656 120030422A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMRGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27656BR 7485 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030514000242003051400024NM 2003 5 14 AALA20030011 120030106A32304134191 LINE BOEING757 757223 1384957NM RT MLG LEAKING A AALAK NONE K FLUID LOSS ININSP/MAINT 1 SW21691AA 25697 HYDRAULIC QTY LEAK RT MAIN GEAR FLEX LINE FOR TRUCK POSITION ACT. REMOVED AND REPLACED FLEX LINE, OPS AND LEAK CHECKED OK ACT CHECKED NORMAL. (M) 2L72 4F RTA2NM 20030514001782003051400178NM 2003 5 14 03FDEA00659 120030429A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 HORZ STABILIZER CENTER BOX LT NR 1 BARREL NUT HOLE FOUND WITH CORROSION. REAM BORE UP TO 1.549 INCH CORROSION STILL PRESENT ON THE SIDE OF BEARING SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR. 2L73 4F RTA22WE 20030514002032003051400203NM 2003 5 14 03FDEA00715 120030430A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 O/B FLAP O/B HINGE ATTACHMENT TO FLAP (LOWER FWD HOLE, 5 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP. 2L73 4F RTA22WE 20030604000852003060400085NM 2003 6 4 UPS03440499 120030413A5320 CLIP BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 BS 1040 STR 4L TIE CLIP CORROSION. BS 1040 STR 4L TIE CLIP REINSTALL AS PER SRM 51-30-02. CORROSION BLEND OUT 0.040 X 1 X 1 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030515000252003051500025EA 2003 5 15 SWIA200311946 120030331A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 RIGHT LOWER WING PLANK AT WS 148.19 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED RIGHT LOWER WING PLANK IAW CRJ REO 601R-57-21-130 REV D AND 601R-57-21-131 REV NC. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-130. NO CRACKS NOTED. 2L72 4F RTA21EA 20030515000582003051500058GL 2003 5 15 C2XA03IA049 220030512A7200AE3007A1P ENGINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW271397010601 145146 CAE311047 IAH - FLT 2074 - PILOT REPORTED THAT DURING CRUISE THE NR 2 ENGINE FAILED AND AUTO-SHUTDOWN. THE CREW THEN PROCEEDED TO ISOLATE THE ENGINE BY PERFORMING PRECAUTIONARY SHUTDOWN PROCEDURES. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE. 2L72 4F4 FRTT00011ATTE6CH 20030612000622003061200062SO 2003 6 12 SWIA200312036 120030528A5753 BRACKET EMB 120 EMB120ER 3260203SO TE FLAPS CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW 120151 RIGHT FLAP LOWER MOVEABLE PANEL HAS INBOARD ROLLER BRACKET BROKEN. REMOVED AND REPLACED FLAP PANEL ROLLER BRACKET IAW EMB SRM 51-40-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20030613000552003061300055EU 2003 6 13 UPS03140797 120030604A2120 ENGINE AIRBUSA300 A300F4622R 3930360EU COCKPIT ODOR A IPXAK NONE O OTHER ININSP/MAINT 1 SO01135UP 0819 STRONG KEROSENE ODOR DURING ENTIRE FLIGHT. STARTED BOTH LT & RT ENGINES PER MM 71-00-00-5 AND PRESSURIZED A/C PER 21-31-00-0. NO ODOR NOTED, A/C OK FOR SERVICE. 2L72 4F RTA35EU 20030320000102003032000010NM 2003 3 20 USAABB03007 120030112A33509221009 BATTERY BOEING757 7572B7 1384964NM EXIT SIGN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19612AU 27124 PHL - FOUND EXIT IDENTIFIER AT R4 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030122000992003012200099EU 2003 1 22 HEEA083487 120030107A642010531821 PITCH LINK BOLKMS105 BO105S 5626006EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 TAIL ROTOR PITCH CONTROL LINKS WORN. REPLACED LINKS. 1G72 3U H3EU 20030122002552003012200255EU 2003 1 22 DHL2003362004 120030116A2697 WIRE AIRBUS300 A300B4203 3930306EU FIRE LOOP CHAFED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01362DH 84 NR 2 ENGINE "A" LOOP LIGHT ILLUMINATED. TRANSFERRED TO DMI #11627 IAW MEL 26-12-01-1. PLACARDS INSTALLED. REF. DMI 11627 NR 2 ENGINE "A" LOOP LIGHT ILLUMINATED. FOUND WIRE W4T16 CHAFED IN AFT PYLON T-BOX. REPAIRED CHAFED IAW STANDARD MAINTENACE PRACTICES. OPS CHECKED FIRE LOOP IAW M/M 26-12-00. 2L72 4F RTA35EU 20030123000232003012300023NM 2003 1 23 2003UALA00039 120030109A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 STATION 1640 RBL 58 FLOORBEAM UPPER CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIR T CAP INSTALLED. 2L72 4F4 FRTA2NM E17NE 20030327000372003032700037NM 2003 3 27 AWXA200300309 120030228A5320146N524010 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON SUPPORT ANGLE ON UNDER SIDE OF SHEAR DECK AT BS 1715, LBL 25-30. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT BS 1715, LBL 25-30; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 146N5240-10. 2L72 4F RTA2NM 20030327000632003032700063NM 2003 3 27 C1HA200388001 120030223A2121 FAN BOEING727 7272S7 138407ZNM CABIN OVERHEATED A C1HAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL15688CA 22344 ON DESCENT WE NOTICED AN ELECTRICAL SMOKE ODOR THE ODOR DISSAPATED AFTER THE GASPER FAN WAS TURNED OFF. INSPECTED GASPER FAN FOR EVIDENCE OF OVER HEATING. RESET C/B AND CHECKED PER 727MM 21-23-00. OPS NORMAL. 2L73 4F A3WE 20030303001072003030300107NM 2003 3 3 0300356642 120030218A5330 SKIN BOEING747 747212B 1384886NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01642NW 21942 During "L" check found crack in fuselage skin at aft cargo door cutout upper forward corner BS 1830 STR 26R Repaired per EA 66-193973. 2L74 4F A20WE 20030324000972003032400097EU 2003 3 24 AWXA200300081 120030127A2910762A000004AMDTB ACTUATOR AIRBUS320 A320231 3930325EU ZONE 191 WORN A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28621AW5200 053 FLT 0250 - F/O NOTED A/C REQUIRED MORE RT RUDDER THAN NORMAL. F/A STATED SHORTLY AFTER T/O, A/C VIB AND NOISE FROM APPROX ROW 4, PAST OVERWING EXIT. AT 29000 FT AT .78 MACH LOUD VIB COULD BE HEARD AND FELT ON FLT DECK, VIB NOTICED ON SEATS AS WELL AS FLOOR. VIB INCREASED AS A/C TURNED AND DECREASED TO ORIGINAL AT STRAIGHT AND LEVEL. STRAIGHT AND LEVEL FLIGHT 2 TO 3 DEGREES LT WING LOW AND 1.5 DEGREES RUDDER TRIM RT. REDUCING AIRSPEED FROM 303 TO 270 KIAS REDUCED NOISE AND VIB. MAINT PERFORMED FREE PLAY CHECK OF RUDDER AND ELEVATOR AND FOUND ALL 3 RUDDER ACTS OUT OF LIMITS AND RT & LT BLUE ELEV SERVO CONTROLS WORN, LT GREEN ELEV SERVO CONTROL. R & R YELLOW RUDDER SERVO CONTROL IAW AMM AND GREEN AND YELLOW RUDDER2L72 4F RTA28NM 20030327001992003032700199SW 2003 3 27 CA030211012 120030130A5530410008173 SKIN GULSTM690TP 690 0141720SW GARRTTTPE331TPE3315251K NM VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TWO INCH CRACK FOUND IN LEFT HAND VERTICAL STABILIZER WHILE COMPLYING WITH SB 218 1H72 3T4 T 2A4 E2WE 20030424000272003042400027NM 2003 4 24 ZW0A0303203 120030319A3350 LIGHT BOEING757 757231 1384950NM CABIN DISCONNECTED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13715TW 28483 THE MOST FORWARD SECTION OF EGRESS LIGHTS WERE INOPERATIVE. RECONNECTED THE FWD LAMP ASSEMBLY. CHECK-C 3-29-2002. 2L72 4F RTA2NM 20040223000492004022300049EA 2004 2 23 SVU2004F00001 120031230A274170609 CONTROL UNIT CNDAIRCL604 CL604 1900301EA GE CF34 CF34* NE HORIZONTAL STAB FAILED B SVURO OTHER O OTHER NRNOT REPORTED 1 SW19323FX3355 5447 STAB CHANNEL NR 1 FAILED. (WO NR 33978) 2L72 4F4 FRTA21EA E15NE 20030725000102003072500010NM 2003 7 25 DL73G030584 120030624A253081150417 COFFEEMAKER BOEING737 73735B 13844BMNM FWD GALLEY SPARKS A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27221DL 23970 COFFEEMAKER HAS ELECTRICAL SPARKS. REPLACED DISPENSER. 2L72 4F RTA16WE 20030806000772003080600077SO 2003 8 6 C2XA03SH221 120030711A541014576631621 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 145477 DURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030812000302003081200030NE 2003 8 12 HEEA088394 120030715A243229490001 BATTERY SKRSKYS76 S76A 8143006NE MASTER OVERHEATED E HEEAO OTHER M OVER TEMP NRNOT REPORTED 1 SW034253S 760035 MASTER BATTERY OVERHEATING. SHOP REPAIR. 1G72 3U H1NE 20030903000462003090300046EU 2003 9 3 PYF2003F00000 120030414A62203130136500000 DAMPER AEROSPSA319 SA319B 8680607EU TMECA AST14TASTAZOU14B 60014EU MAIN ROTOR HEAD FAULTY E PYFCO OTHER O OTHER NRNOT REPORTED 1 AL03119PH 853 2119 PILOT REPORTED GROUND RESIDENCE, UPON PULLING TO A HOVER HE STATED THAT HE HAD A 3 PER REV VIBERATION. AND MADE PRECAUTIONARY LANDING. UPON LANDING AND SHUTTING DOWN, HE NOTICED THAT THE MAIN ROTOR LIMITING CABLE WAS SEPARATED. 1G71 4U3 U H1IN E13EU 20030610001242003061000124SW 2003 6 10 HEEA087021 120030604A6230406010429101 PIN BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 MAIN ROTOR HEAD PIN WORN. 1G71 3U O H2SW 20030612001532003061200153WP 2003 6 12 UPS03840742 120030508A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766-1806 LONG 17L IS CRACKED. REMOVED CRACKED LONG 17L AND END FITTING AND REPLACED WITH NEW LONG 17L AND END FITTING IAW DC8 SRM 51-1-20D & 51-1-21. FABBED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 5 1-1-8. 2L74 4F RT4A25 20030612001862003061200186NM 2003 6 12 2003UALA00449 120030524A2910 FITTING BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE HYD SYSTEM LEAKING A UALAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29901UA 25001 B-HYDRAULIC SYSTEM QUANTITY AND PUMP LOW PRESSURE LIGHTS ILLUMINATED. INSPECTION FOUND THAT THE RETURN LINE CHECK VALVE FITTING ON THE HYDRAULIC FLAP DRIVE MOTOR SHEARED OFF AT THE BOSS. THE FITTING WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND THE FILTERS WERE CHANGED. OPERATIONAL CHECKS OF ALL PUMPS ASSOCIATED WITH SYSTEM 'B' AND NR 2 ENGINE RUN WAS ACCOMPLISHED TO VERIFY 'B' SYSTEM HYDRAULICS OPERATE NORMALLY. 2L72 4F4 FRTA16WE E2GL 20030617001482003061700148EA 2003 6 17 QXEA200300582 120030512A5754 SLAT CNDAIRCL600 CL6002C10 1390015EA LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - SLAT CHAFING AGAINST LEADING EDGE ON LEFT HAND WING. REPAIRED IAW HORIZON AIR EA R-57-32. 2L72 4F RTA21EA 20030617001332003061700133SW 2003 6 17 HEEA087466 120030612A291070061J175W216A HOSE BELL 407 407 1182206SW HYD SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 HYD SYSTEM HOSE HAS CORROSION AT SLEEVE NEAR HOSE. REPLACED HOSE. 1G71 3U O H2SW 20030521001522003052100152WP 2003 5 21 MWEA030198 120030430A3030 HEATER DOUG DC9 DC932 3022066WP PITOT TUBE INOPERATIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31501ME 47132 AUX PITOT HEAT SHOWS NO AMPS AND PITOT STALL HEATER ANNUNCIATOR LIGHT CAME ON. REMOVED AND REPLACED AUX PITOT TUBE. 2L72 4F A6WE 20030521000232003052100023WP 2003 5 21 DHL2003604511 120030428A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN IT, STA XS 461.372. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON LT WING CTR L/E FORMER AT XS 461.372 IAW SRM 57-2-0 PG 9-10 SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030618001592003061800159SW 2003 6 18 HEEA087507 120030612A3310SM20ACD300A21 RELAY BELL 407 407 1182206SW COCKPIT LIGHT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 COCKPIT LIGHT RELAY INOPERATIVE. 1G71 3U O H2SW 20030618001882003061800188SW 2003 6 18 HEEA087365 120030611A2510407070620139 PANEL BELL 407 407 1182206SW COCKPIT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 HEADLINER CRACKED BEYOND REPAIR. 1G71 3U O H2SW 20030527000372003052700037NM 2003 5 27 DLM88030327 120030401A2120 ODOR DOUG MD88 MD88 3023688NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27944DL 49817 ON APPROACH TO BOS AFTER LANDING GEAR WAS LOWERED- BOTH AFT LAV SMOKE DETECTORS SOUNDED- AT THE SAME TIME AFT F/AS SMELLED A BURNING ODOR. ALSO BOTH PILOTS SMELLED SAME ODOR IN COCKPIT SIMULTANEOUSLY. AFTER LANDING ALARMS CEASED AND ODOR WENT AWAY. REMOVED RT ACM TURB INLET AND EXHAUST DUCT FOR INSP. NO OIL FOUND. BOROSCOPED NR 1 AND 2 ENGS BEARING AREAS, NO OIL RESIDUE FOUND. C/W OPN 5088 AND OPN 5089, ALL CK OK. INSTALLED GEAR PINS AND CYCLED GEAR HANDLE SEVERAL TIMES. NO LEAKS NOTED. ACFT OK FOR SERVICE. 2L72 4F RTA6WE 20030523000972003052300097WP 2003 5 23 MWEA030219 120030519A531359114481 FRAME DOUG DC9 DC982 3022082WP STA 560 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 LIGHT CORROSION ON AFT SIDE OF MID PIT FRAME CHANNEL FRAME STATION 560 AND LONGERON 30. REMOVED CORROSION. 2L72 4F A6WE 20030619000362003061900036GL 2003 6 19 HEEA087190 220030609A732023007827 VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 VALVE INOPERATIVE. SCRAPPED. 1G71 3U3 U H2SW E1GL 20030623000572003062300057WP 2003 6 23 GTIA030354 120030510A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND DENT AT FS 351 BETWEEN LONGERONS 19 AND 20R. CUT OUT DAMAGE. FABRICATED 9 FINGER DOUBLER. FABRICATED 11 SKIN. FABRICATED 5 DOUBLER. INSTALLED 5 AND 9 DOUBLERS AND 11 NEW SKIN. (M) 2L72 4F A6WE 20030701000062003070100006SW 2003 7 1 HEEA087860 120030614A6320407040628101 TUBE BELL 407 407 1182206SW MRGB OIL SYS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 MAIN ROTOR GEARBOX OIL TUBE HAS CORROSION FOUND UNDER ADEL CLAMP NOT VISIBLE UNTIL REMOVED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030707000322003070700032NM 2003 7 7 AALA20030155 120030204A3397 WIRE BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21915AN 29516 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 6E AND 12 BROKEN. SECURED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030701000422003070100042SW 2003 7 1 HEEA086959 120030603A2435206062200123 STARTER GEN BELL 407 407 1182206SW ENGINE VIBRATION E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH779 53396 STARTER GEN HAS A HIGH FREQUENCY VIBRATION. REPAIRED. NO PROBLEM FOUND. 1G71 3U O H2SW 20030707001562003070700156EU 2003 7 7 03FDEA00988 120030627A7830 THRUST REVERSER AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 THRUST REVERSER ASSY-REPAIR OF FORMED ZEE ON CORE NACELLE INNER SURFACE. FACT 27JUN03 12:16 BFM R WORK COMPLIED ON EA NR 6-7832-70958_EXHAUST-TR ASSY-REPAIR OF FORMED ZEE ON CORE, COWL INNER SURFACE. 2L72 4F4 FRTA35EU E13NE 20030709001242003070900124EU 2003 7 9 MALA030291 120030605A211011341041 COMPRESSOR SAAB SF340 340B 7860101EU AIR CON ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15427XJ 340B427 SUPPLEMENTAL A/C PRODUCING ELECTRICAL BURNING ODOR IN A/C. MAINTENANCE REMOVED AND REPLACED SUPPLEMENTAL A/C COMPRESSOR MOTOR P/N 1134104-1, SN/ON 1031, SN/OFF 822. REMOVED AND REPLACED DRIVE BELT P/N 232L100, OPS CHECKS GOOD AT THIS TIME. MXC NOTIFIED REMOVED FROM DMR. 2L72 4T RTA52EU 20030710001142003071000114NE 2003 7 10 DHL2003747006 220030610A7261 ENGINE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE NR 1 MALFUNCTIONED A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO01747DH 22253 700363 IN-FLIGHT ENGINE NR 1 OIL FILTER BYPASS LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURES, SHUT DOWN ENGINE AS PER ABNORMAL PROCEDURES. DIVERTED TO KMCI. ON SHORT FINAL, LIGHT DID EXTINGUISH. INSPECTED FILTER, CHECKED GOOD. LEAK CHECKED GOOD ON ENGINE RUN. LIGHT DEFERRED PER MEL 79-4, DMI 13220. REF DMI NR 13220 NR 1 ENGINE OIL FILTER BYPASS LIGHT DMI INCORRECTLY DEFERRED UNDER MEL 79-4. CORRECT DMI SHOULD BE DHL MEL 79-2 PLACARD & DMI SHEET CHANGED TO REFLECT CORRECT MEL REF. REF DMI 13220 IN FLIGHT NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY INCLUDING OIL FILTER BYPASS SWITCH. SEE ITEM 1P LOG 327820. THIS CLEARS DMI 13220. PLACARD REMOVED. 2L73 4F4 F A3WE E2EA 20030107001212003010700121NM 2003 1 7 QXEA03000009 120030106A5270 HANDLE BOMBDRDHC8 DHC8401 1390041NM ZONE 800 A QXEAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 NM09403QX 4037 GEG - FLIGHT 2396 - CREW DIVERTED TO GEG WHEN DURING FLIGHT THE FUSELAGE DOOR WARNING STAYED ON FOR APPROXIMATELY 5 MINUTES. NO PROBLEM WITH PRESSURIZATION WAS EXPERIENCED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EXTERNAL DOOR HANDLE NOT FULLY IN THE RECESS. THE INTERNAL HANDLE MECHANISM WAS ADJUSTED AND A FUNCTIONAL CHECK WAS PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030109000742003010900074NM 2003 1 9 MWEA030026 120030109A5310993053875 DOUBLER DOUG MD88 MD88 3023688NM STA 475 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CUSP MEMBRANE CORRODED RIGHT SIDE AT STATION 475 AT LIGHTING HOLE. -- REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER AND SUPPORT GRILL. 2L72 4F RTA6WE 20030113000562003011300056NM 2003 1 13 PCAA0301013 120030112A7930PW120A ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LEFT LEAKING A PCAAO OTHER K FLUID LOSS APAPPROACH 1 EA13846EX257203454 326 121143 ELM-PIT FLIGHT#3856. CREW REPORTED LEFT ENGINE BELOW 40 PSI.WHILE ON APPROACH INTO PIT. ENGINE SHUT DOWN, EMERGENCY DECLARED. MAINTENANCE COMPLIED WITH UNSCHEDULED MAINTENANCE INSPECTION IN ACCORDANCE WITH PRATT AND WHITNEY MAINTENANCE MANUAL 05-50-00. NO DEFECTS WERE NOTED. REMOVED AND REPLACED MAIN AND SCAVANGE OIL FILTERS. INSPECTED AND FOUND CUT O-RING ON PROPELLER CONTROL UNIT.REMOVED AND REPLACED PROPELLER CONTROL UNIT AND PROPELLER CONTROL UNIT ADAPTER O-RINGS IN ACCORDANCE WITH ALLEGHENY AIRLINES JOBCARDS 008-6110-303 AND 008-6120-304 AND DEHAVILLAND DASH 8 MAINTENANCE MANUAL 61-10-00. GROUND RAN AIRCRAFT FOR APPROXIMATELY 25 MINUTES. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030114002052003011400205NM 2003 1 14 VNAA0301002 120030101A2450230GC02Y02 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT FAILED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07422JS151405079 3018 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AREA. MAINTENANCE INSPECTED AND FOUND THE 1VE PANEL WARM. MAINTENANCE THEN REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030124000842003012400084NM 2003 1 24 UPS03240057 120030107A5280 DOOR BOEING727 72721C 138400MNM WING LG R/H DOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01934UP 19135 INSPECTION TYPE:C WING LANDING GEAR DOOR R/H SIDE CRACK FOUND ON INSIDE OF DOOR REAR S PAR OF DOOR 19TH UP FROM BOTTOM OF DOOR CRACK IS ALONG BETWEEN 2 RIV ET HOLES REPAIR CARRIED OUT IAW SRM 51-40-2 2L73 4F A3WE 20030128001082003012800108NM 2003 1 28 PCAA0301025 120030127A3242DSC252A40230 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003NM OUTBOARD LEFT BURST A PCAAK NONE K FLUID LOSS NRNOT REPORTED 1 EA13843EX 335 BOS-FLIGHT#3898. CREW REPORTED MAIN AND EMERGENCY BRAKES FAILED AND LOSS OF #2 HYDRAULIC CONTENTS. MAINTENANCE REPLACED LEFT OUTBOARD BRAKE FLEX LINE. #2 HYDRAULIC SYSTEM SERVICED AND LINE BLED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030129000852003012900085SW 2003 1 29 HEEA083987 120030117A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20030210000352003021000035EA 2003 2 10 QXEA0300020 120030108A2820D98C07606 SENSOR CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAILED A QXEAK NONE J WARNING INDICATION CRCRUISE 1 NM09615QX369 10065 PDX-LEFT FUEL LOW PRESSURE CAUTION LIGHT ON INFLIGHT. REMOVED AND REPLACED ENGINE FEED PRESSURE SENSOR. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030219001602003021900160EU 2003 2 19 USAASA03005 120030117A3350321430 BATTERY AIRBUSA319 A319112 3930323EU CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19750UW 1315 BOS - THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT FAILED. MAINTENANCE REPLACED BATTERY. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20030220000702003022000070WP 2003 2 20 ABXA030073 120030129A532099234847 INTERCOSTAL DOUG DC9 DC941 302207NWP E/E BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23957AX 47759 INTERCOSTAL WAS CRACKED TWO PLACES, FS 180, LBL 22. REPAIRED AREA IAW DC-9 SRM 51-10-3, 51-10-3B, AND REA D953-46196. 2L72 4F A6WE 20030225000142003022500014SW 2003 2 25 HEEA084233 120030120A5320407070620156 HEADLINER BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 HEADLINER CRACKED. 1G71 3U O H2SW 20030228000952003022800095EU 2003 2 28 MALA030172 120030220A3150 WEU SAAB SF340 340B 7860101EU A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15361PX 340B249 DURING CLIMBOUT ON FLIGHT #2726, FLAP CAUTION LIGHT ILLUMINATED. FLAPS OPERATED NORMAL ON APPROACH. AIR RETURN TO MEM. MAINTENANCE RE-RACKED WARNING ELECTRICAL UNIT. PERFORMED OPS CHECK OF FLAP SYSTEM IAW SF3 MM 27-51-00-5 PROCEDURE 3. OPS CHECK GOOD. A/C RETURNED TO SERVICE 2L72 4T RTA52EU 20030306000102003030600010 2003 3 6 HEEA084723 420030217A2340 SWITCH BELL 412 412 1182202SW PA SIREN BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 1267 33076 PA SIREN POWER SWITCH BROKEN. FUSE F101 BAD. REPLACED POWER SWITCH AND FUSE. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000672003030600067SW 2003 3 6 HEEA084778 120030221A7810212061202010 DUCT BELL 412 412 1182202SW EXHAUST SYS CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 EXHAUST DUCT CRACKED. 1G72 4U H4SW 20030310000892003031000089 2003 3 10 HEEA084993 420030227A3120811B CLOCK BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 DIGITAL CLOCK WILL NOT KEEP TIME. REPAIRED. 1G72 4U H4SW 20030310001082003031000108SW 2003 3 10 HEEA085015 120030227A2841214066212103 PROBE BELL 214 214ST 1182106SW FUEL QUANTITY LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806119 28140 FOUND FUEL LEAKING THROUGH CENTER OF PROBE. ALSO CAPACITANCE VALVES CHECKED HIGH. 2G72 4U H10SW 20030310001302003031000130NM 2003 3 10 EIA2003034 120030225A5300UNK DOOR FRAME BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 BULK PIT DOOR CUT OUT HAS BENT AND GOUGED EDGE APPROXIMATELY 14 IN. UP FROM FORWARD LOWER CORNER. CORRECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECTION OF AREA, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-157-2 Rev A 2L74 4F A20WE 20030313001302003031300130CE 2003 3 13 KKI2003F00000 120030128A6123 PIN CESSNA310 310F 2074216CE CONT O470 IO470D 17026SO FEATHERING WRONG PART A KKIAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW99317L 3100126 C510517280 DURING ANNUAL INSPECTION, IT WAS FOUND THAT FEATHERING PIN ASSY MOUNTED ON THIS PROPELLER IS WRONG PART. PART AS INSTALLED IS MOUNTED ON TOP OF TWO RIVETS IN SPINNER BULKHEAD, CAUSING PART TO BE BENT OVER THE RIVETS AND WEARING ON BLADE CLAMPS. LEFT UNREPAIRED IT COULD SERIOUSLY COMPROMISE INTEGRITY OF THE BLADE CLAMP OR LATCH ASSY COULD FINALLY BREAK DUE TO STRESS. LATCH ASSY SHOULD HAVE CAST INTO ASSY, STAND-OFFS ON BOTTOM TO GIVE CLEARANCE FOR RIVETS. CORRECT ASSY SHOULD ALSO HAVE INDENTIONS CAST INTO MOUNTING POINTS TO GIVE CLEARANCE FOR PROP FLANGE MOUNTING BOLTS. ASSY AS MOUNTED HAS BEEN FORCED INTO POSITION AND PROP MOUNTING BOLTS HAVE LEFT THREAD GOUGES WHERE BOLT WAS FORCED PAST ASSY. 1L72 3O3 O 3A10 3E1 20030121000112003012100011NM 2003 1 21 SWAA030072 120030113A532065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER CLIPS CRACKED, BS 727B, STR 4L AND BS 847, STR 4R. REMOVED AND REPLACED BOTH STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030122001402003012200140NM 2003 1 22 DL757030014 120030102A5315146N51114 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27610DL 22817 THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE ALL OF THE DAMAGE, THE UPPER CAP WAS TRIMMED OFF FROM LBL 60 TO RBL 60. A NEW CAP WAS FABRICATED AND INSTALLED PER ER/A 384247-14, REV A. 2L72 4F RTA2NM 20030314001332003031400133WP 2003 3 14 GTIA030110 120030211A5313 LONGERON DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 PAX CABIN, LONGERON 17L CRACKED AT STATIONS 236, 370 AND 427. REMOVED LONGERON 17L FROM STA 417 TO STA 436. REMOVED CRACKED LONG. 17L FROM STA 303 TO STA 323. REMOVED LONGERON 17L FROM FS 230-250. REMOVED LONGERON 17L FROM FS 380 - FS 398. LOCATED AND DRILLED SPLICE. INSTALLED LONGERON REPAIRS AND SPLICES. 2L72 4F4 F A6WE E2EA 20030122001602003012200160NE 2003 1 22 HEEA083539 120030113A6700 BEARING SKRSKYS76 S76A 8143006NE BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K 760082 BELLCRANK HAS WORN BEARINGS. REPLACED WITH SERVICEABLE BEARINGS. 1G72 3U H1NE 20030326000272003032600027EU 2003 3 26 AUS20030122 120030124A6123750420504 O-RING FOKKERF27 F27MK50 EU PWA PWA120PW125B NE PROPELLER FAILED W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) LT ENGINE FEATHERING PUMP INLET BOBBIN O-RING SEAL FAILED. LOSS OF ENGINE OIL. 2H72 4T4 TRTA817 E20NE 20030327000022003032700002 2003 3 27 AT0300008 420030325A31604082170912 DISPLAY BOEING717 717200 1383700NM COCKPIT ODOR A ZZDAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO15945AT 55008 ELECTRICAL FUMES IN COCKPIT ON TAKEOFF. RETURNED TO AIRPORT. LDG WT 102.5. 2L72 4F TRA6WE 20030326000462003032600046 2003 3 26 CA030210005 420030205A34189754421422 TRANSMITTER PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL AOA UNSERVICEABLE W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) DURING THE OPERATIONAL TEST OF THE PROBE DE-ICE SYSTEM, IT WAS NOTICED THAT THE RT VANE HEAT WAS U/S. THE RT AOA TRANSMITTER WAS REPLACED WITH NEW AND THE OPERATIONAL TEST PREFORMED SATISFACTORY. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030324000442003032400044EU 2003 3 24 A1U2003F00000 120030216A530210530401118 SKIN BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE VERTICAL STAB DAMAGED E A1UAO OTHER O OTHER NRNOT REPORTED 1 CE03440SL7012 7158 7158 THE AIRCRAFT WAS LOCATED ON A HELIPAD, ON START UP THE PILOT NOTICED A ABNORMAL VIBRATION AT APPROX 45 PERCENT N1 / 25 PERCENT ROTOR, AND ABORTED THE START. UPON FURTHER INSPECTION A DENT APPROX 5 INCHES LONG, AND A TEAR APPROX 4 INCHES LONG, ON THE LEADING EDGE OF THE VERTICAL STABILIZER STARTING APPROX 5 INCHES BELOW THE GEARBOX MOUNT AND CONTINUING DOWNWARD TOWARD THE LEFT HAND SIDE WERE DISCOVERED. THE DAMAGED WAS DETERMINED TO BE UNAIRWORTHY. SUSPECTED CAUSE OF DAMAGE IS ICE BEING SLUG FROM THE MAIN ROTOR OR MAIN ROTOR HUB DURING THE START PROCEDURE. ICING CONDITIONS WERE PRESENT AT THE TIME. TT 7012.4 TOTAL LANDINGS: 22,595 1G72 3U3 U H13EU E5NE10 20030324001002003032400100NM 2003 3 24 AWXA200300091 120030128A532065535953 REVEAL BOEING737 737300 1384610NM DOOR FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/4 INCH CRACK WAS FOUND ON R-1 DOOR FORWARD UPPER REVEAL BS 305, STR 16 R/H. MAINTENANCE REMOVED R-1 DOOR FORWARD UPPER REVEAL; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3-4. 2L72 4F RTA16WE 20030326001072003032600107EA 2003 3 26 A6WA200340032 120030304A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT WINDOW FAILED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 RT WINDOW HEAT CAUTION MESSAGE REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD A THIS TIME. 2L72 4F4 FRTA21EA E15NE 20030722000092003072200009NM 2003 7 22 2003F00437 120030124A5514 HINGE PIN BOEING727 727222 1384073NM HORIZONTAL STAB CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND HORIZONTAL STAB, LEFT OUTER HINGE PIN, IS CRACKED AND CORRODED. REMOVED AND REPLACED HORIZONTAL STAB RIGHT OUTER HINGE PIN. (M) 2L73 4F A3WE 20030422001562003042200156WP 2003 4 22 MWEA030129 120030305A7620 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE RIGHT FAILED A MWEAE ENGINE SHUTDOWN E VIBRATION/BUFFET CLCLIMB 1 GL31216ME 47740 665323 AT 32,500 FEET AIRCRAFT SUFFERED SEVERE ENGINE VIBRATION, RIGHT ENGINE OIL PRESSURE WENT TO ZERO AND RIGHT HYDRAULIC FLUIDS QUANTITY WAS AT ZERO. REMOVED AND REPLACED ENGINE. 2L72 4F4 F A6WE E2EA 20030421001262003042100126WP 2003 4 21 IXXA0300018O 120030223A3260 CONNECTOR DOUG DC8 DC873F 302199FWP MLG DOWNLOCK LOOSE A IXXAO OTHER N FALSE WARNING LDLANDING 1 SW11605AL916872337 46106 DURING FINAL APPROACH FOR LANDING INTO PHIK. CREW NOTED NOSE LANDING GEAR DOWN AND LOCKED LIGHTS WERE NOT ILLUMINATED. USING VISUAL INDICATOR CREW VERIFIED GEAR WAS SAFE. ADDITIONALLY CREW PERFORMED FLY-BY OF CONTROL TOWER AND AGAIN CONFIRMED GEAR WAS IN SAFE CONDITION. CREW COMPLETED AN UNEVENTFUL LANDING IN PHIK. UPON INSPECTION MAINTENANCE DISCOVERED ELECTRICAL CONNECTOR ON NOSE LANDING GEAR DOWNLOCK SWITCH INSECURE. THIS CONNECTOR WAS SECURED AND THE SYSTEM OPERATIONALLY CHECKED GOOD. ALL WORK WAS PERFORMED PER APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20030321000802003032100080NM 2003 3 21 2003UALA00222 120030227A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29953UA 26700 STATION 188 FRAME CRACKED AT WL 207 LEFT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030805000142003080500014CE 2003 8 5 HYI2003F00005 120030521A2400CM358950 MASTER SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LT PANEL FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE0168752534 402C0518 SWITCH FAILED, MAINTENANCE REPLACED SWITCH AND RETURNED THE AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20030724000672003072400067NM 2003 7 24 AWXA200300764 120030619A57206569646150 COVER BOEING737 7373Y0 1384671NM RT WING CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK THE RT WING T/E FLAP WELL CORNER BOX COVER PLATE WAS FOUND CHAFED, OUTBOARD OF THE NR 2 PYLON. MAINTENANCE REMOVED CHAFED RT WING T/E FLAP WELL CORNER BOX COVER PLATE; FABRICATED A NEW REPLACEMENT COVER PLATE; INSTALLED REPAIR PART IAW AWA ER 03-5750-03175-TB1. 2L72 4F RTA16WE 20030806001572003080600157SO 2003 8 6 C2XA03SH211 120030701A531114522461011 FRAME EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 DURING C-CHECK, THE DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030902001352003090200135NM 2003 9 2 03FDEA00939 120030618A5710ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RT- O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT POINT BUSHING FOUND LOOSE. RT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT POINT BUSHING REPLACED IAW EA 1-5750-69375, TITLE: WINGS- TRAILING EDGE FLAP- RT OUTBOARD FLAP- INBOARD SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030814000382003081400038NM 2003 8 14 SWAA031765 120030807A2560P2070001 FLASHLIGHT BOEING737 7377H4 1384404NM FWD CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29431WN 29845 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY FLASHLIGHT PER MM. 2L72 4F RTA16WE 20030724000432003072400043NM 2003 7 24 DL757030542 120030612A5330148N32112 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27614DL 22821 FUSELAGE, SKIN, FS 1723 STRINGER 19R, REPAIR OF DENT. A DENT WAS FOUND IN THE FUSELAGE SKIN AND CUTOUT. A REPAIR DOUBLER WAS INSTALLED WITH A MINIMUM OF THREE ROWS OF REPAIR FASTENERS. ERA 384755-14 REV B. 2L72 4F RTA2NM 20030729000462003072900046NM 2003 7 29 ZW0A0305708 120030702A256069B148553 SPRING BOEING757 757231 1384950NM GIRT BAR BENT A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13721TW 29954 THE EVACUATION SLIDE LEAF RETENSION SPRINGS WERE REPLACED ACCOUNT BENT AT THE L1 AND R2 CABIN DOORS. 2L72 4F RTA2NM 20030729000532003072900053WP 2003 7 29 ZW0A0305901 120030716A2910 HYDRAULIC LINE DOUG DC9 DC983 3022083WP HYD SYSTEM LEAKING A ZW0AA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE13110HM 49787 JUST AFTER TAKE OFF CREW REPORTED SMOKE IN CABIN WITH CORRESPONDING LOSS OF RH HYDRAULIC SYSTEM. FLIGHT RETURNED TO STL. CREW MANUALLY EXTENDED THE LANDING GEAR. THE NOSE GEAR HYDRAULIC "UP" LINE, BETWEEN THE E AND E COMPARTMENT AND THE FWD CARGO COMPT, WAS REPAIRED DUE TO LEAKING. THE SMOKE WAS CAUSED BY HYDRAULIC FLUID INTO THE APU INLET. 2L72 4F RTA6WE 20030815000252003081500025SW 2003 8 15 HEEA088538 120030722A7120 BEARING BELL 206 206L3 1182108SW LEG ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 BEARING WORN. SHOP REPAIR. 1G71 3U H2SW 20030822001682003082200168WP 2003 8 22 UPS03841024 120030723A5544565622911 WEB DOUG DC8 DC873F 302199FWP RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 INSIDE RUDDER NR 2 HINGE CUTOUT WEB IS CRACKED AT ZR 159.094. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 5656229 AND SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20030821002592003082100259WP 2003 8 21 GTIA030588 120030630A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND RIGHT INBOARD SEAT TRACK UNDER G2 CORRODED AT FS 200-256. REMOVED SECTION OF SEAT TRACK, RIGHT INBOARD AT FS 200 TO 265. FABRICATED LOCATED AND DRILLED NEW SECTION OF SEAT TRACK. INSTALLED NEW SECTION OF TRACK. (M) 2L72 4F A6WE 20030826000742003082600074EU 2003 8 26 3144052803 120030523A6410355A12005004 BLADE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR DELAMINATED E S4WAK NONE O OTHER ININSP/MAINT 1 WP075226R2066 3144 22090 T/R BLADES NEED PAINTING. 1G71 3U3 U H9EU E00054EN 20030910001162003091000116NM 2003 9 10 2003UALA00556 120030714A1430 BOLT BOEING777 777222 1385219NM PWA PW4077PW4077 NE FLAPERON LOOSE A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29770UA 26925 FLAPERON BOLT LOOSE. 2L72 4F4 FRTT0001SE E46NE 20030910001292003091000129NM 2003 9 10 MWEA030344 120030827A532099306121 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 SUBFLOOR BETWEEN FRAME STATION 984 & 1003 CORRODED AT CUSP. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030930000432003093000043NE 2003 9 30 2003UALA00662 220030829A7320 ENGINE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE RIGHT MALFUNCTIONED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29668UA 30024 727574 POWER LOSS ON RIGHT ENGINE. INADEQUATE FUEL SUPPLY PROVIDED TO ENGINE. NO INDICATION OF MECHANICAL OR ELECTRONIC SYSTEM FAULTS. NO FURTHER ANOMALIES INDICATED. 2L72 4F4 FRTA1NM E24NE 20030909000682003090900068CE 2003 9 9 52034 120030628A3260H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162CE LANDING GEAR FAULTY A AMWAO OTHER N FALSE WARNING APAPPROACH 1 CE07126YV UE126 DURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3GREEN) INICATIONS. LANDING NORMAL WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED ON THE TAXI WAY AND THE AIRCRAFT WAS TOWED TO THE HANGAR. MAINTENANCE REPLACED THE UPLOCK SWITCH. NO TEARDOWN REPORT WILL BE REQUIRED DUE TO THE PART NOT BEING A REPAIRABLE PART. 2L72 4T RTA24CE 20030909000762003090900076SO 2003 9 9 SWIA200312299 120030823A2797 WIRE EMB 120 EMB120ER 3260203SO COCKPIT DAMAGED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07251YV 120251 CAPT'S FLIGHT DIRECTOR PITCH WANDERS IN FLIGHT. FIRST OFFICERS AUTOPILOT WAS ENGAGED AND THE AUTOPILOT FAIL ILLUMINATED ON MAP. REPAIRED WIRING TO NR 1 GO-AROUND SWITCH AND COPILOTS TRIM SWITCH WIRES ON YOKE. AP SYSTEM OPS CHECKED GOOD IAW MM 22-11-00. 2L72 4T RTA31SO 20031007001252003100700125WP 2003 10 7 MWEA030373 120030916A533059360023 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 DENT LOCATED BETWEEN LONGERON 26 LEFT AND 25 LEFT AT STATION 694. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20031021000692003102100069SO 2003 10 21 SIMA200325902 120030915A2611 SMOKE DETECTOR EMB 135 EMB135KL 3260302SO CARGO BAY MALFUNCTIONED A SIMAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21801AE 145469 IND - FLT 4296 - IN FLIGHT DURING CLIMB PASSING 600 FT BAGGAGE SMOKE LIGHT ILLUMINATED. CREW DISCHARGED BOTTLES, DECLARED EMERGENCY LANDED WITHOUT INCIDENT. INSPECTED BAGGAGE SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. RAI FIRE BOTTLES AND A/C RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031021002402003102100240SO 2003 10 21 C2XA03SH337 120030920A531014521699003 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 SHV-DURING C-CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031022001122003102200112EA 2003 10 22 COMA0360420 120030921A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01528CA 7841 DURING DECENT INTO DTW RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20031027000552003102700055NM 2003 10 27 0301796314 120030922A2530 OVEN BOEING747 747451 1384940NM GALLEY 1B BURNED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01674NW 30269 DURING FLIGHT, THE NR 2 OVEN IN GALLEY 1B EMITTED A BURNING ODOR. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED OVEN. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040115001422004011500142 2004 1 15 DL777031107 420031018A256562772215 SLIDE BOEING777 777232 1385232NM L2 DOOR UNSECURE A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27862DA 29734 UPON OPENING L2 DOOR, SLIDE CAME UNLATCHED. DID NOT DEPLOY. REINSTALLED SAME. 2L72 4F RTT00001SE 20040210001092004021000109EU 2004 2 10 USAA030312 120031124A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORROSION .125 SQUARE INCH AREA, LBL 17.75 FRAME 55. DAMAGED TRACK REPLACED WITH NEW SECTION PER SRM 57-74-00 AND SRM 51-72-11. (M) 2L72 4F RTA46NM 20030910000152003091000015WP 2003 9 10 DHL2003604546 120030519A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTBD STUB WING FORMER AT STA XS. 512.000 WITH 1.000 CRACK IN IT. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030910000272003091000027EU 2003 9 10 BAQA088185 120030720A2121 BLADE BOLKMSBK117 BK117C1 5626025EU BLOWER FAN SEPARATED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY71 0188 7544 FAN BLADE DEPARTED HUB. REPLACED WITH SERVICEABLE UNIT. 1G72 3U NCH13EU 20031030000272003103000027NM 2003 10 30 UPS03441285 120030905A5712 RIB BOEING747 747121 1384871NM NR19 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 19 V/C FLAP O/B LINKAGE I/B RIB NR 1, NR 7 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION. NR 1, NR 7 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTION. 2L74 4F A20WE 20031103000192003110300019NM 2003 11 3 DL777030873 120030924A2530267SV CHILLER BOEING777 777232 1385232NM A3 GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27877DA 29739 ELECTRICAL ODOR FROM AFT GALLEY CHILLERS. REMOVED AND REPLACED A3 CHILLER. 2L72 4F RTT00001SE 20031031000562003103100056NM 2003 10 31 QXEA200301207 120030926A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 SEAT TRACK NO.11 HAS PITTING CORROSION AT STATION 445. REPAIRED IAW DHC-8 SRM 51-40-11, 51-40-00 AND RD 8-53-1339. 2H72 4T4 TRTA13NM E20NE 20031107001682003110700168NM 2003 11 7 AALA20031050 120030922A3397 WIRE BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21372AA 25199 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT STATION 870. RECONNECTED WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031110000422003111000042SO 2003 11 10 C2XA03TY193 120031008A532014520600003 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 TYS DURING A SCHEDULED 3C INSPECTION THE RT SIDE OF THE RAMP ANGLE WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030730001152003073000115WP 2003 7 30 03FDEA01149 120030725A5753 SKIN DOUG DC10 DC1010 3022110WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 COMPLY WITH EA 8-5750-70992. RT INBD FLAP UPPER SKIN REPAIR AT XIFH 279.360. CLOSING ACTION ON 07-23-03 COMPLIED WITH EA 8-5750-70992. 2L73 4F A22WE 20030731000042003073100004NM 2003 7 31 03FDEA01132 120030724A2910BACH8C04NN0103 HYDRAULIC LINE BOEING727 727200 138407ENM PWA JT8 JT8D* NE HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25246FE 22068 PASSING 17,000 FEET IN A NORMAL CLIMB BOTH HYDRAULIC SYSTEM "A" PUMP LOW PRESSURE LIGHTS CAME ON, FOLLOWED BY A COMPLETE LOSS OF SYSTEM "A" QUANITY. PERFORMED STABILIZERS EXECUTED CHECKLIST IAW QRH. DECLARED IFE AND LANDED UNEVENTFULLY AT IAH. INSTALLED NEW LINE ON 'A' SYSTEM PRESSURE TRANSMITTER.OPS. AND LEAK CHECK OK. REF: MM 29-11-00-6PG1B.OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20030918000112003091800011NM 2003 9 18 03FDEA01510 120030911A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 DAMAGED STRINGER BS 647 STR 21R. CUT OUT DAMAGE & REPAIRED PER SRM 51-10-3 FIG 1 2L73 4F RTA3WE 20031117000532003111700053NM 2003 11 17 DHL2003749501 120030919A5730 SKIN BOEING727 7272J0 138407ENM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK, WS 464 UPPER LT WING L/E SURFACE IS CRACKED AT RIVET (SKIN). REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2 AND CUT OUT DAMAGED AREA DIM 2.375 X 1.25 INCHES. FABBED DOUBLERS FROM 2024 T3 .050 PO 90096 DIM 7.25 X 6 INCHES AND 7.25 X 4.5 INCHES AND FILLER FROM 2024 T3 .040 PO 90024 DIM 2.375 X 1.25 INCHES IAW B-727 SRM 57-30-4 FIG 4 SHEET 6 REPAIR III. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED IAW B-727 SRM 57-30-4 FIG 4. 2L73 4F RTA3WE 20031119000432003111900043 2003 11 19 QXEA200301225 420031008A3160C19190AB04 DISPLAY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09413QX4133 4133 4060 ON FLIGHT 2292 DURING TAKEOFF AFTER GEAR HANDLE WAS SELECTED UP THE NR2 MFD FLICKERED FOR JUST A MOMENT AND THEN WE GOT A CHECKED MESSAGE ON THE ED AND NR 2 MFD. RAN EMERGENCY CHECKLIST, ALL INDICATIONS NORMAL BUT MESSAGE DIDN'T GO AWAY. REMOVED AND REPLACED NR 2 MFG. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUNED TO SERVICE. 2H72 4T RTA13NM 20040114002102004011400210NM 2004 1 14 MWEA030481 120031215A53305911410531 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FUSELAGE SKIN DENTED AT STATION 237 LONGERON 18 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F RTA6WE 20031217000632003121700063WP 2003 12 17 DHL2003807519 120031015A53203750257U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 FWD CARGO COMPT SPLICE FITTING CRACKED 9.000 L-31R STA 610.000. MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING WITH NEW FASTENERS AND PRC SEALANT IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20031217000932003121700093NM 2003 12 17 QXEA200301463 120031120A2797 WIRE DHAV DHC8 DHC8202 2809007NM LT WING BROKEN A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09362PH 518 ON FLIGHT 2246 SPOILER 2 PFCS SWITCH LIGHT ILLUMINATED IN FLIGHT. REPAIRED BROKEN WIRES ON LEFT WING SPOILER CLUTCH QUADRANT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. 2H72 4T RTA13NM 20031218000422003121800042NM 2003 12 18 AWXA200301501 120031126A3350100865 BATTERY BOEING757 7572S7 1384962NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 DURING INSPECTION FOUND THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY (M731), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20031229001822003122900182SO 2003 12 29 SWIA200312677 120031116A5311 FRAME EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07227SW 120304 RIGHT WING FRAME 16 HAS A CRACKED SKIN CLIP (BOTTOM). DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER SKIN CLIP AT FRAME 16 OF RIGHT WING PER SRM 51-40-2. NO LEAKS NOTED. 2L72 4T RTA31SO 20031229001182003122900118NM 2003 12 29 SWAA032724 120031214A335065C27095 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 AFT RT FUSELAGE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20031231000162003123100016NE 2003 12 31 TSAA0379039 220030223A726169726881 SWITCH BOEING737 7372M6C 1384708NM PWA JT8 JT8D9A 52048NE ENG OIL BYPASS INOPERATIVE A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13805AL 21809 P666775 DURING CLIMB, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE NR 1 ENGINE WAS SHUTDOWN IAW THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED IN HNL WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE OIL BYPASS SWITCH AND THE OIL FILTER ELEMENT. THE NR 1 ENGINE OIL TANK WAS DRAINED AND SERVICED. GROUND OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTA16WE E2EA 20031231000302003123100030NM 2003 12 31 TSAA0328194 120031202A2822 PUMP BOEING737 73776N 13844CHNM NR 1 FUEL MALFUNCTIONED A TSAAO OTHER J WARNING INDICATION CLCLIMB 1 WP13749AL 32738 DURING CLIMB, THE NR 1 AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. ERTURNED TO HNL. TROUBLESHOOT PER FIM 28-22-804, FAULT FOUND TO BE IN THE LOW FUEL PRESSURE INDICATING CIRCUIT. DEFER PER MEL 28-3-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031231001132003123100113 2003 12 31 GTIA030942 420031022A2340 INTERPHONE DOUG DC9 DC981 3022081WP CABIN SHORTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 CALL SYSTEM C/B POPS WHEN ANY CALL BUTTON PRESSED. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F A6WE 20031231001312003123100131EU 2003 12 31 MALA030556 120031217A36107063250 DUCT SEAL BAC 146 AVRO146RJ85A1500097EU BLEED AIR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15504XJ E2311 DURING FLIGHT 3441, RIGHT ZONE HI TEMP ANNUNCIATOR CAME ON AT FLIGHT LEVER 350. AIR RETURN TO MSP. MAINTENANCE REPLACED Y-DUCT SEALS ON LEFT Y-DUCT AS REQ P/N 706-3-250 REF 409 215043 & CONT CARD 096333 FOR DETAILS. 2H74 4F RTA49EU 20031009000272003100900027SO 2003 10 9 SIMA200317404 120030619A2460 RELAY EMB 135 EMB135LR 3260305SO APU INOPERATIVE A SIMAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW21731BE 145356 DURING CLIMB CREW REPORTED AN ELECTRICAL EMERGENCY ABNORMAL EICAS MESSAGE ABOUT 1 SECOND AFTER TURNING APU OFF AS PER CLIMB-OUT PROCEDURE. AIRCRAFT WAS RETURNED TO FIELD. THE CREW RESTARTED THE APU AND REESTABLISHED ELECTRICAL POWER TO THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED RELAYS K0018 AND K0019 (P/N M83536/19-008L AND M83536/19-008L) IAW WITH EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031010000542003101000054NM 2003 10 10 03FDEA01563 120030918A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 2 DENTS IN 3 INCH AREA, ON FWD CARGO FRAME, BS 500 BETWEEN STR 23R AND 24 R. **SD** COMING 2L73 4F RTA3WE 20031009000282003100900028SO 2003 10 9 SIMA200315302 120030601A3350 CONNECTOR EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT DISCONNECTED A SIMAO OTHER L NO TEST ININSP/MAINT 1 SW21810AE 145525 CREW REPORTED GALLEY EMERGENCY LIGHTS AND RIGHT BULKHEAD EMERGENCY LIGHT WERE INOPERATIVE. FOUND CONNECTOR BY SERVICE DOOR OVERHEAD CEILING PANEL DISCONNECTED AT P8530. RECONNECTED CONNECTOR, OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20040108001152004010800115EU 2004 1 8 KBM2003F00065 120031019A6220XEMRE8RSA8 BEARING SNIAS 350 AS350B1 8680811EU MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 BLUE MAIN ROTOR, PITCH CHANGE ROD, UPPER AND LOWER ROD END. BEARING HAS EXCESSIVE PLAY. BOTH MEASURED .012 INCH, WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW. 1G71 3U H9EU 20031124000762003112400076NM 2003 11 24 QXEA200301410 120031108A2610 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 200 ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09413QX 4060 ON FLIGHT 2294 CHECK FIRE DETECTION LIGHT CAME ON IN FLIGHT THEN WENT OUT AFTER SEVERAL SECONDS. MASTER WARNING CAME ON WITH CHECK FIRE DETECTION, BUT NO OTHER LIGHTS OR INDICATIONS CAME ON OR STAYED ON. TROUBLESHOOT SYSTEM IAW FIM 26-10-00 AND RAN AIRCRAFT ENGINES AT POWER FOR 10 MINUTES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031125000012003112500001NM 2003 11 25 DHL2003748011 120031122A3350 LIGHT BOEING727 727225 1384077NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01748DH 22440 EMERGENCY LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW BMM CHAPTER 33-50-00, OPS CHECKED GOOD. 2L73 4F A3WE 20031125001712003112500171 2003 11 25 SWAA032468 420031106A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031202000842003120200084EA 2003 12 2 ASOA03526 120031020A7830600592111 DIODE CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11848AS 7339 FLT 4529 - DURING CLIMB-OUT FROM ATL-MGM, THE CREW RECEIVED A LEFT THRUST REVERSER UNLOCK AMBER CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE LEFT ENGINE WAS REDUCED TO FLIGHT IDEL FOR A SINGLE ENGINE LANDING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED TERMINAL DIODE MODULE 207-7 AND ZENER DIODE 1CR1KE. OPS CHECK OF THE SYSTEM GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031203001172003120300117EU 2003 12 3 A6WA200360066 120031106A5753 STRUCTURE BAG BAE146BAE146200A 1500266EU TE FLAP DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31292UE E2087 OVERSIZED BUSHING REQUIRED IN TWO PLACES ON RIGHT FLAP P/N HC579L1400-001, S/N 838H52-86. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1701-692001. (M) 2H74 4F RTA49EU 20040121000992004012100099WP 2004 1 21 GTIA030996 120031118A2751 INDICATOR DOUG DC9 DC981 3022081WP STAB TRIM STICKING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 STAB TRIM INDICATOR ON PEDESTAL STICKS WHEN MOVING. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F A6WE 20040123000802004012300080EA 2004 1 23 SVU2004F00011 120031218A2740 CAPACITOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MCV BROKEN B SVURO OTHER O OTHER NRNOT REPORTED 1 SW19906SW6680 901 7510 MOTOR CONTROL UNIT CAPACITOR BROKEN MAKING CHANNEL NR 1 INOPERATIVE. 2L72 4F4 FRTA21EA E15NE 20031204000892003120400089WP 2003 12 4 UPS03841400 120030907A53409887940501 ATTACH ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, FWD PIT SMOKE BARRIER UPPER ATTACH ANGLE CORRODED NEAR CENTER LINE. REMOVED CORR IAW DC8 SRM 51-1-8, ORIG .063 INCH, REMOVED .014 INCH, REMAINING .049 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FORMED 2 ANGLES AND SPLICE ANGLE IAW DC8 SRM 51-1-4 & DAC DWG 9887940, HT TREATED IAW DC8 SSRM 51-1-1, ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED 2 ANGLES AND SPLICE ANGLE IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20031202001642003120200164SO 2003 12 2 SIMA200328802 120031013A33207287503607 LIGHT EMB 145 EMB145LR 3260212SO GALLEY INOPERATIVE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21633AE 145148 CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE GALLEY AREA. MAINTENANCE REMOVED AND REPLACED THE FORWARD PASSENGER LIGHT ASSEMBLY ABOVE ROW 2A IAW RMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031208001472003120800147NM 2003 12 8 2003UALA00802 120031022A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 SHEAR TIE AT STA 639 BELOW STR 7 LT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20031209000422003120900042EA 2003 12 9 SWIA200312549 120031015A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 1 SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07597SW3018 3018 7293 FLT SPLR FAULT STATUS MESSAGE ILLUMINATED AFTER SPOILERS DEPLOYED IN FLIGHT. MESSAGE CLEARED ON SHUTDOWN. AFTER SHUTDOWN, SPOILERON FAULT ILLUMINATED. REMOVED AND REPLACED NR 1 SPOILER ELECTRONIC CONTROL UNIT IAW CRJ MM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20031211000102003121100010NM 2003 12 11 AWXA200301376 120031028A5320654583468 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK A .375 INCH CRACK WAS FOUND ON TIE STRAP AT LOWER FORWARD SIDE OF BEAM BS 344, LBL 51. MAINTENANCE CUT OUT DAMAGE ON TIE STRAP BS 344, LBL 51; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1-4. 2L72 4F RTA16WE 20031020002662003102000266NM 2003 10 20 03283407 120031010A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27407FJ 3157 DURING INSPECTION THE EMERGENCY LIGHTS NEAR SEATS 4 AND 5 B AND C WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030919001152003091900115EU 2003 9 19 AWXA200300926 120030802A5320D5323028120140 ANGLE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK A .5000 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FAIRING SUPPORT ANGLE AT FR 34, Y1600, Z2000. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT FR 34, Y1600, Z2000; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-10, & 12, FIG. 2 & 3. 2L72 4F RTA28NM 20030917000592003091700059CE 2003 9 17 DXTA200300104 120030827A3110 CIRCUIT BREAKER CESSNA750 750 2076810CE COCKPIT TRIPPED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07908QS 7500108 DURING CLIMB THRU 7000 FEET " REMOTE CB TRIPPED" CYAN CAS MESSAGE ILLUMINATED AND ELECTRICAL FIRE SMELL WAS NOTED IN COCKPIT, NO SMOKE SEEN IN AIRCRAFT. FOUND PASSENGER SAFETY SIGN ON ESCAPE HATCH SHORTED. REMOVED AND REPLACED PASSENGER SAFETY SIGN WITH NEW SIGN IAW CITATION 750 INTERIOR MAINTENANCE MANUAL, CHAPTER 25-94-14. 2L72 4J RTT00007WI 20030918000202003091800020NM 2003 9 18 2003F00563 120030627A5320 CLIP BOEING737 7372L9 1384497NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37464AT 21278 DURING C-CHECK INSPECTION AND WHILE ACCOMPLISHING SERVICE BULLETIN SB 737-53-1204, THE UPPER AND LOWER ATTACH ANGLES WHERE FOUND TO BE CRAKCED AT THE INTERCOSTAL ATTACH POINT, BS 294.5 AND STRINGER 12L. THE REPAIRS ARE BEING ACCOMPLISHED ON NON-ROUTINE 031770. TOTAL CYCLE 41351, TOTAL TIMES 46985.2. (M) 2L72 4F RTA16WE 20030922000672003092200067NM 2003 9 22 AWXA200300944 120030819A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 19 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030923000312003092300031WP 2003 9 23 DHL2003604560 120030520A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING LW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING CENTER L/E FRAME CRACKED 1.000, XFS.366.500 (UPPER INNER). STOP DRILLED CRACK AT XFS.366.500 AND FABRICATED ANGLE DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D PG.9, SRM 51-1-21 PG.1 2L74 4F RT4A25 20030924000702003092400070NM 2003 9 24 2003UALA00627 120030815A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 BS 616L FRAME CRACKED BELOW FLOOR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030924001252003092400125 2003 9 24 AALA20030817 420030730A2565D03654122 SLIDE BOEING757 757223 1384957NM R1 DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21663AM 25297 UPON ARRIVAL R1 SLIDE FELL FROM COVER ASSEMBLY WHEN DOOR OPENED BY SKYCHEF CATERING. DOOR ASSIST BOTTLE DEPLETED. SLIDE DID NOT DEPLOY. REPLACED R1 SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030924001182003092400118EU 2003 9 24 226080903 120030809A21505613C000002 ACM PILATSPC12 PC1245 7090551EU AIR CONDITIONINGWORN E S4WAO OTHER O OTHER CRCRUISE 1 WP07308NA 226 ECS WILL NOT COOL AIR BELOW 105 DEGREES F. 1L71 3T RTA78EU 20040127002332004012700233WP 2004 1 27 ASAA0380655 120031015A53473930566117 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND SEAT TRACK CORRODED. REPLACED SEAT TRACK. (M) 2L72 4F A6WE 20040130001262004013000126NM 2004 1 30 DHL2003750009 120031225A2741129700008 ACTUATOR BOEING727 7272M7 138407SNM CRUISE TRIM FAILED A DHLAO OTHER O OTHER DEDESCENT 1 SO01750DH 21951 STABILIZER JAMMED ONLY IN NOSE UP TRIM. NOSE DOWN TRIM WORKS NORMAL DURING DESCENT. PERFORMED ABNORMAL PROCEDURE WITH NO RESULT. FLAPS 15 DEGREES LANDING IN CVG. REMOVED AND REPLACED CRUISE TRIM ACTUATOR AND MAIN ELECTRIC STAB TRIM ACTUATOR IAW B-727 M/M 27-40-31. SYSTEM OPS CHECKED GOOD IAW B-727 M/M 27-40-00. LUBED JACK SCREW. 2L73 4F A3WE 20040204001752004020400175SO 2004 2 4 GLBA2003141 120031030A3210 LANDING GEAR EMB 120 EMB120ER 3260203SO MAINS FROZEN A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03293UX 120293 RT MLG WOULD NOT RETRACT, DEICE GEAR. OPS CK GOOD. 2L72 4T RTA31SO 20040212000782004021200078NE 2004 2 12 MDR03016 120030619A6320643520017014 HOUSING SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE M/R GEARBOX CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09164AC 1671 A6039 64334D MGB, UPPER HOUSING, CRACKED UNDER NR 1 INPUT, LT SIDE. THE FIELD CREW NOTICED OIL LEAKING FROM MGB UPPER HOUSING UNDER NR 1 INPUT. INITIAL INSPECTION BY SHOP INDICATED OIL RESIDUE IN AREA, BUT NO CRACK WAS NOTICED. FPI INDICATED NO CRACK. HEAT GUNS WERE USED TO INDUCE HEAT IN THE SUSPECTED AREA TO SIMULATE MGB OPERATING TEMPERATURE. MAGNESIUM EXPANDED ENOUGH FOR FPI TO DETECT THE CRACK. THE CRACK IS LOCATED IN THE RADII DIRECTLY UNDER THE LEFT INPUT CONNECTING FLANGE THAT PROTRUDES IN THE UPPER HOUSING APPROXIMATELY 3 INCHES LONG. PROBABLE CAUSE IS UNKNOWN AT THIS TIME. 2G72 4U4 U H4EA E15EA 20040217000222004021700022EU 2004 2 17 ASOA03688 120031211A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE LEFT AND RIGHT OUTBOARD SEAT TRACKS AND THE RIGHT INBOARD SEAT TRACK, BETWEEN FS 23-29 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SEAT TRACKS AND THE RIGHT INBOARD SEAT TRACK, BETWEEN FS 23-29 IAW SRM 51-25-01, 51-25-04 AND 53-00-00. (M) 2H72 4T RT 20040301000532004030100053SW 2004 3 1 QS72004F00001 120030212A6310212040687001 COUPLING BELL BELL 206 206B 1181511SW ALLSN 250C 250C* GL M/R DRIVESHAFT WORN B QS7RO OTHER O OTHER NRNOT REPORTED 1 NM09921RB 2624 RECEIVED FROM MFG AS NEW, COUPLING HAS ROUGH WEAR PATTERNS ON THE TEETH, SHOWS EVIDENCE OF BEING INSTALLED ON A SHAFT, AND HAS A WEAR PATTERN WHERE THE SEAL WOULD NORMALLY RIDE. BELL HAS RECENTLY IMPOSED A 3000 HOUR OVERHAUL OF THE DRIVESHAFT, PART RECEIVED WITHOUT HISTORICAL SERVICE RECORD. SN A5000. 1G71 3U3 U H2SW E4CE 20040324000042004032400004WP 2004 3 24 ASAA0380706 120031103A5320993053873 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CUSP WEB IS CORRODED ON LOWER SIDE AT FORWARD OUTBOARD AT FS 731-750. INSTALLED DOUBLER PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20040401000362004040100036WP 2004 4 1 ASAA0380407 120030421A532199365833 FLOORBOARD DOUG DC9 DC982 3022082WP FUSLEAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS TWO PUNCTURES. REPLACED FLOORBOARD PER SRM. (M) 2L72 4F A6WE 20040413000392004041300039NM 2004 4 13 ASAA024015A 120030319A530065C25230 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 727E RBL 8-12 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031215000132003121500013NM 2003 12 15 QXEA200301427 120031114A3060 CONTROL UNIT BOMBDRDHC8 DHC8401 1390041NM DE-ICE SYSTEM OUT OF TOLERANCEA QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 PDX- ON FLIGHT 2355 WHILE CLIMBING EN ROUTE AND OUTSIDE AIR TEMPERATURE AT -4 DEGREES CELCIUS, PROPELLER DE-ICE CAUTION LIGHT ILLUMINATED. RAN EMERGENCY CHECKLIST AND AFTER CYCLING THE SELECTOR SWITCH ONCE PER THE CHECKLIST THE LIGHT WENT OUT, BUT THE SYSTEM NEVER WORKED AGAIN. RECALIBRATED TMCU IAW TASK 30-61-06-820-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040916000112004091600011WP 2004 9 16 Y2PA03025 120031209A4900914F5674 RELAY DOUG DC9 DC932F 3022067WP APU FAILED A Y2PAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23208US 47220 CREW WORKING ELECTRICAL PROBLEM ON LT BUSS USING COM W/APU STARTED & RUNNING. APU LOW OIL PRESSURE LIGHT & OIL TEMP HIGH LIGHT ILLUM. APU SHUTDOWN. A/C OPS ON NR 2 GEN & BATTERIES. AN EMERGENCY DECLARED, A/C GIVEN DIRECT TO SDF & VECTORED FOR APPROACH. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AT SDF. NR 2 GENERATOR REMAINED OPERABLE DURING DESCENT AND LANDING. MANTENANCE DISPATCHED TO SDF FOUND THE APU OIL REQUIRED SERVICING. APU OIL WAS SERVICED AND THE SYSTEM THEN CHECKED GOOD IAW DC-9 MM 49-10-0. LT GENERATOR SYS THEN OPERATIONALLY CHECKED GOOD IAW THE DC-9 MM 24-20-6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A6WE 20060801001322006080100132WP 2006 8 1 IXXA060575S 120030909A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 4994 DURING ROUTINE C CHECK, FOUND SEAT TRACK "B" GOUGED AT STATION 244. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0. 2L74 4F RT4A25 20060801001442006080100144WP 2006 8 1 IXXA060587S 120030922A5712 RIB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE UPPER SURFACE RIB CRACKED AT STATION 454. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 51-1-8, 51-1-20D, AND 57-3-3. 2L74 4F RT4A25 20030905001122003090500112NM 2003 9 5 DL757030639 120030713A5210404002 RESERVOIR BOEING757 757232 1384965NM L-1 DOOR DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27643DL 23997 FOUND L1 DOOR ASSIST RESERVOIR LOW ON PRESSURE. SERVICED SAME. 2L72 4F RTA2NM 20030910001932003091000193CE 2003 9 10 2003F00551 120030716A553110164000017 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1969547 UE189 AT SCHEDULED EMPANNAGE ZONAL INSPECTION, VERTICAL STABILIZER TOP FORWARD RIB SHOWING CRACK ON RIGHT SIDE. STOPPED DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER REPAIR IAW 1900D STRUCTURAL REPAIR MANUAL, CHAPTER 51-70-05. (M) 2L72 4T RTA24CE 20030911000932003091100093WP 2003 9 11 DHL2003873500 120030613A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ 46091 RT WING CTR L/E UPPER PLATING CORRODED STA XFS.460.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12. REMOVED CORROSION FROM RT WING CTR L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. REMOVED CORRODED SKIN IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN IAW SRM 57-3-3 PG 12. CLEANED,TREATED AND PRIMED NEW SKIN INNER FACE IAW SRM 51-1-8B. INSTALLED NEW SKIN IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20030910001842003091000184SO 2003 9 10 SIMA200322506 120030810A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21819AE 145566 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. BLENDED THE DAMAGE AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR DOUBLER, FILLER, SHIMS AND REPAIR PLATE. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2681. (M) 2L72 4F RTT00011AT 20030912000552003091200055WP 2003 9 12 DHL2003604592 120030614A5751 PANEL DOUG DC8 DC873F 302199FWP LT AILERON DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBD AILERON UPPER PLATING SHOWS INTERIM REPAIRS BETWEEN STA XA 441.000 - XA 542.000. PERFORMED MAJOR REPAIR IAW EODHL-030570, ED-3398. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030570, ED-3398. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-030570, ED-3398. CLEANED, TREATED AND PRIMED THE NEW SKIN PANEL IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9 INSTALLED NEW SKIN PANEL ON LT WING INBD AILERON UPPER PLATING, STA XA 441.000 - XA 542.000 USING NEW FASTENERS IAW EODHL-030570, ED-3398 AND SRM 51-1-21 PG 1. SEE N\R 4049 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20030729001262003072900126EA 2003 7 29 SWIA200312199 120030718A5220H381933 HANDLE CNDAIRCL600 CL6002B19 1900309EA COCKPIT DEFECTIVE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07720SW 7297 COCKPIT EMERGENCY EXIT HATCH EXTENSION HANDLE WILL NOT STOW. REMOVED AND REPLACED FLIGHT DECK EMERGENCY HATCH EXTENSION HANDLE ASSEMBLY IAW CMM 52-22-03. 2L72 4F RTA21EA 20031003000292003100300029NM 2003 10 3 AALA20030528 120030502A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21699AN 27051 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21D INOPERATIVE. CONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007000302003100700030 2003 10 7 AALA20030809 420030715A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21668AA 25333 DURNG ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING NEEDS REPLACEMENT. REPLACED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031007001062003100700106NM 2003 10 7 SWAA032004 120030908A55516551524 FITTING BOEING737 7373H4 1384600NM TAIL CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR LT/RT AFT LUGS CORRODED. REPAIRED AFT LUGS PER SRM. 2L72 4F RTA16WE 20031021000842003102100084NM 2003 10 21 AALA20031009 120030915A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROWS 24 THROUGH 36. REPLACED BATTERY PACK AND REPAIRED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031021002712003102100271NM 2003 10 21 03FDEA01573 120030918A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION C53-224-01 AND GOUGED METAL AT FASTENER HOLE LOCATIONS ON FLOORBEAM AT BS 950F, LBL 42-RBL 38. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 20031022000382003102200038EA 2003 10 22 SWIA200312420 120030914A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERONS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07405SW8298 8298 7029 SPOILERON STATUS MSG WHEN RIGHT SPOILERON FULLY DEPLOYED. IF LEFT UP FOR SEVERAL SECONDS, INBOARD GROUND SPOILER FAULT FOLLOWS. ROLL DISCONNECT CREATES A SPOILERON CAUTION MSG WHEN RIGHT SPOILERON DEPLOYED.REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20030910000502003091000050SW 2003 9 10 HEEA088918 120030812A2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL SYSTEM INTERMITTENT E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW036559Z 36019 SIGNAL COND UNIT HAS INTERMITTENT LOW LEVEL LIGHT. 1G72 4U H4SW 20031029000202003102900020NM 2003 10 29 ASAA0340114 120030305A5320654769024 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR SUPPORT BS 773 RBL 13 WL 152. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031030000172003103000017NM 2003 10 30 UPS03441275 120030905A5712 RIB BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 21 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 21 V/C FLAP O/B LINKAGE IB RIB NR 7 ROTARY ACTUATOR MOUNTING AREA FOUND CORRODED ( COUNT FROM IB CLOCKWISE ). NR 7 BOLT AREA REPAIRED IAW RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F4 F A20WE E20EA 20031031000442003103100044WP 2003 10 31 UPS03841326 120030922A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP MAIN CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, SEAT TRACK CORRODED AT STA 305 LBL58. REMOVED SEAT TRACK BETWEEN STA 290-330, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3 FIG14 2L74 4F RT4A25 20031103000842003110300084GL 2003 11 3 ALG2003F00076 220030729A732323070100 GOVERNOR BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE FLUCTUATES E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW035756N 45546 CAE860301 AFTER TAKE OFF, ENGINE BEGAN SURGING, AIRCRAFT WAS YAWING LT AND RT, TORQUE WAS FLUCTUATING +/- 30 PERCENT. THROTTLE CONFIRMED OPEN, ENGINE BEEPED TO MAXIMUM N2 AND NR WOULD NOT GO ABOVE 94 PERCENT, UPON LANDING THE MECHANIC REMOVED AND REPLACED THE GOVERNOR AND STARTER GENERATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E1GL 20031022001082003102200108EU 2003 10 22 XNOA01154 120030918A2612 WARNING LIGHT AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE ILLUMINATED A XN0AEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23371PC 157 517443 DURING CLIMB AT FL 170 NR 1 ENG (B) LOOP LT ILLUM WITH LOOPS LT ON MWP. CHECKLIST CARRIED OUT AND ENG FIRE WARN REMAINED ON AFTER POSITIVE TEST OF LOOP (A). INFLIGHT ENG FIRE PROC CARRIED OUT AND A/C RETURNED TO HONG KONG. NOTE: FIRE WARNING CEASED WITH FUEL LEVER IN (OFF) POS. ENG FIRE AGENTS NOT DISCHARGED. INSPECTED ENG NO LEAKS FOUND. FOUND LT UPPER CORE (B) LOOP OPEN CIRCUIT. IAW A300 MEL 26-12-01 CAT B TRANSFERRED TO DMI NR 3526. FOUND BROKEN WIRE ON NR 1 ENG UPPER "B" LOOP FWD CONNECTOR. REPAIRED WIRE IAW A300 AWM & AMM 70-71-12. OPS CK GOOD. THIS ACTON CLEARS DMI 3561, PLACARDS REMOVED. 2L72 4F4 FRTA35EU E23EA 20031022001402003102200140EU 2003 10 22 AWXA200301082 120030913A5320D5347209400200 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND AT FASTENER HOLE ON MAIN CABIN FLOOR SUPPORT AT Y558 (LBL 22), JUST FORWARD OF FR 66. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOOR SUPPORT FROM FR 64 TO FR 70; INSTALLED NEW REPLACEMENT FLOOR SUPPORT IAW A320 SRM 51-42-11, PG. 25, FIG. 9. 2L72 4F4 FRTA28NM E311NE 20031110001142003111000114NM 2003 11 10 ABXA030405 120031027A2120 CLAMP BOEING767 767281 1385109NM A/C SYSTEM MISALIGNED A ABXAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL23795AX 23145 WITH EQUIPMENT COOLING SELECTED TO OVERRIDE, COULD NOT MAINTAIN CABIN PRESSURIZATION IN AUTO OR MANUAL. WHEN EQUIP COOLING SELECTED BACK TO AUTO ALL SYSTEMS CHECKED OK. THE CREW DESCENDED THE AIRCRAFT AND WENT ON OXYGEN FOR A SHORT PERIOD OF TIME. FOUND LEFT HAND AC EXT CONNECTION ELBOW CLAMP MISALIGNED. REALIGNED CLAMP. LEFT HAND PNEUMATIC SUPPLY CHECK VALVE ABOVE EXT CONNECTION HAD A BLOWN GASKET. REPLACED GASKET. CLAMP AND GASKET LEAK CHECKED GOOD. FORWARD EQUIPMENT CHECKED GOOD IAW 21-58-00-5. AUTO CABIN PRESSURIZATION CHECKED GOOD IAW B 767 MM FIM 21-30-00. 2L72 4F RTA1NM 20031120000412003112000041NM 2003 11 20 QXEA200301237 120030927A5320 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FRONT SPAR SHROUD BLEED PIPE LOWER SUPPORT BRACKET IS CRACKED ON RIGHT HAND SIDE OUTBOARD OF TEE PIPE ASSEMBLY. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20040129001142004012900114EA 2004 1 29 COMA0460002 120031229A2750860D10018ABC CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01959CA15359 7116 FLIGHT 5073 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20031103000362003110300036NM 2003 11 3 DL73G030894 120031001A2912000 FILTER BOEING737 737330 13844BJNM HYD SYSTEM CONTAMINATED A DALAA UNSCHED LANDING O OTHER LDLANDING 1 SO27241DL 23833 LOST SYSTEM-B PRESSURE ON LGA FINAL. DIVERT JFK, NORMAL LANDING. PER MM REPLACED RESERVOIR PRESS MODULE FILTER DUE WATER FOUND IN BOWL CAP AND HOUSING ON ENG. RUN-UP SYSTEM OPS CHECK OK. LEAK CHECK OK. 2L72 4F RTA16WE 20031103000602003110300060GL 2003 11 3 C2XA03CL171 220031001A720023070401 ENGINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XAB EMER. DESCENT YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 SW2713968108185054 145138 311035 STL FLIGHT NR 2368 THE CREW REPORTED THE NR 1 ENGINE UNCOMMANDED SHUT DOWN ON APPROACH INTO STL.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031106001682003110600168NM 2003 11 6 QXEA200301386 120031025A612078249028 PCU DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE MALFUNCTIONED A QXEAO OTHER O OTHER CRCRUISE 1 NM09369PH* 2536 513 SEA- NR 1 ENGINE AFTER SETTING TORQUE YAWED LEFT AND THEN ENGINE SOUND INCREASED DRASTICALLY. GLANCED AT GAUGES ON ABORT, POWER REDUCTION, ENGINES RETURNED TO NORMAL. NO WARNING LIGHTS. REMOVED AND REPLACED PCU AND TSCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031107001522003110700152WP 2003 11 7 GTIA030742 120030921A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND CABIN FLOORBOARD STATION 1174-1250 CENTER HAS EDGE DELAMINATION AND MISSING INSERT. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20031110001272003111000127NM 2003 11 10 AWXA200301346 120030930A575465C266852 WEDGE BOEING737 7373G7 1384595NM L/E SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK THE NR 4 SLAT WEDGE WAS FOUND DISBONDED AT THE LOWER INBOARD END. MAINTENANCE CUT OUT DAMAGE ON NR 4 SLAT WEDGE; FABRICATED A REPAIR DOUBLER; BONDED REPAIR DOUBLER TO SLAT IAW B737-300 SRM 51-70-10, REPAIR 7, FIG 16, PG 67-69. 2L72 4F RTA16WE 20031112000032003111200003NE 2003 11 12 2003UALA00812 220031027A7261 STUD BOEING757 757222 1384956NM PWA 2037 PW2037 NE SCAV PUMP FAILED A UALAED ENGINE SHUTDOWN RETURN TO BLOCK KMJFLUID LOSS OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 WP29549UA 25397 RIGHT ENGINE SHUT DOWN DURING TAXI DUE TO HIGH ENGINE OIL TEMP. FUEL OIL HEAT EXCHANGER AND VALVE WERE REPLACED AND PROBLEM SEEMED FIXED. NO DISCREPANCIES FOR NEARLY FOUR WEEKS. THEN LOW OIL QUANTITY AND INCREASING OIL TEMPERATURE HIT AGAIN. NR 5 BEARING PRESSURE AND SCAVENGE TUBES REPLACED WITH NO EFFECT. ROOT CAUSE FINALLY FOUND AS THE RETAINING STUDS ON THE GEARBOX SCAVENGE PUMP FAILED AND ONE HELICOIL STRIPPED. COA WRITTEN TO INCORPORATE FIX. COA ACCOMPLISHED ON THIS ENGINE AND NO FURTHER DISCREPANCIES FOUND. 2L72 4F4 FRTA2NM E17NE 20031124000032003112400003NM 2003 11 24 QXEA200301455 120031104A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 NR 5 SEAT TRACK HAS CORROSION ON THE INBOARD FACE OF THE RIGHT HAND LUG 2 INCHES AFT OF X467. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36, RD 8-53-7636 AND HORIZON AIR EA 2-53-507. 2H72 4T RTA13NM 20031124000272003112400027NM 2003 11 24 03FDEA01937 120031113A5710 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE OUTBOARD FLANGE SIDE CORRODED (WING SIDE). LT O/B FLAP, INBD HINGE FITTING LOWER BOLT HOLE O/B FLANGE SIDE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DWG ARC0502. 2L73 4F RTA22WE 20040108001412004010800141EU 2004 1 8 KBM2003F00075 120031021A5210350A25134620 PAD SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DOOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 RT SLIDING DOOR FRICTION PAD SLIDER WORN EXCESSIVELY. REMOVED AND REPLACED WITH NEW. (K) 1G71 3U3 U H9EU E19EU 20040113001112004011300111 2004 1 13 BAQA091168 420031110A225043800100010 FIBER OPTIC GYRO UROCOPEC135 EC135P1 8680990EU SAS SYSTEM INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME2924 0009 FIBER OPTIC GYRO PRODUCING YAW INTERMITTENT INTERRUPTIONS. KEEPS GOING OFFLINE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U O H88EU 20040113000132004011300013EU 2004 1 13 BAQA090674 120031203A6420 BEARING BOLKMS117 BK117B1 5626012EU FORK LINK WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME W7846 7235 FORK LINK BEARING HAS PLAY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20040113001562004011300156NM 2004 1 13 MWEA030497 120031224A32407972148583 LINE BOEING717 717200 1383700NM LT BRAKE DEFECTIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31907ME 55171 HYDRAULIC LOW QUANTITY LOW ANNUNCIATOR ILLUMINATED. TROUBLESHOOT TO LEFT SYSTEM BRAKE PRESSURE RETURN LINE AT OUTBOARD ANTI-SKID VALVE IN RIGHT WHEEL WELL BRAKE SHELF. INSTALLED FLEX LINE, LEAK CHECKED GOOD. 2L72 4F TRA6WE 20031217001482003121700148SO 2003 12 17 LR7A03086 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE CANNING A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND AFT FUSELAGE SKIN WARPED AND OIL CANNED FS 737E-777E, LBL 60, WL 147-200. REPLACED LT AFT FUSELAGE SKIN FS 737E-777E IAW SRM SMP 583 51-60 & 51-70. NR 2021. 2H74 4T A1SO 20031219001872003121900187NM 2003 12 19 CALA0300706 120031208A5730 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733132 29281 INSPECTION FOUND A 4.5 INCH CRACK IN RIGHT WING FIXED LEADING EDGE SKIN BETWEEN OSS 397 AND OSS 421. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, OP 4 AND SRM 57-41-01. 2L72 4F RTA2NM 20031223001262003122300126EU 2003 12 23 MALA030539 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 15A, 15B FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 15A, 15B IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20040105000882004010500088NM 2004 1 5 QXEA200301568 120031218A1430 RIVET DHAV DHC8 DHC8202 2809007NM LT NACELLE LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX - SMOKING RIVETS OUTBOARD LEFT HAND NACELLE JUST FORWARD OF PANEL 419CT AND INBOARD OF OUTBOARD FLAP. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20031231000632003123100063EA 2003 12 31 A6WA200340179 120031118A5753 VANE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 RIGHT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE HAS THREE MINOR CHAFES AT WS 56.177, WAS 104.429 AND WS 140.364. ALL THREE CHAFES ARE LESS THAN .001 INCHE DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE AT WS 56.177, WS 104.429 AND WS 140.364 BY BLENDING DAMAGED AREAS, RESTORING FINISH AND APPLYING TEFLON FILLED ABRASION RESISTANT COATING IAW BOMBARDIER, INC REO 601R. (M) 2L72 4F RTA21EA 20040106001572004010600157EA 2004 1 6 03353647 120031219A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27647BR 7399 DURING INSPECTION THE FORWARD EXTERNAL PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040106002092004010600209WP 2004 1 6 GTIA030986 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND FLOOR PANEL STATION 1174-1287 DETERIORATING, BROKEN INSERTS EDGE SEAL BROKEN OUT. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040120000242004012000024NM 2004 1 20 03FDEA02302 120031226A5350AKC75915 BEAM DOUG MD11 MD11 3023602NM ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 TAIL CONE AFT SNUBBER LT AND RT LOWER STIFFENER FOUND CHAFED. REMOVED AND REPLACED TAILCONE AFT SNUBBER LT & RT LOWER STIFFENER AS PER SRM 51-35-01 VOL. II. STIFFENER FABRICATED AS PER DWG AKC7591. 2L73 4F RTA22WE 20031124000152003112400015NM 2003 11 24 QXEA200301437 120031114A2810 O-RING DHAV DHC8 DHC8202 2809007NM ZONE 100 LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09348PH 484 PDX- ON FLIGHT 2048 FUEL DRIP FROM SPR DOOR. RESEATED ADAPTER HOUSING O-RING UNDER FUEL CAP. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031126000652003112600065EA 2003 11 26 QXEA200301473 120031122A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT ACTIVATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09606QX 10023 ON FLIGHT 2490 FIRE SYSTEM FAULT STATUS MESSAGE. COMPLIED WITH FIM TASK 26-10-00-810-805-A01. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031202001292003120200129EU 2003 12 2 A6WA200360058 120031018A2597 WIRE BAG BAE146BAE146200A 1500266EU SLIDE BATTERY LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 DURING SLIDE DEPLOYMENT FOR FUNCTION TEST LIGHTS CAME ON AND THEN OFF AFTER FULL DEPLOYMENT, INSPECTION FOUND WIRES PULLED OUT OF BATTERY CONNECTORS. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE AND DISCREPANCY FORWARDED TO SLIDE SHOP. (M) 2H74 4F RTA49EU 20040123000792004012300079CE 2004 1 23 FPI2003F00011 120031107A7921654585 OIL COOLER CESSNA210 T210N 2073456CE CONT O550 IO550* SO ENGINE CRACKED D FPIAO OTHER O OTHER NRNOT REPORTED 1 SO154702C1630 21063591 821016R OIL COOLER CRACKED AT UPPER FOREMOUNTING FLANGE. 1H71 3O3 O 3A21 E3SO 20060801000872006080100087WP 2006 8 1 IXXA060544S 120030906A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND L-1 DOOR CUTOUT UPPER AFT CORNER CRACKED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS. IAW DC8 SRM 51-1-21, 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20030819001602003081900160NM 2003 8 19 2003UALA00598 120030722A5754 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 9 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29770UA 26925 T/E WEDGE DELAMINATED, SLAT NR 9. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED AND REPLACED T/E SLAT. 2L72 4F4 FRTT0001SE E46NE 20030401001322003040100132WP 2003 4 1 DHL2003804524 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART HAS 1 IN CRACK AT STA XFS 778.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030403000842003040300084NM 2003 4 3 CALA0300157 120030331A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND AFT CARGO COMPARTMENT LOWER LOBE INTERIOR FRAME CORRODED AT BS 847 BETWEEN S28L AND S28R. REPAIRED IAW SRM 53-00-07, FIGURE 208. 2L72 4F RTA16WE 20030407000742003040700074SO 2003 4 7 SIMA200302002 120030116A5610163500112 WINDSHIELD EMB 135 EMB135KL 3260302SO COCKPIT FAILED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21818AE 145561 ORD - FLT 4371 - DURING FLIGHT CREW REPORTED THE FIRST OFFICERS WINDSHIELD BUBBLING AND ARCING WITH ANTI-ICING TURNED ON. CREW LEFT ICING CONDITONS AND CONTINUED TO ORIGINAL DESTINATIONS WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030410000542003041000054WP 2003 4 10 GTIA030093 120030212A5320 DOUBLER DOUG DC9 DC981 3022081WP LAVATORY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND AFT CABIN LAVATORY AREA LEFT FLOOR ANGLE DOUBLER CORRODED. FABRICATED A NEW ANGLE DOUBLER. (M) 2L72 4F A6WE 20030414000802003041400080NM 2003 4 14 AUS20030280 120030212A5330 SKIN BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 3 CARGO DOOR CUTOUT AFT LOWER CORNER CONTAINED LEVEL 2CORROSION IN THE AREA LOCATED BETWEEN SKIN LAMINATIONS AT STA 1140 TO 1148 AND BETWEEN STRINGER 26 RT AND STRINGER 27 RT. FOUND DURING CPCP INSPECTION IAW C53-111-01. 2L73 4F4 FRTA3WE E2EA 20030416002212003041600221 2003 4 16 MWEA030162 420030407A34426225135003 PEDESTAL DOUG DC9 DC932 3022066WP RADAR ANTENNA DEFECTIVE A MWEAA UNSCHED LANDING O OTHER CRCRUISE 1 GL31215ME 47744 RADAR WEATHER UNREADALBE IN CRUISE. REMOVED AND REPLACED ANTENNA PEDESTAL. 2L72 4F A6WE 20030417000622003041700062CE 2003 4 17 DXTA200300002 120030128A3240651710212 HYDROMECH UNIT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE BRAKE ASSY LEAKING E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07345QS4713 5600445 POWER BRAKE LITE AND ANTI SKID INOP LITE ON IN FLIGHT. 2L72 4F4 FRTA22CE E25EA 20030422000512003042200051EA 2003 4 22 ASOA03105 120030313A5346 SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING A C-CHECK INSPECTION IN MCN, THE LEFT AND RIGHT ENGINE SUPPORT BEAMS AT BL 36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CRACKED LEFT AND RIGHT ENGINE SUPPORT BEAMS AT BL 36.20 IAW ASA EO 600-53-0073. (M) 2L72 4F RTA21EA 20030423001522003042300152WP 2003 4 23 ZW0A0303012 120030306A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13967TW 53617 THE FUSELAGE SKIN WAS DAMAGED AT STA 154 TO 160. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL. 2L72 4F RTA6WE 20030424000332003042400033WP 2003 4 24 ZW0A0303211 120030313A5280 CHANNEL DOUG DC9 DC983 3022083WP MLG DOOR CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13110HM 49787 DURING CHECK-C, THE RIGHT WHEEL WELL FWD MAIN GEAR DOOR FRAME CHANNEL WAS CRACKED. REPLACED SECTION OF FRAME CHANNEL PER SRM 51-10-04, 51-20-0, 51-30-2, AND 51-3-05. 2L72 4F RTA6WE 20030430001162003043000116 2003 4 30 03FDEA00607 420030423A3197 WIRE HARNESS AIRBUS310 A310 EU RIGHT ECAM DAMAGED A FDEAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO25429FE 364 ON LANDING STBY PROBE HEAT, PILOTS RIGHT ECAM DISPLAY, PITCH TRIM NR 2, YAW DAMP NR 2, & ATS NR 2 ALL FAILED AT ONCE. ALSO IRU'S WENT TO INDEPENDENT OPS. ENG NR 2 N2 CB POPPED. FACT 25APR03 19:09 RNO U C/W E.A. 6-2400-70271 THE R/H ECAM WIRE WAS CAPPED AND TAPPED AND WILL BE DEFERRED UNDER A SEPARATE WRI. ON INSPECTION OF WIRE BUNDLE, THE DAMAGED AREA WAS NOT IN CONTACT WITH ANY STUCTURE/CHAFFING POINT BUT WAS NEAR TWO VERY TIGHT TYWRAPS. ALSO LOCATED IN A BEND OF THE WIRE BUNDLE. THE DAMAGED WIRES WERE ON THE OUTSIDE OF THE WIRE BUNDLE AND TURN RADIUS. 2L72 4F RTA35EU 20030501000082003050100008WP 2003 5 1 AALA20030269 120030220A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 TUL - FOUND AFT LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB CRACKED STATION 1004. INSTALLED DOUBLER ON LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB PER SRM 53-05 FIG 32. (M) 2L72 4F RTA6WE 20030502000382003050200038WP 2003 5 2 ASAA0380145 120030222A5320593641311N SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, RIGHT MLG DOOR WHEEL BUMPER SUPPORT CRACKED. REPLACED BUMPER SUPPORT PER MD-80 SB 32-197. (M) 2L72 4F A6WE 20030502000822003050200082NM 2003 5 2 AWXA200300369 120030414A33501012623 LIGHT BOEING737 737277 1384570NM SEAT ROW 9 BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28180AW 22647 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 9 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030501001292003050100129NM 2003 5 1 ASAA0310026 120030222A5720655081449 ANGLE BOEING737 737210C 1384459NM LT WING TE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND LEFT WING TRAILING EDGE SIDE SUPPORT ANGLE AT WING STATION 337L, WATERLINE 180 CHAFED. REMOVED AND REPLACED SUPPORT PER SRM. (M) 2L72 4F A16WE 20030505001742003050500174NM 2003 5 5 SWAA030846 120030411A53106545785 WINDOW FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW FRAMES CRACKED AT RT WINDOWS NR 12 & 30. REMOVED AND REPLACED WINDOW FRAMES PER SRM. 2L72 4F RTA16WE 20030506001162003050600116NM 2003 5 6 03FDEA00470 120030417A5752 STRUCTURE BOEING727 727200 138407ENM AILERON TAB DEBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT OUTBOARD AILERON TAB I/B AFT CORNER DISBONDED. 2L73 4F RTA3WE 20030507000142003050700014EU 2003 5 7 CA030407010 120030321A5311350A23103600 FRAME AEROSPAS355 AS355F2 8680812EU ALLSN 25OC 250C20R GL TAIL BULKHEAD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5460 (CAN) DURING A 6000 HR. 2T AIRFRAME INSPECTION, TAILBOOM TAILCONE AREA WAS INSPECTED AS AN REQUIREMENT OF EUROCOPTER S/B 55.00.09 'CHECK OF FIN ATTACHMENT FRAME. A CRACK WAS FOUND EMANATING FROM AN ANCHOR NUT ATTACHMENT RIVET IN TWO DIRECTIONS. THIS CRACK HAD PROGESSED APPROXIMATELY 1.5' UNDER THE FIN ATTACHMENT. FRAME WAS REPLACED WITH NEW AND S/B 55.00.09 COMPLIED WITH. 1G72 3U3 U H11EU E4CE 20030506001792003050600179WP 2003 5 6 ASAA0380225 120030307A575359304942 VANE DOUG DC9 DC982 3022082WP RT TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP VANE DENTED ON OUTBOARD END LOWER SURFACE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM. (M) 2L72 4F A6WE 20030508001542003050800154NM 2003 5 8 QXEA0300516 120030418A5510 RIB BOMBDRDHC8 DHC8401 1390041NM ZONE 300 BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 RT HORIZONTAL STAB TIP FOR LEADING EDGE HAS A BENT RIB INSIDE TIP FAIRING. REPAIRED IAW HORIZON AIR EA 6-55-29. 2H72 4T RTA13NM 20030509000842003050900084NM 2003 5 9 HOC2003F00000 120030420A532065255899 FLOOR SUPPORT BOEING727 727231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK FLOOR SUPPORT AT STA 848 BL 0, WAS FOUND CRACKED. 2L73 4F4 F A3WE E2EA 20030513002412003051300241EA 2003 5 13 ASOA03157 120030412A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN CONTAMINATED A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SO11862AS 7476 FLT 4318 - DURING FINAL APPROACH INTO ATL FROM CAK, THE CREW RECEIVED A SMOKE TOILET CAUTION MESSAGE AFTER STARTING THE AUXILIARY POWER UNIT, ACCOMPANIED BY A FUEL SMELL AND SMOKE IN THE CABIN NEAR THE LAVATORY AREA. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT AND LEFT COALESCER BAGS ON THE WATER SEPARATOR ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030509001662003050900166NM 2003 5 9 USAASB03051 120030406A335020121 POWER SUPPLY BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19531AU 24478 MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030609000372003060900037NM 2003 6 9 03FDEA00786 120030513A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE CORRODED. 2L73 4F RTA22WE 20030609001912003060900191NM 2003 6 9 CA030520002 120030516A291082950010369 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM LEAKING W O OTHER K FLUID LOSS CLCLIMB 1 CA (CAN) ON CLIMB OUT NR 2 HYDRAULIC SYSTEM FAILED. CREW PERFORMED ALTERNATE GEAR EXTENTION AND LANDED AT DESTINATION WITH OUT FURTHER INCIDENT. MAINTENANCE FOUND LT WING FLIGHT SPOILER UNLOADING HYDRAULIC LINE TO HAVE A PIN HOLE AT THE SECOND ELBOW FROM THE OUTBOARD SIDE OF THE LINE. LINE WAS REPLACED. IPC REF 19-00-00 FIG 25 ITEM 140. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030610000322003061000032NM 2003 6 10 03144408 120030524A2120 SMOKE DORNERDO32 DO328300 NM CABIN DETECTED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27408FJ 3160 DURING CRUISE, THE CREW REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO ORF. INITIAL INSPECTIONBY CONTRACT MX LED TO SUSPECT CABIN LIGHTS. THE CABIN LIGHTS WERE RENDERED INOP. IAW MEL 33-20. LATER INSPECTION AND TROUBLESHOOTING AT BOS FOUND NO SIGNS OF BURNING, MELTING OR ARCING, AND ALL LIGHTING CIRCUIT BREAKERS REMAINED SET. ALL OPERATIONAL CHECKS WERE SATISFACTORY FOR 90 MINUTES. THE CABIN A/C PACKS WERE RUN WITH NO ODOR OR SIGN OF SMOKE. UNABLE TO DUPLICATE ANY MALFUNCTION. 2H72 4T RTA55NM 20030611001402003061100140EA 2003 6 11 2003F00363 120030122A7830TY214810A CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER FAILED A FDKAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07506MJ 10073 ASH - FLT 6743 - PHX-TUS, AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT THRUST REVERSER UNSAFE MESSAGE. MAINTENANCE REPLACED THE RIGHT ISOLATION CONTROL VALVE. (M) 2L72 4F RTA21EA 20030617003312003061700331SW 2003 6 17 HEEA087042 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20030523000652003052300065NM 2003 5 23 QXEA0300530 120030501A3230483004 VALVE BOMBDRDHC8 DHC8401 1390041NM ZONE 700 MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09402QX4337 4337 4032 PDX- ON FLIGHT 2358 AIRCRAFT RETURNED TO FIELD WHEN ON TAKEOFF GEAR DIDN'T RETRACT. RECEIVED 3 GREEN, 3 RED, GEAR HANDLE LIGHT AND LANDING GEAR INOPERATIVE CAUTION LIGHT. DID ALTERNATE GEAR EXTENSION TO NORMAL LANDING. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030619000412003061900041SW 2003 6 19 HEEA087386 120030611A3212407073848101 BOTTLE BELL 407 407 1182206SW FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 FLOAT BOTTLE LEAKING AT FUSIBLE PLUG. TO BE SENT TO BELL HELICOPTER TEXTRON. 1G71 3U O H2SW 20030618001822003061800182SW 2003 6 18 HEEA087149 120030609A6710206001053005 BEARING BELL 206 206L3 1182108SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 BELLCRANK ASSY HAS WORN BEARINGS. REPLACED BEARING (4 EACH) 206001053005 DUE TO WORN. REPAIRED. 1G71 3U H2SW 20030630000052003063000005NE 2003 6 30 MALA030220 220030401A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 4 SHUTDOWN A MALAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION LDLANDING 1 GL15448XJ 340B448 ON LANDING APPROACH ON FLIGHT 3401, NR 4 ENGINE SHUTDOWN. NO INFORMATION AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20030711001092003071100109EA 2003 7 11 COMA0360298 120030626A2750860D10018ABCD COMPUTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SO01986CA 7174 FLIGHT 5422 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20030630000212003063000021NM 2003 6 30 ANCF200300015 120030527A21506411371 SWITCH BOEING767 767383 1385214NM PACK OVERHEAT MALFUNCTIONED W ANCFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23984AN 24357 LT PACK INOPERATIVE, LIGHT ILLUM. EICAS MSG L PACK TEMP DISPLAYED. LIGHT DID NOT EXTIN WHEN STBY SELECTED AND RESET PUSHED. AIRCRAFT RETURNED. LT PACK TEMPERATURE CONTROL (PTC) BITE PROCEDURE WAS PERFORMED IAW FIM 21-51-00 FIG 103, COMPRESSOR OUTLET OVERHEAT SWITCH WAS REPLACED IAW AMM 21-51-19 AND LH PACK FLOW CARGO AIR CONDITIONING CONTROLLER (PFCAC) WAS RESET (M1610). TESTS WERE PERFORMED WITH SATISFACTORY RESULTS. 2L72 4F RTA1NM 20030709000842003070900084NM 2003 7 9 03156415 120030605A3350 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27415FJ 3170 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CENTER EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED A LOOSE CONNECTOR FOR THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030710000792003071000079EU 2003 7 10 DHL2003366500 120030530A5320A53612000381 FLOOR SUPPORT AIRBUS300 A300B4203 3930306EU FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 FLOOR PANEL SUPPORT BETWEEN FRAME 7R AND FRAME 10R IS CRACKED. REMOVED FLOOR PANEL SUPPORT IAW A300 SRM 51-30-30. PERFORMED MATERIAL ID IAW A300 ASTM 1476-97. FABBED NEW PART IAW A300 BLUE PRINT 53612000. ALODINED AND PRIMED AND PAINTED IAW A300 SRM 51-40-12. INSTALLED PART IAW A300 SRM 51-30-30. 2L72 4F RTA35EU 20030714001002003071400100EA 2003 7 14 03182667 120030701A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CONTAMINATED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27667BR 7535 DURING MAINTENANCE INSPECTION, THE FORWARD SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL CLEANED MOISTURE FROM THE FLOOR LIGHT SECTION CONNECTOR. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030717000312003071700031SW 2003 7 17 HEEA088008 120030622A5620407030607115 WINDOW BELL 407 407 1182206SW LITTER DOOR CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 LITTER DOOR WINDOW IS CRAZED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030114001342003011400134NM 2003 1 14 SWAA030039 120030107A53126545409631 PRESSURE PANEL BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663, RBL 39.5. REPAIRED WEB PER SWA EA. 2L72 4F A16WE 20030114001412003011400141NM 2003 1 14 SWAA030043 120030107A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED BC1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP NEAR FWD GALLEY. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030129000462003012900046SW 2003 1 29 HEEA083959 120030117A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH1410 53283 MAIN ROTOR BLADE CRACKED AND SEPARATED NEAR THE OUTBOARD TRIM TAB. 1G71 3U O H2SW 20030211000092003021100009EA 2003 2 11 03041623 120030210A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER TOTAKEOFF 1 EA27623BR 7192 After Take-off, crew received a nose door warnng and gear disagree warning message.Maintenance personnel removed and replace Prox sensor target bracket. Ops ckecked good, aircraft returned to service. 2L72 4F RTA21EA 20030212000422003021200042WP 2003 2 12 ARWA20030106 120030128A7932AS3209237 PACKING DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE OIL SYS LEAKING A ARWAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19784AL62296416 46135 671111 INFLIGHT OIL QUANTITY GRADUALLY DROPPED TO ZERO, SUBSEQUENTLY OIL PRESSURE FLUCTUATED BETWEEN 45 36 PSI. OIL PRESSURE LIGHT ON, PERFORMED IN FLIGHT NR 3 ENGINE SHUTDOWN AS PER ABNORMAL WIND MILL OIL PRESSURE 10 PSI. DECLARED EMERGENCY. PERFORMED FUEL DUMP PROCCEDURE IN ORDER TO LAND AT MPTO WITHOUT INCIDENTS. REPLACING O-RING TO OIL FILTER STRAINED ELEMENT AND INSPECTED STRAINER FOR CONTAMINENTS. NONE NOTED. PERFORMED LEAK AND OPERATIONAL CHECKED IAW PW MM 72-00. ENGINE OPERATIONAL NORMAL. NO LEAKS NOTED. 2L74 4F4 F 4A25 1E8 20030212000972003021200097NM 2003 2 12 AWXA200300122 120030206A531369353521 TIE CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW0 0 23733 MCN - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 3 R/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 3 R/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 38, FIG. 8, AND SRM 51-40-05, PG. 1-4, FIG. 1-2, PG. 7, FIG. 4. 2L72 4F RTA16WE 20030219000842003021900084NM 2003 2 19 SWAA030298 120030207A335020121 CHARGER BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER AND CHARGED BATTERY PER MM. 2L72 4F RTA16WE 20030116002832003011600283SW 2003 1 16 HEEA083143 120030108A6220206011139001 ARM BELL 206 206L3 1182108SW M/R HEAD DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 MAIN ROTOR HEAD RUBBER EXPANDED ON ARMS. 1G71 3U H2SW 20030117001162003011700116SW 2003 1 17 HEEA083197 120030108A6510 BRACKET BELL 206 206L3 1182108SW T/R DRIVESHAFT MISMANUFACTURED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW036610Y PHI240 51419 RT BRACKET IS APPROXIMATELY 1/2 INCH SHORT, CAUSING IMPELLER NOT TO BE CENTERED. REPAIRED. 1G71 3U H2SW 20030223000012003022300001SO 2003 2 23 C2XA03SH011 120030222A530014522226003 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030224000322003022400032NE 2003 2 24 HEEA084152 120030211A67207610305003042 BEARING SKRSKYS76 S76A 8143006NE T/R PITCH LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 TAIL ROTOR PITCH LINK HAS WORN BEARINGS. REPLACED 8 EACH SB5081-102 BEARINGS DUE TO WORN; 8 EACH 76106-07017-103 RETAINER BEARINGS DUE TO WORN AND 4 EACH PHIS76-225 DECAL DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030225000682003022500068GL 2003 2 25 HEEA084290 220030211A7532 HOUSING BELL 206 206L3 1182108SW ALLSN 250C 250C* GL BLEED VALVE LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q FF34230 51540 BLEED VALVE HOUSING IS LOOSE. REPAIRED. 1G71 3U3 U H2SW E4CE 20030226000422003022600042SW 2003 2 26 HEEA084331 120030211A7722407375001105 INDICATOR BELL 407 407 1182206SW MGT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 MGT INDICATOR WILL ONLY READ 75 DEGREES IN FLIGHT. 1G71 3U O H2SW 20030227001052003022700105 2003 2 27 HEEA084411 420030212A3454071121627 CONTROL UNIT BELL 214 214ST 1182106SW VOR SYS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M 28102 WILL NOT CHANGE FREQUENCY. FOUND CORROSION ON SWITCH S104 AND INSERT FACEPLATE, LOCK RING AND PHOTOCELL V101 BAD. UNIT NEEDS KNOB KIT. CLEANED CORROSION AND REPLACED FACEPLATE, LOCK RING AND PHOTOCELL. REPAIRED. BENCH CHECK GOOD. 2G72 4U H10SW 20030228000172003022800017NM 2003 2 28 SWAA030397 120030219A335007912 COVER BOEING737 7373H4 1384600NM FWD CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 EEPLS COVERS LOOSE AT ROWS NR 4, NR 5 AND NR 6. SECURED COVERS PER MM. 2L72 4F RTA16WE 20030303001312003030300131SW 2003 3 3 HEEA084555 120030214A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032260813842 33075 MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS A CRACK NEAR THE SPLICE AREA. 1G72 4U H4SW 20030304000062003030400006SW 2003 3 4 AC2A084862 120030224A282023062792 TUBE BELL 430 430 1182150SW FUEL SYSTEM CHAFED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT1142 49089 FUEL TUBE HAS A GROOVE ON THE EXTERNAL SIDE OF THE FLARE. REPLACED WITH NEW TUBE ASSEMBLY. 1G72 3U RTH9SW 20030306000632003030600063WP 2003 3 6 MWEA03127 120030305A532199365507 FLOOR PANEL DOUG DC9 DC981 3022081WP STA 220 - 229 CUT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 LARGE CABIN CENTER FLOOR PANEL LOCATED FROM FRAME STATION 200 TO 229 BETWEEN #2 AND #3 SEAT TRACK HAS A CUT IN TOP SURFACE AT FORWARD END. -- REPAIRED PANEL. 2L72 4F A6WE 20030310000362003031000036NM 2003 3 10 DHL2003748004 120030308A33501000679 LIGHT BOEING727 727225 1384077NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01748DH 22440 1) FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE.2) REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECKED NORMAL IAW M/M 33-50-01. 2L73 4F A3WE 20030310001022003031000102 2003 3 10 HEEA085007 420030227A2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 LIFE VEST LEAKS. 1G72 4U H4SW 20030311000122003031100012SW 2003 3 11 HEEA085033 120030228A6510206040339009 BEARING BELL 206 206L3 1182108SW T/R DRIVE SHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038590X BT1569 51494 NICKS AND VARNISH CHIPPING. REPLACED BEARING 206040339009, S/N ZV66256 DUE TO ROUGH; SHAFT 206040365125, S/N BT212 DUE TO BELOW MIN ON FLANGE. REPAIRED. 1G71 3U H2SW 20030311000392003031100039 2003 3 11 HEEA085055 420030228A2300CIX100LVHGK374 HOUSING BELL 206 206L3 1182108SW HEADSET JACK DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 HEADSET JACK PULLED OUT OF HOUSING. REPLACED CORD. 1G71 3U H2SW 20030122000152003012200015SW 2003 1 22 HEEA083402 120030109A2432RG222 BATTERY BELL 206 206L1 1182107SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0383MT 485 45492 MAIN BATTERY VOLTAGE DROPPED. 1G71 3U H2SW 20030314001772003031400177CE 2003 3 14 WVE2003F00004 120030117A3260 SWITCH LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP MLG INDICATOR FAILED B WVERO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 EA09428FX 164 WHEN LANDING GEAR WAS EXTENDED, FLIGHT CREW REPORTED NO GREEN LIGHT (DOWN AND LOCKED INDICATION) ON LEFT MAIN LANDING GEAR. INFLIGHT EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO PROBLEMS. AFTER LANDING MAINTENANCE VERIFIED GEAR WAS DOWN AND LOCKED. DEFECTIVE INTERNAL MICROSWITCH IN RETRACTION ACTUATOR. 2L72 4F4 FRTT00008WIE6WE 20030317000812003031700081NM 2003 3 17 03FDEA00242 120030303A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 36L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030319000702003031900070 2003 3 19 MEX2003001 420030103A22104034241974 COMPUTER DOUG MD80 MD83 3023681NM NR 1 ENGINE FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23861LF 49826 ATL-MEX - FLT 601 - AIRCRAFT RETURNED TO GATE DUR TO DFGC NR 1 FAILURE, AFTER ENGINES STARTED, DFGS NR 1 WAS NOT WORKING PROPERLY. COMPUTER NR 1 WAS REPLACED IAW MM 22-01-01, AND SWITCHES WERE RE-ESTABLISHED, TESTS OK. (M) 2L72 4F RT 20030319000752003031900075WP 2003 3 19 MEX2003023 120030202A323139567851 LINK DOUG DC9 DC987 3022087WP MLG DOOR FAILED A ASMFC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SW23755RA 49727 FLT 929 - MTY-MEX - AIRCRAFT RETURNED TO GATE, AFTER RETRACTING LANDING GEAR, HAD STRONG VIBRATION. AIRCRAFT RETURNED WITH RIGHT NOSE LANDING GEAR DOOR OPEN. FOUND FORWARD DOOR LINK LEVER BYPASS DID NOT WORK, DOOR LINK WAS REPLACED IAW MM 32-22-01, ALL CORRECT. 2L72 4F RTA6WE 20030319001182003031900118NM 2003 3 19 USAA030015 120030205A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19342US45328 23511 CLT - FOUND SKIN CRACKED 2.5 INCH, LEFT AFT FUSELAGE BS 727E STRINGER 23. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20030123000092003012300009NM 2003 1 23 2003UALA00008 120030103A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 767, STRINGER 9R, FUSELAGE FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030325000252003032500025NM 2003 3 25 AWXA200300140 120030129A53106546956506 BEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MAJOR REPAIR - DURING C-14 CHECK A 2 INCH CRACK AND CORROSION WAS FOUND ON SHEAR BEAM WEB BS 480 TO BS 500. MAINTENANCE REMOVED DAMAGED SHEAR BEAM WEB BS 480 TO BS 500; FABRICATED A NEW REPLACEMENT WEB IAW DWG 65-46956; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030324000512003032400051WP 2003 3 24 ABXA030108 120030310A3230 PUSHROD DOUG DC9 DC931 3022065WP MLG DISCONNECTED A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23947AX 47004 AFTER TAKE-OFF, UNABLE TO RAISE GEAR HANDLE. RAN CHECK LIST AND DETERMINED THAT AIRCRAFT FAILED TO GO INTO FLIGHT MODE (GROUND SHIFT IN GROUND MODE) - PULLED CIRCUIT BREAKERS AND DETERMINED THAT THE GROUND SHIFT WAS BAD. FOUND GROUND SHIFT MECHANISM PUSHROD DISCONNECTED. ATTACHED PUSHROD SHIFT MECHANISM IAW DC-9 MM 32-52-07-2-001. 2L72 4F A6WE 20030325000612003032500061NM 2003 3 25 AWXA200300224 120030301A3350900835A BATTERY PACK BOEING737 737277 1384570NM FUSELAGE DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 DURING INSPECTION THE AFT LT ENTRY DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE AFT GALLEY EMERGENCY LIGHTS, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030325000982003032500098EU 2003 3 25 AWXA200300260 120030301A5315D5347210420290 SPLICE AIRBUS320 A320231 3930325EU FLOORBEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON THE BOTTOM SURFACE OF THE UPPER LEG ON FLOORBEAM SPLICE, FR 66+7, Y765. MAINTENANCE REMOVED CORRODED SPLICE AT FR 66+7, Y765; FABRICATED A NEW REPLACEMENT SPLICE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6-7. 2L72 4F RTA28NM 20030418000482003041800048WP 2003 4 18 UPS03840183 120030131A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, STATION 1720 LONG 14R IS CRACKED. REMOVED CRACKED LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON AND INSTALLED REPAIR SPLICES IAW SRM 53-2-2 FIG 10 AND 11. 2L74 4F RT4A25 20030421000502003042100050NE 2003 4 21 QXEA0300306 220030301A74213038916 IGNITER DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 400 MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09369PH 513 AG0107 SEA ON FLIGHT 2222- NR 1 ENGINE WILL NOT LIGHT OFF ON START SEQUENCE. RAN CHECKLIST, ATTEMPTED SECOND START WITH NO SUCCESS. REMOVED AND REPLACED NR 1 ENGINE INBOARD AND OUTBOARD IGNITORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030421002022003042100202EA 2003 4 21 2003F00229 120030209A2760604509697 CONTROLLER CNDAIRCL604 CL604 1900301EA SPOILER FAILED A UG8AO OTHER J WARNING INDICATION LDLANDING 1 GL23599DA 5498 GROUND SPOILERS DID NOT DEPLOY AT KPTK. NO DISCREPANCIES WERE DISCOVERED DURING TROUBLESHOOTING, AND SEVERAL OPERATIONAL CHECKS PER THE CL604 MM TASK 27-61-00-720-802. THE PSEU (CONTROLLER) WAS CHANGED AS A PRECAUTION PER BOMBARDIER RECOMMENDATION. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20040329000142004032900014NM 2004 3 29 ASAA0340320 120030725A5320654587545 FLOOR SUPPORT BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND SUPPORT ANGLE AT SERVICE DOORWAY CORRODED AT FS 328-295. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030716001032003071600103 2003 7 16 HEEA087972 420030628A22107612723 INDICATOR SKRSKYS76 S76C 8143008NE AFCS CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 CONDENSATION IN TOP INDICATOR. TO BE SENT TO VENDOR. 1G72 3U NCH1NE 20030423001662003042300166EU 2003 4 23 MALA030202 120030303A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15428XJ 340B428 DURING 4Y/2Y INSPECTION IN CWA, FRAME 258 TOP HAS CORROSION AT LBL 6. MAINTENANCE COMPLETED REPAIR IAW EO S53108. A/C RELEASE DATE 3/9/03. REF 409 176207 FOR DETAIL. 2L72 4T RTA52EU 20030424000232003042400023WP 2003 4 24 UPS03840316 120030313A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, BLENDOUT JUST BELOW CUSP LINE AT STA -67 IS BEYOND LIMITS. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030730000542003073000054NM 2003 7 30 ABXA030280 120030708A3350BPS73 BATTERY PACK BOEING767 767281 1385109NM CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23774AX 22789 WHEN TESTED EMERGENCY LIGHTS, LIGHT OVER COCKPIT DOOR WAS INOP. TWO EACH LIGHTS AT ENTRANCE DOOR GOOD. ALSO, SPARE LIGHT SUPPLY INOP. REPLACED MAIN EMERGENCY BATTERY POWER SUPPLY IAW B767 AMM 33-51-07. OPS CHECKED GOOD. 2L72 4F RTA1NM 20030730000572003073000057WP 2003 7 30 ABXA030296 120030624A532049125402 FITTING DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 ANGLE RIGHT BUTT LINE 34 UNDER FLOOR LINE WAS CRACKED AFT SIDE OF FS 965. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20030730000912003073000091WP 2003 7 30 ABXA030301 120030701A532099578943 INTERCOSTAL DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 AFT INTERCOSTAL CRACKED WHERE FORWARD AIRSTAIR DOOR MECHANISM ATTACHES. REPAIRED INTERCOSTAL IAW DC-9 SSRM K05159. 2L72 4F A6WE 20040223001662004022300166SO 2004 2 23 QRX2004F00000 120031205A783094HEN102RA SWITCH GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE THRUST REVERSER FAILED B QRXROO OTHER OTHER O OTHER NRNOT REPORTED 1 SW0584GV 2334 584 SWITCH FAILED. FOUND THE SWITCH HOUSING FULL OF WATER. THIS SWITCH IS LOCATED ON THE TOP SIDE OF THE ENGINE NACELLE. IT APPEARS TO HAVE WATER MIGRATING THROUGH THE SWITCH PLUNGER INTO THE HOUSING. THIS COULD COME FROM BEING PARKED IN THE RAIN OR AIRCRAFT BEING WASHED. 2L72 4F4 FRTA12EA E00057EN 20030827000202003082700020EU 2003 8 27 03FDEA00944 120030621A5320A53986733000 INTERCOSTAL AIRBUS300 A300B4605R 3930308EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE 742 THE INTERCOSTAL IS DAMAGED AND DEFORMED BETWEEN FRAME 86 AND 87 AT STR 40R. REMOVED DEFORMED SUPPORT ANGLE AND FABRICATED NEW SUPPORT ANGLE AND INSTALLED IAW A300-600 SRM 51-40-20. WORK DOCUMENTED ON M-1805 NR N00245 2L72 4F RTA35EU 20030722001042003072200104NM 2003 7 22 SWAA031477 120030702A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 12L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030805001002003080500100EA 2003 8 5 ASOA03266 120030618A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 FLT 4585 - DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTIN OF THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030806000672003080600067SO 2003 8 6 C2XA03TY097 120030727A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713990 145277 TYS- DURING A SCHEDULED 2C INSPECTION THE LT AND RT AISLE OMEGA BEAM AT THE SECOND CARBON CROSS BAR WAS FOUND CORRODED. MAINTENANCE CUT OUT DAMAGED SECTIONS ON LT AND RT FLOORBEAM, FAB EXTERNAL ANGLE SHIM AND FILLER ALODINED, PRIMED, PAINTED AND INSTALLED FA PARTS IAW EMB 145 SRM 53-21-10 AND EMB 145 CPM 51-21-04, 05.06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030801001202003080100120WP 2003 8 1 MWEA030288 120030722A2621892857 FIRE BOTTLE DOUG DC9 DC932 3022066WP ENGINE DISCHARGED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31202ME 47672 EXTIGUISHING AGENT TWO LOW LIGHT ILLUMINATED, THERMAL BOTTLE DISCHARGED TO ZERO PSI. REMOVED AND REPLACED BOTTLE. 2L72 4F A6WE 20030902001562003090200156NM 2003 9 2 DHL2003755010 120030709A324026011825 BRAKE BOEING727 727225 1384077NM PWA JT8 JT8D* NE LEFT SEIZED A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01755DH 21857 DURING TAXI, BRAKES SEEMED TO LOCK AND NOT RELEASE. SUSPECT LEFT BRAKE. REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY AND MAIN WHEEL ASSEMBLY DUE TO BRAKE SEIZURE DAMAGE IAW 727 M/M 32-45-1 & 32-41-32. OPS CHECKED SERVICEABLE. 2L73 4F4 F A3WE E2EA 20030903001742003090300174NM 2003 9 3 AALA20030739 120030711A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21784AN 29588 DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD EMERGENCY EXIT ILGHT AT FORWARD GALLEY INOPERATIVE. REPLACED LEFT FORWARD EMERGENCY EXIT LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030904000722003090400072NM 2003 9 4 QXEA200301051 120030830A243611521085 GCU BOMBDRDHC8 DHC8401 1390041NM NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09402QX1273 1273 4032 GEG- ON FLIGHT 2314 NR 1 DC GENERATOR ILLUMINATED FOLLOWED BY NR 1 DC GENERATOR HOT CAUTION LIGHT 30 SECONDS LATER. SECURED DC GENERATOR PER CHECKLIST WITH DC GENERATOR HOT CAUTION EXISTING. REMOVED AND REPLACED NR 1 DC GCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030807000502003080700050EA 2003 8 7 COMA0360343 120030804A5330601R3114627 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01920CA23288 7022 DURING COMPLIANCE OF TASK 002-53-160-610, 2 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL 9.0 AND RBL 9.0. THE CRACKS RANGE FROM 2.5 TO 3 INCHES IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV B, DATED 6-8-2003, AND REO 601R-53-41-162, DATED 6-9-2003. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20030814000222003081400022NM 2003 8 14 SWAA031734 120030803A531465476937 KEELBEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND KEELBEAM CORRODED AT BS 727, STR 27L. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F A16WE 20030813000722003081300072EA 2003 8 13 SWIA200312084 120030608A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS FAILED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07903SW 7425 ON TAXI OUT OUTBOARD GROUND SPOILERS, FLIGHT SPOILERS, SPOILERONS CAUTION MESSAGES. REMOVED AND REPLACED NR 1 SECU. OPS CHECKS GOOD. S/N OFF 1254. 2L72 4F RTA21EA 20030723001272003072300127EU 2003 7 23 AWXA200300624 120030502A5320D539747600400 PROFILE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, LBL 686MM. MAINTENANCE CUT OUT DAMAGED AREA OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, LBL 686MM; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW AWA ER 26-5341-03142-TB5. 2L72 4F RTA28NM 20030821002862003082100286WP 2003 8 21 AT0300021 120030718A3397 WIRE DOUG DC9 DC932 3022066WP CABIN DISCONNECTED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15837AT 45774 EMERGENCY PATH WIRING OPEN-UNDER LIGHT TRACK/ONE SECTION OF LIGHTS WAS INOPERATIVE. RECONNECTED WIRING. 2L72 4F A6WE 20030821002792003082100279NM 2003 8 21 USAASB03123 120030727A2197 WIRE BOEING737 7373B7 1384580NM CABIN PRESSURE CHAFED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19397US 23319 ORD - FLT 299 - EN ROUTE FROM PHL TO ORD, AT FL350, THE CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 11,500 FEET. CREW DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET. CREW REGAINED CONTROL OF CABIN IN STANBY MODE. HIGHEST CABIN RATE OF DESCENT WAS 800 FEET PER MINUTE. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT ORD. MAINTENANCE REPAIRED CHAFED WIRES AT CONNECTOR D640 (W034), WIRE NR 034-22, NR 040-22, NR 043024, NR 020-22 AND NR 017-24. ALSO, REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, P/N 763810-1, SELECTOR PANEL P/N 711002-5, AND AFT OUTFLOW VALVE P/N 711003-3, AS PRECAUTIONARY. PRESSURIZATION CONTROL SYSTEM FUNCTIONAL TEST GOOD PER MM 2L72 4F RTA16WE 20030910002062003091000206EU 2003 9 10 MALA030381 120030813A215012502101 BLOWER MOTOR SAAB SF340 340B 7860101EU A/C SYSTEM FAILED A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15407XJ 340B407 SUPPEMENTAL AC EMITS BURNING SMELL. FROM LOG PG NR 1177492, REMOVED AND REPLACED BOTH EVAPORATOR BLOWER MOTORS PN 1250210-1 IAW SAAB AMM 20-10-00 2L72 4T RTA52EU 20030911001202003091100120WP 2003 9 11 DHL2003873568 120030701A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT ELEVATOR UPPER PLATING IB SECTION HAS INTERIM FLUSH REPAIR AND SEVERAL DEFLECTED AREAS, FROM STA XAR.0.000 TO XE.132.000. PERFORMED MAJOR REPAIR IAW EODHL-030604, ED-3410. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL IAW EODHL-030604, ED-3410. CLEANED, TREATED AND PRIMED NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON RT ELEVATOR UPPER SURFACE IB SECTION (STA. XAR.0.000 XE.132.000) USING NEW FASTENERS IAW EODHL-030604, SRM 51-1-21. 2L74 4F RT4A25 20030926001362003092600136EA 2003 9 26 A6WA200340127 120030826A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT BRAKE FAILED A A6WAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 GL31412AW 7582 FLAP FAIL WARNING INFLIGHT WITH NO MOVEMENT AFTER FLAP SELECTION. INTERROGATED FECU, RIGHT BRAKE AND POSITION SENSORING UNIT (BPSU) FAIL. REMOVED AND REPLACED RIGHT BPSU. 2L72 4F4 FRTA21EA E15NE 20031001000592003100100059NM 2003 10 1 03FDEA00429 120030410A3210 INDICATOR BOEING727 727200 138407ENM MLG ILLUMINATED A FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25467FE 21449 RETRACTED GEAR, L AN R MAIN GEAR UNSAFE-RED, NOSE GEAR GREEN. EXTENDED GEAR - ALL 3 LANDING GEAR SAFE -GREEN PER CREW CONVERSATION : NOSE GEAR RETRACTED NORMAL AND NO GREEN LIGHT ON (VARIES FROM ACTUAL WRITE UP). ADDITIONAL INFO, GEAR WAS DROPPED TO SLOW A/C FOR RAPID DESCENT GEAR EXTENDED NORMALLY.AT ABOUT 20 MILES OUT IT WAS DECIDED TO RETRACT GEAR UNTIL CLOSER TO RUNWAY. WHEN RETRACTED NOSE GEAR CAME UP AND LIGHT OUT NORMAL. MAIN GEAR WENT TO INTRANSIT /UNSAFE AND AFTER A REASONABLE TIME GEAR AND DOOR LIGHTS STAYED ON PER BOOK GEAR WAS SEL DOWN AND THREE GREEN ON... INSPECTED ALL LANDING GEAR AND INDICATION COMPONENTS JACKED A/C CYCLED LANDING GEAR MULTIPLE TIMES-NO DEFECTS NOTED. 2L73 4F RTA3WE 20031002000732003100200073SO 2003 10 2 C2XA03TY150 120030910A532014522460015 GUSSET EMB 135 EMB135ER 3260203SO ALLSN AE3007AE3007C GL GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE GALLEY FLOOR AFT GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F4 FRTT00011ATTE6CH 20031002000042003100200004EU 2003 10 2 A6WA200360034 120030906A5230 SKIN BAC 146 146200A 1500266EU CARGO DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 DAMAGE EXTERNAL SKIN TO THE FORWARD CARGO DOOR MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060001. (M) 2H74 4F A49EU 20031007000532003100700053NM 2003 10 7 AALA20030717 120030708A3241S274TI1018 SHUTOFF VALVE BOEING757 757223 1384957NM ANTI SKID SYS DEFECTIVE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21633AA 24591 AFTER TAKEOFF, RIGHT HYDRAULIC SYSTEM BEGAN LOOSING QUANTITY. AIRCRAFT RETURNED TO SJU WITHOUT FURTHER INCIDENT. REPLACED BOTH ANTI-SKID SHUTOFF VALVES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002552003102100255NM 2003 10 21 03FDEA01608 120030917A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 RT OB FLAP OB HINGE (A/C SIDE); IB AND OB UPPER ACTUATOR ATTACH LUG FOUND CORRODED AT BORES AND SPOT FACES. ** S/D ** COMING 2L73 4F RTA22WE 20031022000532003102200053NM 2003 10 22 QXEA200301155 120030911A5310 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX- RIGHT SERVICE DOOR APERTURE IS NICKED ON FORWARD SIDE 13.5 INCHES DOWN FROM TOP. REPAIRED IAW Q400 SRM 51-26-10, 51-00-02, 51-00-04 AND RD 8/4-53-666. 2H72 4T RTA13NM 20031022000872003102200087NM 2003 10 22 03FDEA01747 120031015A5753 BOLT BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE TE FLAPS MISSING A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO25468FE 21452 AFTER SEVERAL SUCCESSFUL FLAP RETRACTION CYCLES, OUTBOARD FLAPS STOPPED AT 5 DEG & STAYED THERE WHILE FLAPS 2 WERE COMMANDED, ALTERNATE FLAP SELECTION WAS UNABLE TO MOVE THEM FURTHER UP OR DOWN. USE OF NORMAL HYD MOTOR WAS ABLE TO DRIVE OUTBOARDS DOWN. BUT NO SECOND ATTEMPT WAS MADE TO RETRACT THEM. TROUBLESHOT O/B FLAP DRIVE SYS IAW FEDEX MM, FOUND BOLT MISS NR 7 FLP CARRIAGE LOWER ACCESS CVR I/B SIDE. SPCT MISSING BOLT OF BIND BETWEEN MIDFLAP/FLAP TRCK CAUSE OB FLAP SYS TEMPORARILY INACTIVE. REPLACED MISSING BOLT. INSPECTED OB FLAP SYS/SAFETYS, NO ISSUES. OP CHECK FLAP DRIVE SYS TO FULL EXTREMES 50 TIMES. NO PROBLEMS. 2L73 4F4 FRTA3WE E2EA 20031023000412003102300041EU 2003 10 23 AWXA200301089 120030913A5320D5347112420100 WEB AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-07 CHECK CORROSION WAS FOUND ON FLOOR SHEAR WEB BETWEEN FR 69-70, AT RBL 49. MAINTENANCE REMOVED CORRODED FLOOR SHEAR WEB FR 69-70, RBL 49; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW 51-44-11, PG. 6, 8-25, & A24-A25, FIG. 2-7. 2L72 4F RTA28NM 20040115000582004011500058NM 2004 1 15 DL73G031086 120031214A335002031461201 LENS BOEING737 737330 13844BJNM CABIN CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27241DL 23833 REPLACED 2 LEFT EMERGENCY EXIT LIGHT ASSY, OPS CHECK NORMAL. 2L72 4F RTA16WE 20031113000112003111300011 2003 11 13 BAQA090154 420031024A3423258719343 COMPASS AGUSTAA109 A119 0261102EU COCKPIT INACCURATE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035LF 1481 14010 MAG COMPASS 20 DEGREES OFF AND DG INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H7EU 20031105000092003110500009EU 2003 11 5 03FDEA01843 120031031A5415 MOUNT AIRBUS300 A300F4605R 3930327EU NR 1 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25660FE 759 COMPLY WITH EA 6-5450-73844A PYLONS/NACELLS - NR 1 ENGINE PYLON FWD MOUNT CORROSION REPAIR. CLOSING ACTION ON 10/31/03 ON N/R S00016. COMPLIED WITH EA 6-5450-73844A. 2L72 4F RTA35EU 20031106000122003110600012NM 2003 11 6 AWXA200301358 120031013A5315146N5417 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1470, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM BS 1470, LBL 2; FABRICATED A REPAIR ANGLE & FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1. 2L72 4F RTA2NM 20031106000482003110600048SO 2003 11 6 C2XA03SH408 120031022A531514530633003 FLOORBEAM EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV- DURING C-CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 203 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031106001842003110600184NM 2003 11 6 03FDEA01861 120031103A5315651627910 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION AROUND SEVERAL NUT PLATE HOLES IN LONGITUDINAL FLOORBEAM, LBL 25, WL 208, BS 760 - 850. 2L73 4F RTA3WE 20031106001382003110600138SO 2003 11 6 C2XA03TY176 120031005A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713994 145291 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR SUPPORT CENTER OMEGA BEAM. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20031112000152003111200015NM 2003 11 12 2003UALA00820 120031030A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 SHEAR TIE HAS CORROSION, STA. 1628 TO STA 1620, AND STR 29L AND 28L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20031112000742003111200074NM 2003 11 12 ASAA2003B 120030316A5320 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND DAMAGE ON STRINGER CLIP AT BS 767, STRINGER 26R AND WL 146. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031112001002003111200100EU 2003 11 12 AWXA200301380 120031109A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 PHX - EEL - DURING INSPECTION FOUND A WIRE BROKEN ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040112000472004011200047EA 2004 1 12 2004F00019 220030121A7313RA9093 SPRING BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA POPPET VALVE BROKEN A YADAO OTHER J WARNING INDICATION NRNOT REPORTED 1 AL0345GL UC45 LOW FUEL PRESSURE LIGHT CAME ON IN FLT, ELECTRIC BOOST PUMP WAS TURNED ON AND EXTINGUISHED LIGHT. MAINTENANCE REMOVED THE LOW PRESSURE FUEL PUMP AND FOUND THE DRIVESHAFT HAD SHEARED. THE PUMP WAS REPLACED. DISASSEMBLY OF THE PUMP DISCLOSED THAT THE POPPET VALVE SPRING P/N RA 9093 HAD FAILED AND PIECES OF THE SPRING HAD BEEN INGESTED BY THE PUMP ROTOR, SEIZING THE ROTOR. (M) 2L72 4T4 TRTA24CE E4EA 20040304001502004030400150NM 2004 3 4 ASAA0340348 120031201A3397 CONNECTOR BOEING737 7374Q8 138447QNM EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING LINE CHECK, FOUND NEAR ROW 23 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20031215000472003121500047NE 2003 12 15 2003UALA00827 220031102A7261 SCREW BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE BEARING RETAINERLOOSE A UALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP29657UA 27112 NR 2 ENGINE FLAMEOUT. FLAME OUT WAS CAUSED BY FUEL LEAK AT THE AIR/OIL COOLER MUSCLE LINE. THE FUEL MUSCLE LINE WAS REPLACED AND THE ENGINE WAS REMOVED WITH IN 25 CYCLES DUE TO A SURGE ABOVE 1.25 EPR CAUSED BY THE FLAME OUT. THE MUSCLE LINE FAILED DUE TO VIBRATION CAUSED BY THE ANGLE GEARBOX. THE ANGLE GEARBOX HAD THREE BEARING RETAINING SCREWS LOOSE AND ONE HAD FALLEN OUT. ROOT CAUSE OF THE FAILURE APPEARS TO BE INSUFFICIENT RETENTION OF THE AB4 BEARING RETAINING SCREWS. THE ADDED ADDITION OF LOCKING LIQUID WILL BE USED ON FUTURE BUILDS IN THE ANGLE GEARBOX. 2L72 4F4 FRTA1NM E24NE 20031211001982003121100198EU 2003 12 11 USAA030255 120031030A5320D534209300000 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT CORRODED 1.8 INCH BY 1.7 INCH BY .020 INCH DEEP, FS 67 INBOARD OF -Y 114 FLOOR. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-40-00. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040427000522004042700052EU 2004 4 27 ERAA093695 120030930A3212D24873102 FLOAT BOLKMS105 BO105S 5626006EU MLG INOPERATIVE A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 6811 RT FLOAT ASSY DUE INSPECTION. COVER WORN. FWD END CAP DETERIORATED CYLINDER DUE HYDRO TEST 4/04. FLOAT BRG DELAMINATED AT FOREWARD GIRT. PERFORMED 18 MONTH INSPECTION. CHANGED FLOAT BOTTLE, FLOAT BRG, MANIFOLD AND FLOAT COVERS. REPAIRED WIRE HARNESS AND REPLACED RIVNUTS IN SUPPORT TUBE. CHECKED FOR COMPLIANCE WITH 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1 AND 802-25-2. 1G72 3U H3EU 20060801001482006080100148WP 2006 8 1 IXXA060591S 120030910A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP TOP SKIN GOUGED AT STATION XF103. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 57-7-0, AND 51-1-8. 2L74 4F RT4A25 20030819000062003081900006EU 2003 8 19 BAQA088147 120030718A7810117651121 TAILPIPE BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101750B1 41560NE ENGINE CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1077 7243 TAIL PIPE ASSY CRACKED ON INTERNAL CONE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE10 20030331000682003033100068EA 2003 3 31 ASOA03092 120030308A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO11874AS 7551 DURING HANGER MAINTENANCE, THE LT ANGLE BRACKET UNDER THE ENGINE SUPPORT BEAM FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ANGLE BRACKET UNDER THE ENGINE SUPPORT BEAM FRAME IAW SRM. 2L72 4F4 FRTA21EA E15NE 20030401000592003040100059NM 2003 4 1 CA030224004 120030219A492038042816 APU BOEING737 737217 1384464NM PWA JT8 JT8D17A 52049NE APU BAY FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN) PRIOR TO PUSH BACK, AIRCRAFT RAPIDLY FILLED CABIN WITH SMOKE, AIRCRAFT DEPLANNED. CAUSED BY THE BLEED FROM THE APU (BURNED OIL CONTAMINATION) APU CHANGED AND COLLESTER BAGS REPLACED. AC SERVICEABLE 2L72 4F4 F A16WE E2EA 20030414001312003041400131SO 2003 4 14 CA030311007 120030227A27401430011 CONTROL CABLE PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA STABILATOR FRAYED W D RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN) STABILATOR TRIM BINDING DUE TO FRAYED WIRES, DISCOVERED DURING PRE-FLIGHT. 1L72 3O3 O 1A10 1E4 20030416003912003041600391SO 2003 4 16 SWIA200311712 120030111A3010 PRESSURE SWITCH EMB 120 EMB120ER 3260203SO DEICE BOOT MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07298SW 120328 MIDDLE RIGHT WING DEICE BOOT LIGHT CAME ON INFLIGHT, BOTH TIMERS. RETURNED TO SLC. REMOVED AND REPLACED THE PRESSURE SWITCH FOR THE RIGHT MIDDLE WING DEICER. RAN THE ENGINES AT ALL POWER SETTINGS. NO FAULTS NOTED AT THIS TIME. P/N OFF: 211C117-183, S/N OFF: U08021A. 2L72 4T RTA31SO 20030424000832003042400083 2003 4 24 GLBA2003038 420030324A34546226137201 RECEIVER BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03253GL11887 UE253 NR 1 NAV FAILED. REMOVED AND REPLACED NR 1 NAV VIR32. 2L72 4T RTA24CE 20030424000942003042400094SO 2003 4 24 SWIA200311835 120030317A27503075001007 FCU EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07190SW5029 2719 120050 FLAP CONTROL FAULT FOR INBOARD FLAPS UPON RETRACTING FLAPS AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL AND FCU FOR TROUBLESHOOTING. RAN FLAPS UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 20030423002102003042300210NE 2003 4 23 UPS03440288 220030313A7200JT97Q ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7A 52054NE NR 4 FAILED A IPXAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING CE F.O.D. VIBRATION/BUFFET TOTAKEOFF 1 SO01526UP 21937 DURING T/O AND CLIMB, TOWER NOTICED AND NOTIFIED FLT 6703 THAT SMOKE WAS TRAILING FROM NR 4 ENGINE. AT 6500 FEET CREW REPORTED A BANG AND ASSOCIATED ROLL BACK OF N1/N2. CREW FOLLOWED SEVERE ENGINE DAMAGE CKLIST. FUEL DUMPED AND AIRCRAFT 526 ON FLT 6703 RETURNED TO PHL. REMOVED AND REPLACED NR 4 ENG ASSY IAW MM TASK CARD 5000 PG 1-27. 2L74 4F4 F A20WE E20EA 20030428000562003042800056NM 2003 4 28 OZI2003F00001 120030102A5315001A534C4061338 FLOORBEAM DORNERDO32 DO328300 NM FUSELAGE CORRODED A OZIAO OTHER O OTHER NRNOT REPORTED 1 SO07430Z 6656 3127 FORWARD SIDE OF LAVATORY FLOORBEAM (FRAME 35) CORRODED. 2H72 4T RTA55NM 20040126000352004012600035SW 2004 1 26 HEEA087819 120030623A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 FLAP RESTRAINT STICKING. SHOP REPAIR. 1G71 3U H2SW 20040122001232004012200123WP 2004 1 22 GTIA030972 120031110A5710 FRAME DOUG DC9 DC983 3022083WP LT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND LEFT WING AT NR 1 SLAT AND WING ANTI-ICE TELESCOPING DUCT LOWER PANEL STRUCTURE CRACKED AT FORWARD OUTBOARD CORNER IN RADIUS. REMOVED AND REPLACED FRAME. (M) 2L72 4F RTA6WE 20031204000482003120400048WP 2003 12 4 AALA20031042 120030921A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21582AA 53159 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE IN THE AFT CABIN SECTION OF THE AIRCRAFT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031209000712003120900071NM 2003 12 9 SWAA032371 120031027A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 854, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031210000922003121000092EA 2003 12 10 COMA0360516 120031126A5210 CAM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01966CA 7132 FLIGHT 5850 AFTER TAKEOFF RECEIVED A CABIN DOOR OUTER HANDLE AND OVERBOARD COOL CAUTION MESSAGE. AIRCRAFT RETURNED TO DEPARTING CITY (CVG). REPLACED THE ROLLER CAM FOR THE CABIN DOOR INNER HANDLE. 2L72 4F RTA21EA 20030923001452003092300145EU 2003 9 23 AWXA200300972 120030822A33501012881 LIGHT AIRBUS320 A320231 3930325EU SEAT ROW 9 LT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28631AW 077 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040211000152004021100015NM 2004 2 11 USAA030322 120031228A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19586US49931 23931 CLT - FOUND SKIN CRACKED 2.250 INCH, 4 INCHES FORWARD OF FS 727E .500 INCH ABOVE S-24R ON SKIN. INSTALLED DOUBLER 24 INCHES BY 30 INCHES PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040301001002004030100100EU 2004 3 1 RYN2004F00002 120031019A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 A (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 AND STRINGERS 34R TO 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 FROM STRINGER 34R TO 34L IN FORWARD PIT. 2L72 4F4 FRTA28NM E40NE 20031212001602003121200160 2003 12 12 GTIA030850 420031021A2564R0202A211 LIFE RAFT DOUG DC9 DC981 3022081WP CABIN FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 DTW - FOUND DURING MINI-EVACUATION DEMONSTRATION, ONE CHAMBER OF RAFT FAILED TO INFLATE. REMOVED AND REPLACED AFT. (M) 2L72 4F A6WE 20040412001442004041200144NM 2004 4 12 ASAA024016A 120030322A53206547690 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT IS CORRODED AT BS 727-727F. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031217000642003121700064WP 2003 12 17 DHL2003805585 120030820A573056563511 SKIN DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING FUSELAGE NR 706 UPPER FAIRING SKIN DELAMINATED, STA 912.000 - STA 980.000. REMOVED AND REPLACED LEFT WING TO FUSELAGE UPPER FAIRING NR 706 (STA 912.000 - 980.000) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030926000272003092600027NM 2003 9 26 AWXA200300990 120030826A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28807AW 1064 FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041124000062004112400006CE 2004 11 24 EHA2004F00005 120031112A3040MS24166D1 RELAY BEECH 200 B200C 1152924CE PWA PT6 PT6* 52043EA WINDSHIELD HEAT STUCK E EHAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 AL03134WJ BL134 RT WINDSCREN SHATTERED AT FL250. NO LOSS OF CABIN PRESSURE OCCURED. LANDED SAFELY WITHOUT INCIDENT. UPDATE TO PREVIOUS SDR DATED 11/11/03. UPON DISASSEMBLY AND TESTING, IT WAS DETERMINED THAT THE CAUSE OF THE INCIDENT WAS THE WINDSHIELD HEAT RELAY. 1L72 4T3 T A24CE E2NE 20060801000882006080100088WP 2006 8 1 IXXA060545S 120030907A5512 SKIN DOUG DC8 DC871F 302199DWP ZONE 300 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE UPPER SURFACE CORRODED AT STATION XFS178. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 55-2-1, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060801001432006080100143WP 2006 8 1 IXXA060586S 120030923A5712 RIB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE UPPER SURFACE RIB CRACKED AT STATION 322. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 51-1-8, 51-3-0, AND 57-3-3. 2L74 4F RT4A25 20031121000792003112100079NM 2003 11 21 VNAA0310021 120031028A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07463PS175663369 3087 ON ENGINE START EMERGENCY LIGHTS ROW 7, 8, & 9 BLINK ON AND OFF. MAINTENANCE INSPECTED AND REPLACED THE 7LK BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040113001652004011300165SO 2004 1 13 RAIA00311295 120031128A3240156221 PRESSURE SWITCH EMB 145 EMB145 3260210SO BRAKE SYS LEAKING A RAIAO OTHER J WARNING INDICATION LDLANDING 1 CE03803HK 145077 BGM- HYDRAULIC SYSTEM 1 FAILURE. MAINTENANCE REMOVED AND REPLACED BRAKE PRESSURE SWITCH. 2L72 4F RTT00011AT 20040114000292004011400029SO 2004 1 14 C2XA03CL211 120031225A326085271 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO LT MLG FAULTY A C2XAO OTHER N FALSE WARNING APAPPROACH 1 SW2714991 145278 CLE FLIGHT 2249 THE CREW REPORTED THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED ON THE EICAS DURING FLIGHT. MAINTENANCE INSPECTED THE LEFT MAIN GEAR AND REPLACED BOTH DOWNLOCK PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD. P/N 8-527-1, S/N 14544. 2L72 4T RTT00011AT 20040114001342004011400134NE 2004 1 14 DL75K031065 220031130A7321 EEC BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 SO276701 41502 30187 716540 CREW REPORTS AT FL350 NR 2 ENGINE SHUT ITSELF DOWN FOR NO APPARENT REASON. NO COCKPIT INDICATIONS TO WARN OF ANY ENG PROBLEMS BEFORE THE SHUTDOWN. REPLACED EEC. 2L72 4F4 FRTA2NM E17NE 20031216000222003121600022EA 2003 12 16 MASA200300450 120031112A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA E/E BAY DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07501MJ 10047 PHX- PAX DOOR EMERGENCY OVERWING LIGHT AND SERVICE DOOR LIGHT INOP. MX REPLACED THE NR 1 AND 2 EMERGENCY LIGHT BATTERY PACKS. OP CHECKS GOOD. 2L72 4F RTA21EA 20031218000622003121800062NM 2003 12 18 03FDEA02000 120031128A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 CTR CARGO RT TUNNEL BETWEEN STA 5-113 TO STA 1541 NR 38 LONGERON SPLICE FOUND CRACK. REMOVED DAMAGED LONGERON SPLICE AS PER SRM 51-31-01, VOL.II AND FABRICATED NEW SPLICE AS PER DRAWING A5A7114. INSTALLED NEW SPLICE AT CENTER CARGO RT TUNNEL BETWEEN STA 5-113 TO 1541, NR 38 LONGERON AS PER DRAWING N5A6774. 2L73 4F RTA22WE 20031218001432003121800143NM 2003 12 18 CALA0300687 120031204A5720655081386 ANGLE BOEING737 737524 1384721NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916648 28909 RT WING 90 DEGREE GREEN ANGLE CRACKED AT FORWARD SIDE OF RT MLG INBOARD DOOR OPENING WBL 71 UNDER STRUT DOOR. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-02. 2L72 4F RTA16WE 20031219001452003121900145NM 2003 12 19 03FDEA02128 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. 2L73 4F RTA22WE 20031222000602003122200060WP 2003 12 22 ASAA0380628 120031011A53305936004 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CEHCK, FUSELAGE SKIN CORRODED AT FS 769-788, BETWEEN LONGERON 30 AND 29R UNDER FAIRING RUB STRIP AND AROUND FASTENER HOLES. REPAIRED PER EA 5330-01708. (M) 2L72 4F RTA6WE 20040105000782004010500078 2004 1 5 372PA0038 420031024A2210 CONNECTOR BOEING737 737306 13844BGNM GE CFM56 CFM56* 13802NE AUTOPILOT 1,2 DIRTY A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05372PA 23546 AUTO PILOT B WILL NOT ENGAGE AND AUTO PILOT A IS INTERMITTENT. REMOVED DIRT FROM AUTO PILOT A AND AUTO PILOT B CONNECTORS. A AND B SYSTEMS TEST OK IAW MM 22-10-00. 2L72 4F4 FRTA16NE E2GL 20040106000042004010600004WP 2004 1 6 DHL2003802572 120031202A5310 DOOR FRAME DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 WEAR DAMAGE TO THE RIGHT FUSELAGE FWD CTR SECTION LOWER CARGO COMPARTMENT DOOR JAMB AROUND STA 324.000, L-32R (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART O6,10-01.001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AND EXTERNAL REPAIR DOUBLER AND TWO FILLERS IAW ED EDU38-5, DWG U38-R05. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED THE REPAIR DOUBLER AND BOTH TWO FILLERS ON DOOR JAMB (LOWER CARGO COMPT AROUND STA 324.000, L-32R) USING NEW FASTENERS IAW ED EDU38-5, DWG U38-R05, SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031010000232003101000023NM 2003 10 10 USAABB03162 120030908A3350873100151REV12 LIGHT BOEING767 7672B7 1385107NM 12GF INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 FOUND FLOOR LEVEL EMERGENCY LIGHTING AT ROWS 6GF THROUGH 12GF INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. OPS CHECK GOOD. (M) 2L72 4F RTA1NM 20040114000582004011400058EA 2004 1 14 A6WA200340163 120031111A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE LIGHTNING STRIKEA A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31401AW 7280 RT FUSELAGE SKIN AT FS409 AND 48 STRINGER 23R HAS LIGHTNING DAMAGE WITH A TEMPORARY REPAIR IAW MFG REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED SECTION OF FUSELAGE SKIN, FABRICATED REPAIR DOUBLER FROM 2024-T42 .063 INCH PO NR 169562 AND INSTALLED IAW CRJ200 SRM 53-00-31 REPAIR NR 1 AND WVAC EO 601R-53-4381. 2L72 4F4 FRTA21EA E15NE 20040115000952004011500095NM 2004 1 15 03FDEA02285 120031229A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, I/B FLAP O/B AFT HINGE LOWER SIDE LOAD ROLLER BOLT ATTACHMENT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75227, TRAILING EDGE AND TRAILING EDGE DEVICES. RT INBOARD FLAP AFT OUTBOARD HINGE UPSTOP BRACKET REPAIR. 2L73 4F RTA22WE 20031126000612003112600061NM 2003 11 26 CALA0300665 120030716A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND FLOORBEAM CORRODED IN FORWARD GALLEY AREA AT STA 328, RBL 29. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20030429000162003042900016NM 2003 4 29 P5CA0300809 120030127A5312 BULKHEAD BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 FWD PRESSURE BULKHEAD FOUND CRACK ON F/S 1HR 12:30 O'CLOCK. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH STRAP & DOUBLER PER SRM 51-40-03 FIG-2. 2L74 4F A20WE 20030428001912003042800191SO 2003 4 28 RAIA00303096 120030331A3350 SOCKET EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DIRTY A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03816HK 145055 STL- CEILING EMERGENCY LIGHT 3RD FROM BACK INOP. CLEANED LIGHT SOCKET, OPS CHECK OK. 2L72 4T RTT00011AT 20030430001362003043000136NM 2003 4 30 SWAA030913 120030421A5320BAC1518 STIFFENER BOEING737 737317 138447PNM LT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 6.75. R&R VERTICAL STIFFENER PER SRM. 2L72 4F RTA16WE 20030501000392003050100039WP 2003 5 1 AALA20030267 120030220A5310 DOOR FRAME DOUG DC9 DC983 3022083WP EMERGENCY EXIT CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 TUL - FOUND RIGHT AFT OVERWING EXIT JAMB IS CRACKED UPPER SIDE AFT OF CENTER. INSTALLED DOUBLER PER SRM 53-05-00 FIG 32. (M) 2L72 4F RTA6WE 20030502002392003050200239NM 2003 5 2 03FDEA00593 120030423A5310 STANCHION DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LOWER FORWARD CARGO AFT BULKHEAD STANCHION P/N A6A7094-17 AT STA X = -9.0 FOUND CORROSION (6 PLACES) ON FASTENERS HOLES. 2L73 4F RTA22WE 20030505000052003050500005WP 2003 5 5 03FDEA00446 120030415A5754 SLAT TRACK DOUG DC10 DC1030 3023501WP LT WING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 COMPLY WITH EA 8-2780-68790 FLIGHT CONTROLS-SLATS-REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9. CLOSING ACTION ON 04/14/03. COMPLIED WITH EA 8-2780-68790 FLIGHT CONTROLS-SLAT- REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9. 2L73 4F A22WE 20030508000172003050800017NM 2003 5 8 DL757030339 120030405A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27698DL 29911 AFTER TAKE OFF FLIGHT ATTENDANTS REPORTED OIL ODOR IN CABIN. CREW ALSO DISCRIBED WHAT THEY SAID WAS A BURNED OIL ODOR. NO VISIBLE SMOKE NOTED THROUGH OUT AIRCRAFT. PERFORMED DUCT BURNOUT PROCEDURE USING APU AIR RUNNING EACH A/C PACK SEPERATELY AT FULL HOT. NO ODOR. ENGAGED UTILITY BUSSES POWERED ALL OVENS AND COFFEEMAKERS. INSPECTED LAVS AND GALLEYS ALSO ALL CABIN LIGHTING. NO ODOR NOTED. 2L72 4F RTA2NM 20030613000012003061300001NM 2003 6 13 EIA2003076 120030523A7160 ENGINE BOEING747 747212B 1384886NM NR 1 BIRD INGESTION A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 POST FLIGHT WALKAROUND FOUND BIRD STRIKE NR 1 ENGINE. FOUND 2 EACH N1 FAN BLADES DAMAGED ENGINE INSPECTED IAW MM 72-00-00. REMOVED AND REPLACED NR 1 AND NR 2 BLADES IAW WC F7208 RII ACCOMPLISHED. 2L74 4F A20WE 20030521000342003052100034WP 2003 5 21 MWEA030193 120030428A79307938314506 LINE DOUG DC9 DC981 3022081WP ENGINE OIL LEAKING A MWEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL31803ME 48029 RIGHT OIL PRESSURE LOW ANNUNCIATOR CAME ON, AND OIL QUANTITY WAS DECREASING. FOUND LINE THAT GOES TO OIL PRESSURE LEAKING AT FITTING. REMOVED AND REPLACED OIL LINE AND SERVICED OIL TO FULL, PERFORMED LEAK CHECK. CHECKED GOOD. 2L72 4F A6WE 20030521000652003052100065WP 2003 5 21 DHL2003804897 120030125A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E FORMER UPPER PART WITH 1.000 AT STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LT WING CTR L/E FORMER UPPER PART AT XFS 379.000 IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030617002082003061700208NM 2003 6 17 QXEA200300714 120030601A5512 SKIN BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT SPAR CAP AND Y605D-39.17. REPAIRED IAW Q400 SRM 51-21-10, PAGE 204-205 AND SRM 51-25-10, PAGE 201-205. 2H72 4T RTA13NM 20030618001512003061800151EA 2003 6 18 COMA0360274 120030612A2710 AILERON CNDAIRCL600 CL6002B19 1900309EA WING BINDING A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01708CA 7235 FLIGHT 5523 AILERON BINDING IN FLIGHT. COULD NOT DUPLICATE, INSPECTED AILERON CONTROL PATH AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20030618000192003061800019GL 2003 6 18 HEEA087121 220030610A73210164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 ANTICIPATOR ROUGH, CAUSING TRIM MOTOR SLOW RESPONSE. 1G72 3U3 U H1NE E1GL 20030623001132003062300113EA 2003 6 23 A6WA200340083 120030519A5753 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 LEFT INBOARD FLAP HAS WORN RIVET HEADS ON INBOARD RIB OUTER FACE. REPLACED DISCREPANT RIVETS IAW CRJ SRM CHAP 51 AND WVAC EO 601R-57-4038. (M) 2L72 4F RTA21EA 20030714000572003071400057NM 2003 7 14 SWAA031382 120030620A5520BACB28AK04 BUSHING BOEING737 7377H4 1384404NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED PM CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB HINGE HARDWARE AND BUSHINGS PER SRM. 2L72 4F RTA16WE 20031203001212003120300121EU 2003 12 3 ASOA03558 120031015A5320 PLATE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING A C-CHECK IN BNA, THE FLOOR PLATE ON THE RIGHT SIDE BETWEEN FS 35 AND FS 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR PLATE ON THE RIGHT SIDE BETWEEN FS 35 AND FS 36 IAW SRM 51-25-01 AND 51-25-02. (M) 2H72 4T RTA53EU 20031205000672003120500067 2003 12 5 249TR0020 420031113A22104084042911 COUPLER BOEING737 7372K5 138448XNM YAW DAMPER FAILED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05249TR 22598 YAW DAMPER SWITCH WILL NOT LOCK ON. TRIPS BREAKER. PLACED ON MEL 22-3-1. 11/20/2003: REPLACED YAW DAMPER COUPLER. OPS NORMAL PER MM 22-12-01. CLEARED MEL 22-3-1. 2L72 4F RTA16WE 20031209000012003120900001WP 2003 12 9 IXXA0300069O 120031028A7797 WIRE HARNESS DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C1 13802EU NR 1 ENGINE DAMAGED A IXXAEC ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW11825BX844181368 45978 692256 ON TAKEOFF FROM KLRD TO KTOL NR 1 EGT FLUCUATED WILDLY BETWEEN 700 DEGREES AND OFF SCALE HIGH (1000). BOTH ANALOG AND DIGITAL EGT FOLLOWED THROTTLE BUT CONTINUED TO FLUCTUATE ERRATICALLY TO 1000 DEGREES. FUEL FLOW FLUCTUATES 150-200 LBS PRECAUTIONARY ENGINE SHUTDOWN PERFORMED AT 0404Z OIL PRESS 1LB AT 28 N1. N1 AND N2 APPEARED NORMAL, ALL OTHER ENGINE PARAMETERS NORMAL. CREW CONTINUED FLIGHT. MAINTENANCE RAN NR 1 ENG IAW ATI ERH 70.01.01 AND PERFORMED POWER ASSURANCE TEST IAW ATI ERH 91.01.03. NO FLUCUTATION IN ENGINE PARAMETERS NOTED. PIGTAIL FOR NR 1 ENGINE WAS REMOVED AND REPLACED PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20031209002252003120900225NM 2003 12 9 CALA0300621 120031020A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 MAINTENANCE DISCOVERED AN EXISTING TRIM-OUT TO THE INNER SKIN OF THE FORWARD CARGO DOOR AT AN UPPER LIGHTENING HOLE LOCATION. A PERMANENT REPAIR WAS INSTALLED TO THE INNER SKIN IAW ECRA 5232-01037. 2L72 4F RTA16WE 20031209000812003120900081 2003 12 9 SWAA032347 420031024A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031210001062003121000106NM 2003 12 10 03FDEA01996 120031126A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 FUSELAGE, STA Y=275 NOSE RADOME CUTOUT FUSELAGE EXTERIOR SKIN RIGHT UPPER FOUND WITH CRACK. FUSELAGE STA Y=275 NOSE RADOME FUSELAGE EXTERIOR SKIN CARRIED OUT REPAIR IAW SRM 53-00-01, FIG 5, VOL I. 2L73 4F RTA22WE 20031209002612003120900261NM 2003 12 9 AWXA200301362 120031014A5320146N53236 SUPPORT ANGLE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE BS 1701-1720, LBL 45. MAINTENANCE REMOVED DAMAGED AFT SHEAR DECK LOWER SUPPORT ANGLE FROM BS 1701 TO BS 1720, LBL 45; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 146N5323; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 1. 2L72 4F RTA2NM 20031210000852003121000085NM 2003 12 10 SWAA032618 120031127A3350079123 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29421LV 32452 DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20031211000302003121100030WP 2003 12 11 ABXA030428 120031027A523059101419 PAN DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 FORWARD LOWER CARGO DOOR OUTER PAN HAD CRACK INDICATION AT FORWARD HINGE AREA. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM. 2L72 4F A6WE 20031021000932003102100093SO 2003 10 21 SIMA200323601 120030819A27503631001007 ECU EMB 145 EMB145LR 3260212SO E/E BAY MALFUNCTIONED A SIMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW21651AE 145422 LRD - FLT 3453 - DURING APPROACH, CREW REPORTED THE FLAPS WOULD NOT DEPLOY. FOLLOWED AOM PROCEDURES AND LANDED WITHOUT FLAPS WITH NO OTHER PROBLEMS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030923001912003092300191NM 2003 9 23 USAABB03140 120030817A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 FOUND EMERGENCY EXIT LIGHTS NEAR LEFT MID LAVATORY INOPERATIVE. MAINTENANCE REPAIRED FAULTY WIRING AFT OF THE LAVATORY. (M) 2L72 4F RTA1NM 20040203000602004020300060NM 2004 2 3 ASAA0310160 120030320A53476546817 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 663-727B, RIGHT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040202001332004020200133NM 2004 2 2 UPS04541725 120031231A5347 SEAT TRACK BOEING757 75724APF 1384969NM EXPANSION LINK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE: C, CORROSION ON EXPANSION LINK SEAT TRACK BS 886 - 893 RBL 45 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED LINK, FABRICATED AND INSTALLED REPLACEMENT LINK IAW SRM 53-00-52, SRM 51-10-02 & SRM 51-40-02. 2L72 4F RTA2NM 20040205000442004020500044EU 2004 2 5 206571 120031122A7720 PANEL SAAB SF340 SF340A 7850100EU CTOT MALFUNCTIONED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL1740SZ 34040 FLT NR 4645 FROM PIT TO SDF. ON TAKE-OFF, AIRCREW NOTICED CTOT DID NOT ARM. AIRCRAFT RETURNED TO GATE. 2L72 4T RTA52EU 20040205000582004020500058EA 2004 2 5 ASOA03675 120031223A3350BR9279106 SIGN CNDAIRCL600 CL6002B19 1900309EA EMERGENCY SIGN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT SIGN FLOODLIGHT IN THE GALLEY BUT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN FLOODLIGHT ASSEMBLY IN THE GALLEY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030714000822003071400082NM 2003 7 14 SWAA031417 120030625A3350101073 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030717000802003071700080SW 2003 7 17 HEEA088072 120030705A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D152 51106 BATTERY WEAK. SHOP REPAIR. 1G71 3U H2SW 20030718000092003071800009NM 2003 7 18 TSAA0353118 120030506A53136545776 STRINGER BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 CORROSION DISCOVERED ON STRINGER LOCATED AT BS 967, LBL 7. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-1. (M) 2L72 4F RTA16WE 20030707001072003070700107WP 2003 7 7 UPS03840860 120030616A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LEFT WING LE. OB. LOWER RIB IS CRACKED AT XFS 622.5 STOP DRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030716000572003071600057WP 2003 7 16 GTIA030464 120030508A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT PIT CORRODED FLOOR WEB AT FS 1250 APPROX 10 INCHES INBOARD OF CUSP LINE RIGHT SIDE, CORRODED FASTENER AT CUSP LINE AFT SIDE OF FRAME 1250. FABRICATED NEW WEB. INSTALLED NEW WEB. (M) 2L72 4F A6WE 20030717000522003071700052SW 2003 7 17 HEEA088028 120030630A2820407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL SYSTEM STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 FUEL PRESSURE SWITCH STICKS CLOSED. REPLACED SWITCH. 1G71 3U O H2SW 20030127001502003012700150SW 2003 1 27 HEEA083685 120030115A3212206050247138 COVER BELL 407 407 1182206SW EMERGENCY FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 EMERGENCY FLOAT COVER TORN. 1G71 3U O H2SW 20030128000962003012800096SW 2003 1 28 HEEA083843 120030116A6230406010429101 PIN BELL 407 407 1182206SW M/R DRIVE LINK GALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 GALLING AND PITTING ON THE INBOARD END OF THE MAIN ROTOR DRIVE LINK PIN. 1G71 3U O H2SW 20030204001002003020400100NM 2003 2 4 SWAA030127 120030119A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 848 STR 16L AND BS 972 STR 21L. REPAIRED FUSELAGE SKIN CRACKS PER SRM. 2L72 4F RTA16WE 20030207000712003020700071CE 2003 2 7 GLBA2003016 120030206A280010038100511 FUEL CAP BEECH 1900 1900D 1154162CE A GLBAD RETURN TO BLOCK K FLUID LOSS CLCLIMB 1 NM0394GL UE94 LH FUEL CAP LEAKING FUEL, R&R FUEL CAP 2L72 4T RTA24CE 20030207000852003020700085NM 2003 2 7 DHL2003747004 120030206A2610 FIRE DETECTOR BOEING727 727224 1384076NM A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01747DH 22253 1) #1 ENGINE GROUND CIRCUIT DETECTOR LIGHT ILLUMINATED.2) REMOVED AND REPLACED #1 ENGINE FIRE DETECTOR IAW 26-11-22. SYS OPS CHECKED GOOD IAW 26-11-0. 2L73 4F A3WE 20030218002402003021800240NM 2003 2 18 SWAA030235 120030131A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING CONNECT POINT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030221000372003022100037NM 2003 2 21 QXEA0300148 120030124A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- LEFT HAND WING NR 1 FLAP TRACK, LOWER TRACK, UPPER SURFACE HAS DIVOTS. REPAIRED IAW DHC-8 RD 8-57-985 AND SRM 51-00-06. 2H72 4T RTA13NM 20030224000922003022400092SW 2003 2 24 HEEA084213 120030120A5320 STRUCTURE BELL 407 407 1182206SW STORAGE BIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 INTERIOR STORAGE BIN STRUCTURE IS CRACKED. 1G71 3U O H2SW 20030114002622003011400262WP 2003 1 14 ZW0A0300601 120030112A3350408822101 BATTERY DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13948TW 49575 THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE FROM ROW 12 THRU 17. REPLACED THE BATTERIES IN THE B5-102 BATTERY PACK. CHECK-C 12-17-2002 STL. --CLOSED-- 2L72 4F RTA6WE 20030116000082003011600008SW 2003 1 16 ERAA082950 120030106A6230 BUSHING BELL 412 412 1182202SW ROTOR HEAD WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01416EH13561 A100112 33011 HUB & SLEEVE ASSY HAS WORN S/P LINK AND WORN COLLECTIVE BUSHINGS. DISASSEMBLED TO FASCILITATE COLLECTIVE LEVER BUSHING REPLACEMENT. REPAIRED COLLECTIVE TEFLON BUSHINGS & SPACERS 4 S/P LINK SPHERICAL BRGS, 1 DRIVE LINK SPHERICAL BRG, BEARINGS IN LINERS, COLLECTIVE PINS, AND TRUNNION. REPLACED DRIVE LINK ASSY. REASSEMBLED HUB & SLEEVE ASSY REATTACHED TO SWASHPLATE SN RE-10098. INSTALLED COLLECTIVE LEVER WITH NEW PINS AND SAFETIED. LUBRICATED WITH MOBIL 28. REPAIRED IAW 412 &N CR&O CH 62, MM 62, & SPM TT 13560.9 TSO 1158.8. 1G72 4U H4SW 20030121000462003012100046SW 2003 1 21 HEEA083248 120030108A2560206072841111 SEAT BELT BELL 206 206L3 1182108SW COCKPIT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 LT FWD FACING SEAT BELT IS BROKEN AT SPRING. REPAIRED. 1G71 3U H2SW 20030225000482003022500048SW 2003 2 25 HEEA084268 120030129A5260212075418105 ACTUATOR BELL 412 412 1182202SW ENTRANCE STEP CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 SURFACE RUST ON SHAFT AND CAP ON HOUSING FOR WIRING. HOUSING COVERED WITH DIRT. 1G72 4U H4SW 20030324000792003032400079CE 2003 3 24 AMWA8 120030212A5711 SPAR CAP BEECH 1900 1900D 1154162CE WING CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07182YV UE182 UPON A DETAILED INSPECTION MAINTENANCE FOUND THE ELECTRIC LINE CHAFING ON RIGHT FORWARD WING SPAR IN THE WHEEL WELL. BLENDED LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT IS REQUIRED. 2L72 4T RTA24CE 20030325000492003032500049 2003 3 25 AWXA200300198 420030220A256560592101 CONTROL CABLE AIRBUS320 A320232 3930326EU SLIDE BOTTLE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW286216585 770 DURING C-04 CHECK THE LT OVER WING ESCAPE SLIDE RESERVOIR BOTTLE FLEXIBLE CONTROL CABLE ASSEMBLY WAS FOUND TO HAVE A BROKEN END FITTING. MAINTENANCE REMOVED AND REPLACED THE LT OVER WING ESCAPE SLIDE RESERVOIR BOTTLE. 2L72 4F RTA28NM 20030307001362003030700136WP 2003 3 7 AALA20030108 120030124A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21562AA 49344 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACTS FOR TAIL CONE LIGHTS AND RECHARGED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030313001062003031300106CE 2003 3 13 C8F2003F00001 120030203A323050410012 BELLCRANK CESSNA402 402A 207590MCE CONT O520 TSIO520E 17040SO RT MLG INOPERATIVE E C8FAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP134576Q 402A0076 275118A AFTER TAKE OFF FROM HNL PILOT NOTICED DECREASING MANIFOLD PRESURE ON RIGHT ENGINE, AND DECIDED TO RETURN TO HNL. DURING LANDING APPROACH PILOT NOTICED AND UNSAFE RIGHT GEAR LIGHT, ATTEMPT WAS MADE TO RECYCLE LANDING GEAR BUT WAS UNSUCCESSFUL. HE THEN TRIED THE EMERGENCY HAND CRANK THAT ALSO FAILED TO CORRECT THE RIGHT MAIN LANDING GEAR UNSAFE PROBLEM. EMERGENCY PROCEDURES WERE CARRIED OUT AND UPON LANDING THE RIGHT MAIN LANDING GEAR COLLAPSED ON ROLL OUT. AIRCRAFT WAS THEN SECURED MY MAINTENANCE AND TOWED TO MAINTENANCE FACILITY, WERE IT WAS FOUND THAT THE RIGHT RETRACT BELLCRANK WAS FOUND TO CRACKED AND SEPARATED FROM THE REST OF THE ASSEMBLY. ALSO NOTICED THAT BOLT PN NAS 464P426 TO BE SHEARED AS WELL. 1L72 3O3 O A7CE E8CE 20030313001202003031300120SW 2003 3 13 FTU2003F00002 120030207A2913P366D PUMP GULSTM690TP 690B 7630516SW GARRTTTPE331TPE3315 01514WP THREADED WRONG MISMANUFACTURED B FTURO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NE0532BW 11545 WHEN PUMP WAS INSTALLED, IT WAS DISCOVERED THAT THE THREADS ON THE IN AND OUT PORTS WERE STRAIGHT THREAD. THE FITTINGS THAT ARE CALLED OUT IN THE IPC ARE PIPE THREAD, BECAUSE OF THE LIMITED SPACE AT THE PUMP MOUNTED POSITION. OVERHAUL PUMP WAS CHANGED AND THE WRONG TYPE INSTALLED. 1H72 3T4 T 2A4 E4WE 20030317000292003031700029NM 2003 3 17 03FDEA00162 120030218A5710ARB2850505 RIB DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING, FOUND TRACK NR 16 INBOARD STRUCTURAL RIB CRACKED. LT WING LEADING EDGE AND LEADING EDGE DEVICES, RIB INBOARD SLAT TRACK NR 16. SUPPORT FABRICATION CARRIED OUT IAW EA 1-5740-67574. CRACKED RIB REMOVED IAW SRM 51-31-01 VOL. II. AND REPLACED NEW FABRICATED RIB IAW SRM 51-31-01 VOL. II. 2L73 4F4 FRTA22WE E13NE 20030122000352003012200035SW 2003 1 22 HEEA083422 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000432003012200043SW 2003 1 22 HEEA083430 120030109A8000A1077 RELAY BELL 206 206L3 1182108SW STARTING SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 START RELAY WILL NOT DISENGAGE. 1G71 3U H2SW 20030122002142003012200214NM 2003 1 22 DL76G030055 120030113A33501000677 LIGHT BOEING767 7673P6 1385105NM COCKPIT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27154DL 25241 COCKPIT EMERGENCY LIGHTS INOP, EXIT SIGN ABOVE COCKPIT DOOR. REPLACED LIGHT ASSY. FOUND ON LAYOVER. 2L72 4F RTA1NM 20030317001022003031700102NM 2003 3 17 03FDEA00262 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 22R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030317001442003031700144NM 2003 3 17 03FDEA00308 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 CORROSION ON FRAME AT WL 208 BS 1166 RBL 65. 2L73 4F RTA3WE 20030318000292003031800029NE 2003 3 18 ERAA085147 120030213A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE DEBONDED H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01577EH2808 760222 WORN DOUBLER DEBONDING. R & R EXTERNAL DOUBLER, R & R FWD INT DOUBLERS AND REMOV AND REBONDED C CHANNEL REFINISH AND BALANCE. 1G72 3U H1NE 20030418001272003041800127EA 2003 4 18 SWIA200311783 120030211A274170607 INDICATOR CNDAIRCL600 CL6002B19 1900309EA MACH TRIM MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07588SW 7069 STAB TRIM/MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT IAW 27-41-00. NO DEFECTS NOTED AT THIS TIME. A/C RELEASE TO CAT II STATUS. S/N OFF: 540. 2L72 4F RTA21EA 20030731000472003073100047NM 2003 7 31 QXEA200300874 120030723A2434 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT ACTIVATED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09412QX 4059 SEA-ON FLIGHT NUMBER 2333, AFTER TAKEOFF, NR 1 DC GENERATOR CAUTION LIGHT. PERFORMED CHECKLIST. LIGHT STAYED OUT. RESET NR 1 DC GENERATOR. PERFORMED OPERATIONAL CHECK AND VISUAL CHECK OF NR 1 DC GENERATOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030801000352003080100035WP 2003 8 1 GTIA030509 120030613A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND MID PIT STATION 636-712 STRINGER 18L FLOOR WEB CORRODED. REMOVED FLOOR WEB FROM LEFT SIDE AT STATION 598-712. LOCATED AND DRILLED NEW WEB. INSTALLED NEW FLOOR WEB. (M) 2L72 4F A6WE 20030807000382003080700038NM 2003 8 7 C1HA200394010 120030603A2751 SWITCH BOEING727 727290 138408WNM TE FLAPS MALFUNCTIONED A C1HAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15294AS 22146 TAKEOFF ROLL GOT T/O WARNING HORN. ABORTED T/O, BEFORE RETURNING TO GATE CYCLED THE FLAPS AND RAN POWER UP, T/O WARNING HORN WENT AWAY. AFTER RETURNING TO GATE CYCLED FLAPS, NO TROUBLE FOUND. THE 5 DEG FLAP SWITCH CHANGED PRECAUTIONARY. 2L73 4F A3WE 20030724001002003072400100NM 2003 7 24 AWXA200300758 120030622A532065479573 WEB BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK CORROSION WAS FOUND AROUND 3 EACH FASTENER HOLES ON AFT CARGO DOORWAY LOWER WEB, AT AFT INBOARD CORNER BS 792, RBL 21, WL 157. MAINTENANCE REMOVED AND REPLACED AFT CARGO DOORWAY LOWER WEB BS 792, RBL 21 IAW B737-300 SRM 51-40-02 PG 5 & 42 FIG 10. 2L72 4F RTA16WE 20040301000152004030100015EU 2004 3 1 KBM2004F00012 120031126A6510593404 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R DRIVESHAFT WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH1166 2884 TAIL DRIVE SHAFT NR 5 BEARING, WORN. REMOVED AND REPLACED WITH NEW BEARING. (K) 1G71 3U3 U H9EU E19EU 20030829001832003082900183NM 2003 8 29 SWAA031794 120030809A55236959227 BUSHING BOEING737 7373A4 1384585NM ELEVATOR TABS WORN A SWAAK NONE E VIBRATION/BUFFET CLCLIMB 1 SW29676SW 23288 AIRFRAME VIBRATION ON CLIMB-OUT AND DESCENT, REMOVED AND REPLACED HARDWARE AND BUSHINGS ON BOTH LT AND RT ELEVATOR TAB ROD ENDS PER MM. 2L72 4F RTA16WE 20030724001262003072400126NM 2003 7 24 DLM88030574 120030623A25303750001117B COFFEEMAKER DOUG MD88 MD88 3023688NM FWD GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27907DL 49538 PRIOR TO LANDING ATTENDANTS REPORTED BURNING RUBBER ODOR IN FWD GALLEY/FC AREA. ATTENDANTS TURNED EVERYTHING OFF AND GALLEY POWER WAS REMOVED. JUST BEFORE LANDING SMOKE STARTED COMING FROM 1ST CLASS COFFEEMAKER, HALON FIRE EXTINGUISHER DISCHARGED. REPLACED COFFEEMAKER AND TRAY INSP AREA FOR ODOR OR BURNED/DAMAGED WIRING, NONE FOUND. CYL COFFEE POT, CHECK GOOD. OK FOR SERVICE. 2L72 4F RTA6WE 20030728000222003072800022NM 2003 7 28 SWAA031552 120030714A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728001272003072800127NM 2003 7 28 SWAA031431 120030629A3350702409 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 FWD ENTRY DOOR EMERGENCY EXIT LIGHT (JUST LEFT OF F/A SEAT) BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030903000332003090300033NM 2003 9 3 GH62003F00000 120030502A5610210807004 WINDOW PIPER PA60 PA60601P 7106012NM LYC O540 IO540S1A5 41532EA HARTZLHCC3Y HCC3YR2 NE COPILOT SIDE FAILED B GH6RO OTHER O OTHER NRNOT REPORTED 1 NM13663W 1488 62P929816505L1865048A 4044A WHILE CLIMBING OUT AFTER TAKEOFF, AT APPROX 20,000 FT, CO-PILOT WINDOW EXPERIENCED A CATASTROPHIC FAILURE. WINDOW SHARDS CONTACTED RT PROPELLER. PARTIALLY RIPPING HOT PROP BOOTS. PILOT RETURNED FOR INSPECTION AND REPAIR. CAUSE UNKNOWN/ SUSPECT CRACKS IN ATTACH AREA WHICH IS COVERED BY PRO-SEAL. INSPECT FOR CRACKS. (NM 02 FSDO INCIDENT NR 1NM 13200314) 1M72 3O3 ORTA17WE 1E4 5 CP25EA 20030903002722003090300272SO 2003 9 3 C2XA03SH273 120030817A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV DURING C CHECK APU FIREWALL CRACKED AT THE RIGHT HAND UPPER VERTICAL STIFFENER. MAITENANCE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030904001342003090400134NM 2003 9 4 DLM88030624 120030710A7711 O-RING DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE DETERIORATED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27914DE 49957 718177 RT EPR INDICATES HIGH ALL OTHER INDICATIONS NORMAL WITH THROTTLES ALLIGNED AT 15,000 FT 20 DEG TAT RT EPR IND 1.9 AND LT EPR IND 1.4. RAN ALT TEST OF ENGINE PRESSURE RATIO INDICATING SYSTEM PER AMM OPN CKS OK. FOUND O-RINGS ON NOSE BULLET PROBE IN POOR CONDITION REPLACED SAME. OK FOR SVC. 2L72 4F4 FRTA6WE E9NE 20030825000362003082500036WP 2003 8 25 UPS03840884 120030616A5712 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 LEFT WING LE UPPER RIB IS CRACKED AT XFS 741.25. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 57-2-0 FIG. 2 2L74 4F4 FRT4A25 E2GL 20030822001702003082200170WP 2003 8 22 UPS03841026 120030722A573038877762 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 RIGHT WING LOWER SKIN DOUBLER AT XW 408 IS CORRODED BEYOND LIMITS BETWEEN CENTER AND REAR SPAR. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 3887776 AND SRM 51-1-20D. 2L74 4F RT4A25 20030822000852003082200085NM 2003 8 22 03FDEA01307 120030807A5753 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 3A L2 LT WING -2 FB FLAP I2 FB HINGE FITTING 28 WING SIDE 29 FWD ATTACHMENT I2 FB BOLT HOLE FOUND CORROSION. LT WING - O/B FLAP I/B HINGE FITTING ( WING SIDE ) FWD ATTACHMENT I/B HOLE REPAIRED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030730000702003073000070WP 2003 7 30 ABXA030271 120030222A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME AT STA 243.5. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-21, 51-3-0, AND 51-1-20D. 2L74 4F 4A25 20030825000522003082500052NM 2003 8 25 UPS03641135 120030816A5420 PYLON BOEING767 76734AF 1385212NM LT PYLON DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01301UP 27239 INSPECTION TYPE:N/A FOUND HOLE IN PYLON LT ENG, .250 INCH HOLE. REMOVED CHANNEL & TWO CLIPS TO GAIN ACCESS TO WEB, NR SH39550. FAB'D NEW WEB & SPLICE PLATE. 2L72 4F RTA1NM 20030910001512003091000151NM 2003 9 10 UIEA200300046 120030817A215071923811 ACM BOEING747 747230B 1384889NM A/C BAY MALFUNCTIONED A UIEAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15512MC 21220 DIVERSION TO JFK, WHILE CLIMBING THROUGH FL350, CABIN ALT WENT OT 11,000 FEET. DIFF PRESSURE WAS 6.0. AT FL300, CABIN ALT WAS 10,400 FEET. DIFF PRESSURE WAS 6.0 AT FL290 DIFF PRESSURE WAS 6.2 CABIN ALT 7800 FEET. DIVERTED TO JFK. PRESSURIZED A/C ON GROUND, NO LEAKS. NOTED DMI M03-110 NR 1 PACK COMPLETELY LOCKED OUT. REACTIVATED AND CHANGED TO MEL 21-3-2-B. PACK TO BE OPERATED IN MANUAL IN FLIGHT ONLY WITH BYPASS IN FULL HEAT POSITION. REMOVED AND REPLACED NR 1 ACM IAW MM 21-51-04. OPS CHECK OK. (M) 2L74 4F A20WE 20030911000902003091100090WP 2003 9 11 DHL2003873565 120030704A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 AFT ACCY COMPT FORMER CRACKED 1.000 STA 640.000 BETWEEN L-26L AND L-27L. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030924000732003092400073NM 2003 9 24 2003UALA00631 120030805A5754114N300334 WEDGE BOEING BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29526UA A20314 24994 T/E WEDGE DELAMINATION MAJOR REPAIR ACCOMPLISHED.REPAIRED T/E WEDGE. 2L72 4F4 FRTA2NM E17NE 20030930000402003093000040NM 2003 9 30 2003UALA00659 120030830A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29368UA 24537 FWD RT DOOR CUT OUT FRAME IS CRACKED BELOW THE UPR STOP FITTING. MAJOR REPAIR ACCOMPLISHED, INSTALLED FRAME. 2L72 4F4 FRTA16WE E2GL 20031007000822003100700082NM 2003 10 7 SWAA031956 120030829A57546573714 SKIN BOEING737 7373L9 1384470NM NR 5 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C3 CHECK, FOUND NR 5 L/E SLAT CRACKED NEAR OUTBD END. REPAIRED NR 5 L/E SLAT PER SWA EA. 2L72 4F RTA16WE 20031028001322003102800132SO 2003 10 28 SIMA200324601 120030831A53471453369003 SEAT TRACK EMB 135 EMB135LR 3260305SO COCKPIT DIRTY A SIMAO OTHER O OTHER TOTAKEOFF 1 SW21738NR 145401 BGR - FLT 4622 - DURING TAKEOFF, THE FIRST OFFICERS SEAT SLIPPED LOOSE TO THE FULL AFT POSITION. MAINTENANCE FOUND THE OUTBOARD SEAT TRACK TO BE DIRTY. SEAT TRACKS WERE INSPECTED, SEAT TRACK PIS WERE REMOVED, CLEANED AND REINSTALLED IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031029000142003102900014NM 2003 10 29 ASAA0340110 120030301A5320 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON DOOR FRAME CLOSE OUT WEB AT BS 847 WL 156 AND RBL 24. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031029000952003102900095NE 2003 10 29 KBM2003F00010 220030711A75329550164960 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH2397 2884 BLEED VALVE DOES NOT REMAIN CLOSED. REMOVED AND BENCH TSTED AND LUBRICATED NO DEFECTS NOTICE AND INSTALLED SAME BLEED VALVE.(K) 1G71 3U3 U H9EU E19EU 20031110001962003111000196NM 2003 11 10 SWAA032241 120031010A53206517583 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED, WL 177, LBL 5.7. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031031000372003103100037NM 2003 10 31 UPS03441328 120030905A5311 FRAME BOEING747 747121 1384871NM MLG WW BLKHD CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WLG WHEEL WELL STA 1241 BULKHEAD UPPER SECTION AREA CORROSION REVEALED AT LBL 65, 70, 74 AND 90. UPPER SECTION REPAIRED AS PER RS 53-48-35072 REFER CWS FOR WORK DETAIL AND ENGINEERING FILE NO : 747-53-20158 DUE TO BLEND DEPTH 0.090 INCH X 2 INCHES X 3 INCHES AREA EXCEEDS SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F A20WE 20031103001302003110300130NM 2003 11 3 03FDEA01754 120031009A5753 FITTING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP I/B HINGE FITTING (WING SIDE) - LOWER I/B ATTACHMENT TO REAR SPAR, HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71748, WINGS - RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F4 FRTA22WE E13NE 20031112000552003111200055 2003 11 12 SWIA200312585 420031105A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07295UX8631 8631 120295 YAW ENGAGED, RUDDER TRIM AT 6, WHEN AUTO-PILOT ENGAGED, PLANE YAWED LEFT AND RIGHT HARD MOMENTARILY. REMOVED AND REPLACED F/O'S APC 65B IAW MM 22-10-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20031119000582003111900058WP 2003 11 19 DHL2003873012 120031011A5270 STRIKER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RT MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01873SJ 46091 AFTER DEPARTURE DOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED APPROPRIATE ABNORMAL PROCEDURE AND LIGHT WENT OUT AFTER CYCLING GEAR ONCE. PERFORMED BITE CHECK ON MAIN GEAR DOOR PROXIMITY BOX CHECKED GOOD, ADJUSTED RIGHT MAIN GEAR DOOR STRIKER. CYCLED SYSTEM SEVERAL TIMES. OPS CHECKED GOOD AT THIS TIME IAW DC-8 M/M 32-60-0. 2L74 4F4 FRT4A25 E2GL 20031112001112003111200111EU 2003 11 12 BAQA090690 120031013A28221176415103 PUMP BOLKMS117 BK117A3 5626015EU FUEL BOOSTER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LG94 7032 WILL NOT TRANSFER FUEL. THIS PUMP WAS ACCIDENTALLY SENT OUT FOR REPAIR REPLACED WITH SERVICEABLE, ASSET UNIT. 1G72 3U H13EU 20031117001032003111700103WP 2003 11 17 MWEA030409 120031007A531359364369 LONGERON DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 LONGERON 13 RIGHT AT STATION 1309 IS CRACKED AT UPPER AND LOWER FRAME ATTACH FASTENERS. REMOVED DAMAGED LONGERON SECTION. FABRICATED AND INSTALLED REPAIR SPLICE AND INSTALLED REPLACEMENT LONGERON SECTION. 2L72 4F4 F A6WE E2EA 20031121000772003112100077NM 2003 11 21 03FDEA01945 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 RIGHT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING ACTUATOR HOLE INBOARD CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, O/B HINGE FITTING ACTUATOR HOLE I/B CORROSION REMOVED AND REPLACED AS PER FEDEX EA 1-5740-74252 TITLE : WINGS - LT & RT O/B FLAP - O/B HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20031217000252003121700025EA 2003 12 17 COMA0360504 120031113A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01949CA 7080 RT 718 FRAME FLANGE CRACKED BELOW STRINGER 10. REPAIRED FRAME IN ACCORDANCE WITH REO 601R-53-61-193. 2L72 4F RTA21EA 20031219000372003121900037SO 2003 12 19 SWIA200312639 120031119A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07284YV7486 7486 120284 EMERGENCY LIGHTS WILL NOT TEST ROW 6 OVERHEAD; FLOOR BETWEEN ROW 3 AND 6. REMOVED AND REPLACED MIDDLE BATTERY PACK WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20031222000902003122200090NM 2003 12 22 USAA030237 120031030A5320 SILL BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 FOUND CHORD CORRODED 1 INCH BY 1 INCH, L1 DOOR LOWER SILL INBOARD CHORD, BS 331, LBL 58 CABIN FLOOR LEVEL. REMOVED SURFACE CORROSION FROM INBOARD CHORD, SUPPORT BEAM REPLACED WITH NEW PART IAW SRM 51-10-02. (M) 2L72 4F RTA2NM 20031222000272003122200027NM 2003 12 22 QXEA200301527 120031207A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PDX - NR 10 SEAT TRACK IS CORRODED BETWEEN X345 AND X348. REPAIRED IAW DHC-8 SRM 51-20-36. 2H72 4T RTA13NM 20030912001412003091200141NM 2003 9 12 AWXA200300899 120030809A3397ABS0374A24 WIRE HARNESS AIRBUSA319 A319132 3930340NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28830AW 1565 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT CABLE FROM SEAT TO WALL RECEPTACLE AT SEAT ROW 16 LT, OPERATIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20040105001462004010500146WP 2004 1 5 ABXA030483 120031212A533059114273 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 CRACK IN FUSELAGE SKIN AT STA 996 ABOVE LONGERON 16 LEFT. REPAIRED CRACK IAW DC-9 SRM 53-04. 2L72 4F A6WE 20031202000232003120200023WP 2003 12 2 ASAA0380498 120030617A33506011779 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040311000192004031100019NM 2004 3 11 ASAA0310099 120030306A533065516242 DOUBLER BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SKIN DOUBLER AT BS 987, STRINGER 23R-24R GOUGED AND DENTED. REMOVED AND REPLACED INTERNAL DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20031203000132003120300013NM 2003 12 3 GAIA03134ST 120031024A552165C376631 SPAR BOEING727 727243 138408DNM LT ELEVATOR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURNG C-CHECK INSPECTION FOUND LEFT ELEVATOR REAR SPAR CRACKED NEAR NR 3 HINGE FITTING. REF FASI N/R NR 61506, REPLACED LEFT ELEVATOR REAR SPAR IAW S/B 727-55-0089 REV 1. (M) 2L73 4F RTA3WE 20031202000982003120200098NM 2003 12 2 USAA030219 120031020A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US 23876 CLT - FOUND SKIN CRACKED 1 INCH, FS 727D JUST BELOW S23R. INSTALLED DOUBLER AND FILLER PER TR 53-60-03. (M) 2L72 4F RTA16WE 20031208000882003120800088SO 2003 12 8 CHQA000427 120031026A2751 WARNING LIGHT EMB 145 EMB145LR 3260212SO TE FLAPS FALSE INDICATIONA CHQAO OTHER N FALSE WARNING DEDESCENT 1 GL11266 145241 DURING DESCENT INTO PWM, RECEIVED A FLAP LOW SPEED INDICATION ON THE EICAS WITHOUT SELECTING THE FLAPS. SHORTLY THEREAFTER RECEIVED A FLAP FAIL/SPS ADVANCED WITH AN AMBER DASH IN THE FLAP INDICATION. COMPLETED QRH, DECLARED AN EMERGENCY WITH ATC, AND LANDED AT PWM SUCCESSFULLY. MAINTENANCE CHECKED AND RESET THE FLAP SYSTEM. NO DEFECTS WERE NOTED. 2L72 4T RTT00011AT 20031208001452003120800145NM 2003 12 8 2003UALA00800 120031021A5320 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 STA 663 AT STR 10L STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20031209001322003120900132NM 2003 12 9 QXEA200301345 120031008A5551 ATTACH FITTING DHAV DHC8 DHC8202 2809007NM ZONE 300 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 HORIZONTAL STAB RIGHT HAND FORWARD ATTACH FITTING HAS SCRATCH MARKS AND SMALL DRILL START ON OUTBOARD FACE OF LUB. REPAIRED IAW RD 8-55-847. 2H72 4T RTA13NM 20031209001922003120900192WP 2003 12 9 UPS03841493 120031026A53403755822502N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 350 BETWEEN LONG 35L AND 36 BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 51-1-20D. 2L74 4F RT4A25 20031015000062003101500006 2003 10 15 USAASA03103 420030831A2565C37103101 RELEASE CABLE AIRBUSA319 A319112 3930323EU GIRT BAR WRONG PART A USAAK NONE O OTHER ININSP/MAINT 1 EA19757UW 1342 THE FORWARD LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY ESCAPE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20030919001132003091900113EU 2003 9 19 AWXA200300924 120030803A5320D5397470700000 PROFILE AIRBUS320 A320232 3930326EU CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT CENTER PROFILE AT FR 58, STR 40 LT. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT CENTER PROFILE FR 58, STR 40 LT IAW A320 SRM 51-42-11, PG. 21-22, FIG. 8, AND PG. 7-10, & 12, FIG. 2 AND 3. 2L72 4F RTA28NM 20030923001952003092300195WP 2003 9 23 AALA20030896 120030824A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217508 49802 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK 135 AND 104. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040130000072004013000007NM 2004 1 30 SWAA032838 120031230A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 202, RT SIDE. REPAIRED FRAME BFG ER. 2L72 4F RTA16WE 20040130000862004013000086NM 2004 1 30 DHL2003742565 120031121A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, AFT CARGO FLOOR SUPPORT BENT STA 955E LBL12. REMOVED DAMAGED FLOOR SUPPORT STA 955E LBL 12 AND MADE NEW FROM BAC1500-6199.7075-T6 (68.5 X .75 X 1.25 X 1.25 X 1.25 X .75 INCH) PO 335824 AS PER SAMPLE IAW B727 SRM 53-10-2 FIG 8, PART TREATED AND PRIMED IAW B727 SRM 51-10-2. PART INSTALLED IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040130000182004013000018NM 2004 1 30 SWAA032811 120031224A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND CRACKED STR 6R AT BS 1011. REPAIRED DAMAGED AREA PER SRM. 2L72 4F RTA16WE 20040206000102004020600010EU 2004 2 6 KBM2003F00088 120031101A6420350A27119123 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 NR 1 AND NR 2 PUSH-PULL TUBE BEARING ARE WORN. REPLACED WITH 2 NEW BEARINGS. 1G71 3U3 UNCH9EU E19EU 20040204001802004020400180CE 2004 2 4 55631 120031028A3240 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG WEAK A AMWAO OTHER O OTHER LDLANDING 1 CE07133YV UE133 AFTER LANDING CAPT REPORTED BRAKES WEAK. MAINTENANCE BLED BRAKES. OPS CK NORMAL. (BLED BRAKES CAPT SIDE AND SERVICED RESERVOIR). 2L72 4T3 TRTA24CE E2NE 20040401000252004040100025NM 2004 4 1 AALA20031250 120031031A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21192AN 32386 MIA - DURING OVERNIGHT MANTENANCE, FOUND SEAT 18D EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTION. RECONNECTED SEAT 18D EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040308001412004030800141NM 2004 3 8 ASAA0310233 120030326A5320654963152 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SUPPORT ANGLE AT BODY STATION 520, STRINGER 19R-26R CORRODED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031217000862003121700086WP 2003 12 17 0302109945 120031030A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING M-CHECK FOUND CRACK IN SKIN AT NR 6 FORWARD STOP OF DOOR 1L. REPAIRED PER EA 99-196420. 2L72 4F A6WE 20031217000882003121700088WP 2003 12 17 ABXA030448 120031107A532099105035 WEB DOUG DC9 DC932 3022066WP AFT CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 CUSP WEB HAD 5 EACH CRACKS BETWEEN FS 945 AND 965. REMOVED AND REPLACED SECTION OF CUSP WEB IAW DC-9 SRM 51-30-2, 51-30-1 AND 50-01. 2L72 4F A6WE 20040316000292004031600029WP 2004 3 16 ASAA0380289 120030404A571099375887 SHEAR TIE DOUG DC9 DC982 3022082WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2 AND 30-5. (M) 2L72 4F A6WE 20040206000522004020600052WP 2004 2 6 ASAA0380767 120031121A53135936071503 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND LONGERON CORRODED AT FS 1218. REMOVED CORROSION. INSTALLED STRAP AND FILLER PER SRM 51-10-3 AND 53-02. (M) 2L72 4F RTA6WE 20040211000132004021100013WP 2004 2 11 GTIA031046 120031219A3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23833NK 49449 FLT 594 - MCO - NOSE GEAR UNLOCK LIGHT ON INTERMIT DURING CLIMB. CHECKED RESISTANCE VALUES ON THE OVERCENTER AND UP POSITION SENSORS. CHECKS OK. ADJUSTED GAP ON NOSE GEAR UP/DOWN AND LOCKED POSITION PROXIMITY SENSOR. PERFORMED NOSE GEAR RETRACT CHECK AND FOUND OK. (M) 2L72 4F RTA6WE 20031210001552003121000155WP 2003 12 10 AALA20031356 120031130A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21570AA 49352 BOS LT AFT STAIRWELL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AFT STAIRWELL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA6WE 20031212001172003121200117NM 2003 12 12 SWAA032452 120031106A52106545877 STRUCTURE BOEING737 7373H4 1384600NM ENTRY DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR FWD LOWER CORNER CUTOUT CRACKED 2.0 IN. REPAIRED PER EA. 2L72 4F RTA16WE 20031215001242003121500124WP 2003 12 15 AALA20030959 120030904A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21495AA 49733 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE COMMON TO BATTERY B5-107. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215001942003121500194EU 2003 12 15 USAA030257 120031101A5315D5347209000400 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW 0885 FOUND BEAM CORRODED 3 CM BY 2.2 CM CORRODED THROUGH STRUCTURE, FRAME 66 AT LAV'S AFT INBOARD ATTACHMENT + Y80 CM. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-42-11 AND 51-72-11. CORROSION LEVEL 1, TASK NR JA-160-53500. (M) 2L72 4F RTA28NM 20031212000432003121200043NM 2003 12 12 CALA0300643 120031114A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND HAT CHANNEL FOR ANTENNA CORRODED AT STA 727D +12, S27L. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030819001872003081900187 2003 8 19 SWAA031782 420030809A2565D31354 SLIDE BOEING737 7377H4 1384404NM FWD ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030820001132003082000113NM 2003 8 20 UPS03240995 120030716A5754 SKIN BOEING727 72725C 138400HNM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, NR 3 SLAT OUTER SKIN CRACKED ADJACENT TO I/B HOOK ATTACH POINT. HFEC INSP CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT CRACK CONFIRMED & END MARKED. REPAIR CARRIED OUT IAW SRM 51-10-1, 57-50-3 & 51-30-3. 2L73 4F A3WE 20030820001202003082000120NM 2003 8 20 2003UALA00532 120030701A2163 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE AIR TEMP SENSOR ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29198UA 28716 RETURNED TO FIELD DUE TO TOTAL AIR TEMPERATURE SENSOR MESSAGE. REPLACED CURRENT SENSING RELAY R7430. NO PROBLEMS NOTED SINCE REPLACEMENT OF RELAY. 2L74 4F4 FRTA20WE E24NE 20030820002032003082000203EU 2003 8 20 ASOA03331 120030720A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A GROUND INSPECTION IN VPS, THE EMERGENCY LIGHT AT ROW 13 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AT ROW 13. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030328000692003032800069NM 2003 3 28 CALA0300135 120030321A5320 SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912313 23364 INSPECTION FOUND LT AFT LAV FORWARD WALL SUPPORT HAT SECTION CORRODED AT NUT PLATES. INSTALLED A NEW SECTION OF WALL SUPPORT HAT SECTION IAW SRM 51-40-01. 2L72 4F RTA16WE 20030401000402003040100040SO 2003 4 1 C2XA03BT045 120030328A323414532170401 LEVER EMB 145 EMB145 3260210SO MLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2727962 145110 CREW REPORTED "AFTER TAKEOFF FROM PHL ENROUTE TO CLE, LANDING GEAR WOULD NOT RETRACT. HANDLE WORKED FINE. (DIVERTED TO EWR, LANDED UNEVENTFULLY) POST FLIGHT INSPECTION REVEALED NO GEAR PINS IN LANDING GEAR." AIRCRAFT MAINTENANCE FERRIED TO BTV GEAR DOWN, MAINTENANCE REMOVED AND REPLACED LT NR 2 MAIN LANDING GEAR PROXIMITY SWITCH IAW EMB145 AMM, REMOVED AND REPLACED LGEU IAW EMB145 AMM AND REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM. OPS. CHECKED LANDING GEAR GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030820002432003082000243EA 2003 8 20 ASOA03313 120030715A5330601R35004311 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE LEFT AND RIGHT SIDE INTERNAL DOUBLER AT FS 640 BETWEEN STRINGERS 10 L/R AND 11 L/R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT SIDE INTERNAL DOBLER AT FS 640 BETEEN STRINGERS 10 L/R AND 11 L/R IAW ASA EO 600-53-0107 AND ASA EO 600-53-0109. (M) 2L72 4F RTA21EA 20030820001332003082000133NM 2003 8 20 CALA0300433 120030619A5511 SPAR BOEING737 7373T0 1384582NM HORIZONTAL STAB DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 AN EXISTING REPAIR ON THE RT HORIZONTAL STABILIZER FRONT SPAR NEEDED TO BE REPLACED. THE EXISTING REPAIR WAS LOCATED AT STAB STA 245 ON THE FORWARD FLANGES OF THE UPPER AND LOWER CHORDS. THE SPAR CHORDS WERE REPAIRED IAW ECRA 5510-01682. 2L72 4F RTA16WE 20030625001232003062500123NM 2003 6 25 AWXA200300327 120030328A2730S251N2062 ACTUATOR BOEING757 757225 1384959NM ELEVATOR WORN A AWXAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 WP28913AW17255 22207 DURING CLIMBOUT FL 200 RECEIVED EICAS STATUS ELEV ASYM, TURNED BACK. ON SHORT FINAL AT POWER REDUCTION FOR LANDING (10 FT ABOVE GROUND LVL), VIOLENT CONTROL COLUMN SHAKING OCCURRED (NOT STICK SHAKER). MX TROUBLESHOT & FOUND FAULT BALL FOR ELEV ASYM LIMIT ACTUATOR TRIPPED ON RT ELEV ASYM LIMIT MODULE. RESET MODULE & PERFORMED BITE CHECK ON LT & RT ELEV ASYM MODULES. BITE CHECK GOOD. PERFORMED ELEVATOR CONTROL SYSTEM TEST PER T/C F1B27623, TEST WAS GOOD. PERFORMED ELEV TEST WITH EACH INDIVIDUAL HYD SYS, NO FAULTS NOTED. AS PRECAUTION REPLACED ELEV ASYM ACTUATOR, OPS CHECK GOOD. *S/D* VENDOR TEARDOWN OF ELEV ASYM LINEAR ACTUATOR S/N 194 ONLY FOUND INDICATION OF NORMAL WEAR. UNIT REPAIRED & TESTED. 2L72 4F RTA2NM 20030403000362003040300036EU 2003 4 3 46831 120030402A2422 WARNING LIGHT SAAB SF340 SF340A 7850100EU MAIN INVERTER ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17108CQ 340A108 FLIGHT 4536 PIT-HGR. JUST AFTER TAKE-OFF FROM PIT DURING CLIMB THE MAIN INVERTER FAIL LIGHT ILLUMINATED. CREW FOLLOWED QRH AND SWITCHED TO THE STANDBY INVERTER. TRANSFER WAS GOOD WITH NO SYSTEM FAILS. A/C TURNED AROUND AND RETURNED TO GATE AT PIT. A/C WAS TAKEN OUT OF SERVICE. 2L72 4T RTA52EU 20030821002352003082100235NM 2003 8 21 QXEA200300917 120030724A2520 PANEL DHAV DHC8 DHC8202 2809007NM CABIN CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- FLIGHT ATTENDANT SEAT SUPPORT SHEAR PANEL ATTACHED TO OUTBOARD SIDE OF NR 4 SEAT TRACK IS CORRODED AND CRACKED AT AFT END. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20030401000082003040100008EA 2003 4 1 03090647 120030331A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27647BR 7399 DURING MAINTENANCE INSPECTION, AN EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030402000342003040200034NM 2003 4 2 2003UALA00309 120030323A3230 SWITCH BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29310UA 23671 AIRCRAFT RETURNED TO FIELD WHEN THE LANDING GEAR FAILED TO RETRACT. A FAILED S106 LANDING GEAR SAFETY SWITCH CAUSED THE AIRCRAFT TO REMAIN IN THE GROUND MODE, RESULTING IN THE GEAR FAILING TO RETRACT. THE S106 LANDING GEAR SAFETY SWITCH WAS REPLACED AND THE LANDING GEAR EXTENDED AND RETRACTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20030404000012003040400001NM 2003 4 4 372PA0017 120030324A335094145 LIGHT BOEING737 737306 13844BGNM CABIN INOPERATIVE A PIDAO OTHER L NO TEST NRNOT REPORTED 1 SO05372PA 23546 EMERGENCY FLOOR LIGHTING INOP FROM 21 AFT. REPLACED AFT SECTION EMERGENCY LITE STRIP PER MM 25-61-01. OPS CHECK OK. 2L72 4F RTA16NE 20030401001362003040100136SO 2003 4 1 CMI2003F00000 220030320A7313641482 B-NUT CESSNA421 421C 2076016CE CONT O520 GTSIO520* 17032SO FUEL INJECTOR UNDERTORQUED G CMIAO OTHER RF PARTIAL RPM/PWR LOSS FLT CONT AFFECTED NRNOT REPORTED 1 NM078430N 421C0490 NR 2 ENGINE STARTED RUNNING ROUGH. PILOT LANDED AND HAD PROBLEM CHECKED. NR 5 CLYINDER FUEL INJECTOR LWE B-NUT WAS LOOSE ON INJECTOR DUE TO IMPROPER TORQUE DURNING MAINTENANCE. 1L72 3O3 O A7CE E7CE 20030410001582003041000158NM 2003 4 10 SWAA030712 120030329A3350604222 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED C1 CHECK, BOTH FWD AND AFT GALLEY EMERGENCY LIGHT BATTERY PACKS FAILED, OPS CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20030425000712003042500071EU 2003 4 25 MALA030212 120030318A2435 STARTER GEN SAAB SF340 340B 7860101EU RIGHT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15449XJ 340B449 DURING FLIGHT 2902, LT DC GEN CAUTION LIGHT ILLUMINATED. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RT STARTER/GEN AND LT DC GCU. 2L72 4T RTA52EU 20030429000372003042900037WP 2003 4 29 03FDEA00199 120030303A2780ARH7024615 CONTROL CABLE DOUG DC10 DC1010 3022110WP NR 7 SLAT BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 AT MOBILE AEROSPACE ENGINEERING (VENDOR) BFM FOUND DURING C-CHECK INSPECTION THE NR 7 SLAT EXTEND CABLE LT WING, UNRAVELED, ALL STRANDS BROKEN EXCEPT FOR ONE. REMOVED AND REPLACED NR 7 SLAT EXTEND CABLE. TENSIONED LT NR 7 SLAT AND EXTEND RETRACT CABLE, AND OPS CHECKED GOOD, ALL IAW MM 27-80-00-5. 2L73 4F A22WE 20030429001002003042900100WP 2003 4 29 ZW0A0304201 120030409A3350408822101 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139405T 53141 THE EGRESS LIGHTS WERE INOPERATIVE IN THE FIRST CLASS SECTION AND FROM ROW 14 THRU 20. REPLACED THE BATTERIES IN THE BATTERY PACK FOR FIRST CLASS AND FOR ROW 14 THRU 20. CHECK-C 10-19-2002 STL. 2L72 4F RTA6WE 20030430001762003043000176NM 2003 4 30 SWAA030903 120030422A29106544546 LINE BOEING737 7373G7 1384595NM HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29671SW 23785 AIR TURNBACK. LOST A-SYSTEM HYDRAULICS. FOUND, HYD LINE LEAKING AT RT MLG ACTUATOR UPSIDE. REMOVED AND REPLACED HYD LINE FOR RT MLG ACTUATOR PER MM. 2L72 4F RTA16WE 20030502002082003050200208NM 2003 5 2 UPS03M40443 120030315A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE:C SEAT TRACK AT RBL 27.5 BETWEEN STA 1264-1273 FOUND CORRODED. CORROSION REMOVED AT SEAT TARCK STA 1264-1273 RBL 27.5 & FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I & 51-21-01 VOL II REV 32. NEW SEAT TRACK REWORKED & HOLES PICKED OUT AS PER SRM 53-70-00 VOL I REV 32, NEW SEAT TRACK PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 VOL I REV 32 AT STA 1364-1273 RBL 27.5. 2L73 4F RTA22WE 20030505000892003050500089NM 2003 5 5 03FDEA00502 120030417A5330 PANEL BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 CABIN BS 1176.9 LEFT SIDE GILLINER CLOSE OUT CRACKED. REPAIRED CLOSEOUT IAW FED EX SRZ 25-016A. 2L73 4F RTA3WE 20030506001142003050600114EA 2003 5 6 COMA0360209 120030421A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR INOPERATIVE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01977CA 7157 FLIGHT 51231 SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. REPLACED POWER STRIP. 2L72 4F RTA21EA 20040614001632004061400163EU 2004 6 14 RYN2004F00025 120030916A2612350F51000 CONTROL PANEL AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE E/E BAY FAULTY A RYNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07391LF 676 AFTER TAKE OFF FROM ATL, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED WITH NO ECAM MESSAGE. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ANNUNCIATOR LIGHT TEST AND INTERFACE BOARD. OPERATIONAL CHECKED NORMAL. NO FAULTS NOTED. 2L72 4F4 FRTA28NM E311NE 20030926001092003092600109NM 2003 9 26 2003UALA00642 120030822A5330 SKIN BOEING747 747422 1384935NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29197UA 26901 EXTERNAL SKIN STA 2215 NEAR STR 31L IS DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR. 2L74 4F4 FRTA20WE E46NE 20030926001462003092600146EU 2003 9 26 AWXA200301007 120030901A5411D5453003220000 RIB AIRBUS320 A320231 3930325EU NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-03 CHECK A 1.5 INCH CRACK WAS FOUND ON NR 1 PYLON LOWER AFT FIXED FAIRING RIB 14. MAINTENANCE REMOVED CRACKED NR 1 PYLON LOWER AFT FIXED FAIRING RIB; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-12, 10, 12, AND 22, FIG 2, 3, &. 8, AND SRM 51-44-11, PG. 1 AND 4, FIG. 1. 2L72 4F RTA28NM 20041201001522004120100152EA 2004 12 1 MASA200300521 120031230A2612 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA MALFUNCTIONED A MASAK NONE N FALSE WARNING ININSP/MAINT 1 SW07510MJ 10101 FIRE SYSTEM FAULT MSG. MX PLACED ON MEL. 2L72 4F RTA21EA 20030815000822003081500082SW 2003 8 15 HEEA088584 120030725A7714412075008111 INDICATOR BELL 412 412 1182202SW TORQUE CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 MOISTURE INSIDE TORQUE INDICATOR FACE. SHOP REPAIR. 1G72 4U H4SW 20030328000062003032800006EA 2003 3 28 CA030213001 120030208A792128E997 OIL COOLER DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE ENGINE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN) NR 1 ENGINE OIL COOLER FOUND LEAKING FROM LOWER COOLING FINS. OIL COOLER REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030821000572003082100057NM 2003 8 21 03FDEA00836 120030523A5753ARC0502506 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP-HINGE FWD FITTING FOUND OUTBOARD ACTUATOR BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER CMM 57-44-08 AND FEDEX EA 1-5740-68424 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030821001682003082100168NM 2003 8 21 03FDEA01030 120030703A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 FRAME DENTED BS 520 STR 22R TO 24R. REPAIRED FRAME BS 520, STR 22R TO 24R PER SRM 51-40-03. 2L73 4F RTA3WE 20030404000202003040400020NM 2003 4 4 DHL2003726002 120030404A5347 SEAT TRACK BOEING727 727228 1384083NM COCKPIT DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01726DH 20409 S/O'S SEAT WILL NOT LOCK INTO RAIL FOR SIDEWAY MOVEMENT. CLEANED AND LUBRICATED SEAT RAILS AND LOCKING MECHANISM PER M/M 2510. OPS NORMAL. 2L73 4F RTA3WE 20030331000542003033100054WP 2003 3 31 AALA20030245 120030225A2163 GASKET DOUG DC9 DC982 3022082WP TEMP SENSOR FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21242AA 49255 EN ROUTE MIA-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. PERFORMED PROCEDURE, LIGHT DID NOT EXTINGUISH AFTER 2 MINUTES. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED LEFT PNEUMATIC SUPPLY TEMPERATURE SENSOR GASKET BROKEN. PRESSURIZED PNEUMATIC DUCTS, NO FURTHER LEAKS NOTED. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030403000372003040300037NM 2003 4 3 AMTA200300252 120030222A335020121 LIGHT BOEING757 75723N 1384973NM DOOR SLIDE INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 L2 EXTERIOR EMERGENCY DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER IAW MM 33-51-07, OK FOR SERVICE. (M) 2L72 4F RTA2NM 20030408000182003040800018WP 2003 4 8 ASAA0380106 120030125A5330591022832Y SKIN DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OAK - DURING C-CHECK, FOUND FUSELAGE SKIN CREASED/GOUGED AT FS 1485-1497. BLENDED CREASED/GOUGED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F A6WE 20030328000772003032800077NM 2003 3 28 CH1A200393006 120030323A3350 LIGHT BOEING727 727212 138407GNM EMERGENCY EXIT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15293AS 21348 FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE 2L73 4F A3WE 20030407000042003040700004NM 2003 4 7 ASAA0310004 120030109A33508621004 BATTERY BOEING737 7372X6C 1384552NM FWD CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - FORWARD EMERGENCY SLIDE EXIT LIGHT ILLUMINATED. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHT TESTED NORMAL. (M) 2L72 4F RTA16WE 20030410000572003041000057NM 2003 4 10 SWAA030640 120030320A552065C27351 HINGE FITTING BOEING737 7373H4 1384600NM LT & RT ELEVATORCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND BOTH LT/RT ELEVATOR NR 6 HINGE FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT/RT NR 6 HINGE FITTINGS PER SRM AND SWA ACO. 2L72 4F RTA16WE 20030417000782003041700078NM 2003 4 17 P5CA0300746 120030126A5414 CAP BOEING747 747200 1384847NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 NR 4 PYLON WING KNEE-PAD (NU-CAP) PANEL TRAILING EDGE FASTENER HOLE BROKEN OUT. REPAIRED AND FILLED AREA, RE-DRILLED HOLE AND PROTECTED IAW SRM 51-40-00. 2L74 4F RTA20WE 20030424001702003042400170SO 2003 4 24 LR7A03025 120030313A5320 PLATE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 CHECK INSPECTION PER JOB CARD HC5315 FOUND RT FS 858 SUPPORT PLATE CRACKED AT RBL 65, WL 180. PLATE REPLACED IAW SRM SMP 583 51-60 AND 51-70. NR 2160. 2H74 4T A1SO 20030429000812003042900081NM 2003 4 29 P5CA0300827 120030410A5320 INTERCOSTAL BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 BODY GEAR W/W STA 1394 - STA 1416 1 INCH CRACK INTERCOSTAL AT LONGERON BOX. REPAIR PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20030429001382003042900138NM 2003 4 29 AUS20030291 120030212A5315 FLOORBEAM BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AFT CARGO FLOORBEAM ANGLE CONTAINED LEVEL 2 CORROSION IN AREALOCATED AT BS 1166 ABOVE STRINGER 27L BETWEEN BL16L AND BL23L. FOUND DURING INSPECTION IAW CPCP C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030430002212003043000221SO 2003 4 30 SWIA200311917 120030425A213122201T011400 CONTROLLER EMB 120 EMB120ER 3260203SO CABIN PRESSURE MALFUNCTIONED A SWIAG O2 MASK DEPLOYED P NO WARNING INDICATION CLCLIMB 1 NM07236SW4382 2124 120312 PAX 02 MASKS DEPLOYED IN FLIGHT CLIMBING THROUGH 8,000 FEET. NOTICED DELTA-P WAS AT 7,000 FT AND THE CABIN WAS LESS THAN ZERO. REMOVED AND REPLACED ALTITUDE CONTROLLER IAW MM 21-30-01. OPS CHECK GOOD, NO DEFECTS NOTED. 2L72 4T RTA31SO 20030430002652003043000265NM 2003 4 30 SWAA030826 120030413A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29762SW 27876 EEPLS COVER LOOSE AT ROW NR 1 ABC. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030505000732003050500073 2003 5 5 SWAA030871 420030419A2565D31354 SLIDE BOEING737 7373Q8 1384670NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030514002082003051400208NM 2003 5 14 03FDEA00722 120030430A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE WING SIDE LINK ATTACHMENT HOLE LOCATION QTY 2 EACH CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69243 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH & RH OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030602000132003060200013SO 2003 6 2 ASOA03192 120030501A33503071BPE BULB EMB 120 EMB120RT 3260202SO CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11264AS 120165 DURING A GROUND INSPECTION IN ATL, THE RIGHT EMERGENCY EXIT LIGHT AT ROW 8 B/C WAS FOND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EMERGENCY EXIT LIGHT LAMP AT ROW 8 B/C. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030604000082003060400008NM 2003 6 4 AALA20030475 120030420A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21776AN 29582 DURING OVERNIGHT MAINTENANCE, MID-GALLEY WALL MOUNTED EMERGENCY EXIT LIGHT AT 2R DOOR INOPERATIVE. REPLACED MID-GALLEY WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT 2R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030604001692003060400169NM 2003 6 4 UPS03440589 120030412A575365B078701 RIB BOEING747 747121 1384871NM NR 7 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING - NR 7 VC FLAP O/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLE BORE AREA FOUND CORROSION AT HOLE NR 4 ( VIEW FROM I/B). BOLTS HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030605001572003060500157GL 2003 6 5 BAQA086321 220030502A7320 ADJUSTER AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20F 03013GL FUEL CONTROL LOOSE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911TM705 336443 5059 ENGINE N1 IDLE ADJUSTMENT SCREW HAS FREE MOVEMENT EITHER RIGHT HAND OR LEFT HAND. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H11EU E4CE 20030611000512003061100051NM 2003 6 11 CA030428010 120030428A792128E997 OIL COOLER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 1 ENGINE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA 19776 (CAN) DURING SCHEDULED MAINTENANCE, NR 1 ENGINE OIL COOLER WAS FOUND LEAKING. OIL COOLER REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030612000902003061200090NM 2003 6 12 UPS03M40720 120030403A5350 SKIN DOUG MD11 MD11 3023602NM ZONE 316 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE: C, AFT ACCESSORY COMPT ZONE 316 RT FAIRING ATTACHMENT ANCHOR NUT SKIN FOUND CORRODED. RT FAIRING ATTACHMENT ANCHOR NUT SKIN REMOVED AND FOUND OUT OF LIMIT PER SRM 53-00-01 VOL I REV 32. CORROSION BLEND OUT AREA TRIMMED PER EN:10 06-03. HFEC INSP CARRIED OUT PER NDT SPM REV 10 06-10-01-001 & NO CRACKS EVIDENT. FABRICATED REPAIR PARTS, PROTECTED AND INSTALLED AS PER EN: 1006-03. 2L73 4F RTA22WE 20030612001802003061200180SO 2003 6 12 C2XA03TY084 120030602A532014522460015 GUSSET EMB 145 EMB145LR 3260212SO GALLEY SUPPORT CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING A SCHEDULED INSPECTION THE AFT GUSSET IN THE GALLEY WAS FOUND CORRODED AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030506002092003050600209WP 2003 5 6 ASAA0380235 120030307A53102929169 ANGLE DOUG DC9 DC982 3022082WP GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR ESCAPE SLIDE GIRT BAR FITTING FORWARD MOUTN ATTACH ANGLE. REPLACED ATTACH ANGLE PER SRM. (M) 2L72 4F A6WE 20030513002602003051300260EU 2003 5 13 ASOA03148 120030405A33503011210 LIGHT AEROSPATR72 ATR72 EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030513002662003051300266EU 2003 5 13 A6WA200360017 120030423A5730 PANEL BAC 146 146200A 1500266EU LT WING LE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LT WING LEADING EDGE PANEL 464AT HAS SEVERAL ELONGATED HOLES. REPAIRED IAW RIL HC5459009 AND FAX BARA/AVR/6365/03-DC. 2H74 4F A49EU 20030514000092003051400009EA 2003 5 14 ASOA03147 120030402A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GALLEY DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11874AS 7551 DURING DESCENT INTO ATL FROM FLO, THE FLIGHT ATTENDANT NOTICED A STRANGE ODOR IN THE GALLEY SIMILAR TO A MATCH STRIKE WHICH ALSO OCCURRED IN THE COCKPIT AND DISSIPATED ALMOST IMMEDIATELY AFTERWARDS. THE FLIGHT ATTENDANT MADE AN INSPECTION OF THE CABIN BUT COULD NOT LOCATE THE ORGIN OF THE ODOR. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE THE ODOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030513002752003051300275WP 2003 5 13 AALA20030216 120030204A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE PUNCTURED A AALAK NONE O OTHER ININSP/MAINT 1 SW21574AA 53151 SCREW PUNCHED HOLE IN CUSP. CLEAN DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01-00 FIG 4 SH 3. (M) 2L72 4F A6WE 20030514000812003051400081 2003 5 14 SWAA030982 420030502A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030529000852003052900085SW 2003 5 29 HEEA086659 120030521A6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 TAIL ROTOR HAS WORN BUSHINGS. REPAIRED. 1G72 4U H4SW 20030530000882003053000088CE 2003 5 30 050516 120030507A6100 SOLENOID BEECH 1900 1900D 1154162CE RT ENGINE STUCK A AMWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CE07171ZV UE171 ON FLIGHT 5534 UPON THE TAKEOFF ROLL THE RIGHT ENGINE WOULD ONLY GO TO 1550 RPM. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LOW PITCH SOLENOID TO BE STUCK. MAINTENANCE CLEANED AND LUBED THE SOLENOID. 2L72 4T RTA24CE 20030605000702003060500070 2003 6 5 ABXA030141 420030506A2211 COMPUTER DOUG DC9 DC941 302207NWP AUTOPILOT MALFUNCTIONED A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23970AX 47494 WITH AUTOPILOT ON DURING TURNS, THERE WAS EXTREME AND EXCESSIVE UNCOMMANDED ELEVATOR INPUTS. VERIFIED. RERACKED PITCH AND ROLL COMPUTERS. VERSINE LIFT CHECKED GOOD IAW DC-9 AMM CHAPTER 22. 2L72 4F A6WE 20030609000092003060900009EA 2003 6 9 SWIA200311976 120030518A3231 MECHANISM CNDAIRCL600 CL6002B19 1900309EA NLG DOOR DAMAGED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07405SW 7029 HYDRAULIC SYSTEM NR 3 PRESSURE BLEEDS OFF ALLOWING THE NOSE DOOR TO OPEN IN FLIGHT. REMOVED AND REPLACED RIGHT NOSE LANDING GEAR ''DOOR OPERATION MECHANISM'' PIVOT BOLT FOR CAM ROLLER. ALSO CLEANED AND LUBED ASSOCIATED HARDWARE. OPERATIONAL CHECKS GOOD IAW 32-22-15. REMOVED AND REPLACED NOSE DOOR MANUAL BYPASS VALVE IAW CRJ MM 32-34-40. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR IAW CRJ MM 32-34-00, 32-30-00. OPS CHECK GOOD AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20030611000552003061100055GL 2003 6 11 CA030430006 220030413A732123065104 FUEL CONTROL BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) 1ST START ATTEMPT FAILED TO LIGHT OFF. 2ND START ATTEMPT DELAYED LIGHT OFF. HUNG START AT 50 PERCENT N1, COULD NOT GET ABOVE 98 PERCENT. SHUT DOWN ENGINE - CHANGED FUEL CONTROL UNIT. 1G71 3U3 U H2SW E4CE 20030617002782003061700278SW 2003 6 17 HEEA087033 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH1412 53283 MAIN ROTOR DRIVE UNIVERSAL WORN. 1G71 3U O H2SW 20030613001422003061300142NM 2003 6 13 SWAA031223 120030602A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS PANEL CRACKED AT BS 664, LBL 36. REPAIRED PRESS WEB PER SWA EA. 2L72 4F RTA16WE 20030523000792003052300079 2003 5 23 SWAA031107 420030515A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030523000602003052300060NM 2003 5 23 SWAA031121 120030519A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, BETWEEN STR 18R AND STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030613000682003061300068SO 2003 6 13 C2XA03BT065 120030605A2150 COOLING TURBINE EMB 145 EMB145LR 3260212SO NR 2 ODOR A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2716954 145072 CREW REPORTED, NR 2 AIR CONDITIONING PACK PRODUCES SMOKE AND BURNING ODOR AFTER A FEW MINUTES OF OPERATION. MAINTENANCE INSPECTED AND PLACED SYSTEM ON MEL, AIRCRAFT RELEASED IAW MEL 21-51-00, UNDER PLACARD NUMBER 024810. AIRCRAFT RETURNED ON FLIGHT 2433 LATER IN THE DAY AND MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE NR 2 AIR CONDITIONING PACK COOLING SYSTEM IAW EMB145 AMM 21-50-00. OPS CHECKED GOOD, NO SMOKE OR BURNING ODOR NOTED. MEL CLEARED AND AIRCRAFT RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030612001852003061200185NE 2003 6 12 2003UALA00446 220030527A7261 ENGINE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE NR 2 MALFUNCTIONED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29673UA 29241 NR 2 ENGINE SHUTDOWN DUE TO OIL QUANTITY AND OIL PRESSURE. FOUND THE NR 3 OIL SCAVENGE CHIP DETECTOR WORN THRU THE HOUSING CAUSING THE PROPE TO FALL PARTIALLY OUT OF THE HOUSING LEAVING THE CHECK VALVE OPEN. THE PROPE WAS SAFETY WIRED TO THE ADJACENT PROPE AND WAS NOT ABLE TO ALLOW THE CHECK VALVE TO FUNCTION CORRECTLY. REMOVED THE SAFETY WIRE AND ALLOW THE PROPE AND HOUSING TO WORK AS INTENDED. THERE IS A CHECK OF THE HOUSING IN THE MM FOR THE WEAR. 2L72 4F4 FRTA1NM E24NE 20030522000832003052200083WP 2003 5 22 GTIA030302 120030421A5330 PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 RIGHT OUTBOARD LOWER WEDGE PANEL UPPER SIDE HAS DENT/ GOUGE. CUT OUT DAMAGED SKIN. FABRICATED REPAIR DOUBLER. MATERIAL SUBSTITUATION FOR FILLER AND DOUBLER FROM 2014T6 TO 7075T6. INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA6WE E2EA 20030521000152003052100015WP 2003 5 21 DHL2003801063 120030408A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 410.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS 410.250 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBER ANGLE WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001362003052100136WP 2003 5 21 DHL2003801037 120030408A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING- LT INBOARD STUB WING UPPER SKIN CRACKED 5.000 INCHES AT STA XS 250.000. REMOVED DAMAGED LT INBOARD STUB WING UPPER SKIN IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. FABRICATED NEW SKIN (7075-T6 AL0.063) IAW SRM 57-7-3 PG 11. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030618001092003061800109SW 2003 6 18 HEEA087497 120030612A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 BLOWER ASSY FWD BEARING ROUGH. REPLACED. 1G71 3U O H2SW 20030619000142003061900014SW 2003 6 19 AC2A086764 120030528A3150 WARNING LIGHT BELL 430 430 1182150SW ALLSN 250C 250C* GL COCKPIT ILLUMINATED E AC2AO OTHER J WARNING INDICATION CRCRUISE 1 SO07430CH 49037 ECU LIGHT AND AUDIO FOR NR 1 ENGINE CAME ON IN FLIGHT. PILOT FOLLWED PROCEDURES CHECKLIST. TRANSITIONED NR 1 FADEC TO MANUAL MODE. LANDED WITHOUT FURTHER PROBLEMS. MECHANIC FOUND NR1 ENGINE N1 FAULT CODE CAUSED LIGHT TO ILLUMINATE. MECHANIC FOLLOWED FAULT ISOLATION MANUAL. WIRING AND CONNECTIONS WERE CHECKED AND FAULTS WERE CLEARED. AIRCRAFT WAS GROUND RUN AND FLOWN WITH NO FURTHER FAULTS. CAUSE OF PROBLEM NOT KNOWN. 1G72 3U3 URTH9SW E4CE 20030630000412003063000041EU 2003 6 30 AWXA200300617 120030502A5320D5397470600400 PROFILE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 53, STR 38 L/H TO STR 38 R/H. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 53, STR 38 L/H TO STR 38 R/H IAW A320 SRM 53-41-14, PG. B22. 2L72 4F RTA28NM 20030707000612003070700061CE 2003 7 7 DXTA200300040 120030601A2751 RESOLVER CESSNA750 750 2076810CE TE FLAPS INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07939QS882 7500193 FLAPS FAIL AMBER CAS MESSAGE ILLUMINATED AND FLAPS INDICATOR JUMPED FROM 0-35 DEGREES IN LEVEL CRUISE FLIGHT ABOVE 250 KIAS ON 3 DIFFERENT OCCASIONS. - INSPECTED AND FOUND RESOLVER GROUND (GT048) LOOSE. TIGHTENED GROUND TERMINAL. 2L72 4J RTT00007WI 20030716001012003071600101NE 2003 7 16 HEEA087970 120030621A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 THE "C" CHANNEL HAS SOME DEBONDING AND THE TOP OUTSIDE DOUBLER SEPERATED. 1G72 3U H1NE 20030707000592003070700059NM 2003 7 7 AALA20030666 120030616A3350 CONNECTOR BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21346AN 33085 DURING OVERNIGHT MAINTENANCE, RIGHT AFT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. TIGHTENED RIGHT AFT EMERGENCY EXIT DOOR LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030707001472003070700147WP 2003 7 7 UPS03840872 120030617A5754 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING CENTER LE LOWER SKIN IS CRACKED JUST AFT OF IB END OF SLOT DOOR AT 225. STOPDRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW E.O. DC8-5720-4087. 2L74 4F RT4A25 20030710000202003071000020EA 2003 7 10 ASOA03237 120030529A3350601R461041 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A GROUND INSPECTION IN DFW, A FLOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED WATER FROM THE FLOOR EMERGENCY LIGHT TRACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030710000332003071000033NM 2003 7 10 USAABB03086 120030603A33508731002511REV15 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19624AU 27245 FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030711000722003071100072NM 2003 7 11 C1HA200382006 120030625A2611824PY SMOKE DETECTOR BOEING727 7272S7 138407ZNM LAVATORY WILL NOT TEST A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15682CA 22019 SMOKE DETECTOR IN FWD LAV WILL NOT TEST EVERY TIME. 2L73 4F A3WE 20030403000292003040300029NM 2003 4 3 03FDEA00363 120030401A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION ON LONGITUDINAL BEAM UPPER FLANGE AT NUT PLATE HOLES BS 758-850 R25 WL 208. CORROSION ON LONGITUDINAL BEAM UPPER FLANGE BS 758-850 RBL 25 WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED BEAM IAW SRM 51-30-5 AND 51- 30-2. 2L73 4F RTA3WE 20030409000022003040900002WP 2003 4 9 03FDEA00399 120030408A5347 SEAT TRACK DOUG DC10 DC1030 3023501WP FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25317FE 46835 N 317 MAIN CARGO COMPT, SEAT TRACK IS CRACKED 10 INCHES LONG AT FS 960 LBL 28. REMOVED DAMAGED PORTION OF SEAT TRACK FROM STA 949 TO 989 AND R & R IAW SRM 53-70-00. REPAIR PARTS FABRICATED ON TRAVELER T2/323005 AND T2/323056, PAINTED IAW SRM 51-21-02. INSTALLED REPAIR PARTS IAW SRM 53- 70-00 2L73 4F A22WE 20030410000922003041000092NM 2003 4 10 SWAA030664 120030322A57536546434369 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C2 CHECK, FOUND LT INBOARD AFT T/E FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED INBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030414000432003041400043EU 2003 4 14 CA030312018 120030218A6730SC5072 SERVO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR FAILED W O OTHER F FLT CONT AFFECTED HOHOVERING 1 CA (CAN) PILOT REPORTS THAT SERVO IS HARD TO MOVE. WHEN SERVO IS MOVED BY PILOT INPUT TO TAIL ROTOR PEDALS, THE SERVO MOVES THE PEDAL FULL FORWARD TO ITS STOPS OR FULL AFT DEPENDING ON WHICH PEDAL IS MOVED. THIS SHOULD NOT HAPPEN, THE PEDALS SHOULD ONLY MOVE AS FAR AS THE PILOT MOVES THEM. 1G71 3U3 UNCH9EU E19EU 20030410000312003041000031WP 2003 4 10 GTIA030085 120030209A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR SUPPORT STATION 200 LBL 15 RBL 5 CORRODED. FABRICATED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030416001642003041600164NM 2003 4 16 DLM88030302 120030329A3350 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27955DL 49886 EMERGENCY TRACK LIGHTS INOP FROM SEAT 31 THRU AFT SECTION. REPLACED BLOWN FUSE F1 ON AFT POWER SUPPLY. 2L72 4F RTA6WE 20030425000452003042500045NM 2003 4 25 UPS03440393 120030302A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, AFT LOWER CARGO DOOR CUTOUT UPPER CORNERS TWO FASTENER HOLES FOUND CRACK REVEALED FWD CORNER CRACKED HOLE AT SKI AND BEAR STRAP LAYER. AFT CORNER CRACKED HOLE AT BEAR STRAP LAYER. FOR DETAIL PLS REFER ATTACHED SKETCH. FWD UPPER CORNER REPAIRED AS PER HX RS R53-61-34990 & AFT UPPER LOWER REPAIRED AS PER HX RS R53-61-34981 & UPS EA 747-53-20127 & B747-53-20128. 2L74 4F RTA20WE 20030425001052003042500105NM 2003 4 25 DLM88030212 120030305A5730 PANEL DOUG MD88 MD88 3023688NM LEFT WING LEAKING A DALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO27911DE 49967 FUEL LEAK LEFT WING INNER COVER SECOND PANEL FROM FUSELAGE. REPAIRED LEAK. 2L72 4F RTA6WE 20030428000722003042800072NM 2003 4 28 QXEA0300429 120030403A5410 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX- NR 2 NACELLE FINGERNAIL DECKING AND SUPPORT BRACKET CRACKED AT AFT FINGERNAIL ATTACHMENT POINT. REPAIRED IAW RD8/4-54-033 AND RD8/4-54-044. 2H72 4T RTA13NM 20030428000732003042800073NM 2003 4 28 QXEA0300430 120030403A5410 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX-NR 1 NACELLE FINGERNAIL DECKING AND SUPPORT BRACKET CRACKED AT AFT FINGERNAIL ATTACHMENT POINT. REPAIRED IAW RD8/4-54-033 AND RD8/4-54-044. 2H72 4T RTA13NM 20030430002292003043000229EU 2003 4 30 AWXA200300434 120030426A33501013101 LIGHT AIRBUS320 A320231 3930325EU L-1 DOOR LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 LAS - EEL - DURING INSPECTION MAINTENANCE DISCOVERED THE L-1 DOOR EMERGENCY EXIT LIGHT FIXTURE LOOSE. REMOVED AND REPLACED L-1 DOOR EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030502002802003050200280NM 2003 5 2 03FDEA00211 120030303A5510ALC8102 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 7L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030505000872003050500087NM 2003 5 5 DHL2003741531 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS PILLOWING FWD BS 1070 AT STR 22R. REMOVED FASTENERS AT FWD BS 1070 AT STR 22R IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-30-0 FIG 2 FROM 2024-T3 .071 PO 9912398 SIZE 10 X 13.25 INCH. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030502000682003050200068WP 2003 5 2 ASAA0380180 120030301A52505926003511 DOOR DOUG DC9 DC982 3022082WP CARGO BARRIER PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND MID CARGO BAY BARRIER DOOR IS PUNCTURED ON INNER FACE. REPAIRED WITH BONDED 7075-T6 FILLER AND DOUBLER PER SRM 51-70-2. (M) 2L72 4F A6WE 20030502002822003050200282NM 2003 5 2 DHL2003741544 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS 3 DENTS FWD BS 1110 ABOVE AND BELOW STR 19 R. DAMAGED FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT 2 EACH DAMAGED AREA (2 DENTS IN 1 CUT OUT) DIM 2 X 1 INCH AND FABBED REPAIR DOUBLER THAT INCORPORATES N/R 43432, 43433, 43433 MADE FROM 2024-T3 .063 INCH PO 9912495 DIM 62.5 X 16 INCHES IAW B-727 SRM 53-30-1 FIG 1, 53-30-2 FIG 2. REMOVED PREVIOUS REPAIR FOR ACCESS IAW B-727 51-30-2. TREAT, PRIME, INSTALLED DOUBLED IAW B-727 SRM 51-10-2, 53-30-1 FIG 1, 53-30-2 FIG 2. 2L73 4F RTA3WE 20030506000352003050600035NM 2003 5 6 252TR0004 120030423A2910 PRESSURE SWITCH BOEING737 737228 13844AGNM HYD SYSTEM LEAKING A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05252TR 23001 B-CHANNEL AUTO PILOT WILL NOT ENGAGE. PLACED B-CHANNEL AUTO PILOT ON MEL CONT 0423001. REMOVED AND REPLACED HYD PRESSURE SWITCH. OPS AND LEAK CHECKS GOOD IAW MM 22-11-391 2L72 4F RTA16WE 20030717000572003071700057 2003 7 17 HEEA088050 420030708A2220214074301105 AMPLIFIER BELL 214 214ST 1182106SW SCAS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 SCAS AMPLIFIER KICKS OFF LINE. 2G72 4U H10SW 20030114000392003011400039NM 2003 1 14 SWAA030028 120030104A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1012, STR 7L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030124000942003012400094NM 2003 1 24 QXEA0300119 120030122A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09345PH1044667 476 SEA ON FLIGHT 2134- NO.1 AC GENERATOR CAUTION LIGHT ILLUMINATED. RESET PER EMERGENCY CHECKLIST WITH NO CHANGE. REMOVED AND REPLACED NO.1 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030128000182003012800018GL 2003 1 28 HEEA083770 220030115A720023063392 ENGINE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENG BAY OVERSPEED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 ENGINE OVERSPEED. REPLACED WITH SERVICEABLE ENGINE. 1G71 3U3 UO H2SW E1GL 20030128000292003012800029GL 2003 1 28 HEEA083781 220030115A723023064570 LINER BELL 407 407 1182206SW ALLSN 250C 250C* GL COMPRESSOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH 53401 CRACKS AROUND THE INSIDE EDGE OF LINER AT END THAT MOUNTS TO SHIELD. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000902003012800090SW 2003 1 28 HEEA083839 120030116A6230406010428109 BUSHING BELL 407 407 1182206SW M/R HEAD SET WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH2479 53401 MAIN ROTOR HEAD BUSHING SET WORN. 1G71 3U O H2SW 20030128001602003012800160 2003 1 28 MWEA030046 420030126A34254055900906 SYMBOL GENERATOR DOUG DC9 DC982 3022082WP COCKPIT INOPERATIVE A MWEAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 GL31809ME 48071 FIRST OFFICER PRIMARY FLIGHT DISPLAY AND NAVAGATION DISPLAY LOST POWER. -- REMOVED AND REPLACED #2 SYMBOL GENERATOR. 2L72 4F A6WE 20030131001732003013100173NM 2003 1 31 UPS03240113 120030112A5310 CHANNEL BOEING727 72722C 138400FNM BS 1263 R/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI BS1263 R/H, VENTRAL STAIR TORQUE BOX HORIZ. BEAM IS CRACKED AT I/B U PPER RADIUS CHANNEL REPLACED IAW DRAWING 65C13874& SRM 51-30-02 2L73 4F A3WE 20030204000502003020400050NM 2003 2 4 SWAA030221 120030129A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SPECIAL VIST, FOUND A 7.0 LONG FUSELAGE SKIN CRACK, BS 727E+12, ABOVE STR 5R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030204002342003020400234NM 2003 2 4 SWAA030207 120030126A33506574550 BATTERY BOEING737 7373A4 1384585NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030213000162003021300016NM 2003 2 13 CA030123008 120030114A2910 MODULE BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE HYD 'A' SYSTEM FAILED W A UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB, IT WAS OBSERVED THAT THE 'A' SYSTEM HYDRAULICS OVERHEAT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. THE 'A' SYSTEM HYDRAULIC MODULE WAS REPLACED AND CHECKED SERVICEABLE IAW WITH MM 29-11-52. 3. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L73 4F4 F A3WE E2EA 20030214000852003021400085WP 2003 2 14 ASAA0380055 120030105A57549937467525 DOOR DOUG DC9 DC983 3022083WP L/E SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT NR 5 SLAT NR 13 TRACK DOOR IS CRACKED. REPLACED TRACK DOOR PER BAC DWG 9937467. (M) 2L72 4F RTA6WE 20030219001162003021900116 2003 2 19 SWAA030342 420030211A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030219001412003021900141NM 2003 2 19 USAA030004 120030107A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19391US49267 23313 PIT - FOUND SKIN CRACKED 1.5 INCH LONG CRACK, STATION 727E LEFT SIDE STRINGER 22L. DOUBLER AND TRIPLER INSTALLED PER EA 75613. (M) 2L72 4F RTA16WE 20030223000032003022300003SO 2003 2 23 C2XA03SH013 120030222A530014526437001 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030224000872003022400087SW 2003 2 24 HEEA084208 120030120A5320407070620111 TRIM PANEL BELL 407 407 1182206SW AFT CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 AFT CABIN TRIM PANEL IS CRACKED. 1G71 3U O H2SW 20030116001292003011600129 2003 1 16 HEEA083074 420030108A2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 VHF TRANCEIVER DIGITS ARE INTERMITTENT. DISPLAY WOULD INTERMITTENTLY GO DIM AND STAY DIM FOR A WHILE THEN COME BACK UP. REPLACED V901 PHOTOCELL AND DISPLAY LENS. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030121001582003012100158GL 2003 1 21 HEEA083316 220030109A725023062087 CHECK VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL TURBINE OIL SMOKE E HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03206FS 51506 TURBINE OIL PRESSURE CHECK VALVE SMOKING ON SHUTDOWN. REPAIRED. 1G71 3U3 U H2SW E1GL 20030304001012003030400101 2003 3 4 HEEA084603 420030214A3442 FUSE BELL 412 412 1182202SW WX RADAR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 1132 33002 WEATHER RADAR POWERS UP BUT DOES NOT WORK. FOUND F101 FUSE BAD, REPLACED, REPAIRED, BENCH CHECK GOOD. 1G72 4U H4SW 20030225000692003022500069SW 2003 2 25 HEEA084292 120030211A5260407301110 STEP BELL 407 407 1182206SW ENTRY STEP CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 STEP PITTED BEYOND LIMITS. 1G71 3U O H2SW 20030226000682003022600068SW 2003 2 26 HEEA084355 120030211A2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL QTY SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 SIGNAL COND UNIT MALFUNCTIONED, FUEL LOW LEVEL LIGHT ON WITH 500 LBS OF FUEL. 1G71 3U O H2SW 20030227001072003022700107NE 2003 2 27 HEEA084413 220030212A74214053T22P06 IGNITER BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 ENGINE HARD TO START. REPLACED IGNITERS. 2G72 4U4 U H10SW E8NE 20030228000262003022800026NM 2003 2 28 SWAA030386 120030215A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING OTS, FOUND FUSELAGE SKIN CRACKED 4 LONG AT BS 476, STRINGER 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030228001132003022800113SW 2003 2 28 HEEA084468 120030213A3212OHSS2061003 COVER BELL 206 206L3 1182108SW EMERGENCY FLOAT DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 LT FWD, RT FWD FLOAT COVERS DETERIORATED. SCRAPPED. 1G71 3U H2SW 20030324000302003032400030NM 2003 3 24 CALA0300137 120030321A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912313 23364 INSPECTION FOUND AFT GALLEY FLOORBEAM CORRODED AT FORWARD AND AFT FLANGES AT STA 986, LBL 10 TO RBL 20. REMOVED AND REPLACED T-CAP IAW SRM 51-20-02. 2L72 4F RTA16WE 20030324000482003032400048WP 2003 3 24 ABXA030102 120030219A5320D0489822 WEB DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 RIGHT CUSP WEB DOUBLER WAS CRACKED AND BULGED AT APPROXIMATELY STA 619. INSTALLED NEW CUSP WEB IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20030325000062003032500006WP 2003 3 25 03FDEA00343 120030322A2912 FILTER DOUG MD10 MD1010F WP NR 3 HYD SYS INOPERATIVE A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25399FE 48262 AT CRUISE NR 3 HYD WENT TO 0.1 QTY. FOLLOWED PROCEDURE IN QRH - COULD NOT EXT SLATS. EXECUTED A NO SLAT/FLAPS 22 DEG LANDING. CHECKED LT & RH CASE DRAIN & PRESS FILTERS FOR METALLIC RESIDUE. R & R ALL ENGINE HYD FILTERS, R & R NR 3 LOWER ENGINE HYD PUMP PER MM 29-11-01-2 REPLACED UPPER PUMP PER M/M 29-11-01-2.REPL MAIN FILTERS. FILLED SYS. BLED AND RAN ENGINE. FLIGHT CONT LEAK CHECK GOOD. RAN FLT CONT CHECKS PER M/M 27-85-01 RTS PASSED. 2L73 4F RTA22WE 20030306000472003030600047SW 2003 3 6 HEEA084761 120030218A2422214175104101 INVERTER BELL 214 214ST 1182106SW AC SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 INVERTER INOPERATIVE. 2G72 4U H10SW 20030311000042003031100004SW 2003 3 11 HEEA085028 120030228A6420206011810135 ROTOR HEAD ASSY BELL 206 206L3 1182108SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N4204 51512 TAIL ROTOR HEAD HAS HOLE ON END. REPAIRED. 1G71 3U H2SW 20030311000072003031100007SW 2003 3 11 HEEA085031 120030228A6330 BEARING BELL 206 206L4 1182110SW LINK ASSY SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W LK3841 52033 MAIN ROTOR GEARBOX MOUNT LINK ASSY HAS A LOWER ELASTOMERIC BEARING SEPARATED 360 DEGREES. 1G71 3U NCH2SW 20030506000042003050600004NM 2003 5 6 CALA0300218 120030426A5230146N61003 SKIN BOEING757 757224 1384958NM L4 DOOR PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0918119 27561 PUNCTURE DAMAGE TO INNER SKIN OF L4 DOOR. REPAIR PUNCTURE DAMAGE PER EC/RA 5210-01692. 2L72 4F RTA2NM 20030507000532003050700053NE 2003 5 7 AUS20030352 120030324A2520337657079101 SEAT BACK SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE CABIN CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PASSENGER SEAT BACK ASSEMBLY CRACKED ACROSS ENTIRE WIDTH. SUSPECT CAUSED BY PASSENGERS PUSHING/PULLING BACK ON SEAT. SEAT BACK IS MANUFACTURED FROM COMPOSITE MATERIAL. 1G72 3U3 UNCH1NE E19EU 20030509001322003050900132EA 2003 5 9 COMA0360232 120030507A2721601R5122623 SWITCH CNDAIRCL600 CL6002B19 1900309EA INST PANEL UNCONTROLLABLE A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01805CA 7354 RUDDER TRIM RUNAWAY DURING FLIGHT. REPLACED THE RUDDER/AILERON TRIM CONTROL PANEL. 2L72 4F RTA21EA 20030513001112003051300111NM 2003 5 13 CH1A200395057 120030426A5320 SUPPORT BOEING727 727290 138408WNM TRUNNION BEARINGCORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LT FWD TRUNNION BEARING SUPPORT HAS CORROSION. 2L73 4F A3WE 20030513000842003051300084NM 2003 5 13 UPS03240665 120030418A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, RT MLG DOOR, DOOR SKIN ON O/B SECTION OF DOOR ASSY CRACKED BS 910 AREA OF CRACKED SKIN TRIMMED OUT IAW SRM 52-80-02. HFEC INSP. CARRI ED OUT AROUND CUTOUT AT R/H MLG DOOR SKIN ON O/B SECTION OF DOOR ASS Y IAW B727 NDTM PT 6 510000 FIG 4. REPAIR CARRIED OUT IAW SRM 52- 80-02 2L73 4F A3WE 20030515001352003051500135NM 2003 5 15 AWXA200300479 120030424A531365516982 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND AT RIVET HOLES ON STRINGER 4 LT, BS 908-909. MAINTENANCE REMOVED 12 INCH SECTION OF STRINGER SPLICE ON STRINGER 4 LT, BS 908-909; FABRICATED A REPAIR CHANNEL PER DWG 65-51698-2; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 38. 2L72 4F RTA16WE 20030604000172003060400017NM 2003 6 4 GAIA03016OP 120030516A7500131962 LINE BOEING727 727251 138408HNM NR 3 ENGINE LEAKING A GAIAO OTHER M OVER TEMP CRCRUISE 1 SW07252US 19971 RIGHT STRUT OVERHEAT LIGHT CAME ON IN FLIGHT. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED 13TH STAGE MOD VALVE SENSE LINE ON NR 3 ENGINE. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030605000062003060500006 2003 6 5 AUS20030431 420030419A2397DG25ARM30020E30 INSULATOR BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL COMMS SYS FAILED W O OTHER D INFLIGHT SEPARATION LDLANDING 1 AUS (AUS) WIRE SEPARATED FROM AIRCRAFT AT FEED THROUGH INSULATOR. LONG WIRE IS USED FOR MILITARY OPERATIONS. 1L72 4T4 T A24CE E4EA 5 CSTC 20030605000532003060500053EU 2003 6 5 UPS03140660 120030505A5270 POWER SUPPLY AIRBUSA300 A300F4622R 3930360EU DOOR WARNING FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01131UP 0816 AUTONOMOUS STANDBY POWER SUPPLY UNIT FAILED BITE TEST R&R AUTONOMUS STANDBY POWER SUPPLY POWER M/M 52-73-18. THIS CLEARS M 259193 PLACARD REMOVED. 2L72 4F RTA35EU 20030606000772003060600077NM 2003 6 6 03FDEA00772 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B CTR BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030609000302003060900030NM 2003 6 9 03FDEA00790 120030521A5753 RIB DOUG MD11 MD11 3023602NM LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LT WING: LEADING EDGE RIB AT SLAT TRACK NR 16 FOUND WITH HAIRLINE CRACK. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II AND DRAWING ARB2850. 2L73 4F RTA22WE 20030514001792003051400179NM 2003 5 14 03FDEA00660 120030501A7932ST104YM1 TRANSMITTER BOEING727 727200 138407ENM NR 2 ENGINE READS HIGH A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25490FE 21493 NR 2 OIL PRESSURE AT 54 PSI TUS RWY 29R WIND 280/11 25' C WITH STANDARD POWER SET. OIL PRESSURE 5 PSI HIGHER THAN NR 3 AND 10 PSI HIGHER THAN NR 1 ENTIRE FLIGHT. REPLACED NR 2 PRESSURE TRANSMITTER PER M/M 79-33-001-4, NO HELP. ADJUSTED NR 2 OIL PRESSURE RELIEF VALVE PER P/W JT8D M/M 72-61-00. 32 OIL PRESSURE READS 44 PSI AT IDLE. NO LEAKS NOTED, ENG NR 2 COWLINGS CLOSED. 2L73 4F RTA3WE 20030521000052003052100005NM 2003 5 21 DHL2003780007 120030516A5210 STOP BOEING727 727223 1384074NM PAX DOOR OUT OF ADJUST A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01780DH 22006 ON TAXI-IN AT CVG, FORWARD-ENTRY LIGHT ILLUMINATED ON S/O PANEL. BEFORE OPENING THE DOOR S/O NOTICED THE HANDLE MOVED ABOUT 1.5 INCHES UP OUT OF THE FULL CLOSED POSITION. ADJUSTED DOOR STOPS, CLEANED, AND LUBED CAM TRACKS. OPS CHECKED GOOD IAW BMM CHAPTER 52-11-01. 2L73 4F A3WE 20030521000062003052100006WP 2003 5 21 DHL2003801052 120030407A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING CTR L/E INNER DOUBLER WITH 0.500 INCH CRACK IN STA XOLDI 6.250. REMOVED INNER DOUBLER CRACKED IAW SRM 51-1-20D PG 9. FABRICATED NEW DOUBLER (2024-T3 AL0.080) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER AND AREA PG 9-10 AND SRM 51-1-20D PG 21. 2L74 4F RT4A25 20030612000312003061200031WP 2003 6 12 ZW0A0305201 120030528A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT EXPOSED A ZW0AO OTHER O OTHER NRNOT REPORTED 1 CE13982TW 53632 THE EGRESS LIGHTING HAD WIRES EXPOSED AND PULLED OUT AT CABIN ROWS 15 AND 16. MADE AIRWORTHY REPAIR TO WIRING. CHECK-C 11-19-02 STL. 2L72 4F RTA6WE 20030617001852003061700185NM 2003 6 17 QXEA200300592 120030430A7110 CHANNEL BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - NR 2 ENGINE LOWER COWL Z MEMBER (LT HAND) IS CRACKED AT AFT END. FABRICATED AND INSTALLED NEW IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030617003122003061700312NM 2003 6 17 SWAA031267 120030607A33501000679 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2L72 4F A16WE 20030620000882003062000088NE 2003 6 20 AMTA200300699 220030521A7320 EEC BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE SURGES A AMTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL11558TZ 32592 LEFT ENGINE SURGING, ALL ENGINE PARAMETERS FLUX, UNLATCHED LEFT EEC SURGING AND ENG PARAMETERS FLUX STOPPED. DURNG T/S FOUND LEFT PF RAKE ON OUTBOARD SIDE OF LEFT ENGINE MISSING 1 PITOT HEAD, 3RD FROM OUTBOARD. APPLY THE TEMPORARY REPAIR PER AMM 77-11-04-422-001-R00. ITEM CARRIED OVER REF ITEM 1 LP 601247 DISC 7700/741 FOR PERMANENT REPAIR. (M) 2L72 4F4 FRTA2NM E12EU 20030702000272003070200027NM 2003 7 2 TSAA0353108 120030424A53306545805 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13817AL 39735 TRIMMED OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED REPAIR DOUBLER FORM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS PER SRM 53-30-3, FIGURE 1. APPLIED FILLET SEAL WITH BMS 5-95 SEALANT AROUND EDGES OF REPAIR. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3361. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030702000362003070200036NM 2003 7 2 USAABB03076 120030516A33509221009 BATTERY BOEING757 7572B7 1384964NM R3 DOOR DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 CLT - EXIT IDENTIFIER AT DOOR R3 FLASHING. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030630000632003063000063SW 2003 6 30 ALGA087765 120030625A6220406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03557AL177 53243 UNIVERSAL WORN, RATCHETY, AND BINDING. REMOVED AND REPLACED. 1G71 3U O H2SW 20030708001092003070800109NM 2003 7 8 DHL2003754010 120030621A3260 WARNING LIGHT BOEING727 727223 1384074NM MLG DOOR ILLUMINATED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01754DH 22008 AFTER TAKEOFF, RIGHT GEAR DOOR LIGHT ON AND RED GEAR DOORS ON PILOT ANNUNCIATOR ON WHEN GEAR HANDLE PLACED DOWN ALL GEAR INDICATIONS NORMAL. OPS CHECKED RIGHT GEAR DOOR IAW M/M 32-61-01. NO DEFECTS NOTED. 2L73 4F A3WE 20030714000942003071400094NM 2003 7 14 SWAA031352 120030615A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, BELOW STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030714001602003071400160EU 2003 7 14 I05R088093 120030711A3340315152 LIGHT SNIAS 350 AS350* EU EXTERIOR BURNED OUT E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 353 3560 PART KEPT BURNING OUT BULB AND SYSTEM FUSE. REPLACED PART 1G71 3U H9EU 20030714000182003071400018NM 2003 7 14 SWAA031421 120030626A27316959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB INPUT ROD HARDWARE, BUSHING AND ALL HINGE ATTACH POINT HARDWARE PER MM. 2L72 4F RTA16WE 20030716000892003071600089NM 2003 7 16 USAABB03098 120030622A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19629AU 27807 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6, 9, 13, 18, 26 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030717000702003071700070SW 2003 7 17 HEEA088062 120030605A243230703001 BATTERY BELL 412 412 1182202SW MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 MASTER BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030110000412003011000041NM 2003 1 10 03004405 120030104A3350 BATTERY DORNERDO32 DO328300 NM CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27405FJ 3155 DURING MAINTENANCE INSPECTION, EMERGENCY PATH LIGHTING AFT OF SEAT 9A WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL CHARGED BATTERIES WITH AC POWER, OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T RTA55NM 20030115001962003011500196SW 2003 1 15 ERAA082944 120030106A6410212010750105FM BLADE BELL 412 412 1182202SW TAIL ROTOR DAMAGED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01419EH1742 BLADE TIP VOIDED. INSPECTED, REPLACED TIP CLOSURE. REPLACE BUFFER PADS 2 EA ON LOWER SURFACE. 1G72 4U H4SW 20030128000342003012800034SW 2003 1 28 HEEA083787 120030115A282123066697 FILTER BELL 407 407 1182206SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 53188 FILTER FOUND IN BYPASS CONDITION. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030613000452003061300045SO 2003 6 13 SWIA200312066 120030424A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07220SW 120288 AT FRAME 13, BELOW FLOOR COCKPIT ENTRY DOOR, BOTH FRAME DOUBLERS CRACKED. DISCOVERED DURING C-CHECK. DOUBLERS APPLIED TO AREAS MENTIONED IAW SRM 120 51-10-02. 2L72 4T RTA31SO 20030617001702003061700170SW 2003 6 17 HEEA087470 120030612A53207620901001054 BRACKET BELL 407 407 1182206SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 BRACKET CRACKED. SCRAPPED. 1G71 3U O H2SW 20030617002682003061700268SW 2003 6 17 HEEA087027 120030604A6720406040453101 SEAL BELL 407 407 1182206SW TAIL ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03402PH 53159 TAIL ROTOR CONTROL SEAL AND ADAPTER LEAKING. TO BE SENT TO MFG FOR CREDIT. 1G71 3U O H2SW 20030520001252003052000125NE 2003 5 20 2003F00264 220030321A723065196842 DOME BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE NR 2 ENGINE DAMAGED A P9RAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11919PG 22604 P708804 NR 2 ENGINE WENT INTO A CONTINUOUS COMPRESSOR STALL SHORTLY AFTER LANDING GEAR RETRACTIONON TAKEOFF AT MSP. EGT CLIMBED INTO AND STABILIZED IN THE RED ARC FOR 1 MINUTE, RETARDED ENGINE THROTTLE TO IDEL POSITION AND ENGINE STABILIZED, ALL OTHER SYSTEMS NORMAL. AIRCRAFT RETURNED TO MSP WITH THE ENGINE AT IDLE. ENGINE WAS SHUTDOWN UPON RETURN TO THE GATE. TOTAL ENGINE OPERATION WAS 48 MINUTES. IT APPEARS AT THIS TIME THAT THE NOSE DOME CAUSED THE COMPRESSOR STALL, DUE TO FAILURE OF THE ATTACHING HARDWARE. POSSIBLE OVER TORQUE OF THE STUDS. (M) 2L73 4F4 FRTA3WE E2EA 20030523001422003052300142WP 2003 5 23 DHL2003604518 120030427A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD L/E FORMER AT STA XFS 722.500 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AT XFS 722.500 IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030623000602003062300060NM 2003 6 23 KPVA200315 120030320A335010005511 LIGHT DHAV DHC8 DHC8103 1386005NM COCKPIT MALFUNCTIONED A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13805WP 353 FOUND COCKPIT PORT EMERGENCY LIGHT DIM. REMOVED AND REPLACED LIGHT. (M) 2H72 4T RTA13NM 20030623000952003062300095WP 2003 6 23 GTIA030402 120030511A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND CABIN RIGHT INBOARD SEAT TRACK CORRODED FS 1073-1309. SEAT TRACK OUT OF LIMITS AT STATION 1287. CUT OUT DAMAGED SECTION OF RIGHT INBOARD SEAT TRACK FROM FS 1223 TO 1309. FABRICATED REPLACEMENT SECTION OF SEAT TRACK. INSTALLED NEW TRACK. (M) 2L72 4F A6WE 20030626000112003062600011NM 2003 6 26 03FDEA00452 120030416A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 STRINGER HAS CORROSION (C53-113-01-2) 28L BS 950E+3 LBL 16 WL 150. REPAIRED STR. 28L B.S. 950E+3 LBL1 6 WL 150 IAW SRM 53-10-3. 2L73 4F RTA3WE 20030717001002003071700100NM 2003 7 17 TSAA0333131 120030531A3350861002 BATTERY PACK BOEING737 737282C 13844AUNM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13826AL 23051 REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030701000262003070100026EU 2003 7 1 I05R087790 120030521A2121420800001 BLOWER SNIAS 350 AS350B2 8680813EU FWD EVAPORATOR DAMAGED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP05557CB322 3431 FORWARD EVAPORATOR BLOWER BRUSHES NOT SEATED: INOPERATIVE, REPLACED BLOWER 1G71 3U H9EU 20030709000352003070900035WP 2003 7 9 AALA20030589 120030520A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217525A 49917 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT ROWS 18-26 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT BATTEYR FOR ROW 18-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000872003070900087WP 2003 7 9 MWEA030242 120030609A2510 SEAT BELT DOUG DC9 DC932 3022066WP COCKPIT BROKEN A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31401ME 47133 CAPTAIN'S SEAT BELT BROKE. RESECURED SEAT BELT AT MOUNT. 2L72 4F A6WE 20030711000602003071100060NM 2003 7 11 DHL2003745015 120030625A2510 SEAT BOEING727 727224 1384076NM COCKPIT DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01745DH 20665 F/O'S SEAT BACK OF SEAT WILL NOT LATCH COMPLETELY. TIGHTENED LOOSE RT RECLINE LOCK RELEASE CABLE MOUNT. F/O'S SEAT OPS CHECKED GOOD PER M/M 25-10-40. 2L73 4F A3WE 20030115000972003011500097SW 2003 1 15 ALGA082886 120030107A6310406040516101 SHAFT BELL 407 407 1182206SW FREEWHEEL UNIT WORN H ALGAK NONE O OTHER ININSP/MAINT 1 FS01697AL2457 A4668 53374 DURING 2500 HR OVERHAUL OF FREEWHEEL UNIT. FOUND INPUT DRIVE SPLINES WORN BELOW LIMITS. 1G71 3U O H2SW 20030401001092003040100109WP 2003 4 1 DHL2003804001 120030103A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP NR 4 WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01804DH 46124 NR 4 SMOKE DETECTOR DOES NOT TEST. ITEM TRANSFERRED TO DMI LOG PER 26-6-1. DMI 11469, PLACARD INSTALLED. 2L74 4F RT4A25 20030129000222003012900022SW 2003 1 29 HEEA083932 120030117A6220 SPRING BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH A734 53198 MAIN ROTOR HEAD FRAHM ASSY HAS TWO BROKEN SPRINGS. 1G71 3U O H2SW 20030131001382003013100138SO 2003 1 31 C2XA03BT020 120030129A33501317 BULB EMB 145 EMB145LR 3260212SO CABIN AREA FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2712540 145537 BTV---CO2002, CREW REPORTED, EMERGENCY LIGHT OVER SERVICE DOOR INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT SOCKET IAW EMB145 AMM #33-50-10. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20030207001252003020700125NM 2003 2 7 03FDEA00101 120030203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO BAY FRAME IS GOUGED AT BS 600 LBL 50 WL 173. 2L73 4F RTA3WE 20030212000922003021200092SO 2003 2 12 CA030120007 120030117A24352CM306D4 STARTER GEN EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA ENGINE FAILED W O OTHER H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 CA (CAN) DURING A ROUTINE MAINTENANCE INSPECTION IN THE AREA AT THE REAR OF THE RT ENGINE COMPARTMENT IT WAS NOTICED THAT THERE WAS AN ABUNDANCE OF METALLIC DUST IN THE AREA SURROUNDING THE REAR OF THE STARTER GENERATOR. A THOROUGH INVESTIGATION REVEALED THE DUST TO BE THE CAUSE OF THE COOLING FAN ON THE REAR OF THE STARTER GENERATOR SHAFT TO BE SHEARED OFF AT ITS PRETENSION FITTING (THE STARTER GENERATOR SHAFT DID NOT FAIL BUT RATHER THE COOLING FAN ITSELF FAILED WHERE IT ATTACHES TO THE SHAFT). IT IS SUSPECTED THAT THE COOLING FAN CAME LOOSE FROM THE STARTER GENERATOR SHAFT CAUSING THE FAN TO BREAK.MAINTENANCE REPLACED THE STARTER GENERATOR AND THE AIRCRAFT WAS RETURNED BACK TO SERVICE. 1L72 4T4 T A21SO E4EA 20030213000432003021300043SW 2003 2 13 CA030204011 120030106A632023009342 RETAINER BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL GEARBOX BROKEN W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) DURING ENGINE GEARBOX OVERHAUL A 3 INCH PIECE OF BALANCED RATAINING RING FOUND LAYING INSIDE GEARBOX. THE REMAINING BALANCED RATAINING RING WORE A STEP IN RETAINING RING GROOVE OF THE HELICAL TORGUEMETER GEARSHAFT. ROLLS ROYCE HAS BEEN NOTIFIED AND PICTURES FORWARDED TO THEM. 1G71 3U3 U H2SW E4CE 20030219000782003021900078NM 2003 2 19 SWAA030259 120030202A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (3 EA) AT BS 360 AT STR 4L, BS 908 AT STR 4L AND BS 908 AT STR 4R. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030219001212003021900121NM 2003 2 19 SWAA030350 120030212A335015AT17 SWITCH BOEING737 7377H4 1384404NM COCKPIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29401WN 29813 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT ILLUMINATE FROM COCKPIT SWITCH. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PER MM. 2L72 4F RTA16WE 20030221000642003022100064EU 2003 2 21 MALA030160 120030219A2620 SMOKE DETECTOR BAC 146 AVRO146RJ85A1500097EU A MALAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL15531XJ E2365 UPON ROTATION OF FLIGHT #3655, CARGO SMOKE NWS ILLUMINATED AND AFT CARGO SMOKE ILLUMINATED. FA'S DID NOT SMELL SMOKE, NO SMOKE NOTED. CREW DID NOT BLOW BOTTLES, RETURNED TO MSP W/FIRE TRUCKS STANDING BY. AIR RETURN TO MSP. MAINTENANCE COMPLETED NRWC #169910 W/CONT CARDS. REPLACED AFT CARGO SMOKE DETECTOR, FLT DECK CONTROL UNIT AND REPAIRED CHAFFED WIRES TO SMOKE DETECTION AND EXTINGUISHING SYSTEMS CHECK GOOD. 2H74 4F RTA49EU 20030223000122003022300012SO 2003 2 23 C2XA03SH021 120030222A530014521725013 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK THE RIGHT HAND SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030224000592003022400059NE 2003 2 24 HEEA084180 120030212A6730 BEARING SKRSKYS76 S76A 8143006NE M/R SERVO WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 0658D 760076 MAIN ROTOR SERVO HAS A PIVOT BEARING WORN. IN SHOP REPAIR. 1G72 3U H1NE 20030304000432003030400043SW 2003 3 4 HEEA084577 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 WORN BEARINGS. REPLACED 2 EACH 412-010-427-101 BEARINGS DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030306001052003030600105SW 2003 3 6 HEEA084812 120030221A2510412070820101 SEATBACK CUSHION BELL 412 412 1182202SW CREW SEAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 SEAT BACK CUSHION TORN. REPAIRED. 1G72 4U H4SW 20030307000912003030700091 2003 3 7 HEEA084893 420030227A34427021450601 COMPUTER SKRSKYS76 S76A 8143006NE WX RADAR SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH 760224 WEATHER RADAR COMPUTER WILL NOT PAINT. 1G72 3U H1NE 20030307001972003030700197 2003 3 7 HEEA084912 420030225A2210214074301105 AMPLIFIER BELL 412 412 1182202SW SCAS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 SCAS WILL AMPLIFIER NOT HOLD PITCH CHANNEL. 1G72 4U H4SW 20030117000082003011700008SW 2003 1 17 HEEA083153 120030108A3213206030104023 FITTING BELL 206 206L3 1182108SW MLG CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 CROSSTUBE FITTING ASSY WORN AND CORRODED. SCRAPPED. 1G71 3U H2SW 20030127001082003012700108 2003 1 27 HEEA083662 420030114A237080510800001 CONTROL BOX BELL 407 407 1182206SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 DATA BOX SKYWATCH UNREADABLE CAUSING FALSE TARGETS TO DISPLAY. COULD NOT DUPLICATE PROBLEM. BENCH CHECK GOOD. 1G71 3U O H2SW 20030127002702003012700270GL 2003 1 27 HEEA083746 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 HIGH TOT. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030128000302003012800030GL 2003 1 28 HEEA083783 220030115A723023064570 LINER BELL 407 407 1182206SW ALLSN 250C 250C* GL COMPRESSOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 LINER CRACKED IN DOUBLE LIP AREA. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000612003012800061SW 2003 1 28 HEEA083815 120030116A6300 BUSHING BELL 407 407 1182206SW LEVER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH AFS1348 53399 MAIN ROTOR LEVER ASSY HAS BUSHINGS WORN. 1G71 3U O H2SW 20030128000832003012800083SW 2003 1 28 HEEA083837 120030116A6230406010428109 BUSHING BELL 407 407 1182206SW M/R HEAD SET WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH680 53003 MAIN ROTOR HEAD BUSHING SET WORN. 1G71 3U O H2SW 20030131001882003013100188NM 2003 1 31 AWXA200300097 120030131A2121424B2003 FILTER AIRBUSA319 A319132 3930340NM ZONE 130 CONTAMINATED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28805AW0 0 1049 PHX - AIR TURN BACK - FLT 0001 - ON TAKEOFF FROM PHX EN ROUTE FOR ORD FUMES WERE NOTICED IN MID-CABIN, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED POWER RUN AT ALL SETTINGS ISOLATING THE NO.1 AND NO. 2 ENGINES BLEEDS AND APU BLEED, UPON INSPECTION FOUND RE-CIRCULATION FAN FILTERS DIRTY. REMOVED AND REPLACED BOTH FILTERS. 2L72 4F RTA28NM 20030203001632003020300163EA 2003 2 3 DSF2003F00000 220030102A7321 ROD END PIPER PA31T PA31T2 7103127SO PWA PT6 PT6* 52043EA FUEL CONTROL SEIZED E DSFAK NONE O OTHER ININSP/MAINT 1 GL25440S 31T8166016 UNABLE TO CONTROL ENGINE WITH POWER LEVER. ACCESS TOTAL INFLIGHT FEATHERING. FUEL CONTROL LINKING ROD END SEIZED, PREVENTED OPERATION OF FCU. 1L72 3T3 TRTA8EA E2NE 20030204002382003020400238NM 2003 2 4 SWAA030210 120030129A33501000679 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29091SW 22963 L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20030206001552003020600155EA 2003 2 6 COMA0360081 120030204A284073664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SO01709CA11303 7238 FLIGHT 5543 LEFT FUEL PUMP CAUTION AND FUEL IMBALANCE CAUTION MESSAGE.REPLACED THE FUEL COMPUTER. 2L72 4F RTA21EA 20030207001172003020700117NM 2003 2 7 03FDEA00079 120030128A5320 WEB BOEING727 727233 138408ANM PWA JT8 JT8D* NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 WEB CRACKED AT LIGHTING HOLE, BS 1239, LBL 20, WL 170, AFT AIRSTAIR AREA. REPAIRED CRACK IN LIGHTING HOLE IAW SRM 51-40-02. 2L73 4F4 FRTA3WE E2EA 20030210001322003021000132WP 2003 2 10 DHL2003806003 120030209A2611 DETECTOR DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01806DH 46002 1) LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM SHOWS CODE AC7444/FALSE ALARM WITH MX INDICATOR. SYSTEM OK LIGHT ON.2) DEFERRED AC7444 IAW MEL 26-10-1)-B), PAGE 6.(ALL OTHER FAULTS ANNUNCIATED BY MX DISPLAY). DMI #11944. 3) REF. DMI #11944 LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM SHOWS CODE AC7444/FALSE ALARM WITH MX INDICATION. SYSTEM OK LIGHT ON.4) REPLACED FAULTY DETECTOR S/N AC744 PER DC-8 SUPPLEMENTAL M/M 26-15-05. OPS CHECKED SERVICEABLE PER DC-8 SUPPLEMENTAL M/M 26-16-00. DMI #11944 CLEARED. PLACARD REMOVED. 2L74 4F RT4A25 20030212000692003021200069NM 2003 2 12 CA030117007 120030117A3260H1010153 UPLOCK SWITCH BOEING BOEING727 72725C 138400HNM PWA JT8 JT8D7B 52053NE NLG FAILED W L ABORTED APPROACH N FALSE WARNING APAPPROACH 1 CA 1Q1396 (CAN) ON FINIAL APPROACH INTO YYC WHEN GEAR DOWN SELECTED, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR CYCLED, NO CHANGE. AFTER 2 MIN DELAY GREEN LIGHT ILLUMINATED. MANUAL EXTENDION INDICATION ALIGNMENT MARKS CONFIRMS GEAR DOWN AND LOCKED. SYSTEM COULD NOT BE FAULTED BY MAINTENANCE. MAINTENANCE SUSPECTED THE UPLOCK SWITCH. BOTH UPLOCK AND POSITION SWITCHES REPLACED. NO FURTHER PROBLEMS HAVE BEEN REPORTED. 2L73 4F4 F A3WE E2EA 20030218000012003021800001EU 2003 2 18 0302101 120030210A3150 WARNING SYSTEM SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE CONFIGURATION ACTIVATED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL17108CQ 340A108 FLT 4516, AIRCRAFT WAS ON TAKE-OFF ROLL WHEN THE IT GOT A CONFIGURATION WARNING. THE CREW ABORTED TAKE-OFF AND RETURNED TO THE GATE. AIRCRAFT TAKEN OUT OF SERVICE 2-10-03 AT 1830 2-11-03 AIRCRAFT BEING FERRIED LYH TO FWA AT 1255 ETA 1510. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030219000082003021900008NM 2003 2 19 LER2003F00000 120030203A7810 DUCT PIPER PA60 PA60601P 7106012NM LT & RT ENGINE CHAFED E LERAK NONE O OTHER ININSP/MAINT 1 NM11442AF1168 61P063779632 THE ALUMINUM U-SHAPED DUCT CONNECTING THE FUEL SERVO TO THE INTER COOLER WAS FOUND TO BE CHAFING ON THE EXHAUST PIPE ON BOTH ENGINES. UPON FURTHER INSPECTION THE LT DUCT WAS FOUND TO BE WORN TO THE POINT OF PENETRATION THROUGH THE TUBE IN THE FORM OF SMALL HOLES FROM VOIDS IN A PREVIOUS WELD REPAIR. A CHECK OF THE RIGHT DUCT INDICATED THAT IT HAD BEEN PREVIOUSLY REPAIRED ALSO. THIS AIRCRAFT HAS BEEN MODIFIED WITH A INTER COOLER, MODIFIED TURBOCHARGERS. THIS APPLICATION HAS SMALL CLEARANCE BETWEEN THE TWO PARTS WITH NO MEANS OF PREVENTING CONTACT. PREVENTED BY INSTALLATION OF A STANDOFF ATTACHED TO THE EXHAUST AND INTAKE TUBES WITH HIGH TEMPERATURE CLAMPS TO PREVENT CONTACT. 1M72 3O RTA17WE 20030116000722003011600072SW 2003 1 16 HEEA083032 120030106A2430SM20ACD200A21 RELAY BELL 206 206L3 1182108SW DC SYSTEM FAILED E O OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 BATTERY SYSTEM STAYS ON WITH SWITCH IN OFF POSITION. 1G71 3U H2SW 20030121000972003012100097SW 2003 1 21 HEEA083285 120030109A2810206362002101 FUEL CAP BELL 206 206L3 1182108SW FUEL STORAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 FUEL CAP HANDLE WILL NOT STAY DOWN. SCRAPPED. 1G71 3U H2SW 20030314001702003031400170NM 2003 3 14 USAABB03029 120030301A3397 WIRE BOEING767 767201 1385125NM GE CF6 CF680 30025NE EMERGENCY LIGHTSLOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 FOUND FOUR EMERGENCY LIGHTS INOPERATIVE AFT OF THE LEFT MID LAVATORY. MAINTENANCE FOUND A WIRE LOOSE ON A LIGHT ASSEMBLY AND SECURED IT. 2L72 4F4 FRTA1NM E13NE 20030317001292003031700129NM 2003 3 17 03FDEA00289 120030303A5710 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING FOUND OUTBOARD HINGE OUTBOARD HOLE CORRODED AFTER BUSHING REMOVAL. 2L73 4F RTA22WE 20030121003392003012100339EA 2003 1 21 HNAA0300001 120030117A6100SF1423 PROPELLER DHAV DHC8 DHC8311 1386006EA #1 PROP A HNAAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 EA07333EN1784 1784 221 NUMBER 1 PROPELLER DUE TO POSSIBLE OVR TORQUE CONDITION. REMOVED AND INSPECTED PROP AND REINSTALLED. 2H72 4T RTA13NM 20030122000232003012200023SW 2003 1 22 HEEA083410 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X394 51412 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000452003012200045 2003 1 22 HEEA083432 420030109A3120CK726424 CLOCK BELL 206 206L3 1182108SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 CLOCK DOES NOT RUN WITH GOOD POWER AND GROUND. SCRAPPED. 1G71 3U H2SW 20030321000872003032100087NM 2003 3 21 2003UALA00230 120030303A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29328UA 24148 E AND E COOLING OUTFLOW CUTOUT SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED. 2L72 4F4 FRTA16WE E2GL 20030730001392003073000139SO 2003 7 30 SIMA200316004 120030528A532014521725013 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21648AE 145225 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED A NDT INSPECTION. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-036R1, FIG 5. (M) 2L72 4T RTT00011AT 20030421000272003042100027EA 2003 4 21 SWIA200311805 120030221A2797 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS TRIPPED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07589SW 7072 FLAP FAIL AFTER TAKEOFF. RETURNED TO FIELD. RESET CIRCUIT BREAKER 1F4 AND 2F4. OPS CHECK GOOD AFTER RESET OF CIRCUIT BREAKERS. 2L72 4F RTA21EA 20040223001902004022300190WP 2004 2 23 ABXA040028 120031230A5311591359577 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 CRACKED FRAME AT LONGERON 2 LT, STA. 1076. REPLACED SECTION OF FRAME BETWEEN LONGERON 3 LT AND 3 RT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040226000292004022600029NM 2004 2 26 ASAA0310675 120031222A521090100721 SNUBBER BOEING737 737210C 1384459NM L1 DOOR DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 JNU - DURING OPERATION OF L1 DOOR, DOOR WAS FOUND TO BE DIFFICULT TO OPEN. REPLACED THE L1 DOOR SNUBBER AND LUBED ACCESS POINTS, THEN DOOR OPERATED NORMALLY. (M) 2L72 4F A16WE 20030827001082003082700108NM 2003 8 27 CALA0300469 120030816A5522 SKIN BOEING737 737524 1384721NM LT ELEVATOR GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714629 27533 INSPECTION FOUND SKIN UPPER SURFACE OF LT ELEVATOR GOUGED. THE SKIN WAS REPAIRED IAW ECRA 5520-01335. 2L72 4F RTA16WE 20030828001022003082800102NM 2003 8 28 MWEA030319 120030821A532099365335 WEB DOUG MD88 MD88 3023688NM FUSELAGE TORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 COCKPIT SUB FLOOR HAS A .5 INCH HOLE TORN IN IT AT STATION 148 8 INCHES RIGHT OF AIRCRAFT CENTER LINE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030902001862003090200186NM 2003 9 2 03FDEA00974 120030626A7930JT8D15AQM ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D15A 52051NE NR 2 MALFUNCTIONED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO25236FE 21330 708951 AT FL330, NR 2 ENGINE OIL TEMP ROSE TO HIGH IN THE YELLOW RANGE. ADDING FUEL FLOW BY INCREASING THROTTLE DID NOT HELP. AFTER 15 MINS IN YELLOW BAND, SHUTDOWN NR 2 ENGINE IAW ENGINE FAILURE/SHUTDOWN CHECKLIST. WHEN THROTTLE RETARDED TO IDLE, NR 2 ENG OIL TEMP ROSE ABOVE RED LINE BY 10 DEGREES. SHUTDOWN SUCCESSFUL, LANDED AT KCLE WITH NO FURTHER INCIDENT. IAW WORK CARD 70TOOO2 REPLACED NO.2 ENGINE. 2L73 4F4 FRTA3WE E2EA 20030725000442003072500044EU 2003 7 25 CX7A194J0346 120030531A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT ENG TAILPIPE MALFUNCTIONED A CX7AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL03307CE 340B204 TAILPIPE HOT LEFT ENGINE ON THE CLIMBOUT. 2L72 4T RTA52EU 20030728000662003072800066NM 2003 7 28 SWAA031538 120030712A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 752, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030728001182003072800118NM 2003 7 28 SWAA031542 120030712A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 44. REPAIRED FLOORBEAM PER T1-453-037. 2L72 4F RTA16WE 20030806000052003080600005 2003 8 6 AGQA088274 420030707A2312064105430 TRANSCEIVER BELL 206 OH58A 1181579SW ALLSN 250C T63* 03002GL COCKPIT INOPERATIVE B AGQAO OTHER O OTHER NRNOT REPORTED 1 EA1354AG 7120721 TRANSCEIVER INOPERATIVE, WON'T TRANSMIT OR RECEIVE. 1G71 3U3 U H2SW E4CE 20030902000912003090200091SO 2003 9 2 SWIA200312144 120030624A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07568SW5862 5862 120343 EMERGENCY LIGHTS ROW 9B/C INOPERATIVE. REMOVED AND REPLACED ELBP (AFT) IAW MM 33-50-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20030903000752003090300075EA 2003 9 3 JBXA03015 120030716A2720 TRIM TAB CNDAIRCL600 CL6002B19 1900309EA RUDDER OUT OF TRIM A JBXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05593ML 7465 FLIGHT 5164 ON START OF TAKEOFF ROLL HAD TAKEOFF CONFIG WARNING AND RUDDER DISAGREE WARNING ABORTED TAKEOFF. FOUND RUDDER TRIM OUT OF RANGE. RESET RUDDER TRIM TO ZERO TAKEOFF CONFIG NORMAL AIRCRAFT CONTINUED IN SERVICE. 2L72 4F RTA21EA 20030903000812003090300081NE 2003 9 3 SWIA200312180 220030712A7261 ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT & RT OVERSERVICED A SWIAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07224SW 120294 AFTER SWITCHING FROM APU TO ENGINE BLEED, SMOKE FILLED THE AFT CABIN . SMOKE AND ODOR DISSIPATED GRADUALLY PRIOR TO LANDING. FOUND LEFT AND RIGHT ENGINES TO BE OVER-SERVICED. REMOVED 1 QT OF OIL FROM EACH ENGINE. RAN ENGINES AND AIRCONDITIONING PACKS IAW 21-00-00. NO SMOKE NOTED AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 20030812000742003081200074SW 2003 8 12 HEEA088596 120030721A3340G62504 SEARCH LIGHT BELL 412 412 1182202SW EXTERIOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 SEARCH LIGHT STAYS IN THE ON POSITION. SHOP REPAIR. 1G72 4U H4SW 20030807000262003080700026NM 2003 8 7 UIEA200300038 120030624A5312 PRESSURE PANEL BOEING747 7472D3B 1384805NM NLG WW CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15506MC 21252 DURING C-CHECK, NOSE GEAR WHEEL TOP AT BS 366 LBL 11 FOUND CRACK FROM EDGE AND EXTENDED INBOARD APPROXIMATE 1 INCH IN LENGTH. DEFECT FOUND DURING L-CHORD REPLACEMENT AT STATION BS 340, LBL 11.33. REPAIR CARRIED OUT AS PER BOEING TELEX SEP-SIN-03-40H AND 8110-3. TRIMMED CRACK AREA INCLUDING .030 INCHE INSURANCE CUT. PERFORMED HFEC INSPECTION TO INSURE CRACK FREE-CONDITION. INSTALLED THREE FILLERS AND A DOUBLER TO TOP PANEL WEB AND CHORD. (M) 2L74 4F RTA20WE 20030911000252003091100025NM 2003 9 11 03FDEA01102 120030709A5730 SKIN DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 RT WING UPPER SURFACE FOUND CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL. RT WING UPPER SURFACE CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL REPAIR CARRIED AS PER FEDEX EA 1-5720-69365 WINGS OUTER WING / RT OUTER AFT SKIN PANEL - CORROSION REWORK. 2L73 4F RTA22WE 20030731000572003073100057EA 2003 7 31 QXEA200300876 120030721A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 BOI-FORWARD CARGO BAY CENTER CHIMNEY IS TORN. REPLACED FORWARD CARGO BAY CHIMNEY WITH SERVICEABLE ONE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030912000422003091200042WP 2003 9 12 DHL2003604718 120030522A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING INBD L/E LOWER PLATING CRACKED 1.000, AROUND STA XFS 597.500. PERFORMED MAJOR REPAIR IAW EODHL-030527, ED-3290. REMOVED FASTENERS, PERFORMED STOP HOLE ON CRACK END USING 0.250 DIA DRILL IAW EODHL-030527, ED-3290. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER IAW EODHL-030527, ED-3290. CLEANED, TREATED AND PRIMED DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON LT OUTER WING INBD L/E LOWER PLATING AROUND STA XFS 597.500 USING NEW FASTENERS IAW EODHL-030527, ED-3290, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030916000912003091600091WP 2003 9 16 GTIA030659 120030827A2150 ACM DOUG DC9 DC982 3022082WP RIGHT ODOR A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23800NK 49144 WITH RIGHT AC PACK ON, OILY ODOR IN THE CABIN, ODOR CEASES WITH RIGHT PACK OFF, OIL FOUND ON SIDE PANELING AT THE END RIGHT OVERWING EXIT. INSPECTED RIGHT ACM FOUND VERY LITTLE, CLEANED OIL AND RAN ACM NO LEAKS NOTED, NO ODOR IN CABIN, OPS CHECKS NORMAL. (M) 2L72 4F A6WE 20030916001102003091600110 2003 9 16 AALA20030886 420030821A22102VA3925G1 ACTUATOR AIRBUS300 A300B4605R 3930308EU RUDDER DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2141063 506 EN ROUTE JFK-MIA, AIRCRAFT HAD OSCILLATIONS THAT WERE LATERAL IN MOTION. CREW DECLARED AN EMERGENCY AND AIRCRAFT RETURNED TO JFK WITHOUT FURTHER INCIDENT. REPLACED YAW DAMPNER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030930000582003093000058NM 2003 9 30 P5CA0300937 120030906A291019650176 HOSE BOEING747 747283B 1384867NM NR 1 ENGINE CHAFED A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23921FT 21575 ON MECHANIC PREFLIGHT FOUND HYD FLUID LEAKING FROM NR 1 ENG. REPAIRED PRESSURE LINE IAW 20-11-05 PERFORMED LEAK CHECK IAW 29-11-00. 2L74 4F A20WE 20030930001092003093000109NM 2003 9 30 03FDEA01491 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG CORRODED. 2L73 4F RTA22WE 20030116002792003011600279SW 2003 1 16 HEEA083139 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 MAIN ROTOR FLAP RESTRAINT STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030117000372003011700037NM 2003 1 17 QXEA0300088 120030115A3230471515 HARNESS BOMBDRDHC8 DHC8401 1390041NM ZONE 100 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM09401QX3796 4031 BOI - FLIGHT 2300 - THE CREW RETURNED TO FIELD, WHEN AFTER TAKEOFF, THE GEAR WOULD NOT RETRACT ONCE THE GEAR LEVER WAS SELECTED UP. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 2 NOSE LANDING GEAR WOW HARNESS. GEAR RETRACTION TESTS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030118000062003011800006SO 2003 1 18 C2XA03TY009 120030118A534014522161011 DOUBLER EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 TYS, During a scheduled inspection corrosion was found on the galley spar joint caps by the sevice door. Maintenance removed and replaced the doubler on galley forward sill, alodined, primed and painted. I/A/W-EMB-135/145-GST-1927/02A, CMP-51-21-04/05/06. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2L72 4T RTT00011AT 20030625000892003062500089NM 2003 6 25 F3LA200300066 120030218A5313 STRINGER BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED HEAVY CORROSION AT STR 27-L BETWEEN STA 945 AND STA 953.5. REPLACED STRINGER FROM STA 945 TO STA 967.5, LBL 3, STR 27-L, PER SRM 53-10-3, 51-20-2 AND 51-30-5. 2L72 4U RTA16WE 20030224001192003022400119NM 2003 2 24 CALA0300069 120030223A5330 SKIN BOEING757 757224 1384958NM STA 1510 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0926123 28966 INSPECTION FOUND FUSELAGE SKIN AT STA 1510 UNDER L/H AFT AIRPHONE ANTENNA CORRODED. INSTALLED REPAIR IAW SRM 53-00-01, FIGURE 204. 2L72 4F RTA2NM 20030227000332003022700033EU 2003 2 27 NSVA200300013 120030224A3200HP848430621 CONTROL VALVE SAAB SF340 340B 7860101EU MAIN GEAR INOPERATIVE A NSVAAO UNSCHED LANDING OTHER GJ MULTIPLE FAILURE WARNING INDICATION APAPPROACH 1 EA27299CJ 340B299 On Final into ORF from LGA: Crew selected gear down, with Hyd pump "ON", gear failed to extend. The gear in transient light remained on. Crew initiated emergency gear extension procedures as per checklist blowing the explosive bolts causing the gear to lower and lock. Pilot reported that aircraft landed with no nose wheel steering and had minimal breaking action. Captain reported normal operational use of brakes and steering during taxi check. MX R&R landing gear control valve IAW SAAB AMM Chapter 32-31-15. R&R Landing gear control handle IAW SAAB AMM 32-31-05-02. Op's check good. Aircraft returned to service. 2L72 4T RTA52EU 20030227001272003022700127GL 2003 2 27 HEEA084433 220030213A7261174000101 FILTER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE OIL WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 ENGINE OIL FILTER BYPASS INDICATOR WEAK. 1G71 3U3 U H2SW E1GL 20030305000922003030500092WP 2003 3 5 CALA0300092 120030303A5311 BELTFRAME DOUG DC9 DC981 3022081WP STA 1416 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1416, LONGERON 4L TO 4R. INSTALLED NEW FRAME IAW SRM 51-00. 2L72 4F A6WE 20030306000822003030600082SW 2003 3 6 HEEA084792 120030221A6730212076004101 SERVO BELL 412 412 1182202SW TAIL ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0321498 36003 TAIL ROTOR SERVO LEAKING IN STATIC POSITION. REPAIRED. 1G72 4U H4SW 20030310001502003031000150NM 2003 3 10 EIA2003018 120030227A5300UNK STRAP BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Lap repairs from STA 1460-2180 at Stringer 19R requires an additional strap. CORRECTIVE ACTION: Install external strap per ECRA 481-53-169-2 Rev A 2L74 4F A20WE 20030313001332003031300133WP 2003 3 13 AALA20030079 120030118A3397 WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21586AA 53249 DFW - DURING OVERNIGHT MAINTENANCE, WHILE TROUBLESHOOTING 21AB EMERGENCY EXIT LIGHT BATTERY DISCOVERED BROKEN WIRE ON PLUG. REPLACED EMERGENCY EXIT LIGHT BATTERY AND MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030121000702003012100070SW 2003 1 21 HEEA083270 120030108A6730206076031023 SERVO BELL 206 206B3 1181506SW FLIGHT CONTROL LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032753F14125 2729 FLIGHT CONTROL SERVO LEAKING. REPAIRED. 1G71 3U H2SW 20030121002562003012100256GL 2003 1 21 HEEA083366 220030109A731347101 FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE ERODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X3327 51552 WEAR ON OUTSIDE DIAMETER, CLEANED AND INSPECTED UNIT. FOUND INNER TIP ERODED. OVERHAULED NOZZLE. 1G71 3U3 U H2SW E4CE 20030319000772003031900077NM 2003 3 19 MEX2003035 120030213A2420 GCU DOUG MD80 MD83 3023681NM LEFT FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS652265393 49643 FLT 198 - MLM-TIJ - AIRCRAFT RETURNED TO GATE, FAIL LIGHT AC/CROSSTIE LOCK-OUT OFF RESET PROCEDURE WS PERFORMED AND LIGHT WAS TURN OFF, BUT LIGHT L GEN OFF APPEARS. GCU WAS NOT POSSIBLE RESET AND ENGINES WERE SHUTDOWN. REPORT WAS DEFERRED UNDER MEL 24-1-1 AND AIRCRAFT WAS REFUELED. DURING OVERNIGHT SERVICE, GENERATOR (P/N 976J252-8) AND GCU WERE CHANGED IAW MM 24-20-01, ALL CORRECT. (M) 2L72 4F RT 20030320000222003032000022 2003 3 20 USAASA03009 420030124A2565 SLIDE AIRBUSA319 A319112 3930323EU OVERWING MALFUNCTIONED A USAAD RETURN TO BLOCK JW WARNING INDICATION INADEQUATE Q C TXTAXI/GRND HDL 1 EA19730US 1182 DCA - FLT 393 - EN ROUTE DCA-NAS, THE OVERWING SLIDES WERE INDICATING NOT ARMED. THE AIRCRAFT RETURNED TO GATE. MAINTENANCE ARMED THE OVERWING SLIDES. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030327002002003032700200SW 2003 3 27 CA030211013 120030205A6300206040106001 SPRING BELL BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL MAIN DRIVESHAFT BROKEN W K NONE O OTHER ININSP/MAINT 1 CA AMN10463 (CAN) UPON DISSASSEMBLY OF DRIVESHAFT FOR ROUTINE SERVICING AND INSPECTION IN ACCORDANCE WITH BELL 206L-1 MM , SUBJECT SPRING WAS FOUND BROKEN AND DISLODGED WITHIN THE COUPLING HOUSING CAUSING DAMAGE TO BOTH THE SPHERICAL COUPLING SURFACE AND OUTER COUPLING.NO SIGNS OF COUPLING OVERHEAT NOR GREASE LEAKAGE WAS FOUND. DRIVESHAFT COUPLING COMPONENTS REPLACED WITH NEW PARTS. 1G71 3U3 U H2SW E1GL 20030324000842003032400084WP 2003 3 24 ARWA20030301 120030309A29103777589501 HOSE DOUG DC8 DC862 3021970WP HYD SYSTEM LEAKING A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19802BN 45909 IN FLIGHT LOSS OF HYDRAULIC QUANTITY OF PRESSURE; PERFORMED APPROACH CHECKLIST. FOUND HYDRAULIC PRESSURE HOSE LEAKING AT NR 2 ENGINE. REMOVED AND REPLACED HYDRAULIC HOSE ON HYDRAULIC PUMP IN ACCORDANCE WITH MM 20-12-0. SERVICE HYDRAULIC RESERVOIR IAW MM 12-30-1. OPERATIONAL CHECK FOR LEAK AND RUN UP. NO LEAK NOTED IAW MM 29-10-72 AND 71-00. 2L74 4F 4A25 20030324000932003032400093EU 2003 3 24 03083305 120030324A33501317 LAMP JETAIRJETSTMJETSTM4101 1500501EU A VTZAK NONE O OTHER ININSP/MAINT 1 EA27305UE 41019 During maintenance inspection, the fwd. overhead emergency light was found to be inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2L72 4T RTA41NM 20030324001282003032400128NM 2003 3 24 UPS03440336 120030305A5310 FITTING BOEING747 747200 1384847NM LH BS 1480 B/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C LH BS 1480 B/H - CRACKS REVEALED ON THE OUTER CHORD SPLICE FITTING HOLE #23 RUNNING I/B & O/B & ALL GREATER THAN 0.100" LONG. PLS REFER FIGURE ATTACH. OUTER CHORD SPLICE FITTING HOLE #23 CRACK OUT OF SB 747-53A2390 LIMIT FITTING REPLACED AS PER 747-53A2390 AND EO B747-5310-10732-I. 2L74 4F RTA20WE 20030417001852003041700185EA 2003 4 17 SWIA200311776 120030210A3244 TIRE CNDAIRCL600 CL6002B19 1900309EA NR 1 & 4 BLOWN A SWIAO OTHER O OTHER LDLANDING 1 NM07409SW 7056 NR 1 AND 4 MAIN TIRES FAILED ON LANDING. REMOVED AND REPLACED NR 1 AND 4 MAIN WHEEL ASSY. 2L72 4F RTA21EA 20030421001142003042100114NM 2003 4 21 ZW0A0302901 120030303A3350 BULB DOUG MD80 MD83 3023681NM EMERGENCY LIGHT BURNED OUT A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139414W 53189 TWO EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROW 4. REINSTALLED THE LAMPS INTO THE SOCKET AND OPERATED OK. CHECK-C 11-6-02 STL. 2L72 4F RT 20030421001322003042100132NM 2003 4 21 VNAA0302027 120030227A6120 PRESSURE SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT PROPELLER FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07460PS 3061 DURING FLIGHT, THE CREW RECEIVED A RIGHT HAND PROP OIL PRESSURE LOW CAS MESSAGE. ALL OTHER ENGINE INDICATIONS WERE NORMAL AND WITH MAINTENANCE CONTROL, CONCLUDED THERE WAS AN INDICATION PROBLEM. THE CREW REQUESTED PRIORITY HANDLING FROM PHL ATC THEN DIVERTED TO PHL AS A PRECAUTION. FLIGHT 4152 THEN LANDED WITH NO FUTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE OIL PRESSURE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030424000052003042400005 2003 4 24 SWIA200311829 420030313A22156225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CLCLIMB 1 NM07226SW7299 7299 120296 THE AUTOPILOT PITCHES UP AND DOWN DURING CLIMBOUT AND IN LEVEL FLIGHT ON BOTH FLIGHT DIRECTORS. REPLACED ELEVATOR SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040227000452004022700045NM 2004 2 27 ASAA0340354 120031208A5420311A151911 SUPPORT BOEING737 7374Q8 138447QNM NR 2 PYLON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01756AS 25097 GYR - DURING SI CHECK, FOUND NR 2 ENGINE PYLON OUTBOARD FAN COWL SUPPORT INBOARD AND OUTBOARD CHORD GOUGED. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20030828000272003082800027NE 2003 8 28 00094 220030530A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT X ENGINE FLAMEOUT CLCLIMB 1 SW05299TW 24D299 251679 PILOT REPORTED LT ENGINE FLAME-OUT WHILE CLIMBING THRU 41,300 FT. DESCEND AND RELIGHT PERFORMED. UPDATE AFTER MAINTENANCE. 2L72 4J4 J A10CE 1E16 20030828001982003082800198NM 2003 8 28 CALA0300477 120030822A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A .5 INCH CRACK IN MAIN DECK FLOOR SUPPORT AT STA 540, BL 0 TO LEFT I/B SEAT TRACK. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030731001392003073100139NM 2003 7 31 QXEA200300916 120030723A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09357PH* 450 504 PDX- ON FLIGHT 2052 PORTION OF EMERGENCY TRACK LIGHTING INTERMITTENT. REMOVED AND REPLACED BATTERIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030806000882003080600088SO 2003 8 6 C2XA03TY106 120030801A534714530658003 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION SEAT TRACK RF2 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW-EC5340-01048. 2L72 4F RTT00011AT 20030806001432003080600143NM 2003 8 6 AWXA200300820 120030709A5315D53472189202 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292 AT FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM 1292 AT FR 68; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20030902001772003090200177GL 2003 9 2 2003F00428 320030714A6111114HCA0 BLADE MCAULY B5JFR36C1103JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR36B5JFR36C1103GL PROPELLER CRACKED B O OTHER O OTHER NRNOT REPORTED 1 SO05 15090622 940863 940863 PROPELLER WAS REMOVED AND SENT TO PIEDMONT AVIATION COMPONENT SEVICES (REPAIR STATION QWPR503X)FOR VIBRATION /MCCAULEY ALERT SERVICE BULLETIN 246. DURING DISASSEMBLY FOUND OIL IN NR 4 BLADE BORE DUE TO NICK IN PLUG SEAL, LEADING TO BELIEVE THE CAUSE OF VIBRATION. UPON FLUORESCENT PENETRANT INSPECTION FOUND NR 2 BLADE P/N 114HCA-0, S/N NC033 (T.S.N. 15,090.86; T.S.O. 622.15) WITH AN INDICATION PER MCCAULEY ASB 246B/REV 2. 2L72 4T RTA41NM 6 CP15NE 20030829001222003082900122NM 2003 8 29 SWAA031807 120030811A53126545819121 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W UPPER WEB CRACKED AT THE LT/RT TIRE BRAKE ATTACH HOLES. REPAIRED UPPER WEB PER SWA EA. 2L72 4F RTA16WE 20030903001992003090300199NM 2003 9 3 AALA20030686 120030624A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21373AA 25200 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 24B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 24B. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030905001552003090500155NM 2003 9 5 DLM88030663 120030718A3222 SCHRADER VALVE DOUG MD88 MD88 3023688NM NLG LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27988DL 53339 ON TAKEOFF NLG DID NOT APPEAR TO RETRACT, HAD RED UNSAFE LIGHT ILLUMINATED. RAN POM PROCEDURE NLG REMAINED UNSAFE IN RETRACT POSITION-REPLACED NLG SCRADER VALVE FOR LEAKING. 2L72 4F RTA6WE 20030904001742003090400174NE 2003 9 4 AALA20030638 220030602A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RIGHT FAILED A AALAF ACTIVATE FIRE EXT. Y ENGINE STOPPAGE TOTAKEOFF 1 SW21469AA 49599 709969 TPA - FLT 1525 - AT TPA ON TAKEOFF ROLL, ENGINES APPROACHING TAKEOFF THRUST, RIGHT ENGINE FAILED. EGT EXCEEDED 700 C DEGREES. FIRE BOTTLE NR 2 WAS USED. REPLACED NR 2 ENGINE. ACCOMPLISHED TRIM RUN UP AND LEAK CHECK. REPLACED NR 2 FIRE BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 F A6WE E9NE 20030905001772003090500177EA 2003 9 5 ASOA03365 120030808A3350BF10044004 SIGN CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11844AS 7317 FLT 4784 - DURING A GROUND INSPECTION IN ATL, AN EMERGENCY FLOOR LIGHT STRIP, SERVICE AND PASSENGER DOOR EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030805000682003080500068EU 2003 8 5 ASOA03250 120030604A5320 DOUBLER AEROSPATR72 ATR72 EU PAX DOOR STEP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD PASSENGER/CREW DOOR FIRST STEP SUPPORT DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE FORWARD PASSENGER/CREW DOOR FIRST STEP SUPPORT DOUBLER IAW ASA EO 72-52-0070. (M) 2H72 4T RT 20030807000472003080700047EA 2003 8 7 COMA0360344 120030801A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SO01912CA22781 7011 FLIGHT 5878 GEAR DISAGREE WARNING DURING CRUISE FLIGHT. REPLACED THE PSEU. 2L72 4F RTA21EA 20030812000902003081200090EU 2003 8 12 HEEA088630 120030719A32131175000211 SKID BOLKMS117 BK117A1 5626010EU MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC 7152 WORN EXCESSIVELY THROUGH TO BASE METAL. SCRAPPED. 1G72 3U H13EU 20030729000342003072900034EA 2003 7 29 03196698BR 120030715A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27698BR 7799 DURING CRUISE THE FLIGHT CREW REPORTED LAV SMOKE INDICATION. AS A PRECAUTION FLIGHT WAS DIVERTED TO GRR. AIRCRAFT LANDED WITHOUT INCIDENT. PASSENGERS DEPLANED, MAINTENANCE PERSONNEL FOUND LAV SMOKE DETECTOR INOPERATIVE. SMOKE DETECTOR WAS REMOVED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICED NORMALLY AT GATE. 2L72 4F RTA21EA 20030730000142003073000014WP 2003 7 30 ABXA030211 120030527A5347S49258487075 SEAT TRACK DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 SEAT TRACK BUTT LINE '0' WAS CORRODED, FS 541 TO FS 619. REPAIRED SEAT TRACK, BUTTLINE '0', FROM STA 160 TO STA 645 IAW DC-9 SRM. 2L72 4F A6WE 20030825000382003082500038WP 2003 8 25 UPS03840886 120030616A5720 STIFFENER DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C3 LEFT WING TE. VERTICLE STIFFNER IS CRACKED PAST STOPDRILL AT XW 0 REMOVED EXISTING DOUBLER,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED FILLER AND REINSTALLED REPAIR DOUBLER I.A.W. DC8-5720-7767-A 2L74 4F RT4A25 20030825001692003082500169WP 2003 8 25 DHL2003873519 120030620A5347S2772660 SEAT TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE WORN A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01873SJ83849 46091 ITEM REF.: N/R 0843.: MAIN CARGO COMPT NR 5 TRACK LUG WORN BETWEEN STA.1680.000 AND STA.1695.000. CUT OUT NR 5 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG.49-50. FABRICATED SPLICES (7075-T6 0.160) IAW SRM 53-2-3 PG.49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG.49-50, SRM 51-3-0 PG.1. 2L74 4F4 FRT4A25 E2GL 20030827001172003082700117NM 2003 8 27 CALA0300455 120030808A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND CHORD CORRODED AROUND NUTPLATE HOLE AT FS 967, LBL 42. AN UPPER CHORD REPAIR WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20030910001992003091000199NM 2003 9 10 UIEA200300045 120030819A36103206257 RELIEF VALVE BOEING747 747212B 1384886NM NR 4 ENGINE DEFECTIVE A UIEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA15808MC 21048 MIP/POS-AIR TURNBACK, AFTER T/O AND DURING CLIMB, NR 4 ENGINE FIRE WARNING CAME ON. WHEN NR 4 THROTTLE WAS CLOSED THE TEMP WENT BACK TO NORMAL. THROTTLE WAS ADVANCED AGAIN THE TEMP STARTED TO GO UP. NOTICED HIGH STAGE BLEED VALVE LIGHT, ON AND OFF. CLOSED NR 4 BLEED VALVE AND TEMP STAYED NORMAL WHEN THROTTLE WAS ADVANCED. RETURNED TO MIA. SECURED CLAMP FOUND LEAKING AT REGULATOR VALVE. LOCKED OUT HIGH STAGE VALVE PER DDPG. RAN ENGINE IAW MM 71-00-00. ALL CHECKS NORMAL. R&R NR 4 ENGINE HIGH STAGE VALVE IAW MM 36-11-05. OPS AND LEAK CHECK OK. R&R NR 4 ENGINE HIGH STAGE ELECTRICAL CORE HARNESS. OPS CHECK OK. R&R NR 4 ENGINE PRV IAW MM 36-11-03. LEAK CHECK OK. PERFORMED ENGINE RUN PER MM 71-00-00. ALL OK. (M) 2L74 4F A20WE 20030912001282003091200128NM 2003 9 12 AWXA200300895 120030711A53126516300512 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 14, WL 218.5. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD WEB AT LBL 14, WL 218.5; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, FIG 209, PG 265-274. 2L72 4F RTA16WE 20030926001572003092600157NM 2003 9 26 HNAA0300043 120030825A3350 CONNECTOR DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT DISCONNECTED A HNAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA07966HA 452 CREW REPORTED RED FLOOR EMERGENCY LIGHTS WERE INOP AT MID CABIN. FOUND WIRE DISCONNECTED AT CONNECTOR. RESECURED WIRE. 2H72 4T RTA13NM 20030930000692003093000069EU 2003 9 30 MALA030404 120030823A3150005WS00 WEU SAAB SF340 340B 7860101EU LT ENGINE MALFUNCTIONED A MALAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15441XJ 340B441 DURING FLIGHT 2925, WHEN RT ENGINE WAS STARTED THE LT ENGINE FIRE LIGHT ILLUMINATED. MAINTENANCE REPLACED WEU IAW SF340-MM 31-50-05-4 PN OFF/ON 005WS00, SN/OFF 1463, SN/ON 1301. STARTED RT AND LT ENGINES OPS CHECK GOOD IAW SF340 MM-31-50-00. 2L72 4T RTA52EU 20031003000082003100300008EU 2003 10 3 AALA20030907 120030827A3610 CLAMP AIRBUS300 A300B4605R 3930308EU EQUIP BAY LOOSE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW2150051 459 AFTER TAKEOFF SMOKE OR BURNING SMELL IN CABIN DETECTED. CREW DECLARED AN EMERGENCY AND RETURNED TO BOG WITHOUT FURTHER INCIDENT. TIGHTENED SEVERAL PNEUMATIC DUCT CLAMPS. SWAPPED MINIMUM EQUIPMENT BAY DETECTOR WITH ZONE 125 DETECTOR. HISTORY OF HOT FLOORS AND LEAKS AND APU BLEED ON MEL. SYSTEM LEAK AND OPS CHECK NORMAL. (M) 2L72 4F RTA35EU 20030908002462003090800246 2003 9 8 SWIA200312353 420030825A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07251YV6776 5420 120251 F/O AUTOPILOT FAILING AFTER 2 MINUTES INFLIGHT. INDICATION LIGHTS: R & E AMBER, FCP AP, GLARE AP FLICKERING DURING FAILURE. REPLACED NR 2 AUTOPILOT COMPUTER. OPS CHECK GOOD. 2L72 4T RTA31SO 20031003000092003100300009NM 2003 10 3 AALA20030929 120030827A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 AFT GALLEY EMERGENCY LIGHT CROSSOVER WAS INOPERATIVE. BATTERY PACK FAILED DUAL FEED CHECK. SECURED WIRING AND REPLACED THE LENS COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031021002012003102100201NM 2003 10 21 AALA20030501 120030425A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21182AN 29592 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING FROM ROW 16D-32D INOPERATIVE. SECURED EMERGENCY EXIT PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031027000742003102700074EU 2003 10 27 MALA030432 120030919A2150 A/C PACK BAC 146 AVRO146RJ85A1500097EU NR 1 & 2 SMOKE A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15504XJ E2311 AFTER STARTING APU AND TURNING ON PACK 1 & 2 CREW NOTICED SMOKING AND ODOR. MAINTENANCE PERFORMED PACK BURN PROCEDURE AS REQUIRED. NUMBER 1 & 2 PACKS ALL CHECKS GOOD AT THIS TIME. REF AVRO AMM CHAPTER 36/21 SUNSTRAND APU MM. 2H74 4F RTA49EU 20031029000172003102900017EU 2003 10 29 ASOA03468 120030930A33503012000 POWER SUPPLY AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 FLT 4517 - DURING A GROUND INSPECTION IN MGM, AN OVERHEAD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHTS POWER SUPPLY AT 61 WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031029000962003102900096NM 2003 10 29 0301846634 120030925A2530 COFFEEMAKER BOEING747 747227B 1384888NM GALLEY BURNED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01634US 22234 DURING FLIGHT, AN ELECTRICAL BURNING ODOR EMITTED FROM THE NBR 2 AFT COFFEEMAKER. PULLED CIRCUIT BREAKER AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED COFFEEMAKER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040128000312004012800031NM 2004 1 28 03FDEA02223 120031221A5753ARC2517501 STRAP DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING - INBD FLAP OUTBD HINGE (FLAP SIDE), INBD STRAP, PIVOT POINT BORE CORRODED. LEFT WING - INBD FLAP OUTBD HINGE (FLAP SIDE), INBD STRAP REMOVED AND REPLACED AS PER SRM 51-33-01, VOL II AND AMM 20-50-02. 2L73 4F RTA22WE 20030910000732003091000073WP 2003 9 10 DHL2003604638 120030531A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 INTERIM REPAIR ON UPPER SKIN OF LT INBOARD FLAP, BETWEEN STA XW.2.000 - XW.91.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030566, ED-3396. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030566, ED-3396. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-030566, ED-3396. CLEANED, TREATED AND PRIMED NEW SKIN PANEL IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON LT INBOARD FLAP UPPER SURFACE, STA XW 2.000 - XW 91.000 WITH NEW FASTENERS IAW EODHL-030566, ED-3396 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031027001362003102700136NM 2003 10 27 PCAA0309117 120030926A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13811AW 201 DURING ROUTINE MAINTENANCE VISIT IT WAS DISCOVERED THAT THE FIRST EMERGENCY FLOOR LIGHT HAD A BROKEN WIRE. WIRE WAS RESPLICED, AND THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031106001862003110600186SO 2003 11 6 C2XA03SH386 120031014A531514522459000 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10 FIGURE 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031107000332003110700033EA 2003 11 7 QXEA200301392 120031104A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09603QX 10011 BOI- ON FLIGHT NUMBER 2458, BURNING OIL SMELL IN AIRCRAFT CABIN WITH APU IN OPERATION AND BLEED AIR EXTRACTION. OIL SMELL WENT AWAY WITH APU SHUTDOWN. RAN APU SEVERAL HOURS WITH BLEEDS ON IN DIFFERENT CONFIGS. NO OIL SMELL OR HOT OVERHEAT SMELL AT ANY TIME. APU OIL LEVEL CHECKS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031107000992003110700099NM 2003 11 7 03309402 120031105A2121AE1716D02 COOLING FAN DORNERDO32 DO328300 NM CABIN FAILED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27402FJ 3147 DURING FLIGHT 6276 TAXI SMOKE WAS IDENTIFIED IN THE CABIN. EMERGENCY WAS DECLARED AND PASSENGER WERE DEPLANED ON TAXIWAY. THE GROUND COOLING FAN WAS IDENTIFIED AS THE CAUSE AND WAS SUBSEQUENTLY REPLACED. 2H72 4T RTA55NM 20031110001222003111000122 2003 11 10 AWXA200301344 420031102A2565D30664105 SLIDE AIRBUS320 A320231 3930325EU L-1 DOOR FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW3305 893 091 PHX - EEL - DURING INSPECTION EMERGENCY LIGHT TEST FAILED STEP 7 OF T/C R1A25301. MAINTENANCE REMOVED AND REPLACED L-1 DOOR SLIDE IAW T/C R1C25304, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030911000292003091100029EA 2003 9 11 SWIA200312317 120030802A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 PAX DOOR HANDLE IS CRACKED. (DISCOVERED DURING C-CHECK) PAX DOOR HANDLE REMOVED, SANDED, PRIMED, PAINTED AND INSTALLED IAW MM 52-11-03-400-801. 2L72 4F4 FRTA21EA E15NE 20040112000922004011200092WP 2004 1 12 GTIA031002 120031113A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND CABIN METAL FLOOR PANEL IS CRACKED AT FS 389 RIGHT OUTBOARD PANEL. REMOVED CABIN FLOOR PANEL. TRIMMED OUT DAMAGE. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. INSTALLED RIGHT OUTBOARD FLOOR PANEL. (M) 2L72 4F A6WE 20031119000142003111900014WP 2003 11 19 UPS03841371 120030925A5712 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, RT WING LE. RIBS CRACKED AT XFS760 UPPER,XFS 766.25 UPPER, XFS 822.5 LOWER STOP DRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATE CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. 57-2-0 FIG. 2 2L74 4F4 FRT4A25 E2GL 20040113001752004011300175WP 2004 1 13 AALA20031471 120031225A3397 WIRE DOUG DC9 DC982 3022082WP CABIN CHAFED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21291AA 49303 DFW SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT ROWS 20 TO 31. REPAIRED CHAFFED WIRE ON EMERGENCY LIGHTING FOR SEAT ROWS 20 TO 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031215001332003121500133WP 2003 12 15 AALA20031173 120031021A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21289AA 49301 DFW - MAINTENANCE OBSERVED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY INOPERATIVE AT SEAT 9D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031217001632003121700163 2003 12 17 AWXA200301536 420031114A2565416N21133 BLOCK BOEING757 7572G7 1384963NM GIRT BAR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28908AW 24233 DURING C-12 CHECK CORROSION WAS FOUND ON THE L-1 DOOR GIRT BAR CENTERING BLOCK. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR GIRT BAR CENTERING BLOCK IAW B757-200 SRM 51-40-02, PG 1, PARA 9A & 9B. 2L72 4F RTA2NM 20031223001552003122300155SO 2003 12 23 C2XA03SH494 120031213A532014525480003 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031222001202003122200120WP 2003 12 22 2003F00648 120030908A520059260033 DOOR DOUG DC9 DC915F 3022037WP AFT CARGO COMPT DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 FOUND DURING 4C CHECK, AFT CARGO COMPARTMENT BARRIER DOOR, DAMAGED INNER AND OUTER SKIN AND HONEYCOMB CORE. DAMAGED PARTS WERE REPLACED BY NEW ONE. (M) 2L72 4F A6WE 20031229001362003122900136 2003 12 29 SWAA032731 420031214A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING RON, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031007000022003100700002 2003 10 7 AALA20030399 420030402A2565 BOTTLE BOEING767 767223 1385123NM ESCAPE SLIDE MALFUNCTIONED A AALAK NONE O OTHER ININSP/MAINT 1 SW21316AA 22318 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FORWARD ENTRY SLIDE DID NOT INFLATE. REPLACED EMERGENCY EXIT SLIDE DOOR ASSIST BOTTLE AND REINSTALLED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040106001282004010600128NM 2004 1 6 AT0300037 120031218A3350 BATTERY BOEING717 717200 1383700NM CABIN DISCONNECTED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15955AT 55017 GALLEY AND STATION 218 EMERGENCY LIGHTS INOP. FOUND BATTERY UNPLUGGED FROM B5-259. RECONNECTED, OP CHECK OK. 2L72 4F TRA6WE 20031125000052003112500005WP 2003 11 25 DHL2003802506 120031106A5712 FRAME DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING L/E FORMER CRACKED 1.000 STA XFS 333.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. STOP DRILLED CRACK AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031203000492003120300049NM 2003 12 3 GAIA03155ST 120031024A5347BAC1520792 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED BS 870 TO 1010 LBL 24.75. REF FASI N/R NR 61884, REPLACED SEAT TRACK BS 870 TO 1010 LBL 24.75 PER B727 SRM 53-10-5 FIG 1. (M) 2L73 4F RTA3WE 20040115001352004011500135NM 2004 1 15 DL75K031100 120031217A3397 WIRE HARNESS BOEING757 757232 1384965NM CABIN DISCONNECTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO276703D 30234 FOUND ON INSPECTION SEAT 34D EMERGENCY TRACK LIGHTING INOP. FOUND SEAT HARNESS DISCONNECTED. RECONNECTED HARNESS LIGHT, OPS GOOD. 2L72 4F RTA2NM 20040122000512004012200051EA 2004 1 22 ASOA03623 120031203A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUTOUT ON THE LEFT AND RIGHT SIDES AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE SKIN AT THE NOSE LANDING GEAR CUTOUT ON THE LEFT AND RIGHT SIDES AT FS 235 IAW ASA EO 600-53-0104. (M) 2L72 4F RTA21EA 20031203001612003120300161WP 2003 12 3 AALA20031021 120030918A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROWS 8 THROUGH 10. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031208000892003120800089NM 2003 12 8 QXEA200301321 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 LEFT OUTBOARD TRACK NR 3 SEAT ATTACH AREA CORROSION TOP APPROXIMATELY X525.00. REPAIRED IAW RD 8-53-1342 AND DHC-8 SRM 51-20-16 AND 51-20-26. 2H72 4T RTA13NM 20031209000462003120900046NM 2003 12 9 P5CA0300975 120031029A1430BACB30MTG BOLT BOEING747 747283B 1384867NM BULKHEAD SHEARED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 BODY STATION 2360 - (AFT PRESSURE BULKHEAD) TWO SHEARED BOLTS AT STRINGERS 11R & 20R. REPLACED BROKEN BOLTS - DETAILED VISUAL INSPECTION AND TORQUE CHECK REMAINING BOLTS - FOUR BOLTS FOUND BOTTOMED OUT. ADDED WASHERS AND RETORQUED PER SB 747-53A2474. 2L74 4F A20WE 20031209002112003120900211 2003 12 9 SWIA200312561 420031029A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER MALFUNCTIONED A SWIAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 NM07563SW8580 8580 120338 F/O'S STICK SHAKER (CLACKER) ON TEST FUNCTION WEAK AND SOMETIMES NOTHING AT ALL. REPLACED F/O'S STICK SHAKER. OPS TEST GOOD. 2L72 4T RTA31SO 20030923000132003092300013CE 2003 9 23 XTA200300097 120030822A3234 SELECTOR CESSNA650 650 2076802CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 GL07789QS 6507089 AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT, THE LANDING GEAR HANDLE WOULD NOT MOVE UP. ACCOMPLISHED AIR TURN BACK TO DSM, AIRCRAFT LANDED WITHOUT INCIDENT. ITEM IS UNDER INVESTIGATION. 2L72 4F A9NM 20030922000972003092200097WP 2003 9 22 DHL2003809001 120030912A3350 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01604AL 46047 DURING PREFLIGHT EMERGENCY EXIT LIGHTS AND STANDBY ATTITUDE INDICATOR WERE FOUND INOPERATIVE. TROUBLESHOT SYSTEM, FOUND EMERGENCY LIGHTS NOT GETTING ENOUGH POWER FROM AC BATTERY. REPLACED AC BATTERY. SYSTEM OPS CHECKED GOOD IAW 33-50-0. 2L74 4F RT4A25 20040128001612004012800161NM 2004 1 28 QXEA200301605 120031220A5410 MOUNT DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- LOWER INNER TRUSS MOUNTS TUBE HAS FIVE CHAFE SPOTS IN A FOUR INCH AREA NEAR FUEL FLOW TRANSMITTER. REPAIRED IAW HORIZON AIR EA 2-54-198. 2H72 4T RTA13NM 20040203000132004020300013WP 2004 2 3 ASAA0380555 120030816A335060030451 LIGHT DOUG DC9 DC983 3022083WP ROW 26 INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 PDX LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FOUND INOPERATIVE AT ROW 26. REPLACED ASSOCIATED BATTERIES. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040203003282004020300328EA 2004 2 3 MASA200300485 120031212A3260 BRACKET CNDAIRCL600 CL6002B19 1900309EA PROX SENSOR OUT OF ADJUST A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0737228 7228 ASH 6075 LAS, AIRCRAFT RETURNED TO FIELD REPORTING NLG DISAGREE AND GEAR DOOR WARNING MSG IN-FLIGHT DURING GEAR RETRACT. A/C BEING FERRIED TO PHX FOR MX 12/12/2003. MX ADJUSTED THE PROX CENTERING BRACKET. OP CHECKS GOOD, NO PARTS USED. 2L72 4F RTA21EA 20040205000092004020500009CE 2004 2 5 GLBA2003148 120031113A2750SM50D7 RELAY BEECH 1900 1900D 1154162CE TE FLAP STUCK A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03220GL UE220 FLAPS STUCK AT 17 DEG, REMOVED AND REPLACED FLAP RELAY PN SM50D7. OPS CHECKS GOOD. 2L72 4T RTA24CE 20040401000202004040100020NM 2004 4 1 AALA20031151 120031014A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21698AN 26980 SEA - MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH FLOOR LIGHT INOPERATIVE AT SEAT 25D. RESEATED CONNECTOR AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031212000252003121200025 2003 12 12 SWAA032421 420031031A2565D31354 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20031212000782003121200078EU 2003 12 12 MALA030495 120031106A3150006WS00 WEU SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15442XJ 340B442 DURING FLIGHT 3177, LEFT BLEED LEAK LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED WEU P/N ON OFF 006WS00,S/N ON 1576, S/N OFF 1584, IAW SAAB MM 31-50-05-4. CHECKS GOOD REF 409CARD 215389, SEE CONTINUATION CARD 067901 FOR FURTHER DETAILS. 2L72 4T RTA52EU 20031212000902003121200090NM 2003 12 12 SWAA032407 120031101A52406545871 DOOR FRAME BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20040525000422004052500042EU 2004 5 25 2004F00132 120030916A5347D5311281403501 SEAT TRACK AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND SEAT TRACK CORRODED BETWEEN FRAMES 20 AND 21 AT RBL 32. REMOVED AND REPLACED SEAT TRACK FROM RBL 32, FRAME 12 TO 24. (M) 2L72 4F RTA28NM 20030311000892003031100089EA 2003 3 11 COMA0360136 120030309A5610NP1393221 WINDOW CNDAIRCL600 CL6002B19 1900309EA L/H CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01973CA15823 7146 FLIGHT 5788 PILOTS SIDE WINDOW CRACKED.REPLACED WINDOW 2L72 4F RTA21EA 20030313001402003031300140NE 2003 3 13 GTIA020035 220030202A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217A 52053NE NR 2 MALFUNCTIONED A GTIAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL23809NK 49503 726974 DTW - FLT 313 - AFTER START AND PRIOR TO TAXI, RIGHT ENGINE N2 DROP TO 44 PERCENT, N1 19 PERCENT, AND EGT 535 DEG. RETURNED TO GATE. NR 2 ENGINE REQUIRES CHANGED IN REF TO LOG PG 91117-1. REMOVED AND REPLACED NR 2 ENGINE IAW MD80 MM 71-00-00. LEAK CHECKED GOOD. (M) 2L72 4F4 FRTA6WE E9NE 20030314000352003031400035NM 2003 3 14 2003740521 120030221A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT, WEB AT C-2 DOOR LOWER CUTOUT STR 27R HAS SPOTS OF CORROSION WITH EXFOLIATION AND CRACKING UNDERNEATH FITTING STA 950F. REMOVED AFT CARGO COMPT WEB AND DOOR LOWER STR 26R FOR REPAIR IAW SRM 51-30-2, FABRICATED NEW WEB DIMENSIONS 5 FT X 4.5 FT USING 7075 T6 .063 PO 9911918 IAW SRM 53-10-2 FIG 6. ALODINED AND PRIMED NEW WEB IAW SRM 57-10-2. INSTALLED NEW WEB IAW SRM 51-30-2. 2L73 4F RTA3WE 20030314002102003031400210WP 2003 3 14 0300401239 120030306A7830 COWLING DOUG DC10 DC1030 3023501WP NR 2 THRUST/REV SEPARATED A NWAAO OTHER D INFLIGHT SEPARATION LDLANDING 1 GL01239NW* 8328 48290 DURING LANDING A PORTION OF THE NR 2 ENGINE RT THRUST REVERSER TRANSLATING COWL SEPARATED FROM THE AIRCRAFT. THE SEPARATED PART CAME TO REST ON THE RUNWAY. THE AIRCRAFT CONTINUED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE RT THRUST REVERSER ASSEMBLY. 2L73 4F A22WE 20030314002202003031400220EA 2003 3 14 03053664 120030222A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT EMER LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27664BR 7528 LEFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE 2L72 4F4 FRTA21EA E15NE 20030327000802003032700080 2003 3 27 C1HA200397009 420030212A3422 INDICATOR BOEING727 727270 138408PNM COCKPIT INOPERATIVE A C1HAO OTHER O OTHER CLCLIMB 1 GL15697CA 23052 CAPTAINS HORIZONTAL SITUATION INDICATOR FLAG IN SIGHT (DIVERSION). REPLACED NR 2 DIRECTIONAL GYRO. 2L73 4F RTA3WE 20030422000462003042200046SO 2003 4 22 ASOA03065 120030217A33971317 WIRE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11261AS 120141 FLT 4241 - DURING A GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP AND REPAIRED A BROKEN WIRE (P/N M22759209) TO THE LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 20030327002012003032700201SW 2003 3 27 CA030212002 120030210A2435301792KDN CONNECTOR BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL STARTER GEN CORRODED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE GEN LIGHT CAME ON AND WOULD NOT RESET. ON INSPECTION AFTER MUCH TROUBLE SHOOTING, PIN 'B' ON THE MAIN STARTER/GENERATOR CONNECTOR PLUG IN THE ENGINE COMPARTMENT WAS THE PROBLEM. THE LOCKING MECHANISM FOR PIN 'B' WAS NOT HOLDING THE FEMALE END OF THE PIN IN PLACE AND ALLOWED THERECEPTACLE TO MOVE BACK. THE MALE END HAD APPROXIMATELY 1/8' ENGAGEMENT AND SHOULD HAVE HAD 1/2 INCH ENGAGEMENT. WHEN TROUBLE SHOOTING THE PROBLEM THE GENERATOR WAS PRODUCING 28 VOLTS ON THE GENERATOR SIDE OF THE LINE CONTROL RELAY BUT THE GENERATOR WOULD NOT COME ON LINE AND CHARGE THE BATTERY OR SUPPLY THE AIRCRAFT SYSTEMS. THERE WAS ENOUGH CONTACT ON THE PIN 'B' TO HAVE THE GENERATOR COME ONLINE ON A COLD START BUT1G71 3U3 U H2SW E1GL 20030801000152003080100015EU 2003 8 1 2003F00496 120030515A5753 TRACK AIRBUS320 A320233 3930329EU T/E FLAP FAIRINGDENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND LEFT WING FAIRING TRACK, 533CB INTERIOR, DENTED. REPAIRED FAIRING TRACK IAW SRM 51-77-12 PAGE 10, FIGURE 3. (M) 2L72 4F RTA28NM 20030805001142003080500114SO 2003 8 5 SIMA200319705 120030710A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21814AE 145541 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTIN OF OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND EXTERNAL ANGLE, ANGLE, FILLER, AND TWO SHIMS. REPAIR DONE IAW EMB SRM 53-21-10 AND CPM 51-61-00. (M) 2L72 4F RTT00011AT 20030423001612003042300161EU 2003 4 23 MALA030200 120030314A5310 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15367PX 340B271 RT FUSELAGE HAS 2 DENTS AT STA 315, BETWEEN SL1615 AND SL1617. MAINTENANCE COMPLETED REPAIR IAW EO S53143. 2L72 4T RTA52EU 20030423001792003042300179NM 2003 4 23 VNAA0303019 120030316A7931 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE TRANSDUCER FAILED A VNAAO OTHER N FALSE WARNING CLCLIMB 1 GL07471PS 3007 DURING CLIMBOUT, THE CREW HAD NO OIL PRESSURE INDICATION ON THE LEFT HAND ENGINE AND RETURNED TO DAY. MAINTENANCE INSPECTED AND FOUND A DIRTY TRANSDUCER CONNECTOR AND A POPPED CIRCUIT BREAKER. MAINTENANCE THEN CLEANED THE CONNECTOR AND RESET THE CIRCUIT BREAKER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030424000282003042400028WP 2003 4 24 ZW0A0303204 120030317A3350 LENS DOUG DC9 DC983 3022083WP EMERGENCY LIGHT MISSING A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13979TW 53629 THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROW 11 TO 14, AND THE EGRESS LIGHT LENS WAS MISSING AT THE LEFT SIDE NUMBER 2 CABIN DOOR. REPLACED LAMP MODULE P/N 7732 AT ROW 10, AND REPLACED THE MISSING LENS P/N 0105607-301. CHECK-C 10-11-02 STL. 2L72 4F RTA6WE 20030723000352003072300035WP 2003 7 23 MEX2003247 120030617A27801969135 PULLEY DOUG DC9 DC982 3022082WP SLAT DRIVE FAILED A ASMFK NONE O OTHER ININSP/MAINT 1 SW23491SH 49150 DURNG SLATS CABLE ADJUSTMENT WAS FOUND RUBBING BETWEEN CABLE PULLEYS OF SLAT NR '0', LOCATED IN THE RT OF THE SLAT DRIVE MECHANISM. BOTH PULLEYS WERE REPLACED AND GAINED ENOUGH SEPARATION. CABLE DEFLECTION WAS MEASURED, FOUNDED 25/34 INCHES, WITHIN LIMITS IAW MM CHAPTER 27-00-00 PATE 208A. (M) 2L72 4F A6WE 20030826001082003082600108NM 2003 8 26 S03853022 120030513A5330 SKIN BOEING737 737800* NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED W SAJFO OTHER O OTHER TXTAXI/GRND HDL 1 WP03 29106 B-18611 FUSELAGE SKIN FLUSH REPAIR LOCATED BETWEEN STA. 360 TO 380 / S-20R TO S-21R. REPAIR IAW EO 738-53-00-0021. TO MEET REQUIREMENT OF CCAA AD 2003-03-020. 2L72 4F4 FRTA16WE E2GL 20030826001562003082600156WP 2003 8 26 MEX2003336 120030208A793042D1091A PRESSURE SWITCH DOUG DC9 DC983 3022083WP LT ENGINE FAILED A ASMFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW23838AM 49397 FLT 944 - CUN-MEX - AIRTURN BACK, FILTER OBSTRUCTED LEFT ENGINE LIGHT CAME ON. DURING REVISION, AFTER ENGINE RUNNING, DETECTED OIL IN THE COWLING DUCT FROM THIRTEENTH STAGE TO THE FUEL HEATER DAMAGED, FILTER COVER SOLDER OUT, COWLING DAMAGED, HEATER FUEL VALVE OPENED ALL TIME AND FUEL FLOW TRANSMITTER WITH INCORRECT INDICATION. THE COWLING WAS PROVISIONALLY REPAIRED. THE LOW OIL PRESSURE ALARM, HEATER FUEL VALVE AND FUEL FLOW TRANSMITTER WERE REPLACED. GENERAL REVISION AND OVERWEIGHT LANDING INSPECTION WERE PERFORMED FOR CONDITION TO WIRING, DUCTS AND COMPONENTS, ALL CORRECT. THE LEFT ENGINE WAS TESTED IAW MM 71-00-01 ALL CORRECT. (M) 2L72 4F RTA6WE 20030827001342003082700134NM 2003 8 27 CALA0300457 120030809A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FLOORBEAM FLANGE AT NUTPLATE HOLE CORRODED, FS 947, LBL 5. A REPAIR STRAP WAS INSTALLED SRM 53-00-51, PAGE 213. 2L72 4F RTA16WE 20030828000342003082800034NM 2003 8 28 NACA20030087 120030606A27511812993 INDICATOR BOEING727 727100 1384036NM COCKPIT STICKS A NACAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AL03992AJ1410 19428 DURING FLAP RETRACTION INBOARD FLAPS INDICATED MOVEMENT STOPPED AT 4 DEGREES. REPLACED FLAP POSITION INDICATOR, CHECKED GOOD. 2L73 4F RTA3WE 20030829000042003082900004 2003 8 29 52510 420030712A3418 STALL WARNING BEECH 1900 1900D 1154162CE COCKPIT MALFUNCTIONED A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07142ZV UE142 ON FLIGHT 700 FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO, DURING THE TAKEOFF ROLL STALL WARNING WENT OFF AND WOULD NOT RESET. THE AIRCRAFT WAS RETURNED TO GATE WITH NO FURTHER INCIDENT. THE CREW WAS THEN GIVEN AIRCRAFT 3199Q TO COVER THE LINE. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY EVEN AFTER A TEST FLIGHT. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030729001452003072900145WP 2003 7 29 ABXA030293 120030624A52103559807503 HOUSING DOUG DC9 DC932 3022066WP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 PASSENGER ENTRY DOOR HANDLE HOUSING WAS CRACKED. REPLACED ENTRY DOOR HANDLE AND ATTACHING HARDWARE IAW DC-9 SRM 51-30-1, 51-30-2, AND 51-30-5. 2L72 4F A6WE 20030807000732003080700073NM 2003 8 7 AWXA200300844 120030713A5420311A1680105 ANGLE BOEING737 7373G7 1384595NM NR 2 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-14 CHECK A .25 INCH CRACK WAS FOUND ON ANGLE AT LT POSITION OF NR 2 PYLON AFT KEEL, ABOVE TURBINE FIRE SLEEVE NAC STA 254.52. REMOVED DAMAGED ANGLE AT LT POSITION OF NR 2 PYLON AFT KEEL NAC STA 254.52; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 PG 4, FIG 2 & SRM 51-40-02 PG 3 - 4 & 38, FIG 8. 2L72 4F RTA16WE 20030812000222003081200022NE 2003 8 12 HEEA088369 120030710A62107615009100041A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K13301 760047 MAIN ROTOR BLADE HAS A CRACK IN THE ABRASION STRIP NEAR STATION 152.5 INCHES WITH THE FIBERGLASS BELOW THE STRIP CRACKED AND SEPARATED. THE TIP RIB AND NUT PLATE ARE BOTH UNBONDED. 1G72 3U H1NE 20030903002052003090300205NM 2003 9 3 QXEA200301035 120030825A5230 RETAINER DHAV DHC8 DHC8202 2809007NM CARGO DOOR BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- CARGO DOOR SEAL RETAINER IS BENT IN TWO PLACES AT AFT BOTTOM EDGE OF DOOR. REPAIRED IAW DHC-8 RD 8-52-086. 2H72 4T RTA13NM 20030904000122003090400012NE 2003 9 4 AWXA200300776 220030704A75301777MK2 BLEED ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE ENGINE FAULTY A AWXAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP28814AW1067710677 1281 ON TAKE OFF ROLL AT PHX EN ROUTE TO YYC, EGT LIMIT EXCEEDED (645) DEGREES. ABORTED TAKEOFF AND RETURNED TO GATE. MECHANIC REMOVED AND REPLACED THE 2.5 BLEED (LPC MASTER) ACTUATOR IAW AWA T/C R5M75307 AND PERFORMED POWER ASSURANCE TESTS IAW AWA T/C F5M71312 AS REQUIRED. VENDOR TEARDOWN OF LPC BLEED MASTER ACTUATOR S/N 1777839 CONFIRMED FAILURE OF UNIT. DURING RIG INVESTIGATION THE PISTON WOULD NOT EXTEND, ERRATIC MOVEMENT WAS ALSO FOUND DURING VELOCITY CHECKS, AND HIGH INTERNAL LEAKAGE WAS NOTED. REPLACED TORQUE MOTOR FOR ERRATIC MOVEMENT, AND REPLACED SEAL (P/N STD949-77) FOR INTERNAL LEAKAGE. UNIT TESTED IAW CMM 75-38-02, REV. 1. 2L72 4F4 FRTA28NM E311NE 20030905000442003090500044SO 2003 9 5 C2XA03TY141 120030828A532014522461011 PLATE EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 TYS DURING A SCHEDULED 2C INSPECTION THE RT AFT CROSS BEAM PLATE WAS CORRODED. MAINT R&R THE AFT CROSS BEAM PLATE IAW EMB 135/145 SRM 51-10-02 ALLODINED, PRIMED AND PAINTED REWORK AREA IAW EMB 135/145 CPM 51-21-04'05'06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030903001812003090300181WP 2003 9 3 AALA20030406 120030403A21331036361 RELIEF VALVE DOUG DC9 DC982 3022082WP A/C BAY DEFECTIVE A AALAB EMER. DESCENT O OTHER DEDESCENT 1 SW21245AA 49257 DFW - FLT 1713 - EN ROUTE PHL-DFW, LEFT PACK QUIT AT 31,000. COULD NOT HOLD CABIN PRESSURE OR FIX PROBLEM WITH CHECKLIST. DID EMERGENCY DESCENT, DEPLOYED 02 MASKS. LANDED DFW WITHOUT INCIDENT. REPLACED FORWARD OVER-PRESSURE RELIEF VALVE. ACCOMPLISHED LEAK CHECK AND TEST SYSTEM. PRESSURIZED AIRCRAFT AND ALL CHECKS NORMAL. REPLACED AS PRECAUTIONARY LEFT PACK TURBINE INLET. OUTLET SWITCHES LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905002112003090500211SO 2003 9 5 C2XA03CL153 120030825A33501010861 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2712567 145623 CLE FLT NR 2004 THE CREW REPORTED EMERGENCY EXIT SIGN ABOVE GALLEY DOOR NOT ILLUMATING. MAINTENANCE REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20030908001592003090800159EA 2003 9 8 SWIA200312234 120030803A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA T/E FLAP ACTIVATED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07905SW 7437 AFTER TAKEOFF, DURING FLAP RETRACTION FROM 20 DEGREES TO 8 DEGREES, 'FLAPS FAIL' CAUTION MESSAGE DISPLAYED. RETURNED TO SMF. PERFORMED POWER DOWN PROCEDURE. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030825001242003082500124EU 2003 8 25 AWXA200300813 120030720A2560P20700012015 FLASHLIGHT AIRBUS320 A320232 3930326EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28667AW 1710 LAS - EMERGENCY EQUIPMENT - DURING INSPECTION FOUND THE EMERGENCY FLASH LIGHT IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030822000492003082200049NM 2003 8 22 2003UALA00562 120030716A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 SEAT TRACK CORRODED LBL 12 FROM BS 859-999. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030916000822003091600082WP 2003 9 16 GTIA030629 120030725A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND CABIN FLOOR PANEL RIGHT STATION 826-869 DELAMINATED AND EDGE DAMAGE. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030826000842003082600084EU 2003 8 26 YENA200314 120030712A3260664700500A4D CONTROL UNIT AIRBUS320 A320232 3930326EU LANDING GEAR FAULTY A YENAK NONE J WARNING INDICATION CLCLIMB 1 EA15519JB 2646 1398 DURING GO-AROUND LANDING GEAR DID NOT RETRACT, ECAM CALLED FOR RECYCLING THE L/G HANDLE, LANDING GEAR RETRACTED NORMALLY. LANDING GEAR CAME DOWN NORMAL FOR SPEED APPROACH & LANDING. BITE TEST LGCIU 1 & 2 THROUGH CFDS IAW 32-69-00, NO DEFECT NOTED. AIEMAN SHOWS LGCIU NR 1 FAULT. REMOVED AND REPLACED LGCIU NR 1 PRECAUTIONARY PER MCC REQUEST IAW 32-31-71. 2L72 4F RTA28NM 20030826001662003082600166SO 2003 8 26 SWIA200312099 120030613A275012064207615 CONTROL LEVER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07233SW6820 6820 120307 FLAPS WILL NOT EXTEND PAST 25 DEGREE SETTING EVEN WHEN 45 DEGREE IS SELECTED.FLAP SELECTOR WOULD NOT SLIDE SMOOTHLY INTO 45 DEGREE DETENT. REPLACED FLAP SELECTOR LEVER. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20030909002052003090900205WP 2003 9 9 ABXA030337 120030801A5347S4925848M3600 SEAT TRACK DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 CORROSION ON SEAT TRACK AT STA 275, 294, 320, 351, 380 AND 408. REPLACED CENTER SEAT TRACK STA 160 - 588 IAW DC-9 SRM 51-30-1 AND SSRM K05406. 2L72 4F A6WE 20030910001322003091000132NM 2003 9 10 03FDEA01215 120030725A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE CORRODED. LT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE REPAIRED AS PER FEDEX EA 1-5750-71881 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F4 FRTA22WE E13NE 20030911000202003091100020NM 2003 9 11 UPS03441151 120030827A3510 REGULATOR BOEING747 747123 1384873NM OXYGEN SYSTEM INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 02 REGULATOR DOES NOT SHOW FLOW INDICATION IN NORMAL/ON POSITION R/R S/O REGULATOR ASSY, IAW MM 35-11-07 OP CKD OK 2L74 4F A20WE 20030911001512003091100151WP 2003 9 11 DHL2003873588 120030703A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING OB FLAP UPPER FWD PLATING SHOWS AN INTERIM REPAIR BETWEEN STA XF.225.000 - XF.235.000. PERFORMED MAJOR REPAIR IAW EODHL-030610, ED-3441. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030610, ED-3441. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN SEGMENT, A SPLICE STRAP AND INNER DOUBLER IAW EODHL-030610, ED-3441. CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT INTERIOR SURFACE, THE SPLICE STRAP AND INNER DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED THE NEW SKIN SEGMENT, SPLICE STRAP AND INNER DOUBLER ON RT WING OTBD FLAP UPPER FWD PLATING IAW EODHL-030610, ED-3441, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912001042003091200104NM 2003 9 12 AWXA200300862 120030713A532065C334191 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT LAVATORY FLOOR SHEAR WEB BS 1016-1032, BL 0 TO LBL 30, WL 208. MAINTENANCE FOUND PREWORK MEASUREMENT TO BE OUT OF LIMITS; REMOVED FLOOR SHEAR WEB BS 1016-1032, BL 0 TO LBL 30; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3-5, 38, AND 42, FIG 8 AND 10. 2L72 4F RTA16WE 20030929000892003092900089WP 2003 9 29 UPS03841158 120030826A5754 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, RT WING L/E SKIN IS CRACKED AT LOWER SURFACE XFS 304. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX C. 2L74 4F RT4A25 20030929001212003092900121SO 2003 9 29 CHQA000418 120030907A2120 SMOKE EMB 145 EMB145 3260210SO CABIN DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11836 SMOKE IN CABIN DURING FLT TOWARDS REAR OF PAX CABIN. INSPECTED ENGINE BLEED SYSTEM IAW EMB 135 MM 36-11. INSPECTED APU BLEED SYSTEM IAW EMB 135 MM 36-10. INSPECTED NR 1 AND NR 2 PACKS IAW EMB 135 MM 21-00. NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTT00011AT 20031001001202003100100120NM 2003 10 1 USAA030173 120030828A5414311A14001 SKIN BOEING737 737401 1384701NM NACELLE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US41222 23886 PIT - FOUND STRUT SKIN PANEL .75 INCH CRACK, PANEL DOUBLER NR 5827R STATION 206.50 TO 215.00. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TR 54-30-07 AND EA 76836 AND SRM 51-20-10. (M) 2L72 4F RTA16WE 20031002001132003100200113NM 2003 10 2 QXEA200301098 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 2 SEAT TRACK IS CORRODED BELOW LEFT HAND LUG TWO INCHES AFT OF STATION X467. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031021001152003102100115 2003 10 21 USAASA03115 420030921A2565 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19743UW 1277 CLT - THE FORWARD RIGHT SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE FORWARD RIGHT EMERGENCY ESCAPE SLIDE ASSEMBY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030909001602003090900160SW 2003 9 9 HEEA088899 120030401A6720 BUSHING BELL 206 206L3 1182108SW DRIVE LINK WORN B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0353119 51575 BUSHINGS WORN REPLACED COLLAR SET 206-011-005-101 DUE TO SPLINES PITTED. REPAIRED. 1G71 3U H2SW 20031022001542003102200154SO 2003 10 22 C2XA03TY167 120030923A531514521700005 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713995 145295 DURING A SCHEDULED 2C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED. MAINT. CUT OUT THE AFFECTED AREA AND FAB. A NEW FLOORBEAM, INSTALL A DOUBLER FILLER AND SHIMS. ALLODINED,PRIMED AND PAINTED IAW EMB 135/145 SRM 53-21-10 AND EMB 145 CPM 51-21-04,05.06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T4 FRTT00011ATTE6CH 20031029000902003102900090NM 2003 10 29 USAABB03176 120030929A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT WEAK A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU 22199 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 WEAK. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20031120000142003112000014NM 2003 11 20 AWXA200301223 120030922A575365C2630925 ANGLE BOEING737 737301 1384611NM TE FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON ANGLE, TOP OF NR 6 FLAP FAIRING, FORWARD OF CLOSEOUT DOOR WBL 191. MAINTENANCE REMOVED CRACKED ANGLE AT WBL 191; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65C26309; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, PG 4, FIG 4. 2L72 4F RTA16WE 20040127002132004012700213WP 2004 1 27 ASAA0380787 120031119A53219936544501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS EDGE DAMAGE AND INSERTS MISSING AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040129001712004012900171NM 2004 1 29 DHL200374262 120031123A5230 SKIN BOEING727 727225 1384077NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 1 CARGO DOOR AFT SIDE SKIN BEHIND THE REPAIR IS DENTED. CUT OUT DAMAGED LWR SECTION OF SKIN & FABED NEW FROM 2024-T3 .040, PO 900355 DIM 58.5 X 14.375 INCH AND DOUBLERS 6 EA FROM 2024-T3 .063, PO 900355, DIM 5 X 8 INCH, 5.5 X 4.5 INCH, 8.875 X 4.5 INCH, 6.75 X 4.5 INCH, 5.125 X 4.75 INCH, AND 8 X 4.75 INCH, IAW B727 SRM 52-00-3 FIG 1. ALL REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALL NEW REPAIR PARTS IAW B727 SRM 52-00-3 FIG 1. 2L73 4F A3WE 20031112000172003111200017NM 2003 11 12 2003UALA00822 120031030A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29373UA 24638 AFT PIT FRAME STA. 835 IS BENT AND CRACKED IN RADIOUS VIEWED FROM UNDERSIDE RBL 18. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031117000822003111700082SW 2003 11 17 ALG2003F00089 120030823A6720206001058101 CONTROL ROD BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL TAILBOOM CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032762D 45280 CAE860103 DURING PHASE INSPECTION, TAIL ROTOR LONG CONTROL WAS FOUND TO BE CORRODED AT OR NEAR NYLATRON STRIP CAUSING THE STRIPS TO BE LOOSE. 1G71 3U3 U H2SW E1GL 20031105000422003110500042WP 2003 11 5 ABXA030398 120031007A5220995773412 INTERCOSTAL DOUG DC9 DC931 3022065WP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 LEFT AFT OVERWING DOOR HAD CRACKED INTERCOSTAL AT LATCH HANDLE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20031105000892003110500089NM 2003 11 5 2003UALA00805 120031025A335060243 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29364UA 24533 EEL LIGHTS INOP FROM ROW 19 AFT. REPLACED EEL LIGHT STRIPS AT ROWS 19-20. 2L72 4F4 FRTA16WE E2GL 20031106000862003110600086WP 2003 11 6 UPS03841519 120031028A5310 WINDOW FRAME DOUG DC8 DC873F 302199FWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 CAPTS WINDOW FRAME CORROSION. REMOVED CORROSION & APPLIED ZINC CHROMATE. LOWER CORNER IN SERVICEABLE CONDITION. OK TO CONTINUE. 2L74 4F RT4A25 20031107000692003110700069 2003 11 7 03303320 420031030A3160701167112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A VTZAO OTHER O OTHER UKUNKNOWN 1 EA27320UE 41043 BOTH ELECTRONIC INSTRUMENT DISPLAY UNITS WERE IDENTIFIED AS GOING BLANK DURING OPERATION OF AIRCRAFT. NR 1 SYMBOL GENERATOR AND NR 1 AIR DATA COMPUTER WERE FOUND TO BE FAULTY AND WERE REPLACED. AFTER REQUIRED OPERATIONAL CHECKS THE DISPLAYS OPERATED CORRECTLY AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20031107001332003110700133SO 2003 11 7 SIMA200327910 120031003A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED NEW SERVICE DOOR SILL IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 51-20-03, 51-40-02 AND 51-40-06. (M) 2L72 4F RTT00011AT 20040112000802004011200080NM 2004 1 12 AWXA200301570 120031221A2560P4010021 BATTERY BOEING737 7373B7 1384580NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28332AW 23384 PHX - EMERGENCY EQUIPMENT - AFT CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040113000292004011300029SW 2004 1 13 ERAA091807 120031020A3212D24921119 FLOAT BELL 412 412 1182202SW MLG LEAKING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03417EH1879 33031 FORWARD CHAMBER HAS LEAK / CHAFING. FLOAT INSPECTION COMPLIED WITH. ALL SERVICEABLE IAW 412-SI-2. 1G72 4U H4SW 20040112001642004011200164NM 2004 1 12 03FDEA02226 120031223A5744 HINGE FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, INBOARD FLAP OUTBOARD HINGE FITTING INBOARD PIVOT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75213 - WINGS, TRAILING EDGE & TRAILING EDGE DEVICES, RT INBOARD. FLAP HINGE BRACKET REPAIR 2L73 4F RTA22WE 20040113001792004011300179EU 2004 1 13 RAIA00312296 120031201A2910 HYDRAULIC LINE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM LEAKING A RAIAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 CE03551HK 41040 STL- LOST HYDRAULIC PRESSURE, RESERVOIR EMPTY. MAINTENANCE REPAIRED HYDRAULIC PRESSURE TUBING. 2L72 4T RTA41NM 20030926001042003092600104NM 2003 9 26 C1HA200383009 120030828A3260 SOCKET BOEING727 7272S7 138407ZNM MGL INDICATOR DIRTY A C1HAK NONE P NO WARNING INDICATION CRCRUISE 1 GL15683CA 22490 R. MAIN GEAR RED (INTRANSIT) LIGHT INOPERATIVE. DOES NOT ILLUMINATE DURING GEAR EXTENSION OR RETRACTION. BULB TEST GOOD. REMOVED AND CLEANED RED (TRANSIT) LIGHT SOCKET/RECEPTICLE ASSY FUNCTIONAL CHECK GOOD IAW MM REF 32-61-91 PG. 401 STEP 5. OK FOR SERVICE 2L73 4F A3WE 20030929000412003092900041EA 2003 9 29 08270324 120030827A2497MS3126F2039 CONNECTOR DHAV DHC6 DHC6 2802606EA PWA PT6 PT6A27 52043EA MCAULY4HFR344HFR34C762 NE COCKPIT ARCED E HKGAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW17122SA 515 PILOT REPORTED DURING CRUSE FLT SMOKE ENTERED COCKPIT FROM AC ELECTRICAL PANEL AREA. NO SYSTEM MALFUNCTION WAS NOTED. NO ELECTRICAL POWER WAS LOST. ONCE ON GROUND DC POWER COULD NOT BE TURNED OFF THROUGH NORMAL SWITCHING. BATTERY WAS DISCONNECTED TO REMOVE DC POWER FROM AIRCRAFT. MAINTENANCE HAS DISCOVERED THAT SMOKE CAME FROM CONNECTOR J31, LOCATED IN LEFT OVERHEAD PANEL IN COCKPIT. CAUSE IS STILL UNDER INVESTIGATION. 1H72 3T4 TRTA9EA E4EA 6 C3PNE 20040930001122004093000112NE 2004 9 30 WX0400001 220030103A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE RIGHT OUT OF ADJUST A WXOAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP19891GA 49423 ON A FLIGHT FROM DEN TO LAS, UPON APPLICATION OF TAKEOFF POWER THE CREW OBSERVED A GREAT LAG IN THE RT N1, N, SPOOL UP, AND EPR INCREASED ONLY TO SLIGHTLY OVER 1.03. N1 AND N2 MADE IT UP TO 65 PECENT AND 68 PERCENT RESPECTIVELY AFTER THROTTLE ADVANCEMENT WHILE EPR DID NOT INCREASE FURTHER. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED TEST AND ADJUSTMENTS ON THE RT ENGINE IAW AMM 71-00-00. ENGINE RUNS SHOWED EPR AND SPOOL TIME TO BE WITHIN LIMITS. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTA6WE E2EA 20060801001132006080100113WP 2006 8 1 IXXA060563S 120030924A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND INTERCOSTAL CORRODED BETWEEN STATION 980, AND 1000 AT LONGERON 35 LEFT. REMOVED CORROSION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, 51-30-30, 53-2-0, AND DOUGLAS DRAWING 5779959. 2L74 4F RT4A25 20030812000952003081200095EU 2003 8 12 HEEA088641 120030717A6520350A33215300 BEARING AEROSPAS355 AS355* EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE 3234 TAIL ROTOR BEARING WORN. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030819000482003081900048EA 2003 8 19 A6WA200340110 120030717A5710 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA STUBWING CHAFED A A6WAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL31413AW 7585 LT INBOARD FLAP VANE HAS A PROTRUSION THAT IS CHAFING THE FLAP STUB WING STRUCTURE. PERFORMED A MAJOR REPAIR TO LEFT FLAP VANE BY REPLACEMENT OF LOOSE FASTENERS. WORK ACCOMPLISHED IAW WEST VIRGINIA AIR CENTER. EO 601R-57-4131 AS APPROVED BY FAA 8110-3. (M) 2L72 4F RTA21EA 20030819001702003081900170NM 2003 8 19 371PA0028 120030713A339758782 WIRE BOEING737 737306 13844BGNM EMERGENCY LIGHT DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. REPLACED FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING CABLE. OPS CHECK NORMAL. 2L72 4F RTA16NE 20030819000742003081900074NM 2003 8 19 CALA0300389 120030715A2612G718505 CONTROL PANEL BOEING737 7373T0 1384582NM FIRE DETECTION MALFUNCTIONED A CALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW27693516956 23589 THE CARGO FIRE DETECTION LOOP LIGHTS ILLUMINATED AFTER DEPARTING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE COCKPIT FIRE SUPRESSION PANEL WAS REMOVED AND REPLACED IAW MM 26-23-10 AND 26-16-10. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA16WE 20030820000612003082000061NM 2003 8 20 03FDEA00920 120030617A2752ARC0503504 ACTUATOR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING - O/B FLAP O/B HINGE O/B ACTUATOR BORE FOUND CORROSION. - RIGHT WING - O/B FLAP O/B HINGE O/B ACTUATOR BORE REPAIRED AS PER FEDEX EA 1-5750-69373. 2L73 4F RTA22WE 20030401001552003040100155WP 2003 4 1 DHL2003804665 120030116A57105769933184 VANE DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT OUTBD SLOT VANE AT STA XS 520.000 HOLES ELONGATED. PERFORMED MAJOR REPAIR IAW EO DHL 030101 , ED-3211. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1, TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030101 , ED-3211 , FABRICATED REPAIR DOUBLER, A FILLER (7075T6AL-0.063) AND INTERNAL DOUBLER IAW EO DHL 030101 , ED -3211. CLEANED , TREATED AND PRIMED INNER SURFACE IAW SRM51-1-8B. APPLIED PRC SEALANT AND DOUBLERS AT RT OUTBD SLOT VANE STA. XS 520.000 MKI 2L74 4F RT4A25 20030821001572003082100157NM 2003 8 21 03FDEA01175 120030728A5320A5A7114507 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 CTR CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 46L SPLICE FITTING FOUND CRACK. CTR CARGO STA 5-113 THRU STA 1541 CRACK LONGERON 46L SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG A5A7114 AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20030407001062003040700106NM 2003 4 7 UIEA200300010 120030225A542065B89058502 STIFFENER BOEING747 747243B 1384830NM NR 3 NACELLE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15540MC 22508 DURING CURRENT C-CHECK, AT SIAEC FOUND NR 2 PYLON (NR 3) LONGITUDINAL STIFFENER VERTICAL FLANGE, BELOW PRECOOLER EXHAUST VENT, CRACKED THREE PLACES AT NAC 245, 247 AND 257. PYLON PREVIOUSLY MODIFIED PER SB 747-54-2163 AND 747-54-2091 WHICH CONSISTS OF AN UPPER ANGLE INSTLALED ON THE STIFFENER FROM NAC 234 TO 272 ALONG WITH AN EXTERNAL SKIN DOUBLER. ADDITIONAL REPAIR CONSISTS OF A LOWER ANGLE INSTALLED FROM NAC 234-252. CRACK AT NAC 257 MAY BE LEFT AS IS. HFEC INSPECTED ALL OPEN HOLES COMMON TO BOTH ANGLES AND HOLES IN THE REMAINING REPAIR. NO ADDITIONAL CRACKING FOUND ON STIFFENER ON ALUMINUM SKIN. REPAIR ANGLE INSTALLED PER STANDARD SRM PRACTICES IAW S/B'S MENTIONED ABOVE. (M) 2L74 4F A20WE 20030408000142003040800014WP 2003 4 8 ASAA0380101 120030123A5311991967563 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OAK - FOUND DURING C-CHECK, FRAME IS CORRODED IN AFT CARGO BAY AT FS 1271. CUT OUT CORRODED SECTION. INSTALLED NEW SECTION AND SPLICE PER SRM 51-10-3, 53-01, 51-30-2 AND 53-03. (M) 2L72 4F RTA6WE 20030410002212003041000221NM 2003 4 10 DL76G030308 120030331A33501317 LIGHT BOEING767 767332 1382001NM EXTERIOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO271602 29694 ON L/O FOUND 2L DOOR EXT EMERGENCY LIGHT INOP. RELAMPED, CHECKS OK. 2L72 4F RTA1NM 20030416001522003041600152NM 2003 4 16 AALA20030190 120030210A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21799AN 30258 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35HG INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030416003732003041600373EA 2003 4 16 SWIA200311694 120030107A27604916405 PCU CNDAIRCL600 CL6002B19 1900309EA NR 2 SPOILERON MALFUNCTIONED A SWIAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07446SW 7666 CONFIG SPOILER MASTER WARNING MESSAGE CAME ON AT 70 PERCENT FOR TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED RIGHT SIDE SPOILERONS (BOTH) INBOARD PCU'S PER MM 27-62-01. LEAK AND OPS CHECK GOOD. MDC & SECU FLAGGED BOTH PCU'S ON TROUBLESHOOTING. AFTER PCU CHANGE, RECEIVED FLT SPOILER AND GROUND SPOILER FAULTS AND SECU NR 2 WOULD NOT RESET. REMOVED AND REPLACED NR 2 SECU PER MM 27-61-05. SYSTEM OPS CHECK GOOD. ALL SPOILER/SPOILERONS WORK PER MM. I/B PCU P/N: 27000-7, S/N OFF: 5660, O/B PCU P/N: 27000-7, S/N OFF: 5656. 2L72 4F RTA21EA 20030417000492003041700049WP 2003 4 17 IXXA0300008O 120030128A7197 CONNECTOR DOUG DC8 DC871 302199AWP EGT HARNESS DIRTY A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11829BX860921207 45994 AFTER DEPARTURE FROM LRD DURING CRUISE CREW NOTED NR 3 ENGINE EGT ROSE ABNORMALLY. CREW SHUTDOWN NR 3 ENG PER COMPANY POLICY. AIRCRAFT RETURNED TO LRD FOR AN UNEVENTFUL LANDING. UPON INSPECTION MAINTENANCE DISCOVERED DIRTY CONNECTIONS IN THE EGT HARNESS. MAINTENANCE CLEANED CONNECTIONS AND RAN ENGINE PER APPLICABLE AIRPLANE MANUALS. AFTER A GOOD OPERATIONAL CHECK THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20030417001802003041700180 2003 4 17 SWIA200311771 420030208A3197 WIRE EMB 120 EMB120ER 3260203SO RT MLG WW SHORTED A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 NM07298SW 120328 FDAU AND DFDR LIGHTS CAME ON IN FLIGHT. CIRCUIT BREAKER FOR FDAU FOUND POPPED AND SMELLED SMOKE AT THE SAME TIME. FOUND W501-0018-22 SHORTING TO GROUND FROM LEFT AILERON RIVET INSIDE WHEEL WELL. REPAIRED WIRE IAW WM 20-00-00. OPS CHECK OF FDAU AND DFDR GOOD IAW MM 31-30-00. 2L72 4T RTA31SO 20030423001532003042300153NM 2003 4 23 UPS03240279 120030226A5310 DOUBLER BOEING727 727108C 1384039NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, ON REMOVAL OF WINDOW FRAME TO FACILITATE BS 870 FITTING REPLACEMENT CORROSION FOUND ON FLANGE OF WINDOW FRAMES, FRAME AT BS 880 AT LWR AFT CENTER. CORROSION BLENDED OUT IAW SRM 51-10-6 & AREA OF DAMAGE FOUND OUTSIDE LIMITS IAW SRM 56-20-1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 56-20-03 FIG 1. 2L73 4F A3WE 20030428000212003042800021WP 2003 4 28 GTIA030256 120030227A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE CABIN CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 CABIN INTERIOR STA 788-965 LBL 54 FLOOR WEB`S CORRODED IN SEVERAL AREAS. REMOVED DAMAGED AREA. FABBED WEB REPAIR. INSTALLED REPAIR WEB. 2L72 4F4 FRTA6WE E2EA 20030429001362003042900136NM 2003 4 29 AUS20030289 120030212A5313 STRINGER BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AFT CARGO STRINGER 27L CONTAINED LEVEL 2 CORROSION IN AREALOCATED BETWEEN BS950D AND BS1030. FOUND DURING CPCP INSPECTION IAW C53-013-01. 2L73 4F4 FRTA3WE E2EA 20030425001162003042500116 2003 4 25 DL76S030239 420030313A2565 LANYARD BOEING767 767332 1382001NM ESCAPE SLIDE SEPARATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27136DL 23146 DOOR DIFFICULT TO ARM/DISARM. SLIDE PACK FELL OUT WHILE DOOR WAS OPENING (2R). INSTALLED NEW SLIDE, OPS NORMAL. 2L72 4F RTA1NM 20030430000142003043000014 2003 4 30 NACA20030082 420030403A221025858001 COUPLER BOEING727 727100 1384036NM YAW DAMPER OSCILLATES A NACAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 AL03930FT3317 3317 19387 RIGHT ON TAKE-OFF, UPPER YAW DAMPER OSCILATE AUTO PILOT DISENGAGE, LIGHT STAYED ON, WIND SHEAR CAUTION LIGHT STAYS ON. REPLACED UPPER YAW DAMPER COUPLER AND TESTED GOOD. 2L73 4F RTA3WE 20030430002142003043000214NM 2003 4 30 VNAA0304019 120030418A2450230GC02Y02 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE 1VE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07425JS830 77 3037 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ECU FAIL INDICATION AND ABORTED TAKEOFF. WHILE TAXIING BACK TO THE GATE, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AND THE CREW EVACUATED THE AIRCRAFT. THE CREW THEN TAXIIED THE AIRCRAFT BACK TO THE GATE. MECHANICS WERE SENT FROM PIT WITH A 1VE PANEL. MAINTENANCE THEN INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030505001152003050500115WP 2003 5 5 MWEA030180 120030424A57553923255504 BRACE DOUG DC9 DC981 3022081WP RT WING CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 RIGHT WING INBOARD FLIGHT SPOILER CENTER SUPPORT BEAM CRACKED AT UPPER ATTACH POINT. LOCATED AND INSTALLED NEW BRACE. 2L72 4F A6WE 20030505002212003050500221NM 2003 5 5 03FDEA00552 120030421A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION WHILE WORKING N00328 FOUND STRINGER CORRODED AT FASTENER HOLES COMMON TO STANDOFF BS 510 STR 27L. 2L73 4F RTA3WE 20030506001152003050600115NM 2003 5 6 PCA0300848 120030412A5347 SEAT TRACK BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEVEL 1 CORROSION SEAT TRACK STA 1046 RBL 99.0. REPAIRED PER SRM 53-10-05. 2L74 4F A20WE 20030505001042003050500104NM 2003 5 5 03FDEA00207 120030303A5510ALC8102 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 3L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR. 2L73 4F RTA22WE 20030506000462003050600046EA 2003 5 6 COMA0360210 120030421A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR INOPERATIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01924CA 7026 FLIGHT 5809 1ST SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. REPLACED POWER STRIP. 2L72 4F RTA21EA 20030508001402003050800140NM 2003 5 8 DLM88030383 120030423A3350 LIGHT DOUG MD88 MD88 3023688NM EMERGENCY EXIT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27907DL 49538 AFT EMERGENCY EXIT LIGHTS INOPERATIVE - FOUND RACK BAD - P/N 60-1177-9 S/N 223 - REPLACED SAME 2L72 4F RTA6WE 20030513000742003051300074EU 2003 5 13 RAIA00304124 120030428A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT FAULTY A RAIAO OTHER L NO TEST NRNOT REPORTED 1 CE03574HK 41093 EMERGENCY ESCAPE LIGHTS INOP ROWS 1&2. REPAIRED FAULTY WIRING AT FWD EMERGENCY LIGHT TRACK, OPS CK OK. 2L72 4T RTA41NM 20030602001022003060200102 2003 6 2 SWAA031171 420030527A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030602000032003060200003SO 2003 6 2 ASOA03194 120030501A3350D36604001 BATTERY EMB 120 EMB120RT 3260202SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11274AS 120229 FLT 4374 - DURING A GROUND INSPECTION IN ATL, THE EXTERIOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTEYR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030605001242003060500124WP 2003 6 5 ZW0A0304901 120030515A3350 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139401W 53137 THE EMERGENCY LIGHTS IN THE CEILING ABOVE THE CATWALK IN THE TAIL, THE EMERGENCY LIGHT IN THE TAIL JUST ABOVE THE AFT END AREA OF THE CATWALK, AND THE EMERGENCY EXIT LIGHT AT THE RIGHT FWD WING EXIT, WERE ALL INOPERATIVE. REPLACED THE BATTERIES PN 408822-101 IN THE POWER SUPPLY FOR THE CATWALK CEILING LIGHT, REPLACED THE BULB PN 7732 FOR THE TAIL LIGHT, AND REPLACED THE BULB PN 1315 FOR THE EXIT LIGHT. CHECK-C 11-16-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030515000472003051500047EA 2003 5 15 SWIA200311920 120030424A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07498SW 7483 STAB CHANNEL NR 2 WILL NOT ENGAGE. PERFORMED SELF TEST ON HSTCU AND FOUND NO FAULTS. HSTCU GREEN TEST PASSED. ENGAGED STAB CHANNEL NR 2, OPERATED HST FROM PILOT AND COPILOT'S TRIM BUTTONS. OPERATE GOOD. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20030520000562003052000056NM 2003 5 20 AMTA200300514 120030416A2612 CIRCUIT CARD BOEING757 75733N 1384931NM RT ENG FIRE FAILED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11556TZ 32590 ENGINE FIRE LP 2 DISPLAYED, RT ENGINE. SWAPPED CONTROL CARDS M683, M684 RT ENGINE FIRE LOOP 1 AND 2 FOR TROUBLESHOOTING PER GMM CHAP 8. P/N'S FOR BOTH CARDS ARE S332T301-181. NEW S/N FOR M683 IS 21788, NEW S/N FOR M684 IS 21781. BOTH CARDS OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030612000092003061200009SO 2003 6 12 SWIA200312017 120030425A5420 BRACKET EMB 120 EMB120ER 3260203SO HYD POWERPACK CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07295SW 120322 BLUE HYDRAULIC SYSTEM PACK LOWER BRACKET CRACKED FOUND DURING C-CHECK INSPECTION. INSTALLED NEW LOWER SUPPORT BRACKET FOR BLUE SYSTEM HYDRAULIC PACK. 2L72 4T RTA31SO 20030617002832003061700283SW 2003 6 17 HEEA087317 120030611A5610407030115123 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 WINDSHIELD IS CRAZED. REPLACED WINDSHIELD. 1G71 3U O H2SW 20030520000682003052000068SO 2003 5 20 SIMA200309611 120030403A5313AL2024T3 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 ABI - DUIRNG A MBV INSPECTION, STRINGER 19L AT FRAME 53 WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M) 2L72 4F RTT00011AT 20030618000712003061800071NM 2003 6 18 SWAA031295 120030609A32606552850 CIRCUIT CARD BOEING737 737317 138447PNM E/E BAY FAULTY A SWAAK NONE N FALSE WARNING CLCLIMB 1 SW29661SW 23173 NLG RED UNSAFE LIGHT ILLUMINATED WITH GEAR UP. CYCLED GEAR, SYSTEM NORMAL THROUGH DURATION OF FLIGHT. REMOVED AND REPLACED M983 CIRCUIT CARD PER MM. 2L72 4F RTA16WE 20030523001142003052300114NM 2003 5 23 2003UALA00422 120030513A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29322UA 23954 FLOOR EEL LIGHTS AFT THIRD OF CABIN INOPERATIVE. CLEANED CONNECTOR AT AFT GALLEY POWER STRIP. 2L72 4F4 FRTA16WE E2GL 20030619000762003061900076SW 2003 6 19 HEEA087411 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030619000462003061900046SW 2003 6 19 HEEA087196 120030609A6330 SEAL BELL 206 206L4 1182110SW SUPPORT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 GEARBOX SUPPORT SEAL LEAKING. REPAIRED. 1G71 3U NCH2SW 20030624000752003062400075EA 2003 6 24 SWIA200312071 120030530A3397 CONNECTING ROD CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07408SW 7055 FIRST ROW OF ORANGE EMERGENCY LIGHTS IN CABIN NOT ILLUMINATING. SECURED LOOSE CONNECTOR AT ROW 1-C. OPS CHECK GOOD. 2L72 4F RTA21EA 20030630000062003063000006EU 2003 6 30 CX7A194J35 120030404A26131734362450 SENSOR SAAB SF340 340B 7860101EU TAILPIPE INOPERATIVE A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03303CE 340B194 RIGHT TAILPIPE HOT LIGHT ILLUMINATED ON TAKEOFF ROLL. 2L72 4T RTA52EU 20030701000152003070100015SW 2003 7 1 HEEA087869 120030617A3411407075042101 PITOT LINE BELL 407 407 1182206SW PITOT/ STATIC CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 PITOT LINE HAS DEVELOPMENT OF CORROSION DUE TO TREATMENT USED DURING MANUFACTURE PROCESS. REPLACED TUBE. 1G71 3U O H2SW 20030707001732003070700173EU 2003 7 7 03164305 120030613A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27305UE 41019 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PERSONNEL DISCOVERED THE AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030714001392003071400139NM 2003 7 14 DL73S030495 120030528A555165737823 ATTACH FITTING BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 STABILIZERS / HORIZONTAL / ATTACH FITTINGS / LT, RT AND CENTER SECTION - CORROSION: WHILE ACCOMPLISHING AN INSPECTION OF THE HORIZONTAL STABILIZER ATTACH LUGS PER EO 3-69697-3. MAINTENANCE DISCOVERED CORROSION IN ALL FUSELAGE AND STABILIZER LUGS AND ON MOST OF THE LUG FACES. ER/A 412532-14 PROVIDED INSTRUCTIONS TO MACHINE THE BORES AND LUG FACES TO REMOVE ALL CORROSION. 2L72 4F RTA16WE 20030127000872003012700087NM 2003 1 27 SWAA030066 120030112A2560PH22300L STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROWS NR 8 AND NR 10 AT BOTH ABC AND DEF. SECURED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20030128001092003012800109 2003 1 28 219PA0006 420030127A2210 AUTOPILOT SYS BOEING737 737222 1384473NM A PIDAK NONE O OTHER CRCRUISE 1 SO05219PA 19956 Elevator channel of auto pilot will not stay engaged. Re-racked A/P pitch control channel unit. Ops chks good IAW MM 22-10-10. 2L72 4F A16WE 20030129000802003012900080SW 2003 1 29 HEEA083984 120030117A7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20030204000612003020400061NM 2003 2 4 SWAA030173 120030123A532065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 867, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030219000482003021900048CE 2003 2 19 LX52003F00001 120030124A30801013810125 VALVE BEECH B300 B300 1159232CE PWA PT6 PT6A11 52043NE BRAKE DEICE STICKING B LX5RO OTHER O OTHER NRNOT REPORTED 1 GL19981LL 495 FL265 THERE IS A PERSISTANT PROBLEM WITH THIS SERIES BRAKE DEICE VALVE STICKING IN THE OPEN POSITION. THIS PROBLEM SEEMS TO BE GREATER DURING THE WINTER (EXTREME COLD) BUT IT DOES OCCUR AT ALL TIMES OF THE YEAR. 2L72 4T3 TRTA24CE E4EA 20030220000432003022000043WP 2003 2 20 ABXA030044 120030113A5315991556171 FLOORBEAM DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23977AX 47513 F.S. 1072 FLOORBEAM UPPER ANGLE CRACKED, RBL 54. REPAIRED FS 1072 FLOORBEAM UPPER ANGLE AT RBL 54 IAW DC-9 SRM. 2L72 4F A6WE 20030117000292003011700029SW 2003 1 17 HEEA083164 120030108A6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 TRANSMISSION RESTRAINT WORN. REPAIRED. 1G71 3U H2SW 20030220001382003022000138WP 2003 2 20 MWEA030052 120030203A531299122433 BULKHEAD DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31207ME 47794 STATION 965 RIGHT, FORWARD PYLON, BULKHEAD WEB HAS TWO SMALL CRACKS EMANATING FROM SNAPS AT OUTBOARD SIDE NEXT TO LONGERON 11 AND LONGERON 10. CUT OUT DAMAGE, FABRICATED DOUBLER, INSTALLED TWO EACH OF DOUBLERS AND PARTITION GUIDE. 2L72 4F A6WE 20030221000962003022100096NM 2003 2 21 0300255642 120030219A7920 PWA BOEING757 757251 1384970NM PWA 2037 PW2037 NE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01542US 26489 716410 During climb flight crew was unable to keep the cockpit warm. Flight crew began to adjust pack temp position/control. Smoke began to enter the AC cabin and a smoke detector sounded. Flight crew returned AC to departure airport. Maintenance found oil in the left pack and the 10th stage bleed of engine #1. Engine #1 replaced. Maintenance also replaced the left ram air door actuator and left trim air valve. 2L72 4F4 FRTA2NM E17NE 20030226000392003022600039SW 2003 2 26 HEEA084328 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 LIGHT STAYS ON. REPLACED FUEL CELL PRESSURE SWITCH 1G71 3U O H2SW 20030304000462003030400046EA 2003 3 4 COMA0360130 120030301A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01735CA 7267 FLIGHT 5614 CABIN DOOR WARNING MESSAGE.CLEANED DIRT AND DEBRIS FROM DOOR LATCH MECHANISM. DOOR OPERATION NORMAL. 2L72 4F RTA21EA 20030304000692003030400069NM 2003 3 4 DL73S030070 120030115A52306547952524 DOOR FRAME BOEING737 737232 1384475NM C2 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 DOOR / C-2 CARGO DOOR / FWD FRAME / LAP SPLICE : CRACK REPAIR THE C-2 CARGO DOOR WAS FOUND WITH A 1" CRACK IN THE UPPER AND LOWER FRAME WEB AT THE LAP JOINT FOR THE TWO FRAMES. THE CRACK WAS STOP DRILLED IN BOTH MEMBERS AND REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 384452-14, REV A. 2L72 4F RTA16WE 20030307001962003030700196NM 2003 3 7 UPS03240257 120030214A5330 SKIN BOEING727 727108C 1384039NM NOSE W/W L/H CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI AIR LEAK COMING FROM WHAT APPEARS TO BE CRACK IN SKIN OF NOSE W/W L/ H SIDE ABOVE DECAL FOR STRUT SERVICING. CRACKED AREA CUTOUT IAW SRM 51-40-2 DOUBLER, FILLER & SHIM FABRICATE D IAW SRM 51-40-2.. HFEC C/O AROUND CUTOU ON THE AREA - NO DEFECTS F OUND. REPAIR PARTS INSTALLED IAW SRM 51-40-2 2L73 4F A3WE 20030311000632003031100063EU 2003 3 11 HEEA085080 120030228A6410355A09103601 BEARING AEROSPAS355 AS355* EU T/R BLADE DELAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03974AE253 6459 2653 TAIL ROTOR BLADE BEARING IS WORN, DETERIORATED AND DELAMINATED. 1G72 3U H11EU 20030121002262003012100226EU 2003 1 21 MALA030109 120030112A3230D49410001 CONTROL UNIT SAAB SF340 340B 7860101EU LANDING GEAR MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15360PX 340B220 LANDING GEAR FAILS TO RETRACT WHEN SELECTED. INSPECTED LANDING GEAR, FOUND NO NOTICEABLE DEFECTS, ALL GEAR MECHANISMS LOOK OK. NO HYDRAULIC LEAKS. OK TO BE FERRIED TO MSP FOR FURTHER TROUBLESHOOTING AND REPAIRS FROM INL TO MSP. MAINTENANCE INSPECTED LANDING GEAR, FROM LOG PAGE 1113269, REPLACED LANDING GEAR CONTROL UNIT. OPS CHECK GOOD. 2L72 4T RTA52EU 20030319000462003031900046WP 2003 3 19 GTIA030071 120030206A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FS 1250 L28R FLOOR SUPPORT CRACK IN RADIUS. STOP DRILLED ANGLE SUPPORT IN STATION 1250, L28R. (M) 2L72 4F A6WE 20030320000362003032000036NM 2003 3 20 USAASB03002 120030104A3260 WARNING LIGHT BOEING737 7374B7 1384702NM MLG MALFUNCTIONED A USAAO OTHER N FALSE WARNING DEDESCENT 1 EA19426US 24548 PHL - FLT 773 - PREPARING TO LAND AT PHL FROM PWM, CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS WHEN SELECTING GEAR HANDLE TO DOWN POSITION. MULTIPLES ATTEMPTS TO CONFIRM GEAR WAS DOWN AND LOCKED PRODUCED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED GEAR HANDLE LINKAGE. OPERATED GEAR HANDLE SEVERAL TIMES. OPERATIONAL CHECK AND INDICATION CHECK NORMAL. (M) 2L72 4F RTA16WE 20030320001122003032000112NM 2003 3 20 2003UALA00103 120030125A3231N273N20121 LINK BOEING757 757222 1384956NM NLG SEQ VALVE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29590UA 28708 LEFT MAIN LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. CYCLED GEAR STILL DID NOT RETRACT. SEQUENCE VALVE LINK FAILED. REPLACED LINK ASSEMBLY 2L72 4F RTA2NM 20030327000392003032700039NM 2003 3 27 AWXA200300311 120030228A5320146N524012 ANGLE BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK CORROSION WAS FOUND ON SUPPORT ANGLE ON UNDER SIDE OF SHEAR DECK AT BS 1715, LBL 17-20. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT BS 1715, LBL 17-20; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 146N5240-12. 2L72 4F RTA2NM 20030326000472003032600047SO 2003 3 26 AUS20030128 120030103A315080054141 ANNUNCIATOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE CENTRAL WARNING WRONG PART W O OTHER W INADEQUATE Q C CRCRUISE 1 AUS (AUS) INCORRECT ANNUNCIATOR ASSEMBLY FITTED. PN 80054141 WAS FITTED INSTEAD OF THE CORRECT PN 80054153. UNAPPROVED/INCORRECT PART. PERSONNEL/MAINTENANCE ERROR. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20030321001152003032100115 2003 3 21 MWEA030137 420030321A34189650041027 STALL WARNING DOUG DC9 DC932 3022066WP COCKPIT FAILED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31501ME 47132 STALL INDICATING FAILURE LIGHT CAME ON. -- REMOVED AND REPLACED #2 STALL WARNING COMPUTER. 2L72 4F A6WE 20030326000752003032600075GL 2003 3 26 0074567 320030324A6110C083867 CLAMP BEECH 100 B100 1152919CE GARRTTTPE331TPE331* 01514WP HARTZLHCB4T HCB4TN3 GL PROP BLADE CORRODED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 EAA1506 CORRISION ON CLAMP ASSEMBLY 1L72 4T3 T A14CE E2WE 6 CP40EA 20030417000232003041700023WP 2003 4 17 UPS03840071 120030123A3350 RELAY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS WILL NOT CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY RELAY UNIT IAW MM 33-5 0-01. OPS CHECK NORMAL. 2L74 4F RT4A25 20030418000622003041800062NM 2003 4 18 QXEA0300269 120030207A5411 FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - AFT NACELLE FRAME CRACKED AT STATION XN210.00, ON OUTBOARD SIDE OF NACELLE, NEXT TO TRAILING EDGE OF WING. REPAIRED IAW HORIZON AIR EA 6-54-193. 2H72 4T RTA13NM 20030327000062003032700006EU 2003 3 27 AWXA200300269 120030301A5320D5347112420000 PLATE AIRBUS320 A320231 3930325EU 5320 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF HORIZONTAL WEB (SHEAR PLATE) AT FR 69-70, LBL 49. MAINTENANCE REMOVED CORRODED SHEAR PLATE AT FR 69-70, LBL 49; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-9, & 21-22, FIG. 65 & 66. 2L72 4F RTA28NM 20030423000762003042300076EU 2003 4 23 HE66085915 120030407A6330L633M2010101 MOUNT UROCOPEC135 EC135T1 5620026EU GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 FS01135CR763 0164 GEARBOX MOUNT LEAKING. REPLACED. 1G72 3U H88EU 20030423001062003042300106CE 2003 4 23 GLBA2003014 120030130A213113037432 CONTROLLER BEECH 1900 1900D 1154162CE CABIN PRESSURE FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03240GL565 UE240 A/C WOULD NOT PRESSURIZE, R&R CABIN PRESSURE CONTROLLER OPS CHK GOOD 2L72 4T RTA24CE 20030321000772003032100077NM 2003 3 21 2003UALA00218 120030223A5754114W411010 SKIN BOEING777 777222 1385219NM NR 14 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 TRAILING EDGE WEDGE, SLAT NR 14, DELAMINATED REPAIRED TRAILING EDGE WEDGE, SLAT NR 14. 2L72 4F RTT0001SE 20030728001092003072800109 2003 7 28 SWAA031626 420030721A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030801000262003080100026WP 2003 8 1 GTIA030534 120030614A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FRAME AT STATION 370 LONGERON 27R HAS DAMAGE FORWARD CARGO DOOR CUTOUT. REMOVED TWO SECTION FRAMES FROM STATION 370 B/N 27L-27R AND B/N 27R-18R. INSTALLED NEW FRAME FROM STRINGER 18R-28L STATION 370. (M) 2L72 4F A6WE 20030801000782003080100078NM 2003 8 1 UPS03240948 120030607A5320 SILL BOEING727 727185C 138406NNM PWA JT8 JT8D NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C CRACKS ON LT SILL IN NLG WHEEL WELL AT FWD END AND THE 6TH RIVET FROM FWD. HFEC TO CONFIRM CRACK. CUTOUT MADE AND STOP DRILLED, REPAIRED IAW SRM 51-40-02. 2L73 4F4 F A3WE E2EA 20040223000662004022300066WP 2004 2 23 UPS04841688 120031230A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, RT WING LE UPPER RIB IS CRACKED AT XFS 291. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLERS I.A.W. SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030828001702003082800170NM 2003 8 28 SWAA031865 120030820A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030829001972003082900197WP 2003 8 29 GTIA030622 120030726A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND SUB FLOOR CRACKED AT CUTOUT FOR FORWARD LAVATORY DUMP. TRIM OUT CRACK. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20030829002022003082900202NM 2003 8 29 USAA030131 120030731A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19523AU48516 23858 PIT - FOUND SKIN CRACKED AT STATION 727E, 4 INCHES ABOVE S24L. INSTALLED INTERIM DOUBLER PER EA 87406. (M) 2L72 4F RTA16WE 20030724000292003072400029NM 2003 7 24 DL73S030530 120030606A555165475953 FITTING BOEING737 737232 1384475NM HORIZONTAL STAB GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 THE UPPER ATTACH LUG OF THE HORIZONTAL STABILIZER CENTER SECTION WAS FOUND WITH A GOUGE FROM INTERFERENCED WITH AN IMPROPERLY INSTALLED FASTENER ON ADJACENT STRUCTURE. THE GOUGE WAS BLENDED TO A SMOOTH CONTOUR AND NDT INSPECTED. THE GOUGED FITTING WAS AUTHORIZED FOR SERVICE WITH REPETITIVE INSPECTION REQUIREMENTS PER ER/A 385224-14AD. 2L72 4F RTA16WE 20030724001312003072400131NM 2003 7 24 DL757030579 120030620A5330141N33313 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 422 & 434 AND BETWEEN STRINGERS 15L & 16L. THE DENT WAS REMOVED WITH A 12.6 X 11.9 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385124-14, REV A. 2L72 4F RTA2NM 20030805000972003080500097EU 2003 8 5 SIMA200319703 120030627A5330AL2024T3 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21340RC 340B340 ABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE AT STRINGER 420.9 AND STATION 425.5 ABOVE STRINGER 1501. RECONTOURED DENTS AND PERFORMED A EDDY CURRENT INSPECTION. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS005555 PARA 8, 340 SRM (72LKS 3079 REV 41) CHAPTER 53-70-10 FIG 209. (M) 2L72 4T RTA52EU 20030801000222003080100022WP 2003 8 1 2003F00505 120030709A3350AD4002P BATTERY DOUG DC9 DC931 3022065WP CABIN DISCHARGED A A4JAO OTHER O OTHER ININSP/MAINT 1 SO35934LK 48157 DURING B-CHECK PIE MAINTENANCE, FOUND EMERGENCY LIGHTS AT BOTH FORWARD OVERWING EXITS DIM. REPLACED BATTERIES IN EMERGENCY LIGHT POWER PACK ASSEMBLIES IAW MM 33-53-0, SYSTEM CHECKS NORMAL. (M) 2L72 4F A6WE 20030807001072003080700107CE 2003 8 7 GLBA2003114 120030805A3244 TIRE BEECH 1900 1900D 1154162CE MAIN WHEEL ASSY SEPARATED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03261GL53 2821 UE261 NR 2 TIRE TREAD CAME OFF. REMOVED AND REPLACED NR 1 & 2 WHEEL ASSY. 2L72 4T RTA24CE 20030812000422003081200042 2003 8 12 HEEA088378 420030715A22307611133 AMPLIFIER SKRSKYS76 S76A 8143006NE ROLL SLICE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03763P 760166 ROLL SLICE AMPLIFIER INOPERATIVE WENT FULL LEFT AND STOPPED. 1G72 3U H1NE 20030903002372003090300237EA 2003 9 3 03235663 120030823A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27663BR 7527 DURING MAINTENANCE INSPECTION THE FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FORWARD EMERGENCY LAMP. A SATISFACTORY OPERATIONAL OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030903002082003090300208EA 2003 9 3 QXEA200300970 120030812A2550 SUPPORT BRACKET CNDAIRCL600 CL6002C10 1390015EA CARGO BAY CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX- AFT CARGO BAY NET SUPPORT BRACKET HAS A .5000 INCH CHAFE AT THE AFT SECTION OF THE SUPPORT BRACKET JUST ABOVE THE CABLE PULLEY. REPAIRED IAW HORIZON AIR EA R-53-124. 2L72 4F RTA21EA 20030905002292003090500229SO 2003 9 5 C2XA03TY124 120030811A534714530659009 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713989 145271 TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF6 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030813002142003081300214NM 2003 8 13 SWAA031711 120030729A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26R AND STR 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030814000212003081400021NM 2003 8 14 SWAA031733 120030803A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20030728001292003072800129NM 2003 7 28 SWAA031433 120030629A53126546568 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED SPECIAL VISIT, FOUND AFT PRESS BULKHEAD CORRODED AT BS 1016, LBL 3. REPAIRED BULKHEAD PER SRM. 2L72 4F A16WE 20030825000982003082500098NM 2003 8 25 VNAA0308002 120030804A2440 FUSE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EXTERNAL POWER BLOWN A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07426JS 3038 WITH THE EXTERNAL POWER HOOKED UP, SMOKE ENTERED THE FLIGHT DECK AND THE PASSENGERS WERE DEPLANED. MAINTENANCE INSPECTED AND REPLACED BOTH FUSES IN THE GROUND POWER SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANAUL 24-00-00, BUT GROUND POWER WAS STILL INOP. MAINTENANCE THEN DEFERRED THE GROUND POWER SYSTEM , 24-24 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030825001102003082500110EU 2003 8 25 03230302 120030818A3397 SPLICE JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27302UE 41013 DURING MAINTENANCE INSPECTION THE MID EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL RECONNECTED THE SPLICE IN THE EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20030825000682003082500068WP 2003 8 25 UPS03841000 120030723A572046143901 ATTACH FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:SP UPPER ATTACH FITTING AT STRINGER 61 IS CRACKED AT XRS 255. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4614390 AND SRM 51-1-20D. 2L74 4F RT4A25 20030826001522003082600152EU 2003 8 26 SIMA200320810 120030726A3350330115 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21370AM 340B370 SJT - FLT 3676 - CREW REPORTED THE EXIT LIGHTS ADJACENT TO OVERWING EMERGENCY EXITS WILL NOT STAY ILLUMINATED DURING TEST. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 23LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030827001232003082700123NM 2003 8 27 CALA0300367 120030708A3397BR963512024 WIRE HARNESS BOEING757 757224 1384958NM CABIN DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717122 27564 INSPECTION FOUND THE FLOOR PROXIMITY LIGHT WIRE HARNESS. DAMAGED IN TWO PLACES BETWEEN SEATS 15-25. THE WIRE HARNESS WAS REPLACED IAW ACM DRAWING BR2013-P-757CO/-1/-2/-3. 2L72 4F RTA2NM 20030910002162003091000216EU 2003 9 10 MALA030356 120030702A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING C-CHECK INSPECTION IN CVG, FLOOR FRAME 18 UPPER SURFACE HAS MULTIPLE CRACKS AND CORROSION, FROM 3.2500 INCH RIGHT OF NR 3 SEAT RAIL AND ENDS UNDERNEATH NR 4 SEAT RAIL. MAINTENANCE REPAIRED IAW EO NR A53124, REFER TO 409 NR 128103 FOR FURTHER DETAIL. A/C RELEASE DATE 7/25/2003. 2H74 4F RTA49EU 20030911001042003091100104NM 2003 9 11 03FDEA01089 120030709A5510 BARREL NUT DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT HORIZONTAL STAB NR 3 BORE CORROSION EXCEEDED LIMIT. LT HORIZONTAL STAB NR 3 BORE CORROSION REPAIR CARRIED OUT IAW EA 1-5510-71837, STABILIZERS- HORIZONTAL STAB BARREL NUT BORES- CORROSION REMOVAL- BORE 3 LEFT. 2L73 4F4 FRTA22WE E13NE 20030930001112003093000111NM 2003 9 30 03FDEA01489 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) ACTUATOR MOUNT I/B LUG CORRODED. 2L73 4F RTA22WE 20031002001212003100200121NM 2003 10 2 QXEA200301105 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 12 SEAT TRACK IS CHAFED ON BOTTOM OF CAHNNEL AND ON LT AND RT SIDES OF SEAT RAIL BORE INNER DIAMETER FORWARD OF STATION X 545. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-3644. 2H72 4T RTA13NM 20030905002342003090500234WP 2003 9 5 DHL2003873591 120030705A5210 SKIN DOUG DC8 DC873F 302199FWP PAX DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 FORWARD PASSENGER ENTRANCE DOOR SKIN HAS INTERIM REPAIR AT FS 25 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030619, ED-3438. REMOVED FASTENERS, TRIMMED OUT THE SKIN SEGMENT IAW EODHL-030619, ED-3438. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER AND A FILLER IAW EODHL-030619, ED-3438. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER ON FWD PASSENGER ENTRANCE DOOR SKIN (FS 25.000) USING NEW FASTENERS IAW EODHL-030619, ED-3438, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030908002892003090800289NM 2003 9 8 SWAA031938 120030828A53306545766 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG AT BS 520, STR 12L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031006000822003100600082NM 2003 10 6 249TR0019 120030912A335020131A BATTERY BOEING737 7372K5 138448XNM EMERGENCY LIGHT DISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 FORWARD EMERGENCY LIGHT BATTERY WILL NOT HOLD A CHARGE. REPLACED EMERGENCY LIGHT BATTERY IAW MM 25-60. OPS. CHECKS OK. 2L72 4F RTA16WE 20031008000442003100800044NM 2003 10 8 VNAA0309006 120030808A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07430JS4540 148 3044 THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT 9A WAS INOP. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031015000042003101500004SO 2003 10 15 GLBA2003136 120030919A2121EVAC2322C2 COOLING FAN EMB 120 EMB120ER 3260203SO CABIN SMOKE A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03293UX5850 120293 SMOKE IN CABIN, R&R GROUND COOLING FAN OPS CHECK GOOD. 2L72 4T RTA31SO 20031022001502003102200150EA 2003 10 22 SWIA200312435 120030922A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO BAY DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 CARGO PIT; STEP SUPPORT IS CRACKED AND BROKEN OUT ALONG LENGTH OF IB SIDE. (DISCOVERED DURING C-CHECK INSPECTION) NEW CARGO PIT STEP PLATE SUPPORT INSTALLED IAW CRJ AMM 20-21-00 AND CRJ SRM 51-41-02. PN: 601R35205-37 2L72 4F4 FRTA21EA E15NE 20031028001152003102800115NM 2003 10 28 AALA20030994 120030911A33500201991008 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A K NONE L NO TEST ININSP/MAINT 1 SW21642AA 24600 TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROW 15D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031029000472003102900047NM 2003 10 29 ASAA0310401 120030506A53306545778 SKIN BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND SKIN PANEL AT BS 925, STRINGER 24R DENTED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20040204000832004020400083NM 2004 2 4 AWXA200301274 120031002A53206545855524 WEB BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF RT AFT OUTBOARD SHEAR WEB AT BS 1015, RBL 43.5, WL 207. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED RT AFT OUTBOARD SHEAR WEB AT BS 1015, RBL 43.5; FABRICATED A NEW REPLACEMENT WEB IAW DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 12, SHT 1-3. 2L72 4F4 FRTA16WE E2GL 20040204001762004020400176NE 2004 2 4 006876 320031029A6111 BLADE AEROSPATR42 ATR42* 8680900EU PWA PW121 PW121 52124NE HAMSTD14SF 14SF* NE PROPELLER CRACKED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 CRACK IN BLADE POSITION NR 2 ENGINE SIDE. 2H72 4T4 TRTA53EU E20NE 6 CP7NE 20031103000132003110300013NM 2003 11 3 DLM88030865 120030922A2530 COFFEEMAKER DOUG MD88 MD88 3023688NM AFT GALLEY DIRTY A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27920DE 53423 ON TAKEOFF FROM ATLANTA THERE WAS AN ODOR OF BURNED RUBBER IN CABIN. NO SMOKE DETECTORS NOR ALARMS WENT OFF NOR ANY SMOKE OR HEAT NOTICED BY CREW OR PASSENGERS. ODOR DISSIPATED DURING CLIMBOUT AND WAS GONE AT LEVEL OFF. MTC PERFORMED OPN 5088 DUCT BURNOUT. DURING INSPECTION FOUND BURNT DEBRIS ON AFT GALLEY COFFEEMAKER HOT PLATE. CLEANED HOT PLATE AND ODOR WENT AWAY. 2L72 4F RTA6WE 20031105000582003110500058NM 2003 11 5 SWAA032311 120031020A53306545773 SKIN BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D+12, ABOVE STR 10R. REPAIRED SKIN PER ERO. 2L72 4F RTA16WE 20031106002402003110600240WP 2003 11 6 GTIA030719 120030826A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND MID PIT HAS CORROSION AT FRAME STATION 522, STATION 598. FOUND OUT OF LIMITS AT STATION 522. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR ANGLE AND DOUBLER. (M) 2L72 4F A6WE 20030912000092003091200009NM 2003 9 12 AWXA2003007AA 120030702A27512061141 INDICATOR BOEING737 7373S3 1384711NM COCKPIT FALSE INDICATIONA AWXAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 WP28312AW110241843 24060 ON DECENT INTO BUR EN ROUTE FROM PHX TRAILING EDGE FLAPS LOCKED OUT BETWEEN 1 AND 2 DEGREES. RUNWAY TO SHORT AT BUR, DIVERTED TO LAX WITH LONGER RUNWAY. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR, OPERATIONAL CHECK WAS GOOD IAW BMM 27-58-41, PG. 401-404. VENDOR FUNCTIONAL TEST OF FLAP POSITION INDICATOR S/N 1686 WAS NO FAULT FOUND, INSPECTED AND TESTED IAW CMM 27-50-03. 2L72 4F RTA16WE 20031117000612003111700061EA 2003 11 17 COMA0360449 120031003A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA MAINS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01514CA 7809 FLIGHT 5894 LANDING GEAR FAILED TO RETRACT. PARKING BRAKE AND ANTI SKID CAUTION MESSAGE. COULD NOT DUPLICATE. LANDING GEAR RETRACTION CHECKS NORMAL. 2L72 4F RTA21EA 20031118001202003111800120NM 2003 11 18 03282402 120031009A3350 LIGHT DORNERDO32 DO328300 NM CABIN MALFUNCTIONED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27402FJ 3147 DURING INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED A SATISFACTORY OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20040113000722004011300072EU 2004 1 13 BAQA091661 120031219A6330L633M2010103 PISTON UROCOPEC135 EC135P2 EU MRGB MOUNT LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03868ME12 0288 MAIN ROTOR GEARBOX MOUNT LEAKING/PISTON RETRACTED. HARDCARD ENCLOSED. PART REPLACED WITH SERVICABLE UNIT. 01/06/2004 1G72 3U H88EU 20040114000172004011400017NM 2004 1 14 2003UALA00839 120031105A335060243 LAMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 24251 EMERGENCY EXIT FLOOR LIGHTING PULLED UP AND INOPERATIVE AT ROW 21. REPLACED LIGHT STRIP. 2L72 4F4 FRTA16WE E2GL 20031218001362003121800136WP 2003 12 18 UPS03841586 120031119A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, FINGER DOUBLER IS CORRODED BEYOND LIMITS STATION 879-902 AT LBL 64. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-7-1 FIG 10, 51-1-21. 2L74 4F RT4A25 20031219000062003121900006WP 2003 12 19 ABXA030453 120031114A57403914724501 FITTING DOUG DC9 DC931 3022065WP LT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 LT MLG WW OUTBOARD APPROXIMATELY FS 730 SUPPORT BRACKET CRACKED FOR UPPER INBOARD BONDED PANEL LINK. REPLACED FITTING IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20031222000482003122200048EA 2003 12 22 COMA0360532 120031207A531160036030 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01721CA 7259 CRACK NOTED AT FS 718.00 RT BETWEEN STRINGER 11 - 12. REPAIRED PER SERVICE BULLETIN 601R-53-055 PART B PER EA 10-5320-00242. 2L72 4F RTA21EA 20031223001652003122300165EA 2003 12 23 ASOA03551 120031031A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11862AS 7445 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20031010000662003101000066EA 2003 10 10 SWIA200312417 120030912A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07405SW8874 6618 7029 FLIGHT SPOILER STATUS MESSAGE. RESET CB'S. REPLACED LEFT SPOILERON SYSTEM 1 ACTUATOR PER MM 27-62-01. LEAK AND OPS CHECK OK. 2L72 4F RTA21EA 20031125000552003112500055WP 2003 11 25 DHL2003807510 120031007A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT WING CENTER L/E FORMER CRACKED 0.500 AT STA 367.000. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125000832003112500083WP 2003 11 25 DHL2003805573 120030807A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E CORRODED FROM STA XFS 297.500 - XFS 310.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG 44. FABRICATED SKIN SPLICE IAW SRM 57-2-1 FIG 44. CLEANED, TREATED AND PRIMED SKIN SPLICE INTERIOR SURFACE IAW SRM 51-1-8B. INSTALLED NEW SKIN SPLICE WITH NEW FASTENERS ON LEFT CTR L/E (STA XFS 297.500 - XFS 310.250) IAW SRM 57-2-1 FIG 44, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. SEE N/R 0184 FOR CTR L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031204000372003120400037WP 2003 12 4 GTIA030844 120031011A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FLOOR SUPPORT AT FS 146 TO 154 LBL 53 HAS CORROSION. FLOOR SUPPORT REMOVED. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20031204001692003120400169CE 2003 12 4 AMWA63 120031010A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07218YV UE218 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RIGHT SIDE NEAR THE FORWARD, CENTER AND AFT STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031205000292003120500029NM 2003 12 5 DLM88030919 120031012A79301163P0041 SWITCH DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE SHORTED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27977DL 53258 726944 AIR TURNBACK, RIGHT ENGINE OIL FILTER CLOGGED MESSAGE ON EOAP. T/S--SHOOK DOWN WIRING AT ENGINE -NTF. CHECKED AND REPLACED MAIN ENGINE OIL FILTER AND DETECTOR--NTF. REPLACED BAD OIL DIFF PRESSURE SWITCH. LEAK AND OPERATIONAL CHECKS OK. 2L72 4F4 FRTA6WE E9NE 20031209001782003120900178WP 2003 12 9 ABXA030407 120031013A531359203192 LONGERON DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 LONGERON 30 CRACKED LEFT AND RIGHT FLANGES SM 243 - 245. REPLACED LONGERON 30, STA 230 - 265 IAW REA D953-48386MR. 2L72 4F A6WE 20031208000712003120800071NM 2003 12 8 AWXA200301292 120031013A5315146N5417 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1362, RBL 14. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM BETWEEN BS 1343 AND BS 1365, RBL 14; FABRICATED 4 EACH REPAIR ANGLES & 2 EACH CHANNELS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 1. 2L72 4F RTA2NM 20031210000322003121000032NM 2003 12 10 MWEA030469 120031203A521099557529 BEAM DOUG MD88 MD88 3023688NM PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FORWARD PASSENGER DOOR TOP BEAM IS CRACKED AT FORWARD END. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20031121000522003112100052NE 2003 11 21 SWAA032490 220031110A72509995M22 BLADE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 2 ENGINE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 720487 DURING SCHEDULED C4 CHECK, NR 1 ENG FAILED BORESCOPE INSPECTION DUE MISSING MATERIAL AT 1 EA HPT BLADE T/E. REMOVED AND REPLACED NR 2 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20031217000922003121700092NM 2003 12 17 AWXA200301487 120031106A532069387902 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER CLIP BS 578, STR 10 RT. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP BS 578, STR 10 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-38790; INSTALLED REPAIR PART IAW B737-200 SRM 51-40-02 FIG 2, 3 & 8 PG 1, 23 & 38. 2L72 4F RTA16WE 20031219000912003121900091NM 2003 12 19 2003UALA00919 120031201A339758781 WIRE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29946UA 26687 EEL FLOOR STRIP DOES NOT ILLUMINATE FROM SEAT 14 BACK. REPLACED EEL PATH LIGHTING CABLE FROM ROW 14 ABC AFT. 2L72 4F4 FRTA16WE E2GL 20031223000312003122300031NM 2003 12 23 SWAA032634 120031201A53106547978 CREASE BEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 727C+8, LT SIDE, BS 727B+8, RT SIDE. REPAIRED CREASE BEAM SECTIONS PER SRM. 2L72 4F RTA16WE 20031229000162003122900016NM 2003 12 29 SWAA032711 120031210A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 AFT UPPER FLASHLIGHT CHARGE LIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030918000212003091800021NM 2003 9 18 2003F00564 120030424A5330 SKIN BOEING737 7372L9 1384497NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37464AT 21278 DURING C-CHECK INSPECTION, THE FUSELAGE WAS FOUND TO BE CRACKED AT THE R1 DOOR LOWER AFT CORNER. THE CRACK WAS 2.5 TO 3 INCHES AND VERIFIED BY NDT. ALL REPAIRS HAVE BEEN ACCOMPLISHED ON NON ROUTINE 031033. TOTAL AIRCRAFT TIME 46985.2, TOTAL CYCLES 41351. (M) 2L72 4F RTA16WE 20030919000372003091900037NM 2003 9 19 375PA0017 120030807A56105717623134 WINDOW BOEING737 737317 138447PNM COCKPIT CRACKED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05375PA 23812 FIRST OFFICER'S SIDE WINDOW CRACKED. REPLACED R-2 WINDOW IAW MM 56-12-11. OPS CHECKS GOOD IAW MM 30-41-12. 2L72 4F RTA16WE 20040109000512004010900051WP 2004 1 9 Y2PA03019 120030905A2612 FIRE DETECTOR DOUG DC9 DC915F 3022037WP CARGO BAY MALFUNCTIONED A Y2PAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23199US 47153 LOWER CARGO FIRE WARNING CAME ON IN FLIGHT. AC IN HOLD BECAUSE AIRPORT WAS CLOSED FOR THUNDERSTORMS. LOWER CARGO FIRE WARNING ANNUNCIATOR CAME ON. CREW REFERRED TO COM AND FOLLOWED PROCEDURES. CREW DECLARED EMERGENCY AND DIVERTED. ON DESCENT, LIGHT WENT OUT. AC LANDED WITHOUT FURTHER INCIDENT. ON GROUND, AREA INDICATED BY WARNING WAS INSPECTED AND NO EVIDENCE OF FIRE OR SMOKE WERE FOUND. DETECTION SYS WAS DEFERRED AND AC CONTINUED TO DESTINATION WHEN WEATHER IMPROVED. NO FURTHER PROBLEMS WERE ENCOUNTERED. UPON RETURN, LOWER CARGO SMOKE DETECTION SYS WAS OPERATIONALLY CHECKED IAW CARGO SMOKE DETECT MM AND OPS CKD GOOD, NO DEFECTS NOTED. AC RETURNED TO SERVICE. UNABLE TO DUP PROBLEM. (M) 2L72 4F A6WE 20031202000352003120200035NM 2003 12 2 ASAA0340085 120030228A5320656571035 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON NR 3 VHF ANTENNA CHANNEL. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031125001122003112500112SW 2003 11 25 2003F00615 120030607A21971N4005 WIRE FRCHLDSA227 SA227DC 3377521SW AIR DISTRIBUTIONBROKEN A BSAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM05453LA DC852B GDV - FLT 2578 - ON DESCENT TO THE STATION, HOT AIR AND SMOKE STARTED COMING OUT OF THE RIGHT BLEED, WITH THE RIGHT BLEED SHUTOFF AND DEFERRED. CREW FOLLOWED PROCEDURES AND LANDED AT THE NEXT STATION, WHICH WAS THE CLOSEST. THE FLOW CONTROL VALVE WAS RECEIVING AN UNCOMMANDED OPEN SIGNAL, THE ENVIRONMENTAL AIR DUCTING GOT HOT, WHICH CAUSED SMOKE. FOUND INTERMITTENT FAILURE DUE TO BROKEN WIRE ON A DIODE ON THE BLEED SWITCH. THE DIODE WIRE HAD BROKEN AT THE CRIMP CONNECTOR, WHICH WOULD OPEN AND CLOSE THE CIRCUIT, CAUSING AND UNCOMMANDED BLEED VALVE OPENING. THE DEFERRED RIGHT ACM WAS ALSO REPLACED AT THIS TIME. (M) 2L72 4T RTA18SW 20031202001342003120200134EA 2003 12 2 A6WA200340152 120031028A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RIGHT WING UNDERSIDE SKIN HAD NUMEROUS SCRATCHES AND GOUGES OUTBOARD OF WS 178 BETWEEN X163-X199. BLENDED AND SMOOTHED OUT DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION OF AREAS, ALODINED PRIMED AND TOP COATED ALL BARE METAL IAW WVAC EO 601R-57-4317. (M) 2L72 4F RTA21EA 20031203000502003120300050NM 2003 12 3 GAIA03156ST 120031024A53117075T6 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME DETNED IN RADIUS AT BS 720 STR 17 RT. REF FASI N/R NR 61885, CUT OUT DAMAGE 1 INCH BY 1 INCH AND INSTALLED REPAIR PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20040115001152004011500115NM 2004 1 15 03FDEA02088 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE FOUND WITH 7 LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE 7 CRACKED LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. AND SRM 51-38-01 VOL. II. 2L73 4F RTA22WE 20040121000712004012100071EA 2004 1 21 ASOA03606 120031125A335058351 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A GROUND INSPECTION IN IAH, THE FLOOR EMERGENCY LIGHT STRIP IN THE FORWARD SECTION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ORANGE FLOOR EMERGENCY LIGHT STRIP IN THE FORWARD SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031205000362003120500036NM 2003 12 5 DLM88030926 120031013A3350LP7265001 BULB DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER L NO TEST ININSP/MAINT 1 SO27911DE 49967 EMERGENCY LIGHT INOP AT 25E. RELAMPED, CHECKS NORMAL. 2L72 4F RTA6WE 20031001000552003100100055NM 2003 10 1 CALA0300570 120031001A5330 SKIN BOEING777 777224 1385225NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777014 29862 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT BS 655-676, S26L-S27L FORWARD OF L-2 DOOR. THE SKIN WAS REPAIRED IAW ECRA 5330-03287. A DIP WAS INITIATED TO REINSPECT THE REPAIR AREA AT A THRESHOLD OF 30,000 TOTAL FLIGHT CYCLES AND REPEAT THE INSPECTION TASK AT EVERY 8,000 FLIGHT CYCLES THEREAFTER. 2L72 4F RTT00001SE 20030909002372003090900237GL 2003 9 9 67341 320030719A6111114HCA BLADE MCAULY JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MCAULY5JFR36B5JFR36C1103GL PROPELLER CRACKED B EY2RK NONE O OTHER UKUNKNOWN 1 GL03 952540 41076 952540 CRACK ON BLADE. 2L72 4T3 TRTA41NM E2WE 6 CP15NE 20031002000262003100200026EU 2003 10 2 A6WA200360035 120030906A5310 STRUCTURE BAC 146 146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 FOUND CRACK AT RIVET LOCATION JUST AFT OF FRAME 29 STRINGER 13 LT. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060002. (M) 2H74 4F A49EU 20031003000902003100300090NM 2003 10 3 DHL2003743014 120030913A3350MISC062 BATTERY BOEING727 727225 1384077NM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 EMERGENCY EXIT LIGHTS FAILED TO OPERATE DURING STANDBY POWER CHECK AND DURING NORMAL OPERATIONS. REPLACED EMERGENCY EXIT LIGHT BATTERIES. OPS CHECKED GOOD IAW B727 M/M 33-50-71. P/N OFF AND ON: MISC-062. 2L73 4F A3WE 20031006000402003100600040NM 2003 10 6 QXEA200301125 120030912A521085210127051 STRUT DHAV DHC8 DHC8202 2809007NM PAX DOOR MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09347PH 480 ON FLIGHT 2074 FLIGHT ATTENDANT REPORTS PASSENGER DOOR IS VERY HARD TO OPEN. REMOVED AND REPLACED OVERCENTER GAS SPRING FORWARD DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031021000962003102100096SO 2003 10 21 SIMA200324611 120030821A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21716AE 145264 ABI - FOUND DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2779. (M) 2L72 4F RTT00011AT 20030910000792003091000079WP 2003 9 10 DHL2003604556 120030528A573057624433 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING T/E LOWER PANEL INTERNAL AND EXTERNAL SKIN DELAMINATED (NR 577B ACCESS). REMOVED AND REPLACED DELAMINATED LOWER PANEL ON LT WING T/E (NR 577B ACCESS) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031029001212003102900121EU 2003 10 29 KBM2003F00016 120030812A2110590008 COMPRESSOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE AIR CONDITIONER INOPERATIVE E KBMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP19230SH105 2337 BURNING ODOR IN CABIN AND A/C SYSTEM SUSPECTED TO BE INOPERATIVE. INSPECTED, REMOVED AND REPLACED A/C COMPRESSOR.(K) 1G71 3U3 UNCH9EU E19EU 20031027001402003102700140NE 2003 10 27 225035 220030929A7200500809501 MANIFOLD DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE 8TH STAGE BLEED BROKEN B T48RO OTHER O OTHER NRNOT REPORTED 1 GL09 718236 8TH STAGE BLEED MANIFOLD BROKE AND BECAME LODGED BETWEEN PRIMARY FUEL MANIFOLD AND DIFFUSER FAIRING. RESULTING IN PIN HOLE CHAFE IN PRIMARY MANIFOLD. 2L72 4F4 FRT E9NE 20031120000882003112000088NE 2003 11 20 NACA20030116 220031014A8500R2800 ENGINE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 3 MAKING METAL A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F1117 1117 533265 P31893 NR 3 ENGINE SHUT DOWN DUE TO LOSS OF BMEP. ENGINE MAKING METAL, REPLACED ENGINE. 2L74 4R4 R A781 5E8 20040212000912004021200091CE 2004 2 12 8394094 120031209A1430AN17517A BOLT RAYTHN BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA CONTROL HORN BENT A JJBAK NONE O OTHER ININSP/MAINT 1 EA01839CA4758 UE385 DURING DETAIL NR 6 INSPECTION FOUND RUDDER CONTROL HORN MOUNT BOLT BENT AND TORQUE TUBE MOUNT BOLTS LOOSE. 2L72 4T3 TRTA24CE E2NE 20031112000262003111200026NE 2003 11 12 SWIA200312577 220031028A7261 ENGINE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE NR 1 LACK OF LUBE A SWIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 NM07567SW 120342 SHUT DOWN NR 1 ENG ON TAXI DUE TO LOSS OF OIL PRESSURE. SERVICED ENGINE WITH OIL AND TIGHTENED OIL FILL CAP. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20030918000072003091800007NM 2003 9 18 03FDEA01506 120030911A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 FRAME CRACKED BS 360 LBL 2 WL 155. CUT-OUT CRACK DAMAGE ON FRAME PER 727 SRM 51-10-1. FABRICATED REPAIR ANGLE FROM 7075T6 .050, LOT 508357 PER 727 SRM 51-40-3. LOCATED & DRILLED ANGLE PER 727 SRM 51- 40-3. ALODINED, PRIMED & PAINTED ANGLE PER 727 SRM 51-10-2. INSTALLED REPAIR ANGLE PER 727 SRM 51-30-2 AND 51-40-3. 2L73 4F RTA3WE 20031119001302003111900130NM 2003 11 19 2003UALA00762 120031005A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 FUSELAGE SKIN DENTED STA 927 BELOW STR 20L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031120000662003112000066NM 2003 11 20 QXEA200301255 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 6 SEAT TRACK CHANNEL HAS LITE PITTING AT STATION X545.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36 AND RD 8-53-784. 2H72 4T RTA13NM 20031208000422003120800042CE 2003 12 8 297031 120031022A3150 CIRCUIT CARD BEECH 1900 1900C 1154161CE MASTER CAUTION MALFUNCTIONED A NSVAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27207CJ UC107 DURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TO INDICATE THAT BOTH THE LEFT AND RIGHT GEN TIES WERE OPEN ONE ATTEMPT WAS MADE TO RESET. DID NOT RESET, THE TAKEOFF WAS ABORTED. 2L72 4T RTA24CE 20031209000212003120900021EA 2003 12 9 COMA0370042 120031022A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA2599 10064 FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPLACED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031209000522003120900052NM 2003 12 9 UPS03441481 120031017A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, DURING RAP INSPECTION ITEM N525UP-41-02 BS 375-390 STR 26L-27L REPAIR DOUBLER WITH TWO REPAIR FASTENER ROWS ONLY REPAIR REQ'D. BS 375-390 S26L-S27L FX SKIN EXTERIOR PREVIOUSLY DOUBLER REMOVED AS PER SRM 51-30-02 AND SKIN CUTOUT ENLARGED AS PER SRM 53-30-03 FIG 1. ALL FASTENER HOLES AND SKIN CUTOUT HFEC ACCOMPLISHED AS PER NTM PART 6 51-00-00 FIG 1 & 4 AND NO DEFECT FOUND. EXTERIOR REPAIR DOUBLER FABRICATED & INSTALLED AS PER SRM 53-30-03 FIG 1. 2L74 4F A20WE 20031209000942003120900094NM 2003 12 9 SWAA032314 120031018A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STR SPLICE 14R CRACKED AT BS 908. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20031209001662003120900166WP 2003 12 9 DHL2003809003 120031031A5250 DOOR DOUG DC8 DC873F 302199FWP COCKPIT OUT OF ADJUST A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL 46047 COCKPIT DOOR IS HARD TO OPEN FROM THE OUTSIDE. DOOR JAMMED CLOSED. ADJUSTED COCKPIT DOOR PER M/M 52-10-0. OPS CHECKED GOOD. 2L74 4F RT4A25 20031209001862003120900186NM 2003 12 9 UPS03441512 120031016A531269B11571 BULKHEAD BOEING747 747212B 1384886NM RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, RT MLG WW BS 1241 BULKHEAD CORRODED AT WL 143 BETWEEN RBL 1 & 3 AREA AS MARKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.116 X 1 X 1 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO HX RS R57-12-35092 & UPS AUTH 747-57-20049, CIC APPLIED IAW EO M5100-2780-E. 2L74 4F A20WE 20040122000522004012200052EA 2004 1 22 ASOA03643 120031212A5210601R3807423 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11905EV 7632 DURING A HANGAR INSPECTION, THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR THE CRACK AND REPLACE DOOR CABLE ANCHOR FITTING WITHIN 100 FLIGHT HOURS IAW REO 601R-52-11-272. (M) 2L72 4F RTA21EA 20040127001772004012700177WP 2004 1 27 ASAA0380648 120031015A532199366921 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC DURING 30K CHECK, FLOORBOARD IS CORRODED AT FS 1113-1174, AND HAS 15 INSERTS EITHER CRACKED, MISSING, OR CORRODED. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20031014001312003101400131NM 2003 10 14 SWAA032161 120030925A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BELOW STR 15L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031014001502003101400150NM 2003 10 14 SWAA032057 120030916A2560PH22300L STRIP BOEING737 7373H4 1384600NM AFT CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 EEPLS PHOTOLUMINESCENT STRIP LOOSE LAST 4 ROWS IN CABIN LT SIDE. SECURED STRIP PER MM. 2L72 4F RTA16WE 20030917000772003091700077EU 2003 9 17 ALGA089090 120030910A6510C651A2001101 DISC PACK UROCOPEC120 EC120B 8680987EU T/R DRIVESHAFT CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL88 1263 FOUND ONE CRACKED LAMINATE ON TAIL ROTOR DISC PACK. REMOVED AND REPLACED. 1G72 3U NCR0001RD 20030918000462003091800046WP 2003 9 18 GTIA030488 120030624A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FOUND FORWARD CABIN CRACKED/DAMAGED ON WEB STATION 180 RBL 24 TO 30. REMOVED DAMAGED WEB AREA. FABRICATED NEW WEB AND SPLICE. INSTALLED WEB AND SPLICE. (M) 2L72 4F A6WE 20031212000272003121200027NE 2003 12 12 SWAA032423 220031102A7260641000 GEARBOX BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 2 ENGINE LEAKING A SWAAK NONE KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW29092SW 22964 687780 LOSS OF ALL OIL QTY INDICATION AT NR 2 ENGINE. REMOVED AND REPLACED ACCY GEAR BOX PER MM. 2L72 4F4 F A16WE E2EA 20030916001292003091600129NM 2003 9 16 AALA20030587 120030519A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21942AN 30084 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT OPPOSITE FIRST CLASS CLOSET INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT AT FIRST CLASS CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030924000462003092400046NM 2003 9 24 DLM88030760 120030817A30301049491 HEATER DOUG MD88 MD88 3023688NM STATIC PORT BURNED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27972DL 53215 PASSING 26000 THE FLT/ATT NOTIFIED COCKPIT THAT THEIR WAS AN ELECTRICAL ODOR IN THE AREA OF SEAT 22A. FOLLOWED POM. RETURNED TO CVG. ODOR CONTINUED FOR 15 MINS. NEVER REACHED FWD CABIN OR COCKPIT. NO SMOKE. TROUBLESHOT FOUND LEFT STATIC PORT HEATER INOPERATIVE AND BURN DAMAGED. REPLACED SAME. 2L72 4F RTA6WE 20040112000462004011200046EA 2004 1 12 033526691 120031218A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE RT WING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040109000632004010900063WP 2004 1 9 AALA20031262 120031113A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21407AA 49318 DURING OVERNIGHT MAINTENANCE, FOUND BOTH AFT OVERWING AUXILIARY UPPER EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-105 FOR AFT OVERWING AUXILIARY UPPER EXIT ILGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031124000592003112400059CE 2003 11 24 GLBA2003151 120031119A2750 FLAP BEECH 1900 1900D 1154162CE WING STUCK A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03253GL UE253 FLAPS STUCK AT 17 DEGREES. ADJUSTED FLAP SAFETY SWITCH B27RW82255518T OPS CK GOOD 2L72 4T RTA24CE 20031217001732003121700173NM 2003 12 17 SWAA032647 120031202A53106546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 807 LBL 1 WL 149. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031217001772003121700177NE 2003 12 17 PCAA0312148 220031211A7261 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 OVERSERVICED A PCAAA UNSCHED LANDING WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA13830EX 155 FLIGHT 3760, DIVERTED DUE TO SEVERAL PASSENGERS DETECTED A BURNING ODOR THROUGHOUT CABIN, PILOT ALSO DETECTED BURNING ODOR COMING FROM ALL VENT UPON OPENING COCKPIT DOOR. EMERGENCY WAS DECLARED AND THE PASSENGER COMPARTMENT WAS PREPPED FOR SAME. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOTH ENGINES AND APU. MAINTENANCE FOUND NR 2 ENGINE OIL OVERSERVICED. APU BLEEDS WERE RAN AND AIRCRAFT ENGINES WERE RUN INDEPENDENTLY, NO BURNING ODORS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031222001092003122200109NM 2003 12 22 MEX2003534 120031125A3411 PITOT TUBE BOEING757 7572Q8 1384972NM RT AUXILARY DAMAGED A ASMFD RETURN TO BLOCK GJ MULTIPLE FAILURE WARNING INDICATION TXTAXI/GRND HDL 1 SW23805AM 26272 AIRCRAFT RETURNED TO GATE DUE TO (R AUX PITOT) LIGHT WAS TURNED ON AND THE CABIN TEMPERATURE CONTROL HAD A FAILURE, TEMP REACHED 37 DEGREES CELSIUS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE RELATED PITOT WIRES/CONNECTORS AND THE CABIN TEMP CONTROL WERE VERIFIED. THE RT AUXILIARY PITOT WAS REPLACED AND SYSTEMS WERE TESTED IAW MM 34-11-01 AND 21-61-00 RESPECTIVELY, ALL OK. (M) 2L72 4F RTA2NM 20031222001072003122200107 2003 12 22 USAABB03210 420031110A3197 WIRE BOEING767 767201 1385125NM INSTRUMENT PANELCHAFED A USAAK NONE O OTHER APAPPROACH 1 EA19649US 23901 WHEN SPEEDBRAKES WERE ARMED, SPARKS WERE NOTED IN THE PEDESTAL. MAINTENANCE REPAIRED CHAFED WIRING TO THE INSTRUMENT LIGHTS. (M) 2L72 4F RTA1NM 20040105000472004010500047NM 2004 1 5 DL733031022 120031116A335020121 POWER SUPPLY BOEING737 7373B7 1384580NM ROW 24ABC INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27952WP 23378 EMERGENCY PATH LIGHTS BETWEEN ROWS 18 - 24 INOP. FOUND WIRES SHORTED AT ROW 18. REPLACED LIGHT SOCKET AND HARNESS AT ROW 18. POWER SUPPLY DAMAGED DUE TO SHORT. REPLACED PWR SUPPLY AND BATTERY. EMERGENCY LIGHTS NOW CK GOOD. 2L72 4F RTA16WE 20031229001392003122900139NM 2003 12 29 SWAA032734 120031215A57536546486 WEDGE BOEING737 7373G7 1384595NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED C4 CHECK, FOUND RT WING T/E MID FLAP OUTBOARD SIDE OF THE INBOARD T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED WEDGE PANEL PER MM. 2L72 4F RTA16WE 20040120000192004012000019GL 2004 1 20 DXTA200300206 220031221A753223074337EX BLEED VALVE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LT ENGINE FAILED E DXTAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07903QS 7500162 CAE330305 DURING TAXI OUT ENGINE (FAILED L) RED CAS MESSAGE ILLUMINATED. LT ENGINE ROLL BACK FROM IDLE AND HAD UNCOMMANDED SHUTDOWN. REMOVED & REPLACED ENGINE BLEED VALVE IAW ALLISON/ROLLS-ROYCE MM CHAPTER 75-31-15, GROUND RUNS & OPS CHECKS GOOD. 2L72 4J4 FRTT00007WITE6CH 20031125001422003112500142NM 2003 11 25 ASAA0310502 120030602A5347BAC1520841 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 540-706, LEFT BUTTOCK LINE 25 CORRODED. REMOVED DAMAGED SECTION OF SEAT TRACK AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031202001522003120200152NE 2003 12 2 MEX2003500 220031021A7230 BLADE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE COMPRESSOR DAMAGED A ASMFK NONE O OTHER ININSP/MAINT 1 SW21169PL 53175 DURING TRANSIT CHECK, DETECTED DAMAGE ON LEFT ENGINE C1 FAN BLADE AND A .40625 INCH PER .0625 INCH DAMAGE IN THE NOISE SUPPRESSOR. BLADE WAS BLENDED IAW MM 72-00-00. DURING OVERNIGHT SERVICE, BLADE BLENDING WAS INSPECTED IAW MM 78-33-21, FOUND ALL CORRECT AND BOROSCOPIC INSPECTION WAS PERFORMED TO C-6 AND C-7 IAW MM 72-00-0, NO DAMAGES WERE FOUND. (M) 2L72 4F4 FRTA6WE E9NE 20031203000842003120300084NE 2003 12 3 HALA0300969 220031101A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RIGHT SHUTDOWN A HALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13478HA 55123 13247 RT ENGINE INFLIGHT SHUTDOWN. CREW REPORTED SHUTDOWN RT ENGINE IN FLIGHT, DECLARED AN EMERGENCY AND LANDED SAFELY AT HONOLULU. (M) 2L72 4F4 FTRA6WE E00061EN 20031204000992003120400099WP 2003 12 4 UPS03841410 120030911A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 RIGHT CRACKED BETWEEN FS 1768-1776. REMOVED L-17RT TO FOM, FABBED NEW -35 SPLICE DOUBLER IAW DAC DWG 56493 27, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20040121000082004012100008NM 2004 1 21 SPAA0300067 120031223A335010617844 BATTERY PACK BOEING737 7372Y5 1384554NM EMERGENCY LIGHT INTERMITTENT A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28712S 23038 ON PREFLIGHT CHECK, NOTED MID CABIN CEILING EMERGENCY LIGHT SIGN FLICKERING. REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD. 2L72 4U RTA16WE 20031211000952003121100095NM 2003 12 11 03FDEA01792 120031021A2750 FLAP BOEING727 727200 138407ENM WING OUT OF RIG A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25479FE 21461 UPON TAKEOFF WHILE RETRACTING THE FLAPS FROM 5 DEGREES TO 2, BOTH FLAP INDICATIONS STUCK BETWEEN 5 AND 2 AND INTRANSIT LIGHT SHOWED AMBER, THE S/O'S VERIFICATION PANEL SHOWED ALL LED'S DOWN. AFTER APPROX 5 MIN THE LED'S RANDOMLY SEQUENCED TO 2, 3, 6, 7 AND INTRANSIT LIGHT CHANGED TO GREEN, THE FLAP GAUGE NEVER MOVED FROM THE STUCK POSITION BETWEEN 2 DEGREES AND 5. REFERENCED THE QRH. THE FLAP HANDLE WAS DIFFICULT TO MOVE DURING BOTH RETRACTION AND EXTENSION. THE FLAPS EXTENDED NORMALLY TO 5 DEGREES AND THEN ALL THE WAY TO FLAPS 30 ON THE RETURN. RIGGED FLAPS PER MM 27-51-00-2. SPOILER RIG ACCOMPLISHED IAW MM 27-61-005-2. AILERON RIG CHECK ACCOMPLISHED IAW MM 27-10-000-5 AND WO 24672. 2L73 4F RTA3WE 20030915000562003091500056NE 2003 9 15 HEEA089003 120030331A6230 BEARING SKRSKYS76 S76A 8143006NE ROTATING SCISSORWORN B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S A19200428 760035 WORN BEARINGS. REPLACED 4 EACH BEARING SB5200-103 DUE TO WORN. REPAIRED. 1G72 3U H1NE 20030916001072003091600107EU 2003 9 16 AALA20020557 120030429A3234224TS05Y MODULE AIRBUS300 A300B4605R 3930308EU MLG HANDLE INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2170079 619 MIA - FLT 404 - EN ROUTE MIA-MCO - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIR INTERRUPTED AND LANDED MIA WITHOUT INCIDENT. REPLACED HANDLE MODULE CONTROL UNIT. ACCOMPLISHED ALL REQUIRED CHECKS PER MM AND TESTER SIM9066. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030922000862003092200086NM 2003 9 22 KQ72003F00000 120030713A5711 SPAR BOEING727 72723 1384004NM WING CORRODED B KQ7RO OTHER O OTHER NRNOT REPORTED 1 SW17727WF 20045 DURING C1 AND C2 CHECK, CPCP GENERAL VISUAL INSP OF WING REAR SPAR FOR CORROSION, DISCOVERED SEVERAL AREAS OF CORROSION AND CRACKING. PERFORMED A NDT INSP HFEC AND CONFIRMED DAMAGE FOUND BY VISUAL INSP. REMOVED WING FUEL PANELS, INSPECTED INTERIOR OF FUEL CELL AREA, NO VISUAL DEFECTS NOTED. UPON REMOVAL OF SPAR CHORD DISCOVERED CORROSION BETWEEN WING UPPER SKIN PANELS AND UPPER REAR SPAR CHORD. REMOVE AND REPLACE ENTIRE UPPER SPAR CHORD, INCLUDING OB SECT OF WINGLET MOD AND INSTALL. FOUND SEVERAL AREAS OF EXFOLIATED CORROSION BETWEEN UPPER WING SKIN AND SPAR CHORD. THESE AREAS WERE UNDETECTABLE DURING VISUAL PERFORMED OF A SUSPECTED AREA FOR CORROSION AND CRACKING. UPPER REAR SPAR CHORD WAS REPLACED. 2L73 4F A3WE 20030924000432003092400043NM 2003 9 24 DL76S030756 120030813A5753113T122634 SUPPORT BEAM BOEING767 767332 1382001NM TE FLAPS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27122DL 23436 CORROSION WAS FOUND IN THE HOLE BORES OF 4 ATTACH FASTENERS ON THE 9-10 BEAM ASSEMBLY FOR THE OUTBOARD SUPPORT OF THE INBD FLAP ATTACH ASSEMBLY. THE HOLES WERE OVERSIZED TO REMOVE CORROSION, HFEC INSPECTED, AND REPAIR BUSHINGS INSTALLED TO RESTORE THE HOLE SIZES. THE REPAIR WAS ACCOMPLISHED IAW ER/A 385566-14, REV A. 2L72 4F RTA1NM 20030924001282003092400128 2003 9 24 AALA20030750 420030701A2565 SPRING BOEING757 757223 1384957NM GIRT BAR OUT OF ADJUST A AALAK NONE O OTHER ININSP/MAINT 1 SW21695AN 26975 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWELVE GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWELVE GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040127001912004012700191WP 2004 1 27 ASAA0380790 120031119A532199365461 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DISBONDED AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040128001252004012800125SO 2004 1 28 SWIA200312717 120031228A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07209SW8211 6878 120269 FLAP DISAGREEMENT AFTER TAKEOFF AND ON THE GROUND ON TAXI IN. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS AND LEAK CHECKS GOOD. P/N: 343100-1001, S/N ON: 6024, S/N OFF: 0127. 2L72 4T RTA31SO 20040130002442004013000244EA 2004 1 30 SWIA200312758 120031128A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 OUTER FLANGE ON FUSELAGE FRAME AT FS 220 AND STR 23L IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ DWG 600-34013 & RII 53-401. 2L72 4F RTA21EA 20040203000642004020300064WP 2004 2 3 ASAA0380633 120031011A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 PDX PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040204000902004020400090GL 2004 2 4 109102103MT 220031021A73231090631531 LEVER AGUSTAA109 A109 0260109EU ALLSN 250C 250C20B 03013GL P/T GOVERNOR WORN B JBZRK NONE O OTHER ININSP/MAINT 1 WP2721RX 150 7131 DURING ROUTINE MAINTENANCE THE LEVER WAS DETERMINED TO BE WORN BEYOND LIMITS. PROBABLE CAUSE WAS LOOSE HARDWARE ATTACHING LEVER TO CONTROL LINKAGE. REF AGUSTA M.M. 76-20-00 PG 209 D 1 REQUIRES NUT TO BE "FINGER-TIGHT",TIGHTEN TO NEXT COTTER PIN SLOT AND INSTALL COTTER PIN. 1G72 3U3 U H7EU E4CE 20040204001862004020400186EU 2004 2 4 203121 120031105A2612 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE ENGINE TAILPIPESILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17152CQ 152 ON TAKEOFF AIRCREW RECEIVED TAILPIPE HOT LIGHTS FOR BOTH ENGINES. PILOT FOLLOWED QRH AND RETURNED TO PIT. 2L72 4T4 TRTA52EU E8NE 20031215001092003121500109WP 2003 12 15 AALA20030962 120030904A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21219AA 49171 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT ROWS 7 THROUGH 12. REPLACED BATTERY PACK B5-101. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040323000202004032300020EU 2004 3 23 BAQA092571 120031229A670010545372 ROD END BOLKMS117 BK117A1 5626010EU FLT CONTROLS WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1360 7243 MECHANIC SCRAPPED ROD END AT SITE. UNIT REMOVED DUE TO EXCESSIVE PLAY. REPLACED WITH SERVICABLE UNIT. 02/09/2004 1G72 3U H13EU 20030814001522003081400152NM 2003 8 14 AALA20030411 120030404A3350 BULB BOEING757 757223 1384957NM EMERGENCY LIGHT CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21695AN 26975 DFW - DURING OVERNIGHT MAINTENANCE, AFT CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BULB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030815000352003081500035 2003 8 15 HEEA088513 420030715A2350AA34300 INTERPHONE BELL 206 206L3 1182108SW COCKPIT DISTORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 INTERPHONE MODULATION DISTORTED. 1G71 3U H2SW 20030815000912003081500091 2003 8 15 HEEA088371 420030722A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S11287 760035 AFCS ACTUATOR STUCK FULL DEFLECTION LEFT NR 1. 1G72 3U H1NE 20030815000972003081500097NE 2003 8 15 KBMA088331 220030712A75329550164960 BLEED VALVE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE ENGINE STUCK B KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 BLEED VALVE FLAG SHOWING, SUSPECT BLEED VALVE WONT CLOSE. INSTALLED SERVICEABLE BLEED VALVE . 1G71 3U3 U H9EU E19EU 20030820001452003082000145NM 2003 8 20 UPS03441098 120030722A541165B9041247 FRAME BOEING747 747123 1384873NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, NR 2 PYLON REAR MOUNT BULKHEAD FOUND CRACKED AT FORWARD AND AFT FRAME WEB AT STA 221. NR 2 PYLON REAR MOUNT BULKHEAD REPAIRED PER HX RS R54-53-35045 AND UPS ENGINEERING FILE NUMBER 747-54-20039. 2L74 4F A20WE 20030820001562003082000156EA 2003 8 20 COMA0360366 120030810A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01868CA 7427 FLIGHT 5528 FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20030331000132003033100013EU 2003 3 31 136821 120030330A3246175K882 TIRE SAAB SF340 SF340A 7850100EU NLG WORN A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL1719XS 340A019 FLT 4511 DURING TAKEOFF ROLL PILOT REPORTED THAT THE NOSE WHEELS HAD SEVERE VIBRATION TAKE OFF ABORTED AIRCRAFT RETURNED TO GATE MAINTENANCE INSPECTED NOSE GEAR AND FOUND NO DEFECTS TIRES WERE FLAT SPOTTED AND REPLACED PER SF340 M/M AIRCRAFT RELEASED FOR SERVICE 2L72 4T RTA52EU 20030402000152003040200015EA 2003 4 2 03091623 120030401A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CENTER EMERGENCY LIGHT WAS INOPERATIVE.MAINTENANCE PERSONNEL REPLACED AN INVERTERIN THE EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030820002092003082000209EA 2003 8 20 ASOA03338 120030725A33503071BPE LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING SCHEDULED MAINTENANCE IN MCN, THE ENTRANCE EMEGENCY LIGHT ON THE FORWARD WALL WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACD THE INOPERATIVE EMERGENCY LIGHT LAMP. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030820000642003082000064NM 2003 8 20 03FDEA01062 120030706A5347S4929148S SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 FORWARD CABIN - R1 DOOR ENTRANCE TRACK FOUND CORRODED AT STA 430. CORROSION BLENDED CARRIED OUT FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1. 2L73 4F RTA22WE 20030821001772003082100177NM 2003 8 21 03FDEA01308 120030807A5753 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 SNRM N0568 3A L2 LT WING - I2 FB FLAP 2 FB HINGE FITTING 28 FLAP SIDE 29 ACTUATOR ATTACHMENT I2 FB 26 2 FB BOLT HOLE FOUND CORROSION. LT WING - I/B FLAP ( FLAP SIDE ) O/B HINGE ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES REPAIRED AS PER CMM 57-52-03. 2L73 4F RTA22WE 20030416002692003041600269SO 2003 4 16 C2XA03SH099 120030408A531014521699003 BUTT STRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 DURING C-CHECK, THE LT BUTT STRAP WAS FOUND TO HAVE CORROSION BY FRAME 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030417000052003041700005SO 2003 4 17 LR7A03001 120030117A5512 SKIN LKHEED382 382G 526414USO HORIZONTAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 472 4606 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB0503 FOUND RT HORIZONTAL STAB L/E IMPACT DAMAGE WITH DENT AND 1.5 INCH CRACK AT RT HSS 275, FS 1052, WL 276. REPAIRED OUTER SKIN IAW SRM SMP 583 51-140-14 AND INNER SKIN IAW 51-140-14. NR 0008 AND 0071. 2H74 4T A1SO 20030417000142003041700014NE 2003 4 17 P5CA0300726 220030121A7200 ENGINE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 2 FAILED A P5CAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 WP23920FT 22237 702203 AT TOP OF CLIMB 37.0, NR 2 ENG FAILED WITH NO APPARENT CAUSE. TRIED RAPID RELIGHT, NO START. CHECKED ENG INTAKE AND EXHAUST AREA, OK. PERFORMED ENG OIL FILTER AND ALL MAGNETIC PLUGS, OK PER MM 72-00-00. ALSO HI-PWR CHECKS OK BY CREW IAW GMM 6-18-3. PERFORMED FUEL PUMP PRESS, 700 PSI, WITHIN LIMITS. 2L74 4F4 F A20WE E3NE 20030417001312003041700131NM 2003 4 17 UPS03440145 120030131A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, M/D - BS 1840 BETWEEN STR 12R AND 14R ATT FRAME FOUND CRACKED. BS 1840 BETWEEN STR 12R AND 14R FRAME I/B CRACKED AREA REPAIRED PER SRM 53-10-04 FIGURE 87. 2L74 4F RTA20WE 20030424000502003042400050NM 2003 4 24 QXEA0300325 120030227A5350 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261LT, AFT FLANGE BETWEEN CAMLOC HOLES 1-5. BLENDED DAMAGED AREA. 2H72 4T RTA13NM 20030425000062003042500006WP 2003 4 25 UPS03840385 120030314A5530 FITTING DOUG DC8 DC873F 302199FWP JACKSCREW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, LEFT SIDE VERTICAL ATTACH STRAP FOR JACKSCREW TRIM MOTOR SUPPORT BASE CRACKED AT FASTENER HOLE. REMOVED SUPPORT FITTING IAW DC8 SRM 51-1-21 & 51-3-0. LOCATED AND DRILLED UP SUPPORT FITTING 2649617 IAW DC8 SRM 51-1-21 & 51-3-0. INSTALLED SUPPORT FITTING IAW DC8 SRM 51-1-21 & 51-3-0. 2L74 4F RT4A25 20030424001962003042400196EA 2003 4 24 SWIA200311847 120030323A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG FALSE INDICATIONA SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07941SW 7750 LEFT MAIN LANDING GEAR DID NOT EXTEND INITIALLY ON APPROACH TO TUS. RECEIVED ASSOCIATED GEAR DISAGREE MESSAGE. AFTER 15 SECOND DELAY THE LANDING GEAR EXTENDED AND ALL THREE GEAR LIGHTS INDICATED GREEN. JACKED AIRCRAFT AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST AS PER CRJ MM 32-30-00. CYCLED GEAR 7 TIMES, NO DEFECTS NOTED. 2L72 4F RTA21EA 20030428001652003042800165WP 2003 4 28 03FDEA00417 120030409A5420 BRACKET DOUG DC10 DC1030 3023501WP NR 1 PYLON BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR 1 PYLON NUT PLATE BRACKET BROKEN FOR 473FL LT SIDE. CLOSING ACTION ON 04/09/03 REMOVED BRACKET IAW SRM 51-35-01. RECEIVED NEW BRACKET FROM FAB SHOP ON TRAVLER T2/324972, DRILLED AND LOCATED PER SRM 51-31-01. TREATED AND PRIMED PER SRM 51-21-01, INSTALLED PER SRM 51-35-01. 2L73 4F A22WE 20030429001212003042900121NE 2003 4 29 RAIA00304106 220030407A732031055016 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03557HK5423 41074 75126 RIGHT ENGINE INTEGRATED ELECTRONIC CONTROL FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED INLET TEMP SENSOR, OPS CHECK OK. 2L72 4T4 TRTA41NM E18NE 20030428001902003042800190SO 2003 4 28 RAIA00303095 120030331A3350 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03803HK 145077 FLOOR PATH LIGHT INTERMITTENT. MAINTENANCE SECURED CONNECTOR AT FLOOR PATH LIGHT STRIP, OPS CHECK OK. 2L72 4F RTT00011AT 20030501001742003050100174NM 2003 5 1 ASAA0310082 120030304A5310656717218 HINGE FITTING BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND RT MLG STRUT DOOR HINGE FITTING AT BS 685, WING STATION 114R CORRODED. REMOVED AND REPLACED FITTING PER SRM. (M) 2L72 4F RTA16WE 20030502000832003050200083NE 2003 5 2 AWXA200300370 220030414A7200 ENGINE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28645AW 238 DURING TOGA POWER APPLICATION NR 2 ENGINE SPOOLED UP SLOWER THAN NR 1 ENGINE CAUSING AN ISSUE ON WET RUNWAY, REJECTED TAKEOFF APPROX 15 KTS. INITIAL SPOOL DIFFERENCE WAS ATTRIBUTED TO ENGINES NOT BEING EXACTLY MATCHED AT 1.05 EPR. ON 2ND ATTEMPT ENGINES MATCHED AT 1.05 FOR POWER APPROX 1 SECOND, POWER WAS NORMALLY ADVANCED BUT NR 2 ENGINE SEEMED TO HANG AT 1.05 EPR. POWER ADVANCE WAS HALTED AT ABOUT 1.3, NR 2 ENGINE CAUGHT UP IN ABOUT 2 SECONDS, ADVANCE CONTINUED TO TOGA, NORMAL OPERATION FROM THERE. MX COMPLIED WITH FUP FROM POWER PLANT ENGINEERING AND REMOVED 1 EACH PLUG FROM ACTIVE CLEARANCE CONTROL VALVE IAW T/C R5M71306. PERFORMED HIGH POWER ASSURANCE TEST IAW T/C F5M71302, BOTH ENGINE EPR'S MATCH. 2L72 4F4 FRTA28NM E311NE 20030502001722003050200172WP 2003 5 2 03FDEA00566 120030421A5320ANB7245 BRACKET DOUG DC10 DC1030 3023501WP WING TO BODY WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 NR S-27 COMPLY WITH EA8-5331-68781 FUSELAGE-WING TO BODY FILLET- ATTACH BRACKET WEAR REPAIR P/N ANB7245. COMPLIED WITH EA8-5331-68781 FUSELAGE-WING TO BODY FILLET- ATTACH BRACKET WEAR REPAIR P/N ANB7245. 2L73 4F A22WE 20030508001452003050800145SO 2003 5 8 C2XA03IA043 120030502A33501683 BULB EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2719554 145587 DURING "A" CHECK THE MECHANIC NOTED THAT THE GALLEY OVERHEAD EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BULB, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030509000222003050900022EU 2003 5 9 A6WA200360011 120030411A5730 SKIN BAC 146 146200A 1500266EU WING DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 DENT MAPPING 8 DENT OUT OF LIMITS OF SRM. REPAIR REQUESTED FROM BAE SYSTEMS, REF AVMAX FAX 1538-6080002. (M) 2H74 4F A49EU 20030507001472003050700147NE 2003 5 7 ALG2003F00056 220030315A73219794099203 O-RING TMECA UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE FUEL CONTROL LEAKING E ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03526AL729 1281 34311 DURING POST FLIGHT, PILOT DISCOVERED STRONG FUEL ODOR, HE NOTIFIED MAINTENANCE FOUND THE FUEL LEAK COMING FROM THE FUEL CONTROL (T) FITTING, HE REMOVED THE (T) FITTING AND REPLACED THE ORING. THE AIRCRAFT WAS GROUND RUN AND LEAK CHECKED AND RETURNED TO SERVICE. 1G72 3U3 UNCR0001RD E34NE 20030514002372003051400237NE 2003 5 14 GTIA030261 220030417A7230606113 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE COMPRESSOR DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 48087 L/P 60611-3 NR ENG DAMAGE ON FAN BLADE. L/P 60612-1 NR 2 ENG FWD OF REAR CLAM SHELL ACOUSTIC LINER DAMAGED AT 12 OCLOCK POSITION TO 9 OCLOCK POSITION. L/P 60612-3 NR 2 ENG FOUND ACOUSTIC LINER DAMAGE JUST AFT OF IGV, FWD OF C1, 12 OCLOCK POSITION. C/A: L/P 60611-3 REPAIRED FAN BLADE. REPAIRS TEST 1 FOR FINAL RETURN SERVICE. L/P 60612-1 (TRANSFERRED TO NEW SDR FORM GTIA03-0313 ON CARRYOVER) L/P 60612-3 REPAIRED NR 2 ENG ACOUSTIC LINER JUST AFT OF IGV, FWD OF C1 12 OCLOCK POSITION. 2L72 4F4 F A6WE E2EA 20030527000882003052700088WP 2003 5 27 AALA20030380 120030328A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21274AA 49271 DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030605000292003060500029EU 2003 6 5 SIMA200313204 120030507A3234D49412001 CONTROL HANDLE SAAB SF340 340B 7860101EU MLG INOPERATIVE A SIMAO OTHER O OTHER APAPPROACH 1 SW21373AE 340B373 TYR - FLT 3583 - ON APPROACH, LANDING GEAR WOULD NOT COME DOWN ON FIRST TWO ATTEMPTS. ON THIRD ATTEMPT GEAR EXTENDED. CREW HAD 3 GREEN AND CONTINUED TO LAND SAFELY AT TYR. POST FLIGHT REVEALED NO VISUAL ABNORMALITIES TO CREW. MEL WAS ISSUED AND AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030606000222003060600022WP 2003 6 6 03FDEA00745 120030517A5280 SKIN DOUG DC10 DC1010 3022110WP ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 N 1059 SMALL WINGLET FAIRING AT TOP OF LT MLG STRUT DOOR IS CRACKED AND MISSING A PIECE. CHAFFED IN SEVERAL AREAS. CLOSING ACTION ON 05/13/03. REMOVED SKIN AND BACK PLATE IAW SRM 51-31-01. FAB NEW SKIN FROM 7075-T6.065, BATCH 0000509285 BACK PLATE FROM 2024-T3 .063 BATCH 0000545293. INSTALLED NEW SKIN AND BACK PLATE IAW SRM 51-31-01. 2L73 4F A22WE 20030605001232003060500123NM 2003 6 5 MEX2003123 120030406A3610 CLAMP DOUG MD80 MD83 3023681NM PNEUMATIC SYS LOOSE W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23XAMRM 53066 DURING TRANSIT, HIGH TEMPERATURE LIGHT OF TAIL COMPARTMENT COME ON WITH LEFT AIR CONDITIONING SYSTEM ON. LEFT AIR CONDITIONING SYSTEM WAS DEFERRED IAW MEL, CATEGORY C. AT BJX, PNEUMATIC LEAK WAS FOUND DUE TO LOSE CLAMP. CLAMP WAS REPOSITIONED AND TORQUED IAW MM, TESTS CORRECT. 2L72 4F RT 20030609000312003060900031WP 2003 6 9 03FDEA00789 120030521A5753 FLAP TRACK DOUG DC10 DC1010 3022110WP TE FLAPS WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 LT INBD FLAP TRACK UPPER ROLLER SURFACE WORN ALONG WITH SIDE ROLLER SURFACE. FOUND LT I/B FLAP TRACK UPPER ROLLER SURFACE ALONG WITH SIDE ROLLER SURFACE TO BE OUT OF LIMITS IAW DC-10 CMM 57-52-01 REMOVED AND REPLACED TRACK IAW M/M 51-32-01. 2L73 4F A22WE 20030609001732003060900173NE 2003 6 9 CA030430009 220030425A7421311614401 PLUG PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL IGNITOR STUCK W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) THREADS BADLY DAMAGED ON PLUG AS REMOVAL WAS DIFFICULT DURING SCHEDULED HOT SECTION INSP. PWC S/B 14336, REPLACEMENT OF PLUG , PERFORMED. NEW PLUG HAS AN ANTI-SEIZE COATING. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20030611000242003061100024NM 2003 6 11 EVAS092013 120030515A5754 DOUBLER DOUG MD11 MD11F 3023600NM LT WING LE CRACKED W QOCFK NONE O OTHER ININSP/MAINT 1 WP0316111 48787 DURING PERFORM E/O V02102, FOUND CRACK ON RIGHT AND LEFT WING FIXED LEADING EDGE STRINGER DOUBLER AT STATION XOS 906. INSTALLATION OF INTERNAL DOUBLERS MADE FROM TI-6AI-4V 0032 (THICK AT STATION XOS 906). 2L73 4F RTA22WE 20030610000222003061000022NM 2003 6 10 2003UALA00444 120030521A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 EEL LIGHTING IN FIRST CLASS CABIN INOPERATIVE 2L72 4F4 FRTA16WE E2GL 20030612000222003061200022NM 2003 6 12 P5CA0300883 120030528A5412 BULKHEAD BOEING747 7472U3B 1384846NM PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 CRACKS FOUND ON AFT TORQUE BULKHEAD ON NR 1 & 4 PYLONS. REPAIRED PER SB 54-2201 BOEING PAO R11-03-00004H. 2L74 4F RTA20WE 20030610000742003061000074NM 2003 6 10 DL73G030415 120030502A30405893543130 CONTROLLER BOEING737 73735B 13844BMNM WINDSHIELD FAILED A DALAB EMER. DESCENT A FLAME/FIRE CRCRUISE 1 SO27224DA 24269 WHILE PREFORMING FCF FLIGHT - R-1 WINDSHIELD TERMINAL BLOCK AREA, UPPER RT CORNER, BEGAN TO SMOKE AND SPARK FOLLOWED BY FLAME APPEARING FOR SEVERAL SECONDS. REPLACED R-1 WINDOW ASSY, R-1 WINDOW HEAT CONTROLLER AND R-1 ANTI-ICE CIRCUIT BREAKER. 2L72 4F RTA16WE 20030613000932003061300093NM 2003 6 13 UPS03440804 120030516A532065B0421740 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - STA 560 STR 23R ATTACH TIE CLIP FOUND CORROSION REVEALED. M/D BS 560 S-23R ATT TIE CLIP REPLACED AS PER SRM 51-10-01 DUE TO CORROSION BLENDED AREA .5 X 1 X 0.030 INCH MATL REMAINS, EXCEED SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F RTA20WE 20030617000992003061700099NM 2003 6 17 QXEA200300680 120030608A7110 COWLING BOMBDRDHC8 DHC8401 1390041NM NR 1 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - NR 1 LOWER COWL OIL COOLER APERTURE FORWARD RIGHT HAND SIDE HAS A 1 INCH LONG CHAFE. REPAIRED IAW HORIZON AIR EA 6-71-92. 2H72 4T RTA13NM 20030521002002003052100200NM 2003 5 21 SWAA031063 120030511A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 8 & 15 INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROW 8 & ROW 15. REPAIRED WIRE AT D1072 CONNECTOR PER MM. 2L72 4F RTA16WE 20030523000332003052300033NM 2003 5 23 DL738030390 120030426A3350767 BULB BOEING737 737832 13844CFNM RT OVERWING BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27388DA 30375 RIGHT OVERWING AFT EMERGENCY LIGHT INOP. RELAMPED SAME, OPS CHECK GOOD. 2L72 4F RTA16WE 20030617002742003061700274SW 2003 6 17 HEEA087031 120030604A6710406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 MAIN ROTOR DRIVE UNIVERSAL WORN. 1G71 3U O H2SW 20030523000532003052300053 2003 5 23 SWAA031114 420030518A25654A3902 GIRT BAR BOEING737 7377H4 1384404NM SERVICE DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR WILL NOT STOW PROPERLY. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030623001052003062300105NM 2003 6 23 USAASB03068 120030520A3397 CONNECTOR BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US 22954 PIT - MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTOR. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030624000202003062400020NM 2003 6 24 VNAA0306002 120030603A3243S4340200001 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE BRAKE FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07425JS3276 3037 EN ROUTE, THE CREW RECEIVED A EMERGENCY PARKING BRAKE VALVE ACCUMULATOR LOW CAS MESSAGE IN FLIGHT. THE ACCUMULATOR WAS SERVICED AND THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE THEN INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031208001662003120800166NM 2003 12 8 AWXA200301328 120031001A53476545410200 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND ON FLOORBEAM AT FASTENER HOLE BS 727B, RBL 25. MAINTENANCE TRIMMED OUT CRACK ON FLOORBEAM BS 727B, RBL 25; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR STRAPS; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-03289-TB6. 2L72 4F RTA16WE 20031209000912003120900091NM 2003 12 9 SWAA032357 120031025A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E -747, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031209001902003120900190WP 2003 12 9 UPS03841491 120031026A534037558261N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 300 BETWEEN LONGERON 31L-32L HAS A CRACKED BATHTUB FITTING. REMOVED AND REPLACED FITTING IAW DWG 3755826 AND SRM 51-1-20D, 53-2-0 FIG 2D. 2L74 4F RT4A25 20031210000432003121000043NM 2003 12 10 AWXA200301499 120031113A532069434771 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MINOR REPAIR - DURING C-15 CHECK A .5625 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOOR CHANNEL AT BS 807, RBL 24. MAINTENANCE REMOVED CRACKED CHANNEL IN AFT CARGO COMPARTMENT FROM BS 807 TO BS 827, RBL 24; FABRICATED A NEW REPLACEMENT PANEL PER DWG 69-43477; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 4B, FIG 10, 5 B & C & FIG 14, 7D. 2L72 4F RTA16WE 20030919000122003091900012WP 2003 9 19 03FDEA01240 120030810A5753ARC0502 HINGE DOUG DC10 DC1030F 3023504WP RT FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 MDIS 311 57-10 0008862 01AUG03 BFM CLOSE RD COMPLY WITH E.A. 8-5750-70999 WINGS-RT OB 27D FLAP-IB HINGE-ACTUATOR ATTACH LUG FACE CORROSION REPAIR ENT BY 3A 39014C RPT BY 3A 39014C. FACT08AUG03 04 3A29 BFM R COMPLIED WITH E.A. 8-5750-70999 WINGS-RH OB FLAP IB HINGE-ACTUATOR ATTACH LUG FACE CORROSION REPAIR MAE ENT BY 3A 39014C RPT BY 3A 39014C. 2L73 4F RTA22WE 20030919000592003091900059EA 2003 9 19 COMA0360353 120030809A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA MLG INOPERATIVE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01920CA 7022 DURING FLIGHT 5813A, GEAR DISAGREE WARNING MESSAGE APPEARED IN FLIGHT. AIRCRAFT PERFORMED UNSCHEDULED LANDING AT CKB. PERFORMED A FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION SYSTEM OF THE LANDING GEAR IAW CRJ200 AMM 32-30-000-720-801. COULD NOT DUPLICATE. FUNCTIONAL TEST CHECK GOOD. 2L72 4F RTA21EA 20030918000912003091800091NM 2003 9 18 PCAA0308090 120030803A2434 GENERATOR DHAV DHC8 DHC8102 2809003NM DC SYSTEM LIGHTNING STRIKEA PCAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA13846EX 326 20 MINUTES PRIOR TO LANDING AT BDL A/C EXPERIENCED A LIGHTNING STRIKE. BOTH DC GEN WENT OFF LINE. ONE GEN WAS ABLE TO RESET. FLT CONTINUED TO BDL & LANDED WITHOUT FURTHER INCIDENCE. MAINT PERFORMED A LIGHTNING STRIKE INSPECTION IAW DEHAV DASH 8 MM, PWA MM, & HAMILTON SUNDSTRAND MM. NR 2 BLADE ON RT PROP ASSY REPLACED DUE TO DAMAGE. DUE TO NR 1 DC GEN BEING INOP MAINT REPLACED THE NR 1 D.C. GENERATOR. A PATCH ON RT ELEVATOR TRIM TAB HAD SHOWN SIGNS OF BURNING ON THE OUTBOARD TRAILING EDGE, WITH NO DAMAGE TO THE TRIM TAB. THIS FINDING WAS DEFERRED AS NOT AFFECTING THE SAFETY OF FLIGHT. OPERATIONAL AND LEAK CHECKS OF AFFECTED SYSTEMS WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030922001022003092200102EU 2003 9 22 BAQA089221 120030914A28449550171990 SENSOR UROCOPEC135 EC135T1 5620026EU FUEL PRESSURE LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME 132 FUEL PRESSURE SENSOR LEAKING OUT OF SIDE HOLE. REMOVED FROM ENGINE NR 30068. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040128001372004012800137NM 2004 1 28 QXEA200301593 120031226A3080697079003 BRUSH BLOCK BOMBDRDHC8 DHC8401 1390041NM ZONE 500 INOPERATIVE A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09409QX1933 1933 4051 SEA FLIGHT 2289 RETURN TO FIELD, PROP DEICE CAUTION LIGHT ILLUMINATED. REPLACED NR 1 PROP BRUSH BLOCK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203000662004020300066WP 2004 2 3 ASAA0380799 120031119A532199365371 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 120-160. REPLACED INSERTS IAW SRM 53-05. (M) 2L72 4F RTA6WE 20040205000342004020500034NM 2004 2 5 EIA2003153 120031019A5312 BULKHEAD BOEING747 747132 1384882NM LT WING WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 LT WING WW BAY 1241 CANTED PRESSURE BULKHEAD WEB CORRODED FROM LBL 50-97 LBL. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 479-53-176. 2L74 4F A20WE 20040217001792004021700179EU 2004 2 17 PG92004F00007 120031109A6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU TAIL ROTOR CRACKED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP196093R1437 2415 TAIL ROTOR BLADE SPAR CRACKED. (RMA NR R045704) (K) 1G71 3U H9EU 20031212000732003121200073NM 2003 12 12 03FDEA01896 120031022A5320ADA8424517 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 FWD CARGO COMPARTMENT - TRANSVERSE LONGITUDINAL SPLICE 46L AT STA 1119 HAS 1 EACH CRACK APPROXIMATELY 1 INCH IN LENGTH. CRACKED SPLICE AT FORWARD CARGO COMPARTMENT STA 1119, LONGERON 46L REMOVED AS PER SRM 51-33-01, VOL II AND REPLACED WITH NEW FABRICATED SPLICE AS PER DRAWING ADA 8424 AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20031215000592003121500059NM 2003 12 15 0302076310 120031115A2597 WIRE BOEING747 747451 1384940NM GALLEY BROKEN A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL01670US 24225 DURING FLIGHT, AN ELECTRICAL BURNING SMELL EMITTED FROM THE COFFEEMAKERS IN GALLEY 3B. PULLED CIRCUIT BREAKERS AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPAIRED WIRE AND REPLACED TERMINAL FOR HOTPLATE IN GALLEY 3C POSITIONS 3-47. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040525000362004052500036EU 2004 5 25 2004F00126 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 39R IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 39R. (M) 2L72 4F RTA28NM 20031217000582003121700058WP 2003 12 17 DHL2003805579 120030825A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING CORRODED, AROUND STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) AND A FILLER (7075-T6 AL0.050). CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERNAL SURFACE AND THE FILLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR DOUBLER AND A FILLER ON RIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING (AROUND STA.XW.485.000) USING NEW FASTENERS. SEE N/R 0119 FOR RIGHT INBD L/E REMOVAL AND REINSTALLATION. 2L74 4F RT4A25 20030624000852003062400085NM 2003 6 24 DL757030456 120030510A5330146N34101 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27609DL 22816 DENT CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND WITH MULTIPLE DENT LOCATIONS BETWEEN FS 1570 & 1615 AND BETWEEN STRINGERS 18L & 22L. THE DENTS WERE REMOVED WITH CUTOUTS TO THE SKIN AND REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384846-14, REV A. 2L72 4F RTA2NM 20030624000962003062400096NM 2003 6 24 DL757030470 120030518A2560 BATTERY BOEING757 757232 1384965NM MEGAPHONE DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27609DL 22816 MEGAPHONE L1 CLOSET INOPERATIVE. REPLACED BATTERIES 2L72 4F RTA2NM 20030707000752003070700075NE 2003 7 7 2003UALA00263 220030311A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 BIRD INGESTION A UALAEA ENGINE SHUTDOWN UNSCHED LANDING TCJENGINE CASE PENETRATION F.O.D. WARNING INDICATION CLCLIMB 1 WP29544UA 25322 726726 A/C EXPERIENCED BIRD STRIKE IN THE NR 2 (RIGHT) ENGINE. UPDATE ROOT CAUSE DETERMINED TO BE AN 8-12 LB. CANADAN GOOSE. EWR DOES HAVE A WILDLIFE MITIGATION PROGRAM; HOWEVER, DISCUSSIONS ARE CONTINUING TO IMPROVE THEIR PROGRAM. 2L72 4F4 FRTA2NM E17NE 20030708000942003070800094WP 2003 7 8 UPS03840930 120030616A5313 LONGERON DOUG DC8 DC873F 302199FWP PWA JT3D JT3D3 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C LONGERON 17L AND FWD END FITTING CRACKED AT BS 1768 REMOVED LONGERON 17L AND END FITTING. LOCATED, DRILLED LONGERON AND END FITTING IAW SRM 51-1-24. REMOVED AND REINSTALLED HYDRAULIC CASE AND LINES AT STA 1768 IAW MM 20-12-00. INSTALLED LONGERON END FITTING IAW SRM 51-1-21, 51-1-20D. 2L74 4F4 FRT4A25 1E8 20030630000842003063000084SW 2003 6 30 HEEA087846 120030621A6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 UNABLE TO TRACK. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030711000222003071100022SO 2003 7 11 C2XA03SH199 120030622A575314568000414 SKIN EMB 145 EMB145LR 3260212SO TE FLAP DELAMINATED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK THE RIGHT INBOARD FLAP WAS FOUND TO HAVE DELAMINATION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 IC 20003-14512058. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030716000032003071600003NM 2003 7 16 2003F00405 120030314A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND DENT ON FORWARD CARGO FRAME AT BS 720A, STRINGER 24L. FABRICATED REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRAME STATION 720A STRINGER 24L. (M) 2L73 4F A3WE 20030717000472003071700047SW 2003 7 17 HEEA088023 120030626A5630407706301106 WINDOW BELL 407 407 1182206SW PAX DOOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 PAX DOOR HAS A HOLE IN WINDOW. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030114000892003011400089NM 2003 1 14 CALA0300008 120030112A5320 WEB BOEING737 7373T0 1384582NM STA 500D-520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917321 23372 INSPECTION FOUND A 1" CRACK IN CENTER FLOOR WEB AT STA 500D-520. A REPAIR WAS INSTALLED IAW SRM 51-40-00. 2L72 4F RTA16WE 20030127002122003012700212SW 2003 1 27 HEEA083702 120030115A7160 LATCH BELL 407 407 1182206SW COWL DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 CRACKED AT LATCH AND CORROSION. 1G71 3U O H2SW 20030128000882003012800088SW 2003 1 28 HEEA083838 120030116A6230406010428109 BUSHING BELL 407 407 1182206SW M/R HEAD SET WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 3696 53323 MAIN ROTOR HEAD BUSHING SET WORN. 1G71 3U O H2SW 20030130000312003013000031NM 2003 1 30 0300136718 120030127A5311 WEB BOEING747 747251F 1384898NM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 During "L" check found crack in nose wheel wheel top panel frame web at BS 284 LBL 10. Repaired per EA 67-165037. 2L74 4F A20WE 20030203001672003020300167NE 2003 2 3 EGR2003F00000 120030103A55007620924004045 FITTING SKRSKYS76 S76B 8143007NE PWA PT6 PT6* 52043EA STABILIZER CRACKED B EGRRK NONE O OTHER ININSP/MAINT 1 EA17181RX 760410 FOUND SUPPORT FITTING CRACKED AT RT UPPER STABILIZER ATTACH POINT FLANGE. REPLACED SUPPORT FITTING WITH NEW PART. 1G72 4U3 T H1NE E2NE 20030328000842003032800084EA 2003 3 28 COMA0360066 120030130A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA INTERCOSTAL CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01989CA 7215 LT FS 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 IS CRACKED. REPAIRED LT FS 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 I/A/W WVAC E.O. 601R-53-3826. 2L72 4F RTA21EA 20030204000172003020400017EA 2003 2 4 OG52003F00000 120030106A65101885 FITTING SCWZER269 269D 8059501EA LYC O360 HIO360* 41514EA D/SHAFT ZERT INCORRECT A OG5RO OTHER O OTHER TXTAXI/GRND HDL 1 GL212086F S1999 S1754 AFTER ENGAGEMENT OF ROTOR SYSTEM, TAIL ROTOR DID NOT MOVE. INVESTIGATION FOUND BALL MISSING OUT OF ZERT, ALLOWING GREASE TO ESCAPE ALLOWING BUMPER TO WEAR ALLOWING SHAFT TO DECOUPLE. 1G71 3U3 O0 4H12 1E10 20030206001492003020600149NM 2003 2 6 03FDEA00035 120030115A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 MECHANICAL DAMAGE ON FLOORBEAM BS 990, RBL 37.5, WL 207. REPAIRED FLOORBEAM BS 990 RBL 37.5 WL 207 IAW SRM 53-10-8. 2L73 4F4 FRTA3WE E2EA 20030206001592003020600159EA 2003 2 6 A6WA200340019 120030121A2421 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 LACK OF LUBE A A6WAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 GL31409AW 7447 IDG NR 2 CAS MESSAGE DURING TAKEOFF POWER APPLICATION SERVICED NR 2 IDG WITH OIL. NO LEAKS NOTED. (M) 2L72 4F RTA21EA 20030208000072003020800007SO 2003 2 8 RAIA00301026 120030127A2913PV303211 PUMP EMB 145 EMB145 3260210SO MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03809HK7849 894 145187 5272-ECM- RIGHT HAND HYDRAULIC PUMP PRESSURE FOLLOWS THROTTLE MOVEMENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP, OPS AND LK CH OK. 2L72 4F RTT00011AT 20030218002162003021800216NM 2003 2 18 SWAA030309 120030209A57536546436237 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING WALK ROUND INSPECTION, FOUND LT OTBD T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT OTBD T/E FLAP PER MM. 2L72 4F RTA16WE 20030219000182003021900018 2003 2 19 VJ32003F00022 420030124A3120115EG7780 CLOCK GROB 120 G120A 1660208EU LYC O540 AEIO540D4D5 EA COCKPIT BROKEN B VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP07867AF 85007 RL2451848A LT HAND STOP PIN BROKEN OFF FROM NORMAL USE. 1L71 3O3 ORTA49CE 1E4 20030116000472003011600047 2003 1 16 HEEA083006 420030106A2562ELT910 ELT BELL 206 206L3 1182108SW CABIN INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 ELT INOPERATIVE. 1G71 3U H2SW 20030116000832003011600083 2003 1 16 HEEA083043 420030106A2312064101900 TRANSCEIVER BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 PRESET WOULD NOT CHANGE. CLEANED FREQUENCY SELECTOR WAFERS AND SW102 SWITCH. REPLACED BROKEN KHZ SWITCH HOUSING. REPAIRED PROBLEM. REPLACED BROKEN HINGE ON RECEIVER BOARD. REGLUED DISPLAY LENS AND APPLIED DOW CORNING NR 4 COMPOUND TO DS501 DISPLAY. REPAIRED STRIPPED SCREW HOLE IN CHASSIS FOR FACEPLATE. BENCH CHECK GOOD. 1G71 3U H2SW 20030116002452003011600245WP 2003 1 16 ZW0A0300302A 120030106A3350408822101 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13960TW 49231 AN EMERGENCY CEILING LIGHT AT ROW 11, ROW 27 TO AFT CABIN CEILING LIGHTS, AND BOTH AFT OVERWING EMERGENCY EXIT SIGNS WERE ALL INOPERATIVE. REPLACED THE LAMP AT ROW 11, AND REPLACED THE BATTERY PACK FOR THE AFT CABIN CEILING LIGHTS, AND FOR THE AFT OVERWING EXIT SIGNS. 2L72 4F A6WE 20030116002592003011600259NM 2003 1 16 ABXA030018 120030106A5310140T2102331 SHEAR TIE BOEING767 767281 1385109NM FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 FORWARD CARGO LOWER LOBE STA 742, CORRODED SHEAR TIE, BETWEEN STRINGER 39 LEFT - 39 RIGHT. CORRODED SHEAR TIE REMOVED, NEW SHEAR TIE INSTALLED IAW SRM. 2L72 4F RTA1NM 20030220001322003022000132NM 2003 2 20 F3LA200300025 120030122A5320 SUPPORT BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 25039 DURING C-4 CHECK, INSPECTION REPORTED I-BEAM, LT SIDE INBD OF L-2 DOOR TOP SIDE, CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS. FABRICATED REPLACEMENT SHIM PER EA 53-737-193. INSTALLED SHIM ON SUPPORT PER EA 53-737-193. INSTALLED SUPPORT PER SRM 51-40-02. 2L72 4F RTA16WE 20030224001062003022400106SW 2003 2 24 HEEA084221 120030120A5320407070620140 HEADLINER BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 HEADLINER CRACKED. 1G71 3U O H2SW 20030224001462003022400146NM 2003 2 24 AWXA200300197 120030216A5320146N5416 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON NUT PLATES OF FLOOR SUPPORT BS 1330, LBL 7. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED AREA ON FLOOR SUPPORT BS 1330, LBL 7; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-2, & 4-6. 2L72 4F RTA2NM 20030227001122003022700112SW 2003 2 27 HEEA084418 120030212A2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035980691 28140 MAIN BATTERY DISCHARGED, WON'T START AIRCRAFT. 2G72 4U H10SW 20030228000412003022800041NM 2003 2 28 CALA0300070 120030226A5210 SKIN BOEING737 7373T0 1384582NM L-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND A 1/2" CRACK IN L-2 DOOR AT WEB OPENING ON INTERIOR SKIN ABOVE INSTALLED TORQUE TUBE. INSTALLED REPAIR IAW ECRA 5210-01653. 2L72 4F RTA16WE 20030305000192003030500019NM 2003 3 5 C1HA200381002 120030112A3260 SWITCH BOEING727 7272S7 138407ZNM MLG INDICATOR DIRTY A C1HAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15681CA 22020 NOSE GEAR DOOR ANNUNCIATOR REMAINED ILLUMINATED AFTER LANDING. CLEANED AND LUBED NOSE GEAR DOOR SWITCHES, OPS NORMAL. 2L73 4F A3WE 20030307000712003030700071NM 2003 3 7 SWAA030485 120030304A53306546525 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 360, STRINGER 14L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030310000012003031000001SO 2003 3 10 C2XA03SH044 120030310A530014533822016 STRINGER EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK STRINGER 21 RIGHT WAS FOUND TO HAVE CORROSION BETWEEN SPLICES AT FRAMES 52 TO 53 AND FRAMES 60 TO 61. MAINTENANCE REMOVED AND REPLACED AFFECTED STRINGER IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030310000792003031000079 2003 3 10 HEEA084983 420030227A34427007700614 INDICATOR BELL 412 412 1182202SW WX RADAR SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 WEATHER RADAR INDICATOR CAUSES VHF UNIT TO BREAK SQUELCH ON FREQ 129-77 MHZ AND CONSTANT NOISE. 1G72 4U H4SW 20030311000012003031100001NM 2003 3 11 2003UALA00241 120030303A5730 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29650UA 25287 LEFT WING #2 SLAT SKIN HAS A SHARP DING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND REPAIRED SKIN. 2L72 4F4 FRTA1NM E24NE 20030317001432003031700143NM 2003 3 17 03FDEA00307 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 520, BETWEEN STR 24L AND 25L. 2L73 4F RTA3WE 20030320000912003032000091NM 2003 3 20 2003UALA00077 120030121A5411 SPAR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29646UA 25283 RT PYLON, STA 180 JUST FORWARD OF WING FRONT SPAR, UPPER SPAR WEB IS CRACKED IN WEB RADIUS. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH DOUBLER ANGLE. 2L72 4F4 FRTA1NM E24NE 20030327000822003032700082SO 2003 3 27 C2XA02SH182 120030201A531014522460013 BUTT STRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727523 145389 DURING C-CHECK CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO HAVE CORROSION AND GOUGING. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030326001112003032600111EA 2003 3 26 A6WA200340037 120030312A3244 TIRE CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A A6WAO OTHER O OTHER LDLANDING 1 GL31417AW2844 7610 UPON LANDING, MKE, NR 3 MLG TIRE BLEW CAUSING DAMAGE TO RIGHT INBOARD FLAP REPLACED RIGHT INBOARD FLAP IAW AMM. RIGGED FLAP IAW AMM. OPS CHECK GOOD. 2L72 4F RTA21EA 20030418001162003041800116WP 2003 4 18 UPS03840216 120030129A5320 PAN DOUG DC8 DC873F 302199FWP L2 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C3, L2 LOWER FWD DOOR JAMB CORNER CRACKED TWO PLACES. FAB NEW SEAL RETAINER IAW DAC DWG 5751115. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FAB PAN REPAIR DOUBLER IAW DAC DWG 5751040, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAL RETAINER AND DOUBLER AND DOOR PAN IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20030418001452003041800145NM 2003 4 18 QXEA0300302 120030223A33506138001 BATTERY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 INTERMITTENT A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09407QX863 4049 PDX- AFT EGRESS LIGHTS AND EMERGENCY LIGHTS IN AFT GALLEY INTERMITTANT OPERATION. REMOVED BATTERIES FROM EPS4 AND INSTALLED NEW BATTERIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030418000892003041800089WP 2003 4 18 MWEA030108 120030214A213320219742 OUTFLOW VALVE DOUG DC9 DC932 3022066WP CABIN PRESSURE INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31502ME 48132 FLOW LIGHT ILLUMINATED, FOLLOWED BY TRANSFER LOCKOUT LIGHT, STANDBY LIGHT ON PRESSURE CONTROLLER. DID QRH PROCEDURES. COULD NOT CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR AND TWO BELLY DRAINS. INSTALLED NEW SEAL FOR LEFT REVERSER BELL CRANK. 2L72 4F A6WE 20030716000832003071600083NM 2003 7 16 2003F00427 120030309A5311 FRAME BOEING727 727222 1384073NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND TIE FRAME CRACKED AT BS 480, STRINGER 17L. FABRICATED REPAIR ANGLES. TREATED AND PRIMED FABRICATED REPAIR ANGLES. INSTALLED AT STATION 480, STRINGER 17L. (M) 2L73 4F A3WE 20030422000672003042200067SO 2003 4 22 SIMA200307004 120030306A532014522178005 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR LOWER CENTER SILL FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED SILL AND INSTALLED NEW IAW EMB STATEMENT IC2003-145/0818 AND EMB SRM, EMB 145/1142 REV 20, CHAPTERS 51-40-02, 51-20-03 AND 51-40-06. (M) 2L72 4T RTT00011AT 20030422001502003042200150NM 2003 4 22 EIA2003031 120030228A5313UNK STRINGER BOEING747 747132 1384882NM PWA JT9 JT9D3 52050NE FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 STRINGER 20L AR BS 524, CORRODED AT STRINGER SPLICE AND WINDOW FORGING. REPAIRED IAW ECRA 481-53-178-2. INSTALLED STRINGER SPLICE IAW B747 SRM 51-30-02, PGS 58-59. REMOVED CORROSION IAW B747 SRM 53-10-01 FIG 1 SH 1-66. 2L74 4F4 F A20WE E20EA 20030423000852003042300085EU 2003 4 23 HE66085950 120030411A6330L633M2010103 MOUNT UROCOPEC135 EC135T1 5620026EU GEARBOX DEFECTIVE E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 FS01135CR 0164 AIRCRAFT BECAME ROUGH IN FLIGHT INSPECTED MOUNTS AND NOTICED THEY FAILED 1G72 3U H88EU 20030423001892003042300189NM 2003 4 23 VNAA0303010 120030309A5270 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR ILLUMINATED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07429JS 3043 EN ROUTE, THE CREW EXPERIENCED A DOORS LIGHT ON THE RED WARNING PANEL AND A TEMPORARY LOSS OF CABIN PRESSURIZATION. ONCE PRESSURIZATION CONTROL WAS REGAINED, IT WAS NORMAL FOR THE REST OF THE FLIGHT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL AND COULD NOT DUPLICATE ANY PROBLEM WITH THE PRESSURIZATION SYSTEM. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040225001652004022500165NM 2004 2 25 DLM88031133 120031224A2120 ODOR DOUG MD88 MD88 3023688NM COCKPIT DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27902DE 53379 ON CLIMBOUT STRONG ELECTRICAL BURNING ODOR IN COCKPIT AND FORWARD CABIN. PERFORMED OPN 5088, NO PROBLEMS FOUND. RAN ENGINES AT POWER WITH PACKS ON, WING AND ENGINE ANT-ICE ON AND OFF. NO PROBLEMS FOUND. 2L72 4F RTA6WE 20030827001802003082700180SO 2003 8 27 C2XA03CL144 120030812A335020131A BATTERY PACK EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716944 145045 BDL FLIGHT NR 2351 THE CREW REPORTED THE EMERGENCY LIGHTING DID NOT TEST AFT OF THE EMERGENCY EXIT ROW. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030722000612003072200061NM 2003 7 22 SWAA031501 120030702A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 10R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030723000502003072300050 2003 7 23 USAABB03107 420030707A3417 ADC BOEING767 7672B7 1385107NM COCKPIT FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19651US44188 24764 EN ROUTE, FIRST OFFICER'S AIRSPEED AND ALTIMETER FLAGS CAME INTO VIEW, AND THE AUTOPILOT AND AUTO THROTTLE TRIPPED OFF. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ADC. (M) 2L72 4F RTA1NM 20030724000322003072400032NM 2003 7 24 DL76S030533 120030610A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM EMERGENCY LIGHTSINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27135DL 25145 EMERGENCY LIGHTS FROM ROW 34 AND BACK BOTH SIDES INOP. FOUND SHORTED SEAT HARNESS AT SEAT 36AB REPAIRED SAME. REPLACED PWR SUPPLY D9048 DUE TO BLOWN FUSE. 2L72 4F RTA1NM 20030724001242003072400124NM 2003 7 24 DLM88030573 120030622A2612 CONNECTOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE SHORTED A DALAFEA ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27967DL36667 53116 718151 DURING FLIGHT 269 ATL OMA RIGHT ENGINE FIRE WARNING BOTH LOOPS ENGINE WAS SHUTDOWN BOTH FIRE BOTTLES DISCHARGED. A/C DIVERTED TO LIT. REPAIRED LOOPS A AND B FOR SHORTED CONNECTORS. 2L72 4F4 FRTA6WE E9NE 20030725000202003072500020EU 2003 7 25 03FDEA00826 120030529A7830491B1313033007 STRIP AIRBUS300 A300F4605R 3930327EU THURST REVERSER GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 NR 265 #2 ENG I/B T/R LOWER FRAME GOUGED. REMOVED AND REPLACED I/B T/R LOWER FRAME IAW S/B 78-1109 @ MAE UNDER WO 22920. ** S/D 2L72 4F RTA35EU 20030731001302003073100130NM 2003 7 31 QXEA200300822 120030710A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - PANEL 261HT HAS CHAFING AROUND FLANGES. MOSTLY AFT EDGE AND FORWARD RIGHT EDGE. REPAIRED IAW Q400 RD 8/4-53-521, PAGE 4, STEPS 4 THRU 7 AND RD 8/4-53-521, STEP 9. 2H72 4T RTA13NM 20030806001562003080600156NM 2003 8 6 AWXA200300829 120030721A3030C16195AA PROBE AIRBUSA319 A319132 3930340NM ZONE 120 FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28808AW757 1088 ON TAKEOFF AT PHX EN ROUTE FOR EWR RECEIVED ECAM MESSAGE FOR CAPTAINS PITOT PROBE FAILURE. DUE TO ICING CONDITIONS AT EWR TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED PITOT PROBE (9DA1), OPERATIONAL TEST WAS GOOD PER AMM 34-11-15. VENDOR CONFIRMED FAILURE OF PITOT PROBE S/N 7385, UNIT BEYOND ECONOMICAL REPAIR, SCRAPPED AT VENDOR. 2L72 4F RTA28NM 20030903000382003090300038WP 2003 9 3 ARWA20030606 120030625A32304771392501 PIN DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE MLG DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 ON WALK-AROUND FOUND LT MAIN LANDING GEAR EYEBOLT ACTUATOR WITH EXCESSIVE GAP AT PIN BOSS ATTACHMENT. REMOVED LT MAIN LANDING GEAR ROUTED TO SHOP FOR ACTUATOR PIN REPLACEMENT, REINSTALLED SERVICIABLE MAIN LANDING GEAR IAW MM 32-11-0, OPERATIONAL LEAK CHECK OK IAW MM 32-30-0 PAGE 201. 2L74 4F4 F 4A25 1E8 20030904000182003090400018WP 2003 9 4 ARWA20030704 120030709A7997 WIRE DOUG DC8 DC861 3021952WP OIL PRESS IND CHAFED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO1929UA 46159 AFTER TAKE-OFF NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED ACCOMPLISHED APPROPRIATE CHECKLISTS, AND RETURNED TO SJU. REMOVED AND CHECKED NR 1 ENGINE MAIN OIL FILTER, FOUND OK. RE-INSTALLED FILTER, FOUND TWO WIRES WERE CHAFING WITH COWLING SPLICE AND RE-ROUTED. ENGINE RUN PERFORMED, ALL CHECK NORMAL IAW MM 71-00 - 79-32-2 AND MM 20-50-1 2L74 4F 4A25 20030904000382003090400038EA 2003 9 4 SWIA200312276 120030710A5320601R3111358 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 FLOORBEAM CLIP CRACKED AT FS 280.00; RBL 9.0 OUTBOARD. DISCOVERED DURING C-CHECK, CLIP REPLACED IAW CRJ SRM 51-42-06. P/N 601R31113-58 2L72 4F RTA21EA 20030905001792003090500179WP 2003 9 5 AALA20030455 120030411A2120 SEAL DOUG DC9 DC982 3022082WP A/C BAY LEAKING A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW21295AA 49307 DFW - FLT 1938 - DFW-CLE, ON CLIMB-OUT, TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. FOLLOWED CHECKLIST AND LIGHT EXTINGUISHED WHEN LEFT PACK WAS TURNED OFF. LIGHT ILLUMINATED AGAIN WHEN POWER ADVANCED TOWARD CLIMB POWER. RETARDED POWER AND LIGHT EXTINGUISHED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT PACK HEAT EXCHANGER EXHAUST SLIP DUCT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030728000782003072800078NM 2003 7 28 SWAA031568 120030715A3350101073 LENS BOEING737 7373H4 1384600NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS FELL OFF. REINSTALLED LENS PER MM. 2L72 4F RTA16WE 20030729001052003072900105NE 2003 7 29 MEX2003211 220030506A7321 FUEL CONTROL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE CONTAMINATED A ASMFO OTHER J WARNING INDICATION TOTAKEOFF 1 SW23161PL 49764 FLT 6427 - LAS-MTY - DURING TAKEOFF, ENGINE NR 2 TEMP GOT 603 C OF EGT. TEMPERATURE WAS DECREASED TO 595 DEGREES CELSIUS. FCU WATER TRAMPS WERE DRAINED AND BOTH ENGINES WERE TRIMMED IAW MM 71-00-00. DURING OVERNIGHT SERVICE, TRIM TO BOTH ENGINES WERE PERFORMED AND PARAMETERS WERE CORRECT. ADDITIONALLY, OIL FILTERS WERE CHECKED IAW 71-00-00, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20030730000622003073000062WP 2003 7 30 ABXA030299 120030625A52103925134503 FITTING DOUG DC9 DC932 3022066WP AFT ENTRY DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 AFT ENTRANCE DOOR INTERNAL FITTING CRACKED AT TOP LEFT DOOR STOP. REPLACED FITTING IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030821001632003082100163NM 2003 8 21 03FDEA01027 120030703A5510ALC8106 FITTING DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 EMPENNAGE - LEFT HORIZONTAL STABILIZER NR 14 BORE BOTTOM CORROSION EXCEEDED LIMIT. EMPENNAGE - LEFT HORIZONTAL STABILIZER NR 14 FITTING FABRICATED IAW FEDEX EA 1-5510-71835 - STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL - BORE 14 LEFT - FITTING ALC8106-1 - FABRICATION. 2L73 4F RTA22WE 20030825000022003082500002NM 2003 8 25 UPS03441129 120030806A571265B101496 RIB BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RT WING LE NR 18 VC FLAP IB ARM OB RIB AT ILES 802 CRACKED. STOP DRILLED CRACK TRIMMED OFF STIFFENER THE REPAIR FTG AND THE REPAIR STRAP INSTALLED IAW HXRS NR R57-41-35055 AND EO B747-5740-19118-A ISSUED FOR REPLACE THE RIB WITHIN 18 MONTHS AND PERFORM REPEAT DETAIL VISUAL INSP. AT 77 DAY INTERVALS FOR GENERAL REPAIR INTEGRITY AND CRACK PROPAGATION. 2L74 4F A20WE 20030821001782003082100178NM 2003 8 21 03FDEA01275 120030807A5753 HINGE FITTING DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING - INBOARD FLAP OUTBOARD HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTCHMENT INBOARD & OUTBOARD BORE HOLES FOUND CORROSION. LT WING - INBOARD FLAP OUTBOARD HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTACHMENT INBOARD & OUTBOARD HOLE BORES REPAIRED AS PER FEDEX EA 1-5750-63117, TITLE WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- LT INBOARD FLAP OUTBOARD HINGE BORE REPAIRS 2L73 4F RTA22WE 20030910000232003091000023WP 2003 9 10 DHL2003604554 120030519A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD L/E UPPER SKIN CRACKED 1.500 AT XFS.207.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38, TR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38, TR 57-85. CLEANED, TREATED, PRIMED AREA, FILLER AND DOUBLER INNER PART IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38, TR 57-85. 2L74 4F RT4A25 20030912000722003091200072WP 2003 9 12 DHL2003604751 120030616A1430 FASTENER DOUG DC8 DC873F 302199FWP LT WING SHEARED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING NR 1 ALT TANK FWD LWR PART HI-LOK SHEARED. PERFORMED MAJOR REPAIR IAW BOEING TELEX SEUL-030613 AND SEULIM-03-00019H, FAR FORM 8110-3 DATED JUNE 16, 2003. REMOVED OLD SEALANT IAW EA-04923. CLEANED AND INSPECTED AREA IAW SEULIM-03-00019H, FAA FORM 8110-3. RESEALED AREA IAW SRM 51-1-12. SEE N/R 3824 FOR LEAK CHECK. 2L74 4F RT4A25 20030930000342003093000034NM 2003 9 30 2003UALA00635 120030820A3233651781914 ACTUATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NLG FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29319UA 23951 ON GEAR RETRACTION NOSE GEAR RED AND GREEN LIGHTES REMAINED ON WITH GRINDING SOUND. ALSO AIR NOISE AS IF GEAR DID NOT FULLY RETRACT. FOUND NOSE GEAR LOCK ACTUATOR LEAKING. REPLACED ACTUATOR. ACCOMPLISHED SEVERAL GEAR SWING AND MANUAL EXTENSION. NO SYSTEM FAULT NOTED. ALL INDICATIONS FOUND NORMAL. 2L72 4F4 FRTA16WE E2GL 20031002000552003100200055WP 2003 10 2 UPS03841212 120030831A5340575072671 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, INTERCOSTAL BETWEEN STA. 260-280 IS CRACKED AT LONG. 33R REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG.5750726,AND SRM. 51-1-20D. 2L74 4F RT4A25 20031002000832003100200083NM 2003 10 2 CALA0300521 120030910A5330 BULKHEAD BOEING737 737524 1384721NM FUSELAGE CANNING A CALAK NONE O OTHER ININSP/MAINT 1 SW2714667 28927 INSPECTION FOUND SKIN WEB OIL CANNED AT AFT PRESSURE BULKHEAD FORWARD SIDE RT LOWER SECTION BETWEEN S23R AND Z-CHANNEL. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-80-08, FIGURE 201. 2L72 4F RTA16WE 20031006000372003100600037NM 2003 10 6 QXEA200301123 120030909A5711 SPAR BOMBDRDHC8 DHC8401 1390041NM ZONE 500 OUT OF LIMITS A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 FRONT SPAR 2 LEADING EDGE ATTACH FLANGE HOLES ARE OUT OF LIMITS. BEYOND .263" DIAMETER Y150.300. REPAIRED IAW Q400 RD 8/4-57-203, TASK 51-00-02-250-801 AND HORIZON AIR EA 6-57-173 2H72 4T RTA13NM 20031006001022003100600102NM 2003 10 6 2003UALA00670 120030906A5315 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29664UA 29236 FLOORBEAM STIFFENER AT STA 246, LBL 40 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW STIFFENER. 2L72 4F4 FRTA1NM E24NE 20031006000612003100600061CE 2003 10 6 AMWA35 120030907A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV UE163 RIB AT CSS 39.289 AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 ON RH SIDE AND STRG P/N 101-640000-39 STRG P/N 101-640000-37 (4EA CRACKS ON THIS RIB) 2L72 4T RTA24CE 20031009000322003100900032SO 2003 10 9 SIMA200324401 120030827A335078241 INVERTER EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 CREW REPORTED AN OVERHEAD EMERGENCY LIGHT IN THE CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031027000602003102700060NM 2003 10 27 F3LA200300148 120030925A5315 FLOORBEAM BOEING737 73736E 138443ANM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING A-4 CHECK, INSPECTION REPORTED FLOOR BEAM AT STA. 947.5 CORRODED ON TOP CAP, UPPER AND LOWER SURFACE. FABRICATED AND INSTALLED REPLACEMENT TEE CHORD CAP AND REPAIR SPLICES IAW SRM 53-60-51 AND EA B3-53R-10150. 2L72 4F4 FRTA16WE E2GL 20031027001382003102700138NM 2003 10 27 03FDEA01631 120030924A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 FWD CARGO BAY FRAME DENTED BS 500, STR 24R. DENT OUT OF LIMITS. REPAIRED FRAME BS 500, STR 24R PER SRM 51-40-3 FIG 1 AND EA 7-5310-70515. 2L73 4F RTA3WE 20031027000642003102700064NM 2003 10 27 UPS03441266 120030903A541165B9031077 FRAME BOEING747 747121 1384871NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C NR 4 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT OB FORWARD FRAME WEB. FRAME WEBS REPLACED AND REPAIRED AS IAW RS R-54-53-35064 INSPECTIONS TO CONTINUE IAW UPS EO B747-5410-13908 ( UPS ENGINEERING FILE NR 747-54 -20040 RAISED). 2L74 4F A20WE 20031118000452003111800045EU 2003 11 18 AWXA200301160 120030924A5320D53112070200 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF Y765 FLOOR SUPPORT AT FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y765 FLOOR SUPPORT FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 PG 8-10 & 12 FIG 2 & 3. 2L72 4F RTA28NM 20031030000302003103000030NM 2003 10 30 UPS03441288 120030905A5712 RIB BOEING747 747121 1384871NM NR 18 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, RT WING NR 18 V/C FLAP I/B LINKAGE O/B RIB NR 1 TO NR 3, NR 5, NR 6 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 3, NR 5, NR 6 AND NR 8 BOLT HOLES REPAIRED AS PER RS 574135066 AND REFER EO B747574019269A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20031031000412003103100041NM 2003 10 31 UPS03441332 120030830A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT SIDE AT STA 570 EQUIPMENT COOLING OUTLET CUTOUT FWD FASTENER HOLE FOUND ONE EACH HOLE CRACKED APPROX .0625 INCHES IN LENGTH RUNNING AFT. PLS REEFR ATT. SKETCH. FX STA 560 TO 580 COOLING OUTLET CUTOUT WAS REPAIRED AS PER EO B747-5330-6909-D. 2L74 4F A20WE 20031106001602003110600160NM 2003 11 6 03FDEA01848 120031021A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACH LUG, INBOARD HOLE FOUND CORRODED. 2L73 4F RTA22WE 20031107001672003110700167NM 2003 11 7 AALA20031036 120030918A33500211720004 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21775AN 29584 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROW 34. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20031110001892003111000189NM 2003 11 10 SWAA032234 120031010A3350079123 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS TRACK COVER PER MM. 2L72 4F RTA16WE 20030917000552003091700055CE 2003 9 17 DXTA200300112 120030911A3234 HANDLE CESSNA560 560XL 2076702CE MLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07668QS 5605268 "GEAR UNLOCK" LIGHT REMAINED ILLUMINATED AFTER GEAR HANDLE PLACED IN THE UP POSITION. PERFORMED LANDING GEAR FUNCTIONAL TEST, CHECKED GOOD. CHECKED RIGGING ALL UP LOCK SWITCHES AND HOOKS, FOUND THE NOSE LANDING GEAR UPLOCK TO BE OUT OF RIG, ADJUSTED UPLOCK HOOK AND RIGGED SWITCH. PERFORMED GEAR FUNCTIONAL CHECK, CHECKED GOOD, PERFORMED EMERGENCY GEAR FREE FALL ALSO CHECKED GOOD IAW 560XL MM CHAPTER 32-30-05. 2L72 4F RTA22CE 20040112001332004011200133SO 2004 1 12 C2XA03CL208 120031220A3230 LANDING GEAR EMB 135 EMB135LR 3260305SO NLG & MLG MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714516 145323 BNA FLIGHT 2885, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM BNA. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20040112002482004011200248WP 2004 1 12 AALA20031456 120031221A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21428AA 49340 DFW SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 18D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20031118000102003111800010NM 2003 11 18 UPS03541349 120031006A2622466040 EXTINGUISHER BOEING757 75724APF 1384969NM COCKPIT MISMARKED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01450UP 25472 FIRE EXTINGUISHER ON FLIGHT DECK HAS NO HYDROSTATIC OR MANUFACTURE DATE. REMOVED AND REPLACED FIRE EXT. 2L72 4F RTA2NM 20031121000572003112100057CE 2003 11 21 AMWA81 120031104A526012940003541 RISER BEECH 1900 1900D 1154162CE AIRSTAIR DOOR CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127YV UE127 WHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE AIRSTAIR DOOR FOWARD STEP RISER WAS FOUND TO BE CRACKED. 2L72 4T RTA24CE 20031124000362003112400036NM 2003 11 24 AWXA200301426 120031027A5320654659260 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT CHANNEL AT BS 860, LBL 8.10. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT CHANNEL AT BS 860, LBL 8.10; FABRICATED A NEW REPLACEMENT SECTION OF CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG 201, SHEET 2. 2L72 4F RTA16WE 20040113000992004011300099EU 2004 1 13 BAQA089815 120031029A243245033502 BATTERY UROCOPEC135 EC135T1 5620026EU MASTER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME363 0157 LANDING LIGHT, SEARCH LIGHT, POSITION LIGHT, CYCLIC TRIM INOPERATIVE. PART LASTED ONLY 170.3 HOURS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 11/10/03 1G72 3U H88EU 20040113001322004011300132NM 2004 1 13 03FDEA02253 120031226A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP O/B FWD HINGE ACTUATOR MOUNT O/B LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75210. WINGS, TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031217001362003121700136NM 2003 12 17 SWAA032718 120031211A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 847 LBL 3. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031218001092003121800109NM 2003 12 18 2003UALA00897 120031124A5320 STIFFENER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29645UA 25280 FLOORBEAM STATION 246 STIFFENER IS CRACKED AT LBL 26, FWD SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER PER SRM 51-40-2 AND BAC DWG 141T5814. 2L72 4F4 FRTA1NM E24NE 20031218000582003121800058EA 2003 12 18 03334645 120031130A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27645BR 7383 DURING INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031219001012003121900101NM 2003 12 19 2003UALA00930 120031203A5240 DOOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE E/E BAY OPEN A UALAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 WP29941UA 26676 UNABLE TO PRESSURIZE AIRCRAFT. E&E DOOR WAS FOUND TO BE OPEN. MAINTENANCE WAS DONE IN E&E BAY PRIOR TO THIS FLIGHT (PA SYSTEM). DOOR SWITCH WAS CLEANED AND LUBED PRECAUTIONARY. DOOR WAS THEN CLOSED PROPERLY. 2L72 4F4 FRTA16WE E2GL 20031222000062003122200006EU 2003 12 22 AWXA200301518 120031123A5414D54530052202 SKIN AIRBUS320 A320232 3930326EU NR 2 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 DURING C-06 CHECK CORROSION WAS FOUND ON INBOARD SKIN OF NR 2 PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED CORRODED SKIN PANEL FROM NAC STA 8370 TO NAC STA 9782; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG D54530052; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 1. 2L72 4F RTA28NM 20040105001572004010500157CE 2004 1 5 AMWA109 120031222A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07139ZV UE139 DURING INSPECTION, FIVE CRACKS FOUND IN THIS RIB, THREE ON THE RT SIDE AND TWO ON THE LT SIDE LOCATED ON THE STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-45, 101-640000-42 & 101-640000-38. LT STRINGER P/N 101-640000-43, 101-640000-37. 2L72 4T RTA24CE 20040106001932004010600193NM 2004 1 6 AALA20031212 120031103A33500201720003 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139367 25194 DFW - DURING OVERNIGHT MAINTENANCE, FOUND SEAT 3AB EMERGENCY LIGHT WIRE HARNESS INOPERATIVE. REPLACED SEAT 3AB LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040106000972004010600097NM 2004 1 6 DHL2003742527 120031120A5311 FRAME BOEING727 727225 1384077NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CABIN CRACK FILLER AND BENT FRAME STA 372 STR 5R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA AS REQUIRED FOR REPAIR DIMENSION 3.5 X 3.5 INCH IAW B-727 SRM 57-40-3 FIG 1. FABRICATED ANGLE REPAIR IAW B-727 SRM 53-10-2 FIG 3. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED ANGLE REPAIR AND FILLER IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040108000752004010800075NE 2004 1 8 UO22003F00007 220031013A727030607424 DUCT AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE NR 2 ENGINE CRACKED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19377SC 66 P112312 NR 2 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS. 2L73 4F4 FRTA46EU E1NM 20031126000442003112600044WP 2003 11 26 DHL2003805574 120030820A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 KEEL BEAM LWR SECTION INTERCOSTAL 0.500 CRACKED, STA 940.000. REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-20D PG 21. FABRICATED INTERCOSTAL IAW SRM 53-2-0 PG 1. HEAT TREATED IAW SRM 51-1-1 PG 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED INTERCOSTAL IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031125000762003112500076WP 2003 11 25 DHL2003805596 120030905A54205756829U501 CLIP DOUG DC8 DC873F 302199FWP NR 4 PYLON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 NR 4 PYLON 497 ACCESS PANEL INTERNAL PART CLIP CRACKED AT STA 321.000. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-18B. INSTALLED NEW CLIP WITH NEW FASTENERS ON NR 4 PYLON 497 ACCESS PANEL STA 321.000 IAW SRM 51-1-20D PAGE 9. 2L74 4F RT4A25 20031125001352003112500135NM 2003 11 25 ASAA0310250 120030327A7110 SKIN BOEING737 737298C 1384490NM NR 1 COWLING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL SKIN NACELLE STATION 211.25 GOUGED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20031125001482003112500148NM 2003 11 25 ASAA0310149 120030317A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 400-480, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040126000172004012600017EU 2004 1 26 BAQA091971 120031226A2436D26 VOLT REGULATOR AEROSPAS365 AS365N2 8680815EU GENERATOR FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME92 6417 VOLTAGE REGULATOR WILL NOT CONTROL VOLTAGE OF GENERATOR. REPLACED WITH SERVICEABLE UNIT. 01/14/2004 1G72 3U RTH10EU 20040126000282004012600028NE 2004 1 26 HEEA087793 120030621A6730 BEARING SKRSKYS76 S76A 8143006NE SERVO WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 1363 760076 MAIN ROTOR SERVO, BEARINGS WORN. SHOP REPAIR. 1G72 3U H1NE 20031208001282003120800128 2003 12 8 RAIA00310266 420031023A22147003652902 AUTOPILOT SYS AEROSPATR42 ATR42300 8680920EU INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03423TE106723295 119 AUTO DISPLAY UNIT GAVE STRAIGHT LINE INDICATION. MAINTENANCE REMOVED AND REPLACED THE ADU. 2H72 4T RTA53EU 20031209000552003120900055NM 2003 12 9 UPS03441484 120031015A574065B1447225 FITTING BOEING747 747212B 1384886NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01525UP 21939 INSPECTION TYPE: C, CORROSION REVEALED AT LT WING LANDING GEAR SUPPORT BEAM O/B END AFT FITTING FIVE INDICATIONS AT 2, 6, 7, 9, 11 O'CLOCK RESPECTIVELY WERE FOUND EXCEEDED THE 50 PERCENT ACCEPTANCE LIMIT PER NTM PT4. 57-40-03. REMOVAL OF THE FITTING FOR FURTHER INVESTIGATION ACTION IS NECESSARY. LT WLG SUPPORT BEAM O/B END FITTING REPLACED AS PER MM 57-15-01 & LT WING LANDING GEAR RETRACTION CARRIED OUT AS PER MM 32-32-00. 2L74 4F A20WE 20031209002172003120900217SO 2003 12 9 C2XA03TY187 120030910A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2714543 145553 EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACKS IAW EMB AMM 33-50-04. LIGHTS OPERATIONALY CHECKED GOOD. AIRCRAFT RELEASED. 2L72 4T RTT00011AT 20031010000022003101000002NM 2003 10 10 QXEA200301141 120030915A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09413QX 4060 ON FLIGHT 2309 EN ROUTE TO ACV AT 21,000 MSL, IAS 250 KIAS, MAIN GEAR DOORS CYCLED OPEN AND CLOSED ONCE VERY QUICKLY. ADJUSTED LANDING GEAR DOOR CLOSE PROXIMITY SENSOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031015000712003101500071NM 2003 10 15 USAASB03173 120030926A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19446US 24873 MAINTENANCE REPORTED THE BULLNOSE AISLE EMERGENCY LIGHT, ABOVE SEAT 7D, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY, P/N 2417N504-8, AND THE M1134 CHARGER ASSEMBLY. REINSTALLED SAME BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030918000302003091800030NM 2003 9 18 GAIA03036SP 120030719A5315 FLOORBEAM BOEING727 727* NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CARGO DECK BS 580, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS, FASI N/R 35930. REMOVED AND REPLACED SPLICE PLATE P/N AE 727-1-42-11, PO NR 319397 IAW STC AE 179850-DTD 4-7-93. (M) 2L73 4F RTA3WE 20030922000162003092200016WP 2003 9 22 2003F00558 120030819A4920 TURBINE WHEEL HONEYWELL 8598DHF DOUG DC9 DC9* WP APU ENGINE FAILED B O OTHER T ENGINE CASE PENETRATION NRNOT REPORTED 1 WP07502ME P27751C 502ME POSSIBLE UNCONTAINED FAILURE OF TURBINE WHEEL. 2L72 4F A6WE 20030915000452003091500045SW 2003 9 15 HEEA088920 120030820A3110230375011103 PANEL BELL 230 230 1182149SW COCKPIT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 LIGHTED PANEL RECEIVED BROKEN WHEN UNPACKED. 1G72 3U NCH9SW 20030916001242003091600124NM 2003 9 16 AALA20030508 120030429A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21906AN 29508 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SEAT MOUNTED LIGHTS AT ROWS 9-11R INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030922000082003092200008EU 2003 9 22 MALA030374 120030813A3260 CONNECTOR SAAB SF340 340B 7860101EU RT MLG LOOSE A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15426XJ 340B426 DURING FLIGHT NR 3260, RT MLG DOWN/LOCK INDICATION INOPERATIVE. RT MAIN GEAR LIGHTS INOP WHEN GEAR SELECTED DOWN, RAN QRH TRANSIT HANDLE LIGHT WAS OUT LIGHT TESTED OK. MAINTENANCE FOUND CONNECTOR PLUG 5GA/P1 LOOSE, CLEANED AND RESECURED AS REQUIRED. OPS CHECK GOOD.PER SF340 32-30-00-5. 2L72 4T RTA52EU 20030922001072003092200107EU 2003 9 22 BAQA089237 120030919A6720 BEARING BOLKMS117 BK117A1 5626010EU PITCH LINK WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME351 2214 7243 PITCH LINK BEARINGS WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030924001082003092400108 2003 9 24 03FDEA01392 420030826A2565 SLIDE AIRBUS310 A310 EU DOOR DEPLOYED A FDEAO OTHER O OTHER LDLANDING 1 SO25414FE 400 DOOR L1 OPENED PROPERLY, HOWEVER "EMERGENCY SLIDE" AT LEFT FRONT ENTRANCE DOOR (L1) DID NOT DEPLOY UPON ACTIVATION. MANUAL HANDLE WAS LIKEWISE UNSUCCESSFUL. FACT 06AUG03 16:47 ABQ R REMOVED OLD SLIDE AND INSTALLED SERVICABLE SLIDE ASSY IAW M/M 25-61-21-4-02 2L72 4F RTA35EU 20040128001002004012800100WP 2004 1 28 AALA20031478 120031228A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219681B 53631 AUS DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY OVERHEAD LIGHTS AT 14DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY OVERHEAD LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040130000342004013000034NM 2004 1 30 SWAA032827 120031228A2560PL2230LH00 STRIP BOEING737 7373Q8 1384670NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED AT ROW 9 ABC. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20040130000262004013000026NM 2004 1 30 SWAA032805 120031223A53306545771 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040205000192004020500019NM 2004 2 5 EIA2003155 120031021A5315 FLOORBEAM BOEING747 747132 1384882NM FUSELAGE MISREPAIRED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 EXISTING REPAIR FOUND AT UPPER DECK FLOORBEAM UPPER STA. 440 RBL 7.5 TO RBL 27 REPLACED IAW EIA ENGINEERING. REMOVED EXISTING REPAIR, NDT AREA, FABBED AND INSTALLED NEW REPAIR IAW ECRA 479-53-182-2. 2L74 4F A20WE 20040206000772004020600077WP 2004 2 6 DHL2004806505 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH 46002 MAIN CARGO COMPT NR 5 FLOOR TRACK PLUG WITH LUG WORN AT STA 160.000. REMOVED PLUG WITH WORN LUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 5 FLOOR TRACK STA 160.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040212001782004021200178NM 2004 2 12 AWXA200301589 120031205A575465C26602218 WEDGE BOEING737 73733A 1384673NM NR 5 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-18 CHECK THE NR 5 SLAT OB END UPPER WEDGE TRAILING EDGE SKIN WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED PREVIOUS REPAIR AND DELAMINATED SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW 737-300 SRM 51-70-10, FIG. 16, PG. 67. 2L72 4F RTA16WE 20040217001522004021700152NM 2004 2 17 DHL2003745028 120031230A3260 SWITCH BOEING727 727224 1384076NM MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 WHEN PLACING LANDING GEAR HANDLE TO (OFF) POSITION AFTER TAKE-OFF AND DURING SHALLOW BANK TURNS, FORWARD INSTRUMENT PANEL (DOOR) LIGHT AND S/O'S PANEL R GEAR DOOR) LIGHT ILLUMINATED. DOOR ANNUNCIATOR LIGHTS EXTINGUISH WHEN LANDING GEAR HANDLE PLACED TO (OFF) POSITION IN WINGS LEVEL FLIGHT. TROUBLESHOOTING RT MAIN GEAR DOOR SYSTEM FOUND DIRTY AND LOOSE MAIN GEAR DOOR SWITCH ASSEMBLY. CLEANED AND TIGHTENED SWITCH. OPS CHECKED GOOD IAW B-727 M/M 32-12-01. APPLIED SEALANT TO SWITCH CONNECTORS. AS PRECAUTION ORDERED DOOR SWITCH AND ACTUATOR FOR SHIP TO RIDE (S.T.R.) IN EVENT OF REPEAT WRITE-UP. 2L73 4F A3WE 20040301000802004030100080SO 2004 3 1 SIM2004F00000 120031008A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL GALLEY CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21722AE 145287 DURING INSPECTION THE LT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMIT BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED THE CORROSION BY CREATING A CUT OUT IN THE DAMAGED FLANGE AND WEB OF THE LT FLOORBEAM. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS FOR REPAIR. REPAIR DONE IAW MFG SRM. 2L72 4F4 FRTT00011ATTE6CH 20040401000532004040100053EU 2004 4 1 USAA030325 120031202A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .5 INCH BY .5 INCH AREA, AT LBL 17.75 FRAME 54. MODIFIED PART INSTALLED. INSTALLED NEW SECTION OF SEAT TRACK PER SRM 53-31-15 FIG 201. (M) 2L72 4F RTA46NM 20040308000502004030800050EU 2004 3 8 03FDEA00435 120030412A4920 APU AIRBUS330 A300* EU APU BAY LEAKING A FDEAC ABORTED TAKEOFF BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 SO25676FE 790 DURING TAKEOFF APPROX 600 FT, CAPT SMELLED SMOKE BY MAIN DECK CARGO, SMOKE DET RT MID 2 SMOKE LOOP FOLLOWED BY LT MID 2 LOOP. DURING PROCEDURES ON DOWNWIND BOTH LIGHTS WENT OUT. ON FINAL BOTH MID 2 LOOPS ILLUM'D AND ON TOUCHDOWN MID 1 LEFT & RIGHT LOOPS ILLUMINATED. DURING GROUND EVACUATION R-1 WAS USED, DOOR OPENED BUT SLIDE DID NOT INFLATE. SMOKE RELATED ISSUE HAS BEEN ISOLATED TO APU LOAD COMPRESSOR BYPASS OIL LEAK REF: DISC 49-50/3233. 2L72 4F RTA26NM 20031211000782003121100078NM 2003 12 11 AWXA200301413 120031026A573065C262711 SKIN BOEING737 7373G7 1384595NM LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-13 CHECK .3125 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN ABOVE NR 2 SLAT OUTBOARD AUXILIARY TRACK. MAINTENANCE PERFORMED BOND REPAIR ON LT WING LEADING EDGE SKIN ABOVE NR 2 SLAT OUTBOARD AUXILIARY TRACK IAW B737-300 SRM 51-70-17, PG 27 REPAIR 7. 2L72 4F RTA16WE 20031212001332003121200133WP 2003 12 12 AALA20031204 120031101A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21244AA 49256 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHT ASSEMBLY AT SEAT 7D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031215000082003121500008NM 2003 12 15 AWXA200301444 120031106A532069353522 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN TIE CLIP AT BS 663.75, STR 10 RT. MAINTENANCE REMOVED CRACKED TIE CLIP AT BS 663.75, STR 10 RT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW SRM 51-40-02 PG 1 & 38 FIG 8. 2L72 4F RTA16WE 20031211001172003121100117WP 2003 12 11 AALA20031395 120031207A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21439AA 49457 DFW FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040520002682004052000268EU 2004 5 20 2004F00119 120030910A5320 FLOOR SUPPORT AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 48 AND FRAME 50 ABOVE STRINGER 38L IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 48L TO 52L, STRINGER 38L IN AFT LOWER CARGO BAY. (M) 2L72 4F RTA28NM 20031212001042003121200104NM 2003 12 12 SWAA032399 120031030A53116546500 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED AT STR 9L, BS 867, BS 907, AND BS 747. REPAIRED FRAMES PER BFG ER. 2L72 4F RTA16WE 20031217000892003121700089EA 2003 12 17 COMA0360510 120031120A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01443CA10694 7539 FLIGHT 5375 FLAPS FAILED. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20030926000772003092600077NM 2003 9 26 0301655641 120030827A2913 O-RING BOEING757 757251 1384970NM HYD PUMP RUPTURED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01541US 26488 LEFT HYDRAULIC QUANTITY DECREASED TO .14, EDP DEPRESSURIZED. WITH ELECTRIC PUMP OFF QUANTITY CONTINUED TO DECREASE UNTIL THERE WAS A TOTAL LOSS OF FLUID. AIRCRAFT DIVERTED TO ALB DECLARING A YELLOW EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND LEAK AT RUPTURED O-RING AT DEPRESSURIZATION MODULE PLUG. REPLACED O-RING AND FOUND FERROUS AND NON FERROUS FILINGS IN LEFT CASE DRAIN FILTER. REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP (55-2911-9-0014, S/N OFF 22458) AND LEFT ELECTRIC HYDRAULIC PUMP (55-2911-9-0013, S/N OFF 56185. 2L72 4F RTA2NM 20030926001132003092600113NM 2003 9 26 2003UALA00646 120030821A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29365UA 24534 MAIN CABIN FLOORBEAM AT BS 927 AT RBL 45 IS CRACKED AFT SIDE UNDER T-CAP. MAJOR REPAIR ACCOMPLISHED, INSTALLED SUPPORT ANGLE AND STRAPS. 2L72 4F4 FRTA16WE E2GL 20030818000152003081800015NE 2003 8 18 HEEA088424 120030806A28417645001078103 INDICATOR SKRSKYS76 S76A 8143006NE FUEL QTY MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 RT NEEDLE BAD. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030820001252003082000125WP 2003 8 20 UPS03841109 120030725A5320561378523 WEB DOUG DC8 DC873F 302199FWP COCKPIT SUBFLOORCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C2, VERTICLE WEB IN COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS AT STA -80 LBL 50 AT FUSELAGE SKIN. REMOVED, FABRICATED AND REPLACED WEB/DOUBLER IAW DWG 5613785 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20030331000572003033100057CE 2003 3 31 AMWA17 120030305A5346 FINGER DOUBLER BEECH 1900 1900D 1154162CE RT ENG TRUSS CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07237YV UE237 WHILE PERFORMING AN "A" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND THAT THE FINGER DOUBLER WAS CRACKED. MAINTENANCE REMOVED AND REPAIRED THE FINGER DOUBLER. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030331001172003033100117NM 2003 3 31 DHL2003720003 120030325A3231 DOOR BOEING727 727228 1384083NM MLG LACK OF LUBE A DHLAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01720DH 19544 NOSE GEAR WOULD NOT EXTEND ACCOMPLISHED ABNORMAL PROCEDURE AND NOSE GEAR EXTENDED. LUBRICATED ALL DOOR LATCHES AND PERFORMED GEAR SWING NUMEROUS TIMES IAW B-M/M 32-30-00. NO DEFECTS NOTED. 2L73 4F RTA3WE 20030821002342003082100234NM 2003 8 21 0301426627 120030731A3350 BATTERY PACK BOEING747 747251B 1384892NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01627US 21709 DURING LINE CHECK, FOUND A-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030401001192003040100119WP 2003 4 1 DHL2003804511 120030117A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER UPPER PART CRACKED AT XFS 454.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030404000242003040400024NM 2003 4 4 DHL2003746004 120030403A3350 BATTERY BOEING727 727224 1384076NM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01746DH 22252 EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE OVER FORWAR ENTRY DOOR DURING STANDBY POWER CHECK. REPLACED BATTERIES AND LIGHT ASSEMBLY IN ENTRYWAY IAW M/M 33-50-71. OPS CHECKED GOOD. 2L73 4F A3WE 20030331000092003033100009EU 2003 3 31 03FDEA00354 120030328A5510 RIB AIRBUS310 A310 EU HORIZONTAL STAB CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25443FE 283 LT HORIZONTAL STAB. INTERIOR RIB 5 UPPER CHORD AT REAR SPAR IS CRACKED AT HOISTING POINT WRITTEN ON FEDEX N/R N00494 UNDER MAE W/O NR 13350 CUT OUT DAMAGED SECTION IAW/SRM 51-71-50 FABRICATED REPAIR ANGLE OF 7075T6 BATCH NR 7R00115001 IAW/SRM 51-71-50 INSTALLED REPAIR ANGLE IAW/SRM 51-40-21. COMPLETED UNDER MAE W/O NR 13350 ON FEDEX NR. N00494. 2L72 4F RTA35EU 20030331000122003033100012EU 2003 3 31 117521 120030330A2751522858 INDICATOR SAAB SF340 SF340A 7850100EU COCKPIT STICKING A UHLAL ABORTED APPROACH O OTHER LDLANDING 1 GL1735SZ 35 FWA DURING APPROACH TO LAND WITH FLAPS SELECTED TO 20 DEGREES, RT FLAP INDICATED 20 DEGREES, LT INDICATED 0 CIRCLED AROUND FOR ANOTHER APPROACH RESET FLAPS 20 BOTH FLAPS INDICATED CORRECTLY WITH NO FLAP WARNING LIGHT ON THE CWP MAINTENANCE INSPECTED AIRCRAFT AND REPLACED FLAP POSITION INDICATOR IAW SF340 M/M 39-40-30-4 PERFORMED OPS CHECKS PER M/M NO FURTHER DEFECTS NOTED AIRCRAFT RELEASED FOR SERVICE 2L72 4T RTA52EU 20030403001292003040300129NM 2003 4 3 DL733030313 120030329A5415311A11112 FITTING BOEING737 737347 1384647NM NR 2 PYLON CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 THE AFT LUG OF THE CROWN BEAM FITTING ON THE NR 2 ENGINE PYLON WAS FOUND WITH CORROSION IN THE HOLE BORE. THE BORE WAS OVERSIZED TO 3.10 INCH TO REMOVE THE CORROSION. A STEEL REPAIR BUSHING WAS INSTALLED AND THEN A NEW BEARING. THE REPAIR WAS ACCOMPLISHED PER ER/A 384677-14. 2L72 4F RTA16WE 20030408000872003040800087NM 2003 4 8 03FDEA00396 120030407A5313 STRINGER BOEING727 727200 138407ENM BS 560+17 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 N01236 CRACKED STRINGER AT BS 560+17 STR 23 LT. 2L73 4F RTA3WE 20030411000072003041100007NM 2003 4 11 SWAA030741 120030403A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C4 CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS AT STRINGER 10R, BS 727B+15, BS 727C+12, BS 727D+5, AND BS 727E+13. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030416002232003041600223NM 2003 4 16 AALA20030225 120030222A3350 CONNECTOR BOEING757 757223 1384957NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21640A 24598 DFW - DURING OVERNIGHT MAINTENANCE, LOWER OVERWING EMERGENCY EXIT LIGHTS AT SEAT 16D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20030416002422003041600242NM 2003 4 16 CALA0300179 120030406A5315 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT STA 294.5, RBL 35-50. REPAIRED FLOORBEAM IAW SRM 53-10-51. 2L72 4F4 FRTA16WE E2GL 20030424000342003042400034WP 2003 4 24 ZW0A0303201 120030317A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13978TW 53628 THE EGRESS LIGHT WAS INOPERATIVE AT ROW 21 AND 28. SECURED LOOSE BULB AT BOTH LOCATIONS. CHECK-C 8-17-2002 MCI. 2L72 4F RTA6WE 20030428000452003042800045EA 2003 4 28 SWIA200311865 120030331A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07454SW681 681 7749 FLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES TO 8 DEGREES. PERFORMED QRH AND RETURNED TO MEM FOR 8 DEGREE LANDING. REMOVED AND REPLACED RIGHT FLAP BPSU IAW MM 27-51-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20030428001292003042800129WP 2003 4 28 ZW0A0303908 120030402A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13925TW 49357 THE FUSELAGE SKIN WAS DAMAGED AT STA 591 TO 596, BELOW LONGERON 26R, 6 INCHES BY 5 INCHES AND 0.074 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3. 2L72 4F A6WE 20030429001542003042900154EA 2003 4 29 CA030317001 120030315A2721601R512263 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA 21409 (CAN) 6 TO 7 MINUTES AFTER TAKE OFF RUDDER STARTED MOVING FULL RIGHT, RUDDER TRIM. APPLIED LT TRIM - STOPPED AT 1.25 RT DEFLECTION. RUDDER TRIM STUCK. EMERGENCY DECLARED AND DIVERTED TO TPA. R&R'D AILERON TRIM PANEL 2L72 4F4 FRTA21EA E15NE 20030501000912003050100091 2003 5 1 2003F00241 420030205A344506650012704 INDICATOR SWRNGNSA227 SA227AC 8780603SW VSI FAILED A BSAAO OTHER O OTHER DEDESCENT 1 NM05430MA AC710B FLT 2579 - BIL - NR 1 VSI FAILED DURING DESCENT. CREW LANDED WITH NO FURTHER INCIDENT AFTER DECLARING EMERGENCY. TCAS/VSI INDICATOR WAS BAD. REPLACED VSI/TCAS INDICATOR, SYSTEM TEST GOOD. (M) 2L72 4T RTA8SW 20030501001032003050100103WP 2003 5 1 GTIA030212 120030310A5730 PANEL DOUG DC9 DC983 3022083WP LEFT WING TORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND LEFT WING FUEL PANEL NR 1365C LANDING FUEL STRIP TORN. CUT OUT DAMGAED AREA AT XRS290 IAW EA 57300304. FABRICATED -7 FILLER AND -3 DOUBLER. FABRICATED -5 DOUBLER. INSTALLED -5 DOUBLER. INSTALLED -7 FILLER AND -3 DOUBLER. (M) 2L72 4F RTA6WE 20030502001332003050200133NM 2003 5 2 377PA0014 120030414A335002049001 LIGHT BOEING737 7373L9 1384470NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05377PA 23718 ROW 1 THRU 5 EMERGENCY PATH LIGHTS INOP. REPLACED LAMP CONNECTING STRIP PER MM 33-50-00. OPS CHECK OK. 2L72 4F RTA16WE 20030502002192003050200219WP 2003 5 2 EIA2003057 120030411A5330 SKIN DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09916F 47044 FUSELAGE SKIN AT LWR AFT CORNER OF MAIN DOOR JAMB CRACKED. REPAIRED PER DC9 SRM 53-05 FIG 103 PAGE 407-418 & 420. REPAIR IS CAT-B N5343 ASSIGNED INSP WITHIN 28,000 CYCLES PER SRM 51-10-5C (EDDY CURRENT). 2L72 4F A6WE 20030505002132003050500213NM 2003 5 5 03FDEA00517 120030418A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 GOUGE ON INNER SKIN AT BS 1041 LBL 25 WL 146. 2L73 4F RTA3WE 20030506000312003050600031EA 2003 5 6 SWIA200311883 120030416A3234750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07926SW 7687 GEAR DISAGREE ON FINAL. RECYCLED 3 TIMES, THEN DID A MANUAL RELEASE. REMOVED AND REPLACED MLG SELECTOR VALVE IAW CRJ MM 32-32-00. PERFORMED MULTIPLE GEAR SWINGS. ALL OPS CHECK GOOD. 2L72 4F RTA21EA 20030507000812003050700081CE 2003 5 7 AUS20030369 120030311A574011412003824LH3 FITTING BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3A NE WING DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING FORWARD ADAPTER PLATE DAMAGED. FASTENER HOLES ELONGATED. FRETTING AND CORROSION ALSO EVIDENT. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030507001872003050700187SO 2003 5 7 C852003F00001 120030401A2840550697 TRANSMITTER PIPER PA31 PA31325 7103105SO LYC O540 TIO540* 41532EA LT WING CORRODED B C85RK NONE O OTHER ININSP/MAINT 1 NE014039L3858 318112013 DURING ANNUAL INSPECTION. FUEL LEAK WAS NOTED FROM LEFT WING. EXTENSIVE CHECKING SHOWED LEAKS FROM BOTH INBOARD AND OUTBOARD FUEL SENDERS. SENDERS WERE FOUND TO BE BADLY ROTTED AND CORRODED, BUT WERE STILL OPERATING AND INDICATING PROPERLY. REPLACING SENDER UNITS AND GASKETS CORRECTED THE FUEL LEAK PROBLEM. CAUSE DETERIORATION OF SEALANT USED WHEN FACTORY BUILT. 1L72 3O3 O A20SO E14EA 20030509001312003050900131NM 2003 5 9 PCAA0304072 120030408A551085510202006 STRUCTURE DHAV DHC8 DHC8102 2809003NM HORIZONTAL STAB SEPARATED A PCAAO OTHER E VIBRATION/BUFFET APAPPROACH 1 EA13804EX159657756 227 CREW REPORTED AIRFRAME VIBRATION OCCURED 3 TIMES ON APPROACH. FLIGHT ATTENDANT REPORTED A VERY LOUD VIBRATION IN FORWARD PART OF CABIN, AND NR 2 ENGINE NH INCREASED 1.5 PERCENT DURING VIBRATION PERIOD. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED INBOARD RIGHT HORIZONTAL STABILIZER LEADING EDGE DEICE BOOT HAD SEPERATED. LEADING EDGE WAS REPLACED IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 MAINTENANCE MANUAL. OPERATIONAL CHECK WAS GOOD. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030515000322003051500032EA 2003 5 15 03124705 120030504A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 DURING MAINTENANCE INSPECTION, THE NR 3 CABIN CEILING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030604001032003060400103NM 2003 6 4 UPS03440518 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 940 LT STRINGER 25L FRAME FOUND CRACKED. REF NRC 7344 FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030602001592003060200159NM 2003 6 2 VNAA0305020 120030529A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN DOOR FAILED A VNAAO OTHER O OTHER CRCRUISE 1 GL07431JS 3028 EN ROUTE AT 25,000 FEET, THE CREW RECEIVED A DOORS LIGHT ON THE RED WARNING PANEL. THE CREW DESCENDED AND THE LIGHT WENT OUT AT 13,000. UPON ARRIVAL AT CLT, OUTSTATION MAINTENANCE INSPECTED THE WIRING AND CLEANED THE MAIN CABIN DOOR PROXI SENSORS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. THE AIRCRAFT WAS THEN PRESSURIZED WITH THE CREW AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030605001132003060500113CE 2003 6 5 GLBA2003058 120030501A2130MS3548976 GROMMET BEECH 1900 1900D 1154162CE PRESSURE SEAL FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03257GL UE257 CABIN PRESSURIZATION SYSTEM FAILED IN FLIGHT, REPLACED PRESSURE SEAL GROMMET AND REINSTALLED OUTFLOW VALVE OPS CHECK GOOD. 2L72 4T RTA24CE 20030605001592003060500159WP 2003 6 5 ABXA030144 120030515A2740 STABILIZER DOUG DC9 DC941 302207NWP VIBRATION A ABXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL23957AX 47759 SUSPECT FLIGHT CONTROL MALFUNCTION OF STABILIZER. DURING FLIGHT, THE AIRCRAFT EXHIBITED INCREASING TURBULANCE AND VIBRATION. THE AUTO PILOT WAS ENGAGED AND WORKING PROPERLY WITH NO NOTED PROBLEMS. FLIGHT LEVEL WAS AT 240, 330 KIAS. AS SOON AS AIRSPEED WAS REDUCED 10 KTS., THE PROBLEM WENT AWAY. OPENED ACCESS PANEL 6401, VISUALLY INSPECTED JACKSCREW THROUGH FULL OPERATION. INSPECTED ELEVATOR TAB BEARINGS, INSPECTED RUDDER AND TAB BEARINGS. RAN THROUGH FULL OPERATION, NO DEFECTS NOTED IAW DC09 MM 27-40-00-02. AIRCRAFT RELEASED FOR EVALUATION FLIGHT. EVALUATION FLIGHT WAS SATISFACTORY. 2L72 4F A6WE 20030609000152003060900015SO 2003 6 9 SWIA200311983 120030520A3260 SQUAT SWITCH EMB 120 EMB120ER 3260203SO MLG FAULTY A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07561SW 120335 AFTER T.O GEAR WOULD NOT RETRACT,. USED ''DOWNLOCK RED BUTTON'' TO RETRACT THE GEAR. ''IDLE AND UNLOCK'' LIGHT ILLUMINATED, AUTO PRESSURIZATION WOULD NOT PRESSURIZE, TCAS REMAINED ON.TROUBLESHOT SYSTEM. FOUND RIGHT LANDING GEAR WEIGHT ON WHEELS SWITCH FAULTY. REPLACED WEIGHT ON WHEELS SWITCH WITH SERVICEABLE UNIT. CYCLED GEAR. OPS CHECK GOOD. 2L72 4T RTA31SO 20030609001342003060900134NM 2003 6 9 AWXA200300579 120030522A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1 THRU 4 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 3 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030611000402003061100040WP 2003 6 11 MEX2003172 120030511A53502672491 LOCK DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE RADOME BROKEN W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23803ML 49726 THE RADOME RIGHT LOCK WAS BROKEN BY F.O.D. THE RADOME LOCK WAS REPLACED IAW MM 53-51-02, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20030612000192003061200019SO 2003 6 12 C2XA03SH163 120030529A531514530628001 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED BEAM IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030612000612003061200061SO 2003 6 12 SWIA200312035 120030527A27503075001007 FCU EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07196SW4431 3307 120151 ON TAXI OUT, WHILE SELECTING FLAPS 15 DEGREES, A CONTROL FAULT ON THE FLAP WARNING INDICATOR ILLUMINATED. OUTBOARD FLAPS SHOW ONLY ONE BAR DOWN. INSTALLED SERVICEABLE FCU IAW 27-50-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20030611001602003061100160EU 2003 6 11 MALA030281 120030523A243523080031 STARTER GEN SAAB SF340 SF340A 7850100EU ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15106XJ 340A106 AFTER TAKEOFF OF FLIGHT NR 3388, LT GEN OVERTEMP LIGHT ILLUMINATED AFTER TAKEOFF. QRH ADVISED MAINTENANCE. AIR RETURN TO MSP. MAINTENANCE REPLACED LT STARTER/GEN AS PER TASK CARD 243103 P/N 23080-031, S/N OFF 9531, S/N ON 3595. OPS CHECK GOOD. 2L72 4T RTA52EU 20030612000682003061200068SO 2003 6 12 C2XA03TY079 120030530A532014522226003 GUSSET EMB 145 EMB145LR 3260212SO LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING A SCHEDULED 2C INSPECTION THE LAV FLOOR SUPPORT GUSSETS IN ZONE 261DF AND 262CF WERE CORRODED. MAINT INSPECTED AREA, REMOVED AND REPLACED RIVETS ON LT AND RT GUSSETS AS NEEDED. REMOVED AND REPLACED THE CENTER GUSSET, PRIMED AND PAINTED IAW SRM 135/145 51-40-02, EC 2003-145/1150 AND CPM51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030520000962003052000096 2003 5 20 USAASA03032 420030417A2565D31516113 SLIDE AIRBUSA321 A321211 3930370EU CABIN MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19186US 1701 TPA - FAULT MESSAGE, 'EPSU EXT LOAD FWD L', RESULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY ESCAPE SLIDE DUE OT SLIDE LIGHT FAILURE. ALSO, REPLACED THE FORWARD RIGHT SLIDE DUE TO HIGH SLIDE LIGHT HARNESS RESISTANCE. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030521001552003052100155WP 2003 5 21 DHL2003604501 120030505A57305705518503 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING LWR SURFACE- LT NR 540 LWR ACCESS DOOR OUTER SKIN DELAMINATED FROM XS 475.000 - XS 507.000. REMOVED AND REPLACED LT LWR ACCESS DOOR NR 540 (STA 475.000 - 507.000) IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030521000572003052100057WP 2003 5 21 MWEA030199 120030501A56105912290506 WINDSHIELD DOUG DC9 DC914 3022034WP COCKPIT CRACKED A MWEAB EMER. DESCENT O OTHER CRCRUISE 1 GL31600ME 45725 FIRST OFFICER'S WINDOW SUDDENLY CRACKED. REMOVED AND REPLACED WINDSHIELD. 2L72 4F A6WE 20030618001642003061800164 2003 6 18 HEEA087142 420030610A2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 FM NR 1 AND 2 RECEIVE SELECTOR SWITCHES ARE OPPOSITE. COULD NOT VERIFY COMPLAINT. FOUND SWITCH S1 NOISY AND CAPACITOR C30 BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1G72 3U H1NE 20030523001072003052300107NM 2003 5 23 QXEA0300520 120030418A5310 STRUCTURE DHAV DHC8 DHC8202 2809007NM ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX-BOTTOM DAMAGE ON STRUCTURE AND STARTING TO CRACK AT RIGHT HAND EMERGENCY DOOR. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-00-06. 2H72 4T RTA13NM 20030523001172003052300117NM 2003 5 23 2003UALA00425 120030513A3260 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG ILLUMINATED A UALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP29390UA 24665 AIRCRAFT HAD AN UNSAFE GEAR INDICATION ON APPROACH. FLEW A MISSED APPROACH AND USED ALTERNATE GEAR EXTENSION PROCEDURE. 2L72 4F4 FRTA16WE E2GL 20030529000782003052900078NE 2003 5 29 HEEA086520 120030521A62107615009100050A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH12137 760224 SEPERATED ON THE LOWER SIDE NEAR STATION 44. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20030619000262003061900026SW 2003 6 19 HEEA087375 120030611A5320407070620156 PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 HEADLINER PANEL CRACKED. 1G71 3U O H2SW 20030619000832003061900083SW 2003 6 19 HEEA087217 120030609A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q249 51540 MAIN BATTERY WEAK. 1G71 3U H2SW 20030625000432003062500043EU 2003 6 25 AWXA200300597 120030515A33971703302 TERMINAL AIRBUS320 A320231 3930325EU ZONE 900 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 DURING C-01 CHECK THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR IAW A320 ESPM 20-48-24, PG. 18, OPERATIONAL CHECK WAS GOOD IAW AMM SUBTASK 33-51-00-710-051. 2L72 4F RTA28NM 20030625000592003062500059NM 2003 6 25 DHL2003747510 120030513A5754 STIFFENER BOEING727 727224 1384076NM LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING "C" CHECK N/R 53650 LT WING LE CAVITY LE STA. 1307 VERTICAL STIFFENER IS CRACKED AT BOTTOM END (FRONT SPAR WBL 92.8. REMOVED L/H WING ACCESS PANEL 6303 TO FACILITATE SM WORK IAW B-727 M.M. 57-30-0. REMOVED LT WING FUEL TANK ACCESS 7340 TO FACILITATE SM WORK IAW B-727 M/M 28-14-11. STOP DRILL CRACK IAW B-727 SRM 51-10-1. 4) HFEC VERIFIED STOP DRILL CRACK IAW B-727 PT-6 NDT M/M 51-00-00 FIG. 23. FABRICATED REPAIR DOUBLER TREATED AND PRIMED ALL PARTS AND AREAS. 2L73 4F A3WE 20030630000702003063000070 2003 6 30 BAQA087577 420030618A221041600297006 MODULE UROCOPEC135 EC135P1 8680990EU TRIM ACTUATOR FAULTY B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TS 0167 AT INSTALLATION FOUND UNIT TO BE FAULTY-CAUTION WARNING TRIM/ACTUATION. SAME PROBLEM WITH THIS UNIT BEFORE REPAIR. REPLACED WITH ORIGINAL UNIT. 1G72 3U O H88EU 20030701000252003070100025EU 2003 7 1 I05R087789 120030522A5320C345A52011201 SUPPORT UROCOPEC130 EC130B4 EU ANTENNA CRACKED B I05RO OTHER O OTHER NRNOT REPORTED 1 WP0526LB 920 3514 ANTENNA HAS A CRACKED SUPPORT, REPLACED SUPPORT. 1G72 3U H9EU 20030707001232003070700123NM 2003 7 7 AWXA200300734 120030608A53156546812193 FLOORBEAM BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOORBEAM AT BS 992, RBL 23-47, WL 208. MAINTENANCE FOUND PRE-WORK MEASUREMENT OF MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM BS 992, RBL 23-47, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG 6546812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10, FIG. 2. 2L72 4F4 FRTA16WE E2GL 20030715000082003071500008NE 2003 7 15 CA030526002 220030525A7230 BLADE LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122B02 54555NE NR 3 ENGINE DAMAGED W E ENGINE SHUTDOWN E VIBRATION/BUFFET CLCLIMB 1 CA (CAN) AIRCRAFT RETURNED TO STATION AFTER TAKE OFF DUE TO NR 3 ENGINE HIGH VIBRATION ( 2.5 UNITS ) DURING CLIMB. ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE STATION WITH NO FURTHER PROBLEM.RECTIFICATION: THE COMPLETE SET OF FAN BLADES WAS REPLACED AND AFTER VERIFICATION, THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 20030630000882003063000088SW 2003 6 30 HEEA087850 120030614A5610407030115125 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 WINDSHIELD CRAZED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000932003071700093EU 2003 7 17 BAQA087887 120030624A77129550176240 TRANSMITTER AEROSPSA365 SA365N 8680669EU TORQUE FLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM 6396 TORQUE FLUCTUATES. REMOVED FROM ENGINE NR 12051. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030108000082003010800008NM 2003 1 8 DHL2003743001 120030108A2611 BATTERY BOEING727 727225 1384077NM A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01743DH 22438 1) LOWER CARGO SMOKE/FIRE DETECTION SYSTEM GREEN LIGHT INOP.2) REMOVED AND REPLACED CCU IAW M/M 26-16-00. NO HELP, TRANSFERRED TO DMI #11515 IAW B-727 MEL 26-19 CAT. "C". PLACARDS INSTALLED.3) REF. DMI #11515 LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM 1 GREEN LIGHT INOP. 4) REMOVED AND REPLACED BATTERIES IAW M/M 26-16-0. THIS CLEARS DMI #11515 PLACARD INSTALLED. 2L73 4F A3WE 20030129000272003012900027SW 2003 1 29 HEEA083937 120030117A6300407010206103 SPRING BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 SPRING ELASTOMER IS DETERIORATED AND TORN. 1G71 3U O H2SW 20030204000772003020400077 2003 2 4 SWAA030164 420030122A256565C16820 CLIP BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR CLIP HOOK LOOSE. SECURED CLIP HOOK PER MM. 2L72 4F RTA16WE 20030204001032003020400103NM 2003 2 4 SWAA030097 120030116A27316545166 BEARING BOEING737 7372H4 138448CNM BOTH ELEV'S WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB CONTROL ROD BEARING ASSY'S PER MM. 2L72 4F A16WE 20030205001302003020500130NM 2003 2 5 DL76L030035 120030107A2910S271T4529 PRESSURE SWITCH BOEING767 767332 1382001NM HYD SYSTEM FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27184DN 27111 XXX IR - AFTER T/O RT ENGINE PRIMERY HYD PUMP PRESS LIGHT CAME ON OVERHEAD AND EICAS. FLUID QUANTITIES OK. REPLACED S31 PRESSURE SWITCH, OPS CHECK/LEAK CHECK OK. 2L72 4F RTA1NM 20030207001352003020700135NM 2003 2 7 QXEA0300006 120030104A36208209732 SWITCH BOMBDRDHC8 DHC8401 1390041NM BLEED AIR SYS MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09403QX 4037 SEA ON FLIGHT 2388- NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED INFLIGHT. CAUTION LIGHT EXTINGUISHED ABOUT FIVE MINUTES AFTER EMERGENCY/ABNORMAL CHECKLIST WAS COMPLETED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT HAND BLEED OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030210000302003021000030EA 2003 2 10 03039660 120030208A335064645 LIGHT CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27660BR 7519 During maintenance inspection at CAE, it was discovered that the emergency floor track lights were inoperative between seat rows 1 and 4. The aircraft was determined capable of safe flight and was ferried to ORD for corrective action. Maintenance personnel removed and replaced the forward emergency floor track light strip. An operational check was satisfactory and the aircraft was returned to service. 2L72 4F RTA21EA 20030211000142003021100014WP 2003 2 11 ZW0A0301901 120030210A3350408822101 BATTERY DOUG DC9 DC982 3022082WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13924TW 49100 THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE IN FIRST CLASS AND AT ROWS 10 TO 14. REPLACED THE BATTERIES IN THE BATTER PACK AT BOTH LOCATIONS. CHECK-C 3-18-02 STL. --CLOSED-- 2L72 4F A6WE 20030212000762003021200076EA 2003 2 12 CA030120001 120030116A2497 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TERMINAL BLOCK LOOSE W AD UNSCHED LANDING RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB, FLIGHT CREW RECEIVED EICAS MESSAGES THAT FOLLOW "LT WINDOW HEAT, LT STATIC HEAT, LT AOA HEAT, STBY PITOT HEAT, BASE PITOT HEAT" SINCE ICING CONDITION EXISTED AHEAD, IT WAS DECIDED TO RETURN TO DEPARTURE BASE IT WAS FOUND THAT TWO WIRES, XD14H10B AND XD14J10B, ON TERMINAL BLOCK ITEM NR 75 (TB1-3) WERE LOOSE, AND CAUSED THE WIRES NOT TO SUPPLY POWER TO THE CIRCUIT BREAKERS CBP3 B1 THRU B13. NUTWAS REMOVED BY USING FINGERS ONLY. COMPONENTS REPLACED: 75 - TERMINAL BLOCK - MS27212-2-5 95 -BUSBAR - S1448-4-24-2 100 - WASHER - NAS1149D0363J105 - NUT - MS21042L3 BOTH WIRES GOING FROM TB1 TO CIRCUIT BREAKERS B1 AND B13 ( 6 TO 8 INCHES LONG) 2L72 4F4 FRTA21EA E15NE 20030213000892003021300089EA 2003 2 13 COMA0360088 120030212A7810 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01729CA 7265 FLIGHT 5719 R/H THRUST REVERSER UNLOCK CAUTION DURING T/O.SECURED REVERSER AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20030625000712003062500071NM 2003 6 25 F3LA200300043 120030128A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED L-1 DOOR MOP SILL U-CHANNEL CORRODED FROM STA 312 TO STA 344. REPLACED U-CHANNEL PER SRM 51-40-02. 2L72 4F RTA16WE 20030218000062003021800006NM 2003 2 18 03FDEA00084 120030105A5753ARC2513501 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 SNRM N0557 - LT WING INBOARD T/E FLAP OUTBOARD LOWER SIDE AT FLAP SIDE, AT PIVOT PIN BORE HOLE FOUND CORROSION. ** S/D ** COMING 2L73 4F RTA22WE 20030218000202003021800020NM 2003 2 18 03FDEA00117 120030210A5310507945177 DOOR FRAME BOEING727 727200 138407ENM PWA JT8 JT8D* NE FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FORWARD ENTRY DOOR FRAME CHAFED JUST BELOW LOWER HINGE. BLENDED AND TREATED FORWARD ENTRY DOOR FRAME IAW E.A. 7-5210-68181 2L73 4F4 FRTA3WE E2EA 20030219000272003021900027NM 2003 2 19 2003UALA00161 120030211A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29511UA 24799 SKIN DAMAGE BY JETWAY FORWARD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPLACED. 2L72 4F4 FRTA2NM E17NE 20030219000752003021900075NM 2003 2 19 SWAA030254 120030131A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, WL 208 AND LBL 54. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20030220000852003022000085EA 2003 2 20 QXEA0300083 120030115A2820D98C07606 SENSOR CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM DEFECTIVE A QXEAK NONE O OTHER UKUNKNOWN 1 NM09601QX856 10009 PDX-RIGHT PRIMARY EJECTOR PRESSURE SENSOR SWEATING. REMOVED AND REPLACED PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030116000792003011600079SW 2003 1 16 HEEA083039 120030106A2430SM20ACD200A21 RELAY BELL 206 206L3 1182108SW DC SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 GENERATOR DROPPING OFF LINE. 1G71 3U H2SW 20030220001812003022000181 2003 2 20 ARWA20030201 420030202A342225883025 GYRO DOUG DC8 DC862 3021970WP COCKPIT MALFUNCTIONED A ARWAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19810BN 45905 NR 2 RADIO MAGNETIC INDICATOR (RMI) HAS "OFF" FLAG AND CAPTAIN'S HORIZONTAL SITUATION INDICATOR (HSI) HAS "OFF" FLAG. FLAGS COME IN VIEW INTERMITTENTLY "CONTINOUSLY" AND IN TURNS. NO HEADING MOVEMENT WITH "OFF" FLAGS IN VIEW. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO (DG) IAW MM 34-21-1. OPERATIONS CHECK NORMAL IAW MM 34-21-0. 2L74 4F 4A25 20030228000032003022800003 2003 2 28 HEEA084390 420030212A2300N0001552 ANTENNA BELL 407 407 1182206SW COMMS CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 ANTENNA HAS CORROSION AT COAX CONNECTION. SCRAPPED. 1G71 3U O H2SW 20030303000072003030300007SW 2003 3 3 HEEA084480 120030214A3340212075139001 LANDING LIGHT BELL 412 412 1182202SW EXTERIOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 LANDING LIGHT WILL NOT COME ON. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030310001212003031000121WP 2003 3 10 CALA0300108 120030308A5311 FRAME DOUG DC9 DC982 3022082WP STA 1309 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 INSPECTION FOUND BELTFRAME LOWER CHANNEL AND WEB CORRODED AT STA 1309 FROM LONGERON 28L TO 28R. REPAIRED IAW SRM 53-03, PAGE 04A, FIGURE 2A. 2L72 4F A6WE 20030310001282003031000128EU 2003 3 10 NSVA200300018 120030308A750051533171 SENSOR SAAB SF340 340B 7860101EU INOPERATIVE A NSVAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA27252CJ 340B252 During descent into LGA the right engine bleed air annunicator illuminated. Engine was shut down and emergency was declared. Landing was uneventful. Maintenance removed and replaced the bleed air sensor loop per maintenance manual instructions. Operational check was good. 2L72 4T RTA52EU 20030310001612003031000161NM 2003 3 10 EIA2003026 120030228A5300UNK STRAP BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 Fuselage Right Side Interior, Corrosion along skin longitudinal splices to stringer 12, STA 1740-2240. CORRECTIVE ACTION: Repaired per ECRA 481-53-169-2 Rev A. Removed corrosion per B747 SRM 51-10-01, pgs 13 & 14. Fab'd and installed quadrupler strap per B747 SRM 51-10-02, pg 7. 2L74 4F A20WE 20030313001872003031300187EU 2003 3 13 AALA20030147 120030203A3350321441 POWER SUPPLY AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW2140064 507 JFK - FLT 780 - EN ROUTE SDQ-JFK, EMERGENCY EXIT LIGHTS FLASH INTERMITTENTLY. LANDED JFK WITHOUT INCIDENT. REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030319001052003031900105SO 2003 3 19 C2XA03CL073 120030317A3260852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO LEFT GEAR FAULTY A C2XAK NONE J WARNING INDICATION APAPPROACH 1 SW2715948 145056 CLE FLIGHT# 2052 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS IMMEDIATELY AFTER GEAR EXTENSION BEFORE LANDING.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE LEFT MAIN GEAR AFT WOW PROXIMITY SENSOR.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030320001082003032000108NM 2003 3 20 2003UALA00099 120030128A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 STATION 178 BULKHEAD FORWARD WEB HAS A DENT NEXT TO UPPER RADOME MOUNT ON OUTBOARD SIDE. MAJOR REPAIR ACCOMPLISHED. FILLER AND DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030123000342003012300034NM 2003 1 23 2003UALA00055 120030114A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29951UA 26696 FORWARD NOSE STATION 188, OUTBOARD FRAME CHORD CRACKED JUST ABOVE STRINGER 17R, 1IN BELOW WEB. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED WEB ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030303001822003030300182SW 2003 3 3 HEEA084565 120030214A6210412015300109 BLADE BELL 412 412EP 1182205SW MAIN ROTOR OUT OF BALANCE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03412PH11275 36140 MAIN ROTOR BLADE NEEDS TO BE REBALANCED ACCORDING TO SPECS. 1G72 4U H4SW 20030326000892003032600089NM 2003 3 26 2003UALA00292 120030218A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 STATION 188 LT FUSELAGE FRAME CRACKED IN RADIUS ON AFT SIDE AT WL 208. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED REPAIR ANGLES. 2L72 4F4 FRTA16WE E2GL 20030417001002003041700100NM 2003 4 17 QXEA0300225 120030116A5310 BULKHEAD BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX- FORWARD PRESSURE BULKHEAD DENTED AT RT STRINGER 16. REPAIRED IAW HORIZON AIR EA 6-53-181. 2H72 4T RTA13NM 20030421000112003042100011EA 2003 4 21 QXEA0300256 120030213A2612CN6280052003 FIRE LOOP CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09601QX 10009 PDX ON FLIGHT 2528-SUPP- FIRE SYSTEM FAULT STATUS MESSAGE COMES ON INTERMITTENTLY. REMOVED AND REPLACED RIGHT HAND ENGINE FIRE SENSOR W17 LOOP-A. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030721001442003072100144EU 2003 7 21 MALA030330 120030703A7720 INDICATOR SAAB SF340 340B 7860101EU LT ENGINE FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15437XJ 340B437 DURING FLIGHT 3056, CREW REPORTED LT ITT GAUGE WAS FLUCTUATING. INFLIGHT LEFT ITT GAUGE WENT TO ZERO FOR APPROXIMATELY 2 MINUTES. RETURNED TO NORMAL READING ON ITS OWN. ALL OTHER LEFT ENGINE INDICATIONS WERE NORMAL ENTIRE TIME. AIR RETURN TO MEM. MAINTENANCE PERFORMED FUNCTIONAL CHECK OF LT ITT INDICATING SYSTEM AS PER SAAB AMM 77-20-00-5. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY AT THIS TIME. 2L72 4T RTA52EU 20030422000592003042200059NM 2003 4 22 MEX2003089 120030321A32503800014 VALVE BOEING757 7572Q8 1384972NM NLG STEERING MALFUNCTIONED A ASMFO OTHER F FLT CONT AFFECTED LDLANDING 1 SW23801AM 25624 TIJ-MEX - AFTER LANIDNG IN GROUND TO TURN THE STEERING WHEEL TO THE RT WAS VERY HARD, WITH CODE OF FAIL 32-51-07-04. IN HANGAR NOSE WHEEL STEERING SYSTEM ADJUSTMENT AND TEST WERE PERFORMED IAW MM 32-51-00, TESTS CORRECT. (M) 2L72 4F RTA2NM 20030423001902003042300190NM 2003 4 23 UPS03240292 120030225A3270 YOKE BOEING727 727108C 1384039NM TAILSKID CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C&SI, DURING REMOVAL OF TAILSKID ACTUATOR FITTING, TAILSKID YOKE ASSY FOUND CRACKED. TAILSKID YOKE ASSY REPLACED IAW MM 32-71-41. 2L73 4F A3WE 20040223000332004022300033NM 2004 2 23 AWXA200400018 120031224A53206935365 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND ON CABIN FLOOR INTERCOSTAL AT FLOOR ATTACH SCREW HOLE BS 380 TO BS 400 , BL "0", WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL FROM BS 380 TO BS 400 , BL "0", WL 208; FABRICATED A NEW REPLACEMENT INTERCOSTAL IAW DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, FIG. 3, SHT 1. 2L72 4F RTA16WE 20030730000232003073000023WP 2003 7 30 ABXA030190 120030609A3230 SPACER DOUG DC9 DC931 3022065WP LT MLG WORN A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23941AX 47419 GEAR DOOR OPEN LIGHT AND LEFT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. FOUND LEFT MAIN DOOR LATCH SWITCH ACTUATOR BINDING. REMOVED AND REPLACED SPACER, REINSTALLED SWITCH. PERFORMED GEAR SWING. OPS CHECKED GOOD IAW DC-9 MM 32-10-00. 2L72 4F A6WE 20040301000072004030100007 2004 3 1 KBM2004F00000 420031102A34215040017901 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ATTITUDE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH777 3141 ATTITUDE INDICATOR SHOWS 6 DEGREES RT AND 10 DEGREES DOWN IN LEVEL FLIGHT. REMOVED AND REPLACED WITH SERVICEABLE ATTITUDE INDICATOR. 1G71 3U3 U H9EU E19EU 20030724001092003072400109NE 2003 7 24 DLM90030569 220030621A72614A7119 PUMP DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 2 ENGINE MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27913DN19701 FAAL1293 53393 020017 UPON SHUTDOWN AT GATE LEFT ENG HAD SMOKE AND SOME FLAME AROUND CORE ENGINE IN THE REAR. PERFORMED TS PER AMM 71-09 PG 9, RAN ENG NO FURTHER SMOKE OR FLAME OBSERVED. ALL INSP GOOD PER M/M. MTC STILL IN WORK DUE HISTORY R&I OIL SCAVENGE PUMP. REPLACED ENGINE OIL SCAVANGE PUMP PER AMM CHAPT 79. PERFORMED DRY MOTOR LEAK CHECK AND ENG RUN PER PREFLIGHT HANDBOOK TESTS 1 AND 3, NO SMOKE ON SHUTDOWN. A/C OK FOR SERVICE. 2L72 4F4 FRTA6WE E40NE 20030724001132003072400113EU 2003 7 24 AWXA200300669 120030606A261273040102 FIRE DETECTOR AIRBUS320 A320231 3930325EU NR 2 ENGINE MALFUNCTIONED A AWXAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP28620AW178273691 052 FALSE FIRE WARNING - NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AT GATE WITH BOTH ENGINES SHUTDOWN. MAINTENANCE REMOVED AND REPLACED NR 2 FIRE DETECTION UNIT IAW AMM 26-12-34, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030722000302003072200030NM 2003 7 22 2003F00458 120030310A5754 SKIN BOEING727 727222 1384073NM RT WING SLAT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT RT WING LEADING EDGE ABOVE NR 5 INBOARD SLAT TRACK LEADING EDGE CUTOUT UPPER RADIUS. STOP DRILLED CRACK AT RIGHT WING LEADING EDGE NR 5 SLAT TRACK CUT OUT, AT WING STATION 383. FABRICATED REPARI DOUBLER. ALODINED, PRIMED AND INSTALLED DOUBLER. (M) 2L73 4F A3WE 20030805001072003080500107SO 2003 8 5 SIMA200319708 120030710A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21814AE 145541 ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED TWO REPAIR ANGLES AND SHIMS. REPAIR DONE IAW EMB STATEMENT IC2003-145/2225-A AND SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-24-01 FIGURE 201. (M) 2L72 4F RTT00011AT 20030807000562003080700056EA 2003 8 7 03211708 120030730A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 DURING INSPECTION, THE CREW REPORTED THE AFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE AFT EMERGENCY EXIT LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030902001122003090200112WP 2003 9 2 2003F00394 220030424A7321307080022 FUEL CONTROL LEAR 35 31A 5170531CE GARRTTTFE731TFE73123B WP NR 1 ENGINE CONTAMINATED G L ABORTED APPROACH XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 SO35288FF 2010 108 P99329 AFTER NR 1 ENGINE FLAMEOUT ON APPROACH, FUEL CONTROL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. CONTROL FOUND TO CONTAIN METAL CONTAMINATION. AFTER EVALUATION/DETERMINATION THAT ENGINE-DRIVEN FUEL PUMP WAS SOURCE OF CONTAMINATION,THE ENGINE-DRIVEN FUEL PUMP, FUEL CONTROL, FUEL HEATER, FLOW DIVIDER, AND MANIFOLDS REPLACED. 2L72 4F4 FRTA10CE E6WE 20030904001062003090400106NM 2003 9 4 QXEA200300979 120030812A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX-DURING LIGHTNING STRIKE INSPECTION FOUND BURN MARK AT STRINGER 2 AND 3 AT STATION X49.502 JOINT. REPAIRED IAW Q400 SRM 53-10-31, PG 208 2H72 4T RTA13NM 20030904001792003090400179WP 2003 9 4 AALA20030623 120030503A2120 CLAMP DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW217549A 53031 DFW - FLT 1113 - AFTER TAKEOFF EN ROUTE, DFW-TPA, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. CREW EXTINGUISHED LIGHT. RETURNED DFW AND LANDED WITHOUT INCIDENT. TIGHTENED CLAMP ON DUCT JUST DOWNSTREAM OF RIGHT PACK TEMPERATURE CONTROL VALVE AND ACCOMPLISHED LEAK CHECK. SYTSEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030905001892003090500189NM 2003 9 5 USAA030148 120030803A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US52572 22953 CLT - FOUND SKIN CRACKED THREE PLACES, THREE INCH CRACK 1.5 INCHES FORWARD STATION 727E, 1 INCH CRACK AFT OF 727E, .75 INCH CRACK .375 INCH AFT OF 727E. INSTALLED DOUBLER AND TRIPLER AT STATION 727E AT S24R PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20030723000992003072300099EA 2003 7 23 COMA0360322 120030714A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01971CA16977 7145 FLIGHT 5698 GEAR DISAGREE WARNING DURING APPROACH. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20030825000862003082500086NM 2003 8 25 CALA0300438 120030805A5514 BUSHING BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717640 28901 INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER FORWARD LUG CORRODED AROUND BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW SRM 55-10-10. 2L72 4F RTA16WE 20030825001112003082500111NM 2003 8 25 03230430 120030818A3350 PIN DORNERDO32 DO328300 NM CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27430FJ 3209 DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL RESECURED THE GROUNDING PIN AT 41VPND. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030911000952003091100095WP 2003 9 11 DHL2003873502 120030612A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT WING CENTER L/E FORMER CRACKED 0.250 AT XFS 316.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9,10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911002002003091100200WP 2003 9 11 AALA20030333 120030227A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND STATION 218 INBOARD OF FORWARD LAVATORY TRACK NR 2. SUBFLOOR WEB CRACKED AT NUTPLATE HOLE. INSTALLED DOUBLER TO SUBFLOOR WEB AT STATION 218 INBOARD OF SEAT TRACK NR 2 PER SRM 53-01-00. (M) 2L72 4F A6WE 20030926001392003092600139WP 2003 9 26 EIA2003111 120030829A24322634006106 BATTERY DOUG DC9 DC915F 3022037WP MASTER OVERHEATED A EIAAK NONE MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09915F 47061 ON POST FLIGHT INSPECTION A/C HAD SMOKE COMING FROM E & E COMPARTMENT DRAIN HOLES. REMOVED AND REPLACED BOTH MAIN BATTERIES AND BATTERY CHARGER IAW AMM 24-30-01 AND 24-30-22 OPS CHECK IAW WITH AMM. 2L72 4F A6WE 20030909002552003090900255WP 2003 9 9 AMTA200301016 120030802A5752 SPAR CAP LKHEED1011 10113853 5265020WP LT AILERON DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 FOUND LEFT OUTBOARD AILERON LOWER SPAR CAP HAS ELONGATED FITTING ATTACH HOLES. REPAIRED LOWER SPAR CAP IAW ER/A L10-57R-5262. (M) 2L73 4F A23WE 20031002001442003100200144WP 2003 10 2 MWEA030370 120030911A7931811131 REGULATOR VALVE DOUG DC9 DC981 3022081WP ENGINE OIL SYS INOPERATIVE A MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31803ME 48029 NOTICED ENGINE OIL PRESSURE INCREASED FROM 47 PSI TO 60 PSI. REMOVED AND REPLACED PRESSURE REGULATOR VALVE. 2L72 4F A6WE 20031014001242003101400124NM 2003 10 14 SWAA032168 120030927A5755BAC57302 ATTACH FITTING BOEING737 7373H4 1384600NM RT WING SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C4 CHECK, FOUND NR 5 GROUND SPOILER INBD ACTUATOR SUPPORT LUG BROKEN AT T/E SHELF PANEL ROD. REPAIRED NR 5 GROUND SPOILER PER SWA EA. 2L72 4F RTA16WE 20031020001172003102000117NM 2003 10 20 371PA0031 120031004A3350 STRIP BOEING737 737306 13844BGNM CABIN CONTAMINATED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 EMERGENCY EXIT LIGHTS NOT ALL WORKING. CLEANED AND REMOVED MOISTURE FROM STRIPS AND TRACK. INSTALLED COVER PER MM 33-50-00. 2L72 4F RTA16NE 20031028000022003102800002WP 2003 10 28 MWEA030396 120030926A2797 WIRE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE ELEV CONNECTOR BROKEN A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31810ME 48072 ELEVATOR POWER ON WOULD NOT ILLUMINATE WHEN CHECKED DURING TAXI CHECKLIST, ELEVATOR PUSHED FORWARD TO0 EASY. REMOVED AND REPLACED CONNECTOR, ALSO FOUND BROKEN WIRES, SPLICED IN NEW WIRES. 2L72 4F4 F A6WE E2EA 20031119001202003111900120NM 2003 11 19 2003UALA00749 120031006A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 FUSELAGE STRINGER S-20L DENTED AT BS 1690 LAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040115001342004011500134NM 2004 1 15 DL73S031099 120031216A5330654577646 SKIN BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 THE FUSELAGE SKIN WAS FOUND CORRODED AT THE FWD INBD CORNER OF THE AFT LAV SERVICE DOOR CUTOUT NEAR FS 987 AND STRINGER 27R. THE DAMAGE WAS REMOVED WITH A 4 X 4 INCH CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 087716-14, REV A. 2L72 4F RTA16WE 20040129001762004012900176NM 2004 1 29 DHL200374264 120031123A5310 DOOR FRAME BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, MAIN E&E COMPARTMENT DOOR CUTOUT FWD FRAME CORRODED/EXFOLIATED, 100 PERCENT MATERIAL LOSS BS 424, BL 0 - RBL 5 WL 150. REMOVED FASTENERS FOR ACCESS AS REQUIRED, FABRICATED NEW FWD FRAME IAW B727 SRM 51-30-2, FABRICATED NEW FWD FRAME AT BS 424 BL 0 - RBL-5 WL 150 MAT USED 7075-T6,.040 PO 9912620 DIM 23.75 X 7 INCH IAW B727 SRM 53-10-8 FIG 3 AND 51-40-2. ALODINE AND PRIME IAW B727 SRM 51-10-2, INSTALLED NEW FWD FRAME IAW B727 SRM 51-30-2. 2L73 4F A3WE 20031028000512003102800051EA 2003 10 28 03267691 120030924A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27691BR 7740 DURING INSPECTION THE FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F4 FRTA21EA E15NE 20031107001092003110700109 2003 11 7 AALA20031051 420030916A3445IND7879 DISPLAY BOEING767 767323 1385205NM COCKPIT MALFUNCTIONED A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21372AA 25199 AFW - TCAS DISPLAY UNIT STARTED FLASHING OFF AND ON FOLLOWED BY SMOKE COMING OUT OF IT. REMOVED AND INSPECTED UNIT FOUND INTERNAL CIRCUITRY BURNED. REMOVED AND REPLACED TCAS DISPLAY UNIT. OPS CHECK GOOD. (M) 2L72 4F RTA1NM 20031110001102003111000110 2003 11 10 SWIA200312537 420031020A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS FAULTY A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07215SW3975 3975 120281 CAPTAIN'S AUTOPILOT FAILED IN FLIGHT DURING CLIMB. REMOVED AND REPLACED CAPTAIN'S APC-65B. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030730000632003073000063NE 2003 7 30 ABXA030208 220030610A7200CF680A ENGINE BOEING767 767281 1385109NM GE CF6 CF680A 30025NE NR 2 MALFUNCTIONED A ABXAK NONE E VIBRATION/BUFFET CLCLIMB 1 GL23783AX1414 23016 580185 LEVELING AT FL39 M.8-AIRCRAFT EXPERIENCED AN UNUSUAL VIBRATION IN YAW/SHAKING, WITH A SLAPPING NOISE TO THE RIGHT OF THE COCKPIT. ALL NORMAL WHEN THRUST RETARDED FROM CLIMB THRUST, SOUNDED AND LEFT LIKE A DOOR OR PANEL WAS OPEN. REMOVED AND REPLACED THE NR 2 ENGINE IAW BOEING MM. 2L72 4F4 FRTA1NM E13NE 20040108001232004010800123CE 2004 1 8 KZ52003F00000 120031008A5320504400287877 STIFFENER BEECH 65 65 1152802CE LYC O720 IO720* 41546EA AFT BULKHEAD CRACKED D KZ5RO OTHER O OTHER NRNOT REPORTED 1 GL155079E10256 LF52 INSPECTION REVEALED THE PART TO BE CRACKED BETWEEN RIVET HOLES WHERE STIFFNER WAS ATTACHED TO AFT BULKHEAD. NO FURTHER DAMAGE WAS NOTED AFTER PART WAS REMOVED.(K) 1L72 3O3 O 3A20 1E15 20040113000322004011300032NE 2004 1 13 NACA20030127 220031218A7421 SPARK PLUG DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 1 CYLLINDER CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL0343872163 163 533294 35358 NR 1 ENGINE SHUT DOWN. SUSPECT NR 1 CYLINDER. INSPECTED ALL CYLINDERS FOR CRACKED HEADS, NONE FOUND. REPLACED NR 1 CYLINDER FRONT & REAR SPARK PLUGS. CHECKED GOOD. 2L74 4R4 R A781 5E8 20031117000892003111700089NM 2003 11 17 DHL2003749511 120030920A5320 FLOOR SUPPORT BOEING727 7272J0 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DURING C-CHECK AT FLIGHTSTAR IN JACKSONVILLE, FL., AFT PIT FLOOR SUPPORT FROM STA 950E TO 990 LBL 6 HAS SEVERAL DENTS. REMOVED AFT PIT FLOOR SUPPORT FROM STA 950 E TO 990 LBL 6 IAW B727 SRM 51-30-2. DRILLED NEW FLOOR SUPPORT PO 328319, P/N BAC 1500-6199 DIM. 5 FT 10 INCHES AS PER SAMPLE IAW B-727 SRM 51-20-1. INSTALLED NEW FLOOR SUPPORT IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20031119000332003111900033SO 2003 11 19 LR7A03082 120031009A5312LS3872 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 463 4606 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB3200 FOUND FS 617 LMLG AFT BULKHEAD WEB CRACKED AT RBL 64, WL 180. REPLACED WEB CENTER PANEL IAW SRM SMP 583 51-70 AND DWG 339149. NR 0053. 2H74 4T A1SO 20031119000442003111900044NM 2003 11 19 QXEA200301226 120031007A243051539008B GCU DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09353PH9599 9599 496 NR 1 DC GENERATOR CAUTION CAME ON 35 MINUTES INTO FLIGHT. WOULD NOT RESET IAW CHECKLIST. REMOVED AND REPLACED DC GCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031119000782003111900078WP 2003 11 19 MWEA030415 120031013A5313591140514 LONGERON DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 LONGERON 4 LEFT HAS A CRACK AT STATION 160. -- FABRICATED AND INSTALLED SPLICE AND LONGERON SECTION. 2L72 4F A6WE 20031120000742003112000074NM 2003 11 20 QXEA200301262 120030929A5340 CLIP DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FRAME CLIP IS DAMAGED INBOARD END BEHIND NR 1 SEAT TRACK AT FRAME 291.400 FORWARD SIDE. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040115000062004011500006NM 2004 1 15 03FDEA02021 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 3 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031222000562003122200056WP 2003 12 22 GTIA030952 120031104A5712 RIB DOUG DC9 DC983 3022083WP LT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND LT WING LEADING EDGE CAVITY AT STATION XRS 320 BETWEEN 9TH AND 10TH TRACK FROM INBOARD 2ND RIB FROM INBOARD CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR ANGLE. INSTALLED REPAIR ANGLE. (M) 2L72 4F RTA6WE 20031224000372003122400037WP 2003 12 24 GTIA030944 120031031A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND DENT AT FS 190.5 BETWEEN LONGERONS 26 AND 22L, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED NEW SKIN AND DOUBLERS. INSTALLED NEW SKIN AND DOUBLERS. (M) 2L72 4F RTA6WE 20031223001672003122300167EA 2003 12 23 A6WA200340168 120031111A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31401AW 7280 FOUND FS 300.8, STRINGER 24R, STRINGER HAS .097 INCH HOLE DRILLED THROUGH LOWER EDGE. TRIMMED OUT DAMAGE ON STRINGER 24R AT FS 300.8. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED A FILLER FROM 2024 T3 .063 INCH WVAC PO NR 27603/1 AND INSTALLED IAW WVAC EO 601R-53-4387A. REF AWAC WO55526 MWC31 FOR INSTALL OF DOUBLER. (M) 2L72 4F RTA21EA 20031229000352003122900035SO 2003 12 29 LR7A03099 120031121A5320 INTERCOSTAL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION FOUND RT MLG FS 477 INTERCOSTAL BEAM INBOARD AND OUTBOARD CAPS CRACKED AT RBL 63, WL 200. REPLACED BEAM IAW SRM SMP 583 51-60 & 51-70. NR 2141. 2H74 4T A1SO 20030918000742003091800074EU 2003 9 18 U30A200300024 120030731A27601111A000001 SOLENOID AIRBUS320 A320212 3930322EU ZONE 622 INTERMITTENT A U30AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA17265AV 427 ON GROUND IN CUN AFTER FLT 306 PIT-CUN, SLATS LOCKED AND WTB (WING TIP BRAKES) MESSAGE ON ECAM. CUN MAINTENANCE RESET THE WTB OF THE SLAT SYSTEM ON GROUND IAW AMM TASK 27-80-00-869-060 AND SYSTEM RESET AND OPS CK'D NORMAL. AIRCRAFT RETURNED TO SERVICE. UPON RETURN TO BWI, DURING A "DAILY" CK IN BWI, A BITE CHECK WAS PERFORMED OF THE SFCC (SLAT FLAP CONTROL COMPUTER) & HAD NO FAULTS BUT INDICATED THE RT WTB SOLENOID HAD A SHORT CIRCUIT. MAINTENANCE REPLACED THE RT WTB SOLENOID PER AMM TASK 27-81-51-401 AND OPS CK'D THE SLATS WTB PER AMM TASK 27-81-00-710-001. OPS CK AND LEAK CK OK. 2L72 4F RTA28NM 20030919000282003091900028NE 2003 9 19 NACA20030105 220030807A8530356994 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 17 NR 4 ENG CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F961 961 533265 33553 NR 4 ENGINE SHUT DOWN DUE TO NR 17 CYLINDER LOW COMPRESSION ON PATTERNS. REPLACED NR 17 CYLINDER. OP CHECKED GOOD. 2L74 4R4 R A781 5E8 20031009001222003100900122NE 2003 10 9 IXXA0300059O 220030917A7261 VALVE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3 52039NE OIL PRESSURE MALFUNCTIONED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11728PL 45918 DURING CLIMB NR 4 ENG QTY DROPPED & OIL PRESS ROSE TO 60 PSI, TEMP INCREASED. POWER WAS REDUCED PARAMETERS REDUCED OIL PRESS, OIL TEMP REDUCED 20 DEGREES & OIL QTY INCREASED. OIL PRESS LIGHT NEVER ILLUM & OIL PRESS NEVER DROPPED BELOW 40 PSI. MX REMOVED & INSPECTED NR 4 ENG OIL FILTER. OIL FILTER REPLACED. MX INSPECTED ENG, NO LEAKS. ENG RESERVICED & RUN AT IDLE, NO LEAKS. ENG RUN AT PART PWR FOR 5 MINS, TAKEOFF PWR FOR 5 MINS & CLIMB PWR FOR 5 MINS. QTY CHECK OK, OIL PRESS 57 PSI, INSPECTED OIL PRESS RELIEF VALVE, NO DEFECTS. REINSTALLED VALVE. MX ADJUSTED NR 4 ENG OIL PRESS RELIEF VALVE. IDLE PRESS 39 PSI T/O POWER 52 PSI, SYS LEAK CHECK GOOD. OIL QTY INDICATING SYS OP CHECK OK. 2L74 4F4 F 4A25 1E8 20030923000832003092300083WP 2003 9 23 DHL2003604776 120030529A53403641592N ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FWD ACCESSORY COMPT FITTING ATTACHING FLOORBEAM TO CUSP EXTRUSION AT STA 25.000 L-21R CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-3-0 PG 1. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FITTING IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030923001262003092300126WP 2003 9 23 DHL2003604723 120030525A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT INNER WING UPPER SKIN CORRODED AROUND STA XRS 184.000 BETWEEN CTR SPAR AND S-9R. REMOVED FASTENERS, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED SKIN AREA IAW EODHL-030534, ED-3356. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.125) IAW EODHL-030534, ED-3356. CLEANED, TREATED AND PRIMED DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON RT INNER WING UPPER SKIN AROUND STA XRS 184.000 WITH NEW FASTENERS IAW EODHL-030534, ED-3356 AND SRM 51-1-21 PG 1. FOR LEAK CHECK SEE N/R 3824. 2L74 4F RT4A25 20040128000452004012800045WP 2004 1 28 ABXA030484 120031212A5330591970735 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 FUSELAGE SKIN BULGED AND RIVET PULLED AT STA 1072. REPAIRED AREA IAW DC-9 SRM 53-04. 2L72 4F A6WE 20040128001632004012800163NM 2004 1 28 QXEA200301607 120031219A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX- NR 4 SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11, RD 8-53-4472 AND RD 8-53-1102. 2H72 4T RTA13NM 20040203000312004020300031WP 2004 2 3 ASAA0380563 120030825A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 PREFLIGHT CHECK, FOUND FIRST FIVE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040210000932004021000093EU 2004 2 10 USAA030293 120031122A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH, RBL 17.75 FRAME 59. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040213000202004021300020NM 2004 2 13 2003UALA00983 120031224A5312 BULKHEAD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STA. 178 VERTICAL WEB AT RBL 5.7 HAS TOOLING MARKS IN UPPER SECTION. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20040217001832004021700183SO 2004 2 17 FXTA2003001 120031211A323246933000 IDLER LINK PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR1 GL ACTUATOR FAILED E FXTAO OTHER O OTHER NRNOT REPORTED 1 AL014505222569 318152063 NOSE GEAR COLLAPSED ON ROLL OUT AFTER LANDING. NOSE GEAR IDLER LINK FAILED AT ACTUATOR ATTACH POINT. WE ARE REPLACING ALL THE NOSE GEAR LINKS IN OUR FLEET AS THEY BECOME AVAILABLE FROM MFG. UNTIL THE NEW LINKS ARE AVAILABLE, WE ARE DYE PENETRANT INSPECTING THE LINKS IN USE AND CHECKING THE RIGGING FOR PROPER ADJUSTMENT. 1L72 3O3 O A20SO E14EA 5 CP33EA 20031215000402003121500040NM 2003 12 15 0302056718 120031115A261121561 AMPLIFIER BOEING747 747251F 1384898NM MAIN DECK FAULTY A NWAAO OTHER N FALSE WARNING CRCRUISE 1 GL01618US 21122 DURING CRUISE, THE NR 5 MAIN DECK CARGO SMOKE DETECTION SYSTEM INDICATED A FIRE. THE OVERHEAD CARGO FIRE LIGHT ILLUMINATED AND THE MASTER FIRE WARNING ACTIVATED. VISUALLY INSPECTED CARGO ON MAIN DECK WITH NO SIGNS OF FIRE OR SMOKE. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 5 -A- AND -B- SMOKE DETECTORS AND THE NR 5 SMOKE DETECTOR AMP. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040407000352004040700035NM 2004 4 7 TSAA0353208 120031125A53206545866 LEG ASSY BOEING737 737230 1384401NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. REMOVED ANGLES. FABRICATED A FILLER AND STRAP FROM 7075-T6 PER FIGURE 1. ALODINED AND TWO COATS BMS 10-11 TYPE II PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS AND ANGLES. REPAIR COMPLETED IAW ECO 3295 AND DEVIATION A. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030926000262003092600026NM 2003 9 26 AWXA200300989 120030826A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 1 LT BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28154AW 23776 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 1 LT WAS BROKEN AND PULLED FROM SEAT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 1 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030814000062003081400006 2003 8 14 SWAA031718 420030731A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030819000832003081900083NM 2003 8 19 2003UALA00549 120030709A5313 STRINGER BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 CORROSION IN CENTER OF STRINGER 5L AT STA 1924, LBL 4, WL 92. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20030818000492003081800049EU 2003 8 18 BAQA088669 120030807A2435 BRUSHES UROCOPEC135 EC135T1 5620026EU STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH1352 99732 0131 STARTER GEN HAS BRUSHES WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030819001552003081900155NE 2003 8 19 2003UALA00512 220030619A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 BIRD INGESTION A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29442UA 780 RETURN TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL AND SUBSEQUENT SHUTDOWN. REPLACED ENGINE. DISASSEMBLY OF REMOVED ENGINE REVEALED FRACTURED 3RD STAGE BLADE AS ROOT CAUSE. FURTHER ANALYSIS OF BLADE FRACTURE AREA REVEALED BIRD DEBRIS AS MOST LIKELY SOURCE OF FRACTURE INITIATION. BIRD REMAINS WILL BE SENT TO THE SMITHSONIAN FOR SPECIES IDENTIFICATION, AND DATA ENTERED INTO INDUSTRY FOD DATABASE. 2L72 4F4 FRTA28NM E40NE 20040719002532004071900253NM 2004 7 19 USAA030275 120031204A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 FOUND INTERCOSTAL CRACKED 1 INCH, STATION 660, S16R WIGN SCAN LIGHT INTERCOSTAL. REPAIRED CRACK PER EA 94837. (M) 2L72 4F RTA2NM 20030924001152003092400115SO 2003 9 24 BSY2003F00020 220030722A7414103493504 MAGNETO BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO LEFT INOPERATIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0727MT TH1120 299408R LT ENGINE WOULD ONLY REACH 2000 RPM ON TAKEOFF. FOUND LEFT MAGNETO DEAD. REMOVED AND REPLACED LT MAGNETO. OPS CHECK GOOD. 1L72 3O3 O 3A16 E5CE 20050202001152005020200115NM 2005 2 2 0704025 120030923A575369372098 SUPPORT BOEING737 737230C 1384472NM RT TE FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 RT IB FLAP OB GIMBAL SUPPORT CRACKED. 2L72 4F A16WE 20030815000882003081500088NE 2003 8 15 HEEA088428 120030802A52107620902019048 FITTING SKRSKYS76 S76A 8143006NE CREW DOOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 CREW DOOR FITTING BROKEN. SCRAPPED. 1G72 3U H1NE 20030820000622003082000062NM 2003 8 20 03FDEA01064 120030708A5753ARC41251 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LEFT OUTBOARD FLAP, FOUND 01 EACH CRACK ON NOSE RIB SUPPORT ISLAND, APPROX 0.25 INCH IN LENGTH. REPAIR CARRIED OUT AS PER EA 1-5750-71833 WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR. 2L73 4F RTA22WE 20030820001842003082000184NM 2003 8 20 2003UALA00559 120030715A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 MAIN CABIN FLOORBEAM TOP CAP GOUGED AT BS 340, RBL 28 TO RBL 30. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP WITH SPLICE SECTION, ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030404001332003040400133 2003 4 4 DL76G030098 420030127A23301301394100 MODULE BOEING767 767332 1382001NM CABIN FAULTY A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO271604R 30180 ELECTRICAL ODOR FWD CABIN VICINITY ENT SYSTEM EQUIPMENT. SECURED BOTH UTILITY BUSSES FOR REMAINDER OF FLT. FOUND VCC/VMOD B AD, SHUTDOWN IFE SYS PULLED AND COLLARD VCC C/B 1.2 3.4 5 ON C/B PNL 101 LOWER E/E BAY. NDS VCC P/N 250008689 MFG P/N 1301394-001. PDX FWD TO MCO/PLAC AS PER MEL 25-20-02J. 2L72 4F RTA1NM 20030407000122003040700012WP 2003 4 7 ASAA0380067 120030111A143026R161 DOME NUT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PANEL LANDING HAS CORRODED DOME NUTS AT FS 786. REPLACED DOME NUTS PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20030410000272003041000027NM 2003 4 10 SWAA030605 120030316A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT BROKEN ADJACENT TO AFT ENTRY DOOR. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2L72 4F RTA16WE 20030414000312003041400031NM 2003 4 14 ANCF200300014 120030408A2910271N61192 HOSE BOEING757 757200 1384950NM HYD SYSTEM RUPTURED W ANCFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO23262CT 26246 LT HYD QTY DECREASED DURING FLT. PRESSURE ONLY DECREASED AFTER ENGINES WERE REDUCED FOR DESCENT & THEN PTU BECAME INOPERATIVE. BECAUSE LT QTY IN 0, RT ENG PUMP OVERHEAT LIGHT ON ALSO. FLT RETURNED TO BOGOTA. INSPECTION WAS FOUND MLG DOWNLOCK HOSE RUPTURED. THIS AIRCRAFT HAS ACCOMPLISHED THE SB 757-29-0056, AND REMOVED HOSE HAS PN: 271N6119-2. PTU CONTROL PRESSURE SWITCH WAS FOUND WITH FAULT. MAIN LANDING GEAR DOWNLOCK HOSES WERE REPLACED, PTU FILTER MODULE WAS INSPECTED AND WAS FOUND IN NORMAL CONDITION. PTU AND HYD PRESSURE SWITCHES WERE REPLACED AND TESTED IAW AMM. EDP (LT) WAS REPLACED IAW AMM. "HIGH ENERGY STOP/HEAT DAMAGE CONDITION INSPECTION" WAS PERFORMED IAW AMM WITH NORMAL CONDITION. 2L72 4F RTA2NM 20030416001132003041600113NM 2003 4 16 DL76L030247 120030316A3350 POWER SUPPLY BOEING767 767332 1382001NM EMERGENCY LIGHT DAMAGED A DALAH DEACTIVATE SYST/CIRCUITS L NO TEST ININSP/MAINT 1 SO27188DN 27583 SEAT ROW 1 THROUGH 5 LT & RT EMERGENCY LIGHTS INOP. TROUBLESHOT PER WDM FOUND SEAT 2AB FORWARD FRONT ILLUMINATOR DAMAGED. DISCONNECTED WIRING PLUG AND REMOVED ILLUMINATOR FROM SEAT VERIFIED THAT AFT ILLUMINATOR IS OPERATING NORMALLY, NEEDS 1 EACH ILLUMINATOR MFG P/N 0201991008. FORWARD ILLUMINATOR TO MCO E 514642002 AND PLACARD REF MEL 33-51-03. REPLACED FORWARD LEFT POWER SUPPLY AS PRECAUTIONARY, PERFORMED SATISFACTORY OPERATIONAL TEST OF THE EMERGENCY ESCAPE PATH MARKING SYSTEM PER AMM. 2L72 4F RTA1NM 20030417001482003041700148SO 2003 4 17 SWIA200311759 120030131A2150 BUSHING EMB 120 EMB120ER 3260203SO A/C PACK LACK OF LUBE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07190SW 120050 BOTH AIR CONDITIONING PACKS FAILED IN THE NORMAL POSITION. SMOKE FILLED THE CABIN AND COCKPIT. VERY LIMITED AIRFLOW IN LOW/LOW CONFIGURATION. LUBRICATED LEFT AND RIGHT ACTUATOR PIVOT BUSHINGS, CLEANED OIL FROM CONNECTORS. FREED RIGHT RAM AIR CHECK VALVE FROM OBSTRUCTION. OPS CHECK GOOD. RAN AIR CONDITIONING EXTENSIVELY, NO FURTHER PACK FAILURES NOTED. 2L72 4T RTA31SO 20030423000072003042300007NE 2003 4 23 AUS20030257 220030219A7532 BLEED VALVE BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE COMPRESSOR FRACTURED W C ABORTED TAKEOFF ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 1 ENGINE THIRTEENTH STAGE BLEED VALVE SEPARATED. 2L73 4F4 FRTA3WE E2EA 20030424001822003042400182SO 2003 4 24 LR7A03037 120030313A5343 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5323 FOUND LT FS 517 MLG BEAM INBOARD CAP CRACKED AT LBL 63, WL 265. REPAIRED IAW SRM SMP 583 53-40-17. NR 2238. 2H74 4T A1SO 20030423001592003042300159EU 2003 4 23 MALA030198 120030313A7931IPTE1191000200 TRANSMITTER SAAB SF340 340B 7860101EU OIL PRESSURE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15428XJ 340B428 PROP OIL PRESSURE FLUCTUATING IN GREEN ARK AND PERODICALLY PEGGING HIGH FOR A SECOND, THEN TO GREEN ARK. ALL OTHER PROP INDICATIONS NORMAL. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RT TRANSMITTER POL PRESS ENG/GB/PN OFF AND ON IPTE119-1000-200D1, SN/OFF 3975-3-72/81, SN/ON 5587-2-438 IAW CHP 71, OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA52EU 20031014000072003101400007EU 2003 10 14 BAQA089605 120031002A31501179405207 CONTROL PANEL BOLKMS117 BK117B1 5626012EU ANNUNCIATOR DEFECTIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117US 7175 PANEL WAS JUST REPAIRED UNDER PO 2-021656-01, UNABLE TO RESET MASTER CONTROL WHEN ECS IS ON (THIS IS THE ORIGINAL PROBLEM). UNIT WAS ALSO DAMAGED IN SHIPPING TO JACKSONVILLE FROM AEC (BROKEN MOUNTING TAB). FED EX AIRWAY BILL #6413 5829 9550. PANEL IS PACKAGED THE SMAE WAY IT ARRIVED IN JACKSONVILLE. RENTAL UNIT STILL ON SHIP (S/N 0055) FROM PO 2-021394-03. RENTAL CHARGES SHOULD STOP OCCURING AT THIS TIME SINCE REPAIR AND SHIPPING WAS NOT DONE CORRECTLY. 1G72 3U H13EU 20031014000292003101400029SO 2003 10 14 ENE2003F00000 220030903A8530TIST712ACA CYLINDER HEAD CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO ENGINE FAILED E ENECO OTHER O OTHER NRNOT REPORTED 1 AL038337Q283 U20603198 247849R CYLINDER HEAD FAILED ON TAKEOFF. SUBSEQUENT OPERATION LEAD TO COMPLETE SEPERATION OF HEAD FROM CYLINDER. THIS WAS MINIMAL OPERATION. PROBABLE CAUSE OF FAILURE ARE MATERIAL COMPOSITION, HEAT TREATMENT, AND MACHINING OR CASTING INDUCED WEAKNESSES. 1H71 3O3 O A4CE E5CE 20031124000952003112400095WP 2003 11 24 DHL2003802520 120031114A53203750257U1 SPLICE DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 FWD CARGO COMPT SPLICE FITTING 7.000 CRACK (STA 600.000 - 620.000, L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20031121000702003112100070EA 2003 11 21 COMA0370050 120031111A3020GG670800025 VALVE CNDAIRCL600 CL6002C10 1390015EA AFT EQUIP BAY FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01331CA 10061 FLIGHT 5095 RECEIVED A RT BLEED AND COWL CAUTION DURING CRUISE FLT. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT CVG. REPLACED THE RIGHT ENGINE PRSOV. 2L72 4F RTA21EA 20031125000562003112500056WP 2003 11 25 DHL2003807509 120031007A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 LEFT WING CENTER L/E FORMER CRACKED 0.500 AT XOLDI 6.2246. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10 SRM 51-1-20D PG 9 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040121000152004012100015NM 2004 1 21 03FDEA02271 120031226A5744ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING O/B FLAP O/B HINGE ACTUATOR I/B MOUNT LUG I/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75202, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES- RT OUTBOARD. FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031202000942003120200094NM 2003 12 2 USAA030207 120030924A5315 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 FOUND FLOORBEAM WORN, 1 INCH BY 1 INCH, AT STATION 780, LBL 18. REPAIR ANGLE FABRICATED AND INSTALLED PER EA 94780. (M) 2L72 4F RTA2NM 20031204001122003120400112WP 2003 12 4 UPS03841430 120030923A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, AFT ACCY COMPT FS 1580 FLOORBEAM REPAIR ANGLE IS CORRODED AT RBL 48. REMOVED FLOORBEAM REPAIR, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED NEW REPAIR ANGLE, ALODINED AND PRIMED IAW DC8 SRM 53-2-0 AND 51-1-8 AND INSTALLED ANGLE IAW DC8 SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20031209002162003120900216EA 2003 12 9 SWIA200312566 120031102A27507455001 LEVER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07466SW 7856 FLAPS FAIL MESSAGE CAME ON AFTER TAKEOFF WHEN SELECTING FLAPS 0 TO FLAPS 8. RETURNED TO SLC. REPLACED FLAP CONTROL HANDLE IAW 27-51-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20031014001652003101400165NM 2003 10 14 SWAA032089 120030918A5315BAC1605 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO COMPT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FLOORBEAMS CORRODED AT BS 727, AND BS 727D. REPAIRED BEAMS PER SWA EA. 2L72 4F RTA16WE 20031021001532003102100153NM 2003 10 21 AALA20030601 120030526A3350 SOCKET BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21178AA 32398 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 17D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030917000712003091700071SW 2003 9 17 ALGA089096 120030911A6210406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03409AL381 53494 UNIVERSAL FOUND WORN, BINDING AND RATCHETY. REMOVED AND REPLACED BY FIELD MAINT. 1G71 3U O H2SW 20030918000442003091800044NM 2003 9 18 GAIA03032SP 120030719A5311 FRAME BOEING727 7272J0 138407ENM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS DENTS INTO THE RADIUS BETWEEN STRINGER 15L AND 17L FASI N/R 35752. CUT OUT DAMAGES AREAS, FABRICATED REPAIR DOUBLER, MATERIAL USED 7075-T6 .063 PO NR 9912571 DIM 18.5 INCH BY 6.5 INCH. TWO ATTACH ANGLES P/N BAC1505-100617 PO NR 9912743 DIM 3 INCH BY 3 INCH, INSTALLED REPAIRS IAW B727 SRM 53-10-4. (M) 2L73 4F RTA3WE 20030917000722003091700072EU 2003 9 17 BAQA089045 120030827A77141179405303 INDICATOR BOLKMS117 BK117B2 5626013EU TRIPLE TACH MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA031174U30 7146 REQUEST WARRANTY REPAIR. NR 1 N2 NEEDLE READS 2 PERCENT WHEN POWERED UP. NR 1 N2 NEEDLES READS 100 PERCENT, NR 2 N2 NEEDLES READS 99 PERCENT, AND NR READS 98 PERCENT AT FULL "FLY" RPM. PART ONLY LASTED 29.5 HOURS FROM THE LAST REPAIR. UNIT SENT OUT TO AEC FOR WARRANTY REPAIR UNDER RO:9-090002-19 W/O AN MMIR. JUAN CALLED 9/8/2003 AND ASKED FOR AN MMIR TO BE FILLED OUT. THIS WAS FILLED OUT AND FAXED 9/9/2003. 1G72 3U NCH13EU 20030922000702003092200070NM 2003 9 22 AWXA200300947 120030804A5320D5397470900000 PROFILE AIRBUSA319 A319132 3930340NM CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 63, BETWEEN STR 39 LT AND 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 63, BETWEEN STR 39 LT AND 39 RT; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-9, 12, AND 21-22. 2L72 4F RTA28NM 20030430000652003043000065NM 2003 4 30 USAABB03042 120030312A3260MS25237387AS15 BULB BOEING757 7572B7 1384964NM COCKPIT BURNED OUT A USAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 EA19632AU 27810 PIT - FLT 391 - ON APPROACH, CREW DID NOT RECEIVE A GREEN SAFE INDICATION ON THE RIGHT MAIN LANDING GEAR. NO OTHER ABNORMAL INDICATIONS WERE PRESENT. CREW PERFORMED A GO-AROUND. TOWER CONFIRMED ALL GEAR WERE DOWN. FLIGHT LANDED WITHOUT FURTHR INCIDENT. MAINTENANCE REPLACED THE LIGHT BULB. (M) 2L72 4F RTA2NM 20030430002302003043000230EU 2003 4 30 AWXA200300433 120030425A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28654AW 1050 LAX - AIR TURN BACK - FLT 0081 - ON CLIMB OUT OF LAX EN ROUTE FOR PHX, FLIGHT ATTENDANT REPORTED AN ELECTRICAL BURNING ODOR AT MID CABIN. TURNED OFF GALLEY POWER, NO HELP; DECLARED AN EMERGENCY AND RETURN TO LAX. PILOT ALSO OBSERVED A HOT WAX ODOR IN FLIGHT THAT WAS ISOLATED TO THE NO. 2 AIR CONDITIONING PACK. MAINTENANCE INSPECTED MID CABIN AREA OVERHEAD POWER SUPPLY UNITS, NO ELECTRICAL ODOR WAS DETECTED. RAN BOTH AIR CONDITIONING PACKS TO FULL HOT AND COLD, NO ODORS NOTED. PRIOR TO THIS FLIGHT NUMEROUS SEALS WERE REPLACED ON BOTH AIR CONDITIONING PACKS, SUSPECT WAX FROM SEALS MAY HAVE PRODUCED BURNING ODOR. 2L72 4F RTA28NM 20030505002332003050500233WP 2003 5 5 UPS03840449 120030412A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C1 TWO STOP DRILLED HOLES ON OUTER SKIN AT STA 400 LONG 30R. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030507000672003050700067WP 2003 5 7 CA030411002 120030408A2820369H81443 SWITCH HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL FUEL BYPASS CRACKED W O OTHER L NO TEST NRNOT REPORTED 1 CA (CAN) FUEL BYPASS SWITCH REMOVED FOR TESTING AND FOUND TO BE UNSERVICEABLE DUE TO ELECTRICAL MALFUNCTION. UPON FURTHER INSPECTION IN COMPONENET SHOP THE END FITTING BASE WAS FOUND TO BE CRACKED 1G71 3U3 U H3WE E4CE 20030513001002003051300100NM 2003 5 13 AWXA200300503 120030420A533065558721 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND ON INNER SKIN AT R-2 DOOR HINGE CUTOUT, AFT OF CABIN WINDOW AT BS 950. MAINTENANCE CUTOUT CRACK ON INNER SKIN AT R-2 DOOR HINGE CUTOUT BS 950; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5311-03114-ES3. 2L72 4F RTA16WE 20030513001332003051300133NM 2003 5 13 DL738030388 120030426A3260ADH3721R SWITCH BOEING737 737832 13844CFNM NLGWW MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO273745B 32373 AFTER T/O RAISED LANDING GEAR AND NO GEAR CAME UP. SOUNDED LIKE POSSIBLE LOOSE TREAD. WITH HANDLE UP ALL 3 RED AND ALL 3 GREEN LTS ON. LOWERED HANDLE. ALL 3 LIGHTS IMMED WENT GREEN. NORMAL LANDING AT 146.2 REPLACED ALT GEAR EXT HANDLE DOOR SWITCH AND ACTUATOR PER MM 32. JACKED A/C FOR GEAR SWING. GEAR OPS NOW CHECKS GOOD. RESTORED A/C TO NORMAL. INSTALLED PRESSURE PANEL IN NOSE W/W. LDG WEIGHT BELOW MAX LDG WEIGHT. NO ACTION REQUIRED. 2L72 4F RTA16WE 20030514000552003051400055NM 2003 5 14 SWAA030978 120030428A5315654680977 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, RBL 15. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030514000402003051400040EU 2003 5 14 YENA200306 120030427A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15556JB 1904 A LOW LEVEL INTERMITTENT ALARM HEARD DURING ROLL OUT 5-7 SEC, A STRONG ELECTRICAL ODOR. SHOWED CREW REGARDING THE COCKPIT DOOR ENTRANCE DEY PAD THAT IF A BUTTON IS PUSHED, THE NOISE HEARD IS SAME BUT LOWER TONE. PERFORMED OPS CHECK OF COCKPIT DOOR, SYS OPS CHECK GOOD. UNABLE TO DUPLICATE. INSPECTED COCKPIT AREA & INSTRUMENTS, FWD & MAIN E/E BAY. NO SIGN OF DEFECT OR ODOR FROM ELECTRICAL BURN. CHECKED PACKS FOR POSSIBLE CAUSE, NO FAULT. TOOK A/C OUT FOR HIGH POWER RUN. TRANS ELECTRICAL SEVERAL TIMES, NO SYS DEFECT NOTED. INSPECTED ENTIRE LIVE TV SYS, NO FAULT NOTED. DUE TO LTV AFT BAY SMOKE DETECTOR ALARM TONE SIMILAR TO COCKPIT KEY PAD INSPECT SYS WITH NO FAULT NOTED. SYSTEM OPS CHECK GOOD. 2L72 4F RTA28NM 20030515000692003051500069EA 2003 5 15 SWIA200311923 120030428A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07909SW4371 4371 7558 AFTER TAKEOFF AND CLIMBING THROUGH 500 FT AGL, THE STAB CH1 INOP MESSAGE ILLUMINATED. RAN QRH PROCEDURE. MESSAGE PERSISTED. INSTALLED SERVICEABLE HORIZONTAL STABILIZER ACTUATOR IAW MM 27-42-01 AND RII 27-415. OPS CHECK GOOD. NO DEFECTS NOTED. ALSO INSTALLED SERVICEABLE MOTOR CONTROL UNIT IAW MM 27-42-05. OPS CHECK GOOD. NO DEFECTS NOTED. ALL PANELS CHECKED AND SECURED. MCU P/N: 706-3, S/N OFF: 218. 2L72 4F RTA21EA 20030527000642003052700064WP 2003 5 27 AALA20030389 120030331A3350 LIGHT DOUG DC9 DC982 3022082WP ROW 20 INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217541A 49995 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT ROW 20 INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030528000262003052800026 2003 5 28 BAQA085970 420030415A3400066304607 INDICATOR AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL NAVAGATION PRECESSES E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01911KY112 5101 UNIT PRECESSES BADLY AT TIMES. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H11EU E4CE 20030602001272003060200127NM 2003 6 2 SWAA031165 120030524A52416547952 SKIN BOEING737 7372H4 138448CNM FWD SVC DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR OUTER SKIN CRACKED. REMOVED AND REPLACED FWD SVC DOOR PER MM. 2L72 4F A16WE 20030604000132003060400013EA 2003 6 4 A6WA200340067 120030513A5753 VANE CNDAIRCL600 CL6002B19 1900309EA TE FLAP CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 FLAP VANE HAS A CHAFE APPROX .004 INCH DEEP BLENDED DAMAGED AREA IAW WVAC EO 601R-57-3998. (M) 2L72 4F RTA21EA 20030604001792003060400179NM 2003 6 4 UPS03440599 120030412A575365B106252 RIB BOEING747 747121 1384871NM NR 23 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT WING - NR 23 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1 TO 8. ( VIEW FROM I/B ) BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND EO B747-5740-18687-A. 2L74 4F A20WE 20030514001072003051400107NM 2003 5 14 SWAA031008 120030506A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 384 AT STR 15R, BS 450 AT STR 17R & BS 460 AT STR 26L. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20030606000182003060600018NM 2003 6 6 03FDEA00756 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHING POINT, I/B FWD BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030606000302003060600030NM 2003 6 6 03FDEA00732 120030515A5330 TRIPLER BOEING727 727200 138407ENM FUSELAGE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25258FE 20940 COMPLY WITH E.A. 7-5330-70385 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR. FACT 15MAY03 21:19 BFM U COMPLIED WITH E.A. 7-5330-70385 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR. 2L73 4F RTA3WE 20030521000772003052100077WP 2003 5 21 DHL2003804900 120030125A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING CTR L/E FORMER UPPER PART AT STA XFS 347.750 WITH 1.000 INCH CRACK. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9 - 10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER ANGLE INNER SIDE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AND NEW FASTENERS IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20030521001372003052100137WP 2003 5 21 DHL2003801038 120030415A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT WING - CTR L/E FORMER WITH 2.000 INCH CRACK IN STA XFS 310.250. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (7075-T6 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030520001452003052000145CE 2003 5 20 2003F00274 120030412A2131 CONTROLLER LEAR 60 60LEAR 5170707CE CABIN PRESSURE MALFUNCTIONED A UG8AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23699DA 237 CABIN PRESSURE CONTROLLER MALFUNCTIONING IN AUTO MODE. AIRCRAFT ABORTED ITS TAKEOFF. DEFER PER MEL SECTION 21-1. MO410-1, AFL NR 00817. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA10CE 20030523000152003052300015EA 2003 5 23 2003F00296 120030506A3297601577889 HARNESS CNDAIRCL600 CL6002B16 1900305EA NOSE GEAR ERRATIC A O2GAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NE03601BE4230 5103 TAKING OFF FROM ORH, THE LANDING GEAR WAS RETRACTED, LANDING GEAR RETRACTED BUT THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. LANDING GEAR WAS EXTENDED AND A SAFE INDICATION WAS PRESENT, 3 GREEN AND NO NOSE GEAR LIGHT. GEAR REMAINDER OF FLIGHT. AIRCRAFT LANDED WITOUT FURTHER INCIDENT. FOUND HARNESS ERRATIC AND IT WAS REPLACED. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20030610001202003061000120SW 2003 6 10 HEEA087017 120030604A6230406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH3251 53038 DISSIMILAR METAL CORROSION DUE TO STAINLESS STEEL BUSHING IN ALUMINUM CASTING. 1G71 3U O H2SW 20030611000632003061100063EA 2003 6 11 CA030516001 120030515A2710 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE AILERON JAMMED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) SHORTHLY AFTER TAKE OFF THRU FL250 THE AILERON SYSTEM JAMMED, FLIGHT CREW SUSPECTED ICE AS THERE WASHEAVY RAIN WHILE DEPARTING, THE FIRST OFFICER SIDE WAS AFFECTED, PILOTS SIDE WAS OK (AFTER CONTROL COLUMN DISCONNECT INVESTIGATION UNDERWAY, 2L72 4F4 FRTA21EA E15NE 20030613000582003061300058NM 2003 6 13 UPS03440792 120030510A5340 FITTING BOEING747 747200 1384847NM LT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, LT MLG W/W STA 1480 CUTOUT PNL O/B OF O/B TRUNNION FITTING AREA FOUND CORRODED AT ACCESS PANEL AREA. CORROSION BLEND OUT (0.030 X 1 X 3 INCH) BULKHEAD WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F RTA20WE 20030613001212003061300121NM 2003 6 13 SWAA031196 120030529A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND 3 EA STRINGER SPLICES CRACKED AT BS 908, STRINGERS 10R AND 4L, AND BS 817 TO BS 847, STRINGER 4L. REPAIRED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030612001402003061200140WP 2003 6 12 UPS03840729 120030503A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, AFT CARGO PIT RT TUNNEL FUSELAGE SKIN AND L22R REPAIR NOT PER SRM STA 1230-1240 L22R-L21R. REMOVED OLD DOUBLER AND LONG AND SPLICE FABBED NEW DOUBLER, TRIPLER, LONGERON SECTION. INSTALLED DOUBLER, TRIPLER, LONGERON SECTION LONGERON SPLICE, END FITTING IAW DC8 SRM 53-2-2 & 51-1-20D. 2L74 4F RT4A25 20030529000382003052900038NE 2003 5 29 HEEA086502 120030520A26127630607902101 FIRE DETECTOR SKRSKYS76 S76A 8143006NE NR 2 ENGINE SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322342 760096 NR 2 ENGINE FIRE WARNING LIGHT CAME ON IN FLIGHT. MAINTENANCE FOUND NR 2 ENGINE FORWARD FIRE DETECTOR SHORTED. 1G72 3U H1NE 20030620000772003062000077NM 2003 6 20 USAA030073 120030410A5320654580730 SUPPORT BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 PIT - FOUND ANGLE SUPPORT CRACKED .5 INCH, AT UPPER SIDE OF STRINGER 13R AT STATION 291.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2L72 4F RTA16WE 20030707001132003070700113CE 2003 7 7 JAFA65SA01 120030626A2612 FIRE DETECTOR CESSNA500 500CESSNA 2076602CE PWA JT15 JT15* 52060NE LT ENGINE CHAFED G JAFAO OTHER N FALSE WARNING CRCRUISE 1 GL1965SA 6861 5000114 PCE76278 LEFT ENGINE FIRE WARNING LIGHT FLICKERED ON INTERMITTENTLY. INSPECTION FOUND LOOP CHAFING AGINST OTHER WIRING AND TUBING ON THE ENGINE AND A MINOR LEAK IN A BLEED AIR LINE COUPLING. 1L72 4F4 T A22CE E1NE 20030708000352003070800035WP 2003 7 8 UPS03840896 120030603A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C3 LONGERON 17L AND FWD END FITTING CRACKED AT BS 1768 REMOVED LONGERON 17L AND END FITTING LOCATED AND DRILLED LONGERON AND END FITTING IAW SRM 51-1-24. REMOVED AND INSTALLED HYDRAULIC CASE AND LINES AT STA 1768 IAW MM 20-12-00. INSTALLED LONGERON AND END FITTING IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20030707001792003070700179EU 2003 7 7 AWXA200300746 120030612A5320D5397470700000 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT (SEALING PROFILE) AT FR 58, Y-25. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED CORRODED FLOOR SUPPORT AT FR 58, Y-25; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-8, 10, 12, FIG. 2 AND 3. 2L72 4F RTA28NM 20030710000972003071000097NM 2003 7 10 DHL2003721006 120030616A2613 CONNECTOR BOEING727 727228 1384083NM OVERHEAT DETECT DAMAGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01721DH 19545 LOWER AFT BODY HEAT HAS NO TEST FUNCTION. TRANSFERRED TO DMI 13272 MEL 26-10-2 CAT C. PLACARD INSTALLED SP 26-10-2 COMPLIED WITH. REF DMI 13272 LOWER AFT BODY HEAT. REMOVED AND CLEANED CONNECTORS ON BOTH ENDS OF DETECTOR. RE-INSTALLED, OPS CHECKED GOOD. THIS CLEARS DMI 13272. 2L73 4F RTA3WE 20030711000022003071100002NM 2003 7 11 DHL2003727005 120030603A3234 HANDLE BOEING727 727228 1384083NM MLG LACK OF LUBE A DHLAO OTHER WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01727DH 20204 AFTER TAKEOFF LANDING RETRACTION DID NOT INDICATE NORMALLY, ALL GREEN AND ALL RED LIGHTS ON FORWARD PANEL WERE ILLUMINATED. ON S/O PANEL TAIL SKID AND R GEAR DOOR LIGHTS WERE ILLUMINATED, L GEAR DOOR LIGHT WAS NOT ILLUMINATED. FOUND HANDLE STIFF TO PULL OUT AND GO THROUGH OFF POSITION. LUBED HANDLE AND PERFORMED GEAR SWING PER B-727 M/M 32-32-0. OPS CHECKED GOOD THROUGH SEVERAL CYCLES. NO FURTHER DEFECTS NOTED. 2L73 4F RTA3WE 20030710001392003071000139EU 2003 7 10 MALA030309 120030607A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15505XJ E2313 DURING C-CHECK IN CVG, FORWARD CARGO BAY FLOOR SUPPORT ANGLES AT FRAME 21, FR 22, AND FR 23 WERE CORRODED BEYOND LIMITS AND REQUIRED REPLACEMENT PER SRM. REF 409 NR 127723, 24 AND 25 FOR DETAIL. 2H74 4F RTA49EU 20030116002012003011600201SW 2003 1 16 HEEA083116 120030108A6700 BEARING BELL 206 206B3 1181506SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 ROTORCRAFT FLIGHT CONTROL BELLCRANK HAS A WORN BEARING. IN SHOP REPAIR. 1G71 3U H2SW 20030107000132003010700013NM 2003 1 7 C8GA20030001 120030104A7931ST104Z TRANSMITTER BOEING727 727227 1384078NM ENGINE INOPERATIVE A C8GAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO15894274150 21365 Flt 738 from TOL to MTY. On take off roll, #1 engine oil pressure dropped to 30 psi. Temperature and quantity OK. Aborted take off and returned to gate with no further incidents. Found #1 engine oil pressure transmitter inoperative. Replaced transmitter. Ops and leak check good. Aircraft returned to service. 2L73 4F A3WE 20030127000012003012700001SW 2003 1 27 HEEA083564 120030113A6330206033505101 ARM BELL 206 206L3 1182108SW NODAL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038590X 51494 TRANSMISSION NODAL ARM ASSY HAS CORROSION AT ATTACH POINT. REPAIRED. 1G71 3U H2SW 20030128000752003012800075SW 2003 1 28 HEEA083829 120030116A6300406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH2493 53401 MAIN ROTOR LEVER ASSY WORN. 1G71 3U O H2SW 20030129000412003012900041SW 2003 1 29 HEEA083954 120030117A6420 BEARING BELL 407 407 1182206SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53400 53003 WORN FEATHERING BEARING. REPAIRED. 1G71 3U O H2SW 20030129000622003012900062SW 2003 1 29 HEEA083976 120030117A6320407040624101 LINE BELL 407 407 1182206SW MRGB OIL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 MAIN ROTOR GEARBOX OIL LINE CORRODED UNDER B-NUT SLEEVE. 1G71 3U O H2SW 20030328000822003032800082EA 2003 3 28 COMA0360058 120030128A5553601R55310025 BUSHING CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01967CA16115 7134 DURING LUBRICATION OF HORIZONTAL STABILIZER PIVOT POINT, THE VERTICAL STABILIZER RT FITTING WAS FOUND TO HAVE BUSHING MIGRATED.PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING ON VERTICAL STABILIZER RT FITTING, FABRICATED BUSHING PN 601R55310025 FROM BUSHING PN 601R55310025 AND INSTALLING FABRICATED I/A/W CRJ REO 601R5531043. 2L72 4F RTA21EA 20030207001102003020700110NM 2003 2 7 03FDEA00069 120030122A5311 FRAME BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 AFT CARGO BAY UPPER FRAME FLANGE PUNCTURED, STA 1130 RBL 21. REPAIRED PUNCTURED FRAME IAW SRM 53-10-1. 2L73 4F4 F A3WE E2EA 20030212000862003021200086NM 2003 2 12 CALA0300037 120030211A5320 STIFFENER BOEING737 7373Q8 1384670NM STA 1121 BENT A CALAK NONE O OTHER ININSP/MAINT 1 SW0914384 26313 INSPECTION FOUND FUSELAGE SECTION 48 HORIZONTAL STIFFENER BENT AT STA 1121, LBL 24. REPAIRED IAW SRM 51-70-11. 2L72 4F RTA16WE 20030214000532003021400053WP 2003 2 14 ASAA0380033 120030104A53455952421503 FITTING DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, G-1 GALLEY LOWER INBOARD MOUNT FITTING IS CORRODED. REPLACED FITTING PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20030214000642003021400064WP 2003 2 14 ASAA0380045 120030105A532199366013 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL HAS DAMAGED EDGE. REPLACED PANEL PER SRM 53-05 AND 51-10-4. (M) 2L72 4F RTA6WE 20030221000512003022100051EU 2003 2 21 AWXA200300078 120030127A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 221 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28648AW19845 770 PHX - EEL - DURING INSPECTION THE EMERGENCY LIGHTS FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (10WL) FORWARD LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030303000052003030300005SW 2003 3 3 HEEA084478 120030214A7921 SEAL BELL 412 412 1182202SW COOLER TUBE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032149S 36002 EXCLUDER SEAL LEAKING DUE TO ROD WORN IN SEAL AREA. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030306000712003030600071SW 2003 3 6 HEEA084782 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 STEP ACTUATOR WILL NOT STOW COMPLETELY. 1G72 4U H4SW 20030306000912003030600091NM 2003 3 6 PCAA0303050 120030303A291082970010445 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003NM LEFT LEAKING A PCAAK NONE K FLUID LOSS APAPPROACH 1 EA13982HA 380 SYR-FLIGHT#3963. CREW REPORTED THAT THE #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED AFTER GEAR EXTENSION. 1.4 QUARTS REMAINING IN #2 SYSTEM. MAINTENANCE REPLACED A HYDRAULIC LINE IN THE LEFT WHEEL WELL IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 MAINTENANCE MANUAL CHAPTER 29-00-00. LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030306001172003030600117EA 2003 3 6 03064648 120030305A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27648BR 7406 DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT THE LT AFT EXTERIOR, AND THE SERVICE DOOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE SERVICE DOOR LIGHT AND THE POWER SUPPLY FOR THE EXTERIOR EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030121000282003012100028SW 2003 1 21 HEEA083220 120030108A7120206064107109 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 ENGINE MOUNT LEG ASSY HAS A WORN BEARING. SCRAPPED. 1G71 3U H2SW 20030317000642003031700064NM 2003 3 17 03FDEA00201 120030304A5311 FRAME BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 DENTED FRAME BS 950E, LBL 31, WL 150. DENT IN FRAME AT B.S. 950E, LBL 31, WL 150 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED FABRICATED U CHANNEL IAW EA 7-5310-69418 AND ER 03-1450 . 2L73 4F4 F A3WE E2EA 20030320000162003032000016NM 2003 3 20 USAABB03020 120030210A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW1 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19611AU 27123 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030320001092003032000109NM 2003 3 20 2003UALA00100 120030127A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 FRAME AT STATION 867 ABOVE STRINGER 9R CRACKED OUT OF FASTENER HOLE FOR BRACKET SUPPORT FOR AIR GRILL RAIL. MAJOR REPAIR ACCOMPLISHED. INSTALLED FABRICATED J-ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030327000582003032700058NM 2003 3 27 C1HA200383004 120030228A2612 FIRE LOOP BOEING727 7272S7 138407ZNM NR 1 ENGINE OUT OF POSITION A C1HAO OTHER N FALSE WARNING CRCRUISE 1 GL15683CA 22490 ENGINE NR 1 FIRE WARNING GROUND FAULT DETECTOR LIGHT ILLUMINATED IN FLIGHT ,PERFORMED ENGINE FIRE WARNING TEST PROCEEDURE COM 2,26.31 TESTED NORMAL. LIGHT REMAINED ON UNTIL DECENT INTO MSP. REPOSITIONED FIRE LOOP IN MULTIPLE AREAS OF POSSIBLE FAULT AREAS NR 1 ENGINE GROUND FAULT DETECTOR LIGHT REMAINS OUT OK FOR SERVICE 2L73 4F A3WE 20030321000452003032100045NM 2003 3 21 CALA0300125 120030320A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT NUTPLATES ON FORWARD FLANGE AT STA 328, RBL 15 TO RBL 23. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, PAGE 205, 51-20-01, AND 51-40-02. 2L72 4F RTA16WE 20040324000242004032400024WP 2004 3 24 ASAA0380721 120031111A533059114003 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND NOSE WHEELWELL LEFT AFT DOOR AFT HINGE CUTOUT OUTER SKIN IS CRACKED. STOP-DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-05. (M) 2L72 4F RTA6WE 20030723000632003072300063NM 2003 7 23 TSAA0353137 120030505A5330 SKIN BOEING737 73725A 1384481NM FUSELAGE DENTED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DENT DISCOVERED AT BS 376 ALONG STRINGER 17 LT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 1. (M) 2L72 4F RTA16WE 20030422000152003042200015EA 2003 4 22 ASOA03057 120030213A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 FLT 4418 - DURING A GROUND INSPECTION IN ATL, THE FLOOR EMERGENCY LIGHTS FROM ROWS 1-5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY FLEX LAMP STRIP FROM ROWS 2-5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030827001842003082700184GL 2003 8 27 C2XA03IA085 220030822A7260 TOWERSHAFT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 ENGINE DAMAGED A C2XAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SW27129227523 34 145338 CAE311160 ACFT N12922, FLT NR 2962 (BTV - CLE) DURING CLIMB-OUT THROUGH 18,000 FT, THE NR 2 ENGINE SHUTDOWN UNCOMMANDED. THE CREW WAS UNABLE TO RESTART. ACFT DIVERTED TO SYR AND LANDED SAFETY. MECHANICS WERE DISPATCHED TO ACFT. INITIAL FINDINGS INDICATE METAL ON THE OIL TANK MAG PLUG, WITH NO EVIDENCE OF EXTERNAL DAMAGE OR LEAKAGE. UPDATE 8/27/03 - THE ENGINE WAS INTERNALLY INSPECTED AND DAMAGE WAS FOUND ON THE TOWER SHAFT GEAR. THE ENGINE WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20030331001372003033100137NM 2003 3 31 DHL2003740518 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH FUSELAGE FRAME AT STA 580 IS DENTED AND CRACKED BETWEEN STR 16R-17R. REMOVED DAMAGED AREA, NO CRACK FOUND. FABRICATED REPAIR PART FROM 7075-T6 .063 AL PER SRM 51-40-3. TREATED, PRIMED AND INSTALLED PER SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20030407000222003040700022WP 2003 4 7 ASAA0380077 120030113A5310995577961 ACCESS PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, ACCESS PANEL BENEATH SEAT IN COCKPIT IS BENT AND TORN. INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F RTA6WE 20030410000482003041000048WP 2003 4 10 GTIA030091 120030129A5310 BEAM DOUG DC9 DC981 3022081WP CARGO DOORWAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND AFT CARGO PIT CORROSION, BARE METAL AND CRACKED SEALANT ALL ALONG INBOARD FRAME AT DOOR JAMB BEAM. REMOVED DOOR JAMB BEAM. LOCATED AND DRILLED NEW AFT CARGO DOOR BEAM. INSTALLED AFT CARGO DOOR JAMB BEAM. (M) 2L72 4F A6WE 20030414000202003041400020NM 2003 4 14 SWAA030735 120030401A531065C27314 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 727, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20030410002312003041000231 2003 4 10 BAQA085196 420030320A34215040017926 GYRO BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101750B1 41560NE ATTITUDE INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA031174U2752 7146 SKEWED 8 DEGREES TO THE LT WHEN SPOOLED UP. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 UNCH13EU E5NE10 20030415000792003041500079NM 2003 4 15 CA030328005 120030227A5330 SKIN BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA 54897 (CAN) FUSELAGE SKIN CRACK APPROXIMATELY 3 INCHES IN LENGTH BETWEEN BS 767+10 AND BS 787 - STR 17 LT REPAIR IAW 737-200 SRM 53-30-3 FIG.1. 2L72 4F4 F A16WE E2EA 20030416000152003041600015WP 2003 4 16 UPS03840000 120030107A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01798UP 45898 INSPECTION TYPE: PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECK'S GOOD IAW MM 33-50-01. S/N ON 10886, S/N OFF 348. 2L74 4F RT4A25 20030416000242003041600024EA 2003 4 16 SWIA200311683 120030107A274070607 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07906SW 7510 ON DESCENT INTO SMF, RECEIVED AN AP PITCH TRIM CAUTION MESSAGE AND A STAB TRIM 1 STATUS MESSAGE. COMPLIED WITH QRH AND RECONNECTED STAB TRIM NR 1. AFTER 5 MINUTES THE MESSAGE REOCCURED. RETURNED TO LAX. REPLACED HSTCU WITH SERVICEABLE UNIT. OPS CHECK GOOD AT THIS TIME. S/N OFF: 846. 2L72 4F RTA21EA 20030417001072003041700107NM 2003 4 17 PCAA0302035 120030204A3297 WIRE DHAV DHC8 DHC8102 2809003NM MLG LOOSE A PCAAO OTHER N FALSE WARNING LDLANDING 1 EA13806EX 263 LGA-FLIGHT 3800 CREW REPORTED THAT UPON GEAR DOWN SELECTION RECEIVED THREE RED GEAR LIGHTS. GEAR HANDLE WAS CYCLED ONE TIME AND RECEIVED THREE LIGHTS. ALTERNATE EXTENSION WAS PERFORMED. MAINTENANCE TESTED GEAR HANDLE SOLENOID AND FOUND IT OPERATED NORMALLY. A LOOSE WIRE WAS FOUND ON LANDING GEAR INHIBIT SWITCH. THE LOOSE WIRE WAS RE SECURED. A TEST FLIGHT WAS PERFORMED TO CHECK LANDING GEAR EXTENSION AND RETRACTION SYSTEM. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030428000332003042800033WP 2003 4 28 GTIA030178 120030304A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 LBL 9 LBL 13 FLOOR SUPPORT CORRODED. FABBED NEW FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030428000492003042800049NM 2003 4 28 OZIA200341003 120030117A5230001A535A6027200 FITTING DORNERDO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR LATCHGOUGED A OZIAK NONE O OTHER ININSP/MAINT 1 CE05410Z 7126 3125 FOUR EACH CARGO COMPARTMENT LATCH FITTINGS HAVE VARIOUS DEGREES OF GOUGE DAMAGE. 2H72 4T4 FRTA55NM E35NE 20030425000602003042500060SW 2003 4 25 TU32003F00006 120030318A6330222010500109 MOUNT BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL MAIN ROTOR WORN B TU3RO OTHER O OTHER NRNOT REPORTED 1 WP07303PS771 23016 ATTACHING END OF FLEXTURE WORN AND NEEDS BUFFER PAD REPLACED. 1G72 3U3 UNCH9SW E1GL 20030428000402003042800040WP 2003 4 28 GTIA030166 120030223A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO STA 148 LBL 8 INCHES CORRODED ON TRACK. REMOVED FLOOR SUPPORT STA148 TI 200 LBL 8. FABRICATED NEW TRACK. INSTALLED FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030429001062003042900106SO 2003 4 29 C2XA03SH103 120030413A531014522226003 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV - DURING C-CHECK, THE CENTER BUTT STRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030428001792003042800179EA 2003 4 28 COMA0360187 120030407A3230 DRAG BRACE CNDAIRCL600 CL6002B19 1900309EA NLG LACK OF LUBE A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01940CA 7048 FLIGHT 5756 GEAR DISAGREE WARNING, NLG DID NOT RETRACT. LUBRICATED THE NLG DRAG BRACE, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20030827001312003082700131NM 2003 8 27 CALA0300403 120030721A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO PIT INTERCOSTAL AT STA 520, LBL 48. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 2L72 4F RTA16WE 20030828001912003082800191NM 2003 8 28 CALA0300447 120030807A3260 SENSOR BOEING737 737524 1384721NM RT MLG OUT OF ADJUST A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2716617 27330 THE CREW WAS UNABLE TO RAISE THE GEAR AFTER TAKEOFF. THE GEAR HANDLE WAS IN THE OFF POSITION WITH THREE GREEN AND THREE RED INDICATION LIGHTS. THE AIRCRAFT WAS RETURNED TO EWR. TROUBLESHOOTING FOUND THE RIGHT MAIN GEAR SAFETY SENSOR OUT OF ADJUSTMENT. THE SENSOR GAP AND TELEFLEX CABLE WERE ADJUSTED IAW MM 32-09-01. A GEAR SWING WAS PERFORMED AND ALL OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20030722001002003072200100WP 2003 7 22 DHL2003806011 120030706A2611327 LAMP DOUG DC8 DC873F 302199FWP SMOKE DETECTOR BURNED OUT A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01806DH 46002 NR 2 SMOKE DETECTOR WILL NOT TEST. ENTERED ON DMI 13448 AS PER DHL MEL 26-6-2 CAT C PLACARD INSTALLED. REF DMI 13448 - NR 2 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 2 SMOKE DETECTOR PER DACO 26-10-5. OPS CHECKED OK. THIS CLEARED DMI 13448. PLACARD REMOVED. 2L74 4F RT4A25 20030723000682003072300068NM 2003 7 23 SWAA031465 120030703A5312956440 STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD STRAP CRACKED AT BL 0, WL 175 TO WL 242. REPAIRED STRAP PER SRM. 2L72 4F RTA16WE 20030801000122003080100012WP 2003 8 1 GTIA030517 120030620A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FORWARD CABIN SUBFLOOR CORRODED AT FLOOR SUPPORT LBL 9 STAITON 160 TO 200 AND HAS A PINHOLE FROM SCREW STATION 168. CUTOUT FLOOR WEB. FABRICATED NEW WEB. FABRICATED SPLICE. INSTALLED FLOOR WEB. INSTALLED SPLICE REPAIR. (M) 2L72 4F A6WE 20030805000772003080500077EA 2003 8 5 ASOA03350 120030713A532060034017351 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURING HANGAR MAINTENANCE AT CKB, THE CHANNEL AT FS 280 BETWEEN RBL AND LBL 9 WAS FOND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CHANNEL ANGLE IAW SRM 51-42-13. (M) 2L72 4F RTA21EA 20030903001312003090300131WP 2003 9 3 WX030008 120030713A2497 WIRE DOUG DC9 DC983 3022083WP GENERATOR SYS LOOSE A WXOAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP17860GA 49786 EN ROUTE FROM LAS TO COS FLT CREW LOST LT GEN, LT AC BUSS, LT DC BUSS, AND X-TIE OPEN. THE A/C X TIE RESET HAD NO EFFECT. THE CREW CYCLED THE GEN RESET, GEN VOLTS/FREQS CAME BACK UP BUT WOULD NOT RESET TO THE LT BUSS. CREW RETURNED TO LAS. THE GEN RESET ON THE SECOND ATTEMPT. NORMAL INDICATIONS FOR THE REMAINDER OF THE FLT. CONTRACT MX CND THE PROBLEM ON THE GROUND. THE LT GCU WAS SWAPPED WITH THE APU GCU FOR T/S. A/C WAS RETURNED TO SERVICE. 3 DAYS LATER THE CREW REPORTED AC X TIE LOCK OUT LIGHT ILLUM, LT GEN VOLT FLUCTUATES +/- VOLTS. UPON FURTHER INVESTIGATION MX FOUND A LOOSE WIRE ON THE GEN TERMINAL BLOCK. THE WIRE WAS SECURED AND A GROUND RUN PERFORMED WITH NO FURTHER PROBLEMS REPORTED. (M) 2L72 4F RTA6WE 20030905000362003090500036SO 2003 9 5 C2XA03CL137 120030805A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2711565 145621 CLT FLIGHT NR 2223 THE CREW REPORTED NR 1 FLOOR PROXIMITY STRIP INOP. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT INVERTER,OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030905001852003090500185EA 2003 9 5 ASOA03366 120030808A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11844AS11097 7317 FLT 4784 - DURING A GROUND INSPECTION IN ATL, THE NR 1 AND 2 EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030813001172003081300117WP 2003 8 13 AALA20030742 120030712A335060030451 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219622A 53593 SEA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BATTERY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030825001742003082500174WP 2003 8 25 03FDEA01205 120030803A5730 RING DOUG DC10 DC1030F 3023504WP GE CF6 CF650* 30018NE RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 R/H WING FUEL TANK ACCESS PANEL CHAFE RING HAS PITTED CORR. REMOVED AND REPLACED CHAFE RING AND GANG CHANNEL IAW SRM 51-42-04 AND SRM 51-31-01 AT MAE ON N/R N00926 2L73 4F4 FRTA22WE E23EA 20030912001252003091200125NM 2003 9 12 AWXA200300892 120030725A53206547690 SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK 5 EACH CRACKS WERE FOUND ON INBOARD LEG OF SUPPORT ZEE (TRANSITION PANEL) AT BS 727C-747, RBL 20. MAINTENANCE REMOVED SUPPORT ZEE AT BS 727C-747, RBL 20; FABRICATED A NEW REPLACEMENT SUPPORT ZEE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 10. 2L72 4F RTA16WE 20030916000742003091600074WP 2003 9 16 GTIA030639 120030728A5313 STRINGER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND CABIN STRINGER 18R WEB CORRODED FS 1214. CUTOUT DAMAGED SECTION OF WEB. FABRICATED WEB DOUBLER. INSTALLED WEB DOUBLER. (M) 2L72 4F RTA6WE 20030916000882003091600088EA 2003 9 16 REXA03004 120030820A2613355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A REXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO258409N 7409 ON CLIMB-OUT, RECEIVED 14TH STAGE LEFT DUCT WARNING MESSAGE. REMOVED AND REPLACED LEFT PYLON SENSING ELEMENT A59WK. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS. (M) 2L72 4F RTA21EA 20030929001182003092900118SO 2003 9 29 RAIA00309233 120030901A3350 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03806HK 145112 EMERGENCY LIGHT ON STAIR INOP. SECURED CONNECTOR TO STAIR EMERGENCY LIGHT. 2L72 4F RTT00011AT 20030429002132003042900213EU 2003 4 29 03102317 120030412A33503022471 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27317UE 41031 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT AFT EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030430001142003043000114NM 2003 4 30 03FDEA00605 120030425A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FLOORBEAM UPPER FLANGE BS 360, LBL 3 TO RBL 2, WL 208. 2L73 4F RTA3WE 20030501000162003050100016SO 2003 5 1 SIMA200302202 120030115A5313 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21653AE 145433 ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED EDDY CURRENT INSPECTION OF THE AREA. NO DEFECTS NOTED. FABRICATED AND A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-24-02, AND STANDARD SRM PRACTICES. (M) 2L72 4T RTT00011AT 20030502001662003050200166NM 2003 5 2 DHL2003741546 120030416A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FLOORBEAM AT BS 1070 LWR FLANGE FWD SIDE AT APPROXIMATELY LBL 14.0 CORRODED. DAMAGE FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG 2. CUT OUT DAMAGED AREA DIMENSIONS 2 X 4 INCHES ON LWR FLANGES IAW B-727 SRM 53-10-8 FIG 2. FABRICATED ONE T-ANGLE FILLER DIMENSIONS 2 X 4 INCHES USING EXTRUSION BAC 1490-2685 PO 302024 AND STRAP DIMENSIONS 2 X 14 INCHES USING .100 7075-T-6 PO 9911586 AND TWO ANGLES DIMENSIONS 3.25 X 15 INCHES USING BACF505-106617 PO 990143 IAW B-727 SRM 53-10-8 FIG 2. ALODINED AND PRIMED ALL REPAIR PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW B-727 53-10-8 FIG 2. 2L73 4F RTA3WE 20030630000092003063000009WP 2003 6 30 IXXA0300038O 120030528A3260H141003 DOWNLOCK SWITCH DOUG DC8 DC873F 302199FWP MLG FAILED A IXXAO OTHER N FALSE WARNING APAPPROACH 1 SW11602AL919282393 45991 ON FINAL APPROACH FROM TOL TO MCI UPON GEAR EXTENSION, GREEN GEAR DOWN LIGHTS DID NOT ILLUMINATE. CREW PERFORMED ABNORMAL PROCEDURES, INDICATION REMAINED THE SAME. AFTER TOWER VISUALLY CONFIRMED GEAR DOWN CREW MADE UNEVENTFUL LANDING IN MCI. UPON INSPECTION MAINTENANCE FOUND THE DOWNLOCK POSITION SWITCH CONNECTOR DEFECTIVE. SWITCH WAS REPLACED AND SYSTEM OPERATIONALLY CHECKED NORMAL. ALL WORK PERFORMED PER APPLICABLE MANUALS 2L74 4F RT4A25 20030505002242003050500224NM 2003 5 5 03FDEA00549 120030421A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION ON REINFORCEMENT FRAME FROM RBL 24 TO LBL 24, WL 208, STA 1176. 2L73 4F RTA3WE 20030506002472003050600247WP 2003 5 6 ASAA0380211 120030304A5347S0006211 CARGO TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND MID CARGO BAY TRACK IS CORRODED AT FS 588-636. REPLACED DAMAGED SECTION OF TRAKC PER SRM 53-05. (M) 2L72 4F A6WE 20030507001722003050700172NE 2003 5 7 MEX2003126 220030408A7320 FUEL CONTROL DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE LT ENGINE MALFUNCTIONED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23216AM 49586 CAPTAIN REPORTED, WHEN ANTI-ICE WAS TURNED ON LT ENGINE, EPR`S WENT DOWN AND RT ENGINE TO SLOW ACCELERATION REQUIRING 40 SECONDS TO ACCELERATE. DURING OVERNIGHT SERVICE LINE PS4 IN RIGHT FCU WAS DRAINED IAW MM, ANTIFLUCTUATION VALVES AND FCU ACCELERATION CAM WAS LUBRICATED AND ENGINES WERE TESTED, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20030508000912003050800091NM 2003 5 8 2003UALA00402 120030429A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29655UA 25393 TEMPORARY DOUBLER OVER THE 3 INCH X 4 INCH HOLE IN ACFT FUSELAGE, 1 FOOT AFT OF AFT MAIN CARGO AREA LOADING LIGHT, ON RIGHT SIDE OF ACFT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPLACED. 2L72 4F4 FRTA1NM E24NE 20030507002072003050700207NM 2003 5 7 CH1A200395020 120030411A5320 CHANNEL BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 ZEE CHANNEL AT L1 DOOR SILL AREA IS CORRODED BETWEEN BS 320 & BS 336 LBL 62. 2L73 4F A3WE 20030513000232003051300023EA 2003 5 13 03130658 120030510A2560P4010021 BATTERY CNDAIRCL600 CL6002B19 1900309EA FLASHLIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CAPTAIN'S EMERGENCY FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS FERRIED FROM IND TO ORD WHERE MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY FLASHLITE BATTERY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030513002622003051300262EA 2003 5 13 ASOA03138 120030331A5346 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11843AS 7310 DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030514000442003051400044EA 2003 5 14 COMA0360230 120030504A3260 TARGET CNDAIRCL600 CL6002B19 1900309EA PROXIMITY SENSOROUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01952CA 7092 LANDING GEAR DISAGREE WARNING; NLG DID NOT RETRACT. ADJUSTED THE NLG CENTERED PROXIMITY SENSOR TARGET. 2L72 4F RTA21EA 20030514002202003051400220NM 2003 5 14 03FDEA00640 120030429A5753ARC41252 RIB DOUG MD11 MD11 3023602NM RT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING, FOUND OUTBOARD FLAP, INBOARD STOP BOLT SUPPORT ISLAND WITH CRACK. REMOVED AND REPLACED AS PER 51-31-01 VOL. I. 2L73 4F RTA22WE 20030515001902003051500190NM 2003 5 15 AWXA200300515 120030414A53156546544547 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 YVR - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH CRACK WAS FOUND ON VERTICAL FLOORBEAM WEB AT LT OUTBOARD SIDE BS 695, LBL 57. MAINTENANCE REMOVED DAMAGED SECTION OF VERTICAL FLOORBEAM WEB AT LT OUTBOARD SIDE BS 695, LBL 57; FABRICATED A NEW REPLACEMENT SECTION OF WEB, A WEB FILLER, AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-2 FIG 1. 2L72 4F RTA16WE 20030515001242003051500124NM 2003 5 15 AWXA200300533 120030513A3350900835A BATTERY BOEING737 737277 1384570NM EMERGENCY LIGHT DEFECTIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28189AW 22656 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT CIRCUIT BREAKER WAS FOUND POPPED. MAINTENANCE RESET EMERGENCY EXIT LIGHT CIRCUIT BREAKER AND REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030609001932003060900193GL 2003 6 9 CA030520004 120030520A2731 CONTROLLER BOMBDRBD700 BD7001A10 1390006GL RROYCEBR700 BR700710A22009500NE ELEVATOR TAB MALFUNCTIONED W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 CA (CAN) AFTER 10 LANDINGS A STAB TRIM MSG. ATTEMPTED 2 RESETS OF CHANNELS 1 & 2 STAB STUCK AT 5.8 UNITS. LANDED IN OUT OF TRIM CONDITION AT CYUL. INVESTIGATION ON GOING. 2L72 4F4 FRTT00003NYE00061EN 20030610000432003061000043WP 2003 6 10 ABXA030168 120030415A531359516857 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 LONGERON 30, DEEPLY PITTED AT FS 756. REPAIRED LONGERON 30 IAW DC-9 SRM 53-02. 2L72 4F A6WE 20030610000932003061000093NM 2003 6 10 DL767030437 120030505A5744113T12721 SUPPORT FITTING BOEING767 767232 1385132NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27113DA 22225 THE HOLE BORES FOR THE FLAP ATTACMENTS ON THE INBD SUPPORT FITTING ON THE LT INBD FLAP ON THE LT WING WERE FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES, HFEC INSPECTION, INSURANCE REAM, AND INSTALLATION OF ALUMINUM BUSHINGS PER ER/A 384975-14, REV B. 2L72 4F RTA1NM 20030611001512003061100151EA 2003 6 11 ASOA03203 120030509A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11856AS 7404 FLT 4382 - DURING A GROUND INSPECTION AT MGM, THE NR 1 AND NR 3 CEILING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 3 CEILING EMERGENCY EXIT LIGHT LAMPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030612000652003061200065SO 2003 6 12 C2XA03TY077 120030530A531014522178005 DOOR FRAME EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING A SCHEDULED 2C CHECK CORROSION WAS FOUND ON THE SERVICE DOOR SILL, JUST BELOW THE SILL PLATE. MAINT CLEANED CORROSION, FILLED AREA WITH EPOXY RESIN, FABRICATED, ALODINED, PAINTED AND INSTALL REPAIR DOUBLER IAW 135/145 SRM 51-40-02, 51-10-02, CPM 51-21-05-06- AND GST 1927/O2A. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030523000942003052300094WP 2003 5 23 MWEA030226 120030519A5230JO602483 DOUBLER DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 MID CARGO DOOR HANDLE CUT OUT REPAIR DOUBLER IS CRACKED. FABRICATED AND INSTALLED CARGO DOOR HANDLE SCUFF PLATE. 2L72 4F A6WE 20030618000242003061800024SW 2003 6 18 HEEA087333 120030611A6510 BEARING BELL 407 407 1182206SW T/R DRIVE SHAFT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH3063 A1860 53378 BEARING MOUNT AREA HAS DAMAGE. REPLACED. 1G71 3U O H2SW 20030617002062003061700206SW 2003 6 17 HEEA087307 120030611A6410 BLADE BELL 407 407 1182206SW T/R HUB ASSY DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH5125 53146 53397 CLICK NOISE WHEN BLADES ARE FLAPPED. REPAIRED. 1G71 3U O H2SW 20030618000952003061800095NM 2003 6 18 SWAA031280 120030607A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED IN SEVERAL AREAS. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030623001082003062300108NM 2003 6 23 USAASB03069 120030525A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 23740 CLT - MAINTENANCE REPORTED THE RIGHT EMERGENCY LIGHTS AT THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030709000242003070900024WP 2003 7 9 AALA20030558 120030510A33501032200 SWITCH DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21417AA 49328 DURING OVERNIGHT MAINTENANCE, EMERGENCY EAC BUS OFF LIGHT ILLUMINATES WHEN EMERGENCY POWER IS SELECTED. REPLACED EMERGENCY AC BUS LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709000592003070900059 2003 7 9 C2XA03IA066 420030625A3444 WARNING LIGHT EMB 145 EMB145LR 3260212SO GROUND PROX ILLUMINATED A C2XAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW2711548 145565 THE CREW NOTED GROUND PROX ALERT TOO LOW GEAR AT 600 FEET ON APPROACH. THE APPROACH WAS ABORTED. THE CREW PERFORMED A MANUAL OVERRIDE OF THE GEAR, AS PRECAUTION. VERIFIED THE GEAR WAS DOWN AND LOCKED AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED ALL LANDING GEAR GROUND PROX SWITCHES WERE SECURE, NO DEFECTS NOTED. CHECKED THE PILOTS CMC FOR MESSAGES, NONE NOTED. THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR AND THE GPWS SYSTEM, NO DEFECTS NOTED. REMOVED THE MEL FOR THE GPWS SYSTEM. 2L72 4T RTT00011AT 20030709001182003070900118NM 2003 7 9 373PA0015 120030611A335020121 POWER SUPPLY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 AFT LEFT CABIN UPPER BIN EMERGENCY LIGHTS INOP. REPLACED AFT LEFT OVERHEAD EMERGENCY LIGHT POWER SUPPLY IAW MM 33-51-51. 2L72 4F RTA16WE 20030710001122003071000112NM 2003 7 10 CALA0300325 120030617A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 1016, BL 0. THE ANGLE WAS REPLACED IAW SRM 51-10-02 AND ECRA 5311-01152. 2L72 4F RTA16WE 20030922001052003092200105EU 2003 9 22 BAQA088911 120030830A2435524031 STARTER GEN AEROSPAS365 AS365N2 8680815EU ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME1438 6417 STARTER GEN INOPERATIVE. WILL START MOTOR, BUT WILL NOT GENERATE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030923000292003092300029WP 2003 9 23 DHL2003604543 120030502A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBD L/E UPPER PLATING SHOWS ELONGATED HOLE AT XFS.710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG.38. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CUT OUT DAMAGED AREA IAW SRM 57-2-1 FIG.38. FABRICATED FILLER (7075-T6 0.050) AND DOUBLER (7075-T6 0.063) IAW SRM 57-2-1 FIG.38. CLEANED, TREATED AND PRIMED INNER SIDE OF FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9 2L74 4F RT4A25 20040127001802004012700180WP 2004 1 27 ASAA0380645 120031015A53219936651515 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 OKC - FOUND DURING 30K CHECK, FLOORBOARD PUNCTURED AT FS 1079-1117. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20040127002012004012700201WP 2004 1 27 ASAA0380667 120031015A52109955763L111 INTERCOSTAL DOUG DC9 DC982 3022082WP PAX DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND L1 DOOR INTERCOSTAL CRACKED UNDER DOOR HANDLE. REMOVED AND REPLACED INTERCOSTAL IAW SRM. (M) 2L72 4F A6WE 20040129000372004012900037EU 2004 1 29 MALA030595 120031218A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 DURING C-CHECK INSPECTION IN LCQ, SEATS 12A & 12B FRAMES CRACKED. ACCOMPLISHED WELD REAPAIRS ON SEAT FRAMES 12A, 12B IAW MESABA EO A25031 DATED 6/FEB 2001. A/C RELEASE DATE 12/31/03. REF 1196437 FOR DETAIL. 2H74 4F RTA49EU 20040204002212004020400221EU 2004 2 4 DHL2003366008 120031112A523094FS494295133 PIN AIRBUS300 A300B4203 3930306EU CARGO DOOR FAILED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01366DH 249 DURING CLIMB OUT THE UPPER DECK MAIN CARGO DOOR NOT LOCKED LIGHT ILLUMINATED ON S/O'S PANEL ALONG WITH THE DOORS LIGHT ON THE MASTER WARNING PANEL (MWP). PERFORMED EMERGENCY PROCEDURE IAW AOM. INSTALLED NEW BUSHING AND NEW PIN AS PER M/M 52-33-00, OPS CHECKED OK. 2L72 4F RTA35EU 20040210001012004021000101EU 2004 2 10 USAA030278 120031124A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK APPROX .125 INCH AREA, LBL 37.50 10 INCHES AFT OF FRAME. DAMAGED TRACK REMOVED, REPLACED WITH NEW PER SRM 51-74-0 AND 51-72-11. (M) 2L72 4F RTA46NM 20040211000042004021100004NM 2004 2 11 USAABB03230 120031226A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM SEAT ROW 33 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19621AU 27200 FOUND THE AISLE EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 33 INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20031210000812003121000081EU 2003 12 10 AALA20031304 120031120A3230A82505403 ROD FOKKERF28 F28MK0100 4990807EU NLG BROKEN A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW211463A 11483 ORD T1755/20 EN ROUTE ORD-MSP UNABLE TO RAISE NOSE GEAR. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED ADJUSTABLE ROD FOR NOSE GEAR SELECTOR VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20031212000172003121200017NM 2003 12 12 SWAA032438 120031103A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER FWD CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031211000842003121100084NM 2003 12 11 03FDEA01904 120031111A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-224-04) BS 1130 FLOORBEAM UPPER CHORD AROUND HOLES AND UNDER NUT PLATES, LBL 48, WL 208. 2L73 4F RTA3WE 20040308001532004030800153NM 2004 3 8 ASAA0310680 120031222A533065458001 SKIN PANEL BOEING737 7372Q8C 138448SNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 219, STRINGER 24L DENTED. REMOVED DAMAGED AREA AND REPAIRED SKIN PANEL PER SRM. (M) 2L72 4F A16WE 20031215000922003121500092NM 2003 12 15 QXEA200301435 120031112A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX- LEFT HAND SIDE OF FUSELAGE HAS DENT 1 INCH AFT OF ICE SHIELD AT STATION X320.000 AND Z155.550. REPAIRED IAW DHC-8 RD 8-53-2432. 2H72 4T RTA13NM 20030925000702003092500070WP 2003 9 25 AALA20030894 120030824A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21467AA 49597 DURING OVERNIGHT MAINTENANCE, AFT CEILING EMERGENCY EXIT LIGHTS AND EVACUATION SLIDE LIGHTS INOPERATIVE. REPLACED AFT RIGHT LAV EMERGENCY EXIT LIGHT BATTERY PACK AND CHARGERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030925000942003092500094 2003 9 25 00113 420030915A3420 AMPLIFIER AMD FALC20FALCON 2720302EU COCKPIT MISINSTALLED E HAEAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 SW05295TW 5 PILOT REPORTED BOTH RMI AND DIRECTIONAL GYRO FROZE AND FLAGGED AT THE SAME TIME, DIVERTED FLIGHT TO LRD FOR NORMAL LANDING. WILL UPDATE THIS REPORT AFTER MAINTENANCE. MAINTENANCE FOUND SERVO AMP IMPROPERLY SEATED, NR 1 AND 2 COMPASS SYSTEM OPERATIONALLY CHECK GOOD. 2L72 4F A7EU 20040721000352004072100035WP 2004 7 21 AALA20030840 120030806A2170 WATER SEPARATOR DOUG DC9 DC982 3022082WP CABIN AIR CONTAMINATED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW21459AA 49564 ON LANDING, SMOKE IN CABIN AFTER APU START. AIRCRAFT LANDED WITHOUT INCIDENT. APU SHUTDOWN AND SMOKE DISSIPATED. INCIDENT APPEARS TO BE CAUSED BY RESIDUAL HYD FLUID LEFT FROM A PREVIOUS REPAIR. REPLACED COALESCER BAGS ON LT AND RT WATER SEPARATORS. CLEANED APU INELT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030930000782003093000078WP 2003 9 30 ABXA030351 120030818A534039216711 FITTING DOUG DC9 DC932F 3022067WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 LT FRAME 294 ENG. FITTING CRACKED AT CARGO FLOOR ATTACH POINT. REPLACED FITTING IAW DC-9 SRM 51-10-4, 51-30-5 AND 51-30-1. 2L72 4F A6WE 20030905002362003090500236WP 2003 9 5 DHL2003873598 120030708A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING TOP AFT PANEL PLATING CORRODED AROUND STA XRS 728.000 S-5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. BLENDED OUT THE DAMAGED AREA, PERFORMED NDT INSPECTION AROUND REWORK AREA IAW DC8 NDT SPM PART 6-10-001. CLEANED, TREATED AND PRIMED. FABRICATED A REPAIR DOUBLER IAW EODHL-030621, ED-3470. CLEANED, TREATED AND PRIMED DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON RT OUTER WING TOP AFT PANEL PLATING (STA XRS.728.000, S-5) USING NEW FASTENERS IAW EODHL-030621, ED-3470, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. SEE N/R 2088 FOR LEAK CK. 2L74 4F RT4A25 20030909000662003090900066NM 2003 9 9 VNAA0308019 120030826A2611SD9422AOAO SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY MALFUNCTIONED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07423JS8400 67 3032 THE CREW RECEIVED A LAV SMOKE DETECTOR INOP INDICATION. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031002001032003100200103SO 2003 10 2 C2XA03TY157 120030910A321323092032003 AXLE EMB 135 EMB135ER 3260203SO RT MLG DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716502 145166 DURING A SCHEDULED INSPECTION THE RIGHT MLG RETRACTION AXLE CHROME PLATED AREA DAMAGED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG RETRACTION AXLE I/A/W-EMB-135-AMM-32-10-03. OPS AND LEAK CHECKED GOOD. 2L72 4F RTT00011AT 20031003000812003100300081NM 2003 10 3 03FDEA01524 120030829A5753 HINGE DOUG MD11 MD11 3023602NM LT WING OB FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING OUTBOARD FLAP HINGE (A/C) SIDE FWD SEAL ATTACHMENT STRIP FOUND CRACKED. 2L73 4F RTA22WE 20031028000722003102800072EU 2003 10 28 YENA200324 120030922A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU EMERGENCY LIGHT NICKED A YENAK NONE O OTHER ININSP/MAINT 1 EA15503JB 1123 EMMERGENCY LIGHT HARNESS AT LT ROW LOCATION 3, 6, 8, 10, 12, 14, 18, 22 AND 26 HAS NICKS AND POSSIBLE DAMAGE. REPAIRED HEAT SRINK TUBING IAW ESPM 20-53-29 AT 6 LOCATIONS AND REPLACED HARNESS AT ROW 14, 22, 26. 2L72 4F RTA28NM 20031028001402003102800140NM 2003 10 28 ASAA0340083 120030228A532069434961 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR TO SIDEWALL WEB AT BS 847 TO 867. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031110001132003111000113 2003 11 10 SWIA200312540 420031021A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07221SW6733 1201 120290 WHEN AP ON CAPT'S SIDE, TRIM FAIL AND RED AUTO PILOT FAIL ON MAP AND COMPUTER FLAG ON CA ATTITUDE. FGS 1 DC CIRCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 APC-65 IAW MM 22-10-02. OPS CHECK GOOD. 622-8318-402, S/N ON: 1641, S/N OFF: 3788. 2L72 4T RTA31SO 20031106000752003110600075NM 2003 11 6 03FDEA01825 120031029A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-111-01, 2) FWD CARGO COMPARTMENT STR 28R BS 680 RBL 6 WL 148. FWD CARGO BAY STR 28R BS 680 WAS OUT OF LIMITS. FABRICATED NEW STRINGER SPLICE & INSTALLED PER SRM 51-30-02. 2L73 4F RTA3WE 20031106001552003110600155SO 2003 11 6 C2XA03TY175 120031005A532014522460015 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713994 145291 DURING A SCHEDULED INSPECTION THE FORWARD FUSELAGE GUSSET WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE FUSELAGE GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20031105000492003110500049NM 2003 11 5 CALA0300613 120031031A533065C35772 SKIN BOEING737 737524 1384721NM FUSELAGE CHAFED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914628 27532 UPPER FUSELAGE SKIN WORN AT STA 867 RBL 5 AND LBL 5 UNDER DORSAL FIN, APPROX 3 X 10 INCH. CUT OUT DAMAGE AND REPAIRED PER SRM 53-00-01 FIG 202. 2L72 4F RTA16WE 20031110001862003111000186GL 2003 11 10 SWAA032257 220031012A73218063208 MEC BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563B1US GL NR 1 ENGINE FAULTY A SWAAK NONE Y ENGINE STOPPAGE LDLANDING 1 SW29368SW 26579 NR 1 ENGINE SHUT DOWN. FOUND, NR 1 ENGINE FUEL SHUTOFF VALVE, VALVE SWITCH, FUEL PUMP AND MEC FAULTY. REMOVED AND REPLACED SHUTOFF VALVE, VALVE SWITCH, FUEL PUMP AND MEC PER MM. 2L72 4F4 FRTA16WE E2GL 20031112000782003111200078NM 2003 11 12 AWXA200301401 120031014A5315146N5444 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM FROM BS 1503 TO BS 1513, RBL 9. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM FROM BS 1503 TO BS 1513, RBL 9; FABRICATED 2 EACH FILLERS, AND 2 EACH REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 6 FIG 1. 2L72 4F RTA2NM 20031009000942003100900094EA 2003 10 9 03260650 120030917A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27650BR 7418 DURING INSPECTION THE RIGHT HAND EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20031119000612003111900061NM 2003 11 19 C8GA20030023 120031010A3260656021123 ACCESSORY UNIT BOEING727 7272A1 138407FNM MLG DEFECTIVE A C8GAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO15286SC2248 21601 FLT 711 FROM DEN TO TOL. ON TOUCHDOWN IN TOL, THE LT, RT & NOSE RED GEAR UNSAFE LIGHTS CAME ON IN CONJUNCTION WITH THE THREE LIGHTS. INITIATED GO AROUND, RECYCLE GEAR AND GREEN LIGHTS CAME ON. AGAIN ON TOUCHDOWN, THE THREE RED GEAR UNSAFE LIGHTS CAME ON. RECYCLED GEAR AND DID A FLY BY AND THE TOWER CONFIRMED THE GEAR DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. OPERATIONAL CHECKS WERE ACCOMPLISHED AND REPLACED THE LANDING GEAR ACCESSORY UNIT IAW MM 32-09-122 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030814000722003081400072SO 2003 8 14 SWIA200312119 120030522A4910 FIREWALL EMB 120 EMB120ER 3260203SO APU CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07189SW 120048 APU FIREWALL CRACKED AT UPPER LT AND RT CORNERS. FOUND DURING C-CHECK INSPECTION. REPAIRED IAW SRM 120 53-30-04. 2L72 4T RTA31SO 20030815000392003081500039SW 2003 8 15 HEEA088551 120030803A7810212061202009 EXHAUST DUCT BELL 412 412 1182202SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 CRACK FOUND AROUND MOUNTING SURFACE OF EXHAUST DUCT. SHOP REPAIR. 1G72 4U H4SW 20030815000302003081500030SW 2003 8 15 HEEA088547 120030728A7712206075739103 TORQUEMETER BELL 206 206L3 1182108SW COCKPIT FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 ENGINE TORQUEMETER FLUCTUATES. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030820002132003082000213EU 2003 8 20 ASOA03321 120030719A33503011052 COVER AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT COVER AT THE SERVICE DOOR WAS FOUND TO BE UNSECURED. MAINTENANCE RESECURED THE EMERGENCY EXIT LIGHT COVER AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030403000732003040300073SO 2003 4 3 C2XA03CL082 120030401A3260W001089224 WIRE EMB 145 EMB145ER 3260211SO WARNING SYS SHORTED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714943 145040 CLE FLT 2224 THE CREW REPORTED THAT THE LANDING GEAR AURAL WARNING SOUNDED ON TAKEOFF WITH THE GEAR SELECTED AND INDICATING UP. AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED SHORTED WIRE BEHIND AURAL WARNING RACK W001-0892-24. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030402000702003040200070NM 2003 4 2 2003UALA00347 120030210A5754114W413015 WEDGE BOEING777 777222 1385219NM NR 5 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 T/E WEDGE DELAMINATED - NR 5 SLAT O/B FOAM SEAL MISSING. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. INSTALLED MISSING SECTION OF BULB SEAL FOAM INSERT. 2L72 4F RTT0001SE 20030408001262003040800126WP 2003 4 8 AMTA200300222 120030213A3397 WIRE LKHEED1011 10113853 5265020WP EMERGENCY LIGHTSDAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11162AT 1220 EGRESS LIGHTS INOPERATIVE AT THE FORWARD GALLEY. REMOVED AND REPLACED TRANSITION CABLE FROM A/C RIGHT SIDE FLOOR LIGHT STRIP TO FWD GALLEY FLOOR STRIP SYSTEM. OPS OK REF MM 33-50-01. (M) 2L73 4F A23WE 20030410000232003041000023WP 2003 4 10 GTIA030083 120030215A5320 INTERCOSTAL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FORWARD CARGO COMPARTMENT APPROX STATION 370 INTERCOSTAL BY LONGERON 30 HAS CORROSION. REMOVED INTERCOSTAL. FABRICATED NEW FS 370 INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2L72 4F A6WE 20030411000052003041100005NM 2003 4 11 SWAA030729 120030402A33506104789 BATTERY BOEING737 7372H4 138448CNM FUSELAGE INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED PM CHECK, FOUND BOTH FWD ENTRY AND FWD SVC EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PER MM. 2L72 4F A16WE 20030416001342003041600134NM 2003 4 16 DLM88030271 120030322A2910P24000008254HH LINE DOUG MD88 MD88 3023688NM RT HYD MODULE LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO27972DL 53215 ON DESCENT RT HYD QTY DROPPED TO 2 QTY AND PRESS TO ZERO C/W EMERGENCY PROCEDURES TURNED XFER PUMP OFF. REPLACED RT HYD LINE TO FILTER MODULE. 2L72 4F RTA6WE 20030417000352003041700035EU 2003 4 17 MALA030130 120030126A3230104627003 JACKSHAFT BAC 146 AVRO146RJ85A1500097EU MLG INOPERATIVE A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15516XJ E2334 LEFT MAIN DID NOT COME UP AFTER UP SELECTION AS REPORTED BY DLH TOWER AND RED INDICATION IN COCKPIT. AFTER RECYCLING THE GEAR DOWN AND RESELECT UP, NO PROBLEMS NOTED. NO PROBLEMS PUTTING IT DOWN ON APPROACH TO MSP. MAINTENANCE FOUND LT OLEO OVERCENTER LOCK JACK NOT WORKING PROPERLY. REPLACED LT OLEO JACK P/N 104627003 IAW AMM 32-31-14, AND 32-30-00. FAULT ISOLATION TABLE. GEAR SWINGS ALL GOOD. SN/ON DRG/148/89, SN/OFF DH-0241-98. 2H74 4F RTA49EU 20030417000632003041700063NM 2003 4 17 PCAA0301028 120030130A3350 BULB DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BURNED OUT A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13831EX 160 DURING ROUTINE MAINTENANCE VISIT FLOOR TRACK EMERGENCY LIGHTING HAD 1 BULB INOPERATIVE AT SEAT 8DF. SOCKET FOR BULB WAS REPLACED ON FLOOR TRACK EMERGENCY LIGHT AT SEAT 8DF. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030424000982003042400098EA 2003 4 24 SWIA200311839 120030221A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07908SW 7540 FS 621.0 LEFT FLOORBEAM ANGLE LBL 42 CRACKED. FOUND DURING C-CHECK INSPECTION. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-61-117. 2L72 4F RTA21EA 20030424001732003042400173SO 2003 4 24 LR7A03028 120030313A5320 CHANNEL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 RT WING-TO-FUSELAGE FAIRING CHANNEL CRACKED AT FS 532, RBL 86, WL 237. REPAIRED IAW LAC MEA 382-53-03-010. NR 2209. 2H74 4T A1SO 20030430000632003043000063NM 2003 4 30 USAA030031 120030320A5711 SPAR BOEING737 737401 1384701NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US 23885 PIT - FOUND UPPER REAR SPAR CRACKED 1 INCH IN LENGTH TWO EACH, RIGHT WING UPPER REAR SPAR AT RSS 224.14. ACCOMPLISHED OVERSIZE OF HOLES AND INSTALLATION OF REPAIR DOUBLER PER EA 75898. (M) 2L72 4F RTA16WE 20031120000262003112000026NM 2003 11 20 AWXA200301235 120030922A53206546812175 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT INBOARD LEG BS 1006-1016, LBL 37, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 1006-1016, LBL 37, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51, PG 111 FIG 101. 2L72 4F RTA16WE 20040112000172004011200017WP 2004 1 12 AALA20031240 120031108A3350AAP3274A CHARGER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21572AA 49458 DURING OVERNIGHT MAINTENANCE, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED TAILCONE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031126000262003112600026EU 2003 11 26 MALA030500 120031102A5321 FLOOR PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434XJ 340B434 DURING 4K INSPECTION IN LCQ, FIRST OFFICERS FLOOR PANEL CORRODED AT STA 179 RBL 25. VENDOR CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MESABA EO S53186 DATED 03 NOV 03. 2L72 4T RTA52EU 20040115001212004011500121NM 2004 1 15 03FDEA02098 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363BL. LT CENTER SECTION OF NR 1 BANJO FITTING AJC7051-505 AFT FACE FLANGE 1 CRACK LOCKBOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20031212001552003121200155WP 2003 12 12 GTIA030859 120031013A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND DENT AT FS 1276 TO FS 1315 BETWEEN LONGERONS 23 AND 24L, REQUIRES REPAIR. DENT AT FS 1276 SHOULD BE INCORPORATED INTO THIS REPAIR. CUT OUT DAMAGED SECTION OF SKIN FROM STATION 1276-1315. FABRICATED INNER DOUBLERS, FINGER DOUBLER AND NEW SKIN. INSTALLED DOUBLER AND SKIN. (M) 2L72 4F A6WE 20031215000512003121500051NM 2003 12 15 2003UALA00832 120031105A5320 INTERCOSTAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT PIT INTERCOSTAL HAS CORROSION STA 1500 TO 1513 STR 30R TO STR 29R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW PART PER SRM 51-40-02 & BOEING DWG 146N5451. 2L72 4F4 FRTA2NM E17NE 20031215000862003121500086NM 2003 12 15 03FDEA01955 120031113A5753 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT OUTBOARD FLAP FOUND OUTBOARD HINGE FITTING ACTUATOR HOLE I/B CORRODED. COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20031217000142003121700014NM 2003 12 17 CALA0300657 120031120A5420 WEB BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND A 3 INCH CRACK IN WEB AT NR 1 PYLON STRUT. REPAIRED IAW ECRA 5421-01002. 2L72 4F RTA16WE 20031217001832003121700183 2003 12 17 SWIA200312602 420031109A2210 INDICATOR EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07288SW 120316 CA'S AP DOES NOT HOLD ALTITUDE. REMOVED AND REPLACED NR 1 APC-65B. OPS CHECK GOOD IAW MM 22-11-00. P/N: 622-8317-402, S/N OFF: 4147. 2L72 4T RTA31SO 20031217001302003121700130 2003 12 17 03340311 420031206A22117010680938 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AUTOPILOT INOPERATIVE A VTZAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA27311UE 41029 DURING APPROACH TO IAD CREW REPORTED THE AUTOPILOT SYSTEM PITCHING UP AND DOWN WHILE AIRCRAFT WAS UNDER CAPTAINS CONTROL. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFUL AND PASSENGER DEPLANED NORMALLY. THE FCC WAS FOUND TO BE FAULTY AND WAS REPLACED. A SATISAFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031222000672003122200067WP 2003 12 22 ASAA0380616 120031007A532199365501 FLOORBOARD DOUG DC9 DC983 3022083WP FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS CORRODED AROUND INSERTS AT FS 160-190. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031222000992003122200099 2003 12 22 USAASA03127 420031109A2565 CABLE AIRBUSA319 A319112 3930323EU ESCAPE SLIDE BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19763US 1360 DURING INSPECTION, FOUND THE CABLE END ON THE LEFT OVERWING SLIDE BROKEN NEAR THE SLIDE BOTTLE. MAINTENANCE REPLACED THE LEFT OVERWING SLIDE BOTTLE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031223000902003122300090NM 2003 12 23 SWAA032701 120031210A335010114 LIGHT BOEING737 7373Q8 1384670NM PAX DOOR GROUNDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SPECIAL VISIT FOUND LOWER R1 AND L1 EMERGENCY LIGHTS INOP. REPAIRED GROUNDED WIRE PER WDM AND MM. 2L72 4F RTA16WE 20031231001282003123100128NM 2003 12 31 AWXA200301631 120031214A5330654577678 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AT STR 26 LT, BS 727A & BS 727B. MAINTENANCE CUT OUT DAMAGED SKIN AT STR 26 LT, BS 727A & BS 727B; FABRICATED A REPAIR PLATE AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 201 PG 201-203. 2L72 4F RTA16WE 20031020001002003102000100WP 2003 10 20 ABXA030373 120030909A52306914025501 BEAM DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 AFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED ON AFT SIDE. REPLACED AFT LOWER CARGO DOOR BEAM NR 2 END FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030501000132003050100013WP 2003 5 1 AALA20030279 120030227A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21245AA 49257 TUL - FOUND FRAME WEB IS CRACKED AT STATION 1463, RIGHT SIDE, INBOARD EDGE, APPROX 1:30 POSITION. INSTALLED DOUBLER ON FRAME WEB PER SRM 51-70-04 FIG 2 SH 2. (M) 2L72 4F A6WE 20030501000382003050100038EA 2003 5 1 ASOA03115 120030318A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO11860AS 7433 FLT 4736 - DURING DESCENT INTO MYR FROM ATL, THE CREW RECEIVED A SMOKE TOILET AMBER MESSAGE ALONG WITH A NOTICEABLE ODOR OF SMOKE IN THE COCKPIT AND CABIN. A THIN HAZE OF SOME OCCURRED IN THE CABIN AND DISSIPATED ALONG WITH THE ODOR SHORTLY AFTERWARDS. THE RIGHT PACK OUTLET TEMPERATURE SPIKED TO 79 DEGREES CELSIUS SHORTLY AFTER TRANSFERRING THE BLEEDS TO THE AUXILIARY POWER UNIT. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RAN THE ENGINES SWITCHING THE PACKS BETWEEN THE AUXILIARY POWER UNIT AND THE ENGINES WITH NO SMOKE OR ODOR RE-OCCURRING. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030501000892003050100089SW 2003 5 1 2003F00239 120030109A5230 MECHANISM FRCHLDSA227 SA227DC 3377521SW CARGO DOOR LACK OF LUBE A BSAAK NONE O OTHER ININSP/MAINT 1 NM05453LA DC852B SEA - FLT 6006 - CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHT CAME ON DURING CLIMB AT 9,000 FEET. CREW RETURNED TO STATION. DOOR CLOSING PROCEDURES OR DOOR HARD TO CLOSE. CLEANED AND LUBED CARGO DOOR CLICK CLACKS AND SWITCHES. DOOR CYCLED MULTIPLE TIMES WITH NO DEFECTS NOTED. TEST FLIGHT WAS THEN COMPLETED WITH NO DEFECTS NOTED. (M) 2L72 4T RTA18SW 20030501001082003050100108NM 2003 5 1 ASAA0310027 120030223A5420 FILLER BOEING737 737210C 1384459NM RUB STRIP MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 2 ENGINE INBOARD COWL RUBSTRIP LOWER CORNER AT NACELLE STATION 99.25, WING STATION 191 MISSING FILLER SECTION. ADDED MISSING FILLER AND INSTALLED STRAP PER SRM. (M) 2L72 4F A16WE 20030502001442003050200144NM 2003 5 2 SWAA030832 120030414A53106935365 SHEAR TIE BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L & 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030502001582003050200158NM 2003 5 2 03FDEA00476 120030417A5414 SKIN BOEING727 727200 138407ENM NR 3 NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE LOWER COWLING UPPER FRAME NEXT TO OIL TANK ACCESS DOOR HINGE HAS CHAFING CONDITION. 2L73 4F RTA3WE 20030502002142003050200214EU 2003 5 2 AWXA200300397 120030404A5320D5347112320300 SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON LOWER SURFACE OF SHEAR WEB (SUPPORT) 147MM FORWARD OF FR 70, AND INBOARD OF THE RT OUTBOARD CREASE BEAM ANGLE. MAINTENANCE REMOVED CORRODED SUPPORT FR 70; FABRICATED A NEW REPLACEMENT SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 53-41-17, PG 8 & 16, FIG 1, SRM 51-44-11, PG 16, 19, & 20, FIG 2, SRM 51-42-11, PG 8-10, 12, & 21-22, FIG 2, 3, & 8, AND SRM 51-74-00, PG 9-10. 2L72 4F RTA28NM 20030502001972003050200197 2003 5 2 UPS03840429 420030417A2565 SLIDE DOUG DC8 DC871F 302199DWP PAX DOOR DETERIORATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: PFLT, CREW ENTRY DOOR ESCAPE SLIDE COMING APART. RE-ATTACHED CREW ENTRY ESCAPE SLIDE COVER & SECURED TO DOOR. 2L74 4F RT4A25 20030505002472003050500247NM 2003 5 5 03FDEA00522 120030418A5753 FAIRING BOEING727 727200 138407ENM LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LEFT WING NR 2 FLAP TRACK MOVABLE FAIRING GOUGED ON INNER SURFACE OUTBOARD SIDE AFT OF FORWARD STIFFENER. *S/D* REPAIRED IAW BOEING 727-200 SRM 57-20-04. 2L73 4F RTA3WE 20030509000722003050900072NM 2003 5 9 HOC2003F00010 120030428A5320 SUPPORT BRACKET BOEING727 727231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON LEFT, OUTBOARD DITCHING PAN SUPPORT BRACKET. STA 1176-1183. 2L73 4F4 F A3WE E2EA 20030604001772003060400177NM 2003 6 4 UPS03440597 120030415A575365B078702 RIB BOEING747 747121 1384871NM NR 20 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT WING - NR 20 VC FLAP O/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 6, 7. BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030605000172003060500017NM 2003 6 5 S03226019 120030410A2612350059 CIRCUIT CARD BOEING747 747* NM PWA JT9 JT9D7R4G2 52054NE WW FIRE DETECT MALFUNCTIONED W SAJFO OTHER N FALSE WARNING CLCLIMB 1 WP03 24308 WHEEL WELL FIRE WARNING WAS TRIGGERED AFTER LANDING GEAR SELECTED UP, CREW FOLLOWED QRH PROCEDURE TO DOWN MLG, WARNING LIGHT WENT OUT FOR 1 SEC THEN CAME ON AGAIN. GROUND CHECK FOUND NO OIL/AIR LEAKAGE. ALL WHEELS AND BRAKES WERE CHECKED NORMAL. A/C BACKED INTO SERVICE TO TPE. SENSORS /WIRING CONDITION CHECKED STILL NORMAL. THE W/W FIRE DETECTION CONTROL CARD WERE REPLACED. NO FURTHER WARNING TRIGGERED EVER SINCE. 2L74 4F4 FRTA20WE E3NE 20030605001402003060500140SO 2003 6 5 SWIA200311965 120030510A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07268UE6121 4502 120207 ON INITIAL POWER UP OF THE AIRCRAFT, A FLAP CONTROL FAULT CAME ON AND WOULD NOT RESET UNTIL THE BIT AND THE PST BUTTONS WERE PUSHED. REMOVED AND REPLACED VERSION II FCU AND ANNUNCIATOR UNIT WITH SERVICEABLE VERSION I FCU AND ANNUNCIATOR UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030610000732003061000073NM 2003 6 10 DL757030414 120030502A3240 PIN BOEING757 757232 1384965NM NR 4 BRAKE MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27626DL 22916 NUMBER FOUR BRAKE WEAR PINS MISSING. REPLACED NUMBER FOUR BRAKE ASSY AND LEAK CHECKS OK. 2L72 4F RTA2NM 20030610000702003061000070NM 2003 6 10 DL76S030411 120030501A5330146T31621 SKIN BOEING767 767332 1382001NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27127DL 24077 THE FUSELAGE SKIN WAS DAMAGED FROM A LIGHTNING STRIKE AT FS 1219 AND STRINGER 3R. THE DAMAGED SECTION OF SKIN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS. THE UNDERLYING STRINGER WAS CUT AND A NEW SECTION SPLICED IN PER B767-300 SRM. THE REPAIR WAS DOCUMENTED PER ER/A 384955-14. 2L72 4F RTA1NM 20030612000862003061200086WP 2003 6 12 UPS03840709 120030521A53404750418U2 ATTACH FITTING DOUG DC8 DC871F 302199DWP FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STATION 1220 AT LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D. 2L74 4F RT4A25 20030612001152003061200115NM 2003 6 12 UPS03240753 120030526A5313 STRINGER BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, ON REMOVAL OF BLIND FASTENER STRINGER FOUND DAMAGED (CRACKED) AT FUSELAGE HOLE STRINGER 26L AT BS 320. CRACK CONTAINED IAW SRM 53-10-3. HFEC INSP CARRIED OUT ON THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 FIG 4 &16 RESULT. NO DEFECTS FOUND CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM 53-10-3. 2L73 4F A3WE 20030613000752003061300075SO 2003 6 13 C2XA03SH171 120030608A531014521950001 CROSSBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030618000362003061800036NM 2003 6 18 SWAA031329 120030611A53116546546 FRAME BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 800, BETWEEN STR 23R AND STR 24R. REPAIRED FUSELAGE FRAME PER SWA EA. 2L72 4F A16WE 20030620000522003062000052WP 2003 6 20 GTIA030378 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND FLOOR SUPPORT STATION 160-200 LBL 44 HAS CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030624000732003062400073SO 2003 6 24 LR7A03046 120030529A5320 WEB LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 1963 4606 DURING SCHEDULED A CHECK INSPECTION PER JOB CARD HA1200 FOUND FS 1023 WEB CRACKED RBL 5 TO RBL 29 AT WL 177. AIRCRAFT FERRIED UNPRESSURIZED TO EGSC FOR REPAIR. AT EGSC REPAIRED WEB IAW SRM SMP 583-51-140-10. REF MA SOW MA/I/A56A NRWC 004. LP 09023, ITEM M1. 2H74 4T A1SO 20030620000212003062000021SW 2003 6 20 HEEA086943 120030603A3212206050247132 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 EMERGENCY FLOAT COVER TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030630000402003063000040EU 2003 6 30 AWXA200300616 120030502A5320D5347047821000 PROFILE AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 50, STR 38 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CENTER PROFILE FR 50, STR 38 LT; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND 2 EACH SPLICE DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-05341-03142-TB5. 2L72 4F RTA28NM 20030718000192003071800019NM 2003 7 18 USAASB03083 120030614A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEAT ROWS 3, 4 AND 5 AND THE EXIT LIGHT ABOVE THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, P/N 2013-1A, AND CHARGER ASSEMBLY IN THE ENTRYWAY CEILING, RIGHT SIDE. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030708000592003070800059SO 2003 7 8 SWIA200312096 120030519A5720 CLIP EMB 120 EMB120ER 3260203SO WING CLIP DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07296SW 120325 WING CLIP JUST IN FRONT OF NR 2 FUEL LEVEL STICK AT RT WING IS CRACKED. (DISCOVERED DURING C-CHECK.)REMOVED DAMAGED WING CLIP AS REQUIRED. INSTALLED NEW WING CLIP IN RH WING . NO LEAKS NOTED AT THIS TIME. 2L72 4T RTA31SO 20030709001172003070900117NM 2003 7 9 CALA0300311 120030612A5414 SKIN BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND A .25 INCH CRACK ON LIP OF HOLE CUT ON O/B SIDE OF ACCESS PANEL 5727L OF NR 1 PYLON. REPAIRED ACCESS PANEL IAW ECRA 5430-01230. 2L72 4F RTA16WE 20030711000922003071100092 2003 7 11 ZW0A0305502 420030626A256561571127 SLIDE BOEING757 757231 1384950NM DEPLOYED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13711ZX 28481 AFTER CHECK-C AND DURING A MINI CABIN EVACUATION THE ESCAPE SLIDE AT THE LEFT SIDE NUMBER 4 CABIN DOOR DEPLOYED AND INFLATED, BUT FELL TO THE GROUND. THE GIRT BAR WAS WITH THE SLIDE. 2L72 4F RTA2NM 20030709000702003070900070EA 2003 7 9 03153652 120030601A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27652BR 7429 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT FWD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030108000592003010800059EA 2003 1 8 COMA0360009 120030101A2620365000183 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO LEAKING A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01821CA11111 7420 FLIGHT 5814 CARGO BOTTLE LOW MESSAGE.REPLACED THE CARGO FIRE BOTTLE. 2L72 4F RTA21EA 20030128000952003012800095SW 2003 1 28 HEEA083842 120030116A6230406010429101 PIN BELL 407 407 1182206SW M/R DRIVE LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 MAIN ROTOR DRIVE LINK PIN WORN. 1G71 3U O H2SW 20030128002722003012800272NM 2003 1 28 C1HA200397004 120030123A2611 SMOKE DETECTOR BOEING727 727270 138408PNM LAVATORY FAULTY A C1HAO OTHER N FALSE WARNING UKUNKNOWN 1 GL15697CA 23052 FWD LAV SMOKE DETECTOR CHIRPING. R&R FWD LAV SMOKE DET BAT OPS NORMAL. 2L73 4F RTA3WE 20030129000362003012900036SW 2003 1 29 HEEA083949 120030117A6420 BEARING BELL 407 407 1182206SW T/R HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53324 53461 TAIL ROTOR HEAD FEATHERING BEARING WORN. REPAIRED. 1G71 3U O H2SW 20030131000342003013100034NM 2003 1 31 CA030103020 120030102A2742AC817728 CONNECTOR BOEING737 7372T5 1384474NM PWA JT8 JT8D17 52049NE STAB ACTUATOR BURNED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA (CAN) DURING OVERNIGHT CHECK IN THE HANGER, AVIONICS FOUND THE A/P STAB TRIM MOTOR C/B WAS POPPED. TRIED A RESET BUT NO JOY AND C/B FELT ODD. TURNED A/C POWER OFF AND C/B WOULD NOT RESET. C/B REPLACED. C/B RESET BUT POPPED A FRACTION OF A SECOND LATER. AVIONIC WENT TO STAB BAY TO REMOVE PLUG FROM MOTOR AND NOTED BAY HAD SMOKE. INVESTIGATION REVEALED THAT MOTOR CONNECTOR PLUG AND APPROX. 3 INCHES OF ASSOCIATED WIRING SHOWED SIGNS OF OVERHEATING, ARCING, ETC. THE PLUG, SOME WIRING AND THE MOTOR WERE REPLACED. 2L72 4F4 FRTA16WE E2EA 20030204000222003020400022SO 2003 2 4 UG82003F00000 120030104A32601159SCAV5131 SQUAT SWITCH GULSTMGV GULFSTREAMGV3980116SO MLG FAILED E UG8AO OTHER J WARNING INDICATION CLCLIMB 1 GL23910DC2468 544 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF OUT OF KTEB. ALL WOW INDICATED AIR MODE EXCEPT COMBINED WOW WHICH WAS AMBER GROUND. AT 1+03 HOURS AFTER TAKEOFF. COMBINED WOW WENT TO AIR. THE GEAR WAS RETRACTED AND ALL SYSTEMS RETURNED TO NORMAL. A FAULTY WEIGHT ON WHEELS SWITCH. REPLACED ALL SUSPECTED WEIGHT ON WHEELS SWITCHES AS A PRECAUTION. SINCE DEFECT COULD NOT BE DUPLICATED. PERFORMED ALL REQUIRED OPERATIONAL CHECKS IAW MM AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA12EA 20030204000512003020400051NM 2003 2 4 SWAA030200 120030126A32106546109 ARM BOEING737 7373H4 1384600NM LT/RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED A2 CHECK, SWA SI 11251-32, FOUND BOTH LT/RT MLG CLEVIS BEAM ARMS CORRODED. REMOVED AND REPLACED BOTH LT/RT MLG CLEVIS BEAM ARMS PER MM. 2L72 4F RTA16WE 20030204001362003020400136CE 2003 2 4 VJ32003F00019 120030115A3610RA216CW PUMP BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO DRY AIR FAILED B VJ3RK NONE O OTHER ININSP/MAINT 1 WP078173C216 CE1541 DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANES ARE WORN. RECOMMENDATION IS TO LOOK AT MANUFACTURE PROCESS. 1L71 3O3 O 3A15 E5CE 20030204001962003020400196CE 2003 2 4 2003F00100 120030120A572026111441 BRACKET CESSNA CESSNA208 208B 2073701CE FLAP ACTUATOR CRACKED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL031276P2858 00852 STRUCTURAL FAILURE (SUPPORT ASSY- FLAP ACTUATOR) PILOT REPORTED FLAPS SELECTED TO 10 DEG, FLAPS OPERATED TO 10 DEG, AT THE NEXT FLAP SELECTION THE FLAP CIRCUIT BREAKER TRIPPED, CIRCUIT BREAKER WOULD NOT RESET. STANDBY FLAP SW WAS NOT USED AND BREAK-AWAY WIRE INTACT. FURTHER VISUAL INSPECTION OF THE FLAP SYSTEM BY MAINTENANCE PERSONNEL FOUND THE FLAP ACTUATOR SUPPORT BRACKETS CRACKED AND BROKEN. 1H71 3T A37CE 20030218002232003021800223NM 2003 2 18 SWAA030288 120030206A3350311500 LENS BOEING737 7373H4 1384600NM FWD ENTRY DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EXIT LIGHT COVER PER MM. 2L72 4F RTA16WE 20030218002722003021800272SO 2003 2 18 C2XA03SH001 120030218A530014522460015 GUSSET EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV-DURING C CHECK THE AFT FLOOR GUSSET WAS FOUND TO HAVE NUMEROUS AREAS OF CORROSION AND GOUGING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030116000312003011600031 2003 1 16 HEEA082988 420030107A2300N0000039 FILTER SKRSKYS76 S76A 8143006NE TRANSMIT LINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 OUTERLINK TRANSMIT LINE FILTER FAILS TO TRANSMIT SIGNALS TO SATELLITE. SHOP REPAIR. 1G72 3U H1NE 20030116000842003011600084 2003 1 16 HEEA083044 420030106A2312064101900 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT FAULTY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035014Y 45219 TRANSCEIVER DISPLAY FAULTY. REPLACED BAD DS506 DISPLAY. ALSO REPLACED BAD DISPLAY LENS. BENCH CHECK GOOD. 1G71 3U H2SW 20030116002232003011600223SW 2003 1 16 HEEA083129 120030108A6220206011105001 BEARING BELL 206 206L3 1182108SW P/C TRUNNION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 RED MAIN ROTOR PITCH CONTROL LINK UPPER TRUNNION BEARING WORN. SCRAPPED. 1G71 3U H2SW 20030226000602003022600060SW 2003 2 26 HEEA084349 120030211A6340407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 DUAL TACH INDICATOR DROPPED TO ZERO IN FLIGHT. (ROTOR NEEDLE) 1G71 3U O H2SW 20030305000142003030500014NM 2003 3 5 2003UALA00224 120030227A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29555UA 26647 STA 600 FUSELAGE EXTERNAL SKIN HAS 3 EA DENTS AND GOUGES ABOVE DOUBLER AT STR 17L. MAJOR REPAIR ACCOMPLISHED. SKIN PANEL WAS REPLACED FROM STA 594 TO 660 BUTT JOINT AND FROM STR 14L SKIN LAP TO STR 19L SKIN LAP, SPLICE DOUBLER AT STA 594. 2L72 4F4 FRTA2NM E17NE 20030307000682003030700068NM 2003 3 7 SWAA030420 120030220A53126446568 BULKHEAD BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED (4 EA) AT 8:00 O'CLOCK POSITION RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA. 2L72 4F A16WE 20030307001512003030700151NM 2003 3 7 AALA20030160 120030205A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21360AA 24041 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 35H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR ON SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030307001682003030700168NM 2003 3 7 AALA20030049 120030119A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21786AN 30250 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT AT SEAT 4G INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY ON SEAT 4G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030311000102003031100010NM 2003 3 11 HNAA0300014 120030307A272085540001005 RUDDER DHAV DHC8 DHC8201 2809001NM TAIL CRACKED A HNAAO OTHER O OTHER ININSP/MAINT 1 EA07989HA175106682 427 Top forward rudder skin has a crack. Repaired rudder skin. 2H72 4T RTA13NM 20030312000592003031200059NM 2003 3 12 AWXA200300252 120030228A53156545834107 STRAP BOEING737 7373G7 1384595NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW0 0 24633 MCN - MAJOR REPAIR - DURING C-14 CHECK A 5/16" CRACK WAS FOUND ON STRAP, LOWER SURFACE OF FLOOR BEAM, BS 328, LBL 16. MAINTENANCE REMOVED DAMAGED AREA OF STRAP; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13, PG. 1-3, FIG. 1. 2L72 4F RTA16WE 20030313000812003031300081GL 2003 3 13 BAQ2003F00000 220030305A72606894171 GEARBOX AGUSTAA109 A109 0260109EU ALLSN 250C 250C20B 03013GL ENGINE MAKING METAL E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA032MF 7277 THE ENGINE WITH SUBJECT GEARBOX STARTED MAKING METAL ON MAINTENANCE RUNS AFTER ENGINE INSTALLATION. METAL FOUND ON GEARBOX CHIP PLUG. AFTER OPENING UP GEARBOX, FOUND UNIDENTIFIED METAL RING INSIDE. NO VISIBLE SIGN OF DAMAGE TO GEAR TRAIN. RETURNED GEARBOX, FOR FURTHER EVALUATION. 1G72 3U3 U H7EU E4CE 20030314000122003031400012EU 2003 3 14 XG3R084839 120030227A6320350A32310121 FRICTION RING UROCOPEC130 EC130B4 EU M/R GEARBOX SCORED H XG3RO OTHER K FLUID LOSS NRNOT REPORTED 1 FS0126LB 442 3514 MAIN TRANSMISSION INPUT SEAL LEAK REQUIRED REPLACEMENT OF THE BAB-DRR SEAL. REPLACED FRICTION RING ALONG WITH SEAL. TO PRECLUDE THE INPUT SEAL FROM LEAKING AGAIN THE FRICTION RING WAS REPLACED AT THE SAME TIME. 1G72 3U H9EU 20030314000932003031400093NM 2003 3 14 SWAA030541 120030309A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030121000372003012100037SW 2003 1 21 HEEA083229 120030108A7810206064300005 EXHAUST PIPE BELL 206 206L3 1182108SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 EXHAUST ASSY CRACKED. REPAIRED. 1G71 3U H2SW 20030317000912003031700091NM 2003 3 17 03FDEA00252 120030304A5510 NUT DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 11R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. 2L73 4F4 FRTA22WE E13NE 20030318002142003031800214SO 2003 3 18 C2XA03IA032 120030313A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714920 145380 During scheduled maintenance the overwing emergency exit lights were found to be inoperative. Maintenance removed and replaced the emergency light battery charger assembly. The emergency light system operationally tested good and the aircraft was approved for return to service. 2L72 4T RTT00011AT 20030122002532003012200253SW 2003 1 22 HEEA083566 120030113A6320206033506101 RESTRAINT BELL 206 206L3 1182108SW BEARING BORE MISREPAIRED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 ONE BEARING BORE NOT CHAMFER TO PROPER DEGREE TO ALLOW BEARING STAKE TO FOLD. 1G71 3U H2SW 20030327001172003032700117SO 2003 3 27 C2XA03CL046 120030220A335066368 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716525 145403 DURING ROUTINE MAINTENANCE THE AFT EMERGENCY AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030325000542003032500054NM 2003 3 25 AWXA200300216 120030301A27512061141 INDICATOR BOEING737 73733A 1384673NM COCKPIT UNRELIABLE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28166AW39679995 23627 ON CLIMB FROM PHX EN ROUTE TO LAX TRAILING EDGE FLAPS SPLIT AND WERE ASYMMETRIC AT 1 AND 2 DURING FLAP RETRACTION FROM FLAP 5 TAKEOFF. TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE LEFT FLAP POSITION INDICATOR CIRCUIT BREAKER POPPED BEHIND FIRST OFFICER SEAT. REPLACED FLAP POSITION INDICATOR IAW BMM 27-58-41-401, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030325000022003032500002NM 2003 3 25 03080406 120030321A5246001D524A100002 PANEL DORNERDO32 DO328300 NM FUSELAGE DEPARTED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27406FJ 3156 DURING CLIMB, THE CREW REPORTED HEARING A LOUD BANG FOLLOWED BY AIRFRAME VIBRATION. THE FLIGHT RETURNED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND THAT THE OXYGEN SERVICE FAIRING PANEL HAD DEPARTED THE AIRCRAFT. THE PANEL WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030417001642003041700164NE 2003 4 17 QXEA0300244 220030208A72304124T3P03 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX2406 10033 GEE965293 NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO BLADES BROKEN, ANOTHER WITH POSSIBLE CRACK. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. 2L72 4F4 FRTA21EA EOOO63EN 20030327001272003032700127SO 2003 3 27 C2XA03CL064 120030222A335074441 SIGN EMB 135 EMB135ER 3260203SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2725504 145186 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN OVER THE SERVICE/GALLEY DOOR WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT SIGN OVER THE SERVICE/GALLEY DOOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040504000212004050400021EA 2004 5 4 A6WA200340096 120030604A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 RIGHT SIDE UNDER FLOORBEAM STRUCTURE IS CRACKED AT FS 621 RBL 33, WL 73 DAMAGED STRUCTURE WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW REO 601R-53-61-004 REV B. (M) 2L72 4F RTA21EA 20030717000172003071700017SW 2003 7 17 HEEA087994 120030620A6711406010413119 TUBE BELL 407 407 1182206SW PITCH LINK CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03491PH3360 53386 CORROSION DAMAGED BEYOND LIMITS DUE TO INADEQUATE PROTECTION DURING MFG PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030717000792003071700079GL 2003 7 17 HEEA088071 220030704A7320P155150GE1A TORQUE SENSOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 INTELLISTART LIGHT. SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030422000952003042200095SO 2003 4 22 SIMA200307901 120030222A532014522461011 GUSSET EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, RIGHT BEAM GUSSET AT FRAME 20 IS CORRODED. REMOVED AND INSTALLED NEW RIGHT BEAM GUSSET AT FRAME 20 IAW EMB 135 SRM 51-20-03, 51-40-02. (M) 2L72 4F RTT00011AT 20040223000702004022300070 2004 2 23 SWIA200312743 420031231A2297 PIN EMB 120 EMB120ER 3260203SO CONNECTOR LOOSE A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07215SW 120281 F/O'S AUTOPILOT DOES NOT CAPTURE GLIDE SLOPE. GS ARM STAYS ILLUMINATED THRU-OUT APPROACH. RE-INSERTED AND SECURED PIN 44 OF P0175 BACK INTO CONNECTOR OF A/P COMPUTER NR 2. OPS CHECK GOOD IAW 22-10-00. 2L72 4T RTA31SO 20030827000062003082700006EU 2003 8 27 03FDEA00956 120030623A5753 CHANNEL AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE T/E FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 MDIS 658 57-10 0006637 21JUN03 BFM CLOSE R COMPLY WITH E.A. 6-5752-70956 WINGS-BASIC-REPAIR OF FLAP TRAILING EDGE (Z CHANNEL) FACT 23JUN03 17:40 BFM R COMPLIED WITH EA NR 6-5752-70956 WINGS-BASIC-REPAIR OF FLAP TRAILING EDGE (Z-CHANNEL) IAW/SRM 51-71-40 PAGE 201. 2L72 4F4 FRTA35EU E13NE 20030826000922003082600092WP 2003 8 26 FRISBY03001 120030226A291041022021 HOUSING DOUG DC9 DC982 3022082WP HYD SYSTEM CRACKED B UFHRO OTHER K FLUID LOSS CLCLIMB 1 SO05IDANV14590 730C 80C369 AFTER TAKE-OFF OF ALITALIA (ALI) MD-80 AIRCRAFT I-DANV(80C369) ON 26 FEBRUARY 2003, AIRCRAFT EXPERIENCED HYDRAULIC FLUID LEAK DURING FLAP RETRACTION. AFTER THE AIRCRAFT LANDED, PTU, P/N 4100310-6, S/N 730C WAS REPLACED. THE SUBJECT PTU WAS RETURNED TO THE MANUFACTURE FOR A FAILURE INVESTIGATION, AND INSPECTION REVEALED THE DRAIN PORT HOUSING, P/N 4102202-1, HAD CRACKED COMPLETELY AROUND THE CIRCUMFERENCE. SUBJECT PTU HAD ACCUMULATED 29,221 FLIGHT HOURS, AND 22,663 CYCLES SINCE NEW. SUBJECT HOUSING HAD ACCUMULATED A TOTAL OF 14,590 HOURS SINCE INSTALLATION IAW S.B. 4100310-29-0031 (AD 92-33-03). 2L72 4F A6WE 20030828000582003082800058NM 2003 8 28 P5CA0300922 120030819A575365B084232 PANEL BOEING747 747200 1384847NM T/E FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 RT IB MID FLAP WITH SIGNS OF DELAMINATION AT MID LWR FLT PANEL. CORRECTIVE ACTION TAKEN: DELAMINATION PANEL REPLACED SRM 51-10-01 / 51-30-02 MM 51-24-11 2L74 4F RTA20WE 20030828001952003082800195NM 2003 8 28 CALA0300467 120030814A5730 PANEL BOEING737 7373T0 1384582NM RT WING DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 INSPECTION FOUND RT WING PANEL UPPER SURFACE DELAMINATED O/B OF MLG. THE PANEL WAS REPAIRED IAW BOEING DRAWING 65-50820-188. 2L72 4F RTA16WE 20030829001122003082900112NM 2003 8 29 SWAA031880 120030821A552365C26384 BEARING BOEING737 7377H4 1384404NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED PM CHECK, SWA SI 11038-55,FOUND RT ELEVATOR TAB HINGE BEARINGS WORN AT NR 1, NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPLACED HINGE BEARINGS AT NR 1, NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2L72 4F RTA16WE 20030829001442003082900144NM 2003 8 29 SWAA031838 120030815A25606557463 CLIP BOEING737 7377H4 1384404NM FWD ENTRY DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29787SA 29812 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER CLIP LOOSE. SECURED RETAINER CLIP PER MM. 2L72 4F RTA16WE 20030723000702003072300070NM 2003 7 23 SWAA031467 120030703A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C2 CHECK, FOUND BOTH SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH SERVICE DOOR LIGHT ASSY'S PER MM. 2L72 4F RTA16WE 20030723000732003072300073EA 2003 7 23 03187674 120030706A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27674BR 7601 DURING MAINTENANCE INSPECTION, THE RT MID EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030723000802003072300080NM 2003 7 23 AWXA200300797 120030616A57206569646111 ANGLE BOEING737 7373Y0 1384671NM NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-14 CHECK .5625 INCH CRACK WAS FOUND ON LOWER LEG OF INBOARD ANGLE IN FLAP WELL OUTBOARD OF THE NR 1 PYLON WS 201.09. MAINTENANCE REMOVED INBOARD ANGLE LT WS 201.09; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-69646; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20030723000532003072300053WP 2003 7 23 GTIA030476 120030515A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 PILOT FLOOR PANEL GOUGE AND BARE METAL. UPON FURTHER INVESTIGATION GOUGE IS A CRACK. FABRICATED PLATE AND DOUBLER. INSTALLED PLATE AND DOUBLER. (M) 2L72 4F A6WE 20030722001272003072200127EU 2003 7 22 AWXA200300652 120030604A3251710TS06Y11 TRANSMITTER AIRBUS320 A320231 3930325EU INSTRUMENT PANELDEFECTIVE A AWXAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 WP28622AW3963315670 054 STEERING FAILURE - BSCU 1 FAULT ON TAXI AIRCRAFT COULD NOT BE STEERED WITH RUDDER PEDALS OR TILLER. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS N/W/S HAND WHEEL TRANSMITTER UNIT (1GC) IAW AMM 32-51-11-401, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN REPORT OF NOSE WHEEL STEERING CONTROLLER S/N 188 CONFIRMED FAILURE OF UNIT. MICRO SWITCH (P/N TS116067) WAS FOUND INTERMITTENT, AND THE PLATE DRIVE, MAIN SPRING (P/N TS116022-4), AND RINGS (P/N TS116095-3) WERE FOUND WORN BEYOND LIMITS. UNIT WAS OVERHAULED PER CMM 32-51-11. 2L72 4F RTA28NM 20030902000882003090200088EA 2003 9 2 SWIA200312137 120030620A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT FALSE ACTIVATIONA SWIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM07438SW 7574 LEFT EMERERGENCY CAUTION LIGHT ILLUMINATED RIGHT AFTER TAKEOFF. WE RAN THE QRH AND DECIDED TO RETURN TO SLC TO VERIFY THE DOOR. INSPECTED LEFT OVERWING ''E'' EXIT SENSOR AND SENSOR PLATES. NO DEFECTS NOTED - OPERATIONAL CHECKS OF PROXIMITY WARNING SYSTEM SATISFACTORY. NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20030902001192003090200119NM 2003 9 2 PCAA0306079 120030612A5347852320490CV553 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13817EX30300 191 DURING (C) CHECK INSPECTION AT MAINTENANCE SERVICES. BARE METAL AND MINOR CORROSION WAS FOUND ON RIGHT INBOARD SEAT TRACK FLOOR FLANGES BETWEEN STA. 182.00 AND STA. 600.00. INSPECTED AND FOUND TO BE OUT OF LIMITS BETWEEN STA. 214.7 AND 216.5. REPAIR DAMAGED AREA IAW DASH-8 REPAIR DRAWING RD8-53-1339 ,MAINTENANCE SERVICES.EAM DOC-22456/1533-01 AND DASH-8 AIRCRAFT STRUCTURAL REPAIR MANUAL. 2H72 4T RTA13NM 20030902001922003090200192NE 2003 9 2 DXTA200300050 220030618A7532674102 BLEED VALVE CESSNA560 560XL 2076702CE PWA 530 PW535A NE ENGINE CLOSED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07801QS 5600601 DURING TAKEOFF ROLL, WINDSHIELD HEAT AND MASTER WARNING ANNUNCIATORS ILLUMINATED. VALVES WERE CLOSED AND SWITCHES WERE OFF. - RAN AIRCRAFT AND DUPLICATE SQUAWK. REMOVED AND REPLACED BLEED AIR VALVE IAW 560 MM CH 30-41-00. 2L72 4F4 FRTA22CE E00053EN 20030904000782003090400078NM 2003 9 4 QXEA200301041 120030820A5720 BRACKET DHAV DHC8 DHC8202 2809007NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- RIGHT HAND LOWER BRACKET AT RIGHT WING STATION 139.00YW IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20030729001432003072900143WP 2003 7 29 ABXA030290 120030704A57553923254503N SUPPORT BRACKET DOUG DC9 DC941 302207NWP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 LEFT INBOARD SPOILER TORSION BAR SUPPORT BRACKET CRACKED AT UPPER END. REPLACED SUPPORT IAW SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20030825000492003082500049NM 2003 8 25 UPS03441130 120030726A5712112U804066 RIB BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RT WING NR 3 NACELLE RIB POST 2EA ATT HOLES FOUND CRACK INDICATION AT FRONT SPAR WEB. NR 3 NACELLE RIB REPAIRED AS PER B747-5720-11421-F AND RT FRONT SPAR WEB REPLACED AS PER B747-5720-11421-F 2L74 4F A20WE 20030821002392003082100239NM 2003 8 21 QXEA200300924 120030718A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- RIGHT HAND OUTBOARD NR 10 SEAT TRACK HAS LIGHT SURFACE CORROSION AT STATION X366.050-376.110. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD R-53-1342. 2H72 4T RTA13NM 20030827001362003082700136NM 2003 8 27 2003UALA00566 120030716A5320 FLOOR SUPPORT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29663UA 27160 CORROSION OUT OF LIMITS ON FLOOR SUPPORT ANGLE AT STA 368. OTBD BY LWR AFT R-2 DOOR ON STRUCTURE. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION. 2L72 4F4 FRTA1NM E24NE 20030910001272003091000127NM 2003 9 10 MWEA030342 120030827A5320993653425 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 PASSENGER ENTRY FLOOR SUPPORT IS CORRODED AT STATION 200 AND IS 11 INCHES LEFT OF AIRCRAFT CENTER LINE. 2L72 4F RTA6WE 20030910001732003091000173SO 2003 9 10 SIMA200321005 120030727A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED A FILLER, EXTERNAL ANGLE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142, REV 22, CHAPTER 53-21-10 FIG 202. (M) 2L72 4F RTT00011AT 20030911001822003091100182WP 2003 9 11 DHL2003806013 120030731A5250 LATCH DOUG DC8 DC873F 302199FWP COCKPIT LACK OF LUBE A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01806DH 46002 COCKPIT DOOR LATCH HARD TO OPEN. LUBED COCKPIT DOOR. OPS CHECKED GOOD IAW MM 52-10-00. 2L74 4F RT4A25 20030911001872003091100187WP 2003 9 11 AALA20030335 120030227A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND DEEPLY BLENDED AREA AT STATION 1429 BETWEEN LONGERONS 3R AND 2R. INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F A6WE 20030929000972003092900097WP 2003 9 29 UPS03841166 120030827A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, INTERCOSTAL BETWEEN STA. 80-100 AT LONGERON 28 RT IS CORRODED BEYOND LIMITS REMOVED,FABRICATED AND REPLACED INTERCOSTAL IAW SRM. 53-3-2 FIG. 5 AND 51-1-20D. 2L74 4F RT4A25 20030926001612003092600161NM 2003 9 26 CALA0300506 120030830A5310 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND FORWARD BAGGAGE BIN SKIN SHEAR TIE CORRODED AT STA 460, S28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR DOUBLER AND SHEAR TIE WERE INSTALLED IAW SRM 53-00-07. 2L72 4F RTA16WE 20031001000432003100100043WP 2003 10 1 UPS03841188 120030810A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, CORROSION ON FLOORBEAM UNDER SIDE AT STA 1660 LBL 38.5 REMOVED CORR IAW DC8 SRM 51-1-8. MAT'L REMAINING 0.00 FROM .125 FOUN D OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR AN GLE AND FILLERS IAW DC8 SRM 53-2-0 FIG 1B & TR 53-124. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE AND FILLERS IAW DC 8 SRM 53-2-0 FIG 1B AND TR 53-124. 2L74 4F RT4A25 20030908001602003090800160SO 2003 9 8 SWIA200312235 120030803A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO CABIN DISCHARGED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07298SW 120328 FORWARD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FWD EMERGENCY BATTERY PACK IAW 33-50-02. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030908002702003090800270SO 2003 9 8 SWIA200312361 120030826A3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203SO LT MLG OUT OF ADJUST A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07232SW 120306 UPON SELECTING GEAR DOWN RIGHT MAIN EXTENDED NORMALLY, NOSE GEAR ABOUT 5-10 SECONDS LATER, LEFT MAIN INDICATED RED LIGHTS ONLY THEN NORMAL AFTER 45 SECONDS TO 1 MINUTE, THE GEAR WAS FELT THUD COINCIDING WITH GEAR DOWN INDICATION. ADJUSTED LEFT OUTBOARD SEQUENCE VALVE. OPS CHECKS GOOD. 2L72 4T RTA31SO 20030909002032003090900203EA 2003 9 9 JBXA03016 120030731A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNSECURE A JBXAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO05592ML 7410 FLIGHT 5197 FROM BHM TO DCA RETURNED TO FIELD DUE TO AN OUTER PAX DOOR HANDLE MESSAGE. FOUND HANDLE IMPROPERLY STOWED. OPS CHECKED GOOD. AC RETURNED TO SERVICE. 2L72 4F RTA21EA 20030909002152003090900215WP 2003 9 9 ABXA030331 120030808A531359114279 LONGERON DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 LONGERON 17 CRACKED ON AFT SIDE OF BULKHEAD FS 965. REPLACED LONGERON IAW DC-9 SRM. 2L72 4F A6WE 20031002000852003100200085NM 2003 10 2 C1HA200386001 120030908A5313 STRINGER BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 CORROSION ON STRINGER 29 LT AT BS 950B+8. 2L73 4F A3WE 20031014001602003101400160 2003 10 14 SWAA032067 420030917A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031021001052003102100105EU 2003 10 21 A6WA200360042 120030924A5313 STRINGER BAC 146 146200A 1500266EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 FOUND STRINGER 33 LEFT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101. REV AVMAX NON-ROUTINE 1204 FOR REPAIR. REPAIRED STRINGER IAW SRM 53-00-12 FIG 207. (M) 2H74 4F A49EU 20031028001102003102800110 2003 10 28 KBM2003F00005 420030725A34225050031904 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19270SH 1864 DIRECTIONAL GYRO IS INOPERATIVE. REPLACED WITH SERVICEABLE D.G. 1G71 3U3 UNCH9EU E19EU 20031029000382003102900038NM 2003 10 29 ASAA0340084 120030228A53206573746 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR SUPPORT BS 773 RBL 8 WL 152. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20031029001322003102900132NE 2003 10 29 KBM2003F00027 220030904A74219550175400 IGNITER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE RIGHT ERRATIC E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P1091 2347 4126 IGNITER WORN AND OPERATING ERRATICLY. REPLACED RT IGNITER WITH NEW.(K) 1G71 3U3 UNCH9EU E19EU 20031105000882003110500088NM 2003 11 5 2003UALA00804 120031027A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 STA 986 RBL 28 CABIN FLOORBEAM T-CAP HAS CORROSION ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031106001652003110600165NM 2003 11 6 03FDEA01853 120031021A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RIGHT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), HINGE LUG OUTBOARD HOLE FOUND CORRODED. 2L73 4F RTA22WE 20031110001692003111000169NM 2003 11 10 03FDEA01871 120031105A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 WHILE WORKING CARD NR N01362, FOUND CORROSION ON FLOORBEAM STA 312, RBL 14, WL 208. FLOORBEAM AT BS 312 WAS OUT OF LIMITS. REMOVED DAMAGED BEAM & REPAIRED. INSTALLED NEW SECTION PER SRM 53-10-8 FROM RBL 14 TO LBL 65. 2L73 4F RTA3WE 20031110001882003111000188 2003 11 10 SWAA032233 420031010A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20030917001002003091700100CE 2003 9 17 2003F00561 120030806A712012991004717 TRUSS BEECH 1900 1900D 1154162CE ENGINE CRACKED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1969549 UE194 AT SCHEDULED MAGNUFLUX INSPECTION, ENGINE TRUSS WAS DETERMINED TO HAVE A RADIAL CRACK IN THE LOWER RIGHT GUIDE PIN RADIUS. RAYTHEON AIRCRAFT COMPANY, THE MANUFACTURER, DETERMINED THAT THE BOSS GUIDE WAS NOT REPAIRABLE AND THAT ITS REPLACEMENT WOULD REQUIRE USE OF THE PRODUCTION JIG. NO REPAIR WAS AUTHORIZED. ENGIEN TRUSS WAS REPLACED WITH SERVICEABLE UNIT. (M) 2L72 4T RTA24CE 20030917001242003091700124NM 2003 9 17 F3LA200300123 120030801A5210 SNUBBER BOEING737 7373L9 1384470NM PAX DOOR INOPERATIVE A F3LAK NONE O OTHER ININSP/MAINT 1 NM03313FL 3452 26442 DURING C-3 CHECK, INSPECTION REPORTED R-1 DOOR LOCK PIN INOPERATIVE. ADJUSTED SNUBBER ON R-1 DOOR PER MM 52-41-00, PAGE 504, STEP 5. 2L72 4F RTA16WE 20040109000582004010900058NM 2004 1 9 TSAA0253252 120030114A5330 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 CUT OUT DAMAGED SKIN AREA AT BS 520 MAINTAINING A .50 INCH MINIMUM RADIUS AND 2D EDGE MARGIN. VERIFIED EDGE OF TRIM USING HFEC METHOD. ENLARGED TRIMMED AREA BY .04 INCH AS AN INSURANCE CUT. FABRICATED TWO .063 INCH STRUCTURAL FILLERS AND A .071 INCH DOUBLER FROM 2024-T3 CLAD MATERIAL. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER. INSTALLED REPAIR PARTS, HI-LOCKS AND RIVETS WET WITH BMS 5-95 SEALANT BETWEEN THE FAYING SURFACES. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES. REPAIR COMPLETED IAW ECO 3324, FIURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040113000412004011300041EU 2004 1 13 AALA20031461 120031221A2450 CIRCUIT BREAKER AIRBUS300 A300B4605R 3930308EU COCKPIT FAULTY A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2114065 508 SJU T1218/21 EN ROUTE SJU-JFK GOT AC BUS ONE OFF LIGHT ON OVERHEAD ELECTRICAL PANEL AND LOSS OF ASSOCIATED AIRCRAFT ELECTRICAL SYSTEMS. RETURNED SJU AND LANDED WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER 5XN FOR NORMAL BUS ONE SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20031118000702003111800070EU 2003 11 18 XNOA01158 120031008A2997 CONNECTOR AIRBUS300 A300B4203 3930306EU HYD PUMP DIRTY A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23372PC 196 DURING ENG START & TAXI BLUE PUMP PRESS LOW LT STAYED ON, THEN HYD QTY LOSS OCCURRED & RETURNED TO BLOCKS. QTY STABILIZED AT BOTTOM OF GREEN ARC. CLEANED & RESECURED CONNECTOR AT ENG DRIVEN PUMP. SERVICED HYD SYS HEAD PRESS & HYD FLUID QTY, PUMP OPS CK NORMAL & NO LEAKS NOTED IAW A300 AMM 29-10-00. 2L72 4F RTA35EU 20031120001022003112000102WP 2003 11 20 ZW0A0306301 120030922A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139407R 49400 A FUSELAGE DENT WAS FOUND IN SEMI-CRITICAL AREA BEYOND MM LIMITS 34-11-01, PAGE 228, PARAGRAPH C.2 DENT IS 0.017 AT 4.25 INCHES RT ALTERNATE STATIC PORT. REPAIRED RT ALT STATIC PORT IAW SRM 53-04, FIG 12C. CHECK-C 3-26-03 STL. --CLOSED-- 2L72 4F RTA6WE 20040112001602004011200160WP 2004 1 12 GTIA030998 120031115A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND R1 DOOR THRESHOLD AREA CORRODED AT FS 168-200 57 INCHES RBL. FOUND CORROSION ON FLOOR SUPPORT AT FS 154-200 RBL 52 INCHES. FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED NEW SUPPORT. (M) 2L72 4F A6WE 20040113001962004011300196SO 2004 1 13 RAIA00312307 120031208A325013BF7184 POTENTIOMETER EMB 145 EMB145LR 3260212SO NLG STEERING DEFECTIVE A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03816HK 145055 STL- NWS INOP. MAINTENANCE REMOVED AND REPLACED RUDDER PEDAL POT. 2L72 4T RTT00011AT 20031219001522003121900152NM 2003 12 19 03FDEA02138 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORRODED. RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-08 AND DWG ARC0502 AND FEDEX EA 1-5750-73358, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031218001182003121800118NM 2003 12 18 2003UALA00909 120031125A5340 STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29370UA 24539 TIE STRAP CRACKED AT STR 10R BS 663. MAJOR REPAIR ACCOMPLISHED. REPLACED TIE STRAP. 2L72 4F4 FRTA16WE E2GL 20031223001472003122300147CE 2003 12 23 DXTA200300195 120031125A2710666000162 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS BROKEN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07652QS 5605152 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031229000522003122900052NM 2003 12 29 AALA20031424 120031212A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21360AA 24041 EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 33HJ. REPAIRED BROKEN WIRE AT LOWER SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20031229001152003122900115NM 2003 12 29 SWAA032721 120031213A29101U1234 VALVE BOEING737 7373Q8 1384670NM HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29689SW 23387 AFTER TAKEOFF LOST A SYSTEM HYDRAULIC PRESSURE. RETURNED TO BNA FOR LANDING. REMOVED AND REPLACED MANUAL SHUTOFF VALVE PER MM. 2L72 4F RTA16WE 20040105000332004010500033NM 2004 1 5 DL76L031016 120031115A2121211002939 FAN BOEING767 767332 1382001NM RECIRCULATION FAILED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27190DN 28447 TAKEOFF ABORTED AT 120 KTS. F/A REPORTED STRONG ELECTRICAL FUMES EMANATING FROM RT SIDE OF MID GALLEY. INSPECTED GALLEYS EQUIPMENT PACK BAY 1 AND 2 AND BOTH ENG, NO ODORS NOTED. AT DEPARTURE CAPT REPORT RT RECIRCULATION FAN INOP. PER PRECAUTION DEACTIVATED RT RECIRC FAN PULLED AND SECURED. REPLACED RT RECIRCULATION FAN. OPS NORMAL. 2L72 4F RTA1NM 20031231001302003123100130NM 2003 12 31 AWXA200301633 120031203A5754 SKIN BOEING737 737301 1384611NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK THE LT WING NR 3 SLAT WAS FOUND DELAMINATED AT OUTBOARD UPPER TRAILING EDGE, SLAT STA 329.75. MAINTENANCE REMOVED DELAMINATED SECTION OF SKIN AT OUTBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TO SLAT SKIN IAW B737-300 SRM 51-70-10, FIG 1, 5, & 16, PG 1, 31, 33, 41, 43-44, & 67-69. 2L72 4F RTA16WE 20040105001262004010500126NM 2004 1 5 SWAA032765 120031218A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 847, LBL 17, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031014000542003101400054 2003 10 14 SWAA032180 420030930A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031014000912003101400091NM 2003 10 14 SWAA032211 120031004A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E - 2, ABOVE STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040105000042004010500004NM 2004 1 5 DL757030995 120031109A5754 SKIN BOEING757 757232 1384965NM LT WING SLAT GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 NR 2 SLAT GOUGED. COMPLETED PERMANENT REPAIR PER SRM 51-70-10D REF SRM 57-43-02D. C/W PERMANENT REPAIR ON OPN 1000 CARDS 1135-1143. 2L72 4F RTA2NM 20040108001082004010800108EU 2004 1 8 KBM2003F00058 120031013A2121900A6044 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE CONDENSER FAN INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV33 3296 A/C BLOWS WARM AIR. INSTALLED REPAIRED MOTOR. 1G71 3U3 U H9EU E19EU 20040109000222004010900022NE 2004 1 9 MEX2003399 220030829A732078360018072 EEC BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23301AM24261 30045 AIRCRAFT RETURNED TO PLATFORM , DURING TAXI, RT ENGINE SHUT OFF SLOWLY. DURING REVISION WERE DETECTED EICAS MESSAGES R ENG FUEL SOL, R ENG OIL PRESS. R ENG PRI CONT AND R ENG SEC CONT. THE ENGINE WAS CHECK FOR CONDITION AND DETECTING FLAME EVIDENCE IN TURBINE SECTION, THE MOTOR WAS MOTORIZED. AIRCRAFT WAS SENT TO HANGAR. THE RT ENGINE FUEL CONTROL AND EEC WERE REPLACED IAW MM 73-21-01 AND 04, ALL TESTS CORRECT.(K) 2L72 4F4 FRTA2NM E17NE 20040112000112004011200011NM 2004 1 12 USAASB03214 120031213A335020121 POWER SUPPLY BOEING737 7373B7 1384580NM EMERGNECY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19371US 22950 MAINTENANCE REPORTED THE LT OVERWING HATCH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040114001742004011400174EA 2004 1 14 MASA200300404 120031011A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA E/E BAY INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727172 7172 ASH 2835 PHL- THREE SECTIONS OF THE EMERGENCY ESCAPE PATH LIGHTING WERE INOP. MECHANIC REPLACED THE NR 3 INVERTER. OPS CHK GOOD. 2L72 4F RTA21EA 20031125000612003112500061WP 2003 11 25 DHL2003802516 120031115A5712 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 LEFT WING L/E FORMER L/E CRACK 0.500, STA XFS 616.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031202000562003120200056EU 2003 12 2 USAASA03122 120031017A3240C20216332292C CONTROL UNIT AIRBUSA319 A319112 3930323EU BRAKE SYSTEM FAILED A USAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA19764US8316 1369 ON TAXI OUT, CREW RECEIVED THE MASTER WARNING NR 2 BRAKES, AND LOST BOTH NOSE WHEEL STEERING AND BRAKES. BOTH RETURNED APPROXIMATELY TEN SECONDS LATER, RESULTING IN A VIOLENT STOP AND THE INJURY OF THREE FLIGHT ATTENDANTS. MAINTENANCE PERFORMED BITE OF THE BSCU, BRAKE STEERING CONTROL UNIT, AND FOUND THE NR 1 CHANNEL FAILED AND THE NR 2 CHANNEL NOT PICKING UP THE LOAD. THE BSCU WAS REPLACED. (M) 2L72 4F RTA28NM 20031202000862003120200086EA 2003 12 2 ASOA03524 120031018A5320601R3111353 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING A C-CHECK IN MCN, THE BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKETS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20031202000992003120200099NM 2003 12 2 USAABB03184 120031010A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT WILL NOT TEST A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 6, 13, 18, 23, 26, 29 AND 33 NOT TESTING PROPERLY. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031203000542003120300054NM 2003 12 3 GAIA03146ST 120031024A53117075T6 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME DENTED IN RADIUS BS 560 ABOVE STR 17 RT. REF FASI N/R NR CUT OUT DAMAGE 1 INCH BY 1 INCH, INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20040120000312004012000031NM 2004 1 20 03FDEA02295 120031226A5350AKC75436 STIFFENER DOUG MD11 MD11 3023602NM ZONE 300 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT TAIL CONE TOP MOST HORIZONTAL STIFFENER BELOW THE UPPER DOOR HINGE ASSY FOUND CHAFED AT ITS END AREA. RT TAILCONE TOP MOST STIFFENER BELOW UPPER DOOR HINGE BEAM REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II AND DWG AKC7543. 2L73 4F RTA22WE 20031208001792003120800179WP 2003 12 8 ABXA030399 120031008A533059114065 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 FUSELAGE SKIN HAD 1.5 INCH TEAR/CRACK IN SKIN FORWARD ENTRANCE DOOR CUTOUT FORWARD SIDE BETWEEN STOP F4 AND F5. REPAIRED AREA IAW REA D953-48357MR. 2L72 4F A6WE 20031209002052003120900205SO 2003 12 9 SWIA200312555 120030930A5720 CLIP EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07565SW 120340 FOUR CRACKED SKIN SUPPORT CLIPS ON RT WING, RIB 15 LOWER SURFACE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FOUR SKIN SUPPORT CLIPS ON RIGHT WING, RIB 15 LOWER SURFACE PER SRM 51-40-02 AND RII 57-301. 2L72 4T RTA31SO 20031209001472003120900147NM 2003 12 9 QXEA200301362 120031026A5420 ANGLE DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 SEALING ANGLE FOR LOWER COWL ABOVE OIL COOLER IS CHAFED ON INBOARD ANGLE SIDE. REPAIRED IAW DHC-8 RD 8-54-967. 2H72 4T RTA13NM 20031210001382003121000138WP 2003 12 10 AALA20031346 120031130A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217540A 49994 DTW) EMERGENCY EXIT LIGHT ABOVE FORWARD OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT ABOVE FORWARD OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031020002972003102000297NM 2003 10 20 2003UALA00725 120030929A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29379UA 24654 SKIN LAP REPAIR AT STA 328 AND STR 24R. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030915001152003091500115WP 2003 9 15 ANCF200300023 120030904A3220 STRUT DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED W ANCFA UNSCHED LANDING O OTHER CLCLIMB 1 SO23190AN 53190 DURING TAKE OFF NOSE STRUT DIDN´T WORK NORMAL, AFTER TAKE OFF WHEN GEAR HANDLE WAS SWAS UP, NOSE GEAR DIDN´T LOCK AND A STRONG NOISE WAS FELT. THE SEALS WERE REPLACED ON NOSE GEAR STRUT. SERVICE OLEO NEUMATIC WAS ACCOMPLISHED IAW AMM 32-21-02 PAG 801 AND AMM 32-21-02 PAG 301 2L72 4F RTA6WE 20030922000822003092200082NM 2003 9 22 AWXA200300959 120030805A5315D5347218920200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y1162 FLOORBEAM AT FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1162 FLOORBEAM FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 53-00-14, PG. 105-106, PARA 4B, FIG. 102. 2L72 4F RTA28NM 20030924000742003092400074NM 2003 9 24 2003UALA00632 120030804A5754114T411122 WEDGE BOEING BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 12 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29618UA 00055 21878 T/E WEDGE DELAMINATED. T/E WEDGE REPLACED. 2L72 4F4 FRTA1NM E3NE 20040128000322004012800032NM 2004 1 28 DHL2003748014 120031223A3150 WARNING SWITCH BOEING727 727225 1384077NM STABILIZERS MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01748DH 22440 RTO - DUE TO T/O WARNING HORN SOUNDING AT 1.4 EPR, AIRSPEED WAS ZERO, TRIM WAS IN GREEN ARC, FLAPS SET TO 15 DEGREES, AND SPEEDBRAKE STOWED. REMOVED AND REPLACED UPPER STAB WARNING SWITCH IAW 727 M/M CHAPTER 31-26-24. OPS CHECKED GOOD. 2L73 4F A3WE 20040129001282004012900128NM 2004 1 29 DHL200374250 120031123A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM LBL 50 - RBL 50 WL 208, AS VIEWED FROM NWW DOGHOUSE AREA. REMOVED 9G BULKHEAD, FLOORBOARDS AND SHEAR WEB FOR ACCESS IAW B727 SRM 51-30-2 AND MM 53-20-11. REMOVED DAMAGED UPPER CHORDS BS 344 AND FABBED NEW FROM BAC 1505-29222 PO 3348139 DIM 11.75 INCH LONG IAW B727 SRM 51-20-1 & 53-10-2 FIG 7. NEW CHORD TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 51-30-2. REINSTALLED SHEAR WEB, FLOORBOARDS AND 9G BULKHEAD IAW B727 SRM 51-30-2 & MM 53-20-11. 2L73 4F A3WE 20040130002042004013000204WP 2004 1 30 ABXA040017 120031223A524099115799 BEAM DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 FORWARD RIGHT SERVICE DOOR HAD A CRACK ON UPPER HORIZONTAL BEAM FORWARD END. REPAIRED UPPER BEAM OF SERVICE DOOR IAW DC-9 SRM 52-05. 2L72 4F A6WE 20040203000262004020300026NM 2004 2 3 ASAA0310525 120030906A3350S106 BATTERY BOEING737 7372Q8C 138448SNM EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 ANC - DURING SCHEDULED MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT THE R2 DOOR WILL NOT ILLUMINATE. REPLACED BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M) 2L72 4F A16WE 20040205000942004020500094 2004 2 5 GLBA2003156 420031122A3414 INDICATOR BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM03247GL UE247 FO'S AIRSPEED FAILED TO WORK ON TAKE OFF, REMOVED AND WARMED FO'S AIRSPEED IND PN1303800057 INSTALLED ASI RUN UP ON PITOT STATIC TEST OPS CK GOOD. 2L72 4T RTA24CE 20040204000882004020400088NM 2004 2 4 QXEA200301289 120031007A5260 SILL DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-CORROSION AROUND AIRSTAIR DOOR SILL NUT PLATES FORWARD OF AFT HINGE TO FORWARD OF FORWARD HINGE. REPAIRED IAW DHC-8 SRM 51-10-16, SRM 51-20-36 AND SRM 51-40-00. 2H72 4T4 TRTA13NM E20NE 20040217001892004021700189EU 2004 2 17 CX7A194J0359 120031216A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE ILLUMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03307CE 340B204 LT TAILPIPE HOT LIGHT ILLUMINATED. ABORTED T/O. 2L72 4T RTA52EU 20040226000212004022600021NM 2004 2 26 ASAA0370003 120030404A5320143A948535 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01607AS 29751 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT AFT BULKHEAD OF FORWARD CARGO AREA. REPLACED FLOOR SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20040301000192004030100019 2004 3 1 KBM2004F00016 420031223A34215040017901 GYRO SNIAS 350 AS350BA 8680817EU ATTITUDE IND INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P738 2347 INDICATOR SHOWS 30 DEGREES NOSE DOWN AND 15 DEGREES RT BANK IN LEVEL FLIGHT, REMOVED AND REPLACED.(K) 1G71 3U NCH9EU 20040316000182004031600018NM 2004 3 16 ASAA0370015 120031020A5320146A75036 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01617AS 30542 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT RAIL. SPLICED FLOOR SUPPORT RAIL PER SRM. (M) 2L72 4F RTA16WE 20031217000012003121700001EU 2003 12 17 038191 120031113A2701 CONTROL COLUMN SAAB SF340 SF340A 7850100EU COCKPIT VIBRATION A UHLAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL1719XS 340A019 SHORTLY AFTER TAKEOFF CREW EXPERIENCED SEVERE FLIGHT CONTROL VIBRATION PRIMARILY IN THE PITCH AXIS AND SOME IN ROLL, A MECHANIC WAS IN THE JUMPSEAT AND COMFIRMS THE YOKES WERE VIOLENTLY VIBRATING. CAPT REPORTED IT FELT LIKE HE WAS FIGHTING THE AUTOPILOT. AUTOPILOT WAS NOT ENGAGED, AND WAS ON MEL FOR FERRY FLIGHT TO FWA. 2L72 4T RTA52EU 20031215000492003121500049NM 2003 12 15 2003UALA00830 120031103A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29373UA 24638 STR SPLICE IS CRACKED ON STR 4L AT STA 907. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20031217000122003121700012NM 2003 12 17 CALA0300655 120031120A5420 STRAP BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND A 6 INCH CRACK IN I/B STRAP ON NR 1 PYLON AT STA 363.5. REPAIRED IAW ECRA 5421-01002. 2L72 4F RTA16WE 20030926001472003092600147EU 2003 9 26 AWXA200301008 120030901A7500 CONNECTOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE PRESS REGULATOR DAMAGED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28646AW35736 271 EN ROUTE, AFTER TAKEOFF BLEEDS OFF RECEIVED ECAM MESSAGE NR 2 ENG BLEED ABNORMAL PRESS. TURNED OFF APU BLEED SWITCH NR 2 ENG BLEED ONLY AT 24 PSI, DIVERTED FOR REPAIR. MAINT REMOVED AND REPLACED BLEED PRESS REG VALVE CTRL SOLENOID (10HA2), DUE TO CLASS 3 FAULT ALSO REPLACED BLEED PRESS TRANSDUCER (8HA2) IAW AMM 36-11-16. CONNECTOR AT BLEED PRESS REG VALVE CONTROL SOLENOID (10HA2) WAS FOUND DAMAGED AND LOOSE, REPLACED CONNECTOR AND BACKSHELL IAW ESPM 20-53-51. LEAK AND OPERATIONAL CHECKS WERE GOOD, NR 2 BLEED AT IDLE IS 22 PSI, 32 PSI AT 35 PERCENT N1, AND 42 PSI AT PRV REGULATION, OPENS AT 8 PSI, NO LEAKS NOTED. PART NAME; BLEED PRESS TRANSDUCER, MFG; LABEM SA, P/N; ZRA1990030. 2L72 4F4 FRTA28NM E311NE 20030929000172003092900017NM 2003 9 29 373PA0021 120030828A5330 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 SKIN CRACKED AT FWD E&E EQUIPMENT COOLING DUCT. REPAIRED PER BOEING SB 737-53-1117. 2L72 4F RTA16WE 20040917000632004091700063NM 2004 9 17 2004F00329 120031215A3397W3532003622 WIRE BOEING757 757236 1384971NM L2 DOOR LIGHT BROKEN A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11521NA 25592 EMERGENCY EGRESS LIGHTS OVERHEAD OF ROWS 10, 12 AND 14 ILLUMINATE INTERMITTENTLY WITH THE COCKPIT SWITCH IN THE ARMED OR OFF POSITION. REPAIRED BROKEN WIRE TERMINAL AT TEST PUSH BUTTON OVER THE L2 DOOR IAW BMM 20-00-00. EMERGENCY LIGHTS TESTED GOOD. (M) 2L72 4F RTA2NM 20040915001402004091500140NE 2004 9 15 2004F00342 220031230A7320FFG021BH GOVERNOR BOEING757 757236 1384971NM RROYCERB211 RB211535E4 54555NE RT FUEL FLOW FAILED A P9RAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SO11521NA 25592 30924 AT FLIGHT LEVEL 350, JFK-POS - RIGHT ENGINE ROLLED BACK. ALL PARAMETERS EXCEPT EPR, WHICH WENT HIGH AND EVENTUALLY DISAPPEARED. PRESSURE TESTED P1 PROBE LINES, ACCOMPLISHED WIRING CONTINUITY CHECKS ON RIGHT ENGINE EEC TO EPR TRANSMITTER. ALL CHECKED GOOD. AIRCRAFT FERRIED POS TO MIA FOR FURTHER TROUBLESHOOTING ON 12/31/03. TROUBLESHOOTING CONTINUED. REMOVED AND REPLACED RIGHT EPR TRANSMITTER IAW BMM 71-00. GROUND RUN CHECKED GOOD. PERFORMED ACCEL/DECEL CHECK ON RIGHT ENGINE. NO DISCREPANCY NOTED. JFK - REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR. REMOVED AND REPLACED RIGHT FFG IAW BMM 73-21-01. (M) P9RA 2L72 4F4 FRTA2NM E12EU 20050816001212005081600121NM 2005 8 16 SWAA032608 120031126A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D-CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED AT BS 867, STR 8L, BS 360, STR 8R AND BS 787, STR 8R. REPAIRED FRAMES PER BFG ER. 2L72 4F RTA16WE 20060731000152006073100015WP 2006 7 31 IXXA060474S 120030209A5753 PANEL DOUG DC8 DC871F 302199DWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND LEFT FLAP ICE BREAKER PANEL CRACKED AT STATION XF219. REPAIRED PER TIMCO EO REO609034 AND DC8 SRM 51-3-0. 2L74 4F RT4A25 20040121000762004012100076EU 2004 1 21 ASOA03616 120031106A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN BNA, THE LT AND RT SEAT TRACKS BETWEEN FRAMES 36 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT SEAT TRACKS BETWEEN FRAMES 36 AND 39 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20031124000932003112400093WP 2003 11 24 DHL2003807502 120031008A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 VERTICAL STAB INTERIM REPAIR ON L/E LEFT UPPER SIDE, STA ZFS 350.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 55-2-1 FIG 14, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040311000402004031100040NM 2004 3 11 ASAA0310141 120030316A7110170030121 FRAME BOEING737 737298C 1384490NM NR 2 COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 210-264 CRACKED. REMOVED AND REPLACED COWL FRAME PER SRM. (M) 2L72 4F RTA16WE 20031203000772003120300077EA 2003 12 3 2003F00627 120030202A5610NP1393225 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A FDKAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07503MJ 10058 RETURNED TO FIELD FOR CAPTAINS WINDSHEILD CRACKED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD. (M) 2L72 4F RTA21EA 20031204000262003120400026EA 2003 12 4 A6WA200340140 120031006A2421 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31436AW 7734 ABORTED TAKEOFF AT 70 KNOTS WITH IDG NR 2 CAS MESSAGE. SERVICED IDG NR 2 IAW AMM 12-13-24, SERVICE APPROXIMATELY 2 QUARTS. (M) 2L72 4F RTA21EA 20031204000302003120400030WP 2003 12 4 AMTA200301277 120030815A5754 SKIN LKHEED1011 10113851 5265010WP NR 7 SLAT DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FOUND 7R SLAT SKIN DENTED AT OUTBOARD LEADING EDGE. REPAIRED SLAT SKIN IAW SRM 57-51-00, FIG 807. (M) 2L73 4F A23WE 20040120000522004012000052NM 2004 1 20 03FDEA02288 120031229A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING, O/B FLAP I/B HINGE FITTING I/B PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200. WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031210000172003121000017NM 2003 12 10 XNOA1167 120031203A2697 WIRE BOEING727 727200 138407ENM OVERHEAT LOOP CHAFED A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23793A 20774 ON TAXI OUT AFT LOWER BODY OVERHEAT ILLUMINATED. REPAIRED CHAFED WIRE AT LOWER BODY HEAT LOOP, STAIRWELL POS, IAW B727MM 26-14-0. OPS CHECK NORMAL. 2L73 4F RTA3WE 20031209001722003120900172WP 2003 12 9 ABXA030412 120031014A57129919327503 RIB DOUG DC9 DC932 3022066WP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 END OF LEADING EDGE RIB RIGHT WING CRACKED AT STA 353. REPAIRED DAMAGED RIB IAW DC-9 SRM 57-06. 2L72 4F A6WE 20031211000722003121100072NM 2003 12 11 03314402 120031110A2120001D904A1200006 RELAY DORNERDO32 DO328300 NM COCKPIT FAILED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27402FJ 3147 DURING TAXI TO GATE THE FLIGHT CREW REPORTED SMOKE IN THE AFT CABIN AREA. PASSENGERS WERE DEPLANED AT GATE. THE PROBLEM WAS TRACED BACK TO SPEED SENSOR RELAY ON 20VE PANEL. IT WAS VERIFIED BY THE PITOT STATIC SYSTEM TEST WHICH CAUSED HX FAN TO INTERMITTENTLY SHUT OFF AT AIRSPEEDS OF LESS THAN 120 KNOTS. 2H72 4T RTA55NM 20030916001012003091600101EU 2003 9 16 ASOA03384 120030724A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING A C-CHECK IN BNA, THE AFT CENTER SEAT TRACK FROM FS 39-41 IAW SRM 51-25-04. (M) 2H72 4T RT 20030917000792003091700079EU 2003 9 17 BAQA089101 120030911A6330L633M2010105 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135QC17 0281 MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030922000902003092200090CE 2003 9 22 K5LA620J 120030805A3230V31 SAFETY SWITCH BEECH 200 A200 1152921CE PWA PT6 PT6A41 52043EA MLG BROKEN E K5LAO OTHER O OTHER NRNOT REPORTED 1 EA05636B BC61 AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. GEAR REMAINED DOWN AND LOCKED. AFTER LANDING IT WAS DETERMINED A WIRE ON THE LANDING GEAR EMERGENCY SAFETY SWITCH HAD BEEN BROKEN OFF DURING INSPECTION AND LUBE OF NOSE GEAR CHAIN. JACKING THE AIRCRAFT AND DOING A RETRACT CHECK AFTER LUBING THE CHAIN OR ANY TYPE OF GEAR WORK WOULD PREVENT THIS. 1L72 4T4 T A24CE E4EA 20030923000562003092300056WP 2003 9 23 DHL2003604711 120030611A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FUSELAGE NOSE SECTION EXTERIOR SKIN CRACKED 0.825 AROUND AFT LOWER JAMB OF RAM AIR EXHAUST DOOR STA FS 12.000, L-27L. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END (0.250) DIA IAW EODHL-030548, ED-3383. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (2024-T3 AL0.071) IAW EODHL-030548, ED-3383. CLEANED, TREATED AND PRIMED DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON FUSELAGE NOSE SECTION EXTERIOR SKIN STA FS -12.000, L-27L WITH NEW FASTENERS IAW EODHL-030548, ED-3383, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030925000162003092500016EA 2003 9 25 ASOA03409 120030901A3610KMM67080001001 BRACKET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11712EV 10074 DURING A HANGAR CHECK IN BTR, THE LT ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 IAW ASA EO 700-36-0003B. (M) 2L72 4F RTA21EA 20030716000922003071600092NM 2003 7 16 USAABB03091 120030614A33509221009 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 MCO - FOUND EXIT IDENTIFIERS AT DOORS L3, L4 AND R4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030127000822003012700082SW 2003 1 27 HEEA083653 120030114A282070079H100F210 HOSE BELL 407 407 1182206SW FUEL DIST KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 FUEL HOSE ASSY KINKED. 1G71 3U O H2SW 20030128000532003012800053 2003 1 28 HEEA083806 420030116A34424000038 CONTROL HEAD BELL 407 407 1182206SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 WHEN KEY DID NOT GET FORWARD AND REVERSE POWER. FOUND SWITCH S2, VOLUME KNOB AND FACEPLATE BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1G71 3U O H2SW 20030205001332003020500133NM 2003 2 5 DL76L030040 120030109A733042D356 TRANSMITTER BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27197DN 28454 727678 AFTER T/O AND REACHING FL230 GOT EICAS CAUTION MSG, RT ENG FUEL FILTER. NO CHANGE WITH POWER REDUCTION. REPLACED FUEL FILTER AND PRESSURE TRANSMITTER. 2L72 4F4 FRTA1NM E24NE 20030207000152003020700015NE 2003 2 7 DLM88030047 220030112A7261 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 LEAKING A DALAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27965DL 49984 718039 ON CLIMB OUT, SMOKE VISIBLE WITH SMOKE DETECTORS AUDIBLE IN CABIN AT FL 230. PACKS NORMAL TEMPS. FOUND INTERNAL OIL LEAK ON NUMBER 1 ENGINE - REPLACED SAME. 2L72 4F4 FRTA6WE E9NE 20030210001192003021000119NM 2003 2 10 QXEA0300064 120030111A5320 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- PANEL 262HT FORWARD BOTTOM FLANGE IS CHAFFED ON THE ENTIRE LENGTH. REPAIRED IAW HORIZON AIR EA 6-53-173 AND DHC-8 400 TASK 51-00-02-250-801. 2H72 4T RTA13NM 20030210001352003021000135WP 2003 2 10 CALA0300027 120030209A5313 LONGERON DOUG DC9 DC982 3022082WP STA 1418 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0972822 49482 INSPECTION FOUND A 2" CRACK IN LONGERON 2R AFT OF STA 1418. A SPLICE REPAIR WAS INSTALLED IAW ECRA 5311-01132. 2L72 4F A6WE 20030217000072003021700007NM 2003 2 17 CALA0300049 120030215A5315 FLOORBEAM BOEING737 7373T0 1384582NM STA 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, BL 0 TO LBL 18. THE UPPER CHORD OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851, REV. B. 2L72 4F RTA16WE 20030625000692003062500069NM 2003 6 25 HNAA0300008 120030209A210078279018 ACM DHAV DHC8 DHC8102 2809003NM TAIL ODOR A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA07936HA124361598 145 FAINT MELTING PLASTIC ODOR REPORTED BY PASSENGER AND FLIGHT ATTENDANT, RETURNED TO GATE. INSPECTED AIRCRAFT, SUSPECT INVERTERS, MEL'D. PASSENGER IN ROW 9 COMPLAINED OF BURNING ODOR ON DESCENT. THE ODOR BECAME STRONGER AS DESCENT CONTINUED, CONFIRMED BY FLIGHT ATTENDENT. COULD NOT TELL IF ELECTRICAL OR SMOKE. ON FERRY FLIGHT ODOR AGAIN IN CABIN AND FLIGHT DECK. DIVERTED TO RDU. RAN AIRCRAFT, OK WITH BLEEDS OFF, FERRIED TO ORF. REPLACED AIR CYCLE MACHINE. 2H72 4T RTA13NM 20030218002182003021800218NM 2003 2 18 SWAA030315 120030207A5520BACB28AM07 BUSHING BOEING737 7373L9 1384470NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C1 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER SWA SI AND MM. 2L72 4F RTA16WE 20030115000942003011500094SW 2003 1 15 AC2A082965 120030109A2435C400B3N001 CONTACTOR BELL 430 430 1182150SW STARTER GEN DEFECTIVE H AC2AK NONE L NO TEST ININSP/MAINT 1 FS01430CT999 49089 STARTER ENGAGES WHEN BATTERY IS TURNED ON. REPLACED CONTACTOR. 1G72 3U RTH9SW 20030116002812003011600281SW 2003 1 16 HEEA083141 120030108A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR FLAP STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 MAIN ROTOR FLAP REATRAINT STICKING IN DOWN POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030228000782003022800078NM 2003 2 28 ASAA0340002 120030102A33978100022601 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01782AS 25113 PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 17, 18, 19, DISCONNECTED WIRES. RECONNECTED WIRES, OPS CHECKED NORMAL. (M) 2L72 4F RTA16WE 20030303000412003030300041 2003 3 3 HEEA084501 420030214A3421504001790116 GYRO BELL 412 412 1182202SW COCKPIT PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 HORIZON GYRO PRECESSES. IN SHOP REPAIR. 1G72 4U H4SW 20030324001372003032400137SO 2003 3 24 C2XA03IA033 120030319A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715555 145594 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT THE OVERWING EMERGENCY LIGHTS WON'T ILLUMINATE. IAH- MAINTNEANCE REMOVED AND REPLACED THE #3 EMERGENCY LIGHT BATTERY IAW EMB-145-MM- 33-50-04, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030325000382003032500038EU 2003 3 25 AWXA200300155 120030204A5315D53112935202 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM FR 20, RBL 28. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM FR 20, RBL 28; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG. 201, PG. 201-206. 2L72 4F RTA28NM 20030307001272003030700127WP 2003 3 7 AALA20030099 120030120A5342 ATTACH ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21598AA 53288 TUL - FOUND LEFT AFT END OF VERTICAL STAB JOINT IS CRACKED BETWEEN FASTENERS .5 INCH. INSTALLED SKATE ANGLE REPAIR DOUBLER PER AARD 53-10-00-2. (M) 2L72 4F RTA6WE 20030307001882003030700188NM 2003 3 7 AALA20030077 120030119A3397 WIRE BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21352AA 24033 SFO - DURING OVERNIGHT MAINTENANCE, SEAT 31B EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030310000842003031000084 2003 3 10 HEEA084988 420030227A344280510800001 CONTROL BOX BELL 412 412 1182202SW WX RADAR SYS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 WX RADAR SYS TAS FAIL IS DISPLAYED ON SCREEN AND IT WOULD NOT CALIBRATE. 1G72 4U H4SW 20030314001222003031400122CE 2003 3 14 CCA2003F00000 120030125A27302300003171 CONTROL CABLE LEAR 35 31 5170530CE GARRTTTFE731TFE731* 01518WP ELEVATOR WORN B CCARK NONE O OTHER ININSP/MAINT 1 EA1790BA 640 018 FOUND LT AFT ELEVATOR CABLE MISROUTED AND CUTTING INTO STRUCTURE RIB AT FRAME 29 STA 541.57. CABLE REPLACED DURE TO WEAR AT STRUCTURE RIB. CABLE HAD 640.6 SINCE NEW INSTALLED 10/7/2000. 2L72 4F4 FRTA10CE E6WE 20030121003372003012100337EA 2003 1 21 COMA0360039 120030120A5350 FAIRING CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO01435CA 7473 FLIGHT 5877 RUMBLING NOISE AND VIBRATION FELT IN AIR FRAME.REPLACED MISSING SEALANT AT WING TO FUSELAGE FAIRING. 2L72 4F RTA21EA 20030122001012003012200101EU 2003 1 22 HEEA083488 120030107A716010560133 RING ASSEMBLY BOLKMS105 BO105S 5626006EU BELLMOUTH CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381992 S827 BELLMOUTH RINGS CRACKED. REPLACED ENGINE BELLMOUTH RINGS. 1G72 3U H3EU 20030327000222003032700022NM 2003 3 27 AWXA200300293 120030318A2120424B2003 CARTRIDGE AIRBUSA319 A319132 3930340NM AIR CIRCULATION CONTAMINATED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP28818AW 1375 ON DESCENT INTO PHX EN ROUTE FROM PHL AT APPROXIMATELY 12000 FT THE FLIGHT ATTENDANT AND PASSENGERS COMPLAINED OF A STRONG ODOR SIMILAR TO BURNING RUBBER. MAINTENANCE REMOVED AND REPLACED RECIRCULATION FILTER CARTRIDGE IAW AMM TASK 21-21-000-001. RAN BOTH ENGINES NO ODOR WAS PRESENT. 2L72 4F RTA28NM 20030317001492003031700149NM 2003 3 17 03FDEA00313 120030225A5753 FLAP TRACK DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING INBOARD FLAP TRACK 3 EA ATTACH POINTS FOUND WITH CORROSION. 2L73 4F RTA22WE 20030317001542003031700154EU 2003 3 17 DHL2003367507 120030227A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH42274 265 Item Ref. N/R 0029518:Main cabin floor seat track scallops at STA. 3360 Fr. 54 L/side has gouges. Corrective action:Blended out gouges IAW A300 SRM 53-10-00,alodined IAW A300 SRM 51-40-12,primed IAW A300 SRM 51-40-12,painted IAW A300 SRM 51-40-12. Blended area found within limits IAW A300 SRM 53-10-00. Orig mat.thicknesso.138,mat. removed 0.002. 2L72 4F RTA35EU 20030320000642003032000064NM 2003 3 20 03FDEA00331 120030318A5320 WEB BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 CORROSION ON UPPER SURFACE OF HORIZONTAL WEB INBOARD OF STRINGER 18A, BS 908 RBL 66 WL 189. 2L73 4F RTA3WE 20030321001012003032100101EU 2003 3 21 2003UALA00244 120030227A5754D5746019800000Z SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 LT SLAT DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29410UA 463 SKIN ON NR 1 LT SLAT LEADING EDGE IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLUSH SKIN REPAIR ON #1LH SLAT L/E. 2L72 4F4 FRTA28NM E40NE 20030731000302003073100030NM 2003 7 31 QXEA200300905 120030719A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- LEFT HAND INBOARD NR 5 SEAT TRACK IS GOUGED ON UPPER FLANGE AT STATION X501.00. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20030326000882003032600088NM 2003 3 26 2003UALA00288 120030313A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29560UA 26660 EXTERIOR EMERGENCY SLIDE LIGHT IS INOP AT DOOR 1R. RELAMPED 2L72 4F4 FRTA2NM E17NE 20030421001362003042100136 2003 4 21 VNAA0302022 420030224A3418 STALL WARNING DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07457PS 3048 DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE PUSHER AND FLIGHT 4140 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4140 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030421000342003042100034EU 2003 4 21 MALA030179 120030224A3230 LANDING GEAR SAAB SF340 340B 7860101EU MAIN CONTAMINATED A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15415XJ 340B415 AFTER TAKEOFF OF FLIGHT 3075, LANDING GEAR UNSAFE INDICATOR WOULD NOT EXTINGUISH AFTER A NORMAL TIME PERIOD AFTER T/O. LIGHT REMAINED ON WITH HYDRAULIC PUMP RUNNING CONSTANTLY UNTIL GEAR WAS SELECTED BACK DOWN. GEAR GOT 3 GREEN DOWN AND NORMAL LANDING ACCOMPLISHED. AIR RETURN TO DTW. MAINTENANCE CLEANED ICE AND SLUSH BUILD UP OFF ALL THREE GEAR LEGS. ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20030730000982003073000098WP 2003 7 30 AMTA200300892 120030523A5720 STIFFENER LKHEED1011 10113853 5265020WP WING CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11162AT 1220 WING FORWARD SPAR VERTICAL STIFFENER CRACKED. REPAIRED VERTICAL STIFFENER IAW EO L10-57AD-0606. (M) 2L73 4F A23WE 20030806001092003080600109SO 2003 8 6 C2XA03TY115 120030801A534714532606015 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION SEAT TRACK LW4 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20040226000082004022600008WP 2004 2 26 ASAA0380379 120030421A5320993653423 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 196. REPLACED DAMAGED SUPPORT PER SRM 51-10-4. (M) 2L72 4F A6WE 20030717000042003071700004SW 2003 7 17 HEEA087981 120030701A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322608 33075 STARTER GEN WILL NOT TURN OVER. SHOP REPAIR. 1G72 4U H4SW 20030722001072003072200107NM 2003 7 22 SWAA031480 120030703A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20030828000102003082800010WP 2003 8 28 ARWA20030312 120030315A5347 CARGO TRACK DOUG DC8 DC862F 3021972WP FUSELAGE BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, THE FOLLOWING WAS FOUND; MAIN CARGO DOOR COMPARTMENT STA 420, LBL 50 TRACK WITH BREAKAGE. CUT AWAY DAMAGED SECTION OF TRACK IAW DC8 SRM 53-2-3, PREPARED A NEW SECTION OF TRACK AND FABRICATED SPLICES IAW DC8 SRM 53-2-3, PRIMED PARTS IAW DC8 SRM 51-1-8, INSTALLED PARTS IAW DC8 SRM 53-2-3. 2L74 4F 4A25 20030828001172003082800117WP 2003 8 28 MWEA030291 120030728A532159366605 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 AFT CARGO COMPARTMENT CENTER FLOORBOARD BETWEEN STATION 1231-1322 IS DAMAGED. FABRICATED AND INSTALLED NEW FLOORBOARD. 2L72 4F A6WE 20030724001152003072400115EU 2003 7 24 AWXA200300671 120030603A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 241 FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW4837 064 DURING C-04 CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT INDICATED A FAULT. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) AND BATTERY PACK IAW AMM TASKS 33-51-38-000-001 AND 33-51-38-400-001, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030725000152003072500015NM 2003 7 25 DL75A030590 120030626A3397 WIRE BOEING757 757212 1384951NM SEAT ROW 40DEF BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27757AT 23127 EMERGENCY PATH LIGHT INOP AT ROW 40DEF. REPAIRED BROKEN WIRE UNDER SEAT TRACK, OPS NORMAL. 2L72 4F RTA2NM 20030724000952003072400095NM 2003 7 24 DL757030559 120030619A5330146N37506 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 FUSELAGE, SKIN AT STA 1685-1695 AND STRINGER 17R TO 19R. SEVERAL SKIN LOCATIONS WERE FOUND DAMAGED. SKIN CUTOUTS WERE MADE AND A REPAIR DOUBLER AND TRIPLER INSTALLED TO REPAIR THE DAMAGE. ACCOMPLISHED PER ER/A 385112-14. 2L72 4F RTA2NM 20030812000652003081200065SW 2003 8 12 HEEA088537 120030726A2842206063613003 SWITCH BELL 206 206L1 1182107SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035019F 45244 LOW LEVEL LIGHT DOES NOT GO OFF WHEN A/C IS SERVICED WITH FUEL. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030813000532003081300053NM 2003 8 13 2003UALA00470 120030604A5320 CLIP BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29604UA 21865 BS 1346, STR 34R, FRAME ATTACH CLIP REQUIRES REPLACEMENT FOR STRINGER REPAIR. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2L72 4F4 FRTA1NM E3NE 20030813000662003081300066NM 2003 8 13 UPS03440838 120030518A5320 FLOOR SUPPORT BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, BULK CARGO STA 1920-2040 RBL 22 FLOOR SUPPORT UPPER AND LWR SURFACE FOUND CORRODED. BULK CARGO STA 1920 TO 1990 RBL 22 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 DUE TO COROSION BLEND AREA (1 INCH X 6 INCH X 0.026 INCH) OUT OF SRM 53-10-01 FIG 1 LIMITATION & AREA BS 1990 TO 2040 R22 FLOOR SUPPORT AREA CORROSION REMOVED & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 WITHIN SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F RTA20WE 20030903002352003090300235NM 2003 9 3 03233410 120030821A33508GH00247308 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27410FJ 3165 DURING MAINTENANCE INSPECTION THE LAV EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AN AIRCRAFT WAS RELEASED FOR CONTINUED SERVICEDCN#147612-07 2H72 4T RTA55NM 20030904001302003090400130NM 2003 9 4 DL757030616 120030703A5330146N35317 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27686DA 27589 FUSELAGE SKIN FS 1510 STR 28R-29R AND 28L-29L: AIRFONE ANTENNA CUTOUT CORROSION REPAIR. THE AIRFONE ANTENNA CUTOUTS AT FS 1510 BETWEEN STRINGERS 28R & 29R AND BETWEEN 28L & 29L WERE FOUND CORRODED. THE CUTOUTS WERE ENLARGED TO REMOVE THE CORROSION DAMAGE. THE CUTOUTS WERE THEN REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385303-14, REV A. 2L72 4F RTA2NM 20030905000142003090500014SO 2003 9 5 LR7A03061 120030725A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT CARGO DOOR FS 968 SKIN DENTED AT BL 0. REPAIRED IAW SRM SMP 583 51-140-12. NR 2104. 2H74 4T A1SO 20030822001602003082200160NM 2003 8 22 UPS03441116 120030728A5330 SKIN BOEING747 747123 1384873NM BS1241 RBL24 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C INSTALL A NEW REPAIR DOUBLER AT BS 1241 - RBL 24 AS PER TELE UPS-HKG-03-001 FOR ACCOMPLISH SB 747-51A2054. CORROSION REMOVED AT RBL 16 AREA EXCEEDED SRM 53-10-01 FIG 1 LIMITATION AFTER DOUBLER REMOVED CORROSION BLEND OUT 0.045 INCH MAX NEW REPAIR CARRIED OUT AS PER RS R-53-48-35046 AT BS 1241 RBL 11.33 TO RBL 33.99 AREA AND EO B747-5310-16853. 2L74 4F A20WE 20030728000382003072800038NM 2003 7 28 SWAA031565 120030714A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1011, STR 7L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030825000772003082500077NM 2003 8 25 EIA2003106 120030725A3350S1356B37 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 DURING GROUND TEST FOLLOWING FLIGHT EVALUATION EMERGENCY CEILING LIGHT AFT UPPER DECK ILLUMINATES FOR ABOUT 3 SECONDS BEFORE GOING OUT. (DMI 763) 2L74 4F A20WE 20030827001152003082700115NM 2003 8 27 CALA0300413 120030725A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND L-ANGLE CORRODED AT STA 951-995, RBL 55. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030911001902003091100190WP 2003 9 11 AALA20030338 120030313A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 TUL - FOUND DENT IN FUSELAGE SKIN, REF ADL0008. INSTALLED DOUBLER PER SRM 53-04-00 PAGE 60G FIG 12B SHEETS 35. (M) 2L72 4F A6WE 20030930001222003093000122NM 2003 9 30 03FDEA01478 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) O/B PIVOT LUG HOLE CORRODED. 2L73 4F RTA22WE 20030929001162003092900116 2003 9 29 RAIA00308231 420030829A3425HG2010AC02 DISPLAY EMB 145 EMB145LR 3260212SO NR 2 AHRS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK275 145044 AHRS NR 2 FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS. 2L72 4T RTT00011AT 20031001000482003100100048WP 2003 10 1 UPS03841193 120030812A5313564932744 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C1 AFT FUSELAGE TAIL SECTION AT FS 1766-1780 L17R IS CRACKED. REMOVED L17 RT TO FOM LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONGERON AND END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20031014001562003101400156NM 2003 10 14 SWAA032071 120030917A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030909000452003090900045EA 2003 9 9 SWIA200312324 120030808A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 FS 484 RT INTERCOSTAL O/B FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. ''A''. P/N: S6144-14 2L72 4F RTA21EA 20031028000752003102800075NM 2003 10 28 MWEA030398 120030928A2760 HANDLE BOEING717 717200 1383700NM CONT O520 TSIO520* 17040SO SPOILERS MALFUNCTIONED A MWEAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL31906ME 55170 SPOILER HANDLE WILL NOT STAY IN THE UP AND LOCKED POSTION. PERFORMED FAULT ISOLATION MANUAL BITE TEST, NO FAULTS, OPERATION CHECK NORMAL. 2L72 4F3 OTRA6WE E8CE 20031028000792003102800079NM 2003 10 28 2003UALA00737 120031002A21508102044 CONTROL VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE RT PACK FLOW FAILED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29783UA 26950 RT AIR CONDITIONING PACK FLOW CONTROL VALVE STATUS MESSAGE. RT LOWER FLOW CONTROL VALVE FAILED DUE TO BAD PROXIMITY SWITCH. RT LOWER FLOW CONTROL VALVE REPLACED. 2L72 4F4 FRTT0001SE E46NE 20031028000852003102800085NM 2003 10 28 UPS03541441 120031015A5610 WINDOW BOEING757 75724APF 1384969NM COCKPIT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01411UP 23851 INSPECTION TYPE: AS, R2 WINDOW WILL NOT FULLY CLOSE. AWAITING LOG PAGE. 2L72 4F RTA2NM 20031118001082003111800108NM 2003 11 18 AWXA200301184 120030912A5321144N533040 FLOOR PANEL BOEING757 7572S7 1384962NM CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK CABIN FLOOR PANEL K-1 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1. 2L72 4F RTA2NM 20040114000222004011400022NM 2004 1 14 XNOA1161 120031024A7931 PRESSURE SWITCH BOEING727 727200 138407ENM NR 2 ENGINE LEAKING A XN0AED ENGINE SHUTDOWN RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL23793A 20774 NR 2 ENG LOW OIL PRESS WARNING LT & LOSS OF OIL PRESS. SHUT DOWN ON TAXI OUT. FOUND NR 2 ENG OIL PRESS SWITCH LEAKING. REMOVED AND REPLACED NR 2 LOW OIL PRESS SWITCH AS REQ IAW B727 MM REF 79-33-1, OPS AND LEAK CHECK. DURING TROUBLESHOOTING FOUND LOW OIL PRESS LT INOP. TRANSFERRED TO DMI 3677 IAW ENA B727 MEL REF 79-4, CAT B PLACARDS INSTALLED. 2L73 4F RTA3WE 20040210000172004021000017WP 2004 2 10 UPS03841591 120031118A5330 SKIN DOUG DC8 DC871F 302199DWP FWD FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION -12 AT LONG. 27L HAS FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF SHUTTER BOX OPENING. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND IN STALLED FILLER AND DOUBLER IAW DC8-5330-4732. 2L74 4F RT4A25 20031031000022003103100002 2003 10 31 SWIA200312459 420030925A3418C818022 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE STICK SHAKER MALFUNCTIONED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07288SW8225 8225 120316 NR 2 STALL SHAKER INOPERATIVE. REPLACED NR 2 STALL SHAKER. SYSTEM TESTS NORMALLY IAW MM 27-34-00. 2L72 4T4 TRTA31SO E20NE 20031029001152003102900115SO 2003 10 29 C2XA03SH363 120030930A335020131A BATTERY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 DURING C CHECK THE GALLEY EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AND PERFORMED AN OPERATIONAL CHECK WHICH WAS GOOD, IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031113000242003111300024WP 2003 11 13 BAQA089829 220031008A7321307080022 FUEL CONTROL LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP ENGINE MALFUNCTIONED B BAQAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 EA0330DK 1569 345 CAUSING FUEL FLOW FLUX. REPLACED WITH SERVICEABLE UNIT. 2L72 4F4 F A10CE E6WE 20031106002212003110600221NM 2003 11 6 ASAA0310478 120030520A52406545871523 SKIN BOEING737 737290C 138448VNM R1 DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE R1 DOOR SKIN AT FUSELAGE STATION 295, RIGHT BUTTOCK LINE 68 CRACKED. REPAIRED DOOR SKIN PER EA. (M) 2L72 4F A16WE 20031110001412003111000141 2003 11 10 C8GA20030025 420031028A3418 PITOT TUBE BOEING727 727200 138407ENM AIR SPEED OBSTRUCTED A C8GAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO15713AA 22469 FLT 717 FROM ELP TO STL. ON TAKEOFF ROLL, THE CAPTAIN'S AIRSPEED INDICATOR READ 30 KNOTS LESS THAN THE FIRST OFFICER POSITION. ABORTED TAKEOFF AND AIRCRAFT RETURNED TO RAMP WITHOUT FURTHER INCIDENT. INSPECTED CAPTAIN'S PITOT PROBE AND FOUND DEBRIS LODGED IN PITOT TUBE. CLEAN DEBRIS AND BACK FLUSH PITOT LINE IAW B727 MM 34-11-00, PAGE 209B. OPS CHECKS GOOD, NO OTHER DEFECT NOTED AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20031113000222003111300022EU 2003 11 13 BAQA090019 120030920A2842L284M30C1001 PROBE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE FUEL SYSTEM MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911BG 0015 REMOVED DUE TO FUEL QUANTITY DEGRADED READING 31 HZ DURING TROUBLESHOOTING. REPLACED WITH SERVICEABLE UNIT. 10/17/03 1G72 3U3 UO H88EU E42NE 20040113000932004011300093NM 2004 1 13 UPS03241671 120031223A3350 LIGHT BOEING727 727108C 1384039NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT FOR CABIN INOP. REMOVED AND REPLACED CABIN EMERGENCY LIGHTING FIXTURE PER MM 33-50. OPS CHECKS NORMAL AT THIS TIME. 2L73 4F A3WE 20040112002512004011200251WP 2004 1 12 AALA20031429 120031214A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21447AA 49473 DFW SEAT MOUNTED EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 25D. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20031124000872003112400087WP 2003 11 24 DHL2003807512 120031010A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT OUTER WING OUTBD L/E UPPER SKIN CORRODED STA XFS 716.250 - XFS 735.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 TR 57-85. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38 TR 57-85. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW SRM 57-2-1 FIG 38 TR 57-85, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040114001912004011400191SO 2004 1 14 MASA200300434 120031103A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07830MJ6133 145259 ASH 2743 CLT. 2 PORTIONS OF THE FLOOR PROXIMITY LIGHTING STRIPS INOPERATIVE. MECHANIC REPLACED THE BATTERY CHARGER, OP CHECKS GOOD. 2L72 4T RTT00011AT 20031212001772003121200177EA 2003 12 12 COMA0370038 120031019A3234533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01390CA788 10106 FLIGHT 9463 GEAR DISAGREE WARNING - LANDING GEAR DID NOT EXTEND. REPLACED THE SELECTOR VALVE. 2L72 4F4 FRTA21EA E15NE 20031215001662003121500166WP 2003 12 15 AALA20031142 120031010A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 31. REPAIRED ELECTRICAL WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031217001292003121700129WP 2003 12 17 ARWA20031205 120031205A7730 SOCKET LKHEED1011 1011385115 5265015WP INSTRUMENT PANELMALFUNCTIONED A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO19307GB 193U1131 NR 2 ENGINE GREEN LIGHT DID NOT COME ON FOR TAKEOFF AT TTPP. TAKEOFF ABORTED AND RETURNED TO RAMP. RESET LIGHT SOCKET ON ANNUNCIATOR PANEL. OPERATIONAL CHECK NORMAL IAW MM 71-00-20. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A23WE 20031217001532003121700153EU 2003 12 17 03FDEA02044 120031204A5753 FLAP TRACK AIRBUS310 A310 EU ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25430FE 394 LT WING TE, MIDPOINT BETWEEN NR 1 O/B PYLON AND I/B NR 3 FLAP TRACK EVIDENCE OF CRACK AT RIVET HEAD TO EDGE LWR SKIN. REQUEST NDT TO CONFIRM. REMOVED FASTENER IAW A310 SRM 51-40-21, ROTO TESTED HOLE IAW NTM 51-10-00-01 NO CRACKS FOUND, FABRICATED REPAIR PARTS IAW EA6-5710-73485A DWG R57249152. INSTALLED REPAIR PARTS IAW EA6-5710-73485A DWGR 57249152. DOME SEALED FASTENER IAW A310 SRM 51-76-20, LEAK CHECK IAW AMM A310-28-11-00-5. 2L72 4F RTA35EU 20031217001612003121700161EU 2003 12 17 AWXA200301534 120031213A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU SEAT ROW 3 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 DURING 4-DAY CHECK 2 EACH EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 3 LT WERE FOUND INOPERATIVE. MAINTENANCE DISCOVERED A BROKEN WIRE STRAND GOING TO THE LIGHT HOUSING AT SEAT ROW 3 LT, REPAIRED BROKEN WIRE, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031218000472003121800047EA 2003 12 18 03325690 120031121A2720 PEDAL CNDAIRCL600 CL6002B19 1900309EA COCKPIT OUT OF ADJUST A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27690BR 7739 DURING UNKNOWN PHASE OF AIRCRAFT OPERATION A CLICKING NOISE WAS REPORTED IN THE CAPTAINS RUDDER CONTROL PEDALS. THE NOISE WAS IDENTIFIED AS A LOOSE RUDDER PEDAL PIVOT ASSEMBLY. THE ASSEMBLY WAS LUBRICATED AND RETORQUED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031219000742003121900074NM 2003 12 19 AWXA200301516 120031202A5730114N2106 SKIN BOEING757 7572G7 1384963NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28908AW 24233 DURING C-12 CHECK A 3 INCH CRACK WAS FOUND ON RT WING UPPER LEADING EDGE SKIN AT NR 8 SLAT INBOARD CORNER. MAINTENANCE REMOVED CRACKED RT WING UPPER LEADING EDGE SKIN PANEL FROM WS 425.50 TO WS 471.30; FABRICATED 3 EACH REPAIR STRAPS & FILLERS; INSTALLED REPAIR PARTS IAW AWA ER 19-5700-00012-DD5. 2L72 4F RTA2NM 20031223000572003122300057NM 2003 12 23 SWAA032678 120031207A53126546568 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT BL 0. REPAIRED WEB SECTION PER SWA EA. 2L72 4F RTA16WE 20031222001262003122200126NM 2003 12 22 AMTA200301416 120031119A2612 WARNING LIGHT BOEING757 75723N 1384973NM LT ENGINE FIRE ILLUMINATED A AMTAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL11523AT 30232 EICAS STATUS MSG LEFT ENGINE FIRE LOOP NR 1 DISPLAYED. DEFERRED PER MEL 26-11-1. (M) 2L72 4F RTA2NM 20031224000652003122400065SO 2003 12 24 C2XA03SH496 120031213A532014526437001 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE RIGHT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT OMEGA BEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031229001082003122900108NM 2003 12 29 AWXA200301552 120031202A53206516300 SUPPORT BOEING737 737375 13844BNNM FUSELAGWE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-04 CHECK A 1.1875 INCH CRACK WAS FOUND COMING FROM HI-LOK FASTENER EXTENDING TOWARD BEND RADIUS ON HORIZONTAL SUPPORT IN FORWARD E&E COMPARTMENT, BS 179.5, LBL 25.5, WL 195.5. MAINTENANCE CUT OUT CRACKED AREA OF HORIZONTAL SUPPORT AT BS 179.5, LBL 25.5, WL 195.5; FABRICATED A REPAIR ANGLE AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG 207. 2L72 4F RTA16WE 20031229001382003122900138NM 2003 12 29 SWAA032733 120031215A575465C26602 WEDGE BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND NR 5 L/E SLAT T/E WEDGE INBOARD END DELAMINATED. REPAIRED WEDGE PER SRM. 2L72 4F RTA16WE 20031231000622003123100062WP 2003 12 31 GTIA030920 120031029A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP COCKPIT DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND COCKPIT FLOOR PANEL NR 4411A DELAMINATED. REPAIRED COCKPIT FLOOR PANEL. (M) 2L72 4F RTA6WE 20040105000282004010500028EU 2004 1 5 AALA20031440 120031216A3350 LIGHT AIRBUS300 A300B4605R 3930308EU SEAT 18C BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW218067A 510 SEAT MOUNTED EMERGENCY LIGHT IS BROKEN AT SEAT 18C. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20031009000632003100900063EA 2003 10 9 SWIA200312387 120030902A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA CONNECTOR BROKEN A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07445SW 7651 (STALL FAIL) MESSAGE WHILE ENROUTE COMPLIED WITH THE APPROPRIATE QRH PROCEDURE. REPAIRED BROKEN WIRE AT CONNECTOR FOR CAPT STICK SHAKER. 2L72 4F RTA21EA 20031006001922003100600192NM 2003 10 6 03FDEA01663 120031001A5230 FRAME BOEING727 727200 138407ENM MAIN CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 MAIN CARGO DOOR FWD SIDE FRAME GOUGED 12" FROM LWR CORNER . 2L73 4F RTA3WE 20040106001092004010600109NM 2004 1 6 DHL2003742530 120031124A5720 STIFFENER BOEING727 727225 1384077NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, RT WING L/E BL 92 INT FRAME VERT STIFFENER IS CRACKED ON BOTTOM THRU FASTENER HOLE. CUT OUT DAMAGED AREA DIM 2.5 X 2 INCH IAW B-727 SRM 51-40-4. FABRICATED NEW FILLER IAW B-727 SRM 51-40-4. TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED FILLER AND DOUBLER ON RT WING L/E STA 130 INT FRAME IAW B-727 SRM 51-30-2 AND 51-40-4. 2L73 4F A3WE 20031125000792003112500079WP 2003 11 25 DHL2003805562 120030806A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT OUTER WING INBD L/E FORMER CRACKED 1.000, STA XFS 660.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RIGHT OUTER WING INBD L/E FORMER STA XFS 660.000 (UPPER PART) WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031126000362003112600036EA 2003 11 26 COMA0360488 120031106A2710600908002 PULLEY CNDAIRCL600 CL6002B19 1900309EA AILERON SYS DEFECTIVE A COMAB EMER. DESCENT F FLT CONT AFFECTED CRCRUISE 1 SO01918CA 7018 FLIGHT 5369 DURING CRUISE FLIGHT THE AILERON CONTROLS SEEMED TO REQUIRE MORE THAN NORMAL FORCE TO OPERATE. CREW ELECTED TO PERFORM AN EMERGENCY DESCENT TO LOWER ALTITUDE WHERE THE AILERONS RETURNED BACK TO NORMAL OPERATION. REPLACED AILERON CONTROL PATH PULLEYS. 2L72 4F RTA21EA 20040122000392004012200039NM 2004 1 22 ASAA20040122 120030324A541065C2630924 ANGLE BOEING737 737490 1384715NM NR 2 PYLON CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01703AS 28893 DURING C-CHECK, FOUND CRACKED ANGLE ON NR 2 PYLON OUTBOARD SIDE COMMON TO UPPER T/E PANEL. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040115001842004011500184NM 2004 1 15 AWXA200400015 120031227A5311651630086 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LCQ - MAJOR REPAIR - DURING C-17 CHECK HFEC INSPECTION INDICATED A CRACK ON BS 178 BULKHEAD LT SIDE CHORD, LBL 70, WL 207. MAINTENANCE REMOVED DAMAGED LT SIDE CHORD AT LBL 70, WL 207; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, PG 38. 2L72 4F RTA16WE 20040121001042004012100104NM 2004 1 21 03FDEA02329 120031230A5744ARC119113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75201, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031208000342003120800034NM 2003 12 8 QXEA200301310 120031022A3310 RHEOSTAT DHAV DHC8 DHC8202 2809007NM OVERHEAD LIGHT FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09356PH 502 ON FLIGHT NUMBER 2155, FO OVERHEAD MAP LIGHT NOT ILLUMINATED WHEN RHEOSTAT TURNED UP. SMOKE POURED OUT OF THE PLASTIC NEAR THE LIGHT. DEACTIVATED FO'S MAP LIGHT BY PULLING CIRCUIT BREAKER AND COLLARED. REMOVED AND REPLACED FIRST OFFICERS OVERHEAD MAP LIGHT REHOSTAT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031204001332003120400133SO 2003 12 4 C2XA03SH401 120031020A532014521725001 SILL EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 DURING C-CHECK THE LT SILL AT FR 18 TO FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031209002422003120900242NM 2003 12 9 AT0300035 120031104A33508039251 BATTERY BOEING717 717200 1383700NM EMERGENCY LIGHT DISCHARGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15960AT 55022 BATTERY PACK AT B5-119 FOR EMERGENCY PATH LIGHTING WOULD NOT ILLUMINATE. REPLACED BATTERY ASSEMBLY, OPS CHECK GOOD. SUSPECT FUSE AT PIN 10 IS BLOWN. 2L72 4F TRA6WE 20031209000432003120900043EA 2003 12 9 SWIA200312550 120031026A2760270003 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07405SW 7029 ON TAXI INTO SLC FLT SPOILER MESSAGE ON EICAS. REPLACED RIGHT INBOARD FLIGHT SPOILER PCU WITH SERVICEABLE UNIT IAW CRJ MM 27-62-01. LEAK AND OPS CHECKS OK. S/N OFF: 0038. 2L72 4F RTA21EA 20040127001512004012700151NM 2004 1 27 ASAA0310187 120030321A531565466114 FLOORBEAM BOEING737 737298C 1384490NM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FLOORBEAM AT BS 540, LEFT BUTTOCK LINE 25, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M) 2L72 4F RTA16WE 20040128000902004012800090NE 2004 1 28 AWXA200301636 220031229A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LEFT MALFUNCTIONED A AWXAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 WP28655AW 1075 PHX - ABORTED TAKEOFF - FLT 0075 - ON TAKEOFF AT PHX EN ROUTE FOR SEA WHEN THRUST LEVERS ADVANCED TO 1.05 EPR THE LT ENGINE WAS SLOWER TO SPOOL THAN RT ENGINE, NO ECAM WARNINGS OR CAUTIONS OF ANY KIND, REJECTED TAKEOFF. RECONFIGURED SETTINGS, TAXIED BACK TO RUNWAY, AND TOOK OFF WITHOUT FURTHER INCIDENT. 2L72 4F4 FRTA28NM E40NE 20030916001332003091600133WP 2003 9 16 GTIA030642 120030722A5310 DOOR FRAME DOUG DC9 DC983 3022083WP MID CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND MID CARGO DOOR JAMB BEAM CORRODED AT DOOR OPENING IN PREVIOUS REWORKED AREAS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20030923000802003092300080WP 2003 9 23 DHL2003604689 120030520A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT OUTER WING INBD EXTENDED L/E LOWER PLATING CRACKED 1.650 AROUND STA XFS 597.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 21. PERFORMED STOP HOLE ON CRACK END USING 0.250 DIA DRILL IAW EODHL-030520, ED-3352. PERFORMED EDDY CURRENT INSPECTION IAW NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) IAW EODHL-030520, ED-3352. CLEANED, TREATED AND PRIMED DOUBLER INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON RT OUTER WING INBD EXTENDED L/E LOWER PLATING (AROUND STA XFS 597.500) USING NEW FASTENERS IAW EODHL-030520, ED-3352, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923000632003092300063WP 2003 9 23 DHL2003604754 120030527A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING EXTENDED L/E OTBD VANE HAS SEVERAL ELONGATED HOLES AND INTERIM REPAIR AT STA XOLDI 67.000. REMOVED FASTENERS, REMOVED EXISTING INTERIM REPAIR. TRIMMED OUT ELONGATED HOLES SKIN AREA. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075-T6 AL0.071) AN INTERNAL DOUBLER (7075-T6 AL0.050) AND A FILLER (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE, INTERNAL DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED EXTERNAL DOUBLER AND INTERNAL DOUBLER AND FILLER ON RT WING EXTENDED L/E OTBD VANE STA XOLDI 67.000 WITH NEW FASTENERS. 2L74 4F RT4A25 20040128001272004012800127SO 2004 1 28 LR7A03110 120031204A5312 PRESSURE PANEL LKHEED382 382G 526414USO MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 5025 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND FS 517 RT MLG WHEEL WELL SKIN CRACKED AT BELLY SKIN ATTACHMENT RBL 35, WL 126. REPAIRED IAW SRM SMP 583 51-140-12. NR 2018. 2H74 4T A1SO 20040203000522004020300052NM 2004 2 3 ASAA0310238 120030327A33508821004 BATTERY PACK BOEING737 737210C 1384459NM EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 AFTER RECON, FOUND AFT TWO PALLETS EMERGENCY FLOOR TRACK LIGHTS BLINKING. REMOVED AND REPLACED BATTERY PACKS, THEN LIGHTS OPERATED NORMAL. (M) 2L72 4F A16WE 20040130002062004013000206WP 2004 1 30 ABXA040015 120031222A5310992340650 SHEAR TIE DOUG DC9 DC932 3022066WP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 SHEAR TIE FS 622 WAS CRACKED, LONGERON 25 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040130002282004013000228NM 2004 1 30 AWXA200400041 120031217A5320141N516137 FLOOR SUPPORT BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - MAJOR REPAIR - DURING C-12 CHECK CORROSION WAS FOUND ON FLOOR ATTACH FITTING BS 365-377, RBL 50. MAINTENANCE REMOVED CORRODED FLOOR ATTACH FITTING BS 365-377, RBL 50; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW B757 SRM 51-40-02 FIG 9. 2L72 4F RTA2NM 20040205000982004020500098NM 2004 2 5 HNAA0300071 120031117A6123M390166141P RELAY DHAV DHC8 DHC8201 2809001NM AUTOFEATHER DEFECTIVE A HNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA07986HA1843818438 421 AUTOFEATHER DID NOT ARM AT 97 PERCENT, 60 KTS, ABORTED TAKEOFF. REPLACED AUTOFEATHER CONTROL RELAY. 2H72 4T RTA13NM 20040204000802004020400080EU 2004 2 4 AWXA200301271 120031020A33501012881 LIGHT AIRBUS320 A320231 3930325EU SEAT ROW 3 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 3 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040205001182004020500118CE 2004 2 5 GLBA2003158 120031125A2750100384040 MOTOR BEECH 1900 1900D 1154162CE TE FLAPS FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03220GL1612 UE220 FLAPS WILL NOT RETRACT, REPLACED SWITCH PN 27RW82255518T AND FLAP MOTOR PN 100-384040. OPS CK GOOD. 2L72 4T RTA24CE 20040210001152004021000115WP 2004 2 10 ASAA0380777 120031119A53305911405503 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND DENT IN LEFT FUSELAGE SKIN AT STATION 214 JUST BELOW LONGERON AT 17. REPAIR IAW SRM. (M) 2L72 4F RTA6WE 20031212000942003121200094NM 2003 12 12 SWAA032411 120031101A53306552988 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040520002232004052000223EU 2004 5 20 2004F00113 120030915A5310D5347218820200 STRUCTURE AIRBUS320 A320233 3930329EU CABIN FLOOR CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, OFUND CORROSION ON AFT CABIN FLOOR STRUCTURE AT FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. (M) 2L72 4F RTA28NM 20031215001702003121500170WP 2003 12 15 AALA20031064 120030924A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21462AA 49592 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040722000112004072200011EU 2004 7 22 USAA040285 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .175 SQUARE INCH, FS 65 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20030926000052003092600005NM 2003 9 26 QXEA200301025 120030823A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 FUSELAGE SKIN IS DENTED AT RIGHT HAND STATION X326.5 THROUGH X329 AND Z84.0. REPAIRED IAW DHC-8 SRM 51-20-26 AND HORIZON AIR EA 2-53-38. 2H72 4T RTA13NM 20030929000282003092900028NM 2003 9 29 03FDEA01419 120030901A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING O/B FLAP VANE NR 2 FROM I/B TEE FITTING FWD BORE FOUND CORRODED. 2L73 4F RTA22WE 20041004000692004100400069CE 2004 10 4 AK62004F00002 120031014A57115022050201 SPAR CAP CESSNA421 421B 2076014CE CONT O520 GTSIO520H 17032SO LT WING CORRODED B AK6RO OTHER O OTHER NRNOT REPORTED 1 SW19777TS6200 421B0352 DURING AN ATTEMPT TO REPAIR CORROSION AROUND THE LT WING FLAP BELLCRANK, LOCATED IN THE EXHAUST GAS TRAIL ON LOWER SIDE OF WING. DISCOVERED SEVERE INTERGRANULAR CORROSION ON LOWER SPAR CAP (JUST OB OF FACTORY SPLICE PLATE). 1L72 3O3 O A7CE E7CE 20060802001102006080200110WP 2006 8 2 IXXA060498S 120030123A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND EMPENNAGE FRAME CRACKED AT STATION 1960 LEFT SIDE WHERE HORIZONTAL STIFFENER FASTENS TO FRAME. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20, AND 51-1-21. 2L74 4F RT4A25 20030815000802003081500080SW 2003 8 15 HEEA088549 120030728A7922209070262101 INDICATOR BELL 412 412 1182202SW ENG OIL TEMP READS HIGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032014K 33020 TEMPERATURE READS HIGH. SHOP REPAIR. 1G72 4U H4SW 20030401001382003040100138NM 2003 4 1 DHL2003745009 120030401A3260 WARNING SYSTEM BOEING727 727224 1384076NM MLG DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01745DH 20665 RED "DOORS" LIGHT AND YELLOW "RT GEAR DOOR" INTERMITTENTLY COMES ON IN FLIGHT WITH GEAR HANDLE IN THE "OFF" POSITION. RIGHT LANDING GEAR DOOR WARNING SYSTEM DEFERRED IAW MEL 32-1, DMI #12425. PLACARD INSTALLED. CAT. "C" DEFERRAL. 2L73 4F A3WE 20030403000872003040300087NM 2003 4 3 CALA0300160 120030328A5510 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0910323 23374 WHILE PERFORMING A PERMANENT REPAIR OF THE LT HORIZONTAL STABILIZER LE SKIN AT LE STA 69.93 IN IAH PER SRM 55-10-01, FIGURE 203, MAINTENANCE NOTED THE REQUIRED FLUSH REPAIR WAS NOT APPLICABLE TO THIS AREA BECAUSE THE DAMAGED AREA WAS CLOSE TO A RIB. THE REPAIR WAS REDONE IAW ECRA 5510-01668. 2L72 4F RTA16WE 20030404001202003040400120WP 2003 4 4 ASAA0380089 120030117A3350TTL1110B SWITCH DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01974AS 53450 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING WAS DETERMINED TO BE INTERMITTENTLY INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHT SWITCH IN COCKPIT. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030411000102003041100010NM 2003 4 11 SWAA030749 120030405A3210A6545800219 FITTING BOEING737 7373H4 1384600NM LT & RT MLG WW CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT & RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG WALKING BEAM FITTINGS PER MM. 2L72 4F RTA16WE 20030415000312003041500031EA 2003 4 15 CA030318007 220030306A72303031951 STATOR VANE DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA 1ST STAGE COMPR FRACTURED W O OTHER DEJINFLIGHT SEPARATION VIBRATION/BUFFET WARNING INDICATION LDLANDING 1 CA (CAN) PILOT REPORTED A LOUD BANG AND TORQUE DROPPING OFF ON LANDING. THE SUBJECT ENGINE WAS REMOVED FROM SERVICE AND SENT FOR INVESTIGATION AND REPAIR. INVESTIGATION RESULTED IN THE FINDING OF ONE MISSING FIRST STAGE STATOR VANE (I.E. 1 OF 44) FROM THE 1ST STAGE STATOR VANE ASSY. THE FRACTURED STATOR VANE CAUSED DOWNSTREAM COMPRESSOR DAMAGE, WHICH FURTHER RESULTED IN THE COMPRESSOR STALLING (I.E. LOUD BANG) AND THE ENGINE TO LOSE POWER (I.E. TORQUE DROPPING OFF). 1H72 3T4 TRTA9EA E4EA 20030416001402003041600140NM 2003 4 16 AALA20030008 120030105A2910655372811 HYDRAULIC LINE BOEING757 757223 1384957NM HYD SYSTEM PUNCTURED A AALAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21645AA 24603 MIA - FLT 938 - EN ROUTE CCS-MIA, EICAS MESSAGE DISPLAYED LOSS OF HYDRAULIC QUANTITY OF CENTER HYDRAULIC SYSTEM. LEFT AND RIGHT CENTER ELECTRIC HYDRAULIC PUMP SWITCHES TURNED OFF. CAPTAIN DECLARED EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. INSPECTED AND FOUND PUNCTURED LINE FROM THE NR 1 CENTER ELECTRIC PUMP TO FILTER MODULE. REPLACED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416002222003041600222NM 2003 4 16 AALA20030211 120030219A3350 LIGHT BOEING757 757223 1384957NM EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21613AA 24489 DFW - DURING OVERNIGHT MAINTENANCE, AFT DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT DOOR EXTERIOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030416003612003041600361NM 2003 4 16 UPS03240123 120030106A5311 FRAME BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C&SI, CORROSION ON FRAME AT INTERSECTION WITH NLG WW & BS 300 RT SIDE. REPAIR CARRIED OUT IAW SRM 51-10-6, MM 20-40-00, SRM 51-30-02, & DRAWING 6518915. 2L73 4F A3WE 20030417000032003041700003NM 2003 4 17 UPS03440023 120030116A1430BACB30US18K59 BOLT BOEING747 747259B 1384804NM BULKHEAD BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE: C, CENTER TANK RIGHT FS 1241 AFT BULKHEAD FITTING ATT BOLT FOUND LEAKAGE AS MK. A 1.125 INCH DIAMETER BROKEN BOLT REPLACED AS PER MM 20-51-01 AND REFER CWS FOR WORK DETAIL. 2L74 4F RTA20WE 20030416002792003041600279NM 2003 4 16 QXEA0300448 120030410A2611 WARNING SYSTEM DHAV DHC8 DHC8202 2809007NM ZONE 200 FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM09360PH 515 SEA-ON FLIGHT NUMBER 2002, ON PUSHBACK, MASTER WARNING SMOKE LIGHT CAME ON FOR ABOUT 15 SECONDS, THEN WENT OUT. INVESTIGATED BOTH SMOKE DETECTORS IN AFT CARGO BAY, NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK, OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417000822003041700082WP 2003 4 17 MWEA030054 120030203A53129912243107 BULKHEAD DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31207ME 47794 AT APPROXIMATELY STATION 965 RIGHT FORWARD BULKHEAD WALL HAS A CRACK APPROXIMATELY SIX INCHES INBOARD OF OUTSIDE BULKHEAD ATTACH ANGLE, CRACK IS EMITTING FROM BOLT HOLE FOR THE LOWER SPAR. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED WEB. 2L72 4F A6WE 20030425000122003042500012EU 2003 4 25 MALA030209 120030326A21507769106 ACM SAAB SF340 340B 7860101EU RIGHT ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15414XJ 340B414 DURING FLIGHT 2723, OIL ODOR IN CABIN TO COCKPIT. NO GATE OR AIR RETURN. APPEARS TO BE WORSE WHEN BLEEDS ARE OPEN. MAINTENANCE REPLACED RT ACM IAW J/C 215181 P/N ON/OFF 776910-6, SN/OFF 841119, SN/ON 861121. OPS CHECK GOOD, NO ODOR PRESENT. 2L72 4T RTA52EU 20030424000362003042400036NE 2003 4 24 MWEA030136 220030320A7320 FUEL CONTROL DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE LT ENGINE OUT OF ADJUST A MWEAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL31301ME 47190 LEFT ENGINE HUNG AT ABOUT 45 PERCENT AND ROLLED BACK TO ABOUT 40 PERCENT. ADJUSTED IDLE AND DRAINED MOISTURE TRAP. 2L72 4F4 F A6WE E2EA 20030428000422003042800042 2003 4 28 GTIA030168 420030216A2565 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE ESCAPE SLIDE BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 LT 1 DOOR EVACUATION SLIDE LANYARD BROKEN. REMOVED BROKEN LANYARD. REPLACED L1 DOOR EVACUATION SLIDE LANYARD. 2L72 4F4 FRTA6WE E2EA 20030425000692003042500069WP 2003 4 25 MWEA030154 120030401A55125936112501 PLATE DOUG DC9 DC981 3022081WP HORIZONTAL STAB DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 LEFT HORIZONTAL STABILIZER CONSTANT UPPER FORWARD PLATE IS DAMAGED 2.5 INCH AFT OF FWD EDGE 1 INCH FROM INBOARD EDGE. FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIMS. 2L72 4F A6WE 20040206000142004020600014NM 2004 2 6 DHL2003754019 120031203A3230 SWITCH BOEING727 727223 1384074NM MLG DIRTY A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01754DH 22008 AFTER T/O GEAR HANDLE WOULD NOT RAISE ABOVE OFF POSITION. ABNORMAL PROCEDURE, LANDING GEAR LEVER WILL NOT GO UP PAST OFF. COMPLIED WITH RETURNED TO EWR FOR UNEVENTFUL LANDING. FOUND MAIN SAFETY SWITCH DIRTY AND CAKED WITH RESIDUE. CLEANED SAME, OPS CHECKED GOOD ON GROUND AT EWR IAW 727 M/M 32-09-121. 2L73 4F A3WE 20040206000242004020600024NM 2004 2 6 USAABB03232 120031228A3350 SOCKET BOEING757 7572B7 1384964NM R3 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 CLT - FOUND THE R3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SOCKET ASSEMBLY FOR EMERGENCY LIGHT AT R3 DOOR. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20040205000702004020500070NE 2004 2 5 ASOA03661 220031218A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF343B1 NE RIGHT BIRD INGESTION A ASOAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO11719EV 10099 AFTER DEPARTURE, WHILE CLIMBING THROUGH 7,000 FT A/C EXPERIENCE MULTIPLE BIRDSTRIKES. FLT ATTENDANT REPORTED SOUND OF IMPACT PLUS A HIGH FREQUENCY VIBRATION TOWARDS THE REAR OF THE AIRCRAFT. THERE WERE NO ABNORMAL INDICATIONS PRESENT IN THE COCKPIT INCLUDING ENGINE PARAMETERS, BUT CAPTAIN DECLARED AN EMERGENCY AS A PRECAUTION. A/C RETURNED AND LANDED SAFELY IN SLC. MX PERFORMED BIRDSTRIKE INSPECTION WITH NO DAMAGE NOTED TO ANY AIRCRAFT STRUCTURE OF FUSELAGE. HOWEVER, MAINTENANCE DID FIND EVIDENCE OF A BIRDSTRIKE ON THE RT ENGINE INLET COWL AND ENGINE WITH EVIDENCE OF COMPRESSOR INGESTION. AFTER THE COMPLETION OF BOROSCOPE INSPECTION TO THE RT ENGINE, NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040211000022004021100002NM 2004 2 11 USAASB04005 120030105A29135718610 PUMP BOEING737 737401 1384701NM HYD SYSTEM OVERHEATED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19405US 23885 CLT - FLT 1456 - EN ROUTE FROM DCA TO FLL, THE B-SYSTEM ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE B-SYSTEM ELECTRIC HYDRAULIC PUMP PER MM 29-15-22. ALSO, REMOVED AND REPLACED B-SYSTEM CASE DRAIN FILTER. OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20040304001672004030400167WP 2004 3 4 ASAA0380840 120031221A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 PDX LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-15. REPLACED TW LIGHT MODULES. LIGHTS THENOPERATED PROPERLY. (M) 2L72 4F RTA6WE 20031211001682003121100168WP 2003 12 11 AALA20030909 120030818A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21403A 49314 LGA - DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT CABIN EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031216000232003121600023EA 2003 12 16 MASA200300452 120031114A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727318 7318 PHX-IAH, LEFT HAND EXTERIOR, AFT EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB, OP CHECKS GOOD. 2L72 4F RTA21EA 20031217001082003121700108EU 2003 12 17 2003UALA00844 120031107A2910 DAMPENER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29410UA 463 LANDED UNDER AMBER ALERT DUE TO FAILURE OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. SUBSEQUENT REPLACEMENT WITH NEW YAW DAMPER AND OPERATIONS CHECK WERE ACCOMPLISHED WITH NO FURTHER ANOMALY. 2L72 4F4 FRTA28NM E40NE 20040607000532004060700053WP 2004 6 7 04FDEA01613 120031201A5512 SKIN PANEL DOUG DC10 DC1010 3022110WP HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25383FE 46616 HORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANELS CRACKED. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-72224 (REF FEDEX NRC N0410) REPLACED PANELS: ALC7205-1, ALC7206-1, ALC7207-1, ALC7208-1. 2L73 4F A22WE 20040713000902004071300090NM 2004 7 13 TSAA0453007 120031120A53206546563 SPLICE BOEING737 737230 1384401NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE DAMAGED AREA, VERIFIED CORROSION FREE USING 10X INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20050222002222005022200222 2005 2 22 ERAA097086 420031016A2562 SWITCH BELL 412 412 1182202SW ELT STUCK E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03167EH 66791 33089 G SWITCH WAS STUCK, NOW IS TOO SENSITIVE. BATTERY EXPIRED ACTION TAKEN, REPLACED G SWITCH, REPLACED BATTERY PACK. REPLACED G SWITCH. REPLACED BATTERY PACK, TESTED ELT IAW ARTEX PROCEDURES. 1G72 4U H4SW 20030819001912003081900191NM 2003 8 19 SWAA031780 120030808A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 DURING SCHEDULED C2 CHECK, FOUND EEPLS SECTION CRACKED AND LENS MISSING. REMOVED AND REPLACED EEPLS SECTION AND INSTALLED LENS. 2L72 4F RTA16WE 20030402000552003040200055NM 2003 4 2 2003UALA00332 120030325A335020131 BATTERY PACK BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29917UA 25384 EMERGENCY ELECTRICAL LIGHTING (EEL) ADJACENT TO ROW 18 INOPERATIVE. REPLACED EEL BATTERY PACK AND FEEDER STRIP. 2L72 4F4 FRTA16WE E2GL 20030821001262003082100126NM 2003 8 21 03FDEA00898 120030617A5753ARC41252 STOP FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT WING O/B FLAP STOP FITTING (NR 2 FLAP VANE TRACK) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-67554 PT 1 - WINGS OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR. 2L73 4F RTA22WE 20030404000412003040400041NM 2003 4 4 DL73S030090 120030125A2110 DUCT BOEING737 737232 1384475NM RT PACK FOD A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27321DL 23093 A/C DIVERTED TO ATL EN ROUTE BHM TO CVG WITH RIGHT PACK TRIP OFF AND DUCT OVERHEAT SHORTLY AFTER T/O FROM BHM. PROCEDURES RAN AND PACK RESET SUCCESSFULLY. SHORTLY THEREAFTER HAD FUMES IN ENTIRE AIRPLANE. RAN SMOKE/FUMES PROCEDURE WITH NO AVAIL. OPERATED RT PACK ON GROUND IN ATL WITH NO OVERHEAT OR ABNORMALITIES. REMOVED DEBRIS FROM DUCT. 2L72 4F RTA16WE 20030414000462003041400046CE 2003 4 14 CA030312021 120030308A79311303800455 INDICATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3A NE OIL PRESSURE FAILED W D RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CA (CAN) DURING TAXI, FLIGHT CREW NOTED INCREASE IN OIL TEMPERATURE ON RIGHT ENGINE. CREW ELECTED TO RETURN TO GATE. MAINTENACE FOUND OIL TEMP PORTION OF DUAL INDICATOR (PRESSURE) AT FAULT. INDICATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20030411000172003041100017NM 2003 4 11 SWAA030756 120030404A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030410000492003041000049NM 2003 4 10 SWAA030635 120030320A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 505 AND BS 508, ABOVE STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030424000522003042400052NM 2003 4 24 QXEA0300376 120030319A5410 SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - NR 2 COWL AFT CONE SUPPORT CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030429000312003042900031NM 2003 4 29 P5CA0300810 120030127A5522 PANEL BOEING747 747283B 1384867NM ELEVATOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 ELEV NR 334JB HONEYCOMB PANEL HAS A HOLE AND DELAMINATION. REPAIRED BY BONDING FIBERGLASS PLIES USING VACUUM BAG PER SRM 51-40-09. 2L74 4F A20WE 20030429001202003042900120SO 2003 4 29 RAIA00304104 120030407A3610S20226 SEAL EMB 145 EMB145LR 3260212SO NR 2 ENGINE DETERIORATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03821HK 145068 MLI- ENGINE NR 2 BLEED LEAK WARNING. MAINTENANCE REMOVED AND REPLACED GAMA DUCT O-RING, OPS CHECK OK. 2L72 4T RTT00011AT 20030501001122003050100112WP 2003 5 1 ASAA0380121 120030204A57535913528 SEALANT DOUG DC9 DC983 3022083WP TE FLAP MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OAK - DURING C-CHECK, LT WING TRAILING EDGE OUTBOARD FLAP HINGE PIVOT BOLT SEALANT WAS FOUND TO BE MISSING. REPLACED SEALANT IAW ALASKA EA 57-50-10198. (M) 2L72 4F RTA6WE 20030505001102003050500110NM 2003 5 5 AWXA200300428 120030403A5320BAC1493557 CHANNEL BOEING757 757225 1384959NM FLOORBEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM CHANNEL AT BS 377 TO BS 410, RBL 15. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM CHANNEL BS 377 TO BS 410, RBL 15; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 141N5162-6; INSTALLED REPAIR PART IAW B757-200, SRM 51-40-02, PG 7-8. 2L72 4F RTA2NM 20030506001962003050600196EA 2003 5 6 A6WA200340040 120030330A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA AIR CONDITIONINGCONTAMINATED A A6WAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL31431AW 7256 SMOKE FROM LEFT PACK ON ROTATION UPON INVESTIGATION FOUND SMOKE TO BE FROM RESIDUAL DE-ICE FLUID. OPERATED ENGINE AT POWER WITH BLEEDS OPEN AND CLEARED COCKPIT AND CABIN FROM SMOKE. NO FURTHER DEFECTS AT THIS TIME. (M) 2L72 4F RTA21EA 20030506001372003050600137WP 2003 5 6 GTIA030188 120030223A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 RBL 9 INCHES TO RBL 48 INCHES, 2 EA, SUPPORT FLOOR CORRODED. FOUND THE AREA STA 200 RBL 9, RBL 40 STA 200 OUT OF LIMIT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20030509000532003050900053 2003 5 9 UO22003F00001 420030425A8300 GEARBOX RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP ENGINE FAILED B UO2RE ENGINE SHUTDOWN O OTHER NRNOT REPORTED 1 GL19894CA 258366 P107285 IN FLIGHT SHUTDOWN, SUSPECT TRANSFER GEARBOX FAILURE. METAL WAS FOUND INSIDE THE TRANSFER GEARBOX. ENGINE IS IN TEARDOWN AND EVALUATION AT THIS TIME. 2L72 4F4 FRTA3EU E6WE 20030513001512003051300151NM 2003 5 13 QXEA0300453 120030406A5414 SKIN BOMBDRDHC8 DHC8401 1390041NM NR 1 NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 NR 1 NACELLE OUTBOARD NACELLE DOOR 412 BL HAS CRACKS AROUND TEN SPOT WELDS ON AFT EDGE OF DOOR, OUTER SKIN. REPAIRED IAW HORIZON AIR EA 6-71-85. 2H72 4T RTA13NM 20030530000342003053000034 2003 5 30 HEEA086540 420030522A3455071121005 CONTROLLER SKRSKYS76 S76A 8143006NE ADF MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 ADF CONTROLLER IS UNREADABLE. IN SHOP REPAIR. 1G72 3U H1NE 20030604001722003060400172NM 2003 6 4 UPS03440592 120030412A575365B078791 RIB BOEING747 747121 1384871NM NR 8 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C LT WING - NR 8 VC FLAP I/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1,2,6 & 8. (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 & UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030521000092003052100009WP 2003 5 21 DHL2003804909 120030211A5751 SKIN DOUG DC8 DC873F 302199FWP LT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT INBOARD AILERON L/E UPPER SKIN SURFACE WITH 0.500 INCH CRACK AT STA XA.502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 PG 2. REMOVED UPPER SKIN ON LT INBOARD AILERON L/E STA XA. 502.000 IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6 0.040) IAW SRM 57-8-1 PG 2. CLEANED, TREATED AND PRIMED INNER SKIN IAW SRM 51-1-8B. INSTALLED NEW SKIN ON LT INBOARD AILERON L/E IAW SRM 57-8-1 PG 2 , SRM 51-1-21 PG 1, SRM 51-1-15 PG 1 FOR REMOVAL/INSTALLATION SEE N/R 2152 AND REBALANCE SEE N/R 2658. 2L74 4F RT4A25 20030521000222003052100022WP 2003 5 21 DHL2003604503 120030427A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBOARD L/E FORMER AT STA XFS 835.000 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AT XFS 835.000 IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030610000402003061000040EU 2003 6 10 188721 120030527A7600 WARNING LIGHT SAAB SF340 SF340A 7850100EU COCKPIT ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1743SZ 340A043 FLIGHT 4506 FROM PIT TO CRW. SHORTLY AFTER TAKEOFF AFTER THE LANDING GEAR RETRACKED, AIRCRAFT RECEIVED THE FLIGHT IDLE STOP OPEN LIGHT. AIRCREW CYCLED THE GEAR AND THE FLIGHT IDLE STOP OPEN LIGHT STAYED ILLUMINATED. AIRCRAFT RETURNED SAFELY TO PIT. 2L72 4T RTA52EU 20030610000722003061000072NM 2003 6 10 DL73S030413 120030430A53109078224 GUSSET BOEING737 737232 1384475NM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 FUSELAGE / L1 DOOR OPENING / FWD FRAME / LOWER HINGE CUTOUT:GUSSET CRACK REPAIR THE FWD FRAME OF THE L1 DOOR OPENING STRUCTURE WAS FOUND WITH A CRACK IN THE 'H' GUSSET AT THE LOWER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 384998-14, REV A. 2L72 4F RTA16WE 20030611001112003061100111EU 2003 6 11 HEEA086715 120030521A243230248001 BATTERY BOLKMS105 BO105S 5626006EU MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036607K S841 BATTERY HAS NO CHARGE. REPAIRED. 1G72 3U H3EU 20030612001882003061200188NM 2003 6 12 EIA2003073 120030501A5315 FLOORBEAM BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 STA 440 RBL 52.0, FLOORBEAM WEB IS CRACKED RIGHT BELOW SEAT TRACK. 2L74 4F RTA20WE 20030613000072003061300007EA 2003 6 13 SWIA200312060 120030421A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 FS 280 PILOT'S BULKHEAD LBL 90 AFT FLOOR ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-138 NC. 2L72 4F4 FRTA21EA E15NE 20030613000952003061300095NM 2003 6 13 UPS03440806 120030523A5753 SKIN BOEING747 747200 1384847NM TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FX FLAP JOINT OUTER SKIN AT BS 1688 S46R 1EA TOP ROW FASTENER HOLE (JUST AFT OF EXISTING REPAIR PATCH) FOUND CRACKED APPROX 0.040 INCH RUNNING AFT. REF NRC 7496 & 7484 FOR SKIN REPAIRED AS PER SRM 53-30-03 FIG 17. 2L74 4F RTA20WE 20030618000622003061800062NM 2003 6 18 SWAA031307 120030611A52406547952 SKIN BOEING737 7373H4 1384600NM SERVICE DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR SKIN CRACKED AT AFT LOWER CORNER CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030620000332003062000033SW 2003 6 20 HEEA087432 120030612A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 LEFT FUEL PRESSURE LOW LIGHT FUNCTIONS INTERMITTENTLY. 1G71 3U O H2SW 20030618000272003061800027NM 2003 6 18 SWAA031321 120030613A53126545819121 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND NLG W/W CRACKED (2 EA) AT RT UPPER WEB TIRE BRAKE ATTACH HOLES. REPAIRED UPPER WEB PER SWA EA. 2L72 4F RTA16WE 20030623000342003062300034NM 2003 6 23 2003F00374 120030319A3010 BOOT DHAV DHC8 DHC8103 1386005NM CORRODED A KPVAK NONE O OTHER ININSP/MAINT 1 WP13805WP 353 DE-ICE BOOT LEADING EDGE 513BL SURFACE CORROSION ALONG TRAILING EDGE TOP AND BOTTOM, LEFT SIDE. REMOVED SURFACE CORROSION AND TREATED. APPLIED PAINT, COATING IAW 8 MM 30-10-46 PAGE 231. (M) 2H72 4T RTA13NM 20030717000772003071700077GL 2003 7 17 HEEA088069 220030705A7320DPUA0101 COMPUTER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 INTELLASTAR INTERMITTENT LIGHT. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20030710001262003071000126 2003 7 10 372PA0032 420030608A2230580291025 CONTROL CABLE BOEING737 737306 13844BGNM AUTO THROTTLE FAILED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05372PA 23546 AUTO THROTTLE INOP. RELEASED PER MEL 22-4. 6/18/03: NR 2 ENGINE TELEFLEX CABLE REPLACED ON 06/10/03 PER MM 76-11-07 & 76-11-00. NO AUTO THROTTLE FAILURES HAVE OCCURRED BY PIREP OR INFLIGHT FAULT HISTORY SINCE. REF MM 22-04-00. MEL CLEARED. 2L72 4F RTA16NE 20030710001282003071000128EU 2003 7 10 03169317 120030618A3350 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DAMAGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27317UE 41031 DURING MAINTENANCE INSPECTION, THE FWD CABIN EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED THE WIRING FOR THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030711001002003071100100EU 2003 7 11 DHL2003366519 120030520A5320SR531799A0040 SILL AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 CORROSION ON LOWER SILL, AFT CARGO DOOR AT STA 3845 BELOW SILL DEPRESSOR. REMOVED CORROSION IAW A300 SRM 51-11-12 ORIG. THICKNESS .157 REMOVED .049 REMAINING .108 OUT OF LIMITS. REMOVED LATCH FITTING, WEB, SUPPORT STRUCTURE FOR REPAIR. REMOVED ROLLER TRAY, TRANSITION PANEL FOR ACCESS IAW A300 SRM 51-30-30, 53-17-00. REMOVED OLD DOOR SILL. REINSTALLED NEW DOOR SILL, LATCH FITTING, SUBSTRUCTURE, WEB, ROLLER TRAY, TRANSITION PANEL IAW A300 SRM 51-30-30, 53-17-00. REMOVED AND REINSTALLED DOOR SILL, CABLE IAW A300 MM 25-51-55, OPS CHECK GOOD. 2L72 4F RTA35EU 20030430001922003043000192NM 2003 4 30 SWAA030934 120030426A32106582770 FITTING BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG WALKING BEAM FITTING CORRODED. REMOVED AND REPLACED RT MLG WALKING BEAM FITTING PER MM. 2L72 4F RTA16WE 20030430000332003043000033EA 2003 4 30 COMA0360220 120030428A326016600101 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01973CA23121 7146 FLIGHT 5527 LANDING GEAR DISAGREE, NOSE LANDING GEAR DID NOT EXTEND. REPLACED THE NOSE LANDING GEAR UPLOCK. 2L72 4F RTA21EA 20030430001572003043000157NM 2003 4 30 SWAA030878 120030418A3350300432 LIGHT BOEING737 7377H4 1384404NM EXIT SIGN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29719SW 27853 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030501001042003050100104NM 2003 5 1 ASAA0310031 120030225A5310BAC15061308 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SHEAR TIE AT BODY STATION 986, STRINGER 20L-21L CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. (M) 2L72 4F RTA16WE 20030506000192003050600019NM 2003 5 6 03FDEA00559 120030421A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON SKIN BS 720D-720E LBL 24 - WL 151. 2L73 4F RTA3WE 20030506001192003050600119NM 2003 5 6 CALA0300225 120030425A5315101362404 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAO OTHER O OTHER NRNOT REPORTED 1 SW0977303 23354 FLOORBEAM CORRODED AT STATION 284 RBL 42 BELOW SEAT TRACK. REMOVED DAMAGED SECTION. FABRICATED NEW FLOORBEAM, TREATED, PRIMED AND INSTALLED PER SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 20030506001652003050600165WP 2003 5 6 ASAA0380223 120030307A575359304942 VANE DOUG DC9 DC982 3022082WP TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP VANE DENTS ON INBOARD END. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER SRM. (M) 2L72 4F A6WE 20030507001342003050700134EA 2003 5 7 CA030330002 120030325A2710600908002 PULLEY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON CONTROL SEIZED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA 22606 (CAN) FLT CREW REPORTED A/P TRIM CAUTION MSG ACCOMPANIED WITH FLASHING 'A' ON THE PFD WHILE CLIMBING THROUGH 25,000 FT (OAT -25C). AFTER A/P WAS DISENGAGED, THE AILERONS WERE NOTABLY STIFF. AN EMERGENCY WAS DECLARED AND THE CREW ELECTED TO DIVERT.UPON REACHING FL150 (OAT -14C), THE CREW REPORTED THAT THE AILERON MOVEMENT SUDDENLY RETURNED TO NORMAL AND THAT THE STIFFNESS WAS NO LONGER EVIDENT. THE AIRCRAFT CONTINUED ON THE DIVERSION AND LANDED WITHOUT FURTHER INCIDENT. INSPECTION OF THE RIGHT WING CABLE RUN FOUND PULLY P/N 600-90800-2 AT WS 291.5 SEIZED. 2L72 4F4 FRTA21EA E15NE 20030508001102003050800110NM 2003 5 8 DLM88030373 120030418A26131173T0640 SENSOR DOUG MD88 MD88 3023688NM EMPENNAGE LOOSE A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27920DL 49644 TAIL TEMP HIGH MESSAGE DURING CLIMBOUT. FOUND CLAMP LEAKING FROM LT PRESSURE REGULATOR VALVE AND SECURED BOTH CLAMPS. REPLACED BOTH TEMP COMPT. OVERHEAT SENSORS FOR PRECAUTION PERFORMED GROUND CHECK AT NORMAL T/O PER PFHB 9-0-7-7 TEST B-TAIL HIGH TEMP LIGHT DID NOT ILLUMINATE. TESTS GOOD. 2L72 4F RTA6WE 20030509000232003050900023NM 2003 5 9 MEX2003136 120030414A3320 CONTROL PANEL DOUG MD88 MD88 3023688NM LIGHTS FAILED A ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23162PL 49765 AIRCRAFT RETURN TO PLATFORM DUE TO F ELECTRICAL PANEL OUT OF SERVICE. TECHNICAL PERSONNEL REPORTED THAT THE CENTRAL PANEL INTEGRAL LIGHTS BREAKER POPPED OUT. REPORT WAS DEFERRED IAW MEL 33-1. AT MEX WIRE WAS REPAIRED IAW MM 33-13-03 AND TEST WERE CORRECT IAW MM 33-13-02. (M) 2L72 4F RTA6WE 20030513001262003051300126WP 2003 5 13 UPS03840676 120030413A534058903141 FITTING DOUG DC8 DC873F 302199FWP A/C BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C1, STA. 45-70 AT APPROX. LBL. 48 AT OVERHEAD IN AC BAY HAS A CRACKED FITTING. REMOVED,FABRICATED AND INSTALLED FITTING IAW DWG. 5890314,AND SRM 51-1-20D,51-3-0 2L74 4F RT4A25 20030514000982003051400098NM 2003 5 14 SWAA030999 120030505A5753 SKIN BOEING737 737301 1384611NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C2 CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20030604000032003060400003SO 2003 6 4 SIMA200311803 120030421A531314525768617 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 ABI - DURING A IMBV INSPECTION STRINGER 19L WAS FOUND TO HAVE A 2.3 INCHES LONG CHAF BELOW SRM LIMITS. BLENDED THE CHAFE AREA AND PERFORMED AN NDT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A REPAIR DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/1332. (M) 2L72 4F RTT00011AT 20030604000332003060400033SO 2003 6 4 SIMA200312705 120030416A532014522459003 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION GALLEY CENTER BEAM RAMP CORRODED. REMOVED AND REPLACED CENTER GALLEY BEAM IAW EMB 135 SRM 51-40-2/04, 51-20-03. (M) 2L72 4F RTT00011AT 20030604001602003060400160NM 2003 6 4 UPS03440580 120030412A575365B106251 RIB BOEING747 747121 1384871NM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 LT WING - NR 4 VC FLAP I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1, 3, 4, 6 & 8. ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030714000632003071400063NM 2003 7 14 SWAA031365 120030616A53306546881 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1016, BETWEEN STR 3R AND 4R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030127000112003012700011 2003 1 27 HEEA083587 420030114A34215040017928 INDICATOR BELL 412 412 1182202SW STANDBY ATTITUDEPRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 STANDBY ATTITUDE PRECESSES. SHOP REPAIR. 1G72 4U H4SW 20030127000692003012700069EU 2003 1 27 MALA030107 120030111A3230 LANDING GEAR BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15525XJ E2350 DURING FLIGHT 3511, UPON GEAR RETRACTION THE LEFT MAIN GEAR WOULD NOT RETRACT. RECEIVED RED INDICATOR AND RED UNSAFE LIGHT IN GEAR HANDLE. CYCLED GEAR 3 TIMES WITH NO LUCK. AIR RETURN TO DTW. MAINTENANCE REMOVED ICE BUILDUP FROM BOTH LT & RT MLG WHEEL WELLS. CLEANED AND LUBRICATED BOTH MLG'S. PERFORMED 10 NORMAL GEAR RETRACTIONS AND EXTENSIONS. TESTS ALL CHECK GOOD AT THIS TIME. 2H74 4F RTA49EU 20030128000142003012800014GL 2003 1 28 HEEA083766 220030115A725023062087 CHECK VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE SMOKE E HEEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW03742PH 53461 CHECK VALVE SMOKING ON SHUTDOWN. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128001992003012800199NM 2003 1 28 AWXA200300027 120030111A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28817AW 1373 SAN - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT CABIN EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030128002712003012800271NM 2003 1 28 371PA0015 120030118A56105893543129 WINDOW BOEING737 737306 13844BGNM A PIDAA UNSCHED LANDING O OTHER CLCLIMB 1 SO05371PA 23543 #1 captain's window cracked climbing through 17000 feet. Removed and replaced #1 captain'swindow per MM 56-11-11 2L72 4F RTA16NE 20030131000772003013100077SO 2003 1 31 C2XA03TY015 120030131A575114569009406 BRACKET EMB 145 EMB145LR 3260212SO DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 TYS, During a scheduled inspection both left hand outbd aileron PCA attachmrnt points have migrating bushings. Maintenance removed and replaced the aileron attchment bracket I/A/W-EMB-SRM-51-21-04/05/06 and EC5750-0117. Aircraft will be released to service upon complection of inspection. 2L72 4T RTT00011AT 20030203000212003020300021CE 2003 2 3 CA030113005 120030110A5520115610010125 SPLINE ADAPTER BEECH BEECH 100 A100 1152915CE PWA PT6 PT6A34 52043EA ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 19863 B169AB169B (CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS, THE SPLINES WERE FOUND CRACKED AT SEVERAL LOCATIONS, THIS IS THE 7TH SDR REGARDING THESE SPLINES AND A TOTAL OF 11 SPLINES FOUND CRACKED. THE ELEVATORS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. WE ARE CURRENTLY CONDUCTING A FLEET INSPECTION. 1L72 3T4 T A14CE E4EA 20030203002072003020300207EA 2003 2 3 A6WA200340004 120030102A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY MALFUNCTIONED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31422AW 7341 STRONG FUEL ODOR WHEN APU WAS START AND BLEED SWITCH OVER IN FLIGHT, CONTINUED UNTIL APU WAS SHUTDOWN. PLACED APU ON MEL. (M) 2L72 4F RTA21EA 20030204000822003020400082NM 2003 2 4 SWAA030140 120030120A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME LOWER SIDE CRACKED AT BS 460, STR 28. REPAIRED CRACKED SECTION OF FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20030205000352003020500035NM 2003 2 5 SROM200300002 120030104A7810 FAIRING BOEING737 737205 1384456NM NR1 ENG TAILPIPEGOUGED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 1 TAIL PIPE FAIRING LOPWER CORNER DAMAGED. REPAIRED PER SRM 54-10-1. MONOR REPAIR. 2L72 4F RTA16WE 20030213001042003021300104EA 2003 2 13 COMA0360097 120030210A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORZ. STAB UNRELIABLE A COMAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 SO01716CA7271 7250 FLIGHT 5438 STAB CHANNEL 1 IS INOP.REPLACED THE HSTA. 2L72 4F RTA21EA 20030218000022003021800002EA 2003 2 18 03025319 120030125A3260 UPLOCK SWITCH CNDAIRCL600 CL6002B19 1900309EA GARRTTTPE331TPE331* 01514WP LT MLG OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27319UE 41042 LT MLG INDICATOR RED LIGHT ILLUMINATED. ADJUSTED LT MLG UPLOCK SWITCHES, OPS CHECKED OK. 2L72 4F3 TRTA21EA E2WE 20030218002082003021800208NM 2003 2 18 SWAA030296 120030207A3350101114 LENS BOEING737 7373H4 1384600NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20030219001492003021900149EU 2003 2 19 USAABA03002 120030122A335032146210 POWER SUPPLY AIRBUS330 A330323 3930335EU L3 DOOR FAULTY A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19672UW 0333 PHL - EPSU SHOWS A UNIT FAULT. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA46NM 20030604001872003060400187NM 2003 6 4 UPS03440608 120030413A5330 SKIN BOEING747 747121 1384871NM WINDOW BELT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BET. BS 1438 - 1460 RT WINDOW FORGINGS FOUND CORRODED. WINDOW FORGING AREA SKIN REPAIRED AS PER HX RS R53-21-35018 AND ENG'R FILE 747-53-20137. CORROSION BLEND OUT 0.043" X 1" X 1". 2L74 4F A20WE 20030515001782003051500178NM 2003 5 15 AWXA200300521 120030509A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 5 INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28156AW 23778 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030604001062003060400106NM 2003 6 4 UPS03440521 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 960 BET S23 - 24R FRAME FOUND CRACK. BS 960 BETWEEN S23R TO S25R FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20030605000432003060500043NM 2003 6 5 WRLA200311 120030515A2613355194310 SENSOR DOUG MD11 MD11F 3023600NM NR 2 ENG OVRHT SHORTED A WRLAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA27276WA 48632 ENGINE 2 ANTI-ICE OFF LEVEL 1 ILLUMINATED WHEN ENGIEN 2 ANTI-ICE SELECTED ON. ENGINE 2 ANTI-ICE DUCT FAIL LEVEL 3 ILLUMINATED. SECURED NR 2 ENGINE. FOUND DUCT OVERHEAT SENSOR SHORTED TO GROUND, D1-90 PN 35519-4-310 PERFORMED MANIFOLD OVERHEAT AND AIR SYSTEM TEST ALL INDICATION NORMAL. PERFORMED ENGINE RUN NR 2 CYCLED ENGINE 2 ANTI-ICE VALVE SEVERAL TIMES ALL INDICATIONS NORMAL. REPLACED DUCT OVER HEAT SENSOR. (M) 2L73 4F RTA22WE 20030606000072003060600007SO 2003 6 6 GLBA2003063 120030518A7700 WARNING LIGHT EMB 120 EMB120ER 3260203SO LT ENGINE ILLUMINATED A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03299UX 120299 LEFT ENGINE T6 RED ANN. CAME ON AND AUDIO WARNING T6 SOUNDED, PREFORM GROUND RUN AND FOUND ALL PARAMETERS TO BE WITH IN LIMITS 2L72 4T RTA31SO 20030606000552003060600055EA 2003 6 6 COMA0360239 120030518A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01708CA2293 7235 FLIGHT 5237 EMERGENCY LIGHTING IS INOPERATIVE. REPLACED ALL FOUR DISCHARGED EMERGENCY BATTERY PACKS (SAME P/N). 2L72 4F RTA21EA 20030521001342003052100134NM 2003 5 21 DHL2003740003 120030502A33501000677 LIGHT BOEING727 7272Q9 138448MNM PAX DOORWAY INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01740DH 21930 EMERGENCY EXIT LIGHT IN ENTRYWAY VERY DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW B727 M/M 33-50-111. OPS CHECKED SATISFACTORY. 2L73 4F RTA3WE 20030522000102003052200010NM 2003 5 22 0300996638 120030518A29133508806 PUMP BOEING747 747251B 1384892NM HYD SYSTEM LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01638US1748 1748 23549 DURING CRUISE THE HYDRAULIC FLUID QUANTITY IN THE NR 4 SYSTEM INDICATED ZERO. AIRCRAFT CONTINUED TO DESTINATION, ALTERNATELY EXTENDED THE LANDING GEAR AND LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 4 ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030613000662003061300066WP 2003 6 13 UPS03840798 120030604A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, OPS NORMAL. 2L74 4F RT4A25 20030613001262003061300126NM 2003 6 13 SWAA031201 120030529A2560P4010021 BATTERY BOEING737 7375H4 138449DNM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 AFT CABIN LOWER EMEGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20030617001592003061700159SW 2003 6 17 HEEA087299 120030611A6300407010206103 BEARING BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 MAIN ROTOR DRIVE HAS A WORN BEARING. 1G71 3U O H2SW 20030521001752003052100175NM 2003 5 21 DHL2003783008 120030515A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 SHORTED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01766AT 21999 DURING CLIMBOUT OF CVG, NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED INTERMITTENTLY THEN REMAINED ON. FOUND LOOP CONTACTING LOWER ENGINE COWL. RE-SECURED LOOP. OPS CHECKED NORMAL IAW M/M 26-21-0. 2L73 4F A3WE 20030617002292003061700229EA 2003 6 17 QXEA200300702 120030516A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - COPILOTS OUTBOARD SEAT TRACK WORN ON THE TOP INBOARD EDGE. REPAIRED IAW SRM 51-12-00, PAGE 6. 2L72 4F RTA21EA 20030617002882003061700288SW 2003 6 17 HEEA087321 120030611A5610407030118107 CHIN BUBBLE BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 WINDOW CRAZED AROUND OUTER EDGE. REPLACED WINDOW. 1G71 3U O H2SW 20030618000652003061800065 2003 6 18 HEEA087128 420030610A34424000023 TRANSCEIVER SKRSKYS76 S76A 8143006NE WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 CAUSES STATIC IN OTHER RADIOS. HAS LIMITED TRANSMIT RANGE IN FLIGHT. SHOP REPAIR. 1G72 3U H1NE 20030221000162003022100016NM 2003 2 21 AWXA200300063 120030111A531265163007 WEB BOEING737 737300 1384610NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT SIDE OF BULKHEAD WEB BS 178, LBL 4.7, WL 201, CONFIRMED BY HFEC. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG. 287-288J, FIG. 211. 2L72 4F RTA16WE 20030221000432003022100043NM 2003 2 21 QXEA0300154 120030123A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX- NR 2 NACELLE OUTBOARD FIREWALL IS CRACKED AT THE BEND ABOVE FIRE LOOP BRACKET. REPAIRED IAW DHC-8 RD 8-54-806. 2H72 4T RTA13NM 20030224001362003022400136NM 2003 2 24 AWXA200300186 120030128A5320146N5447 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1471, STR 28 - 29R. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AREA OF FLOOR SUPPORT BS 1471, STR 28 - 29R; FABRICATED REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1-7. 2L72 4F RTA2NM 20030114002522003011400252EA 2003 1 14 COMA0360020 120030111A3240428853 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA9533 7017 FLIGHT 5897 ANTI-SKID GEAR DISAGREE WARNING WHILE LANDING GEAR INTRNASIT.REPLACED THE ANTI-SKID CONTROL UNIT. 2L72 4F RTA21EA 20030121000522003012100052SW 2003 1 21 HEEA083254 120030108A3212206073926107 RELIEF VALVE BELL 206 206L3 1182108SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 EMERGENCY FLOAT RELIEF VALVE LEAKING. REPAIRED. 1G71 3U H2SW 20030303001992003030300199WP 2003 3 3 DHL2003804544 120030130A27505751153501 LINK DOUG DC8 DC873F 302199FWP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF. N/R: LH FLAP DRIVE LINK INNER BUSHING FLANGEPOINT "J" WITH .500 LONG CRACK IN IT. CORR: R/R LH FLAP DRIVE LINK @ STA. 219.99 IAW M/M 27-51-4 PG. 201 -204 REFERENCE N/R 0607 FOR OP'S CHECK 2L74 4F RT4A25 20030225000262003022500026SW 2003 2 25 HEEA084245 120030120A5210407070620205 COVER BELL 407 407 1182206SW DOOR STRIKER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 DOOR STRIKER COVER CRACKED. 1G71 3U O H2SW 20030225000672003022500067SW 2003 2 25 HEEA084289 120030211A3212 VALVE BELL 206 206L1 1182107SW FLOAT BOTTLE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032764F 0365 45279 EMERGENCY FLOAT BOTTLE HAS CORROSION ON VALVE. REPAIRED. 1G71 3U H2SW 20030226000102003022600010SW 2003 2 26 HEEA084308 120030211A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 TAIL ROTOR DISC PACK PITTING ON DISC. 1G71 3U O H2SW 20030227000462003022700046 2003 2 27 HEEA084377 420030211A2350AMS44 KNOB BELL 407 407 1182206SW AUDIO CONTROL LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 LOOSE KNOBS. REPLACED BAD RECEIVE VOLUME KNOBS AND BAD ICS/VOX KNOB. TIGHTENED LOOSE PILOT RECEIVE VOLUME KNOB SHAFT. REPAIRED. BENCH CHECK GOOD. 1G71 3U O H2SW 20030310001382003031000138NM 2003 3 10 EIA2003011 120030226A5300UNK SKIN PANEL BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 External Skin Repair, at Station 1580 Stringer 35L to 36L is not per S.R.M. CORRECTIVE ACTION: Removed external skin repair, fabricated new fillers,(2 ea.) and doubler. Alodined, primed and installed per Boeing SRM 51-30-03, Page 2A-2F, and SOPM Ch. 20-41-02, Page 17-19. Category "B" Repair, COI #052 initiated. 2L74 4F A20WE 20030311000962003031100096EA 2003 3 11 COMA0360139 120030303A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO01999CA 7230 FLIGHT 5609 GEAR DISAGREE WARNING, NLG DOORS OPEN WARNING.NLG CENTERED, PROX SENSOR TARGET OUT OF RANGE, ADJUSTED PROX SENSOR. 2L72 4F RTA21EA 20030317000532003031700053NM 2003 3 17 SWAA030569 120030311A53116546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 500D, BELOW STR 10R. R&R SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030121002572003012100257NE 2003 1 21 PCAA0301001 220030101A7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RT ENGINE LOW A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA13804EX 227 ABE- PIT FLIGHT 3511 CREW REPORTED WHILE ON DESCENT THROUGH 8000 FT UNKNOWN SMELL WAS NOTICED IN COCKPIT AND CABIN. SMELL WAS SUSPECTED TO BE SMOKE COMING FROM NR 1 ENGINE BLEED. EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED APU AND SURROUNDING AREA. NO DEFECTS WERE NOTED. ENGINE OILS WERE CHECKED, AND RIGHT ENGINE FOUND TO BE 3 QUARTS LOW, LEFT ENGINE 1 QUART LOW. OIL WAS SERVICED. AIRCRAFT GROUND RAN FOR 20 MINUTES WITH BLEEDS ON. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030122000102003012200010SW 2003 1 22 HEEA083397 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 MAIN BATTERY WEAK. SCRAPPED. 1G71 3U H2SW 20030122000942003012200094WP 2003 1 22 ZW0A0300902 120030119A33507732 BULB DOUG DC9 DC983 3022083WP A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13982TW 53632 IN ARM EGRESS FLOOR LIGHT OUT AT ROW 5 DUE TO WEAR OF DESIGN DEFICIENCY. RESEATED BULB IN ROW 5 EGRESS FLOOR LIGHT SOCKET. EMERGENCY EGRESS LIGHT SYSTEM OPS CHECK PER MM33-59-00. CKECK-C 11-19-02 STL. --CLOSED-- 2L72 4F RTA6WE 20030529000492003052900049SW 2003 5 29 HEEA086640 120030521A3212412050013113 FLOAT BELL 412 412 1182202SW MLG LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 MLG EMERGENCY FLOAT REINFORCEMENTS LOOSE. 1G72 4U H4SW 20030617003002003061700300NM 2003 6 17 SWAA031218 120030602A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND SHEAR TIES CORRODED (2 EA) AT BS 747, WL 148, RBL 10 AND BS 847, WL 148, BL 0. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20030701000272003070100027EU 2003 7 1 HEEA087879 120030110A6220704A3363315651 STOP AEROSPAS355 AS355* EU MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034031L2195 2907 MAIN ROTOR SPHERICAL STOP WORN AND HAS BULGING RUBBER. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030625000252003062500025WP 2003 6 25 MWEA030234 120030528A5340993666441 ATTACH FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 KINGPOST ATTACHING FITTINGS AT STATION 1322 AND LONGERON 30 HAS BAD EDGE DISTANCE AND CORROSION REPAIR IN THE AREA WILL MAKE HOLES UNUSABLE. -- FABRICATED AND INSTALLED FITTINGS. 2L72 4F A6WE 20030707000452003070700045NM 2003 7 7 AALA20030111 120030125A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21913AN 29514 DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. REPLACED LEFT AFT OVERWING EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030709000952003070900095WP 2003 7 9 MWEA030244 120030610A2150 FITTING DOUG DC9 DC981 3022081WP LT AC PACK LOOSE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31805ME 48031 LEFT PACK INOPERATIVE. FOUND AUG VALVE FITTINGS LOOSE. RESECURED LOOSE FITTINGS. 2L72 4F A6WE 20030709001012003070900101SO 2003 7 9 C2XA03CL108 120030611A335074441 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714933 145018 THE CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT MARKING SIGN. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030717000162003071700016SW 2003 7 17 HEEA087993 120030701A2432 CELL BELL 407 407 1182206SW BATTERY BURNED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 9900455 53266 BATTERY CELL BURNED. REPLACED BATTERY. 1G71 3U O H2SW 20030109001202003010900120WP 2003 1 9 ABXA030005 120030105A273099185296 RIB DOUG DOUG DC9 DC932 3022066WP RT. ELEVATOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 03340 47426 RIGHT ELEVATOR CRACKED ON INBOARD BULKHEAD COMMON TO FORWARD TORQUE TUBE. CRACK WAS IN LOWER FLANGE AT SPLICE AREA TO HINGE FITTING. VERIFIED WITH X-RAY AND BORESCOPE VISUAL. REPLACED RIGHT ELEVATOR IAW DC-9 MM. 2L72 4F A6WE 20030115000952003011500095SO 2003 1 15 C2XA03CL011 120030114A750014531128402 MANIFOLD EMB 145 EMB145ER 3260211SO #2 ENGINE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 DURING INSPECTION MAINTENANCE FOUND THE #2 ENGINE BLEED DUCT MANIFOLD CRACKED APPROX. 4.5 INCHES.THE DUCT IS LOCATED AT THE 14 STAGE BLEED VALVE AT THE TOP OF THE ENGINE.MAINTENANCE REPLACED THE 14TH STAGE CUSTOMER BLEED DUCT MANIFOLD.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030124000102003012400010NM 2003 1 24 219PA0005 120030124A33501000679 LIGHT BOEING737 737222 1384473NM A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05219PA 19956 Emergency light above aft service door inop. Removed and replaced emergency light above aft service door Ref. MM 33-50-09. Ops. chk. good per MM 33-50-01. 2L72 4F A16WE 20030128000012003012800001SW 2003 1 28 ALGA084009 120030120A6320407040035101 BEVEL GEAR BELL BELL 407 407 1182206SW TRANSMISSION SCORED H ALGAK NONE O OTHER ININSP/MAINT 1 FS01697AL2457 A388 53374 ON DISSASSEMBLY FOUND 30 BOLTS ON GEAR SHAFT WERE LOOSE, MATING SURFACE FRETTED BEYOUND LIMITS IN CR&O MANUAL. THIS WAS THE FIRST TIME UNIT WAS DISSASSEMBLED SINCE NEW. REMOVED AND REPLACED BEVEL GEAR. 1G71 3U O H2SW 20030129000192003012900019SW 2003 1 29 HEEA083929 120030117A6220 SPRING BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH A519 53003 MAIN ROTOR HEAD FRAHM ASSY HAS SPRINGS BROKEN. 1G71 3U O H2SW 20030129001552003012900155EU 2003 1 29 HEEA084007 120030114A3340 BRACKET BOLKMS105 BO105S 5626006EU LANDING LIGHT CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 BOTH LANDING LIGHTS HAVE CRACKED MOUNT BRACKETS. REPLACED LIGHTS. 1G72 3U H3EU 20030129001832003012900183NM 2003 1 29 UPS03240101 120030107A5310 WINDOW FRAME BOEING727 72722C 138400FNM BS 1100 L/H S12 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C&SI CRACK ON WINDOW FRAME BS 1100 L/H STR. 12 CRACK STOP DRILLED IAW SRM 51-10-1 SEE SMRO EO 2003-003-009 FOR REPAIR INSTRUCTION. UPS ENG. FILE NO. 727-53-20092 2L73 4F A3WE 20030208000052003020800005SO 2003 2 8 RAIA00301022 120030122A3210852701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03802HK2234 145066 5264-PIT- MAIN GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED #1 GEAR PROX SWITCH, OPS CK OK. 2L72 4F RTT00011AT 20030210000342003021000034NM 2003 2 10 QXEA0300019 120030107A27207G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM RUDDER INOPERATIVE A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09366PH 510 SEA-ON FLIGHT NUMBER 2065, ON DEPARTURE WHEN AIR SPEED INCREASED ABOVE 140 KTS, MASTER CAUTION ILLUMINATED WITH RUDDER PRESSURE & RUDDER FULL PRESSURE CAUTION LIGHTS. COMPLETED ABNORMAL/EMERGENCY CHECKLIST AND MAINTAINED 200 KTS. REMOVED AND REPLACED BOTH RUDDER HYD DUAL PRESSURE SWITCHES. OPERATIONAL TEST OF PRESSURE REGULATOR AND ACTUATOR SOLENOID VALVES CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030218000032003021800003EA 2003 2 18 03025319A 120030125A3260 DOOR CNDAIRCL600 CL6002B19 1900309EA GARRTTTPE331TPE331* 01514WP LT MLG OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27319UE 41042 GEAR HANDLE IN TRANSIT RED LIGHT AND LT RED MAIN GEAR LIGHT ILLUMINATED AFTER TAKEOFF. ADJUSTED MAIN LANDING GEAR DOORS, OP'S CHECKED GOOD. 2L72 4F3 TRTA21EA E2WE 20030220001732003022000173WP 2003 2 20 ARWA20030109 120030130A3260805008 PROXIMITY SENSOR LKHEED1011 1011385115 5265015WP MLG FAILED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19307GB 193U1131 DURING RETRACTED GEAR RED INTRANSIT LIGHT ON FLIGHT ENGINEER PANEL SHOWS RT GEAR DOOR LIGHT ON WITH GEAR DOWN. ALL INDICATIONS NORMAL. WITH GEAR UP NO FEEL VIBRATION. RETURNED TO MIA. REMOVED AND REPLACED PROX SWITCH CARD J-7. PERFORMED MAIN LANDING GEAR RETRACK SEVERAL TIMES, OPERATIONS NORMAL IAW MM 32-30-00 PG. 501. 2L73 4F A23WE 20030221000832003022100083NM 2003 2 21 AWXA200300178 120030129A5320146N5444 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT FRAME AFT CARGO COMPARTMENT, BS 1510, RBL 11. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SECTION OF FLOOR SUPPORT FRAME BS 1510, RBL 11; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1. 2L72 4F RTA2NM 20030226000652003022600065EU 2003 2 26 NSVA200300012 120030223A7500 CONNECTOR SAAB SF340 340B 7860101EU A NSVAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27252CJ 340B252 First flight from CHO-RH Bleed air light on in flight. RH Engine shut down, emergency declared. Aircraft diverted to PHL, landing was uneventful. MX T/S/Bleed Air indicating system IAW SAAB AMM 36-00-00 Fault Isolation. Found slight corrosion and moister on connector at fire loop fuselage and flap swing down panel. Cleaned connector and replaced corroded washer. OP's check good. 2L72 4T RTA52EU 20030303000222003030300022SW 2003 3 3 HEEA084489 120030214A3246412050015010 CROSSTUBE BELL 412 412 1182202SW MLD CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 FWD CROSSTUBE COLLAR CRACKED. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030304000452003030400045EA 2003 3 4 COMA0360129 120030301A3030355483255 SENSING ELEMENT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE MALFUNCTIONED A COMAA UNSCHED LANDING JN WARNING INDICATION FALSE WARNING CLCLIMB 1 SO01815CA 7397 FLIGHT 5578 ANTI-ICE DUCT WARNING MESSAGE.REPLACED FUSELAGE SECTION OF BLEED LEAK SENSING ELEMENTS. 2L72 4F RTA21EA 20030306000212003030600021 2003 3 6 HEEA084734 420030217A2340 KNOB BELL 412 412 1182202SW INTERPHONE BOX CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 7806817 33115 SELECTOR KNOB CRACKED AND CAN'T LISTEN TO COMM 1 IN ANY POSITION. FOUND LIGHT PANEL, SWITCH S1, VOLUME KNOB AND TRANSMIT KNOB BAD, ALSO SWITCHES S2 THROUGH S11 HARD TO SWITCH. CLEANED AND LUBED SWITCHES S2 THROUGH S11, REPLACED LIGHT PANEL, SWITCH S1, VOLUME KNOB AND TRANSMIT KNOB. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000522003030600052SW 2003 3 6 HEEA084767 120030221A3246412050015110 SKID BELL 412 412 1182202SW MLG CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 RT SKID TUBE IS CRACKED. 1G72 4U H4SW 20030307001902003030700190 2003 3 7 HEEA084909 420030228A22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS CHATTERING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 AFCS ACTUATOR CHATTERS. 1G72 3U H1NE 20030314001322003031400132WP 2003 3 14 GTIA030109 120030204A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP PWA JT8 JT8D NE FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FLOOR SUPPORT STA 180, RBL6 TO RBL44 IS CORRODED. REMOVED FLOOR SUPPORT. DRILL AND LOCATE. INSTALLED FLOOR SUPPORT ANGLE. INSTALLED FLOOR SUPPORT. 2L72 4F4 F A6WE E2EA 20030318000982003031800098NM 2003 3 18 2003UALA00274 120030314A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE DETERIORATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 EEL PATH LIGHTS FROM FORWARD GALLEY TO BUSINESS CLASS ON RH SIDE VERY DIM. REPLACED BATTERY PACK 2L72 4F4 FRTA1NM E24NE 20030121002812003012100281NM 2003 1 21 CALA0300015 120030119A5347 SEAT TRACK BOEING777 777224 1385225NM BS 1495-1525 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0978005 27581 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1495-1525, RBL 75. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 3. 2L72 4F RTT00001SE 20030122000842003012200084 2003 1 22 HEEA083476 420030110A2312066107800 RECEIVER BELL 412 412 1182202SW GLIDESLOPE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 GLIDESLOPE RECEIVER IS INOPERATIVE. IN SHOP REPAIR. 1G72 4U H4SW 20030319000562003031900056NM 2003 3 19 HALA0200013 120030113A5311 FRAME BOEING717 717200 1383700NM FUSELAGE CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP13477HA 55122 HNL - FOUND LEVEL 2 CORROSION ON THE LOWER HORIZONTAL LEG OF THE 5971057-3 AND 4 FRAMES AT BS 852. CORROSION WAS 100 PERCENT THROUGH HORIZONTAL LEG OF THE FORM AT THE SCREW ATTACH POINTS ON THE LOEWR SIDE. DAMAGE WAS REMOVED BY TRIMMING AND INSTALLING AN ANGLE DOUBLER. (M) 2L72 4F TRA6WE 20030320000402003032000040NM 2003 3 20 USAASB03008 120030114A2611100064904 SMOKE DETECTOR BOEING737 7374B7 1384702NM AFT CARGO BIN INOPERATIVE A USAAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19784AU 25023 PHL - FLT 1761 - EN ROUTE AT FL310, CREW RECEIVED AN AFT CARGO FIRE INDICATION FAULT FOLLOWED BY AN AFT CARGO FIRE INDICATION 3 TO 4 MIN LATER. CAPTAIN DISCHARGED FIRE BOTTLES AND INDICATION IMMEDIATELY EXTINGUISHED. CREW DECLARED AN EMERGENCY AND DIVERTED. AFTER LANDING, AFT CARGO BIN OPENED ON TAXIWAY. NO EVIDENCE OF FIRE OR SMOKE. CREW RESTARTED THE ENGINES AND TAXIED TO THE GATE. MAINT CONFIRMED NO EVIDENCE OF FIRE. FOUND AFT CARGO BIN SMOKE DETECTOR INOP. R & R AFT CARGO SMOKE DETECTOR PER MM 26-15-00 WITH NUMEROUS DETECTOR BATTERIES ALSO, REMOVED AND REPLACED BOTH NR 1 AND NR 2 FIRE BOTTLES, CARGO FIRE BOTTLE SYSTEM METERING VALVE AND DIVERTER VALVE PER MM 26-19-01. OPERATIONAL CHECK NORMAL. (M)2L72 4F RTA16WE 20030320000602003032000060NM 2003 3 20 03FDEA00327 120030317A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 STRINGER END CRACKED AT FASTENER BS 720B PLUS 4 STR 15L. REPAIRED STR 15L BY SPLICING IN NEW REPAIR SECTION STRINGER FROM BS 720A+13, AFT TO LIGHT. REPAIR DONE PER 727 SRM 53-10-3 FIG 1 DETAIL 2. 2L73 4F RTA3WE 20030801000062003080100006WP 2003 8 1 GTIA030524 120030618A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND CABIN FLOORBOARD FS 160-200 LBL 24 INCHES DELAMINATED AND CORRODED INSERTS AND FASTENERS. REMOVED FLOORBOARD. FABRICATED NEW PANEL INSTALLED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030417001982003041700198WP 2003 4 17 ZW0A0302101 120030212A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13964TW 53614 THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE AT ROWS 28 AND 29, AND THE EGRESS FLOOR LIGHT WAS INOPERATIVE AT ROW 21. REPLACED THE BATTERIES IN B5-107 BATTERY PACK, PN 408822-101, FOR THE CEILING LIGHTS, AND RESEATED THE LAMP INTO THE SOCKET FOR THE EGRESS LIGHT. CHECK-C 5-25-02 STL. 2L72 4F RTA6WE 20030417000252003041700025NM 2003 4 17 PCAA0301023 120030126A2910 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM LEAKING A PCAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA13833EX 282 LGA-ITH FLIGHT 3799 CREW REPORTED NR 2 HYDRAULIC QUANTITY LOSS ON TAKEOFF. ISOLATION VALVE LIGHT ILLUMINATED, GEAR PARTIALLY RETRACTED, AND ROLL SPOILER OUTBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED BLUE FLEX LINE AT DRAG STRUT ACTUATOR. HYDRAULIC SYSTEM SERVICED AND BLED. AIRCRAFT GROUND RAN WITH NO LEAKS FOUND. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030422000232003042200023NE 2003 4 22 A6WA200330006 220030309A7261 OIL SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119C NE NR 2 ENGINE OVERSERVICED A ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23335LS 3035 IN CRUISE AT 29,000 FEET, NR 2 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 51-55. INSPECTED AND FOUND OIL OVERSERVICED. REMOVED ONE QUART OF OIL. INSPECTED AND CLEANED OIL PSI CANNON PLUG. GROUND RAN GOOD. (M) 2H72 4T4 TRTA45NM E20NE 20030325000442003032500044NM 2003 3 25 AWXA200300168 120030127A5321146N5300 FLOOR PANEL BOEING757 7572S7 1384962NM GALLEY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND LOWER FLANGE UPPER TEE CAP OF AFT GALLEY DECK PLATE BS 1681 - 1720, LBL 51 TO RBL 51. MAINTENANCE REMOVED AFT GALLEY SHEAR PLATE BS 1681 - 1720, LBL 51 TO RBL 51; FABRICATED A NEW REPLACEMENT AFT GALLEY SHEAR PLATE; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 3-4, 11-12. 2L72 4F RTA2NM 20030327000762003032700076NM 2003 3 27 C1HA200396003 120030227A3231 SWITCH BOEING727 7272J4 1384006NM MLG DOOR LOCK MALFUNCTIONED A C1HAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15696CA 22574 DURING TAXI IN LAS NOSE GEAR DOOR LIGHT ILLUMINATED. OPENED NOSE GEAR DOORS AND INSPECTED DOOR LOCK SWITCH. ADJUSTED NOSE GEAR DOOR ADJ. STRUT & OPS CHECKED DOORS IN REF. TO M/M CH 32-22-01 OPS NORMAL 2L73 4F RTA3WE 20030807000222003080700022NM 2003 8 7 USAA030112 120030611A5320 SILL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US37758 24552 FOUND DOOR SILL CORRODED 2 INCHES BY 6 INCHES - 2 INCHES BY 2 INCHES, Z-ANGLE, AFT SERVICE DOOR CUTOUT, STATION 951 S-17R. REMOVED CORROSION, ALODINE, PRIME PER SRM 51-10-2, 51-20-01. (M) 2L72 4F RTA16WE 20030828000182003082800018NE 2003 8 28 RK26001 220030617A7261 WARNING SYSTEM BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE COCKPIT ACTIVATED E ERYAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE0780DX RK26 PCE100231 TAKEOFF ABORTED DUE TO ILLUMINATION OF LT OIL FILTER BYPASS LIGHT AND LT ENGINE OIL PRESSURE EXCEEDING RED LINE AT TAKEOFF POWER. 2H72 4F4 FRTA16SW E25EA 20030828000422003082800042NM 2003 8 28 XNOA01132 120030610A7711 PROBE BOEING727 727227 1384078NM PWA JT8 JT8D7B 52053NE NR 1 ENGINE PLUGGED A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23793A 20774 653588 ABORTED T/O AT 100 KNOTS DUE TO HIGH EPR ON NR 1 ENG. ALL PARAMETERS WERE LOW. ALL OTHER NR 1 ENG PARAMETERS DID NOT MATCH NR 2 AND NR 3. INSPECTED AND FOUND NR 1 ENG PT'S PROBE PLUGGED. CLEANED OUT PROBE AND INSTALLED NOSE DOME IAW B727 MM 71-10-41. PERFORMED ENG RUN IAW B727 MM 71-00 AND TRIM TABLE 71-00-51 PG 216. SYS OPS CHECK GOOD. NO DEFECTS NOTED. 2L73 4F4 F A3WE E2EA 20030828001252003082800125 2003 8 28 MWEA030310 420030815A34189650041027 CONNECTOR DOUG DC9 DC932 3022066WP COCKPIT DEFECTIVE A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31207ME 47794 STALL INDICATION FAILURE LIGHT CAME ON. REMOVED AND REPLACED FIRST OFFICER'S STICK SHAKER CONNECTOR. 2L72 4F A6WE 20030829000392003082900039NM 2003 8 29 CALA0300492 120030825A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND RT AFT LAV WALL SUPPORT HAT SECTION CORRODED. THE WALL SUPPORT HAT SECTION WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030729000172003072900017NM 2003 7 29 03201451 120030720A242024381 CONTROL UNIT DORNERDO32 DO328300 NM RIGHT MALFUNCTIONED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA27451FJ 3205 DURING DESCENT, THE FLIGHT CREW REPORTED RECEIVING A RIGHT HAND ALTERNATOR FAIL AND THE PRESENCE OF AN ELECTRICAL BURNING SMELL IN THE FRONT OF AIRCRAFT THAT DISPATED UPON LANDING. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE RIGHT HAND ALTENATOR CONTROL UNIT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20030321000782003032100078NM 2003 3 21 2003UALA00219 120030224A5754114W413015 SKIN BOEING777 777222 1385219NM NR 3 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 ROLLER WORN, TRAILING EDGE WEDGE, SLAT NR 3, DELAMINATED. REPAIRED DELAMINATED TRAILING EDGE WEDGE, SLAT NR 3 AND ROLLER. 2L72 4F RTT0001SE 20030730000732003073000073WP 2003 7 30 ABXA030263 120030223A5230 DOOR FRAME DOUG DC8 DC863F 302198FWP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 147. CUT AND REMOVED DOOR FRAME SECTION, FABRICATED AND INSTALLED FRAME SECTION AND SPLICES IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-20D. 2L74 4F 4A25 20030730000902003073000090WP 2003 7 30 ABXA030305 120030618A522059101595 PAN DOUG DC9 DC941 302207NWP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 RIGHT FORWARD EMERGENCY OVERWING EXIT DOOR HAD CRACKED PAN AT AFT SIDE LOWER JAMB SUPPORT FITTING. REPAIRED AREA IAW DC-9 SRM 52-51. 2L72 4F A6WE 20030303000612003030300061NM 2003 3 3 SWAA030394 120030219A3350610478 HOUSING BOEING737 7375H4 138449DNM CABIN DEFECTIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT MID CABIN OVERHEAD. REMOVED AND REPLACED BATTERY PACK HOUSING PER MM. 2L72 4F RTA16WE 20030324000032003032400003WP 2003 3 24 03FDEA00337 120030319A3040SYLZ517671 ANTI-ICE SYSTEM DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE RT WINDSHIELD INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25314FE1379313793 48312 RIGHT WINDSHIELD ANTI/ICE INOPERATIVE LIGHT ILLUMINATED SHORTLY AFTER TAKE OFF. REMOVED AND REPLACED RIGHT WINDSHIELD IAW M.M. 56-11-00-2. REMOVED AND REPLACED WINDSHIELD ANTI/ICE CONTROLLER IAW MM 30-41-01-2. GROUND OPS CHECK NORMAL. 2L73 4F4 F A22WE E23EA 20030418000302003041800030NM 2003 4 18 VNAA0302004 120030208A2612 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FIRE FALSE INDICATIONA VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07472PS 3008 THE CREW RECEIVED A LAV FIRE LIGHT INDICATION AND IT WOULD NOT EXTINGUISH. THERE WAS NO FIRE. MAINTENANCE CONTROL DEFERRED THE LAV FIRE EXTINGUISHING SYSTEM WITH CODE 26-4 C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030327001812003032700181SO 2003 3 27 C2XA03TY012 120030124A3260 CONNECTOR EMB 145 EMB145LR 3260212SO PROX SWITCH LOOSE A C2XAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW2715912 145439 DURING A REPOSITION FLIGHT FROM TYS TO IAH, THE AIRCRAFT HAD AN AIR RETURN FOR A LT LANDING GEAR DISAGREE MESSAGE. MAINTENANCE FOUND A LOOSE CONNECTOR PLUG ON THE LT GEAR PROX SWITCH. RESECURED CANNON PLUG, SWUNG THE GEAR 10 TIMES, OPERATIONAL CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2L72 4T RTT00011AT 20030418000962003041800096WP 2003 4 18 UPS03840198 120030128A53203646772 FITTING DOUG DC8 DC873F 302199FWP RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, CORROSION IN RT FWD UPPER CORNER OF RT MLG WHEEL WELL. REMOVED FITTING PN 3646772, REMOVED CORROSION FROM WEB IAW DC8 SRM 51-1-8, LESS THAN . 002 INCH, W/IN LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW FITTING P/N 3646772, LOCATED DRILL AND INSTALLED FITTING IAW DC8 SRM 51-1-21. REMOVED FLOORBOARD FROM STA 850-890 RBL 40 & FILLET PANEL 292F TO GAIN ACCESS TO REPAIR, INSTALLED FLOORBOARD AND FILLET PANEL IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030417000132003041700013EU 2003 4 17 MALA030119 120030122A3230 SWIVEL SAAB SF340 SF340A 7850100EU DRAG BRACE LEAKING A MALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL15027XJ AFTER TAKEOFF OF FLIGHT 2753, CREW GOT A HYDRAULIC MASTER CAUTION LIGHT AND NOTED HYDRAULIC QUANTITY WAS AT ZERO. EMERGENCY DECLARED, WAS AT 300 PSI. MAIN WAS A ZERO I/B AND O/B WAS AT 300 PSI. MAINTENANCE FOUND RT MAIN LANDING GEAR DRAG BRACK HYDRAULIC SWIVEL LEAKING. REMOVED AND REPLACED, OPS CHECKED. ALL CHECKS GOOD. 2L72 4T RTA52EU 20030418000242003041800024NM 2003 4 18 VNAA0302012 120030214A2820 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE REFUEL PANEL FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07432JS 3045 EN ROUTE, THE CREW RECEIVED A FUEL ASYMMETRY CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE COAX CONNECTOR ON THE REFUEL PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030723000202003072300020CE 2003 7 23 RU3A03011 120030616A3610 SENSE LINE BEECH 300 300BEECH 1152930CE RT BLEED SYS DAMAGED A RU3AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2173 FF8 EN ROUTE AT FL200 RIGHT BLEED AIR FAIL ANNUNCIATOR LIGHT ILLUMINATED. EXECUTED EMERGENCY ROCEDUES AND LANDED AT NEAREST AIRPORT. FBO MAINTENANCE TROUBLESHOT SYSTEM AND FOUND HOLE IN RIGHT BLEED AIR SENSING LINE. SPLICE LINE AND OPS CHECK GOOD. (M) 2L72 4T A24CE 20030723000392003072300039NM 2003 7 23 USAABB030106 120030630A2910BACH8B06RR0554B LINE BOEING757 757225 1384959NM RTMLG WW RUPTURED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19603AU 22198 AFTER TAKEOFF FROM CLT, CREW COULD NOT GET THE LANDING GEAR TO RETRACT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT GEAR TILT ACTUATOR FLEX LINE, WHICH HAD RUPTURED. (M) 2L72 4F RTA2NM 20030422001352003042200135EA 2003 4 22 QXEA0300319 120030304A2710AL00102 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA ZONE 300 INOPERATIVE A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09614QX998 998 10049 SEA ON FLIGHT 2516- ABORTED TAKEOFF DUE TO TAKEOFF ROLL CONFIG/AILERON WARNING AND AURAL WARNING. TAKEOFF CONFIG OKAY. ADVISORY MESSAGE WAS PRESENT. REMOVED AND REPLACED AILERON TRIM ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040225001692004022500169NM 2004 2 25 DL73G031137 120031226A2750275701135 TRANSDUCER BOEING737 7373L9 1384470NM TE FLAPS FAILED A DALAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 SO27232DZ 24220 FLAP LOCKOUT ON SELECTION FROM 5 TO 15 FLAPS. SPLIT FLAP INDICATION, LEFT 5, RIGHT 10. REPLACED LEFT FLAP POSITION TRANSDUCER. 2L72 4F RTA16WE 20030827000532003082700053NM 2003 8 27 03FDEA00993 120030628A261365249201 CONTROL UNIT BOEING727 727200 138407ENM E/E BAY FAULTY A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 SO25481FE 21463 REPEAT WRITEUP. ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. COMPLIED WITH RED TABS AND LIGHT EXTINGUISHED WHEN NR 1 BLEED AIR SWITCH CLOSED AND LEFT, PACK TURNED OFF. REMAINED OFF FOR REST OF FLIGHT. INSPECTED NR 1 STRUT OVHT. DETECTOR SENSOR CONNECTORS NO DAMAGE NOTED, CLEANED CONNECTOR ENDS WITH CONTACT CLEANER. AFTER READING WIRING DIAGRHAM ENCH ENG. STRUT HAS A SEPARATE CONTROL UNIT INSIDE THE FIRE AND OVHT.DET. MODULE REMOVED AND REPLACED THE FIRE AND OVHT. DET. MODULE UNIT IAW MM 26-14-000-0 SYS OPS CK GOOD IAW MM 26-14-00-5. 2L73 4F RTA3WE 20030806001162003080600116SO 2003 8 6 C2XA03SH254 120030803A5311145337302 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030812000112003081200011GL 2003 8 12 HEEA088415 220030720A74219550175400 IGNITER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 ENGINE WOULD NOT START. IGNITER TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U3 U H1NE E1GL 20030904000732003090400073NM 2003 9 4 QXEA200301045 120030830A3610310848802 VALVE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE BLEED AIR SYS FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09364PH 524 AG0069 PDX- ON FLIGHT 2147 AFTER ENGINE START WHEN SELECTING BLEEDS ON, HAD VERY LIGHT SMOKE ON FLIGHT DECK. SMOKE CLEARED OUT IN 2 TO 5 MINUTES. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE P2.5/PD AIR SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030905001472003090500147NE 2003 9 5 DL76L030657 220030715A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 MAKING METAL A DALAO OTHER J WARNING INDICATION CRCRUISE 1 SO27175DN47013 24803 724142 L OIL FILTER CAUTION AND STATUS MESSAGE CAME ON IN FLIGHT WHILE CRUISING AT FL350. REPLACED NR 1 ENGINE. FOUND MCD COVERED WITH BEARING METAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2L72 4F4 FRTA1NM E24NE 20030825001022003082500102NM 2003 8 25 03FDEA01315 120030809A5753ARC0502403 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 SNRM N 741 3A L2 FH WING 2FB FLAP I2 FB HINGE 28 2FC SIDE 29 CORROSION FOUND ON FWD ATTACHMENT HOLE 2FB BORE. 2L73 4F RTA22WE 20030729000612003072900061EA 2003 7 29 QXEA200300851 120030718A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 PDX- FORWARD CARGO BAY CHIMNEY AT DOOR ENRTY HAS A TEAR IN THE WEBBING. REMOVED AND REPLACED FORWARD CARGO BAY CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030825000442003082500044WP 2003 8 25 UPS03841093 120030724A53204641324N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 STATION 1690 LONG. 24L TO FRAME FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. SRM. 51-1-21,53-1-0,AND DWG. 4641324 2L74 4F RT4A25 20030910000872003091000087WP 2003 9 10 DHL2003604644 120030512A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING OUTBOARD FLAP UPPER FWD PLATING HAS AN INTERIM REPAIR, AT STA XF 345.000 - XF 350.000 (MAJOR REPAIR). REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030508, ED-3282. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN SEGMENT AND A SPLICE STRAP IAW EODHL-030508, ED-3282. CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT INTERIOR SURFACE AND THE SPLICE STRAP IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SEGMENT AND SPLICE STRAP ON RT WING OUTBOARD FLAP UPPER PLATING, STA XF 345.000 - XF 350.000 USING NEW FASTENERS IAW EODHL-030508, ED-3282 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001022003091100102CE 2003 9 11 DXTA200300067 120030714A3210 HUB CAP CESSNA560 560XL 2076702CE PWA 545 PW545A NE MLG OUT OF POSITION E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07699QS 5605199 ABORTED TAKE-OFF DUE TO ANTI SKID LIGHT THEN BRAKES FAILED, USED EMERGENCY BRAKE TO STOP AIRCRAFT. - NOTED LEFT WHEEL HUB CAP TRANSDUCER CLIP POSITIONED INCORRECTLY, REPOSITIONED HUB CAP. BLED BRAKES, OPERATIONAL CHECK GOOD. ALL WORK DONE IAW CHAPTER 32-42-00 OF THE CITATION 560XL MM. 2L72 4F4 FRTA22CE E00059EN 20030912001222003091200122NM 2003 9 12 AWXA200300889 120030729A53206558293503 ATTACH ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON CABIN CEILING ATTACH ANGLE AT THE L-2 DOOR CUTOUT BS 987, LBL 25. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT THE L-2 DOOR CUTOUT BS 987, LBL 25; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 65-58293; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 1. 2L72 4F RTA16WE 20030929000652003092900065EU 2003 9 29 AWXA200301015 120030831A5210FE1740011 DAMPER AIRBUS320 A320231 3930325EU PAX DOOR FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW3605523196 67 DURING C-03 CHECK THE L-2 DOOR ASSIST DAMPER CYLINDER FAILED FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR DAMPER CYLINDER IAW AMM SUBTASKS 52-13-14-020-050-0 & 52-13-14-420-051-0. ADJUSTED AND SERVICED IAW SUBTASK 52-13-14-820-050-0 & 52-13-14-200-001; OPERATIONAL CHECK GOOD IAW SUBTASK 52-13-14-210-060-0. VENDOR FUNCTIONAL CHECK OF DAMPER CYLINDER S/N 101 CONFIRMED FAILURE OF UNIT. REAR CUP WAS FOUND RUSTED & PITTED, FRONT CUP WAS FOUND LOW ON FLUID, AND DETERIORATED SEALS WERE FOUND ON THE PERCUSSION AND BOTTLE ASSEMBLY, REPLACED ALL DAMAGED PARTS AND COMPLIED WITH SERVICE BULLETINS FE174-52-1, 2, & 3R1 CHANGING PART NUMBER TO FE174-0011. 2L72 4F RTA28NM 20030930001272003093000127NM 2003 9 30 03FDEA01473 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) O/B PIVOT LUG HOLE CORRODED. 2L73 4F RTA22WE 20031007000542003100700054NE 2003 10 7 ASOA03400 220030826A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT BIRD INGESTION A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SO11855AS 7395 872714 DURING TAKEOFF, AT APPROX 4,000 A BIRD WAS INGESTED INTO THE RIGHT ENGINE AND IT SHUT DOWN. THE CREW COMPLIED WITH QRH PROCEDURES, DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20031007000862003100700086NM 2003 10 7 SWAA031984 120030905A3350BR2013 LENS BOEING737 7372T4 1384492NM EEPLS MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 EEPLS LIGHT AND LENS MISSING AT ROW NR 8. INSTALLED EEPLS LIGHT AND LENS ASSY PER MM. 2L72 4F A16WE 20031008000552003100800055WP 2003 10 8 UPS03841226 120030827A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, STATION 1320 LONGERON 31 RT AND FRAME ARE CORRODED BEYOND LIMITS, REMOVED,FABRICATED AND REPLACED LONGERON SECTION BETWEEN STA. 1230 TO 1320 I.A.W. SRM. 53-4-1 FIG. 43A,AND REMOVED CORRODED AREA ON FRAME,FABRICATED AND INSTALLED FILLER AND DOUBLER I.A.W. SRM. 53-2-0 FIG.2 2L74 4F RT4A25 20030827001702003082700170SO 2003 8 27 C2XA03SH299 120030827A531514522461011 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE RIGHT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 204 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030828000882003082800088NM 2003 8 28 DL757030620 120030707A3350 LIGHT BOEING757 757232 1384965NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27660DL 24422 EMERGENCY LIGHT ABOVE ROW 36 INOPERATIVE, RELAMPED SAME. OPERATIONAL CHECKS OK. 2L72 4F RTA2NM 20030724000602003072400060EU 2003 7 24 AWXA200300715 120030607A5210FE174003 CYLINDER DAMPER AIRBUS320 A320231 3930325EU PAX DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK THE R-1 DOOR ASSIST MECHANISM WAS FOUND OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE R-1 DOOR ASSIST MECHANISM IAW AMM TASK 52-11-14-820-002 AND 52-11-14-501. 2L72 4F RTA28NM 20030801001272003080100127WP 2003 8 1 MWEA030263 120030701A53119911839213 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 FRAME WEB STATION 1463 AT LONGERON 181 IS CRACKED. FABRICATED AND INSTALLED NEW WEB AND DOUBLER. 2L72 4F A6WE 20030801001302003080100130WP 2003 8 1 MWEA030281 120030712A712059124431 YOKE DOUG DC9 DC932 3022066WP RT ENGINE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31203ME 47673 EVIDENCE OF CORROSION AND GALLING INSIDE LOWER HALF OF RIGHT PYLON MOUNT YOKE CUP. REMOVED AND REPLACED RIGHT ENGINE YOKE MOUNT. 2L72 4F A6WE 20030829002112003082900211NM 2003 8 29 USAA030130 120030709A5320 ANGLE BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 PIT - FOUND RIGHT CREASE BEAM INNER CHORD Z-STATION 947.5 TO 986.5 PLUS 8 INCHES, WITH THREE CORRODED AREAS OF CORROSION, 3 INCHES BY 2 INCHES, 2 INCHES BY 2 INCHES, 4 INCHES BY 2 INCHES. REPLACED Z-ANGLE PER SRM 53-60-15. (M) 2L72 4F RTA16WE 20030903002112003090300211EA 2003 9 3 QXEA200300971 120030811A2550 SUPPORT BRACKET CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX- AFT CARGO BAY NET SUPPORT BRACKET ABOVE DOOR HAS CABLE CUTS AT AFT END ADJACENT TO COUNTER BALANCE PULLEY. REPAIRED IAW HORIZON AIR EA R-53-124 AND REO 670-53-61-080. 2L72 4F RTA21EA 20030807000602003080700060SO 2003 8 7 C2XA03IA074 120030803A3260852701 PROXIMITY SENSOR EMB 145 EMB145 3260210SO NLG INOPERATIVE A C2XAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW2715973 145159 FLIGHT 2819, THE CREW NOTED THAT THE AIRCRAFT HAD NO INDICATION FOR NOSE GEAR DOWN. THE APPROACH WAS ABORTED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030813000422003081300042NM 2003 8 13 2003UALA00456 120030529A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29310UA 23671 LT FUSELAGE EXTERNAL SKIN DENTED AT STA 445 BETWEEN STRINGERS 18L & 19L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030813002112003081300211NM 2003 8 13 SWAA031708 120030729A3350311500 LENS BOEING737 7377H4 1384404NM EXIT SIGN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29711HK 27845 OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 1 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20030825001732003082500173WP 2003 8 25 DHL2003873581 120030704A53203750257U1 SPLICE DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 ITEM REF.: N/R 1212.: FWD. CARGO COMPT. SPLICE FITTING 9.000 CRACKED (STA.600.000 - 620.000, L-31L) (MAJOR REPAIR) PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG.21. 2L74 4F4 FRT4A25 E2GL 20030826001712003082600171SO 2003 8 26 SWIA200312131 120030622A3397 WIRE EMB 120 EMB120ER 3260203SO CABIN CHAFED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07189SW 120048 RIGHT SIDE FORWARD EMERGENCY LIGHT OVERWING LIGHT INOP. FOUND WIRE W602-0055-20 CHAFING. REPAIRED WIRE IAW MM 20-21-00 AND REMOVED AND REPLACED FUSE XF0016. LIGHT OPS CHECKED GOOD. 2L72 4T RTA31SO 20030825000072003082500007NM 2003 8 25 UPS03441104 120030718A5312 PRESSURE PANEL BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C NOSE WHEEL WELL COMPARTMENT TUNNEL - AT STA 240 CEILING AREA THE CABIN HORI FLOOR SUPPORT WEB AREA AFT SURFACE CORROSION FOUND AT BL 0. FLOOR SUPT WEB REPAIRED IAW SRM 51-40-02 FIG.1 DUE TO BLENDED DEPTH 0.043 INCH, WIDTH .7500 INCH AND LENGTH 2 INCH EXCEEDS SRM 53-10-01 FIG.1 LIMITATION. 2L74 4F A20WE 20030827001092003082700109NM 2003 8 27 CALA0300470 120030817A5512 SKIN BOEING737 7373T0 1384582NM HORIZ STAB BIRD STRIKE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714346 23584 INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN AND RIB AT STA 86.66 DAMAGED DUE TO A BIRD STRIKE. 2L72 4F RTA16WE 20030911000412003091100041NM 2003 9 11 DHL2003743013 120030717A2612 DETECTOR BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FIRE WARNING MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01743DH 22438 NR 3 DETECTOR CIRCUIT GROUND FAULT LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. INSPECTED NR 3 ENGINE DETECTOR CIRCUIT GROUND - NO FAULTS FOUND AND NO LIGHTS ILLUMINATED. OPS CHECKED GOOD IAW M/M 26-11-0. TRANSFERRED NR 3 GROUND DETECTOR FAULT TO DMI NR 13579 IAW DHL MEL 26-9 CAT. "C" PLACARD INSTALLED. RE: DMI NR 13579 - NR 3 ENGINE GROUND FAULT LIGHT ON. REPOSITION NR 3 ENGINE FIRE LOOP. CHECKED GOOD IAW 26-10-00. CLEARS DMI NR 13579. PLACARD REMOVED. 2L73 4F4 F A3WE E2EA 20030911000792003091100079WP 2003 9 11 DHL2003873509 120030617A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING INBD L/E FORMER CRACKED 0.250 AT STA XFS.660.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911002132003091100213EU 2003 9 11 DHL2003365012 120030805A3260 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU NLG CONTAMINATED A DHLAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01365DH 149 NOSE GEAR DOWN AND LOCK LIGHT ON S/O PANEL DID NOT ILLUMINATE WHEN GEAR EXTENDED. ABNORMAL PROCEDURE COMPLETED. WHEN BELOW 500 FT AGL GPWS "TOO LOW", GEAR WARNING SOUNDED. CLEAN PROXIMITY SENSORS AT NOSE GEAR AND FOUND GREASE ON SENSORS. PERFORMED BITE TEST IAW AMM 32-30-00 NPF. VERIFIED GPWS BOX SECURED. TEST NORMAL PER AMM 34-48-00. 2L72 4F RTA35EU 20030916000012003091600001NE 2003 9 16 MEX2003360 220030813A7310MA20A10011 SHUTOFF VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENGINE FAILED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW23806AM 26273 AIRCRAFT RETURN TO PLATFORM AFTER LEFT ENGINE WAS STARTED. THE LT FUEL SPAR VALVE LIGHT COME ON AND THE LEFT ENGINE SHUTDOWN WITH CODE 282209. DURING REVISION, WAS DETECTED FUEL SHUTOFF VALVE ACTUATOR DAMAGED, THE FUEL SHUTOFF VALVE ACTUATOR WAS REPLACED IAW MM, ALL TESTS CORRECT. DURING OVERNIGHT SERVICE THE FUEL SHUTOFF VALVE ACTUATOR WAS TESTED IAW MM AGAIN, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20030930000392003093000039NM 2003 9 30 2003UALA00656 120030831A3350 BULB BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29219UA 30551 EMERGENCY LIGHT ON SIDE OF SEAT 2E AND 3F INOPERATIVE. RELAMPED. 2L72 4F4 FRTT0001SE E46NE 20030926001182003092600118NM 2003 9 26 AT0300025 120030902A33508039251 CHARGER BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15953AT 55015 EMERGENCY LIGHT ABOVE SEAT ROW 16 INOPERATIVE. REPLACED EMERGENCY LIGHT CHARGER (POWER SUPPLY). 2L72 4F TRA6WE 20030908002472003090800247EA 2003 9 8 SWIA200312354 120030823A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A SWIAO OTHER K FLUID LOSS CRCRUISE 1 NM07407SW4292 4292 7034 NR 2 HYD SYSTEM LOST QUANTITY WITH PRESSURE AT 33,000 FT. NR 2 ENGINE DRIVEN PUMP RAN DRY FOR 33 MINS. REMOVED AND REPLACED NR 2 ENGINE HYD PUMP AND PRESSURE STEEL LINE AND PRESSURE RETURN LINE AND SERVICED NR 2 HYD SYSTEM. OPS CHECKS AND LEAK CHECKS GOOD IAW 29-13-00. 2L72 4F RTA21EA 20030909002832003090900283NM 2003 9 9 QXEA200300953 120030806A2820 O-RING DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 NM09362PH 518 PSC- ON FLIGHT 2092 FUEL LEAK ON NR 2 ENGINE AHEAD OF FUEL DOOR. REMOVED AND REPLACED O-RINGS ON MASTER REFUEL/DEFUEL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031007001052003100700105NM 2003 10 7 SWAA032003 120030908A5320BAC1503 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND BULKHEAD TO KEEL BEAM STIFFENERS CRACKED (2 EA) BS 727, WL 151 BOTH LBL 6 AND RBL 6. REMOVED AND REPLACED STIFFENERS PER SRM. 2L72 4F RTA16WE 20031014001122003101400112NM 2003 10 14 SWAA032155 120030924A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014002122003101400212CE 2003 10 14 BAQA089548 120031004A2752505212223 ACTUATOR BEECH 100 100BEECH 1152916CE TE FLAP WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G B144 ACTUATOR WORN. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20031020003012003102000301NM 2003 10 20 2003UALA00727 120030929A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29176UA 24383 EEL LIGHT INOP AT ROW 32HJK. RELAMPED, CHECKS GOOD. 2L74 4F4 FRTA20WE E24NE 20031028001752003102800175EU 2003 10 28 USAASA03094 120030818A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19716UW 1055 PHL - THE RIGHT WING EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING TEST. MAINTENANCE REPLACED THE RIGHT SIDE EMERGENCY LIGHT BATTERY. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20031118001182003111800118NM 2003 11 18 AWXA200301194 120030912A5321146N5750152 FLOOR PANEL BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-09 CHECK CABIN FLOOR PANEL T-3 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 146N5750, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1. 2L72 4F4 FRTA2NM A12EU 20040115001002004011500100NM 2004 1 15 03FDEA02339 120031230A5320AJC705515 BEAM DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 AFT FUSELAGE RT MOST BEAM AT STA X = -60 / Y = 2007 TOP REPAIR DOUBLER FOUND CRACK. DOUBLER DOUBLER REMOVED AND REPAIR AS PER SRM 53-00-01 VOL. I AND SRM 51-33-01 VOL. I. 2L73 4F RTA22WE 20031112000962003111200096 2003 11 12 BAQA090582 420031008A343523081057 STARTER GEN UROCOPEC135 EC135P1 8680990EU ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH565 0179 ENGINE WOULD NOT START. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE STARTER GEN. 1G72 3U O H88EU 20031015000562003101500056 2003 10 15 USAASA03092 420030817A2565C37103101 RELEASE CABLE AIRBUSA319 A319112 3930323EU ESCAPE SLIDE WRONG PART A USAAK NONE O OTHER ININSP/MAINT 1 EA19760US 1354 THE FORWARD RIGHT EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLDIE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20030909000362003090900036SO 2003 9 9 C2XA03SH318 120030906A531514530633003 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030909001422003090900142SO 2003 9 9 SWIA200312369 120030826A2797 WIRE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TRIM SWITCH LOOSE A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07270YV 120270 CAPTAIN'S ELECTRIC TRIM SWITCH UP POSITION INOP. FOUND TERMINAL SOLDER JOINT LOOSE ON TRIM SWITCH. RESOLDERED WIRE TO TERMINAL. OPS CHECK OK. 2L72 4T4 TRTA31SO E20NE 20040212000862004021200086EU 2004 2 12 WRNA200300014 120031210A361032022001 CHECK VALVE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 ENGINE FAULTY A WRNAJA DUMP FUEL UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DEDESCENT 1 SO05502TA 075 455289 NR 2 ENGINE HAD SEVERE VIBRATION ON DESCENT FROM 29,000 FT. ENGINE PARAMETERS WERE ALL OK EXCEPT N1 NR1 85 PERCENT, NR 2 60 PERCENT VIBRATION STOPPED WHEN THROTTLE BOUGHT BACK BELOW 53.5 PERCENT. FUEL DUMPED. NORMAL LANDING. TROUBLESHOT TO FAULTY IP CHECK VALVE. REPLACED VALVE IAW MM 36-11-13. ENGINE RUN IAW MM 72-00-00. NO VIBRATION NOTED. PRECAUTIONARY BORESCOPE ACCOMPLISHED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20031030000392003103000039NM 2003 10 30 UPS03441297 120030906A5712 RIB BOEING747 747121 1384871NM NR 7 V/C FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 7 V/C FLAP O/B LINKAGE O/B RIB NR 1, NR 4 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1, NR 4 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS. 2L74 4F A20WE 20040212001252004021200125WP 2004 2 12 ABXA030473 120031212A32505616554 CYLINDER DOUG DC8 DC863F 302198FWP RT BOGIE TRIM LEAKING A ABXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23816AX 46093 HYDRAULIC QUANTITY GRADUALLY DECREASED DOWN TO 7 GALLONS. LOSS OF HYDRAULICS EMERGENCY PROCEDURE FOLLOWED. MAINTENANCE FOUND RT BOGIE TRIM CYLINDER LEAKING. REPLACED RT BOGIE TRIM CYLINDER IAW MM 32-33-01-2. 2L74 4F 4A25 20031117001002003111700100WP 2003 11 17 MWEA030406 120031007A5310591008529 DOOR FRAME DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE GALLEY BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 FORWARD GALLEY DOOR IS CATCHING ON DOOR JAMB, JAMB IS BENT AT TWELVE O'CLOCK POSITION. STRAIGHTENED EDGE, FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20040109000462004010900046WP 2004 1 9 GTIA031014 120031117A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND RT COCKPIT FLOOR PANEL HAS CRACK, HAT CHANNEL BENT, DELAMINATED AT RUB STRIP, CORRODED, PLASTIC BARRIER BROKEN SEAL LOOSE AND TORN. FABRICATED NEW PANEL. (M) 2L72 4F A6WE 20040113002012004011300201SO 2004 1 13 C2XA03CL186 120031112A335078241 INVERTER EMB 135 EMB135LR 3260305SO CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2728529 145512 DURING ROUTINE MAINTENANCE THE LEFT SIDE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031121000582003112100058 2003 11 21 55959 420031107A34181143800515 COMPUTER BEECH 1900 1900D 1154162CE STALL WARNING MALFUNCTIONED A AMWAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 CE071472Y UE142 STALL WARNING SYS WON`T GIVE WARNING AT 84-90 KNOTS. DURING TAKEOFF ROLL STALL WARNING HORN SOUNDED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED STALL WARNING COMP. P/N 1143800515, S/N 285. 2L72 4T RTA24CE 20040311000452004031100045NM 2004 3 11 ASAA0310116 120030307A7110652377414 FRAME BOEING737 737298C 1384490NM NR 1 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 179 CHAFED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20031215001552003121500155WP 2003 12 15 AALA20031186 120031029A33508039001 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21961TW 53611 DFW - DURING OVERNIGHT MAINTENANCE, FOUND OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERY FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031217001572003121700157NM 2003 12 17 P5CA0301006 120031211A3610 VALVE BOEING747 747200 1384847NM NR 1 ENGINE STUCK A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23524UP 21446 662348 NR 1 ENG HUNG START AT 28-29 PERCENT N2. FOUND PYLON VALVE STUCK OPEN, CYCLED SAME ENG START NORMAL. 2L74 4F RTA20WE 20031219001432003121900143NM 2003 12 19 03FDEA02126 120031128A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. AREA REPAIR CARRIED OUT AS PER EA 1-5750-73351, WINGS, TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20031222000122003122200012NM 2003 12 22 F3LA200300159 120031204A5420 WEB BOEING737 73736E 138443ANM NR 2 PYLON CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED NR 2 ENGINE PYLON LOWER AFT STRUT FAIRING WEB CRACKED AND PULLED FASTENERS AT STIFFENER. REPLACED WEB ON NR 2 ENGINE PYLON LOWER AFT STRUT FAIRING PER SRM 51-40-02 AND EA B3-54R-10217. 2L72 4F RTA16WE 20031106002062003110600206NE 2003 11 6 GTIA030081 220030219A7230780830 INLET GUIDE VANE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 ENGINE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 MCO - FOUND LEFT NR 2 ENGINE 10 O'CLOCK POSITION FACING FRONT OF ENGINE CRACK ON IVG NEAR BASE APPROXIMATELY 2 INCHES IN LENGTH UNABLE TO STOP DRILL. REMOVED AND REPLACED THE NR 2 ENGINE IGV. (M) 2L72 4F4 F A6WE E9NE 20031105000212003110500021EU 2003 11 5 MALA030462 120031006A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, FOUND FRAME 18 HAS CORROSION IN SEVERAL SPOTS FROM 17 INCHES RIGHT OF CENTER TO 40 INCHES RIGHT OF CENTER. MX REPAIRED FRAME IAW EOA53138. REFER TO LOG PAGE 189911 FOR DETAIL. A/C RELEASE DATE 10/12/03. 2H74 4F RTA49EU 20031106000372003110600037NM 2003 11 6 03FDEA01811 120031021A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LEFT WING OUTBOARD FLAP OUTBOARD FWD HINGE INBOARD ACTUATOR LUG BORE FOUND CORRODED. 2L73 4F RTA22WE 20031009000442003100900044SO 2003 10 9 SIMA200321603 120030730A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 DURING SCHEDULED MAINTENANCE CHECK, THE EXIT LIGHT AT ROWS 12C WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 5 INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040112002242004011200224NM 2004 1 12 SWA2004F00003 120031031A5753654792328 SPAR BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE RT MIDFLAP CRACKED D SWAAO OTHER O OTHER NRNOT REPORTED 1 NM01379SW 1892 26584 CRACKED AT O/B AFT FLAP TRACK ATTACH HOLES. 2L72 4F4 FRTA16WE E2GL 20040112002022004011200202NM 2004 1 12 2003UALA00960 120031215A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29171UA 24322 STATION 100 LWR CHORD CRACKED JUST I/B OF STR 47L. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER MM 53-10-89. 2L74 4F4 FRTA20WE E24NE 20040311000592004031100059NM 2004 3 11 ASAA0310104 120030306A53106546564127 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SHEAR TIE AT BS 986, STRINGER 23R CORRODED. REMOVED AND REPLACED SHEAF TIE PER SRM. (M) 2L72 4F RTA16WE 20031212000282003121200028NM 2003 12 12 SWAA032424 120031103A33501000679 LIGHT BOEING737 7372T4 1384492NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 EMERGENCY EXIT LIGHT ABOVE R2 DOOR LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20031215000252003121500025NM 2003 12 15 SWAA032524 120031116A335065C25093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20031217001162003121700116NM 2003 12 17 2003UALA00854 120031112A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29362UA 24455 FRAME 188 LEFT BOTTOM IS DAMAGED BY AN OVER LENGTH SCREW INSTALLED IN A CLAMP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20031218000612003121800061NM 2003 12 18 03FDEA01999 120031128A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 CTR CARGO LEFT TUNNEL BETWEEN STA 5-113 TO STA 1541 NR 37 LONGERON SPLICE FOUND CRACK. REMOVED CRACKED LONGERON SPLICE AS PER SRM 51-31-01, VOL. II AND FABRICATED NEW SPLICE AS PER DRAWING A5A7114. INSTALLED NEW SPLICE AT CENTER CARGO LT TUNNEL BETWEEN STA 5-113 TO STA 1541, NR 37 LONGERON AS PER DRAWING N5A6774. 2L73 4F RTA22WE 20031218001402003121800140NM 2003 12 18 QXEA200301500 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 3 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF RAILS FROM 5 TO 8 INCHES AFT OF X510. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-3644. 2H72 4T RTA13NM 20031218001472003121800147SO 2003 12 18 C2XA03CL196 120031202A2120 ODOR EMB 145 EMB145 3260210SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2722971 145149 THE CREW REPORTED ON APPROACH AFTER STARTING THE APU HAD A BURNING ODOR IN THE COCKPIT AND CABIN. ALSO REPORTED THE BURNING ODOR AT THE GATE WITH THE APU OFF. MAINTENANCE INSPECTED THE CABIN AND COCKPIT LIGHTING SYSTEM, THE RADIO EQUIPMENT FANS AND AVIONICS BAY AREA. ALSO INSPECTED THE CABIN/COCKPIT COOLING FANS WITH NO DEFECTS FOUND. THE APU WAS OPERATIONAL CHECKED AS WAS THE COOLING/HEATING SYSTEM. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20031219001102003121900110NM 2003 12 19 03FDEA02054 120031205A5320 WEB BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25198FE 19154 ON WEB AT BS 600 STR 26R. REMOVED CORROSION ON WEB & FOUND STR 26R OUT OF LIMITS. REPAIRED STR 26R AT BS 600 & WEB PER SRM 53-10-3 & 51-20-1. 2L73 4F RTA3WE 20031219001502003121900150NM 2003 12 19 03FDEA02136 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORRODED. 2L73 4F RTA22WE 20031222001162003122200116EU 2003 12 22 SIMA200332403 120031114A335066902 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A SIMAO OTHER L NO TEST NRNOT REPORTED 1 SW21376AE 340B376 EMERGENCY ROW FLOOR LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY CABIN ESCAPE LIGHT ASSEMBLY. (M) 2L72 4T RTA52EU 20031224000192003122400019WP 2003 12 24 GTIA030744 120031005A716059306451 ACOUSTIC LINER DOUG DC9 DC983 3022083WP NR 2 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 ON WALK AROUND FOUND NR 2 ENGINE INLET ACOUSTIC LINING DAMAGED 15 BY 39 SECTION MISSING NO DAMAGE TO HONEYCOMB STRUCTURE. REMOVED AND REPLACED NR 2 ENGINE NOSE COWL AS REQUIRED. NO FURTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20031229001452003122900145NM 2003 12 29 UPS03241661 120031216A2610 SWITCH BOEING727 72725C 138400HNM FIRE DETECTOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 NR 1 ENGINE FIRE SWITCH WILL NOT ILLUMINATE DURING TEST. PERFORMED ADJUST / TEST PER 26-11-02 PG 501, SYS OPS CHECK AT THIS TIME. 2L73 4F A3WE 20040105001482004010500148WP 2004 1 5 ABXA030478 120031216A335060030451 POWER SUPPLY DOUG DC9 DC941 302207NWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23979AX722 47492 EMERGENCY LIGHTS INOPERATIVE, LOW CHARGE. REPLACED EMERGENCY LIGHT BATTERY PACK POWER SUPPLY IAW DC9 MM. OPS CHECK GOOD. 2L72 4F A6WE 20040106000522004010600052EA 2004 1 6 COMA0360553 120031215A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO01979CA16389 7159 RIGHT FORWARD SIDE OF FS 621 BULKHEAD IS CHAFED AT FOUR LOCATIONS. REMOVED FASTENERS, BLENDED OUT DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION, ALODINED AND INSTALLED FASTENERS IAW WVAC EO 601R-53-4466. 2L72 4F RTA21EA 20031231000922003123100092WP 2003 12 31 GTIA030930 120031110A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSLEAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND FLOORBOARD CENTER FS 617 CORNER DELAMINATED. REPAIRED DELAMINATION. (M) 2L72 4F RTA6WE 20040114001812004011400181SO 2004 1 14 MASA200300424 120031025A2560P2070009120 MOUNT EMB 145 EMB145LR 3260212SO RROYCEDART DART* NE FLASHLIGHT CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07849MJ 145534 ASH NR 2828. FWD EMERGENCY FLASHLIGHT MOUNT BROKEN. MECHANIC REPLACED MOUNT. OP CHECKS GOOD. 2L72 4T4 TRTT00011AT 20040115001562004011500156 2004 1 15 XNOA1171 420031209A3417 INDICATOR AIRBUS300 A300B4203 3930306EU COCKPIT INOPERATIVE A XN0AC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL23474AS 219 ABORTED T/O DUE TO NO AIR SPEED INDICATION ON F/O'S ASI. LOW RANGE LEAK TEST IS GOOD ON F/O'S ASI SYSTEM. OPS CK GOOD IAW A-300 AMM 34-11-10. (CLOSED) 2L72 4F RTA35EU 20040120000182004012000018EU 2004 1 20 S9HA265YA 120031201A6420 SPAR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED D S9HAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 WP19352NT2046 2553 PILOT HEARD USUAL NOISE WHILE FLEXING TAIL ROTOR BLADES DURING PREFLIGHT. MAINTENANCE REPLACED THE TAIL ROTOR WITH A SERVICEABLE TAIL ROTOR FROM A ANOTHER AIRCRAFT. UPON TEAR DOWN INSPECTION A CRACK IN THE SPAR 10MM WIDE BY 150MM IN LENGTH ON THE LEADING OF THE SPAR. PILOT REPORTED THAT NO UNUSUAL NOISES WERE HEARD DURING PREFLIGHT ON THE PREVIOUS DAY AND NO UNUSUAL VIBRATIONS FELT IN THE PEDALS OR AIRFRAME DURING FLIGHT THE PREVIOUS DAY. TAIL ROTOR SENT TO THE MANUFACTURE FOR EVALUATION. 1G71 3U3 UNCH9EU E19EU 20031202000482003120200048NM 2003 12 2 USAABB03186 120031011A335020121 CHARGER BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 FOUND FRONT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER. (M) 2L72 4F RTA1NM 20031204000182003120400018WP 2003 12 4 GTIA030874 120031020A5320 FITTING DOUG DC9 DC982 3022082WP CARGO DOOR FRAMECRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 AFT PIT DOOR UPPER STOP, FORWARD FITTING CRACKED. REMOVED DAMAGED FITTING. REPLACED FITTING. (M) 2L72 4F A6WE 20031208001072003120800107NM 2003 12 8 AWXA200301305 120031001A5315654681138 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CHORD BS 986, RBL 4 TO RBL 46. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED T-CHORD BS 986 FROM LBL 52 TO RBL 52; FABRICATED A NEW REPLACEMENT T-CHORD; INSTALLED REPAIR PART IAW AWA ER 03-5300-03289-T5B. 2L72 4F RTA16WE 20031208000732003120800073NM 2003 12 8 AWXA200301294 120031013A5315145N5416 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1320 AND BS 1330, RBL 2. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM BETWEEN BS 1235 AND BS 1340, RBL 2; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM AND REPAIR SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 6. 2L72 4F RTA2NM 20031210001542003121000154WP 2003 12 10 AALA20031359 120031202A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21584AA 53247 PHX AFT CABIN DROP CEILING PANELS AND AFT ACCESSORY CEILING AND SLIDE ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. REPLACED B5-27 AND B5-28 BATTERY PACKS IN AFT RIGHT CEILING AT STATIONS 1322R AND 1338R. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20030924000102003092400010EU 2003 9 24 197022503 120030225A30605341312053 SENSOR PILATSPC12 PC1245 7090551EU OAT FAILED E S4WAO OTHER J WARNING INDICATION CRCRUISE 1 WP07613NA3688 197 PROP HEAT CAWS ILLUMINATED IN FLIGHT. 1L71 3T RTA78EU 20031231000722003123100072EU 2003 12 31 ASOA03571 120031107A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 FLT 4194 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS REMAINED ON WITH SWITCH IN ANY POSITION. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT IN 73WL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20031229001712003122900171NM 2003 12 29 C1HA200382011 120031215A5543 SKIN BOEING727 7272S7 138407ZNM RUDDER TAB CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15682CA 22019 LOWER RUDDER TAB UPPER LEFT AND RIGHT SIDE IS DEBONDED AND CRACKED. 2L73 4F A3WE 20031229001352003122900135SO 2003 12 29 MASA200300469 120031130A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07834MJ 145340 EMERGENCY LIGHT AT EXIT INOP. MX RELAMPED LIGHT, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20031010000042003101000004EA 2003 10 10 QXEA200301143 120030917A2810D98C09602 PRESSURE SENSOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09607QX506 505 10024 SMF- DURING PREFLIGHT FUEL WAS DRIPPING FROM CENTER OF FUSELAGE WITH BOOST PUMPS SELECTED ON, FUEL WAS LEAKING AT A MUCH FASTER RATE. REMOVED AND REPLACED NR 2 ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20031014000112003101400011 2003 10 14 BAQA089448 420030926A2312069102525 TRANSCEIVER BOLKMS117 BK117A3 5626015EU COCKPIT MALFUNCTIONED B BAQAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA0339181177 7003 UNIT WILL NOT POWER UP AT ALL.COMPLETELY INOPERATIVE. ALSO, IT HAS A BURNED ODOR. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20031231001022003123100102NM 2003 12 31 TSAA0353047 120030219A53136545815 STRINGER BOEING737 737282C 13844AUNM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13826AL 23051 CUTOUT AND REMOVED DAMAGED PART OF STRINGER. FABRICATED REPAIR PARTS PER TABLE 1 FROM 2024-T4 AND 7075-T6 CLAD. ALODINED AND PRIMED REPAIR PART. INSTALLED THE REPAIR PART IAW SRM 53-10-3, FIGURE 1. (M) 2L72 4F RTA16WE 20031124000342003112400034NM 2003 11 24 AWXA200301424 120031113A21337110033 OUTFLOW VALVE BOEING737 7373G7 1384595NM ZONE 280 FAILED A AWXABA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 WP28309AW153223950 24711 EN ROUTE FROM SMF TO PHX AT FL 320 CABIN PRESSURE WARNING SOUNDED, FLIGHT CREW VERIFIED LOSS OF PRESSURE AND INITIATED EMERGENCY DESCENT TO FL 100, OXYGEN MASKS WERE DEPLOYED AND AUTO CONTROL WAS SWITCHED TO STANDBY. MAINTENANCE REMOVED AND REPLACED THE AFT OUTFLOW VALVE IAW T/C R6A21001, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF CABIN PRESSURE CONTROLLER S/N 8711489 COULD NOT CONFIRM REASON FOR REMOVAL, UNIT TESTED GOOD IN ALL MODES. VENDORS FUNCTIONAL TEST OF OUTFLOW VALVE S/N 177964 WAS NO FAULT FOUND. THE ONLY DISCREPANCY FOUND WAS INDICATOR LAMP FAILS TO OPERATE NORMALLY, ADJUSTED INDICATOR SWITCH IAW CMM 21-33-00. 2L72 4F RTA16WE 20031204000082003120400008WP 2003 12 4 GTIA030886 120031023A3397 SPLICE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND LEFT AFT STAIRWELL COMPARTMENT AND 4 EACH EMERGENCY LIGHTS INOPERATIVE. FOUND A BAD SPLICE. REPAIRED SPLICE. (M) 2L72 4F A6WE 20040122001032004012200103EA 2004 1 22 ASOA03587 120031118A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA AIR CON SYS ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11844AS 7317 FLT 4441 - DURING CLIMB-OUT FROM PFN-ATL, THE CREW NOTICED A STRONG OIL ODOR FROM THE AIR CONDITIONING SYSTEM. THE ODOR WAS ALSO NOTICED DURING THE FLIGHT AT LOW AND IDLE POWER SETTINGS. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHING AND ALSO THE LEFT AND RIGHT COALESCER BAGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031204001482003120400148WP 2003 12 4 03FDEA01763 120031016A5753 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP LT TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 LT INBOARD FLAP INBOARD TRACK SUPPORT BRACKETS CORROSION. COMPLIED WITH EA 8-5750-7, WINGS - LT INBOARD FLAP INBOARD TRACK SUPPORT BRACKETS CORROSION REPAIRED. 2L73 4F A22WE 20031204001622003120400162EU 2003 12 4 MALA030464 120030926A5320 ANGLE BAC 146 AVRO146RJ85A1500097EU VERTICAL STAB CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, LEFT HAND VERTICAL STAB TO FUSELAGE CLOSING ANGLE CRACKED 1 INCH LENGTH. MAINTENANCE REPAIRED IAW EO A55013. 2H74 4F RTA49EU 20031204001672003120400167CE 2003 12 4 AMWA61 120031015A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0723YV UE26 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE BY THE FOWARD AND AFT STRINGER INTERSECTION. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20031204001572003120400157NM 2003 12 4 QXEA200301291 120031016A5210 TRACK DHAV DHC8 DHC8202 2809007NM ZONE 800 DIRTY A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09354PH 498 ON FLIGHT 2017 MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. CLEANED DEBRIS FROM TRACK. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031210000672003121000067NM 2003 12 10 03FDEA01972 120031121A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT OUTBOARD FLAP FOUND INBOARD HINGE PIVOT BOLT HOLE NR 3 I/B FLANGE SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031209000182003120900018EU 2003 12 9 YENA200333 120031029A3350116502 LAMP AIRBUS320 A320232 3930326EU EMERGENCY LIGHT BURNED OUT A YENAK NONE O OTHER ININSP/MAINT 1 EA15507JB 1240 EMERGENCY EXIT SIGN LIGHTS INOPERATIVE AT RT OVERWING EXIT AND AFT LAV AISLE SIGN. REMOVED AND REPLACED EMERGENCY EXIT SIGN LAMPS AT RT OVERWING AND AFT LAV AISLE. 2L72 4F RTA28NM 20040127002392004012700239WP 2004 1 27 ASAA0380665 120031015A53113924829507 FRAME DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND FRAME 522 ABOVE LONGERON 6L GOUGED AND CRACKED. REPAIRED PER SRM. (M) 2L72 4F A6WE 20031014000882003101400088NM 2003 10 14 SWAA032214 120031003A29106544548 LINE BOEING737 7373H4 1384600NM HYD SYSTEM LEAKING A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW29324SW 23414 LOST 'A' SYSTEM HYD, NR 1 ENG HYD LOW PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED LT ELEVATOR PCU HYD PRESS LINE AND 'A' SYSTEM CASE DRAIN FILTER PER MM. 2L72 4F RTA16WE 20031020001252003102000125SO 2003 10 20 RAIA00309251 120030928A36108166011 BLEED VALVE EMB 145 EMB145 3260210SO BLEED AIR SYS STUCK A RAIAA UNSCHED LANDING JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03806HK9742 145112 5316- STL- HIGH STAGE BLEED VALVE FAIL MESSAGE AND REPORTED SMOKE IN CABIN. MAINTENANCE REMOVED AND REPLACED HIGH STAGE VALVE. VALVE STUCK OPEN CAUSED SMOKE IN CABIN. 2L72 4F RTT00011AT 20030919000782003091900078NM 2003 9 19 03FDEA01259 120030811A2613 OVERHEAT LOOP BOEING727 7272S2F 1384O81NM AFT AIRSTAIRS INTERMITTENT A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25208FE 22930 APPROX ONE HOUR INTO FLIGHT 28 DURING CRUISE NO TURBULENCE 29 EPR 27S 231 1.59 232 1.83 233 1.56_N2_231 86 25_232 86 25_ 233 85 25 LOWER AFT BODY OVERHEAT LIGHT FLICKERING. CHECKLIST ACCOMPLISHED-LT WENT OUT THEN BEGAN TO FLICKER AGAIN. LANDED GTF. REMOVED AND REPLACED R2 FH OVERHEAT DETECTOR LOOP IN AFT AIRSTAIR AREA. LOWER AFT BODY OVERHEAT SYS OPS CHECK NORMAL ON GROUND AT THIS STATION. REF B 727 MM 26-14--2. 2L73 4F A3WE 20040130000142004013000014NM 2004 1 30 SWAA032807 120031224A3350 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 FWD EPLS LIGHT INOP AND WIRES EXPOSED. RELAMPED BULB AND RESECURED WIRE COVER PER MM. 2L72 4F RTA16WE 20040204000622004020400062NM 2004 2 4 DHL2003782012 120031017A3350MISC062 BATTERY BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01769AT 21998 ON PRE-FLIGHT FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. SWITCH IN OFF POSITION DURING PRE-FLIGHT. TROUBLESHOT SYSTEM FOUND PORTABLE EMERGENCY EXIT LIGHTS WITH LOW VOLTAGE .7 VDC / CHARGED BATTERIES / TESTED BATTERIES AFTER CHARGE / FOUND FULLY CHARGED TO 2.6 VDC / TESTED SYSTEM IAW M/M 33-50-101 ITEM (N) SYSTEM OPS CHECKED GOOD AT THIS TIME. AS PRECAUTION DUE TO PREVIOUS WRITE UP REF. LOG PAGE NR 361302 ITEM 1P EMERGENCY EXIT LIGHTS BATTERIES WILL BE REPLACED. REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS FOR FORWARD ENTRY DOOR AND COCKPIT DOOR QUANTITY 4 - P/N: MISC062 IAW DHL B-727 M/M 33-50-101. OPS CHECKED SATISFACTORY. 2L73 4F4 F A3WE E2EA 20040211000012004021100001WP 2004 2 11 AMTA200301497 120031217A3350582217 BATTERY PACK LKHEED1011 10113853 5265020WP EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 RIGHT A/C FORWARD BY R1 DOOR EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER PACK BATTERY PER AMM 33-51-00. OPS CHECK NORMAL PER 33-51-00. (M) 2L73 4F A23WE 20040212001292004021200129EU 2004 2 12 F3LA200300177 120031211A2750 FILTER AIRBUSA318 A318111 3940019EU VALVE BLOCK MALFUNCTIONED A F3LAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM03802FR 1991 BLOCK TURNBACK. FLIGHT CREW REPORTED F/CTL SLAT SYS 1 FAULT. COMPLETED CONTINUITY CHECK BETWEEN SFCC NR 1 AND SLAT FFPU IAW ASM 27-81-00 SCH06 AND CHECKED GOOD. REPLACED FILTER IAW TSM ON FLAP/SLAT VALVE BLOCK NR 1 IAW MM 27-84-53-400-03. 2L72 4F RT 20040212001762004021200176NM 2004 2 12 AWXA200301587 120031207A5310655287897 CREASE BEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF CREASE BEAM (INNER CHORD) BETWEEN BS 952 AND BS 985, LBL 53 AND LBL 56. MAINTENANCE REMOVED AND REPLACED INNER CHORD FROM BS 952 TO BS 985, LBL 53 TO LBL 56 IAW B737-300 SRM 51-40-02, FIG. 12, PG. 3-4, 6-10, & 16. 2L72 4F RTA16WE 20040212001342004021200134NM 2004 2 12 DHL2003742516 120031120A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, FUSELAGE EXTERNAL SKIN BS 630 STR 23R WITH A DENT. CUT DAMAGE AREA DIM 1 X 1 .125 X .75 INCH IAW B-727 SRM 53-30-3. FABRICATED DOUBLER REPAIR DIM 11.5625 X 8.5 INCH USING 2024 T3 .080 PO 90013 IAW B-727 SRM 53-30-3 FIG 1. ALODINED AND PRIMED IAW B-727 51-10-2. INSTALLED DOUBLER REPAIR AT FUSELAGE EXTERNAL SKIN BS 630 STR 23R IAW B-727 SRM 53-30-3 FIG 1. 2L73 4F A3WE 20040217000982004021700098NM 2004 2 17 HNAA0300089 120031228A6123 AUTOFEATHER SYS DHAV DHC8 DHC8201 2809001NM MALFUNCTIONED A HNAAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 EA07985HA 479 AUTOFEATHER FAILS TO ARM ON TAKEOFF. MECHANIC TRIMS ENGINES AND AUTO FEATHER ARMS AT 83-85 TQ, SHUT DOWN ENGINE POWER, DOWN UP AND NEXT ENGINE RUN, AUTO FEATHER REVERTS TO ARMING AT 100-103 TQ. AUTOFEATHER FAILED TO ARM ON TAKE OFF ROLL AGAIN. MECHANIC PREFORMED LRU CODE VERIFICATION, ECU SETUP AND CENTER TRIM ECU, PERFORMED ENGINE TRIM AND AUTO FEATHER ARMS AS REQUIRED. 2H72 4T RTA13NM 20040301000732004030100073WP 2004 3 1 AAL2004F00001 120030928A5313 LONGERON DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21484AA 49677 CRACK ON LONGERON 46 AT STA 700. CRACKED IN SECTION NEXT TO LOWER ATTACH FASTENER. SPLICED IN NEW SECTION OF LONGERON FROM STA 180 TO STA 235. 2L72 4F4 F A6WE E2EA 20040304000262004030400026SO 2004 3 4 MYN2004F00000 220031213A741410357586 GEAR CIRRUSSR SR22 2130001GL CONT O550 IO550* SO LT MAGNETO BROKEN B MYNRA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL11622C 577 0368 AIRCRAFT MADE LOUD POPPING NOISE ON TAKE OFF, LANDED SAFELY, FOUND DISTRIBUTOR GEAR IN LEFT MAG HAD 7 BROKEN OFF TEETH. AIRCRAFT DELIVERED NEW 11/26/02. 1L71 3O3 ONTA00009CHE3SO 20031217000712003121700071WP 2003 12 17 DHL2003807525 120031010A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 MAIN CARGO COMPT NR 2 TRACK LUGS WORN AT STA 1396.000. TRIMMED OUT WORN AREA IAW SRM 53-2-3 PG 17, FIG 6D. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW PLUG WITH NEW FASTENERS ON MAIN CARGO COMPT NR 2 TRACK AT STA 1396.000 IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040416000042004041600004NM 2004 4 16 ASAA0240ZZZ 120030323A531065C31240 DOOR FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND AFT CARGO DOOR CUT OUT FORWARD FRAME CLOSE OUT PANEL HAS CORROSION AT BS 794, RBL 38 AND WL 161. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040128001222004012800122SO 2004 1 28 SWIA200312714 120031226A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07233SW1948 1948 120307 IN CRUISE, NOTICED ELEVATOR TRIM SNAPBACK WITH AUTOPILOT ENGAGED, FL 230 AND -31 DEGREES C. DISCONNECTED AUTOPILOT, MANUALLY ATTEMPTED TO MOVE TRIM, UNABLE TO MOVE TRIM. REGAINED TRIM CONTROL AT 4000 FT AND + 6 DEGREES. REPLACED RIGHT AND LEFT ELEVATOR TRIM TAB ACTUATORS IAW EMB 120 MM 27-32-02. OPS CHECK GOOD. P/N: 5299-1, S/N ON: 633, S/N OFF: 728, S/N ON: 938, S/N OFF: 535. 2L72 4T RTA31SO 20040130000222004013000022NM 2004 1 30 SWAA032817 120031225A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED PMC CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 765, JUST ABOVE STR 24R. REPAIRED DAMAGED AREA PER SRM. 2L72 4F RTA16WE 20040128001702004012800170NM 2004 1 28 AWXA200400005 120031204A57206569846150 PLATE BOEING737 73733A 1384673NM LT FLAP WELL CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK FOUND INSPECTION COVER IN LT FLAP WELL CHAFING ON LT OUTBOARD FORE FLAP JUST OUTBOARD OF NR 3 FLAP TRACK WS 205 LT. MAINTENANCE REMOVED CHAFED INSPECTION PLATE LT FLAP WELL WS 205 LT; FABRICATED A NEW REPLACEMENT PLATE; INSTALLED REPAIR PART IAW AWA ER 03-5750-03352-TB3. 2L72 4F RTA16WE 20040130000462004013000046NM 2004 1 30 VNAA0312009 120031217A3230 PILOT VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07425JS 3037 THE CREW REPORTED RECEIVING A EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND THE PILOT VALVE STUCK. MAINTENANCE THEN CLEANED AND LUBED THE PILOT VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040204001902004020400190NM 2004 2 4 03FDEA01869 120031030A2820AAL728933 LINE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 DURING THE PRESSURE TEST OF TAIL TANK FUEL SHROUD DRAIN SYSTEM FOUND TAIL TANK TRANSFER FUEL SHROUD TUBING LOCATED AT STA. Y 1791 LT SIDEWALL OF CENTER CARGO WITH A CRACK LINE MEASURED APPROX. 1 INCH IN LENGTH. COMPLIED WITH EA 1-2822-71762 FUEL SYSTEM - FUEL SHROUD AND DRAIN - CRACK REPAIR ON TUBE FOR TAIL TANK. 2L73 4F4 FRTA22WE E13NE 20040210001222004021000122WP 2004 2 10 IXXA0300074O 120031113A8000 PLATE DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C1 13802EU NR 4 ENGINE LOOSE A IXXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW11825BX844691427 45978 693220 JUST AFTER LEVEL OFF AT 33.0 NR 4 ENGINE OIL QUANTITY DECREASED RAPIDLY WITH LOW OIL PRESSURE (13PSI) AND NR 4 OIL PRESS LIGHT ILLUMINATED UP FRONT. ENGINE WAS SHUT DOWN AT 0340Z, WTIH OIL QUANTITY AT 3 QUARTS- OIL PRESSURE WENT TO ZERO AT 0349 AND REMAINED THERE FOR REST OF FLIGHT. MAINTENANCE FOUND COVER PLATE OF STARTER LOOSE. THEY CORRECTED LEAK SOURCE AT STARTER, COMPLIED WITH ATI ENGINE RUN HANDBOOK AND ERH PROCEDURES. NO LEAKS NOTED ON ENGINE RUN. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20031211001212003121100121WP 2003 12 11 AALA20031329 120031125A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21419AA 49331 DEN AFT RIGHT LAV OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR AFT RIGHT LAV OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031215001422003121500142WP 2003 12 15 AALA20031117 120031005A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 BNA - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE MID CEILING LOCATION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040415000742004041500074WP 2004 4 15 ASAA0380743 120031114A57305930577501 SKIN DOUG DC9 DC983 3022083WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE BETWEEN STATION XCW 121.688 AND XCW 104.500 CRACKED. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20040518000802004051800080NM 2004 5 18 EIA2004010 120030129A335069B4601014 MODULE BOEING747 747132 1384882NM EMERGENCY LIGHT MALFUNCTIONED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WITH SW ON OR OFF. R&R LITE MODULE PER MM 33-51-04 2L74 4F A20WE 20040913001432004091300143NM 2004 9 13 0704010 120031003A52456548685101101 DOOR BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE A/C BAY DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 LT AC BAY DOOR DELAMINATED AT BS 634. 2L72 4F4 F A16WE E2EA 20060801001552006080100155WP 2006 8 1 IXXA060476S 120030208A5712 RIB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE RIB AT STATION 341 CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20030820000042003082000004WP 2003 8 20 03FDEA01305 120030814A5753 HINGE DOUG DC10 DC1030 3023501WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 COMPLY WITH EA8-5750-60625. WINGS- RT WING I2FB FLAP 2FB FLAP HINGE SUPPORT LOWER 2FB SUPPORT - CORROSION INSPECTION AND REPAIR. CLOSING ACTION ON 82 F11 2F3 ON 2FR JOB ACCOMPLISHED ON N2FR S00033 2C REWORK LOWER 2FB HOLE ON EA 8-5740-70995A 2C S00043 LOWER I2FB HOLE ON EA 8-5740-70995A 28 LOWER I2 FB BUSHING REPLACED PER CMM 57-44-07 ON EA 8-5750-60625. REINSTALLATION ON EA 8-5740-70995A IAW. 2L73 4F A22WE 20030403000652003040300065EU 2003 4 3 ASOA03058 120030213A33502275941249 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11635AS 372 DURING A HANGAR CHECK IN MCN, THE FLOOR EMERGENCY LIGHT AT SEATS 14 A-B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A FLOOR EMERGENCY LIGHT GROUND WIRE AT SEATS 14 A-B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030819002412003081900241NM 2003 8 19 2003UALA00527 120030630A2131763810 CONTROLLER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EE BAY FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29920UA 25387 AIRCRAFT RETURNED TO THE FIELD WHEN IT WAS UNABLE TO PRESSURIZE AFTER TAKEOFF. THE CABIN PRESSURE CONTROLLER FAILED. REPLACED PRESSURE CONTROLLER, TESTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20030821002322003082100232 2003 8 21 252TR0007 420030731A2230 COMPUTER BOEING737 737228 13844AGNM AUTOTHRUST SYS MALFUNCTIONED A PIDAK NONE O OTHER CLCLIMB 1 SO05252TR 23001 ON CLIMB ONLY AUTO THROTTLES WILL NOT MATCH THE PDC CLIMB EPR. THE HIGHER YOU CLIMB THE MORE THE AUTO THROTTLES PULL THE POWER BACK. AUTO THROTTLES WORK IN ALL OTHER PHASES OF FLIGHT. PLACED AUTO THROTTLE SYSTEM ON MEL 22-4. 8/7/2003: REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101. 2L72 4F RTA16WE 20030403001252003040300125GL 2003 4 3 DL733030162 220030218A7310S332A0041 HOSE BOEING737 737347 1384647NM CFMINTCFM56 CFM563B1US GL NR 2 ENGINE LEAKING A DALAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO27304WA 23345 72071 ON ARRIVAL DEN FOUND FUEL LEAKING FROM RT ENGINE. INSP FOUND MAIN FUEL LINE FROM PYLON TO ENG FUEL PUMP LEAKING AT SWEDGED END / PYLON SIDE. REPLACED SAME. 2L72 4F4 FRTA16WE E2GL 20030331001472003033100147NM 2003 3 31 DHL2003742001 120030110A3297 MODULE BOEING727 727225 1384077NM MLG MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01742DH 21290 WITH LANDING GEAR HANDLE IN UP POSITION, WARNING HORN SOUNDS CONTINUOUSLY AND ALL THREE RED GEAR UNSAFE LIGHTS ARE ILLUMINATED. RESEATED LANDING GEAR ELECTRONIC MODULE; PERFORMED OPERATIONAL TEST OF LANDING GEAR ELECTRONIC MODULE IAW B-727 M/M 32-09-121, CYCLE LANDING GEAR HANDLE SEVERAL TIMES, SYSTEM CHECKED NORMAL. 2L73 4F A3WE 20030410001392003041000139 2003 4 10 SWAA030693 420030326A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD CABIN DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20030410001922003041000192NM 2003 4 10 DL76G030122 120030201A3350 LIGHT BOEING767 767332 1382001NM EXTERIOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO271602 29694 THREE EACH EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED, ALL CHECK OK. 2L72 4F RTA1NM 20030410000722003041000072NM 2003 4 10 SWAA030649 120030320A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 4R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030408001052003040800105SW 2003 4 8 20034 120030407A3222OAS545115 STRUT SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP NLG DISCHARGED E STZAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 AL03505FS AC591B NOSE LANDING GEAR TRANSITION ANNUNCIATOR WOULD NOT EXTINQUISE AFTER LANDING GEAR RETRACTION. FOUND NOSE LANDING GEAR STRUT TO BE IN NEED OF SERVICE, (WHEN ON JACKS, THE NOSE STUT WOULD NOT FULLY EXTEND AND ALIGN ON THE CENTERING CAM) SERVICED THE STRUT WITH FLUID AND NITROGEN IAW MM, AND THE OPERATIONAL CHECKS WERE SATISFACTORY. 2L72 4T3 TRTA8SW E2WE 20030416001052003041600105NM 2003 4 16 SWAA030784 120030407A5315BAC1509 FLOORBEAM BOEING737 7373G7 1384595NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 767 PLUS 3, LBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030417000802003041700080NE 2003 4 17 XNOA01102 220030131A7200 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 MALFUNCTIONED A XN0AC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL23473AS 203 ON TAKEOFF, POWER APPLICATION NR 2 ENG N2 INDICATED LOW. TAKEOFF REJECTED (NO HIGH ENERGY STOP). AS PER MAINTENANCE CONTROL INLET & EXHAUST INSPECTED. NO DEFECT NOTED. ACCOMPLISHED POWER RUN TO 70 PERCENT. FOUND FUEL FLOW N2 & EGT IN PARAMETERS. DEFERRED PER MEL 77-11-01 SECTION 2. DMI 3107 ASSIGNED. 2L72 4F4 FRTA35EU E23EA 20030424001112003042400111NM 2003 4 24 QXEA0300404 120030323A3350526011 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 200 INTERMITTENT A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09358PH19021 506 COCKPIT EMERGENCY LIGHT SWITCH ILLUMINATES INTERMITTANTLY WITH NO SWITCH ACTION. REMOVED AND REPLACED REMOTE ELECTRONICS UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030423001072003042300107EU 2003 4 23 U30A200300005 120030209A2611 SMOKE DETECTOR AIRBUS320 A320212 3930322EU LAVATORY FAULTY A U30AO OTHER N FALSE WARNING CRCRUISE 1 EA17265AV 427 DURING CRUISE ON FLT 304 BWI-PUJ, ECAM MESSAGE APPEARED "SMOKE-LAVATORY DET FAULT". ON GROUND IN PUJ TESTED SYSTEM & FOUND FWD LAV DETECTOR FAULT. DEFERRED PER MEL 26-17-01 (LAV "A"). UPON RETURN TO BWI, T/S SYSTEM PER TASK 26-17-00-810-801 WITH NO FAULT CONFIRMATION. SYSTEM OPERATIONALLY TESTED OK. A/C RETURNED TO SERVICE. 2L72 4F RTA28NM 20030429000722003042900072NM 2003 4 29 P5CA0300820 120030410A5347BAC13201566 SEAT TRACK BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 SEAT TRACK STA 360 TO STA 420 LBL 91.045 LEVEL 1 CORROSION. REMOVED AND REPLACED TRACK PER SRM 53-10-05 FIG 1. 2L74 4F A20WE 20030429001112003042900111EU 2003 4 29 RAIA00304099 120030402A3060 BLADE JETAIRJETSTMJETSTM4101 1500501EU PROP DE ICE SYS PEELING A RAIAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 CE03562HK 41078 RIC- CREW REPORTED NR 1 ENGINE VIBRATION. MAINTENANCE FOUND NR 1 PROP DE-ICE MAT PEELING OFF. RESECURED MAT, OPS CK OK. 2L72 4T RTA41NM 20030430000552003043000055NM 2003 4 30 USAA030029 120030321A5530 SUPPORT FITTING BOEING737 737301 1384611NM VERTICAL STAB WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US42512 23558 PIT - FOUND TERMINAL SUPPORT FITTING HAS TWO WORN BOLTS, VERTICAL STABILIZER AFT TERMINAL SUPPORT FITTING BOLT HOLES. REWORKED WORN HOLES PER EA 94263A, THIS IS AN INTERIM REPAIR. (M) 2L72 4F RTA16WE 20030430002262003043000226NM 2003 4 30 AWXA200300438 120030415A534569489027 PLATE BOEING737 73733A 1384673NM GIRT BAR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - EES - DURING C-17 CHECK CORROSION WAS FOUND ON TOP SURFACE OF GIRT FITTING ATTACH BRACKET (PLATE) AT L-2 DOOR FWD FITTING. MAINTENANCE REMOVED AND REPLACED GIRT FITTING ATTACH BRACKET AT L-2 DOOR PER T/C C1D25018. 2L72 4F RTA16WE 20030502000162003050200016WP 2003 5 2 AMTA200300401 120030327A33505165744 CHARGER LKHEED1011 10113853 5265020WP EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 L1 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER IAW MM 33-51-00. OPS CHECK GOOD. (M) 2L73 4F A23WE 20030501001702003050100170NM 2003 5 1 ASAA0310075 120030304A53206517684581 INTERCOSTAL BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND INTERCOSTAL AT BS 294, STRINGER 7L CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20030502001462003050200146NM 2003 5 2 SWAA030834 120030414A33506042221 LIGHT BOEING737 7373H4 1384600NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT AT FLOOR LEVEL INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AND BATTERY PACK. 2L72 4F RTA16WE 20030502002162003050200216EU 2003 5 2 DHL2003364009 120030425A2612 CONNECTOR AIRBUS300 A300B4203 3930306EU FIRE LOOP LOOSE A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01364DH 141 ENGINE NR 2 LOOP A-LIGHT ILLUMINATING INTERMITTENTLY. ENGINE LOOP ABNORMAL COMPLETED. LOOP-B TESTED NORMALLY. ON ENGINE 2 LOOP-A, FOUND CONNECTOR LOOSE BY PYLON AREA. CLEANED AND RE-SECURED CONNECTOR. LOOP-A TESTED NORMAL AS PER A300 M/M 26-12-12. 2L72 4F RTA35EU 20030505002712003050500271EU 2003 5 5 148571 120030422A2497 WIRE SAAB SF340 SF340A 7850100EU BUSS TERMINAL LOOSE A UHLAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL17146SD 146 ON TAXI OUT FOR FLIGHT 4553 PIT-FWA, EXPERIENCED LEFT AVIONICS BUS FAILURE. RESET, CAME ON THEN BACK OFF WHEN TRANSMITTING. PIT MAINTENANCE FOUND A LOOSE WIRE ON AVIONICS BUS TERMINAL SWITCH AND TIGHTENED THE TERMINAL. OPS CHECK GOOD IAW SAAB 340 AMM 24-00-00. THE FLIGHT WAS THEN MADE WITHOUT EVENT. 2L72 4T RTA52EU 20030502002292003050200229EU 2003 5 2 AWXA200300391 120030405A5315D5347217220290 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292 FROM AFT SIDE OF FR 66 TO AFT SIDE OF FR 67. MAINTENANCE REMOVED CORROSION ON UPPER SURFACE OF FLOORBEAM Y-1292 AT FR 66 TO FR 67 AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED DAMAGED FLOORBEAM; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7, 39-40, FIG 18 AND SRM 51-49-00 PG 24. 2L72 4F RTA28NM 20030505000952003050500095NM 2003 5 5 PCA0300833 120030411A5311 FRAME BOEING747 747249F 1384849NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEVEL 1 CORROSION BS 220 S42R 545F FRAME WEB. REPAIRED PER SRM 51-40-02. 2L74 4F A20WE 20030506000242003050600024NM 2003 5 6 03FDEA00529 120030418A5414 SKIN BOEING727 727200 138407ENM NR 3 NACELLE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE UPPER NACELLE EXTERIOR SKIN HAS GOUGE NEXT TO NR 1 LATCH. REPAIRED NR 3 ENGINE NACELLE IAW BOEING 727-200 SRM 54-30-03. 2L73 4F RTA3WE 20030514000542003051400054NM 2003 5 14 SWAA030977 120030430A5523REP4M6 BEARING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED C4 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER OHM. 2L72 4F RTA16WE 20030513002392003051300239EA 2003 5 13 ASOA03175 120030420A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING A C-CHECK IN MCN, THE STRINGER UNDER THE WATER TANK AT FS 589 AND FS 620 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE STRINGER UNDER THE WATER TANK AT FS 589 AND FS 620 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030515001382003051500138NM 2003 5 15 AWXA200300482 120030429A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 LCQ - MAJOR REPAIR - DURING C-17 CHECK A CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 207, LBL 11. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 207, LBL 11; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG 265-272. 2L72 4F RTA16WE 20030602000652003060200065EU 2003 6 2 CA030424004 120030421A212025W783016011 DUCT ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE7313A 01518WP RAM AIR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 1000 HR INSPECT, AFT BAGGAGE COMPARTMENT INTERIOR WAS REMOVED, ALLOWING INSPECTION ACCESS TO THE RAM AIR DUCT. THIS PLASTIC DUCT IS LOCATED ON THE RIGHT HAND SIDE TUCKED TIGHTLY AGAI NST THE FUSELAGE SKIN AT STA 350. DURING INSPECTION, A 10 INCH CIRCULAR CRACK WAS FOUND IN THE DUCT ADJACENT TO THE FUSELAGE SKIN AT APPROX. STRINGER 6R (COUNTING DOWN FROM UPPER STRINGER). THE NATURE OF THIS CRACK ALLOWED THE DUCT TO OPEN UP WHEN INTERNAL PRESSURE WAS APPLIED. THIS CRACK WAS ONLY EVIDENT BY FEEL, OR USING A FLASHLIGHT AND MIRROR.THE DUCT IS USED TO CLEAR THE FUSELAGE INTERIOR INTHE EVENT OF IN-FLIGHT FIRE/SMOKE. REPLACEMENT OF THE DUCT WAS REQUIRED. 2L72 4F4 FRTA16NM E6WE 20030520001122003052000112NM 2003 5 20 AALA20030445 120030411A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21362AA 24043 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 9H INOPERATIVE. REPLACED EMERGENCY LIGHT CONNECTOR AT SEAT 9H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030609000782003060900078EA 2003 6 9 QXEA0300630 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS469, 3 INCHES ABOVE STRINGER 14R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030522000472003052200047WP 2003 5 22 GTIA030309 120030421A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 CABIN STA 203, RBL 5, LBL 19 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED FLOOR SUPPORT. 2L72 4F4 F A6WE E2EA 20030926001012003092600101CE 2003 9 26 255032 120030902A5220 HANDLE BEECH 1900 1900D 1154162CE EMERGENCY EXIT OUT OF POSITION A NSVAO OTHER O OTHER NRNOT REPORTED 1 EA27149CJ UE49 EMERGENCY EXIT DOOR OVER SEAT 6A OUTSIDE HANDLE NOT FLUSH WITH DOOR SKIN. OUTSIDE HANDLE IS RECESSED INTO DOOR WHEN CLOSED. REMOVED DOOR FROM OUTSIDE AND REINSTALLED DOOR. IAW MM 52-20-00 HANDLE IS FLUSH. 2L72 4T RTA24CE 20030815000852003081500085SW 2003 8 15 HEEA088484 120030708A3212206030104023 FITTING BELL 206 206L3 1182108SW CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 FITTING ASSY HAS EXCESSIVE WEAR ON INSIDE WHERE EAR FROM CROSSTUBE PAD RUBS. SCRAPPED. 1G71 3U H2SW 20030819000702003081900070EA 2003 8 19 COMA0370023 120030807A5270 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA PAX DOOR FALSE INDICATIONA COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01369CA 10079 FLIGHT 5717 AVIONICS DOOR CAUTION MESSAGE DURING T/O. COULD NOT DUPLICATE. INSPECTED DOOR AND WARNING SYSTEM, NO FAULTS FOUND. 2L72 4F RTA21EA 20030819001092003081900109WP 2003 8 19 UPS03840915 120030616A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, LEFT WING CENTER L/E UPPER RIBS ARE CRACKED AT XS 497.491 AND XS484.895. STOP DRILLED CRACKS. NDT VERIFIED CRACKS. STOPDRILL, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20030819001382003081900138NM 2003 8 19 CALA0300360 120030625A5230 SKIN BOEING737 737824 13844BZNM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726226 28935 MAINTENANCE DISCOVERED A DENT IN THE FORWARD CARGO DOOR OUTER SKIN. THE DENT WAS CUT OUT. FINAL CUTOUT DIMENSIONS WERE 2 X 6.5 INCH. A REPAIR WAS INSTALLED IAW ECRA 5230-01726. 2L72 4F RTA16WE 20030819000592003081900059NE 2003 8 19 0301219860 220030629A72307036024 FUEL CONTROL DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE MALFUNCTIONED A NWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL01769NC 47757 707924 DURING TAKEOFF ROLL, FLIGHT CREW OBSERVED A FLOCK OF BIRDS PASS CLOSE TO THE AIRCRAFT AND THEN HEARD A POSSIBLE ENGINE COMPRESSOR STALL. FLIGHT CREW ABORTED TKAEOFF AT 118 KNOTS. MAINTENANCE INSPECTED BOTH ENGINES FOR EVIDENCE OF A BIRD STRIKE, NONE FOUND. DURING ENGINE RUN-UP, NR 1 EXPERIENCED A COMPRESSOR STALL. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL CONTROL. 2L72 4F4 FRTA6WE E2EA 20030820001952003082000195NM 2003 8 20 03FDEA01264 120030721A5543 TAB BOEING727 727100 1384036NM ZONE 300 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25103FE 19199 LOWER RUDDER TAB 2FH SIDE IS DELAMINATED 13 22 ABOVE PUSH ROD ATTACH FITTING. 2L73 4F RTA3WE 20030331000872003033100087SO 2003 3 31 C2XA03SH064 120030329A531014521721005 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE CENTER BUTT STRAP BETWEEN FRAMES 14 AND 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 53-20-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030401001252003040100125WP 2003 4 1 DHL2003804517 120030117A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 434.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030820000962003082000096WP 2003 8 20 UPS03840984 120030718A5610 WINDOW DOUG DC8 DC871F 302199DWP COCKPIT STUCK A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01702UP 45902 UNABLE TO OPEN CAPTAIN`S SLIDING WINDOW. RIGGED UPLOCK BAR OF CAPT SLIDING WINDOW 56-10-03. 2L74 4F RT4A25 20030404001312003040400131NM 2003 4 4 DL767030284 120030327A5754114T411121 WEDGE BOEING767 767232 1385132NM L/E SLAT DEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27104DA 22216 LEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14. 2L72 4F RTA1NM 20030414000592003041400059SW 2003 4 14 HEEA085855 120030327A2841412375001105 INDICATOR BELL 412 412 1182202SW FUEL QTY DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 FUEL INDICATOR HAS ONE LED SEGMENT OUT. 1G72 4U H4SW 20030416000832003041600083NM 2003 4 16 DHL2003780006 120030412A2612 DETECTION SYS BOEING727 727223 1384074NM WW FIRE DETECT WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01780DH 22006 WHEEL WELL FIRE TEST FUNCTION INOPERATIVE. DEFERRED IAW 727 MEL 26-8 SP 26-8 REQUIRED DMI 12549 PLACARD INSTALLED. WORKING DMI 12549, WHEEL WELL FIRE TEST INOPERATIVE. TESTED WHEEL WELL FIRE DETECTORS, OPS CHECKED GOOD. THIS CLEARS DMI 12549, A/C SAFE FOR FLIGHT. 2L73 4F A3WE 20030416004082003041600408 2003 4 16 SWIA200311702 420030114A34177858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AIR DATA MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07413SW4591 3273 7102 'R AOA HEAT' MESSAGE ON TAKEOFF ON EFD NR 1. RETURNED TO SLC. REPLACED RIGHT AIR DATA CONTROLLER. OPS CHECK GOOD IAW 30-31-15. 2L72 4F RTA21EA 20030424001022003042400102NE 2003 4 24 XNOA01110 220030326A7200 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 MALFUNCTIONED A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23473AS 203 ENGINE 1 N1 114 EGT 410 DEGREE C N2 47 PERCENT FF 2300. ACTED LIKE A HUNG START AT 50 SEC. WE REJECTED TAKE OFF. PERFORMED ENG RUN. ALL PARAMETERS NORMAL IAW A300 MM 72-00. INSPECTED NR 1 ENG. NO DEFECTS NOTED. 2L72 4F4 FRTA35EU E23EA 20030429000862003042900086 2003 4 29 AWXA200300363 420030328A256565659733 FITTING BOEING737 7373S3 1384711NM GIRT BAR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 LCQ - EES - DURING C-18 CHECK CORROSION WAS FOUND ON THE L-1 DOOR AFT GIRT BAR ATTACH FITTING BS 344. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR AFT GIRT BAR LOCK AND ATTACH FITTINGS. PART NAME; LOCK, MFG; BOEING, P/N; 65-65972-3. 2L72 4F RTA16WE 20030428001432003042800143NM 2003 4 28 DHL2003741524 120030320A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS PILLOWING FWD BS 420 AT STR 20R. STRIPPED PAINT ON AFFECTED AREA IAW B-727 MM 51-20-01. REMOVED FASTENERS PREVIOUS REPAIR IAW B-727 SRM 51-30-2 AND FOUND CORROSION ON REPAIR OUT OF LIMITS IAW B-727 SRM 51-30-1 FIG 1 WITHIN CORROSION NOTED ON SKIN AT 2 EACH AREAS. CUT OUT DAMAGED AREAS DIM 3.75 X 2.875 INCH AND 2.875 INCH IAW B-727 SRM 53-30-3 FIG 4. FABRICATED DOUBLER FROM 2024 T-3 0.50 PO 9912380 DIM 22.5 INCH X 10.5 INCH AND 2 EACH FILLERS FROM 2024 T-3 0.40 PO 9912380 DIM 3.75 X 2.875 INCH AND 2.75 INCH X 2875 INCH IAW B-727 SRM 53-30-2 FIG 1 AND 53-30-3 FIG 4. PARTS ALODINED AND PRIMED IAW B-727 SRM 51-10-2. 2L73 4F RTA3WE 20030430001032003043000103EU 2003 4 30 0311833002 120030428A33506047051 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27330UE 41098 DURING OVERNIGHT MAINTENANCE, MAINTENANCE PEROSNNEL DISCOVERED THE FOWARD SECTION OF THE EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PEROSONNEL REPLACED THE #1 EMERGENCY BATTERY POWER SUPPLY AND PERFORMED AN OPERATIONAL CHECK THAT WAS SATISFACTORY. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4T RTA41NM 20030501000982003050100098SW 2003 5 1 2003F00243 120030205A792031080811 LINE FRCHLDSA227 SA227DC 3377521SW LT ENGINE OIL CRACKED A BSAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM051119K DC830B MWH - FLT 2563 - LEFT OIL PRESSURE LIGHT CAME ON, OIL PRESSURE GAGE READ 0. PULLED STOP AND FEATHER AS ENGINE STARTED TO LOSE TORQUE. CREW LANDED WITH NO FURTHTER INCIDENT. OIL LEAK IN PROP GOVERNOR AREA. REPLACED LINE, CHECKED LINE POSITION FOR ALL LINES. GOURND RUNS AND TEST FLIGHT GOOD. (M) 2L72 4T RTA18SW 20030502000912003050200091NM 2003 5 2 AWXA200300381 120030414A5330654577578 SKIN BOEING737 7373G7 1384595NM FUSELAGE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C-17 CHECK A 6 INCH CREASE WAS FOUND IN FUSELAGE SKIN AFTER REMOVING EXISTING DOUBLER AT BS 837, STR 25 RT. MAINTENANCE CUT OUT UPPER AND LOWER SKIN TO REMOVE CREASE AT BS 837, STR 25 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH FILLERS, A DOUBLER, AND A TRIPLER. INSTALLED REPAIR PARTS IAW AWA ER 03-5331-03101-TB1. 2L72 4F RTA16WE 20030501001772003050100177NM 2003 5 1 ASAA0310087 120030305A52476550904585 DOOR FRAME BOEING737 737298C 1384490NM APU CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DUIRNG D-CHECK, FOUND APU DOOR FRAME AT BS 1150, BUTTOCK LINE 0 CRACKED. REMOVED AND REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20030506002222003050600222WP 2003 5 6 ASAA0380206 120030304A5321995791821 FLOOR PANEL DOUG DC9 DC982 3022082WP FS BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS BROKEN END AT FS 924-1004. BONDED DAMAGED AREA WITH FIBERGLASS CLOTH AND EPON 828 RESIN PER SRM 51-70-3. (M) 2L72 4F A6WE 20030507000622003050700062EU 2003 5 7 CA030324010 220030324A7230 BOLT GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU ENGINE FAILED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 CA (CAN) LP OGV S BOLT FAILED DURING GROUND RUN. THE DAMAGED WAS CONTAINED WITHIN THE ENG. ENG SUFFERED FROM HIGH VIBRATION AND THEN A BOROSCOPE WAS PERFORMED AND THE LP COMPRESSOR ROTOR WAS FOUND DAMAGED. ENG STRIP CONFIRMED THAT ONE OFF OGV BOLT WAS MISSING. MISSING BOLT FOUND TRAPPED BEHIND ANOTHER OGV MOUNTING BOLT. IMPACT DAMAGE FOUND BEHIND REAR ROTOR SPOOL AND ALL HP COMPRESSOR STAGES 1 TO 12 FOUND WITH IMPACT DAMAGED. ROLLS ROYCE MOD 5270 CORRECT THAT PROBLEM BY INTRODUCING NEW SECURING BOLTS AND NUTS. TAKE NOTE THAT ENG 11355 HAD ALREADY MOD 5270 EMBODIED FROM NEW MANUFACTURE. RRC STANDARD BUILT IS TO MOD 5270 AND RRC TECH INSTRUCT STI 625/1 REQUIRES THAT ONLY NEW BOLTS AND NUTS BE INSTALLED. 2L72 4F4 FRTA12EA E2EU 20030507002092003050700209NM 2003 5 7 CH1A200395029 120030410A5315 FLOORBEAM BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON CABIN FLOORBEAM AT LBL 45 & LBL 55 AT BS 1075 2L73 4F A3WE 20030630000112003063000011NM 2003 6 30 DHL2003747512 120030513A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING "C" CHECK, N/R 53655, CABIN INTERIOR AT BS 560 DENT AND CRACK BTW. ST. 16R-17R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREAS DIMENSIONS 1 X 1 INCH IAW B-727 SRM 51-40-3 FIG. 1. FABRICATED ANGLE REPAIR USING 7075-T6 .063 P.O. 9912475 DIMENSIONS 8 X 6 INCHES IAW B-727 SRM 51-40-3 FIG. 1. ALODINED AND PRIMED ALL REPAIR PARTS I.A.W. B-727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B-727 SRM 51-40-3 FIG. 1. 2L73 4F A3WE 20030508001282003050800128NM 2003 5 8 UPS03440623 120030413A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C M/D - BS 1020, S3R FRAME TIE CLIP FOUND CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030507001792003050700179CE 2003 5 7 CGO2003F00006 120030327A30101283840545 CONTACTOR BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE HORIZ STAB DEICEFAILED B CGORO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL03740TA RK123 INVESTIGATED PILOT COMPLAINT OF FAILED HORIZONTAL STABILIZER DEICE SYSTEM, FAIL INDICATION. REQUIRED REPLACEMENT OF HORIZONTAL STAB. DEICE SYSTEM MOSFET CONTACTORS K251, K252, K253, K254 TO RECTIFY AND OBTAIN SUCCESSFUL OPERATIONAL TEST. FAILED UNITS SHOWED VARIOUS INTERNAL FAULTS. PN 1283840545 UNITS (MFG PN 114192) HAVE BEEN SUPERSEDED BY PN 128-384054-7 (MFG PN 11419-3); RELIABILITY MAY BE IMPROVED OVER THE -5 UNITS. MOSFET CONTACTORS ARE FOUND TO FREQUENTLY BE THE SOURCE OF FAILED HORIZONTAL STABILIZER DEICE SYSTEM FAILURES. PART TT SINCE NEW/ REPAIRED UNKNOWN. AIRCRAFT TT 3336.1 HOURS/ 2693 CYCLES. 2H72 4F4 FRTA16SW E25EA 20030514001912003051400191WP 2003 5 14 03FDEA00705 120030509A2910 LINE DOUG DC10 DC1010 3022110WP HYD SYSTEM DAMAGED A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO2510060 46970 HYD SYS 3 ELEV OFF LIGHT & NR 3 HYD SYS QTY LOSS, EN ROUTE. ACCOMPLISHED RED TABS AND LANDED ATL. MANUFACTURED HYDRAULIC LINE AND ACCOMPLISHED REPAIR PER M/M 20-10-01-02, PRESSURIZED NUMBER THREE HYDRAULIC SYSTEM AND LEAK CHECKED GOOD. COMPLIED WITH EA NR 8-2912-71222 PART 1. NOTE ITEM GENERATED DUE TO FAILED HYD LINE IN NR 3 SYSTEM REPAIRED AS NOTED ABOVE. 2L73 4F A22WE 20030528001072003052800107SW 2003 5 28 HEEA086615 120030521A5260212075418107 ACTUATOR BELL 412 412 1182202SW STEP FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 STEP ACTUATOR WILL NOT RETRACT. 1G72 4U H4SW 20030605001392003060500139WP 2003 6 5 TN8A200300001 120030505A57205142056 ATTACH ANGLE DOUG DC3 R4D8Z 3021476WP WING CORRODED E TN8AK NONE O OTHER ININSP/MAINT 1 AL0331TN 13709 17175 WHILE CHANGING A WING INSPECTION OF UNDER SURFACE OF WING ATTATCH REVEILED CORROSION REQUIREMENT REPLACEMENT OF ATTATCH ANGLE AND ASSOCIATED WING SKIN. 2L72 4R 6A2 20030515001432003051500143EU 2003 5 15 AWXA200300528 120030504A3397ABS0374A24 WIRE HARNESS AIRBUS320 A320231 3930325EU SEAT ROW 13 SHORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 13 LT READS OPEN. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHT WIRING AT SEAT ROW 13 LT IAW ESPM 20-48-14, PG 12-13, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030514001352003051400135NM 2003 5 14 SWAA031021 120030507A531465621257 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C3 CHECK, FOUND KEELBEAM CORRODED AT BS 500D + 10 LT. REPAIRED KEELBEAM PER SWA EA. 2L72 4F RTA16WE 20030609001922003060900192NM 2003 6 9 CA030520003 120030516A2797 WIRE BOEING737 7372Q9 138448MNM PWA JT8 JT8D9A 52048NE NR 2 SLAT BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CA (CAN) FIVE WIRES DAMAGED FROM ARCING, AT WIRE CLAMP LOCATED OUTBOARD OF NR 2 SLAT OUTBOARD ATTACH ARM AT LT WING STATION 480. NO EVIDENCE OF RUBBING OR CHAFING.WIRE BUNDLE CLAMPS FOUND TO BE IN COMPLIANCE WI TH AD CF-84-08R2. SUSPECT BRITTLE WIRING DUE AGE OF AIRCRAFT. WIRING REPAIRED.TIME 57911.22 CYCLES 55034. 2L72 4F4 F A16WE E2EA 20030523000822003052300082EA 2003 5 23 QXEA0300553 120030503A5753 VANE CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 CKB - LEFT INBOARD FLAP VANE HAS THREE MINOR CHAFES ON LEADING EDGE. REPAIRED IAW WVAC EO 601R-57-3975. 2L72 4F RTA21EA 20030617001022003061700102GL 2003 6 17 ERAA087093 220030519A7320252466715H GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL ENGINE STIFF E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01292EH11791 562 GOVERNOR HARD TO OPERATE. HAS DROOPING, STIFF THROTTLE. REPAIRED AND TESTED IAW MFG OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20030618001192003061800119SW 2003 6 18 HEEA087501 120030612A6510PHI40702 SHAFT BELL 407 407 1182206SW BLOWER ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 BLOWER ASSY BEARING ROUGH. REPLACED. 1G71 3U O H2SW 20030528000352003052800035SW 2003 5 28 ERAA086445 120030425A6510212040600005 HANGER ASSY BELL 412 412 1182202SW T/R DRIVESHAFT VIBRATION E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01169EH16680 33064 HANGER ASSY HAS HIGH FREQUENCY VIBRATION. OUTER COUPLING AND BRG HANGER HAD PRIMER PAINTED ON. NO DEFECTS NOTED FOR HIGH FREQUENCY VIBRATION. DISASSEMBLED, STRIPPED PRIMER, CLEANED & VISUALLY INSPECTED ALL PARTS. HAD CAD PLATING REPAIRED. REASSEMBLED IAW 412-CR&O INSTALLING NEW SEAL.PURGE LUBED BRG WITH MOBIL 28,REPACKED COUPLING WITH GREASE 9-20-01. 1G72 4U H4SW 20030620000272003062000027SW 2003 6 20 HEEA086949 120030603A3212206050247138 COVER BELL 407 407 1182206SW FLOAT ASSY TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH 53399 FLOAT COVER ASSY TORN. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030620000852003062000085EU 2003 6 20 USAASA03037 120030502A3610342B030000 CONTROLLER AIRBUSA321 A321211 3930370EU LT ENG PYLON MALFUNCTIONED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19164UW 1425 EN ROUTE PIT-DEN, WHILE IN CRUISE FLIGHT, AT FL350, ECAM MESSAGE 'L WING LEAK' CAME ON, FOLLOWED BY A LOS OF CABIN PRESSURE. A RAPID DESCENT WAS MADE. THE FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS FERRIED TO PIT FOR MAINTENANCE. A LEFT ENGINE HIGH PRESSURE VALVE WAS REPLACED FOR T/S PURPOSES. A LEFT ENGINE PNEUMATIC CONTROL THERMOSTAT WAS REPLACED TO FIX THE PROBLEM. (M) 2L72 4F RTA28NM 20030707000892003070700089NM 2003 7 7 03181425 120030630A3350 BATTERY PACK DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27425FJ 3189 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE BATTERY PACK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030707000762003070700076NE 2003 7 7 2003UALA00283 220030317A726153B031 BEARING BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 2 ENGINE SPALLED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 WP29219UA8824 30551 AIRCRAFT RECEIVED NR 2 ENGINE HIGH OIL TEMP AND LOW OIL PRESSURE INDICATIONS. REMOVED AND REPLACED ENGINE 222142. SHOP TEARDOWN REVEALED FAILURE OF THE NR 1 BEARING. CAGE FRACTURED OVER AN ARC OF 180 DEGREES. OUTER RACE SEVERELY SPALLED 360 DEGREES ON THE AFT PORTION OF THE RACE. 2L72 4F4 FRTT0001SE E46NE 20030711000062003071100006EU 2003 7 11 MTNA20031 120030311A3213200684001 DRAG BRACE FOKKERF27 F27MK500 4990629EU MLG BROKEN A MTNAO OTHER J WARNING INDICATION APAPPROACH 1 SO33712FE 4350 10613 THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED ON APPROACH INTO EWN. THE FLIGHT CREW PERFORMED THE EMERGENCY LANDING GEAR PRECEDURES AND DID A FLY-BY AT EWN. THE AIRCRAFT WAS DIVERTED TO ISO. THE AIRCRAFT LANDED AT ISO WITH THE RIGHT MAIN LANDING GEAR UNLOCKED. ON LANDING THE GEAR COLLAPSED. 2H72 4T A817 20030711000712003071100071SO 2003 7 11 C2XA03SH203 120030626A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714960 145100 SHV-DURING C-CHECK THE CENTER FLOORBEAM BETWEEN FRAMES 16 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030714001082003071400108EA 2003 7 14 COMA0360306 120030629A5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01797CA9650 7344 FLIGHT 5620 THE LEFT WINDSHIELD SHATTERED DURING CLIMBOUT OF ATL, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE LEFT WINDSHIELD. 2L72 4F RTA21EA 20030108000472003010800047EA 2003 1 8 COMA0360006 120030104A3610 COUPLING CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CRCRUISE 1 SO01712CA 7244 FLIGHT 5239 LEFT 14TH STAGE BLEED AIR DUCT WARNING.TIGHTENED LOOSE BLEED AIR COUPLING AT THE T/R PDU 2L72 4F RTA21EA 20030114000292003011400029 2003 1 14 SWAA030042 420030107A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030127000422003012700042 2003 1 27 HEEA083619 420030114A345713824120234 GPS BELL 407 407 1182206SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 GPS RECEIVER WOULD NOT POWER UP. COULD NOT DUPLICATE PROBLEM. REPLACED FILTER LENS. BENCH CHECK GOOD. 1G71 3U O H2SW 20030127002082003012700208SW 2003 1 27 HEEA083700 120030115A5310206064516001 SUPPORT BELL 407 407 1182206SW ENG OIL TANK CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 AFT ENGINE OIL TANK SUPPORT CRACKED. 1G71 3U O H2SW 20030128000562003012800056SW 2003 1 28 HEEA083810 120030116A3210400052015101 STRAP BELL 407 407 1182206SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH3257 53283 MLG STRAP MISSING RUBBER PAD. 1G71 3U O H2SW 20030128002592003012800259SW 2003 1 28 HEEA083906 120030117A6320406340100101 PUMP BELL 407 407 1182206SW M/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03742PH 53461 MAIN ROTOR GEARBOX OIL PUMP LEAKING. 1G71 3U O H2SW 20030410002492003041000249NM 2003 4 10 F3LA200300032 120030127A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL CORRODED AT STA 727 +5, LBBL 8.10. FABRICATED REPAIR PARTS PER SRM 53-60-53, 53-00-53, AND 51-41-02. 2L72 4F RTA16WE 20030204001092003020400109NM 2003 2 4 SWAA030086 120030115A53146545866 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 DURING SCHEDULED C2 CHECK, FOUND BS 670 KEEL BEAM OUTER SKIN CRACKED 1.1 INCHES ON THE LT AND RT SIDE. REPAIRED SKIN PER SRM AND SWA T1. 2L72 4F RTA16WE 20030214000102003021400010NM 2003 2 14 2003F00095 120030107A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE CABIN LOOSE G K NONE L NO TEST ININSP/MAINT 1 GL11526AT 30735 (ORIG-CLOSED) DURING SCHEDULED MAINTENANCE EGRESS LIGHTING INOPERATIVE FROM ROWS 14 THROUGH 21. MAINTENANCE FOUND LOOSE WIRE AND RESECURED THE WIRE. EGRESS LIGHTING OPERATIONAL CHECK NORMAL. 2L72 4F4 FRTA2NM A12EU 20030625000772003062500077NM 2003 6 25 F3LA200300050 120030129A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL CORRODED AT STA 727 TO STA 947, LBL 3. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-60-53. REPLACED FLOOR SUPPORT BETWEEN STA 727 AND STA 947 PER SRM 53-60-53 AND 51-40-02. 2L72 4F RTA16WE 20030220000622003022000062NM 2003 2 20 ABXA030063 120030212A2497 TERMINAL BLOCK BOEING767 767205 1385121NM NOSE E&E BAY BURNED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23713AX 23058 WHILE PERFORMING ROUTINE MAINTENANCE AT ILN, MAINTENANCE FOUND WIRING BURNED OFF STUDS 5 AND 6, STA. 172 IN NOSE. STUD 4 HAD DAMAGE ALSO. REMOVED AND REPLACED TERMINAL BLOCK 5020, REPAIRED WIRES IAW WDM 24-51-11, SHEET 2. 2L72 4F RTA1NM 20030225000022003022500002SO 2003 2 25 C2XA03SH028 120030225A530014522459001 ANGLE EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 SHV-DURING C-CHECK RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030116000352003011600035GL 2003 1 16 HEEA082994 220030109A72306893614 NUT BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL NR 2 BEARING MISMANUFACTURED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03141BH 51303 CAE890396 COMPRESSOR NR 2 BEARING NUT HAS IMPROPER MACHINING OF AFT THREADS. 1G71 3U3 U H2SW E1GL 20030116000812003011600081 2003 1 16 HEEA083041 420030106A230002000002 AMPLIFIER BELL 206 206L3 1182108SW COMM SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 WHELAN AMPLIFIER BLOWING THE FUSE. REPLACED FUSE Q7, Q8 TRANSISTORS DUE TO SHORTED. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116002952003011600295EA 2003 1 16 QXEA0300081 220030114A732054012811 CARTRIDGE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09404QX 4046 FA0092 SEA ON FLIGHT 2372- RETURNED TO FIELD DUE TO NO.2 FADEC CAUTION ILLUMINATED DURING FLIGHT. AIRCRAFT LANDED WITHOUT INCEDENT. REMOVED AND REPLACED P2.2 BLEED VALVE SCREEN CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20030119000012003011900001NE 2003 1 19 RAIA00301006 220030103A730031055017 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE DEFECTIVE A RAIAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 CE03571HK3762 41090 75104 5487-STL- LEFT ENGINE QUIT DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE #1 INLET TEMPERATURE SENSOR, OPS CK OK. 2L72 4T4 TRTA41NM E18NE 20030305000832003030500083EU 2003 3 5 HEEA084666 120030213A6720 BEARING AEROSPAS355 AS355* EU P/CONTROL ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034000L 2873 TAIL ROTOR PITCH CONTROL ROD SPHERICAL BEARING IS OUT OF LIMITS. 1G72 3U H11EU 20030227000872003022700087SO 2003 2 27 C2XA03CL053 120030226A33501317 BULB EMB 145 EMB145 3260210SO CABIN BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712967 145133 DURING ROUTINE MAINTENANCE THE RIGHT HAND EMERGENCY EXIT CEILING LIGHT WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030228001242003022800124SW 2003 2 28 HEEA084471 120030213A2497SM20ACD200A21 RELAY BELL 206 206L3 1182108SW ELECTRICAL MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 RELAY MALFUNCTIONED, WARNING HORN NOISE, ANTI COLLISION LIGHT WAS BLINKING AND CAUTION PANEL LIGHT ON. FOUND BATTERY SWITCH OFF. CYCLED BATTERY SWITCH TWICE WITH NO CHANGE. 1G71 3U H2SW 20030303001172003030300117SW 2003 3 3 HEEA084534 120030214A2841393008047 INDICATOR BELL 412 412 1182202SW FUEL QTY STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 FUEL QTY INDICATOR NEEDLE STICKS COMING DOWN. 1G72 4U H4SW 20030307000022003030700002SO 2003 3 7 C2XA03SH35 120030307A530014534608007 SKIN EMB 145 EMB145LR 3260212SO CARGO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 SHV DURING C CHECK CORROSION WAS FOUND ALONG CARGO FLOOR SKIN BETWEEN FRAMES 65 TO 68 AT STRINGERS 21L AND 2OR. MAINTENANCE REMOVED AFFECTED SKIN IAW CONTINENTAL EXPRESS EC 5330-01234. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030310000662003031000066SW 2003 3 10 HEEA084970 120030227A3213412030437103 CAP BELL 412 412 1182202SW MLG CROSSTUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 MLG CROSSTUBE CAP RUBBER WORN. REPAIRED. 1G72 4U H4SW 20030311000032003031100003SW 2003 3 11 HEEA085027 120030228A6420MS211536 BEARING BELL 206 206L3 1182108SW ROD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 TAIL ROTOR HEAD CONTROL ROD HAS A WORN BEARING. SCRAPPED. 1G71 3U H2SW 20030313000832003031300083SW 2003 3 13 JJWA0049743 120030210A243615891F VOLT REGULATOR BELL 206 206B 1181511SW DC SYSTEM FAILED E JJWAO OTHER O OTHER NRNOT REPORTED 1 SO1725PM 1839 VOLTAGE REGULATOR FAILED ON TAKEOFF, CAUSED BOTH COMM RADIOS TO FAIL WITH SMOKE OBSERVED FROM COLLINS 251 COMM RADIO. REPLACED REGULATOR, SERVICED GILL BATTERY AND OVERFLOW BOTTLE, ADJUSTED REG TO 27.5 VDC, BORROWED RADIOS TO USE WHILE COMM ARE REPAIR, NO OTHER DAMAGE FOUND. 1G71 3U H2SW 20030122001052003012200105EU 2003 1 22 HEEA083491 120030107A2435200SGL100912 BRUSHES BOLKMS105 BO105S 5626006EU STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381832 18501 S828 STARTER GENERATOR HAS WORN BRUSHES. REPLACED BRUSHES. 1G72 3U H3EU 20030123000392003012300039NM 2003 1 23 2003UALA00064 120030116A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29501UA 24622 FLOORBEAM CRACKED AT FLOOR SUPPORT ATTACH CLIP, STA 700 LBL 46. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20030318000432003031800043WP 2003 3 18 03FDEA00318 120030314A5720 STRINGER CLIP DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 RIGHT WING NR 3 FUEL TANK HAS A CRACKED UPPER BUTTERFLY CLIP AT STA XORS 402. THIS WAS FOUND DURING A ROUTINE INSPECTION. 2L73 4F A22WE 20030418001192003041800119WP 2003 4 18 ZW0A0302602 120030220A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY SIGN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13901TW 49166 AFTER ARRIVAL DURING P-S FOUND CABIN EXIT SIGN NOT COMING ON. EMERGENCY EXIT SIGNS BATTERY REPLACED TWS 82-4388 CPN 753-4697. OPS CHECK BY TURNING SYSTEM ON AND OFF. CHECK-C STL 6-28-02. 2L72 4F A6WE 20030418001382003041800138SO 2003 4 18 SWIA200311795 120030217A7500 WYE DUCT EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE ENGINE DAMAGED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07217SW 120286 ON TAKEOFF ROLL RIGHT T6 GAP WENT TO 300 DEGREES IN BOTH DIGITAL AND ANALOG WITH NO POWER LOSS TO THE ENGINE. ABORTED TAKEOFF. FOUND BLEED AIR DUCT ON TOP OF T6 PROBE RING TOUCHING BOTH RINGS. REMOVED AND REPLACED BLEED AIR WYE OFF OF ENGINE, TIGHTENED CLAMPS, AND ADJUSTED WHEEL WELL FEED THROUGH TUBE CLAMP AND BRACKET. 2L72 4T4 TRTA31SO E20NE 20030718000392003071800039NM 2003 7 18 USAASB03080 120030612A2420735511A CSD BOEING737 7374B7 1384702NM ENG ACCY GEARBOXFAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19785AU40456 25024 PHL - FLT 685 - ON CLIMB-OUT FROM PHL, EN ROUTE TO FLL, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT FLICKERED SEVERAL TIMES. GENERATOR DRIVE TEMPERATURES, 'IN' AND 'RISE', WERE AT MAXIMUM VALUES. AT THIS POINT, THE HIGH OIL TEMPERATURE LGIHT ILLUMINATED. CAPTAIN DISCONNECTED THE NR 1 ENGINE CSD BUT REPORTED HE DID NOT GET A GOOD DISCONNECT. AFTER ATTEMPTED DISCONNECT, RESIDUAL VOLTAGE READ 15 VOLTS WITH BOTH THE 'IN' AND 'RISE' TEMPERATURES READING OFF SCALE HIGH. LOW OIL PRESSURE LIGHT CONTINUED TO FLICER AFTER DISCONNECT. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED THE NR 1 ENGINE CSD PER MM 24-11-11. ALSO, REMOVED AND REPLACE2L72 4F RTA16WE 20030423001692003042300169NM 2003 4 23 ZW0A0303102 120030314A3350 BATTERY PACK BOEING757 757231 1384950NM EMERGENCY LIGHT DISCHARGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13727TW 30340 THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 18 LT AND 23 RT SIDE, AND THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 18 AND THE REAR LAV. REPLACED LAMPS P/N 8074-1 FOR THE OVERHEAD LIGHTS, AND REPLACED THE BATTERY PACK P/N 2013-1A FOR THE EGRESS LIGHTS. CHECK-C 1-7-03 MCI. 2L72 4F RTA2NM 20030611000862003061100086SW 2003 6 11 HEEA086694 120030522A6220412010216107 BEARING BELL 412 412 1182202SW PENDULUM ASSY ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L7157 33023 MAIN ROTOR PENDULUM BEARING ROUGH. SHOP REPAIR. 1G72 4U H4SW 20030611001312003061100131NM 2003 6 11 DL76S030454 120030510A3241 CONNECTOR BOEING767 767332 1382001NM ANTISKID MODULE DAMAGED A DALAO OTHER N FALSE WARNING LDLANDING 1 SO27130DL 24080 UPON TOUCHDOWN - NORMAL RATE APP 140 KTS. AUTOBRAKES DISARMED, AUTO SPEEDBRAKE DID NOT EXTEND UNTIL T/R EXTENDED,WHEEL BRAKES LEFT SIDE NEVER GOT ABOVE 0 INDICATION;RT SIDE BRAKES UP 5 & 6. EXITED AT EOR DUE TO BRAKING. REPLACED WHEEL ASSY 1,2,5,& 6. PERFORMED BURST TIRE INSP PER05-51-16-2. DURING TRANSDUCER SPIN TEST FOUND NR 1 BRAKE NOT RESPONDING; FOUND PUSHED BACK PIN ON CANNON PLUG FOR ANTISKID VALVE MODULE. RESEATED, SYS CKS OK. 2L72 4F RTA1NM 20030611001422003061100142EA 2003 6 11 ASOA03204 120030510A5220H341933 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11859AS 7421 DURING A C-CHECK IN MCN, THE COCKPIT EMERGENCY ESCAPE HATCH OUT HANDLE WOULD NOT DEPLOY. MAINTENANCE REMOVED AND REPLACED THE COCKPIT EMERGENCY ESCAPE HATCH OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030612000502003061200050WP 2003 6 12 ABXA030173 120030501A5711995750513N FITTING DOUG DC9 DC932 3022066WP REAR SPAR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 RIGHT INBOARD FIXED VANE NR 2 SUPPORT CRACKED. REPLACED BROKEN FITTING IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030617000102003061700010EU 2003 6 17 AUS20030477 120030430A5347 SEAT TRACK AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CABIN FLOOR STRUCTURE CONTAINED LEVEL 2 CORROSION IN THEFOLLOWING AREAS:- 1. DOOR CUTOUT REAR RADIUS AT L1 DOOR2. CENTRE ATTACHMENT ANGLE (LOCATED BETWEEN FORWARD AND REAR RADIUS OF L1 DOOR GUSSETS 3. LT REAR PASSENGER DOOR SILL. RT OUTBOARD SEAT TRACK AT SIX LOCATIONS BETWEEN FR18 AND FR215. RT REAR DOOR SILL AREA AT- A. REAR GUSSET (RADIUS) SILL. CENTRE STRIP BETWEEN FORWARD AFT GUSSET. 2L72 4F4 FRTA28NM E29NE 20030611001432003061100143EA 2003 6 11 2003F00364 120030515A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA NR 2 ENGINE FAILED A FDKAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07510MJ 10101 FRL - FLT 6570 - SAN-TUS, RETURNED TO FIELD DUE TO LOSS OF NR 2 ENGINE EDP HYD PRESSURE. MAINTEANCE PERFORMED MAINTENANCE ACTION FOR MEL 29-11-01 AND RETURNED A/C TO SERVICE. MAINTENANCE REPLACED THE PUMP. (M) 2L72 4F RTA21EA 20030617002402003061700240NM 2003 6 17 QXEA200300729 120030613A27313994001011 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM ELEVATOR TRIM FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09411QX235 235 4055 SEA - FLIGHT 00310 - DURING APPROACH AND AIRCRAFT AT FULL LANDING CONFIGURATION, THE CREW RECEIVED A MASTER CAUTION. CREW ACKNOWLEDGED THE MASTER CAUTION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ELEVATOR TRIM ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030521001602003052100160NM 2003 5 21 SWAA031080 120030514A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 827 AT STR 25L, BS 847 AT STR 22L, BS 787 AT STR 25L & BS 807 AT STR 25L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030523000802003052300080NM 2003 5 23 SWAA031108 120030516A2731251A2345 TORQUE TUBE BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C4 CHECK, SWA SI 11038, LT ELEVATOR TAB FAILED FREE PLAY CHECK. FOUND,PLAY AT ELEVATOR TORQUE TUBE ASSY BETWEEN LT ELEVATOR INPUT ROD ARM AND OUTER TUBE. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM. 2L72 4F RTA16WE 20030618000382003061800038NM 2003 6 18 SWAA031331 120030614A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 36. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20030626000042003062600004WP 2003 6 26 UPS03840430 120030418A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: PFLT, 2 INCH GOUGE IN NR 4 PIT SLOPING WALL 3 FT ALT OF BULKHEAD AFTER PULLING BACK THE LINER, FOUND FRAME CRACKED. REMOVED FLOOR PANEL IN NR 4 PIT RIGHT SIDE FWD TO INSPECT FLOOR SUPPORT FRAME FOR DAMAGE . KMA 56755 / ACCOMPLSIHED PERMANENT REPAIR PER APP C E.O. DC8-5320-8724-A. KMA 56755 REINSTALLED FLOOR PANEL. 2L74 4F RT4A25 20030714000502003071400050 2003 7 14 SWAA031375 420030620A2565D31354 SLIDE BOEING737 7373H4 1384600NM PAX DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030707001142003070700114SO 2003 7 7 XGN2003F00001 220030616A8520643200 CRANKCASE BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO ENGINE CRACKED E XGNAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW051096W CE436 CRACK WAS DISCOVERED WHILE LOOKING FOR THE SOURCE OF AN OIL LEAK. 1L71 3O3 O 3A15 E5CE 20030114000582003011400058NM 2003 1 14 SWAA030005 120030102A52416545871 PLATE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED BC2 CHECK, FOUND FWD SVC DOOR LOWER AFT STOP BACKUP PLATE CRACKED. REMOVED AND REPLACED FWD SVC DOOR PER MM. 2L72 4F RTA16WE 20030114001222003011400122NM 2003 1 14 SWAA030027 120030106A321165465113 TRUNNION PIN BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030116000262003011600026 2003 1 16 HEEA082983 420030107A34168503S20LW INDICATOR SKRSKYS76 S76A 8143006NE ALTIMETER READS HIGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ 760231 COPILOT ALTIMETER INDICATES 110 FEET AT SEA LEVEL. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030116000572003011600057 2003 1 16 HEEA083016 420030106A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMM SYS ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 MIXER BOX ERRATIC. REPAIRED. 1G71 3U H2SW 20030116000992003011600099SW 2003 1 16 HEEA083053 120030107A6510206061432117 IMPELLER BELL 206 206L3 1182108SW T/R BLOWER DEFECTIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 TAIL ROTOR BLOWER IMPELLER DEFECTIVE. 1G71 3U H2SW 20030127001692003012700169SW 2003 1 27 HEEA083691 120030115A2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 98136 53400 STARTER GEN BRUSHES WORN. REPAIRED. 1G71 3U O H2SW 20030127002782003012700278GL 2003 1 27 HEEA083754 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 MGT HIGH ABOVE 3000 FEET AT CRUISE. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030212000732003021200073EA 2003 2 12 CA030119005 120030108A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LT SIDE WINDOW CRACKED, WINDOW ASSY REPLACED. 2L72 4F4 FRTA21EA E15NE 20030213000882003021300088EA 2003 2 13 COMA0360087 120030212A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA 7017 FLIGHT 5612 CABIN DOOR WARNING AFTER T/O.CLEANED SNOW AND ICE FROM DOOR WARNING SENSORS. 2L72 4F RTA21EA 20030218002582003021800258NM 2003 2 18 SWAA030359 120030212A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030221000232003022100023NM 2003 2 21 AWXA200300073 120030104A5755 STRUCTURE BOEING737 7373G7 1384595NM SPOILER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C-13 CHECK 2 EACH BULGES WERE FOUND ON UPPER SURFACE SKIN OF LT WING NR 2 SPOILER. MAINTENANCE REMOVED 2 EACH BULGES ON UPPER SURFACE SKIN OF LT WING NR 2 SPOILER; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 57-70-01, PG. 209-210. 2L72 4F RTA16WE 20030224000862003022400086GL 2003 2 24 HEEA084207 220030120A7230407070211102 PLENUM BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 PLENUM IS CRACKED. 1G71 3U3 UO H2SW E4CE 20030306000322003030600032SW 2003 3 6 HEEA084745 120030217A5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ACTUATOR CAUSES RIGHT STEP NOT TO EXTEND. REPAIRED. 1G72 4U H4SW 20030307000522003030700052NM 2003 3 7 SWAA030440 120030226A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030311000362003031100036GL 2003 3 11 HEEA085052 220030228A732066917201361 SOLENOID VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL FUEL TRIM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 WOULD NOT START WITH INTELLISTART SYSTEM ON LINE. 1G71 3U3 U H2SW E1GL 20030314001962003031400196GL 2003 3 14 0065074 320030121A6110C13019 CLAMP HARTZL BEECH 90 F90 1152909CE PWA PT6 PT6* 52043EA HARTZLHCB4T HCB4TN3 GL PROP HUB CORRODED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 EAA1241 EAA1241 CORROSION ON PROPELLER HUB CLAMP 1L72 4T3 T A31CE E2NE 6 CP40EA 20030319000102003031900010WP 2003 3 19 GTIA030010 120030111A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CABIN FLOOR PANEL AFT AUX TANK AFT CENTER HAS SOFT/MUSHY/DETERIORTATION. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030320001192003032000119NM 2003 3 20 2003UALA00109 120030128A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29955UA 26703 178 BULKHEAD, FORWARD WEB, LOWER RADOME MOUNT RT, CRACKED AT UPPER INBOARD END. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030122000512003012200051 2003 1 22 HEEA083439 420030109A3140 BATTERY BELL 206 206L3 1182108SW COMPUTER DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 0358 51412 INTELLASTART PROCESSOR SUSPECT INTERNAL BATTERY DEAD. 1G71 3U H2SW 20030122001152003012200115EU 2003 1 22 HEEA083497 120030107A3340D3040E LANDING LIGHT BOLKMS105 BO105S 5626006EU EXTERIOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 LANDING LIGHT WILL NOT RETRACT. REPLACED WITH SERVICEABLE LIGHT. 1G72 3U H3EU 20030122001772003012200177NE 2003 1 22 HEEA083543 220030113A720030176003B ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 ENGINE POWER SECTION PRODUCING LOW POWER N1. TO BE SENT TO VENDOR. 1G72 4U4 U H4SW E22EA 20030326000772003032600077NE 2003 3 26 2003UALA00191 220030220A723051H14701 VANE BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 2 ENGINE BROKEN A UALAEA ENGINE SHUTDOWN UNSCHED LANDING ARJFLAME/FIRE PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29105UA 26473 717610 NR 2 ENGINE EXPERIENCED COMPRESSOR STALL. READINGS DROPPED AFTER A/C REACHED ALTITUDE. THE 7TH STAGE COMPRESSOR BLADE FAILED AT THE ROOT AND DAMAGED THE HPC, CAUSING THE ENGINE TO SURGE. T HE BLADE FAILURE WAS CAUSED BY THE VANE ARM ON THE 6TH STAGE VSV BEING BROKEN AT THE 6 O'CLOCK POSITION. THE ENGINE WAS REMOVED AND OVERHAULED. 2L74 4F4 FRTA20WE E24NE 20030731001002003073100100NM 2003 7 31 QXEA200300805 120030708A33506104789 BATTERY PACK DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09369PH9825 9825 513 PDX- FORWARD TWO LIGHTS ON EMERGENCY FLOOR PATH LIGHTING IN CABIN ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS PS1 AND PS2. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030801001132003080100113EA 2003 8 1 COMA0360336 120030725A3230200811620 ROLLER CNDAIRCL600 CL6002B19 1900309EA NLG WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01916CA 7014 FLIGHT 5154 GEAR DISAGREE WARNING, NLG INDICATED INTRANSIT. COULD NOT DUPLICATE CYCLED LANDING GEAR MULTIPLE TIMES WITH NO DISCREPANCY. REPLACED A WORN NLG UPLOCK ROLLER. 2L72 4F RTA21EA 20030325000032003032500003EU 2003 3 25 03081315 120030322A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP EMER EXIT UNSECURE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27315UE 41033 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE 6A SIDEWALL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL FOUND THAT THE LAMP HAD COME LOOSE IN THE SOCKET. THE LAMP WAS SECURED, AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20030326000422003032600042EU 2003 3 26 AUS20030193 120030219A2810D2825003200200 COUPLING AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE FUEL STORAGE FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING FUEL CONNECTOR COUPLING NOT BONDED TO FRONT SPAR. THE REFUEL/DEFUEL COUPLING ALSO FAILED BONDING CHECK. 2L72 4F4 FRTA46NM E29NE 20030417000022003041700002EU 2003 4 17 RAIA00301016 120030116A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03554HK 41067 MX - STL - EMERGENCY ESCAPE PATH LIGHTS OUT AT ROWS 8, 9, AND 10. RE-SECURED CONNECTOR AT EMERGENCY PATH LIGHT STRIP, OPS CHECK OK. 2L72 4T RTA41NM 20030327001902003032700190EA 2003 3 27 CA030211002 120030204A7921C6L10211 BRACKET DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA OIL COOLER CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) OIL COOLER BRACKET IS A WELDED ASSEMBLY FROM FACTORY. CRACKS ORIGINATED FROM MOUNTING HOLES AND 'RELIEF' AREA. 1H72 3T4 TRTA9EA E4EA 20030714001382003071400138NE 2003 7 14 DLM88030494 220030527A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 OUT OF TRIM A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27906DE37446 53415 725380 RTB NR 2 ENG FAILED TO ACCELERATE ABOVE IDLE DURING THROTTLE ADVANCE FOR T/O. PEAK OF EGT APPROX 490 RPM STAYED AROUND 47 PERCENT N2 ABORTED TAKEOFF BELOW 60 KTS. TRIMMED ENGINE, CHECKS GOOD. 2L72 4F4 FRTA6WE E9NE 20030417001142003041700114EU 2003 4 17 MALA030137 120030130A2150 CLAMP BAC 146 AVRO146RJ85A1500097EU NR 2 PACK LOOSE A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15501XJ E2208 SMOKE COMING FROM TAIL OF A/C IN SDF AFTER FLIGHT 3512. MAINTENANCE FOUND LOOSE CLAMP AND HOSE ON NR 2 PACK. RESECURED, OPS CHECKS GOOD. (AVIATION SERVICES INC AP457922137). 2H74 4F RTA49EU 20030422001392003042200139NE 2003 4 22 P5CA0300772 220030304A7532670333 COMPRESSOR BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE NR 3 ENGINE STALLED A P5CAO OTHER O OTHER CRCRUISE 1 WP23524UP 21446 517897 AT FLT LEVEL 19.0 WHEN THRUST LEVER WAS RETARDED NR 3 ENG COMPRESSOR STALLED. REMOVED AND REPLACED FLOW DIVIDER AND SECURE PT 2 LINE. OPERATIONAL CHECK OK ON ENGINE RUN UP. APPARENT FAILURE OF ENG BLEED SYSTEM ON DESCENT WHEN THROTTLE WAS RETARDED. 2L74 4F4 FRTA20WE E20EA 20030828001122003082800112NM 2003 8 28 MWEA030326 120030822A5320993658045 INTERCOSTAL DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 AFT PIT INTERCOSTAL AT AIRCRAFT CENTER LINE BETWEEN FRAME STATION 1309 & 1287 IS CRACKED IN SEVERAL PLACES. FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F RTA6WE 20030829001312003082900131 2003 8 29 SWAA031859 420030819A2565D31354 HANDLE BOEING737 7373H4 1384600NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 AFT SVC DOOR EMERGENCY EVAC SLIDE PULL HANDLE LOOSE. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030903000162003090300016GL 2003 9 3 ALG2003F00066 220030620A732023072725 HMU BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE LEAKING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03687AL1313 53366 CAE847018 DURING REFUELING. AFTER A/C WAS REFUELED OFFSHORE AT WC-560. THE MECHANIC NOTICED A STEADY FLOW OF FUEL FROM THE OVERFLOW DRAIN LINE. HE INSPECTED THE LEAK AND FOUND THE HMU LEAKING. HE REMOVED AND REPLACED THE HMU AND COMPLIED WITH A LEAK CHECK AND AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20030724001072003072400107NM 2003 7 24 DLM90030567 120030621A32205940497511 STRUT DOUG MD90 MD9030 3023690NM NLG LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27901DA 53381 AFTER TAKEOFF NOSE GEAR UNSAFE LIGHT STAYED ILLUMINATED. CYCLED GEAR IAW POM GEAR REMAINED UNSAFE. FOUND NOSE STRUT LEAKING. REPACKING NOSE STRUT. 2L72 4F RTA6WE 20030728000892003072800089 2003 7 28 SWAA031621 420030721A2565D31354 SLIDE BOEING737 7373G7 1384595NM SERVICE DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2L72 4F RTA16WE 20030806000392003080600039GL 2003 8 6 C2XA03TY102 220030730A720023070402 ENGINE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL ZONE 400 LACK OF LUBE A C2XAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW27295155842 5842 145309 CEA311481 THE LT ENGINE IMPENDING OIL BYPASS INFLIGHT. AFTER APPROXIMATELY 2 MINUTES OIL PRESSURE DROPPED INTO THE RED, 32 PSI AND DROPPING. THE CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. LANDED AT MEM. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW-TASK CARD 6271001, OPERATIONAL AND LEAK CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030828001642003082800164NM 2003 8 28 USAASB03135 120030810A33501012721 LIGHT BOEING737 7373B7 1384580NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19383US 22956 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 22C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT 22C. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030903001022003090300102NE 2003 9 3 MEX2003212 220030506A7220 INLET BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE ENGINE DAMAGED A ASMFK NONE O OTHER ININSP/MAINT 1 SW23802AM 26270 FLT 6444 - MEX-HMO - DURING TRANSIT CHECK, DETECTED FAN INLET GUIDE DAMAGED BY AND FOD. IN THE HANGAR THE FAN INLET GUIDE WAS REWORKED, TEST PERFORMED IAW 72-00-00, ALL CORRECT. (M) 2L72 4F4 FRTA2NM E17NE 20030903001052003090300105 2003 9 3 USAASA03082 420030727A2565C37103101 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE O OTHER ININSP/MAINT 1 EA19746UW 1297 CLT - THE FORWARD LEFT EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP REPLACED THE RELEASE CABLE AND RETURNED TO SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20030904001882003090400188WP 2003 9 4 AALA20030720 120030707A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21241AA 49254 DFW - BOTTOM LAMP IN TAILCONE THREE LAMP ASSEMBLY AND AFT CABIN CEILING EMERGENCY LIGHTS ARE INOPERATIVE NEAR AFT LAVATORIES. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030806000562003080600056SO 2003 8 6 C2XA03BT072 120030714A32343631101007 SELECTOR EMB 145 EMB145ER 3260211SO COCKPIT DIRTY A C2XAO OTHER N FALSE WARNING LDLANDING 1 SW2713936 145025 CREW REPORTED, LANDING GEAR WARNING ON LANDING WITH LANDING GEAR DOWN AND THREE GREEN LIGHTS. MAINTENANCE CLEANED LANDING GEAR HANDLE CANNON PLUG, OPS CHECKED SYSTEM GOOD IAW EMB145 MM 32-32-00. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030806001472003080600147SO 2003 8 6 C2XA03SH244 120030731A531114521721005 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 DURING C-CHECK, FOWARD DIGITAL BUTTSTRAP WAS FOUND TO HAVE CORROSION AT FRAME 15. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030812000912003081200091EU 2003 8 12 HEEA088631 120030719A32131175000212 SKID BOLKMS117 BK117A1 5626010EU MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC 7152 WORN EXCESSIVELY THROUGH TO BASE METAL. SCRAPPED. 1G72 3U H13EU 20030821000192003082100019NM 2003 8 21 USAABB03119 120030724A33501000679 LIGHT BOEING767 767201 1385125NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19646US 23898 PHL - FOUND THE PORTABLE EMERGENCY LIGHT ABOVE THE COCKPIT DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA1NM 20030825000812003082500081EA 2003 8 25 03219685 120030807A335059257 INVERTER CNDAIRCL600 CL600* EA CABIN FAULTY A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27685BR 7712 DURING MAINTENANCE INSPECTION, NUMEROUS EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED INVERTER, AN OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20030910001982003091000198WP 2003 9 10 MEX2003379 120030821A243243B034LB03 BATTERY DOUG DC9 DC987 3022087WP E/E BAY OVERHEATED A ASMFO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW23214AM 49585 FLT 519 - MEX-VSA - AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF HOT BATTERIES AND SMOKE UNDER THE FUSELAGE. DURING REVISION DETECTED BATTERIES AND BATTERIES CHARGER WITH OVERHEAT. THE BATTERIES AND BATTERY CHARGER WAS REPLACED IAW MM 24-30-01/02, ALL CORRECT. (M) 2L72 4F RTA6WE 20030911000072003091100007EU 2003 9 11 03FDEA01249 120030811A5311 FRAME AIRBUS300 A300F4605R 3930327EU CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 AFT CARGO FRAME (C58) 20 INCH TO THE RT OF CENTER HAS A 1 INCH CRACK IN FRAME. REPAIRED: IAW (EA6-5310-71398) BY CUTTING OUT CRACKED SECTION IAW SRM 51-27-00, NDT THE CUT OUT. REMOVED AFFECTED FASTENERS AND CABLE SUPPORTS AS REQUIRED, FLAP-PEEN AREA FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER. 2L72 4F RTA35EU 20030730000152003073000015WP 2003 7 30 ABXA030212 120030528A532039136472N FITTING DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 CABIN FLOORBEAM END FITTINGS FS 973, RIGHT BUTTLINE 58, LEVEL I CORROSION. REPLACED FLOORBEAM END FITTINGS IAW DC-9 SRM. 2L72 4F A6WE 20030729001342003072900134SO 2003 7 29 SWIA200312201 120030718A275012064207615 CONTROL HANDLE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07233SW220 220 120307 ON APPROACH, WHEN SELECTING FLAPS 45 GOT CONTROL FAULT. REPLACED FLAP CONTROL LEVER ASSY IAW MM 27-50-00. OPS CHECK OK 2L72 4T4 TRTA31SO E20NE 20030930000272003093000027NM 2003 9 30 03FDEA01463 120030906A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 MAIN DECK CARGO COMPT. FLOOR TRACK AT STA 635, X = -8.5 FOUND CRACKED, APPROX. 3 INCHES LONG. 2L73 4F RTA22WE 20030929000182003092900018NM 2003 9 29 801DM0011 120030827A3397 WIRE BOEING757 757200 1384950NM EMERGENCY LIGHT BROKEN A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05801DM 26240 EMERGENCY PATH LIGHT AT SEAT ROW 8C AND D INOPERATIVE. LIGHT DISCONNECTED. REPAIRED BROKEN WIRE AND CONNECTED LIGHT ON SEAT ROW 8C AND D. EMERGENCY PATH LIGHT OPS CHECKS GOOD IAW SWPM 20-10-11, AAC DWG. 143335002, REV.A DATED 9/5/02, 143335111 REV.B DATED 9/7/02. 2L72 4F RTA2NM 20030930000522003093000052EU 2003 9 30 MALA030388 120030827A2910711493 SELECTOR VALVE BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM LEAKING A MALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15517XJ E2335 AIR RETURN TO OKC DUE TO GREEN HYD SYSTEM LOW ON FLUID. FERRIED TO MSP. FOUND STBY GEN SELECTOR VALVE LEAKING HYD FLUID. FROM LOG SHEET DISC 17: RESEALED RIGHT WING ROOT PER EOA57042 LEAK CHECK GOOD REMOVED AND REPLACED STBY GEN SELECTOR VALVE PN 71149-3 SN OFF F9818862 SN ON F971762. REMOVED AND REPLACED NR 3 ENG EDP PN 521449 SN OFF F9830152 SN ON F9829513 IAW 29-10-17 OPS AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20030929001092003092900109NM 2003 9 29 AWXA200301023 120030815A5753657193091B SKIN BOEING737 737277 1384570NM LT WING TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK THE LT OUTBOARD HINGED FLAP TRAILING EDGE SKIN WAS FOUND DELAMINATED. MAINTENANCE PERFORMED HONEYCOMB REPAIR ON TRAILING EDGE SKIN OF LT OUTBOARD HINGED FLAP IAW B737-200 SRM 51-40-20, FIG. 10, PG. 40-41. 2L72 4F RTA16WE 20031006001272003100600127 2003 10 6 RAIA00309241 420030912A34257003360948 DISPLAY JETAIRJETSTMJETSTM4101 1500501EU AHRS INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03558HK9197 533 41071 FO'S AHRS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 AHRU. 2L72 4T RTA41NM 20031007000762003100700076 2003 10 7 SWAA031950 420030830A2565 INDICATOR BOEING737 7372H4 138448CNM SLIDE BOTTLE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031007001132003100700113EU 2003 10 7 03243316 120030831A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING MAINTENANCE INSPECTION THE LEFT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031007000852003100700085EU 2003 10 7 03242313 120030829A3350OL3071BPRGPL BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27313UE 41026 DURING MAINTENANCE INSPECTION THE EMERGECNY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT FILAMENT. A SATISFCTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031022000922003102200092NM 2003 10 22 03FDEA01736 120031014A5330 STRINGER BOEING727 727200 138407ENM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25493FE 21531 BULGE ON EXTERNAL SKIN BS 1050 AT STR 27L. CUT OUT & REMOVED DAMAGED STRINGER BS 1040-1060 STR 27L. FABRICATED & INSTALLED REPAIR IAW SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20031021002962003102100296NM 2003 10 21 PCAA0309114 120030918A33506038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM POSITION 500 INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13845EX31784260 344 CREW REPORTED THAT THE EMERGENCY LIGHTING FOR SEAT 1F WAS BURNT OUT FOR BOTH THE SIDE WALL AND AT THE FLOOR LEVEL LIGHTING. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THAT SEVERAL BULBS WERE BURNT OUT AND THAT THE POSITION 500 POWER SUPPLY WAS AT FAULT. THE EMERGENCY LIGHT FORWARD RIGHT HAND POWER SUPPLY AND 5 BULBS WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20031027000482003102700048NM 2003 10 27 03FDEA01610 120030923A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION 3) BS 990 FLOORBEAM RBL 23 WL 200. 2L73 4F RTA3WE 20031029000822003102900082NM 2003 10 29 ASAA0240216 120030329A5320654963175 SUPPORT ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY FLOOR TO AFT BULKHEAD SUPPORT ANGLE HAS CORROSION AT NUT PLATES. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031110001662003111000166NM 2003 11 10 SWAA032248 120031013A57546573714 WEDGE BOEING737 7373H4 1384600NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT T/E WEDGE DELAMINATED AT OUTBD END. REPAIRED WEDGE PER SRM. 2L72 4F RTA16WE 20031119001492003111900149SO 2003 11 19 SWIA200312485 120031001A2120 ODOR EMB 120 EMB120ER 3260203SO CABIN DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07215SW 120281 TAXIING OUT IN AUTO/NORM (FOR LESS THAN 1 MINUTE) DETECTED SMOKE. TURNED PACKS BACK TO LOW/LOW. NO ABNORMAL INDICATION ON PNEUMATIC PANEL BUT F/A REPORTED SMOKE IN CABIN & SMOKE IN LAV. TURNED OFF RECIRCS & PACKS, RETURNED TO GATE. SMOKE REMAINED BUT NO NEW SMOKE. FOUND PACKS TO BE FROZEN (ICED UP). DEFROSTED PACKS. COULDN'T DUPLICATE ANY PROBLEMS. 2L72 4T RTA31SO 20040129001252004012900125NM 2004 1 29 DHL200374249 120031209A5754 SKIN BOEING727 727225 1384077NM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 4 SLAT IS CRACKED AT ACCESS PANEL LOWER ATTACH ANGLE AT THE RIB INBD OF ANTI ICE DUCT. REMOVED DAMAGED AREA DIM 1.125 INCH AND FABRICATED NEW DOUBLER FROM 2024 T3 .050 PO 900274 DIM 6 X 1 INCH AND FILLER FROM 2024-T3 .040 PO 900471 1.125 X 1 INCH IAW B727 SRM 51-40-3, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER AND FILLER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040204001512004020400151NM 2004 2 4 EIA2003134 120031020A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE WORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 FUSELAGE SKIN WORN AT INTERFACE OF VERTICAL STAB SEAL RT SIDE BS 2280-2416 REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2 2L74 4F A20WE 20031103000882003110300088SW 2003 11 3 ALG2003F00080 120030703A6510206033412123A BRACKET BELL 206 206L 1181522SW NR 5 AFT BRKT MISMANUFACTURED E ALGAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 WHEN TRIED TO PUT PART IN FIXTURE FOR LOCATING, RADIUS HAS A LARGE BELLY, WOULDN`T ALLOW BRACKET TO FIT IN FIXTURE. REVIEW MFG PROCESS. 1G71 3U H2SW 20031106001452003110600145EA 2003 11 6 SWIA200312532 120031020A2720 JACKSHAFT CNDAIRCL600 CL6002B19 1900309EA RUDDER OUT OF ADJUST A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07589SW 7072 WHEN DOING RUDDER PRE-TAXI CHECK, UNUSUAL CLICKING SOUND (APPROX 1/2 TRAVEL) WITH BUMP FELT ON PEDDLES ON CAPTS SIDE. RETURNED TO GATE. REPLACED RUDDER PEDAL ADJUSTMENT JACK SHAFT AND SCREW. OPS CHECKS GOOD IAW 27-21-05. P/N ON 600-90223-5. 2L72 4F RTA21EA 20031112000892003111200089NM 2003 11 12 C1HA200394037 120031108A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK BS 344 - 480 LBL 24.75 HAS CORROSION AND WORN AREAS. 2L73 4F A3WE 20031113000142003111300014CE 2003 11 13 BAQA090538 120031028A30002724130201 VALVE LEAR 35 35A 5170602CE ANTI ICE SYSTEM MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0330DK 9837 345 LIGHT REMAINS ON WITH SWITCH OFF. REPLACED WITH SERVICEABLE UNIT. 2L72 4F A10CE 20031118000312003111800031NM 2003 11 18 AWXA200301146 120030903A5730656964612 PANEL BOEING737 7373Q8 1384670NM RT WING TE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK THE RT WING TRAILING EDGE CLOSE-OUT PANEL CHAFED AT WBL 200. MAINTENANCE FABRICATED AND INSTALLED A REPAIR PLATE ON CLOSE-OUT PANEL AT WBL 200 IAW B737-300 SRM 51-20-01 PARA G. 2L72 4F RTA16WE 20031121000042003112100004EA 2003 11 21 03318677 120031114A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 EA27677BR 7652 DURING APPROACH TO PWM ON FLIGHT 7628 CREW RECEIVED A FLAP FAIL MESSAGE. CREW CANCELLED LANDING CLEARANCE AND PERFORMED PROCEDURES TO VERIFY THAT FLAPS HAD FAILED AT ZERO DEGREES. FLIGHT DIVERTED TO MHT AND LANDED UNEVENTFULLY. A SATISFACTORY OPERATIONAL CHECK OF THE FLAP SYSTEM WAS PERFORMED AND NO FAULTS WERE FOUND. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040112000902004011200090WP 2004 1 12 GTIA031004 120031116A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND AFT PIT STATION 1338, FRAME CORRODED BOTH SIDES AT LONGERON 22-23L, WEB WALL CORRODED ON AFT SIDE AT LONGERON 26-25R, WEB WALL AND STIFFENER AT LONG 26L. REMOVED CORROSION AT WEB AND SITFFENER AT L26L STATION 1338. MATERIAL LOSS OUT OF LIMITS. REMOVED STIFFENER, HAT. FABRICATED TWO DOUBLER. INSTALLED REPAIR AT WEB. LOCATED AND DRILLED NEW PART. INSTALLED NEW PART. (M) 2L72 4F A6WE 20040112001412004011200141NM 2004 1 12 CALA0300718 120031222A5514 FITTING BOEING737 7373T0 1384582NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 INSPECTION FOUND RT HORIZONTAL STABILIZER AFT UPPER ATTACH, FWD ATTACH LUG CORRODED AROUND BUSHING AND FACE OF LUG. REMOVED BUSHING AND FOUND CORROSION ON ID AND BOTH FACES. SPOT FACED 0.012 INCH AND REAMED BORE ID TO 1.530 INCH. FABRICATED AND INSTALLED OVERSIZE BUSHING PER SRM 55-10-10. 2L72 4F RTA16WE 20040113001062004011300106SW 2004 1 13 ALGA091409 120031209A6320 RETAINER CLARK 1000 1000CLARK 2230102SW GEARBOX BEARING DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAG70725 FOUND BEARING RETAINER RING SEPARATING FROM BEARING. RETURNED TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R 2A6 20040113002172004011300217SO 2004 1 13 C2XA03SH501 120031217A532014525137001 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040113002192004011300219SO 2004 1 13 C2XA03SH499 120031217A532014522460015 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040226000132004022600013WP 2004 2 26 ASAA0380419 120030501A33501001191 LIGHT DOUG DC9 DC983 3022083WP PAX CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01950AS380311174 53023 OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030723001312003072300131EU 2003 7 23 AWXA200300694 120030505A5320D53911609250 PROFILE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK A .25 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT SPLICE AT FR 31, RBL 28. MAINTENANCE REMOVED DAMAGED SECTION OF PROFILE AT FR 31, RBL 28; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE, AND SPLICE REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1. 2L72 4F RTA28NM 20030826001802003082600180EU 2003 8 26 VY1L110910 120030228A6520770441 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED L VY1LO OTHER O OTHER NRNOT REPORTED 1 SW194TV 274 2936 MAGNETIC SEAL CRACKING AFTER 274 HOURS. 1G71 3U3 U H9EU E19EU 20030828000392003082800039EU 2003 8 28 U30A200300017 120030619A3320350E5500202 COMPUTER AIRBUS320 A320214 3930316EU NR 2 FAULTY A U30AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA17263AV1928 1928 1860 CRUISE, ELECTRICAL SMELL ON FLT DECK & AFT CABIN. SMELL COINCIDE WITH SEATBELT SIGNS ON. TURNED SEATBELT SIGN OFF & SMELL DISSIPATES. IN CLEAR SKY, TURNED SEATBELT SIGN ON & F/A REPORTED SMELL. ON DESCENT F/A REPORT SMELL STRONGER, 2 F/A'S COMPLAINING OF NOSE BLEED & OTHER OF TIGHT CHEST. DECLARED EMERGENCY, LANDED W/O INCIDENT. MX INSPECTED & COULD NOT SMELL ODORS, POWERED UP, ENG RUNS PERFORMED & ALL SYS OPS. SMELLS NOT DUPLICATED & NO DEFECTS. ECAM MSG, NR 2 SDAC INOP. NR 2 SDAC DEFERRED. ACFT FERRIED, NO ODORS. REPLACED NR 2 SDAC & OPS CK'D OK. THE REMOVED SDAC HAD ELECRICAL ODOR. UNIT SENT FOR REPAIR & EVALUATION. PERFORMED OPS CKS OF READING LIGHT SYS, EMERGENCY PSU, VES & CIDS, NO DEFECTS. 2L72 4F RTA28NM 20030828001372003082800137EA 2003 8 28 ASOA03349 120030802A5210H341433 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 FLT 4236 - DURING A GROUND INSPECTION IN ATL, THE MAIN PASSENGER DOOR WOULD NOT OPEN FROM OUTSIDE WITH THE HANDLE. MAINTENANCE LUBRICATED THE MAIN PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030902001182003090200118GL 2003 9 2 UIAFAA9205 120030705A2910DSC252B40124 LINE BOMBDRBD700 BD7001A10 1390006GL PWA PW120 PW123 NE HYD SYSTEM LEAKING Z O OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 TW0015239 571 2123207 AFTER TAKE OFF FOUND NR 2 HYD SYSTEM QTY IND. (0), LANDING GEAR CAN NOT RETRACT; A/C LANDING AT TSA INSPECTOR NLG RETRACTION ACTUATOR FLEX HOSE FOUND LEAKING, IAW AMM32-20-16 REPLACED NLG FLEX HOSE AND REPLACED NR 2 ENG EDP ASSY IAW AMM 29-00-00AND OPERATIONAL CHECK NORMAL. 2L72 4F4 TRTT00003NYE20NE 20030902001312003090200131EU 2003 9 2 03FDEA01056 120030707A5347A5327828822401 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25659FE 757 MAIN CARGO COMPT FLOOR SEAT TRACK DAMAGED A 6 INCH CRACK IN SEAT TRACK ADAPTER AT 12R, FR 59 AND Y1456. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW EA. (6-2550-71920) REV PT 2. 2L72 4F RTA35EU 20030902001442003090200144 2003 9 2 0301266636 420030707A2330 DECODER BOEING747 747251B 1384892NM ZONE D BURNED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01636US 23547 DURING CLIMB, AN ELECTRICAL ODOR EMITTED BY DOOR 2R. AIRCRAFT DECLARED A YELLOW EMERGENCY, RETURNED TO SPN, AND LANDED WITHOUT INCIDENT. REPLACED 'D' ZONE COLUMN TIMER DECODER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030724001202003072400120NM 2003 7 24 AWXA200300676 120030506A53206916970501 ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK .1875 INCH CRACK WAS FOUND ON SIDE ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED SIDE ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-16970; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 10 & 11. 2L72 4F RTA16WE 20030728000402003072800040NM 2003 7 28 SWAA031521 120030711A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030729000052003072900005EA 2003 7 29 03198637 120030717A2613 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA NLG WW DIRTY A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27637BR 7308 DURING APPROACH, THE CREW REPORTED A MLG BAY OVERHEAT WARNING WHEN THE GEAR WAS LOWERED. MAINTENANCE PERSONNEL CLEANED AND RESEATED THE LT AND RT GEAR BAY LOOP CONNECTORS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030903001952003090300195NM 2003 9 3 AALA20030681 120030620A2421 PIN BOEING767 767323 1385205NM IDG BENT A AALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SW21384AA 26996 FOUR HOURS INTO FLIGHT R GEN DRIVE ILLUMINATED STEADY WITH GEN DRIVE EICAS MESSAGE. COMPLIED WITH QRH AND DISCONNECTED IDG. REPEAT WRITE-UP 37, 50. BPCU AND IDG PREVIOUSLY REPLACED. T/S PER FIM 24-20-00 AND WD 24-11-21 AND FOUND PINS 2 AND 8 ON IDG D10966J CANNON JACK BENT, REALIGNED THEM, RECCON AND SERVICED IDG AND RAN RIGHT ENGINE DURING 15 MINUTES WITH ALL ELECTRICAL POWER SUPPLIED BY THE RIGHT GENERATOR. BPCU BITE TEST ACC AND NO FAULTS SHOWN. RT ENGIEN GEN SYSTEM OK FOR SERVICE. (M) 2L72 4F RTA1NM 20030905000222003090500022SO 2003 9 5 LR7A03068 120030725A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND LT FS 597 'L' BRACKET CRACKED AT LBL 22, WL 285. REPLACED BRACKET IAW SRM SMP 583 51-60 AND 51-70. NR 2113. 2H74 4T A1SO 20030905001582003090500158NM 2003 9 5 DL76K030672 120030718A3397 WIRE BOEING767 767332 1382001NM CABIN SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27171DZ 29690 IRREG FIRST CLASS EMERG LIGHTS INOP. REPLACED BATTRY PACK M736-READS 2 VOLTS-NO HELP. FOUND SHORT AT/BELOW SEAT 1E REPAIRED WIRING TESTS OK. 2L72 4F RTA1NM 20030904001582003090400158WP 2003 9 4 DHL2003873575 120030708A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING OTBD FLAP LOWER AFT PLATING HAS AN INTERIM REPAIR FROM STA XF 415.000 TO XW.408.000. PERFORMED MAJOR REPAIR IAW EODHL-030609, ED-3429. REMOVED THE EXISTING DOUBLER AND FASTENERS IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL IAW EODHL-030609,ED-3429. CLEANED, TREATED AND PRIMED THE NEW SKIN PANEL INTERIOR SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN PANEL ON LT WING OTBD FLAP LOWER AFT PLATING (STA XF415.000 - XW 408.000) USING NEW FASTENERS IAW EODHL-030609, ED-3429, SRM 51-1-21 PG 1 AND SRM 51-1-21A PG 3. 2L74 4F RT4A25 20030814001102003081400110NE 2003 8 14 RAIA00306166 220030618A7200TPE33114GR ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LEFT FAULTY A RAIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CE03561HK13077 41077 75093 LT ENGINE LOW TORQUE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. 2L72 4T4 TRTA41NM E18NE 20030821002192003082100219NM 2003 8 21 03FDEA00810 120030523A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP - HINGE AFT FITTING FOUND INBOARD PIVOT BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69255 - WINGS - RIGHT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030825001452003082500145WP 2003 8 25 GTIA030598 120030725A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FORWARD CABIN STATION 200-256 RIGHT SIDE OUTBOARD WEB PANEL, PNENOLIC, HAS DISBONDED AT HAT SECTION AND MISSING HAT SECTION 55 INCHES. FABRICATED NEW SECTION OF HAT. INSTALLED NEW SECTION OF HAT CHANNEL. (M) 2L72 4F RTA6WE 20030729000572003072900057NM 2003 7 29 QXEA200300882 120030718A6123 POTENTIOMETER DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS OUT OF ADJUST A QXEAK NONE O OTHER TOTAKEOFF 1 NM09364PH 524 PDX- ON FLIGHT 2147 AUTOFEATHER "ARM" LIGHT CAME ON DURING TAKEOFF AT 95 PERCENT TORQUE AND 70 KIAS. PERFORMED AUTOFEATHER ARMING POTENTIOMETER ADJUSTMENT TEST IAW RIGGING MANUAL 7-31. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030822001562003082200156NM 2003 8 22 QXEA200300946 120030731A5330 PAINT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX- PAINT SCRAPED FROM FUSELAGE SKIN 6 INCHES FROM LOWER AFT CORNER OF SERVICE DOOR. REPAIRED IAW HORIZON AIR EA 6-53-289. 2H72 4T RTA13NM 20030825000032003082500003NM 2003 8 25 UPS03540950 120030702A5753113N2800 FLAP BOEING757 75724APF 1384969NM LT WING DAMAGED A IPXAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SO01458UP 25479 INSPECTION TYPE:ARSV ON ARRIVAL SERVICE WALK INSP, FOUND LEFT INBOARD AFT FLAP PUSHROD BROKEN, PRECING THROUGH THE INBOARD CANOE FAIRING. I/B TE FLAP APPEARS TO HAVE STRUCTURAL DAMAGE. R&R AFT I/B TRAILING EDGE FLAP IAW MM 27-51-02, ADJUSTMENT OAN TEST CA RRIED OUT PER 27-51-02. I/B TE FLAPS CHECKS OUT OK. 2L72 4F RTA2NM 20030827001052003082700105NM 2003 8 27 CALA0300418 120030727A5320 STIFFENER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND BULKHEAD CENTER CHANNEL STIFFENER AT BOTTOM RT SIDE, STA 1016 CORRODED. A REPAIR WAS INSTALLED IAW DRAWING 65C28106-1 AND EA 5310-04045, OP2. 2L72 4F RTA16WE 20030909001462003090900146CE 2003 9 9 S2YA03014 120030416A24371143800311 METER BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA COCKPIT INACCURATE A S2YAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL1379SK 422 UE79 DURING FLIGHT 1075, THE CREW DISCOVERED A SPLIT BETWEEN THE DC LOAD METERS, LEFT HAD 17 PERCENT AND THE RIGHT HAD 45 PERCENT. THE CREW CONSULTED WITH MECHANIC AND MADE AN AIR TURNBACK. MECHANIC INSPECTED THE SYSTEM, SWAPPED THE METERS AND DETERMINED THE LEFT METER WAS DEFECTIVE. MECHANIC REPLACED THE METER AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T3 TRTA24CE E2NE 20030911001602003091100160WP 2003 9 11 AALA20030331 120030225A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 FOUND CORROSION NR 3 SEAT TRACK. BLENDED AND ROUTED OUT CORROSION ALODINE AND PRIMED INSTALLED PLUG REPAIR PER 53-05-00 AND AARD 53-20-00-10 51-10-3 AND PAINTED. (M) 2L72 4F A6WE 20030926000222003092600022GL 2003 9 26 0067538 320030821A6110D50172 LATCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MCAULY5JFR C5JFR36C1104GL PROPELLER CRACKED B EY2RO OTHER O OTHER NRNOT REPORTED 1 GL03 960663 960663 CRACK ON LATCH PAWL. 2L72 4T3 TRTA41NM E2WE 5 CP15NE 20030929001012003092900101EU 2003 9 29 MALA030402 120030904A2750 CONTROL UNIT BAC 146 AVRO146RJ85A1500097EU TE FLAP INOPERATIVE A MALAO OTHER O OTHER LDLANDING 1 GL15512XJ E2326 UPON SELECTION OF FLAP 18 THERE WAS NO FLAP MOVEMENT AND A FLAP FAULT LIGHT CAME ON. FLAPS STAYED AT ZERO DURING LANDING. BRAKE TEMP WAS KEPT BELOW 400C. DID A FLAP RESET AND PERFORMED A FLAPLESS LANDING INSPECTION. ALL CHECKS GOOD. 2H74 4F RTA49EU 20030930000852003093000085WP 2003 9 30 ABXA030348 120030815A533059114123 SKIN DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 BULGE IN FUSELAGE SKIN, CUPPED OR BROKEN FASTENERS, FS 332, LONGERON 30. REPLACED DAMAGED AREA IAW DC-9 SRM. 2L72 4F A6WE 20030930001142003093000114NM 2003 9 30 03FDEA01487 120030907A5754 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 LT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB CRACKED. LT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. 2 & SRM 51-35-01 VOL. 2. 2L73 4F RTA22WE 20031001000202003100100020NM 2003 10 1 QXEA200301081 120030826A5330 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CHAFING UNDER PANELS 262LT, 262UT, AND 262AT ON FORWARD SIDE OF FUSELAGE APERATURE. REPAIRED IAW DHC-8 SRM RD 8-57-1434. 2H72 4T RTA13NM 20031002001232003100200123NM 2003 10 2 QXEA200301107 120030827A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 NR 1 SEAT TRACK BOTTOM OF CHANNEL IS LIGHTLY SCRATCHED ONE INCH FORWARD OF STATION X312. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031021002622003102100262NM 2003 10 21 03FDEA01591 120030919A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CORROSION ON FLOOR BEAM B/S 312, LBL 42. 2L73 4F RTA3WE 20030909001242003090900124SW 2003 9 9 ALGA088784 120030818A5320206064902035S CHANNEL BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL6498 53240 CHANNEL CRACKED LOWER EDGE AND MIDDLE CHANNEL. PROBABLE CAUSE IS ASB407-02-54. REC. DOUBLERS AT RECEPTICALE AREAS. 1G71 3U3 UO H2SW E1GL 20031110001552003111000155NM 2003 11 10 03FDEA01855 120031021A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 LT WING INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT BORE FOUND CORROSION. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5750-73337, 2L73 4F RTA22WE 20031120001072003112000107NE 2003 11 20 QXEA200301273 220031011A73204120T00P15 COMPUTER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 MALFUNCTIONED A QXEAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 NM09615QX2531 2531 10065 965361 ON FLIGHT 2447 RECIEVED MOMENTARY WHITE (LEFT FADEC FAULT 1) MESSAGE FOLLOWED ABOUT ONE HOUR LATER WITH YELLOW (LEFT ENGINE FLAMEOUT) AND GREEN (LEFT AUTO IGNITION) MESSAGE UPON RETARDING THROTTLES AT TOP OF DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED DIGITAL ENGINE COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040204000492004020400049WP 2004 2 4 UPS03841383 120030922A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 STATION 320 TO 418 SEAT TRACK IS WORN BEYOND LIMITS AT LBL 45 REMOVED SEAT TRACK SECTION BETWEEN STA. 310-590,FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC8-5320-8309 APPX. B 2L74 4F RT4A25 20040212000712004021200071NM 2004 2 12 HNAA0300078 120031121A531385300130101 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07914HA 53 CORROSION ON STR SPLICE AT STR 32S AND FRAME X351. 2H72 4T RTA13NM 20031103000802003110300080WP 2003 11 3 UPS03841348 120031002A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. OPS CHECK GOOD EAW MM CH 33. S/N ON UP03889, S/N OFF 255, P/N ON 60-1223-5. 2L74 4F RT4A25 20031028001482003102800148NM 2003 10 28 GAIA03096 120030910A5315 FLOORBEAM BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND FORWARD LAVATORY FLOORBEAM UPPER 'T' CORRODED BS 344 RBL 25 TO RBL 50 ALSO AT LBL 25. REF FASI N/R 53195, REPLACED FLOORBEAM UPPER 'T' CAP RBL 60 TO LBL 60 PER B77 53-10-8 FIG 3 AND 51-30-2. (M) 2L73 4F A3WE 20040212001502004021200150CE 2004 2 12 XVQ2003F00000 120031120A322212170875 BEARING CESSNA210 210M 2073450CE CONT O520 IO520* 17032SO MCAULYD3A34 D3A34C401 GL NOSE GEAR FAILED E XVQAO OTHER O OTHER NRNOT REPORTED 1 SO17823AR 21062661 295138R 002242 AIRCRAFT WAS FORCED TO MAKE A GEAR UP LANDING, DAMAGING PROP AND ENGINE. THE CAUSE WAS FOUND TO BE THE FAILURE OF A BEARING/WHEEL ASSEMBLY THAT ACTUATES THE NOSE GEAR DOORS CLOSING MECHANISM. THE BEARING FAILED ALLOWING THE WHEEL PORTION TO SHIFT OUTBOARD EXPOSING THE ATTACHING BOLT WHICH WAS NOW STRIKING THE SIDE OF THE NOSE GEAR FORK. THIS BOLT JAMMED THE FORK IN THE UP POSITION. IF THE ASSY WAS DESIGNED WITH A LARGE AREA WASHER INSTALLED INBOARD AND OUTBOARD OF THE BEARING THE WHEEL WOULD NOT SHIFT IF BEARING FAILED. 1H71 3O3 O 3A21 E5CE 5 CP47GL 20031112001162003111200116WP 2003 11 12 ABXA030427 120031027A523059101415 PAN DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 FORWARD LOWER CARGO DOOR PAN WAS CRACKED AT AFT LOWER STOP. FORWARD LOWER CARGO DOOR WAS REPLACED ON JC 0314 IAW DC-9 MM. 2L72 4F A6WE 20031117000362003111700036EA 2003 11 17 QXEA200301219 120031004A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 FORWARD BAG PIT CHIMNEY AT ENTRANCE OF DOOR WAY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20031107001572003110700157NM 2003 11 7 ASAA0310446 120030515A5730654641917 SKIN BOEING737 737290C 138448VNM LT WING WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STATION 360 WORN. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20040112001752004011200175NM 2004 1 12 2003UALA00969 120031218A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STA 887 STRINGER 8L HAS A CRACKED SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20040112001872004011200187NM 2004 1 12 03FDEA02229 120031223A5744 HINGE FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING INBD FLAP OUTBD HINGE FITTING OUTBD PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75212, TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113001142004011300114EU 2004 1 13 BAQA089830 120031113A6240117945661 INDICATOR BOLKMS117 BK117B1 5626012EU MAST MOMENT ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 INDICATOR WILL NOT GO FULL SCALE DEFLECTION, AND FLUCTUATES ERRATICALLY. REPLACED WITH SERVICEABLE UNIT. 11/18/03 1G72 3U H13EU 20031120000982003112000098WP 2003 11 20 ABXA030393 120031013A32607000010101ABX WARNING SWITCH DOUG DC9 DC931 3022065WP MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23946AX3530 47003 ON FINAL APPROACH, GEAR WENT DOWN AND GEAR DOOR OPEN LIGHT WENT OUT. AT 400 AGL, GEAR DOOR OPEN LIGHT CAME BACK ON. DID MISSED APPROACH. CYCLED THE GEAR EARLY FOR SECOND APPROACH. ON FINAL FOR SECOND APPROACH, GEAR DOOR OPEN LIGHT CAME BACK ON. FOLLOWED ABNORMAL AND PULLED EMERGENCY GEAR EXTENSION HANDLE. LANDED STRAIGHT AHEAD ON RUNWAY AND STOPPED IAW ABNORMAL WITHOUT INCIDENT. REMOVED AND REPLACED MAIN GEAR DOOR POSITION SWITCH. OPS CHECKED GOOD AT THIS TIME IAW DC-9 MM 32-60-03-2-0101. 2L72 4F A6WE 20031124000822003112400082WP 2003 11 24 DHL2003805549 120030728A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 791.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO N/R 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20040115001072004011500107NM 2004 1 15 03FDEA02083 120031207A5340 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 1 BANJO FITTING (AJC7051-505) LOWER CORNER OF FWD FACE ATTACHED ANGLE FOUND WITH A HAIRLINE CRACK MEASURED APPROX 0.5 INCH. NDT - HFEC CARRIED OUT ON ANGLE AT RT CENTRE SECTION OF NR 1 BANJO FITTING LOWER CORNER FWD FACE AND FOUND ANGLE CRACK FREE. 2L73 4F RTA22WE 20031212000222003121200022NM 2003 12 12 SWAA032418 120031031A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STRINGER CLIP AT 10L, BS 663. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20031216000842003121600084NM 2003 12 16 SWAA032580 120031120A53306552880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20031217000182003121700018EA 2003 12 17 03325689 120031121A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27689BR 7737 DURING INSPECTION THE AFT EMERGECNY TRACK LIGHTING STRIP WAS FOUND INOPERATIVE. THE LIGHTING STRIP WAS IDENTIFIED AS THE CAUSING THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031215001392003121500139WP 2003 12 15 AALA20031120 120031004A3350BPS73 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21576AA 53153 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031218000102003121800010NM 2003 12 18 MWEA030453 120031125A53459936534183 CHANNEL DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CORROSION FOUND J-CHANNEL FRAME STATION 160-200, EIGHTEEN INCHES INBOARD OF FORWARD GALLEY SERVICE DOOR. FABRICATED AND INSTALLED NEW J-CHANNEL. 2L72 4F RTA6WE 20030917000582003091700058CE 2003 9 17 DXTA200300114 120030912A2720 WARNING LIGHT CESSNA750 750 2076810CE YAW DAMPER ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07931QS 7500064 DURING TAKE OFF "YAW DAMPER LOWER-OFF" CAS MESSAGE CAME ON, ABORTED TAKE OFF. - PURGED OUT PITOT TUBES FOR WATER AND DEBRIS, COMPLIED WITH YAW DAMPER OPS CHECK AND PITOT STATIC SYSTEM LEAK CHECK IAW CESSNA 750 MM CHAPTER 27-24-00 & 27-20-00 AND FAR 91.411. 2L72 4J RTT00007WI 20030918000842003091800084 2003 9 18 CYO2003F00000 420030716A34516222175001 INDICATOR LEAR 25 25B 5170511CE GE CJ610 CJ610* 30006NE DME SHORTED B CYOVO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW05140CA 140 AIRCRAFT WAS ENROUTE FROM BRO TO LIT. FLIGHT CREW EXPERIENCED SLIGHT SMOKE AND A BURNING ODOR, THEY THEN DIVERTED TO SHV. MAINTENANCE CREW INSPECTED AND FOUND DME INDICATOR SHORTED INTERNALLY. 2L72 4J4 J A10CE 1E16 20040106000032004010600003WP 2004 1 6 DHL2003802571 120031203A5730 SKIN DOUG DC8 DC873 302199CWP RT WING DELAMINATED I DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING CENTERWING 723 PANEL LOWER SKIN DELAMINATED STA 742.000. REMOVED AND REPLACED NR 723 PANEL ASSY ON RIGHT WING CENTERWING, STA 742.000 IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040112000182004011200018WP 2004 1 12 AALA20031239 120031108A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21513AA 49890 DURING OVERNIGHT MAINTENANCE, FOUND TAIL COMPARTMENT CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED TAIL COMPARTMENT CEILING EMERGENCY EXIT LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031125000712003112500071WP 2003 11 25 DHL2003805604 120030820A2780 SHAFT DOUG DC8 DC873F 302199FWP L/E SLOT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT OTBD SLOT TORQUE TUBE CRANK CRACKED. REMOVED TORQUE TUBE IAW OHM 27-37-6 PG 2. REMOVED AND REPLACED CRANK ASSY IAW SRM 51-1-21 PG 1. REINSTALLED TORQUE TUBE ON RIGHT OTBD SLOT IAW OHM 27-37-6 PG 2, 3, 4. FOR OPS CHECK SEE N/R 1896. 2L74 4F RT4A25 20031126000962003112600096SO 2003 11 26 C2XA03SH453 120031112A532014522226003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE LEFT AND RIGHT OMEGA BEAM BUTTSTRAPS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAPS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040121000852004012100085EA 2004 1 21 A6WA200340197 120031220A2750 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A A6WAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL31441ZW 7777 UNCOMMANDED FLAP ACTUATION IN FLIGHT AT CRUISE 0-6 DEGREES WITH FLAP SETTING ZERO ALL OTHER SETTINGS NORMAL OPERATION. REMOVED AND REPALCED FECU AND FLAP HANDLE. (M) 2L72 4F RTA21EA 20040122000882004012200088EU 2004 1 22 2004F00040 120031210A282031080511 LINE BAG JETSTMJETSTM3101 1500215EU FUEL SYSTEM CHAFED A B16AK NONE K FLUID LOSS ININSP/MAINT 1 NE05539PA 741 FUEL FOUND LEAKING FROM LT ENGINE AFTER SHUTDOWN. VISUAL INSPECTION, FOUND CHAFED LINE. FUEL LINE REPLACED ON NR 1 ENGINE IAW J-31 AMM 20-10-00. VISUAL LEAK CHECK CARRIED OUT IAW J-31 AMM 51-11-00. FOUND SERVICEABLE P/N 3108051-1, ALSO FUEL FLEX LINE ON NR 1 ENGINE IAW J-31 AMM 20-10-00, P/N 1379305-A119. (M) 2L72 4T RTA21EU 20040122000952004012200095EU 2004 1 22 ASOA03634 120031207A33503011210 LIGHT AEROSPATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING HANGAR MANITENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031204001142003120400114WP 2003 12 4 UPS03841432 120030925A531325972422 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, LONGERON 6R STA 12 HAS CORROSION ON FLANGE. REMOVED CORR OUT OF LIMITS IAW DC8 SRM 51-1-8 & 53-2-0. MAT ID PO 409830 .2 7075-T6.050 IAW REO G09499 PG 4. FABBED REPAIR DOUBLER IAW REO G0949 9, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO G09 499 AND DC8 SRM 51-1-20D. 2L74 4F RT4A25 20031209002002003120900200EA 2003 12 9 SWIA200312504 120031010A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621.0; RBL 43.0. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV A AND RII 53-401. P/N: 601R53-61-117-2. 2L72 4F4 FRTA21EA E15NE 20031209002092003120900209 2003 12 9 SWIA200312559 420031025A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07433SW 7550 DURING STALL TEST, SHAKER DOES NOT ACTIVATE. REPAIRED BROKEN WIRE IAW CL 600 WDM 20-00-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20031014000402003101400040EU 2003 10 14 AWXA200301064 120030909A5320D5347112420100 WEB AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF RT AFT WEB (SHEAR PLATE), FORWARD SIDE OF FR 70, JUST BELOW CABIN FLOOR PANEL. MAINTENANCE REMOVED CORRODED SHEAR PLATE BETWEEN FR 69 AND FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG A20-A24, FIG 59 AND PG A23, FIG 60. 2L72 4F RTA28NM 20030922000612003092200061NE 2003 9 22 MALA030369 220030804A7220 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FLAMED OUT A MALAEC ENGINE SHUTDOWN ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 GL15410XJ 340B410 ON TAKEOFF OF FLIGHT NR 2932, AT APPROXIMATELY 80 KNOTS LT ENGINE FLAMED OUT. CREW HEARD A LOUG BANG, FA WITNESSED A LARGE FLAME FROM LT ENGINE EXHAUST PIPE. FLIGHT WAS ABORTED AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ASSEMBLY PN CT7-9B SN/OFF GE-E785746 SN/ON GE-E785718, AND PGB ASSEMBLY PN 5074T51G10 SN/ON IHI00343, SN/OFF IH100567. 2L72 4T4 TRTA52EU E8NE 20030923000682003092300068WP 2003 9 23 DHL2003604789 120030608A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 EXTERNAL FUSELAGE SKIN CRACKED 0.450, STA 1160.000 BETWEEN L-26R AND L-28R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030555, ED-3311. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030555, ED-3311. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6 AL0.125) AND DOUBLER (7075-T6 AL0.125) IAW EODHL-030555, ED-3311. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL-030555, ED-3311, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030924000292003092400029NE 2003 9 24 DL76L030737 220030809A73218010003 FUEL CONTROL BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE SURGES A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO27194DN 28451 724691 3 HRS INTO FLT LEFT ENG STARTED SURGING LEFT EPR CYCLES. BETWEEN 1. 20 - 1.23 N1 CYCLES WITH THROTTLES RETARDED 80.5 TO 81.8 ALL OTHER ENG PARMETERS CYCLING IN SIMILAR RANGE FLT LEVEL 320 TRYED ALT EEC BUT NO HELP HAD NO EFFECT FUEL FUEL FLOW 4520-4650 STABILIZED AT 13K FEET - REPLACED FUEL METERING UNIT. 2L72 4F4 FRTA1NM E24NE 20040217001202004021700120NM 2004 2 17 DHL200374259 120031124A5347BAC1520792 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742 21290 DURING (C) CHECK; DISCREPANCY IS AS FOLLOWS NR 60134; UPPER FUSELAGE LBL 42 INCHES, BS 380 SEAT TRACK IS DAMAGED CA ;DAMAGED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG.3 REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW PN 1520-792 PO NR 900203 DIM.135 .2500 LONG IAW 727 SRM 53-10-5 FIG 7. 2L73 4F A3WE 20040309001592004030900159WP 2004 3 9 GTIA031056 120031117A5230 SUPPORT FITTING DOUG DC9 DC981 3022081WP CARGO DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND AFT CARGO DOOR CRACKED ANGLE SUPPORT UPPER AFT SIDE. REMOVED CRACKED ANGLE SUPPORT. INSTALLED NEW ANGLE SUPPORT FITTING. (M) 2L72 4F A6WE 20031212001672003121200167WP 2003 12 12 AALA20030920 120030831A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217534A 49988 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY LIGHT WAS INOPERATIVE IN TAILCONE AND AFT CABIN CEILING. REPLACED BATTERY PACK B-5-27. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040802000582004080200058NM 2004 8 2 ASAA0340361 120031213A532065479573 MEMBRANE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01713AS 30161 OAK - DUIRNG C-CHECK, FOUND BILGE DOOR MEMBRANE CORRODED ON TOP SIDE IN MULTIPLE LOCATIONS. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20050202000542005020200054NM 2005 2 2 0704007 120031007A57306550820285 PANEL BOEING737 737230C 1384472NM LT WING DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 L MLG T/E UPPER FIXED PANEL DELAMINATED ON UPPER AND LOWER SKIN. 2L72 4F A16WE 20050222002632005022200263GL 2005 2 22 ERAA097115 220031112A72306851574 SCROLL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE BROKEN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03131EH 595 BROKEN STUDS ON SCROLL. OVERHAUL, INSPECTED, WELD REPAIRED CRACK, INSTALLED (24) EACH NEW STUDS, STRESS RELIEVED, REPLACED (2) EACH INSERTS, AND APPLIED. 1G72 3U3 U H3EU E4CE 20030820001172003082000117NM 2003 8 20 UPS03M40990 120030722A3350 LIGHT DOUG MD11 MD11F 3023600NM CABIN WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01270UP INSPECTION TYPE:N/A EMERGENCY LIGHT TEST FAIL. PLACED ON DFRL M263353. OPS TESTED GOOD PER FIM 33/51/02. THIS CLEARS DFRL M263353. 2L73 4F RTA22WE 20030819001952003081900195SO 2003 8 19 SWIA200312206 120030716A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07214SW5967 5967 120280 EMERGENCY LIGHTS IN ROW 9 COME ON MOMENTARILY AND THEN GO OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4 IAW MM 33-50-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20030331000162003033100016EA 2003 3 31 A6WA200340022 120030106A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 HYDRAULIC BRACKET AT FS 656 RT SIDE AT STRINGER 9 HAS AN ELONGATED THRU HOLE AT HYDRAULIC PRESSURE LINE REMOVED BRACKET, REPAIRED, AND REINSTALLED. PERFORMED NDT WITH NO INDICATIONS NOTED. 2L72 4F RTA21EA 20030331000422003033100042WP 2003 3 31 AALA20030189 120030209A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 SAN - DURING OVERNIGHT MAINTENANCE, AFT HALF OF SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030821001472003082100147NM 2003 8 21 03FDEA00883 120030616A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25492FE 21530 CORROSION (C53-100-01) IN RT MLG WHEEL WELL ON UPPER SURFACE OF STRINGER 18A SHELF FROM BS 900 TO BS 940. 2L73 4F RTA3WE 20030401001712003040100171WP 2003 4 1 DHL2003804781 120030212A5730570551849 SKIN DOUG DC8 DC873F 302199FWP ACCESS DOOR DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING LOWER ACCESS DOOR NR 540 WITH EXTERNAL SKIN DELAMINATED. R & R LT LOWER EXTERNAL ACCESS DOOR NR 540 IAW SRM 51-3-0 PG. 1 2L74 4F RT4A25 20030408000282003040800028SO 2003 4 8 SIMA200302701 120030122A335020131A POWER SUPPLY EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21707EB 145195 BOS - FLT 4644 - CREW REPORTED LEFT ESCAPE HATCH EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A POWER SUPPLY UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030410000742003041000074NM 2003 4 10 SWAA030650 120030320A2560PH22300L STRIP BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 6 & ROW 7 ABC. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20030410001402003041000140NM 2003 4 10 SWAA030694 120030326A5523BACB28AM07 BUSHING BOEING737 7373TO 138447GNM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C3 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR INBD TAB HINGE HARDWARE AND BUSHING PER MM. 2L72 4F RTA16WE 20030404000752003040400075NM 2003 4 4 DL764030079 120030122A3350D71701100 BATTERY BOEING767 767432ER 1385134NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27844MH 29717 EMERGENCY LIGHT BATTERY PACK INOP. REPLACED BATTERY PACK. 2L72 4F RTA1NM 20030410002402003041000240NM 2003 4 10 DL76L030102 120030128A28207G1018 PRESSURE SWITCH BOEING767 767332 1382001NM NR 2 ENGINE FAULTY A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27185DN 27961 LEFT AFT BOOST PUMP LIGHT ILLUMINATED IN FLT. REPLACED LEFT AFT BOOST PUMP PRESSURE SWITCH AS PER M/M, OPS CHECKS OK. 2L72 4F RTA1NM 20030408001202003040800120NM 2003 4 8 377PA0012 120030329A3350 LIGHT BOEING737 7373L9 1384470NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05377PA 23718 EMERGENCY LIGHTS INOPERATIVE, 20 AFT. CLEANED STRIP CONNECTIONS AT AFT END FROM MOISTURE/WATER. LIGHTS CHECK, OK, IAW MM 33-50-00. 2L72 4F4 FRTA16WE E2GL 20030422000182003042200018WP 2003 4 22 GTIA030122 120030301A3231 DOOR DOUG DC9 DC982 3022082WP NLG OPEN A GTIAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 GL23823NK 48020 DEN - FLT 980 - UPON ROTATION AND GEAR UP, ENCOUNTERED VIBRATION IN NOSE WHEEL AS IF DOOR STAYED OPEN. ON TAXI, IN RIGHT NOSE GEAR DOOR WAS OPEN. INSPECTED NOSE GEAR DOOR, LINKAGES/STRUT/TORQUE LINKS. NO DEFECTS NOTED. TESTED NOSE GEAR DOOR LOCKS BY PULLING ON IT, THEY REMAINED LOCKED. NO DEFECTS NOTED, OK TO CONTINUE. (M) 2L72 4F A6WE 20030422000942003042200094SO 2003 4 22 SIMA200307902 120030222A532014521718003 ANGLE EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING A IMBV INSPECTION LT BEAM RAMP ANGLE IS CORRODED AT FRAME 19-20. REMOVED AND INSTALLED NEW BEAM RAMP ANGLE IAW EMB 135 SRM 51-20-01, 51-20-03, 51-40-02 AND 51-40-04. (M) 2L72 4F RTT00011AT 20030424001082003042400108WP 2003 4 24 IXXA0300028O 120030320A3260 PROXIMITY SENSOR DOUG DC8 DC873F 302199FWP MLG DOOR FALSE INDICATIONA IXXAO OTHER J WARNING INDICATION TOTAKEOFF 1 SW11602AL91695374 45991 AFTER TAKEOFF FROM KLAX TO KTOL DOOR NOT LATCHED LIGHT REMAIN ILLUMINATED. GEAR WAS RECYCLED TWICE WITH NO CHANGE. UP LATCH CHECK WAS SATISFACTORY. INSPECTION IS ON GOING. ADDITIONAL INFORMATION WILL BE PROVIDED AS IT BECOMES AVAILABLE. AFTER INSPECTION OF AIRCRAFT MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR NOT LATCHED PROXIMITY SWITCH AND PROXIMITY SWITCH STRIKER. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DOUGLAS AIRCRAFT MAINTENANCE MANUAL. 2L74 4F RT4A25 20030424001362003042400136NM 2003 4 24 F3LA200300112 120030228A5730 SKIN BOEING737 7373Q8 1384670NM RT WING CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03318FL 2093 26293 DURING EXIT CHECK, INSPECTION REPORTED RT WING LE SKIN PANEL CRACKED AT WBL 324. FABRICATED AND REPAIRED SKIN PANEL PER SRM 51-70-5, REPAIR 7 AND SRM 51-70-11, FIGURE 1. 2L72 4F RTA16WE 20030425001082003042500108NM 2003 4 25 DLM90030216 120030303A2910 LINE DOUG MD90 MD9030 3023690NM LT MLG WW CRACKED A DALAO OTHER K FLUID LOSS CLCLIMB 1 SO27906DA 53386 RT SYS HYD PRESS DROPPED TO 0 PASSING APPROX 18K QTY ON RT SIDE WENT UP TO 27 QTS. RAN CHECKLIST. WHEN RT ENG PUMP WAS OFF WITH AUX PUMPS ON, PRESS ON RT SIDE WENT FROM 0 TO 700 PSI. THE LT PRESS WENT FROM 3000 TO 2800 PSI. AUX PUMPS AND RT ENG PUMPS NOW IAW CHECKLIST. MTC FOUND CRACKED LINE IN LT W/W, REPLACE LT RESERVOIR AND ENGINE DRIVEN PUMP. 2L72 4F RTA6WE 20030502000432003050200043WP 2003 5 2 ASAA0380155 120030224A532199365441 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030501002032003050100203NM 2003 5 1 ASAA0310036 120030225A532065319601 PAD BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, STANSION PAD AT BS 520, RIGHT BUTTOCK LINE 55 CORRODED. REMOVED AND REPLACED STANSION PAD PER SRM. (M) 2L72 4F RTA16WE 20030505000972003050500097NM 2003 5 5 PCA0300842 120030410A5230 SKIN BOEING747 747249F 1384849NM CARGO DOOR GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 AFT CARGO DOOR DEEP GOUGE 12 INCHES BELOW MASTER LATCH HANDLE. REPAIR SRM 51-40-01. 2L74 4F A20WE 20030505001642003050500164NM 2003 5 5 03FDEA00464 120030416A5414 SKIN BOEING727 727200 138407ENM NR 3 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE NACELLE INBOARD SKIN CHAFED AND CRACKED 1 INCH LONG. *S/D* REMOVED AND REPLACED DAMAGED LONGERON IAW BOEING 727-200 51-30-02. 2L73 4F RTA3WE 20030506000612003050600061NM 2003 5 6 03FDEA00649 120030429A5711 SPAR DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING FOUND REAR SPAR LOWER CAP WITH CORROSION AT XORS 1090. 2L73 4F RTA22WE 20030507000262003050700026NE 2003 5 7 AUS20030329 120030317A32465003488 WHEEL SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 751 (AUS) NOSE WHEEL HALF CRACKED AT INSIDE BEAD AREA. CRACK LENGTH 85MM(3.34IN). CRACK HAD NOT PROPAGATED COMPLETELY THROUGH THE WHEEL AND WAS NOT VISIBLE FROM THE OUTSIDE AND WAS FOUND WHEN THE WHEEL WAS DISASSEMBLED FOR A TYRE CHANGE. 1G72 3U3 UNCH1NE E19EU 20030508000082003050800008NM 2003 5 8 QXEA0300526 120030501A5210 BUSHING BOMBDRDHC8 DHC8401 1390041NM ZONE 800 WORN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09406QX3982 4048 PDX - FLIGHT 388 - CREW REPORTED THE MAIN CABIN DOOR WAS JAMMED AND WOULD NOT OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED A BUSHING ON THE LEFT STRUT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030507002122003050700212NM 2003 5 7 CH1A200395014 120030409A5320 ANGLE BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 ANGLE BETWEEN STA. 1030 AND 1050 STR 27R CORRODED 2L73 4F A3WE 20030530001152003053000115CE 2003 5 30 CA030508002 120030416A3397L139A22L139B22 WIRE HARNESS BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA STA. 278.5-176, BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA 11184 (CAN) DURING ROUTINE MAINTENANCE, CABIN BEGAN TO FILL WITH SMOKE. A/C POWER WAS DISCONNECTED & A SEARCH WAS CONDUCTED TO LOCATE THE SOURCE. IT WAS FOUND THAT THE PASSENGER COMPARTMENTENTRANCE LIGHTING SYSTEM WAS AT FAULT. WIRE HARNESS W185 HAD CHAFFED ON THE AIRCRAFT STRUCTURE IN T HE CABIN DOOR UNDER FLOOR AREA AND SHORTED TO GROUND. THE INSULATION ON WIRES HAD MELTED AWAY CAUSING THE SMOKE IN THE CABIN. AN INSPECTION OF THE ENTIRE WIRE BUNDLE FROM HOT BATTERY BUSS IN THE RIGHT WING ROOT THROUGH THE AIRCRAFT FUSELAGE TO THE CABIN DOOR AREA REVEALED SEVERAL SCORCHED WIRES. THESE WIRES WERE REPAIRED AS NECESSARY. 1L72 4T4 T A24CE E4EA 20030605000072003060500007EU 2003 6 5 AUS20030432 120030409A5341 BOLT BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT WING ATTACHMENT LUG MOUNT BOLTS (3 OFF) CORRODED. LT WING ATTACHMENT LUG MOUNT BOLT HEAD DISLODGED. FOUND DURING INSPECTION IAW AD/BAE146/052 AMDT1. 2H74 4F4 F A49EU E6NE 20030521001042003052100104WP 2003 5 21 DHL2003801051 120030405A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 MAIN CARGO COMPT NR 6 TRACK LUGS WORN IN MANY POINTS, STA 1553.000 - STA 1593.000 (40.000). CUT OUT DAMAGED TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SPLICE (7075-T6 0.100). CLEANTED, TREATED AND PRIMED SPLICE IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICE ON NR 6 TRACK IAW SRM 53-2-3 PG 49-50. 2L74 4F RT4A25 20030612001552003061200155WP 2003 6 12 UPS03840744 120030513A5510 CAP DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, RT HORZ STAB INBOARD BOX LOWER CAP CRACKED. REMOVED RT HORZ LEADING EDGE CAP LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20030522000592003052200059WP 2003 5 22 0300899610 120030505A213039613011 VALVE DOUG DC9 DC932 3022066WP RT PACK INOPERATIVE A NWAAB EMER. DESCENT S AFFECT SYSTEMS DEDESCENT 1 GL01610NW 47432 ON DESCENT BUT LEVEL AT FL240 THE CABIN ALTITUDE AND MASTER WARNING LIGHTS ILLUMINATED. CABIN CLIMBED AT 1500 FPM AND EMERGENCY DESCENT WAS INITIATED. CABIN MASKS DEPLOYED DURING THE RAPID DESCENT TO 11,000 FEET YET CABIN ALTITUDE NEVER INDICATED OVER 12,000 FEET. CREW REGAINED CONTROL OF CABIN PRESSURE AND WARNING INDICATIONS EXTINGUISHED. LANDING AT VPS WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 PACK FLOW CONTROL VALVE BAD AND RIGHT HEAT EXCHANGER SEAL LEAKING. REPLACED BOTH AND CLEARED ALL FAULTS ON THE PRESSURE CONTROLLERS AND BITE CHECKED THEM AGAIN. 2L72 4F A6WE 20030527000072003052700007WP 2003 5 27 DHL2003604524 120030429A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING INBOARD L/E FORMER AT STA XFS 591.250 WITH 0.500 INCH CRACK. STOP DRILLED CRACK AT STA XFS 591.250 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030617002252003061700225EA 2003 6 17 QXEA200300695 120030531A5230 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 CKB - CARGO DOOR FORWARD EDGE FRAME IS SCRATCHED AND GOUGED. REPAIRED IAW CRJ 700 SRM 51-25-00. 2L72 4F RTA21EA 20030617002092003061700209SW 2003 6 17 HEEA087308 120030611A6420 BEARING BELL 407 407 1182206SW T/R HUB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH4233 53198 53209 WORN FLAPPING BEARINGS. REPAIRED. 1G71 3U O H2SW 20030528000012003052800001NE 2003 5 28 HEEA086579 120030522A3150PHISK76571 PANEL SKRSKYS76 S76A 8143006NE COCKPIT MISSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 CENTER PANEL MISSING. SHOP REPAIR. 1G72 3U H1NE 20030618001392003061800139EA 2003 6 18 COMA0360264 120030610A5242 DOOR CNDAIRCL600 CL6002B19 1900309EA EXTERNAL POWER OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01963CA 7127 FLIGHT 5843 UNUSUAL NOISE FROM RT SIDE OF AIRCRAFT. FOUND THE EXTERNAL POWER SERVICE DOOR OPEN. INSPECTED FOR DAMAGE AND SECURED DOOR CLOSED. 2L72 4F RTA21EA 20030619000172003061900017SW 2003 6 19 HEEA087180 120030609A6320206040531001 CASE BELL 206 206L3 1182108SW M/R GEARBOX CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671 51301 CORRODED MOUNTING HOLES; LINER WORN; CORRODED ORING GROOVE. 1G71 3U H2SW 20030707000252003070700025WP 2003 7 7 AALA20030597 120030523A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21569AA 49351 DURING OVERNIGHT MAINTENANCE, CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030702000112003070200011NM 2003 7 2 TSAA0352107 120030427A53306545849 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13816AL 23122 REMOVED DAMAGED AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR DOUBLER FROM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED DOUBLER PER FIGURE 1. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3360. (M) 2L72 4F RTA16WE 20030707001972003070700197WP 2003 7 7 UPS03840874 120030618A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 385. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030709000292003070900029WP 2003 7 9 AALA20030575 120030516A3350 LIGHT DOUG DC9 DC982 3022082WP AFT AIRSTAIR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21510AM 49804 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY SIDEWALL EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED FORWARD AFT TAIL CONE ON SIDEWALL EMERGENCY EXIT IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030709001312003070900131NM 2003 7 9 PCAA0306077 120030615A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY FALSE INDICATIONA PCAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA13849EX1989 337 FLIGHT 3875 FROM ORF-LGA APPROXIMATELY 30 MILES SOUTH DQO, CARGO BAY SMOKE DETECTOR LIGHT ILLUMINATED. CREW ADVISED FLIGHT ATTENDANT, FA THEN INSPECTED THE CARGO AREA DETERMINED THE PROBLEM TO BE INDICATION ONLY. FLIGHT DIVERTED TO PHL AND CFR INSPECTED CARGO AREA ON TAXIWAY. AIRCRAFT TAXI TO THE GATE. PHL MAINTENANCE FOUND NR 2 SMOKE DETECTOR INOP, WILL NOT TEST MEL 2608 CAT C ISSUED. FLIGHT CONTINUED ON TO LGA. LGA MAINTENANCE REMOVED AND REPLACED NR 2 SMOKE DETECTOR IAW MM CHAPTER 26-12-00, OPS CHECK GOOD. 2H72 4T RTA13NM 20030710001232003071000123NE 2003 7 10 C1HA200392002 220030616A7230 COMPRESSOR BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE NR 3 ENGINE STALLED A C1HAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL15292AS 21458 ON POWER UP 1.4 EPR CHECK NR 3 ENGINE COMPRESSOR STALL FOLLOWED BY EPR FLUCTUATION APPROX .2 TO .3. ALL OTHER ENGINE INDICATIONS NORMAL. 2L73 4F4 F A3WE E2EA 20030711000302003071100030EU 2003 7 11 DHL2003366512 120030608A5311A5397310720000 FRAME AIRBUS300 A300B4203 3930306EU FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH36541 249 STUB FRAME AT FR63A L46 IS CRACKED. RECEIVED STUB FRAME P/N A5397310720000, PO 413461.4. LOCATED, DRILLED AND DEBURRED IAW A300 DWG R53970189. INSTALLED STUB FRAME IAW A300 DWG. R53970189 AN A300 SRM 51-30-35. 2L72 4F RTA35EU 20030709001102003070900110SO 2003 7 9 C2XA03SH180 120030612A540014576631621 STRUCTURE EMB 145 EMB145LR 3260212SO ZONE 400 CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 DURING C-CHECK THE NUMBER ONE LOWER COWLING AFT EDGE MEMBER WAS FOUND CHAFED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030108000012003010800001NM 2003 1 8 PCAA0301008 120030107A521085210240007 HAND RAIL DHAV DHC8 DHC8102 2809003NM BROKEN A PCAAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 EA13828EX 392 HAND RAIL STRUT ON RIGHT SIDE OF AIRSTAIR DOOR FOUND BROKEN. DOOR WOULD NOT OPEN. AIRSTAIR DOOR HAND RAIL SUPPORT STRUT REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030103000612003010300061 2003 1 3 C2XA03BT002 420030101A2300 SPEAKER EMB 145 EMB145LR 3260212SO CABIN ODOR A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2714907 145468 EWR---CO4097, CREW REPORTED, "SMOKE SMELL COMING FLIGHT ATTENDANTS PA IN FRONT". MAINTENANCE INSPECTED WIRES FOR FLIGHT ATTENDANTS PA AND SPEAKERS. DID NOT FIND ANY SIGN OF BURNING. OPS. CHECKED GOOD. IAW EMB145 MM #23-32-00. 2L72 4T RTT00011AT 20030127000662003012700066GL 2003 1 27 HEEA083644 220030114A72406854255 VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE STICKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03498PH 53399 BURNER DRAIN VALVE STICKING. REPAIRED. 1G71 3U3 UO H2SW E1GL 20030128000382003012800038SW 2003 1 28 HEEA083791 120030115A282123066697 FILTER BELL 407 407 1182206SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH 53399 FILTER BYPASS INDICATOR POPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030128002422003012800242SW 2003 1 28 HEEA083891 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030129000302003012900030SW 2003 1 29 HEEA083943 120030117A6420407012101111 ROTOR HEAD BELL 407 407 1182206SW TAIL ROTOR SEIZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH3827 53228 TAIL ROTOR TRUNNION SPLINES ARE SEIZED TO TAIL ROTOR GEARBOX OUTPUT SHAFT SPLINES. REPAIRED. 1G71 3U O H2SW 20030203000022003020300002EU 2003 2 3 CA030110002 120030108A2750SD3452597XA CONTROL CABLE STBROSSD3 SD360300 EU PWA PT6 PT6A65AR 52043NE TE FLAPS BROKEN W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN) PILOT REPORTED THAT FLAPS WOULD NOT EXTEND TO SELECTED POSITION. THEY WOULD FALL 2-4 DEGREES SHORT OF SELECTED POSITION. RETRACTION WAS OKAY. INVESTIGATION BY MAINTENANCE REVEALED THAT AFT RIG PINS FOR FLAP SELECTION CABLE LEVER AND QUADRANT ASSEMBLY WOULD NOT FIT WHEN THE SELECTOR RIG PIN WAS INSTALLED. FURTHER INVESTIGATION REVEALED A BROKEN FLAP SELECTOR CABLE IN THE ROOF OF THE FUSELAGE AT STATION 74. 2H72 4T4 TRTA41EU E4EA 20030203000792003020300079SW 2003 2 3 ALGA084071 120030131A632023030990 SHAFT CLARK 1000 1000CLARK 2230102SW GEARBOX DEFECTIVE H ALGAK NONE O OTHER ININSP/MAINT 1 FS01PARTO ON INSTALLATION GEARSHAFT WOULD NOT FIT INSIDE OIL PUMP DRIVE GEAR. 1Q71 3R 2A6 20030204000442003020400044NM 2003 2 4 SWAA030215 120030129A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 639, RBL 70, WL 209. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030204002722003020400272NM 2003 2 4 VNAA0301020 120030120A2730 REGULATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ELEVATOR FAILED A VNAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL07424JS 3033 DURING CLIMBOUT, THE CREW RECEIVED AN ELEVATOR TRIM FAIL INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE INSTRUCTED TO DIVERT TO DAY AND LANDED WITHOUT ANY FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE 49CC AND 59CC REGULATORS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030212000352003021200035NM 2003 2 12 AUS20030049 120030120A5315 FLOORBEAM BOEING727 7272J4 1384006NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLOORBEAM CORRODED AT BS 870 LBL 65 AND RBL 65. 2L73 4F4 FRTA3WE E2EA 20030216000042003021600004EU 2003 2 16 RAIA00302036 120030203A3200DHE1148 PROXIMITY SWITCH AEROSPATR72 ATR72202 8680940EU MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03723TE6038 283 5462-STL- LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED R/H MLG 1/B PROXIMITY SWITCH, OPS CK OK. 2H72 4T RTA53EU 20030218002012003021800201NM 2003 2 18 SWAA030338 120030208A53306545768 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030219000402003021900040WP 2003 2 19 MWEA030098 120030214A53209915558178 CLIP DOUG DC9 DC981 3022081WP Z 74 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 UPPER INNER JAMB ATTACH CLIP AT Z74 RIGHT SIDE AFT PRESSURE BULKHEAD HAS A .5" CRACK. -- FABRICATED AND INSTALLED CLIP. 2L72 4F A6WE 20030219000562003021900056NM 2003 2 19 SWAA030237 120030201A3397BR2013 WIRE BOEING737 7377H4 1384404NM CABIN EXPOSED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29714CB 27848 EEPLS WIRES EXPOSED IN CABIN. SECURED WIRES PER MM. 2L72 4F RTA16WE 20030221000732003022100073NM 2003 2 21 QXEA0300187 120030126A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 12 SEAT TRACK HAS LIGHT CORROSION AT STATION 516. REPAIRED IAW RD 8-53-3644, DHC-8 SRM 51-20-16 AND SRM 51-20-36 2H72 4T RTA13NM 20030116001532003011600153GL 2003 1 16 HEEA083095 220030108A7412106149501 IGNITER BOX BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 IGNITER BOX INOPERATIVE. WILL NOT LIGHT OFF. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U3 U H2SW E1GL 20030121001372003012100137GL 2003 1 21 HEEA083306 220030109A753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION LDLANDING 1 SW036160Y 51609 AFTER LANDING AND TAKE OFF, TOT INCREASED 30 DEGREES ABOVE NORMAL AND AFTER A FEW MINUTES RETURNED TO NORMAL THAN RAN 30 DEGREES HIGHER THAN NORMAL. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 U H2SW E1GL 20030328000872003032800087EA 2003 3 28 COMA0360126 120030227A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER DEDESCENT 1 SO01796CA8730 7338 PILOTS SIDE WINDOW CRACKED. REPLACED PILOTS SIDE WINDOW. 2L72 4F RTA21EA 20030304000812003030400081NM 2003 3 4 DL757030114 120030128A5330143N347111 SKIN BOEING757 757232 1384965NM FS 580, S-28 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27685DA 27588 FUSELAGE / SKIN / FS 580 / STRG. 28L-28R : GROUND DAMAGE REPAIR THE FUSELAGE SKIN WAS FOUND WITH A CREASE AND A GOUGE JUST AFT OF FS 580 BETWEEN STRINGERS 28L & 28R. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUMDOUBLER PER ER/A 384442-14, REV A. 2L72 4F RTA2NM 20030305000572003030500057CE 2003 3 5 GLBA2003028 120030304A30004E31961GLA BRUSH BLOCK BEECH 1900 1900D 1154162CE A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 NM03170GL1646 UE170 LH PROP DEICE INOP, REPLACED BRUSH BLOCK 2L72 4T RTA24CE 20030226000312003022600031SW 2003 2 26 HEEA084321 120030211A2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 SWITCH STICKS, NO PRESS LIGHT ON SHUTDOWN. 1G71 3U O H2SW 20030303000732003030300073NM 2003 3 3 SWAA030425 120030223A55306552490118 BEAM BOEING737 7373H4 1384600NM VERTICAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED D-CHECK, FOUND VERT STAB RT T/E BEAM CRACKED AT FIN STA 81.8. REMOVED AND REPLACED RT T/E BEAM PER SRM. 2L72 4F RTA16WE 20030324001172003032400117NM 2003 3 24 AWXA200300107 120030206A3350BR964411 LIGHT BOEING757 7572G7 1384963NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 PHX - EEL - DURING INSPECTION, THE EMERGENCY SEAT LIGHT WAS FOUND INOPERATIVE AT LEFT HAND ROW 7 . MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT LEFT HAND SIDE ROW 7 AS REQUIRED. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030310001002003031000100 2003 3 10 HEEA085005 420030227A2561PHI10088 COVER BELL 412 412 1182202SW LIFE VEST TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 LIFE VEST COVER POCKET TORN. 1G72 4U H4SW 20030313001642003031300164EU 2003 3 13 AALA20030118 120030127A3350 POWER SUPPLY AIRBUS300 A300B4605R 3930308EU CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2140064 507 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 28-35 INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030313002242003031300224NM 2003 3 13 QXEA0300198 120030124A5414 PANEL DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 2 NACELLE PANEL 424AR HAS A GOUGE IN CENTER OF PANEL. REPAIRED IAW HORIZON AIR EA 2-71-193. 2H72 4T RTA13NM 20030314002282003031400228EU 2003 3 14 03065321 120030306A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP EMER EXIT LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27321UE 41045 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE RT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE LAMP SOCKET IN THE LIGHT ASSY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20030317000542003031700054NM 2003 3 17 SWAA030570 120030311A53306545785 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUT CRACKED AT RH WINDOW # 9. REPAIRED SKIN PER SWA ERO. 2L72 4F RTA16WE 20030123000102003012300010NM 2003 1 23 2003UALA00009 120030104A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 STATION 847 FRAME CRACKED AT RIVET HOLE AT STR 9R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030317001132003031700113NM 2003 3 17 03FDEA00272 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 32R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030319000172003031900017WP 2003 3 19 GTIA030019 120030106A7900 OIL SYSTEM DOUG DC9 DC941 302207NWP NR 2 ENGINE FLUCTUATES A GTIAK NONE J WARNING INDICATION CRCRUISE 1 GL23130NK 47604 ACY - FLT 277 - GATE RETURN, NR 2 OIL PRESSURE FLUCTUATING. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F A6WE 20030319000432003031900043WP 2003 3 19 GTIA030068 120030205A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FLOOR PANEL STATION 160-200 HAS BLUE WATER AND DETERIORATION. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20030731000982003073100098NM 2003 7 31 QXEA200300894 120030726A1430 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM ROTATING BEACON SPINNING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX- FIVE NUTPLATES UNDER RED ROATING BEACON ARE SPINNING. REPLAIRED IAW Q400 SRM 51-42-05. 2H72 4T RTA13NM 20030418000192003041800019EU 2003 4 18 QXEA0300276 120030214A33505515800106 SIGN FOKKERF28 F28MK4000 4990810EU ZONE 200 MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09497US 11173 PDX- FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20030421000602003042100060EA 2003 4 21 QXEA0300310 120030223A4990WE38762931 SWITCH CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09614QX 10049 PDX ON FLIGHT 2536- APU FAULT FOLLOWED BY APU SHUTDOWN PER CHECKLIST. REMOVED AND REPLACED OIL FILTER DELTA PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030418000912003041800091NM 2003 4 18 EIA2003006 120030221A261130326E8 SMOKE DETECTOR BOEING747 747132 1384882NM CARGO BAY DEFECTIVE A EIAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09479EV 19898 FWD LOWER CARGO FIRE WARNING LIGHT ILLUMINATED. NR1 BOTTLE FIRED. REMAINED ILLUMINATED, VISUAL SCAN INDICATED NO FIRE. NR 1 BOTTLE DISCHARGED LIGHT DID NOT ILLUMINATE. HOWEVER SQUIB TEST INDICATED BOTTLE NR 1 (FWD) DID DISCHARGE, CARGO FIRE LIGHT WENT OUT AT 4200FT. 2L74 4F A20WE 20030423000792003042300079EU 2003 4 23 BAQA085926 120030407A672041800876800 ACTUATOR UROCOPEC135 EC135T1 5620026EU TAIL ROTOR WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01554ME1134 0154 TAIL ROTOR ACTUATOR HAS EXCESSIVE PLAY AND INTERMITTENT LIGHTS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030327000262003032700026EU 2003 3 27 AWXA200300298 120030323A2910 SELECTOR VALVE AIRBUS320 A320231 3930325EU GREEN HYD SYS LEAKING A AWXAO OTHER J WARNING INDICATION DEDESCENT 1 WP28626AW 65 EN ROUTE FROM PHX TO PDX APPROXIMATELY 2 HOURS INTO FLIGHT RECEIVED A GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL ECAM MESSAGE, FOLLOWED BY A NR 1 ENGINE GREEN SYSTEM HYDRAULIC PUMP LOW PRESSURE. FOLLOWED ECAM PROCEDURES AND SHUTDOWN THE POWER TRANSFER UNIT AND GREEN HYDRAULIC SYSTEM PUMP UNTIL ON FINAL APPROACH. DECLARED EMERGENCY, GREEN HYDRAULICS SYSTEM WORKED FINE ON LANDING. MAINTENANCE FOUND THE LEAK MEASUREMENT SELECTOR VALVE LEAKING. REMOVED AND REPLACED LEAK MEASUREMENT SELECTOR VALVE. OPERATIONAL AND LEAK CHECK GOOD IAW AMM 29-19-41-401. 2L72 4F RTA28NM 20030718000052003071800005NM 2003 7 18 TSAA0333128 120030529A33508610066 BATTERY PACK BOEING737 737230 1384401NM EMERGENCY LIGHTSINOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13823AL 23154 REPLACED FORWARD ENTRY DOOR EMERGENCY BATTEYR PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20040224000562004022400056WP 2004 2 24 ASAA0380257 120030309A33501001101 LIGHT DOUG DC9 DC983 3022083WP CABIN MALFUNCTIONED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01969AS 53063 OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR WOULD NOT EXTINGUISH WITH SWITCH OFF. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030902001502003090200150SO 2003 9 2 SWIA200312162 120030630A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07189SW2037 2037 120048 EMERGENCY LIGHTS INOP (MIDDLE SECTION).REPLACED CENTER ELBP. OPS CHECK GOOD. 2L72 4T RTA31SO 20030902001692003090200169NE 2003 9 2 2003F00396 220030709A7260SLSTD208 GARLOCK SEAL PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2B NE ENGINE DEFECTIVE E E ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 SO19399AC 317552038 L749261A DURING RETURN FLIGHT FROM (MYNN) INBOUND TO TMB, BETWEEN BIMINI AND MIAMI LT ENGINE OIL PRESSURE STARTED FLUCTUATING. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN ON LT ENGINE. NO OTHER OCCURENCES. FINDINGS: OIL FLUCTUATING DUE TO LOSS OF OIL THROUGH HYDRAULIC PUMP ACCESSORY DRIVE GARLOC SEAL. NEW HYDRAULIC PUMP ACCESSORY DRIVE GARLOC SEAL INSTALLED. 1L72 3O3 O A20SO E14EA 20030728001432003072800143WP 2003 7 28 AAL2003F00012 120030318A5347 SEAT TRACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170529 49921 NR 2 SEAT TRACK, CORRODED. INSTALLED SEAT TRACK PLUG SRM 53-05-4A. 2L72 4F4 F A6WE E2EA 20030807001022003080700102NM 2003 8 7 EIA2003099 120030725A5714 SKIN BOEING747 747212B 1384886NM CENTER TANK CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 UPON REMOVAL OF FASTENERS FOR ADJACENT S/M REPAIR, CENTER TANK UPPER AFT SKIN PANEL WAS FOUND CORRODED AT STA 1237, RBL 37 UNDERNEATH LONGITUDINAL FLOORBEAM LOWER CHORD. DAMAGED AREA REPAIRED PER ECRA 485-57-154-2. 2L74 4F A20WE 20030812000532003081200053SW 2003 8 12 HEEA088475 120030714A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z12061 33077 MAIN ROTOR BLADE FIBERGLASS AT THE MIDSPAN TAB BROKEN AND CRACKED THROUGH THE TRAILING EDGE SPAR. BLADE HAD WATER NEAR THE ROOT END ON THE TRAILING EDGE SIDE. 1G72 4U H4SW 20030814000832003081400083EA 2003 8 14 SWIA200312089 120030528A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 FS 621.0 RBL 36 FLOOR SUPPORT ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV A. 2L72 4F4 FRTA21EA E15NE 20030807000582003080700058SO 2003 8 7 C2XA03SH263 120030805A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK, THE CARGO DOOR CUT OUT LOWER BEAM BETWEEN FRAMES 65 AND 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030905000082003090500008SO 2003 9 5 LR7A03055 120030725A5312 PRESSURE PANEL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND RMLG FS 517 WEB CRACKED AT RBL 61, WL 160 APPROX 1.5 IN. REPAIRED IAW LAC MEA 382-53-03-057. NR 2087. 2H74 4T A1SO 20030905002252003090500225SO 2003 9 5 C2XA03SH301 120030827A531514530633003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030908001722003090800172SO 2003 9 8 SWIA200312242 120030803A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO CABIN DISCHARGED A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07250YV 120250 EMERGENCY LIGHTS FROM ROW 6 FORWARD INOP. REMOVED AND REPLACED THE NR 1 ELBP WITH SERVICEABLE UNIT IAW 33-51-01. OPS CHECKS GOOD. S/N OFF: 1210/04-96 2L72 4T RTA31SO 20030813001702003081300170NM 2003 8 13 SWAA031680 120030727A57546546430122 SKIN BOEING737 7373H4 1384600NM RT WING LE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED C2 CHECK, FOUND RT INBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED RT INBD T/E FORE FLAP PER MM. 2L72 4F RTA16WE 20030821002612003082100261NM 2003 8 21 USAASB03108 120030713A335030043229 LIGHT BOEING737 7374B7 1384702NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19779AU 24996 BOS - MAINTENANCE REPORTED THE FORWARD RIGHT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030825001312003082500131SO 2003 8 25 C2XA03SH290 120030824A716014575001403 INTAKE EMB 145 EMB145LR 3260212SO NR 1 COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK THE NUMBER ONE ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030822001132003082200113 2003 8 22 RAIA00307187 420030708A3442MI5853505 TRANSCEIVER AEROSPATR42 ATR42300 8680920EU WEATHER RADAR WILL NOT TEST A RAIAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE03421TE9695 8004 102 5635-MLI- WEATHER RADAR WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR RECEIVER TRANSMITTER. 2H72 4T RTA53EU 20030730000432003073000043NM 2003 7 30 P5CA0300902 120030712A275065B1595051 PUSHROD BOEING747 747200 1384847NM T/E FLAP MALFUNCTIONED A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23524UP 21446 UPON ARRIVAL NOTED NR 5 & 6 CANOE FAIRING DROOPING. REMOVED AND REPLACED I/B MID FLAP PUSH RODS AND T/E FLAP PUSHROD AND SUPPORT FITTING NR 5 CANOE. 2L74 4F RTA20WE 20030911001222003091100122NM 2003 9 11 03FDEA01294 120030806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBD FLAP OUTBD HINGE ( A/C SIDE ) FWD MOST ATTACH HOLES CORRODED AT BORES. RT WING OUTBD FLAP ( A/C SIDE ) OUTBOARD HINGE FWD ATTACHMENT INBOARD AND OUTBOARD HOLES REPAIRED AS PER CMM 57-44-09. 2L73 4F RTA22WE 20030916000492003091600049NM 2003 9 16 03FDEA01002 120030625A5753ARC70541 FLAP TRACK DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT WING - OUTBOARD TRAILING EDGE FLAP VANE, NR 2 TRACK SUPPORT ASSY FOUND FORWARD MOUNT BOLT HOLE SURFACE WITH CORROSION (NUMBERED FROM INBOARD). REPAIR CARRIED OUT AT LT WING OUTBOARD TRAILING EDGE FLAP VANE NR 2. TRACK SUPPORT ASSY FWD MOUNT BOLT HOLE IAW EA 1-5750-71731 : WINGS - RIGHT AND LEFT OUTBOARD FLAP VANE - NR 2 TO TRACK SUPPORT CORRODED. 2L73 4F RTA22WE 20030916000132003091600013WP 2003 9 16 MEX2003314 120030727A3810 LINE DOUG DC9 DC987 3022087WP POTABLE WATER BROKEN W ASMFO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW23754RA 49641 DURING TRANSIT CHECK WAS DETECTED POTABLE WATER LEAK, DRAINING TO THE ELECTRIC/ELECTRONIC COMPARTMENT. TCAS AND FDAU WERE WET. AIRCRAFT WAS SENT TO THE HANGAR. DURING REVISION WAS DETECTED NIPPLE AND SUPPLY LINE BROKEN THE 218 STATION. THE NIPPLE AND SUPPLY LINE WERE REPLACED, ALL TESTS CORRECT. 2L72 4F RTA6WE 20030911001362003091100136NM 2003 9 11 03FDEA01322 120030815A5320 WEB BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 CORROSION ON WEB AT STA 986, STR 29R, WL 148 . REPAIRED WEB AT B.S. 986, STR 29R, WL 148 IAW SRM 53-10-4 FIG 15. 2L73 4F RTA3WE 20030910002232003091000223EU 2003 9 10 MALA030391 120030728A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 DURING C-CHECK IN CVG, NR 2 SEAT RAIL IS CORRODED BEYOND LIMITS, FROM FRAME 20 FORWARD. MAINTENANCE REPAIRED IAW EO NR 53026. A/C RELEASE DATE 8/11/03, REFER TO 409 NR 128568 FOR DETAIL. 2H74 4F RTA49EU 20030925000502003092500050NM 2003 9 25 USAA030157 120030804A5311 FRAME BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US40913 23987 FOUND FRAME CRACKED AT RIVET, STATION 440 S8L AND S9L FRAME. CUT OUT DAMAGED AREA AND INSTALLED DOUBLERS PER TYP REP 53-10-20A. (M) 2L72 4F RTA16WE 20030926001032003092600103NM 2003 9 26 C1HA200396018 120030829A3260 MODULE BOEING727 7272J4 1384006NM MLG MALFUNCTIONED A C1HAO OTHER J WARNING INDICATION CLCLIMB 1 GL15696CA 22574 ON DEP NOSEGEAR UNSAFE LT REMAINED ILLUM ON GEAR RETRACT. CYCLED GEAR, THEN TO OFF POSITION, NO CHANGE. VISUALLY VERIFIED NOSEGEAR DOOR CLOSED. THROUGH TELE CONFERANCE, CONFIRMED THAT IT IS RED NOSE GEAR LIGHT THAT ILLUMINATED. NOT NOSE GEAR DOOR LT. INPECT WIRING BETWEEN NOSE GEAR POSITION SWITCH, NOSE GEAR LOCK SWITCH FOR SHORTS. CHECKED FOR SHORTS FROM LANDING GEAR TO NOSE GEAR SWITCHES, CKD SWITCH S92 LANDING GEAR LEVER DN SWITCH FOR SHORTS. CKD LT MODULE (LANDING GEAR) LIGHT L-802 FOR SHORTS. ALL OK REPAIRED FRAYED WIRE IN NOSE GEAR WHEEL AREA FROM BRAIDED CONDUIT OF NOSE GEAR LOCK SWITCH TO NOSE GEAR POSITION SW REF MM CH 20 STD PRAC. R/R LANDING GEAR UNIT PERFORMED NOSE GEAR SWING. ALL CHECKS OK. 2L73 4F RTA3WE 20031002000092003100200009NM 2003 10 2 UIEA200300056 120030912A2131 CONTROLLER BOEING747 7472D7B 1384803NM CABIN PRESSURE MALFUNCTIONED A UIEABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15526MC 22337 DURING CRUISE FL370, PACKS NR 1 & 2 OPERATING, NR 1 PACK AIRFLOW APPROX 20 PSI & NR 2 PACK AIRFLOW 33 PSI, CABIN BEGAN TO CLIMB RAPIDLY. RATE LIMIT LIGHT ON. CABIN SHOWED A MOMENTARY DESCENT THEN BEGAN TO CLIMB RAPIDLY. SELECTED MANUAL PRESSURE. CABIN CONTINUED TO CLIMB RAPIDLY & ALTITUDE WARNING HORN ON. THIRD PACK WAS TURNED ON & OUTFLOW VALVES IMMEDIATELY SELECTED TO CLOSE. CABIN CONTINUED TO CLIMB. EMERGENCY DESCENT INITIATED. AFTER RECTIFICATION OF APU, ALL 3 PACKS CHECKED OK FOR NORMAL OPS AS PER AMM 5-51-08. EXCESSIVE CABIN PRESSURE LEAK CHECK CARRIED OUT WITH GOOD RESULTS. CHECKED UP TO 4 PSI AT 500 V/S. PRESSURE BLKHDS ETC CHECKED NO DEFECTS OR LEAKS AS PER 5-51-08. A/C SERVICEABLE. (M)2L74 4F RTA20WE 20031002001392003100200139NM 2003 10 2 CALA0300523 120030912A3350B21506 FUSE BOEING737 737524 1384721NM POWER SUPPLY BLOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2762631 27535 INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT ABOVE FIRST/COACH DIVIDER INOPERATIVE. REPLACED PICO FUSES IN POWER SUPPLY FOR LIGHT. 2L72 4F RTA16WE 20031003000422003100300042NM 2003 10 3 AWXA200301046 120030909A5420655226333 CLIP BOEING737 737277 1384570NM NR 1 NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .1250 CRACK WAS FOUND IN RADIUS OF NR 1 ENGINE LT FIXED FAIRING CLIP AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED CLIP ON NR 1 ENGINE LT FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT CLIP IAW DWG 65-52263; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. 1. 2L72 4F RTA16WE 20031015000542003101500054EA 2003 10 15 ASOA03453 120030920A5260 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS AND RIG CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031021002092003102100209NM 2003 10 21 AALA20031020 120030919A33500201720001 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21191AN 32385 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROW 17D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030908001922003090800192 2003 9 8 SWIA200312269 420030818A22138220044001 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07459SW1145211452 7782 ALTITUDE PRESELECT NOT HOLDING ALTITUDE/DEPARTED PRESELECT AND RAN UP AND DOWN UNCONTROLLABLE. PRESELECT KNOB WOULD NOT CONTROL. DISENGAGED AP AND HAND FLEW PLANE. REMOVED AND REPLACED FCP IAW MM 22-10-07. FCP & AP OPS CHECK GOOD IAW MM 22-11-07. 2L72 4F RTA21EA 20031029000432003102900043NM 2003 10 29 ASAA0310399 120030506A53306545800 SKIN BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND SKIN PANEL AT BS 273, STRINGER 24R DENTED. CUT OUT DAMAGED AREA AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031029000772003102900077NM 2003 10 29 ASAA0240221 120030401A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 DURING C-CHECK, FOUND CORROSION ON FRAME SHEAR TIE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031110001762003111000176NE 2003 11 10 MEX2003457 220030210A7321 FUEL CONTROL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LT ENGINE OUT OF TRIM A ASMFK NONE O OTHER ININSP/MAINT 1 SW23162PL 49765 FLT 494 - MID-MEX - AFTER LEFT ENGINE STARTING WITH N2 BELOW MINIMUMS, SL 22 DEGREES CELSIUS AND 54 PERCENT OF N2, REMAINING IN VALUES OF 46 PERCENT AND 470 DEGREES CELSIUS OF EGT. STARTING VALVE WAS CLOSED STILL REMAINING BELOW MINIMUM SAME VALVES. RIGGING AND TRIMMING PROCEDURE WAS PERFORMED IAW MM 71-00-00. (M) 2L72 4F4 FRTA6WE E9NE 20031119000462003111900046WP 2003 11 19 0301909941 120030831A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013324L 47103 DURING APB WEB INSPECTION FOUND 1.5 IN CRACK IN SKIN 4 IN OUTBOARD OF THE DOOR JAMB. REPAIRED IAW EA 99-195996. 2L72 4F A6WE 20031121000022003112100002 2003 11 21 AWXA200301460 420031117A3414 INDICATOR BOEING737 7373B7 1384580NM COCKPIT MALFUNCTIONED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28328AW 23377 DURING TAKEOFF ROLL AT MSY EN ROUTE FOR PHX THE FIRST OFFICERS AIRSPEED INDICATOR FLAGGED MOMENTARILY, REJECTED TAKEOFF. RESET NO FURTHER EVENTS ON SUBSEQUENT TAKEOFF. 2L72 4F RTA16WE 20040204000732004020400073CE 2004 2 4 55265AMWA 120031015A32101143640681 LANDING GEAR BEECH 1900 1900D 1154162CE MAINS MALFUNCTIONED A AMWAO OTHER J WARNING INDICATION LDLANDING 1 CE07173YV UE173 UPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN). CREW GOT THREE DOWN AND LOCKED INDICATIONS AND LANDING SAFETY WITH NO FURTHER INCIDENTS. P/N 1143640681 S/N506D95 PCB TIME DELAY RELAY. 2L72 4T RTA24CE 20040210000822004021000082EU 2004 2 10 USAA030314 120031202A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .5 INCH BY .5 INCH AREA, RBL 17.75 AT FRAME 68. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20040212000432004021200043NM 2004 2 12 COOSDR030158 120031201A5730 SKIN BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE LT WING CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23395AJ 21100 LT WING, LOWER SKIN, LOWER SURFACE, ACCESS DOOR CUTOUT CORRODED. (K) 2L73 4F4 FRTA3WE E2EA 20031031000732003103100073NM 2003 10 31 DL757030839 120030912A5330146N36109 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27660DL 24422 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 1646 BETWEEN STRINGERS 29L & 29R. THE CORROSION WAS REMOVED WITH A 3 X 3.5 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385620-14, REV A. 2L72 4F RTA2NM 20031119000472003111900047NE 2003 11 19 GLBA2003138 220031010A7323 GOVERNOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE OUT OF RIG A GLBAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NM03170GL UE170 RT ENGINE FUEL FLOW AND PROP TORQUE FLUX, RIGGED RT GOV INTERCONNECT. 2L72 4T4 TRTA24CE E26NE 20031118000362003111800036EU 2003 11 18 AWXA200301151 120030924A5320D5367009922200 BRACKET AIRBUS320 A320232 3930326EU FLOOR PANEL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FLOOR PANEL BRACKET (CONNECTING PLATE) AT Y1162. MAINTENANCE REMOVED CORRODED FLOOR PANEL CONNECTING PLATE AT Y1162, FABRICATED AND INSTALLED A NEW REPLACEMENT CONNECTING PLATE PER DWG D53670099. 2L72 4F RTA28NM 20031105000862003110500086NM 2003 11 5 QXEA200301355 120031028A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8401 1390041NM NR 1 MALFUNCTIONED A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09400QX 4030 GEG- ON FLIGHT 2371 NR 1 AUTOFEATHER TEST FAILS. FOUND FAULT CODE 494 CHANNEL A AND B OF NR 1 PEC. PERFORMED FIM TASK 61-20-10-810-805. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031106002012003110600201EA 2003 11 6 ASOA03463 120030929A3350111RJ7001 STRIP CNDAIRCL600 CL6002C10 1390015EA CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11703EV 10038 FLT 4247 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP ON THE FORWARD LEFT SIDE BY THE GALLEY WAS FOUND MISSING. MAINTENANCE INSTALLED THE EMERGENCY FLOOR LIGHT PHOTO LUMINESCENT TAPE ON THE FORWARD LEFT SIDE BY THE GALLEY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031106002372003110600237WP 2003 11 6 GTIA030722 120030904A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND WEB AT FS 1155 RBL 54, CORRODED, GOUGED, AND CRACKED. REMOVED WEB FROM STATION 1098-1174. FABRICATED WEB. INSTALLED NEW FABRICATED WEB. (M) 2L72 4F A6WE 20031113000272003111300027EU 2003 11 13 BAQA090155 120031028A2121 RELAY UROCOPEC135 EC135T1 5620026EU BLOWER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118WS1804 2005 0089 BLOWER STOPPED WORKING. AT ONE TIME, TAPPING ON THE RELAY GOT IT TO WORK AGAIN, BUT ONLY ONCE. IT SEEMS TO BE THE RELAY. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040113001352004011300135NM 2004 1 13 03FDEA02256 120031226A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, I/B FLAP O/B HINGE FITTING I/B PIVOT LUG BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75213. TRAILING EDGE & TRAILING EDGE DEVICES. RT INBOARD. FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040113002052004011300205SO 2004 1 13 C2XA03CL217 120031225A335020131A BATTERY EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716510 145251 THE CREW REPORTED THE EMERGENCY EXIT LIGHTING WOULD NOT REMAIN ILLUMINATED DURING TESTING. MAINTENANCE RECHARGED THE EMERGENCY EXIT LIGHTING BATTERIES. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031124000892003112400089WP 2003 11 24 DHL2003807555 120031107A2711 TAB DOUG DC8 DC873F 302199FWP AILERON BINDING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING - WHEN DISCONNECT PUSH ROD, AILERON CONTROL TAB DOES NOT HAVE FREE MOVEMENT. REMOVED AND REPLACED RIGHT AILERON CONTROL TAB IAW MM 27-11-4 PG 201-203. FOR OPS CHECK SEE NR 2035. 2L74 4F RT4A25 20031125001052003112500105NM 2003 11 25 AALA20031294 120031118A335002031461201 COVER BOEING737 737823 13844BZNM CABIN MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21956AN 30090 TPA RIGHT HAND AFT EMERGENCY EXIT SIGN COVER MISSING. REPLACED RIGHT HAND AFT EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040114001332004011400133NM 2004 1 14 2003UALA00883 120031119A219791318506 RELAY BOEING757 757222 1384956NM PWA 2037 PW2037 NE AFT PIT P-70 BURNED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29544UA 25322 GROUND CREW REPORTED SMOKE IN AFT PIT. SMOKE FROM DUCTING AND FORWARD WALL AREA. CAUSE APPEARS TO BE A STUCK AFT CARGO HEATER RELAY. STUCK RELAY ALLOWED HEATER TO OVERHEAT TO POINT WHERE SILICONE WRAPPED HEATER RIBBON MELTED, CAUSING SMOKE. MELTING OF RIBBON WIRE CAUSED OPEN CIRCUIT, ALLOWING HEATER TO SHUT DOWN. RELAY K10083 PER WDM 21-44-11. RELAY, HEATER AND FAN REPLACED. 2L72 4F4 FRTA2NM E17NE 20040113002292004011300229NM 2004 1 13 QXEA200301586 120031226A2612 CONNECTOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE CARGO BAY NOT SEATED A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09369PH 513 NR 1 BAGGAGE SMOKE WARNING WILL NOT TEST. RESEATED CONNECTORS ON NR 1 AND NR 2 SMOKE DETECTORS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040114001572004011400157NM 2004 1 14 03FDEA02010 120031203A5753ARC1991 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 3 IB FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20031216000722003121600072NM 2003 12 16 SWAA032568 120031121A3350101073 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C4 CHECK, FOUND AFT DOOR SIDE WALLS EMERGENCY EXIT LIGHTS INOP. RELAMPED EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20031218000342003121800034 2003 12 18 SWIA200312629 420031125A3418 STICK SHAKER EMB 120 EMB120ER 3260203SO NR 2 STALL WARN INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM0716731 120190 NR 2 STALL STICK SHAKER INOP. REPLACED NR 2 STICK SHAKER. OP CHECK GOOD. 2L72 4T RTA31SO 20031229000632003122900063NM 2003 12 29 QXEA200301557 120031210A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 DENT ON LT FUSELAGE JUST AFT OF LEFT HAND ICE SHIELD BELOW PREVIOUS REPAIR. REPAIRED IAW HORIZON AIR EO 6-53-320. 2H72 4T RTA13NM 20040105000292004010500029EU 2004 1 5 AALA20031437 120031216A3350A3060719102 LIGHT FOKKERF28 F28MK0100 4990807EU ROW 10 LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW211469D 11502 ORD FLOOR TRACK LIGHTING AT ROW 10 IN MAIN CABIN DISCONNECTED AND LOOSE. REPLACED FLOOR TRACK LIGHTING AT ROW 10 IN MAIN CABIN. SYSTEM GROUND CHECK NORMAL OPERATION. 2L72 4F RT 20031009000482003100900048SO 2003 10 9 SIMA200318104 120030629A3350 SIGN EMB 135 EMB135LR 3260305SO OVERWING INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 MAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT SIGN TO BE INOPERATIVE. (M) 2L72 4F RTT00011AT 20031009000802003100900080SO 2003 10 9 SWIA200312402 120030809A5720 CLIP EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07298SW 120328 RIGHT OUTBOARD WING, STATION 15, LOWER WING CLIP (FWD OF MIDDLE CLIP) CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED LOWER WING SUPPORT CLIP (FWD OF MIDDLE CLIP) OF RIGHT OUTBOARD WING RIB 15 PER MM 28-10-00. 2L72 4T RTA31SO 20031010000052003101000005NM 2003 10 10 USAABB03152 120030830A3350873100151REV12 LIGHT BOEING757 757225 1384959NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU 22192 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20040106000682004010600068SO 2004 1 6 SWIA200312695 120031214A3320 BALLAST EMB 120 EMB120ER 3260203SO GALLEY FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07237SW 120314 GALLEY LIGHT AND COFFEE POTS WENT OUT/INOP AND SMOKE WAS SMELLED IN CABIN. FOUND GALLEY BALLAST TO BE BAD. REMOVED AND REPLACED BALLAST IAW MM 25-30-04. OPS CHECK GOOD. 2L72 4T RTA31SO 20031125001652003112500165NM 2003 11 25 ASAA0310514 120030603A5753657190241 STRUCTURE BOEING737 7372X6C 1384552NM T/E FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING TRAILING EDGE OF THE MIDFLAP AT WING STATION 175.5 CHAFED. REPAIRED MIDFLAP PER EA. (M) 2L72 4F RTA16WE 20031126000142003112600014SO 2003 11 26 RAIA00311280 120031104A3297 WIRE HARNESS EMB 145 EMB145LR 3260212SO BRAKE SYSTEM DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03810HK 145231 5316-PIT- BRAKE OVER TEMP ADVISORY NR 2 BRAKE. MAINTENANCE DEFERRED PER MEL 32-40-01. SUBSEQUENTLY CLEARING DMI BY REPAIRING WIRE HARNESS. 2L72 4T RTT00011AT 20031126001102003112600110SO 2003 11 26 C2XA03BT098 120031017A3397110049 WIRE EMB 145 EMB145ER 3260211SO ALLSN AE3007AE3007C GL CABIN BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712946 145052 EWR---CO3256, CREW REPORTED (ON WALKAROUND), THAT THE EMERGENCY EXIT SIGN NEAR THE PASSENGER DOOR IS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE NEAR PASSENGER DOOR, REPAIRED BROKEN WIRE, AND OPS CHECKED EMERGENCY LIGHTS GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031126000622003112600062NM 2003 11 26 DXTA200300167 120031121A3231 ARM GULSTM200 200 4500308NM RT MLG DOOR MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07702QS 070 AFTER SELECTING GEAR UP, THE RIGHT GEAR WOULD NOT INDICATE UP, HAD RED GEAR DISAGREEMENT LIGHT. REMOVED LT & RT MAIN GEAR DOOR ASSEMBLY ARMS AND INSTALLED NEW ARMS OF SUPERCEDED P/N'S. PERFORMED MAIN GEAR DOORS OUTBOARD AND INBOARD RIGS AND OPS CHECKS. GEAR OPS CHECKS AND DOOR LATCHING PRESSURES CHECKED GOOD. ALL WORK ACCOMPLISHED IAW GULFSTREAM 200 MM CHAPTER 32-10. 2L72 4F RTA53NM 20031203001502003120300150WP 2003 12 3 AMTA200301240 120030925A5730 SKIN LKHEED1011 1011385115 5265015WP LT WING CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 193B1230 FOUND LEFT UPPER WING SKIN CRACKED PAST STOP DRILL. AT AFT SPAR FORWARD OF INBOARD FLAP PYLON. STOPPED DRILLED/HFEC COMPLETE, COLD WORKED HOLE AND FINAL REAMED TO .250 PER SRM 57-32-00, TREATED PRIMED AREA IAW SRM 51-21-00. (M) 2L73 4F A23WE 20040121000602004012100060EA 2004 1 21 ASOA03600 120031123A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11906EV 7642 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 ON THE LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT SIDE IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040121000272004012100027NM 2004 1 21 03FDEA02320 120031229A5510ALC81072 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB RT UPPER CENTER PLANK NR 26R BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-75197: HORIZONTAL STAB BARREL NUT BORE 26 RT FITTING FABRICATION. 2L73 4F RTA22WE 20031205000402003120500040NM 2003 12 5 DLM88030930 120031014A5330593600419 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27911DL 49542 CORROSION WAS FOUND ON THE FUSELAGE SKIN AT FS 712 BETWEEN LONGERONS 29L & 30. THE CORROSION WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087519-14. 2L72 4F RTA6WE 20031209002322003120900232WP 2003 12 9 ARWA20031003 120031020A5270 WARNING LIGHT DOUG DC8 DC863F 302198FWP MLG DOOR FALSE ACTIVATIONA ARWAO OTHER J WARNING INDICATION CLCLIMB 1 SO19441J 45688 LANDING GEAR DOOR NOT LATCH LIGHT ILLUMINATED AFTER TAKEOFF; PERFORMED ABNORMAL CHECKLIST, LIGHT WENT OUT. CLEANED, INSPECTED & LUBRICATED LANDING GEARS AND DOORS IAW DC8 MM 12-81-1. ACCOMPLISHED GEARS SWING IAW DC8 MM 32-30-0. NO DEFECTS NOTED. 2L74 4F 4A25 20031208000542003120800054NM 2003 12 8 03FDEA01788 120031021A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25269FE 21675 COMPLY WITH EA 7-5310-73207 FUSELAGE - MAINFRAME - KEEL BEAM T-ANGLE REPAIR. COMPLIED WITH EA 7-5310-73207 FUSELAGE - MAIN FRAME - KEEL BEAM T-ANGLE REPAIR AT MAE. 2L73 4F RTA3WE 20040126000262004012600026 2004 1 26 HEEA087791 420030620A22127000299909 CONTROLLER SKRSKYS76 S76C 8143008NE AUTOPILOT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 FD SEL SEGMENT BLOCK IS INTERMITTENT. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20031014000892003101400089NM 2003 10 14 SWAA032213 120031006A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20031020002232003102000223NM 2003 10 20 UPS03441338 120031005A3350 LIGHT BOEING747 747121 1384871NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:N/A AFT EMERGENCY LIGHT AT L1 DOOR INOP. PERFORMED OPS CHECK IAW MM 33-51-00, OPS CHECK NORMAL. 2L74 4F A20WE 20031210001402003121000140NM 2003 12 10 AALA20031350 120031201A2932211C223301 PRESSURE SWITCH BOEING767 767323 1385205NM HYD SYSTEM FAULTY A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW2139367 25194 HNL T162/01 EN ROUTE HNL-LAX CENTRAL HYDRAULIC PRIME MESSAGE AND PRESSURE LIGHT ON NUMBER 2 CENTER ELECTRIC HYDRAULIC PUMP ILLUMINATED. RETURNED HNL. REPLACED PRESSURE SWITCH FOR CENTER HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA1NM 20031209002382003120900238EA 2003 12 9 COMA0360481 120031103A2910AE2460010H0264 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM CHAFED A COMAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO01915CA24179 7013 DURING FLIGHT 5588 FROM ATL, HYD NR 2 LO PRESS CAUTION MESSAGE APPEARED IN FLIGHT AT 27000 FT. AIRCRAFT PERFORMED UNSCHEDULED LANDING AT CKB AND FOUND RIGHT ENG HYD PRESS LINE AE2460010H0264 CHAFED ON FUSELAGE AND SUPPORT CLAMP BROKEN OFF THE FRAME. 2L72 4F RTA21EA 20031210001342003121000134NM 2003 12 10 AALA20031286 120031117A2750285N001140 FSEU BOEING757 757223 1384957NM E/E BAY LOOSE A AALAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21195AN 32389 MIA T921/17 EN ROUTE MCO-MIA TRAILING EDGE FLAPS DISAGREE LIGHT ON ENGINE INDICATING AND CREW ALERT SYSTEM. LANDED MIA WITHOUT INCIDENT WITH FLAPS AT 20 ABNORMAL CONFIGURATION. RESEATED NUMBER ONE FLAP/SLAT ELECTRICAL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20030917000922003091700092NM 2003 9 17 AMTA200301085 120030823A2560 BATTERY BOEING737 73783N 13844HINM FLASHLIGHT DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11304TZ 30675 ALL F/A JUMPSEAT EMERGENCY FLASHLIGHT ARE WEAK AND BATTERIES NEED REPLACED. REMOVED AND REPLACED ALL F/A JUMPSEAT EMERGENCY FLASHLIGHTS. OPS NORMAL PER M/M 25-64-00. OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030922000552003092200055NM 2003 9 22 QO12003F00000 120030624A2497W46702520 WIRE BOEING737 7373Q8 1384670NM MISROUTED B QO1YK NONE W INADEQUATE Q C ININSP/MAINT 1 EA33SUZCF 26283 ROUTINE MAINT WORK REVEALED THAT A/C HAD BEEN OPERATING WITH A WIRE ROUTING DEVIATING WIRE ROUTING REQUIRED BY SB. ON E1-3 ELECTRONIC SHELF, WIRE W467-025-20 HAD NOT BEEN REROUTED TO D8937J CONNECTOR AS INSTRUCTED BY SB 737-27A1206, FIG 5, FLAGNOTE 9. DETECTED DEFECT AFTER YAW DAMPER SERVO TEST FAILED. AS A RESULT OF THE FAULTY WIRE ROUTING, YAW DAMPER COUPLER ONCE MORE FAILED DURING TESTING. INSP OF E1-3 ELECTRONIC SHELF REVEALED 3 RADIO ALTIMETER INTER FACE WIRES; W011-2014-22R, W011-2015-22B AND W011-8725-24 MISSING. SB FIGURE 20 INTRODUCED THESE WIRES AS A PART OF WIRE CHANGE FOR THE RUDDER SYSTEM IMPROVEMENT SB, RULED BY AD. WITH RADIO ALTIMETER INTERFACE MISSING, RECTIFIED CONDITION. 2L72 4F RTA16WE 20030923001562003092300156WP 2003 9 23 AALA20030438 120030313A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW219615W 53562 FOUND CORROSION ON SEAT TRACK STATION 588-798. REPLACED NR 3 CHAIR TRACK STATION 588-798 PER SRM 53-05-00 FIG 4F. (M) 2L72 4F RTA6WE 20040130000152004013000015NM 2004 1 30 SWAA032808 120031226A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED PMC CHECK, FOUND 2 FUSELAGE SKIN CRACKS AT BS 727E+3, STR 22L AND BS 727E+17, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040129000882004012900088NM 2004 1 29 DHL200342544 120031121A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, STR 27 L BETWEEN STA 620-640 AT POWER CABLE STAND-OFF. REMOVED FASTENERS FOR ACCESS AS REQ'D IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT STA 630 STR 27 L, CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1AREA OF CUT OUT 3 INCHES AND FABRICATED STRINGER REPAIR USING BAC 1498-25 PO335792 DIM 13 INCHES AND ONE FILLER USING BAC1498-25 PO335792 DIM 3 INCHES IAW B727 SRM 53-10-3 FIG 1. ALODINE AND PRIMED ALL REPAIR PARTS IAW B727 SRM 51-10-2 AND INSTALLED REPAIR AND STAND-OFF IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20040130002052004013000205WP 2004 1 30 ABXA040021 120031223A532099236693 ANGLE DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 SUBFLOOR AND ANGLE CRACKED AT BUTTLINE 0, STA 160. REPAIRED SUBFLOOR IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040203000122004020300012NM 2004 2 3 ASAA0310175 120030320A541165479691 LONGERON BOEING737 737298C 1384490NM NR 2 NACELLE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL LONGERON AT NACELLE STATION 170.50 - 221 GOUGED. REMOVED AND REPLACED LONGERON IAW SRM. (M) 2L72 4F RTA16WE 20040204000752004020400075EU 2004 2 4 U30A200300035 120031017A5210FE174001 CYLINDER AIRBUS320 A320212 3930322EU PAX DOOR DISCHARGED A U30AK NONE O OTHER ININSP/MAINT 1 EA17265AV 427 AFTER MAINTENANCE ACCEPTANCE FLIGHT ASSOCIATED WITH AN 8C CK & 10 YR INSP., ON FLT 9265 YWG-YWG, THE L2 PAX/CREW DOOR DAMPER & EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW (LEAKING NITROGEN).REPLACED THE L2 PAX/CREW DOOR DAMPER I/A/W AMM 52-13-14-401. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040212000072004021200007WP 2004 2 12 UPS03841624 120031122A574037048411 FITTING DOUG DC8 DC871F 302199DWP RT WING TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C1 STRINGER END FITTING IS CRACKED AT NR 3 ALT TANK AT XRS 74 AT STRINGER 51. REMOVED AND REPLACED FITTING I.A.W. DWG. 3704841 AND SRM.51-1-20D, 51-3-0. 2L74 4F RT4A25 20040212001092004021200109WP 2004 2 12 IXXA0300085O 120031212A793039605740 INDICATOR DOUG DC8 DC871F 302199DWP NR 2 OIL PRESS INOPERATIVE A IXXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW11821BX844341536 45811 ON CRUISE FROM KTOL TO KLRD NR 2 ENGINE OIL PRESSURE INDICATOR WENT TO 2 PSI. OIL PRESSURE LIGHT PRESS TO TEST OKAY. COMPLIED WITH ABNORMAL CHECKLIST. ALL OTHER ENGINE INDICATIONS NORMAL. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 OIL PRESSURE GAGE. OPERATIONAL CHECK GOOD ON GROUND IAW ALL APPLICABLE MANUALS. NO OTHER DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040316000132004031600013WP 2004 3 16 ASAA0380279 120030402A53403936668507 FITTING DOUG DC9 DC983 3022083WP FLOOR SUPPORT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK DURING 15K CHECK, FOUND FLOOR SUPPORT FITTING BETWEEN PANELS C1 AND C2 IS CRACKED. REPLACED FITTING PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20031215000652003121500065EA 2003 12 15 COMA0370052 120031114A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA 10062 PRESSURE BULKHEAD WEB AT FS 1098 STR 8R, 9R IS CRACKED AT NR 4 HYD LINE CONNECTION. PERFORMED MAJOR REPAIR IN ACCORDANCE WITH CANADAIR REO 670-53-61-034 REV B. 2L72 4F RTA21EA 20031215001962003121500196EU 2003 12 15 USAA030239 120031026A5210 SKIN AIRBUSA321 A321211 3930370EU L3 DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19165US9631 1431 CLT - FOUND DOOR SKIN CRACKED 2.5 INCH, L3 DOOR UPPER FORWARD CORNER OF EXT DOOR SKIN. IDENT PART CHANGE AND INSTALLED WITH FASTENERS PER SRM 52-42-11. (M) 2L72 4F RTA28NM 20040520001042004052000104SO 2004 5 20 RAIA00404013 120030422A3040163500111 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT SHORTED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03824HK1602 145498 ELECTRIC ODOR ON FLIGHT DECK. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD. 2L72 4T RTT00011AT 20060801002482006080100248WP 2006 8 1 IXXA060489S 120030124A5320 FLOOR SUPPORT DOUG DC8 DC871F 302199DWP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND COCKPIT FLOOR PANEL 674A ATTACH ANGLE CORRODED. REMOVED DAMAGED ATTACH ANGLE. FABRICATED NEW ATTACH ANGLE, LOCATED, DRILLED TRIMMED, TREATED, PRIMED AND INSTALLED NEW ATTACH ANGLE IAW DC8 SRM 51-1-8, 53-2-0, 53-7-3 51-9-0, AND 51-3-0. 2L74 4F RT4A25 20060328002012006032800201SO 2006 3 28 MASA200300501 120031218A2731 WARNING LIGHT EMB 145 EMB145LR 3260212SO TRIM SYSTEM ILLUMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07831MJ 145273 ASH NR 2715, CLT RETURNED TO FIELD WITH A PITCH TRIM INOP WARNING MSG. MX RESET THE SYSTEM. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20030818000812003081800081 2003 8 18 HEEA088627 420030709A3120206070275005 CLOCK AEROSPAS355 AS355* EU COCKPIT INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03732AE 2873 DOES NOT KEEP CORRECT TIME. 1G72 3U H11EU 20030819000472003081900047NE 2003 8 19 A6WA200340104 220030624A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 MALFUNCTIONED A A6WAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL31443AW 7781 ABORTED TAKEOFF, 140 KNOTS NR 2 ENGINE N2 DROPPED OFF TO APPROX 50-60 PERCENT. ON TAKEOFF ROLL, BRAKE MAX TEMPS WERE 11, 9, 7, 8 ABORTED TAKEOFF, TAKEOFF AT 1655Z MARKED FDR AT 1704Z. PERFORMED ACCELERATION/DECELERATION CHECKS AND POWER ASSURANCE CHECKS, NO DEFECTS NOTED. COULD NOT DUPLICATE. INSPECTED TIRES AND BRAKES AS PER AMM 05-51-29, OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20030821000432003082100043NM 2003 8 21 03FDEA01020 120030624A5753ARC198413 FITTING DOUG MD11 MD11 3023602NM TE FLAP HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE INBOARD SIDE CORRODED (FLAP SIDE). LEFT WING - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING PIVOT BEARING MOUNT HOLE INBOARD SIDE CORROSION (FLAP SIDE) REPAIR CARRIED-OUT IAW FEDEX EA 1-5750- 69352 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030328001002003032800100EU 2003 3 28 CX7A194J32 120030304A26121734362450 SENSOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7ACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL03306CE 340B203 LT TAILPIPE HOT LIGHT DURING T/O AT 200 FT REPORTED BY CREW 2L72 4T RTA52EU 20030331000982003033100098NM 2003 3 31 CALA0300147 120030327A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917619 27332 INSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT AT STA 344, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-40-3. 2L72 4F RTA16WE 20030820002112003082000211EA 2003 8 20 ASOA03332 120030721A5320 BRACKET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11709EV 10068 DURING A HANGAR CHECK IN BTR, THE BLEED AIR DUCT SUPPORT BRACKET ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BLEED AIR DUCT SUPPORT BRACKET ON THE LEFT SIDE IAW ASA EO 700-36-0003A. (M) 2L72 4F RTA21EA 20030401001262003040100126WP 2003 4 1 DHL2003804518 120030125A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 603.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED ANGLE DOUBLER (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030403000922003040300092EA 2003 4 3 COMA0360173 120030330A2621346000371 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA11622 7241 FLGIHT 5198 - CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLES 2L72 4F RTA21EA 20030403001302003040300130NM 2003 4 3 DL733030314 120030329A53306545767132 SKIN BOEING737 737347 1384647NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 470 BETWEEN STRINGERS 22L & 23L. THE DENT WAS REMOVED WITH A 7 INCHES CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384681-14, REV A. 2L72 4F RTA16WE 20030328000502003032800050SO 2003 3 28 C2XA03TY041 120030327A531014521725615 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716954 145072 DURING A SCHEULED INSPECTION THE SERVICE DOOR AFT SILL WAS FOUND TO CORRODED BETWEEN FRAMES 21 AND 22A. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20030407000512003040700051NM 2003 4 7 KPVA20035 120030131A33506104781 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EXIT SIGN INOPERATIVE A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13807WP643 023 LEFT AFT EXIT EGRESS, AFT CEILING AISLE, LEFT AFT EXIT SIGN AND LEFT AFT MID CABIN EXIT LOCATOR LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY NR 3357, PAG 3 AND OPS CHECK IAW DHC-8 MM 33-51-00 PAGE 201-202. OPS CHECK GOOD. (M) 2H72 4T RTA13NM 20030416000692003041600069NM 2003 4 16 QXEA0300439 120030410A2930 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007NM NR 2 CONTAMINATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09367PH 511 PDX - FLIGHT 2131 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND AIR IN THE NR 2 HYDRAULIC SYSTEM. THE HYDRAULIC SYSTEM WAS BLED AND OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20030423000872003042300087EU 2003 4 23 XG3R085889 120030401A3310013020020010 POWER SUPPLY UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE INSTRUMENT PANELSHORTED E XG3RO OTHER O OTHER NRNOT REPORTED 1 FS0126LB 550 3514 23017 PARTIAL FAILURE OF POWER SUPPLY. EXPERIENCED A BACKLIGHTING FAILURE OF THE COMM RADIOS, ENGINE CONTROL PLATE AND TFO PANEL. USING THE WIRING DIAGRAM , 33-10-00-001, PAGE 1002, I TRACED THE FAILURE TO PIN 12 OF THE NORMAL LIGHTING POWER SUPPLY (148L). ALTHOUGH THE COMPASS AND INSTRUMENT PANEL PLATE ARE ALSO PART OF THE NORMAL LIGHTING POWER SUPPLY, THAT SECTION OF THE POWER SUPPLY WAS WORKING NORMALLY, IT WAS ONLY PIN 12 (28V/P5) THAT HAD FAILED. 1G72 3U3 U H9EU E00054EN 20030424000572003042400057NM 2003 4 24 QXEA0300332 120030227A5350 FLANGE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261FT, AFT FLANGE, BETWEEN CAMLOC HOLES. BLENDED DAMAGED AREA. 2H72 4T RTA13NM 20030424001952003042400195EA 2003 4 24 SWIA200311846 120030322A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE ACTIVATIONA SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07412SW 7101 DURING CLIMBOUT CABIN DOOR LATCH CAUTION ON EICAS (PAX DOOR LATCH CAUTION). CABIN WAS HOLDING PRESSURE. OUT OF 25,000 FT PASSENGER DOOR WARNING EICAS MESSAGE APPEARED. RETURNED TO SLC. INSPECTED PASSENGER DOOR, NO DEFECTS NOTED. INTERROGATED PSEU, NO FAULTS FOUND. PRESSURIZED AIRCRAFT IAW MM 21-31-00. NO DEFECTS NOTED, CANNOT DUPLICATE AT THIS TIME. 2L72 4F RTA21EA 20030425000912003042500091NM 2003 4 25 QXEA0300398 120030316A5420 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND LOWER COWL UPPER ANGLE IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030429000102003042900010NM 2003 4 29 P5CA0300789 120030216A5730 SKIN BOEING747 747283B 1384867NM RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RIGHT WING L/E LWR SURFACE STA 1380-1385 FOUND CORROSION IN LWR SURFACE. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH DOUBLER PER SRM 57-30-03 FIG -9. 2L74 4F A20WE 20030424002062003042400206WP 2003 4 24 UPS03840366 120030312A5500 FITTING DOUG DC8 DC873F 302199FWP EMPENNAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, EMPENNAGE LT FITTING CRACKED FROM LBL 2-LBL 8 SECOND J BEAM FROM BELLY SKIN. PERFORMED HFEC IAW NDT SPM 06-10-01. FOUND CRACK ON FITTING REMOVED FITTING TO FOM. LOCATED DRILLED DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030428001492003042800149EA 2003 4 28 03098658 120030407A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CENTER CABIN EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030429000742003042900074NM 2003 4 29 P5CA0300819 120030410A5330 SKIN BOEING747 747249F 1384849NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 B-STA 460 ABOVE IL DOOR CUTOUT CENTER 2.5 INCH CRACK. REPAIRED PER SRM 53-10-04 5B 747 53A 2396. 2L74 4F A20WE 20030501001832003050100183NM 2003 5 1 ASAA0310065 120030301A5230654795711 PLATE BOEING737 737298C 1384490NM CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AFT PIT DOOR TRANSITION PLATE AT BS 772-847, RIGHT BUTTOCK LINE 20 CORRODED. REMOVED AND REPLACED TRANSITION PANEL PER SRM. (M) 2L72 4F RTA16WE 20030502001892003050200189EU 2003 5 2 AWXA200300415 120030417A5340D5323003020000 FITTING AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND FORWARD CARGO FRAME CUTOUT AFT SIDE FITTING, FR 28, STR 35 RT. MAINTENANCE REMOVED DAMAGED FORWARD CARGO FRAME CUTOUT AFT SIDE FITTING, FR 28, STR 35 RT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 5-6. 2L72 4F RTA28NM 20030502000252003050200025NM 2003 5 2 USAABB03054 120030402A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6 AND 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20030506000622003050600062EU 2003 5 6 03FDEA00650 120030429A5730 PANEL AIRBUS300 A300B4605R 3930308EU RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25682FE 800 DEEP GOUGE IN RT WING L/E PNL 612B, FOUND TO BE OUT OF LIMITS PER IAW SRM 57-41-11. REPLACED PNL, TREATED, PRIMED AND PAINTED PER IAW SRM 51-40-44, SRM 51-75-10 AND SRM 51-21-10. 2L72 4F RTA35EU 20030508000352003050800035WP 2003 5 8 DHL2003807006 120030503A3260 STRIKER DOUG DC8 DC873F 302199FWP MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01807DH 45990 GEAR NOT LATCHED LIGHT ILLUMINATED, RAN GEAR OR DOOR NOT LATCHED LIGHT ILLUMINATED ABNORMAL PROCEDURE, DOOR NOT LATCHED LIGHT EXTINGUISHED. TROUBLESHOT SYSTEM PER DC-8 M/M 32-60-00. ADJUSTED BOTH MAIN DOOR LT/RT ROLLER/STRIKER ASSEMBLIES AND PERFORMED GEAR SWING IAW DC-8 M/M 32-12-1. OPS CHECKED GOOD OK FOR SERVICE. 2L74 4F RT4A25 20030513001212003051300121 2003 5 13 DL764030384 420030424A2565 BULB BOEING767 767* NM SLIDE INDICATOR BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27832MH 29704 DOOR 4R SLIDE ARM LIGHT INOPERATIVE. RELAMPED SAME 2L72 4F RTA1NM 20030602001602003060200160NE 2003 6 2 VNAA0305019 220030529A73208110995L27 HMU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07437JS1809051 3055 DURING TAKEOFF, THE LEFT HAND ENGINE WAS ONLY PRODUCING 90 PERCENT TORQUE AND THE CREW ABORTED TAKEOFF. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND REMOVED THE LEFT HAND ELECTRONIC ENGINE CONTROL, AND THE LEFT HAND HYDROMECHANICAL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030609000552003060900055WP 2003 6 9 ZW0A0305003 120030521A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13905TW 49157 THE EMERGENCY LIGHTS AT BOTH AFT OVERWING EXITS, AND THE RT SIDEWALL EMERGENCY LIGHT IN THE TAILCONE, WERE INOPERATIVE. REPLACED THE BATTERY PN 408822101 IN THE BATTERY PACK FOR THE EXIT LIGHTS, AND REPLACED THE LAMP PN 1315 IN THE TAIL CONE. CHECK-C 12-03-2002 STL. 2L72 4F A6WE 20030609001272003060900127EU 2003 6 9 MALA030274 120030504A5530 ANGLE BAC 146 AVRO146RJ85A1500097EU VERTICAL STAB CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15525XJ E2350 DURING C-CHECK INSPECTION IN CVG, LT VERTICAL STAB TO FUSELAGE CLOSING ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED CLOSING ANGLE IAW EO A55024. REF 409 118064 FOR DETAIL. A/C RELEASE DATE 5/21/03. 2H74 4F RTA49EU 20030609000932003060900093EU 2003 6 9 AWXA200300574 120030521A5210FE1740031 CYLINDER AIRBUS320 A320231 3930325EU R-1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW4734 81 DURING 4-DAY CHECK THE R-1 DOOR ASSIST BOTTLE PRESSURE WAS FOUND AT 500 PSI. MAINTENANCE REPLACED O-RING SEALS ON R-1 DOOR DAMPER CYLINDER ASSEMBLY; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030611000162003061100016WP 2003 6 11 GTIA030324 120030506A5522 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE RT ELEVATOR CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23815NK 49415 MISSING MATERIAL FROM TIP END RT ELEVATOR AT RT ELEVATOR MOST OUTBOARD STATIC WICK AREA, DUE TO CORROSION. REMOVED AND REPLACED DOUBLER WITH NEW PART. FABRICATED PART IAW MFG DRAWING NR 5910412 INSTALLED IAW SRM 51-30 STANDARD PRACTICES. 2L72 4F4 FRTA6WE E2EA 20030612000102003061200010SO 2003 6 12 SWIA200312018 120030425A5330 SKIN EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07295SW 120322 CRACK ON SKIN SUPPORT LEFT SIDE OF COCKPIT BEHIND DV WINDOW. FOUND DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT LEFT SIDE OF COCKPIT AFT OF DV WINDOW PER MM 53-00-00 AND 51-00-00. 2L72 4T RTA31SO 20030612000412003061200041 2003 6 12 CALA0300270 420030528A2565D29982107 SLIDE DOUG DC9 DC982 3022082WP R-1 DOOR DISCHARGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2792874307862234 49122 INSPECTION FOUND THE R-1 DOOR SLIDE PRESSURE LOW. THE EMERGENCY DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-00. 2L72 4F A6WE 20030521001782003052100178WP 2003 5 21 DHL2003801073 120030505A5230 BEAM DOUG DC8 DC873F 302199FWP DOOR CRANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 UPPER CARGO DOOR LOCK PINS MECH BEAM CRACKED 1.000 INCH AT STA 230.000. REMOVED AND REPLACED DAMAGED BEAM AT STA 230.000 AND SECURED WITH BOLTS AND RIVETS IAW SRM 51-1-21 PG 1, SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20030523001322003052300132NM 2003 5 23 QXEA0300504 120030419A5310 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX-DENT DAMAGE BETWEEN X281.0 AND X301.0, STRINGER 6 AND STRINGER 7. REPAIRED IAW RD84-53-443 AND HORIZON AIR EA 6-53-171. 2H72 4T RTA13NM 20030527000782003052700078WP 2003 5 27 AALA20030453 120030413A25601001191 FLASHLIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21221AA 49172 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT PORTABLE FLASHLIGHT DIM. REPLACED FORWARD EMERGENCY EXIT PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030618000812003061800081NM 2003 6 18 SWAA031318 120030611A57536546434 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29647SW 27717 DURING SCHEDULED C3 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED AT OUTBD END. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040114000322004011400032NM 2004 1 14 SWAA032768 120031218A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 44, WL 208, BS 986.5, LBL 12, WL 208, BS 986.5, LBL 13.5, BS 986, LBL 14, WL 209, BS 986, LBL 44, WL 209, BS 986.5 LBL 16, WL 210, BS 947.5, RBL 11, WL 208, BS 947.5, RBL 15 WL 208, BS 947, RBL 8, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040114000982004011400098NM 2004 1 14 DL73S031036 120031117A5330654577561 SKIN BOEING737 737232 1384475NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 THE FUSELAGE SKIN WAS FOUND DAMAGED AROUND 2 NUT PLATE HOLES USED FOR ATTACHMENT OF A WING TO FUSELAGE FAIRING PANEL AT FS 760 BETWEEN STRINGERS 19R & 20R. THE DAMAGED HOLES WERE REMOVED WITH 1.5 X 1 INCH LOCAL CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER/TRIPLER REPAIR PER ER/A 087539-14, REV A. 2L72 4F RTA16WE 20040114001012004011400101NM 2004 1 14 DL73S031040 120031121A5330 SKIN PANEL BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 DURING ACCOMPLISHMENT OF 03-058543-03, ME-01 EXISTING REPAIRS AND NEW CRACK DAMAGE WERE NOTED ON THE KEEL BEAM LOWER SKIN PANEL. THE SUBJECT SKIN PANEL WAS REPLACED PER INSTRUCTIONS CONTAINED IN ERA 385772-14. 2L72 4F RTA16WE 20031125001392003112500139NM 2003 11 25 ASAA0310148 120030317A53476573746 SEAT TRACK BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 807-867, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20031125001472003112500147NM 2003 11 25 ASAA0340124 120030310A572069773281 CHANNEL BOEING737 737490 1384715NM LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 PAE - DURING C-CHECK, FOUND LEFT WING UPPER INBOARD TRAILING EDGE PANEL SUPPORT CHANNEL CRACKED WBL 87. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20031212001742003121200174EA 2003 12 12 COMA0360520 120031127A3251 TRANSFORMER CNDAIRCL600 CL6002B19 1900309EA STEERING SYS MALFUNCTIONED A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO01506CA 7793 FLIGHT 5118) DURING APPROACH TO CVG RECEIVED A STEERING INOPERATIVE CAUTION, FIRE TRUCKS WERE CALLED OUT, AIRCRAFT LANDED SAFELY. REPLACED THE LT AND RT ROTARY VARIABLE DIFFERENTIAL TRANSFORMER. 2L72 4F RTA21EA 20031217000522003121700052WP 2003 12 17 DHL2003805540 120030729A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OUTBD L/E FRAME CRACKED 0.500 AT STA XFS 835.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032). INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10. REFER TO NR 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031217001502003121700150NM 2003 12 17 DHL2003742506 120031201A5347 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, CABIN SEAT TRACK LBL 42 BS 990/1050 HAS CORROSION. FOUND SEAT TRACK TO BE OUT OF LIMIT AT LBL 42 BS 990-1080 IAW SRM B-727-53-10-1 FIG 3. FABRICATED SEAT TRACK AT LBL 42 BS 990-1080 MAT USED BAC1520-792 PO 99125 DIAMETER 60 INCHES IAW B-727 SRM 53-10-5 FIG 2. ALODINE AND PRIME IAW B-727 SRM 51-10-2. INSTALLED NEW SEAT TRACK BS 990 TO 1050 LBL 42 INCHES IAW B-727 SRM 53-10-5 FIG 7. 2L73 4F A3WE 20031222000542003122200054WP 2003 12 22 ASAA0380621 120031007A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC - FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS DELAMINATED AT TWO LOCATIONS BETWEEN FS 541 AND 617. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20031219001582003121900158NM 2003 12 19 03FDEA02144 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE BORE CORRODED. LT WING, O/B FLAP I/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73357 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031223000132003122300013NM 2003 12 23 SWAA032655 120031203A55536546872 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB LT ATTACH FITTING AFT BODY LUG CORRODED. REPAIRED LUG PER SRM AND BFG ER. 2L72 4F RTA16WE 20031223000302003122300030NM 2003 12 23 SWAA032633 120031201A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20031229000102003122900010WP 2003 12 29 ABXA030463 120031124A52309957664503 INTERCOSTAL DOUG DC9 DC941 302207NWP FWD CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 FORWARD LOWER CARGO DOOR INTERCOSTAL WEB CRACKED AT LOWER AFT SIDE BY DOOR STOP MARKED AS NR 6. REMOVED AND REPLACED INTERCOSTAL IAW DC-9 MM AND ON ABX NON ROUTINE CARD 0228. 2L72 4F A6WE 20031231000472003123100047EA 2003 12 31 ASOA03581 120031115A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA AIRSTAIR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11859AS 7421 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040105000952004010500095WP 2004 1 5 DHL2003802528 120031117A53203758497IN FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 2.000, STA 1180.000 - STA 1200.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031010000782003101000078EU 2003 10 10 03260308 120030917A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27308UE 41023 DURING INSPECTION THE EMERGENCY LIGHT ON THE FOWARD BULKHEAD WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL FOUND A WIRE DETACHED FROM THE IN LINE CONNECTOR AND RESECURED IT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4T RTA41NM 20040114002292004011400229EA 2004 1 14 033286256 120031124A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING HEAVY CHECK INSPECTION THE FLOORBEAM AT FS 360 LBL 9 WAS IDENTIFIED AS HAVING HEAVY CORROSION. FLOORBEAM WAS REPAIRED IAW SRM AND AIRCRAFT WAS RELEASED FOR SERVICE UPON COMPLETION OF HEAVY CHECK INSPECTION. 2L72 4F RTA21EA 20031124000522003112400052NM 2003 11 24 03FDEA01911 120031113A5320 WEB BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 CORROSION (C53-224-04), SHEAR WEB BS 1166-1173, RBL 53-62, WL 208. 2L73 4F RTA3WE 20040311000342004031100034NM 2004 3 11 ASAA0310126 120030309A532069439467 CHANNEL BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND CHANNEL AT BS 301-320, BUTTOCK LINE 0 CRACKED. REMOVED AND REPLACED CHANNEL PER SRM. (M) 2L72 4F A16WE 20031204000602003120400060WP 2003 12 4 AALA20031017 120030917A33500201991008 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2170529 49921 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROW 7D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031204002042003120400204WP 2003 12 4 UPS03841456 120031017A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 FOUND EXTENSIVE CORROSION AT STATION 1746 SEVERAL RIVETS PULLED THROUGH SKIN. SKIN IS CRACKED AT L36 AND STA 1746. REMOVED FASTENERS IN CORRODED AREA FOUND L36 AFT OF STA 1746. REMOVED 9 X 6 SECTION OF SKIN REF SRM 53-02-011 NR 39550, REF ECA 56908 LOG PAGE 039299 PAGE 27. 2L74 4F RT4A25 20031205000652003120500065NM 2003 12 5 UPS03441458 120031012A541065B90411603 FRAME BOEING747 747200 1384847NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, NR 2 PYLON - LT AND RT NAC STA 286.5 FRAME FOUND CRACKED. DURING DIAG BRACE STEEL FITTING MOD ACCOMPLISHMENT. LT AND RT NAC STA 286.5 FRAME REPLACE AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20031205000092003120500009NM 2003 12 5 C1HA200381030 120031021A3350 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 L-2 AND R-2 DOOR EMERGENCY SLIDE LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY. OPS CHECK WAS GOOD. REF: 727 MM 33-50-51. 2L73 4F A3WE 20031210000452003121000045CE 2003 12 10 ACE112503 120031125A3260 WARNING SYSTEM BEECH 1900 1900C 1154161CE COCKPIT MALFUNCTIONED E YADAO OTHER N FALSE WARNING APAPPROACH 1 AL03113AX UC41 NOSE GEAR FAILED TO SHOW DOWN AND LOCKED UNTIL GEAR WAS CYCLED TWICE. MAINTENANCE COULD NOT DUPLICATE FAULT. 2L72 4T RTA24CE 20030916001372003091600137WP 2003 9 16 GTIA030630 120030725A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND COCKPIT FLOOR PANEL LEFT INBOARD STATION 120-148 CRACKED AND CORRODED. FABRICATED FLOOR PANEL. (M) 2L72 4F RTA6WE 20030918000122003091800012NM 2003 9 18 03FDEA01509 120030911A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CREASED & DENTED SKIN , BS 620 TO BS 640 STR 21. CUT OUT DAMAGED SKIN BS 620 TO 640 STR 21 RT 4.3 X 19.7 AND INSTALLED REPAIR DOUBLER TRIPLER AND FILLER IAW FEDEX EA 7-5330-70507. 2L73 4F RTA3WE 20030919001432003091900143 2003 9 19 2904031103 420030311A34215040017901 GYRO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE COCKPIT INOPERATIVE E S4WAO OTHER O OTHER NRNOT REPORTED 1 WP074027Q3196 2904 9456 DIRECTIONAL GYRO INOPERATIVE. 1G71 3U3 U H9EU E00054EN 20030919001512003091900151EU 2003 9 19 AWXA200300931 120030803A5320D53470478204 PROFILE AIRBUS320 A320232 3930326EU CARGO DOORWAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT TRANSITION PROFILE BETWEEN FR 58 AND FR 60. MAINTENANCE REMOVED PROFILE FROM FR 58 TO 60; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW AWA E.R. 26-5320-03154-SS1. 2L72 4F RTA28NM 20040217001932004021700193CE 2004 2 17 DXTA200300140 120031016A2432 ODOR CESSNA500 560CESSNA 2076750CE BATTERY BAY DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07304QS 5600408 ELECTRICAL ODOR ORIGINATING FROM CABIN AREA. SAME ODOR NOTICED IN BATTERY COMPARTMENT ON POST FLIGHT. - RAN AIRCRAFT AT CRUISE POWER FOR ONE HOUR, NO CIRCUIT BREAKERS POPPED, BATTERY TEMP STAYED AT 47 DEGREES F, TURNED A/C FREON UNIT ON , AVIONICS ON , AIRCRAFT SIMULATED CRUISE FLIGHT ON GROUND, DID NOT NOTICE ANY TYPE OF ELECTRICAL ODOR. 2L72 4F RTA22CE 20031211001162003121100116NM 2003 12 11 AALA20031394 120031206A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21775AN 29584 DFW FIRST CLASS GALLEY WALL MOUNTED EMERGENCY LIGHT ASSEMBLY ACROSS FROM 1L DOOR INOPERATIVE. REPLACED FIRST CLASS GALLEY WALL MOUNTED EMERGENCY LIGHT ASSEMBLY ACROSS FROM 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040309001572004030900157WP 2004 3 9 GTIA031061 120031112A7830 EXHAUST DUCT DOUG DC9 DC981 3022081WP THRUST REVERSER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND RIGHT ENGINE T/R S/N 49507 ACOUSTIC EXHAUST DUCT INTERIOR NUMEROUS AREAS OF DELAMINATION. REPAIRED DAMAGED AREA. (M) 2L72 4F A6WE 20030618001112003061800111NM 2003 6 18 SWAA031289 120030609A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030619000042003061900004SW 2003 6 19 HEEA087175 120030609A6320 SEAL BELL 206 206L1 1182107SW OIL PUMP LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0383MT SP502 45492 GEARBOX OIL PUMP SEAL LEAKING. REPLACED SHAFT 357950110932 DUE TO WORN SPLINES. REPAIRED. 1G71 3U H2SW 20030528000732003052800073NM 2003 5 28 AMTA200300601 120030418A5330 SKIN BOEING757 75733N 1384931NM FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11553TZ 32587 FUSELAGE SKIN DENTS AFT OF L2 DOOR REQUIRE PERMANENT REPAIR. REPAIRED SKIN DAMAGE IAW ER/A 757-53R-5145. (M) 2L72 4F RTA2NM 20030619000312003061900031SW 2003 6 19 HEEA087380 120030611A5210407070620218 PANEL BELL 407 407 1182206SW DOOR TRIM CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 CREW DOOR TRIM PANEL CRACKED. 1G71 3U O H2SW 20030624000312003062400031NM 2003 6 24 CALA0300313 120030614A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND AFT BAGGAGE BIN STRAP CORRODED BETWEEN STA 777 AND 847, RBL 20. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030630000132003063000013NM 2003 6 30 DHL2003782005 120030529A3260 PROXIMITY SWITCH BOEING727 727227 1384078NM MLG DOOR OBSTRUCTED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01769AT 21998 DURING GEAR RETRACTION THE RED LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. COMPLIED WITH ABNORMAL PROCEDURES ON PAGE 6.2.70. FOUND LEFT GEAR PROXIMITY SWITCH WIRE BUNDLE OBSTRUCTING PROXIMITY SWITCH. REPOSITIONED AND SECURED WIRE BUNDLE IAW M/M 32-30-0. OPS CHECKED NORMAL IAW M/M 32-31-0. 2L73 4F A3WE 20030702000122003070200012EA 2003 7 2 A6WA200340049 120030328A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31431AW 7256 ONE LIGHTENING STRIKE DAMGED AREA IN OPEN BAY AT FS 265, BETWEEN STRINGERS L25 AND L26 TRIMMED OUT DAMAGED AREA OF SKIN PANEL. COMPLIED WITH EDDY CURRENT OF CUT LINE FROM DAMAGE REMOVAL. NO INDICATIONS NOTED AT THIS TIME. FABRICATED FILLER. COMPLIED WITH WVAC EO 601R-53-3909 STEPS 3 THROUGH 9 AND 11. OK TO INSTLAL. COMPLIED WITH STEPS 12. (M) 2L72 4F RTA21EA 20030711001122003071100112CE 2003 7 11 GLBA2003095 120030627A7500 TUBE BEECH 1900 1900D 1154162CE BLEED AIR DAMAGED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03170GL UE170 RIGHT BLEED AIR FAIL. REPAIRED SPLIT EVA TUBING, OPS CK GOOD. 2L72 4T RTA24CE 20030702000492003070200049WP 2003 7 2 GTIA030398 120030513A5320 SUPPORT ANGLE DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND FORWARD SIDE OF FORWARD BULKHEAD, STATION 36 RBL 4, SUPPORT ANGLE ON SHELF BELOW RADAR ANTENNA IS CRACKED IN RADIUS (DOT LP005) PEELING PAINT/BARE METAL UPPER SURFACE ON SHELF. REMOVED CRACKED SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE. (M) 2L72 4F A6WE 20030110000682003011000068WP 2003 1 10 ZW0A0300401 120030106A3350LP7732001 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139628W 53598 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 4 TO 5. REPLACED SECTION OF LIGHTS. CHECK-C12-23-2002. --CLOSED--- 2L72 4F RTA6WE 20030124000142003012400014WP 2003 1 24 ZW0A0301101 120030123A33507732 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13963TW 53613 EGRESS LIGHTS INOP IN ROW 16 THROUGH 25. REPLACED SEVERAL LAMPS IN EGRESS LIGHT SYSTEM AND OPS CHECK NORMAL PER MM. LAST CHECK-C STL 5-20-02. --CLOSED-- 2L72 4F RTA6WE 20030127000242003012700024 2003 1 27 HEEA083600 420030114A3442MI5852013 INDICATOR BELL 412 412 1182202SW RADAR SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 RADAR INOPERATIVE. SHOP REPAIR. 1G72 4U H4SW 20030127001582003012700158SW 2003 1 27 HEEA083688 120030115A2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH341 3780 53283 STARTER GEN BRUSHES WORN. REPAIRED. 1G71 3U O H2SW 20030128001032003012800103NM 2003 1 28 03FDEA00042 120030115A73318TJ95GAB3 INDICATOR BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE COCKPIT ERRATIC A FDEAO OTHER N FALSE WARNING TOTAKEOFF 1 SO25206FE4820 4820 22928 ON TAKEOFF ROLL, JUST PRIOR TO V1, ALL 3 FUEL FLOW INDICATIONS BECAME ERRATIC. AFTER TAKEOFF ALL 3 FUEL FLOW INDICATORS WERE READING APPROX CORRECT BUT FLUCTUATIONS +/- 2000 LBS. AFTER 10 MINUTES ALL THREE FUEL FLOW GAUGES BECAME COMPLETELY ERRATIC AND UNUSABLE. CHECKED 28VDC AND 115VDC TO FUEL FLOW POWER SUPPLY CONNECTOR D100 AT PINS 2 AND 7 AND GROUNDS AT PINS 1 AND 6 WHILE SHAKING OUT WIRING. CHECK WIRING FOR SHORTS TO GROUND AND CONTINUITY FROM POWER SUPPLY TO F/ F INDICATORS WHILE SHAKING OUT WIRING. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY IAW MM. TAXIED AIRCRAFT AND RAN ALL THREE ENGINES TO HIGH POWER IAW JRH. ALL FUEL FLOW INDICATIONS CHECKED NORMAL. AIRCRAFT OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20030128001672003012800167WP 2003 1 28 ZW0A0300802 120030106A5320 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C IN THE NLG WHEEL WHEEL A CRACK WAS FOUND ON RT SIDE OF NOSE GEAR WHEEL WELL JUST ABOVE THE RT FWD NOSE GEAR DOOR FWD HINGE, 8 INCHES AFT OF STA 37 ON WHEEL WELL CUTOUT SUPPORT ANGLE ON THE RT SIDE. CRACK WAS THROUGH FASTENER. TWO STACKED DOUBLERS INSTALLED. STOP DRILLED CRACK AND REPAIRED PER SRM 53-01, PAGE 10. 2L72 4F A6WE 20030214001042003021400104NE 2003 2 14 0302081 220030208A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE LEFT FAILED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17146SD 146 514 DGR725688 FLIGHT 4506 PIT-CRW. DURING CLIMB, CREW NOTICED THE LEFT ENGINE TORQUE FLUCTUATING +/- 30-40 PERCENT AT A POWER SETTING OF ABOUT 90-100 PERCENT. ALSO HAD AN ERRATIC LEFT PROP RPM. A SLIGHT YAW WAS FELT WHILE A MORE NOTICABLE ENGINE SURGE WAS HEARD. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW DECLARED AN EMERGENCY AND STARTED THE RETURN TO PIT. CREW ENGAGED TORQUE MOTOR LOCK-OUT FOR THE LT ENGINE. THE PROBLEM WENT AWAY AFTER TML ENGAGED. AIRCRAFT RETURNED TO PIT SAFELY AND WAS TAKEN OUT OF SERVICE 2-8-03 AT 1355. AIRCRAFT FERRIED TO FWA 2-9-03, ARRIVED AT 1313. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030219001392003021900139NM 2003 2 19 USAA030002 120030106A5754 SKIN BOEING737 7373B7 1384580NM L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US47389 23318 PIT - FOUND SKIN CRACKED .5 INCH IN TWO PLACES, NR 6 SLAT LOWER LEADING EDGE SKIN NEAR ACTUATOR FITTING. REPAIRED WITH FILLER AND DOUBLER PER SRM 57-43-01 FIG 206. (M) 2L72 4F RTA16WE 20030224000272003022400027WP 2003 2 24 MWEA030110 120030221A534039151501 SUPPORT FITTING DOUG DC9 DC981 3022081WP BEAM #1 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 PAX DOOR INERCOSTAL SUPPORT FITTINGS AT DOOR CENTER LINE ABOVE BEAM #1 CRACKED. -- LOCATED, DRILLED AND INSTLALLED SUPPORT FITTINGS. 2L72 4F A6WE 20030116002052003011600205SW 2003 1 16 HEEA083120 120030108A6700 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 ROTORCRAFT FLIGHT CONTROLS BELLCRANK HAS WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030304000102003030400010SW 2003 3 4 AC2A084866 120030224A6420222012734005 CONE SET BELL 430 430 1182150SW TAIL ROTOR GROOVED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT 49089 TAIL ROTOR CONE SET WAS GROOVED. REPLACED CONE SET. 1G72 3U RTH9SW 20030227001362003022700136EU 2003 2 27 AWXA200300209 120030210A3350ABS0374A24 CABLE AIRBUS320 A320232 3930326EU SEAT ROW 9 R/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW0 0 1079 PHX - EEL - DURING P-06 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 R/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT SEAT ROW 9 R/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030303001162003030300116SW 2003 3 3 HEEA084533 120030214A2840384178103 SWITCH BELL 412 412 1182202SW FUEL SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 SIDE TO SIDE TOTAL READINGS AT 240 LBS. REPLACED SWITCH. 1G72 4U H4SW 20030324000012003032400001NM 2003 3 24 03080417 120030321A3350 LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27417FJ 3174 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS AT SEAT ROWS 4 AND 6 WERE INOPERATIVE. MAINTENANCE PERSONNEL RESET THE FLOOR LEVEL EMERGENCY LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20030325000902003032500090EA 2003 3 25 03084660 120030325A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA RT OVERWING INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27660BR 7519 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030307000692003030700069 2003 3 7 SWAA030483 420030304A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20030307001802003030700180EU 2003 3 7 AALA20030069 120030116A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211442E 11437 DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT AT SEAT ROW 19 INOPERATIVE. REPLACED OVERWING EMERGENCY EXIT LIGHT AT SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030310001192003031000119WP 2003 3 10 CALA0300103 120030307A5330 SKIN DOUG DC9 DC981 3022081WP STA 1338 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 INSPECTION FOUND 0.01" CRACK IN FUSELAGE SKIN AT STA 1338 BELOW LONGERON 4R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220. 2L72 4F A6WE 20030314000762003031400076NM 2003 3 14 CALA0300082 120030302A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM STA 664 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914307 23358 INSPECTION FOUND A .5 INCH CRACK IN PRESSURE DECK WEB AT STA 664, RBL 30. REPAIRED PRESSURE WEB IAW SRM 53-60-51. 2L72 4F RTA16WE 20030122000662003012200066SW 2003 1 22 HEEA083454 120030109A3212OHSS2061003 COVER BELL 206 206L3 1182108SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 EMERGENCY FLOAT COVER WORN. TO BE SENT TO VENDOR. 1G71 3U H2SW 20030318000232003031800023 2003 3 18 BAQA085114 420030310A3421C17027AA01 INDICATOR UROCOPEC135 EC135T1 5620026EU ATTITUDE INACCURATE H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01511ME1648 0143 ADU 3000 FAILS FAR 91-411 CHECK. ALTITUDE INACCURATE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030318001992003031800199NM 2003 3 18 UPS03240294 120030220A5310 SEAT TRACK BOEING727 727108C 1384039NM BS 344 & 480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI CORROSION ON SEAT TRACK LBL 42.84 BETWEEN BS 344 & 480 SEAT TRACK REMOVED IAW SRM 51-30-2. NEW SEAT TRACK FABRICATED IAW S RM 51-20-1. NEW SEAT TRACK REPROECTED IAW SRM 51-10-2.NEW SEAT TRACK INSTALLED IAW SRM 51-30-2 2L73 4F A3WE 20030320000532003032000053NM 2003 3 20 USAASB03023 120030210A2781 MODULE BOEING737 737401 1384701NM INDICATOR FAILED A USAAO OTHER N FALSE WARNING DEDESCENT 1 EA19420US 23987 CLT - FLT 1132 - ON DESCENT INTO CLT, PASSING THROUGH FL190 AT 310 KNOTS, THE AMBER LEADING EDGE TRANSIT LIGHT ILLUMINATED. CREW SLOWED AIRCRAFT DOWN TO 230 KNOTS AND FELT AN AIRCRAFT VIBRATION WITH A SLIGHT RIGHT HAND ROLL TENDENCY. A FLAPS 15 LANDING WAS ACCOMPLISHED AS THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED INSPECTION OF LEADING EDGE SLAT DEVICES. NO FAULTS FOUND. ACCOMPLISHED TROUBLESHOOTING PER MM CHAPTER 27. REMOVED AND REPLACED THE M229 LEADING EDGE FLAP AND SLAT INDICATING MODULE AND FAULT CLEARED. ALSO, PERFORMED AUTOPILOT CHECK WITH NO FAULT RECORDED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20030321000062003032100006NM 2003 3 21 SWAA030627 120030319A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 518 @ STR 19R, BS 800 @ STR 21L & BS 942 @ STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030728001032003072800103 2003 7 28 SWAA031586 420030718A2565D31354 SLIDE BOEING737 7372H4 138448CNM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030730001212003073000121NE 2003 7 30 2003F00486 220030705A7261 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE NR 3 LEAKING A RYNAE ENGINE SHUTDOWN KMJFLUID LOSS OVER TEMP WARNING INDICATION DEDESCENT 1 CE07875AA 21387 DURING DESCENT AT FORT LAUDERDALE (KFLL), THE CREW SHUTDOWN NR 3 ENGINE DUE TO EXCESSIVELY HIGH OIL TEMPERATURE, FLICKERING FILTER BYPASS LIGHT, LOW OIL PRESSURE ON THE GATE AND LOW OIL PRESSURE LIGHT ON STEADY AS WELL AS DECREASING OIL PRESSURE. LANDED AT KFLL WITHOUT INCIDENT. INSPECTED AND FOUND ITNERNAL OIL LEAK BETWEEN NR 4 AND NR 5 ENGINE BEARINGS. REMOVED AND REPLACED NR 3 ENGINE. TRIMMED ENGINE. LEAK AND OPERATIONAL CHECKED NORMAL. (M) 2L73 4F4 FRTA3WE E2EA 20030801000182003080100018WP 2003 8 1 GTIA030544 120030613A5230 STOP FITTING DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND FORWARD PIT, DOOR STOPPER CORRODED 4 EACH AS MARKED. REMOVED AND REPLACED 4 EACH FORWARD PIT DOOR STOPS. (M) 2L72 4F A6WE 20030418001032003041800103WP 2003 4 18 UPS03840207 120030204A5711 SPAR DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C3, LT WING UPPER FRONT SPAR SHOWS EVIDENCE OF STRESS CORROSION AT APPROX ST A XRS 540. REMOVED CORROSION IAW DC8 SRM 51-1-8, FAB REPAIR STRAP AND FILLER IAW R EO G09022. ALODINED AND PRIMED REPAIR IAW DC8 SRM 51-1-8. INSTALLED REPAIR STRAP AND FILLER IAW REO G09022. FAB AND INSTALLED 1 BUSHING .3775 IAW DAC DWG 4709981 & REO G09022 AND DC8 SRM 51-1-25. 2L74 4F RT4A25 20030422000412003042200041EA 2003 4 22 ASOA03075 120030222A5346 SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A HANGAR CHECK IN MCN, THE UPPER AND LOWER WEB AT BL 0 ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE UPPER AND LOWER WEB AT BL 0 ENGINE SUPPORT BEAM IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20030422000522003042200052EU 2003 4 22 ASOA03104 120030312A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11635AS 372 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMLBY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030422001162003042200116NM 2003 4 22 GAIA03014OP 120030313A33501000679 LIGHT BOEING727 727223 1384074NM CABIN WEAK A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 L1 EMERGENCY EXIT LIGHT WEAK. REMOVED AND REPLACED L1 EMERGENCY EXIT LIGHT. OPS CHECK GOOD. (M) 2L73 4F A3WE 20030327001572003032700157SO 2003 3 27 C2XA03SH003 120030218A531014521713005 BEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 16 AND 24. MAINTENANCE REMOVED AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030801000752003080100075WP 2003 8 1 GTIA030539 120030610A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - LEFT ALTERNATE STATIC PORT FAILED AERODYNAMIC CLEANLINESS TEST AT 2D, 3C, 41 ON MYLAR OVERLAY. UPON REMOVAL OF STATIC PORT DOUBLER CORROSION WAS FOUND UNDER DOUBLER ON SKIN AND ON FINGER DOUBLER. FABRICATE DOUBLER REPAIR. INSTALLED DOUBLER REPAIR. (M) 2L72 4F A6WE 20030806000132003080600013EU 2003 8 6 BAQA088114 120030722A2435 BRUSHES AEROSPSA365 SA365N 8680669EU STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM1023 2345 6396 STARTER GENERATOR HAS BRUSHES WORN. 1G72 3U H10EU 20030806000252003080600025 2003 8 6 BAQA088122 420030717A3442MI5852001 RADAR LEAR 35 35A 5170602CE COCKPIT WEAK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0330DK 677 345 RADAR WEAK RETURNS. WRONG P/N R/T INSTALLED ON AIRCRAFT. HAS 12 INCH DISH. REPLACED WITH SERVICEABLE UNIT. 2L72 4F A10CE 20030805000992003080500099EA 2003 8 5 ASOA03265 120030618A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11869AS 7479 DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIPS WERE FOUND TO BE BURNED OUT. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030801001142003080100114NE 2003 8 1 COMA0360339 220030724A7200CR343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAA UNSCHED LANDING EY VIBRATION/BUFFET ENGINE STOPPAGE CLCLIMB 1 SO01807CA8585 7364 807603 FLIGHT 5284 LEFT ENGINE OIL PRESSURE WARNING AND SMALL VIBRATION, ENGINE THEN FAILED. REPLACED ENGINE. 2L72 4F4 FRTA21EA E15NE 20040226000162004022600016NM 2004 2 26 ASAA0370004 120030408A5320146A940118 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01607AS 29751 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT TEE. REPLACED FLOOR SUPPORT TEE PER SRM. (M) 2L72 4F RTA16WE 20030718000382003071800038NM 2003 7 18 USAASB03079 120030612A33501010428 SOCKET BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19785AU 25024 MAINTENANCE REPORTED THE OVERHEAD EMERGENCY LIGHT SOCKET IN THE BULLNOSE AT SEAT 10D WAS DISLODGED. MAINTENANCE REASSEMBLED SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030723000412003072300041WP 2003 7 23 MEX2003257 120030629A3340 LIGHT DOUG DC9 DC987 3022087WP TAIL CONE INTERMITTENT A ASMFO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML 49726 AIRCRAFT RETURNED TO GATE, TAIL CONE LIGHT CAME ON INTERMITTENTLY. LIGHT TEST, SAFETY MECHANISM AND SW OF TAIL CONE WERE CHECK IAW MM 52-70-11, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030722000562003072200056NM 2003 7 22 SWAA031496 120030706A5330589357 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON FO'S FWD WINDOW POST. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030827000982003082700098NM 2003 8 27 CALA0300425 120030730A5230 SKIN BOEING737 737524 1384721NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND IN AFT CARGO DOOR SKIN APPROXIMATELY 23 INCHES FROM FORWARD EDGE AND 23 INCHES FROM TOP EDGE. 2L72 4F RTA16WE 20030827001582003082700158NM 2003 8 27 2003UALA00612 120030807A5330 SKIN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29815UA 867 SKIN DAMAGE AFT LOWER OF DOOR 2L BETWEEN FRAMES 69 AND 70 AT STRINGER 23L. MAJOR REPAIR ACCOMPLISHED. EXTERNAL SKIN DOUBLER INSTALLED. 2L72 4F4 FRTA28NM E40NE 20030829001902003082900190WP 2003 8 29 GTIA030617 120030725A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND MAIN CABIN FLOOR PANEL STATION 1041 TO STATION 1079 HAS DETERIORATED/SOFT MUSHEY AND CORROSION AT INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030902000382003090200038WP 2003 9 2 L062003F00000 120030530A612022000407101 MOTOR CVAC 340 340CVAC 242270AWP FEATHER PUMP INOPERATIVE B LO6BO OTHER O OTHER NRNOT REPORTED 1 SW177813B 265 FOUND FEATHER PUMP INOPERATIVE. DURING PREFLIGHT RUNUP FOR TRAINING FLIGHT. TROUBLESHOOT FOUND ALL ELECTRICAL SYSTEMS OPERATING NORMALLY. PUMP DRIVE MOTOR DETERMINED TO BE INOPERATIVE. 2L72 4R 6A6 20030902000982003090200098WP 2003 9 2 BSY2003F00014 220030613A7320 COMPUTER LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE731* 01518WP FUEL SYSTEM FAILED E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL078040A 048 P74328 LEFT FUEL COMPUTER DROPPED OFFLINE, 100 MILES LINER RT FUEL COMPUTER DROPPED OFFLINE. ON APPROACH, PILOT RESET LEFT COMPUTER, THEN HE TRIED TO RESET RIGHT COMPUTER THE ENGINE SHUT DOWN BOTH COMPUTERS. RAN AIRCRAFT AND FOUND H VALVE LOWER FORWARD COUPLING (SHOOT) LEAKING HOT AIR INTO TAIL CONE AREA RT COUPLING. OPS CHECKS GOOD. 2L72 4F4 F A10CE E6WE 20030829000792003082900079NM 2003 8 29 DHL2003746011 120030711A3350 LIGHT BOEING727 727224 1384076NM L1 DOOR UNSECURE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01746DH 22252 EMERGENCY EXIT LIGHT FELL OFF. RE-SECURED L1 DOOR GROUND EXIT LIGHT, OPS CHECKED NORMAL IAW B727 M/M 33-50-00. 2L73 4F A3WE 20030728000642003072800064NM 2003 7 28 VNAA0307006 120030722A29134208601 PUMP DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE HYD SYSTEM FAILED A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL07471PS3346 3007 ON APPROACH INTO PHL THE FLIGHT CREW RECEIVED A FLAP CONTROL FAIL EICAS MESSAGE. THE FLIGHT CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND A FERRY FLIGHT WAS COMPLETED TO DAY. IN DAY MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC AC MOTOR/PUMP ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-11-04. FUNCTIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030724000842003072400084NE 2003 7 24 DL76G030555 220030617A7320233N62058 CONTROL PANEL BOEING767 7673P6 1385105NM GE CF6 CF680C2B6 30025NE NR 2 ENG FUEL FAULTY A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27155DL 25269 690372 RT ENGINE TOOK ONE MINUTE TO SHUTDOWN WHEN FUEL CONTROL SWITCH MOVED TO SHUTOFF. REPLACED FIRE CONTROL PANEL. 2L72 4F4 FRTA1NM E13NE 20030728000842003072800084 2003 7 28 SWAA031638 420030722A2565D31354 SLIDE BOEING737 7377H4 1384404NM SERVICE DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030812000592003081200059SW 2003 8 12 HEEA088505 120030725A6340412075010111 INDICATOR BELL 412 412 1182202SW TRIPLE TACH STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 TRIPLE TACH NEEDLES STICK TOGETHER. 1G72 4U H4SW 20030806001462003080600146NM 2003 8 6 AWXA200300821 120030707A5320D53974920011 PROFILE AIRBUSA319 A319132 3930340NM CARGO BAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 DURING C-04 CHECK .25 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT CEILING PANEL FORWARD PROFILE AT FORWARD END OF FR 51, Y1397. MAINTENANCE CUT OUT DAMAGED SECTION OF PROFILE AT FORWARD END OF FR 51, Y1397; FABRICATED A SPLICE REPAIR AND FILLER; INSTALLED REPAIR PART IAW AWA ER 26-5320- 03154-SS1. 2L72 4F RTA28NM 20030903002212003090300221NM 2003 9 3 QXEA200301007 120030816A3040 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09412QX 4059 SEA- ON FLIGHT 2265 WINDSHIELD CONTROL LIGHT CAME ON WHEN WINDSHIELD SELECTOR TURNED TO WARM UP AFTER ACCOMPLISHING CHECKLIST. PERFORMED TEST OF PILOT AND CO-PILOT WINDOW ANTI-ICING SYSTEM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030903001462003090300146NM 2003 9 3 AWXA200300803 120030712A5210 BOTTLE AIRBUSA319 A319132 3930340NM PAX DOOR DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28823AW 1463 CMH - EMERGENCY EVACUATION SYSTEM - DURING ROUTINE MAINTENANCE CHECK THE R1 DOOR ASSIST BOTTLE PRESSURE WAS FOUND LOW. MAINTENANCE SERVICED THE R-1 DOOR ASSIST BOTTLE PER AMM 52-10-00 PAGES 300-301 AS REQUIRED. 2L72 4F RTA28NM 20030821000302003082100030EU 2003 8 21 03FDEA00912 120030619A5315 FLOORBEAM AIRBUS300 A300B4605R 3930308EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE 742 FWD CARGO FLOORBEAM (27) RIGHT SIDE 24 INCHES FROM CENTERLINE HAS CRACK IN UPPER SECTION. REPAIRED FLOORBEAM (27) IAW A300-600 SRM 53-10-15. 2L72 4F RTA35EU 20030822000722003082200072NM 2003 8 22 0301166306 120030622A3350 POWER SUPPLY BOEING747 747451 1384940NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOP FROM ROWS 72-80 IN THE UPPER DECK. REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. REFERENCE LOG PAGE 2001935. 2L74 4F RTA20WE 20030825001192003082500119 2003 8 25 ABXA030327 420030812A2565101623303 SLIDE BOEING767 767281 1385109NM GE CF6 CF680A 30025NE L1 DOOR OUT OF POSITION A ABXAK NONE J WARNING INDICATION UKUNKNOWN 1 GL23767AX 265 22785 AFTER CLOSING ENTRY DOOR, ENTRY DOOR ANNUNCIATOR LIGHT ON. WENT TO RESECURE DOOR AND UPON OPENING, EMERGENCY SLIDE BEGAN TO FALL OUT OF DOOR. MAINTENANCE INSPECTED GIRT BAR MECHANISM. NO DEFECTS NOTED AT THIS TIME. REPLACED L1 SLIDE ASSEMBLY IAW B767 MM 25-66-01-4. DOOR OPENED AND CLOSED AND SLIDE ARMED SMOOTHLY. 2L72 4F4 FRTA1NM E13NE 20030730000502003073000050WP 2003 7 30 ABXA030257 120030312A5200 DOOR FRAME DOUG DC8 DC863F 302198FWP DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 UPPER LATCH HOOK MOUNT HOLE AT STA 176.5 HAD CRACK INDICATION. REPLACED STUB FRAME IAW ABX REA D852-46043MR. 2L74 4F 4A25 20030915000762003091500076EU 2003 9 15 BAQA088826 120030902A77141179405603 INDICATOR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101650B1 41560NE N1 ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME1763 7235 N1 INDICATOR GIVING ERRATIC INDICATIONS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20030912001562003091200156NM 2003 9 12 AWXA200300908 120030811A2560P4010021 BATTERY BOEING737 737277 1384570NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28180AW 22647 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD LOWER CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE FORWARD LOWER CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030924000972003092400097EU 2003 9 24 223050303 120030503A24305243212137 DRIVE SHAFT PILATSPC12 PC1245 7090551EU NR 2 GENERATOR FAILED E S4WAO OTHER J WARNING INDICATION CRCRUISE 1 WP07317NA 223 NR 2 GENERATOR CAWS LIGHT ILLUMINATED DUE TO FAILURE OF NR 2 GENERATOR DRIVE SHAFT. 1L71 3T RTA78EU 20030930001012003093000101SO 2003 9 30 C2XA03IA092 120030827A2120U627F DUCT EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW2713550 145575 THE CREW NOTED A STRONG ODOR OF SMOKE AFTER LANDING IN THE COCKPIT, AND, FORWARD CABIN AREA (SMELLED LIKE ELECTRICAL WIRING). MCI- MAINTENANCE RESECURED VENTILATION DUCT FOR THE LEFT HAND MAIN DISTRIBUTION BOX. NO FURTHER SMELL NOTICED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030930000152003093000015EA 2003 9 30 QXEA200301068 120030905A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 BOI- FORWARD CARGO COMPARTMENT CHIMNEY IN DOORWAY IS TORN. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20031001000922003100100092EA 2003 10 1 COMA0360439 120030927A2910AE2460010H0264 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01982CA 7168 FLIGHT 5096 HYDRAULIC SYSTEM 2 LOW PRESSURE WARNING.REPLACED LEAKING PRESSURE LINE IN PYLON. 2L72 4F RTA21EA 20031003001042003100300104SO 2003 10 3 C2XA03CL163 120030914A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716944 145045 CLE FLIGHT 2135 THE CREW REPORTED THE EMERGENCY SIGN ON THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031006001562003100600156 2003 10 6 SWAA031959 420030901A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031014001102003101400110NM 2003 10 14 SWAA032133 120030921A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031021002292003102100229SO 2003 10 21 SIMA200326804 120030920A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 ABI - DURING A MBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMTIS. CUT OUT DAMAGE SECTION OF BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142, REV 22, CHAPTER 53-21-10 FIG 201 AND CPM 51-61-00. (M) 2L72 4F RTT00011AT 20030909001452003090900145EA 2003 9 9 SWIA200312372 120030901A2752852D10011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07915SW3506 3506 7615 FLAPS FAIL MESSAGE. FLAPS STOPPED AT 38 DEGREES. FLAPS WOULD NOT RAISE ON GROUND. REMOVED AND REPLACED LEFT INBOARD FLAP OUTBOARD ACTUATOR IAW MM 27-53-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20030910000612003091000061WP 2003 9 10 DHL2003604782 120030608A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 UPPER EXTERNAL FUSELAGE SKIN CORRODED AT STA 680.000, L-2L - L-2R. PERFORMED MAJOR REPAIR IAW EODHL-030540, ED-3308. REMOVED FASTENERS, REMOVED CORROSION ON AFFECTED AREA , FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT AFFECTED AREA IAW EODHL-030540, ED-3308. PERFORMED EDDY CURRENT INSPECTION, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FINGER DOUBLER (02 EA) AND DOUBLER IAW EODHL-030540, ED-3308. CLEANED, TREATED, PRIMED FINGER DOUBLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FINGER DOUBLERS AND DOUBLER WITH NEW FASTENERS IAW EODHL-030540, ED-3308, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031027001142003102700114CE 2003 10 27 FTU2003F000AA 120031007A7714EM8001 TACH GENERATOR BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA RT ENGINE MALFUNCTIONED E FTUAO OTHER O OTHER NRNOT REPORTED 1 NE05875DM BB1354 DURING ATTEMPT TO START RT ENGINE, THERE WAS NO NG RPM FROM THE RIGHT ENGINE INDICATION. FURTHER INVESTIGATION LEAD TO THE REMOVAL OF THE NG TACH GENERATOR AT WHICH TIME IT WAS DETERMINED THE GENERATOR DRIVE SHAFT WAS BROKEN. OTHER PIECE OF THE DRIVE SHAFT WAS FOUND STILL IN PLACE. INSTALLED A REPLACEMENT TACH GENERATOR, OPS CHECKED GOOD. REASON FOR FAILURE IS SUSPECTED, GENERATOR WAS SEIZED INTERNALLY. 1L72 4T3 T A24CE E2NE 20040114000702004011400070NM 2004 1 14 DL764030986 120031106A2781849704 PSEU BOEING767 767432ER 1385134NM L/E SLAT FAULTY A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27839MH 29712 DURING C/O FROM LAX, L/E SLAT ASYM MSG CAME ON INTERMITTENTLY THEN REMAINED ON, LEVEL OFF LIGHT EXTINGUISHED DURING LATER STAGES OF DESCENT ON RETURN TO LAX. FIX FSEU FAULTED LAST FLT L/E INBD ASYM MSG NR 27-81020 PSEU FAULTED NR 304 SW NR 8 INBD SLAT CHECKED PROX SW TO TARGET CLEARANCE PER MM, FOUND WITHIN LIMITS. CLEANED SWITCH AND TARGET REPLACED PSEU, OPS CHECK NORMAL. 2L72 4F RTA1NM 20031103001182003110300118EU 2003 11 3 AWXA200301115 120030925A5414D54530052200201 SKIN AIRBUS320 A320232 3930326EU NR 2 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION,PITTING WAS FOUND ON THE NR 2 PYLON OUTBOARD AFT FIXED FAIRING AT STA.4067. MAINTENANCE FOUND IT TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN IAW A320 SRM 54-54-11 PG. 2 AND 3 FIG. 1 AND SRM 54-50-00 PG. 103,105,106 AND 110 FIG. 101 TABLE 101 FIG 104. 2L72 4F RTA28NM 20040329000432004032900043NM 2004 3 29 ASAA0340324 120030725A534065C161218 FITTING BOEING737 7374S3 1384711NM GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - DURING C-CHECK, FOUND CORROSION ON GIRT BAR FLOOR FITTING AT STATION 334 AND STRINGER 17. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031119000972003111900097NM 2003 11 19 AWXA200301217 120030930A5753694754216 ANGLE BOEING737 7373G7 1384595NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MINOR REPAIR - DURING C-17 CHECK A .7500 INCH CRACK WAS FOUND ON RT WING INBOARD UPPER TRAILING EDGE FIXED FAIRING LOWER INBOARD ANGLE ATTACH BRACKET, AT WING TO BODY FAIRING ATTACH POINT BS 727. MAINTENANCE REMOVED CRACKED LOWER INBOARD ANGLE ATTACH BRACKET AT BS 727; FABRICATED A NEW REPLACEMENT ANGLE ATTACH BRACKET; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1. 2L72 4F RTA16WE 20031106000922003110600092NM 2003 11 6 AWXA200301341 120031020A57546546421221 SLAT BOEING737 737277 1384570NM NR 1 DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK THE NR 1 LEADING EDGE SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER SURFACE WS 510 TO WS 512 LT. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 L/E SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-02, REPAIR 5, FIG 14. 2L72 4F RTA16WE 20031106001302003110600130NM 2003 11 6 SWAA032271 120031015A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 240 AND LBL 10. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20031103001092003110300109NM 2003 11 3 AWXA200301133 120030905A53122024T3032 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK HFEC INSPECTION IDENTIFIED A .8750 INCH CRACK IN BS 178 BULKHEAD WEB AT WL 200, LBL 5.7. MAINTENANCE CUTOUT CRACK ON BS 178 BULKHEAD WEB AT WL 200, LBL 5.7; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, PG. 275-285, FIG. 210. 2L72 4F RTA16WE 20040112000982004011200098NM 2004 1 12 F3LA200300183 120031219A5311 FRAME BOEING737 73736N 1384408NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED FRAME CRACKED AT BIN RAIL ATTACH BRACKET HOLE, STA 907, BETWEEN STR 8L AND 9L. REPAIRED PER SRM 53-00-07 FIG 202, STEPS 1-10. 2L72 4F RTA16WE 20040112002212004011200221NM 2004 1 12 QXEA200301575 120031221A3060 DEICE SYSTEM BOMBDRDHC8 DHC8401 1390041NM PROPELLER MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09409QX 4051 SEA FLIGHT 2382 PROP DEICE CAUTION LIGHT ILLUMINATED DURING FLIGHT. PER CHECKLIST, TURNED OFF, THEN ON, LIGHT WENT OUT THEN CAME BACK ON. INTERROGATED CDS, NO FAULTS NOTED. GROUND RUN AIRCRAFT TO OPERATIONAL CHECK PROP DEICE SYSTEM SEVERAL TIMES. DEICE SYSTEM CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040112001852004011200185EU 2004 1 12 AWXA200301253 220031013A7200 ENGINE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 1 MALFUNCTIONED A AWXAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP28332AW4750610047 23384 720703 AIR TURN BACK - FLT 0751 - ON FULL THRUST BLEEDS OFF TAKEOFF OUT EN ROUTE FOR MSP NR 1 ENGINE EGT OVER-TEMPED AT 973 DEGREES FOR 35 SECONDS, EGT STAYED ABOVE 935 FOR 1 MINUTE, TURNED BACK, EGT REMAINED BELOW LIMITS THROUGHOUT DESCENT AND LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW R5M71001, F5M75001, AND F8M71001, OPERATIONAL CHECK OF NEW ENGINE WAS GOOD. TEARDOWN FINDINGS OF ENGINE S/N 720703 FOUND HEAVY BURNING IN ONE AREA OF HIGH PRESSURE TURBINE (HPT) SHROUD AND VANES, AND HEAVY RUB AND BURNING ON 100 PERCENT OF THE HPT BLADES, REPLACED DAMAGED COMPONENTS IAW CFMI CFM56-3. 2L72 4F4 FRTA16WE E21EU 20031125000502003112500050WP 2003 11 25 DHL2003802505 120031106A5712 FRAME DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 RIGHT WING L/E FORMER CRACKED AT STA XFS 483.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. STOP DRILLED AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040113001742004011300174WP 2004 1 13 AALA20031470 120031225A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21291AA 49303 DFW OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROWS 23 TO 27. REPLACED BATTERY PACK FOR EMERGENCY LIGHTING AT SEAT ROWS 23 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031216000182003121600018SO 2003 12 16 MASA200300406 120031012A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07825MJ 145179 CLT-HSV AN EMERGENCY EXIT LIGHT AT ROW 12R INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4T RTT00011AT 20031218001102003121800110 2003 12 18 2003UALA00898 420031125A2330 ANODE TERMINAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE VIDEO MONITOR FAILED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29506UA 24627 ELEC BURNING ODOR EMANATING FROM VIDEO MONITOR. MONITOR WAS REPLACED. FOUND UNIT TO EMIT AN ELECTRICAL ODOR UPON INITIAL POWER UP TESTING. UNIT HAD A FAILURE OF THE HIGH VOLTAGE CRT ANODE TERMINAL OF THE FLYBACK TRANSFORMER. THIS FAILURE IS RARE. 2L72 4F4 FRTA2NM E17NE 20031218000712003121800071NM 2003 12 18 AWXA200301506 120031104A575365464311 SKIN BOEING737 7373G7 1384595NM TE FLAP CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK FOUND THE LT WING OUTBOARD FOREFLAP LEADING EDGE CHAFING AGAINST THE AFT BOX PANEL AT FLAPWELL OUTBOARD OF NR 3 FLAP TRACK RS 275.03. MAINTENANCE REMOVED THE LT WING OUTBOARD FLAP WELL BOX PANEL AT RS 275.03; FABRICATED A NEW REPLACEMENT PANEL; INSTALLED REPAIR PART IAW AWA ER 03-5752-03317-DL1. 2L72 4F RTA16WE 20031223000212003122300021NM 2003 12 23 SWAA032624 120031129A531265465658 BULKHEAD BOEING737 7373H4 1384600NM AFT FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 6L. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031229001172003122900117NM 2003 12 29 SWAA032723 120031214A3350100067 LIGHT BOEING737 7372H4 138448CNM R2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SC FOUND R2 DOOR EXIT LIGHT INOP. REMOVED AND REPLACED SERVICE LIGHT PER MM. 2L72 4F A16WE 20031231000082003123100008NM 2003 12 31 2003F00658 120031114A3350900542 BATTERY BOEING727 7272J0 138407ENM R2 EXIT DOOR INOPERATIVE A P9RAK NONE O OTHER ININSP/MAINT 1 SO11910PG 22606 R2 ENTRY DOOR EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY SUPPLY IAW BMM 33-50-71. (M) 2L73 4F RTA3WE 20040105001112004010500111WP 2004 1 5 DHL2003802527 120031117A53203758496IN FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 AFT CARGO COMPT FITTING CRACKED 2.000 STA 1160.000 - 1180.000, L-35L. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031009000772003100900077EA 2003 10 9 SWIA200312399 120030911A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040106000162004010600016WP 2004 1 6 DHL2003802558 120031124A53204751820 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 822.500 LBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 822.500 LBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201843 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040105001532004010500153CE 2004 1 5 AMWA88 120031205A1430 RIVET BEECH 1900 1900D 1154162CE LT MLG WW LOOSE A AMWAK NONE O OTHER ININSP/MAINT 1 CE07161YV UE161 LEFT WHEEL WELL GRAVEL FENDER INBOARD UPPER ATTACH POINT AT KEEL HAS LOOSE RIVETS CAUSING WEAR ON KEEL BEAM. REPAIRED BY INSTALLING DOUBLER ON KEEL BEAM USING ADHESIVE AND HUCK BOLT FASTENERS IN ACCORDANCE WITH ENGINEERING REPORT 4849-3. 2L72 4T RTA24CE 20040106000542004010600054NM 2004 1 6 AWXA200301560 120031217A3397ABS0374A24 WIRE AIRBUSA319 A319132 3930340NM CABIN CHAFED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28824AW 1490 JFK - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE AT FORWARD & OVERWING AREA. MAINTENANCE REMOVED AND REPLACED LT & RT OVERWING EMERGENCY POWER SUPPLY UNITS (11WL & 12WL), REPAIRED DAMAGED WIRE AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD. PART NAME; ESPU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 3777, TT; 9441, TC; 3578, LOC; ZONE 241. PART NAME; ESPU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 3758, TT; 9441, TC; 3578, LOC; ZONE 242. 2L72 4F RTA28NM 20040106000822004010600082SO 2004 1 6 C2XA03SH508 120031218A532014521718003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE LEFT HAND RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040114000502004011400050NM 2004 1 14 DLM88030965 120031028A3242329001469 BRAKE DOUG MD88 MD88 3023688NM NR 2 MAIN SEIZED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27946DL 49819 GROUND ABORT NR 2 BRAKE LOCKED UP DURING TAXI. REPLACED NR 2 ASSY PER M/M. ALSO REPLACED NR 2 WHEEL ASSY PER M/M. 2L72 4F RTA6WE 20031125000072003112500007WP 2003 11 25 DHL2003805513 120030815A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT WING CTR L/E FORMER CRACKED (STA XFS 335.250 - XFS 329.000). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. HEAT TREATED IAW SRM 51-1-1 PG 17. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031202000032003120200003NM 2003 12 2 ASAA0310468 120030515A5311BAC1518431 FRAME BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 420, LEFT BUTTOCK LINE 20, RIGHT BUTTOCK LINE 31 CORRODED. REPAIRED FRAME PER EA. (M) 2L72 4F A16WE 20031202000492003120200049NM 2003 12 2 USAASB03180 120031010A253060001083 CONTROLLER BOEING737 737301 1384611NM OVEN TEMP OVERHEATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19334US4485 23231 EN ROUTE FROM CLT TO DFW, CREW REPORTED AN ELECTRICAL BURNING ODOR IN FORWARD GALLEY. OVEN, CONTROLLER AND BACKWALL OF GALLEY WAS HOT. TURNING OFF GALLEY POWER APPEARED TO BE OF SOME HELP. FLIGHT LANDED AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE IN DFW PULLED OVEN CONTROL UNIT AND FOUND UNIT TO SMELL BURNED. OPERATED GALLEY LIGHTS. NO TROUBLE FOUND. PULLED AND COLLARED OVEN AND COFFEEMAKER CIRCUIT BREAKERS. RELEASED AIRCRAFT ON MEL 25-10. THREE DAYS LATER, ON OCTOBER 13TH IN PHL, CREW REPORTED FEELING HEAT AND DETECTING ODOR IN FORWARD GALLEY AGAIN. APPEARS TO BE COMING FROM OVEN CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY OVEN TEMP CONTROLLER. OPS CHECK GOOD. CLEARED MEL 252L72 4F RTA16WE 20031202001372003120200137NM 2003 12 2 GAIA03114SP 120031022A5320 ANGLE BOEING727 727223 1384074NM LT MLG WW CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076831 20184 DURING B-CHECK AT DFW, FOUND CORROSION ON AN ANGLE IN THE LEFT MAIN LANDING GEAR WHEEL WELL AT THE 950 BULKHEAD. THE CORROSION WAS REMOVED AND THE ANGLE WAS REPAIRED PER THE B727 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031203000582003120300058NM 2003 12 3 GAIA03158ST 120031024A25502956 RESTRAINT BOEING727 727243 138408DNM FUSELAGE WORN A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURNG C-CHECK INSPECTION FOUND MAIN CARGO PALLET SIDE RESTRAINTS WORN. REF FASI N/R NR 61123, REMOVED AND REPLACED SIDE RESTRAINTS BS 348 TO 1168 IAW KHA EA-B7-53-113, RESTRAINT P/N 2956 PO NR 34817. (M) 2L73 4F RTA3WE 20031202001612003120200161NM 2003 12 2 2003F00605 120031026A3350900542 POWERPACK BOEING727 727200 138407ENM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE O OTHER ININSP/MAINT 1 SO11910PG 22606 AISLE EMERGENCY EXIT LIGHT AT ROW 20 INOPERATIVE. REMOVED AND REPLACED BATTERY POWER PACK AT ROW 20 IAW B727 MM, 335071. (M) 2L73 4F RTA3WE 20031204001282003120400128SO 2003 12 4 C2XA03SH396 120031018A335078241 INVERTER EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725504 145186 DURING C-CHECK THE NR 1 EMERGENCY AISLE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB 135 AMM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031208001612003120800161NM 2003 12 8 AWXA200301323 120031006A533065C252045 SKIN BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK CORROSION WAS FOUND ON LT WING UPPER SURFACE AT THE WING TO BODY FAIRING BS 578, UPON FURTHER INVESTIGATION A .25 INCH CRACK WAS FOUND ON S-11 HORIZONTAL FLANGE AT THE 13TH FASTENER HOLE OUTBOARD OF THE WING ROOT. MAINTENANCE BLENDED OUT CORROSION; MATERIAL LOSS WITHIN LIMITS; PERFORMED HFEC INSPECTION OF BLEND, NO CRACKS NOTED; CUT OUT DAMAGED SECTION OF S-11 HORIZONTAL FLANGE AND PERFORMED HFEC INSPECTION OF CUTOUT; FABRICATED A -4 FILLER, AND -2, -3, & -5 REPAIR ANGLES; INSTALLED REPAIR PARTS IAW AWA ER 03-5723-03295-ES1. 2L72 4F RTA16WE 20031209001362003120900136EA 2003 12 9 QXEA200301319 120031007A5754 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 RIGHT WING PANEL 622DB LEADING EDGE OF PANEL IS CHAFED. REPAIRED IAW CRJ-700 AMM 27-81-25-820-901 AND EO 601R-57-4253 AND HORIZON AIR EA R-57-48. 2L72 4F RTA21EA 20031209001842003120900184NM 2003 12 9 UPS03441502 120031011A541269B9031077 BULKHEAD BOEING747 747200 1384847NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT WEB APPROX 2 X 1 INCH RESPECTIVELY. NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FWD AND AFT WEB REPAIRED AS PER RS R54-53-35087 AND UPS ENGINEERING FILE 747-54-20042. 2L74 4F RTA20WE 20040122001012004012200101 2004 1 22 WRLA200325 420031208A34182568A13 SENSOR DOUG MD11 MD11 3023602NM AOA DAMAGED A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11271WA 48518 UPON PASSING ACCELERATION ALTITUDE A/C SUSTAINED MULTIPLE MALFUNCTIONS. PASSING 1968 FT OCH ALT GCP WENT TO BLANK. SIMULTANEOUSLY CAPT SIDE FD BLANK. CAPT SIDE ALT READOUT INDICATED 1500 FT LOW, VERIFIED WITH LUKE AFT DEP. CAPT SIDE AIRSPEED INDICATED 20-30 KTS SLOWER THAN F/O SIDE. LVL 2 'SEL ELEV FEEL MAN' LATER EXTINGUISHED. LVL 2 'LSAS ALL FAIL ALERT. PERFORMED PILOT & STATIC LEAK CHECKS & VERIFICATION OF INDICATIONS ALL GOOD. RAN ALL LSAS & WERE GOOD. PERFORMED, ELEV FEEL ZRTS AND IT CHECKED GOOD. PROBLEMS WERE CAUSED BY IMPROPERLY INSTALLED AOA SENSOR REMOVED AND REPLACED ANGLE OF ATTACH SENSOR. (M) 2L73 4F RTA22WE 20031014001462003101400146 2003 10 14 SWAA032061 420030915A2565D31354 GIRT BAR BOEING737 7377H4 1384404NM AFT ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29413WN 29819 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20031020001812003102000181NM 2003 10 20 DL73S030813 120030903A53306545866585 SKIN PANEL BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334DL 23105 THE LOWER SKIN PANEL OF THE KEEL BEAM STRUCTURE WAS FOUND WITH AREAS OF CORROSION BETWEEN FS 661 & 724 AND BETWEEN LBL 6 & RBL 6. THE DAMAGED PANEL WAS REMOVED AND A NEW PANEL FABRICATED AND INSTALLED. THE REPAIR WAS ACCOMPLISHED PER BAC S/B 737-53-1104 AND ER/A 087153-14. 2L72 4F RTA16WE 20031021000472003102100047 2003 10 21 USAASA03105 420030902A2565C37103103 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19732US 1203 CLT - THE AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M) 2L72 4F RTA28NM 20031210001792003121000179NM 2003 12 10 CALA0300679 120031130A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716648 28909 INSPECTION FOUND LT Z-ANGLE CORRODED AT L-2 DOOR SILL, STA 977. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20031217000032003121700003EU 2003 12 17 BAQA089604 120031006A2700365A27353502 LEVER AEROSPAS365 AS365N2 8680815EU ROLL CRANK DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME7126 6417 ROLL CRANK LEVER DAMAGED. REPLACED WITH SERVICEABLE UNIT 10/15/03. 1G72 3U RTH10EU 20031211001722003121100172WP 2003 12 11 AALA20030917 120030831A3350 CONNECTOR DOUG DC9 DC982 3022082WP COCKPIT DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21259AA 49289 DFW - DURING OVERNIGHT MAINTENANCE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. CLEANED AND RESEATED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040614002092004061400209CE 2004 6 14 GUU2004F00008 120031124A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178153317255 UE137 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040709000712004070900071SO 2004 7 9 C2XA03BT110 120031119A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 CREW REPORTED TWO STRIPS OF EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, NO FAULTS NOTED, OPS CHECKED GOOD IAW EMB145 AMM NR 33-50-00. 2L72 4F RTT00011AT 20030925001012003092500101 2003 9 25 DXTA200300122 420030919A2210 BUNGEE CYLINDER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LT ELEVATOR LOOSE E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07930QS 7500130 PITCH VIBRATION IN FLIGHT CONTROLS WITH AUTO PILOT ON, VIBRATION INCREASED AS SPEED INCREASED. NOTICED AT 250 KTS AND 10000FT, VIBRATION ALSO COULD BE HEARD AS LOW FREQUENCY SOUND. TIGHTENED LT ELEVATOR BUNGEE AND ADJUSTED ELEVATOR CABLE TENSION IAW CESSNA 750 MM 27-30-00. 2L72 4J4 FRTT00007WITE6CH 20030815000072003081500007NM 2003 8 15 AALA20030553 120030511A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21676AN 29426 JFK - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR LIGHT SECTION INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT FLOOR LGIHT WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030819001052003081900105NM 2003 8 19 UPS03240921 120030605A5280 HINGE BOEING727 727185C 138406NNM RT MLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, RT MLG BODY DOOR HINGE UNDER SAFETY BAR HAS SUSPECT CRACK. HFEC INSP CARRIED OUT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT: CRACK CONFIRMED. HINGE HALF REMOVED IAW SRM 51-30-02. NEW HINGE HALF FITTED IAW SRM 51-30-02. 2L73 4F A3WE 20030331000762003033100076NM 2003 3 31 AWXA200300319 120030327A2910R291206EE0250T HOSE BOEING737 7373Q8 1384670NM RT MLGWW BURST A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28327AW 23507 ON CLIMB OUT FROM DEN EN ROUTE FOR PHX, THE RT MAIN LANDING GEAR INDICATED BOTH RED AND GREEN, ACCOMPANIED BY HYDRAULIC SYSTEM PRESSURE AND QUANTITY LOSS. DECLARED EMERGENCY AND TURNED BACK TO DEN, LANDED WITHOUT FURTHER EVENT. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND RT MAIN LANDING GEAR PRESSURE LINE RUPTURED. AWA MAINTENANCE TECHNICIANS DISPATCHED FROM PHX. 2L72 4F RTA16WE 20030401001072003040100107WP 2003 4 1 DHL2003803004 120030320A5347 SEAT TRACK DOUG DC8 DC873 302199CWP COCKPIT LACK OF LUBE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01803DH 46123 S/O'S SEAT DIFFICULT TO MOVE FORE AND AFT. LUBED F/O'S AND S/O'S SEAT TRACKS AND CHECKED MOVEMENT. OK PER M/M 25-11-1. 2L74 4F RT4A25 20030328000762003032800076NM 2003 3 28 CH1A200384005 120030324A2612 CIRCUIT BREAKER BOEING727 7272S7 138407ZNM FIRE WARNING TRIPPED A C1HAK NONE N FALSE WARNING ININSP/MAINT 1 GL15684CA 22491 DURING FIRE WARNING TEST CONTROLLER ENGINE FIRE PROTECTION TEST RELAY AND ALARM BELL CIRCUIT BREAKER POPPED 2L73 4F A3WE 20030401001312003040100131WP 2003 4 1 DHL2003804523 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 616.250 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030408000782003040800078NM 2003 4 8 03FDEA00386 120030404A2162 WARNING LIGHT BOEING727 727200 138407ENM PWA JT15 JT15D1 52060NE AIR CONDITIONER FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25234FE 21328 EQUIPMENT COOLING LIGHT CAME ON IN FLIGHT. PULLED RADIO ALT CB VIA THE QRH AND LIGHT WENT OUT FOR A FEW MINUTES. LIGHT THEN CAME BACK ON STEADY. QHR SAID LAND, ASAP. ON RETURN TO MEMPHIS, LIGHT WENT OUT A COUPLE OF TIMES IN THE DESCENT BUT WAS ON MOST OF THE TIME. ADDITIONALLY WE ALL NOTICED A BURNING SMELL AFTER TAKE OFF THAT GRADUALLY DIMINISHED. FOUND LIGHT BULB BASE WORN AWAY. WITH BASE WORN AWAY THIS PUTS LIGHT IN THE PUSH-TO-TEST MODE. ALSO FOUND BURNT MARKS ON SIDE OF LIGHT LENSE FRAME WHICH COULD HAVE CAUSED SMELL. REPLACED LAMP AND CLEANED LENSE FRAME IAW SMP. TESTED AIRFLOW DETECTOR IAW 727 MM 21-58-031-4. EQUIP COOLING SYSTEM GROUND CKS, NORMAL. 2L73 4F4 FRTA3WE E1NE 20030408001222003040800122NM 2003 4 8 ABXA030127 120030403A5250 DOOR BOEING767 767205 1385121NM PWA JT9 JT9D* NE COCKPIT INOPERATIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23713AX 23058 COCKPIT DOOR WOULD NOT OPEN, BINDED ON CEILING UNHINGED DOOR. REINSTALLED COCKPIT DOOR AND ADJUSTED TABS IAW B767 MM. COCKPIT DOOR OPS CHECKED GOOD. 2L72 4F4 FRTA1NM E20EA 20030415001572003041500157WP 2003 4 15 UPS03839996 120030102A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS TEST INOP. REPLACED EMERGENCY LIGHTS BATTERY AND RELAY PACK PER MM 33-50-01. 2L74 4F RT4A25 20030417000382003041700038EA 2003 4 17 SWIA200311732 120030122A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA STAB TRIM CHAFED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07589SW 7072 STAB CHANNEL NR 1 FAILED ON PUSHBACK. FOUND A CHAFED WIRE AT CONNECTOR J3CP WIRE CD83622WHT. RE-PINNED WIRE IAW CRJ WM 20-00-00. PERFORMED OPS CHECK OF STAB TRIM SYSTEM IAW CRJ MM 27-41-00. CHECKS GOOD. 1/26/2003 - STAB TRIM CHANNEL 1 FAILED. 2L72 4F RTA21EA 20030429000122003042900012NM 2003 4 29 P5CA0300802 120030129A5320 PANEL BOEING747 747283B 1384867NM CABIN CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 UPPER DECK SIDE WALL PANEL CRACK ON CLIP AT FRAME STA 500, STR 10, 10A, 11A, 12. NEW CLIP FABRICATED SRM 53-10-20 & SRM 51-40-03 FIG 4. PROTECTED PER SRM 51-10-02, RIVETS PER SRM 51-30-02. 2L74 4F A20WE 20030430000182003043000018EU 2003 4 30 AWXA200300451 120030331A5320D53230256201 ANGLE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A 5/16 INCH CRACK WAS FOUND ON ATTACH ANGLE AT AFT UPPER CORNER OF PANEL 191AB ATTACH POINT FR 34, STR 31 LT. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ANGLE PER DWG C3 D53230256; INSTALLED REPAIR PART IAW AWA E.R. 26-5336-03113-SS1. 2L72 4F RTA28NM 20030430000502003043000050NM 2003 4 30 2003UALA00388 120030419A3411 LINE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE PITOT STATIC LEAKING A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29349UA 24253 AIRCRAFT RETURNED TO FIELD WHEN A LEAK IN THE PITOT STATIC SYSTEM RESULTED IN UNRELIABLE AIR DATA. FLEX LINE WAS FOUND TO BE LEAKING FROM UPPER RT PITOT TUBE TO FIRST ELBOW . 2L72 4F4 FRTA16WE E2GL 20030430000792003043000079SO 2003 4 30 SIMA200309012 120030312A532014522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 ABI - THIS IS A LEVEL TWO FINDING FOUND DUIRNG AN IMBV INSPECTION, FORWARD PASSENGER DOOR FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW EMB135 SRM 51-40-02 ND ETN EB 53-032R1. (M) 2L72 4F RTT00011AT 20030430001932003043000193NM 2003 4 30 SWAA030933 120030427A57536546435 SKIN BOEING737 7375H4 138449DNM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/4D CHECK, FOUND RT OUTBOARD AFT T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED RT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20030502000552003050200055WP 2003 5 2 ASAA0380167 120030228A532199365465 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN PANEL HAS CORRODED/MISSING INSERTS AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05 AND 53-24-0. (M) 2L72 4F A6WE 20030502001762003050200176NM 2003 5 2 AWXA200300373 120030415A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW 23219 PHX - MAJOR REPAIR - DURING INSPECTION A 3.5 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 748, STR 18 RT. MAINTENANCE PERFORMED TEMPORARY REPAIR BY CUTTING OUT DAMAGED AREA OF SKIN; FABRICATING A REPAIR PLATE; INSTALLING REPAIR PART AND BLIND RIVET REPAIR IAW B737-300 SRM 53-00-01 PG 204-206 FIG 202. REPAIR TO BE REINSPECTED EVERY 2500 FLIGHT HOURS, PERMANENT REPAIR TO BE ACCOMPLISHED WITH 20,000 FLIGHT HOURS. 2L72 4F RTA16WE 20030502000142003050200014NM 2003 5 2 AMTA200300387 120030322A33508100022608 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 EGRESS FLOOR LIGHTS FROM 37ABC TO 38ABC. REMOVED AND REPLACED LIGHT ASSEMBLY AT ROW 37 IAW AMM 33-51-11. OPS CHECK OK. (M) 2L72 4F RTA2NM 20030505002192003050500219EA 2003 5 5 COMA0370011 120030419A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01355CA972 10067 FLIGHT 5693 GEAR DISAGREE WARNING. REPLACED THE L/G SELECTOR VALVE. 2L72 4F RTA21EA 20030505001332003050500133NM 2003 5 5 DHL2003741534 120030323A5720 STIFFENER BOEING727 727200 138407ENM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, LT WING FRONT SPAR VERTICAL STIFFENER HAS TWO CRACKS AT LOWER TWO RIVETS AT LEADING EDGE STA 90. REMOVED FASTENER AT LT WING FRONT SPAR VERTICAL STIFFENER CUT OUT DAMAGE AREA DIM APPROX 2.375 BY 2.4375 INCH IAW B-727 SRM 51-40-1 FIG 1. PART MADE FROM 7075 T-6 .050 PO 9912380 C FILLER 1 INCH DIM APPROX 2.375 BY 2.4375 INCH AND DOUBLER 8.875 INCH BY 2.625 INCH IAW B-727 SRM 57-10-2 FIG 3 AND 51-40-9 FIG 1. PART BAC METAL TREATED WITH ALODINE AND PRIMER IAW B-727 SRM 51-10-2. INSTALLED ANGLE REPAIR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030509000582003050900058SO 2003 5 9 CTU2003F00005 220030416A8550AS3570223 O-RING CESSNA210 T210N 2073456CE CONT O520 TSIO520R 17040SO OIL FILTER ADAPTLEAKING B CTURO OTHER K FLUID LOSS NRNOT REPORTED 1 GL216410N 21062986 O-RING FAILED TO SEAL PROPERLY ALLOWING OIL TO LEAK AT THE OIL FILTER ADAPTER TO ENGINE ATTACHMENT. CAUSE OF THE FAILURE COULD BE ATTRIBUTED TO O-RING TOTAL TIME. ALL WORK WAS DOEN IAW MM AND INSTRUCTIONS CONTAINED IN AD 96-12-22. 1H71 3O3 O 3A21 E8CE 20030509000632003050900063NM 2003 5 9 HOC2003F00016 120030428A5311 FRAME BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B HOCRK NONE O OTHER ININSP/MAINT 1 WP0754348 21967 DURING A (C) CHECK CORROSION WAS NOTED ON LOWER FRAME, STA 1130 AT 27R. 2L72 4F4 FRTA16WE E2EA 20030514001312003051400131NM 2003 5 14 SWAA031017 120030505A53116546569 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, WL 209 & RBL 45. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030515001062003051500106NM 2003 5 15 03FDEA00620 120030425A5510 FITTING DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 HORIZONTAL STABILIZER CENTER BOX LT SIDE BARREL NUT HOLE NR 26 FOUND FITTING WITH CORROSION (BOTTOM & BEARING SURFACE). HORIZONTAL STABILIZER CENTER BOX LT SIDE BARREL NUT HOLE NR 26L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-69219 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE 26 LT FITTING FABRICATION. 2L73 4F RTA22WE 20030530000192003053000019 2003 5 30 HEEA086535 420030522A2312064100900 TRANSCEIVER KTR905 SKRSKYS76 S76A 8143006NE VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 VHF TRANSCEIVER IS WEAK WITH VOLUME ALL THE WAY UP. IN SHOP REPAIR. 1G72 3U H1NE 20030530001202003053000120SO 2003 5 30 SIMA200313203 120030506A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21644AE 145204 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS NOTED. FABRICATED A REPAIR ANGLE, AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M) 2L72 4T RTT00011AT 20030604001902003060400190NM 2003 6 4 UPS03440611 120030410A5412 BULKHEAD BOEING747 747121 1384871NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, NR 3 PYLON REAR ENGINE MOUNT BULKHEAD AFT FRAME FOUND CRACKED AT 4 O/C POSITION ( LOOKING FORWARD ). NR 3 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER HX RS R54-53-35008 AND UPS REPAIR AUTHORIZATION 747-54-20034 DVI AND HFEC INSPECTIONS TO CONTINUE PER UPS EO B747-5410-13908 IAW SB 747-54A2202. 2L74 4F A20WE 20030521000182003052100018NM 2003 5 21 DHL2003783007 120030515A2610 WARNING HORN BOEING727 727227 1384078NM COCKPIT MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01766AT 21999 ON PREFLIGHT CHECK, NO HORN DURING ENGINE OR WHEEL WELL FIRE TEST. REMOVED AND REPLACED AURAL WARNING DEVICE (BOX ASSEMBLY) & OPS TESTED NORMAL PER M/M 26-11-0. 2L73 4F A3WE 20030606000942003060600094NM 2003 6 6 COOSDR030021 120030501A5755 SKIN BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 5 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23902PG 139 20725 LEFT WING, GROUND SPOILER NR 5, PN 65-17348-71, SN 139, WITH DELAMINATION. 2L73 4F4 FRTA3WE E2EA 20030522000332003052200033SO 2003 5 22 C2XA03CL101 120030428A3240156221 PRESSURE SWITCH EMB 145 EMB145ER 3260211SO FUSELAGE LEAKING A C2XAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2712934 145019 CLE FLIGHT 2779 THE CREW REPORTED A NR 2 HYDRAULIC LOW FLUID MESSAGE IN FLIGHT. THE CREW DECLARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 BRAKE PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030610000792003061000079NM 2003 6 10 DL76P030420 120030504A3350BPS73 BATTERY BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO271402A 25989 DURING L/O CHECK FOUND ALL E-PATH LIGHTS FROM ROW 35 AFT INOP. REPLACED BATTERY SLED M9010 ALL E-PATH LTS OPS CKS NML. 2L72 4F RTA1NM 20030613000772003061300077SO 2003 6 13 C2XA03SH173 120030608A531514522461003 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030617000942003061700094EA 2003 6 17 QXEA200300665 120030530A2820L92B13602 CARTRIDGE CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09615QX1538 1538 10065 PDX- ON FLIGHT 2493 AFTER TAKEOFF GOT A LEFT TRANSFER SHUT OFF VALVE AMBER MESSAGE. NO CENTER TANK FUEL ABNORMALITIES NOTICED. AUTO TRANSFER APPEARED EXCESSIVE BUT NO ABNORMAL IMBALANCE OR ANY FUEL LOSS NOTED. APPROXIMITLY 15 MINUTES AFTER DEPARTURE LEFT TRANSFER SHUT OFF VALVE MESSAGE WENT OUT. REMOVED AND REPLACEDLEFT HAND FUEL TRANSFER SHUT OFF VALVE CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030612002052003061200205SO 2003 6 12 SWIA200312054 120030526A3231 SEQUENCE VALVE EMB 120 EMB120ER 3260203SO LT MLG DOOR FAILED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07566SW 120341 ON DEPARTURE ON GEAR RETRACTION LEFT GEAR WOULDN`T COME UP ON FIRST ATTEMPT WITH BOTH LT AND RT A AND B RED INDICTAION LIGHT ON BOTH A AND B GREEN LIGHT ON. LEFT GEAR DOOR DID NOT APPEAR TO OPEN. CYCLED GEAR AND GEAR RETRACTED. ADJUSTED LEFT GEAR INBOARD DOOR SEQUENCE VALVE. OPERATED LANDING GEAR. OPS CHECK GOOD. 2L72 4T RTA31SO 20030617001062003061700106NM 2003 6 17 QXEA200300683 120030608A7110 WEB BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - NR 1 ENGINE LOWER COWL AFT CONE VERTICAL WEB LOWER LEG ANGLE IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030618000102003061800010 2003 6 18 HEEA087488 420030612A2300N0001552 ANTENNA BELL 407 407 1182206SW COMMS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 ANTENNA RECEIVES INTERMITTENTLY. 1G71 3U O H2SW 20030528000182003052800018SW 2003 5 28 HEEA086583 120030428A5302204030958002S SUPPORT BELL 412 412 1182202SW TAILBOOM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 33113 36019 FOUND WHAT APPEAR TO BE SEVERAL CORROSION PITS ALONG LOWER AFT EDGE OF PART OF TAILBOOM SUPPORT, WHICH WERE COVERED BY FACTORY COATING. 1G72 4U H4SW 20030701000022003070100002SW 2003 7 1 HEEA087856 120030418A6300407040553101 DRAIN LINE BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER NRNOT REPORTED 1 SW03491PH 53386 DRAIN TUBE HAS CORROSION CAUSED BY DISSIMILAR METALS USED IN MANUFACTURING PROCESS. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030625000152003062500015WP 2003 6 25 03FDEA00800 120030524A5410 RIB DOUG DC10 DC1010 3022110WP NR 3 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25364FE 46600 NR 855 NR 3 ENGINE RTCORE COWL FWD RIB CRACKED AT UPPER L/E RADIUS. CLOSING ACTION ON 05/24/03. REMOVED FASTENERS FOR ACCESS IAW SRM 51-31-01. WELLED CRACK ON MAE TRAVELER T2/336399 IAW SRM 54-31-01. REINSTALLED FASTNERS IAW SRM 51-35-01, PAINTED TEFLON PAINT IAW SRM 51-21-01 INSTALLED CORE COWL IAW M/M 71-13-01-0. 2L73 4F A22WE 20030707000442003070700044WP 2003 7 7 AALA20030631 120030602A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21244AA 49256 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING FROM ROW 3-20 INOPERATIVE. RESEATED EMERGENCY EXIT PATH LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030707000552003070700055WP 2003 7 7 AALA20030516 120030430A3397 CONNECTOR DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21490AA 49683 DURING OVERNIGHT MAINTENANCE, FORWARD SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING CONTROL MODULE CONNECTOR BROKEN. REPAIRED FORWARD SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING CONTROL MODUEL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030708000532003070800053EA 2003 7 8 SWIA200312090 120030604A5415 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA ANGLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 280 LBL 9.0 FLOORBEAM INBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK) ANGLE REPLACED IAW CRJ SRM 51-40-11. P/N: 601R311011-73SA 2L72 4F RTA21EA 20030708000752003070800075NM 2003 7 8 AWXA200300646 120030513A53116545409602 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON MAIN WHEEL WELL UPPER COMPRESSION FRAME AT BS 663, RBL 24.5. MAINTENANCE REMOVED VERTICAL STIFFENER, WEB DOUBLER, VERTICAL ANGLE, AND FORWARD AND AFT STIFFENER BRACKETS TO FACILITATE REPAIR; CUT AND TRIMMED DAMAGE ON UPPER COMPRESSION FRAME; FABRICATED A NEW REPLACEMENT FRAME SEGMENT; INSTALLED REPAIR PART AND REINSTALLED PARTS REMOVED TO FACILITATE REPAIR IAW E.R. 15-5311-03141-JS1. 2L72 4F RTA16WE 20030708000912003070800091WP 2003 7 8 UPS03840927 120030613A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, 8 PREVIOUS BLENDOUTS BELOW C-PIT DOOR BETWEEN LONG. 34R TO 30R FROM STA. 1220 TO 1260 CUT AND REMOVED SKIN SECTION FROM STATION 1190-1230 BETWEEN LONG 29R TO 34R,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED SKIN SECTION AND SPLICE DOUBLERS IAW DC8-5330-18928-A AND SAA SK 807-033. 2L74 4F4 FRT4A25 E2GL 20030708001062003070800106WP 2003 7 8 UPS03840905 120030603A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C3, LONGERON 17R CRACKED AT BS 1768. REMOVED L17R AND END FITTING IAW SRM 51-1-21. LOCATED AND DRILLED NEW LONGERON SECTION AND END FITTING IAW SRM 51-1-24. INSTALLED LONGERON AND FITTING IAW SRM 51-1-21 AND 51-1-120D. 2L74 4F RT4A25 20030709001202003070900120NM 2003 7 9 250TR0019 120030610A3350 BULB BOEING737 7372K5 138448XNM EMERGENCY LIGHT BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 OVERWING EMERGENCY LIGHT INOP. RELAMPED OVERWING EMERGENCY LIGHT. 2L72 4F RTA16WE 20030709000332003070900033WP 2003 7 9 AALA20030467 120030417A3350 CONTACTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21438AA 49456 AUS - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 17-21 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030711000742003071100074NM 2003 7 11 EIA2003089 120030619A3350 BATTERY PACK BOEING747 747SR46 1384816NM EMERGNECY LIGHT INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09478EV 21033 CREW SERVICE DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK AND EXIT SIGN OPS CHECKED IAW 33-53-00. AIRCRAFT IN MAINTENANCE FROM 6-19-03 TIL 06-24-03. 2L74 4F RTA20WE 20030711000752003071100075EU 2003 7 11 DHL2003368006 120030626A3260 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01368DH 207 AFTER TAKEOFF LANDING GEAR HANDLE COULD NOT BE RAISED USING SYSTEM 2. PERFORMED ABNORMAL PROCEDURE PER AOM. AFTER CLEANING PROXIMITY DETECTORS AND CONNECTORS, PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM WITH NO DEFECTS NOTED IAW M/M 32-31-11. OPS CHECKED GOOD ON BOTH SYSTEMS. 2L72 4F RTA35EU 20030327001012003032700101SO 2003 3 27 C2XA03CL008 120030108A2120 ODOR EMB 145 EMB145ER 3260211SO COCKPIT DETECTED A C2XAO OTHER D INFLIGHT SEPARATION TXTAXI/GRND HDL 1 SW2714937 145026 SYR FLIGHT 2479 THE CREW REPORTED UPON APU START THERE WAS A STRONG ELECTRICAL ODOR IN THE COCKPIT. THE ODOR DISSIPATED ON SHUTDOWN. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 49-00-00. 2L72 4F RTT00011AT 20030127000212003012700021 2003 1 27 HEEA083597 420030114A3442MI5851352 INDICATOR BELL 412 412 1182202SW RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 RADAR SYSTEM KICKS OFF AFTER 30 MINUTES. SHOP REPAIR. 1G72 4U H4SW 20030127001332003012700133SW 2003 1 27 HEEA083676 120030115A3212206050247132 COVER BELL 407 407 1182206SW EMERGENCY FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 EMERGENCY FLOAT COVER HOOK AND LOOP WILL NOT HOLD ANYMORE. 1G71 3U O H2SW 20030203000812003020300081SW 2003 2 3 BAQA082912 120030110A2422SPS1307 INVERTER BELL 222 222U 1182140SW AC SYSTEM MALFUNCTIONED H BAQAK NONE O OTHER ININSP/MAINT 1 FS01222MN3086 47534 INVERTER TRIPS ON AND OFF EVERY 10-15 SECONDS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H9SW 20030204000672003020400067NM 2003 2 4 SWAA030194 120030125A57556546552 SPOILER BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND NR 9 SPOILER DELAMINATED AT INBD EDGE LOWER SURFACE. REPAIRED SPOILER PER SRM. 2L72 4F RTA16WE 20030212000612003021200061EA 2003 2 12 CA030116002 120030108A2913601R751133 PUMP CNDAIRCL604 CL604 1900301EA GE CF34 CF343A1 30015NE HYD SYSTEM FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CA (CAN) PRODUCTION FLIGHT TEST NR 4 DATED 8 JAN 03, HYDRAULIC NR 2 HI TEMP CAUTION POSTED JUST AFTER LEVELING ATF 410 TEMP MAXIMUM 104C, RT ENGINE SHUTDOWN, TEMP DECREASE TO NORMAL LIMIT. ENGINE RELIT PRIOR TO LANDING. EDP REMOVED AND INSTALLED. GROUND RUN CARRIED OUT AND TEMP INCREASE NORMALLY WHEN COMPARE WITH NR 1 HYD TEMP. AIRCRAFT RETURN TO FLIGHT TEST STATUS. PRODUCTION FLIGHT TEST NR 5 DATED 8 JAN 03, HYDRAULIC NR 2 HI TEMP REPEAT OF PREVIOUS SNAG, AIRCRAFT LANDED SINGLE ENGINE WITH NR 2B PUMP SELECTED ON. CASE DRAIN ASSEMBLY REMOVED AND EDP REMOVED PRODUCTION FLIGHT TEST NR 6 AIRCRAFT FLEW SERVICEABLE. 2L72 4F4 FRTA21EA E15NE 20030213000192003021300019EA 2003 2 13 CA030124001 220030124A7310304599701 TUBE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA PORT ENGINE BROKEN W D RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 10851 (CAN) BOTH ENGINES RUNNING WHILE ON THE RAMP. WHEN POWER WAS APPLIED TO THE PORT ENGINE TO TURN THE A/C THE ENGINE RETURNED TO MIN. FLOW OF 38 PERCENT UNCOMMNANDED. THERE WAS NO RESPONSE ON THE POWER LEVER. A/C HANGARED AND PORT ENGINE INSPECTED. THE PY GOVERNING AIR PRESSURE, HEATED LINE PN 3044599701 WAS FOUND BROKEN AT THE FITTING FLANGE ON THE FCU. LINE REPLACED, GROUND RUN SERVICEABLE AND A/C RETURNED TOSERVICE. 1L72 4T4 T A24CE E4EA 20030314000292003031400029WP 2003 3 14 03FDEA00107 120030204A5730 SKIN DOUG DC10 DC1030 3023501WP RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25318FE 46837 RIGHT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108 RT WING SKIN PANEL AT STA XIS 168.66 TO XORS 130.40, STRINGER 1R AND 22R, AREAS 1 THRU 33 PER SRM CHAPT 51 AND SRM 57-10-00 IN COMPLIANCE WITH EA 8-5710-67582. REF SNRM N111, N177, AND N776. 2L73 4F A22WE 20030220000292003022000029NM 2003 2 20 03FDEA00125 120030213A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 DENTS IN FUSELAGE EXTERNAL SKIN, STA 1030 TO 1050, STR S27R TO S28R. REPAIRED SKIN DENT AT FUSELAGE EXTERNAL SKIN, B.S 1030-1050, STR 27R-28R. ALL WORK DONE IAW SRM 53-30-1 FIG 1, SRM 53-30-3 FIG 1. 2L73 4F A3WE 20030221000892003022100089NM 2003 2 21 CALA0300060 120030220A335020131A BATTERY PACK BOEING757 757224 1384958NM R-2 DOOR INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW0917122 27564 THE EMERGENCY EXIT LIGHT EXIT LOCATOR SIGN AT R-2 DOOR WAS FOUND INOPERATIVE DURING SERVICE CHECK TEST. TWO EMERGENCY EXIT LIGHTS ON OVERHEAD BIN FORE AND AFT OF R-2 DOOR WERE INOPERATIVE. THE BATTERY PACK AND CHARGER ABOVE R-2 DOOR WERE REMOVED AND REPLACED IAW MM 33-51-07. 2L72 4F RTA2NM 20030224000902003022400090SW 2003 2 24 HEEA084211 120030120A5320407070620112 TRIM PANEL BELL 407 407 1182206SW CABIN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 CABIN TRIM PANEL CRACKED. 1G71 3U O H2SW 20030304000672003030400067SO 2003 3 4 C2XA03CL063 120030304A323121180100004 ACTUATOR EMB 145 EMB145ER 3260211SO NOSE GEAR SLOW A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714945 145049 CVG FLIGHT#2695 THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT CLOSE ON CLIMBOUT.THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030305000282003030500028NM 2003 3 5 C1HA200395005 120030120A3320 LIGHT BOEING727 727290 138408WNM CABIN DISLODGED A C1HAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15295AS 22147 CENTER CABIN CEILING EXIT LIGHT FELL DOWN. REINSTALLED CENTER CABIN CEILING EXIT LIGHT IAW B-727 MM REF 20-80-1. 2L73 4F A3WE 20030306000772003030600077NM 2003 3 6 PCAA0303049 120030305A5522 ELEVATOR DHAV DHC8 DHC8102 2809003NM LEFT WORN A PCAAK NONE O OTHER ININSP/MAINT 1 EA13847EX 333 DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING AN A-4 INSPECTION, LEFT ELEVATOR HORN UPPER SKIN WAS FOUND TO HAVE 3 RIVET HOLES OVERSIZED AT STATION YH145.80. LEFT ELEVATOR HORN SKIN WAS REPAIRED IN ACCORDANCE WITH DER 8110-3 FORM FROM CALLAHAN AIRCRAFT SERVICES IDENTIFICATION NUMBER CAS-AAL111. LEFT ELEVATOR BALLANCE CHECKED IN ACCORDANCE WITH DEHAVILLAND DASH 8 STRUCTURAL REPAIR MANUAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030306000942003030600094SW 2003 3 6 HEEA084802 120030221A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 STARTER GENERATOR INOPERATIVE. 1G72 4U H4SW 20030307000702003030700070NM 2003 3 7 SWAA030484 120030304A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 4R CRACKED BETWEEN BS 663 AND BS 727. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20030307001192003030700119EU 2003 3 7 AALA20030080 120030119A5320 SUPPORT AIRBUS300 A300B4605R 3930308EU FUSELAGE FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW217083A 645 JFK - DURING OVERNIGHT MAINTENANCE, FOUND CHAFED AND BURNED WIRING LOCATED LEFT SIDE OF FUSELAGE DUE TO FAILURE OF PLASTIC SUPPORT. REPLACED WIRE BUNDLE SUPPORT AND WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20030307001922003030700192WP 2003 3 7 ABXA030105 120030220A5200591036751 DOUBLER DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 AFT PRESSURE BULKHEAD DOOR DOUBLER WAS CRACKED AT 5:00 O'CLOCK POSITION. REPAIRED IAW DC-9 SRM 52-05. 2L72 4F A6WE 20030121002102003012100210SW 2003 1 21 HEEA083353 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0353119 51575 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030121002642003012100264EA 2003 1 21 COMA0360036 120030119A7897 WIRE CNDAIRCL600 CL6002B19 1900309EA A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01486CA 7707 FLIGHT 5852 LEFT ENGINE REVERSER UNLOCKED WARNING MESSAGE.REPAIRED CHAFED WIRE AT T/R WIRE HARNESS. 2L72 4F RTA21EA 20030314002332003031400233NM 2003 3 14 UPS03240282 120030217A5330 SKIN BOEING727 727108C 1384039NM BS 1183 S9 & 10 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C&SI SKIN BULGING JUST FWD OF 1183 AND BETWEEN STR 9R & 10R AREA FOUND CORRODED OUTSIDE LIMITS IAW SRM 51-30-01. DAMAGED AREA CU T OUT IAW SRM 51-30-3 AT STR. 9.REMOVED CORROSION IAW SRM 51-20-01 F OUND WITHIN LIMITS IAW SRM 53-30-01. STRINGER TIE REMOVED IAW SRM 51 -10-2. NEW FILLER & DOUBLER FABRICATED IAW SRM 53-30-3. REPAIR INSTA LLED IAW SRM 53-30-3 2L73 4F A3WE 20030122000192003012200019SW 2003 1 22 HEEA083406 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108PH508 51334 MAIN BATTERY WEAK. 1G71 3U H2SW 20030324000082003032400008EU 2003 3 24 116933 120030321A7720 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE TORQUE FAILED A UHLAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 GL17152CQ 152CQ DURING TAKEOFF, FLIGHT NR 9450 HAD A LOSS OF INDICATION ON THEIR ITT AND TORQUE INDICATORS ON THE LEFT. AIRCREW RETURNED THE AIRCRAFT TO TTN. 2L72 4T4 TRTA52EU E8NE 20030326000792003032600079NM 2003 3 26 2003UALA00200 120030224A3610 SHUTOFF VALVE BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 BLEED FAILED A UALAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29176UA 24383 724683 NR 2 BLEED EICAS CAME ON DURING TAKEOFF. FLIGHT CONTINUED TO CRUISE, THE HIGH PRESSURE SHUTOFF VALVE WAS DEFECTIVE. REPLACED VALVE. 2L74 4F4 FRTA20WE E24NE 20040329000402004032900040WP 2004 3 29 ASAA0380390 120030421A5320593659215 SUPPORT ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FORWARD PIT STATION 523, BULKHEAD SUPPORT ANGLE CORRODED. REPLACED SUPPORT ANGLE PER SRM. (M) 2L72 4F A6WE 20030418001292003041800129 2003 4 18 SWIA200311785 420030215A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07294SW6783 6783 120321 AUTOPILOT FAIL AND TRIM FAIL LIGHT ON MAP CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. RAN THROUGH TESTS. OPS CHECK GOOD. 2L72 4T RTA31SO 20030421000062003042100006WP 2003 4 21 UPS03840232 120030212A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP AFT CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS AT STA 1580 AT LBL 5. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER IAW SRM 53-2-0 FIG 1G. 2L74 4F RT4A25 20030417000942003041700094EA 2003 4 17 SWIA200311750 120030130A3397 STUD CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSLOOSE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07449SW 7699 EMERGENCY LIGHTS WON'T TURN ON AT FLIGHT ATTENDANT STATION WHEN COCKPIT EMERGENCY LIGHT SWITCH IS IN ARM POSITION. TIGHTENED GROUNDING STUD FOR FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH LOCATED BEHIND CLOSET. OPS CHECK GOOD. 2L72 4F RTA21EA 20030716000072003071600007WP 2003 7 16 GTIA030452 120030612A3260 BULB DOUG DC9 DC982 3022082WP MLG INDICATOR BURNED OUT A GTIAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23823NK 48020 NOSE WHEEL NLG INDICATOR NOT OUT WHEN GEAR DOWN. LANDING GEAR NOSE LIGHT OUT. LUBRICATED NOSE GEAR VISUAL IND LEVER INDICATOR PRITRUDES .375 INCHES ABOVE TOP SURFACE OF PEDESTAL COVER PLACT WITH HYDRAULIC PRESSURE APPLIED. RELAMPED NOSE GEAR GREEN DOWN AND LOCKED LIGHTS AND OPS NORMAL. (M) 2L72 4F A6WE 20030724000452003072400045EU 2003 7 24 AWXA200300628 120030521A5340D53974672000 ATTACH ANGLE AIRBUS320 A320231 3930325EU BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-03 CHECK A .3125 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FORWARD BULKHEAD PANEL ATTACH ANGLE AT UPPER LT CORNER. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER; STOP DRILLED CRACK; FABRICATED A NEW REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 26-5314-00011-JS4. 2L72 4F RTA28NM 20030805000822003080500082EU 2003 8 5 ASOA03248 120030604A33503011210 LIGHT AEROSPATR72 ATR72 EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030807000422003080700042NM 2003 8 7 C1HA200393010 120030708A33501001141 BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOP. 2L73 4F A3WE 20030903001422003090300142 2003 9 3 2003F00528 420030624A34526226523208 CONTROL HEAD BEECH 1900 1900D 1154162CE TRANSPONDER BURNED A GUUAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO1987550 UE205 FLT 9158 - NAS - AFTER TAKEOFF, SMOKE IN COCKPIT FROM TRANSPONDER FACE PANEL. RETURNED TO NAS. LANDED WITHOUT INCIDENT. FOUND TRANSPONDER CONTROL HEAD BURNED INTERNALLY. REMOVED AND REPLACED CONTROL HEAD. NO DEFECTS NOTED. (M) 2L72 4T RTA24CE 20030903000832003090300083WP 2003 9 3 MEX2003270 120030707A2612892809040001 CONTROL UNIT DOUG DC9 DC982 3022082WP FIRE DETECTION FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23505MD2478 49149 DURING PREFLIGHT TRANSIT CHECK WAS DETECTED THE ENGINE FIRE ALARM SYSTEM DID NOT CANCEL AURAL WARNING. DURING REVISION RIGHT ENGINE LOOP B, BREAKER B-1 AND AMPLIFIER A2-6 WERE WITH DAMAGES. THE DUAL CONTROL UNIT WAS REPLACED IAW MM, ALL TESTS CORRECT. 2L72 4F A6WE 20030806000812003080600081NM 2003 8 6 AWXA200300808 120030717A2751 INDICATOR BOEING737 73733A 1384673NM TE FLAPS MALFUNCTIONED A AWXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP28164AW 23625 ON APPROACH WHEN FLAP EXTENDED TO 5 DEG, FLAP INDICATOR SPLIT AT 2 DEG, FORWARD AND OVERHEAD PANELS WERE GREEN, RETURNED FLAPS TO 1 DEG AND NEEDLES REMAINED SPLIT FOR APPROX 10 MIN THEN REALIGNED AT 1 DEG. SELECTED FLAPS TO 5 DEG AND SYSTEM OPERATED NORMALLY. LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED A FLAP POSITION INDICATION TEST SEVERAL TIMES IAW BMM 27-58-01, UNABLE TO DUPLICATE PROBLEM. INSPECTED THE FLAP TRANSMITTER AND INDICATOR CONNECTIONS, NO DEFECTS WERE NOTED. A FUP WAS WRITTEN FOR FOLLOW UP MAINTENANCE TO BE ACCOMPLISHED ON 07/21/2003. MX REMOVED & REPLACED FLAP POSITION INDICATOR & REPLACED BOTH LT & RT TRANSMITTERS IAW BMM 27-58-12, OPS CHECK OF FLAP INDICATION SYS GOOD. 2L72 4F RTA16WE 20030815000042003081500004WP 2003 8 15 GTIA030566 120030630A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FLIGHT COMPARTMENT FLOOR SUPPORT CORRODED AT FS 149-160 12 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20030826000302003082600030NM 2003 8 26 03FDEA01376 120030806A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE (OUTBOARD) FOUND CORROSION. RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE (OUTBOARD) REPAIR CARRIED OUT AS PER EA 1-5750-71799 : WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20030909000812003090900081 2003 9 9 SWIA200312301 420030819A3418607300001 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07459SW 7782 STALL FAIL CAUTION ILLUMINATED. REMOVED AND REPLACED STALL COMPUTER AND MACH TRANSDUCER IAW A/C MM 27-35-25. BOTH OPS CHECKS GOOD. P/N: 3995100208, S/N OFF: 162, S/N ON: 149. 2L72 4F RTA21EA 20030911000882003091100088WP 2003 9 11 DHL2003873532 120030623A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 NOSE SECTION LT TUNNEL FRAME AT STA -32.000 WITH 2.000 CRACK. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG.2. REMOVED DAMAGED FRAME IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FRAME IAW SRM 53-2-0 FIG 2. HEAT TREATED IAW SRM 51-1-1 PG 11. CLEANED, TREATED AND PRIMED FRAME IAW SRM 51-1-8B. INSTALLED FRAME WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911002102003091100210NM 2003 9 11 QXEA200300958 120030806A2810 ACCESS PANEL DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM OPEN A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09352PH 494 SEA- ON FLIGHT 2180 RETURNED TO FIELD DUE TO FUEL PANEL ACCESS DOOR OPENED IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. CLOSED FUEL PANEL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030730001442003073000144NM 2003 7 30 USAASB03090 120030624A2820693733588 CONTROL PANEL BOEING737 7373B7 1384580NM COCKPIT FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19514AU1752 23700 CLT - FLT 1125 - EN ROUTE PIT TO MSY, THE FUEL CROSSFEED VALVE WOULD NOT CLOSE AND THE LEFT CENTER BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED WITH 1,000 LBS OF FUEL IN THE TANK. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE P5-2 FUEL PANEL AND THE RIGHT CENTER LOW PRESSURE SWITCH, P/N 7G110-6. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030911002122003091100212EA 2003 9 11 QXEA200300976 120030812A2131GG670950265 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA CABIN PRESSURE FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09604QX211 211 10019 PDX- ON FLIGHT 2494 RIGHT PACK CAUTION MESSAGE DURING DESCENT. PERFORMED CAUTION ABNORMAL CHECKLIST FOLLOWED BY UNPRESSURIZED FLIGHT CHECKLIST AFTER DESCENDING BELOW 10,000 MSL. REMOVED AND REPLACED NR 2 ACSC. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030926000332003092600033NM 2003 9 26 03FDEA01394 120030827A2751 TRANSMITTER DOUG MD11 MD11 3023602NM TE FLAPS FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25604FE 48460 ON TAKEOFF RECEIVED LEVEL 2 "FLAP DISAGREE" ALERT. RIGHT INBOARD FLAP WENT TO 30 DEG., OTHER FLAPS WERE 25 DEG. RAN CHECKLIST AND RETURNED TO RPLB. ACN RELEASED FOR SERVICE PER MEL/CDL: 27-54-01CATEGORY: C EXPIRATION: 05SEP03 "MEL 27-54-01: FLAP POSITION INDICATOR - INOP. VERIFY SYMMETRICAL FLAP MOVEMENT PRIOR TO TAXI FOR EACH B LOCKOUT." (RIGHT INBOARD FLAP). R&R RIB FLAP POSITION TRANSMITTER PER MD 11 MM 27-54. 2L73 4F RTA22WE 20030929000832003092900083NM 2003 9 29 CALA0300513 120030904A5347 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND LT TIE DOWN RAIL CORRODED AT FASTENERS ON LOWER SURFACE AT STA 947 IN THE AFT CARGO COMPARTMENT. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20030930001192003093000119NM 2003 9 30 03FDEA01481 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B ACTUATOR LUG HOLE CORRODED. 2L73 4F RTA22WE 20031001000172003100100017WP 2003 10 1 ARWA20030907 120030903A5411 SPAR CAP DOUG DC8 DC861 3021952WP NR 4 PYLON DAMAGED A ARWAO OTHER O OTHER ININSP/MAINT 1 SO1929UA 46159 DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON INTERIOR STA YOP 225 LT LOWER SPAR CAP WITH STACK, BY ACCESS DOOR NR 426. 2L74 4F 4A25 20030908003432003090800343NM 2003 9 8 SWAA031927 120030828A552365C26384 HINGE BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED C3 CHECK, (SI 11138-55), RT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB ASSY PER MM. 2L72 4F RTA16WE 20030909002782003090900278 2003 9 9 RAIA00307199 420030727A3418C850176 VANE JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING FAULTY A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03557HK14097 41074 5375-BWI- RIGHT STALL WARNING WHEN ICE PROTECTION SELECTED. MAINTENANCE REMOVED AND REPLACED AOA VANE. 2L72 4T RTA41NM 20031002000652003100200065NM 2003 10 2 QXEA200301091 120030831A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 TWO CRACKS IN THE UNDERLYING STRUCTURE OF THE LT HAND NACELLE FIREWALL COMING OUT OF RIVET HOLES. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-54-180. 2H72 4T RTA13NM 20031003000322003100300032EU 2003 10 3 AALA20030538 120030507A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211413A 11376 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTING AT ROW 4 INOPERATIVE. REPLACED AFT CEILING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031028000692003102800069WP 2003 10 28 G6OA093003 120030929A261230231R17 FIRE DETECTOR DOUG DC10 DC1030F 3023504WP GE CF6 CF650* 30018NE FWD LOWER CARGO FAULTY A G6OAA UNSCHED LANDING BN SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CRCRUISE 1 EA27609GC 46932 NR 3 LOWER FWD CARGO FIRE LIGHT CAME ON STEADY THEN BECAME INTERMITTENT. SMELLED SMOKE IN CARGO BAY BRIEFLY. 2L73 4F4 FRTA22WE E23EA 20031103000672003110300067NM 2003 11 3 03FDEA01609 120030908A5753ARC050311 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 SNRM N0455: LT OB FLAP OB HINGE (A/C SIDE); IB AND OB UPPER ACTUATOR ATTACH LUG FOUND CORRODED AT BORES AND SPOT FITTING. CORRECTIVE ACTION SNRM N0455 : LT OB FLAP OB HINGE (A/C SIDE) IB AND OB UPPER ACTUATOR ATTACH LUG BORES AND SPOT FACES CORRODED AREA REPAIR CARRIED OUT IAW EA NR 1- 5750-71756 : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OB FLAP OB HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20031027000812003102700081SO 2003 10 27 SWIA200312514 120031011A2720 PEDAL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RUDDER RESTRICTED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07207SW 120266 AFTER ROTATION, RT RUDDER PEDAL RESTRICTED, WITH ABOUT 1 INCH OF MOVEMENT. RAN QRH JAMMED RUDDER PROCEDURE, TURNED OFF BLUE SYSTEM AND NORMAL RUDDER TRAVEL RETURNED.AFTER RUDDER DEFLECTIONS LEFT AND RIGHT WITH BLUE AND GREEN SYSTEMS IN DIFFERENT CONFIGURATIONS, COULD NOT DUPLICATE THE DISCREPANCY ABOVE. OPS CHECK GOOD. UPDATE 10/14/03: REMOVED AND REPLACED BLUE HYD RUDDER ACTUATOR DUE TO FAILURE OF HEALTH CHECK. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20031022001472003102200147EA 2003 10 22 SWIA200312432 120030922A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07903SW 7425 FS 484 LT INTERCOSTAL OB FLANGE LBL 36 AND ANGLE LBL 27 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. ''A''. REPAIR ANGLE P/N: S6144-14 2L72 4F4 FRTA21EA E15NE 20031022001572003102200157SO 2003 10 22 C2XA03SH344 120030924A541114576631608 RIB EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL NR 1 COWL CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK MAINTENANCE FOUND THE NR 1 LOWER ENGINE COWLING CENTER RIB TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-21-04 AND 51-21-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031028000202003102800020NM 2003 10 28 UPS03441273 120030917A575365B078305 RIB BOEING747 747121 1384871NM TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, LT WING NR 5 VC FLAP O/B LINKAGE I/B RIB CRACKED AT LINKAGE BOLT HOLT HEAD SECTION. LT WING NR 5 VC FLAP O/B LINKAGE I/B RIB REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20031119001402003111900140SO 2003 11 19 CHQA000425 120031011A2612 FIRE DETECTOR EMB 145 EMB145LR 3260212SO CARGO BAY MALFUNCTIONED A CHQAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 GL11273 145331 BAGGAGE FIRE LIGHT CAME ON DURING INITIAL DESCENT INTO LGA. DID NOT RECEIVE AN EICAS MESSAGE WITH IT. NO VISIBLE SIGNS OF SMOKE OR HEAT. DISCHARGED FIRE EXTINGUISHER BOTTLE. CONTINUED FLIGHT AND LANDED AT LGA WITHOUT INCIDENT. NO EVIDENCE OF FIRE WAS FOUND. REMOVED AND REPLACED HIGH RATE DISHARGE AND BAGGAGE METERING BOTTLE IAW MM 26-23-01. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040114000712004011400071NM 2004 1 14 DL767030987 120031106A5320 WEB BOEING767 767232 1385132NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27102DA 22214 HFEC INSPECTION OF THE AFT P-DOME WEB LAP JOINTS PER AD 88-19-03 REVEALED 26 CRACKS EMANATING FROM FASTENER HOLES ALONG THE LOWER ROW OF THE WEB LAP JOINT BETWEEN WL 190 & 230 (APPROX 210) ON THE RIGHT SIDE OF THE P-DOME. 2L72 4F RTA1NM 20031112000582003111200058NM 2003 11 12 AWXA200301394 120031019A533065C3380012 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MAJOR REPAIR - DURING C-21 CHECK A .75 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE ON FORWARD UPPER CORNER OF R-1 DOOR, BS 292.50. MAINTENANCE PERFORMED HFEC ON CRACK AND IDENTIFIED CRACK END; STOP DRILLED CRACK IN FUSELAGE SKIN AT R-1 DOOR FORWARD UPPER CORNER, BS 292.50; FABRICATED 3 EACH REPAIR DOUBLERS PER DWG 65C33800; INSTALLED REPAIR PARTS IAW EO 53-31-02. 2L72 4F RTA16WE 20031112001152003111200115WP 2003 11 12 ABXA030435 120031107A33505708458503 BATTERY PACK DOUG DC8 DC863 302198AWP CABIN DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX869 46122 DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY DEAD. REPLACED EMERGENCY BATTERY PACK. SYSTEM CHECKED GOOD IAW DC8 MM 33. 2L74 4F 4A25 20031103001452003110300145NE 2003 11 3 IXXA0300064O 220031024A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE NR 3 FLAMED OUT A IXXAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SW11830BX751961986 45973 693581 IN CRUISE FROM KTOL TO KLAX NR 3 ENGINE FLAMED OUT. ALL TANK SELECTORS AND CROSSFEEDS CLOSED (FULL UP POSITION) CREW RAN CFM-56 FLAME OUT/ INFLIGHT CHECK LIST. OIL PRESSURE NOTED AT ZERO. DISCONTINUED CHECK LIST AND SHUTDOWN ENGINE. CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT ENGINE PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. ENGINE IS FULLY OPERATIONAL AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20031103000912003110300091WP 2003 11 3 ABXA030378 120031001A571436463261 SUPPORT FITTING DOUG DC8 DC861 3021952WP CENTER WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 CORROSION ON UPPER CHORD OF CENTER WING REAR SPAR AT PRESSURE BULKHEAD F.S. 855, LEFT BUTT LINE 11 - 21. REMOVED AND INSTALLED BLOWOUT PANEL 3 EA. VERTICAL STIFFENERS, WEB ATTACH ANGLE, DOUBLER, FITTING AND SHEAR WEB ATTACH ANGLE IAW DC-8 SRM 51-30-0 AND 51-1-21. INSTALLED -3, -5, -11 FILLER, -9 AND -7 STRAP IAW DC-8 SRM 53-2-5. INSTALLED SPAR CAP ATTACH ANGLE P/N 3646326-1, 4648716-1 ANGLE WEB AT LEFT BUTT LINE 22 AND 5644011-1 ANGLE IAW DC-8 SRM 53-2-5 AND 51-1-20D. 2L74 4F 4A25 20031106002002003110600200NM 2003 11 6 ASAA0310473 120030515A5320BAC1509100146 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT FUSELAGE STATION 827, STRINGER 26R-27R CORRODED. CUT OUT DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20031006001402003100600140NM 2003 10 6 SWAA032034 120030909A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031121000822003112100082WP 2003 11 21 ABXA030441 120031030A5730591215642 SKIN DOUG DC9 DC914 3022034WP LEFT WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 RIGHT WING UPPER SKIN CORRODED AND PULLED RIVETS JUST INBOARD OF SPOILER ACTUATOR. REPLACED SECTION OF STRINGER AND SPLICE IAW DC-9 SRM 51-70-5 AND 51-30-5. 2L72 4F A6WE 20040112001512004011200151NM 2004 1 12 AALA20031459 120031221A2910 O-RING BOEING757 757223 1384957NM HYD SYSTEM DAMAGED A AALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW21641AA 24599 DFW EN ROUTE FLL-LAX CENTER HYDRAULIC SYSTEM DROPPED TO .34. LANDED DFW WITHOUT INCIDENT. REPLACED LEAKING CENTER HYDRAULIC SYSTEM ELECTRIC PUMP O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031212000122003121200012NM 2003 12 12 SWAA032433 120031104A55236941641 HINGE BRACKET BOEING737 7372H4 138448CNM LT ELEVATOR TAB WORN A SWAAK NONE FE FLT CONT AFFECTED VIBRATION/BUFFET NRNOT REPORTED 1 SW29074SW 22674 ABOVE 150 KNOTS SPEED, ACFT VIBRATION FELT. REMOVED AND REPLACED LEFT ELEVATOR INBD TAB HINGE BRACKET AND HARDWARE PER MM. 2L72 4F A16WE 20030915000482003091500048SW 2003 9 15 HEEA088928 120030826A6220206011132113A GRIP BELL 206 206L3 1182108SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 FOUND RETAINER BORE PITTING DUE TO INSUFFICIENT AMOUNT OF PROSEAL AT TIME OF GRIP ASSEMBLY. 1G71 3U H2SW 20030923001172003092300117WP 2003 9 23 DHL2003604699 120030527A53403754918U1 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT. FITTING CRACKED 1.000 AT STA. 1210.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, SRM 51-1-20D PG.9,21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG.9. 2L74 4F RT4A25 20040128000522004012800052NM 2004 1 28 AWXA200301613 120031215A531565528942 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON FLOOR SUPPORT CHANNEL AT BS 540, RBL 0 TO RBL 25. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT CHANNEL AT BS 540, RBL 0 TO RBL 25; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 FIG 2, PG 4. 2L72 4F RTA16WE 20040129000942004012900094WP 2004 1 29 0403 220031230A7261 SHAFT LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP OIL PUMP SHEARED E BSYAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL07130F 011405700197044 P89119 LEFT ENGINE LOST OIL PRESSURE ON DESCENT INTO COLUMBUS OHIO. SHUT DOWN ENGINE. FOUND ENGINE DRIVEN OIL PUMP SHAFT SHEARED. C/W SOAP SAMPLE AND REMOVED AND REPLACED PUMP OPS. CHECKS OK. 2L72 4F4 F A10CE E6WE 20040203000252004020300025NE 2004 2 3 ASAA0380519 220030701A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RIGHT FAILED A ASAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 NM01953AS 49386 LAX - A LOUD BANG AND VIBRATION FROM RT ENGINE CLIMB AT FL24500 OUT OF LAX. SUSPECT COMPRESSOR STALL. DECLARED EMERGENCY AND RETURNED TO LAX. ENGINE WAS REPLACED. SUBSEQUENT ENGINE TEARDOWN REVEALED A COMPLETE FAILURE OF THE T-3 AND T-4 STAGES, AND THIS FAILURE APPEARED TO BE THE RESULT OF T-3 BLADE ROOT RUB. DOWNSTREAM VANE AND OTHER DAMAGE WAS CAUSED BY THE (LIBERATED) TURBINE BLADES. (M) 2L72 4F4 F A6WE E9NE 20040204000692004020400069NM 2004 2 4 QXEA200301296 120031016A3260 INDICATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 WILL NOT TEST A QXEAO OTHER PL NO WARNING INDICATION NO TEST APAPPROACH 1 NM09374PH 528 ON FLIGHT 2037 DURING APPROACH RT MAIN GEAR GREEN DOWN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. GEAR CONFIRMED DOWN THROUGH ALTERNATE EXTENSION LIGHTS. RT MAIN GEAR DOWN LIGHT WILL NOT TEST. AIRCRAFT LANDED WITHOUT INCIDENT. CYCLED GEAR UP AND DOWN, FUNCTIONED NORMALLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040205000422004020500042NM 2004 2 5 UIEA200300062 120031113A2120 ODOR BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL COCKPIT DETECTED A UIEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15492MC 29253 PO83 ICN/HKG SMOKE IN COCKPIT: WHEN PARKING BRAKE SET, ELECTRICAL FUMES (BURNING ODOR) AND SMOKE CAME FROM RUDDER PEDALS AREA. ALL ELECTRICAL EQUIPMENT SHUTOFF. SMOKE AND FUMES WENT AWAY. REMOVED MAIN DECK CEILING PANEL AND SIDE PANEL OF PEDESTAL, ALSO REMOVED PFD, ND, EICAS CDU AND ACP. INSPECTED ALL THE INSIDE AREA AND PARK BRAKE RELAY. NO DEFECT FOUND. CLEANED INLET AREA OF AIR CONDITIONING, NO ADVANCED SMOKE ODOR. 2L74 4F4 FRT1384945 E23EA 20040212002012004021200201NM 2004 2 12 CALA0300723 120031228A5312 BULKHEAD BOEING737 7373T0 1384582NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND CORROSION ON APB WEB FORWARD FACE IB OF S27L ALONG LOWER RIVET ROW AT STA 1016. THE CORRODED SECTION OF WEB WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-80-08 AND MFG DRAWING NR 65C28106-1. 2L72 4F RTA16WE 20040308001652004030800165NM 2004 3 8 ASAA0310226 120030326A5320 STRAP BOEING737 737298C 1384490NM FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND STRAP AT BS 908, STRINGER 26L-26R WORN. REMOVED AND REPLACED STRAP PER SRM. (M) 2L72 4F RTA16WE 20031215000942003121500094NM 2003 12 15 MWEA030444 120031120A5347593054769 SEAT TRACK DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CORROSION ON NR 1 SEAT TRACK AT STATION 625. CUT OUT DAMAGE AND INSTALLED REPAIR. 2L72 4F RTA6WE 20040614002382004061400238NM 2004 6 14 RYN76394A 120031019A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077639U 19912 DURING A SCHEDULED INSPECTION FOUND FUSELAGE SKIN AT STA 303 STR 17-18R, UNDER FORWARD LAV SERVICE PANEL, HAS EXFOILIATED CORROSION. 2L73 4F4 F A3WE E2EA 20030813001242003081300124NM 2003 8 13 USAA030120 120030717A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19523AU 23858 PIT - FOUND SKIN CRACKED 3 INCHES, STATION 727E, 4 INCHES ABOVE S-24L. INSTALLED INTERIM DOUBLER PER EA 87406. (M) 2L72 4F RTA16WE 20030819000142003081900014NM 2003 8 19 USAA030102 120030701A5315 FLOORBEAM BOEING737 737401 1384701NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US40808 23986 FOUND FLOORBEAM CORRODED .5 INCH BY 1 INCH AREA, FLOORBEAM STATION 947 LBL 24.75 TO RBL 24.75. REPAIR FLANGE PER TYPICAL REPAIR 53-60-02 REV A, PART B. (M) 2L72 4F RTA16WE 20030819002312003081900231 2003 8 19 DXTA200300052 420030621A3415PH11001RCJW PITOT TUBE CESSNA750 750 2076810CE CONTAMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07904QS 7500210 YAW DAMPER & MACH TRIM DISENGAGED DURING TAKEOFF ROLL, ABORTED TAKEOFF. FOUND WATER SITTING IN RT PITOT TUBE. REMOVED RT PITOT TUBE AND CLEANED AND REINSTALLED PITOT TUBE, PERFORMED OPERATIONAL CHECK OF AIR DATA SYSTEMS AND YAW DAMPENER SYSTEMS IAW HONEYWELL PRIMUS 2000 OPERATING MANUAL. PITOT/STATIC LEAK CHECK GOOD ON LT AND RT PITOT/STATIC SYSTEMS IAW FAR 91.411. 2L72 4J RTT00007WI 20030819001002003081900100NM 2003 8 19 C1HA200396013 120030804A335037067001 BATTERY BOEING727 727200 138407ENM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA AFT AIRSTAIRS OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT BATTERY, OPS CHECK NORMAL. 2L73 4F RTA3WE 20030821000502003082100050NM 2003 8 21 03FDEA01059 120030702A5712ARB2850505 RIB DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LEFT WING, LEADING EDGE RIB CRACK INBOARD OF NR 16 SLAT TRACK. LEFT WING, LEADING EDGE RIB CRACK INBOARD OF NR 16 SLAT TRACK REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20030821000832003082100083NM 2003 8 21 03FDEA00930 120030612A5510ALC8100 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STAB UPPER CENTER PLANK 26L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 B PT1 LIMITATIONS. HORIZONTAL STAB CENTER PLANK 26L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030402000452003040200045NM 2003 4 2 2003UALA00322 120030325A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29789UA 26935 SKIN AND STRINGER S38-L DAMAGED BETWEEN STA 508 AND 529. MAJOR REPAIR ACCOMPLISHED. DOUBLER APPLIED ON FUSELAGE SKIN LOCATED LEFT SIDE BELOW STR 38 LT BETWEEN STA 508 AND 529. 2L72 4F4 FRTT0001SE E46NE 20030407000392003040700039WP 2003 4 7 GTIA030024 120030120A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSDAMAGED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT ROW 2, 4, 5, 7, 9, 11, 15, 19, 21, 22, 29, 30 AND 32. REPAIRED WIRING. (M) 2L72 4F A6WE 20030414000832003041400083NM 2003 4 14 AUS20030283 120030212A531169148714 FRAME BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME LOWER LEG LOCATED AT ZONE 1 BS 580 BETWEEN STRINGER 27 RT AND STRINGER 28 RT CONTAINED LEVEL 2 CORROSION. FOUND DURINGCPCP INSPECTION IAW C53-113-01. 2L73 4F4 FRTA3WE E2EA 20030410002422003041000242 2003 4 10 DL76L030125 420030203A23301301394100 VIDEO UNIT BOEING767 767332 1382001NM CABIN SHORTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27180DN 25985 SAN FWD TO MCO AND PLACARD PER MEL M25-25-02J. STATED THE AVU IN FWD CLOSET HAS INTERNAL SHORT, DISCONNECTED AVU AND PULLED AND COLLERED C/BS. ATL REPLACED VCC AVU AND WHEN POWER WAS TURNED ON FOUND SMOKE COMING FROM THE VMOD. REPLACED VMOD AND OPS CHECK GOOD. 2L72 4F RTA1NM 20030416000542003041600054NM 2003 4 16 HNAA0300016 120030331A3233 SPRING DHAV DHC8 DHC8102 2809003NM ACTUATOR ROD BROKEN A HNAAO OTHER J WARNING INDICATION CRCRUISE 1 EA07934HA47721 139 NR 2 MLG AFT INBOARD GEAR DOOR CAME OPEN IN FLIGHT. FOUND DOOR ACTUATOR ROD AND ALT EXTENSION SPRING BROKEN. REPLACED ROD AND SPRING. 2H72 4T RTA13NM 20030416004022003041600402EA 2003 4 16 SWIA200311695 120030113A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN SHORTED A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07597SW 7293 EMERGENCY LIGHTING SYSTEM HAS 3 STRIPS OF FLOOR LIGHTING INOP. THE LIGHT AT EXIT ROW 8 ON THE LEFT SIDE OF AIRCRAFT AT SEAT 8A IS INOP. FOUND NR 5 FLOOR LIGHT STRIP SHORTED. DISCONNECTED STRIP, LIGHTS WORK GOOD. REMOVED AND REPLACED NR 5 EMERGENCY FLOOR LIGHT STRIP. OPS CHECK GOOD. 2L72 4F RTA21EA 20030421002012003042100201NM 2003 4 21 UIEA200300013 120030307A7714473271 SENSOR BOEING747 7472D7B 1384803NM NR 1 ENGINE MALFUNCTIONED A UIEAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 EA15523MC 21782 JFK/MXP - INFLIGHT ENGINE SHUTDOWN. NR 1 ENGINE N1 EXCEEDANCE DURING DESCENT PROFILER WHILE A/T ENGATED AND THROTTLES MOVING FORWARD. N1 136.9 PERCENT FOR 11 SECONDS. EGT 666, N2 92.4, F/F 3218. NR 1 ENGINE SHUTDOWN IAW FHB. PERFORMED ENGINE OVERSPEED INSPECTION IAW 72-00-00 PAGE 680. NIL FOUND. SUSPECTED BAD N1 TRANSMITTER. REMOVED AND REPLACED NR 1 ENGINE N1 FAN SPEED SENSOR IAW 77-12-01-401. OPERATED NR 1 ENGINE MAX POWER ASSURANCE TEST 4. ALL FIGURES WITHIN LIMITS. N1 INDICATION NORMAL IAW 71-00-00. (M) 2L74 4F RTA20WE 20030423001432003042300143WP 2003 4 23 ZW0A0303002 120030310A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139402W 53138 THE EGRESS LIGHT WAS INOPERATIVE AT ROW 16 AND AT ROWS 20 TO 23. REPLACED THE LAMP P/N 79991-000 AT ROW 16, AND RESEATED THE CONNECTOR AT ROW 23. CHECK-C 9-4-02 STL. 2L72 4F RTA6WE 20030428001672003042800167WP 2003 4 28 03FDEA00412 120030409A3340 LIGHT DOUG DC10 DC1030 3023501WP STROBE FAILED A FDEAO OTHER N FALSE WARNING ININSP/MAINT 1 SO25320FE 47835 UPPER AND LOWER BEACON FAILS FLASH RATE CHECK. CLOSING ACTION 04/09/03. REMOVED AND REPLACED UPPER AND LOWER BEACON ASSEMBLIES. OP'S CHECK GOOD IAW M/M 33-45-00-4. 2L73 4F A22WE 20030428001962003042800196NM 2003 4 28 0300756739 120030406A5414 SKIN BOEING747 747251F 1384898NM NR 1 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01639US 23887 DURING H-CHECK, FOUND CRACK IN NR 1 PYLON SKIN AT NACELLE STA 174. REPAIRED PER EA 67-165061. 2L74 4F A20WE 20030429000532003042900053NM 2003 4 29 372PA0020 120030407A3350BP573 POWER SUPPLY BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 AFT STRIP OF EMERGENCY EXIT FLOOR PATH LIGHTING DIM. REPLACED BATTERY PACK AND BATTERY PACK POWER SUPPLY PER MM 33-51-51. 2L72 4F RTA16NE 20030429002042003042900204NM 2003 4 29 CALA0300192 120030412A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND AFT BAGGAGE BIN STRAP JUST INSIDE DOOR WHERE THRESHOLD WEB ATTACHES CORRODED. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030430000752003043000075SO 2003 4 30 SIMA200389005 120030307A531014529150001 CROSSBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE 145164 THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION CROSSBEAM CORRODED AT FRAME 22. REMOVED AND INSTALLED NEW CROSSBEAM SUPPORT IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M) 2L72 4F RTT00011AT 20030430000482003043000048NM 2003 4 30 2003UALA00391 120030423A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29653UA 25391 BS 1197, STRINGER 35R-38R HAS 24 INCH CREASE EXTERIOR SKIN. 2L72 4F4 FRTA1NM E24NE 20030502001782003050200178CE 2003 5 2 GLBA2003041 120030402A2150 SHUTOFF VALVE BEECH 1900 1900D 1154162CE ENVIRO SYSTEM OUT OF ADJUST A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03219GL UE219 RIGHT ENVIRO FAIL. ADJUSTED PRSOV, OPS CHECK GOOD. 2L72 4T RTA24CE 20030502002252003050200225NM 2003 5 2 EIA2003063 120030416A5312 BULKHEAD BOEING747 747273C 1384896NM LT MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 STA 1241, LT WHEEL WELL AFT PRESSURE BULKHEAD, PRESSURE ANGLE (65B10821-1) IS CORRODED BEYOND THE SRM ALLOWABLE LIMITS AND REQUIRES REMOVAL AND REPLACEMENT. STA 1241 LT WHEEL WELL AFT PRESSURE BULKHEAD REPAIRED PER ECRA 471-57-212-2 AND ECRA 471-57-214-2. 2L74 4F A20WE 20030505001462003050500146NM 2003 5 5 03015 120030423A213065B0263729 CONTROL PANEL BOEING747 747132 1384882NM CABIN PRESSURE DAMAGED A KCSAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL23709CK 20247 FL 35.0, HEARD LOUD NOISE WITH CABIN ALTITUDE RAPIDLY CLIMBING AND UNABLE TO CONTROL IN AUTO OR MANUAL. DESENDED TO FL 27.0 WAS ABLE TO MAINTAIN CABIN ALTITUDE OF 16,000 FT. COUNTINUED REMAINDER OF FLIGHT ON OXYGEN. 2L74 4F A20WE 20030506001322003050600132WP 2003 5 6 GTIA030146 120030221A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE STA 180 TO 160 DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FWD CABIN STA 180 TO 160 LBR 8 INCHES TO 44 INCHES (20X36) FLOOR PANEL SOFT/ MUCHEY DAMAGED DETERIORATED CORR. INSERTS. FABRICATED NEW PANEL. 2L72 4F4 FRTA6WE E2EA 20030508000692003050800069NM 2003 5 8 DL764030357 120030415A3350 BULB BOEING767 767 UTILUSENM ESCAPE SLIDE BURNED OUT A DALAO OTHER O OTHER NRNOT REPORTED 1 SO27832MH 29704 2L DOOR SLIDE LIGHT INOPERATIVE AT DEPARTURE. RELAMP OPS NOW CHECKS NORMAL. 2L72 4F RTA1NM 20030508001082003050800108NM 2003 5 8 DL73S030370 120030417A3350BPS73 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER L NO TEST ININSP/MAINT 1 SO27308DL 23080 ON LAYOVER FOUND EMERGENCY LIGHTS INOP ROWS 1-4----REMOVED AND REPLACED POWER SUPPLY AND SYSTEM CHKS OK 2L72 4F RTA16WE 20030513000882003051300088NM 2003 5 13 UPS03240670 120030415A5330 BUTT JOINT BOEING727 72722C 138400FNM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE:C&SI NDT INSP. HAS INDICATION OF MATERIAL LOSS AT BS 1080 BUTT JOINT BETW EEN S2L & 2R. VISUAL INSP. CARRIED OUT CORROSION FOUND TO EXTEND UP TO S3L NEW CUT OUT LINE MADE IAW 69-62161 S3L REPAIR CARRIED OUT IAW DRAWINGS 69-6 2161 & UPS EO B727-5330-1177-M 2L73 4F A3WE 20030515001202003051500120SO 2003 5 15 C2XA03BT057 120030428A2497 CONTACTOR EMB 145 EMB145 3260210SO COCKPIT FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2734111 145659 EWR---CO2853, CREW REPORTED, STRONG ELECTRICAL ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED ESSENTIAL BUSS CONTACTOR (EBC) IAW EMB 145 XR MM 24-60-03. OPS CHECKED GOOD. NO ELECTRICAL ODOR SMELL WAS FOUND AT THIS POINT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030530000532003053000053NE 2003 5 30 HEEA086550 120030522A324030242 BRAKE ASSY SKRSKYS76 S76A 8143006NE MLG LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW031546G 760076 LT WHEEL BRAKE LEAKING. SHOP REPAIR. 1G72 3U H1NE 20030602001412003060200141NM 2003 6 2 SWAA031152 120030522A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CRACKED, BS 947.5, LBL 53. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20030604001282003060400128NM 2003 6 4 UPS03440543 120030406A5711 SPAR BOEING747 747121 1384871NM NR 3 SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LT WING UPPER SURFACE FRONT SPAR RABBET AREA PANEL FOUND BULGE AT NR 3 SLAT I/B AREA AS MARKED. LT WING UPPER SURFACE FRONT SPAR REPAIRED AS PER RS R57-25-35006 AND ENGINEERING FILE NUMBER 747-57-20040 AT NR 3 SLAT I/B AREA WS 1336 2L74 4F A20WE 20030515000092003051500009NM 2003 5 15 03126406 120030506A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27406FJ 3156 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS AT SEAT ROWS 9 AND 10 WERE INOPERATIVE. MAINTENANCE PERSONNEL RESET THE CIRCUIT BREAKER FOR THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030515001482003051500148 2003 5 15 AWXA200300464 420030504A2565 BOTTLE BOEING757 7572S7 1384962NM ESCAPE SLIDE READS LOW A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW610526249 23323 PHX - EES - DURING INSPECTION THE R-4 DOOR MOUNTED EMERGENCY ESCAPE SLIDE NEEDLE WAS OUT OF GREEN BAND. MAINTENANCE REMOVED AND REPLACED THE R-4 DOOR EMERGENCY ESCAPE SLIDE IAW AWA T/C R1C25602. 2L72 4F RTA2NM 20040113001642004011300164EU 2004 1 13 BAQA091261 120031030A2435524031 BRUSHES AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365KY1269 6529 STARTER-GEN BRUSHES WORN BEYOND LIMITS. BEARING WORN. OVERHAULED STARTER GENERATOR. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H10EU E19EU 20040113001702004011300170NM 2004 1 13 TSAA0375198 120031210A7500655812310 DUCT BOEING737 7372T4 1384492NM NR 1 ENGINE FAILED A TSAAO OTHER J WARNING INDICATION CLCLIMB 1 WP13807AL 23443 FLT 240 - HNL-OGG - ENGINE NR 1 OVERHEAT LIGHT CAME ON JUST AFTER TAKEOFF. PULLED THROTTLE BACK AND THE LIGHT WENT OUT. EGT IN GREEN THE ENTIRE TIME. REMOVED AND REPLACED NR 1 COWL ANTI-ICE UPPER DUCTING. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040113000752004011300075NM 2004 1 13 03FDEA02239 120031223A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 ON TOP OF FLOORBEAM STA 328 RT SIDE THERE IS A DENT. REWORKED AREA IAW SRM 51-40-1. NDT FOUND TO BE CRACKED. CUT OUT CRACKED AREA IAW SRM 51-40-4. FABRICATED REPAIR ANGLES IAW SRM 51-40-4. INSTALLED REPAIR ANGLES IAW SRM 51-40-4 & 51-30-2. 2L73 4F RTA3WE 20040114000272004011400027SO 2004 1 14 C2XA03TY220 120031226A531514521700007 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS DURING A SCHEDULED 3C INSPECTION THE LEFT OMEGA BEAM WAS CORRODED AT THE BOTTOM OF THE GALLEY RAMP ANGLE. MAINT REMOVED THE OMEGA BEAM, FAB SPLICE DOUBLER, ALODINED, PRIMED AND INSTALL SPLICE DOUBLER AND INSTALL THE NEW OMEGA BEAM IAW EMB 135/145 SRM 51-40-02; 53-21-10; CPM 51-21-04-05 AND SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031202000152003120200015WP 2003 12 2 GTIA030730 120030905A3150 WARNING LIGHT DOUG DC9 DC982 3022082WP COCKPIT ILLUMINATED A GTIAK NONE J WARNING INDICATION ININSP/MAINT 1 GL23817NK 49141 LEFT ICE PROT TEMP HI-LIGHT ILLUMINATES WITH AIRFOIL ANTI-ICE ON. CLOSING X-FEED VALVE EXTINGUISHES LIGHT. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F A6WE 20031216000072003121600007NM 2003 12 16 QXEA200301445 120031118A5310 DOOR FRAME DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX- BAGGAGE DOOR SURROUND STRUCTURE IS CHAFED AT BOTH TOP DOOR STOP FRAME AREAS. REPAIRED IAW DHC-8 RD 8-53-5461 AND SRM 51-00-06. 2H72 4T RTA13NM 20031219000102003121900010WP 2003 12 19 ABXA030457 120031119A532039135771 INTERCOSTAL DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 INTERCOSTAL CRACKED AT STA 389 BUTTLINE XERO AT FLOORBEAM ATTACH POINT. REPAIRED IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20031222001292003122200129SO 2003 12 22 SIMA200332703 120031120A2510 PIN EMB 135 EMB135LR 3260305SO COCKPIT SEAT LACK OF LUBE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21716AE 145264 CREW REPORTED SEAT TRACK WOULD NOT LOCK. MAINTENANCE REMVOED AND LUBRICATED THE LT AND RT LOCKING PINS AND LUBRICATED THE PIN SHAFTS. THE PINS WERE REINSTALLED IAW WORK CARD 25-200-07. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20031224000042003122400004WP 2003 12 24 GTIA030820 120030929A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN STATION 1309 RBL 46 FLOOR WEB CRACKED UNDERNEATH SEAT TRACK. TRIMMED OUT DAMAGED/CRACKED AREA. DRILLED AND LOCATED FILLER AND DOUBLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F A6WE 20031231000012003123100001WP 2003 12 31 GTIA030907 120031106A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 CABIN STATION 160 RBL 30 - RBL 37 FLOORBEAM CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20031014001762003101400176NM 2003 10 14 SWAA032078 120030918A2730656531014 TORQUE TUBE BOEING737 7373H4 1384600NM RT & LT ELEVATORWORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATORS FAILED THE FREE PLAY CK. REMOVED AND REPLACED ELEVATOR CONTROL TORQUE TUBE ASSY PER MM. 2L72 4F RTA16WE 20031009000532003100900053NM 2003 10 9 03FDEA01698 120031003A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 FWD CARGO SIDE FRAME DENTED STA 720 LBL 34 WL 160. DENT OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED FRAME BS 720, LBL 34, WL 160 IAW SRM 53-10-1, 51-40-3 FIG 1 AND FED EX EA 7-5310-55029. 2L73 4F RTA3WE 20031020003142003102000314 2003 10 20 SWIA200312450 420030922A3418501125904 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA STICK PUSHER DEFECTIVE A SWIAK NONE F FLT CONT AFFECTED LDLANDING 1 NM07946SW 7776 ON LANDING FLARE ELEVATOR HUNG AT LAST FEW DEGREES OF TRAVEL. AFTER LANDING CREW NOTICED A CATCH IN THE ELEVATOR TRAVEL IN LAST THIRD OF UP TRAVEL. REPLACED STALL STICK PUSHER ACTUATOR SERVO IAW MM 27-35-15. OPS CHECKED GOOD. 2L72 4F RTA21EA 20040311000552004031100055NM 2004 3 11 ASAA0310097 120030306A5347BAC15201397 CARGO TRACK BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND CARGO TRACK AT BS 780, RIGHT BUTTOCK LINE 15 CORRODED. REMOVED AND REPLACED TRACK PER SRM. (M) 2L72 4F RTA16WE 20031202001392003120200139EA 2003 12 2 ASOA03510 120031013A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11867AS 7463 DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52-00. (M) 2L72 4F RTA21EA 20030609001592003060900159CE 2003 6 9 DXTA200300034 120030519A215073838415 ACM CESSNA650 650 2076802CE AIR CON DEFECTIVE E DXTAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07779QS 6507079 UPON TAXI, AN ELECTRICAL ODOR WAS DETECTED, FOLLOWED BY SMOKE IN THE COCKPIT. AFTER INTIAL ATTEMPTS TO ISOLATE PROBLEM (PACS, RADIOS, ECT) WE SHUT DOWN ENGS AND SYSTEMS. THE SMOKE WAS PREVELENT THROUGHOUT AIRPLANE. FOUND AFT AIR CYCLE MACHINE DEFECTIVE. 2L72 4F A9NM 20030610000582003061000058NM 2003 6 10 C1HA200388006 120030523A3350ADMISC062 BATTERY PACK BOEING727 7272S7 138407ZNM COCKPIT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15688CA 22344 COCKPIT EMERGENCY EXIT LIGHT IS INOP 2L73 4F A3WE 20030612000552003061200055WP 2003 6 12 ABXA030178 120030513A5320991050119 WEB DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 LEFT CUSP WEB EXFOLIATED BETWEEN FS 256-275. REPLACED CUSP WEB AT STA 237 TO 296 IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 20030520000742003052000074WP 2003 5 20 GTIA030254 120030415A3397 CONNECTOR DOUG DC9 DC981 3022081WP BATTERY PACK LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 MCO - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE OUTPUT CONNECTION ON BATTERY PACK FOR TAIL COMP EMERGENCY LIGHTS, OPS CHECKOK IAW MM 33-53-00. (M) 2L72 4F A6WE 20030523000462003052300046EA 2003 5 23 QXEA0300574 120030515A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX- DAMAGED RIVET 10 INCHES AFT OF FIRST OFFICERS SIDE WINDOW ON STRINGER 11AR. REPAIRED IAW HORIZON AIR EA R-53-106 AND REO 670-53-00-036. 2L72 4F RTA21EA 20030523000612003052300061NM 2003 5 23 QXEA0300529 120030501A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAPS ILLUMINATED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09403QX 4037 SEA- ON FLIGHT 2296 ON SHORT AND FINAL INTO SEA FLAP POWER CAUTION LIGHT ILLUMINATED WHEN FLAP SELECTED FROM 5 DEGREES TO 15 DEGREES. FLAPS STOPPED AT 10 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. CLEARED FLAP POWER CAUTION LIGHT AND PERFORMED OPERATIONAL CHECK OF WING FLAPS IAW Q400 TASK 27-50-00-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030523001212003052300121NM 2003 5 23 2003UALA00427 120030513A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29786UA 26938 EXTERNAL EEL LIGHT INOP AT DOOR 4R. RELAMPED EXTERNAL EEL LIGHT. 2L72 4F4 FRTT0001SE E46NE 20030523000342003052300034EA 2003 5 23 QXEA0300616 120030519A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 400 ILLUMINATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09607QX 10024 DEN ON FLIGHT 2443 ABORTED TAKEOFF DUE TO LEFT REVERSE UNSAFE CAUTION MESSAGE CAME ON AT THE BEGINING OF THE TAKEOFF ROLL. COMPLIED WITH FUNCTIONAL TEST OF LEFT REVERSER IAW 78-30-00-720-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030523000902003052300090WP 2003 5 23 MWEA030216 120030519A5347SRO953011115 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FIRST OFFICER'S AFT OUTBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED TRACK. 2L72 4F A6WE 20030717000352003071700035NE 2003 7 17 AC2A087919 120030602A54107630307019042 LATCH SKRSKYS76 S76A 8143006NE NACELLE DOOR BROKEN B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO075447C 760180 RT FWD ENGINE COWL LATCH FAILED IN FLIGHT. UPON LANDING IT WAS DISCOVERED THAT THE COWLING HAD LIFTED 2 INCHES ON RIGHT HAND SIDE. THE LATCH HOOK ON THE FWD. LATCH WAS COMPLETELY MISSING AND THE AFT LATCH WAS CLOSED BUT NOT HOOKED TO THE AIRFRAME FITTING. FWD. LATCH HOOK WAS REPAIRED. 1G72 3U H1NE 20030708000482003070800048WP 2003 7 8 UPS03840827 120030526A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C1, STA. 1690 AFT SIDE LONG. 30L END FITTING AND LONGERON SECTION IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING,FABRICATED AND REPLACED LONGERON SECTION IAW DWG. 5649329 AND SRM.53-2-2 FIG. 10 AND 51-1-21,51-1-20D. 2L74 4F RT4A25 20030709000022003070900002WP 2003 7 9 GTIA030430 120030511A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND CABIN LEFT INBOARD SEAT TRACK CORRODED FS 1309-1214. CUT OUT LEFT INBOARD SEAT TRACK. LOCATED AND DRILLED NEW SECTION OF SEAT TRACK. INSTALLED LEFT INBOARD SEAT TRACK. (M) 2L72 4F A6WE 20030714000992003071400099NM 2003 7 14 371PA0027 120030629A3350 LIGHT BOEING737 737306 13844BGNM CABIN CONTAMINATED A PIDAO OTHER L NO TEST NRNOT REPORTED 1 SO05371PA 23543 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING SYSTEM INOP. CLEANED FLUID FROM TRACK AND LIGHT SYSTEM. OPS CHECKS NORMAL. 2L72 4F RTA16NE 20030110000512003011000051WP 2003 1 10 MWEA030029 120030110A5330591142267 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE UNWANTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 REPAIR HOLE IN FUSELAGE SKIN WHERE EMERGENCY LOCATING TRANSMITTER WAS REMOVED. -- FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER. 2L72 4F A6WE 20030128000452003012800045GL 2003 1 28 HEEA083798 220030115A732023072725 HYDROMECH UNIT BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 HMU PRODUCING ROTOR DROOP IN FLIGHT. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030129001152003012900115SW 2003 1 29 HEEA083998 120030117A5200407064807119 SUPPORT BELL 407 407 1182206SW ENG BAY DOOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 ENGINE BAY DOOR SUPPORT HAS ELONGATED MOUNT HOLE. 1G71 3U O H2SW 20030205000472003020500047NM 2003 2 5 SROM200300014 120030116A5414657377482 SKIN BOEING737 737205 1384456NM ZONE 400 CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA 1310 23466 DURING C CHECK INSPECTION FOUND NR 2 ENGINE IB NACELLE SKIN CRACKED BETWEEN NR 3 & 4 RIBS, 27 INCHES FROM LOWER EDGE. CUT OUT DAMAGE 1.3 X 1.5 INCHES, FABRICATED REPAIR DOUBLER, ALODINED & PRIMED PART AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2, 51-10-3 & 54-30-1. 2L72 4F RTA16WE 20030211000062003021100006EU 2003 2 11 03028330 120030128A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP CABIN DAMAGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27330UE 41098 FORWARD EMERGENCY TRACK LIGHTING INOPERATIVE. REPAIRED WIRING AND REPLACE NR 1 POWER SUPPLY, OPS CHECKED OK. 2L72 4T3 TRTA41NM E2WE 20030212000902003021200090EU 2003 2 12 WRNA200300004 120030207A2710A5766100117500 AILERON AIRBUS300 A300B4203 3930306EU DELAMINATED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05505TA 271 On walk around found R/H I/B aileron to have damage. This damage is on the top trailing edge where a section of skin is peeling aft (approx. 4' width and 8" in length) exposing honeycomb.Corrective Action: Removed and replaced right wing in-board all speed aileron I/A/W MM 27-11-28. Functional ck satisfactory on ground. A/C prepared for Test Flt per GMM procedures. Test Flt.C/W and functional ck satisfactory A/C returned to service. 2L72 4F RTA35EU 20030401001062003040100106WP 2003 4 1 DHL2003803003 120030212A2611 SMOKE DETECTOR DOUG DC8 DC873 302199CWP NR 13 MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01803DH 46123 SMOKE DETECTOR NR 13 TEST IMPROPERLY LIGHT STAY'S ON. RELAMPED NR 13 SMOKE DETECTOR, NO HELP. DEFERRED IAW MEL 26-6-1 DMI 11984. 2L74 4F RT4A25 20030214000462003021400046NM 2003 2 14 P5CA0300754 120030129A5320NONE INTERCOSTAL BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND ON INTERCOSTAL BTWN LBL 25-LBL 45 AND SHEARED RIVETS ON FWD CARGO SEAT TRACK. DAMAGED INTERCOSTAL REMOVED NEW FABRICATED H/F 2024 T3 0050 THK PER SAMPLE PER SRM 59-10-21. PROTECTED AREA PER SRM 51-10-02 RIVETED PER SRM 51-30-02. 2L74 4F A20WE 20030218002462003021800246NM 2003 2 18 SWAA030242 120030131A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, ABOVE STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030219000072003021900007SO 2003 2 19 HJL2003F00000 220030124A7414 DISTRIBUTOR GEARBENDIX MOONEYM20 M20K 5870220SW CONT O360 TSIO360LB 17025SO RT MAGNETO FAILED G HJLAK NONE O OTHER ININSP/MAINT 1 SW174710H D02AA087R 250473 247441R 810470 AIRCRAFT FAILED TO RUN/ LESS THAN 500 FT/MIN CLIMB. UPON INSPECTION FOUND TEETH IN DISTRIBUTOR GEAR SHEARED- 30 DEGREE. 1L71 3O3 O 2A3 E9CE 20030219000322003021900032SW 2003 2 19 ALG2003F00008 120030104A2697 WIRE BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE NR 2 FIRE DETECTBROKEN E ALGAK NONE O OTHER ININSP/MAINT 1 SW03393AL 28117 ON THE PREFLIGHT CHECK, NR 2 FIRE DETECTION SYSTEM INOPERATIVE. A WIRE WAS FOUND BROKEN AT THE NR 2 FIRE DETECTION AMPLIFIER. 2G72 4U4 U H10SW E8NE 20030219000372003021900037WP 2003 2 19 MWEA030091 120030213A53129915558248 CLIP DOUG DC9 DC981 3022081WP FWD APB BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 UPPER AND LOWER ANGLE SUPPORT ON FORWARD SIDE OF AFT PRESSURE BULKHEAD FORMER IS BENT RIGHT OUTBOARD AREA SECOND FORMER DOWN FROM TOP. -- LOCATED AND DRILLED AND INSTALLED NEW CLIP. 2L72 4F A6WE 20030221000032003022100003NM 2003 2 21 AWXA200300019 120030108A2620 WARNING LIGHT AIRBUSA319 A319132 3930340NM APU FIRE PANEL FALSE ACTIVATIONA AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28809AW 1111 ON CLIMB OUT AT FL 180 NR 2 ENGINE, NR 2 DISCHARGE LIGHT ILLUMINATED, NO OTHER INDICATIONS. DIVERTED TO MCI AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE AT MCI PLACED THE SYSTEM ON MEL, COND. 1, "ENG 2 AGENT 2 DISCHARGE LIGHT SYSTEM INOP", AND PERFORMED MAINTENANCE PROCEDURES ASSOCIATED WITH MEL VERIFYING DISCHARGE BOTTLE WAS PROPERLY CHARGED. MAINTENANCE CONFIRMED FAULT AND FOUND DISCHARGE LIGHT CAME ON WITHOUT AN ECAM WARNING AFTER THE NR 2 ENGINE FIRE TEST BUTTON WAS PRESSED. ALSO DISCOVERED THAT TAPPING THE ENGINE / APU FIRE PANEL CAUSED THE DISCHARGE LIGHT TO EXTINGUISH. REMOVED AND REPLACED ENGINE / APU FIRE PANEL ; PERFORMED FUNCTIONAL AND OPERATIONAL TESTS IAW AMM 26-12-401, ALL TESTS PASSED. 2L72 4F RTA28NM 20030221000692003022100069SO 2003 2 21 C2XA03CL044 120030218A33207287500603 HARNESS EMB 145 EMB145LR 3260212SO CABIN SHORTED A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2713975 145163 LIT FLIGHT#2474 THE CREW REPORTED THE CABIN LIGHT AT ROW 6A SHORTED OUT CAUSING SPARKS AND ELECTRICAL SMELL IN THE CABIN.MAINTENANCE INSPECTED AND REPLACED THE WIRING HARNESS ASSEMBLY FOR ROW 6A LIGHTING.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20030224001292003022400129SO 2003 2 24 C2XA03IA023 120030221A793123073715 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO ENGINE INOPERATIVE A C2XAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW2713550 145575 IAH- FLIGHT 7834, ON TAKEOFF ROLL THE CREW NOTED THAT THE #2 LOW OIL PRESSURE WARNING ILLIMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE #2 LOW OIL PRESSURE SWITCH IAW AEMM 79-31-01, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030115001142003011500114EU 2003 1 15 BAQA082883 120030107A6410365A12002002 BLADE AEROSPSA365 SA365N 8680669EU TAIL ROTOR DAMAGED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01199SM421 6396 TAIL ROTOR BLADE NEEDS TO BE REFINISHED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030304000712003030400071NM 2003 3 4 DLM88030073 120030117A21305953625521 DUCT 5953625521 DOUG MD88 MD88 3023688NM AFT AIR COND BAYCRACKED A DALAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO27923DL UNK 49705 AFTER T/O AIRCRAFT WOULD NOT PRESSURIZE. BOTH PACKS WERE ON FLOW LIGHT ILLUMINATED. FOUND RT HOT AIR MANIFOLD DUCT CRACKED - REPLACED SAME 2L72 4F RTA6WE 20030225000852003022500085SW 2003 2 25 HEEA084299 120030211A6321 BOLT BELL 407 407 1182206SW R/BRAKE CALIPER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 316 53283 ROTOR BRAKE CALIPER HAS WORN BOLTS. 1G71 3U O H2SW 20030228000822003022800082WP 2003 2 28 ASAA0380006 120030103A533059364353 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, FUSELAGE SKIN DENTED AT FS 1124. INSTALLED INTERNAL DOUBLER OVER DENT PER SRM 53-04. (M) 2L72 4F RTA6WE 20030303000502003030300050SW 2003 3 3 HEEA084507 120030214A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 STARTER GENERATOR DRAGGING CAUSING ENGINE TO START HOTTER THAN NORMAL. 1G72 4U H4SW 20030325000152003032500015EU 2003 3 25 AWXA200300125 120030201A5210FE240004 SNUBBER AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE DOORS WEAK A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW19896 770 MCN - EMERGENCY EVACUATION - DURING C-04 CHECK, THE L-1 DOOR SNUBBER WAS FOUND TO BE WEAK DURING OPERATION. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR SNUBBER CYLINDER PER AIRBUS AMM TASK'S 52-13-14-020-057, AND 52-13-14-220-053. OPERATIONAL CHECK WAS PERFORMED PER 52-10-00-710-051 AND WAS FOUND GOOD. 2L72 4F4 FRTA28NM E311NE 20030325000782003032500078EU 2003 3 25 AWXA200300245 120030301A5315D5347209400200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-03 CHECK CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF CABIN FLOORBEAM AT Y512, FR 66 -1 TO +5. MAINTENANCE REMOVED CORRODED FLOORBEAM FROM FR 64 TO FR 70, Y512; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6 & 7. 2L72 4F RTA28NM 20030325001002003032500100EU 2003 3 25 AWXA200300263 120030301A5315D5347209800600 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF CABIN FLOORBEAM AT FR 66+7, Y919. MAINTENANCE REMOVED CORRODED FLOORBEAM AT FR 66+7, Y919; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6-7, AND SRM 51-49-00, PG. 5-6, TABLE 1. 2L72 4F RTA28NM 20030306000792003030600079SW 2003 3 6 HEEA084789 120030221A5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 STEP ACTUATOR ONLY TRAVELS HALF WAY BEFORE STOPPING. 1G72 4U H4SW 20030311000112003031100011CE 2003 3 11 2003NSVA00020 120030309A52101295140791 SUPPORT BEECH BEECH 1900 1900D 1154162CE BROKEN A NSVAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27243CJ UE43 During taxi out the cabin door light illuminated. Crew taxied back to gate and FO was able to open the door without pushing in the door lock release button. Maintenance found the door handle upper support assembly broken. Replace the support and returned the aircraft to service. 2L72 4T RTA24CE 20030311000322003031100032GL 2003 3 11 HEEA085049 220030228A732025490926 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036748D 51106 FUEL CONTROL HAS NO ADJUSTMENT LEFT FOR LIGHT OFF. INTERMITTENTLY FAILS TO LIGHT OFF. SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030311001052003031100105 2003 3 11 249TR0014 420030303A22301633568801 COMPUTER BOEING737 7372K5 138448XNM A PIDAK NONE R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO05249TR 22598 PDC dumps data during take off, auto throttles retarding from climb power when EPR selected, (major power reduction). Unable to duplicate. Swapped PDC com. from A/C 251TR per MM 34-18-11. Ops chk good per MM 34-18-0 2L72 4F RTA16WE 20030313002122003031300212WP 2003 3 13 AALA20030180 120030207A3397 WIRE DOUG DC9 DC982 3022082WP A/C BAY DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21488AA 49681 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FOR TAIL CONE JETTISON INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE FOR TAIL CONE JETTISON LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030314000442003031400044WP 2003 3 14 ABXA030084 120030226A5280 STRUCTURE DOUG DC9 DC931 3022065WP MLG DOOR CONTAMINATED A ABXAO OTHER O OTHER APAPPROACH 1 GL23945AX 47551 UPON INITIAL GEAR EXTENSION, GEAR DID NOT EXTEND. AUX/ALT HYDRAULIC PUMPS WERE ON. ENGINE HYDRAULIC PUMPS WERE HIGH HYDRAULIC PRESSURE / QUANTITY WERE NORMAL. AFTER APPROXIMATELY 20 SECONDS, CREW RECYCLED LANDING GEAR AND GEAR EXTENDED NORMALLY. FOUND EXCESSIVE WATER COMING FROM INSIDE THE GEAR DOORS. LUBRICATED GEAR AND DRAINED WATER. OPS CHECKED GOOD IAW DC-9 MM 32-30-00-2-0003. OPS CHECKED GOOD AND NO DEFECTS NOTED. 2L72 4F A6WE 20030314001492003031400149NE 2003 3 14 048548 220030307A7230PT6A67DGG GAS GENERATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 2 ENGINE FAILED A AMWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE07131YV7201 7201 UE131 CREW WAS ON TAKE OFF ROLL WHEN POWER WAS APPLIED TO THE NR 2 ENGINE. THE CREW HEARD A LOUD BANG FROM THE RIGHT SIDE OF THE AIRCRAFT. THEY ABORTED THE TAKE OFF AND TAXIED BACK DOWN TO THE GATE. THEY PROCEEDED TO PERFORM A CHECKLIST BY VISUALLY INSPECTING ENGINE FROM THE CABIN. MAINTENANCE REMOVED AND REPLACED THE GAS GENERATOR. THE TEARDOWN REPORT REVEALED THAT THE GAS GENERATOR CASE WAS FOUND WITH ONE DIFFUSER PIPE LOOSE AND IT WILL BE REPAIRED. 2L72 4T4 TRTA24CE E26NE 20030317000222003031700022NM 2003 3 17 03FDEA00155 120030221A5313 STRINGER BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON STR 28R, BS 480-484, WL 150, INBOARD SIDE. REMOVED CORROSION FROM STR 28R AT B.S 480+4 INCH, FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED AND PRIMED REPAIR PARTS, AND INSTALLED IAW SRM 51-10-4, 53-10-1, 53-10-3, 51- 30-2 AND MM 51-20-151-7. 2L73 4F4 F A3WE E2EA 20030317000612003031700061NM 2003 3 17 03FDEA00196 120030303A5320 STRINGER CLIP BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON STRINGER CLIP, BS 720C STR 26R. REMOVED STRINGER CLIP BS 720C STR 26R, REMOVED CORROSION ON CLIP IN A 1 INCH X 1 INCH AREA. BLENDED 0.020 INCH FROM 0.040 INCH OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPLACEMENT STR CLIP FROM 7075 T6 X 0.040 INCH NR 472905 IAW SRM 51-30-1 AND REINSTALLED AT BS 720C STR 26R IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20030122001192003012200119EU 2003 1 22 HEEA083498 120030107A2432RG390E BATTERY BOLKMS105 BO105S 5626006EU MAIN INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03135AE80 S838 AIRCRAFT WILL NOT START. REPLACED MAIN BATTERY. 1G72 3U H3EU 20030327000052003032700005NM 2003 3 27 AWXA200300268 120030313A335020131A BATTERY BOEING737 7373S3 1384711NM CABIN DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28312AW 24060 UPON ARRIVAL AT AIRCRAFT THE FLIGHT CREW FOUND THE EMERGENCY LIGHTS ON. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS, EMERGENCY LIGHT TEST WAS GOOD. 2L72 4F RTA16WE 20030730001362003073000136SO 2003 7 30 SIMA200313901 120030515A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO E/E BAY FAULTY A SIMAO OTHER N FALSE WARNING DEDESCENT 1 SW21640AE 145183 OKC - FLT 3949 - DURING DESCENT CREW RECEIVED LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCIDENT REPORTED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM. OPERAITONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030731000512003073100051EA 2003 7 31 QXEA200300841 220030720A7200312162701 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA NR 1 FLUCTUATES A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09403QX3784 2763 4037 PCEFA0097 PSC - FLIGHT 2390 ENROUTE SEA-BOI DIVERTED INTO PSC NR 1 ENGINE LOW OIL PRESSURE AND FLUCTUATING. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20030416003172003041600317NM 2003 4 16 AALA20030308 120030225A5315143T5132 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21366AA 25193 AFW - UPPER SURFACE OF FLOORBEAM STATION 764 HAD CORROSION BLENDED BEYOND SRM LIMITS. REMOVED CORROSION PER REF B. VERIFY CORROSION COMPLETELY REMOVED. FABRICATE AND INSTALLED REPAIR STRAP. (M) 2L72 4F RTA1NM 20030418000092003041800009NM 2003 4 18 UPS03440178 120030130A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C M/D, R2 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED AT BS 805 BELOW STR 24. M/D - R2 DOOR FUSELAGE CUTOUT REVEALED PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 805 BELOW STR 24. 2L74 4F RTA20WE 20030417001712003041700171NM 2003 4 17 UPS03240160 120030202A7830 SKIN BOEING727 72725C 138400HNM THURST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, SUSPECT CRACK ON NR 3 ENG TR LWR DOOR INNER UPPER SKIN. NDT PERFORMED AND TWO CRACKS DETECTED AND ENDS MARKED. CRACKED ENDS TERMINATED BY STOP DRILLING WITH .1875 INCH HOLE DIAMETER SRM SUPP 78-30-01 FIG 201 PARA 2. DAMAGED RAMP SKIN REPAIR CARRIED OUT SRM SUPP 78-30-0 1 FIG 201 PARA 3 TO 6. 2L73 4F A3WE 20030417000992003041700099EA 2003 4 17 QXEA0300220 120030202A53209847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09615QX 10065 CENTER CHIMNEY ON FORWARD CARGO BAY IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030421002092003042100209NM 2003 4 21 AMTA200300370 120030217A5330 SKIN BOEING757 75723N 1384973NM FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 FOUND 53 FUSELAGE, 30 PLATE/SKINS, DENT IN SKIN LOWER FUSELAGE STATION 540 AT STRINGER 28 MARKED IN RED. REPAIRED PER SRM 53-00-01-1. SEE ABOVE AND M12A FOR OTHER WORK ACCOMPLISHED. (M) 2L72 4F RTA2NM 20030422001132003042200113SO 2003 4 22 SIMA200305007 120030213A5320 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21639AE 145182 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED BY BLENDING. CUT OUT A 1.062 INCH BY .562 INCH PORTION NEAR THE AFT END. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED TWO DOUBLERS FOR THE REPAIR TO THE CUTOUT AREAS. REPAIR DONE IAW EMB REPAIR STATEMENT 1C2003-145/0562 AND STANDARD SRM, SRM 145/1142 REV 20 PRACTICES. (M) 2L72 4T RTT00011AT 20040329000492004032900049WP 2004 3 29 ASAA0380389 120030421A53409936534327 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND FUSELAGE STATION 200 LBL 8 FITTING CORRODED. REPLACED FITTING PER SRM. (M) 2L72 4F A6WE 20040225001702004022500170NE 2004 2 25 DL777031138 220031226A7261 ENGINE BOEING777 777232 1385232NM RROYCERB211 RB211TRENT76 NE NR 1 LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27863DA5653 29735 051399 EXCESSIVE OIL CONSUMPTION LEFT ENGINE DUE TO REPORT OF LEFT ENGINE HOC AND AT ROLLS ROYCE RECOMMENDATION, REPLACE THE LEFT ENGINE. 2L72 4F4 FRTT00001SEE39NE 20030722000352003072200035NM 2003 7 22 2003F00463 120030123A5260 TORQUE BOX BOEING727 727222 1384073NM AIR STAIR CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 AT C-CHECK, FOUND CRACK ON AIRSTAIR TORQUE BOX, STATION 1263. CUTOUT CRACKED AREA AND INSTALLED DOUBLER. (M) 2L73 4F A3WE 20030722000412003072200041EU 2003 7 22 MALA030327 120030702A5330 SKIN SAAB SF340 340B 7860101EU TAIL CONE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 RIGHT FUSELAGE TAIL CONE UPPER SKIN HAS .070 INCH DENT STA 804.75, 1.5 INCH IN DIAMETER, 12.5 INCHES ABOVE WL113.8. MAINTENANCE REPAIRED DAMAGE DENT IAW EO S53165. REF TO 409 NR 192042 FOR FURTHER DETAIL. A/C RELEASE DATE 7/6/03. 2L72 4T RTA52EU 20030721001322003072100132NM 2003 7 21 SWAA031515 120030708A53106935365 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031202000742003120200074NM 2003 12 2 USAABB03191 120031016A3350412N11681SP LIGHT BOEING757 7572B7 1384964NM ROW 25 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU 27123 FOUND EMERGENCY LIGHT, BULLNOSE, AT ROW 25 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20031202001232003120200123EA 2003 12 2 A6WA200340149 120031020A2711 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM ILLUMINATED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31453AW 7838 ABORTED TAKEOFF AT 49,400 LBS AT 95 KNOTS FOR CONFIG WARNING, BRAKING ACTION MEDIUM. NO BRAKE WARNINGS RECEIVED. COMPLIED WITH RTO INSPECTION IAW 05-51-27. NO DEFECTS NOTED. AILERON TRIM WAS RESET TO ZERO. SHOWED RIGHT WING UP DURING TAKEOFF. (M) 2L72 4F RTA21EA 20031203001332003120300133EU 2003 12 3 A6WA200360048 120031004A5522 SKIN BAG BAE146BAE146200A 1500266EU ELEVATOR DELAMINATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 DENTS LEFT AND RIGHT ELEVATORS MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810004. (M) 2H74 4F RTA49EU 20031204001042003120400104WP 2003 12 4 UPS03841422 120030917A53115613861119 FRAME DOUG DC8 DC873F 302199FWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, COCKPIT UNDER FLOOR AREA STA -117 LT SIDE BOTTOM OF FRAME AT CUSP AREA HAS CORROSION ON DWD AND AFT SIDE OF FRAME. REMOVED KICK PANEL LT COCKPIT FLOOR. REMOVED FRAME, OUT OF LIMITS. REMOVED 2 EA T-ANGLE ATTACH ANGLES. RECEIVED Z-FRAME HT TREATED TO T-6 CONDITION FABBED IAW DAC DWG 5613861. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW Z-FRAME IAW DC8 SRM 51-1-20D & 51-3-0. REINSTALLED KICK PANEL. REMOVED IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040121001012004012100101NM 2004 1 21 03FDEA02326 120031230A5744ARC199113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75201, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040123000442004012300044NE 2004 1 23 MDR03034 120031118A6520643566507101 GEAR SKRSKYS64 S64F 8142610NE PWA JFTD12JFTD12A4A 52047NE T/R GEARBOX CRACKED E JYDRK NONE O OTHER ININSP/MAINT 1 NM09159AC876 A8128 64084 TAIL ROTOR GEARBOX WAS REMOVED FROM AC FOR MAKING METAL. TAIL ROTOR GEARBOX WAS DISASSEMBLED IN THE OVERHAUL SHOP AND VISUALLY FOUND A CRACKED GEAR TOOTH ON THE OUTPUT GEAR. DURING THE MPI INSPECTION, WAS CONFIRMED THE TOOTH WAS CRACKED AND NO OTHER CRACKS WERE FOUND. CRACK IS LOCATED.2500 INCH FROM THE BASE OF THE GEAR TOOTH ON THE DRIVE SIDE OF THE TOOTH AND EXTENDS LENGTH WISE APPROX 2 INCH CURVING UP TO THE TOP OF THE TOOTH, DIVIDING INTO THREE CRACKS ON THE TOP OF THE TOOTH. PROBABLE CAUSE IS UNKNOWN AT THIS TIME. 2G72 4U4 U H6EA E15EA 20040123000692004012300069EA 2004 1 23 WVE2003F00026 120031216A5312MM67036182005 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE AFT CARGO BAY CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09614QX 10049 LT PRESSURE BULKHEAD WEB AT FS1098, BL3441, STR8-9, FOUND TO BE CRACKED. CUT OUT DAMAGED WEB. PERFORMED AN EDDY CURRENT INSPECTION TO ENSURE ALL DAMAGE WAS REMOVED AND NO CRACKS EXIST. NO INDICATIONS FOUND. WET INSTALLED FABRICATED FITTING PN 670-53-61-026-1 AND FASTENERS. RESTORED ELECTRICAL CONTINUITY SURFACE. RESTORED BONDING SURFACE. PRESSURIZATION CHECK GOOD IAW CRJ700 AMM 21-31-00-910-801-A01. ALL WORK PERFORMED IAW MFG REO NR 670-53-61-034, DATED 2003-09-05. (EA09200601238) 2L72 4F4 FRTA21EA E15NE 20031204001312003120400131SO 2003 12 4 C2XA03SH399 120031019A541114576631621 RIB EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 1 NACELLE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 DURING C-CHECK THE NR 1 ENGINE LOWER COWLING AFT RIB WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 54-10-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031204001162003120400116WP 2003 12 4 UPS03841434 120030925A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C3 L1 FWD PASSENGER LWR AFT DOOR JAMB CORNER EXT FUSELAGE SKIN CRACKED AT FASTENER HOLE MARKED. REPAIRED L1 FWD PASSENGER LWR AFT DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 15. 2L74 4F RT4A25 20031210000122003121000012NM 2003 12 10 SWAA032611 120031125A53306552988 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031211000832003121100083NM 2003 12 11 03FDEA01907 120031112A5320 BEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 CORRODED LONGITUDINAL BEAM BS 846, LBL 44, WL 208. 2L73 4F RTA3WE 20030919000632003091900063NM 2003 9 19 0301556717 120030809A2611 TERMINAL BOEING747 747251F 1384898NM NR 4 FIRE LOOP DAMAGED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01617US 21121 DURING CLIMB WITH NR 4 ENGINE FIRE LOOP -A- ON MEL, THE FAULT DETECTION ANNUNCIATOR ILLUMINATED FOR THE NR 4 ENGINE B-FIRE DETECTOR. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. REPLACED TERMINALS FOR (A) AND (B) FIRE LOOPS AND REPLACED THE RIGHT SIDE SEGMENT OF THE UPPER CORE FIRE LOOP. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030922000422003092200042EU 2003 9 22 RAIA00308208 120030804A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAO OTHER L NO TEST NRNOT REPORTED 1 CE03566HK 41084 CABIN EMERGENCY FLOOR STRIP LIGHT INOP. SECURED ELECTRICAL CONNECTOR. 2L72 4T RTA41NM 20030923000972003092300097WP 2003 9 23 DHL2003604601 120030522A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT. WING OB L/E UPPER SKIN CORRODED STA. XFS.710.000 PERFORMED MAJOR REPAIR IAW EODHL-030517, ED-3306. REMOVED FASTENERS AND EXISTING DOUBLER AND FILLER IAW SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM. FOUND OUT OF LIMITS. TRIMMED OUT THE CORRODED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.063) AND TWO FILLERS (7075-T6 AL0.050) IAW EODHL-030517, ED-3306. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLER AND FILLERS ON RT WING OB L/E UPPER SKIN (STA. XFS.710.000) USING NEW FASTENERS. 2L74 4F RT4A25 20040202001362004020200136NM 2004 2 2 UPS04541728 120031231A5347 SEAT TRACK BOEING757 75724APF 1384969NM EXPANSION LINK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE: C, CORROSION ON EXPANSION LINK SEAT TRACK BS 880 - 900 LBL 45 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED LINK, FABRICATED LINK AND INSTALLED REPLACEMENT LINK IAW SRM 53-00-52, SRM 51-10-2 & SRM 51-40-02. 2L72 4F RTA2NM 20030827001642003082700164EU 2003 8 27 MALA030362 120030730A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 DURING 4K INSPECTION IN CWA, UPPER FLANGE ON BOTTOM FUSELAGE FRAME STA 294 HAS CORROSION RBL 30.5 MAINTENANCE REPAIRED DAMAGE IAW EO NR $53108. REFER TO 409 NR 192516 FOR DETAIL. A/C RELEASE DATE 7/31/03. 2L72 4T RTA52EU 20030829000152003082900015NM 2003 8 29 CALA0300480 120030822A5514 BUSHING BOEING737 737524 1384721NM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714645 28906 INSPECTION FOUND LT HORIZONTAL STABILIZER CENTER FORWARD SPAR LOWER AFT LUG PITTED AT BUSHING. A NEW BUSHING WAS INSTALLED IAW CMM 55-10-06. 2L72 4F RTA16WE 20030828000592003082800059NM 2003 8 28 P5CA0300920 120030819A5753 PANEL BOEING747 747200 1384847NM T/E FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23524UP 21446 LT INBND MID FLAP DELAMINATION AT MID UPPER FLT PNL. CORRECTIVE ACTION TAKEN: DELAMINATION PNL - REPLACED- SRM 51-30-02 2L74 4F RTA20WE 20030721001392003072100139NM 2003 7 21 SWAA031452 120030630A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOORS AND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHTS HAVE SEVERAL LAMPS INOP. RELAMPED EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20030723001262003072300126EU 2003 7 23 AWXA200300623 120030501A5320D53231388200 ANGLE AIRBUS320 A320231 3930325EU DOOR CUTOUT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SPLICE ANGLE AT AFT LOWER CORNER OF THE FORWARD CARGO DOOR CUTOUT, FR-28. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SPLICE ANGLE AT AFT LOWER CORNER OF THE FORWARD CARGO DOOR CUTOUT, FR-28; FABRICATED A NEW REPLACEMENT SPLICE ANGLE PER DWG C2D53231388; INSTALLED REPAIR PART IAW AWA ER 26-5323-03141-SS2. 2L72 4F RTA28NM 20030729000202003072900020EA 2003 7 29 03195428A 120030714A21505729C000003 A/C PACK CNDAIRCL600 CL6002B19 1900309EA A/C BAY MALFUNCTIONED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27428FJ 3193 DURING CRUISE, THE CREW REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO RIC, LANDED UNEVENTFULLY, AND DEPLANED NORMALLY. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT ENVIRONMENTAL CONTROL UNIT (A/C PACK). AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030807000842003080700084NM 2003 8 7 03219406 120030807A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27406FJ 3156 DURING MAINTENANCE INSPECTION THE NR 7 EMERGENCY BATTERY WAS DISCOVERED INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20030806000092003080600009SW 2003 8 6 ALGA088116 120030716A6220406310405101 LINK BELL 407 407 1182206SW PITCH CONTROL WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03405AL798 53480 PITCH CONTROL LINK WORN AND RATCHETY. REPLACED IN FIELD. 1G71 3U O H2SW 20030807000542003080700054EA 2003 8 7 03210636 120030729A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27636BR 7307 DURING INSPECTION THE CREW REPORTED THE 2 EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED 2 RT EXTERNAL EMERGENCY LAMPS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FROM CONTINUED SERVICE. 2L72 4F RTA21EA 20030903000352003090300035NM 2003 9 3 DHL2003726010 120030715A5610 LATCH BOEING727 727228 1384083NM COCKPIT WINDOW LACK OF LUBE A DHLAO OTHER O OTHER LDLANDING 1 SO01726DH 20409 DURING LANDING ROLL OUT, CAPTAIN'S SLIDING WINDOW CAME UNSEATED LOST PROPER SEAL. FOUND WINDOW HANDLE LOCKING MECHANISM STICKING. LUBED HANDLE. OPS CHECKED GOOD IAW M/M 12-25-71. 2L73 4F RTA3WE 20030903001102003090300110WP 2003 9 3 2003F00537 120030403A5330 SKIN DOUG DC9 DC987 3022087WP FUSELAGE DENTED A WXOAK NONE O OTHER ININSP/MAINT 1 WP17948MA 49778 FOUND DENT IN FUSELAGE SKIN FS 240 LEFT FUSELAGE AT L17L. CUT OUT DENT. FABRICATED AND INSTALLED DOUBLER IAW DC9/MD-80 SRM 53-04-0, 51-30-2, 51-10-3 AND 53-04 FIG 38. (M) 2L72 4F RTA6WE 20030904001922003090400192WP 2003 9 4 AALA20030674 120030618A2120 CLAMP DOUG DC9 DC982 3022082WP A/C BAY LOOSE A AALABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 SW2116545 53027 DFW - FLT 1347 - EN ROUTE STL-MSY, AT LEVEL OFF ALTITUDE 33,000 FEET, PRESSURIZATION FLOW LIGHT ILLUMINATED WITH RATE OF CLIMB AT MAXIMUM INDICATION. BOTH PACKS WERE IN AUTO WITH BOTH FLOW INDICATION AT LOW. INITIATED RAPID DESCENT AND DEPLOYED OXYGEN MASKS. NOTICED OUTLFOW VALVE WAS AT FULL CLOSED. WHEN AT LOWER ALTITUDE CABIN WAS STILL NOT PRESSURIZING, BUT RIGHT PACK FLOW INDICATION WAS AT 1:00 O'CLOCK POSITION AND LEFT FLOW CONTROL POSITION AS STILL AS LOW. TIGHTENDED CLAMP ON DUCT TO RIGHT TEMP CONTROL VALVE CLAMP. REPLACED OXYGEN GENERATORS IN CABIN/COCKPIT/LAVATORIES AND STOWED MASKS. REPLACED WATER COALESCER SEPARATOR BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030903002522003090300252SO 2003 9 3 C2XA03SH308 120030829A532014521275001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE LEFT HAND SILL BETWEEN FR 18-20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND SILL BETWEEN FR 18-20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030821000652003082100065NM 2003 8 21 03FDEA00926 120030617A5753ARC2512204 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING- I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE FOUND CORROSION. RIGHT WING- I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69374, TITLE: WINGS- TRAILING EDGE FLAP- INBOARD TRAILING EDGE FLAP- OUTBOARD SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030730001162003073000116WP 2003 7 30 03FDEA01146 120030725A5347FX6010964 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 MAIN CARGO DECK SEAT TRACK LBL 48 STA 1129 TO 1219 HAS 3EA GOUGED AREAS. CLOSING ACTION ON 07/20/03, REMOVED AND REPLACED SEAT TRACK 53-70-00. PARTS FAB ON TRAVELERS 348514,T2/348516,T2/348515. 2L73 4F A22WE 20030916000512003091600051CE 2003 9 16 52776AMWA1 120030720A243051538001A GENERATOR BEECH 1900 1900D 1154162CE DC SYSTEM FAILED A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07237YV2292722927 UE237 ON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RT GENERATOR WOULD NOT STAY ONLINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. MAINTENANCE REMOVED AND REPLACED GENERATOR, GCU AND REPAIRED A WIRE ON THE GENERATOR. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DATE. REFER TO SDR 52776. 2L72 4T RTA24CE 20030826001062003082600106CE 2003 8 26 06092003 120030609A3230MS24171D1 RELAY BEECH 1900 1900C 1154161CE LANDING GEAR FAILED E YADAK NONE J WARNING INDICATION APAPPROACH 1 AL03112AX218 UC45 LANDING GEAR FAILED TO EXTEND USING GEAR SELECTOR - HAND PUMPED GEAR DOWN. 2L72 4T RTA24CE 20030929001222003092900122NM 2003 9 29 HNAA0300045 120030908A53308553007 SKIN DHAV DHC8 DHC8102 2809003NM ZONE 200 DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07906HA4876848768 9 AIRCRAFT SUSTAINED DAMAGE FROM GROUND EQUIPMENT CAUSING MAJOR REPAIR. 2H72 4T RTA13NM 20030926001442003092600144NM 2003 9 26 AWXA200301005 120030830A2930350E550020 CONTROL UNIT AIRBUSA319 A319132 3930340NM ZONE 120 FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28829AW7303 1563 ON CLIMB OUT EN ROUTE, PRIOR TO FLAP RETRACTION, RECD ECAM WARNING FOR GREEN HYD SYS FAILURE IND LOW GREEN PRESS AND QTY. FOLLOWED ECAM PROCED AND TURNED OFF NR 1 ENG DRIVEN HYD PUMP (EDP), PWR TRANS UNIT (PTU), TURNED EDP BACK ON AND PRESS RETURNED TO NML, TURNED ON PTU AND ECAM WARNING FOR GREEN HYD SYS FAILURE REAPPEARED. RE-ACCOMPLISHED PROCEDURES, TURNED EDP BACK ON. MAINT TROUBLESHOT, OPERATIONAL TEST OF GREEN HYD SYS WAS GOOD. RAN ENG AND OPERATED THE PTU, PTU WAS GOOD IN BOTH DIRECTIONS, ALL PRESS AND QTY INDICATED NORMAL. AS PRECAUTION REMOVED AND REPLACED SIGNAL DATA ACQUISITION UNIT (SDAC), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030930000562003093000056SO 2003 9 30 WVBA2003003 120030820A3232AN8374D FITTING PIPER PA31 PA31350 7103110SO ACTUATOR CRACKED E WVBAO OTHER O OTHER NRNOT REPORTED 1 AL01300ED 317852008 LANDING GEAR WOULD NOT EXTEND WITH GEAR HANDLE. GEAR LOWERED AND LOCKED WITH EMERGENCY PUMP HANDLE. UPON EXAMINATION FOUND LOWER FITTING ON LEFT INNER GEAR DOOR ACTUATOR CRACKED AND HOSE CHAFED TO BOTTOM FITTING. THE PROBLEM SEEMED TO COME FROM A ACTUATOR HOSE THAT WAS SLIGHTLY TO LONG AND TIRE THAT HAS A LARGER DIAMETER THAN THE TIRES NORMALLY USED. WE ARE CYCLING THE LARGER TIRES OUT OF OUR SYSTEM. AIRCRAFT REPAIRED AND RETURNED TO SERVICE. 1L72 3O A20SO 20031001000562003100100056NM 2003 10 1 03256413 120030913A2424 WIRE DORNERDO32 DO328300 NM MAIN ELECTRICAL LOOSE A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA27413FJ 3167 FLIGHT CREW REPORTED VISABLE WHITE SMOKE IN CABIN AND LT PACK FAIL MESSAGE. MAINTENANCE PERSONNEL DETERMINED SMOKE TO BE RESULT OF MAIN ELECTRICAL BUS BEING UNTIED WHICH RESULS IN FANS BEING INOPERATIVE. MAINTENANCE PERSONNEL RETIED MAIN BUS AND PERFORMED SATISFACTORY OPERATIONAL CHECK AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20031002000912003100200091NM 2003 10 2 C1HA200386007 120030908A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 BS 480 LBL 25 SEAT TRACK HAS CORROSION AROUND FASTENER. 2L73 4F A3WE 20031002001492003100200149NM 2003 10 2 03FDEA01468 120030909A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 MAIN CARGO DOOR STUB FRAME IS CRACKED AT O/B FLANGE THRU FASTENER HOLE, 69 INCHES AFT OF FWD FRAME 3 INCHES BELOW UPR FRAME. REPLACED PER SRM 51-30-2. 2L73 4F RTA3WE 20031014000752003101400075 2003 10 14 SWAA032199 420031003A2565 INDICATOR BOEING737 7373A4 1384585NM ESCAPE SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 2174 23253 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20031021001512003102100151NM 2003 10 21 AALA20030950 120030903A3350P4010051112 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21647AM 24605 JFK - FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 16 THROUGH 24. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031027000152003102700015EA 2003 10 27 WVE2003F00013 120030907A5320S399LT ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CORRODED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09620BR 7179 (ANGLE) AREA IS PRONE TO CORRODION DUE TO EXPOSURE TO WEATHER. CORROSION IN THIS AREA IS FAIRLY COMMON ON HIGH TIME AIRCRAFT. 2L72 4F4 FRTA21EA E15NE 20031027000942003102700094NM 2003 10 27 ASAA02402BB 120030330A51006573783 SKIN BOEING737 7374Q8 138447QNM HORIZONTAL STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 DURING C-CHECK, FOUND LEFT HORIZONTAL STAB LE HAS DENT AT 91 IN OUTBOARD FROM REMOVEABLE LE SKIN INBOARD END. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031118000612003111800061EU 2003 11 18 AWXA200301176 120031004A3510G2N21229 CONTAINER AIRBUS320 A320232 3930326EU EMERGENCY EQUIP FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK THE R-2 DOOR EMERGENCY OXYGEN DOOR FAILED TO DEPLOY ON MASK DROP TEST. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR EMERGENCY OXYGEN CONTAINER IAW AMM 35-21-41-020-051, AND 35-21-41-420-051, OPS CHECKED GOOD IAW AMM 35-23-00-710-050-A. 2L72 4F RTA28NM 20031118000862003111800086NM 2003 11 18 C1HA200394019 120031009A3350 POWER SUPPLY BOEING727 727290 138408WNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15249AS 22146 EMERGENCY EXIT AISLE LIGHT BETWEEN L2 AND R2 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW CHAMPION AMM 33-51-00; OPS CHECK GOOD. 2L73 4F A3WE 20031120000732003112000073NM 2003 11 20 QXEA200301261 120030928A5340 CLIP DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 FRAME CLIP IS DAMAGED INBOARD END BEHIND NR 1 SEAT TRACK AT FRAME 312.350 FORWARD SIDE. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040204000742004020400074NM 2004 2 4 PCAA0310124 120031017A33506013211 POWER SUPPLY DHAV DHC8 DHC8* NM EMERGENCY LIGHT INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13824EX2323623236 387 WHILE IN ROUTINE MAINTENANCE IN MIDDLETOWN, PA. DURING OPERATIONAL TEST, MAINTENANCE FOUND ROW 4AC EMERGENCY LIGHT DIM, TWO AISLE LIGHTS DIM AND LEFT AFT FUSELAGE LIGHT DIM. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031029001342003102900134EU 2003 10 29 KBM2003F00029 120030830A21500600018 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE AIR CONDITIONER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 A/C DOES NOT BLOW COLD AIR. REPLACED A/C BELT WITH NEW. 1G71 3U3 UNCH9EU E19EU 20031117000382003111700038SO 2003 11 17 C2XA03SH373 120031007A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 DURING C-CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031119001262003111900126NM 2003 11 19 2003UALA00756 120031007A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29536UA 25156 INBD CAP OF FRAME AT STA 1681 WL 209 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REPAIR IAW EVA MOCI-8433A. 2L72 4F4 FRTA2NM E17NE 20031119001122003111900112EU 2003 11 19 2003UALA00740 120031003A5522 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT ELEVATOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29402UA 439 WATER INGRESS WAS FOUND AT 2 LOCATIONS ON THE RT ELEVATOR. DAMAGE ON UPPER SKIN IS 2.8 BY 2 INCHES AND IS 127 INCHES FROM IB EDGE AND 20 FROM TRAILING EDGE. MAJOR REPAIR ACCOMPLISHED. REPAIR DAMAGED AREAS PER SRM 55-21-11 TO ELIMINATE WATER INGRESSION. 2L72 4F4 FRTA28NM E40NE 20031106002122003110600212NM 2003 11 6 ASAA0340312 120030707A33978100022605 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 14-17 INOPERATIVE. RECONNECTED WIRES. OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20031105000102003110500010NM 2003 11 5 03FDEA01842 120031031A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25270FE 22035 CORROSION (C53-111-01, 2) FWD CARGO COMPARTMENT AFT SIDE OF BS 720A FRAME RBL 9 WL 148. INVESTIGATED & REMOVED CORROSION 2 X3 X .007 ON FRAME, 1 X 3 X .009 ON SHEAR TIE. BOTH ORIGINAL THICKNESS AT BS 720A, RBL 9, WL 148; BOTH ARE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1, DETAIL 1, FABRICATED, ALODINED, PRIMED & PAINTED REPAIR SHEAR TIE. USED 7075T6 .063 IAW SRM 53-10-4 FIG 15, SHT 1. REMOVED DAMAGE & INSTALLED FABRICATED SHEAR TIE AT BS 720A, RBL 9, WL 148 IAW 727 SRM 53-10-4, FIG 15 SHT 1. 2L73 4F RTA3WE 20031112000222003111200022SO 2003 11 12 C2XA03SH444 120031112A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV-DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040109000312004010900031NE 2004 1 9 MEX2003467 220031006A7200JT8D ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE NR 1 DAMAGED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23751RA33062 49779 AIRCRAFT ARRIVED WITH ONE BLADE OF LEFT ENGINE C1 DISK WITH DAMAGES OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE LEFT ENGINE WAS REPLACED IAW MM 71-00-00, TESTS CORRECT.(K) 2L72 4F4 FRTA6WE E2EA 20040113001232004011300123EU 2004 1 13 YENA200343 120031224A5270DHE1141 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU CABIN DOOR INTERMITTENT A YENAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15581JB131 2141 ON TAKEOFF CONTINUOUS INTERMITTENT ECAM RIGHT AFT CABIN DOOR UNLOCK INDICATIONS ONLY STOPPED WITH EMER CNX. CABIN CREW HAD CIDS CAUTION DOOR UNLOCK INDICATIONS AND CABIN DOOR WITH CABIN LIGHTS FLICKERING. REMOVED & REPLACED PROXIMITY SWITCH 17WV2 PER AMM 52-71-11. CLEANED CONNECTOR, OPS CHECK OK. 2L72 4F RTA28NM 20040112000992004011200099WP 2004 1 12 GTIA031012 120031124A5340 FITTING DOUG DC9 DC981 3022081WP NGL WW CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FOUND NLG W/W STATION 69.5 LEFT SIDE UPPER OUTBOARD TEE FITTING CRACKED LBL 16 INCHES. REMOVED DAMAGED FITTING. INSTALL NEW TEE FITTING. (M) 2L72 4F A6WE 20040112001722004011200172WP 2004 1 12 GTIA031026 120031123A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND CABIN LEFT, INBOARD, FLOOR PANEL 200-256 SEVERAL CORRODED INSERTS, CRACKS/DELAMINATED AT CORNERS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20031120001172003112000117NM 2003 11 20 SWAA032455 120031106A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND CORROSION ON LT AND RT HORIZ STAB CTR CENTER SECTION FWD AND AFT LUG FACES AND BORE. REMOVED CORROSION PER SRM. 2L72 4F RTA16WE 20040112002452004011200245WP 2004 1 12 AALA20031484 120031230A213320219742 ACTUATOR DOUG DC9 DC982 3022082WP CABIN PRESSURE FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21578AA 53155 TPA T1709/30 AIRCRAFT WOULD NOT PRESSURIZE. REPLACED CABIN PRESSURE OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040114000882004011400088NM 2004 1 14 DL757031030 120031105A5210BACB10B79LT BEARING BOEING757 757232 1384965NM L2 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 NR 264 HMV3 L2 ENTRY DOOR INSPECTION OPN 5836 CP53-231-01I. ROLLER CORRODED EPAS HAMMER ROLLER CORRODED 2L. REMOVED EPAS ROLLER AT L2 DOOR, NO FURTHER CORROSION FOUND. OK TO INSTALL L2 DOOR. INSTALLED EPAS ROLLER AT L2 DOOR POSITION. OPN OF EPAS SYSTEM TO BE CW ON DOOR INSTALLATION. THIS BEARING WORKS WITH THE TRIGGER MECHANISM ON THE UPPER GUIDE ARM OF THE DOOR TO SET OFF THE EPAS BOTTLE WHEN THE SLIDE ID DEPLOYED. IPC 52-11-01-24 ITEM 270. 2L72 4F RTA2NM 20040115000242004011500024NM 2004 1 15 03FDEA02039 120031203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25276FE 22041 CRACKED FRAME AT BS 640, RBL 9, WL 155.5. CUT OUT CRACK ON FRAME AT BS 640, RBL 9, WL 155.5. REMOVED 2X2 INCH. FABRICATED REPAIR PARTS FROM 7075-T6 .063 INCH, LOT 516678. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30- 2, 53-10-1, 51-40-3. (CLOSED) 2L73 4F RTA3WE 20031217002132003121700213EA 2003 12 17 SWIA200312620 120031124A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R31113-58. 2L72 4F RTA21EA 20031222000402003122200040NM 2003 12 22 F3LA200300165 120031205A5320 SILL BOEING737 73736E 138443ANM FUSLEAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON L-1 MOP SILL, STA 312-344. REPLACED L-1 MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20031223000062003122300006NM 2003 12 23 AWXA200301524 120031207A534065468823 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER CLIP AT BS 360, STR 14 RT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 360, STR 14 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-46882; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20031223001842003122300184WP 2003 12 23 GTIA030829 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200-205, 21 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW CABIN FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20031229000362003122900036SO 2003 12 29 LR7A03100 120031121A53103314718 BEAM LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND LT MLG FS 517 VERTICAL BEAM CORRODED AT TRACK ATTACHMENT, LBL 60, WL 151 & 185. REPAIRED IAW LAC MEA 382-25-03-074 R1. NR 2225. 2H74 4T A1SO 20031229000892003122900089NM 2003 12 29 03FDEA02200 120031213A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN CARGO DECK RT STA 455 TO STA 515 SEAT TRACK AT X=27.5 RT SEAT TRACK HAS HEAVY CORROSION. REMOVED AS PER SRM 53-70-00 FIG. 1 VOL. I AND INSTALLED NEW SEAT TRACK AT MAIN DECK CARGO RT STA 455 TO 525 AS PER SRM 53-70-00 FIG. 1 VOL I. 2L73 4F RTA22WE 20031010000242003101000024NM 2003 10 10 USAABB03164 120030911A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 17 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031010000602003101000060NM 2003 10 10 CALA0300535 120030918A5347 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND IMPACT DAMAGE TO AFT BAGGAGE BIN LT TIE DOWN RAIL AT BS 787. REPLACED TIE DOWN RAIL IAW SRM 53-00-53. 2L72 4F RTA16WE 20031126000792003112600079SO 2003 11 26 C2XA03SH411 120031024A711014576094604 LONGERON EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714542 145547 SHV- DURING C-CHECK THE RT LOWER COWLING OUTBOARD LONGERON WAS FOUND TO BE CHAFED APPROXIMATELY 7 INCHES FORWARD OF AFT END. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031202000882003120200088NM 2003 12 2 USAA030212 120031008A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19504AU49469 23379 FOUND SKIN CRACKED 1.5 INCH, LEFT AFT FUSELAGE 3 INCHES FORWARD OF BS FRAME 747 S21-L. DOUBLER AND TRIPLER INSTALLED PER SRM 53-00-01 FIG 229 AND DETAIL VII. (M) 2L72 4F RTA16WE 20031203001362003120300136EU 2003 12 3 A6WA200360053 120031007A5320 PAN BAG BAE146BAE146200A 1500266EU CARGO DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 AFT BAGGAGE DOOR INTERFACE DAMAGE TO THE FORWAD EDGE OF THE AFT BAGGAGE DOOR PAN, LOCATED NEXT TO THE LOWE SHOOT BOLT GUIDE. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810009. (M) 2H74 4F RTA49EU 20031209000452003120900045NM 2003 12 9 P5CA0300973 120031028A5753 SUPPORT ANGLE BOEING747 747283B 1384867NM RT TE FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RIGHT I/B MID FLAP O/B L-SUPPORT ANGLE CRACKED 5 INCHES. REPAIR CARRIED OUT IAW SRM 51-40-03. 2L74 4F A20WE 20031209000822003120900082NM 2003 12 9 SWAA032348 120031024A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, ABOVE STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031014000702003101400070NM 2003 10 14 SWAA032204 120031003A57536546430129 SKIN BOEING737 7373Y0 1384671NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED C4 CHECK, FOUND LT INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20040204000632004020400063NM 2004 2 4 DHL2003745022 120031018A3260 CONNECTOR BOEING727 727224 1384076NM PWA JT8 JT8D* NE RT MLG DOOR LOOSE A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 GEAR DOOR LIGHT ON PILOT'S PANEL AND RT GEAR DOOR LIGHT ON S/O'S PANEL ILLUMINATED WHEN GEAR LEVER MOVED TO OFF. PERFORMED ABNORMAL PROCEDURE AND LIGHTS EXTINGUISHED. FOUND CONNECTOR LOOSE ON RIGHT MAIN LANDING GEAR DOOR WARNING SWITCH. CLEANED AND RESECURED CONNECTOR. PERFORMED ADJMENT / TEST IAW B-727 M/M 32-62-11. OPS CHECKED NORMAL. 2L73 4F4 F A3WE E2EA 20040205000262004020500026NM 2004 2 5 EIA2003163 120031020A5320 CLIP BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 STIFFENER CLIP FOR DIAGONAL BRACE CRACKED AT FS 380 LBL 10 WL 160 IN LEFT NOSE TUNNEL. REMOVED DAMAGED STIFFENER, FABBED NEW AND INSTALLED IAW SRM 51-10-01, 51-10-02, 51-30-05 AND 51-30-02. 2L74 4F A20WE 20040205001152004020500115EA 2004 2 5 A6WA200340167 120031111A5720 BEAM CNDAIRCL600 CL6002B19 1900309EA LT WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31401AW 7280 LT OB FLAP HAS THE OB HING BEAM DAMAGED BY A SCREW BETWEEN THE HINGE AND THE FITTING. CLEANED DAMAGED AREA, BLENDED SMOOTH, PERFORMED ROTO/FLAP PEEN OF REPAIR AREA, ALODINED AND TREATED IAW ORIGINAL CONFIGURATION IAW WVAC EO 601R-57-4391. 2L72 4F RTA21EA 20040206000782004020600078WP 2004 2 6 DHL2004806506 120031228A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 4 FLOOR TRACK PLUG WITH LUGS WORN STA 275.000. REMOVED PLUG WITH LUGS WORN IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 4 FLOOR TRACK IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040213000302004021300030EU 2004 2 13 365031 120031230A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A NSVAK NONE L NO TEST ININSP/MAINT 1 EA27277MJ 340B277 EMERGENCY LIGHTS INOPERATIVE ON SEATS 2 AND 3, REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IN AISLE SEAT 3A PERFORMED OPS CHECK IAW MM CHECKED GOOD, REMOVED AND REPLACED POWER SUPPLY. 2L72 4T RTA52EU 20031210000312003121000031NM 2003 12 10 MWEA030463 120031203A5320993653415 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 REMOVED J-CHANNEL FLOOR SUPPORT AT FRAME STATION 200. FABRICATED AND INSTALLED J-CHANNEL. 2L72 4F RTA6WE 20040316001002004031600100WP 2004 3 16 ASAA0380301 120030408A53205936597535 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 1117 AT FASTENER HOLES. REPLACED SUPPORT PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20031215001912003121500191WP 2003 12 15 AALA20031207 120031102A3350AAP3274A CHARGER DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21964TW 53614 DFW - DURING OVERNIGHT MAINTENANCE, FOUND AFT RIGHT AND LEFT SIDE OVERWING DOOR EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031217000222003121700022EA 2003 12 17 COMA0360506 120031118A2720601R512261 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO01920CA 7022 FLT 5826 RUDDER CONFIGURATION WARNING DURING T/O. REPLACED THE RUDDER TRIM PANEL. 2L72 4F RTA21EA 20040614001872004061400187NM 2004 6 14 RYN2004F00012 120030908A5230MS2000116 HINGE BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE CARGO DOOR CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE078878Z 21451 AT (B) CHECK FOUND. MAIN CARGO DOOR AFT HINGE WITH 2 CRACKED LOBES ON THE AFT PART OF THE AIRFRAME HINGE. DRILLED, TREATED, PRIMED AND INSTALLED NEW HINGE SECTION ON MAIN CARGO DOOR. 2L73 4F4 F A3WE E2EA 20030923001802003092300180 2003 9 23 AALA20030839 420030806A3417C17001CA01 MODULE BOEING737 737823 13844BZNM E/E COMPT FAILED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21962AN 30858 AIRCRAFT EXPERIENCED LOSS OF CAPTAINS AIR DATA INSTRUMENTS. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S PITOT AIR DATA MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030924000692003092400069EU 2003 9 24 197051603 120030516A28209630426713 CHECK VALVE PILATSPC12 PC1245 7090551EU FUEL SYSTEM FAILED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07613NA3779 197 FUEL TRANSFERS FROM RT TO LT WING WHILE AIRCRAFT IS NOT IN USE. 1L71 3T RTA78EU 20050103000622005010300062SO 2005 1 3 C2XA03IA999 120030226A33507287103507 CONTROL MODULE EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714902 145496 IAH - DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT NOT ARMED CAUTION, AND EXIT LIGHTS CAME ON EVERY TWO (2) MINUTES FOLLOWING RESET FROM OFF TO ARMED. IAH - MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE. PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041108001192004110800119CE 2004 11 8 DJFA200300006 120031204A3244220K281 TIRE CESSNA500 560CESSNA 2076750CE MLG FAILED E DJFAO OTHER O OTHER LDLANDING 1 EA23501CW247 5600050 DURING LANDING AIRCRAFT PULLED TO THE LEFT. AFTER THE AIRCRAFT SLOWED THERE DIRECTIONAL CONTROL WAS LOST AND THE AIRCRAFT WENT OFF THE LEFT SIDE OF THE RUNWAY DUE TO THE LEFT TIRE BEING FLAT. 2L72 4F RTA22CE 20030815000492003081500049SW 2003 8 15 HEEA088557 120030801A2911212076007003 ACCUMULATOR BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 HYD SYSTEM ACCUMULATOR LEAKING FLUID. SHOP REPAIR. 1G72 4U H4SW 20030815000522003081500052SW 2003 8 15 HEEA088496 120030706A282023001986 TUBE BELL 206 206L3 1182108SW FUEL SYSTEM CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 FUEL TUBE CHAFED. SCRAPPED. 1G71 3U H2SW 20030819002012003081900201NM 2003 8 19 SWAA031778 120030809A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 727A, STR 19L AND STR 25L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030819000952003081900095WP 2003 8 19 UPS03841046 120030708A53476015176 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, CABIN FLOOR TRACK -F- HAS WORN SCALLOPS FROM STA 740-770. REMOVED DAMAGED SEAT TRACK AND SPLICED NEW SEAT TRACK AND ADDED 2 SPLICE CHANNELS IAW UPS EO DC8-5320-5167. FABRICATED, LOCATED AND DRILLED HOLES IAW UPS EO DC8-5320-5167 AND DWG DC8-53B-003. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21D AND 51-3-0. 2L74 4F RT4A25 20030820001052003082000105WP 2003 8 20 UPS03840852 120030618A2910171K0066CR0301 LINE DOUG DC8 DC871F 302199DWP RT MLG RUPTURED A IPXAH DEACTIVATE SYST/CIRCUITS KG FLUID LOSS MULTIPLE FAILURE LDLANDING 1 SO01701UP 45938 AFTER LANDING LOST ALL HYDRAULIC PRESSURE AND QUANTITY. AIR BRAKE USED TO STOP AIRCRAFT. FOUND RT MLG BOGIE TRIM CYLINDER PRESSURE LINE RUPTURED, REPLACED SAME. SERVICED RESERVOIR, BLED HYDRAULIC PUMPS, OPERATED ALL HYDRAULIC POWERED SYTEMS TO REMOVE AIR FROM SYSTEM. CHECKED CASE DRAIN FILTERS AS A PRECAUTION. NO METAL FOUND. 2L74 4F RT4A25 20030822000622003082200062NM 2003 8 22 03FDEA01180 120030731A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 NOSE WHEEL WELL SKIN GOUGED AROUND PANEL OPENING NR 3124, BS 247. 2L73 4F RTA3WE 20030401000072003040100007EA 2003 4 1 03089664 120030330A33502013BR BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27664BR 7528 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE #2 EMERGENCY BATTERY PACK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030404001212003040400121WP 2003 4 4 ASAA0380108 120030125A33501001191 BATTERY DOUG DC9 DC983 3022083WP FWD CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01972AS 53448 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN FIRST CLASS WAS FOUND INOPERATIVE. REPLACED BATTERY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030407001052003040700105NM 2003 4 7 UIEA200300009 120030224A541465B9124138 SKIN BOEING747 747243B 1384830NM NR 3 NACELLE DELAMINATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15540MC87875 22508 DURING CURRENT C-CHECK AT SIAEC, FOUND NR 3 ENGINE LEFT FAN COWL DELAMINTED APPROXIMATELY 8 INCHES BY 8 INCHES IN GENERAL REWORK AREA NOTED BY SB 78-2150 DURING TRAS LOCK MODIFICATION. THE OUTER DELAMINTED SKIN AND FILLER WERE STAGGER CUT TO REMOVE DELAMINATED AREA. PERFORMED HFEC OF SKIN CUT EDGES. NO CRACKING DETECTED. FABRICATED REPLACEMENT STAGGERED FILLER AND TWO ADDITIONAL STAGGERED REPAIR DOUBLERS WITH A 3 INCH AND 1.5 INCH OVERLAP. A STRUCTURAL HOT BOND METHOD WAS USED TO INSTALL REPAIR DOUBLERS AND FILLERS IAW SRM 51-40-06 PAR 3K. PART NUMBER BECAME 673U0032-39 AFTER MODIFICATION FROM 65B91241-38. (M) 2L74 4F A20WE 20030408000332003040800033EA 2003 4 8 SIMA200302903 120030127A79314120T16P01 TRANSMITTER CNDAIRCL600 CL6002C10 1390015EA LT ENG OIL PRESSINOPERATIVE A SIMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21503AE 10021 DFW - FLT 3811 - DURING FLIGHT, CREW REPORTED THE NR 1 OIL PRESSURE IN THE RED. CREW FOLLOWED AOM PROCEDURES AND SHUT DOWN THE ENGINE. AIRCRAFT WAS RETURNED TO DFW AND AN EMERGENCY WAS DECLARED UPON LANDING. NO FURTHER INCIDENTS WERE DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT OIL PERSSURE TRANSMITTER IAW CRJ MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20030408001312003040800131NM 2003 4 8 AWXA200300337 120030406A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM ZONE 242 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28801AW16488 889 PHX - EEL - RT EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN ARMED AND POWER INTERRUPTION OCCURS. MAINTENANCE REMOVED AND REPLACED RT MID CABIN EMERGENCY POWER SUPPLY UNIT (12WL) AND EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030410001822003041000182CE 2003 4 10 FFS2003F00017 120030211A52601144000271 SKIN BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA AIRSTAIR DOOR CORRODED A FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575P 21680 UC95 EXTERIOR SKIN OF AIRSTAIR DOOR SHOWED CORROSION BLISTERS UNDER PAINT. COIN TAP INSPECTION REVEALED AREAS OF DISBOND FROM HONEYCOMB CORE. INTERNAL INVESTIGATION FOUND MISSING, CORRODED PATCHES OF HONEYCOMB APPARENTLY CAUSED BY MOISTURE INTRUSION THROUGH THE HOLES IN THE INNER SKIN FOR THE FASTENERS OF THE INNER DOOR TRIM. THE INNER TRIM WAS ORIGINALLY FASTENED WITH SCREWS INTO RUBBER EXPANDING WELLNUTS. THE WELLNUTS HAD BEEN REPLACED WITH RIVNUTS AND NUT PLATES, WHICH MAY NOT HAVE PROVIDED THE SEAL TO PREVENT THE WATER INTRUSION. THE AREA IS SUBJECT TO WATER, SNOW AND CONTAMINATION FALLING FROM PASSENGERS FT WHEN BOARDING UP THE AIRSTAIR. 2L72 4T4 TRTA24CE E4EA 20030414001272003041400127CE 2003 4 14 CA030311001 120030310A57536525115 RIB CESSNA 652500021 CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE TE FLAP WORN W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING A PHASE 5 INSPECTION THE FLAP RIB EXTENSIONS WERE FOUND WORN BY THE RIVETS SECURING THE FLAP TRACKS TO THE WING TRAILING EDGE. DAMAGE WAS DOCUMENTED AND REPAIRED AS PER IN HOUSE SB.THE RT INBOARD CENTER HINGE WAS REPLACED. 1L72 4F4 F A22CE E1NE 20030416003352003041600335NM 2003 4 16 UPS03440045 120030103A5311 FRAME BOEING747 747259B 1384804NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01527UP 21730 INSPECTION TYPE:C, RIGHT BS 1480 BULKHEAD NR 11 HOLE FOUND CRACK AT BULKHEAD FRAME RUNNING FWD AND AFT APPROX .0625 INCH AND THROUGH THICKNESS RESPECTIVELY. CRACKED FASTENER HOLE REWORKED AS PER RS NR R534334957 DUE TO DIMENSION OF HOLE EXCEEDED S/B REPAIR LIMIT. 2L74 4F RTA20WE 20030416003382003041600338WP 2003 4 16 UPS03840036 120030103A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE: C2, RADIOGRAPHIC (X-RAY) INSPECTION DETECTED 4 CRACKS ON THE R-2 DOOR UPPER AFT CORNER APPROX .406, 1.11, 1.64, 1.74 INCHES IN LENGTH, AT STA 1660 LONG 10R APPROX. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 16. 2L74 4F RT4A25 20030428000462003042800046 2003 4 28 LR7A03038 420030403A34440131909010 ANTENNA LKHEED382 382G 526414USO GROUND PROX SHORTED A LR7AAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03401LC 531 4606 DURING FLIGHT, CREW REPORTED TCAS FAILED, FOLLOWED SHORTLY BY GPWS AND RADIO ALTIMETER FAILURE. SMOKE AND FUMES NOTED IN COCKPIT. DEACTIVATED TRANSPONDER, GPWS AND TCAS SYSTEMS AND SMOKE SUBSIDED. DIVERTED TO RJTY. FOUND RADIO ALTIMETER R/T UNIT FAILED AND PRODUCING SMOKE DUE TO SHORTED XMIT ANTENNA. REPLACED R/T UNIT AND XMIT ANTENNA. VISUALLY INSPECTED TCAS AND GPWS, NO DEFECTS NOTED. TCAS RTS IAW HN3443 AND GPWS CHECKED IAW HB3400.18. LP 11680, ITEM 1. 2H74 4T A1SO 20030428000832003042800083NM 2003 4 28 DHL2003741517 120030320A5330 SKIN BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS PILLOWING BETWEEN BS 294 AND 312 AT STR. 24 R. REMOVED RT FLOOR PANEL IN DOG HOUSE FOR ACCESS STA. 294 TO 330 RBL 30 IAW B-727 SRM 51-30-3. 2) CUT-OUT 2 EACH DAMAGE AREA 5 INCHES X 1.7500 INCH OF 8 INCHES X 1.7500 INCH IAW B-727 SRM 53-30-3 FIG. 3. 3) FABRICATED REPAIR DOUBLER 8 INCHES X 22 INCHES 2024-T3 .063 P.O. NR 9912380 IAW B-727 SRM 53-30-3 FIG. 3. 4) TREATED AND PRIMED IAW B-727 SRM 51-10-2. 5) INSTALLED REPAIR DOUBLER IAW B-727 SRM 53-30-3 FIG. 3. 6) INSTALLED ACCES PANEL IAW B-727 SRM 51-30-1. 2L73 4F4 FRTA3WE E2EA 20030429000322003042900032SO 2003 4 29 C2XA03CL090 120030409A32347455501 SELECTOR EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A C2XAO OTHER O OTHER CLCLIMB 1 SW2716954 145072 CLE FLIGHT 3160 CREW REPORTED LANDING GEAR LEVER LOCKED DOWN AFTER TAKEOFF HAD TO PRESS DOWNLOCK RELEASE TO RETRACT GEAR AS PER QRH. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER AND RELAYS K0024,K0025, AND K0453. OPERATIONAL CHECKS GOOD. 2L72 4T RTT00011AT 20030430001182003043000118NM 2003 4 30 03FDEA00602 120030424A2612 SMOKE DETECTOR BOEING727 727200 138407ENM MAIN CARGO INOPERATIVE A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25479FE 21461 INFLT RECEIVED MAIN CARGO SMOKE ALARM SEC NR 3 C/W RED TABS AND LIGHT EXT. A/C RECEIVED TO GATE NO FIRE OR SMOKE NOTED AT ARRIVAL. INSPECTED MAIN CARGO DECK SEC NR 3 NO INDICATIONS OF FIRE .CAN AYY 5070 HAD APPX 180 LBS OF DRY ICE MED EQUIP AT SECTION NR 3 RT. PERF M.C. SMOKE DET SYS ADJ/TEST PER M.M. 26-16-001-5 OP'S CK'S NORMAL. R&R NR 3 SMOKE DET AS A PREC. PER M.M. 26-16-001-4, SYS OP'S CK'S OK PER M.M. 26-16-001-5. 2L73 4F RTA3WE 20030430001742003043000174NM 2003 4 30 SWAA030860 120030417A57556546451 SKIN BOEING737 7373H4 1384600NM RT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C4 CHECK, FOUND NR 6 FLIGHT SPOILER DELAMINATED ABOVE ACTUATOR ATTACH POINT. REMOVED AND REPLACED NR 6 FLIGHT SPOILER PER MM. 2L72 4F RTA16WE 20030501001872003050100187NM 2003 5 1 ASAA0310037 120030225A534765419866 CARGO TRACK BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, CARGO TIE DOWN SUPPORT FITTING AT BS 540, LEFT BUTTOCK LINE 40 CORRODED. REMOVED AND REPLACED TIE DOWN SUPPORT PER SRM. (M) 2L72 4F RTA16WE 20030501000702003050100070WP 2003 5 1 GTIA030204 120030228A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND L-1 DOOR UPPER FRAME AFT OUTER RADIUS CRACKED. STOP DRILL CRACK. (M) 2L72 4F RTA6WE 20030505001232003050500123NM 2003 5 5 03FDEA00484 120030417A5330 DOUBLER BOEING727 727200 138407ENM LOWER FUSELAGE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 LOWER FUSELAGE JUST FORWARD OF AFT AIRSTAIR LEFT SIDE HAS A LOOSE DOUBLER. *S/D* REMOVED AND REPLACED REPAIR DOUBLER IAW BOEING 727 SRM 53-30-3. 2L73 4F RTA3WE 20030506000742003050600074WP 2003 5 6 03FDEA00569 120030421A5347 SEAT TRACK DOUG DC10 DC1030 3023501WP MAIN CARGO DECK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 MAIN CARGO DECK SEAT TRACK STA 675 TO 735 RBL 75 AT TRACK FLANGE CLIP NUT HOLES TOP AND BOTTOM CORRODED. CLOSING ACTION ON 04/14/03. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REINSTALLED NEW SEAT TRACK IAW SRM 51-31-01, FAB NEW SEAT TRACK ON MAE TRAVELER T2/326222. 2L73 4F A22WE 20030506000862003050600086NE 2003 5 6 03115324 220030425A7200310349015 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LEFT MALFUNCTIONED A VTZAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27324UE 41017 75118 DURING CRUISE, THE CREW REPORTED THAT THE LT ENGINE -OIL CONTAM- LIGHT HAD ILLUMINATED FOLLOWED BY LT ENGINE LOW OIL PRESSURE. THE CREW COMPLIED WITH THE QRH AND SECURED THE ENGINE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT ENGINE. OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA41NM E18NE 20030506001572003050600157WP 2003 5 6 ASAA0380213 120030304A532199366543 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS SEVERAL LOOSE OR MISSING INSERTS AT FS 1155-1250. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030507000582003050700058EU 2003 5 7 AUS20030357 120030320A77970301528030 WIRE HARNESS SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU ENGINE INDICATORFAULTY W O OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 1 ENGINE NH HARNESS INTERNAL FAULT (OPEN CIRCUIT). 2G72 4U4 U H4EU E12NE 20030508000962003050800096NM 2003 5 8 QXEA0300497 120030420A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - PANEL 262FT HAS CHAFE DAMAGE ON LOWER SURFACE. REPAIRED IAW RD 8/4-53-521. 2H72 4T RTA13NM 20030513001012003051300101EU 2003 5 13 AWXA200300504 120030507A2597 WIRE AIRBUS320 A320231 3930325EU ESCAPE SLIDE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-03 CHECK THE LT EMERGENCY ESCAPE SLIDE ARMED LIGHT WOULD NOT COME ON WITH THE FORWARD OR AFT OVER WING EXIT DOOR HANDLES OPEN AND BOTH EXITS ARMED. MAINTENANCE TROUBLESHOT SYSTEM USING A320 ASM 52-73-00 AND FOUND A WIRE BROKEN AT TERMINAL A OF LT EMERGENCY EXIT SLIDE ARMED CONNECTOR (2WN2). RE-TERMINATED WIRE IAW ESPM 20-48-21, PG. 12-22. OPERATIONAL CHECK WAS GOOD IAW AMM TASK 52-73-00-710-002. 2L72 4F RTA28NM 20030513001972003051300197NM 2003 5 13 QXEA0300474 120030421A3040SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09347PH1386413864 480 SEA- ON FLIGHT 2008 LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED DURING FLIGHT. WHEN SWITCHED TO WARM-UP AS PER CHECKLIST, CAUTION LIGHT EXTINGUISHED AND REMAINED OFF THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030513002182003051300218NM 2003 5 13 CH1A200397011 120030418A5753 FLAP TRACK BOEING727 727270 138408PNM NR 7 CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 7 FLAP TRACK CENTER FAIRING AFT FITTING HAS SOME CORROSION. 2L73 4F RTA3WE 20030514000802003051400080NM 2003 5 14 SWAA030981 120030502A335010126211 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 EMERGENCY EXIT LIGHT LENS BROKEN NEXT TO FWD F/A SEAT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20030528001012003052800101SW 2003 5 28 HEEA086610 120030521A6720 BEARING BELL 212 212 1181420SW BELLCRANK ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736J 31140 BELLCRANK ASSY HAS WORN BEARINGS. REPLACED BEARING DW-4 DUE TO WORN AND SLEEVE 120-015-4KA DUE TO WORN. REPAIRED. 1G71 4U H4SW 20030604000722003060400072NM 2003 6 4 UPS03240545 120030411A5751 HINGE BOEING727 72722C 138400FNM LT WING OB TAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, O/B AILERON, LT WING, O/B TAB HINGE HAS EXCESSIVE CORROSION 2ND I/ B IS CRACKED AND THE OTHER TWO ARE PITTED EXTENSIVELY. TAB HINGES REPLACED IAW SRM 51-30-02 FOR O/B AILERON TAB INSTALLATION REF. NRC 664356 2L73 4F A3WE 20030605000932003060500093NM 2003 6 5 UPS03240687 120030415A5755 PANEL BOEING727 72722C 138400FNM NR 9 SPOILER CONTAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C&SI, AFTER X-RAY INSP. NR 9 SPOILER FOUND TO HAVE WATER INGRESS AND CELL DISTORTATION SPOILER PANEL REPLACED IAW MM 27-61-01 & MM 27-62-01 2L73 4F A3WE 20030627000032003062700003CE 2003 6 27 DXTA200300020 120030430A3260 UPLOCK SWITCH CESSNA650 650 2076802CE LT MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07710QS 6507100 AFTER TAKE OFF FROM ORD, DURING GEAR RETRACTION GEAR UNLOCK LIGHT STAYED ON. CYCLED GEAR BUT NO HELP. - FOUND LT UPLOCK ACTUATOR ASSEMBLY, UPLOCK SWITCH AND LT MLG CAMBER OUT OF ADJUSTMENT. 2L72 4F A9NM 20030609001572003060900157NM 2003 6 9 HNAA0300024 120030522A5610NP15790112 WINDSHIELD DHAV DHC8 DHC8102 2809003NM COCKPIT CRACKED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07935HA18620 142 CREW REPORTED SMOKE COMING FROM THE F/O'S FRONT WINDSCREEN ELECTRICAL TERMINAL AREA FOLLOWED BY THE WINDSCREEN SHATTERING. REPLACED F/O'S WINDSCREEN. 2H72 4T RTA13NM 20030606000402003060600040NM 2003 6 6 IU62003F00019 120030410A2761654494713 HOUSING BOEING BOEING737 737* NM ACTUATOR BROKEN B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 32363 9321 ACTUATOR HOUSING HAS A BROKEN LUG. 2L72 4F RTA16WE 20030520001442003052000144CE 2003 5 20 2003F00273 120030409A2131 CONTROLLER LEAR 60 60LEAR 5170707CE CABIN PRESSURE MALFUNCTIONED A UG8AO OTHER J WARNING INDICATION TOTAKEOFF 1 GL23699DA 237 CABIN PRESSURIZING AS THROTTLES ARE ADVANCED FOR TAKEOFF. UNABLE TO DETERMINE CAUSE. CONTRACTED AN OUTSIE AGENCY FOR ASSISTANCE. AN OPERATIONAL CHECK OF THE CABIN PRESSURIZATION SYSTEM WAS COMPLIED WITH PER LEAR 60 MM 21-30-00. NO DEFECTS NOTED. AIRCRAFT WAS RETUREND TO SERVICE, AND RETURNED TO HOME BASE. (M) 2L72 4F RTA10CE 20030610000852003061000085NM 2003 6 10 DL757030426 120030503A5330146N37506 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27609DL 22816 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1710 JUST BELOW THE STRINGER 14R SKIN LAP JOINT. THE DENT WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384813-14, REV A. 2L72 4F RTA2NM 20030613000342003061300034EA 2003 6 13 JBXA03008 120030605A261224403615 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA RT ENGINE BROKEN A JBXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO05592ML 7410 FLIGHT NUMBER 5115 FROM LGA TO RDU DIVERTED INTO PHL FOR A MLG BAY OVERHEAT. ON ARRIVAL MX FOUND RT LOOP BROKEN. REMOVED AND REPLACED RT SENSING ELEMENT. 2L72 4F RTA21EA 20030523001112003052300111EA 2003 5 23 QXEA0300619 120030519A3250 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09606QX 10023 SEA-ON FLIGHT NUMBER 2504, ON ROLLOUT AS NOSE GEAR TOUCHES DOWN, GOT A CAUTION STEERING INOPERATIVE MESSAGE. FOLLOWED APPROPRIATE PROCEDURE. C/W CRJ700-SL-32-019, NOSE WHEEL STEERING CAUTION EXTINGUSHED. NOSE WHEEL STEERING OPERATIONAL CHECK WAS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030528000112003052800011GL 2003 5 28 ERAA086433 220030411A7250E23031938 NOZZLE BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL NR 2 SEPARATED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01130EH162 558 NR 2 NOZZLE HAS SEPARATION FROM INNER BAND. 1G72 3U3 UNCH3EU E4CE 20030529000412003052900041SW 2003 5 29 HEEA086632 120030521A6230 BEARING BELL 412 412 1182202SW M/R LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 WORN BEARING. REPLACED BEARING 412010427101 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030618000032003061800003SW 2003 6 18 HEEA087328 120030611A6510 BEARING BELL 407 407 1182206SW T/R DRIVESHAFT ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH3730 A625 53142 T/R DRIVESHAFT BEARING ROUGH. REPLACED BEARING 407-040-339-101, S/N ZV15304 DUE TO ROUGH. REPAIRED. 1G71 3U O H2SW 20030623001142003062300114EA 2003 6 23 A6WA200340086 120030510A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 RIGHT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. REMOVED CRACKED PORTION OF ANGLE AND INSTALLED NEW ANGLE IAW BOMBARDIER AEROSPACE REO 601R-53-61-117 REV B. (M) 2L72 4F RTA21EA 20030708000712003070800071NM 2003 7 8 AWXA200300642 120030513A53116545409602 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON MAIN WHEEL WELL COMPRESSION CHORD AT BS 663, LBL 24.5. MAINTENANCE REMOVED WEB STIFFENER, FLOOR BEAM FITTING, AND 2 EACH ANGLE STIFFENERS TO FACILITATE REPAIR; REMOVED DAMAGED PORTION OF UPPER CAP COMPRESSION BEAM; FABRICATED A NEW REPLACEMENT CHORD SEGMENT; INSTALLED REPAIR PART AND REINSTALLED PARTS REMOVED TO FACILITATE REPAIR IAW E.R. 15-5311-03141-JS1. 2L72 4F RTA16WE 20030714000082003071400008NM 2003 7 14 CALA0300345 120030630A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND BOTTOM SURFACE OF R-2 DOOR THRESHOLD WEB CORRODED AT STA 986.5 TO 990. THE LOWER SILL WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030716000492003071600049SO 2003 7 16 SIMA200315501 120030601A273041012130103 DAMPER EMB 135 EMB135KL 3260302SO RT AILERON BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21837AE 145647 DURING PHASE 4 INSPECTION, THE RT AILERON DAMPER CONTROL ROD WAS FOUND TO BE BROKEN CAUSING DAMAGE MOUNTING BRACKET ON THE AILERON. RAI RT AILERON DAMPER IAW AMM 27-12 & RAI RT AILERON IAW AMM 27-12. FCF PERFORMED AND FOUND TO BE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030717000922003071700092EU 2003 7 17 BAQA087769 120030625A77129550176240 TRANSMITTER AEROSPSA365 SA365N 8680669EU ENG TORQUE READS LOW B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM 6396 TORQUE TRANSMITTER READS LOW. REMOVED FROM ENGINE 12051 REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030109000332003010900033NM 2003 1 9 0300026305 120030102A2530191AC3 MOTOR BOEING747 747451 1384940NM Zone 900 BURNED A NWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL01665US 23820 During flight a flight attendant reported an electrical fume odor coming from galley elevator when in overide position. Aircraft continued to destination and landed without incident. Replaced elevator motor actuator. Operational check good. 2L74 4F RTA20WE 20030114001442003011400144EU 2003 1 14 DHL2003362001 120030110A3242C200601004 BRAKE AIRBUS300 A300B4203 3930306EU A DHLAAO UNSCHED LANDING OTHER J WARNING INDICATION CLCLIMB 1 SO01362DH 84 1) AFTER TAKEOFF BRAKE HOT LIGHT ILLUMINATED, COMPLETED ABNORMAL PROCEDURES. BRAKES HOT LIGHT ILLUMINATED AGAIN.2) DEFERRED #7 BRAKE IAW MEL 32-42-09 DMI #11551. SPECIAL PROCEDURES COMPLIED WITH.3) REF. DMI #11551. AFTER TAKEOFF BRAKES HOT LIGHT ILLUMINATED, COMPLETED ABNORMAL PROCEDURES. BRAKES HOT LIGHT ILLUMINATED AGAIN.4) REMOVED AND REPLACED #7 BRAKE ASSEMBLY WITH SERVICEABLE UNIT IAW M/M 32-42-27. THIS CLEARS DMI #11551. 2L72 4F RTA35EU 20030115001212003011500121 2003 1 15 BAQA082904 420030109A34217000788175 INDICATOR BELL 222 222U 1182140SW ATTITUDE MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01219HM4424 47573 ATTITUDE INDICATOR SLOW TO CORRECT AFTER ANGLE CHANGE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H9SW 20030116001242003011600124NM 2003 1 16 PCAA0301016 120030115A7600JV5 SWITCH ACTUATOR DHAV DHC8 DHC8102 2809003NM COCKPIT BENT A PCAAK NONE S AFFECT SYSTEMS NRNOT REPORTED 1 EA13843EX 335 PIT-FLIGHT#3729. CREW REPORTED THEY HAD NO FLIGHT IDLE STOP ON POWER LEVER QUADRANT (BOTH). MAINTENANCE INSPECTED AREA AND FOUND THE MICRO SWITCH ARM FOR THE BETA WARNING HORN SYSTEM WAS BENT CAUSING BINDING. SWITCH ARM WAS STRAIGNTENED, AND SYSTEM FUNCTIONALLY CHECKED SEVERAL TIMES. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP TO THE PROBLEM DURING MAINTENANCE RON, SWITCH ASSEMBLY WAS INSPECTED. THE SWITCH ARM WAS FOUND BENT AND OUT OF ADJUSTMENT. SWITCH ARM WAS REPLACED, SWITCH STRIKE PLATE WAS ADJUSTED, AND SPRING WAS REPLACED. OPERATIONAL CHECK WAS GOOD. WORK PERFORMED IN ACCORDANCE WITH INSTRUCTIONS FROM AD 2000-02-13.AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030116001312003011600131 2003 1 16 HEEA083076 420030108A2312064105430 TRANSCEIVER BELL 206 206B3 1181506SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 INTERMITTENTLY READOUT WILL COME UP 13 ON BOTH SIDES AND CAN'T SWAP SIDE TO SIDE. REPLACED BAD DS901 DISPLAY AND BAD V901 PHOTOCELL. ALSO REPLACED BAD RF CONNECTOR. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001412003011600141 2003 1 16 HEEA083085 420030108A3452066106200 TRANSPONDER BELL 206 206B3 1181506SW ATC SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032753F 2729 ATC TRANSPONDER NOT TRANSMITTING. FOUND PHOTOCELL V301 BAD, PHOTOCELL LENS MISSING AND CODE SWITCHES NOISY. REPLACED PHOTOCELL V301, LENS AND CLEANED CODE SWITCHES. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030116001872003011600187 2003 1 16 HEEA083098 420030108A345713824120234 RECEIVER BELL 206 206L3 1182108SW GPS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033107N 51512 GPS INTERMITTENTLY DROPS OFF LINE. FOUND UNIT LOST POWER DURING TEST AND FILTER DISPLAY BAD. REBOOTED UNIT AND REPLACED FILTER LENS. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20030128000102003012800010 2003 1 28 BAQA084019 420030122A221041800500001 ACTUATOR AEROSPAS365 AS365N2 8680815EU TRIM MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME317 6417 ERROR CODE NR 1 ON AUTO-PILOT TEST. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030128000872003012800087EA 2003 1 28 03024653 120030114A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA A VTZAK NONE O OTHER ININSP/MAINT 1 EA27653BR L/H EMERGENCY LIGHT INOP. R&R BULB, OP'S CK'D OK 2L72 4F RTA21EA 20030128001102003012800110SW 2003 1 28 HEEA083852 120030116A6230406010129101 ROD BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 MAIN ROTOR ROD ASSY WORN. 1G71 3U O H2SW 20030203001732003020300173NM 2003 2 3 DHL2003749001 120030131A2611 DETECTOR BOEING727 727200 138407ENM A DHLAKO NONE OTHER O OTHER NRNOT REPORTED 1 SO01749DH 22013 1) SMOKE DETECTOR SENSOR IN POSITION #8, RIGHT SIDE IS BROKEN OFF.2) REPLACED DETECTOR PICKUP IAW AEI M/M CHAPTER 26. 2L73 4F RTA3WE 20030203002052003020300205WP 2003 2 3 IZ22003F00002 220030103A731069254513 SOLENOID VALVE MTSBSIMU2 MU2B25 5780409CE GARRTTTPE331TPE33110 01514WP FUEL SYSTEM LEAKING B IZ2RK NONE K FLUID LOSS ININSP/MAINT 1 SW15281MA267 261 P106016 VALVE LEAKING FUEL BETWEEN THE SOLENOID AND VALVE BODY DUE TO BLOWN ORING. 1H72 3T4 T A2PC E4WE 20030204002892003020400289NM 2003 2 4 AWXA200300104 120030203A3350285T00976 CARD BOEING757 757225 1384959NM ZONE 100 - FUSELFAILED A AWXAK NONE P NO WARNING INDICATION ININSP/MAINT 1 WP28914AW0 0 22208 PHX - EEL - DURING INSPECTION BRAKE TEMPERATURE, R/H WHEEL WELL, AND EMERGENCY UNARMED LIGHTS WERE FOUND TO BE INOPERATIVE IN THE DIM TEST MODE. MAINTENANCE REMOVED AND REPLACED LIGHT CARD M10267 WHICH WAS FOUND TO BE DEFECTIVE. OPERATIONAL AND FUNCTIONAL TEST OF THE SYSTEMS WERE SUCCESSFUL. 2L72 4F RTA2NM 20030218001162003021800116NM 2003 2 18 VNAA0302009 120030211A3300 SOCKET DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07463PS 3087 THE CREW REPORTED THE AFT EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY TRACK LIGHTING LIGHT STRIP SOCKET IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELESASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030219000212003021900021SW 2003 2 19 YT22003F00000 120030107A6230206010446105 IDLER LINK BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL COLLECTIVE DAMAGED A YT2RO OTHER O OTHER NRNOT REPORTED 1 WP0160SM 1175 52176 REPLACED COLLECTIVE IDLER LINK ASSEMBLY. 1G71 3U3 UNCH2SW E1GL 20030219000462003021900046CE 2003 2 19 JGV2003F00000 120030201A252049190821 SEAT CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP MOUNTING BASE CRACKED B JGVRK NONE O OTHER ININSP/MAINT 1 CE09350CD 6500190 WHEN REMOVING THE INTERIOR FOR A PHASE INSPECTION, TECHNICIANS NOTICED THE CRACKED SEAT BASE UPON REMOVAL. NUT WAS OBVIOUSLY OVERTORQUED. IF THERE WERE BUSHINGS INSIDE THE SEAT FRAME TUBES THIS MIGHT NOT HAVE HAPPENED OR IT LARGE AREA WASHERS WERE INSTALLED IT MAY PREVENT THIS. PHOTOS ATTACHED. 2L72 4F4 F A9NM E6WE 20030219001002003021900100 2003 2 19 SWAA030322 420030210A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030220000512003022000051NE 2003 2 20 0300243220 220030217A7321 WOODWARD AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE A NWAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 GL01320US WYG52772 213 731201 During top of descent engine #1 experienced a compressor stall and flamed out. Flight crew performed an uneventful single engine landing. Maintenance replaced the Hydro Mechanical Unit. 2L72 4F4 FRTA28NM E29NE 20030221000272003022100027NM 2003 2 21 QXEA0300135 120030128A2120 SMOKE DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09368PH 512 SEA-ON FLIGHT NUMBER 2255, CABIN FILLED WITH SMOKE DURING TAXI AFTER COMPLYING WITH BETA LOCKOUT RESET PROCEDURES. GROUND RAN ENGINES WITH BLEED AIR AT SEVERAL POWER SETTINGS. NO EVIDENCE OF SMOKE IN FLIGHT COMPARTMENT OR CABIN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030225000922003022500092EA 2003 2 25 COMA0360116 120030224A2910848847 PUMP CNDAIRCL600 CL6002B19 1900309EA 3B WEAK A COMAO OTHER S AFFECT SYSTEMS APAPPROACH 1 SO01937CA15074 7044 FLIGHT 9450 GEAR DISAGREE WARNING.REPLACED HUDRAULIC PUMP 3B. 2L72 4F RTA21EA 20030304000852003030400085NM 2003 3 4 DL777030134 120030208A21508102099 ACM BOEING777 777232 1385232NM LEDT PACK UNSERVICEABLE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27866DA 29738 GOT SMELL OF OIL WITH VIBRATION AFTER T/O 30 MINUTES LATER L PACK MODE EICAS MESSAGE AND STATUS MESSAGE ECON COOL VALVE L INSPECTED L PACK ACM FOUND BLADE MISSING FROM ACM TURBINE SECTION FWD TO MCO/PLAC PER MEL 21-52-01 C/P DISCONNECTED CLEARED STATUS MESSAGE INSPECTED L PACK ACM - FOUND BLADED MISSING FROM ACM TURBINE SECTION - FWD TO MCO/PLAC PER MEL 21-52-01 - C/P DISCONNECT - CLEARED STATUS MSG OK ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2L72 4F RTT00001SE 20030305000732003030500073EU 2003 3 5 HEEA084656 120030212A2913 SEAL BOLKMS105 BO105S 5626006EU HYD PUMP LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW035031U AH62893 S678 HYDRAULIC PUMP HAS A SEAL LEAKING. 1G72 3U H3EU 20030307000642003030700064 2003 3 7 SWAA030414 420030222A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030307001342003030700134NM 2003 3 7 DHL2003755005 120030305A3220 VALVE BOEING727 727225 1384077NM A DHLAO OTHER JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 SO01755DH 21857 1) DURING GEAR RETRACTION NOSE GEAR VIBRATED AND SOUNDED LIKE THE NOSE GEAR DOOR WAS NOT CLOSED. NOSE GEAR LIGHT ON S/O'S PANEL AND DOOR LIGHT ON FRONT PANEL WAS ILLUMINATED UNTIL FL 24.0 THEN LIGHTS WENT OUT.2) UPON INSPECTION FOUND NOSE GEAR STRUT FLAT. FOUND SCHRADER VALVE LEAKING. REMOVED AND REPLACED SCHRADER VALVE AND SERVICED STRUT IAW DHL B727 M/M 12-15-24. INSPECTED NOSE GEAR AND DOORS, NO DEFECTS NOTED. TAXIED A/C AND LEAK CHECKED STRUT. NO DEFECTS NOTED THIS STATION. 2L73 4F A3WE 20030310001062003031000106 2003 3 10 HEEA085011 420030227A2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN LEAKING E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032014K 33020 LIFE VEST FAILED 3 MONTH (LEAKING). 1G72 4U H4SW 20030310001322003031000132NM 2003 3 10 EIA2003036 120030227A5300UNK SPLICE BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 MAIN CABIN L/H INTERIOR CORROSION ALONG SKIN LONGITUDINAL SPLICE AT STRINGER 19L, BS 1960 to 2180. CORRECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECTION, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-169-2 Rev A 2L74 4F A20WE 20030121001672003012100167SW 2003 1 21 HEEA083320 120030109A2435 FAN BELL 206 206L3 1182108SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 2153 51520 STARTER GEN COOLING FAN SPLINES WORN. REPAIRED. 1G71 3U H2SW 20030314001292003031400129WP 2003 3 14 GTIA030106 120030226A215054140031 CONTROL VALVE DOUG DC9 DC981 3022081WP LT PACK TEMP STUCK A GTIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23806NK 48051 VERY COLD IN CABIN, BOTH PACKS IN AUTO-LOST PRESSURE CABIN ALT CLIMBING EVEN THOUGH OUTFLOW VALVE FULL FWD AND LOCKED EMERGENCY DECENT AND DIVERTED. CAUGHT CABIN ALT (COULD NOT CONTROL CABIN) AND IT DESCENDED WITH AIRCRAFT RIGHT AIRCRAFT PAC SHUTDOWN CABIN ALT LIGHT ON. TRANSFER LOCKOUT AND STANDBY BLUE LIGHTS ON. TROUBLESHOT SYSTEM FOUND LEFT WING ANTI-ICE THERMOSTAT GASKET BLOWN. ALSO FOUND LEFT PACK TEMP CONTROL VALVE STRUCK IN COLD POSITION, REMOVED AND REPLACED VALVE. INSTALLED NEW GASKET LEFT WING ANTI-ICE THERMOSTAT PERFORMED CABIN PRESSURE OPERATION. NO DEFECTS NOTED. BOTH TEMP CONTROL VALVES OPERATES NORMALLY IN AUTO AND IN MANUAL, OK TO CONT. 2L72 4F A6WE 20030319001012003031900101NM 2003 3 19 TSAA0333021 120030202A33501000679 BATTERY PACK BOEING737 73725A 1384481NM PAX CABIN INCORRECT A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13819AL 23791 REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030731000992003073100099NM 2003 7 31 QXEA200300897 120030725A5240 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM SERVICE DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX- FOUND SMALL DENT ON BOTTOM OF AFT SERVICE DOOR. REPAIRED IAW HORIZON AIR EA 6-52-302. 2H72 4T RTA13NM 20030325000512003032500051NM 2003 3 25 AWXA200300206 120030219A3150 WARNING SYSTEM BOEING737 7373G7 1384595NM COCKPIT ACTIVATED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28160AW 23782 ON TAKEOFF AT PHX EN ROUTE FOR TUS WHEN THROTTLES ADVANCED AND TOGA BUTTON SELECTED THE CONFIGURATION WARNING HORN SOUNDED. DISCONNECTED AUTO-THROTTLES AND REJECTED TAKEOFF AT LOW SPEED. AFTER CLEARING RUNWAY CHECKED CONFIGURATION, FLAPS WERE AT 5 AND INDICATING, SPEEDBRAKE WAS DOWN AND IN DETENT, TRIM HOWEVER WAS AT END OF GREEN (A/C NOSE UP). TRIMMED SLIGHTLY NOSE DOWN AND ADVANCED THROTTLES, NO WARNING HORN SOUNDED. INFORMED TOWER AND WAS CLEARED FOR TAKEOFF, CONTINUED TO TUS WITH NO FURTHER PROBLEMS. 2L72 4F RTA16WE 20040322002032004032200203NE 2004 3 22 ERAA092660 120031009A62107615009043050 TIP CAP SKRSKYS76 S76 8143010NE TMECA ARRIELARRIEL1 60030NE M/R BLADE CRACKED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03574EH5073 760369 LEADING EDGE CRACKED AWAY FROM FIBERGLASS. SENT TO CTI. INSPECTED IAW SA4047-76-5 REV 11; REPLACED ABRASION STRIP IAW RS-005N-III. REPAIRED SKIN AT LEADING EDGE AND DOUBLER JUNCTION IAW RS-005N-X111. REPLACED BOTH FORWARD INTERNAL DOUBLERS AND REB ON D C CHANNEL IAW DRWG NR 76150-09043 SPEC 38023-15000; MODIFIED EXTERNAL DOUBLERS IAW RS-017-1; REPAIRED SKIN BLISTERS IAW RS-005N-11; REMOVED FOD IAW ORI 76150-50-005 SECTION IX REV N; REFINISHED IAW DRWG NO 76150-09043; STATIC BALANCE IAW RS-005N-VI. 1G72 3U3 U H1NE E19EU 20030418000782003041800078NM 2003 4 18 PCAA0302043 120030219A3397 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13831EX 160 DURING ROUTINE MAINTENANCE VISIT THE LAST TWO EMERGENCY LIGHTS ON FLOOR LIGHTING STRIP WERE FOUND INOPERATIVE. A BROKEN WIRE WAS REPAIRED NEAR ROW 9 ON FLOOR TRACK LIGHTING. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030718000342003071800034 2003 7 18 USAASB03085 420030616A23304976500001 VIDEO MONITOR BOEING737 737301 1384611NM FWD CABIN SMOKE A USAAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA19574US45589 23739 EN ROUTE, CLIMBING THROUGH FL240, THE FORWARD CABIN FLIGHT ATTENDANT REPORTED A BURNING/ELECTRICAL ODOR IN THE FORWARD GALLEY AND FORWARD CABIN AREA. GALLEY POWER WAS IMMEDIATELY SHUT OFF PER QUICK REFERENCE HANDBOOK PROCEDURES AND ODOR STOPPED. NO SMOKE OR FLAMES WERE NOTED. FLIGHT CONTINUED TO DCA WITH GALLEY POWER OFF AND NO FURTHER PROBLEMS. IT WAS REPORTED THAT THE FORWARD GALLEY OVEN WAS NOT ON AT THE TIME OF THE REPORTED PROBLEMS. MAINTENANCE FOUND THE NR 2 VIDEO MONITOR EMITTING THE BURNING/ELECTRICAL ODOR. REMOVED AND REPLACED NR 2 VIDEO MONITOR. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030722000662003072200066NM 2003 7 22 SWAA031455 120030702A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP (6 EA) IN CABIN. REPAIRED WIRING AND RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20030723000262003072300026NM 2003 7 23 UIEA200300027 120030627A2600 WARNING LIGHT BOEING747 747212B 1384886NM CARGO FIRE FALSE INDICATIONA UIEAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15808MC 21048 TURN BACK, AFTER TAKEOFF THE LOWER CARGO FIRE PROTECTION AFT LIGHT CAME ON AND WENT OUT 2-4 SECONDS AFTER SILENCING THE BELL. ACCOMPLISHED CHECKLIST AND DUMPED FUEL. RETURNED TO GYE AIRPORT. FUEL DUMPED 43,000 KGS. LOWER CARGO FIRE PROTECTION CHECKED PER MM 26-15-01. OPERATIONAL CHECK OK. (M) 2L74 4F A20WE 20040226000152004022600015NM 2004 2 26 ASAA0370005 120030408A5320146A940116 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01607AS 29751 OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT TEE. REPLACED FLOOR SUPPORT TEE PER SRM. (M) 2L72 4F RTA16WE 20040301000412004030100041EA 2004 3 1 ASO2004F00001 120030729A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG ILLUMINATED A ASOAO OTHER N FALSE WARNING APAPPROACH 1 SO11832AS 7243 DURING APPROACH, AT APPROXIMATELY 2,800 FEET AND 180 KNOTS THE CREW RECEIVED AN GEAR DOWN DISAGREEMENT ON THE NOSE WHEEL. QRH PROCEDURES WERE COMPLIED WITH AND THE GEAR CAME DOWN NORMALLY. FIRE EQUIPMENT WAS DISPATCHED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE JACKED AND SWUNG THE LANDING GEARS TEN TIMES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030825000702003082500070 2003 8 25 RAIA00307089 420030711A319705135505 DATALINK JETAIRJETSTMJETSTM4101 1500501EU FDR DISCONNECTED A RAIAO OTHER F FLT CONT AFFECTED LDLANDING 1 CE03573HK 41092 5588-STL- DURING LANDING ROLLOUT AT DEC AILERON CONTROLS JAMMED TO THE RIGHT AND RETURNED TO NEUTRAL DURING TAXI. MAINTENANCE FOUND THE FLIGHT DATA RECORDED LEFT AILERON SENSOR LINKAGE (INSTALLED BY STC ST01617NY) DISCONNECTED. THE LINKAGE WAS REMOVED. SUBSEQUENTLY THE LINKAGE HAS BEEN REMOVED FROM THE AIRCRAFT FLEET. THE STC IS IN RE-DESIGN. 2L72 4T RTA41NM 20030827001732003082700173SO 2003 8 27 C2XA03IA086 120030821A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712569 145630 IAH - DURING SCHEDULED MAINTENANCE THE RIGHT CENTER FAIRING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP ON THE EMERGENCY LIGHT ASSEMBLY AND OPERATIONALLY CHECKED THE LIGHT. 2L72 4T RTT00011AT 20030828001822003082800182NM 2003 8 28 SWAA031852 120030815A532065C28106 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND CHANNEL STIFFENERS CRACKED (2 EA) BS 1016 PRESS BULKHEAD AT BL O BELOW WL 200 AND WL 204. REPAIRED BULKHEAD PER BOEING DWG. 2L72 4F RTA16WE 20030829000892003082900089NM 2003 8 29 P5CA0300912 120030813A80117401795 STARTER BOEING747 747236B 1384804NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23924FT 21730 702225 NR 4 ENG STARTER FAILED ON ENG START. ALL ENG PARAMETERS NORMAL. REMOVED AND REPLACED NR 4 ENG STARTER PER MM 80-11-04. REPLACED STARTER COUPLING AS PRECAUTIONARY STARTER TEST NORMAL PER MM 80-11-04. 2L74 4F4 F A20WE E3NE 20030829000962003082900096NM 2003 8 29 S2YA03012 120030314A2841 INDICATOR DORNERDO32 DO328300 NM FUEL SYSTEM INACCURATE A S2YAO OTHER N FALSE WARNING CRCRUISE 1 GL13354SK 3126 DURING FLIGHT 2017, THE FUEL QUANTITY IN THE RIGHT FEEDER TANK DROPPED BELOW 150 LBS. THE CREW NOTICED CAS MESSAGES FOR FUEL CONTAMINATION, RT FEEDER TANK LOW AND RIGHT FUEL ACCURANCY FAIL. MECHANIC CLEARED THE CAS MESSAGES AND FUELED THE AIRCRAFT. NO FURTHER DISCREPANCIES NOTED. 2H72 4T RTA55NM 20030905000302003090500030SO 2003 9 5 LR7A03074 120030725A53203906245 ATTACH ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER SB 382-53-61 FOUND LT FS 497 ATTACH ANGLE CRACKED APPROX 4 INCHES LBL 61, WL 256. REPAIRED IAW LAC MEA 382-53-03-044. NR 2160. 2H74 4T A1SO 20030903002732003090300273SO 2003 9 3 C2XA03SH280 120030818A711014576608003 SKIN EMB 145 EMB145LR 3260212SO LT COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK LEFT LOWER ENGINE COWLING WAS FOUND TO BE GOUGED APPROXIMATELY 24 INCHES FROM AFT END. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A PATCH REPAIR IN ACCORDANCE WITH EMB 145 SRM 54-40-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2L72 4T RTT00011AT 20030813000222003081300022GL 2003 8 13 HEEA088561 220030731A732023007827 VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610C 51425 VALVE WOULD NOT CYCLE. SHOP REPAIR. 1G71 3U3 U H2SW E1GL 20030813000842003081300084NM 2003 8 13 2003UALA00483 120030606A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 CABIN FLOORBEAM CORRODED AT BS 852, RBL 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLES. 2L72 4F4 FRTA1NM E24NE 20030813000592003081300059NM 2003 8 13 UPS03440831 120030515A5412 BULKHEAD BOEING747 747200 1384847NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, NR 2 PYLON REAR ENGINE MOUNT BULKHEAD 5EA FASTENER HOLE CRACKED AT FRAME WEB. NR 2 PYLON REAR ENGINE MOUNT BULKHEAD FRAME WEB REPAIRED AS PER HX RS R54-53-35022 AND UPS EO B747-5410-17055-B. 2L74 4F RTA20WE 20030826000582003082600058CE 2003 8 26 5300010503 120030105A2421913723 GENERATOR CESSNA560 560XL 2076702CE PWA 545 PW545A NE RT ENGINE WORN E S4WAK NONE J WARNING INDICATION UKUNKNOWN 1 WP07613GY52 5605300 AC BEARING CAUTION ON RIGHT ENGINE ILLUMINATED. 2L72 4F4 FRTA22CE E00059EN 20030827000272003082700027EU 2003 8 27 03FDEA00946 120030621A5320A5327534420000 CROSSBEAM AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE 742 AFT CARGO CROSSBEAM AT FRAME 59 IS CRACKED APPROX 1 INCH, 4 INCHES RIGHT OF CENTER. REAIRED CROSSBEAM IAW A300-600 SRM 53-10-15 BY CUTTING AND SPLICING IN A NEW SECTION OF BEAM. WORK DOCUMENTED ON M-1805 NR N00080 2L72 4F4 FRTA35EU E13NE 20030826000192003082600019NM 2003 8 26 03FDEA01365 120030806A5744ARC0502505 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LEFT WING OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) ACTUATOR HOLE FOUND CORROSION. LT WING OUTBD FLAP INBD HINGE BRACKET (WING SIDE) ACTUATOR HOLES REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-71797, TITLE - WINGS - LT AND RT O/B FLAP - I/B HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20030826000372003082600037NM 2003 8 26 03FDEA01340 120030815A528069163395 FITTING BOEING727 727200 138407ENM NLG DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 CORROSION ON UPPER SURFACE OF NLG DOOR UPPER FITTING ON BS 227.9 BULKHEAD LBL 8, WL 180. REMOVED NLG UPPER FITTING AND LOCATED AND BACK DRILLED NEW FITTING. INSTALLED FITTING WET WITH SEALANT IAW SRM 51-30-2. 2L73 4F RTA3WE 20030827001402003082700140NM 2003 8 27 2003UALA00554 120030708A5754114T310035 WEDGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29641UA 25091 TRAILING EDGE WEDGE SKIN DELAMINATED, SLAT NR 6 MAJOR REPAIR ACCOMPLISHED. REPLACED T/E WEDGE. 2L72 4F4 FRTA1NM E24NE 20030909001442003090900144EA 2003 9 9 SWIA200312371 120030830A2761 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA SPOILER FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07431SW 7536 RIGHT SPOILERONS FAULT STATUS MESSAGE THAT WOULD NOT CLEAR. INSTALLED SERVICEABLE PCU ACTUATOR ON RIGHT SPOILERON, INBOARD POSITION. OPS CHECK GOOD IAW 27-60-00. 2L72 4F RTA21EA 20030911001282003091100128NM 2003 9 11 03FDEA01208 120030804A5754 SLAT TRACK DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING, FOUND NR 16 SLAT TRACK INBOARD MOST FITTING WITH CRACK. CRACKED RIB ON LH WING, NR 16 SLAT TRACK INBOARD MOST FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20030912000652003091200065WP 2003 9 12 DHL2003604651 120030528A5753 FLAP DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING INBD FLAP HAS THREE INTERIM REPAIRS FROM STA XW 2.000 CANT TO XW 91.000. PERFORMED MAJOR REPAIR IAW EO DHL 030514, ED-3300. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED SKIN PANEL IAW EO DHL 030514, ED-3300. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN PANEL IAW EO DHL 030514, ED-3300. CLEANED TREATED & PRIMED NEW SKIN PANEL IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW SKIN PANEL ON RT WING INBD FLAP (STA XW 2.000 CANT - XW 91.000) USING NEW FASTENERS IAW EO DHL 030514, ED-3300, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20030911001522003091100152EA 2003 9 11 AALA20030325 120030311A5320 WEB DHAV DHC3 DHC3 2800202EA FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21567AA 327 FOUND CRACK IN LEFT CUSP AT STATION 229. INSTALLED NEW CUSP SLEET FROM STATION 218-237 AND INSTALLED DOUBLER AT STATION 223 PER AARD 53-00-00-02 FIG 1 SHEET 1. (M) 1H71 3R A815 20030925001062003092500106EU 2003 9 25 XNOA01148 120030826A2910 HOSE AIRBUS300 A300B4203 3930306EU HYD SYSTEM BROKEN A XN0AD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL23371PC DURING TAXI LOW LEVEL LIGHT ON BLUE SYSTEM HYDRAULICS. FOUND INBOARD AILERON BLUE SYSTEM ACTUATOR HOSE BROKEN. REPLACE THE HOSE. NO LEAK FOUND. OPERATION NORMAL IAW A300 MM 27-11-00. 2L72 4F RTA35EU 20031002000952003100200095NM 2003 10 2 C1HA200386011 120030909A5347 SEAT TRACK BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 SEAT TRACK CORRODED BS 1090/1130 RBL 25. 2L73 4F A3WE 20030909000402003090900040SO 2003 9 9 C2XA0303SH319 120030908A33501317 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715948 145056 SHV- DURING C CHECK EMEREGENCY LIGHT ON PANEL 243 ALC FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BULB. RETESTED AFFECTED EMERGENCY LIGHT AND OPERATED GOOD IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030909002842003090900284NM 2003 9 9 QXEA200300952 120030806A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CABIN FAILED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09356PH131808287 502 BLI- 'SUP' AIRCRAFT RETURNED TO FIELD DUE TO INTERMITTENT SMOKE WARNING INDICATIONS SHORTLY AFTER TAKEOFF. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031003000922003100300092 2003 10 3 C1HA200381029 420030913A3417 ADC BOEING727 7272S7 138407ZNM COCKPIT FAILED A C1HAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15681CA 22020 CAPT'S AIR DATA COMPUTER FAILED IN FLIGHT. ADVISED COMPANYVIA AIRINC. DIVERTED TO DFW. REPLACED NR 1 ADC PER M/M 34-12-11. OP'S. CHECK GOOD. RII NOT REQUIRED. QUICK DISCONNECTS INSTALLED BY VENDOR PER 12-12-00. 2L73 4F A3WE 20031014000172003101400017NM 2003 10 14 UPS03541237 120030918A7160 ACOUSTIC LINER BOEING757 75724APF 1384969NM RT ENGINE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01402UP 23724 RT ENGINE HAS DENT & DELAMINATION ON INLET SOUND ABSORBENT LINER. REPAIRED DENT IN RT NOSE COWL ACOUSTICAL LINER PER MM 72-33-05-8 PG 1. 2L72 4F RTA2NM 20031029001202003102900120EU 2003 10 29 KBM2003F00015 120030819A335016061 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE EMERGENCY LIGHT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH2600 2884 BATTERY LIGHT ILLUMINATES IN FLIGHT FOUND NR 19 CELL REVERSE POLARITY. REMOVED AND REPLACED WITH SERVICEABLE CELL. REPLACED WITH SERVICE BATTERY. 1G71 3U3 U H9EU E19EU 20031029001352003102900135EU 2003 10 29 KBM2003F00030 120030824A5270SP381200 SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DOOR WARNING FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH2618 2884 RT SIDE BAGGAGE DOOR WARNING LIGHT IS INOPERATIVE. REPLACED SWITCH WITH NEW.(K) 1G71 3U3 U H9EU E19EU 20031030000562003103000056NM 2003 10 30 UPS03441319 120030922A5340 FITTING BOEING747 747121 1384871NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, DURING PERFORMING BS 1000 RT BATH TUB FITTING REPLACEMENT AS PER EO NR B747-5310-18579A, IT WAS FOUND 3 EA OF FASTENER HOLES SEAM AT I/B VERT FLANGE AND 6 EA OF FASTENER HOLES FOUND OVERSIZED DIAMETER .309 INCH IN O/B HORIZ FLANGE. THE BATH TUB FITTING REPAIRED AS PER RS NR R53-23-25077 AND AS PER EO B747-5310-17015-C FOR FURTHER INSPECTION. 2L74 4F A20WE 20031031000662003103100066NM 2003 10 31 DL73G030831 120030912A2750D229 CONNECTOR BOEING737 7373L9 1384470NM RT FLAP XMITTER BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO27232DZ 24220 ON APPROACH INTO BOS SET FLAPS TO 2, FLAP IND SHOWED LT FLAP AT ALMOST 1. RT FLAP JUST OUT OF UP, NO ROLL. FOUND WIRES TO PINS 1 AND 2 OF D229 RT FLAP POS XMITTER PLUG BROKEN AT PINS. CRIMPED NEW PINS, OPERATED FLAPS, SYS OK. 2L72 4F RTA16WE 20031110001652003111000165NM 2003 11 10 SWAA032247 120031013A3350101114 LENS BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN OUTBD OF FWD F/A'S SEAT. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20031113000322003111300032EU 2003 11 13 BAQA089648 120031010A6730L673M40A1001 ACTUATOR UROCOPEC135 EC135T1 5620026EU FENESTRON WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH1035 0131 FENESTRON ACTUATOR WORN. REPLACED WITH SERVICEABLE UNIT. 11/03/03. 1G72 3U H88EU 20031117000432003111700043EU 2003 11 17 2003UALA00735 120030930A5520 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ELEVATOR CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29401UA* CG1442 435 WATER INGRESSION FOUND AT THE FOLLOWING LOCATIONS: LT ELEVATOR UPPER SURFACE - 2 2" BY 2" AREAS, 3.5 INCHES FWD OF TRAILING EDGE, 160.8 AND 187.6 " FROM THE IB END. LWR SURFACE HAS 7 2' BY 2" AREAS, 3.5 " FWD OF TE AND 139.2, 146.2, 153.6, 160.7, 175.3, 181.6, 187.6 INCHES FROM IB EDGE. REPAIRED DAMAGED AREAS IAW SRM 55-21-11 TO ELIMINATE WATER INGRESSION. 2L72 4F4 FRTA28NM E40NE 20030917001062003091700106EA 2003 9 17 ASOA03393 120030822A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 DURING A C-CHECK IN MCN, THE AFT CARGO WALL FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT CARGO WALL FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20031120000122003112000012NM 2003 11 20 AWXA200301221 120030920A55146553746U281 SHIELD BOEING737 737301 1384611NM HORIZONTAL STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT HORIZONTAL STABILIZER PANEL (9123) METAL SHIELD (BLADE), AT STAB STA 67.54, STAB LBL 21.75. MAINTENANCE REMOVED CRACKED LT HORIZONTAL STAB BLADE, AT STAB STA 67.54, STAB LBL 21.75; FABRICATED A NEW REPLACEMENT BLADE; INSTALLED REPAIR PART IAW B737-300 SRM 51-20-01, PG 1, SRM 51-70-05, PG 1, AND SRM 51-40-02, PG 1. 2L72 4F RTA16WE 20031121000032003112100003EA 2003 11 21 03320645 120031116A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A VTZAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA27645BR 7383 DURING CRUISE EN ROUTE TO SYR ON FLIGHT 7414 CREW REPORTED A FLAP FAIL AT ZERO DEGREES. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040108001512004010800151NM 2004 1 8 AMTA200301250 120030929A5330 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 FUSELAGE SKIN CORRODED AT LOWER ATC ANTENNA MATING SURFACE. REPAIRED SKIN IAW MFG ER 03-3513.(K) 2L72 4F4 FRTA2NM A12EU 20040112002812004011200281NM 2004 1 12 AALA20031434 120031213A3350S283T014 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21371AA 25198 EMERGENCY FLOOR PATH LIGHTING AT 22, 23, AND 24HJ, INOPERATIVE. REPLACED BATTERY PACK M732 FOR 22, 23, AND 24HJ EMERGENCY FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040113002282004011300228EA 2004 1 13 QXEA200301484 120031125A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX- LIGHTING DAMAGE ON RIVET AT FUSELAGE STATION 1093.20, RIGHT SIDE FIVE INCHES ABOVE SKIN LAP JOINT. REPAIRED IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20040114000112004011400011NM 2004 1 14 03FDEA01925 120031117A5510 STRUCTURE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB LT UPPER CENTER PLANK NR 25L BARREL NUT BORE FOUND CORROSION ON SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STAB LT UPPER CENTRE PLANK 25L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. 2L73 4F4 FRTA22WE E13NE 20040113000452004011300045EA 2004 1 13 COMA0360564 120031218A5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER APAPPROACH 1 SO01949CA20763 7080 FLIGHT 5815 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20031124001292003112400129NM 2003 11 24 GAIA03139ST 120031024A5347BAC1520841 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND CABIN SEAT TRACK CORRODED RBL 45, BS 720 TO 870. REF FASI N/R NR 61684. REPLACED SEAT TRACK RBL 45 BS 720 TO 870 IAW 53-10-5 FIG 7 AND 53-10-2 FIG 7. (M) 2L73 4F RTA3WE 20031126000132003112600013EU 2003 11 26 RAIA00311283 120031108A2910 HYDRAULIC LINE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM LEAKING A RAIAO OTHER K FLUID LOSS LDLANDING 1 CE03556HK 41073 9870-SGF- NOSE LANDING GEAR WOULD NOT EXTEND. HYDRAULIC LEAK. MAINTENANCE REMOVED AND REPLACED NR 1 HYDRAULIC PUMP AND PRESSURE LINE. 2L72 4T RTA41NM 20031126000642003112600064CE 2003 11 26 DXTA200300165 120031119A3411 PITOT TUBE CESSNA750 750 2076810CE RIGHT OBSTRUCTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07958QS 7500158 ON TAKEOFF ROLL AT 70 KTS THE FOLLOWING EICAS MESSAGES APPEARED: YD OFF LOWER, MACH TRIM OFF, FGC ADC MISCOM, ABORTED TAKEOFF. DURING VISUAL INSPECTION NOTED A BLOCKAGE IN THE RT PITOT TUBE, PURGED RT PITOT LINE AND PITOT TUBE, NOTED MUD LIKE SUBSTANCE WAS REMOVED DURING PURGING. PERFORMED PITOT STATIC LEAK CHECK AND ADC SYSTEMS CHECK, OPERATIONAL TEST OF BOTH SYSTEMS CHECK GOOD. WORK DONE IAW CESSNA 750 MM CHAPTER 34-11-08. 2L72 4J RTT00007WI 20031215001642003121500164WP 2003 12 15 AALA20031114 120031007A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21972TW 53622 SFO - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT STATION 812 THROUGH 925. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20031217001962003121700196NM 2003 12 17 AWXA200301489 120031124A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 18 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 PHX - EEL - DURING 8-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031217001972003121700197NM 2003 12 17 AWXA200301490 120031124A33501010421 HOUSING BOEING757 7572S7 1384962NM SEAT ROW 6-8 LT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTS SEAT ROWS 1-8 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULLNOSE LIGHT HOUSING BETWEEN SEAT ROWS 6-8, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20031218000162003121800016NE 2003 12 18 MALA030509 220031124A7200AVRO146RJ85A ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 VIBRATION A MALAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 GL15519XJ E2344 ON DESCENT NR 3 ENG VIBRATED N1 & N2 DROPPED, EGT FLUCUATED BETWEEN 640-680 DEG. SHUTDOWN OF ENG 3 PER QRH. MX COMPLETED VARIOUS INSPECTIONS, BORESCOPES & INSTALLED 3 ENGINE FERRY KIT. REMOVED CARD FOR DOWNLOAD, INSTALL & DOWNLOAD ON NEW CARD. DOWNLOADED A/C INFO ONTO NEW FADAMS CARD. VERIFY TEMP & DURATION OF NR 3 ENG. NR 3 ENG TEMP WAS 691 FOR 208 SECONDS. INSPECT NR 3 ENG OIL CHIP DETECTOR. REMOVED, INSPECTED, RE-INSTALLED CHIP DETECTOR. NO CONTAMINATION. INSPECT EXHAUST FOR METAL. INSPECTED NR 3 EXHAUST, NO METAL CONTAMINATION. FAN ROTATES FREELY, WITH NO INDICATION OF AUDIBLE DEFECTS. BORESCOPE LAST TWO EXHAUST STAGES FOR METAL. REPLACED ENG REF WORK BACKAGE DATED 11-25-03, ALL CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20031218000442003121800044EU 2003 12 18 008181 120031129A6120 CONNECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE ECU DAMAGED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL17138SD 138 462 DRG855983 AIRCRAFT ABORTED TAKEOFF WHEN ERRATIC TORQUE INDICATIONS WERE OBSERVED ON THE NR 2 ENGINE. ENGINE TORQUE INDICATION WAS FLUCTUATING FROM 50 TO 120 WITH CTOT ENGAGED. AT 1350Z, FWA MX REPORTED OF TIGHTENING A LOOSE BACKSHELL ON A ECU CONNECTOR. THE AIRCRAFT WAS GROUND RAN, OPERATIONAL CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20031218001052003121800105NM 2003 12 18 2003UALA00893 120031122A3260 TARGET BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE MLG OUT OF ADJUST A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29914UA 25381 RETURNED TO DEN, UNABLE TO RETRACT LANDING GEAR. FOUND BOTH ACTUATOR TARGETS FOR AIR AND GROUND SAFTEY SENSORS OUT OF ADJUSTMENT. TARGETS WERE ADJUSTED AS WELL AS THE TELEFLEX CABLE. 2L72 4F4 FRTA16WE E2GL 20031014000572003101400057 2003 10 14 SWAA032177 420030929A2565D31354 SLIDE BOEING737 7373L9 1384470NM FWD ENRTY DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20040130000372004013000037NM 2004 1 30 SWAA032831 120031229A3350100031 LIGHT BOEING737 7372H4 138448CNM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20040128002032004012800203WP 2004 1 28 UPS04841678 120031230A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 CREW PREFLIGHT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW 33-50-01-2. 2L74 4F RT4A25 20040205000122004020500012NE 2004 2 5 NACA20030121 220031115A74141083154 BRUSHES DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE DISTRIBUTOR BROKEN A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 AL03779TA84 84 51946 45529 36710 NR 2 ENGINE SHUT DOWN DUE TO L-2 PRIMARY CIRCUIT OPEN. FOUND BROKEN BRUSHES, REPLACED LT DISTRIBUTOR. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040213000162004021300016NM 2004 2 13 2003UALA00976 120031220A5347 SEAT TRACK AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29821UA 944 CABIN SEAT TRACK OB FR 62 FWD, SEVERAL LUGS WITH LIGHT CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED DAMAGED SECTION IAW SRM 53-00-15. 2L72 4F4 FRTA28NM E40NE 20040217000352004021700035EU 2004 2 17 ASOA03687 120031204A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 DURING A C-CHECK IN BNA, THE RIGHT OUTBOARD SEAT TRACK SECTION BETWEEN FS 13-23 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK SECTION BETWEEN FS 13-23 IAW SRM 51-25-01 AND 51-25-04. (M) 2H72 4T RT 20040401000262004040100026EU 2004 4 1 AALA20030939 120030902A33506104789 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211424M 11407 ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 13 AND 14. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20050816000812005081600081NM 2005 8 16 SWAA032477 120031107A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND 3 EA STRINGER CLIPS CRACKED AT BS 737, STR 19R, BS 727B, STR 21R, AND BS 727A, STR 21R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060801000312006080100031WP 2006 8 1 IXXA060518S 120031008A5310 TORQUE BOX DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND L-2 DOOR CUTOUT LOWER FORWARD TORQUE BOX WEB CRACKED. REMOVED DAMAGED WEB. FABRICATED NEW WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D, AND DOUGLAS DRAWING 9751060. 2L74 4F RT4A25 20060801001032006080100103WP 2006 8 1 IXXA060554S 120030925A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 MISREPAIRED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND L-2 DOOR CUT-OUT LOWER FORWARD CORNER REPAIR DOES NOT COMPLY WITH AD 2000-20-08. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-20D, 51-1-21, AND 51-1-21. 2L74 4F RT4A25 20070503002332007050300233NM 2007 5 3 AT0700051 120031022A5311 FRAME BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15992AT 55136 A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. FORMERS AT STA 200 DAMAGED. FABRICATED REPLACEMENT SECTION OF FORMERS STATION 200, MATERIAL 7075 T6 INSTALLED PER B717-SRM 53-00-06 FIG 2. 2L72 4F TRA6WE 20030813001552003081300155NM 2003 8 13 SWAA031665 120030728A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 1003, STR 21L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20030815000952003081500095 2003 8 15 HEEA088442 420030725A3457N0002000 GPS SKRSKYS76 S76A 8143006NE COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035435V 760158 GPS INTERMITTENTLY TRANSMITS AFTER ONE HOUR OF OPERATION. 1G72 3U H1NE 20030820002452003082000245 2003 8 20 USAABA03012 420030430A25654A38571 REGULATOR AIRBUS330 A330323 3930335EU ESCAPE SLIDE FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19 DURING SLIDE TESTING IN THE SHOP, THE SLIDE DID NOT INFLATE WHEN THE REGULATOR WAS ACTIVATED. AFTER APPLYING A SHARP RAP TO THE REGULATOR, THE SLIDE INFLATED NORMALLY. MAINTENANCE IN THE SHOP FOUND THE REGULATOR BORE SCORED WHICH WAS MOST LIKELY CAUSED BY CHATTERING OF THE SPRING WASHERS. (M) 2L72 4F RTA46NM 20030821000402003082100040NM 2003 8 21 03FDEA01015 120030626A5754ARC0503504 HINGE DOUG MD11 MD11 3023602NM LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE INBOARD FOUND CORROSION. RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE INBOARD CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5740-71734 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED. 2L73 4F RTA22WE 20030821001372003082100137EU 2003 8 21 03FDEA00888 120030616A532053610270127 ATTACH ANGLE AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25658FE 752 FWD AVIONICS FLIGHT COMPT RT INBOARD OVERHEAD FLOOR SPT ATTACH ANGLE CRACKED AT STA 972. FR10 AS SEEN FROM ACCESS DOOR. REMOVED AND REPLACED ANGLE IAW SRM 51-40-21 ON N00283. 2L72 4F RTA35EU 20030404001422003040400142NM 2003 4 4 SWAA030462 120030301A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, RBL 40. REPAIRED BEADED WEB PER SWA T1. 2L72 4F RTA16WE 20030328000562003032800056NE 2003 3 28 C8GA2003008R 220030320A7200 ENGINE BOEING727 727225 1384077NM PWA JT8 JT8D9A 52048NE NR 3 LEAKING A C8GAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15808EA54210 22439 666631 ON CLIMB OUT, NR 3 ENGINE OIL QUANTITY DECREASED STEADILY TO APPROXIMATELY ONE GALLON. AIR TURNBACK TO BOSTON AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND SERVICE NR 3 ENGINE OILS. RAN ENGINE ON GROUND AND NO OIL LOSS OR LEAKS WERE NOTED ON GROUND IAW MM 79-31-0. AIRCRAFT RETURNED TO SERVICE. ON CLIMB OUT, NR 3 ENGINE OIL QUANTITY DECREASED STEADILY. AIRCRAFT AIR TURNBACK TO BOSTON AND LANDED WITHOUT INCIDENT. RAN ENGINE PER MM 71-00-67 PAGE 211 AND NOTED EXCESSIVE OIL COMING FROM BREATHER. SUSPECT #5 BEARING CARBON SEAL BAD. PREPARED ENGINE FOR FERRY FLIGHT. REPLACED THE NR 3 ENGINE, LEAK, TRIM AND OPERATIONAL CHECK GOOD PER MM 71-00. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20030408000822003040800082WP 2003 4 8 03FDEA00390 120030405A5280 DOOR DOUG MD10 MD1010F WP GE CF6 CF66D 30020GL MLG GOUGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25393FE 46627 RT MLG DOOR AFT OUTBOARD PAN HAS 6 INCH LONG GOUGE. LONG GOUGE HAS CRACK, REMOVED CORNER PAN. RECEIVED NEW PAN DRILLED HOLES TREATED PRIMED AND PAINTED AND INSTALLED IAW SRM 52-10-00, 51-35-01,51-35-02,51-31-01 AND 51-21-01. 2L73 4F4 FRTA22WE E23EA 20030407000962003040700096NM 2003 4 7 TSAA0353003 120030129A53306546529 SKIN BOEING737 7372M6C 1384708NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 EXTERIOR 1 INCH CRACK BETWEEN BS 440 AND BS 460 AT BL 0. TRIMMED OUT DAMAGED AREA ON LOWER LOBE ANTENNA CUT OUT. PERFORMED NDT INSPECTION OF CUTOUT, SKIN AND SATELLITE HOLES USING HFEC, NO DEFECTS NOTED. FABRICATED A .063 INCH THICK FILLER AND .071 INCH THICK REPAIR DOUBLER FORM 2024-T3 CLAD SHEET. ALODINED AND PRIMED REPAIR PARTS AND BARE SURFACES WITH MIL-C-5541 AND BMS 10-11 TYPE 1. INSTALLED REPAIR PARTS USING RIVETS, WASHERS AND BOLT IDENTIFIED IN FASTENER CODE TABLE. REPAIR COMPLETED IAW ECO 3329. (M) 2L72 4F RTA16WE 20030408000962003040800096NM 2003 4 8 2003UALA00316 120030331A3350362624 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29905UA 25005 FLIGHT CREW REPORTED THAT THE EMERGENCY ESCAPE LIGHTING (EEL) IN THE AFT 8 FEET OF CABIN WERE INOPERATIVE. REPLACED LIGHT STRIPS AT SEAT 15C, 17C 19C. OPS CK OK. 2L72 4F4 FRTA16WE E2GL 20030414000692003041400069EU 2003 4 14 AUS20030239 120030228A5311D53112169200 FRAME AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT SIDE DOOR FRAME CRACKED IN HOLE NR 4 FOUND DURING EDDY CURRENT INSPECTION IAW NDT TESTING MANUAL 53-11-53. 2L72 4F4 FRTA28NM E29NE 20030416002762003041600276EA 2003 4 16 QXEA0300443 120030407A527070821142 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09613QX2296 10045 FAT-ON FLIGHT NUMBER 2490, AFTER APU SHUTDOWN, APU DOOR OPEN CAUTION MESSAGE DISPLAYED, PER CHECKLIST, RESTARTED APU. CAUTION MESSAGE EXTINGUISHED. REMOVED AND REPLACED APU DOOR ACTUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030416003962003041600396EA 2003 4 16 SWIA200311714 120030112A3040 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDSHIELD TEMP MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07926SW 7687 AFTER LANDING, SMOKE IN COCKPIT, STOPPED WHEN LT WINDSHIELD HEAT TURNED OFF. REMOVED AND REPLACED WINDSHIELD TEMPERATURE CONTROLLER. INSPECTED WIRING AND OPS CHECKED WINDSHIELD HEAT FOR HALF HOUR. OPS CHECK GOOD. 2L72 4F RTA21EA 20030424000792003042400079WP 2003 4 24 ZW0A0303302 120030322A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139619V 53566 BOTH AFT OVERWING EXIT LIGHTS AND THE EGRESS LIGHT AT ROW 15 WERE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK 60-1177-9LB, AND THE LAMP FOR THE EGRESS LIGHT P/N 7732. CHECK-C 10-30-02 STL. 2L72 4F RTA6WE 20030425001102003042500110NM 2003 4 25 DLM90030219 120030226A3244 TIRE DOUG MD90 MD9030 3023690NM LT MLG FAILED A DALAO OTHER O OTHER LDLANDING 1 SO27913DN 53393 ON LANDING BOTH LT MAIN TIRES BLEW. EMERGENCY VEHICLES CONFIRMED BLOWN TIRES AND SOME DAMAGE TO THE STRUT AND WING OCCURRED. TOUCHDOWN WAS VERY SMOOTH WITH CONTAMINATED RUNWAY AND MAX AUTOBRAKES SELECTED. BRAKES, DACMS, AND CONTROLLER CHANGED. 2L72 4F RTA6WE 20030428000582003042800058NM 2003 4 28 OZI2003F00003 120030117A5315001A534C4061338 FLOORBEAM DORNERDO32 DO328300 NM ZONE229 CORRODED A OZIAO OTHER O OTHER NRNOT REPORTED 1 SW07410Z 7126 3125 FORWARD SIDE OF LAVATORY FLOORBEAM (FRAME 35), CORRODED. 2H72 4T RTA55NM 20030424002002003042400200 2003 4 24 SWIA200311851 420030323A2210 RELAY EMB 120 EMB120ER 3260203SO TRIM PROXIMITY MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07234SW 120308 AFTER TAKEOFF WITH AUTOPILOT SELECTED TO CAPTAIN'S SIDE, TRIM FAIL ILLUMINATED ON MAP MOMENTARILY, BUT THEN EXTINGUISHED. AUTOPILOT WAS ENGAGED; ON DESCENT PLANE PITCHED DOWN AND LIGHT CAME ON AGAIN. REPLACED TRIM PROXIMITY RELAY K0393. BOTH AUTOPILOT FLIGHT DIRECTOR SYSTEMS OPERATE NORMALLY PER MM 22-11-00. 2L72 4T RTA31SO 20030429000932003042900093SW 2003 4 29 A2D2003F00000 120030402A321040113 LEG ASSY AIRTRCAT400 AT400 0390202SW GARRTTTPE331TPE331* 01514WP HARTZLHCB3T HCB3TN5 GL LT MLG BROKEN G A2DGO OTHER O OTHER ININSP/MAINT 1 SW11237448759 400A0429 LT LANDING GEAR LEG DEVELOPED SURFACE DEFECT (CRACK) A SHEER WAS PROLONGED FROM THE DEFECT THROUGH THE 1 INCH GEAR LEG THICKNESS. THE AIRCRAFT LANDED WHEN A LOUD POP WAS HEARD BY THE PILOT. HE PULLED UP AND MADE AN EMERGENCY LANDING AFTER THE GEAR LEG FELL OFF THE AIRCRAFT. 1L71 3T3 T A9SW E2WE 6 CP15EA 20030428001022003042800102EU 2003 4 28 MALA030227 120030403A2120 ODOR SAAB SF340 SF340A 7850100EU COCKPIT DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL1576XJ 340A076 DURING FLIGHT 3148, BURNING ODOR IN COCKPIT. 2L72 4T RTA52EU 20031219000702003121900070NM 2003 12 19 CALA0300704 120031208A5730 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733132 29281 INSPECTION FOUND A 6.25 INCH CRACK IN RT WING FIXED L/E SKIN AT STA OSS 421- OSS 471. THE SKIN WAS REPLACED IAW EA 5731-01010, REV D, OP 3. 2L72 4F RTA2NM 20031219001622003121900162EU 2003 12 19 YENA200340 120031205A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15528JB8670 1591 EMERGENCY LIGHT TEST FAILS IAW 33-51-00-01-1. REMOVED AND REPLACED EPSU IAW 33-51-38. OPERATIONS CHECK NORMAL. 2L72 4F RTA28NM 20031223000832003122300083NM 2003 12 23 VNAA0312004 120031206A2612 FIRE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE APU WILL NOT TEST A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL07463PS 3087 THE CREW REPORTED THAT THE APU FIRE TEST WON'T TEST. MAINTENANCE THEN DEFERRED THE APU FIRE TEST WITH THE CREW IN ACCORDANCE WITH 49-1 C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031229001442003122900144NM 2003 12 29 UPS03241659 120031215A3350 LIGHT BOEING727 72730C 1384009NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 EMERGENCY EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, SYS GROUND CHECK GOOD. 2L73 4F A3WE 20040105001592004010500159CE 2004 1 5 AMWA110 120031222A553111464000038 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07139ZV UE139 DURING INSPECTION FOUR CRACKS FOUND ON THIS RIB, TWO ON THE LT SIDE AND TWO ON THE RT SIDE LOCATED ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46 & 101-640000-38. LT STRINGER P/N 101-640000-39 & 101-640000-45. 2L72 4T RTA24CE 20040106000932004010600093SO 2004 1 6 C2XA03TY214 120031218A532014529150007 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS DURING A SCHEDULED 3C INSPECTION THE Z-PROFILE BEHIND SERVICE DOOR AT GALLEY WAS CORRODED. MAINT REMOVED AND REPLACED THE Z-PROFILE IN GALLEY IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040106000842004010600084SO 2004 1 6 C2XA03SH507 120031218A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712924 145311 SHV- DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031009000342003100900034SO 2003 10 9 SIMA200320809 120030726A3350SJG022100 TERMINAL BLOCK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A SIMAO OTHER O OTHER CRCRUISE 1 SW21649PP 145234 CREW REPORTED THE EMERGENCY LIGHT NOT ARMED LIGHT ILLUMINATED DURING FLIGHT WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED THE GROUND BLOCK, GROUND JUNCTION, IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031020001722003102000172NM 2003 10 20 DL777030808 120030824A38102920016101 VALVE BOEING777 777232 1385232NM WATER SYS FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27866DA 29738 AFTER TAKEOFF NO WATER PRESSURE IN GALLEYS OR LAVS. FOUND PRESELECT OVERFLOW VALVE FAILED AND REPLACED SAME. 2L72 4F RTT00001SE 20040106002272004010600227WP 2004 1 6 GTIA030974 120031115A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 176, 25 INCHES RBL. REMOVED CORRODED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW SUPPORT. (M) 2L72 4F A6WE 20040108000872004010800087EU 2004 1 8 KBM2003F00037 120031002A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 HALF SHELL BEARINGS HAVE CRACKED. REPLACED WITH NEW HALF SHELL BEARINGS. 1G71 3U3 U H9EU E19EU 20040112000022004011200002WP 2004 1 12 AALA20031241 120031108A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21559AA 53089 DURING OVERNIGHT MAINTENANCE FOUND AFT UPPER CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT UPPER CABIN EMERGENCY LIGHT BATTERY PACK B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031125001682003112500168NM 2003 11 25 SWAA032496 120031111A3350101073 LIGHT BOEING737 7373H4 1384600NM COCKPIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED D CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY PER WDM. 2L72 4F RTA16WE 20031125001602003112500160NM 2003 11 25 ASAA0310490 120030526A531465476938 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE KEEL BEAM AT FUSELAGE STATION 800, RIGHT BUTTOCK LINE 6 CORRODED. REPAIRED KEEL BEAM PER EA. (M) 2L72 4F A16WE 20031202001302003120200130EA 2003 12 2 ASOA03514 120031016A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11860AS 7433 FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY CEILING LIGHT AT ROW FIVE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031203000452003120300045EA 2003 12 3 2003F00635 120030930A5270 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA OVERWING EXIT FALSE INDICATIONA FDKAO OTHER N FALSE WARNING CRCRUISE 1 SW07507MJ 10077 REPORTED THAT THE LT OVERWING EXIT CAUTION INTERMITTENLY ILLUMINATED IN FLIGHT. MAINTENANCE RESEATED THE EXIT DOOR AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. (M) 2L72 4F RTA21EA 20031205000072003120500007NM 2003 12 5 C1HA200397016 120031021A3350 BATTERY BOEING727 727270 138408PNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK NORMAL IAW MM 33-50-61. 2L73 4F RTA3WE 20040122001062004012200106EA 2004 1 22 ASOA03657 120031216A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, BL 27.00-36.00 ON THE LEFT AND RIGHT SIDES WRE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20040122001382004012200138NM 2004 1 22 ASAA0310182 120030321A5315 FLOORBEAM BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 663-706, RIGHT BUTTOCK LINE 25 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040122001322004012200132 2004 1 22 GTIA030966 420031108A2565 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND RIGHT CABIN FLOOR PANEL 886-946 METAL SUPPORT WORN THROUGH, CRACKED. REMOVED WORN SUPPORT. INSTALLED NEW SUPPORT CHANNEL. (M) 2L72 4F RTA6WE 20031208001642003120800164NM 2003 12 8 AWXA200301326 120030930A5414311A145013 SKIN BOEING737 7373G7 1384595NM LT NACELLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DURING C-17 CHECK A .375 INCH CRACK WAS FOUND ON LT PYLON ACCESS LAND (5727L) NAC STA 219. MAINTENANCE STOP DRILLED CRACK LT PYLON ACCESS LAND NAC STA 219 AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER AND FILLER WASHERS; INSTALLED REPAIR PARTS IAW ER 03-5433-01037-DL1. 2L72 4F RTA16WE 20030918000902003091800090GL 2003 9 18 2003F00571 320030806A6111114HCA0 BLADE MCAULY B5JFR36C1103JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR36B5JFR36C1103GL PROPELLER CRACKED B K NONE O OTHER ININSP/MAINT 1 SO05 130901205 020627 020627 PROPELLER WAS REMOVED AND SENT TO PIEDMONT AVIATION COMPONENT SERVICES (REPAIR STATION QWPR503X) FOR MCCAULEY ALERT SERVICES BULLETIN 246B/REV 2 INSPECTION. DURING FLUORESENT PENETRANT INSPECTION FOUND NR 1 BLADE P/N 114HCA-0, S/N PE006 (TSN 13,090.01; TSO 1,205.41) WITH AN INDICATION PER MCCAULEY ASB 246/REV 2. 2L72 4T RTA41NM 6 CP15NE 20030924000592003092400059NM 2003 9 24 DL73G030774 120030820A5330 SKIN BOEING737 7373L9 1384470NM DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27231DN 23717 RT FUSELAGE SKIN / STA 312-360 / S14-S19. DAMAGED REPLACEMENT SKIN SECTION FABRICATED IAW ER/A 423343-14. 2L72 4F RTA16WE 20040129000082004012900008EA 2004 1 29 COMA0360579 120031227A5330601R35005 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01956CA19994 7105 DENT .018 DEEP IN LEFT FUSELAGE LOWER SKIN AT FS 580.00 + 30 BELOW STR 20 L. RECONTOURED SKIN DAMAGE AREA IAW WVAC EO NR 601R-53-4489. 2L72 4F RTA21EA 20040129001862004012900186NM 2004 1 29 AALA20040030 120031219A5320 SILL BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21386AA 27060 AFW CORROSION FOUND ON 1.5 BY .7 INCH AREA, DEPTH .040, OF FORWARD CARGO DOOR LOWER MAIN SILL NEAR STA 613. THICKNESS PRIOR TO CORROSION REMOVAL WAS .276. REMOVED FASTENERS AS REQUIRED FOR BLENDOUT. ENSURE NO CORROSION ON FASTENERS OR IN HOLES. REMOVED ALL CORROSION. INSPECTED USING HFEC FOR CRACKS. ROTO-PEEN BLENDED SURFACES. ALODINE AND PRIME BLENDED AREA WITH TWO COATS PRIMER. APPLIED DYNOL TO ENTIRE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040204001362004020400136EU 2004 2 4 YENA200329 120031027A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15546JB4705 1827 EPSU INT EMERGENCY RT FAULT ON EMERGENCY LIGHTS TEST. REMOVED AND REPLACED RT EPSU IAW AMM 33-51-38, OPS CHECK GOOD. 2L72 4F RTA28NM 20040204001932004020400193 2004 2 4 SWIA200312567 420031027A2210 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07217SW6318 2122 2242 120286 FO SIDE AUTOPILOT CAUSES CONTROL WHEEL TO SHAKE. REMOVED AND REPLACED NR 2 APC COMPUTER WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040206000352004020600035EU 2004 2 6 USAASA03144 120031228A335032145510 POWER SUPPLY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19182UW 1536 LAX - THE L2 DOOR EMERGENCY POWER SUPPLY UNIT DID NOT TEST DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040213000012004021300001WP 2004 2 13 MEX203546 120031204A3244H445X16520 TIRE DOUG DC9 DC987 3022087WP PWA JT8 JT8D1 52044NE LT MLG DEBONDED W ASMFO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SW23205AM 49405 AFTER LANDING WAS LISTED AN STRONG NOISE IN THE MAIN LANDING GEAR. DURING REVISION OF THE MENTIONED AREA WERE FOUND SEVERAL DAMAGES IN THE NEARBY AREA OF THE LEFT MLG CAUSED BY A TREAD SEPARATION. AC WAS CARRIED TO THE HANGAR TO REPAIR THE FOLLOWING AFFECTED ITEMS: THE TORQUE LINK DAMPER, INBOARD FLAP, TRAILING EDGE LOWER FIXED PANEL, MLG FIXED DOOR, MLG WATER SPREAD DEFLECTOR, MLG FIXED DOOR FWD AND AFT RODS, MLG FITTING LOWER SURFACE, BREAK AFT HOSE QUICK DISCONNECT COUPLING. 2L72 4F4 FRTA6WE E2EA 20040213000332004021300033NM 2004 2 13 CALA0300726 120031231A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 A 3 INCH CRACK WAS FOUND IN LT FUSELAGE SKIN AT STA 727D, S23L DURING A WALKAROUND INSPECTION. THE SKIN WAS REPAIRED IAW ECRA 5330-03090. 2L72 4F RTA16WE 20030430001532003043000153 2003 4 30 SWAA030882 420030420A2565 GIRT BAR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030501002102003050100210EA 2003 5 1 ASOA03123 120030321A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 FLT 4425 - DURING A GROUND INSPECTION IN ATL, THE FORWARD EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR FLEX LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030501000712003050100071WP 2003 5 1 GTIA030198 120030217A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND MID PIT LONGERON 18L UPPER WEB BETWEEN STATION 598 AND 617 CORRODED. CUT OUT DAMAGED WEB. FABRICATED NEW WEB. INSTALLED NEW WEB REPAIR. (M) 2L72 4F RTA6WE 20030505000292003050500029NM 2003 5 5 2003UALA00300 120030319A2780 CONTROL UNIT BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE LE SLATS MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29609UA 21870 A/C RECEIVED EICAS MESSAGE. LEADING EDGE SLAT REMAINED IN EXTENDED POSITION. CLEARED BITE HISTORY FROM PSEU. CYCLED FLAPS AND COULD NOT DUPLICATE EICAS MESSAGE. 2L72 4F4 FRTA1NM E3NE 20030506002002003050600200NM 2003 5 6 ASAA0240031 120030129A52476550904 SKIN BOEING737 737490 1384715NM APU DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01796AS 28891 PAE - WHILE PERFORMING C-CHECK, FOUND DENT IN APU EXTERIOR DOOR SKIN 14 INCHES FROM FORWARD EDGE 4 INCHES FROM LEFT EDGE. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030506001972003050600197WP 2003 5 6 ASAA0380111 120030130A33501001191 LIGHT DOUG DC9 DC983 3022083WP FWD PAX ENTRY MALFUNCTIONED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01969AS 53063 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR ILLUMINATED WITH SWITCH TURNED OFF. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20030514001592003051400159EU 2003 5 14 RAIA00304116 120030417A30103D354701 PRESSURE SWITCH JETAIRJETSTMJETSTM4101 1500501EU DE ICE SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03569HK14345 41088 AIRFRAME DE-ICE FAULT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED CCT2 DE-ICE PRESSURE SWITCH, OPS CHECK GOOD. 2L72 4T RTA41NM 20030609000022003060900002EA 2003 6 9 COMA0360243 120030517A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01484CA 7702 DAMAGE TO A/C FUSELAGE UNDER CARGO DOOR, REPAIRED I/A/W REO NO. 601R-53-61-718. 2L72 4F RTA21EA 20030514002072003051400207NM 2003 5 14 03FDEA00664 120030501A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-111-01) ON TOP OF FRAME BS 720D, LBL 8-22 WL 156. REPAIRED PER EA 7-5310-69680 AND SRM 51-40-3. 2L73 4F RTA3WE 20030609001992003060900199 2003 6 9 HEEA086572 420030522A34578143902240B GPS SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 GPS LOSES RAIM. SHOP REPAIR. 1G72 3U H1NE 20030521001872003052100187NM 2003 5 21 AWXA200300538 120030415A533065458001133 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.4375 INCH CRACK WAS FOUND AT FASTENER HOLE ON SKIN OF L-1 DOOR CUTOUT, LOWER AFT CORNER BS 334, LBL 63. MAINTENANCE REMOVED CENTER SCUFF PLATE ATTACH ANGLE; HFEC INSPECTION INDICATED CRACKS ON ALL 3 LAYERS. TRIMMED OUT CRACK IN BEAR STRAP AND SKIN; PERFORMED HFEC TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER, TRIPLER AND FILLER; INSTALLED REPAIR PARTS, AND REINSTALLED CENTER SCUFF PLATE ATTACH ANGLE IAW AWA ER 03-5300-03126-SS1. 2L72 4F RTA16WE 20030522000202003052200020NM 2003 5 22 2003UALA00412 120030505A2750 FLAP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29788UA 26942 AIRCRAFT HAD FLAP DRIVE FAILURE INVOLVING PRIMARY AND SECONDARY SYSTEMS. CENTER ACE WAS REPLACED AS PRECAUTIONARY. DETAILED TESTS OF FLAP PRI CONTROL VALVE AND FLAP SECODARY MODES PASSED WITH NO FAULTS. 2L72 4F4 FRTT0001SE E46NE 20030619000842003061900084SW 2003 6 19 HEEA087218 120030609A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y214 51556 MAIN BATTERY WEAK. 1G71 3U H2SW 20030707001062003070700106WP 2003 7 7 UPS03840859 120030616A5712 RIB DOUG DC8 DC873F 302199FWP RIGHT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 785. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER I.A.W. SRM. 57-2-0 FIG.2 2L74 4F RT4A25 20030110000282003011000028EA 2003 1 10 COMA0360014 120030108A2750852D10011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA R/H MALFUNCTIONED A COMAL ABORTED APPROACH S AFFECT SYSTEMS APAPPROACH 1 SO01937CA14323 7044 FLIGHT 5878 FLAPS FAILED WHEN SELECTED TO 45 DEGREES.REPLACED THE R/H INBD FLAP ACTUATORS. 2L72 4F RTA21EA 20030127001572003012700157SW 2003 1 27 HEEA083687 120030115A6510206061432121 HOUSING BELL 407 407 1182206SW BLOWER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 TAIL ROTOR BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20030127002832003012700283NM 2003 1 27 03FDEA00025 120030115A5230 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D* NE CARGO DOOR CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 AFT NR 2 LWR CARGO DOOR CHAFING IN EXTERIOR SKIN 3-12 INCHES FROM FORWARD EDGE 0-3 INCHES FROM UPPER EDGE. REPAIRED IAW EA. 2L73 4F4 FRTA3WE E2EA 20030128000242003012800024GL 2003 1 28 HEEA083776 220030115A741223064130 IGNITER BOX BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH 53461 IGNITER BOX DELAYED LIGHT OFFS. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128000682003012800068SW 2003 1 28 HEEA083822 120030116A6230406010413117 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR CORRODED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03405PH 53207 MAIN ROTOR PITCH LINK HAS CORROSION ON TUBE ENDS NOT VISIBLE UNTIL PAINT REMOVED. 1G71 3U O H2SW 20030128002252003012800225NM 2003 1 28 AWXA200300037 120030103A5320655289412 FLOOR SUPPORT BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 YVR - MAJOR REPAIR - DURING C-14 CHECK 2 EACH .5 INCH CRACKS WERE FOUND ON FLOOR SUPPORT CHANNEL AT BS 540, BL 0. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT CHANNEL AT BS 540, FROM LBL 23 TO RBL 23; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT CHANNEL PER DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030204000912003020400091NM 2003 2 4 SWAA030150 120030121A57536546431280 FLAP BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD T/E FORE FLAP LOWER SURFACE CRACKED. REMOVED AND REPLACED FLAP ASSY PER MM 2L72 4F RTA16WE 20030204001682003020400168NE 2003 2 4 SWAA030094 220030115A7230CFM563 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 2 LEAKING A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29642WN 27715 858458 ODOR IN CABIN DURING RT A/C PACK SYS IN USE. TERMINATED FLT AT TPA FOR INSPECTION OF NR 2 ENG AND FOUND OIL LEAK AT 6 O'CLOCK POSITION IN COMPRESSOR SECTION. REMOVED AND REPLACED NR 2 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20030207001042003020700104NM 2003 2 7 03FDEA00060 120030121A2120 ODOR BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE CABIN DETECTED A FDEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25487FE 21490 LEFT PACK CAUSES FUMES IN COCKPIT WHEN SELECTED TO MOMENTARY WARM TEMP. TWO CREW MEMBERS NOTICED DULL HEADACHE AND ONE CREW MEMBER COMPLAINED OF BURNING EYES. RAN LEFT PACK WARM POSITION WITH NO FUMES OR OTHER DEFECTS NOTED PER B727- 200MM 21-55-000-5. OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20030207001302003020700130NM 2003 2 7 ZW0A0301505 120030201A3350408822101 BATTERY DOUG MD80 MD83 3023681NM CABIN DISCHARGED A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE139420D 49824 THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. 2L72 4F RT 20030212000702003021200070SW 2003 2 12 CA030117008 120030115A32601E9516 DOWNLOCK SWITCH SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP SWITCH FAILED W L ABORTED APPROACH N FALSE WARNING APAPPROACH 1 CA (CAN) ON APPROACH THE LT MLG FAILED TO INDICATE DOWN AND LOCKED, EMERGENCY EXTENSIONS WERE PERFORMED BUT GEAR STILL FAILED TO INDICATE DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. A SUBSEQUENT INSPECTION COULD NOT DUPLICATE THE DEFECT, LT I/B DOWN LIMIT SWITCH. THE LANDING GEAR TESTED EXTENSIVLY AND THE AIRCRAFT RETURNED TO SERVICE. THE SWITCH IS AN IMPROVED SWITCH INSTALLED PER S/B 32-025.IT IS OUR EXPERIENCE THAT THE AIRCRAFT EQUIPPED WITH THE MAGNETIC LANDING GEAR INDICATOR SYSTEMS ARE PROBLEMATIC WHEN OPERATED IN COLDER TEMP S. 2L72 4T4 TRTA8SW E4WE 20030304000912003030400091NM 2003 3 4 DLM88030168 120030220A5350591009113 RADOME DOUG MD88 MD88 3023688NM FORWARD CRUSHED A DALAK NONE C F.O.D. APAPPROACH 1 SO27919DL 49584 BIRD STRIKE ON APPROACH RWY19R APPROX 400 FT AGL 126 KTS REPLACED RADOME WITH PART BORROWED FROM A/A 2L72 4F RTA6WE 20030625001122003062500112NM 2003 6 25 F3LA200300095 120030303A5754 SKIN BOEING737 73736E 138443ANM NR 1 SLAT CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 3265 25159 DURING C-3 CHECK, INSPECTION REPORTED SURFACE CRACK ON NR 1 SLAT, INBD OF SLAT ACTUATOR. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 57-45-01, 57-43-01 AND 51-30-2. 2L72 4F RTA16WE 20030316000022003031600002SO 2003 3 16 C2XA03SH054 120030316A530014532606017 TRACK EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 SHV DURING C CHECK LEFT HAND UPPER SEAT TRACK NUMBER 4 WHERE FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED TRACK IAW EMB 135 AMM 53-01-00. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030317000272003031700027NM 2003 3 17 03FDEA00160 120030220A5750ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP, OUTBOARD AFT HINGE, OUTBOARD BORE FITTING, FOUND CORROSION. TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP, OUTBOARD HINGE BRACKET REPAIR CARRIED-OUT IAW EA 1-5750-67572. 2L73 4F4 FRTA22WE E13NE 20030318000012003031800001NM 2003 3 18 SWAA030579 120030314A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030318002162003031800216NM 2003 3 18 AWXA200300286 120030117A53306573746 PANEL BOEING737 737277 1384570NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW0 0 22647 LCQ - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON KEEL BEAM PANEL BETWEEN THE L/H AND R/H WHEEL WELLS BS 600 TO 724. MAINTENANCE REMOVED EXISTING DOUBLER; PERFORMED NDT INSPECTION OF CRACK; REPLACED BLIND FASTENERS WITH SOLID FASTENERS; FABRICATED REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 53-30-3, FIG. 40, PG. 151. 2L72 4F RTA16WE 20030319001042003031900104NM 2003 3 19 TSAA0333023 120030204A33201000679 LIGHT BOEING737 73776N 13844CHNM PAX CABIN INOPERATIVE A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13743AL 28654 REPLACED FORWARD ENTRY DOOR EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20030320000482003032000048NM 2003 3 20 USAASB03018 120030205A3260189929 SENSOR BOEING737 7373B7 1384580NM RT MLG W/W MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19392US 23314 PIT - FLT 231 - AFTER TAKEOFF, CREW REPORTED LANDING GEAR LEVER WOULD NOT MOVE TO RETRACT GEAR. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED, REPLACED AND ADJUSTED THE S106 AIR SAFETY SENSOR PER MM 32-09-01. ALSO, REMOVED AND REPLACED THE M991 PRINGED CIRCUIT BOARD. ACCOMPLISHED GEAR SWING PER MM 32-32-00. OPS CHECK GOOD. 2L72 4F RTA16WE 20030417000532003041700053NM 2003 4 17 UPS03440092 120030125A3350 LIGHT BOEING747 747123 1384873NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 INSPECTION TYPE: PFLT, MAIN ENTRY DOOR JAMB EMERGENCY EXIT LIGHT INOPERATIVE. CHECKS NORMAL, UNABLE TO DUPLICATE. 2L74 4F A20WE 20030417001132003041700113EU 2003 4 17 MALA030144 120030124A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15520XJ E2345 DURING C-CHECK IN CVG, NR 4 SEAT TRACK HAS CORROSION BETWEEN FRAME 18-20. MAINTENANCE REPAIRED DAMAGE IAW EO A53026. A/C RELEASE DATE 1/30/03. 2H74 4F RTA49EU 20030418000382003041800038WP 2003 4 18 MWEA030073 120030212A5320593643613 CLIP DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LONGERON 11 AND IT'S CLIP ARE DAMAGED FORWARD RIGHT OF AFT PRESSURE BULKHEAD. REMOVED CLIP AND DAMAGED SECTION OF LONGERON. AFTER REMOVAL OF SHOVEL FOUND LONGERON 11 NOT DAMAGED. INSTALLED SHOVEL CLIP. 2L72 4F A6WE 20030421001682003042100168SW 2003 4 21 2003F00220 120030102A5270 WARNING LIGHT FRCHLDSA227 SA227DC 3377521SW CARGO DOOR ILLUMINATED A BSAAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM05453LA DC852B FLT 1411 - OLM - CARGO DOOR LIGHT CAME ON DURING CLIMB. CREW RETURND TO STATION. NO MECHANICAL PROBLEMS WERE NOTED. DOOR WAS OPENED, SHUT AND RELATCHED. NO PROBLEM WAS NOTED. FLIGHT WAS CONTINUED WITH NO FURTHER PROBLEMS. (M) 2L72 4T RTA18SW 20030422001032003042200103SO 2003 4 22 SIMA200307005 120030305A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706PG 145194 ABI - DURING A IMBV INSPECTION, THE OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT 4 INCH SECTION OF DAMAGED OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, TWO SHIMS. REPAIR DONE IAW EMB SRM (SRM EMB 145/1142 REV 20) CHAPTER 53-21-10 FIG 202. (M) 2L72 4F RTT00011AT 20030801000822003080100082SO 2003 8 1 11871 120030731A532014521725015 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV DURING C CHECK SERVICE DOOR AFT SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED SECTION IAW EMB 145 SRM 53-21-10 AND EC 5320-01089. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030801000982003080100098EA 2003 8 1 COMA0360314 120030705A7910 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE LOW A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01506CA 7793 FLIGHT 5560 RT ENGINE OIL PRESSURE LOW AND FLUCTUATING. SERVICED OIL TANK WITH 2 1/2 QUARTS OIL. 2L72 4F RTA21EA 20030424000092003042400009SO 2003 4 24 SWIA200311833 120030315A2797 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAP ACTUATORDAMAGED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07190SW 120050 FLAP CONTROL FAULT INDICATED FOR INBOARD FLAPS. FLAPS WOULD NOT RETRACT ON THE GROUND. REMOVED AND REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR WITH A NEW PART. OPS CHECK OF FLAPS PERFORMED SATISFACTORY. P/N ON MS3476L12-10S. 2L72 4T4 TRTA31SO E20NE 20030723001182003072300118NM 2003 7 23 DL73K030507 120030603A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 A 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 525 JUST ABOVE STRINGER 16L RUNNING ALONG THE EDGE OF THE INTERNAL BONDED WAFFLE DOUBLER. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 385203-14. 2L72 4F RTA16WE 20030825000922003082500092NM 2003 8 25 03FDEA01232 120030808A5720ARC41252 STOP FITTING DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 AFT RT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED 2C LENGTH CRACK APPROX. RT WING OUTBOARD FLAP INBOARD STOP FITTING CARRIED OUT REPAIR AS PER EA 1-5750-71804 (WINGS - TRAILING EDGE FLAPS - LT AND RT OUTBOARD FLAP SECONDARY STOP BOSS REPAIR). 2L73 4F RTA22WE 20030826000792003082600079EU 2003 8 26 31440707031 120030707A6730SG5083 SERVO SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1B 6OO30NE FLIGHT CONTROL LEAKING E S4WAK NONE O OTHER ININSP/MAINT 1 WP075226R2196 3144 22043 SERVO LEAKING. 1G71 3U3 U H9EU E19EU 20030829001852003082900185NM 2003 8 29 SWAA031796 120030808A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 895 AT STR 14R AND BS 866 AT STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030725000052003072500005NM 2003 7 25 AWXA200300751 120030625A53206545834551 CHANNEL BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1.1875 INCH CRACK WAS FOUND ON INTERCOSTAL AT BS 327, LBL 46, WL 208.5. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 327, LBL 46, WL 208.5; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 9-11. 2L72 4F RTA16WE 20030807000272003080700027EU 2003 8 7 USAABA03024 120030621A2400755017B IDG AIRBUS330 A330323 3930335EU RT ENGINE INOPERATIVE A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19675US11517 0370 CREW RECEIVED THE ECAM WARNING 'ELEC GEN 2 FAULT'. THE GENERATOR WOULD NOT RESET. CREW ATTEMPTED TO START THE APU. THE APU WOULD NOT START AT FL360 OR FL300. APU FINALLY DID START AT 14,000 FEET. MAINTENANCE REPLACED THE GCU, BUT FINAL FIX WAS TO REPLACED THE IDG. AFTER EXTENSIVE T/S THE APU WAS REPLACED. (M) 2L72 4F RTA46NM 20030908002642003090800264CE 2003 9 8 AMWA25 120030724A53441294400493 HINGE BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07131YV UE131 DURING ABC CHECK, THE CARGO DOOR HINGE WAS FOUND CRACKED. REPLACED HINGE IN ACCORDANCE WITH BEECH SRM 52-90-01. NO TEAR DOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030814001322003081400132NM 2003 8 14 0301186717 120030630A5312 BULKHEAD BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING L-CHECK FOUND CRACK ON RT WING LANDING GEAR PRESSURE DECK CANTED BULKHEAD AT BS 1243 RBL 75. REPAIRED PER EA 67-165075. 2L74 4F A20WE 20030730000862003073000086NM 2003 7 30 ABXA030278 120030616A335020131A BATTERY PACK BOEING767 767281 1385109NM CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23767AX 22785 DURING MAINTENANCE INSPECTION, FOUND BATTERY PACK DEAD. REPLACED BATTERY PACK IAW 33-51-00-2. 2L72 4F RTA1NM 20030730001332003073000133NM 2003 7 30 MEX2003224 120030612A3241392492 SERVO VALVE DOUG MD88 MD88 3023688NM ANTI-SKID SYS FAILED A ASMFO OTHER J WARNING INDICATION UKUNKNOWN 1 SW23169PL 53175 FLT 501 - MEX-OAX - AIRCRAFT ARRIVED WITH CAPTAIN REPORT TIRE NR 4 OF MLG WITH DAMAGE. THE TIRE NR 4 WAS REPLACED BUT ANTI-SKID NO TEST. EXTERIOR DOUBLER SERVO VALVE WAS REPLACED IAW MM 32-43-03, ALL TESTS CORRECT. (M) 2L72 4F RTA6WE 20030926000402003092600040NM 2003 9 26 XE42003F00000 120030703A5534591413811 BRACKET BOEING717 717200 1383700NM RUDDER LIMITER BROKEN B XE4RO OTHER O OTHER NRNOT REPORTED 1 SO19937AT 55091 DURING ROUTINE INSPECTION OF THE TAIL COMPARTMENT, RUDDER LIMITER BRACKET ASSEMBLY, PN 5914138503 WAS FOUND BROKEN. THERE WAS NO INBOUND REPORT OF RUDDER LOAD FEEL OR HANDLING PROBLEMS ON THE FLIGHT. SUSPECT CONNECTING LINKAGE (ITEM NR 105) MOVED WITH RIGH PIN INSTALLED, CAUSING BRACKET (ITEM NR 85) TO BRAKE. 2L72 4F TRA6WE 20031002001302003100200130NM 2003 10 2 AWXA200301041 120030815A5754654642389 SKIN BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A .1250 INCH CRACK WAS FOUND ON NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR AT WBL 230 LT. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR ASSEMBLY AT WBL 230 LT IAW B737-200 SRM 51-30-02, PARA B & E. 2L72 4F4 FRTA16WE E2EA 20031006000032003100600003EA 2003 10 6 COMA0360406 120030907A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01472CA 7667 FLIGHT 5921 FLAPS FAIL CAUTION MESSAGE. LT AND RT BPSU OUT OF RIG - ADJUSTED RIGGING. 2L72 4F RTA21EA 20031006000212003100600021EU 2003 10 6 MALA030412 120030812A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK IN CVG, NR 1 SEAT RAIL CORROSION. MAINTENANCE REPAIRED IAW EO NR A53026, REFER TO 409 NR 190258 FOR DETAIL. A/C RELEASE DATE 9/2/03. 2H74 4F RTA49EU 20031006000802003100600080CE 2003 10 6 AMWA53 120030903A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07167YV UE167 WHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLNAGE AT CANTED STAB. STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE RT SIDE AT THE FWD SIDE,. REPAIRED CRACK TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-91, 51-70-03 2L72 4T RTA24CE 20031007000962003100700096NM 2003 10 7 SWAA031994 120030907A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW NR 7. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20031015000582003101500058NM 2003 10 15 USAASB03157 120030831A33501012623 LIGHT BOEING737 737301 1384611NM SEAT 10 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 FOUND EMERGENCY EXIT LIGHT AT SEAT 10 ABC INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA16WE 20031021002162003102100216SO 2003 10 21 SIMA200325304 120030901A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21717AE 145272 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND INSTALLED A NEW SILL. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, 51-40-02 AND EMB REPAIR STATEMENT IC2003-145/0818. (M) 2L72 4F RTT00011AT 20030909001562003090900156 2003 9 9 BAQA088908 420030829A34215000B36 INDICATOR BEECH 100 100BEECH 1152916CE ATTITUDE GYRO INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 509 B144 CO PILOTS ATTITUDE INDICATOR INOP. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20030909002682003090900268EU 2003 9 9 RAIA00308226 120030829A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU CABIN BROKEN A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03552HK 41057 MX-STL- MAIN DOOR LOWER EMERGENCY LIGHT INOP. REPAIR BROKEN WIRE AT LIGHT ASSEMBLY. 2L72 4T RTA41NM 20030910000472003091000047 2003 9 10 HEEA088917 420030812A2210412074030101 AMPLIFIER BELL 412 412 1182202SW INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 ISOLATION AMPLIFIER CAUSES ADI TO TILT 30 DEGREES LEFT QUADRANT. 1G72 4U H4SW 20031028000372003102800037NM 2003 10 28 03269410 120030926A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27410FJ 3165 DURING INSPECTION THE EMERGENCY PATH LIGHTING AT ROWS 7 THRU 9 WERE REPORTED INOPERATIVE. MAINTENANCE PERSONNEL ADJUSTED THE PATH LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031027000382003102700038NM 2003 10 27 CALA0300557 120030925A5320 PAN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE LAVATORY FLOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND RT AFT LAV PAN CORRODED AT STA 1028, RBL 18. A NEW LAV PAN WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20031023000752003102300075CE 2003 10 23 DXTA200300097 120030822A32307093011 CONTROL UNIT CESSNA650 650 2076802CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07789QS2172 6507089 AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT, THE LANDING GEAR HANDLE WOULD NOT MOVE UP. ACCOMPLISHED AIR TURNBACK TO DSM, AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR CONTROL UNIT IAW CESSNA 650 MM CHAPTER 32-30-01. OPERATIONAL CHECK OF SYSTEM GOOD IAW CESSNA 650 MM CHAPTER 32-30-01. 2L72 4F A9NM 20031028000672003102800067 2003 10 28 751PA0023 420030924A2230 CONTROL UNIT BOEING757 757200 1384950NM FLAP/SLATS MALFUNCTIONED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05751PA 23928 AUTO THROTTLE DISCONNECTS WHEN CAPTURING ALTITUDE EPR & SPD SWITCHES WON'T ENGAGE. PLACED ON MEL 22-11-4. 09/26/2003: REPLACED NR 1 FLAP/SLAT ELECTRIC UNIT & OPS CHECKED OK PER MM 22-11-00. REMOVED MEL 22-11-4. 2L72 4F RTA2NM 20031120000812003112000081EU 2003 11 20 MALA030456 120031009A5311 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN CWA, CORROSION FOUND ON FRAME 294 RBL 24, BLENDED OUT DAMAGE, FABRICATED DOUBLER IAW EO NR 53102. A/C RELEASE DATE 10/12/2003. REFER LOG PAGE 195763 FOR DETAIL. 2L72 4T4 TRTA52EU E8NE 20031120001292003112000129NM 2003 11 20 AWXA200301454 120031106A52105079453 SKIN BOEING737 7373G7 1384595NM PAX DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-15 CHECK A .5625 INCH CRACK WAS FOUND ON L-1 DOOR INNER SKIN AT FORWARD END OF HANDLE MECHANISM BS 326. MAINTENANCE CUT OUT CRACK IN L-1 DOOR INNER SKIN; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 52-00-01 FIG 202 PG 203-204. 2L72 4F RTA16WE 20040114000482004011400048NE 2004 1 14 DLM88030962 220031028A7250JT8D219 TURBINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED A DALAAF UNSCHED LANDING ACTIVATE FIRE EXT. R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO27973DL29641 53241 725945 ON TAKEOFF CLIMBING THRU 180, RIGHT ENG LOST POWER WITH NO FIRE INDICATION. REDUCED THRUST AND LANDED. UPON LANDING FIRED BOTH BOTTLES DUE EGT RISE. FOUND ON INSPECTION RIGHT ENG TURBINE FAILURE. REPLACED ENGINE. 2L72 4F4 FRTA6WE E9NE 20040115001232004011500123NM 2004 1 15 03FDEA02100 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 361DL. LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACK LOCK BOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040329001212004032900121 2004 3 29 2003UALA00876 420031119A344206650080405 TRANSCEIVER BOEING747 747422 1384935NM PWA 4056 PW4056 NE WX RADAR FAILED A UALAHC DEACTIVATE SYST/CIRCUITSABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29122UA 29168 WINDSHEAR WARNING (NO AURAL) CAME ON ABOUT 80 KTS ON T/O ROLL. RTO DISENGAGED AT 50 KTS. *S/D* BOTH WX RADAR R-T UNITS WERE REPLACED. BOTH UNITS PASSED ALL TESTS WHEN SUBSEQUENTLY TESTED IN THE SHOP. ONE OF THE TWO UNITS HAD A QUALIFIER FAULT STORED IN FAULT HISTORY THAT MAY HAVE CAUSED THE WINDSHEAR WARNING. 2L74 4F4 FRTA20WE E24NE 20031110000742003111000074CE 2003 11 10 AMWA71 120031105A553111464000057 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07165YV UE165 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGES AT CANTED STAB STA 69.184 WAS FOUND CRACKED, ONCE ON THE LEFT AND ONCE ON THE RIGHT SIDE. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20040112000752004011200075SO 2004 1 12 C2XA03IA113 120031221A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT AT THE COCKPIT ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM. 2L72 4T RTT00011AT 20031120000552003112000055NM 2003 11 20 QXEA200301243 120030929A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 NR 7 SEAT TRACK REQUIRES REPLACING. REPAIRED IAW DHC-8 SRM 51-40-11, 51-30-26 AND RD 8-53-1102. 2H72 4T RTA13NM 20031121000392003112100039EA 2003 11 21 HNAA0300068 120031102A3260858601 PSEU DHAV DHC8 DHC8311 1386006EA MLG DEFECTIVE A HNAAO OTHER J WARNING INDICATION CRCRUISE 1 EA07343EN2166824 340 ALL THREE AMBER LIGHTS ILLUMINATED THREE TIMES IN FLIGHT. REPLACED PSEU. 2H72 4T RTA13NM 20031126000942003112600094SO 2003 11 26 C2XA03CL178 120031023A335078241 INVERTER EMB 145 EMB145ER 3260211SO CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715932 145015 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGNS IN AISLE OVER EXIT DOORS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040114001722004011400172EU 2004 1 14 MALA030474 120031016A33506013211 BATTERY PACK SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A MALAK NONE L NO TEST NRNOT REPORTED 1 GL1576XJ 340A076 SEVERAL CABIN EMERGENCY LIGHTS WOULD NOT COME ONLINE. MAINTENANCE REPLACED 22LN AND 24LN BATTERY PACKS PN 61-0478-9 SN/OFF ELB085, SN/ON ELB502, POWER SUPPLY PN 60-1321-1, SN/OFF 18246 SN/ON 14582. OPS CHECKS GOOD. 2L72 4T RTA52EU 20040115000312004011500031NE 2004 1 15 SW07200300010 220030902A72304120T01P02 COMPRESSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE FOD G FDKAEC ENGINE SHUTDOWN ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW07507MJ1610 10077 GEE965376 THE CREW REPORTED A COMPRESSOR STALL DURING TAKEOFF. THE ENGINE WAS REMOVED AND REPLACED. 2L72 4F4 FRTA21EA EOOO63EN 20040115000972004011500097WP 2004 1 15 03FDEA02283 120031227A5753ARC2512502 HINGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 COMPLY WITH EA 8-5740-73863. WINGS- RIGHT INBOARD FLAP, REWORK OF CORROSION IN AFT HINGE ASSY PIVOT BORE. CLOSING ACTION ON 12/24/03. ON N/R S00032. COMPLIED WITH EA 8-5740-73863. 2L73 4F A22WE 20031216000022003121600002NM 2003 12 16 AWXA200301472 120031106A5320693535214 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 639, STR 2 RT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 639, STR 2 RT IAW B737-300 SRM 51-40-02, PG 1, 38 & 45 FIG 8 & 12. 2L72 4F RTA16WE 20031218001132003121800113EU 2003 12 18 2003UALA00902 120031125A5522 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT ELEVATOR CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29404UA 450 LEFT ELEVATOR UPPER SKIN HAD ONE AREA OF WATER INGRESS. MAJOR REPAIR ACCOMPLISHED. DAMAGE REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205, SHEET 3. 2L72 4F4 FRTA28NM E40NE 20031217001782003121700178NM 2003 12 17 DHL2003720011 120031124A3350 LIGHT BOEING727 727228 1384083NM PAX DOOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01720DH 19544 LT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW 727 M/M 33-50-111. OPS CHECKED SERVICEABLE. 2L73 4F RTA3WE 20031218001412003121800141SO 2003 12 18 C2XA03TY202 120031203A553014520736003 SUPPORT FITTING EMB 135 EMB135ER 3260203SO VERTICAL STAB DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727506 145206 DURING A SCHEDULED 2C INSPECTION THE LT AND RT VERT STAB SPHERICAL BEARINGS HAD AXIAL PLAY. MAINT REMOVED THE SPHERICAL BEARINGS, REAMED AND INSTALL THE 1ST OVERSIZE BUSHINGS, REINSTALL BEARINGS AND PERFORMED A DIEHEDRIAL CHECK IAW EC5510-01045; EC5510-01069 AND EMB 135 AMM 51-50-01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20031223000562003122300056NM 2003 12 23 SWAA032677 120031207A3350610478 POWER SUPPLY BOEING737 7373T5 1384608NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT RT SIDE, SECOND FROM AFT END. REMOVED AND REPLACED POWER SUPPLY ASSY PER MM. 2L72 4F RTA16WE 20040105001502004010500150CE 2004 1 5 AMWA108 120031222A553111464000061 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07139ZV UE139 DURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON RT SIDE ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46. 2L72 4T RTA24CE 20030917000842003091700084 2003 9 17 S2YA03026 420030807A34177014700919 ADC DORNERDO32 DO328300 NM COCKPIT INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13358SK5651 3188 FLT 2324 - MKE-RDU - DURING FLIGHT, THE NR 2 AIR DATA COMPUTER DROP OFF LINE. THE CREW PERFORMED AN AIR TURNBACK TO MKE AND MADE AN OVERWEIGHT LANDING. MAINTENANCE REPLACED THE ADC AND OPS CHECKED THE SYSTEM WITH NO DEFECTS NOTED. MAINTENANCE ALOS PERFORMED AN OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS NOTED. (M) 2H72 4T RTA55NM 20031009000662003100900066 2003 10 9 SWIA200312390 420030908A3497W110083120 WIRE EMB 120 EMB120ER 3260203SO AOA RELAY DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07189SW 120048 LEFT AOA SENSOR FAILED FFOD TEST. REPAIRED DAMAGED WIRES W110-0831-20 GOING TO RELAY K0551-X1 AND WIRE W110-1125-14 GOING TO RELAY K091-AZ . OPS CHECK GOOD IAW MM 30-32-00. 2L72 4T RTA31SO 20040105001742004010500174NM 2004 1 5 AWXA200301618 120031207A53206546812 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT BS 951-964, LBL 45. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 951 TO BS 964, LBL 45; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, FIG 12, PG 1 & 45. 2L72 4F RTA16WE 20040109000232004010900023NE 2004 1 9 MEX2003400 220030829A732078360018072 EEC BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23301AM450 30045 AIRCRAFT RETURN TO PLATFORM, DURING RT ENGINE START WITHOUT EPR AND EGT INDICATIONS ON PRIMARY DISPLAY AND EGT INDICATION ONLY ON SECONDARY DISPLAY WITH CIRCUIT BREAKER THROWN AWAY P6, M16,17,18,22,23 AND 24. DURING REVISION WERE DETECTED EICAS MESSAGES P ADC R/EEC, P ADC I/EEC, AND EPCS PAGES P 273-14, P273-15, 16,17, 18, 19, 20. R ENG OIL COOL AND R ENG PRIM CONT. THE RT ENGINE EEC WAS REPLACED IAW MM 73-21-04, ALL TESTS CORRECT. THE RT ENGINE WAS STARTED WITH ALL INDICATIONS CORRECT.(K) 2L72 4F4 FRTA2NM E17NE 20031202000612003120200061NM 2003 12 2 USAASB03179 120031012A2701 CONTROL COLUMN BOEING737 737301 1384611NM COCKPIT STIFF A USAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA19563AU 23551 EN ROUTE FROM CLT TO RDU, CREW REPORTED STIFF FLIGHT CONTROLS, ELEVATOR AND AILERONS. FEELS SOMEWHAT LIKE MANUAL REVERSION. DURING FLARE ON FINAL, THE CONTROL COLUMN BOUND FOR A MOMENT AND THEN BROKE FREE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED VISUAL INSPECTION OF ELEVATOR SURFACES, HINGES AND TABS. PERFORMED VISUAL INSPECTIONS OF ELEVATOR CABLES, PULLEYS, MECHANICAL AND HYDRAULIC COMPONENTS IN TAIL SECTION AND UNDER COCKPIT FLOOR. OPERATED ELEVATORS MANUALLY AND HYDRAULICALLY FERRY FLIGHT FROM RDU TO CLT. MAINTENANCE FERRY FLIGHT ARRIVED IN CLT WITH NO PROBLEMS NOTED. INBOARD FLIGHT CREW REPORTED NO ABNORMAL FLIGHT CHARACTERISTICS. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20031202000082003120200008NM 2003 12 2 ASAA0310451 120030515A5315BAC15061702 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 543-602, BUTTOCK LINE 0 CORRODED. REMOVED CORROSION AND REPAIRED PER EA. (M) 2L72 4F A16WE 20031203000932003120300093SW 2003 12 3 2003F00628 120030630A8200 WATER INJECTION SWRNGNSA227 SA227AC 8780603SW ENGINE MALFUNCTIONED A BSAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM05160MC 733B CAWI DID NOT FIRE. INSUFFICIENT AWI FLOW, HOT WEATHER OPS, OAT WAS APPROXIMATELY 100 DEGREES FARENHEIT. ADJUSTED CAWI FLOW VALVE OUT ONE FULL TURN. GROUND RUN CHECK GOOD WITH 30 PERCENT RISE IN TORQUE. (M) 2L72 4T RTA8SW 20031203001592003120300159WP 2003 12 3 AALA20031039 120030920A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21485AA 49678 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 8 THROUGH 12. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040121000672004012100067EA 2004 1 21 ASOA03597 120031122A5200601R3807413 ANCHOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040123000342004012300034EU 2004 1 23 KBM2003F00087 120031031A243223761 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE MASTER UNSERVICEABLE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 BATTERY VOLTAGE DROPS TO 12V DURING START WITH SLOW ACCELERATION. INSTALLED SERVICEABLE BATTERY. 1G71 3U3 U H9EU E19EU 20031204001532003120400153EA 2003 12 4 PNSA031002 220031018A7414103493101 MAGNETO PIPER PA32 PA32301 7103207SO LYC O540 IO540K1G5 41532EA ENGINE FAILED E PNSAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL038327S85 85 328106039 L1020648A DEPARTED DLG AT APPROX 250 AGL ENGINE BEGAN RUNNING ROUGH AND LOST PARTIAL POWER. AIRCRAFT MADE UNEVENTFUL LANDING AT AIRPORT. MAINT FOUND RIGHT MAGNETO CAUSED PROBLEM. MAGNETO REPLACED AIRCRAFT RETURNED TO SERVICE. 1L71 3O3 O A3SO 1E4 20031204000852003120400085WP 2003 12 4 UPS03841393 120031012A5310 DOOR FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: ASV, CRACK IN FUSELAGE DOOR JAM, PIT 31. CRACK STARTS AT JAM GOES TO FIRST ROW OF RIVETS AND INCLUDES SECOND LAYER OF SKIN, LOWER AFT CORNER. *S/D* REMOVED DAMAGE, FABRICATED DOUBLER AND TRIPLER, INSTALLED REPAIR PER SRM 53-02-00-0. 2L74 4F RT4A25 20031208000562003120800056EU 2003 12 8 03FDEA01793 120031023A54102442302541 STRUCTURE AIRBUS300 A300F4605R 3930327EU NR 1 & 2 PYLON CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25660FE 759 COMPLY WITH EA 6-5410-73845 PYLONS/NACELLES - NR 1 AND NR 2 ENGINE CORE COWL CHAFING REPAIR. COMPLIED WITH EA 6-5410-73845 PYLONS/NACELLES NR 1 AND NR 2 ENGINE CORE COWL CHAFING REPAIR. 2L72 4F RTA35EU 20031209001162003120900116NM 2003 12 9 VNAA0310018 120031022A7603 POWER LEVER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE FAILED A VNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07442JS 3060 DURING TAKEOFF, THE CREW EXPERIENCED A LEFT HAND POWER LEVER BEING STIFF AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND LUBED THE POWER LEVER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040126000382004012600038SW 2004 1 26 HEEA087809 120030613A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P12213 33012 SEPARATION ON THE IB ABRASION STRIP ON THE TOP SURFACE NEAR THE IB END. THE LOWER EROSION SHIELD IS TORN ON THE IB END. SENT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20031209002222003120900222NM 2003 12 9 CALA0300618 120031102A5512 SKIN BOEING737 737524 1384721NM HORIZONTAL STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714628 27532 INSPECTION FOUND RT HORIZONTAL STABILIZER LOWER SKIN GOUGED AT STAB STA 111. THE GOUGED AREA OF SKIN WAS REMOVED AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 55-10-01, FIGURE 207. 2L72 4F RTA16WE 20030919000822003091900082WP 2003 9 19 ARWA20030709 120030731A323056165545503 CYLINDER DOUG DC8 DC863F 302198FWP RT MLG INOPERATIVE A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO19661AV 45969 AFTER LANDING, LOST ALL HYDRAULIC FLUIDS. FOUND RT BOGIE TRIM CYLINDER IAW MM 32-33-1 ALTERNATE METHOD. OPERATIONAL CHECK NORMAL. 2L74 4F 4A25 20030922000032003092200003 2003 9 22 IF12003F00000 420030722A34617003974905 COMPUTER GULSTMG1159 GIV 3980115SO RROYCETAY TAY6108 NE NR 1 FAILED E IF1AO OTHER O OTHER NRNOT REPORTED 1 EA23614RD3951 1006 FLIGHT COMPUTER, NR 1 POSITION, FAILED. 2L72 4F4 FRTA12EA E25NE 20030923001412003092300141NM 2003 9 23 PCAA0308101 120030821A712087110021003 STRUT DHAV DHC8 DHC8102 2809003NM RT ENGINE MOUNT BROKEN A PCAAK NONE O OTHER ININSP/MAINT 1 EA13828EX 392 DURING AN -A- LEVEL INSPECTION, THE RT ENGINE INBOARD AFT HORIZONTAL MOUNT STRUT ASSY WAS FOUND TO BE BROKEN. THE AFT HORIZONTAL MOUNT STRUT ASSY WAS REPLACED, AND AIRCRAFT HAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20030925000402003092500040 2003 9 25 AALA20030764 420030710A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21669AA 25334 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS NEEDING REPLACED. REPLACED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030923001082003092300108WP 2003 9 23 DHL2003604724 120030620A573097510822 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT INNER WING LE SLANT PANEL UPPER CAP SHOWS CORROSION BETWEEN XFS.93.000 AND XFS.107.500, REPAIR DOUBLERS. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-2-1 FIG.37, SRM 57-3-3 FIG.2. REMOVED CORROSION ON UPPER CAP IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG.37. REMOVED CORRODED UPPER CAP IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CLEANED AREA AND APPLIED PRC ON FAYING SURFACES IAW SRM 51-1-12 PG.1. INSTALLED NEW UPPER CAP WITH NEW FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. FOR LEAK CHECK SEE NR 3824. 2L74 4F RT4A25 20040204000352004020400035NM 2004 2 4 DHL2003751012 120031016A3350 LIGHT BOEING727 727264 138408MNM PWA JT8 JT8D* NE CABIN DISLODGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01751DH 22982 EMERGENCY EXIT LIGHTS ABOVE MAIN ENTRY DOOR FELL OUT. RESECURED EMERGENCY EXIT LIGHTS OVER MAIN ENTRY DOOR IAW M/M 33-50-01. OPS CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040206000282004020600028 2004 2 6 SIMA200334101 420031204A22103621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO INOPERATIVE A SIMAO OTHER J WARNING INDICATION CRCRUISE 1 SW21835AE 145634 ORD - FLT 3967 - DURING CRUISE FLIGHT CREW REPORTED A MAIN AND BACKUP TRIM INOPERATIVE WARNING. MAIN SYSTEM WAS RESTORED BY RESETTING BREAKER. BACKUP TRIM WOULD NOT RESTORE. MAINTENANCE LUBRICATED THE BACKUP TRIM SWITCH AND DRAINED THE NR 1 AND 2 PITOT SYSTEM IAW EMB MM. THE HSCU WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCARFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040301000292004030100029EU 2004 3 1 PG92004F00008 120031110A6230 BUSHING UROCOPEC130 EC130B4 8680989EU SCISSOR LINK SEIZED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19130PH465 S2493 3670 SCISSOR LINK HAS A SEIZED BUSHING. (RMA NR R045786) (K) 1G72 3U H9EU 20040524000912004052400091GL 2004 5 24 KBM2004F00105 220031217A732123070606 FUEL CONTROL BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE OUT OF ADJUST E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 FUEL CONTROL COULD NOT ADJUST. REMOVED AND REPLACED. 1G71 3U3 U H2SW E4CE 20040510002872004051000287NM 2004 5 10 2003UALA00825 120031029A2560BACR13CE2 RELAY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY EXIT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29675UA 29243 LT OVERWING EXIT FAILS SQUIB-SPOILER TEST. SQUIB FAILED TEST DUE TO INTERMITTENT RELAY K839. REPLACED RELAY AND SQUIB TESTED OK. RELAY WAS PART NUMBER 3SAH1326A2 OR BACR13CE2 . 2L72 4F4 FRTA1NM E24NE 20040713001452004071300145NM 2004 7 13 AMTA200301532 120031229A335020131A BATTERY PACK BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11523AT 30232 L1 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK NR 731 POWRER SUPPLY IAW MM 33-51-07. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030929000462003092900046NM 2003 9 29 03FDEA01406 120030903A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25275FE 22040 LT KEEL BEAM AT STA 740 HAS DAMAGED HOLE DUE TO A SEIZED FASTENER IN KEELBEAM. REMOVED AND REPLACED DAMAGED LT KEELBEAM STA 740 IAW FED EX EA 7-5330-54955, DWG 65-54577-21, AND SRM 53-30-3 FIG. 3. LEAK CHECK GOOD ON DISTRIBUTION DUCTS. REMOVED FOR ACCESS IAW FED EX MM 36-00-000-5 COMPLIED WITH FED EX EA. 7-5330-54955. 2L73 4F RTA3WE 20040902001592004090200159EU 2004 9 2 2004F00262 120031014A3260 WARNING LIGHT AIRBUS320 A320233 3930329EU NLG DOOR ILLUMINATED A RJEFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23457TA 902 DURING TAKEOFF, THE LANDING GEAR DOOR NOT CLOSED INDICATION WAS SHOWN AND THE LANDING GEAR UPLOCK SYSTEM OF THE NOSE LANDING GEAR SYSTEM HAD AN INCORRECT INDICATION OF THEIR POSITION IN THE COCKPIT INSTRUMENTS. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAL STATION, MAINTENANCE TECHNICIANS PERFORMED INSPECTION OF THE NOSE LANDING GEAR AS PER AMM 32-31-00-810, INSPECTION OF SENSORS 24 GA AND 25 GA PER AMM 32-31-00-720 WAS PERFORMED AND NO DISCREPANCY WAS FOUND. ALSO, THE PRESSURE OF THE NOSE LANDING GEAR SHOCK ABSORBER WAS CHECKED PER AMM 12-14-32-614-004. PERFORMED RETRACTIONS AND EXTENSIONS OF THE NOSE LANDING GEAR PER AMM 32-31-00-720-003. A FLIGHT TEST WAS PERFORMED AND ALL R2L72 4F RTA28NM 20060801000492006080100049WP 2006 8 1 IXXA060529S 120030911A5340 FITTING DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FITTING CORRODED AT STATION FS 1124 LONGERON 27 LEFT. REMOVED DAMAGED FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20060801002462006080100246WP 2006 8 1 IXXA060488S 120030124A5210 BEAM DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX886872760 46065 DURING ROUTINE C CHECK, FOUND L-1 DOOR FORWARD INTERNAL TOP SIDE CORNER ON FIRST HORIZONTAL BEAM FROM TOP FORWARD SIDE CRACKED IN RADIUS. STOP DRILLED CRACKED, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 52-2-0, 51-1-8 AND 51-1-21. 2L74 4F RT4A25 20030812000892003081200089EU 2003 8 12 HEEA088628 120030720A32101055000126 RING BOLKMS117 BK117A1 5626010EU BEARING CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03217UC 7152 CORROSION DAMAGE BEYOND LIMITS IN BOLT RECESSED AREA. SCRAPPED. 1G72 3U H13EU 20030814000622003081400062EA 2003 8 14 SWIA200312189 120030604A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELA EMERGENGECRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 ANGLES AT FS 589 & FS 605 LT O/B END CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R35011-11. 2L72 4F4 FRTA21EA E15NE 20030814001002003081400100SO 2003 8 14 RAIA00306158 120030607A32420132AFU1 SENSOR EMB 145 EMB145LR 3260212SO NR 1 BRAKE FALSE INDICATIONA RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03819HK 145062 NR 1 BRAKE OVERTEMP INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE TEMP SENSOR. 2L72 4T RTT00011AT 20030820001422003082000142NM 2003 8 20 CALA0300408 120030616A5753 SKIN BOEING737 737824 13844BZNM IB FLAP DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717233 28943 INSPECTION FOUND THE RT WING I/B MAIN FLAP LOWER SKIN DENTED WITH A .5 INCH CRACK INSIDE THE DENT. THE AREA WAS REPAIRED IAW ECRA 5750-03785 AND A DIP WAS ISSUED TO INSPECT THE REPAIR DAILY PER PART TWO UNTIL PERMANENT REPAIR IS ACCOMPLISHED PER PART THREE WITHIN 10 DAYS. 2L72 4F RTA16WE 20030821000522003082100052NM 2003 8 21 03FDEA01050 120030625A5753ARC70531 SUPPORT DOUG MD11 MD11 3023602NM FLAP TRACK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LEFT WING - OUTBOARD TRAILING EDGE FLAP VANE, NR 1 TRACK SUPPORT FOUND AFT HOLE AND EXTERIOR SURFACE AREA CORRODED (NUMBERED FROM INBOARD). LT WING OUTBOARD TRAILING EDGE FLAP VANE NR 1 TRACK SUPPORT REMOVED AND REPLACED AS PER MM 27-50-32-4. 2L73 4F RTA22WE 20030331001362003033100136NM 2003 3 31 DHL2003740517 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO015311 FUESLAGE FRAME AT STA 540 IS DENTED BETWEEN STR 16R-17R. CUT OUT DENTED AREA AND FABRICATED REPAIR PER SRM 51-40-3. TREATED AND PRIMED REPAIR PARTS AND INSTALLED PER SRM 51-40-1 FIG 1. 2L73 4F RTA3WE 20030401000982003040100098NM 2003 4 1 DHL2003754002 120030318A3260 WARNING LIGHT BOEING727 727223 1384074NM GEAR DOOR ILLUMINATED A DHLAO OTHER JE WARNING INDICATION VIBRATION/BUFFET CRCRUISE 1 SO01754DH 22008 DURING CRUISE IN LIGHT TURBULENCE DOOR ANNUNCIATOR LIGHT ILLUMINATED, AND BANGING FELT THROUGH FLOOR OF COCKPIT. PERFORMED ABNORMAL PROCEDURE AND WITH GEAR HANDLE UP LIGHT DID NOT ILLUMINATE AGAIN. CYCLED GEAR THRU SEVERAL EXTENSIONS AND RETRACTIONS. ALL LIGHTS, DOORS AND MECHANICAL OPERATIONS WERE NORMAL IAW B-727 M/M 32-30-00. NO DEFECTS NOTED. 2L73 4F A3WE 20030415000182003041500018SW 2003 4 15 CA030314003 120030313A291070061H000A154A LINE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL HYD SYSTEM WRONG PART W O OTHER W INADEQUATE Q C NRNOT REPORTED 1 CA (CAN) DURING AN UNSCHEDULED INSPECTION IN FORWARD TRANSMISSION DECK AREA, IT WAS DISCOVERED THAT A HYDRAULIC PRESSURE LINE FROM PUMP TO FILTER HOUSING APPEARED TO BE STRESSED AT HYDRAULIC FILTER FITTING. IT WAS REVEALED UPON INVESTIGATION OF HOSE ASSY, P/N WAS INCORRECT AND LENGTH WAS TOO SHORT. IT WAS ALSO FOUND THAT IN ORDER FOR THIS PARTICULAR HOSE TO BE INSTALLED AN OVERSIZED MS21919WDG CLAMP WAS INCORPORATED. CORRECT P/N ASSYS ARE FOUND IN BELL IPC FOR THE 206 A/B SERIES. 1G71 3U3 U H2SW E4CE 20030428001042003042800104NM 2003 4 28 UPS03240411 120030328A5320 BRACKET BOEING727 727173C 1384059NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, INTERCOSTAL IN AFT FREIGHT HOLD CRACKED BS 1040 BS 1060 (SUPPORTS DOOR HOLD-PEN BRACKET). FABRICATED INTERCOSTAL BRACKET IAW SRM 51-20-1, REPROTECTED BRACKET IAW SRM 51-20-2. INTERCOSTAL INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20030428001212003042800121WP 2003 4 28 CALA0300169 120030405A5311 FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714816 49370 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 1418, L2L TO L2R. REMOVED AND REPLACED BELTFRAME IAW SRM 51-30-05. 2L72 4F4 F A6WE E2EA 20030428001832003042800183EU 2003 4 28 AWXA200300355 120030408A33501013081 LIGHT AIRBUS320 A320232 3930326EU ZONE 220 BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28638AW 455 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE FORWARD INBOARD BULKHEAD NEAR THE L-1 DOOR WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ON THE FORWARD INBOARD BULKHEAD AT THE L-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030428000442003042800044 2003 4 28 SWIA200311864 420030330A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07268UE6530 6530 120207 ON TAKEOFF ROLL AT 90 KTS (INTERMITTENTLY) AND LANDING ROLL TRIM FAIL ILLUMINATION ON MAP AND MASTER CAUTION SYSTEM. REMOVED FIRST OFFICER'S AUTOPILOT COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030428001892003042800189SO 2003 4 28 RAIA00303094 120030331A801135059105 STARTER EMB 145 EMB145LR 3260212SO ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03816HK8836 145055 STL- LT HAND ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED AIR TURBINE STARTER, OPS CHECK OK. 2L72 4T RTT00011AT 20030430000012003043000001NM 2003 4 30 S03J26017 120030424A26122156756A FIRE DETECTOR BOEING747 747400 NM GE CF6 CF680C2* GL CARGO BAY MALFUNCTIONED W SAJFO OTHER N FALSE WARNING LDLANDING 1 WP03 30759 B-18701 AFTER CARGO FIRE WARNING ON BEFORE LANDING. REPLACE NR 2 WATER SEPERATOR AND SMOKE DETECTOR 1A. 2L74 4F4 FRTA20WE E23EA 20030430002192003043000219NM 2003 4 30 VNAA0304020 120030419A2612440TS08Y01 CONTROL PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT ENG FIRE FAILED A VNAAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL07440JS19491 3058 EN ROUTE TO TYS, THE CREW RECEIVED A RIGHT HAND ENGINE FIRE INDICATION. FLIGHT 4002 LANDED AT TYS SAFELY. MECHANICS WERE SENT FROM DAY TO INSPECT THE AIRCRAFT. MAINTENANCE THEN INSPECTED AND REPLACED THE FIRE DETECT BOX, OVERHEAD FIRE PANEL, NR 2 DATA ACQUISITION UNIT, ALL THE RIGHT HAND FIRE LOOPS, AND BOTH RIGHT HAND FIRE BOTTLES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. MAINTENANCE THEN REQUESTED A FUNCTIONAL CHECK FLIGHT. THE FUNCTIONAL CHECK FLIGHT WAS PERFORMED AND THERE WERE NO DEFECTS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030501001072003050100107NM 2003 5 1 ASAA0310048 120030227A54136573771 LONGERON BOEING737 737210C 1384459NM NR 1 NACELLE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND NR 1 ENGINE COWL LOGINTUDINAL AT NACELLE STATION 175.5 CHAFED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIRS PER SRM. (M) 2L72 4F A16WE 20030506001912003050600191WP 2003 5 6 ASAA0380218 120030307A53202929169 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CORROSION ON CENTER PANEL MOUNTING SUPPORT. REPLACED FLOOR PANEL MOUNTING SUPPORT. (M) 2L72 4F A6WE 20030506000222003050600022NM 2003 5 6 03FDEA00556 120030421A5311 FRAME BOEING727 727200 138407ENM FUSELAGE PUNCTURED A FDEAO OTHER O OTHER LDLANDING 1 SO25466FE 21292 BS 1130 FRAME PUNCTURED FROM FLOOR PANEL FASTENER LBL 21 - WL 153. 2L73 4F RTA3WE 20030509000952003050900095EU 2003 5 9 2003F00251 120030505A6320C632A2111601 FREEWHEEL UNIT UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE M/R GEARBOX DRAGGING E K NONE O OTHER ININSP/MAINT 1 SW09120EB124 124 1034 34158 DURING DAILY INSPECTION, MECHANIC NOTED FREEWHEELING UNIT STAYED ENGAGED WHEN MOVING MAIN ROTOR FORWARD OR BACKWARD. CONDITION WAS VERIFIED BY PERFORMING AUTO-ROTATION DURING OPS CHECK FLIGHT. MAIN GEARBOX TO BE REPLACED IAW MANUFACTURER. 1G72 3U3 UNCR0001RD E34NE 20030513002282003051300228SO 2003 5 13 C2XA03SH118 120030425A531014522460013 BUTT STRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 SHV DURING C CHECK RIGHT HAND BUTTSTRAP FOUND TO HAVE CORROSION AT FRAME 22. MAINTENANCE REMOVED DAMAGE AREA AND REPAIRED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030514001202003051400120NM 2003 5 14 SWAA031031 120030508A531065C22909 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED, BS 500C STRINGER 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030515001142003051500114SO 2003 5 15 SWIA200311928 120030501A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07196SW6469 6469 120151 FIRST 4 EMERGENCY FLOOR LIGHTS AND FIRST 2 OVERHEAD EMERGENCY LIGHTS OUT. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030602001722003060200172NM 2003 6 2 AALA20030489 120030422A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21783AN 30004 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 2D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 2D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030604000942003060400094NM 2003 6 4 UPS03440508 120030411A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 2180 BET STR 24 - 25L. FRAME WEB FOUND CRACK. FX FRAME WEB REPAIRED AT BS 2180 BTN STR 24L AND STR 25L AS PER SRM 53-10-04 FIG 39. 2L74 4F A20WE 20030605000492003060500049 2003 6 5 WX030003 420030411A2565 COVER DOUG DC9 DC983 3022083WP ESCAPE SLIDE DEBONDED A WX0AO OTHER O OTHER TXTAXI/GRND HDL 1 WP17860GA 49786 DURING A ROUTINE TURN IN SLC, FLT ATTEND OPENED AFT SERVICE DOOR & OBSERVED SLIDE TO BE UNSECURE. EMERGENCY MX CALLED OUT. FOUND SLIDE & COVER TO BE LOOSE. SLIDE & COVER WERE RESECURED & A/C RETURNED TO SERVICE. ON FOLLOWING TURN IN RNO, SERVICE DOOR WAS AGAIN OPENED BY FLT ATTEND. SLIDE AND COVER WERE AGAIN NOTED TO BE UNSECURE. MX WAS CALLED AGAIN, FOUND THE SLIDE AND COVER WAS LOOSE. THE SLIDE AND COVER WERE RESECURED AND THE AIRCRAFT RETURNED TO SERVICE. UPON ARRIVAL AT THE FAT MX BASE, MAINTEANCE INSPECTED SLIDE INSTALLATION. IT WAS FOUND THAT SLIDE COVER WAS DEBONDED FROM DOOR FAIRING. COVER WAS REATTACHED IAW AMM 20-20-01 AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO FURTHER DIFFICULTIES WITH T2L72 4F RTA6WE 20030606000852003060600085NM 2003 6 6 03FDEA00764 120030513A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP O/B HINGE (FLAP SIDE), FWD ATTACHING POINT, I/B AFT BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR 2L73 4F RTA22WE 20030604002052003060400205NM 2003 6 4 UPS03440633 120030404A783065B97235143 SLEEVE BOEING747 747121 1384871NM NR 1 ENGINE DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, NR 1 ENGINE - FAN THRUST REVERSER SLEEVE DEBONDED REVEALED AT EXTERNAL SKIN BETWEEN 3 AND 4 O'CLOCK. NR 1 ENGINE THRUST REVERSER SLEEVE REPAIRED AS RS R78-30-35003 AND UPS EO B747-7830-18689-A. 2L74 4F A20WE 20030609001222003060900122WP 2003 6 9 ABXA030151 120030520A573099194041 PANEL DOUG DC9 DC932 3022066WP LT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 WHILE PERFORMING ROUTINE LINE MAINTENANCE, A FUEL LEAK WAS DISCOVERED AT THE LT WING FUEL PANEL 1307. FURTHER INSPECTION REVEALED A CRACK ON THE FUEL PANEL FLANGE. REPAIRED CRACK IAW DC-9 SRM 57-03, FIG 23. 2L72 4F A6WE 20030520000582003052000058NM 2003 5 20 AMTA200300499 120030411A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11526AT 30735 FORWARD THREE EGRESS LIGHTS NOT ILLUMINATED. RECONNETED LOOSE WIRE SECURED LIGHT ASSY. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030609000772003060900077EA 2003 6 9 QXEA0300629 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT FS421, 2 INCHES BELOW STRINGER 14R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030611000392003061100039WP 2003 6 11 MEX2003171 120030511A2410595233B CSD DOUG DC9 DC987 3022087WP NR 2 ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23205AM 49405 DURING TAXING, THE CSD TEMPERATURE INDICATES 380 DEGREES ON ENGINE NR 2. THE CSD, AC GENERATOR AND CSD EXCHANGER WERE REPLACED IAW MM 24-10-01. MM 24-10-01 AND MM 24-10-03, RESPECTIVELY, TEST CORRECT. 2L72 4F RTA6WE 20030612001232003061200123NM 2003 6 12 UPS03440767 120030519A5313BAC14981947075 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 1958 S13R, STRINGER END FOUND CRACK. M/D BS 1958 S13R STRINGER END CRACKED REPAIRED AS PER SRM 53-10-03 FIG 12. 2L74 4F RTA20WE 20030617002842003061700284SW 2003 6 17 HEEA087318 120030611A5610407030115125 WINDSHIELD BELL 407 407 1182206SW COCKPIT CRAZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 WINDSHIELD IS CRAZED. REPLACED WINDSHIELD. 1G71 3U O H2SW 20030618001732003061800173 2003 6 18 HEEA087511 420030612A34424000023 TRANSCEIVER SKRSKYS76 S76A 8143006NE WX RADAR SYS MALFUNCTIONED E O OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 TRANSCEIVER HAS STATIC IN FLIGHT. SHOP REPAIR. 1G72 3U H1NE 20030529000272003052900027NE 2003 5 29 HEEA086625 220030521A732032447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TORQUE SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 UNCONTROLLABLE TORQUE SPLIT. TESTED AND FOUND SERVO VALVE LEAKAGE CAUSING UNEVEN FLOW BETWEEN SIDES. POLISHED SERVO VALVES AND LEVER. UNIT TESTED SATISFACTORY. 1G72 4U4 U H4SW E22EA 20030623000782003062300078SO 2003 6 23 2003F00386 120030524A29101159SCH5125 VALVE GULSTMGV GULFSTREAMGV3980116SO HYD SYSTEM MALFUNCTIONED A UG8AO OTHER J WARNING INDICATION APAPPROACH 1 GL235101 550 UNABLE TO GET NORMAL LANDING GEAR EXTENSION. PERFORMED EMERGENCY LANDING GEAR EXTENSION. T/S LANDING GEAR SYSTEM INDICATED A MALFUNCTION OF THE LANDING EAR HYDRAULIC SELECTOR VALVE LOCATED IN THE MAIN WHEEL WELL. REPLACED LANDING GEAR HYDRAULIC SELECTOR/DUMP VALVE. LANDING GEAR OPERATIONAL CHECKS NORMAL IAW GULFSTREAM MM. (M) 2L72 4F RTA12EA 20030619000742003061900074SW 2003 6 19 HEEA087408 120030611A6510407340339101 BEARING BELL 407 407 1182206SW T/R DRIVE OVERHEATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 TAIL ROTOR DRIVE BEARING PRODUCING HIGH TEMP. 1G71 3U O H2SW 20030623000102003062300010NM 2003 6 23 AMTA200300654 120030516A3350 STRIP BOEING737 73783N 13844HINM EMERGENCY EXIT DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11321TZ 28249 THE FLOOR EGRESS FROM SEATS 1-7 ABC IS CRACKED AND DISCOLORED. REMOVED AND REPLACED DAMAGED SECTION OF PHOTOLUMINESCENT STRIP REF MM 33-51-15-2. (M) 2L72 4F RTA16WE 20030624000552003062400055NM 2003 6 24 CALA0300292 120030606A5340654681287 FITTING BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND LEFT O/B SUPPORT FITTING CORRODED BETWEEN STA 1006 AND 1016, LBL 36. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030624000762003062400076SO 2003 6 24 SWIA200312072 120030602A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07299SW4715 4715 120329 FIRST THREE (FORWARD) EMERGENCY EXIT FLOOR LIGHTS, AS WELL AS FIRST (FORWARD) OVERHEAD POD LIGHT INTERMITTENT OPERATION. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. 2L72 4T RTA31SO 20030630000722003063000072EU 2003 6 30 BAQA087772 120030624A6210L621M1010054 BLADE UROCOPEC135 EC135T1 5620026EU MAIN ROTOR WILL NOT BALANCEB BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME1733 0157 BLADES REMOVED BECAUSE THEY APPEAR TO BE HEAVY AND WILL NOT BALANCE. BLADES WERE JUST IN REPAIR IN APRIL. BLADES HAVE ONLY 84.8 HOURS ON THEM SINCE LAST REPAIR. 1G72 3U H88EU 20030709000082003070900008WP 2003 7 9 GTIA030439 120030515A5321 FLOORBOARD DOUG DC9 DC981 3022081WP CABIN DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND CABIN FLOOR PANEL AFT OF R-1 DOOR IS DELAMINATED. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20030709000482003070900048WP 2003 7 9 GTIA030444 120030508A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND AFT FUSELAGE LEFT SIDE STATION 1429 TO 1448 HAS CORROSION AT T-CAP VENTRAL STAIRWAY. REMOVED INTERCOSTAL. REMOVED DAMGED CAP ANGLE. FORMED NEW INTERCOSTAL AND CAP ANGLE. INSTALLED NEW INTERCOSTAL. INSTALLED NEW CAP ANGLE. (M) 2L72 4F A6WE 20030709001212003070900121EU 2003 7 9 MALA030300 120030605A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15446XJ 340B446 WHILE TRYING TO COMPLETE OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM TASK CARD 335003 LIGHTS 32LN AND 33LN WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY 21LN, P/N 3301-51, SN/OFF 2180, SN/ON 2206 IAW SF340 AMM 33-50-10. 2L72 4T RTA52EU 20030127000512003012700051SW 2003 1 27 HEEA083629 120030114A243231908001 BATTERY BELL 407 407 1182206SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 BATTERY HAS LOW CHARGE. REPAIRED. 1G71 3U O H2SW 20030129000982003012900098SW 2003 1 29 HEEA083991 120030117A7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20030204002882003020400288NM 2003 2 4 F3LA200300020 120030122A5320 INTERCOSTAL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL CORRODED BETWEEN STA 294.5 AND 277, LBL 12. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. REPLACED INTERCOSTAL PER SRM 51-40-02. 2L72 4F RTA16WE 20030203001802003020300180CE 2003 2 3 FPI2003F00001 120030114A3233 HOUSING CESSNA210 210N 2073453CE ACTUATOR CRACKED A FPIAK NONE O OTHER ININSP/MAINT 1 SO156195N 491 21062966 FOUND LANDING GEAR ACTUATOR CRACKED IAW SB. 1H71 3O 3A21 20030218000092003021800009NM 2003 2 18 03FDEA00096 120030119A5753 HINGE BRACKET DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 SNRM N0927, LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORES FOUND CORROSION. SNRM N0927 REPAIR CARRIED OUT AT LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORES IAW EA 1-5750-67559: WING TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F4 FRTA22WE E13NE 20030220000382003022000038CE 2003 2 20 047205 120030124A5270 SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA PAX DOOR DIRTY A AMWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07242YV UE242 AFTER DEPARTING, THE CREW HAD THE PASSENGER DOOR ANNUNCIATOR ILLUMINATE. THE CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE SWITCHES. NO PARTS WERE USED. TEARDOWN REPORT WILL NOT BE REQUIRED. 2L72 4T3 TRTA24CE E2NE 20030220000962003022000096 2003 2 20 QXEA0300091 420030114A3444 WARNING SYSTEM DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAK NONE N FALSE WARNING CRCRUISE 1 NM09379PH 530 SEA-ON FLIGHT NUMBER 2251, GPWS CAUTION LIGHT ILLUMINATED IN FLIGHT. CHECKLIST COMPLIED WITH. PERFORMED EGPWS OPERATIONAL TEST. NO DEFECTS FOUND. SYSTEM TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030220001742003022000174WP 2003 2 20 ARWA20030110 120030130A2910 HOSE DOUG DC8 DC863 302198AWP HYD SYSTEM LEAKING A ARWAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO19345JW 46042 AFTER LANDING, LOST HYDRAULIC PRESSURE. T/S HYDRAULIC LEAK TO THE RT BOGIE TRIM CYLINDER HYDRAULIC FLEX LINE. REMOVED AND REPLACED BOGIE TRIM HYDRAULIC HOSE ASSEMBLY IAW MM 20-12-0; SERVICED MAIN HYDRAULIC RESERVOIR SYSTEM IAW MM 12-30-1, BLED HYDRAULIC SYSTEM AND LEAK, CHECKED BOGIE TRIM CYLINDER IAW MM 29-00. NO LEAKS FOUND. 2L74 4F 4A25 20030116000152003011600015NE 2003 1 16 HEEA082972 120030107A673041004076 HOUSING SKRSKYS76 S76A 8143006NE MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546K 0981 760082 PIN PLUG IN MAIN ROTOR SERVO HOUSING BLEW OUT DURING FINAL TEST. 1G72 3U H1NE 20030121000652003012100065WP 2003 1 21 0300089993 120030115A5330 SKIN DOUG DC9 DC931 3022065WP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 During "L" check found crack in forward service door aft lower corner jamb on skin and doubler. Repaired per EA 99-190893. 2L72 4F A6WE 20030304000302003030400030EU 2003 3 4 HE66084850 120030228A6330L633M2010101 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX DEFECTIVE H HEEAO OTHER O OTHER CRCRUISE 1 FS01135CR741 0164 MAIN ROTOR GEARBOX ARIS MOUNT FAILED. REPLACED. 1G72 3U H88EU 20030304000972003030400097 2003 3 4 HEEA084599 420030214A3442MI5851345 INDICATOR BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 WEATHER RADAR SYSTEM WILL NOT PAINT. FOUND LOGIC NR 1 BOARD BAD, REPLACED IC U1251, U1258, U1211, U1213, U1201, REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030227000612003022700061 2003 2 27 HEEA084380 420030211A3423C2300L424B COMPASS BELL 407 407 1182206SW COCKPIT OSCILLATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 COMPASS OSCILLLATES DURING COMPASS SWING 5-10 DEGREES. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20030228000882003022800088WP 2003 2 28 ASAA0380011 120030103A53475936594527 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY TRACK CORRODED AT CLIP NUT HOLES AT FS 525-785. REPLACED DAMAGED SECTION PER SRM 53-05 AND 51-30-5, AND 51-10-4. (M) 2L72 4F RTA6WE 20030303000242003030300024SW 2003 3 3 HEEA084492 120030214A3212412050017133 COVER BELL 412 412 1182202SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 EMERGENCY FLOAT COVER IS WORN. REPLACED WITH SERVICEABLE FLOAT COVER. 1G72 4U H4SW 20030303000522003030300052SW 2003 3 3 HEEA084508 120030214A30402314M2218 ARM BELL 412 412 1182202SW WINDSHIELD WIPERSTIFF E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WINDSHIELD WIPER ARM STIFF, CANNOT ADJUST TENSION. SCRAPPED. 1G72 4U H4SW 20030307000092003030700009 2003 3 7 HEEA084879 420030227A2312064100900 TRANSCEIVER SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 TRANSMITTER SIDETONE DROPS OFF LINE. SHOP REPAIR. 1G72 3U H1NE 20030310000562003031000056 2003 3 10 HEEA084960 420030227A22114025008918 COMPUTER BELL 412 412 1182202SW AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 AFCS COMPUTER PITCH CHANNEL MOVES FORE/AFT WITHOUT PILOT INPUT. REPAIRED. 1G72 4U H4SW 20030311000162003031100016SW 2003 3 11 HEEA085037 120030228A2820206063653001 TUBE BELL 206 206L3 1182108SW FUEL DIST CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03205FC 51130 FUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED. 1G71 3U H2SW 20030313002092003031300209NM 2003 3 13 AALA20030177 120030207A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21383AN 26995 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030314001652003031400165CE 2003 3 14 S2YA03004 120030123A243523078019 STARTER GEN BEECH 1900 1900D 1154162CE PWA PT6 PT6A11 52043NE NR 2 ENGINE INOPERATIVE A S2YAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 GL13118SK9349 509 UE108 AFTER STARTING THE NR 2 ENGINE, THE CREW HAD DIFFIUCULTY GETTING THE NR2 GENERATOR ON LINE. THEN THERE WAS A FIRE INDICATION ON THE RIGHT ENGINE, THE CREW PULLED THE FIRE HANDLE BUT DID NOT BLOW THE BOTTLE. MECHANIC INSPECTED THE SYSTEM AND FOUND THE RIGHT GENERATOR GARLOC SEAL TO BE LEAKING. MECHANIC REPLACED THE SEAL AND THE RIGHT GENERATOR, OPS CHECKED THE SYSTEM AND REALEASED THE AIRCRAFT TO SERVICE. 2L72 4T3 TRTA24CE E4EA 20030314001892003031400189CE 2003 3 14 048803 120030313A6120186641001 SOLENOID BEECH 1900 1900D 1154162CE STUCK A AMWAO OTHER O OTHER LDLANDING 1 CE0710675 10675 UPON LANDING ON FLIGHT 5487 IN PHILADELPHIA PENNSYLVANIA, THE CREW THOUGHT IT WAS A DESTABILIZING FLARE DUE TO LEFT QUARTERING TAILWIND. THEY WENT AROUND TO LAND ON A DIFFERENT RUNWAY TO FIND IN THE FLARE IT WAS THE LEFT PROP THAT WAS IN GROUND FINE WHEN THE POWER LEVER WAS RETARDED TO IDLE. THE CREW THOUGHT ABOUT SHUTTING DOWN THE LEFT ENGINE BUT WAS UNABLE TO TELL DEFINITELY WHICH OF THE PROPS HAD BEEN IN GROUND FINE. DUE TO THE SEVERITY OF THE LAST TWO APPROACHES AND THE SLICKNESS OF THE RUNWAY AT THE TIME, THEY DECIDED TO DECLARE AN EMERGENCY AND HAVE GROUND VEHICLES STANDING BY. THEY LANDING WITHOUT ANY FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE FOUND THE LEFT LOW PITCH SOLENOID TO BE INOPERATIV2L72 4T RTA24CE 20030317000122003031700012NM 2003 3 17 03FDEA00142 120030220A5313 STRINGER BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION IN SEVERAL AREAS IN STRINGER 26R FROM BS 620 TO 720A. REMOVED AND REPLACED STRINGER SECTION AT BS 675 - 720+10 IAW SRM 53-10-3. 2L73 4F4 F A3WE E2EA 20030317001352003031700135NM 2003 3 17 03FDEA00299 120030312A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 DENT IN FRAME, FWD CARGO BAY, BS 520 STR 24R. 2L73 4F RTA3WE 20030318001202003031800120NM 2003 3 18 BJNA03027 120030211A5315 FLOORBEAM BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOORBEAM LOCATED IN THE FORWARD CARGO COMPARTMENT AT FS 500 PLUS 40 INCH BL 12R, AREA OF CORROSION IS APPROXIMATELY 3 INCHES BY 1 INCH ON THE FRAME LOWER FORWARD FLANGE. REMOVED THE CORRODED SECTION AND FABRICATED AND INSTALLED A REPAIR ANGLE IAW BOEING 737 SRM 53-10-4 FIGURE 7, 6, 8, AND 9. (M) 2L72 4F RTA16WE 20030319000512003031900051WP 2003 3 19 GTIA030076 120030129A5310 DOOR FRAME DOUG DC9 DC981 3022081WP CARGO BAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND FORWARD CARGO PIT CORROSION, BARE METAL AND CRACKED DAMAGED SEALANT ALL ALONG INBOARD FRAME AT DOOR JAMB PANEL FROM 3 O'CLOCK TO 9 O'CLOCK POSITION. FOUND CORROSION OUT OF LIMITS. CUT OUT FORWARD CARGO DOOR JAMB PANEL FROM 5 O'CLOCK TO 7 O'CLOCK FS 370-427. LOCATED AND DRILLED NEW FORWARD CARGO DOOR JAMB PANEL FROM 5 O'CLOCK TO 7 O'CLOCK FS 370-427. INSTALLED WEB STATION 364-423 AT FORWARD CARGO DOOR. (M) 2L72 4F A6WE 20030319000692003031900069WP 2003 3 19 DHL2003873005 120030318A2611 LAMP DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01873SJ 46091 1) #4 SMOKE DETECTOR WILL NOT TEST.2) TRANSFERRED TO DMI LOG IAW DC-8 MEL 26-6-2, CAT. "C", DMI #12300 PLACARD INSTALLED. 3) REF. DMI #12300 #4 SMOKE DETECTOR WILL NOT TEST.4) RELAMPED SMOKE DETECTOR. OPS CHECKED GOOD PER M/M 26-10-0. THIS CLEARS DMI #12300. 2L74 4F RT4A25 20030320000152003032000015NM 2003 3 20 USAABB03019 120030208A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19607AU 22203 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030320000902003032000090NM 2003 3 20 2003UALA00074 120030121A3350 LIGHT BOEING777 777222 1385219NM ESCAPE SLIDE BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29229UA 30557 DOOR 4A EXTERNAL EMERGENCY SLIDE LIGHT INOPERATIVE. SLIDE LIGHT REPLACED. OPS CHECKED OK. 2L72 4F RTT0001SE 20030321000562003032100056EA 2003 3 21 COMA0360158 120030319A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01986CA14000 7174 FLIGHT 5113 R/H WINDSHEILD HEAT CAUTION MESSAGE.REPLACED THE WINDSHIELD HEAT CONTROLLER. 2L72 4F RTA21EA 20030321000752003032100075NM 2003 3 21 2003UALA00216 120030223A5754114W413016 SKIN BOEING777 777222 1385219NM NR 12 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29205UA 28714 TRAILING EDGE WEDGE, SLAT NR 12, DELAMINATED. BULB SEAL FOAM FILLER SECTION MISSING. REPAIRED TRAILING EDGE WEDGE, SLAT NR 12 AND REPLACED FOAM FILLER. 2L72 4F RTT0001SE 20030416002922003041600292WP 2003 4 16 AALA20030301 120030307A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21295AA 49307 DFW - DURING OVERNIGHT MAINTENANCE, DETACHABLE EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REPLACED DETACHABLE EMERGENCY EXIT DOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030418000122003041800012NM 2003 4 18 UPS03440181 120030131A5320 ANGLE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C M/D, R4 DOOR AFT UPPER CORNER FOUND CRACKED (AS MARKED). M/D - R4 DOOR AFT UPPER CORNER REPAIRED AS PER SRM 51-10-02 FIG 10. 2L74 4F RTA20WE 20030421000662003042100066EA 2003 4 21 SWIA200311815 120030301A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07440SW3366 3366 7589 SPOILERONS FAULT MESSAGE. REPLACED RIGHT SPOILERON OUTBOARD PCU IAW CRJ MAMM 27-62-01. OPS AND LEAK CHECKS OK. 2L72 4F RTA21EA 20030417000982003041700098EA 2003 4 17 QXEA0300219 120030201A2611474075 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09601QX* * 10009 TUS ON FLIGHT 2534- MASTER WARNING SMOKE AFT LAVATORY MESSAGE. FLIGHT ATTENDANT ADVISED NO SMOKE PRESENT. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309001682004030900168WP 2004 3 9 GTIA031068 120031227A2810 BLADDER DOUG DC9 DC983 3022083WP FUEL SYSTEM LEAKING A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23832NK 49618 DTW - FUEL LEAKING FROM FUSELAGE AFT OF WHEEL WELL. REMOVED AND REPLACED AFT AUX BLADDER. LEAK CHECK GOOD. INSPECTED INSTALLATION OF AFT AUX TANK BLADDER AND FUEL DRAIN SHROUDS. NO LEAKS NOTED. (M) 2L72 4F RTA6WE 20040520002202004052000220NM 2004 5 20 2004F00110 120031211A242097654981R GENERATOR BOEING727 727222 1384073NM NR 3 ENGINE FAILED A RYNAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 SW077640U 19913 DURING TAKEOFF FROM BNA, AIRCRAFT LOST NR 3 GENERATOR, EPR WENT TO 1.6 AND OIL PRESSURE FELL TO REDLINE. PERFORMED ENGINE SHUTDOWN PROCEDURES AND DECLARED EMERGENCY. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. DURING GROUND RUN OF ENGINES, FOUND NR 3 GENERATOR DEFECTIVE. ALL OTHER PARAMETERS CHECKED NORMAL. REMOVED AND REPLACED NR 3 GENERATOR. ALL SYSTEMS OPS CHECKED NORMAL. (M) 2L73 4F A3WE 20031216000102003121600010NM 2003 12 16 QXEA200301448 120031105A5751 SKIN DHAV DHC8 DHC8202 2809007NM RT AILERON DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- RIGHT HAND AILERON TOP SKIN HAS A BURN HOLE AT RIVET ON TRAILING EDGE. REPAIRED IAW DHC-8 RD 8-57-2702 AND HORIZON AIR EA 2-57-241. 2H72 4T RTA13NM 20031217000352003121700035WP 2003 12 17 DHL2003805507 120030803A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RT WING CTR L/E FRAME 0.250 CRACKED, STA XFS 347.750. REMOVED FASTENERS IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.040) (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040910000662004091000066SO 2004 9 10 X6PA200300004 120030828A571278500003 RIB PIPER PA34 PA34200 7103405SO RT WING CRACKED A X6PAK NONE O OTHER ININSP/MAINT 1 SO33997BW 347450064 WHILE PERFORMING A 100 HOUR INSPECTION A 1 INCH CRACK AND WARPAGE OF WING RIB P/N 78500-003 AT WING STATION 69.24 RIGHT. A NEW RIB WAS INSTALLED P/N 78500-003 PER AC 43. 13-1B AND A 337 COMPLETED. PIPERS NEW RIB P/N 78500-003 CONTAINS REINFORCEMENT WHICH SHOULD PREVENT SIMILAR CRACKS FROM FORMING IN THE FUTURE. (M) 1L72 3O A7SO 20060801000392006080100039WP 2006 8 1 IXXA060523S 120030924A5322 SHEAR TIE DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND SHEAR TIE CORRODED AT STATION 1020 FROM LONGERON 31 RIGHT TO LONGERON 34 RIGHT. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-8, 53-4-1, AND 51-1-20D. 2L74 4F RT4A25 20030819001112003081900111WP 2003 8 19 UPS03840917 120030619A53405652580 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C, STATION 1875 AT LONGERON 36 LARGE FITTING IS CRACKED INSIDE 62 TAIL COMPARTMENT. REMOVED AND REPLACED FITTING IAW DWG 5652580 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20030819001532003081900153NM 2003 8 19 2003UALA00510 120030617A2421690712 GASKET BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CSD LEAKING A UALAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 WP29936UA 26667 AIRCRAFT ABORTED TAKEOFF WHEN THE NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED. FOUND CSD LEAKING FROM SIGHT GLASS. REINSTALLED GASKET. SERVICED THE CSD, RAN ENGINE WITH NO LEAKS NOTED. 2L72 4F4 FRTA16WE E2GL 20030820000142003082000014NM 2003 8 20 03FDEA00950 120030616A5753ARC0502 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LT WING, O/B FLAP I/B HINGE LOWER O/B STUD BORE AFT SURFACE FOUND CORROSION. AFT SURFACE OF O/B STUD BORE REPAIRED AS PER CMM 57-44-08, WITHIN ALLOWABLE LIMIT AS PER CMM 57-44-08 AT LHW O/B FLAP I/B HINGE. 2L73 4F RTA22WE 20030820000912003082000091 2003 8 20 234TR0001 420030715A34578221155121 GPS BOEING737 737228 13844AGNM COCKPIT MALFUNCTIONED A PIDAK NONE O OTHER CRCRUISE 1 SO05234TR 23004 GPS WILL NOT ACQUIRE ANY SATELLITES. REMOVED AND REPLACED GNLU. GPS NOW ACQUIRES SATELLITES ON GROUND. 2L72 4F RTA16WE 20030819001632003081900163NM 2003 8 19 2003UALA00602 120030710A5754 WEDGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29512UA 24809 DELAMINATION AND INFLIGHT SEPARATION OF NR 6 SLAT T/E WEDGE. MAJOR REPAIR ACCOMPLISHED. REPLACED SLAT T/E WEDGE. 2L72 4F4 FRTA2NM E17NE 20030331000862003033100086SO 2003 3 31 C2XA03SH063 120030329A531014521721005 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE RT BUTT STRAP AT FRAME 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030821002632003082100263WP 2003 8 21 GTIA030591 120030702A2540 FLOOR PANEL DOUG DC9 DC982 3022082WP LAVATORY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FORWARD LAVATORY VANITY WALL UNDER SINK AREA FLOOR CORRODED. REMOVED FLOOR. FABRICATED NEW FLOOR. INSTALLED NEW FLOOR. (M) 2L72 4F A6WE 20030331000702003033100070EU 2003 3 31 ASOA03094 120030216A5310 THRESHOLD AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, PASSENGER DOOR DRAIN GUTTER THRESHOLD BETWEEN FRAMES 36L TO 39L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED PASSENGER DOOR DRAIN GUTTER THRESHOLD BETWEEN FRAMES 36L TO 39L IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030403001012003040300101NM 2003 4 3 DL72S030148 120030210A5330 SKIN BOEING727 727225A 1384077NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO278875Z 21293 TWO EXISTING SMALL REPAIR DOUBLERS WERE INSTALLED ON THE AIRCRAFT AT THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT. ONE REPAIR WAS FOR A SMALL CRACK IN THE SKIN AT THE EDGE OF THE DOOR AND THE OTHER FOR A BLENDOUT OF A LIGHTNING STRIKE. BOTH REPAIR WERE TEMPORARY AND WERE REMOVED. BOTH DAMAGE CUTOUT LOCATIONS WERE INSPECTED AND REPAIRED WITH A SINGLE EXTERNAL REPAIR DOUBLER PER ER/A 384476-14, REV A. 2L73 4F RTA3WE 20030421001732003042100173WP 2003 4 21 GTIA030124 120030223A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL11809NK 49503 FTW - FOUND FORWARD CABIN STATION TO STATION 148 RBL 17 TO 45 (11 BY 13) FLOOR PANEL SOFT/MUSHY. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20030421001952003042100195WP 2003 4 21 GTIA030132 120030216A5330 DOUBLER DOUG DC9 DC983 3022083WP FORWARD PIT CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FORWARD PIT STATIC ALTERNATE PORT DOUBLER BETWEEN L27L ND L26L STATION 446-463 IS CORRODED. REMOVED DOUBLER. INSTALLED NEW STATIC ALTERNATE PORT DOUBLER. (M) 2L72 4F RTA6WE 20030730000952003073000095WP 2003 7 30 ABXA030312 120030630A5420 PANEL DOUG DC8 DC863F 302198FWP NR 3 PYLON DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX 45927 COI 43055-01, NR 3 PYLON INBOARD STRESS PANEL. REPAIRED AREA IAW REA D854-47544MR, REV A. 2L74 4F 4A25 20040223000102004022300010CE 2004 2 23 00123 120031231A3260 WARNING LIGHT LEAR 24 24D 5170311CE MLG MALFUNCTIONED E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05266TW 266 PILOT REPORED AFTER DEPARTURE, THAT THE MAIN GEAR IN TRANSIT LIGHTS REMAINED ILLUMINATED WHEN THE GEAR WAS RAISED, GEAR TRANSIT LIGHTS WOULD GO OUT WHEN GEAR WAS LOWERED, PILOT DIVERT. MAINTENANCE INSPECTED LANDING GEAR SWITCHES AND WIRE HARNESS CYCLED GEAR FOUND ALL OPERATING NORMAL AT THIS TIME. 2L72 4J A10CE 20040225001622004022500162NM 2004 2 25 DLM88031130 120031224A2432203BC1021 CHARGER DOUG MD88 MD88 3023688NM E/E COMP MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS M OVER TEMP TXTAXI/GRND HDL 1 SO27911DL 49542 AFTER PDC AND CREW WALKAROUND, RAMP NOTED SMOKE (ACTUALLY STEAM) FROM E&E DOOR AREA. DISCOVERED SHIPS BATTERIES IN OVERHEATED STATE AND BATTERY CHARGER FAIL IN HIGH CHARGER MODE. REPLACED BATTERY & CHARGER. 2L72 4F RTA6WE 20030827001562003082700156NM 2003 8 27 2003UALA00605 120030802A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29367UA 24536 AFT CABIN BS 941.5 RBL 45.5 HAS FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW PARTS. 2L72 4F4 FRTA16WE E2GL 20030829000912003082900091NM 2003 8 29 P5CA03000917 120030818A8012 WARNING SYSTEM BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL COCKPIT ACTIVATED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23496MC 29257 704882 DURING ENG START NR 4 ENG AUTO START EICAS MESSAGE STARTER VLV LIGHT FAILED TO EXTINGUISH WITH SWITCH PUSHED IN. ITEM DEFERRED PER MEL 80-11-01. 2L74 4F4 FRT1384945 E23EA 20030902001282003090200128NM 2003 9 2 AWXA200300782 120030608A542065C28701 ANGLE BOEING737 7373Y0 1384671NM Z-ANGLE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK, A .7500 INCH CRACK WAS FOUND ON NR 2 PYLON "Z" ANGLE AT THE FRONT SPAR FITTING, STA 271.4. MAINTENANCE TRIMMED OUT DAMAGE; FABRICATED A NEW SECTION OF ANGLE; INSTALLED REPAIR PART IAW E.R. 03-5741-03169-ES1. 2L72 4F RTA16WE 20030903001322003090300132 2003 9 3 2003F00541 420030501A341457532755695 INDICATOR GULSTMG1159 G1159A 3970109SO COCKPIT MALFUNCTIONED A ZLWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW1585VT 449 AIRCRAFT STARTED ITS TAKEOFF ROLL AT TUL. THE CREW NOTICED NO AIRSPEED INDICATION ON THE PILOTS SIDE AND THEY REJECTED THE TAKEOFF. TAXIED THE AIRCRAFT BACK TO HANGAR 31 WHRE THE INDICATORS WERE SWAPPED AND FUNCTIONAL CHECKED. BOTH SYSTEMS OPERATED NORMALLY PER GULFSTREAM MM. (M) 2L72 4F A12EA 20030902001952003090200195CE 2003 9 2 GLBA2003106 120030712A3250 LANDING GEAR BEECH 1900 1900D 1154162CE NOSE MALFUNCTIONED A GLBAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03226GL UE226 NOSE WHEEL CHANGED POSITION ABRUPTLY ON TAKEOFF. INSPECTED A/C PERFORMED HIGH SPEED TAXI CND. 2L72 4T RTA24CE 20030903000422003090300042EU 2003 9 3 YZ42003F00000 120030521A262033370004 HOUSING AMD FALC20FALCON200 2730150EU GARRTTATF3 ATF3* 29002WP EXTINGUISHER FAILED B YZ4RO OTHER O OTHER NRNOT REPORTED 1 SO05200WY 509 THE HOUSING ASSY, PN 33370004, DID NOT RECEIVE ENOUGH FORCE TO DETACH THE END OF THE HOUSING ASSEMBLY PREVENTING THE PLUG VALVE, PN 13038, FROM BEING EXPELLED AND ALLOWING FIRE EXTINGUISHER FROM EXPELLING TO THE POSSIBLE FIRE. 2L72 4F4 FRTA7EU E7WE 20030822000332003082200033NM 2003 8 22 03FDEA01046 120030626A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 MAIN DECK - AT BS 755, LEFT X=8.5, FLOOR TRACK CRACKED. MAIN DECK - BS 755, LT X=8.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00,VOL I. 2L73 4F RTA22WE 20030911000672003091100067WP 2003 9 11 DHL2003873510 120030617A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LT WING IB L/E FORMER CRACKED 0.250 AT STA XFS.597.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030826001822003082600182EU 2003 8 26 VY1L103171 120030106A7931704A37642042 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE OIL PRESSURE FAILED L VY1LO OTHER O OTHER NRNOT REPORTED 1 SW19121US54 1447 TRANSMITTER, FAILED IN SERVICE WITH ONLY 54.3 TT OPERATING HOURS. 1G71 3U3 UNCH9EU E19EU 20030911001582003091100158WP 2003 9 11 AALA20030323 120030310A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21459AA 49564 FOUND CORROSION ON NR 1 SEAT TRACK STATION 1024. REPLACED NR 1 SEAT TRACK FROM STATION 864 TO 1031 AND SPLICED TWO PLACES PER SRM 53-05-00. (M) 2L72 4F A6WE 20030407000472003040700047 2003 4 7 GTIA030036 420030201A2565 SLIDE DOUG DC9 DC982 3022082WP CABIN DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 LAS - FLT 1108 - L-2 SLIDE PACK WAS FOUND LYING ON FLOOR. REINSTALLED L-2 SLIDE PACK IAW MD80 MM 25-62-00. OPS CHECK NORMAL AT THIS TIME. (M) 2L72 4F A6WE 20030402000222003040200022NM 2003 4 2 0300666313 120030331A2530 OVEN BOEING747 747451 1384940NM NR 2 GALLEY SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01673US 30268 DURING FLIGHT SMOKE EMITTED FROM THE NR 2 GALLEY OVEN, POSITION 2-34. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN, OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20030410002102003041000210WP 2003 4 10 GTIA030158 120030129A5310 BEAM DOUG DC9 DC981 3022081WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 MID CARGO DOOR FRAME CORROSION, BARE METAL, CRACKED SEALANT ALL ALONG DOOR JAM BEAM. REMOVED DOOR JAMB BEAM L28R STA 598 TO 731 RT. HOLES LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED DOOR JAMB BEAM STA 598 TO 731. 2L72 4F4 F A6WE E2EA 20030415000272003041500027EU 2003 4 15 CA030317018 120030304A6320 GEARBOX SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) MAIN GEARBOX CHIP LIGHT CAME ON DURING FLIGHT.PILOT LANDED AND INSPECTED THE MGB CHIP PLUG. NO METAL FOUND. HE CALLED THE BASE AND WE ADVISED HIM TO CHECK THE MAST BEARING CHIP DETECTOR AND CHECK TO MAKE SURE THE LIGHTS STILL WORKED. NO METAL FOUND. AIRCRAFT FINISHED THE DAY AND WAS CHECKED AGAIN UPON RETURN. NO METAL FOUND. 1G71 3U3 UNCH9EU E19EU 20030408001122003040800112NM 2003 4 8 2003UALA00357 120030329A3350 BULB BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29667UA 29239 EXTERIOR EMERGENCY LIGHT IS INOP AT DOOR 1L. RELAMPED LIGHT 2L72 4F4 FRTA1NM E24NE 20030408001232003040800123WP 2003 4 8 AMTA200300214 120030211A3350516574 CHARGER LKHEED1011 10113853 5265020WP CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11163AT 1229 CEILING EGRESS LIGHTS OUT FROM D-1 LAV TO LEFT P4A DOOR. REMOVED AND REPLACED EMERGENCY CHARGER AFT IAW 33-51-03, OPS CHECK OK. (M) 2L73 4F A23WE 20030416001212003041600121NE 2003 4 16 DLM88030261 220030320A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27963DL34404 49982 725393 AFTER GEAR RETRACTION THERE WAS A STRONG BURNED RUBBER ODOR IN THE COCKPIT AND THE CABIN THAT DISSIPATED AFTER SEVERAL MINUTES. NO OTHER ABNORMAL INDICATION. FLT ATTN REPORTED THAT A SIMILAR ODOR OCCURRED THIS MORNING ON DEPARTURE FROM DAB. REPLACED NR 2 ENGINE, PERFORMED DUCT BURNOUT. 2L72 4F4 FRTA6WE E9NE 20030416002142003041600214WP 2003 4 16 AALA20030057 120030108A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170401 49312 TUL - FOUND .1875 INCH CRACK EXTENDING FROM LOWER FASTENERS IN SHEAR TIE AT STATION 1380 ABOVE RIGHT ENGINE PYLON. INSTALLED DOUBLER PER AARD 53-30-00-02. (M) 2L72 4F A6WE 20030416001352003041600135NM 2003 4 16 AALA20030005 120030103A2910BACH8A04EE0557B HYDRAULIC LINE BOEING757 757223 1384957NM HYD SYSTEM RUPTURED A AALAK NONE K FLUID LOSS CRCRUISE 1 SW21691AA 25697 DFW - FLT 1108 - EN ROUTE CUN-DFW, CAPTAIN REPORT LEFT HYDRAULIC QUANTITY LOSS. CAPTAIN DECLARED EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. FOUND RUPTURED LINE IN LEFT WHEEL WELL. REPLACED LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030424001372003042400137EU 2003 4 24 UQR2003F00000 120030317A27521391T1005 ACTUATOR ISRAEL1124 1124 4500102EU GARRTTTFE731TFE73131G 29003NE LT TE FLAPS FAILED B UQRRO OTHER J WARNING INDICATION APAPPROACH 1 WP01140DR 242 P77223 ON APPROACH TO LANDING, THE FLAPS WERE MOVED FROM THE 12 DEGREE POSITION TO THE 20 DEGREE POSITION. AT THIS TIME THE AIRCRAFT BEGAN TO ROLL TO THE LEFT AND HAD TO BE CORRECTED BY FULL AILERON DEFLECTION TO THE RIGHT. THE CREW LANDED THE AIRCRAFT WITH FULL AILERON DEFLECTION AND FLAPS SELECTED TO THE 20 DEGREE POSITION. IT WAS DETERMINED THAT THE LEFT INBOARD ACTUATOR FAILED INTERNALLY AND DID NOT MOVE, CAUSING THE LEFT FLAP TO TWIST RATHER THAN EXTENDING. THE ASSYMETRY SYSTEM LOOKS AT THE OUTBOARD FLAP ACTUATORS, THEREFORE, THE UNBALANCE SYSTEM DID NOT SHUT OFF THE FLAP MOTOR UNTIL THE LEFT FLAP WAS BOUND UP COMPLETELY. 2M72 4F4 F A2SW E6WE 20030428000372003042800037WP 2003 4 28 ZW0A0303702 120030401A3350408822101 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139681B 53631 THE NEXT TO LAST RED EGRESS LIGHT ADJACENT TO AFT LAVS, AND THE LOWER LAMP IN EMERGENCY SLIDE LAMP TRIPLE FIXTURE IN TAIL CONE, WERE INOPERATIVE. RESEATED LAMP FOR EGRESS LIGHT, AND REPLACED BATTERIES IN POWER SUPPLY FOR TAIL CONE. CHECK-C 11-13-02 STL. 2L72 4F RTA6WE 20030430000472003043000047NM 2003 4 30 2003UALA00392 120030304A5754114W41607 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED. REMOVED, REPAIRED AND REINSTALLED WEDGE, NR 6 SLAT. 2L72 4F4 FRTT0001SE E46NE 20030430000742003043000074EU 2003 4 30 SIMA200307404 120030322A335066902 LIGHT SAAB SF340 340B 7860101EU ROW 8A & 7A INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21901AE 340B401 SJT - FLT 3676 - EMERGENCY EXIT FLOOR LIGHTING STRIP AT ROW 8A AND 7A BROKEN AWAY FROM SIDE WALL OF AIRCRAFT. WIRE LEADS BROKEN OFF AT FRONT STRIP. AIRCRAFT WAS FERRIED TO DFW FOR REPAIRS. REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IAW SAAB AMM 33-50-20. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030505000452003050500045NE 2003 5 5 ARWA20030404 220030413A732271128726 FUEL CONTROL DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 ENGINE MALFUNCTIONED A ARWAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO19661AV 45969 671003 NR 4 ENGINE HUNG START IN SKGO, SLOW TO SPOOL ON GROUND AND SLOW TO SPOOL IN FLIGHT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL UNIT (FCU) IAW DC-8 MM 73-20-1. LEAK CHECK OK. OPERATIONAL CHECK PERFORMED IAW MM 71-00 ON RUN UP FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20030505001622003050500162NM 2003 5 5 03FDEA00466 120030416A5410 SKIN BOEING727 727200 138407ENM NR 3 NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE NACELLE SKIN CHAFED AROUND NR 4 INBOARD LATCH. *S/D* REPAIRED SKIN AT NR 4 LATCH IAW BOEING 727-200 SRM 54-10-03. 2L73 4F RTA3WE 20030912000472003091200047WP 2003 9 12 DHL2003604676 120030707A5320 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT CARGO COMPT DOOR NR 4 FRAME ANGLE BROKEN, STA 1440.000 CORR REMOVED BROKEN ANGLE IAW SRM 51-3-0 PG 1. FABRICATED NEW ANGLE IAW SRM 53-2-0 PG 1-2. CLEANED, TREATED, AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030912000492003091200049WP 2003 9 12 DHL2003604533 120030430A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING- CTR L/E INNER PART DOUBLER CRACKED, XFS 322.750. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, IAW SRM 51-1-20D PG 21. FABRICATED NEW DOUBLER IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 14. CLEANED, TREATED AND PRIMED DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER ON CTR L/E INNER PART (RT WING) XFS 322.750 IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030912000562003091200056WP 2003 9 12 DHL2003604582 120030619A575556551662 SKIN DOUG DC8 DC873F 302199FWP NR 2 SPOILER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT NR 2 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 2 SPOILER ON RT WING IAW 27-81-1 PG 201-206. FOR OPS CHECK SEE N/R 0531. 2L74 4F RT4A25 20031001000642003100100064 2003 10 1 BAQA088952 420030922A22117004206901 COMPUTER BOLKMS117 BK117A1 5626010EU CSAS INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03136AE 7234 CSAS COMPUTER UNIT IS INOPERATIVE. REPLACED WITH REPAIRED, SERVICEABLE UNIT. 1G72 3U H13EU 20031002000362003100200036NM 2003 10 2 WRLA200318 120030831A2700 SENSOR DOUG MD11 MD11 3023602NM NR 2 ENGINE MALFUNCTIONED A WRLAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA27277WA 48743 AFTER TAKEOFF APPROX 800 FT LEVEL 3, NR 2 ENGINE ANTI-ICE DUCT ILLUMINATED TRI TONE SOUND. SHUT DOWN ENGINE NR 2 AS PER VOLUME 1, DUMPED FUEL AS PER VOLUME 1 RETURNED TO FIELD, DEPARTURE FIELD JTY. REPLACED NR 2 ANTI-ICE VALVE. SWAPPED NR 2 AND NR 3 PRESSURE SWITCHES. CHECKED DUCT DAMAGE NOT FOUND ANY DAMAGE. ESC RTS TEST PASSED. ANNUNCIATE LIGHT TEST (R2-5527 RESET) AND THEN ENGINE RUN-UP CHECKED (GROUND IDLE RUN EPR 1.21) ANTI-ICE SYSTEM NORMAL. THE DUCT OVERHEAT SENSORS WERE REPLACED IN LAX D1-91 AND D1-89. (M) 2L73 4F RTA22WE 20031002000462003100200046WP 2003 10 2 UPS03841202 120030825A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, RT WING LE UPPER SURFACE HAS 6 CRACKED FASTENER HOLES BETWEEN XFS 597.5 TO XFS 628.75. BLENDED OUT CORRODED AREAS, CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLER AND FILLERS I.A.W SRM. 57-2-1 FIG. 3B,57-3-0 FIG. 18. 2L74 4F RT4A25 20031001000942003100100094WP 2003 10 1 AMTA200301102 120030825A5310 SHEAR TIE LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 FRAME, SHEAR TIE CRACKED AND CORRODED OUT OF LIMITS AT FS 1800 FROM STRINGER 33 TO STRINGER 36. REMOVED CRACKED AND CORRODED SECTION OF SHEAR TIE AND REPLACED WITH NEW SECTION IAW SRM 51-40-01. (M) 2L73 4F A23WE 20031006000242003100600024NM 2003 10 6 QXEA200301119 120030904A5414 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 DIAPHRAM STRUCTURE AT AFT OUTBOARD SIDE OF LT HAND NACELLE STATION YW191.200 JUST BELOW UPPER WING SKIN TRAILING EDGE IS CRACKED. REPAIRED IAW Q400 SRM 51-40-11. 2H72 4T RTA13NM 20030908003292003090800329 2003 9 8 SWAA031905 420030826A2565D31354 SLIDE BOEING737 7372H4 138448CNM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20031028000062003102800006WP 2003 10 28 03FDEA01654 120030929A78309072M10P01 ADAPTER DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE ZONE 400 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25308FE 48297 EXHAUST THRUST REVERSER HAS A CHAFED UPPER ADAPTER. COMPLIED WITH E.A.8-7832-71004.EXHAUST THRUST REVERSER CHAFED UPPER ADAPTER. 2L73 4F4 F A22WE E23EA 20031027000052003102700005WP 2003 10 27 MWEA030391 120030925A5532591213071 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE VERTICAL STAB GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31209ME 47730 LEFT SIDE OF VERTICAL STABILIZER SKIN UNDER VERTICAL TO HORIZONTAL STABILIZER, FAIRING HAS A GOUGE FROM TOP SKIN RADIUS EXTENDING DOWN AT 1.5 INCHES. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F4 F A6WE E2EA 20031022001232003102200123NM 2003 10 22 QXEA200301173 120030921A2160 CONTROLLER DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09364PH 524 ON FLIGHT 2107 CABIN AUTO TEMPERATURE CONTROL INOPERATIVE. MANUAL MODE WORKS FINE AND FLIGHT COMPARTMENT AUTO-MANUAL WORK. RAN CHECKLIST AND RESET CIRCUIT BREAKER, STILL UNCONTROLLABLE IN CABIN AUTO MODE. PERFORMED FUNCTION TEST OF TEMPERATURE CONTROL SYSTEM TASK 21-60-00-720-801 IAW DHC-8 AMM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031028001272003102800127EA 2003 10 28 ASOA03481 120031004A5320601R3501163 SEAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE CARGO COMPARTMENT SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT SEAL PLATE IAW SRM 51-00. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031027000712003102700071EU 2003 10 27 MALA030430 120030918A5347 SEAT TRACK SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 DURING 4-K INSPECTION IN CWA, FOUND RT SEAT TRACK LBL WEB IS CORRODED. MAINTENANCE COMPLETED REPAIR IAW EO S53077 FROM STA 299-311. A/C RELEASE DATE IS 9/25/03 REF TO 409 193452 FOR DETAIL. 2L72 4T4 TRTA52EU E8NE 20031029000152003102900015 2003 10 29 ASAA0380530 420030707A25653961896501 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01953AS 49386 PDX - PREFLIGHT CHECK, FORWARD PAX (L-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20031029000452003102900045NM 2003 10 29 ASAA0310402 120030506A53306545775 SKIN BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND SKIN PANEL AT BS 901, STRINGER 23R DENTED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20040115001612004011500161NM 2004 1 15 DLM88031116 120031221A3260 SENSOR DOUG MD88 MD88 3023688NM LT MLG DIRTY A DALAK NONE N FALSE WARNING CLCLIMB 1 SO27976DL 53257 LT MAIN LDG GEAR LIGHT REMAINED ON WITH GEAR DOOR OPEN LIGHT ILLUM AFTER T/O. REFERRED TO POM AND CYCLED GEAR. WHEN LIGHT EXTINGUISHED MAIN GEAR DOOR EXT BEFORE LT MAIN LDG GEAR LIGHT. CLEANED LT MLG DOOR PROX SENSOR. RAN GEAR DOOR. IND NORMAL. NO FAULTS ON PSEU. 2L72 4F RTA6WE 20040127002402004012700240WP 2004 1 27 ASAA0380677 120031015A532199366921 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 OKC - DURING 30K CHECK, FOUND CABIN FLOORBOARD HAS 15 CORRODED INSERTS AT FS 1113-1174. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F A6WE 20040129001172004012900117EU 2004 1 29 0302203255 120031218A5315 FLOORBEAM AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01355NW 807 DURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 1292 FRAME 66. REPAIRED PER EA 32-197317. 2L72 4F RTA28NM 20040204001552004020400155NM 2004 2 4 EIA2003145 120031023A291060B0025436 HOSE BOEING747 747212B 1384886NM NR 3 HYD SYS CHAFED A EIAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09486EV 20888 AFTER TAKE-OFF NR 3 HYD SYSTEM QUANITY DROPPED TO ZERO, EDP PRESSURE INDICATING ZERO, ADP PRESSURE NORMAL. ON CHECK FOUND NR 3 ENGINE EDP PRESSURE HOSE CHAFED, REPLACED PRESSURE HOSE IAW MM 29-00-00, LEAK CHECK GOOD ON ENGINE RUN. 2L74 4F A20WE 20031030000532003103000053NM 2003 10 30 UPS03441316 120030903A5310 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, FX - BS 2300 FRAME BELOW FLOOR SHEAR TIE FOUND CORRODED AS MARKED AT BL 0. CORROSION BLEND OUT 0.050 X 1 X 2 INCH. M/D BS 2300 BL SHEAR TIE REPAIRED PER SRM 53-10-04 FIG 3. 2L74 4F A20WE 20031031000352003103100035EA 2003 10 31 COMA0370033 120030930A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01379CA1132 10102 FS 1098.20 BULKHEAD BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW MFG REO 670-53-61-034 REV. B. 2L72 4F4 FRTA21EA E15NE 20031031000642003103100064NM 2003 10 31 DLM88030829 120030909A2497 STUD DOUG MD88 MD88 3023688NM EPC LOOSE A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO27910DL 49541 ON CLIMBOUT LOST LT DC AND AC BUSSES WITH APU POWERING BUSS. APU VOLTS/FREQS GOOD. MULTIPAL C/B POPPED LT AC BUS BREAKER LT TR1 AND TR2 EMER AC BUS FEED - F25 F16. LOST FMS MPC DFGC LDC BUS MSG ILLUMINATED. REPLACED LT APU CONTROL RELAY AND GCU. 2L72 4F RTA6WE 20031106001082003110600108NM 2003 11 6 QXEA200301378 120031031A3150 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09406QX 4048 BZN- ON FLIGHT 2381 TAKEOFF WARNING HORN SOUNDS AS POWER LEVERS/TORQUE REACHED 50 PERCENT TORQUE. ABORTED TAKEOFF AT 79 KNTS. AUTOFEATHER FAILED TO ARM. COMPLIED WITH AUTOFEATHER TEST, GROUND RAN AIRCRAFT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031106000412003110600041NM 2003 11 6 SWAA032292 120031017A3350BR2013 LIGHT BOEING737 7375H4 138449DNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29505SW 24182 EEPLS INOP BETWEEN ROWS NR 10 AND 11. REPAIRED EEPLS PER MM. 2L72 4F RTA16WE 20031110000502003111000050SO 2003 11 10 RAIA00310273 120031028A34110851HU PITOT TUBE EMB 145 EMB145 3260210SO NR 2 INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03802HK12438 145066 5304-RDU- PITOT NR 2 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 2 PITOT TUBE. 2L72 4F RTT00011AT 20031110001432003111000143NE 2003 11 10 03293421 220031020A7320 EEC DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE FAILED A VTZABE EMER. DESCENT ENGINE SHUTDOWN O OTHER DEDESCENT 1 EA27421FJ 3179 DURING DESCENT CREW REPORTED A LT FADEC FAULT WITH NO ITT INDICATION. CREW SHUT DOWN ENGINE AS A PRECAUTION AND DECLARED EMERGENCY. FLIGHT LANDED UNEVENTFULLY. THE EEC WAS REPLACED 2H72 4T4 FRTA55NM E35NE 20031113000032003111300003EU 2003 11 13 BAQA089814 120031007A7712G555674 TRANSDUCER BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101650B1 41560NE NR 2 ENGINE FLUCTUATES B BAQAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 EA03945ME 7235 ENGINE NR 2 TORQUE FLUCTUATIONS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20031118000152003111800015WP 2003 11 18 UPS03841358 120031007A3350 LIGHT DOUG DC8 DC873F 302199FWP ENTRY DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: N/A ONE EMERGENCY LIGHT INOPERATIVE AT CREW ENTRY DOOR. RELAMPED. OPS CK OKAY. 2L74 4F RT4A25 20040112001672004011200167WP 2004 1 12 AALA20031229 120031106A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21413AA 49324 DFW - DURING OVERNIGHT MAINTENANCE, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 INOPERATIVE. REPLACED BATTERY FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 7 THROUGH 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040112002252004011200225 2004 1 12 SWAA032799 420031222A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 R2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20040113000402004011300040CE 2004 1 13 BAQA090302 120031028A323166003611 SOLENOID VALVE LEAR 55 55LEAR 5170702CE MLG LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 11343 092 SOLENOID VALVE LEAKING. REPLACED WITH SERVICEABLE UNIT. 2L72 4F A10CE 20040113000032004011300003EU 2004 1 13 BAQA091571 120031208A6320 BEARING UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE LEVER WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME 051810 0009 BEARINGS AND BUSHINGS WORN. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 UO H88EU E42NE 20040114000762004011400076NM 2004 1 14 03FDEA01960 120031121A5510 BARREL NUT DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB RIGHT UPPER FWD SPAR NR 1R BARREL NUT BORE FOUND CORROSION EXCEEDED EO 1-5510-7-5000 LIMITATIONS. HOR STAB RH UPPER FWD SPAR #1R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. 2L73 4F RTA22WE 20031212001182003121200118NM 2003 12 12 SWAA032501 120031112A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT ROW 3. REPAIRED EEPLS WIRE PER MM. 2L72 4F A16WE 20031218000252003121800025NM 2003 12 18 0302116314 120031124A3350 LAMP BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01674US 30269 DURING L-CHECK, FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 10L-22L. RELAMPED EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20031223001702003122300170EU 2003 12 23 ASOA03544 120031029A33503011210 LIGHT AEROSPATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGTH WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031231000882003123100088WP 2003 12 31 GTIA030929 120031110A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND CABIN FLOOR PANEL AT FS 400-480 DELAMINATED. FABRICATED NEW PANEL. (M) 2L72 4F RTA6WE 20031229000212003122900021NM 2003 12 29 250TR 120031212A33506104789 BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 RIGHT HAND OVERWING & FLAP EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK M193 AND REFLECTOR. OPS CHECKS GOOD PER MM 33-51-1. 2L72 4F RTA16WE 20031229001542003122900154EA 2003 12 29 SWIA200312659 120031205A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 280 RT FLOORBEAM RBL 90 INBOARD AND OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 & RII 53-401. 2L72 4F RTA21EA 20031124000982003112400098WP 2003 11 24 DHL2003805504 120030813A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER CRACKED 4.000, AT STA XFS 341.500 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER IAW SRM 57-2-0 PG 9-10 (7075-T6 0.040). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON RIGHT WING CTR L/E FORMER, STA XFS 341.500 (LWR PART) IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 1. 2L74 4F RT4A25 20031125000122003112500012WP 2003 11 25 DHL2003805526 120030803A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 467.323 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 9 SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20031125001272003112500127NM 2003 11 25 ASAA0310265 120030401A5320 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIR INTERCOSTAL ANGLE AT BS 947-948, WATERLINE 206-208 CORRODED. REPLACED ANGLE PER SRM. (M) 2L72 4F RTA16WE 20031125001592003112500159NM 2003 11 25 ASAA0310414 120030509A532065458059 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND STRINGER CLIP AT BODY STATION 277, STRINGER 26L CRACKED. REPLACED STRINGER CLIP PER SRM. (M) 2L72 4F A16WE 20031126001042003112600104SO 2003 11 26 C2XA03SH463 120031119A531514532636401 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER REINFORCEMENT REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030506001702003050600170WP 2003 5 6 ASAA0380247 120030307A32013961989501 GUARD DOUG DC9 DC982 3022082WP LT MLG CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND LEFT MLG SPLASH GUARD CRACKED AT WELD. REPLACED WELDED AREA PER MM PROCEDURES. (M) 2L72 4F A6WE 20030508001232003050800123NM 2003 5 8 UPS03440618 120030412A575465B101485 RIB BOEING747 747121 1384871NM NR 9 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C LHW, NR 9 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 3 ( VIEW FROM I/B ). RIB MOUNT BOLT HOLE BORE EXCEED LIMIT AFTER CORR BLEND OUT. SUPPORT RIB REPLACED AS PER SRM 51-10-01 PAGE 8 AT LHW NR 9 VC FLAP O/B I/B ROTARY ACTUATOR ATTACH. 2L74 4F A20WE 20030509001422003050900142EU 2003 5 9 MALA030264 120030508A2930 INDICATOR SAAB SF340 SF340A 7850100EU HYD PRESSURE MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1598XJ 340A098 MAIN HYDRAULIC PRESSURE INDICATED ZERO INFLIGHT. HYD CAUTION LIGHT ILLUMINATED ON CLIMBOUT. RETRACTING GEAR WAS NORMAL FOLLOWED APPRORIATE QRH LISTS. AIR RETURN TO MSP. MAINTENANCE FOUND HYDRAULIC PRESSURE INDICATOR DROPPING TO ZERO INTEMITTANTLY REPLACED INDICATOR OPS CHECKS GOOD. 2L72 4T RTA52EU 20030513002592003051300259EU 2003 5 13 A6WA200360016 120030424A5414 PANEL BAC 146 146200A 1500266EU NR 4 PYLON CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 NR 4 PYLON PANEL 481 AT LOWER FORWARD RIGHT ATTACH HOLE CHAFED BADLY FROM LOOSE AND VIBRATING SCREW. HOLE WORN EXCESSIVELY. REPAIRED PANEL IAW BARA/AVR/6361/03-D. (M) 2H74 4F A49EU 20030530000222003053000022SW 2003 5 30 HEEA086676 120030522A6510212040600005 HANGER ASSY BELL 412 412 1182202SW T/R DRIVE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 TAIL ROTOR DRIVE SPLINES HAVE LARGE DEEP PIT. IN REPAIR. 1G72 4U H4SW 20030602000382003060200038NM 2003 6 2 CA030513004 120030512A323282970019007 CYLINDER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG DOOR ACT CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 14465 (CAN) REMOVED FROM AIRCRAFT, GEAR NOT RETRACTING FULLY. DURING OVERHAUL IN THE SHOP, MAJOR CORROSION WAS NOTED IN THE UPLOCK ROD BORE, RENDERING THE HOUSING BER. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030602000472003060200047SO 2003 6 2 AUS20030413 220030403A7310630119 FITTING PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360E 17025SO HARTZLHCC2Y BHCC2YF2 GL FUEL DIST FRACTURED W O OTHER KE FLUID LOSS VIBRATION/BUFFET CRCRUISE 1 AUS 1270 (AUS) LEFT ENGINE FUEL LINE FITTING FAILED. FUEL LEAK. 1L72 3O3 O A7SO E9CE 5 CP920 20030529000802003052900080 2003 5 29 HEEA086654 420030521A2340A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 LIGHTED PANEL WORN OUT AROUND SELECTOR KNOB. REPLACED BAD LIGHT PANEL AND BAD S6 SWITCH, BAD SELECTOR KNOB AND BAD VOLUME KNOB. BENCH CHECK GOOD. 1G72 4U H4SW 20030604001162003060400116NM 2003 6 4 UPS03440531 120030413A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 960 FRAME CRACKED BTN S11-12L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20030605001202003060500120WP 2003 6 5 MEX2003147 120030427A7500 HEAT EXCHANGER DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE NR 2 ENGINE FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23216AM3259717433 49586 AIRCRAFT RETURN TO PLATFORM, ENGINE NR 2, FUEL LEAK. THE FUEL/OIL TEMPERATURE EXCHANGER WAS REPLACED IAW MM, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20030515001522003051500152EU 2003 5 15 142691 120030424A6120 CONNECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE AUTOCOARSEN LOOSE A UHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL17123XS 123 360 DRG486887 FLIGHT 4550 FWA-PIT. DURING TAXIING FROM GATE THE AUTOCOARSEN CAUTION LIGHT ILLUMINATED AFTER THE AUTOCOARSEN SYSTEM WAS SELECTED ON. A/C RETURNED TO GATE AND WAS TAKEN OUT OF SERVICE AT 0500 4-24-03. FLIGHTS SWAPPED TO A/C 101CN. DURING TROUBLESHOOTING FWA MX FOUND THE CANNON PLUG BETWEEN THE LH P3 SWITCH & 161VP P8 LOOSE. FWA MX RESEATED THE SAME CONNECTOR, PERFORMED GROUND RUNS FOR OPERATIONAL CHECKS OF THE AUTOCOARSENING SYSTEM. OPERATIONAL CHECKS WERE SATISFACTORY. A/C RETURNED TO SERVICE AT 1646 4-24-03. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030521001092003052100109WP 2003 5 21 DHL2003801039 120030415A5311 FRAME DOUG DC8 DC873F 302199FWP TAIL CONE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 TAIL CONE RT FRAME WITH 0.750 INCH CRACK IN STA 1940.000. REMOVED FASTENERS IAW SRM 51-1-21A PG 1-4, SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA 1940.000 IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-20 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21A PG 1-4 AND SRM 1-1-21 PG 1. 2L74 4F RT4A25 20030521001272003052100127NM 2003 5 21 DHL2003720004 120030515A2611 SMOKE DETECTOR BOEING727 727228 1384083NM NR 3 WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01720DH 19544 ON PRE-FLIGHT FOUND NR 3 SMOKE DETECTOR RT NOT TESTING. ITEM PLACED ON DMI LIST IAW MEL 26-14-1 CONTROL NR 12940 CAT-C. PLACARD INSTALLED. REF DMI NR 12940, ON PRE-FLIGHT FOUND NR 3 SMOKE DETECTOR RT NOT TESTING. REMOVED AND REPLACED DETECTOR NR 3 RT TEST LAMP, OPS CHECKED GOOD IAW BMM CHAPTER 26-17-00. THIS CLEARS DMI 12940. 2L73 4F RTA3WE 20030522000602003052200060WP 2003 5 22 0300889921 120030505A2150 A/C PACK DOUG DC9 DC932 3022066WP SMOKE A NWAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL01943N 47647 AFTER TAKEOFF A HOT HEAVY RUBBER SMELL WENT THROUGHT THE CABIN AND COCKPIT. THE FORWARD LAVATORY DETECTOR ACTIVATED AND THE LEFT AIR COND TEMP HI LIGHT ILLUMINATED SOON AFTERWARDS. COM COMPLIED WITH, AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO GTF. LANDING WAS UNEVENTFUL AND THE LIGHT EXTINGUISHED ALONG WITH THE ODOR DISSIPATING. SOON AFTER THE LEFT PACK WAS SHUTDOWN. MAINTENANCE PLACED THE LEFT PACK ON MEL AS NO TROUBLE WAS FOUND IN GTF. AIRCRAFT HAS RETURNED TO MSP FOR CONTINUED MAINTENANCE. 2L72 4F A6WE 20030612001052003061200105NE 2003 6 12 CALA0300280 220030601A7200 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE FAILED A CALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW2714816 49370 717362 THE AIRFRAME SHUDDERED SLIGHTLY AND WAS ACCOMPANIED BY AN AUDIBLE BOOM AFTER TAKEOFF FROM IAH AT ABOUT 3,000 FEET. THE NR 1 ENGINE SUBSEQUENTLY AUTO SHUTDOWN. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. INITIAL FINDINGS REVEALED METAL IN THE TAILPIPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. EXAMINATION OF THE ENGINE REVEALED HEAVY DAMAGE TO THE HPC 12TH AND 13TH STAGES WITH METAL IN THE TAILPIPE FROM HPC STATOR VANE. THE ENGINE WAS NEVER REPAIRED. THE AIRCRAFT IS EXITING THE CONTINENTAL FLEET. 2L72 4F4 F A6WE E9NE 20031202001672003120200167NM 2003 12 2 ASAA0310253 120030327A53116554957507 FRAME BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FRAME AT BS 500A, STRINGER 24L DENTED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040116000132004011600013NM 2004 1 16 03FDEA02188 120031215A5753ARC74901 FITTING DOUG MD11 MD11 3023602NM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RIGHT WING INBOARD FLAP VANE INBOARD ATTACHMENT T- FITTING, 3 EA HOLE BORE SIZE EXCEED LIMIT. INBD FLAP VANE OUTBD ATTACHMENT 'T' FITTING REMOVED AND INSTALLED NEW FITTING AS PER AMM 27-50-22. 2L73 4F RTA22WE 20040121000352004012100035NM 2004 1 21 03FDEA02312 120031229A5311ADA0049 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 FRAME ADJACENT TO LONGERON 12 AT LT STA 1541 FOUND WITH DENT. STA 1541 LONGERON 12L DENT FRAME REPAIRED AS PER SRM 53- 30-00 FIG. 1 VOL. I AND FEDEX EA 1-5310-75223 - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NO. 1-2520-7- 3308). 2L73 4F RTA22WE 20040121001052004012100105NM 2004 1 21 03FDEA02330 120031230A5753ARC119113 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LT WING OUTBOARD FLAP OUTBOARD HINGE FITTING OUTBOARD PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75201, TRAILING EDGE AND TRAILING EDGE DEVICES- LT OUTBOARD. FLAP. OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040122000472004012200047WP 2004 1 22 2004F00050 120030823A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A A4JAK NONE O OTHER ININSP/MAINT 1 SO35418GE 49418 DURING MAINTENANCE IN PIE, THE MID CABI HAD SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. A LOOSE WIRE TO THE CONNECTOR AT MID CABIN SECTION WAS FOUND, RESECURED IAW MD80 MM 33-53-0. OPS CHECK GOOD. (M) 2L72 4F A6WE 20040123000032004012300003WP 2004 1 23 ASAA0380699 120031028A53475936663505 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND AFT CARGO BAY TIE DOWN TRACK IS CORRODED. REPLACED TIE DOWN TRACK EPR SRM 51-30-1. (M) 2L72 4F RTA6WE 20040120000112004012000011 2004 1 20 2003UALA00979 420031220A2330285W00351 CONTROL UNIT BOEING777 777222 1385219NM PWA PW4077PW4077 NE SEAT SEU FAILED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29781UA 26945 SMOKE AND ODOR REPORTED IN CABIN. F/A DISCONNECTED SEVERAL WIRES UNDER 19C AND 18C, CREW REPORTED GALLEY POWER AND SEAT POWER TURNED OFF PRECAUTIONARY, SMOKE AND ODOR DISSAPATED. SEAT ELECTRONIC UNIT AT SEAT 18D FAILED. UNIT WAS REPLACED. SYSTEM OP NORMAL. UNIT WAS OPENED IN SHOP AND CAPACITOR WAS FOUND BURNED. 2L72 4F4 FRTT0001SE E46NE 20031208000162003120800016 2003 12 8 UPS03841578 420031126A2565 GIRT BAR DOUG DC8 DC873F 302199FWP PAX DOOR SLIDE OUT OF POSITION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: PFLT, MAIN CABIN DOOR GIRT BAR WON'T ATTACH TO FLOOR MOUNTS. MAIN CABIN DOOR SLIDE DEFERRED PER MEL 52-7-4 REF M271227. REPOSITIONED GIRT BAR, CHECKS OK. REF LP90923 2L74 4F RT4A25 20031209000612003120900061NM 2003 12 9 SWAA032361 120031026A57536546434370 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED C4 CHECK, FOUND RT WING INBD AFT T/E FLAP DISBONDED AT OUTBD END. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20031210000372003121000037NM 2003 12 10 UPS03M41571 120031121A4950 PANEL DOUG MD11 MD11F 3023600NM APU DIRTY A IPXAK NONE J WARNING INDICATION CLCLIMB 1 SO01253UP INSPECTION TYPE:N/A AFTER ENGINE START (ALL 3) APU SHUT DOWN. LOST ENG NR 2 PNEUMATIC BLEED. MX DEF THE WRITE UP AND MANUALLY LOCKED THE NR 2 BLEED VALVE CLOSED. AFTER T/O & CLIMBING OUT PASSING AT 10,000 RECVD AIR SYS 1 PRESSURE LOW LIGHT. LOST THE PRESSURE ON 1 PNEUMATIC SYSTEM. IN AUTOMATIC MODE & SYS 3 DID NOT P/U SYS 1 OR 2. INSPECTED SYSTEM DEFERRED APU LOAD BLEED VALVE 49-51-1-1DMP COMPLIED W/ACTIVATED NR 2 SYSTEM PLACARD INSTALLED DI M270927 REMOVED & CLEANED C/P'S ON LOAD CONTROL VALVE CLEARED ALL FAULTS FROM CFDS OPS TEST OF APU BLEED SYS NORMAL. NO FAULTS, OK FOR SERVICE. THIS CLEARS M270927. 2L73 4F RTA22WE 20040128000262004012800026SO 2004 1 28 RAIA00312323 120031221A801135059105 STARTER EMB 145 EMB145LR 3260212SO NR 1 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03810HK9721 3876 145231 PIT- NR 1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 AIR TURBINE STARTER. 2L72 4T RTT00011AT 20031014000522003101400052NM 2003 10 14 SWAA032182 120031001A575465C26602312 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED A1 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END UPPER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2L72 4F RTA16WE 20031009001242003100900124NE 2003 10 9 QXEA200301137 220030916A7520310848802 VALVE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 400 MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09354PH 498 AG0085 ON FLIGHT 2208 BLEED SMOKE IN CABIN. REMOVED AND REPLACED NO.2 ENGINE P2.5/P3 SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20031210001262003121000126NM 2003 12 10 03FDEA02093 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 02 EA LOCK BOLT COLLARS CRACKED. LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL.II & INSTALLED AS PER SRM 51-33-01, VOL.II. 2L73 4F RTA22WE 20031210001462003121000146EU 2003 12 10 AALA20031362 120031202A3350P4010051124 CHARGER AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW218067A 510 JFK IN SEAT EMERGENCY LIGHTS AT ROWS 7C THROUGH 17C INOPERATIVE. REPLACED CHARGER AND BATTERY FOR IN SEAT EMERGENCY LIGHTS AT ROWS 7C THROUGH 17C. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA35EU 20030613000392003061300039 2003 6 13 SWIA200311995 420030514A3418 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07433SW 7550 PILOT STICK SHAKER INOP. BROKEN WIRE. DISCOVERED DURING C-CHECK. INSTALLED NEW TERMINAL ENDS ON PILOT SIDE STICK SHAKER WIRES IAW AWM CHAPTER 27-35-00. OPS TESTED SPS (PRE-FLIGHT TEST) IAW AMM TASK 27-35-01-710-801. TEST SERVICEABLE. 2L72 4F4 FRTA21EA E15NE 20030617002612003061700261SW 2003 6 17 HEEA087481 120030612A6321D01631 PAD BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 ROTOR BRAKE PAD WORN. 1G71 3U O H2SW 20030617000092003061700009NM 2003 6 17 AUS20030476 120030506A5410 FAIRING BOEING747 747438 NM RROYCERB211 RB211524G19 NE NR 2 ENGINE MISSING W K NONE OD OTHER INFLIGHT SEPARATION ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE TRANSFER DRIVE FAIRING MISSING. DAMAGE TO BLOCKERDOORS AND FLAPS. 2L74 4F4 FRTA20WE E30NE 20030523000522003052300052 2003 5 23 SWAA031113 420030518A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD PAX DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030527001052003052700105CE 2003 5 27 2003F00315 120030424A3240A41130 SWITCH CESSNA750 750 2076810CE BRAKE SYSTEM BROKEN A UG8AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL235112 7500010 DURING TAXI TO TAKEOFF, THE NO TAKEOFF CAUTION APPEARED ON THE EICAS. SIMULTANEOUSLY, THE PARK BRAKE PRESS LOW MESSAGE WAS ILLUMINATED. THE CREW TAXIED BACK TO GM BASE AND ANOTHER AIRCRAFT WAS UTILIZED FOR THE FLIGHT. UPON TROUBLESHOOTING, THE PARK BRAKE SWITCH WAS FOUND TO BE FAULTY. THE CONTACT PLUNGER HAD DETERIORATED, THUS NO ACTUATING THE CONTACTS. SWITCH WAS REPLCED AND OPERATION WAS NORMAL. (M) 2L72 4J RTT00007WI 20030617003082003061700308NM 2003 6 17 SWAA031264 120030608A53116935365 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BELOW STR 14L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030618001312003061800131NE 2003 6 18 HEEA087138 120030610A29107665009801105 MODULE SKRSKYS76 S76C 8143008NE HYD SYS CLOGGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 MODULE RETURN FILTER CLOGGING. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20030620000582003062000058EA 2003 6 20 ASOA03232 120030523A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11849AS 7347 FLT 4677 - DURING APPROACH INTO ATL FROM MCN, THE CREW SELECTED GEAR DOWN BUT THE NOSE GEAR WOULD NOT EXTEND. A GEAR DISAGREE WARNING WAS RECEIVED AND QRH PROCEDURES WERE COMPLIED WITH. THE CREW TURNED OFF HYDRAULIC 3A AND 3B AND THE NOSE GEAR EXTENDED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT, NOSE LANDING GEAR SELECTOR AND PRIORITY VALVES. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030618001802003061800180GL 2003 6 18 HEEA087518 220030610A753223053176 BLEED VALVE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035031U S678 ENGINE RUNNING HOT. SHOP REPAIR. 1G72 3U3 U H3EU E4CE 20030624000992003062400099NM 2003 6 24 DLM88030473 120030518A3897 WIRE DOUG MD88 MD88 3023688NM POT WATER SWITCHBURNED A DALAK NONE O OTHER ININSP/MAINT 1 SO27904DL 49535 POTABLE WATER FILL/VENT VALVE C/B POPPING AND WILL NOT RESET FOUND POTABLE WATER SELECTOR SWITCH AND SOME ASSOCIATED WIRING CHARED. REPLACED SWITCH AND REPAIRED DAMAGED WIRING. 2L72 4F RTA6WE 20030707001382003070700138NM 2003 7 7 AWXA200300711 120030617A29131009202397 PACKING AIRBUSA319 A319132 3930340NM NR 1 ENGINE FAILED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 WP28818AW 1375 ON APPROACH INTO PHX EN ROUTE FROM PHL RECEIVED GREEN HYDRAULIC SYSTEM LOW LEVEL INDICATION ON LIGHT PANEL. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE SERVICED 6 QUARTS IN GREEN HYDRAULIC SYSTEM AND INSPECTED AIRCRAFT FOR EVIDENCE OF HYDRAULIC LEAKS, NO LEAKS WERE NOTED. ON ENGINE START HYDRAULIC FLUID WAS FOUND DRIPPING FROM NR 1 ENGINE DRAIN MAST. INSPECTED NR 1 ENGINE AND DISCOVERED FLUID LEAK AT PRESSURE LINE FITTING THAT CONNECTS TO NR 1 ENGINE DRIVEN HYDRAULIC PUMP. REMOVED AND REPLACED O-RING SEAL AT FITTING OF HYDRAULIC PUMP, RAN ENGINE, LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20030709000752003070900075EA 2003 7 9 03155625 120030604A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 DURING MAINTENANCE INSPECTION, THE LT MID OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030711000192003071100019SO 2003 7 11 C2XA03SH196 120030622A532014524131001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK THE MAIN DOOR SILL WAS FOUND TO HAVE CORROSION AROUND NUT PLATES. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030714000702003071400070 2003 7 14 SWAA031385 420030621A256565C19901 CABLE BOEING737 7373H4 1384600NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20030714001262003071400126EU 2003 7 14 DHL2003367005 120030701A2612 CONTROLLER AIRBUS300 A300B4203 3930306EU FIRE DETECTOR MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01367DH 265 WHEN TESTING FIRE DETECT LOOPS, ENGINE NR 1 FIRE WARNING LIGHT ON MASTER WARNING PANEL WILL NOT COME ON EITHER ON -A- OR -B- LOOPS. REPLACED MASTER WARNING CONTROLLER AS PER M/M 33-15-11. OPS CHECKED NORMAL. TEST PER M/M 33-15-00. OK FOR SERVICE. 2L72 4F RTA35EU 20030717000852003071700085SW 2003 7 17 HEEA088077 120030708A5340206033109001 FITTING BELL 206 206L3 1182108SW FUSELAGE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 EXCESSIVE WEAR FROM EARS ON CROSSTUBE PAD. REPLACED FITTINGS. 1G71 3U H2SW 20030115002202003011500220NM 2003 1 15 QXEA0300079 120030112A308010200002 SWITCH BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09404QX 4046 PDX- DE-ICE PRESSURE CAUTION LIGHT IN FLIGHT. ISOLATED SYSTEM AS PER CHECKLIST. ALL BOOT INDICATIONS NORMAL EXCEPT NO.2 INBOARD TAIL BOOT ILLUMINATED LATE AND STAYED ILLUMINATED LONGER THAN NORMAL. DE-ICE PRESSURE INDICATED 17 PSI ON NO.1 AND 21 PSI ON NO.2. REMOVED AND REPLACED NO.2 LOW PRESSURE WARNING SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030116000512003011600051SW 2003 1 16 HEEA083010 120030106A5210 FITTING BELL 206 206L3 1182108SW STRUT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671 51301 RIGHT REAR DOOR STRUT END FITTINGS WORN. SCRAPPED. 1G71 3U H2SW 20030116001942003011600194 2003 1 16 HEEA083106 420030108A3457 CONNECTOR BELL 206 206L1 1182107SW GPS ANTENNA LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032764F 2022041 45279 FITTING CONNECTOR LOOSE IN BASE OF ANTENNA (INTERMITTENT SIGNAL). SCRAPPED. 1G71 3U H2SW 20030103000662003010300066EU 2003 1 3 RAIA00301001 120030101A2700L850178 STALL WARNING JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03571HK 41090 5538-STL- STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE STALL WARNING VANE, OPS CK OK. 2L72 4T RTA41NM 20030213000692003021300069NM 2003 2 13 0300116717 120030115A2612 CONTROL BOX BOEING747 747251F 1384898NM FIRE WARNING MALFUNCTIONED A NWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL01617US 21121 DURING FLIGHT, THE FIRE WARNING LIGHTS CAME ON DIM AND FIRE WARNING BELL SOUNDED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE AURAL WARNING CONTROL BOX. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030214000542003021400054WP 2003 2 14 ASAA0380035 120030104A532199578053 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23972AS 53448 OKC - FOUND DURING 30K CHECK, COCKPIT LEFT SIDE FORWARD FLOOR PANEL IS CRACKED. REPAIRED CRACK PER MM 25-00-00, 3E. (M) 2L72 4F RTA6WE 20030218001742003021800174NM 2003 2 18 QXEA0300166 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 4 SEAT TRACK HAS CHAFING AT STATION 338. REPAIRED IAW RD 8-26-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030221000532003022100053NM 2003 2 21 AWXA200300079 120030110A531265163007 BULKHEAD BOEING737 737300 1384610NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C-14 CHECK A 1 INCH CRACK WAS FOUND BS 178 BULKHEAD WEB, LBL 5.7, WL 212.5. MAINTENANCE REMOVED STIFFENER AND "L" ANGLE TO ACCESS DAMAGE; CUTOUT CRACKED AREA OF BS 178 BULKHEAD WEB, LBL 5.7, WL 212.5; PERFORMED A HFEC INSPECTION OF CUOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS AND REMOVED STIFFENER AND "L" ANGLE IAW B737-300 SRM 53-10-08, PG. 287-288J, FIG. 211. 2L72 4F RTA16WE 20030224001002003022400100WP 2003 2 24 MWEA030111 120030222A25109957871502 FLANGE DOUG DC9 DC932 3022066WP COCKPIT ELONGATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 FIRST OFFICER AFT INBOARD SEAT TRACK FOUND ENLONGATED HOLES. -- REMOVED AND REPLACED UPPER FLANGE OF FIRST OFFICER'S INBOARD SEAT TRACK. 2L72 4F A6WE 20030625001032003062500103NM 2003 6 25 F3LA200300084 120030220A5320 WEB BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED WEB BETWEEN STA. 332 AND STA. 344, AFT OF R-1 DOOR, CORRODED ON BOTTOM SIDE. REMOVED DAMAGE ON WEB, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2, PAGES 1-3 AND SOPM 20-41-02. 2L72 4U RTA16WE 20030307000422003030700042NM 2003 3 7 SWAA030458 120030228A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29744SW 29490 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW NR 2 AND ROW NR 21. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20030307001042003030700104NE 2003 3 7 HEEA084902 120030228A6220 BEARING SKRSKYS76 S76A 8143006NE LEVER ASSY WORN E O OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 MAIN ROTOR HEAD LEVER ASSY BEARINGS ARE WORN. IN SHOP REPAIR. 1G72 3U H1NE 20030312000512003031200051WP 2003 3 12 CALA0300113 120030307A5754 SKIN DOUG DC9 DC981 3022081WP FLAP VANE DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914871 48022 MAINTENANCE FOUND THE R/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED. THE FINAL TRIM OUT AREA MEASURED 4.3" X 6.4". THE SKIN WAS REPAIRED IAW ECRA 5750-03756. 2L72 4F A6WE 20030318001852003031800185 2003 3 18 P5CA0300779 420030314A3443270409 ANTENNA BOEING747 747200 1384847NM INOP ANTENNA MALFUNCTIONED A P5CAK NONE O OTHER CRCRUISE 1 WP23524UP 21446 BOTH WEATHER RADAR SYS INOP NO RETURN & TEST FUNCTION. REPLACED WEATHER RADAR ANTENNA. OPS CHK ACCOMPLISHED PER MM 34-43-00 2L74 4F RTA20WE 20030401000892003040100089NM 2003 4 1 DHL2003746003 120030313A2612 FIRE DETECTOR BOEING727 727224 1384076NM APU WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01746DH 22252 APU FIRE TEST INOPERATIVE. TRANSFERRED TO DMI 12262 MEL 26-11 CAT-C. PLACARD INSTALLED. IN REF TO DMI 12262. APU FIRE TEST INOPERATIVE. REMOVED AND REPLACED APU FIRE TEST RELAY. NO HELP, DMI 12262 REMAINS OPEN. 2L73 4F A3WE 20030122000012003012200001 2003 1 22 HEEA083388 420030109A344280510800001 CONTROL BOX BELL 206 206L3 1182108SW WX RADAR SYSTEM FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03906PH 51048 DISPLAYED INPUT FAIL AND DISPLAYS FAIL WHEN PERFORMING SELF TEST. 1G71 3U H2SW 20030123000072003012300007SO 2003 1 23 C2XA03CL021 120030122A3350GS8506DC WIRE EMB 145 EMB145ER 3260211SO CABIN BROKEN A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2715941 145035 MKE FLIGHT#2135 THE CREW REPORTED THE EMERGENCY EXIT AISLE PATH LIGHTING FROM ROW 7 FORWARD WAS INOPERATIVE.THEY ALSO REPORTED THE EXIT LIGHT ON THE FORWARD CABIN PARTITION AND THE LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED A BROKEN GROUND WIRE (GS8506DC)FOR THE EMERGENCY LIGHTS BATTERY 2,INVERTER 2 AND INVERTER 3.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030123000382003012300038NM 2003 1 23 2003UALA00061 120030115A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 CABIN FLOORBEAM STATION 947, RBL10 TO RBL53, WL 208 UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030320001832003032000183NM 2003 3 20 SWAA030606 120030317A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ( 4 EA ) AT STR 14L, BS 430, BS 460, BS 471 & BS 500. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030731000602003073100060NM 2003 7 31 QXEA200300879 120030721A2611302133 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY WILL NOT TEST A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09358PH4080 506 PSC-ON FLIGHT NUMBER 2105, NR 2 TEST BAGGAGE SMOKE WARNING WILL NOT TEST. REMOVE AND REPLACED NR 2 BAGGAGE SMOKE DECTECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030801000112003080100011NM 2003 8 1 AMTA200300770 120030612A3397 WIRE BOEING757 75723N 1384973NM CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 EGRESS FLOOR LIGHTING INOPERATIVE FROM SEAT ROW 22 TO 31. RECONNECTED WIRES TO EGRESS LIGHT AT ROW 28 AND AT ROW 30. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030731001152003073100115NM 2003 7 31 QXEA200300792 120030622A5551 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB GROOVED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - LEFT HAND FORWARD ATTACH POINT FOR HORIZONTAL STAB HAS GROOVE CUT INTO BORE FOR BARREL NUT ON FORWARD AND AFT SIDES. REPAIRED IAW Q400 SRM 51-14-00, PAGE 221, TASK 51-14-00-350-804. 2H72 4T RTA13NM 20030326000672003032600067 2003 3 26 CA030205006 420030205A6122CT2CE10381 CAM DHAV DHC2 DHC2MK3 2800107EA PWA PT6 PT6A27 52043EA HARTZLHCB3T HCB3TN3 GL PROP GOVERNOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1305213052 (CAN) DURING INSPECTION CRACKS WERE FOUND ON THE CAM ASSY FOR THE PROP GOVERNOR. THE CRACKS WERE LOCATED WHERE THE SCREWS ATTACH THE BRACKET ASSY TO THE ENGINE FIRE WALL. FIG 76 ITEM 24 IN THE TURBO BEAVER IPC. BRACKET WAS REPLACED WITH A NEW UNIT FROM VIKING AIRCRAFT. 1H71 3T4 T A806 E4EA 6 CP15EA 20030326000052003032600005EU 2003 3 26 AUS20030090 120030129A3230HP848430721 CONTROL VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE MLG FAULTY W O OTHER O OTHER DEDESCENT 1 AUS 4934 (AUS) LANDING GEAR CONTROL VALVE SUSPECT FAULTY. (P) 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20030327000972003032700097SO 2003 3 27 C2XA03CL003 120030104A32348271011 SELECTOR EMB 145 EMB145ER 3260211SO MLG INOPERATIVE A C2XAO OTHER O OTHER CLCLIMB 1 SW2712934 145019 CLE FLIGHT 3014 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT UNLESS THE DOWNLOCK RELEASE BUTTON WAS PRESSED. MAINTENANCE REPLACED THE LANDING GEAR LEVER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030421000152003042100015SO 2003 4 21 G1159A 120030225A215020392541 COOLING TURBINE GULSTMG1159 G1159A 3970109SO ZONE 200 ODOR E KKYAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NE03165G 4253 414 CLIMBING THRU 3000 FT CABIN FILLED WITH SMOKE EXITING FROM VENTILATION DUCTS. PILOTS CLOSED BLEED AIR VALVES & SMOKE SUBSIDED. ACFT RETURNED, NO INDICATIONS OF A PROBLEM OCCURRED. INSPECTION COULD NOT DETERMINE SOURCE FOR SMOKE. NO RESIDUAL SMOKE OR SIGN OF SMOKE REMAINED IN CABIN. INSPECTION OF APU, ENGINES, OIL & AIRFRAME SYSTEMS REVEALED NO REASON FOR SMOKE. EXTENSIVE INVESTIGATION REVEALED NOTHING. SUSPECT COOLING TURBINE MAY HAVE HAD AN INTERNAL LEAK, ALLOWING OIL TO ENTER VENTILATION SYSTEM & BEING HEATED BY BLEED AIR WAS CAUSE OF SMOKE. AFTER HI POWER GROUND RUNS & TEST FLT, NO FURTHER DIFFICULTY EXPERIENCED. ACFT FERRIED TO OXC, REPLACEMENT OF COOLING TURBINE ACCOMPLISHED. 2L72 4F A12EA 20030417000862003041700086NM 2003 4 17 QXEA0300212 120030201A3080 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 200 ILLUMINATED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09409QX 4051 YYC-DEICE CAUTION LIGHT ILLUMINATED INFLIGHT, ISOLATED SYSTEM AS PER CHECKLIST. NR 1 & 2 DEICE PRESSURE INDICATED 18 PSI. NR 1 INTAKE BOOT DIDN'T ILLUMINATE. NO FAULTS INDICATED ON CDS. PERFORMED OPERATIONAL TEST OF DEICE SYSTEM. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030722000782003072200078EU 2003 7 22 MALA030339 120030712A2420HE83305 SENSOR BAC 146 AVRO146RJ85A1500097EU NR 4 ENGINE MALFUNCTIONED A MALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 GL15505XJ E2313 DURING FLIGHT 3581 EN ROUTE TO OMA, NR 4 ENGINE DRIVE HIGH TEMP LIGHT ILLUMINATED ON SHORT FINAL, RAN QRH LIGHT REMAINED ON. MAINTENANCE REMOVED AND REPLACED NR 4 IDG ENGINE SENSOR SWITCH PER AMM 24-12-11. OPS AND LEAKS CHECKS GOOD. 2H74 4F RTA49EU 20030423000982003042300098EU 2003 4 23 U30A200300001 120030105A5210 SEAL AIRBUS320 A320212 3930322EU DOOR BOTTLE DAMAGED A U30AK NONE O OTHER ININSP/MAINT 1 EA17265AV 427 DURING DAILY INSPECTION AFTER FLT 305 IN BWI, THE L1 CREW/PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. SERVICED THE EMERGENCY OPERATION CYLINDER WITH NITROGEN I/A W AMM 52-10-00-614-001. AIRCRAFT RETURNED TO SERVICE. ON JAN 8, REPLACED SEAL P/N, FE240-221-001 AND ASSOCIATED PACKINGS. SERVICED WWITH NITROGEN AND LEAK CK OK. 2L72 4F RTA28NM 20040223000442004022300044WP 2004 2 23 ARWA20031207 120031219A5312 BULKHEAD DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45688 NR 970. DURING (C) CHECK INSPECTION, NLG WW RT TUNNEL STATION 8.000 PRESSURE BULKHEAD FORWARD FACE. NOSE LANDING GEAR RT FITTING WITH CORROSION AT L-31. 2L74 4F 4A25 20031211000372003121100037NM 2003 12 11 QXEA200301396 120031106A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8401 1390041NM NR 1 ENGINE WILL NOT TEST A QXEAK NONE O OTHER UKUNKNOWN 1 NM09400QX 4030 LWS-ON FLIGHT NUMBER 9852, AUTO FEATHER TEST FAILED ON NR 1 ENGINE. INTERROGATED CDS. FAULTS 420 FOUND. CLEARED FAULTS. C/W AUTO FEATHER OPERATIONAL TEST, TESTED GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031211001352003121100135NM 2003 12 11 AALA20031340 120031128A3350 LIGHT BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 LAX LEFT HAND AFT DOOR EMERGENCY FLOOR FLOOD LIGHT BASE ASSEMBLY LENS LOOSE. REPLACED LEFT HAND AFT DOOR EMERGENCY FLOOR FLOOD LIGHT BASE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20030919001162003091900116EU 2003 9 19 00105 120030811A2133 OUTFLOW VALVE AMD FALC20FALCON 2720302EU CABIN PRESSURE MALFUNCTIONED E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05221TW 221 DURING CLIMBOUT, THE CABIN PRESSURE BEGAN TO CLIMB AND DESCEND AT HIGH RATES UNTIL THE CABIN STOPPED PRESSURIZING AT ALL. CONTINUED TO BE ERRATIC UNTIL LANDING. MAINTENANCE R & R PESSURIZATION RATE CONTROLLER OP'S AND LEAK CHECK GOOD. 2L72 4F A7EU 20030922000652003092200065 2003 9 22 XNOA01146 420030820A2312 RADIO AIRBUS300 A300B4203 3930306EU VHF SYSTEM INOPERATIVE A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23473AS 203 NR 1 VHF RADIO WILL NOT TRANSMIT OR RECEIVE. NR 2 VHF WILL ONLY TRANSMIT ON 121.9. DISCONNECTED AND RECONNECTED THE CAPTAINS FREQUENCY SELECT PANEL AND AUDIO SELECT PANEL. PERFORMED OPERATIONAL CHECKOUT OF THE NR 1 VHF COMM.SYS. ON FREQUENIES 129.07 AND 121.9.SYSTEM OPS CHECKS IAW MM 23-21-00. DISCONNECTED AND RECONNECTED THE F/O'S FREQUENCY SELECT PANEL AND THE AUDIO SELECT PANEL. PERFORMED OPERATIONAL CHECKOUT OF THE NR 2 VHF COMM. SYS. ON FREQS 129.07 & 133.225. SYS OPS CHECKS IAW MM 23-21-00. 2L72 4F RTA35EU 20030922001302003092200130NM 2003 9 22 AWXA200300962 120030805A5320D5348004800103 SILL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28802AW 924 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF LOWER R-2 DOORWAY SHAPE SILL BS 2280, STR 23 RT. MAINTENANCE REMOVED CORRODED SHAPE SILL AT BS 2280, STR 23 RT; FABRICATED A REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 7-20, TABLE 1-10, FIG. 2-7. 2L72 4F RTA28NM 20030923001312003092300131NM 2003 9 23 371PA0030 120030825A3350 CONNECTOR BOEING737 737306 13844BGNM EMERGENCY LIGHT DIRTY A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE AFT 12 FEET. CLEANED FLOOR PATH LIGHTING CONNECTORS AND REPLACED TRACK COVER IAW MM 33-51-21. 2L72 4F RTA16NE 20030924000882003092400088EU 2003 9 24 AWXA200300980 120030825A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 221 FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW4350628932 054 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHT SYSTEM THE FORWARD L/H EMERGENCY POWER SUPPLY UNIT FAILED TEST FOR EXTERNAL LOADS FORWARD LEFT AND COMM FORWARD LEFT MESSAGES ON CIDS PANEL. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), FUNCTIONAL CHECK OF SYSTEM WAS GOOD. 2L72 4F RTA28NM 20040128001482004012800148EU 2004 1 28 MALA030574 120031212A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15403XJ 340B403 DURING 4K INSPECTION IN LCQ, FS 620 TO FS 686, LT BL 18.3 SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK SECTION FROM FS 620 - FS 686 IAW MESABA EO A53060 DATED 3 NOV 2003. A/C RELEASE DATE 12/24/03. 2L72 4T RTA52EU 20040204001372004020400137EU 2004 2 4 102803 120031027A2400 SWITCH PILATSPC12 PC1245 7090551EU COCKPIT MISINSTALLED E ESUAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 CE03102RR 316 IT WAS DISCOVERED THAT THE HALF BANK SWITCH AND THE AUTOPILOT TEST SWITCH HAVE BEEN INSTALLED INCORRECTLY SO THAT WHEN DEPRESSING EITHER SWITCH THE OTHER FUNCTION WAS PERFORMED. THE PANEL CONTROL UNIT THAT THESE ARE IN HAD JUST BEEN REPLACED AND A 8130 ISSUED BY MFG PN U1452 1L71 3T RTA78EU 20040204002172004020400217WP 2004 2 4 UPS03841556 120031023A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE: C2, STATION 1755 LONG. 14L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STA. 1744 TO 1755 I.A.W. SRM. 53-2-2 FIG. 10. 2L74 4F RT4A25 20040210000322004021000032WP 2004 2 10 UPS03841609 120031021A5321 FINGER DOUBLER DOUG DC8 DC873F 302199FWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, CORROSION AND SHEARED RIVETS ON WEB FINGER DOUBLER COCKPIT SHEAR WEB UNDER F/E STA RT CUSP FS -12.000 TO -32.000. REMOVED CORRODED FINGER DOUBLER IAW DC8 SRM 51-1-21, CUT OUT DAMAGE IN WEB IAW DWG SRO8530026, REMOVED CORROSION ON CUSP IAW DC8 SRM 51-1-8, WITHIN LIMITS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED CUSP IAW DC8 SRM 51-1-8 FABBED - 15 WEB FILLER, -13 FINGER DBLR, -17 AND -3 SPLICES IAW DWG SRO8530026. ALODINED, PRIMED, AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20. 2L74 4F RT4A25 20040308001442004030800144NM 2004 3 8 ASAA0310231 120030326A7110657377380 SKIN BOEING737 737298C 1384490NM NR 2 COWLING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL SKIN AT NACELLE STATION 160.75-225.75 GOUGED. REMOVED AND REPLACED COWL SKIN PER SRM. (M) 2L72 4F RTA16WE 20031215000242003121500024NM 2003 12 15 SWAA032523 120031116A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED PM CHECK, FOUND 1 LONG CRACK AT FUSELAGE SKIN, BS 790, WL 208 LT SIDE. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040412001722004041200172WP 2004 4 12 ASAA0380728 120031111A532199365471 INSERT DOUG DC9 DC983 3022083WP FLOORBOARD CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 180-200. REPLACED FLOORBOARD PER SRM 53-05 AND 51-10-4. (M) 2L72 4F RTA6WE 20040520002272004052000227EU 2004 5 20 2004F00114 120030911A5321 FLOOR PANEL AIRBUS320 A320233 3930329EU AFT CARGO BAY CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON FLOOR PANEL NR 152EF IN AFT CARGO BAY. FABRICATED, TREATED, PRIMED AND INSTALLED AFT CARGO COMPARTMENT FLOOR PANEL NR 152EF. (M) 2L72 4F RTA28NM 20040721000292004072100029WP 2004 7 21 AALA20030850 120030811A28223980001 PUMP DOUG DC9 DC982 3022082WP CTR FUEL TANK FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21210AA 49161 DFW-MCO - DURING CLIMB-OUT, FORWARD CENTER PUMP BREAKER POPPED. NO FEED FROM CENTER FUEL TANK. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED BOTH CENTER TANK BOOST PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040223000452004022300045WP 2004 2 23 CNMA200300011 120031217A2720 RUDDER DOUG DC10 DC1030 3023501WP TAIL STUCK A CNMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW0759083 47926 ON SHORT FINAL AND FLARE RUDDER PEDALS COULD NOT BE MOVED. RUDDER PEDALS COULD NOT BE MOVED ON TAXI IN. TILLER OPERATION NORMAL. CAPTAINS AND CO-PILOTS SAME. LIMITED TRAVEL AT GATE. TAXI CHECK OF RUDDER PEDALS NORMAL. F/O DID NOTICE ALOT OF RUDDER FORCE ON TAKEOFF WITH SYMETRICAL THRUST AND NO CROSSWIND. 2L73 4F A22WE 20030827000142003082700014NM 2003 8 27 03FDEA00829 120030526A5753ARC199113 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 SNRM N0860 - LT WING - OUTBOARD TRAILING EDGE FLAP - OUTBOARD AFT FLAP-HINGE FOUND PIVOT BEARING HOLES LT AND RT WITH BUSHINGS LOOSE (FLAP SIDE). SNRM N0860: LOOSE BUSHINGS LT AND RT OF PIVOT BEARING HOLES REPLACED WITH OVERSIZED BUSHINGS IAW EA 1-5750-69348 - WINGS - LT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030728000432003072800043NM 2003 7 28 VNAA0307007 120030722A3231001A322A1500000 CONTROL ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NLG DOOR FAILED A VNAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07431JS 3028 DURING CRUISE FLIGHT FROM CHS TO PHL THE FLIGHT CREW EXPERIENCED AN AIR NOISE COMING FROM THE FRONT OF THE AIRCRAFT. AFTER CONSULTING WITH MAINTENANCE CONTROL THE FLIGHT CREW DIVERTED TO PIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT FORWARD NOSE LANDING GEAR DOOR CONTROL ROD HAD FAILED. MAINTENANCE REPLACED THE CONTROL ROD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-80-00. FUNCTIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030801001182003080100118WP 2003 8 1 MWEA030286 120030708A801038334221 STARTER DOUG DC9 DC914 3022034WP ENGINE FAILED A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31700ME 45696 LEFT ENGINE WOULD NOT START. REMOVED AND REPLACED LEFT STARTER. 2L72 4F A6WE 20030806001372003080600137SO 2003 8 6 C2XA03IA071 120030710A32309650976003202 COMPUTER EMB 145 EMB145LR 3260212SO GPWS FAILED A C2XAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW2717560 145605 DURING APPROACH THE CREW NOTED THAT THE TOO LOW GEAR WARNING ON SHORT FINAL DESPITE EICAS SHOWING DOWN WITH THREE (3) GREEN. ABORTED APPROACH, PERFORMED A GO-AROUND AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED GPWS COMPUTER IAW EMB-145 MM 34-44-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. PART NUMBER 965-0976-003-202-202. 2L72 4T RTT00011AT 20030801000972003080100097 2003 8 1 COMA0360325 420030715A3442 RADAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE COCKPIT INTERMITTENT A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SO01729CA 7265 FLIGHT 5563 RADAR CONTROL FAULT MESSAGE. COULD NOT DUPLICATE. FUNCTIONAL CHECK OF RADAR SATISFACTORY. 2L72 4F4 FRTA21EA E15NE 20030903001582003090300158CE 2003 9 3 WVE2003F00010 120030628A242130728692 SPLINE ADAPTER LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP LT ENGINE CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09412FX 103 P116196 DURING 600 HOUR INSPECTION OF THE ALTERNATOR SPLINE ADAPTOR IT WAS FOUND TO BE CRACKED. 2L72 4F4 FRTT00008WIE6WE 20030905000092003090500009SO 2003 9 5 LR7A03056 120030725A532033383531 FITTING LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2134 4606 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5323 FOUND LMLG FS 497 BULKHEAD FITTING CRACKED AND ATTACHING FASTENERS SHEARED AT LBL 62, WL 256. REPLACED FITTING IAW SRM SMP 583 51-70. NR 2082. 2H74 4T A1SO 20030813000162003081300016NE 2003 8 13 HEEA088604 220030806A7320222360010105 CONVERTER BELL 222 222U 1182140SW LYC LTS101LTS101750A1 41560NE TORQUE SPLIT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 INTERMITTENT TORQUE SPLITS FROM 1 TO 8 PERCENT. SHOP REPAIR. 1G72 3U3 U H9SW E5NE 20030806000872003080600087SO 2003 8 6 C2XA03SH227 120030718A531014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 145477 SHV- DURING C-CHECK, THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030812000512003081200051SW 2003 8 12 HEEA088458 120030720A2500206072216103 SEATBACK CUSHION BELL 206 206L3 1182108SW CABIN TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 SEAT CUSHION TORN. REPAIRED. 1G71 3U H2SW 20030825000472003082500047WP 2003 8 25 UPS03841091 120030726A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C2 STATION 1754 LONG. 14R IS CRACKED. REMOVED DAMAGED LONGERON SECTION BETWEEN STA. 1742 TO 1765, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION I.A.W. SRM. 53-2-2 FIG. 10 2L74 4F RT4A25 20030910001902003091000190NM 2003 9 10 USAASB03136 120030811A3260189929 UPLOCK SENSOR BOEING737 737301 1384611NM RT MLG FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19353US 23556 PHL - FLT 1948 - AFTER TAKEOFF AND GEAR RETRACTION FROM PHL, THE RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN UP OR OFF POSITION. CREW CYCLED THE GEAR DOWN AND RECEIVED ALL THREE GREEN LIGHTS. CREW DECIDED TO RETURN TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED FAULT ISOLATION 32-61-00, SHEET 5. FAULT CONFIRMED. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR PER MM 32-61-21-401. INDICATION CHECKS NORMAL. (M) 2L72 4F RTA16WE 20030911002422003091100242WP 2003 9 11 DHL2003604589 120030611A5350 FRAME DOUG DC8 DC873F 302199FWP TAILCONE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 TAIL CONE SECTION FRAME CRACKED 1.000 STA 1923.000 RT SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030731000332003073100033NM 2003 7 31 QXEA200300774 120030625A7110 WEB BOMBDRDHC8 DHC8401 1390041NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - NR 2 LOWER COWL HAS CRACK OF BYPASS DOOR WEB AT UPPER ANGLE. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030929000392003092900039NM 2003 9 29 03FDEA01424 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING I/B FLAP VANE I/B TEE FITTING AFT BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE I/B TEE FTG AFT BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490. 2L73 4F RTA22WE 20050202000602005020200060NM 2005 2 2 0704017 120031006A541465ND543001 ACOUSTIC PANEL BOEING737 737230C 1384472NM NR 1 ENGINE CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW9992 9992 20257 NR 1 ENG NOSE COWL ACOUSTIC PANEL CORRODED 6 TO 9 O'CLOCK. 2L72 4F A16WE 20060313001082006031300108SO 2006 3 13 LR7A03098 120031121A5100 REPAIR LKHEED382 382G 526414USO RT ELEVATOR NONE A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5511 NOTED RT ELEVATOR NON-FLUSH REPAIR AT HSS 164. REPAIRED IAW SRM SMP 583 51-140-10. 2H74 4T A1SO 20030819000672003081900067EA 2003 8 19 SWIA200312125 120030616A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-51. 2L72 4F4 FRTA21EA E15NE 20030818000042003081800004GL 2003 8 18 HEEA088389 220030710A72000292005310 ENGINE SKRSKYS76 S76C 8143008NE ALLSN 250C 250C30S 03013GL MALFUNCTIONED E HEEAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW03505PH1110 760505 ENGINE PRODUCING LOWER POWER ASSURANCE MARGIN TREND. TO BE SENT TO VENDOR. 1G72 3U3 UNCH1NE E1GL 20030820001492003082000149EA 2003 8 20 QXEA200300934 120030730A5414 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 UPPER TRANS COWL HAS FOD DAMAGE AT 12 O'CLOCK POSITION OF NR 1 ENGINE. REPAIRED IAW HORIZON AIR EO R-54-33 AND REO 670-54-23-129. 2L72 4F RTA21EA 20030820001852003082000185NM 2003 8 20 2003UALA00560 120030715A3230 LANDING GEAR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE MALFUNCTIONED A UALAO OTHER JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 WP29820UA 898 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED THE LANDING GEAR LEVER. REPLACED THE LANDING GEAR CONTROL AND INTERFACE UNIT (LGCIU). UNIT FAILED TEST 6DA AND 6BC DUE TO DEFECTIVE SOLDER JOINTS. 2L72 4F4 FRTA28NM E40NE 20030820000062003082000006NM 2003 8 20 03FDEA01303 120030814A2780UNK SWITCH BOEING727 727200 138407ENM LE FLAPS FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25280FE 22347 DURING FLAP RETRACTION L/E FLAP AMBER LIGHT REMAINED ILLUMINATED 26 S/O PANEL SHOWED 237 L/E SLAT NOT RETRACTED. REMOVED AND REPLACED BOTH RETRACT & EXTEND SWITCHES ON NR 7 SLAT ACTUATOR IAW 727-200 M/M 27-82-011-4. TESTED AS PER SAME REFER. OPS CHECKS GOOD. STOWED JUMPER IS IN S/O'S DESKTOP. 2L73 4F RTA3WE 20030404000612003040400061NM 2003 4 4 DL757030246 120030316A3350 BATTERY PACK BOEING757 757232 1384965NM EMERGENCY LIGHT UNSERVICEABLE A DALAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO27662DN 24991 REPLACED BATTERY PACK ON F/C CHARGER FOR SEAT PATH LIGHTING. 2L72 4F RTA2NM 20030407000032003040700003NM 2003 4 7 ASAA0310003 120030106A335086210144 BATTERY BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 DURING SCHEDULED MAINTENANCE INSPECTION, FOUND NO LED INDICATION OF AFT CONTROL MODULE FUNCTION. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES ON PALLETS 10-5, 5-5, AND 6-9, REMOTE ASSEMBLY RECEIVERS ON PALLETS 10-5 AND 5-5, FORWARD CONTROL MODULE (P/N 87-3-2030-4-1), AND FORWARD AND AFT CONTROL MODULE BATTERIES (P/N 86-2-1015-1), THEN LIGHTS TESTED NORMAL. (M) 2L72 4F A16WE 20030403000932003040300093EA 2003 4 3 COMA0360174 120030330A2620601R514133 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA FIRE BOTTLE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA 7241 FLIGHT 5843 CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE FIRE PANEL. 2L72 4F RTA21EA 20030408000892003040800089CE 2003 4 8 040503 120030405A3260404EN16 SWITCH BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE LT MLG WORN E YADAO OTHER N FALSE WARNING APAPPROACH 1 AL03111AX UC81 PILOT REPORTED HAVING TO CYCLE THE LANDING GEAR TO GET THE LEFT MAIN TO INDICATE DOWN AND LOCKED (GREEN) - MAINTENANCE REPLACED THE LEFT MAIN GEAR DOWN AND LOCK SWITCH. 2L72 4T4 TRTA24CE E4EA 20030404001732003040400173NM 2003 4 4 SWAA030571 120030312A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030407001042003040700104NM 2003 4 7 UIEA200300008 120030208A2612897080 WARNING SYSTEM BOEING747 747271C 1384869NM APU FIRE FALSE ACTIVATIONA UIEAFH ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 EA15537MC 22403 AFTER 3 HOURS IN CRUISE, FULL APU FIRE WARNING LIGHTS AND BELL ON. APU FIRE HANDLE PULLED AND BOTTLE DISCHARGED. LIGHT WENT OUT WHEN BOTTLE DISCHARGED. AREA INSPECTED. NO EVIDENCE OF FIRE OR PNEUMATIC DUCT DAMAGE. APU DEFERRED INOPERATIVE PER MEL 49-01 AND APU FIRE EXTINGUISHING SYSTEM DEFERRED PER MEL 26-8. DMI'S M03-023 AND M03-024. REMOVED AND REPLACED A5 FIRE WARNING CARD PER MM 26-45-01. FUNCTION CHECK SATISFACTORY. REMOVED AND REPLACED A12 FIRE WARNING CARD PER MM 26-15-01. FUNCTION CHECK SATISFACTORY. ALSO, FOUND A/T CONNECTORS ON FIRE WARNING LOOP APU DOOR IN BAD CONDITION. R & R BOTH CONNECTORS PER MM 20-62-16. FROM DMI M03-023, REPLACED APU FIRE BOTTLE PER MM 26-22-01 P/N 34504901P. (M) 2L74 4F A20WE 20030410000762003041000076NM 2003 4 10 SWAA030651 120030322A3350071701100 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29708SW 27842 DURING SCHEDULED RON, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20030417001462003041700146 2003 4 17 XNOA01104 420030211A3414 INDICATOR AIRBUS300 A300B4203 3930306EU COCKPIT FAILED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23224KW 073 NR 2 AIRSPEED INDICATOR POWER OFF FLAG SHOWING. REMOVED AND REPLACED THE F/O'S MACH/AIRSPEED INDICATOR. PERFORMED OPERATIONAL CHECK OF THE F/O'S MACH/AIRSPEED INDICATION SYSTEM. OPS CHECKS IAW CHAPTER 34-12-00. 2L72 4F RTA35EU 20030417001472003041700147EA 2003 4 17 SWIA200311758 120030128A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07438SW3401 3401 7574 GLD UNSAFE CAUTION MESSAGE AFTER LANDING. REPLACED NR 2 SECU IAW 27-61-06. OPS CHECK GOOD. 2L72 4F RTA21EA 20030424001092003042400109WP 2003 4 24 IXXA0300029O 120030321A3260 LANDING GEAR DOUG DC8 DC862 3021970WP MAIN FALSE INDICATIONA IXXAO OTHER J WARNING INDICATION LDLANDING 1 SW11728PL833151447 45918 DURING FLIGHT FROM KWAK TO RJTY LANDING GEAR WAS PUT IN DOWN POSITION. THERE WAS NO LEFT GEAR INDICATION. THE GEAR WAS RECYCLED AND IT INDICATED GEAR DOWN. MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR A TOTAL OF FIVE TIMES. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DOUGLAS AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 20030425000112003042500011NM 2003 4 25 UPS03M40361 120030205A5730 SKIN DOUG MD11 MD11F 3023600NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP INSPECTION TYPE: C, RT WING TOP EXTERNAL SURFACE AT STA XORS 683-700 AFT OF STRINGER 1 FOUND CORRODED AT 3 PLACES AS MARKED. AT STA XORS 685 MAT REMOVED 0.023 ORIGINAL THICK 0.200, FOUND OUT OF LIMIT PER SRM 57-10-00 VOL 1 FIG 32 REV 32. 10X MAGNIFIED VISUAL INSP ON BLEND OUT AREA CARRIED OUT PER EN1001-03, SHOT PEEN CUTOUT AS PER DPS4999 & REWORKED AREA REPROTECTED PER SRM 51-21-01 VOL 2 REV 32. 2L73 4F RTA22WE 20030429000212003042900021NM 2003 4 29 P5CA0300797 120030129A5347 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 FWD CGR SHEARED RIVETS ON SEAT TRACK & CRACK ON INTERCOSTAL BETWEEN LBL 25-LBL 45. DAMAGED INTERCOSTAL REMOVED NEW FABRICATED H/ 2024 T30.050 THK PER SAMPLER SRM 53-10-21. PROTECTED AREA PER SRM 51-10-02, RIVETED PER SRM 51-30-02. 2L74 4F A20WE 20030430000872003043000087NM 2003 4 30 USAA030023 120030304A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US47398 23319 CLT - FOUND SKIN CRACKED 3.25 INCH, STATION 520 AND STRINGER 16R. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20030501001512003050100151NM 2003 5 1 ASAA0310015 120030216A5320655383911 STRIP BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING SCHEDULED D-CHECK, FOUND TRANSITION STRIP AT BS 500-560, STRINGER 27R CRACKED. REMOVED AND REPLACED TRANSITION STRIP PER SRM. (M) 2L72 4F RTA16WE 20030501002082003050100208 2003 5 1 ASAA0380269 420030317A2565D29982107 SLIDE DOUG DC9 DC983 3022083WP PAX DOOR FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS1842 53019 OAK - DURING 15K CHECK, FOUND FORWARD PASSENGER L1 DOOR EMERGENCY SLIDE FAILED LIGHT CHECK. REPLACED EMERGENCY SLIDE PER TASK CARD 24655000. (M) 2L72 4F RTA6WE 20030501000782003050100078WP 2003 5 1 GTIA030222 120030311A5730 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND LEFT WING LOWER FUEL TANK ACCESS PANEL NR 5 HAS CRACK AT FASTENER HOLE, DAMAGED COUNTER SINK. PART REPLACED WITH NEW PANEL. (M) 2L72 4F RTA6WE 20030505002372003050500237NM 2003 5 5 AWXA200300387 120030416A335020131A BATTERY PACK BOEING737 73733A 1384673NM ZONE 200 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 PHX - EEL - EMERGENCY ESCAPE PATH LIGHT SYSTEM WAS FOUND ACTIVATED. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS IAW T/C A1C33011, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030505002502003050500250NM 2003 5 5 CALA0300203 120030418A5320 PLATE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717306 23357 INSPECTION FOUND THE NR 3 COMMUNICATION ANTENNA ATTACHMENT/MOUNTING PLATE CORRODED AROUND RIVETS NEXT TO COAX CONNECTOR AT STA 727D, BL 0. A NEW ANTENNA MOUNT PLATE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20030506000902003050600090NM 2003 5 6 03FDEA00611 120030421A5754 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING L/E SLAT TRACK NR 16 INBOARD FITTING FOUND CRACKED. LT WING LEADING EDGE SLAT TRACK NR 16 INBOARD FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II AND DWG ARB2850. 2L73 4F RTA22WE 20030513002732003051300273EA 2003 5 13 ASOA03149 120030406A2133GG670980033 OUTFLOW VALVE CNDAIRCL600 CL6002C10 1390015EA CABIN PRESSURE INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11705EV 10051 DURING CLIMB-OUT FROM ATL-PFN, AT APPROXIMATELY 10,000 FT THE CREW RECEIVED AN AMBER CABIN ALTITUDE MESSAGE ALONG WITH CABIN ALTITUDE CLIMBING RAPIDLY. THE CAPTAIN LEVELED THE AIRCRAFT OFF TO 10,000 FEET, DECLARED AN EMERGENCY AND RETURNED TO ATL, LANIDNG SAFELY. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROL SYSTEM OUT FLOW VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030604001672003060400167NM 2003 6 4 UPS03440587 120030412A575365B078711 RIB BOEING747 747121 1384871NM LT WING FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C LT WING, NR 7 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 6 & 7 ( VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-47-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030605000452003060500045EA 2003 6 5 A6WA200340068 120030520A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 FUSELAGE SKIN IS DAMAGED AT PASSENGER DOOR CUTOUT FS 349. REPAIRED FUSELAGE SKIN AT PASSENGER DOOR CUTOUT FS 349 IAW BOMBARDIER INC REO 601R-53-21-078. (M) 2L72 4F RTA21EA 20030605001632003060500163EU 2003 6 5 S9HA265Y1 120030425A2150060018 A/C PACK SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE CABIN FAILED E S9HAO OTHER O OTHER NRNOT REPORTED 1 WP19356NT 2280 864 AIR CONDITIONING BLOWING WARM AIR. INSPECTION REVEALED BELT MELTED ON THE PULLEY. REPLACED THE COMPRESSOR ASSY WITH SERVICEABLE UNIT, INSTALLED NEW BELT. SYSTEM SERVICED IAW MFG INSTRUCTIONS. POSSIBLE COMPRESSOR FAILED INTERNALLY CAUSING THE BELT TO BREAK. AIR CONDITIONING SYSTEM IS INSPECTED, BEARING GREASED AT MFG RECOMMENDED INTERVALS. CLOSER INSPECTION DURING THE DAILY INSPECTION TO CHECK FOR SIGNS OF OVERHEATING OR LOSS OF GREASE THAT MIGHT INDICATE IMPENDING FAILURE. 1G71 3U3 UNCH9EU E19EU 20030514001282003051400128NM 2003 5 14 SWAA031014 120030506A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 384, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030520001112003052000111NM 2003 5 20 AALA20030408 120030403A33501000679 LIGHT BOEING767 767223 1385123NM COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21332AN 22331 JFK - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY OVER DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030612001752003061200175SO 2003 6 12 SWIA200312048 120030526A27503075001017 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS FAILED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07197SW 120186 FLAP CONTROL FAULT DURING FLAP BITE TEST AND WILL NOT RESET. INSTALLED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-06. OPS CHECKS GOOD. S/N OFF: 0230. 2L72 4T RTA31SO 20030613000312003061300031EA 2003 6 13 COMA0360254 120030531A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA EXTERNAL POWER UNSECURE A COMAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 SO01977CA 7157 FLIGHT 5316 EXTERNAL POWER SERVICE DOOR OPEN IN FLIGHT. INSPECTED DOOR AND AREA FOR DAMAGE, NONE FOUND AND CLOSED DOOR. 2L72 4F RTA21EA 20030521001952003052100195NM 2003 5 21 SWAA031058 120030511A53106546541 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R & STR 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030522000382003052200038WP 2003 5 22 0301009955 120030425A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01922RW 47182 DURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN UPPER STATION 76.5 RBL 14. REPAIRED PER EA 99-190971. 2L72 4F A6WE 20030617002732003061700273NM 2003 6 17 QXEA200300608 120030501A7110 SUPPORT BOMBDRDHC8 DHC8401 1390041NM NR 2 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - NR 2 ENGINE LOWER COWL AFT CONE SUPPORT CRACKED. REPAIRED IAW DHC-8 Q400 SRM 71-61-06, PAGE 1-2. 2H72 4T RTA13NM 20030530000622003053000062EA 2003 5 30 2003F00337 120030423A3200 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA NLG ILLUMINATED A MASAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SW0747202 7202 RETURNED TO FIELD. GEAR DISAGREE WARNING MESSAGE ON TAKEOFF. MAINTENANCE TROUBLESHOT AIRCRAFT IAW AMM. NO DEFECTS NOTED. (M) 2L72 4F RTA21EA 20030623000032003062300003 2003 6 23 MEX2003193 420030526A31309804700042 RECORDER BOEING757 7572Q8 1384972NM FLT DATA FAILED A ASMFK NONE O OTHER ININSP/MAINT 1 SW23301AM 30045 DURING TRANSIT CHECK, FLT REC OFF LIGHT TURNED ON. ASSOCIATED BRAKES WERE RESET BUT FAIL CONTINUES. WIRING WAS CHECKED IAW WDM 31-31-03, ALL CORRECT. FLIGHT DATA RECORDER AND FDAU WERE REPLACED IAW MM 31-31-03, ALL TESTS CORRECT. (M) 2L72 4F RTA2NM 20030623000402003062300040WP 2003 6 23 GTIA030348 120030514A5321 FLOORBOARD DOUG DC9 DC982 3022082WP CABIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FLOORBOARD STATION 1174-1294 LBL 44-54 CRACKED AND DELAMINATED IN SEVERAL AREA. REPAIRED FLOORBOARD. (M) 2L72 4F A6WE 20030624000482003062400048NM 2003 6 24 CALA0300301 120030609A551065C251563 FITTING BOEING737 7373T0 1384582NM HORIZONTAL STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND A 4 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, LBL 10. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-47598 AND SRM 51-40-2. 2L72 4F RTA16WE 20030625000262003062500026WP 2003 6 25 MWEA030235 120030528A5320993666483 SUPPORT ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 AFT CARGO COMPARTMENT SUPPORT ANGLE HAS CORROSION ON BOTTOM SIDE AT STATION 1320 ADJACENT TO LONGERON 30 (BELOW SUPPORT ANGLE. FABRICATED AND INSTALLED SUPPORT ANGLE. 2L72 4F A6WE 20030630000312003063000031NM 2003 6 30 AWXA200300606 120030527A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 9 BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28179AW 22646 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030707000802003070700080NM 2003 7 7 DHL2003740004 120030628A5210 HANDLE BOEING727 7272Q9 138448MNM FWD DOOR INOPERATIVE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01740DH 21930 FORWARD ENTRY DOOR EXTERIOR HANDLE WILL NOT STAY IN THE FLUSH POSITION. HANDLE WAS OUT OF FLUSH POSITION OR 90 DEGREES OUT OF DETENT. CLEANED AND LUBRICATED EXTERIOR AND INTERIOR DOOR HANDLES, CLEANED VENTILATION HOLE HANDLE EXTERIOR CHECKED OPS GOOD IAW M/M 52-00. 2L73 4F RTA3WE 20030710000112003071000011WP 2003 7 10 GTIA030446 120030528A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND CABIN LEFT OUTBOARD SEAT TRACK CORRODED ON UPPER AND LOWER SIDES FS 1155-1231 HIDDEN DAMAGE FOUND UPON PANEL REMOVAL. REMOVED LEFT OUTBOARD SEAT TRACK. LOCATED AND DRILLED TWO SEAT TRACK WITH TWO SPLICE. INSTALLED SEAT TRACK. (M) 2L72 4F A6WE 20030714001632003071400163SW 2003 7 14 ALGA087904 120030702A6240407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH WILL NOT TEST B ALGAO OTHER L NO TEST NRNOT REPORTED 1 SW03437AL 53141 DUAL TACH NEEDLE ON INDICATOR WILL NOT TEST. 1G71 3U O H2SW 20030716000612003071600061WP 2003 7 16 GTIA030468 120030511A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND MAIN CABIN FS 730 CENTER FLOOR PANEL HAS BROKEN INSERT. REMOVED FLOORBOARD. FABRICATED FLOOR PANEL. INSTALLED NEW PANEL. (M) 2L72 4F A6WE 20030107000792003010700079NM 2003 1 7 CALA0300003 120030106A5330 SKIN BOEING737 7373T0 1384582NM AFT OF EXH DCT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914335 23573 INSPECTION FOUND A 1/4" CRACK IN BELLY SKIN AFT OF EXHAUST DUCT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894. 2L72 4F RTA16WE 20030128001682003012800168WP 2003 1 28 ZW0A0300803 120030107A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C IN THE CABIN A CORRODED FLOOR SUPPORT CAP WAS FOUND AT STA 1155, LBL 22 TO 44. REMOVED CORRODED CAP. CLEANED AREA AND INSTALLED NEW FABRICATED CAP PER SPM 6-70-01. 2L72 4F A6WE 20030213000042003021300004NM 2003 2 13 CA030121003 120030101A278269619433 BEARING BOEING737 7372T5 1384474NM PWA JT8 JT8D17 52049NE SLAT ACTUATOR LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON 9 JAN 2003 IT WAS FOUND THAT THE ROLLER BEARING ON THE NR 5 SLAT OUTBOARD TRACK HAD BECOME DETACHED AND THE CONTROL ARM HAD WORN THROUGH THE TOP WING SKIN FORWARD OF THE FRONT SPAR. UPON REMOVAL OF THE ACCESS PANEL ALL THE PARTS WERE FOUND INSIDE INCLUDING A BROKEN COTTER PIN. IT LOOKED LIKE THE CASTELLATED NUT HAD BEEN ABLE TO ROCK BACK AND FORTH UNTIL THE COTTER PIN BROKE AND THEN FELL OUT ALLOWING THE NUT TO BACK OFF AND THE ROLLER TO BECOME DETACHED. 2L72 4F4 FRTA16WE E2EA 20030218000162003021800016NM 2003 2 18 03FDEA00111 120030120A5753ARC050214 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING O/B FLAP I/B HINGE ACTUATOR I/B ATTACHMENT HOLE FOUND WITH A GROOVE MARK. COMPLIED WITH FEDEX EA 1-5750-67561. WING TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP, INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20030219001022003021900102NM 2003 2 19 SWAA030328 120030206A256010107451 SIGN BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20030220000682003022000068WP 2003 2 20 ABXA030069 120030123A57129919301506 RIB DOUG DC9 DC941 302207NWP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23957AX 47759 NR 2 SLAT TRACK CUT-OUT INBOARD LEADING EDGE RIB LOWER HORIZONTAL FLANGE HAD A 3.5 INCH CRACK. REPAIRED AREA IAW DC-9 REA D957-46167. 2L72 4F A6WE 20030114002512003011400251EA 2003 1 14 COMA0360019 120030110A5210600319413 BEARING CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR STIFF A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01957CA 7109 FLIGHT 5179 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.REPLACED THE LOWER TORQUE TUBE BEARINGS. 2L72 4F RTA21EA 20030116001012003011600101 2003 1 16 HEEA083054 420030107A34570110005400 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108PH 51334 GPS INTERNAL BATTERY LOW. SLOW TO ACQUIRE STATIONS. 1G71 3U H2SW 20030130001512003013000151NM 2003 1 30 F3LA200300002 120030111A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED TOP SIDE OF I-BEAM AT STA 947 BETWEEN LT AND RT SEAT TRACKS. REMOVED CORRODED SECTION OF FLOORBEAM UPPER CAP PER SRM 53-00-51, FIG 202. FABRICATED AND INSTALLED SECTION OF STA 947.5 UPPER CAP PER SRM 53-00-51, FIG 202, SOPM 20-41-02, SRM 53-00-51, FIG 202 AND SRM 51-40-02. 2L72 4F RTA16WE 20030121000932003012100093SW 2003 1 21 HEEA083281 120030108A3246206324008 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 SKID TUBE HAS CORROSION. SCRAPPED. 1G71 3U H2SW 20030121001702003012100170GL 2003 1 21 HEEA083322 220030109A7320 BELLOWS BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL FUEL CONTROL ASSDIRTY E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW032268V 330170 3605 HIGH STARTING TEMP AND NO START DERICH ADJUSTMENT LEFT. FOUND START DERICHMENT BELLOWS WAS NOT OPERATING PROPERLY. REMOVED BELLOWS TO INSPECT, AND FOUND BELLOWS SEATING SERVICE IN THE COVER, AND ON THE BELLOWS TO BE DIRTY. CLEANED BOTH AND TESTED AGAIN. START DERICH OPERATED PROPERLY. UNIT TESTED SATISFACTORY. 1G71 3U3 U H2SW E4CE 20030304000182003030400018SW 2003 3 4 AC2A084874 120030302A341256B25A PROBE BELL 430 430 1182150SW OAT LOOSE H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CT1142 49089 PROBE IS LOOSE. REPLACED PART 1G72 3U RTH9SW 20030305000772003030500077EU 2003 3 5 HEEA084660 120030213A6420 BEARING AEROSPAS355 AS355* EU TAIL ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 MA1127 3004 TAIL ROTOR HEAD HAS WORN BEARINGS. 1G72 3U H11EU 20030227001032003022700103SW 2003 2 27 HEEA084407 120030212A2420SM20ACD300A21 CONTACTOR BELL 407 407 1182206SW ELECTRICAL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03408PH 53228 INTERMITTENT IGNITION DURING START. 1G71 3U O H2SW 20030307000132003030700013 2003 3 7 HEEA084883 420030227A34221113025 INDICATOR SKRSKYS76 S76A 8143006NE HSI SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03764P 760276 COPILOT HSI INDICATOR CIRCUIT BREAKER WILL NOT RESET. 1G72 3U H1NE 20030314000572003031400057NE 2003 3 14 AT030003 220030129A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 FAILED A ZZDAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO15965AT 55026 CLIMBING THROUGH 16,000 FEET RIGHT ENGINE ROLLED BACK TO IDLE POWER. ENGINE SURGE RIGHT LIGHT CAME ON WITH A MESSAGE TO INCREASE ENGINE BLEED. RPM LOW LIGHT ALSO CAME ON. THROTTLE WAS BROUGHT BACK TO IDLE AND ANTI-ICE WAS TURNED. THROTTLE WAS ADVANCED. ENGINE REMAINED IN IDLE (N1 21 PERCENT - N2 62 PERCENT) N1 VIBE WAS 99. ENGINE WAS SHUTDOWN AND RESTARTED, START WAS NORMAL BUT ENGINE REMAINED IN IDLE WHEN THROTTLE WAS ADVANCED. ENGINE WAS SHUTDOWN AGAIN AND AIRCRAFT LANDED IN BMI. REMOVED AND REPLACED THE NR 2 ENGINE. 2L72 4F4 FTRA6WE E00061EN 20030314001142003031400114NM 2003 3 14 SWAA030557 120030310A2731MS27645 BEARING BOEING737 7373H4 1384600NM RH ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RH ELEVATOR TAB FAILED FREE PLAY INSPECTION. R&R RH ELEVATOR PUSH ROD CRANK ASSY BEARING PER MM. 2L72 4F RTA16WE 20030314001512003031400151EU 2003 3 14 PA03002 120030120A5522S25TE4135 SKIN BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP LT ELEVATOR LE CORRODED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL2348FB 9630 DHB259 257129 WHILE PERFORMING INSPECTION ON THE ELEVATORS, FOUND CORROSION ON THE UPPER AND THE LOWER LEADING EDGE SKIN SURFACES OF THE LEFT ELEVATOR. THE CORROSION WAS CONCENTRATED WHERE THE SKIN IS FASTENED TO THE ELEVATOR FRONT BEAM. AFTER REMOVING THE CORROSION AND BLENDING THE AREA FOUND THAT TWO SIGNIFICANT AREAS WHERE THE CORROSION WENT BEYOND THE LIMITS OF THE SRM. DETERIORATION OVER TIME. C/A: REPAIRED MINOR SURFACE CORROSION ON THE INBOARD LEADING EDGE OF THE ELEVATOR IAW MFG FIELD REPAIR, CORROSION ON ELEVATOR, LEADING EDGE SKIN, BETWEEN INNER HINGE AND CENTER HINGE. 2L72 4F4 F A3EU E6WE 20030317000352003031700035NM 2003 3 17 03FDEA00169 120030224A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON FLOORBEAM REPAIR FILLER B.S. 1070, RBL 42 TO LBL 36. REMOVED CORROSION ON FLOORBEAM REPAIR FILLER BS 1070. FOUND TO BE OUT OF LIMITS. REMOVED FILLER, FABRICATED REPLACEMENT AND INSTALLED IAW SRM 53-10-1, 53-10-8. 2L73 4F4 F A3WE E2EA 20030122000552003012200055 2003 1 22 HEEA083443 420030109A2300H1037 HEADSET BELL 206 206L3 1182108SW COMMS SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 NO COMMUNICATION. REPLACED HEADSET. 1G71 3U H2SW 20030122000872003012200087SW 2003 1 22 HEEA083479 120030110A7810212061202009 DUCT BELL 412 412 1182202SW EXHAUST SYS CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 EXHAUST DUCT CRACKED. TO BE SENT TO VENDOR. 1G72 4U H4SW 20030318000272003031800027NE 2003 3 18 ERAA085145 120030213A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE DEBONDED H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01577EH2808 760222 WORN DOUBLER DEBONDING. KEVLAR SKIN DAMAGE IN ZONE A & D ON SN A175-03491 R & R EXTERNAL DOUBLERS, R & R FWD INT DOUBLERS AND REMOVE AND REBONDED C CHANNEL, REFINISH AND BALANCE. REPAIRED SKIN DAMAGE ON SN A175-03491. 1G72 3U H1NE 20030326000132003032600013EA 2003 3 26 AUS20030101 220030131A8520LW13792 SEAL MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL CRANKSHAFT DETERIORATED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) CRANKSHAFT SEAL DETERIORATED AND LEAKING. CONTAMINATION OF STARTER AND ALTERNATOR. 1H71 3O3 ONC3A23 E286 5 CP920 20030418000342003041800034WP 2003 4 18 MWEA030099 120030214A53105952368185 DOOR FRAME DOUG DC9 DC981 3022081WP VENTRAL DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 UPPER PORTION OF VENTRAL DOOR JAMB IS CRACKED ALONG THE LEFT SIDE. DRILLED UP AND INSTALLED DOOR JAMB. 2L72 4F A6WE 20030421001062003042100106NM 2003 4 21 DLM88030193 120030224A2612474007 MODULE DOUG MD88 MD88 3023688NM FIRE DETECTION WILL NOT TEST A DALAK NONE L NO TEST ININSP/MAINT 1 SO27927DA 49714 CARGO FIRE DETECTION SYSTEM ARMED LIGHTS AND SQUIB LIGHTS DO NOT ILLUMINATE DURING SQUIB TEST. REPLACED CONTROL MODULE. 2L72 4F RTA6WE 20030422000662003042200066SO 2003 4 22 SIMA200305002 120030218A350092185A010100 CONTROLLER EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A SIMAB EMER. DESCENT O OTHER CLCLIMB 1 SW21635AE 145158 PIT - FLT 4345 - CREW REPORTED DURING CLIMB THROUGH 17,000 FT, CABIN ALTITUDE EXCEEDED 14,500 FT, OXYGEN MASK DEPLOYED IN MAIN CABIN. THE FLT CREW PERFORMED EMERGENCY DESCENT OT 10,000 FT REGAINED CONTROL OF CABIN ALTITUDE AND DIFFERENTIAL PRESS. THE FLT CREW THEN CLIMBED BACK TO 15,000, SYSTEM OPERATED MANUALLY ON DESCENT, APPROACH AND LANDING. THE AUTO PRESSURIZATION SYSTEM IS ALREADY ON MEL. MAINTENANCE REMOVED AND REPLACED THE PRESSURE DIGITAL CONTROLLER IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20030422000702003042200070SO 2003 4 22 SIMA200307912 120030227A532014525381003 DOUBLER EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION DOUBLER AT RIGHT HAT BEAM FRAME 23 CORRODED. REMOVED AND INSTALLED SERVICEABLE DOUBLER AT RIGHT HAT BEAM AT FRAME 23 IAW EMB SRM 51-20-03, 51-40-02. (M) 2L72 4T RTT00011AT 20030731001432003073100143EU 2003 7 31 2003F00494 120030515A5753 BEARING AIRBUS320 A320233 3930329EU T/E FLAP FAIRINGWORN A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK 632CB, WITH FREEPLAY AT STATION 3059. REPLACED BEARINGS OF STAY ASSEMBLY IAW PMS 01-05-27. (M) 2L72 4F RTA28NM 20030801000592003080100059SO 2003 8 1 ASOA03284 120030703A33503071BPE LIGHT EMB 120 EMB120RT 3260202SO CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11240AS 120060 DURING HANGAR MAINTENANCE IN MCN, AN EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20030929001032003092900103EU 2003 9 29 AWXA200301018 120030828A33971260A1183APN CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 26 LT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 MCN - EEL - DURING C-03 CHECK FOUND A DAMAGED RECEPTACLE AND CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT. MAINTENANCE REMOVED AND REPLACED RECEPTACLE AND CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031001000362003100100036WP 2003 10 1 UPS03841178 120030807A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, AFT CARGO PIT AT FS 1150 L32 RT-L33 RT BANANA FITTING IS CRACKED. REMOVED (2) BANANA FITTINGS STA 1152 AND 1160 L33R-L30R. UPON FURTHER INSPECTION BANANA FITTING NOTED TO BE CRACKED. REC'D, LOCATED, AND DRILLED (2) BANANA FITTINGS IAW DC8 SRM 51-1-24. INSTALLED NEW BANANA FITTINGS IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030908001702003090800170EA 2003 9 8 SWIA200312241 120030807A27604916405 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07597SW5184 5184 7293 'FLT SPOILERS FAULT' STATUS MESSAGE APPEARED DURING TAXI. REMOVED AND REPLACED SECU NR 2 IAW MM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20030908003182003090800318NE 2003 9 8 SWAA031896 220030823A7230CFM56 COMPRESSOR BOEING737 7375H4 138449DNM GE CFM56 CFM563B1 13802NE NR 1 ENGINE STALLED A SWAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW29512SW 24189 722212 AIR TURNBACK, NR 1 ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20030909000242003090900024EA 2003 9 9 SWIA200312335 120030824A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913SW 7597 FS 484 RT INTERCOSTAL O/B FLANGE CRACKED RBL 36. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRT REO 601R-53-41-059 REV. 'A'. 2L72 4F RTA21EA 20031006001452003100600145NM 2003 10 6 SWAA032011 120030907A2560PH22300L LIGHT BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT SECTION MISSING BETWEEN ROW NR 19 ABC AND ROW NR 21 ABC. INSTALLED STRIP PER MM. 2L72 4F RTA16WE 20031006001112003100600111NM 2003 10 6 2003UALA00679 120030909A2742 TURNBUCKLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB UNSAFETIED A UALAK NONE O OTHER ININSP/MAINT 1 WP29372UA 24637 HORIZONTAL STABILIZER ADJUSTMENT TURNBUCKLE FORWARD OF CABLE DRUM IN FORWARD EQUIPMENT AREA NOT SAFETY WIRED. MAJOR REPAIR ACCOMPLISHED, SAFETY WIRED TURNBUCKLE. 2L72 4F4 FRTA16WE E2GL 20031008000252003100800025NM 2003 10 8 HOC2003F00022 120030826A5311 FRAME BOEING727 727224 1384076NM FUSELAGE CORRODED B HOCRO OTHER O OTHER NRNOT REPORTED 1 WP0779749 22451 DURING A C-CHECK CORROSION WAS NOTED ON SUPPORT FRAME AT STA 720-720A, BLO-13 LBL. 2L73 4F A3WE 20031008000322003100800032NM 2003 10 8 QXEA200301128 120030915A5730 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 BOI- DURING WALKAROUND ON LINE CHECK FOUND A DENT IN LEFT HAND WING BOTTOM SKIN, BETWEEN STATIONS 510 AND 494 JUST AFT OF LEADING EDGE PANELS 513DL AND 513CL. REPAIRED IAW HORIZON AIR EA 6-57-176. 2H72 4T RTA13NM 20031014000632003101400063NM 2003 10 14 SWAA032189 120031002A53126545409 PRESSURE PANEL BOEING737 7375H4 138449DNM MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL 31.5. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20031014001962003101400196NM 2003 10 14 SWAA032101 120030921A55206959227 HINGE BOEING737 7373K2 13844BANM LT ELEVATOR WORN A SWAAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SW29345SA 23786 AIRFRAME VIBRATION FELT, IN AFT CABIN FELT STRONGER. REMOVED AND REPLACED LT ELEV TAB NR 1 HINGE BUSHING AND REMOVED AND REPLACED LT ELEV TAB PER MM AND SWA SI. 2L72 4F RTA16WE 20031020000642003102000064NM 2003 10 20 VNAA0310003 120031003A2611 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY DIRTY A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07439JS 3057 THE CREW REPORTED RECEIVING A LAV SMOKE FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND CLEANED THE CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20031029000762003102900076NM 2003 10 29 ASAA0310523 120030816A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 8-9 INOPERATIVE. REPLACED BATTERY PACKS, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20031103000452003110300045WP 2003 11 3 03FDEA01703 120031004A2612 COMPUTER DOUG MD10 MD1010F WP FIRE DETECTION MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25570FE 47829 ON CLIMBOUT PASSING THROUGH 10,000 FT CREW HAD A FWD CARGO FIRE HEAT. PUSHED FLASHING DISCHARGE SWITCH AND DID AN EMERGENCY RETURN FULL STOP TO DFW. COMPLETED QRH RED TABS FIRE WARNING WAS OUT PRIOR TO LANDING. AFTER BLOCK IN OF AIR TURN BACK MSC WAS CHECKED FOR FAULTS, NO FAULTS FOUND. REMOVED AND REPLACED MSC IAW AMM 31-42-01-4.OP'S CK GOOD.REF WRI 31-41/0594. ACCOMPLISHED EA 8-2610-73820, INSTALLING A DIODE AND MOD BLOCK TO SEPERATE UPPER AND LOWER CARGO FIRE WARNING SYSTEMS. OP'S CK GOOD. REMOVED AND REPLACED NR 1 CARGO FIRE BOTTLE IAW AMM 26-22-01-4. OP'S CK GOOD. REMOVED AND REPLACED ALL 4 FWD LWR CARGO SMOKE DETECTORS IAW AMM 26-14-01-04. OPS CK GOOD. 2L73 4F RTA22WE 20031029000082003102900008NM 2003 10 29 ASAA0340107 120030301A532069434561 STRAP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON STRAP AT BS 839-859 WL 160 AND RBL 19. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20030806000412003080600041SO 2003 8 6 C2XA03SH253 120030803A531014522460015 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 DURING C-CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030806001502003080600150SO 2003 8 6 C2XA03IA068 120030628A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716911 145446 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030423001382003042300138EA 2003 4 23 RU3A03003 120030217A493038826081 HOUSING CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE APU FUEL FILTERCRACKED E RU3AO OTHER O OTHER NRNOT REPORTED 1 SW1587 5190 APU FUEL FILTER HOUSING ATTACHMENT FLANGES, CRACKED. THIS IS THE 5TH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, 3 ON N86, AND 2 ON N87. 2L72 4F4 FRTA21EA E15NE 20030722000592003072200059NM 2003 7 22 SWAA031499 120030705A3233064100512 ACTUATOR BOEING737 7372H4 138448CNM NLG FAULTY A SWAAO OTHER J WARNING INDICATION APAPPROACH 1 SW29090SW 22905 AFTER GEAR EXTENSION, NLG RED UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED GEAR ALL LIGHTS OPERATED NORMAL. REMOVED AND REPLACED NLG MAIN ACTUATOR AND DOWNLOCK ACTUATOR PER MM. 2L72 4F A16WE 20030722000542003072200054EA 2003 7 22 HNAA0300032 120030711A326010449101 SPRING DHAV DHC8 DHC8311 1386006EA NR 2 MLG BROKEN A HNAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA07329EN221443412 DCL357790 290 ON APPROACH TO CLT THE RIGHT MAIN GEAR HAD UNSAFE LIGHT. USED ALTERNATE GEAR EXTENTION ON NEXT APPROACH. RIGHT GEAR RED LIGHT, DOOR LIGHT AND HANDLE LIGHT ON. ALTERNATE INDICATION SHOWS ALL GEAR DOWN AND LOCKED. FOUND SPRING ON THE STABILIZER STAY STRUT BROKEN, REPLACED BOTH INBOARD AND OUTBOARD SPRINGS. 2H72 4T RTA13NM 20030724000722003072400072EU 2003 7 24 AWXA200300769 120030606A5312D53370801204 BULKHEAD AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 MCN - MAJOR REPAIR - DURING C-04 CHECK A .1875 INCH CRACK WAS FOUND ON RT BULKHEAD WEB FR 35 AT LOWER MOST OUTBOARD HOLE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED REPAIR DOUBLERS AND A BRACKET ASSEMBLY; INSTALLED REPAIR PARTS IAW AWA ER 26-5331-02151-TB2A. 2L72 4F RTA28NM 20030829000622003082900062WP 2003 8 29 DHL2003873010 120030723A5610 ODOR DOUG DC8 DC873F 302199FWP WINDSHIELD DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01873SJ 46091 F/O'S WINDSHIELD STINKS, SMELLS LIKE HOT INSULATION. REMOVED EXCESS GLUE FROM TOP OF F/O'S WINDSHIELD. INSPECTED ELECTRICAL WIRING AND CONNECTIONS FOR HEAT, NO DEFECTS NOTED PER M/M 56-10-0. 2L74 4F RT4A25 20030902000422003090200042EU 2003 9 2 CX7A194J0349 120030615A2613173436450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE OVERHEATED A CX7AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL03307CE 340B204 LT TAILPIPE HOT CWP ON. 2L72 4T RTA52EU 20030722000872003072200087EU 2003 7 22 AWXA200300787 120030612A5320D5397470600600 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT (PROFILE) AT FR 56, Y10. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED PROFILE AT FR 56, Y10; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 7-10 & 12 FIG 2 & 3. 2L72 4F RTA28NM 20030807001042003080700104NM 2003 8 7 EIA2003101 120030725A5340 FITTING BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 FWD CARGO PIT AFT PRESSURE BULKHEAD STA 1000, BATH-TUB FITTING BETWEEN STA 38-39L CRACKED. REMOVED AND REPLACED TWO EACH FITTINGS BETWEEN STA 38-39L, STA 1000, P/N 65B16518-1 AND 65B16517Y3 PER B747 SRM 51-32-02, PGS 8 & 9, 51-10-01, PGS 6 & 7, 53-10-03, PG 1, 53-10-21, FIG 2, 51-10-02, PGS 6 & 7, BSOPM 20-41-02, PGS 7-15. 2L74 4F A20WE 20030813002102003081300210 2003 8 13 SWAA031707 420030731A2565D31354 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2L72 4F A16WE 20030903002032003090300203NM 2003 9 3 QXEA200301033 120030823A5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX- CABIN FLOOR BOARD SUPPORT AT NR 4 SEAT TRACK VERTICAL HOLE IS OVERSIZED AND SURROUNDING MATERIAL IS WORN THIN. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20030904001622003090400162WP 2003 9 4 DHL2003873617 120030705A532046401111N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 NOSE SECTION INTERIOR END FITTING 3.000 INCH CRACK STA 0.000-8.000, L-33L (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON NOSE SECTION INTERIOR (STA 0.000-8.000, L-33L) SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030814001282003081400128NM 2003 8 14 2003UALA00576 120030719A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29380UA 24655 MAIN CABIN FLOORBEAM STA 947.5 HAS CORRODED T- CAP BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP SECTION SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030815000362003081500036SW 2003 8 15 HEEA088524 120030712A2915204076036005 MASTER CYLINDER BELL 412 412 1182202SW ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MAIN ROTOR BRAKE MASTER CYLINDER HAS NO OUTPUT PRESSURE. IN SHOP REPAIR. 1G72 4U H4SW 20030821001612003082100161NM 2003 8 21 03FDEA01162 120030723A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RIGHT WING - O/B FLAP (FLAP SIDE) O/B HINGE I/B PIVOT HOLE AND I/B PIVOT LUG INNER AND OUTER LUG SURFACES FOUND CORRODED. 2L73 4F RTA22WE 20030822000322003082200032NM 2003 8 22 03FDEA01045 120030626A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 MAIN DECK - AT BS 695, LEFT X=8.5, FLOOR TRACK CRACKED. MAIN DECK - AT BS 695 TO BS745 X=8.5 LT CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I. 2L73 4F RTA22WE 20030825001322003082500132SO 2003 8 25 C2XA03SH289 120030824A532014521721005 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK CENTER BUTTSTRAP WAS FOUND TO HAVE CORROSION AT NUTPLATES BETWEEN FRAMES 14 AND 17. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030911001422003091100142NM 2003 9 11 03FDEA01321 120030815A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 CORROSION ON LT KEELBEAM CORD AT STA 950D, WL 148. ACCESSED LT KEELBEAM. REMOVED CORROSION ON L/HKEEL BEAM CORD AT BS 950D+15, WL 148. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED KEELBEAM IAW FED EX EA 7- 5310-72313. PERFOMRED SHEAR TIE REPAIR AND REINSTALLED. ALL ACCESS IAW SRM 51-30- 2, 53-10-1, 53-10-4. 2L73 4F RTA3WE 20030916001082003091600108NE 2003 9 16 AALA20030872 220030816A7230 BLADE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ENGINE BIRD INGESTION A AALAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SW2176202 53292 EN ROUTE BJX-DFW, ON TAKEOFF, AIRCRAFT EN COUNTERED MULTIPLE BIRD STRIKES. RIGHT ENGINE BEGAN SURGING. RETURNED TO BJX WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED DAMAGED 1ST STAGE FAN BLADES, FRONT AND REAR OUTER FAN CASES PER MX CHECK MANUAL CARDS 72-91-11 AND 72-94-12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA6WE E9NE 20030910001532003091000153WP 2003 9 10 GTIA030609 120030629A7830 ACCOUSTIC LINER DOUG DC9 DC982 3022082WP THRUST REVERSER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - NR 1 ENGINE THRUST REVERSER INNER ACCOUSTIC CORE HAS COME OUT/DELAMINATED. REPAIRED DAMAGED ACCOUSTIC AREA. (M) 2L72 4F A6WE 20030929001322003092900132SO 2003 9 29 GLBA2003128 120030907A2750 BEARING EMB 120 EMB120ER 3260203SO TE FLAPS OUT OF POSITION A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03108UX 120108 FLAPS WOULD NOT RETRACT, REPOSITION LT OB ROLLER BEARING. 2L72 4T RTA31SO 20031002000312003100200031NE 2003 10 2 AALA20030545 220030508A7200 ENGINE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE NR 1 VIBRATION A AALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW211427A 11412 DURING LEVEL FLT AT 31,000 FT, AIRSPEED 270 KNTS, ON SELECTING 250 KNTS, NR 1 ENG INDICATED HIGH VIB ON MFDU ACCOMPANIED BY AUDIBLE NOISE & VIBRATION FELT THROUGH A/C. ATTEMPTED ICE CLEARING PROCEDURES WITH NO SUCCESS. ADVANCING THROTTLE ABOVE 1.14 EPR CAUSED AN IMMEDIATE & SUSTAINED VIB WITH ASOCIATED IND ON MFDU. N1 IND HIGH VIB ON BOTH VIB CHANNELS. N2 SLIGHTLY HIGHER THAN IND ON NR 2 ENG, ALL OTHER ENG IND APPEARED NORM. NR 1 ENG LEFT AT IDLE FOR LAST 390 MINUTES OF FLT. SINGLE ENG PROCEDURES FLOWN WITH NO ADVERSE RESULTS. LANDED DFW WITHOUT INCIDENT. ALL CHECKS GOOD, VIB .4 AT TAKEOFF, AS EPR ENGINEERING. NO FURTHER MAINTENANCE REQUIRED. A/C RETURNED TO SERVICE. SYS GRND CHECKED NORM. (M) 2L72 4F4 FRT E25NE 20031002000372003100200037NM 2003 10 2 USAA030176 120030827A5553 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US 23984 FOUND FITTING CORRODED AND PITTING 1 INCH, VERTICAL STAB AFT OUTBOARD LUG AFT CLEVIS BETWEEN CLEVIS AND T-FITTING 3-6 O'CLOCK. REMOVED AND REPLACED BUSHING PER EA 76801. (M) 2L72 4F RTA16WE 20031003000782003100300078NM 2003 10 3 03FDEA01527 120030902A5753ARC0503504 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP OUTBOARD HINGE (A/C SIDE) OUTBOARD ACTUATOR ATTACH BORE FOUND CORRODED. 2L73 4F RTA22WE 20031014001382003101400138NM 2003 10 14 SWAA032055 120030914A57536546435333 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29647SW 27717 DURING SCHEDULED C4 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20031020001572003102000157NM 2003 10 20 DL767030786 120030826A3350S283T0143 POWER SUPPLY BOEING767 767232 1385132NM CABIN DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27102DA 22214 EMERGENCY LIGHTS STAY ON IN F/C GALLEY AND RT SIDE OF F/C SECTION. REPLACED POWER SUPPLY. 2L72 4F RTA1NM 20031021002752003102100275NM 2003 10 21 QXEA200301146 120030917A5410 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA RT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX- AFT END OF RT HAND NACELLE FINGERNAIL DECK IS CRACKED AROUND BOLT HOLES. REPAIRED IAW Q400 SRM 51-00-02, TASK 51-00-02-250-801 AND RD 8/4-54-044. 2H72 4T4 TRTA13NM E00062EN 20031022000852003102200085NM 2003 10 22 03FDEA01765 120031017A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 STA 950F, WL 208, LBL 30 & 36 FLOORBEAM HAS TOOL MARKS. BLENDED TOOL MARKS FROM 950F FLOORBEAM WL 208, LBL 30-36, REMOVED 1 X1 X.150 & 1 X2 X.045 FROM ORIGINAL OF .225 . OUT OF LIMIT PER SRM 51-10-1. CUT OFF DAMAGE SECTION OF FLOOR BEAM, AFT UPPER FLANGE LBL 17.4-37.8 BS 950F, WL. 208. REPAIRED FLOORBEAM IAW FED EX EA. REPAIRED ACCESS SEAT TRACK FROM BS 950F 10 TO B/S 950E 10 PER SRM 53-10-5. 2L73 4F RTA3WE 20030909002382003090900238NE 2003 9 9 ABXA030323 220030804A7200JT3D7 ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 3 OVERHEATED A ABXAE ENGINE SHUTDOWN M OVER TEMP TOTAKEOFF 1 GL23816AX509253081 46093 671253 DURING TAKEOFF, NR 3 ENGINE EGT WENT TO 600 DEGREES. RETARDED THROTTLE AND EGT DECREASED INTO NORMAL RANGE. OTHER INSTRUMENTS DECREASED AS WELL. SECURED ENGINE PER ABNORMAL PROCEDURES. EGT AT 600 DEGREES FOR APPROXIMATELY 15 SECONDS. NR 3 ENGINE WAS SHUTDOWN AT 0506Z. OIL PRESSURE WAS AT 25 PSI FOR ONE HOUR THEN WENT TO 0 PSI FOR REMAINDER OF FLIGHT 1 HOUR 20 MINUTES. REPLACED NR 3 ENGINE IAW JOBCARDS 8090507 DC8-8-A AND DC8-8B. 2L74 4F4 F 4A25 1E8 20031121000152003112100015 2003 11 21 SWAA032465 420031106A2565D31354 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040113002412004011300241 2004 1 13 QXEA200301303 420031012A3418 STALL WARNING BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAK NONE N FALSE WARNING CRCRUISE 1 NM09405QX 4047 PDX - FLIGHT 2289 PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED AFTER TOUCHDOWN. COMPLIED WITH CHECKLIST AND TESTED STALL SYSTEM. RESET STICK PUSHER CIRCUIT BREAKER IAW SERVICE LETTER DH8-400-SL-31. NO PARTS REPLACED OPERATIONS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031112000972003111200097EU 2003 11 12 BAQA090583 120031025A249745023502 MASTER SWITCH UROCOPEC135 EC135P1 8680990EU FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME747 0009 NR 2 BUS TIE WILL NOT STAY CLOSED. GOES INTO TEST MODE BY ITSELF. NR 2 ENGINE WILL NOT TEST. HARD CARD ENCLOSED. REPLACED WITH CANNED, SERVICEABLE UNIT. 1G72 3U O H88EU 20031031000142003103100014NM 2003 10 31 DHL2003742014 120031001A561058935841 WINDOW BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE COCKPIT FAILED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01742DH 21290 L5 WINDOW SHATTERED DURING FLIGHT. OUTER AND INNER PANE. ABNORMAL PROCEDURE PERFORMED. RII REMOVED AND REPLACED L5 WINDOW IAW B727 M/M 56-11-41. 2L73 4F4 F A3WE E2EA 20031105000312003110500031SO 2003 11 5 C2XA03CL173 120031004A3350375921 LIGHT EMB 145 EMB145ER 3260211SO ALLSN AE3007AE3007C GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715932 145015 CLE FLIGHT NR 2066 THE CREW REPORTED THE EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT EXIT LOCATOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20031106000772003110600077 2003 11 6 SWIA200312525 420031017A22106229968001 DAMPER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07406SW1029910299 7030 YD ONE INOP STATUS MSG APPEARED 4 TIMES IN AIR AND TWICE ON GROUND. YD 1 WOULD RESET AND THEN FAIL REPEATEDLY. REMOVED AND REPLACED NR 1 YAW DAMPER IAW CRJ MM 22-22-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20031107000182003110700018SO 2003 11 7 C2XA03SH432 120031107A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK STRINGER 19 RIGHT BETWEEN FRAME 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031107000372003110700037NM 2003 11 7 HNAA0300061 120031103A522085310480 SKIN DHAV DHC8 DHC8102 2809003NM ESCAPE HATCH DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07930HA 126 REPAIR FOR DENTED ROOF SKIN AFT OF COCKPIT ESCAPE HATCH. 2H72 4T RTA13NM 20030918001232003091800123GL 2003 9 18 VE32003F00000 220030703A729723004963 WIRE HARNESS BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE BURNED B VE3RO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP23306FD3468 51360 HELICOPTER WAS BEING GROUND RUN AFTER A MAIN DRIVESHAFT REPACK. THE ENGINE ELECTRICAL HARNESS CAUGHT FIRE. THE FIRE PROPAGATED ABOUT 4 INCHES ALONG THE HARNESS BEFORE IT WAS EXTINGUISHED. THE FIRE WAS SMALL AND CONTAINED TO THE HARNESS ONLY. NO OTHER DAMAGE WAS NOTED. NO WORK HAD BEEN PERFORMED IN ORON THE ENGINE. THE FIRE OCCURED AT THE DIODE IN THE WIRE OF THE ANIT-ICE SOLENOID CIRCUIT. THE HARNESS HAS A CHAFE GUARD AND WAS TY-WRAPPED IN THIS AREA. NO SPECIFIC RECOMMENDATION TO PREVENT RECURRENCE. 1G71 3U3 U H2SW E1GL 20031008000132003100800013EA 2003 10 8 032253706 120030910A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 DURING MAINTENANCE INSPECTION THE NR 3 EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031010000212003101000021NM 2003 10 10 USAASB03158 120030831A2530500387D4 COFFEEMAKER BOEING737 7373B7 1384580NM NR 2 GALLEY ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19519AU 23705 EN ROUTE CLT-MDT, CREW NOTED A HEAVY ELECTRICAL BURNING SMELL IN THE FIRST CLASS CABIN. NO SMOKE WAS SEEN. SMOKE/FIRE PROCEDURES WERE ACCOMPLISHED. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 COFFEE MAKER IN THE FORWARD GALLEY WITH BURNED COFFEE FROM OVER BREWING. ALSO, FOUND BURNED FOOD ON OVEN HEATING ELEMENT. THE COFFEE MAKER WAS REPLACED AND THE OVEN CLEANED. THE ENGINES WERE RUN INDIVIDUALLY AND TOGETHER, ISOLATING COMPONENTS DURING THE RUN. NO ODORS WERE NOTED. (M) 2L72 4F RTA16WE 20031119001482003111900148SO 2003 11 19 SWIA200312484 120030928A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07271YV 120271 NACELLE FLAPS DISAGREE WHEN SELECTED UP FROM 45 DEGREES. REMOVED AND REPLACED LEFT NACELLE ACTUATOR IAW EMB 120 MM 27-50-00 RII 27-307. ALL OPS CHECKS GOOD. 2L72 4T RTA31SO 20031121000312003112100031 2003 11 21 03315688 420031111A31606229810016 DISPLAY CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27688BR 7723 RIGHT PRIMARY FLIGHT DISPLAY WAS FOUND INOPERATIVE. THE DISPLAY UNIT WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED ON THE FLIGHT DISPLAY SYSTEM AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031117000792003111700079 2003 11 17 P5CA0300957 420031004A22102530624926 CONTROL PANEL BOEING747 747236B 1384804NM COCKPIT JAMMED A P5CAO OTHER I FLT. ATTITUDE INST. CRCRUISE 1 WP23924FT 21730 ALTITUDE ALERT CONTROL FROZEN. REMOVED AND REPLACED AUTOPILOT FLT DIRECTOR PANEL. 2L74 4F A20WE 20040112000822004011200082NM 2004 1 12 AWXA200301572 120031208A53206545834252 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND IN TWO PLACES ON UPPER SURFACE OF INTERCOSTAL AT BS 294.5, LBL 12. MAINTENANCE REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS, REMOVED INTERCOSTAL AT BS 294.5, LBL 12; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1. 2L72 4F RTA16WE 20030910000212003091000021WP 2003 9 10 DHL2003604553 120030520A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 INTERIM REPAIR ON TOP SURFACE OF LT WING L/E (STA XS 246.518-250.089) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38, TR NR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38, TR NR 57-85. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER INNER SIDE IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER WITH NEW FASTENRES IAW SRM 57-2-1 FIG 38, TR 57-85. 2L74 4F RT4A25 20031028000042003102800004CE 2003 10 28 DXTA200300129 120030927A3260 UPLOCK SWITCH CESSNA560 560XL 2076702CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07692QS 5605092 AFTER TAKE-OFF FROM HYA NOSE GEAR WOULD NOT STAY UP AND LOCKED AFTER RETRACTION, DIVERTED INTO SWF. JACKED AIRCRAFT AND PERFORMED GEAR SWINGS, UNABLE TO DUPLICATE SQUAWK ON GROUND. FOUND EMERGENCY GEAR RELEASE CABLE HAS EXCESSIVE TENSION, RE-RIGGED CABLE IAW CE 560XL MM CHAPTER 32-30-08. FOUND NOSE LANDING GEAR UP-LOCK SWITCH AT MAX ADJUSTMENTS AND OUT OF RIG, REPLACED NOSE LANDING GEAR UP-LOCK SWITCH IAW CE 560XL MM CHAPTER 32-30-05 OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA22CE E00059EN 20040113001892004011300189EU 2004 1 13 USAASA03132 120031125A3350321430 BATTERY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19111US 1114 THE EMERGENCY LIGHTS FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040127002152004012700215WP 2004 1 27 ASAA0380789 120031119A532199365881 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS 53018 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DISBONDED AT FS 427-446. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040416000032004041600003NM 2004 4 16 ASAA0240BBB 120030322A53206547959 STRAP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 DURING C-CHECK, FOUND CORROSION ON STRAP UNDER FRAME AT BS 794. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040329000202004032900020WP 2004 3 29 ASAA0380392 120030421A53219936639613 FLOORBOARD DOUG DC9 DC982 3022082WP FUSLEAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING 30K CHECK, FOUND CABIN FLOORBOARD CRACKED. REPAIRED FLOORBOARD PER SRM. (M) 2L72 4F A6WE 20031119000402003111900040EU 2003 11 19 AWXA200301203 120030924A5320D53911600202 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING C-04 CHECK CORROSION WAS FOUND ON FWD CARGO COMPARTMENT RT PROFILE BETWEEN FR 31 & FR 34, AT FASTENER HOLES. MAINTENANCE CUTOUT CORROSION ON RT PROFILE BETWEEN FR 31 AND FR 34; FABRICATED A PROFILE REPAIR SECTION AND SPLICE DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5320-03154-SS1. 2L72 4F RTA28NM 20031119000712003111900071WP 2003 11 19 ABXA030389 120030923A53205956034514 ATTACH FITTING DOUG DC9 DC932F 3022067WP CARGO TRACK CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 CRACKED ATTACH FITTING STA. 980, BETWEEN LONGERON 28 - 27 RT. REPLACED ATTACH FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20031110000622003111000062SO 2003 11 10 RAIA00310271 120031022A49504952304 BLEED VALVE EMB 145 EMB145 3260210SO APU FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK 145068 5693-STL- APU BLEED FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED APU BLEED VALVE. 2L72 4F RTT00011AT 20031112000052003111200005NM 2003 11 12 2003UALA00814 120031028A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29393UA 24668 STA 500A STR 7R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20040113001202004011300120EA 2004 1 13 03360631 120031226A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27631BR 7261 DURING INSPECTION THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040113000982004011300098NE 2004 1 13 ALGA091288 120031126A6320E6893672 PINION GEAR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03518AL CAG90817 760134 CAE890074S FOUND SPALLING ON PINION GEAR TEETH. SENT PART TO VENDOR FOR WARRANTY CREDIT. 1G72 3U3 U H1NE E1GL 20040114001892004011400189GL 2004 1 14 MASA200300432 220031030A7261 OIL SYSTEM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT ENGINE LEAKING A MASAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07856MJ2734 145626 CAE312146 NR 2 ENGINE WOULD NOT START WITH ASSOCIATED SMOKING. THE CREW SHUT DOWN THE ENGINE. THE ENGINE WAS STILL PRODUCING SMOKE AFTER SHUT DOWN SO THE CREW DISCHARGED THE ENGINE FIRE EXTINGUISHER. AN OIL LEAK WAS FOUND AT THE ENGINE STARTER AREA. MECHANIC IS IN THE PROCESS OF MAKING NECESSARY REPAIRS TO RESOLVE OIL LEAK. 2L72 4T4 FRTT00011ATTE6CH 20031216000522003121600052NM 2003 12 16 SWAA032538 120031117A335007912 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 EEPLS COVER MISSING BETWEEN ROWS 11 AND 12. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20031217001352003121700135NM 2003 12 17 SWAA032717 120031211A53116546551 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D-CHECK, FOUND FRAME CORRODED AT BS 807, RBL 4. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031126001022003112600102SO 2003 11 26 C2XA03SH461 120031119A531514521700007 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20031218000282003121800028EA 2003 12 18 SWIA200312623 120031124A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 621 LT FLOORBEAM ANGLE LBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401. 2L72 4F RTA21EA 20031218001152003121800115NM 2003 12 18 2003UALA00906 120031125A5330 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29370UA 24539 SHEAR TIE CRACKED STR 3L BS 500B. ALSO SHEAR TIE CRACKED AT STR 16L BS 500A. MAJOR REPAIR ACCOMPLISHED. REPLACED BOTH SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20031222000702003122200070WP 2003 12 22 ASAA0380606 120031007A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 FOUND FLOORBOARD FIBERGLASS CLOTH TORN FROM UPPER SURFACE AT FS 1079-1117. REPLACED FLOORBOARD PER SRM 53-03. (M) 2L72 4F RTA6WE 20031219001702003121900170NM 2003 12 19 QXEA200301507 120031120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 NR 1 SEAT TRACK HAS LITE SURFACE CORROSION ON TOP OF RAILS 7 INCHES AFT OF X354. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20031223001362003122300136NM 2003 12 23 03FDEA02177 120031212A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25287FE 21849 CORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 360 LBL 0 TO 10. 2L73 4F RTA3WE 20031223000652003122300065NM 2003 12 23 F3LA200300171 120031211A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL STA 947 - 967, LBL 16. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-60-51 AND 51-40-02. 2L72 4F RTA16WE 20031231000822003123100082WP 2003 12 31 GTIA030922 120031003A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND AFT PIT STATION 1309, LEFT SIDE HAS CORROSION AT INERCOSTAL. REMOVED INTERCOSTAL. LOCATED AND DRILLED HOLES IN NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. (M) 2L72 4F RTA6WE 20031014001772003101400177 2003 10 14 SWAA032077 420030918A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 AFT ENTRY DOOR EVAC SLIDE OUT OF POSITION. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040112000092004011200009WP 2004 1 12 AALA20031263 120031112A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21205AA 49155 DFW - DURING OVERNIGHT MAINTENANCE, FOUND CEILING EMERGENCY LIGHTS AT ROWS 21D INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040121000332004012100033NM 2004 1 21 03FDEA02314 120031226A5510ALC81041 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STAB LT UPPER CENTER PLANK 15L BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-75222, HORIZONTAL STAB BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2L73 4F RTA22WE 20040311000482004031100048NM 2004 3 11 ASAA0310127 120030310A57546546419 SKIN BOEING737 737210C 1384459NM L/E SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND RIGHT WING FIXED LEADING EDGE NR 5 SLAT AT WING STATION 440 CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA. (M) 2L72 4F A16WE 20031203001832003120300183WP 2003 12 3 GTIA030900 120031108A3350 LIGHT DOUG DC9 DC983 3022083WP TAILCONE INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 DTW - FOUND TAILCONE EMERGENCY LIGHT HAS ONE BULB INOPERATIVE. RESECURED LOOSE POWER WIRE AND RESEATED BULB TO CONTACT POWER TERMINAL. SYSTEM CHECKS GOOD. (M) 2L72 4F RTA6WE 20031203000292003120300029EU 2003 12 3 COEA0301711 120031007A3230AC64208 SELECTOR VALVE FOKKERF27 F27MK500 4990629EU MLG MALFUNCTIONED A COEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM13711FE 10383 AFTER DEPARTING ANC CREW NOTICED WITH GEAR UP AND IN LOCKED POSITION THE MAIN PNEUMATIC PRESSURE LEAKED EXCESSIVELY. CREW ELECTED TO RETURN TO ANC. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T A817 20031204000442003120400044WP 2003 12 4 GTIA030839 120031001A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN SUB FLOOR CORRODED AT FS 200 16 INCHES LBL. CUT OUT CORRODED AREA. FABRICATED 1 FILLER AND 1 DOUBLER. INSTALLED FILLER AND DOUBLER. FLOOR SUPPORT CORRODED. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20031209000362003120900036SO 2003 12 9 SWIA200312543 120031003A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07215SW 120281 PAX ENTRY AREA; FLOORBOARD FRAMES, CORROSION AT VARIOUS LOCATIONS AS MARKED. DISCOVERED DURING C-CHECK. REPLACED CENTER FLOORBOARD BRACKET AFT OF GALLEY AND REMOVED, TREATED AND PRIMED NUMEROUS SURFACE CORROSION AREAS IAW SRM 51-10-02. 2L72 4T RTA31SO 20031222001342003122200134EA 2003 12 22 COMA0360535 120031208A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA23644 7031 WHILE PERFORMING TASK CARD 002-57-540/640-603 FOUND LEFT WS 85.50 DRAIN HOLE FORWARD SCREW HOLE CRACKED. DRILLED HOLE, PERFORMED EDDY CURRENT INSP, FABRICATED AND INSTALLED FREEZE PLUG IAW BOMBARDIER, INC REO 601R-57-21-383. 2L72 4F RTA21EA 20031223001442003122300144CE 2003 12 23 DXTA200300183 120031126A2710666000162 CONTROL CABLE CESSNA560 560XL 2076702CE AILERONS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07684QS 5605084 PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03. 2L72 4F RTA22CE 20031224000222003122400022NM 2003 12 24 USAASB03204 120031121A3260655825029 CIRCUIT CARD BOEING737 737301 1384611NM MLG INDICATOR FAILED A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19574US 23739 ON FINAL APPROACH, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS AFTER GEAR WAS SELECTED DOWN. CREW RAISED THE GEAR AD EXECUTED A GO-AROUND. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND ON THRID GEAR CYCLE, RED UNSAFE LIGHTS REMAINED EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE JACKED THE AIRCRAFT, REPLACED M986 LOGIC CARD AND ACCOMPLISHED A GEAR SWING. OPS CHECK GOOD PER MM 32-61-00. (M) 2L72 4F RTA16WE 20031229000062003122900006WP 2003 12 29 ABXA030464 120031124A55535939711501 ANGLE DOUG DC9 DC941 302207NWP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 EXTERIOR SURFACE OF VERTICAL STABILIZER AT FORWARD RIGHT FUSELAGE ATTACH POINT HAD CRACK. REMOVED AND REPLACED VERTICAL ATTACH ANGLE IAW DC-9 SRM. 2L72 4F A6WE 20031229000782003122900078NM 2003 12 29 PCAA0312149 120031214A335061047811 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT FAULTY A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13818EX 235 WHILE AIRCRAFT WAS IN MAINTENANCE IT WAS DISCOVERED DURING TEST THAT SEVERAL OVERHEAD AND OUTSIDE EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE FOUND POSITION 300 POWER SUPPLY WITH GROUND WIRE BROKEN AND ASSOCIATED BATTERY OVERHEATING. BOTH WERE REPLACED BUT PROBLEM STILL EXISTED. SUSPECT OTHER BATTERIES WERE AT FAULT, AND ALL BATTERIES WERE REMOVED AND RERPLACED, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031229000912003122900091WP 2003 12 29 MWEA030494 120031215A3260H146 DOWNLOCK SWITCH DOUG DC9 DC932 3022066WP MLG INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31301ME 47190 RT MLG GREEN LIGHT STAYED ON. REPLACED RT MLG DOWNLOCK SWITCH. 2L72 4F A6WE 20031229000312003122900031SO 2003 12 29 LR7A03092 120031121A5330 SKIN LKHEED382 382G 526414USO FUSELAGE LOOSE A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION, FOUND LOOSE FASTENERS FS 245-245E FUSELAGE SKIN, LBL 60-RBL 60, WL 230. REPLACED 400 EA RIVETS IAW AC 43.13-1B AND SB 382-53-42. NR 2068. 2H74 4T A1SO 20040105001772004010500177NM 2004 1 5 AWXA200301621 120031209A575465C2660399 SLAT BOEING737 737301 1384611NM NR 3 DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-18 CHECK THE NR 3 SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER TRAILING EDGE. MAINTENANCE REMOVED DELAMINATION ON INBOARD UPPER TRAILING EDGE OF NR 3 SLAT; FABRICATED REPAIR DOUBLERS; BONDED DOUBLERS ON SLAT IAW B737-300 SRM 51-70-10, FIG 16, PG 67-69. 2L72 4F RTA16WE 20031009000422003100900042EA 2003 10 9 SIMA200325901 120030910A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21504AE 10044 DFW - FLT 3650 - AFT EMERGENCY FLOOR LIGHTS INOPERATIVE. R & R AFT BATTERY PACK. (M) 2L72 4F RTA21EA 20031009000032003100900003NM 2003 10 9 USAA030194 120030910A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU50821 23514 FOUND SKIN CRACKED 2.250 INCH, JUST BELOW S23R AT FS 730. INSTALLED DOUBLER/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M) 2L72 4F RTA16WE 20031014000022003101400002EU 2003 10 14 BAQA089521 120030930A243245033502 BATTERY UROCOPEC135 EC135T1 5620026EU MASTER MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03485AE175 0273 ENGINE WON'T CRANK WITH BATTERY POWER BOX. BOX TESTS WHEN EVER MASTER BATTERY SWITCH IS ENERGIZED. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040106002072004010600207WP 2004 1 6 GTIA030988 120031107A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND DENTS AT FS 232 BETWEEN LONGERONS 18 AND 19L AND AT FS 220 BETWEEN 18 TO 20L. DENTS ARE WITHIN ONE INCH OF STRUCTURE AND REQUIRE REPAIR. CUT OUT DAMAGE. CUT OUT MEASURES 18 INCHES BY 26 INCHES. FABRICATED NEW SKIN, FINGER DOUBLER AND DOUBLERS. REMOVED DAMAGED SECTION OF LONGERON. LOCATED AND DRILLED NEW LONGERON. INSTALLED LONGERON. INSTALLED SKIN, FILLER AND DOUBLERS AND FINGER DOUBLER. (M) 2L72 4F RTA6WE 20040108001462004010800146EU 2004 1 8 PG9A118859 120030713A33407050A4334014 STROBE UROCOPEC130 EC130B4 EU TMECA ARRIELARRIEL2B NE EXTERNAL FAILED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19130PH37 3670 (STROBE UNIT) UNIT FAILED WITH 37 HOURS TOTAL TIME.(K) 1G72 3U3 U H9EU E00054EN 20031124000772003112400077NM 2003 11 24 F3LA200300153 120031114A3230C202163382D32 CONTROL UNIT AIRBUSA319 A319111 3930336NM INOPERATIVE A F3LAO OTHER J WARNING INDICATION CRCRUISE 1 NM03907FR5002 1743 EN ROUTE TO DEN, ECAM STATUS SHOWED FOLLOWING MESSAGE: INOP SYS: ANTI SKID, N/W STRG/ BRK SYS 1, BRK SYS 2. N/W STEERING SWITCH WAS ON. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED IN DEN WITHOUT INCIDENT. AIRCRAFT HAD NO N/W SHEERING AND NO SYS 1 OR SYS 2 BRAKING. BRAKING ACCOMPLISHED PER ABNORMAL PROCEDURES. AFTER TROUBLESHOOTING, REPLACED BSCU AND OPS CHECKED GOOD PER AMM 32-42-34. REPLACED BRAKE SELECTOR VALVE AND PERFORMED HYD LEAKAGE TEST PER AMM 32-42-11-000-001. PERFORMED OPERATIONAL TEST OF BSCU PER AMM 32-46-00-001 AND CHECKED GOOD. 2L72 4F RTA28NM 20031125000432003112500043WP 2003 11 25 DHL2003805521 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/E FORMER CRACKED 1.000 AT STA XS 467.323 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030919001412003091900141NM 2003 9 19 C8GA20030020 120030815A29135509808 PUMP BOEING727 727200 138407ENM HYD SYS DEFECTIVE A C8GAO OTHER J WARNING INDICATION CRCRUISE 1 SO15713AA2182 22469 DEPARTED STL HAD NO INDICATION OF A PROBLEM UNTIL 150 MILES OUT OF TOL. A-SYSTEM QUANTITY GAUGE SHOWED A SUDDEN LOSS OF INDICATED HYDRAULIC QUANTITY. FOLLOWED CCIA “A” SYSTEM FAIL PROCEDURE, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINATION IN TOL WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE A-SYSTEM HYDRAULIC PUMP WAS REPLACED. SERVICED AND BLEED HYDRAULIC SYSTEM IAW B727 MM 29-11-31, ALL SYSTEMS OPS CHECKED NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20030919001492003091900149NM 2003 9 19 AWXA200300929 120030817A335030043233 RECEPTACLE BOEING737 73733A 1384673NM EMERGENCY LIGHT CORRODED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28164AW 23625 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED LENS COVER AND FOUND RECEPTACLE HALF FULL WITH WATER, PLACED ON MEL 33-14, COND. 1, (EXTERIOR EMERGENCY LIGHT INOP). IN PHX ON 07/17/2003, MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT ASSEMBLY, BATTERY CHARGER, AND BATTERY. OPERATIONAL TEST OF R-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS GOOD. 2L72 4F RTA16WE 20030923000042003092300004CE 2003 9 23 DXTA200300095 120030816A3241 BRAKE ASSY CESSNA500 560CESSNA 2076750CE ANTI SKID SYS MALFUNCTIONED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07331QS 5600331 PILOT REPORTED AT LOW SPEED TAXIING STRAIGHT AHEAD, ANTI SKID IS CYCLING MAKING THE BRAKES SLIP. AIRCRAFT RETURNED TO BLOCK. FOUND NO FAULTS ON ANTI SKID FAULT DISPLAY UNIT. ANTI SKID SELF-TEST CHECKED GOOD, VERIFIED PROPER BRAKE PRESSURE AT BOTH BRAKES IAW CE 560 MM CHAPTER 32-42-00. OPS AND LEAK CHECK GOOD. 2L72 4F RTA22CE 20030924000992003092400099NM 2003 9 24 03FDEA01347 120030810A5753ARB2431 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 LT WING O/B T/E, I/B FLAP HINGE BRACKET ASSY FOUND FWD O/B UNDERWING FITTING WITH LOWER SURFACE CHAFFED. ( LOCATED APPROX. 5 INCH FROM FITTING L/E ) BLENDED CARRIED OUT & FOUND WITH IN LIMIT AS PER FEDEX EA 1-5720-68430 WINGS - OUTER WING - O/B FLAP I/B FLAP HINGE BRACKET SUPPORT. 2L73 4F RTA22WE 20030924001202003092400120 2003 9 24 174042903 420030429A22209754421422 PROBE PILATSPC12 PC1245 7090551EU AOA FAILED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07562NA 174 RT AOA PROBE FAILS TO HEAT. 1L71 3T RTA78EU 20030923001012003092300101WP 2003 9 23 DHL2003604673 120030531A5210 SKIN DOUG DC8 DC873F 302199FWP PAX DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 INTERIM REPAIR (2 INCH X 1 INCH) AND WEAR AROUND STA. 32.000 LT LWR SIDE OF FWD PASS. DOOR EXTERNAL SKIN. PERFORMED MAJOR REPAIR IAW EODHL-030559, ED-3297. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG.1. CUT OUT DAMAGED AREA IAW EODHL-030559, ED-3297. PERFORMED EDDY CURRENT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6 AL0.050) AND DOUBLER (7075-T6 AL0.063) IAW EODHL-030559, ED-3297. CLEANED, TREATED AND PRIEMD AREA AND FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED (PRC) SEALANT ON FAYING SURFACES. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW EODHL-030559, ED-3297, SRM 51-1-20D PG.9, SRM 51-1-21 PG.1. REFER TO J/C 8-21-30-002 FOR LEAK CHECK 2L74 4F RT4A25 20030924000372003092400037NM 2003 9 24 DL757030750 120030814A2422100201021 INVERTER BOEING757 757232 1384965NM FWD E/E UNSERVICEABLE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27674DL 25979 ELECTICAL TYPE FUMES AND HAZE THROUGHOUT CABIN AFTER TAKE OFF. REMOVED STATIC INVERTER (2 CB PULLED 6D10 6L11) RESET CB'S AND REPLACED STATIC INVERTER PERFORMED EQ. COOLING BITE TEST, ALL INDICATIONS NORMAL. 2L72 4F RTA2NM 20040128001762004012800176SO 2004 1 28 C2XA03IA117 120031230A326023092900001 UPLOCK EMB 145 EMB145ER 3260211SO LT MLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW271393613221 145025 IAH FLIGHT 2072, PILOT REPORTED THAT THE LEFT MAIN LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR UPLOCK BOX. THE LANDING GEAR EXTENSION/RETRACTION SYSTEM WAS OPERATIONALLY CHECKED AND NO DISCREPANCIES WERE FOUND. 2L72 4F RTT00011AT 20040203000872004020300087WP 2004 2 3 ASAA0380577 120030902A33506011779 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS3791014043 49232 SEA LINE CHECK, RT AND LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040204000472004020400047NE 2004 2 4 101703 220031001A72503023411 BLADE CESSNA500 500CESSNA 2076602CE PWA JD15 JT15D1A NE TURBINE SECTION FRACTURED E ESUAO OTHER MJ OVER TEMP WARNING INDICATION LDLANDING 1 CE03125DS1255 1255 5000258 76754 HT BLADE FAILURE, 4 BLADES FRACTURED MID SPAN REMAINING SET HAS IMPACT DAMAGE, AS WELL AN IMPACT DAMAGE DOWNSTREAM IN THE ENGINE. ENGINE TIME SINCE OVERHAUL 1255.5 CYCLES SINCE O/H 843. THE BLADES ARE NEW AT THE OVERHAUL. 1L72 4F4 F A22CE E25EA 20040211000032004021100003NM 2004 2 11 USAABB03229 120031225A335086210066 BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU 22201 PHL - FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 9 DEF AND 29 DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20040212001792004021200179NM 2004 2 12 AWXA200301590 120031208A5311BAC15171491 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-18 CHECK A.6250 INCH CRACK WAS FOUND ON FRAME AT BS 294.5, STR 7 RT. MAINTENANCE REMOVED DAMAGED AREA OF FRAME AT BS 294.5, STR 7 R/H; FABRICATED 2 EACH REPAIR CHANNELS AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG. 201, PG. 202-203. 2L72 4F RTA16WE 20031210001882003121000188WP 2003 12 10 03FDEA01804 120031025A5753ARB01542 HINGE BRACKET DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25397FE 46631 NR S 9 COMPLY WITH EA8-5750-73194. WINGS-RT IB FLAP-OB HINGE BRACKET, CORROSION REPAIR P/N ARC0154-2. CLOSING ACTION ON 10/22/03. COMPLIED WITH EA 8-5750-73194. 2L73 4F4 F A22WE E23EA 20031211001302003121100130WP 2003 12 11 AALA20031402 120031208A3350AAP3274A CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21274AA 49271 DTW FORWARD OVERWING EMERGENCY EXIT LIGHT OVER EXIT DOOR INOPERATIVE. REPLACED FORWARD OVERWING EMERGENCY EXIT LIGHT OVER EXIT DOOR BATTERIES AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031211001952003121100195EU 2003 12 11 USAA030251 120031029A5320D6347209200000 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19700UW15568 0885 FOUND FLOOR SUPPORT CORRODED 8 CM BY 5 CM AREA, LEFT OUTBOARD FRAME 68, OUTBOARD OF Y 1114. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-42-11. CORROSION LEVEL 2, TASK NR JA 260-53500-007. (M) 2L72 4F RTA28NM 20031125001202003112500120NM 2003 11 25 ASAA310262 120030401A532065566562 FITTING BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIR TORQUE BOX AT BS 947-948, WATERLINE 206-208 CORRODED. REPLACED FITTING PER SRM. (M) 2L72 4F RTA16WE 20031125000222003112500022WP 2003 11 25 DHL2003807545 120031018A5730 PLATE DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 RIGHT WING CENTER L/E OUTER PLATING LOWER PART HAS CORROSION AT STA 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ASTAR ED EDU 21-8, ASTAR DWG U21-R08. PERFORMED NDT INSPECTION IAW NDT STANDARD PRACTICE MANUAL PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW ASTAR ED EDU21-8, ASTAR DWG U21-R08. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENER IAW ASTAR ED EDU21-8, ASTAR DWG 021-R08, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031125001062003112500106EU 2003 11 25 AALA20031295 120031119A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2119059 469 JFK EMERGENCY LIGHT ON SEAT 25G INOPERATIVE. RESECURED SEAT 25G EMERGENCY LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20031203000212003120300021NM 2003 12 3 GAIA03120ST 120031024A5754 RIB BOEING727 727243 138408DNM NR 5 SLAT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION, FOUND NR 5 SLAT RIBS CRACKED INBOARD AND OUTBOARD SIDES OF ACTUATOR ATTACH POINT. REF FASI N/R NR 61216, REPLACED CRACKED RIBS 2024 T-3 .063 INCH PO NR 900103 IAW B727 SRM 57-50-2. (M) 2L73 4F RTA3WE 20040114001782004011400178EA 2004 1 14 MASA200300414 120031016A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717337 7337 ASH NR 6491. PHX-ICT. CABIN EMERGENCY LIGHT BURNED OUT. MECHANIC REPLACED BULB. 2L72 4F RTA21EA 20040123000822004012300082NM 2004 1 23 UIEA200300063 120031113A2133 OUTFLOW VALVE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL CABIN PRESSURE FALSE INDICATIONA UIEACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA15493MC 29254 GT840 TLV/AMS OUTFLOW VALVE MESSAGE: OUTFLOW VALVE R ON TAXI OUT FOR TAKEOFF. ACCOMPLISHED CMC GROUND TEST. SYSTEM PASSED, ADVISORY MESSAGE CLEARED. SYSTEM OPERATION OK. 2L74 4F4 FRT1384945 E23EA 20040127001482004012700148NM 2004 1 27 ASAA0310194 120030321A54206547966507 CLIP BOEING737 737298C 1384490NM NACELLE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK FOUND NR 1 ENGINE COWL FRAME ATTACH CLIPS AT NACELLE STATION 102.60 BROKEN. REMOVED AND REPLACED CLIPS PER SRM. (M) 2L72 4F RTA16WE 20031014000622003101400062NM 2003 10 14 SWAA032190 120031002A5315BAC1509 FLOORBEAM BOEING737 7375H4 138449DNM MID CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20031014000712003101400071NM 2003 10 14 SWAA032203 120031003A53306545768 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT EDGE OF EQUIPTMENT COOLING EXHAUST DUCT CUT OUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030917001152003091700115EA 2003 9 17 A6WA200340109 120030718A491038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE AFT SEIZED A E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL31420AW3123 7640 AFTER ROTATION SMELLED SOMETHING HOT, APU EGT ABOVE RED LINE, APU SHUTDOWN AND TRANSFERRED BLEEDS TO ENGINE. SMOKEY ODOR DISAPPEARED. REMOVED APU SEIZED. REMOVED AND REPLACED APU. NO FURTHER INCIDENT. (M) 2L72 4F4 FRTA21EA E15NE 20031211001852003121100185EU 2003 12 11 A6WA200360052 120031007A5753 FLAP TRACK BAC 146 146200A 1500266EU T/E FLAP WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 FOUND RIGHT NR 2 FLAP TRACK LOWER SURFACE WEAR MARK. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810008. (M) 2H74 4F A49EU 20030919000322003091900032NE 2003 9 19 161711 220030811A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE LEFT MALFUNCTIONED A UHLAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL17148SD 340A148 132 DRG189689 08/11/03 APPROX. 1845(UTC), AIRCRAFT N148SD, FLT 4534 PIT-HGR. ON CLIMB, CREW OBESEVERED LT TQ AND NP INDICATIONS OF ZERO, AND NG FLUCTUATIONS. AT 2500FT, THE LT CHIP DETECTOR LIGHT ILLUMINATED. DURING LANDING SMOKE WAS NOTED IN THE CABIN ALONG WITH CARGO SMOKE LIGHT. AIRCRAFT LANDING, STOPPED AIRCRAFT ON TAXI WAY AND SHUT DOWN BOTH ENGINES. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030924000482003092400048NE 2003 9 24 DLM88030762 220030817A7230 COMPRESSOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE DAMAGED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27902DE38067 53379 718134 LT ENGINE SLOW TO ACCEL ON GROUND. ENGINE DID PRODUCE T/O POWER TO MATCH RT ENGINE HOWEVER LT N1 94 PERCENT AND RT N1 90 PERCENT LT EGT 600 RT 560. UPON SELECTION OF CLIMB POWER 3 COMPRESSOR STALLS NOTED. LT ENGINE PULLED BACK TO IDLE STALLS STOPPED. COMPRESSOR STALL CHECK LIST WAS RUN AND THROTTLE ADVACED TO 80 PERCENT NO MORE STALLS HOWEVER LT EPR 20 PERCENT LESS THAN RT WITH THROTTLES MATCHED. FOUND DAMAGE IN COLD STREAM AT BLEED VALVES. ENGINE REPLACED 2L72 4F4 FRTA6WE E9NE 20040130002392004013000239EA 2004 1 30 SWIA200312753 120031209A2621897889 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA APU DISCHARGED A SWIAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 NM07413SW 7102 APU FIRE WARN IN FLIGHT. APU FIRE BOTTLE WAS FIRED. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE OR HEAT DAMAGE. REMOVED AND REPLACED THE APU FIRE BOTTLE ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. S/N OFF: 60810EL, P/N: 897776-01, S/N OFF: 01659. 2L72 4F RTA21EA 20040202001392004020200139NM 2004 2 2 UPS04541747 120031231A5347BAC15202474 SEAT TRACK BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01407UP 23729 INSPECTION TYPE: C, CORROSION ON SEAT TRACK AROUND FASTENER HOLES BS 565 AND BS 615 BL 0 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 53-00-02. THE SRM REPAIRED PER GOODRICH ER 04-1022. 2L72 4F RTA2NM 20040205000832004020500083NM 2004 2 5 AWXA200400080 120031231A57536546486156 WEDGE BOEING737 737301 1384611NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK THE LT INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DISBONDED 7-10 INCHES FROM THE INBOARD END. MAINTENANCE REMOVED DELAMINATED AREA OF LT INBOARD MID FLAP TRAILING EDGE WEDGE; FABRICATED REPAIR DOUBLERS; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-10 FIG 31, PG 88F-88H. 2L72 4F RTA16WE 20040210000892004021000089EU 2004 2 10 USAA030304 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED, 2 SQUARE INCHES, FRAME 59 PLUS 10 INCHES LBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040213000192004021300019NM 2004 2 13 2003UALA00981 120031223A3350 SOCKET BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT SHORTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29771UA 26932 CEILING EMERGENCY LIGHT AT 35 AND 36G OUT. REPAIRED SHORTED SOCKET AND REPLACED EMERGENCY LIGHT POWER SUPPLIES. 2L72 4F4 FRTT0001SE E46NE 20031215000692003121500069WP 2003 12 15 0302081224 120031001A2540 PAN DOUG DC10 DC1030 3023501WP AFT LAVATORY CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01234NW 46912 DURING M-CHECK FOUND CORROSION ON AFT LAVATORY PAN ASSEMBLY. REPAIRED PER EA 12-196591. 2L73 4F A22WE 20040415000762004041500076WP 2004 4 15 ASAA0380745 120031114A532199365861 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD STATION 920 TO 1003, RBL 22 TO RBL 44 PUNCTURED. REPAIRED PER SRM. (M) 2L72 4F RTA6WE 20040525000462004052500046EU 2004 5 25 2004F00136 120030912A5321 PAN AIRBUS320 A320233 3930329EU AFT LAVATORY CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M) 2L72 4F RTA28NM 20070406001762007040600176NM 2007 4 6 AT0700024 120030930A5340 ATTACH FITTING BOEING717 717200 1383700NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15949AT 55003 T-CLIP CRACKED AT STA 58-750 FRP. REPLACED T-CLIP AT STA 58.75 PER DWG 9911502 AND B717 SRM 51-41-01. MATERIAL USED 7075-0, 2 X 3 INCHES LONG. HEAT TREATED TO 7075-T6 AS PER 98 PMS 247 PS-01. 2L72 4F TRA6WE 20030814000652003081400065EA 2003 8 14 SWIA200312223 120030729A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07406SW 7030 EMERGENCY LIGHT FLOOR TRACK INOP AT AISLE 2. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR TRACK STRIP AT AISLE 2 PER AMM 33-51-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030820001472003082000147EU 2003 8 20 UPS03141112 120030812A2510 PANEL AIRBUS300 A300B4622R 3930312EU ENTRY DOOR OUT OF ADJUST A IPXAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 SO01148UP 831 CLIMBING THRU FL320 DOOR SLIDE ARMING BUZZER AND LIGHT CAME ON. NO ECAM MESSAGE OR WARINING CAME ON. NO LOSS OF PRESSURIZATION. SLIDE WAS DISARMED. GREEN DOOR LOCKING INDICATOR SHOWED HALF RED. FOUND CAMLOCK BEHIND DOOR HANDLE INTERFERRING WITH DOOR HANDLE. RESECURED CAMLOCK. FOUND DOOR UPPER PANEL OUT OF ADJUSTMNET AND INTERFERRING WITH DOOR HANDLE. INSTALLED SHIMS AT PANEL ATTACH POINTS TO GAIN PROPER CLEARANCE. PANELS REMOVED AND REINSTALLED. OPS CHECK OF DOOR VISUAL LOCK FLAG FOUND SATISFACTORY. 2L72 4F RTA35EU 20030819001942003081900194SO 2003 8 19 SWIA200312205 120030722A3350 SOCKET EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT CRACKED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07295SW 120322 EMERGENCY EXIT LIGHTED SIGN BY FLIGHT ATTENDANT SEAT LOWER FIXTURE BROKEN. INSTALLED NEW LIGHT FIXTURE. OPS CHECK GOOD. 2L72 4T RTA31SO 20030401000502003040100050EU 2003 4 1 CA030220005 120030219A5520 BALANCE WEIGHT STBROSSD3 SD360 8100606EU PWA PT6 PT6A65AR 52043NE HARTZLHCB5M HCB5MP3 GL ELEVATOR SEPARATED W O OTHER FD FLT CONT AFFECTED INFLIGHT SEPARATION LDLANDING 1 CA 21093 (CAN) AIRPORT PERSONNEL APPROACHED MAINT WITH PIECE OF METAL THAT HAD BEEN FOUND ON RUNWAY. SUSPECTED IT WAS OURS DUE TO COLOR. IDENTIFIED AS A BALANCE WEIGHT ASSY FROM ELEVATOR TRIM TAB ON A SHORTS SD3-60. CHECKED A/C AT THE RAMP, FOUND THAT A/C HAD TAB WITH MISSING BALANCE WEIGHT. IT HAD APPARENTLY BROKEN AWAY UPON LANDING. PILOT RECEIVED NO INDICATION THAT PART HAD SEPARATED DURING LANDING PHASE. A/C RETURNED TO MAINT, REPLACEMENT TAB WAS INSTALLED. AREA OF SEPARATION IS IMPOSSIBLE TO SEE. TAB CONTROL ROD MUST BE DISCONNECTED SO TAB CAN BE DEFLECTED ENOUGH TO GIVE BALANCE WEIGHT A GOOD WIGGLE TO CHECK FOR POSSIBLE SEPARATION. 2H72 4T4 T A41EU E4EA 6 CP44GL 20030401001662003040100166WP 2003 4 1 DHL2003804775 120030212A535056563501 FILLET DOUG DC8 DC873F 302199FWP WING TO BODY DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING, WING TO FUSELAGE FILLET INNER SKIN DELAMINATED , STA 826.000 - STA. 912.000. R & R PANEL ON LT WING, WING TO FUSELAGE STA. 826.000-STA. 912.000 IAW SRM 51-3-0 PG. 1 2L74 4F RT4A25 20030820000602003082000060NM 2003 8 20 03FDEA00902 120030612A5754ARC2850506 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 RIGHT WING L/E NR 16 SLAT TRACK I/B RIB FOUND CRACKED. SNRM N0066 - NEW RIB FABRICATED AS PER DRAWING NR ARB2850. CRACKED RIB ON RIGHT WING L/E NR 16 SLAT TRACK I/B AREA REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20030402000642003040200064NM 2003 4 2 2003UALA00341 120030303A5754114W425012 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 10 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 10 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030403001222003040300122NM 2003 4 3 DL733030146 120030212A555365468728 FITTING BOEING737 737347 1384647NM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308WA 23441 CORROSION WAS FOUND IN THE BORES OF BOTH THE REAR SPAR LT AND RT PRIMARY AND FAIL-SAFE FIN LUGS. THE BORES WERE ENLARGED TO REMOVE CORROSION. ALSO, THE FORWARD FACE OF THE LHS PRIMARY FIN LUG WAS SPOTFACED TO REMOVE CORROSION. REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2L72 4F RTA16WE 20030401000442003040100044SO 2003 4 1 C2XA03SH080 120030331A5320 SUPPORT EMB 145 EMB145LR 3260212SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK THE SUPPORT PLATE BETWEEN LT OMEGA BEAM AND LT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030410001012003041000101NM 2003 4 10 SWAA030673 120030324A33506104791 CHARGER BOEING737 7372T4 1384492NM CARGO BAY FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED PM CHECK, FOUND BOTH LT & RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY CHARGER BASE PER MM. 2L72 4F A16WE 20030416001822003041600182NM 2003 4 16 AALA20030247 120030225A3350 LIGHT BOEING777 777223 1385213NM CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21791AN 30254 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT FORWARD OF COACH INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BULB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030430000932003043000093NM 2003 4 30 USAABB03050 120030322A4990 BEARING SEAL BOEING757 7572B7 1384964NM APU LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19633AU 27811 DEN - FLT 167 - EN ROUTE PHL-PHX, WITH THE LT GENERATOR ON MEL AND APU OPERATING, THE CREW NOTED A DECREASE IN THE PAU OIL FROM FULL TO REFILL. SHORTLY THEREAFTER THE APU PERFORMED AN AUTO SHUTDOWN. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN DEN REPLACD THE APU OIL LINE. MAINTENANCE IN PHX (FL 9242) RAN THE APU AND COULD NOT FIND AN OIL LEAK. ON THE SUBSEQUENT FLIGHT 162, THE APU WAS AGAIN OPERATING DUE TO THE LEFT GENERATOR MEL, AND THE APU LOST OIL AGAIN. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MAIN LOAD COMPRESSOR BEARING SEAL LEAKING AND REPLACED TE APU. (M) 2L72 4F RTA2NM 20030429000512003042900051EA 2003 4 29 03100622 120030410A3350364911 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK FWD ORANGE LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030430001302003043000130NM 2003 4 30 SWAA030919 120030423A53306545785 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED C4 CHECK, FOUND PAX WINDOW CUTOUT CRACKED AT RT NR 1 WINDOW LOWER AFT CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20030501000792003050100079WP 2003 5 1 GTIA030226 120030316A5320 CLIP DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND FORWARD CARGO FS 237 INTERCOSTAL CLIP CRACKED STRINGER 28L. REMOVED INTERCOSTAL CLIP. FABRICATED CLIP. INSTALLED INTERCOSTAL CLIP. (M) 2L72 4F RTA6WE 20030506000972003050600097NM 2003 5 6 03FDEA00642 120030428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACH POINT BORE HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH AND RH OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030505002302003050500230NM 2003 5 5 DHL2003741543 120030323A5754 ANGLE BOEING727 727200 138407ENM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, LT WING LEADING EDGE AT LEADING EDGE STA 130 IS CRACKED. REMOVED EXISTING FASTENERS TO GAIN ACCESS TO THE REPAIR AS PER B-727 SRM 51-30-2. CUT DAMAGED AREA AS PER B-727 SRM 51-40-3 FIG 1. FABRICATED REPAIR ANGLES MATERIAL USED P/N 60-18001. PO 3077124 SIZES 11 X 1 INCH AND 8.5 X 1 INCH. TREATED AND PRIMED AS PER B-727 SRM 51-10-2. INSTALLED REPAIR ANGLES AS PER B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030509000042003050900004EU 2003 5 9 USAABA03008 120030403A3350321430 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 PHL - FOUND BATTERY FAULT AT 4R DOOR EPSU. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA46NM 20030513000132003051300013NM 2003 5 13 250TR0014 120030429A5320 WEB BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 WEB PANEL CRACKED BELOW LEFT TRANSITION ANGLE BS440 (FORWARD CARGO BIN). FABRICATED AND INSTALLED NEW WEB PER DWG 69C41473. 2L72 4F RTA16WE 20030513001342003051300134NM 2003 5 13 DLM90030389 120030426A2780878201 SENSOR DOUG MD90 MD9030 3023690NM NR 1 SLAT TRACK INTERMITTENT A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27912DN 53392 AFTER T/O SLAT DISAGREE LIGHT REMAINED ON AFTER SLATS WERE RETRACTED. FOLLOWED POM PROCEDURE. FOUND LT WING SLAT SENSOR C D1-64 TO BE INTERMITTENT. REMOVED AND REPLACED SAME PER M/M. CYCLED FLAPS SEVERAL TIMES. ALL INDICATIONS NORMAL. 2L72 4F RTA6WE 20030514000352003051400035SO 2003 5 14 RAIA00304111 120030408A301014530609401 PRECOOLER EMB 145 EMB145 3260210SO ANTI ICE SYS CLOGGED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03821HK9156 145068 9880-MLI- ANTI-ICE FAIL MESSAGE. MAINTENANCE FOUND PRECOOLER CLOGGED. REMOVED AND REPLACED PRECOOLER, OPS CHECK OK. 2L72 4F RTT00011AT 20030602000042003060200004SO 2003 6 2 SIMA200312713 120030419A531014522460013 BEAM EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21642AE 145193 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED NEW CENTER BEAM IAW EMB 145 SRM 51-40-02/04/06, 51-20-03. (M) 2L72 4T RTT00011AT 20030602001192003060200119NM 2003 6 2 SWAA031157 120030523A3350207377 LENS BOEING737 7372T4 1384492NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 EEPLS MISSING LENS AND BULB AT MID CABIN. INSTALLED EEPLS LENS AND BULB PER MM. 2L72 4F A16WE 20030602000182003060200018NM 2003 6 2 USAA030041 120030416A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU50845 23381 PIT- FOUND SKIN WITH CHAF MARKS THROUGH WEAR STRIPS, STATION 880-887 STRINGER 1L-1R. BLEND DAMAGED AREA, INSTALL DOUBLER, TRIPLER, COUNTER BORE, INTERNAL DOUBLER (WEB PLATE) PER EA 76023. (M) 2L72 4F RTA16WE 20030514002012003051400201WP 2003 5 14 03FDEA00696 120030508A5410 PLATE DOUG DC10 DC1010 3022110WP NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25375FE 46613 NR 3 ENGINE O/B T/R TRANSILATING COWL UPPER SLEVE WALL PANEL CRACKED. REMOVED SIDEWALL PANEL PLATE IAW SRM 51-35-01. RECEIVED NEW PART ON TRAVELER T2/331654, LOCATED AND DRILLED HOLES IAW SRM 51-35-01, PRIMED IAW SRM 51-21-01, INSTALLED PLATE IAW SRM 51-35-01. 2L73 4F A22WE 20030520001012003052000101NM 2003 5 20 AALA20030355 120030320A3397 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21786AN 30250 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4D INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 4D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030610000862003061000086NM 2003 6 10 DLM88030427 120030503A5342591214186 ANGLE DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27908DE 53417 THE RT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND WITH A CRACK NEAR CANTED FS 1474. THE CRACK WAS REMOVED WITH A TRIMOUT TO THE HORIZONTAL FLANGE OF THE ANGLE. THE AREA WAS REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384977-14, REV A. 2L72 4F RTA6WE 20030606000472003060600047CE 2003 6 6 NE52003F00000 120030515A3710442CW PUMP CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO VACUUM SYS INOPERATIVE B NE5RO OTHER O OTHER NRNOT REPORTED 1 GL13635MA 402C0634 VACUUM PUMP INOPERATIVE 1L72 3O3 O A7CE E8CE 20030611000902003061100090SW 2003 6 11 HEEA086698 120030522A6220412310400101 BEARING BELL 412 412 1182202SW M/R ROD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03214981026 36003 MAIN ROTOR ROD BEARING HAS WEAR. 1G72 4U H4SW 20030613001102003061300110NM 2003 6 13 SWAA031251 120030605A53206545409 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20030613001392003061300139NM 2003 6 13 SWAA031220 120030603A3260FCA410 RELAY BOEING737 7373TO 138447GNM COCKPIT FAULTY A SWAAO OTHER J WARNING INDICATION CRCRUISE 1 SW29697SW 23838 NOSE GEAR UNSAFE LIGHT IS ILLUMINATED WHEN GEAR IS RETRACTED. REMOVED AND REPLACED NOSE GEAR LATCHING RELAY AND M983 GEAR RED LIGHT CARD PER MM. 2L72 4F RTA16WE 20030617002342003061700234EA 2003 6 17 QXEA200300703 120030524A7120 FITTING CNDAIRCL600 CL6002C10 1390015EA NR 1 ENGINE SCORED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - INSPECTED NR 1 AFT ENGINE THRUST FITTING AND FOUND OUTER SURFACE TO BE SCORED ACROSS FACE. REPAIRED IAW HORIZON AIR EA R-71-36. 2L72 4F RTA21EA 20030617003222003061700322NM 2003 6 17 SWAA031273 120030607A57546573714 SLAT BOEING737 7372T4 1384492NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED 1/2D CHECK, FOUND NR 3 L/E SLAT CRACKED AT OUTBD AUX TRACK CUTOUT. REPAIRED NR 3 L/E SLAT PER SRM. 2L72 4F A16WE 20030617002132003061700213NM 2003 6 17 QXEA200300721 120030605A5210 SKIN BOMBDRDHC8 DHC8401 1390041NM PAX DOOR DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - FOUND ADDITIONAL DAMAGE TO MAIN CABIN DOOR. TWO DENTS 6.5 INCHES APART. IMPACT AT THESE POINTS HAS CAUSED LARGER DENT. REPAIRED IAW HORIZON AIR EA 6-52-295, RD 8/4-52-126 AND Q400 SRM 51-25-05, PAGE 208. 2H72 4T RTA13NM 20030522001242003052200124 2003 5 22 SWAA031126 420030519A256565C16820 HOOK BOEING737 7373H4 1384600NM ESCAPED SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINER HOOK LOOSE. SECURED FWD RETAINER HOOK PER MM. 2L72 4F RTA16WE 20030620000402003062000040NM 2003 6 20 USAABB03084 120030603A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19630AU 27808 FOUND FLOOR LEVEL EMERGENCY LGIHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030623000292003062300029 2003 6 23 USAABB03072 420030514A2565D30654122 LANYARD BOEING757 7572B7 1384964NM ESCAPE SLIDE FRAYED A USAAK NONE O OTHER ININSP/MAINT 1 EA19625VJ 27246 FOUND FRAYED LANYARD ON R1 DOOR SLIDE. MAINTENANCE FOUND THAT THE COVER ATTACH LANYARD WAS FRAYED. THE SLIDE WAS REPLACED. (M) 2L72 4F RTA2NM 20030624000412003062400041NM 2003 6 24 CALA0300323 120030609A5330 SKIN BOEING737 737824 13844BZNM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 A FUELING TRUCK STRUCK THE AIRCRAFT ON THE FUSELAGE SKIN BETWEEN STA 1040 AND 1088 AND BETWEEN STRINGERS 18R AND 20R. THE DAMAGE INCLUDED PUNCTURED AND DENTED SKIN, SEVERED STRINGERS, A TWISTED STRINGER, DENTED SHEAR TIES, AND A DENTED FRAME. THE DAMAGED AREAS WERE REPAIRED IAW ECRA 5330-03258. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5330-03258 WITHIN 24 MONTHS. 2L72 4F RTA16WE 20030707001112003070700111WP 2003 7 7 UPS03840864 120030616A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LEFT WING LE. UPPER RIBS ARE CRACKED AT XFS 781.25,XFS 797.5, XFS 803.75. STOP DRILLED CRACKS,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20031211001792003121100179NM 2003 12 11 USAABB03207 120031003A335020121 CHARGER BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19619AU 27198 CLT - FOUND BULLNOSE EMERGENCY LIGHT AT STATION 1190 LEFT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY. (M) 2L72 4F RTA2NM 20031217000412003121700041WP 2003 12 17 DHL2003807532 120031024A572036169622 CLIP DOUG DC8 DC873F 302199FWP WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NR 4 MAIN TANK INTERIOR (1EA) CLIP CRACKED, STA XRS 172.000 S-75R (INSIDE ACCESS DOOR 505D). REMOVED AND REPLACED (1EA) CRACKED CLIP IN NR 4 MAIN TANK STA XRS 172.000 S-75R, REF ACCESS DOOR 505D IAW SRM 51-1-20D PG 21, 9. REFER TO NR 1482 FOR LEAK CHECK. 2L74 4F RT4A25 20030925000482003092500048 2003 9 25 AALA20030772 420030707A2565 SPRING BOEING757 757223 1384957NM GIRT BAR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21636AM 24594 DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS NEEDING REPLACED. REPLACED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030925001042003092500104NM 2003 9 25 VK62003F00000 120030806A27416355B000103 ACTUATOR BOEING737 737* NM STAB TRIM FOD B VK6RO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL09 3860 VHVOB A WASHER WAS FOUND LOOSE INSIDE OF THE STABILIZER TRIM ACTUATOR. THE WASHER IN QUESTION IS NOT PART OF THE BILL OF MATERIAL FOR THE 6355B0001-03 ACTUATOR. THE LOOSE WASHER CAUSED AN INTERMITTENT FAULT THAT LEAD TO THE REMOVAL OF THE ACTUATOR. 2L72 4F RTA16WE 20040819000172004081900017EU 2004 8 19 KBM2004F00165 120030826A78100292808740 STRAP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HEAT SHIELD DETERIORATED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 MO 5 HEAT SHIELD STRAP BRACKET HEAT SHRINK IS DETERIORATED. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20050222002202005022200220 2005 2 22 ERAA097083 420030823A25624530190 ELT BOLKMS105 BO105S 5626006EU CABIN CRACKED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03130EH 558 ELT CRACKED DUE BATTERY CHANGE SUB ASSY AND TOP COVER CRACKED. REPLACED SUB ASSY AND TOP COVER, PRODUCT LABEL AND BATTERY TESTED.. 1G72 3U H3EU 20060801001562006080100156WP 2006 8 1 IXXA060477S 120030204A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND FRAME DAMAGED AT STATION 1903 LEFT SIDE ABOVE HINGE CUT OUT. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR IAW DC8 SRM 51-1-8, 53-2-0, AND 51-1-21. 2L74 4F RT4A25 20070503002322007050300232NM 2007 5 3 AT0700050 120031022A5311 FRAME BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15992AT 55136 A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. FORMERS AT STA 180 DAMAGED. FABRICATED REPLACEMENT SECTION OF FORMERS STATION 180, MATERIAL 7075 T6 INSTALLED PER B717-SRM 53-00-06 FIG 2. 2L72 4F TRA6WE 20030819000032003081900003EU 2003 8 19 BAQA087936 120030708A6240L771M40C1003 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE RPM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH8 0131 TRIPLE RPM INDICATOR LASTED LESS THAN 8 HOURS OF FLIGHT TIME. REQUEST WARRANTY. RMA R043477 REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030402000472003040200047NM 2003 4 2 2003UALA00324 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT STA 1420 BETWEEN STR 25L AND 26L, UPPER FRAME FLANGE DENTED MAJOR REPAIR ACCOMPLISHED. PERFORMED FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20030328000192003032800019SW 2003 3 28 CA030218004 120030212A6510206040106001 SPRING BELL BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL DRIVESHAFT BROKEN W O OTHER O OTHER NRNOT REPORTED 1 CA AMN10022 (CAN) SPRING BROKE, TURNED SIDEWAYS AND CHAFED SPHERICAL COUPLING AND PLATE. 1G71 3U3 U H2SW E4CE 20030331001122003033100112EU 2003 3 31 DHL2003365002 120030327A261232402808 CONTROL BOX AIRBUS300 A300B4203 3930306EU NR 2 FIRE LOOP MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01365DH 149 ENGINE NR 2 LOOP "A" WILL NOT TEST. TRANS TO DMI 12384 PER MEL 26-12-01 CAT "B" PLACARD INSTALLED. CHECKED NR 2 ENGINE "B" LOOP SYSTEM AND CHECKED OK. REF. DMI #12384 - ENGINE #2 LOOP "A" WILL NOT TEST. REMOVED AND REPLACED NR 2 ENGINE FIRE DETECTION CONTROL BOX. OPS CHECKED OK IAW M/M 26-11-12. THIS CLEAR DMI 12384 PLACARD REMOVED. 2L72 4F RTA35EU 20030404001662003040400166NM 2003 4 4 SWAA030558 120030311A33506556633 LENS BOEING737 7373H4 1384600NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 EMERGENCY EXIT LIGHT LENS FELL OFF AT LT MID CABIN. REINSTALLED LENS PER MM. 2L72 4F RTA16WE 20030408001082003040800108EA 2003 4 8 2003F00216 120030220A3230601R751461E SOLENOID VALVE CNDAIRCL600 CL6002B16 1900305EA NOSE WHEEL WELL INOPERATIVE A UG8AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23241FB 5102 NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF, NOSE GEAR DOORS DID NOT OPEN. INOPERATIVE NLG DOOR SOLENOID VALVE. VERIFIED THROUGH TROUBLESHOOTING METHODS THAT 'DOOR OPEN' SOLENOID COIL WAS ELECTRICALLY OPEN. INSTALLED OVERHAULED SOLENOID VALVE, OPS AND LEAK CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4F RTA21EA 20030410001412003041000141 2003 4 10 SWAA030695 420030326A2565D31354 SLIDE BOEING737 7373H4 1384600NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030414000482003041400048CE 2003 4 14 CA030312023 120030308A3241 WARNING LIGHT CESSNA500 550 2076604CE PWA 530 PW530A NE BRAKE ANTI-SKID ILLUMINATED W O OTHER J WARNING INDICATION LDLANDING 1 CA (CAN) DURING APPROACH, ANTI-SKID INOP ANNUNC ILLUM. EMERG SYS WAS UTILIZED FOR FINAL BRAKING. ILLUM OF ANTI-SKID ANNUNC, NORMAL BRAKING, ANTI-SKID OR POWER BRAKES ARE BLOCKED, ARE NOT AVAILABLE BY DESIGN. EMER BRAKING MUST BE UTILIZED. A/C WAS RETURNING FROM TRIP ENCOUNTERING RAINS AND CONDENSATION. NOT VERIFIED AS TO WAS ANTI-SKID INOP ANNUNC ILLUMIN AS FAULT COULD NOT BE REPEATED MOISTURE COULD BE POSSIBILITY. POWER BRAKE SYS INCLUDING ANTI-SKID PORTION WAS CHECKED FOR FUNCTION AND BLED. DURING MAINT, AIR IN BRAKING SYS, PRECHARGE VALUE ON ACCUM WAS LOWER THAN SPECIFIED. POSSIBLE THAT AIR IN SYS PROVIDED FEEDBACK TO DIGITAL ANTI-SKID MONTIORING SYSTEM, IND SYS FAULT, DISABLING NORMAL POWERBRAKING. 1L72 4F4 F A22CE E00053EN 20030408000532003040800053SO 2003 4 8 030035164 120030404A54111159P20502511 FRAME GULSTMG1159 G1159A 3970109SO LT PYLON CRACKED B Y3PRK NONE O OTHER ININSP/MAINT 1 SO35323JH 434 LEFT HAND PYLON FRAME (WEB) AT FS 556 HAS 2 HORIZONTAL CRACKS RUNNING BETWEEN 2 HYDRAULIC LINE CONNECTIONS. SHEAR WEB PART NUMBER 1159P20502-511. CRACKS ARE WHERE THE FOLLOWING HYDRAULIC LINES ARE ATTACHED TO WEB WITH BULKHEAD FITTING: AE700755-1 (FLEX LINE), 1159P20518-103S20, 1159P20518-123-P-12. 2L72 4F A12EA 20030417001432003041700143NM 2003 4 17 PCAA0302038 120030207A3350 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13833EX 282 DURING SCHEDULED MAINTENANCE VISIT EMERGENCY LIGHTS WOULD NOT TURN OFF WHEN SELECTED TO OFF POSITION IN COCKPIT. LIGHTS WOULD ONLY REMAIN OFF IN ARM POSITION. EMERGENCY LIGHTING SYSTEM TROUBLESHOT. ALL 6 BATTERY PACKS, FLIGHT COMPARTMENT SWITCH, AND POWER CONTROL BOX WERE REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030417001452003041700145NM 2003 4 17 XNOA01103 120030211A2612 WARNING LIGHT BOEING727 727227 1384078NM CARGO FIRE FALSE ACTIVATIONA XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL2379754 21363 DURING DE-ICE AFT LOWER CARGO FIRE WARNING AND BELL, DISPLAY READ AFT FIRE. VISUALLY INSPECTED AFT LOWER CARGO AREA, ALL CLEAR. NO DEFECTS. PERFORMED SYSTEMS CHECK OF LOWER AFT PIT FIRE DETECTION SYSTEM. OPS CHECK GOOD IAW SECURE-A-PLANE TECHNOLOGY MANUAL. A/C OK FOR SERVICE. 2L73 4F A3WE 20030424002122003042400212WP 2003 4 24 UPS03840373 120030313A5310 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, MAIN CABIN FLOOR PANEL STA 220 PANEL-A FOUND SPLICE CORRODED. REMOVED FLOORBOARD SPLICE, FABRICATED NEW SPLICE IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SPLICE IAW DC8 SRM 5 3-2-3. 2L74 4F RT4A25 20030424000622003042400062CE 2003 4 24 GLBA2003036 120030321A2697 WIRE BEECH 1900 1900D 1154162CE LT ENG FIRE EXT BROKEN A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03211GL UE211 LT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUM. REPAIRED BROKEN WIRE SPLICE ON LEFT ENG FIRE BOTTLE SQUIB. 2L72 4T RTA24CE 20030425000372003042500037SO 2003 4 25 RAIA00303083 120030324A32501170A180001 POTENTIOMETER EMB 145 EMB145 3260210SO NLG STEERING MALFUNCTIONED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03806HK89570 145112 GRR- AIRCRAFT PULLS HARD RIGHT DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED STEERING FEEDBACK POTENTIOMETER, OPS CK OK. 2L72 4F RTT00011AT 20030428001222003042800122NM 2003 4 28 CALA0300170 120030405A5330 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT STA 837-867, STRINGER 1. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2L72 4F4 FRTA16WE E2GL 20030428001952003042800195SO 2003 4 28 C2XA03IA035 120030408A323023092900401 UPLOCK EMB 145 EMB145LR 3260212SO LT MLG WW MALFUNCTIONED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2713553 145585 ELP- FLIGHT 2833, DURING CLIMB THE CREW NOTED THAT THE LANDING GEAR DISAGREE MESSAGE APPEARED. THE CREW RETURNED THE AIRCRAFT TO ELP AND LANDED WITHOUT INCIDENT. ELP- MAINTENANCE RESET THE UPLOCK HOOK ON THE LEFT MLG UPLOCK BOX IAW EMB-145 MM 32-32-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030430002582003043000258NM 2003 4 30 SWAA030819 120030411A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030502001982003050200198NE 2003 5 2 AWXA200300416 220030414A7300HAD22308 THERMOCOUPLE AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE NR 2 ENGINE DEFECTIVE A AWXAO OTHER S AFFECT SYSTEMS DEDESCENT 1 WP28820AW 1397 ON DESCENT WITH AUTO THROTTLE ON 11,000 FT, NR 2 ENGINE SPOOLED NORMALLY TO MAINTAIN MANAGED SPEED, NR 1 ENGINE DID NOT SPOOL FOR 3 TO 4 SECONDS. NR 1 ENGINE WENT TO CLIMB THRUST RESULTING IN SUBSTANTIAL YAW (3 TO 5 DEG) ROLL OF 2 TO 3. ON IDLE DESCENT 6000 FT NR 1 ENGINE FUEL FLOW 800, NR 2 ENGINE 1450 WITH HIGH N1, N2 & EPR. TURNED OFF AUTO THROTTLES, APPROACH & LANDING NORMAL. MX TROUBLESHOT SYS USING TSM 73-00-00-810-877 AND FOUND NR 2 ENGINE IDLING HIGH. MX FOUND FADEC NR 2 A & B FAULTS FOR FUEL TEMP SENSOR (4017KS). REMOVE & REPLACED NR 2 ENGINE FUEL TEMP SENSOR. OPS & LEAK CHECK GOOD. AUTO FLT SYS & FADEC INDICATE NO FAULTS. PERFORMED HIGH POWER ASSURANCE TEST, OPS NORMAL & ALL PARAMETERS MATCH.2L72 4F4 FRTA28NM E311NE 20030509001352003050900135NM 2003 5 9 CALA0300235 120030509A53116545801512 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0977303 23354 CORROSION ON TOP OF FRAME AT STA 227.8, WL 148. COMPLETED INTERIM REPAIR AND PLACED ON DIP PER ECRA 5311-01148. 2L72 4F RTA16WE 20030513000952003051300095EU 2003 5 13 AWXA200300497 120030429A5320D5391160160 SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK 4 EACH CRACKS WERE FOUND AT RIVET HOLES ON FORWARD CARGO COMPARTMENT CEILING PANEL SUPPORT, AFT BULKHEAD FR 34, RBL 10 & 28, LBL 10 & 28. MAINTENANCE ROUTED OUT HOLES; FABRICATED ANGLE DOUBLERS AND FILLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5327-02143-JS1. 2L72 4F RTA28NM 20030514001752003051400175NM 2003 5 14 P5CA0300875 120030504A2910 WARNING LIGHT BOEING747 7472U3B 1384846NM NR 1 HYD SYS ILLUMINATED A P5CAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP23923FT 22769 NR 1 HYD SYS HEAT LIGHT ON. RAN AND CHECKED ENG & ADP'S OPERATING FLAPS TEMPS WERE SIMILAR & BELOW 100 C PER TEMP IND. DEFERRED O/TEMP LIGHT PER MEL 29-10. 2L74 4F RTA20WE 20030529000482003052900048SW 2003 5 29 HEEA086639 120030521A6210412030437103 CAP BELL 412 412 1182202SW M/R BLADE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 CAP HAS RUBBER WORN. 1G72 4U H4SW 20030708001132003070800113NM 2003 7 8 AALA20030616 120030529A2934 SENSOR BOEING757 757223 1384957NM HYD QTY MALFUNCTIONED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21691AA 25697 CLIMBING OUT OF FL350 EICAS DISPLAYED LOSS OF LT HYD SYS QTY, RSVS LINE ON OVHD PANEL ILLUMINATED. AILERON INPUT, ON AUTOPILOT) INCREASED BY 3 UNITS. A LOUD BANG HEARD IN AIRFRAME. ABOUT ONE MINUTE AFTER INDICATIONS, BOTH PUMP PRESS LIGHTS WERE EXTINGUISHED ON LT SIDE. AN LEFT SYSTEM PRESSURE WAS NORMAL ON EICAS DURING DESCENT THROUGH 10,000 HYD QTY RETURNED FROM 0.0 TO 1.09 NORMAL. PLACARDED L HYD QTY IN COCKPIT (EICAS) INOPERATIVE PER MEL. ALL HYD QUANTITIES CHECKED AND FULL. NO LEAKS FOUND. PERFORMED WALKAROUND INSPECTION WITH ALL PUMPS ON. ALL FLIGHTS CONTROLS OPERATED NORMAL. REPLACED HYDRAULIC QUANTITY MONITOR UNIT PER M/M ALL REQUIRED TESTS CHECKED OK. REMOVED PLACARD CLEARED MIC SHEET. (M) 2L72 4F RTA2NM 20030710000292003071000029NM 2003 7 10 USAASB03073 120030604A523010608211 SEAL BOEING737 737401 1384701NM CARGO DOOR LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19424US 23991 MCO - FLT 553 - EN ROUTE FROM RSW TO CLT, CAPTAIN REPORTED THE ALTITUDE WARNING HORN BEGAN SOUNDING AND THAT THE CABIN PRESSURE WAS CLIMBING. CREW WAS UNABLE TO CONTROL CABIN PRESSURE AT ALTITUDE. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL LEAKING. REPOSITIONED SEAL. LEAK CHECK GOOD. ALSO, FOUND APU DUCT FLEXIBLE BOOT SEAL HAD A BROKEN CLAMP. REMOVED AND REPLACED CLAMP. PERFORMED HULL LEAK DOWN RATE CHECK PER MM 05-51-91. CHECKS GOOD. (M) 2L72 4F RTA16WE 20030711000942003071100094 2003 7 11 GLBA2003085 420030617A22101303800031 TRANSDUCER BEECH 1900 1900D 1154162CE RUDDER BOOST MALFUNCTIONED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03208GL22835 UE208 RUDDER PEDALS STIFF WHEN POWER ADDED. REMOVED AND REPLACED RT RUDDER BOOST TRANSDUCER, OPS CK GOOD WITH DEAD WEIGHT TESTER. 2L72 4T RTA24CE 20030714000392003071400039NM 2003 7 14 SWAA031411 120030622A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727E PLUS 12 AT STR 19R AND BS 520 AT STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030714001532003071400153 2003 7 14 HEEA088092 420030709A2212117884141 CONTROL UNIT BOLKMS117 BK117A1 5626010EU AUTOFLIGHT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 POSSIBLE DAMAGE DUE TO SHORT IN WIRING HARNESS. SENT TO AMERICAN EUROCOPTER CORP. FOR WARRANTY REPAIR. 1G72 3U H13EU 20030716000362003071600036NM 2003 7 16 TSAA0353151 120030430A53136546525 STRINGER BOEING737 73725A 1384481NM FUSELAGE GOUGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 DAMAGED OR GOUGE STRINGER DISCOVERED AT BS 382. CUTOUT GOUGED AREA. FABRICATED FILLER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 3. (M) 2L72 4F RTA16WE 20030128002322003012800232SW 2003 1 28 HEEA083884 120030116A6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 MAIN ROTOR UNIVERSAL HAS BEARING WEAR. 1G71 3U O H2SW 20030204002022003020400202NE 2003 2 4 SWAA030130 220030117A7200CFM563 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 1 BIRD STRIKE A SWAAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW29364SW 26575 722398 IN FLT SHUTDOWN, DIVERSION, DECLARED EMERGENCY, DURING TAKEOFF, NR 1 ENG DEVELOPED SEVERE VIBRATION. DIVERTED TO OAK. FOUND FOD TO NR 1 ENG. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20030204002462003020400246NM 2003 2 4 SWAA030232 120030130A32116546113 TRUNNION PIN BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030205000892003020500089NM 2003 2 5 UPS03240133 120030120A5330 SKIN BOEING727 72722C 138400FNM AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 INSPECTION TYPE:SP CRACK FOUND ON FUSELAGE ABOVE # 1 ENGINE STATION 1183 STRINGER 4L-8L REMOVED PREVIOUS REPAIR DOUBLER AND DAMAGED AREA I.A.W. SRM.53-30-3 FIG. 26 & 24, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I.A.W. SRM. 53-30-3 FIG. 26 & 24 AT STA. 1183 BETWEEN STRINGER 4L TO 8L 2L73 4F A3WE 20030207000972003020700097NM 2003 2 7 03FDEA00052 120030120A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 FRAME CRACKED IN THE FWD CARGO BAY STA 660 RBL 3 WL 148 UNDER FLOOR SUPPORT. FWD CARGO FRAME CRACKED AT BS 660 RBL 3 WL 148 OUT OF LIMITS PER SRM 53-10-4. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3 2L73 4F RTA3WE 20030213000612003021300061EU 2003 2 13 00076 120030202A7500 LINE AMD FALC20FALCONE 2720305EU BLEED AIR LOOSE E HAEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05285TW 285 PILOT REPORTED ODOR OF BURNING WIRES , RETURN TO DEPARTURE AIRPORT. MAINTENANCE FOUND LOOSE BLEED AIR LINE BEHIND CO-PILOT RADIO RACK, GROUND RUN CHECK GOOD. 2L72 4F A7EU 20030213000752003021300075NM 2003 2 13 03032424 120030201A2612 WARNING SYSTEM DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE FALSE ACTIVATIONA VTZAFEA ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27424FJ 3185 DURING CLIMB, CREW RECEIVED LT ENGINE FIRE INDICATION, CREW DISCHARGED FIRE BOTTLE AND INDICATION PERSISTED; SECOND BOTTLE WAS DISCHARGED AND INDICATION WENT OUT. FLIGHT CREW SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY WITH ATC. AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED FIRE BOTTLES, INSPECTED ENGINE FOR SIGNS OF FIRE AND PERFORMED OPERATIONAL CHECK OF FIRE DETECTION SYSTEM. OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 FRTA55NM E35NE 20030219001182003021900118NM 2003 2 19 SWAA030344 120030211A335057771 CAP BOEING737 7372T4 1384492NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AT FWD CABIN. INSTALLED END CAP PER MM. 2L72 4F A16WE 20030221000592003022100059NM 2003 2 21 QXEA0300183 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 5 SEAT TRACK HAS SCRATHES AT STATION 445-455. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030224000962003022400096SW 2003 2 24 HEEA084217 120030120A5320407070620137 PANEL BELL 407 407 1182206SW PAX DOOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 PAX DOOR INTERIOR PANEL CRACKED. 1G71 3U O H2SW 20030116000052003011600005GL 2003 1 16 ERAA082947 220030106A7320252466715H GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE FLUCTUATES H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01298EH11924 S845 GOVERNOR PRODUCING FLUCTUATING TORQUE. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A 1G72 3U3 U H3EU E4CE 20030121000272003012100027SW 2003 1 21 HEEA083219 120030108A7120206064107109 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036603X 51412 ENGINE MOUNT LEG ASSY HAS A WORN BEARING. SCRAPPED. 1G71 3U H2SW 20030304000482003030400048SW 2003 3 4 HEEA084580 120030214A6230 BEARING BELL 412 412 1182202SW M/R MAST LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 A1999 36005 MAIN ROTOR MAST LINK HAS WORN BEARINGS. REPAIRED. 1G72 4U H4SW 20030305000412003030500041 2003 3 5 HEEA084623 420030214A2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 VHF TRANSCEIVER BNC CONNECTOR PULLED OUT. REPLACED BROKEN J9082 RF CONNECTOR. REPAIRED PROBLEM. ALSO REPLACED BAD Q102 TRANSISTOR INSULATOR. ADJUSTED CARRIER SQUELCH, MIC GAIN, TRANSMIT COMPRESSOR AND SIDETONE. BENCH CHECK GOOD. 1G72 4U H4SW 20030227000402003022700040 2003 2 27 HEEA084375 420030211A2340AA21400 SIREN BELL 407 407 1182206SW PA SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 PA SYSTEM SIREN INOPERATIVE, BURNS FUSE. 1G71 3U O H2SW 20030228000892003022800089SW 2003 2 28 HEEA084455 120030213A6510206040322001 BUSHING BELL 206 206L4 1182110SW SHAFT HANGER CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F 52038 TAIL ROTOR DRIVESHAFT HANGER BEARING SEAL SEPARATED. REPLACED 2 EACH BEARINGS 206040339103 DUE TO SEAL SEPARATED. REPLACED 2 EACH BUSHINGS 206040322001 DUE TO CORROSION. REPAIRED. 1G71 3U NCH2SW 20030324000172003032400017NM 2003 3 24 2003UALA00268 120030312A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29957UA 26707 BS 178 BULKHEAD AT LOWER LT RADAR MOUNT IS CRACKED AT LOWER INBOARD HOLE . MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20030324000812003032400081WP 2003 3 24 ARWA20030208 120030220A2611100064901 SMOKE DETECTOR DOUG DC8 DC861 3021952WP CARGO BAY FAILED A ARWAO OTHER L NO TEST NRNOT REPORTED 1 SO1929UA 46159 ON PRE-FLIGHT FOUND FORWARD "A" BELLY LOWER CARGO SMOKE DETECTOR INOPERATIVE. ENTERED ITEM ON DMI 17493 AS PER MEL 2G-10-1-0-1 CAT "B". REMOVED AND REPLACED SMOKE DETECTOR UNITS (SDUS) S/N 4566, 14470 & 13067 AS PER STC ST00746LA-D. OPERATIONAL CHECK GOOD. THIS CLEARS DMI 17493 (FORWARD A BELLY INOP LOWER CARGO SMOKE DETECTOR. SYSTEM CHECK NORMAL IAW STC # ST00746LA-D. 2L74 4F 4A25 20030307001312003030700131WP 2003 3 7 AALA20030103 120030123A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21593AA 53256 TUL - FOUND FUSELAGE SKIN IS CRACKED THROUGH RIVET STATION 1380 RIGHT SIDE JUST ABOVE PYLON. DOUBLER INSTALLED PER SRM 53-01, FIG 2 SHEET 3 AND AARD 53-30-00-00 REV DATED 8-30-02. (M) 2L72 4F RTA6WE 20030310000752003031000075 2003 3 10 HEEA084979 420030227A34526221270001 TRANSPONDER BELL 412 412 1182202SW ATC SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 ATC TRANSPONDER HAS LOW POWER OUT. SCRAPPED. 1G72 4U H4SW 20030311000262003031100026EU 2003 3 11 MALA030188 120030309A33506013211 POWER SUPPLY SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15115XJ EMERGENCY LIGHTS AT LH AND RH AFT EXTERNAL LIGHTS 3LN, & 4LN, PASSENGER EMERGENCY LIGHTS 41LN, 42LN,43LN, AND FLOOR PROX SIGNS 49LN AND 50LN INOP. MAINTENANCE FOUND EMERGENCY POWER SUPPLY AT 24LN AT FAULT, REMOVED AND REPLACED POWER SUPPLY WITH SERVICABLE UNIT PN 60-1321-1 SN/OFF 17511, SN/ON 17653. IAW MAL TASK CARD #335002 OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE6 20030311000342003031100034NM 2003 3 11 PCAA0303051 120030222A575185740004001 AILERON DHAV DHC8 DHC8102 2809003NM LEFT CRACKED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13824EX247573929 387 DURING C LEVEL INSPECTION LEFT AILERON SKIN FOUND TO BE CRACKED AT OUTBOARD ATTACH POINT, LOWER SKIN AT CORNER OF ATTACH POINT CUT OUT. CRACK WAS REPAIRED IN ACCORDANCE WITH PIEDMONT ENGINEERING DRAWING EO8-57-03-0248 AND APPROVED THROUGH CALLAHAN REPAIR SERVICES DERT-230219-CE IDENTIFICATION # CAS-AAL106. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030318000812003031800081WP 2003 3 18 ASAA0380018 120030103A5321993659947 FLOOR PANEL DOUG DC9 DC983 3022083WP CARGO BAY DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL EDGE DAMAGED AT FS 636-693. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030418001112003041800111NM 2003 4 18 UPS03240223 120030222A3350 LIGHT BOEING727 727180C 138406GNM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01920UP 19873 EMERGENCY EXIT LIGHT AT CREW ENTRANCE DOOR INOP. RESET LIGHT PACK, CHECKS GOOD. 2L73 4F A3WE 20030418001372003041800137SO 2003 4 18 SWIA200311794 120030219A5753 STRUCTURE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LT TE FLAP CRACKED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07566SW 120341 FOUND LEFT INBOARD FLAP INBOARD BUTTE DOOR CRACKED. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD BUTTE DOOR BEARING BRACKET WITH NEW BRACKET IAW EMB120 MM 20-10-01. P/N: 120-22883-001. 2L72 4T4 TRTA31SO E20NE 20030422000642003042200064NM 2003 4 22 MEX2003092 120030322A32503800014106 VALVE BOEING757 7572Q8 1384972NM NLG STEERING MALFUNCTIONED A ASMFD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SW23801AM 25624 MEX-TIJ - AIRCRAFT RETURNED TO GATE, NOSE WHEEL TURN TO THE RIGHT DURING TAKEOFF AND IT WAS ABORTED, DURING REVISION WAS DETECTED METER VALVE VERY HOT. IN HANGAR, NOSE WHEEL STEERING VALVE WAS REPLACED IAW MM 32-51-00, TESTS CORRECT. (M) 2L72 4F RTA2NM 20030421001762003042100176WP 2003 4 21 GTIA030128 120030221A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND FORWARD CABIN STATION 206 TO STATION 160 LBL 44 INCHES TO LBL 56 INCHES, 12 BY 40, SOFT/MUSHEY DETERIORATED. FABRICATED CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040329001782004032900178NM 2004 3 29 2003UALA00864 120031116A2133 MOTOR BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE OUTFLOW DOOR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29620UA 21880 RETURNED TO FIELD DUE TO CABIN PRESSURIZATION PROBLEMS. AUTO CABIN INOP EICAS MESSAGE. MANUAL CONTROL FAILED ON DESCENT. *S/D* THE OUTFLOW DOOR DC MOTOR WAS FOUND TO FAIL WHEN COLD SOAKED. 2L72 4F4 FRTA1NM E3NE 20030805000962003080500096EU 2003 8 5 USAASA03081 120030715A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19716UW 1055 CLT - THE EMERGENCY LIGHT SYSTEM FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE BATTERY AT EMERGENCY POWER SUPPLY UNIT 11WL. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030422000072003042200007EA 2003 4 22 ASOA03076 120030222A5346 SUPPORT CNDAIRCL600 CL6002B19 1900309EA LT & RT ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A HANGAR CHECK IN MCN, THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0073. (M) 2L72 4F RTA21EA 20030826000642003082600064NE 2003 8 26 2904062803 220030628A75327100B BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE DEFECTIVE E S4WAK NONE R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 WP074027Q92 2904 9456 BLEED VALVE WILL NOT CLOSE UNTIL 101 PERCENT NG. 1G71 3U3 U H9EU E19EU 20030828000892003082800089NE 2003 8 28 DL76L030621 220030708A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE RIGHT BIRD STRIKE A DALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO271200K40464 28457 724685 BIRDSTRIKE RT ENGINE. HIGH VIBES DURING CLIMB UP TO 3.8 N1.DUMPED 33K POUNDS FUEL. OVERWEIGHT LANDING AT SINK RATE OF 100FPM. ENGINE SHUT DOWN AFTER LANDING. BLADE DAMAGE FOUND ON THREE BLADES. LPC AND HPC BOROSCOPE PERFORMED IAW M/M. NO DEFECTS NOTED. FULL SET OF FAN BLADES REPLACED IAW M/M. ENG. RUN AND VIBE SURVEY IAW M/M. ALL SATISFACTORY. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2L72 4F4 FRTA1NM E24NE 20030828000962003082800096NM 2003 8 28 DL767030615 120030706A335020131A BATTERY PACK BOEING767 767232 1385132NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27108DL 22220 FOUND F/C EMERGENCY PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED M9008 BATTERY PACK. OPS CHECK NORMAL. 2L72 4F RTA1NM 20030829001962003082900196EA 2003 8 29 ASOA03347 120030801A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 FLT 4244 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE MAIN PASSENGER DOOR WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACD THE BOTTOM STEP ON THE MAIN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030902000902003090200090EA 2003 9 2 SWIA200312143 120030624A5210 ROLLER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FROZEN A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07435SW 7555 PAX DOOR WARNING MESSAGE ON DESCENT, NO PRESSURE DROP. INSPECTED PAX DOOR, FOUND INNER DOOR HANDLE DETENT ROLLER FROZEN IN RETRACTED POSITION. REMOVED AND REPLACED ROLLER SHAFT PER CRJ MM 52-11-02. OPS CHECK GOOD. P/N OFF: 582-20352. 2L72 4F RTA21EA 20030728000392003072800039 2003 7 28 SWAA031545 420030714A2565D31354 SLIDE BOEING737 7377H4 1384404NM ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29728SW 27860 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030724000372003072400037NM 2003 7 24 DL76L030537 120030610A2710 BEARING BOEING767 767332 1382001NM TORQUE TUBE FAILED A DALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO27177DN 25122 DURING TAXI OUT AILERONS WERE STIFF AND BINDING WOULD NOT RETURN TO CENTER WITH OUT EXTRA FORCE. DISC CTL RD AT CA DRUM-RT LCCA OUTPUT/RT LCCA TORQ TUBE.FIM 27-11-00 TBL10. T/S PER FIM 27-11-00 FIG 106 STEP 2. F/O CONT WHEEL STIFF. DISC UPPER/LWR INPUT RODS FROM LT LCCA TO LCCA TORQ TUBE. DISC INPUT ROD FROM FEEL/CTR UNIT TO LCCA T TUBE. INSTD FEEL CTR UNIT BRG. RECONN RT LCCA OUTPUT/RTLCCA T TUBE. INSP PNL AREA AND PCA ROD ENDS. ALL CK GOOD. NO ROD OR TOUCHED. NO RII RQD. PNL INSTALLED. 2L72 4F RTA1NM 20030725000372003072500037SO 2003 7 25 RAIA00305132 120030505A27513631001005 CONTROL UNIT EMB 145 EMB145LR 3260212SO TE FLAP IND FALSE INDICATIONA RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK8588 2093 145044 FLAP LOW SPEED MESSAGE. MAINTENANCE DEFERRED PER MEL 27-53-00, SUBSEQUENTLY REMOVING AND REPLACING THE FLAP ELECTRIC CONTROL UNIT. 2L72 4T RTT00011AT 20030730000062003073000006WP 2003 7 30 ABXA030199 120030415A531337592221 LONGERON DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23843AX 46017 AFT CARGO STATION 1270, STRINGER 36, CRACKED. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED LONGERON REPAIR IAW REA D853-46699MR. REMOVED AND REPLACED DAMAGED 3759222-1 SPLICE FITTING IAW REA D853-46699MR. 2L74 4F 4A25 20030813001992003081300199 2003 8 13 SWAA031647 420030723A25656557463 ATTACH FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER MM. 2L72 4F RTA16WE 20030904000982003090400098EA 2003 9 4 QXEA200301015 120030823A1430 BOLT CNDAIRCL600 CL6002C10 1390015EA LT WING WORN A QXEAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 NM09611QX 10041 PDX- FUEL DRIPPING FROM NR 4 FLAP HANGER NACELLE ON LEFT WING. FOUND LEAK AT NR 4 FLAP CANOE FORWARD FLAP HINGE BOX BRACKET INBOARD FORWARD BOLT HEAD. REMOVED AND REPLACED BOLT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030905001072003090500107NM 2003 9 5 DL76S030633 120030711A3350333101582 BATTERY BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27118DL 23277 ON TRANSIT CHECK SQUIB TEST RIGHT EMERGENCY ESCAPE LIGHT DID NOT ILLUMINATE DURING TEST ONE. REMOVED AND REPLACED RT OFF WING ESCAPE SYSTEM BATTERY AND POWER PACK PER M/M. SQUIB TEST CKS NML. 2L72 4F RTA1NM 20030825001552003082500155NM 2003 8 25 AMTA200300890 120030707A3350 POWER SUPPLY BOEING737 73783N 13844HINM CABIN MALFUNCTIONED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11310TZ 28243 ALL EGRESS LIGHTS AROUND LEFT AFT SERVICE DOOR INOPERATIVE. RESET POWR SUPPLY WITH SWITCH PER 737 MM 33-51-00. LIGHTS OPS CHECKED NORMAL. (M) 2L72 4F RTA16WE 20030822000732003082200073EA 2003 8 22 COMA0360369 120030817A53116003603023 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA10366 7306 CRACKS NOTED IN THE FLANGE RADIUS OF LT AND RT FRAMES AT FS 178. DAMAGE REPAIRED IAW S/B 601R-53-055 PART B AND C PER EA 10-5320-00242. 2L72 4F RTA21EA 20030825001142003082500114WP 2003 8 25 ABXA030317 120030721A53305910228187 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23969AX 47464 CRACKS IN SKIN JUST AFT OF CANTED FRAME 1197 BELOW LG 13 L. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030728000772003072800077NM 2003 7 28 SWAA031567 120030715A33506556633 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29409WN 27896 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030825000782003082500078NE 2003 8 25 EIA2003108 220030809A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 2 VIBRATION A EIAAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 NM09485EV 20712 662506 AT 200 MILES FROM ZURICH FL 400 AT 1/2 THROTTLE NOTICED SHUDDER AND STALL. FUEL OFF THEN ON EGT DROP BUT NO RELIGHT SHUTDOWN CHECKLIST C/W. RAN INFLIGHT ENG START CHECK LIST RELIGHT BUT ENG SHAKING INCREASED TOWARD IDLE. SHUT ENG DOWN AND INFLIGHT SECURING CHECK LIST FOR ENG NR 2. THIS SDR TO REMAIN OPEN TIL FINAL DETERMINATION OF CAUSE. 2L74 4F4 F A20WE E20EA 20030827000862003082700086SO 2003 8 27 C2XA03CL118 120030702A3350110049 POWER SUPPLY EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714940 145033 DURING ROUTINE MAINTENANCE THE LT AND RT EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030910002172003091000217EU 2003 9 10 MALA03057 120030704A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING C-CHECK INSPECTION IN CVG, NR 1 SEAT RAIL FROM FRAME 18 TO 20 IS CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED PER EO NR A53026. REFER TO 409 NR 128123 FOR DETAIL. A/C RELEASE DATE 7/25/03. 2H74 4F RTA49EU 20030911000122003091100012EU 2003 9 11 UPS03141146 120030826A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01129UP 0814 EVACUATION SLIDE OR SLIDE RAFT WARNING LIGHT INOPERATIVE. DEFERRED IAW 52-73-01-01 OF MEL M265419 PLACARD INSTALLED RESEATED C/P ON POWER SUPPLY OPS CHECKED GOOD THIS CLEARS M265419 PLACARD REMOVED 2L72 4F RTA35EU 20030929000762003092900076NM 2003 9 29 03FDEA01445 120030901A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LEFT WING O/B FLAP I/B HINGE (A/C SIDE) LOWER ATTACHMENT BORE MATING SURFACE FOUND WITH CORROSION. 2L73 4F RTA22WE 20031001000262003100100026NM 2003 10 1 CALA0300516 120030908A5311 FRAME BOEING737 737724 13844BYNM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733714 28785 INSPECTION FOUND FRAME GOUGED UNDER Z-CHANNEL IN AFT CARGO COMPARTMENT AT STA 947.5, S25R. REPAIRED DAMAGED FRAME SECTION IAW ECRA 5311-01165. 2L72 4F RTA16WE 20031006001392003100600139NM 2003 10 6 SWAA032033 120030910A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 15R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031002000532003100200053WP 2003 10 2 UPS03841209 120030827A53403758497U2 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C2, LONG. 35R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA. 1140 AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG. 3758497,AND SRM. 51-1-20D. 2L74 4F RT4A25 20031014001252003101400125 2003 10 14 SWAA032167 420030927A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20031020001912003102000191NM 2003 10 20 DLM88030816 120030906A2920 HYDRAULIC LINE DOUG MD88 MD88 3023688NM HYD SYSTEM CHAFED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO27908DL 49539 RT HYD SYS FAIL RT HYD SYS PRESS LOW ON AOP WITH HYD PRESS AND QTY DECREASING. REPLACED CHAFED LINE IN AFT CARGO COMPT. 2L72 4F RTA6WE 20031027000122003102700012CE 2003 10 27 HYI2003F00013 120030806A801299103971 RELAY CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO STARTER BURNED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01106CA 402C1020 PILOT REPORTED RT STARTER STAYED ENGAGED. MECHANIC REMOVED AND REPLACED START RELAY AND RELEASED AIRCRAFT BACK TO SERVICE. 1L72 3O3 O A7CE E8CE 20031021002802003102100280NM 2003 10 21 CALA0300538 120030919A5347 SEAT TRACK BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND SEAT TRACK CORRODED AT STA 328-360, RBL 22. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52. 2L72 4F4 FRTA16WE E2GL 20031027000682003102700068CE 2003 10 27 8433001 120030717A2720 BOLT RAYTHN BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA CONTROL HORN LOOSE A JJBAK NONE O OTHER ININSP/MAINT 1 EA01843CA2665 672 UE382 DURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE 2L72 4T3 TRTA24CE E2NE 20031110001572003111000157NM 2003 11 10 SWAA032261 120031015A53116546529 FRAME BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT FUSELAGE FRAME, BS 440 WL 208. REPAIRED FRAME PER SWA EA. 2L72 4F A16WE 20031119000362003111900036NM 2003 11 19 AWXA200301199 120031001A3246 RETAINER BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE NR 3 MLG WHEEL MISSING A AWXAK NONE O OTHER TXTAXI/GRND HDL 1 WP28325AW 23260 ON ROLL BACK PRIOR TO TAXI RT INBOARD MAIN LANDING GEAR WHEEL ASSEMBLY WAS NOTICED COMING OFF AXLE. UPON FURTHER INVESTIGATION THE NR 3 WHEEL RETAINER RING WAS FOUND MISSING AND THE AXLE NUT WAS BACKED OFF. DAMAGE WAS NOTED TO THE WHEEL AND BRAKE ASSEMBLIES, THE HUB CAP AND WHEEL SPEED TRANSDUCER, AND RT MAIN LANDING GEAR INNER CYLINDER ASSEMBLY. MAINTENANCE REMOVED AND REPLACED ALL DAMAGED PARTS. 2L72 4F4 FRTA16WE E2GL 20031119000482003111900048NM 2003 11 19 DHL2003784006 120031010A2120 ODOR BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE COCKPIT DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01767AT 22001 STRANGE SMOKE ODOR IN COCKPIT. APPEARS TO BECOME MUCH STRONGER WITH GASPER FAN ON. DEFERRED IAW DHL MEL 21-24, CONTROL NR 14407. PLACARD INSTALLED. 2L73 4F4 F A3WE E2EA 20040114000402004011400040NM 2004 1 14 DLM88030952 120031025A3350 FUSE DOUG MD88 MD88 3023688NM BATTERY CHARGER BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27900DE 53372 EMERGENCY EXIT PATHWAY LIGHTS INOP AT ROWS 31 THRU 38. REPLACED 5 AMP FUSE ON BATTERY CHARGER, OPS CHECK NORMAL. 2L72 4F RTA6WE 20040129000632004012900063SO 2004 1 29 SWIA200312735 120031213A246051539014A GCU EMB 120 EMB120ER 3260203SO NR 2 MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM07579SW 120347 ON LANDING, SMOKE ODOR IN COCKPIT, EVIDENCE OF SMOKE FROM RIGHT DC RELAY BOX. WIRE FROM BUSS TIE 2 CONTACTOR TO RCCB BUS BAR AND BUSS TIE 2 CONTACTOR SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED NR 2 BUSS TIE CONTACTOR AND CABLE IAW WM 24-35-00. REPLACED WIRE TERMINALS AND GENERATOR 2 CONTACTOR K0012, APU FEEDER PROTECTION RELAY, APU START CONTACTOR AND BUSS BARS W1264 & W1261 DUE TO BURNING. REMOVED AND REPLACED MAIN GCU IAW 24-30-022. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20040212000602004021200060 2004 2 12 AK02003F00003 420030829A25624520133 BATTERY CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL ELT INOPERATIVE B AK0MK NONE O OTHER ININSP/MAINT 1 AL03378SP100 01224 U20606322 812400 812400 DURING AN ANNUAL INSPECTION OF THE ELT UNIT, THE ELT BATTERY PACK WAS INSPECTED FOR CORROSION IAW FAR 91.207 PARA (D). VOLTAGE WAS PRESENT AT THE POWER SUPPLY PLUG PRIOR TO DISCONNECTING. THE BATTERY POWER SUPPLY ELECTRICAL PLUG WAS DISCONNECTED AND INSPECTED OK, NO CORROSION. THE BATTERY POSITIVE TERMINAL WAS CHECKED WITH A VOLTMETER, VOLTAGE WAS NOT PRESENT AT THE CONNECTION PLUG POWER TERMINAL END. THE BATTERY PACK POWER AND GROUND ARE ROUTED THROUGH A CIRCUIT BOARD GLUED INSIDE OF THE HOUSING. ONE OF TWO FUSES SOLDERED ON THE BOARD TESTED (OPEN), CAUSE UNKNOWN. 1H71 3O3 O A4CE E5CE 5 CP47GL 20031031000082003103100008SO 2003 10 31 SWIA200312466 120030929A3350 FUSE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE BATTERY PACK BLOWN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07217SW 120286 EMERGENCY LIGHTS NOT WORKING CENTER SECTION. REPLACED BLOWN FUSE AT NR 1 ELBP, OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20031029000842003102900084NM 2003 10 29 ASAA0310501 120030602A53306545776 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 DURNG SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 747-749, STRINGER 19R CRACKED. REMOVED DAMAGED SECTION OF SKIN AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031112000342003111200034NM 2003 11 12 03FDEA01721 120031008A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 LT WING OB FLAP IB HINGE (FLAP SIDE) BRACKET- IB ACTUATOR LUG AND HOLE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031118000392003111800039EU 2003 11 18 AWXA200301154 120030924A5320D5311282600101 TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF Y503 DUMMY RAIL AT FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED AND REPLACED Y503 DUMMY RAIL AT FR 16 IAW A320 SRM 51-42-11 PG 23-28, FIG 9-12. 2L72 4F RTA28NM 20031119001172003111900117 2003 11 19 2003UALA00746 420031005A2210 AUTOPILOT SYS BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COCKPIT MALFUNCTIONED A UALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP29341UA 24245 WITH EITHER AUTO PILOTS ENGAGED AND ATTEMPTING TO ACCELERATE THE AIRCRAFT PITCHES UP. UPDATE DURING BITE CHECK OF THE AUTOPILOT BITE, FOUND FCC-B FAULTED, DADC2 FAULTED. DURING FULL TEST OF AUTOPILOT, OBSERVED FAULT WITH AFAU. REPLACED FCC-B, DADC, AND AFAU. ACCOMPLISHED THE AUTOPILOT CAT III CHECK WITH NO FAULTS FOUND. 2L72 4F4 FRTA16WE E2GL 20031031000572003103100057NM 2003 10 31 QXEA200301208 120030926A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 SEAT TRACK NR 10 HAS PITTING CORROSION AT STATION 366. REPAIRED IAW DHC-8 SRM 51-40-11, 51-40-00 AND RD 8-53-1339. 2H72 4T4 TRTA13NM E20NE 20031107001362003110700136SO 2003 11 7 SIMA200327903 120030930A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE 145582 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. REMOVED CORROSION BY CREATING A CUTOUT IN THE FLANGED AND WEB AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 22, 53-21-10 FIG 201 SHEET 2 AND CPM 51-21-06. (M) 2L72 4F RTT00011AT 20031107001032003110700103NM 2003 11 7 AALA20031058 120030916A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21359AA 24040 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040113001372004011300137NM 2004 1 13 03FDEA02258 120031226A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING, O/B FLAP O/B FWD HINGE SIDE SUPPORT MOUNT MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75217. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040113001502004011300150EU 2004 1 13 AWXA200301603 120031225A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW44484977 064 LAS - EEL - DURING 8-DAY CHECK LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) CAUSES CIDS FAULT. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031121000402003112100040EU 2003 11 21 0302013251 120031023A5315 FLOORBEAM AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01351NW 766 DURING M-CHECK FOUND CORROSION ON FLOORBEAM AT BS 1292 FRAME 66. REPAIRED PER EA 32-195731. 2L72 4F RTA28NM 20031126000012003112600001NM 2003 11 26 QXEA200301466 120031120A36201173T076207 SWITCH BOMBDRDHC8 DHC8401 1390041NM NACELLE FAILED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09406QX 4048 SEA- ON FLIGHT 2038 NR 2 BLEED HOT CAUTION LIGHT IN FLIGHT. FOLLOWED CHECKLIST. AFTER NR 2 BLEED TURNED OFF, LIGHT GOES OUT. REMOVED AND REPLACED BOTH NACELLE DUCT LEAK OVER TEMPERATURE SWITCHES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040115000322004011500032NE 2004 1 15 SW07200300005 220030606A72504120T01P02 TURBINE BLADES CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENGINE MISSING G FDKAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW07504MJ285 10066 E965355 THE MAINTENANCE PERSONNEL DISCOVERED 2ND STAGE HIGH PRESSURE TURBINE BLADES MISSING FROM THE TURBINE WHEEL. 2L72 4F4 FRTA21EA EOOO63EN 20031217001862003121700186EA 2003 12 17 SWIA200312605 120031116A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW 7578 STAB TRIM AND MACH TRIM FAILED DURING FLT. REPLACED CAPTAIN'S TRIM DISCONNECT SWITCH. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20031219000592003121900059WP 2003 12 19 UPS03841642 120031115A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, STATION 920 LONG 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-2 FIG 5. 2L74 4F RT4A25 20031219001552003121900155NM 2003 12 19 03FDEA02141 120031130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT, INBOARD HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73358, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - R/H OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20031224000072003122400007WP 2003 12 24 GTIA030817 120030928A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND FLOORBOARD STATION 598-636 DENTED/CRACKED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20040105001652004010500165CE 2004 1 5 AMWA98 120031216A532012943006023 DOUBLER BEECH 1900 1900D 1154162CE FUSELAGE DEBONDED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV UE133 DURING SCHEDULED ABCD STRUCTURAL INSPECTION, ONE RIGHT BONDED DOUBLER WAS FOUND TO BE DISBONDED. 2L72 4T RTA24CE 20031007000142003100700014NM 2003 10 7 AALA20030523 120030505A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21674AN 29424 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGTHS AT SEAT 1E INOPERATIVE. REPLACED EMEREGNCY EXIT SEAT LIGHT AT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20040108000912004010800091 2004 1 8 KBM2003F00041 420031004A34215040032902 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 GYROSCOPIC ATTITUDE INDICATOR IS INOPERABLE. INSTALLED OVERHAULED ATTITUDE GYRO. (K) 1G71 3U3 UNCH9EU E19EU 20040108001132004010800113EU 2004 1 8 KBM2003F00063 120031018A6230704A341301141 CONTROL CABLE SNIAS 350 AS350BA 8680817EU COLLECTIVE BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2490 2300 CONTROL CABLE, COLLECTIVE BINDING AT MID RANGE OF TRAVEL. REMOVED AND REPLACED WITH NEW PART, SAME NUMBER. 1G71 3U NCH9EU 20040109000282004010900028WP 2004 1 9 MEX2003490 120031015A5270 TARGET DOUG DC9 DC9* WP PWA JT8 JT8D* NE PAX DOOR OUT OF ADJUST W ASMFO OTHER N FALSE WARNING NRNOT REPORTED 1 SW23501AM 49188 AIRCRAFT RETURNED OF FLIGHT, FORWARD DOOR LIGHT COME ON. TECHNICAL PERSONNEL CHECKED DOOR BEING CLOSED. LIGHT INDICATION WAS DEFERRED IAW MM 52-7. DURING OVERNIGHT SERVICE, AND DOOR TARGET WAS ADJUSTED. OPERATIONAL TEST WAS PERFORMED IAW MM 33-30-00.(K) 2L72 4F4 F A6WE E2EA 20031204000422003120400042WP 2003 12 4 AALA20031087 120030929A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21266AA 49291 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE FIRST CLASS OVERHEAD. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031209001052003120900105 2003 12 9 SWAA032334 420031023A2565D31354 SLIDE BOEING737 7377H4 1384404NM L2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 L2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20031209001562003120900156NM 2003 12 9 QXEA200301374 120031028A5753 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX- LEFT HAND OUTBOARD FLAP UPPER INBOARD SURFACE AT WING STATION YW174.0 HAS CHAFE DAMAGE ON REPAIR DOUBLER. REPAIRED IAW DHC-8 SRM 51-00-05, 51-20-26 RD 8-57-2049 AND HORIZON AIR EA 2-57-133B. 2H72 4T RTA13NM 20031014000982003101400098NM 2003 10 14 SWAA032145 120030923A53406557463 BRACKET BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACHMENT BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20031211000232003121100023NM 2003 12 11 DHL200375110 120031028A33501000677 LIGHT BOEING727 727264 138408MNM COCKPIT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 DURING PREFLIGHT CHECK FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER 33-50-00 PG 501. OPS CHECK OK. 2L73 4F A3WE 20031211000852003121100085 2003 12 11 03FDEA01897 420031110A34142083121 INDICATOR BOEING727 727200 138407ENM COCKPIT FAILED A FDEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25205FE8560 8560 22927 F/O'S MACH AIRSPEED INDICATOR INOP, FLAG IN VIEW. REPLACED F/O MACH/AIRSPEED INDICATOR. OPS CHECKS NORMAL ON GROUND AT THIS STATION IAW MM 34-12-000-5. 2L73 4F RTA3WE 20031212000582003121200058NM 2003 12 12 AWXA200301418 120031021A71106555226327 CLIP BOEING737 737277 1384570NM NR 2 COWLING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 MCN - MINOR REPAIR - DURING C-21 CHECK A .25 INCH CRACK WAS FOUND ON L-ANGLE CLIP AT UPPER AFT END OF NR 2 ENGINE COWLING. MAINTENANCE REMOVED CRACKED L-ANGLE CLIP; FABRICATED A NEW REPLACEMENT CLIPPER DWG 65-552263-27; INSTALLED REPAIR PART IAW B737-22 SRM 51-30-02, PG 1, FIG 7, SECT 4. 2L72 4F RTA16WE 20031210001132003121000113NE 2003 12 10 ARWA20031105 220031130A7230 COMPRESSOR DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 ENGINE STALLED A ARWAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 SO19784AL499604456 46135 671244 ON FLIGHT 410, THE NR 4 ENGINE COMPRESSOR STALLED, FOLLOWED BY LOSS OF POWER. ACCOMPLISHED IN FLIGHT ENGINE SHUTDOWN AS PER FOM; ENGINE SHUTDOWN AT 14:35, THE WINDMILLING OIL PRESSURE WAS ZERO. 2L74 4F4 F 4A25 1E8 20030915000432003091500043 2003 9 15 BAQA088790 420030819A34250130004801 CDI UROCOPEC135 EC135T1 5620026EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME1957 0143 CDI INOPERATIVE. 1G72 3U H88EU 20030923001382003092300138WP 2003 9 23 0301611225 120030819A2420977J1504 GENERATOR DOUG DC10 DC1030 3023501WP NR 2 ENGINE FAILED A NWAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL01225NW21780338 46582 DURING CRUISE, NR 2 GENERATOR TRIPPED OFF AND THEN NR 1 CSD TEMPERATURE CLIMBED AND TRIPPED OFF. FLIGHT DUMPED 70,000 LBS OF FUEL AND RETURNED TO DTW. MAINTENANCE REPLACED THE NBR 1 GENERATOR AND SERVICED CSD AND REPLACED NR 2 GENERATOR CONTROL, GENERATOR, CSD CONTROLLER, AND CSD. OPERATIONAL CHECK OK. 2L73 4F A22WE 20030923000672003092300067WP 2003 9 23 DHL2003604721 120030528A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING CTR L/E UPPER PLATING HAS CORROSION AND INTERIM REPAIR FROM STA XFS 341.500 TO XW 257.000. REMOVED INTERIM REPAIR AND FASTENERS. REMOVED CORROSION ON LT WING CTR L/E UPPER PLATING, FOUND OUT OF LIMITS. TRIMMED OUT CORROSION SKIN AREA. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED REPAIR DOUBLER (7075-T6 AL0.071), TWO FILLERS (7075-T6 AL0.063). CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE AND FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLERS ON LT WING CTR L/E UPPER PLATING, XFS 341.500 - XW 257.000, WITH NEW FASTENERS IAW EODHL-030560, ED-3388, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040130000492004013000049NM 2004 1 30 VNAA0312012 120031220A4920 BLEED VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE APU FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07434JS 3051 DURING TAKEOFF, THE LEFT BLEED VALVE FAILED TO CLOSE WITH THE APU ON AND THE CREW ABORTED TAKEOFF. THE CREW THEN PERFORMED CHECK OF THE SYSTEM WITH THE APU BLEED OFF AND IT OPS CHECKED GOOD. MAINTENANCE THEN DEFERRED THE APU BLEED SYSTEM IN ACCORDANCE WITH 49-1-1C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030604001332003060400133NM 2003 6 4 UPS03440553 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D - BS 920 LT STRINGER 25L FRAME FOUND CRACKED. REF NRC 7348 FRAME REPAIRED AS PER SRM 53-10-04 FIG.24. 2L74 4F A20WE 20030604001702003060400170NM 2003 6 4 UPS03440590 120030413A575365B078762 RIB BOEING747 747121 1384871NM NR 19 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT WING - NR 19 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 6 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A. 2L74 4F A20WE 20030604000452003060400045SO 2003 6 4 SIMA200310607 120030415A21214611028900 FAN EMB 135 EMB135KL 3260302SO COCKPIT FAILED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21831AE 145616 DURING CRUISE FLIGHT, THE CREW REPORTED AN ELECTRICAL ODOR IN COCKPIT. AIRCRAFT WAS DIVERTED TO TOL AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE COCKPIT RECIRCULATION FAN IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030515001792003051500179NM 2003 5 15 AWXA200300522 120030510A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 13 LOOSE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28157AW 23779 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT IS LOOSE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030520000022003052000002SO 2003 5 20 CA030401002 120030331A32301754400 FITTING PIPER PA23 PA23250 7102308SO LYC O540 TIO540C1A 41532EA DRAG LINK CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THREE CRACKS WERE FOUND ON THE RIGHT MAIN LANDING GEAR OUTBOARD TUBE ASSEMBLY P/N 1742002 OF THE DRAG LINK FITTING SUPPORT. THE CRACKS ARE LOCATED AROUND THE LOWER MOUNTING BOLTHOLE OF THE TUBE ASSEMBLY.AFTER REMOVAL OF THE DRAG LINK SUPPORT ASSEMBLY, THE FORWARDSUPPORT FITTING WAS FOUND WITH TWO CRACKS ALONG THE EACH SIDE OF THE CASTING SEAM TO THE MOUNTING BOLT HOLE. 1L72 3O3 O 1A10 E14EA 20030521000452003052100045WP 2003 5 21 DHL2003804895 120030211A57305769857382 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING CTR L/E LWR PART SHOWS ELONGATED HOLES AROUND STA XS 521.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030114, ED-3215. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. BLENDED OUT DAMAGED AREA IAW EODHL-30114,ED-3215. FABRICATED DOUBLER (7075-T6AL-0.071) IAW EODHL-030114, ED-3215. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED DOUBLER AT RT WING CTR L/E LWR PART WITH NEW FASTENERS IAW EODHL-030114, ED-3215 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030521001652003052100165 2003 5 21 SWAA031085 420030514A2565D31354 SLIDE BOEING737 7377H4 1384404NM PAX DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29713SW 27847 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030522000432003052200043 2003 5 22 304AW0001 420030511A2230 COMPUTER BOEING737 7373G7 1384595NM AUTOTHROTTLE MALFUNCTIONED A PIDAK NONE O OTHER TOTAKEOFF 1 SO05304AW 24011 AUTO THROTTLE DISCONNECTED ON TAKEOFF ROLL. REMOVED AUTO THROTTLE COMPUTER AFTER TROUBLESHOOTING. REINSTALLED AUTO THROTTLE COMPUTER AND PERFORMED BITE TEST PER MM 22-10-04. OPS CHECKED NORMAL. 2L72 4F RTA16WE 20030612002042003061200204 2003 6 12 SWIA200312053 420030528A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING FAILED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07271YV 120271 LEFT STALL WARNING SYSTEM FAILED INFLIGHT WITH ASSOC WARNING ON MAP, AND RED LIGHT ILLUMINATED ON STALL SYSTEM PANEL. FOLLOWED QRH AND TURNED OFF LEFT STALL SYSTEM. REPLACED NUMBER 1 STALL WARNING COMPUTER. OPS CHECK GOOD. 2L72 4T RTA31SO 20030528000632003052800063EU 2003 5 28 BAQA086419 120030515A6420360A33107003 SPIDER AEROSPAS365 AS365N2 8680815EU TAIL ROTOR HEAD CRACKED E BAQAO OTHER O OTHER NRNOT REPORTED 1 FS012XJ 5608 6089 PITCH EAR IS CRACKED. COPY OF TAIL ROTOR HEAD COMPONENT CARD SHOWING INSTALLATION OF S/N:S38 REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030528000322003052800032NE 2003 5 28 ERAA086442 220030425A732032447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TORQUE SPLIT E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01167EH 33089 TORQUE SPLIT 20 PERCENT IN CRUISE FLIGHT SENT INTO MANUFACTURER FOR REPAIR. DISMANTLED AND COMPONENT EXAMINATION FOUND SERVO VALVE ORIFICES AND LEVER TO BE CONTAMINATED WITH OILY BROWN SOOT PAST. APPRECIABLE WEAR WAS EVIDENT ON THE SERVO VALVE LEVER AND ORIFICES. RECOMMENDED OVERHAUL BASED ON DEGREE OF REPAIRS REQUIRED TO RETURN SUBJCT TORQUE CONTROL TO A SERVICEABLE STATE. CUSTOMER WILL BE NOTIFIED OF THE INVESTIGATIVE FINDINGS ABOVE AND UPON ACCEPTANCE OF QUOTATION NECESSARY REPAIRS WILL BE PERFORMED 1G72 4U4 U H4SW E22EA 20030619000092003061900009NE 2003 6 19 AC2A086766 120030529A2821173547502 FILTER HOUSING SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL SPRING CLIP RETABROKEN E AC2AK NONE O OTHER ININSP/MAINT 1 SO077266F 760273 DURING SCHEDULED FILTER REPLACEMENT THE SPRING CLIP RETAINER WAS FOUND BROKEN AND FELL OUT OF THE HOUSING IN PIECES WHEN THE FILTER WAS REMOVED. FILTER HOUSING WAS REPLACED. 1G72 3U3 U H1NE E1GL 20030630000352003063000035EU 2003 6 30 AWXA200300611 120030502A5311D53370239200 FRAME AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING C-04 CHECK AFTER FIRST OVERSIZE OF FASTENER HOLE COMMON TO SKIN 2 EACH 1/8 INCH CRACKS WERE FOUND ON FRAME 39, THIRD FASTENER HOLE BELOW STR 14 L/H. MAINTENANCE REAMED OUT HOLE TO SECOND OVERSIZE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; CUTOUT DAMAGED SECTION OF FRAME 39 AT THIRD FASTENER HOLE BELOW STR 14 L/H; FABRICATED A REPAIR ANGLE AND FRAME FILLER; INSTALLED REPAIR PARTS IAW E.O. 53-14-20. 2L72 4F RTA28NM 20030702000072003070200007NM 2003 7 2 GAIA03017OP 120030610A2170 COALESCER BAG BOEING727 727251 138408HNM CABIN CONTAMINATED A GAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07252US 19971 DURING CLIMB-OUT, CREW NOTICED A STRONG, SMOKEY SOLVENT ODOR COMING FROM AIR VENTS. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED BOTH WATER SEPARATOR SOCKS. INSPECTED ENTIRE AIRCRAFT, RAN ENGINES, AND PRESSURIZED AIRCRAFT TO 5 PSI DIFFERENTIAL PRESSURE. NO DEFECTS NOTED. OPERAITONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030709001052003070900105CE 2003 7 9 GLBA2003071 120030530A2750 SWITCH BEECH 1900 1900 1154160CE TE FLAPS OUT OF ADJUST A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03118UE 118UE AIRCRAFT RETURNS, FLAPS WILL NOT RETRACT. ADJUSTED FLAP SAFETY SWITCH, OPS CK GOOD. 2L72 4T RTA24CE 20040308001312004030800131NM 2004 3 8 ASAA0310249 120030327A7110 WEB BOEING737 737298C 1384490NM NR 1 COWLING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL WEB AND FRAME AT NACELLE STATION 99.25 CHAFED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M) 2L72 4F RTA16WE 20040802000212004080200021SO 2004 8 2 2004F00222 120031220A53474046711144 SEAT TRACK GULSTMGV GULFSTREAMGV3980116SO FUSELAGE CORRODED A UG8AK NONE O OTHER ININSP/MAINT 1 GL23661GA 561 FOUND THE LEFT CABIN SEAT TRACK HAD SUSTAINED CORROSION DUE TO WATER INTRUSION FROM THE LEFT NR 6 EMERGENCY CABIN WINDOW. THE CAUSE OF THIS DEFECT WAS DUE TO WATER INTRUSION. MAY WANT TO INCREASE THE INSPECTION FREQUENCY IN THIS AREA. THE SEAT TRACK WILL BE REPLACED DURING SCHEDULED MAINTENANCE IN FEB 2004. (M) 2L72 4F RTA12EA 20050202000572005020200057NM 2005 2 2 0704011 120031009A524565486854 SKIN BOEING737 737230C 1384472NM E/E BAY DOOR DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW70152 20257 RT AC BAY DOOR DELAMINATED FROM BS 556 TO BS 596. 2L72 4F A16WE 20060313001092006031300109SO 2006 3 13 LR7A03101 120031121A5100 REPAIR LKHEED382 382G 526414USO NONE A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2356 4763 DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 NOTED LT AILERON UPPER SURFACE NON-FLUSH REPAIR AT AS 40-55. REPLACED AILERON UPPER SURFACE SKIN IAW SRM SMP 583 51-60 & 51-70. 2H74 4T A1SO 20030820000132003082000013NM 2003 8 20 03FDEA00949 120030621A5610 WINDSHIELD DOUG MD11 MD11 3023602NM COCKPIT DAMAGED A FDEAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO25593FE 48551 AT FL 330 .84 MACH, OBJECT HIT WINDSCREEN IN 2 PLACES AND FRACTURED R1 FROM BOTTOM UPWARDS. CONT TO FRACTURE SPREAD ACROSS WINDSHIELD. SPIDER WEB AT LOWER PORTION OF R1 THROUGH TO UPPER PORTION. FACT R/R R1 WINDSHIELD ASSY PER MD-11M/M 56-11-01-4. AFTER R1 FRACTURE RECEIVED MULTIPLE LEVEL 2 ALERTS. ATS DROPPED OFF. FLT DIR BIASED OUT OF VIEW, FLEW A/C MAN. CAP'T AND F/O SPEED DIFFERED BY 30 KNTS+. ALL ALERTS WENT AWAY AND CAME BACK AFTER 30-60 SEC. A/P AND ATS AVAIL DURING INTERIM WHEN ALERTS NOT ILLUM. FACT SUSP ICE INGESTION INTO PITOT SYSTEM. PURGED SAME, NO FOREIGN MATERIAL NOTED. REF MM 34-11-00-2. REMOVED AND REPLACED NR 1 & 2 CADC'S PRECAUTIONARY. REF MM 34-16-01-4. OK FOR SERVICE. 2L73 4F RTA22WE 20030820001022003082000102NM 2003 8 20 UPS03241049 120030711A5311 FRAME BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, FRAME CRACKED AT BS 1070 AND ATTACH POINT FOR AFT LWR CARGO DOOR. CRACKED FRAME AT BS 1070 REMOVED AND NEW FRAME INSTALLED IAW DRAWING NR65-18622. 2L73 4F A3WE 20030328000012003032800001CE 2003 3 28 CA030212004 120030212A2910124K0016CL0150 HOSE CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE BRAKE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN) WHEEL WELL FOUND SOAKED WITH HYDRAULIC FLUID , AFTER LAST FLIGHT OF THE DAY. FOUND BRAKE FLUID RESEVOIR DEPLETED. TOPPED OFF BRAKE FLUID RESEVOIR BUT WAS UNABLE TO DETECT LEAK UNTIL THE A/C WAS ON JACKS. WE HAVE HAD 2 PRIOR OCCURRENCES AND DETERMINED THAT WITH THE GEAR EXTENDED THE FLEX LINE IS TAUT. THIS IS REQUIRED IN ORDER TO CLEAR THE WHEEL WELL ON RETRACTION. THERE IS QUITE A LOAD JUST BEHIND THE LOWER FITTING. 1L72 4F4 F A22CE E1NE 20030401000932003040100093NM 2003 4 1 DHL2003748003 120030304A3350 LIGHT BOEING727 727225 1384077NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01748DH 22440 FORWARD ENTRY EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING STANDBY POWER CHECK. CLEANED AND RE-SECURED EMERGENCY EXIT LIGHT ASSEMBLY IAW B727 M/M 33-50-71. OPS CHECKED SERVICEABLE IAW B727 M/M 33-50-91. 2L73 4F A3WE 20030403000442003040300044NM 2003 4 3 AMTA200300285 120030227A28226075504 PUMP BOEING757 75728A 1384976NM FUEL BOOST INOPERATIVE A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11521AT 24368 RIGHT AFT FUEL BOOST PUMP C/B POPPED. PERFORMED INSULATION RESISTANCE AND BONDING CHECKS PER MM 28-22-03. OPS CHECKED OK. REFERENCE LP 543952 FOR RIGHT AFT BOOST PUMP REMOVED AND REPLACED. (M) 2L72 4F RTA2NM 20030821001352003082100135NM 2003 8 21 03FDEA00874 120030614A5610NBA6045501 WINDSHIELD DOUG MD11 MD11 3023602NM COCKPIT CRACKED A FDEAA UNSCHED LANDING O OTHER CRCRUISE 1 SO25595FE 48553 CAPT'S WINDSHIELD CRACKED. 15JUN03 09:03 SIN R, CAPT'S WINDSHIELD REMOVED AND REPLACED AS PER AMM 56-11-01. WINDSHIELD ANTI-ICE SYSTEM OPERATION TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 30-41-00. WINDSHIELD DEFOG SYSTEM OPERATION TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 30-42-00. R/I 15JUN03 09:04 SIN R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. 2L73 4F RTA22WE 20030404000282003040400028NM 2003 4 4 DL738030280 120030326A2750 WARNING LIGHT BOEING737 737832 13844CFNM FLAPS ILLUMINATED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27380DA 30266 AT CRUISE - FL 390 - YAW DAMPER DISENGAGED AND WAS RESET. LEADING EDGE IN TRANSIT LIGHTS WERE OBSERVED ON OVERHEAD. FOLLOWED BY L/E LIGHTS ON FWD PANEL WITH T/E. FLAPS INDICATING 1/2 DEG. DESCENT INITIATED AND FLAPS RETRACTED FULLY ON THEIR OWN. CHECKED SYSTEM PER FIM AND TESTED FSEU WITH NO VCM MSGS. ALL FLAP AND PROX SWITCHES TEST NORMALLY. ENTIRE SYSTEM TESTS PER FIM 27-81/806. FDAU SHOWS FLAP HANDLE INPUT TO THE NR 1 DETENT. PERFORMED PHASE 1 OVERSPEED INSPECTION PER M/M 05-51-08-2. 2L72 4F RTA16WE 20030408000052003040800005WP 2003 4 8 ASAA0380079 120030113A5347 CARGO TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY LEFT TRACK IS CORRODED AT FS 1079-1222. REPLACED TRACK PER SRM 53-05. (M) 2L72 4F RTA6WE 20030414000572003041400057SW 2003 4 14 HEEA085853 120030326A2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 SIGNAL COND UNIT MALFUNCTIONED. FUEL LOW LIGHT WILL NOT GO OUT. 1G72 4U H4SW 20030416002802003041600280WP 2003 4 16 AALA20030280 120030305A32225963254501 STRUT DOUG DC9 DC982 3022082WP NLG DEFECTIVE A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21290AA 49302 MIA - FLT 1578 - EN ROUTE MIA-ATL, ON TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT PROPERLY. SEVERAL LOUD THUMPS HEAD AT HIGH SPEED ON TAKEOFF ROLL. RETURNED MIA WITHOUT INCIDENT. INSTALLED SERVICEABLE NOSE GEAR STRUT. ACCOMPLISHED NOSE GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030417000342003041700034EU 2003 4 17 MALA030127 120030121A801050113775008 STARTER BAC 146 AVRO146RJ85A1500097EU NR 4 ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15510XJ E2323 DURING FLIGHT 3656 A/C DID AN AIR RETURN DUE TO STARTER OPERATING LIGHT COMING ON DURING CLIMBOUT, INTERMITTANT DURING APPROACH OUT AT SHUTDOWN UNABLE TO PERFORM QRH AT SHUTDOWN. MAINTENANCE REPLACED NR 4 STARTER MOTOR, OPS CHECK GOOD PER AMM 80-10-11. P/N 501-13775-008, SN/OFF TE2520, SN/ON TE2169. 2H74 4F RTA49EU 20030417000372003041700037WP 2003 4 17 IXXA0300007O 120030126A27603644322509 BELLCRANK DOUG DC8 DC871F 302199DWP SPOILERS CRACKED A IXXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW11823BX848521319 46064 AFTER TAKEOFF SPOILER EXTENDED LIGHT ILLUM. ACFT EXHIBITED INAPROPRIATE FLT CHARACTERISTICS. RETURNED FOR UNEVENTFUL LANDING. MX NOTED SPOILER HYD RESERVOIR LOW. MX SERVICED SPOILER RESERVOIR, INSPECTED SPOILER PANELS, CABLES, ACTUATORS AND ALL NORMAL. RETURNED TO SERVICE. UPON SUBSEQUENT TAKEOFF CLIMB SPOILER EXTEND LIGHT AGAIN ILLUMINATED. ACFT EXHIBITED INAPROPRIATE FLT CHARACTERISTICS. ABORTED CLIMB, RETURNED FOR UNEVENTFUL LANDING. MX INSPECTION REVEALED BROKEN INBD & OUTBOARD SPOILER CRANK ASSY ON INBD LT WING GROUND SPOILER. BOTH CRANK ARMS REPLACED, REPLACEMENT OF SPOILER TAKEOFF WARNING SWITCH ALL MX INCLUDING A OVERWEIGHT LANDING INSPECTION PERFORMED PER APPLICABLE ACFT MM. 2L74 4F RT4A25 20030709001322003070900132WP 2003 7 9 MWEA030245 120030612A215039271012 VALVE DOUG DC9 DC982 3022082WP AIR CONDITIONINGINOPERATIVE A MWEAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL31810ME 48072 AFTER PUSH BACK RIGHT PACK WAS NOT PUTTING OUT AIR FLOW AND INDICATOR WAS AT ZERO PSI. REMOVED AND REPLACED AUGMENTATION VALVE. 2L72 4F A6WE 20030711000842003071100084EA 2003 7 11 COMA0360291 120030624A27604916405 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO01933CA5449 7040 FLIGHT 5797 SPOILER AND FLIGHT SPOILER CAUTION MESSAGE. REPLACED THE NR 2 SECU. 2L72 4F RTA21EA 20030717000022003071700002SW 2003 7 17 HEEA087979 120030625A6220206011117003 RESTRAINT BELL 206 206L3 1182108SW FLAP WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341791 51465 MAIN ROTOR HEAD FLAP RESTRAINT IS WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030108000152003010800015WP 2003 1 8 MWEA030008 120030107A53209912246121 WEB DOUG DC9 DC981 3022081WP STA 1389 TOOL DAMAGE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 REMOVED FRAME WEB AT FRAME STATION 1389 FROM LONGERON 30-24 LEFT TO FACILITATE OTHER MAINTENANCE. -- REMOVED WEB, FOUND SECTION HAS DOUBLE DRILL HOLES. -- FABRICATED AND INSTALLED NEW WEB. 2L72 4F A6WE 20030114002542003011400254EA 2003 1 14 COMA0360022 120030111A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER S AFFECT SYSTEMS DEDESCENT 1 SO01918CA13937 7018 FLIGHT 5621 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.REPLACED THE PDU 2L72 4F RTA21EA 20030114002612003011400261NM 2003 1 14 QXEA0300044 120030112A5270 SWITCH BOMBDRDHC8 DHC8401 1390041NM ZONE 800 FROZEN A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 YYC - FLIGHT 2333 - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF THE FORWARD BAGGAGE DOOR WARNING LIGHT ILLUMINATED AND THE AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT CARGO DOOR PROXIMITY SWITCH FROZEN. THE SWITCH WAS THAWED AND OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20030127001462003012700146SW 2003 1 27 HEEA083683 120030115A3212206050247137 COVER BELL 407 407 1182206SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 EMERGENCY FLOAT COVER WORN. 1G71 3U O H2SW 20030127002602003012700260SW 2003 1 27 HEEA083735 120030115A2821222366621103 FILTER BELL 407 407 1182206SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03501PH 53401 INTERMITTENT FUEL FILTER LIGHT. 1G71 3U O H2SW 20030128002602003012800260NM 2003 1 28 DHL2003751002 120030125A331069174388 CONTROL MODULE BOEING727 727264 138408MNM COCKPIT FAULTY A DHLAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01751DH 22982 AFTER CLOSING MAIN CARGO DOOR, A STRONG ODOR BECOMES PRESENT IN COCKPIT. ODOR LESSENS WITH ENGINE BLEEDS TO PACKS. ODOR PRESENT WITH L OR R AND BOTH PACKS. FOUND ODOR COMING FROM F/E LT CONTROL PANEL - REMOVED AND REPLACED F/E LT CONTROL MODULE ASSEMBLY AND OPS CHECKED NORMAL IAW B727 M/M 33-10-00. 2L73 4F A3WE 20030130001582003013000158NM 2003 1 30 F3LA200300007 120030117A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED TOP SURFACE OF I-BEAM AT STA 967 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-51, FIG 101. REMOVED DAMAGE PER SRM 53-00-51, FIG 203. FABRICATED AND INSTALLED REPAIR STRAPS FOR FLOORBEAM AT STA 967, LBL 17.5 TO RBL 5, PER SRM 53-00-51, FIG 203, AND SOPM 2041-02. 2L72 4F RTA16WE 20030131001482003013100148EA 2003 1 31 HNAA0300006 120030129A335040005130003 SWITCH DHAV DHC8 DHC8311 1386006EA INOPERATIVE A HNAAK NONE N FALSE WARNING CRCRUISE 1 EA07342EN17097 395 EMERGENCY FLOOR LIGHTS BLINKED DURING ENTIRE FLIGHT. REPLACED NORM\ON SWITCH ON FLIGHT ATTENDANT CONTROL PANEL. 2H72 4T RTA13NM 20030204002712003020400271NM 2003 2 4 VNAA0301019 120030118A3250 CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NLG STEERING FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE NOSE WHEEL STEERING CONTROL MANIFOLD CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030214000122003021400012WP 2003 2 14 2003F00097 120030109A25602463 PANEL LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE EVAC WARNING INOPERATIVE G K NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EVAC WARNING PANEL AT L1 DOOR HAS NO TONE DURING TEST. REMOVED AND REPLACED EVAC WARNING PANEL AT L1 DOOR. 2L73 4F4 F A23WE A12EU 20030218001782003021800178NM 2003 2 18 QXEA0300170 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 4 SEAT TRACK HAS SCRATCHES AT STATION 410-420. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030218002532003021800253NM 2003 2 18 SWAA030253 120030201A27506573271 TORQUE TUBE BOEING737 7373H4 1384600NM LT WING BROKEN A SWAAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW29330SW 23694 T/E FLAPS INDICATED 5 DEGREE SPLIT ON APPROACH AND WOULD NOT RETRACT AFTER LANDING. FOUND LEFT FLAPS INBD TORQUE TUBE BROKEN, REMOVED AND REPLACED LEFT INBD TORQUE TUBE PER MM. 2L72 4F RTA16WE 20030221000842003022100084NM 2003 2 21 AWXA200300179 120030128A5320146N5417 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT BS 1461 - 1471, ABOVE STR 28R. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SUPPORT ANGLES BS 1461 - 1471; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-12, PG. 1-17, FIG. 1 & 2, AND SRM 51-40-02, PG. 1-3. 2L72 4F RTA2NM 20030221000932003022100093SW 2003 2 21 AC2A084146 120030209A3213430036140105 CROSSTUBE BELL 430 430 1182150SW MLG CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH275 49037 CROSSTUBE IS CORRODED. CROSSTUBE WAS REPLACED 1G72 3U RTH9SW 20030225000462003022500046SW 2003 2 25 HEEA084265 120030129A6710214001970111 ACTUATOR BELL 214 214ST 1182106SW FLT CONTROL WILL NOT TEST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 ACTUATOR WILL NOT TEST PROPERLY, TRIPS OFF ON TAKE OFF. 2G72 4U H10SW 20030303000372003030300037SW 2003 3 3 HEEA084499 120030214A6220412310400101 ROD END BEARING BELL 412 412 1182202SW MAIN ROTOR HEAD WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20030306000422003030600042SW 2003 3 6 HEEA084755 120030218A3210407030112105 FITTING BELL 407 407 1182206SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 RT AFT CROSSTUBE FITTING DAMAGED WHEN CROSSTUBE SHIFTED. REPLACED FITTING. 1G71 3U O H2SW 20030306000662003030600066SW 2003 3 6 HEEA084777 120030221A7810212061202009 DUCT BELL 412 412 1182202SW EXHAUST SYSTEM CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 CRACK IN WELD OF EXHAUST DUCT AT AFT LT CORNER. REPAIRED. 1G72 4U H4SW 20030306000902003030600090SW 2003 3 6 HEEA084799 120030221A243523046020 STARTER GEN BELL 412 412 1182202SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 STARTER GENERATOR WILL NOT COME ON LINE. 1G72 4U H4SW 20030117001432003011700143SW 2003 1 17 HEEA083212 120030108A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW DROOP COMPT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ACTUATOR MOTOR WILL NOT MOVE ARM IN EITHER DIRECTION. 1G71 3U H2SW 20030121002002003012100200SW 2003 1 21 HEEA083344 120030109A243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03205FC 51130 MAIN BATTERY WEAK. REPLACED BATTERY. 1G71 3U H2SW 20030318001162003031800116NM 2003 3 18 BJNA03023 120030203A5330 SKIN BOEING737 737282 13844ATNM FUSELAGE CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 DURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN FUSELAGE SKIN OF THE FORWRAD ENTRY DOOR LOWER HINGE CUTOUT. CRACK EXTENDS FROM THE RADIUS OF THE HINGE CUTOUT FORWARD 1.9 INCHES, TERMINATING AT A FASTENER HOLE. CRACK IS SIMILAR TO THOSE SHOWN IN 737 SRM 53-30-3 FIGURE 31, HOWEVER THE CRACK EXTENDS PAST THE MAXIMUM 1.7 INCH CUTOUT SHOWN IN THE SRM REPAIR. ENGINEERING DESIGNED AND OBTAINED APPROVAL FOR PERMANENT REPAIR. CRACKED SKIN WAS REMOVED, FABRICATED REPAIR DOUBLER AND FILLER PER REPAIR ENGINEERING ORDER REQ-L00625 REVISION A, DATED 01/28/2003. AS REQUIRED BY FINAL REPAIR ENGINEERING ORDER, REPAIR IS TO BE REINSPECTED AT 60,000 CYCLES, AND THEN REPEATED AT 4,000 CYCLE INTERVALS. (M) 2L72 4F RTA16WE 20030320000462003032000046NM 2003 3 20 USAASB03014 120030125A2120 ODOR BOEING737 737301 1384611NM COCKPIT DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19340US 23237 ATL - FLT 704 - DURING CRUISE, EN ROUTE FROM CLT TO ATL, CREW REPORTED A STRONG ODOR OF JET FUEL IN THE COCKPIT AT TWO DIFFERENT TIMES. ODOR APPEARED TO BE COMING THROUGH THE LT PACK. FLIGHT ATTENDANTS AND PASSENGERS DID NOT NOTICE ODOR. FLIGHT LANDED AT ATL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED EXTERIOR OF AIRCRAFT AND OPENED BOTH ENGINE COWLS FOR EVIDENCE OF FUEL/OIL LEAKS. NO LEAKS NOTED. RAN BOTH ENGINES AND PACKS AND PRESSURIZED AIRCRAFT. COULD NOT DUPLICATE ODOR. ALL SYSTEMS CHECK NORMAL. (M) 2L72 4F RTA16WE 20030320000992003032000099NM 2003 3 20 2003UALA00090 120030121A3350 CHARGER BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 EXTERNAL EEL LIGHT RT SIDE, BOTH AFT ASSY, INOP. REPLACED BATTERY CHARGER. 2L74 4F4 FRTA20WE E24NE 20030325000762003032500076NM 2003 3 25 AWXA200300242 120030217A57526546455527 TAB BOEING737 7373S3 1384711NM LT AILERON WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW14782 24060 DURING C-11 CHECK THE LT AILERON BALANCE TAB INBOARD AND OUTBOARD HINGES WERE FOUND TO HAVE EXCESSIVE PLAY. MAINTENANCE REMOVED AND REPLACED THE LT AILERON BALANCE TAB IAW T/C R3M27014, AND REPLACED THE INBOARD AND OUTBOARD L/H AILERON BALANCE TAB HINGES IAW OHM 57-50-25, PG. 702-703. 2L72 4F RTA16WE 20030320001732003032000173NM 2003 3 20 SWAA030620 120030318A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED D CHECK, FOUND BOTH LH & RH FUSELAGE FRAMES CRACKED AT BS 188, WL 208. R&R LH & RH FRAMES PER SRM. 2L72 4F RTA16WE 20030321000342003032100034NE 2003 3 21 2003UALA00190 220030218A7322 FMU AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 ENGINE INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29814UA 862 V10399 DURING CLIMBOUT NR 2 ENGINE SHUTDOWN DUE TO FMU ECAM WARNING. FUEL METERING UNIT (FMU) REPLACED, 2L72 4F4 FRTA28NM E40NE 20030303000902003030300090SW 2003 3 3 HEEA084521 120030214A243230126002 BATTERY BELL 412 412 1182202SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 MAIN BATTERY WEAK. REPAIRED. 1G72 4U H4SW 20030321001112003032100111NM 2003 3 21 2003UALA00257 120030308A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BURNED OUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 DOOR 1R EMERGENCY SLIDE LIGHT ON OUTSIDE OF FUSELAGE IS INOP. REPLACED/RELAMPED BURNED OUT LIGHT. 2L72 4F4 FRTA2NM E17NE 20030324000722003032400072CE 2003 3 24 AMWA10 120030211A5411 SPAR CAP BEECH 1900 1900D 1154162CE NACELLE CHAFED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07142ZV UE142 UPON A DETAILED INSPECTION MAINTENANCE FOUND THAT THE LEFT AND RIGHT LOWER SPAR CAP BEHIND NACELLE INNER WAS CHAFED. BLENDED BOTH OF THE LOWER SPAR CAPS IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JMP/0209-03. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030418000422003041800042WP 2003 4 18 MWEA030070 120030217A53205910130338 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE MISSING A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 AFT PRESSURE BULKHEAD RIGHT UPPER CORNER OF SPLICE DOUBLER BETWEEN LONGERON 4 RIGHT AND LONGERON 6 RIGHT HAS A MISSING END ON THE OUTBOARD SIDE. REMOVED SPLICE DOUBLER, FABRICATED AND INSTALLED NEW SPLICE DOUBLER. 2L72 4F A6WE 20030421002152003042100215CE 2003 4 21 2003F00230 120030310A2740H517A TRANSMITTER CESSNA750 750 2076810CE VERTICAL STAB INOPERATIVE A UG8AO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL235113 7500013 UPPER RUDDER A-B FAILED TWICE. ABLE TO RESET TO B-CHANNEL. REPLACED UPPER RUDDER POSITION TRANSMITTERS. RIGGED AND TESTED PER CESSNA MM. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20030723000012003072300001WP 2003 7 23 GTIA030491 120030619A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FOUND MID PIT FS 630 STRINGER 28R INTERCOSTAL CORRODED. FABRICATED NEW T-ANGLE. (M) 2L72 4F A6WE 20030723000712003072300071NM 2003 7 23 SWAA031468 120030703A3350079123 LIGHT BOEING737 7373H4 1384600NM CABIN FLOOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK WORN AT ROW 9. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM. 2L72 4F RTA16WE 20030723000952003072300095EU 2003 7 23 AWXA200300770 120030701A2560P20700012015 FLASHLIGHT AIRBUS320 A320232 3930326EU LAVATOR INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28665AW 1644 PHL - EMERGENCY EQUIPMENT - THE AFT CENTER EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED ON MEL 25-60-08, COND 1 FLASHLIGHT INOPERATIVE. WHEN AIRCRAFT ARRIVED IN PHX MAINTENANCE REMOVED AND REPLACED THE AFT CENTER EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030424000172003042400017NM 2003 4 24 UPS03240323 120030306A5711 SPAR BOEING727 72725C 138400HNM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 INSPECTION TYPE: C, LT WING REAR SPAR HAS ONE CRACK AND 2 CORROSION INDICATIONS AT WS 193 TO 196. REPAIR CARRIED OUT IAW SRM 51-20-04. 2L73 4F A3WE 20040223001762004022300176WP 2004 2 23 ABXA040011 120031203A5210 SKIN DOUG DC8 DC861 3021952WP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 L1 FORWARD PAX DOOR, LOWER AFT CORNER HAD A CRACK IN EXTERNAL SKIN. REMOVED DAMAGED AREA, REPAIRED SKIN / DOUBLER TRIM OUT IAW SRM 53-2-0 AND REA D853-48470MR. 2L74 4F 4A25 20030826000592003082600059 2003 8 26 5300051203 420030512A34207012100825 DISPLAY CESSNA560 560XL 2076702CE COCKPIT FAULTY E S4WAK NONE O OTHER CRCRUISE 1 WP07613GY336 5605300 NR 2 RMU DISPLAY IS UNREADABLE. 2L72 4F RTA22CE 20030827001252003082700125NM 2003 8 27 CALA0300411 120030724A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717316 23367 INSPECTION FOUND A .2500 INCH CRACK IN INTERCOSTAL AT STA 328, LBL 36. THE INTERCOSTAL WAS REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20030828000712003082800071NM 2003 8 28 DLM88030641 120030714A2421 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE LT ENGINE FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO27932DL 49719 AFTER TAKE OFF LT GENERATOR FAILED. STARTED APU AND PUT THE APU GENERATOR ON LINE. APU GENERATOR KICKED OFF LINE WITH AN AC CROSSTIE LOCKOUT. DIVERTED REPLACED LT GENERATOR AND GCU. 2L72 4F4 FRTA6WE E2EA 20030728000072003072800007NM 2003 7 28 SWAA031524 120030711A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4L, BS 620 AND BS 680. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030805000052003080500005EA 2003 8 5 WVE2003F00009 120030430A783022850232101 ARM CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER BROKEN B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09570ML 7206 DURING ROUTINE LINE MAINTENANCE, IT WAS DISCOVERED THAT THE RT THRUST REVERSER NR 1 BLOCKER DOOR HINGE ARM HAD BROKEN RESULTING IN DAMAGE TO THE SURROUNDING STRUCTURE. IT IS ASSUMED THE DAMAGE OCCURRED DURING THE LAST THRUST REVERSER DEPLOYMENT. 2L72 4F RTA21EA 20030417001332003041700133WP 2003 4 17 UPS03840148 120030130A53205750540501N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, CRACKED FITTING BETWEEN STA 660 AND 680 AT LONGERON 11R IN MAIN CABIN. REMOVED AND REPLACED FITTING IAW DWG 5750540, AND SRM 51-1-20D. 2L74 4F RT4A25 20030424000672003042400067NM 2003 4 24 IU62003F00002 120030221A2761654494710 HOUSING BOEING BOEING737 737* NM ACTUATOR BROKEN B IU6RO OTHER O OTHER NRNOT REPORTED 1 NM01 4834 HOURING IS BROKEN OFF AT BEARING LUG. NORMAL CYCLING AND LOADS ON UNIT, TOTAL TIME AND MATERIAL OF HOUSING ARE A FACTOR. (CB4, JOB NR 174743) 2L72 4F RTA16WE 20030424001282003042400128WP 2003 4 24 UPS03840351 120030312A571037048412 FITTING DOUG DC8 DC873F 302199FWP LEFT WING TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C2, NR 2 MAIN FUEL TANK HAS STRINGER END FITTING CRACKED AT OUTBOARD SIDE OF XRS 50 AT STRINGER 51. REMOVED, FABRICATED AND INSTALLED FITTING IAW DWG 3704841 AND SRM 51-1-20D. 2L74 4F RT4A25 20030425000642003042500064CE 2003 4 25 ZSE2003F00001 120030319A526050430043619 CHANNEL BEECH 200 200BEECH 1152920CE PWA PT6 PT6A60A 52043NE AIRSTAIR DOOR CRACKED D ZSEAO OTHER O OTHER NRNOT REPORTED 1 CE01498AC BB287 CHANNEL CRACKED AT AFT. 4 RIVET HOLES FOR THE DOOR HINGE HALF. 1L72 4T4 T A24CE E4EA 20030428001322003042800132WP 2003 4 28 ZW0A0303907 120030402A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13925TW 49357 THE FUSELAGE SKIN WAS DAMAGED AT STA 596 TO 605, LONGERON 26R AREA. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3. CHECK-C 8-15-02 STL. 2L72 4F A6WE 20030429000992003042900099CE 2003 4 29 FPI2003F00008 120030326A57110024300187 SPAR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO151844712810 TH883 AT ANNUAL INSPECTION, CRACKS WERE FOUND IN FORWARD AND AFT CARRY THRU SPAR WEB FACES. THE CRACKS WERE FOUND ABOVE THE INSTALLED WEB REPAIR KITS AT THE UPPER SPAR FITTINGS. THESE NEW CRACKS APPEAR TO HAVE BEEN CAUSED BY THE INSTALLATION OF THE WEB REPAIR KITS TRANSFERING STRESS TO THE UPPER CORNERS OF THE WEBS. (AD-90-08-14) 1L72 3O3 O 3A16 E5CE 20030429001042003042900104SO 2003 4 29 C2XA03SH101 120030413A531014522226003 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV - DURING C-CHECK, THE LEFT HAND BUTT STRAP BETWEEN FRAMES 60 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030425001022003042500102WP 2003 4 25 MWEA030155 120030331A2923414472 PUMP DOUG DC9 DC981 3022081WP HYD SYS DEFECTIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31807ME 48033 ON PUSH BACK AUXILIARY HYDRAULIC PUMP CIRCUIT BREAKER POPPED. REMOVED AND REPLACED AUXILIARY HYDRAULIC PUMP. 2L72 4F A6WE 20030501001142003050100114WP 2003 5 1 ASAA0380123 120030209A5320S000925 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OAK - DURING C-CHECK, FOUND MID CARGO BAY LEFT FLOOR SUPPORT CRACKED AT TRACK ATTACH RIVET. REPLACED FLOOR SUPPORT AT FS 560 PER SRM 51-10-4 AND 30-2. (M) 2L72 4F RTA6WE 20030502000182003050200018SO 2003 5 2 SIMA200309019 120030314A531014522460013 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21707EB 145195 ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION CENTER BEAM GUSSET CORRODED IN GALLEY. INSTALLED NEW GALLEY CENTER BEAM GUSSET IAW EMB 135 51-20-03, 51-20-01, 51-40-02, 51-40-04 AND 51-40-06. (M) 2L72 4F RTT00011AT 20030501000652003050100065WP 2003 5 1 GTIA030195 120030218A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FTW - FOUND CABIN FLOORBOARD STATION 864-875 DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030506000452003050600045EU 2003 5 6 MALA030239 120030416A3350 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15428XJ 340B428 DURING FLIGHT 428, 2 FLOOR TRACK LIGHTS INOP. MAINTENANCE REPLACED LIGHT STRIP, OPS CHECK GOOD. 2L72 4T RTA52EU 20030506000522003050600052WP 2003 5 6 UPS03840456 120030331A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, AFT FUSE L17LT AND END FITTING CRACKED AT FS 1770. REMOVED LONG 17LT & END FITTING. LOCATED AND DRILLING NEW END FITTING IAW DC8 SRM 51-1-24. INSTALLED LONGERON & END FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030513000172003051300017EU 2003 5 13 AALA20030318 120030317A3350502A LIGHT FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211423A 11406 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT IN LEFT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPS. (M) 2L72 4F RT 20030513001392003051300139NM 2003 5 13 F3LA200300117 120030411A5320 FLOOR SUPPORT BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 3468 24856 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT STA. 772, BETWEEN RBBL 8.10 AND LBBL 12.5. FABRICATED AND INSTALLED REPAIRS PER SRM 53-00-53. 2L72 4F RTA16WE 20030513002542003051300254EA 2003 5 13 ASOA03176 120030420A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DUIRNG A C-CHECK IN MCN, CROSS SUPPORT AT FS 589 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CROSS SUPPORT AT FS 589 BETWEEN LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20030509001002003050900100SW 2003 5 9 AC2A086261 120030409A6320 PRESSURE SWITCH BELL 430 430 1182150SW ALLSN 250C 250C* GL GEARBOX OIL FALSE INDICATIONE AC2AO OTHER J WARNING INDICATION CRCRUISE 1 SO07430CV 49072 WHEN AIRCRAFT IS FLOWN THROUGH RAIN THE TRANSMISSON OIL, RED WARNING LIGHT COMES ON. THE LIGHT GOES OUT SHORTLY AFTER AIRCRAFT IS NOT IN RAIN. THE PRESSURE AND TEMPERATURE ARE IN THE NORMAL RANGE WHEN THE LIGHT COMES ON. CLEANED TRANSMISSION OIL PRESSURE SWITCH TERMINAL FREE OF ALL WATER. FUNCTION TEST GOOD. 1G72 3U3 URTH9SW E4CE 20030513002492003051300249EU 2003 5 13 ASOA03160 120030414A33503011210 LIGHT AEROSPATR72 ATR72 EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20030527000902003052700090WP 2003 5 27 AALA20030377 120030328A3397 TERMINAL DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21246AA 49258 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS FROM ROW 18-21 INOPERATIVE. SECURED EMERGENCY EXIT CEILING LIGHT TERMINAL AT BATTERY. GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030604000152003060400015SO 2003 6 4 SIMA200311314 120030418A531014521713005 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21708AE 145205 DURING AN IMBV INSPECTION, THE GALLEY CENTER HAT BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED AREA OF THE HAT BEAM, CLEANED AND TRETED THE AREA. FABRICATED A REPAIR DOUBLER AND ATTACHED. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 21, CHAPTERS 53-21-10 FIGURE 204. (M) 2L72 4F RTT00011AT 20030604001452003060400145NM 2003 6 4 UPS03440565 120030410A5320 SUPPORT BRACKET BOEING747 747121 1384871NM KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, KEELBEAM PANEL SUPPORT SURFACE FOUND SURFACE CORROSION AT STA 1276 TO STA 1287 RBL 16. CORROSION BLEND OUT (0.020 X 1 X 1). KEEL BEAM PNL SUPPORT REPLACED AS PER SRM 51-10-01 P.8. 2L74 4F A20WE 20030609001152003060900115EA 2003 6 9 03140705 120030520A3350 LIGHT CNDAIRCL600 CL600* EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27705BR DURING MAINTENACE INSPECTION, FORWARD OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY LIGHT, AN OPERATIONAL CHECKED SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20030515000342003051500034EA 2003 5 15 03122659 120030502A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030609002012003060900201 2003 6 9 HEEA086574 420030522A34578143902240B GPS SKRSKYS76 S76A 8143006NE COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 INTERMITTENTLY WILL NOT READ DATABASE CARD. SHOP REPAIR. 1G72 3U H1NE 20030609000062003060900006WP 2003 6 9 ARWA20030502 120030512A793042D491C PRESSURE SWITCH DOUG DC8 DC863F 302198FWP NR 1 ENGINE FAILED A ARWAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19906R 46087 NR 1 ENGINE LOST OIL QTUANTITY. ENGINE WAS SHUT DOWN. AIRCRAFT LANDED IN KMIA WITHOUT INCIDENTS. FOUND NR 1 ENGINE OIL PRESS DIFFERENTIAL SWITCH LEAKING. REMOVED AND REPLACED SWITCH IAW DC8 MM 79-31-06. PERFORMED ENGINE RUN UP AND OPS CK IAW DC8 MM 71-00 FOUND NORMAL. 2L74 4F 4A25 20030610001042003061000104GL 2003 6 10 HEEA086998 220030604A732023072725 HMU BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 STARTS HOT ON BACK TO BACK STARTS WITH TOT REACHING 780 TO 790 DEGREES CELCIUS. REPLACED HMU. 1G71 3U3 UO H2SW E4CE 20030612000882003061200088WP 2003 6 12 UPS03840712 120030528A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY AND RELAY UNIT IAW MM 33-50-01. CHECKS GOOD. 2L74 4F RT4A25 20030610000092003061000009SO 2003 6 10 C2XA03BT060 120030523A3230355022002 ELECTRICAL BOX EMB 145 EMB145 3260210SO MLG FAULTY A C2XAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW2712122 145684 CREW REPORTED, LANDING GEAR WOULD NOT RETRACT. MAINTENANCE TROUBLESHOT SYSTEM, REMOVED AND REPLACED THE LEFT HAND MAIN LANDING GEAR, NOSE LANDING GEAR PROXIMITY SWITCHES AND LANDING GEAR HANDLE. PERFORMED TEST FLIGHT TO VERIFY THE REPAIR, TEST FLIGHT FAILED AIRCRAFT RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU) IAW EMB145XR MM 32-32-01. GEAR SWING PERFORMED, OPS CHECKS GOOD IAW EMB145XR MM 32-30-00. AIRCRAFT RELEASE FOR TEST FLIGHT, AIRCRAFT TEST FLOWN SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030617001352003061700135GL 2003 6 17 ERAA087096 220030520A7323252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE FAILED E ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01298EH10482 S845 ENGINE GETS 100 PERCENT N1 BUT FALLS OFF WHEN PULLING PITCH. DROPS EARLY / OUT OF SERVICE LIMITS. HAS STIFF THROTTLE SHAFT, CORRODED, UNDER SIZE ECCENTRIC SHAFT. REPAIRED AND TESTED IAW HONEWELL OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20030521001892003052100189EU 2003 5 21 AWXA200300540 120030515A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 263 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28667AW 1710 SAN - EEL - DURING 4-DAY CHECK THE AFT CABIN EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT (13WL) BATTERY PACK IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030522001062003052200106NM 2003 5 22 CALA0300257 120030520A5414 SKIN BOEING737 7373T0 1384582NM NR 1 NACELLE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON UPPER SURFACE PANEL 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230. 2L72 4F RTA16WE 20030521001282003052100128NM 2003 5 21 DHL2003726005 120030515A2612 FIRE LOOP BOEING727 727228 1384083NM NR 3 SHORTED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01726DH 20409 ENGINE NR 3 SYSTEM-B FIRE DETECTION LIGHT ILLUMINATED. TRANSFERRED TO DMI NR 12942 PER DHL MEL 26-13-1 CAT-C. PLACARD INSTALLED. MAINTENANCE CONTROL WAS NOTIFIED. REF DMI NR 12942 NR 3 ENGINE SYSTEM B-LOOP FIRE DETECTION. TROUBLESHOT TO SHORTED FIRE WALL LOOP. PART ORDERED. DMI 12942 REMAINS OPEN. REF DMI 12942 - NR 3 ENGINE B-SYSTEM FIRE LOOP INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE LOOP, NO HELP. FOUND NEW PART BAD FROM STOCK. CLEANED OIL FROM CONNECTORS, OPS CHECKED GOOD PER M/M 26-11. THIS CLEARS DMI 12942, PLACARDS REMOVED. 2L73 4F RTA3WE 20030522000812003052200081SO 2003 5 22 C2XA03SH137 120030518A532014525991003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 SHV DURING C-CHECK LEFT HAND LOWER LINING CARGO SUPPORT AT FRAME 61 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030527000112003052700011WP 2003 5 27 DHL2003801065 120030403A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 RT WING INBOARD L/E FORMER WITH 1.000 INCH CRACK AT STA XFS 597.500. STOP DRILLED CRACK AT STA XFS 597.500 IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCEMENT (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ON INBOARD L/E FORMER (RT WING) IAW SRM 57-2-0 PG 9-10 AND SRM 51-1-20D PG 21. 2L74 4F RT4A25 20030617002672003061700267NM 2003 6 17 QXEA200300613 120030508A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - SHIMS BETWEEN FORWARD, LEFT HAND, H-STAB TO V-STAB ATTACH POINT ARE EXTRUDING. REPAIRED IAW Q400 AMM TASK 55-10-00-400-801. 2H72 4T RTA13NM 20030618000222003061800022SW 2003 6 18 HEEA087331 120030611A6510 BEARING BELL 407 407 1182206SW DRIVE SHAFT OVERHEATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH A1187 53283 BEARING IS GETTING HOT AND HEAT IS TRAVELING DOWN SHAFT. REPLACED. 1G71 3U O H2SW 20030618000442003061800044NM 2003 6 18 SWAA031336 120030614A3350BR2013 COVER BOEING737 7372T4 1384492NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED A1 CHECK, FOUND EEPLS COVER STRIP CRACKED AT MOST FWD 24. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F A16WE 20030623000532003062300053WP 2003 6 23 GTIA030361 120030508A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND FORWARD CARGO JAMB BEAM CRACKED AT AFT DOOR STOP. REMOVED FORWARD CARGO JAMB BEAM. LOCATE AND DRILL NEW JAMB BEA. INSTALLED NEW JAMB BEAM. (M) 2L72 4F A6WE 20030624000722003062400072WP 2003 6 24 0301109138 120030608A2150 DUCT DOUG DC9 DC915 3022036WP LT ACM OUTLET SEPARATED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL019348 45787 AT THE TOP OF THE CLIMB NEAR FL270 THE FLIGHT CREW NOTICED CABIN PRESSURE WAS CLIMBING AT 1500 FPM. VERIFIED OUTFLOW VALVE FULLY CLOSED BOTH PACKS OPERATING AND AC AUTO-SHUTOFF WAS IN OVERRIDE. INITIATED AND EMERGENCY DESCENT BUT CABIN MASKS DEPLOYED BEFORE AIRCRAFT COULD GET LOW ENOUGH. FLIGHT CONTINUED TO BUF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE BOOTS OFF THE LEFT ACM DISCHARGE DUCT DISCONNECTED. REINSTALLED BOOTS, ALL CONNECTIONS FROM ACM INSPECTED AND OPS CHECKED. AIRCRAFT RETURNED TO SERVICE AFTER MASKS REPACKED. 2L72 4F A6WE 20030702000162003070200016NM 2003 7 2 AMTA200300716 120030527A3350 LIGHT BOEING737 73783N 13844HINM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11302TZ 32576 PROX LIGHT FORWARD ENTRANCE FOR EMERGENCY EGRESS LIGHTS INOPERATIVE AND BROKEN IN PIECES. REMOVED AND REPLACED PROX LIGHT ASSEMBLY FOR EGRESS LIGHTING AT FORWARD ENTRANCE OPS CHECKS NORMAL. (M) 2L72 4F RTA16WE 20030626000152003062600015NM 2003 6 26 2003UALA00363 120030404A5250AR47261 STRIKER BOEING777 777222 1385219NM PWA PW4077PW4077 NE COCKPIT BURNED A UALAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29214UA782 30220 ELECTRICAL ODOR IN COCKPIT AND CABIN. FLIGHT DECK DOOR IN AIRCRAFT HAD BURNED STRIKER ASSEMBLY. DISCREPANT STRIKER REPLACED, 2L72 4F4 FRTT0001SE E46NE 20030707001172003070700117EU 2003 7 7 VY1L110906 120030228A6420355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED L VY1LO OTHER O OTHER NRNOT REPORTED 1 SW194TV 457 2936 TAIL ROTOR LAMINATED BEARING CRACKED. 1G71 3U3 U H9EU E19EU 20030711001212003071100121WP 2003 7 11 MWEA030260 120030630A5534591218835 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 STATION 1420 LEFT SIDE INNER VERTICAL STABILIZER TO FUSELAGE FITTING IS CRACKED. FABRICATED AND INSTALLED ANGLE. 2L72 4F A6WE 20030717000242003071700024SW 2003 7 17 HEEA088001 120030627A6720407001732101 BELLCRANK BELL 407 407 1182206SW T/R CONTROL WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 TAIL ROTOR CONTROL BELLCRANK HAS A WORN SLEEVE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030106001582003010600158NE 2003 1 6 HEEA082809 120030102A63217665009803103 POWERPACK SKRSKYS76 S76A 8143006NE ROTOR BRAKE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 ROTOR BRAKE CONTINUES TO MOTOR. WON'T SHUT OFF. 1G72 3U H1NE 20030127002742003012700274GL 2003 1 27 HEEA083750 220030115A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03492PH 53390 CAUSING NOISE WHEN ENGINE IS ACCELERATED FOR GROUND IDLE. REPLACED BLEED VALVE. 1G71 3U3 UO H2SW E4CE 20030128000202003012800020GL 2003 1 28 HEEA083772 220030115A720023063392 ENGINE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENG BAY MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 CAE847312 ENGINE MAKING METAL. REPLACED WITH SERVICEABLE ENGINE. 1G71 3U3 UO H2SW E1GL 20030204001112003020400111NM 2003 2 4 SWAA030088 120030115A53116520722 FRAME BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BIN ATTACH BRACKET BS 440 BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20030205001312003020500131WP 2003 2 5 MWEA030055 120030205A57539958000161 DOUBLER DOUG DC9 DC981 3022081WP O/B FLAP CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 RIGHT OUTBOARD FLAP HAS MODERATE CORROSION ON INTERNAL SKIN SURFACE AND FRAME. -- REMOVED WEB AND CORRSION, FABRICATED AND INSTALLED WEB AND DOUBLER. 2L72 4F A6WE 20030206000442003020600044 2003 2 6 DLM11030010 420030102A2330 DISPLAY DOUG MD11 MD11 3023602NM ENTERTAIN SYS FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27809DE 48480 SEAT 1B VIDEO SCREEN HAD ELECTRICAL ODOR. LIQUID SPILLED IN AREA ODOR DISSIPATED SCREEN NOW INOPERATIVE. REACTIVATED SEAT ENTERTAINMENT SYS. FOUND BAD SDU CAUSED SCC IN AUDIO/VIDEO UNIT TO FAIL. REPLACED SDU AND AUDIO/VIDEO UNIT LOADED S/W SEAT ENTERTAINMENT SYS OPS NORMAL. 2L73 4F RTA22WE 20030210001232003021000123NM 2003 2 10 QXEA0300066 120030110A5320 STRINGER CLIP BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- STRINGER 22L TIE CLIP WHERE STRINGER MEETS THE AFT SIDE OF FRAME X789.102 IS CHAFED ON THE TOP. REPAIRED IAW DHC-8 400 SRM 51-14-00, 53-40-03, 51-21-10 AND TASK 51-00-02-250-801. 2H72 4T RTA13NM 20030210001272003021000127NM 2003 2 10 QXEA0300070 120030106A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX- CHAFE ON OUTBOARD END OF LEFT HAND FLAP ON TOP SKIN. REPAIRED IAW DHC-8 400 SRM 57-52-30 AND 51-25-05. 2H72 4T RTA13NM 20030625000742003062500074NM 2003 6 25 F3LA200300048 120030129A5320 CHANNEL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT STA 727 TO STA 947, LBL 12.5 CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. REPLACED FLOOR SUPPORT PER SRM 53-60-53 AND 51-40-02. 2L72 4F RTA16WE 20030214001092003021400109WP 2003 2 14 ASAA0380057 120030105A57309937576506 PANEL DOUG DC9 DC983 3022083WP RT WING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING LOWER LEADING EDGE PANEL 1248C HAS 3 ELONGATED HOLES. INSTALLED DOUBLERS PER SRM 51-07. (M) 2L72 4F RTA6WE 20030218000382003021800038NM 2003 2 18 AWXA200300016 120030106A3240 BRAKE ASSY AIRBUSA319 A319132 3930340NM MAIN INOPERATIVE A AWXAK NONE O OTHER TXTAXI/GRND HDL 1 WP28812AW 1178 WHILE TAXING TO GATE, ARRIVING, BRAKES WERE GRABBING AND RELEASING ALMOST UNCONTROLLABLY. MAINTENANCE PERFORMED A BITE CHECK ON BRAKE STEERING CONTROL UNIT (BSCU) 1 AND 2 AND FOUND NO FAULTS. RESET BSCU 1 AND 2 IAW AMM 32-42-00-810-912. BRAKING FUNCTIONS NORMAL DURING MAINTENANCE TAXI. NO GRABBING FELT IN A/C OR RUDDER PEDALS. SUBSEQUENT TROUBLESHOOTING REVEALED THAT ALL 4 BRAKES WERE BLED OF AIR IAW TROUBLE SHOOTING MANUAL AMM 32-42-00-810-912. 2L72 4F RTA28NM 20030218000732003021800073NM 2003 2 18 AMTA200300129 120030123A3397 WIRE BOEING757 75723N 1384973NM CABIN LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11527AT 30886 THREE EGRESS TRACK LIGHTS INOPERATIVE AT SEAT 28 DEF. SECURED WIRE OK FOR SERVICE. (M) 2L72 4F RTA2NM 20030219000852003021900085NM 2003 2 19 SWAA030300 120030208A335020131A CHARGER BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED RON, FOUND EEPLS INOP AT ROWS 9, 7 AND 11. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PER MM. 2L72 4F RTA16WE 20030220000652003022000065WP 2003 2 20 ABXA030066 120030206A5310 THRESHOLD DOUG DC8 DC863 302198AWP PAX DOORWAY BENT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 MAIN CABIN DOOR THRESHOLD LIP WAS RAISED PREVENTING DOOR FROM OPENING. REPAIRED RAISED LIP ON THRESHOLD OF MAIN CABIN DOOR AS REQUIRED IAW DC-8 MM. 2L74 4F 4A25 20030220001182003022000118NM 2003 2 20 QXEA0300112 120030123A5270 SWITCH BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DIRTY A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09414QX 4061 GTF-ON FLIGHT NUMBER 2321, ON TAKEOFF ROTATION FUSELAGE DOORS CAUTION LIGHT ILLUMINATED. FORWARD BAGGAGE DOOR LIGHT SHOWED OPEN. UNABLE TO PRESSURIZE AIRCRAFT. INSPECTED FORWARD CARGO DOOR AND SWITCHES. CLEANED AND LUBED SWITCHES. OPERATED DOOR, NO WARNINGS AT THIS TIME. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030116001702003011600170SO 2003 1 16 C2XA02SH164 120030103A53201452249003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV- DURING C-CHECK RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND REPLACED AFFECTED RAMP ANGLE. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030304000992003030400099 2003 3 4 HEEA084601 420030214A3442MI5851345 INDICATOR BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032258F 33073 WEATHER RADAR SYSTEM FAILS TO DISPLAY PROPERLY. FOUND LOGIC NR 1 BOARD BAD. REPLACED SEVERAL ICS. REPAIRED A BROKEN FOIL FROM PIN 19 OF J1201 HEADER TO PIN 11 OF U1260. BENCH CHECK GOOD. 1G72 4U H4SW 20030225000642003022500064SW 2003 2 25 HEEA084286 120030211A6220 SEAL BELL 206 206L3 1182108SW ROTOR HEAD LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033116L A2359 51529 SLINGING GREASE FROM OUTBOARD SEAL WHITE GRIP. REPAIRED. 1G71 3U H2SW 20030227000912003022700091SO 2003 2 27 C2XA03CL054 120030226A33501317 BULB EMB 145 EMB145 3260210SO CABIN BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712967 145133 DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT ON THE CEILING WAS FOUND INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030228000022003022800002SW 2003 2 28 HEEA084386 120030211A2420FCB405AT4 CONTACTOR BELL 407 407 1182206SW ELECTRICAL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 DURING START ATTEMPTS STARTER FAILED TO CATCH. 1G71 3U O H2SW 20030303000152003030300015 2003 3 3 373PA0006 420030303A2230 THROTTLE CONTROL BOEING737 7373Y0 1384671NM A PIDAK NONE O OTHER CLCLIMB 1 SO05373PA 23749 Auto throttle on #2 engine will not maintain N1. Lever moves forward & aft one inch during climb/take-off. Adjusted low idle speed, ran engine, operates within limits per MM 71-00-01 p.222 2L72 4F RTA16WE 20030307000452003030700045NM 2003 3 7 SWAA030463 120030227A53116546546 FRAME BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, WL 161 AND RBL 19 TO RBL 28. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030307000532003030700053NM 2003 3 7 SWAA030441 120030224A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 867, BELOW STR 13R AND BS 847, BELOW STR 14R. REPAIRED SKIN PER SWA ACO AND ERO. 2L72 4F RTA16WE 20030313001792003031300179WP 2003 3 13 AALA20030135 120030131A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21582AA 53159 DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 10 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030314000622003031400062NM 2003 3 14 CALA0300025 120030128A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914320 23371 INSPECTION FOUND A CRACK IN THE PRESSURE DECK WEB AT STA 665 - 675, RBL 35 - 45. THE CRACK WAS ESTIMATED TO BE .5 - .75 INCH LONG. THE AREA WAS REPAIRED IAW SRM 53-60-51, FIGURE 203 AND ECRA 5310-04316. 2L72 4F RTA16WE 20030314000682003031400068NM 2003 3 14 CALA0300047 120030214A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM STA 663.75 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0971314 23365 INSPECTION FOUND A .75 INCH CRACK IN BOTH THE LEFT HAND AND RIGHT HAND PRESSURE DECK AT STA 663.75. BOTH LOCATIONS WERE REPAIRED IAW SRM 53-60-51. 2L72 4F RTA16WE 20030317000322003031700032NM 2003 3 17 03FDEA00166 120030224A5330 SKIN BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 SKIN DENT, BS 720B+3, JUST BELOW STR 17R, REWORKED SKIN DENT, BS 720B+3 BELOW STR 17R. A=1.8 Y=.062 A/Y=12.9 AND OIL CANNED. OUT OF LIMITS IAW 53-30-01. REMOVED DAMAGED AREA 2.3 X 2.9. FABRICATED, ALODINED, PRIMED AND PAINTED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3. 2L73 4F4 F A3WE E2EA 20030122001462003012200146NM 2003 1 22 DL757030024 120030105A8011 STARTER BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. EBJVIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SO27667DN53984 25035 716328 DURING ENGINE START RT ENGINE SHUTTERING WAS FELT DURING NORMAL START SEQUENCE. GROUND CREW NOTICED SPARKS AND SMOKE OUT OF RT ENGINE DURING START. RT ENGINE FIRE INDICATION AND SHUTDOWN. DISCHARGED BOTH FIRE BOTTLES. FOUND NR 2 ENG STARTER HAD UNCONTAINED FAILURE. REPLACED STARTER, STARTER DUCT, OIL LINE FROM GEARBOX TO SCAVENGE PUMP, SCAVANGE PUMP LUBE ASSY, PMA HARNESS, OIL LINE FROM SCAVENGE PUMP TO TOP OF OIL TANK, BOTH ENGINE FAN COWLS, ENG HYD PUMP, HYD PRESSURE AND CASE DRAIN FILTERS, FIRE LOOP AND BOTH FIRE BOTTLES. SERVICED HYD AND OIL, RAN ENGINE. ALL CKS GOOD. 2L72 4F4 FRTA2NM E17NE 20030123000172003012300017NM 2003 1 23 2003UALA00033 120030107A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29355UA 24361 CORROSION ON RIGHT CREASE BEAM INBOARD CHORD FROM BS 294 TO BS 334. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2L72 4F4 FRTA16WE E2GL 20030317000992003031700099NM 2003 3 17 03FDEA00260 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 20R FOUND CORRODED AT THE BEARING SURFACES. 2L73 4F RTA22WE 20030319000122003031900012 2003 3 19 GTIA030014 420030102A2565 PIN DOUG MD80 MD83 3023681NM TAIL SLIDE DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 LGA - FLT 1865 - FOUND TAIL COMPARTMENT SLIDE COVER PINS OUT ON RIGHT SIDE AND HALF OUT ON LEFT SIDE. REINSTALLED TAIL COMPARTMENT SLIDE COVER PINS LEFT AND RIGHT SIDE. (M) 2L72 4F RT 20030806000332003080600033 2003 8 6 BAQA088150 420030718A3421109290 GYRO BOLKMS117 BK117B1 5626012EU YAW CSAS INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G9066 7179 YAW CSAS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030801001232003080100123WP 2003 8 1 MWEA030301 120030730A5313592480225 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 STATION 408 LONGERON 17 RIGHT IS CRACKED. FABRICATED AND INSTALLED NEW SECTION OF LONGERON. 2L72 4F A6WE 20030806000102003080600010SW 2003 8 6 ALGA088117 120030716A6220406310405101 LINK BELL 407 407 1182206SW PITCH CONTROL WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03405AL634 53480 PITCH CONTROL LINK BEARING LOOSE WORN AND RATCHETY.REPLACED IN FIELD. SUBMITTED BY:PRESTON BARZARE 1G71 3U O H2SW 20030829000322003082900032NM 2003 8 29 CALA0300490 120030824A5347 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND SEAT TRACK CORRODED AT STA 296, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-40352 AND SRM 51-40-02. 2L72 4F RTA16WE 20030902001492003090200149SO 2003 9 2 SWIA200312161 120030610A5415 SUPPORT EMB 120 EMB120ER 3260203SO HYD PACK CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07563SW 120338 RT HYDRAULIC PACK LOWER SUPPORT, CRACKED IB EDGE. (DISCOVERED DURING C-CHECK)REPLACED RIGHT HYD PACK LOWER SUPPORT. 2L72 4T RTA31SO 20030903001002003090300100 2003 9 3 RJEF598H1 420030627A3421H321BHM1 INDICATOR AIRBUS320 A320233 3930329EU COCKPIT INOPERATIVE A RJEFK NONE O OTHER ININSP/MAINT 1 SO23465TA 1374 MSY - 221 - AIRCRAFT AT GATE, THE STANDBY HORIZONTAL INDICATOR WENT INOPERATIVE AND THE AIRCRAFT STOOD ON GROUND FOR MAINTENANCE. TECHNICIANS REPLACED AND TEST THE STANDBY HORIZONTAL PER AMM 34-22-24. RESULTS WERE SATISFACTORY AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20030903002772003090300277SO 2003 9 3 C2XA03SH278 120030818A321014571035414 CAP EMB 145 EMB145LR 3260212SO RT MLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV DURING C CHECK RIGHT MAIN LANDING GEAR LOWER BEARING CAP WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR LOWER BEARING CAP IN ACCORDANCE WITH EMB 145 AMM 32-10-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2L72 4T RTT00011AT 20030904001422003090400142WP 2003 9 4 DHL2003873608 120030703A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 RT OUTER WING AFT TOP PANEL PLATING AROUND STA XRS.693.000, S-3 S-5R CORRODED (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION FROM DAMAGED AREA. FOUND OUT OF LIMITS. BLENDED OUT DAMAGED AREA IAW EODHL-030622, ED-3469. PERFORMED EDDY CURRENT INSPECTION AROUND REPAIR AREA IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW EODHL-030622, ED-3469. CLEANED, TREATED AND PRIMED DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER WITH NEW FASTINERS IAW SRM 51-1-20B PG 5, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. FOR LEAK CHECK SEE N/R 2088. 2L74 4F RT4A25 20030812000882003081200088EU 2003 8 12 HEEA088626 120030310A243230248001 BATTERY BOLKMS105 BO105S 5626006EU MASTER WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037170D S840 MASTER BATTERY WEAK. REPAIRED. 1G72 3U H3EU 20030822000762003082200076NM 2003 8 22 03FDEA01080 120030709A5330 SKIN BOEING727 727200 138407ENM FUSELAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 EXTERIOR SKIN HAS SEVERAL LIGHTNING STRIKES FROM BS 334 TO BS 351 STR 25R TO STR 27R. REMOVED DAMAGE ON 7EA LIGHTNING STRIKES BS 334-351, STR 25-27 RT 5EA AREA. REMOVED DAMAGE BY DRILLING OUT DAMAGE AND INSTALLING FASTENERS PER SRM 53-30-3, 1EA AREA FOUND TO BE WITHIN LIMITS BY BLENDING OUT DAMAGE, 1EA AREA REPAIRED BY CUTTING OUT DAMAGE IN 1 X 1 INCH AREA AND REPAIRING PER SRM 53-30-3, FIG 1. 2L73 4F RTA3WE 20030911000272003091100027NM 2003 9 11 03FDEA01231 120030808A5753ARC41251 FITTING DOUG MD11 MD11 3023602NM TE FLAPS CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. LT WING OUTBOARD FLAP INBOARD STOP FITTING CARRIED OUT REPAIR AS PER EA 1-5750-71804 ( WINGS - TRAILING EDGE FLAPS - LEFT AND RIGHT OUTBOARD FLAP SECONDARY STOP BOSS REPAIR). 2L73 4F RTA22WE 20030911000722003091100072 2003 9 11 AWXA200300802 420030713A3442 CONTROL UNIT AIRBUS320 A320232 3930326EU ADIRU MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28661AW 1284 ABORTED TAKEOFF - FLT 0299 - DURING TAKEOFF ROLL AT MIA EN ROUTE TO PHX THE CREW ABORTED TAKEOFF DUE TO AN INERTIAL REFERENCE (NR 2 IR) FAULT AT 90 KTS. AIRCRAFT TAXIED BACK TO GATE AND MEL 34-10-01 COND. 4, "NR 2 IR INOP" WAS ISSUED. ON 07/14/2003 MAINT R & R THE NR 2 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW T/C R2A34304, AUTO LAND TEST WAS GOOD PER T/C A1B22307. VENDORS BENCH TEST OF ADIRU S/N 1531 COULD NOT VERIFY REASON FOR REMOVAL. PERFORMED THERMAL CALIBRATION OF UNIT, UNIT TESTED IAW CMM TP1011, REV. 22. 2L72 4F RTA28NM 20030911001122003091100112WP 2003 9 11 MWEA030327 120030821A2613 SENSOR DOUG DC9 DC981 3022081WP TAIL TEMP FALSE INDICATIONA MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31803ME 48029 THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AND THEN WENT OUT. PERFORMED LEAK CHECKS OF ALL PNEUMATC DUCTS IN AFT ACCESSORY COMPARTMENT. NO LEAKS NOTED. PERFORMED ADJUSTMENT TEST OF TAIL COMPARTMENT TEMPERATURE HIGH SYSTEM. NO DEFECTS NOTED. 2L72 4F A6WE 20030911001272003091100127NM 2003 9 11 03FDEA01213 120030729A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND WITH CORROSION IN HOLE. LT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71810, TITLE: WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP NR 3 AND NR 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20030912000742003091200074WP 2003 9 12 DHL2003604774 120030617A532037504981 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT ACCESSORY COMPT FRAME SPLICE FITTING HAS A 2.000 CRACK, STA 660.000 L-35L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, ATM PO201385, DWG 3750498. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SPLICE FITTING IAW DWG 3750498. PERFORMED LIQUID PENETRANT INSPECTION TO NEW SPLICE FITTING IAW DC8 NDT SPM PART 08-00-02/06. CLEANED, TREATED AND PRIMED NEW SPLICE FITTING IAW SRM 51-1-8B. INSTALLED SPLICE FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030912001602003091200160EU 2003 9 12 AWXA200300912 120030802A5320D5391379020002 PROFILE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28653AW 1003 MCN - MINOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON FWD CARGO COMPARTMENT PROFILE AT FR 28, STR 38 RT. MAINTENANCE CUTOUT DAMAGED SECTION OF PROFILE AT FR 28, STR 38 RT; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND A SPLICE PLATE; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1. 2L72 4F RTA28NM 20030925000032003092500003NM 2003 9 25 USAABB03129 120030804A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY, NO HELP. REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030926000592003092600059EA 2003 9 26 COMA0360388 120030824A2420820465 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA ADG MALFUNCTIONED A COMAA UNSCHED LANDING HS ELECT. POWER LOSS-50 PC AFFECT SYSTEMS CLCLIMB 1 SO01477CA2940 7670 FLIGHT 6519 ADG AUTO DEPLOYED AFTER T/O. REPLACED THE ADG CONTROL UNIT. 2L72 4F RTA21EA 20030911000532003091100053NM 2003 9 11 03FDEA01157 120030728A5315651785566 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 PLATE ON 25G BEAM UNDER FE'S SEAT BULGED. ACCESSED FLOOR PANELS; REMOVED 25G BEAM; REPLACED WITH NEW PART; PER SRM 51-30- 2; REINSTALLED ACCESSED GROUP. 2L73 4F RTA3WE 20030930000602003093000060NM 2003 9 30 P5CA0300939 120030908A3697 WIRE BOEING747 7472U3B 1384846NM RT WING LE DAMAGED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23923FT 22769 RT WING LEADING EDGE OVERHEAT LIGHT ON WITH SMALL INCREASE OF PWR. FOUND DAMAGED WIRE AT SWITCH 1046 REPAIRED WIRE PER 20-50-2. 2L74 4F RTA20WE 20030930000632003093000063WP 2003 9 30 ZW0A0306201 120030906A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13954U 49426 THE AFT EXIT DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPAIRED BROKEN WIRES IN CEILING. CHECK-C 6-17-03 STL. 2L72 4F A6WE 20030930001202003093000120NM 2003 9 30 03FDEA01480 120030902A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG O/B SIDE SURFACE CORRODED. 2L73 4F RTA22WE 20031001000742003100100074NM 2003 10 1 2003UALA00712 120030826A3620 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COCKPIT ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29336UA 24240 ON CLIMB OUT OF OMA CREW GOT BLEED TRIP OFF LIGHTS & ANOTHER WING BODY OVERHEAT INDICATION. CAUSED BY FAILURE OF PRE-COOLER PNEUMATIC VALVE DUE TO PLUGGED ORIFICE. REPLACED PRE-COOLER VALVE. HIGH STAGE VALVE AND PRECOOLER VALVE SENSOR WERE REPLACED AS A PRECAUTIONARY MEASURE. RAN ENGINE AND OPERATIONAL CHECK OF THE SYSTEM TESTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20030908002782003090800278EA 2003 9 8 SWIA200312376 120030904A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07448SW 7678 NOSE GEAR NOT DOWN AND LOCKED. DOORS OPEN AND MAIN GEAR SHOW DOWN AND LOCKED BUT NOSE GEAR DON'T INDICATE DOWN AND LOCKED. ACCOMPLISHED NOSE GEAR UP LANDING. NO INJURIES SUSTAINED. NTSB INVESTIGATING. REPLACED LANDING GEAR NOSE ASSY AND COMPONENTS IAW 32-00-00. LANDING GEAR OPS CHECKS GOOD. 2L72 4F RTA21EA 20030909002622003090900262SO 2003 9 9 RAIA00308220 120030817A783083990137 SWITCH EMB 145 EMB145 3260210SO THRUST REVERSER MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03805HK 145096 5263-GRR- ENGINE NR 1 THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE PLACED NR 1 T/R ON DEFERRAL IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 T/R LOWER OUTBOARD SWITCH. 2L72 4F RTT00011AT 20031001000852003100100085EA 2003 10 1 0300052 120030926A26113601881000390 FIRE LOOP DHAV DHC8 DHC8311 1386006EA NR 1 ENGINE FALSE INDICATIONA HNAAO OTHER N FALSE WARNING CRCRUISE 1 EA07284BC 336 WARNING LIGHT, AND NR 1 ENGINE A LOOP LIGHT ILLUMINATED. SELECTED B LOOP AND FAULT A LOOP WENT OUT ALL ENGINES INDICATIONS NORMAL. 2H72 4T RTA13NM 20031002000672003100200067NM 2003 10 2 QXEA200301092 120030831A5414 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 L-BRACKET SUPPORTING FILLET SKIN PANEL OF NACELLE FAIRING IS CRACKED AT INBOARD EDGE OF NR 1 NACELLE STATION YW139.00. REPAIRED IAW DHC-8 SRM 51-20-26, 51-40-11, RD 8-54-440 AND HORIZON AIR EA 2-54-182. 2H72 4T RTA13NM 20031006000012003100600001EA 2003 10 6 COMA0360405 120030905A2750860D10018ABC FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01818CA11793 7408 FLIGHT 5476 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20031009000252003100900025SO 2003 10 9 SIMA200322301 120030807A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DIRTY A SIMAK NONE O OTHER ININSP/MAINT 1 SW21649PP 145234 CREW REPORTED THE EMERGENCY EXIT LIGHT AT SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR FOR THE EXIT LIGHT TO BE DIRTY. THE CONNECTOR WAS CLEANED AND RESECURED. OPS CHECK OF EMERGENCY LIGHTS WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20031021000622003102100062 2003 10 21 USAASA03110 420030909A2565 RELEASE CABLE AIRBUSA319 A319112 3930323EU EVAC SLIDE INCORRECT A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19745UW 1289 PHL - THE AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20031021002692003102100269NM 2003 10 21 03FDEA01575 120030918A532065233316 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 BS 440, STR 5 LT STR CLIP CRACKED. REMOVED DAMAGED STR CLIP AT BS 440 STR 5 LT DRILLED NEW STR CLIP AND INSTALLED IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20031021002992003102100299WP 2003 10 21 ABXA030364 120030919A2120 ODOR DOUG DC9 DC941 302207NWP PWA JT8 JT8D* NE COCKPIT DETECTED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23972AX 47631 INTERMITTENT BURNING ODOR UNDER FIRST OFFICER'S GLARESHIELD. ANTI-FOG C/B'S WERE PULLED FOR ENTIRE FLIGHT. INSPECTED WIRING UNDER GLARESHIELD, BEHIND FIRST OFFICER'S INSTRUMENT PANEL AND FORWARD ACCESSORY COMPARTMENT. ALL SYSTEMS WERE ON, ALL LIGHTS WERE FULL BRIGHT FOR TWO HOURS. NO DEFECTS NOTED AT THIS TIME. NO EVIDENCE OF BURING ODOR. 2L72 4F4 F A6WE E2EA 20031027000172003102700017EA 2003 10 27 COMA0360427 120030924A2120601R9521171 DUCT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE LEAKING A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01988CA 7204 FLIGHT 5119 DURING CRUISE FLIGHT CABIN ALTITUDE WAS INCREASING, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE LEFT FUSELAGE SUPPLY (Y) DUCT. 2L72 4F4 FRTA21EA E15NE 20031028001782003102800178NM 2003 10 28 ASAA0340074 120030227A5320654769024 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031023000582003102300058EA 2003 10 23 SWIA200312448 120030920A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07908SW5432 5432 7540 AFTER FLAPS REACHED 45 DEGREES WE RECEIVED A FLAPS FAIL MESSAGE.REMOVED AND REPLACED FLAP PDU OPS CHECK GOOD IAW CRJ MM 27-52-01.P/N 865D100-7 S/N OFF 0831 S/N ON 0706. 2L72 4F4 FRTA21EA E15NE 20031028000842003102800084NM 2003 10 28 2003UALA00770 120031010A5270 CONNECTOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE PROXIMITY SWITCHLOOSE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29840UA 1522 RETURN TO FIELD DUE TO A FWD CARGO DOOR ECAM MESSAGE. LOOSE CONNECTOR ON SENSOR 28WV AIRFRAME SIDE, SECURED THE CONNECTOR TO THE CARGO DOOR PROXIMITY SENSOR 28WV. 2L72 4F4 FRTA28NM E40NE 20031119001042003111900104WP 2003 11 19 MWEA030422 120031012A2611CGAB140000 SMOKE DETECTOR DOUG DC9 DC932 3022066WP CARGO INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31207ME 47794 DURING FLIGHT THE MASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS FOUND, NO POWER TO CARGO DETECTION PANEL. REMOVED AND REPLACED CARGO SMOKE DETECTORS, OHMED AND MEGGED ALL WIRING TO CARGO SMOKE DETECTOR. 2L72 4F A6WE 20040212000742004021200074NM 2004 2 12 F3LA200300166 120031205A5320 ANGLE BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03314FL 1426 25256 DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE ON MOP SILL SUPPORT ANGLE, STA. 326, LBL 57. REPLACED ANGLE UNDER MOP SILL IAW SRM 51-40-02. 2L72 4F RTA16WE 20040212001392004021200139NE 2004 2 12 757BJ0004 220031212A7320 GOVERNOR BOEING757 757236 1384971NM RROYCERB211 RB211535C37 54555NE FUEL FLOW LEAKING A PIDAK NONE K FLUID LOSS ININSP/MAINT 1 SO05757BJ 22176 FUEL LEAKING UNDER NR 2 ENGINE. REPLACED FUEL FLOW GOVERNOR SOLENOID VALVE IAW MM 73-21-15. OPS CHECK NORMAL DURING ENGINE RUN IAW MM 71-00-00. 2L72 4F4 FRTA2NM E12EU 20031103001122003110300112NM 2003 11 3 AWXA200301136 120030904A5315BAC150310281 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 LCQ - MAJOR REPAIR - DURING C-16 CHECK INTERGRANULAR CORROSION WAS FOUND AT FASTENER HOLES ON UPPER SURFACE OF FLOOR BEAM AT BS 294, LBL 12 TO LBL 30. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGE ON UPPER T CHORD AT BS 294, LBL 12 TO LBL 30; FABRICATED 4 EACH -2 AND 4 EACH -3 REPAIR ANGLES, AND NEW REPLACEMENT SECTION OF UPPER T CHORD; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, PG. 223, FIG. 110. 2L72 4F RTA16WE 20031030000142003103000014SO 2003 10 30 C2XA03SH361 120030930A33505113WW LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714991 145278 DURING C CHECK THE LT EMERGENCY EXIT WALL LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LAMP IAW EMB 145 AMM 33-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031105000432003110500043WP 2003 11 5 ABXA030396 120031006A57115911300501 SPAR CAP DOUG DC9 DC931 3022065WP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 CRACK ON UPPER SPAR CAP REAR SPAR XCW '0' TO XCW '10' RIGHT. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20031106000472003110600047SO 2003 11 6 C2XA03SH407 120031022A532014529150003 CROSSBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714542 145547 SHV- DURING C-CHECK THE RT CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20031112001202003111200120CE 2003 11 12 BAQA088982 120031013A32335081016417 ACTUATOR BEECH 90 C90 1152913CE PWA PT6 PT6* 52043EA LT MAIN GEAR FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0390LF 663 LJ852 MLG ACTUATOR FAILED END PLAY INSPECTION. 1000 CYCLE / 30 MONTH INSPECTION. REPLACED WITH SERVICEABLE UNIT. 10/20/03 1L72 3T3 T 3A20 E2NE 20031009001072003100900107NM 2003 10 9 F3LA200300135 120030917A5320 SILL BOEING737 73736E 138443ANM L2 DOOR CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED MOP SILL CORRODED INSIDE L2 DOOR SILL. REPLACED L-2 DOOR MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20031119000022003111900002EA 2003 11 19 03280652 120031007A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27652BR 7429 DURING INSPECTION, THE CEILING EMERGENCY LIGHT 2ND FROM FROM WAS FOUND INOPERATIVE. MAINTNANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F4 FRTA21EA E15NE 20031120000932003112000093EU 2003 11 20 DHL2003366007 120031015A523094FS494295133 SHEAR PIN AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE CARGO DOOR BROKEN A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01366DH 249 IMMEDIATELY AFTER GEAR RETRACTION THE MAIN CARGO DOOR NOT LOCKED LIGHT ILLUMINATED ON S/O'S PANEL. PERFORMED EMERGENCY PROCEDURE PER AOM. ILLUMINATED ENTIRE FLIGHT. FOUND SHEAR PIN BROKEN. REMOVED AND REPLACED PIN P/N: 94FS494295-133 AMM 52-36-11. DOOR AND LIGHTS OPERATE AND LOCK NORMALLY. 2L72 4F4 FRTA35EU E23EA 20031124000262003112400026NM 2003 11 24 P5CA0300983 120031110A27214011315111 COMPUTER BOEING747 747200 1384847NM ELEVATOR FAILED A P5CAK NONE O OTHER CLCLIMB 1 WP23524UP 21446 RUDDER RATIO LIGHT CAME ON AFTER T/O AT 250 KTS. LIGHT REMAINED ON & WENT OUT AFTER LANDING. REMOVED AND REPLACED ELEVATOR FEEL UNIT PER MM 27-31-14 , CHECK OK. 2L74 4F RTA20WE 20031117000862003111700086GL 2003 11 17 ALG2003F00092 220030824A7321M3899926NB98SN CONNECTOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL SENSOR CONTAMINATED E ALGAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03416AL 53046 CAE847085 IN FLIGHT, FADEC FAILED IN-FLIGHT, LIGHTS AND HORN SIMULTANEOUSLY HAD 2 TO 4 PERCENT DROP IN NP. MATCHED TORQUE IN CONTROLLED NP/NR WITH COLLECTIVE AND THROTTLE. MAINTENANCE CLEANED CONNECTOR ON COMPRESSOR SPEED SENSOR ON ENGINE. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20040113002322004011300232NM 2004 1 13 QXEA200301561 120031215A5720 ATTACH BRACKET DHAV DHC8 DHC8202 2809007NM LT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX - LT WING LEADING EDGE 511AL OUTBOARD LOWER ATTACH BRACKET SHOWS EVIDENCE OF CRACKING. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20040113002072004011300207SO 2004 1 13 C2XA03SH525 120031230A541314576094607 LONGERON EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 DURING C CHECK THE INBOARD UPPER LONGERON WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031124000742003112400074NM 2003 11 24 CALA0300648 120031114A541565C2630811 FITTING BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714320 23371 INSPECTION FOUND A 2 INCH CRACK IN NR 1 PYLON FORWARD FITTING AT LOWER I/B CORNER. THE NR 1 PYLON FORWARD FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20031217001712003121700171NM 2003 12 17 SWAA032645 120031202A57536546486 WEDGE BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED AFT WEDGE PANEL PER MM. 2L72 4F RTA16WE 20031218001532003121800153NM 2003 12 18 03FDEA02041 120031204A575465185337 FITTING BOEING727 727200 138407ENM NR 1 SLAT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25257FE 20939 WINGS BASIC- REWORK OF SLIGHT GOUGE IN L/E SLAT ACTUATOR FITTING. COMPLIED WITH ALL ASPECTS OF EA 7-5740-73855. 2L73 4F RTA3WE 20031223000202003122300020NM 2003 12 23 SWAA032623 120031129A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C3 CHECK, FOUND RH OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20031223000102003122300010EU 2003 12 23 035801 120031210A2430 GENERATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT DC SYSTEM FAILED A UHLAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 GL1743SZ 340A043 406 WHEN A/C GOT TO CRUISE ALTITUDE THE RIGHT DC GEN FAILED BRIEFLY. THE CREW GOT IT TO RESET, THEN IT FAILED AGAIN AND WOULD NOT RESET. A/C RETURNED TO PIT. IT WAS TAKEN OUT OF SERVICE 12-10-03 AT 2310(LT). 2L72 4T4 TRTA52EU E8NE6 20031224000462003122400046WP 2003 12 24 ASAA0380611 120031007A53475930566 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 OKC - FOUND 15K CHECK, CABIN SEAT TRACK IS CORRODED AT FS 1098-1217. REPLACED SEAT TRACK PER SRM 53-05. (M) 2L72 4F RTA6WE 20040106001332004010600133NM 2004 1 6 03FDEA02214 120031219A5753 VANE DOUG MD11 MD11 3023602NM T/E FLAP DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING INBOARD FLAP VANE FOUND WITH DELAMINATION. COMPLIED WITH FEDEX EA 1-5750-75198, TITLE - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBD FLAP VANE SKIN DELAMINATION. REPAIR. 2L73 4F RTA22WE 20040105000092004010500009NM 2004 1 5 DL73S031001 120031108A53126546568567 BULKHEAD BOEING737 737232 1384475NM AFT FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312DL 23084 A SMALL CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE FS 1016 AFT P-DOME WEB AT BL 0, WL 244. THE CRACK EMANATED IN 2 DIRECTIONS FROM THE HOLE AND WAS TOTAL OF .625 INCH LONG (INCLUDING HOLE DIA). THE CRACK WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 385883-14, REV A. 2L72 4F RTA16WE 20031009000722003100900072 2003 10 9 SWIA200312394 420030907A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07442SW 7609 STALL FAIL CAUTION CAME ON JUST AFTER TAKEOFF. COMPLIED WITH QRH. MESSAGE STILL ON FOR LANDING. A/C HANDLED OK THRU-OUT FLIGHT. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW 27-34-00. OPS CHECK GOOD. S/N OFF: 835. 2L72 4F RTA21EA 20031020001372003102000137EA 2003 10 20 03281657 120031008A3231750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG DOOR INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27657BR 7491 DURING CLIMB CREW RECEIVED A NOSE GEAR DOOR OPEN MESSAGE. CREW RETURNED TO FIELD AND LANDED UNEVENTFULLY, NO EMERGENCY WAS DECLARED. PASSENGERS WERE DEPLANED AT GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NOSE GEAR SELECTOR DOOR VALVE. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030916000372003091600037NM 2003 9 16 C1HA200394016 120030717A3260 WARNING LIGHT BOEING727 727290 138408WNM MLG DOOR ILLUMINATED A C1HAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL15294AS 22146 ON GEAR EXTENSION ALL DOOR LIGHTS ILLUMINATED ALONG WITH TAIL SKID LIGHT. GO AROUND INITAITED. ON SECOND GEAR EXTENSION ALL LIGHTS AND INDICATIONS NORMAL - COULD NOT DUPLICATE. 2L73 4F A3WE 20040115001182004011500118NM 2004 1 15 03FDEA02095 120031207A1430NAS10805 COLLAR DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363PL. LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20040114001462004011400146NM 2004 1 14 DLM88031074 120031209A53305936004503 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27952DL 49883 THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED. THE CORROSION WAS REMOVED WITH A 4 X 7 INCH CUTOUT THROUGH BOTH LAYERS. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385988-14, REV A. 2L72 4F RTA6WE 20040115000232004011500023NM 2004 1 15 03FDEA02038 120031203A5320 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25276FE 22041 CORROSION ON STRINGER CLIP AT BS 540, STR 28L. REMOVED CORROSION ON STRINGER CLIP AT B.S. 54O STR 28L. FOUND OUT OF LIMITS. REPLACED STRINGER CLIP PART 65-45313-6 ALL WORK DONE IAW SRM 51-30-2, SRM 53-10-1, SRM 51-30- 5, SRM 51-30-6. 2L73 4F RTA3WE 20031126000512003112600051WP 2003 11 26 03FDEA01978 120031124A2752AMB7252502 ATTACH FITTING DOUG DC10 DC1010 3022110WP T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 REMOVE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING STEP'S 1 THRU 8 RIGHT SIDE. REMOVED FLAP ACTUATOR AND INSTALLED IAW MM 27-52-01-2 AND ACCOMPLISHED EO 8-5720- 7-2302 STEP NR 1 THRU NR 8 RIGHT SIDE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING REPLACEMENT. 2L73 4F A22WE 20031126000532003112600053NM 2003 11 26 QXEA200301471 120031120A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM AFT LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09407QX 4049 PDX- AFT AIRSTAIR IS DIFFICULT TO SLIDE. CLEANED AND LUBED AFT AIRSTAIR SLIDE ASSEMBLY. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031203001562003120300156NM 2003 12 3 AALA20031136 120031012A3350 BATTERY DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219630A 53561 DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT AFT SERVICE DOOR. SECURED DISLODGED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20031204000692003120400069NM 2003 12 4 03285452 120031012A3350321431 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27452FJ 3214 DURING INSPECTION THE FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FORWARD EMERGENCY BATTERY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031208001692003120800169 2003 12 8 AWXA200301331 420031027A3460 COMPUTER AIRBUSA319 A319132 3930340NM FLT MANAGEMENT MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TOTAKEOFF 1 WP28833AW 1844 AT POWER UP FOR TAKEOFF AT RNO EN ROUTE FOR PHX REJECTED TAKEOFF AT 10-15 KTS DUE TO ASYMMETRIC THRUST CONDITION. NR 1 ENGINE WAS AT TOGA THRUST AND NR 2 ENGINE AT 1.1 EPR, NO ECAM WARNING DISPLAYED. MAINTENANCE RESET FLIGHT MANAGEMENT GUIDANCE COMPUTERS 1 & 2, PERFORMED FULL TOGA ENGINE RUN UP, EPR BOTH ENGINES NORMAL. 2L72 4F RTA28NM 20031209002282003120900228EU 2003 12 9 MALA030483 120031027A3230D49410001 CONTROL UNIT SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAL ABORTED APPROACH P NO WARNING INDICATION LDLANDING 1 GL15435XJ 340B435 DURING FLIGHT 3328, THE LT MLG GREEN LIGHT DID NOT ILLUMINATED WHEN THE GEAR WAS EXTENDED FOR LANDING. PUT GEAR DOWN AND LEFT MAIN GREEN LIGHT DIDN'T COME ON, BUT TRANSIT LIGHT WAS OUT. CREW WENT AROUND AND TRIED AGAIN, AND AGAIN. LEFT MAIN GEAR LIGHT DID NOT COME ON. CHANGED THE BULB AND TRIED AGAIN BUT STILL NO LIGHT INDICATION. TRIED ONE MORE TIME AND GOT 3 GREEN, NEVER GOT THE TRANSIT LIGHT TO GO OUT. MAINTENANCE REPLACED LT LANDING GEAR CONTROL UNIT IAW AMM 32-31-5. P/N ON/OFF D494-10-001, S/N ON 149/09-86, S/N OFF 646/09-97. ALSO NO FLASHED CANNON PLUG 5GA-P1 AND GEAR DOWN SWITCH. CYCLED GEARS 15 TIMES, ALL CHECKS GOOD IAW AMM 32-30-00-5. 2L72 4T RTA52EU 20031209002512003120900251NM 2003 12 9 UPS03241536 120031010A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE: C, NLG WW BS 243 ROW OF RIVETS BELOW RT FWD PRESSURE PANEL HAVE CRACKS. HFEC CORFIRMED CRACKS, AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC COFIRMS NDF ON CUTOUT, REPAIRED IAW SRM 51-40-2 FIG 1. 2L73 4F A3WE 20031210002182003121000218NM 2003 12 10 UPS03441540 120031108A3350900835A BATTERY PACK BOEING747 747200 1384847NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE :AS BOTH UPPER DECK SERVICE DOOR UPPER SILL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSY. RELAMPED AS REQUIRED IAW 33-00. 2L74 4F RTA20WE 20031210002222003121000222WP 2003 12 10 UPS03841552 120031019A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 REPAIR DOUBLER INSTALLED WITH ALL BLIND FASTENERS ON FUSELAGE LOWER SKIN AT STATION 35 AT LONG 32R REMOVED EXISTING DOUBLER, CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20030918000492003091800049NM 2003 9 18 DL738030704 120030729A3350 FUSE BOEING737 737832 13844CFNM EMERGENC LIGHTS BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO273754A 29626 EMERGENCY FLOOR LIGHTS INOP ROW 4 TO 15. REPLACED FUSE AT PWR SUPPLY M1676 2L72 4F RTA16WE 20030923001192003092300119WP 2003 9 23 DHL2003604707 120030228A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT INNER WING CENTER EXTENDED L/E UPPER SKIN CORRODED AROUND STA. XFS.341.500 TO XOLDI 6.2246. REMOVED FASTNERS. REMOVED CORROSION FOUND OUT OF LIMITS. TRIMMED OUT CORRODED AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.071) AND SIX FILLERS (7075-T6 AL0.063) IAW EODHL-030543, ED-3388. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLERS AND FILLERS ON LT INNER WING CTR. EXTENDED LE UPPER SKIN AROUND STA. XFS. 341.500 TO XOLDI 6.2246 USING NEW FASTENERS. 2L74 4F RT4A25 20040129000052004012900005EA 2004 1 29 COMA0360576 120031227A5315601R350313 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01956CA19994 7105 THE FLOORBEAM CAP BETWEEN FS 559+12 TO FS 620, LBL 27 WAS CORRODED. REMOVED THE CORRODED FLOORBEAM CAP AND INSTALLED A NEW BEAM CAP IAW WVAC EO 601R-53-4501. 2L72 4F RTA21EA 20030729001402003072900140WP 2003 7 29 ABXA030233 120030610A532099576646N INTERCOSTAL DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 FORWARD LOWER CARGO DOOR LOWER AFT STOP FITTING INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20030417000412003041700041SO 2003 4 17 SWIA200311735 120030124A5753 ROLLER EMB 120 EMB120ER 3260203SO RT TE FLAP BROKEN A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07251YV 120251 RT OUTBOARD FLAP HAS A BROKEN HINGE ROLLER ON INBOARD END OF CAVITY COVER. REPLACED AND SECURED HINGE ROLLER ON INBOARD END OF FLAP CAVITY COVER FOR OUTBOARD RIGHT FLAP. 2L72 4T RTA31SO 20030423000212003042300021SW 2003 4 23 AUS20030236 120030224A27522736053003 ACTUATOR SWRNGNSA227 SA227* SW TE FLAPS WORN W O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 AUS 3135 (AUS) LT AND RT FLAP ACTUATOR BRUSHES AND BEARINGS WORN. FLAP CONTROLAND FOLLOW UP POTENTIOMETERS FAULTY. 2L72 4T RTA5SW 20030423000832003042300083EU 2003 4 23 BAQA085899 120030402A3150B19030GB03 DISPLAY UROCOPEC135 EC135T1 5620026EU COCKPIT FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME1680 0143 NR 2 LANE FAILURE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20030327000942003032700094SO 2003 3 27 C2XA03BT042 120030317A3350 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2719554 145587 EMERGENCY EXIT SIGN ON THE STEP INTO COCKPIT INOP. REPAIRED BROKEN WIRE. OPS CHECK GOOD IAW EMB145AMM 20-00-00. 2L72 4T RTT00011AT 20040324000022004032400002WP 2004 3 24 ASAA0380711 120031103A5321493653711 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FLIGHT DECK FLOOR PANEL FASTENERS AND WASHERS ARE CORRODED AT FS 155. REPLACED DAMAGED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20030717000062003071700006SW 2003 7 17 HEEA087983 120030701A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149810618 36003 MAIN ROTOR BLADE HAS A HOLE NEAR MID SPAN TAB. SHOP REPAIR. 1G72 4U H4SW 20040223000322004022300032SO 2004 2 23 FFK2004F00001 120031117A2432G35 BATTERY PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO NOSE BAG AREA UNSERVICEABLE B FFKRO OTHER O OTHER NRNOT REPORTED 1 SO0588WA 347570274 DURING AIRCRAFT STARTUP PILOT HAD HARD TIME STARTING THE ENGINES. AFTER TRYING FOR A FEW MINUTES WITH NO SUCCESS, PILOT WENT TO GET THE GROUND POWER UNIT, UPON RETURNING THE AIRCRAFT BATTERY HAD CAUGHT FIRE MELTING SOME FIBERGLASS AROUND THE BATTERY BOX AND THE TOP OF THE NOSE BAGGAGE AREA AND SOME ELECTRICAL WIRING. FIRE WAS EXTINGUISHED AND NO FURTHER DAMAGE WAS DONE TO THE AIRCRAFT. DUE TO THE COLD TEMPERATURE AND POSSIBLY WEAK BATTERY, IT OVERHEATED. 1L72 3O3 O A7SO E9CE 20030829000582003082900058WP 2003 8 29 DHL2003801088 120030723A2510 MECHANISM DOUG DC8 DC873F 302199FWP F/O SEAT LACK OF LUBE A DHLAO OTHER O OTHER TOTAKEOFF 1 SO01801DH 46033 F/O'S SEAT SLIDES BACK ON T/O, NOT LOCKED IN PLACE. CLEANED F/O'S SEAT TRACK LOCK PIN HOLES, AND LUBRICATED SEAT LOCK PIN MECHANISM PER M/M 12-84-1. F/O'S SEAT OPS CHECKED GOOD. 2L74 4F RT4A25 20030829000742003082900074NE 2003 8 29 NACA20030094 220030717A8530356994 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE FAILED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL031377K509 509 44596 P33921 NR 2 ENGINE BACKFIRING & RUNNING ROUGH. REPLACED NR 13 CYLINDER DUE TO EXHAUST VALVE SPRING FAILURE. 2L74 4R4 R 6A3 5E8 20030722001332003072200133NM 2003 7 22 AWXA200300660 120030517A53126516300 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 1.0, WL 192. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT RBL 1.0, WL 192 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08 PG 213. 2L72 4F RTA16WE 20030728000022003072800002 2003 7 28 SWAA031589 420030717A2565D31354 SLIDE BOEING737 7373H4 1384600NM SERVICE DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030728000472003072800047NM 2003 7 28 SWAA031604 120030720A3350300432 LIGHT BOEING737 7373H4 1384600NM EXTERIOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20030812000442003081200044NE 2003 8 12 HEEA088403 120030802A62207610608000050 DAMPENER SKRSKYS76 S76A 8143006NE MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW034253S 760035 MAIN ROTOR DAMPENER LEAKING. SHOP REPAIR. 1G72 3U H1NE 20030813000882003081300088NM 2003 8 13 2003UALA00488 120030607A3260 WARNING HORN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE MLG ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29217UA 30550 RED MAIN GEAR STEERING INDICATION AND WARNING HORN OCCURRED DURING TAKEOFF. 2L72 4F4 FRTT0001SE E46NE 20030902000642003090200064EA 2003 9 2 COW2003F00000 120030502A6710269A55753 SUPPORT SCWZER269 269D 8059501EA LYC O360 HIO360* 41514EA IDLER PULLEY FAILED D C0WMO OTHER O OTHER NRNOT REPORTED 1 GL23103WP6665 51573 ON 5/2/03, WHILE ON FINAL APPROACH TO AIRPORT, PILOT HEARD A LOAD EXPLOSION, FOLLOWED BY A LOSS OF ENGINE TACH. PILOT INITIATED AUTOROTATION TO OPEN FIELD ON AIRPORT PROPERTY. ON 5/3/03, DISCOVERED CLUTCH CONTROL SPRING HANGING OVER EXHAUST AND IDLER PULLEY SUPPORT EARS STILL ATTACHED. INVESTIGATOR RETRIEVED PART FOR FURTHER ANALYSIS. 1G71 3U3 O0 4H12 1E10 20030903001412003090300141NE 2003 9 3 2003F00527 220030620A72003044700 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT FAILED A GUUAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO1969547 UE189 PS114408 FLT 9214 - MIA - DURING TAKEOFF JUST AFTER BRAKE RELEASE, AN EXPLOSION WAS HEARD IN THE LEFT ENGINE. ABORTED TAKEOFF. REMOVED LEFT ENGINE. DETERMINED POEWR SECTION HAS MAJOR INTERNAL DAMAGE. REPLCED LEFT ENGINE. ROUTED FAILED ENGINE FOR FURTHER ANALYSIS AND REPAIR. (M) 2L72 4T4 TRTA24CE E26NE 20030905002032003090500203SO 2003 9 5 C2XA03SH296 120030827A532014522226003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715948 145056 SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030904001552003090400155WP 2003 9 4 DHL2003873577 120030630A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 AFT PASSENGER DOOR FWD LOWER JAMB CORNER SHOWS INTERIM REPAIR AT STA 1620.000, L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18 PG 2-4. REMOVED FASTENERS AND INTERIM REPAIR. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER AND TRIPLER. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER AND TRIPLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER AND TRIPLER ON AFT PASSENGER DOOR FWD LOWER JAMB CORNER WITH NEW FASTENERS IAW SRM 53-2-0 FIG 18 PG 2-4, SRM 51-1-15 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20030814000962003081400096NM 2003 8 14 2003UALA00583 120030721A2497 WARNING LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 1 IDG INOPERATIVE A UALAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 WP29796UA 26931 NR 1 ENG IDG DRIVE LIGHT INOP, IDG OIL LEVEL BLANK AND NO AMBER INDICATION ON SYNOPTIC. FOUND WIRE HARNESS W0623 CHAFFED AT SEVERAL CLAMP LOCATIONS. REPLACED WIRE HARNESS AND OIL LEVEL INDICATION REMAINED BLANK. FOUND IDG INTERNAL CHARGE PRESSURE SWITCH FAILED OPEN AT PINS 10 AND 11 CONNECTOR DM24001C. REPLACED IDG. 2L72 4F4 FRTT0001SE E46NE 20030825001282003082500128SO 2003 8 25 C2XA03BT081 120030813A32221170C000001 STRUT EMB 145 EMB145ER 3260211SO NLG STICKS A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27139298942 7104 145009 EWR---CO2049, CREW REPORTED, "ON LIFT OFF, RECEIVED AIR/ GROUND FAIL MESSAGE ON EICAS. GEAR WOULD NOT RETRACT. MESSAGE DID NOT GO AWAY. RETURNED TO NEWARK." MAINTENANCE TROUBLESHOT AND FOUND NOSE LANDING GEAR STRUT STICKING. SERVICED STRUT IAW EMB145 MM 32-20-01, OPS. CHECKED GOOD ON GROUND, REQUESTED TEST FLIGHT TO VERIFY REPAIR. AIRCRAFT TEST FLOWN SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030825001472003082500147NM 2003 8 25 AALA20030672 120030616A2421 IDG BOEING767 767323 1385205NM RT ENGINE MALFUNCTIONED A AALAK NONE J WARNING INDICATION CLCLIMB 1 SW21371AA 25198 SFO - FLT 310 - RIGHT IDG DRIVE LIGHT FLICKERED ALMOST CONSTANTLY. IN CLIMB, EICAS GEN DRIVE LIGHT FLASHED ON SEVERAL TIMES BUT ALWAYS WENT OUT PRIOR TO IDG DISCONNECT. PROBLEMS SEEMED OT BE ASSOCIATED WITH HIGHER CLIMB POWER SETTINGS AT CRUISE, ALL SYSTEMS NORMAL. REMOVED AND REPLACED GARLOCK SEAL. REMOVED AND REPLACED RIGHT IDG PER MM 24-11-01-4. LEAK AND OPS CHECK NORMAL LIGHT CHECKS NORMAL. (M) 2L72 4F RTA1NM 20030825001512003082500151NM 2003 8 25 AALA20030664 120030604A5311 FAILSAFE BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21362AA 24043 AFW - FOUND LOWER MAIN SILL FAIL SAFE CHORD HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCH. REMOVED ALL CORROSION PER 767 SRM. REPLACED BOLT BACB30NN, COUNTERSINK WITH BACB30N, PROTRUDING HEAD. INSTALL BOLTS WET USING BMS 5-95 SEALANT. ROTO-PEEN BLENDED SURFACE. ALODINE AND PRIME BLENDED AREA. (M) 2L72 4F RTA1NM 20030909002092003090900209EU 2003 9 9 BAQA088334 120030806A7720430109910 SENSOR BOLKMS117 BK117A3 5626015EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03391811345 7003 PILOTS REPORTED TEMP SENSOR ASSY TOT SPLITS. POSSIBLE INTERNAL AIR LEAK IN TEMP. COMPENSATOR. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030911001132003091100113NM 2003 9 11 03FDEA01292 120030806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 RT OUTBD FLAP INBD HINGE ( A/C SIDE ) MOST FWD ATTACH HOLES FOUND CORROSION AT INBD AND OUTBD BORES. RT WING OUTBD FLAP ( A/C SIDE ) I/B HINGE FWD ATTACHMENT I/B AND O/B HOLES REPAIRED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20030925000882003092500088EU 2003 9 25 2003F00584 120030812A243240711 BATTERY FOKKERF27 F27MK600 4990706EU RT/LT OVERHEATED A COEAA UNSCHED LANDING M OVER TEMP CRCRUISE 1 NM13729FE 10385 APPROX 65 NM FROM SITKA, BATTERY OVERTEMP ILLUMINATED IN FLIGHT. CREW ELECTED TO DIVERT TO JUNEAU WHERE MAINTENANCE WAS AVAILABLE. LANDED UNEVENTFULLY. JNU MAINTENANCE REMOVED AND REPLACED BOTH BATTERIES. AIRCRAFT RETURNED TO SERVICE. COMPANY INITIATED A FLEET CAMPAIGN DIRECTIVE TO MEASURE BATTERY CHARGING VOLTAGE ON ALL FOKKER AIRCRAFT. THIS ACTION DID NOT INDICATE A PROBLEM. THESE NI CAD BATTERIES DO NOT HAVE A DEDICATED CHARGER. BATTERIES ARE CHARGED DIRECTLY OFF THE DC BUS. THE COMPANY BATTERY SHOP IS NOW SUBJECTING NEWLY SERVICED BATTERIES TO AN EXTENDED CHARGE, TO DETECT CELL BARRIER DAMAGE. (M) 2H72 4T A817 20030930000282003093000028NM 2003 9 30 03FDEA01462 120030908A574365863891 TEE FITTING BOEING727 727200 138407ENM MLG GOUGED A FDEAK NONE N FALSE WARNING ININSP/MAINT 1 SO25233FE62581 21327 RT MLG I/B FORWARD TRUNNION MOUNT FITTING GOUGED. REPAIRED FORWARD TRUNNION MOUNT IAW FEDEX EA 7-5740-54980 DATED 09/17/03. REFERENCE SNRM N00419 / WO 00023911 2L73 4F RTA3WE 20031001001102003100100110NM 2003 10 1 03272416 120030929A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27416FJ 3171 DURING INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED A SATISFACTORY OPERATIONAL CHECK AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2H72 4T RTA55NM 20031002001532003100200153NM 2003 10 2 03FDEA01518 120030911A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CORROSION ON FLOORBEAM UPR FLANGE UPR SURFACE STA. 1010 RBL 25-45 WL 208. 2L73 4F RTA3WE 20031001000062003100100006NM 2003 10 1 QXEA200301074 120030827A5230 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 CARGO DOOR EXTERIOR SKIN PATCH HAS A GOUGE 1.0 INCH BY .250 INCH BY .017 INCH DEEP. REPAIRED IAW DHC-8 SRM 51-20-16, 51-40-00, RD 8-52-021 AND HORIZON AIR EA 2-52-183. 2H72 4T RTA13NM 20031003000162003100300016NM 2003 10 3 AALA20030940 120030902A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 EMERGENCY EXIT ILGHTS INOPERATIVE AT ROW 32AB. BATERY PACK FAILED DUAL FEED CHECK. RECONNECTED LOOSE CANNON PLUG AT SEAT 32AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031003000372003100300037EA 2003 10 3 ASOA03424 120030908A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE FUSELAGE SKIN AT THE AUXILIARY POWER UNIT INLET, FS 654.50 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE SKIN AT THE AUXILIARY POWR UNIT INLET, FS 654.50 IAW ASA EO 600-53-0121. (M) 2L72 4F RTA21EA 20031006000712003100600071CE 2003 10 6 AMWA45 120030907A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07159YV UE159 RIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-37 AND STRG P/N 101-640000-39 (2EA CRACKS ON THIS RIB). 2L72 4T RTA24CE 20031021002542003102100254SO 2003 10 21 C2XA03SH343 120030922A532014521725615 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 DURING C CHECK THE RIGHT HAND SILL BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MIANTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031022000142003102200014WP 2003 10 22 MWEA030389 120030922A534799578551 SEAT TRACK DOUG DC9 DC981 3022081WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 FIRST OFFICERS SEAT TRACK (FORWARD INBOARD) HAS WORN AREAS. FABRICATED AND INSTALLED NEW SEAT TRACK. 2L72 4F A6WE 20031029000872003102900087NM 2003 10 29 USAABB03174 120030923A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19622AU 27201 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 5, 18, 26, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA2NM 20031029000722003102900072NM 2003 10 29 ASAA0340096 120030228A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE AT BS 727D LBL 2 AND WL 159. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031103001212003110300121EU 2003 11 3 AWXA200301118 120030926A5320D5348004820100 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON A SHAPE SILL AT THE R-2 DOOR FRAME 67. MAINTENANCE REMOVED AND REPLACEDSHAPE SILL AT R-2 DOOR FRAME 67 IAW A320 SRM 51-42-11 PG 21-22 FIG 8 AND SRM 51-44-11 PG 19-20 AND SRM 51-42-11 PG 8-12 FIG. 2 AND 3. 2L72 4F RTA28NM 20031112000282003111200028SO 2003 11 12 C2XA03TY179 120031016A531514521715003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713994 145291 DURING A SCHEDULED 2C INSPECTION THE RT FLOORBEAM TOP PLATES AT FR 20 AND FR 22 WERE CORRODED AT THE NUT PLATE HOLES. MAINT INSTALLED THE RT FLOORBEAM TOP PLATES AT FR.20 - 22. IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. AT COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20031107001162003110700116NM 2003 11 7 ASAA0310435 120030512A5320BAC1509100146 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 879, RIGHT BUTTOCK LINE 8 CORRODED. CUTOUT DAMAGE AND REPAIRED FLOOR SUPPORT PER SRM. (M) 2L72 4F A16WE 20031120000862003112000086 2003 11 20 MEX2003466 420031005A3415 PITOT TUBE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE AIRSPEED OBSTRUCTED W ASMFA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW23158PL 49761 AIRCRAFT RETURN OF FLIGHT DUE TO LEFT VELOCIMETER WAS OUT OF SERVICE. DURING REVISION WAS DETECTED THAT THE PITOT TUBE WAS OBSTRUCTED BY A BEE. PITOT TUBE WAS BLOW IAW MM 34-11-02, TEST IN GROUND WERE CORRECT. 2L72 4F4 FRTA6WE E2EA 20031124000022003112400002NM 2003 11 24 QXEA200301453 120031104A1430 RIVET DHAV DHC8 DHC8202 2809007NM ZONE 300 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX- BROKEN RIVET ON LEFT HAND SIDE OF VERTICAL STABILIZER ALONG TOP EDGE, MID POINT OF STABILIZER. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20040112002442004011200244WP 2004 1 12 AALA20031485 120031230A2720 RUDDER DOUG DC9 DC982 3022082WP TAIL MALFUNCTIONED A AALAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 SW21242AA 49255 DFW T497/30 ON LANDING DFW, RUDDER TRAVEL UNRESTRICTED, LIGHT DID NOT ILLUMINATE. SPEED WENT BELOW 140 KTS AND STILL NO LIGHT. GO-AROUND WAS ACCOMPLISHED DUE TO CROW-WIND LIMITATIONS OF 12 KTS. ON SECOND APPROACH LANDING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AREA DOWN RUDDER MECHANISM FOR CONDITION AND SECURITY. SYSTEM GROUND CHECKED NORMAL OPERATION. UNABLE TO DUPLICATE. 2L72 4F A6WE 20031217000502003121700050WP 2003 12 17 DHL2003805538 120030728A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING OTBD L/E FRAME CRACKED 0.500 AT STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. REFER TO N/R 0249 FOR LEFT OUTER WING OUTBD L/E REMOVAL/REINSTALLATION. 2L74 4F RT4A25 20031217001372003121700137EA 2003 12 17 03341648 120031207A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA OVERWING LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27648BR 7406 DURING INSPECTION THE LT OVERWING EXIT LIGHT WAS FOUND INOPERATIVE. THE POWER SUPPLY ASSEMBLY WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031217001822003121700182 2003 12 17 MALA030504 420031122A34206225812001 DETECTOR SAAB SF340 SF340A 7850100EU COCKPIT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1579XJ 340A079 DURING FLT, YELLOW HEADING FLAG REPEATEDLY CAME ON, COULD BE FAILURE ON BOTH SIDES. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 2 FLUX DETECTOR UNIT P/N 622-5812-001, S/N ON 29146, S/N OFF 10863. PERFORMED COMPASS SWING PROCEDURE IAW 34-21-00, ALL CHECKS GOOD. 2L72 4T RTA52EU 20031219000392003121900039EA 2003 12 19 SWIA200312641 120031127A2750601R930507 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07962SW 7859 FLAPS FAIL MESSAGE INFLIGHT WITH FLAPS SELECTOR AT 8. FOLLOWED QRH AND LANDED FLAPS 8. REMOVED AND REPLACED FECU IAW CRJ MM 27-50-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20031223000462003122300046NM 2003 12 23 SWAA032667 120031205A531096380 BEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND STUB BEAM INBOARD CHORD CORRODED AT BS 616, LBL 65. REPAIRED BEAM PER SRM AND BOEING SB. 2L72 4F RTA16WE 20031223000722003122300072SO 2003 12 23 C2XA03BT116 120031209A3350 CONNECTOR EMB 145 EMB145 3260210SO CABIN DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715973 145159 CREW REPORTED, EMERGENCY LIGHT INOPERATIVE ON SIDE WALL OF CABIN. MAINTENANCE RESECURED CONNECTOR TO THE EMERGENCY LIGHT AND OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20031223001072003122300107NM 2003 12 23 QXEA200301543 120031206A5720 ATTACH FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 LEFT HAND OUTBOARD FLAP NR 4 CARRIAGE FRONT SPAR ATTACH BRACKET INBOARD FITTING AND OUTBOARD LUG IS CHAFED. REPAIRED IAW Q400 RD 8/4-57-228. 2H72 4T RTA13NM 20031223001222003122300122EU 2003 12 23 MALA030532 120031201A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 10D FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 10D IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031229001102003122900110NM 2003 12 29 AWXA200301554 120031125A53126516300 BULKHEAD BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, AFT SIDE, AT RBL 5, WL 200.25 TO WL 201.25. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY CRACK END, STOP DRILLED CRACK, RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08 PG 275, FIG 201. 2L72 4F RTA16WE 20031231000592003123100059EA 2003 12 31 A6WA200340181 120031118A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 TEMPORARY REPAIR ON RT FORWARD FUSELAGE SKIN JUST FORWARD OF FS 202.75 BULKHEAD, DENT 4 INCHES BY .062 INCH DEEP. TEMP REPAIR WAS PERFORMED IAW REO 601R-53-11-327. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 202.75 TO FS 204, BETWEEN STRINGERS 12R AND 13R BY REMOVING TEMPORARY REPAIR, RE-CONTOURING DAMAGED AREA, PERFORMING EDDY CURRENT INSPECTION, INSTALLING THREE RIVETS, APPLYING PROTECTIVE TREAT AND FINISH. (M) 2L72 4F RTA21EA 20031229001462003122900146NM 2003 12 29 UPS03241662 120031212A2611 SMOKE DETECTOR BOEING727 72725C 138400HNM CARGO BAY INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 LOWER CARGO COMPARTMENT SMOKE DETECTION MX LIGHT ON. DISPLAYED ITEM MX MESSAGE SCU (B). PERFORMED MX ISOLATION METHOD FOR SCU (B) MESSAGE IAW 26-19-00. NO DEFECT NOTED OR REPEAT MESSAGE. 2L73 4F A3WE 20031125000772003112500077WP 2003 11 25 DHL2003805551 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 LEFT OUTER WING INBD L/E FORMER CRACKED 0.500 AT STA XFS.578.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040311000542004031100054NM 2004 3 11 ASAA0310105 120030306A5320BAC14902807 STIFFENER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND FRAME REINFORCEMENT CHORD AT BS 947, STRINGER 20R-23R CORRODED. REMOVED DAMAGED SECTION AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20031208000332003120800033CE 2003 12 8 216120203 120031202A2160 CONTROL VALVE LEAR 60 60LEAR 5170707CE FLOW CONTROL DEFECTIVE E CVGAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01216BX 103 SMOKE IN CABIN, FUMES, DECLARED EMERGENCY AND RETURNED TO BED. FOUND FLOW CONTROL VALVE DEFECTIVE. REPLACED FLOW CONTROL VALVE IAW LEAR 60 AMM 21-40-00. 2L72 4F RTA10CE 20031208001152003120800115NM 2003 12 8 AWXA200301313 120031008A53206546592 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT RBL 3, BS 860. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF FLOOR SUPPORT AT RBL 3, BS 860; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53 FIG 201 PG 1. 2L72 4F RTA16WE 20031208001312003120800131NE 2003 12 8 PCAA0310129 320031026A6110 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF7 NE NR 1 PROP OUT OF RIG A PCAAO OTHER J WARNING INDICATION CRCRUISE 1 EA13840EX 327 FLIGHT 3961 INTO DCA, NR 1 PROPELLER WAS UNABLE TO BE REDUCED BELOW 930 RPM IN CRUISE FLIGHT. MAINTENANCE RE-RIGGED NR 1 ENGINE PROPELLER CONTROL UNIT AND GROUND RAN AIRCRAFT, OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP7NE 20031210000052003121000005NM 2003 12 10 03FDEA02077 120031207A1430 COLLAR DOUG MD11 MD11 3023602NM STABILIZER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE FOUND WITH 04 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 4 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II AND REPLACED AS PER SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20040129000262004012900026NM 2004 1 29 AWXA200400013 120031227A53126516300 BEAM BOEING737 7373B7 1384580NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND AT 2 INCH HOLE ON BS 178 BULKHEAD RT VERTICAL BEAM WEB RBL 17.1, WL 192.5. MAINTENANCE CUT OUT DAMAGED AREA ON BS 178 BULKHEAD VERTICAL BEAM WEB RBL 17.1, WL 192.5; FABRICATED A NEW SECTION OF WEB AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08 FIG 212. 2L72 4F RTA16WE 20040202001442004020200144WP 2004 2 2 UPS04841719 120031231A5310 SHEAR TIE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, EXTERIOR FUSELAGE, 4 DENTS IN SKIN OVER BELLFRAMES, AND GOUGES BETWEEN LONG 21L - 24L, FOUND SHEAR TIE CRACKED AT STA 100 BETWEEN LONG 23L AND 24L. CUT OUT DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED SHEAR TIE SECTION AND DOUBLER IAW SRM 53-2-0 FIG 2B. 2L74 4F RT4A25 20040203000622004020300062WP 2004 2 3 ASAA0380599 120031002A33500105603 LIGHT DOUG DC9 DC982 3022082WP ROW 9 INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA PREFLIGHT CHECK, FOUND EMEREGNCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 9 FORWARD. REPAIRED ASSOCIATED JUMPER WIRE TO BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040203001272004020300127SO 2004 2 3 SWIA200312776 120031209A572012061341615 CLIP EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07221SW 120290 LEFT WING 1ST FUEL PANEL OUTBOARD OF NACELLE OUTBOARD CLIP IS CRACKED AT AFT END, RIB 16. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SERVICEABLE CLIP TO LEFT WING 1ST FUEL PANEL OUTBOARD OF NACELLE, OUTBOARD CLIP IAW EMB SRM 51-40-00. 2L72 4T RTA31SO 20040204001252004020400125NM 2004 2 4 EIA2003126 120030928A3350 BATTERY PACK BOEING747 747273C 1384896NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 PILOT REPORTED EMERGENCY LIGHT OVER CREW DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-07 AND LIGHT ASSY IAW MM 33-51-07. OPS CK GOOD. 2L74 4F A20WE 20040217000422004021700042EU 2004 2 17 2004F00068 120030926A5320D53470490000000 PLATE AIRBUS320 A320233 3930329EU FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 SW07951LF 460 AT C-CHECK, FOUND INTERCOSTAL AT AFT CARGO COMPARTMENT FRAME 48 TO 49, LBL 27 WITH SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL PLATE AT AFT CARGO COMPARTMENT, FRAME 48 TO FRAME 49, LBL 27. (M) 2L72 4F RTA28NM 20040301001082004030100108 2004 3 1 RYN2004F00009 420030915A2565D5348015800500 ATTACH FITTING AIRBUS320 A320233 3930329EU GIRT BAR CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY, FORWARD GIRT BAR ATTACH FITTING PLATE, WITH CORROSION. REMOVED AND REPLACED FORWARD GIRT BAR ATTACH FITTING PLATE ON AFT CABIN NR 2 RT DOORWAY. 2L72 4F RTA28NM 20031211000982003121100098NM 2003 12 11 S03453085 120030716A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE CORRODED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 29031 B-18208 FUSELAGE-AFT BELLY SKIN SERIOUS CORROSION BETWEEN BS 1660 AND BS 1680, S-50R, S-51L. REPAIR PER EO 744-53-00-0011. 2L74 4F4 FRTA20WE E24NE 20031215001832003121500183EA 2003 12 15 ASOA03533 120031024A3240M23902988487 PIN CNDAIRCL600 CL6002C10 1390015EA MLG SHORTED A ASOAK NONE N FALSE WARNING CRCRUISE 1 SO11719EV 10099 FLT 4393 - DURING CRUISE FROM ATL-BTR, APPROXIMATELY 31,000 FT, RECEIVED AN AURAL BRAKE OVERHEAT MASTER WARNING AND A BRAKE OVERHEAT EICAS WARNING. DURING DESCENT WHEN THE AIRSPEED SLOWED TO 220 EXTENDED THE MLG AND CONSULTED THE QRH. THE RT INBOARD BRAKE WAS IN THE RED WITH NR NUMBER INCREASING RAPIDLY. WITH THE GEAR DOWN THE TEMP DECREASED AND THEN INCREASED TO TWENTY AND THE BRAKE TEMP MONITORING SYS BECAME ERRATIC. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED SAFELY IN BTR. MAINTENANCE CLEANED EXCESSIVE MOISTURE OUT OF THE BRAKE TEMP SENSOR CONNECTOR AND RESET THE PUSH PIN IN THE TC06P1 AND FOUND PIN A SHORTING AGAINST THE CASE OF THE SENSOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040316000882004031600088WP 2004 3 16 ASAA0380280 120030403A532099512559 BRACKET DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND RIGHT OVERWING TO BODY FAIRING SUPPORT BRACKET IS CRACKED. REPLACED BRACKET PER SRM 51-10-04, 30-2 AND 10-3. (M) 2L72 4F RTA6WE 20040324000092004032400009NM 2004 3 24 ASAA0340342 120031114A5420311A15191112 SUPPORT BOEING737 7374Q8 138447QNM NR 2 NACELLE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01755AS 25096 GYR - DURING SI CHECK FOUND SUPPORT CHORD GOUGED ON NR 2 PYLON AT NAC 166.5 TO 196. REPAIRED IAW EA. (M) 2L72 4F RTA16WE 20040412000132004041200013WP 2004 4 12 ASAA0380733 120031111A532199365582515 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1134-1174. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20030923001162003092300116WP 2003 9 23 DHL2003604664 120030621A5753 PLATE DOUG DC8 DC873F 302199FWP RT WING FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 RT WING INBD FLAP UPPER PLATING SHOWS DENTS AND WEAR OUT OR LIMITS BETWEEN STA XW 104.000 TO XW 115.000. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG.1. CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL ( 2024-T3AL 0.063) AND THREE FILLERS AS INDICATED BELOW, TWO FILLERS OF 2024-T3AL 0.025 AND ANOTHER ONE OF 2024-T3AL 0.016 IAW EO DHL 030567, ED 3385. CLEANED TREATED AND PRIMED THE NEW SKIN PANEL INTERIOR SURFACE AND FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE NEW SKIN PANEL AND FILLERS ON RT WING INBD FLAP UPPER PLATING (STA. XW 104.000 - XW 115.000) USING NEW FASTENERS. 2L74 4F RT4A25 20030814001512003081400151NM 2003 8 14 AALA20030650 120030610A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21601AN 27052 MIA - DUIRNG OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 16D SMASHED. REPLACED EMERGENCY EXIT SEAT LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20030818000302003081800030NE 2003 8 18 HEEA088382 120030716A2400A1077B RELAY SKRSKYS76 S76A 8143006NE DC SYSTEM WILL NOT TEST E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 WILL NOT PASS ERB TEST, DC POWER FALLS OFF LINE. 1G72 3U H1NE 20030818000462003081800046SW 2003 8 18 ALGA088662 120030806A6240407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH MALFUNCTIONED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03557AL 53243 REPAIR DUE TO ROTOR NEEDLE FALLS TO ZERO WHEN THROTTLE IS REDUCED. 1G71 3U O H2SW 20030328000392003032800039SO 2003 3 28 C2XA03TY024 120030210A531014522460013 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE LT OMEGA BEAM AND RAMP ANGLE WERE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA; FAB FILLER, SHIM, EXTERNAL LT RAMP ANGLE IAW EMB 135/145 SRM 53-21-10. ALODINED AND PRIMED IAW EMB 135/145 CPM51-21-04;05. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030821000022003082100002NM 2003 8 21 USAASB03114 120030718A253041600011G COFFEEMAKER BOEING737 737301 1384611NM FWD GALLEY ODOR A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19352US 23555 DURING CRUISE, EN ROUTE FROM DFW TO CLT, THE FLIGHT ATTENDANT REPORTED A BURING RUBBER ODOR IN THE VICINITY OF THE GALLEY COFFEE MAKERS. POWER WAS REMOVED FROM THE COFFEE MAKERS AND THE ODOR DISSIPATED. FLIGHT CONTINUED ONTO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD COFFEE MAKERS, AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030821002382003082100238EU 2003 8 21 RAIA00306177 120030629A793056774098010 GAUGE AEROSPATR72 ATR72202 8680940EU COCKPIT FAULTY A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03722TE19486396 220 5642-STL- LEFT ENGINE NO OIL TEMP AND LOW OIL PRESSURE. MAINTENANCE REMOVED AND REPLACED THE OIL TEMP/PRESS GAUGE. 2H72 4T RTA53EU 20030410001772003041000177NM 2003 4 10 DHL2003741508 120030323A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, BS 680 CIRCUMFERENTIAL DENTED WITH UNFILLED DRILL HOLE BETWEEN STRINGERS 16 LT AND 17 LT. REMOVED FASTENERS IAW B-727 SRM 51-30-2. CUT OUT DAMAGE IAW SRM 53-10-2. FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-10-2 AND 53-10-4 FIG 2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030416000182003041600018 2003 4 16 SWIA200311676 420030101A2350509111 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUDIO SYSTEM MALFUNCTIONED A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07270YV6161 6161 120270 ON TAKEOFF THE CAPTAIN'S AUDIO PANEL FAILED. RETURNED TO LAX. REPLACED CAPTAIN'S AUDIO PANEL WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20030428000252003042800025WP 2003 4 28 GTIA030171 120030306A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 PAX CABIN LT SIDE INBOARD STA 886 TO STA 926, FLOOR PANEL CRACKED. FABRICATED FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20030428000142003042800014EA 2003 4 28 QXEA0300416 120030331A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09609QX 10031 SEA- ON FLIGHT 2467 CHIMNEY IN FORWARD CARGO COMPARTMENT HAS SOME BROKEN MESH. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030430001542003043000154NM 2003 4 30 SWAA030881 120030419A3350100885 POWER SUPPLY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D CHECK, FOUND EEPLS INOP ( 5 EA ) IN AFT CABIN. R&R POWER SUPPLY PER MM. 2L72 4F RTA16WE 20030502001622003050200162NM 2003 5 2 03FDEA00479 120030417A5414 SKIN BOEING727 727200 138407ENM NR 3 NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 NR 3 ENGINE UPPER COWLING LOWER EDGE SKIN SEPARATED, BENT AND CHAFED AT NR 3 FRAME. 2L73 4F RTA3WE 20030507000552003050700055EA 2003 5 7 AUS20030354 220030320A8530SL32006WA20P CYLINDER ROBSINR22 R22MARINER 7640115NM LYC O320 O320B2C 41508EA ENGINE DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 CYLINDER LOW COMPRESSION. 1G71 3O3 O H10WE E274 20030507001712003050700171SO 2003 5 7 HYI2003F00004 220030327A8550535634 PIN CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO OIL PUMP DRIVE SHEARED D HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01548GA167 402C0653 823463 TACHOMETER INOPERATIVE, RT DRIVE GEAR DOWEL PIN BROKE ON OIL PUMP GEAR. REMOVED OIL PUMP HOUSING COVER, REPLACED DRIVE PIN AND REINSTALLED COVER. 1L72 3O3 O A7CE E8CE 20030508001412003050800141EU 2003 5 8 03FDEA00669 120030502A5712A57246814 RIB AIRBUS300 A300B4605R 3930308EU LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25682FE 800 COMPLY WITH E.A. 6-5751-70370 WINGS-FIXED TRAILING EDGE- RIB 7A (LT) GOUGE REPAIR, P/N A572-46814. FACT 02MAY03 12:14 BFM U COMPLIED WITH E.A. 6-5751-70370 WINGS-FIXED TRAILING EDGE-RIB 7A (LT) GOUGE REPAIR P/N A572-46814 AT MAE 2L72 4F RTA35EU 20030513002712003051300271EA 2003 5 13 ASOA03142 120030401A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11907EV 7648 FLT 4414 - DURING A GROUND INSPECTION IN MGM, THE RIGHT WING FORWARD EMERGENCY LIGHT WAS FOND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING FORWARD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030514001412003051400141NM 2003 5 14 SWAA031041 120030509A53306545767 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 4R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030514000532003051400053NM 2003 5 14 SWAA030976 120030430A33506104781 BALLAST BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20030515000892003051500089 2003 5 15 DXTA200300029 420030506A3421 INDICATOR CESSNA500 560CESSNA 2076750CE ATTITUDE MALFUNCTIONED E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07371QS 5600471 DURING TAKEOFF ROLL CAPTAIN'S ATTITUDE INDICATOR INDICATED 5 DEGREES NOSE DOWN WITH 3 DEGREES RIGHT BANK. REJECTED TAKEOFF. FOUND NR 1 VERTICAL GYRO DEFECTIVE. REPLACED UNIT AND OPS CHECKED GOOD. 2L72 4F RTA22CE 20030515000912003051500091EU 2003 5 15 03FDEA00725 120030510A2197 WIRE AIRBUS310 A310 EU TERMINAL BLOCK LOOSE A FDEAA UNSCHED LANDING FW FLT CONT AFFECTED INADEQUATE Q C CLCLIMB 1 SO25419FE 345 AFTER LEVEL OFF AT CRUISE AT FL350, CABIN RATE ECAM WARNING ILLUMINATED. FOLLOWED ECAM STEPS AND QRH PROCEDURES. WAS UNABLE TO CONTROL CABIN ALTITUDE. WHILE LEVEL AND IN MANUAL PRESSURIZATION, CABIN ALT STABILIZED AT 14,900 FT. WITH ALL OUTFLOW VALVES CLOSED. EQUIPMENT COOLING LOW FLOW ILLUMINATED. ECAM ASKED FOR EXTRACT OVERBOARD WHICH INCREASED CABIN ALTITUDE. RETURNED TO SUBIC. CHD GROUND AT PIN 13A AND 13B OF CABIN PRESSURE CTRL 105HM AND 106HM, FOUND BOTH 13A OF 105HM AND 106HM, BLOCK 158VT NR 10 PIN -J- AND NR 1 PIN -B- LOOSE. FIXED AND SECURED TERMINAL BLOCKS PER SMP FOR PRECAUTIONARY. REMOVED AND REPLACED 159GB AND 60GB RELAY SYS 1 AND 2. 2L72 4F RTA35EU 20030604000632003060400063WP 2003 6 4 UPS03840478 120030402A571056168692 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C3, NR 3 FUEL TANK STRINGER 74 STRAP CRACKED STA XRS 22 ACCESS PANEL 506C. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABBED 1 EA FITTING P/ N 5616869-2 FROM 7075-T6511 BAR STOCK PO 334935 IAW DAC 5616869. L OCATED DRILLED DEBURRED IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW D C8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. LEAK CHECK TO BE ACCO MPLISHED ON UPS TASK CARD NO 8000 ITEM 38. 2L74 4F RT4A25 20030605000742003060500074NM 2003 6 5 MEX2003150 120030501A3241426412 CONTROL UNIT BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE ANTI-SKID SYS FAILED W ASMFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23805AM6170 6170 26272 DURING TRANSIT CHECK CAPTAIN REPORTED NORM ANTI-SKID AND ALTN ANTI-SKID MESSAGES IN EICAS. MESSAGE APPEARED EVERY TIME THAT THE PARKING BRAKES WERE USED. FIM PROCEDURE WAS ACCOMPLISHED BUT NO FAILURE CODE APPEARS. AIRCRAFT WAS SENT TO THE HANGAR. ANIT-SKID AND AUTO-BRAKE CONTROL UNIT WAS REPLACED AND TESTS WERE PREFORMED IAW MM. 2L72 4F4 FRTA2NM E17NE 20030520000982003052000098 2003 5 20 USAASA03010 420030128A2565 GIRT BAR AIRBUS320 A320214 3930316EU ESCAPE SLIDE LACK OF LUBE A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19106US6127 1044 LGA - THE L1 DOOR WAS DIFFICULT TO KEEP IN THE ARMED POSITION. MAINTENANCE CLEANED AND LUBRICATED THE GIRT BAR ASSEMBLY AND LOCKING MECHANISM, AND REPLACED THE L-1 DOOR EMERGENCY EVACUATION SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20030609000382003060900038NM 2003 6 9 C1HA200396005 120030519A5347 SEAT TRACK BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 PITTING CORROSION AND GOUGING ON NR 2 SEAT TRACK AT LBL22, BETWEEN BS 480 & 620. 2L73 4F RTA3WE 20030522000242003052200024NM 2003 5 22 2003UALA00416 120030506A2421 WARNING LIGHT BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE LT GENERATOR ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29615UA 21876 A/C RECEIVED LEFT GENERATOR DRIVE LIGHT INDICATION. DISCONNECTED IDG AND FELT VIBRATION. REMOVED AND REPLACE THE LEFT IDG. SHOP FINDINGS SHOW THAT THE UNIT HAD A FAILURE IN THE HYDRAULIC LOG. 2L72 4F4 FRTA1NM E3NE 20030522000482003052200048WP 2003 5 22 GTIA030283 120030414A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 RT FUSELAGE STA 927 TO 946 CUSP WEB CORRODED. CUT OUT DAMAGED WEB SECTION. FABRICATED NEW WEB SECTION AND DOUBLER. INSTALLED NEW WEB SECTION AND DOUBLER. 2L72 4F4 FRTA6WE E2EA 20030609000682003060900068EA 2003 6 9 QXEA0300620 120030517A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 RIVET DAMAGED AT .5 INCHES BELOW BOTTOM EDGE OF ADG DOOR, 15INCHES AFT OF FS169. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8. 2L72 4F RTA21EA 20030611000892003061100089SW 2003 6 11 HEEA086697 120030522A3212412050017135 COVER BELL 412 412 1182202SW EMERGENCY FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 COVER END FLAPS HOOK AND LOOP FABRIC WORN OUT. TO BE SENT TO VENDOR FOR REPAIR. 1G72 4U H4SW 20030611000982003061100098SW 2003 6 11 HEEA086706 120030522A5320 NUT PLATE BELL 412 412 1182202SW STIFFENER BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321498 36003 NUT PLATE BROKEN. SCRAPPED. 1G72 4U H4SW 20030617001512003061700151NM 2003 6 17 QXEA200300708 120030609A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - PROVIDE A PERMANENT REPAIR TO DAMAGED FUSELAGE SKIN STRAP AT STATION X156-X176.00 AT STRINGER 205. REPAIRED IAW HORIZON AIR EA 6-53-259. 2H72 4T RTA13NM 20030612001832003061200183NM 2003 6 12 2003UALA00400 120030524A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE GALLEY INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29675UA 29243 EMERGENCY EEL LIGHT INOP AT LT AFT GALLEY. REPLACED EEL STRIP ASSEMBLY. 2L72 4F4 FRTA1NM E24NE 20030523000382003052300038NM 2003 5 23 DL73G030394 120030425A531265163007 BULKHEAD BOEING737 73735B 13844BMNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27223DZ 23972 THE FS 178 BULKHEAD WEB WAS FOUND WITH 3 TYPICAL CRACKS, 1 AT LBL 5.7 & WL 200, 1 AT RBL 5.7 & WL 200, AND 1 AT RBL 5.7 & WL 211. THE CRACKS ARE TYPICAL OF AD 2000-05-29 AND BAC S/B 737-53A1173. THE CRACKS WERE REPAIRED WITH ALUMINUM REPAIR DOUBLERS PER THE BAC 737 SRM AND PER ER/A 384881-14AD. 2L72 4F RTA16WE 20040122000502004012200050EA 2004 1 22 ASOA03641 120031211A5260601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11908EV 7654 DURING A C-CHECK, THE TOP STEP PANEL ASSEMBLY OF THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP PANEL ASSEMBLY ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20031015000702003101500070NM 2003 10 15 AMTA200301242 120030930A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11524AT 30233 FORWARD CABIN EMERGENCY FLOOR PATH LIGHTING FRONT FOUR LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD 2 FULL LENGTH LIGHT ASSEMBLIES. OPS CHECKS GOOD REF MM 33-51-11-3. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20031211000282003121100028WP 2003 12 11 ABXA030431 120031027A523059101419 PAN DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 FORWARD LOWER CARGO DOOR WAS CRACKED IN OUTER PAN AROUND HI-LOK AT FORWARD LOWER STOP. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM. 2L72 4F A6WE 20030916000082003091600008NM 2003 9 16 S03J25023 120030523A2530JD001005 COFFEEMAKER BOEING747 747400 NM GE CF6 CF680C2* GL GALLEY ODOR W SAJFO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP03 37067 WHITE SMOKE AND BURNING ODOR COMING FROM GALLY HOT POT AREA. HOT POT REMOVED AND ALL CB IN GALLY PULLED, SMOKE DISAPPEARED IMMEDIATELY. GROUND CHECK FOUND HOT POT MALFUNCTION GOT WHITE SMOKE AND BURNING ODOR. INFORM CPCS TO REPLACE HOT POT AND FOR MAINT PRECAUTION HOT POT RECEPTACLE REPLACED . HOT POT FUNCTION TEST NORMAL AND GALLEY HOT POT AREA CONDITION CHECK NORMAL. 2L74 4F4 FRTA20WE E23EA 20040206000012004020600001SW 2004 2 6 11280376 120031128A7603C810242 CONTROL CABLE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCB3T HCB3TN5 GL ZONE 400 CHAFED E D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW17228AM33082166 TC300 P54062 BVA7662 DURINE TAKE OFF PREP, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWER LEVER CABLE HAD BROKEN INSIDE THE CABLE HOUSING IN THE ENGINE COMPARTMENT. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20040217001882004021700188CE 2004 2 17 2004F00002 120031231A2750262228112 BELLCRANK CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE TE FLAPS CRACKED G K NONE O OTHER ININSP/MAINT 1 AL05331AK1196 208B0739 WELDS ARE CRACKED AND/OR MISSING IN THE TUBE TO ARM WELD AREAS AS DEPICTED IN SB PAGE 14, DETAIL B OF MFG SB CAB 03-11 AND IAW ASSOCIATED AD FOR THE CARAVAN. AREA 1 WELD HAS CRACKS. AREA 2 HAS WELDS MISSING. DETAIL C, AREA 3 WELDS MISSING. THIS PART WAS BEING INSPECTED IAW SB WHEN FOUND. TOTAL PART HOURS 1196.7 TOTAL LANDINGS 3321. SAFETY ISSUE. 1H71 3T3 T A37CE E4EA 20040301000752004030100075WP 2004 3 1 AAL2004F00004 120031003A5711 SPAR CAP DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RT WING DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21411AA 49322 RT WING REAR SPAR LOWER CAP DAMAGED (GROUND DAMAGE). INSTALLED SERVICEABLE LOWER CAP DOUBLER AND FILLER IAW ESO 80559. 2L72 4F4 F A6WE E2EA 20040316000912004031600091WP 2004 3 16 ASAA0380315 120030414A532059133161 BRACKET DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - FOUND DURING 15K CHECK, RUDDER YAW DAMPNER ACTUATOR ATTACH BRACKET CORRODED. REPLACED BRACKET PER MM 20-30-01. (M) 2L72 4F RTA6WE 20040316000982004031600098WP 2004 3 16 ASAA0380359 120030418A21205910090137 PLENUM DOUG DC9 DC983 3022083WP RT HEAT EXCHANGEWORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND RIGHT HEAT EXCHANGER PLENUM AREA WORN THROUGH DUE TO RUBBING ON EXIT DUCT. CUT OUT DAMAGED AREA AND WELDED IN A DOUBLER PER DRS 10.225. (M) 2L72 4F RTA6WE 20031211001822003121100182NM 2003 12 11 USAABB03196 120031024A335086210066 BATTERY BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19626AU 27303 LAX - ALL TEN FLOOR EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED ALL OF THE BATTERIES. (M) 2L72 4F RTA2NM 20040413000502004041300050NM 2004 4 13 ASAA024016G 120030322A5320654769010 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORRSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727F TO 837. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040930000882004093000088EU 2004 9 30 A6WA200360070 120031212A5313 STRINGER BAC 146 146200A 1500266EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND STRINGER 34R HAS CORROSION. MAINTENANCE REPAIRED STRINGER 34R BETWEEN FRAMES 20B AND 21 IAW BAE FAX BARA/AVR/6609/03-DC AND IAW BAE SRM 51-43-00. (M) 2H74 4F A49EU 20060801000192006080100019WP 2006 8 1 IXXA060513S 120030121A5330 DOUBLER DOUG DC8 DC871F 302199DWP ZONE 100 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX826872760 46065 DURING ROUTINE C CHECK, FOUND AIR START DOOR CUTOUT DOUBLER GOUGED. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-8, 51-1-21 AND DOUGLAS DRAWING NUMBER 5614438. 2L74 4F RT4A25 20030815000642003081500064SW 2003 8 15 HEEA088461 120030713A6420212011701101FM1 ROTOR HEAD BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D5162 33076 TAIL ROTOR HEAD HAS WORN FEATHERING BEARINGS. REPAIRED. 1G72 4U H4SW 20030819002162003081900216NM 2003 8 19 2003UALA00579 120030719A3350M1137 CHARGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29346UA 24250 EEL INOP FROM ROW 15 TO AFT EXIT DOOR. REPLACED AFT LT BATTERY PACK, CHARGER AND EEL LIGHT CABLE FROM ROW 16 TO AFT DOORS. 2L72 4F4 FRTA16WE E2GL 20030820001692003082000169NM 2003 8 20 CALA0300380 120030712A5230 SKIN BOEING737 737524 1384721NM AFT CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711641 28902 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED 39 INCHES FROM FORWARD EDGE AND 19 INCHES FROM TOP. REPAIRED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030331001232003033100123NM 2003 3 31 DHL2003740503 120030204A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FUESLAGE UPPER MAIN DECK CARGO DOOR FUSLAGE FRAME 480 CRACKED FWD SIDE WHERE ATTACH TO FUSELAGE SKIN. CUT OUT DAMAGED FLANGE AND FABRICATED REPAIR FROM 7075-T6 AND FILLER FROM 7075-T6 .063 PER SRM 53-10-4 FIG 1. PARTS TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-4, FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20030403000432003040300043NM 2003 4 3 AMTA200300259 120030223A3350 FUSE BOEING757 75723N 1384973NM POWER SUPPLY BLOWN A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11524AT 30233 ROW 23 EMERGENCY EXIT AISLE LIGHT INOPERATIVE. REPLACED POWER SUPPLY FUSE AT POWER SUPPLY M733 PER 33-51-07-2. OP SCHECK GOOD AT THIS TIME. (M) 2L72 4F RTA2NM 20030414000282003041400028NM 2003 4 14 SWAA030736 120030401A32106546113 PIN BOEING737 7373H4 1384600NM LT MLG TRUNNION CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C1 CHECK, FOUND LT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED LT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20030430000172003043000017EU 2003 4 30 AWXA200300452 120030331A5320D53230256201 ANGLE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1/4 INCH CRACK WAS FOUND ON ATTACH ANGLE AT AFT UPPER CORNER OF PANEL 192AB ATTACH POINT FR 34, STR 31 R/H. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ANGLE PER DWG C3 D53230256; INSTALLED REPAIR PART IAW AWA E.R. 26-5336-03113-SS1. 2L72 4F RTA28NM 20030429001732003042900173NM 2003 4 29 CA030321005 120030314A3210467065 BRACKET BOMBDRDHC8 DHC8400 NM PWC 150 PW150A EA LT MLG BROKEN W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER TAKE-OFF FROM BASE THE MLG WAS SELECTED UP, THE NLG AND RT MLG RETRACTED NORMALLY, BUT THE LT MLG DID NOT ACHIEVE AN UP AND LOCKED STATUS MLG WARNING LIGHTS ON AND LT MLG DOORS REMAINED OPEN. THE AIRCRAFT MADE A NORMAL LANDING AT NEXT BASE.INSPECTION OF THE LH MLG REVEALED THAT THE LT LOWER STRUT FAIRING ASSY ALONG WITH FAIRING ATTACHMENT BRACKET HAD SEPARATED FROM ITS UPPER ATTACHMENT POINT AND WAS BENT REARWARDS AND DOWN. IT WAS ASCERTAINED THAT THE REASON THAT THE LH MLG DID NOT FULLRETRACT WAS THAT THE SEPARATION AND RELOCATION REARWARDS OF THE LH LOWER STRUT FAIRING ASSY PREVENT ED THE MLG UPLOCK HOOK FROM ENGAGING THE UPLOCK ROLLER. THE LT LOWER STRUT FAIRING ASSY WAS REMOVED FROM THE LANDING 2H72 4T4 TRTA13NM E00062EN 20030430000072003043000007NM 2003 4 30 QXEA0300491 120030411A5350 FAIRING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - WING TO FUSELAGE FAIRINGS, PANEL 261CT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451. 2H72 4T RTA13NM 20030430001392003043000139NM 2003 4 30 SWAA030910 120030423A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 4 EA ) AT BS 616 AT STR 4R, BS 727D AT STR 8R, BS 500B AT STR 4R & BS 520 AT STR 8R. R&R STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030502000672003050200067WP 2003 5 2 ASAA0380179 120030301A52505926003511 DOOR DOUG DC9 DC982 3022082WP CARGO BARRIER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND FORWARD CARGO BAY BARRIER DOOR IS CRACKED. REPAIRED CRACKS WITH BONDED 7075-T6 FILLER AND DOUBLER PER SRM 51-70-2. (M) 2L72 4F A6WE 20030506000802003050600080NM 2003 5 6 03FDEA00584 120030423A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FRAME BS 720C, LBL 4 - RBL 4, WL 148. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20030508000842003050800084NM 2003 5 8 AWXA200300470 120030505A3350BR9660106 LIGHT BOEING737 73733A 1384673NM R-2 DOOR MISSING A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28175AW 23634 SJC - EEL - FLIGHT CREW REPORTED THE R-2 DOOR EMERGENCY EXIT LIGHT WAS MISSING. MAINTENANCE REPLACED THE R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLE, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030508001392003050800139NM 2003 5 8 DL757030382 120030422A3244B757M TIRE BOEING757 757232 1384965NM MLG FAILED A DALAO OTHER O OTHER TOTAKEOFF 1 SO27679DA 26955 NR 2 MLG TIRE CAP SEPERATED DURING T/O. REPLACED NR 2 MLG WHEEL ASSEMBLY 2L72 4F RTA2NM 20030513000382003051300038NM 2003 5 13 03FDEA00707 120030508A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LT WING- O/B FLAP L/E STOP BOLT SUPPORT ISLAND FOUND CRACKED. 2L73 4F RTA22WE 20030528000572003052800057EU 2003 5 28 HEEA086743 120030522A6730SC5084 SERVO AEROSPAS355 AS355* EU CYCLIC DAMAGED E HEEAO OTHER EK VIBRATION/BUFFET FLUID LOSS NRNOT REPORTED 1 SW03973AE2317 3229 FEED BACK IN CYCLIC AND SEEP FROM BOTTOM SHAFT SEAL. TO BE SENT TO VENDOR. 1G72 3U H11EU 20030610000412003061000041WP 2003 6 10 ABXA030166 120030415A53105911412 DOOR FRAME DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 EVIDENCE OF CORROSION DETECTED AROUND FORWARD LOWER CARGO DOOR JAMB LOWER SET SCREW FITTINGS, BETWEEN SKIN LAYERS. REPAIRED AREA IAW REA D953-47181MR AND DC-9 SRM 53-05. 2L72 4F A6WE 20030612001042003061200104NM 2003 6 12 CALA0300279 120030602A3350 BATTERY BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2727205 30577 THE EMERGENCY EXIT LIGHTS AT ROWS 12 - 20ABC FAILED THE BATTERY CAPACITY CHECK. THE EMERGENCY EXIT LIGHT BATTERY PACKS M1694 AND M1670 WERE REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20030522000842003052200084WP 2003 5 22 GTIA030304 120030416A5412 FIRESEAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE NR 2 ENGINE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 NR 2 ENGINE APRON UPPER 4TH FROM FORWARD FIRESEAL CRACKED. REMOVED CRACKED FIRESEAL. FABRICATED NEW FIRESEAL. INSTALLED NEW FIRESEAL. 2L72 4F4 F A6WE E2EA 20030527000792003052700079NM 2003 5 27 AMTA200300606 120030425A5330 SKIN BOEING757 75733N 1384931NM FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11554TZ 32588 FUSELAGE SKIN DENTED AFT OF L2 DOOR. REPAIRED SKIN IAW ER/A 757-53R-5153. (M) 2L72 4F RTA2NM 20030523000352003052300035NM 2003 5 23 DL75A030391 120030427A3350 LIGHT BOEING757 757212 1384951NM 40DEF INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27757AT 23127 EMERGENCY LIGHT AT SEAT 40 DEF INOP. RELAMPED SAME. 2L72 4F RTA2NM 20030529000042003052900004NM 2003 5 29 AALA20030433 120030410A5315 FLOORBEAM BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21621AM 24579 TUL - FOUND TOP OF FLOORBEAM CORRODED AT STATION 1640. REMOVED DAMAGED SECTION OF BEAM. INSTALLED NEW SECTION PER SRM 51-70. (M) 2L72 4F RTA2NM 20030617002702003061700270SW 2003 6 17 HEEA087028 120030604A6310 SEAL BELL 407 407 1182206SW SUPPORT LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03493PH A1514 53393 SEAL LEAKING. TO BE SENT TO MFG FOR CREDIT. 1G71 3U O H2SW 20030620000652003062000065NM 2003 6 20 USAA030068 120030516A5320654580733 ANGLE BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US40222 23989 PIT - FOUND ANGLE CRACKED .5 INCH, ABOVE STRINGER 11R STATION 291.5. DEFECTIVE PART REPLACED WTH IDENTICAL PART NR. (M) 2L72 4F RTA16WE 20030701000372003070100037SW 2003 7 1 HEEA086954 120030603A6510206061432121 HOUSING BELL 407 407 1182206SW BLOWER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 TAIL ROTOR DRIVE BLOWER HOUSING CRACKED. TO BE SENT TO VENDOR. 1G71 3U O H2SW 20030702000042003070200004 2003 7 2 AMTA200300769 420030612A2565 COVER BOEING737 73783N 13844HINM ESCAPE SLIDE DISLODGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11312TZ 32579 FOUND R-1 DOOR SLIDE FALLING OUT OF COVER. RESTOWED SLIDE IN COVER, OK FOR FLIGHT. (M) 2L72 4F RTA16WE 20030708000282003070800028SO 2003 7 8 CY42003F00002 220030331A8530FRCN712ACA CYLINDER HEAD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE SEPARATED A CY4RO OTHER O OTHER NRNOT REPORTED 1 AL0373047143 20700556 280019R CYLINDER HEAD SEPARATED FROM THE BARREL. 1H71 3O3 O A16CE E5CE 20030710000282003071000028NM 2003 7 10 USAA030086 120030524A5320 WEB BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU58093 22204 CLT - FOUND WEB CRACKED .25 INCH, STATION 560, NR 1 CARGO DOOR CUTOUT, DOOR STOP FITTING, UNDER S18R-S22R. REMOVED FRAME WEB AND REPLACED PER EA 87260. (M) 2L72 4F RTA2NM 20030710001022003071000102SO 2003 7 10 C2XA03CL111 120030614A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714522 145383 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT IN THE CEILING AT ROW 2 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 2. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030710001442003071000144NM 2003 7 10 EIA2003082 120030614A5313 STRINGER BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 STR 42A LEFT CRACKED AT STA 240. REMOVED DAMAGED Z-STRINGER, FABBED NEW PART AND INSTALLED PER B747 SRM 51-30-02, 51-20-01, SOPM 20-41-02 AND SRM 51-10-02. 2L74 4F RTA20WE 20030710001402003071000140 2003 7 10 MALA030312 420030613A34206226342022 DISPLAY SAAB SF340 340B 7860101EU EFIS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15447XJ 340B447 DURING FLIGHT 3056 LT EFIS TUBE WENT BLANK AFTER TAKEOFF. AIR RETURN TO MSP. MAINTENANCE REPLACED LT LOWER EHSI SCREEN P/N 622-6342-022, SN/OFF 5287, SN/ON 3061, PER SAAB AMM 34-24-15-4. OPS CHECK GOOD. 2L72 4T RTA52EU 20030114000302003011400030 2003 1 14 SWAA030044 420030105A2565D31354 SLIDE BOEING737 737317 138447PNM FWD SVC DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030529000112003052900011CE 2003 5 29 2003F00328 120030116A5311671261713 FRAME CESSNA750 750 2076810CE FUSELAGE CRACKED A UG8AK NONE O OTHER ININSP/MAINT 1 GL235114 7500017 FOUND DURING INSPECTION TAILCONE BELTFRAME AT FUSELAGE STATION 691 IS CRACKED. RANDOM CRACKING ORIGINATING AT ASSEMBLY PROCESS OF TAILCONE. REPLACED BELTFRAME P/N 6712617-13. (M) 2L72 4J RTT00007WI 20030625000612003062500061NM 2003 6 25 DHL2003747509 120030514A5754 SUPPORT BOEING727 727224 1384076NM SLAT ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 DURING C CHECK, UPON REMOVAL OF NR 7 SLAT ACTUATOR SUPPORT STRUCTURE FOUND O/B MOUNT CRACKED AND I/B MOUNT CHAFED. REMOVED FUEL TANK ACCESS PANEL 7615 AND 7618 IAW B-727 M.M. 28-11-21. REMOVED DAMAGED ANGLES AND INSTALLED NEW FABBED FROM BAC1503-100145 P.O. 2889131, DIM 9 X 4 IAW S/M 727-57-0130 REV. 2 FIG. 1. REINSTALLED FUEL TANK PANELS IAW B-727 M.M. 28-11-21. 2L73 4F A3WE 20030701000312003070100031EU 2003 7 1 HEEA087883 120030624A24352520M RELAY BOLKMS105 BO105S 5626006EU STARTER FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033071K S859 NR 2 ENGINE WOULD NOT SPOOL. FOUND THAT 109J STARTER RELAY WOULD NOT ENERGIZE 209J NR 2 STARTER RELAY. REPLACED WITH SERVICEABLE PART. 1G72 3U H3EU 20030707000212003070700021NM 2003 7 7 AUS20030458 120030429A29127592113101 FILTER BOEING737 7377BX 13844D2NM HYDRAULIC SYS FAULTY W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) HYDRAULIC RESERVOIR PRESSURISATION MODULE FILTER FAULTY. 2L72 4F RTA16WE 20030707001842003070700184SO 2003 7 7 RAIA00305150 120030524A2611 WARNING LIGHT EMB 145 EMB145 3260210SO LAV SMOKE ILLUMINATED A RAIAO OTHER N FALSE WARNING DEDESCENT 1 CE03801HK 145053 UPON DECENT INTO STL LAV SMOKE INDICATION. MAINTENANCE INSPECTED THE LAV AND OPS CHECKED THE SMOKE DETECTION SYSTEM, NO EVIDENCE OF SMOKE AND OPS CK GOOD. 2L72 4F RTT00011AT 20030709000062003070900006WP 2003 7 9 GTIA030434 120030514A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND CABIN FLOOR SUPPORT CORRODED FS 1309-1338 LBL 17. REMOVED FLOOR SUPPORT. DRILLED AND LOCATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20030711000242003071100024SO 2003 7 11 C2XA03SH201 120030623A531514532637401 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 DURING C-CHECK LEFT HAND FLOORBEAM AT FRAME 19 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 51-30-01 AND 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030711000792003071100079NM 2003 7 11 DHL2003781005 120030625A5270 CONNECTOR BOEING727 727227 1384078NM PAX DOOR DIRTY A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01781DH 21996 AFT ENTRY DOOR WARNING DOES NOT ILLUMINATE WITH DOOR OPEN. CLEANED CONTACTS AT CONNECTION 4554. AFT ENTRY DOOR WARNING OPS CHECKED GOOD IAW 52-70-01. 2L73 4F A3WE 20030717000862003071700086 2003 7 17 HEEA088078 420030704A344280510800001 DISPLAY BELL 206 206L1 1182107SW WX RADAR SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032135V 45657 CDU SCREEN IS BLANK. TO BE SENT TO VENDOR FOR WARRANTY REPAIR. 1G71 3U H2SW 20030115000432003011500043GL 2003 1 15 0064492 320030109A6111C6536 COUNTERWEIGHT MCAULY C5KFR3633110JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MCAULY5JFR C5JFR36C1104GL PROPELLER CORRODED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 951370 951370 CORROSION ON COUNTERWEIGHT. 2L72 4T3 TRTA41NM E2WE 5 CP15NE 20030115002142003011500214NM 2003 1 15 DLM88030045 120030110A2400UNK WIRE DOUG MD88 MD88 3023688NM E/E COMPARTMENT BURNED A DALAO OTHER A FLAME/FIRE ININSP/MAINT 1 SO27992DL 53344 WIRE BUNDLE AT STATION 110 PANEL, FORWARD AND BELOW THE COCKPIT TEMP CONTROLLER, SHORTED AND CAUGHT FIRE, WHILE REMOVING CONTROLLER. CA REPAIRED DAMAGED WIRE. 2L72 4F RTA6WE 20030127000572003012700057 2003 1 27 HEEA083635 420030114A342150400179015 INDICATOR BELL 407 407 1182206SW ADI ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 ADI QUICK ERECT KNOB ERRATIC OPERATION. REPAIRED. 1G71 3U O H2SW 20030127002412003012700241SO 2003 1 27 C2XA03BT016 120030126A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN AREA FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2714568 145628 EWR---CO2664, CREW REPORTED, "LEFT AND RIGHTHAND AFT EMERGENCY LIGHTS INOPERATIVE." MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTING #4 POWER SOURCE CHARGER IAW EMB145 AMM #33-50-04. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20030128001882003012800188WP 2003 1 28 ZW0A0301106 120030117A5512 SKIN DOUG DC9 DC983 3022083WP HORIZ STAB CRACKED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139629H 53599 DURING CHECK-C 4 EACH CRACKS AROUND BOLT HEAD LE HORIZONTAL STABILIZER 1-8 INCH APPROXIMATELY 19 INCHES FROM LE LEFT HAND HORIZONTAL STABILIZER. REPAIR COMPLETED PER SRM 51-70-4. 2L72 4F RTA6WE 20030204000922003020400092 2003 2 4 SWAA030151 420030121A256565C19901 CABLE BOEING737 7373H4 1384600NM R2 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2L72 4F RTA16WE 20030127000172003012700017 2003 1 27 HEEA083593 420030114A2300G4434A CONTROL HEAD BELL 412 412 1182202SW COMMS SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 COMMS SYSTEM CONTROL HEAD VOLUME FLUCTUATES DURING FLIGHT. SHOP REPAIR. 1G72 4U H4SW 20030127000832003012700083NM 2003 1 27 PCAA0301021 120030120A3397 WIRE DHAV DHC8 DHC8102 2809003NM CABIN DAMAGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13816EX 329 DURING ROUTINE MAINTENANCE VISIT EMERGENCY EXIT LIGHT FOUND INOPERATIVE AFT OF RIGHT FORWARD ESCAPE DOOR. LAMP WIRE SPLICE REPAIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030204000682003020400068NM 2003 2 4 SWAA030195 120030124A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20030204002362003020400236NM 2003 2 4 SWAA030209 120030128A57116959886 SPAR BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND RT MLG BEAM REAR SPAR CHORD CRACKED. REMOVED AND REPLACED RT MLG BEAM REAR SPAR CHORD PER BFG ER. 2L72 4F RTA16WE 20030206001932003020600193SO 2003 2 6 C2XA03IA017 120030206A32307455501REVF CONTROL HANDLE EMB 145 EMB145LR 3260212SO COCKPIT INTERMITTENT A C2XAK NONE O OTHER CLCLIMB 1 SW2713538 145527 IAH- FLIGHT 2804, GEAR LEVER DISAGREE- GEAR DID NOT CYCLE UP- HAD TO "JIGGLE" GEAR LEVER TO UP POSITION TO CYCLE. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030218002562003021800256 2003 2 18 SWAA030353 420030213A2565D31591478 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR SPACER BUSHINGS MISSING. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20030118000032003011800003 2003 1 18 C2XA03TY006 420030118A3443DMNI5042 ANTENNA EMB 145 EMB145LR 3260212SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 Tys, During a scheduled inspection the lower TCAS antenna base was found corroded. Maintenance removed and replaced the antenna. I/A/W-EMB-145-34-43-02, operational checked good. The aircraft will be released upon complection of the inspection. 2L72 4T RTT00011AT 20030304000232003030400023 2003 3 4 BAQA084826 420030226A3413501121001 GYRO AGUSTAA109 A109E 0260119EU VERTICAL MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01109UP226 11061 PILOT'S GYRO OFF FLAG STAYS IN VIEW. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH7EU 20030324001342003032400134EA 2003 3 24 COMA0370007 120030322A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA LANDING GEAR INOPERATIVE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01369CA474 10079 FLIGHT 9455 NWS INOP MESSAGE.REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20030307001912003030700191WP 2003 3 7 ABXA030103 120030220A53004894213523 SPACER DOUG DC9 DC931 3022065WP VERT. STAB. CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 VERT. STAB. RIGHT ATTACH ANGLE WAS CRACKED BELOW RAM AIR OPENING. REPAIRED IAW DC-9 SRM 53-05. 2L72 4F A6WE 20030311000172003031100017SW 2003 3 11 2003F00139 120030228A2820206063653003 TUBE BELL 206 206L3 1182108SW FUEL DIST CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03205FC 51130 FUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED. 1G71 3U H2SW 20030317000082003031700008NM 2003 3 17 03FDEA00135 120030218A2750651781820 ACTUATOR BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE LE FLAP FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25258FE5702 4056 20940 AFTER TAKEOFF, WHEN RETRACTING FROM FLAPS, 5 DEG TO 2 DEG, LEADING EDGE FLAPS AMBER REMAINED ON, RIGHT SIDE LEADING EDGE FLAP NR 4 REMAINED OUT. AFTER FOLLOWING RED TABS, AT FLAPS, 2 DEG LEADING EDGE, NR 5 REMAINED OUT. WITH FLIGHT CONTROL WHEEL RELAXED, A/C ROLLED LEFT. PLACED NR 5 LEADING EDGE FLAP ACTUATOR /27-81-022-4. FLAP SYSTEM OP CHECKS GOOD. 2L73 4F4 FRTA3WE E2EA 20030402000162003040200016NM 2003 4 2 03FDEA00170 120030224A5710ARB2850505 SUPPORT DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING L/E SLAT TRACK, NR 16 RIB SUPPORT, INBOARD SIDE FOUND CRACKED, APPROXIMATELY 1 INCH IN LENGTH. LT WING L/E SLAT TRACK NR 16 RIB SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20030121003302003012100330GL 2003 1 21 HEEA083381 220030109A73135233600 FUEL NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 FUEL NOZZLE DELAYED LIGHT OFF. REPLACED FUEL NOZZLE. 1G71 3U3 U H2SW E4CE 20030121003362003012100336NM 2003 1 21 AWXA200300052 120030120A30306937346146 MODULE BOEING737 7373S3 1384711NM -N/A- ARCED A AWXAK NONE O OTHER CRCRUISE 1 WP28315AW2362011624 23734 LAS - DIV - FLT771 FROM PHX TO SMF A BLUE ARCING EMMENATED BRIEFLY FROM BEHIND THE OVERHEAD PANEL WITH AN AUDIBLE POP AND BRIEF FLICKER OF THE FORWARD PANEL BACKGROUND LIGHTING, ADDITIONALLY A BRIEF ODOR OF OZONE WAS NOTED. MAINTENANCE REMOVED AND REPLACED THE P5-9 PITOT STATIC WINDOW MODULE PER BMM 30-09-11 AND ALSO REMOVED AND REPLACED THE LEFT HAND ANGLE OF ATTACK SENSOR PER AMERICA WEST TASKCARD#'S R1A27002 AND A1B27003. SUPPLEMENTAL SDR WILL BE SUBMITTED ONCE TEARDOWN REPORT HAS BEEN ACQUIRED. 2L72 4F RTA16WE 20030204002092003020400209NM 2003 2 4 SWAA030139 120030120A57536546430122 SKIN BOEING737 7373H4 1384600NM FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED BC3 CHECK, FOUND RT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED IN A 6 INCH DIAMETER CENTER SECTION. REMOVED AND REPLACED INBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20030224000162003022400016EU 2003 2 24 BAQA083516 120030116A7712 INDICATOR BOLKMS117 BK117A1 5626010EU ENGINE TORQUE MALFUNCTIONED H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME2007 7243 TORQUE NEEDLE SPINS. REPLACED WITH SERVICEABLE INDICATOR. 1G72 3U H13EU 20030224001522003022400152EU 2003 2 24 U30A200300006 120030219A2560P2070001214 FLASHLIGHT AIRBUS320 A320214 3930316EU #1 FWD F/A SEAT INOPERATIVE A U30AK NONE O OTHER ININSP/MAINT 1 EA17260AV 1564 After Flt 257 in EWR, during weekly service, the # 1 Forward Flight Attendant Emergency flashlight was inop. Replaced flashlight. 2L72 4F RTA28NM 20030228000182003022800018NM 2003 2 28 SWAA030398 120030219A33506104789 BATTERY BOEING737 7373H4 1384600NM AFT CABIN FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 AFT ENTRY AND AFT SVC DOOR EMERGENCY EXIT SIDE WALL LIGHTS ILLUMINATED WITH SWITCH OFF. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20030228001052003022800105WP 2003 2 28 DHL2003806004 120030226A2611302314 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01806DH 46002 1) #4 SMOKE DETECTOR WON'T TEST.2) REMOVED AND REPLACED #4 SMOKE DETECTOR WITH SERVICEABLE ASSEMBLY IAW M/M 26-16-5. OPS CHECKED GOOD. 2L74 4F RT4A25 20030228001192003022800119WP 2003 2 28 ABXA030090 120030131A53002024T3 DOUBLER DOUG DC9 DC931 3022065WP RT. WHEEL WELL CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CORROSION ON RIGHT WHEEL WELL UPPER PRESSURE PANEL DOUBLER STATION 722, RIGHT BUTT LINE 56. FABRICATED NEW DOUBLER IAW DWG #9910155 AND DC-9 SRM. 2L72 4F A6WE 20030304000942003030400094NM 2003 3 4 DLM88030178 120030222A2910AS15308K0254 HOSE DOUG MD88 MD88 3023688NM TAIL COMPARTMENTDAMAGED A DALAO OTHER K FLUID LOSS CLCLIMB 1 SO27932DL 49719 RT HYDRAULIC SYSTEM QUANTITY LOST ON CLIMBOUT. GEAR MANUALLY EXTENDED. DOORS REMAINED OPEN DURING LANDING. FOUND RT ENGINE HYDRAULIC FLEX LINE TO FILTER MODULE LEAKING. REPLACED SAME. LEAK CHECKS GOOD. 2L72 4F RTA6WE 20030304000962003030400096NM 2003 3 4 DL733030199 120030226A261172130000008 SMOKE DETECTOR BOEING737 737347 1384647NM LAVATORY MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 SO27308WA 23441 RT AFT LAV SMOKE DETECTOR LIGHT AND CHIME CAME ON AND OFF IN FLT. REPLACED SMOKE DETECTOR UNIT 2L72 4F RTA16WE 20030310000392003031000039SW 2003 3 10 HEEA084946 120030227A3213212321103 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 CROSSTUBE HAS SEVERAL SPOTS OF CORROSION BEYOND LIMITS. SCRAPPED. 1G72 4U H4SW 20030310001112003031000111 2003 3 10 HEEA085018 420030228A34570110050400 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381SP 51029 GPS CURSOR INOPERATIVE IN TCAS MODE. 1G71 3U H2SW 20030310001402003031000140NM 2003 3 10 EIA2003013 120030226A5300UNK SUPPORT FITTING BOEING747 747132 1384882NM A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 L/H Main Gear Wheel @ STA 1241 BL) to 43" WL 175" (approx) longitudinal support fitting has two double drilled holes (1 ea) in the flanges. CORRECTIVE ACTION: Complied with ECRA # 481-53-190-2 (Removed & Replaced Support Fitting) 2L74 4F A20WE 20030117000882003011700088NM 2003 1 17 2003UALA00011 120030104A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29355UA 24361 CRACK IN UPPER FLANGE OF CABIN FLOOR INTERCOSTAL AT BS 346 FLOORBEAM BL0 SEEN FROM LOWER SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2L72 4F4 FRTA16WE E2GL 20030314002052003031400205NM 2003 3 14 0300495511 120030124A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01511US 23199 DURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT BS 345 LBL 7. REPAIRED PER EA 55-121560. 2L72 4F RTA2NM 20030317000482003031700048NM 2003 3 17 03FDEA00184 120030226A3231 DOOR BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE RT MLG MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25463FE 22551 DURING GEAR RETRACTION, THE RT GEAR DOOR LIGHT AND PILOTS GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. RECYCLED GEAR IAW RED TABS AND LIGHTS EXTINGUISHED. OPERATED RIGHT DOOR FOR MAIN GEAR WITH GROUND RELEASE HANDLE OPERATES NORMAL IAW M/M 32-62-011-5. 2L73 4F4 F A3WE E2EA 20030121002802003012100280 2003 1 21 HEEA083370 420030109A34215040006914 INDICATOR BELL 206 206B3 1181506SW ATTITUDE INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032268V 3605 ATTITUDE INDICATOR SHOWS 10 DEGREE BANK IN LEVEL FLIGHT AND ON THE GROUND. 1G71 3U H2SW 20030122000222003012200022SW 2003 1 22 HEEA083409 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801777 51074 MAIN BATTERY WEAK. 1G71 3U H2SW 20030122000722003012200072 2003 1 22 HEEA083460 420030109A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMMS SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 SELECTOR KNOB HARD TO TURN. SHOP REPAIR. 1G71 3U H2SW 20030325000532003032500053NM 2003 3 25 AWXA200300211 120030218A531065468225 CREASE BEAM BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-11 CHECK EXFOLIATION CORROSION WAS FOUND ON CREASE BEAM WEB AT BS 727E+10, STR 17 LT. MAINTENANCE REMOVED CORRODED CREASE BEAM WEB BS 727E+10, STR 17 LT; FABRICATED A NEW REPLACEMENT CREASE BEAM WEB PER DWG 65-46822-5; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030327000192003032700019NM 2003 3 27 AWXA200300287 120030226A5312651630084 BULKHEAD BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT WL 190, BL 0, UNDER VOR/LOC ANTENNA MOUNT. MAINTENANCE CUTOUT CRACKED BS 178 BULKHEAD WEB AT WL 190, BL 0; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, FILLER AND 3 EACH SHIMS; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-11, FIG. 10, DETAIL VI. 2L72 4F RTA16WE 20030318000862003031800086WP 2003 3 18 ASAA0380023 120030104A57555930976505 STRUCTURE DOUG DC9 DC983 3022083WP RT SPOILER CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT GROUND SPOILER IS CHAFED ON BOTTOM INBOARD TRAILING EDGE. REPAIRED DAMAGED AREA PER SRM 51-70-1B. (M) 2L72 4F RTA6WE 20030418000372003041800037WP 2003 4 18 MWEA030096 120030217A533059364365 FINGER DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 EXCESS FINGER DOUBLER MATERIAL EXTEND UNDER LONGERON 12 RT STA 1338 FORWARD TO THE VERTICAL SPLICE OF THE SKIN PANEL. REPAIRED LONGERON SPLICE AND TRIMMED BACK FINGERS TO MINIMIZE EDGE DISTANCE TO AVOID OVERLAP CONDITION WITH REPAIR FINGER DOUBLER. 2L72 4F A6WE 20030731000522003073100052NE 2003 7 31 QXEA200300840 220030718A7320311717502 HMU DHAV DHC8 DHC8201 2809001NM PWA 120 PW123D 52152NE NR 2 ENGINE MALFUNCTIONED A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09359PH2007 514 IDA - FLIGHT 2198 ABORTED TAKEOFF NR 2 ENGINE SLOW TO ACCELLERATE. REPLACED NR 2 HMU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20030807000312003080700031EU 2003 8 7 USAABA03025 120030702A249755T142 WIRE HARNESS AIRBUS330 A330323 3930335EU LT ENGINE INOPERATIVE A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19673UW 0337 THE LEFT GENERATOR WENT INOPERATIVE AND COULD NOT BE RESET. THE APU WAS STARTED, BUT PERFORMED AND AUTO SHUTDOWN AFTER FIVE MINUTES OF OPERATION. FLIGHT RETURNED TO LGW. EN ROUTE BACK TO LGW, THE APU WAS RESTARTED, BUT SHUTDOWN AGAIN. MAINTENANCE REPLACED THE IDG WIRING HARNESS. THE APU FUEL/OIL SEPARATOR WAS SUMPED AND THE APU OPERATED FOR THREE HOURS. (M) 2L72 4F RTA46NM 20030423001742003042300174NM 2003 4 23 P5CA0300780 120030316A2751 CONNECTOR BOEING747 7472U3B 1384846NM TE FLAP INDICATODAMAGED A P5CAO OTHER N FALSE WARNING DEDESCENT 1 WP23923FT 22769 OUTBOUND FLAPS WOULD NOT EXTEND NORMALLY, HAD TO BE EXTENDED ELECTRICALLY. FOUND LOOSE PIN ON OUTBOARD RT POS TRANSMITTER CONNECTOR. REPINNED CONNECTOR & OPERATED FLAPS PER 27-51-00. 2L74 4F RTA20WE 20040225001772004022500177NE 2004 2 25 DL73S031146 220031228A7200 ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 MALFUNCTIONED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27310DA47335 709159 23082 709159 AFTER T/O, NR 2 ENGINE WENT TO FULL THEN DROVE TO IDLE. ENGINE DATA READ ON FDR. REPLACED NR 2 ENGINE. 2L72 4F4 FRTA16WE E2EA 20030717001022003071700102EU 2003 7 17 USAASA03066 120030618A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19758US 1348 THE AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE RIGHT CENTER EMERGENCY POWER SUPPLY UNIT. SYSTEM TESTS OK. (M) 2L72 4F RTA28NM 20030723000052003072300005EU 2003 7 23 SIMA200313902 120030516A2910AE83011E B-NUT SAAB SF340 340B 7860101EU HYD LINE DAMAGED A SIMAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SW21235AE 340B235 DURNIG TAXI IN ARICRAFT, LOST HYDRAULIC POWER. MAINTENANCE FOUND A BAD B-NUT ON THE NR 4 BRAKE LINE. LINE AND B-NUT WERE REPLACED IAW SAAB MM. LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20030723000322003072300032 2003 7 23 WRLA200315 420030616A2565 SLIDE DOUG DC10 DC10 N/A-SDRNM PAX DOOR MALFUNCTIONED A WRLAK NONE O OTHER ININSP/MAINT 1 EA27541SA 46541 DURING A FUNCTIONAL CHECK OF RT FORWARD DOOR SLIDE ASSY (R1) DOOR FAILED TO OPEN TO ITS FULL TRAVEL. DOOR PNEUMATIC ACCUMULATOR BOTTLE NOTED TO HAVE BEEN AT LOW SIDE OF ITS GREEN SERVICING INDICATION BAND. THE DOOR WAS CLOSED AND THE DOOR PNEUMATIC ACCUMULATOR BOTTLE WS SERVICED TO HIGH SIDE ON THE SERVICING INDICATOR. THE DOOR WAS ACTUATED WITH THE EMERGENCY OPERATING HANDLE AND THE DOOR OPERATED IAW THE MM. THE SLIDE RAFT DEPLOYED WITH NO PROBLEMS NOTED. NON-ROUTINE ITEMS WERE WRITTEN CHECK THE RIGGING ON THE R1 DOOR ASSY. 2L73 4F RTA22WE 20030826000852003082600085 2003 8 26 YENA200322 420030819A31603907130402 DISPLAY AIRBUS320 A320232 3930326EU COCKPIT FAULTY A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA155O5JB13447 1173 ON DESCENT SD (LOWER ECAM DISPLAY) BEGAN TO FLICKER ON & OFF FOLLOWED BY DISTINCT SMELL OF ELECTRICAL (ACRID) SMOKE (NOTE: NO SMOKE IN COCKPIT); SD WAS TURNED OFF AND SMELL DISSIPATED WITHIN 3 MINUTES. NO CIRCUIT BREAKERS POPPED. SD NEVER GOT WARM TO TOUCH. INITIALLY THE ITEM WAS DEFERRED PER MEL 31-63-01 AND THE FINAL ACTION WAS REPLACEMENT OF THE DU PER MM 31-63-22. 2L72 4F RTA28NM 20030828000072003082800007WP 2003 8 28 ARWA20030318 120030315A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STA 1280, BTW L29R AND L31R SKIN WITH NICKS. TRIMMED OUT DAMAGE AREA IAW AS ELEVEN INC DRAWING AS11490 SHEET 1 OF 2 AND 2 OF 2, DATED 02/19/03; FABRICATED FILLER, DOUBLER AND TRIPLER IAW AS ELEVEN INC DRAWING AS11490 SHEET 1 OF 2 AND 2 OF 2, DATED 02/19/03; TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8, AND INSTALLED PARTS IAW AS ELEVEN INC DRAWING AS11490 SHEET 1 OF 2 AND 2 OF 2, DATED 02/19/03. 2L74 4F 4A25 20030903001172003090300117 2003 9 3 USAABA03013 420030410A2565 SLIDE AIRBUS330 A330323 3930335EU RT DOOR MALFUNCTIONED A K NONE L NO TEST ININSP/MAINT 1 EA19674UW 0342 DURING A RE-CHECK OF THE RIGHT MID DOOR SLIDE INFLATION TEST, THE SLIDE DID NOT INFLATE WHEN THE LANYARD WAS ACTUATED. WHEN THE SLIDE WAS REMOVED FROM THE AIRCRAFT AND MAINTENANCE ATTEMPTED TO DEPRESSURIZE THE INFLATION BOTTLE, THE BOTTLE FIRED AND THE SLIDE DEPLOYED. THE SLIDE REGULATOR PERFORMED A HANGFIRE. THE REGULATOR WAS SENT TO GOODRICH. NO CONCLUSIVE RESULTS WERE OBTAINED FOR THE FAULT. US AIRWAYS IS ACCOMPLISHING GOODRICH ALERT SERVICE BULLETIN 25A341 ON ITS REGULATOR VALVES. (M) 2L72 4F RTA46NM 20030902000412003090200041EU 2003 9 2 OLR2003F00000 120030523A6230350A37100206 STAR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE FORK CHAFED E OLRAO OTHER O OTHER NRNOT REPORTED 1 WP11853HW5035 2741 THE UPPER SERVO ROD END BEARING RUBBED AGAINST INNER PORTION OF NON ROTATING STAR ATTACHMENT FORK. WEAR WAS 3.0MM. MAX WEAR IN THIS AREA IS 2.5 MM. REPLACED STAR WITH NEW (PN 350A3700207). 1G71 3U3 U H9EU E19EU 20030904001682003090400168WP 2003 9 4 DHL2003873555 120030703A53305710370505 PANEL DOUG DC8 DC873F 302199FWP FUSELAGE DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 LOWER FUSELAGE NR 739 LOWER PANEL WITH EDGES UNBONDED; STA 1100.000 - STA 1120.00 (RT SIDE). REMOVED RT LWR FUSELAGE PANEL NR 739 BETWEEN STA 1100.000-STA 1120.00 IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ASSY IAW SRM 1-3-0 PG 1. 2L74 4F RT4A25 20030728001332003072800133NM 2003 7 28 AMTA200300899 120030707A3397 WIRE BOEING757 75723N 1384973NM CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 FLT 584 - EMERGENCY FLOOR TRACK LIGHTS ROW'S 22 THROUGH 24 INOPERATIVE. RECONNECTED WIRING AT ROW 24, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030911000262003091100026EU 2003 9 11 RAIA00308214 120030815A3150 WARNING LIGHT AEROSPATR72 ATR72202 8680940EU COCKPIT ILLUMINATED A RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03721TE 217 ELECTRICAL SMOKE WARNING INDICATION DURING FLIGHT. MAINTENANCE PERFORMED GROUND ENGINE RUN AND OPS CK CABIN LIGHTING AND COULD NOT DUPLICATE, NO ELECTRICAL ODOR. NO EVIDENCE OF EQUIPMENT OVERHEATING. 2H72 4T RTA53EU 20030916000332003091600033WP 2003 9 16 03FDEA01113 120030718A5297 WIRE DOUG DC10 DC1010 3022110WP PACK DOOR CORRODED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25397FE 46631 ON CLIMBOUT PASSING FL280 (AIR COND DOORS) LIGHT ILLUMINATED INTERMITTENTLY, WENT OUT AT 16000 FEET ON DESCENT. PRESSURIZATION REMAINED ON SCHEDULE ENT BY: 308389 RPT BY: 061284 FACT 18JUL03 12:26 STL R FOUND LT AFT PACK DOOR SWITCH WIRES CORRODED AND BROKEN AT CONNECTOR P1-1618. REPLACED CONNECTOR SWP 20-31. OPS CHECK NORMAL IAW M/M 52-70-07-2 RII:131618 ENT BY: 308389 RPT BY: 308389 2L73 4F A22WE 20030822001662003082200166WP 2003 8 22 UPS03841022 120030723A551456545017 ANGLE DOUG DC8 DC873F 302199FWP HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2 LEFT HORIZONTAL STAB AT XFS 32 L-ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 5654501 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20030822001452003082200145NM 2003 8 22 C1HA200381020 120030806A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CORROSION ON FLOORBEAM AT FS 1110 BETWEEN LBL 45 AND RBL 55. 2L73 4F A3WE 20030825001612003082500161WP 2003 8 25 GTIA030600 120030725A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FTW - FOUND FORWARD CABIN STATION 200 TO 260, CENTER, FLOOR PANEL HAS DETERIORATED/CRACK ON EDGE/CORRODED AT INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20030910000962003091000096NM 2003 9 10 MWEA030352 120030902A53305936667501 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 TWO EACH DENT LOCATED AT STATION 1254 LONGERON 28 LEFT. FABRICATED AND INSTALLED INTERNAL DOUBLER. 2L72 4F RTA6WE 20030910001312003091000131NM 2003 9 10 MWEA030345 120030827A490039619131 DRAIN MAST DOUG MD88 MD88 3023688NM APU BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 RIGHT AUXILIARY POWER UNIT OVERBOARD DRAIN MAST IS BROKEN. FABRICATED AND INSTALLED REPLACEMENT DRAIN MAST. 2L72 4F RTA6WE 20030912000042003091200004NM 2003 9 12 ABXA030328 120030813A2612 FIRE LOOP BOEING767 767281 1385109NM GE CF6 CF680A 30025NE INOPERATIVE A ABXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23789AX 23022 580247 DURING CLIMBOUT, GOT LEFT ENGINE FIRE INDICATIONS. BELL, SHUT OFF SW, T-HANDLE, MASTER WARNING, EICAS MSG. SHUT DOWN AND SECURED ENGINE. CREW PERFORMED AN AIR TURN BACK TO OAK WHERE THE AIRCRAFT LANDED AT APPROXIMATELY 285,000 LBS AS A RESULT OF AN EMERGENCY RETURN. AIRCRAFT LANDED WITH A LOW SINK RATE. AIRCRAFT LANDED WITH OUT INCIDENT. REPLACED NR 1 ENGINE LOOP 2 FIRE DETECT CARD M682 AND FIRE/OVERHEAT CARD IAW B767 AMM 26-10-01-4. OVERWEIGHT LANDING INSP. COMPLIED WITH PER B767 MM 05-51-35-2. NO DEFECTS NOTED. TROUBLESHOOTING STILL IN PROGRESS AT THIS TIME. REMOVED AND REPLACED BROKEN SPRING ON RECOUP DUCT IAW CF6MM 71-00-02. NO DEFECTS NOTED ON ENGINE RUN. 2L72 4F4 FRTA1NM E13NE 20030911002282003091100228NM 2003 9 11 DHL2003742013 120030821A1430 FASTENER BOEING727 727225 1384077NM FIRE LOOP LOOSE A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01742DH 21290 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED (P6-3 PANEL). INSPECTED FIRE LOOP ON NR 3 ENGINE. FOUND LOOSE FASTENER AND SECURED IAW B-M/M 20-80-1. NO DEFECTS NOTED. 2L73 4F A3WE 20030926000092003092600009NM 2003 9 26 QXEA200301028 120030820A5711 SPAR DHAV DHC8 DHC8202 2809007NM ZONE 600 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 GOUGE ON RIGHT HAND WING FORWARD SPAR TOP FLANGE AT YW201.9. REPARIED IAW DHC-8 SRM 51-00-06 AND RD 8-57-1675. 2H72 4T RTA13NM 20030930000072003093000007NM 2003 9 30 AWXA200301026 120030906A2530416000123 COFFEEMAKER BOEING737 7373Y0 1384671NM AFT GALLEY OVERHEATED A AWXAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28334AW6567 2985 23747 AFTER TAKEOFF, EN ROUTE, A BURNING ODOR WAS REPORTED IN THE AFT CABIN. INTENSITY WAS INCREASING UNTIL GALLEY POWER RE-CIRCULATION FAN WAS SELECTED OFF. TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE AFT LT COFFEE MAKER OVERHEATING. REMOVED AND REPLACED THE AFT LT COFFEE MAKER IAW T/C R1D25001, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20031002000902003100200090NM 2003 10 2 C1HA200386006 120030908A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 CORROSION ON FLOORBEAM UPPER CHORD AT BS 1166 RBL 45. 2L73 4F A3WE 20031006001252003100600125EU 2003 10 6 RAIA00309239 120030912A2910 LINE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM CHAFED A RAIAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 CE03551HK 41040 HYDRAULIC FAILURE. MAINTENANCE REPAIRED CHAFED HYD PRESSURE LINE IN RIGHT NACELLE. 2L72 4T RTA41NM 20031021002652003102100265NM 2003 10 21 03FDEA01580 120030918A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 CORROSION ON SKIN BS 684 BETWEEN STRINGER 27 RT AND STR 28 RT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS FABRICATED REPAIR PLATE IAW SRM 53-30-3 FIG 3A. 2L73 4F RTA3WE 20030908002932003090800293 2003 9 8 SWAA031942 420030901A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. SECURED SLIDE ASSY INTO CONTAINER PER MM. 2L72 4F RTA16WE 20030908002972003090800297NM 2003 9 8 SWAA031915 120030825A5313BAC1498 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C4 CHECK, FOUND STRINGER 27L CORRODED AT BS 988. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F A16WE 20031027000842003102700084EU 2003 10 27 DXTA200300130 120030928A3150 SWITCH BRAERO1000 HAWKER1000 7450005EU TRIM STUCK E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07550QS 259050 TAKEOFF ABORTED AT 75KTS FOR THE CONFIGURATION WARNING HORN THAT WAS ACCOMPANIED BY THE RED FLASHER. TROUBLESHOT SYSTEM, APPLIED POWER AND PERFORMED A COMPLETE SYSTEM OPS CHECK FOUND THE COPILOTS TRIM SWITCH WAS STICKING, CLEANED AND LUBED THE SWITCH, SYSTEM OPS CHECKED GOOD IAW HONEYWELL SPZ-8000, ARKANSAS AEROSPACE DRAWING A1-SB-005 REV B. 2L72 4F RTA3EU 20031110000932003111000093SO 2003 11 10 C2XA03SH425 120031104A532014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 SHV- DURING C-CHECK, THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031120000992003112000099NM 2003 11 20 03FDEA01708 120031007A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25217FE 22938 CORROSION ON RT KEEL BEAM BS 950F 8 O/B FLANGE. *S/D* BLENDED CORROSION ON RT KEEL BEAM BS 950F 8 O/B FLANGE AND FOUND OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED REPAIR STRAP. ALL WORK DONE IAW SR 27-53- 023A. 2L73 4F RTA3WE 20040115001502004011500150NM 2004 1 15 DL73S031111 120031219A2731 TAB BOEING737 737247 138448DNM LT & RT ELEVATORFLUTTER A DALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO27243WA 23517 ON CLIMB FROM CVG AT 250 - 280 KTS. F/A REPORTED VIBRATION IN AFT OF AIRCRAFT. VERIFIED BY F/O. NO CHANGE WITH CHANGE IN AIRSPEED, ON DESCENT F/A NOTICED VIBES, SIGNIFICANTLY REDUCED AIRSPEED BELOW 250 KTS. REPLACED LEFT AND RIGHT ELEVATOR TABS. 2L72 4F A16WE 20040210000392004021000039WP 2004 2 10 UPS03841617 120031114A53403641004U1 FITTING DOUG DC8 DC871F 302199DWP LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C1 LT WHEEL WELL OB FITTING UPPER STA. 902 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG.3641004 AND SRM.53-2-0 FIG.8 2L74 4F RT4A25 20031117000312003111700031NM 2003 11 17 QXEA200301213 120031003A2611 O-RING DHAV DHC8 DHC8202 2809007NM ZONE 400 FAILED A QXEAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 NM09354PH 498 ON FLIGHT 2006 DURING TAXI OUT, LAVATORY SMOKE ALARM ACTIVATED FOR 1 MINUTE, THEN RESET BY FLIGHT ATTENDANT. FLIGHT ATTENDANT REPORTED SMOKE/FUMES ODOR AND HAZE/SMOKE IN CABIN NO FIRE/SMOKE IN LAVATORY. RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE NL PROBE AND O-RINGS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031107001202003110700120SO 2003 11 7 SIMA200327908 120031004A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21824AE 145584 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM EMB-145/1142 REV 22, CHAPTER 53-21-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20031112001292003111200129EU 2003 11 12 BAQA089758 120031007A7160430110217 ACTUATOR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101600A 41560NE ENGINE FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G67 7179 ACTUATOR ONLY LASTED 67.1 HOURS SINCE OVERHAUL. TORQUE AND N1 FLUCTUATING. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 10/22/03 1G72 3U3 U H13EU E5NE 20040109000182004010900018WP 2004 1 9 EOO2003F00004 120031002A6220369A13063 BEARING HUGHES369 369D 4470706WP ALLSN 250C 250C20 03013GL M/R HUB FAILED B EOORO OTHER O OTHER NRNOT REPORTED 1 AL035074R 0048 1151D 369A1306-3 BEARING FOUND WITH TEFLON LINER FAILED. MDNC SOR NR 300194 AND MAINTENANCE DISCREPANCY REPORT DATED 02 OCT 2003. 1G71 3U3 U H3WE E4CE 20040113001292004011300129EU 2004 1 13 BAQA091523 120031213A2435150SG117Q STARTER GEN AEROSPAS355 AS355* EU ALLSN 250C 250C20 03013GL ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911KY785 5101 STARTER GEN HAS BRUSHES AND SPRING BROKEN. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 12/15/03 1G72 3U3 U H11EU E4CE 20030122000682003012200068 2003 1 22 HEEA083456 420030109A2350PHI001L0001201 MIXER BOX BELL 206 206L3 1182108SW COMMS SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331801 51074 MIXER BOX HAS LOW VOLUME ON ICS AND STATIC. SHOP REPAIR. 1G71 3U H2SW 20030326000112003032600011SO 2003 3 26 AUS20030099 120030131A32114016 CONNECTOR MAULE MX7 MX7180 5460185SO LYC O360 O360C1F 41514EA HARTZLHCC2Y HCC2YR1 GL MLG DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR OLEO CONNECTOR DISTORTED. OLEO CONNECTORRETAINS THE UNDERCARRIAGE SPRING AND SECURES THE OLEO ASSEMBLY TO THE FUSELAGE. FOLLOWING DISASSEMBLY, THE OLEOS WERE FOUND TO BE LOW ON OIL. THE AN6-21 BOLTS USED TO SECURE THE STRUT TO THE FUSELAGE WERE BENT THROUGH APPROXIMATELY 20 DEGREES. THE TWO OLEO O-RINGS IN EACH UNIT SHOWED EVIDENCE OF DAMAGE DURING ASSEMBLY. THE LOWER LEFT UNDERCARRAIGE "A" FRAME ATTACHMENT BEARING PNO SBG 65 WAS SHATTERED FROM SEIZING DUE LACK OF LUBRICATION. 1H71 3O3 ONC3A23 E286 5 CP920 20030327001612003032700161SO 2003 3 27 C2XA03SH008 120030219A531014521721005 STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING C-CHECK THE FOWARD DIGITAL ON LEFT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS EC 5320-01074. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030326000012003032600001NM 2003 3 26 AUS20030072 120030119A2530 OVEN BOEING737 737800* NM GALLEY ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) SMOKE ODOR IN REAR CABIN. ODOR WAS TRACED TO REAR GALLEY OVEN. 2L72 4F RTA16WE 20030327000702003032700070NM 2003 3 27 C1HA200393004 120030216A3260 WIRE BOEING727 727212 138407GNM MLG DOOR SWITCH BROKEN A C1HAO OTHER N FALSE WARNING DEDESCENT 1 GL15293AS 21348 ON GEAR EXTENSION THE RT MAIN LANDING GEAR DOOR ANNUNCIATOR DID NOT ILLUMINATED ON THE S/O PANEL. REPAIRED BROKEN WIRE AT RT MLG DOOR SWITCH PER WDM. 2L73 4F A3WE 20030417001972003041700197NM 2003 4 17 P5CA0300762 120030204A5347 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK FOUND ON SEAT TRACK STA 1817/LBL 98 WL 208. DAMAGE AREA TRIMMED OUT. REINFORCED WITH NEW SEAT TRACK PER SRM 53-10-05. 2L74 4F A20WE 20030422000242003042200024NM 2003 4 22 HALA0300104 120030307A4920495122 BLEED VALVE BOEING717 717200 1383700NM APU LEAKING A HALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13476HA 55118 FLT 522 - LIH - ELECTRICAL BURNING ODOR THROUGH OUT AIRCRAFT WHILE TAXI TO THE GATE. REMOVED AND REPLACED APU MODULATING BLEED AIR VALVE. OPS AND LEAK CHECK GOOD. OK FOR SERVICE. (M) 2L72 4F TRA6WE 20030716000402003071600040SO 2003 7 16 SIMA200316402 120030612A3411K0057 RELAY EMB 135 EMB135KL 3260302SO PITOT SYSTEM INOPERATIVE A SIMAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW21803AE 145483 CREW RECEIVED A PITOT THREE INOPERATIVE ON EICAS. MESSAGE FLICKERING THEN EXTINGUISHED. AFTER MESSAGE EXTINGUISHED FA REPORTED SMOKE IN GALLEY AND CREW NOTED ODOR IN COCKPIT. CREW DECLARED EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 3 PITOT TUBE CURRENT SENSING RELAY, AND RELAY BASE, IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20030422000782003042200078SO 2003 4 22 SIMA200307913 120030227A532014522459003 SUPPORT EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION GALLEY CENTER BEAM RAMP CORRODED. REMOVED AND INSTALLED SERVICEABLE GALLEY CENTER BEAM RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M) 2L72 4T RTT00011AT 20030424000062003042400006EA 2003 4 24 SWIA200311830 120030315A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA LEFT OVERWING INOPERATIVE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07439SW 7578 LEFT CENTER OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP ON LEFT CENTER OVERWING EMERGENCY LIGHT. OPS CHECK GOOD. 2L72 4F RTA21EA 20040226000092004022600009WP 2004 2 26 ASAA0380417 120030429A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 SEA PREFLIGHT CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20030829001882003082900188 2003 8 29 SWAA031799 420030810A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM 2L72 4F RTA16WE 20030729000452003072900045NM 2003 7 29 ZW0A0305702 120030702A256069B148551 SPRING BOEING757 7572Q8 1384972NM GIRT BAR DEFORMED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13702TW 28162 THE EVACUATION SLIDE GIRT BAR RETENSION LEAF SPRINGS WERE ADJUSTED ACCOUNT DEFORMED ON THE L1, R1, L2, R2, L4, AND R4 CABIN DOOR. 2L72 4F RTA2NM 20030731001422003073100142NM 2003 7 31 2003F00493 120030310A5730 SKIN BOEING727 727222 1384073NM WING CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK ON LEADING EDGE WING SKIN AT NR 5 OUTBOARD SLAT TRACK. STOP DRILLED CRACK. FABRICATED DOUBLER. ALODINED AND PRIMED AREA REPAIR DOUBLER. INSTALLED AT RIGHT WING NR 5 OUTBOARD SLAT TRAKC LEADING EDGE CUT OUT. (M) 2L73 4F A3WE 20030731001492003073100149WP 2003 7 31 GTIA030512 120030612A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - FOUND AFT PIT CEILING STATION 1338 LBL 49 LAV FLOOR CRACKED. FOUND FLOORBOARD FRAME CORRODED AND OUT OF LIMITS. FABRICATED LEFT AFT LAV FLOORBOARD FRAME. FABRICATED LEFT AFT LAV FLOORBOARD. INSTALLED LEFT AFT LAV FLOORBOARD. (M) 2L72 4F A6WE 20040112001112004011200111 2004 1 12 MEX2003444 420030923A34174040800912 ADC BOEING757 757200 1384950NM COCKPIT FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23703AM 27203 FLT 928 - MEX-MTY - AIRCRAFT RETURNED TO PLATFORM, DURING TAXI AFTER ENGINE STARTING EICAS OVERSPEED MESSAGE WENT ON. DURING REVISION CADC NR 2 WAS ALARMED, SO IT WAS REPLACED IAW MM 34-12-01, ALL TESTS CORRECT. (M) 2L72 4F RTA2NM 20040415000202004041500020GL 2004 4 15 ERAA093717 220030927A7320252466715 GOVERNOR BOLKMS105 BO105A EU ALLSN 250C 250C20B 03013GL ENGINE INOPERATIVE B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH6008 S675 N2 DROPS OFF 10-12 PERCENT IN CRUISE FLIGHT AND VERY STIFF ARM. INTERNAL COMPONENTS VERY WORN FOR LOW TIME USED. POSSIBLE EXTERNAL VIBRATIONS. REPAIRED AND TESTED IAW MFG OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20031212001512003121200151WP 2003 12 12 GTIA030852 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200-208 60 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20031215001712003121500171WP 2003 12 15 AALA20031065 120030924A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP A/C BAY DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21285AA 49297 DTW - FOUND DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE IN THE AFT TAIL EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20031218000512003121800051NM 2003 12 18 03327416 120031123A3350 BATTERY PACK DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27416FJ 3171 DURING INSPECTION THE FORWARD EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE 4LK BATTERY PACK WAS FOUND TO BE THE CAUSE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031223001832003122300183WP 2003 12 23 GTIA030830 120031001A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FOUND CABIN FLOOR SUPPORT 2 INCH LONG CORROSION AT FS 200 51 INCHES LBL. REMVOED FLOOR SUPPORT. FABRICATED NEW CABIN FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20031229000712003122900071NM 2003 12 29 03FDEA02185 120031214A5753 TRACK DOUG MD11 MD11 3023602NM ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LT WING, INBOARD FLAP CENTER VANE TRACK CUTOUT DENTED. INBOARD FLAP CENTER VANE TRACK CUTOUT DENTED, REPAIR CARRIED OUT AS PER EA 1-5750-75184, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBOARD FLAP / CTR. RIB ASSY AND SKIN. 2L73 4F RTA22WE 20031229000852003122900085NM 2003 12 29 DHL2003742505 120031202A5720 ATTACH ANGLE BOEING727 727225 1384077NM NR 7 SPOILER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, N/R 60695 NR 7 SPOILER FITTING FWD ATTACHMENT ANGLES AT FALSE SPAR ARE CORRODED AND CRACKED WITH LOOSE AND PULLING FASTENERS. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2 AND CUT OUT DAMAGED AREA AT NR 7 SPOILER FITTING FWD ATTACHMENT ANGLE DIMENSIONS 21 INCHES IAW B-727 SRM 51-40-3 FIG 1 AND 57-20-1 FIG 2. FABRICATED NEW ANGLE MAT USED BAC 1524-1432 PO 991286 AND ONE SPLICE DIM 12 INCHES SAME MATERIAL IAW B-727 SRM 51-40-3 FIG 1. ALODINED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED NEW ANGLE AND SPLICE LEFT WING T/E FALSE SPAR IAW B-727 SRM 51-40-3. 2L73 4F A3WE 20031231000692003123100069EA 2003 12 31 ASOA03567 120031104A5320601R53611174 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621 WERE 3 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040105000492004010500049NM 2004 1 5 DL73S031024 120031116A3397 WIRE BOEING737 737232 1384475NM CABIN SEAT 22-25SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27311DL 23083 ON L/O FOUND EMERGENCY LIGHTS AT SEAT ROWS 22-25 INOP AND L2 EXIT IDENTIFIER INOP. REPAIRED DAMAGED WIRE. 2L72 4F RTA16WE 20031010000862003101000086 2003 10 10 BAQA089381 420030927A23126226389001 RADIO AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE VHF SYSTEM WEAK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 6036 WEAK AUDIO. REPLACED WITH SERVICEABLE UNIT. 9/25/03 1G72 3U3 U H10EU E19EU 20040105000842004010500084NM 2004 1 5 QXEA200301566 120031217A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM LT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PDX - LEFT HAND NACELLE INNER FIREWALL IS CRACKED AT THE BEND. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00. 2H72 4T RTA13NM 20040108000722004010800072EU 2004 1 8 B1E2003F00001 120031013A7921L792M3007215 SHAFT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE OIL COOLER FAN SHEARED E B1EAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SO17158BC 0134 BB11196 DURING A LAW ENFORCEMENT FLIGHT, PART 91 THE NR 1 ENGINE OIL COOLER SHAFT SHEARED CAUSING ENGINE OIL TEMPERATURE TO INCREASE TO ABOUT 120 C WHILE ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. AIRSPEED WAS INCREASED AS RECOMMENDED IAW MFG MM TO SLIGHTLY ABOVE 80 KNTS FROM 60 KNTS. OIL TEMPERATURE DID NOT DECREASE. PRECAUTIONARY LANDING WAS MADE. REPLACED OIL COOLER HUB WITH MFG PN L792M3007215. PERFORMED LEAK CHECK AND OPS CHECK, ALL ENGINE PARAMETERS ARE WITHIN LIMITS. 1G72 3U3 UO H88EU E42NE 20031126000982003112600098SO 2003 11 26 C2XA03SH458 120031119A532014524131009 BRACKET EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 SHV-DURING C-CHECK THE PASSENGER DOOR THRESHOLD L-BRACKETS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKETS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040311000562004031100056NM 2004 3 11 ASAA0310094 120030305A52606553889163 TORQUE BOX BOEING737 737298C 1384490NM AIRSTAIR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND AIRSTAIR TORQUE BOX WEB AT BS 937, STRINGER 8L CORRODED. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20031203000412003120300041EU 2003 12 3 COEA0304729 120031023A261251227105 FIRE LOOP FOKKERF27 F27MK600 4990706EU RT ENGINE MALFUNCTIONED A COEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM13729FE 10385 RT ENGINE FIRE WARNING ACTIVATED 5 MINUTES AFTER T/O FROM SEA. RT ENGINE SHUT DOWN. PILOTS REQUESTED RETURN TO SEA. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO SEA WITHOUT INCIDENT. INSPECTION OF THE AIRCRAFT NO EVIDENCE OF A FIRE. MAINTENANCE TESTED EACH FIREWIRE AND COUPLING ON RT ENGINE. REPLACED ALL DEFECTIVE FIREWIRES AND COUPLINGS. REMOVED AND REPLACED RT ENGINE FIRE BOTTLES AND CARTRIDGES. A/C RETURNED TO SERVICE. (M) 2H72 4T A817 20031203001042003120300104NM 2003 12 3 USAA030225 120031106A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US36763 24893 FOUND SKIN CRACKED 1.5 INCH, STATION 727D, BELOW STRINGER 23L. CUT OUT DAMAGE AND INSTALLED DOUBLER PERMANENT REPAIR PER TYP REP 53-60-03. (M) 2L72 4F RTA16WE 20031204000672003120400067EU 2003 12 4 03284316 120031011A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27316UE 41055 DURING INSPECTION THE LT FOWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031210000092003121000009NM 2003 12 10 03FDEA02123 120031128A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20030919001502003091900150NM 2003 9 19 AWXA200300930 120030814A542065C26309 SUPPORT BOEING737 7373G7 1384595NM PYLON FAIRING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 DURING C-17 CHECK A 2.8750 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON FAIRING SUPPORT NAC STA 259.38. MAINTENANCE REMOVED CRACKED FAIRING SUPPORT; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA. D. 2L72 4F RTA16WE 20030925000532003092500053WP 2003 9 25 GTIA030666 120030830A2170 COALESCER BAG DOUG DC9 DC983 3022083WP CABIN COOLING CONTAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 AIR CONDITIONING HAS THE ODOR OF BURNED OIL WHEN THE LT MIX VALVE MOVES RT OF .25 ON THE COLD SIDE THE ODOR IS LIKE BURNED OIL AND IT HURTS THE EYES. REMOVED AND REPLACED AIR CONDITIONING COALESCER BAGS, OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20030923000792003092300079WP 2003 9 23 DHL2003604686 120030517A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP PAX DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 AFT LOWER CORNER OF AFT PASSENGER DOOR JAMB WITH 1.000 CRACK IN IT. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18 SHEET 1, TR 53-134, TR 53-135, DWG 5750776, DWG SR08530021. CUT OUT DAMAGED AREA AND FABRICATED FILLER (7075-T6 AL0.080) AND (2) DOUBLERS (7075-T6 AL0.090) (7075-T6 AL0.125) IAW SRM 53-2-0 FIG 18 SHEET 1, TR 53-134, TR 53-135, DWG 5750776, DWG SR08530021. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLERS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 18 SHEET 1, TR 53-134, TR 53-135, DWG 5750776, DWG SR08530021, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923001392003092300139 2003 9 23 XNOA01147 420030820A3421 INDICATOR AIRBUS300 A300B4203 3930306EU HSI INOPERATIVE A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23371PC 157 CAPTAIN'S HSI COURSE BAR FROZEN. R&R'D CAPTAIN'S HSI IAW A300 MM 34-21-22. OPS CHECK GOOD IAW A300 MM 34-21-22. 2L72 4F RTA35EU 20040130000812004013000081NM 2004 1 30 DHL2003742558 120031125A575465172769 RIB BOEING727 727225 1384077NM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, NR 4 SLAT HAS SEVERAL CRACKS IN RIB INBD SIDE OF THE ACTUATOR, VIEWED THRU THE ACCESS HOLE. REMOVED DAMAGED RIB & INSTALLED NEW, P/N 65-17276-9 PO 3348104 IAW 727 SRM 51-30-2. REMOVED AND REPLACED THE NR 4 SLAT FOR STRUCTURAL ACCESS IAW B727 MM 27-81-11. 2L73 4F A3WE 20040203000422004020300042NM 2004 2 3 ASAA0340017 120030117A57536546486 WEDGE BOEING737 737490 1384715NM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 WHILE PERFORMING C-CHECK, FOUND LT IB MIDFLAP T/E WEDGE HAS A DENT APPROX 3 IN FROM END. (M) 2L72 4F RTA16WE 20040210001112004021000111EU 2004 2 10 USAA030307 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW17500 0333 CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH, FRAME 58 LBL 17.75. DAMAGED SECTION REPLACED WITH NEW PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040218000082004021800008EU 2004 2 18 AWXA200301608 120031226A2780 CIRCUIT BOARD AIRBUS320 A320231 3930325EU LT SFCC MALFUNCTIONED A AWXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP28633AW3028923879 082 EMERGENCY LANDING, ON FINAL APPROACH, EN ROUTE, SLATS LOCKED AT POSITION 1, FLAPS OPERATED NORMALLY. DECLARED EMERGENCY, LANDED FLAPS 3, SLATS 1 IAW ECAM QRH "SLAT BREAK LOCKED". MAINTENANCE REMOVED AND REPLACED NR 1 SLAT FLAP CONTROL COMPUTER (SFCC) IAW AMM 27-51-34, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL CHECK OF SFCC CONFIRMED FAILURE OF UNIT. SLAT LVDT INTERFACE CHECKS FAILED DUE TO R44 & R53 ON SLAT LANE-1 CIRCUIT BOARD OUT OF TOLERANCE. REPLACED RESISTORS R44 & R53 ON SLAT LANE-1 CIRCUIT BOARD (A10), ALSO REPLACED CROSS LANE RAM U23 ON SLAT OUTPUT CIRCUIT BOARD (A9) DUE TO BITE FAULT. MAINTENANCE ACCOMPLISHED IAW CMM 27-03-11, REV. 2. 2L72 4F RTA28NM 20040413000052004041300005NM 2004 4 13 ASAA024018D 120030323A53116546548 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT 747 AND WL 148. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040614002292004061400229 2004 6 14 266 420030529A3160 DISPLAY EMB 145 EMB145 3260210SO COCKPIT MALFUNCTIONED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL11834 AVIONIC BUTTON ON NR 2 PFD BLACK AND CK PFD2 ON EICAS SMOKE FOR UNDER PFD. FOUND PFD BURNT SMELL. REMOVED AND REPLACED F/O'S PFD. 2L72 4F RTT00011AT 20040427000462004042700046EU 2004 4 27 ERAA093698 120031226A3212D24873102 FLOAT BOLKMS105 BO105S 5626006EU MLG WORN A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 5566 18 MONTH FLOAT INSPECTION DUE. FLOAT COVER (P/N OHSS-BO105-2) WAS WORN AND TORN EXCESSIVELY AND FWD END CAP PN C24814-114 WAS ALSO WORN AND TORN EXCESSIVELY. FORWARD CHECK VALVE ON FLOAT BAG (#1 COMPARTMENT ) WAS LEAKING. ONE OF THE WORM CLAMPS HOLDING BOTTLE ONTO SUPPORT TUBE WAS WORN (NO LONGER WOULD TIGHTEN UP) ACTION TAKEN: PERFORMED 18 MONTH INSPECTION ON ASSY USING ERA WORK FORMS AND AIR CRUISERS M/M. CHANGED FLOAT COVER, END CAP, WORM CLAMP, AND ONE CHECK VCALVE. BAG PASSED ALL TESTS. C/W SB'S 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1 & 802-25-2. 1G72 3U H3EU 20030807000142003080700014NM 2003 8 7 USAA030115 120030708A532065C281066 STIFFENER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 PIT - FOUND STIFFENER CORRODED 2 INCHES BY 6 INCHES, STATION 1016 AT BL 0 BETWEEN PRESSURE WEB AND CHANNEL STIFFENER. KIT NR 65C28106-1 AND 65C28106-16 REPAIRED PER EO 5302V112 REV A. (M) 2L72 4F RTA16WE 20030807000162003080700016NM 2003 8 7 USAA030123 120030611A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US48615 23231 PIT - FOUND FRAME CRACKED 4 INCHES, STATION 500 BETWEEN STRINGER 26L-26R. INSTALLED TWO DOUBLERS PER SRM 51-70-11 FIG 1, DETAIL NR 2, PAGE 6. (M) 2L72 4F RTA16WE 20030903001122003090300112EU 2003 9 3 Y2PA03013 120030422A3097 WIRE AMD FALC20FALCOND 2720304EU WINDSHIELD LOOSE A Y2PAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23821AA 203 DURING CRUISE AT FL350, ENCOUNTERED INTERMITTENT SMOKE IN COCKPIT. CREW DECIDED TO DIVERT. DURING DESCENT SMOKE BECAME MORE CONSTANT. DECLARED AN EMERGENCY AND LANDED AS SOON AS POSSIBLE AT NEAREST SUITABLE AIRPORT (SBN). A USA MECH WAS DISPATCHED TO T/S THE PROBLEM. USAA MX FOUND A LOOSE WIRE AT THE WINDSHIELD HEAT TERMINAL BLOCK. THE WIRE TERMINAL WAS TIGHTENED AND THE WINDSHIELD HEAT OPS CHK GOOD PER THE FALCON MM 30-40-1. NO FURTHER DEFECTS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE ENGINES ON THIS AIRCRAFT WERE RUN AND THE ELECTRICAL SYSTEM OF THE AIRCRAFT WAS FULLY POWERED UP WITH NO INDICATION OF ANY SMOKE TO DETERMINE THE PROBLEM HAD BEEN RECTIFIFIED. (M) 2L72 4F A7EU 20030904000912003090400091NM 2003 9 4 QXEA200300997 120030812A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GROOVED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX- NR 5 SEAT TRACK HAS A GROOVE IN THE LOWER SURFACE AT STATION X520.000. REPAIRED IAW DHC-8 RD 8-53-1339. 2H72 4T RTA13NM 20030813000262003081300026NE 2003 8 13 HEEA088568 220030720A7320324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 UNABLE TO OBTAIN N1 TOPPING ON THIS UNIT, AFTER RERIGGING AND INTERCONNECT ADJUSTMENTS, STILL WOULD NOT GET 98 PERCENT. REPLACED. 1G72 4U4 U H4SW E22EA 20030814000492003081400049NM 2003 8 14 UPS03441054 120030718A5310 FRAME BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FRAME FOUND CORROSION AT STA 920 FROM BL 0 - LBL 10. CORROSION BLEND OUT 0.050 X 1 X 1 INCH. BODY FAIRING SUPPORT FRAME REPAIRED AS PER SRM 53-50-04 FIG 2. 2L74 4F A20WE 20030814000602003081400060EA 2003 8 14 SWIA200312166 120030705A2751 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07587SW 7062 FLAPS AT 30 DEGREES. RIGHT FLAP 30/LEFT AT 28. REMOVED & REPLACED LEFT FLAP POSITION TRANSMITTER IAW 27-55-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20030911001332003091100133WP 2003 9 11 UPS03841034 120030705A5320 FITTING DOUG DC8 DC871F 302199DWP FUSE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C2, AFT ACCESSORY COMPT AT STA 1660 RT SIDE BELOW CUSP FITTING IS CORRODED. REMOVED FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW FITTING IAW DAC DWG 4773143. ALODINE AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20030929000132003092900013EU 2003 9 29 AWXA200301013 120030822A5414D54530052201 SKIN AIRBUS320 A320232 3930326EU NR 1 PYLON CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW 543 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED SECTION OF NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED NEW SKIN PER DWG 54-D54510054; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 21-22 FIG 8. 2L72 4F RTA28NM 20030929000272003092900027NM 2003 9 29 03FDEA01418 120030901A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING O/B FLAP VANE MOST I/B TEE FITTING NR 1 FOUND FORWARD BORE CORRODED. RT WING O/B FLAP VANE MOST I/B TEE FITTING (NR 1) FWD CORRODED BORE REPAIRED AS PER EA 1-5750-73297 WITH TITLE : WINGS - TRAILING EDGE DEVICES - RH O/B FLAP VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20030916001422003091600142EU 2003 9 16 F5H2003F00000 120030708A29107907015E VALVE BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP HYD SYSTEM INOPERATIVE B F5HRO OTHER O OTHER NRNOT REPORTED 1 GL13130YB4 NA0285 AFTER INSTALLATION VALVE OPERATION FELT NORMAL. AFTER 1ST FLIGHT THE VALVE STIFFENED UP (WHILE UNDER HYDRAULIC PRESSURE) AND WAS DIFFICULT TO SHUTOFF IN THE FIRST INCH OF TRAVEL. OPERATES NORMAL WITH NO PRESSURE. 2ND REPLACEMENT VALVE WORKS FINE. 2L72 4F4 F A3EU E6WE 20030930000942003093000094EU 2003 9 30 AWXA200301031 120030908A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 241 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW7748 192 527 DURING INSPECTION TEST OF EMERGENCY LIGHTS BY "EMERGENCY LIGHT SYSTEM" PUSH BUTTON FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY, AND EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK FAILED, PART BAD FROM SUPPLY. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL) AGAIN AND SYSTEM FUNCTIONAL CHECK WAS GOOD. PART NAME; ESPU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 3309, TT; 7412, TC; 2827, LOC; ZONE 241, REASON; PART BAD FROM SUPPLY. 2L72 4F RTA28NM 20030930000572003093000057NM 2003 9 30 P5CA0300940 120030908A2613 CONNECTOR BOEING747 7472U3B 1384846NM RT WING DETECTORDISCONNECTED A P5CAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP23923FT 22769 AFT 20 MINUTES INTO CRUISE RT WING L/E OVERHEAT LIGHT ILLUMINATED. REMAINED ON UNTIL BLOCK IN. FOUND NR 3 PYLON DETECTOR S1046 SHORTED. DISCONNECTED S1046. ITEM DEFERRED PER MEL 26-22-03A. SECOND LOOP OPS NRML PER MM 26-15-00 2L74 4F RTA20WE 20030908002672003090800267 2003 9 8 SWIA200312358 420030822A22106226284006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07224SW 120294 THE AUTOPILOT FAILURE WITH AP LIGHT ON FCP AND AUTOPILOT PANEL. THE CAPTAIN'S AP WAS SELECTED. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL APPG5A WITH SERVICEABLE UNIT. AUTOPILOT OPS CHECK GOOD IAW 22-10-00. PN: 622-6284-006. 2L72 4T RTA31SO 20030908002882003090800288NM 2003 9 8 SWAA031937 120030828A53126545819 PRESSURE PANEL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND NLG W/W CEILING CRACKED AT OUTBD SIDE OF RT TIRE BRAKE ASSY. REPAIRED CEILING WEB PER SWA EA. 2L72 4F RTA16WE 20031001000382003100100038WP 2003 10 1 UPS03841181 120030807A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C1, AFT CARGO PIT AT FS 1140-1150 L35L INTERCOSTAL ATTACH FITTING IS CRACKED. VERIFIED CRACK IAW DYE PENETRANT TEST IAW DPS 4.707.1, REMOVED FITTIN G IAW DC8 SRM 51-1-20D, RECEIVED NEW FITTING P/N 3758497.1N PO NR 3541 22 LOCATED AND DRILLED IAW DC8 SRM 51-1-20D, AND INSTALLED IAW DC8 S RM 51-1-20D 2L74 4F RT4A25 20031006001712003100600171WP 2003 10 6 03FDEA01657 120030929A5240AKC70111 HINGE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE SERVICE DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25308FE 48297 COMPLY WITH EA 8-5240-71005. DOORS-SERVICE, TAIL CONE, PATIO DOOR HINGE REPAIR P/N AKC7011-1. CLOSING ACTION ON 09/25/03.ON N/R S00013.COMPLIED WITH EA 8-5240-71005. DOORS SERVICE, TAIL CONE, PATIO DOOR HINGE REPAIR P/N AKC 7011-1. 2L73 4F4 F A22WE E23EA 20031003000402003100300040NM 2003 10 3 AWXA200301044 120030827A53206916970501 ATTACH ANGLE BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON ATTACH ANGLES AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED 2 EACH NEW REPLACEMENT ATTACH ANGLES IAW DWG'S 69-16970-501 AND 69-76555-3; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-30-02, PG. 39, FIG. 11. 2L72 4F RTA16WE 20031014001592003101400159NM 2003 10 14 SWAA032068 120030917A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 EMERGENCY FLASH LIGHT INOPERATIVE IN AFT CABIN LOWER POSITION. REMOVED AND REPLACED FLASH LIGHT AND BATTERY PER MM. 2L72 4F RTA16WE 20030910000672003091000067NM 2003 9 10 DHL2003782010 120030827A3260 UPLOCK SENSOR BOEING727 727227 1384078NM LT MLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01769AT 21998 DURING CLIMBOUT FROM BOS THE LEFT RED GEAR UNSAFE LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. AIRSPEED LESS THAN 270 KIAS FOR THE DURATION OF THE FLIGHT. CHECKED LEFT GEAR UP LOCK SENSOR. FOUND ADJUSTMENT OUT OF LIMIT. ADJUSTED SAME TO WITHIN LIMITS. OPS CHECKS GOOD IAW B727 M/M 32-61-81. 2L73 4F A3WE 20031027000502003102700050NM 2003 10 27 03FDEA01613 120030924A5320 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CRACK IN STR CLIP AT BS 950B STR 9 LT. 2L73 4F RTA3WE 20031119000882003111900088NM 2003 11 19 AWXA200301208 120031012A3397BMS13311122 WIRE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE SEAT ROW 12 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13 & 14 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2EA 20040212001712004021200171NM 2004 2 12 2003UALA00974 120031218A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 STA 907 STR 4 LT STRINGER SPLICE CRACKED IN TWO PLACES, CRACKS EMANATING FROM 2 RIVETS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040407000342004040700034NM 2004 4 7 TSAA0353212 120031111A53306545849 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED DOUBLER AND FILLER FROM .063 INCH, 2024-T3. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS EPR FIGURE 1. REPAIR COMPLETED IAW ECO 3391. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20031105000232003110500023SO 2003 11 5 C2XA03SH389 120031016A532014522178005 SILL EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV-DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20031106001902003110600190NM 2003 11 6 SWAA032278 120031016A53306546596 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, BELOW STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031106002292003110600229NM 2003 11 6 ASAA0310479 120030520A532065516983 SPLICE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE STRINGER SPLICE AT FUSELAGE STATION 887-934, STRINGER 24L CORRODED. REPLACED STRINGER SPLICE PER SRM. (M) 2L72 4F A16WE 20031103000922003110300092WP 2003 11 3 ABXA030380 120031002A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 AFT SERVICE DOOR JAMB UPPER AFT CORNER 3 INCHES X 8 INCHES AREA OF LIGHT SURFACE CORROSION AND A .1875 INCH CRACK AT FASTENER HOLE ON EXTERIOR FUSELAGE SKIN. REPAIRED AREA (REMOVED LIGHT SURFACE CORROSION, TRIMMED OUT CRACK, FABRICATED DOUBLERS -19, -21 AND FILLER -23, INSTALLED) IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-20D, AND REA D853-48038MR. 2L74 4F 4A25 20031106002242003110600224NM 2003 11 6 ASAA0310457 120030515A53116546527 FRAME BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 PAE - DURING C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 420, STRINGER 23L-24L DENTED. REMOVED DAMAGE AND REPAIRED FRAME PER SRM. (M) 2L72 4F A16WE 20031112000852003111200085NM 2003 11 12 C1HA200394034 120031107A5347 SEAT TRACK BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 SEAT TRACK AT BS 689.5 - 741 LBL 24.75 HAS CORROSION AND WORN AREAS. 2L73 4F A3WE 20030917001032003091700103NM 2003 9 17 GAIA03046SP 120030719A53146518636378 KEELBEAM BOEING727 7272J0 138407ENM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND RIGHT WHEEL WELL BS 870 AND KEEL BEAM, VERTICAL STIFFENER CRACKED FASI N/R 35583. REPLACED VERTICLE ANGLE, P/N 65-18636-378 IAW B727 SRM 51-30-2. (M) 2L73 4F RTA3WE 20030918000242003091800024NM 2003 9 18 GAIA03042SP 120030719A5347BAC1520792 SEAT TRACK BOEING727 727* NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED LBL 45 BS 720D FASI N/R 36068. REPLACED DAMAGED PARTS 90 INCHES LONG P/N BAC1520-792 AND BAS 1593-100122 IAW B-727 SRM 53-10-5 FIG 1. (M) 2L73 4F RTA3WE 20031009001022003100900102EU 2003 10 9 180131 120030917A2731 MOTOR SAAB SF340 SF340A 7850100EU ELEVATOR TRIM INOPERATIVE A UHLAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 GL17118SD 118 FLT 4588 PIT-IPT. DURING CLIMB OUT AND DESCENT FLIGHT CREW NOTICED THAT THE MAIN ELEVATOR WARNING LIGHT WAS ILLUMINATED. THE CREW FOLLOWED THE QRH AND DISCONNECTED THE AUTO-PILOT, THEY THEN NOTICED THAT THE MAIN ELEVATOR TRIM WAS INOPERATIVE AND NOT TRIMMING AT ALL. A/C RETURNED TO PIT AND TAKEN OUT OF SERVICE AT 1735(LT) 2L72 4T RTA52EU 20031119001432003111900143NM 2003 11 19 QXEA200301231 120031003A5510 MOUNT BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 300 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX- HORIZONTAL STABILIZER FORWARD MOUNT SHIMS SHOW SIGNS OF SHIMS SEPARATING AND STARTING TO CURL. REPAIRED IAW Q400 SRM TASK 55-10-00-000-801. 2H72 4T4 TRTA13NM E00062EN 20031121000432003112100043NM 2003 11 21 SWAA032515 120031113A2730REP4M6 BEARING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATORS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR CONTROL ROD AFT BEARINGS PER MM 2L72 4F RTA16WE 20040106002222004010600222NM 2004 1 6 SWAA032689 120031208A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 PHX - DURING SCHEDULED C4 CHECK FOUND SKIN CRACK AT BS 520 STRINGER 12R. REPAIRED CRACK PER SRM. (M) 2L72 4F RTA16WE 20040112000932004011200093WP 2004 1 12 AALA20031248 120031110A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGNECY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21573AA 53092 DFW - DURING OVERNIGHT MAINTENANCE, FUOND OVERHEAD EMERGENCY PATH LIGHTS FORWARD OF AIRSTAIR DOOR INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY PATH LIGHTS FORWARD OF AIRSTAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040113000972004011300097NM 2004 1 13 F3LA200300184 120031219A2612472622 MODULE BOEING737 73736N 1384408NM FIRE DETECTION FAULTY A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 2985 28563 DURING C-7 CHECK, INSPECTION REPORTED FIRE WARN LIGHT ON P-7, ENG 1/2 OVERHEAT LIGHTS ON P-8 AND CONTROL CABIN ALARM BELL DID NOT OPERATE IN STEPS 1 G-3 AND 1 G-7 OF FIRE WARNING SYSTEM TEST. TEST 1 G-10 PASSED. REPLACED FIRE DETECTION MODULE PER MM 26-10-01. PERFORMED ENGINE FIRE DETECTION OPERATIONAL TEST PER MM 26-11-00 AND CHECKED GOOD. PERFORMED APU FIRE DETECTION OPERATIONAL TEST PER MM 26-15-00 AND CHECKED GOOD. 2L72 4F RTA16WE 20031124001262003112400126NM 2003 11 24 GAIA03149ST 120031024A53117075T6 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME DENTED IN RADIUS BS 680 ABOVE STRINGER 17 RT. REF FASI N/R NR 61832, CUT OUT DAMAGE 1 INCH BY 1 INCH AND INSTALLED REPAIR DOUBLER 8 INCH BY 6 INCH PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20031216000512003121600051NM 2003 12 16 SWAA032537 120031117A3350101110 LENS BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 LT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20031217001942003121700194 2003 12 17 AALA20031326 420031124A2565 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR MALFUNCTIONED A AALAK NONE O OTHER ININSP/MAINT 1 SW21553AA 53083 L2 DOOR SLIDE INADVERTENTLY AND UNSUCCESSFULLY DEPLOYED BY CABIN SERVICE. DRIVER OPENED AFT SERVICE DOOR WHILE SLIDE WAS ARMED. RUG TRUCK PLATFORM PREVENTED FULL DEPLOYEMENT OF SLIDE. REPLACED SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20031218001492003121800149NM 2003 12 18 HNAA0300076 120031113A533085320313 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE BUCKLED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07914HA 53 A/C SUFFERED HARD LANDING RESULTING NUMEROUS AREAS OF BUCKLED FUSELAGE SKIN ON LHS. REPAIR IS TO HEAVY WINDOW BETWEEN THE F/SPAR AND R/SPAR. 2H72 4T RTA13NM 20031222000802003122200080NM 2003 12 22 GAIA03162OP 120031119A33501000679 LIGHT BOEING727 727224 1384076NM COCKPIT INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW0769739 20667 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20031229001312003122900131EA 2003 12 29 MASA200300467 120031128A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777302 7302 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MX RELAMPED. 2L72 4F RTA21EA 20031231000312003123100031NM 2003 12 31 TSAA0233261 120031221A335086210151 BATTERY PACK BOEING737 737209 13844AENM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 REPLACED NR 1 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040106000182004010600018WP 2004 1 6 DHL2003802559 120031124A532047518202 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 UPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 822.500 RBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 822.500 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201844 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040106001892004010600189NM 2004 1 6 AALA20031226 120031105A33501722331 CONNECTOR BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21376AN 25445 SFO - DURING OVERNIGHT MAINTENANCE, FOUND SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32H INOPERATIVE. REPLACED CONNECTOR FOR SEAT 32H MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031015000632003101500063NM 2003 10 15 USAASB03151 120030825A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US 23992 MAINTENANCE REPORTED THE LEFT MID-CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY PER MM 33-51-51. OPS CHECKS GOOD. (M) 2L72 4F RTA16WE 20040106002312004010600231WP 2004 1 6 GTIA031034 120031030A711059306451 ACCOUSTIC LINER DOUG DC9 DC983 3022083WP NR 1 NOSE COWL CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND CORRODED ACOUSTIC PANEL FORWARD AND AFT SECTION NR 1 ENGINE NOSE COWL. REMOVED NR 1 ENGINE NOSE COWL. INSTALLED SERVICEABLE NR 1 ENGINE NOSE COWL. (M) 2L72 4F RTA6WE 20040120000162004012000016NM 2004 1 20 P5CA0301008 120031220A7312A26602 VALVE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 1 ENGINE FAILED A P5CAO OTHER J WARNING INDICATION CLCLIMB 1 WP23923FT 22769 702032 NR 1 ENG FUEL HEAT FAILED IN OPEN POS WITH ICING LIGHT ON, FUEL TEMP MAX. PER FIM 73-01-00 PG 203 FOUND ZERO VOLTAGE AT SOCKETS BAND ON FUEL HEAT VLV CONNECTOR. REMOVED AND REPLACED FUEL HEAT VLV IAW MM 73-14-01, OPS NORMAL ON ENG RUN. 2L74 4F4 FRTA20WE E3NE 20040120000172004012000017NM 2004 1 20 XNOA1172 120031220A2121 COOLING FAN BOEING727 727100 1384036NM LT A/C PACK FAILED A XN0AO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23704A 19504 LT A/C PACK FILLS COCKPIT WITH SMOKE. TRANSFERRED TO DMI 3727 PER ENA MEL 21-5-2 CAT "C" PLACARDS INSTALLED. R&R LT PACK COOLING FAN, OPS CHECKS GOOD IAW B-727 MM 21-52-91. THIS CLEARS DMI 3727 PLACARDS REMOVED. (CLOSED) 2L73 4F RTA3WE 20031202000192003120200019SO 2003 12 2 ASOA03467 120030929A3350AD2047 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11267AS 120198 DURING A HANGAR INSPECTION IN HOT, THE FORWARD SECTION OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20031203001112003120300111NM 2003 12 3 USAA030233 120031026A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US48550 23319 FOUND SKIN CRACKED 1.4 INCH LONG, STATION 727D PLUS 2 INCHES BELOW S23R. INSTALLED DOUBLER PER EA 94836. (M) 2L72 4F RTA16WE 20031204001592003120400159EU 2003 12 4 MALA030466 120030929A5753 FLAP TRACK BAC 146 AVRO146RJ85A1500097EU RT WING CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 DURING C2 INSPECTION IN CWA, FOUND RIGHT FLAP POSITION TRACK NR 2 AFT LINK FWD PIN CORRODED. FOUND RIGHT FLAP POSITION TRACK NR 2 AFT LINK BUSHING CORRODED. MAINTENANCE REPLACED PER EO AD020307. REFER TO 409 189962, 63, AND 64 FOR ADDITIONAL INFORMATION. 2H74 4F RTA49EU 20031209000892003120900089NM 2003 12 9 SWAA032355 120031025A53126516300 BULKHEAD BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 201, RBL 5.5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20031209001042003120900104NM 2003 12 9 SWAA032333 120031023A335065C27095 BATTERY PACK BOEING737 7372H4 138448CNM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 R2 DOOR EMERGENCY LIGHT BATTERY PACK WOULD NOT CHARGE. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20031210001072003121000107NM 2003 12 10 03FDEA01997 120031128A5712 RIB DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT WING LOWER WINGLET INTERIOR RIB FOUND CRACK AT THE FWD EDGES. 2L73 4F RTA22WE 20030918000412003091800041NM 2003 9 18 GAIA03039SP 120030719A5753 SKIN BOEING727 7272J0 138407ENM TE FLAP DEBONDED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 DURING C-CHECK, FOUND LEFT WING OUTBOARD AFT FLAP T/E DISBONDED AREAS BETWEEN WBW .348 AND WBL 442 FASI N/R 35939. CUT OUT DELAMINATED AREAS, FABRICATED FILLER FROM MATERIAL 2024-T3 .016, PO NR 209415 DIM 6.75 INCH BY 7 INCH. FABRICATED DOUBLER FROM MATERIAL 2024-T3 .016, PO NR 209415 DIM 8.25 INCH BY 10 INCH. INSTALLED IAW B727 SRM 57-50-1, 57-50-2 FIG 4, 51-40-6 FIG 1. (M) 2L73 4F RTA3WE 20030918000682003091800068NM 2003 9 18 PCAA0308089 120030801A3350 CONNECTOR DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHTSLOOSE A PCAAK NONE O OTHER NRNOT REPORTED 1 EA13814EX 318 CREW REPORTED THAT THE EMERGENCY LIGHTS FLICKER ON AND OFF IN FLIGHT. MAINTENANCE CLEANED AND INSPECTED THE CONNECTOR ON THE EMERGENCY LIGHTS CONTROL BOX. OPERATIONAL CHECK WAS GOOD ON THE GROUND. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP MAINTENANCE REPLACED THE EMERGENCY LIGHTS CONTROL BOX LATER THAT DAY. 2H72 4T RTA13NM 20030919000922003091900092EU 2003 9 19 36020109031 120030109A2110590008 COMPRESSOR SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE AIR CONDITIONER LEAKING E S4WAK NONE K FLUID LOSS ININSP/MAINT 1 WP07820NA106 3602 22342 AIR CONDITIONING COMPRESSOR LEAKING AT INPUT SEAL. 1G71 3U3 U H9EU E00054EN 20040713000912004071300091CE 2004 7 13 S2YA03034 120031129A275011436103227 GUIDE BEECH 1900 1900D 1154162CE SWITCH FAILED A S2YAO OTHER O OTHER APAPPROACH 1 GL1381SK UE81 FLT 1655 - GRB-CWA - DURING FLIGHT, THE CREW SELECTED 17 DEGREES OF FLAPS BUT TH FLAPS CONTINUED TO 35 DEGREES. MAINTENANCE INSPECTED THE FLAP SYSTEM WHICH OPERATED NORMALLY AND FOUND FLAP SWITCH PANELS DETENTS TO BE WORN. MAINTENANCE REPLACED THE PANEL AND INSPECTED A/C BECAUSE OF THE FLAP OVERSPEED, NO FURTHER DEFECTS WHERE NOTED. (M) 2L72 4T RTA24CE 20041202000992004120200099 2004 12 2 MASA200300504 420031221A2210701700082407 COMPUTER EMB 145 EMB145LR 3260212SO AUTOPILOT INOPERATIVE A MASAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SW07843MJ113175647 145478 CREW REPORTED AUTO-PILOT DISCONNECT IN-FLIGHT DUE TO AN IC600 FAULT. MX REPLACED THE IC600 COMPUTER. OP CHECKS GOOD. 2L72 4T RTT00011AT 20060801001022006080100102WP 2006 8 1 IXXA060553S 120031006A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION 1748 LONGERON 10 RIGHT. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-1, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20030813001612003081300161NM 2003 8 13 SWAA031671 120030725A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 EEPLS LOOSE AT ROW NR 8. REMOVED AND REPLACED EEPLS STRIP AT ROW NR 8 PER MM. 2L72 4F RTA16WE 20030814000122003081400012NM 2003 8 14 SWAA031724 120030801A533065C2084333 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT LOWER AFT CORNER OF AIRSTAIR CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030818000242003081800024SW 2003 8 18 HEEA088457 120030708A2841206063633101 INDICATOR BELL 206 206L3 1182108SW FUEL QTY STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03129MR 51129 FUEL QTY INDICATOR STICKS. 1G71 3U H2SW 20030819001212003081900121EA 2003 8 19 03222627 120030810A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 DURING MAINTENANCE INSPECTION THE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OVERHEAD EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20030819001422003081900142EA 2003 8 19 SWIA200312148 120030625A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 FS 193 ELECTRICAL BAY LT FLOOR CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE IAW CRJ REO 601R-53-11-081 REV NC. 2L72 4F4 FRTA21EA E15NE 20030819002002003081900200NM 2003 8 19 SWAA031777 120030807A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 363, BETWEEN STR 13R AND STR 14R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030820002242003082000224NM 2003 8 20 USAASB03102 120030705A3350110049 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, P/N 201301A, AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20030402000412003040200041NM 2003 4 2 2003UALA00318 120030325A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 CABIN BODY FRAME STRINGER CLIP IS CRACKED AT BS 706, STR 4R. MAJOR REPAIR ACCOMPLISHED. NEW CLIP INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030820001042003082000104NM 2003 8 20 UPS03241052 120030806A3350 LIGHT BOEING727 72725C 138400HNM DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 L-1 DOOR EMERGENCY LIGHT TEST INOPERABLE. REMOVED AND REPLACED AND CKD OK USED AMERICAN AIRLINES BORROWED PART MM 33-50-01 P/N ON OFF 10-0067-9, S/N OFF 7012 S/N ON 22921. 2L73 4F A3WE 20030821000562003082100056NM 2003 8 21 03FDEA00830 120030526A5753 BUSHING DOUG MD11 MD11 3023602NM TE FLAP HINGE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LEFT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD AFT FLAP - HINGE FOUND HYDRAULIC ACTUATOR ROD-END MOUNT HOLES BUSHINGS LT AND RT LOOSE. LOOSE BUSHINGS AT LT AND RT OF ACTUATOR MOUNT HOLES REPLACED WITH OVERSIZED BUSHINGS AS PER FEDEX EA 1-5750-69348 - WINGS - LEFT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030401001802003040100180WP 2003 4 1 DHL2003873002 120030226A3510 HOSE DOUG DC8 DC873F 302199FWP OXYGEN MASK KINKED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01873SJ 46091 FIRST OBSERVERS 02 MASK DOES NOT ALLOW O2 TO FLOW IN NORMAL ONLY IN EMERGENCY. FOUND O2 MASK HOSE KINKED BEHIND REGULATOR. UNKINKED AS REQUIRED. FIRST OBSERVERS 02 MASK OPS CHECKED NORMAL IAW DC8 M/M 35-10-8. 2L74 4F RT4A25 20030414000342003041400034NE 2003 4 14 S03228014 220030322A7320 ENGINE BOEING747 747209B NM PWA JT9 JT9D7R4G2 52054NE NR 4 FLAMED OUT W SAJFO OTHER AJ FLAME/FIRE WARNING INDICATION CRCRUISE 1 WP03 24308 CREW REPORT NR 4 ENGINE FLAMED OUT IN FLT DUE TO NO FUEL SUPPLY INITIAL INVESTIGATION FOUND NO.4 CROSSFEED VALVE STUCKED AT CLOSE POSITION AND CAUSED NR 4 MAIN FUEL USED UP. INITIAL ACTION. MAR/24, IAW AMM 28-22-00, REPLACED NR 4 CROSSFEED VALVE ACTUATOR AND FUEL TRANSFER TEST NORMAL. MAR/24, IAW AMM 72-00-00, PERFORMED NR 4 ENG WINDMILL INSPECTION NORMAL. PARTS SENT TO VENDER FOR INVESTIGATION. 2L74 4F4 FRTA20WE E3NE 20030415000322003041500032NE 2003 4 15 CA030318008 220030306A8530 CYLINDER HEAD DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE ENGINE SEPARATED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CYLINDER HEAD SEPARATION FROM BARREL AD 78-08-07 1H71 3R3 R A806 5E1 20030416001072003041600107NM 2003 4 16 SWAA030785 120030406A5754 SKIN BOEING737 7373H4 1384600NM LT & RT SLATS DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED D-CHECK, FOUND NR 2 AND NR 5 L/E SLATS DELAMINATED. REPAIRED NR 2 AND NR 5 L/E SLAT PER SRM. 2L72 4F RTA16WE 20030425000312003042500031EU 2003 4 25 RAIA00303077 120030318A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03554HK 41067 STL- FLOOR ESCAPE PATH LIGHTING OUT ROWS 4 - 6. MAINTENANCE RESECURED LOOSE CONNCETOR AT LIGHTING STRIP, OPS CHECK OK. 2L72 4T RTA41NM 20030502000452003050200045WP 2003 5 2 ASAA0380157 120030224A532199365531 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED DAMAGED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F A6WE 20030505000562003050500056SO 2003 5 5 C2XA03SH108 120030421A532014521725013 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 SHV-DURING C-CHECK THE RIGHT HAND SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20030502000222003050200022WP 2003 5 2 ASAA0380135 120030215A5313124288688869 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, SECTION ON LONGERON CORRODED IN AFT CARGO BAY AT FS 1255. REPLACED DAMAGED SECTION OF LONGEORN PER SRM 51-30-5 AND 53-02. (M) 2L72 4F A6WE 20030506000732003050600073WP 2003 5 6 03FDEA00570 120030421A5753 SUPPORT DOUG DC10 DC1030 3023501WP RT O/B FLAP CRACKED A FDEAO OTHER O OTHER LDLANDING 1 SO25320FE 47835 RIGHT O/B FLAP I/B HINGE FAIRING SUPPORT STRUCTURE CRACKED LWR AFT END OF HINGE. CLOSING ACTION ON 04/15/03. REMOVED SUPPORT STRUCTURE IAW SRM 51-31-01, FOUND -T- ANGLE CRACKED. REMOVED -T- ANGLE IAW SRM 51-31-01. SENT TO FAB, FAB SUPPORT AND -T- ANGLE ON TRAVELER T2/326984. INSTALLED REPAIR PARTS IAW SRM 51-31-01. PAINTED PARTS IAW FED-EX ENG REPORT 99-15 REV B. 2L73 4F A22WE 20030506001492003050600149CE 2003 5 6 A832003F00000 120030325A323315257003 ACTUATOR CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP MLG FAILED B A83RA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1724VB 6500121 ON TAKEOFF, THE LANDING GEAR WAS RETRACTED. THE LOW HYDRAULIC ANNUNCIATOR LIGHT ILLUMINATED. FLIGHT CREW LANDED BACK AT AIRPORT. ON INSPECTION HYDRAULIC FLUID WAS LEAKING IN LEFT MLG WHEEL WELL. FURTHER INSPECTION NOTED THE LEFT MLG HYDRAULIC ACTUATOR HAD A 7 INCHES LINER CRACK ON THE 9 INCHES CYLINDER BODY ASSEMBLY. THE UNIT WAS SCRAP. ASSY MFG DATE FEB 86 FLUID TYPE MIL-H-83282. OPERATOR PRESSURE 3000 PSI. NOTE: PN 9914170. UNIT FAILED 203 LDS, 139 HRS SINCE INSTALLED. MAIN GEAR LOCK SIDE BRACE REPLACED. (SEE NR 200214240) 2L72 4F4 F A9NM E6WE 20030506002322003050600232WP 2003 5 6 ASAA0380208 120030304A532052929169 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING 30K CHECK, RIGHT FORWARD FLOOR PANEL SUPPORT IS CORRODED AT FS 180. REPLACED SUPPORT TRACK PER SRM 51-30-2 AND 30-5. (M) 2L72 4F A6WE 20030507001692003050700169CE 2003 5 7 CGO2003F00004 120030328A8097SM400D791 RELAY RAYTHN390 390 CE LT ENGINE INOPERATIVE B CGORO OTHER O OTHER NRNOT REPORTED 1 GL031XT 125 RB36 TROUBLESHOT COMPLAINT OF LT ENGINE NOT CRANKING. FOUND 80K1 LT ENGINE START RELAY COIL NOT ENERGIZING OR CLOSING CONTACTS WITH POWER TO COIL INPUTS. REPLACED RELAY, STARTER CRANKING OPERATIONS NORMAL. HAVE NOTED THIS SAME COMPONENT TO BE CAUSE OF SIMILAR FAILURE ON OTHER AIRCRAFT. AIRCRAFT AND PART TT: 125.9 HOURS. 17 2 3F RTA00010WI 20030507002132003050700213NM 2003 5 7 S03J32009 120030226A3260284U119581 BRACKET BOEING747 747400 NM LT MLG WW MISINSTALLED W SAJFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP03 1263 B-18705 AFTER A/C TOOK OFF, CAPTAIN CALLED BACK: LT MLG TILT MESSAGE CAME ON. CHECK TILT SENSOR FUNCTION NORMAL. INSPECTION FOUND CLEARANCE BETWEEN SENSOR AND TARGET OUT OF LIMITS. BECAUSE THE TARGET BRACKET WAS IMPROPERLY INSTALLED. REINSTALLED GEAR TILT TARGET BRACKET. ADJUSTED CLEARANCE IAW AMM 32-61-22,PFM L/G OPER TEST NORMAL. FWD THIS EVENT TO TRAINNING DEPARTMENT AS A TRAINNING MATERIAL. 2L74 4F RTA20WE 20030508000342003050800034WP 2003 5 8 DHL2003802006 120030503A2612 CONNECTOR DOUG DC8 DC873 302199CWP FIRE LOOP DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01802DH 46076 NR 2 ENGINE FIRE DETECTOR SHORT CIRCUIT LIGHT CAME ON (LOOP "A") DURING TAXI, OK ON LOOP "B". DEFERRED PER MEL 26-2-3, CONTROL 12777. REF. DMI 12777 - NR 2 ENGINE FIRE DEFECT SHORT CIRCUIT LIGHT CAME ON (LOOP "A") DURING TAXI. OK ON LOOP "B". TROUBLESHOT FOUND ENGINE WIRE HARNESS RIDING "A" LOOP CONNECTOR & WIRE ON FORWARD INBOARD SIDE OF NR 2 ENGINE FAN COWL SECTION. ADJUSTED WIRE BUNDLE PER M/M 20-50-0. OPS CHECKED NORMAL. CLEARED DMI 12777. A/C OK FOR SERVICE. 2L74 4F RT4A25 20030514000422003051400042EA 2003 5 14 COMA0360225 120030501A3230 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01927CA 7031 LANDING GEAR DISAGREE WARNING, NLG INDICATED UNSAFE. COULD NOT DUPLICATE. MLG AND NLG PRIORITY VALVES WERE REPLACED FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20030513002332003051300233NM 2003 5 13 SCNA03001 120030423A3350 LIGHT BOEING737 7378Q8 13844BXNM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15801SY 30332 BULL NOSE EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. RELAMPED - OPS CHECKED GOOD 2L72 4F RTA16WE 20030515001152003051500115EA 2003 5 15 SWIA200311929 120030504A7830 SWITCH CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07432SW 7548 RECEIVED A RIGHT THRUST REVERSER UNLOCKED MESSAGE IN FLIGHT. NO CONTROLABILITY PROBLEMS. RAN QHR PROCEDURE. OPERATION NORMAL. MEGGED WIRES 2KE59B20 AND 2KE23N22 FROM STOW SWITCH PINS 3 & 5. CHECK OK. REPLACED STOW SWITCH PER MM 78-37-01. SYSTEM OPS CHECK OK. P/N: 228-50741-115. 2L72 4F RTA21EA 20030530001122003053000112NM 2003 5 30 CA030507006 120030504A3260841005 PSEU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG MALFUNCTIONED W O OTHER J WARNING INDICATION DEDESCENT 1 CA 1961719617 (CAN) PRIOR TO LANDING , RT MLG GEAR DOWN LIGHT ILLUMINATED WITHOUT GEAR SELECTION AND GEAR WAS NOT DOWN. INTRANSIT LIGHTS ILLUMINATED AND STAYED ON. NO WARING HORNS. GEAR SELECTED DOWN AND LOCKED NORMALLY. IN TRANSIT LIGHT REMAINED ON. MAINTENANCE UNABLE TO FAULT DURING GROUND GEAR SWINGS. PSEU AND LANDING GEAR SELECTOR REPLACED ON SPECS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030602000012003060200001NM 2003 6 2 HALA0300292 120030430A5270 SWITCH BOEING767 76733A 1385209NM APU DOOR INOPERATIVE A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13580HA 28140 APU FAULED TO START. APU DOOR LIGHT CAME ON, NO APU FAULT LIGHT, NO RPM OR EGT. T/S PER FIM 49-11-00/101, FIG 104 BLOCK 24A HIGH RESISTANCE AT PIN 7 OF RELAY DS47. REPLACED DOOR SWITCH, RESISTANCE NOW NORMAL. APU STARTED NORMAL THREE TIMES. SWITCH REPLACED PER MM 49-15-02-4. OK FOR SERVICE. (M) 2L72 4F RTA1NM 20030529000562003052900056SW 2003 5 29 HEEA086643 120030521A3246412050015110 SKID BELL 412 412 1182202SW MLG CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 SKID TUBE CRACKED AT LOW RING MOUNT HOLE. 1G72 4U H4SW 20030605000312003060500031EA 2003 6 5 A6WA200340073 120030504A5320 STRIKER CNDAIRCL600 CL6002B19 1900309EA DOOR SEAL DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31422AW 7341 DAMAGE AT EXISTING REPAIR ON PASSENGER DOOR SEAL STRIKER FS 310, LOWER FRAME/LATCH. REMOVED DAMAGED SECTION OF SEAL STRIKER AND INSTALLED A NEW SECTION OF SEAL STRIKER IAW REO 601R-52-11-008 ISSUE B. (M) 2L72 4F RTA21EA 20030604000422003060400042SO 2003 6 4 SIMA200312718 120030422A532014521725013 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21709GB 145211 THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB SRM 51-40-02. (M) 2L72 4F RTT00011AT 20030611000182003061100018WP 2003 6 11 GTIA030326 120030506A3397 WIRE DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE EMERGENCY LIGHT UNSECURE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 L1 DOOR EXIT IDENTIFIER, INOPERATIVE. T/S AND FOUND POWER WIRE NOT SECURED. SECURED POWER WIRE. 2L72 4F4 F A6WE E2EA 20030611000692003061100069NE 2003 6 11 HEEA086553 120030522A7500650852402 VALVE SKRSKYS76 S76A 8143006NE BLEED SYSTEM POPPED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03762P 760060 END OF SWIVEL FITTING POPPED OFF WHEN INSTALLING. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030612001312003061200131NM 2003 6 12 UPS03440777 120030519A5313 STRINGER BOEING747 747200 1384847NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FWD CARGO COMPT BELOW FLOOR BIGLE SURFACE STRINGER END TO SKIN SURFACE FOUND CORROSION CRACK AT STA 820 TO STA 823 STG 47L. CORROSION BLEND OUT 0.060 X 0.5 X 0.5 INCH BS 820-830 STRINGER S47L REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F RTA20WE 20030617000952003061700095NM 2003 6 17 QXEA200300662 120030530A242131708001A GENERATOR DHAV DHC8 DHC8202 2809007NM NR 2 ENGINE FAILED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09367PH7997 1922 511 SEA- ON FLIGHT 2043 ABORTED TAKEOFF NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030520000942003052000094NM 2003 5 20 2003F00263 120030318A3350 LIGHT BOEING727 727200 138407ENM FWD GALLEY BROKEN A GUUAK NONE O OTHER ININSP/MAINT 1 SO11910PG 22606 EMERGENCY LIGHTING BY FORWARD GALLEY AFT SIDE BROKEN. RE-INSTALLED FORWARD GALLEY EMERGENCY STRIP IAW 25-30-344. (M) 2L73 4F RTA3WE 20030521001332003052100133WP 2003 5 21 DHL2003801030 120030423A57405769859163 FITTING DOUG DC8 DC873F 302199FWP LT STUB WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH78807 46033 LT STUB WING UPPER SURFACE ZEE PAN WITH 2.000 INCH CRACK STA XS 250.089. REMOVED DAMAGED ZEE PAN FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE PAN FITTING IAW SRM 51-3-0 PG 1 SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030523000932003052300093WP 2003 5 23 MWEA030225 120030519A523059101419 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 MID CARGO DOOR INNER PAN IS CRACKED FORWARD END JUST BELOW TORQUE TUBE FITTING. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20030617001082003061700108SW 2003 6 17 HEEA087290 120030611A6710407001523101 IDLER ASSY BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 BELLCRANK HOUSING WORN/BEARING ROUGH. TO BE SENT TO MFG. 1G71 3U3 UO H2SW E1GL 20030617002432003061700243NM 2003 6 17 QXEA200300585 120030514A5320 SUPPORT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - LEFT HAND COCKPIT BULKHEAD HAS CHAFED VERTICAL SUPPORT MEMBER AT STATION X-39 X Y33L. REPAIRED IAW HORIZON AIR EA 6-53-254. 2H72 4T RTA13NM 20030618002042003061800204NE 2003 6 18 HEEA087521 220030610A73239550171990 SWITCH AEROSPAS355 AS355* EU TMECA ARRIELARRIEL2B NE LOW FUEL LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03973AE 3229 LOW FUEL SWITCH LEAKING FROM VENT HOLE. TO BE SENT TO VENDOR. 1G72 3U3 U H11EU E00054EN 20030623000832003062300083EU 2003 6 23 USAASA03044 120030519A335032145510 BATTERY PACK AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19182UW 1536 LAX - THE PASSENGER MID AFT EMERGENCY POWER SUPPLY BATTERY PACK WAS FOUND INOPERATIVE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030620000462003062000046WP 2003 6 20 GTIA030383 120030519A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND CABIN STATION 182 UPPER SURFACE CORRODED FS 234-241, CUSP. CUT OUT DAMAGE IN WEB. DRILLED AND LOCATED WEB AND REPAIR DOUBLER. INSTALLED WEB AND DOUBLER. (M) 2L72 4F A6WE 20030701000182003070100018SW 2003 7 1 HEEA087872 120030610A2510407370720101 RESTRAINT BELL 407 407 1182206SW COCKPIT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 RESTRAINT WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20030707001192003070700119NE 2003 7 7 6370103 220030311A7230BRR20791 COMPRESSOR WHEEL GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE RT ENGINE CRACKED E E7JAO OTHER O OTHER NRNOT REPORTED 1 NE03509QS 637 DISCOVERED DURING SCHEDULED MAINTENANCE. RT ENGINE FAN DISK FOUND CRACKED WHILE PERFORMING SCHEDULED NON DISTRUCTIVE TESTING IAW AD AND MFG SB. FAN DISK PN BRR20791, SN CTDK 7185 ENGINE TYPE BR700-710A1-10, SN 11386. REMOVED LP FAN MODULE 31, PN M31-113, SN 31101204, TSN 1374.2 CSN 589. INSTALLED LP FAN MODULE 31, PN M31-113, SN 31101175, TSN 878.9, CSN 395. CRACKED MEASURED APPROXIMETLY ONE QUARTER INCH IN LENGTH. 2L72 4F4 FRTA12EA E00057EN 20030714000832003071400083NM 2003 7 14 SWAA031341 120030615A3350AD20131A CHARGER BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAULTY A SWAAO OTHER N FALSE WARNING CRCRUISE 1 SW29368SW 26579 CABIN EMERGENCY EXIT LIGHTS CAME ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20030714001352003071400135NM 2003 7 14 DHL2003754012 120030702A3233 SWITCH BOEING727 727223 1384074NM MLG ACTUATOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01754DH 22008 RIGHT MAIN GEAR DOOR LIGHT AND S/O PANEL AND RED DOOR LIGHT ON FORWARD PANEL ARE ILLUMINATED WHEN GEAR WAS LOWERED FOR LANDING 3 GREEN GEAR LIGHT. VISUAL INSPECTION INDICATED DOOR CLOSED. ADJUSTED AND CLEANED ACTUATOR SWITCH. OPERATED SEVERAL TIMES. OPS CHECKED GOOD PER M/M 32-34-00. 2L73 4F A3WE 20030207001402003020700140NM 2003 2 7 QXEA0300010 120030102A5542 SKIN BOMBDRDHC8 DHC8401 1390041NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX3241 4048 PDX - AIRCRAFT HAS A 7.5 INCH CRACK ON THE RIGHT SIDE OF THE TRAILING RUDDER. MAINTENANCE REPAIRED THE CRACK IN THE RUDDER SKIN IAW EA 6-55-22. 2H72 4T RTA13NM 20030114000352003011400035NM 2003 1 14 SWAA030022 120030106A53116546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20030127000722003012700072GL 2003 1 27 HEEA083646 220030114A75106899080 VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL BLEED AIR SYS LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 VALVE LEAKS DURING ENGINE START UP. REPAIRED. 1G71 3U3 UO H2SW E1GL 20030127000992003012700099EA 2003 1 27 COMA0360044 120030127A5743 BUSHING CNDAIRCL600 CL6002B19 1900309EA WS 13.10 RT DISPLACED A COMAO OTHER O OTHER ININSP/MAINT 1 SO01967CA16115 7134 DURING THE ACCOMPLISHMENT OF COMAIR EO 32-068 THE AFT BUSHING OF THE RIGHT MAIN LANDING GEAR ACTUATOR SIDE STAY SHAFT WAS DISPLACED.INSTALLED OVERSIZE BUSHING P/N 601R57-21-153-11 I/A/W BOMBARDIER REO 601R-57-21-153 REV. NC. 2L72 4F RTA21EA 20030127002812003012700281NM 2003 1 27 MWEA030027 120030109A5320993053875 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CUSP MEMBRANE CORRODED RIGHT SIDE AT STATION 492 AT LIGHTING HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20030128001692003012800169WP 2003 1 28 ZW0A0300804 120030107A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ZW0AK NONE O OTHER ININSP/MAINT 1 CE13951U 49245 DURING CHECK-C MAINT FOUND A CORRODED CABIN FLOOR SUPPORT CAP AT STA 1250, LBL 22 TO 44. REMOVED CORRODED CAP. CLEANED AREA AND FABRICATED AND INSTALLED NEW CAP PER SPM 6-70-01. 2L72 4F A6WE 20030129000052003012900005SW 2003 1 29 HEEA083915 120030117A6220407001524105 BELLCRANK BELL 407 407 1182206SW M/R HEAD DEBONDED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 MAIN ROTOR HEAD BUFFER WASHER, RUBBER DEBONDING. 1G71 3U O H2SW 20030210000492003021000049EA 2003 2 10 QXEA0300032 120030108A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 PDX- FORWARD CARGO BAY CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030218001772003021800177NM 2003 2 18 QXEA0300169 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 4 SEAT TRACK HAS SCRATCHES AT STATION 380-390. REPAIRED IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030220001752003022000175NE 2003 2 20 ARWA20030111 220030131A7532563883 BLEED VALVE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE FAILED A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO19784AL67537419 461635 645355 ON TAKE-OFF UNABLE TO ATTAIN MAXIMUM POWERN ON NR 2 ENGINE WITH THROTTLE FIRE WALL EPR 1.36 N1 98 N2 95 FIREWALL POWER. AIRCRAFT ABORTED TAKE-OFF AIRCRAFT RETURNED TO BLOCK. REMOVED AND REPLACED SURGE BLEED VALVE IAW MM 75-30-3. PERFORMED OPERATIONS CHECK AND TEST OF NR 2 ENGINE SURGE BLEED VALVE IAW MM 75-30-3 AND MM 71-0. OPS CHECK FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20030224000382003022400038 2003 2 24 HEEA084159 420030212A3434 LENS SKRSKYS76 S76A 8143006NE MARKER LIGHT MISSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 5845 760035 AMBER LENS MISSING. FOUND AMBER LENS BROKEN. ALSO 3 EACH HOOD COVERS MISSING. REPLACED LENS AND HOOD COVERS. REPAIRED. BENCH CHECK GOOD. 1G72 3U H1NE 20030116001562003011600156 2003 1 16 HEEA083097 420030108A345713824120234 RECEIVER BELL 206 206L1 1182107SW GPS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0320898 45721 FUNCTION BUTTONS REQUIRE 2-3 PUSHES THE CHANGE FUNCTION. SOME BUTTONS HAVE MARKINGS WORN OFF. ALL FUNCTION BUTTONS AND SWITCHES BAD. ALSO FOUND DISPLAY LENS BAD AND D12, D16 AND D42 BACKLIGHTING BULBS BAD. REPLACED ALL FUNCTION BUTTONS AND SWITCHES, DISPLAY LENS AND D12, D16, D42 BULBS. REPAINTED FACEPLATE AND UNIT BENCH CHECK GOOD. 1G71 3U H2SW 20030121001462003012100146GL 2003 1 21 HEEA083310 220030109A751023007827 SOLENOID VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ANTI- ICE SYSTEMDAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033207Q 51540 SOLENOID VALVE CAUSING CIRCUIT BREAKER TO POP AND SMOKE. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20030304000212003030400021EU 2003 3 4 BAQA084129 120030213A5320365A38301402 SUPPORT AEROSPAS365 AS365N2 8680815EU UNKNOWN WORN H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01915ME1500 6417 BEARING IN END OF BAR WORN TO LIMITS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U RTH10EU 20030305000032003030500003 2003 3 5 HEEA084608 420030214A3442MI585202 INDICATOR BELL 412 412 1182202SW ANT PEDESTAL NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WEATHER RADAR MAKES LOUD NOISE DURING OPERATION. ADJUSTED B305 MOTOR AND REPLACED NEGATOR SPRINGS. BENCH CHECK GOOD. 1G72 4U H4SW 20030305000122003030500012NM 2003 3 5 2003UALA00203 120030224A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 FUSELAGE EXTERNAL SKIN IS DENTED AND CRACKED AT BS 1520, STRINGER 23R. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED WITH DOUBLER. 2L72 4F4 FRTA2NM E17NE 20030225000962003022500096EA 2003 2 25 COMA0360119 120030221A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA A COMAL ABORTED APPROACH JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01917CA 7017 FLIGHT 5623 GEAR DISAGREE WARNING - NLG DID NOT EXTEND.COULD NOT DUPLICATE. EXTENSION AND RETRACTION CHECKS WERE NORMAL. 2L72 4F RTA21EA 20030228000132003022800013 2003 2 28 SWAA030436 420030221A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD ENTRY DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20030303000872003030300087NE 2003 3 3 HEEA084518 220030214A732325249995 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 HIGH SIDE GOVERNOR FAILURE. REPAIRED. 1G72 4U4 U H4SW E22EA 20030310000682003031000068SW 2003 3 10 HEEA084972 120030227A3213412050045107 CROSSTUBE BELL 412 412 1182202SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K4892 36001 MLG CROSSTUBE HAS MECHANICAL DAMAGE BEYOND LIMITS. SCRAPPED. 1G72 4U H4SW 20030314001632003031400163CE 2003 3 14 S2YA03002 120030120A3230101388008 VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA HYDRAULIC SYS INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13891SK20481 UE89 SHORTLY AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT THE GEAR DID NOT RETRACT. THE CREW DID AN AIR-TURN-BACK AND HAD AN UNEVENTFUL LANDING. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE HYDRAULIC SERVICE VALVE. MECHANIC OPS CHECKED THE SYSTEM WITH NO FURTHER DEFECTS AND RELEASED THE AIRCRAFT BACK TO SERVICE. 2L72 4T3 TRTA24CE E2NE 20030122002152003012200215 2003 1 22 HEEA083556 420030113A3444 COAX BELL 206 206L3 1182108SW RADAR ANTENNA DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 13907 51131 RADAR ALTIMETER ANTENNA COAX CONNECTORS DAMAGED (SHIELD BROKEN). SCRAPPED. 1G71 3U H2SW 20030122002202003012200220SW 2003 1 22 HEEA083560 120030113A6220206011100105 ROTOR HEAD BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116L 51529 SLINGING GREASE FROM OUTBOARD SEAL WHITE GRIP. REPLACED HUB ASSY. 1G71 3U H2SW 20030317001102003031700110NM 2003 3 17 03FDEA00269 120030304A5510 NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 29R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 2L73 4F RTA22WE 20030319000252003031900025 2003 3 19 GTIA030048 420030127A2565 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND TAILCONE ESCAPE SLIDE LANYARD MISSING. INSTALLED LANYARD. (M) 2L72 4F A6WE 20030418000502003041800050WP 2003 4 18 UPS03840185 120030204A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C1, STATION 280-300 LONGERON 28L IS CORRODED BEYOND LIMITS. REMOVED LONGERON 28L FROM STATION 265 TO 290, FABRICATED AND INSTALLED LONGERON SECTION, INSTALLED 2 LONGERON SPLICES AND REPLACED 2 BATHTUB FITTINGS IAW DWG 9754913 AND SRM 53-2-2 FIG 10, 53-2-0 FIG 2D. 2L74 4F RT4A25 20030418000862003041800086EU 2003 4 18 MALA030162 120030219A7997 WIRE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE OIL TEMP IND BROKEN A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15448XJ 340B448 IN CRUISE ON FLIGHT 3086, RT OIL TEMP PEGGED INFLIGHT. FOLLOWED QRH ALL OTHER INDICATIONS NORMAL. AIR RETURN TO MSP. MAINTENANCE REPAIRED BROKEN WIRE AND REPLACED CANNON PLUG, OPS CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20030327001042003032700104SO 2003 3 27 C2XA03CL018 120030119A2120 SMOKE EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714998 145302 CLE FLIGHT 2059 THE CREW REPORTED A LAV SMOKE WARNING WITH A LIGHT HAZE OF SMOKE WITH ANTI-ICE SYSTEM ON. THE HAZE CLEARED WITH ANTI-ICE SYSTEM OFF. MAINTENANCE INSPECTED AND RAN ANTI-ICE SYSTEM TESTS AND WAS UNABLE TO DUPLICATE HAZE OR SMOKE. ALL INDICATIONS WERE NORMAL. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20030731001142003073100114NM 2003 7 31 QXEA200300804 120030624A5514 SHIM BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - PEEL SHIMS EXTRUDING AT RIGHT HAND FORWAD V-STAB TO H-STAB CONNECTION POINTS. REPAIRED IAW Q400 AMM TASK 55-10-60-000-801, PAGE 3, PARAGRAPH 3. 2H72 4T RTA13NM 20030805000692003080500069SO 2003 8 5 ASOA03249 120030604A3397M2275941249 WIRE EMB 120 EMB120 3260201SO EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11239AS 120057 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ABOVE THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE WIRES TO THE EMERGENCY LIGHT BEHIND THE CEILING PANEL DISCONNECTED AND RE-CONNECTED THEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4T RTA31SO 20040225000992004022500099EU 2004 2 25 MALA040130 120031219A5330 SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 DURING 4K INSPECTION, AIRCRAFT HAS A DENT ON RT ICE GUARD 3RD SECTION FROM BOTTOM. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER AND TRIPLER REPAIR IAW MESABA EO NR S53194, DATED 09 JAN 04. 2L72 4T RTA52EU 20030716001152003071600115NE 2003 7 16 HEEA088045 120030704A63217665009803105 MODULE SKRSKYS76 S76A 8143006NE ROTOR BRAKE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03792P 760193 ROTOR BRAKE MODULE INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1G72 3U H1NE 20030718000032003071800003NM 2003 7 18 TSAA0333126 120030531A335086210066 BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHTSINOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13807AL 23443 REPLACED NR 4 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20030722001162003072200116 2003 7 22 SWAA031424 420030627A2565D31354 SLIDE BOEING737 7373H4 1384600NM FWD PAX DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20030826000732003082600073EU 2003 8 26 3144012703 120030127A62203500A31191600 STARFLEX SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE MAIN ROTOR WORN E S4WAK NONE O OTHER NRNOT REPORTED 1 WP075226R1813 3144 22043 YELLOW STARFLEX BUSHING WORN AT JOINT. 1G71 3U3 U H9EU E00054EN 20030829000312003082900031NM 2003 8 29 CALA0300489 120030824A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294.5, RBL 41. THE FLOORBEAM UPPER CHORD SECTION WAS REMOVED AND A NEW UPPER CHORD WAS INSTALLED IAW SRM 53-10-51. 2L72 4F RTA16WE 20030725000352003072500035EU 2003 7 25 RAIA00305149 120030521A7712 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU TORQUE INDICATORDIRTY A RAIAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 CE03572HK 41091 ENGINE NR 1 TORQUE INDICATION ERRATIC. MAINTENANCE CLEANED CONNECTOR ON NR 1 ENGINE TORQUE RING. 2L72 4T RTA41NM 20030728000562003072800056NM 2003 7 28 SWAA031613 120030720A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, WL 208 AND LBL 11 TO RBL 11. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20030812000202003081200020NE 2003 8 12 HEEA088367 120030712A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR ERODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03761PH8093 760224 PRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OR TAIL ROTOR BLADE. 1G72 3U H1NE 20030813001722003081300172NM 2003 8 13 SWAA031682 120030728A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (5 EA) AT BS 727B AT STR 7L, BS 663 AT STR 10L, BS 500D AT STR 8L, BS 380 AT STR 8L AND BS 360 AT STR 5L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030904000142003090400014 2003 9 4 2003UALA00519 420030625A3442 TRANSCEIVER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE WX RADAR SYS INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29474UA 1475 RETURNED TO FIELD DUE TO INOPERATIVE WEATHER RADAR. INOPERATIVE WEATHER RADAR CAUSED BY FAULT IN RECEIVER/TRANSMITTER. RECEIVER/TRANSMITTER REPLACED. SHOP TEST CONFIRMED PREAMP FAILURE IN RECEIVER/TRANSMITTER. 2L72 4F4 FRTA28NM E40NE 20030904000522003090400052EA 2003 9 4 SWIA200312258 120030811A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07441SW 7602 (STAB TRIM CH 1 INOP) MESSAGE DURING CRUISE, WOULD NOT ENGAGE. REMOVED AND REPLACED PILOTS STAB TRIM DISCONNECT SWITCH WITH A SERVICEABLE UNIT IAW MM 27-41-30. OPS CHECKS GOOD. 2L72 4F RTA21EA 20030908002082003090800208EA 2003 9 8 SWIA200312294 120030719A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 589 + 605 TRANVERSE BEAM ANGLES LBL 42 CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R-35011-13 2L72 4F RTA21EA 20030813001422003081300142NM 2003 8 13 SWAA031755 120030806A532065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030814001032003081400103EU 2003 8 14 RAIA00306159 120030607A3350 SWITCH JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DEFECTIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03550HK 41039 EMERGENCY LIGHTS CAME ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT SWITCH. 2L72 4T RTA41NM 20030814001632003081400163WP 2003 8 14 GTIA030578 120030709A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FTW - FOUND WEB CORRODED STATION 236-256 RBL 44-54. REMOVED WEB. FABRICATED NEW WEB. INSTALLED NEW WEB. (M) 2L72 4F A6WE 20030725000062003072500006NM 2003 7 25 AWXA200300752 120030625A5315BAC1493308 CHANNEL BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK A .6875 INCH CRACK WAS FOUND ON STRAP LOWER SURFACE OF TRANSVERSE FLOORBEAM AT BS 328, BL 0. MAINTENANCE STOP DRILLED CRACK ON STRAP LOWER SURFACE OF TRANSVERSE FLOORBEAM AT BS 328, BL 0; FABRICATED A STRAP REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 PG 213-219, FIG 204. 2L72 4F RTA16WE 20030915000802003091500080 2003 9 15 BAQA089027 420030908A34215040017926 GYRO BOLKMS117 BK117B1 5626012EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 ATTITUDE INDICATOR DRIFTS 15 (+/-) DEGREES IN LEVEL FLIGHT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030915000792003091500079GL 2003 9 15 ALGA089030 220030908A725023032345 COUPLING CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL N1 GALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO N1 COUPLING FOUND TO HAVE INTERNAL SPLINES GALLED ON INSPECTION. 1Q71 3R3 U 2A6 E1GL 20030910000932003091000093NM 2003 9 10 MEX2003280 120030710A2741 MODULE BOEING757 7572Q8 1384972NM STAB TRIM MALFUNCTIONED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23301AM 30045 AIRCRAFT RETURNED TO GATE, EICAS STATUS MESSAGE ELEV ASYM. FIM PROCEDURE WAS PERFORMED WITH NEGATIVE RESULTS IAW 27-09-00 FIG 106 PAGE 150. THE STAB/TRIM ALL LOCK AND ASYM MODULE WAS INTERCHANGED IAW FIM PROCEDURE 27-09-00, ALL TESTS CORRECT. (M) 2L72 4F RTA2NM 20030910001672003091000167SO 2003 9 10 SIMA200321804 120030731A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB145/1142 REV 22, CHAPTER 53-24-02 FIG 201. (M) 2L72 4F RTT00011AT 20030911000332003091100033NM 2003 9 11 03FDEA01257 120030812A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 FASTENER HOLES ON FLOORBEAM LOWER SIDE OF FLANGE STA 560 LBL -25 WL 208 CORRODED. REMOVED CORROSION ON FLOORBEAM LOWER SIDE OF UPPER TEE BS 560, LBL 0-25, WL 208. REPAIRED IAW FED EX EA 7-5310-72311. 2L73 4F RTA3WE 20030926000872003092600087EA 2003 9 26 COMA0360391 120030828A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01409CA 7441 CABIN DOOR HANDLE CAUTION DURING T/O. COULD NOT DUPLICATE. DOOR OPERATION NORMAL. 2L72 4F RTA21EA 20031003000642003100300064SO 2003 10 3 C2XA03SH327 120030913A531014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031006001242003100600124NM 2003 10 6 AWXA200301062 120030908A33506104789 BATTERY PACK BOEING737 737277 1384570NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK, FUNCTIONAL CHECK OF EMERGENCY EVACUATION LIGHT SYSTEM FOUND THE RT OVER WING, RT AND LT EMERGENCY ESCAPE SLIDE, AND RT AFT WING (EXTERNAL) LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVER WING, AND RT AFT CARGO COMPARTMENT EMERGENCY LIGHT BATTERY PACKS, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD IAW T/C A1C33006. 2L72 4F RTA16WE 20031021002852003102100285NM 2003 10 21 CALA0300543 120030920A52106516479 GATE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE PAX DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717328 23458 INSPECTION FOUND R-1 DOOR UPPER GATE CORRODED. THE UPPER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20040113002392004011300239NM 2004 1 13 QXEA200301308 120031020A27423994001011 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM HORIZ STAB FAILED A QXEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM09405QX5053 4047 PDX-ON FLIGHT 2289, IDA-SEA FLIGHT DIVERTED TO PDX DUE TO PITCH TRIM CAUTION INFLIGHT. PITCH TRIM INOPERATIVE. TRIM INDICATION SHOWING FULL NU POSITION. OCCURRED AT FL 240 AT 240 KIAS; AUTO PILOT DISENGAGED WITH AUTO TRIM FAIL MESSAGE ON PFD. REMOVED AND REPLACED PITCH TRIM ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040204000862004020400086NM 2004 2 4 QXEA200301280 120031008A3220 ARM DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 700 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 NOSE LANDING GEAR TRAILING ARM GOUGED AND CHAFED OVER 3 INCH AREA ON BOTTOM FORWARD END. REPAIRED IAW RD8-32-289. 2H72 4T4 TRTA13NM E20NE 20040204001342004020400134CE 2004 2 4 DXTA200300147 120031024A326067420288 SPACER CESSNA750 750 2076810CE NLG MISSING E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07936QS 7500036 AFTER TAKE-OFF DURING GEAR RETRACTION ONLY THE LEFT MAIN RETRACTED, AN ATTEMPT WAS MADE TO CYCLE THE GEAR AND WHEN HANDLE WAS PUT IN THE DOWN POSITION THREE GREEN AND NO RED INDICATION NOTED, FOLLOWING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION. JACKED AIRCRAFT AND FOUND NLG STRIKER TO BE LOOSE, UPON FURTHER INVESTIGATION FOUND STRIKER TO BE MISSING SPACER AND DAMAGED. REPLACED NLG CAM AND SPACER IAW CESSNA 750 MM CHAPTER 32-20-02. COMPLIED WITH LANDING GEAR FUNCTIONAL TEST IAW MFG 750 MM CHAPTER 32-00-01, SERVICED HYDRAULIC RESERVOIR IAW CHAPTER 12 OF MFG 750 MM, OPERATIONAL CHECKED GOOD. 2L72 4J RTT00007WI 20031031000762003103100076NM 2003 10 31 DL757030842 120030912A5330143N36211 SKIN BOEING757 757232 1384965NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27660DL 24422 THE FUSELAGE SKIN WAS FOUND WITH 2 DEEP GOUGE BLENDS AT STRINGER 9L BETWEEN FS 760 & 778. THE DAMAGES WERE REMOVED WITH 2 CUTOUTS AND REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER/TRIPLER REPAIR PER ER/A 385646-14, REV A. 2L72 4F RTA2NM 20031028001372003102800137NM 2003 10 28 GAIA03101 120030910A5347 SEAT TRACK BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED AT BS 760, RBL 45.5. REF FASI N/R 53265, REPLACED SEAT TRACK RBL 45.5, BS 760 TO 840 PER B727 SRM 51-30-2. (M) 2L73 4F A3WE 20031031000182003103100018SO 2003 10 31 SWIA200312471 120030910A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07297SW 120327 LT ANGLE CRACKED COCKPIT ENTRY BELOW FLOOR. (DISCOVERED DURING C-CHECK INSPECTION) APPLIED DOUBLER TO LT BRACKET BELOW FLOOR AT COCKPIT IAW SRM120 51-10-02 . 2L72 4T4 TRTA31SO E20NE 20031103001172003110300117EU 2003 11 3 AWXA200301113 120030925A5420D54630462202203 ANGLE AIRBUS320 A320232 3930326EU LT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-07 CHECK A CRACK WAS FOUND ON THE LEFT PYLON PANEL ATTACH ANGLE. (PROFILE). MAINTENANCE CUTOUT AFFECTED AREA, FABRICATED A REPAIR PARTS, SPLICE AND FILLER. IAW A320 SRM 54-52-12 PAGE 215-220 FIG.203 SHEET 1 AND 2. 2L72 4F RTA28NM 20031105000672003110500067NM 2003 11 5 SWAA032282 120031017A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29782SA 29808 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED (10 EA) ROWS NR 1, 3, 5, 7, 8, 11, 12, 16, 17 AND 18. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040106001832004010600183NM 2004 1 6 SWAA032690 120031208A57536546431 STRUCTURE BOEING737 7373A4 1384585NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 PHX - DURING SCHEDULED C4 CHECK, FOUND OUTBOARD FOREFLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FOREFLAP PER MM. (M) 2L72 4F RTA16WE 20040112001142004011200114EA 2004 1 12 A6WA200340186 120031206A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA SUBFLOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 THE LEFT AND RIGHT SIDE UNDERFLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621, WL 73, LBL 40. REPAIRED LEFT AND RIGHT UNDERFLOOR SUPPORT STRUCTURE IAW BOMBARDIER, INC REO 601R-53-61-117 REV B. (M) 2L72 4F RTA21EA 20040113000582004011300058EU 2004 1 13 MALA030564 120031204A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4K INSPECTION IN LAKE CITY, FL, FS 294 LEFT SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 294 IAW MESABA EO A53060 DATED NOV 3, 2003, REV II. 2L72 4T RTA52EU 20040113001092004011300109EU 2004 1 13 BAQA091148 120031113A6210L621M1010054 BLADE UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE MAIN ROTOR WILL NOT BALANCEB BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME2141 0144 MAIN ROTOR BLADE WILL NOT BALANCE. INSTALLED CANNED UNITS OFF OF A/C. 1G72 3U3 U H88EU E34NE 20040112000522004011200052EA 2004 1 12 03356693 120031222A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27693BR 7761 DURING INSPECTION THE LT FORWARD OVERWING EMERGENCY LAMP WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20031121000892003112100089NM 2003 11 21 03FDEA01943 120031119A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 LEFT OUTBOARD FLAP, OUTBOARD HINGE FITTING ACTUATOR MOUNT HOLE INBOARD CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20031124000222003112400022EU 2003 11 24 03324315 120031120A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27315UE 41033 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING 3RD STRIP WAS FOUND INOPERATIVE. THE FAULT WAS FOUND TO BE A LOOSE CONNECTOR AND THE CONNECTOR WAS RESECURED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040114000752004011400075NM 2004 1 14 03FDEA01961 120031121A5510 BARREL NUT DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 HORIZONTAL STAB RIGHT UPPER AFT PLANK 35R BARREL NUT BORE FOUND CORROSION EXCEEDED EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STAB RT UPPER AFT PLANK 35 RT BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. 2L73 4F RTA22WE 20031218001662003121800166NM 2003 12 18 MWEA030466 120031203A5522991848061 SPACER DOUG MD88 MD88 3023688NM ELEVATOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FABRICATE SPACER FOR ELEVATOR SKIN REPAIR. FABRICATED AND INSTALLED SPACER. 2L72 4F RTA6WE 20031223001212003122300121EU 2003 12 23 MALA030546 120031202A2520 SEAT FRAME BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 DURING C-CHECK INSPECTION, FOUND SEAT 12B, 12D FRAME CRACKED. ACCOMPLISHED WELD REPAIR ON SEAT FRAME 12B, 12D IAW MESABA EO A25031 DATED 6 FEB 2001 REV IR. REFER TO 409 944800 FOR DETAIL. 2H74 4F RTA49EU 20031224000552003122400055NM 2003 12 24 GAIA03163OP 120031120A33501000679 LIGHT BOEING727 727223 1384074NM CABIN INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW076831 20184 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THA THE L1 DOOR EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE (M) 2L73 4F A3WE 20040106000672004010600067EA 2004 1 6 SWIA200312694 120031214A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB DIRTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07912SW 7595 STAB/MACH TRIM FAILED FFOD CHECKS. TRIM DISENGAGES DURING CH 2 TEST AND NOSE DOWN OPERATION. CLEANED STAB/TRIM DISCONNECT SWITCHES. OPS CHECK GOOD. 2L72 4F RTA21EA 20031231001172003123100117WP 2003 12 31 GTIA030917 120031101A5330 SKIN DOUG DC9 DC983 3022083WP FUSLEAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND FUSELAGE SKIN DENTED/GOUGED STATION 1250-1260 LONGERON 19R. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20030917001042003091700104EA 2003 9 17 ASOA03392 120030821A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WLS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WS 53-60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20030918000162003091800016NM 2003 9 18 03FDEA01513 120030911A532065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 STA 950D, STRINGER 2L CLIP IS CRACKED. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 950D, STR 2L PER SRM 51-30-2. 2L73 4F RTA3WE 20031008000282003100800028NE 2003 10 8 COMA0360412 220030915A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE LOW A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01914CA 7012 RT ENGINE LOW OIL PRESSURE WARNING 3 TIMES. FOUND ENGINE OIL SYSTEM 5 QUARTS LOW. SERVICED OIL SYSTEM. 2L72 4F4 FRTA21EA E15NE 20031007000412003100700041EU 2003 10 7 2003F00593 120030805A6720 COMPUTER BOLKMS117 BK117B2 5626013EU YAW INOPERATIVE A A1URA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 CE03880SL 7130 PILOT REPORTED YAW CSAS FAILURE EN ROUTE TO HOSPITAL. NO COCKPIT INDICATIONS, ONLY INTERMITTENT UNCOMMANDED TAIL ROTOR INPUTS. AIRCRAFT RETURNED TO BASE FOR MX. AFTER TROUBLESHOOTING YAW SYSTEM, FOUND YAW COMPUTER TO BE INOPERATIVE. REMOVED AND REPLACED COMPUTER, OPS CHECKS GOOD. (M) 1G72 3U NCH13EU 20040106000592004010600059EA 2004 1 6 COMA0360554 120031215A5753601R1430352 CAP CNDAIRCL600 CL6002B19 1900309EA T/E FLAP CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO01979CA16389 7159 RIGHT INBOARD FLAP LEADING EDGE VANE MIDDLE CAP P/N 601R14303-52 IS CHAFED .017 INCH AT FLAP STATION 60. REMOVED AND REPLACED CAP P/N 601R14303-52 IAW CRJ 200 SRM 51-42-10. 2L72 4F RTA21EA 20031202000472003120200047NM 2003 12 2 USAASB03185 120031017A335020121 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 MAINTENANCE REPORTED THE AFT LEFT ENTRY DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 2013-1A. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20031126000702003112600070NM 2003 11 26 AWXA200301480 120031122A2915651782120 MODULE BOEING737 737301 1384611NM HYD SYSTEM FAILED A AWXAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28326AW5797116711 23258 ON DESCENT, A-SYSTEM HYDS FAILED, A/C WAS TOWED OFF RUNWAY TO GATE. MX FOUND CHECK VALVE BLOWN OUT OF A-SYSTEM HYD PRESSURE MANIFOLD, R / R A-SYSTEM HYD PRESSURE MODULE ASSY IAW BMM. DUE TO LOSS OF FLUID REPLACED A-SYSTEM HYD EDP IAW T/C R5M29001, A-SYSTEM HYD ELECTRIC PUMP IAW T/C R4M29002, & A-SYSTEM HYD FILTERS, OPS & LEAK CHECK GOOD. TEARDOWN ANALYSIS OF HYD PRESSURE MODULE ASSY CONFIRMED FAILURE OF UNIT. FOUND UNIT IN OVERALL WORN CONDITION REQUIRING OVERHAUL, CHECK VALVE MISSING & WRONG P/N PRESSURE SWITCH INSTALLED. INSTALLED A NEW CHECK VALVE & REPLACED PRESSURE SWITCH, 10 EACH O-RINGS, 5 EACH BACK-UP RINGS, AND FILTER ELEMENT. 2L72 4F RTA16WE 20031203000522003120300052NM 2003 12 3 GAIA03154ST 120031024A5347BAC1520841 SEAT TRACK BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK LBL 24.75 BS 760 TO 850 CORRODED. REF FASI N/R NR 61875, REPLACED SEAT TRACK LBL 24.75 BS 760 TO 850 PER B727 SRM 51-30-2. (M) 2L73 4F RTA3WE 20040121000132004012100013NM 2004 1 21 03FDEA02267 120031226A5744ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING O/B FLAP I/B HINGE ACTUATOR O/B MOUNT I/B AND O/B SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040123000432004012300043 2004 1 23 KBM2003F00086 420031031A34241394T10072 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TURN COORDINATORNOISY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 TURN COORDINATOR MAKES LOUD SQUEEKING NOISE. MEL NR 10. 1G71 3U3 U H9EU E19EU 20031204000642003120400064EA 2003 12 4 COMA0360456 120031014A2613355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT PYLON CHAFED A COMAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SO01785CA 7326 FLIGHT 5808 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED BLEED LEAK SENSING ELEMENT IN PYLON. 2L72 4F RTA21EA 20031208001492003120800149SO 2003 12 8 C2XA03CL180 120031027A33503025101 LIGHT EMB 145 EMB145ER 3260211SO RT OVERWING INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714938 145029 DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20031209000302003120900030EA 2003 12 9 COMA0360470 120031025A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01796CA10650 7338 FLIGHT 5480 HYDRAULIC SYSTEM 8 LOW PRESSURE WARNING. REPLACED THE 3B HYDRAULIC PUMP. 2L72 4F RTA21EA 20031209000682003120900068NM 2003 12 9 SWAA032368 120031027A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 431, STR 26L, AND BS 512B, STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20031209001992003120900199WP 2003 12 9 MWEA030440 120031103A5310593666095 SPLICE DOUG DC9 DC981 3022081WP FRAME CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 AFT BAG PIT LEFT CARGO TRACK SPLICE PLATE CORRODED AT FRAME STATION 1212. FABRICATED AND INSTALLED SPLICE. 2L72 4F A6WE 20031209002392003120900239NM 2003 12 9 HNAA0300058 120031023A33506013211 BATTERY PACK DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT MALFUNCTIONED A HNAAO OTHER O OTHER CRCRUISE 1 EA07997HA 507 EMERGENCY LIGHT FLICKER INTERMITTENTLY DURING FLIGHT. REPLACED BATTERY PACK. 2H72 4T RTA13NM 20031209000412003120900041EA 2003 12 9 SWIA200312548 120031019A2400 SOCKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CALL LIGHT DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07466SW 7856 DURING TAXI OUT, WHEN F/A CALL BUTTON WAS SELECTED, BOTH CALL AND EMERGENCY ILLUMINATED ON PANEL, ALL LIGHTS BUT PA ILLUMINATED ON F/A'S PANEL. NO COCKPIT/CABIN COMM OR PA ANNOUNCEMENTS WERE POSSIBLE. FOUND A MELTED LIGHT SOCKET ON AFT OVERWING COCKPIT CALL LIGHT. REPLACED LIGHT SOCKET ASSY IAW CRJ WM 20-00-00. PERFORMED OPS CHECK OF P/A SYSTEM. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040126000492004012600049EU 2004 1 26 BAQA091231 120031129A3310LRA15 CONTROL UNIT UROCOPEC135 EC135P1 8680990EU INSTRUMENT LIGHTINOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH1783 0069 CONTROL UNIT HAS 5 VOC INOPERATIVE. PART REPLACED WITH SERVICEABLE UNIT. 01/08/2004 1G72 3U O H88EU 20030916000102003091600010NE 2003 9 16 S03279072 220030910A72611A6902 PACKING BOEING747 747200 1384847NM PWA JT9 JT9D7R4G2 52054NE NR 2 ENG GB LEAKING W SAJFE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP03 24308 NR 2 ENGINE OIL LOSS IN FLIGHT, CREW FOLLOW THE ABNORMAL PROCEDURE TO MAKE A IFSD BEFORE LANDING. GROUND CHECK FOUND OIL EXTERNAL LEAKING FROM MGB MCD AND THE PROBE WAS NOT INSTALLED PROPERLY. MAIN GEARBOX MCD PACKING REPLACED. RE-SERVICE OIL SYSTEM TO NORMAL LEVEL. ENGINE IDLE RUN TEST NORMAL. REFER TO EAR FOR FURTHER INFORMATION AND PREVENTIVE ACTION. 2L74 4F4 FRTA20WE E3NE 20031210001472003121000147WP 2003 12 10 AALA20031363 120031202A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21976TW 53626 RDU AFT VENTRAL STAIR AREA OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES FOR AFT VENTRAL STAIR AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA6WE 20031211001182003121100118NM 2003 12 11 AALA20031312 120031123A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 MIA SEAT 3B EMERGENCY LIGHT INOPERATIVE. REPLACED FIRST CLASS EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20031211001362003121100136EU 2003 12 11 AALA20031341 120031128A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW213075A 606 MIA EMERGENCY EXIT LIGHTS AT DOOR 3R INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT DOOR 3R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20030918000872003091800087CE 2003 9 18 IMJ2003F00001 120030620A2742 MOTOR LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP STAB ACTUATOR INOPERATIVE B IMJRO OTHER O OTHER NRNOT REPORTED 1 EA25511WP 183 CREW NOTICED SECONDARY TRIM (ON AUTOPILOT) DID NOT SEEM TO BE WORKING PROPERLY IN CRUISE. DISENGAGED AUTOPILOT AND TRIED TO TRIM MANUALLY. FOUND TRIM INOPERATIVE IN PRIMARY, SELECTED SECONDARY AND CONFIRMED IT WAS INOPERATIVE ALSO. AIRCRAFT WAS IN COMPLIANCE WITH AD 2003-06-51. BOTH SYSTEMS HAD PASSED PREFLIGHT CHECKLIST FUNC TEST. SUSPECT THAT BOTH ELECTRIC MOTORS WITHIN THE STAB TRIM ACTUATOR FAILED. THE UNIT WAS REPLACED ALONG WITH CONTROL BOX PRECAUTIONARY AND AIRCRAFT RETURNED TO SERVICE. BOTH COMPONENTS WERE RETURNED TO MFG IAW TECH SERVICE REQUEST. 2L72 4F4 FRTT00008WIE6WE 20030919000852003091900085NE 2003 9 19 HXS2003F00003 220030613A7200ARRIEL1B ENGINE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAKING METAL B HXSRA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 AL056094U3747 2751 4815 PILOT IN FLIGHT NOTICED AN ENGINE CHIP LIGHT. HE THEN LANDED AND THEN FOUND SMALL FLAKE OF WHAT APPEARED TO BE CARBON WHICH IS CLASSIFIED IN MFG MM AS CATEGORY ONE WHICH ALLOWS ONLY CLEANING OF THE PLUG AND CONTINUED SERVICE. PILOT TOOK OFF AND HEADED FOR HIS BASE. ON THE WAY THERE HE GOT ANOTER ENGINE CHIP LIGHT AND HE LANDED AT HIS BASE. THE DECISION WAS MADE TO GROUND THE AIRCRAFT AND CHANGE ENGINES. REMOVED ENGINE SN 4815 AND INSTALLED SN 477. ENGINE WILL BE SENT FOR EVALUATION AND REPAIR. 1G71 3U3 UNCH9EU E19EU 20030923001882003092300188WP 2003 9 23 AALA20030862 120030817A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217548A 53030 DURING OVERNIGHT MAINTENANCE, SEAT 7D AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED SEAT 7D EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040206000342004020600034SO 2004 2 6 SIMA200334408 120031117A532014500222001 PROFILE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE 145301 ABI - DURING A IMBV INSPECTION, THE RIGHT PROFILE AFT OF FRAME 18 WAS FOUND CORRODED BELOW LIMITS AROUND NUT PLATE. CUT OUT SECTION OF CORRODED PROFILE, PERFORMED NDT INSPECTION AND TREATED BARE METAL. FABRIATED A REPAIR ANGLE. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3289 DATED NOV 17, 2003. (M) 2L72 4F RTT00011AT 20040206000402004020600040WP 2004 2 6 ASAA0380827 120031216A53109707970 SHEAR TIE DOUG DC9 DC983 3022083WP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01950AS 53023 OAK - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT FS 1287. REPLACED SHEAR TIE PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040210000962004021000096EU 2004 2 10 USAA030296 120031122A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .150 SQUARE INCH AREA, FRAME 57.3 RBL 17.75. DAMAGED TRACK REMVOED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20040301000312004030100031EU 2004 3 1 PG92004F00010 120031102A5610350A25900400 WINDSHIELD UROCOPEC130 EC130B4 8680989EU COCKPIT CRACKED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19130PH439 3670 WINDSHIELD CRACKED. (RMA NR 045563) (K) 1G72 3U H9EU 20040301000862004030100086NM 2004 3 1 AMTA200301524 120031228A2611 CIRCUIT CARD BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE RT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL11516AT 27972 STATUS MSG RT ENG OH LP 2. SWAPPED LP 2 CARD WITH THE LP1 CARD ON ENG 2. PERFORMED BITE TEST. NO MESSAGE ON STATUS PAGE OR MECHANIC PAGE. 2L72 4F4 FRTA2NM A12EU 20031212001252003121200125NM 2003 12 12 AWXA200301431 120031027A575365C2630935 DOUBLER BOEING737 7373G7 1384595NM FLAP TRACK CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MINOR REPAIR - DURING C-13 CHECK A .75 INCH CRACK WAS FOUND ON NR 3 FLAP TRACK INNER STRAP (DOUBLER), AT AFT EDGE WBL 191. MAINTENANCE REMOVED CRACKED DOUBLER ON NR 3 FLAP TRACK WBL 191; FABRICATED A NEW REPLACEMENT DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 11. 2L72 4F RTA16WE 20040324000232004032400023WP 2004 3 24 ASAA0380689 120031020A53305936007501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01960AS 53074 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 1287. INSTALLED REPAIR DOUBLER PER SRM 53-04. 9M) 2L72 4F RTA6WE 20040413000422004041300042NM 2004 4 13 ASAA024017B 120030322A532069434772 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 PAE - DURING C-CHECK, FOUND CORROSION ON WEB AT BS 767-794. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040930001292004093000129EU 2004 9 30 A6WA200360069 120031209A5330 SKIN BAG BAE146BAE146200A 1500266EU FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVIT LOCATIONS. MAINTENANCE CUT OUT DAMAGE TO SKIN IAW BAE FAX BARA/AVR/6603/03-DC. NDT HFEC CARRIED OT IAW BAE FAX BARA/AVR/6603/03-DC, NO CRACKS NOTED. INSTALLED FREEZE PLUG IAW BAE FAX BARA/AVR/6603/03-DC. (M) 2H74 4F RTA49EU 20060801000642006080100064WP 2006 8 1 IXXA060530S 120030911A575157630902 FITTING DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND RT WING INBOARD AILERON INBOARD HINGE FITTING CRACKED. REMOVED CRACKED FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20030814000772003081400077NM 2003 8 14 CALA0300377 120030704A5330 SKIN BOEING737 737524 1384721NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716649 28910 THE FUSELAGE SKIN WAS FOUND DAMAGED AFT OF BS 1088 BETWEEN STRINGER 18L AND 20L. THE TRIM OUT TO REMOVE DAMAGE MEASURED 1.3 X 1.15 INCH. THE AREA WAS REPAIRED IAW ECRA 5330-03264. 2L72 4F RTA16WE 20030818000782003081800078SW 2003 8 18 HEEA088614 120030723A6420212011701101FM1 BLADE BELL 412 412 1182202SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03330088541 36004 HOLE IN BLADE OUT OF LIMITS. REPLACED BLADE 212-010-750-113, S/N A-12427, T.T. 1415:50 DUE TO HOLE. REPAIRED. 1G72 4U H4SW 20030819000912003081900091NM 2003 8 19 SWAA031768 120030806A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20030331000962003033100096NM 2003 3 31 CALA0300145 120030327A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED BETWEEN STA 816 AND 819. REPAIRED DOOR IAW SRM 52-00-01, FIGURE 203. 2L72 4F RTA16WE 20030820002182003082000218EA 2003 8 20 ASOA03337 120030725A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11861AS 7445 DURING A C-CHECK IN MCN, THE RIGHT AFT FUSELAGE CABIN AIR HOOKUP DOOR FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACD THE CRAFTED DOOR LAND IAW SRM 51. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030404000502003040400050NE 2003 4 4 DL757030182 220030222A7320DPN736001778 EEC BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE UNSERVICEABLE A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO27653DL 24393 716363 LT ENGINE PRIMARY CONTROL STATUS MSG, LT ENGINE FAILED. REPLACED NR 1 ENGINE EEC. PERFORMED WINDMILL INSPECTION ON ENGINE. NO DEFECTS NOTED. 2L72 4F4 FRTA2NM E17NE 20030402000112003040200011EU 2003 4 2 030903291 120030331A3350 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27329UE 41097 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FWD FLOOR EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030404001542003040400154NM 2003 4 4 SWAA030536 120030310A3350604222 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR AND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHTS BATTERY PER MM. 2L72 4F RTA16WE 20030410001022003041000102NM 2003 4 10 SWAA030674 120030323A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 506, STR 14L & BS 510, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030416002442003041600244SO 2003 4 16 C2XA03SH096 120030408A531014522460015 BUTT STRAP EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK, THE AFT DIGITAL BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 16 TO 18. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED DIGITAL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20030416003462003041600346EU 2003 4 16 RAIAOO301008 120030103A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03550HK 41039 SECTION OF PATH LIGHTS INOPERATIVE. RE-SECURED EMERGENCY PATH LIGHT CONNECTOR, OPS CHECK OK. 2L72 4T RTA41NM 20030423002012003042300201CE 2003 4 23 HYI2003F00003 120030305A8011642085A15R CLUTCH CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO STARTER FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NM0126632674 402C0404 823398R CREW REPORTED LEFT ENGINE FAILED TO START. MECHANIC REMOVED AND REPLACED STARTER CLUTCH. ON INSPECTION OF REMOVED STARTER CLUTCH, MECHANIC FOUND DRIVE GEAR TOOTH SHEARED. RECOVERED SINGLE TOOTH FROM OIL PUMP. RETURNED AIRCRAFT TO SERVICE AFTER FURTHER INSPECTION OF ACCESSORY GEARS. CLUTCH TO BE RETURNED TO MANUFACTURER FOR FURTHER EVALUATION. 1L72 3O3 O A7CE E8CE 20030428000602003042800060NM 2003 4 28 OZI2003F00005 120030117A5230001A535A6027200 FITTING DORNERDO32 DO328300 NM CARGO DOOR LATCHGOUGED A OZIAO OTHER O OTHER NRNOT REPORTED 1 SW07410Z 7126 3125 4 EA CARGO COMPARTMENT LATCH FITTINGS HAVE VARIOUS DEGREES OF GOUGE DAMAGE. 2H72 4T RTA55NM 20030429000892003042900089WP 2003 4 29 03FDEA00432 120030411A5230 SEAL DOUG DC10 DC1030 3023501WP CARGO DOOR TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 AFT PIT LOWER CTR DOOR SEAL TORN. CLOSING ACTION ON 04/11/03. NEW SEAL FAB ON TRAVELER T2/324829, LOCATED AND DRILLED IAW SRM 51-31-01, TREATED AND PRIMED IAW SRM 51-21-01, TO BE INSTALLED ON W/C 53SI1516-01. 2L73 4F A22WE 20030429000972003042900097NM 2003 4 29 CH1A200395012 120030410A5412 FIREWALL BOEING727 727290 138408WNM NR 2 NACELLE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 NR 2 ENGINE FIREWALL FIRE BOX CRACKED 2 PLACES 2L73 4F A3WE 20030429001132003042900113GL 2003 4 29 RAIA00304101 220030403A7532 BLEED VALVE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COMPRESSOR FAILED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03810HK 145231 RIC- AUTO TAKEOFF THRUST CONTROL, NO WARNING. MAINTENANCE CHANGED COMPRESSOR BLEED VALVE, OPS CHECK OK. 2L72 4T4 FRTT00011ATTE6CH 20030502002052003050200205NM 2003 5 2 UPS03M40441 120030315A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP INSPECTION TYPE: C, SEAT TRACK AT LBL 27.5 BETWEEN STA 824-840 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK LBL 27.5 AT STA 824-840 FOUND EXCEED LIMIT PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK & SPLICE REWORKED & HOLES PICK OUT AS PER SRM 53-70-00 VOL I REV 32 & PROTECTED AS PER SRM 51-21-01 VOL II REV 32. NEW SEAT TRACK & SPLICES INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 824-840 LBL 27.5. 2L73 4F RTA22WE 20030924000452003092400045NM 2003 9 24 DL757030759 120030816A3350 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27611DL 22818 FOUND BROKEN EMERGENCY LIGHTING WIRE UNDER SEAT 27F AND EMERGENCY SEAT MOUNTED LIGHTS INOP ROW 27 TO ROW 40 - REPAIRED WIRING 2L72 4F RTA2NM 20030924000912003092400091NM 2003 9 24 AWXA200300983 120030816A532069353521 STRINGER CLIP BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON TOP LEG OF STRINGER CLIP 21 RT, FORWARD SIDE OF BS 787. MAINTENANCE REMOVED CRACKED STRINGER CLIP 21 RT, BS 787; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, STEP 4B-4E, FIG. 007. 2L72 4F RTA16WE 20040202000172004020200017WP 2004 2 2 UPS04841710 120031231A53403755843502N FITTING DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, STATION 1228 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20040130000412004013000041NM 2004 1 30 SWAA032796 120031221A53106546533 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, RBL 10, WL 148.5. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20031215000762003121500076 2003 12 15 AWXA200301462 420031118A2565D30665105 LIGHT AIRBUS320 A320231 3930325EU EVAC SLIDE INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW259702637 091 PHX - EEL - DURING INSPECTION EMERGENCY LIGHTS FAILED TEST AT AFT LT EMERGENCY POWER SUPPLY UNIT. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE IAW R1C25304, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040407000722004040700072EU 2004 4 7 2004F00091 120030926A7120 MOUNT AIRBUS320 A320233 3930329EU NR 1 ENGINE DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07951LF 460 AT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT STOP SERIAL NR 0313-PTE HAS GOUGING IN BOLT HOLES. CLEANED NR 1 ENGINE FORWARD MOUNT STOP, S/N 0313. NO GOUGING NOTED. DIMENSIONS CHECKED AND FOUND TO BE WITHIN LIMITS. (M) 2L72 4F RTA28NM 20031216000902003121600090EA 2003 12 16 03332664 120031128A2540AE0405A02 FAN CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAILED A VTZAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 EA27664BR 7528 DURING APPROACH OF FLT NR 7678 TO ORD FROM FSD CREW REPORTED A LAVATORY SMOKE DETECTOR SOUNDING AND SMOKE IN THE CABIN. CREW COMPLETED LAVATORY SMOKE QRH AND SMOKE DISSIPATED. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. THE LAVATORY FAN WAS FOUND TO BE CAUSING THE SMOKE AND WAS REPLACED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040427000242004042700024WP 2004 4 27 FJT03102491 220031014A72503588251 BEARING LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP RT ENGINE FAILED E FJTAA UNSCHED LANDING RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 SO03249B 7146 3039 240 P74676 CREW REPORTED, A SLIGHT FLUX WAS NOTED IN RT ENG INSTRUMENTS. A CHECK OF EEC WAS PERFORMED WITH NO EFFECT. ENG CONTINUED WITH UNCOMMANDED SHUT DOWN, CREW ELECTED TO SHUT DOWN ENG AND LAND, AN EMERGENCY WAS DECLARED AND UNEVENTFUL LANDING WAS MADE. MAINT DISCOVERED METALLIC MATERIAL IN ENGINE OIL FILTER,OIL SAMPLE WAS OBTAINED AND SENT FOR TESTING. INVEST REVEALED THAT ENGINE COMPRESSOR AND FAN SECTIONS ROTATED FREELY. IT WAS NOTED THAT ACCY DRIVE SECTION WAS DIFFICULT TO TURN, METAL WAS NOTED ON ACCY GB DRAIN PLUG. ENGINE WAS DISASSEMBLED FOR EVAL AND IT WAS DISCOVERED THAT NR 5 BRG HAD FAILED AND SUBSEQUENTLY ALLOWED THE HP IMPELLER TO CONTACT ITS SHROUD. HP SHAFT AND NR 5 BEARING DAMAGED BEYOND REPAIR.2L72 4F4 F A10CE E6WE 20030926001482003092600148NE 2003 9 26 82703 220030827A8530116733 CYLINDER DOUG DC3 DC3C 3021457WP PWA R1830 R183090D 52020NE NR 1 SEPARATED E VLLAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 GL059923S 394 25964 17645 AT CRUISE POWER FOR OVER 5 HOURS IN ROUTE MWO-LRD LEFT ENGINE STARTED RUNNING ROUGH. AIRCRAFT DIVERTED TO AUS. FOUND NR 1 CYLINDER HEAD SEPARATED FROM THE BARREL. 2L72 4R4 R A669 5E4 20040722000032004072200003EU 2004 7 22 USAA040286 120031123A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 CLT - FOUND SEAT TRACK CORRODED .125 INCH LONG, FS 64 RBL 17.75. DAMAGE TRACK REMOVED AND REPLACED WITH NEW PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20030813000292003081300029 2003 8 13 HEEA088573 420030729A34224020936903 INDICATOR BELL 412 412 1182202SW GYRO 3-AXIS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 AFTER WARM UP, GYRO 3-AXIS INDICATOR WON'T SLAVE COMPASS CARD. SHOP REPAIR. 1G72 4U H4SW 20030331000082003033100008EA 2003 3 31 03086628 120030327A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27628BR 7240 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK AT SEAT ROW 1 WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CONNECTOR FOR THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030821000622003082100062NM 2003 8 21 03FDEA00929 120030619A5512ALC8100 SKIN DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 HORIZONTAL STAB UPPER FWD PLANK 14L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 B PT1 LIMITATIONS. HORIZONTAL STAB UPPER FWD PLANK 14L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT REWORK /REPAIR 1-5510-7-5000. 2L73 4F RTA22WE 20030821002052003082100205NM 2003 8 21 03FDEA00812 120030523A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 LEFT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP - HINGE ASSY FOUND PIVOT BEARING OUTBOARD BORE HOLE WITH MINOR CORROSION (ON FLAP SIDE). REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69347 - WINGS - LEFT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR. 2L73 4F RTA22WE 20030407000232003040700023WP 2003 4 7 ASAA0380090 120030117A5310SR095200089 SPACER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, AFT CARGO BAY DOOR LOWER BEAM SPACER IS CORRODED. REPLACED EXISTING DOUBLER PER SRM 51-30-5 AND 53-05. (M) 2L72 4F RTA6WE 20030407000642003040700064SO 2003 4 7 SIMA200300801 120030103A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 ABI - DURING AN IMBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWARD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION, TWO DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 (SRM 145/1142, REV 20) 53-21-10 PARA 4, AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20030407000072003040700007WP 2003 4 7 ASAA0380001 120030101A3350 POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 PDX - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN FIRST CLASS. REPLACED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. 2L72 4F A6WE 20030414000062003041400006NM 2003 4 14 SWAA030763 120030405A53106557463 FITTING BOEING737 7373G7 1384595NM GIRT BAR ATTACH CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/2 D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED GIRT BAR ATTACH FITTING PER SRM. 2L72 4F RTA16WE 20030416001702003041600170NM 2003 4 16 DLM88030315 120030401A3350 CHARGER DOUG MD88 MD88 3023688NM EMERGENCY LIGHTSFAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27913DE 49956 DURING LAYOVER, FOUND AFT SECTION OF EMERGENCY LIGHTS FROM SEAT 31 AFT WERE INOPERATIVE. REPLACED FUSE IN EMERGENCY LIGHT BATTERY CHARGER, NOW OP NORMAL. 2L72 4F RTA6WE 20030428001472003042800147NM 2003 4 28 AWXA200300352 120030407A274065C3475111A ACTUATOR BOEING737 7373S3 1384711NM HORIZONTAL STAB WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW285648440 23734 YVR - FLIGHT CONTROL - DURING C-16 CHECK THE HORIZONTAL STABILIZER MANUAL TRIM WAS FOUND TO HAVE 3/4 TURN SLACK IN EITHER UP OR DOWN DIRECTION. MAINTENANCE FOUND LT AND RT STAB HINGE FITTINGS FRETTING AROUND BEARINGS; REMOVED AND REPLACED LT AND RT HINGE FITTINGS AND BEARINGS IAW BMM 27-41-31, PG 401, AND ER 03-5512-03094-TB1. ALSO FOUND DRUM ON STAB TRIM ACTUATOR CAN BE TURNED 1/4 TURN WITHOUT MOVING JACK SCREW; REMOVED AND REPLACED STAB TRIM GEARBOX ACTUATOR IAW T/C R6C27008. FUNCTIONAL CHECK OF STAB TRIM SYSTEM C/W IAW T/C F6A27005. VENDOR TEARDOWN OF STAB TRIM ACTUATOR S/N KE000458 CONFIRMED FAILURE DUE TO NUMEROUS WORN PARTS. REPLACED WORN BEARINGS. 2L72 4F RTA16WE 20030429000282003042900028NM 2003 4 29 P5CA0300812 120030127A5347 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CRACK ON SEAT TRACK RBL-25 STA 910. DAMAGED PORTION FLOOR TRACK REMOVED, NEW PORTION FABRICATED H/F 7178-76511 EXTRU BAC 1520-1682 PER SRM 53-11-25 SRM 51-40-02 (7075T6 TMSGO) RIVETED PER SRM 51-30-02. 2L74 4F A20WE 20030430000092003043000009NM 2003 4 30 QXEA0300487 120030419A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - GOUGE ON FUSELAGE SKIN AT X57 AND STRINGER 31R. REPAIRED IAW HORIZON AIR EA 6-53-246 AND RD 8/4-53-529. 2H72 4T RTA13NM 20030430000702003043000070NM 2003 4 30 USAABB03049 120030322A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 4 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19630AU 27808 CLT - FOUND EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030430001942003043000194NM 2003 4 30 SWAA030932 120030427A53116546529 FRAME BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, BETWEEN STR 27R & STR 28R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20030505000672003050500067NM 2003 5 5 CALA0300213 120030422A5330 SKIN BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916642 28903 THE AIRCARFT FUSELAGE SKIN SUSTAINED LIGHTNING STRIKE DAMAGE AT STA 747 S1R AND STA 727 S1R. THE DAMAGE WAS IN THE FORM OF A .5 INCH CRACK AND A .1562 INCH HOLE. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2L72 4F RTA16WE 20030506000112003050600011WP 2003 5 6 03FDEA00535 120030418A2750D425TB PULLEY DOUG DC10 DC1030 3023501WP RIGHT WING BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 RT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. 2L73 4F A22WE 20030508000162003050800016NM 2003 5 8 DLM88030337 120030404A2910NAS161212A O-RING DOUG MD88 MD88 3023688NM RT HYD SYSTEM FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27940DL 49813 RT HYD QTY DROPPED FROM 10 QTS TO 4 QTS IN FLT WHEN RT SYSTEM WAS TURNED OFF QTY ROSE TO 15 WHEN RT SYS TURNED ON FOR LANDING SYS QTY DROPPED TO 1 QTY PRESSURE REMAINED GOOD. LEAK FROM RIGHT SYSTEM PRESSURE FILTER MODULE REDUCER - REPLACED O-RING. 2L72 4F RTA6WE 20030509000602003050900060EU 2003 5 9 AL05200301779 120030411A793070BM035410 MODULE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE INOPERATIVE B HXSRO OTHER O OTHER NRNOT REPORTED 1 AL056302Y1556 9007 9634 THE PILOT CALLED IN LOW OIL PRESSURE AND DECLARED AN EMERGENCY. LANDED THE HELICOPTER SAFELY. PRELIMINARY INVESTIGATION SHOWED THAT THE OIL EVACUATED OUT THE EXHAUST PIPE INDICATING LOSS OF LABYRINTH SEAL PRESSURIZATION. THE RETURN OIL STRUT TUBE HAD ALSO COKED SHUT, WHICH CAN ALSO CAUSE THE OIL PRESSURE TO OVERCOME THE LABYRINTH SEAL PRESSURE. THIS OIL STRUT RETURNS OIL FROM THE REAR MAIN BEARING. THIS MODULE IS POST TU MOD NR 274, 281, 283, AND 284. THIS IS A MODIFICATION BY FACTORY OF THE REAR BEARING HOUSING TO CHANGE OIL PRESSURES AT THE REAR BEARING TO PREVENT COKING. THIS MODIFICATION SET DISCONTINUES THE REQUIREMENT OF THE MANUAL CLEANING OF THE REAR BEARING. 1G71 3U3 U H9EU E19EU 20030509000812003050900081NE 2003 5 9 REX2003F00000 220030424A7261 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SCAV PUMP DISCONNECTED A REXAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO258532G 7532 GEE873056 ENROUTE, FLIGHT 5849 WAS LEVELING AT FL130 AND RECEIVED A RT ENG OIL PRESS MESSAGE ON EICAS. CREW CONTACTED MAINT AND SHUT DOWN RT ENGINE 2-3 MINUTES AFTER INITIAL MESSAGE, USING APPROVED CHECKLIST. CREW DECLARED AN EMERG WITH ATC AND WAS APPROVED TO CONTINUE TO DISTINATION. VISUAL APPROACH AND LANDING WITHOUT INCIDENT WAS MADE AT DTW. MAINT FOUND C-SUMP SCAVENGE LINE DISCONNECTED ON RT ENG. LINE HAD BEEN DISCONNECTED TO FACILITATE OTHER MAINT DURING A HANGER VISIT IN SBN PRIOR TO FLIGHT. ENG HAD BEEN LEAK CHECKED FOLLOWING MAINT IN SBN, WITH NO INDICATION OF LEAKS. LINE WAS RECONNECTED AND ENGINE WAS SERVICED WITH OIL IN DTW. FOLLOWING A SUCCESSFUL LEAK CHECK, A/C WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030508001262003050800126NM 2003 5 8 UPS03440621 120030414A531065B0831517 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C M/D- BS 1301 S15-16R FRAME SHEAR TIE CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20030513001702003051300170NM 2003 5 13 2003UALA00378 120030414A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 CABIN FLOORBEAM STA 947 UPPER CAP HAS FREEZE PLUG DRILLED INTO EDGE AT APPROXIMATE LBL 20. REMOVED, MANUFACTURED AND INSTALLED UPPER "T" CAP. 2L72 4F4 FRTA16WE E2GL 20030513001772003051300177NM 2003 5 13 C8GA20030009 120030420A3210 LANDING GEAR BOEING727 727223 1384074NM MAINS LACK OF LUBE A C8GAO OTHER J WARNING INDICATION APAPPROACH 1 SO15715AA 22470 DURING APPROACH, THE NOSE GEAR DID NOT EXTEND WHEN THE GEAR WAS LOWERED. GEAR WAS RECYCLED AND NOSE GEAR EXTENDED NORMALLY AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED, CLEANED AND LUBED NOSE GEAR MOUNTS, LINKS AND ACTUATOR MOUNTS. TROUBLESHOOT BY EXTENDING AND RETRACTING HYDRAULIC COMPONENT SYSTEMS. JACKED AIRCRAFT NOSE FOR GEAR EXTENSION AND RETRACTION TEST. CYCLED GEAR SIX FULL TIMES RETRACT AND EXTEND. OBSERVED NORMAL OPERATIONS FOR ALL TEST AND NO DEFECTS NOTED IAW B727 MM 32-33-0 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030529000742003052900074SW 2003 5 29 HEEA086516 120030521A80115034T70P04 SEAL BELL 214 214ST 1182106SW STARTER LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 STARTER SEAL LEAKING 2G72 4U H10SW 20030602001202003060200120 2003 6 2 SWAA031158 420030522A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20030514001252003051400125NM 2003 5 14 SWAA031036 120030508A3610332A13171 DUCT BOEING737 7373H4 1384600NM NR 2 ENGINE LOOSE A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29333SW 23697 DUAL AIR TURNBACK, NR 2 ENG OVERHEAT LIGHT ILLUMINATED WITH THROTTLE LEVER ADVANCEMENT. FOUND NR 2 ENG 9TH STG PNEUMATIC BLEED AIR DUCT MANIFOLD LOOSE. TIGHTENED DUCT MANIFOLD BOLTS PER MM. 2L72 4F RTA16WE 20030521001862003052100186WP 2003 5 21 DHL2003604523 120030429A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT OUTER WING INBOARD L/E FORMER CRACKED (0.500 INCH), STA 653.750. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030521001252003052100125NM 2003 5 21 C1HA200395062 120030515A3350 LIGHT BOEING727 727290 138408WNM OVERWING DISLODGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 EMERGENCY EXIT LIGHT IN THE AISLE OVERWING IS LOOSE AND CAME OFF EN ROUTE. 2L73 4F A3WE 20030611001372003061100137EA 2003 6 11 ASOA03205 120030510A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 FLT 4469 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT OVER THE RIGHT WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP OVER THE RIGHT WING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030612001362003061200136WP 2003 6 12 UPS03840724 120030505A53403649114U FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C-2, MAIN CABIN CORRODED FITTING CENTER WING BOX TO SHEAR WEB ATTACH FITTING STA 920 RBL 66 APX. REMOVED AND REPLACED FITTING AND INSTALLED IAW DC8 SRM 51-3-2 AND 51-1-20D. 2L74 4F RT4A25 20030612001892003061200189NE 2003 6 12 EIA2003075 220030514A7261 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 4 MALFUNCTIONED A EIAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09486EV 20888 685894 NR 4 ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE, AFTER SHUTDOWN ENGINE WINDMILLED FOR 20 MINUTES. REMOVED AND REPLACED NR 4 ENGINE PER WORKCARD F7201, F7202, F7203 AND F7207, OPS CHECK GOOD. 2L74 4F4 F A20WE E20EA 20030613000632003061300063NM 2003 6 13 UPS03440799 120030515A5314 STRUCTURE BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FX - KEELBEAM BOX EXTERNAL LOWER STRUCTURE LOWER SURFACE FOUND CORROSION AT STA 1255 TO STA 1260 RBL 7 TO RBL 9. CORROSION BLEND OUT 0.070 X 2 X 4 INCH. KEELBEAM LOWER STRUCTURE CORROSION REPAIR BETWEEN BS 1256 AND BS 1265, RBL 7 TO RBL 9 AS PER SRM 53-10-01 FIG 1, RS R53-49-35033 AND UPS ENG'R FILE 747-53-20143. 2L74 4F RTA20WE 20030528000532003052800053EU 2003 5 28 HEEA086739 120030522A632095460137520 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU GEARBOX LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03855PH 3351 GEARBOX MAGNETIC SEAL LEAKING. TO BE SENT TO VENDOR. 1G71 3U H9EU 20030528000972003052800097SW 2003 5 28 HEEA086606 120030521A6710212001035101 FORCE GRADIENT BELL 412 412 1182202SW CYCLIC FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 ATT MODE FAILED 2 SECOND BEEP TEST. REPLACED CAP 212-001-046-003 DUE TO WORN; ACTUATOR 212-001-048-001 DUE TO WORN. REPAIRED. 1G72 4U H4SW 20030618001452003061800145EA 2003 6 18 COMA0360269 120030611A3260 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01917CA 7017 FLIGHT 5233 GEAR DISAGREE WARNING DURING APPROACH. COULD NOT DUPLICATE. CLEANED AND LUBED NOSE LANDING GEAR. 2L72 4F RTA21EA 20030619000942003061900094SW 2003 6 19 HEEA087418 120030611A6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20030505000602003050500060NM 2003 5 5 CALA0300206 120030421A5320 WEB BOEING737 7373T0 1384582NM AFT BAG BIN CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717306 23357 INSPECTION FOUND AFT BAG BIN THRESHOLD WEB CORRODED IN SEVERAL SPOTS. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20030505001202003050500120EU 2003 5 5 AWXA200300404 120030407A5320D53475765204 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND AT 3 AREAS ON UPPER SURFACE OF THE AFT BULK CARGO DOOR SILL FROM BS 2829.6 TO 2882.9. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT DAMAGED AREAS OF AFT BULK CARGO DOOR SILL BS 2829.6 TO 2882.9; FABRICATED 3 EACH REPAIR FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW A320 SRM 51-41-99 PG 62, 103, 217-223, SRM 51-75-12 PG 4-5 AND SRM 51-21-11, PG 2-5. 2L72 4F RTA28NM 20030506001332003050600133WP 2003 5 6 GTIA030148 120030221A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE FUSELAGE DETERIORATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 FORWARD CABIN STA 200 TO 256 FLOOR PANEL SOFT/ MUSHEY DETERIORATED, CORR. INSERTS, LBR 22 TO LBR 44 (21X56). FABRICATED NEW PANEL. 2L72 4F4 FRTA6WE E2EA 20030507000752003050700075EU 2003 5 7 CA030411004 120030406A2913704A33690004 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HYDRAULIC PUMP CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING ROUTINE INSPECTION AME DISCOVERED HYDRAULIC PUMP BELT TO BE CRACKED (APPROXIMATELY HALF WIDTH). BELT WAS REPLACED AND A/C RETURNED TO SERVICE. 1G71 3U3 UNCH9EU E19EU 20030508000632003050800063EU 2003 5 8 03FDEA00670 120030502A2760 STRIP AIRBUS300 A300B4605R 3930308EU RT WING SPOILER CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25682FE 800 RT WING NR 3 SPOILER T/E STEEL STRIP CRACKED. R & R STRIP PER IPER IAW SRM 51-40-23 & 57-72-11.AND SRM 57-72-11 WO 22877 AT MAE. 2L72 4F RTA35EU 20030513002122003051300212SO 2003 5 13 C2XA03BT055 120030422A261114534156401 MODULE EMB 145 EMB145ER 3260211SO SMOKE DETECTOR INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2715948 145056 BAGGAGE SMOKE WARNING LIGHT ON OVERHEAD DOES NOT LIGHT UP DURING TEST. REMOVED AND REPLACED RELAY K0629 PLUS APU MODULE ASSY IAW EMB MM 26-13-10. OPS CHECK GOOD. RELAY IAW WMB MM CHAP 20. OPS CHECK GOOD. 2L72 4F RTT00011AT 20030604000012003060400001NM 2003 6 4 AALA20030511 120030429A2560 FLASHLIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21368AA 25195 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT AT RIGH MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT AT RIGHT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030604000392003060400039SO 2003 6 4 SIMA200312703 120030501A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21807AE 145506 DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED AN NDT INSPECTION AND FABRICATED AN INTERNAL DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT 1C2003-145/1485. (M) 2L72 4F RTT00011AT 20030604001262003060400126NM 2003 6 4 UPS03440541 120030413A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FLOORBEAM UPPER STRUCTURE CORROSION. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 3. CORROSION BLEND OUT 0.060 X 2 X 2 INCHES. EXCEED SRM LIMIT. 2L74 4F A20WE 20030604001432003060400143NM 2003 6 4 UPS03440563 120030412A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, BS 740 BET S24-25R FRAME FOUND CRACK. BS 740 STR 24R - STR 26R FRAME REPAIRED AS PER SRM 53-10-04 FIG.35 2L74 4F A20WE 20030520001172003052000117WP 2003 5 20 GTIA030268 120030410A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 FTW - DENT AT FS 373 BETWEEN LONGERONS 21 AND 22R, DENT IS WITHIN ONE INCH OF FRAME AND REQUIRES REPAIR. CUT OUT DAMAGED SECTION. FABRICATED 4 SKIN AND 6 AND 10 DOUBLERS. INSTALLED REPAIR SKIN AND DOUBLERS. (M) 2L72 4F RTA6WE 20030515000272003051500027EA 2003 5 15 SWIA200311912 120030303A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 RIGHT WING FUEL PANEL REBATES HAVE CORROSION UNDER PANELS 610AB, 640AB, 640CB, 640DB, 640FB, 650AB. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-57-21-030 REV A, UNDER PANEL 610AB MAX MAT'L LOSS .001, 640AB MAX MAT'L LOSS .007, 640CB MAT'L LOSS .010, 640DB MAX MAT'L LOSS .005, 650AB MAT MAT'L LOSS .001. HFEC INSPECTION C/W ON BLENDED WING FUEL TANK LID REBATES AS REQUIRED IAW REO 601R-57-21-030. NO CRACKS FOUND. REWORKED AREAS ROTO PEENED IAW CRJ SRM 51-24-11. 2L72 4F RTA21EA 20030610000952003061000095NM 2003 6 10 DL757030440 120030507A5330143N36504 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27613DL 22820 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION JUST ABOVE THE STRINGER 19R SKIN LAP JOINT AT FS 771. THE CORROSION WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384898-14, REV A. 2L72 4F RTA2NM 20030612000262003061200026SO 2003 6 12 C2XA03TY076 120030527A27614188009007 ACTUATOR EMB 145 EMB145ER 3260211SO SPEED BRAKE DEFECTIVE A C2XAB EMER. DESCENT I FLT. ATTITUDE INST. DEDESCENT 1 SW2714943 145040 TYS DURING A DESCENT INTO THE EWR AREA PILOT ENGLEBERT, FLIGHT 2560 HAD TWO UNCOMMANDED ROLLS TO THE RIGHT. A/C LANDED SUCCESSFULLY AND WAS FERRIED TO TYS. MAINT REMOVED AND REPLACED LT & RT PCA SOLENOIDS & LT & RT SPEED BRAKE ACTUATORS IAW AMM 27-12-01 AND 27-13-01. OPS AND LEAK CHECKS GOOD. A/C WAS REL. FOR TEST FLIGHT AND WAS TEST FLOWN SUCCESSFULLY WITHOUT ANY DEFECTS OR PROBLEMS AND WAS REL TO SERVICE. 2L72 4F RTT00011AT 20030617001222003061700122GL 2003 6 17 HEEA087460 220030612A74216899084 IGNITER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE BURNED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 DELAYED STARTS. IGNITER BURNED. REPLACED IGNITER. 1G71 3U3 UO H2SW E1GL 20030624000082003062400008EA 2003 6 24 A6WA200340078 120030528A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 PASSENGER DOOR SEAL STRIKER IS DAMAGED AT FS 349 MIDWAY TOP TO BOTTOM. REPAIRED DAMAGE TO PASSENGER DOOR SEAL STRIKER FS 349 IAW BOMBARDIER REO 601R-52-11-008 REV B. (M) 2L72 4F RTA21EA 20030630000732003063000073GL 2003 6 30 HEEA087835 220030620A753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 BLEED VALVE MAKING ENGINE RUN HOT. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20030707000482003070700048NM 2003 7 7 AALA20030499 120030426A3397 CONNECTOR BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21352AA 24033 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING AT 23B INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING WALL TO SEAT HARNESS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20030711000662003071100066WP 2003 7 11 CALA0300333 120030623A335041B030CF00101 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTINOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2792874 49122 INSPECTION FOUND THE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00, PAGE 407. 2L72 4F A6WE 20030711001112003071100111EA 2003 7 11 COMA0360300 120030626A2460 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYSTEMMALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01807CA 7364 FLIGHT 5595 HYDRAULIC PUMP 1B CAUTION MESSAGE. RESET CIRCUIT BREAKER. SYSTEM TEST NORMAL. 2L72 4F RTA21EA 20030714000612003071400061NM 2003 7 14 SWAA031363 120030618A3350AD20131A BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20030108000092003010800009WP 2003 1 8 MWEA030001 120030106A213039271411 VALVE DOUG DC9 DC981 3022081WP RIGHT PACK DEFECTIVE A MWEAC ABORTED TAKEOFF J WARNING INDICATION CLCLIMB 1 GL31806ME 48032 NOTICED RIGHT AIRPACK CYCLING ON AND OFF. -- REMOVED AND REPLACED PRESSURE REGULATOR VALVE, TURBINE INLET SWITCH AND COMPRESSOR DISCHARGE SWITCH. 2L72 4F A6WE 20030128000272003012800027GL 2003 1 28 HEEA083779 220030115A726123064560 LINE BELL 407 407 1182206SW ALLSN 250C 250C* GL ENGINE OIL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03494PH 53396 LINE SEEPING OIL. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E4CE 20030128001052003012800105SW 2003 1 28 HEEA083849 120030116A6230 BUSHING BELL 407 407 1182206SW PC LEVER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH AFS2197 53400 MAIN ROTOR PITCH CHANGE LEVER BUSHINGS WORN. 1G71 3U O H2SW 20030129000392003012900039SW 2003 1 29 HEEA083952 120030117A6210 BLADE BELL 407 407 1182206SW T/R HEAD PEELING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53396 53188 PEELING PAINT ON TAIL ROTOR BLADES AND HIGH FREQUENCY VIBRIATION. REPAIRED. 1G71 3U O H2SW 20030203001692003020300169CE 2003 2 3 FFS2003F00007 120030111A3010129970C321 TUBE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA DEICE TUBE CRACKED D FFSAK NONE O OTHER ININSP/MAINT 1 AL01575D 20267 UE24 WHILE INVESTIGATING A RT BLEED AIR FAIL ANNUNCIATOR. DISCOVERED THE WELD FOR THE PRESSURE SWITCH CRACKED ON THE RT WING DEICE TUBE, INBOARD OF THE RT INSTRUMENT AIR VALVE. REMOVED TUBE AND DISCOVERED THAT THE B-NUT FLARE WAS MISFORMED AND PARTIALLY RESTRAIGHTENED. 2L72 4T3 TRTA24CE E2NE 20030204000312003020400031NM 2003 2 4 SWAA030188 120030123A3350101073 LENS BOEING737 7373H4 1384600NM FWD CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED D CHECK, FOUND CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT FWD CABIN LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20030204001382003020400138CE 2003 2 4 W532003F00000 120030115A8120227450 COUPLING CESSNA414 414 2075908CE CONT O520 TSIO520* 17040SO TURBOCHARGER SPLIT A W53SK NONE O OTHER ININSP/MAINT 1 SO3569917 4140643 FOUND TURBO COUPLING CLAMP SPLIT AROUND CLAMP, WITH NO SAFETY CABLE AND TORQUE STAMPED PLATE. THIS CONDITION UNDETECTED COULD CAUSE A MAJOR FIRE OR HEAT COMING OUT OF TURBO. 1L72 3O3 ORTA7CE E8CE 20030213000802003021300080EU 2003 2 13 03FDEA00066 120030121A2730 ELEVATOR AIRBUS310 A310222 3930315EU PWA JT9 JT9D* NE EMPENNAGE MALFUNCTIONED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25456FE 318 ELEVATOR PITCH FORCE VERY HIGH IN ALL FLIGHT PHASES, NO PITCH FEEL FAULT INDICATES. PERFORMED TSM 27-31-00 FIG 101 FROM STEPS 1 - 13, ALL NORMAL AND COMPARED TO AC 422 CONTROL COLUMN TENSION, THE SAME. CANNOT DUPLICATE ON GROUND. HOWEVER CANNOT PERFORM ADJ/TEST DUE TO NO EQPT/TESTER AVAIL SUBIC. A/C IN NORMAL CONFIG. SUSPECT NEED TO CHECK AGAIN THE E2LO & E2RO ELEV AFT CABLES FOR PROPER TENSION THAT WAS REPLACED ON DEC 11, THEN THE TROUBLE STARTED TO APPEAR. FOR CONTINUATION ** S/D ** COMING 2L72 4F4 FRTA35EU E20EA 20030213001032003021300103WP 2003 2 13 2003F00075 120030102A3350363674 LAMP LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE ROW 1 INOPERATIVE G AMTAK NONE L NO TEST ININSP/MAINT 1 GL11162AT 1220 EGRESS PATHWAY LIGHTING AT ROW 1 LT INOPERATIVE. REPLACED MISSING EGRESS PATHWAY LIGHTING AT ROW 1 L/H AS REQUIRED. 2L73 4F4 F A23WE A12EU 20030521001502003052100150WP 2003 5 21 MWEA030196 120030501A5230995766442 INTERCOSTAL DOUG DC9 DC981 3022081WP CARGO DOOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 MID CARGO DOOR LOWER AFT STOP SUPPORT INTERCOSTAL WEB AND ANGLE HAVE ENLONGATED FASTENER HOLES. LOCATED, DRILLED AND INSTALLED NEW WEB AND ANGLE. 2L72 4F A6WE 20030618001042003061800104NM 2003 6 18 SWAA031287 120030605A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, WL148, RBL 15. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030617003232003061700323NM 2003 6 17 SWAA031274 120030606A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 743 AT STR 19L, BS 767 AT STR 20R AND BS 947 AT STR 22R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20030620000022003062000002 2003 6 20 HEEA087228 420030610A34570845000000 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F WILL NOT MAINTAIN PRESET WAYPOINTS AFTER POWER IS REMOVED FROM THE AIRCRAFT. SHOP REPAIR. 1G71 3U H2SW 20030626000202003062600020NM 2003 6 26 2003UALA00371 120030404A335020121 POWER SUPPLY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 FLIGHT CREW REPORTED THAT AFT SECTION OF FLOOR EEL INOPERATIVE. REPLACED AFT EEL POWER STRIP. 2L72 4F4 FRTA16WE E2GL 20030707000492003070700049NM 2003 7 7 AALA20030105 120030124A3350 LAMP BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21941AN 29534 MIA - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMREGENCY EXIT LIGHT INOPERATIVE. RESEATED LEFT AFT OVERWING EMERGENCY EXIT LAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA16WE 20030714000232003071400023NM 2003 7 14 SWAA031395 120030623A532065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030718000202003071800020 2003 7 18 WRLA200313 420030620A22114059001908 COMPUTER DOUG MD11 MD11 3023602NM NR 2 POSITION FAILED A WRLAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27273WA 48519 DURING CLIMB-OUT WITH AUTO PILOT OFF, A PULSATION OR HYSTERESIS IS FELT IN THE PTICH AXIS, CONTINUED DURING CRUISE FLIGHT. MORE PRONOUNCED AT HIGHER SPPEDS, INTERMITTENT ASYMMETRIC FLUTTER OF ELEVATOR DISPLAY ON CONFIGURATION SYNOPTIC PAGE. THE AIRCRAFT RETURNED TO DEPARTURE STATION ANC. LRU FAULT REVIEW FAILED NR 2 FCC-2. ACCOMPLISHED R-T-S FCC-2 TEST FAILED. REMOVED AND REPLACED FCC-2 R-T-S TEST PASSED. NO FAULTS NOTED PER MM 22-10. REPLACED FLIGHT CONTROL COMPUTER. (M) 2L73 4F RTA22WE 20030707002012003070700201WP 2003 7 7 UPS03840876 120030617A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C3, LEFT WING LE LOWER RIB IS CRACKED AT XFS 578.75 STOPD RILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20030709000542003070900054WP 2003 7 9 GTIA030424 120030516A5310 BEAM DOUG DC9 DC981 3022081WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND MID CARGO COMP, JAMB BEAM CORRODED STATION 636 TO 693. REMOVED BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. (M) 2L72 4F A6WE 20030709000912003070900091SO 2003 7 9 C2XA03IA061 120030608A2751 WARNING LIGHT EMB 145 EMB145LR 3260212SO TE FLAPS ILLUMINATED A C2XAO OTHER N FALSE WARNING LDLANDING 1 SW2748901 145501 INBOUND, PILOT REPORTED A FLAP FAIL MESSAGE. THE AIRCRAFT LANDED WITH THE FLAPS AT ZERO WITHOUT INCIDENT. MAINTENANCE RESET THE FLAP SYSTEM, PERFORMED A OPERATIONAL CHECK OF THE FLAP SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030709000042003070900004WP 2003 7 9 GTIA030432 120030512A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND CABIN FS 1112 RIGHT FLOOR PANEL CRACKED. REMOVED OUTBOARD RIGHT FLOOR PANEL. FABRICATED DOUBLER REPAIR. INSTALLED DOUBLER REPAIR. INSTALLED FLOOR PANEL. (M) 2L72 4F A6WE 20030710000532003071000053WP 2003 7 10 DHL2003807008 120030520A52701EN32R POSITION SWITCH DOUG DC8 DC873F 302199FWP CARGO DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01807DH 45990 AT FL 370 BELLY DOOR OPEN LIGHT ILLUMINATED AIRPLANE WAS PRESSURIZING NORMALLY RAN ABNORMAL PROCEDURE DESCENDED TO FL 290. REMOVED AND REPLACED A PIT DOOR POSITION SWITCH PER M/M 52-31-1, OPS CHECKED GOOD. 2L74 4F RT4A25 20030714000292003071400029NM 2003 7 14 SWAA031401 120030621A53206549892 STRUCTURE BOEING737 7373H4 1384600NM AFT CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED D CHECK, FOUND UPPER TEE STRUCTURE CORRODED AT BS 1016, WL 208, BETWEEN LBL 5 AND LBL 28. REPAIRED TEE STRUCTURE PER SRM. 2L72 4F RTA16WE 20030711000762003071100076NE 2003 7 11 EIA2003090 220030625A7261 LINE BOEING747 747273C 1384896NM PWA JT9 JT9D7J 52054NE NR 4 BEARING BROKEN A EIAAFEJAACTIVATE FIRE EXT. ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09471EV 20651 689564 ENGINE NR 1 FIRE LIGHT ILLUMINATED DISCHARGED BOTH FIRE BOTTLES. EGT RED BALL AND NACELLE INDICATES IN RED ZONE SHUT DOWN ENG DUMPED FUEL LANDED JFK. NTSB NOTIFIED. INVESTIGATION IN PROGRESS. NR 4 BEARING OIL PRESSURE LINE BROKE EARLY INDICATION OF CAUSE. 2L74 4F4 F A20WE E20EA 20030216000012003021600001EU 2003 2 16 RAIA00302034 120030203A301013730897K CURRENT LIMITER JETAIRJETSTMJETSTM4101 1500501EU BLOWN A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03555HK 41072 5480-STL- ELEVATOR ANTI-ICE FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED CURRENT LIMITER 1HJ1, OPS CK OK. 2L72 4T RTA41NM 20030625000872003062500087NM 2003 6 25 F3LA200300061 120030213A5315 FLOORBEAM BOEING737 7372Y5 1384554NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE, STA 794, LBL 8. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-05, SRM 53-10-05, FIG 11, SHEET 2, AND SOPM 20-41-02. 2L72 4U RTA16WE 20030226000252003022600025SW 2003 2 26 HEEA084317 120030211A3212407350302101 FLOAT BELL 407 407 1182206SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 FLOAT BAG FAILED 6 MONTH INSPECTION (LEAKING). 1G71 3U O H2SW 20030303002002003030300200WP 2003 3 3 DHL2003804546 120030116A5730 SKIN DOUG DC8 DC873F 302199FWP CORRODED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH77866 46124 ITEM REF>: N/R: 0237 LH WING L/E UPPER SKIN CORRODED BETWEEN STA. XFS566.250 AND XFS585.000 ( MAJOR REPAIR)CORR: PERFORMED MAJORIAW SRM 57-2-1 PG. 2 REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 REMOVED CORROSION ON LH WING UPPER SKIN ( STA. XFS566.250-585.000) IAW SRM 51-1-8 PG. 17-18FOUND OUT OF LIMITS IAW SRM 57-2-0 PAGE 16 . TRIMMED OUT DAMAGED AREA IAW SRM57-2-1 PG. 2 FABRICATED FILLER (7075 T6AL.050) & DOUBLER (7075T6AL.063) IAW 57-2-1 PAGE 2 CLEANED , TREATED AND PRIMED FILLER & DOUBLER IAW SRM 57-2-1 PG 2 , SRM 51-1-21 PG.1 FOR L/E REMOVAL / INSTALLATION SEE N/R 0319 2L74 4F RT4A25 20030306000202003030600020 2003 3 6 HEEA084733 420030217A2340A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 AUDIO FADES IN AND OUT. FOUND R72 VOLUME POT BAD, FACEPLATE UNREADABLE AND SELECTOR KNOB CRACKED. REPLACED. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030307002022003030700202SO 2003 3 7 C2XA03BT034 120030304A33501317 LIGHT EMB 145 EMB145LR 3260212SO FAULTY A C2XAO OTHER O OTHER ININSP/MAINT 1 SW2716918 145397 BTV---CO2491, DURING SERVICE/ROUTINE INSPECTION FOUND OVERHEAD EMERGENCY LIGHT AT ROW 18 INOPERATIVE.....MAINTENANCE REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT IAW EMB145 AMM #33-50-08. OPS. CHECKED GOOD. 2L72 4T RTT00011AT 20030310000262003031000026SW 2003 3 10 HEEA084935 120030227A7120 BEARING BELL 412 412 1182202SW TRIPOD ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ENGINE MOUNT TRIPOD ASSY BEARINGS ARE WORN. SCRAPPED. 1G72 4U H4SW 20030310000452003031000045SW 2003 3 10 HEEA084950 120030227A6710214001347005 ACTUATOR BELL 412 412 1182202SW M/R HEAD STICKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 ACTUATOR ROTARY STICKING. 1G72 4U H4SW 20030311000272003031100027EU 2003 3 11 MALA030191 120030310A335021LN BATTERY PACK SAAB SF340 340B 7860101EU A MALAO OTHER J WARNING INDICATION ININSP/MAINT 1 GL15402XJ 340B402 DURING OPS TEST OF EMERGENCY LIGHTS (TASK CARD #335003) MAINTENANCE FOUND EMERGENCY BATTERY PACK 21LN INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK 21LN, OPS CHECK OK. 2L72 4T RTA52EU 20030313001282003031300128NM 2003 3 13 0300486642 120030225A5330 SKIN BOEING747 747212B 1384886NM CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01642NW 21942 During "L" check found corrosion under seal plane area on upper forward corner of #3 LH passenger door. Repaired per EA 66-193805. 2L74 4F A20WE 20030313002012003031300201WP 2003 3 13 AALA20030169 120030206A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN UNSECURE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21297AA 49309 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AFT LAVATORY AREA INOPERATIVE. SECURED EMERGENCY EXIT AISLE LIGHT BATTERY FOR TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030320001182003032000118NM 2003 3 20 2003UALA00108 120030126A3350 CHARGER BOEING777 777222 1385219NM EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29799UA 26926 EMERGENCY LIGHTS INOPERATIVE, ROW 17 TO 28, RIGHT AISLE. REPLACED BATTERY CHARGER ABOVE DOOR NR 3 RIGHT. 2L72 4F RTT0001SE 20030122001092003012200109GL 2003 1 22 HEEA083493 220030107A7323252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037136H11954 S833 ENGINE DECELERATION, FOUND SEVERAL TEST POINTS TO BE SLIGHTLY EARLY, BUT WELL WITHIN SERVICE LIMITS. SPLIT UNIT AND INSPECTED INTERIOR OF DRIVE BODY. DURING INSPECTION OF DRIVE BODY INTERIOR FOUND NO DISCREPANCIES. COULD NOT DETERMINE ANY REASON FOR THIS UNIT TO HAVE CAUSED AN ENGINE DECELERATION. 1G72 3U3 U H3EU E4CE 20030331001202003033100120NM 2003 3 31 DHL2003740001 120030121A56105717623093 WINDOW BOEING727 7272Q9 138448MNM COCKPIT BURNED A DHLAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01740DH 21930 L-2 WINDOW BURNED AND OUTER PANE CRACKED. REMOVED AND REPLACED L-2 WINDOW IAW M/M 56-12-11. OPS CHECKED GOOD. NO LEAKS NOTED. 2L73 4F RTA3WE 20030327000442003032700044NM 2003 3 27 AWXA200300316 120030301A33501010421 HOUSING BOEING757 757225 1384959NM EMERGENCY LIGHT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-09 CHECK A 1 INCH CRACK WAS FOUND ON BULL NOSE EMERGENCY LIGHT HOUSING AT SEAT ROW 7 LT. MAINTENANCE REMOVED AND REPLACED BULL NOSE EMERGENCY LIGHT HOUSING AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20030325000122003032500012NM 2003 3 25 AWXA200300114 120030126A531165C807351 FRAME BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B1US GL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 DURING C-14 CHECK SEVERAL SPOTS OF INTERGRANULAR CORROSION WERE FOUND ON INNER FRAME RT SIDE OF AFT CABIN BS 967 TO BS 1006. MAINTENANCE REMOVED INNER FRAME RT SIDE OF AFT CABIN BS 967 TO BS 1006; FABRICATED A NEW REPLACEMENT INNER FRAME PER DWG 65C80735; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F4 FRTA16WE E2GL 20030416003892003041600389SO 2003 4 16 SWIA200311753 120030110A5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07294SW 120321 SUPPORT BRACKET CRACKED AT LEFT SIDEWALL AFT OF CAPTAIN'S DV WINDOW. FOUND DURING C-CHECK INSPECTION. NEW BRACKET INSTALLED IAW SRM 120 51-10-02. 2L72 4T RTA31SO 20030417002112003041700211NM 2003 4 17 QXEA0300260 120030212A5410 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - NR 1 ENGINE LOWER COWL: RT SUPPORT ANGLE NEXT TO BYPASS DOOR CRACKED AT AFT UPPER END. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030327002022003032700202EA 2003 3 27 CA030212003 220030210A73203010458 ROD END BEECH 99 99 1154002CE PWA PT6 PT6A28 EA FCU DAMAGED W E ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 CA (CAN) PILOT REPORTED THAT ON DESCENT THAT HE COULD NOT ACHIEVE ANYTHING LESS THAN 1000 FT POUNDS TORQUE ON THE LT ENGINE WHEN PULLING THE POWER LEVER BACK TO IDLE. PILOT LANDED AND SHUT ENGINE OFF AND TAXIED TO TERMINAL. MAINTENANCE FOUND ROD END FROZEN DUE TO MOISTURE. ROD ENDS WERE CLEANED, DRIED AND LUBRICATED TO ENSURE MOISTURE DID NOT PENETRATE BALL AGAIN. 1L72 3T4 T A14CE E4EA 20030421000632003042100063EA 2003 4 21 SWIA200311812 120030217A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT CORRODED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07443SW 7638 EMERGENCY ROW EXIT LIGHTS OUT IN THE BACK SECTION. FOUND WIRE PIGTAIL FOR AFT LIGHT SECTION TO BE CORRODED. REPLACED PIGTAIL. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20030421001272003042100127WP 2003 4 21 IXXA0300019O 120030305A3230 MECHANISM DOUG DC8 DC873F 302199FWP MLG UPLOCK OUT OF ADJUST A IXXAO OTHER J WARNING INDICATION CRCRUISE 1 SW11606AL893491904 46044 AFTER DEPARTURE FROM BGTL TO KWRI DURING GEAR RETRACTION CREW NOTED DOOR NOT LATCHED LIGHT ILLUMINATED. CREW CYCLED GEAR, LIGHT EXTINGUISHED AND GEAR PASSED UPLATCH CHECK. CREW MADE UNEVENTFUL LANDING IN KWRI. MAINTENANCE PLACED ITEM ON MEL. AIRCRAFT WAS MOVED TO GSO FOR T/S OF MEL ITEM. GSO MAINTENANCE ADJUSTED RT MLG UPLATCH INTERLOCK MECHANISM AND ACHEIVED A GOOD OPERATIONAL CHECK. ALL WORK COMPLETED PER APPLICABLE MANUALS AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20030716000862003071600086NM 2003 7 16 USAABB03096 120030621A335086210066 BATTERY PACK BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 ALL FLOOR LEVEL EMERGENCY LIGHTS FAILED TO TEST. MAINTENANCE REPLACED ALL THE BATTERY PACKS. (M) 2L72 4F RTA2NM 20030724000242003072400024NM 2003 7 24 AWXA200300687 120030515A5730654549611 SKIN BOEING737 737277 1384570NM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DURING C-15 CHECK CORROSION WAS FOUND ON LT WING LOWER SURFACE SKIN AT NR 2 FLAP TRACK ATTACH POINT. MAINTENANCE REMOVED CORROSION ON LT WING LOWER SURFACE SKIN BY MACHINING A FLAT STEP; PERFORMED A HFEC INSPECTION TO VERIFY MACHINED AREA WAS NOT CRACKED; FABRICATED AN ANTI-FRET STRIP AND TAPERED SHIM; INSTALLED REPAIR PARTS IAW 15-5724-03155-SS1. 2L72 4F RTA16WE 20030825000712003082500071EU 2003 8 25 0301423255 120030731A21501263A000003 ACM AIRBUS320 A320212 3930322EU A/C BAY OVERHEATED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01355NW 310 16765 DURING TAKEOFF, STRONG SMELL OF SMOKE WAS NOTICED IN CABIN. FLIGHT CREW DECLARED A YELLOW EMERGENCY AND RETURNED TO DEPARTING STATION. FLIGHT LANDED OVERWEIGHT BUT EVERYTHING ELSE WAS NORMAL. MAINTENANCE INSPECTED DUCTS, GALLEYS, AND LIGHTS; NO FAULT FOUND. MAINTENANCE FOUND THE NR 1 PACK OVERHEATING. REPLACED THE ACM WHICH TESTED AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20030828001592003082800159 2003 8 28 USAASA03088 420030809A2565 SLIDE AIRBUS320 A320214 3930316EU SERVICE DOOR DEFECTIVE A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19102UW 0844 PHL - RECEIVED 'EPSU EXT LOAD AFT L' FAULT DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT LEFT SERVICE DOOR EMERGENCY ESCAPE SLIDE. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20030829000462003082900046WP 2003 8 29 DHL2003801087 120030721A323257155835501 DOOR ACTUATOR DOUG DC8 DC873F 302199FWP LANDING GEAR FAILED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 AFTER GEAR RETRACTION DOOR NOT LATCHED AND RIGHT DOOR UNSAFE LIGHT ILLUMINATED. RAN ABNORMAL PROCEDURE, LIGHT ONLY WENT OUT AFTER UP LATCH CHECK. REMOVED AND REPLACED DOOR ACTUATOR AND VALVE ASSEMBLY PER M/M 32-32-7. GROUND OPS CHECKED NORMAL. 2L74 4F RT4A25 20030724000612003072400061EU 2003 7 24 AWXA200300716 120030608A5330D5347041020000 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 DURING C-04 CHECK CORROSION WAS FOUND ON SKIN AT AFT LOWER FUSELAGE FR 62 AND FR 63, BETWEEN STR 41 LT AND STR 41 RT, IFPC ANTENNA CUTOUT. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT DAMAGED SKIN; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11 PG 209-214, FIG 203. 2L72 4F RTA28NM 20030728001142003072800114NM 2003 7 28 SWAA031523 120030711A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20030801001312003080100131WP 2003 8 1 MWEA030289 120030724A5220 DOOR DOUG DC9 DC932 3022066WP EMERGENCY EXIT NOISY A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31502ME 48132 PASSENGER REPORTED LARGE AMOUNTS OF AIRFLOW AROUND EMERGENCY EXIT DOOR. INSPECTED EMERGENCY DOOR, SEALS AND LATCHING MECHANISMS. OPERATIONS CHECK GOOD NO DEFECTS FOUND. 2L72 4F A6WE 20030801000382003080100038NM 2003 8 1 AMTA200300711 120030526A2613 CONNECTOR BOEING757 75723N 1384973NM OVERHEAT SYS DEFECTIVE A AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11514AT 27971 LEFT ENGINE OVERHEAT LP2 INDICATION ON STATUS PAGE, INTERMITTENT. REMOVED AND REPLACED CONNECTOR D41162P IAW WDM 26-11-11 AND 26-11-12. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20030903000902003090300090EA 2003 9 3 A6WA200340119 120030813A2740 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A A6WAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 GL31416AW 7603 FOUND STAB TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET FOR QRH. MACH TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PER QRH. (M) 2L72 4F RTA21EA 20030714001242003071400124EU 2003 7 14 DHL2003368007 120030628A3260D5002011 MODULE AIRBUS300 A300B4203 3930306EU MLG FAILED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01368DH 207 LANDING GEAR COULD NOT BE RAISED. COMPLETED ABNORMAL. SWITCHED TO SYSTEM 1 OPS NORMAL. REMOVED AND REPLACED PROXIMITY DETECTOR MODULE UNIT IAW MM 32-61-12. CHECKS OK. 2L72 4F RTA35EU 20030124001022003012400102NM 2003 1 24 AWXA200300067 120030123A3350BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 18 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW0 0 24711 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES AT EMERGENCY LIGHT ASSEMBLY SEAT ROW 18 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030129000282003012900028SW 2003 1 29 HEEA083938 120030117A6300407010206103B SPRING BELL 407 407 1182206SW MAIN ROTOR DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 SPRING ELASTOMER IS DETERIORATED AND TORN. 1G71 3U O H2SW 20030130000792003013000079NM 2003 1 30 P5CA0300734 120030122A5210NONE SKIN BOEING747 7472U3B 1384846NM 1 L/H DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 EVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 L/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO THE VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN REPAIR CARRIED OUT IAW SRM 52-10-02, FIG. 9. 2L74 4F RTA20WE 20030212000852003021200085WP 2003 2 12 CALA0300035 120030211A5347 SEAT TRACK DOUG DC9 DC982 3022082WP #2 GALLEY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0969826 49486 INSPECTION FOUND R/H O/B SEAT TRACK CORRODED AT GALLEY MOUNT FOR #2 GALLEY. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE 4F. 2L72 4F A6WE 20030213000082003021300008NM 2003 2 13 CA030122002 120030121A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8400 NM PWC 150 PW150A EA NLG CENTERING FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) LANDING GEAR DID NOT RETRACT AFTER UP SELECTION, FLIGHT RETURNED TO BASE, PASSENGERS OFF LOADED. NLG CENTERING PROXIMITY SENSOR FOUND TO GIVE FAULTY INDICATIONS ON PSEU, PROXIMITY SENSOR REPLACED. 2H72 4T4 TRTA13NM E00062EN 20030213000782003021300078NM 2003 2 13 MWEA030089 120030212A5313591141011 LONGERON DOUG MD88 MD88 3023688NM STA 313 DEFORMED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 LONGERON 23 LEFT WAS FOUND DEFORMED AT STATION 313. -- REPAIRED LONGERON. 2L72 4F RTA6WE 20030625000862003062500086NM 2003 6 25 F3LA200300058 120030201A532065479573 INTERCOSTAL BOEING737 7373M8 1384615NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO DOOR SILL CORRODED. FOUND CORROSION BEYOND LIMITS PER SRM 53-60-15. INSTALLED REPLACEMENT AFT CARGO DOOR SILL INTERCOSTAL PER SRM 53-60-15 AND 51-40-02. 2L72 4F RTA16WE 20030224000242003022400024 2003 2 24 BAQA084098 420030207A34215040017926 GYRO BOLKMS117 BK117A1 5626010EU COCKPIT SLOW H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01955ME1472 7243 SLOW TO ERRECT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H13EU 20030116000632003011600063SW 2003 1 16 HEEA083022 120030106A6320PHI206052 MAGNETIC SEAL BELL 206 206L3 1182108SW M/R GEARBOX LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0331077 51520 MAIN ROTRO GEARBOX LEAKING. REPLACED WITH SERVICEABLE SEAL. 1G71 3U H2SW 20030116001252003011600125SO 2003 1 16 C2XA03CL013 120030114A335078241 INVERTER EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2713964 145123 CLE FLIGHT#2099 THE CREW REPORTED 2 EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST.MAINTENANCE INSPECTED AND REPLACED THE #2 INVERTER.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20030117001012003011700101SW 2003 1 17 HEEA083191 120030108A3212206050248117 FLOAT BELL 206 206L3 1182108SW EMERGENCY FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 FLOAT BAG ASSY LEAKS. 1G71 3U H2SW 20030305000022003030500002 2003 3 5 HEEA084607 420030214A3442MI5852013 INDICATOR BELL 412 412 1182202SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WEATHER RADAR WILL NOT PAINT GREEN ON TEST OR DURING LONG FLIGHTS. FOUND TEST PATTERN ERRATIC AND COLORS TURN ALL RED INTERMITTENTLY. REPLACED U1312, U1313 ICS ON VIDEO BOARD. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20030307001402003030700140EU 2003 3 7 AALA20030113 120030124A28101608565 VALVE FOKKERF28 F28MK0100 4990807EU MAIN FUEL TANK DEFECTIVE A AALAA UNSCHED LANDING K FLUID LOSS TOTAKEOFF 1 SW211423A 11406 ORD - FLT 1371 - EN ROUTE ORD-XNA ON TAKEOFF, HAD SEVERAL REPORTS OF FUEL STREAMING OFF RIGHT WING. NO NOTICEABLE DIFFERENCE IN FUEL QUANTITY NOTED. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN TANK OVERFLOW VALVE. (M) 2L72 4F RT 20030308000062003030800006SO 2003 3 8 RAIA00302052 120030221A3412CS50006004A RELAY EMB 145 EMB145LR 3260212SO A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03811HK 145256 5305-PIT-TAT 2 HEAT INOP WITH SMOKE IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED NUMBER 2 TAT HEAT RELAY AND SOCKET, OPS CK OK. 2L72 4T RTT00011AT 20030902001252003090200125NM 2003 9 2 AWXA200300779 120030607A53306545770139 SKIN BOEING737 7373Y0 1384671NM ZONE 200 - FUSELDENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-14 CHECK, DENTS FOUND ON CROWN SKIN FROM BS 540 TO BS 727, STR 4 LT TO STR 10 LT. MAINTENANCE REMOVED AND REPLACE SKIN FROM BS 540-727 STR 4 LT TO STR 10 LT IAW SRM 51-40-02 PG. 38, FIG. 8 AND AWA E.R. 03-5100-01187-JS1C. 2L72 4F RTA16WE 20030903000602003090300060SO 2003 9 3 CSL2003F00000 220030702A8550641250 SEAL CESSNA414 414 2075908CE CONT O520 TSIO520* 17040SO CRANKSHAFT LEAKING B CSLRO OTHER O OTHER NRNOT REPORTED 1 CE01515ST1259 4140169 ENGINE OIL SEEN LEAKING UPON DESCENT FROM 20,000 FT, LEAK TRACED TO CRANKSHAFT OIL SEAL. UPON REMOVAL SEAL WAS FOUND TO BE SEVERELY WORN ON SEALING EDGE, TO THE POINT OF BEING WORN THROUGH, AROUND APPROX 50 PERCENT OF ITS SURFACE. NEW SEAL SOLVED PROBLEM, OLD SEAL APPEARED WEATHER CHECKED. 1L72 3O3 ORTA7CE E8CE 20030903000582003090300058SO 2003 9 3 CHQ000414 120030716A2611 SMOKE DETECTOR EMB 145 EMB145 3260210SO CARGO BAY MALFUNCTIONED A CHQAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL11565 TAXING TO RUNWAY, BAGG SMOKE WARNING LIGHT ILLUMINATED ON THE EICAS. THE BAGG COMPARTMENT EXT. BUTTON WAS PUSHED. WE RETURNED TO THE GATE AND EVACUATED THE PASSENGERS. ALL THE APPR. CHECKLISTS AND PROCEDURES WERE COMPLETED. THE FIRE AND RESUE DEPARTMENTS WERE NOTIFIED AND RESPONDED. NO FIRE OR SMOKE WAS FOUND. 2L72 4F RTT00011AT 20030814000972003081400097NM 2003 8 14 UPS03241064 120030714A5523 TAB BOEING727 72725C 138400HNM ELEVATOR CONTAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 INSPECTION TYPE: C, FOLLOWING X-RAY INSPECTION OF RT ELEVATOR TAB, WATER INGRESS FOUND ON RT ELEVATOR TAB AT APPROX ELEV STA 95 TO ELEV STA 105. REPAIR CARRIED OUT IAW SRM 51-40-05. 2L73 4F A3WE 20030814001132003081400113NM 2003 8 14 CALA0300416 120030725A5553 BUSHING BOEING737 737524 1384721NM VERTICAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716642 28903 INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHING CORRODED AT LT O/B AFT LOCATION. THE BUSHING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-52274. 2L72 4F RTA16WE 20030909002162003090900216NE 2003 9 9 BAQA088195 220030805A7310796929 METERING VALVE AEROSPAS365 AS365N2 8680815EU TMECA ARRIELARRIEL1C 60030NE ENGINE MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 FUEL FLOW METER COULD NOT SET. WOULD NOT GIVE CORRECT BURN RATE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 URTH10EU E19EU 20030911002452003091100245WP 2003 9 11 DHL2003604576 120030606A5753 ANGLE DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LT WING OUTBD FLAP (TEE) ANGLE CRACKED 2.000 AT STA XF.165.000. REMOVED DAMAGED (TEE) ANGLE AT STA XF.165.000 IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED ARE IAW SRM 51-1-8B. INSTALLED NEW (TEE) ANGLE IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030911001772003091100177WP 2003 9 11 DHL2003873607 120030701A5754 VANE DOUG DC8 DC873F 302199FWP L/E SLOT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ83849 46091 WING VANE SLOT SHOWS HOLES ELONGATED AT XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030627, ED-3455. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030627, ED-3455. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND INTERNAL DOUBLER AND DOUBLER. CLEANED, TREATED AND PRIMED FILLER INTERNAL PART, INTERNAL DOUBLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND INTERNAL DOUBLER AND DOUBLER WITH NEW FASTENERS IAW EODHL-030627, ED-3455 IAW SRM 51-1-21 PG, SRM 51-1-20D PG9 AND CONICAL WASHERS IAW SRM 51-1-26 FIG 1. 2L74 4F RT4A25 20030929000512003092900051NM 2003 9 29 03FDEA01427 120030903A5753 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING I/B FLAP VANE O/B TEE FITTING MID BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG MID BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490. 2L73 4F RTA22WE 20030729001292003072900129EA 2003 7 29 SWIA200312184 120030715A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG MALFUNCTIONED A SWIAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 NM07935SW 7725 ON FINAL, AFTER PLACING THE LANDING GEAR LEVER DOWN, THE MAIN LANDING GEAR DID NOT UNLOCK. A DISAGREE MESSAGE APPEARED. WHEN EXECUTING THE MISSED APPROACH, THE GEAR DEPLOYED AND LOCKED. PERFORMED GEAR INSPECTION ON ALL GEARS. NO DEFECTS NOTED. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKS GOOD IAW MM 32-32-00. 2L72 4F4 FRTA21EA E15NE 20030730001372003073000137SO 2003 7 30 SIMA200314802 120030515A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21644AE 145204 DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND TREATED THE BARE METAL SURFACE. FABRICATED A REPAIR DOUBLER AND INSTALLED. REPAIR DONE IAW EMB STATMENT IC2003-145/1604, PARA 12. (M) 2L72 4T RTT00011AT 20030911002402003091100240WP 2003 9 11 DHL2003604590 120030611A5350 TIE DOUG DC8 DC873F 302199FWP TAILCONE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FUSELAGE TAIL CONE INTERIOR RT TIE 1.000 CRACKED AT STA 1923.000. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20031006001302003100600130NM 2003 10 6 SWAA032024 120030910A335007912 COVER BOEING737 7372H4 138448CNM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS MISSING FROM FWD CABIN. INSTALLED COVERS PER MM. 2L72 4F A16WE 20031006001852003100600185NM 2003 10 6 03FDEA01675 120031001A532065453132 STRINGER CLIP BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25469FE 21581 CRACK IN STRINGER CLIP AT BS 950C, STRINGER 5 RT. REPLACED CLIP. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 5RH IAW SRM 51-30-2 & 51-30-5 2L73 4F4 FRTA3WE E2EA 20031007000882003100700088NM 2003 10 7 SWAA031986 120030905A335007912 COVER BOEING737 7372H4 138448CNM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED A1 CHECK, FOUND EEPLS COVERS MISSING AT ROWS NR 13 AND 18. INSTALLED COVERS PER MM. 2L72 4F A16WE 20031003000742003100300074NM 2003 10 3 03FDEA01531 120030906A5753ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT ATTACHMENT BORE BUSHING FOUND LOOSE. 2L73 4F RTA22WE 20031008000502003100800050NM 2003 10 8 UPS03441232 120030904A5347BAC15201566 CARGO TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C U/D, BS 480 - 500 RBL 65 TIE DOWN TRACK LT FLANGE CORRODED. CORROSION BLEND OUT 0.045 INCH X 1 INCH X 12 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. CORROSION REMOVED IAW SRM 51-10-01. SEAT TRACK REPAIRED REFER TO SRM 53-10-05 FIG 6. CIC APPLIED IAW EO M5100-2780-E 2L74 4F A20WE 20031014001792003101400179NM 2003 10 14 SWAA032099 120030920A278238180010035 ACTUATOR BOEING737 7377H4 1384404NM SLAT LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29404WN 27892 AIR TURNBACK, L/E DEVICES WOULD NOT FULLY RETRACT. FOUND INTERNAL LEAK AT L/E SLAT HYD ACTUATORS NR 1, NR 2, NR 3, NR 4, NR 6, AND NR 7. REMOVED AND REPLACED L/E SLAT HYD ACTUATORS PER MM. 2L72 4F RTA16WE 20031015000222003101500022EA 2003 10 15 ASOA03433 120030911A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A C-CHECK IN MCN, THE FORWARD SIDE OF FS 640 FRAME AT THE ENGINE SUPPORT BEAM AS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED FS 640 FRAME AT THE ENGINE SUPPORT BEAM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031015000482003101500048EU 2003 10 15 ASOA03451 120030918A33503012000 POWER SUPPLY AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AT 43WL, 61WL, 73WL AND 62WL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20031021000372003102100037WP 2003 10 21 GTIA030702 120030909A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23816NK 49140 FTW - FLIGHT COMPARTMENT STATION 120-160, LEFT SIDE FLOOR PANEL HAS PUNCTURE/CRACK. REPAIRED FLOOR PANEL. (M) 2L72 4F A6WE 20031021000542003102100054WP 2003 10 21 GTIA030688 120030921A2560 STRIP DOUG DC9 DC983 3022083WP CABIN MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 AFT GALLEY EMERGENCY GLOW PATH STRIP IN FRONT OF GALLEY CART IS MISSING. REPLACED MISSING GLOW PATH STREP IN AFT GALLEY, OPS CHECK OK. (M) 2L72 4F RTA6WE 20031021001562003102100156 2003 10 21 AALA20031014 420030916A3418 SENSOR BOEING757 757223 1384957NM STALL WARNING FAILED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21639AA 24597 TUL - FLT 535 - AIRCRAFT EN ROUTE TUL TO DFW, DURING ROTATION STICK SHAKER ACTIVATED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT NOT OVERWEIGHT. ACCOMPLISHED MCDP FAULT CHECK AND REPLACED ANGLE OF ATTACH SENSORS AND STALL WARNING CARDS. SYSTEM GROUND AND FCF CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 20031021002182003102100218SO 2003 10 21 SIMA200325305 120030902A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21717AE 145272 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFED BY BLENDING AREA. PERFORMED EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ONE REPAIR ANGLE, TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2917 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031022001382003102200138EU 2003 10 22 AWXA200301080 120030912A5210FE240221001 DIAPHRAGM AIRBUS320 A320231 3930325EU PAX DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 DURING INSPECTION FOUND THE L-2 DOOR EMERGENCY OPERATION CYLINDER PRESSURE GAUGE READING ZERO. MAINTENANCE REMOVED AND REPLACED THE DIAPHRAGM IN PERCUSSION MECHANISM OF L-2 DOOR EMERGENCY OPERATION CYLINDER, SERVICED TO PROPER PRESSURE, LEAK AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031029000702003102900070 2003 10 29 ASAA0380540 420030720A25653961896501 LANYARD DOUG MD80 MD83 3023681NM ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 PREFLIGHT CHECK, AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RT 20031028000242003102800024NM 2003 10 28 CALA0300565 120030927A5512 SKIN BOEING737 737524 1384721NM HORIZONTAL STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716647 28908 INSPECTION FOUND LOWER SURFACE OF LT HORIZONTAL STABILIZER SKIN DENTED APPROXIMATELY 8 INCHES FORWARD OF AFT SPAR AND 102 INCHES O/B OF FUSELAGE. A REPAIR WAS INSTALLED IAW SRM 55-10-01. 2L72 4F RTA16WE 20031028000402003102800040EA 2003 10 28 SWIA200312453 120030903A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07916SW 7634 FS 280 RT FLOORBEAM RBL 9.0 I/B & O/B ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20031119000532003111900053NM 2003 11 19 CALA0300587 120031011A5320 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714324 23375 INSPECTION FOUND MAIN DECK LT AND RT LAV WALL SUPPORT CHANNELS CORRODED AT STA 993, LBL 16-44 AND RBL 16-44. NEW LAV WALL SUPPORT CHANNELS WERE INSTALLED IAW SRM 51-10-2. 2L72 4F RTA16WE 20040128000652004012800065NM 2004 1 28 QXEA200301584 120031226A5260 AIRSTAIR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09411QX 4055 SEA- ON FLIGHT 2371 FLIGHT ATTENDANT REPORTS AFT AIR STAIRS HARD TO SLIDE. CLEANED AND LUBED TRACKS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040129001182004012900118EA 2004 1 29 COMA0460004 120031230A2750860D10018ABC CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01712CA20002 7244 FLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20030310001362003031000136NM 2003 3 10 EIA2003008 120030222A5300 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 FRAME CRACKED STA 340, 1 INCH BELOW STRINGER 16 LEFT. REMOVED DAMAGE, FABRICATED DOUBLER -2 DOUBLER, FILLER-4 DOUBLER, PER ECRA 481-53-1752 & 51-10-02 PG 7, SOPM PER 20-41-02 PG 10 2L74 4F A20WE 20030313001072003031300107CE 2003 3 13 COE2003F00000 120030215A3110C6625040101 AMMETER CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA COCKPIT INOPERATIVE A COEAO OTHER O OTHER NRNOT REPORTED 1 NM13720FX86 208B0452 IN FLIGHT, ABOUT 20 MILES SOUTH OF AIRPORT, THE AMMETER DROPPED TO (0), ONLY SHOWS SYSTEM VOLTAGE. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. AFTER TROUBLESHOOTING, AMMETER WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 1H71 3T3 T A37CE E2NE 20030121003252003012100325 2003 1 21 HEEA083376 420030109A342150400179015 INDICATOR BELL 206 206L3 1182108SW ADI FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ADI WORKED FOR 2.5 HOURS THEN QUIT. REPAIRED. 1G71 3U H2SW 20030122001542003012200154NM 2003 1 22 DL757030060 120030114A26213460000104 FIRE BOTTLE BOEING757 757232 1384965NM CARGO BAY DEFECTIVE A DALAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO27606DL 22813 CARGO BTL 1 EICAS MSG ILLUMINATED ALONG WITH DISCHARGE LIGHT ON CENTER CONSOLE FIRE PANEL. REPLACED CARGO FIRE BOTTLE NR 1. OPS CHECK OK. NO MESSAGES OR LIGHTS ON FLIGHT DECK. 2L72 4F RTA2NM 20030317001702003031700170NM 2003 3 17 371PA0018 120030313A30405717623134 SLIDING WINDOW BOEING737 737306 13844BGNM A PIDAA UNSCHED LANDING O OTHER CRCRUISE 1 SO05371PA 23543 #2 sliding window RT cracked with window heat on. Turned off window heat. Outer pane cracked. Returned to field. Ferried to ATL. R & R co-pilot's sliding window per MM 56-12-11 and co-pilot's side window heat controller (precautionary) per MM 30-41-11. Ops chk OK. 2L72 4F RTA16NE 20030318000882003031800088WP 2003 3 18 ASAA0380025 120030104A575339195822 FITTING DOUG DC9 DC983 3022083WP RT WING FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RT WING OUTBOARD FLAP VANE NR 4 FITTING IS WORN. REPLACED FITTING PER CMM 27-50-02. (M) 2L72 4F RTA6WE 20030321000142003032100014NM 2003 3 21 2003UALA00168 120030212A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 STATION 188 RT SIDE FRAME CRACKED IN RADIUS AT WL 207. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED RT SIDE FRAME. 2L72 4F4 FRTA16WE E2GL 20030321000962003032100096NM 2003 3 21 UPS03440326 120030304A5340 SEAT TRACK BOEING747 747200 1384847NM U/D CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C U/D SEAT TRACK FOUND HEACY CORR AS MARKED. CORROSION BLEND OUT 0.055"X1"X3" SEAT TRACK REPLACED AT U/D BS 480 - BS 530RBL 65 AS PER SRM 51-10-01 P.8. 2L74 4F RTA20WE 20030421000102003042100010 2003 4 21 UPS03840238 420030225A2565 SLIDE DOUG DC8 DC873F 302199FWP CABIN LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 ESCAPE SLIDE NOT SECURE AND GIRT BAR NOT TOTALLY IN SLIDE SLEEVE. SECURED ESCAPE SLIDE TO BRACKET WITH CAMLOCK FASTENER. REPOSITIONED GIRT BAR IN SLIDE SLEEVE. OK TO CONTINUE. 2L74 4F RT4A25 20030421001292003042100129NM 2003 4 21 VNAA0303002 120030303A21505584C000 SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT A/C PACK TEMPFAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07328JS1232 3030 AFTER DEPARTING PIT, THE CREW ADVISED MAINTENANCE CONTROL OF A LEFT HAND PACK FAIL INDICATION. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO PIT. MAINTENANCE THEN INSPECTED AND REPLACED THE OVERTEMP SWITCH ON THE LEFT HAND PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030422000432003042200043EA 2003 4 22 ASOA03070 120030220A78301267587 PDU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE THRUST REVERSER INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11854AS 7382 FLT 4385 - DURING CRUISE FROM ATL-CRW, AT APPROXIMATELY 27,000 FEET THE CREW RECEIVED A LEFT THRUST REVERSER UNLOCK LIGHT. THE CREW PERFORMED AN EMERGENCY STOW WITH NO CHANGE. AN EMERGENCY WAS DECLARED, EMERGENCY PROCEDURES WERE FOLLOWED AND THE AIRCRAFT DIVERTED TO TYS, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20030422001022003042200102SO 2003 4 22 SIMA200307106 120030216A531514522461015 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 THIS IS A LEVEL 2 FINDING, DURING AN IMBV INSPECTION RIGHT OMEGA BEAM TRIANGLE CAP AT FRAME 19 CORRODED. REOVED AND INSTALLED NEW TRIANGLE CAP IAW 135 SRM 51-40-02, 51-20-03, 51-40-04 AND 51-40-06. (M) 2L72 4F RTT00011AT 20030421001902003042100190NM 2003 4 21 USAABB03040 120030311A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20030806001002003080600100SO 2003 8 6 C2XA03TY114 120030801A534714532606017 SEAT TRACK EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 DURING A SCHEDULED INSPECTION SEAT TRACK LW5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048. 2L72 4F RTT00011AT 20040225001732004022500173NM 2004 2 25 DL757031141 120031227A33500201720001 LIGHT BOEING757 757232 1384965NM CABIN SEAT 4CD BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27683DA 27103 ON INSPECTION FOUND EMERGENCY PATH LIGHT BROKEN OFF SEAT AT 4CD. REPLACED LIGHT ASSY, SHROUD-BACKING PLATE AND LENS. OPS OF LIGHT NORMAL. 2L72 4F RTA2NM 20030722000432003072200043NE 2003 7 22 MALA030329 220030704A7320 HMU SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 2 ENGINE MALFUNCTIONED A MALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL15119XJ 340A119 AT 16000 FT ICE FULL APPROX 4 MIN IN VMC COND. NR 2 ENG TORQUE UNCOMMANDED WENT TO 30 PERCENT TORQUE & ITT PEGGED OVERTEMP LIGHT ILLUM APPROX 5 SEC UNTIL RT PL RETARDED. RAN QRH AFTER LOCKING OUT BOTH TORQUE MOTORS & DETERMINED IT WAS NOT AN INDICATION PROBLEM. SHUTDOWN NR 2 ENG. MX PERFORMED BORESCOPE DUE TO TEMPS IN EXCESS OF 960 DEGREES BUT LESS THAN 970 DEGREES, FOR 2 SECONDS ON RT ENG. NO DISCREPANCIES NOTED. REPLACED RT HMU. MX BOROSCOPED COMP & HOT SECTION. CHECKED ENG CHIP DETECTOR & SCAVANGE SCREENS, NO FAULTS FOUND, REPLACED ECU DUE TO PRIOR PART HISTORY. ALL CHECKS GOOD. ALL RUNS TEST GOOD. 2L72 4T4 TRTA52EU E8NE6 20030724001142003072400114 2003 7 24 AWXA200300670 420030606A2565D30664109 SLIDE AIRBUS320 A320231 3930325EU R-1 DOOR FAULTY A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28629AW6251 076 DOOR EMERGENCY ESCAPE SLIDE ARM LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR EMERGENCY ESCAPE SLIDE IAW T/C R1C25304, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20030825001132003082500113WP 2003 8 25 ABXA030307 120030721A32607000010101 SWITCH DOUG DC9 DC941 302207NWP NLG FAULTY A ABXAO OTHER N FALSE WARNING CRCRUISE 1 GL23956AX 47620 DURING CRUISE FLIGHT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. RIGHT HYDRAULIC SWITCH ON, 3000 PSI DID NOT RESOLVE THE PROBLEM. WHEN GEAR SELECTED DOWN, UNSAFE LIGHT REMAINED ILLUMINATED. GEAR DOWN LIGHT REMAINED OFF. DECLARED EMERGENCY. REPLACED THE NOSE GEAR DOWN LOCK SWITCH IAW AMM 32-60-01-2. SWUNG THE GEAR SEVERAL TIMES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 20030902000572003090200057EU 2003 9 2 R7M2003F00000 120030205A5532 SKIN SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE VERTICAL STAB CRACKED E R7MRO OTHER O OTHER NRNOT REPORTED 1 NM07392LG 3252 RT CRACK, THREE WORKING RIVETS. SUSPECT IMPROPERLY SHIMMED AT FACTORY INSTALLATION. NO SHIMS FOUND AT REMOVAL OF FIN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20030729000232003072900023EA 2003 7 29 03196698 120030715A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27698BR 7799 DURING CRUISE THE FLIGHT CREW REPORTED LAV SMOKE INDICATION. AS A PRECAUTION FLIGHT WAS DIVERTED TO GRR. AIRCRAFT LANDED WITHOUT INCIDENT. PASSENGERS DEPLANED, MAINTENANCE PERSONNEL FOUND LAV SMOKE DETECTOR INOPERATIVE. SMOKE DETECTOR WAS REMOVED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICED NORMALLY AT GATE. 2L72 4F RTA21EA 20030903001222003090300122 2003 9 3 2003F00535 420030816A3442 TRANSCEIVER AIRBUS320 A320233 3930329EU WEATHER RADAR DAMAGED A SOKFA UNSCHED LANDING O OTHER CRCRUISE 1 SO23482TA 1482 SJO - FLT 691 - DURING CRUISE, THE WX R/T FAILED, THE AIRCRAFT RETURNED TO SJO STATION FOR MAINTENANCE. AFTER LANDING AT SJO, TECHNICIANS FOUND WEATHER RADAR TRANSCEIVER DAMAGED. IT WAS REMOVED AND REPLACED TRANSCEIVER, P/N 622-5132-622, AND PERFORMED INSTALLATION AND OPERATIONS PER MM 34-41-33. ALL RESULTS WERE SATISFACTORY AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20030903001972003090300197CE 2003 9 3 2003F00547 120030724A5350 RADOME RAYTHNDH125 HAWKER800 7450004CE FUSELAGE LIGHTNING STRIKEA ZLWAO OTHER S AFFECT SYSTEMS CRCRUISE 1 SW15800MJ 258226 THE AIRCRAFT WAS STUCK BY LIGHTNING DURING FLIGHT. THE FLIGHT CREW NOTICED THE RADAR SCREEN WENT BLANK THEN CAME BACK UP AND FUNCTIONED NORMALLY. THE RADOME HAD BEEN BURNED AND THE LEFT ELEVATOR TRIM TAB HAD A HOLE IN THE TRAILING EDGE. THE LIGHTNING STRIKE INSPECTION AS COMPLETED AND THE DAMAGED COMPONENTS WERE REPLACED. (M) 2L72 4F RTA3EU 20030908002522003090800252EA 2003 9 8 SWIA200312343 120030825A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 AFT COMPARTMENT; FS 625.0; STR 14R HAS A CRACKED ATTACH ANGLE. DISCOVERED DURING C-CHECK. REPLACE ANGLE IAW CRJ SRM 51-42-06, 51-40-11, 51-25-16. P/N: 601R-35012-52 2L72 4F RTA21EA 20030731000072003073100007NM 2003 7 31 QXEA200300906 120030719A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX- LEFT HAND INBOARD NR 5 SEAT TRACK HAS A GOUGE IN CENTER OF TRACK AT STATION X467.000. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20030827001032003082700103NM 2003 8 27 CALA0300399 120030718A2432263BA1012 BATTERY BOEING777 777224 1385225NM GE GE90 GE9090B NE E/E BAY FAULTY A CALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW277601018688 29480 THE CREW RECEIVED A BATTERY AND BATTERY CHARGER STATUS MESSAGE AT LEVEL OFF AFTER DEPARTING IAH. THE MESSAGES WERE ACCOMPANIED BY A STRONG ELECTRICAL SMELL IN THE COCKPIT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MAIN AIRCRAFT BATTERY AND BATTERY CHARGER IAW MM 24-31-01. 2L72 4F4 FRTT00001SEE00049EN 20030909002002003090900200CE 2003 9 9 ZES2003F00001 120030627A3260S31762 SQUAT SWITCH CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT MLG OUT OF ADJUST E ZESAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA03400LX1650 5600453 PILOT REPORTED THAT AFTER TAKEOFF FROM BHB THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT WOULD NOT PRESSURE, AND DAVTRON CLOCKS DID NOT START RUNNING. PILOTS DIVERTED FLIGHT TO BGR. TECHNICIAN FOUND THE LEFT SQUAT SWITCH SLIGHTLY OUT OF ADJUSTMENT, ADJUSTED SWITCH AND PERFORMED A SQUAT SWITCH CHECKOUT AND A GEAR SWING. CHECKED SATISFACTORY. 2L72 4F4 FRTA22CE E25EA 20031006001292003100600129 2003 10 6 SWAA032023 420030911A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE IN FLOOR ATTACH FITTINGS. ADJUSTED FITTINGS PER MM. 2L72 4F RTA16WE 20031006001732003100600173WP 2003 10 6 03FDEA01651 120030926A5753 HINGE DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL RT TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25397FE 46631 RT OB FLAP, IB HINGE FITTING MOUNT STUD BORES AND FACES (ON FITTING) CORRODED FACT 26SEP03 21:39 BFM U REWORKED BORES AND FACES, FOUND TO BE WITHIN LIMITS IAW CMM 57-44-08 AT BFM/MAE. 2L73 4F4 F A22WE E23EA 20031020000442003102000044SO 2003 10 20 RAIA00310225 120031005A3230 LANDING GEAR EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 5688-STL- NOSE LANDING GEAR WILL NOT RETRACT. MAINTENANCE PERFORMED NUMEROUS LANDING GEAR OPERATIONAL CHECKS AND COULD NOT DUPLICATE PROBLEM. 2L72 4T RTT00011AT 20031020002072003102000207NM 2003 10 20 DLM88030820 120030908A3350RPS1B POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27986DL 53313 F/C CABIN EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2L72 4F RTA6WE 20031021000912003102100091SO 2003 10 21 SIMA200326802 120030920A531514522460013 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 ABI - DURING AN MBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 AS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF THE CETNER FLOORBEAM, CLEANED, AND TREATED THE REPAIR AREA. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB, EMB 145/1142 REV 22, CHAPTER 52-3-22-10 FIG 201, SHEET 2 CPM 51-21-04, 51-21-05, 51-21-06 AND STANDARD SRM PRACTICES. (M) 2L72 4F RTT00011AT 20031021002922003102100292NM 2003 10 21 03FDEA01057 120031021A5311 FRAME BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25192FE 19085 NR 174 CORROSION (C53-132-02) BS 870, LWR CHORD LBL 12-16, WL 148. R/R CHORD. 2L73 4F RTA3WE 20030909001592003090900159 2003 9 9 SWIA200312307 420030824A2215 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 NM07190SW 120050 WITH AUTOPILOT ENGAGED ON EITHER C/A OR F/O SIDE, AP MAKES UNCOMMANDED SLOW ROLL LEFT OR RIGHT. AUTOPILOT FAIL LIGHT ON MAP DOES NOT ILLUMINATE. REMOVED AND REPLACED THE AILERON AUTOPILOT SERVO IAW EMB120 MM 27-00-03. AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20031027000592003102700059NE 2003 10 27 AT0300027 220030923A7200BR700715A130 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE LEFT FAILED A ZZDAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO15924AT 55080 NR 1 ENGINE FAILURE, ENGINE AUTO SHUTDOWN, TGT NOT EXCEEDED, ENGINE RELIGHT ATTEMPTED, ENGINE SURGING, MANUAL ENGINE SHUTDOWN. ENGINE NOT SHUTDOWN FOR MORE THAN 30 MINUTES. REMOVED AND REPLACED NR 1 ENGINE. 2L72 4F4 FTRA6WE E00057EN 20031029000372003102900037NM 2003 10 29 ASAA0340117 120030305A53106546550 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 DURING C-CHECK, FOUND CORROSION AT SHEAR TIE AT BS 787 RBL 18 AND WL 156. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20031118001112003111800111NM 2003 11 18 AWXA200301187 120030912A5321144N533022 FLOOR PANEL BOEING757 7572S7 1384962NM CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL M-2 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1. 2L72 4F RTA2NM 20031120000482003112000048 2003 11 20 SWIA200312496 420031006A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07288SW4661 4661 120316 CAPTAIN'S AUTOPILOT AND TRIM FAIL. REPLACED CAPTAIN'S AUTO PILOT COMPUTER. OPS CHECK GOOD. 2L72 4T RTA31SO 20031103001232003110300123NM 2003 11 3 03FDEA01733 120031008A5753ARC199114 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT LUG SURFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT LUG SURFACE FOUND CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20031118000542003111800054EU 2003 11 18 AWXA200301169 120030924A5347D53472209220 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON PASSENGER SEAT RAIL AT Y765 AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SEAT RAIL Y765 AT FR 66; FABRICATED A NEW REPLACEMENT SEAT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 6-7. 2L72 4F RTA28NM 20031106001892003110600189NM 2003 11 6 SWAA032277 120031016A53116546529 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, WL 154 AND RBL 1.5. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20031106002042003110600204EA 2003 11 6 ASOA03478 120031003A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT SIDE BRACKETS AT FS 718 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CRACKED BRACKETS AT FS 718 IAW ASA EO 600-53-0067A. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20031110000762003111000076CE 2003 11 10 AMWA73 120031105A553111464000059 RIB BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07165YV UE165 WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, TO THE RIB FLANGES AT CANTED STAB STA 54.026 WERE FOUND CRACKED IN THREE PLACES ON THE LEFT AND THREE PLACES ON THE RIGHT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03. 2L72 4T RTA24CE 20040113000422004011300042CE 2004 1 13 BAQA090685 120031110A61215485020 ACTUATOR BEECH 100 100BEECH 1152916CE PROP SYNC FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 10070 B144 ACTUATOR WILL NOT CENTER IN ONE DIRECTION. REPLACED WITH SERVICEABLE UNIT. 11/11/03 1L72 3T A14CE 20040112002462004011200246NM 2004 1 12 AALA20031483 120031230A3350 CONNECTOR BOEING757 757223 1384957NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21173AN 32399 MIA NO TRIP/30 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 3JH INOPERATIVE. FOUND SIDEWALL PLUG DISCONNECTED AND RECONNECTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040112002542004011200254NM 2004 1 12 AALA20031432 120031214A3350 BATTERY BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21658AA 24616 MIA) EXTERIOR EMERGENCY EXIT LIGHT AT L2 INOPERATIVE. REPLACED POWER SUPPLY M733 FOR EXTERIOR EMERGENCY EXIT LIGHT AT L2. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA2NM 20040112001312004011200131WP 2004 1 12 GTIA031010 120031113A5320 ANGLE DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FTW - FOUND PAX CABIN CRACKED ANGLE UNDER CABIN FLOOR AT FS 828, 42 RBL. STOP DRILLED AT CRACKED ANGLE. FABRICATED TWO REPAIR ANGLES. INSTALLED ANGLE REPAIR. (M) 2L72 4F A6WE 20040112001742004011200174EU 2004 1 12 03FDEA02233 120031223A2120B38QA6505 ISOLATION VALVE AIRBUS310 A310 EU A/C SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO25443FE 283 ON DEPARTURE OUT OF MEM AT 3,000 VERY STRONG ODOR IN COCKPIT / TURNED BACK TO MEM. ON DESCENT TO 3,000 ODOR CAME BACK. AVIONICS FLOW LIGHT CAME ON DURING DEPT. FOLLOWED ECAM SELECTED, OVERBOARD. REMOVED AND REPLACED ISOLATION VALVE PER AIR BUS MM 21-23-12-4. OPS CHECK GOOD. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG B38QA6505, POS P2 SRL 2014, TAG 999062 ON MFG B38QA6505 SRL 102, TAG 265720. 2L72 4F RTA35EU 20031121000232003112100023EU 2003 11 21 03317317 120031003A3220AIR8358611 LANDING GEAR JETAIRJETSTMJETSTM4101 1500501EU NOSE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27317UE 41031 DURING INSPECTION THE NOSE LANDING GEAR ASSEMBLY HAD A CRACK IDENTIFIED FOWARD OF THE STEERING RACK. THE LANDING GEAR ASSEMBLY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4T RTA41NM 20031124001312003112400131NM 2003 11 24 GAIA03138ST 120031024A5320 ATTACH ANGLE BOEING727 727243 138408DNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME ATTACH ANGLE CRACKED BS 680 AT MAIN CARGO DOOR LOWER SILL BEAM. REF FASI N/R NR 61679, ACCOMPLISHED REPAIR BY REPLACEMENT IAW B727 SRM 53-10-2 FIG 3. (M) 2L73 4F RTA3WE 20031125000282003112500028WP 2003 11 25 DHL2003805563 120030808A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 INTERIM REPAIR ON RIGHT INBD FLAP UPPER SURFACES, STA XW.106.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2, FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED INTERNAL AREA IAW SRM 51-1-8B. FABRICATED NEW PLATING IAW SRM 57-7-1 PG 2 FIG 1. CLEANED, TREATED AND PRIMED NEW PLATING INTERNAL PART IAW SRM 51-1-8B. INSTALLED NEW PLATING ON RIGHT INBD FLAP UPPER SURFACE, STA XW.106.000 IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20031212000112003121200011NM 2003 12 12 SWAA032480 120031107A53146545866 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM SECTION CORRODED FROM BS 727 TO BS 727+9 RT SIDE. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20031212000832003121200083NM 2003 12 12 SWAA032431 120031103A5315BAC1505 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 774, LBL 3, LBL 8, LBL 13, LBL 18, RBL 8, AND RBL 3. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20031219000332003121900033EA 2003 12 19 SWIA200312635 120031115A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07917SW7 7 7641 BOTH I/B GROUND SPOILERS SHOW FAULT. REMOVED AND REPLACED NR 2 SECU PER AMM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20031219001852003121900185NM 2003 12 19 MWEA030479 120031209A5320993061218 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FRAME STATION 980 RIGHT CUSP SUBFLOOR CUTOUT CORRODED ON BOTTOM SIDE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20031219001092003121900109NM 2003 12 19 374PA0005 120031121A5330 SKIN BOEING737 73736M 138443BNM FUSELAGE DAMAGED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05374PA 28333 FUSELAGE DAMAGED LEFT SIDE FROM BS 907 TO BS 927 AT STR 16 LT, AT BS 907 BETWEEN STR 21 LT AND 22 LT AND FRAME SHEAR TIE DAMAGED AT BS 908 BETWEEN STR 21 LT AND STR 22 LT. REPAIRED DAMAGE PER EA NOS 53-327, 53-331, AND 53-332. 2L72 4F RTA16WE 20031223001882003122300188WP 2003 12 23 GTIA030809 120030923A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND FLOORBOARD DELAMINATED. FABRICATED NEW LT FLOORBOARD. (M) 2L72 4F A6WE 20031231000752003123100075WP 2003 12 31 GTIA030932 120031107A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSLEAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND MAIN FLOORBOARD RIGHT OUTBOARD STATION 446-522 HAS CHANNEL AND STRIPS SEPARATING ON BOTTOM. REBOARDING CHANNEL AND STRIPS. (M) 2L72 4F RTA6WE 20031231000912003123100091WP 2003 12 31 GTIA030924 120031101A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND CABIN FLOOR PANEL STATION 927-1003, CORNERS SEPARATING, BENT, EDGE GOUGED. FABRICATED NEW CABIN FLOOR PANEL. (M) 2L72 4F RTA6WE 20030919000182003091900018SW 2003 9 19 2003F00512 120030702A53022060221131 FITTING BELL 206 OH58A 1181579SW ALLSN 250C T63A720 03002GL VERTICAL FIN CRACKED D KFZGO OTHER O OTHER NRNOT REPORTED 1 SW09411NS5987 7221411 FOUND CRACK RADIATING FROM TOP AFT MOUNTING HOLE TO TRAILING EDGE. APPROX 1 INCH IN LENGTH. MILITARY BULLENTIN NR OH-58-03-ASAM-06 ADDRESSES A PROBLEM THE ARMY HAS INCURRED WITH THE OH-58 AIRCRAFT. MANY OF THESE AIRCRAFT ARE IN THE CIVIL AND PUBLIC USE ARENA OF AVIATION. THE ARMY NOW HAS A RECURRING EDDY CURRENT INSP. DUE ON THE VERTICAL FIN ASSEMBLY. 1G71 3U3 U H2SW E4CE 20031010000522003101000052NM 2003 10 10 03FDEA01565 120030918A531165163279 FAILSAFE BOEING727 727200 138407ENM FRAME CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 N00917 FRAME FAIL SAFE CHORD CRACKED BS 804 AT STR 14L. **SD** COMING 2L73 4F RTA3WE 20040210000642004021000064NM 2004 2 10 TSAA0333204 120031129A33501000679 BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHT DISCHARGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20031112000542003111200054SO 2003 11 12 SWIA200312584 120031104A2121AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203SO CABIN MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07216SW7336 5657 120285 SMOKE IN PASSENGER CABIN WHILE PARKED AT GATE WITH APU RUNNING. REMOVED AND REPLACED RIGHT GROUND COOLING FAN IAW 21-51-03. 2L72 4T RTA31SO 20031103000792003110300079WP 2003 11 3 UPS03841346 120030921A53133702969N LONGERON DOUG DC8 DC873F 302199FWP AC COMPARTMENT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C1, STATION 70 LONGERON 36 RT. UPPER FLANGE IS CRACKED REMOVED AND REPLACED LONGERON IAW DWG.3702969,AND SRM. 51-1-21, 51-1-20D. 2L74 4F RT4A25 20030917001232003091700123CE 2003 9 17 000102 120030731A32601CH16 SWITCH LEAR 24 24B 5170306CE MLG MALFUNCTIONED E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05233TW 24B221 AIRCRAFT DEPARTED TUS BOTH MAIN GEAR RED LIGHTS STAYED ON, GEAR WAS RECYCLED LIGHTS STAYED ON DIVERTED TO ELP FOR MAINTENANCE. MAINTENANCE REPLACED SWITCH AND GROUND OPS CHECKS GOOD. 2L72 4J A10CE 20031010000552003101000055NM 2003 10 10 03FDEA01562 120030918A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 DENT IN FWD CARGO FRAME, BS 520 BETWEEN STR 22R AND 23R. **SD** COMING 2L73 4F RTA3WE 20031118000072003111800007NM 2003 11 18 UPS03241354 120030909A5315 FLOORBEAM BOEING727 7271A7C 13840X2NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 INSPECTION TYPE: C, ON INSPECTION OF CONTROL CABLES BS 740 - 950 CRACK FOUND ON FLOORBEAM WEB BS 520 LBL 50. REPAIR CARRIED OUT IAW SRM 51-40-2 2L73 4F A3WE 20040108001312004010800131NE 2004 1 8 Z1R2003F00001 120031020A14307615009143041 SCREW SKRSKYS76 S76C 8143008NE M/R TIP CAP CORRODED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11761AF903 760524 RED BLADE M/R TIP CAP SCREWS: LARGE SCREWS HAD DEVELOPED CORROSION AROUND TOP TWO THREADS. INSTALLATION, TORQUED LARGE SCREW 100 IN/LBS. REMOVAL (LARGE SCREWS) TORQUE 150-130 IN/LBS. SMALL SCREWS (INSTALL) TORQUE 30 IN/LBS. SMALL SCREWS (REMOVAL) TORQUE 70-30 IN/LBS.(K) 1G72 3U NCH1NE 20040113000162004011300016NE 2004 1 13 ERAA091805 120030913A6410S611730101045 BLADE SKRSKYS61 S61N 8142104NE TAIL ROTOR DEBONDED B ERAAO OTHER O OTHER NRNOT REPORTED 1 EA03563EH21845 61808 TRAILING EDGE ERRODED AND UNBONDED. SENT FOR REPAIR INSPECTED IAW SA 4045-31E CHAPTER / SECTION 65-20-01 AND NAVAIR 0395B-126 CHANGE 1; REPLACED RUBBER CAP IAW S61 L/N SRM SA 4045-31E CHAPTER 65-20-01 PROCEDURE 13 AND CHAPTER 65-10-01 PROCEDURE 5.A; REPLACED TRAILING EDGE CAP IAW SES 611038 AND DRWG S6117-30101; REPLACED TIP CAP 61 N/L. SRM SA 4045-31E CHAPTER 65-20-01 PROCEDURE 34 AND 35; REFINISHED IAW S61 L/N SRM SA4045-31E PROCEDURE 1,3 AND SS 9208; STATIC BALANCED IAW SES 611038 AND S6117-30101 @ TT 23284.7. 2G72 4U 1H15 20040113001832004011300183EU 2004 1 13 RAIA00312298 120031203A2460A2104F PDU JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A RAIAB EMER. DESCENT O OTHER CLCLIMB 1 CE03566HK7676 1769 41084 STL- CAPTAINS EFIS TUBE INOP. MAINTENANCE REMOVED AND REPLACED LT POWER DISTRIBUTION UNIT. 2L72 4T RTA41NM 20040114001802004011400180SO 2004 1 14 MASA200300422 120031023A2611FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CARGO BAY FAILED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07846MJ 145507 ASH NR 2818. BAGGAGE COMP SMOKE DETECTOR FAIL MSG. MECHANIC REPLACED SMOKE DETECTOR. 2L72 4T4 FRTT00011ATTE6CH 20031124000312003112400031NM 2003 11 24 QXEA200301417 120031104A27609670021 SWITCH BOMBDRDHC8 DHC8401 1390041NM ZONE 300 FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09408QX 4050 ON CLIMBOUT, SHORTLY AFTER ACCELERATING THROUGH 180 KTS, SPOILER OUTBOARD CAUTION MESSAGE LIGHT ILLUMINATED. RAN ASSOCIATED CHECKLIST AND CONTINUED TO PDX WITH SPEED LIMITED TO 1200 KIAS MAX. REMOVED AND REPLACED NR 2 OUTBOARD SPOILER SYSTEM LOW PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031215000702003121500070EU 2003 12 15 03294319 120031021A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27319UE 41042 DURING INSPECTION THE EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. THE BATTERIES WERE IDENTIFIED AS THE CAUSE AND SUBSEQUENTLY REPLACED. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM WAS ACCOMPLISHED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20031216000312003121600031NM 2003 12 16 SWAA032601 120031122A3520289801240 MASK BOEING737 7377H4 1384404NM CABIN TORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29765SW 29805 DURING SCHEDULED RON CHECK, (DUE TO SWA SDR SWAA03-2584) FOUND PAX O2 SYS MASKS TORN AT PSU'S 12 DEF, 19 ABC, 20 ABC, 23 ABC AND 9 DEF. REMOVED AND REPLACED O2 MASKS PER MM. 2L72 4F RTA16WE 20031216000562003121600056NM 2003 12 16 SWAA032542 120031118A5311BAC1506 FRAME BOEING737 7373H4 1384600NM RT MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED D CHECK, FOUND RT MLG W/W CUTOUT FRAME LOWER CHORD CRACKED AT BS 679, RBL 67. REPAIRED LOWER FRAME SECTION PER SRM. 2L72 4F RTA16WE 20031217001662003121700166NM 2003 12 17 QXEA200301548 120031208A5260 MECHANISM BOMBDRDHC8 DHC8401 1390041NM AIRSTAIR DIRTY A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09411QX 4055 FLIGHT ATTENDANT REPORTS AFT AIRSTAIR BINDING. CLEANED RELEASE MECHANISM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031218000932003121800093EU 2003 12 18 2003UALA00881 120031121A5520 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT ELEVATOR CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29403UA 442 LOWER PANEL OF LT ELEVATOR FOUND WITH WATER INGRESSION IN AREA APROX 1.5 BY 1.4 INCHES LOCATED APPROXIMATELY 2 IN FROM I/B EDGE AND 33 INCHES FROM TRAILING EDGE. MAJOR REPAIR ACCOMPLISHED. A REINFORCING REPAIR WAS ACCOMPLISHED PER SRM 55-21-11. REPAIR NR 5D ON PG 219 USING FIG 204 SHEET NR 2. 2L72 4F4 FRTA28NM E40NE 20031218001232003121800123NM 2003 12 18 03FDEA02003 120031130A5350 FRAME DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 FORWARD TAIL CONE MOST AFT STA 2244 (UPPER HINGE AREA) FRAME FOUND CRACKED. FRAME AND ANGLE REPAIRED AS PER SRM 53-00-01 FIG. 9 VOL. I AND SRM 51-31-01 VOL. II. 2L73 4F RTA22WE 20031219000562003121900056WP 2003 12 19 UPS03841639 120031115A53403755842U1 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: C1, BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 1220 BETWEEN LONG 28L-29L. REMOVED AND REPLACED FITTING IAW DWG 3755842 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20031222000102003122200010NM 2003 12 22 03FDEA02158 120031209A5755FX65246087 RIB BOEING727 727200 138407ENM NR 4 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25257FE 20939 LT WING AFT SPAR, NR 4 SPOILER ACTUATOR INBOARD SUPPORT RIB IS CRACKED. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-30-2. RECEIVED NEW FABRICATED SUPPORT ANGLE P/N FX65-24608 -7, ON TRAVELER T2/385523. LOCATED & DRILLED NEW PART IAW SRM 51-20-1. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-30-2 & 51-20-4. LEAK CHECK TO BE DONE ON TANK CLOSE CARD N00826. 2L73 4F RTA3WE 20031224000572003122400057EU 2003 12 24 A6WA200350067 120031209A5753 STRUCTURE BAC 146 146200A 1500266EU TE FLAP DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 134-6070002. (M) 2H74 4F A49EU 20031229001532003122900153EA 2003 12 29 SWIA200312658 120031031A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07594SW 7285 CARGO PIT CRACKS FOUND ON FLOOR LANDING PLATE AT FS 589.00 LBL 42 WL 73.50 AND FS 605.00, LBL 42 WL 73.5. REPAIRED DAMAGED AREAS IAW CRJ REO 601R-53-61-433 REV A. 2L72 4F RTA21EA 20031231000942003123100094WP 2003 12 31 GTIA030939 120031107A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND MAIN CABIN FLOORBOARD STATION 200 CHANNEL ON LOWER SIDE IS SEPARATING. REBONDED HAT CHANNEL. (M) 2L72 4F RTA6WE 20031229001812003122900181SO 2003 12 29 SWIA200312676 120031116A5330 SKIN EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07227SW 120304 SKIN CORROSION AT FRAME 30 BELLY; EXFOLIATION CORROSION. DISCOVERED DURING C-CHECK INSPECTION. PERFORMED REPAIR OF CORRODED AREA AT FRAME 30 BETWEEN STRINGERS 21R & 21L PER EMBRAER APPROVED REPAIR IC2003-120/4120 DATED 12/4/03. 2L72 4T RTA31SO 20031020002202003102000220WP 2003 10 20 UPS03841368 120030924A5347S4889185 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C1 SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 1582 AT RBL 25. REMOVED SEAT TRACK SECTION BETWEEN STATION 1490 AND 1600, FABRICATED AND INSTALLED SEAT TRACK IAW DWG S2400463, AND SRM 53-2-3 FIG 13. 2L74 4F RT4A25 20040108001142004010800114EU 2004 1 8 KBM2003F00064 120031018A71700174078010 DRAIN VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 9666 AIRCRAFT STARTS SLOW, MUST INCREASE TO 750 DEGREE TO 760 DEGREE TO START. REMOVED AND REPLACED WITH OVERHAULED START DRAIN VALVE. 1G71 3U3 U H9EU E19EU 20040114001182004011400118NM 2004 1 14 DL757031051 120031124A2530831620401 OVEN BOEING757 757232 1384965NM MID GALLEY MALFUNCTIONED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27642DL 23996 DIVERSION INTO DEN FOR SMOKE AND SMELL IN CABIN. REPLACED MID GALLEY OVEN. 2L72 4F RTA2NM 20031124001322003112400132NM 2003 11 24 GAIA03148ST 120031024A5311 FRAME BOEING727 727243 138408DNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND FUSELAGE FRAME DENTED IN RADIUS BS 480 ABOVE STRINGER 17 RT. REF FASI N/R NR 61830, CUT OUT DAMAGE AND INSTALLED 9 INCH BY 6 FT REPAIR DOUBLER PER B727 SRM 51-40-3 FIG 1. (M) 2L73 4F RTA3WE 20031125001522003112500152NM 2003 11 25 ASAA0310508 120030603A5311BAC15171062 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 787, STRINGER 19L-26L CORRODED. REMOVED CORROSION AND REPAIRED FRAME PER SRM. (M) 2L72 4F RTA16WE 20031203001812003120300181WP 2003 12 3 AALA20031104 120031003A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217519A 49896 DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 26 THROUGH 31. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20040121000792004012100079EU 2004 1 21 ASOA03614 120031106A5320 CHANNEL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN BNA, THE TEE CHANNEL AT THE INBOARD SIDE OF THE ENTRANCE SILL AREA BETWEEN FRAMES 36 AND 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A DOUBLER UNER THE T-CHANNEL AT THE INBOARD SIDE OF TEH ENTRANCE SILL AREA BETWEEN FRAMES 36 AND 38 IAW SRM 51-21-42 AND 51-25-01. (M) 2H72 4T RTA53EU 20040122000942004012200094EA 2004 1 22 ASOA03658 120031216A5310 RIB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO 600-57-0042. (M) 2L72 4F RTA21EA 20040123000062004012300006WP 2004 1 23 ASAQA0380700 120031029A53305911401 SKIN DOUG DC9 DC983 3022083WP FUSELAGE SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 OAK 15K CHECK, FOUND FUSELAGE SKIN HAS THREE SCRATCHES AT 22 INCHES AFT OF L1 DOOR LOWER CORNER. PERFORMED CLASS 1 PERMANENT REPAIR PER SRM 53-04. (M) 2L72 4F RTA6WE 20040120000082004012000008CE 2004 1 20 DXTA200300204 120031216A3242215297 BRAKE ASSY CESSNA500 560CESSNA 2076750CE LEFT FAILED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07311QS 5600311 LEFT BRAKE APPEARS TO GRAB LEFT WITH VERY LITTLE BRAKE APPLICATION, AIRCRAFT RETURNED TO BLOCK. TROUBLESHOT AND FOUND LEFT SIDE BRAKE FAULTY, REPLACED LT BRAKE ASSEMBLYIAW CESSNA MM CHAPTER 32-42-01. 2L72 4F RTA22CE 20040121000502004012100050EA 2004 1 21 ASOA03585 120031117A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11850AS 7355 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTAL AT FS 484, RBL 38 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040126000422004012600042EU 2004 1 26 BAQA091617 120031224A2422SPS1307A INVERTER AEROSPAS365 AS365N2 8680815EU ELECTRICAL INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME791 6417 INVERTER INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 01/06/2004 1G72 3U RTH10EU 20031208001102003120800110EU 2003 12 8 AWXA200301308 120031021A5270DHE1141 PROXIMITY SENSOR AIRBUS320 A320231 3930325EU L-2 DOOR DEFECTIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28621AW 053 DURING C-03 CHECK THE L-2 DOOR SLIDE ARM LIGHT WOULD NOT ILLUMINATE DURING FUNCTIONAL CHECK. MAINTENANCE TROUBLESHOT DOOR ARMING SYSTEM IAW AMM 52-73-00, FOUND DOOR ARM PROXIMITY SENSOR BAD. REMOVED AND REPLACED L-2 DOOR SLIDE ARM PROXIMITY SENSOR IAW AMM 52-73-11-000-002, AND AMM 52-73-11-400-002, OPERATIONAL CHECK GOOD PER TASK 52-73-00-710-050. 2L72 4F RTA28NM 20031205000602003120500060EA 2003 12 5 SWIA200312519 120031013A2750 BRAKE CNDAIRCL600 CL6002B19 1900309EA FLAP PDU MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07932SW9 9 7714 AFTER TAKEOFF WHEN THE FLAPS WERE SELECTED UP, GOT THE FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED RIGHT MOTOR BRAKE UNIT ON FLAP PDU. SYSTEM OPS CHECKS GOOD IAW 27-52-05. 2L72 4F RTA21EA 20031209002752003120900275EA 2003 12 9 COMA0360483 120031104A2750860D10018AB CONTROL BOX CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01971CA17192 7145 FLIGHT 5825 FLAP FAIL CAUTION DURING TEST AT 20 DEGREE FLAP POSITION. REPLACED THE FECU. 2L72 4F RTA21EA 20030916001532003091600153NM 2003 9 16 03FDEA01131 120030724A2613 WARNING LIGHT BOEING727 727200 138407ENM ZONE 200 FALSE ACTIVATIONA FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 SO25492FE 21530 DURING CRUISE GOT LOWER AFT BODY OVERHEAT LIGHT. ENGINE ANTI-ICE WAS OPEN. RED TABS COMPLETED DETERMINED NR 2 ENG ANTI-ICE WAS CAUSE OF OVERHEAT LIGHT. WHEN NR 2 ENGINE ANTI-ICE CLOSED DUCT TEMP DECREASED BELOW 50 DEGREES C OVERHEAT LIGHT WENT OUT. RAN ENGINE NR 2 JRH CHAPTER 5 AND PERFORMED OPERATIONAL CHECK IAW MM 30-21- 011-4 AND 30-21-031-4. OPERATIONAL CHECK GOOD. REPOSITIONED LOOP TO COMPLY WITH MM 26-14-001-2. 2L73 4F RTA3WE 20030918000612003091800061NM 2003 9 18 DL764030717 120030803A2710 PCU BOEING767 767432ER 1385134NM AILERON UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27845MH 29719 RT INBOARD AILERON, OUTBOARD PCU BINDING. PCU BROKEN AT ROD END. AUTOPILOT LIGHT COMES ON DURING TURN AND DESENT. REPLACED PCU 2L72 4F RTA1NM 20030919000722003091900072EU 2003 9 19 194962 120030812A6120 CONTROLLER SAAB SF340 SF340A 7850100EU AUTOCOARSEN MALFUNCTIONED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 FLT NR 4516 ON 8/12/03 LYH - PIT, ON TAKEOFF ROLL AUTOCOARSEN SYSTEM FAILED TO ARM WITH TQ ABOVE 80 PERCENT, CAPTAIN ABORTED TO AND RETURNED TO GATE. 2L72 4T RTA52EU 20030923000142003092300014EU 2003 9 23 AWXA200300965 120030820A3510 FITTING AIRBUS320 A320232 3930326EU OXYGEN MASK LOOSE A AWXAO OTHER S AFFECT SYSTEMS NRNOT REPORTED 1 WP28655AW 1075 CAPTAINS O2 MASK LEAKS, GOT MASK TO STOP LEAKING BY LEAVING OUT OF BOX AND RESETTING. MAINTENANCE FOUND A LOOSE FITTING AT CAPTAINS O2 MASK TEST BUTTON, TIGHTENED FITTING, TESTED, RE-STOWED MASK WITH NO LEAKAGE NOTED. 2L72 4F RTA28NM 20030923000852003092300085WP 2003 9 23 DHL2003604738 120030622A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 LOWER FUSELAGE PLATING SHOWS 04 SPOTS OF CORROSION BETWEEN STA 743.000 AND STA 767.000, L-35L TO L-35R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT THE DAMAGED SKIN AREA IAW EODHL-030518, ED-3389. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (7075-T6 AL0.100) IAW EODHL-030518, ED-3389. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON LWR FUSELAGE PLATING BETWEEN STA 743.000 - 767.000, L-35L TO L-35R USING NEW FASTENERS. 2L74 4F RT4A25 20030924000132003092400013NM 2003 9 24 DL757030720 120030803A33500201720002 LIGHT BOEING757 757232 1384965NM R2 DOOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27636DL 23763 R2 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSY, CHECKS OK. 2L72 4F RTA2NM 20030925000132003092500013EU 2003 9 25 AALA20030829 120030803A2842SIC50774 COMPUTER AIRBUS300 A300B4605R 3930308EU FUEL QTY FAILED A AALAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 SW2180057 465 EN ROUTE ALL FUEL QUANTITY INDICATIONS FAILED. AIRCRAFT DIVERTED MIA AND LANDED WITHOUT INCIDENT. REPLACED FUEL QTY PROCESSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 20040128000722004012800072SO 2004 1 28 C2XA03SH522 120031230A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV-DURING C-CHECK THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040106000422004010600042WP 2004 1 6 DHL2003802529 120031118A57203755028504 CLIP DOUG DC8 DC873 302199CWP WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH81763 46076 NR 2 MAIN TANK CLIP CRACK 4.000, STA XRS 22.750 BETWEEN S-5L AND REAR SPAR. REMOVED CRACK CLIP AND INSTALLED A NEW ONE AT STA XRS 22.750, BETWEEN S-5L AND REAR SPAR (NR 2 MAIN TANK) IAW SRM 51-1-20D PG 21, 9 REFER TO NR 1467 FOR LEAK CHECK. 2L74 4F RT4A25 20040311000352004031100035NM 2004 3 11 ASAA0310137 120030314A53206563849 SUPPORT ANGLE BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 PAE - DURING C-CHECK, FOUND SUPPORT ANGLE AT BS 358, RIGHT BUTTOCK LINE 12, RIGHT BUTTOCK LINE 36 CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M) 2L72 4F A16WE 20040311000612004031100061NM 2004 3 11 ASAA0310103 120030306A532069514761 SUPPORT BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 OKC - DURING D-CHECK, FOUND SEAT TRACK SUPPORT AT BS 520, RIGHT BUTTOCK LINE 46 CORRODED. REMOVED AND REPLACED SUPPORT PER SRM. (M) 2L72 4F RTA16WE 20031203000222003120300022NM 2003 12 3 GAIA03133ST 120031024A5330 SKIN BOEING727 727243 138408DNM C-2 DOOR CUTOUT DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND C-2 DOOR CUTOUT AFT FRAME BS 990 INNER SKIN DENTED BETWEEN STRINGER 26RT AND 27 RT. REF FASI N/R NR 61483, CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR PER B727 SRM 53-10-2 AND 51-40-2. (M) 2L73 4F RTA3WE 20031203001752003120300175WP 2003 12 3 GTIA030866 120031025A2560 BATTERY DOUG DC9 DC982 3022082WP FLASHLIGHT WEAK A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 TOP AFT EMERGENCY FLASHLIGHT WAS WEAK BATTERY. RESECURED CONNECTION TO FLASHLIGHT BATTERY, OPS CHECKS NORMAL. (M) 2L72 4F A6WE 20031203000422003120300042NM 2003 12 3 GAIA03142ST 120031024A5313BAC1498145 STRINGER BOEING727 727243 138408DNM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING C-CHECK INSPECTION FOUND AFT CARGO COMPARTMENT STR 27 LT CORRODED FROM STATION 950 TO 1010. REF FASI N/R NR 61702, REPLACED STRINGER 27LT BS 950 TO 1010 IAW B727 SRM 53-10-1 AND 51-30-2. (M) 2L73 4F RTA3WE 20040123000352004012300035EU 2004 1 23 KBM2003F00093 120031020A6220126891P BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE STARFLEX WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 LOWER END BEARINGS WORN BEYOND LIMITS. REPLACED WITH NEW LOWER END BEARINGS. 1G71 3U3 UNCH9EU E19EU 20031204000662003120400066EA 2003 12 4 COMA0360459 120031013A2910601R7528623 LINE CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYSTEM BROKEN A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01982CA 7168 HYDRAULIC SYSTEM 2 LOW PRESSURE WARNING AND LOSS OF ALL FLUID. REPLACED BROKEN RETURN LINE AT NR 2 HYD MANIFOLD. 2L72 4F RTA21EA 20031204001032003120400103WP 2003 12 4 UPS03841417 120030912A5320561667319 INTERCOSTAL DOUG DC8 DC873F 302199FWP CARGO PIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE: C3, CRACK IN D-PIT DOOR HINGE LWR FWD HINGE. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-3-0, MAT'L ID 2024-0.050 INCH PO 414492.1 IAW DAC DWG 5616673 HT TREATED FROM 2024-0 TO 2024T4, LOCATED AND DRILLED INTERCOSTAL IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20031205000202003120500020NE 2003 12 5 DL76P030906 220031008A7230PW40603 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A DALAA UNSCHED LANDING RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO27140LL13120 727893 25988 727893 ON T/O NR 1 ENG COMPRESSOR STALLED AT 500 FT AGL, COMPLETED CHECKLIST PER QRH RETURNED FOR LANDING RSW. MAX EGT 850C FOR APPROX 1 MIN 30 SECS. ENG SHUTDOWN BY CREW. REPLACED NR 1 ENG PER TRANS 1T148. 2L72 4F4 FRTA1NM E24NE 20031208000392003120800039NM 2003 12 8 UPS03441459 120031009A5310 BEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, LT SIDE BS 300 NOSE WHEEL WELL VERTICAL BEAM WEB ONE CRACK REVEALED AT INSULATION BLANKET STAND OFF HOLE BETWEEN 1 TO 2 HORIZONTAL STIFFENERS (COUNT FROM UPPER) AS MARKED. VERTICAL WEB REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20031208001022003120800102NM 2003 12 8 QXEA200301331 120031014A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - LEFT OUTBOARD NR 1 SEAT TRACK CORROSION OUTBOARD LUG AND BARE METAL SEAT ATTACH AREA, APPROXIMATELY X312.00. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20031208000312003120800031EU 2003 12 8 AWXA200301408 120031111A5210FE240221001 SEAL AIRBUS320 A320231 3930325EU R-1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING INSPECTION FOUND THE R-1 DOOR ASSIST BOTTLE PRESSURE LOW (BOTTLE DISCHARGED). MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR ASSIST DAMPER CYLINDER DIAPHRAGM AND SEALS, SERVICED CYLINDER, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20031208000432003120800043 2003 12 8 VNAA0310013 420031020A3418 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AOA FAILED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07430JS 3044 DURING TAKEOFF, THE CREW RECEIVED A AOA FAIL CAS MESSAGE WHILE ENCOUNTERING A STRONG CROSS WIND AND ABORTED TAKEOFF. THE FLIGHT WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040128001152004012800115NM 2004 1 28 QXEA200301591 120031228A5210 SEAL BOMBDRDHC8 DHC8401 1390041NM ZONE 800 FROZEN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09410QX 4053 SEA- ON FLIGHT 2397 MAIN CABIN DOOR IS DIFFICULT TO OPEN. SUSPECTED FROZEN MOISTURE ON SEAL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20031212000012003121200001NM 2003 12 12 PCAA0311137 120031107A5320 STRUCTURE DHAV DHC8 DHC8102 2809003NM FUSELAGE CRACKED A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13848EX 331 FLIGHT 3555, INTO NEWBURG NEW YORK EXPERIENCED GEAR UNSAFE LIGHT ILLUMINATION WHEN GEAR SELECTED DOWN. THE GEAR WAS CYCLED, STILL NO CHANGE. CREW THEN COMPLIED WITH ALTERNATE EXTENSION PROCEDURES. AIRCRAFT FERRIED INTO MIDDLETOWN WHERE UPON FURTHER INVESTIGATION MAINTENANCE FOUND NOSE GEAR DECK CRACKED. REPAIRS UNDERWAY PER REQUIRED REPAIR DRAWINGS. 2H72 4T RTA13NM 20030922000462003092200046SO 2003 9 22 RAIA00308212 120030815A3242 WARNING LIGHT EMB 145 EMB145LR 3260212SO MLG BRAKE FALSE INDICATIONA RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03811HK 145256 OUTBOARD BRAKE INOP FAULT INDICATION. MAINTENANCE INSPECTED OPS CHECKED GOOD WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20040130002142004013000214NM 2004 1 30 ABXA040023 120030929A143011T17509X BOLT BOEING767 767231 1385131NM RT WING SPAR BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23702AX 22566 RIGHT MAIN LANDING GEAR ACTUATOR ATTACH FITTING AT REAR SPAR AREA HAD BROKEN BOLT HEADS, 2 EACH, AT AFT AND FRONT OUTBOARD SIDE OF ACTUATOR. REMOVED AND REPLACED FASTENERS AT REAR SPAR IAW BOEING SRM 51-00-00. 2L72 4F RTA1NM 20040203000732004020300073WP 2004 2 3 ASAA0380545 120030726A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 15 FORWARD. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040204000282004020400028NM 2004 2 4 2003UALA00776 120031016A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29531UA 25042 FUSELAGE SKIN ON STA 610 AT STR 16LT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040204000452004020400045NM 2004 2 4 S03428074 120030911A2820 VALVE BOEING747 747400 NM PWA 4056 PW4056 NE NR 1 MAIN TANK FAILED W SAJFO OTHER O OTHER TXTAXI/GRND HDL 1 WP03 24309 B18271 20 MINS AFTER REFUELING COMPLETED AND WITH CORRECT LEVEL IN EACH TANK FUEL SPILL FROM LT SURGE TANK. REPLACED NR 1 MAIN TANK REFUELING VLV IN LAX. PARTS FROM UA. REPLACED NR 1 CROSSFEED VALVE AND BOOSTER PUMP BYPASS CHECK VALVE WHILE A/C ARRIVED TPE. 2L74 4F4 FRTA20WE E24NE 20040316000902004031600090WP 2004 3 16 ASAA0380313 120030414A53203936595545 SUPPORT DOUG DC9 DC983 3022083WP CARGO TRACK CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OAK - DURING 15K CHECK, FOUND AFT CARGO BAY TIE DOWN TRACK SUPPORT IS CORRODED AT FS 1117 BETWEEN LONGERON 28R AND 27R. REPLACED TIE DOWN TRACK SUPPORT PER SRM 51-10-4 AND 30-5. (M) 2L72 4F RTA6WE 20031215001042003121500104NE 2003 12 15 MALA030502 220031116A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT MALFUNCTIONED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL15408XJ 340B408 785786 DURING FLIGHT 3327, LOST LT TORQUE, NG AND GOT A CHIP LIGHT. PILOT FOLLOWED QRH, SHUTDOWN ENGINE. AIR RETURN TO MSP. MAINTENANCE REPLACED LT ENGINE DUE TO ABNORMAL ENGINE INDICATIONS, S/N OFF 785786, S/N ON 785800. 2L72 4T4 TRTA52EU E8NE 20030929000242003092900024NM 2003 9 29 03FDEA01413 120030830A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 LT WING- I/B FLAP O/B HINGE LOWER BORE FOUND CORRODED. (FLAP SIDE). 2L73 4F RTA22WE 20050223001172005022300117EU 2005 2 23 ERAA097534 120031221A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM BROKEN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03153EH 702 GUIDE ASSY HAS STICKING SWITCH. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SPRING, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB -BO105 REM 405. 1G72 3U H3EU 20040130002122004013000212WP 2004 1 30 ABXA040008 120031126A5330 SKIN DOUG DC8 DC861 3021952WP FUSELAGE MISREPAIRED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23848AX 46032 L2 DOOR LOWER AFT CORNER HAD A REPAIR THAT DID NOT RESEMBLE SERVICE ENGINEERING SKETCH ES00863. REMOVED DISCREPANT REPAIR, FABRICATED REPAIR DOUBLERS AND FILLER, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0 AND REA D853-48474MR. 2L74 4F 4A25 20040202001502004020200150WP 2004 2 2 UPS04841744 120031230A53133648667 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, FWD SIDE STATION 70 LONGERON 30R IS CRACKED. REMOVED AND REPLACED LONGERON IAW DWG 3648667 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040206000582004020600058WP 2004 2 6 ASAA0380805 120031123A532199365511 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOORBOARD PER SRM 53-05. (M) 2L72 4F RTA6WE 20040304001452004030400145WP 2004 3 4 ASAA0380718 120031112A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. REPLACED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040614002472004061400247NM 2004 6 14 RYN2004F00022 120030814A291010605634 LINE BOEING727 727222 1384073NM PWA JT8 JT8D1 52044NE NR 2 HYD PUMP CHAFED A RYNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE077638U 19911 ON CLIMB OUT, LOST HYDRAULIC A-SYSTEM. ACCOMPLISHED APPROPRIATE CHECK LIST AND MANUALLY EXTENDED THE LANDING GEAR. EMERGENCY DECLARED AND AIRCRAFT RETURNED. AIRCRAFT LANDED MDT WITHOUT INCIDENT. REPLACED NR 2 ENGINE HYDRAULIC PUMP FLEX PRESSURE LINE. LEAK CHECKED NORMAL. 2L73 4F4 F A3WE E2EA 20040709001082004070900108SO 2004 7 9 C2XA03BT109 120031119A1420 CONNECTOR EMB 145 EMB145XR 3260214SO GPU FIRE A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2718114 145664 CREW REPORTED, GPU CAUGHT FIRE AT CONNECTOR END AND BURNED AIRCRAFT AT GPU RECEPTICAL (GPU WAS ARCHING WHEN GPU CORD WAS PULLED). MAINTENANCE INSPECTED FUSELAGE AND GPU RECEPTICAL AND FOUND NO DAMAGE. OPS CHECKED AIRCRAFT FOR EICAS MESSAGES AND CONDITION. OPS CHECKED GOOD IAW EMB 145 AMM 24-40-00. 2L72 4F RT 20030925000752003092500075WP 2003 9 25 GTIA030556 120030617A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FOUND MID PIT STATION 655 674 STRINGER 30 CORROSION AT FASTENERS. FABRICATED NEW LONGERON SECTION FROM STATION 665 TO STATION 798. FABRICATED NEW LONGERON SPLICE. INSTALLED SPLICE. INSTALLED STRINGER 30. (M) 2L72 4F A6WE 20040825002612004082500261SO 2004 8 25 XPA200300001 120030828A78206871800 MUFFLER PIPER PA32 PA32260 7103206SO ENGINE SEPARATED A X6PAA UNSCHED LANDING DB INFLIGHT SEPARATION SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO334800S3732 321185 MADE AN UNSCHEDULED LANDING, THE PILOT REPORTED SMOKE IN THE COCKPIT. AFTER LANDING AT OGB. FOUND THAT THE EXHAUST STACK HAD SEPARATED FROM THE MUFFLER. BECAUSE OF THIS, THE COWL SUSTAINED DAMAGE AT THE EXHAUST STACK PORT. THE AIRCRAFT WAS 10 HOURS FROM BEING DUE A 100 HOUR INSPECTION. MORE ATTENTION IS BEING GIVEN TO THIS AREA TO PREVENT PROBLEM. (M) 1L71 3O A3SO 20050202000612005020200061NM 2005 2 2 0704018 120031004A575365ND719023 PANEL BOEING737 737230C 1384472NM LT WING TE FLAPSDELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07737TW9992 9992 20257 LT WING INBD TE MID FLAP PANEL DELAMINATED AT WBL 121. 2L72 4F A16WE 20060801001202006080100120WP 2006 8 1 IXXA060570S 120030909A5311 FRAME SPLICE DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND FRAME SPLICE CORRODED AT STATION 245 BETWEEN LONGERONS 34 AND 35 LEFT. REMOVED CORRODED FRAME SPLICE, FABRICATED NEW FRAME SPLICE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FRAME SPLICE IAW DC8 SRM 53-2-0, AND TIMCO REPAIR ENGINEERING ORDER REO-G09471. 2L74 4F RT4A25 20030813000742003081300074 2003 8 13 0301116628 420030610A223060B80099203 CONTROL PANEL BOEING747 747251B 1384892NM AUTOTHROTTLE SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01628US648792206 22389 DURING FLIGHT THE RATING SELECT SWITCH BEGAN SMOKING. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED AUTOTHROTTLE TAT/EPRL CONTROL PANEL. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030815000712003081500071SW 2003 8 15 HEEA088448 120030723A6410206016201131 BLADE CLARK 1000 1000CLARK 2230102SW TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03266P 707 TAIL ROTOR BLADE HAS FRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE. 1Q71 3R 2A6 20030820000192003082000019NM 2003 8 20 03FDEA00850 120030603A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-113-01,1) IN STR 27L BS 720F + 13 STR 27L BS 720F + 13 FOUND TO BE OUT OF LIMITS. REMOVED STR 27L FROM 720E + 10 TO 720F + 18. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS, ALL WORK DONE IAW SRM 53-10-3. REINSTALLED GASPER AIR FAN, REMOVED FOR ACCESS AND FUNCTIONAL CHECKED. FUNCTIONAL CHECK GOOD. DONE IAW SRM 51-30-2, EXTRUSION BAC1498-131 LOT 504089 AND BAC 1498-147 LOT 504090. 2L73 4F RTA3WE 20030820000402003082000040NM 2003 8 20 03FDEA01013 120030625A5744ARC050311 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 LT WING - OUTBOARD T/E FLAP, OUTBOARD FWD HINGE FITTING FOUND OUTBOARD LOWER REAR SPAR ATTACH MOUNT HOLE WITH CORROSION (WING SIDE FITTING). REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69356 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20030820000652003082000065NM 2003 8 20 03FDEA01108 120030718A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 SKIN GOUGED IN 3 PLACES BS 384 BELOW STR 24L. REPAIRED SKIN BS 384 BELOW STR 25L IAW SRM 53-30-3 DETAIL 1. 2L73 4F RTA3WE 20030821000812003082100081NM 2003 8 21 03FDEA00932 120030620A5510ALC8100 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25588FE 48490 LEFT HORIZONTAL STAB UPPER CENTER PLANK 20L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LEFT HORIZONTAL STAB UPPER CENTER PLANK 20L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000. 2L73 4F RTA22WE 20030417000642003041700064NE 2003 4 17 IXXA0300009O 220030130A7297 CONNECTOR DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ENGINE EGT DIRTY A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11823BX848701301 46064 AFTER DEPARTURE FROM LRD IN CRUISE EN ROUTE TO DFW, CREW NOTED ABNORMAL RISE IN NR 1 ENGINE EGT. POWER WAS RETARDED ON NR 1 ENGINE AND TEMP RISE STOPPED. DURING DESCENT INTO DFW NR 1 EGT AGAIN BEGAN TO RISE ABNORMALLY, AS A PRECAUTIONARY ACTION NR 1 ENGINE WAS SHUT DOWN. AN UNEVENTFUL LANDING WAS MADE IN DFW. MAINTENANCE PERFORMED INSPECTION OF NR 1 ENGINE EGT SYSTEM AND FOUND SEVERAL CONNECTORS DIRTY. MAINTENANCE CLEANED, SECURED CONNECTORS AND OPERATIONALLY CHECKED EGT SYSTEM. ALL WORK WAS COMPLETED PER APPLICABLE MANUALS. AFTER GOOD OPERATIONAL CHECK THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20030424001482003042400148NM 2003 4 24 QXEA0300369 120030312A1430 RIVET BOMBDRDHC8 DHC8401 1390041NM ZONE 100 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 TWO RIVETS MISSING FROM CEILING OF NOSE LANDING GEAR COMPARTMENT AT X-141, Y .5 LEFT AND RIGHT, Z112. REPAIRED IAW DHC-8-400 SRM 51-42-05-330-801, PAGE 201. 2H72 4T RTA13NM 20030424001762003042400176SO 2003 4 24 LR7A03031 120030313A5522 STRAP LKHEED382 382G 526414USO ELEVATOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2161 4590 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST2708 FOUND LT ELEVATOR LOWER SKIN INNER STRAP BROKEN AT TRAILING EDGE HSS 67 & 76. REPAIRED IAW LAC MEA 382-55-03-013. NR 2243. 2H74 4T A1SO 20030424002142003042400214WP 2003 4 24 UPS03840375 120030322A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C2, A/C ACCESSORY BETWEEN STA 8 TO 25 AT STA 25 LONG 31L CLIP HAS CORROSION BETWEEN BOLTS. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. MAT ID FOR REP ANGLE 7075-0 .100 FILLER 7075-T6 .090 IAW DC8 SRM 53-3-3 AND REO G09155. HT TRT IAW TPS 1003 REV A 7075-0 CONDITION TO 7075-T6. FAB REPAIR ANGLE AND FILLER IAW G08155. INSTALLED REPAIR ANGLE AND FILLER IAW REO G09155. 2L74 4F RT4A25 20030425000432003042500043EU 2003 4 25 U30A200300011 120030326A3350 LIGHT AIRBUS320 A320212 3930322EU CABIN INTERMITTENT A U30AO OTHER O OTHER CRCRUISE 1 EA17265AV 427 DURING CRUISE ON FLT 313 CUN-BWI, THE EMERGENCY EXIT LIGHTS IN THE CENTER OF AIRCRAFT FLASH SPORADICALLY. ON GROUND IN BWI, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS PER AMM TASK 33-51-00-710-001, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. SDR UPDATED 12 JUNE 2003. AIR CARRIER HAS SUBMITTED TWO PREVIOUS SDR'S U30A200300007 & U30A200300009 ON SAME SYSTEM WITH SIMILAR PROBLEMS. A SUBSEQUENT INVESTIGATION REVEALED THAT AIRBUS S/B A320-33-1018 IDENTIFIES THESE PROBLEMS AND THIS S/B WAS NOT EMBODIED AT THE TIME. CARRIER GENERATED AN EO WHICH MODIFIES EPSU FROM P/N 3214-52 TO 3214-54. MODS TO FOUR EPSU'S COMPLETED ON 6/5/03. EMER EXIT LIGHT SYS HAS NOT FAULTED SINCE 3/31/03. THIS SDR U30A200300011 IS CLOSED.2L72 4F RTA28NM 20030429000292003042900029NM 2003 4 29 PCA0300814 120030127A5320 FLOOR SUPPORT BOEING747 747283B 1384867NM FUSELAGE DISTORTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LWR-LOBE AFT CRG DISTORTION ON THE FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1900-1920. DAMAGED PORTION FLOOR TRACK REMOVED, NEW SECTION INSTALLED PER SRM 53-40-02 & PER SRM 51-30-02. 2L74 4F A20WE 20030429000422003042900042NM 2003 4 29 AT0300011 120030409A33508039251 BATTERY PACK BOEING717 717200 1383700NM EMERGENCY LIGHT DISCHARGED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15987AT 55088 EMERGENCY LIGHTS AT SEATS 11-19 AND 25-31 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER B717 M/M 33-51-03 AT STATION 804R, OPS CHECK GOOD. 2L72 4F TRA6WE 20030430000202003043000020EU 2003 4 30 AWXA200300449 120030401A5320D53470481206 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FITTING FLOOR SUPPORT IN AFT CARGO COMPARTMENT FR 52, RBL 28. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5325-00280-JL1. 2L72 4F RTA28NM 20030430001592003043000159NM 2003 4 30 SWAA030876 120030419A57546573714 SKIN BOEING737 7373H4 1384600NM NR 6 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/2D CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT MIDDLE AUX TRACK. REPAIRED NR 6 L/E SLAT PER SRM. 2L72 4F RTA16WE 20030430001402003043000140NM 2003 4 30 SWAA030909 120030423A532065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 7 EA ) AT BS 380 AT STR 8L, BS 616 AT STR 4L, BS 727D AT STR 6L, BS 767 AT STR 3L, BS 867 AT STR 3L, BS 500D AT STR 8L & BS 500D AT STR 7L. R&R STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20030501000022003050100002SO 2003 5 1 SIMA200302205 120030119A532014525480003 SILL EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE 145160 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-40-06 AND EMB 145 CPM 51-21-04 THROUGH 51-21-06. (M) 2L72 4T RTT00011AT 20030430001242003043000124NM 2003 4 30 03FDEA00579 120030423A5270 WARNING LIGHT BOEING727 727200 138407ENM ZONE 200 ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25268FE 21674 REPEAT 3RD TIME IN 5 DAYS. MAIN CARGO DOOR LIGHT CAME ON WHEN CLIMBING ABOVE 290. LIGHT FLICKERED INITIALLY THEN CAME ON STEADY. DESCENDING DOWN TO 290 LIGHT WENT OUT MOMENTARILY. DIVERTED A/C AND FOLLOWED RED TAB PROCEDURES. LIGHT CAME ON AND OFF INTERMITTENTLY DURING DESCENT AND WENT AT 18K. TROUBLESHOT PER 727 WDM 52-31-01 AND ALL PREVIOUS WRI'S. R & R CARGO DOOR ARM DISARM RELAY R9015 PER SMP. PRESSURIZED A/C TO 6.5 DIFFERENTIAL ALL OPERATIONS NORMAL THROUGH PRESSURIZATION AND DEPRESSURIZATION. CYCLED DOOR NUMEROUS TIMES WITH NORMAL INDICATION EVERY TIME. 2L73 4F RTA3WE 20030502000952003050200095 2003 5 2 FWTA200341601 420030414A31406227999003 COMPUTER BOEING767 767300 1385204NM GE CF6 CF680C2B7 NE COCKPIT FALSE INDICATIONA FWTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19316LA 30842 DURING CLIMB EICAS MSG Z1583200, FWD OVERHEAT DISPLAYED AND OVERHEAT LIGHT ILLUM. AFTER SELECTOR WAS POSITIONED T STBY, 5 MINUTE DELAY. AFTER SELECTOR WAS POSITIONED TO OVERRIDE, EICAS MSG. FWD EQUIPMENT COOLING DISPLAY AND NO COOLING LIGHT ILLUM. RETURNED TO SEGU. MAINTENANCE CHECKED IN ACC FIM 21-58-00, PAGE 141 AND MM 28-51-17, PAGE 201-202 WAS CHECKED EICAS MSG NO OBSERVATIONS FOUND. OVER WT LANDING AT SEGU, LANDING WT WAS 163,400. MAINTENANCE WAS INSPECTED ACC- TASK 05-51-35-212 OP1, PHASE 1 EXAMINATION, FOUND OKAY. 2L72 4F4 FRTA1NM E13NE 20030502001082003050200108NM 2003 5 2 PCA0300839 120030410A5230 SKIN BOEING747 747249F 1384849NM CARGO DOOR DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 AFT CARGO DOOR EXTERIOR SKIN - OIL CAN - 10 INCHES AFT AND 20 INCHES BELOW LATCH. REPAIR PER 52-00-03 FIG 4. 2L74 4F A20WE 20030505000082003050500008NM 2003 5 5 DHL2003741553 120030323A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C-CHECK DISCREPANCY AS FOLLOWS, BS 848 RT SIDE STR 17 BELOW THE FLOOR IS CRACKED AFT AT CIRCUM. CUT OUT AREA OF SKIN FOR ACCESS IAW B-727 SRM 53-30-3 FIG 3 DIM 10 X 3.75 INCH. CUT OUT DAMAGED SECTION OF STRINGER DIM 25 INCHES LONG IAW B-727 SRM 51-40-4 FIG 1. FABBED REPAIR DOUBLER FOR SKIN FROM 2024 T3 .250 PO 9912497 DIM 22 X 9 INCH AND FILLER, SAME MAT, DIM 10 X 2.875 INCH IAW B-727 SRM 53-30-3 FIG 3. FABBED REPAIR ANGLES 2 EACH, 1 EACH FROM LN 9496-55, PO 9911379 AND 1 EACH FROM 60-32849 PO 288949 DIM 10.5 INCH EACH IAW B-727 SRM 51-40-4 FIG 1. ALL PARTS TREATED AND PRIMED IAW B-727 SRM 51-40-4 FIG 1 AND 53-30-3 FIG 3. 2L73 4F RTA3WE 20030505000832003050500083EA 2003 5 5 SWIA200311888 120030414A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FALSE ACTIVATIONA SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07915SW 7615 FLAP FAIL MESSAGE APPEARED WITH FLAP SELECTED TO FLAPS 8. FLAP FAILED IN UP POSITION. RESET FLAP SYSTEM AND INSPECTED FLAP SURFACES. INSPECTION REVEALED NO IRREGULARITIES. RECORDED FLAP SYSTEM FAULT CODES. FLAPS OPS CHECKED NORMAL. RAN FLAPS UP AND DOWN SEVERAL TIMES. NO FAULTS NOTED. 2L72 4F RTA21EA 20030507002102003050700210NM 2003 5 7 CH1A200395030 120030409A5320 WEB BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 CORROSION FOUND ON FLOOR WEB UPPER SURFACE FWD OF AFT ENTRY DOOR CUTOUT LBL 14 TO RBL 14 BS 1173. 2L73 4F A3WE 20030509001652003050900165NM 2003 5 9 USAASB03046 120030329A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US 23984 PIT - DUIRNG OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 12 THROUGH 19, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1136 BATTERY CHARGER ASSEMBLY AND THE BATTEYR PACK, P/N 2013-1A. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20030509000592003050900059CE 2003 5 9 SVV2003F00001 120030406A32603581507715 UPLOCK BRACKET BEECH 36 A36 1151604CE CONT O520 IO520* 17032SO RT WHEELWELL WORN E SVVAO OTHER O OTHER NRNOT REPORTED 1 AL059468Q E314 ACTUATOR ROD TO RT GEAR, FAILED. APPARENT CAUSE MAY HAVE BEEN DIRT AND DEBRIS ON UPLOCK ROLLER. ALSO, FOUND A SLIGHTLY WORN UPLOCK BRACKETT. ALL AD`S AND SERVICE BULLETINS COMPLIED WITH. (RECD 4/22/03 CW) 1L71 3O3 O 3A15 E5CE 20030513001742003051300174NE 2003 5 13 2003UALA00382 220030415A7230 COMPRESSOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 WP29643UA 25093 COMPRESSOR STALL ON NR 1 ENGINE. ENGINE SURGED ON CLIMB AND RECOVERED. BOROSCOPE FOUND CRACK ON 14TH STAGE STATOR AND BENT 14TH AND 15TH STAGE BLADES. ENGINE WAS REMOVED AND THE HPC WILL BE OVERHAULED. UPON DISASSEMBLY OF THE HPC NO STATORS WERE CRACKED AND THERE WERE NO BENT BLADES. INSPECTION OF THE REAR HOOK WEAR IN THE COMPRESSOR SHOWED NO UNUSUAL DISTRESS. ROOT CAUSE: INCREASED TIP CLEARANCE IN THE HPC. 2L72 4F4 FRTA1NM E24NE 20030513000022003051300002GL 2003 5 13 TZM2003F00000 120030321A3110133065 DIODE AMTR SKYSMISMITHMINIPLA05625N3GL LYC O540 TIO540* 41532EA INSTRUMENT PANELLOOSE E TZMAO OTHER O OTHER NRNOT REPORTED 1 SW05301PJ25 610146077 PILOT EXPERIENCED A SMALL AMOUNT OF SMOKE FROM UNDER INSTRUMENT PANEL BY CIRCUIT BREAKER PANEL. INSPECTION FOUND ALTERNATOR FUSES BLOWN AND DIODES LOOSE. MOUNT FUSES REPLACED DIODES TIGHTENED WITH NO FURTHER PROBLEMS. 1B71 3O3 ONCEXPA1B71E14EA 20030514000302003051400030EU 2003 5 14 AALA20030257 120030301A3397 WIRE FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211411G 11369 DURING OVERNIGHT MAINTENANCE, NR 4 OVERHEAD 6 VOLT CENTER AISLE EMERGENCY SPOT LIGHTING INOPERATIVE. REPAIRED NR 4 OVERHEAD 6 VOLT CENTER AISLE EMERGENCY SPOT LIGHTING WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 20030514001872003051400187NM 2003 5 14 03FDEA00666 120030501A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CORROSION (C53-113-01, 2) ON FRAME + SHEAR TIE FWD AND AFT SIDES BS 1166 WL 146 LBL 12. CORROSION ON FRAME AND SHEAR TIE FOUND TO BE OUT OF LIMITS PER SRM 51-30-2. CUT OUT SECTION SHEAR TIE. FABRICATED REPAIR PARTS FROM BAC 1490-2738 7075 T6 LOT 487559 7075 T6 .100 LOT 381963 PER SRM 53-10-4 FIG B. ALODINE AND PRIMED PER SRM 51-10-2. INSTALLED FASTENERS COMMON TO REPAIR AREA. 2L73 4F RTA3WE 20030602001532003060200153NM 2003 6 2 SWAA031141 120030520A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT BS 947, WL 208 AND LBL 53. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20030604001552003060400155NM 2003 6 4 UPS03440575 120030413A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, SEAT TRACK FOUND CORROSION. CORROSION BLEND OUT ( 0.050 X 5/8 X 2 INCHES). M/D SEAT TRACK REPAIRED AT BS 770-850 LBL 98 AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20030602000932003060200093 2003 6 2 SWAA031185 420030528A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F A16WE 20030515001232003051500123NM 2003 5 15 AWXA200300532 120030513A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 18 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28179AW 22646 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030520000912003052000091NM 2003 5 20 USAABB03062 120030417A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND AISLE EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 18DEF INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA2NM 20030606000872003060600087NM 2003 6 6 03FDEA00762 120030513A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B CTR BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR. 2L73 4F RTA22WE 20030522000492003052200049WP 2003 5 22 GTIA030312 120030417A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE FUSELAGE BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 CABIN FLOOR PANEL AT FS 200-237 CENTER IS BROKEN IN CENTER. FABRICATED NEW FLOOR PANEL. 2L72 4F4 F A6WE E2EA 20030522000362003052200036NM 2003 5 22 2003UALA00082 120030123A3412102LA2AG PROBE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TAT MALFUNCTIONED A UALAO OTHER G MULTIPLE FAILURE CRCRUISE 1 WP29648UA 25285 AT FL 370, AUTO THROTTLE AND AUTO PILOT DISENGAGED. TCAS, GROUND PROXIMITY, FLIGHT DIRECTOR, AND TAT INOPERATIONAL. *S/D* REPLACED TAT PROBE AND ANOMALY WAS CORRECTED. 2L72 4F4 FRTA1NM E24NE 20030609001292003060900129EU 2003 6 9 MALA030276 120030504A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15525XJ E2350 DURING C-CHECK INSPECTION IN CVG, NR 3 SEAT TRACK HAS CORROSION FROM FRAME 10-20A. MAINTENANCE REPAIRED SEAT TRACK IAW EO #A53026. REF TO 409 # 118106 FOR DETAIL. A/C RELEASE DATE 5/21/03. 2H74 4F RTA49EU 20030617000192003061700019NE 2003 6 17 AUS20030484 220030417A7200 ENGINE CESSNA500 500CESSNA 2076602CE PWA JT15 JT15D1 52060NE RIGHT SEIZED W O OTHER EXJVIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 AUS (AUS) RT ENGINE FAILED AND COULD NOT BE RESTARTED. INVESTIGATION FOUNDTHE ENGINE SEIZED. 1L72 4F4 F A22CE E1NE 20030617002392003061700239EA 2003 6 17 QXEA200300731 120030614A26119847101505 CAGE CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09603QX 10011 BOI- CHIMNEY AT FORWARD CARGO DOORWAY DAMAGED. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030617001762003061700176NM 2003 6 17 QXEA200300689 120030603A7110 ANGLE BOMBDRDHC8 DHC8401 1390041NM RT COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - RIGHT LOWER COWL FORWARD CONE SUPPORT BRACKET UPPER ANGLE CRACKED AT FORWARD FOUR RIVETS. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20030618000792003061800079SW 2003 6 18 HEEA087342 120030611A6510407040303119A SHAFT BELL 407 407 1182206SW BLOWER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03742PH 53461 WORN SPLINES. REPAIRED. 1G71 3U O H2SW 20030527000172003052700017WP 2003 5 27 NACA20030084 120030503A733240020 PRESSURE SWITCH DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE ENGINE FALSE INDICATIONA NACAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AL032907F3622 3622 44636 37306 FUEL PRESSURE LIGHT ILLUMINATED DURING TAKEOFF ROLL. REPLACED NR 2 ENGINE FUEL PRESSURE WARNING SWITCH. 2L74 4R4 R 6A3 5E8 20030620000792003062000079NM 2003 6 20 USAA030076 120030515A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US 23311 FOUND SKIN CRACKED 1 INCH, S22R BETWEEN FRAME STATION 727D AND 727E. INSTALLED DOUBLER PER EA 87231. (M) 2L72 4F RTA16WE 20030624000882003062400088NM 2003 6 24 DL757030462 120030512A5330146N378014 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27627DL 22917 FUSELAGE SKIN WAS FOUND DENTED AT FS 1695 ABOVE THE STRINGER 26R SKIN LAP JOINT. THE DAMAGED AREA OF SKIN WAS REMOVED WITH A 3 X 9 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385021-14,REV B. 2L72 4F RTA2NM 20030624000142003062400014NM 2003 6 24 USAABB03074 120030515A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU 27124 THE FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 FAILED. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20030710000922003071000092CE 2003 7 10 GLBA2003083 120030615A2751 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS DIRTY A GLBAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM03245GL UE245 FLAPS WOULD NOT RETRACT AFTER T/O. CLEANED SPLIT FLAP SWITCH, OPS CK GOOD. 2L72 4T RTA24CE 20030711001022003071100102NM 2003 7 11 VNAA0306010 120030617A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN INOPERATIVE A VNAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07438JS 3056 THE CREW REPORTED THAT SOME OF THE EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE FLOOR EMERGENCY LIGHTING STRIPS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20030714001342003071400134EU 2003 7 14 DHL2003365010 120030701A5230 SKIN AIRBUS300 A300B4203 3930306EU CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH 149 SMALL DENT FOUND AFT OF LOWER REAR CARGO DOOR AT STA NR 4096 (1617 INCHES). DEFERRED PER GMM 3.5 CAT I IAW A300 SRM 51-41-10 PG 701. CONTROL NR 13411. PLACARD INSTALLED. REF: DMI 13411 SMALL DENT FOUND AFT OF LOWER REAR CARGO DOOR AT STA NR 4096 (1617 INCHES). CUT OUT DAMAGE,0 PERFORMED HFEC OF CUT OUT REPAIRED IN ACCORDANCE AIRBUS A300 SRM 53-10-10-PG 714-718. THIS CLEARS DMI 13411. 2L72 4F RTA35EU 20030127000792003012700079SW 2003 1 27 HEEA083652 120030114A282070079H100F210 HOSE BELL 407 407 1182206SW FUEL DIST CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 FUEL HOSE ASSY PROTECTIVE COVERING IS CHAFED THROUGH. 1G71 3U O H2SW 20030127002912003012700291NM 2003 1 27 03FDEA00032 120030115A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 FRAME DENTED AT BS 1030 ABOVE STR 26R. REPAIRED DAMAGED FRAME AT BS 1030 ABOVE STR 26R PER SRM AND EA. 2L73 4F RTA3WE 20030128000522003012800052 2003 1 28 HEEA083805 420030116A34424000035 TRANSCEIVER BELL 407 407 1182206SW WX RADAR SYS WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 WEATHER RADAR TRANSCEIVER TRANSMITS AND RECEIVES WEAK AND BROKEN. FOUND OSCILLATOR BOARD HAS BAD OVEN. SCRAPPED UNIT. 1G71 3U O H2SW 20030128002652003012800265EA 2003 1 28 COMA0360053 120030125A30307858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01989CA12065 7215 FLIGHT 6562 TAT AND R/H PITOT HEAT CAUTION MESSAGE.REPLACED THE #2 ADSHC. 2L72 4F RTA21EA 20030207001142003020700114NE 2003 2 7 NACA20030072 220030206A8530404482 CYLINDER PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE #9 BROKEN A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL031377K2114 2114 P28818 44596 P28818 DISCREPANCY: #2 ENGINE SHUT DOWN DUE TO A #9 CYLINDER DOUBLE SHORTED SECONDARY.CORRECTIVE ACTION: REPLACED #9 CYLINDER. BROKEN VALVE SEAT. 2L74 4R4 R A781 5E8 20030210000522003021000052EA 2003 2 10 QXEA0300035 120030111A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA COCKPIT DETECTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09601QX 10009 BOI ON FLIGHT 2447- VERY NOTICEABLE MUSTY FOUL ODOR THROUGHOUT CABIN AND COCKPIT. DISSIPATES IN ABOUT FIVE MINUTES AFTER APU SHUTDOWN. RETURNS WITH APU START UP. ALSO NOTED SMELL IN DESCENT FROM 10,000 TO GROUND. OPERATED AIRCRAFT WITH APU AIR WITHOUT ENGINES RUNNING. NO UNUSUAL ODOR NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030210000812003021000081SO 2003 2 10 C2XA03CL031 120030204A5210 DOOR EMB 135 EMB135LR 3260305SO FORWARD FUSELAGEOUT OF ADJUST A C2XAK NONE O OTHER TXTAXI/GRND HDL 1 SW2727523 145389 LEX FLIGHT#2326 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN AND CLOSE PROPERLY.MAINTENANCE INSPECTED AND REPLACED THE CABIN DOOR FRAME SEAL AND ADJUSTED THE MAIN CABIN DOOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20030210001062003021000106NM 2003 2 10 QXEA0300054 120030107A5320 FITTING BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX-CLEAT CRACKED FOR SUPPORT STRUCTURE FOR VHF ANTENNA AT AFT OUTBOARD OUTSIDE CORNER. REPAIR IAW HORIZON AIR EO 6-53-162. 2H72 4T RTA13NM 20030214000672003021400067WP 2003 2 14 ASAA0380047 120030105A57535912149511 FITTING DOUG DC9 DC983 3022083WP T/E FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT WING OUTBOARD FLAP MID FITTING HAS TOOLING MARKS AND GOUGES, TWO PLACES. REPAIRED PER EA 5750-01759. (M) 2L72 4F RTA6WE 20030217000112003021700011EU 2003 2 17 MALA030156 120030214A242051634002 GCU SAAB SF340 SF340A 7850100EU ELECTRICAL FAILED A MALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL15110XJ 340A110 DURING FLIGHT 3294, ON MISSED APPROACH RT AC GEN CAUTION LIGHT ILLUMINATED, RH AC GEN WAS UNABLE TO RESET AND WAS TURNED OFF PER QRH. AIRCRAFT IN ICING CONDITIONS FOR APPROXIMATELY 10 MINUTES WITH RH AC GEN OFFLINE. MAINTENANCE REPLACED GEN, DID NOT FIX, INSTALLED ORIGINAL AC GEN INSTALLED AC GCU OPS CHECK GOOD. 2L72 4T RTA52EU 20030218001842003021800184NM 2003 2 18 QXEA0300176 120030125A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - NR 2 SEAT TRACK HAS PITTING CORROSION AT STATION 455. REPAIRED IAW RD 8-53-1342, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20030219000982003021900098NM 2003 2 19 SWAA030316 120030208A5523BACB28AK04 BUSHING BOEING737 7377H4 1384404NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29745SW 29491 DURING SCHEDULED PM CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 AND NR 4 HINGE HARDWARE AND BUSHINGS PER SWA SI AND MM. 2L72 4F RTA16WE 20030220000262003022000026NM 2003 2 20 03FDEA00122 120030213A5311 FRAME BOEING727 727233 138408ANM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 STA 1010, LBL 63, WL 215, FRAME HAS A GOUGE. 2L73 4F RTA3WE 20030224000292003022400029CE 2003 2 24 BAQA084137 120030219A3297 WIRE BEECH 100 100BEECH 1152916CE MLG SELECTOR BROKEN H BAQAO OTHER O OTHER NRNOT REPORTED 1 FS01999G 53 B144 WIRE BROKEN IN HANDLE. REPLACED WITH SERVICEABLE UNIT. 1L72 3T A14CE 20030224001352003022400135NM 2003 2 24 AWXA200300185 120030128A5320146N5447 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1475, STR 28 - 29L. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AREA OF FLOOR SUPPORT BS 1475, STR 28 - 29L; FABRICATED REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1-7. 2L72 4F RTA2NM 20030228000852003022800085WP 2003 2 28 ASAA0380008 120030103A57209957498501 SUPPORT DOUG DC9 DC983 3022083WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING TRAILING EDGE INNER SUPPORT FORMER CRACKED AT FORWARD EDGE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-10-2, 51-10-4, AND 51-30-2. (M) 2L72 4F RTA6WE 20030304000082003030400008SW 2003 3 4 AC2A084864 120030224A6410MS276414 BEARING BELL 430 430 1182150SW TAIL ROTOR WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CT 49089 TAIL ROTOR BEARINGS ARE WORN. REPLACED WITH NEW BEARINGS. 1G72 3U RTH9SW 20030305000062003030500006 2003 3 5 HEEA084611 420030214A2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 TRANSCEIVER WILL NOT TRANSMIT. REMOVED CORROSION FROM UNDER VCO SHIELD AND APPLIED HUMISEAL TO AREA FOR CORROSION CONTROL. ALSO REMOVED CORROSION FROM CHASSIS. REPLACED 2 BAD FLEX CABLES ON SERIAL BOARD. ADJUSTED CARRIER SQUELCH, TRANSMIT COMPRESSOR AND SIDE TONE. BENCH CHECK GOOD. 1G72 4U H4SW 20030306000052003030600005SW 2003 3 6 HEEA084718 120030217A632194501031 BRAKE ASSY BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 MAIN ROTOR BRAKE HAS WORN PUCKS. REPAIRED. 1G72 4U H4SW 20030307000922003030700092NE 2003 3 7 HEEA084894 120030227A6230 BEARING SKRSKYS76 S76A 8143006NE M/R SCISSORS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH A18500621 760078 MAIN ROTOR ROTATING SCISSORS HAVE WORN BEARINGS. REPAIRED. 1G72 3U H1NE 20030625001112003062500111NM 2003 6 25 F3LA200300094 120030302A5240 PANEL BOEING737 7372Y5 1384554NM LAV SERVICE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03921WA 3501 23039 DURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SERVICE PANEL CORRODED AT FWD HINGE. FOUND TO BE OUT OF LIMITS PER SRM 51-30-02. FABRICATED REPLACEMENT PANEL AND DOUBLER PER EA 52F-737-091. ALODINED PER SRM 51-21-41, PRIMED AND PAINTED PER SOPM 20-41-02. INSTALLED DOUBLER AND PANEL PER EA 52F-737-091. INSTALLED HATCH ASSY. ON PANEL PER SRM 51-40-02. 2L72 4U RTA16WE 20030310000652003031000065SW 2003 3 10 HEEA084969 120030227A3213412030437103 CAP BELL 412 412 1182202SW MLG CROSSTUBE WORN E O OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 MLG CROSSTUBE CAP RUBBER WORN. REPAIRED. 1G72 4U H4SW 20030310001172003031000117WP 2003 3 10 CALA0300101 120030307A5311 FRAME DOUG DC9 DC982 3022082WP STA 1418 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 INSPECTION FOUND A 1" CRACK IN FRAME RADIUS AT STA 1418, LONGERON 2L AND 2R. REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-04332. 2L72 4F A6WE 20030311000502003031100050SW 2003 3 11 HEEA085065 120030228A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034180F233 MAIN BATTERY WEAK. 1G71 3U H2SW 20030313002192003031300219NM 2003 3 13 QXEA0300193 120030124A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING NR 4 FLAP TRACK, OUTBOARD LOWER TRACK. UPPER SURFACE PITTED. REPAIRED IAW HORIZON AIR EA 2-57-220. 2H72 4T RTA13NM 20030313002262003031300226NM 2003 3 13 QXEA0300200 120030123A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM T/E FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT HAND WING, NR 5 FLAP TRACK, UPPER DEAD WEIGHT ROLLER TRACK SURFACE IS PITTED. REPAIRED IAW HORIZON AIR EA 2-57-221. 2H72 4T RTA13NM 20030314001192003031400119 2003 3 14 SWAA030563 420030311A25656557463 FITTING BOEING737 7373H4 1384600NM AFT SVC DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING LOOSE. SECURED ATTACH FITTING PER MM, 2L72 4F RTA16WE 20030328000272003032800027WP 2003 3 28 03FDEA00284 120030307A2810 FITTING DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 RIGHT WING NR 3 TANK HAS A CRACKED SPAR TO RIB FITTING AT STATION XORS 402, SPAR STATION S37 INSIDE TANK PLATE 634AT. THIS WAS FOUND DURING ROUTINE INSP. ON W/C 28C1503-02 AT MAE, AND WILL BE WORKED ON N/R N00838, UNDER W/O 13338 REMOVED AND REPLACED FITTING IAW SRM 51-31-01. ORDERED NEW FITTING, DRILLED AND INSTALLED FITTING I.A.W. SRM 51-31-01. 2L73 4F A22WE 20030318000362003031800036SW 2003 3 18 ERAA085161 120030218A6420 BEARING BELL 412 412 1182202SW TAIL ROTOR HEAD ROUGH H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01419EH15246 HB580 TRUNNION FEELS ROUGH, PITCH HORN BUSHINGS & INBOARD BOLTS, NUTS & WASHERS MISSING. REMOVED TRUNNION, HOUSINGS, SCRAPPED TRUNNION & TRUNNION BEARINGS. INSTALLED NEW TRUNNION, BEARINGS & SEALS. REASSEMBLED, TORQUED, SAFTIED, MARVEL BALANCED IAW 412 CR&O &TB 412-95-134. 1G72 4U H4SW 20030318001302003031800130NM 2003 3 18 GAIA03002BOP 120030203A7500652244117 DUCT BOEING727 727223 1384074NM NR 2 ENGINE BLOWN A GAIAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07856AA 20997 FLT - 272 - MSP-MCI - AT APPROXIMATELY 200 FEET AGL THE NR 2 ENGINE HAD A FIRE INDICATION. THE CREW DECLARED AN EMERGENCY AND SHUTDOWN THE NR 2 ENGINE AS PER EMERGENCY PROCEDURES. UPON ENGINE SHUTDOWN, THE FIRE INDICATION EXTINGUISHED. AIRCRAFT PERFORMED AN AIR TURN BACK TO MSP. AN UNEVENTFUL LANDING WAS MADE. FOUND 13TH STAGE SADDLE DUCT BLOWN. REMOVED AND REPLACED DUCT. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20030320000442003032000044NM 2003 3 20 USAASB03012 120030118A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHTSDAMAGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19521AU 23856 GSO - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEATS 7 AND 18, LT SIDE, INOPERATIVE. MAINTENANCE REPAIRED WIRING ON SEATS 7ABC AND 18ABC. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20030320001232003032000123NM 2003 3 20 2003UALA00113 120030128A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29353UA 24321 FRAME CRACKED AT BS 847 STRINGER 9R AT STOW BIN SUPPORT RAIL. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR. 2L72 4F4 FRTA16WE E2GL 20030122000112003012200011SW 2003 1 22 HEEA083398 120030109A2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 MAIN BATTERY VOLTAGE DROPPED TO SEVEN VOLTS. SCRAPPED. 1G71 3U H2SW 20030122001292003012200129EU 2003 1 22 HEEA083500 120030107A7933TM41039 INDICATOR BOLKMS105 BO105S 5626006EU TRIPLE OIL TEMP READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036607K S841 NR 1 ENGINE OIL TEMP GAUGE STICKS 40 DEGREES LOWER THAN NR 2. 1G72 3U H3EU 20030122002032003012200203NM 2003 1 22 DHL2003742004 120030122A2611 LAMP BOEING727 727225 1384077NM A DHLAKO NONE OTHER L NO TEST ININSP/MAINT 1 SO01742DH 21290 1) #2 SMOKE DETECTION TEST LIGHT INOPERATIVE.2) RELAMPED #2 SMOKE DETECTOR IAW M/M 26-17-02, SYSTEM OPS CHECKED GOOD. 2L73 4F A3WE 20030320001702003032000170NM 2003 3 20 SWAA030616 120030318A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A + 16, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20030321000432003032100043NM 2003 3 21 CALA0300123 120030320A5330 SKIN BOEING777 777224 1385225NM BS 626 NICKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2774007 29477 INSPECTION FOUND FUSELAGE SKIN NICKED AT BS 626, S3L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53-00-01, REPAIR 2, FIGURE 202. 2L72 4F RTT00001SE 20030731001222003073100122EA 2003 7 31 QXEA200300780 120030630A2120 SEAL CNDAIRCL600 CL6002C10 1390015EA ACM WORN A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09606QX 10023 BOI- ON FLIGHT 2524 AFTER TAKEOFF RECIEVED RIGHT BLEED DUCT WARNING. AUTO SYSTEM TEMPORARY SHUT OFF RIGHT BLEED SYSTEM AND MESSAGE CHANGED TO A CAUTION. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ACM SEALS AND COUPLING. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20030801001012003080100101EA 2003 8 1 COMA0360319 120030710A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN LOOSE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01457CA 7612 FLIGHT 5869 EMERGENCY FLOOR PATH LIGHTING IS INOP AT ROW 8. REPAIRED LOOSE WIRE CONNECTOR AT ROW 8. 2L72 4F RTA21EA 20030416002432003041600243NM 2003 4 16 CALA0300180 120030406A5330 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE WINDOW POST CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912319 23370 INSPECTION FOUND A 2 INCH CRACK IN SKIN OF PILOT'S LT WINDOW POST. REPAIRED IAW SRM 53-10-01. 2L72 4F4 FRTA16WE E2GL 20030418000692003041800069NM 2003 4 18 QXEA0300279 120030206A5320 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - FORWARD SUPPORT ANGLE UNDER PANEL 262AT HAS CHAFE DAMAGE ON TOP SURFACE. REPAIRED IAW HORIZON AIR EA 6-57-118. 2H72 4T RTA13NM 20030418001282003041800128SO 2003 4 18 SWIA200311784 120030212A2730 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO LT ELEVATOR MALFUNCTIONED A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07207SW 120266 ABORTED TAKEOFF WITH AURAL WARNING. REPOWERED AIRCRAFT AND DID A COMPLETE AURAL WARNING SYSTEM RESET. NOW IT WILL NOT PASS A STATIC TEST. REPLACED LEFT PROXIMITY SENSOR IAW 27-32-00. 2L72 4T RTA31SO 20030417000482003041700048WP 2003 4 17 IXXA0300006O 120030123A5270 MECHANISM DOUG DC8 DC863F 302198FWP MLG DOOR OUT OF ADJUST A IXXAO OTHER N FALSE WARNING CLCLIMB 1 SW11867BX83172800 46049 AFTER TAKEOFF GEAR DOORS NOT LATCHED LIGHT ILLUM, AFTER GEAR RETRACTION. CREW PERFORMED UPLATCH CHECK DOORS NOT LATCHED CONTINUED TO BE ILLUM. CREW PERFORMED GEAR CYCLE, DOORS NOT LATCHED LIGHT CONTINUED TO REMAIN ILLUM. CREW NOTED NO BUFFET, YAW OR ABNORMAL AUDIBLE WARNINGS. HYD PRESS & QTY INDICATED NORMAL. UNEVENTFUL LANDING. WHEN LANDING GEAR WAS EXTENDED ALL DOWN AND LOCKED INDICATIONS WERE NORMAL INCLUDING THE DOOR NOT LATCHED LIGHT. MX DEFFERED REF DMI 27086. ACFT REPOSITIONED TO TOL FOR INVESTIGATION. MX FOUND LT MAIN GEAR DOOR FOLLOW UP MECH REQUIRED ADJUSTMENT. PERFORMED ALL REPAIRS AND SUBSEQUENT GEAR SWINGS IAW APPLICABLE ACFT MANUALS. PLACARD 27086 REMOVED AND ACFT RETURNED TO SERVICE. 2L74 4F 4A25 20030722000292003072200029NM 2003 7 22 2003F00457 120030310A5522 PANEL BOEING727 727222 1384073NM LEFT ELEVATOR CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077640U 19913 AT C-CHECK, FOUND CRACK AT LEFT ELEVATOR BALANCE BAY PANEL 9720. ROUTED CRACKED AREA ON LT ELEVATOR BALANCE PANEL NR 9720. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M) 2L73 4F A3WE 20030418001532003041800153NM 2003 4 18 PCAA0302045 120030222A2120 ODOR DHAV DHC8 DHC8102 2809003NM CABIN DETECTED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA13839EX 226 PJL-FLIGHT 3800 CREW REPORTED A BURNT OIL ODOR FROM BLEEDS WITH POWER BELOW 30 PERCENT TORQUE DURING DESCENT. ODOR WAS MORE NOTICEABLE ON THE NR 2 ENGINE. MAINTENANCE RAN THE AUXILIARY POWER UNIT BLEED AND FOUND NO DEFECTS. BOTH ENGINES WERE RUN WITH P3 AIR ON, AND NO OIL ODOR WAS NOTED FROM EITHER ENGINE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20030421002062003042100206NM 2003 4 21 AMTA200300332 120030310A3350D71702001 POWER SUPPLY BOEING737 73783N 13844HINM COCKPIT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11301TZ 28239 FORWARD SECTION OF FLOOR PATH LIGHTING SYSTEM INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY PER MM 33-51-06-2. (M) 2L72 4F RTA16WE 20030829000012003082900001CE 2003 8 29 AKG2003F00001 120030702A712045A34361009 MOUNT BRACKET BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112NE LT ENGINE SCORED B AKGRK NONE O OTHER ININSP/MAINT 1 CE0588UA 3908 RF49 SCORING DISCOVERED DURING ACCOMPLISHMENT OF AD2002-01-23 ON LEFT ENGINE AFT FLANGE OF THE FORWARD ENGINE CARRY-THROUGH BRACKET. THE SCORE LINES ARE PARALLEL AND APPEAR TO HAVE BEEN PART OF THE MANUFACTURING PROCESS. APPEARANCE OF THESE SCORE LINES IS CAUSED FOR A CLOSER INSPECTION PROCEDURE. THESE SCORE LINES MAY INDUCED STRESS RISERS IN THE BRACKET. 2H72 4F4 FRTA16SW E25EA 20030728000942003072800094NM 2003 7 28 SWAA031575 120030717A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (4 EA) AT BS 540 AT STR 4R, BS 908 AT STR 4R, BS 908 AT STR 4L AND BS 360 AT STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20030729000852003072900085NM 2003 7 29 QXEA200300744 120030607A5510 SHIM BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA HORIZ STAB DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - SHIMS UNDER FORWARD RIGHT HAND MOUNT FOR HORIZONTAL STABILIZER HAVE EXTRUDED OUT. REPAIRED IAW RD 8/4-55-089. 2H72 4T4 TRTA13NM E00062EN 20030731000832003073100083EA 2003 7 31 QXEA200300811 120030701A7120 LINK CNDAIRCL600 CL6002C10 1390015EA ENGINE MOUNT DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX - NR 1 ENGINE FORWARD MOUNT, UPPER DOG BONE LINK. HAS THREE INDENTATIONS. REPAIRED IAW HORIZON AIR EA R-71-50. 2L72 4F RTA21EA 20030801001282003080100128WP 2003 8 1 MWEA030276 120030715A523039260461 FITTING DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD CARGO DOOR INTERIOR FITTING CRACKED INBOARD OF FORWARD HINGE. FABRICATED AND INSTALLED FITTINGS. 2L72 4F A6WE 20030806000072003080600007EU 2003 8 6 BAQA088142 120030718A2822430112812 PUMP BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101* NE FUEL SYSTEM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911WS373 7068 UNIT HAD AN INTERNAL SEAL FAILURE. FUEL PUMP FAILED DURING INITIAL GROUND RUN. ENGINE HARD TO START, THEN FUEL JUST POURED OVERBOARD WITHOUT MOTORING ENGINE. REPLACED WITH SERVICEABLE UNIT. 7/22/03 1G72 3U3 U H13EU E5NE 20030903001942003090300194NM 2003 9 3 AALA20030740 120030711A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21784AN 29588 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED RIGHT FORWARD EMERGENCY EXIT LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTT00001SE 20030903002492003090300249EA 2003 9 3 03234677 120030822A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27677BR 7652 DURING MAINTENANCE INSPECTION THE NR 2 EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EXTERIOR EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CEHCK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030905001912003090500191NM 2003 9 5 USAA030141 120030814A5753 SKIN BOEING737 737301 1384611NM T/E FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US47187 23237 PIT - FOUND AFT FLAP EXTERIOR SKIN DELAMINATED, 6 INCHES - 11 INCHES FROM OUTBOARD END AND 5 INCHES FROM L/E. COMPOSITE DELAMINATED, RIGHT WING INBOARD AFT FLAP TOP SURFACE. INTERIM HOT METAL BOND CORE REPLACEMENT AND UPPER SKIN SECTION PER TR 57-53-01A. (M) 2L72 4F RTA16WE 20030812000612003081200061 2003 8 12 HEEA088514 420030712A3423C2300DL4B COMPASS BELL 206 206L3 1182108SW COCKPIT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 COMPASS LEAKING. 1G71 3U H2SW 20030813000362003081300036SW 2003 8 13 HEEA088536 120030803A6710206062721109 ACTUATOR BELL 206 206L3 1182108SW MAIN ROTOR SLOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 MAIN ROTOR ACTUATOR HAS SLOW MOVEMENT. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20030806000742003080600074SO 2003 8 6 C2XA03SH235 120030728A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 SHV- DURING C-CHECK, THE T-REINFORCEMENT ON STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030807000042003080700004EU 2003 8 7 ASOA03260 120030615A3350 SOCKET AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11535AS 464 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATVE. MAINTENANCE ADJUSTED THE PASSENGER DOOR EMERGENCY LIGHT LAMP SOCKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030814000792003081400079NE 2003 8 14 SWIA200312191 220030714A7200PW118B ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RIGHT MALFUNCTIONED A SWIAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM07221SW1199911999 120290 RIGHT NP FLUCTUATING +/- 3 PERCENT. LOSS OF RT TORQUE GAUGE, LOSS OF RT OIL PRESSURE. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. REMOVED AND REPLACED RT ENGINE WITH A SERVICEABLE ASSY. OPS AND LEAKS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20030911002332003091100233WP 2003 9 11 DHL2003604608 120030616A5230561667356 TRACK DOUG DC8 DC873F 302199FWP CARGO DOOR BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 "D" BELLY DOOR AFT TRACK BROKEN, STA 1440.000. REMOVED BROKEN AFT TRACK IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW AFT TRACK ON "D" BELLY DOOR, STA 1440.000 IAW SRM 51-1-21 PG 1. FOR OPS CHECK SEE N/R 0530. 2L74 4F RT4A25 20030912001172003091200117NM 2003 9 12 AWXA200300885 120030723A53206546959 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 LCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR WEB RT SIDE BS 500D-520. MAINTENANCE REMOVED CORRODED SHEAR WEB RT SIDE BS 500D-520; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-4695-9; INSTALLED REPAIR PART IAW B737-300 SRM 53-30-13, FIG 101, PG 1. 2L72 4F RTA16WE 20030929001142003092900114EU 2003 9 29 RAIAOO308229 120030828A7500ATD50N DUCT AEROSPATR72 ATR72202 8680940EU RT ENGINE CRACKED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03723TE 283 RT ENGINE WILL NOT MAKE TORQUE WITHIN TURBINE TEMPERATURE LIMITS. MAINTENANCE REMOVED AND REPLACED THE SURGE VALVE DISCHARGE DUCT. GROUND RUN ACHIEVED TARGET TORQUE. 2H72 4T RTA53EU 20030915000872003091500087EU 2003 9 15 BAQA088244 120030731A79300235237790 CHIP DETECTOR AEROSPSA365 SA365N 8680669EU ENGINE SHORTED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM 6396 CHIP DETECTOR HAS A ELECTRICAL CONNECTION LOOSE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H10EU 20030912000592003091200059WP 2003 9 12 DHL2003604731 120030521A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 MAIN CARGO COMPT FRAME SHOWS INTERIM REPAIR AT STA 1580.000, L-21R TO L-19R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110, SRM 51-1-1, DPS 7.00-01. TRIMMED OUT DAMAGED FRAME AND FABRICATED NEW FRAME SEGMENT AND SPLICE ANGLES 2 EA WITH IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. PERFORMED HEAT TREATMENT TO NEW FRAME SEGMENT AND SPLICE ANGLES IAW SRM 51-1-1, DPS 7.00-01. CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT AND SPLICE ANGLES IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND SPLICE ANGLES WITH NEW FASTENERS IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030912000842003091200084NM 2003 9 12 AWXA200300832 120030709A5315D5347220924500 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR BEAM Y1292 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 6-7. 2L72 4F RTA28NM 20031003000962003100300096SO 2003 10 3 C2XA03BT091 120030913A3350110049 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 CREW REPORTED, "EMERGENCY EXIT SIGN BACKLIGHT INOPERATIVE ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY EXIT LIGHT BATTERY PACK. IAW EMB145 AMM #33-50-04. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20031003000982003100300098NM 2003 10 3 CALA0300528 120030913A2612 FIRE DETECTOR GARRTT BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE APU INOPERATIVE A CALAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2758606 P100654 27319 THE APU FIRE DETECTION LIGHT ILLUMINATED WHILE ENROUTE FROM PHL TO IAH. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE WARNING LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE APU FIRE DETECTION ELEMENT M334 WAS FOUND AT FAULT. THE FIRE DETECTION ELEMENT WAS REMOVED AND REPLACED. THE FIRE DETECTION SYSTEM PASSED ALL FUNCTIONAL TESTS. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED IAW MM 26-22-00. 2L72 4F4 FRTA16WE E2GL 20031006000152003100600015EU 2003 10 6 MALA030414 120030812A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15523XJ E2348 DURING C-CHECK IN CVG, NR 4 SEAT RAIL CORROSION. MAINTENANCE REPAIRED IAW EO A53026. REFER TO 409 190260 FOR DETAIL. A/C RELEASE DATE 9/2/03. 2H74 4F RTA49EU 20031007000212003100700021NM 2003 10 7 AALA20030533 120030505A2910 LINE BOEING767 767323 1385205NM HYD SYSTEM DAMAGED A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21373AA 25200 DURING CLIMB, RECEVIED EICAS MESSAGE, LOW CENTER HYDRAULIC QUANTITY. PERFORMED PROCEDURE, TURNED OFF CENTER PUMPS WITH CENTER SYSTEM SHOWING APPROX .25 QUANTITY. RETURNED TO ORD, ACCOMPLISHED ALTERNATE GEAR AND FLAP EXTENSION. LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT MLG TRUCK POSITION ACTUATOR LINE AND NR 1 CENTER HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20031008000032003100800003NM 2003 10 8 03251413 120030908A3350362624 LAMP DORNERDO32 DO328300 NM EMERGNECY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27413FJ 3168 DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY TRACK LIGHTING STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20031007001162003100700116NM 2003 10 7 DHL2003721008 120030917A5270 WARNING LIGHT BOEING727 727228 1384083NM E/E DOOR ILLUMINATED A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01721DH 19545 REJECTED TAKEOFF DUE TO ILLUMINATION OF EQUIPMENT ACCESS LIGHT ON SECOND OFFICERS PANEL. WT - 147.1, AIRSPEED - 70 KTS, OAT - 22 C, PRESS ALT - 460', BRAKE ENERGY ZONE: NORMAL. ITEM TRANSFERRED TO DMI 14168 PER MEL 52-4 CAT-C. PLACARD INSTALLED. REF DMI 14168, REJECTED T/O DUE TO EQUIPMENT ACCESS DOOR LIGHT ILLUMINATING. INSPECTED EQUIPMENT ACCESS DOOR. OPERATED SEVERAL TIMES, OPS CHECKED GOOD IAW BMM CHAPTER 52-40-11, REJECTED T/O DUE TO INDICATION ONLY THIS CLEARS DMI 14168, PLACARD REMOVED. 2L73 4F RTA3WE 20031021000552003102100055WP 2003 10 21 GTIA030709 120030904A5320 CLIP DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FTW - FOUND FORWARD PIT FS 237 INTERCOSTAL CLIP CRACKED STRINGER 27L. REMOVED BROKEN INTERCOSTAL. FABRICATED NEW INTERCOSTAL CLIP. INSTALLED NEW INTERCOSTAL CLIP. (M) 2L72 4F A6WE 20031021002302003102100230SO 2003 10 21 C2XA03SH332 120030920A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO DOORWAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 SHV-DURING C CHECK THE CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20031022000112003102200011NM 2003 10 22 F3LA200300141 120030920A5320 INTERCOSTAL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03315FL 1337 25159 DURING C-4 CHECK, INSPECTION REPORTED LONGITUDINAL INTERCOSTAL AT RBL 24 BETWEEN STA 947 AND STA 967 CORRODED. 2L72 4F RTA16WE 20030910000422003091000042EA 2003 9 10 HEEA088224 220030713A732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6 PT6* 52043EA FREE TURBINE FAILED E HEEAC ABORTED TAKEOFF J WARNING INDICATION CLCLIMB 1 SW0321498 36003 ON LIFT OFF, NR 1 ENGINE GOVERNOR HAD A LOW SIDE FAILURE. REPLACED GOVERNOR. 1G72 4U3 T H4SW E2NE 20031112001132003111200113NM 2003 11 12 DHL2003746013 120031108A5230 STRUCTURE BOEING727 727224 1384076NM MAIN CARGO DOOR CRACKED A DHLAKO NONE OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 FOUND CRACK IN HEAVY STRUCTURE UPPER FORWARD CORNER OF MAIN CARGO DOOR. RII REQUIRED. ALUM 2024-T3, 090, PO21582, FASTENERS USED HL18-6-10 HI LOKS, AND NAS 1103-11 BOLTS. MADE AND INSTALLED REPAIR DOUBLER IAW AERONAUTICAL SOLUTION REPORT 03-0061R. 2L73 4F A3WE 20031103000622003110300062NM 2003 11 3 03FDEA01682 120031002A5720 VENT BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25468FE 21452 LT WING FWD VENT BOX TAB CRACKED AT STA. 656.60. REPAIRED IAW EA 7-5710-55011. 2L73 4F RTA3WE 20031106000692003110600069 2003 11 6 SWAA032299 420031017A2565D31354 SLIDE BOEING737 7377H4 1384404NM ENTRY DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20031105000622003110500062WP 2003 11 5 UPS03841498 120031025A5313975491331N LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:C2 STATION 360 LONG 35L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONGERON BETWEEN STATION 190 TO 390 IAW DWG 9754913 AND SRM 51-1-20D. 2L74 4F RT4A25 20040112000912004011200091NM 2004 1 12 AWXA200301580 120031204A575369737595 STIFFENER BOEING737 73733A 1384673NM T/E FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LOWER LEG OF STIFFENER INSIDE THE NR 3 FLAP TRACK FAIRING, NEAR AFT END OF FAIRING WBL 191. MAINTENANCE REMOVED CRACKED STIFFENER AT WBL 191; FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6 & 7. 2L72 4F RTA16WE 20040109000592004010900059 2004 1 9 AMTA200301424 420031123A2565 SENSOR BOEING757 75723N 1384973NM GIRT BAR DIRTY A AMTAK NONE O OTHER ININSP/MAINT 1 GL11527AT 30886 FOUND DOOR 2L 'SLIDE ARMED' LIGHT INOPERATIVE. CLEANED SENSOR FOR GIRT BAR, CYCLED GIRT BAR NUMEROUS TIMES. SYSTEM OPS CHECK GOOD IAW MM 25-66-11-2. (M) 2L72 4F RTA2NM 20040112000532004011200053SO 2004 1 12 C2XA03CL203 120031218A335020131A BATTERY PACK EMB 135 EMB135ER 3260203SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716510 145251 DURING ROUTINE MAINTENANCE THE SECOND AND THIRD EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040109000542004010900054WP 2004 1 9 GTIA031024 120031123A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND CABIN CENTER FLOORBOARD STATION 1174-1231 HAD DELAMINATED/PUNCTURES 8 AREA. FABRICATED NEW CABIN CENTER FLOORBOARD. (M) 2L72 4F RTA6WE 20040114001112004011400111NM 2004 1 14 DL73S031046 120031123A2612 FIRE DETECTOR BOEING737 737247 138448DNM APU BAY MALFUNCTIONED A DALAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO27376DL24216 23603 000000 PRIOR TO TIME OF DESCENT, APU FIRE WARNING. ACCOMPLISHED EMERGENCY PROCEDURES. BOTTLED DISCHARGED. LIGHT REMAINED ILLUMINATED. INSPECTED APU EXHAUST AND APU COMPARTMENT FOR DAMAGE OR EVIDENCE OF FIRE, NONE FOUND. APU WAS NOT RUNNING AT TIME OF FIRE WARNING. SUSPECT DETECTION SYSTEM FAULT. 2L72 4F A16WE 20040114001322004011400132 2004 1 14 DLM88031064 420031127A31604056510903 DISPLAY DOUG MD88 MD88 3023688NM COCKPIT CONTAMINATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27964DL 49983 DURING APPROACH THE COCKPIT HAD A VERY STRONG ELECTRICAL SMELL AND SLIGHT HAZE IN THE AIR. THE ELEC/BURNING SMELL WAS VERY OVERPOWERING. WENT ONTO OXYGEN, DECLARED AN EMERGENCY AND LANDED. REPLACED F/O NAV DISPLAY. 2L72 4F RTA6WE 20040115000492004011500049NM 2004 1 15 AWXA200301513 120031205A5210 COVER BOEING737 737277 1384570NM PAX DOOR HINGE DAMAGED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28178AW 22645 DURING CLIMB OUT OF OAK EN ROUTE FOR PHX A VERY LOUD SQUEALING SOUND WAS OBSERVED COMING FROM THE L-1 DOOR LOWER FORWARD HINGE SEAL, PRESSURIZATION WAS NORMAL, TURNED BACK TO OAK DUE TO LOUD NOISE. MAINTENANCE FOUND THE LOWER HINGE COVER DAMAGED. REMOVED AND REPLACED L-1 DOOR LOWER FORWARD HINGE COVER IAW BMM 25-21-331, PRESSURIZATION CHECK WAS GOOD, NO LEAKS NOTED. 2L72 4F RTA16WE 20031219000052003121900005 2003 12 19 234TR0013 420031204A2230 TRANSMITTER BOEING737 737228 13844AGNM NR 1 THROTTLE OUT OF ADJUST A PIDAO OTHER O OTHER CRCRUISE 1 SO05234TR 23004 LEFT POWER LAGS FROM IDLE TO POWER IN FLIGHT WITH AUTOTHROTTLES ON. ADJUSTED NR 1 THROTTLE TRANSMITTERS PER MM 22-31-81. OPS CHECKS GOOD ON GROUND RUN. 2L72 4F RTA16WE 20031222001312003122200131NM 2003 12 22 AMTA200301406 120031120A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11520AT 27976 EGRESS LIGHTS INOPERATIVE FROM ROW 35 AFT. FOUND WIRE LOOSE UNDER PLASTIC COVER AT ROW 35. RECONNECTED PER MM 33-51-11. OPS CHECK NORMAL. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20031222000012003122200001WP 2003 12 22 ARWA20032101 120031206A2761 SPOILER LKHEED1011 1011385115 5265015WP NR 2 MALFUNCTIONED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19307GB 193U1131 AFTER LANDING FOUND NR 4 SPOILER STILL UP ON RIGHT WING, NR 2 SPOILER FLOATING AND WILL NOT REACT TO INPUTS ON RIGHT WING AND THE RIGHT WING MOVES VERY SLOWLY. 2L73 4F A23WE 20031223001002003122300100SO 2003 12 23 SWIA200312653 120031208A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO FLAPS FAILED A SWIAO OTHER KF FLUID LOSS FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07561SW8609 8609 120335 ON TAXI OUT HAD LOSS OF HYDRAULIC PRESSURE ON BLUE SYSTEM. RETURNED TO GATE. REPLACED RIGHT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00 AND RII 27-307. OPS AND LEAK CHECKS GOOD. 2L72 4T RTA31SO 20031231000542003123100054WP 2003 12 31 GTIA030910 120031105A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FS CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 PASSENGER CABIN LT IB SEAT TRACKS FS 237 THROUGH 826 HAVE BARE METAL, GOUGES, AND LIGHT CORROSION. FS 288 LT IB SEAT TRACK MATERIAL LOSS NOT WITHIN LIMITS. REMOVED SEAT TRACK SECTION STATION 266-304. FABRICATED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK SECTION. (M) 2L72 4F RTA6WE 20031125000862003112500086WP 2003 11 25 DHL2003805541 120030729A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH78174 46125 RIGHT WING CTR L/R FORMER 1.000 CRACKED, STA XFS 304.000 (LWR SECTION). PERFORMED STOP HOLE ON CRACK END (0.250) IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20031203001272003120300127EA 2003 12 3 A6WA200340155 120031030A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31457AW 7854 AIRCRAFT HAS PETROLEUM ODOR. ACCOMPLISHED PACK BURN. COULD NOT DETECT ANY ODORS AT THIS TIME. (M) 2L72 4F RTA21EA 20040122000052004012200005EA 2004 1 22 SWIA200312725 120031224A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSLAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 FS 280 RT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11 AND RII 53-401. 2L72 4F RTA21EA 20040121000912004012100091EA 2004 1 21 A6WA200340191 120031212A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 REINFORCEMENT ANGLES, P/N 601-36001-29/30 FOUND CRACKED. REINFORCEMENT ANGLES, P/N 601-36001-29/30. REPLACED DURING INCORPORATION OF SERVICE BULLETING 601R-53-061. (M) 2L72 4F RTA21EA 20040123000152004012300015 2004 1 23 ASAA0380701 420031031A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01961AS 53075 PDX PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20031209001312003120900131NM 2003 12 9 QXEA200301344 120031014A5753 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 CHAFING TOP INBOARD OF THE OUTBOARD FLAP ON LEFTHAND WING. REPAIRED IAW RD 8-57-1734. 2H72 4T RTA13NM 20030918000092003091800009NM 2003 9 18 03FDEA01508 120030911A5320 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25221FE 20932 CRACK IN STRINGER CLIP AT BS 720B, STRINGER 7 RT. REMOVED AND REPLACED CRACKED STRINGER CLIP AT BS 720B, STRINGER 7 RT. 2L73 4F RTA3WE 20030919000792003091900079NM 2003 9 19 03FDEA01251 120030810A2613 OVERHEAT LOOP BOEING727 7272S2F 1384O81NM FUSELAGE CHAFED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25208FE 22930 DURING CRUISE FLIGHT AT FL 330 MACH .82, THE LOWER AFT BODY OVERHEAT LIGHT STARTED TO LIGHTLY FLICKER INTERMITTENTLY. LIGHT RARELY FLICKERED ON AND WAS MOSTLY COMPLETLEY OUT. SUSPECTED A SHORT IN THE IND SYSTEM. FURTHER DOWN LINE THE WARNING LIGHT FLICKERED MORE OFTEN AND WAS CLOSE TO FULL BRIGHTNESS. FOLLOWED RED TAB PROCEDURES WITH ALL THREE THROTTLES AT IDLE AND ALL BLEEDS OFF. LIGHT WOULD NOT EXTINGUISH. ENGINE OR WING ANTI-ICE NEVER USED. STRUT AND AFT BODY OVERHEAT TESTS NORMAL. VISUALLY INSPECTED VENTRAL STAIR AREA FOR DUCT LEAKS, NONE NOTED. FOUND DETECTION LOOP CHAFING ALONG ROUTING BETWEEN FRAME STA'S 1240 TO 1303 LEFT HAND SIDE, MOVED ELEMENT AWAY FROM STRUCTURE. 2L73 4F A3WE 20030919001392003091900139EU 2003 9 19 164771 120030815A7997 WIRE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE OIL PRESS TRANDUSHORTED A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17148SD 340A148 462 DGR186989 CLIMBING AT AT 9K FT. WHEN THE LT ENGINE OIL PRESS. WARNING LIGHT ILLUMINATED. THE CREW NOTICED THAT THE LH PROP OIL PRESSURE WAS AT ZERO. THE CREW REDUCED POWER TO THE LT ENGINE AND RETURNED TO PIT. A/C REMOVED FROM SERVICE AT 2230 HDQ TIME. PIT MX T/S LT ENGINE OIL PRESS SYSTEM, FOUND AND REPAIRED A SHORT IN THE LT PROP OIL PRESS TRANDUCER CONNECTION. A/C WAS GROUND RUN AND RETURNED TO SERVICE 8-16-03 @1030 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20030922001112003092200111CE 2003 9 22 DXTA200300085 120030813A3230 SWITCH CESSNA650 650 2076802CE NOSE CENTERING OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07787QS 6507087 LANDING GEAR WOULD NOT RETRACT ON CLIMB OUT, AFTER TRYING TO RETRACT THE GEAR SEVERAL TIMES, THE GEAR DID RETRACT. FOUND NOSE GEAR CENTERING SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND RAN GEAR SEVERAL TIMES, OPS CHECK GOOD ALL WORK DONE IAW CESSNA 650 MM CHAPTER 32-60-00. 2L72 4F A9NM 20030923000812003092300081WP 2003 9 23 DHL2003604717 120030608A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL89636 46047 FUSELAGE NOSE SECTION SKIN CRACKED 1.125, STA 12.000 L-27R AT STRUCTURAL MODIFICATION. PERFORMED MAJOR REPAIR IAW EODHL-030549, ED3384. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END USING A 0.250 DIA DRILL IAW EODHL-030549, ED-3384. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (2024-T3 AL0.071) IAW EODHL-030549, ED-3384. CLEANED, TREATED AND PRIMED DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON FUSELAGE NOSE SECTION SKIN, STA 12.00 L-27R USING NEW FASTENERS IAW EODHL-030549, ED-3384, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030923001602003092300160NM 2003 9 23 AALA20030859 120030815A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21392AN 29429 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 20040128000182004012800018NM 2004 1 28 FDE2004F00001 120031215A5753ARC74901 FITTING DOUG MD11 MD11 3023602NM ZONE 600 OUT OF LIMITS A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RIGHT WING INBD FLAP VANE INBD ATTACHMENT T-FITTING , 2 EA HOLE BORE SIZE EXCEED LIMIT. RIGHT WING - INBD FLAP VANE INBD ATTACHMENT T-FITTING REMOVED AND INSTALLED NEW FITTING AS PER AMM 27-50-22. 2L73 4F RTA22WE 20040128000682004012800068SO 2004 1 28 C2XA03SH517 120031230A532014521275013 SILL EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040205000042004020500004NM 2004 2 5 P5CA0300985 120031113A7600 SENSE LINE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 3 ENGINE LOOSE A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23496MC 29257 704916 START FAILURE NR 3 ENGINE - RETURN TO BLOCKS. INSPECTED NR 3 ENGINE, FOUND CDP SENSE LINE AT EEC LOOSE. CLEANED AND PROPERLY SECURED CDP LINE. ENGINE RUN ACCOMPLISHED WITH ALL PARAMETERS NORMAL. 2L74 4F4 FRT1384945 E23EA 20040205000792004020500079EA 2004 2 5 ASOA03651 120031215A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11856AS 7404 FLT 4807 - DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205001112004020500111SO 2004 2 5 BSY2003F00025 120031021A3260 DOWNLOCK PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL MLG LACK OF LUBE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL07525AA 318052111 RL750161A OJ10249A RT GEAR NO DOWN AND LOCK LIGHT. CLEANED AND LUBED RT GEAR DOWN AND LOCK MECHANISM, JACK AIRCRAFT, SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. 1L72 3O3 O A20SO E14EA 5 CP33EA 20040210000332004021000033WP 2004 2 10 UPS03841610 120031021A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE: C3, AFT ACCESSORY COMP DOUBLER AROUND OUTFLOW VALVE CORRODED AT FWD CORNER. REMOVED EXISTING EXT DBLR AT FS 1620 L32R IAW DC8 SRM 51-1-20D. CUTOUT CORRODED INNER DBLR AND SKIN , FABBED REPAIR DOUBLER, FILLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7 AND REO G09567 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER, FILLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7 AND REO G09567. 2L74 4F RT4A25 20031212000072003121200007NM 2003 12 12 SWAA032475 120031107A3350BR2013 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C2 CHECK, FOUND EEPLS RED LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F A16WE 20031215000912003121500091EA 2003 12 15 SWIA200312591 120031105A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07910SW 7566 AFTER DEPARTURE, MACH TRIM AND STAB TRIM CAUTION MESSAGES APPEARED. FOLLOWED QRH PROCEDURE, MESSAGES STILL APPEARED. RETURNED TO AIRPORT. REMOVED AND REPLACED CAPTAIN TRIM DISCONNECT SWITCH. OPS CHECK GOOD. 2L72 4F RTA21EA 20040308001302004030800130NM 2004 3 8 ASAA0380690 120031024A335060030451 CONNECTOR DOUG MD80 MD83 3023681NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01981AS 53472 PDX PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FLASH INTERMITTENTLY IN 1ST CLASS CABIN. SECURED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20031217000392003121700039WP 2003 12 17 DHL2003807500 120031009A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH84293 45990 NOSE SECTION FUSELAGE - EXTERNAL SKIN CRACKED 0.750 AT STA 53.000, L-29L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13. REMOVED DOUBLER AND FASTENERS IAW SRM 51-3-0 PG 1, SRM 51-1-20D PG 21. TRIMMED OUT CRACKED AREA IAW SRM 53-2-0 FIG 13 (SHEET 1). FABRICATED DOUBLER (2024-T3AL 0.071) AND FILLERS (2024-T3AL 0.050) IAW SRM 53-2-0 FIG 13 (SHEET 1, 5, 6). CLEANED, TREATED AND PRIMED FILLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLERS AND DOUBLER WITH NEW FASTENERS IAW SRM 53-2-0 FIG 13 (SHEET 1, 5 ,6) SRM 51-1-20D PG 9. 2L74 4F RT4A25 20030926000912003092600091NE 2003 9 26 03FDEA01395 220030827A7261 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE NR 1 LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25481FE 21463 709284 AT FL 330 NR 1 OIL QTY WENT RAPIDLY TO ZERO. OIL PRESS DROPPED TO 30 PSI. ENGINE SHUTDOWN IAW RED TABS. REMOVED AND REPLACED NR 1 ENG ASSY AS PER WORK CARD 70T0001-01, A/C OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20070406001742007040600174NM 2007 4 6 AT0700022 120030930A5311 FRAME BOEING717 717200 1383700NM FUESLAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15949AT 55003 RIGHT HAND FUSELAGE FRAME DAMAGED AT STA 47.875. REPLACED FUSELAGE FRAME AT STA 47.87 PER DWG 9911501 AND B717 SRM 51-41-01 (RT SIDE). 2L72 4F TRA6WE